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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2 b+ R) v" ]& t# L& M$ U o" b 民用航空词典 $ d$ [, J) e/ P( t波音商用飞机集团/ {- Z- z6 t+ c, i BOEING COMMERCIAL AIRPLANE GROUP9 z, J; V; v2 |. [: }+ i 英汉对照民用航空词典B OEING# g, r2 v a: f6 X. @ TECHNICAL DICTIONARY 1 9 X* `. x1 m" G2 e: TA 9 G* ]& Q% y' g& T1 iABEAM (ABM), Beside: An aircraft is abeam a station3 c( q, ]; i: i- d9 r) L when that station is 90° to the right or left of the track of! y P, d7 i( x# n. c) k the aircraft.6 ~: ?5 z- F& \% @1 Q ABSOLUTE ALTITUDE, The actual distance the aircraft8 x! N* ? u2 P8 @+ v is above the ground.% X1 I# R# o8 w0 w) G' O. r V) Y ABSOLUTE PRESSURE, Pressure of a liquid or gas( A; {% H8 T# T8 s6 }6 A+ J1 n9 v measured relative to a vacuum. . |. v* N" b& S. o) UACARS, SEE - AIRCRAFT (OR ARINC) REPORTING - q% K. j! V. U* ^% L% {/ gADDRESSING AND COMMUNICATION SYSTEM * M3 M# p) B% e+ cACCELERATION, The rate of change in velocity with " z; J" N2 Q& \+ rrespect to time.; J. V. A! {! n1 _9 W; _" u ACCESSORY GEARBOX, A part of the engine, 8 _' A) R M$ J4 O; Fmechanically driven by a compressor or an angle 9 ?7 H' J' n6 x" Kgearbox, for driving components necessary for engine , e% o. K( \1 ?* B/ v) ^6 I4 w正切, ; M7 @ A4 t; T8 k1 V Oand airplane operations.- O% p5 h- G2 S6 N 当电台在飞机左侧或右侧方与航迹成90 度时,飞机正 $ v: x; Z" T: Y7 [% M( [6 I* V切电台。 3 w4 e$ ?/ Y2 O( N绝对高度,! B; {+ C# f4 x7 v# }$ D 飞机离地面的实际距离。* [! ^! ]% `, p& I1 L" ^; g 绝对压力,! I3 ~6 M0 }; c, i/ V# D4 }7 { 相对于真空(无压力)测得的液体或气体的压力。 # Q/ L" _3 B! ~1 O8 a0 v飞机通信寻址和报告系统, ! u; A) l, v5 K4 }见Aircraft(or ARINC)Reporting Addressing and2 V0 r' y5 a r* w& t% l' y* |+ { Communication System. 4 e2 z4 R4 f: n' W5 V$ N |5 {加速度, & h+ t/ S$ |3 l0 v随时间变化的速度改变率。' m5 E% K+ i7 C; h) d2 y5 m+ A# P8 e% \* @ 附件齿轮箱,0 S) b; ^3 k) Y9 C2 x3 U8 T$ _ 发动机的一部份,由压气机或伞齿轮箱带动,用来驱动3 P& t9 A! ?+ A- t 一些使发动机和飞机工作的部件 + V1 f* R+ K! j6 m英汉对照民用航空词典B OEING ; m( x9 ^9 V1 ^3 ]3 UTECHNICAL DICTIONARY 2 2 d$ M* x7 @! `9 KACCUMULATOR (NO. 1), A container with hydraulic7 q# A6 i- h) O- _9 q ts when normal hydraulic supply is not 8 g: |8 O! N" g7 E- `9 ^5 ^4 S' svailable. ; V" l: p( B0 @* N' kCCUMULATOR (NO. 2), In a computer, a special \: D* s; a! b- y+ Ftorage register associated with the arithmetic logic unit, / `% L2 ?2 Y3 q1 M6 Tolding the results of a computation or data % `% b+ K) s6 f, t7 v- Z y/ rACTUATOR, A mechanical device operated electrically, n8 L6 s6 o9 Z! \. khydraulically, pneumatically or mechanically for( o* Q# ` J( F( l transmitting motion between components. 5 q6 [ M$ }8 b3 K$ CADC, SEE - AIR DATA COMPUTER% l- m. |& X8 B, C( }/ F' g ADF, SEE - AUTOMATIC DIRECTION FINDER : s) t! ?9 D" M, a/ wADI, Attitude Direction Indicator, An electronic display of 5 T( F7 N& |; n# P/ @airplane attitude information in pitch and roll.; \2 a h8 k4 M# ^, f 蓄压器(NO.1), " h! @8 t7 H% H. j, C含有靠干燥空气或氮气增压的液压油的容器。当没有正 1 S( | t. k- Z) ~% l* s常的液压源可用时,该容器可用以驱动部件。 1 z t5 D4 `# u+ @存储器(NO.2), " p% n% t* ]2 N计算机中,一种与算术逻辑组件有关系的特别存储寄存9 Y( D( k t2 l# s! w; V$ h 器,用来存放运算结果或数据传输。" ^3 W. s9 y* R( w 飞机状态监控系统,) C ?6 E/ {8 O& `+ M( m 见Aircraft Condition Monitoring System 3 w0 _4 b$ G& M* p+ e3 H2 r5 hfluid pressurized by dry air or nitrogen for operation of4 `' j' N8 Y$ @ componen $ e X8 w( X) {7 I* e6 }! R5 Ta K9 S, r5 l0 z0 Z0 G+ j A ( Y O4 y0 I. j3 d; {! is % x+ |+ E/ ^8 J; c% \used for h " V0 G; V8 [ N jtransfer.4 ? D8 P7 b4 ~. h; b1 K ACMS, SEE - AIRCRAFT CONDITION MONITORING J" E$ V/ r* R; a. C8 | SYSTEM .( P9 ?2 {' K( I9 q/ D6 ] 作动筒,, X9 `4 E7 V9 r) m 由电,液压,气源或机械驱动的机械装置,用于传送部 - k: }3 k* q: N, P9 e件之间的运动。1 A0 Y8 u8 E$ n2 s" d' |" d 大气数据计算机, 7 j9 \ M6 ~! `6 E" h见Air Data Computer. 8 O# p8 V! C6 F* K! x L自动定向仪, / o/ _- u g: A5 t; O见Automatic Direction Finder.6 f# [ D8 n0 c6 f0 a" `" S 姿态指引仪,) N$ J5 Z: O2 h. k! s& A8 ^ 用来显示飞机的俯仰姿态和坡度的电子显示。& R$ P0 a0 q5 f6 O0 U 英汉对照民用航空词典B OEING6 K: p# c8 g# V9 a# T TECHNICAL DICTIONARY 37 e9 q& f8 i$ K4 Z: l$ n AERONAUTICAL RADIO INCORPORATED, ARINC is 3 L9 t( F) B( L. O% `0 Y2 U, 6 z/ q# S7 S6 C& inufacturers, and foreign flag airlines. ARINC" I8 q. W% o5 d1 M( t, d4 Y evelops and publishes standards for electronic& g' B* I5 e& h2 i' j: u5 p, F8 @5 m quipment and systems. Z: Y8 Y, H9 k1 y. u% s Q2 Z6 ` GILITY TUNING, The capability of the DME to + y8 Q5 U( i' b3 I' ?lternately tune between two different DME stations in 4 f: S: {9 j0 E4 zrder to get two distance readings from one 5 U8 ^8 U# F' T" a tterrogator." m$ a2 A$ [9 A6 s ~ ge ' L) Z8 q7 C' p7 k- O! x. \& `ILERON FORCE LIMITER, An electro-mechanical ?/ n/ q5 l$ P, c IR CLEANER, A component in the pneumatic system . m$ Q0 X8 T' cupply to the air( `3 f# b5 w# q onditioning system." [* Q8 G) f' V m, K$ M. O 订并出版- w; r- X( ~" J7 X4 w+ B* K 子设备和系统的规范。7 @3 G2 i9 M2 `& V 快速调谐, 1 e/ @$ ?0 _6 \, @1 e0 Q6 G8 }, |机载DME通过交替调谐两部地面DME电台以测得来自 0 q2 u2 X7 _+ B" {, F" S( k同一台询问机的两个距离数据的能力。 ' s5 Z7 ^, Z8 W8 s8 r翼操纵力限制器, ' ?& C1 |* n; h0 V" A& L" h装置。在自动驾驶工作期间,用来限制驾驶盘9 [ S" T S6 W1 d. Q; g 气清洁器, 0 l& Q% E' O; d# i; R% P5 |0 m% P部件。用于去除供空调系统使用的发9 I- E3 I8 t. N! O& u" w O a corporation whose principal stockholders are United' N; c1 u9 U, R8 F( o States scheduled airlines, air transport companies - S! r' F! r& r1 S8 D2 faircraft ma ( e) b% Y) X5 r) x! zd* ^5 F& N& k$ y+ d b e+ C( ~$ ~3 l: Q* G4 `8 w A 1 Y1 l: N4 h9 v5 {7 [$ |$ d5 _$ Fa* E K# n2 x, ]- H8 X o ; m S& h! S- Oin" L* r. E; A! o0 Q$ J9 Q AILERON, A hinged moveable part on the trailing ed ! O! b% d8 l- aof each wing for airplane roll (wing up and wing down) 9 [: r' c& W# d+ R3 icontrol. 4 H7 V0 p! b' c6 Q1 t9 mA : w" J4 S& D& @device for limiting the control wheel movement by the1 b7 e! M! {( m2 \& ~* u autopilot during autopilot operation. 2 R; N, D7 R# Q8 F$ a' w+ {4 OA1 {8 ]3 E$ ~! ?6 u0 {: R8 q for removing dirt from the engine air s: }1 G8 s( s% O1 T7 P1 i# m& [ c D% G; a/ o6 [; z7 S6 c% q5 V航空无线电公司,7 C$ l4 @" l2 }8 ?( A' i 主要股东为美国定期的航空公司、航空运输公司、飞机 2 j/ V; j4 M9 k6 `1 g3 J制造厂和外国领队航空公司的组织。其目的是制 5 n! _, W' n s% G% t( Q2 m6 Z- A" j6 b7 s% c副翼, ' D5 Y2 g9 }: K- r& {铰连在每个机翼后缘的可动部件,用于控制飞机的滚转 5 @8 T5 k3 M5 G(机翼向上和向下)。 6 Z5 \; o3 f" I% r7 e6 O' o' c: _. Y2 s0 v 一种机电- J! K1 f c" ]3 b 的动作量。2 W' G T4 t8 j0 Y! w4 i4 [7 }& b8 Y* U3 C 气源系统里的一个) f* G1 m+ o7 F4 c d" e; ] 动机引气中的灰尘。$ x1 i% N6 p/ _+ e 英汉对照民用航空词典B OEING8 {5 f/ O; g; P+ E Y TECHNICAL DICTIONARY 4 : a" Y! p& s* @, [AIRPORT ELEVATION/FIELD ELEVATION, The 2 }2 a- D5 A5 G3 { h. L# m0 xhighest point of an airport's usable runways measured ' j2 D. F3 ]& f2 Win feet from mean sea level. In a few countries, the- t& W/ C$ o& _! b a7 ?3 k# f airport elevation is determined at the airport reference * T, U4 y( L2 r: u: f8 ]; K8 E7 ~; upoint. & `# m' w }( L5 N* f; `# N: ZAIR ROUTE TRAFFIC CONTROL CENTER (ARTCC), ! h" ]7 z E2 ~+ G# }ervice4 `( I2 A3 W( S4 L" ~4 }3 m+ u5 x" l ase of 8 P! Q. a) Z2 d. t% xus flow of air traffic./ V5 y# m# y# q4 p IR CYCLE MACHINE, A compressor and turbine on a9 C1 K4 q" L( z ommon shaft for cooling the air in an air conditioning3 |6 v9 m: h( v3 M! R ystem. The air is cooled by expansion from high to low 6 ]5 H$ }* I% j: j. w' w. B; Fressure across the turbine. The compressor is driven / N, X, h! s; r0 Vy the turbine. " j0 }; |/ o8 E8 B$ m中航路交通管制中心(ARTCC),* C9 O8 |% l. `7 f6 F. n+ ? 域范围内使用仪表飞行规则飞行的飞机提 9 D/ Y5 w2 l( K0 j! {# W管制(ATC),2 Y4 X4 B1 ?2 L5 K5 y 涡轮冷却器,6 o$ S# j A! a% I 是装在同一的压气机和涡轮,用于冷却空调系 ( q: t5 s* e( ^统中的空气。气经压气机压缩后,由热交换器移去热量, E; `: I; Z' [& m2 r" i$ N 然后经过涡轮令涡轮带动压气机。通过涡轮之空气,温 8 {, [3 u6 h$ ?# b6 f3 I# F3 z度下降。 & D$ Q7 l+ a3 I9 z6 P+ s( u/ QA facility established to provide air traffic control s ) y+ K& }( O; n/ c0 E u% f: _to aircraft operating on IFR flight plans within controlled2 C1 [" Q- F4 _% t1 i/ V airspace and principally during the enroute ph6 W V. j7 U8 ?, p" n* S- u. C flight. % N1 }+ `, J) F4 K J# d2 ]" pAIR TRAFFIC CONTROL (ATC), A service operated by 2 W8 S6 y3 P: D4 P6 I2 Qappropriate authority to promote the safe, orderly and' _# X/ g) T0 z expeditio1 g/ r$ }2 _* U( `% l! j7 @ A # X9 n4 J7 T, }5 ^7 mc - Z! i, a+ r7 r! t& |5 _, ?! ks& v, @) S. x8 p' a" x8 O& ~" F p : R1 r4 r. R- W1 s* }, ]b 6 z0 {1 o( {" H+ K. I {; X机场标高, : e( I ]% B9 o" E2 R$ }3 ?指海平面与机场可用跑道最高点之间的距离,单位是英* |9 F, f1 U& ~- a3 M* J 尺。有几个国家的机场标高是由机场基准点而决定的。 + B. P3 E* d; f. o" v8 @& l0 j1 e9 ^2 j$ D9 [" G9 c给在控制空6 X9 e9 F# I+ H* ? 供空中交通管制服务的站台。6 o0 _$ \/ r6 a0 j" V$ f: ]% ^ 空中交通 + h% [+ f/ N% U# j2 o4 A* l由有关当局管理,旨在促进安全,秩序,和效率的空中2 A% n5 T V- e& w- [ 交通服务。 . s3 N3 R. q; l. ]# O$ @根转轴上 * q* Q8 B( [, y3 ^. C" j0 N# J4 y# c, i s0 g) s c6 s$ V1 |6 G英汉对照民用航空词典B OEING4 R0 u" c9 y) g$ o: ? TECHNICAL 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) u5 Q: o9 y) Z data information, such as altitude and airspeed, based 9 h! d* Z, F/ l& P* ~" Lon pressure and temperature measurements. 2 H Z2 j3 D/ a6 ees air - c9 D+ t" f5 N% w7 R5 m( @8 J9 }# k! |IR TRAFFIC CONTROL, A system comprised of& D m% H) ~% [+ q# D round and airborne components used to identify, track * u6 a# u9 Z5 S. d" P5 q, wOUND SENSOR, An electrical device operated ) d, U3 c* A1 A' Z! M% [6 _6 Wy the landing gear, which transmits on ground/in air , p! m+ t; t8 N3 z% q: bformation for system operation in flight or on the Q# c- P/ S' P. K: t+ k& } round.8 _: @* w6 ]" ?, y: e IRBORNE VIBRATION MONITOR, The AVM takes1 x$ u+ c5 N4 E4 }; N. u& C/ q e signal from the engine mounted accelerometer and ( }: e3 {" {8 p malculates the vibration on that engine. ! ?- B& [, l4 F: ?) @corridor equipped with radio navigation* r4 Y; o! C1 L8 }' z3 K9 P# Z* o aids.* P$ T& I2 G- v& Y8 w/ J AIRCRAFT (or ARINC) COMMUNICATIONS$ H: S. N. `. l+ s/ L1 h+ l ADDRESSING AND REPORTING SYSTEM, An9 G7 z9 E r1 Q) M1 E, H7 U2 j7 @ addressable digital data link system which permits the 2 Q# R; }* H( t% Q( N3 U5 |exchange of data and messages between an aircraft& |& j) y5 [- ?" G and a ground-based operations center over a radio ' e8 q, ?2 y: A% Y, L/ Znetwork. 9 j4 H. T' C) XAIRCRAFT CONDITION MONITORING SYSTEM, A* ^# s9 f- O" @* b system of sensors and recorders to monitor various5 q: M: T/ t8 r" A: I airplane systems' performance and status.% I0 t- D5 J3 N3 w! I 机,& O% U3 Q k, F& Z/ { 中交通管制,7 Y/ u" w' Y X6 }" L e 一个由地面设备和机载设备组成的系统。用来对飞机进 8 M$ Q7 B7 I1 x/ c/ C1 |地传感器, & n G$ m% G& G0 x一个由起落架操作的电气装置。用于给空中或地面的飞% ~% P7 ^, W# A# [ 系统运作传输地面/空中信息。(有些系统只能在地面+ E0 K1 S: S/ G% J; U& d 用) & E5 g5 \9 E; i& A1 z3 v; ], B载振动监测器(AVM), , s5 h% N0 p% A R j) mAVM从装在发动机上的加速器取得信号后计算出该发) _& ]7 [+ i. h, L% [ 机上的振动。 5 I3 y1 P' h2 t5 `" d7 Y- ~% e a( N式建立的控制区域,内有无线电导航设备。6 ~$ Y- C3 u( {) v" s 飞机通讯寻址和报告系统,+ @! l! d$ e' S7 g+ | N- f 有种可寻址的数据通讯系统。利用该系统可使飞机与地, l' `( y8 A2 O" V2 T# D 面操作中心通过无线电网络进行数据和信息的交换。 " k/ ?7 w/ C8 o0 P0 ~8 m% J飞机状态监控系统, 6 g0 `0 q5 `8 Y9 J3 N2 \4 ^" P9 L一个利用传感器和记录仪对各种飞机系统的性能以及 ; P0 p6 l8 _. c) }状态进行监控的系统。 ( Q# E! C3 y; `& U9 FA, d8 ?0 v. k9 D& v& j/ V8 P3 R g . \ K: ~# f2 E: t( Gand locate aircraft. 1 x2 e) d6 L# k6 FAIR/GR , _4 B" ^3 x% l5 d Db; o g \& d; f: e5 Y in # y+ P% n( `1 d: R6 w; a+ `g 3 T/ g9 K7 `* Z R. F0 C2 PA % u% N0 R {, \3 H0 u, ~th * [4 X P% W5 T3 U3 Q. A. @c2 k( l4 l+ L s0 `: o) q AIR WAY, A control area or portion thereof established 9 z4 C8 h. a Qin the form of a ' l% U: o; x% E2 d" x3 l5 U大气数据计算/ s: ]6 c g# a4 I3 r6 H: W 根据量取压力和温度而产生大气数据资料(高度、空速 1 r& K; b& ]# G ^# [等)的计算机。 9 O) r% b; Z1 Z! A0 t0 Q( u1 ]6 X$ D: |6 b6 n1 v, D7 r8 W行识别,跟踪和定位。 3 I. `: F$ U+ v; m2 D6 E7 R: k* g4 @! Z4 u) c3 J$ i: a: F9 k/ P& ^! D7 H 使 - o( J8 d( |& d0 {) X {0 B% ]/ N- @+ h! n. C" ?5 a# w+ u! e) S$ s* d- t 航线, ) N( u" C; q n以走廊形 # \! q: j) M8 n! o+ Z英汉对照民用航空词典B OEING 0 y; D ]) |. W L7 ZTECHNICAL DICTIONARY 6: U' n' Z! e, Z AIRFOIL, A surface designed to obtain a useful reaction,3 g0 X) \2 D& h such as lift, from the air through which it moves. Wings,* W" P7 T# H$ m" A# a- i% W stabilizers and control surfaces are airfoils. 6 V% d! E5 n: W* G! n3 i# OAIRSPEED (IDS, TDS), The speed of the airplane . ]0 J3 i2 K* x# B5 m5 a# ^3 zrough the air.! h) e4 v$ \+ D7 I1 h D INDEX, An adjustable pointer on the + F$ @/ O/ f1 M1 i( ?$ r# C' N2 virspeed indicator.# l) A* A$ h% k' o and legal ability , e( y! q' [0 d9 F" T3 W: i3 j; gfly. 9 J* t# `7 S4 x* \5 Dm, for example, the procedure for finding the/ H6 _8 L2 G6 D6 `: G8 F& F1 D quare root of a number. $ R8 r- j1 W3 r \4 jy 4 e0 k: m5 O) B/ @re, wind,' O6 Z: d/ ?$ b! z7 k and aircraft flap setting. 4 h& g; C) \* y3 m: }. u是翼面。" Q0 o* ?8 Z( [6 _ 速, , I6 ~! I0 B" B2 Q飞机在空气中运动的速度。 6 L) a M, P4 U$ M# C) S" q2 ^+ J3 F0 _$ C' W; @( x9 H 在空速表上可以调整的指针。+ U0 y5 T8 d/ O( s9 a 机械飞行能力、和合法性的飞机状态。8 u' ]* L& L9 ~; h! O! z* G 一步一步的解题方法。例如,计算一个数的平方根的步 , a$ X* f' W- n; j' b) Q0 c( ]' }3 j. ]. h7 @9 d6 h% e3 z. X6 f% v" F& } 资料的法定文件。( v4 I! `% ~% G/ o# K 翼位置成函数关系。6 T4 d' B2 c+ Q8 p9 U( ~5 L2 F th* Z& P% r& F& H. X9 s2 Q) U AIRSPEE ) T: |* U2 ^, F" F" E* k. ^7 ya 5 g; W% C( z3 t. o/ w1 pAIRWORTHINESS, The condition of the aircraft with4 }5 s; y( X0 e2 y, e( a; _/ [; E respect to its aerodynamic, mechanical,3 U5 s; d2 e) m3 f7 { to* l3 z* a( M5 J6 n ALGORITHM, A step-by-step procedure for solving a( a6 X2 T6 l% }5 Y9 o a, P* A8 U proble% z" Y' t% D" {2 o s 5 m7 ^7 U( S1 z) l( N+ J1 L1 l' s9 aAIRPLANE FLIGHT MANUAL (AFM), The legal : \ E' i! K: s8 @/ Pdocument containing performance and operating limits, ) g$ D A w& a; m/ coperating procedures, and takeoff and landing8 E- Q- l1 l1 d' Q- I performance." R- Q* F7 `: i' D {( v5 T7 J AIRPORT ANALYSIS, A comprehensive set of takeoff 5 x' T) M$ K+ _- b! Fweight limitations for a given airport runway, generall 3 `* c3 F/ A& t) m2 F; Mpresented as a function of airport temperatu 0 y: V& |- O. o) d5 c翼面,: ^% }+ x4 X7 S+ N& S 用以从气流中获得反作用力(如升力)的表面。机翼, 5 g: [# l( G7 [& q3 R安定面和操纵面都6 N, c# g) A; C/ ]/ r$ Y# B- o) W6 M) p7 k" |3 v" D空速指标 2 y8 {* |$ M4 R: C8 t6 V# q d, z适航性, # Y- H* p& K; O有关气动能力、 3 N1 t& R6 L1 d% H$ q" a演算法,6 B& _" N) K8 ?. e+ F, _9 `! x" M8 U/ t# U飞机飞行手册(AFM),- D W8 B( w% E6 Y, r& q2 X 包合性能极限,操作极限,操作程序,起飞和着陆性) J, f% R! ]; p1 m2 R0 h( C# H/ `' @2 B& {; l) ^机场分析,/ C; `! Z3 F) W0 ]* X0 m; ] 一套针对给定的机场跑道的详细重量限制资料。通常与7 E ?: q1 t' a, R. S2 e 机场温度、风、和飞机襟 G) ]( z9 S' U' O% ]; b; a英汉对照民用航空词典B OEING' P# X8 a$ \8 J* ^ TECHNICAL DICTIONARY 7 5 x+ D- Q" k% R; y# m- ~) g" c/ p NAIRSPEED BUGS, Adjustable pointers on the airspeed$ l* }+ ^ ?( N; T" E6 v5 `$ S indicator. L8 M4 Q' a- w6 E: q* n7 A# R) _ALLOY, A mixture of a basic metal and small amounts+ H& X) {: Q2 c6 c- F# Y f other metals to change the properties of the basic9 P9 I) N2 d& @& A etal. ) N5 Y+ M7 T v1 [7 y. kMinimum airplane speed. 1 y4 x5 i0 A+ Z7 P- }e of4 L! n- s7 w2 G2 X itting airplane angle relative to ; @# Y3 G1 D: \0 e, i" hirstream for the stall warning system.& z9 W2 }1 N6 ? another.' z: X& I8 Z7 n: Z. I; a LTERNATE , An additional airport selected during0 d: Q% A* m: L9 D5 U4 p! P& d$ w) q2 |* u1 A* q T# Q合金,/ Q+ ] V% Z5 P# {& `6 Y7 l( X 在金属中加人少量其他金属,而改变其性质的一种金属 8 L% o0 E& W4 h' B; E$ M合物。- |) x$ W% }7 G4 v) _6 ?. O 飞机的最小速度。$ _- D2 v [: `5 O 速警告系统传输飞机对 - |/ A d6 q3 c流的相对角度。5 n( k1 w( f$ R! L3 o) U 由一个状况改换到另一个。3 v8 m0 a; E7 _8 l 降场,2 A4 E) k; H, Q1 h& x+ J D( V9 u 划时,除了目标机场之外,所选的另一个机0 j6 `+ y& J% e7 C6 F o 0 J. h5 e8 j# m# q5 z. Gm 2 [% x3 `2 D' W& I4 rALPHA SPEED,. s7 u0 E0 [7 Q2 T/ G. M ALPHA VANE, A small moveable airfoil on the sid! t+ d; l. |: k( i$ J the fuselage transm* r. p5 X J/ o9 A1 z8 v2 p a - w {+ i/ u8 H2 O( sALTERNATE, To change from one condition to 5 l' z" O0 V4 X9 `# r3 ]A 0 w3 g, o1 U) r6 A R Hflight planning, usually near the destination airport, to be 5 q: _9 L! u; Sused when it is desirable to divert from the original 5 @3 T% x5 ]) |# `destination airport.6 @) t Z1 Z. k* ~ 空速游标$ m+ o& D2 s0 }1 i 空速表上的可调指标。1 K& w' v% Z, | I% J! p8 s6 Q C9 D' x迎角速度, - H2 f+ C/ k8 l. v: V2 `) Y. j迎角叶片, 6 q' V# N$ M7 i8 e+ A1 G- E- k位于机身侧的可动小翼面。为失& P! g& {3 g+ k# L! m4 R' b+ z; n: e3 y, J+ q9 ^5 I交替, - o4 R5 L" f: R6 z( U9 m+ z3 P w( G8 Z. T; Q1 a制订飞行计 4 S u: f+ }. g场。通常在目标机场附近,以备不去目标机场时,改降之 8 L% F0 u0 L2 Z5 @% @, k3 N用。 ; j+ s, P; h, Y, H5 U英汉对照民用航空词典B OEING! J* m; g! W+ _: U$ t! P TECHNICAL DICTIONARY 8) p$ b& q& _( s# `, M& D* {, K ALTERNATE AERODROME, An aerodrome to which 1 V# n) z$ u+ d2 y4 E: Gan aircraft may proceed when it becomes either/ B0 m. K: ]) C7 G) @ possible or inadvisable to proceed to or land at the 2 Y% E" N8 l# Q; I& [. Yerodrome of intended landing. - \1 G& U$ r4 u3 y9 z6 GTER SETTING, The adjustment of the altimeter 7 Y; T/ w. e/ r; l( Haccount for local variations in atmospheric pressure.2 }9 b) h% t! k8 u LTITUDE ACQUIRE, A digital flight control system. Q0 U( b9 Z# w# }2 U! i ode to transition from climb (or descend) to level flight.' H6 n( }0 \$ [8 b1 ]4 g LTITUDE ALERT, A flight deck alert occuring when the: Z) R1 U& D' t- q9 U irplane approaches or departs a selected altitude., p8 k$ \, j; s. s t LTITUDE CAPABILITY, The maximum altitude at) r% g& t/ P; h2 L$ t8 ^- L hich the airplane can be flown at for a given thrust, 1 z$ l; q. \4 u6 j$ E4 X7 mpeed and atmosphere condition.( \7 r9 |2 M$ p! ~ LTITUDE HOLD (ALT HOLD), A mode of the autopilot ! e) G/ Q% b* {r flight director to maintain a selected altitude. 4 S& ]" R4 t o7 n) C: r% Dirplane's altitude during VNAV operation. 5 ~1 @& k: U# e' U: _0 v机场着陆时,可作着陆使用的( x A1 Q3 z# r, K! N+ N( h 场。( a) t; L/ h) o9 I G8 E0 o# D, X) q6 h) t3 U: l0 B' t根据当地大气压力变化而对高度表所做的调整。2 V9 x5 x: s& W2 |7 F 一种数字式飞行操纵系统,从爬升(或下降)改平的模; U, V! Z5 A: N/ d1 O% O5 A( _# ~4 j2 n' ~5 b度警告,- r3 U: p3 U/ q& J0 o* P 当飞机接近或偏离选定高度时,所出现的驾驶舱警告。 9 z& C, O7 q. `8 G% U M高度能力,: E0 o1 C3 N+ t0 y 在给定的推力,速度和大气状况下,飞机能飞达的最大1 S g' a% M3 }* Q+ r h 高度。 ' L1 {0 j7 ~4 B, l5 g4 h( r# L) [高度保持(ALT HOLD),7 s) C2 @! c ]6 I7 J 自动驾驶仪或飞行指引仪保持在选定高度的一种方式。 ( y9 ?% t$ {# p1 Y1 t8 Y6 M* g5 _; l7 K* t- U. R; M5 M, i( B' _ 员对飞行高度的控制。 7 N0 h) ?) D8 `( j0 him* N' Z0 B; C: t. u* f) c a% A+ ~( r8 w& O1 Y/ O4 b ALTIME. s! w4 P& Z/ H- G" X0 T to9 n' n3 [& p4 C4 F" B A' u, |, E8 [- K; u- G7 ~ m 3 \$ _; |/ f' C+ |5 h& Z& fA4 h6 m m/ [( X$ i a ' C `- s/ a t ~A$ k* n" T9 ?# D1 n0 E w ' k" r9 E: w8 s; K+ w1 y$ s; Is: z: P$ J& U' w5 d f0 H4 E% X+ J A 2 |, D8 H! k1 {' d& X! m6 |# Jo * t0 l5 t. D$ S7 F/ {- `* c) `' KALTITUDE INTERVENTION, Pilot control of the Y( l$ B& m8 U; M6 e3 v$ a. d a) W, a9 V: X/ g, l/ W9 [7 g& s/ Q1 a AMBIENT, The surrounding atmosphere./ J9 U7 r- x# n+ {; b/ I 备用机场, 7 }/ S! f- Y% J当不可能或不适宜在预选5 y" a% u! w% o+ o: s2 ]! X9 J' Y$ k/ ?& S' b" o& g4 t$ s { 高度表设定( c5 e9 r0 R8 z 高度截获,$ i8 ? g7 ]$ T& L* U9 g: g, m+ S b' r0 G- c* p8 @: l7 ]' h: G D. T高度干预: O3 E& e0 ~$ P 在垂直导航工作过程中,飞行; _6 T, P* A" C1 k7 I2 w 周围环境(地面气层), : G8 }* |4 b* h& g. l" [" K物体周围的环境(特别指大气)。 - G, Y, O V* K! X" g% K英汉对照民用航空词典B OEING ! c# \/ T' X3 E' TTECHNICAL DICTIONARY 9 6 z& T* _8 P% e# m" z$ NAMBIENT PRESSURE, Pressure of air surrounding an3 q9 n; V0 Z% @ object, measured in pounds per square inch (psi) . M& } ^( b* k MBIENT TEMPERATURE, Temperature of air 8 T+ X6 t* \) n- h- Vmpere. 5 u, q6 h( J! Surrent waveform.9 _- R2 j* Z2 C6 u/ P) z4 i) p2 |" f g an / H/ N# ^: X) Y7 ]- s ]/ ^8 gnalog signal to a digital signal.& o* g2 b. \) J; a7 b* O$ Z ore inputs4 B7 v5 m6 a7 i* G, c; \& l; ~8 ? f binary digital information and one output. The output2 u3 A3 x& m. x4 m 1 only when all of the inputs are 1. The output is 0 $ z- h- i* [4 ^: Vhen any one or more inputs are 0. : H- X! Q2 r. y6 A `6 M( d4 a8 _; M面气压),5 e+ W. Y( E: j' S5 i& _# ? 境温度,% R0 _+ }6 a k) U 气温度,用摄氏度(°C)或华氏(°F)来1 ~5 k& N# J! [3 N, t: ^0 C" Z1 w" K1 `4 M3 G) ` N' V' S3 Z1 [电压或电流波形的幅度。4 [- A% F1 o7 j" U( h- d+ y 性变化的信号来工作,或产生连续性变化的信号7 H$ I: }: M7 Z7 Q, A, v& p$ T4 @ 统。 ; _; v5 u M7 S将模拟式信号,转换成数值式。 ; {: |/ ~) {* S4 J' k) e) i0 |: p一种有两个或两个以上的二进位数字信息输人,一个输! U* A2 J/ D9 K* h! z3 G 的装置或电路。当所有输人为1,输出为1。当任何一个$ O7 _; p2 ?/ o3 r8 _: u8 T 一个以上的输人为0时,输出为0。" L% Z( T" {- ?( O A 1 l9 E! D+ R0 m) \+ G; fsurrounding an object, measured in degrees Celsius) Y, \- @( Z, h- ]8 ]( h. N* m (°C)or degrees Fahrenheit (°F).- H! [ B. H0 y* `4 b, R; C AMPERE, A unit of electrical current. One volt across 1 Q! i7 o- p) V8 F1 M& Gone ohm of resistance causes current flow of one ( s, p& N3 a: \* @a- j2 H' z9 X0 o- L$ K; j9 x& b AMPLITUDE, The size or magnitude of a voltage or9 c/ b1 O' H& `$ ]4 g5 a c: E c 7 a4 B" Q, h D- d* i$ F: sANALOG, Quantities or representations that are - Z; F+ m! i9 t/ M% ^variable over a continuous range. / v& @8 n0 N% p9 A" R4 XANALOG-TO-DIGITAL, The process of convertin9 B+ [/ _) M0 R! b$ B+ y# K9 G a * \& W2 u* I7 X* q' c* }AND GATE, A device or circuit with two or m$ w/ {. k5 {7 O- m- l2 E o& S2 O' ^. m% ] is 2 q4 I/ e* n: F j# a% K1 Pw * \! [4 R6 @$ r环境压力(地 - g3 T$ {7 h4 A% z6 t5 @物体周围的空气压力,用每平方英寸多少磅(psi)来: _( @, j' S5 y* j% E; ] 度量。. o, x! K8 [- \* X, X4 b7 B: ?+ a' w; F* C+ j6 \$ i6 |# k* c物体周围的空. Q2 Y1 o# C- G) O0 d1 O: z 度量。 - w, v) P4 ?( j! _# A" `安培,; h4 j' Z, O& }. ] 电流的单位。 ! i+ h. x, i0 N1伏电压在1欧姆的电阻上所产生的电流为* I* f" m8 d5 Q4 Q# ]9 \ 1安培9 t c/ q9 W$ D( Z& V4 I 振幅, " ?3 t1 @+ f* L* z" n模拟式,* W; L" I( Q6 O% N/ b J* \- I 用连续 7 c6 P! h( q1 i4 `$ }: p8 M: j. m+ k2 G 从模拟式到数字式, # B! }% {5 F* K+ k& g与门, 8 h& Q" O3 U/ s8 a5 u& }1 A4 z& E# I3 c2 J, S) c; T% t) D: D0 L6 l, t/ o英汉对照民用航空词典B OEING ; W" H& X6 W- _. r h( E7 bTECHNICAL DICTIONARY 10 ; [* \/ p% |; P# {* l9 W$ LANEROID, A sealed flexible device containing air at low: M0 h0 [5 E; e8 j2 H- Z# X2 h pressure, which expands or contracts during change of6 f: }$ E( J6 Z9 U$ ~0 R3 p$ ] ressure outside the device. ! B2 w/ y+ |# N9 Y7 Nically+ W: [# O; H& z5 F6 `4 W5 L2 q r changing the direction f5 d/ c! e$ _+ ?) P+ P f drive.4 A1 G! l1 t8 {' \ of the wing chord in5 v' f: a1 z# G' I+ b, H lation to the free stream airflow as it moves forward 9 A1 K$ K& X" E# _rough the air. ' c& O5 ]# x; z/ \& Z9 Dal axis of the& F* W+ F6 e3 u% O8 e0 s! m aircraft. 8 p! ?& A& {* k8 }; Y* Z胀或收缩。 . R; G0 f! O& ?' u+ u* Q箱。是改变驱动方向的机械装置。$ A8 c+ C# Z0 p6 g7 O+ l" Y 机翼翼弦在空气中向前运动时与自由气流之间的夹角。 . l4 C% a& {8 n( m. J4 r- L$ T \0 Q4 u+ N: jp % x0 ~9 q# N' wANGLE GEARBOX, A part of an engine, mechan 9 T& u* }1 c' ~& s8 ]% R7 Z" ndriven by the compressor, which drives the accessory1 w* g) L( }- S5 E) s gearbox. A mechanical device fo % [ N! }$ i0 m7 ?9 G! j" n% Bo9 n' H, Y C: \2 C ANGLE OF ATTACK, The angle% t% x5 y8 l9 s/ C2 K re % R+ p1 x$ W/ q/ s0 gth ' T9 Z9 k2 u O! N% L; _& nANGLE OF INCIDENCE, The acute angle which the$ g; v3 {7 k/ w: O- Y F wing chord makes with the longitudin % B8 }5 D4 n! x, r3 V" F; @6 d膜盒," R8 I, p* g* M' }8 V$ L* I0 I 内含低压空气的密封弹性装置。当它周围的压力变化 5 d6 @8 [ r" s p# j' m$ \时,会膨 ) j& _& s1 P% T h: N/ l伞齿轮箱,, Q# j8 G- r* X! X0 j# i# I7 M 发动机的一部分。被压气机以机械方式驱动,然后驱动& v( T: Q% v+ } w- a( x7 \ 附件齿轮 0 _& b! j! _8 ^6 Z+ i6 [" K+ M3 G迎角, P& e4 Q& Q, t4 v0 q安装角, ' P: U- T8 L0 h飞机的纵轴与机翼弦线所形成的锐角 % A4 p- O# N9 L2 B2 Z, Q2 {英汉对照民用航空词典B OEING & j# b) K' d4 P0 o( S" mTECHNICAL DICTIONARY 11& |% T5 R) ~6 [3 r& ~+ m ANNUNCIATIONS, Audio or visual indications used to 2 `+ C5 v$ V- y: Q. _& S' j8 Z( Tcall attention to an event that has taken place. - O- E) Q2 J! X# rANNUNCIATOR, A visual device consisting of a number ( I7 J7 v/ X* aly. + O" c9 H' l, J7 ]3 N( oANODE, The element toward which the principal stream & z9 Y2 b" P; r& }: hof electrons flows.2 O; h0 D3 Q' N. Q% m D3 X ANOMALY, Not normal./ T4 B9 C# ]% d ANTENNA, A device which, used in conjunction with a / S/ J3 V$ W: Ptransmitter or receiver, is used for radiating or receiving! o$ |( [7 K5 U) z) {* c1 _1 x radio waves.% e. t7 Y: V. ]# B NTI-ICING, A method of preventing ice formation on 2 M4 B+ e( _( Z. ke wing leading edges and engine nacelles.- c! L. B) b' P NTI-SKID, A system for providing maximum braking% s/ k `8 J/ D+ {3 q4 m ithout skidding for any runway condition. Anti-skid % Y2 C0 g R1 `- h N& Q& J( domponents are part of the brake system.9 P _1 z5 e$ c3 _) }" W. U: K( h 告, - ?" |/ I; G* v, i2 I, M当发生事件时,以声音或目视指示形成的提示信号。 " G. ]! j' W: }; I% H7 D: s {/ `与之有关的电路的现有情况或已存在的% K1 M5 D* N2 l0 m) @- M+ Q @ F- R正极," b2 n0 j2 I+ \/ ^9 T 主电子流向的极位。 ( u# |0 o# M5 A异常,# v" Q# u" h' K4 p! R 不正常。 ' k; e- }1 H5 ^8 I- o1 y k/ u# x, I7 {天线, 4 A3 g+ p/ R. |( }9 R7 | h- P一种与发射机或接收机共同工作来发射或接收无线电 6 I5 l3 a8 F+ V% x+ X) X7 G9 |波的装置。% H9 {' ~% |& f' @+ [* p 冰, ' {" ~4 S- \2 m6 U, P9 B+ z6 `3 t防滑系统, 1 h, o. w) c4 z* Y% @一种在任何跑道状况下,都能提供最大的刹车能力而不 1 q: e- b3 a$ b( i2 x+ ]使轮胎打滑的系统。防滑部件是刹车系统的一部分。4 F/ i: m$ p1 K7 v' ] of lights. Each light indicates the condition which exists* G2 M& i2 e2 |$ d9 N3 ~ or has existed in an associated circuit and is labeled+ O; l1 D# ?+ V according + Y& a9 X# l5 QA + W! l6 x- L0 l1 c- hth * o7 J7 c- ^+ ^1 ^A 3 W, y, P( F' H; }- m3 nw : e! z. j9 x% E- U. I, ^3 x, E4 fc % l5 S: W- @* g- Y0 _, x2 F' S& v信号牌, % n2 r, M$ w, m9 v" T6 W* h由一系列指示灯组成的目视装置。每个指示灯都有相应 ( j. a1 E1 ?% w, X* F; s2 n的标记,用来显示' \: {! q4 k6 T" i; T7 u+ u# B1 r: F% @7 v0 p x* y2 d5 T, D7 z7 g防止机翼前沿和发动机短舱结冰的一种方法。 ( x. I4 ^, W8 e j英汉对照民用航空词典B OEING8 o0 _$ h( h7 H1 H. k' ?4 \ TECHNICAL DICTIONARY 12 . r( K& |8 O- K* qAPPENDIX, A supplement to the Airplane Flight Manual u9 @' S& V2 c tained in the basic manual. A 3 C Y( N3 G+ k' D5 q1 Y; rollection of supplementary material at the end of a6 n K: `$ v5 U2 d* ^; ]" S ook. 4 W! m& C6 h0 ^8 U" kof the 0 S3 ]* I: d3 u0 _8 Q" `* frsion link on the landing gear. ( u' Q& Q2 f- p" a! S/ iAPPROACH MODE, An autopilot/flight director mode$ I! F r8 I% A5 t/ m, |' Z which is a combination of localizer for roll control and* l( o" b7 l* D* R; l% R2 |4 @ glide slope for pitch control. This mode is used when full # {# Q3 M3 f x( m W% {instrument landing system is available.( z% m! Q8 h( A) x: y2 I APU, SEE - AUXILIARY POWER UNIT 9 Y9 X$ x. m) g/ r- fARINC, SEE - AERONAUTICAL RADIO 1 h( F5 d) V% l" Q9 v! y' UINCORPORATED . U0 A* A+ n) m% z# A$ n* n: `ARM, To make ready for operation.6 V$ v( k2 [. J: e 附录, 2 x) @. V; E6 y& q; L飞机飞行手册的附件,包含基本手册中未提到的飞机形* E! C0 S1 Z! y7 f8 p 态的其他性能。是附在手册末的补充材料。 2 r( [( P9 V0 ~. ~顶销,& R( O- m3 q. x& D2 o 用于连接起落架扭力臂两部份的销子。 ; z o7 `+ i0 a进近方式,- [* L0 {1 b1 ^/ U6 i; }. C5 d 一种综合了控制横侧的航道信号和控制俯仰下滑信号 . ^; H# i' B& P" U( U的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系 : s5 C2 h' b+ d6 U统正常时才使用。 ! o( `1 m S3 d辅助动力装置, * H! @& s, I# s. B; U' l( s见Auxiliary Power Unit 8 ?# q5 n6 ]* ^* Fcontaining additional performance for aircraft 7 s2 t$ P! v! j% c: C9 iconfigurations not con 6 s6 m7 J$ ?6 |; c+ S+ h& D& }6 Q" H& U Qc ) c& v% P$ t3 z6 Ib! O1 K! f X9 b6 z APEX PIN, A pin for joining the two sections " O7 K& f q$ ~; r( gto , k( y0 f$ s6 q6 v" y& D9 i6 H7 g& r7 h' E5 h7 k* u* N航空无线电公司, : f3 v' f* v/ f- U$ `- `7 `7 \: S% W见Aeronautical Radio Incorporated.2 f, F0 Z* d; d, T! G 预位, . `& B! B1 Y5 a! K部件可以开始工作的状态。 3 r1 f9 A% V) l# [英汉对照民用航空词典B OEING 8 g4 L3 N( q7 J6 r* ATECHNICAL DICTIONARY 13/ ~ b6 i C, l, T! H ARC, The curved track over the ground of an aircraft ) \4 K* M" p/ U5 J" N3 b+ nflying at a constant distance from a measuring / R6 X, _0 h- T/ P Y1 zequipment (DME). : N2 s, ^7 J% t0 Y0 m; ?in the limits of self-contained system7 I2 t1 A9 g1 I [) h& { apability. " u0 o2 D! C' i7 m( Atem for opposing or restricting$ R; Q1 f6 B9 ~) D ovement. ( F3 s' b* U) F5 }& }5 Z8 z6 oSPIRATED TAT PROBE, A sensor that measures total" z, ?4 U. C M! M8 O9 W, p9 k- ?4 b' _ ir temperature when the airplane is in the air and that * Y2 K# L5 s8 j- c$ W- ~7 Heasures outside air temperature when the airplane is! {- @& G5 u b n the ground. The outside air temperature is measured% J- `8 _6 ?. c. _, @ SSEMBLY, The fitting together of a complete structure , B4 d( h( v' N E$ h# r3 ]SSUMED TEMPERATURE REDUCED THRUST, The1 P+ ]0 R4 g8 L2 ` ATC, SEE - AIR TRAFFIC CONTROL . j# b5 g" D/ U4 x6 V0 Z4 P' M9 [3 x% f# U6 X系统中所产生的一种用以抗拒 / M o: ^1 C, B7 r9 v作或限制动作的力。/ [+ D; h% i# X" U! W2 W9 @ 头, + m. U- h' C e2 k/ ~7 C) ]用来测量飞机在空中时的总大气温度和在地面时的外 R- d) l5 }: L/ ]温度。地面外界温度的测量是利用引气将外界空气吸入; }7 F3 w' r8 q- i" U0 @ 头,以达到测量的目的。 8 ^4 r, }" c, m1 }! B: U. t配, % n6 {# D, O' [, ~5 z* B7 a7 y一个完整的结构或组件的过程。 ( E1 h' A+ O/ s5 V \- c/ }假设温度而得的减推力,$ r, C7 S9 W' Y( { 推力设定值时,假定一个比实际外界空气温& u5 |/ m5 u9 W( O3 ]7 g; G6 o 空中交通管制,; V5 }3 b. F5 {1 Z! ^+ C. `1 ^# @& H 见Air Traffic Control " J) J \' X, q: b eAREA NAVIGATION/RNAV, A method of navigation) S9 }+ y! w& z" _ that permits aircraft operations on any desired course% Y q4 x; Q/ x, m n( w3 I# z9 G within the coverage of station-referenced navigation , {5 U; A0 n& D1 E, C, lsignals or with; m" j9 v! L( D c8 N! I- N5 l; R, L ARTIFICIAL FEEL, A force developed in the flight% H7 |, R9 P; g! w7 ~2 ~ control or brake sys ' f2 Z" i- N: K# }! p/ Bm 9 q4 q0 P- o7 k; e0 `8 l: vA/ M) l( k v* h) V% K a9 i- m5 P! [- U. r6 { m . ?1 n! O! w2 i6 y7 ?3 No 8 Z$ ]: m+ H! tby using bleed air to draw ambient air through the! O4 a2 n* f5 s+ g sensor when the airplane is not moving.% f* x/ d. `# l/ s0 w A8 |: t8 W% r w8 P or unit. . D* G: Z& V* ^/ K; M* e' K( b6 wA 7 x, F6 F8 d, hlower thrust obtained by setting a higher than actual9 r& v7 P1 c6 B; ]# I Outside Air Temperature (OAT)., \% }' A- [$ q 弧线, * h8 b6 j: J& K' N飞机在围绕DME台等距飞行时的弧形航迹。 - H* ~) Q, f# k区域导航, + c$ @$ ]3 p( d# j' o/ z容许飞机飞行在有电台参考的导航信号或自备系统能% E9 U4 }! W) A5 q J6 r 力极限范围内,飞行任何预定航线的一种导航方法。2 y* P5 m/ p2 N$ y) V9 B6 d 模拟感觉 , u. r2 J' G5 z) l: W" {9 }在飞行操纵系统或刹车8 t; B* Q( U' r1 _9 b* k0 c( A0 | G" A! q0 R0 g6 D4 X8 w' U 吸气式总温探 ' R3 o& U2 | U: f+ L( q9 V9 C, n" S6 N) w( j' V: S5 M; i6 P4 o: T( |7 o- m r: X2 G& ?6 I# I, L8 D7 E, | 组合成 ) g% ^) b. \- ~0 B3 m* e4 Q6 B# y4 V- a在选择起飞 ! n8 v' `6 E( _3 C度高的温度而得到的推力。用这种方法可以减少发动机的( [% K# O, o# F( i 磨损和维护费用。 " d0 a9 `' g9 |5 G+ l1 @: K' [% _6 x# M$ l0 b# B6 o, G 英汉对照民用航空词典B OEING 9 ^- i0 J ?- k/ f4 @& qTECHNICAL DICTIONARY 14 & X4 y: a- [/ Y/ H; `. m3 v& W& TATE, SEE - AUTOMATIC TEST EQUIPMENT * a! M* b6 d$ \1 H4 g7 Q8 O {6 \ATMOSPHERIC PRESSURE, Pressure of air due to the . L8 V2 F- Y9 ]( Rarth's atmosphere, expressed in pounds per square" @. |: F- o* ~; U& a s ch (psi) or inches of mercury (in Hg) or millibars (mB). : F+ ]6 w d- S) \TTITUDE, The relative orientation of the airplane with" v- V0 [8 k+ [" M spect to pitch, roll, and yaw. 2 o& e7 J1 o# x7 T8 `0 S. `UDIO CONTROUSELECTOR PANEL, The panel in0 S. O/ Y3 g: ]3 o5 e6 F e airplane which controls and selects the routing of$ P- ~- K( m6 x: w6 j, d udio.: h- w/ _8 Y6 y* ] UTOLAND, Automatic landing using the Digital Flight2 E# E/ B: e# W' b ontrol System.% O7 l, h3 e* D n. 2 v* G0 ?' X$ WM, A system & g4 ]1 W7 {* d0 f$ y. aomposed of all necessary subsystems needed to guide; F" u( g0 c) Q9 K e flight of an airplane.# I. r B7 u$ b' _ EQUIPMENT, System test * Q! _6 j( g0 l1 Q! Iquipment that operates under computer control. 7 ?- m; W' s9 v装置,

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e ( x( C; T K: T, h, }, gin 4 ]5 b, w8 b- q- w& e) L/ TA 7 v$ h$ }4 j$ w6 ?+ r1 T) Rre* T+ g' r( s! Y5 Q' z A 9 z- o( m) e; O5 O# eth 6 |' t8 b% B" Z4 i0 n6 ]a V# ^& L. c h& p2 B* H7 C A( g g1 O) n' s C 8 e# ?/ ]' l: C' HAUTOMATIC DIRECTION FINDER, A system which # o1 ]: i( b3 ~, M0 J: Z/ Jdetermines the direction of a radio statio8 }, R+ @4 |8 [( z' H4 p" k H% y% Z AUTOMATIC FLIGHT CONTROL SYSTE 4 q4 Y5 }% S D7 vc; w( r+ C+ V) h6 b& X th+ j& G/ ] e9 w8 i4 g AUTOMATIC TEST7 z5 m& t/ G# v3 ]3 D7 Z/ R e . R: O# {( U0 {, S自动测试' ^7 ?+ V* O4 k8 D* S6 y 见Automatic Test Equipment.* W9 u; d7 _8 B/ f8 h1 e" A# z& s 大气压力,0 S; P8 r( M; ~! f 由于地球周围的大气而产生的空气压力,以每平方寸多 ' A' |' O8 c$ J \# }: f( C4 P磅(psi)或多少寸高水银柱(in Hg)或毫巴(mB)来 c8 \: E. I4 _" c8 J; E 示。 + `. S* o" r7 B+ d) j飞机姿态,6 Q' P# X" ]8 ~( S/ g) X W 飞机与俯仰,坡度,和偏航有关的相对方向。 ; z: J( ]! R5 ?音频选择面板,/ D8 Y9 @2 u- ]& { 飞机内用来控制和选择音频通路的面板。 6 S1 K8 @7 B' p# M自动着陆,' K* |- E8 U/ L 使用数字式飞行操作系统来进行自动着陆。* D$ T/ p0 t. k, { n 的系统。 9 q$ W, g, y" x8 p7 {9 E$ i: e( Y- C' D系统所组成的一个系统。 ! } V0 S, k! q- u; g5 U/ [在计算机控制下运作的系统测试装置。 5 x6 i$ r! ]% g/ S* l: E+ T) U, y. {% Y! b0 S) m+ C @6 w 自动定向仪(ADF),* ^/ R, L E8 z6 h: ] 确定无线电台方向 7 H" u, [6 |$ e }, w8 ?自动飞行控制系统5 c1 i& P Y- d v) ~6 k 由所有能引导飞机飞行的子5 Q5 Y9 ]9 K" N6 [% k' f 自动测试装置,3 \# e: G: p! n, @& p; ` 英汉对照民用航空词典B OEING N0 K% f0 U% r: _$ t! Q8 b* O- @ TECHNICAL DICTIONARY 15 : L* d/ k. O+ i: e* I0 CAUTOPILOT, A system which automatically controls _# I! l2 c. ]2 D* d" l+ { and guides the flight of an airplane.- }/ M! K' G' I! { AUTOPILOT FLIGHT DIRECTOR SYSTEM, An M/ Q0 w, \+ D5 Y/ Ztor " L$ `6 n& ~' S) CUTOTHROTTLE, A system which automatically . ^- h9 @0 i2 I4 Y I( A+ u' ^ontrols the throttles of an airplane.5 v' L/ n3 S$ I! ~- g POWER UNIT, A small turbine engine in' i) S* \3 F- } e airplane for supplying electrical and pneumatic& h. H$ k& E, \, D5 B* i ower for systems operation on the ground or in flight.' e. e$ t- T. w VM, SEE - AIRBORNE VIBRATION MONITOR& |0 \0 R2 h& m XIAL FLOW COMPRESSOR, A type of compressor/ p. `6 M& `& U sed in a gas turbine engine in which air passes through 1 s/ Q6 W9 o$ m2 M% D1 N6 `XIS, An imaginary straight line or an actual physical4 c2 J( X. `0 H7 V% i omponent (such as an axle) around which a body can% g% O: j1 a4 u) D tate.+ ~7 f3 ?* V, ?1 Y8 r( O& V# v! L 仪, . w3 v/ A. w m6 ^" E# k8 T3 z% u$ Z* T2 i' `# h 自动驾驶飞行指引系统, * M' q, v6 ?/ X* z% r* e$ k& j5 L动驾驶和飞行指引功能的系统。2 q, ]" X8 r% i% A( Z 动油门, ' C: s, R E9 z7 z) \自动控制飞机油门的系统。5 F3 I9 n, l7 N% h 是飞机内的小涡轮发动机,在地面或空中给各系统提供+ \/ E2 h# }9 q5 u 源和气源。/ f: l$ H, B# g z 称。 9 B, s/ V2 k* Z- }& i8 E* |载振动监视器, ' k- H) N8 W/ c% q& Y, y: s见Airborne Vibration Monitor/ p- _5 E# P" S integrated system containing autopilot and flight direc : i- D! c, i: ]: e4 qfunctions.% }5 L& b" R2 o$ f/ d) @$ q A ' u& u- b% x5 S3 v0 Nc k6 f8 s: V/ }6 x* v AUXILIARY+ P/ L* s2 m; [: F: e- Q; G th9 ?6 b& u( }, C5 G' h6 A p0 F( J" U4 J/ O5 X AVIONICS, An acronym designating the field of aviation 2 @2 l: q; {' a3 f1 m. ~% |electronics.4 x' g+ p6 A. A9 N A ; c" D4 W( h8 a) X, [A 2 E+ ]4 }& h1 ]8 F% I/ Hu ) N1 }9 y* W- t5 i/ f# |; Lthe compressor in a straight flow, front to rear.5 V1 y( |- A. t A & v/ O( X! F1 t/ [# [c $ _# a, g5 s' k, f. h; ~ro ! n) B \ P( Q" {自动驾驶 5 N4 R+ s3 V0 B' K4 _动操纵和引导飞机飞行的系统。 ; U' j, u) V& G7 A+ Y0 j一个综合自: Y5 |2 W$ D$ t) V7 }" S- W: z- J7 r ?6 p! u辅助动力装置,' l6 E3 m2 i) C2 q" s( g5 G0 X! J; \! z7 _- o航空电子学, ! z5 U- m$ R9 N; b' W( B6 y是航空电子领域的一特有名# l+ @! L6 N8 l3 Y1 C" b; {3 [, ^+ P, K! E( @+ T. J& ~1 F3 x$ H& i0 i; _ 流压缩机,7 s7 V! T: O6 I( n: _" m7 D 一种用于燃气涡轮发动机内的压气机。空气由发动机的 1 \$ o% l2 L$ ~+ }9 i7 i; Y部流出。* g- N9 v+ o8 B6 g! F 线, 9 ^8 J" B8 O- i: T2 U% [可让物体围绕着作旋转运动的一个想像的直线或实际: e! J1 Q8 ?) a. g& v6 j' t+ k' ^ r% F" G 在的部件(如轴)。 2 G* y* [9 |2 Z# b5 D- L; [1 w3 R" n: _* y- v+ ?% y, v前部轴向流人,压缩后,由后5 O4 N: h- @: m' \) A( F Q( D4 p, L) j2 j9 K4 I8 F5 q+ {1 ` M) q英汉对照民用航空词典B OEING ( v. \$ v1 W1 L9 _TECHNICAL DICTIONARY 16 , z! R6 Q4 W, Y, [" }4 OB ) K. {$ }6 `5 [) x! {9 XACKCOURSE APPROACH, An approach to a runway7 p8 @5 Z' s- t7 U versed. 4 t; k4 S6 y$ w/ v3 P& ]* J# \6 }, sown on the EFIS that1 E( o6 R, m7 o8 R# X @ oes not readily change, for example, navigational aids.- w& N" F* ?) i9 j4 k vement in the tank or reservoir. ' f8 Q8 i3 B% p: D0 p# O# r7 x. }ALANCE TAB, A small hinged moveable part on the6 I$ Z7 l7 c2 ~, T+ ~ ailing edge of a control surface (aileron, elevator,7 c3 c4 H7 L- c4 `# i n; Q$ e 航道进近, d, w% u& C4 ]4 {( [) k. B: A相反的进近方向。当反航道进近时,无下滑 - t! G1 A: w' D$ P: |& W, ?2 i& Q显示在电子飞行仪表系统上不经常改变的数据。例如:& Y5 C/ T% e4 f& w; Y" _4 u 航设备。9 [6 [3 j* ~- S2 S7 R: w 在燃油箱或滑油箱内阻止液体流动的隔板。 ' E- S9 P6 J4 }# X( _- `3 x动补偿片,) t5 d; t4 v; T$ y 铰接在操纵面后缘(副翼,方向舵,升降舵)的可动部。 3 d2 M( f5 [* [4 S$ d与操纵面相反,以帮助操纵面运 5 s# ^0 [- ] i+ H# MB 1 i3 l- z3 a$ t- J o! B! f3 w1 m' [which is opposite the normal approach. For a1 H9 R2 @. {; F6 H6 A6 \: r backcourse approach, glide slope signals are not: u2 R! r" W7 @1 h) @* a$ l available and the sense of localizer signals must be/ m+ Z5 i5 u! l* t& J re; a5 K2 y& j/ J BACKGROUND DATA, Data sh! P6 f+ k3 R% U* T d ) j: i7 w" t7 L* s: g0 t0 f2 eBAFFLE, A partition in a tank or reservoir to prevent6 }) }1 X z1 z0 ~. h+ l4 { fluid mo+ E+ i# S6 a! b& V B . a" n, ~. M/ ~/ V3 vtr . \/ Z3 n- A( qrudder).The tab moves in an opposite direction to the$ c B# s% `' n+ I' e4 q- ]9 V" @ control surface for assisting movement of the control : `* d, M6 A* m- |2 X% g7 A2 csurface.2 w2 o9 T3 j9 i+ d5 |: j% J7 ^# `( ?- N9 f3 @ 与正常进近' `6 l7 o+ J$ c0 N! i1 { 道信号并且航道信号也必须逆反。 : q6 ]! V" x4 X; u( m背景数据, e3 H5 R7 L& o( K' S( K) ^6 {1 w2 {缓冲隔板, / l4 ]3 @. |3 T2 O7 K8 M* C0 k4 n+ V/ O! ^6 T8 Z/ M随动补偿片的动作方向3 k. e) c; D1 i 动,减小操纵力。$ ^( w& @& X2 j! R- m0 ] B3 O# ] 英汉对照民用航空词典B OEING 6 {6 S8 p; R; w; E8 qTECHNICAL DICTIONARY 17 8 |; A; |+ l6 e$ I" {BALANCED FIELD LENGTH, The field length/ @3 A1 T9 s% k/ c; B b1 [ associated with optimum aircraft performance when' r! B5 B& }% q8 D, z% S bstacles are not a constraint. In this case, after engine' [ f- z; y+ @: b ilure at V1, the distance required to accelerate, takeoff0 M& P( o/ ?3 u3 K$ l, \ nd reach a height of 35 feet is equal to the distance , u0 ]" b9 O4 F4 G6 pALLAST, A weight installed in an aircraft to maintain 6 {# c; O6 N2 A! Q& mALL NUT, A fixed spherical nut driven by the 7 Q9 ]9 F5 k) c9 b& g3 n& w" q4 fAR OUT OF VIEW, A signal used to remove the flight5 @8 B: u2 @" j4 V' n) U; t- D3 @ AROMETRIC PRESSURE, The pressure of air above4 z$ F! C8 b$ [ g) or% y' c" ^6 O# H5 I+ L5 F4 v+ T+ W% n millibars (MB). . Y: V. N+ F8 t& O$ MATTERY, An electrical device for changing stored7 T% S5 K7 ?% I( i 性能的场长。在此 9 t4 Y8 o" b! G8 Z况下,V1时发动机故障,要完成加速、起飞、离地35 ' b! H( ?' s* M/ ~ r尺所需距离等于相同速度下完成全停所需的距离。 + g+ _# V5 I6 X, U9 `舱物,; ^% `5 j8 G% i# N N( Z7 j" l, Q- n 重心在许可范围内面装载的配重物。 1 h, ^8 @8 T! ?4 T4 r0 ^3 U形螺母,- \3 s1 C9 C% u0 z: v' i8 B5 b7 O 的固定的球形螺母,用以使襟翼和水平+ ^7 {2 ~. x& D 引杆消失, 2 J0 }4 ^: j& m! S' Q, d: w指引杆的信号。3 `, \- ^8 [: ^$ P: d# r9 c 压, , s% y3 M' g! z! X! b压力。通常以多少寸高水银柱(in 9 @! ?* T* p" W" _6 x: ]瓶, + K7 B( L: Z# G; K ]5 _' n% _的化学能转变为直流电的电气装置。* q6 Z8 ?1 {3 d* G, P$ k# j o6 y/ Y$ `6 f9 D! V% u9 o% _ fa) X! Z- h" N0 N/ M u0 b# Z a " Y& Y" B9 R+ V X0 Mrequired to stop from the same speed. - X+ e4 H) f* G9 J* h1 ?7 kB # x) @1 t% _( h0 h# Q& [the center of gravity within allowable limits. 5 i; f) J7 y# BB 5 D! p# Q# R1 [9 F: J* w7 [jackscrew for flap and stabilizer movement.& l- u8 a; T' t6 i" m) W B 8 [$ ~6 `6 s- b' r) q# ~* cdirector command bar(s).# \" g: Z5 R V" v4 U* q. W B" X8 P5 G$ }5 w# H3 h# w: } zero pressure measured in inches of mercury (in H- \0 x" h# b+ L1 C in1 s6 k" f$ u0 t: l" _& r BASE METAL, The underlining metal to which alloying 2 {! t9 m# z. o$ F$ B# Sagents or metals are added./ G9 n, x8 b% ~4 j# a B 3 A/ f) w! ^- s! @, m/ w" Gchemical energy into direct electric current." X7 t- p7 o* b 平衡场长, . x6 `+ ^8 _% P# L$ i当障碍物非限制因素使飞机达到最佳 . N) j U9 E4 y# y: k4 w! t+ o& v1 |5 k P: a8 K4 p. |' R% k# y5 R8 F$ R5 ^" x/ D9 e: `为保持飞机 - Q& @7 E! M i/ e, A- T8 R6 B* a: V( w5 m+ a7 e由粗重螺杆驱动2 Q3 W& {" t; j) D" ^8 M 安定面运动。1 Z. ?, i' _4 U# S3 v X, \( W4 o 用于除去飞行 ) a* u9 `: x+ t2 F( z [; l2 C5 q9 G4 v: _- m% d 零压力以上的空气0 n' n- b) Z) O+ c Hg)或毫巴(MB)来表示。 ; M: K8 l: e2 i9 q$ `. @4 u基底金属,1 G* {$ J! f2 s: R" Q 指合金中的主要金属成份。 5 T' l K% s& \- B! K _3 O( a4 J3 l将储蓄$ B, R, f @" W# i/ B1 L* o 英汉对照民用航空词典B OEING% n: y4 q$ e/ c; T TECHNICAL DICTIONARY 18 . N ~ [% a( }& m+ ^. pBATTER * H! m: L- r; v/ odirect cu # v- X' L1 }- v( _5 q* c1 Ipower su0 V9 B5 u$ f, y8 R2 Y$ l; W% Y7 h/ A Y BUS, An electrical conductor supplied with - y2 [# |) _" X/ Hrrent from the battery or transformer-rectifier for% D8 t9 g4 z2 j0 r9 R% N) z pply to operating components.. _ I) {& r0 X) T$ _ CHARGER, An electrical device supplied0 w6 N, \5 \1 x3 M% J3 y) d, }& x& }' y/ j ith alternating current, which produces a direct current/ V9 ]9 x" z$ h& }1 B utput for charging the battery on the airplane.$ x: \& ]" w- U5 D AY, A compartment in the airplane structure./ r2 \. a) g) [8 H7 k CD, SEE - BINARY CODED DECIMAL% S8 \7 m; r4 W. i W( Y EACON, A device which emits a signal for use as a 2 S/ U/ h( y" [4 y& ^uidance or warning aid.- F+ j/ \5 E( w5 j5 ] BEARING (NO. 2), The direction from an airplane to a * z: [$ j6 P; P2 \$ w1 Dground station.4 n7 @( u" o# A9 s6 A$ N& W4 A 瓶汇流条,; F& E7 a, T( E% N; ]1 I 将从电瓶或变压整流器来的直流电供给工作部件的导7 Y x) K$ ~3 f$ R& ^ 体。# k; b: \4 ~* e+ g0 T6 ` 瓶充电器, ( v: x" s# X3 k: ^" y1 U, X3 M' m2 L用交流电向飞机内电瓶充电的电气装置。带有交流电的/ p3 y. A" }% r" X$ j 气装置,该装置产生直流电向飞机上的电瓶充电。& L0 b+ R6 l8 G' r' ` 舱, t) { K* ]5 ]: E飞机结构中分隔的空间。9 b+ J9 L: F% R: a! w) @ 二进制编码, ; z/ G2 C( k- F2 }见Binary Coded Decimal o% z4 V# `6 \6 u6 z BATTERY 5 \' l' p3 u$ j! y4 I% {w! C8 D5 A+ ~# H Q: w' i o* _) ]0 P9 P2 n5 g- `1 o* @ B: K3 Z% w# h* X/ I3 ^9 R5 E/ n! P B; O: _7 `, q3 N9 g& N B* u/ V- T1 D4 }0 M g O! n" n) T4 U' W1 S; iBEARING (NO. 1), A surface that supports a moving 6 o A, a5 I! k1 ^$ L; V) Zpart and reduces friction between the two.* ]. X+ o/ T9 u1 r4 U+ R% l m+ T7 ~! ^& o) d! Z, C2 d v! c$ O0 ^4 e$ ]( c4 i* o7 K P& U2 T, A3 l- m: R2 f8 Y' ~5 @, ^- [, f T/ R$ x! u6 ^ ^( N7 P' z; e9 d: G+ Q 信标,# t6 n, U4 P' C/ R, f 发射引导或警告用信号的装置。& V0 L* }+ Z5 n6 @( k 方位(NO.2), 7 M ~8 m$ e- ]; T6 G& q1 m从一架飞机到地面台的方向。 ) s3 f% } F. Q轴承(NO.1),* P% J+ h/ X/ W 用于减轻机械转动磨擦的机械装置。 : E- Q- P7 L- u F$ q英汉对照民用航空词典B OEING & r3 ^5 J9 a; s/ ?1 F2 T: WTECHNICAL DICTIONARY 19( Z0 o4 b$ ]' _/ H BELLCRANK, A double lever in the control syst; p# y0 i3 L. J6 @ changing direction of motion.% S) C' t& c* ]& u x/ l* k, \ em for' \ U `( @* Q, m8 C ct in the1 r% C( b) n( a4 T, U neumatic system for absorbing expansion of duct due4 z# T" X) o# G! D& i heat. * g+ j' H# ?. B) ^2 a# r/ ]ELLOWS (NO. 2), Corrugated folded or pleated & g# j: u* \) ?) ]ontainer or compartment used to measure pressure.9 ~$ h! Q4 _& n+ C0 G% a EZEL, The part of an instrument case for locking the3 D6 e. H& l* L lass.+ N6 l$ L6 P9 I$ H9 g IAS, The potential difference applied between two @. b8 V" H4 E oints for controlling a circuit." v6 \ e; @9 e6 K- l BILGE, The lowest part of an aircraft fuselage. A place 5 w$ L7 w C: I+ f% k4 jwhere water, dirt and other contaminants collect.7 s2 @7 A+ Q/ \# S9 z 气源系统内提供管道热胀冷缩所需要的余地的波状8 N" a; V, I3 q3 s5 y 轫管。- Q1 I* D X% I* ^ 空膜盒, 0 Y5 o; s* ^1 ]% R+ ~8 o$ `一种具有波状表面的容器。用于量测气压。 v! C/ v0 W6 G( s/ }* ] 嵌沟缘, ' R" f u1 F H! \- y) h" ?5 W将表面玻璃固定在仪表上的圈状零件。 & U& s8 r+ e [$ k% V3 Y压, " R2 \# e$ }5 l! w' J2 D在控制电路的两点之间的电位差。8 Z6 B3 g' K, x+ ]. W: e 机身腹部,% e( m7 `, q' ]& d& b 机身的最底部,通常水,脏物,和其他外来物集存于此。 0 l# M+ s; I# ^) `. E3 I9 rBELLOWS (NO. 1), A corrugated flexible du 0 n# G6 f: ~ ~p 6 r6 {" g/ `% _: U8 \2 U" A6 oto 3 F5 ?' o& t" U8 F1 h! TB 7 D0 ^$ o4 \$ O' b5 ~( q0 yc6 y$ l8 Z- X- N9 w B3 [, @& x! `& v) o* O' B g, t( F! }. q; c1 S7 ] B 8 g2 T$ g5 Z/ d9 [p3 Z6 k @' G/ {5 s* e( ?: H o 直角摇臂, * s' @6 ]8 U4 W& H+ x6 K在操纵系统中改变运动方向用的双臂摇臂。6 r" W) \" M! Z, e; J 波纹管,. @7 D/ p; d! G! S1 m0 N7 G0 Y6 l7 _/ H% k8 V% [' ?! n! \; w# O; t& K0 L( J* I* d3 s1 K9 e: T) r5 r/ G" l& ?. G' o英汉对照民用航空词典B OEING$ j% e P7 N. |, I+ P& m [' F TECHNICAL DICTIONARY 20 : B; h, A; m I1 J; ?1 ?/ W3 ]4 N, V0 DBINARY CODED DECIMAL, A system of coding each2 X# Y" N4 N0 G, O3 t. [) q6 w digit in a decimal number using the binary equivalent. ) [5 c, g) v4 {BINARY NUMBER SYSTEM, A number system using, y% h/ s* z, D3 \7 V9 P | s1 l& W5 W1 f6 c- S0 u$ I IT, In the binary number system, the smallest unit of6 t1 o! r1 A" s, F/ |, y6 F formation, consisting of a 0 or a 1. 6 J, C8 S8 h3 F, m# u4 vITE, SEE - BUILT-IN TEST EQUIPMENT 3 V8 D8 H: D% j" x! ILANK DISPLAY, A display that does not have any - Q% |3 w# E! a. ~7 odications, normally due to failure. ( X* n' {0 }3 B) y9 ALACK BOX, A container for electronic circuits to record $ Q2 X- C5 `; {# sight data.6 ]' u( @. }; n LEED AIR, Air taken from the engine to power various* R- W+ H( K: [! U8 [ ircraft accessories. 0 Q* o5 i! Z4 q/ H$ KA valve in the pneumatic system for air9 M1 n; V4 P1 i; x. ?8 l( J( i9 l supply from the engine or auxiliary power unit to the 6 u3 E0 H2 C3 g4 ~pneumatic manifold. A valve on the engine for reducing' A* t5 t$ y6 q0 p/ n( z pressure in the compressor section.+ H9 S+ W# _/ } 进制,( y7 W6 l; w0 L/ o9 b: p' m( U 进制,4 [1 t8 s0 e9 } e5 Z0 ~ 一般用0和1)和2为底的数字系统。 * w; ~2 B. B* g* a特(二进位数),1 W3 Z* Y R: n; z$ u; y* l 二进制中的最小信息单位,包括0或1。7 J/ e8 r& P- D0 R 内自测系统, 3 W# a y8 |5 k: K" X J. r- d, x. ?见Built-in Test Equipment. i, y; m) g, O two symbols (usually denoted 0 and 1) and having 2 a" ~" t0 W* E6 }1 L3 @3 ^. v0 z its base.2 J/ z% G/ ]+ L9 Z3 S+ f B $ n3 \! @4 T. h0 s5 \2 D% Iin % H+ {6 f$ n) H9 u P$ iB ! U% Z: X$ E) Z- EB( f. V( n+ ^ r( V" Q" C in2 e6 X% ` f! N& X' L: Y B 1 R o* e. T! x% C2 [4 ffl ! A! T: R/ {, r( QB l" Z9 |! a! U1 v4 k a) f5 H* u: h) L0 X h% S BLEED VALVE,* S/ L* k( }; _ d- c+ u 二进制编码的十 8 Z% P! e: Q% \8 o一种编码系统。用等效二进制位数编译十进位数的每一 : d4 {* x$ c7 m5 v; y. Z3 l位。 1 G" X* Y+ P$ _; {. a( H# n" X9 X# }$ n+ k) v以两个符号( ; e$ P2 ?/ E6 S- A$ e* z9 T0 u1 A2 V& N, K3 c( _ @( a7 L: f .% _7 L6 o# a+ r$ X- u1 e 白显示,0 h2 [- h- n& @% F4 w 通常因故障而造成的显示器上没有任何指示。 ( O8 g0 ?* V) o" z" E5 V/ Q匣子, : f, `1 q# |# X& q- L# A! R装有用于记录飞行数据的电路系统的容器。 ' `. v+ t# i) N8 \$ n# \气, # t6 E0 k1 e& S取自发动机而用以驱动飞机上之各种附件的空气。 4 \0 ^1 u; B' c2 j3 E9 @ N气源系统内,使来自发动机或辅助动力装置的空气进人 9 A+ C+ k$ I( y' ?$ T) K# s2 L气源支管的活门。发动机上,用来降低压气机压力的活门。+ ~& M4 [7 ` ]9 I/ A) s: v* U# \& o0 r9 z7 [) C3 f! X5 {1 K! \! ?) ]. p2 `' M/ h# Q( r% X! Z1 \* e; f% {引气活门, ' |9 K3 B' i$ a4 {英汉对照民用航空词典B OEING- |" S4 y5 W# m TECHNICAL DICTIONARY 218 i$ ^ V/ {4 I BLOCKER DOOR, A device on the engine for blocking& d, x6 ~5 d" @ the normal airflow during thrust reverser operation. 3 v3 }8 l& @9 y9 r9 N7 A- E FLOWER, An electrically operated fan for circulating air.$ u9 |* c# k8 P! E LOWOUT PANEL, A panel in the structure between I/ e" o0 d, L, d- A5 U, Z6 v: \o compartments that opens to equalize pressure in 5 p" B+ M- ]9 l6 ]: F' Q- j: \3 Me compartments. + k! N: l1 m( [ODY GEAR, The landing gear attached to the $ ^" c3 O+ @$ w+ m6 a" ^' V6 ggrounding. 6 I& q2 ^# p( Z( v2 `; M4 J正常的 ! }# d- L! r& x6 [3 F. B气流。1 s# A+ S/ j4 I/ g1 H7 r4 { 鼓风机, ' D$ |6 |9 N' V3 W用来使空气循环的电动风扇。: j1 P8 o5 E, v' s 压口盖, 3 h; X, k" R6 q4 M4 n两个隔舱之间的口盖,打开后可使两舱压力相等。7 U# J, G1 J1 A: I9 ~4 d- i: b1 h 身起落架, / C- u3 j' o1 i+ F' B* f身构架上的起落架。 3 K+ p# w. k* _) q1 _B / \! L6 X0 w3 ]7 uB6 L! f9 K4 t! N% t* J6 I' o tw n- T" Q4 s" ], c o2 w6 U% B th, }3 q9 @3 o4 z B& X8 A A; W! ?0 Y; I fuselage structure. " o) u2 E z7 L1 w. iBONDING JUMPER, An electrical connection between, t% N5 H# J( W1 U8 m a component and airplane structure for electrical Y2 t- q* I/ a' R& j阻流门,! d5 P! {4 L `, e+ ~+ j 发动机上的一个装置。在反推工作时用于阻挡 4 h5 a! ^. V, Z$ F3 a2 c: ?0 @+ }% m( S2 ]* T% R# `7 z, j5 c. q9 [- l. ~, i装在机/ S9 y" R' l( E9 A 搭接片, , s8 i7 _2 E6 F) y9 k8 s+ t) o连接某个部件与飞机结构以形成接地的电接头。: V% Y; Q. }" u7 L6 K# Z 英汉对照民用航空词典B OEING* d9 H3 F* \# g& p TECHNICAL DICTIONARY 22 4 J2 ?4 r _& d. CBOOLEAN ALGEBRA, A mathematical system for : B; H- p+ k9 U8 Iwriting combinations of logical statements.7 c) Q: ~6 m1 M6 N BOOST PUMP, An electrically operated fuel pump for / B: H' ~! w: x0 g/ m/ b0 E1 ffuel supply from the airplane fuel tank to the fuel, Z8 P' @3 [: J }1 ~* { manifold. & |+ @1 q8 W, DBORESCOPE, An electro-optical device for looking at" b! M1 H% }0 @0 m ternal parts of an engine through holes in the engine.. p+ ^- Z$ v' x orescope ports) ( Z8 H& M9 W$ z8 dOURDON TUBE, A curved flat tube in a pressure gage0 V8 N- t+ K8 l" c5 _ r moving the pointer when pressure changes inside 6 k4 a- V3 _' c# w, Uon the ability of the brakes to% e: m+ y! L% A$ @( Q bsorb a predetermined amount of energy during a/ k, I0 ~6 k6 u jected takeoff. % r/ i3 H% M) R' r3 }用于通过发动机内的孔(孔探口)观察发动机内部件的$ H4 O9 P1 x/ d 光设备。# @7 o' a) u3 T- L 端管,9 s% _( e6 e6 u y' u 测压计内的弯曲扁管,管内压力的变化时它使指针移6 |% C0 I4 G' n) ? 力。 % V! j1 V3 g5 P( B极限重量,& F- \2 H! ~+ R; p5 D4 f1 C" W* S# T9 c1 ?5 t 起飞重量。9 e" y1 C8 j6 n8 c% s8 d 发动机滑油系统与大气相通的通气口。: b6 U) k* K$ D in" W. S2 X" g; V; f7 c (b % \* E' Y' n0 G- f. N6 |6 uB% n1 S+ r' R6 T# E( [2 j fo8 Y/ Y4 a' P6 M the tube.; |! ?; m; k, p5 m BRACKET, To enclose or surround. 8 D3 I) I7 V* oBRAKE ENERGY LIMIT WEIGHT, The maximum; v, R) j# Q( T3 ]* R8 B* u9 T9 M takeoff weight based ; }5 X. r! F$ v5 J/ \7 ya2 ^% t7 Y- j4 c+ G re 2 S( G4 M- V. q0 GBREATHER, A vent to ambient of the engine oil system. $ f" }! n1 V8 @. n) r布尔代数,- ~3 n0 T% z! \4 B* N 一种用于编写复合逻辑命题的数学系统。6 M! O( U+ K- v 增压泵, + u h+ Z) M( c: L1 u- r从飞机油箱向总油管提供燃油的电动泵。" [8 u, C! s! a8 ~9 G' k 孔探仪, 1 P* ^. x3 w7 v: F9 ^ a" q% _" W) X& _! v* P4 B, m 动,以指示压 R4 _1 _' M1 @! g7 G/ |+ Z 托架, & @7 y% C/ a' c: p3 J- D用于作支撑、装托、或围绕之用。 ! I1 \ a$ g' i6 m2 w4 p刹车能量0 ~. h- E+ V" R/ G6 j4 k1 y 中断起飞过程中,取决于刹车吸收预定能量之能力的 , q( C. {1 H' ?8 E! P# {+ y, C" b4 M 通气装置, 0 N% z) r7 z9 T) E3 W英汉对照民用航空词典B OEING) [% `6 u) ~2 w1 R- I0 ] TECHNICAL DICTIONARY 23' O3 P3 V7 K+ W. ? BUFFET, Vibration of the wings and airframe resulting % d2 P2 [4 {6 q( X+ Xfrom unsteady airflow over the wing; caused when / P) L% \ x, R6 wairspeed is too slow, the bank angle is too steep, or , J. @6 |% D- A6 F# w8 eirspeed is too fast. @6 W: Q9 {/ t UILT-IN TEST EQUIPMENT, Equipment installed on " n( a/ I Q# z9 ze airplane and in airplane systems to test the systems 5 s$ U1 Q' D7 Q: c! Y- s& _ithout external test equipment. " v* N4 e" F2 L k, }0 R5 oUFFET MARGIN, The amount of residual maneuver/ S0 I$ S" w; h3 U" d# I0 f1 e( L% X apability present before the onset of buffet.' x; A* v. ?( X; y& m) h0 d+ V UG SPEED, A preselecteed speed to be observed7 ?8 ~" Z. P' K$ I nding sequence.9 a: M( \1 n, v0 [ k( P( z# W1 ~/ H- ~* ]. O4 a ng landing gear operation.+ `% u1 B0 b3 \& S 速度太慢或太快,坡度太大,均会引起抖振。' g$ H( I# t2 H 自检设备,2 l' U: s* X m% J& ^# E6 E4 v2 ` 安装在飞机和飞机系统中,在无外接检测设备情况下,' }9 ?0 k# g5 n3 }. {; S6 `4 ? 用于检测系统的设备。 2 z# z9 x; ^2 R: i1 y" C抖振裕度,' q6 p; c, B9 q2 V5 p8 M6 I* d 飞机在遭遇抖振之前,剩余机动能力的大小。 7 E( N6 l u2 g: _) ?- X; e标速度, ' q2 h. A0 O4 G9 ]在某些机动飞行过程中,特别是在进近和着陆时,飞机* w4 X% q* ? J2 { 预定速度。3 d1 u1 j( E3 Q* H2 N0 u 力装置, 9 O7 A$ x6 X& \ z9 V架工作的一种机械设备(弹簧或减震器)。- u+ b# ~7 j5 i8 r0 V4 B: j3 x6 l 流条, * c# Q) ^- O1 X% @- q& D在部件或组件之间传输电、数据、或定时的单一电线或3 \" G2 k5 r7 u# ]* c* r; u0 G a - ?. i( Y: m, E% j- E+ `4 K% I1 ^6 YB 1 Y2 g% b$ p4 ]$ y i4 U4 I1 vth- w; W* [- m5 l$ ]* @2 q2 x! D w - I) U0 {' Q* S1 E0 {B : Z8 x [; u8 z! X; Ac + g) S9 e& D( u+ D% v; u' j0 qB/ |$ h9 d/ ?+ E' j1 m6 }3 t during certain maneuvers, particularly the approach and3 j" r& X; J3 y9 }+ v la / B) p4 y) Q! p0 p) EBULKHEAD, A structural partition in the fuselage or. P& t3 x7 R2 ]1 K/ q9 b& ^ wing. 8 _+ J$ J2 M; d, V @1 Z$ [+ oBUNGEE, A mechanical device (spring or a shoc" m }4 _ H: z# d absorber) for assisti4 ^( C" M- T. M BUS, A single wire or group of wires which transfers 9 s, u3 a7 b: r$ v. Z( lpower, data, or timing between several units or7 ^3 P1 W2 W: w7 d: Y' _# o" [ modules. 3 A( B% u( }& i; a抖振, 8 _0 p( i" ^- S8 u. n由于机翼上表面的不稳定气流引起的机翼和机体的振 + A1 s: S( w7 x$ Y5 z动。飞行8 w+ p. _. R$ j; s3 l3 _. F) f& X' d/ ~; H 所应保持的6 ]: |! N+ g2 ^: c. o6 x- o 壁板式隔框, & I- ^2 U3 @2 {' y: t4 r机身或机翼内一种结构隔板。 & Q- c: u8 l) ~2 m( P, e" T3 M" N5 Y2 G( ~) O$ Q用于协助起落- f; ~) Z' f: S' P& R) J+ \1 n, d, U 电线组。( i2 z7 _9 \) b; ^$ q N- q; } 英汉对照民用航空词典B OEING " N8 I; A) e- e% S; ~8 P3 nTECHNICAL DICTIONARY 24

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BUS DRUM, A mechanical connection with pulleys, w% ?' N; Z" h cables in the control system. ) I" n* P- n7 X5 v2 V6 l# R6 G# d i1 ~and . t- L' W! {: m: U" il circuits for control and protection of1 H$ s1 ?9 Z, `- ^- d% } lectrical alternating current supply to the airplane. }( e9 u6 j' ` ` duct for closing and opening the duct , s) d) w- t O0 yassage. + _1 s% s& g+ r I8 VUTTOCK LINE, A vertical reference plane along the8 p2 P/ {+ P$ Z; t5 l' h6 u- _ e, M selage for horizontal measurements of the airplane.# K% q+ W, D# J7 j; W/ s 接。 1 n; q- P7 u- P* h. N$ h组件,内含控制和保护飞机交流电源的电# I; q7 }5 Q r, z% f0 l. [) Q2 b) c8 [# ]- P! S( q" |4 @6 i作动简控制的转动装置。用来关闭和 ; F, E4 C/ y2 ?" G7 A& t启管道。 & r( n. U+ t' R+ C% Y' c沿机身走向的垂直参考面,用于飞机的水平测量。 $ e2 H& \6 G% o& K4 m8 ?% k( ABUS PROTECTION PANEL, A module (black box)4 ]+ f" }3 ]" J' I containing electrica 0 C8 ?9 v+ M! ^/ r/ G' me 8 ~* k; ?! U: wBUTTERFLY VALVE, An actuator-operated, rotating : j' |' I8 g. b& W/ F |device in a 9 E" F- ], B2 a1 l& Wp1 r4 [# ?/ G/ T: E( ^- ~8 q B 4 n; W5 |$ [& j6 d D( d2 z. cfu: A. j2 I! e8 _) O) s" h8 P 转动鼓轮,0 J/ A# }; ^ _3 G* N% O, C 在操纵系统中,具有滑轮和钢索的机械式连" o: r5 v) x0 C9 Q' b( O 汇流条防护板, % R" J4 j$ Y. {+ n! w黑匣子式的 $ f" U& s" @# k$ t& D0 k: P1 K# F, `, y" d8 c8 z蝶形活门," G! B. w5 c# ^" i: \# y- y 是一个在管道中由- Z' U# Y4 P. |" `1 D# ?( y: M4 n, w1 x9 l" \8 ?' m# d I0 B 纵剖线,/ T/ r. D7 L4 N r2 d! } 英汉对照民用航空词典B OEING f6 c/ x% M+ d, p+ I/ }( |& {TECHNICAL DICTIONARY 25 ' W! O1 f% X$ @3 _* _; q- H( V' IBYPASS VALVE, A valve through which air or fluid will $ X9 L9 P. u( A" |flow if the normal flow path is blocked. 6 t6 w1 A" X( l8 ?- E/ BBYTE, A group or string of binary digits. A byte is ) c" Y7 S2 q( ^( Y4 p" Msually eight bits long. F6 ]/ d. b1 {$ j- T9 L5 p* Q ABIN ALTITUDE, Atmospheric pressure maintained 2 h: a% R0 Y. i, N& F' W; i+ Rithin the cabin, indicated in terms of feet above sea 8 d, Z5 f" n2 a$ ZALIBRATE, To repair, adjust, fix or correct the # S$ V H& }/ |easuring capabilities of a measuring device.+ e" P3 ?6 z( g" _3 W0 W8 j, G- Q ALIBRATED AIRSPEED (CAS), Indicated airspeed1 o$ ~- K; `7 g AS) corrected for position error.. N, A5 } u- \; ~0 {7 {+ v nical 2 w! @4 d- X; [6 P) Qomponents.9 W! O; C+ ^0 f/ w1 B$ ?* T% X: s 节, ' u! C3 g2 p* [& W2 ]! D, T* X5 J一组或一列二进制数。通常一个字节长8位。 0 a+ t2 ^1 `. e舱高度,* ~8 m- W2 M5 k3 e7 J 座舱内保持的空气压力,以海拔多少英尺表示。* d9 c( y' H4 t) U$ l 准, # ]& y" k1 z0 M9 X w3 T# D修理,调整,定位或改正测量装置的测量功能。 4 P) m2 Z% k/ h# {! i2 ]+ R/ V+ M9 E正空速(CAS), + W+ o7 W1 k& H, O在修正了位置误差之后的指示空速(IAS)。 1 h( b# A: V7 L2 J* x用来移动机件的一种转动装置。 7 U4 [2 {1 ~: H, ^u3 c. a- G m& W$ R5 g$ ^9 s4 Y C 1 b0 n4 {6 y" ]( o" T- bC * h0 X7 S9 e% D2 G% u" Xw 0 J( x v: ?" L1 ^% V3 K7 u$ T; s0 H( R, Tlevel.& ?! r6 }& Z- K5 T4 z C 0 t- m2 i# z& S* Xm 6 }9 [7 O" |8 g+ rC 7 v$ V! Z% l3 W5 I; h, G(I* w6 }9 S7 i6 s. [ CAM, A rotating device for movement of mecha' u8 G# P. F& } y* L5 E8 E C' E% j; Z- L1 J: ]7 F+ {* o+ D. R4 @ 旁通活门 & @% C* n+ M+ Z2 p气流或液流在正常通道阻塞时所经过的活门。% r( [8 N; u5 [. F9 A3 y1 h3 p; ~, i: T; }$ J. p3 M/ L; c* j3 m. {0 q1 M& o* a8 O/ Q! x, ]0 F4 x$ n3 Z/ k* p5 X( m7 K0 a4 J/ M) K凸轮, + E1 y, T' P8 `9 f+ y1 y英汉对照民用航空词典B 7 y4 i' [6 j+ yCAM-OUT, An autopilot condition in which the actuator ! p* e( N% P3 \, Kdetent piston is overridden, either manually or by the 7 N* @; y. n2 _6 cther autopilot actuator.8 I& e- r; `) f3 J' T AP, SEE - CAPTURE/ d8 a- S9 ]' E7 J APACITANCE, The measurement of electrical energy 6 b: {& ]$ F3 B: k& d# z, ^4 Ktored in a capacitor (condenser). 2 @9 g2 O% r# Z' fAPACITOR, An electrical component of two metal # ]/ A% A6 o; Dlates separated by a dielectric material, for storing 2 H) c& s, D- ]* B X+ M# Qlectrical energy.4 _. q0 D2 o7 U CAPTURE, An autopilot or flight director function to 3 K( C/ r' w8 ?, J$ R- r! Macquire a selected mode.+ w2 Q$ m, j4 w; ~ CARD FILE, A container on the airplane for printed % }& D8 n( ~4 W, J) D: Q6 s' }$ dcircuit cards. + W4 U& \2 I6 |3 k m; o5 K1 k一自 * k7 C R( l3 V0 E4 |( a, l动驾驶舵机所超控。 ) S8 ~: {7 `. ~3 Q {截获,/ W" T. G; G6 O3 Z+ a5 \7 z9 N 见Capture+ I1 t$ g2 s+ {9 Z o" L$ z, x7 G: x$ S3 }/ p C " F' N/ _' S$ BC+ |9 ?5 Q6 o* t5 J1 | s! G( g: X8 u5 X* O+ C# V C 3 D; I- W; y% h" \% h( Dp, R' A3 p2 H! r0 R0 L e 9 |1 O! O d" Q" U1 f凸轮不工作, ( i1 _! y% u7 G; o8 o: j# N一种自动驾驶状态。此时舵机锁定活塞被人工或另 * I% J% ]9 h9 u, x3 Z4 d9 x0 t# r! F2 X% U/ g4 B% v4 S9 N' s$ { 电容量, " v4 ?$ ~: w4 S2 {% |电容器内所储存的电能的量度。6 k" q' {7 R! a 容器, . u2 B6 `0 I9 d( j+ E两片金属中间用绝缘材料隔开的电器。用以储存电能。 # s" `9 |! e, w0 D' m截获(CAP), 1 y9 ~* T0 R" R3 B+ [自动驾驶仪或飞行指引仪的获取选定方式的功能。 & H, y+ k( r, W( z2 g$ Z/ o9 G线路板盒,8 o0 i) e7 m. V2 H. k% h8 ? 飞机上安装印刷线路板的容器。 # t, V! |8 d* M: U( i6 v3 x) ?# N7 }0 X7 S& H9 ?2 ZOEING / Y: u$ d/ T+ f; r2 E7 |TECHNICAL DICTIONARY 26 - b$ Z" z8 Y0 D英汉对照民用航空词典B OEING 8 _" U$ [3 x& D* @- c- \6 hTECHNICAL DICTIONARY 27; U# R( z6 T3 n; B' N CASCADE, Two or more similar circuits or amplifying! q$ Z/ O$ \; a* s! g* L. [2 k- Z1 G stages in which the output of one circuit provides the3 m- d" }7 ^- [ put of the next.3 \- r* _8 u! h: w6 Y ASCADE VANE, A vane for turning the engine airflow , B: y; v8 U/ nuring operation of thrust reverser. ) C$ J; W+ X% C D5 c! N$ i+ xASE DRAIN, A drain carrying lubricating and cooling h; a! z' X' _8 Duid from a hydraulic pump. 6 q/ O; a9 `2 w# b7 _0 XATHODE, The element from which the principal : X# g D! P# v' ?4 M3 ztream of electrons flows. ' I4 v2 w4 S. u. p$ v% BATHODE RAY TUBE, An evacuated glass tube with a# z! d9 e0 G% L: O' ~9 U CEILING, The height above the ground or water of the ( p/ f9 ~! }2 c5 R7 s/ R \- Tbase of the lowest layer of cloud below 6000 meters' L/ e; H, Q* z; T3 g6 b (20,000 feet) covering more than half the sky.. _' E2 b N" P3 r3 M 程。该 & l2 z6 }' t. z程中,一个电路的输出为下一个电路的输人。 ) v- g( C9 n3 p8 y ?1 Y叶栅叶片,3 ]- z. u% \$ m \1 V3 X% A9 L 在反推工作时,使发动机气流向相反方向流动的叶片。3 j9 w3 |( c6 n 匣余油管,6 t% I4 i9 d4 e2 W, F 液压泵多余的润滑液及冷却液的排放口。 . D$ J9 M6 K5 I极,6 D5 [( ~' W& o5 u( l6 K 电子流流出的极位。 ) L- a' s! B; g9 B极射线管, : `& `( R" [+ U5 b# @有显象屏幕的真空玻璃管。用于显示信息。; w$ w f8 o. E" i2 w+ d7 ] 云高(云底高), - R0 ^& _2 d! E W' W$ N6000米(20,000英尺)以下已覆盖一半以上天空的最# |' F( }7 c, C: z$ d; p2 D 低云层底距离地面或水面的高度。 8 f, e2 r1 S8 a8 ?4 b% @0 Pin 0 d0 Z1 A+ `) r/ LC' d; C3 z* ?) o% k d9 u$ y& {" c: C: o3 R" R: O C # H$ p3 }: o6 n! t: L, G* Tfl / y* K" M1 H+ S( m/ }C 8 q8 f" Q1 l; ~, ?s ( Q2 p* r* ]- YC , }3 G- Q$ t9 e2 w1 M a' Z/ ?1 Mviewing screen, used for displaying information. ) \2 F* I: n b. H( i级联,' `% t' l8 Y+ _ 两个或两个以上的类似电路的逐级连接或放大过 3 Q: C6 O* [7 C, Q: L k6 s8 r) t' \" t: r6 m0 n0 T, n6 p0 G, e F0 j8 I, u. D. {$ M* j; v7 l: P5 |& d; @+ p. [ 一个具 0 Q" m5 E, [5 U/ y英汉对照民用航空词典B OEING , u$ r1 r/ k3 \6 V' WTECHNICAL DICTIONARY 28 & n; | p) m" KCELSIUS, A temperature scale in which zero is the/ {4 V, Y3 L1 ^+ L( c D freezing point of water and 100 is the boiling point of& X" `! [9 }; F* i/ d( u3 t5 f P water. 8 A+ a- {: I& ^( C; v$ ]- |CENTER OF GRAVITY, The balance point of an object : X& S9 E, X$ i! Ur rigid structure expressed in terms of percent Mean7 s7 S" r* |0 P! I* { erodynamic Chord or in inches from a reference point.- x( b; F1 s: { ENTERING CAM, A cam for moving a mechanism to a( S" b. r; t" j9 M3 n eutral position.' S+ X& g) u9 b) p6 w1 p IGURATION, A configuration of the u: P7 }4 o' C ircraft approved for operation by the local governing 6 U$ E+ i/ U: agency.2 t& ~8 r: d; D5 G9 h ENTRAL PROCESSING UNIT, In a computer or( O2 C6 V7 o( L4 S- U' S igital circuit, the section containing the arithmetic and& F$ N8 L2 @; x3 M gic,control, and internal memory circuits.$ W% `2 a5 a8 A2 U3 G& t) R. k, A5 t2 ` ENTRIFUGAL FLOW COMPRESSOR, A type of; U7 a4 b& ?6 d1 D ompressor in which air is taken into the center of the: B2 ^6 i! o0 B5 r4 Y9 W peller and is slung outward centrifugally into a diffuser7 n9 [ S% M: L) } here it is slowed and pressure is increased.' q- X7 l9 l: f CG, SEE - CENTER OF GRAVITY 8 i" l5 }2 q) y( v& h( X: d构的平衡点,以平均气动力弦的百分比或 - [& m/ y. c# l某一参考点若干英寸来表示。 ( z6 O& \( D- G' c, _" g中凸轮, ) g) W) E; Y V: O& y将机构移向中立位置的凸轮。; t( p3 p9 P- P1 U 格的装机状态,; H0 K" [8 i% k& S0 P" o. a 由当地主管单位批准使用的飞机装机状态。 : J; l! m, U. }中央处理器,2 [' T5 k5 e+ F2 y& E: r 计算机或数字电路中含有运算,逻辑,控制和内部存7 L! W6 v* s5 t. P6 h+ D 储电路的部分。9 J! O* T% A/ p5 O- u 心式压气机,5 T" ?$ i% ]* {. T3 I" |3 V 压气机的一种。当进气到达叶轮中心时,被叶轮离心抛# d0 e' [/ W- U4 @ r 进人扩散器。在扩散器中气体流速减慢,压力增加。& M/ Y5 g2 ^8 M' _ 重心, ' I d; X* {) u# g' p1 X9 e& W见Center of Gravity 0 i3 i" }% z1 ^5 A' Fo. s# X$ s9 j2 Q" ?) M9 ` A! o+ d U8 `: ^# O1 v C( z1 f% _* r, M! f3 K m! ~ n/ _' o) ?4 G7 ^3 J. @7 X CERTIFIED CONF- Q a4 {/ z9 V% U" c a. X6 f& `* b1 T- X/ h* f a , l2 s- X) K- HC 5 z) F6 H& F* M. {# G' B" Sd: {, I9 B" W2 E+ w i/ a7 C, R lo3 R1 [ N+ G8 L4 O C 5 C" [2 S! d1 b) S- X! i1 [c , D& y; J% J1 F3 M: W- p6 P/ Oim - M" F# t& y0 j' P$ W$ bw . l' G0 t0 a- j8 Q摄氏度(°C),: r0 Z) e; [8 W: ~) g9 \6 o 温度的度量单位。在此单位中,0°C表示水的冰点, 6 c `2 m" |, Y, t100°C表示沸点。; B4 F) g' [& V. S$ W/ j9 J$ S: W 重心 ' L+ F3 }# s1 O6 U物体或刚性结 ^& F \3 B" E1 v; q8 T$ L$ b7 ^, [5 A$ ^$ Z; U7 Y$ T3 x" c' c6 E' y/ {2 }" Q; `7 n1 n! b; ^% `/ W2 I/ k- e9 X6 W: ~" o% u3 U* a1 { 英汉对照民用航空词典B OEING + n& J7 L1 p& q& F' F# Q- `0 C! x3 fTECHNICAL DICTIONARY 29 4 Q. ]2 {% E4 B, d+ C/ u& \CHANGEOVER, Conversion from one mode to another.# E6 p( ?! F* p HARGING VALVE, A valve for supplying air or fluid to# }: J% g3 X; u0 V2 l2 s2 L HECK VALVE, A valve allowing flow in only one $ B% Y+ e8 k" m9 C) T, Q. Kirection. See Non-Return Valve.9 a# t" z0 f4 G2 K1 K0 R. h6 Y+ N HECKSUM, In a computer, a summation of digits or 9 F' c0 [, O! {, p9 r mits which are primarily used for error detection." q. R3 G+ g/ L: d- u- c8 B HIP DETECTOR, A magnetic plug in sumps of' S9 m5 e; j% K( J: W6 P bricated components for detection of internal failure of" G7 O# @! a* u2 _% ^ e component. * N8 t# b' e7 a2 x# L& THORD, A structural component of spars or frames. 2 c6 p$ G6 A3 H/ v+ O& P添活门,) F' x; V: A7 Q! i 器充气或加液的活门。- j/ G: L# |5 t) D3 L4 h2 v* U 单向活门, / h7 X5 X) t& }) E$ R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 8 {& Y' g k( {0 d3 u0 k; r% |/ O# ca reservoir. 8 p/ A: {3 F0 I) @$ pC 8 L/ A$ H) A3 W2 |* u$ Z* qd4 w t6 K9 n$ d* L C & p; Q: t' C& u% ~( ^; E, I* F3 k( {b % a7 |. r4 O# c; LC" H+ R1 v) F2 ^8 {. d: v lu. l" N6 R. q; ]8 H9 U th# X: R% q4 x" s8 p C2 ~4 g5 P+ g% ^9 w) R. f, Y 转换, 2 V5 O! e L) m7 x6 H由一个方式转换到另一个方式。 0 I) t4 Y7 ]- |+ s# N" e h$ A2 h; N1 W 用来向储存8 b4 l+ _3 j* C8 s$ j V* ^- E; v$ ~7 m3 T/ z总和校验,; r8 |1 [2 } t4 _1 G. v 计算机中,把那些用来探错误的数宇或位数的总和进 ! D9 | o& o: X/ N. Y- K: F求和计算。2 H! \+ ^ q9 R3 m% a& d4 H* D 属碎屑探测器,, I' B! `- l3 ?" S6 Q+ i: [ 装在被润滑的部件滑油回油管路上的磁性塞子。用来探/ A3 `) j0 X0 h, s& I& q' c) A; r L& i 部件内部有无损坏。 ! N8 y ?3 ~$ s+ k5 X6 a* T弦,6 f1 i+ b: g ^( {8 }4 m# _& n" t 梁或框架的结构部件。 % k6 n2 @/ \6 n% y- u. R# N- `& |3 @# o% A2 C0 h1 d1 h. G! E2 e0 c, `% l, x, B* `: p. x& u. a0 G- `3 W# \; x$ I7 R; `. F& y* U1 Q, i. P( u9 G/ d8 s; l 英汉对照民用航空词典B OEING # G- N6 z: K8 x7 g# tTECHNICAL DICTIONARY 30 ; n( ^+ q$ t# L& S3 f! h% u% b( SCIRCUIT, A closed path through which current flows Y5 d9 q3 \- H3 M ource.# m, w- F2 D! @# A& i IRCUIT BREAKER, A device that automatically 6 O$ B( T+ V; O3 w$ X' veactivate the system. 0 E4 K( |0 A7 c2 `lear of all non-frangible objects which ( \; m7 d) f0 y1 Zay be used as takeoff distance available when; v1 ~2 j, `# g- z alculating a takeoff weight.0 x9 D0 s% ~ P" j2 @ r water under the control of the appropriate6 r* j4 s& p& I; F; P( P8 v6 ?: t uthority,selected or prepared as a suitable area over 2 o8 m( {' r9 b( B: J7 l% T- bhich an aeroplane may make a portion of its initial( B( O9 x6 g ~7 U limb to a specified height.. ~. X$ z$ N+ Y* }& { increasing. . L# U6 u; a+ v- f) i4 M. ]sed : G4 [! p7 z+ R4 l0 k/ H+ h! J: y; wLOCK SIGNAL, A continuous string of pulses used for+ j! o- x, K1 t/ J, Q- P9 O 开关,7 m( U+ z! J- D0 v9 D 故障情况下自动中断电流以保护线路不受过电损8 D6 }9 K& Y5 t" m 体障碍物的区域。在计 ( g; s c, M$ K w7 z5 v( D起飞重量时该区域可作为可用起飞距离。" P2 }5 w; e s& q( i7 W9 E& G& N. r 是在有关当局管辖的地面或水域内一个界限明确的长 6 a3 W t6 d- x# f @% W5 A/ u, R" |形区域。在这个选定的合适区域内,飞机可完成初始爬- U S- m0 h, p* ]6 b u 的一部分,上升到一个指定高度。. |& X( c! T) @ 飞机高度不断增加的飞行阶段。 / m% {3 y( U8 y+ a+ G O: I. C钟脉冲,0 _" V+ E% E* I8 A8 ` 步的连续脉冲信号串。 # z6 D Z* W$ r I6 @4 ufrom a source, through various components, and back % {4 T5 G; j9 V# {* [: Q: F( uto the s # }. ?1 |/ [4 TC 6 {3 m F7 w1 _' |: D& g# k, Minterrupts the flow of electricity (current) during fault 5 ^7 G4 Z6 E- H8 dcondition to protect wiring from excess current. Circuit, F, m! F. x7 q' e breakers are also used as a means to manually: f2 I; z! V9 G& o$ D' w d% g5 W* E) X$ I( a/ W' U8 C CLEARWAY 1, An area beyond the takeoff end of the . W% Q5 T$ J0 n# v+ B i- lrunway which is c % t2 z2 e' z6 R% H3 R1 J' X+ o) nm+ D1 l) d* ] N/ Z/ U c $ |- S. c8 f' R$ J8 cCLEARWAY 2, A defined rectangular area on the * _0 {* t0 l6 G7 Kground o . E* v: @# @" [a " Q/ g# C2 P5 P u# }0 Y) Ew # G! t5 M' ?# y- G" a# bc ; d/ [# X, f5 v) q" }CLIMB, Phase of flight where the altitude is / T3 a% W- @/ T; sCLIMB LIMIT WEIGHT, Maximum takeoff weight ba 4 f7 c' s9 G8 G5 \) aon a minimum climb gradient with one engine g& X6 v" Z8 E* u. s/ ^ inoperative. 5 b3 U. }5 _6 Z+ FC8 A/ o1 x2 `: L synchronization.+ u+ A% M- q5 A; a" {' Y9 z- v6 A4 i 电路,3 L$ D8 W J: d1 N; [+ Q# W; D 一个闭合的回路。电流由源头流出,经过各个元件流回' L5 R: y0 {- s' m 源头。 7 i1 d' H% R! S4 A% u8 {0 ]4 T6 h7 i' a: g% E9 C能在- U- B1 ?, f! H 坏的装置。跳开关也可用于人工使系统无效。 8 {2 l* Y" I2 e- @. Y5 J: c4 t( w一号净空道, + H7 W/ H+ `' X9 K; e5 q* Z是跑道起飞端以外,不含任何刚3 X* h3 W6 W+ G7 t' B4 u) H. C8 B 二号净空道,3 ? a1 y% c8 V5 w9 n6 a1 V7 g& L7 j6 G9 s+ D$ H( p- {7 f; p7 Z" r" f! _% Y# R( V爬升, 1 w6 @4 u1 G3 G5 r; z% `2 m爬升限重, 0 G' N+ s* Z! C4 [6 }2 J7 s取决于由一台发动机工作时的最低爬升梯度的最大起 ! s8 S/ w3 D4 R5 g飞重量。 4 z) ~; ]% [5 g& p4 p, M u. A/ H- q9 h0 ~用于同 6 |3 e; q$ U& g- k5 s4 j+ |! P q英汉对照民用航空词典B OEING 5 f' i; L" O/ O" r; u i7 @# ITECHNICAL DICTIONARY 31 1 w( x+ i0 O* N0 }/ i- c3 z6 N6 HCOALESCER, A device in the water separator for 2 x* A6 S+ Q. e$ _' M% @' ?ollecting moisture from the cold air. . R, d) Z2 l, Q( H, ]) J5 j2 Qn antenna with a receiver or transmitter. 7 ~' o2 a x" i! ghe cable has an inner conductor and an outer 9 e% S/ X* z# P* m Nrounded shield.4 s- S5 M8 N/ g3 \1 n/ t ting one inside the# P' g/ u4 D8 B! j ther for rotating the low and high pressure 6 [6 l; M( h" E" x2 Nompressors by the low and high pressure engine' {: P ?% X% W4 |9 o. N1 c0 e) }0 Z rbines. H! E* E/ }5 |4 |1 s) yOMBUSTION CHAMBER, A part of an engine for" e& r3 j/ p8 ~# }) e, a. i6 V9 [! P1 p urning fuel in the air supplied by the compressor.+ \9 z+ \1 a9 K$ ~& _ 置。' E' Z0 a* Y9 J/ f" y 射机的电缆。电缆 0 V* ^ c9 a8 h中心导体和外层的屏蔽所组成。% H# n! G0 X+ H# J 两个套在一起旋转的轴。用于使发动机低压和高压涡轮 * F+ Z( x1 q9 p, i/ B- j+ B/ {1 h7 ~别带动低压和高压压气机。 - q7 p% c' P! b9 q烧室, $ e. y* s/ k' r发动机的一部分。用来使燃油和压气机所提供的空气相 ' Y( t& Z$ ~- H$ e( d* |合而燃烧。

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发表于 2008-12-24 21:38:35 |只看该作者
c2 A, X$ n' p R2 s- @ COAXIAL CABLE, An electrical cable usually ) G, H/ U2 P" M u+ M; ?connecting a, f! @2 r9 @ ~% }+ p3 T T2 [! O3 l& X, G5 N; Q9 x+ R g * l' @5 R6 w# X; ~. }' @COAXIAL SHAFT, Two shafts rota O& M& ^8 `+ I o . A" H# ?8 j3 N; vc2 c9 I' L3 |+ @" p+ @ tu 5 J7 f* ^2 E- ^; r* Z3 @C% Q' ?2 e! ]" g& I# B; p5 z3 o b& z$ x5 p1 _" l [ 凝聚器, , b0 N* K1 B- f水分离器内收集冷空气中水份的装 # V+ j1 Z* G3 ^& D& y+ e x同轴电缆,, p! t j, ~% I. j$ a$ O9 A$ y 一种通常用来联接天线与接收机或发$ ~& q0 `, ?6 h4 u" h8 s* Q# L( r. P [, S* i! [# A- G# T 同心轴, & J& e2 a2 E; L7 K4 }9 [0 K' r2 {! v2 t! |. l: W$ _% I) f3 A$ W+ N3 ?3 R" f& N3 v* y2 y( ~- `7 i3 n 英汉对照民用航空词典B OEING3 a* i3 {3 d# u TECHNICAL DICTIONARY 32 " V! x6 ]% c7 h9 j" n- A9 N- c0 ?, k( zCOMMAND BAR, A flight director pitch or roll comman* C, m8 p, k- b. q. c, M% U indication. : l, w- K6 Z. t; i% {7 F: d! L. f4 dd; B# v& u! ?: J% Y. P3 |/ D OMPANY ROUTE, A route flown by the airplane . x3 f6 [5 Y& n0 c5 @; l7 J( XOMPASS LOCATOR, A low power, low or medium 2 R9 o0 O4 B4 r) } \, Yequency (L/MF) radio beacon usually installed in. k i+ Z* r6 X$ ~9 P @% q onjunction with the outer or middle marker of an0 ^5 n: k4 E H tor (LOM), A compass / D2 ^1 A) G- m) x3 A9 Flocator installed in conjunction with the outer ' }) r) T I, Qmarker of an instrument landing system. : K# B6 v" ~2 Qss. \# `' i$ x# S* J6 K# \( O5 ^6 v le! i. m* ~. h/ Q) U. o# S- e OMPENSATION, To offset, balance, or counteract. 0 W5 G" Q5 u3 j' J0 K% }* fOMPENSATOR, A dual capacitor for changing the fuel : k% Z1 E% c! l2 }+ P2 }aging circuit capacitance due to changes in fuel7 I# K0 i, d0 T/ C8 U2 @$ h, Z ensity. 1 S6 m$ s/ d4 x) R& r m4 p3 {1 xOMPOSITE MATERIALS, Non-metallic materials used / h7 v& f* Z# d: G" kr airplane construction. Fiberglass, Nomex, Kevlar, & }, } d& K& R! _raphite Epoxy are composite materials. 0 U, x2 p" F- [. [' Y8 l司航路, e" s* I* q) k+ V在飞行管理计算机数据库内由航空公司飞行! J/ E! d& V1 s* `! l* Y 盘定位台, , L) k* C8 Z" [, G6 f, X, ^/ }与仪表着陆进近系统的远距或中距指点标配套安装的* {+ X& P# @, d/ l* x( V6 e 功率、低频、或中频无线电信标装置(低功率NDB台)。- K# J& L* n/ `8 x 程序中用来导航。3 K8 o7 _2 M1 f: h; B t0 k 1.远台, ! g& E0 R% ~; r: ~# t8 m! W- L v, {与仪表着陆进近系统的远指点标配套安装的罗 5 Q; j; S" ?, v8 E/ i% J% y, p9 V盘信标台(NDB)。 3 \* f; ?. d* X偿,% I; k5 t( {1 P T \5 Y0 i 抵消、平衡、或中和。0 @/ f' C- r+ ? 偿器, # Y7 J# c5 b+ Y) t3 j* o在燃油计量电路中,用来改变电路上的电容,以与燃 " b3 @5 r( H' e- Q; g3 c密度改变所引起的电容改变相抗衡的双电容器。 & W0 P x1 v N2 z4 d' B合材料,+ `1 o6 @3 \2 R( g2 V. T) w 用于飞机制造的非金属材料。如纤维玻璃,Nomex, ! V( A1 f+ ]; L C8 C9 Z: P; d" ^evlar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 $ |* g% [ X' k$ W* d* h5 |operator that is normally stored in the flight2 g1 }& I3 M& e management computer's data base.( E9 O0 m. x1 L! B1 u C * J1 P; r5 H" S* ?, W5 z5 \fr" {7 ]3 s( l: J' [+ ~, s, P c! `& e8 A t" [) P" q instrument landing system (ILS). It can be used for! o& n4 J/ F9 Z" I& } G navigation as authorized in the approach procedure. % M" {; O9 C$ m, n$ F, u( \1. Outer Compass Loca * E1 _ u4 b" m2. Middle Compass Locator (LMM), A compa9 h5 x* }4 E9 ?- U+ X locator installed in conjunction with the midd 4 U, z( U' s- D- d) o4 M8 Tmarker of an instrument landing system. / r! P+ |/ c$ |7 A, n: w' Q: r8 ]# H. r; nC0 j% p2 v* f) p0 R4 E0 @ C ( D7 y$ \% O: ?) f# q8 lg) X5 f- q1 h9 e8 Y1 Y+ P% D d* i) }: V7 i8 i- d% {, u7 g C; h5 v+ L. E/ K1 o" H fo. p& l; q' I) H# a: D g 3 r3 D9 Y8 Z \7 w0 s! U7 A1 f指令杆, 3 Y, N! Y [3 I8 z; {% P$ N. k飞行指引仪俯仰或坡度的指令显示。; m- d* v% u- `( U/ @% x v+ O, G+ r+ x* Y, r7 o通常储存 0 Z3 V" u2 U P7 z1 S5 Y9 m0 Z的航路。 - j' b: U5 M, a! d. v& r. [! c2 _$ P, U0 q. {7 R6 [" w; F- g& U经认可后在进近 / P. {4 N) [/ P7 |3 g3 I, |2.中台, 7 j- B! V. f* Q+ Q; [/ G' q) P与仪表着陆进近系统的中指点标配套安装的罗; ^% }" V9 Y/ w+ O 盘定位台(NDB)。 , w6 H, `0 _1 u* q! a K0 [' v2 Y" b3 s2 R% W D8 k5 ^& f5 t7 B. R, {/ H. ]# M. W1 i6 B( T! Z/ D1 f2 U K/ C: @- k1 A6 L% M, |6 r 英汉对照民用航空词典B OEING) c4 V5 U' y: q/ U& v2 A TECHNICAL DICTIONARY 332 v, B) X# Y9 b! K2 R- t3 `0 D by / R) `0 P. P0 y6 ?( ^: Uor increasing air + {/ D, T4 z: W8 u& l' x& c0 qressure and temperature before the air enters the ) G; {9 r0 J3 V% m5 ?+ E( y* {ombustion chamber, Low pressure compressor - front ' u8 @3 y5 d9 U1 l$ r7 Pection of compressor, High pressure compressor- rear4 {- \ r ?9 ^* y! e2 M6 I5 ] OMPRESSOR STALL, An event that occurs when 1 h! Z0 P* N8 Z" G/ K4 I- cere is a complete stoppage of air or reversal of air flow ( s7 T {3 i3 f* D# k0 FCOMPRESSOR SURGE, SEE - COMPRESSOR9 h }, s2 T3 G( B2 o4 e4 | STALL COMPUTED AIRSPEED, Indicated airspeed . m0 t: m' \& N/ P& O% Vcorrected for the static source error.# P# d' Y* v& ^" e 的机械轴来驱 / D3 E& A, N) k2 @,用来增加吸进空气之压力和温度,以供燃烧室使用。7 _8 T3 R( T" {6 `, h 压压气机—压气机的前段,高压压气机—压气机的后 & ` x+ n/ i2 A2 h( h3 g L) }- j: S: ~: Y 气机失速,% U* K" G5 ]. f9 j0 k 当气流完全停止或通过压气机时气流方向逆反的一种 . }: t7 D5 F% ]5 T. ~' s, X压气机喘振,1 v7 l: v. a, v" t( K! k 见Compressor Stall( _& i/ P+ @7 \9 B5 A COMPRESSOR, A rotating part of an engine driven6 t$ a& ]& F7 G8 P2 i3 n0 A a mechanical shaft from the turbines f* w) t9 Y: g) c0 v p : |6 r9 L5 y$ ], J9 E, ac % X1 j* H* K* f# L9 ^" K) @s - X# a5 M9 m0 O- vsection of compressor. : |# c& M7 X, d% RC' t+ S) o+ {( \" a th " y+ j1 i% j7 O3 ]' N0 B5 |' W, ethrough the compressor. + J3 c* @. `% K( E& g% q压气机,2 T# ]8 v9 f( ^5 l# q 发动机内的一个旋转部件。由与涡轮相连& s! z G- N* t9 s6 @3 d$ v& P: s0 P2 [& g7 [1 r. B# j- j' C+ o1 u2 q8 W' _. O3 [+ M0 e( w4 j* s; ]现象。 4 t* q# b% X: B0 e) F4 G8 o2 d" M A* I' I! t 计算空速, 3 b% _+ n7 Q3 H6 V/ F2 g5 B; a修正了静态源误差后的指示空速。* L" q+ Z! w- ?; w' u 英汉对照民用航空词典B OEING5 T6 Q# A4 I2 n i4 f; z8 \ TECHNICAL 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, W! H7 i$ }# t9 O- u operations, manipulates data, and makes decisions. 5 r2 V4 `+ Q" P5 ]$ d8 K% L5 s' Xditioning% ]$ P) g: t7 u z. l5 g* m5 | the air and the& k; v4 o# l% f" w7 u- t frigerant or moisture vapor is changed into a liquid. 7 N; p1 Y( {" z- L2 W& Z& N: Tine . G3 z2 N8 X ]7 s; qONFIGURATION, The position of flight controls, 8 m, q# Q" e9 y5 S" smissing which3 i: Q4 M/ f3 `- Z$ @- T may affect the aerodynamic performance of the 5 s1 s" { f$ P4 d2 kairplane.8 U% \! T, Z _, R; Z# u 置。0 O. q, [0 ]6 |" g: r, k4 G1 r3 N 中能使热能散发到空气中,以及使冷冻剂或湿 / v) K% z2 v0 G转变为液体的部件。 7 z) m- ^' ?% a% @连接到飞机结构上。; b& I( R, W% Y* V/ b* w$ A. S 态,. ]. W9 K! L4 w) @0 e' Q+ F 定飞行阶段中,飞行操纵面,起落架等的位置。 " _; |7 Z- O' `# o2 S), , ~) Z; z3 m( h; e7 |1 U+ [ y1 V# a受到影响。5 h6 t9 T' W# }9 B8 O8 G9 M CONDENSER, The component in an air con ) }4 ]' E; D. e) o9 [6 Qsystem where heat energy is given to 8 g0 `2 x7 Q3 ~; E7 @; {$ j, `re6 P6 `+ P" h' ~: p7 z0 i& I) Q CONE BOLT, A bolt in the shape of a cone for eng I+ }$ K' G6 X5 {8 } |9 p attachment to the airplane structure. . C8 V9 r- s: h# k; g, Y+ U: z7 m) cC& M: Y/ o0 x- o1 s landing gear, etc., for a particular phase of flight, e.g.,& g4 v9 c2 _8 H3 ^3 x* [# Y5 a Takeoff Configuration, Landing Configuration, etc. ' m- `5 G8 @& |, m; f _$ tCONFIGURATION DEVIATION LIST (CDL), Appendix* w: R( j3 ` r7 W& e, M0 y- O G) ] in the Airplane Flight Manual (AFM) allowing operation8 W- C9 t1 k" L( O: g K" A: V of the airplane with certain airframe parts ) R4 K; f! p' Q) D0 a% X. z# U计算机, 8 C5 C7 [: _* ^7 s" e$ j能作算数运算,数据操纵,和决策的装, y4 B; m) {3 P. ^) L8 z( U( ~ 冷凝器, & p, V+ g* M1 ~2 p- P3 i1 n空调系统 b2 M+ w e" f- s: b2 `5 l; a) Y! g1 [ S5 x锥形螺栓,5 G4 }! k6 W I& M 外形是锥形的螺栓,用以将发动机* Q- v+ I }! c) d, X$ P: `; _* D2 Q# ?# X9 @ 在某一特8 D6 X& N. B5 U* g8 X. y 如起飞形态,着陆形态等。+ y2 I6 U. Z {% w# U0 N& ? 缺件单(CDL # L3 H3 j' f8 V/ N4 I+ X% s飞机飞行手册的附录所开列的飞机上某些零件的清单。: ?! Y' o2 H. i6 }/ u9 y 在缺少这类零件时,可以飞行但气动性能可能 8 m8 W, `2 N; G, L' K英汉对照民用航空词典B OEING# k4 v9 H4 z t- o/ ]/ e8 w: O' T) B TECHNICAL 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 + a1 G ]& k: k+ [! H2 jcomponent for changing variable engine gearbox speed! K( _- r* F; x; ]$ @4 K. h ONTROL AXES, The three axes of the airplane which1 E% L( c$ d B" k# Q/ i% h re perpendicular to each other and pass through the& k0 @1 \9 [, g- ~ enter of gravity of the airplane.- a; K. ?- E. w- t+ J. V+ y7 l Pitch axis - Horizontal or lateral axis, passes through" c4 B3 z, P/ A1 Y, l6 U, v3 J, T the airplane from one side to the other - ; X) K7 P& K; y9 r/ Knose up and nose down control is by & v$ e( a( }: L. M( Felevators (and stabilizer for trim).4 ^# `- p8 N3 U+ i) Y Roll axis - Longitudinal axis, passes through the ; x9 G' ]/ c& ]0 \5 `( w- g# Lairplane from front to rear - wing up and 7 k# t( ^. |: U+ c; K& {4 d/ Dwing down control is by ailerons and! E( v% [5 r0 n* I# D flight spoilers. . d' Q5 l8 p% v) S, x& {Yaw axis - Vertical axis, passes through the ! T; d3 ?$ z8 |. [4 M+ Iairplane from top to bottom - left and2 S0 H8 g; H' b2 q. ]1 P right control is by rudder. x! T4 c, `6 t* z8 H0 R2 z- I 置, $ p" q$ ~3 v/ V2 F, r制轴, r& u. H7 \* `& O通过飞机重心互相垂直的三个轴。3 C" ?3 @& W! s6 o 俯仰轴—又称水平轴或横轴。由飞机的一侧通向另$ R& ]# _; P6 D& M 侧。飞机绕此轴转动即造成机首的俯与仰: X; H3 k$ K" E! g 俯仰控制是由升降舵来达成的,水平安定 6 U/ a Q* _7 c6 Q! D" w则为配平之用。* X1 W: h$ i& c& d1 a 横滚轴—又称纵轴。由飞机的前部通向后部。机翼 : Z6 R# P. p5 {. G0 K2 p- u a下运动由副翼和飞行扰流板控制。 l# l! g! I3 }7 {9 N 偏航轴—又称垂直轴。由机身上方通向下方。飞机- W' y: f1 T6 I3 p0 _1 d. `* x1 A 此轴转动即造成机首之左右运动,此一运% a, M) e: D1 W- Y8 q* @) i 由方向舵控制。 ) L! M" s" C! _: ~! ato constant speed to drive the electrical power. ' s9 }5 a. c2 _1 f1 m f( zC : F# x# H7 c" N& j* N% ?a ; s( A' i }; ]+ _8 M! Ic 5 U2 |/ F' v4 ^5 F1 Q恒速驱动装 5 E T$ L- `! w# {将发动机齿轮箱的可变转速转变为恒速以驱动电源的 ~% v5 v. { d 液压机械式部件。0 b! C3 r* t3 s7 x& S* ]1 S$ n5 M$ V p* s& A8 X9 d: u8 o* Z' H+ t m) S* X& \0 k7 F2 m; |' |% q! g; f5 R: r! e- e* p& H" Z& V5 V# `. d; ?4 ~3 G, O" `$ i5 Z' Y* R+ d6 v! ^# G d. }2 a7 r# I& |; X6 M. | c( h英汉对照民用航空词典B OEING/ t( C( _: V8 h/ z# v TECHNICAL DICTIONARY 36: r& B+ ]8 x: q# Z CONTROL COLUMN, A mechanical component used. E6 p' P7 S/ l4 e4 d* D$ ?7 C rs/ [5 p( q; y7 P" R* i$ S% Y nd elevators. 3 y; }6 s2 Q- E2 ]+ uONTROL SURFACE, Moveable panels on wings and 0 o. F0 N% r8 E1 g2 R2 Q1 [il for movement of airplane on pitch, roll and yaw axes.! ?4 G& ~( w( u3 C8 Z8 P, o ONTROL TAB, SEE - BALANCE TAB @8 ^$ A' s& p4 j3 u, e7 G1 ZONTROL AREA, A controlled airspace extending, b5 E- h, {6 H B pwards from a specified limit above the earth. 5 |: b/ b' ]6 S; wONTROL ZONE, A controlled airspace extending" B/ P: O# W. @/ d pwards from the surface of the earth to a specified: T) ?4 S5 C! [1 `. E- y pper limit. . a9 n7 A0 [) V! [9 p/ n6 W8 uis $ f# q+ s0 N- q Lo IFR flights and to VFR flights in accordance 9 M9 U, }7 s6 \) lwith the airspace classification.9 Q6 z) x2 a. @: Y2 S+ k7 V" ^ 机械部 9 h3 P- g: t4 ?( V1 J* e1 V5 |0 i. X3 I& k9 t) Q 操纵面,5 D- Z- Z/ C; d' `5 Q4 p 机翼和机尾上的可动面板,用以操纵飞机俯仰,坡度,; u: g) i5 h4 _. C/ G6 U% c 和偏航运动。1 y* c) p0 m" O5 f* |6 i4 m 操纵片, ! x& I8 x6 x- B" D8 C5 J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. {) S& b7 z1 F$ z a" k( x9 P) Y5 g% e) `/ c8 S C5 c4 E* J9 L* N# M4 [7 \. i ta# H2 p: n8 N, p7 t W C $ ~4 L: i0 D8 R) }+ M" _C" x+ K0 I8 b& l1 J u( `6 Z: P' v7 C2 m+ [8 y9 n C8 A7 {: v9 _+ Z u $ B6 L6 ~" M; [% z( mu& X% O! I$ I3 ^8 ^+ q CONTROLLED AIRSPACE, An airspace of defined. I4 h. A @+ H) d, h dimensions within which air traffic control service / j( p6 T; t: C' pprovided t - J g5 U3 R. @驾驶杆,- v; Q, e7 @9 W0 d: V/ o5 ^" w 飞行员用来操纵副翼、飞行扰流板和升降舵的 % ` x# a9 u$ o8 A! P' @0 C: R4 z6 V+ J D9 _2 w! M. G3 j8 C6 C. Q+ g b3 k0 n5 p管制区域, 7 `. F& k8 P1 f* q高于地面的指定极限以上的受管制的空域。 6 K& X1 o7 B# a7 \ X5 O制范围,/ `: K9 ? u0 h6 s/ m- E 由地面到指定的高度以内的受管制的空域。 ) d# Z: u3 m7 @6 m; I' a, b一个范围明确的空域。在该空域内,仪表飞行规则飞行0 X4 ^* t' Y% O; a4 i P+ o( l1 ]6 e 和目视飞行规则飞行有空中交通管制服务。 : W# E: G- i' T- C0 `) s. Y' k* d9 q* @' T/ l: F+ B# C) W" @受管制空域,$ j/ @4 N( _- v1 J 英汉对照民用航空词典B OEING/ _) T: P) _) N y TECHNICAL DICTIONARY 37 - i# V, z2 n, _CONVERSION, To change into another form. # s5 z1 N1 `( ]. a0 a) b3 V, yCOORDINATES, The intersection of lines of reference, $ z( Y) I* x8 E9 O. Esually expressed in degrees/minutes/tenths of minutes 2 I0 h* B$ y8 A6 P! [) y# Rf latitude and longitude, used to determine position or & V. r# m% @" V" Y; X& u9 L; ]. X+ s/ XCO$ l C$ R( |: L, H destruction of th ' R# N6 o+ t, ]: qchemical conta 1 a, \8 t5 L( B% LCOWL, A remo7 K4 Z& _6 h ]6 O4 h% k for access to th3 w" k5 S- R% u2 J/ c1 A+ L! s Fa . r# l" Z* ^6 j9 NNose Cowl - Front section of the nacelle for air inlet , F& o6 X9 V1 x8 D; Rto the engine.% G. K9 f6 Y( y0 w8 Q Side Cowl - Cover around the sides of the engine. 0 ~5 n0 p8 Y3 q5 Q" NThrust Reverser Cowl - Cover around the core % I" P6 y8 y$ C, ?* |section. - a, v; a" j t# b, O' ]- [Translating Cowl -The moveable outer portion of the d- Q; L$ f8 V9 p( W4 M thrust reverser cowl which is& V2 L, z8 d. r4 ~ operated during reverse thrust.8 I5 b7 d3 g6 T 标, 7 h& c& U6 G( L" b( D基准线的相交点。一般以经纬度的度/分/十分之一分6 X6 m7 p6 |' m2 m, M6 d. l 读数来确定位置和方位。 / Y N$ ~/ v* N1 X( {, T6 l6 i i- b1 k腐蚀 7 V Z( B: @4 T1 Q* I动机外部可拆除的罩子。发动机上的构件必须要取下6 k4 y/ d% ^' r3 O9 U/ h, @, _6 p 流罩后,才能够到。 J3 q+ @7 h$ I$ i9 L: o( ] q) D1 I8 E4 D+ Y6 H% g& b机的短舱的前段。! F7 G7 C( r9 F) |& C, I 侧整流罩一发动机两侧的罩子。& Z: i# z( J% G 反推整流罩一发动机主体外的罩子。 2 L( `+ m8 \* U6 P. U# ]) A移动整流罩一反推整流罩外可移动的部份,在反推工 1 o$ o b% |! L- N$ ?+ Q a$ n$ s7 r作时使用。 5 V9 B$ J) \. Zu a9 J2 h( F3 w7 R o, C+ Y# U& w5 o$ ?7 y location. % V7 E9 p* L! h5 TRROSION, A chemical action which causes gradual 7 G& i, Y. Z9 ]1 n# qe surface of a metal by oxidation or& }8 s; ?6 {! z" W y mination. / g/ m+ I+ ~( \7 m& e% I% \7 E. Bvable cover around the engine sections 8 K$ f% i; ~0 t& x5 a! we components on the engine. & n/ l" f$ v6 u% _( l4 }: y, _n Cowl - Cover around the fan section. * @1 j* a! m) O0 {, E转换,& C+ M: f( I& ?: e. M/ w$ J 改换到另一个方式。 - J! ^2 G' Y q) e, @% i4 V, `* G& H) Q2 X8 K0 w$ `$ E) M* @: M" s' i5 g$ K. ^/ a3 `% J, U' i- Z( G" ~$ c氧化或化学污染造成金属表面逐渐破坏的化学反应。 ! K9 L1 _* K5 U6 M( P发动机整流罩,1 t: G6 m" O8 G% @' X1 K3 s% F6 ?/ F6 }5 H' e+ Z- N) c" y O 扇整流罩一风扇外围的罩子。; p0 S% W) Z: G9 l+ O* g 前整流罩一引导空气进人发动6 d5 `) `, J" I- ]% ?/ } 英汉对照民用航空词典B OEING ! F$ J. T9 ?, K. NTECHNICAL DICTIONARY 38 " ^. P1 @4 `* @$ rCPU, SEE - CENTRAL PROCESSING UNIT7 ~/ v! a0 Q; A9 }3 N CROSS TRACK, At 90 degrees from the desired track* ^0 ^! K5 Z0 y$ D2 O f the airplane. For example, cross track distance is the, x0 z( N; ?" R& t istance from the desired track measured 90 degrees$ P2 m# V$ ]' f3 S$ q& b# R) U om the desired track.6 K V9 t1 f \- W4 i9 z5 P ROSS-CHANNEL, Electrical wire(s) connected from6 _2 r' X: Q! s" i7 X9 {9 c ne system to another like system, for example, FCC. c4 {9 ~, k$ B- {9 M " to FCC "B".' R, c' }8 ~* ]* \ n adjacent engine or one on the other side. 7 s" y8 G+ `; }" A" Wl crossfeed 8 f; ~# |5 B6 N) w/ |" Z" eanifold for fuel flow from one side of the airplane to the " p3 D( D! Z! K% K/ `. ?! ither side.& p2 D; }- R" h* ~9 N; j re d" R3 b; d( u2 K$ ` RUISE ALTITUDE, An altitude or flight level; q7 b0 A" o% C" p/ {0 I' K- l" P. }9 `+ X6 S3 T$ o7 W o7 X7 U& S! Z, ~7 A/ b' L d5 z5 M- p! M/ E# J fr 5 l1 \" m( r/ z: R* R* V% vC # l% i j0 l4 ?3 u: d" R4 To5 T+ r3 b. q a9 h% {9 w* u "A& G$ g) u8 f5 M1 ]) r5 X CROSSFEED, An interconnection between fuel/ w" d3 P( m% c: S manifolds for fuel flow from one side of the airplane to0 a& c# [0 X$ s; W' G3 W# y a 4 @' ~& ]( G! }. n' JCROSSFEED VALVE, A valve in the fue, w) i& l8 c4 p! h5 }' ? m / c* n8 A7 G9 M' _7 ao % L& S/ O8 Z/ I5 ~& A( hCRT, SEE - CATHODE RAY TUBE $ ?8 I* a: j. c: _3 {" ?CRUISE, Phase of flight where altitude and speed a ) u- R8 t2 a# Jbasically constant.& P, _6 k. |- f9 c C ! x! f4 [8 l | amaintained during enroute level flight. 2 S- F& Y8 p- b9 b中央处理器8 P4 C3 e" w) c 见Central Processing Unit. 8 H4 S4 Z# @6 Y6 k6 ]8 |交叉航迹(XTK),- v& P4 G% j2 b 与飞机预计航迹成90°角的航迹。例如,交叉航迹距离( j) D! x: C2 C2 Y8 f! e+ g% r# p" H& ]$ x 是用与预计航迹成90°角量取的到预计航迹的距离。; S5 U4 C5 S/ r) j 通道跨接,' _# J) z( t$ E 电线由一个系统接到另一个类似系统。例如:由FCC' e. `3 B0 U! U1 D5 w) Y “A”6 S* w1 S; a" n( B# D5 y$ Q4 V H 接到FCC“B”. 1 g- G+ \; A. t% H+ ^5 T" `0 r3 n机身另一侧的发动机。. Q) @4 s1 e8 j2 S 于使燃油从飞机的一侧 4 e& T- W3 i/ x向另一侧。$ T3 |) h5 p+ q 见Cathode Ray Tube . K/ z! J' G F& R交输,; X- g, g: }( |( f) Q0 M 燃油支管之间的交连设备。可使燃油从飞机一侧流向邻9 b' l6 k) c# m3 |' c: \ 近的发动机或在9 t# a5 B+ Y& k0 \5 y( ~, \ 交输活门,' I4 M, [+ n& c: p% d! x 燃油交输支管内的一个活门。用 " N9 E% i* o8 c) Q( Z, P% O5 E% a阴极射线管,! C( |/ q9 Y) l ^& j3 ?7 g: a .% `( ]4 @; V: v# H 阶段。- W/ A' T% j; m! E7 g! K 航高度,- a7 Q% o2 G$ l( r 飞行期间,飞机所保持的高度或飞行高 . S7 a1 G- p6 [巡航,- M. Y6 T6 C2 b* ~% ]# G6 h: J4 t& i 飞机的高度和速度基本上没有什么变化的飞行( }2 M" _. T) U* }( k+ R" N; B9 r) m* ]1 K- ?* V! L在航线上水平 ' T5 L4 e- i) P+ \- H) _: `6 [度层。 ; \; j/ R. j: A$ J" u英汉对照民用航空词典B OEING4 c! R3 n+ w q& \; K7 X. h TECHNICAL DICTIONARY 39 3 c2 D; g* t. y3 N' z0 gCSD, SEE - CONSTANT SPEED DRIVE8 Q0 h7 ^ `3 m CURE, A chemical change which takes place in a resin 2 w/ i+ x1 G6 {" [- t2 V) pand fiber based component causing it to solidify. ' Q9 h$ r# g' C1 v, X0 N; zCYCLE, A complete series of events that take place 8 ?5 `' I- |+ r& f! E- N1 ~5 agularly normally in a continual sequence. 2 ]+ K% D( }* M1 T3 g+ }% V% YAMPER, A device for slowing down or limiting . l9 ]- M6 v9 u/ L. UDASHPOT A mechanical damper for slowing down2 N* q: O" I+ T ovement by restricting fluid flow. / p; a. H7 y: l1 b% F+ m0 BD 1 W' r* y7 ^& B9 T( X+ \ATA BASE, Stored information which is used as the' v, X& ^: U9 m' b: _0 n ba* V7 a% R6 q/ j! d DATA BUS, A conductor over which digital data is .+ N7 @6 h' r1 ^& ~ transmitted." }2 q/ f0 ]. C+ z7 b5 _ DECELERATION, To decrease in velocity. 5 D5 n8 X& h" Y, i7 H" b装置,) |4 Z' U" n6 p) C2 r7 C7 U7 {) O" K rive 8 G4 n! T, z6 h' f* {* U& `- r( qre % R l# J* y3 p' A9 jD ) X y Z; G* { \& \D 4 B, T' S) V1 e1 P. D9 f, hmovement. . I! a; t& s- a( n: y6 Xm" U& Y. j2 J) V1 P3 _ X5 i ATA, Another name for information. . \/ {6 | j2 d- n- \4 m8 E2 [+ gD5 h! v! a6 K' R: p. @$ E9 v& X& R sis for computation.5 X+ O( c. ]/ d9 v( [7 e6 B 恒速驱动: L E5 h" i$ k0 r+ t# q. m8 n# F 见Constant Speed D .2 E5 K) H) y, g0 s 期, 7 x; ~- n' i: y1 c不断重复发生的事件的一个完整系列。 " X5 c) }' M. ^2 O- [% j尼器, # t, v+ X2 d* Y0 @/ m% p慢的一种机构。 $ A: Y) }6 O) T+ E% T+ D4 C' f4 Y/ [: `用限制液体流动的方法以减慢物体运动的机械式阻/ b Q o! n8 ~- L+ e% ?% _3 ?$ e7 A9 t$ s. U4 {; c" C. B) f! e" n料的另一名称。 9 [- f9 o, ~& L+ ?据库, ! m1 G. z* ]5 L" _* f8 y+ {3 R数据总线, % @6 y3 o7 E/ P% e2 o一条或一对导线,用来传输数字信息的通道。- L4 \( h/ O" _( u$ S 减速,4 U9 Z6 ^7 X. R! u9 O5 E 速度随时间的递减量。 & H+ t9 z) E& [固化,; [9 `2 L9 J1 } 树脂和纤维部件内化学反应使之成为固体的变化过程。 0 X \9 q# I: X) Y, d! R# Q: q% e9 Z6 `; T5 W! L% B+ ?4 W6 Y1 f: b; {) A/ }( j% a0 v用来使运动减 : C, [3 E: `7 O/ A2 d- [2 ^" v6 e+ M冲器, 5 ]8 U( |! f* U# e; T器。$ j# L2 T/ p/ q1 G# x3 Y 据, 9 O9 z: Q7 e0 b5 P$ M# v3 f4 j& t! z) W$ d% W- i( J. V8 E* f储存起来以便在计算时使用的资料。 + ~- N% x0 w" U9 J- @8 @. @英汉对照民用航空词典B OEING 5 l2 U. E( R' M- ^5 F% [4 g, }8 ?& gTECHNICAL DICTIONARY 40/ u6 Y9 G+ l& d# }. n DECIBEL (db), A unit of gain derived by computing the( Z8 X0 { r! I6 w, Z' o4 |3 a tio of input power to output power.3 k& V, N/ W+ P) ?! x ECISION ALTITUDE/HEIGHT (DA/H), A specified) _0 n: w9 ~; W; R% {; a ltitude or height (A/H) in the precision approach at3 a1 H8 h+ j& [2 D: k hich a missed approach must be initiated if the . Y) b% F% u* f. Z5 a& IECISION HEIGHT (DH) 1, With respect to the : m: S# o6 O3 Q: d- Zproach or f9 z3 @3 \$ }7 p3 W5 I- jexecute a missed approach.; T3 R6 e+ H( O) u proach to trigger the decision of either/ T# E9 k& u/ a& [" k nding or go-around. , M5 V' Q9 E0 q% ^% _# YECOMPRESSION, The loss of internal aircraft air' l2 z5 a5 s: P- q ressure.' Z% [9 D5 U2 Y+ H- B! x/ }8 Z2 ^ E-ENERGIZE, To turn off or cause to not operate./ K! e6 G$ e" ]6 F7 ?/ ` rom the tanks ( G m5 f. c( E( R' u: [using airplane fuel pumps or external suction. * P* G) ?4 \+ c& {算的一个增量单位。分贝 - g0 o6 a+ l* t. e常表示两个声音信号或电力信号在功率或强度方面的( I) `8 {; G1 I' t 对差别的单位,相当于两个水平的比率的常用对数的十* a9 _, M5 a8 f' ~! ?8 a6 w& Z 断高度/高(DA/H),) O+ I, v0 Y0 V% W2 O 在继续进近必需的目视参考没有建立的情况下开始复 T7 Z; K: E ?1 F% p的精密进近中的一个指定高度或高(A/H)。+ [$ ]+ Q& d& O! L/ c* S& ] 断高(DH)1, / Z t+ _* G9 z# p+ k0 a: r操纵而论,指在使用仪表着陆系统或精密着陆雷- B5 c( D* ]( w) s5 q2 N 生继续着陆还是复飞决定的高。 # G* {4 k8 V% |8 m飞机失去内部空气压力。+ h! a( ?. k7 c. l5 f: H. E 开,1 l+ |% C/ h3 `- E 关断或使不工作。! o& ?0 y. K2 t2 S3 ~7 V& h1 h 机的油泵或外部的吸油装置将燃油从燃油箱排1 K* `1 N- ^- _* _ 出的方法。7 |8 ]$ `4 K) @. d ra5 O4 X8 Q/ ~) m0 R0 d D: }& e( s0 D9 S. r a1 C& s/ H! [9 X9 [$ L w! w6 I# I! j: D8 u2 m% Y5 F required visual reference to continue the approach has% Y! [; ]' H. P" u6 W) u/ C( _& t: G not been established. 2 E/ ]/ s4 f' c% yD # r( k' P0 G# o# f% Toperation of aircraft, means the height at which a / A- ^% J' K$ T0 Z1 {7 q4 Wdecision must be made, during an ILS or PAR2 k5 e( y6 p3 ?) c! w instrument approach, to either continue the ap/ O* e: h$ Y" t5 Y( ^4 ]; d7 A to ) r5 K' b) {, @* E7 qDECISION HEIGHT (DH) 2, An altitude used during a- t) T% x; V8 Y$ k8 W" p0 U4 f precision ap T8 i4 k" \0 P" M: `la , E2 x; x6 E+ V1 C) U" yD) A- y/ w1 l+ h) I p 3 ]/ {) Z' I) L- N- d c. @D 8 b! k0 `5 E' [! Q# d4 V4 ?" kDEFUEL, A method for removing fuel f: h/ H }- B+ Q, ]; Y1 o2 d 分贝,) w: @1 z6 ?$ R' H* d 以输人与输出功率的比率来推 8 t7 t2 C3 U3 l6 y9 C; R) v* p3 @- q. j0 l1 f# }" D: X4 C" ~6 {" p/ o/ |& l6 a) H7 x: j( p. y- |2 |- y& @, O2 c) w$ I8 N# d. ^+ q$ ~ c y6 m/ o- Q5 V; X9 `9 l0 z 就飞机 5 S5 T) }. R) ] n8 T5 f3 A8 F; v; u达引导进近时,必须要作出的是继续进近,还是中断进场7 z( `& j6 v5 u8 H1 O 复飞决定时的高。7 \6 h3 | m; ] 决断高(DH)2,' [% x. M) m& @4 F! t0 Q 精密进近时产: \1 G6 x8 r5 e: F, X. I 失压,9 f& V/ o f/ T7 x1 b0 r h2 A) s$ m& l2 ~8 n1 `6 j 排油, 7 B- p$ l- Y' W. Q用飞, \. \% r. d/ {( n$ V2 J 英汉对照民用航空词典B OEING' A& V1 W1 s$ C! o TECHNICAL DICTIONARY 412 o. R0 g) J; y) `" q( q DEFUELING VALVE, A valve in the fuel system for / d8 l6 T. X# C ]# gefueling the tanks and for transferring fuel between the # y/ `" h$ A$ ~E-ICING, Removing ice after it has formed on aircraft. 9 n6 k- v. E+ b# gChange or difference. 6 Z2 o4 v% T/ s2 Z# iEPARTURE CONTROL, A function of an approach% Q3 h- Z% a# X9 h" U ontrol facility providing air traffic control service for" b7 q1 D2 R. _% r4 | eparting IFR and, under certain conditions, VFR ' D6 {6 C% q' K" ZEMODULATION, The process of retrieving information d; y; U: [* X& ^' v) j3 scarrier voltage.7 z* ]* `6 r8 m. G5 n ation.! E( s, C2 W. Y+ j/ } lic% i) }* U5 h- Z$ v0 Q creasing hydraulic reservoir air pressure to : ]" f& ~3 @5 e+ I* _5 M2 imbient pressure. 1 b6 `6 _! O( U* e" o0 G. B2 F箱排油和在燃油箱之间 3 G+ N5 T& w v* m6 b* m送燃油。% J- ^# L0 k; { 冰, + q% U- v8 ~7 s% t4 [0 m! C5 T# Z3 I除去已凝结在飞机上的冰。* e% z+ J; p, ^. s8 d 删去或取消。 5 q% V t0 ^# J2 h; G; p. D量, ; D; L* c5 h% p; c" k2 S变化或差异。- w% J$ J- S5 f, E2 J% p2 z 场控制,# V ^) L2 d! s( V) L$ C 给用仪表飞行规则离场,和在某种情况下用目视飞行1 p* S9 x/ B# d; F 则离场的飞机提供空中交通管制服务的进近管制设施 ' o0 o" Q/ M! D- h4 Y0 g$ f2 |/ g& I" A# x1 b& T! l调, : W S, z" r2 C7 x6 t电压中获得调制电压的处理过程。 + X2 Q' }6 x6 X, T, t5 B5 a* t环境 ( t v" P0 m# n8 x6 e力相同的活门。9 ?) C- {* _; W" v+ V- G d- G0 D; O3 p- b tanks., T1 B" Z4 C( q8 A( ]! K* v D 3 b3 {- A/ ~# a* tDELETE, To remove or cancel. 3 t; @0 N$ h* q& }- t3 A9 QDELTA, 0 D! H: l* T- z# p( PD, o' `6 ?1 A8 R6 [6 z c1 m! a. l' Q1 Y6 F d9 E( m2 S* D0 c; N! U aircraft. 3 j: p7 m. R# s, n) QD |/ R. u% }& i5 L4 P(modulation) voltage from a modulated 0 {6 J( M7 k; iDEMODULATOR, A device or circuit which performs4 z( K! o+ K! z7 a$ Q8 J9 J" h the process of demodul ; S+ ?# h7 d: |7 Y: vDEPRESSURIZATION VALVE, A valve in the hydrau# ] h( E5 C/ A) D- k7 _, B system for de & q/ H+ h v! g* H: Q& W* b4 Ha- k3 D/ t% \" R4 A- r 排油活门,. L7 Z4 p9 ^1 K2 @ 燃油系统中的活门。用以为燃油 $ l. y* b+ p# j( u$ @" B( N6 E- u- j) }; }/ Z, M% d! a* ?# N6 U R2 q1 n* L( H 删除,' d9 l: P! k. A1 c2 m3 q- m2 q4 X7 W) F+ m2 L, F, j2 k6 a" ^8 n5 _4 |6 B! M4 b3 F! A4 U' O 的一种功能 " {) @* F& m6 g) K! d4 U# Y9 a. m6 Y/ T% S+ _从载波! r! b; k0 T- \4 Z' e5 Z 解调器,) U4 @. @: G) x 完成解调过程的装置或电路。 : M1 \3 ]; C8 i) H/ c减压阀, ~9 P: W2 B) z 在液压系统中,将液压油箱空气压力减至与周围/ k, Y6 b r* C; l+ B1 N) `/ A. Y# V 英汉对照民用航空词典B OEING, t! h9 P+ _8 |' M. F* @ TECHNICAL DICTIONARY 42" [1 G5 t6 u2 I; [ DESCENT, Phase of flight where altitude is decreasing.7 t% U# Z# V3 L$ d* A1 i1 r ETAILED FLIGHT PLANNING, The calculation of fuel 2 w3 L- a# O4 M5 n3 O1 A/ a bnd required for a trip by considering each phase of 8 V w# D8 _! [- ^, B9 P$ c; A* iight (climb, cruise, descent, reserves). 5 g9 h. F+ y* |$ r6 ^al or . X3 t* u1 g( J2 B: u# hETENT SOLENOID, An electrical solenoid used for : h- n9 T4 o# P( p$ bt. / S( U* u2 h0 ?4 T2 t$ F# `1 Lspecified course or# [9 n/ Q: U+ E rocedure.; L6 [" O. X# J' t/ u e.& M2 H6 J8 u; j 飞行计划,( b6 ]- t$ R/ ?3 Q 将航班中的每个阶段(如爬升,巡航,下降,备降)都3 r- ~& Y1 g, Z; u7 B$ }' C 人考虑,来计算该航班所需要的燃油量。0 A9 |5 L) B8 y) d; U$ k 用来感应情况之正常与否的电气装置。' q5 y1 _" ]. L2 I6 z0 V2 l! R 定电磁线圈,7 L" W# A c, d8 x6 U 出接通的电磁线圈。, V6 F1 c. N: @% l/ m( }0 K2 e 差, # v L# H6 W! N6 a与指定的航道或程序之差。 6 }3 i9 |& P2 v用气压或液压操作的活门机构中的柔性部件。 ( L/ f) R+ ^& r, }' I# r" zD ' l3 [, @9 I+ a {1 @1 v# Fa 2 @: [5 M, ^9 Efl# F6 W4 l+ o; f8 i2 `' v' c; p; y6 @ DETECTOR, An electrical device for sensing norm, t$ g* ?. _# A' r6 G abnormal conditions. 1 g3 U# Y) `! ~1 Q" TD 7 d+ `; Y7 }. X; h0 P3 j7 C0 t0 M Zcontrolling the engagement of the actuator outpu 2 _( z, \$ _" q- M3 b# W$ h5 B# mDEVIATION, To change from a 3 s/ I6 i$ P2 Np' |9 F' f8 D7 D6 t, U# X& I) F z DIAPHRAGM, A flexible part for operating a valve! A5 b" i$ s' b& c% C2 B# A mechanism by pressur - e. R& f; y2 T7 h5 A, C下降, 8 X" @* E" C3 S$ f0 ~& w* N Z飞机高度不断降低的飞行阶段。 4 L$ N; C! r- F4 p详细 ; y( d$ w5 ? ]4 l6 h2 K* j1 c' d( ^# z5 r 探测器, 9 } d- s" Q6 j! F5 w0 |: P$ a) ~0 `- E1 v' k" K w2 N- f T用于控制作动器输 ) n, `8 V- l! G4 j7 R$ Z2 B& n: b) m- W' D 隔膜,+ }6 w5 J+ k. I" L 英汉对照民用航空词典B OEING) H# G6 A& {9 r, l TECHNICAL DICTIONARY 43 5 m; V+ h" x6 }$ {6 J; u& K; { ~DIELECTRIC, A material which does not conduct # G1 [& t0 h5 X. b$ K; ]$ F4 h3 Telectricity and used between the plates of a capacitor , R5 B- }" T/ c0 o(condenser).8 m( G) y, Q3 D% |8 k6 ]2 G/ [ nother pressure in the same system, measured in 5 r1 H2 ]+ o$ k4 \! q; H. e* z. ?) ^ounds per square inch differential (psid).9 a9 ^: g3 Y6 G* @; G# V4 T IFFUSER, A part of an engine between the4 z5 M' [& q- c0 U% m1 Y3 ^ ompressor and combustion chamber for reducing the, W( U2 S( r: Z( B0 ] air pressure. 1 c! q# o7 b! C0 S1 righ 4 B3 c* @6 \) p' K$ R, M( j( fpulses.( m) ^+ t, r7 a) }& |5 c3 p ignal that is a close approximation of the original* B7 [$ l% W5 L6 J ignal. 7 J2 C c" b6 J/ ^IHEDRAL, The angle between the wing reference % Z. b* V6 E$ u1 G9 g8 \lane and water line. : z1 \" k0 @, o- `: Q8 Y! d的压力,以每平方英寸7 v$ J, }0 a' f0 V 少磅压差计算(psid)。 - u; [- ~: e0 g5 P5 j: {散器, - o# N# ^; z% i发动机内压气机和燃烧室间的一个部件,用来降低空- |" T/ m$ p# \, \) v, ?" |2 i 增高空气压力。$ N1 V& b2 \4 y7 N; Q% }3 V 换, 0 \8 s; Q2 l8 {8 l的连续可 + q4 s# L' _( E9 b0 c; V% Q(模拟)信号的处理过程。; N; P- L0 O7 d, N- u0 X! T4 n0 J 反角, + W( S3 H4 u: X) o( C机翼基准面与水线之间的夹角。8 b' l, ^+ V- O# |4 j5 { DIFFERENTIAL PRESSURE, Pressure relative to# p' n+ V8 B9 u1 x) }9 \) N- Z a 2 ~1 }* h1 O& w |) {- mp* n9 K: e$ l$ @0 G1 @) M D9 p d6 O/ Q, d) @6 i. q c1 J$ |: {3 I- `( N airflow speed and increasing the+ o5 Y7 K# \+ e2 q* f/ R! q DIGITAL, Digital refers to a signal whose amplitude " k" r# g: A+ A' j) F$ ^& mremains constant for a finite period of time. Digital0 a: f, H, |5 a; g$ z! W signals are commonly represented as a series of h' Q0 f6 }% H& C# Y& q, r: D and low$ n5 p+ l2 x( W6 ?( I, t; n3 ~; X k9 w DIGITAL-TO-ANALOG, The process of converting a ; r0 u5 j1 g; P7 b. K/ Odigital signal (binary) to a continuously variable (analog)7 B- ] u4 k$ b# r& ~6 V s( l& v: j- z6 x5 K) E( o& N- m" ] s / _7 [$ L# ?, A& f/ Q8 e* h, @, K; bD" Q& a+ f3 D `; e$ B p ) F( t0 N* `7 c' q& {电介质, 2 c( W5 [8 P: ]' H" \ p一种用于电容器板之间的不导电的材料。 - a# e8 a$ I8 L& e压差,- n" I; }; `; o 相对于同一系统内另一个压力 $ a5 a0 g; z% h$ x; z' S8 h5 J. E: Y& A) Q$ Y- ^: B' n9 Y2 g7 H2 y8 I气流速并 , t, F" ]* |$ L/ {9 c1 E" ~- y1 N% V数字式,& o- S; s! J. s3 J+ Z B 指一种信号。该信号在一定的时间内,振幅保持不变。 6 V" Z5 c& u! N( J z通常由一系列的高低脉冲表示。 % O, k+ F" O' V数一模转3 P3 c% W* \2 q) d 将数字信号(二进制)转换成与原信号相似) h! d0 M' Q8 p- M. {' t8 [# a1 t& r' j2 u3 r* E W6 k0 n5 y) A3 [4 P: G2 d3 I7 ~英汉对照民用航空词典B OEING : u1 G0 e: P8 r Z. ~/ {& ]5 v' b6 uTECHNICAL DICTIONARY 44 & n7 H0 h' q+ S, `DILUTER DEMAND REGULATOR, A component in the 6 X" q% R. {# e4 e3 a+ a3 Pcrew oxygen system which mixes air and oxygen and; o8 w) A. K0 _% [ upplies constant oxygen pressure even if there are: f2 h# I# B- ]( Q: D% V' i hanges in ambient cockpit pressure., Q$ _' E, y7 l0 \ IM, A word value of light. For light control devices - dim5 `7 ?. n( T) H' e7 F9 I1 i8 r the opposite of bright. 7 J! A, Z" u4 y7 DIODE, A device which allows electronic current to flow- q+ j' E" Q8 X5 B! z. c only one direction 2 Q7 h; ^: q0 F9 P# J( {uid in a reservoir. 9 r4 p7 v2 A+ iDIRECT, Straight line flight between two navigational7 G. K% y! k% J; k. j; L aids, fixes, points or any combination thereof. When " l8 E" ~$ k8 J( E: j6 Aused by pilots in describing off-airway routes, points7 C4 ?6 i, C- X2 ]5 o8 x6 Z% L9 o1 C defining direct route segments become compulsory - f' j8 I- L# f9 B& Mreporting points unless the aircraft is under radar: f/ z' o: J( U4 x+ o. d* n control.. B, A# ?0 \( u; g8 W0 `; @, I0 u& K 节器, 2 }' C: k6 k4 x4 p: t将空气和氧气混合, 9 i2 m9 @. F* [ j使驾驶舱环境压力改变,它也能提供恒定的氧气压力。1 h T5 L$ n L A/ U$ Y/ e. j2 @/ O! \2 y$ i- {* C3 b一个形容光线亮度的词。对于灯光控制装置,暗的反5 Z; L, M3 D7 h! t- A 词是亮。, B4 Q% C# _; O( F( C3 e 极管, - o" E% X& [. W1 u5 v只允许电流向一个方向流动的电子装置。 ! ?) }4 P0 K! v器内液体的量。" a8 J! Y' G( t 直飞, 3 j; L2 r* @8 d4 F* j两个导航台,定位点,导航点,或任何的组合之间的直- n4 C& L2 z" ?0 O/ X" j 线飞行。在被飞行员用于描述偏置航路时,除了在雷达控8 C7 j- D) |- q' w& u, m$ Q- C2 y- b 制的情况下,确定直线航段的导航点成为必报点。1 P3 }4 l% L# `( M' R s 7 f& c3 ^ m7 ^6 I' V: O) N: \" u& ec 3 N6 u% |+ ]5 P0 [9 ~% `0 a% {* HD8 i P" w) _3 B) U is / J$ N# O+ S' v1 B0 RD 3 M6 b- n6 F# ]! C8 Y, W9 Yin + `! ~4 j6 d4 j+ O' p; M QDIPSTICK, A calibrated rod or stick for measuring a 6 d, v# i. X8 Yquantity of fl/ W3 V* i! i/ y( }7 b 稀释氧调 " G! ?4 `3 u) X9 X( \, \' t驾驶舱氧气系统中的一个部件,它 - p* ~+ ^/ n2 ^# @. c7 I1 `% t. m' t- O9 t; `: ^! Y8 z+ g" M% ^. s$ `; H& [7 B! v0 @+ P1 }) x7 a1 p" w3 q: `+ u+ q2 A. ?量尺,( a" J4 K+ c5 P+ i 校准过的棒或尺,用于测定蓄液 7 p/ R6 z6 w" j5 @英汉对照民用航空词典B OEING4 X' a, Z$ r+ R( _* z TECHNICAL DICTIONARY 45

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