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英汉对照民用航空词典 [复制链接]

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发表于 2008-12-24 21:35:01 |只看该作者 |正序浏览
英汉对照% {+ E+ q) b: Q* @ 民用航空词典+ j; _% s% J0 u; {) o6 ^3 B 波音商用飞机集团, O4 [1 Y# ]$ S0 q$ `9 D( M% q# M+ [ BOEING COMMERCIAL AIRPLANE GROUP , b5 ]6 [4 ^$ ]/ m& c9 r英汉对照民用航空词典B OEING+ a0 `% ^! R7 x& w TECHNICAL DICTIONARY 1 * I0 |8 i! N5 I! n) n5 X, I9 j6 DA6 ] D+ X. n4 j% R [. o& _3 @( Q5 Y4 @ ABEAM (ABM), Beside: An aircraft is abeam a station! ^3 Z) @( p+ ] when that station is 90° to the right or left of the track of }1 g4 s; E# \" ^the aircraft.9 y/ u* W& x0 O ABSOLUTE ALTITUDE, The actual distance the aircraft( o( y3 U' ~4 t n) E is above the ground.4 M% h4 h ^" M. Z6 H9 T3 g; w# @ ABSOLUTE PRESSURE, Pressure of a liquid or gas % d! j* Z7 {% emeasured relative to a vacuum. 0 Q" r8 O0 h( Y. y- M; {' ^" tACARS, SEE - AIRCRAFT (OR ARINC) REPORTING5 r5 h% _, b4 l9 a ADDRESSING AND COMMUNICATION SYSTEM/ t8 V- m! y; G1 M. B ACCELERATION, The rate of change in velocity with 7 R: M0 H; {7 |5 e$ `) H2 F- {respect to time. 9 A ?% B, s. J$ {# [) dACCESSORY GEARBOX, A part of the engine, 0 L, n# P. j. N( \% W7 r# X9 v; ?! Wmechanically driven by a compressor or an angle: o( i: F$ ?6 z1 ` gearbox, for driving components necessary for engine + X6 g' K; c ]' u8 B: n9 F; A正切,/ f4 C) w- Z! ^- l0 L l! v and airplane operations. ( O( [6 v, B) j当电台在飞机左侧或右侧方与航迹成90 度时,飞机正3 |9 K( h& j- [% { 切电台。4 @" b- S( o' T& T( _, i 绝对高度,8 i% @( {( I) j 飞机离地面的实际距离。) c m- k" S0 R, O 绝对压力,+ l- O$ R# d4 X, n/ a& E 相对于真空(无压力)测得的液体或气体的压力。 9 s5 d8 E- v: ?+ e( ]& I& N9 E飞机通信寻址和报告系统,$ K X$ w5 ?4 ?. D7 ^ 见Aircraft(or ARINC)Reporting Addressing and 8 |& d# M0 N4 p1 {8 L- ^1 A d& ]Communication System.0 D) u; D$ v9 P/ I 加速度,3 W! j" i$ x9 h1 ^( S6 o8 o0 @ 随时间变化的速度改变率。" i1 h6 O) \+ A3 S 附件齿轮箱, 1 j5 U* v x' K( t0 M0 {& ^4 B' j4 w发动机的一部份,由压气机或伞齿轮箱带动,用来驱动6 B5 w2 I; K' p. B, W5 A 一些使发动机和飞机工作的部件" }9 Y; @: U: x6 {5 F, s; s K 英汉对照民用航空词典B OEING 6 t7 ^ B2 C& w9 fTECHNICAL DICTIONARY 2$ m( G0 a# o) ~* Z& i% W9 ~ ACCUMULATOR (NO. 1), A container with hydraulic) {, e/ `# B" l ts when normal hydraulic supply is not+ H& t" V% s- `! g3 a I vailable./ A5 R5 v7 Q4 W3 N9 n4 i CCUMULATOR (NO. 2), In a computer, a special3 j5 y7 S( W5 t5 _3 ` torage register associated with the arithmetic logic unit,6 `( Q0 f2 I% X. C8 B olding the results of a computation or data( `( q- E/ {! Q M; }+ i ACTUATOR, A mechanical device operated electrically,0 x- o! r/ b; o hydraulically, pneumatically or mechanically for' q% B5 ^; v- b transmitting motion between components. / }) c/ y. ~% G' P( j& f: v! bADC, SEE - AIR DATA COMPUTER. N2 }, y$ H1 Q) x' O4 k& S8 v& e5 } ADF, SEE - AUTOMATIC DIRECTION FINDER J+ _' i1 T" D6 PADI, Attitude Direction Indicator, An electronic display of, K8 ? F) \8 J0 x, S w1 p5 d( Y8 D$ `0 E airplane attitude information in pitch and roll. 8 {3 j2 u) ^. n" P- J蓄压器(NO.1), $ j! { y; | q+ i5 ~ E含有靠干燥空气或氮气增压的液压油的容器。当没有正( v! w+ L& m( Q 常的液压源可用时,该容器可用以驱动部件。 2 R2 O) L8 \2 M# Y) j) Q, D存储器(NO.2), ' q! p: r$ g& F8 X2 h: O计算机中,一种与算术逻辑组件有关系的特别存储寄存! r( \8 E8 w4 q! i 器,用来存放运算结果或数据传输。# ?* \9 W% f0 y. F+ \ 飞机状态监控系统, 1 v: o" r2 N4 q: @! \见Aircraft Condition Monitoring System& O% G, W1 D' X9 A fluid pressurized by dry air or nitrogen for operation of 6 _: m! `- x+ r- D0 e! icomponen S+ ?: X& x" }" ^a. j! z4 H# d# @% R# L5 |" R1 Y A9 e% a# K# m0 \0 R s k! {9 [2 k wused for h! Z/ M2 V g9 r! o transfer.* ]2 e; i+ t6 z, N j ACMS, SEE - AIRCRAFT CONDITION MONITORING' y2 ]1 f# A+ Q3 i4 x. j- k5 R SYSTEM . $ y; I& E! j2 Y( T$ S5 ^1 N4 f9 w作动筒,8 b [9 ~' i C. ^+ N! v% ^ 由电,液压,气源或机械驱动的机械装置,用于传送部 ) x( m K4 a$ N! ]" z/ s件之间的运动。 / E% w" C @9 z W3 X大气数据计算机,7 [( d, U0 X8 G9 a: x 见Air Data Computer. : t4 C* h: |3 J# m$ F自动定向仪,0 S! k% l9 {$ m0 g1 B6 Q 见Automatic Direction Finder.' i; i; ~' W0 k& v9 d. n) t 姿态指引仪, 7 q o4 D* D6 Y* b2 o' w3 v用来显示飞机的俯仰姿态和坡度的电子显示。 9 V7 l3 V3 ^, }, w) Z# R! N+ L英汉对照民用航空词典B OEING - c# ~3 X2 ~1 \0 |5 r, f8 t% \TECHNICAL DICTIONARY 3 3 }( j8 F H, O# Z+ |/ c; z; pAERONAUTICAL RADIO INCORPORATED, ARINC is + f; [3 [7 I" d. h4 Q, 1 [9 ` L1 ]& U# ]- K7 r, V ^3 d/ Snufacturers, and foreign flag airlines. ARINC , b( p0 z/ P; l# hevelops and publishes standards for electronic ( `2 i$ M5 J' C* s4 Rquipment and systems. - O# A7 {% t# ^5 {GILITY TUNING, The capability of the DME to6 a* X2 D6 \9 G4 }1 t lternately tune between two different DME stations in6 |$ E! T" w/ [; P5 q rder to get two distance readings from one _ I3 ~5 D8 \$ w, i+ R8 Q* `terrogator. ! h& P$ _; C5 a# _# }ge 7 W4 C% U# k! D& H; G; MILERON FORCE LIMITER, An electro-mechanical& r# n# u [5 a! r9 W* e' W) z IR CLEANER, A component in the pneumatic system8 V* \7 v' x2 l& N# E upply to the air ( N# _6 V* v- T. ?+ Q- sonditioning system.: m2 T @' D1 g3 Z3 t" M 订并出版 , B+ H9 _5 b3 u* o' w子设备和系统的规范。4 F$ f( f$ l) Q' n 快速调谐,* N2 M4 w9 s( g% n1 i* G9 h" l6 h8 W 机载DME通过交替调谐两部地面DME电台以测得来自% F8 [0 ~8 ^: R1 w! L 同一台询问机的两个距离数据的能力。0 X L# i, a O4 b, k5 m 翼操纵力限制器, 6 R! @, X4 w# y" Y7 e+ e装置。在自动驾驶工作期间,用来限制驾驶盘9 b9 {4 |# ?: D1 w 气清洁器,+ v; n2 E/ D3 S' i! l" ?8 F) [ 部件。用于去除供空调系统使用的发7 ~' W( r( Y, v8 h4 ~% G* R a corporation whose principal stockholders are United. \7 _% q8 M9 x States scheduled airlines, air transport companies ; P4 B) j" f9 _aircraft ma * c0 C* X* }: X+ N' t; t; Ad. O5 f+ H, O0 ~& n1 T1 h) v5 O0 }" j e : k* U$ D7 J' N' H" C) v2 d) b* nA * \! I4 p# H6 s& {a7 M) X8 r% [: C" r9 v o( l _* M! _: V* Z) y+ I; b5 H1 u. u in ' Q' h) j( z/ y7 ~, z: y) vAILERON, A hinged moveable part on the trailing ed : X7 ]9 L4 h$ A( D1 K, v& x, ^# Q$ Nof each wing for airplane roll (wing up and wing down) . S7 a& G6 g: }& h/ k) ~control.1 `/ a3 X# V4 ~3 X v' v$ d A . m% F: D ?) V( Z8 [; Fdevice for limiting the control wheel movement by the # ?- p( ^3 T$ ]3 O* L4 K% U3 {autopilot during autopilot operation. 5 C( P5 o8 \* \- x" B+ N& [A; l) `$ h( C' h# r for removing dirt from the engine air s1 C0 ^: ?3 s& V% I- M, ~ E c) @# Z$ Z1 O* o2 `0 C% Y& O 航空无线电公司, % L3 g4 } S6 s. `6 N1 O: [主要股东为美国定期的航空公司、航空运输公司、飞机* k( D) E8 y5 z" ^) [; E 制造厂和外国领队航空公司的组织。其目的是制 $ c, f$ Z0 d `2 n& F; i7 K6 O3 e" k% r3 c Y副翼,, ^9 s2 z k- A- M8 S$ H2 A 铰连在每个机翼后缘的可动部件,用于控制飞机的滚转( u. T& T8 }3 G5 i8 E (机翼向上和向下)。 % D# E+ T: X$ v$ k- Z# F3 d) @$ W一种机电 6 G n5 n9 s; \/ `的动作量。7 q' s7 b$ @$ @+ U$ u7 k) e. C) n: X0 \7 U气源系统里的一个: r$ \: Z5 G3 ^! t: N, T8 B u 动机引气中的灰尘。* r: l8 F; N, O 英汉对照民用航空词典B OEING ! {. A/ D# `% g' _TECHNICAL DICTIONARY 43 Y: A; L6 Y: Z8 m0 O/ |1 R* P AIRPORT ELEVATION/FIELD ELEVATION, The * H/ l4 z# b- I! |8 j8 Phighest point of an airport's usable runways measured & V8 R y, [/ [% S- gin feet from mean sea level. In a few countries, the) K" L4 n8 B9 `+ F0 I airport elevation is determined at the airport reference1 c5 x1 }) g$ ^* F6 Y! G0 A point. 6 ?! v+ Y9 [/ \) G' x' \$ n7 u! ?3 lAIR ROUTE TRAFFIC CONTROL CENTER (ARTCC), ' g0 ^$ ]! t% w9 N8 k5 Q7 ~* C7 j' pervice ! {' p6 Q" r8 O3 f- Oase of5 Y) C% g8 Y* {6 F us flow of air traffic.) Z) A! V& n( W IR CYCLE MACHINE, A compressor and turbine on a 8 n, m8 } C/ o3 v A3 ~( ~3 lommon shaft for cooling the air in an air conditioning1 w' M! v9 V0 Z. L/ j. e; G. H8 p ystem. The air is cooled by expansion from high to low 8 \, g! ]8 u+ g7 v, F# P' oressure across the turbine. The compressor is driven- m- U3 b) l0 ^" a" ] y the turbine. i- j( J9 q" h3 n 中航路交通管制中心(ARTCC), % ^! u( d' I; {4 Z2 j域范围内使用仪表飞行规则飞行的飞机提 4 t; L; A+ `4 |7 b; p% m: u; n管制(ATC), . f6 ~9 O/ Q, n0 X4 o涡轮冷却器,/ @9 P) f3 E5 b# a5 s 是装在同一的压气机和涡轮,用于冷却空调系 ' }% N( p1 N7 S统中的空气。气经压气机压缩后,由热交换器移去热量,# X' ~4 B: X8 _* i" n) y5 s 然后经过涡轮令涡轮带动压气机。通过涡轮之空气,温: L9 Z- ~# t2 v) n6 f 度下降。' g4 v/ R) W: c, r, c A facility established to provide air traffic control s7 G1 a- K5 d8 ` to aircraft operating on IFR flight plans within controlled4 b( @2 e" @! t u$ y3 k airspace and principally during the enroute ph! m& D( f: K7 ~ x! q8 G9 Y/ F flight.1 G. C1 [+ G* S! c AIR TRAFFIC CONTROL (ATC), A service operated by6 h+ s, r4 V9 E5 H appropriate authority to promote the safe, orderly and - I- I ?9 V5 b5 V5 Z) `! sexpeditio: X; t5 |; T8 A" c1 T A; S- X, v; E' d4 u4 k' c c . I( i: g# N- @6 rs 0 C, `7 ], s* b8 W* _% {p $ p5 y$ `6 Y* k: tb ]0 W$ W! b& _/ @; o 机场标高, c; M8 t) r* [2 s0 C, B- L' s6 R3 U 指海平面与机场可用跑道最高点之间的距离,单位是英 ) [! u3 O: n- R* K% n尺。有几个国家的机场标高是由机场基准点而决定的。 . x0 e' J, ^) l% H' f& a8 \' q- M3 u& h A2 e7 M 给在控制空/ o+ l6 w/ y4 y3 q* h+ R 供空中交通管制服务的站台。$ o$ Z O3 T& A) x3 ? 空中交通 9 o1 o1 F# v7 T由有关当局管理,旨在促进安全,秩序,和效率的空中- x5 D' Q5 q/ i# G 交通服务。" s) D8 i" Y l. [( q+ P+ m( k 根转轴上 ], q# _8 Y0 k- X$ I" s8 P2 S* D) N( D9 |4 `/ h N1 ^* [: e9 P0 j8 j% c英汉对照民用航空词典B OEING * g2 }, X) |3 p6 @3 S; xTECHNICAL DICTIONARY 5

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发表于 2008-12-24 21:47:03 |只看该作者
airspace of defined dimensions within which Flight 6 i% X) `1 h4 h/ J" G8 J3 HInformation Service and Alerting Service are provided. . ?2 U$ L) l& V6 O) ^4 uF ) h* V9 d9 M0 \9 f3 M$ Dd0 {; @5 h6 n+ W( k F r& M$ q( x1 J/ W in! d8 G$ L1 m+ t% F& H a . x0 b8 ^, G" y6 eF% t8 ]! R: r! \9 K& ~ s b2 a( _& f) Y! l s. V" X( D1 H1 p% z! X0 l 飞行指引仪自动显示(FDS), " B4 C2 e' m/ ], c. P/ c- z* ^( z当飞行指引仪的开关处于关断的位置时,自动显示的飞2 e( }% @( d z/ e 行指令。 / i X9 m0 C" S- G, h飞航情报区(FIR,UIR), * c6 [$ _$ ?; I3 ]一个有飞行资料服务和警告服务的范围6 C; N- Z. [* j3 }( w7 { 度层。 4 F9 @, I8 Z! }$ ?" B' h9 o) f8 ^50表示 / `" r0 S/ B) n显示自动飞 ! Y Q# g6 y5 K* J英汉对照民用航空词典B OEING 6 h- G0 u" b2 Q, f YTECHNICAL DICTIONARY 64% p, Z9 t" |/ j; [ FLIGHT SPOILER, See Spoiler. . C/ H& ]2 |# p- q4 @: F- aLOAT SWITCH, An electrical switch which opens or( r- }2 ]2 I }* X" m4 i( d8 E loses an electrical circuit depending on fluid quantity in5 T$ z2 K9 o9 }: Y$ h3 [ e reservoir. 4 B: D* v! [* W+ k6 fLIGHT TRAINING DEVICE: Any device having a full* f0 E- F- F7 L: L3 V! A8 B cale replace of instruments, flight deck area or an) x' f8 E3 H0 x nclosed airplane cockpit includes the equipment and+ G* r( k7 @! c1 A rograms necessary to represent the airplane in ground' c) U) w! V$ Y) x nd flight conditions. 5 t+ Y! V% M* S5 z* C7 R; j" dLOAT VALVE, A valve in a fluid reservoir which opens 3 U( V& ^+ ]/ ]# [4 x4 D1 m' and closes an inlet or outlet depending on fluid level. 7 @' o, a+ _- s" Z% c' ?LOWMETER, An electrical transmitter for measuring , E3 C( `4 Y4 e. U4 vthe engine.9 ~0 K; ?1 w: x; x9 W# I3 n LUORESCENT LIGHT, A light emitted by a gas filled/ r" j( V( n+ D4 y9 P# H i" r- E 飞行扰流板, ) L0 n' r: L. d9 q/ [见Spoiler. * k5 H2 ~# Y, k浮子电门," M& U% f5 j* ^3 V* J' e' _ ^ 根据贮液箱内液体的量来接通或断开电路的一种电器 ' b, H Y e, k% ^% }; M开关。 m3 L0 x) f; P4 }7 z$ p$ T 飞行培训设备,7 d* o/ Q- [. ~3 s+ z i 仿仪表、驾驶舱区、或封闭驾驶舱的任何设施仿真装置。 + A: D E* Y8 s$ I4 C1 k" X9 R# u包括可体现飞机地面和空中状态的设备和程序。 8 F7 @ h4 p' ^ O3 ~' T1 }& O浮子活门,! X! k3 R$ n: A4 }; v4 ]1 Y6 a 装在贮液箱内,根据液面的高低来开启和关闭进口或出3 J* X5 } m2 d1 @% C& L) m 口的活门。 6 X$ F4 R% E2 T9 u流量表, 1 T) T2 r6 f/ a' ]5 e用来量度流向发动机的燃油流率的电传感器。8 G) \ M" y, X3 a 萤光, ?* o1 h F: x8 m) g% [由一种特制的充气管所发出的光。7 _2 P0 |; `1 f% ^ F+ Q2 W T( G, l0 h c - f+ j1 N' z/ H7 v( }6 O pth- t7 O2 c0 K4 }% i B F + y& E |. T5 ?8 P. O- `s; V9 i8 E) T: p2 g8 e- F2 H e 1 t/ e" D. O6 A" [9 @8 Qp1 f+ |' R A, s' |) T a7 K7 c$ a* F+ n* k F+ i# D; p# q$ Y3 i+ I a ' w6 C! i4 |2 } z0 ]' I5 v8 EF $ n" N |9 T0 l* x; w( I1 Hthe fuel flow to " v4 L4 b; L3 \. `F; @0 B" B6 l, d tube.5 P6 U- h6 U) W6 b4 q) [ 英汉对照民用航空词典B OEING 1 Y0 `( ~9 [" G& B1 j" HTECHNICAL DICTIONARY 65 " ~9 Q8 Y: b7 zFMC, SEE - FLIGHT MANAGEMENT COMPUTER ( y9 d0 P* z/ e# T9 OFOD, SEE - FOREIGN OBJECT DAMAGE 6 U; @# W$ g B6 vORCE BALANCE VALVE, A valve controlled by the8 o% o; h9 V/ J+ }& f& n OREIGN, Offside; opposite side. + h, u0 |) }. _8 _: B b' HOREIGN OBJECT DAMAGE, Internal engine damage& r4 ~3 h1 d+ G/ @: B ue to objects entering the engine air inlet.6 G. P; I6 {/ K5 P) C RM, SEE - FAULT REPORTING MANUAL % O) m- c3 |7 g1 j9 {UEL CONSERVATION, The activity of planning flight! c" a0 N; k" E2 U ltitudes and cruise speeds so as to minimize fuel. Q) k" Q( R8 m3 P2 q( ^ onsumption. ' Q$ V7 S, L n' `/ F2 x9 y; m4 I" M" FUEL CONTROL UNIT (FCU), A component on the 2 }* M Z, Y9 W9 Z2 Y' d& qngine for controlling fuel flow for starting and engine ; r6 Y0 M% Z$ z7 r$ ]& CF, l+ y. B, N* x. O feel computer in the elevator system for hydraulic " u, c \3 ^; b! n1 C2 r& opressure supply to the elevator actuator.3 w# h8 K% i' f8 q- U( c F 5 K8 F( @$ q" _9 D2 oF, o* ^5 g& h" o x @7 f d 2 ?# q9 m7 q. h" k" A' z7 t1 UF 0 ~ k5 N! p7 s4 V3 d6 F3 G& z% n% qF & x3 G: o# i4 p* z2 ta 3 I, _8 e0 c, e& V. w- d- o9 Jc( f- L7 |- m& t% Y# j+ @ F ! g7 Y& J# R" s/ p1 G8 s5 xe , J4 k& {% s3 Eoperation.2 Y& f) P* d2 p1 y( P 飞行管理计算机, 1 g% f' y. M- Q: G2 u见Flight Management Computer. 3 h! O3 {. i1 ?* R外来物损坏,5 u" F! \. a0 g eign Object Damage/ Z: {, q% Q5 Q6 U( H# u* P5 ~ 见For . . d- \3 W, @: i1 l6 h( ]平衡活门, " \3 d" {( C3 M6 D. [, U内的感觉计算机控制的活门,用来向升降 G% L. N) _/ e) l 外面的, 2 F1 i2 n3 ^2 ~0 p% p8 W8 b" U另一边的,对面的。 " v g. Z& L( Z/ A2 e2 r; j d" G3 p, i外来物损坏,* T7 s4 S. y" v0 D4 l h$ \( T( x 由进人发动机进气口的物体所引起的发动机内部。# x+ q2 V4 K+ N2 \ 故障报告手册, : e+ r" j$ q+ F# O, _5 W7 }见Fault Reporting Manual+ W. L# h8 K" h7 T5 A; ~# Y4 F W5 [8 j9 m/ t由升降舵系统" Q2 X% ~$ |2 n# P5 ~) I' ] 舵舵机提供液压力。0 A* y! z( O! G1 {5 Y. ^ 损坏 ) P. ]$ l: }& ]/ E5 @, ^1 K0 ?6 S2 J4 h! i* q, u7 w- _约燃油,$ q( [- [* r4 `; [. f) w$ ` 为使燃油消耗最少而对飞行高度和巡航速度的计划。8 j. o" `1 _7 ^. I1 B% }4 _ 油控制装置(FCU)," i2 ^) W0 q* X# A3 ~3 g8 f9 M4 e 发动机上的一个部件。在发动机起动和运转时控制燃油) L2 D0 H( S' X( M$ Q$ l0 a/ b7 J- T- n/ H' G3 @/ C: c1 X4 ~$ @! O1 Z4 R, U 流量。4 k7 T7 t4 e: _ 英汉对照民用航空词典B OEING' m0 Z( v# ^0 R: v4 K TECHNICAL DICTIONARY 66! b: R+ S& w! \+ @7 X& j4 }# W FUEL FLOW, The rate at which an engine consumes. G" K$ R) ^) ^- Y4 C0 Q8 q( k UEL HEATER, A component on the engine for heating : {' O+ N( \! o% w3 iUEL JETTISON SYSTEM, A method for reducing 4 X. A6 |6 D& Be 0 G% \! F+ C+ a1 c2 L, ]4 jULL FLIGHT SIMULATION (FFS): A flight training , Q- t2 I: p1 |1 o% sevice that incorporates full visual and motion systems8 k, P' w6 e+ K" f+ i2 l nd specific model airplane. 0 u9 D" h' y1 L6 I* {) {ULL-WAVE RECTIFIER, An electronic circuit which 1 M3 U7 W* Y- @6 ?hanges an alternating current signal into a pulsating 0 {* g) q% M! f2 O8 S6 Hirect current signal.2 s n6 x* {' b) m or& E- J( ~1 L( l AGE PRESSURE, Pressure measured in pounds per. p3 m0 K) ?8 f GALVANIC CORROSION, A form of corrosion caused . k p% S# L2 g8 }9 k7 b! |7 y7 y8 `by the contact of dissimilar metals.5 y3 E' e, ]. ~8 M4 @: {( ^ 油加温器,8 S9 N1 I1 t, f( L6 O8 G+ O 热燃油以防止发动机燃油' W% n6 ~5 w! ]( Y 急放燃油系统,' o8 ]- `- C5 R 中的燃油向外排放以减轻飞机重量的8 Y- K' q _- s# g: g* O 动飞行模拟机(FFS), ! P5 y- P; @. m* h0 S2 ?1 {一种飞行训练器。它综合了完整的视景和运动系统,以6 M, u; B. [( X$ X U* j1 ]" f 具体的机型。 ( \$ l ^" }( \/ r3 I# ?波整流器, 9 h. P# U6 |1 d1 ~用来将交流电信号变成脉冲直流电信号的电路。# j5 a; R+ F4 n/ R$ ^3 h6 S 压, , Y% K- ~4 d/ S8 j: @8 G/ J平方英寸若干磅(psig)磅/平方英寸的计6 _* H z7 p* _2 [/ k- U 电解腐蚀,0 h' o5 ?; E/ F" s8 `! ]0 D 一种由于不同种金属的接触所产生的腐蚀。 & ]. e! h1 ?2 ofuel measured in units of weight per hour.% a3 L9 I( u- `( U' G3 m2 I F 8 e6 Q) v2 R$ j2 I- W# ]fuel to prevent icing conditions in the engine fuel / d4 W+ H. a! T! [- xsystem. 4 g G! Y; V# y7 mF9 `9 c6 d6 ^* O( x9 g( s# y airplane weight by discharging fuel from the tanks to th ! }1 D( i% n8 m% r) q3 }' ?outside. ' z) R `& J" }6 d' KF " }3 y) w7 R0 f7 W2 n' ed 0 k! m/ G9 C5 U' E" na , Y8 N2 @7 [/ S. h5 m# }/ FF% ?# Y7 X6 j4 m f; B2 ] c $ c3 r% o" n8 ^7 |d0 ~: p9 Q7 f) G9 y G l D4 `) G: |% ?0 [0 g: aGAGE, A component for showing quantity, pressure,, w% s2 B$ i6 `. X temperature by a pointer or numeric display.: A) f! j$ K, N8 Q G3 I' P. C! z/ k square inch gauge (psig). L6 `9 N9 o; ?3 F/ e2 D* `/ k 燃油流量, ) M! x. T S9 A5 t5 {1 h, q/ D发动机消耗燃油的速率。以每小时单位重量衡量。. \7 a, [8 Z: {! F6 u1 j3 p# i2 ]$ }6 h: s 发动机上的一个部件,用于加# t# a0 k, Z; c/ L5 P 系统结冰。 G. S" d0 i# `) t% D3 P" j/ _9 y! t* |, O5 A9 ? U$ B! H1 u 一种通过将油箱* ~; v$ R; u. n$ _ c 方法。6 Y3 E9 Y! R& }; K5 O" X5 G/ N* Z1 H: C3 P' }. q: q- P4 e6 F3 K" y3 f! q5 S* Y- C1 f) U4 _* z% g计量仪, + z" Y" v# m+ s2 ^, j, Q0 J由指针或数字显示出数量,压力或温度的部件。+ ~4 @' V. C0 q+ Q- m% I6 L5 C j: p$ B! i. n b; i# I单位是(每& G( d: c" {7 `. E2 a 示压力。2 N/ l* O. y `6 S 英汉对照民用航空词典B OEING 4 B& w9 T+ H; {( \1 }6 X; E% D; YTECHNICAL DICTIONARY 67$ P/ n) d. R' C. r( d/ i* t GASKET, A seal between two flat surfaces. ( Q9 E( i- `, v7 ~! Lbe individually controlled for the amount, y! N- P3 V9 J0 A+ `$ d/ P nd direction of supply.6 T5 Y( b. O w1 ~, } W8 d ATE (NO. 1), Airport location used for# z. x" e3 X( r0 r# q ading/unloading passengers. 9 y+ L* G3 n4 w: lATE (NO. 2), SEE - LOGIC GATE & d1 v+ z& _& l; {2 TATE VALVE, An actuator operated, sliding device in a; R8 e9 n' m* O$ B uct for closing and opening the duct passage. : Q t/ y" V% q间的密封物。 ! ?& f& f8 w! j* [调节供气口可控制空气的量和方向。 " O6 C2 [1 H& a! M, p: g登机门, " a: {- {# | o2 Z3 n- ]' `机场内用于乘客上下飞机的通道。 2 R; Y0 T9 T$ N% l逻辑门, 7 {; f' }1 z; k* j# [/ I见Logic Gate : N9 `2 }6 N) a3 P5 \7 X5 yGASPER AIR, An individual air supply for each4 ]& n9 |; _5 c$ q- A9 X8 C+ q passenger. The air outlets are in the Passenger Service0 Q! }" ]% Z2 F# [% u: g4 e Units and can 2 |7 D4 P6 A3 a/ G# X L+ X: xa: L( g1 C0 ]9 s; r G! ?2 _8 f/ P& }# X/ \ lo ) p+ H" l d+ y Z, m" tG K( \" o R; Q G ( k; d4 {' W& Y" ^- v4 c% u# L( hd - Y! c* I& W5 @; l6 r7 P+ [! V0 v密封垫,5 G! ~- h! B7 ?& H0 H7 Y7 j 两个平面之& g% v# c: a; G# c5 A* } 乘客用空气, h) H c( u1 J: {% U 给每位乘客的单个空气供给。供气口装在乘客服务设备 * `: T* y) H( i! a; ^' s内,个别) E7 j4 x2 [* o6 i4 M% h% `4 K7 m$ C2 |9 ~* U' N6 I8 ]% n 闸板活门,5 J% E2 v3 G7 i i$ M" Y 管道中由作动筒操纵的滑动装置。用来关闭和打开管道3 m9 a$ X( k+ J. h( U6 c 通路。) d6 S$ H! V$ P& Y4 Z4 R 英汉对照民用航空词典B OEING ) j! Q; k8 h% g% e$ tTECHNICAL DICTIONARY 685 o8 H0 B/ `) C/ `! L4 F GATEWAY, A functional unit which connects networks/ L; F2 U+ ] M, T9 l* q) c r systems of different data formats. % i) B5 }) y; x0 C9 Y0 TRS. $ Z) A6 d* I2 O- B oENERATOR, A mechanically driven device for4 ~9 `2 Z2 ^% H* p ENERATOR BREAKER(S) (GB), A device which will 8 s. s/ W8 p$ V) \5 S; J- R3 dtor from the : I, N" [9 Q% o7 T8 Y) c' olectrical bus(es) it powers. 5 K$ ?! V! L( qent with& E) v6 L4 P% x. y# \1 T o rings pivoted on axes at right angles to each other * R) p' o$ y# k8 N" Nllowing movement in two directions used in the flap & i/ r2 @, J+ R# a/ M: z- J( X- L2 Vxtension and retraction system. : ^9 F( ?/ t- Z1 h D接在一起的功能 ) e" [ w/ F7 D, @件。. R* R) `8 h( t ]( n. | o5 C! }( m" v5 u GEAR DOORS, SEE LANDING GEAR DOO + X4 r5 D! ^7 S5 f, a4 M" ?) r" d0 \4 yG$ i2 ^3 d" T. k/ k- A1 ^& O producing alternating current for airplane electrical 1 M! t) w! O1 w4 X, bsystem. $ n. w% P1 F4 r& u7 u% r, z' CG9 v1 Y5 S1 [* K# P- O1 Z* Y/ C separate an electrical power genera / r. ]# Y# ~' n7 o( C; K( m; j* qe & _9 @! L% ]# @, B7 b! B5 wGIMBAL ASSEMBLY, A mechanical compon F- A/ I4 ~5 I+ |/ f1 M7 M( Mtw 7 e4 B1 t$ `. e, B1 S' g' a- Ha. c8 N$ I! @4 Y5 j- B* E e" Z) x1 Q; H1 j Y 闸门, 3 o0 N" y! H7 c3 Q3 _ D# v" p一种将数据格式不同的网络或系统联& W/ n/ s) b" @. c% b8 s5 _ x- G7 m/ f3 F0 P( y 起落架舱门,# g7 u( t, R9 a l. z+ `3 ` J1 B7 ?5 B 见Landing Gear Doors. 7 l! f/ V% j M' w# E; U4 e8 ?* [+ p! f发电机,9 g' \6 p4 v" w0 @' a7 h2 t 为飞机电器系统产生交流电的装置。6 E. `* u; q' J+ u1 G 电机跳开关(GB),! Z" V) L. u9 n; |5 k 机与由它供电的汇流条断开的装置。! G! k. i5 K& [% O, r- r, c& M, E. X 襟翼的伸出和收上系统内的具有两个圆环的机械部件。- u5 x! O) c T 个圆环的旋转轴相互垂直,以使部件在两个方向都能转 + N$ {' n( J4 X( T' \5 d4 `$ J# l* K0 U0 m* C由机械驱动, . k' m, s/ U1 B2 ^* s$ F$ Y% w! [% V; Q3 G$ o2 b2 V$ m, @能将发电 - L+ K, j( f0 H- k( c9 U万向架组件,% |& `. `! F2 R* y% |* v5 `" |: z) k8 E) Z, T g- l( d4 b* z英汉对照民用航空词典B OEING ( n$ k* L, m- b; y( V+ U8 PTECHNICAL DICTIONARY 69 9 u+ |% C$ j" |GIRT BAR, A rod attached to the escape slide which4 i5 I: @5 n# h* I5 R3 l( l6 k engages brackets on the floor for automatic slide9 O1 z) u3 _. {: V! d0 P peration when the doors are opened.' _1 {4 Z* U8 X; S! V LOPE (GS), A vertical path defined by a/ T/ z7 M/ i- n( w8 W ased electronic signal used by an airplane or+ ~" s, q6 p' @: \3 N' M, l& V: L LIDE SLOPE/GLIDE PATH INTERCEPT ALTITUDE, # d. f9 J, ^% @1 G8 U: }% F- xhe intersection of the # f: t* E7 |( `ublished intercept altitude with Terminal charts by the 5 {! U. m) [/ Utart of the glide slope/path symbol, is the precision FAF;3 H6 e! p# I! G; W# e6 ]; Q6 T owever, when ATC directs a lower altitude, the R+ O, w# g+ Y0 S! ^( V ~( f/ \9 Q3 N上之锁钩相齿合,以便滑梯自动工作。$ i6 N0 N- q& w4 K% A 滑道(GS), 3 ~1 I' @0 i; r" Q2 C8 j由进近或着陆期间,飞机或飞行员使用的地面电子信号 5 `# S$ ?& I7 W1 `+ r* j# M) y垂直下滑航道。 3 k& t+ `7 x( D/ x, N- G6 l滑道/下滑航径切人高度, % M0 P) v( }; R+ d进近时切人下滑道/下滑航径的最低高度。在: x8 t' L- f3 c/ C8 m2 \ 最后进近定位点。但当空中交通管制指挥一个. P9 ?/ V& y, | 低的高度时,由此产生的较低切人位是最后进近定位" _( |; j% E/ M$ U' r6 j1 o( b; I8 V9 { o; Y7 p n/ O- ?6 R9 p" I GLIDE S6 {# i5 \2 J# A% x+ _) ` ground b% a: v, q5 V* u7 s$ ~; Z pilot during approach or landing.4 M; i- C6 k% u G" @5 W4 @4 _' G The minimum altitude to intercept the glide slope/path% Y6 R( a) P5 y8 n9 W5 C. P& B on a precision approach. T* w& S& [+ J; A$ L3 s; N, D4 Q p7 j2 Y8 d" o) w: X" v3 C0 C1 e8 r" q s 4 ?( `& i6 h) a9 y: L* q* F' H( Th/ b7 h Z$ k/ i; T2 H resultant lower intercept position is then the FAR.- F8 d, K) ?# m 束缚杆,, d3 f3 D/ k: L6 M 连在逃离滑梯上端的杆子。在机舱门打开时,与机舱5 H1 S. j. I& ?9 B& X2 Q2 \- o/ ?" b4 T2 C* a F7 x# _: L( W5 A( I6 p5 \ 确立的一条) I9 f7 n4 ?: w5 n. I+ W* q& Z/ `% L7 X+ q5 z* T5 f在精密 ) O2 C: ?! i7 T% }* c2 D6 zJeppesen机场图上公布的切人高度与下滑道头的交接 4 T+ ^) ?# |( h点。是精密 , c7 Q3 l1 r* o0 O# K6 k3 p- \1 T. q4 g X5 A6 W- L* H* l2 d0 b, b" h9 r: z* e* \英汉对照民用航空词典B OEING 0 n8 ~; g; a/ H7 G( [' CTECHNICAL DICTIONARY 70 5 H* e5 @. n, @0 i3 D$ _9 c8 UGLOBAL POSITIONING SYSTEM (GPS) (No. 1), A% M- Z8 P: s2 c& j9 ]1 O6 O. m pace-based radio positioning, navigation, and ! s# I4 a" h. D: ^7 m- o) hmetransfer system being developed by U.S.A.2 N1 n n# w- p# V/ @) r+ c/ v epartment of Defense. The system provides highly# k9 z% d' E4 U# l recise" L Q8 k* s; B% p nd provides a worldwide ( q: v9 {9 w$ common grid reference system. The GPS concept is ( W, J1 v, n/ u: gredicated upon accurate and continuous knowledge of5 i9 Y- y# T' k+ L) u! k$ u+ ~ e spatial position of each satellite in the system with3 j4 v! `& P2 U spect to time and distance from a transmitting satellite & \7 o$ |5 `6 N% b1 p. ], Z: _! Qthe user. The GPS receiver automatically selects 6 w2 ~, ~, e7 M5 e; T3 `, Wppropriate signals from the satellite in view and# Y% U" Y( ^& C* u anslates these into a three-dimensional position, 8 u* M/ x( A* R8 R/ t, s. L$ jelocity, and time. ; \/ a5 d0 G2 hLOBAL POSITIONING SYSTEM (GPS) (No. 2), A $ {7 i: |, w# l1 Z6 ingrange navigation system that takes navigation input' t+ a5 r4 j- c1 O- v8 c7 w om transmissions generated by a series of satellites in0 K; @# F! U$ A, l- [4 d LOBAL NAVIGATION SATELLITE SYSTEMS (GNSS),3 n) D$ D9 s6 @# P3 A* K/ A ternational Civil : p! O4 v. N9 v. Jviation Organization (ICAO) to encompass any 2 `0 c' S: K, k% k" [1 W( Z! ydependent satellite navigation system used by a pilot ) z: R, H. ~2 b% v9 d" Eperform onboard position determinations from the . M+ ?% g r0 a$ |- c( C# A7 |O-AROUND (GA), Airplane maneuver where the pilot is+ G8 P; E0 z9 R: i in the final approach phase of flight and decides not to z; d8 c' u0 V# {9 E g% ~land. Thrust is applied and the landing gear retracted so0 B# @; ~, A7 P7 d( w5 ^# w$ b3 { as to climb the airplane to a safe altitude.! w; c& |& r/ l8 h4 Y GO-AROUND THRUST, Maximum engine thrust to be # _' f- N) ]+ F4 Z0 ]$ T+ Z2 Cused during the Go-Around Maneuver.: f- z5 h' p% I3 n" W 统(GPS)(NO.1)," g. y: ?8 _# i 电定位,导航,和时间转移6 _% j- q7 ]7 Q) M* Z- z 统。该系统在全球连接的基础上,给无数备有适当设备 + V1 X2 v6 L9 r: P1 U" x) n户提供高度准确的位置、速度、和精密时间信息。该系 ; A/ h- `: v @ y6 }响,并提供世界通用性座标系统。全球定 ) f+ { g& J7 ~% c2 b( c4 M信息之原/ w! W+ q) b! G 为基础。全球定位系统自动从所见卫星选择合适信号, " A) E, w. C- `4 i- [" B. }( z& W' r并将这些信号转译成三维空间位置、速率、和时间。 3 x8 v. p! I$ Y9 V0 X' |" ]全球定位系统(GPS)(NO.),& a4 I- X) h0 q' L( Q 一种使用一系列同步卫星所发射的信号作为导航输人6 F ~* }. T! ^! R2 p" D 长距离导航系统。 : q- c% l- ?: `' g2 e球导航卫星系统(GNSS), , A( f( A; H/ g航组织采用的“伞形”术语。它包括飞行员 7 g/ F" e) ^- Z% E料做位置判断而使用的任何独立卫 4 p% c/ i$ u& x) f导航系统。 * \* f! G# z' b: w# d% y复飞(GA), 5 z D: K. Z7 ^# C& }6 b1 ]飞行员在最后进近阶段,决定不落地而做的机动动作。 # a6 X5 z* V$ I- ]! q复飞时需加油门,收起落架,以使飞机爬升至安全高度。; ]7 _* j; |$ K 复飞推力, 0 L- \$ |0 I4 U9 O$ _7 A9 x飞机复飞期间使用的最大发动机推力。; J0 O9 ^0 N8 ^( |4 l5 ^ s & E4 c; Q2 Z" `) M8 N3 m, _9 M# g, ^1 Mti% l; d: d- }2 n z) l D 8 r1 W) U" V. x4 |0 _- m3 ]5 h; l7 maccurate position and velocity information, and p/ F( Q& O7 v3 ` _ time, on a continuous global basis, to an unlimited 0 d, |( F, c. K* G" Z K& C' gnumber of properly equipped users. The system is 9 }% w! z3 m) z) {) S( tunaffected by weather, a % B( p5 c f p `6 t) m, d) Fc: [4 B5 F& V' P6 f" J. j- Q p# U7 v, o# A5 h H7 o' @( y th ! o: E9 J& O8 i8 c/ Mre 8 Y6 {8 {5 `: W) Yto * ^: Z& R3 ]" e/ Z& z, g2 Z/ X; }a& f) y) F" g. Q2 g tr6 v3 }2 y" Z, j# ? v 5 s+ v. E, G0 P# y' M$ OG ; q$ f$ e4 ^! clo+ W1 u. F# g: d0 E9 U2 F fr) L( B! E; L: p synchronous orbit. 0 {* Z, B9 v9 DG 9 w! y4 x _- L( P1 J# ZAn "umbrella" term adopted by the In , _7 _2 w' a5 `A 7 i9 l" C$ }0 U+ F6 N4 [in ( o! b/ ?9 [. uto+ k4 [7 I$ t% ^; H satellite data. 0 N3 |2 r9 E- O9 s1 V) ^全球定位系 / g" N# e1 p' h6 p! G由美国国防部研制的空间无线8 ^* {2 `2 G- S5 i# v) ~; D: p( k ?* S- b+ `& U7 }) [: P0 A 统不受天气的影 3 C/ Q/ R) g+ q* U+ P5 N* |) y位系统概念以系统中每个卫星具备相对于发射卫星与用6 C8 C9 k2 P1 X4 \ 户之间的时间和距离的准确且连续的空间位置 ! _1 T( z5 W- n( F$ p( x5 v' L4 O! a' ?' x4 l" H5 d4 {0 Y 2! r2 @2 d/ V. s) e0 P ^: m3 Y6 S. U# i* l. v' q k. d" r4 _0 f1 Q是国际民 4 w! P2 `% V1 Y/ i& ^ u) B A在飞行中根据卫星资 ' S) l7 ]% f/ f4 o( [3 x3 G* @! T* |+ M0 j0 a- y2 B, u 英汉对照民用航空词典B OEING, E$ l# V- ^' U TECHNICAL DICTIONARY 71 A( p: h* ~3 h' j; R9 J GRADIENT, The ratio of height gained or lost in a given 0 E2 T& t- s5 l% `- I+ Vdistance to the distance travelled.& E# Y4 ]- j' o) E+ ~. I {2 ^ rbon! T8 } S' ]6 V3 A; @ r access panels, landing gear doors and flight, ^, _* i# }5 [- l b ontrols.3 P, F* `5 R$ R* e; d IRCLE ROUTE, Is the shortest distance3 A7 i( D; L( b* u o etween two points on the earth's surface. It is the line1 U {8 [' t& H7 a7 o rmed by the surface of the earth on a plane that4 r$ F# n% ?% X/ M8 L; p& b asses thru the center of the earth, the departure point, 7 C( B1 y8 N5 C. m: Et line + Z3 ]6 Z6 ~ d, T! ^, Q, jal Conic Projection - P+ @/ g: a' P4 @3 A+ W) t. cpproximates a great circle route.5 a- c+ R7 L" _! H% g2 q% w3 x# Q. Y GROSS WEIGHT (GW), Total weight of the entire \* a4 O V" R. Hairplane, fuel, oil, cargo, passenger, etc. $ m4 E5 w- P' o' t& f/ H) l& y/ ]5 vGROUND, A part of an electrical circuit or system that $ i/ r) k2 u1 V8 u s- x0 whas zero voltage.( ?' \! ]: X8 d9 @% o GROUND FAULT (NO. 1), System fault that has ' m; T. k0 x( B0 u" z& @occurred since airplane landing. 1 y1 i8 ^ J1 S5 k1 }- D轻的材料。用以制造舱口- |& b3 q9 y/ v& z, i ,起落架舱门和飞行操纵面。 3 h* _9 M/ s2 p3 S6 i5 {圆弧航线, 3 r2 n. g* x" G, |7 l1 w8 Y地球表面两点之间的最短距离是以地球中心为圆心,在 - L* J/ C$ {4 y7 g9 ~1 e飞点和着陆点间所形成的弧线。由大圆弧航线形成的真 : L% f, Z/ S! s* g3 d迹不断改变。在兰伯特等角曲线投影上画的直线接近大 . ]1 a0 y+ I3 J* u; ?. E全重(GW),1 q4 `/ K: ?& b8 S- ]: @ 整架飞机的重量。包括飞机,燃油,滑油,货物,和乘- x7 p \1 s4 _/ F% | 客等等在内。 $ V! [, }! l: a# U地线, 7 z+ Q7 c& d* a2 l1 b$ X4 ]4 R; Q6 z在电路或电气系统中,具有零电压的部份。( j' N+ ~, ?4 _% M) y" R 地面故障(NO.1), S; G* l# Y8 g自飞机着陆后所发生的系统故障。2 L, s" L( B" { GRAPHITE, A strong, light material made from ca! a3 J1 w& F6 \! ]# {2 K% a fo: Z; s: }$ M! p+ G- g; f$ {9 l$ E+ y# o9 L c. y( W$ }; c" L$ q0 A ? GREAT C 8 X) K0 {5 G" C0 G5 c' `b - B: d4 O; Z. M/ [fo6 ?9 ^; B# D# x. ~ p2 I" W. m% ?. o: X+ X \ and the destination location. The true course formed by4 Y* [+ R/ A* I/ K2 m; Q+ T a great circle route constantly changes. A straigh : H( z) L) F* n2 Tdrawn on a Lambert Conform" f: k0 {' ~& f, `+ P- G a 5 A+ ^, e. G/ p0 }3 D; zGROSS PERFORMANCE, Actual or measured- `, G( U4 ^& m+ a: ? performance of the airplane.% f6 N# J$ P8 M! W8 W6 k 梯度, : L; y( `6 z# ?4 f: y3 O在给定的距离内,获得或失去的高度与所经过的距离之' B# J- ]8 |$ D- R, ~6 A, A 比。, Z4 Y6 q7 ^/ E& h5 o9 p 石墨, , B! M' ~( s. D一种由碳纤维所制成的强而 ! Z/ M& P3 L |9 p, y; y# p0 Y; C+ o) J3 K( f' @, L9 E* }( C7 [9 X) V8 m# g2 C N) o9 ?% B4 S8 O2 p. S$ Z( y9 b圆弧航线。 1 }- [" p% N! }( R* y1 Q/ Q总性能,; H1 E. L3 G: h! _" ]+ N! S- a3 W 飞机实际的或量得的性能。 ( w6 A+ J5 }8 [# F5 _3 G. ]英汉对照民用航空词典B OEING2 D$ }+ X6 ]1 ~% |7 o3 e0 l | TECHNICAL DICTIONARY 722 X9 R+ }- c8 P; Q& E GROUND FAULT ( NO. 2), Loss of a ground connection : I, q) M( ]2 g; Eor a short-circuit to ground. # F8 i# S/ q, m. t# AGROUND SPEED (GS), The speed of an aircraft' r0 V% ^- [. x" L# Q" E lative to the surface of the earth.. g/ C) g) A, b# h U6 J ROUND SPOILER, SEE SPOILER2 f2 k; l" W" O/ F ROUND SUPPORT EQUIPMENT (GSE), Equipment0 P' X9 j4 W- F5 {3 m* g4 t+ U sed to service, test, move, power, or repair an airplane 5 Y% U# |+ n6 B, R, C" ~( W1 Ohile it is on the ground. n1 @2 P( v d1 I- f ROUNDING POINT (TERMINAL), An electrical+ Z' F- P3 V" I9 L onnection on the landing gear doors for electrically 8 K5 @6 O2 N: X6 T+ D% Rrounding the airplane. An electrical connection near . X; m! \( J0 r- y' D9 Q* Te fueling station for electrically grounding the fueling3 W. g' C- v. P. u0 T" k, y. R ase. * U0 V5 q1 k" N* tS, SEE - GROUND SPEED 0 j4 w! i1 [0 K. a. m3 _, x5 VSE, SEE - GROUND SUPPORT EQUIPMENT # \/ n. ]4 n. U- w! B% \1 KNO.2),6 P7 s4 Y$ P+ D) ^, B) l% _ 地速(GS), . {0 c. d8 x* h6 g/ K8 K飞机相对于地球表面的速度。9 y4 q& e/ S' N I9 m 地面扰流板,; l+ G7 e4 U- e 见Spoiler - M5 t% z6 T) l& Pre0 O- z7 l5 U2 z! J6 Z G ( z* R7 x4 N) G9 A ?) d" {G + z# I& h. ?* w# c9 vu0 {5 r( @( P+ E; ? w( [! \ r, K7 F6 n G . W) V4 V- |! D+ Rc ; r z6 h0 _4 w ~g' @4 C' j" E9 l r# x th - s0 Q i! @! v; ~b9 Z. m6 H9 v$ R/ p' E- ~ G ' j q' G& |( p# mG , }7 p+ D9 R0 a1 k% _6 |! o: xGUARDED SWITCH, A switch that is protected against" ^/ o6 e5 V* w E# N accidental movement by having a cover installed , N6 Q, A( _% [& r4 tdirectly over it.: \6 v, Y! ^: n 地线故障(7 @' [$ w, r' Y/ ~' e7 ?. f$ x 地线脱断或某线路因短路接地。 & n# y; Q; N% Y$ _; p/ u. }0 r5 B9 W- p r 地面保障设备(GSE),6 j; G* U$ W5 l) X% N# r 当飞机在地面时,用于勤务,测试,搬移,动力, ) C3 a% s7 _6 |8 _或维修用的设备。6 \0 W( l* T" r+ g& ]$ c0 j) D 接地点(接头),4 _( {0 D. s1 ?7 h( n 是在起落架舱门上的一个使飞机电接地的电接头是在 3 l% E/ e" W; w) R: x+ ^' l加油口附近,使加油车或地下油库电接地的电接头。& g [9 a" O) l z3 u& X6 B& B 速(GS),( B Z; n7 L, X- R+ K9 A eed" ~# F3 y5 i7 V1 F( t 供应% ]9 X% y. x, k- ~' ~! ~4 e0 a0 j7 S# _. p% A# m6 r& w见Ground Sp .- @* `$ \( k# w: o 面保障设备(GSE),* X# u, d7 t9 s) M- i# l6 d8 L4 I 见Ground Support Equipment S" D5 O& g. U7 ]! O$ J# f9 ]0 N: _% b# X; f; x9 A4 K& J y: x' j; Y$ Q 带保护罩的开关,8 s6 ~. H9 V3 k; F0 N& o 为防止意外拨动而直接装有罩盖的开关。8 f4 L/ F' B6 l. W: c5 s 英汉对照民用航空词典B OEING 2 E& ^- i+ [1 g+ FTECHNICAL DICTIONARY 73+ F% Z# S8 ]$ Z- V+ e9 o+ I( C GW, SEE - GROSS WEIGHT ! O" k! ~$ J# m& K1 p+ X- }4 Y( QH: i9 A9 T, W" P HAIRLINE CRACK, A serious defect in structure; a: S7 w7 R6 j, V1 `4 O& S crack that shows as a very thin line. - |. e! l1 z1 q+ THARD-OVER, A maximum pitch or roll maneuver. c+ e, ]/ z: |( }$ ? q8 b* KHDG HOLD, SEE - HEADING HOLD 7 W" d8 g9 S! p l4 T% \ w1 s! o2 mEAD END, In a hydraulic actuator, reference to the ' k7 U2 b$ A* b- H) B' `5 w5 uart on the piston side of the actuator. % [8 P. f: j( G1 lHDG SEL, SEE - HEADING SELECT0 V, U7 i0 K" D7 ]( _ H 7 M" Q, }2 Z0 n1 Yp 5 P! V! d" i. |2 {& vHEADING, The direction an airplane is pointed , C8 o* R) e [referenced to true north or magnetic north.8 H; a0 e4 \( D k. v6 H7 F 全重(GW),# b8 t4 W% v, t( [* b 见Gross Weight.! b" S( Z* z, y% Q8 x 细缝裂纹, 1 B$ T( k- q, f' b& J+ i5 X h7 y结构内的严重缺陷;裂纹的外观是一条很细的线。 % [$ R4 ]! k4 B6 v b4 q急偏,' d' }- @4 [% Q4 O E* a9 P* T 最大俯仰或横侧操纵。 2 b% x* ~8 ]6 y, S+ D: |向保持,; {8 k' B0 F/ q/ ]. H2 r+ X 见Heading Hold 6 I) T9 v4 L" y) q; Z$ B4 A8 `7 C. q! L2 Q2 y$ H! \6 H" r5 P& Z航向选择;. N! i; }, F: g# _ 见Heading Select.5 I2 Z& t$ x$ D: F; L 顶端,% a; {( x$ w4 C, d0 U 液压作动筒中与活塞相邻的。 - n) J) r" o& s相对于真北或磁北的飞机指向。) F6 D7 N! f+ [1 f 航向,2 L: s% Z' ?" n8 S3 \0 O: f 英汉对照民用航空词典B OEING . s/ L6 _4 q, E6 v5 U! vTECHNICAL DICTIONARY 74 U `; Q7 D' _6 nHEADING HOLD (HDG HOLD), A mode of the autopilot* @" \9 J0 Q; L# s irplane heading. ; N0 @6 D* n+ V2 ]4 Zt% S4 R, z+ N S, ?0 V" V+ {) k e # M. H$ C' _) k: v) |8 z2 ]om- K1 F8 S- s; o g or' H- y6 u9 y3 ? (HDG HOLD), 9 }/ [) s' T' p; D(HDG SEL),, [0 ]: R- X1 r 交换器, 6 C$ @" k. c4 U4 A有很多通道的金属组件,气体在通道里流过时,一股气 0 @% I0 [, q/ d& J2 q& Z: |可被另一股气流冷却或加热。 ; o# w8 G7 `1 p+ u. _% G$ }5 Qsystem that maintains the existing a, i- n, D3 o3 h* e$ @! Y) ]' c HEADING SELECT (HDG SEL), A mode of the autopilo: Z: ^5 j. G3 y e' ~: f7 a system where the pilot selects the desired airplan4 i# W2 W3 Y0 z: {9 t/ s& r heading. ; F/ ?4 L( y7 t( ^) DHEADWIND, Wind or component of wind coming fr+ ~0 b8 c7 L) E* d: b, b/ w the direction of airplane travel.; ~! |( B8 w+ C, h. y HEAT EXCHANGER, A metal component with many7 L! I4 g. k3 i passages through which a fluid can flow for coolin 7 F, J. r- ?- F+ |# dheating one by another.8 h7 V. Z. ] g6 E 航向保持 * o# j, y9 b Y/ M* i) J* b自动驾驶系统保持现在航向的方式。& Z, V. M& J% }8 a 航向选择 " m( t. P3 [1 u& K* ~5 g; Z自动驾驶系统由飞行员选择航向的方式。 4 u1 i2 _" }& {/ ~" W5 D, P顶风, 0 W' P) w* X# g5 u' B' L: o/ J `来自飞机前方的风或风的分量。 & H0 ]" K. K: K. A# S, I9 \3 O- `' j% j; N" q8 v4 A0 q$ k3 \; O6 m. H 英汉对照民用航空词典B OEING % `) j4 V( {# T8 ^" ]7 o" ?2 Y/ x. [7 ~" KTECHNICAL DICTIONARY 75. N) N' K! |+ \. T HEIGHT ABOVE AIRPORT (HAA), Is the parenthetical0 d! e: }8 t: D+ R8 o* G# a. X figure following MDA which, when added to the airport & t' i, |) l" k) \1 `; ?7 g2 T3 |levation, will give the MDA in feet above mean sea 5 G' O6 R- X$ h0 I1 j, ~4 V8 Fvel. A HAA will follow a DA or DH only when there is6 p! |) t: O( e, K$ a7 P/ J' o o touchdown zone, runway end, or threshold elevation , D4 y0 ~: ?' D+ n3 B4 N), IS the. |4 r* K; x7 M; U$ B4 D( X arenthetical figure following DH, DA or MDA which,1 u8 T$ ?7 B4 @6 x( B) ~1 \9 n hen added to the touchdown zone, runway end, or 6 A# d2 X) z" J& w* Greshold elevation, will give the DH, DA or MDA in feet " Q: L2 s: w8 j: Q* `& G) ?cy of one million cycles per second. $ O$ S" _% I: s' HEXADECIMAL NUMBERING SYSTEM, A numbering3 ]4 E! Y& q. g6 ^0 |' e2 B3 P ystem with sixteen as the base. The system includes$ q9 ~' J- d% x- m. u+ n igits zero through nine, and letters A through F * r9 ?" x- H$ _: ]) k5 \9 Y) rpresenting the numbers ten through fifteen., i7 u3 g" f7 T IGH FREQUENCY (HF), The frequency band between G) N, O* s2 Y6 q, `场标高相加后即是: \- F' A7 Z& c7 F0 W. j DA高于平均海平面的英尺数。只有当接地区跑道顶端或5 a. q; v0 X" I* C, Y 道头标高不可得时,机场上空高度才跟着决断高度(DA1 H( N; n6 g3 x) ^ I# @ DH).% @5 O6 {8 R: z: v% t) e( H! R' K HAT),0 ^4 j' S( g$ V: R6 }1 R 最低下降高度后括号中的数值。它与接地" _: T* H q) M* n# d" x+ o7 d o 、跑道顶端、或跑道头标高相加后即是决断高度(DA,, J1 @" x' U" q' d H)或最低下降高度(MDA)高于平均海平面英尺数。 / W8 Q. a, v' M6 y9 h) T/ X的最低天气条件同时公布的。- T1 h G! I* u- q4 o 率。 - @: C$ T1 ^# i4 Y" q% t: R" q一种以16为底数的编号系统。该系统包括由数字0至* j( y2 z7 B: {3 r8 G4 L# I0 z ,字母A至F代表10至15. V6 U5 g8 S4 k* r, S! m( r 频(HF), 9 }1 Y# Q: q f* b( D赫之间。' Y% X. L, g- L. [, o$ j e: w4 O- J: G) y/ G! K4 K le % x( u/ x/ N* V7 F Un1 E4 j7 \$ G5 p9 w' j! p available.. o4 T1 s' ?- l5 P( \! \5 W F HEIGHT ABOVE TOUCHDOWN (HAT/ k3 d4 w8 _, T* Z' B p- S# r, g( j0 [! N5 c* T w \$ ^4 D( [& m, n: M6 qth 5 U8 a' e3 c' ^above mean sea level. HAT is published in conjunction / b% n0 l0 M5 {3 C( iwith straight-in minimums. ! r C1 l! \, }# vHERTZ (Hz), The standard radio equivalent of ]' z8 i1 r! m$ B: mfrequency in cycles per second of an electromagnetic 2 [, J+ Z3 M+ g. C$ S, e+ swave. One Kilohertz (kHz) is a frequency of one # ~5 H1 ]! H4 C0 m4 t: J ethousand cycles per second. One Megahertz (MHz) is a , v# o( T3 }( F% C1 Ofrequen " O6 H# K1 p9 ?! nH. j! m) U. J, N' _8 W s9 {" ~8 a, j3 t- G/ M5 E( k d: [; c2 v: e! r( h6 A6 M6 S, n re 3 o- O, a: m, X2 [* K: TH ( j/ N A7 ^4 b p6 a% I/ v- P( O3 and 30 MHz.: n% w, R& Z8 h( F: d l: n8 G 机场上空高度(HAA),+ w7 y& a o' u 是MDA后括号内的数值,它与机* G; X, |: _/ V: Q3 A M 2 I9 L# @% |: v9 D) K& o- U& a9 r! M$ \6 \- j: S4 G! E" u9 H8 Y2 C) P: i) i3 q% g离接地点高度() o# @7 [! D' X 决断高度或 1 V# T X: l; b9 D* K. u# B t" M2 MD 5 }6 n, E: s: Q5 S0 Y接地高度是与直接进场着陆 . ] a4 G6 r2 P# O赫兹(HZ),9 d* V$ B! t8 d8 B5 k" ^0 U 单位是周期/秒的电磁波频率的标准射电当量。一千赫 + z9 F0 U. c. W7 ]/ o% p( W0 T6 e兹是每秒一千周期的频率。一兆赫是每秒一百万周期的 + a' b, q. C/ p* ~! Y0 W% v# s. S$ D H/ L 十六进制编号系统, 3 R( W7 t9 C0 }0 v99 ?$ h6 L+ _( c0 o5 E2 Q$ L5 @* m% V* I5 b- `频率带在3至30兆 3 ^+ t/ l$ H% b$ q: \, v英汉对照民用航空词典B OEING& O7 b Y5 d7 ^2 F: P TECHNICAL DICTIONARY 76: r2 A% Z- R) w0 Y: [ HIGH SPEED TAXIWAY/EXIT/TURNOFF (HST), A long . j8 R. W! e8 l/ Q; x( z3 | K K4 sdius taxiway designed and provided with lighting or ( W; `# d- a6 N" [% F karking to define the path of aircraft, traveling at high6 i N" A6 i+ _% g% A6 W7 K6 Z' J p to 60 knots), from the runway center to a, k5 e3 Z& B% {' |5 E( [ the center of a taxiway. Also referred to as long) |# \# ]3 _, f2 S! ^4 A& z+ J$ u" y it or turnoff taxiway. The high speed taxiway is 6 f0 u; x8 \4 ^# k4 M( e% r5 gfter ! E Q- Q5 k. a [+ c% _ancy time. 0 S6 S) ~+ J5 q8 }6 ~$ n- i5 x3 ^r a+ K9 X2 ]( X; V H eavy component during removal and installation on the% [ n( E: v) b4 m$ y& ^) z; A/ V irplane.% d8 ~- X* i0 ? OLDING, Airplane maneuver to keep the airplane from6 z i& [0 j/ w8 D rogressing along the intended route of flight. / P; c: x2 o0 ] _/ `OLDING PATTERN, The predetermined maneuver I1 N5 h o# Z% F c control.+ e( [7 Y, Z9 l9 w# d# F2 W OLD/HOLDING PROCEDURE, A predetermined 8 L) Y" _3 D/ g/ V" I$ M3 M0 _: Maneuver which keeps aircraft within a specified$ ?, R: M' z1 A/ ^) x- @ irspace while awaiting further clearance from air traffic" F! g2 a; s- u0 s6 C6 e ontrol. Also used during ground operations to keep ) b) D: u, y$ ]" fircraft within a specified area or at a specified point ' ?7 P& v7 K% Nhile awaiting further clearance from air traffic control./ c0 [; v4 Q0 U6 C5 ^8 {, K he standard holding time is one minute at or below - p0 y8 w1 \* r0 f; K: E) @$ U4,000 feet or FL 140 and 1 1/2 minutes above. The ; i* R3 A' `! G# f- w+ r; t5 x! Q$ Oeparation between 1 and 1 1/2 minutes is FL 200 in 2 e- q8 t3 z: Y, l+ i, e(HST), : a' d- u4 G" S6 U" T道。该滑行道有灯光和标志表明飞 `7 c3 B; f- v. {8 B( ~( {% T, e# t从跑道中心到滑行道中心一点高速(可大到60海里)通 : T) W7 U1 F7 |: N I* }* D的路径。也被称为大半径出口或脱离道。高速滑行道的 & M+ a. E' x' u' c- D2 N% {计意图是加速飞机着陆后脱离跑道,从而减少跑道占用 7 H' m% D8 ?/ n$ x3 U时间。 h4 A9 l3 w# G4 \ 安装过程中,用于放下或抬起$ N% f# [: E8 W7 F3 T 动机或重部件的装置。* J3 h4 j9 |- o! [ 待,! Z$ X0 Y; Q/ d9 H* ^4 b! E7 S 使飞机不按预定航线继续飞行的机动动作。 - q- _' H$ i3 x8 h1 _3 G待航线,. q1 l3 _0 d/ o5 s 处于指定空域内等待空中交通管制下一步调度 & |; E* V: B2 ?9 x8 C等待程序, $ W: f. q- O! o7 h4 {保持飞机在指定空域等待空中交通指挥的下一步许可 7 `% \* X& e* W" T! C的预定机动动作。也用在地面操纵来保持飞机在指定的地, Z1 k" l5 M( V1 N J- x 区内,或在指定点等待空中交通指挥的下一步许可。标准 5 C4 v5 i. q" \# L的等待时间是在14,000英尺或高度层40以下时1分钟, ) @# W0 D0 y" m8 u5 ^- _" l以上为1分半钟。有些国家以飞行高度层200作1分钟和 * ]# O, R5 p! C1分半钟的划分。 ; l2 n6 f. b" O0 C8 @$ }; g$ xra ' C" i/ C2 c7 c8 c( w3 L. im$ W, Y8 `" G3 Y! w) ^ speed (u * x j. _! |5 m9 m. F% ?5 qpoint on& ]! \) a' h, s6 J radius ex( |3 i6 u3 t, ]( s0 s: ]) _# | designed to expedite aircraft turning off the runway a ! T! h, [2 w' {8 [3 w' Z) vlanding, thus reducing runway occup 5 b9 e4 S0 U( m% nHOIST, A device for lowering and lifting an engine o8 h) h7 d8 P" D* S h 3 a g+ B* n" S$ d; a! U0 G, v* ga 1 U: |/ }9 b u) W9 o: t# O) GH9 ?% M% D- E3 N8 R" R$ a8 Q( K p+ ]2 X/ L5 ?5 h+ e' U N H) S. C- g0 E8 w: ~" L5 ?* p7 L which keeps aircraft within a specified air space while: u" R _. b+ O% ]# y$ R2 M' o awaiting further clearance from air traffi ) `, T. x7 E7 cH * }! `* E: s- x" Om: H+ [3 t7 c: N: S: I a / @7 K G4 \" u; y, tc1 `) A& `. R, | s a/ g: A# j2 @4 {5 s- a* a w : k" f' N) l/ ?! {/ t2 b7 |T6 z- w4 u% F) ?) A$ Q2 O 1 5 u v! G+ x! g/ Ps" Q. o9 q) e' o: \5 k" E' T some countries.* k9 b7 _3 C) }) Y( q2 V" [, s" k 高速滑行道/出口9 z7 @% a9 K+ L1 t+ @ 是一条半径大的滑行8 _& I9 l6 {6 ~& e, N9 s# L/ k) ?) x- [' n, |4 M$ b) k. R3 w9 Y* S. a+ m7 @' f2 ~) [( t9 B- z5 }: x+ O; A5 S' b3 {吊车,( e; ~7 o: V( U6 O 在发动机或重部件拆卸和, V u r$ ]) j1 V0 v( r" O8 x7 Y8 V; f h9 @1 T+ }! J7 ^7 `" {( z/ N$ [# p( Q1 l$ Q" h6 S U- f使飞机) x% E, w! v! s+ m F. v 的预定机动动作。- I) w" ~/ p* p+ g 1 3 W7 ~ f; G* i英汉对照民用航空词典B OEING `7 T [+ b% H6 a4 D TECHNICAL DICTIONARY 77: Y) r* K" `5 W" T HOLDING FIX, A specified fix identifiable to a pilot by3 \; s! e) g7 k- Q6 T NAVAIDs or visual reference to the ground used as a 8 ]( L2 V; {- ?: W3 @) oference point in establishing and maintaining the $ {( E, O& K4 U( B- rosition of an aircraft while holding.( D' u0 @- p% q: w! @8 ~ OMB, A hexagonal material made of metal or4 [7 q o0 ^3 W3 N omex for sandwich construction of panels. , w( t! F( M6 @) uHORIZONTAL STABILIZER, The moveable horizontal 1 ?- N. A4 i% [7 Y, W' S) q5 Dsurface of the empennage used for pitch trim.5 r$ E( n3 v$ k" D$ A HOT BATTERY BUS, A battery bus which is not7 B- R" i0 y+ U' P- y switched and is always energized from the airplane- R7 w+ j* `# Q: B$ R9 I7 j battery.& S( ~, l# Y! E7 q 使用的一个指定. P/ t: z- m* g0 }- O$ K8 O( X2 i9 \ 位点。飞行员可根据导航台或地面目机参考识别该定位! |2 h/ C5 O2 W7 ~1 c# d7 y! w! {4 S, G9 @% y5 |3 o窝,2 s0 [+ R7 g1 F" k9 i. V9 Q 一种用金属或Nomex制成的六角形材料,用以制造夹芯 * H1 r& ~1 o. _. Y! A6 F% T8 Q$ I板。 # y/ i4 e4 R) w# C6 o) L水平安定面, 0 [& O% d: r* {, v* Z. M' P8 B飞机尾翼的可动水平面,用来控制俯仰配平。 & L y% D' m3 Z, T" ?& r热电瓶汇流条, + X6 g+ X2 u1 X$ T6 O无电门控制的电瓶汇流条,始终由飞机电瓶供电。 ' n7 G/ w ]0 A( p/ ?+ H4 Rre5 w ]4 t6 U, Z1 e, a4 ? p ' F9 _- z7 C2 fHONEYC+ D" Q+ {% r$ l: x N; ~6 z v* e$ s2 _+ i9 A 等待定位点,- {$ U8 G6 l! }* l7 Z8 L, W 等待过程中在建立并保持飞机位置时# b) D. h: }7 [9 P. ?' a: @: F' y$ B' ?% K! o' k$ ?+ g$ h, I: C3 o6 C% p& g; D% X7 X. I, q0 p8 |2 q+ p7 m8 {8 X; E- a, q) Y, Q英汉对照民用航空词典B OEING H+ ~! ^" j$ |7 q s TECHNICAL DICTIONARY 78 7 o+ I# d. h, F$ l& m& ?6 C/ qHUB CAP, An external covering to the axle of the main8 y( M4 @8 Y" y/ _3 j, @0 i landing gear wheels./ a# ~) \' i. B% y# U7 P HYDRAULIC FUSE, A device in the hydraulic system: o4 P, B5 D! D* G4 m r stopping fluid flow when a leakage occurs in a line% K& S' C2 g; Q ownstream of the fuse.$ G% x1 H' _! M$ u4 L; O S, SEE - INDICATED AIRSPEED- b( [4 f& k/ Q1 I9 l8 y ER PLUG), An electrical device for# [; @6 M' q3 g2 e+ X# M/ f producing a spark in the combustion chamber.6 K& [" o4 }! L3 U: Q% Z9 z 压保险,. ]/ G" I! C! ^. N 液压系统内的一种装置。用于在保险的下游管线上发生8 s, }* ?! _' G5 ~+ C 漏时,阻止液压油流动。) i. r& x7 |. O 示空速,% L3 v, d. d* n4 Y5 \& y 见Indicated Airspeed / h! U9 c: J kfo x% Q9 S, c) o* a) w3 D1 b# jd ' s! @: {* K# \! \5 x. w MI IA, E8 L; ?2 }; p/ p IGNITER (IGNIT* Q' g& f# @( u0 N/ o9 `% q8 q- y 轮榖帽,* Z# g o1 @% H1 e 主起落架轮轴的外罩。7 b5 H* a! a0 t7 b5 }- n7 i, \+ Q& S L, e+ U. z6 F6 l4 ?; a( v" ~: V7 W# l! b; E$ o0 y) {5 \9 J! @6 ?/ \2 S1 A) g0 K0 D+ J' {, P在燃烧室内产生火花的电器。 ' d" E# O6 S" x5 w点火器(火花塞), & X, e# v+ u" a) T& h1 T4 b英汉对照民用航空词典B OEING 7 U9 c0 h5 t: |) c/ k6 YTECHNICAL DICTIONARY 79" n9 y( ?& L, G- T0 w E0 ^ IGNITION EXCITER, An electrical component for* z+ r; }( k$ [4 L; Y( } supplying high voltage to the igniters for producing a # `+ X& P$ V5 d3 B% B5 @spark.+ x! k9 @3 _2 r/ m2 y5 `# a- I IGNITION SYSTEM, A system for starting or continuing % q4 }5 {, M f. m1 R& R& Y8 Wcombustion of the fuel-air mixture in the engine% y9 S- D9 x5 \% s2 K& M e combustion chamber.. J D! V* L8 \& t" K% L+ I S, SEE - INSTRUMENT LANDING SYSTEM # N4 C5 z' O7 u+ r/ z, P, Q3 G" `PROVED CLIMB PERFORMANCE, The rotation and , x; P8 k6 Z. G. ~" n6 |+ wlimbout speed increased above normal to increase Z! d0 }& @. m: D) ^/ O DICATED AIRSPEED (IAS), The airspeed read $ M$ y( t1 ~9 ?8 Q& |3 v5 s' ~8 Z火系统, 7 H9 v( c" h/ r一个使油气混合物在发动机燃烧室内开始或继续燃烧 " q/ ]3 l! x9 S0 [' R" M! ?系统。$ y2 x! c: t' r5 [8 {# r( l 表着陆系统, : e& ~: w( V/ r2 \) Z, N1 t- Itrument Landing System: V, d) s. \. y c( [' T# D- v, c- O ILLUMINATE, To turn on or to provide light. 6 e! c3 S" Y/ C$ Z- tIL/ N, r" k$ E D) Y4 n) o* E9 P IM6 W: M$ K% Z6 [ c " t* R+ n/ \9 H+ g" Q. Uairplane climb performance, especially if an engine . l# I; x$ q, f( h6 G0 l9 bquits.9 e( l; u+ m7 z IN . G- `, [- R7 u! c0 t9 S" h( ?directly from the airspeed indicator without any & t% n; S, u* g$ f% Z3 tcompensation./ h' A7 I9 y7 j: ] INDICATOR, A component for showing quantity,# A9 y- B {9 a% G9 o pressure, temperature or position by a pointer or * J9 l* [5 S# ^0 bnumerical display. (Similar to gage (gauge)).7 g( V; {% ]5 y' { g; l 点火激励器,+ \; o3 g5 n, V. k4 N4 F$ Y9 u 向点火器提供高电压使之产生火花的电子部件。7 w5 Z, C# H7 ?9 f! L& {& C9 Z- x* s9 }% D3 E, i3 }; L0 |4 {4 q1 u: W4 ]& F6 D 照明, / b+ n8 C3 f) ?打开或提供灯光。# p/ a: i+ y9 ] A. k/ X% D. v$ C0 Z' u6 O2 J: J2 T 见Ins . ) A8 v7 r3 B+ O# P7 q8 T, ~* I, @进爬升性能, 4 p3 S, D" c+ N" f/ O R/ i用大于正常的抬轮和爬升速度,来改善飞机的爬升性& y* E. A. r" [" A2 s 一台发动机不工作时。 o# \" F0 Y" l; @* ~+ J示空速(IAS), " W- S; }$ R0 O( y6 A9 J3 M" ]" ]正直接从空速表上读出的空速。 $ b. [* p, i, v, b- O K指示数量,压力,温度或位置的部件(与) b% _, w6 z' I- ^4 S/ [ 计量仪类似)。 & m8 c% L3 D0 A- m% \9 L4 I/ K! ^/ F$ @; Q: d/ b+ C9 M能,尤其是在 ) R( h. R, f- ~3 @+ a- i* { Y- |$ M3 Z8 K8 ^- F, A 未经任何校+ j6 t e9 }+ q. c 指示器, / V) i, g H& w0 l% G) B2 F2 A用指针或数字来* C: B9 V ?& X, j1 } 英汉对照民用航空词典B OEING8 D) k! U' i! W+ U8 j, m& G& Z TECHNICAL DICTIONARY 80 9 G- g- A7 P5 c8 hINERTIAL REFERENCE SYSTEM, A self-contained,5 U; e0 d$ @7 r, I" H' y; _+ t navigational system based on the measurement of 6 j' j0 Z# W7 Dacceleration and attitude. + f0 N$ J7 F l# R7 pINFLIGHT PERFORMANCE, The performance of the g- u Q3 R W! ~* T# ]& C- Q9 @ IITIAL APPROACH FIX (IAF), The fix which identifies8 ]7 s) o2 w& R2 l2 c$ Q e beginning of the approach to an airport.( F5 l$ T a, f2 n0 f LET GUIDE VANES, A fixed set of blades in front of . n: Y& j' t: b# _n engine compressor for directing airflow to the9 w$ B6 j6 v1 E! j ompressor. 3 U0 B# R1 x' k# `! F$ tNER LOOP CONTROL, For autopilot operation this is# b* `! r4 j( D& w+ ]+ c e basis control of airplane pitch and roll attitude & l+ w( O% n9 |, N" n, H$ c- X中性能, ( x2 ?; C1 W/ L) K飞机的性能。5 S5 {( a8 m3 _; { 起始进近定位点(IAF), * e6 S4 a' Z+ Z% Y. J标志向着陆机场进近开始的定位点。 ) L% a0 {: r* K @# [进口导向叶片," C( _/ B* s& v8 W 发动机压气机前的一组固定叶片,用以引导气流进人压 3 V! t- p( G- ]1 }3 q5 M气机。+ u5 l% l+ h2 s' C8 ^ 环路控制,/ \. [) n# S: N9 ?; `# R: A 对于自动驾驶仪操作,这是无关飞行航道的飞机俯仰姿 0 E" P, @: I9 M制。3 b1 _ d7 N% ?' j/ R( O z9 X aircraft while enroute. , U* I: }7 j }2 e) jIN . b+ K. f0 [, P8 {9 Tth* f8 {/ S1 ]) d4 s1 Y. f: k IN. U- v! h& F' m' ? E$ x a 2 o( ^, a6 h3 {7 J2 P9 K9 ^2 Jc( y8 [1 F. ]0 Y% I# A! m! Y# v IN' \2 s0 J6 ]% A- J, n: n- ? th/ D; l8 R2 q' S without regard to flight path.2 H- Z& o- k% k' d% ^7 O. w6 g: a 惯性基准系统,3 P5 o6 }" t/ U% G* W" g 以测量飞机的加速和姿态为基础的独立导航系统。" K+ m. {4 f$ {5 Q, ?9 ^2 a, Q2 M2 F1 f/ z. u2 P# N. y飞行中- f5 l: v8 n1 }) g" g1 W% r9 c2 y* @/ x1 s- Q态和坡度的基本控 B7 {, c8 \6 `6 O0 F英汉对照民用航空词典B OEING % e: M9 z. [; `" g* H: J Z* n9 Y4 UTECHNICAL DICTIONARY 81 1 i" S* R1 w" ?3 }1 uINNER MARKER, A marker beacon located between . [/ m1 r! k% @6 q9 a8 Tthe middle marker and the end of the ILS runway.( V) o6 P( @$ [ K# f1 B9 `! O! T OP, SEE - INOPERATIVE , o0 `4 [2 |9 J7 S7 n# VOPERATIVE, Not working or operating.+ U0 C4 H1 b6 U* Q; F# a$ ? STRUMENT FLIGHT RULES (IFR), Rules governing4 Y2 Q7 F8 W: g6 t e procedures for conducting instrument flight. Also a8 P) g& Z6 r4 Y H rm used by pilots and controllers to indicate type of . r' d6 m7 P6 D! xight plan. , F+ t$ z* a/ H8 R6 D+ A! CSTRUMENT LANDING SYSTEM, A precision 8 {$ g$ p+ D( n) z# _; r- O4 I: W; fstrument approach system which normally consists of7 a% U- a2 g; V e following airplane components: localizer receiver, " t5 |9 Z0 Y7 C) \/ vlide slope receiver, and marker beacon receiver.3 c( I0 F1 t0 k$ r) l N OLOGICAL CONDITIONS 6 y# ~+ g }) r+ wMC), Meteorological conditions expressed in terms of : e3 k- f4 z2 _9 Eisibility, distance from cloud, and ceiling less than the, b, ^6 n Y( } inimums specified for visual meteorological1 F1 j: S7 J0 L itions.5 M! p# x: L0 P1 q Q9 T STRUMENT RUNWAY, A runway equipped with% R2 x* |5 L( N: _2 x$ b! U4 f lectronic and visual navigation aids for which a 8 }* X+ k: ] f, X. t$ y5 {) grecision or nonprecision approach procedure having1 n0 [2 L, I2 j. X$ }2 ^ 间的信标台。 q! k3 I, m' U0 G2 d 不工作的, ; E1 z: J+ {: I' L- j# b; ~# O见Inoperative, {0 i `8 B: {0 F+ i6 b% t IN. k0 @& \/ b+ S" I/ k: ] IN) t* {1 j0 i5 u' n IN 1 r! n' D! j( N1 {" L- g* v& |th 0 |# S$ t( ?' Q" b9 jte, k5 @" x0 B: [. q' V/ h6 W( [+ X9 ~ fl - }/ Q* r3 Y6 o% G/ ?IN % e( \0 P- ~) l- X1 F# J z+ oin + J+ Q( q8 L0 C: [th5 X: o+ A' R( Q) V g * \) t4 c& F$ @' DINSTRUMENT METEOR- Y A2 A* B' E3 j2 @% j (I$ |' m; |6 \% h& _ v + T. |' [4 _6 rm# {( g2 S" _, [& P2 o cond& m: z) E3 h8 N+ _7 X6 H IN1 v8 b+ t0 g; |9 Q$ W) Z' |6 T% G e 5 t; ]) o2 _: T1 ^4 p \p ) v/ \" c$ X% W i s2 }: Dstraight-in landing minimums have been established.) b. J7 e6 J* F& N7 K1 u 近指点标,# [: [; H; y$ d8 N 位于盲降跑道头和中台之: G' t9 g% n5 S8 ^! S7 v- Y6 {# B3 O+ l# Y. p7 c8 g8 N" W不工作, 3 o' q3 ?3 y9 m. [/ K& g不工作或无法进行操纵。9 U: i$ h5 b2 | 仪表飞行规则(IFR),* G1 k0 M/ C$ ?7 M. ~# B. \! J. s 仪表飞行程序所需遵守的规则。& X5 y# O# S- g( f! D! a 仪表着陆系统, $ n% Y0 E* o* @8 O- N' l6 ?一种精密仪表进近系统。一般由航向道信号接收机,下 * Y% u! {$ d- ~滑道信号接收机,和指点信标接收机所组成。 7 z& N# r" F# }- x* W以能见度,与云的距离,和云幕高低于最小规定的目视! D" k# U! q# q. t/ z6 q& Z) I2 b 象条件的一种气象状态的表达。& U8 {( t4 e: G, r4 i* W 用于以精密或非精密进近程序作订明最低天气标准直 % t8 v- T/ p: x& r着陆的装备有电子和目视助航设备的跑道。6 O6 ~; e9 n) d. Y 仪表飞行气象条件(IMC),, [1 a% ?! I0 {; [ _8 J" m6 T4 L. s' z8 G+ _仪表跑道, & ]/ f7 [$ E1 c( Y% D线* j5 E: K3 g6 D. ? e2 S 英汉对照民用航空词典B OEING# [8 b3 i9 P" B6 k9 O1 y; w: b' X- [. w TECHNICAL DICTIONARY 82( T3 K2 _" ^' g INTEGRAL TANK, A metal container formed by the % s# s. v9 _0 S" D4 @ qlane. + _" X, D3 m3 n0 ycted ) D: E R) ], E: r" p: kcircuits. " h) O0 ^! g1 M: fManual . }( l5 F' E9 V( ^6 \# l9 ~0 Q1 Derformance data providing range as a function of a9 w3 T5 J1 n0 t7 A; l0 w7 l hange in airplane gross weight. $ q8 Z9 N/ B( T4 X" F! nTERNATIONAL RESERVES, Reserves required by 3 |( i! `7 p k$ {( T3 {, ke applicable governing agency when flying . v6 q3 r4 S) R; O4 t$ q& dTERNATIONAL STANDARD ATMOSPHERE (ISA),, c+ E3 E( o i0 K8 t+ { he hypothetical vertical distribution of atmospheric4 c& q3 G; X8 j, D4 Z8 u mperature, pressure, and density as defined by the& c& U. A t" J |' l& P1 R! K' h' f ).' [3 ~8 z, }+ h' R/ N TEGRATOR, An operational amplifier whose output o: T7 h4 E( ~' a7 D; u. foltage is determined by the input voltage, the input* {0 i8 V4 j1 U P% [) x: g! y3 o8 X存燃油的金属容器。 ; U0 Q# `9 P' B. o3 w% f4 N6 G- O: O' T+ x! n+ k- Z飞机总重量的函数提供的性能数; R5 h* L0 g: L5 q2 ?* Z0 o0 c8 h2 S, P% |) N! M际航线备用油量, ) P) |" y/ n9 d% j在国际航线飞行时,有关的政府单位所要求的备用燃油0 Y! x% g! K" Q7 T- S 际标准大气(ISA), 3 L$ g! |* y0 J1 g A国际民航组织(ICAO)规定的,一种只在理论上存在5 y% T! t; W! r) K) Q) @2 J+ y 大气其温度,压力,和密度的垂直分布。* C) x# H Z" R 分器,. r: I3 ?- U& I( U 由输人电压,输人电阻,反馈电容和时间微分而决定其 : F2 J3 |) |8 U. ~4 I; H4 G6 ?, n运算放大器。 - a% @8 j$ j" u/ i6 E' I" y1 bwing structure (spars, ribs, skin) for storage of fuel on8 K( |& d5 y/ y- P6 t the airp" Y- p$ ~0 h# ]7 R' Q. a& V! P# t INTEGRATED CIRCUIT, A small piece of1 q2 k6 j+ A/ Q semiconductive material that contains interconne8 {5 A1 f+ p* p/ L: }' b miniaturized electronic5 U2 S$ \$ t3 w- U- D) o INTEGRATED RANGE, Tabular Operations1 R5 n& l3 H. _, N( C p! Y$ F0 c, E4 ~3 r. o7 y# Q# ^5 U c. R/ q$ q% q0 z j( Y( c ^( h IN 0 w$ H6 }( r' j6 W {. E. zth5 I3 `& R; S, {: B6 Y international air route.4 M8 p4 h! d- {7 Y, s IN% G9 y; ~2 @8 t( l$ \ T ) s/ f. w4 t2 p+ Hte $ C* p) c- P+ W" nInternational Civil Aeronautical Organization (ICAO ; a |" P8 j+ _& E+ g- d7 mIN 9 M+ f" q# T' Bv( u! `4 q$ `4 M resistance, the feedback capacitance, and time ; K+ L3 W! A: @ ]differential.: b4 _! k: m0 N- p' s8 ? 整体油箱,2 B8 v4 ^+ h8 n8 S2 `. h4 T& Z 由机翼结构件(梁、肋、蒙皮)组成,用来在飞机 1 W$ G4 h4 c4 D0 b6 {! n$ m+ h; q* m% ^3 ]0 C6 b- P 集成电路, ( x# @2 n% t- {6 r% I+ k一小片内含相互连接的微缩电路的半导体材料。( @( Q1 O3 H2 X$ M+ E- N* [% s 综合航程 2 s/ F* S9 x4 i- O6 c8 ?* w0 [2 r' a1 s使用手册将航程作为* F5 ?: I2 L( `7 ^: H0 `. v! F: Q. J9 V6 B) c6 [! U) ?7 l6 o0 ?5 N2 q* g 量。! o' w k4 c |8 N+ i& ~1 ~0 ^! g$ P! P- C* U2 }$ P2 o8 E4 k D, I! E/ C8 T9 f* L' E' v/ Y输出电压的+ m9 w) k5 z. n: f 英汉对照民用航空词典B OEING 8 Q% B/ ]: a) `9 X6 j: M" Z2 r& XTECHNICAL DICTIONARY 839 Y% |' `0 a& V+ I$ p ?% o INTERLOCK, A wire connected in series with an5 _% D, X7 q4 W" k+ T+ ? D equipment or device, or a condition that allows1 T- |% A* w* O, c% Y5 T operation if all requirements are met. 3 q. ~' ^# X7 \: r, if the United Nations whose$ S( X% j% V" G8 d0 E I bjective is to develop the principles and techniques of/ y4 E" e0 _, W ternational air navigation and to foster planning and; v. @) ^6 A; @9 m. T Q+ c evelopment of international civil air transport.4 y' h2 n: p" Z' ?+ d, K TERROGATOR, The ground-based surveillance# {* B( L8 m& y% C dar beacon transmitter-receiver, which normally scans " F1 S" v# B v A2 n0 A( Oll ' i4 k. N6 i1 q# L8 l9 O% N7 Don the mode being used to reply. The* Y6 r& O1 M. k$ k) F; J" W" v X plies received are mixed with the primary radar, R l9 j. ?- A' [+ } turns and displayed on the same plan position radar7 n8 `1 i/ A; _+ D cope.0 g8 M; ]7 s, d TERSECTION, # P5 `0 w3 ?% J% k, Q6 G1. A point defined by any combination of courses,2 d% k0 {# M: w8 _, @2 I7 i radials or bearings of two or more navigational9 ]" p9 O* z! s$ x% H* C: w aids. 9 O" N# N2 \6 U1 Z, P2. Used to describe the point where two runways5 ] {* x9 s' G8 m# U: L cross, a taxiway and a runway cross, or two0 \( ]0 c) d% x$ X, [; F taxiways cross.: ?8 W8 P u. F. b cy)/ V3 F2 u3 e% l6 r2 ~ tem. 3 Z- P% A4 f9 L3 Z0 P0 |/ U6 ~5 N3 w4 h( ? ? 当所有条件都满足时才能工作的状态。 0 k5 J" P' h; I4 P( x组织, " U0 K$ D& b" L7 g0 }: t航的原则和技术,促进国际民航- t- n( {( I4 ]5 W# } 输的计划与发展为目标的联合国专业代理组织6 U3 {( O, G) D+ s 问器,0 Q9 h: c3 g( r/ S' ? 一种地面监视雷达信标收发机。通常在工作时与主雷达 . [% g9 j4 h: Y( j3 z' T连续的无线电信号,不断地重复要求与* ]0 i' d- H" u/ \ 接收到的信号相混合,显示在同一平面位置的雷 ) N4 G7 U) n- |/ Y, T: ~达屏幕上。- r) O* i! A9 V9 A 交叉点, . u" F, G/ z* v* d1. 由航线,径向方位线,或两个以上的助航设备! K( a: _/ a7 L) o5 I1 T 的方位交会而确定的一点。 % L& b* L/ ^3 F2 Y2. 指两条跑道的,滑行道与跑道,或两条滑行道5 j2 i# b; D" Q: K 的交叉点。) t- r6 W" t* h* h& u5 L8 x$ A' b INTERNATIONAL CIVIL AVIATION ORGANIZATION,* [9 X; ~& d2 s5 [! Y% s0 R- y6 i6 v! @ A specialized agency o& t/ P/ A8 c- I+ v/ S1 ]7 C o ; ?# P5 d4 C) S1 E3 H, f" Rin! ?! {) W; i8 s5 f8 W' J4 g0 t d 3 E% j) l$ H( Y+ gIN - _4 W6 {( ]9 \/ H5 lra$ `& _) x* y+ ~; ~ in synchronism with a primary radar, transmitting' U7 L* j6 Z3 v4 m# C) c& C0 v discrete radio signals which repetitiously request a # h* [* Y- x- x4 k2 ~transponders + u" G( y0 ? s3 m, Vre# D2 {6 i5 n' e re $ K! H2 [+ u4 z8 }$ T4 t, v' Gs& d7 C3 A2 c5 I O IN : V7 ^3 L1 z. @; X7 f/ UINVERTER, An electrical device for changing direct) k/ A% i. O6 ` u r current to alternating current for standby (emergen 3 d& q* k; Q1 g& \9 x5 ^) `power supply to electrical sys2 V/ L& W; z. N; e6 w! B' } 联锁, # P% H# S1 I+ g一个以串联方式将仪器,设备联接在一起的电路。或 3 }! [! e# Q' g+ J$ h& D _$ e5 `: \! `, E8 F1 k国际民用航空 ; ?+ \ D! |+ X, B9 i一个以增进国际航空导9 l: s/ q5 W, y8 T, T. q! n/ q6 Y3 W: d8 f8 f+ |9 ^/ u1 ]9 `1 ?' ]) y同步扫描,发射不 ' F% ?4 A e6 g8 o, q其工作方式一致的应答机进行回答。所接收到的回答信号 : @5 P1 u# f+ B' b: n与主雷达 6 R8 h9 G: `; P! s+ S变流器, 0 Q- I. i# i5 @0 x) S用来将直流电变成交流电;以供电气系统备用(紧急) 3 w8 ~$ t7 A( {: L( n电源的电气装置。 ( N* w0 R6 h0 N- p. U r英汉对照民用航空词典B OEING' p4 w- b" r! @! p4 ?* G6 S3 p+ C TECHNICAL DICTIONARY 84 / o2 i% S- l I, r3 U# z2 g/ y- I+ t# [IRS, SEE - INERTIAL REFERENCE SYSTEM8 B$ i X$ D( {$ ]6 S ISA DEVIATION, The amount of temperature or ; t0 Q; M0 }( I- z, V: A5 Ysee International. J8 }- U# x& z* ~+ I) `* G tandard Atmosphere). - p$ q ?# K$ SLAND RESERVES, Reserves required by the 8 U1 N) @4 d- a p" g8 {) X) A% gpplicable governing agency when flying routes# e; C) b/ E1 R, _ etween islands with no alternate airports.% Q" P2 w! I) ~$ w9 y CONDITION, Cabin pressure (altitude)9 H8 i! r! W" ?( s, K maining constant with changing airplane altitude.1 f* j2 ~# f+ b8 c ising the9 A) d6 G0 _; e1 N$ J3 h$ A$ U a: p/ C7 m4 ~$ y- G, k8 ^* H$ ]' g6 x& u" ?pressure difference from ISA ( + I; A0 W S4 B) y0 v4 m3 D! CS : L+ [, q- @ qIS 7 F9 j/ ^- a) z1 Ma ( W) a9 ?. x. j& ~# i7 B- {b) B$ Y5 `) A( g+ X' ^ ~ ISOBARIC 1 z5 M2 V! Y$ D1 c- Z' V9 [/ W! ore. h& J: ^8 {9 \; v0 l; G3 S ISOLATION VALVE, A valve in the system for0 ^6 I# T4 K2 y+ y separation of the system into sections. " f+ y$ |! `! A5 U f+ lJ % H$ D* I3 B7 lJACK, A mechanical or hydraulic device for ra " f7 J) {; S3 a8 j" }airplane.: d, r% X* {) @) G+ l8 G JACKING POINT, Location on the airplane for using* _: Y4 j& W5 @2 s! o jack.5 _" v/ q4 i Z: Y& h+ i/ }% g 惯性基准系统 " o4 p+ j7 C2 o2 f- h见Inertial Reference System. # @7 y5 w) n" r8 f* n与国际标准大气之偏差,1 h5 P2 C& [( {+ s9 @$ X* t 压力与国际标准大气的差值(参见国际标准# G8 j3 A# d6 j. _) r' o' G 有关政府单位要求在没有备降场的岛屿间飞行的飞机 4 A% w" c5 }) [! b" j8 C6 z带的备用燃油量。1 Z2 p A4 U# `( n 压状况,) o O" ]) M8 U$ \/ { k3 P! X( y 在飞机改变高度时,座舱压力(即座舱高度)保持不变 % u( x+ X7 ]" |/ ]5 ~状况。 & I* a: h4 U7 ] L% s斤顶, ' `4 [. l: J( _, a# u3 a7 J+ Z3 |用以将飞机抬起的机械式或液压式的装置。 0 d- U& ^% E" J" a; ^$ h! s温度或 + u/ h( l$ e8 Y" H8 X) P/ P大气)。 / `" u4 L" N' {7 e2 U. ^5 X" Y岛屿备用油量,1 T* E: \3 T! ^- E0 I! v3 F9 K# i4 s2 o) ]& j6 B. x4 Z" r9 k% O8 p0 ?( C; \5 r6 w7 l& E6 S5 p 隔离活门,& {' P3 Q$ q3 k 用以将系统分隔成几个部份的活门。; v" ?6 v& F/ q' \% Y5 z/ a! _" P3 T- T& S7 @, I( x& A千斤顶支点, 1 C; u( J: K1 B: G飞机上可以让千斤顶吃力的位置。- v3 P' r% m3 E 英汉对照民用航空词典B OEING5 v. x' `: q! b. T TECHNICAL DICTIONARY 85# q5 d) D5 w8 |' j- S4 z: L7 G JACKSCREW, A rotating threaded rod used to drive + c) V2 r6 w% Omoveable component such as a flap or stabilizer.; S$ |9 Q( D* K B. N a 致动螺杆, , u3 u6 P' p9 [用来使可动部件如襟翼或水平安定面运动的能够旋转 6 q! t0 O8 N9 w" i% H: T的螺杆。 5 E, _. r- o/ [& T' R2 v英汉对照民用航空词典B OEING x, K l5 o0 R7 [* E0 r) o2 PTECHNICAL DICTIONARY 86( }* W! `* B h+ K JET PIPE, A control component in some valves and7 e+ R+ f) @; g a7 g: _ ET PUMP, A component in the fuel system, operated + s$ C* x; q. y- Or removing water and fuel from a fuel % O9 i( Z3 l; I4 E7 ` _nk. + R4 f4 L9 e! [! U) G q. v射泵, 6 o% {1 V) c& h8 ~2 B! a$ x内,由燃油压力来操作,用于从燃油箱中排除2 x; e# G. t* q" L" U3 x% _) P 和燃油的部件。" Q2 R" c2 _9 P; f- `, k; J1 P) s actuators for controlling the flow of hydraulics or) }% H2 ^* `) ]% L4 |5 Q2 L pneumatics.8 a/ _8 y4 P; D J. j8 L7 e" s4 a! g0 w3 R+ p$ a by fuel pressure, fo 1 i7 `+ ~) C- T0 L7 @" G& ` Kta # W: s2 R7 K' t喷射管,* ]& V* Q3 k0 C 在有些活门和作动筒中的控制元件。用于控制液压和 0 @ L, ~' m, p- J# O1 ]气动的流量。 - v, h+ x5 z; d K0 J6 M/ T) e( l& d; ^5 A8 x% ]$ r9 M* U燃油系统 ! Z; m+ o, d/ b1 m: W% f# M. P, A, A3 R& I" ^英汉对照民用航空词典B OEING + H8 r! `. L; N+ xTECHNICAL DICTIONARY 87 - r. K9 p6 z- ]; B8 i) EJOGGLE, An offset in sheet metal construction2 ]& s% j4 s% ?3 ^1 y+ T designed to allow one piece to overlap, either higher or$ i I5 {6 x( F wer, the other piece.1 o3 m8 B! u2 B5 V$ | OULE, A unit of electrical energy of 1 ampere of 8 W) L2 Q9 j( b) h+ @urrent passing through a resistance of 1 ohm for 1 ) p, X' [% r: Q4 V! y$ Uecond. Ignition system energy is measured in joules.0 H+ O2 q, J' t, b UMPER WIRE, An electrical connector for temporarily& r% } S3 j2 I3 R$ n ypassing part of an electrical current. : e& }' y0 v6 U, g- wUNCTION BOX, A container which serves as a joining' e# g& t$ Z! U3 j lace for electrical connections. May also contain ! ~/ U; C" m1 \6 N8 hlectrical components. / E8 s& g$ P0 mEEL BEAM, A structural beam in the fuselage center & h: n5 a4 W1 A9 P* K3 W& Y& vection (wheel well and under wing center section) to 0 L' @; _+ y! N9 ~$ RKEVLAR, A light, strong synthetic material for5 p' S( Q. j. O- R) G secondary airplane structure.4 O R x% B: z& C ,使一件金属与另一* s* u: d1 D1 Y& K 相互叠合。 2 [0 g* @' z7 R, @. v耳, $ T( J$ |6 A3 ^% a/ J' J电能单位。一安培电流通过一欧姆电阻一秒钟所需的电 % C8 I5 y E; ?5 `3 m) E7 @为一焦耳。点火系统的能量用焦耳度量。 : b1 A) `/ u4 p `1 M2 G接线,7 q. e( I$ J8 C" [) I( d" l% r 用来暂时旁通部份电流的电器连接件。 G$ I) }0 N, p! h 线盒, ( b$ t! ~" D) Q9 S ?做为许多电接头的汇集处的容器。也可能内含电器。 ' s# L: z; z+ ]% p梁,5 n/ l- W0 z8 {' \ 机身中段轮舱和翼下中段,用以防止机身弯曲的结构。 ! g3 U& A) S2 q. P/ \* G3 f" yKEVLAR,/ I" X( G2 L$ i* h5 L& Y/ c 一种即轻又强的人工合成材料,可供制造飞机的次要构 # C+ [$ \; |0 Z. \件。 6 W; @, t d. j* qlo& Y5 ?# D( X. t( }- [8 K J7 \4 z( W+ Z- f c & }- x* V+ |$ O, z0 B/ Is 3 Z$ f I) [* a0 ~6 Z& c: G8 FJ 3 ]- R% t8 W( ]2 ~5 Jb 5 r4 W$ o! u) x( bJ: L3 B2 K! n" k- k( F! ?9 E9 e4 l p7 F# X( h1 W+ a" p( D* ~% _ e& d. M: g4 l: \* U8 G6 s K) F, }, h8 M/ w& X, L- | K `3 e0 e0 I" F$ S4 a! w s* _- E T* ~, |9 [* y5 w2 L5 d8 `4 Q prevent the fuselage from bending. 9 ]! L* F* x. _折接,% f0 c! L; q8 I, } 一种平面金属结构设计的弥补法 % ?6 r1 i- e U( }2 _, j; C% S, g" L' b% x. f& Z; \* ?7 z& Z* Q+ o6 `' `' T2 [; n- k9 q: [" p+ T8 e0 H. _# a5 S/ g3 e K3 y( ]; t" j V$ {' F% G- }) R$ X% X英汉对照民用航空词典B OEING 0 ]: P, z M, q x, zTECHNICAL DICTIONARY 88 4 ^5 U1 w3 e& DKILOWATT, An electrical energy unit, equal to one* u8 y- I: t# ]/ e2 X! W thousand watts, for specifying generator power output. 3 c1 z: _1 ?; T0 v5 l1 MKINK, A sharp bend, twist or dent in a section of tubing, . g/ H. a5 G- r' W/ gwire bundle or angle stock.% e( h: Z f- E3 J$ P KNIFE EDGE, A very sharp edge on drilled or machined 9 S* u. N7 Q% H* Ametal which is usually the source point for corrosive " B1 h" s& ~& _4 w. Battack.) J; l8 L m3 w KNOT, One nautical mile per hour. ( q5 m A+ L8 P/ H+ B( aKREUGER FLAP, A type of leading edge flap that is1 B2 S S* K m fixed on the lower side of the wing and rotates forward ! P" V) c/ D8 d3 Z. l3 N! X# ^into the airstream.3 p1 N' G$ Y$ s5 j1 L% x KW, SEE - KILOWATT & v( g5 N) M$ V3 V* }% E! YL ! ~0 m4 ~- d) p# M8 \LABYRINTH SEALS, Rotating and stationary , U" P( @ i3 F' Z, I" a1 Z# d& z: t, Zoverlapping structures which utilize differential air % H& h9 f5 m+ d9 x! E' }pressure to form an external seal. Most commonly used# i9 `- D, E' U8 G+ L5 m! B in turbine engines. o" a, s2 h/ ^9 @( [, B 扭结, $ ?& y6 z8 E" r/ v2 y/ \在管路,电线扎,或角材中的尖角,扭转,和凹坑的部 $ C) P' {3 y! [4 d份。; s" Z8 r* e) \6 u+ [; x% m$ C( z q 刀刃, + P; N- h4 J) k钻制或机制金属的锋利边缘,通常是腐蚀的开始处。 ! S; C* O- ~/ t9 I节(K,KT,KTS),- L: X }6 q7 b0 w# L 每小时一海里的速度。6 d% C0 P' Z, o9 y* h) _ 克鲁格襟翼,+ M" |' X2 }( d& T6 ]9 l2 T3 ]" K 一种前缘襟翼,位于机翼翼根附近,旋转前伸。/ O0 M. N8 |& A+ K% e 千瓦, 4 b1 U; Y# N! v( {见千瓦(Kilowatt! M7 n' M+ g O8 d; ? L+ V 千瓦, * [" N6 B) J+ c2 f$ J2 C+ Q1 D1 H电能单位。等于一千瓦。用以确定发电机的输出功率。# J$ G- d/ p6 N& z6 b+ a# e$ x )。! t0 {- O6 i$ U3 f4 i) J 蓖齿型密封装置,* N3 z, N0 x7 B$ G, l: z 旋转并且固定的重选结构。用气压差动而造成外部的密* P. m1 w( A! i 封。在涡轮发动机上最常用。 $ [% m1 Z" W3 s$ T) G英汉对照民用航空词典B OEING ( m' i# l' F) O, y" d+ j7 c9 CTECHNICAL DICTIONARY 894 V& f) W" r3 g2 F2 B7 p LAMINATED STRUCTURE, Composed of layers of a7 I7 x [6 i* X# Y9 |. C n2 C ake a 7 G( Q; ^, V* L( Rht structure. $ A- r% l- I/ i7 v* |/ c- l2 s4 w.E.D., SEE-LIGHT EMITTING DIODE. 1 K: h6 f$ m6 L$ {3 F6 LANDING GEAR, The nose and main wheels with the 5 V9 Q! z0 Q$ g O$ X' gttachments for supporting the airplane on the ground. # R6 n# D2 d# @( ^LANDING GEAR DOORS, Panels operated by the # u2 I) r s3 F5 t3 f! u4 s4 Ulanding gear for closing wheel wells when the landing 3 C* o f4 T, ~& N7 ?gear is retracted.) M0 V) f3 k: j" y' \2 v+ Y LANDING WEIGHT, Gross weight of the airplane at the U$ |5 Z% |5 z1 {# J+ ^0 @ destination or alternate airport. 0 c% |, R a! ^/ s6 ]5 G4 e7 x发光二极管, ; o! O7 M2 u) t8 G) F; [见Light Emitting Diode ' Q: Q4 x. w' c j9 h8 U6 qcomposite material bonded or cured together to m 4 b2 ?7 w- O; j" c# c) b/ Z+ H( }strong and lig& n( E/ A) F: L" A. ]8 ]: b6 Q L6 n y7 @& R3 _! K5 E6 n5 a2 D/ ^( ?/ Z L ( f; X% [. |2 c3 w6 Y# Aa . G3 y: C7 _9 I: g分层结构, , q# c4 L) Y- D$ I& g) P# P/ d一种牢固而轻的结构。由多层的复合材料胶合或固化而 w+ d0 u2 d$ u 成。 5 t; `6 j6 l0 O1 ]8 y# }" [. D7 f0 a$ @: q$ o起落架, % P% t! D2 _, `; h2 h( p9 t s用以在地面支撑飞机的前轮,主轮及其附件。 * b, d. ~. A; v u3 l4 s2 \! I起落架舱门,# q* P3 B# ?1 ~ 由起落架操作,用以在收上起落架后关闭轮舱的面板。: K! |& j. s* l& \: g* k. C) | 着陆重量, 7 s6 h( o' E0 b: o: d0 ]5 k飞机到目标机场或备降机场时的全重。8 p2 L5 [$ Q* A3 f5 e/ ^* Z 英汉对照民用航空词典B OEING# e0 W! U1 w ]/ U TECHNICAL DICTIONARY 90 % O4 \% l5 I( R7 jLANYARD, A cable for supporting or holding pan / ]' Y! ]0 J2 G' f& Eopen position. 2 X5 X6 h# @* L0 x0 |" ]els in' T. }6 [7 J8 J, c) s AP JOINT, An overlapping sheet of metal, joined to the3 f" e* p" [& i dge of another sheet in aircraft structure. ! V) U6 z" _0 E' m: dASER GYRO, A gyro which uses two laser light beams/ i; Y T: }3 F1 ~/ n measure angular rotation. ( G+ W* b/ I3 G& z.. X% D9 Q0 k0 ]# v& w& n, E ATITUDE, Measurement north or south of the equator 5 L6 o1 D3 ]; @5 H ?s, minutes, and seconds. For INS equipped+ V) N! `0 q% T" f" i degrees, minutes and tenth of minutes. ! L/ o. M7 P9 l) a8 y0 q U- }l device for. R' m% A# Q: e3 ?4 l) d" |, z hanging stored chemical energy into direct current.9 j1 u" J% E+ j5 Z4 m ses lead, lead oxide and sulphuric acid.8 y5 v/ A4 R W! v; i7 x! C 搭接, ' y: y7 @) o) z飞机结构中与相邻金属薄板连接的重选金属薄板。+ b3 Q7 T d; P" A# y* Z7 Q0 j2 { 激光陀螺仪, 2 k, F I7 h/ m; c$ d. p" b一种由两条激光光束来测量旋转角速度的陀螺仪。. y7 ^. ^5 J* m2 W9 H 用以紧固或锁定的装置。- f. H. \/ n: N& ^ 的轴。 ; U. }6 }0 o0 j2 x8 c方式。% y, C: {# o9 x7 \ 度, 3 F$ A ?/ L" r1 X2 W H% i4 ~地球上与赤道平行之弧线。由赤道以北或以南度、分、& {) c/ p4 W' W/ g) } 度量。对于有惯性导航系统的飞机则以度,分,和十等 - | ]. F; C& K, _% k" ]' h9 c- x度量。 9 F$ y2 B3 `' ]/ S酸电瓶,4 a" w. ^7 L% g8 H8 A+ W0 G1 L 将贮存的化学能转变为直流电的电气设备。它使用铅, 7 h. z4 k% [5 O& h8 v* M化铅,和硫酸。 : V4 F/ u5 Z9 h( [9 \: e. ^! s( o$ b3 SL+ F0 z9 G2 v* E' J5 ^ e A) f) _% {# d L & l$ X7 M8 q6 c+ j( k' xto4 t1 h! t& I, }2 [" P LATCH, A device for fastening or locking.+ ]( V" T( l8 B. \; A1 o- i LATERAL AXIS, An axis passing through the airplane's, p& l G- O* N* _8 Z3 r# ~ center of gravity, from wingtip to wingtip6 i( H* o/ L/ v# J LATERAL NAVIGATION, An autoflight mode in which0 T; t2 Z# _( ~& i; g) v the FMCS is used to control the airplane roll. - a3 w+ f3 o" a2 L3 H4 X+ i1 E3 Z' lL 5 l4 d4 w) t3 v! [) qin degree) R0 M+ k- n' q% L aircraft in ; ?" y; m6 Y7 w% c8 K! N' D* aLEAD ACID BATTERY, An electrica d1 w: ]" o2 E. T0 ~ c/ _# }( a, Y, m* v& e2 I U6 L5 T" m# j: M! K3 l, q 牵索,8 @) `/ D$ `$ `7 @) J& G# |/ x' i5 C 用以使面板保持在打开位置的钢索。0 u: j4 d1 U- y9 S. E; W 闩, ' X# Y" y5 Y: p横轴, ; Y3 ]% v! b1 Q通过飞机重心从一侧翼尖通向另一侧翼尖 d. \; c# V2 j+ p" _8 ?3 q# J水平导航, " g* v, \( `6 v' _( Z( X' r! j! J% h8 E使用飞行管理计算机系统控制飞机横侧的一种自动飞/ R! ]/ a( ]' g# M. [& x4 n4 ]' v/ { c0 @) w$ M* Y7 H* J" y8 Q- w1 W2 T/ z: m L* t6 M' S6 j( u% _! I/ b; ^) ]- `8 @. {* N, }/ D, `. L% P/ D( x3 |4 g- S5 {, n9 Z% ^ Z- Y% \2 l( r+ l英汉对照民用航空词典B OEING 8 H7 H8 H L: L* _+ m HTECHNICAL DICTIONARY 91 1 A; X a0 T* t+ s1 Y( tLEADING EDGE, The front edge of a wing, stabilizer or A& N/ k" G* b7 y0 {* m. OED, SEE - LIGHT EMITTING DIODE& y p! G% y+ R' Z+ ?: M EMAC, Acronym for Leading Edge of the Mean 1 W5 ]: F) ?. ^0 p0 o" ]0 d6 I5 Berodynamic Chord. / Y4 q. v# k# _ n7 f7 gIFT, The vertical force produced by the airflow past the A' B l. m/ |" m3 N. Y& Ds of the wing. 1 I5 x( y: k V6 v7 eIGHT EMITTING DIODE, An electronic device which 6 b" A$ P: x& V4 y: w( j+ Utes with red, amber or green light when supplied8 c; C% o; @2 x# ] ctric current. I9 w+ y% F8 Z# V) @) K) Q: ~, V8 {: K! ^control surface.% S& O) [ U9 ~! ^; {2 _+ g- l LEADING EDGE FLAP, SEE - FLAP: `( h7 N; m N L: f" e! r; V* o& @; k5 R L 9 t& D- f# p* a% MA # k6 D: k; E& ?( m( pLEVEL-OFF ALTITUDE, Altitude of which the airflow 0 G! p- ]1 n# @past the upper and lower surfaces of the wing.2 \% P2 z" _" s+ h L$ T# n ^5 H h; E/ n upper and lower surface& E; B9 Z- |% v$ ? L l0 Y3 g4 ^, \8 B illumina ( w3 g+ k& [+ w! F8 {6 mwith ele 9 l1 s& S3 }9 x8 U前缘, 9 J( \ e1 W3 u: Z6 ? K机翼,安定面或操纵面的前部边缘。8 M1 _# |8 z/ H- d! k/ { 前缘襟翼 + i6 @4 i1 X" Q: L# X q2 c见Flap.7 x5 v) `! m! I6 s: C0 W/ t 发光二极管, : c5 ]& n3 I9 B* \: d$ W: [+ }ht Emitting Diode! ^, Q8 F+ K0 g$ q7 _$ p1 _ 见Lig . ( y# F4 b) }$ o% V! z( p; ^; s均气动弦前缘, 5 e6 z u, ?1 v+ F平均气动弦前缘的缩写。见Leading Edge of the Mean ( z* c! w' R5 H- A/ ?% l8 R5 y9 e; @6 ~" {) E" `* E8 ? Aerodynamic Chord. * t/ I( A: i* u3 Y' y力, 5 E A. U4 |) p# m R' \' x过机翼上下表面所产生的垂直力。: x9 j3 y8 v9 n: }7 J+ F9 O7 U 光二极管, . v) g9 g0 b( v通电后能发出红色,琥珀色,或绿色光的电子元件。 , V9 S$ ^' f) ~1 g i4 T; l: e, q* j% i改平高度,. k6 o# y! Y6 e/ H% ] 飞机因巡航时发动机发生故障而下降至的高度。 - d- v" L( O+ h/ i" b. o: N1 i0 ^. f/ g& g3 D) b2 W气流流$ U* k: e, q8 d- O& g* E5 ]" r# D: v) V4 |! K C( O英汉对照民用航空词典B OEING ! ~6 [1 d. H* ^7 m' CTECHNICAL DICTIONARY 92 Z6 z& `3 Q% L3 _1 O1 ZLIGHT PLATE, A component part of an instrument # P- [: w2 c2 o9 z! w, B" ^panel for illumination of words on the panel.# v! u; s: U+ b& a1 b& p* ]" b LIGHT SWITCH, A switch which contains a light. The9 }: q, V9 M7 i" I( B m opened or 9 X; v/ Y9 u3 M) {7 q Plosed.' A! J4 |. x* ~$ B8 g n electric actuator which turns off electrical power to & k8 w( U; G- i% U: n& o& ~e actuator when the actuator reaches its open or " l9 M# ?0 b' Z1 R slosed position. & Z4 I- C8 c$ z# AIMITATIONS, Performance and operational limits7 k9 p+ o5 L, b. c. L sted in the Airplane Flight Manual (AFM), such as+ U" d! u& c; f- k aximum airspeed, maximum altitude and center of # r: g3 g% c3 C. [6 zravity constraints.; ~. t$ a% K c, [& p- ~ y9 Q) a5 Z- x4 a D5 {$ K# N craft during line maintenance$ x/ v5 L7 v8 ~6 R0 g perations.4 p! r" f" m9 h1 ^& n ontrol+ U" ~3 _1 D: H% } display unit allowing control of information to and from ( t- M1 M `3 uthe scratch pad and designated areas of the display." H7 o6 P8 o" p* @4 g 光电门,- _: Q, w" t8 \$ k 电门开关而决定灯的明灭。 4 F3 T4 R1 f5 I1 \' H1 L在电作动筒内,用以在作动简到达打开或关闭位置 4 T' o0 }& G8 Q" ~4 ]5 a, A: q时,切断电源的机械式操作的部件。 1 a% x8 H$ Y) ^各种极限,3 c/ q( o* Y4 r3 n0 h8 l2 |4 q. I 飞机飞行手册(AFM)中列出的性能限度和操作极限,1 p6 z: C3 n) t6 | 如最大空速,最大高度,和重心的限制等。 ' W# s" N* w. b' l; B2 Y在航线维修中,可以在飞机上即时拆换的部件。 ) T4 C; N1 q! W' q飞机管理控制系统的控制显示器上的电门,可控制草稿 $ ^$ I; ^3 I8 c- C# U% h @栏和指定显示处信息的输人和输出。 & P' {7 d& n$ Y$ q2 N9 Nlight either turns on or off as the switch is8 P, w- @) R, Y# _' Y c ; ]3 O# ]* E' R- W% }. [. TLIMIT SWITCH, A mechanically operated component in " e* V3 ^$ f" ~' l8 V- za & T9 N; d: U6 d1 j0 y. W, [th 8 n, U: `% r% L" G% J" jc0 t# M0 b$ Q3 j1 c% w% j) a L. m" [) ^% ]2 C* {( o3 q li- ^; s( B% U6 \6 Q4 T m$ q# G% T! u$ z0 e" c$ s& g g ' A/ s( I- {/ Z3 {. kLINE REPLACEABLE UNIT, A unit which can be readil3 d3 |; g+ K2 k4 e changed on an air $ W5 P' I$ w( Z6 `2 M% po# s) C% |5 _$ l# H8 ?& e) ^ LINE SELECT KEYS, Switches on the FMCS c+ Q' E0 D! A! Z8 l a8 |# c( E 照明板, , Y/ o# O4 e4 _( l仪表板的一个部件,用以照亮仪表板上的文字。+ c F/ ?& z/ Z. g; [0 s$ H, J9 o' f( N Q" {" r6 r带灯的电门。$ u" [3 X5 w. c) f- D 极限电门,& g# X* O: H& C& q# ?5 o- P 航线可换件, 5 J. q( [/ G) g# m" P行选键, ; W+ C# }6 N( z( r0 A英汉对照民用航空词典B OEING# l+ y) J5 J, d* `' [/ A% r7 \ TECHNICAL DICTIONARY 93 5 x# Q) a- B5 W2 T% Q5 o J8 [LINEAR VARIABLE DIFFERENTIAL TRANSFORMER, 0 D# I" c# q$ B) E9 D9 nnsformer with a linear response. 3 L$ o- ~. `$ s [' jNAV, SEE - LATERAL NAVIGATION' \$ `# n! }0 y) p- X OAD AND TRIM SHEET, A form containing tables and " F4 s5 d$ J& u* Qharts to account for the weight and balance effect of all & {/ c) ~. t( ~3 P) jpe of an . {+ P0 U( V$ V( t$ RS approach, normally located at or near the point of ( ^/ q: s- V$ H9 Aecision height.. Q* R) H' ^' R& X1 N: w7 a5 r er t( A9 `: u+ a0 \( S/ Meacon at or near the point of glide slope intercept of an 1 n& C6 ]- n- kS approach. 3 B7 t. _1 U. i) X4 i% fich provides 9 [: ~8 t$ k1 z) _& `" p/ ?lateral course guidance to the runway.' t$ `: z, b. F- b. [! [ 差动变压器,: ]3 u h' Y4 m: s o) n: O$ Y 平导航,% P( Q, t9 t" l/ F. a vigation) h; D0 i! N5 U/ L A differential tra# P3 w# {3 S, \$ g/ c LINK, A short connecting rod for transmitting motion.2 a' T& d" S$ p4 j+ ?! G/ d L , g; @; X" o0 P( EL$ M v1 Q/ X ~+ D6 G( L c! I: j( M" q- O- s items and fuel loaded before each flight. 8 c% T7 Z8 o3 x2 QLOAD FACTOR, The ratio of the lift being produced by 9 a7 b* O4 w( e, H& vthe wings to the weight of the aircraft.* V% X( _/ X' ] LOCATOR MIDDLE MARKER (LMM, MM), A marker $ A c1 x3 D% L I. `beacon that defines a point along the glide slo / k" J. B5 S/ I( o1 z1 uIL0 k7 l- m7 @8 x8 ]$ a @: L" U; @( N d 4 |. k+ S! }4 I2 O- \9 T1 \5 D/ `3 mLOCATOR OUTER MARKER (LOM, OM), A mark / U4 p m) E; D! P& E; K4 Zb & k; p( w( f4 k8 q) _IL " N. H o/ V; [# a' F; F( T7 mLOCALIZER, The component of an ILS wh / _" P6 q# \ [& R6 ]; @$ j线性可变) [' |# {/ F+ \, A L* |" |5 S* ~ 具有线性反应的差动变压器。 ! ^& V6 I7 N+ ?% I连杆,9 ^# C ?5 }& u; Z6 R% Q- E 连接在两个部件之间,用以传递运动的短棒。 4 Y6 U/ X( P" a p+ ~# m5 }1 ]: E! O4 x5 \见Lateral Na . ; W" A8 v# W5 E5 s; J7 z3 v( p重和平衡表,7 W( j/ {, E a0 z 有着显示每个航班前飞机的各项业载和所加燃油对重 5 r; z8 x9 q s1 a1 r( O( O8 ?衡影响的图表的一种表格。 0 }: b* f% n4 K9 t. t& b( q! t7 f- }2 @ 附近的一点的指点标。4 ^, q1 i u0 i) Z4 K 近仪表着陆系统的下滑道截获点附近的指点 0 \0 ?8 j8 \3 \6 `- E) d. h0 N: u4 k5 z' f* D0 k+ O! a仪表着陆系统中的一个部件。它能提供到跑道的水平航) u: ?8 \4 [, V- N0 _ 道引导。 7 a1 r2 {2 n. n7 b% l0 a, W: G( j- Y' {& ~9 P 量和平 # S' W" Q4 q" B6 l装载系数 * c" e/ |$ r5 y4 g( k; ?机翼产生的升力和飞机重量的比值。 3 n, E5 p+ t0 T8 j' k, N中指点标, 2 H6 l9 u: Y" J8 @( s Q用以指示仪表着陆系统进近的下滑道上通常相当于决 + Q4 N, L+ X$ u$ M断高度或其0 ^1 G: r8 C$ Z) I9 R4 K2 [* J 远指点标, ! M; x- ]0 X4 a+ Z' j; |位于或靠 9 Z* s4 Z% o* e6 ?8 D6 _3 |: `, o% B8 `4 Q. V& p航向道,. X( q' O3 @) E, F 英汉对照民用航空词典B OEING/ W1 B3 R) y+ ~" k; V TECHNICAL DICTIONARY 94 4 p6 x- ^5 w r5 T9 C" }: G" T6 D BLOCKBOLT, A steel fastener which prevents unwanted1 x6 K( N3 {8 v0 h% Y7 d rotation by using a collar instead of a nut. $ |5 J9 k: C0 K: J( r, f8 ~6 V# ]OGIC, A representation of complicated electrical and . a1 \1 f5 b0 plectronic circuits by simple symbols called logic; k0 O2 O) X9 J H! h ymbols. ( k5 O. p1 n7 F% X( AOGIC DIAGRAM, A diagram that uses logic gates to( H0 \# t* v. Z) `- j; b; ] present the function of a control circuit.2 v8 ^; q5 m1 F5 c: F% V1 s OGIC GATE, A device or circuit which has no output- d5 P; @: Q! e1 V ntil it is triggered into operation by an input signal. A4 R% d2 K l# W) @, ^; L1 V# d$ c gic gate is an AND, OR, NOT, NAND, NOR, or $ D4 G6 n U3 a: h1 m$ bLOGO LIGHT, A spot or flood type light mounted on' m5 z7 T2 ?5 o3 g, n1 g4 I5 O! Z K aircraft structure and directed toward an airline LOGO or 0 D% R# t$ E+ m7 G, D) Zother message on the fuselage or tail surface; for5 T/ D0 i" F. A. C i/ N visibility during hours of darkness. ) s5 v1 ?' D5 V7 @0 z% X3 M. }. s/ V6 A( L3 s钢紧固件。: q' `. a2 I. Y9 _+ b" m% A% b 逻辑线路, ; e( u& a- B- j( C* ?7 g用简单的逻辑符号来代表复杂的电气电路和电子电路。 , b" H5 U, K8 _- L) p逻辑电路示意图,8 ~& k/ e# q$ W3 o3 H- V 一个用逻辑门来示意控制线路功能的图。 , M R; ]$ d, y' p+ c# [; o. D逻辑门, 4 i# a8 n- _& i/ c只有当输人端有输人信号触发时,才有输出的一种元件 ' Q, v, ?0 T+ e0 w. }+ l或电路。逻辑门分为:与门、或门、非门、与非门、或非' F8 s5 ?1 q C! M7 l" T 门、和异或门。. c% K" y1 N1 R 标志灯, " [- d7 b1 K. b/ Z* P1 x4 W在飞机结构上装置的聚光灯或泛光灯。用于直接照在机 - T2 j+ v2 r' f9 b+ f R$ D0 e身或机尾上的航空公司徽标或其他标志上,在夜航时照亮7 } Z3 H9 U" j8 n5 u 这些标志。 ' U' w$ j5 k- v2 L: y7 z1 FL / C& i6 R( ~: R# F% le % a/ q0 |( G% r; rs7 y+ ^3 H1 ^3 f2 W" b L1 A5 b9 b, `: L z+ X re ( r8 d6 m% {- l/ CL * f. N4 V& A7 A1 |" pu6 p }+ m3 U9 U5 T f% p6 M6 h lo / [7 A: l0 U9 Sexclusive OR. 2 |) w+ r8 q4 S/ c" q% Z保险螺栓 6 @6 n$ t6 {7 g; s0 B/ f6 r用环圈代替螺帽以防止不必要的转动的 4 q# m5 ]. \3 j, A7 W英汉对照民用航空词典B OEING ! i5 ^2 r# g6 f0 PTECHNICAL DICTIONARY 95 3 F- \* b$ X; Q7 t- zLONGERON, A structural component in the horizon j# H1 z% B) j/ ydirection of the fuselage or nacelle. * A( T" q3 g; ^6 ltal ^4 c! A+ R) R7 Q4 H; t( T) @RUISE (LRC), Cruise speed that is . u( K8 a6 V8 H+ H2 v! yssociated with fuel conservation, producing fuel; r' q1 r+ g: C" _+ K7 { ileage one percent less than the maximum fuel : \ l8 Y; n4 i9 Tileage available. ( h( v8 G3 v5 U2 P2 DONGITUDINAL AXIS, An axis passing through the) d" C; K3 N2 u& l irplane's center of gravity, from front to rear. . {8 _5 C* g# d1 ]not; W% v# T( {- T: E7 s/ y OUVER, An opening with slots allowing the passage of# g/ Q3 a) J) i: `6 U2 h {! W! a 远程巡航速度, }7 a$ N& Z! i8 Y- i 一个与节省燃油有关的巡速度。在此巡航速度下,每4 b* U; J. h7 H p 一单位燃油所能飞的哩程,最大的燃油量航程小百分之 3 l6 g% j5 l X8 u; [+ N v; V一。 ; J: t8 s* p3 Z! v5 n8 Q! u9 \! y纵轴, e5 z$ r1 \$ t4 E4 S9 p' j6 v3 S由机头至机尾贯穿机身重心的轴。 7 n/ M$ r5 d: \9 {) [6 {' M4 `0 o叶窗, 9 q" r( q0 m9 {7 |有多条缝的开口。! B$ c. W- L" Y/ W& i LONG RANGE C & s$ C. w! R, n& _9 T3 N8 X* V5 F6 Ta5 u% t5 C4 S: J) V m6 d8 X9 _; l& M, f m ; s, S# Q* P+ T4 ^L4 j% w: e6 s3 R" ], I) p2 I, E. ] a, E3 D1 D0 I9 Y) w' u LOST MOTION DEVICE, A mechanism which does 5 y2 {$ ~9 L% |0 A0 A) X# l$ L+ Koperate a component following initial movement of. s5 S5 W" H9 w" L1 Z; u control input. ( \1 r5 k! J+ R; k# cL8 ]6 e1 P6 Y% A( j air.# _: a7 K2 y: _5 b7 { 大梁,! b/ { z; t' G2 T7 h5 b$ }! C 机身或短舱上水平方向的结构部件。9 `. d) G( m+ u; F2 Q4 y* g. Q- k% _$ z- a0 E x% z" Z d/ ]+ a* o# ~空回装置, # c; p, m2 X# ?+ y, \在控制输人初始动作后,即不再操作部件的机制。用于+ B% b) X. H3 }& ^% h' t 飞行操纵系统内,以防飞机指令互相牵制。 1 N6 A' f1 x2 A% ?" u6 A! b# F/ k; c% B" g让空气流通的8 R: G0 f0 F; s+ B 英汉对照民用航空词典B OEING# g% @' r. f0 n TECHNICAL DICTIONARY 967 I$ O+ N$ W9 R P% r LOW RANGE RADIO ALTIMETER, A system that+ c, P( b; t: H: {# ^ i measures the vertical distance from the airplane to the 9 J) J$ I/ E, G/ I. t- W* l- Trrain. # l( B: l0 G) M8 N" e4 l) k- `/ vRC, Stands for Long Range Cruise speed. Represents ( g1 H5 h7 \! j- b, Pe typical cruise speed for a given jet airplane; usually . | @/ e5 u: s! k( ?( @& Jxpressed as a Mach number. + m& ~( {5 X- c) B. iRRA, SEE - LOW RANGE RADIO ALTIMETER0 p2 ~* c1 ^. F) q3 Z" o% j/ l RU, SEE - LINE REPLACEABLE UNIT$ d- O x+ J$ `9 u. l$ C uce friction& t- u) K- q0 ^$ B# ~ etween moving parts. It can be a natural or an artificial$ c9 j4 x$ d0 e; M$ o4 z aterial. : y: b) U% L7 p6 FAC, SEE - MEAN AERODYNAMIC CHORD, B- z. k4 O" y8 f ft's true+ Y0 ]+ B6 E# ^$ X airspeed to the speed of sound at that point.$ ^9 E7 u9 F8 e7 p; j0 L. p+ i 的系统。9 o: R( s% u" y$ @ 远程巡航速度的缩写。代表喷气式飞机常见的巡航速. j5 @9 X6 J2 X' c# L ,通常以马赫数方式表示。/ d( i7 ^9 t% K( A 空无线电高度表,2 I" U9 p% J) j Radio Altimeter 5 _7 \' W5 O; tte& e9 m, c& q. q& g- F L- N' d/ y+ o t1 q& }2 t th1 e- v/ W: l) ?" m e/ E" l: [. F2 [( u; f1 ? L " N5 L9 u9 A1 ~( WL 9 J3 Z) {5 y/ Z4 lLUBRICANT, A substance used to red' h- f8 S5 \- d: d/ ^& N4 O/ M& Z! x; H b ) G( `) z4 V0 R5 \m 4 A& z( m$ y. D9 U$ ELVDT, SEE - LINEAR VARIABLE DIFFERENTIAL4 N. Q+ D }4 o" H+ E* M1 y. w TRANSFORMER; I! r2 D1 [& X& j. X) b M 6 I) ]7 F+ R3 z$ @8 ~M 3 ]4 p" _' q* t- GMACH NUMBER, The ratio of the aircra) s5 |; e. z" @& G! s/ r 低空无线电高度表, ; \ s9 U' H' B/ O9 E' ^一种测量飞机至地形的垂直距离 9 n9 B- S) c$ J' d8 V远程巡航速度,- s1 h, {& O! a/ v, ^/ r% Z1 o" b' `' k+ ]- q4 X* U) Y+ g2 A# p1 v 见Low Range .8 M: Z5 j; c3 I8 M, T* O! g& s3 W 线可换件,+ z% c# O6 V: s$ X/ O 见Line Replaceable Unit ( z% H$ _* o, b, c. A) V0 C4 a, f7 s6 U2 |; f% G7 ] 用于减轻运动物体之间产生的磨擦的物质。它可以是天" ?+ c8 u5 o$ J% N2 ` 的或人工制造的原料。 & e1 @* l0 Y* W0 R见Linear Variable Differential Transformer! @' ?! T. N- t9 O/ o/ a0 u 润滑剂,) K2 ~+ @5 j* l1 M2 Y# E% a8 K, L; b* W, y& h @4 ? 线性可变差动变压器,9 @ i+ s* L/ \2 {$ q9 y; M M& R0 e7 T* y" \$ Y均气动弦, # F; q1 [6 M/ W; Y% X4 `+ t见Mean Aerodynamic Chord$ w. a* c/ ]! |2 o# }9 n+ X! W, a5 [+ A# p% g( ~2 Y" g" |6 v: P, c9 U4 r, j) ]; b空速与该处音速之比。 . y n( b* ?; p5 ~# U' ^ b马赫数, $ N; v9 f: l7 M) a飞机真& a6 f. `3 A! Z$ B# p 英汉对照民用航空词典B OEING % |0 p! \) m; @4 [; R6 a& ZTECHNICAL DICTIONARY 97* _( n& y* S* M* c& V( f MACH TRIM, Correction to airplane attitude (nose up)( s; m, k3 y8 f+ G2 h during flight at high speed by using the horizontal/ T$ h! ~5 C7 m: P" t tabilizer. + G5 ~* s, T/ YAGNETIC HEADING, The heading of the airplane4 O; n' f9 `% T( X1 Q* q lative to magnetic north.4 z, K# r2 O2 ~ AGNETIC VARIATION (1), The difference between3 y; U5 v7 Q0 a* g) x8 Q agnetic and true north.; @6 d! G% I, x0 m- D+ n' c3 { north.. e; _/ f3 S. H% J! V here is a continuous small change of direction 3 B9 K5 F3 Q1 a wf lines of magnetic force over the surface of the earth ,9 H1 s, t- ` C6 m/ ~- K' o agnetic variation at most locations is not constant over 1 ~1 J0 \7 ~4 |+ D7 hng periods of time. Lines of equal magnetic variation + h0 E. _4 j6 G; O6 u+ xe. (see1 H o" W H1 A& N1 H' N2 k1 P( S9 l tation Declination! ?/ y0 K! i" o5 T B s& D/ h3 w" M0 P" N M 4 {& N; I2 J; c+ O$ N4 E0 z9 Vre $ k2 M: `, q3 pM6 Z8 j7 F' @) Z! r( k m 5 ?8 `# w! i% s- c) P% TMAGNETIC VARIATION (2), The orientation of a 1 S6 d9 t M0 U$ G9 l2 Ihorizontal magnetic compass with respect to true 6 T9 U5 Q2 k$ H/ m7 dBecause t & g, Q/ T# B! H, }0 f Po8 _" ^3 q# H" s% o, _. ^ m, a0 S, l: E$ x2 R" p, y2 B lo- f3 \' i+ h! j0 x0 n2 x$ | (isogonics lines) are updated on Jeppesen charts every3 @7 \. Y6 T1 o! v/ B$ Y five years in accord with worldwide practic G+ y2 \! F \$ _ S ). - q. \# x9 i D) r i4 \8 FMAIN ENGINE CONTROL, A component on the engine 9 {1 v2 @% t7 x* f m/ yration. # o1 D! H; Y' A' v3 n; lMAIN GEAR, The main wheels with the attachments for8 ]% H% e: d& N% Z* B supporting the airplane on the ground.. }( y+ X" X" f& w9 ^ U9 a0 p MAINTENANCE, Work accomplished in support of the 8 I5 N, D8 Z/ {- i1 g3 d! Istructure and systems of an aircraft. It includes,! v. W0 a$ P3 {9 Z1 U5 a$ y5 y t inspection, overhaul, repair, preservation and the% L/ o% F) s# x' k3 k- B replacement of parts.* q( U0 A- {: o 马赫配平, / c9 d9 _: ]) Q用水平安定面对高速飞行中的飞机的俯仰姿态所做的! }1 f N6 f1 Q! D 调整(机头朝上)。 % m$ Z f2 W' k4 ^0 X磁航向,. H; v$ z# o. H: n 相对于磁北的飞机航向。+ C- j" A7 |0 k& x" G! i+ G g 磁差(1), + S' v2 }! U4 x e) r真北与磁北的差别。/ G$ r0 M v6 f* x 断的微量改变,磁偏角在长时间内多数是不一致的。每2 Y$ [4 b6 s; Z V' f 五年Jeppesen手册会按照国际惯例校正等磁偏角线(等3 I; Z5 F' U$ m' \8 C/ D/ g 差线)。(见基点偏差) - k& A! M- C4 X0 w. l9 s, H主起落架,3 G1 T* @) N' A0 C H0 |- M+ d# X 用以在地面支撑飞机的主轮及其附件。 9 F0 d6 q) h4 A, C% R$ n" o4 n维修,% ]1 S3 o) [$ Z' K l3 r 在保障飞机系统和结构时所做的工作。包括检查,大修,9 u0 T( v8 h3 c5 K 修理,保养和部件更换。6 x, K+ y8 |( x2 X5 { for controlling fuel flow for starting and engine ope * u$ j& y, w+ X4 i9 Y% [磁差(2),# N. B$ n0 p9 c" A 相对于真北的水平磁罗盘定位。因为地面的磁力线在作 _8 l* d# S- B, B" b5 z7 {' K. m5 P* F1 x: L( W% f( F! Z! } 主发动机控制器, " G( q N/ ~# U0 [1 N; \发动机上为发动机起动和运转控制燃油流量的部件。 / a& q/ M- Q9 |; A2 E2 Y英汉对照民用航空词典B OEING + S& Z# t6 f! e; d+ `2 Y& xTECHNICAL DICTIONARY 982 U# `& p7 C8 Q9 G: ~& X MANEUVER CAPABILITY, The ability of the aircraft to 0 E# M' v, j9 kertain load factor. 9 K( m. C% J+ R8 w$ uMANEUVER MARGIN, The amount of residual 9 _. i# x6 v( H _& A2 y9 V6 Laneuver capability present before the onset of buffet.( Y) C' H, ~9 L$ M MANIFOLD, A duct or chamber with several inlets and. O* f3 h+ }. a4 u; Y1 L outlets for air or fluid distribution., @' n& H' `+ ?0 O$ y* [$ U the 3 c1 P( N% a9 z$ o5 Q/ \low of 3 ^1 a! y! ?! q7 q/ ]e flight compartment. On specific & A) y$ S- m; U, Q& t( Dccasions it will provide conditioned air.. k) D. g |" e& N1 j4 S* Q3 R omponent by hand.+ N, ~+ S& P% _% d$ W! _ MANUALS, Books with instructions for proper W0 l( J1 m- z) k1 Amaintenance and operation of the airplane systems. # H [2 y0 W' e, z0 O( J) V7 I: b$ TMANUFACTURED RIVET HEAD, The head of a rivet 9 n" P) b* x) @3 U* \3 gthat was preformed during its manufacture (see upset 3 [: o8 r! _2 o6 j" b( uperform certain maneuvers up to a c * f# ^. x& X6 l5 P4 |- I3 Ym8 Y7 p% N) e% x8 \/ R4 r MANIFOLD INTERCONNECT VALVE, A valve in - j @% X& W) n: }, w( Aequipment cooling system for providing a normal f . P$ p7 p2 K0 p5 I) z/ `8 ]- V) k& Srecirculated air to th % n8 S3 R4 ~8 H% D; k- d4 do5 W; h4 b7 i9 [# a2 @* ? MANUAL OPERATION, Method of operating a 7 W' r. y- b! |1 W% b" Mc. O; n0 q$ h+ O$ s6 Q$ b head). . \' z0 V: A( \) W% w" A. Q' qMASS, The quantity of matter in a body. It gives the ! l' p. `9 V4 Pbody weight when it is exposed to gravity. % I& d' f/ C+ |9 y机动能力,6 u( g5 e8 y# v 飞机完成装载系数达到一特定值的机动动作的能力。 " j' V% Q) ~% Q* f" N8 d机动性余度, 4 c$ \: |' e- J飞机在遭遇抖振之前,所剩的操纵能力的大小。 ! |5 @# p0 S3 y* K _总管, - ^. S/ P2 d2 B ]6 o, Y用以空气或液体分布的多进口和多出口的管道或容器。, w" j/ F0 l) A3 n, m; c3 E 总管联接活门, 2 a/ p* s2 w2 U; k设备冷却系统内的活门。用于向机舱提供正常再循环空 2 F. o% C6 ?1 v, M8 o3 O3 s/ {气。在特殊情况下会供给空调空气。) y; Y/ x/ d, y. x7 B& `' s; q/ u, w 人工操作,5 }4 a2 p! m, _ 手工操纵部件的方法。 $ f9 r1 K9 b8 O4 V: |明书。 & P5 _. I- {$ ~1 S3 |& Y6 L铆钉头,! y# m. [+ s) s; B: g! q( o* e 在铆钉制造时已定形的铆钉头。(见膨径头)。 9 [; u/ f8 e) m9 D; U: s, w/ ?质量, 4 l$ r3 j5 F2 G6 g4 _( Z& H一件物体的物质数量。当该物体受到地球引力时质量产 7 _; w5 t9 c& _3 P& D生重量。 : @3 X) P5 k* Y5 Q手册, ' h7 N U ~: f1 D4 s为能正确地维护和操作飞机系统而编写的说 4 _, B7 j+ n) l; F3 Y2 I- q% x机械制造的 ) G; x0 [/ L1 M2 Y1 A- f英汉对照民用航空词典B OEING 9 h+ S* b: h& ~; D3 H2 q0 K jTECHNICAL DICTIONARY 99 7 U$ W9 m& Z p4 ^, bMASS MEMORY, A memory that can store large1 i" A7 p3 S1 G- v6 S amounts of information and hold that information: W8 T2 ?/ N# Q6 F: Y) g1 \' h permanently.- j1 T0 Z1 a% b$ e& M% B- @ AX CLIMB THRUST (MCT), Maximum engine thrust 3 M5 n* j- n; m- V; U; Lximum engine : m6 K, f. Q8 u c F3 rrust to be used continuously when one engine is/ l! }$ C* S- X1 S) O6 T operative. + E4 C4 Q% s& ~ ]% bEOFF THRUST, Maximum engine thrust to be# @" e: X/ J" o3 w' F2 m used during takeoff.6 z% G8 p+ d% ? FF WEIGHT, The maximum take off9 ?$ r& P; y6 y% u. R# s5 X weight as permitted structural limits or performance . p2 {/ `" ? v: plimits, whichever is lower. ! ?5 R7 [0 s+ m, [RANGE CRUISE (MRC), Cruise speed 5 I, z( t8 `1 q+ Pance3 Z. |7 h$ |1 x/ d to locate8 ~) M$ V3 f1 {( n9 P4 E6 T; k$ \ the Center of Gravity. & F) I, T+ N( q) Z" z. z3 r$ L主控台, 6 I, p$ b4 e- T; ~' }* W控制系统操作方式的装置或系统。 ! |# x* Z5 `; c9 J9 `大爬升推力(MCT), ' c5 w/ p$ l( B: X6 _) V6 t飞机爬升期间所能用的最大发动机推力。 # E* o' l$ R& M# RMCT), # N9 v! v9 ~4 m, a! H/ z) e当一台发动机不工作时,可以连续不断地使用的最大发 B2 q J5 U' U: Z% b 动机推力。 ; A5 ]' \/ _- ]1 p起飞期间所能用的最大发动机推力。3 ?2 U5 z) |" l- R& \ 结构极限与性能极限两者中的小者许可的最大起飞重 # b; P! y3 ]0 u- S. z1 m* z3 o3 b- e/ Z# j* M大航程巡航速度,8 X1 P$ Z9 X! q5 i3 \ 最大的巡航速度。0 u4 H) l# _( J1 { e 平均气动弦,- A5 h9 k8 [ A9 H0 V 确定重心位置的基准. c$ r3 H% j2 V; l- o 距离。 / y* u$ h( f* Y. uMASTER, The device or system which controls the! `- G W+ S2 t3 C% e system mode of operation.6 T2 \- [# D2 V! a$ |) s f' x) [ M B* C' B& D$ d0 P/ f. h Vto be used during climb.: b9 F# p3 K9 ]$ e3 m MAX CONTINUOUS THRUST (MCT), Ma2 Q3 f/ r' |* ?/ T: ]0 ~ th - N5 g, L5 \1 Y3 q* lin& R3 h/ M( X( W" e g0 m7 R MAX TAK 5 Y) ~3 [" U; e- j& hMAXIMUM TAKE-O o2 z$ @% M% E( O# _8 g! ^ MAXIMUM 9 O' B7 d6 D7 C" H; kproducing the greatest amount of range. ) A: P! @7 u! o2 n# `- c% rMEAN AERODYNAMIC CHORD, Reference dist+ f- \ t6 a9 Q located at a fixed position on the aircraft used 5 \- U% U* P' J1 T. D7 B大容量存储器, M$ R4 e* P, E" {4 M# Y! [ 可以储存并能永久保留大量信息的存储器。 * F5 z1 l) P- I% G1 T8 g' |3 O+ A% N ~, U, S* a最大连续推力( {7 m5 |6 ^" \$ G7 |/ ~$ F 最大起飞推力, & f, B$ C Y( m3 ~ A2 g最大起飞重量, : Z' W J1 k6 m' h4 Z& k# q! Z( X" f9 g3 |% M! z( Y5 I2 e& W( r+ v, L' [+ S能使飞机航程 / S4 p2 V1 D: Q# K8 l位于飞机上一个固定位置,可用来 ; h" m1 k) x$ g I! d" O3 Z英汉对照民用航空词典B OEING: ~% s* X5 q; f( c K TECHNICAL DICTIONARY 100 8 s' K \3 u, {% r3 M dMEC (NO. 1), SEE - MAIN ENGINE CONTROL Q6 i, o' n8 s/ Z& |* l9 P$ ^% y. M MEC (NO. 2), SEE - MAIN EQUIPMENT CENTER# u7 r) p4 Q/ U EL, SEE - MINIMUM EQUIPMENT LIST / c( p4 j+ ]+ d" H- L/ \tem the memory is where 8 C# L; J. |+ z1 h; xformation is stored. 5 z! l" K" Z/ y, q. L' }: SMETER, Any mechanical or electrical device that is% a" u- Y: d. Z3 R# `8 u air or 5 j/ u: m" x4 N& u# S! N) ypoint along the glide slope of an ILS approach. It is # M- C' l' P& y; gnormally located at or near the point of decision height.% C j3 s5 S# S. S- @" [* p% ?% j1 o0 O$ G b) t. x2 L# ?3 k0 N见Main Engine Control ' _/ t7 g' Z0 e2 i+ J/ e! ZM & n, Q2 F+ ^; A& |: p; c5 GMEMORY, In a digital sys . Y" m& \, @2 B6 yin6 }; Y: Y0 J( [% L% L9 g% s u used to record, indicate, measure or sense a specific/ p( A P9 w5 i' ~ portion of an operation. ! Q( ]: j. G, i$ ?METERING VALVE, A valve for controlling flow of3 g2 i8 y( Q ^2 r) R fluid. 0 M6 ?5 s; x( A6 k P9 QMICRON, A measurement of filter effectiveness, one% ?. K1 L5 g# G; r1 q micron equals one millionth (.000001) of a meter. 1 q) k) U+ ^7 I7 L5 W: N# OMIDDLE MARKER, A marker beacon that defines a7 h! E# v" ?# x7 _$ }( J 发动机主控制 7 n/ B( X, `, {: T; ]- p3 p6 T. z5 `: a% A. C& E; o" Q 设备中心 , m. n* Y+ P$ x E+ C9 N# h见Main Equipment Center 8 Z0 O, z6 y+ h1 ~% ^0 @4 l9 m; j4 y% e- x! D, B/ X$ E$ v0 E- h6 d3 X* a 低设备清单,- p1 L5 o' t, Y( W$ k7 F 见Minimum Equipment List 2 L- |6 {$ K3 I- B" j3 l6 j, d, }6 n' V& `% ^3 _- Y) ~* a8 P6 m) Y1 U1 C6 }' d% E 在数字系统中储存信息的地方。 * O# @" Q4 \& k4 I& O: }9 X; [7 ~* A计量表, ' @" x/ J9 a" L9 ^$ ^0 W) j用于记录,指示,测量,或感受一操作过程的一个特殊0 A4 s ?$ @! s9 k/ u* @$ H& Q7 o4 _ 部份的任何一种机械或电子装置。 + q' d ^9 v0 M& a7 G量活门, / Z# A! V+ I8 Z6 Q3 p# Y6 ?' |用来控制空气或液体流量的活门。 " @9 W7 k! Q6 a& q微米,$ _3 d0 i @$ E3 Y 过滤器效率的计算单位。一微米等于百万分之一米。 : A- F; s/ c' J8 b在用仪表着陆系统着陆时,用来确定下滑道上一点的指- j/ r; M6 }2 z 点信标。它一般位于或靠近决断高度。 / K7 Q( d8 s; S存储器; / F$ O" v& @/ V9 I% c2 w* r) T7 g6 d) r* N6 w 中指点标,! q; {* b5 L! N' y% [0 m 英汉对照民用航空词典B OEING o0 C: l. ~( _% J) W7 g1 N TECHNICAL DICTIONARY 101( W+ h; W; _" | MICRO SWITCH, A miniature mechanical device that # g" W+ s; L" V* j9 s8 Zcompletes or breaks the current path. ( [, t2 E. T6 A.1 R" W. l: m2 s* a5 g. l2 X4 M MIL, One thousandth (.001) of an inch. " ~, P& r, k/ I2 bILLIBARS, A unit of barometric pressure equal to8 @1 J/ [6 ~1 w- p# d approximately 0.75 millimeters of mercury. ! f1 L# m6 c1 J8 v# K/ M8 xThe lowest; R5 t+ A" i3 R( n ltitude to which a descent is authorized for a& L. P$ |2 P( A1 ?3 Z. c3 E; \ onprecision approach. 4 T0 O8 `1 b9 N6 u( h# q. GINIMUM ENROUTE ALTITUDE (MEA), The lowest . g5 ]( q! ]% S( r/ d5 Z' rublished altitude between radio fixes that meets ) x( B% F6 V4 J/ Q. _7 nbstacle clearance requirements between those fixes . N0 y# N0 d, pand in many countries assures acceptable navigational * f1 E0 t+ e# {; z7 F rsignal coverage. # D4 y- P1 e2 e9 u9 Eoperation of the airplane with certain systems or ! o2 v0 B5 S9 ]) t1 {subsystems inoperative.8 W: z3 @0 {- g7 T. W9 [8 g approach R+ _2 |5 o9 E% J% N cannot be completed to a landing and results in a Go- 9 _0 v: [( x: r1 R( dAround.5 z j' Z1 H K- A1 g3 B 一个能形成或切断电流通路的特小型机械设备。 " F7 r4 x+ ]2 i7 Y! w话筒, + B/ y; X% ?+ j" n) \* B话筒一字的缩写。 : c9 K& h" i6 D% a. J6 D8 {8 Y0 A耳, ) f* I, Q ~, D$ H一英寸。& m9 N* ~ \) I7 F. B& g" ~ 毫巴, % s$ @+ ?. w) ^* B一个度量气压的单位,一毫巴约相当于0.75毫米汞柱。 0 V0 C$ V: Q5 W5 |低下降高度(MDA),# m7 f# O3 j$ s& l* U' h! c 飞机作非精密进近时所准许下降的最低高度。 ' c. U8 G1 g3 ?- ]1 r Q1 b低航路高度(MEA),, Q% w; {4 ~+ [: j0 ^* @9 D4 n% ? 在导航用无线电定位点之间,符合越障要求的已公布 ( B F' d$ A: {+ w7 Y" k: N的最低高度。在许多国家,最低航路高度保障了合格导航. X6 s* g* q! @5 D 信号的接收范围。$ ^5 f5 i" d* q# z 最低设备清单,( ?& g/ C! u6 q% _# \4 g2 o$ J2 g, f! { _ 作飞机的文件。5 P7 o; F: E( |) `% w2 p3 a 复飞(MA or GA), 9 Y, e1 Z6 r- T4 E# N8 \飞行员因未能完成仪表进近而导致复飞所采取的一个 ' K- q. x' Q, }机动动作。 - j2 D0 Q$ ], q% U L; ^MIKE OR MIC, A shortened form of microphone / Q, P8 F; q* P! O/ Z/ cM $ a0 ]1 a7 ~ B7 ?' _7 @. gMINIMUM DESCENT ALTITUDE (MDA), 9 X3 X/ K/ g, P U' z) T; Oa . X) B! @' q5 t6 ln0 f# T4 a9 w' X$ k. P9 \1 F* G9 ^ M/ Y6 n+ z, X) a( M) z p 3 \% l4 S- ~- U0 Do 7 E" a* v3 S+ n+ p4 M# BMINIMUM EQUIPMENT LIST, Document prescribing \- i* f8 i- {: v* F" t! W! N2 p z% qMISSED APPROACH (MA or GA), A maneuver U" R5 B4 e1 e& ?conducted by the pilot when an instrument ( L% ?# [. u4 v% `$ ]' W微动电门,# W. ? u& ` }" z0 D. i# _' |5 v4 o7 m 千分之 : O; D9 |6 M1 F& _4 K6 v! w$ `! U# Q: M- e, H3 W4 U! D) |: ]$ P" E ]3 @ 指定飞机在某些系统或子系统不工作的情况下,如; F6 a' f* D( A N' I; s, U" \/ v 英汉对照民用航空词典B OEING. \% H0 g2 |( R9 y4 g- @8 P TECHNICAL DICTIONARY 1027 m/ _4 m y, h& m1 t* h4 ]/ C B) j MIX VALVE, A valve assembly with two or more$ |! O$ D/ A& Q# o: l- }0 U individual valves used for airflow distribution in air0 \4 w/ E, x- Q5 r' F! k, W stem.5 E/ J9 O: [! S7 ^; X MMO, The maximum Mach number at which the aircraft+ a0 K: f/ Y7 V( S. q MODE, A specific operating state or condition; i.e.,- m. E; U: s0 Z, T2 P+ Q9 u$ c3 U Autopilot mode, MAP mode, etc. ' T5 H6 H' b" _- o& ve . h2 A" L; u$ [1 ^- B) t C* H; BMODULE, A housing that contains related system% [7 \' ~* D& c: r T/ I$ R3 A( U! [ MONOCOQUE, A type of construction in which the1 k: ^( b" A- i$ ^/ I/ r ONOPOLE, A speed sensor that senses magnetic $ D( d1 B) D6 {4 S! }pulses from a magnetic nut or gear teeth on a shaft.9 @/ [9 q' W, e: o' S4 b' [ he controller.8 ~. K7 R4 X( g3 R/ p8 V- G MOTOR OPERATED VALVE, A valve using an electric ; {* P/ r- S* ^% i3 rmotor for opening, closing and modulation.1 `! m% w5 W( E- ?" F% D5 s 个以上单 # C6 ^+ f. c; s活门的活门组件。; x' a) b$ z1 `+ l 飞机可使用的最大马赫数。 7 o J+ m% R- P5 b1 J O" L' x式,MAP7 W: a; V" Y5 ?5 O 方式等等。 # y. l+ \" `" n/ \/ }3 U调制,# j$ J7 `) T4 g' k# p 组合两个或两个以上的电子信号,使一个信号随其他信/ n' r' E e1 @+ m, ^ 号的变化而变化。 # Z( J* d1 S' t+ u& E: @. t7 @组件,2 l) w5 |9 n2 Q* \( _' Q3 a 极, ' w: I: s+ h- ]$ U& t帽或齿轮轴上的磁脉冲数的速度# \, g% I: F0 Z3 s5 ~: L) W/ ?! c /分钟。 , D* v# C! ]/ N! r1 Q% \用电马达来开、关和调制的活门。2 R9 @# Y8 m+ G5 v' w conditioning sy ( B, Z) F; v2 U" b. B3 {3 P# J& ?may be operated. 1 Z, _! @0 G/ }' p5 tMODULATION, Combining two or more electrical8 \/ ]4 P! R% ]5 p0 G! o signals with the result that one signal is varied by th ) _9 m5 A7 u; Q8 _( A0 S+ o0 Sothers.7 N1 @3 M8 s- E u3 S components. " \; P4 e- u# u5 q- ^fuselage skin carries all the loads. 1 U F" E& |, oM : e+ l7 k" z# fThese pulses are interpreted as RPM by t* Q+ O$ `; R" U9 S: P9 V- _ 混合活门,9 I0 P: M8 M# H, ]4 W2 e+ y- D" g$ _ 在空调系统内.用以气流分布的具有两个或两+ S3 V1 t' t" s: w6 o3 {! ?% x* w5 m0 D/ P8 q# b MMO, - z% @, [2 X! L方式, - S! h2 O) @/ W/ _- s: z& |一个特定的工作状态或情况,如自动驾驶方 ; ^1 A4 E" ~+ N1 F内装相关的系统部件的机体。 % H4 n+ R5 A5 ^2 k6 g硬壳式, # f& P: H$ \: r( P7 B机身蒙皮承担所有载荷的结构形式。 % H) E# G" h9 Y4 I0 W, _. b& O: {3 M0 d x8 w- Y% X一个能感应到磁螺' d9 Y7 L- y& O1 ` 感应器。这些脉冲可由控制器译成转 ! M2 b9 O' i8 n3 U3 ]1 u9 ~马达操作活门, 5 m! V- E5 T+ f1 y8 w* D- v4 C6 I英汉对照民用航空词典B OEING) _" C1 k9 J# U* H s T TECHNICAL DICTIONARY 103. Q1 N1 c1 L9 ?! ^ MSL ALTITUDE, Altitude expressed in feet measured @+ B1 ]' `& _' T; b2 qom mean sea level.' }* y6 O# {- r% N, T reducing the noise of the airflow through the pneumatic3 [6 E" S5 D1 r# Q" h9 t1 D duct. ; @6 f3 q3 p; E7 y! ?MULTIPLEXER, A device that allows two or more 5 {) p8 H2 \3 S$ D+ n& r, nsignals to be transmitted simultaneously on a single) S. I) b, [# f' p5 [ carrier wave, communications channel, or data bus.+ w( M' i; Z0 a. s d% g essure compressor rotor. 3 f- K' z9 W3 I' p: ~: bN1 BLOOM, A change in engine N1 and thrust indicated" `+ ^" L1 O5 V0 C9 \2 y; t4 g: T7 F N1 gages and detected by the autothrottle BITE ; _7 F3 |+ i& F' B( Gduring throttle hold operation. 5 H( g' v8 p n1 l% X! u, PN2 , High pressure compressor rotor speed. ) F: Y q. Z* X' KACELLE, A streamlined enclosure on the wing or # |9 ]1 \" ~5 l% E/ G面量起的高度。6 }9 ?" J/ {! a 经气源管道所生的噪音 ; U/ q; \ G: ?( k$ I的装置。 f* r( h7 T/ s; O( ?, I- O# h 多路传输器, ( {1 B9 \3 C4 l0 b. c9 j- {一个能让两个或两个以上的信号同时在一道传送波,一) W, y: Y7 z/ s3 s 条通讯线路,或一条资料数据总线上传递的设备。. i F' l% P# k# r+ I3 \, q N1转子转速,& D* r7 K+ @" ~# j) N 发动机低压压气机转子的转速。 , m. P6 ~; s6 x6 s0 r6 ]N1激增, + Q% f1 h7 l( C8 R" B; g油门保持过程中,在N1表上出现的由自动油门自检探) k2 ~/ Y( o# D5 Z' A" ~8 @. {' y Z 测到的发动机N1和推力的变化。 $ L# L/ q& i* v l2 S( i+ A0 NN2转子转速,8 g4 k& |8 A3 T" q: _7 s4 F% R' k1 I+ X 发动机高压压气机转子的转速。# C0 W$ E, H8 a 短舱, 9 Q I8 m7 {( C) P, u# p# q. h机翼或机身上为安装发动机而用的流线形壳体。; T$ s( ]7 |! c% Z& O" }0 J fr2 P3 s: W3 a+ P! h1 P0 _ MUFFLER, A device in the pneumatic system for * y8 m8 L( ]) _/ F8 DN 2 m q* ?# v5 \& ]7 p: R, xN1 , Speed of the low pr2 j J8 j% R, G# C* h on the 7 @ H( f0 q$ c2 \' M2 j4 lN/ N- v! S4 k7 Z$ I0 Z4 K fuselage for the engine. 1 a0 S" C) r" o1 e平均海拔高度,; E' G3 u! G8 T1 B; C 以英尺为单位,由平均海平 9 Q. ]( u+ H9 w3 j消音器,- d* Q, S- ^; o: r$ a% G% H 在气源系统内,用以减低空气流0 L5 ?8 c1 D2 C+ b [2 m* | 英汉对照民用航空词典B OEING; h, B0 N8 A# r6 d$ f TECHNICAL DICTIONARY 104 % m0 K$ i% j9 f: }( D+ VNAND GATE, An AND gate followed by an inverter to , D3 A: D' {: `9 A, ]: aform a binary circuit in which the output is logic 0 if all, A# Y' r7 a0 s; r% G2 O puts are logic 1. 6 m4 y7 I# p8 T; W; @9 _+ xAUTICAL AIR MILES (NAM), The actual air distance * y) o8 k( D. x/ e* S% ~respect to a ' X6 I; q" k8 I9 d* A9 jtationary object.! S4 I" A2 N A, O) c istance: k% \& }8 C6 p' T* s# b8 B" S. S! [7 j travelled in relation to the ground expressed in nautical ) t/ T2 G2 l1 E+ ]& W3 _miles. 1 M" k+ V( X; S3 b& t5 [( hnce equivalent to 6076.1 feet; D6 g) G7 C5 `* |- h r 1852 meters.: n5 o# h! K" v( O hical 3 r* s: y, d1 ?% `- Q# G; h M6 IEGATIVE LOGIC, A form of logic in which the more " X- T2 x% X( {" z& |% Gnegative level represents a logic 1. {. n4 H0 t, [. F# n G6 N EGATIVE RELIEF VALVE, A valve in the1 X) E4 g5 Q' D7 W; c e to be' [6 A8 m1 [9 |" ~ above airplane altitude (or cabin pressure to be below & s6 I) V% w5 D! O. U5 cambient pressure). # @6 V: |& A6 M0 |% E% e$ K' z4 E0 p1 N: J0 q: n人为逻辑1时,输出为逻辑0。 " f8 T/ `4 @4 Q8 R) P. r海里(NAM), % q1 I# I) F9 h' O4 K来表示的飞机在空中所飞过的实际空中飞行距3 G- ^( U- D7 \) l4 ^ 地面物体。7 v a. b3 z# ]# ?$ Y 以海里来表示的飞机相对于地面所飞过的距离。 3 [+ ]" u+ N$ Y: } F: Q里, ! C/ f; R6 G) V4 X9 L4 q& H相当于6076英尺或1852米的距离单位。 & e5 S3 }2 a: w0 Q1 m8 ^+ R+ W导航,6 V* |# f5 [3 ?7 B4 U2 ? 反逻辑, * I2 F! |) [) U; Z [4 I6 S正电压水平越是代表逻辑0,负电压水平则越是代表逻; O! @$ }9 v% a1 `' q- I 释压活门,# L% w; @7 _# \- l% g' _' {8 D 增压系统内,用来防止机舱高度超过飞机高度(或机舱: i9 j6 u4 t' I n 压力低于外界大气压力)的活门。 1 p6 J7 P/ V- s" e vin/ y& X/ X6 Q' I9 } N( \5 b" l/ }; \7 D, w* R+ j flow expressed in nautical miles without * s0 ^' X( V! hs4 s) O# Q/ \, E6 v+ | NAUTICAL GROUND MILES (NGM), The d5 W# g9 ~* n" \0 d( j NAUTICAL MILE, A dista; @2 v+ s: T# P; K* n" A, Q o 3 t% @2 j3 k n' h5 wNAVIGATION, The art of determining the geograp: l4 Y( E- V5 @3 J; o position and maintaining desired direction of an aircraft 4 g9 x9 ? @' J. D9 A' h" m+ Yrelative to the earth's surface. ' F- _4 ~1 U: E- p: K3 j/ }N7 ~" h& Z( y) D A7 q d5 M9 i# _ positive voltage level represents logic 0 and the more6 I5 w# H. _" O% v7 }4 c N1 C. A& y: L: n' [3 E8 l$ y$ D& x& H pressurization system for preventing cabin altitud 7 J t) U0 W- T1 d) \4 ]2 B7 W非与门, 7 I/ S6 q9 C W# T: t% h在与门后面紧跟着一个反向器的二进制电路,当所 a& }) h$ |* q5 x/ X# b o- a+ F4 d& N; B L4 {( s! M7 ^0 n/ [ Q以海里 # ~3 Y* u6 _4 e; x离。空海里无需参考 - q, Q4 A: d* X, `( Y3 `0 y地海里(NGM), 9 E; }5 Y; j0 o% D5 ]* T9 }2 j2 `& x# _决定飞机的地理位置和保持飞机相对于地球表面所希 ( D# L2 }8 e! |1 ?望的方向的技术。 3 q& c- I. E# W9 ]6 l辑1的一种逻辑形式。 ! G* e- |' R; w# D5 L) |, }: L0 J a* ^: r1 t 英汉对照民用航空词典B OEING# m- ~2 E$ g9 I9 {) }6 Z: S, l6 X TECHNICAL DICTIONARY 105 4 W! p. w% ~5 X1 z" y( M& mNEOPRENE, An oil and grease-resistant synthetic# [; h) g8 |8 }) `9 H7 y' X6 I rubber. Used mostly for seals and self lock nuts, etc.0 y( e* o* E4 z( I EUTRAL SHIFT SENSOR, A sensor used for $ l9 j" M$ {1 H9 ]NET PERFORMANCE, Aircraft gross performance 2 B8 r0 ?# J- V1 ocalculation6 T, a- ?9 P: c7 O6 ^ purposes. - _ x# v# }5 {+ S. N% Q! vNICKEL-CADMIUM BATTERY, An electrical device for9 @6 S& }" q5 Y1 p: F. P changing stored chemical energy into direct current. * N$ y" D: P, n# t3 V" }6 E! `ses nickel hydroxide, cadmium hydroxide and 8 D3 ~9 M/ n2 \. `7 T6 lotassium hydroxide. # |5 L% c7 w' G* {NOBLE, A term used to explain the properties of some7 j+ u) B. |) Z# f lements that are chemically inert or inactive. 3 B# X, J. C6 y* s6 KNOISE ABATEMENT PROCEDURE, A flight path and ' Q: [' @9 e) z1 j% B1 f7 o6 Llimb profile designed to limit noise in the airport area.- `4 v4 \4 q. z& u p+ ^, r: @. \7 O construction. (Nomex is a trade name.)0 y: ?" |0 e; `; V- B8 R in only 7 Y9 b( @: C( S3 C7 E; Hone direction. . _$ L: P" l* ~* S) a氯丁橡胶,6 C, B4 o4 i' k" g 一种耐油和油脂的合成橡胶。多用作密封装置或自锁螺 % C2 @( c/ L6 F. H$ l7 H$ w帽,等。 4 ^3 q, u7 g/ c立变换探测器,' P4 A8 F7 m; p7 M |4 f 用于探测升降舵和安定面配平状况的传感器。 1 q. a, b3 ?% ^/ M/ L8 ^: _性能,' M3 j& P8 `* I) {. d) X 机总性能减去由当地有关单位为了使性能计算* ~) }. s6 A) e3 M8 E7 t& H 较为保守所定的一个量后所得的性能。4 E& Y( d! w+ B: J7 [ 为直流电的电器元件。它使用氢氧化 8 f3 }7 ?) F) y) a' b) y6 k0 C, h、氢氧化镉和氢氧化钾。 ( T6 ~$ W7 d8 g性, " J$ n+ j" I, T4 c用于解释有些元素不易起化学作用的特性的名词。 ) A- Y6 P$ T% b4 R/ ~低噪声程序, 3 u- C+ l' Q! U一种为降低机场地区噪声而设计的飞行航迹和爬升剖 ! A- w# N1 \5 o5 s$ H1 w$ G, `; R: l+ j是一种类似纸的材料,用以制作蜂窝结构。(NOMEX5 S Z; y: q2 C- y, a 商品名)。 1 X* @+ N' {! `7 R只允许向一个方向流动的活门。7 A, r0 U e# X# w N5 J7 p. a% T) A. E0 V4 r$ R detecting the elevator and stabilizer trim condition. ) A1 _: T5 y( Xdegraded by an amount determined by the local& f5 q" O/ a! ?! L/ s governing agency for conservative& O4 L' b0 S2 H5 V. _8 F2 ?) c U$ B3 `/ U/ B+ d p # O. K9 L+ P3 [; Ie : r- s1 _6 D/ W6 B8 {; a: [# X9 sc ! ]* r9 |8 x8 F, O O9 W- nNOMEX, Material similar to paper for honeycomb 1 J e2 j: {& Z5 g) s1 kNON-RETURN VALVE, A valve allowing flow3 o7 W* l* h2 c: G% |9 I' @3 w8 Y5 z8 Y' Y# c4 h- `& x/ g1 q3 {9 }8 m5 C; D7 q( E# { Q9 V5 W; x% s以飞 . U4 W2 c7 @& W" a镍镉电瓶, & H+ a E1 p5 `& t将储存的化学能变3 I0 T& j: R" e1 L9 F0 V. V2 k1 W, B: \4 M* @* X" W6 ^5 s- ?6 p( W$ o9 h7 K! B$ J+ E% ~ G# h$ o- L6 z; Q; F# b NOMEX, * Y, T" t! U; Z" |* ~& `8 @ D! M( c, a, ^ 单向活门, . v# P) R. X# i9 {$ o英汉对照民用航空词典B OEING0 T" `; y1 U" X$ }( g: M TECHNICAL DICTIONARY 106 9 i6 S i2 \) ?1 G2 qNONDIRECTIONAL BEACON (NDB), A radio beacon 0 T. b$ ?9 o7 S! |9 C. Q7 x0 Kwhich transmits nondirectional signals whereby the pilot 4 E2 Z$ B- L& x6 S1 Lcan use the ADF to determine his bearing to or from the0 I! v5 I: ]7 T7 Y) } station. 6 W. v" h4 b- M6 x4 sONVOLATILE MEMORY, A type of memory which7 g" R9 t% Z# w$ } does not lose its contents when power is removed.3 E/ l% j0 c% X, v) P! v9 S rm7 O V+ W1 C/ N6 J1 c% V binary circuit in which the output is logic 0 if any of the 4 \2 r# e0 f' [3 j. o0 g8 H qinputs is logic 1.+ t% _8 {6 e; D8 z! [( T NOSE CONE, A device on the front of the engine that* B' P, }8 V, J4 v3 S guides airflow to the primary airflow path of the engine.& s/ B8 u; T1 i& h, ^$ k+ O the nacelle for air inlet to! v9 n5 P9 u, V* Z e engine. $ Y- T* ^- E uOSE DOME, Front section of the engine for ' j$ a! N& {. D- Y! Wtreamlining and directing airflow to the compressor.; p( k$ M/ {: W/ q& Y* D/ l1 V ), 2 q, U/ r" w1 i# f3 I" f6 ~ t2 a能够用自 . M: Y, E4 x# B2 Y1 m6 R6 U* y' A定向仪(ADF)确定他的背台或向台方位。 ~4 m: ~$ ~0 k, ]. G( K久性存储器, . B* N' U- D+ s在失去动力或电力时不会失去记忆内容的存储器。 & }! h, }! {$ b0 A在或门后面紧跟着一个反向器的二进制电路。当任何一 ( ?7 R# J# k9 H/ Y! p; w4 x6 w输人为逻辑1时,输出为逻辑0。 , P- e7 A# f7 r0 ?' m一个位于在发动机前端,用于引导气流通过发动机的主$ P4 T- E0 e E4 |! Q 气流通道的装置。 # h# |4 _6 J2 e& \引导空气进人发动机的短舱前段。 9 K2 M X" F& ~# R0 Q部整流罩,0 ]/ G# ^" B; e& E/ d 用以整流并引导气流进人压气机的发动机前段。& c' z9 f5 F+ V# O3 y( i( M# X9 ]: G6 w N, C* \' \, d3 e; V NOR GATE, An OR gate followed by an inverter to fo F; n q" [/ p) G: S1 l0 G' pa 2 | y9 C3 h: W+ X# n* kNOSE COWL, Front section of ; H/ e" t# x+ u- ]0 V7 zth9 }6 Q1 Z5 u' D7 d N' t3 J) E1 r" b6 D) S' t s$ ?( B4 m: e. J, |* ` 无方向信标(NDB. ?$ l4 X/ ?0 d; h 发射无方向信号的无线电信标台。据此飞行员 ' A: c" b* ?! }8 M; | y3 ^& D% M, O$ Y( J$ l8 R( P8 _' ~7 ~0 [: ~或非门, 4 P# c% a0 p* o( ~5 B/ {# ~2 V- q+ S0 X- A- }- | 进气整流锥,4 x9 ?( r! L- y4 | o: {) t4 b. E 前整流罩,6 g1 L' t0 m' U6 x$ T- X7 x8 _8 i) B' d( z% O9 n英汉对照民用航空词典B OEING / w+ q+ \0 Y. W. ~TECHNICAL DICTIONARY 107 # f5 D& Y0 D8 R, L& X5 ]0 }NOSE GEAR, The front wheels with the attachments for. S3 v/ t+ ^4 G, V" i NOT, A binary circuit with a single output that is always) K, ~! h0 ^# U) L opposite of the single input. Also called an inverter. 5 A$ A3 z. \) Ztion that has the shape of a "V".$ ?- }0 K' Z" |! K' _1 `% e t. , d) N5 X8 m' E F, T% FO-RING, A circular shaped rubber or synthetic material % Z% i" \* W3 b' H2 D* ~2 {7 S& L/ asealing device for pneumatic and hydraulic systems.; q6 h! G* t1 M$ m* l6 b PERATURE - Q0 L. K1 i; j* J2 Ee, ~, F+ |5 X" P: z/ @ in the path of flight. 8 }4 B, u; [ r1 u, oOBSTACLE CLEARANCE, The process of flying the& ~2 n+ n: B c# ] aircraft over all obstructions under the flight path.* h/ I5 h! i- D' X& ^' E( o Which obstructions are considered and the amount of 2 ^- b& J" d; T+ G4 Jvertical altitude required above the obstructions are/ u* `. v/ c2 k9 M, _ r. I determined by local regulatory agency.! q+ e4 p `$ i. m 非门, " V( M% _, p; N I带有始终与单一输人相反的单一输出。也称作反向器。 . j; G- @. N$ L7 I( S C# u一个“V”字形的缺口。 # g* [) A+ L8 A+ j! O, q# c喷嘴, 3 b$ O, C. P9 y; m* S形圈,/ B; P7 H: E: S# v* ]% x5 a8 y" P* o 用于气源和液压系统,圆形的橡胶或合成材料制成的密 0 k% d0 A- \) z: Y% S封装置。9 T5 ~- x( j: z- A8 j( ?7 D- ? 外界大气温度, - T( q% {1 L! h/ G1 B" f见Outside Air Temperature2 G1 ^8 @3 p: i! B supporting the airplane on the ground. " {: k1 h1 ~2 C* \6 k+ G5 rNOTCH, An inden0 t2 k( G5 K# s3 u& L NOZZLE, A shaped device for directing flow in a duc * F3 a& o( @/ @$ g! gO + i3 }8 {" f! g$ S/ fOAT, SEE - OUTSIDE AIR TEM# U! A6 E1 R! c; ?. d7 g OBSTACLE, An obstruction protruding into the airspac9 k8 j H3 K( L' o, Y1 J, q! e 前起落架,: R1 k4 {% c1 r* |3 [) { 用以在地面支撑飞机的前轮及其附件。; Z# D1 {+ L" A0 Y! _7 H6 p& i3 z 凹槽,. F! A, i& z7 W7 P% z' L2 \* f 引导管道内流动方向的具有特别形状的装置。; O' `& W! u# w) o" e& e3 x/ { O1 r0 P! q& S% c+ V& |/ P" h2 s# C4 F& B: j) |! @9 q越障,. E2 N7 I0 V9 G6 E 道上所有障碍物的飞行过程。障碍物的选+ r6 E* B) i. I9 w 择和飞机距离障碍物的高度要求由当地有关管理机构决( J- q! \) ~4 b. T1 t# z 定。 . B! r0 o+ g: ]. ^( z障碍物, % r, V& _7 J& @" v进人飞行航径上空域里的障碍物。 9 s1 k" J/ I6 H( P/ [9 a" d, R& M飞机飞越其航. D8 n- \ d+ {7 n: W 英汉对照民用航空词典B OEING + Z" m% `! |/ U+ m/ q1 JTECHNICAL DICTIONARY 108 7 X) O( a5 |8 P3 I) o; K3 ZOEW, SEE - OPERATING EMPTY WEIGHT - |! v6 g0 n+ U4 T9 I5 }FFSIDE, Opposite side.9 j2 Y0 @4 w- \0 x IL COOLER, A heat exchanger for cooling engine oil5 T8 u0 K2 P( E* h6 h; s" J4 |' l by fuel flow or airflow. 5 A2 V; E7 [. bATOR, A device used to separate unwanted - i2 }2 ] [( J8 k- eir from engine oil returning to a sump or oil tank. H1 K0 q( D8 O$ @* M" T OIL STRAINER, Type of oil filter.) b0 p0 l, H. \* E1 K& T5 _" Z LEO STRUT, SEE - SHOCK STRUT 1 d9 Y% q, `& r9 gNSIDE, Same side.' ]: T5 n5 T" `, y9 G ll weather navigation system. 9 k& H; W5 _4 \0 G% uch is not # q% q$ a0 b, D# V: }& `continuous from power supply to ground due to a break% k" N7 d! r% c" C, p0 D in the wiring or failure of a component. ( s. }7 ?- @7 R2 x见Operating Empty Weight : ^* f8 g: ]; ]3 Z+ f* y3 iO$ t0 S' N9 F$ X7 | O , z- y+ t8 a! W: I7 v, `# f: POIL SEPAR % T* G+ K: n/ h, n. ^1 ]8 Na 7 c! x3 D4 |+ U3 W2 t' F! rO2 D# o3 `" n4 |* z+ C O 7 s. v: p, d4 b1 JOMEGA NAVIGATION SYSTEM (ONS), A worldwide,8 e6 _0 w# C/ ~ a 5 m5 U$ U% Z* I7 b8 K' x( D0 qOPEN CIRCUIT, An electrical circuit whi1 k6 M+ A) n2 [$ `" \ 使用空重, ; K+ c* l: A; ~/ ?- k, o' g( l$ d E; N t, q6 z4 C 面,; {( D6 q9 _4 H7 C 油冷却器, ; a- E7 Y6 |/ H) r+ n3 p. w利用燃油或空气的流动来冷却发动机滑油的热交换器。. e+ l ?: y$ c: q 油分离器,- p9 Z* V) S3 F9 ?# B 一个能从回油槽或油箱发动机滑油中分离出不需要的) h3 r( Q0 x9 k 气的装置。 8 Q) s( p* P5 u8 j% Q滑油筛,2 V: ]" b5 R, `: x$ ` 滑油油滤的一种。1 V0 a( q; P* j7 M 液减震支柱,: [$ o" Q' x# d! M: Z 见Shock Strut 7 ]$ I( [+ D6 {$ {' X+ ?& P+ R# X9 }) K9 p' v; d 相反的一面。 3 \$ ]7 A2 t1 h% m$ g. x+ y. I* d( u9 j" h: I: t8 |, l, s( o8 e) L' r; L' @; z0 V/ ^! r3 v7 x6 ~4 \: i- p9 ~9 _* k6 I6 ?9 S. D4 m( R1 |% T' k! l面, 9 F5 S3 V% |$ b5 Z- q相同的一面。 / E5 V! J0 B; a+ K4 b5 W* o8 s7 `个全球范围内全天候的导航系统。3 n5 E' Y8 a! X2 p9 X 或组件损坏而导致从电源到接地点之间7 U1 q3 c7 b G* ` ` 不通的电路。 " v# X) \( B% k5 Z/ Y5 ?) C0 N$ _1 K3 u7 H奥米加导航系统(ONS),$ ? p3 Y& H4 v/ {+ L& S( B4 ]2 F 开路,) H$ `0 D2 L/ |9 h% F @8 c 由于线路中断/ Q/ r5 M |) M, _6 x1 K- h6 I, L6 @ 英汉对照民用航空词典B OEING 9 s8 a, |/ z. Z9 q9 MTECHNICAL DICTIONARY 109# Q1 N5 C8 D- x8 ^6 j" K9 O OPERATING EMPTY WEIGHT (OEW), The weight of 1 o9 e1 s2 ?4 jan airplane fully serviced, including the crew but without8 w( f, y! }) F; W8 ?; }! ?" {+ S1 R fuel and payload. ' ?4 [7 d5 c1 [; e9 f0 l9 |PERATING ENVELOPE, Defines the environmental# c9 U" u3 Q2 [% M OPTIMUM ALTITUDE, The cruise altitude which results, D) a, t+ x# i in the best fuel mileage.2 W! @4 [; S8 `3 J( p* E* V OR GATE, A device or circuit with two or more inputs of; D. r7 c$ {5 O+ T# U3 ~ binary information and one output. The output is 1 when % _/ {6 D. Y' fany one or more of the inputs is 1. The output is 0 when 2 G7 D0 e) n/ n' d9 |+ F5 l2 ]# qall of the inputs are 0. % X+ N5 ?; w9 q+ A @3 Q. yORIFICE, A specified size hole in component for control 2 L6 E6 l, z# Zof fluid flow from or to the component.$ }, l, R7 Z% i; l3 K' w ORONASAL MASK, An oxygen mask covering only the ; E! I+ d# i) R, d1 D, T4 Pmouth and nose." G4 V& ?! t; M! ]& {4 d' ^( A OSCILLATE, To swing back and forth with a constant, ^/ ~5 R: b$ n+ W* f, \0 G rhythm.' K! i7 N$ b- {/ c% K- z& G 使用空重(OEW), : s; ~! ~. z& l2 T) s6 w0 W$ ^使用包线, " q- `) z P" ^; b& `( d- B确定飞机准予飞行的压力高度、温度和速度的环境极 8 ` d U, l: \) G* B/ o6 ^或门, % l$ w! W, {4 r$ {8 H' x具有两个或两个以上二进制信息输人,和一个输出的装; C4 |- Q" g# S6 u' Q 置或电路。当输人端有一个或多个为逻辑1时,输出为逻3 S% Q0 G, E3 `% |+ c) u 辑1;当输人端都为逻辑0时,输出为逻辑0。6 x, d7 \0 R' V7 S/ c 量孔, 1 F! z' p2 D& F7 \ q. F- ~& h0 v部件上用来控制流往或流出该部件的液流的尺寸已确 ( s' q+ r% k9 i% `5 h定的孔。9 |7 \6 ^0 G2 |' v( i 口鼻罩, * S$ d" L4 |3 w2 i: U仅罩住嘴和鼻子的氧气罩。 Q/ {1 k( ?4 ]; v% z振荡,# N7 H# [5 n c 以恒定节律作前后的摇摆。! A% Y# }2 b+ g; o: p7 o O9 _- p; a' @, s2 e1 _- ^ limits of pressure altitude, temperatures and speed3 a6 g, |* i& l; Y within which the airplane is certified to operate. : A Z8 c6 ]9 c$ w8 j一架勤务完毕的飞机,包括空勤人员,但不含燃油和业$ z0 U0 J5 N3 `5 y# t0 r 载的重量。 " k! a+ ?: f" e3 _限。 4 Y& g$ i1 y+ u& L4 Z$ Q最佳高度, 1 Q8 M2 s, H& B5 H( Z7 G# \可获得最佳燃油哩程的巡航高度。 / z/ S% s/ S, U+ p# \; @英汉对照民用航空词典B OEING 9 b' b; |# |9 y: UTECHNICAL DICTIONARY 110 " z- p" N' C t3 J+ dOUT OF DETENT, A condition away from neutral or a+ `4 r8 b2 M0 } B1 R( r5 V0 N: J+ P9 i OUTER LOOP CONTROL, For autopilot operation this ) \: V8 W: w9 \( E$ w& Wis control of the airplane's flight path to a target. + n9 m: z! `5 v7 A* B9 CExamples are control of heading, altitude, and vertical 3 e% o# ?5 |: z# C+ b- ]# dspeed.7 T' q3 |! |. _8 c% D+ f UTER MARKER, A marker beacon located at or near ! ?' A, V) o" u# me glide slope intercept of an ILS approach. The OM is 1 c( r3 i% t; U& j5 T+ L8 tnormally located four to seven miles from the runway 6 X" ?6 S) k& L3 breshold on the extended centerline of the runway. W9 I+ t- k( }/ zW VALVE, A valve in the fuselage for1 J% Y) G5 ^+ J g the airflow from the fuselage to ambient for$ u$ ^; J. R) a9 O. H ation control. * N% \: C: _" m& B5 ~* ^UTPUT, An information signal going out of a system or+ f* R+ q* ?7 z2 i/ [, B part of a system.0 h+ c& W2 K: Z UTSIDE AIR TEMPERATURE (OAT), Ambient, or free5 [6 r3 O% K$ j- t3 I; k5 U OVERHAUL, To return an aircraft or one of its; }" {* I+ @- I OVERRIDE, Operation of a component by a method& j( N% x2 ^# k j' i6 X different from normal operation. % d4 M; l' n' M/ U" C( w操纵杆离开中立或槽口位置的一种状态。 1 Y" H% q; M+ m/ B/ I; J制, * k5 ~* _4 i' c4 Y- A3 @+ S航向,高度,和垂直速度的控制。 ; k1 |! d% p1 @. z* E& ]指点标,, f/ J; U* i8 |3 ?$ z2 [ 位于或靠近仪表着陆系统下滑道截获点的一个指点信 ; g6 X2 a: I+ B% a# V标台。它通常位于跑道中心线延长线上距离跑道头4至71 F2 C2 s6 G6 Q- Y2 j7 A; k# g 海里。 ( ^1 I& ], G6 l8 ^) V/ r+ e流活门,% Y' q7 P; ~! F: f" ^+ l5 c7 f 机身内用以控制从机身流向外界大气的气流以进行增 }$ l+ B- D6 f1 ~+ R! J控制的活门。 + `5 p0 }" i2 m n9 D输出, $ W* o4 C- W7 r! W; Z' }从一个系统或系统的一部分出来的信息信号。 ) O5 l" `" f. ]0 o# y' c界大气温度(OAT),! a( I; W! ~0 R2 ^- r 外界环境温度或静止大气温度。8 y4 @# q5 V+ h" ~ L 修, 8 O/ r, D) s, k7 c; k将飞机或飞机部件修整到近似全新或制造完成时的状 8 @4 y3 j; ~: M W& ~! {, I超控, , S" F8 n; {, H用不同于正常操作的方法来操作部件。 6 ]8 @) O" A6 o2 e8 Knotched position. # U/ B: U, V5 R0 uO. N/ }2 o9 t9 g: ?; z: V th9 B2 ^2 v' C" ]- `5 Z6 `, z( Y9 i& g th: Y+ T# J$ u+ G, n) @ OUTFLO * \5 O7 [- P9 ^; Bcontrollin 6 f5 D l* p- e+ r vpressuriz$ L" C0 [: A+ z' q1 \ O: K o: p0 D% ] a h3 i4 Z0 N+ T. i# eO$ ]0 m. o+ u" b4 L8 t/ J air static temperature.5 C4 ~7 ]! Z! s components to a like-new or just manufactured5 F4 }, Q# e% }+ u+ y4 ~ condition. ; G! h( O% f, \ I. ^+ O脱离卡挡, 9 [2 \) U* g; B2 j' B外回路控4 p4 K6 v! \3 U, d 用于自动驾驶操作的对飞机飞往目标地的航径控制。例 V% C2 b' T8 @7 n; g6 X+ V4 y" F: Y+ z9 ^8 Y0 s" n3 D% s1 k* A! W( Q# _# p% A$ i" \: w8 f" v1 F' g# E) b) [1 q4 G- y" O ]- d# { O/ |+ X) k2 ^" A* H' s6 y' F( _, Y$ i3 ^( U' p4 Y8 K5 Y; s* f& O态。 , p6 T. h8 j, G( U, v英汉对照民用航空词典B OEING! G% `) d+ V0 }$ R# S( D TECHNICAL DICTIONARY 111: S1 U6 H3 W( G P M3 Y. D% C& ?' k: c ACK VALVE, A valve for supplying air and controlling 4 P j1 n* K0 F$ @* imanifold to the air : w8 O( M# L z" l% J5 y; t' W6 wonditioning system. 1 Q) k3 f2 ~! }( All piece of any substance or & L# o) |& z+ X8 _# ]2 Cphysical matter.8 T+ C( ?( Q8 I h9 l+ u* `1 l; k# B rovides flight crew and attendant announcements, 7 z( f0 h+ y3 O6 R6 m- }oarding music, and chime signals to the passenger * S, C' k7 Y; _, e# L8 J/ M# Rcabin. 4 f; G8 M+ N. n, P6 g% J; NASSENGER ENTERTAINMENT SYSTEM, A system2 m% V! V/ }: n5 c1 c& o tertainment to+ S, o6 w9 D: F: l+ V+ h1 z e passengers.6 l' p0 s6 C5 r' f3 [/ s PAYLOAD, That which is carried to the destination, + y' T2 U5 E5 xuch as passengers, cargo, or mail.. ?0 X8 j8 H# |, \; B& Y CA, SEE - POWER CONTROL ACTUATOR 5 _; `* D3 C- {0 m& }& T2 lPDCS, SEE - PERFORMANCE DATA COMPUTER : s- j5 D- y9 |) Y9 Y9 FSYSTEM 7 G- [! M8 p+ o" h8 [- g调组件活门,; G! Z# J* e$ {, ~( W4 L: ? 由气源支管向空调系统供气并控制该气流的活门。9 \2 D8 a5 ?/ y( `! F" ^ 任何物质或实体非常细小的一部份。 / a3 Q) p$ W( M/ Y2 t旅客广播系统, 1 I- I3 I8 r# F' h! J能使机组人员向客舱进行广播、播放音乐和发出谐音信, {1 ?( N& s2 [2 b2 o4 }1 C 的系统。/ ]4 _# b' ?" _# N7 B 客娱乐系统, 1 t$ Q4 M7 U5 |( ^ ^# O+ M频和/或视频娱乐服务的系统。5 `, g5 b% G& R7 h 由飞机送往目的地的载重,如乘客、货物或邮件。 2 R8 I) I: q: ~* }* K+ e- W4 t( U力控制作动筒, & g3 j# e" V+ o" T+ }见Power Control Actuator A( ?2 C5 m( _# N. O P7 P, F7 @) D: C" V) C- o air flow from the pneumatic! f8 P: ^' x2 T* S5 x c, }# i j8 t8 b: t PARTICLE, A very sma \+ ~ {6 E& s9 ZPASSENGER ADDRESS SYSTEM, A system whic8 H- ^% j1 s* U6 Y) V. Y( { p% h9 w3 `0 T: |+ k) |' E9 ` b 5 R4 q- R N# E' I) }% _7 _3 NP( N: M- m2 k( K7 W) }- `& t8 T9 _ which can provide audio and/or video en x# Z2 a: A/ e9 t1 ^6 h" i% pth( P6 |4 P: X0 i( J1 E% z0 m7 M s; P0 j: P( P) Z' n, W9 [( [" h+ s P / z/ g; M5 }3 kPCU, SEE - POWER CONTROL UNIT# P7 I. {9 w% t6 o) X& K% D; r/ i H w% G/ [# P微粒, _$ R; o0 i9 c( T# E4 m( ?* h: d, t' ^% L; t# P! v7 d2 c, O6 Q' B向旅客提供音 & f( C- N+ c) q6 a+ f9 x业载,2 T+ ~8 w% }3 C0 h$ l% x/ A4 J' y) o9 R .( d: M0 O; m1 b Control Unit * ^% R- j) A/ u& P6 |4 y5 N- F动力控制组件, 8 S1 D# R% I8 T见Power . $ g% Q8 H7 V& w# l3 ^" w4 N性能数据计算机系统, 4 Y! F/ [" R4 P见Performance Data Computer System.- A6 t1 m% v0 f) z" {3 S5 p! [ 英汉对照民用航空词典B OEING " P( Y* ]7 J7 ^" ]9 ^' oTECHNICAL DICTIONARY 112 7 {1 M& d/ I9 ?' q5 u' X: u8 X% ~PEEN, To cause a more corrosion resistant surface by; j' K0 I$ ]! G) t9 m8 b multiple impacting it with a hard material such as steel. x- Y5 A$ d4 n0 L( O) s pellets. Term for this is Shot Peening.% e% D6 A* M# N, {) _3 u. X" Z Defines a position on the aircraft relative to the mean + k5 ^3 Y0 U* P& K' e/ Xaerodynamic chord of the wing. # |# }7 Y& j/ t) ar as a percentage of a fixed ; y1 }$ T w% A- n& kmount rather than revolutions per unit time. & w3 Y8 c! \$ P1 l3 Y& Hamount.8 f' J, |2 U6 S$ _ ERFORMANCE DATA COMPUTER SYSTEM (PDC, 1 ]9 d2 Z% s/ D( f# uPDCS), A device which provides data to achieve the / c/ @( f: N% C* t3 Umost efficient and economical operation of the airplane.6 s ^* Z! ?$ ?9 R6 Z4 Y3 U1 W PHASE OF FLIGHT, A portion of flight specifically % ]* _8 L. G0 @devoted to accomplishing such things as takeoff, climb,. i# y& ]& ]0 s5 B8 q cruise, descent or landing. & S0 L; S; i# k! x这个过程名为喷丸硬化处理。 * X3 v( m" Z r$ @# T平均气动弦百分比,* [& ?8 @5 z7 J. z' {9 c! D 间转数来表示低 : d) S% [! X+ p2 ]6 m( F# ~5 z& f ]* _压压气机转子的转速。) M( s6 [" Z8 _- M" E; c0 I 性能数据计算机系统(PDC,PDCS), & a* P. @# k& X. B+ Z T8 e/ [一个能提供数据,使飞机达到最有效和最经济的操作的 ! l, J' F2 \7 F* R3 ~ j5 l2 F置。 7 U. _- |- T+ C1 k- F6 v/ ^行阶段, g! m3 i o( W& T 飞行中负有一定任务(如起飞、爬升、巡航、下降或$ i0 {" L, W. i. y$ [; P( O 份。 9 b8 v. F3 T! |* Z- T$ V; d0 EPERCENT MEAN AERODYNAMIC CHORD (% MAC),+ z6 t. f b4 T2 N& W PERCENT N 1 , Expresses the speed of the low6 b4 u8 a* h+ X4 q pressure compressor roto0 a" V3 m M+ W0 `4 B a5 Q% S& k% S; }# o$ |, \2 |3 r9 G PERCENT N2 , Expresses the speed of the high , G8 e6 A$ P( {6 C4 Rpressure compressor rotor as a percentage of a fixed ! t6 D7 E- M. Z8 PP# J4 e! A% w: R- @ 喷九,) n$ V. c/ U( ` 为形成防腐能力更强的表面,多次用诸如钢丸的坚硬材7 u4 h9 `. G; s+ Y+ v3 N 料冲击表面。1 T- c9 W) K+ A* `# @" } 用来确定飞机上一点相对于机翼平均气动弦的位置。 ; D. J, q! S1 DN1百分数,* ?; u& Z4 r( m7 `* b. } 以一定量的百分比而不以每一单位时 / q5 F) c7 U" n1 K& U5 y ~& ZN2百分数, ( a; \+ T3 a. `- @以一定量的百分比来表示高压压气机转子的转速。 ( G% H; P% Y$ m3 r! _ f; Z2 ]( I @" m. _6 G6 s+ K& j) y6 L着陆)的部 , F% Q; k& C3 B" P英汉对照民用航空词典B OEING2 E% M* u+ T+ y) Q, R1 k8 Z' S* I TECHNICAL DICTIONARY 113 ! p% W0 R* `( D# s4 u! U# ?# fPHILLIPS HEAD SCREW, A cross point screw with two3 v4 u/ ~! T2 s0 q, f en with a flat tipped Phillips head , m$ e0 f: ^8 ecrewdriver (see Reed and Prince).! M$ O( L2 W! ]; ?5 z* T6 l ITCH, The rotation of an airplane around its lateral& X% g; F- L- |+ j5 H- F5 m/ H8 h xis.4 G) I+ c. E _- I+ A+ e ne % S+ b2 J$ a0 rose up and down movement controlled by the' H/ y& [. M; m: \+ M levators (and stabilizer for trim). $ ~: J$ q7 O, J- `( H2 o* HITCH RATE, The rate at which the airplane moves in3 S; b0 x. V6 }7 X# }* v: {+ Q e pitch axis (nose up, nose down). 3 X/ t' K" b) b& u5 R) Y( e. tTIC TUBE, A tube facing the airstream . U3 b/ n# h$ n$ H8 g" h" Ahich measures ram and static pressure. Used by / y \8 |1 ^" W, u4 Birplane instruments. : q8 U7 p& h& j丝钉。由平 - J7 Z P i1 G7 E十字头螺丝钻驱动。" j! B3 b+ _8 S' R" q" { h 仰,4 c+ C" D5 Z6 s5 {" A6 q% a) [! h 飞机绕横轴运动而造成机头的上下运动。 1 s* q+ h! o* ~* c% r) j9 ]一侧通向另一侧的水平轴或横轴。升降舵控制3 n0 t# E* R3 }& B$ g8 w 头绕此轴作上下的运动。(水平安定面则用以配平。) ( Z4 e: l* l3 i' {. }4 v$ ^! m$ B' G俯仰率, 4 C& e: S T% `9 k) y5 C飞机绕俯仰轴运动(机头向上或向下)的速率。 % P5 K# a# G$ R$ f$ M) @管,) b- ^# w& R) T* b 开口面对气流以量取空气的总压和静压,供飞机仪表使) j/ q1 O0 B9 o# s 的管道。 / t4 {2 b; s6 P- }( a! h0 kdistinct tapers. Driv" H# ^* x; {" ?" E8 [ s $ ^ K$ {6 d/ p: Q% r5 @P3 f2 F: U. q; E3 v+ K1 c! }3 D: d a ! I2 K9 }" x5 W# a9 l% [/ yPITCH AXIS, A horizontal or lateral axis passing- R0 `4 }6 _4 K% E! z3 `6 T through the airplane from one side to the other. Airpla & n0 A2 m! k/ d* K8 ]9 |n 4 R+ i7 t1 Y2 H( y+ P" ee 2 [* j8 R. q- {- a/ J4 W4 A& lP ) }7 d2 O, M4 w2 Oth& p! U+ u$ Q+ E' S PITOT STA - p/ s1 d( n$ {2 Iw$ o! \* _0 y/ R. u% T' P9 f# b4 z" E a & x- S# p+ w Z! U9 k2 u$ |% r十字螺丝钉,' w1 \# y! o- G 螺丝的顶面有两个明显的锥形十字四槽的螺 $ N/ i. W+ D4 l* s6 a3 l. H4 u8 k9 ?/ `6 w2 E0 s- x$ `# A3 w1 E) Q: g( d$ C' J* O# A. r/ X 俯仰轴, 3 e7 c- m/ \2 U4 ]2 w8 e从飞机" R4 E; M" S% {8 P" E9 F S4 r% h$ _9 v 总静压 & u5 J& I& ^4 w: P$ y7 u1 I3 M' n- [) y, N9 ] 英汉对照民用航空词典B OEING # G9 G* l; h* M/ `- f+ `6 ZTECHNICAL DICTIONARY 114 2 ]1 {6 b5 \' W5 r7 n8 MPITOT T $ D* f9 L& r2 w# J6 j+ N1 tmeasure 0 \+ G8 ^4 v) S/ EUBE, A tube facing the airstream which- X& C U+ ]6 r s ram pressure. 4 K- @- D K. y' y( n1 uPLA, SEE - POWER LEVER ANGLE 2 B, ?7 o; [. }0 @r! z6 A' ~! B/ f1 C6 \9 r1 T e , W/ M" V* p8 C. JLEXIGLAS, A registered trade name. A transparent& X# Y* g. o a3 m r any purpose. 0 U: ?" x& Z$ W% PNEUDRAULIC, A system or process which is a ! L) l, H: O% \9 _( f3 tres. ' w3 I. V- ^% W7 J9 E/ f) F% mPNEUMATIC (NO. 1), Cold air, controlled and/or8 o# [/ n6 f9 ~1 o$ e# a" n pressurized.0 O" {; Q A; Z5 y7 s 托管, |: r5 c2 x7 z5 a; A面对气流以量取动压(冲压)的管子。 ) e4 d# {. t J' o# d门杆角度,0 J, z, ]5 T( ]' a: o( X 见Power Lever Angle+ `3 y, n+ I: R3 f" Q4 ~, X g PLACARD, An attached sign providing information o, C4 H1 ]4 v0 G: b' @ instruction. & E* i1 H! r, @* ^, b8 s9 ~PLENUM, An enlargement in a duct which changes th8 }/ l& E9 X( d3 N- `8 v' W$ w4 ` flow characteristics of moving air. Used to remove 2 x- M6 P# [7 C9 K8 d5 `' H+ vpulsations caused by variable airflow.7 [! h9 }: U7 P3 V) v; p: z! ~ P + U8 m1 O3 N) `% p& a4 k8 Jacrylic plastic material used for aircraft windshields and , ?$ p" [' z$ Z: P- }/ M3 lside windows. JARGON TERM - sheet plastic of several% V) G( M6 c7 Q0 ]' x& Y- k types and used fo% D9 x1 J% s/ J PMC, SEE - POWER MANAGEMENT CONTROL 1 q9 S+ O2 O! M7 Q6 h' y) PP- a& D. T3 i/ E; E' `& x combination of hydraulic and pneumatic pressu" ?' D( v! |; f7 P1 p0 G0 z$ o' D9 u, P; d6 A* F7 ?' p4 _8 ]- K# e+ v5 Z5 n" p' ^2 S) d% B5 G: m# V' x# m5 U1 \ 脉动。) j- g# l2 s4 [$ }+ T1 b 机玻璃,! z: w. C% N, [6 n 名。是飞机风档与侧风档所用的透明丙 5 ~6 ^' ?( s8 X+ ?4 Y6 {控制,; K1 r% m. W$ p2 P* v- _ 标牌, ( T. q- {& ^5 D, J+ V提供信息或说明的附贴标志。. _1 i8 o' X3 n; S& t' V 整流腔, & \2 O a9 n7 Q0 l' B. {9 \管道中用以改变运动气流特性的扩大部份。用于消除可7 t# ~5 v2 h/ L/ v: O \ 变气流引起的 7 `3 {/ v% b! A% D- U7 A* T5 o1 F. {# `3 {1 R是一个注册商品 3 ~$ `/ _0 p7 K9 F7 ?/ j3 L烯酸塑胶制品。行家称之为多用途化学合成胶片。 7 h3 Q5 y7 n3 e# ?2 ^动力管理5 { f) `8 a# d) e: x5 x5 ^, L 见Power Management Control. % y+ Z5 N$ @2 g% K3 F动液压,9 |2 P7 L6 z8 i$ N V; C* K3 y 推动的系统或过程。 7 `9 N% v" h/ q- U( ]" _1), 7 @6 M; t$ g: }. D8 |! a4 D; d: E/ p. @( O6 R m ^! L( X M由液压和气压混合 1 ~4 r& T% }2 P( }压缩空气(NO.. ?8 m w! W9 e' v3 `+ F 经控制和/或增压后的冷空气% ?' g2 K+ l! ^2 J( _; @% C% `! v& { 英汉对照民用航空词典B OEING . D( p* K4 z/ m- n) lTECHNICAL DICTIONARY 115( y4 K* q0 B5 v- d3 S PNEUMATIC (NO. 2), Air, controlled and/or " G1 s) T {+ X* p; Rpressurized.2 ^% p$ j. O& K& m0 u1 L, T! g/ ~ OP OUT INDICATOR, A device on a filter which 4 `* {+ c; R; _7 g& E7 c9 Oroughout a material.3 _) W1 C) j& k; `1 O ition.+ q& U9 ]0 g" P POSITIVE, Definite and intentional. c Z9 w$ W. ^+ Z5 U(No.2), , q$ h. D! M4 ]( ^9 u出指示器,: G* v2 }/ t/ W; O9 X' K$ f. U 到达一定的压差时,它会从壳体内 ( S# Q! N, d0 ]( t& T指充满整个物体的细微小孔或空隙。 " P4 J* |/ n( X7 C置基准的飞行管理计算机的一种操作。 $ r# w$ l5 N1 A. |: @! |肯定的, " w6 f! Z8 G- e一定而且有意的。3 w9 B. n. t, h4 e3 E" h- i P ; h# E% G9 X& j6 \4 j' Fprotrudes from its housing when a specific differential 1 h# u" }1 J" Y( d c! Vpressure is reached. / y5 }& v g* Q& i6 B# }5 I3 p( |POROSITY, The term for pores or small cavities' @9 J' H: T4 _5 v+ s+ u8 t th( U# _9 o0 ]3 S' M POSITION SHIFT, An FMC operation used to change + ]( U( B( _+ P+ |0 sthe reference of present pos 4 l/ M0 h6 F; U' P! Y压缩空气 , t0 `+ \8 K7 ?6 g' N& j经控制和/或增压后的空气。 8 b3 o/ U& ^% r8 u' P3 Y# B2 z3 y7 Q' P E/ F, p. C 过滤器的一个装置。. t1 O) b3 {; [' N 伸出来。" l l1 w7 H" J# \! ?' t 气孔, # n; E5 D/ X' J9 n8 t移位,2 v# z- P( g+ N' O% p* q% ^ L 用于改变现在位6 J- H4 c: h, X2 U3 i 英汉对照民用航空词典B OEING / C: c% u& J" l7 e4 m' XTECHNICAL DICTIONARY 116! I+ \4 E) q6 L( j( y/ v POTENTIOMETER, An electrical device for changing$ |& A: W o) `+ i8 v. m+ o the voltage supply to an electrical circuit component. + e! N# d! R) z1 f& }4 {r+ I3 F- m0 n5 q* [ bly for operation of flight controls. 9 t. n1 ]( _& X/ y8 ~+ [OWER LEVER ANGLE, The angular scale on the6 B; h3 v& J! T& i, R! H main engine control for showing movement of the power( z }7 e: \* k! c; b hrottle) lever.% f t8 K, m8 d OWER MANAGEMENT CONTROL, An electronic " A' t3 P( b; qngine control.0 `5 G+ t0 F& w1 l( u OWER TRANSFER UNIT, A hydraulic motor/pump for $ X0 g3 w% u8 v5 ]upplying hydraulic power to components when normal $ S7 C. V( g. l8 J8 Y8 F/ t9 r3 ]" s0 BRECOOLER, A heat exchanger in the pneumatic9 F2 [; b3 K) j/ v9 s lied 2 M) B& b5 Z9 j5 h4 s作动筒, k' s4 P1 O4 }4 W6 G# m件, ; l( p! j- I1 G( h/ T1 K油门杆角度,+ N7 ?8 [8 \& y- t1 p 主发动机控制上用以指示油门杆运动的角刻度。 8 L( P1 B* V5 |0 y动力管理控制, ! y c2 i- G, ]0 M控制发动机的电子装置。 ?2 v5 P# M. G. l. k) k0 t3 ]力转换装置,; d% m2 `$ d, W- ^ 当无正常的液压来源可供使用时,用来向部件提供液压. `2 g" z4 G4 L! H 马达/泵。1 h: R. J4 g1 d3 c9 B/ |6 T 冷器,# K, v" q/ S x 中的一个热交换器。它将发动机引气冷却后 4 y1 Z+ t4 q/ s# @, n1 _供给气源总管。 # n" Q4 p, |. PPOWER CONTROL ACTUATOR, A hydraulic actuato! u: y" \- h/ ^4 g" p3 L9 X assem$ R* O( J( W/ X& v) g POWER CONTROL UNIT, A hydraulic actuator6 Q2 `2 r8 {. s8 ?3 X2 c, ^5 E# p assembly for operation of flight controls.3 d: J* @8 w8 P. ? P 2 V8 j2 y) a- i w(t7 c; y$ w+ Z' |4 U* G# W1 g P2 D4 G( W6 v: t; x8 I& U; w& u e4 M- X/ b5 R9 V- {9 } P. V; \6 X. ^# g1 U s ) T/ m7 J: o/ Q3 hsupply is not available. ! i, x- Z$ ]* l. uP 1 t- z5 X# b" |1 `% U Ksystem for cooling engine bleed air before it is supp 8 S7 b8 P) C5 b6 C% T4 E7 b4 zto the pneumatic manifold.7 Y5 K$ a4 y; e, ]3 C' }: a$ W2 n 分压器, " {8 y0 Q0 K2 K+ `) G- Z0 W h2 T* r用来改变向电路部件所提供之电压的电气装置。7 s' g+ n% U7 f* [; C- O 动力控制 : k; K6 d9 r) S# p6 N1 D4 b2 }. s0 w用以飞行操纵工作的液压作动筒组件。# V2 g# B5 X- |3 O( A 动力控制组; `! c+ Z+ E, o1 _: e4 U4 O 用以飞行操纵工作的液压作动筒组件。 u8 F1 e% q7 b U2 z1 S; s* K0 K, n/ ~( e/ c4 O$ Y动力的液压 4 J/ q6 n# D! Y4 T4 C- [4 ]7 X" {4 c 在气源系统) j1 y6 E( N6 K. D4 U! B 英汉对照民用航空词典B OEING " i/ N- }" i: p: LTECHNICAL DICTIONARY 117 ( E8 i5 `1 p" P6 `7 r+ \3 qPRECISION APPROACH PROCEDURE, A standard 3 R& F, S+ r4 n, D& e; p' i% Z/ _6 xedure in which an electronic5 Y; D" q+ |4 F( H lide slope/glide path is provided; e.g., ILS/MLS and 2 b/ _. [7 f) s" S/ MPAR. 6 b0 G2 b. u0 Y. Y: @) hRESSURE, Force per unit area usually measured in & j$ M, g( G5 E! g- S: mounds per square inch (psi).3 ~! {- }8 {0 z( X, f; T0 D) [' T RESSURE ALTITUDE, The altitude displayed when & n& d. J# ^$ {0 W2 D$ qe barometric pressure on the altimeter is set to 29.92 7 S( S, a5 l' i9 gRESSURE REGULATING AND SHUTOFF VALVE, A : q+ s' U [" u6 E8 A: ^$ ralve in the pneumatic system for regulating bleed air . S) n& S a! `( Y0 c J: zpressure from the engine to the pneumatic manifold." x: h. M; ~- ?. u; G RINTED CIRCUIT CARD, A plastic or fiberglass card 2 V, J3 {8 L9 E1 r8 r; y9 R* qith electronic components and copper strips forming a 8 S' e" w3 H$ k$ I- q* ~, Circuit.- L; v5 ?7 T" N: w; ^/ ` RIORITY VALVE, A valve in the hydraulic system for) J2 B7 z. Y: J' w ROCEDURE TURN, A maneuver where it is J1 n! w6 V& e) g lane # ^, z: _4 X4 Tproach course. + ^3 G, K! ]+ O. d& \' S9 b精密进近程序, + y0 m6 ]- x$ l- {8 v' r9 [己提供有电子下滑道/下滑航径的标准仪表进近程序。 " v2 O1 O# p, p1 q6 ]- P如:仪表着陆系统/微波着陆系统,以及精密进近雷达。: z; b: t) n8 i; Q B2 ]: F' { 压力, 1 p7 W- B# k2 C$ n0 n$ c单位面积上的力。通常用磅/平方英寸(psi)来度量。 9 G6 w& f9 F* x: i, ?5 B9 u$ ~5 q压力高度, {: H0 V0 K. x1 x8 _; q+ j% x4 U当高度表上的气压调至29.92英寸汞柱时显示的高度。 8 x* A5 A8 I* M! _8 V2 C3 C7 }力调节和关断活门,6 \4 v. h9 Z/ g 气源系统中用以调节从发动机到气源总管的引气压力 ! z7 I! S- ?: g( y的活门。 / V8 C+ b+ C0 c5 m8 M刷电路板, 4 J' V. Q v, f1 X% O- K3 `由电子部件和铜丝所组成电路的塑胶或纤维玻璃制* e- s7 Z# j; H( U3 [ [6 o+ Y 薄板。 $ \8 i' j: D' z" {8 e先活门,! G/ y, u- e; o7 S ,用来使各部件照合适顺序操作的活门。* z1 j. H$ R) b 序转弯, ! e, M6 {0 W" d" K" i Z7 Z5 O后进近航道时所做的机动动作。 * N1 {) F% ?7 p winstrument approach proc * w' L/ e5 f- [( E4 [. k1 ]g 1 W/ T6 ] Y7 n: F' JP ) y1 y1 \4 V: E$ _" x! l+ {p5 U3 f9 H, C9 W" J, z( F+ ^( Y$ W% T& s P% I4 W2 T% m8 } th- C9 |" B& |! v; ^% x inches of mercury.% r; G. G; t! N9 a) | P% q, s& w( H3 T9 v3 g2 n* I/ l# A v 4 n2 R1 ?2 z( @P$ I2 \! r; C! Y/ r% E& i1 l& b0 P2 x; j w; |3 E3 E- K* x9 @1 m7 N2 X- X* A c& z( b( n5 G/ H! b2 k P. ~5 s& |: L) `2 u1 x6 L7 H* K/ _ operation of components in proper sequence.' H @6 Y9 u4 d# x) W P. a( x# T6 @1 h( D% w; n necessary to reverse direction to establish the airp 6 ^3 y6 v# g Jon the final ap : m' P$ m% n; X. M8 s, Q. V& B6 q) H2 D4 t6 D/ w/ C: r% R( a: x+ {! ^& B. I' C2 C0 L1 B/ m# k' w$ r7 r c液压系统中6 h6 K) ?+ G- ]- h1 r Z! I' u* _8 p2 s6 ?4 {在飞机必须反向建立最 9 Z2 f" F* @! c- h, l' O英汉对照民用航空词典B OEING 5 ]8 d9 K3 C* W2 x" T+ [+ LTECHNICAL DICTIONARY 118& K. }1 e/ T j+ C PROXIMITY SENSOR, An electromagnetic d ' ?+ G& x2 ?! T) _+ M, | Zsenses the po4 d- `3 C& Z# }3 c Q evice that 3 S" G# S, J& c4 wsition of a moving actuator. The sensor ) B+ @5 }! }$ X. h) S: Ias two or three wires." J2 z: f, P, Q* Q1 j6 } ROXIMITY SENSOR ACTUATOR, A steel plate . v) Q2 N3 e7 X* Z8 D) Rcated on a moving component for operation of/ k# U9 z4 R8 B0 u/ N' s8 l# D roximity sensor. 5 g1 c9 ^5 A. W1 @5 V% t5 N9 {" RROXIMITY SWITCH, A printed circuit card for p3 h9 G6 Q' d) N1 i7 ytransmitting sensor signals to indicating lights and / c1 Z i, I; f8 |6 z% @, d邻近传感器, - p6 ~ r1 O9 T7 _+ y能够感知运动中的作动筒位置的电磁装置。该传感器, Z# \1 L0 f2 U 有两或三根电线。: F; J1 v% q- i+ v( S 邻近传感器作动器, 9 r1 b* V3 @; G位于一个运动部件上,用以操作邻近传感器的钢板。8 M" N% j# A" c- ]+ w# Q' s 近电门,, Q: S0 a. @$ [, s, G 传感器信号传输给指示灯和电路的印刷电路板。8 x8 D) m' ^# S/ U: C' d! ^# n5 K h1 U8 [5 ?, z" c* A1 v; H" | P % ]" b8 r; [ [' O: J8 blo : `1 t) G6 g" v p+ Op+ Z$ S# T, ~, V( m( B6 W6 N P. I) t( \' g6 Q4 i1 t circuits. ( W3 N1 w F' _1 T! `- e2 {$ y; w* G7 s0 |0 R用以将 # I& G4 S4 X. @- W! d; L2 ]6 l7 ]英汉对照民用航空词典B OEING ; ?& j1 ]. Z* R/ K) q$ [- GTECHNICAL DICTIONARY 119, c6 p+ A+ p! m6 a PRSOV, SEE - PRESSURE REGULATING AND! n6 `5 O" m4 \8 `* ^( s, a SHUTOFF VALVE( ?8 G+ T2 M- H0 a, v* w: A6 x3 J TU, SEE - POWER TRANSFER UNIT$ [% _4 ~. n3 d# n! W1 w7 G8 z! K. r& v removal of dirt from the air cleaner.; d: u/ C$ M6 A! _/ o8 h7 ` n 8 v5 I# [- D# z5 \QAD, SEE - QUICK-ATTACH-DETACH! P' m5 [/ W! H- n& K ICK ENGINE CHANGE ( z5 t& J& ^) P1 f; f( F" a5 Lheight above airport elevation.% P; z- q: D t6 l' T/ O NE, Altimeter setting 29.92 inches of mercury, 1013.23 ~) \) J& ~3 o/ G N6 X QNH, Altimeter setting which causes altimeter to read: p! ~( ?9 d# x6 X8 |& Q( i% p height above mean sea level.2 r- D( ^( c$ O( ?& f& T 活门,9 m9 p$ X8 Y$ a2 h u1 N P # M1 |- o8 ]1 A- ?PURGE VALVE, A valve in the pneumatic system for / b& T$ n8 b E9 u) A8 F( @PYLON, A structural component for supporting a/ f* p* V' X. D, r# w+ b+ p! J2 A engine from the wing. 7 G1 \1 l! Y$ R- rQ9 ~. P( [4 T2 p1 m/ K/ ~; @9 K QEC, SEE - QU ) W: H: [) {7 }7 D. V$ |. cQFE, Altimeter setting which causes altimeter to read & a3 b" ~& w7 T$ x1 aQ% J/ @& {* \- P) U; T) n Hectopascals or 1013.2 millibars.- [' P1 L e: b5 N; ^3 K0 w 调压和关断 8 y0 O" I/ c1 P8 z见Pressure Regulating and Shutoff Valve. + |; B4 X, I* ]* y G5 o4 h. |5 v动力转换装置, # v, t7 d8 e7 m见Power Transfer Unit.1 X' _( g$ y# {5 l. s1 _* B2 I 气源系统中用以清除空气清洁器中之灰尘的活门。7 ]5 k& K1 }; N5 I) A' M( o1 O" t 速装卸, # w/ k! O2 {! C$ ~3 `见Quick-Attach-Detach + R0 \% }5 P1 A) k/ r Z+ ?除尘活门, ' u- b- D U3 S$ N- e吊架, * J% {6 `# @4 K" i用以从机翼支撑发动机的结构件。 & |) K: _# v/ R9 k7 S( D' t. ^' u, d# t. d+ \" x/ s0 t0 ^: m, k6 a4 r) n9 I 见Quick Engine Change6 \; }, l8 g) S0 \7 S$ d 快速更换发动机,' {& ?" x( {( C$ w' y, Y/ f: j5 N3 W. s场面气压,4 i8 R, Q: f$ E# j3 h 准高度表设定, 7 ]6 r1 [+ V3 p# ?: w; `# a2英寸汞柱,1013.2百帕斯卡,或1013.2毫4 R2 f- Q5 q3 Y! q, B$ H 修正海平面气压, % O9 c# c6 v. _! ?; p! |& y" u使高度表指示飞机距平均海平面之高度的高度表设定。 # X9 Y3 t( a/ S6 A使高度表指示飞机距机场标高之高度的高度表设定。! A" q& |& O$ o) |! A D5 \& m& p) D) ]1 T( F 29.92 A/ o* u: r( |9 {$ v 巴的高度表设定。 ' F% u8 k- W4 }7 c) t/ E英汉对照民用航空词典B OEING ' t5 J$ l: d! B( K+ yTECHNICAL DICTIONARY 120 0 j2 M, `) Q4 G5 YQUADRANT, A mechanical component shaped like a7 n# M5 R: Y$ O, P quarter of circle for transmitting cable motion in airplane * N+ @ O9 y' QQUENCH, A heat treating process to make the surface+ c4 ]+ \7 _2 _. X( @$ B* ?* } of a metal hard. The metal is taken from the furnace and- {8 R- `: g: k' U0 [ Y QUICK ENGINE CHANGE KIT, A collection of% X7 V/ _; p0 ~) u2 ` e engine positions of a particular model+ W# p- Z D4 X7 R: G! e irplane.2 R9 Z/ P) o) b* o ng/ ] \8 w' P2 n. |. j8 c6 d! r, u2 \ accessories (hydraulic pump, fuel pump, starter) to the # }6 s8 V. D% _: \; Q: ^- dengine accessory gearbox.( s% X/ M1 t# \ S, Established the ! c. N9 ?8 Z6 n+ bminimum amount of time to cool the wheel brakes9 k# G, F# \# D; C# R before the next take off is permitted. 8 }# |$ V- A% t: @" Q0 Z* L进油或水等液体中。 - M( N% `" U, L/ A! g& q% m快速更换发动机成套设备, 9 W: t# s: ]2 O. S* H0 b& m置的所有部件的集合。 4 }2 r" L% K" x9 \" d8 M用以将附件(如液压泵,燃油泵,起动器等)接到发动, n! A P: b) H& @- V 附件齿轮箱上的夹具。 : A9 w+ ^% Z: I, r4 o快速周转极限,( t1 l( R2 D+ X, b1 D+ E1 g 在下一个起飞许可之前,已确定的飞机轮刹车的最少冷+ e# J6 j1 \ L p) t0 D+ A' d( F 却时间。 ) T, j8 y3 i/ E- `control systems.5 M. S# k0 @) b! M0 a1 P dipped in a liquid such as oil or water.3 h) r1 Z: f8 x4 M3 a+ T: k components allowing installation of a basic engine on to) x) u& P6 H6 o: n: O; V any of th% y/ u, b% e9 _3 V9 } a * {% K s- s" J4 {( Y* uQUICK-ATTACH-DETACH, A clamp for attachi* f; t+ N2 E$ E" G$ e% g QUICK TURNAROUND LIMIT ' T) v' C+ L+ ]! c扇形盘, . n/ A i1 ^ k3 p& J飞机操纵系统内,用以传递操纵钢索运动的扇形(四 i/ J3 P- F' @ 分之一圆)机械部件。7 |# T9 O2 J/ O8 v8 k2 v 淬火, k2 j# ~' j& _) @/ M: o一种使金属表面硬化的热处理过程。钢铁从熔炉里被取 3 U& l% l! @. u! a4 i& ?) f1 ^出后再被泡 / s, k( E1 B4 B2 B( U( s$ M; c% ]用以快速地将一台基本发动机安装在一种机型的任何! U; \6 H$ A0 }$ O% ^ 发动机位3 ~) X& Q# Q8 J 快速装卸, * T; n% H0 W/ L( s8 M8 c3 a" M) Y5 c英汉对照民用航空词典B OEING8 U8 Y& T, X% o0 _! g8 @ TECHNICAL DICTIONARY 121 % e) I( Q: S$ S( v3 W" eQUIESCENT, Condition of an electrical circuit when no 8 h0 Y4 q) A# m, g' ~0 I) ERACK, A place for storage of modules in the ) G" Y/ L! d2 S5 c+ {$ m$ n: Clectrical/electronic equipment compartment.1 }2 L0 C! }4 s( U2 w ADAR, A device which measures the time between the + {7 E- ?/ [8 z9 ktransmission and reception of radio pulses and provides % C( o' ~ G/ }( Yinformation on range, azimuth, and/or elevation of 8 F3 j, R# i; P* V* zbjects in the path of the transmitted pulses.* L; h5 @. {% j2 W om a, `& C4 V' s. ]0 A ar.8 S, ~6 b6 f- L RADIO ALTITUDE (HEIGHT) (RA), The distance of an & J3 d. C% p% g$ i7 L0 Waircraft above the ground, as determined by a radio- n- g: ]% J7 b5 E& K& s altimeter system. 8 P; k, x. P5 C+ N7 G8 ` URAM, SEE - RANDOM ACCESS MEMORY 6 X& i1 F7 ]% X. _4 Z* `# qRAM AIR, Outside air that flows through heat 2 I" Q- D N0 a6 B- Y, r( @" [exchangers in the air conditioning packs. % P2 r: R1 T. b支架,. h# v8 z: v4 F$ W 电气/电子设备舱内,用以存放组件的地方。1 t. m4 K: l p0 ~9 x 雷达, , Q0 S, t% d% }测量无线电脉冲从传输到接收所需的时间,并提供范$ K. m% z" C. X( Z; H7 ? 围,方位,和/或脉冲信号传输途径上物体标高的装置。$ d; `. v5 d" Z* z- {; s t+ w5 s 由使用雷达的空中交通管制员给予飞行员的航向。 6 d0 C9 K7 }& N# _! j) F b施发射出来的磁方位线。% a& U/ h: _+ J/ B+ }5 Z- K 无线电高度(RA),6 {0 c) \. j: w9 [( {- L$ O7 S 由无线电高度表系统测定的飞机与地面的距离。 & R; r3 p% W. L0 d$ k随机存取存储器, : A; M3 D; U- E4 s* Q见Random Access Memory / V! ^1 d; @* M `1 {0 }9 tinput signal is applied to it. $ a. C( [: j: F6 fR5 E" o! V" x5 z7 R, X+ d e/ ^* E5 e$ v' _% s! n/ J& h0 @ R+ Z; H" h. z4 F0 p& l1 p o. F3 ] U* R2 _. |) H& t RADAR VECTORS, Headings given to the pilot fr / C: j0 [, I$ j; ?9 E/ y& xcontroller using rad* O5 D3 C9 C: ~) o7 C RADIAL, A magnetic bearing extending from a / E9 f8 f' _5 Z8 ?VORNORTACITACAN navigation facility. 7 B1 @! q1 t+ F( H寂静状态,8 S( a; M& z% a5 e# K5 ?, ^+ v 电路上没有输人信号的状态。 y- F3 {8 U& X# Y 雷达引导,0 o' q6 K0 W! Q; } 径向线, $ s1 Y/ @* U0 m9 ~) o4 u' r/ A由甚高频全向信标/塔康联合定位/塔康系统导航设8 p: D2 G& @; ? 冲压空气,+ h0 ]0 W/ S, L4 \9 f 流过空调组件热交换器的外界空气。! I O9 a+ H" J3 d2 }/ l- Q9 K 英汉对照民用航空词典B OEING # y5 y# H1 s% b- l" ^TECHNICAL DICTIONARY 122" R+ V8 R6 w; @0 h) u( m2 x/ i: V! j+ z RAM AIR TURBINE, A device which extends from the , A- M$ w m: w! d6 `, driven by outside airflow for4 s0 _8 u l2 ?5 S; q; q mergency supply of hydraulic or electric power. 8 p D8 I! C* C6 {& U. t) sANDOM ACCESS MEMORY, A type of memory in 5 w5 Z. ~6 U4 a5 L- fdata can be written into and read out of.( \* ^3 `' U. `. L% J3 } used for short term memory. 0 t4 V; w8 o& F5 \5 dAT, SEE - RAM AIR TURBINE 2 m8 K% l1 D. {# ]ATIO, A specific relationship between one number& n4 s- m; ?7 ] alue and another.! N I S+ O5 l! L, [$ u$ T ATIO CHANGER, A mechanical device for changing 2 E+ g' D" ^- c" s& W& N. G" }* \utput speed or movement relative to input speed or% J1 [+ f1 w9 p9 Z x3 s( } AW DATA, Data from sensors not modified by the user. K, g6 n: S$ E; f* B 况下提, A# M, u, n! F 液压或电源的装置。 $ d v! O+ d. K0 c机存取存储器, ) e/ |/ D$ r( h! M# h一种可以将数据记载和读出的存储器。一般用作短期存$ r1 P c2 M, m5 n" [+ t3 s( m- I8 ? 压空气涡轮,3 l6 U( B1 T7 @! x- D. J# `1 h 见Ram Air Turbine 8 E/ t% _# L% }3 g" K/ Dside of the fuselage * Q4 }. W& I) p' D9 l' ne1 d$ |& l6 I% h& g R J8 w0 X* B: {- H! q( N8 J which the# W2 q* f' o* c Normally / ~% H! I2 ?* w. m- S/ G3 Y( F3 JR- \1 Q% ]+ U+ h" X5 o* s a& @. _ R ' A+ B. q' ~" L# T" u6 e$ Mv4 Q6 ^7 ^9 N5 P7 ? R 3 f% p0 x2 G+ G: c& d! To( Y7 n6 j3 q1 _: p6 A movement. & L- K2 p: |* Y: ~4 H8 i* ?R ( ^) i. c& ^& P/ _0 \! D+ g! l' Qsystem. 8 ?1 A- N* _5 p$ {! f冲压空气涡轮, : D2 O% G: U) A6 S* `从机身一侧伸出,由外界气流驱动,以在紧急情) D% M2 y5 I& D- r/ f. N0 u$ w2 o" g+ O! G- F+ }5 D E8 W3 n% H: B- L8 I+ h, m. e' t' E D/ s; D$ W8 Z, t8 w' o" K- n# X7 k0 i; v. B3 _$ d8 v+ x 比率, % N+ x- X) f: K. e; K* @4 l一个数值与另一个数值之间的一种特殊关系。! K( W1 n9 p( Q9 v0 ]# \, h) M 率转换器,& a( w- O# k% I% u% ^% U5 l 用以改变输出速度或运动与输人速度或运动之间比率 " ^9 t s/ V0 l8 j6 B始数据, ( F+ ~$ R2 r+ u! b5 V' P任何修正的,由传感器得来的数据。0 |3 [1 S5 \0 w2 C% G/ s& Z2 s/ a1 L3 b 的机械装置。 * a' E% z: T: O4 F$ i; j( s1 g f# c" U 没有经使用系统作 ' P { }5 V6 m- `3 s英汉对照民用航空词典B OEING6 j3 m3 s x# b! A0 Z; J! Y' q8 B% d TECHNICAL DICTIONARY 123 $ }4 K$ f2 L5 r# r x* MREAD-ONLY MEMORY, A memory unit in which k' W- m4 O4 z( Uthe computer. Under normal conditions the stored ( g3 I, @3 w. N. Hinformation cannot be changed. % Y& i/ H; ^% M3 I; f! ?ECEPTACLE, One half of a two-piece connector. It is - T! h. W2 q5 k% A# k2 v! qusually mounted on a support, such as a panel.( `1 m* j/ x1 s8 j RECIRCULATED AIR, Conditioned air mixed with air( j3 K: L: g8 H0 P# b from the passenger compartment.8 L% |8 D3 N ^' h5 K( \* I EDUCED THRUST, A thrust level less than maximum- F$ l- e8 A( P: y3 L% m rated thrust. 3 Y8 R1 ~( w1 t: QEED AND PRINCE SCREW, A cross point screw with ! H$ E' I. Q D7 ia single straight line taper driven with a pointed tipped : R$ i' e# M) t6 JED SWITCH, A switch with two magnetic plates acting 1 _4 u8 T# J/ u, ^0 G. l$ qs contacts and operated by a magnet. ; ]# F/ u9 J- H' ^; [) b6 u只读存储器, q- ]4 `( a- k/ _含有由计算机永久存储着的指令或数据的存储器。在一; O! {8 \! h) Q6 x% ~1 u8 @& W 作任何的修改。 0 `& i% n C$ N3 d插座,* T8 A& L; f! D( J* N/ ~. z 由两件组成的连接器的一半。常被安装在支架上。* K% Y" D+ ~: f) D8 [5 \ 如:仪表板。 % \% t6 P2 g4 `& V, T4 g- ~9 P) p+ o再循环空气, 1 k1 W: S% U( E& y( D8 E: A8 `调制后的空气与客舱来的空气之混合。 7 B" p' [! b& y% G! o+ D) T1 y减推力,4 i& m! }* D- g* n N* E 额定推力小的一个推力级。4 L& |9 J, y( e$ M" k/ x 十字螺丝钉, " g- a$ z- z$ ^9 E* m+ O( u的,带有一条直线锥的十字 / [0 C2 Z4 I4 F: W2 e. o舌簧电门, 6 F/ Z$ O4 a4 M F由一个磁体控制使两片磁片接触的电门。# d9 y( @8 H* {6 ?7 D instructions or data are permanently stored for use by , E. c: J* W: k" F5 AR; E2 ? U' c* U1 }5 `( F* k4 q R+ L; e' I6 Q' m4 a7 Y. d6 J; ^ R , d- g0 t' {' t$ f- e0 Q/ bReed and Prince screwdriver. (See Phillips Head.)6 Y3 P( `! U: V R + |/ b0 }- U5 X9 O- za 6 E, S* m' ?! A1 ]- {般情况下不能对存储信息 0 r$ P! Q5 T, M7 K( J( ^- @比最大/ o6 H# e8 g# S1 E# Y 与尖头十字螺旋钻配套使用! x2 c' q* ?, k* f 头螺丝钉。6 p: Z; \: i& D: u* N; _9 U% _* X 英汉对照民用航空词典B OEING8 }6 @1 i( W# E5 S5 z* x( c' C TECHNICAL DICTIONARY 124; j) u1 @8 a1 F8 m* o$ P, g; X' g REFERENCE LINE, A line used in a chart as the& l8 M0 ~8 A4 ]! O: c# P! u( a: V# t starting point for applying corrections to chart input 9 C" d. a! `: q3 S! }$ L0 xalues. One or more reference lines may be used in 0 E+ R9 P" Q% ^% U- i) uuccession.; A; H9 Q$ g3 w& B D TAKEOFF, A takeoff which has been 0 l! c( X& T8 j9 S.# Y* ?! ], w7 e3 [! U# e EGULATING VALVE, A valve for controlling pressure , s% c/ Q0 g L$ s9 GELAXED, The state of an electrical component or * V7 e0 t S, W. }" w) Vwitch that is deenergized. # V" |9 q. h. X1 |+ [RELAY, A switching device in which the contacts are! q4 ?5 c# a/ z1 ]% p opened or closed in response to separate current or. U, d/ [ z2 F; c' k2 V oltage. ' u) m: O1 n URELIEF VALVE, A valve which prevents high pressure; n2 S9 p( {. G a system by venting the system to ambient.- }/ Z W8 _7 m7 A( j- { 起点的线。使用时可用$ x1 N. x O+ s; R, _+ Z; z 条或连续使用多条。8 a! n" Y5 W ^6 b6 C# p3 i 断起飞, [ P* {8 P& C1 L( {# d 离地前被停止的起飞。 & q" v" F4 q, S0 {# a/ D, ?节活门, 7 j8 C; K* ^/ r- G& _+ U8 J$ d制压力或流量的活门。) S, R' Z' Z$ O5 x 放状态,! `( n3 {5 _& K3 M 电器部件或电门处于关闭或没有通电的状态。/ k# t: M) k9 V5 Q 继电器,+ k# s& q" Q: J; y* b 一种电门装置,其接触点随着单独的电流或电压开路或 + B' u4 J# n( {+ k合。 ' X$ }; f4 M) P释压活门, - |+ a& G' h, P通过将系统与外界相通,以防系统内压力过高的活门。. z/ f3 ?' o4 t& z v' ~! y% l! C( a s 6 H, |9 n' G1 cREFUSE/ ^7 U7 g6 n/ [# O stopped before the airplane lifts off the ground) e: m& S+ `& i! g8 F$ L; z R $ e' w5 D8 I" t4 O2 Oor flow. M) p% V( ^& m# J& lR & Y, Z8 p+ Z) i8 O" P L5 Ks 2 `5 K0 W3 w( O) Z# B2 W6 N+ G8 iv 5 A8 ~9 a% d2 U% K' l I( `in 1 ?0 C4 ?7 Z- F2 K2 W6 h8 d9 z2 m基准线, X) n* n( t' q) ^: ~8 v在图表中用作修正图表输人值的 & P$ A9 G- b. q- \( m! p( p$ d0 g1 f4 O, Z+ ]& U. ~5 P4 b) _9 ~9 S0 o$ R3 \在飞机 4 l3 ?$ r/ h) L5 s7 s; X3 E- S. Y7 q 用以控8 m( a) N5 A" |2 h' C7 {8 I# V& `- u: r! Q7 w: P/ v' h1 P% Q英汉对照民用航空词典B OEING + H% l3 F* P+ v0 i% K+ i$ |TECHNICAL DICTIONARY 125 ( C- u$ T5 X5 K: G! ^( @( DRESERVES, The required fuel remaining on-board after1 M8 B: l5 R3 o2 P! n/ V( D ESERVOIR, A container for storage of fluid. 9 s! S% G4 z0 g7 C; Z& _ESTRICTOR, An orifice for reducing the flow and5 `9 L- i9 r7 m ressure of a fluid. 4 b/ ]% E# s: U; U! S' }ESTRICTOR CHECK VALVE, Same as restrictor but ! e4 t+ e% a* K+ }; H% R$ X# ? H7 bllowing flow in one direction only. + U, ~/ F5 D9 D2 sdecrease the3 |0 I l% ~( t' n) ]6 x; ~* U, @ ngine thrust to idle. * I8 D3 w4 |* Q! S1 R: oREVERSION, To change to a pre-determined mode. ' C! M! A1 j5 ]* w+ Zctrical device for changing the 6 b* w/ A0 T( hsistance in an electrical circuit. 0 l k Q5 k- \- z备用燃油, * x; S3 S* ?8 |, N照规定,飞机在到达目标机场后,机上需要的剩余的燃1 C0 z' R6 I4 l! b5 ~& j8 ] 油。 - T' L0 [8 K& l- T2 P( ?储液箱, ) Q. |# g8 R- O; u2 D3 A用以储存液体的容器。 8 m) @ |. X7 {: }( s限流器, / M0 \) u, M9 e8 b用以减低液体流量和压力的量孔。 ) u8 Q1 P* u3 s8 |流单向活门, * q: W; f) M0 s; ~5 `一个与限流器类似,但仅允许流体向单一方向流动的活 ) F+ A9 ?% D" k. {$ E3 A1 n b门。 7 `% @7 _: K4 w3 s* Q8 ^2 T/ E) D门,0 x9 p8 A/ W" z0 G 自动油门的一种方式、用于将发动机推力减小至慢车状0 N1 |& v, K5 Y9 W% q1 p1 R: x+ J" k9 h; B, b; h 改回到预定的方式。 . ~5 S, |2 C4 I" _用以改变电路内电阻的电气装置。 . H: ^' S( w5 q6 `. f1 }+ Narriving at the destination airport as determined by1 @7 B4 T' }5 ?* K% q regulations., O8 M& C$ D1 _ R ! A+ e9 h( z) l- XR6 ?& h# e! |3 E5 j \4 a2 a' ?+ z p+ w, B# _5 T& P$ p R2 v0 o% I1 m- T; [- b2 | a: T$ f0 O% `$ N3 Y RETARD, An autothrottle mode used to" P! N+ J2 {& {" h+ K e. `$ H' \ U ^5 d: U RHEOSTAT, An ele2 B/ s) p$ s# F+ m$ \+ w8 ] re; ~" B, d r! t3 O6 `0 {+ b; F$ Y* Y; F2 J拉回油 ' |- O2 \2 r" r" q3 x9 i5 D0 l# k. S, Q 复原,' s+ r0 K+ J0 ~! r y; C 变阻器, + }( v C: L3 g: f, n1 Q. h5 S# F英汉对照民用航空词典B OEING 4 O+ Q* Q- k' ~! t5 k# lTECHNICAL DICTIONARY 126' s1 ?' O- A* E( o+ x% r RIB, A structural member of airfoil shape in wing, % l" G: ~0 `5 E/ Kstabilizer or control surface. ) r/ `0 p# d# {; lIG PIN, A metal pin for inserting into a moveable ( i. V( m8 [: \# B3 U8 {6 Romponent before adjusting the control cables and ) _3 @; B: ~+ t& Unkage.+ x- ~& y/ ^+ S; h IGGING, An adjustment of airplane controls and doors : [3 a7 E' D/ }5 `2 ]3 g; Fr proper operation. & f" [; G0 q% x# ponditioned air supply to the passenger cabin.$ @7 e5 T) d3 {& I; N. s- K 装销,2 ^: @( e- H, Z; |8 a 在调整操纵钢索和链系之前,插在可动部件内的金属! M9 k! T6 k: E( e( S' K7 z) r( O( U Q: q校装,0 n- e& g) D. s; k, ~) {# {2 @8 \ 使飞机操纵系统和舱门能正常工作而做的装配调整。 # D Y/ W2 _$ G6 |6 O空调系统中,将调节好的空气送到客舱的管道。' S0 S1 A8 }+ I1 p9 L# k; u R " {4 L# }" F$ lc ! [. `, }& W" w. a$ e2 `li $ ^# D, d( O: q9 T' MR3 n4 _2 V- I" ?* _9 Y. }" h/ i fo6 t; e/ f4 b% i6 | ~* c6 }9 E RISER, A duct in the air conditioning system for & |8 L0 Z% W1 nc 3 F5 u) O: r0 v翼肋,2 |0 m' e2 @/ F- Y( y. X/ z 机翼、安定面或操纵面内具有翼剖面形状的结构元件。. {4 i5 I( x# I9 w& V6 l; @1 C4 z9 k( ^$ T( t7 e2 b+ j+ h2 g1 K 立管, , @1 o7 S! E9 V$ f英汉对照民用航空词典B OEING 1 @$ K/ r; {# c5 I1 YTECHNICAL DICTIONARY 127* O# W$ U& n- t. L' o# S/ v8 | ROD END (NO. 1), In a hydraulic actuator, referen) _+ e2 W4 A! x$ Z the part opposite to the piston side of the actuator.4 c. ?7 |$ _- O2 h ce to/ `. \2 y7 }/ L; L D (NO. 2), A mechanical device usually a( {! A; b5 j" T K! L8 N bearing, clevis or similar component attached to the end; F( i# X2 w( w of a link or push-pull type rod. # L- w9 q' d2 b( C6 O% D8 X9 ^OLL, The rotation of an airplane around its longitudinal + W2 b6 D+ l; Y. Gaxis.# q, d, l$ u$ i Y- Q4 G% G- ] OLL AXIS, SEE - LONGITUDINAL AXIS3 t w" Q) ~7 p 连杆端,2 U3 a) h& d' y" V' q' v 杠杆端,2 \/ [7 U! k- | s/ n, _ 一个连在活节连杆一端或推拉杆一端的通常是轴承,& w8 m7 ?9 b2 \/ g5 O9 s 吊环,或类似元件的机械装置。 # O1 r7 P5 E6 U7 A+ n" l滚,2 H( r0 `9 I$ i9 t X" ?1 E 飞机用纵轴作为旋转轴时的运动。& N! \; y" ~6 D" g$ {! @ 横滚轴, R( e" k* A+ v# Q I 见Longitudinal Axis' {* M8 ~, r, m2 G- R V+ g, l% v' P ROD EN# b4 n: v; |# B/ X/ C R / z- s9 E2 C" A! t/ U, SR ' |6 i! v0 Y2 } L' ^( N' v9 y液压作动筒活塞连杆伸出的一端。! D8 i) V* s& y6 C, \* g) K- f2 D$ e" N( {5 M3 w) y& Y0 i# ]) Z英汉对照民用航空词典B OEING5 w, O1 C! r" I% [ TECHNICAL DICTIONARY 128 . O2 P( V4 _3 K8 S) J( SROLL RATE, The rate at which the airplane moves + R. ^, T" Z& R; y* ^' |on the roll axis (wing up, wing down). . J3 B3 J5 {4 m0 p! cOLLOUT, The final phase of landing where the$ }0 I7 q h# s# T! p OTARY VARIABLE DIFFERENTIAL TRANSDUCER, / K; b* b: p& v" G; Z. ?ROTATE, A maneuver conducted during the takeoff& k2 Z; U: B+ o) @ n5 d$ ^. J2 x5 T% U5 W* ^ raise the nose of the airplane into ' d+ a% h- F. r* `e air. B' b" x T* D OTOR, A rotating section of an engine (turbine,0 s4 [) Q- O, s5 ]" Z/ U9 p- L ompressor) or a generator. - o, }$ Y8 p- p# ~ROUTE DISCONTINUITY, An FMC operational# F3 s" [ E" e3 O- G0 b condition, in which parts of a route are not joined or , |; _0 X8 q0 P5 ^1 ~) Wconnected. 0 i& T! n& \( i2 yROUTE LEGS, The portion of a route which connects , `) @, e9 Q2 s9 ktwo way-points together. & Z* b# C" l, ?陆滑跑, 4 w) i4 E" z* T4 [1 U9 ^ w5 S' ]的最后阶段。此时飞机在跑道上减速。 2 v6 q$ m3 ?5 X/ w4 |. N( E3 w0 y: r, i0 D7 W- O; y V, i R 6 }/ D3 V( b; A% V Mairplane is slowing down on the runway., n# D7 J: Z) b% | ROM, SEE - READ ONLY MEMORY - J4 m7 d5 t/ c$ D( k5 i4 dR8 s$ {8 Z1 I7 k2 S A device with a rotary input and a linear response. 9 T2 D& Y8 u0 L7 D* o* s# Z0 |ground roll. At the rotation speed, the pilot pulls back o: Q) q5 V: Q) L- z the control column to Z2 B4 s, J2 _# ]) Q+ Pth 4 r# a% n3 r, G. k8 aR" a: a; C. ]) D( y6 ^$ K+ _ c , l# c9 @ G1 ~0 a' }9 V横滚率, ( x. \5 `, U" p( ^9 l x2 g飞机绕横滚轴运动(机翼向上或向下)的速率。$ E5 _8 I, O8 p- s( I% I. E T; H$ ~+ M 飞机着陆 & r* H+ c% H' \8 \, X只读存储器 " Y M8 O. c: Y: @见Read Only Memory* Z7 Q% C6 f( |$ }% ?9 B- V 旋转可变差动传感器, 1 T- J2 M9 O8 z人和线性感应的装置。0 e0 S- @7 l/ w8 X+ u6 ~! g' W 抬前轮,/ c$ c" ~( D! t 飞机在起飞滑跑期间所做的机动动作。在飞机达到抬前( f0 i2 O% k( b! K, w/ E 发动机(涡轮、压气机)或发电机的转动部份。1 A9 [+ T& [ b( c4 N 航路不连续,% w) Y5 v. Y" R2 t! p; w" j3 A 一种飞行管理计算机的操作状况,航路有些部份不相连- e" H1 b: z q8 c" b+ ~ 或不相通。 7 V' i% O5 P Q; @! F航路段,0 ~! }( x. M/ v; u. R- q 将两个航路点连接起来的航路的一段。 $ a+ n) z: b% W' g9 K6 g+ b2 b# i' Q一个具有旋转输 , N- v" Y$ z5 b4 V- V0 q. l* {轮速度时,飞行员向后带操纵杆,机头上仰,前轮离地。; L) `& [; j5 q 转子, . w- h' [. H1 [, m0 X9 m英汉对照民用航空词典B OEING 1 ]; T5 ?8 j* ZTECHNICAL DICTIONARY 129: F5 l7 r: ^- u. E- A& y RUDDER, A hinged moveable part on the trailing edge 0 b5 P4 g1 l3 L: Z) e5 B% mplane yaw (left and right)" s! P) Q9 {) t# E7 c5 k( A& g2 I ontrol. 0 `$ g8 d) G2 `. NRUNWAY VISUAL RANGE (RVR), The horizontal1 P( O# k4 D) l z1 S* A a pilot can see down the runway when flying an* i1 U- ?, K! E pproach.% W+ L2 _7 Q5 h# t* v* `( ] of iron and iron containing metals." T2 N- s+ i* P! ?: S% B4 p is usually a reddish brown color. 9 p; ~7 u' y. B% kIAL 9 u; y7 K% S, Z1 S+ f' x/ l3 ITRANSDUCER , G; u, J* T/ h0 A1 ?S f/ C" l* [. k# `! S SAFETY RELIEF VALVE, A valve in the pressurization2 }% f, s. a6 Q4 H9 X+ r7 I system for reducing cabin pressure to a safe operating, P" [+ d/ a! d( z2 r0 s# u pressure. # T/ Y1 w7 I! X3 z0 h- h; ESAT, SEE - STATIC AIR TEMPERATURE 9 U; e Y6 h7 \3 X" Z' B或向右)的可动部件。 ' n/ g! }3 ~! H, _' f进场时,飞行员向跑道方向望去所能看到的水平距 # I+ D/ x& s+ s! B& n( l6 T9 T& f. J# }- W$ R2 S 铁和铁类物质的氧化物。常为褐红色。 - u9 `0 I ~; h2 D! u2 l# e4 M见Rotary Variable Differential Transducer2 D- O! x6 t2 L- R& [, J$ z of the vertical stabilizer for air 0 \ o/ Z3 P' M3 s: g2 @4 cc2 t* a4 `/ w6 V distance6 B; w) d; P5 w$ B a 8 \* b: a! Q& k* X; c v" V, z6 ORUST, The oxidation# S" u; r- w6 F It* U& T9 c" P* N, L& k5 a7 X RVDT, SEE - ROTARY VARIABLE DIFFERENT S. l. R0 G5 d1 [* [( m方向舵; ( K4 v6 |/ `: D. B铰连在垂直安定面后缘上,用以操纵飞机偏航(机头向 ( b- ]5 N8 x1 Q6 k( P3 e( Y( \" L1 K: |8 Z+ W跑道视程(RVR), 9 |5 N4 R- ]2 N% i4 K1 e飞机+ s) m! d0 P3 Z% J+ L- U3 F6 r' e$ M$ M3 a 铁锈,. ?/ k5 J f1 A- D1 T- C 旋转可变差动传感器,' K3 _9 `! E \ .' ]# Q7 o$ a+ ]5 \- o 安全释压活门," X* ~2 `5 l5 B! Q 在增压系统中,使座舱压力减低至一个安全的工作压力 : N0 k( }0 M; r的活门。 # T: M/ P* Z1 S# M& S0 w0 y静温,' ^1 |/ z& D* f9 Y; J+ p& G, ~1 ^ 见Static Air Temperature. + D2 u: p( f: s& U6 I6 r" `2 q) t英汉对照民用航空词典B OEING5 L( p% E6 ~9 s# ~# a TECHNICAL DICTIONARY 130. Q: y( x- K! {$ ~ SCAVENGE, To remove oil from the engine bearings or ' _0 J! Q/ @: i& D3 h7 m2 M4 ato remove water/fuel by a pump from a tank. 9 l' J# w- ?3 wCHEDULE GENERATOR, An electronic component in / {5 n; A, P7 e9 m# J C. }e pressurization system for controlling the operation of& h, p/ c. r) S" f- L- f8 l e outflow valve. k* [+ n$ { q CHRAEDER VALVE, A valve for inflation of tires, 6 u5 B V" y* g+ ~truts and accumulators and for pressurizing the water* Q+ X- n7 P/ ?' r6 g% n; ] CR, SEE - SILICON CONTROLLED RECTIFIER a! H* \0 Z8 W1 W$ a0 BCRATCH PAD, An area on the FMCS control display 4 T7 c) b9 n0 s `( sunit used for showing characters activated by the / _6 w m7 k/ Tlphanumeric keys. 5 x9 W! \ P! w) @, ]5 O- XSCSI, SEE - SMALL COMPUTER SYSTEM , K: z# ^3 w# Z n2 _INTERFACE9 r0 y0 a W0 w- {5 L( \ SCUPPER, A shallow receptacle around a filler neck of, D( r4 G% t% w. ^4 @' A$ X a liquid tank to catch any overflow or spillage from the ( z7 E; i8 h7 t. P5 Gservicing operation. The scupper is normally fitted with a: i" `0 _7 a. E& K& R8 n drain overboard.) y3 g* |7 k2 o) J3 D5 P SEA LEVEL, The standard datum plane from which4 g# h+ F, I/ e3 i altitude is measured. # @& ?( B [+ k& f% z7 A- f去油箱内的水和燃( z i; }$ ^8 N' \) a5 { \. H1 O* `. B7 B( w4 L1 M 程序产生器, 6 v5 B. n6 B7 k* C% G$ G在增压系统中,用来控制外流活门工作的电子部件。$ V1 g& O6 }4 {& q# x. D: S8 D chraeder活门,' I3 z8 `2 ~% W7 ` Schraeder公司出品的一种活门,用以为轮胎、减震支 4 N0 s) b6 Z M充气,也用于从外面为水箱增压。 : m, Y. m+ Y& k3 |4 F. h% Y( e可控整流器, 8 Y" R% P: s5 f; H1 g见Silicon Controlled Rectifier6 @$ F) g4 W3 G J! I$ Q S- q' } t0 p; U4 }: V th9 g' I- f8 }- N th 2 F7 d( {3 M4 W& k9 m1 GS! y9 u2 ?! d2 B% A! O& h ] s : a% x/ o6 x: c/ E/ utank from outside.( H% g: a6 I2 t( j& D5 e# g6 d$ B S % N: Q9 ~) W' E, o2 US 9 d- Q' I% y+ Q1 x2 w9 Q' na6 ~2 t0 g% l. e, [7 E+ Q Q 回油, 4 z& i" j* P9 G' h6 x& Z. `除去发动机轴承的滑油,或用泵来除+ m7 e! D6 V3 y4 }; I( I( P" i y8 `0 s! K- ?: r, ZS* {6 J z, p0 C; s 柱和蓄压器* N4 r% ]/ V+ W1 p6 @# f6 }% c0 Z# G' u( i4 O( f( l" v5 T- |+ N9 D稿栏, ( b9 D5 f* D9 oFMCS显示器上的一个区域,用于显示由宇母—数字键 # E3 P. J6 [$ D! A3 m# ]/ ^2 `激发的字符。7 G( G. U; |; ~- s/ H' \5 z1 J 小型计算机系统接口,8 M: F Q+ o9 v( X, k+ g" H 见Small Computer System Interface/ J: l& P# Z' `& L; h& U. e7 ~$ V/ d5 P/ I$ B5 a" x- x! t$ D% m1 i2 t7 c" j$ E! u; n9 g/ I- ?4 {$ ]" i" V. L1 ]; m放泄孔,; [' R. M% d8 y2 n/ k6 |/ L 液体箱的加注咀边所装置的小型容器,用于接取勤务过 ; @' e' u5 a, r: z" s; l程中任何溢流的液体。一般都装有通向机舱外的排泄管9 ^& C3 e6 l8 Y 道。) G0 c$ W7 t: t 海平面, . |% X; {( {1 U( N/ z用作高度测量基准的标准平面。 " @7 F( J! _# Q5 U英汉对照民用航空词典B OEING, b/ i5 M" T# { TECHNICAL DICTIONARY 131* E# [% T$ Q2 k8 M* t" j- { SEA LEVEL STATIC THRUST, Maximum rated power ( E# R! d9 M/ q. n' `. t9 V+ xproduced by a stationary jet engine during ambient- H8 {- |1 a, A X onditions at sea level.7 n' f0 b$ w; v3 ]5 W# m- P s for 0 p r7 X6 s! v3 ureventing air or fluid leakage.) {9 l) G: e$ y* \ SECTOR, A given distance between two checkpoints in: u' p/ Y1 D& y e flight plan.% e% v; o1 S3 o( p% ?5 ^$ @ ELCAL, SEE - SELECTIVE CALLING # v, F j7 e; M6 qSELECTIVE CALLING, A system that automatically 7 X) N7 N: h# Z# GSELECTOR VALVE, A valve in the hydraulic system for% a% g+ W9 ? Y: U, v* e6 Y' Q o one side of the actuator : T; d4 a2 V$ v" T5 und the other side to the return line.0 u" }. R3 ~5 P* ]. Z- O 力,2 I/ ~* _' m: H, M 在海平面环境状态(大气温度、压力)下,一台固定住 % r* ]$ _% k& C# ? T: S, X的喷气发动机所产生的最大推力。2 v+ x( S' _- ~' S 在两表面间防止空气或液体泄漏的元件。 4 |$ N3 _6 R! c) u航段, : @( H; j) N: P7 a: q: }& L& ~飞行计划中,两个检查点之间的已知距离。! C, o1 m& s" B! E: J1 [9 e3 w1 D 择呼叫,* i, p# R+ U) B+ s! q$ f4 ? 见Selective Calling$ c' k3 L' b# g5 ]2 B c * V- y' d) Z& [' c4 cSEAL, A component between two surface8 ^0 {# W3 G7 Z2 H* P3 a; O p; p' ]& J0 C0 O$ o! F7 E th0 q) \' _6 j' G8 @% i {2 p, ` S, s" p3 Y; g3 V* V alerts the flight crew to a call from the airline ground% g" Y* u; j; x- G; m station.! G P# T: l% a( Y' \8 p" H connecting hydraulic supply t3 p1 Z/ N- T" P) U# `' y* } a6 C9 ?7 H4 F1 K3 `# _' G8 C 海平面静推 & q X, T# S G' g3 b) |封严,7 I& J' J. {/ B% y3 w! X n' q- [& i( K4 v% F% U . - m) {" U* q$ M/ D) {, Y选择活门,0 m/ r, d: K+ u# t! K1 T# o 端连* D, s' [ {9 Y. M- ]% I$ U 回油端的活门。9 h6 J6 E3 T9 L 选择呼叫,; }3 o) ]1 v, O U7 L 一个能自动将航空公司地面站呼叫报知机组的系统。 3 B- S6 d, R" a' n; h1 K6 o. n5 O液压系统中,用于将液压源一端连接作动简,另一& p! ~. _8 N+ I! O9 j# b( y ^6 {8 ^5 @2 S4 g, \3 Y2 k; J+ v英汉对照民用航空词典B' p2 k9 X v8 S: _ SELF SEALING COUPLING, A connection between two % D0 h( n- u2 P+ x' V8 tfluid filled hoses for preventing fluid loss when the hoses 1 J4 a5 [, U1 s& _5 Lrated. % f) F9 U/ J9 T9 g7 D7 u& KSEMI-MONOCOQUE, Type of construction in which the f. B" E4 a; D) T7 @' {* D& w SENSOR, An electrical device for detecting variable- j) j* Q, |) ] ENSOR ACTUATOR, A device for operating the, \+ c9 }- h& b0 \ SERVO, An automatic control system which checks its6 w" R0 ?7 g* ?6 h- x3 t0 H gainst its input so as to achieve a desired6 C) |' f' f) z( U& W7 M5 M; F MED, Hydraulic pressure for the servo is. T4 r) |0 h& z3 a resent to allow the servo to internally synchronize to* f; k) j4 w: W( ~( h+ K' x J e proper position, but the mechanical output of the 0 V# V5 f8 d1 k3 B5 G/ `. hervo is not connected.5 Z" q3 s% L7 V5 h0 ~ 自封接头,) m- C5 e) s3 u, F R; h 活门堵住通道,自动封闭而不) @* w% ? ]8 |# Y- G a1 `9 j2 @ 让液体流出。7 @: V7 p3 S4 b' D! T2 R% m 半硬壳式结构,2 R1 t# k7 {- C 使蒙皮,长桁和隔框共同承受所有载荷的构造形式。/ ], F5 L3 u f 感器;5 F1 s# q! M5 c2 B6 U& X 量状况并将结果以信号送至指示器和指示灯的 ; v- J# B1 d% D' P$ B% }! d电气装置。/ ?' X6 G2 _5 m) T9 v 传感器致动器,: r2 P2 o; E. \1 i& l% a5 w; Y/ h) {/ [- m$ Z2 _% Z 伺服系统,) i7 P( w M5 x- C( O 能检查输出和输人数据,以便合适调控的自动控制系 5 ~) T' H# `7 g) W统。 ) o A* ?1 @1 F4 T J; K伺服预位,9 N5 \, p- O6 Y 液压使伺服系统内部同步至适当的位置,但伺服系统的 0 W5 E) f9 D$ Z6 `+ A+ G- Y6 X机械输出还没有接通。 - j/ t6 D% I5 U, v2 Dare sepa7 S& r0 k& J6 \" G# z _5 X skin, stringers and frames carry all the loads. # O P% n6 S4 w9 W7 Fconditions and sending a signal to indicators and lights.3 {; o5 V1 H: V& W# {# e" Z. I S # D) Y1 A" Y5 U) {sensor. ' g p5 I9 l5 Z# `output a& w- a2 x, N; G) v control.) T) f4 F0 o4 h2 L2 z, @ OEING: ~0 e1 J0 |# E, O5 H TECHNICAL DICTIONARY 1321 g7 V% i3 m, x/ l$ b. i SERVO AR . I+ }7 _9 E/ N, I* c( Tp ) N y: u n# I3 @3 B( Cth $ I' p) m1 a2 [8 J; B" ns* V# b( x: O5 W$ \" ]1 s 用以连接两个充满液体的软管的特制接头。在两个管子 + p" O7 Y1 h* Q2 f分开时,接头内的弹簧即使6 Z9 K f* l }; c6 a* s8 j$ j w. W, S! H: x# W2 j 检测变4 p% Q" `1 v8 t3 u 用以操作传感器的装置 . A. T7 |/ C* S& R英汉对照民用航空词典B OEING, l4 u" e+ o3 i. q TECHNICAL DICTIONARY 133 E$ W' q# b( `7 D. K* `+ `' uSERVO ENGAGED, The mechanical output of the" J* i' u' [& k9 x; p servo is connected and the servo can move a surface or + L: b9 \8 Y: @) ?& kontrol2 E d' _3 I5 v$ ]9 G SET SCREW, A small screw (usually headless) used to . I$ O; n" H$ L) ?9 jeel, or knob onto a shaft and prevent* X* G& c3 i v8 a tation.6 C/ X. \& f2 e* I5 F SHEAR, The stress exerted on a material or, assembly 9 i* o5 ~7 z3 H- H, R" ?! uwhich tends to slide the mating surfaces parallel to each 0 Y: B+ w% d( ]: u7 F% N/ \ther.. |6 X* R; Z) l( z5 ~" X7 ~ SHIMMY, Rapid oscillations (left-right) of the landing0 s% j1 T7 T) Y, q- Q) n ear wheels. ) L- E- ~4 Q1 y, L' x2 |) Z+ J预位,# Y. c- B$ Q( A7 q0 Z4 } 伺服系统的机械输出与伺服系统已接通,伺服系统可移( p( L( Q+ S$ z3 z( V 动一个平面或操纵。 6 P6 A( x! X8 @+ |小螺丝钉(一般是没有钉头的)用于将滑轮,车轮,或& z' w/ l& }7 E: W+ w# l 钮紧固在轴轮上被免转动。 , p7 I( @' I k7 s; Q) |7 o3 O7 Yc* Y! g h; g0 [7 q# ]$ s fasten a pulley, wh 0 z7 s' J) d2 U6 Fro 9 r5 K* P7 q5 ~% U7 c# ]: aSG, SEE - SYMBOL GENERATOR; [( B9 u1 ^0 t o % W% [6 I Q7 p) Kg# Q$ d; A- X; C* S6 Q& K4 V! | 伺服系统+ x/ q% c3 j( }" f5 c 定位螺丝钉,9 P$ {7 X" v: N) g. w# ?" z8 I# K4 [: o7 b* r; A 符号发生器,9 N& m& x* D Y" H$ O 见Symbol Generator.0 u9 t/ m: T. i/ `, d; S4 y 剪切力,7 c+ T, N5 w {4 k 加在材料或组件上的应力。该力往往导致互相平行的成' K9 S1 }" Y1 w2 T5 c$ ~9 X0 O! u 对表面滑动。 m) W# p- L3 b% U( Y p1 t 摆振, F5 o8 u+ S" n7 B起落架轮子的快速的左右摆动。6 X: ?1 v8 a. c7 x( s8 Y 英汉对照民用航空词典B OEING* o# J- x4 ]: m/ Y* W- l1 p. { TECHNICAL DICTIONARY 134 : X; n( Z2 E" s7 L# ~SHIMMY DAMPER, A hydraulic device for damping / j& B" H' H' p/ s2 p) Tshimmy in the landing gear wheels. , V) t4 N5 R. p; x) }5 p/ Z2 par for / s n; V; K4 L9 M0 V8 p( gsferring oil from one; Y" N$ b: X9 x% B; n chamber to another through a metering valve.$ f" V( @/ q1 i+ h# w$ n) G* b0 \7 T& r2 S5 S5 p/ E5 ^ 一室以减9 A+ ^' x. c+ T. Y 着陆时产生的冲击震动的部件。 2 ^4 j% @* o- ]: r0 M# CSHOCK STRUT, A component in the landing ge2 V6 x, @/ P [# J5 Z8 R absorbing landing shock by tran/ e6 u0 W& R6 x$ r- h/ ?) ]5 I9 v* I 减摆器,; @; y0 n! z5 K 用以缓冲起落架轮子摆振的液压装置。% J* n- G6 }- k" n 减震支柱 : ~3 F+ V7 a* _7 w- e e/ K. ?. p起落架上通过计量活门将油液从一室转到另 : h/ W0 V9 Y. Q7 U' c `8 \: I4 u& z( S, } 英汉对照民用航空词典B OEING& G3 {: t- ?& S2 A1 U. p' h8 @ TECHNICAL DICTIONARY 1350 C( u1 _3 B8 y$ ] SHORT CIRCUIT, A fault in an electrical circuit 2 ^1 ]9 d+ @# V, o( hoccurring when the power supply goes directly to: @) D9 E( l8 b8 W% m' S/ J; h ground instead of to an electrical component. ; }2 V. M, C7 u; ASHORT RANGE ALTITUDE, A cruise altitude chosen to * g5 ~5 s" K+ q! @inimize fuel burn during short trips. - T- e# ^8 Q* u4 JHROUD, A metal covering for enclosing the APU on2 }" h# B+ R! s e airplane. An external tube for enclosing a fuel hose. ! e2 w Y7 ^( H# fHUTTLE VALVE, A valve in the hydraulic system with2 E3 M0 r( n2 g' U5 B - STANDARD INSTRUMENT DEPARTURE& k# W( P* \. G( V f the + L8 g1 _* X/ Z7 p3 lr access to the components on the engine.; H! ^. F0 H% }- ~% r5 E9 s! S0 M 短路,. d3 |+ h0 }: d; q 短程高度, 3 D) D) n/ Q0 k3 F' D为在短途飞行中使用最少燃油而选的巡航高度。, ^$ f0 Q+ M, m) Z4 T 护罩, - |$ ~( _! i- I" N0 |5 E' w P飞机上包围着辅助动力装置的金属罩。包围着燃油软管 8 ]8 k" N) S$ V6 E用活门,6 E) ~2 B/ ] O: R2 Y 液压系统中,具有两个不同液压输人管和一个输出管 7 u1 x& R: ?+ Y8 j( z的活门。6 J$ K: a6 ~3 F7 k 标准仪表离场, $ k( q. x: l0 u# t/ Y见Standard Instrument Departure1 r0 i! Q- P$ _' _7 A" _% W: Z; d m / H! M: S6 y! G" x4 K; W0 `S 0 K3 @" f* V* z0 b* R" K& v8 i4 \3 oth0 [! B4 k4 l" ?9 e6 {6 g; V! e S9 I8 V& V0 [5 L two different hydraulic supplies and one output to a 6 K+ _ a8 i+ N9 G* ucomponent.& S" v0 {5 ]& b7 e, F' o+ l SID, SEE! I; s& K# t: W; u( U1 _- S SIDE COWL, A removable cover around the sides o 7 @; c7 k) T8 q- [7 P) jengine fo4 ]) ]. S7 Q# C9 e; Y# K& v, P 电路中电源未经电气部件就直接到地线时的电路故障。- e, u/ x* t9 \0 X$ o$ r3 U7 t+ O1 X; P6 W的外管。* _) b/ N6 ~! Z4 k$ I: I0 m4 w9 o6 H7 S* F0 O/ l! d3 O0 @- f 机两侧,被移开后可以够到发动机部件的可卸罩 7 W6 ]) K# G$ M5 W8 n7 M( n e$ V( \2 _4 X" d 侧整流罩, " v! w; w7 m: G* p/ K* K9 O Z- \发动 6 q: ?) _. v- m# A+ \ t7 P8 v5 F英汉对照民用航空词典B OEING - {6 p" R- F7 F L4 Q) lTECHNICAL DICTIONARY 136 4 f0 E* @9 j4 W$ z+ pSIGHT GLASS, A glass window for observing fluid 8 X2 Y# Z1 N) S& b1 m" Gquantity in the reservoir of a machine. o7 }( A- z+ r, that can be used to transport information for- o7 t: w0 `9 B communication, control, or calculation. 0 v1 x4 c% v' A4 NILICON CONTROLLED RECTIFIER, An electronic1 j4 L' |; O7 l8 j4 }( m device allowing current flow in one direction after the7 w. G- v' b2 p# [2 \) Q device has been pulsed at the gate. ) n+ @- q, F# `6 L( Y, ? C9 ZSINGLE SHOT MULTIVIBRATOR, An electrical circuit, D ^2 P% U" `" G- U _ -stable multivibrator. # E1 @$ }" L( T) m' Z5 _0 R0 h: d! }如电流或电压能用于传送、通讯、控制或 : z+ ?2 N' M& w" R. U. }算需要的信息。 & k# e# H) K' t3 P9 |硅控整流器, ; n& U$ P1 t, s; j当其控制极受到脉冲后,允许电流向单一方向流动的电 ' [ y$ |" b. J* Y, _子装置。" ~3 R9 q& p y: i8 J1 k$ } 息多谐振荡器, x* W8 |0 ?, c( B输人信号触发电路时产生的脉冲的电路。又称单 - Z' c+ B0 @( _) n: O pSIGNAL, An electrical quantity, such as a current or / } @, B- W, q7 Tvoltage 9 z" c+ K' E' t6 gS9 y7 J1 g2 b9 \ which produces a pulse when triggered by an input7 k) W! B- r6 ~8 c2 O- d8 r& M signal; a mono " i+ M. G* v) V' X, q检查窗, # ~+ o) Q+ S [# f0 U% F用以观察机器的储液箱内液量的玻璃窗。- s' f& w+ u" ] 信号, 1 W) q) O: {& S, |6 u- u/ {电量的一种。 . T9 D1 g' a4 y. T5 }0 P9 W6 |/ L' A# }: B+ I J4 s1 o8 c& O8 G5 m当一个0 Q3 k; _: j( ~6 o y% _: A% E 稳态多谐振荡器。 " k! b+ b4 t% R英汉对照民用航空词典B OEING" V! E, w5 X4 r$ } TECHNICAL DICTIONARY 137- |" W$ k( L- M5 a8 |; \/ y4 R6 T! `7 c SIMPLIFIED FLIGHT PLANNING, Rapid determination$ \! c# l- W) Y7 [: K! S# F of trip time and fuel using a chart providing these data( \! z6 G0 ?$ b; a, x. s for the entire flight profile from brake release to landing. 5 |1 r7 G) O$ J+ h R& gSLANT RANGE, The line-of-sight distance between two a1 i5 U }$ w+ Zpoints not at the same elevation.+ Z! l N' l) T- Z3 _3 a SLAT, A moveable part on the leading edge of the wing6 {/ t$ V& Z1 o) B$ E3 T for increasing lift at low airplane speeds.% D6 ^5 c. c* g+ }6 i 划, 8 {: h9 [% q% j5 j0 o8 j迅速定出从松* b; f" s/ b( @( @8 n 车到着陆的整个飞行所需的时间和燃油的过程。 ) f/ x5 a( c5 S8 x斜距, S( }' J- M( Z7 i* N4 Z不在同一高度的两点之间的直线距离。 : M4 |" D4 {: M+ q3 M% o% j; _缝翼,, K* L3 D" ^0 ?6 D6 `- B; _ 用以在低速飞行时增加飞机升力的机翼前缘可动部件。 2 r5 r- W2 N4 z' u4 g; e简化飞行计 3 C- t! |' Y0 O: _' @0 W由提供旅途时间和燃油等资料的图表,来. S# t: n$ U$ K1 o# b' u: j1 I- \# a f7 A, X 英汉对照民用航空词典B OEING : N/ |- ]3 J2 o+ U; ]! ?TECHNICAL DICTIONARY 138; p6 s( b* i% ]3 `* ?+ F SLOPE, The amount of incline a runway surface has + z8 m- i" k: n% G& |; o( xrelative to absolute level., r1 t5 i; b a, C9 P5 o SLUSH, Runway contamination made up of a mixture of [- B# x* `/ q' G [8 I; }' Bater, snow and ice. % i3 s7 v+ b- q3 o# q5 k9 uSMALL COMPUTER SYSTEM INTERFACE, An input 1 N, a: M p. H3 j; J$ C+ [1 Qand output bus that provides a standard interface 1 k: U" o+ Q+ Q6 ~) t, Ebetween a computer and peripheral devices. . S3 H" F+ W1 Q3 Z6 X/ {; pSMOKE DETECTOR, A device whereby the flight crew # Q7 I( N5 I' F4 C1 Fan be made aware of smoke or fire in specific areas of$ x/ |# i7 e$ Y) T' J6 A the aircraft. & B7 M/ F2 V6 ]6 a, K3 WSNUBBER, A part of a hydraulic actuator that slows. k" f" {( x; y* }7 G" j4 Y$ b9 v piston speed by restricting flow. ; V/ L. b( O" @OFTWARE, The stored instructions that control the a5 [2 `: V; _, n' D perations of a computer. 9 B8 P3 _: H" ^& k: @, H- P7 s+ ?) Bng2 z7 ~0 \: X! e other devices. 5 J0 ~3 w- Q' h4 {7 MSOLENOID CONTROLLED VALVE, A valve controlled ' D$ \4 R* l) a5 C6 l" M$ Y' uto open or close by the solenoid. ) g% _- z+ O0 B雪泥, / K, }$ D. U2 Z$ a) C$ }积在跑道上含有冰、雪、和水的混合污染物。 - ?$ x; F% v' k+ U小型计算机系统接口,- t' B% X; E$ s0 S: d( `" J 一个能在计算机与周围装置设施之间供给统一接口的5 m" S) c, h( | 人和输出总线。 8 m# t5 v0 k$ T( J7 A烟雾探测器, - n. x' j2 B7 g8 U在机舱或任何指定区域内能测到烟雾或火并报知机组7 o$ o* O6 x, O% f+ U) ? 员的装置。 3 V" P. ?4 C( l- y, m冲器, . M" S7 w: i( x$ {) F; P u液压作动筒中具有节流孔的部份。这些小孔能通过限制 ! |3 l0 h, H0 ^4 e液油,以减低活塞速度。9 X) c& A% e8 p9 E- T" y 储存在计算机的指令程序。用来控制计算机系统的工; E: g7 E% B$ w s+ f; ~7 m 作。1 e) F8 x( `- x4 M$ C; `. p' Z 操纵其他设施的机电装置。3 Y, K; Y! W# h1 b, L+ ]5 j 电磁活门, $ r9 N& B+ T0 o( S用电磁线圈来控制开关的活门 ( B' D! @5 c9 O8 nw. R: ^* y; j. v6 B) B c" c% Z$ @, T0 S* Q S ) U& Y- {; K* I' io 1 N: k S. n( B; YSOLENOID, An electro-mechanical device for operati % `# a, H* a" u- |. v8 R斜度, " |$ Y ~ E, y* `) O跑道表面相对于平面的倾斜量。 $ @$ I! n' L; D6 W! U" x- M& r4 `! V! ?7 ?) F- @- {& G! m( L: R7 [4 W5 J 软件, $ I ~9 o# V- `: f# g电磁线圈, ; Q; C( P% d! ^- d- i用以 ( V7 ^2 }. f9 f/ V( w英汉对照民用航空词典B OEING " \; p' O8 n8 U: ?1 P5 e9 xTECHNICAL DICTIONARY 1396 ~1 G* V8 x8 I0 L7 J J SOLID STATE SWITCH, An electronic circuit that: W/ F2 X: e( J2 |) x3 p4 F provides switching in a current path. 7 ~5 f+ R/ B# K3 }) \% J0 L' x- jSOUND SUPPRESSION LINER, A component in the9 @% _& |6 v1 e2 ~4 e G nose cowl and around the engine for absorbing engine ' s- y7 f" k% |3 fnoise. " S9 H0 D+ ^" E1 J- s6 A9 ySPAR, A principal spanwise beam in the structure of a 9 b5 n# p# ~: p4 Q( M0 \SPEED INTERVENTION, Pilot control of the speed 8 o1 J3 N1 q* }0 ^4 h y& f1 ?SPEED SCHEDULE, The planned speeds for a specific 7 \' ?8 `0 [4 l9 B, O9 o* Lphase of flight. + B7 E; H" r* t9 Y4 s/ a. s' O晶体电门),5 |" x% J m& d% V& w 消音衬, 3 [3 P* q" c4 c在发动机的周围及前整流罩内,用来吸收发动机噪音的0 L% H) H2 w) {* ^' h( T 部件。. ?/ ~# b8 o2 K0 \& I3 F# \4 n; L: E 梁, 1 N0 `- o9 [4 X/ C& U6 J机翼、安定面或操纵面结构中的沿翼展方向的主梁。: @8 N! A. q5 F8 j. v 速度干预,/ Y2 j& D* \% \, v [ 计划速度, ( K4 G; ?& \, H, L+ j为一特定飞行阶段所定的各个速度。 ( S+ l2 i: `! R! `+ @! f! Hwing, stabilizer or control surface. 4 t+ c! G- Q8 m4 k R4 nduring VNAV operation." j0 R: D9 t) p' V( p 固态电门( * j1 C' V" m% Q( k在电流流经途中提供开关的电路。2 J' w# j% ]- m4 Y( e 在VNAV(垂直导航)操作期间,飞行员控制速度。 8 }2 Y& q; g/ t, s3 D" u英汉对照民用航空词典B OEING' s$ f. B% y. t9 o! F5 x TECHNICAL DICTIONARY 140 4 j: y9 u" V x+ n- I# _- wSPIN BRAKE, A device in the nosewheel well for , \4 i/ [9 r# [. y" H/ _; _stopping the wheel rotation after retraction.8 y, X& k, a# n6 D' O2 I7 M4 q6 w SPINNER, An aerodynamic fairing attached to the fan of- j/ R5 Y% \) C' ]/ Y* i! v a turbofan engine. * w7 T: G3 X7 \2 KSPLICE (NO. 1), A connection of two airplane skin $ H+ i3 g( |' [& u2 csections. / \( g5 F; A' ^# R/ ]/ _SPLICE (NO. 2), An electrical connection between two) @: U9 {7 D3 c0 i# O# F wires.! l+ q) i, @9 A3 g8 i; B% `* C 前轮舱内用在起落架收起后不让前轮再转动的装置。7 w" E" M/ i0 u 旋转罩, 1 D( t6 u" E8 I固定在涡轮风扇发动机的风扇上的气动整流罩。( A/ Z3 k+ Y6 a+ l1 _' c( B 拼接, " W- J4 o/ I! ]% b, r3 g8 a飞机蒙皮与蒙皮之间的连接。, O5 }' F2 R2 a 铰接, 6 g6 Z! ^/ f: y9 o4 s. O: H两根电线之间的电接头。# f4 B' w" K2 j/ C8 v) L 停转制动器,+ Z' Y+ n! e/ b3 d- C S 英汉对照民用航空词典B OEING & n% J; S. E( `1 D e0 [% T$ y- f1 u5 NTECHNICAL DICTIONARY 141 2 ^. K D' J) z+ tSPOILER, A hinged moveable panel on top of the wing. " s1 I7 E3 P7 E2 {Flight spoiler- assists ailerons for airplane roll & G: `9 x2 [) O8 b(wing up and wing down) control0 w; g4 i4 F- G$ X. j5 H/ d. H and for aerodynamic braking in L% I; f% q" z+ ^ Ground spoiler-for aerodynamic braking on the * U7 c$ v; ~8 P7 dground only. 4 o& R4 S0 O, Z5 A9 \0 SPRING LOADED, A condition in which one part of a. B( J4 ]" z" Q0 _6 X C evice is held in a particular relationship with another + A, a) i* U1 S' ^1 v% Ft,( i% k% z% |9 X0 H3 E& F: @5 B. m r original position. & e6 n1 m) i( U( G) wSQUAT, Airplane on ground condition. 4 d0 V7 f1 W4 H P- c) d B6 HQUAT SENSOR, SEE - AIR/GROUND SENSOR & K; Y, ~$ C# ? E1 H/ bSQUAT SWITCH, SEE - AIR/GROUND SENSOR : V( X$ k$ j' B- Y, D: G扰流板, ' V+ |, Q' @$ h5 t {4 Q% p1 y铰连在机翼表面上的可动翼板。 * Q, p- z K b飞行扰流板一功用有二。一、协助副翼来操纵飞机 * q+ u5 O9 q- {7 v的滚转。二、用以在飞行中或地面滑" ~. m2 u! k& T% ]2 M 跑时作为减速器。7 a1 |5 I9 z s& r 地面扰流板一仅在地面时作为减速器。* M8 X5 W! \0 J5 k 簧加载的, l7 `# E2 q3 S1 _ 由弹簧使一个装置的两个部份保持特殊关系的一种状 , ~9 ]* o. W& W/ A- |态。该状态允许一定运动,但继而回复原位。 2 ~, z0 r6 G( P, B) X' b# f2 x+ a着陆传感器, V+ o5 B p( z" n und Sensor# F+ E/ h% P8 d4 p2 ^. w. ?' y- b! O flight or on the ground.. I6 X* Y h. K3 F7 I/ r S 3 F0 y# _' r* K. Ld- z9 A# O" t" Q* X- K1 O: [, f part by means of a spring. This allows some movemen $ C2 S7 e1 ~$ S: Rbut returns the parts to thei3 P; k# r/ d5 ~- b# P S9 r! a; D! C0 R1 W) b; _ n2 h8 S/ g0 u+ I; Q! f! n: S着陆,1 k# s% v$ y$ N0 F5 n5 ~ 飞机在地面的状态。 ( O4 H n; _8 ]/ f) p b见Air/Gro 8 S/ N5 R8 f% |0 ]/ E着陆电门,' z$ j! `0 H$ T1 |* I6 J 见Air/Ground Sensor . & i- R* n, u8 b0 J英汉对照民用航空词典B OEING ( ?: E1 h" f) V7 R5 f9 c! ?/ }TECHNICAL DICTIONARY 142. L# d8 I( L" n8 G' f SQUAWK (MODE,CODE, FUNCTION), Activate- n" x7 S. n! l8 W specific modes/codes/functions on the aircraft 8 q, i3 m& a6 }; }0 `7 [ansponder, e.g.,” Squawk Three/Alpha, Two one zero x; q9 V1 _" a8 [five, Low".( s* q6 |: r0 j" y0 o0 `* i8 | SQUIB, An electrically operated pyrotechnic device for , Z2 l6 S; [% T! {% l' Ubreaking a disc in the fire extinguisher bottle to release , _/ ]' [# t" u' _% g3 ]9 ~8 M/ [. athe extinguishing fluid. Also used for escape slide1 N& T+ [# b2 c. U TABILIZER, SEE - HORIZONTAL AND VERTICAL 3 E, J1 q- u# G/ y2 P$ z2 j# zSTABILIZER + `, W2 {- b8 j8 S7 C' ZTABILIZER TRIM, Movement of the horizontal tail to8 }0 O" `4 }! h6 w) L hange the attitude of the airplane about the pitch axis./ x! Z. |3 E9 O+ v8 E0 K TAGE, A numbering system for the compressor and* r& M% ^" T* k: o& N; l turbine of a jet engine.9 h, N3 P! @4 ^ TALL, A flight condition during which lift is destroyed 0 O4 _% D; P' Yue to slow airplane speed or attitude.( I. {3 m3 a6 J, }! U to enter from the top and flow 2 j& U- G2 l. d# i& u. qout to the system. It prevents picking up debris off the , ^+ |4 J" E5 S. }5 b, tbottom of the reservoir. It can also control fluid height in % b! d; [. T) `the reservoir.+ f4 |: z, Y, ?: o3 J U, }+ ^ 能),* G7 n2 Q1 v1 j 使用飞机应答机时的一种常用的指定方式/代码/功 # E* a) } P. ~: ^4 z能。' c: ^: }, j X' Y+ d 管, 3 B( U: |6 a5 O% Y8 o* B- B用以爆破灭火瓶上的圆片,以释放灭火剂的电控烟火装/ t; F* j# z7 O s 置。也用于应急滑梯放出。 , Y- L6 K( u* d& ?0 T- T定面, ( ?+ { [, V+ M见Horizontal and Vertical Stabilizer* \9 G; U4 [ e/ U tr 0 Q9 Y3 e# ~* S# V8 ~4 l- u+ zdeployment. 7 j$ \: T0 y8 u6 c, `+ y% G2 VS : O: V, I# c7 ]3 B- YS! H& @8 t! o- f; p2 m F c 6 b% W. \* r" ~6 [, q8 H, kS% H8 f4 A, c( W H0 H$ U8 M' w) U2 n S1 ~& {3 J( ~* o- q3 y d; i* Z: T9 p, m. ?" [9 b STAND PIPE, A pipe raised up from the bottom of a # \! b5 B2 e. X4 j0 [reservoir that allows fluid - ^! x# m" H+ E8 V& ^) H2 c* x发送信号(方式,代码,功 # t% G& b( W. P) V3 A5 |( k! j& e: j- ~/ U4 ^6 e1 I9 n; @) D( X$ y2 O; W3 y) T) S/ N# s+ W3 `" [# [, { 定面配平,4 z+ x2 ~$ y7 R$ C3 |% s5 q0 a 为改变飞机绕俯仰轴的姿态而做的水平安定面的调整。) @5 A* x' T( Q1 }. D! p) Y 级,% M/ I# O2 m5 h4 { A 用于识别喷气发动机的压气机和涡轮的各个段位的一6 j. C# I4 [' l5 b7 a0 f 种编号系统。 ( M- Q* d0 Z, y5 [; H4 a y失速,2 P- f# i( V. S- D: q1 B) B* F s 飞行速度过低或姿态而引起升力失去的飞行状态。 ! _* q+ U6 ]4 T; b' ?/ x回到系统中,并防止带起容器底部的碎屑。也可控制容+ D) m$ ~5 j: {. A5 u+ a 器内液面的高度。" t2 ? Y9 D7 G4 j6 H {. S6 S2 U% i+ C) @. w 立式管,0 r' p* C/ R* |: h. I/ R 从容器底部立起的管道。能使液体从上流流人,然后外6 ?; O8 }0 H7 y' K9 P- \* m6 D1 Y2 w" s2 s 英汉对照民用航空词典B OEING" y; F" H% u; c4 a- [" l6 s TECHNICAL DICTIONARY 1438 q( K6 h# d, f$ a STANDARD INSTRUMENT DEPARTURE (SID), A $ a* P2 ^$ g9 y# M: ^IFR.6 s! K3 @/ Q. s0 ^ TANDARD TERMINAL ARRIVAL ROUTE (STAR), A ( t# z; t# ^/ c2 H/ u7 I0 _3 S6 V! rublished procedure for approaching an airport IFR. ! B3 H: ]6 g; Q5 uTAR, SEE - STANDARD TERMINAL ARRIVAL2 C. \7 f3 p) `3 ~1 L$ j OUTE" A6 s* F2 v! b# Y; |9 @% P TART VALVE, A valve in the engine start system for 8 ~ |3 F- ~( ?: o# ^upplying air from the pneumatic manifold to the engine 1 \" A* O" G* B! O5 A1 @tarter. ! o) H% g5 R- \; o7 a9 }: ~: ^5 n6 rTATIC AIR TEMPERATURE (SAT or OAT), Ambient4 K9 C6 `" Z# E* o+ M* @2 w9 T or outside air temperature." u5 j: s8 y( a I* r STATIC PORT, A small hole in the fuselage for sensing6 u2 d4 [3 g; g, Z2 O- X" d static pressure for airplane instruments.& O3 X! t7 [: A P% ?* L STATIC PRESSURE, Pressure in the air or fluid at rest2 j, m$ L- E4 V0 B6 n measured in pounds per square inch.9 `$ K; d8 X7 W, }8 B( Z: d ID),0 v/ c6 P0 S! T% @ 用于使用仪表飞行规则离场公布的程序。 . R* d& R- G, x4 E% ?; @4 g B标准到场航线(STAR),! ~2 ]1 F1 w8 } 用于使用仪表飞行规则到场的公布程序。 $ h0 o2 @1 k( b/ G4 R: Q标准到场航线,. J; A/ i2 K: t3 e6 I1 h 见Standard Terminal Arrival Route- @/ C) M2 ?1 H4 D' Q published procedure for departing an airport - m( T& V9 V& Y7 g' y/ [6 wS . `# @- C' O A. G# A2 j! c- ^3 Sp- k& T! A6 I. p' |( c S 4 B8 r( @# p6 G+ }) C( I, FR : {. v4 J V; m, b" ^' w- _1 u$ iS# y$ s$ _& b" b0 m s 5 L# N& I% |2 H( as 4 F! _% j6 ~# r# hS 5 `( F2 w! V! W3 m! n标准仪表离场(S / ^1 ^+ [2 B5 s+ \& G2 p" z M# K; E: f 起动活门, ! N9 p( r F$ b3 {7 i发动机起动系统中,用以从气源总管向发动机起动器供 " `: ~( v) Q% R" o' W# t w3 x的活门。$ P5 O$ U5 H4 F! H) g% `! f) c. x 温(SAT or OAT), 1 z# p+ N: G9 `; t a, ` V1 X环境空气或外界空气的温度。 9 A% x/ O7 F7 q3 D9 C0 v压口, / L4 a$ W9 S$ X5 z9 }位于机身外表,用来为飞机仪表感应静压的小孔。 2 L, e5 _# l8 \: C# r7 T1 Z静压,& E) m" _( a- U- p 静止状态的空气或液体的压力。用磅/平方英寸来度量。6 |. U$ A- _! I$ b9 f" _# X0 V$ S& R# k( T" V4 e8 f. V+ a U. o p! s/ g' W3 W; i/ X, d. ]英汉对照民用航空词典B OEING 3 v* C* G; _/ WTECHNICAL DICTIONARY 144 m/ z4 k; P# _/ c% H2 @ STATION, A vertical reference plane along the fuselage 1 `0 V* `4 r5 f, L4 A" bfor measurements along the fuselage.$ D: F; ^# L, V9 n" B& o; S4 C TATOR, The stationary section of the compressor ' A* k3 U' Y& C: A1 ^etween the compressor stages in the jet engine. % {5 B: m* ]' K3 PTEERING ACTUATOR, A hydraulic actuator on the " y' j# O0 U& j; ]% n' r$ h8 blanding gear shock strut for steering (moving) the 9 h0 J- K: k. N" C, o! x' mnosewheel left or right.* X' X& C" _; y0 ?0 k$ b$ w5 W TEERING TILLER, A hand-operated lever in the9 _$ m! H" `" j# M3 _8 k osewheel left or/ R8 `. i# r& K @ ght. 9 m4 O* H+ u- |, n3 JTICK NUDGER, A device to push the control column. E0 Z B+ p& g7 N rward just before a stall occurs.( A3 ~) U. } |$ r8 ?7 N 站位, - x3 w: `+ M: {$ e! O4 I用以沿机身方向度量的垂直基准平面。4 n8 g- {6 _$ w) Q3 V4 Z0 G 定子, ^( l6 S8 j2 N+ Q) u+ U喷气发动机压气机各级之间的不转动的部份。 % f# p1 r0 e" P弯作动筒, 9 C: c+ q' e" {" ~) K. D减震支柱上,用以使前轮左右转弯的液压7 r0 Q% |1 c8 ^: h' N( @$ h! [' @, {& w 作动简。% e; B% C; G0 t! X 轮转弯手柄, 3 X& x; R0 G3 k# O6 R% S7 a' @内用来使前轮左右转弯的手柄。; u: \7 p7 A0 ? R 动推杆器, , M( m; D% f0 _; w. c" Y1 Z- }2 o7 ~在失速前能将驾驶杆向前推的装置。 9 t; U" S% r/ |4 }- fS ' `9 ]2 K6 G7 f, ^5 j7 Y: ab 3 x! f. l8 w1 _. xS3 ?3 `- f: f9 o3 o1 p S2 `% p: d+ X. M8 v0 p& ? control cabin for steering (moving) the n ) U* N U, [2 z, P+ `0 P; rri3 U3 `. f& B4 |, s4 | S* B2 G6 q. Y) N8 f) W* ^ fo 1 @6 e( L8 q# h x& _$ t0 Y( |* x, J1 v0 ?' h9 P/ i 一个在起落架+ L/ r( u' R; d& N' C. c" h- S& i, ?0 {7 n: p; |: `0 b8 _) T3 s驾驶舱$ q" K/ B: d. z9 e; D* b# B! e) V# B4 h- ?4 n3 T* T$ q+ e英汉对照民用航空词典B OEING 1 D) K# m1 p) E* _! Z$ D" FTECHNICAL DICTIONARY 145& x$ I/ x( [& |8 }( o STICK SHAKER, An electric motor operated devic9 Y$ \ V) Z# D* Q the control column which shakes the column be# K) K' q( F9 Z! B; j stall occurs./ q3 K% N+ Q. s e on0 i* J3 R9 ?9 w) P. h+ u fore the 9 v2 }' w/ ~1 ?) Z- Y4 s) zTOPWAY, An extension beyond the end of the runway * ^. E7 ~4 B$ o" V$ p' k; Which may be used to decelerate the airplane in case of # d+ W9 \5 I6 O% `: ?n aborted takeoff. It cannot be less than runway width7 K* R! o" M, `$ h- X" x' O and must be strong enough to support the airplane- B) t& @: T7 v# Y" w2 n 置。 ; V2 j E& u. U* V% a# f速安全道,% c3 l" \8 z1 z: j" Q9 D 跑道两端,可用作在中断起飞时飞机减速的延伸地带。3 q" G4 ~1 f* [: \# a! B; @ 它的宽度不能窄于跑道,硬度也必须能够支持飞机以免结: r5 n! z7 f! U- ^" Z S* U2 G- R! R1 H% o0 Q. T: }% u w + y" `5 b8 [0 h/ x- w1 xa- I( ~- \% Z0 M2 j+ V/ g without structural damage.+ C7 k" D: v6 H/ } STRAIN, Structural material deformed slightly due to the 4 `; X1 S4 a0 H$ G5 K: X$ paction and forces of stress.+ y4 H2 h w& @2 J& v# K 振杆器, * ]3 o, r& m8 `! z驾驶杆上,在飞机失速前使驾驶杆振动的由电马达操) R/ R* { D5 [# n) U3 D1 g! r9 z5 S2 k 作的装 # I0 [" Y$ S6 _& p; d4 a ^1 H7 {* w) H- p+ G构损坏。 7 P" q# v, f/ A8 h# C# P8 W% h应变,) W* p) r0 R8 b# X( I6 Z! M 因应力作用和受力而轻微变形的结构材料。# e5 _, d5 u( A! }/ ~& ^5 g# K 英汉对照民用航空词典B OEING& W; E* k1 K; ?* L2 c+ \, f9 q TECHNICAL DICTIONARY 1464 t/ I, \4 N$ F2 E4 @& ? STRINGER, Structural components in the fuselage or& q. Y6 i; e: y7 I5 ^ wing for transmitting skin loads to frames or wing ribs.* l2 d& S1 D( K7 g# h STROBE LIGHT, A high intensity flashing light on the+ P7 }2 I X6 H wing tips and empennage. ) l6 i; f. B8 P' L6 VSTRUCTURAL MEMBER, The part of an aircraft : a P* D7 v) K* s4 R0 S+ V" Wstructure that has been designed and constructed to' G; a2 } J0 m$ v; V carry and accept loads and stress.* a+ P6 t' g* ~7 s$ Z# r STRUT, Mechanical components of the landing gear for$ V/ x q) x$ e/ W! j keeping the gear in the extended position.$ y2 S$ T" w9 W W7 D 机身或机翼中,用以将蒙皮载荷传至到隔框或翼肋的结; q) G2 E4 V' q2 N) s 构件。7 m/ A- q y/ I8 [3 T; T; A( {7 Z 频闪灯光, 1 [- V- V, p- B0 w# j位于翼梢和机尾的高强度的闪光灯。2 e% O! Z2 i" u, }3 T# M+ k7 z5 i; @. x 件, 8 u# e2 W' d, ~- s( Z飞机结构的一部份。为运送和承受负载及应力而设计建 # K3 T& P2 v5 t! d9 p成。; m9 d5 C2 k8 E* w6 z6 X 支柱, # v$ m y5 K. H& H+ W起落架上用以使起落架保持在伸出位置的机械式部件。( f D1 |$ @* w! o: u8 ]# a3 E( B 长桁,4 E6 n/ ?0 V: f8 L7 X! J, O! w8 {! ^" Y& a9 ^8 Q; B0 N. o, {+ i- M. A. I6 R7 ? 英汉对照民用航空词典B OEING 3 [: ?+ |7 h+ `$ B/ }3 y1 _TECHNICAL DICTIONARY 147# |- e* P* M) [/ o n SUMMATION UNIT, An electronic component for o/ X4 f1 I1 d! a- c adding fuel quantities in all tanks sending a signal to the( _( F. _' ^* W8 ~# ~: h. g tal fuel quantity display.* ]" [/ O* q! L( T UMP, A lowest point in the engine oil system or fuel 5 i6 D# f8 B3 {9 dnk.0 A7 X$ [& p, E UPPLEMENTAL DATA, Additional data stored in the8 B+ Q& j7 S1 a9 e1 G' D MC memory, supplementing the loaded navigation , _, l0 A+ [: Y; D- D/ S, {9 I+ Wata base.$ Z% d0 o* o0 N n' Y N6 o1 b8 q" ~5 H eviating from normal modes. % U9 o$ B! ~0 f2 r' l: t6 }SURGE, A sudden change in the airflow through the 8 B9 V+ r5 J8 G4 X( E! y% Othe compressor not being able$ b% e8 F% G1 x: Q" o- ]+ u compress the airflow.( M1 g" t& X9 E8 m SWAGE, To squeeze together two or more items to6 g% L$ g, P* G! h form a permanent unit. Example: a lead or steel piece/ r1 x8 ~' y( A on a cable which forms a stop or camlike unit. Also to. i2 k0 G( E* ]( O$ T, k reduce the diameter of tubing.2 x3 n$ N% E1 M6 d, R6 l9 A SWITCH, A device which changes the condition of an8 C" k0 Q L! m" ]8 p$ M& E6 {4 B electrical system from on/off or open/close./ V `- a( o ?( k; i2 }/ ~1 P 燃油总和器, " @; U f5 e* ?. g将所有燃油箱内的燃油量相加,并将总油量用信号传至 # Y; R% |% H/ ~& Z8 O" {/ z量显示器的电子部件。! ?' T. v" `& w 集油槽, 0 {, h! E7 z0 i6 L1 H. R7 g a+ }发动机滑油系统内,或燃油箱内的最低点。 ' W: {0 u3 A j4 g5 s, T增补数据,( y8 X% x+ a q9 e/ |8 G; ^ 飞行管理计算机存储器中的附加数据。用于补充导航数 & [5 z+ n; f$ s据库。 ( i9 r2 Q5 D( O: l% R1 ?5 ]( {9 y3 I$ E2 Q w$ @5 X附加的数字飞行控制系统方式,当偏离正常方式时使4 ?! P9 w. Y: d5 D9 C) n, A8 [% q- c3 x8 t( Q过发动机的压气机的气流的突然改变,而导致& l. R- {5 [- [5 [ 气机不能压缩空气的现象。 7 r& R7 ~( L- [0 K陷型模,$ p( H. T( ^' C, @- y6 k; H 挤压两件或两件以上的物体来制造一件永久性的元件。 1 l6 d3 t6 U0 W如:一块铅或钢在钢索上形成一个止动器或凸轮之类的 - w2 G# \3 z4 @* H8 U件。也可作减小管道的直径之用。/ [; H- U$ A1 q. A* A# ?9 M 开关; 3 g3 @; ?3 ^% q) I改变电气系统通/断或开/关的装置。 1 G& C# ` F5 {. b1 @! P2 ~to 4 O$ V [$ O' a+ J2 K4 T8 q& Y3 ?. Y c7 OS' l" E! I! z+ D' m. ]6 B ta7 [( y# n& d6 q& G) J S 2 L' a8 U* }" A0 ~: e. ^F) q) T% m9 P# b. s4 @" Q d 4 U6 o9 [+ s/ v. ]% ZSUPPLEMENTARY MODES, Additional digital flight 2 `2 L: p5 T$ E w# N; P: Pcontrol system modes that are available, used whe 6 k. M( u5 v3 Nd * T5 C$ ?* z$ |% y1 U4 f3 jcompressor resulting in# }: j% x' I0 D to 5 o9 o6 C, J. k' K2 l$ P: d) V7 h; `- U* v% T$ m# U辅助方式 ( H5 J& l, Z$ E# s2 r8 o: `: n& b! [; x 喘振, j* D# E5 Z0 h a" }$ Q9 Q: { 由于通 , F0 m/ d2 e* q, b4 @# X+ k% s) r0 a) B ~ f8 Y% L8 u5 F5 {/ i3 x, s4 |; D; ~ C3 N6 \( F- z: X3 k 英汉对照民用航空词典B OEING 9 W! v0 p, S; w8 oTECHNICAL DICTIONARY 148 1 C# T9 _+ r' c9 ISWIVEL, A device for rotation of components.. A2 j9 j2 o4 J; m, g" a3 J SWIVEL COUPLING, A junction in hydraulic7 q' `# O" S4 k1 M bes for allowing component movement.1 W" k: ?; H5 M, |- c YMBOL, A graphic view of an aircraft component in a 2 K) v! r' p, G2 |# V1 p# u! aery simplified format. Used on drawings to represent * @% r' \, ^* z6 k9 g$ w de entire component. 5 [( S3 V/ }3 N! fSYMBOL GENERATOR, Generates the video signals 8 ~. W$ f, q' E. `) R" Y7 Mthat are displayed on the EADI and the EHSI. * c2 ~* e( T8 g, ?3 C% \( NSYNCHRONIZER, A device or circuit to make the units / x, r( V) F- l0 xperate in unison. & o! n' a e5 Q( TSYNCHRONOUS, Refers to two or more things which$ X) {6 |: D( G7 H& K' | happen in a system at the same time.. ]' E# X T! o" a3 a- p/ @ 用以使部件旋转的装置。1 v! O/ R! V8 j( F ?7 p Q, f 转动接头,* L) g4 v! }, ~! D 液压管线上,使相邻的液压管能够动的接头。* j0 M3 o7 g# u- h 符号,0 d5 [; E6 l( J6 f 飞机部件的简单示意图。用于绘图以代表部件的整个结% P, a: s8 |6 _) `, `( X 构。 ) z2 `3 y: d3 w+ a& N3 f符号发生器,; l' o M, R; _6 r" k* x 为姿态指引仪和航道罗盘产生图象信号的装置。 + `) {' S- g4 s. P1 \% d& D同步器,$ G, |" h6 A% o( X3 p 使元件操作协调一致的装置或电路。" A. Z6 u, t) z, t8 r 两个以上的东西同时在一个系统中发生。 3 a! N! a2 W6 U$ j5 ^tu6 z. |2 q/ d7 W9 k3 C! R S# u9 n3 m' {& F/ L0 ` v# q4 F# q# l0 B1 |- i" O+ V: G% Z th3 D, T; M+ r+ `4 f o 9 A+ D0 o) U& ?* k转座, % j$ t. a0 t {2 [同步, ( a& W( I* z* e0 u. O7 d指两个或! T3 G1 T0 G% T7 J1 a% z. N 英汉对照民用航空词典B OEING 1 e5 L: I4 E+ l$ d+ h6 ?& D8 w: rTECHNICAL DICTIONARY 149 8 d5 u! {; E- M6 O0 zT/ M A: p9 Y' b; g' R3 _ AB, A small, hinged, moveable part on the trailing $ j* F$ @2 _/ bdge of a control surface (aileron, elevator, rudder). % W1 g+ a' q1 T7 `9 j5 s2 QBalance or control tab - moves in an opposite5 s. V7 s8 ?" S/ o3 v6 @. S direction to the control surface for assisting * `# R4 F9 U" L4 min movement of the control surface.& ^8 |' D1 N2 {6 Z" m7 U Trim tab - provides controlled deflection of ailerons2 t9 g [# k! u, N& y or rudder to compensate for imbalance in+ g \" j- q& l! L1 j thrust or fuel quantity. 3 o( I" c- m3 J/ J0 AStabilizer trim - controlled deflection of the horizontal% O( R* N$ v3 v" M5 h/ ~ cy * h4 t% ]* T+ Pproportional to the speed of rotation. $ B- C% x% K, D9 O& }TAI, SEE -THERMAL ANTI-ICING 2 u4 y Q0 c/ [' cTAIL PIPE, Duct at the back of the engine exhaust. , F) e6 J* K0 g" H+ m# LTAIL WIND, The wind component relative to the % U0 V- x% ~3 @/ V2 d0 ?" y8 sairplane direction and coming from behind the airplane. 9 g c6 p: I9 o3 F/ v! J# ^$ b5 D: N调整片, % U3 f8 C$ ~' g$ t8 L铰接在操纵面(副翼、升降舵、方向舵)后缘的可动小 $ T+ \/ ]7 d4 t( g# ^/ [: I5 {' |; X部件。9 M+ m+ t" z9 T9 M1 w' j( I L 平衡或操纵调整片—与操纵面运动方向相反,用以帮+ S. @7 ?9 ~3 t. ], V 助操纵面运动。 2 b, q6 n# q2 z" U配平调整片—使副翼或方向舵作控制之下的偏转,以0 L/ @. Q- q: C5 f# T: x+ s 补偿推力,或燃油量的不平衡。 ( _+ q/ h( C; o5 d! O8 F安定面配平—使水平安定面作控制之下的偏转,以减 % P' C# |& T8 t. g少操纵力。/ m y* {- }) v! C, [3 \ 机,6 T; O1 w6 Y+ L8 }" ~# ] 提供频率与转速成比例的电流的小发电机。 # T6 H7 q7 w1 O% l热防冰,$ C( u# B8 D1 L& o. V" J3 D1 U. e 见Thermal Anti-Icing & I8 \% V& \8 B( v! j% [T 8 C5 @: E& t6 J" s4 De : T( ^9 Y5 J* O! pstabilizer to reduce control force.1 ?9 I6 ~' Q; M9 @0 q4 \. F TACHOMETER GENERATOR, A small electric( H: J! A0 u) f4 \ generator for supplying current at a frequen* a0 F) `& D2 l, B# b( J* W- M5 H 测速发电6 r: C) F5 \5 i" z. X( @' C% X+ b1 u4 T尾管,0 f" X2 d$ c W 发动机排气管后部,用以排出发动机的废气的管道。 . U: W7 M( d( A e% P& a/ R顺风, + s) ]1 I0 ?7 g; `0 Q飞机后方的来风在飞行方向上的分量。3 w1 @; L) z# m( p; R. l8 z( M 英汉对照民用航空词典B OEING7 w) b. \6 F; A7 \/ n% b3 \( O1 ^ TECHNICAL DICTIONARY 150" g! o8 d/ f, g: d J, L TAKEOFF ANALYSIS, Analysis that evaluates the - j8 M! `& c" @6 d$ i8 l" pairplane takeoff performance capability for a variety of - u, `$ |1 v/ Z* zenvironmental factors at a given runway and airport. 8 N' |* R( u/ K& M' j' cET PARAMETER, A specific goal such as( q+ h8 j# N( F' S8 t# D irspeed, thrust, engine speed, altitude, temperature, or 3 ]* e5 _& ]- } t: w: C4 _te of climb which is to be achieved./ t$ y6 u9 ?6 P0 H7 X$ s ASK TICKET, A computer label used for tracking the# o$ f2 f" G4 ?, A/ I ompletion of a task.# ?1 [0 [7 _7 [" b1 A8 L RATURE6 M4 X& t- [( |) p/ \3 [5 |. s AXI FUEL, Fuel burned from the time the engines are $ I- o( Q% I, K& E( r) {r. # [' B4 s' o4 `" p. YCAS, SEE -TRAFFIC ALERT AND COLLISION 0 s- x5 V: h$ {8 O- T; R6 x) wVOIDANCE SYSTEM ) N5 D7 }) H, C% G欲达到的特定目标,如空速、推力、发动机转速、高度、; @: V' G- h/ {8 ?! h; ] 度或爬升率等。2 _( @- W. H7 B0 J( p s 工作记录单,$ p! Y. G5 Q" n; A8 x 用于追踪工作完成情况的电脑记录单。 % k* J1 F P* H' [! h7 A3 D1 ?6 c' A- m全温,. {. b7 _6 W5 _1 G# o. A 见Total Air Temperature - k" y0 ]8 D* gTARG : [ n2 r! e, N8 Da7 W9 I; K( h3 K. d4 E ra 2 |) ]- k/ R1 ^5 O+ x& V1 y& X, IT, x# X0 X. b* P c1 Z+ g8 W7 r4 {, S. V/ O3 P TAT, SEE - TOTAL AIR TEMPE7 M) i! D- ^% a% ?( t" ~ TAXI, Movement of airplane on the ground using/ b9 o) t2 J% ~' d& A% ]3 m airplane engine power.( n6 S3 l E9 e9 ^! j T4 A& ~& Q# l4 { started until the airplane begins the takeoff maneuve1 Y" Z& s) H H! L T ) j" J8 ^+ e) Z" `/ e- BA + d* B7 v& C5 l2 S" ~; r7 W起飞分析,7 E1 u6 _' k8 M9 Z3 D 对飞机在一个给定的机场和跑道,在各种环境状况下的' Y% N$ |! Z2 D3 t 起飞性能能力的评估。 / Q! ^; g! p, y R. j( Y目标参数, 1 Q; h# g4 d3 e- Y, \6 \1 {" ?: |1 D5 O. ]+ x·) t9 E! c% h: b1 ~7 ~5 L 滑行, 6 E/ K* m+ {1 ?! G行燃油, * [9 q. f) p. U5 B |! M6 Z0 Y8 N; x起动,到飞机开始作起飞动作之间,所消耗的; Z! F; f# x) H A" o 中交通警告与防撞系统,* b/ p. T* C3 `; C* k- }) _ 见Traffic Alert and Collision Avoidance System4 s8 L5 ~5 b9 [4 m7 Y 飞机凭借发动机推力在地面的运动。 6 U' K7 Q4 ]7 {* u2 N2 _6 a- d; Q. Y( C" s 从发动机 4 X8 k% d* g) E1 i% G) r0 c燃油。 - ?7 p! ~- V: g; @0 M7 ^, A* D0 f# J! ~; j9 s& p% N; u& p3 S+ J" q7 o3 f9 |, \英汉对照民用航空词典B OEING* `3 D( B) v# ]3 L! | TECHNICAL DICTIONARY 1519 J! n& R% }8 @% V7 B4 g TCC, SEE - TURBINE CASE COOLING# u# } X% T* ~7 q% T EE, A pipe or tube connector manufactured in the, _- o+ O2 E! Q4 P2 H& v1 Y& y EFLON, A synthetic material for hydraulic and 8 V9 n2 W# w* u# B$ d8 ^neumatic seals. - j0 R8 k* ]/ A( C. M3 MEMPERATURE INDICATION STRIP, Temperature 9 I4 V" K' y+ U$ l5 R- Aensitive tape which changes color at high temperature4 y2 P" B1 ?( [( X: t* p6 | r indicating component exposure to high 7 }% }! E7 p3 f( ~0 N; w+ }4 U. qTEMPERATURE INVERSION, An atmospheric% G3 {2 l4 Y8 m condition which causes the outside temperature to+ C9 c0 j0 z- x! ?: f9 N* R$ I% ~5 R increase as the airplane altitude increases." F9 y$ L- u; ~0 H/ G* a, x TENSIOMETER, An instrument used to measure the 9 O) e! M t4 U' j# `( p% vtension applied to aircraft control cables. % E/ q" E' F9 z冷却, + O* @9 Z2 i& W( xT 0 u4 d8 z( O: V( {8 ?shape of a T9 o) R$ C/ L$ v( `5 ^+ l+ v T 9 m9 @! A; f3 m( u% Rp ( ]# J+ O* G) t% t& Y# L2 r$ gT 8 I5 E. M; Z& D9 R' Ys - A5 U f( Y/ _fo" W. c: V D/ V3 s# _! n temperatures. , {& y; z7 Q, x4 d+ m7 [8 a7 s涡轮机匣 ; U6 A% C! \9 x" \见Turbine Case Cooling. $ E# ?- }" z- F字接头,/ c; r; z; @/ m- @ 的管道连接器。% ]. z! x$ e' l0 U 氟隆, 9 \8 n) r1 t: A/ \) p用于制造液压和气源封严的一种人工合成材料。) X* F3 y8 L0 s0 m 度指示带, % p5 b N3 U) i遇高温变色,以指示部件周围高温的热敏带。 3 O/ H) Z8 C7 e逆温, " V5 ]6 L( I. r, j一种大气状态,引起外界温度随飞机高度增加而增加。 - M0 P& p c* I' \% b( \9 @4 B) E张力计;; T. N; G3 _8 l$ a 用于测量飞机操纵钢索上受到的张力的一种仪表。& c/ M, A, f1 F+ w T7 ~" a7 B& a3 K# t, d 制成T字形2 d7 O s6 N% R: `/ X" U2 I8 U: ]6 V" l; ~4 O+ x2 f+ b$ D3 t1 ~8 Q3 ]8 z8 F英汉对照民用航空词典B OEING, P$ i/ g& T( t' E TECHNICAL DICTIONARY 152 8 W3 t3 s/ v$ z4 {THERM9 M& B: l2 a! ~5 f formatio2 d# x# ], S8 V using ho+ B& M6 S5 _: [, r& K AL ANTI-ICING, A method of preventing ice - W( a( {- H3 s0 K6 ]n on the nose cowl and wing leading edges by, T9 J1 }) g! m9 ~6 G t air. # S# D2 i6 l A4 D8 k2 sTHERMAL t 1 o3 ?* i# I( N* X* R% bin a tube fo en tube& j, h% W! G, y$ J is pressurized with oxygen.6 u' X( F" D4 w; Z0 \. W HERMAL RELIEF VALVE, A valve which opens to - V- c: D9 ?8 I% I# o/ lture. ' \ S- d$ C* sHERMAL SWITCH, SEE -THERMOSTATIC SWITCH/ o0 @4 a0 h: K( A/ b& t. U G e 5 I0 k7 z- ?. M% w8 a& N( X) isistance changes with a change in temperature.) o8 h+ u+ T' C( B% S 防冰,$ Z' o% ^! j8 S$ H! g1 T1 i 用热空气防止发动机前整流罩和机翼前缘结冰的方法。 U* y) ]3 ?& V在管子里,使管子受氧气充压时温度不致于上升的一% t, e. ?% ]5 s 个刷子形导线元件。 7 R. l" b4 v9 B+ T" S控释压活门, 8 W0 L% j8 }$ H$ s3 C过高而打开,以减低流体压力的活门。 8 m+ S+ l% w2 S" U4 y电门," D" h7 c: e( B: |9 o 见Thermostatic Switch, [# C! L" P) y! x6 U2 [4 a COMPENSATOR, A brush-like wire elemen 3 ?* A5 [% k4 O& \r preventing temperature increase wh% w0 s. n2 b3 A8 ?; _ T 6 U6 u, j3 f( J) |decrease fluid pressure due to high fluid tempera ' ]' K! `8 v& {, R/ y- ZT * f8 d) O, t8 [# y0 ^ i/ A, h& LTHERMISTOR, A temperature sensitive resistor whos/ O; J" `- `% G5 z' L, F, v: p re8 S7 f! r' v- q' ^- g0 G6 ^1 w$ H热补偿器, . c% j9 l! H j3 z- \% ~9 Q |- [, ~4 t* K' D+ q# g- q7 X# e p) q: ^8 F 因为流体温度 @- u- C' H; Y3 |3 E" l5 D! y; J5 L7 o/ [. M- m7 k, W# U: j9 Q- x5 ^9 p/ ~6 {/ l' t ,热敏电阻+ N2 Q. a ]% ?$ @7 m 一种电阻值随温度的变化而变化的对温度敏感的电阻。. y5 y2 n" f" {" @3 _! K 英汉对照民用航空词典B OEING . `( s4 Q- ~9 C+ ?) F" d+ {' wTECHNICAL DICTIONARY 153 , }: K* R5 l" n& t: X" Q4 qTHERMOCOUPLE, Two different metal wires joined at9 p0 t) m# K9 I2 }, v4 Q urrent is produced proportional to the temperature 9 N! n% n* b o+ ~9 j8 Adifference.. |7 i5 @' D5 f THERMOSTAT, A component set to operate at a. N8 T9 ?& S& L: w' H efinite temperature for controlling electric circuits and$ v7 V/ l8 a8 K K: @ alves. 7 Z; @, p$ ?7 Y) E6 Rmperature sensitive switch which opens at a preset- D+ Z/ w9 T ~* O1 y# N0 z" z0 r mperature. 8 ]% T1 _3 u nTHR HOLD, SEE -THROTTLE HOLD7 l1 z5 r8 g3 y 即产生与温差成比例的电流。 ) R7 J4 r% H7 j' ^用来在一定温度下操作,以控制电路和活门的部件。) u5 W( G6 m Y' R b3 V9 [" F/ ^3 L 恒温电门,! P0 l. z' j1 A3 }7 _& j 一个热控的、在预定温度断开的热敏电门。 2 q- i# a1 F/ j1 d见Throttle Hold) K# f. U. w! Y3 f1 h both ends for temperature measurement. When both- ~7 \% P5 n% E junctions are at different temperatures, an electric* r' N) K* ^6 @! N, ^ c 5 V; y# f$ e" N+ {# P- t% jd* }' h0 `- N5 S2 K3 Y" ?; ^. _( D v- k. ~( \4 q6 |, r- g, G* x$ B2 E THERMOSTATIC SWITCH, A heat controlled, 4 F# d- M5 `7 `te+ T* |+ r' X* q+ B, O te; A: _" E' P" ^ d* S 热电偶, ) U% d, f+ C/ S1 q用来量取温度,两端相连的两根不同金属导线。当两端 4 F; @: m) N- W; T T6 d# g. V& i之间有温差时,金属丝内 - @$ C' ^% G! W3 x( K2 B恒温器, ! ~, y- J% p: E0 y8 B油门保持, , m j3 k( O c! }* i2 |: C7 _5 W# z1 \0 B. G3 u0 J7 _; Z2 F1 o 英汉对照民用航空词典B OEING ( G: Q' i/ v* e0 ~1 WTECHNICAL DICTIONARY 1542 t7 x; V& g! R( k" ]4 } G' R; s THRESHOLD (NO. 1), The bottom part of an opening in$ h# Z4 J" ^2 i( a9 m a fuselage doorway. # G$ P3 \. Y" R" \1 _/ ~2 r. 2), The approach end of the runway. " U( }- V" j- z: @ t( [THROTTLE LEVER ANGLE, Angle of throttle lever # w' Q V+ z( Y' }; ~6 s( pdisplacement./ l i! B- |( [: N' M; s HROTTLE SPLIT, An engine control condition in which " x C) z( w5 A( Jthe throttle lever angle is different between throttle( W! @, v$ V& P5 W& R$ r levers but the engine thrusts are the same. & Q z+ L; P, _HROTTLE VALVE, A valve in the fuel control unit for % Q7 ?& R+ g# k9 c: M& Hcheduling fuel flow to the engine., _) A$ m0 q4 D8 l! n5 C 机场跑道到场的一端。 * D/ p! ^8 X) g; n9 o2 p0 X. P油门杆角度, K O: _0 m& Y. V Q! c油门杆手柄位移的角度。 7 i( a( E4 M! I r+ T( r$ {油门分叉, 8 { W, L9 Q1 s! p: t1 G1 A一种发动机控制状态。在这种状态下,油门杆之间的油6 \1 e7 \/ W" F7 L 门杆角度不同,但发动机推力相同。8 t. R4 {# L, F% v& b 流活门, , A5 ~9 N9 O0 f( J0 b4 s# e& D燃油控制组件中,用以排定燃油流量的活门。( T2 M( o9 q$ v; y THRESHOLD (NO) e. o$ Q3 ]# w" w THROTTLE HOLD, A mode of the autothrottle where* i9 d2 c% B1 t; E' i the thrust levers remain where placed. 2 Y9 z6 ^. p z/ d- h( u% dT2 L, V- l: g0 l& v# J* ^ T / R% z7 Y) T$ G6 Rs$ s% W) u! k, l8 O0 l' @' ] 门槛,8 l4 m; p# j0 b( W 机身舱门开口的底部。" @, x# o( Z* o# s1 n% F 跑道头, % V9 t7 r7 \& Z7 `) Q油门保持,# w& x; k0 Y& r! |0 k+ K 自动油门的推力手柄不改变位置的方式。4 }$ d* ?1 \, p- r3 [5 Y$ ~1 q! M% P" j. r- }# I+ R$ H, M7 _英汉对照民用航空词典B OEING : ~* T/ z( [: p( f* G: e4 q* b: d7 vTECHNICAL DICTIONARY 155 2 w+ v1 z5 D1 ~2 v a* GTHRUST, The driving force produced by a jet engine. ' D3 V) H! x7 j) S" Z4 S1 tHRUST LIMIT, Maximum allowable thrust for a specific' l4 Y& t! z1 N0 b et of conditions.2 d9 w/ z! [/ n6 y8 z( I. Y" I) D HRUST MODE ANNUNCIATOR, A display unit or part 9 R, |1 i+ _ E- {0 ] k% X5 P( Af a display that shows the engine thrust mode." I. A8 e6 g! F5 ~7 M& C HRUST REVERSER, A mechanical device located in: Q: f2 P' n: z; O4 [. L z5 t; a: G9 Q e fan or exhaust section of the engine for eliminating 9 l9 g* x# E" ?: @$ Lrward thrust by deflecting fan air or exhaust gasses in3 ]9 n# P( H+ ]& l e forward direction can be used for stopping during 1 i9 t, ?! ]. L v( V2 planding and during an RTO.. J: V4 f6 |1 }+ M- _( a; x- R( } 推力, - G g3 p6 l) @1 G力极限,3 b k; Z. s* X m) I' b/ d 在一组特定的状况下,发动机的最大允许推力。; n* z1 ~; M$ z3 Y% M# d! Y 推力方式信号牌,! G+ H9 x5 E7 J$ C 显示发动机推力方式的显示器或显示器的一部份。 2 R! w% ^$ ~7 m3 \反推装置,8 w* t3 Z$ n2 h9 j" v# N3 P 位于发动机的风扇段或排气段的机械装置。该装置通过 ( c" {: ?( P. U* a0 J1 W5 t使风扇空气或排出之废气冲向前方,以消除发动机向前的" K& p, d+ w& A3 s' l D" D- ` 推力,并减短飞机在着陆或中断起飞时的制动距离。' ^" D! [, n% I/ n T4 J5 W/ V3 V. l* Y5 P$ C s - F7 }( ?- }: {: r% ST / r# a. S) m C1 Ho. I% i* y0 _9 @$ t W) h* n T: p3 ~' o! \9 z th6 y5 w3 `* s* M/ } fo. R2 b* Y, g! [. h0 y# u7 L th 7 W/ D; u% F; C1 _' i( a喷气发动机的驱动力。 . Y f4 n2 ?7 W- m$ H) G. V2 _( h' w6 f 英汉对照民用航空词典B OEING* @1 i, R7 b" ~* `8 X7 [. ? TECHNICAL DICTIONARY 1564 i K7 F1 @ [, }0 S THRUST REVERSER COWL, A cover around the thrust X# _# X: r3 sIME DELAY, An electrical circuit for starting/stopping1 T0 o* i5 j$ ~9 ^; d8 ^0 ]! b' Y e flow of electric current to an operating component K1 _8 x. Z7 d" G r a period of time/after a period of time.# ?; x: C* A7 ^3 C6 L) c. f# F0 h5 L- a) d IRE SPEED LIMIT WEIGHT, The maximum weight; ]6 n4 L/ ]/ x. g permitted at takeoff that results in a liftoff speed equal to' E8 Q @ d' C5 V& e8 J7 E3 F# b0 y e rated tire speed.9 q W1 k9 p4 s( d1 p" { OLERANCE, The part of a specific measurement that , k( f: i4 s6 v( ?" kallowed to vary in dimension. Usually given in a plus/ O- h) b5 A3 ~* a- z; X2 I) | ) or minus (-) format. $ S& l& z6 g+ r0 g# k6 O* _CLIMB, The point at which the airplane( F0 D" t) q8 {% @0 ?- V5 l reaches the cruise altitude.9 d6 M# [; X# z: H6 m9 C# t ts the cruise altitude and begins to* K. C4 f j- q descend.' U" `+ Q& f O2 c+ j7 d2 c for transmitting ' U- S: w! {9 _9 T/ w3 e' _' @twisting motion to the control surfaces. ' M; ^4 {+ x' U1 A) _! S0 }: ~ H7 f4 M4 F; f( B' J) _/ T6 c- g! p v2 V/ X9 Q0 k- s3 S 部件以进行维护。8 V7 H; ^* f+ v( ]1 W 延时电路,* ?1 e" k1 K+ T9 \6 I 用以起动/阻止电流在某一段时间内后进人工作部件 + v) r4 [( R4 F* l, H; P4 K2 ~/ |2 y的电路。 ( m. a( q' Z& R i2 N6 O( F- \轮胎速度限重, ' s9 @# O( G; u" {; g飞机起飞时,使离地速度和额定的轮胎速度相同的允许( E8 V8 {1 O' U' `0 Q$ m! b& {5 b 最大重量。 9 k" q. i. o7 y; E* ?) h, N0 A公差,, y( ]0 ~# h+ M) m- G& p 特定量度容许有偏差的部份。通常以(+)或(-) l, V+ u* @' Y7 n( D/ n的形式表示。" J( ?5 S9 ^' ?/ o 爬升顶点,0 e6 D. [! D8 g: u. @ 飞机达到巡航高度开始平飞的那一点。% y }+ O- R4 z3 u( l: g 下降起始点(TOP),% B' E& a" C9 @8 r0 V+ t& h: M 飞机飞离巡航高度而开始下降的那一点。 8 q5 @ B: @0 o+ D& x* k4 i操纵面的管状部件。 + f1 }. K" H, N+ M3 Sreverser of the engine that can be opened to access ( P2 t9 w+ e, R7 Ccomponents for maintenance. - Q- R7 u/ P4 w6 E; \7 X# H" \5 s* XT9 h |9 M- j9 z5 x th ' ]/ l' N9 B) d" L: ]fo # ^/ O+ N2 Z, j9 j/ ~- |, I9 TT 4 x( Z( m% Q) {7 ?th, a+ H5 N2 ]# E) L9 C% E T7 b, C) G0 [ Y7 x4 X) | is 7 y# e e$ H- Q% j(++ X. `+ ~" y& N9 p( y G TOP OF , ~/ N) E! l# e; }3 y8 E; cTOP OF DESCENT (TOP), The point at which the) \0 B5 `& G7 p% J9 O* P( d airplane depar * d; \) t$ }( f. t1 F6 ATORQUE TUBE, A tubular component - c& F* c1 b3 H5 T反推整流罩% D) ]* l" I3 Z" L1 E' t7 } 在发动机反推装置外围的罩子。取下后可以够到内部 - B7 M. w3 }4 j0 z扭力管, 9 |* q% s% u0 q+ T$ D8 i6 ~用以将扭转运动传给 O& {) @4 b8 n3 W' U3 M6 I 英汉对照民用航空词典B OEING; n) Z8 U o, y TECHNICAL DICTIONARY 157/ l" X$ }: Z" \$ b0 Y TORSION, Twisting of a material or part caused by& ]% E* w4 p6 }+ l& ~, O% @/ M# m external stress.- k' g6 y7 f8 Z( Z ORSION LINK, A hinged linkage connecting the inner 5 B: n$ H! Z4 t+ g2 q; knd outer cylinders of a shock strut. 8 f& p+ |$ ^4 B6 ]due to the ram+ K8 W/ I/ t5 s O ffect of high speed flight. 6 ^' ]- i4 l7 H9 u' JURE, Pressure higher than ambient 1 C0 s# u* J+ u) _9 t' Hressure due to air flow, measured in pounds per! L( h3 b& `* \" T# O% M3 m$ m4 | quare inch (psi). ' S( n: u! L$ Ber than: s* {: ]( d1 U, b% W! H7 H+ t: ^ mbient temperature due to the compression of air flow,, L8 i; p' H( J! H- l easured in degrees Celsius (C), or degrees. N9 [ }( K3 s2 w6 L ahrenheit (F).+ J) d7 a- i8 R TOUCHDOWN, The point at which an aircraft first; w: H; B% ^3 S makes contact with the runway. ) B0 [/ J6 {% ?( D生的扭转。 X; o& C: g! Y& j( U 扭力臂, " r* f; Z7 f, ~1 _减震支柱的内筒与外筒之间,用以防止活塞旋转的铰链 * A$ [9 Z# l P0 i连杆。. V( C/ }2 u. G% x7 j+ P8 t 的冲击效应 4 t6 P; A/ H" U. ?( B7 b* J4 t引起的温度的升高的总和。* H) @. P8 a" v0 E- J 总压,, O- ^7 x/ {! q3 z# o3 a 由于空气流动而高于环境压力的压力。常用磅/平方英 " R9 e) `9 n- u; J8 p# [, d(psi)来度量。 " S0 m) X7 L% G1 [0 Q全温, 0 A/ }# p; m; P, f3 t由于气流的压缩而高于环境温度的空气温度。用摄氏 ' }3 d7 n4 x+ m! q! x* Z% ?(°C)或华氏(°F)来量度。5 P# V/ Y3 D) U) R7 I6 j9 [. b- O% H8 w 接地," Y+ o5 u1 R4 k! y. }5 y 飞机降落时,飞机最先接触跑道的一刻。 w5 d! E2 e9 |* l: i& Y$ zT $ d, k# R9 s- F* z( La$ R0 f/ e# y3 T TOTAL AIR TEMPERATURE, Ambient or static air5 x" y! s v& [0 R4 u4 S% G, V( S temperature plus the rise of temperature / w# B2 ]+ V+ E' N; \/ Q, y+ G: X5 Te " d1 I5 i1 ~! ^- i% j& I( @TOTAL PRESS0 I. U, p1 R3 c9 F* R% s: N2 S& r7 @ p " b8 n* J, I+ f4 l! A: Q) Us - c, y& W# w$ sTOTAL TEMPERATURE, Temperature high 5 }5 G* V3 ~9 S3 Wa+ q$ Z1 S# G. ~9 c9 @ m2 u/ z- T* X7 I3 p3 G F 8 U# K& K9 V1 S* n- Y扭曲,$ A; l+ Y, w2 T+ \* T' f 物体受外应力的作用所产) z8 \7 K3 u0 ]" o 空气全温,' A! P: X! v. s 环境温度或静空气的温度,和由于高速飞行# j0 `& `3 u, p" a$ i3 @! G8 E7 r; C/ [, i2 n+ K0 P8 ~9 r4 b+ D, H 英汉对照民用航空词典B OEING # p9 ~& u2 @' DTECHNICAL DICTIONARY 158 / n: l/ z& o5 s. D! Z$ ]TOUCHDOWN ZONE ELEVATION (TDZE), The B& y+ h4 _+ s: t: _ highest elevation in the first 3,000 feet of the landing * r8 Q" v% o( S6 ~/ Lurface. 9 a. `6 o6 P8 r2 w. W6 Xrt of nose or main landing gear for 7 z6 s- F W) n3 o$ {ttaching a tow bar to move the airplane on the ground. 0 [2 b7 f* H" p; q y" H9 G7 ralong.4 E+ u' z6 V3 Z j6 @4 h" f RACK (NO. 2), A navigation term that describes the& b& |. h8 }4 Y6 m- T TRAFFIC ALERT AND COLLISION AVOIDANCE$ \+ [! y, V% Q) _/ ` SYSTEM, A system designed to alert the flight crew to2 N, _0 G8 U1 @% f potential conflicts with other transponder equipped 2 x" n, p$ j- c+ U @8 Gairplanes flying in the same area.& O1 c7 g* g) k7 j! H; u1 X TRAILING EDGE, The rear edge of a wing, stabilizer or 2 o* R. _; B+ ?' Ucontrol surface.3 S: ?4 L/ ]3 ? TRANSDUCER, An electrical device that either takes ! L, Z9 S5 w. L/ velectrical energy and changes it into mechanical 5 b" t: F8 Q3 T" cmovement, or mechanical movement and changes it& F0 \% v$ J% W" [5 S into electrical energy.7 f T7 ` A3 o4 r TRANSFER GEARBOX, SEE - ANGLE GEARBOX % A) m+ n6 p7 p1 h# ]+ e3 S$ U高(TDZE),: K# ?9 O' i0 Z6 W$ t$ i 高标高。 # p, j0 |8 Q+ N% E4 {0 f前起落架或主起落架上,用以接上牵引杆以便在地面上 9 S5 K* l. `! |6 S1 z) q' A动飞机的部份。 # }" N/ i K0 E# \, [* y+ N轨条, n+ { z+ p ?& j) X" @ 迹, 0 D1 a1 ]# t7 @4 |# `形容飞机航迹在地面的投影。- [+ p/ n6 ]: J3 s; Z% \ 空中交通警告与防撞系统,; f- g2 M- G7 A5 p 用来警告机组人员可能与其他装有应答机且在同一区 7 H+ b, g. ]4 A( k6 _7 ]域飞行的飞机有冲突的警报系统。 2 b5 P; A7 H. t- p2 m后缘," B, b( T9 Z0 l5 H 机翼、安定面、或操纵面的后边缘。, U5 y, A+ l7 w+ N 换能器, ' g, z' s. A( f, q0 Q, W能将电能转换为机械运动,或将机械运动转换为电能的5 I! {2 t+ Z$ C: ^ 电气部件。 3 Z' Z3 V* R! m; l转换齿轮箱, - ^" C; _' @8 i见Angle Gearbox . [8 T0 u' Q" `+ W# \6 Zs l8 d0 ?7 H. c$ Y7 I1 I7 L2 ` TOWING LUG, Pa0 z- J# P L# i* L, q a% ~7 S/ K! F9 C1 ~/ g TRACK (NO. 1), A structural member for attaching fixed u" Y5 a* H5 d" G% e2 y9 lcomponents to, or guiding movable components! U8 V- A, X1 Y. Z; F" F$ E T' S7 }/ z4 r( a1 c+ A: M b projection on the earth's surface of the path of an & Y) O7 G9 {8 }7 e" Pairplane. ! J7 [# t9 o; q7 M/ O接地区标+ C+ U0 F. T1 k6 i2 }' b 跑道头端3,000英尺的最 % f5 N& v) p* ?5 l7 Z% Y; ?牵引环, 3 ]! v5 P& T7 H# L1 W* [! h5 [7 q; q8 Y' e. g' S 用以接连固定部件,或引导可动部件的构件。 ' @5 }, e9 m5 m/ O) Q( F' y/ o' e0 D" g: X 导航术语。 9 [$ A7 b. c+ U5 p3 _9 P! ~4 v7 j. b 英汉对照民用航空词典B OEING ~2 J6 U' s. s% t TECHNICAL DICTIONARY 159* z0 U8 z0 R" ^/ W! s- ~ RANSFORMER, An electrical device which uses ( t. f2 X) y- W! aRANSFORMER RECTIFIER UNIT, An electronic ; m0 _" {. T, ~evice for changing alternating current to direct current( K: X- w. X2 n supply airplane electrical systems. d. [& f& w4 m# ?5 q) u$ g lse signals or triggering pulses/ O) ^ G0 `' E, | nd cause component breakdowns or failures.; ^* T s, n; o) b) w It consists of a base, collector ' |6 b: n2 e: k; u. p# V- fnd emitter. Two types of transistors are PNP and NPN. ; u a, w' b' J* N* i2 s$ b( Z% ~* i9 G( R变压器, & M2 A3 I9 k# O. c1 v; v磁感应,将电能从一个电路转换到另一个电7 }, S2 C" [1 M' f9 g 变压整流器, & l6 a% n# q0 H6 j1 ^ F用来将交流电变为直流电供给飞机电气系统的电子装1 ~9 d( _5 r7 _1 s; T$ v, A, z 置。 1 Z i- \" E9 F% [ A7 w瞬变,/ }/ P% p4 N4 l* W9 t u 信号或输电线上的瞬间电涌。这种电涌常会产生一些错$ q# w3 m) I: X; ~8 H 误信号或触发脉冲,造成部件故障或损坏。+ G7 X& J$ ] q4 o 晶体管, + r: S3 P6 }: ]固态电子部件。通常具有三极:基极、集 p1 ?- j0 [( c2 V. e/ A! d极、和发射极。有以下两种:- q# Y m* N g3 `8 }, [ PNP(正负正)基极电位低于发射极。 % P* X) D+ |, xNPN(负正负)基极电位高于集电极。 " O$ I$ O9 O/ h: vTRANSFER MECHANISM, A component for $ b9 H) ~' K+ j: m" Stransferring motion from one place to another. # l: {& H! L( h! M( g! K8 ST2 u5 K9 x6 A. T. Y- O. i1 l C8 \' J electromagnetic induction to transfer electrical energy9 b$ w* Q$ `8 e% S! c from one circuit to another circuit." |8 |& E# @/ J6 J7 }8 l5 K; W T/ Y0 ], s+ }5 ?. `" C8 l5 U d ) t% a6 Q% C3 @& A t6 L; |to: t" d* |1 u5 }) F/ |& ]( h TRANSIENT, A momentary surge on a signal or power $ G" l# _- B* u6 Dline. It may produce fa 7 x2 S2 m6 f) h' v& |- c+ |5 Ua & b! S% ^& k. p( r# w% X! `TRANSISTOR, A solid state electronic component for0 u" y: x& X5 A, r4 [; T use in electrical circuits.: h: Q. P2 w# \ E/ I a% x5 a% U7 b* i! I7 v6 l, j: U$ Z* s 转换机构,8 x: L" I+ J/ q! |) g 将运动由一处转至另一处的部件7 Y1 G. I. h4 h9 I 一种利用电 ( B+ M( Z7 w; ~2 R( h路的电器装置。 ( p. P5 Y p8 s& G5 W' V0 c电路内使用的2 \4 \7 Q8 _, z/ G+ e8 o ^" n4 C) D+ E1 B, v英汉对照民用航空词典B OEING h2 p: J7 t6 ]" I5 oTECHNICAL DICTIONARY 160 ! s8 @. i/ J& {6 ?' ^5 [TRANSITION, To change from one phase of flight to4 s3 ]+ m# `" y. z! Q; P TRANSITION ALTITUDE, The altitude at which the4 b7 s* J) X5 F6 W( f& p ltimeter setting is changed.# n6 H7 ~$ ~( m: m* @ RANSLATING COWL, The movable outer portion of% n. R7 D$ s6 S! w. `4 ` e thrust reverser cowl which is operated during3 O2 I) z: W0 o' |( c verse thrust. 5 l3 s- n+ s4 s3 ]. h5 U: @RANSMITTER, An electrical component for sending- m) y6 D) O2 B4 S E formation from one location to another. : h0 E( v/ P8 u& c1 iTRANSPONDER, A radio transmitter-receiver which& k9 }) l: i. W, L6 l ansmits identifiable signals automatically when the + k3 L0 E: ?8 p( b `& P, ZTRIM, The adjustment of engine and airplane controls1 i$ [, L# k0 c1 P$ p 从一个飞行阶段转成另一个飞行阶段。 ! m1 l) ~6 l/ ]$ V5 h5 H5 |过渡高度, ; G+ O9 n7 h! | p改变高度表设定时的飞机高度。 e8 S5 v2 n1 Q* Y V9 S 平移整流罩,, X$ X2 [, r+ `$ S. l* u 反推过程中使用的反推整流罩外面的可动部份。 ( ^) L$ S# [$ R3 k* a4 e8 ^发射机,) T# ?' n( z! x' P4 V, Z 将信息从一处发至另一处的电气部件。# r# G5 ]( Z) U2 D# r 应答机,, a% z$ n$ s; v; k- D- W( P( Y8 X 在收到合适询问后,能自动发射可识别信号的无线电收; z' S& p+ c7 v7 o8 t8 ~9 F% O 发机。. J) B& J2 H3 B 平,0 X4 t3 K+ o" \# B3 H( i" Y u7 ~ 动机和飞机在平衡的状况下工作而做的发动机 ; e. ^6 |3 K6 E6 Z5 |another.7 ?9 i: d$ a9 R) u( ?$ J0 e7 [3 ] a/ t: I' z) S3 Z0 ^% p- x* } T 3 P! E4 O5 c3 ]& X7 fth% {5 a2 t ?# T7 \ re/ H' ^( i/ l1 b. i, k T1 R+ V/ T" s* o8 b5 M6 c4 J- {7 ? in ! b, F( t$ Y+ g* T# ^& M6 Ptr 9 }$ b' m! S1 d3 d2 [* tproper interrogation is received.3 G# H/ t2 X6 w1 f1 G% h0 K- [2 H# l! \ for a balanced condition of operation.- N( u. w7 `7 V! O1 `) y B; ~# Y 过渡, $ _+ H, q$ a" i" n) ]/ G( q2 W( s9 ] 为使发 7 _2 C( F- `& V) n# G2 I- a$ i和飞机操纵系统的调整。 ( S3 H6 N7 d" q6 h0 g2 e1 e英汉对照民用航空词典B OEING$ }0 y4 v* [% }$ | `* _ TECHNICAL DICTIONARY 161 6 q' g! r$ N- Y7 d3 oTRIM TAB, A small hinged movable part on the trailing, [; u, u' A5 k. f/ C edge of a control surface (aileron, rudder) (see TAB). % S& q# L# h' kL, The total fuel consumed from brake release 7 E9 I6 s( {9 bthrough climb, cruise, and descent, to landing at $ N9 S/ @4 M% p& k$ ?7 X: p& J$ `7 Cdestination.2 F: N1 R! e5 ] RUE AIRSPEED(TAS), The actual speed of the ' Z( U( a* Z; O: [aircraft in relation to the moving air. The true airspeed is ; `" |3 o' i6 H& a) T S6 Yated airspeed corrected for position; u) k$ {6 r3 S3 Q5 y rror, compressibility, and temperature effects. 0 o! B! |! n2 g/ J6 U# V2 Z4 Gribes 7 Y6 ]% |4 B) K' |& V: R wthe output value for each input. V5 ~8 X7 c# f) \0 G$ O ombination. " h" T8 A1 X O% z$ e铰连在副翼和方向舵等操纵面后缘的可动部份。6 t x& G) j# C: ~ 航班燃油, ( l/ X+ D4 g% Q1 @: o. m7 v- V8 `+ c一个航班由松刹车开始,经过爬升、巡航和下降,到) r1 Z* t p9 a7 E- { 目的地着陆为止,所耗的全部燃油。 ( u: |7 T' `9 Q" _3 t* a变压整流装置,3 v; Z& \" E; m1 {/ }% q 见Transformer Rectifier Unit$ i, |1 i3 {; w: Z" z7 ^$ U s! j! @ TRIP FUE 9 e) M, { R1 D( m- ]TRU, SEE -TRANSFORMER RECTIFIER UNIT ' Z9 Y+ G- ]- f1 Q' t: {* M+ c& ~$ fT # C3 Q! W& h$ g+ r8 c. Lequal to the indic e: W% k1 V, e0 o$ C9 G e/ E" k/ E' E8 V d TRUTH TABLE, in digital logic, a table which desc f4 r' z- O) d( la logic function by listing all possible combinations of J: p1 ]1 c3 X& W8 Y/ U! jinput values and shows ) U5 T5 O& l) N! u( V5 u7 `c/ ]* |/ }- V6 V/ C 配平调整片, 7 h8 P/ z) A: a& V: O* S+ d( n% i4 E O8 F' `* w- P( G3 F1 K0 C+ }2 V6 Z b1 W 真空速(TAS); ( G1 @1 j/ g. B! L; O0 ]. e对于流动中的大气的实际速度。由指示空速经过 4 M8 W; V% k; f# z真值表,( V( V- y0 B8 v 数学逻辑中用来表达逻辑函数的表。该表列出了所有可) A. x8 r ~7 F 能的输人组合,和每个输人组合所产生的输出值。 - E5 |! N4 q7 @4 H- {飞机相 * b& S" d: I4 i位置、压力和温度校正而得。! \% o; O9 r1 g; }9 N( L" d 英汉对照民用航空词典B OEING - e/ ~/ b2 G9 | WTECHNICAL DICTIONARY 162 7 [- X. z9 B z. H% p" z, ETURBINE, A rotating part of an engine which/ G% X- G% U: i1 E( `/ } N kinetic energy from the combustion chamber ga: I$ o: P! L: w; d+ i. w extracts 9 S* o ^/ ~# p- sses. " y- \% T N0 {: U/ ihis energy is converted to turbine rotation which ' ^2 ? d6 i" htates the compressors and fan through a coaxial 4 ]6 N) c9 z3 P9 W% G8 z) ?. Vhaft. 3 j% I& p9 u4 X0 K$ ~6 h8 J; R9 y, QTURBINE CASE COOLING, A method of cooling the & H2 y% ~+ h) y6 mngine by using fan air. This cooling process is used to z3 G g' A b. N6 m4 B TURBOFAN, ' v* j# W* W Q' N ]9 Z" C(1). A jet engine in which the first set of blades is a+ e) y& [4 V& h6 U2 K# F1 w4 h2 a( _ large fan., j. S5 s8 n" q$ ~3 N (2). An air driven fan/compressor used in air j6 N: G4 m& j: ]$ Vconditioning system. % ]0 u/ z7 n3 V' jTURBULENCE, The movement or shaking of an 8 v0 c2 P0 W! S. \2 E3 |& fairplane caused by unstable air masses." I7 D, D V" U4 I4 Y. w9 s 涡轮, 9 G! N6 W0 b7 K* o2 y: F4 j/ i发动机内,从燃烧过的高温高压气体中撷取动能的转动 : p- ?/ s8 ]" m; X份。该动能使涡轮转动,涡轮则经由同心轴带动压气机 , R3 Q8 n. z) p8 z w7 V k风扇。/ m' {1 C: @8 V5 ` 涡轮机匣冷却, 3 x, N9 T- o) X0 `% s用风扇空气冷却发动机的一种方法。该冷却过程被用于% P3 H l3 S- [" {+ F' B 效率。 . v" f$ W! Z" r; K* G: f0 s(1).第一组叶片构成一个大风扇的喷气发动机。 7 S8 }6 O- T1 s(2).空调系统内的由空气驱动的涡轮和压气机组合。 ' i6 @: R% u# v: c6 \' F8 {颠簸,! k- k6 _5 l0 c+ T! Q% j 由不稳定的空气团造成的飞机运动或抖动。1 y0 I8 ~, p" h0 i T$ i8 K, l2 ~* \3 g+ A+ ] ro - v% v3 X$ Z% y8 |s . f4 ~6 {/ [' y- t& g8 He & m- ^! X/ K( \3 O* fincrease engine efficiency. " j% t: u5 H, z7 o8 C/ W; L: X! K$ a+ u- U- W. a" D0 I( J( O6 n$ Y7 ~+ e9 U. {# p提高发动机( h. e6 Y4 f- b! t 涡轮风扇,% g! O( y' J6 b# | 英汉对照民用航空词典B OEING 8 z; \8 z5 g! X: Q( ETECHNICAL DICTIONARY 163( p# C/ W0 e" P9 ` TURBULENT AIR PENETRATION SPEED, A speed' e. p2 `- |2 X/ C; D' `0 Q that provides adequate maneuver margins when flying0 \) L/ V8 d5 @, P: V( c; } to unstable air masses. 6 V I. p+ K) w1 t: f# N, [: b4 C! jht 7 u: Y: w2 s- c+ l- u' r' h5 xstment in the control8 L& ~3 q+ v" w$ s) q# z ables./ \( w5 V/ Y: r' u, w UHF, SEE - ULTRA HIGH FREQUENCY # t, o* J7 J& r0 L4 FNDERCARRIAGE, SEE - LANDING GEAR \( n0 E( C2 E( ^ f UNIT, One of the type, a single component. 4 L) X$ z( i: [: E/ D* \UPLOCK, A mechanism on the landing gear for keeping ' P$ p8 K" D' V' H. }+ l. Zthe landing gear in the retracted position in the wheel 1 `+ C: }* d8 A8 a. F8 Bwell.: m V0 O6 q- V7 w* H 速度, + x6 S* j: x* P4 V: L, ?纵裕度的速6 _( }) m: y: [7 `. H7 w# f% T2 d+ @, ^5 a 调整操纵钢索张力的% c2 \2 y( b# c6 ~9 t) h3 H2 o 械装置。 5 Q3 ^, w0 T r# Q% C$ x) ]高频,1 h' e5 \1 D2 p5 [ 见Ultra High Frequency 1 g" [- x8 y& G/ U0 [" Iin + |; y: i# }% t( N& \% F$ fTURNBUCKLE, A mechanical device with left and rig $ |6 F- m a, C7 G6 qhand threads for tension adju + R3 z9 O# F; |* G1 L! @c, ^1 p- q, y5 S U, h6 x' w# W ]- n# u, r R$ n$ v ULTRA HIGH FREQUENCY, The frequency band ! O; g) l0 X$ p2 R/ y9 U* \between 300 and 3000 MHz.# f' [: V% r/ w6 s7 ], X U % J B; x- s# F) I* r颠簸穿过; c, Z. F7 p' \% s, G 飞机飞进不稳定的空气团时,提供适当操) J2 ~# ~" K" a8 s; W: n7 w! n6 U8 u0 J0 m 松紧螺套, + _, C) C t9 Q2 D& X k7 Y8 T具有左旋螺纹和右旋螺纹,用以 7 X! [/ b9 M9 i( t3 V) w$ c7 ]& h- ?1 G. ?/ i( ?3 L" `3 W) V* h* g# V1 m* F 超高频,% l6 }% Z3 b/ W4 s 频率带在300 MHZ至3000 MHZ之间。6 i& z$ B: Y0 q: m* J; V2 K8 ~ 起落架,* e* B( }7 H, c' k/ V) T 见Landing Gear: P6 ?8 `- `' f5 C 单元,/ Z5 x6 o$ E/ T# T 某一类型或某一部件。 7 R+ v1 D: m+ s G% c) p上位锁,5 L2 z# x% V; L4 Q) O6 J/ } 起落架上,用以将起落架保持在轮舱内收上位置的机 , P2 r1 n/ Q5 {5 C构。( A2 F( v, a% |4 I 英汉对照民用航空词典B OEING4 g9 w* j( q, {" _5 B, w8 H( ?+ O TECHNICAL DICTIONARY 164 / d8 f4 c% r: gUPSET HEAD, The head produced on the tail of a rivet ( r0 L6 ~- y2 g: vduring the installation driving process. (See& t `3 ^, G0 I Manufactured Head.)- N9 N; Y1 B' Q: L l) ^ 1 (TAKEOFF DECISION SPEED), Is the maximum 0 j; J# O9 t/ `: ypeed at which the rejected takeoff maneuver can be |/ d) W! T7 C' I% U itiated and the airplane stopped within the remaining 3 q* x* s' _+ {eld length under the conditions and procedures defined 2 @4 p& V8 _/ l( r& l# P% Tthe FAR's. It is the latest point in the takeoff roll where ; S% |4 i7 S; T Q5 Q1 Rstop can be initiated. 0 m! S# g7 G( H" ^ yssure+ v i' \8 F/ E7 r) B dient capability and maneuver margin. 0 M- N7 A+ E% U. gVACUUM, A negative pressure or pressure below 0 F7 f+ v" p" G3 [! n2 eatmospheric, measured in inches or millimeters of ' }% p% _! s0 s1 [0 H) Z' i* J; q6 n/ w7 Bercury.% z$ V9 _ W' d) F$ w+ D8 t is' d# H. y7 T, M3 Q9 p VENT, A small hole orifice or restrictor in a component$ O* {- T3 C, F/ b# y2 m for allowing pressure in the component to be the same 9 Z( G: G8 H% m6 C- C: V/ x( zas ambient pressure. w% z) u% ?6 p) h5 g+ o6 } D 在铆钉铆接过程中,铆钉尾部一端形成的凸头(见 , Y( z, A+ L% P- ZManufactured Head3 S Z5 [- Z2 }9 o$ d u2 j2 K V ( _/ F7 O6 C8 j3 W& G* hV , H( D, K; P5 r# G' q1 ^s3 ?. o4 ~& ^+ a: @ in2 U7 o P3 I$ V+ }5 `, n fi# b1 h# Z! L1 Q' J in- o+ z( [8 o+ B; v a & z% _9 T; g& Z% T8 r7 g! wV2 (TAKEOFF SAFETY SPEED), The speed flown after& K5 J% R9 l( G$ w takeoff during engine-out climbout maneuvers to a! ?. @) L- ]/ r8 w8 Y+ G4 x adequate gra & O- {; T; `$ Z2 E9 z" Nm ( D9 M* j: j( ]6 _3 r' f- vVAPORIZE, The mechanical process in which a liquid& i4 b, D/ L2 R4 {, [8 Y! E changed into a vapor. ' Q2 z; K) y& z" t! RVECTOR, A heading issued to an aircraft to provide- w- O. d* {1 \4 F9 ~' N navigational guidance by radar. * x4 A% O5 q) w" c9 E- u铆钉镦头,/ }8 S! Y3 l3 f, P8 [' @ )。1 F$ p9 R% m1 e 1(起飞决断速度), 9 C H+ {6 t& {. @2 C3 n: S, [) P根据联邦适航条例的规则和程序,飞机能进行中断起飞! d7 r H' v; y- P0 o 在剩余场长内停止的最大速度。它是在起飞滑跑时仍可" b7 |4 q/ e& X, v 住飞机的最后决策点。 ( s1 `; A' D9 ]+ I/ g速度), 2 @2 p% c! t" p! E在一发不工作起飞后的爬升中为保证足够的梯度能力. `7 y) J1 E" a7 ?7 C. f8 N 和操纵裕度所飞的速度。 t1 [5 x) Q* H! l/ Q& r 若干寸(或若干毫米)5 E9 Z, |- X$ z+ p) I 汞柱。 6 I. D6 q" \) j6 F* }8 N: O. z) \) [蒸发,2 O. S. O; O4 x( v9 A6 F: v 液体汽化的物理变化过程。1 r, c) M2 }% ?6 R5 C 引导,2 z- X1 c9 m2 k) T% ` 由雷达提供的航向,以给予飞机导航引导。7 [7 {5 l- T% W% Y: D+ P 通气装置,% E& o/ ?+ |+ {: z 部件内,用以使部件内的压力与周围环境压力相同的小 3 n; [ C! B4 P' _0 A% @" D孔、或限流器。 + B: p* ]# M5 h+ e3 XV. |/ {$ Z% V7 G0 C Y; u0 N7 P7 ^* I7 |- E w: c. a K( S' ~. w& v1 H' S V2(起飞安全. W" K1 ]1 H# `$ |& O) B8 M! F2 ` 真空,5 `9 h: l" k2 p# {$ e 负压或比大气压力低的压力。常用 1 a! H T. v& E5 M% C英汉对照民用航空词典B OEING; @8 M& U N2 ]' }0 o4 c TECHNICAL DICTIONARY 165 + C5 y# \& F' C* V) _3 uVENT SCOOP, An air inlet/outlet on the bottom skin of ) i- H; |; w! c* a4 p( {ir 1 u# O* w& \8 n3 Z$ @VENTURI, A part of pneumatic duct with reduced flow ! d7 o f+ C7 i$ f9 ^2 ^# `$ \rea for airflow measurement. (Principle: As air velocity ' L, m! K# W' ?9 X. h0 U0 [creases, pressure decreases).$ M& N# A# P! O! g& N. h ERTICAL AXIS, A vertical axis passing through the8 G( {8 x$ X1 B+ r airplane from top to bottom. Airplane left and right7 D v5 o4 \% s! V! s" Z' r2 o' _ trolled by the rudder. 5 L6 s3 u8 i+ `+ m, F" bVERTICAL NAVIGATION, Functions which provide u; l9 K% H) |0 Wguidance signals to control the aircraft during climb or& |9 ]7 B8 b( L4 B, A% w$ Z9 _ descent. : F i% u3 F4 i. % N0 O# U$ f$ p0 K/ D! ?通气进气口,7 P; T d) D: M 位于机翼下表面蒙皮上,用以燃油箱通气和提供燃油箱 - J" I' d" f p- ]: X0 ~内正气压的空气进出口。 T* H( j2 f" v( J; P, ^文氏管, : t( `% b0 t$ k& a! O5 d5 }气源导管上,导管截面变小以量取空气流量的那一部 2 @+ a1 t4 b2 u份。(原理,导管截面变小时,流速增高,压力降低。)* v; _* N9 o- n- z! m& X! b 垂直轴, " {3 y( ~1 F# i# D, d由飞机上部至底部的垂直轴。用以操纵方向舵,使飞" `, r" M; C& e7 F3 d* z 右运动。8 [# J1 b( r* l3 h2 O# F 直导航,- v3 e8 I4 S6 I8 [/ H3 f: P3 T+ E5 Q ]7 U* U1 C4 R- m) n the wing for fuel tank venting and supplying positive a * y4 ~) g. H* }0 l+ y0 w fpressure inside the fuel tank.# @8 d2 D C4 l) X5 p. N a+ f; O- l# n8 _8 g) P in9 r4 r$ J7 m+ q& Y$ O V$ ^8 p7 R( N$ ~6 p movement con 4 u w6 v+ h2 J2 L/ _" q+ sVERTICAL SPEED, The rate of change of altitude; a+ E- k# W% O2 U. p 机沿此轴作左 6 u+ k4 ^3 G0 L7 \' S5 X# `5 p& N) O" y2 |9 _ 在爬升或下降期间提供引导信号以控制飞机的功能。 * h7 l8 ^# F% X0 R垂直速度& z$ g% }8 H' Q9 t 飞行高度改变的速率。 / k% B! V" h, q& x* r, o英汉对照民用航空词典B # s. S0 S; r1 ?8 `" C9 k! \- u* FVERY H" o2 p* G% k3 X OEING : a5 a9 H( N( t7 m6 E: sTECHNICAL DICTIONARY 166 # q5 | H @" s" @VERTICAL STABILIZER, A vertical surface of the+ _: u/ n; }+ N/ ^3 M7 j* o- p" ? empennage for stability/control about the vertical axis. 9 [8 M, r7 D6 N! zVERTICAL TRACK, A climb or descent profile.1 @9 I# w' G) Y% E8 p/ x: A3 ^. L9 N IGH FREQUENCY, The frequency band6 _6 Q5 }4 D5 p% k, B( v; c) R VHF OMNI-DIRECTIONAL RANGE, A navigational b% c3 I/ T: @& q+ z X8 v system which tells the airplane's bearing from a VOR ! W! T7 W) X, }2 l/ V7 B2 dround station and its deviation from a selected course$ l# W, [4 {0 s, S5 c; D) _ /from the station." [9 A, W9 c* Q1 z$ J ISCOSITY, In a liquid - it is the resistance to flow.2 L' Z% }& G ~: x; k9 j VMO, The maximum design airspeed at which the [0 | v1 R- l# E3 Hairplane may be operated. T) h. ~; H3 c7 p3 ^. {4 ]3 X3 N 在飞机尾部,用以保持飞机绕垂直轴的稳定性和控制! E( I1 c5 O: S* M6 g4 E# @8 w 的垂直面。; n* G4 X7 D: } Y) Y f 垂直航迹(VTK),1 B+ |9 k6 {+ V/ i- } 爬升或下降剖面。$ m3 T, u5 Z- v; P2 O" {/ z 甚高频, 1 S$ ^; D/ ^& \# T30 MHZ至300 MHZ之间。between 30 and 300 MHz./ z: ], Y1 { @* W VHF, SEE - VERY HIGH FREQUENCY% e: c! ?1 [! ~1 B g5 q% ^) [! n* Z2 J* ]9 \; i" _ to ; O2 x! l x7 P5 i. ~$ pV- Y& q. h2 f/ `; M; D 垂直安定面, ! W% F/ B) \3 p* v M' a* D频率带在+ J& v9 {' i* I0 E1 z8 X 甚高频, / ?4 K% p5 a/ n M; `% f见Very High Frequency. _4 }& ~1 }7 u 甚高频全向信标,! r ~8 }+ Q' [3 U- v8 _( ~3 x& W 系统。该系统可提供飞机到VOR地面台的方 * Z. P# V( Z/ C; D$ |位以及飞机的向/背台飞行的航道偏离。 / o8 ?) n* U. ^6 Z3 i/ R2 o& u粘性,1 Q& z- f! a( i) K+ u7 [ 液体中阻碍液体流动的阻力。% ^# j, O$ `$ B 最大使用空速, 3 S+ M; `' b, I: B1 I飞机可使用的最大设计速度。5 _+ i- }( o4 U0 @ 一种导航6 T) p5 z7 r0 B 英汉对照民用航空词典B OEING" w+ i7 i; _, E# o4 k2 y% u4 O TECHNICAL DICTIONARY 167( b; b# c( A& D- ]5 v2 p VNAV, SEE - VERTICAL NAVIGATION' s0 _" O2 @) T VOLATILE, The ability to vaporize readily.3 K8 o( P& J9 f/ L) h LE MEMORY, In computers, a memory whose , t6 c' X# K- @' Y7 ~* `9 MOR, SEE - VHF OMNI-DIRECTIONAL RANGE . i1 f) F6 X6 [1 `( sVORTAC, A combined VOR and TACAN station.2 b5 f- e: W3 T$ r% b ORTEX CONTROL DEVICE, A small airfoil on the, c& G0 s( U6 L; L5 y, ^ acelle for improving airflow between nacelle and wing . f) T2 P) {5 e1 p" `" P$ A0 aleading edge. , \4 A( E: l( ]6 UVOLATI: c5 m: I7 v) Z8 V0 I* A( s2 L contents are lost when power is removed.* o/ f& L R+ @! N( Z9 z VOLT, The unit of measurement of electromotive force.. r- U$ y* y A! t5 x% R V ( Y* {. [9 s; f/ C5 U+ w+ ]V4 {6 A9 P% [. t/ o+ x n ; Z5 R q- P6 x$ `/ u垂直导航, ! f+ S$ W. r9 z+ b1 t3 c- e2 y. C- w见Vertical Navigation. k, r o, U8 J! B" L2 P 易挥发的,, `- _ M( b) h0 }) }! E1 { 随时可以蒸发的能力。 , z3 S3 B: ^4 c/ Y" {! S. w易失存储器, ( y6 D% j' i& c' I在计算机中,失去电源时存储内容便丢失的存储装置。. l2 F$ \7 ^. b 伏特,) Z5 Q8 p: J5 [/ c9 L* Q( Q 电压的一种计量单位。 , l) H' o2 N" G! l+ [ \4 ^甚高频全向信标, # ?: B7 S' e- q8 xtional Range5 J% v# K5 v" J6 ~7 C( P' N 见VHF Omni-Direc . ' Q g2 h, a. GVORTAC, 4 q e* [ g- w8 k9 r" |6 q) s兼具VOR(甚高频全向信标)和TACAN(战术空中导- X5 @3 I7 y; ?! x- S 航系统,或称“培康”)两种导航设备的导航台。 4 \5 R7 ^6 I! s涡流控制器, 0 x! [2 v, Y u J! E9 P发动机短舱上,用以改善短舱和机翼前缘之间的气流的 . y% N/ H4 a. [小翼片。 / j/ r0 Q- z7 ]英汉对照民用航空词典B OEING - A5 Y P0 C7 ?5 n3 a- CTECHNICAL DICTIONARY 168 2 t3 A# ]6 D; x2 X% y7 z# L: DVORTEX GENERATOR, Small metal airfoils, located on& ?6 d( f" M& U M+ h$ Z5 U wings and fuselage for delaying separation of the air/ ]. y4 I1 E$ o+ ^; g9 @ ating local turbulence# U* G* x" m. f ortex).4 m4 D- |, W2 l- N 357 U5 q6 X- I$ C# m( h0 U2 r+ m stall speed in the landing configuration. 5 ]1 u2 v9 \- D5 t$ y装在机翼和机身表面,以在气流中产生局部紊流(涡 / _; x' q8 [3 B. U ~( ^流),来推迟气流自表面分离的小金属片。 1 L' A3 {2 `( \4 f8 t度),# ^ C" Q; @) { Z+ o2 c' C 在着陆形态时的失速速度的1.3倍。- s, H5 Z' n* E, t7 f# ? 见Vertical Track : f S: F0 ?5 D: A- q2 v: G$ vflowing over the surface by cre. I: _! V5 z- R8 G' y% q/ W (v( E# v$ S1 ~7 w6 G7 h! k5 o- ~ VR (ROTATION SPEED), The speed at which aircraft ) K) z6 L3 W5 A6 Z: ?rotation begins in order to achieve a speed of V2 at 6 |. D# q/ f2 l4 T e" q& B3 @: \3 Ifeet above the runway. : p# z3 x2 d4 R" {1 CVREF The reference speed at the 50 foot height in a- G" q5 B' J/ K, I+ ? normal landing. This speed is generally equal to 1.3 7 v% e; J" |0 _) _5 ntimes the / @/ i! G/ y% _0 @: A; P, jVTK, SEE - VERTICAL TRACK- f5 L0 j2 Z7 b$ m* J' k 涡流产生器, " }% i" A" J% J& D' i7 ZVR(抬轮速 . \: b6 I2 e* u- a7 X2 a7 d" ?+ A在该速度下飞机抬轮开始以便在跑道上空35英尺时达 - X8 Y- I1 x" K; }$ Z到V2速度。 0 B2 r+ N$ }* t5 l' XVREF, , A+ w. m4 Q1 O飞机正常着陆时,高度50英尺时的基准速度。通常是飞 G( H0 s& @# T; ]+ G# c+ d# v3 P9 j9 I6 H5 g* s5 X9 c& [+ @ 垂直航迹, - ]* R" | D- L: Q: ?* I; ]: g% R7 a+ U 英汉对照民用航空词典B OEING 8 Y2 @7 B: t) D% j- qTECHNICAL DICTIONARY 169 g- D; c& E0 |8 x/ f5 tW- P' b! v6 D& C: X8 [) B. x$ v WALKING BEAM, A mechanical component attached to , D6 C' Z: T8 t1 _: w3 E% jthe main landing gear and a hinged support which helps 4 p5 ^/ X/ m" F) D' Sthe actuator during retraction of the main gear.7 `. @3 U! s2 ? ATER LINE, A horizontal reference plane along the3 |9 @7 R* i1 @1 D fuselage for vertical measurements of the airplane. 0 O/ o }6 A+ K2 G* I& yWATER SEPARATOR, A component in the air ! q1 n' K0 C9 Aonditioning system for removing water from the air: M, ?$ N( o4 n$ F9 q/ V2 B7 R7 U 动梁, - H6 S0 b& x0 R4 Z8 b主起落架上,一端连在减震支柱上,另一端连在铰接支 ( z4 U. q; U7 V% O撑上,用以协助作动筒收主起落架的机械部件。 4 m! t0 D+ c4 q+ f: R) B1 t线, 6 a* M3 d2 t8 Z1 p9 z; Z沿着机身展向,用以量取垂直方向的距离(或长度)的! B M! a1 \$ @1 c# f; G6 f2 f 水平基准面。 ! J2 |, ^3 n4 V2 D6 c* x f0 W; G水器,: O" h- t/ [2 L- z- g 空调系统内,用以在空气循环机的空气下游除去空气中! I `8 m) ]3 X, H) N W9 [; @$ {/ v$ F0 H: r2 j$ T( M c & l) s( ]2 [$ |! A' P' ~) C, Pdownstream of the air cycle machine., m* T0 o, j& N# i6 e0 t% I; l; U! b" a* e% d, i0 _- _0 D: H! S* G, p! w1 \! H* m8 U, p的水份的部件。- h1 A; z1 J/ e$ D 英汉对照民用航空词典B OEING" \" |9 o6 B# M TECHNICAL DICTIONARY 170 % }$ @9 Z3 U; Y3 q* }4 D2 wWATT, The basic unit of electrical power. ) j" [$ w5 q. f V9 {( b' `7 xWAYPOINT, A predetermined geographical position 7 H! v5 u N0 z% r) ^( Nused to define a route. The waypoint is usually defined! e9 ?2 p% b) q& f4 n! y in terms of latitude and longitude. 7 w4 @7 {" k7 ~4 ]+ WWEB, The portion of a beam or channel that has been' H) G0 u7 a) s% t& M W- D! B installed between the top and bottom flanges. Its prime: k1 m- x# f& D7 l purpose is to furnish strength. $ D" @. ~% V8 J! P8 A* R. ZWHEEL SPIN UP, Rotational acceleration of the landing' y% t% ^& s& u7 v f the9 i; P) J: |2 ` nding gear (undercarriage) after retraction. - b4 I ]: R6 y电功率的一个基本单位。$ }! U$ R7 m% L- W: \( D& F 位置。通常用经、纬度来表示。0 H' Y3 U' ^& i. l" } 腹板, 2 U2 ^8 q: ~$ \" W* M* R梁的横截面。常见于上横梁与下横梁连接成工字形。主$ b5 u/ h4 `, b" b0 x) M4 C 要作用是受力。 - d0 U' g% v2 D5 N+ B轮加速, 3 q+ N7 m" p% O' g7 q飞机着陆接地时,起落架轮子的旋转加速度。 . x9 z# [: d" C! D轮舱, & n2 _# D. K* i6 a k$ G飞机的一部份,用以在起落架收起之后,收藏起落架的 ! C0 B2 W7 X ^& Y/ H/ u% d' [$ h* g那一部份。 & `9 L Y. B% L: K) Ugear wheels at landing touchdown.! m' M6 ^: \" v6 @7 X# s) x WHEEL WELL, A part of the airplane for storage o - ^# F4 u9 B1 N. g* o0 X0 ]la( u i0 U9 U o2 @; l- z6 E8 g 瓦特(瓦), - [$ U! _) x4 ?, E3 K& k8 l! p航路点,+ F1 G; _& ]' Y; e6 [ 用于决定航线的预定地理 * N1 i* E2 L0 } \; j& |: u. y. T5 B3 F; O8 K英汉对照民用航空词典B OEING 3 r y; f. R- `- `TECHNICAL DICTIONARY 171: k+ R- I# @( f: u/ F/ x6 I WIND COMPONENT, The effective wind relative to the / x% J1 i/ I6 C. M$ Shorizontal axes of the airplane.! i+ u, Q" R- O$ L WINDSHEAR, A change in wind speed and/or direction7 v5 q! ^ C( ~5 Q9 R! b a short distance resulting in a tearing or shearing( s& ]1 @2 L6 B2 Z8 {. ?1 ^3 E effect. It can exist in a horizontal or vertical direction and4 E% n- E2 `3 r1 R0 J: w5 g occasionally in both.7 V3 Q' U- d" g. b5 s$ a" L WING CHORD PLANE, A reference plane from the tip) D# [, y& V+ `* j. y, L* J% b of the leading edge to the tip of the trailing edge of the& }. _7 p$ S' |/ v8 d( H ing.' S0 X3 C: k+ q( W" N ING GEAR, The landing gear attached to the wing 3 K! ^ P z% Ytructure.0 {% S. W$ `) ?. G: k ING ROOT, Part of the wing which is attached to the I3 m1 r$ C. N. i% l- T1 Sselage. 9 r1 S9 @2 n% a. @" OWORD, In a digital computer, a word is a group of bits ) o- E* W2 X$ {( bwith a specified length. The typical digital word is eight 5 z* t. g; Y6 {( k5 R0 }! \$ [9 Ibits long. % z/ k- Z. p. S8 e风向量,6 N+ Z: S( D3 ?7 ~* U7 } N 相对于飞机水平轴的有效风。4 T# r4 c N, a 风切变,( `7 n" g5 ?7 F! H7 [ 短距离内风力或风向的改变而形成的撕拉力和剪切力。 ! t$ z ^. n+ k2 v. `可发生在水平方向或垂直方向,有时会在两个方向上同时3 N+ A! @3 Z/ d0 C; q3 z- z 出现。8 r* c$ p; d2 Y/ E6 H$ z$ n0 ? 翼弦平面, 5 D& ?: e5 C2 _通过机翼前缘顶端和后缘顶端的参考平面。* M n# Q, B3 H 翼下起落架, * v5 _( M3 O8 X2 L* i5 A4 T0 k7 B接连到机翼结构上的起落架。$ z y7 o5 h# E7 t5 m" l3 z 翼根, : b* f U1 Q, m机翼上,与机身相接的部份。 / W2 x( B( w5 \4 d字,. |9 u% W* s3 }) C7 K5 r 在数字计算机中,一个字是由一定长度的一组字节所组7 Y% ~/ K6 e" _* \) X 成。一个典型的数字字,有8个字节。 1 O+ |. f3 V, o6 }6 v( G2 ^7 a) Ain( o2 Y5 ?4 e6 L, |+ C. I, c$ Y w $ T; _3 B* f2 GW0 v6 s! _0 K& z s 1 t0 j) d% j r. z6 j+ ~W 2 M7 N) U/ J1 M2 i1 tfu, w& W) z" |4 ], k 英汉对照民用航空词典B OEING, F' B% p! J! b' H0 G TECHNICAL DICTIONARY 172; {) A- g* ?+ b! q1 b WRAP AR9 X f7 \% s4 m& f& e( L computer's . a6 J6 c1 Y- g* q& U5 KOUND, A BITE test comparing the 3 A a! o: A. Y3 ?* p- i- ]2 xoutput signal with an internally stored value." o; i; G- P" Q5 J XTK, SEE - CROSS TRACK , P W3 |, x% e' r, R3 C7 ?AW AXIS, A vertical axis passing through the airplane 8 v3 {2 c% z5 y) ^: z0 ffrom top to bottom. Airplane left and right movement 8 f: y, a9 k9 Qcontrolled by the rudder. (See Vertical Axis).: D' ]2 q" R9 p AW DAMPER, A system that is used to move the ! D* q$ Z, w& K' }: v! ~( R' c* l; tdder a small amount to oppose airplane yaw.; A+ y0 [+ z' X, N es. V. J% ~1 F: B+ q 回测, ; `# {9 b+ u% a自检系统对计算机的输出信号和内部的存储值进行比 7 S% b( ~" m% P1 b6 o. Y较测试。) {0 F( |4 A" q/ N+ Q" L 交叉航迹,9 s5 V9 {" f1 L+ @' q' d, f 见Cross Track7 V8 R+ T4 c( _4 ^2 H4 s- x X ; O( S j, i. L6 q& w# x6 U% ^) ~$ p& U/ j# L {( P偏航轴,- N% |8 l- w, z4 W 又称垂直轴。由飞机上部通向底部的垂直轴。飞机绕此6 ^( c" P5 L9 ]" ]6 f( b& |0 g) g 轴运动即造成机头的左右运动,这种运动是由方向舵来操 8 Y7 r7 Y& F4 S纵的。 ; q+ F9 y$ i# E: M% ~& y& R* e: E偏航阻尼器, 6 F$ ?# J1 B" _ s; ^; E' ]9 f用来少量移动方向舵,以抵消飞机偏航的系统。 7 I$ [! j. g2 K+ B飞机绕偏航轴运动的速率。 ; X; v5 y, r1 ?5 E# b# @Y" }3 u1 ~' ?6 \" g* } Y 8 o5 s) w H2 s' N1 xY/ L1 c! k, C- y. [9 ` ru! P x( N3 |' e& _* {: ~ YAW RATE, The rate at which the airplane mov# L5 g3 x4 v8 `, [2 k# B around the vertical axis (left, right).* L& z- ^9 d/ G5 B 偏航率,9 o! u6 {7 q# k V, `; y1 k 英汉对照民用航空词典B OEING N( ~: e5 P' O: X2 l8 F, @9 t G TECHNICAL DICTIONARY 173 F4 l$ U1 R! [/ t, y! zZ1 Y8 _, u7 s+ V3 r- q: o" p. `* f ENER DIODE, A special type of diode which, when, _ u* f3 _$ e4 @* Q( E# s0 C8 o2 \ ZERK FITTING, A device through which oil or grease is8 b; K9 f' |. s4 K upplied for lubrication of moving parts.: [5 Q1 B1 j3 e& `6 @ ZFW, SEE - ZERO FUEL WEIGHT& ~' Y M1 @+ y* V7 ^ ZERO FUEL WEIGHT, The maximum allowable weight ( V: L1 J+ a# ]% O: z5 ~: G, ?excluding usable fuel. # b1 H4 l" e* y8 C2 q纳二极管,* h. [! H* S5 _ 又称稳压二极管,是一种电子装置。正常电流可通行无6 _; c$ k7 E8 d( L" n 阻,但反向电流则必须在电压达到预定值之后才能通过。6 m' e6 ?: Z: w( m 在飞机电器系统内做为调压器之用。反向偏压时,它有一3 r6 a% {9 Y: p% a! L7 d0 {$ @ 个恒定的电压下降。 ; p- H6 y7 r- Q7 e3 X1 h& w; hZERK接头, ! G$ y: G( B2 d; I$ T$ b8 }7 _ZERK公司出品,用以接收滑油或润滑脂,以润滑活 / F/ B4 e# w$ k, |5 n, P动部件的装置。; _' d; @( t( }6 y% T5 z 燃油重量,$ S# w2 |; n; }0 U% Q" D$ _& t: e4 m 见Zero Fuel Weight) c7 n( A9 w4 O5 n. h+ }2 ~9 u Z# M$ Y6 h- ]: H; _4 c reverse biased, has a constant voltage drop. This; \! d3 q/ @2 Y! N3 o& j property makes zener diodes useful as voltage + e7 c* J! s4 @1 tregulators.4 |/ ~/ W) t7 U7 P# K s 3 F- h$ s6 i) U5 a* g! f2 h, y% Y p/ k# |1 W4 D& P6 x" l ]4 d* F5 I3 @无燃油重量, 4 o$ S( s8 n; Q8 C3 P) {扣除可用燃油重量之后的最大允许重量。

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22#
发表于 2008-12-24 21:46:54 |只看该作者
TECHNICAL DICTIONARY 63 : N8 I: g& s% G( x' m1 M# P7 KFLIGHT DIRECTOR POP-UP (FDS), The automatic ' }4 x5 c( f/ D, r. n' `7 edisplay of flight director commands with flight direc0 e. Z" c* C6 t/ ] switches in off position. 6 D8 l7 Q' I2 l& rtor b/ ^! A( y1 A" C# Z2 Y LIGHT INFORMATION REGION (FIR,UIR), An3 e8 I) E" M/ {" P, D FLIGHT LEVEL (FL), A level of constant atmospheric % e8 R/ b4 X* D( s9 h- I6 qpressure related to a reference datum of 29.92 inches of ( V8 O& y2 V. m7 K! C0 amercury. Each is stated in three digits that represents & f. \! @$ d8 g$ Hhundreds of feet. For example, flight level 250 $ X8 }. N& c, p' vrepresents a pressure altitude of 25,000 feet.1 C0 [1 c+ {( S, X FLIGHT MANAGEMENT COMPUTER (FMC), An2 e# f" `' [/ ^ airplane computer used for navigational, guidance, and % U4 k' W' H, [" t4 Zperformance computations. # n: I& g1 g' @) S' ~ d' lLIGHT MODE ANNUNCIATOR, A display or part of a" k& r0 K9 C" F2 M$ v. p isplay that shows the autoflight mode of operation. 8 X) ]# h1 s( kLIGHT PLAN, Specified information relating to the j5 h0 |/ j1 ^% l7 Gtended flight of an aircraft, field orally or in writing with ! n7 u8 S* ^7 r: I$ Vn ATC facility.$ P' l9 Z; w- P1 R* @ LIGHT PROFILE, A description of the flight which 3 b0 s- G$ k2 z* Y, y4 M4 ppecifies the climb, cruise and descent altitudes and, o! ` I: s/ T6 \; d$ q peeds to be flown.7 V. n$ N- S# o" w, B+ z K4 g7 X 限定的空域。 ' }7 Y: s/ ~' h5 m8 g高度层(FL), 6 k) Q7 x$ O6 A5 `/ W% K相对于29.92英寸汞柱参考数据的气压恒定的高 ( @0 m/ E: @3 h1 I每层均以三位数表示,一百英尺为单位。如FL 2 8 P$ F) M) U7 J压力高度为25000英尺。 % y* a: O+ o0 ^0 q& h3 M飞行管理计算机(FMC),6 d$ j* U5 j( ?3 x, J; W2 ` 用于导航,指引,和性能计算的飞机计算机。$ x$ u. P7 n$ W# { 飞行方式信号牌,8 F7 `7 _2 d' Q& b 行方式的显示或部份显示。 ( f+ F' O7 H2 X: [) {飞行计划, 9 H# V7 h* G9 J向空中交通管制作的口头或书面报告。内含与航班有关 5 j8 f% ]& b Y+ m6 ^" n4 ^+ x y的详细资料。 6 {) l5 L& J4 S5 @6 C/ ?飞行剖面,. Z3 Y4 W/ b) S+ ] 对一个航班的描述。详细指明爬升,巡航和下降所飞的: y Y) P7 Z7 w5 y 高度和速度。 6 K5 Z" z: s& h2 R& F& FF

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21#
发表于 2008-12-24 21:46:35 |只看该作者
FLARE, A maneuver to transition the airplane fro5 S+ _6 O# p5 g+ l9 A2 P a5 Q P5 _- q9 J! {' w9 {3 ~, \' W FLIGHT CONTROLS, Hinged moveable surfaces o 6 {9 W4 x2 ~$ d. E9 Awings, horizontal stabilizer and vertical sta 7 l& ~% w* W' ]) ?OEING . O8 Q7 x& q* \6 NTECHNICAL DICTIONARY 626 d, a0 E- F0 G a ( n2 Z7 F& y$ s7 }$ Q$ uo$ b. G* ]/ L- k7 T 襟翼速度计划,) Y! O' Q; i7 Q, N4 p. i 提供各个襟翼位置的推荐机动飞行速度,此计划以VREF # b3 t: [- ]9 m9 `加增量为基准。 ! z0 z! z0 P, W4 X9 o拉平, 2 v$ Z4 W) Z* F/ `4 a# A一种将飞机从进近过渡到在! m% ^8 w* X( j+ z! S9 u" J 飞行操纵5 g/ B& ~4 X0 r$ [) |$ v7 _) H 铰连在机翼,水平尾翼和垂直尾翼上的可动 4 F9 ?0 N; G G+ G& g, Y6 B" ?* k6 j3 s9 f q6 q 英汉对照民用航空词典B OEING

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20#
发表于 2008-12-24 21:46:18 |只看该作者
FLAP SPEED SCHEDULE, Provides recommended + t& s& \, o' Lmaneuvering speeds for various flap settings. The fla) Z- Y; S8 {. b z$ Q speed schedule is based! E. K- C e b9 T9 q+ z3 \ p & X( U- C; }9 |2 N ^. J3 F: Won additives to VREF.& `3 f: j7 f n- U; J9 ~% C m4 |; V% `# m5 w+ {7 x pproach to touchdown on the runway. 6 z0 R0 m: E# b" H7 _n the 3 z: c% O, {/ P. U/ tbilizer for 6 L% K, G7 h9 b( J& X; ]irplane control during flight and high speed ground ! u" p& e; r/ L3 C9 Uperations. + |! L) W9 ?- T* {$ b2 HFLIGHT DECK EFFECTS, Indications on the flight deck & X; ?4 B2 ~- s* a' Y) _# t2 v3 l2 |9 ecaused by a system's malfunction.% |6 G. ]( o2 f. z FLIGHT DIRECTOR, A system or portion of a system , O+ q+ c' r! k" a) g/ gwhich presents commands to the flight crew for control 6 M) _5 e2 f# kand guidance of the flight of an airplane.8 z$ ^" C: C/ x* V 跑道上接地的机动动作。% O' i% L. T l3 p8 [ 面, : w; {- L9 P* _* O& V, R! |: B面,用来7 R* |6 o' W4 G' p! Y 飞机飞行时和高速地面操作时,控制飞机。7 H* A5 Q% M. D, n" b: K 驾驶舱效应,* Q6 x) @7 r4 L" u4 ~ 因系统故障而在驾驶舱中出现的指示。 1 `. o. C' }1 _; Y3 S% X飞行指引仪,& m0 }1 K' m9 }, p2 N' D/ C* P 为机组提供控制和引导飞行用的指令的系统,或该系统2 G3 ^' a, W9 s% ? 之一部份。

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19#
发表于 2008-12-24 21:45:56 |只看该作者
edge of the wing used for increasing lift at low airplane3 {$ h6 R" X9 H3 o9 L4 ` speed. Flaps may be triple-slotted.8 t* y# J7 q% P4 ~ FLAP LOAD LIMITER, An electro-mechanical " L2 F3 \' C' G) {1 s5 ucomponent for - K/ h' |- q! Q% i: ~6 A+ Op3 W$ s% [7 r2 h+ n1 q' | FLAP RETRACTION ALTITUDE, An al; ]0 S1 E+ ]8 u4 j1 v$ Z3 ^ fo, ?4 C# B" ?2 t: ? FLAP SETTING, The selected position of the aircraft . H9 M8 p( q! w( k, W- r5 Tflaps and other related high lift devices.. }& \8 Y( M/ ~# u 襟翼(前缘), , h( _! p) F0 _' V8 H铰连在机翼前缘下表面的可动部 % V! M4 `. O! y' y, O. ^- v2 p7 w" p! C Y8 J! `/ h. C 机翼后缘的可动- S6 J. t3 O- @1 O, @5 L: s5 L. Y 缘襟翼可多至三片,每片之间有缝。 9 g/ v% i6 r+ x+ y# l3 i: R% `* S襟翼载荷限制器, $ P) b3 C. @2 P. n+ L" y* I) |' u收襟翼高度, 7 l) \0 b* x3 q襟翼位置设定,: f- N( x3 K% { X: S 飞机襟翼和其他有关增升装置的选定位置。$ i/ M; n: @% |; J) u h- o 英汉对照民用航空词典B

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18#
发表于 2008-12-24 21:45:38 |只看该作者
FLAP (LEADING EDGE), A hinged moveable part on9 G% U, s3 t: k e underside of the leading edge of the wing for ( ^- V, h, O) E/ xcreasing lift at low airplane speed.4 _9 _: ~- p0 V; L2 [7 t LAP (TRAILING EDGE), A movable part on the trailing% ^( o7 u3 [7 s3 `! L2 G preventing further flap extension during d4 x4 c% s) }( d eriods of excessive airplane speed. ! j6 V" o0 X( z! mtitude selected% u8 K# [+ I ~ K6 l r acceleration and retraction of flaps.$ ?9 }2 g& n9 y! e- i 件,在飞机低速飞行时& C5 d% i% z* G; Z* D 加升力。 8 A/ V' N! e6 E翼(后缘), % ]7 `* b* j# i! C1 m* j# e' d部份。在飞机低速飞行时增加升力。后: v- H) k) _2 |' t5 Z 用来防止襟翼在飞机速度过高时过度伸出的机电装置。 ' S" d) ]* x; \3 Y7 h为飞机加速及襟翼收回而选的高度。 * [0 T- f; P9 ^/ Uth / Z. f$ |; {8 w* Ain # J7 Q: y G! D+ RF

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17#
发表于 2008-12-24 21:44:17 |只看该作者
FLAG (NO. 1), A failure indication# Q- Z+ R: O. A! P FLAG (NO. 2), In a computer, an indication that a $ [: a/ i0 ~- f( O. Lparticular operatio* s0 x4 Q; B- o! |4 }6 {# u FLAME ARRESTOR, A device in the fuel system vent7 s2 W$ d, k: G+ V( L3 F lines for preventing a flame fr1 t+ V6 e& Q) S4 h& l) z ta 2 ]! S( S& Y0 ], ~' Z+ s6 IFLANGE, A projection ) k' D; J$ }" l5 x0 ?. ec 8 {9 F$ S+ _8 s固定模拟机 X* F1 ^; c4 z- {& W! @$ \除了没有视景和动感之外. m: A- R) Y' Z, X5 H3 X5 O% ~+ \' W% p) x+ M F故障旗, W* ~/ T- Y' H g: ^; x. d标志, 2 v8 T5 n, Q3 e/ e: O在计算机 ) g8 k- J( r9 `6 c火焰阻止器, 8 L+ p6 p5 d3 q- X燃油系统通; e- i y1 P, r$ u0 {) Q1 q" b- X# F. f, g+ K9 \+ ]发动机法兰盘, 7 i q9 k/ c/ _+ N" N! V, V英汉对照民用航空词典B OEING ; u; Q; p6 ~# a. U0 N4 [TECHNICAL DICTIONARY 61

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16#
发表于 2008-12-24 21:43:50 |只看该作者
FAIRING, A covering over structure providing a smooth% @5 X6 W& B' j surface for airflow. 2 n r j* ?4 Z( pFAN (NO. 1), A rotating part of an engine, driven by the% ]+ X N! z/ h) }; Q low pressure turbine, for air supply to the engine and to % c& S4 j% c4 j2 mthe duct around the front part of the engine. The fan 9 j2 ]5 `6 z, ]( m" kprovides the major portion of engine thrust.) M2 |/ b3 n1 c and operated 5 |+ C K: j8 d8 \1 c$ iy a motor. Fans are usually used to provide cooling or( n$ I( p4 d8 w5 c7 e( ` ir circulation.% ~8 T8 A+ f; [+ b B FAN AIR, The portion of airflow through a turbofan ) j- w$ J) d' M+ [; P. cengine which passes only through the fan.& k; [% q6 ?9 O) R2 m; U 性构件。 5 G% A' \) c% n/ V0 d& w1 n发动机的一个转动件。由低压涡轮驱动,用于给发动机 & V9 @) r5 L3 d3 n- m$ l! r( C及其前部管道供气。发动机推力的大部份来自风扇。 * ]) @5 L' N1 N1 Y) uQ.2), 1 C( V$ x6 r' |片旋转桨# O( G( b6 ]4 Q: K& h 所组成的装置。通常用来提供冷却或空气循环。 0 D" q( e- [1 ?- k3 a0 x风扇气流,7 B: U* u0 ^2 ^" T0 F 在涡轮风扇发动机中,仅仅通过风扇的那部分气流。 b! r" {+ ]& _6 qFAN (NO. 2), A device consisting of one or more5 A1 ~4 p" ` w& y& @ revolving blades attached to a rotary hub( Z& w- @; x( C+ d7 v b. l9 N) g# \; T) k* a a ) \3 d4 S( q4 i/ q% G: m; g4 l. V整流装置, : q' e! v2 {. ]/ y; |8 x* Y: N给气流提供光滑表面以减少阻力的覆盖& K0 V1 m8 _$ G* t: X) c+ e" T 风扇(NO.1),9 _( X( e/ d' i/ @5 n/ ?' `6 A, v% d; A0 ~6 H/ k/ J7 x D风扇(N 6 D& `& ~/ J6 \0 i$ a0 O' B安装在由马达驱动的旋转轮壳上的一片或多 3 z& N% H0 }/ z. X0 H* U9 n( s2 ~3 t$ Y- E7 i9 _英汉对照民用航空词典B OEING) }! ]+ L, d: j* r- [; E2 x9 r TECHNICAL DICTIONARY 57* J9 D' V; P, t8 X FAN COWL, A covering around the fan section of the ; y6 x0 q/ ~7 u* x+ f, e% ^engine that can be opened for access to the / A! l$ A- C: l8 L1 Ucomponents on the engine.$ |! X' Z" o+ F FASTENER, A mechanical device such as a bolt, nail, ' L- Z" s5 K; ]7 q) tvet or screw that is used to tie two objects together.9 j& i8 l5 Y) K- U$ M! O# T, [ l which6 z. b1 B' O" p lane faults. Used by airline mechanics.. S2 G- g7 H2 g' } airplane system / t# k/ S2 A7 f% B: ]- M. |% ^& C8 X: Smalfunctions. 3 L T8 [, y5 F% k固件,) W1 `- J# g. n1 t! x' k 用来将两个物体连接起来的机械装置。如螺栓,钉子,. L9 v" n) x [/ f 钉,或螺钉。 / n$ R# N: f: m# w# b2 {( h {, @断裂,& h; A! \; M | FIM),7 K# x% W1 r: Y+ q2 Z2 f4 [ RM),6 J# q( ^ X1 @( b" i0 T 的故& y H! A) {3 B* ? m 障。 7 P4 O. c2 t" y! a. Qri ! o. k; U8 \+ r9 R' jFATIGUE OR FATIGUE FAILURE, The failure of a ! s- z7 K6 I% a! |+ I7 ?material because of bending, flexing or severe vibration ! h; N) j2 t9 V7 Nforces. * }" i& Z. e+ d4 ?4 y. z9 p. @8 KFAULT ISOLATION MANUAL (FIM), A manua# F$ W$ p [1 W8 M( a0 C' o! s contains procedures for isolating and correcting ) v: a# M; w8 F$ M' k* y- o( Ureported airp - G- r' X7 _5 Q+ l7 T* q5 a1 `FAULT REPORTING MANUAL (FRM), A manual used $ H; O4 V# {: U. Q: j& y- P9 fby flight crews to aid in reporting n! V) A& ~' A4 h6 k& d风扇整流罩,. _+ Y- o( b; G( c* P. D$ a 在发动机风扇周围的可卸盖壳,打开后可以够到发动 0 c& b- x% N. b6 c: F( B机部件。 ( `1 b( i) q# { V. C+ l' h2 U2 C& ~( G, l& C- O( a+ I: p疲劳或疲劳9 |8 q7 g3 C( m: h% T 因弯曲或剧烈振动力所造成的材料断裂。 # E Q1 H. `( K5 B0 [$ _故障隔离手册( 0 ^- V% d y; Z内含隔离并排除飞机故障程序的手册。供航空公司维修0 b7 ]+ q; r5 f* g 机械员使用。 ! j2 t3 C/ }, U' Y1 W: O故障报告手册(F 5 J# ]# `' [9 ] b/ b6 o机组使用的一本手册。用以帮助他们报告飞机系统3 ~. N! L. s3 _ 英汉对照民用航空词典B OEING " @% A# `! X( H( r) F3 u' W" g2 NTECHNICAL DICTIONARY 58 8 n7 l) F. C$ k( {! Y4 K, ?6 WFAYING SURFACE, The overlapping area of adjoining2 g4 P# @# a3 r5 Y6 Y- f1 J surfaces.$ w0 ]" v- W7 w6 D( A FEEDBACK, A part of an output signal which returns to) S* m) h# t% j4 ^; w e input for control or indication.# d9 @% K6 j4 q$ l& | EEDER FIX, The fix depicted on Instrument Approach . P* `" _% N' O3 Q% Orocedure Charts which establishes the starting point of * i8 t7 D, s0 u( Z: c! z2 z3 m/ ye feeder route. 3 H' c4 ~& C3 Y$ go& L" K5 w9 {' ?+ U9 b) _/ u ERRY FLIGHT, Flying an airplane not suitable for : }* ^# v5 ]/ F- f2 {venue (passenger) operations to an airport where ! I: d7 t% i8 X' h/ `- ]' rpairs can be made., X' e- g) H6 C* F IBERGLASS, A material made from glass fibers and" R- i; ^# A7 Q) n; i3 [ sed for aerodynamic fairings and access panels. / v2 X- L# Q2 o7 Kf$ p3 I) M- G. @. S9 g3 @ ILIFORM CORROSION, Thread or string-like2 c/ Q9 j7 L2 b, a0 ^" A$ w ally 1 e0 n+ T2 \1 o: \/ H$ w/ ?4 v反馈, $ A9 p+ |: @. d2 N/ u' v! c+ ^输出信号的一部份,回到输人作为控制或指示之用。) v9 ^6 V3 n, P6 z 支线定位点, 0 O: b0 [* R3 s0 d) H! K, r是在仪表进近程序图的定位点。该定位点建立支线的# I) b$ S6 |& W9 G8 { 起始点。& o( D u0 a) R 械装置。 # g2 S0 E( C3 k2 }& S7 h& u: S运渡飞行, 5 U2 q0 F# ~7 z0 C- l7 l) @% ?将一架不适合营运(带客)飞行的飞,飞到一个可以7 s( H8 D1 |; t9 n$ ^ 维修的机场去。 1 s! w; W$ _+ ^8 G$ N+ w9 ?) V玻璃钢,% R, M; W. D5 \1 a( k& f% `! } 由玻璃纤维制成的一种材料。用于整流罩和各种舱盖。6 g$ V5 F5 b+ v7 j 状腐蚀, . {) G& g8 O% ]/ P9 i; m2 u0 H+ @形成的螺纹或条纹样的腐蚀痕迹。通常出 $ P8 y: Y1 g% gth7 Y$ z# F$ b5 H% k7 I5 V- Y F9 |, F5 J u( o. i7 l+ }0 s; D) j P* L) B* u: J$ a! a% W- L* F: d th / k: }1 m$ R, E5 ~7 }FEEL COMPUTER, A mechanical device sensing J1 f5 {% j7 p* {5 w7 Y+ \airplane speed for supplying variable pressure input t/ I2 m# P0 R/ L1 d the elevator control system.0 ^' F' ^, O$ {' x3 r7 m/ E F: }# @6 f) q M- h& A re , P: ^# @+ n L+ p, m% X$ j$ ]re% p+ ]" d' |( h$ O2 N4 ?3 ]( X F, N7 k1 j1 v% c( f6 c( O% y" o u3 j5 D0 B+ k$ H1 d! \5 A* R: B FIELD LENGTH LIMIT WEIGHT, Maximum takeof 6 j3 o6 `0 S' Q/ q' c: }gross weight based on runway length, slope, wind, and7 a; ^7 f" N8 a) v+ j temperature.9 Z+ {$ U: o1 X1 q, n F / C$ X4 g: j! ]corrosion paths forming on aluminum structures usu , J7 u8 O, Y8 }/ |/ F) n0 Y# munder painted layers.4 W: }& K, W# `1 e0 u 接合面, V2 ?. i7 A# N& f. x* j邻接表面的重叠区域。 1 ~1 @1 f- ~' I8 i$ a; `( F$ ]' s- N) l- F6 q感觉计算机,8 P o: E' m, r0 F: \! J 为向升降舵控制系统输人可变压力而感应飞机速度的 5 n) Z4 L" G9 F8 E5 x3 r& U5 Y- l8 r$ F, r1 G9 t/ B9 a2 F7 ?场长极限重量,4 u- B6 i3 a3 [: e/ n3 m6 @ 由跑道的长度,坡度,风和温度决定的最大起飞总重。4 Q. p3 D$ G# R0 H, U) b% h 线 & Z+ O* V6 d2 y4 Y4 q在铝构件上0 G4 l" m' c+ L8 S2 ]( p6 i1 ^ 现于油漆层下。. j1 T( L, X& `& z 英汉对照民用航空词典B OEING5 m) P# m0 q5 X8 s% L$ ]; f TECHNICAL DICTIONARY 59 \9 F. T4 w5 ?! G. P# S FIM, SEE - FAULT ISOLATION MANUAL+ K. G& q& Q a2 C! F FIN, SEE - VERTICAL STABILIZER& N1 r: e" Q. s% R, A5 n1 j/ u INAL APPROACH COURSE, A straight line extension 6 r) G0 ]7 g% X+ f% L ]f a localizer, a final approach radial/bearing, or a / D* M! l% O- R5 w2 _nway centerline, all without regard to distance." v1 L, B+ e E. ]. U T9 ^ INAL APPROACH FIX, The fix from which the final4 q( e0 p6 N; {4 c pproach (IFR) to an airport is executed and which 9 ?! m' a5 p. C& A3 t* B0 kentifies the beginning of the final approach segment. 7 o& e9 _) v& a5 S5 q0 }6 R mis designated in the profile view of Jeppesen Terminal7 R' ?9 z- ?( @) P2 I& R- o harts by the Maltese Cross symbol for nonprecision a4 S/ _. t; Pl 2 z- I2 Y n8 g2 ?' m6 H2 Ztarts at the FAF When ATC directs a lower-than / C& \8 {3 ~4 M ~2 }( l6 o, ~: yublished Glide slope/path Intercept Altitude, it is the* P/ w! b5 e* h1 h3 U0 r sultant actual point of the glide slope/path intercept.# H$ E, i/ G$ H: C7 ]$ U. D6 j PPROACH, That part of an instrument ; T' f$ j! E* G- gpproach procedure which commences at the specified 9 @ X, H' R' P- E* pnal approach fix or point, or where such a fix or point is( u- X) {: A: a7 u( k8 Q ot specified.; B9 v! x5 a2 Z$ m3 k2 a" l IRE WALL, A fireproof partition or bulkhead between& l. ~& l" Q. n0 }6 }$ e/ ^) a e engine and the airplane structure.( D0 _; |5 A: N5 d hical position determined by visual ' J9 Y% D0 y( V& R9 ^0 @* Preference to the surface, by reference to one or more 9 i( j% {- Z! r# ?6 h- Z5 b' \radio NAVAIDs, by celestial plotting, or by another ' E) l' D9 }9 r/ Dnavigational device. 0 {# _+ _" V- M+ PF3 y- |; D0 D8 M$ R- c& I o * i$ A B" m3 Hru % K, H% S$ _- B1 {& d# {F2 {# r3 u+ G! \. L+ V6 ^ a ) b0 I6 N4 Y( d& ^id , a, `7 l. r4 X! mIt& U! c0 f% N$ V l9 M8 J5 K c % a+ \4 \5 S+ Japproaches and by the glide slope/path intercept point4 P2 F, }2 o+ z1 o2 [7 q9 x on precision approaches. The glide slope/path symbo % ]$ I- X# }3 r+ P) @s: c/ V8 T+ U8 r! [' k, k3 o- I% e- e p" F' C) s4 E5 x9 W! [ re " \1 n+ D6 Q: o, v/ |$ Z( X. NFINAL A0 Q) D! J# [4 H0 u1 Q" \ a 0 c# E; t; I* b! Y( ~* Qfi- z! n- s& t$ w/ W j& g n * r% C$ A# |7 s0 ]F. I h y6 N& l2 d+ D' q th" ]+ A5 ?* k4 U' C FIX, A geograp + Z% ~7 t5 b i! y: a+ S故障隔离手册,- ?$ {8 j$ W0 j; O) U) v 见Fault Isolation Manual. ! \" D# ?+ \+ D; p9 B' V B垂尾,! o# l% B+ h6 l2 L0 k* G 见Vertical Stabilizer ! u$ O9 I3 ]9 T i, _最后进近航道,4 f( b g& Q/ Q 一个着陆航向信标的直线延长线,一条最后进近径向/ ) S7 H; g5 f, j2 T方位线,或一条跑道中心线,均与距离无关。$ \" G( f6 }: g; S7 O 最后进近定位点,6 b: c' Z2 C2 h" k# M- P 向机场作最后进近仪表飞行规则的定位点,也是最后进 9 t4 O: }, W+ W开始的标志。在Jeppesen Terminal charts的剖面图 4 j6 g. ~3 u; E,非精密进近用十字轮符号表示,精密进近用下滑道/: ?- s. p8 L }" e 道切人点表示。下滑道/航道符号始于FAF。当ATC指 ; T; i1 f6 [7 y# c/ y1 V公布的下滑道/航道切人高度时,FAF是由此4 ~: `7 u6 E! K1 K 后进近,% b1 Q3 Z( D O8 Q5 ?* y! k 是仪表进近程序的一部分,始于指定的最后进近定位点 $ E m! O/ I) K) c6 \ Z6 w最后进近点,或者未加指定的一个定位点。 u2 r9 \$ N6 S( m; N火墙, " s" g B- q4 o- D位于发动机与飞机结构之间的耐火隔板。/ l$ P3 E2 w) y/ |5 E( I, y9 H6 m" w由相对于表面的目视参考决定的地理位置,也可以由参 6 L# r7 R# [0 S4 L3 o/ X! Y4 s$ X照一个或多个导航台,天文导航,或其他导航装置来决定。 , f% x. X. T; V1 Y0 K8 A9 S7 N' p, Q+ X% P* @; G' y7 a! p z% T+ B, g- y9 \% S# `引一条低于# K7 U" G' O6 b0 ^ 得到的下滑道/航道的实际点。) {: B$ k8 z8 [0 }" M- S- X% N0 ?* a p: F$ V9 y# {: A4 z( B# h, T7 w! i% n' ^/ N, [0 }; K定位点0 v; C( m+ ^2 F' ]; n+ h 英汉对照民用航空词典B OEING$ j0 d8 z% i' r. y4 w4 u TECHNICAL DICTIONARY 60 5 y9 t3 D0 n) Z6 Z9 j. O! C# NFIXED BASE SIMULATION (FBS), A flight training 8 C8 q- ?, [. i# Xdevice that is identical to the FFS except there is no, o# w) ?. h# K1 ^& R& U9 P: s isual or motion system. $ h, |2 q: [6 t- g4 Lon a display. ! L$ K- Q& l$ X$ O3 T9 Zn has been completed. \% D8 d2 z) G7 mom outside entering the 4 K1 C# B1 a1 N: G5 b! n% e+ \nk. : w) P3 p# D/ q( u9 E- L: j+ Ron the engine for attachment of m/ ^) E" ?# n( `5 U3 Womponents on the engine." O; E+ o8 k* n( B$ W& m' f! }# f7 T (FBS),, H( ?* u7 p- W& M+ [- J/ F+ z+ a$ [ ,其他特点与全动模拟机相同 3 Z: l' X9 S: q! i; B3 z0 G8 q飞行训练设备。% H9 \& s& x5 d6 C4 Z 在显示器上的故障指示。1 v( J8 `' A. b3 H2 b) c 中某一个操作程序完成的指示。 * a- h8 F. w3 G8 U气管内的一个装置。用于防止火焰从外部 ! M& l1 {: K$ h" e: j/ w人油箱。( o1 R# @6 G! @$ p, }! u' u 发动机上用来连接部件的凸缘。! m- D. p, q1 x" h0 F& C v

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EQUIPMENT CENTER, A compartment in the fusela% c8 k- K& l' m2 i" T4 e for storage of modules." Q7 n/ l: l$ d, a$ h( |- O! l ge 1 }' l( w/ ?& J P! j6 a. V5 [SDS, SEE - ELECTROSTATIC DISCHARGE- g4 p3 G1 z6 B @ ENSITIVE DEVICES$ c6 C* { A& D2 {) H STIMATED TIME OF ARRIVAL, For IFR flights, the z& K% |) R4 k; u% l! ^. S1 t me at which it is estimated that the aircraft will arrive $ W- e, P- y F9 c; D0 hver that designated point, defined by reference to & b. e1 j% w# v) n5 Kavigation aids from which it is intended that an7 L1 v$ E" W2 \8 W) |. ~ strument approach procedure will be commenced,or, if% W7 B( n0 i( \+ _! i o navigation aid is associated with the aerodrome, the! U6 n7 P' b, u/ O me at which the aircraft will arrive over the aerodrome. . k3 }2 l e6 a2 s* J# a, For VFR flights, the time at which it is estimated that the# t% S7 u* s* ? UTECTIC SOLDER, An alloy with very low melting 9 B p) S( N; T& Loint which permits automatic fire extinguisher 4 c) V* ]: t$ a, a" ^: @# S2 fVAPORATION, The changing of a solid or liquid into a . T/ [# M8 F1 k8 Z HXCEEDANCE, Any condition that occurs when a* O/ @/ T& [: A; T$ T+ a4 H! @3 g ystem goes beyond its operating limits.% L# L& |- q# X/ }; S# | of electric current to the field : e. b! t. `) C; z M: p v4 mwindings of a generator to produce a magnetic field.( e& b8 i" i/ w0 c4 C9 h 静电放电敏感件,- V/ o1 v3 |' h 见Electrostatic Discharge Sensitive Devices4 _: K/ B% m8 I E% {7 G8 u& @0 N a2 G" W6 ` S" x8 r1 C7 w6 R0 n E 4 V0 P" O6 [ i. nti $ T" k8 {$ G2 A( U. I, [8 P2 v/ Vo9 z& ?0 R; X( N* V% O, u: t. Y n4 T$ s. F: k& t# m9 H6 M9 y in6 Z/ v5 q5 Q8 M2 w' U) _ n 4 r0 p- |3 {6 Y: D1 \ti4 e9 j- q7 {& Z# x7 X2 V F $ l& j5 S) j4 d: O9 zaircraft will arrive over the aerodrome. 0 E' Z+ j! d! G; W7 vE0 Q" J2 q3 e* e# _2 I( c p / s N" [" S1 S+ k: ^discharge in the lavatory.- a5 G( X' k& e) ~& P E ; R# e6 h3 _7 b* _vapor. A thermal caused activity. : `7 [4 Y9 p4 a$ T. D- h, C4 D( I. D* kE6 i% S3 Q. c$ ^9 V" s0 c s6 m: V, T, y! D' f! p9 Y3 U EXCITATION, Supply& s% B' N+ O- n: \% o9 I: z; C0 v. ^ 设备中心3 q+ [" {- _# p 机身内用以贮存各种组件的一个舱。4 F6 R1 X$ K: r4 k* L8 A3 i t" q8 t3 I* k 预计到达时间, ! K$ x' v; M# m& m6 K% D对于使用仪表飞行规则的航班,是飞机到达指定点上空 0 V+ K* ]4 Y2 e的估计时间。它由参照仪表进近程序起始导航台而决定。: ]# D5 W1 g1 y' v$ m 若机场没有相应导航设备,则是飞机到达机场上空的时 , U. H$ h; e7 \& N$ w" }: S间。对于以目视飞行规则飞行的飞机,飞机将到达机场 % ]1 r5 s6 Q8 V# L上空的估计时间。 , w( V" S/ m+ ?( w' e6 I" T/ P$ C熔焊料,/ t1 H; Y2 @6 a- n i) x 一种低熔点的合金,可使厕所内的灭火器遇火时自动1 O0 H9 z$ M% A2 E4 z" E; D G 发,' P5 z: P. D* a* ]6 p) h5 O 变使固体或液体挥发而变成蒸汽的过程。. u. R: N: ]0 ?6 c! O0 R( [ 值, 8 Q& K9 g. S3 `) O2 ? o4 {* a当一个系统超出操作极限时出现的情况。: _1 x) D6 C5 i, H( a 励磁, & Z+ R6 I; ~$ Y# I; o6 T供电给发电机的磁场绕组以产生一个磁场。 % H' O, `% A: s5 D% Y0 }$ O5 u% K2 S+ i: T: f& U4 t- o8 V! N 启用。 % \2 z ~& S# V$ {) m' D- ^& b0 K' m! u, E/ F由于温度的改, E8 w6 w: F# s) s/ n1 x4 ^) G5 H) o+ h- q! P& S+ p 英汉对照民用航空词典B OEING0 G5 w: } @, h( Q, D3 r4 u TECHNICAL DICTIONARY 55: }5 p; C3 K8 K" s& j; [6 b EXHAUST GAS TEMPERATURE, The temperature of* I( t" u* Q) [8 ]) H; E4 ~8 n the engine exhaust measured by thermocouples and 5 L5 y: C. ~% mdisplayed by an indicator for monitoring correct engine+ V, V/ ?, q: I" b) i7 Y operation. 1 I( I% \. {# T% qEXTRUSION, A metal unit that has been forced through % _# p" t" B/ k6 v2 f7 {shaping die while it is in a thermal plastic state. 8 n. W/ m* Z( u! I( PYE REFERENCE POSITION (ERP), The optimum" Z9 K' m A6 z/ S/ x ilot head position to see the airplane instruments.1 o5 d" o' h6 G( q7 Z k ccomplished by adjusting the seat.* C( F& b0 C6 `6 b; {+ p' m AHRENHEIT, The unit of temperature measurement in & w6 `: d/ Y# V% w3 W6 b. n# ahich 32 indicates the freezing point of water and 212 1 t/ s5 I1 ]* u: N6 }" PAIL OPERATIONAL, A system with enough 5 D- B* p I4 v5 x) y* O" k" Ldundancy that a single failure leaves the system fully 0 K4 `4 K- w& i2 v2 ~ot [* X8 e7 |) X& b' ]; B0 f压制品, 7 W% L0 w- u0 N, u! m在热塑状态下,经加压通过压模而制成的金属件。 5 F! b4 k2 E2 \. M$ S) I目视参考位置(ERP),9 o. }. F& C' a 飞行员观察飞机仪表的头部最佳位置。由调整座椅来 & u; e6 _8 D+ S& _到。 , g& c$ \ h+ v8 Y) u氏度, 6 d" e) o, u0 z) a温度的度量单位。32°F表示水的冰点,212°F表示水的1 f: o- _- c' z# E* Y+ { 故障工作,, y7 p4 i# w; e \, C 一个具有足够冗余度的系统,即使一个故障的发生,仍 " U7 z) u, b! D$ \' v# L正常的操作。$ K2 ^ r1 l- @( R* h/ d! b 防护, 6 v k8 ^, ]- Z+ Ya 7 r. X' F3 @" M& N6 sE 9 T3 H( ]6 `8 Y0 U6 Y! a; Ip. _$ V) X- S; Z* ~. n9 I4 R U A * o) p) E0 i" Q. G6 C! h! tF , @. u% L6 O! `( OF: ~( p/ L& T+ }: B# j0 } w 0 W5 b' { i7 i% L( Tindicates the boiling point. ! Q. N* Z& x; MF7 @( [. D) k" L8 k* ~, T: S re8 C( P/ @! T3 n, m operational.8 N4 Z# ^; \2 u FAIL PASSIVE, A system which is designed to be n( T, j- h; R" C! w; t operational for a single failure.: O7 y& f# \9 l5 h 排气温度,0 b8 Q& U" v8 ^3 O; V: J 发动机排出气体之温度。由热电偶量出监控发动机正常4 G/ ?% \5 F( }/ g 工作的仪表指示。& H% w: @' [, Y! K7 @1 V( s6 w6 {; s6 g: U6 y [( J9 W% P- m5 a3 `+ U沸点。 , s" M" k! A) ? {: B8 l; ]' s2 I8 }$ s: _' t2 s. R M然能保持系统完全4 [0 }+ I' v( b0 k% F! m 故障消极 ; |$ T0 g; _- g3 P. h一个按照设计一有故障发生,就不工作的系统。 * O7 _ o0 }% ~" w; K英汉对照民用航空词典B OEING' W: d7 B* Z: h1 s$ X6 W# o; H; } TECHNICAL DICTIONARY 56

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