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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 |倒序浏览
英汉对照, {- y9 u+ w. Q u: c7 } 民用航空词典 9 N+ c; r7 ]3 N- H7 B ]波音商用飞机集团# } g. O8 X$ ?! V, M" W& K BOEING COMMERCIAL AIRPLANE GROUP " T, h- M% g8 o3 `( K英汉对照民用航空词典B OEING 9 x8 _, U1 D& b' FTECHNICAL DICTIONARY 16 z" R" K7 }6 [) a. R5 D A + \/ k! @/ `2 v0 _ABEAM (ABM), Beside: An aircraft is abeam a station( w+ L6 B& r2 S9 y0 _+ \2 S' o when that station is 90° to the right or left of the track of' \6 g" x/ a; C0 t1 p- K# J W the aircraft." D5 x4 V( _+ E0 f$ ] ABSOLUTE ALTITUDE, The actual distance the aircraft * t' ^4 J8 X- a/ Gis above the ground. - R2 Q& M9 _' M6 K2 }. OABSOLUTE PRESSURE, Pressure of a liquid or gas & v1 }# z! x2 A- L8 Gmeasured relative to a vacuum. 3 [. U2 L. P0 Z: uACARS, SEE - AIRCRAFT (OR ARINC) REPORTING: j5 M# i8 P3 N: `+ \9 p# Q ADDRESSING AND COMMUNICATION SYSTEM / F' ]* H! a+ x/ G2 mACCELERATION, The rate of change in velocity with 5 i5 H& g* a# f* xrespect to time. : z: F6 b0 D; C7 `: tACCESSORY GEARBOX, A part of the engine, ! K7 k% G! K5 Y) J1 zmechanically driven by a compressor or an angle/ R, a9 H: S1 n- T3 g, D1 T: r gearbox, for driving components necessary for engine 6 J8 n7 B- p( j) S正切, R! r: ~6 ^* K/ h and airplane operations.0 s: a3 U2 W' E7 i 当电台在飞机左侧或右侧方与航迹成90 度时,飞机正 9 k3 M( I6 |9 {3 ]切电台。5 _6 i9 V" h% F% \! {! X 绝对高度,+ Y1 L6 \; k, x9 d' `- o! m 飞机离地面的实际距离。 9 I% y: B% m$ x6 K$ I8 J, W绝对压力, & A5 u& U9 r( B* `1 }8 _相对于真空(无压力)测得的液体或气体的压力。5 H4 i0 M1 ~, r' e0 j# `4 x/ X3 U 飞机通信寻址和报告系统,/ ]0 j+ V) T2 f- t* f 见Aircraft(or ARINC)Reporting Addressing and, J, w# }, |- o+ Z9 \. ] Communication System. l3 j. U+ w' v. g: o9 g! k加速度, 5 {1 ~$ d$ @8 b# u% W4 U随时间变化的速度改变率。 8 i2 z/ V5 `% j5 R6 \附件齿轮箱, ! J4 f9 r# @$ X( ^. m发动机的一部份,由压气机或伞齿轮箱带动,用来驱动% p, d F+ I3 J! \% _( g 一些使发动机和飞机工作的部件! c, C" k" [) w: `' n1 Z4 x 英汉对照民用航空词典B OEING' u# F' u* I4 ?8 w2 v) B TECHNICAL DICTIONARY 2 " p- B+ | L/ ^ I; Q6 a: B1 \ACCUMULATOR (NO. 1), A container with hydraulic " g8 v- t- I9 {/ v# _ts when normal hydraulic supply is not 3 ]8 A: C9 J6 Hvailable. % H" N: ?& i% h5 @CCUMULATOR (NO. 2), In a computer, a special ( N& S* X0 Z7 Y$ {: qtorage register associated with the arithmetic logic unit, 3 r, q+ r7 i: n9 p9 H+ iolding the results of a computation or data2 s3 K/ K( {0 ?+ n' L ACTUATOR, A mechanical device operated electrically, $ V# D' _4 ^' T( q3 j; }' F( D/ \; e+ Phydraulically, pneumatically or mechanically for , e4 l6 l0 P" M# N6 U# M2 Ctransmitting motion between components.% ?& T4 q R0 w; s: a0 o0 u1 v, d ADC, SEE - AIR DATA COMPUTER 8 e% Q" Q0 ^- p/ Z- z1 wADF, SEE - AUTOMATIC DIRECTION FINDER 8 a1 Y( w, w/ z* `' {* dADI, Attitude Direction Indicator, An electronic display of ( L0 z7 s7 k' I0 C5 xairplane attitude information in pitch and roll. # ]% E( [$ G9 r. N- X蓄压器(NO.1), ! p* Z1 N* Z& Y- @! J含有靠干燥空气或氮气增压的液压油的容器。当没有正9 E9 A& {; {" o. g4 l+ E 常的液压源可用时,该容器可用以驱动部件。 1 c' {1 ~3 _ Q5 T存储器(NO.2),7 E& t! y+ J: @8 s/ C 计算机中,一种与算术逻辑组件有关系的特别存储寄存4 Z! z1 J' Q2 _, ~8 S 器,用来存放运算结果或数据传输。' x6 F1 t5 s2 [: ]0 |& v* C# k2 x1 o 飞机状态监控系统, * f% o: `& W- v1 x( h0 z/ `" _见Aircraft Condition Monitoring System/ A: f* k! Z+ q9 Z- w+ i) z fluid pressurized by dry air or nitrogen for operation of4 i6 q: a- `" X: p5 G7 V componen 9 o: t6 H- E5 m* \a ; H6 v/ t9 ?' e8 ?- d4 @ I: S) [A 6 {! ^. T! e6 j2 ~8 i) R0 n0 Ts / e# U+ h. X& [used for h ^8 C0 _3 k$ x i4 ]% Dtransfer. 8 K$ N4 C0 W( z4 @1 |ACMS, SEE - AIRCRAFT CONDITION MONITORING1 S1 x3 a9 Z- O SYSTEM .1 p- [# d/ l' s' e1 y! j 作动筒, 0 X3 Y+ R+ K7 J& Z- |" I$ S由电,液压,气源或机械驱动的机械装置,用于传送部 ; L& a$ V6 c# v' m. a. h$ q+ R件之间的运动。+ a+ \& Q2 J( E1 t! E 大气数据计算机, 7 V c$ ^& w4 F4 N见Air Data Computer. ) d" J( D5 i/ _7 e5 K自动定向仪, 8 j: `$ X i. ~( x! \$ M9 t见Automatic Direction Finder. 4 i3 S5 p2 U+ P- S, _姿态指引仪, 1 V( q1 u0 |1 P& c/ \5 V9 t用来显示飞机的俯仰姿态和坡度的电子显示。" x) [" K! Z2 r+ ^7 g 英汉对照民用航空词典B OEING 4 I: L# I2 Z3 R# ? {. k! p. G6 vTECHNICAL DICTIONARY 3 a# O3 y% f' O; H3 KAERONAUTICAL RADIO INCORPORATED, ARINC is 5 t6 o' w8 [% |,' M* k$ {" O; G. S nufacturers, and foreign flag airlines. ARINC* d& K$ b* C5 T; F2 S0 B evelops and publishes standards for electronic : j& k* ^* h, u& z* j9 _quipment and systems.9 {5 x( Y" H' p- `5 v7 A GILITY TUNING, The capability of the DME to % T" |' B. c! l% m9 mlternately tune between two different DME stations in2 Z) s3 ~# Q; C, B# l" m rder to get two distance readings from one4 b9 G. L9 k* i) M* |9 d, ] T) M terrogator. + ^( J" e& X5 ~# Uge. @; ]- c1 C% h# v/ u% i( h2 d7 R" Q ILERON FORCE LIMITER, An electro-mechanical8 W0 w- ~1 B) o& }; i) g IR CLEANER, A component in the pneumatic system' }0 Z# O g! T$ z. H3 _% o' l upply to the air 3 f2 n/ Y2 k: Y- g: Wonditioning system. & M U$ [% L- R. ~, P8 d" D5 M订并出版 4 E# B+ P, @ A9 E! N子设备和系统的规范。 0 R0 M) x- {' b4 C) k& k& v$ ?4 I0 r快速调谐, 2 V7 ]& b3 `- L( t$ M机载DME通过交替调谐两部地面DME电台以测得来自 : `( L7 g( E. N9 H. ? p# ?同一台询问机的两个距离数据的能力。 9 T; N$ ^# S7 n% [- L7 W1 e. T. ~& C. _翼操纵力限制器, ' ?* M7 h9 b, \装置。在自动驾驶工作期间,用来限制驾驶盘9 x. J/ z' F' c6 ?" n. r3 E1 O 气清洁器, * ]: J% f( `0 ` Y& X部件。用于去除供空调系统使用的发 , l9 `, _+ C' i" va corporation whose principal stockholders are United) P, Q- C1 l; w6 v# s/ _4 @5 ?- `. z States scheduled airlines, air transport companies # {' c) I/ t$ U9 M+ k: Qaircraft ma/ d! | p s7 T d6 A* p% D. @( d! Y' l e + |4 A0 ` z' P- k0 {A: A7 d+ j2 K" s6 w0 B- j; x- q1 @ a 6 m" G$ l# v7 D. N) \' Fo . G1 y4 ]+ k) yin 4 b t# T9 R+ ?, J- V7 F/ Q. tAILERON, A hinged moveable part on the trailing ed 0 m* h) _# c8 o8 g: Pof each wing for airplane roll (wing up and wing down) ! N, N- N; c1 R0 a6 m9 v# rcontrol.: b: R' G, @/ f4 ~0 J A 3 o8 u5 E2 x( S4 C- J0 H- sdevice for limiting the control wheel movement by the9 D2 A- j$ k- D autopilot during autopilot operation. , K; q" L* f- \- t# EA6 Y# V/ H/ L0 F6 z# L for removing dirt from the engine air s 1 M0 Q2 X z4 Y% ^0 \c " {* C' f/ j+ S$ g* B7 o航空无线电公司,% N, n# W% ?- U0 l# n. \% r" U 主要股东为美国定期的航空公司、航空运输公司、飞机* H* ^9 O6 ]) n0 u6 U 制造厂和外国领队航空公司的组织。其目的是制" a6 ^* J3 \7 ]2 t3 s) i1 \3 l. ~: L+ H 副翼,. {" |/ k# r- r 铰连在每个机翼后缘的可动部件,用于控制飞机的滚转 - B0 @8 j- ^' [+ U) x* [# P(机翼向上和向下)。) l, O* _8 O" {1 F0 Q. V0 N, a8 b. f+ h) C 一种机电 + L# x" l( _( ]' o的动作量。 . x0 P. Z! v5 S$ L5 C. c5 \: E3 B( d$ E5 u* Z 气源系统里的一个 4 S) v+ `& Y7 ]. q; N* [+ T C. m I动机引气中的灰尘。% V* Y. ^' L( d9 ~5 l3 r 英汉对照民用航空词典B OEING6 V/ J! n) ], ~) v# Y TECHNICAL DICTIONARY 4 6 |6 q5 U* F# u% ]5 d1 cAIRPORT ELEVATION/FIELD ELEVATION, The& z7 f5 r3 z2 L( F1 b5 u highest point of an airport's usable runways measured. ]( M' T9 D) I. N" B, N in feet from mean sea level. In a few countries, the % j* x% l7 A3 C* r3 {; }airport elevation is determined at the airport reference 4 @8 d# O* x( i9 c n- s' k/ U3 Gpoint. % S# {. ?: `, \( bAIR ROUTE TRAFFIC CONTROL CENTER (ARTCC), # G7 Y& V3 p# t9 p/ H( yervice/ v `" I' h6 q8 F ase of- Y# {; m% |. g3 z) F* t; S us flow of air traffic. 7 ?8 c f& T* j3 dIR CYCLE MACHINE, A compressor and turbine on a ; N3 T2 o- s c/ U. d' a% x9 pommon shaft for cooling the air in an air conditioning 1 S+ V# ]* [) tystem. The air is cooled by expansion from high to low 9 N: e9 }1 W) Q/ {* N* v) e7 G/ Bressure across the turbine. The compressor is driven' n) ^- G! i6 M7 x* @ y the turbine.* |2 p2 n5 x' z2 C 中航路交通管制中心(ARTCC),2 v8 ~2 r& D: `6 e 域范围内使用仪表飞行规则飞行的飞机提 ( {+ a* q$ _5 O/ e管制(ATC), R- M+ @+ c8 X2 f) F 涡轮冷却器,0 N/ E* q. Z' t/ k& `6 i 是装在同一的压气机和涡轮,用于冷却空调系$ C" F/ B$ b9 x b d 统中的空气。气经压气机压缩后,由热交换器移去热量,, O$ V3 Z x* s 然后经过涡轮令涡轮带动压气机。通过涡轮之空气,温 9 Q7 q) C* `, H. g度下降。 * a V( ~+ Q( z& z' UA facility established to provide air traffic control s2 q' k1 @0 _- n* T5 Y/ w to aircraft operating on IFR flight plans within controlled2 [' s L- R% t( n, O [! g* j$ b airspace and principally during the enroute ph 2 n' m) t- r! q: \flight.+ s: u* d1 _0 g6 |; b0 P8 h$ d4 E AIR TRAFFIC CONTROL (ATC), A service operated by - y+ @5 g1 Y5 m1 gappropriate authority to promote the safe, orderly and / g) J. `. i# B9 q$ ^expeditio! Y& G4 v3 S5 J O A" ~. d9 s2 J9 e" ~ c3 |6 C( S+ k+ |# e6 k P$ I s 2 |3 @" l t; K6 g" ^$ C' X/ `p7 v3 s; @$ a6 Q$ X8 v9 P b 9 x! c; R' J8 `0 S2 D+ @; `2 ]机场标高,' F% R( p" f# u9 p' M 指海平面与机场可用跑道最高点之间的距离,单位是英 ' ]) K1 r0 |- H4 h: W) B尺。有几个国家的机场标高是由机场基准点而决定的。 3 D7 `' {) H2 D: K2 x' A3 }+ T/ E$ L2 o/ X' K给在控制空 5 O# v# t3 ?+ e* t4 y) q" i供空中交通管制服务的站台。 0 l% e4 h, l: l: j: P. }空中交通; }5 z7 D9 Z a* O: J 由有关当局管理,旨在促进安全,秩序,和效率的空中 - P3 A- O! |6 z& G% ?) { ?交通服务。5 b& S5 A9 _* `; C) x: @ 根转轴上6 k; D) G$ R$ i2 f7 @! z# p1 M. g q- u0 Q( J' S! x* t3 O% P/ `. V 英汉对照民用航空词典B OEING * G: n( p3 r z9 _2 uTECHNICAL DICTIONARY 5

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发表于 2008-12-24 21:36:52 |只看该作者
AIR DATA COMPUTER, A computer which produc , y% G& c$ L+ _+ {2 Z: T j* ~data information, such as altitude and airspeed, based% [( `1 Y" `( P+ N$ d on pressure and temperature measurements. ( Y* u4 d1 }, P8 u- ^. q: d% nes air 2 ?2 S ^+ ]/ \7 m1 O a9 R5 CIR TRAFFIC CONTROL, A system comprised of. d4 Y+ U) m5 h& O ] round and airborne components used to identify, track & r( k: r) X# Q% j$ b5 M1 vOUND SENSOR, An electrical device operated + R1 V$ a. e( Z6 ?# j0 U4 U% N' [8 v% Xy the landing gear, which transmits on ground/in air 1 V0 Y- v; X1 |7 G2 P3 } Mformation for system operation in flight or on the r' z1 O+ Z! y3 ?7 Wround.$ E1 p) {4 `2 P# y. i& ` m IRBORNE VIBRATION MONITOR, The AVM takes Z& c' i4 K# ^9 S( h" te signal from the engine mounted accelerometer and% n! L3 k) g1 @. \: l$ Y alculates the vibration on that engine. 0 v* B; j% Z: l8 f" Jcorridor equipped with radio navigation) L; f5 C' r- l+ {4 H! a4 c aids. 8 o' `5 T$ e A, DAIRCRAFT (or ARINC) COMMUNICATIONS + L/ Y1 y3 v2 J. _- r) q" z# F0 HADDRESSING AND REPORTING SYSTEM, An ! [' }/ y7 ?) I% Jaddressable digital data link system which permits the3 _. F8 L# |2 p9 F1 D w' b m exchange of data and messages between an aircraft- p- u/ N K. K6 C" T1 e- L5 c and a ground-based operations center over a radio+ }' h0 w" x: m8 M network. 1 d; R% K, i, x/ q+ @4 {8 DAIRCRAFT CONDITION MONITORING SYSTEM, A 4 F& M5 a% H* nsystem of sensors and recorders to monitor various% h% h+ {) B4 @& F9 M* `: {7 Z airplane systems' performance and status. ! Y$ d. r: x# [: c+ m/ E机,6 `6 p6 r% P7 N 中交通管制,' U8 M) j! T+ F# I 一个由地面设备和机载设备组成的系统。用来对飞机进 ' c+ S+ A' E( }8 W! T. R: f- C地传感器,, ?$ ?1 ~2 c, Y+ ^( M 一个由起落架操作的电气装置。用于给空中或地面的飞 * M% v2 ^) c# D+ J' h3 A5 T f系统运作传输地面/空中信息。(有些系统只能在地面 . H' s ?& f& o. l$ ], @# k" n用) - c; n- n. y X5 Q% x7 w6 c载振动监测器(AVM),. S2 m2 `! {+ x# [. s& I l1 ?8 p AVM从装在发动机上的加速器取得信号后计算出该发; C, l$ D4 s6 |1 |' J 机上的振动。 4 m: l2 | g5 u* \6 F9 U9 k- u式建立的控制区域,内有无线电导航设备。( n9 X3 D& r T% X! a% v: s6 _ 飞机通讯寻址和报告系统,) ^( c1 _7 }& {3 a: B8 S4 `, y. t 有种可寻址的数据通讯系统。利用该系统可使飞机与地 % R( O; q; e5 E面操作中心通过无线电网络进行数据和信息的交换。 : h4 l9 ?( ]" ^1 I! Q$ B' o飞机状态监控系统," w% Y) g/ a. ^# j! n! C: e+ e( _ 一个利用传感器和记录仪对各种飞机系统的性能以及! @7 N7 w7 y8 o4 F, R; X 状态进行监控的系统。 ' c+ b3 ?; U3 H; o+ nA 8 L0 y& B/ w; \( G, gg( Y! t1 @, g3 j& _ and locate aircraft. 9 F; G0 N0 W4 hAIR/GR 7 Z" [8 z' T/ h- k0 r5 `8 P3 @, `b & A+ O# f. T! u$ ]) ~in + l9 R! X! _+ b2 c z% Z# Vg 3 G; G9 C3 u4 V7 {- j5 pA , s# J" ?1 K, Oth& ~9 y- Z( Y. q# T( T( X3 p* b( \ c [. ^' V. z B. e AIR WAY, A control area or portion thereof established9 L, P9 J$ h( F' T2 F( z in the form of a 5 {4 O( s( u( V, s8 {' W大气数据计算 5 n+ @0 K( W, Z+ G+ X根据量取压力和温度而产生大气数据资料(高度、空速 / O* g$ |7 g- H5 `" [7 r z等)的计算机。 4 q9 s6 H$ ]2 d$ f( W* H# ~- }6 L% H. f/ O1 B行识别,跟踪和定位。4 h, ]7 {+ Y- l L8 W/ W j% ^! K1 z8 q) b7 m9 n( R; q: T: b4 Q$ T8 b5 D使0 N7 g# x. X% u% I3 Z; T! k, M5 L. ^% I; T' n2 t2 }5 M& M6 w; }* s4 H航线,! ^ L* ~ g: [2 T% `6 x 以走廊形4 L# z9 T* e4 d0 {0 o' i! Q( W 英汉对照民用航空词典B OEING9 a q# w$ q6 s& l TECHNICAL DICTIONARY 6% J ]* H% R5 ^: F4 L1 k8 z; J AIRFOIL, A surface designed to obtain a useful reaction, J" `, G* @* ]/ a* A such as lift, from the air through which it moves. Wings, * T3 p! w9 c+ ~7 Rstabilizers and control surfaces are airfoils.9 e" u [' ], e; ?5 e) V+ F, {0 D' L# ] AIRSPEED (IDS, TDS), The speed of the airplane ( l3 Y- A6 ]" Hrough the air. , H* S, P8 `4 L9 YD INDEX, An adjustable pointer on the( q( Y' M( {) r irspeed indicator.. T Q/ p+ a' W. C$ v2 t3 W and legal ability1 v: O! D, K: e. E fly.- s; E3 E* X5 _- ~1 Z( q' f7 | m, for example, the procedure for finding the2 P! X) L. ?" n A* Y: y7 S quare root of a number. 0 x3 ^2 k8 l5 Y: Y) ^3 a6 }& Oy : Q7 d/ U' p/ T! d) c8 \4 W m# `* Dre, wind,, K4 j$ _& h: V9 U5 n( t and aircraft flap setting. 9 i+ y P& v# p4 f是翼面。+ |" _% u8 W0 x8 i" Z7 P% U9 w 速,) R9 @/ g$ U+ m& |) O, E) U 飞机在空气中运动的速度。 9 I! d- t. `* @: R2 e; x; R Q( M1 H6 I, ~6 ~* C& { C 在空速表上可以调整的指针。; ^3 | D8 m, i6 M/ `) ~. u 机械飞行能力、和合法性的飞机状态。 0 S/ s0 ?; R* _: f) t一步一步的解题方法。例如,计算一个数的平方根的步4 \: X4 H& A& E* b2 a( F) d0 ]7 F2 u# z: T8 w" ^3 K8 n7 h2 d8 d 资料的法定文件。 " A0 m& [% z3 O2 T0 o翼位置成函数关系。0 [- e4 Y2 `- u th1 F! Y1 _0 P2 D% j AIRSPEE X- O, a2 C, u( ]4 | a% z4 S( |& U/ Y9 ]8 @ AIRWORTHINESS, The condition of the aircraft with! g" q# L6 }9 M- b1 h& i) d respect to its aerodynamic, mechanical, 1 L# L- M' H6 E1 Ato 4 x# L! N3 U! _- ]9 bALGORITHM, A step-by-step procedure for solving a3 M& W- G0 A I0 z* T% L# L! g proble + P6 \+ B- p* m" q, t' L( _" Hs 0 d/ ]! u9 F t, n/ @9 _AIRPLANE FLIGHT MANUAL (AFM), The legal : u, M* q: T$ n% T& ydocument containing performance and operating limits, 4 v3 } e8 m4 M& p/ {% z9 [operating procedures, and takeoff and landing b: E6 S: Y( P6 W9 Z6 B& O performance. $ U9 U" Q6 |: G6 h" `; z8 k2 iAIRPORT ANALYSIS, A comprehensive set of takeoff 9 z7 Q: [* n! f8 U' I, }weight limitations for a given airport runway, generall" u ^2 G" q, o2 ] presented as a function of airport temperatu, }) w2 k/ p0 G. ~; M9 W/ \ 翼面,1 e/ I7 F4 x. c& Y; L' i 用以从气流中获得反作用力(如升力)的表面。机翼,3 G. A3 H8 |) m" M$ Q ~ 安定面和操纵面都5 X) s3 N2 Z2 {( ]. `' r+ u' s! L- ?0 e* B+ @' h* f' P空速指标 + A' v5 }: _$ I9 W1 x0 C8 K* D适航性, % {1 _0 y/ ?0 l) v+ i1 p有关气动能力、 / A' ^* f! K7 S! n1 J" M演算法,! s7 o8 a- q" H5 ~6 H# `3 h3 y* J7 @7 M; E$ C& W* c飞机飞行手册(AFM), 9 g) c9 M, h# Q! Y# W/ w* W8 i包合性能极限,操作极限,操作程序,起飞和着陆性% U9 p8 ?4 M* w/ n& y6 I) L$ [2 S$ h机场分析,9 N) O! }+ }& r: R9 g/ V" V" _ 一套针对给定的机场跑道的详细重量限制资料。通常与 ( y5 `7 B; G0 j机场温度、风、和飞机襟 1 J) p) z5 b1 |英汉对照民用航空词典B OEING& V3 B" E& g( j) j9 X3 ~8 j TECHNICAL DICTIONARY 7# l# P) U% w( z1 `" { AIRSPEED BUGS, Adjustable pointers on the airspeed 6 k& O8 G4 d& i. mindicator. 5 M* j% s5 Z6 R6 E5 \ALLOY, A mixture of a basic metal and small amounts8 u+ F4 D) i6 @+ x" F" j* e f other metals to change the properties of the basic 2 \5 v2 Q5 x5 y7 ?etal. . C! R! h8 C0 O% g7 bMinimum airplane speed. 8 C% @$ l5 v1 ^4 Xe of$ _* J$ {" o$ B) o7 t itting airplane angle relative to ~0 r5 Z$ M5 s( [ ^& zirstream for the stall warning system.9 ?" Z, A7 n* w8 X3 O& F& E& x7 f/ @ another.! x5 d( |6 e. c2 R LTERNATE , An additional airport selected during * B0 K7 D1 x0 r& n4 @: j8 k1 \+ ~# I6 e5 I7 m- W) J合金, 7 X& R, ]- ]8 _4 o0 m在金属中加人少量其他金属,而改变其性质的一种金属 ! _9 C: `4 D" \; ]/ W合物。 6 i# }( C# N' E4 C' X5 ]飞机的最小速度。 . C: J' ?0 K# g速警告系统传输飞机对 1 Y9 y- n; x; r. m. [; w% b% G流的相对角度。 - P) L2 J O+ W x由一个状况改换到另一个。 # P6 t# ?+ ^5 C: `% F降场, ; C, r9 a0 D- a1 F* h) @划时,除了目标机场之外,所选的另一个机 5 k2 T- Q" ~' P; Q, F; `! G, ~o & X+ C6 W5 a% v+ w( s5 Jm) ^; K# C( l" }; r/ q3 M ALPHA SPEED,3 l, z1 S0 i8 X+ ^. | ALPHA VANE, A small moveable airfoil on the sid ( M& \/ D# X1 Uthe fuselage transm : q6 }9 p0 B6 W: G) R ba+ G% v, ~/ o2 k. b7 g ALTERNATE, To change from one condition to9 O4 E' L8 T, D A" W* W& K3 n1 i8 Y+ B0 b flight planning, usually near the destination airport, to be 6 \$ p7 |' k: R0 h, f' v8 D1 |used when it is desirable to divert from the original* l8 D$ R6 O' o destination airport.' K. J6 V* ^/ }* H! F. @ 空速游标 ( \" E$ B1 i7 O B, a6 {: t) s& [空速表上的可调指标。 5 X/ |0 h9 { x; ~) O) _& Z8 v7 B. X2 K4 o* k8 y5 C迎角速度, " w7 N/ t/ q' P迎角叶片, - W+ G$ B1 i, @$ ]# x$ W* `; V) N* {位于机身侧的可动小翼面。为失) m) D o2 q$ A5 z/ r; ?- X- O0 i. A8 R9 P& f0 f 交替, 0 |7 B1 V0 K3 m. }2 I9 y. O& ^! t& P- p# S& F$ ~制订飞行计 $ Z3 G0 R7 t0 Y( J4 X4 ^3 g5 F) w场。通常在目标机场附近,以备不去目标机场时,改降之 + v5 ]" ?+ D/ i9 r; c& H) m0 B4 q用。 ! ~, g' i' K4 N, P: N英汉对照民用航空词典B OEING$ a* A! T& i6 a! y8 R TECHNICAL DICTIONARY 8 @9 p" p \; v, _ALTERNATE AERODROME, An aerodrome to which% }' H( N( ]8 _3 e# P1 e4 s/ T an aircraft may proceed when it becomes either 6 q! a. o5 P3 ~# \" q9 Opossible or inadvisable to proceed to or land at the 5 F% W6 I3 r7 Oerodrome of intended landing. ( q1 @; }) W- r' t, nTER SETTING, The adjustment of the altimeter u O, l: }, O9 K/ haccount for local variations in atmospheric pressure. Q7 y L; Z. ]4 I9 V LTITUDE ACQUIRE, A digital flight control system & O# G" k; F0 H5 lode to transition from climb (or descend) to level flight. r3 Z; ^8 t |2 p1 | LTITUDE ALERT, A flight deck alert occuring when the. ]2 R# i5 e1 l8 E irplane approaches or departs a selected altitude.) L" B+ X4 l+ H6 A. K( a% r5 h LTITUDE CAPABILITY, The maximum altitude at / U- c8 o; F' Hhich the airplane can be flown at for a given thrust, 9 g/ e% Y1 O) c$ Q3 O( r8 I9 p3 w/ ? Fpeed and atmosphere condition.2 u8 b) q8 W) ]7 M LTITUDE HOLD (ALT HOLD), A mode of the autopilot , c7 e& l& u- `: s7 b2 ?r flight director to maintain a selected altitude.! ]8 m3 u% [; }! I irplane's altitude during VNAV operation. 1 V7 Z" l+ Z5 _! V8 F机场着陆时,可作着陆使用的 8 m( k1 ]. @" [, s3 U场。8 `0 L2 k' i I) d3 r2 d7 j+ _3 u. U% @0 r7 Y6 Q! P/ l根据当地大气压力变化而对高度表所做的调整。9 Y" B/ @5 P3 x+ q. } P 一种数字式飞行操纵系统,从爬升(或下降)改平的模' i* q; |0 w7 H& b3 V( a6 E( H* i% u; |; _6 D 度警告,4 }+ H% I A4 R0 S 当飞机接近或偏离选定高度时,所出现的驾驶舱警告。 2 I3 f n/ {0 s% Z5 L高度能力,: u. K G2 d* J: T; C 在给定的推力,速度和大气状况下,飞机能飞达的最大$ q, }# h6 M) p4 z 高度。 9 ~* F! L0 v' U$ F4 |. |4 _1 U高度保持(ALT HOLD), 9 _( b `$ A/ q, b. S6 g& Z6 F自动驾驶仪或飞行指引仪保持在选定高度的一种方式。. Q; R) z" m6 y2 |6 j* e* b; d' B* s/ I; o% @1 C* W员对飞行高度的控制。6 i) W$ a! P( R( m( U9 s im5 C" }6 ~9 w Y' L- V& }' Y( Q; T a) O8 C2 Q+ K" K. G4 v% j0 I/ U ALTIME) F" X1 I& W# r2 E3 c to # X1 x' j) R5 s0 VA 0 W( e0 f3 R! b! R$ N! cm . z/ c- c6 @# J! V$ P& pA# f) ^% N- Z8 d; t" ` a & a/ Z9 S( U- o4 P3 N; M: A+ cA " c/ N0 r8 h6 J- f: C# Mw ' |& v* z9 V6 O' s! f2 Is+ a E+ W7 r+ z: l! a A " \5 P* f/ Q. ~7 fo / L) i% Y+ j4 y- nALTITUDE INTERVENTION, Pilot control of the/ q0 i# R& k' x% m k2 I a & r. c2 f) _: F1 h2 T' B+ mAMBIENT, The surrounding atmosphere.3 r3 ~7 o7 `% Y, z8 V2 o 备用机场,! X/ _: ~8 Q6 Z% N 当不可能或不适宜在预选 - t$ E! m/ u |' E* G# @0 H! H8 @ w4 u: K高度表设定 A* L! z6 P+ d8 |8 A, f高度截获, % ~" m' A% T& _' d( _. i1 A* k/ ^; ?' `4 }4 N) Q5 p9 D) a G7 A; x" _: p; f J高度干预 " }* c6 n/ Q* L在垂直导航工作过程中,飞行. U, [0 g& V) R4 `) G" v9 ? 周围环境(地面气层),* G9 |7 V/ Y% G7 k# K% N 物体周围的环境(特别指大气)。9 g* D, T9 i. s% u 英汉对照民用航空词典B OEING / E# L8 g/ A0 v5 @3 [7 gTECHNICAL DICTIONARY 9& }$ S- b* C# \7 [3 I: f" z AMBIENT PRESSURE, Pressure of air surrounding an' ?+ H" L2 |1 d2 [6 V object, measured in pounds per square inch (psi) .' f, _* `: `" l; _4 e MBIENT TEMPERATURE, Temperature of air q/ y) W. {3 ]! t& cmpere.! U& Z3 F0 W* G urrent waveform. 9 y% |: `9 a4 O; g: }, pg an 7 N' }! b: y8 c7 inalog signal to a digital signal.. F, L) l5 C7 @. ~0 A ore inputs . h4 I3 S( l$ ?" B. ]f binary digital information and one output. The output- |' v! J @' J: N) X# I- D 1 only when all of the inputs are 1. The output is 0 9 r) j4 A. \5 h# L/ h0 vhen any one or more inputs are 0.4 \& Q$ I9 \ [. C; Z 面气压),, d0 ?4 P& A* g& ?% O+ `0 W) M4 o 境温度, 3 _/ A6 q2 u& k; B/ v' ?/ k2 t气温度,用摄氏度(°C)或华氏(°F)来7 b% o/ L0 v5 P+ Z! B6 d* ^0 \: ~; ^8 o6 N+ Q/ |9 K电压或电流波形的幅度。2 _) g7 m7 H0 A& g 性变化的信号来工作,或产生连续性变化的信号) D1 T& a/ a, N4 d! |% G1 g 统。 ' }8 m m+ N2 b/ \+ m将模拟式信号,转换成数值式。 . k) ?5 B+ M, x一种有两个或两个以上的二进位数字信息输人,一个输 + F$ x9 m+ y( P7 I的装置或电路。当所有输人为1,输出为1。当任何一个3 U8 }0 f( s9 s9 z8 ]; F9 \ 一个以上的输人为0时,输出为0。: p% I3 z; F2 Z4 i: E A ; T' s, Y; |0 y+ p9 i2 Xsurrounding an object, measured in degrees Celsius & u3 B- {1 T! K2 w(°C)or degrees Fahrenheit (°F). : ^" q9 N {. BAMPERE, A unit of electrical current. One volt across $ _7 }- a" q3 T' K" a8 m6 Z6 xone ohm of resistance causes current flow of one * `% K% J% k( N! B2 o* G# I" Ga- N. a( m1 }2 _- K AMPLITUDE, The size or magnitude of a voltage or 6 [' v! ~! M" v! jc 1 O9 N( X7 g1 |) wANALOG, Quantities or representations that are: F, W0 [' [# L, k8 c" U/ u variable over a continuous range.% b! c' T% t$ }4 M2 A! L ANALOG-TO-DIGITAL, The process of convertin ( B" b, _" m, Z, T; x$ Pa 7 u+ N% i+ r, L* N1 B6 Y. B: ]AND GATE, A device or circuit with two or m : R* j! t$ V% [1 Fo0 C+ k/ X c9 ]. Y3 m$ L) }' Z is q. t& v4 I7 S- {, A7 j7 R. N2 \! d w ) x- ]% c6 Q- T: s7 T% |6 Z% ~环境压力(地 - C2 b' H/ T) q$ m7 [物体周围的空气压力,用每平方英寸多少磅(psi)来 6 R' ~1 E8 }* w; @度量。 " j3 L- b- P6 V, V% j D: l& U4 T* x, r0 |物体周围的空8 c# p! V5 n0 T; r& e6 q 度量。* y' n* A" `( G9 N- u0 g! ], l 安培,' s, l+ J" I9 y8 w5 k8 D' Q 电流的单位。1 C# u; l7 J* n* f 1伏电压在1欧姆的电阻上所产生的电流为* \' E6 D& K5 o7 b7 }; {5 D, O 1安培 5 s) i- S4 @( B; h [/ t, r% A振幅,7 ?/ s x; h- s6 X# @ 模拟式, / u! Y! s5 i; E+ V! U" ~' n+ f用连续: O& i M' S0 A" F7 x0 |1 A5 i( C0 k% M2 ]7 i: N# V 从模拟式到数字式, f( S& i: S! D& D( _' y: {! _与门, 5 S8 e' A( \6 w+ |; {3 z% Q$ b; k7 Y# a7 y9 ?0 p, R' A: A2 d$ v英汉对照民用航空词典B OEING* h3 S$ v' w$ q, i! B TECHNICAL DICTIONARY 10 * f2 L, q- c8 K' U& I$ Z6 s8 OANEROID, A sealed flexible device containing air at low : w$ [" F& K8 ?' N R- }# gpressure, which expands or contracts during change of4 N4 M8 z: X" q" g- b7 R ressure outside the device.9 B8 w ^5 v& s ically 8 i6 F# `) m0 j# G! K5 ~; V* k D- Sr changing the direction) l) m0 B/ T! m f drive. ' ~7 O. ]) x$ ]of the wing chord in 0 ?. F# H! \: Q3 I+ \lation to the free stream airflow as it moves forward* w8 Y9 p& S, p2 m2 w- p% [ rough the air.2 ?# T Q* S/ z# ~/ b al axis of the. i3 T* S. o# D) q1 [ aircraft. ! W" J1 A& V7 e胀或收缩。 ; [0 T5 c! y$ C0 h箱。是改变驱动方向的机械装置。+ `& _) n8 V' F+ F 机翼翼弦在空气中向前运动时与自由气流之间的夹角。 7 J$ t4 @; q8 W% O/ z# N- g" `& o% z$ j9 ~6 c8 qp ' { x0 B; W+ K" v$ {7 uANGLE GEARBOX, A part of an engine, mechan " j- O& T% g, n- \/ E2 n- mdriven by the compressor, which drives the accessory O% z" w4 |9 |3 A2 Q gearbox. A mechanical device fo3 b: M8 k2 g: N, v o# d. m# C3 g" ]6 w3 c2 M ANGLE OF ATTACK, The angle# N1 q4 C8 s' U" t re ) b9 C# b0 Z* Z- P2 Mth0 G5 W0 c5 m& N* v! ^) K8 A ANGLE OF INCIDENCE, The acute angle which the) h" G1 |. W( ~ wing chord makes with the longitudin8 X+ i* n7 _4 R% e 膜盒,5 o3 J( [! G, K) r& `6 L- S+ e 内含低压空气的密封弹性装置。当它周围的压力变化 # D- g7 D2 d$ Z0 h q$ ~* Q时,会膨9 T {- D/ o6 L5 } 伞齿轮箱, 3 O6 C) n! a- I0 C发动机的一部分。被压气机以机械方式驱动,然后驱动 # a- t( T m; x附件齿轮 ' A4 z) m+ ^" E# u7 d4 E迎角,% B6 M# k' F& b2 s/ \( s 安装角," C9 U# A- q4 V! V" Y# t2 R 飞机的纵轴与机翼弦线所形成的锐角 9 b! H2 d) r2 G0 ]/ Z* J+ ^英汉对照民用航空词典B OEING2 R! [* B r5 w7 O' H* k TECHNICAL DICTIONARY 118 t3 _1 U1 }# ^! Y ANNUNCIATIONS, Audio or visual indications used to * ^' x; `: @7 o/ j7 x6 L9 }call attention to an event that has taken place. + h0 N5 [7 @- w) U) @6 a7 gANNUNCIATOR, A visual device consisting of a number : J b7 U% [# S I) ]ly. 9 r) h+ _: w6 R% h9 F6 {ANODE, The element toward which the principal stream- G$ `7 @3 I' ?+ h9 w. N! m of electrons flows.& b0 C1 ~& I% d ANOMALY, Not normal.5 ?; q7 ?7 V6 E6 N% c1 d4 ? ANTENNA, A device which, used in conjunction with a 4 d$ V: v+ d3 I" D1 ?; gtransmitter or receiver, is used for radiating or receiving6 p/ x( m& R4 i radio waves. 9 H) W2 ]* G& f" M1 N4 x5 w- D$ [NTI-ICING, A method of preventing ice formation on 8 i. T6 E: g+ l- ye wing leading edges and engine nacelles. 5 ^- u. u# P" W' @# q8 qNTI-SKID, A system for providing maximum braking" D: w% p& t6 K8 M/ x; {2 J ithout skidding for any runway condition. Anti-skid% U0 n) K6 L2 }" ~: `2 p omponents are part of the brake system. : Y; _4 o5 C/ I7 {告, & y+ V8 h! |' k, ]0 E当发生事件时,以声音或目视指示形成的提示信号。# _6 H# M3 E% {( E 与之有关的电路的现有情况或已存在的 ! r/ \8 M' H) C% j* B/ P6 m# C. w' J! ], ]: O# }& O5 J0 e 正极, ! {+ f3 }- b' X$ f8 T- s- I主电子流向的极位。 H S; K- j9 D 异常, 1 z$ b+ X X Q/ R不正常。 I$ U; V$ m$ m5 u% m2 i! g5 g天线,4 P/ _! [0 J7 B v4 G 一种与发射机或接收机共同工作来发射或接收无线电 . L& ~, V7 ~$ T波的装置。8 F: s6 j5 e" C! l) s2 Z 冰,9 Y: U. C8 [7 P4 E 防滑系统, " ?/ C- ~/ j- J2 K一种在任何跑道状况下,都能提供最大的刹车能力而不 z1 I$ L) A& `7 a. ~9 ?使轮胎打滑的系统。防滑部件是刹车系统的一部分。1 \; R, x* t$ t of lights. Each light indicates the condition which exists9 ?4 R. W. j: H9 V, D( o or has existed in an associated circuit and is labeled " P% I( ^9 B( i! Faccording . Q/ W7 Y- z9 @! l" dA7 t4 }* B- i9 Z& e& B4 f3 S4 J th6 d$ {6 f6 p, p% ^ A) I# ^8 y P. E! a' e9 {4 { w( G) l; Y' s) l" ]2 I c + P; c$ d5 }; Q. {$ K5 `. R' c- h2 A- U5 j4 O2 a) H$ R) h, O. r信号牌, ; j0 |/ K+ y5 R由一系列指示灯组成的目视装置。每个指示灯都有相应 V7 _6 {* C! m5 o的标记,用来显示4 S! m" l% m/ ^" r2 G0 c; a- a& F& [4 w- M9 }+ \& s9 W9 P. |防止机翼前沿和发动机短舱结冰的一种方法。 : t5 K' C; p0 N) I) |英汉对照民用航空词典B OEING# w8 _+ m3 C4 A! T+ s+ V' K TECHNICAL DICTIONARY 12 n: d; G5 f5 Z5 h" z8 cAPPENDIX, A supplement to the Airplane Flight Manual6 i3 Z3 }+ b6 F( c: d5 z tained in the basic manual. A5 ?( z) \. q' {; c$ Z$ j ollection of supplementary material at the end of a 4 W4 M" y( {6 l+ U1 j7 jook. $ H+ ~7 d" M0 }0 Q2 B: c* }of the 7 n- `* k: P- @5 x- jrsion link on the landing gear.: o/ ^8 w1 e9 l3 S) I) z APPROACH MODE, An autopilot/flight director mode 3 R" M+ `, b& _ W+ g6 t# r( x! h Qwhich is a combination of localizer for roll control and/ d2 d7 U& G4 R; N' s glide slope for pitch control. This mode is used when full 6 X! F/ I8 i1 A( V, B8 H7 oinstrument landing system is available.8 H0 l& @. @, t7 J1 r" s* d APU, SEE - AUXILIARY POWER UNIT 3 R6 e. ~5 z2 I3 l0 o' G" lARINC, SEE - AERONAUTICAL RADIO 9 o5 R* n: R( [; Q8 nINCORPORATED 2 p: Q9 P+ Q6 ^. @ARM, To make ready for operation. 1 V# V8 e. ?, K1 T附录, 0 R# X' r \2 z+ V飞机飞行手册的附件,包含基本手册中未提到的飞机形$ `$ ^) P+ [4 y 态的其他性能。是附在手册末的补充材料。 # ^( w3 Q" X3 c1 s0 U: ~% H顶销, Z6 d1 @1 @7 q! M 用于连接起落架扭力臂两部份的销子。 ) w; r1 ?% |; ~: H9 { E6 X3 V进近方式, : c+ C# Y) N2 o' |3 j一种综合了控制横侧的航道信号和控制俯仰下滑信号 , s* h8 I% R- N$ ~' A的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系- I. Y Q( [# {% U6 x% M# R Z 统正常时才使用。7 O1 v D3 t& ?6 {* \7 t: j 辅助动力装置, 8 B/ ]% B9 L1 b E e见Auxiliary Power Unit; I8 }* s: ~7 v5 | containing additional performance for aircraft 2 o5 o2 f. W) o, E( yconfigurations not con ' d+ T8 u* ?4 E' Xc" B0 @, S i1 y% J& c b 8 C1 N7 W7 }( mAPEX PIN, A pin for joining the two sections& O2 r( N/ i& a" E8 m" N M7 @ to / E! B4 \ m y' B. E, k1 p* U3 t! T9 Y5 K: l1 e 航空无线电公司,$ S$ q3 P0 }, x 见Aeronautical Radio Incorporated. P1 V3 a7 ~8 s! V& [# {$ f 预位,8 j" l/ c/ t: c7 J. U; s 部件可以开始工作的状态。9 x# n9 I# [+ |7 I 英汉对照民用航空词典B OEING, _6 n( \; k/ H" O8 v) n TECHNICAL DICTIONARY 13( E" F8 S' J0 |4 G ARC, The curved track over the ground of an aircraft; `' ]) P! E/ @' N flying at a constant distance from a measuring& ~* k1 G6 }; c( E1 K0 `+ p equipment (DME). ( r/ l, A/ _5 K5 P6 m$ H) h {in the limits of self-contained system 1 _" u3 P5 {. O8 Hapability.3 i% n3 O( v" W2 N h tem for opposing or restricting6 ~9 j+ |5 x7 S$ {& `- t ovement. 3 O. R- U: C2 D+ D2 x1 rSPIRATED TAT PROBE, A sensor that measures total! L- m2 c; w; [2 W2 u ir temperature when the airplane is in the air and that; r6 b, r3 Z7 D' E- |! T easures outside air temperature when the airplane is 6 F/ J# U" p- ?& \9 R+ En the ground. The outside air temperature is measured & o- X6 N, b+ w2 ]8 o1 \7 tSSEMBLY, The fitting together of a complete structure0 r' h5 _2 \1 M9 a, C SSUMED TEMPERATURE REDUCED THRUST, The 2 i4 b; r( q& N5 ~, F( LATC, SEE - AIR TRAFFIC CONTROL- R `/ v1 \4 k [6 Z5 l1 I2 I8 A" e8 N0 c 系统中所产生的一种用以抗拒8 D, A7 i+ ^' Y6 {4 b, ^, P 作或限制动作的力。 3 G* z$ u( E6 J L头," h+ G& G) O# N- r: d 用来测量飞机在空中时的总大气温度和在地面时的外 4 x. q2 N9 |* W9 i1 A0 A; o温度。地面外界温度的测量是利用引气将外界空气吸入, y+ `2 W! f! B/ O1 B) ~6 Y: } 头,以达到测量的目的。 1 G+ ~7 c2 U6 ]: r配, 4 v' e1 e3 |% ~8 f一个完整的结构或组件的过程。 9 R* Y# O3 `; a假设温度而得的减推力,$ S" I8 \- }' J 推力设定值时,假定一个比实际外界空气温 " I/ n6 g9 P6 m# {3 `1 {2 T/ a$ d空中交通管制, 7 x8 o( L3 y/ k见Air Traffic Control! K& E' m. Q/ j+ Z7 G5 ` AREA NAVIGATION/RNAV, A method of navigation5 y7 R! E K2 t( j- ] that permits aircraft operations on any desired course ! R1 r- O, N' t! Q/ Lwithin the coverage of station-referenced navigation& H) _6 u6 Y o7 ]- ^3 E2 }! n signals or with/ q3 N) M& k# _: u c/ F9 c; L* {3 g& Z- w# ^ ARTIFICIAL FEEL, A force developed in the flight M- o4 d; E9 R# icontrol or brake sys 1 Z5 V9 a* P3 y) x' c2 Y& F1 um/ T# U0 _2 Z* U0 F5 { A* t& ]: z4 J/ {5 _" j1 F | a5 P$ L4 b0 N; J m 6 p8 q# i. G, B+ U$ u- Co 6 i4 }% Y8 |8 s4 w0 K) @8 R. ~: e7 y6 kby using bleed air to draw ambient air through the 4 N( b- ~$ n0 R7 Y, b! xsensor when the airplane is not moving. # @4 R, c9 ~7 F" ~4 R% CA 7 D# y( }# g; B: f9 Qor unit. 9 N3 L T# b- i6 _A4 l& n3 S2 h% l* {) H7 d9 H) r lower thrust obtained by setting a higher than actual* \' \& L/ K: x7 Q5 w1 \5 ^ Outside Air Temperature (OAT). 2 k5 p! L& T @6 a( X( ?弧线, % P+ Q7 u8 R( K6 K3 u/ F飞机在围绕DME台等距飞行时的弧形航迹。9 _7 F {' d9 I- h 区域导航, ; J: L: b3 Q, {: C! X* V容许飞机飞行在有电台参考的导航信号或自备系统能2 \! c$ P& ~2 g& D# i 力极限范围内,飞行任何预定航线的一种导航方法。, O2 D- t: d9 X; G2 D 模拟感觉 * R! _( \. H0 X+ V% q+ c4 b在飞行操纵系统或刹车 # f7 ]8 `; M1 g: X+ l4 b" ?& B; G2 e6 \9 t9 A8 q 吸气式总温探 2 X( {, ^7 a8 x8 J7 U, m9 C" q: |$ i% S3 K7 K! V$ a# {5 t. a* j; @) ?1 K' i8 B* Y' y! A, l$ y组合成1 W9 [* [7 W7 T- A% x9 z4 m6 F, |4 |, }1 m6 s. N 在选择起飞 * S! T6 K& G* R8 z度高的温度而得到的推力。用这种方法可以减少发动机的 8 w2 k# ^8 N7 G! E磨损和维护费用。 - f2 `$ {# @- R( d7 c. C9 r3 s) D* j英汉对照民用航空词典B OEING . z$ J" S* V) z; [! u; n( uTECHNICAL DICTIONARY 14 0 J* U$ ?! D; |8 I; ]ATE, SEE - AUTOMATIC TEST EQUIPMENT $ B+ C( C8 o, Z l2 l* ^ATMOSPHERIC PRESSURE, Pressure of air due to the 3 m" d' u9 r: S% M6 Zarth's atmosphere, expressed in pounds per square . v" E2 u* }6 ^ch (psi) or inches of mercury (in Hg) or millibars (mB).5 s/ N& y% Q! p8 ]# w TTITUDE, The relative orientation of the airplane with+ V- G$ C$ k3 I spect to pitch, roll, and yaw. " b* ]( x/ l( y5 R: v6 DUDIO CONTROUSELECTOR PANEL, The panel in# {; n2 @$ `% J# R+ ^' P- T e airplane which controls and selects the routing of+ l) K2 b* n5 z$ U udio. 8 X8 E+ a* K, n7 U8 n$ g. JUTOLAND, Automatic landing using the Digital Flight * U P" ]7 ?7 n9 Oontrol System. % `3 ]" A7 X% e. rn.# U5 b# W' g* M4 v/ w) T, O, ^/ s6 d& m# Q M, A system 2 C3 ]# C; K1 V) }omposed of all necessary subsystems needed to guide * p/ k1 |4 I# D! ` q5 _e flight of an airplane. / h1 t& {/ V" u5 }# G6 I6 wEQUIPMENT, System test, T2 g2 R) ]9 a8 m0 D1 V: k quipment that operates under computer control. . W$ H f6 N0 @% o7 P装置,

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e * w ?: v) }& |2 C- ?# Win J/ W8 ]; j* J+ `: v" x A / V, J8 W, t" O* ?6 F: tre" d% p" Q3 T8 m; ^$ R( M+ { A 1 _6 V% A4 c+ p! z8 N3 X2 hth$ K/ D4 I* [6 R2 l* Q a5 j! D3 B# w/ `& B, T A ( S" ~9 o1 q8 @$ X/ fC 5 l' W' z$ a0 ~6 O3 X$ rAUTOMATIC DIRECTION FINDER, A system which 9 U) i: Y5 E& P$ X( odetermines the direction of a radio statio6 Z2 |5 {4 ~: X' K1 |0 v+ b6 d AUTOMATIC FLIGHT CONTROL SYSTE/ e# e) T6 W# W3 B$ |" v2 } c 2 }4 v) x& k7 k3 w; D5 Oth ) c; t4 u( A; n2 J- k# l( A3 gAUTOMATIC TEST( P7 w: P' W# f7 a& C* @; ^ e 6 C9 r$ b& b' |) K; I( p8 b2 `自动测试, _# b' ^0 l' M C8 U 见Automatic Test Equipment. 4 Q' C! M$ J' q+ F, o& p$ Y大气压力,5 R4 Z- o9 l$ A" n+ {/ D/ { J r4 z/ I) a 由于地球周围的大气而产生的空气压力,以每平方寸多- U. J4 x8 ?4 z; t2 c 磅(psi)或多少寸高水银柱(in Hg)或毫巴(mB)来 1 |' z3 I7 j- f4 x% j2 p示。 + [, a7 J* B3 f( K- ]2 H$ u飞机姿态, ! S/ H3 ]1 F! H+ m, l7 x- u飞机与俯仰,坡度,和偏航有关的相对方向。0 g% I, f' ^5 I, _3 [ 音频选择面板,6 }4 g2 d {, C5 L+ u: ] 飞机内用来控制和选择音频通路的面板。; e+ S# @- w: b: g/ ]+ N1 |5 ^ 自动着陆,: P2 V" ~: Q# J1 C7 U, m+ z 使用数字式飞行操作系统来进行自动着陆。8 c o/ D# ~" | 的系统。 ! p; \) i x4 s' C$ d8 I8 k$ I' [7 v! i) `1 A; L4 v' [* b系统所组成的一个系统。 + ~2 e/ E) y' h. K在计算机控制下运作的系统测试装置。 ! @ f6 M, {3 ^( m8 c1 D- ^+ c8 ^1 V5 s& [% x3 L2 j自动定向仪(ADF), 6 R1 z" ]8 ?; R/ q5 X9 y3 L确定无线电台方向 5 S$ Q/ S* ^0 S' L自动飞行控制系统 % c: J: O1 Y, G u8 ?1 }由所有能引导飞机飞行的子 0 K' L, \& I9 H Z& n7 J! o自动测试装置, , r1 S$ j3 R! D英汉对照民用航空词典B OEING / C- A' Q" Z' @! p- {2 \* gTECHNICAL DICTIONARY 15 & O% U6 @) f9 U O2 IAUTOPILOT, A system which automatically controls' d0 w' Z) m0 ?. }( r and guides the flight of an airplane. b1 k- n0 v1 ^. y7 Y$ E% YAUTOPILOT FLIGHT DIRECTOR SYSTEM, An 6 h4 G: d% A5 f& o8 u4 gtor, H- E+ i6 A' m) F& C8 L UTOTHROTTLE, A system which automatically$ {# h }2 F2 b ontrols the throttles of an airplane. : ~( K, B3 s& |2 ~+ `( JPOWER UNIT, A small turbine engine in! @0 j$ D A# R8 \ j e airplane for supplying electrical and pneumatic / ?5 {0 f$ z" t4 a% ^ower for systems operation on the ground or in flight. , S7 ?5 D+ }- z, t+ {* u1 \VM, SEE - AIRBORNE VIBRATION MONITOR% m; y1 h' Q1 j' ^4 P- i2 _ XIAL FLOW COMPRESSOR, A type of compressor5 ~5 i' O2 Q) d# |$ z3 Q h sed in a gas turbine engine in which air passes through * D. v- Z$ k0 J, n$ x4 D: T' K9 uXIS, An imaginary straight line or an actual physical/ \5 J. N4 z9 j: X omponent (such as an axle) around which a body can & j2 ]1 a' g) d9 Ptate.* n+ c, l+ J+ g5 Z# a$ u' X 仪, }' }9 V, H2 S; i( y% X7 p3 J; O, ~7 J$ W4 S$ D. s 自动驾驶飞行指引系统,; O i& v) J% Z# ~7 u) ^5 M 动驾驶和飞行指引功能的系统。' l0 e$ O( W. ]! R6 V8 x 动油门, 1 G4 ~! c5 y+ `4 }自动控制飞机油门的系统。( R! X% ^, D( `9 X 是飞机内的小涡轮发动机,在地面或空中给各系统提供 % p+ I$ X3 p2 z9 f$ g x源和气源。 3 J4 n& j- C: j8 n9 V: L$ e {称。 / E, }$ C, T4 x' U* S2 I9 D+ l) O载振动监视器, & S2 A7 t5 T% {$ }* X* X见Airborne Vibration Monitor 5 ?) B [- _; P; U8 x# w" ^integrated system containing autopilot and flight direc) m8 w5 Z7 J9 T4 H1 f functions. % n/ H) m6 G$ O6 z* S* BA 7 `" |0 J. G k% @c2 ^9 H" w+ j8 M6 U AUXILIARY4 w: L1 f, g2 [: K2 M. F0 S! B th ) N- B* M/ U. u0 [ u4 L* D8 s* Hp ; G! I9 R. W T3 YAVIONICS, An acronym designating the field of aviation 2 S. N$ i1 f; velectronics. & p% e1 h8 j* F7 } VA! f% J" P* S' I% G5 b A9 A* c( _% I& z4 x* K& b u& G$ l$ P' M4 F6 b the compressor in a straight flow, front to rear./ t$ N7 @5 _& s# g A 6 C/ ^& U1 s( E3 \+ O+ \c * d+ Y8 Q0 _3 u0 P3 S \' F! ?' {ro4 P0 k' A5 P% n9 n D, ~2 K 自动驾驶* \) b- T. a3 w, f/ O* _ 动操纵和引导飞机飞行的系统。 + b% `1 J8 q' W' G- }, n一个综合自5 [& f- W" s4 N( V1 u/ c3 i4 ~$ e/ U" c* |辅助动力装置, ( {8 p9 D7 A! i/ ]4 ^( Q+ N. s! u. k1 o B航空电子学, 0 J g; Y1 ?: Y N- U! v: k, z是航空电子领域的一特有名 m( H2 R0 h9 T& ?: u6 T% ]. Q4 m! q- R6 m4 v% d+ s/ G1 g/ g% p4 |; A 流压缩机, " S: N" X& Y1 w3 V& [' l! G一种用于燃气涡轮发动机内的压气机。空气由发动机的0 |' _( T- F N 部流出。: M' |9 S+ m5 Z- u 线, : |! |0 G1 R$ H可让物体围绕着作旋转运动的一个想像的直线或实际 1 S5 y9 u' p) Y# L8 v在的部件(如轴)。 6 Y; A# N w3 p' n) R# j ]6 [' D: V1 b5 t0 o' Q7 L前部轴向流人,压缩后,由后" S( g% a* b' P. F2 G- i+ a1 v$ b7 x( i( J* n: F. G* \7 n2 {0 i英汉对照民用航空词典B OEING* c, l7 z9 v5 Y5 G8 O TECHNICAL DICTIONARY 16 3 r4 V; c {; P! x0 \8 ^' HB % O% ?( p1 s' Q2 u; N5 M6 e; RACKCOURSE APPROACH, An approach to a runway0 C, K9 j: U, w& ]3 l4 K versed. 1 V9 E; v$ L5 f& zown on the EFIS that5 H' f/ h% t7 B. N- z2 o+ R oes not readily change, for example, navigational aids. : S$ J. `7 d: Y( z7 p; W! ~vement in the tank or reservoir. - l' b0 D" L3 q: x2 W% lALANCE TAB, A small hinged moveable part on the % [7 j& H x& _; ^5 aailing edge of a control surface (aileron, elevator,! z1 |. Z0 c; I4 }4 q8 a; {9 z4 g/ v 航道进近,2 F- }9 C7 s4 \( ~/ i+ A9 ], g" _ [ 相反的进近方向。当反航道进近时,无下滑 ! \) F& U z5 d( s, W# H9 C显示在电子飞行仪表系统上不经常改变的数据。例如: 4 C: m5 E4 C9 w/ D航设备。1 `4 J8 [( u; x9 ~- @- _3 u 在燃油箱或滑油箱内阻止液体流动的隔板。& h, @- u! ^" k2 u1 D& [$ { 动补偿片,% M; k7 ^9 l5 s' U& C% n6 c$ @ 铰接在操纵面后缘(副翼,方向舵,升降舵)的可动部。0 [) ]: S- A/ P" f: Z4 }1 s 与操纵面相反,以帮助操纵面运3 {6 M3 k$ x+ l( x6 E0 p B7 a9 P3 Y+ U$ T; H2 C8 f, J which is opposite the normal approach. For a : R" I) j* r; u% K% f) ?backcourse approach, glide slope signals are not ; T4 M. M1 w7 M" b' i- e0 wavailable and the sense of localizer signals must be2 S/ e/ L! R0 v0 a* C" z7 A re : P# a1 d( k9 t( N+ i4 q) mBACKGROUND DATA, Data sh / l9 S5 F5 l3 cd 7 F+ m5 e; ^2 S2 d) M: vBAFFLE, A partition in a tank or reservoir to prevent/ O) W: o/ J4 g! r- l fluid mo # ~2 P3 k4 D4 i/ LB % N$ e! l# f; s: b2 Ctr2 H" d! V* r' {5 ?$ J$ n. F: l rudder).The tab moves in an opposite direction to the' D6 n4 _5 k; w- q& }0 A6 o) u# m0 B# k, ^ control surface for assisting movement of the control) Z1 R; c& o* C; m& s& ] surface.& k5 J8 }: m0 W$ Q, `7 `# a, O- o1 {7 N 与正常进近; C, j: o+ Q6 R+ U 道信号并且航道信号也必须逆反。 ; h9 H! h6 J/ \, S背景数据, 7 h; d e! f" g$ a* h$ [4 U/ C, j3 ^& I6 i7 B; x" b/ ~缓冲隔板,/ R) i/ }* j2 c1 k* _1 Q X: J9 V3 ~/ k4 {) L2 ^+ b 随动补偿片的动作方向 * k! w" @, `* A/ y* ?# w- v动,减小操纵力。 8 f( C5 a/ C4 J5 H) Y英汉对照民用航空词典B OEING " ~ f. U' |3 Q5 M MTECHNICAL DICTIONARY 17" F+ o8 J0 C- Y) M- [: H5 z BALANCED FIELD LENGTH, The field length9 o9 i7 b o. G2 |- ? associated with optimum aircraft performance when) D; v- A, i) j1 N/ _, H, ^: f bstacles are not a constraint. In this case, after engine$ b& `# U8 z3 f% ?) ~ ilure at V1, the distance required to accelerate, takeoff7 H% W/ z2 C& b! r nd reach a height of 35 feet is equal to the distance- N' I* U0 A! h0 z+ S2 y ALLAST, A weight installed in an aircraft to maintain 5 d6 ]# E- Y5 g" F! \* @ALL NUT, A fixed spherical nut driven by the - N3 T% f/ b6 K2 y9 YAR OUT OF VIEW, A signal used to remove the flight1 L9 u x$ O4 u- ~- I' x AROMETRIC PRESSURE, The pressure of air above' S2 z) u( }3 S& |9 l g) or1 f5 F4 m# Q9 L/ Z millibars (MB).2 j& q$ ~' Q2 l: D8 l3 C ATTERY, An electrical device for changing stored8 G' [& H: c& c" n. I. t9 N+ \8 ~7 g 性能的场长。在此 " R$ N/ {3 P5 k s7 j4 e况下,V1时发动机故障,要完成加速、起飞、离地35 $ n5 @( o% o N. y5 s5 d尺所需距离等于相同速度下完成全停所需的距离。 ! H$ s" N- x9 \: P& w" i舱物, 1 \: Y% z: i8 f: X; U+ h重心在许可范围内面装载的配重物。 - R/ s% j. l0 k% W9 K6 d3 [形螺母,! { L* u6 ^: t8 u( L 的固定的球形螺母,用以使襟翼和水平 0 c' z P+ `) Q引杆消失,5 T% k6 ]% \2 T& t8 x/ ~4 e 指引杆的信号。 : R( `. @, D" r3 z4 K压, ) f0 ^4 m4 F* s2 _" |# J压力。通常以多少寸高水银柱(in 2 [' P; w/ a8 ]. H9 e: T瓶,( j$ n, z7 x1 ]) S4 B- x 的化学能转变为直流电的电气装置。 ; R1 \7 K8 Z: ko ; S y- n0 n( e4 ^fa ; i' \/ l; f5 u' ga$ A. s! k: [" o g" l. R, h5 I. c required to stop from the same speed.$ U" P1 ]+ c+ K2 H4 J B " k* P) F( V6 C& f+ B( zthe center of gravity within allowable limits.# b. P5 J6 R: m6 g* I B2 Z# v6 d, _# ?9 O( `+ o% U7 Y0 ? jackscrew for flap and stabilizer movement.3 O) ^' E z( a2 e: p' s. j4 u' X B# N8 d+ I e/ q8 f. Y6 A/ o director command bar(s). 1 i5 E; A v! G1 [. W5 J6 g+ f# oB " K- L" u" V: t: o' n/ Fzero pressure measured in inches of mercury (in H ( w0 b I/ R1 W x Iin$ {2 W- `4 I( _' k" z, l, q BASE METAL, The underlining metal to which alloying 5 Y* E9 W, s+ H, {; t6 tagents or metals are added. # Z( I; v! V3 V KB 5 `$ L2 Z& v; M( X* uchemical energy into direct electric current.& [: D( p2 a9 w; K& f) Q: a8 ~0 \3 p# N 平衡场长, 6 n; T; C8 o) n( l- z当障碍物非限制因素使飞机达到最佳0 C5 x) M% R2 v* l5 }9 d2 Z y' h1 a9 l1 l3 L7 H5 q5 c; s& j) i6 p/ C: G* K! b1 M X4 k. o9 J: z i0 u9 L( s+ F 为保持飞机 r5 N8 t. q8 `4 o9 I9 K! H* o# o6 Q 由粗重螺杆驱动 % |3 z& u# R2 B( U安定面运动。+ H5 }3 {; Y+ O2 a. b0 S) v8 R! q! U, s2 Y5 K2 A* k, T& O$ Z& J用于除去飞行 # A: U5 b4 a9 V* Z& D/ I' N3 Z) H( h) J9 `5 T! ^# S' n9 S+ I- f& I0 f零压力以上的空气 6 R* H- ^ v( ~Hg)或毫巴(MB)来表示。5 e7 {3 d) T8 Y% X$ d 基底金属, " k- u) ?$ C* \9 K, t7 _6 W指合金中的主要金属成份。 - Z z5 w+ y/ N+ ^* W$ `0 o4 j6 K! _0 [: {' v将储蓄 & L: W+ r1 X" w" ]6 b2 P英汉对照民用航空词典B OEING 0 P I; L9 C, w c8 }TECHNICAL DICTIONARY 18 7 e: s% n. c) z6 JBATTER) ]1 M! Y6 {+ a. B' i; G direct cu3 a: h1 r1 Q- ~8 d9 ? power su & y6 N `( l- R1 x n6 oY BUS, An electrical conductor supplied with , m6 M4 `8 U0 e, }7 V9 x9 d7 Jrrent from the battery or transformer-rectifier for0 N% ~. d9 S1 I$ A3 Y7 u9 k, C: N pply to operating components.7 S3 w1 ?9 Z5 k3 \' @/ X CHARGER, An electrical device supplied ) m n7 p& B1 p- i: s+ N* E; r/ x, bith alternating current, which produces a direct current ( w& C# U$ M8 p6 r* ~7 nutput for charging the battery on the airplane.& o& P$ ] X% {0 e AY, A compartment in the airplane structure.6 E* C0 [, {/ d. k p; |7 F# ? CD, SEE - BINARY CODED DECIMAL ; {* l F: r, oEACON, A device which emits a signal for use as a; p% A8 L0 ]1 {1 o/ ` uidance or warning aid. 8 L1 M7 b* a8 i1 u: T& m' G& tBEARING (NO. 2), The direction from an airplane to a9 ], s0 t% p8 }& [* L9 r$ _ ground station. 5 T& v6 V( u H. k! `1 _6 a! Z瓶汇流条,. [ v' V. H. G& c& G- c 将从电瓶或变压整流器来的直流电供给工作部件的导. j, {: z& v0 D5 L2 i% [6 f 体。, ~0 I* Z7 ] W$ P+ R 瓶充电器, - K c5 _5 X: h5 k" h7 P# ]' `用交流电向飞机内电瓶充电的电气装置。带有交流电的 6 X, q8 o3 C3 J; T. ]* z气装置,该装置产生直流电向飞机上的电瓶充电。 ( c1 H) W; l4 k& n7 L5 U) @ Y* f舱,- l U5 l: b) N" G9 Z) _' k- F1 z 飞机结构中分隔的空间。 4 M9 [7 p- Z2 B j% r8 L二进制编码, + U: \* N: Z6 a8 k见Binary Coded Decimal 0 L5 P: f& ^8 E4 yBATTERY 3 T1 F9 Z4 h- Qw* P9 Z: v+ B" w2 | o ' O8 j! y1 H$ \4 A! C. WB7 t5 w2 W8 D) \, A B2 H6 F( ~! {1 {" A7 I. i( d B3 \8 b; E; }8 ^: W: ]8 f7 Z( t g & P$ i/ R; x |8 N; F9 p$ XBEARING (NO. 1), A surface that supports a moving* F2 n4 w% r- T8 ] part and reduces friction between the two.* Y/ R7 ^3 h, d7 O. ` B. x% w! H% C; c% r8 a) H/ i5 {2 E" Q$ U( |0 R- [1 p& A0 _( \9 N8 @, C& V5 |: G6 F, }3 t# H' j; ?9 Q' V- L: z) C8 K! `' u' C4 o) A3 T2 O3 l( @信标,% P' F3 T6 {5 q6 J7 W4 d% Y, v 发射引导或警告用信号的装置。 ' E& Q; _3 Z3 j. L# T方位(NO.2), . ~( y z+ W1 R7 _从一架飞机到地面台的方向。. y! W" T1 B" t$ E6 C# {* M9 f. a 轴承(NO.1), 7 ?$ f, Y2 d. W& J1 _! }$ U+ @用于减轻机械转动磨擦的机械装置。" K( x+ L; O' f9 o8 z7 Y 英汉对照民用航空词典B OEING . c; W+ D2 Q% y I7 ~: UTECHNICAL DICTIONARY 19; k9 D, _' A P8 z# G' x/ U BELLCRANK, A double lever in the control syst & N1 R" U8 p, x$ Dchanging direction of motion. $ `5 g9 M! \- Wem for 4 W4 e) S7 g$ d# }8 U4 N' Gct in the + q T7 u5 r* w0 mneumatic system for absorbing expansion of duct due * a# M1 M9 _; Mheat.6 v; w* w k) y3 O ELLOWS (NO. 2), Corrugated folded or pleated ( Q: O, `5 `) J1 P2 y; w" @, H: Pontainer or compartment used to measure pressure.) n1 [+ O6 g3 f8 `" b6 b$ I1 M7 T! i0 t- n EZEL, The part of an instrument case for locking the , n1 Q0 }! W2 V; H# elass. ; ~. f( `; F8 @+ tIAS, The potential difference applied between two 8 v9 k+ r; ^3 n+ toints for controlling a circuit. . V$ W; S9 P+ n5 x7 x; i3 k4 _BILGE, The lowest part of an aircraft fuselage. A place ( }4 R3 y! x) b3 R M' Twhere water, dirt and other contaminants collect.2 W. E7 R' Q* N7 L, a 气源系统内提供管道热胀冷缩所需要的余地的波状5 t+ j# C7 \* T; j4 P. O 轫管。! _' e5 m$ }% ?0 ]+ q 空膜盒, 5 y9 I. C( Q: @2 |. U h' y" ^/ a一种具有波状表面的容器。用于量测气压。 9 \# {5 W9 B, c& S. P0 s' L嵌沟缘, 5 f+ |% `. p2 L3 h$ u将表面玻璃固定在仪表上的圈状零件。 5 p8 l- t9 ^, N1 c* d压,: D [. r, e$ R' v3 n( {& i- o 在控制电路的两点之间的电位差。 6 S; G1 M3 k8 A6 @机身腹部,/ T5 [" x5 P* Y) E W 机身的最底部,通常水,脏物,和其他外来物集存于此。 2 B3 u' `. \5 `) p1 ABELLOWS (NO. 1), A corrugated flexible du" K/ t; h9 p6 Q w5 S0 ?% F& V p 8 p0 c* w$ e9 E. k' bto 6 B2 \, J7 U% c+ W8 z: nB4 G6 Y1 ^& u) a2 d$ `, i% Y. N2 c c ! V0 O! U& M& l. s4 P7 [B , G7 ]; X8 t# qg ( X0 L4 B0 `' MB 1 t$ Q9 Y2 `# Z ]5 Np4 X( s0 \* C. [* d% j 直角摇臂, % T' ~( |' R: P P在操纵系统中改变运动方向用的双臂摇臂。6 W0 G* L. t2 S" S5 }5 \ 波纹管, ; x: r1 D x% b# m# E) a" N( L! X( q" c9 Z' y0 y, ]8 m7 U* y# V7 Q4 c: Z: M- Q: N ^; m) @6 D {( c! ^- t7 I# N$ G! k" F1 m5 {" W# w 英汉对照民用航空词典B OEING! O/ O4 j& K; |4 X6 l) e/ L TECHNICAL DICTIONARY 20 # d- ~! H1 c3 J9 c# G% XBINARY CODED DECIMAL, A system of coding each2 m6 |7 G, b$ y' G2 q* U, y# k6 x digit in a decimal number using the binary equivalent.6 V& B4 n) X7 B ` BINARY NUMBER SYSTEM, A number system using. U N2 u, u6 U. W s$ V4 Y J4 s- N7 I S IT, In the binary number system, the smallest unit of / X, o) |2 R) i6 `formation, consisting of a 0 or a 1.# U/ X5 H2 N) K- ~' @1 {4 D T ITE, SEE - BUILT-IN TEST EQUIPMENT . h j& p3 G5 JLANK DISPLAY, A display that does not have any + F7 ~6 T" V& C' ?/ \dications, normally due to failure. - q1 y1 `8 P/ iLACK BOX, A container for electronic circuits to record, a. U" N( p( s8 q ight data. 1 `9 |# A# d4 G- ILEED AIR, Air taken from the engine to power various 6 {) ~1 N( \; S7 ^2 Z7 @ircraft accessories.* d+ Q+ E4 a* R# i A valve in the pneumatic system for air ' `) F/ X. @% n0 ]3 V; E+ ]supply from the engine or auxiliary power unit to the: }- T8 n0 s' B pneumatic manifold. A valve on the engine for reducing 8 y6 ]* q$ N8 Zpressure in the compressor section. 5 b# A& w# `' }$ e) ~进制,8 B' K1 Y" f0 U7 p2 |9 ^8 _8 i 进制,+ t3 j+ E4 r7 y# f 一般用0和1)和2为底的数字系统。 ) g/ {! p, b% h$ T- F0 f: E' G特(二进位数), Q) `: {" E% F5 |! L3 R 二进制中的最小信息单位,包括0或1。2 X5 E/ J* Y, V! p 内自测系统, 1 N7 ]) v! s! O9 k* [; A见Built-in Test Equipment 0 @; `) ^; J! m% k. gtwo symbols (usually denoted 0 and 1) and having 2 a6 G5 ?: u* e' w8 i6 A its base. 5 t8 J& ?/ k) o$ N6 S8 ?B9 @' G, v8 }% Y( G+ @- ` in ! w3 e$ n1 k( Q0 _B+ u' x; U) h0 e+ l B 7 m( W& |# b/ tin % s7 d0 g% e2 d5 z: g) m5 G0 k d* nB7 s P" y8 Q2 T- ~9 C& T$ w fl) g# l0 V8 O3 \# H" N5 c B 8 z- n& ]* P: H/ Sa& R& K Q, |5 P& e+ F5 n BLEED VALVE, ' U. i) h; B$ \; r' e二进制编码的十5 W! G0 Y) x: f: d( E4 P; o7 H+ [ 一种编码系统。用等效二进制位数编译十进位数的每一2 z/ |% O0 ]; {1 [" |7 t 位。 9 y$ o! O' C, l s- Y2 g5 z6 W7 y, @# y, r 以两个符号( + B7 E S: A0 Q+ c! L+ R- ~% k8 Q! X; x, G5 o2 t& b' [: ?/ ^( Z& O8 R . 9 i$ t( b5 G: N: o' p$ G白显示,1 S9 ?2 X8 ^6 |6 Z1 i2 o 通常因故障而造成的显示器上没有任何指示。9 r0 n5 B0 A8 O, E* W8 M% F q 匣子,* X0 K9 u# ]: K: m3 ]2 v2 T2 S 装有用于记录飞行数据的电路系统的容器。# F3 D; V& _# k$ L& w3 J 气,* q, @. _8 Z2 j! ~/ T- s 取自发动机而用以驱动飞机上之各种附件的空气。9 w$ i! U- `3 e7 ^0 R* J' Y 气源系统内,使来自发动机或辅助动力装置的空气进人2 `' U- W7 m$ V* l 气源支管的活门。发动机上,用来降低压气机压力的活门。, F' B7 m: Q: ?4 Y* f& O1 J0 p8 ~- C, \ H9 T8 s3 g( P. X7 N# ?" l. @+ L' ~2 S; l7 o$ b* M 引气活门, / m9 M; n# f' d, z英汉对照民用航空词典B OEING & T% y7 N! ?( e* q6 `$ ETECHNICAL DICTIONARY 212 M! U9 S: E+ b- }* Y( k BLOCKER DOOR, A device on the engine for blocking) r$ M0 T+ d! C% | the normal airflow during thrust reverser operation.5 R2 u8 H9 ~( g( Q, E. M4 ^ LOWER, An electrically operated fan for circulating air. 2 `) @. m$ b: \: [3 U1 n; t* ALOWOUT PANEL, A panel in the structure between 1 H/ H+ D; ?3 g3 Fo compartments that opens to equalize pressure in& t$ u0 }% G4 J6 p9 |8 @. C% D e compartments.. I7 v# Z8 T! ?; Z3 W9 y- ]" X4 ]/ b ODY GEAR, The landing gear attached to the * I! C; N! [2 `% i, P9 }; D+ x# zgrounding., X9 A/ x4 U: G* K. n 正常的5 o/ i! U( p G" L3 p' e2 Z 气流。 : X, s1 z% `2 S8 v6 u( q( z8 x I# B2 }鼓风机,' ?8 n x7 K' {- Y 用来使空气循环的电动风扇。+ N9 }( p$ i" N0 g7 w3 T! f9 F2 ? 压口盖, " H$ d8 y+ L9 `# E两个隔舱之间的口盖,打开后可使两舱压力相等。: A" T( X9 t5 p$ ~2 o 身起落架,3 u- y+ J9 N0 [9 J0 W4 s5 q5 L- V 身构架上的起落架。 $ l3 z( d5 H I- g; h$ iB ) K4 E: N0 J' gB2 l2 g1 E6 e% ^7 e7 s$ H+ P0 T tw & | U4 T- e# [ r( P- B# D3 ~3 q* ath6 \3 z7 q6 Z4 G1 i9 d5 N, b B- l! O9 P( ]" [+ F fuselage structure. i& L! I' E" j& k1 Y/ \BONDING JUMPER, An electrical connection between 4 a5 W% C' I& qa component and airplane structure for electrical , a) {& P, |# ]4 X G阻流门,0 d5 t2 [2 A+ _$ t- k2 a, p4 k 发动机上的一个装置。在反推工作时用于阻挡 / n% i( G" e' s) }( r% k; c/ E K. G1 V. q% B; j7 `9 f- X, `! X& o 装在机 4 @& ~6 {* p. |4 ~$ i搭接片,8 A: v: [9 |: Y3 [- u 连接某个部件与飞机结构以形成接地的电接头。 3 \- \# S( `- C/ H. V/ ]0 l( ^! e# x. q英汉对照民用航空词典B OEING/ q+ i) }: W0 m TECHNICAL DICTIONARY 225 b- i4 t) @1 p* L4 Z7 b BOOLEAN ALGEBRA, A mathematical system for 3 u T) W8 o- V5 {/ kwriting combinations of logical statements.$ q; N8 @) y" t9 t BOOST PUMP, An electrically operated fuel pump for - ^' @, z3 T7 p: F6 n0 s5 U7 o; Yfuel supply from the airplane fuel tank to the fuel 9 R/ M2 t9 [4 F1 M5 _manifold. . D/ i* u/ Z; M% H) J& ZBORESCOPE, An electro-optical device for looking at- O6 b/ A& C& f ternal parts of an engine through holes in the engine. ! {& z! s/ ^: torescope ports) 1 i6 Z6 Q1 g2 x: }! t$ _OURDON TUBE, A curved flat tube in a pressure gage ' G3 O) Q, M6 ^9 A( z2 g% G( f+ [% or moving the pointer when pressure changes inside; U# B% c$ F) ^ on the ability of the brakes to0 a- E1 b# m% L! w( P9 r bsorb a predetermined amount of energy during a, t, Q+ m8 q* a! L% R: m jected takeoff. 4 j6 q. L/ l) E用于通过发动机内的孔(孔探口)观察发动机内部件的 3 D4 f" I; O# k. L& R4 G5 V光设备。 0 ~# W0 W5 Z7 |2 _: T! E& v5 T端管,, S9 w' S1 C4 x# J7 ` 测压计内的弯曲扁管,管内压力的变化时它使指针移 ! F9 i7 ?$ [- z4 @1 ]: V6 X4 i力。 # B) V0 |2 F, O: W极限重量,* m# T8 i( Q- D, |8 J" o9 |, N1 ]! C3 z* B' w起飞重量。 1 ~9 m$ [. n1 V8 R5 H1 L发动机滑油系统与大气相通的通气口。5 v# c& I& w9 }0 x5 ~, W) c in( n0 O! B# O3 X, f( @% y! B (b+ i) a; \& ]2 j3 k B % L- Z% n) f/ rfo" Y8 N& J. [* Q4 k8 r& P6 i9 }& h; U/ f the tube.: k/ g/ b+ W. _* X1 K$ @4 Q* A4 C BRACKET, To enclose or surround. - J, i' B; K) _; L/ t9 MBRAKE ENERGY LIMIT WEIGHT, The maximum$ v, e' N6 J A+ u0 X takeoff weight based8 ?9 t% N* G" Y* ~0 D2 s/ ~ a2 M1 \. R: j( Z4 J/ r re ! M, O' c8 T/ }# x! q" x. H/ WBREATHER, A vent to ambient of the engine oil system. 0 {/ g! e$ ?( h; L布尔代数, 0 H5 J( ~- L- E9 O2 H一种用于编写复合逻辑命题的数学系统。 v0 @( r9 L9 A5 Q增压泵,# [8 f# x8 k3 K) W 从飞机油箱向总油管提供燃油的电动泵。 ; x: R5 U* c: H& n# ]0 e孔探仪, 1 y9 t1 l1 R. D; ?# F6 H* }3 k6 L. Y* F/ N* Q; w: h6 ]: y4 f. y! w动,以指示压/ f4 A: k8 w- y* X+ L( a 托架,+ B* c! _& I/ Q, j: [$ ~: D( K 用于作支撑、装托、或围绕之用。 4 w! _: T5 w: t3 H+ ], k刹车能量4 t0 R8 M+ ^! J. X 中断起飞过程中,取决于刹车吸收预定能量之能力的 # C7 }/ M; M+ |( \/ _8 s) D% l8 g4 i0 N$ U5 K 通气装置,: Y: A+ A4 @% m z3 v6 S 英汉对照民用航空词典B OEING4 t* c' K4 x7 @5 r; M TECHNICAL DICTIONARY 23 9 [0 A+ ]+ D& `, h% b4 V, E# pBUFFET, Vibration of the wings and airframe resulting ( Y( ] u: @$ a Efrom unsteady airflow over the wing; caused when ) E4 W3 {7 f1 rairspeed is too slow, the bank angle is too steep, or , N- ]9 ]) a) M- k0 A1 O# girspeed is too fast.& ^8 B# x7 X! K2 L* _ z UILT-IN TEST EQUIPMENT, Equipment installed on( q! A* C2 v1 X e airplane and in airplane systems to test the systems7 c" S- a$ v" e, A ithout external test equipment.& y8 Z- a/ m8 A* ?* K, ~ UFFET MARGIN, The amount of residual maneuver) q. c8 t% O* E apability present before the onset of buffet. 5 Z" u+ i1 t' p) j a" v/ O2 T! j2 ~UG SPEED, A preselecteed speed to be observed* P: f6 a9 {+ |/ s- t1 L+ I nding sequence. 5 l# N0 ]- f/ \k" }1 @* M. A- d4 _ ng landing gear operation. M, j' p: t, O0 q J速度太慢或太快,坡度太大,均会引起抖振。9 h- r6 Z8 A% w 自检设备,8 u0 q/ K+ F. O! _ 安装在飞机和飞机系统中,在无外接检测设备情况下, ' K, T0 t4 ^0 W用于检测系统的设备。2 R4 C( N: ] C) t4 k: T3 n6 Q 抖振裕度, * u3 ` w9 w9 P" ]5 L6 x飞机在遭遇抖振之前,剩余机动能力的大小。! S; g) x) D7 i- V2 P/ ~ 标速度, # ~8 n9 d) C1 R5 k在某些机动飞行过程中,特别是在进近和着陆时,飞机9 ^ x- x2 ]+ j 预定速度。; j* s* |. M5 K @4 `! S 力装置, ' {" ^3 _, a3 I2 V架工作的一种机械设备(弹簧或减震器)。$ A! y( l9 L' f 流条," {: L6 {$ }, @! n! n5 a" y 在部件或组件之间传输电、数据、或定时的单一电线或 . q( E- H u$ m: x6 m5 Ma) ^! n+ i5 J5 K5 P& _3 L: z B2 r4 U; s/ N- c' A$ Q3 X th6 h# I4 o8 Z; u3 s" a2 d! X3 Z- W- u w 2 s' ~, f' _/ I% qB1 y2 e8 z, S* s* B* ~ c 3 S/ j. L+ s3 ]- g6 A D' k8 Q) B# SB& s2 h, e; z+ t2 m4 T' f during certain maneuvers, particularly the approach and7 }& m$ k4 \+ n m- n) _7 w* { E la' T" [1 ^ T) Q0 k6 [5 l1 } BULKHEAD, A structural partition in the fuselage or + w( N5 d$ b+ G$ }, j8 lwing.) d. y" E. S9 s: c/ F- d BUNGEE, A mechanical device (spring or a shoc % `0 h: |# R( b6 Dabsorber) for assisti , c1 |# L8 C& i T( o+ q3 GBUS, A single wire or group of wires which transfers0 i6 l3 a2 P! G power, data, or timing between several units or$ H" b" O( l2 o; g. k# a# z modules.7 g( j/ R. u8 c! [( l: J' W/ z 抖振,8 U5 k3 Q+ U+ Q( Q- r& x% T 由于机翼上表面的不稳定气流引起的机翼和机体的振1 j7 K1 m! T9 K% i/ Y5 S) t, w 动。飞行5 h. R( }& ~. {8 H- W0 i, q0 C9 i: h9 s5 o2 x所应保持的. Q A4 I A: @4 ]% w 壁板式隔框,7 j/ ^! o" n. q0 H# } 机身或机翼内一种结构隔板。$ |' J1 F7 E9 x# S4 P: y$ m0 T+ _4 I1 m. w5 T6 x$ q 用于协助起落! ~# b6 p6 L) a! ?. V( [+ B' o, b5 m) H 电线组。 + a$ p9 r; E7 [0 P8 O英汉对照民用航空词典B OEING - s7 F$ h% a; E) U+ R6 xTECHNICAL DICTIONARY 24

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BUS DRUM, A mechanical connection with pulleys, Y. b4 Q, I& E0 [! { cables in the control system. ' X& m2 V1 m+ Y2 jand 6 s% z- n5 `# f9 I8 H/ z9 A5 ?l circuits for control and protection of " |: H! |6 Q( u o+ Glectrical alternating current supply to the airplane. 3 C, D" f' X2 ?7 Kduct for closing and opening the duct& K9 \! ?/ C$ T6 t8 X8 _ assage.2 _9 u0 H1 H9 S# E' i( f0 k& z UTTOCK LINE, A vertical reference plane along the * E6 G0 X+ ]" o. t' Cselage for horizontal measurements of the airplane. 0 ] ]- M8 Z. ]( p b& x5 b接。3 m3 O* v! I$ j9 ^# o 组件,内含控制和保护飞机交流电源的电( \9 A$ s% Q" N2 ^8 d& |1 p: ~& Y, p: `' J9 g$ M& v 作动简控制的转动装置。用来关闭和2 n R- U3 _+ v3 F- } 启管道。! v8 e- r7 A8 Q$ P* y* \. v 沿机身走向的垂直参考面,用于飞机的水平测量。 , E4 f- a. ~9 ?& ]BUS PROTECTION PANEL, A module (black box) ' E7 x/ c5 _& s' F. ~containing electrica3 U9 R0 x# J* ~ e7 y1 Z+ x9 c& J3 u* p, {# Y' Y3 P BUTTERFLY VALVE, An actuator-operated, rotating 6 Y3 e& O2 Q: kdevice in a. \! l8 O8 |' n t" W: D$ v, q2 C p 6 _: p, l- \" L" wB- U* D( j( A# a/ X# w fu / q0 l7 P( Z' q; ~3 t+ A9 T转动鼓轮, ]8 Y3 b' {$ n) w: m 在操纵系统中,具有滑轮和钢索的机械式连 - V! r: p# c" D% _汇流条防护板,) l+ }& `; H- w w! A2 n2 Q 黑匣子式的) W( b+ d" F# d# ]2 t) k% {! O; h% _8 c 蝶形活门,! G* H3 D5 f! U9 S; t; ^2 E 是一个在管道中由# N& B+ ?7 x1 L3 A/ |% K& s, K9 Q* b: Z4 g纵剖线, / f6 k3 k# ?8 L$ l+ }! h/ G; i7 d- Z英汉对照民用航空词典B OEING & U# u( Q% K" u4 C3 Q9 v, l0 LTECHNICAL DICTIONARY 25 ( i3 p( X7 F$ D4 p3 ^BYPASS VALVE, A valve through which air or fluid will, L% ~- G% H, \# t8 q8 R1 n. \ flow if the normal flow path is blocked./ ]7 \- g0 P7 M9 q BYTE, A group or string of binary digits. A byte is % i3 C* K9 {$ y" J6 zsually eight bits long. * l! D9 ^. U: I! sABIN ALTITUDE, Atmospheric pressure maintained ( O$ S9 {" }2 x; z# Fithin the cabin, indicated in terms of feet above sea' v0 o6 L. B9 z$ Z5 d ALIBRATE, To repair, adjust, fix or correct the 0 V& p/ b, P1 m$ ]8 q6 O5 o L4 @easuring capabilities of a measuring device. 3 h. Z2 p9 K5 R: xALIBRATED AIRSPEED (CAS), Indicated airspeed# C, K$ B7 x; d$ X) ^1 A' o AS) corrected for position error. 6 D: J& ^0 v- ]. S9 x0 Ynical* m1 d2 j$ F7 d% F# w6 U omponents.+ q; U( k1 m7 s/ }& v" ]: T1 s* l/ e: h1 r% z' ^ 节, 2 Q8 O; J7 s) X3 N+ s D' H一组或一列二进制数。通常一个字节长8位。 3 ]$ G. D& C) t+ {' Z3 L) ~舱高度,2 \. h. A& H/ H. A0 t+ @ 座舱内保持的空气压力,以海拔多少英尺表示。 6 [; a U; d8 X& P; W准, ) ^% D( n/ {; d7 b D修理,调整,定位或改正测量装置的测量功能。 . G1 ~- `0 n. s1 H+ F正空速(CAS),& [( h; U Q% `. R3 R 在修正了位置误差之后的指示空速(IAS)。. h' x6 r4 {/ z8 @# {- G2 r 用来移动机件的一种转动装置。9 |# r" o- l5 ?+ m: y N u ' f. { {0 s: C8 `! u6 JC 7 Y8 x' t1 y! ]C 1 ]8 Z* X7 |9 c L9 ww 9 A) G( Y. s Z) i z& Clevel.: x& X6 b \. ~2 @& I C0 T- S! T- p- o% [ m& ?* k# \5 k v6 H, D. D6 P C/ Y) w7 Z2 h: R; G$ k B) d# } (I z* ?9 h. z; u3 ^CAM, A rotating device for movement of mecha; n# I# y" b7 T3 v' n6 k, k C : L+ g; ]' M# w# q2 q旁通活门 ' F" Y" H; o$ y' x7 h3 }/ o气流或液流在正常通道阻塞时所经过的活门。 7 r# J+ P' `" M: Y' e5 ]3 T5 C) a$ w1 B+ [; W4 Q% f) t3 g/ @- d' x! L( b! Z' l* w% h( ]; ?( A* t: g ~9 ^2 }2 ] u3 z' x/ J! a0 K% Y/ u4 G+ x# Q9 k& F 凸轮,, ] g0 l/ ^% p 英汉对照民用航空词典B 8 h2 x ~# c. u5 \* b3 l, v: Z3 ACAM-OUT, An autopilot condition in which the actuator! J1 ?( |" M: r0 ?& y detent piston is overridden, either manually or by the : }9 s+ s* |: |( c2 `* Y) Z' Ither autopilot actuator. & |2 V* a! F# j/ ?AP, SEE - CAPTURE # @% n& Z$ e+ i1 m4 mAPACITANCE, The measurement of electrical energy : ^0 Y, y7 P: Qtored in a capacitor (condenser).1 J& d; r0 A5 z" e APACITOR, An electrical component of two metal 5 a; M6 s$ u" i# ^9 Z/ [" ^lates separated by a dielectric material, for storing ' H. Y* O7 z9 u' m# m" z. `2 Ilectrical energy. 8 R: ^9 l8 A, Z# ]8 v& uCAPTURE, An autopilot or flight director function to0 x5 w9 m. V' Z% i" _% N. r acquire a selected mode. / A/ R( D* ~; p: \5 gCARD FILE, A container on the airplane for printed * Y# f% s; x: U( Ocircuit cards.3 m( o O" N l; P/ ?1 L 一自, _- y% t9 h6 Y6 ~# b 动驾驶舵机所超控。& A' g4 l$ N7 j: k) H/ k9 w; l: s 截获,, I7 k2 { e* a# S. Q1 ` 见Capture: m, T# U2 T; q+ n' J' N/ ` o, ?' I: H7 A/ \. | C . F% w; D5 f6 XC: C" }4 V0 n, [6 d/ a. F4 z s 1 _' |' g9 z, W" oC $ h' y5 v; k& o E* W2 {p 5 C& w+ ~$ A7 d, D8 H! [1 Ke 2 r, r+ G) ], D9 c8 i凸轮不工作,8 s5 s. G3 W' N y4 ^1 V 一种自动驾驶状态。此时舵机锁定活塞被人工或另+ S' M1 [8 V' q h& E9 S5 Z1 i+ k1 P: }电容量, + T5 o4 m# q; I1 i: E! B/ a2 |电容器内所储存的电能的量度。- r; A( q9 G! F0 Y& e- z 容器, 2 X9 m1 j- W, w+ N% o Z两片金属中间用绝缘材料隔开的电器。用以储存电能。% \9 i- {3 L( H0 ?( g: ~5 ~3 c- Q 截获(CAP),. {3 {1 o* I: r* U& {5 ?7 B+ l 自动驾驶仪或飞行指引仪的获取选定方式的功能。 2 m9 @2 V4 J9 s- G; v) K* L线路板盒,/ ?1 O1 M) Y i! }: X4 X& ] 飞机上安装印刷线路板的容器。 3 X w0 V. H8 U& {) p8 d3 p0 c: | T" b# Y0 ] OEING + |+ l- P+ f0 nTECHNICAL DICTIONARY 26 0 `. ~8 J- h* v y: q( x/ }英汉对照民用航空词典B OEING % d' x& V6 @( P2 d& @TECHNICAL DICTIONARY 27 - q. ^: u! V* `' R5 ACASCADE, Two or more similar circuits or amplifying- G0 B/ f Y3 F+ l# {5 {8 f stages in which the output of one circuit provides the ; B3 E& W! T( D4 ^) j" y8 x, Yput of the next.4 q1 D! n. U6 y% i# w1 f& t- S$ I ASCADE VANE, A vane for turning the engine airflow 8 V+ a, A$ N4 Q8 s% J- Wuring operation of thrust reverser.( J" z% A4 r! }( ]4 f. V! [# A ASE DRAIN, A drain carrying lubricating and cooling: t3 _/ \; J' C/ m uid from a hydraulic pump. $ ?% X7 t. ~% z( s2 @& ~ATHODE, The element from which the principal q7 a4 X" a; V' k( n tream of electrons flows. / I2 d& {# s) h% zATHODE RAY TUBE, An evacuated glass tube with a/ E. s) K9 c; Q) y( R$ \1 a CEILING, The height above the ground or water of the 7 W! a0 N% h- }! F6 J7 t6 |( ~) E, qbase of the lowest layer of cloud below 6000 meters ! P1 W" z& q* |. d2 K(20,000 feet) covering more than half the sky. 8 w) z! ~& _( u! o: Y$ N, G+ w程。该% y* l2 |: {( o+ J4 ] q 程中,一个电路的输出为下一个电路的输人。, N$ `$ \2 ]( R. U 叶栅叶片,8 r+ u I* i' c4 `7 t' z 在反推工作时,使发动机气流向相反方向流动的叶片。 ; Y0 e! ~9 F+ K5 A4 x: h匣余油管,4 P0 m; \) H* X( {& B3 }5 {- e5 ` 液压泵多余的润滑液及冷却液的排放口。 9 [3 t9 B. V& ~! \' X1 j极, 9 Y/ s) T9 v4 ^电子流流出的极位。 * l5 ?5 G" \. \; t+ l6 w [# ^极射线管, # [. Z; I8 O3 R: t+ j |4 B. q有显象屏幕的真空玻璃管。用于显示信息。% ?' j( A7 }! j% F 云高(云底高),, a( x( U3 c# U+ {( x( \, n& E 6000米(20,000英尺)以下已覆盖一半以上天空的最. P; M3 D4 C( d3 C' I% s 低云层底距离地面或水面的高度。 + {9 R% ]! }# c9 k9 j& @in9 U# _& k2 R3 t! W, l C ) ?4 j! @+ Q! t H$ ]# xd / O) n' v7 c9 J `" fC E) I/ M9 P; {7 I0 r& Dfl3 S8 v' h, C/ s& c. R5 n7 _ C 3 e& x0 m/ G1 f* A5 h& Ts 9 L; f& D5 h. f! R: \8 d2 H, ]C# B/ M& k [) }" C, W viewing screen, used for displaying information.- ?: s' X7 I5 K# y 级联, ' R8 Q! D" {2 z* w两个或两个以上的类似电路的逐级连接或放大过" C: R3 C w% j; l; S. M8 |6 C& m; ]1 @8 Z+ u9 o( _7 y. y$ ]: k/ P/ ]4 F2 A( W: G7 W4 r1 V0 B6 H1 Z( T4 |" R& n) J+ D T+ w: `+ U- I9 I3 U 一个具 & T, T. f( }! g8 F. {- H英汉对照民用航空词典B OEING 6 q8 S8 R+ @. I( w5 L8 D1 N* vTECHNICAL DICTIONARY 28 ) I3 [0 E+ C, N* A3 aCELSIUS, A temperature scale in which zero is the6 B0 k. e9 k3 c$ E* L; D, c freezing point of water and 100 is the boiling point of# ]+ P0 N# l; ] water. 2 z1 l; i7 g7 O0 T) {. DCENTER OF GRAVITY, The balance point of an object0 I4 A: {% C6 k* P; K r rigid structure expressed in terms of percent Mean 5 W9 O+ b2 U0 J: v/ f! Jerodynamic Chord or in inches from a reference point.- O- ?9 {% e4 ]9 j- z6 E: e ENTERING CAM, A cam for moving a mechanism to a ( ?4 V, T7 J0 O0 e9 Seutral position. 3 X) _$ b) G* ~5 I4 q( gIGURATION, A configuration of the ! \2 P# z p& rircraft approved for operation by the local governing$ \9 N; R# U: O9 S) b, X gency.* c2 B/ J+ }: Y3 o" @, |8 W ENTRAL PROCESSING UNIT, In a computer or% r' B5 s- p$ b' n; a igital circuit, the section containing the arithmetic and 6 \/ r1 _/ d( N9 [gic,control, and internal memory circuits. f4 b" Z/ ?1 H: |2 l& rENTRIFUGAL FLOW COMPRESSOR, A type of) ~; w3 b/ q; I& \4 a ompressor in which air is taken into the center of the$ l* d* b. ]5 N5 B( f peller and is slung outward centrifugally into a diffuser * n0 j, y; `/ z$ {7 vhere it is slowed and pressure is increased. 9 T' E1 J$ ^1 H2 w4 BCG, SEE - CENTER OF GRAVITY 1 U# T6 s- \1 J7 }5 u构的平衡点,以平均气动力弦的百分比或' |4 w: H- f" `* ? 某一参考点若干英寸来表示。 * X) q/ A" q5 V4 o/ ~. S. U中凸轮, 2 }4 N: A$ V% w5 G6 ?将机构移向中立位置的凸轮。 ! `3 f2 O" e( T9 ], K. r格的装机状态,: m5 E! d3 d; A5 N# o# I2 b 由当地主管单位批准使用的飞机装机状态。 + D( w1 G* y+ k3 t中央处理器,% T/ P6 w M0 p% l 计算机或数字电路中含有运算,逻辑,控制和内部存9 Y0 O/ p5 F" F/ {& [/ q- K 储电路的部分。 4 ~6 s; f2 [8 N4 {2 T v: |$ H心式压气机, : {' o# Y ?7 X& t压气机的一种。当进气到达叶轮中心时,被叶轮离心抛2 I* T1 U8 a$ f 进人扩散器。在扩散器中气体流速减慢,压力增加。 5 L& a% W4 E6 Y6 x3 I重心,: S) [/ |! s/ J3 ` U7 ^ 见Center of Gravity + h% f1 W7 k8 [* {% [2 ^- T, w1 co ( ^; N* X# \& d7 SA( d$ |' p; U. H7 z C2 v/ ?* H/ g1 Z n0 g8 G" w; O [" Q CERTIFIED CONF7 [& d/ D& g% B9 \1 b* c2 m; E a" {% h% x- V2 g" b2 k; Q a 6 Q' Q; c! @" k4 x, LC! A3 u! k. \: u+ O, D* c d5 I% [% A6 a, k1 i: { lo * b- b; c7 c' W) W- N1 J# O' o2 DC4 |! O4 E% g3 g7 f' V2 b! a c+ Y8 b2 H" m: _- @4 R. a, i im & Y! P5 z& C1 `5 ]' y- _w: R* ^3 _( s3 R0 p4 V. J1 T 摄氏度(°C), ' C' [% a" b8 ?8 W1 e温度的度量单位。在此单位中,0°C表示水的冰点,& o9 F" l1 g4 _+ [7 q- \ 100°C表示沸点。 7 @* k1 c; h1 y+ V! [' L: h重心# S" o5 k% H7 p6 g8 B" w 物体或刚性结3 c1 F! y$ h" x% o4 Y7 H- C& ?$ ^, H2 u; F: @$ O2 `5 ~, }8 w; V- ?% W: a0 y3 Q" E2 p; s8 b6 C' w) I) F4 M( |. a: v, G+ @1 [" `" N9 X& n英汉对照民用航空词典B OEING) D1 l5 i& c1 s* b! u. O' m TECHNICAL DICTIONARY 29+ @4 s& U. ^! a! s. G* y CHANGEOVER, Conversion from one mode to another.& W% Q% d* x. ]/ i# X9 B0 X6 ?. t- b HARGING VALVE, A valve for supplying air or fluid to ; J, T: p) b0 o( o1 x* cHECK VALVE, A valve allowing flow in only one ) Z+ Q f) ~2 Z0 J! ^ G/ qirection. See Non-Return Valve.4 X! x r u6 H; G HECKSUM, In a computer, a summation of digits or 5 Q1 K: U6 X8 ?4 F$ y0 Pits which are primarily used for error detection. % {* h6 j5 x& t% I! w/ T% rHIP DETECTOR, A magnetic plug in sumps of 5 a( ~2 U B& H5 z6 q6 s4 Zbricated components for detection of internal failure of 8 Y+ f9 F: B5 h# Te component.2 F" `- `/ c: L6 Y2 W9 r4 I HORD, A structural component of spars or frames. 3 ^. }& y( s' P! m3 Z" L! F添活门, # S/ \0 Q2 w0 h; t( G器充气或加液的活门。 ( v- n; D1 ] I0 X& G1 _/ c单向活门,* O: ~: T: l7 r m" M 仅容许单向流动的活门。见Non-Return Valve

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发表于 2008-12-24 21:38:05 |只看该作者
C' d$ Z" u* S$ W8 L% X% {" P a reservoir. $ _" y" F6 i5 W* _8 k4 H$ CC& A9 _- _: y- C5 W# j d* m& y* H7 J2 H3 Y D C7 y+ a+ z# [9 m6 O, i' |# r b ! x# l$ P0 `: O* U jC' M/ [/ E# T4 d/ v" |3 x9 g lu; ]$ Q6 j% n2 W5 h th 1 Y+ Q& r. W- e6 }* UC$ ?. W: i5 D2 e( z4 q" T 转换, ' D* K! Y' N% I/ N1 ` n由一个方式转换到另一个方式。 " k8 B0 k7 X4 t: y' c' r$ A$ e" f' N6 `: e2 ^+ H& f$ r+ S# | 用来向储存 9 h+ E3 q) ?( |! i- E$ |& ~8 ^( N/ \, Q( b |& P$ B6 o" [5 ` 总和校验,4 q$ ]* @6 T. u/ u- ]8 ^7 Z 计算机中,把那些用来探错误的数宇或位数的总和进 3 i! f( i" s( D+ a7 _$ n求和计算。 + I- j: E( D' K2 L' S4 ]属碎屑探测器,: j3 O; l, @0 @& c: Q 装在被润滑的部件滑油回油管路上的磁性塞子。用来探 1 {! v; n4 @) u" T部件内部有无损坏。. u# W6 ?$ a! f$ Q n* j0 b! Y 弦, ! Z, g6 ?2 F& J/ [* o$ j% Y梁或框架的结构部件。! l8 X# W# `/ H3 m' M4 C$ k. \! W- k; s1 b% |! k1 ^0 A- _2 x5 f1 h/ G, o7 P. l( `8 j4 `, d9 d/ ?$ S# @! s7 W8 ]' l& n5 ^1 b1 `- C7 k0 M 英汉对照民用航空词典B OEING* J( l5 L( O( l# h TECHNICAL DICTIONARY 30 4 _: y) T* m: Z+ QCIRCUIT, A closed path through which current flows& j' \ s. n& t; g ource. % e2 S8 M0 a8 Q I( i- o" uIRCUIT BREAKER, A device that automatically+ w/ m% e6 F; @# Q- g eactivate the system.) [& y1 [7 v4 \) f3 \" U' Y lear of all non-frangible objects which 8 \ ^% s4 v1 C! |4 Kay be used as takeoff distance available when X, S# X1 t) I0 o alculating a takeoff weight. , B2 m F4 Y! J) s: @7 Ur water under the control of the appropriate9 L+ w1 Q2 }+ O# S uthority,selected or prepared as a suitable area over6 d/ ?3 U" {. B hich an aeroplane may make a portion of its initial! i, z% M( \# b limb to a specified height.8 |3 e$ U) H( a! P: y increasing. 0 N/ e# N. a3 b1 u; s, ksed% J4 E) _$ n) A6 R LOCK SIGNAL, A continuous string of pulses used for& ?: Z' P; j p+ r 开关, T+ i1 v5 n* q; S# K 故障情况下自动中断电流以保护线路不受过电损 % M' y' F5 K7 d: U9 q体障碍物的区域。在计- F9 ^; I+ D; b H$ Y 起飞重量时该区域可作为可用起飞距离。 8 `* A f3 d! J' K是在有关当局管辖的地面或水域内一个界限明确的长 \, y* ~5 | f2 c3 f: i 形区域。在这个选定的合适区域内,飞机可完成初始爬 & y/ X8 s# l. {* V: c& Q的一部分,上升到一个指定高度。) G: a+ D& v# H* N. V( U8 Q 飞机高度不断增加的飞行阶段。6 P- y) n. m z% a( _6 f 钟脉冲, 2 d! a+ U( T1 {& j$ Q+ N5 z步的连续脉冲信号串。8 R+ E: q% m* G& e) T from a source, through various components, and back5 J. N. s% |4 e0 p to the s ( [- _9 e& @9 sC & X d5 C7 m; l1 _* }interrupts the flow of electricity (current) during fault8 {7 N2 T# J7 m | q condition to protect wiring from excess current. Circuit + s" O% {& g5 b& l7 E/ n( Lbreakers are also used as a means to manually " r0 y7 M% z* O F# S c& z$ }d % P9 F/ t }* Q, F5 I. vCLEARWAY 1, An area beyond the takeoff end of the # |8 t# D( t6 r" h9 ?runway which is c: N5 |1 @& Y: t! P" n0 k8 U" }# K m D3 b2 j& p! u1 H/ q! [ c5 v% k# B: G/ @9 e/ v; t8 B0 I CLEARWAY 2, A defined rectangular area on the % P. X" n- a3 I7 D/ A& K2 rground o' N2 M) _: W. F5 D) l6 _6 m; A a 6 G' g ^! ?/ X6 A* W! n/ t3 ?w ' Q& a( |# P# \; F% Vc " R q& v: S0 E- ~- D8 _! x- O/ ZCLIMB, Phase of flight where the altitude is 2 ^, z' F1 S! v% g3 W) P6 ]( h. XCLIMB LIMIT WEIGHT, Maximum takeoff weight ba , a; Y0 B& f: Q5 r# f6 m+ a/ u3 lon a minimum climb gradient with one engine 5 {5 b9 k+ }/ P: S* j! uinoperative.2 s+ X+ _; x" B5 N1 u; B: U( I6 b C * {, m$ p2 g# v! ?synchronization.# D* H0 D" M8 t& i6 }4 [' T 电路, k* w3 R/ ?( E- [一个闭合的回路。电流由源头流出,经过各个元件流回! h$ Z7 E J+ _5 E2 v: L, h 源头。' ?6 ]5 ~+ E E1 _. n7 T- M/ q. H8 P' i$ S0 U& a6 J: I1 @" O% @能在 4 k5 T. o$ J5 ], U( C, k坏的装置。跳开关也可用于人工使系统无效。 " e2 o& Z3 @/ F6 \一号净空道,3 ?% ?8 u. V; R6 Z4 _ 是跑道起飞端以外,不含任何刚 ( x) @* f) t, }; T* ]1 w! N l. }+ Z8 b" D 二号净空道,5 S$ U. q" P! z, a* p9 x) E3 G8 j7 h+ t& n/ e9 T. u% Q, ]# l; ~6 P2 T, I爬升, : R6 k5 `- t* `. U0 @& {爬升限重,' q7 N1 U" N/ @0 k% h$ h" |- B 取决于由一台发动机工作时的最低爬升梯度的最大起 9 ?7 v, ~! a# l8 c2 {飞重量。. d# j9 d$ ]2 J& M8 c9 t) { F6 N6 `& ]* h# E m用于同 8 q1 B: n" d5 n' d, S3 |& O英汉对照民用航空词典B OEING 7 J+ I. i: E% ~% | y% m8 u/ K2 jTECHNICAL DICTIONARY 31! \. R% v ?. ~: \+ ~/ A COALESCER, A device in the water separator for - M( g7 L9 G4 s9 `7 ]# a2 Dollecting moisture from the cold air.. v; _. m6 V* W" o) T9 M; f n antenna with a receiver or transmitter. 6 I* P! }* W4 i! S, B! o; T8 i1 Fhe cable has an inner conductor and an outer " y7 L+ V, L$ u& [; P; nrounded shield. 1 ]; y- ]& A/ }, S" c7 bting one inside the* C. X. X" j0 K6 S4 P+ J( e+ l- x ther for rotating the low and high pressure9 ?, E, t$ W) [ s% {& h9 l' {' i& W" }6 Z ompressors by the low and high pressure engine & \5 t1 Q6 C( F* erbines. $ I3 H! q4 _: \: P* DOMBUSTION CHAMBER, A part of an engine for% c8 n+ y9 [! H5 J urning fuel in the air supplied by the compressor. 0 C4 Y0 d( v6 L+ L2 X2 |置。8 L, {! c% v' C 射机的电缆。电缆 ( d) y7 J# i) U/ o0 s% r; g7 u/ c中心导体和外层的屏蔽所组成。 ( h; O7 h; Q( t. a, E两个套在一起旋转的轴。用于使发动机低压和高压涡轮 % L4 \ a$ w" M别带动低压和高压压气机。8 h% i. J# E" F2 d 烧室,, b0 Y, ~/ |: y3 @6 x# C% r! J 发动机的一部分。用来使燃油和压气机所提供的空气相 + _& K/ v" G, t, y5 @$ U合而燃烧。

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发表于 2008-12-24 21:38:35 |只看该作者
c R) m+ Y4 P0 d$ R! v& P: q( |COAXIAL CABLE, An electrical cable usually: B1 B1 U, g6 g1 s connecting a8 @" H5 \8 Q' I3 `' e5 D% D" o T ; g0 I3 T0 d) E5 f2 o* Fg - q% M/ ~# H& K" a& b( rCOAXIAL SHAFT, Two shafts rota - g8 C2 v! [. O# Jo" ~* D+ x* y, u3 J ~$ Z( Q; B4 n' u c, o: d# F. u. P* Z z; y; }' x" P) h tu8 J8 L2 }* [3 i& w% f+ Z C ! b* T& y9 o, U8 V% Gb 0 H( r/ \) \# a. X# B凝聚器,$ W0 N5 D; _4 x! a9 }; R 水分离器内收集冷空气中水份的装 & F5 i) D5 b1 ?% ~$ s C$ e同轴电缆, & G* m7 x* \( G& d6 b1 o& q/ U一种通常用来联接天线与接收机或发6 d- Z" ~) @/ U; J7 v2 L* G) Y M$ C+ ~1 U6 h 同心轴,% r6 u6 M B' y* q: n5 Y( Q5 q$ r& J; C( j3 P' P' V& U( X, E1 _8 Q8 Z) H$ |( u+ y# V2 I9 b& h英汉对照民用航空词典B OEING 0 b2 U. |" k) `* F( a* f" a- ]! \2 lTECHNICAL DICTIONARY 32% Y) a. T9 M, [& M COMMAND BAR, A flight director pitch or roll comman* k' D2 Q# u5 L; n5 V2 c indication.9 `! w+ P' L# a$ A) Z( V$ l+ g- k d2 y: u- l) X% y9 W$ O OMPANY ROUTE, A route flown by the airplane ( |3 [& s+ M1 Z. l8 @" v, Y6 gOMPASS LOCATOR, A low power, low or medium* R) K- m1 Z6 y# b, L! b0 O equency (L/MF) radio beacon usually installed in * L. H9 ?: z+ u5 D8 N/ w+ S- Gonjunction with the outer or middle marker of an, e8 H( K/ i- M# V tor (LOM), A compass: i; v: g2 ~+ S6 F locator installed in conjunction with the outer 6 v" b" u/ O `0 t D( omarker of an instrument landing system.2 {) K2 a, @# I3 [8 `' n: e4 z ss ' @: G* i' Z' Rle {/ |- e0 k4 L, sOMPENSATION, To offset, balance, or counteract. 7 t' \" U5 R4 S E$ e3 cOMPENSATOR, A dual capacitor for changing the fuel + c6 y2 k# L+ ?2 F6 I3 Uaging circuit capacitance due to changes in fuel8 w6 | e/ h! T$ n ensity. 2 G) [- e; R8 { Q% eOMPOSITE MATERIALS, Non-metallic materials used T7 U( w" m+ l r airplane construction. Fiberglass, Nomex, Kevlar,! z% ~6 b# c$ y* ~7 E/ f raphite Epoxy are composite materials. 7 G- N! Z5 C8 A; s; n司航路,6 K7 u3 \: q$ x+ k 在飞行管理计算机数据库内由航空公司飞行8 q3 i9 B( D/ ?. N+ e 盘定位台,6 ~) Y- b( U2 e 与仪表着陆进近系统的远距或中距指点标配套安装的, o$ m0 Y& y7 z$ j 功率、低频、或中频无线电信标装置(低功率NDB台)。1 }- }& A& E4 ^3 w$ W2 D5 M 程序中用来导航。) U' q! Q# R! v5 y M' B 1.远台,4 u* Y5 L5 }9 W* y1 g+ |7 f9 z 与仪表着陆进近系统的远指点标配套安装的罗 % |# O. L( W0 x! g- Y$ f# z( ~* L$ q; n盘信标台(NDB)。 Q& Z. Z z/ ]+ K+ M" y5 M5 t 偿,) E7 C. I1 z1 @; M x& K' p 抵消、平衡、或中和。' W. v3 Q' {& X* r/ O* `7 K 偿器, 9 N5 ]! O9 F. k( ^在燃油计量电路中,用来改变电路上的电容,以与燃 " i8 \6 @7 i& {' u1 k9 P* `密度改变所引起的电容改变相抗衡的双电容器。 2 k7 s' b1 D: f$ J. G5 C' x, I' S合材料, h" `$ X( ^# x0 u' t用于飞机制造的非金属材料。如纤维玻璃,Nomex, - B$ L( j& k' P( S/ kevlar及石墨环氧树脂等,都是复合材料。

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发表于 2008-12-24 21:39:01 |只看该作者
C/ G3 t/ V i7 q8 j* f5 n# Z operator that is normally stored in the flight ( x) P8 i0 ^! U6 a% V/ Y9 [management computer's data base./ Q6 O, _! h; Y+ T% @2 \% z C6 b4 [; Z( V7 V* _2 ? fr 2 F$ o4 [2 {" Wc 3 p: Z% n: r7 \; {- Q2 V2 p/ Einstrument landing system (ILS). It can be used for ' U" n: m- S2 K, d( z2 o; unavigation as authorized in the approach procedure.4 A+ R& R3 {; _/ u 1. Outer Compass Loca : B) U% }" c. @+ h8 w) L2. Middle Compass Locator (LMM), A compa* ?# r+ I0 \# w# f$ O3 [5 X locator installed in conjunction with the midd 5 D2 N: w l0 }& v; P4 e# S5 @marker of an instrument landing system.2 F3 M6 ], A! ?2 j C) l) E' Z2 z. S6 z7 u C+ W& B) \" d8 l1 f$ ~7 Z g $ e1 y0 B5 E& n1 @" V a0 jd + b( G4 p. b9 U5 x$ t! P: KC& w) l) m% ?3 A! ^3 t fo 2 |: ~: {2 v2 q( L& ^g + X) | c+ E+ w+ _0 }& Q指令杆,0 W+ v% X. W& j( Y, Q 飞行指引仪俯仰或坡度的指令显示。5 t4 ]2 s& V+ {0 j5 O( M1 E4 x! P4 N! R/ u4 e' U6 a2 J通常储存, ~, ~; e; t% z- S 的航路。 u( }; O; J2 ^0 [0 D* g0 |: R4 g: Y' ^& @2 `# [9 f6 I; E1 t& L2 X3 Y经认可后在进近( Q5 C5 t* D: l9 J) o+ p) U% K 2.中台,9 i0 D2 @6 S/ U& A+ h& }2 b. D* V 与仪表着陆进近系统的中指点标配套安装的罗2 s1 M" O' K7 ]4 D 盘定位台(NDB)。. i/ ^8 f4 k( X' G) q) Z# |" u, g% P! b+ y; D6 ?+ \) v7 T3 m7 E# s! v& M ?% }$ V! q" a6 B! x R. U! l! T. T* QK8 Q. P: H x! \- W' v( x 英汉对照民用航空词典B OEING6 R d7 ~- N( Q9 r# e TECHNICAL DICTIONARY 33 . ^, ~/ @. ^+ X7 fby" E. I1 s5 T9 Z' P or increasing air ( ?+ x% q) i1 U( G& Cressure and temperature before the air enters the/ w) f5 a3 u0 a5 p4 U7 g ombustion chamber, Low pressure compressor - front1 o5 y6 Y, T! P# R) z ection of compressor, High pressure compressor- rear # v Q- s$ T" n5 a; S5 W% gOMPRESSOR STALL, An event that occurs when 9 m* ]5 g( K, nere is a complete stoppage of air or reversal of air flow ( [! I0 {7 l* z9 k' ~* RCOMPRESSOR SURGE, SEE - COMPRESSOR * I$ B3 h9 Y9 SSTALL COMPUTED AIRSPEED, Indicated airspeed* |6 \0 q9 F" }( I( [ corrected for the static source error. 2 S/ R; N- H0 K2 e) t( a0 x' b的机械轴来驱0 h& E+ w4 C/ K& `2 i3 f5 X8 P ,用来增加吸进空气之压力和温度,以供燃烧室使用。/ \1 Y3 ?$ V# t8 h 压压气机—压气机的前段,高压压气机—压气机的后 ' K4 r, ?* T5 ~2 t' I/ P6 A' `& k9 j* [# w% Q9 l# }* d! [6 t; Y' B* U 气机失速,* N |1 {4 O! { a/ P 当气流完全停止或通过压气机时气流方向逆反的一种 / p1 B& x/ c. |( B压气机喘振,& J9 N4 f( ^, `( @5 A 见Compressor Stall * }$ r J; _! H3 I* ^( }COMPRESSOR, A rotating part of an engine driven' V- u. `5 \/ t: i5 E+ x a mechanical shaft from the turbines f : F0 g( |" i! y! _- q/ mp - c2 @9 A; P% sc 6 _. ^$ W R7 q( C# g' S( ?s/ D5 \, O3 B7 i: A, R# `: Y5 s: a section of compressor.4 {2 |$ I" D! p) f, _1 ? C 7 O r, B2 ~5 G) q& H2 o* Yth0 }5 h4 [4 z! V" [+ i: c through the compressor.6 }0 q# v: j; ? I8 Y 压气机,- L2 j/ p# q" A, t& l 发动机内的一个旋转部件。由与涡轮相连 % Q C/ O6 `. a* u& a& @2 u# N& M: d: ?' d- _. {8 y `9 y8 N7 t& i% d7 C8 B! G! a2 h5 p) J/ ?- K! w6 F, q 现象。' ]* {7 [# S/ P5 x/ a1 S# v6 _! j$ \8 e* c" q( i0 S* q( ] 计算空速, ; j7 z& a( S! D修正了静态源误差后的指示空速。 k/ a& ~+ @: \, o% u* @0 B, d 英汉对照民用航空词典B OEING 2 v5 L/ N; g4 U: hTECHNICAL DICTIONARY 34

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发表于 2008-12-24 21:39:27 |只看该作者
COMPUTER, A device that performs arithmetic 9 P y& M; i3 A, ~operations, manipulates data, and makes decisions.% L7 A' N$ `7 X5 R- ^ ditioning5 K$ Q: w, a3 } the air and the: e) J. l& ^" U9 J frigerant or moisture vapor is changed into a liquid." x7 g3 o/ j5 W9 g+ ` ine w# z" b; Q* Y5 E ONFIGURATION, The position of flight controls, 1 ^! J! x. i3 Q rmissing which% F ]" \; w" f- R8 c may affect the aerodynamic performance of the 8 i* r$ o8 _) {: ]airplane.; W; H8 }: ]: a' Q 置。2 s f- V$ r! t5 E! B: Z5 D 中能使热能散发到空气中,以及使冷冻剂或湿8 g1 R. q: |" b' D: o' | 转变为液体的部件。7 L {; C0 |6 p8 @. }+ U# y$ ^ 连接到飞机结构上。0 O2 ~- w( d# g0 m 态,2 _6 d3 a% ^% [ 定飞行阶段中,飞行操纵面,起落架等的位置。 ! a5 ]% z8 r/ U) s), 5 q3 |% z7 \: f- Q O& J5 i6 A) W* S7 g受到影响。 5 K l* X/ S3 Q/ [& D9 I, L. FCONDENSER, The component in an air con * Q. k4 [: n- F5 _* F# J0 Vsystem where heat energy is given to0 n& L$ A1 B& E. P3 @# B" ^/ @% N re5 Q3 Q# X# A" h% K1 R CONE BOLT, A bolt in the shape of a cone for eng 7 |8 Z) n4 e' P8 C" V7 Sattachment to the airplane structure. , |$ N6 S8 b: v- Z# I# _C 7 p' y6 w' n! Llanding gear, etc., for a particular phase of flight, e.g., + n7 V. F: Q7 h. D; R/ G7 |Takeoff Configuration, Landing Configuration, etc.' v: c7 V+ G6 u y# g CONFIGURATION DEVIATION LIST (CDL), Appendix 8 l: f3 v+ J: J4 B9 rin the Airplane Flight Manual (AFM) allowing operation9 c0 h, Z/ L/ |2 G5 n of the airplane with certain airframe parts 3 Q- N7 `3 U/ i( A计算机,! i, ?$ }- w! N4 I$ m8 H 能作算数运算,数据操纵,和决策的装5 V7 q) P3 z% s: p: h% ~4 L 冷凝器,1 q$ ]4 m- m1 s, P3 e3 o 空调系统1 |1 K! q7 `. `& d( N# |* B/ f" b( f, e5 n9 M1 e$ T锥形螺栓, . W* @- u8 M9 e1 d外形是锥形的螺栓,用以将发动机 0 Z& h6 a/ C; V! {. H% e6 q3 `. @4 Z* L 在某一特- E. z( j1 N+ f9 f/ w/ ^ 如起飞形态,着陆形态等。9 P" @5 u9 L! H 缺件单(CDL; ~# [# W% J; m% e/ v 飞机飞行手册的附录所开列的飞机上某些零件的清单。 $ w$ P7 R; G4 a在缺少这类零件时,可以飞行但气动性能可能# m) {5 }. T2 Q1 l! F* [ 英汉对照民用航空词典B OEING * ]: [4 w: S& K8 v' W6 UTECHNICAL DICTIONARY 35

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发表于 2008-12-24 21:39:49 |只看该作者
CONSTANT SPEED DRIVE, A hydro-mechanical * D" p4 m$ O z Q* hcomponent for changing variable engine gearbox speed, G; Q! X& n& [2 T0 C k7 ?5 J ONTROL AXES, The three axes of the airplane which D# r- [7 g# j0 W1 h' { re perpendicular to each other and pass through the8 k I1 T( m+ j2 s, M1 M enter of gravity of the airplane. % v# u2 n9 L# p0 [2 K9 ~+ n U! wPitch axis - Horizontal or lateral axis, passes through5 e& w9 U, w6 S1 c! d the airplane from one side to the other - 0 [; D: S8 W0 X' Q5 J" ^4 @/ unose up and nose down control is by0 _- h2 d& j) F: y. K elevators (and stabilizer for trim). ) W, q* E3 g& {8 \1 G" tRoll axis - Longitudinal axis, passes through the x9 j$ y- W: E4 ~/ w airplane from front to rear - wing up and, q5 Z& C6 \+ Y5 ?$ b wing down control is by ailerons and' s# _5 _" U, e# L5 N l flight spoilers. # C% b0 d: L7 Q) s; t lYaw axis - Vertical axis, passes through the . @' Y3 U. E" kairplane from top to bottom - left and; \) N2 B2 C6 o right control is by rudder.1 o! T8 t' l# _ q5 J 置,; b( v; X- w* \$ d- t- s 制轴, ( Z( t& G# N" R4 Q; d通过飞机重心互相垂直的三个轴。 ; I: l% L3 C( x( a8 b1 k1 {* z俯仰轴—又称水平轴或横轴。由飞机的一侧通向另 4 I# c: O. C5 r6 q4 V侧。飞机绕此轴转动即造成机首的俯与仰6 k8 m) {6 D u) |0 v) g 俯仰控制是由升降舵来达成的,水平安定 $ C7 t7 _+ g1 G/ J则为配平之用。 5 b1 _ {& F- I" v2 M( r) M横滚轴—又称纵轴。由飞机的前部通向后部。机翼 2 m7 }6 k4 o- U" j7 n下运动由副翼和飞行扰流板控制。 ! F+ w5 J; D: D% B( ^# t9 q偏航轴—又称垂直轴。由机身上方通向下方。飞机 c& a% N- N3 ], v& L# u4 C 此轴转动即造成机首之左右运动,此一运 & k& n& j J! c2 g( ^9 \4 n/ A# H9 W由方向舵控制。 , R: [& x3 h2 S2 Yto constant speed to drive the electrical power.& C# ^& c* q% X G' _3 T C 4 r2 o" |- E5 `; ma N# g% j9 k3 e8 Q8 y7 `c3 N# n1 e. V( b1 F0 z& h 恒速驱动装 ' ?% w, Z$ Z' k! P3 [& }将发动机齿轮箱的可变转速转变为恒速以驱动电源的 . `& l* {, S& M9 T, E- ^液压机械式部件。 _; B8 O) X+ P, O9 |8 r) j" k5 C/ w' D+ p9 m- I/ i" N* B$ B9 ?; c9 @0 K( i8 |0 l: e* w' j4 I* q) }. F4 w+ o) V; S) {: c% O- I4 p7 f) i2 p( @, n: @- [+ S8 Q# _+ e8 Q6 q8 J# [9 S0 m) \# P 英汉对照民用航空词典B OEING- _1 q$ p0 a5 u4 s. l" a TECHNICAL DICTIONARY 36 " S. @8 Z9 g/ S; Q- O! @" PCONTROL COLUMN, A mechanical component used9 P- @5 h2 c0 @ rs $ c- X( L& E" G0 `/ ^' Q4 O, l' mnd elevators. . N! q6 Q7 j6 h& P5 `" yONTROL SURFACE, Moveable panels on wings and2 ]8 A% z0 E& R6 z% _# o# D+ I il for movement of airplane on pitch, roll and yaw axes., |; T! b0 o; S. j5 o0 i$ C ONTROL TAB, SEE - BALANCE TAB / ?2 B: a0 p8 M/ A) d7 oONTROL AREA, A controlled airspace extending5 I( G. M9 @6 V pwards from a specified limit above the earth. $ ]( o/ a8 g2 ?% QONTROL ZONE, A controlled airspace extending 0 ^+ r+ G f% p, C: C8 Ppwards from the surface of the earth to a specified 2 n" l& C% s; D' x N9 o" ~pper limit. 5 n1 w- V3 \+ a. ~: Xis3 y1 w* q- U. f B' T6 _$ ` o IFR flights and to VFR flights in accordance4 Z% G# {7 v0 B3 ~( H with the airspace classification.$ q1 t$ R/ b2 }; h0 ]/ z" H; Q 机械部3 N% c8 T2 |" c: M) T+ b3 l0 B* C- i& {2 `% D8 F' o操纵面, 3 e, w" C2 f: E6 P机翼和机尾上的可动面板,用以操纵飞机俯仰,坡度, : I4 X7 g* C( ]* C+ C5 ?和偏航运动。 8 V% _: x' f% w操纵片,( X [7 V8 c' l* K2 i 见“平衡片”Balance Tab

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10#
发表于 2008-12-24 21:40:09 |只看该作者
by the flight crew for operation of ailerons, flight spoile c/ d( w! ?$ Y! {; x: w' j/ ^a& l; ?- J8 j3 g6 p C 6 m& P3 B7 B% ]ta 6 j6 m# `- ?# l9 r% Y8 C$ q% _- vC& W/ e+ ]5 b4 ? C ) {) S4 B0 m- i C" B! F' {u 4 K' \/ k6 I6 _C e- I! B' [/ y# hu ( u8 Q5 } N, n/ X2 @; ju# E+ l3 `4 t ]0 B l. P' @ CONTROLLED AIRSPACE, An airspace of defined 4 n- O* k% G; K s) ndimensions within which air traffic control service; v+ |5 x0 b2 {' B provided t ) Q7 r7 S+ D+ `- `驾驶杆, 0 R4 E1 y# w! I" [: I飞行员用来操纵副翼、飞行扰流板和升降舵的 * p* F O( Y# A6 i2 P0 I: R! ]3 Y9 T B/ x! q: j9 N; {5 W 管制区域, & s- g+ _$ k$ c9 ]高于地面的指定极限以上的受管制的空域。& x3 Q8 b, s5 w- B! P! f4 F 制范围, : p' R- n! b. [ t4 _+ ^: c由地面到指定的高度以内的受管制的空域。: N1 `& v& i) |' V0 V" q 一个范围明确的空域。在该空域内,仪表飞行规则飞行 # P, S# v' K7 h2 y和目视飞行规则飞行有空中交通管制服务。, D/ C& d0 D8 L0 m" q- U4 V* D1 b) `: Y% {( b2 `9 L0 r 受管制空域,4 F# j9 q0 w3 o' V8 D 英汉对照民用航空词典B OEING / ^$ {1 N4 y& I# @" O4 LTECHNICAL DICTIONARY 37 J/ O! V$ [/ |+ F0 T1 i" vCONVERSION, To change into another form. 9 g, C9 T6 Y6 N) JCOORDINATES, The intersection of lines of reference,$ |3 s# C( F; O& C; E& l sually expressed in degrees/minutes/tenths of minutes3 T8 O/ k% r5 ^ f latitude and longitude, used to determine position or+ R+ P8 u* ~( y5 U* i1 C7 `, n CO3 a8 N! K1 Q- V/ o9 d. r' { destruction of th/ P2 a, h0 | L: ^, Q. k; g chemical conta & W" a& j" I) H* j, |$ SCOWL, A remo3 I+ f9 n& Y! C: @# ^4 Q0 \6 l for access to th ( m- V5 B% ^9 T, o" i! E5 SFa 1 E _# V, c5 O3 YNose Cowl - Front section of the nacelle for air inlet) Z8 \, w3 A6 f8 X$ B to the engine.3 _! i/ O H- e$ m Side Cowl - Cover around the sides of the engine. 1 t4 S* z/ b0 L& u! Y3 O) HThrust Reverser Cowl - Cover around the core + ?0 p# L2 H% R( Gsection. 7 y; `: u% L$ }1 G5 xTranslating Cowl -The moveable outer portion of the# J8 E. c& l( e7 D0 Q thrust reverser cowl which is ' y+ B4 X: ~/ ~4 h l! Y! y+ D* b2 eoperated during reverse thrust. / l i7 @ R/ ]& q/ b标, ( ?: }& L- T$ U N7 D( [基准线的相交点。一般以经纬度的度/分/十分之一分 8 f2 h. S4 {# o- V读数来确定位置和方位。( \4 H$ B/ X. m4 {9 l7 [. d 腐蚀 7 l" ]2 r1 o' r) `( F3 Z动机外部可拆除的罩子。发动机上的构件必须要取下$ V2 j7 E, A. |+ w 流罩后,才能够到。. l8 M) S& Q' Y6 s3 `& j3 r; h, _9 A" O0 g: o! ] p) U 机的短舱的前段。" w- D4 h) Z" ~. A n( x 侧整流罩一发动机两侧的罩子。4 ~. s5 {6 j: [4 b/ s; a; s* Y! ^ 反推整流罩一发动机主体外的罩子。- z) ~: W$ c, ^2 k' j 移动整流罩一反推整流罩外可移动的部份,在反推工 + ~* D) Z3 X2 s4 k# L- V+ }4 k作时使用。0 G5 P7 e% K$ h* u8 g u 3 r8 i; x3 ]- j- G7 L) Jo; E9 P, N5 P8 K' N3 @" ]) B* j location.8 M' o9 @$ u6 Y* |' |$ I6 |, j RROSION, A chemical action which causes gradual # W% u8 p' W ?e surface of a metal by oxidation or" w6 s$ v3 x/ I mination. , G+ P4 M/ `# [0 r) k) c# K7 J) c5 avable cover around the engine sections 5 p! O# S. A' N9 z# ^0 s0 X! B% _e components on the engine. ' k( ?/ l# C% [1 X' ^0 m7 Nn Cowl - Cover around the fan section. ! Q6 g3 o) A) `, G! j转换,; K8 D8 k6 f! R1 D 改换到另一个方式。9 T) N! f7 J# f8 N- _. a1 }5 w% J6 f6 C* T% P! n/ F- @4 @0 _7 _5 F( j- C* l, a0 e. Y4 H2 H* K3 Q4 ? 氧化或化学污染造成金属表面逐渐破坏的化学反应。 5 Z! R! A _& y6 [9 i% p( [发动机整流罩, % d$ o; a8 h# b r6 s1 ^- C+ Z/ ^7 Z3 v+ E) f) r( ~1 J' H; |: K0 Q. [: ]4 g扇整流罩一风扇外围的罩子。 ' i5 W" K+ R" S0 g+ N前整流罩一引导空气进人发动1 u6 H+ k: L- q9 R4 S+ w 英汉对照民用航空词典B OEING - J/ V) f; s# }+ cTECHNICAL DICTIONARY 38 - L6 y" }2 D, G, QCPU, SEE - CENTRAL PROCESSING UNIT5 B7 @6 M" ]# d- Z5 M6 M CROSS TRACK, At 90 degrees from the desired track+ [1 X+ r4 F7 w5 E4 C f the airplane. For example, cross track distance is the - b- N7 R/ w b$ n4 Z0 H& ^* Distance from the desired track measured 90 degrees " E2 \: z0 D( H, J; ^om the desired track.9 l4 E) [7 m- X ROSS-CHANNEL, Electrical wire(s) connected from : `: U( K6 s- B1 O9 o( ?6 @ne system to another like system, for example, FCC5 \3 h" z" f3 r! d0 f7 } " to FCC "B".! r4 L8 ^0 A- r7 h n adjacent engine or one on the other side.5 L3 F% i: `5 x; E6 K& C l crossfeed2 l" {3 s! v, Q% N: x" r4 M anifold for fuel flow from one side of the airplane to the 9 K, V5 k3 i& h: _. X2 Y- ^ther side. " Y% ^" R- ]6 r0 x1 t# P# j' t0 |/ fre " d, a/ N+ o: x) ?' @7 NRUISE ALTITUDE, An altitude or flight level # Q7 |3 Q$ ?$ {/ w: N$ S' S: W- q7 z( W2 B/ q+ n o4 l7 j" w+ x- S2 o8 j# {/ P d) O1 ^/ v/ a( { N fr 9 w0 Q( [, I+ w0 Y' ~2 QC : m/ C/ k9 z6 Ro 7 h L* _) @2 R7 P"A4 D. \' G6 V! A. \ CROSSFEED, An interconnection between fuel . ?/ U- N$ n/ b) t1 ]' ?% z) nmanifolds for fuel flow from one side of the airplane to : n) y' @% j6 ^% T0 Fa ; |# B" S5 ]' _0 gCROSSFEED VALVE, A valve in the fue 9 n5 U2 @( R$ k* O& Tm2 b5 R3 ` [# @" C* @1 s3 P& \1 N3 [ o0 }: B& Q9 N6 ]: K6 O5 { n7 a- r CRT, SEE - CATHODE RAY TUBE3 t6 J5 s7 [$ x2 }% ? CRUISE, Phase of flight where altitude and speed a ; @% q4 I8 {$ V. G1 H3 Ebasically constant.& p# l5 J' ~8 R$ I C & e6 L) A' F1 D# \maintained during enroute level flight. 4 \: M- y5 \: h中央处理器* H8 p' A/ k7 R* t% p$ v, s 见Central Processing Unit.: @, p! p% ?6 ?* G; T# O+ W 交叉航迹(XTK), & r$ ]/ l* T4 ^* g* e: ~# Y与飞机预计航迹成90°角的航迹。例如,交叉航迹距离 " @ [; f$ }/ M3 v3 H* {3 X是用与预计航迹成90°角量取的到预计航迹的距离。 . w2 o6 S2 k9 _4 e通道跨接,8 I. p$ f/ B* @5 z 电线由一个系统接到另一个类似系统。例如:由FCC% z. ^3 Q4 u* Q- {; N$ Z “A”9 [& b( u7 W2 G! L2 I& A& Y: w/ U# [ 接到FCC“B”.5 C0 P: S* m. @+ y4 o 机身另一侧的发动机。 : @: r& @- t0 y; ^: M于使燃油从飞机的一侧 . l; B. T& Y! s, z向另一侧。 0 f# ]' Q" W5 p0 p见Cathode Ray Tube 7 T. w$ m+ w. Y' x交输, ; O7 t. A) b7 Q燃油支管之间的交连设备。可使燃油从飞机一侧流向邻$ V: V: }' \4 v. ~5 w' A# c 近的发动机或在 2 D' p! G- l: E& y1 B( v7 r; T2 W交输活门,7 K( V; O C5 _: I1 D! f$ D 燃油交输支管内的一个活门。用 + x2 E1 h% k S+ m: U" M; Y! T: P: T' t3 x9 e5 P, a' b# T8 [0 t/ b阴极射线管, . S% ^" O6 b6 J3 H- h, ^& B. N. % O3 ?$ ~( U% W# o阶段。# x. o! U9 a0 v# { 航高度, & ^: m9 e. Z3 |飞行期间,飞机所保持的高度或飞行高, r h& z4 x; q/ I) ]1 @* f 巡航, : e4 x w N+ E飞机的高度和速度基本上没有什么变化的飞行! M/ n9 V0 t, w3 R" c6 x5 P# O. u/ x% T) g5 k( B7 d 在航线上水平; w: u; N/ y7 Y T" K& `# z7 { 度层。 # a: M5 ^8 [/ k6 k1 z英汉对照民用航空词典B OEING& _" ]: ~- U" s' u/ } |7 I TECHNICAL DICTIONARY 39- }/ G8 _9 \* }$ t9 s% K# P CSD, SEE - CONSTANT SPEED DRIVE9 P) r" c; Y' v' m CURE, A chemical change which takes place in a resin 0 V5 z b; y" o. e( Iand fiber based component causing it to solidify. : o2 R+ ?8 B# p- C* R) T! q' x# P' eCYCLE, A complete series of events that take place' z! T! _& l, C4 \5 L$ _4 |9 N gularly normally in a continual sequence. 8 v- k/ X9 H/ o' t4 i2 s% CAMPER, A device for slowing down or limiting% S% W. p1 D- N3 X9 M DASHPOT A mechanical damper for slowing down ( e3 ]* b) e( k* |1 vovement by restricting fluid flow.$ b7 [. c: ~& t5 r& A, e% Q D; {1 H2 |+ W6 L. w5 S, ? ATA BASE, Stored information which is used as the) s/ }% v4 G' C G0 l/ Q3 k ba f. _9 _% u$ l% a% x `, {DATA BUS, A conductor over which digital data is . # p+ W+ }8 d8 ?0 i6 B* P9 ~transmitted.3 j+ v3 I. l+ Q' V. f/ }8 Z DECELERATION, To decrease in velocity. ; w" Z) S) H! L; N7 K装置, 3 {8 H. h* r( O. u8 srive. Y- O; R5 ^& ]4 K) J) y re . S6 p' N" ?) F V8 A# I7 b" QD - j3 O1 ], p- }5 K7 ?, CD 5 i! W$ g9 T* f9 z* W0 ^" B( Vmovement. 4 _0 ~' k4 y# r h8 |. ~- em9 a* @. K' R1 U0 P ATA, Another name for information. ' `- f- O8 Z9 G3 j/ {& {D ) | v. n. W P" C0 Q7 osis for computation." ^7 m( H0 t) ~, a 恒速驱动 V: W2 j& C+ T( N 见Constant Speed D .) k5 B- Z( H& @& R. i9 [8 f; { 期,8 B5 k( Y' e! }# S6 w& \' A/ N 不断重复发生的事件的一个完整系列。 6 Y- P9 v: W( ~, T, S尼器,# N- t: s! w$ H3 V1 E 慢的一种机构。8 |4 B7 ~/ }5 l3 Y5 p9 ^& Y' i" Q$ l8 I用限制液体流动的方法以减慢物体运动的机械式阻 $ J6 H1 P) x T1 X5 a; R& x* U& ~! B- x+ U" w, z8 n. w. r. s* V* s) v 料的另一名称。 & y+ Y4 T6 |& s$ Z+ h据库, 2 W9 T' }1 l' _# S+ u数据总线,4 S2 _6 C: E2 h; D/ | 一条或一对导线,用来传输数字信息的通道。1 t+ V. K( V) q! d# t 减速,; G1 a- x' R9 \- Y% N8 C 速度随时间的递减量。) t2 b* K2 v8 @& N. o 固化,# w; Q5 }' O7 Q0 \& M 树脂和纤维部件内化学反应使之成为固体的变化过程。 6 _9 ^& W' g& {) n: h: ]8 w" S$ z2 S4 c$ e, h: M; N E7 ^% U( B 用来使运动减6 ^# d* B) j. ]5 T) T7 z4 u9 ? 冲器, 3 G$ }; X% E& ]7 g- M9 _, i器。, _) D) o) b: H) s 据, . M3 D! _0 w! s* d; M3 F$ j3 Q7 N6 H1 @- L/ R! v, x9 O$ o, {$ `' `/ P储存起来以便在计算时使用的资料。 ; U0 ?: i! Z) C+ {) Y* N/ |英汉对照民用航空词典B OEING . M5 A6 Q; b5 l3 kTECHNICAL DICTIONARY 40* A7 |7 L/ y' l DECIBEL (db), A unit of gain derived by computing the 4 B- O1 v+ ~7 Y2 f, Qtio of input power to output power. 1 n$ r% C9 ^# r4 }5 x/ l, p" gECISION ALTITUDE/HEIGHT (DA/H), A specified3 A, K0 ?/ V* @( Q8 @! i4 ~) J ltitude or height (A/H) in the precision approach at; b% z, ]! X! C5 O$ j hich a missed approach must be initiated if the 9 v0 T7 [: o9 }" d+ CECISION HEIGHT (DH) 1, With respect to the, ~* l5 {7 q4 Z4 w* P0 g* y& K- s proach or; j% w* p* T" I5 C! g execute a missed approach., p! p5 O* s* S4 p- O* X, p, [2 B proach to trigger the decision of either $ Y& q5 ^- e k$ @nding or go-around. / {, [# f0 |2 L/ g; kECOMPRESSION, The loss of internal aircraft air 6 u( H! F7 U# n( }ressure.- H3 V; x# ?" l E-ENERGIZE, To turn off or cause to not operate.. Q' _/ V/ x" Y/ N* {' Y rom the tanks" B6 C$ x( y1 O- ?+ D3 b using airplane fuel pumps or external suction. & X6 J3 C' ~0 o1 A8 |6 E算的一个增量单位。分贝" L5 l7 N$ q5 x 常表示两个声音信号或电力信号在功率或强度方面的 & y. A4 H. K# C9 z0 u0 b. M对差别的单位,相当于两个水平的比率的常用对数的十 1 h; W8 q, D! D2 Y( R断高度/高(DA/H), ( _6 Z- e- s$ q5 C$ s$ \5 L在继续进近必需的目视参考没有建立的情况下开始复 - c0 {4 p' v+ F j3 ?9 x2 X7 W的精密进近中的一个指定高度或高(A/H)。4 T/ ~( E; w0 v+ Q o 断高(DH)1, K5 h! f) ?: k0 B7 m- Y5 }操纵而论,指在使用仪表着陆系统或精密着陆雷+ p. X: G! D4 a# t# `8 I' k 生继续着陆还是复飞决定的高。9 f j0 ~( d2 k' O. w 飞机失去内部空气压力。: Q0 X7 _2 u8 Z. e 开, ; n' a- {! r2 G# K) X关断或使不工作。 0 }* n8 `( J0 c6 Y机的油泵或外部的吸油装置将燃油从燃油箱排 2 t/ b3 a) a* C# ^. d& {出的方法。 - z5 T+ u) |3 H) Mra) g e! f) x0 H- y; G D" [/ n6 M6 h q/ U8 o; U5 b* w& K a 1 i& I, T1 h* P3 `9 Yw 4 O5 \% t3 E d' trequired visual reference to continue the approach has3 E7 z# e$ d1 U8 V% @2 B: u not been established., `# U. Y, Z7 T# U D7 Z s9 _ C! m; T operation of aircraft, means the height at which a( x" C! |, K$ M! X' |& t decision must be made, during an ILS or PAR 5 s {' T& |* `: X. ^) u, h1 \! rinstrument approach, to either continue the ap! o. y7 V% v" m& v4 w to' P" s( V9 j2 R. k' y9 z: X! i DECISION HEIGHT (DH) 2, An altitude used during a - }4 g- X& @7 d4 E1 k! q6 iprecision ap + _7 M" [/ B/ Wla 5 F6 I# d+ d: ]: q" m3 o# V; WD & o0 N* Z( _* ?p- y( q% D( d9 D) g D % t- ?- n, c3 R. JDEFUEL, A method for removing fuel f - Y" j1 N& t1 B0 P分贝, % Y) g; f1 n6 ^% G0 c: x# I以输人与输出功率的比率来推/ d- ^; t! O0 l( }: P& y* G. Z' l6 ^" x f$ D) Y' \& j! s3 P3 l( H) u- f, k* I/ J9 O" W( c H$ d- _% U8 E3 A! p1 {9 l% I! G& Q7 P0 p) @2 N7 J3 L* u9 a; ]. Y' C5 t, \ s4 B" U0 ] 就飞机1 x0 ~" _- p) S 达引导进近时,必须要作出的是继续进近,还是中断进场) g& }3 b* i, D; S8 ^ 复飞决定时的高。 ' D4 ^+ y7 [9 `" H; h! X c决断高(DH)2, + \; @" q( z8 S/ V精密进近时产% o/ p" O1 H% y0 u& R* P 失压, + _3 }. e+ E g6 k) A2 O1 T) O) {1 e排油, * O3 C/ v1 M- m5 g! f7 j3 [: Y用飞 8 V" Q* n5 n. Z0 `& [7 Z% {2 H! c英汉对照民用航空词典B OEING/ b' c* `; S: f' \& v TECHNICAL DICTIONARY 41' [. b" z9 \" _0 B6 v1 K$ a DEFUELING VALVE, A valve in the fuel system for6 V& ?8 ^; e6 m" N$ I+ a0 p efueling the tanks and for transferring fuel between the ! q5 w6 x" f1 o8 ^8 Y @9 HE-ICING, Removing ice after it has formed on aircraft. 9 v, e ]7 O9 i3 j8 BChange or difference.) f; |# g& u- y0 J4 Z EPARTURE CONTROL, A function of an approach 6 k/ S V8 k9 d8 t% o" Wontrol facility providing air traffic control service for 4 j% p9 G! Q! t5 ]5 Z- Neparting IFR and, under certain conditions, VFR; Q) C* M6 {7 T+ Z! D4 ? p) r2 s EMODULATION, The process of retrieving information5 X! ?4 o7 W) L! t- _4 k- d carrier voltage.8 d& h5 ^( ^* v& b9 k' h ation.# B/ J; ?, V! S1 q2 C0 U2 E lic * G" x. X% ?- J+ z. _creasing hydraulic reservoir air pressure to 3 d9 o c( M- h7 F9 c( kmbient pressure.6 J% H, \5 ~/ e# y N' R7 H 箱排油和在燃油箱之间+ R' z2 p5 D, A. a 送燃油。9 _, x2 g3 u, F% @ 冰, 4 v/ z5 V: V& ?除去已凝结在飞机上的冰。 ' i$ Y9 M X! x8 }( @- ^# s* _+ l删去或取消。 ; I) G. b* y9 O7 Q, F+ g量,+ |' Y1 [2 E! \! x" k& B1 Q 变化或差异。" f4 [: Z1 }$ |: s8 w 场控制,* f% t: _+ B2 [. @. Z 给用仪表飞行规则离场,和在某种情况下用目视飞行 1 X% q3 o0 P# a则离场的飞机提供空中交通管制服务的进近管制设施2 K" p* h/ {1 H% x2 P& ^# m# G- k" I3 X- C 调, / y: Z+ ?/ ]5 t电压中获得调制电压的处理过程。 / X% x0 d8 T1 Z) E: s) k环境2 `% o/ u* G, B b0 u- ~/ w5 A5 N 力相同的活门。 6 o6 b! d$ @: X+ v1 H. Ed + d) ~6 l* H/ h" D" T) ?& b; S C# dtanks.9 B: ?3 h8 _) a6 O- R( g+ { D & _ v4 @9 H* z# D0 xDELETE, To remove or cancel. $ N, y+ s( n" A3 s+ LDELTA,6 u L5 |) D0 Z- U i7 q D 0 A& c8 T7 l @( e% L7 jc , K) n; F+ y+ Y7 Kd7 }. D, }+ e: P0 s aircraft. 0 |' `- w: t2 YD ' M/ X5 n' h% J! f(modulation) voltage from a modulated 5 l3 d! Y5 [ Y2 W3 F* h" rDEMODULATOR, A device or circuit which performs9 Q1 E+ R3 }: a the process of demodul B/ e( f" N# O# L m! {. O DEPRESSURIZATION VALVE, A valve in the hydrau% g5 M/ u' k) B system for de; s) d m7 i8 Z- O8 F6 a, @; _" ^! x a ) T, {0 y) C8 i! m排油活门,8 R/ O1 E2 g# l/ x: n6 D7 v# s" F; ] 燃油系统中的活门。用以为燃油 " Q/ w1 T: m' {! N$ J% ^3 A5 L& w9 L9 V- Y& n8 h+ P' P d删除, 8 I, ]2 ?" ?9 n% H, z7 ?/ {+ @$ c4 `' Y/ s" I. R: D+ `- d) g0 g; v1 @3 E9 R* {* Z0 e6 F: P 的一种功能6 d+ I+ c" w' F5 w7 O1 _; ]( V! U, i1 _0 b 从载波 ' X4 l# l# l7 {- L解调器, + l+ Y; z& |) @% Y- X完成解调过程的装置或电路。2 J6 t% |9 Z3 n 减压阀,( Z7 @; c6 i' | H: ~1 U0 { 在液压系统中,将液压油箱空气压力减至与周围0 {9 G' d' C7 i% }; M& z0 f' j j. j( U x) ]" M 英汉对照民用航空词典B OEING3 f$ o% J S! U TECHNICAL DICTIONARY 42 9 I8 ]0 d( w4 [- ~& J% u S QDESCENT, Phase of flight where altitude is decreasing.3 \7 D" f. u5 @3 O5 W1 X ETAILED FLIGHT PLANNING, The calculation of fuel. b8 J) \% p: O% [ nd required for a trip by considering each phase of3 S* v0 w( K! } ight (climb, cruise, descent, reserves). ' d$ ^8 G4 W& G4 bal or 4 F4 y, ~ [$ G2 G3 C9 ^; oETENT SOLENOID, An electrical solenoid used for ) I1 L! _& y4 X4 Lt.8 u! Q, e$ T, A3 G specified course or , c2 ~& o' J6 k1 ~. W9 ]rocedure. n: P* l5 T$ ]4 t" u e.5 X4 p" O9 `: S0 ~ 飞行计划, : _0 `1 [, ^4 A- N5 ^将航班中的每个阶段(如爬升,巡航,下降,备降)都 8 q: G, i7 [$ y# ?+ m人考虑,来计算该航班所需要的燃油量。' {" O/ R9 H0 Z( I9 W 用来感应情况之正常与否的电气装置。 , }1 K9 W9 R9 ~! z0 y定电磁线圈,; ]' B: ~& u7 Q7 q2 V 出接通的电磁线圈。 . d2 |' |+ ]! [% V& T" ]差,3 B( N' j! E" i' c5 P 与指定的航道或程序之差。3 `* G! b3 d* X+ c( \* T 用气压或液压操作的活门机构中的柔性部件。, n" G0 M9 F$ F" C' ] D; R# C- z7 e+ D, k. {2 Q/ ` U* \ a # ~0 _, G. Z' O+ @' `' nfl5 d5 V9 _9 @( o( H9 T; n1 U DETECTOR, An electrical device for sensing norm 9 t8 N+ m7 ^0 r: f% Sabnormal conditions.* T$ F0 |) Y: F# E& E D 6 ~6 v* a5 Q( x% g& acontrolling the engagement of the actuator outpu ( i; [6 `0 y! N' G1 s MDEVIATION, To change from a ! a/ }- C3 `. g h/ |p9 Y; t7 _; c- ~1 `7 }# t& ]' T DIAPHRAGM, A flexible part for operating a valve7 Y0 s4 w5 i* @) r: m1 Y5 f4 w% n mechanism by pressur l/ I' }0 }0 @# M; c, n7 [; E; ^! P下降, + G# e J3 Q! A飞机高度不断降低的飞行阶段。7 e- g+ b4 z' [ 详细 $ c* L6 O R7 }7 a7 z% j& _3 \! `: M3 [5 |- Y* Z 探测器,: v" F+ j( r* a! j* I6 R9 R$ S7 E! g0 |8 \) G+ ~ 用于控制作动器输, [( H- X/ s6 J# b; M( p; ` t" A8 X0 U隔膜, G3 |. x% f: N( n英汉对照民用航空词典B OEING $ `. Y" z+ u( p. t2 _TECHNICAL DICTIONARY 43 / r9 q+ L2 k/ H: Y8 @DIELECTRIC, A material which does not conduct @- A7 s7 J4 H electricity and used between the plates of a capacitor 2 K- W2 [5 J* @. S- n, V8 A(condenser). 1 W5 N. p, s" Q, c- Q; wnother pressure in the same system, measured in $ h: k4 q" c9 V# ?8 i! Aounds per square inch differential (psid).& e! Z8 b, g) m" q$ B0 T IFFUSER, A part of an engine between the& I/ h3 ^/ l% u/ d- |! g ompressor and combustion chamber for reducing the1 r/ L- f' d; I air pressure.9 O5 E6 _9 Z R7 _* x igh 7 p/ L2 g. F- L2 x: N7 A fpulses. ; r9 q8 f# g# p. m9 {ignal that is a close approximation of the original ! E4 ~; \* d( y: B: x: ~0 dignal.) _# j! W7 x0 y# y# V% l IHEDRAL, The angle between the wing reference! d4 G% C" { [. `: c8 n! ` lane and water line.- A2 h$ M b I" x- D- I 的压力,以每平方英寸8 E" U9 ]+ K4 l3 |# a( v 少磅压差计算(psid)。 5 t G) S2 a* `0 w散器, 8 v9 \- n8 v0 c; K5 E发动机内压气机和燃烧室间的一个部件,用来降低空! E" n& }- d! K+ Y 增高空气压力。 # ~+ ? l: b3 V5 C0 O1 e换,& |! H9 Z" ] t+ q' ]1 g; y9 L4 } 的连续可/ _7 G$ Q0 j7 A1 T y" t {3 E (模拟)信号的处理过程。 ) J" a# E$ n0 L! H反角, , V K3 w% i* f" y# a2 {+ S7 d; g, W机翼基准面与水线之间的夹角。: I" Z) Q" Z# h$ i0 C" O( v DIFFERENTIAL PRESSURE, Pressure relative to 3 C; n7 l3 F; _, Q. s8 ra% ^7 U/ `" l7 R p( B% n4 D$ p$ A( S0 ]+ V9 \0 V D/ D3 T( |4 S7 r% E- ]5 z c * n n; T1 p9 M% W& @5 p3 a7 oairflow speed and increasing the: J/ L& R( G/ @, m* ^: ~ DIGITAL, Digital refers to a signal whose amplitude8 Z5 h/ ]4 V% `) e) ~2 _ remains constant for a finite period of time. Digital+ M- [1 r( t2 r' u3 m$ d signals are commonly represented as a series of h * Z0 {9 e- u7 M" @and low. h- t0 X4 c+ N0 U% m DIGITAL-TO-ANALOG, The process of converting a% N7 i- {( U) P1 E digital signal (binary) to a continuously variable (analog); R9 w' U& X& A% g s : A& z4 H6 l( V! d9 t. ys9 \* c I( b, U+ h( i; @ D ' v8 u2 l2 V1 h. _& ]p! C0 {' W9 X4 ]+ J5 N0 {4 V 电介质,! Q* ]7 u1 D# u 一种用于电容器板之间的不导电的材料。 2 }6 F! R- v i) |压差,: i& r* k: G& c: {! S+ n; s 相对于同一系统内另一个压力2 T0 b' T' L1 v+ Z: u" e3 |1 M7 r8 f2 Y9 O0 f8 k, g y/ X7 h 气流速并0 ?. l; d2 g9 Q% u- J 数字式, 6 j/ r6 ~* k+ p& Y2 q% }* C4 v指一种信号。该信号在一定的时间内,振幅保持不变。4 Y5 b7 m! @" x$ c 通常由一系列的高低脉冲表示。$ K _; E, g1 q9 V+ C+ k" e 数一模转. v! V' n3 v8 \0 S 将数字信号(二进制)转换成与原信号相似3 J; I, C. W+ m4 x0 z, ?* R9 k$ b0 Z: C# E8 A L! T9 }$ {6 u, a# H ~英汉对照民用航空词典B OEING ' X, }0 h& w" L: U; Y0 h) _TECHNICAL DICTIONARY 44 + c8 h6 L+ P9 }5 gDILUTER DEMAND REGULATOR, A component in the 8 V" S% |$ ?- A$ |) x# screw oxygen system which mixes air and oxygen and * h- Z5 [) p6 r$ c1 p! s uupplies constant oxygen pressure even if there are : B9 T: t+ u; }4 O& khanges in ambient cockpit pressure.! i' ]3 t3 y' P! e IM, A word value of light. For light control devices - dim : B" m( D5 r. V' ]" S0 T% D6 ethe opposite of bright.2 C$ x S% k# B" [/ f/ q IODE, A device which allows electronic current to flow" U" j* k: Z# E$ ]. `' T: i$ g) m only one direction, v$ y1 C! Z9 A& O' o/ u$ W2 o uid in a reservoir. ) d* M. I- j% x& U% C3 oDIRECT, Straight line flight between two navigational+ u; x/ w k# w aids, fixes, points or any combination thereof. When: f! x( s. r7 {, k used by pilots in describing off-airway routes, points ' N" l7 i, x8 {- _# O2 ~defining direct route segments become compulsory j; y7 y$ x# F3 D1 [. @; @ reporting points unless the aircraft is under radar 9 `9 P6 l3 Q: }' ^5 N) rcontrol. 4 i4 A/ ~* q4 X% a# h8 F$ a; o节器, ! v* d+ j/ T2 Q0 G0 x! _将空气和氧气混合,- G$ @$ i" F( q. j3 l& w 使驾驶舱环境压力改变,它也能提供恒定的氧气压力。 `8 ^' p2 d7 m% J, z# F# B$ B' f! M$ |$ D7 | 一个形容光线亮度的词。对于灯光控制装置,暗的反 9 F* p/ @( Y+ M词是亮。 ' p* N7 y- r3 w0 x) f8 N- h极管,( h$ y& z$ T) L 只允许电流向一个方向流动的电子装置。 2 X( ?# S m9 G( H* k2 r器内液体的量。 - k7 l9 ~$ B8 [0 W! X3 x直飞, 0 k' X8 {$ i7 V! P$ T1 f1 {两个导航台,定位点,导航点,或任何的组合之间的直" A+ v3 |7 r, f8 u 线飞行。在被飞行员用于描述偏置航路时,除了在雷达控1 O5 p/ q" g& W4 \" } 制的情况下,确定直线航段的导航点成为必报点。: d7 D9 T% U* M4 o6 v0 e: a2 q% `* d6 H s # T4 t- |3 Q" j; y! X* c6 gc- W% l2 f, o, n; O, k D3 r) }' }0 N8 M! y is s9 g8 Y! y& L" {6 I2 x1 l% ]D ( K9 T. I% [! Z8 b' o+ u2 fin 1 w0 ?; b% t8 GDIPSTICK, A calibrated rod or stick for measuring a ! o$ ?2 T8 j4 ?9 |5 A5 pquantity of fl' W+ x3 b0 U5 j! l @) c& @2 @ 稀释氧调$ S* V! Z: g3 H. a& @, ? 驾驶舱氧气系统中的一个部件,它 3 Z5 E8 f( U% Z/ @; l! d' d4 L6 r# E( d0 s6 [, O z; V# K% W" q+ X. B( ]) U6 _4 L6 o- |( ^/ C0 t- n5 j3 k7 h/ C6 W# a) Y量尺, . N, N- N. B* a- P' J6 ^校准过的棒或尺,用于测定蓄液/ T( t! A+ ?, Z D. U7 \. g 英汉对照民用航空词典B OEING2 J8 Q6 T( n; J9 w TECHNICAL DICTIONARY 45

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