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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 ! D6 e0 K( _( T9 o/ s `$ n: h民用航空词典- K7 |. Y5 Q0 J9 {! C9 @ 波音商用飞机集团7 D h) K# N) v1 q) r2 h( y BOEING COMMERCIAL AIRPLANE GROUP 7 V! W3 L; @. {9 L英汉对照民用航空词典B OEING0 K5 g+ S1 S' a& V+ K TECHNICAL DICTIONARY 11 h" {: b$ X' T `0 K) L A R7 w |7 ~* fABEAM (ABM), Beside: An aircraft is abeam a station$ b3 j" ~7 X. _, c% p when that station is 90° to the right or left of the track of& P* o" E! ^- n$ ` the aircraft.' g. x# G* M5 f3 _2 \/ H ABSOLUTE ALTITUDE, The actual distance the aircraft 0 m( w i$ c4 ais above the ground.9 }" n8 u( }. O8 _- p0 D ABSOLUTE PRESSURE, Pressure of a liquid or gas) k$ l1 Y% b+ t+ K measured relative to a vacuum. * Q0 O8 ]0 Q, b* F* f/ WACARS, SEE - AIRCRAFT (OR ARINC) REPORTING 5 w8 H$ T6 G3 t- Q, ?* }% dADDRESSING AND COMMUNICATION SYSTEM 5 q. \, L6 K5 E0 HACCELERATION, The rate of change in velocity with ! \1 C7 ?4 p- u; ^& C2 p9 ^respect to time.# b4 g! x& o+ }& D+ f ACCESSORY GEARBOX, A part of the engine, ( _- j3 Y; u& A3 k, F$ tmechanically driven by a compressor or an angle" W) M# j* R/ Z8 z gearbox, for driving components necessary for engine. W# E0 f! A+ {* W 正切, - d( A" \" g& g3 ?% `+ f1 oand airplane operations. , W# L& a& x1 g! B当电台在飞机左侧或右侧方与航迹成90 度时,飞机正% R- ]) n* { y/ E2 H, F. e 切电台。* u5 }8 R) S) K3 `' d- U 绝对高度,' x* s2 T" z& m! K& s* [! o 飞机离地面的实际距离。 5 s. ~2 x4 P5 t绝对压力,( G; L0 y7 D. u) z& ? 相对于真空(无压力)测得的液体或气体的压力。5 F9 @/ `% ]7 {2 S6 M. B 飞机通信寻址和报告系统, ( O6 h$ A1 U. w. \9 h; w' w见Aircraft(or ARINC)Reporting Addressing and3 u4 H3 G2 P* i" x Communication System. 3 p/ H1 H7 Y6 j4 ~( M) B4 t d/ _加速度, 7 r" G! f2 V# ]+ M, M6 S& d随时间变化的速度改变率。 $ p/ C& y: F5 M" m" W2 ^! {附件齿轮箱,( @6 T2 P% p' W: [ 发动机的一部份,由压气机或伞齿轮箱带动,用来驱动 ' X$ [. G* t3 `4 H2 t' C# N- K3 |一些使发动机和飞机工作的部件 : J# q8 R, Q/ p& j3 I% D" W英汉对照民用航空词典B OEING 8 b" j5 ^( {: L/ yTECHNICAL DICTIONARY 2! B- h0 c" }6 `/ e8 h- Q2 v. ] ACCUMULATOR (NO. 1), A container with hydraulic$ E. @. a, `$ z- h! v. f ts when normal hydraulic supply is not 9 O2 l- r1 \' B9 v; X' Lvailable.6 u$ n. w9 S, y# \0 ~ CCUMULATOR (NO. 2), In a computer, a special2 k x' Z& q2 r2 U8 V torage register associated with the arithmetic logic unit, : V/ U0 Y" W2 H4 E) I8 \) H; H4 k( Aolding the results of a computation or data1 t1 l( r$ {/ M3 B. q! s" F ACTUATOR, A mechanical device operated electrically,9 c& S) d# d8 ^; g6 j3 ?, a hydraulically, pneumatically or mechanically for / ^, ?- U/ p" Stransmitting motion between components. 6 w* P1 B* o, _1 s) fADC, SEE - AIR DATA COMPUTER ) C. K% p. A p2 {$ j% QADF, SEE - AUTOMATIC DIRECTION FINDER0 X9 W+ {; B3 k ADI, Attitude Direction Indicator, An electronic display of# P5 I0 l- f$ Z airplane attitude information in pitch and roll.! @& P& t9 f, ^# U 蓄压器(NO.1), ) F" S0 O& ?. |2 O3 G: U. P含有靠干燥空气或氮气增压的液压油的容器。当没有正0 @: g0 C% Y$ i+ I5 t% T 常的液压源可用时,该容器可用以驱动部件。 ' F4 |1 G1 I9 {" ^3 ?2 q存储器(NO.2), : B* a* j7 A v9 f) ]% Q计算机中,一种与算术逻辑组件有关系的特别存储寄存 8 Q1 ^0 ?9 [+ |2 Z; @- G器,用来存放运算结果或数据传输。 ) V0 L3 i8 t6 O) j2 A9 v% {飞机状态监控系统, ' P( t% q* V6 V见Aircraft Condition Monitoring System , g! l% Y$ C( i) W: {. e: i9 Pfluid pressurized by dry air or nitrogen for operation of % a4 w, W# } k0 Mcomponen5 i% Z* e% N& m. \& Y a( J3 x3 J% H+ e* O) V, Z A/ g2 I$ T$ P3 r s ' ~5 M2 t6 R( Dused for h, R" m/ P0 ^% I4 B; Z- T. o2 Z transfer., {/ a( w4 u, S( R4 O+ N ACMS, SEE - AIRCRAFT CONDITION MONITORING6 M6 M" \+ i9 v b4 a6 S4 e9 v SYSTEM . 6 ^* @. H- i7 t. a: m作动筒,3 Z3 A8 o! Z' l9 _ 由电,液压,气源或机械驱动的机械装置,用于传送部 1 S- {( Y. ~+ O6 d件之间的运动。# h. t+ o' k* e0 U- K4 ` 大气数据计算机,1 z, m S! [6 c z8 i 见Air Data Computer./ H7 |* M1 C$ z/ A% F1 w _2 {; b 自动定向仪,( g3 T3 Z; U F8 I5 W 见Automatic Direction Finder. 9 g/ K0 F" d+ K3 F姿态指引仪,. l" y! d" [+ r, ]' d/ E1 s% C 用来显示飞机的俯仰姿态和坡度的电子显示。 $ v- v; s" X5 c- z) A. S英汉对照民用航空词典B OEING & s$ Q/ Z5 f2 k/ F' J b& LTECHNICAL DICTIONARY 3! V+ j9 G/ X" Q4 V ~6 j AERONAUTICAL RADIO INCORPORATED, ARINC is 5 ~- M3 q9 t8 h6 z,% d2 V6 E# x/ n9 v- s0 `) ] nufacturers, and foreign flag airlines. ARINC 1 }+ U# ~+ Y! u7 u4 q+ o! wevelops and publishes standards for electronic & H n9 ]9 W" \- t* F8 S$ Zquipment and systems. ' s% Q0 e, Q" y% O- e7 h/ l3 uGILITY TUNING, The capability of the DME to 1 e3 ^- T' }& v& z9 K) }+ f: Vlternately tune between two different DME stations in % U7 [9 o% Q. k( t: P$ c: }rder to get two distance readings from one5 n( L% h* b* e0 B$ C terrogator.# ]4 t+ Q' {0 G+ [4 n( r* e" t6 O/ u ge. G* x ^0 Z& p N+ L8 u ILERON FORCE LIMITER, An electro-mechanical 9 a2 u8 b! g' K- P. z. @: ^' uIR CLEANER, A component in the pneumatic system ; d. F. I( v% Hupply to the air( s. o+ {" W J% _1 G; g onditioning system.3 X1 ^- f* B# }2 O/ N! I 订并出版 5 o4 Z3 A" |# B( N( g! O/ l子设备和系统的规范。 & p0 `; @; X; F7 h: z快速调谐, ! V) j( a0 H1 v机载DME通过交替调谐两部地面DME电台以测得来自 * F) M% Y9 R1 s1 G9 K: R6 k同一台询问机的两个距离数据的能力。1 P1 g- {* n. a 翼操纵力限制器, 5 k! `4 q: {! u9 @; W装置。在自动驾驶工作期间,用来限制驾驶盘! R; R$ R) i" K, w' g& O) @ 气清洁器,$ h0 N h! B5 @3 d3 I# q. r 部件。用于去除供空调系统使用的发4 w% i' \" G* Q$ W. s3 E- r5 P: \ a corporation whose principal stockholders are United/ h: C& |' s, Q& q6 s5 W* \ States scheduled airlines, air transport companies ) N9 f k* R+ |8 P) @$ f& Eaircraft ma( N, P+ Z3 g5 m7 N, s- @3 c8 f' g d- T' u% o. a0 H K6 O e , R/ K8 R, X5 J9 Z ]A 3 ~4 [; R6 f6 a. j5 ^' J3 s7 t: wa6 \3 y# [ a9 b: W# h* w2 a o , m8 w, {3 ^* r; U1 w7 P5 Cin 5 e w9 @1 Z7 r p# @1 }6 |* eAILERON, A hinged moveable part on the trailing ed 1 N5 @6 K. M1 i' E1 H& Z2 Jof each wing for airplane roll (wing up and wing down)% V. O# {& |: I+ ~: @: f6 d control., G8 y7 G4 {% x A, R, D. H* i$ n, J! z device for limiting the control wheel movement by the. _& |1 g0 H$ G% I; f6 A autopilot during autopilot operation. & E" B+ A+ L- N0 V% NA ) i- m6 r4 W+ z$ `for removing dirt from the engine air s $ n2 a3 l0 g7 r9 X. Y/ Pc2 k! S, d7 j+ A! q ]0 _ 航空无线电公司, 4 |1 t$ J% l1 D主要股东为美国定期的航空公司、航空运输公司、飞机' z& Y ]4 k8 M( W! P$ K4 U 制造厂和外国领队航空公司的组织。其目的是制 - x& o3 e/ A4 y5 ?8 K8 H w0 \- K* E" f D& M; H$ i# |4 k/ k副翼,3 Q' ~! u( l5 f! f/ D 铰连在每个机翼后缘的可动部件,用于控制飞机的滚转 8 _- G. X) }" z( K2 b2 n2 {2 x( l6 Y3 J+ \(机翼向上和向下)。/ s+ s1 Z s3 P8 r$ \9 M1 v; j( _) p( r3 a" F; i一种机电 7 k9 A# T1 `' T+ G8 }: t的动作量。 - U) H7 } R. t$ g4 Q* v% V) i3 X% _5 f/ K0 r% e2 [" j I 气源系统里的一个 4 m& C5 o/ F" Q; r5 L8 F+ z. L( j动机引气中的灰尘。! @. k7 Q4 ]1 E3 F+ ? 英汉对照民用航空词典B OEING8 I" z# _1 W* e, d1 K8 h+ ?. G+ T TECHNICAL DICTIONARY 4/ m' R9 C) |8 ], b% F* Y* { AIRPORT ELEVATION/FIELD ELEVATION, The6 y' A8 d/ i" ?: y4 {( r: Q highest point of an airport's usable runways measured/ g/ I( W: T0 q; a, ]3 M in feet from mean sea level. In a few countries, the9 V- `3 i, N6 c1 e1 {! \, j- z airport elevation is determined at the airport reference ) K" c/ ~& [5 P: Xpoint. + z9 d. k, \8 o: ]2 BAIR ROUTE TRAFFIC CONTROL CENTER (ARTCC),5 x" u9 \4 R* w* F, E8 H ervice & E6 G) t. S W" R5 nase of' I% C. e9 p6 S* D& X; m us flow of air traffic.: J( t6 R! z5 E: p IR CYCLE MACHINE, A compressor and turbine on a# ?; k# w* z$ n0 m5 e ommon shaft for cooling the air in an air conditioning$ b* P" u+ b1 E1 Z2 I, J ystem. The air is cooled by expansion from high to low R; L8 D& v* M ressure across the turbine. The compressor is driven7 n2 b0 W7 C0 M1 k* e( t y the turbine.6 f! a% F- k. s. n% z 中航路交通管制中心(ARTCC), $ a- G9 N w: k0 g) J域范围内使用仪表飞行规则飞行的飞机提 6 C7 k# b! |1 E1 V$ b7 _管制(ATC),! S' |( H0 F2 k 涡轮冷却器,6 T. r* L( N3 m: d+ s 是装在同一的压气机和涡轮,用于冷却空调系+ l6 H7 d8 Z6 d" ?- p3 D 统中的空气。气经压气机压缩后,由热交换器移去热量,0 m) N) b* ?0 x3 N l) s 然后经过涡轮令涡轮带动压气机。通过涡轮之空气,温 : n- ?% P, ?0 Z. A( E/ C度下降。, U+ j8 O0 a. E( `' ?) O, X A facility established to provide air traffic control s + }4 e1 K7 i) ]5 s" Tto aircraft operating on IFR flight plans within controlled. t8 T+ A4 J4 M. t7 h airspace and principally during the enroute ph + s/ a6 ~, ~# R7 e; d/ oflight. + q; w8 U+ ~1 R" [4 X2 lAIR TRAFFIC CONTROL (ATC), A service operated by " U: B0 K8 z( J7 y9 T; ^appropriate authority to promote the safe, orderly and6 I/ E7 W9 j6 @" c. @; P. b" C expeditio) [5 S& P5 D, _8 i6 x# @! _ A . w% I# U1 I E( K1 V" u0 n1 Mc1 R& y. ~, w) K1 T s0 O+ X0 J; c) B2 S( V$ f% f p - H$ [/ K2 O0 ^0 O! n2 Q1 @b % A8 v4 j) D- _4 L3 @: T. M4 h2 c机场标高,8 u$ g# S7 [: h X0 D/ Q 指海平面与机场可用跑道最高点之间的距离,单位是英0 c/ _# d% g% z 尺。有几个国家的机场标高是由机场基准点而决定的。& [( _8 X3 Y- a q, n. U! y$ o4 Q6 `2 L 给在控制空 2 q" i$ v, T7 _* w8 C1 @供空中交通管制服务的站台。4 Q4 c5 D) f0 B& p8 W+ y0 j. F 空中交通 6 E4 A& |) y7 r* i由有关当局管理,旨在促进安全,秩序,和效率的空中2 d7 ^+ t: X1 k. J# k! K 交通服务。 : h2 U) D5 V/ I& e0 _根转轴上 4 E5 i% X2 t7 v- `, p! B8 |; q+ c" \: g; u1 C3 o/ k* M, @ p4 m) d, i# _) w M6 P英汉对照民用航空词典B OEING 1 d9 V* q0 W/ H' j jTECHNICAL 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 # Q$ E. M/ r) R& F" K5 Wdata information, such as altitude and airspeed, based " e' F* k4 B9 x' C6 ion pressure and temperature measurements. + Z: f" g; l8 s/ M" R; V; U3 X$ ees air" L. O7 }2 E* n% v/ t3 z; B$ P IR TRAFFIC CONTROL, A system comprised of4 b; |1 ~ i: B. p) }) f round and airborne components used to identify, track3 P1 H* j0 E/ x9 n$ E8 ^2 c OUND SENSOR, An electrical device operated, E# b% a6 S! D3 {7 j8 o; l y the landing gear, which transmits on ground/in air) X6 C! n1 ?7 A6 ?# B; K; I formation for system operation in flight or on the , g; x+ d+ o( Q: j" P7 {7 Cround.9 q# T, N: f: ]/ J8 v. y IRBORNE VIBRATION MONITOR, The AVM takes5 W: u6 @: k0 {6 q& Z e signal from the engine mounted accelerometer and , W ^: l2 u* D0 ?alculates the vibration on that engine.. n) _) M; K2 i( Y, H corridor equipped with radio navigation/ t% C6 s& g. J$ Y1 c7 Z3 c" W8 k aids.2 o4 z) T1 l8 A1 F- l# e) a- ~ AIRCRAFT (or ARINC) COMMUNICATIONS: ~2 I1 c, b' i# `9 w& e ADDRESSING AND REPORTING SYSTEM, An1 l5 H& y& G, q) U; P addressable digital data link system which permits the 6 k# n+ C( z) v' y% D& X% Aexchange of data and messages between an aircraft % h Q" Y" Y' vand a ground-based operations center over a radio 8 E! k; j5 h O+ W: ^network. ( Q, B# z/ A4 z+ P* s# s0 H+ gAIRCRAFT CONDITION MONITORING SYSTEM, A, c( E, N8 m! j( q# B. T& q) l system of sensors and recorders to monitor various1 Y. s, \6 {* O) z) o/ u T2 M airplane systems' performance and status.9 X l: }0 z$ G) w$ o 机,: Z! @. h+ e' x& U( d+ c 中交通管制,0 |- h' F7 s# |. B Y% H; @! P 一个由地面设备和机载设备组成的系统。用来对飞机进5 C: { \' s8 c+ u7 B) q& d 地传感器,. y( C5 n" c2 z, Z4 ?2 y 一个由起落架操作的电气装置。用于给空中或地面的飞8 d9 ^/ g' n1 o3 M' l( J7 d/ } 系统运作传输地面/空中信息。(有些系统只能在地面 5 N+ z% M& {+ W& V+ G9 ]; L8 r用) 3 d) R* k8 z. E; @. T载振动监测器(AVM), 7 d U4 R( c/ p$ [AVM从装在发动机上的加速器取得信号后计算出该发5 |& b) b, y& l; J1 ` D* ] 机上的振动。 . q) r. Q& R- T7 R式建立的控制区域,内有无线电导航设备。 7 u0 Q8 n1 b9 [: f8 @飞机通讯寻址和报告系统,. o0 S* a1 A' ~3 N- i 有种可寻址的数据通讯系统。利用该系统可使飞机与地1 T. a2 R) }, U/ g 面操作中心通过无线电网络进行数据和信息的交换。 ( |% ?9 _- b/ s. J: j+ F" B# O! {飞机状态监控系统, 1 N1 J/ S' }# a, j一个利用传感器和记录仪对各种飞机系统的性能以及$ Q* a9 T) q; D2 x 状态进行监控的系统。6 `& [! q5 m/ [# _" w A / D' {* m; {, U5 c9 Ng ( x% S$ c7 v8 D& Cand locate aircraft. }" w" v8 x# l" _) U AIR/GR* _+ M# Q3 J7 b$ y; u3 w; S b* O, [: Q; @0 M4 d+ L8 c in2 W! K4 ]2 u. D. t! _ g + ^1 D, | V2 g- F' }: AA e8 x- T8 j- ?/ D! ^: H- X' b' F! M th ! V7 q) r2 i Q. [, \; Nc" {7 k- S, \5 `% `/ ~% s AIR WAY, A control area or portion thereof established) N; u* A9 x5 Y! F/ ^/ X in the form of a ' [) M! }# z/ g# D6 P大气数据计算 " z) R6 v9 o( e# _$ L7 Y根据量取压力和温度而产生大气数据资料(高度、空速 ( {4 K P2 \$ c. |4 f& q等)的计算机。8 P% i5 S% y$ A' ?" M) H) P( ], E! v$ N1 z9 } 行识别,跟踪和定位。9 K4 `& @: O4 E7 T: ^0 k6 Q# ?- R( b. [" _' i& o. m* v! @4 O4 B( m" o1 n: p- f使 ( |; i5 T/ L& p( N: |+ R9 @3 ~+ c [, Y; I3 _3 L k6 b, G& }3 r, z! M; [航线,7 j5 l5 ~8 A" {8 }* q! a% ` 以走廊形 9 q/ ^3 V4 P' c* y4 {英汉对照民用航空词典B OEING ! ~% V! F9 ^# z' T# S4 w5 bTECHNICAL DICTIONARY 6 % i- R' r* X7 l. F/ uAIRFOIL, A surface designed to obtain a useful reaction, 5 T4 h b6 o$ r* k0 w9 Q- Tsuch as lift, from the air through which it moves. Wings,/ l& j( Q. c H) z* O stabilizers and control surfaces are airfoils.6 G! S# q$ B: s4 H4 L AIRSPEED (IDS, TDS), The speed of the airplane $ w8 }" Z( W9 F# |0 i% ?rough the air. % W3 N0 l* y5 _2 nD INDEX, An adjustable pointer on the " I7 Y; D% O; j2 Qirspeed indicator. - N4 s& Z* s% k# l( p4 A1 g& _and legal ability - X: e. P: Z% \% ^3 [* R# m6 ?fly.4 P8 R6 G. O; T) ^: u9 p9 P m, for example, the procedure for finding the ; u5 u1 O4 p. J W: N( H' G) c* rquare root of a number.9 q" I2 ], m! H* H y7 W* n6 ?' L. ~ n" b% y re, wind, ) s; q; O2 [& A& D- D0 U! y7 R/ aand aircraft flap setting.7 q! Y* c1 [% A$ n/ Z" c& \ 是翼面。 : o! E4 n" V4 Z$ |$ P' r# m速,- D2 q/ H7 J! ]0 n* ]% O( | 飞机在空气中运动的速度。 ) _' b+ Z0 g6 D) r- d7 ~( O0 [" F3 l) `* }" h 在空速表上可以调整的指针。4 q- Y& y) d" O0 W: Q! X( _" ? 机械飞行能力、和合法性的飞机状态。 * q. Z9 I# Q1 i2 r% G一步一步的解题方法。例如,计算一个数的平方根的步 5 {; t s$ N7 l# O8 u4 B3 V6 G. R$ N" ]4 g9 W- Z8 j, T5 [7 o! L. ^( r" k 资料的法定文件。! G, h) }! c+ i3 g( i 翼位置成函数关系。 0 x/ ?5 S, ~% A1 ^* \th ' t; d0 A1 [5 q- rAIRSPEE % k( y+ }, o5 e+ J2 \a5 M# [1 g, l; X; @' N @ AIRWORTHINESS, The condition of the aircraft with- O7 z0 o* T' ]. _ respect to its aerodynamic, mechanical, 8 P ]: g, H2 A9 [& d9 A, jto x+ o3 L1 V! k1 a. o/ s( [ ALGORITHM, A step-by-step procedure for solving a6 }+ {% K$ O/ u q proble* u4 r0 x7 @" w s . c- C P# R$ b, a9 Z- kAIRPLANE FLIGHT MANUAL (AFM), The legal 0 E/ z$ L8 A! U" ~/ J. F$ Wdocument containing performance and operating limits,( p% _* t3 ~: A2 u a1 d0 b g operating procedures, and takeoff and landing' j- G) f$ D6 p7 u; N$ u D performance.6 T* |4 W+ C8 |6 _+ p$ a9 x AIRPORT ANALYSIS, A comprehensive set of takeoff! B3 k$ C$ S& @ r. _' ~ {: \ weight limitations for a given airport runway, generall' p9 C. Q# L! O# b' E: N) ^ presented as a function of airport temperatu 5 o4 _& C# b5 k; n: X1 E) G翼面, ( w: i0 H( r. I1 Z用以从气流中获得反作用力(如升力)的表面。机翼,6 \7 K* y4 f& | 安定面和操纵面都 , f8 @( C1 D7 s; Y2 Y) ?; [9 z- w4 N0 v: Y3 i+ ~$ t% _空速指标 ; ?$ k2 }: t' M适航性,% r( ]1 W5 ^8 ^# E- H( W+ k2 w 有关气动能力、" |3 Y3 E* Y+ P1 K6 @ 演算法, , M- _4 e& d) R5 f' N7 r) m' z Q$ i) T! E m; A( p2 h# e飞机飞行手册(AFM), 4 c" G, K9 H0 L4 F, L, C包合性能极限,操作极限,操作程序,起飞和着陆性 / v2 W# X0 s4 J% {( T& a# e" L& n- b3 ]) c- z3 F( k 机场分析,* T/ _7 [, j6 W' T/ m1 R 一套针对给定的机场跑道的详细重量限制资料。通常与 4 K* a/ q$ k) T4 U* D: {机场温度、风、和飞机襟 # s8 x8 w# d; ]英汉对照民用航空词典B OEING & X! x [- }; Q0 z- T6 Z0 \TECHNICAL DICTIONARY 7 , X' @6 r) ]2 ?1 P3 WAIRSPEED BUGS, Adjustable pointers on the airspeed9 C4 ~3 {$ e! {' {6 O indicator.+ q8 P, g) U( b5 q/ f ALLOY, A mixture of a basic metal and small amounts, v. {6 N7 h# T2 x f other metals to change the properties of the basic( p- \- o9 N! e' [( C+ b# X etal. 7 Q$ N& T) l3 [$ W- ~4 q& o) p+ \Minimum airplane speed. 8 ~0 c( i7 K6 U2 M% d# ue of' G4 ?2 v O( n2 F itting airplane angle relative to 8 l3 v) j$ ?3 ?3 x5 K- pirstream for the stall warning system. 9 P) A# E( {! O4 @6 B" W, d! danother.) |. Q( q* E) b6 {3 [; ~ LTERNATE , An additional airport selected during : k, m9 n E7 ^6 P/ A% S- t( w7 r6 x合金,- |+ D2 X: l4 h1 q2 j3 [3 h 在金属中加人少量其他金属,而改变其性质的一种金属1 [/ `1 y8 S+ m X# a 合物。* G" V8 w0 L7 {$ T I; K" F 飞机的最小速度。 ; K0 L6 P, Z! n2 Z. P速警告系统传输飞机对2 d( [# N# Y/ ^0 H/ G* o8 f 流的相对角度。% \% J- T" y) @+ t- c! q 由一个状况改换到另一个。$ F0 g4 v- J4 u- Q0 e1 G/ W& @ 降场, 0 d) L* p, U; ~1 [; Y+ c r划时,除了目标机场之外,所选的另一个机 % d) h+ L1 ^% x) `8 |: `o ! w, W7 Q+ z+ [, C4 n& J' mm% A% B) b- Y' q9 g& M2 i4 [ ALPHA SPEED,' a: v% I2 Q( c3 W# ^; z( c7 u ALPHA VANE, A small moveable airfoil on the sid ( O; m! o8 N9 }0 x3 tthe fuselage transm 9 v3 H9 n; T& L; ~a 8 `) Q8 f% c. o5 _5 [" K ?ALTERNATE, To change from one condition to) c% N8 z4 M6 e8 R A ) C) { p3 @+ [8 F# M5 e* q6 H9 tflight planning, usually near the destination airport, to be 0 t3 u' o5 |: L# l D" i4 ~" Mused when it is desirable to divert from the original ' o. Z- E7 x/ T4 M: Odestination airport. 2 [) n) J* |0 v! J! H5 g' P/ o' T空速游标 4 O2 G$ o1 Z8 z1 a; i! y, ]空速表上的可调指标。 + H7 ~8 m* p9 d& n" r+ c9 l1 S+ R/ I 迎角速度,! _6 H& E' q6 I 迎角叶片,9 m$ D& W9 O9 M# F 位于机身侧的可动小翼面。为失/ x; Q- E {6 `, \. U- o: N1 n" t9 C 交替, 4 W! U! Q5 c/ Y6 [7 J- j) ?" G* b# x* E# ] N制订飞行计 # B( n7 Y. D3 h8 g% p3 s7 M场。通常在目标机场附近,以备不去目标机场时,改降之2 g. T! L+ C2 ?/ G 用。1 `) a; Q( ` F- S 英汉对照民用航空词典B OEING ( {, Q* y I( TTECHNICAL DICTIONARY 8 8 i* K8 |* g+ H5 DALTERNATE AERODROME, An aerodrome to which " ~8 w, |: N/ A8 D7 E Ran aircraft may proceed when it becomes either& W" z0 l( w, J. Q& r9 t. k' S possible or inadvisable to proceed to or land at the4 U, `; o' }7 U5 A) N erodrome of intended landing.% R7 k3 i: e3 P, } TER SETTING, The adjustment of the altimeter2 y4 V V7 S3 {4 F6 p8 s% N account for local variations in atmospheric pressure.3 \! e- R& m0 v$ p* p' a LTITUDE ACQUIRE, A digital flight control system 6 i" `6 @: m4 c6 P4 ~# qode to transition from climb (or descend) to level flight. * L; A0 [3 n, h" \( yLTITUDE ALERT, A flight deck alert occuring when the $ k) Y* G P l3 J% o3 uirplane approaches or departs a selected altitude. - g0 J) [. E: R* e; Y5 _7 \LTITUDE CAPABILITY, The maximum altitude at - T3 m N% X! x$ W, D/ e9 E" t2 Ohich the airplane can be flown at for a given thrust, % j5 y2 s: l% T o) N) J' k* Vpeed and atmosphere condition.0 y, ? J; m$ k. B# l1 H LTITUDE HOLD (ALT HOLD), A mode of the autopilot + C: |: [1 T" D v% T3 A$ d; Rr flight director to maintain a selected altitude. $ s0 F# s4 u. I2 n) {3 wirplane's altitude during VNAV operation.. H3 x( b/ v8 u/ w9 u 机场着陆时,可作着陆使用的9 I; G$ H0 V; m; W6 W v5 g 场。. G U0 U0 Q6 r2 C9 B% |& @2 I" q9 ^& `根据当地大气压力变化而对高度表所做的调整。3 C; _. u* Y: M6 w% u J1 i 一种数字式飞行操纵系统,从爬升(或下降)改平的模 , X) g& w3 Q B% I( c- Q4 ^ u, h度警告, % {8 a+ b9 T: F! z3 Z; E当飞机接近或偏离选定高度时,所出现的驾驶舱警告。" v5 ^& C3 V2 Y p% x 高度能力,+ y$ w( E/ F0 {7 k1 y$ V 在给定的推力,速度和大气状况下,飞机能飞达的最大 / K5 N( X6 Z& ?9 j% V/ ~) Y7 L高度。 ' M v2 Y2 ]9 }! D* V% {5 C1 q高度保持(ALT HOLD),( o9 Z5 n1 q9 o 自动驾驶仪或飞行指引仪保持在选定高度的一种方式。 - L) E7 H) n% D# ^/ ]+ D& x! {# Y* w3 Y7 J员对飞行高度的控制。 # z/ u) z2 N* Him - p6 @" D# P# l6 Ha# R9 g8 n2 K. i' e# j ALTIME8 ~- V2 X) J0 X8 T7 G4 ] to ( T: U. A I" u; `( f! X3 V, JA0 k3 P+ `/ U3 K6 d6 l5 G$ y: z m; K/ W! a# f' T/ ? A( F' ^/ W$ {( a4 }, y$ y a/ v W0 n, ]/ v5 q1 P8 ^/ P, d9 d+ j& ^ A 0 [, e$ J/ v! F% Y) d4 v% ~& Sw ; T: w1 _- n+ e- Ys , u0 g4 ?* y) J) A mA # |2 y; R6 T5 v7 T( `3 Mo 2 V* f9 Z3 d# d5 }3 rALTITUDE INTERVENTION, Pilot control of the8 ~7 l6 d: ~, }/ |, ]5 B) f& P2 B a - [: Z# M, v, m _AMBIENT, The surrounding atmosphere. 1 {5 Y2 X: `% V* t4 p/ g7 L备用机场,* w' i: u" E6 } 当不可能或不适宜在预选6 G6 i, `! z; a- e6 ]- b9 S, p: K6 y" f' W 高度表设定7 O$ K9 x" M" U# X 高度截获, * i2 x5 `6 w6 m3 R0 H$ A+ C/ Z& \6 {* s% I5 e" @ ?" ]9 j( l* ~! @& X: H' N* f2 S! ~/ h高度干预 ! ~/ Z( c/ l1 k1 }在垂直导航工作过程中,飞行 7 s4 g$ o( e. t, U* _周围环境(地面气层),4 P5 L) o( i! N; i% j" H) a 物体周围的环境(特别指大气)。 * m4 B4 k! E9 J/ w1 N" M) z2 h英汉对照民用航空词典B OEING # w; b7 f! \) e4 Y5 }0 fTECHNICAL DICTIONARY 91 r+ E) }1 o4 _. u8 Z AMBIENT PRESSURE, Pressure of air surrounding an 6 P s" ?3 K! ^& \6 A5 {3 [object, measured in pounds per square inch (psi) .: a; M( }; Y- Z& \$ D" N$ |; B& `: ^ MBIENT TEMPERATURE, Temperature of air 6 A0 \* M: U# W/ A. ^mpere. 7 M& p# u3 ^1 F+ a: @9 v- i( e6 wurrent waveform. * L( v: q. Y4 Ig an ; W& H6 _1 G$ M8 \- ]nalog signal to a digital signal.0 A( f1 N( H1 E$ n0 h( r ore inputs 2 | }; t, L; E( a2 E2 t; wf binary digital information and one output. The output - U1 r2 k) q- I/ Z1 T7 J% W1 only when all of the inputs are 1. The output is 0 4 _/ \' p W; w7 Khen any one or more inputs are 0.5 w3 H. U0 [# G1 k7 ^, ^$ o 面气压), 3 ^" B- b' A# h" c2 K0 \2 _境温度,) c' U+ U; w- C1 l 气温度,用摄氏度(°C)或华氏(°F)来% z8 q- Q- a1 i) f, y. B' y3 I, |" p: H3 _) w& {0 a" p) i电压或电流波形的幅度。 5 Z- r$ _6 a u) r, |: F3 q$ K性变化的信号来工作,或产生连续性变化的信号9 c" }7 R0 V' p" F' _' H6 @ 统。 6 E' ]3 A' D) s6 M$ Z2 l将模拟式信号,转换成数值式。 ' ~' u0 c: q2 q0 y, {一种有两个或两个以上的二进位数字信息输人,一个输$ @. z8 n# Q8 g0 H% K8 R- V; ~, | 的装置或电路。当所有输人为1,输出为1。当任何一个+ p0 s3 U5 [0 L8 S( A 一个以上的输人为0时,输出为0。 3 W& i x1 c! y9 ?! e1 {& _# ]A; z4 D" ]% N! y5 L. N; \+ X. y surrounding an object, measured in degrees Celsius 3 p5 V- j( I8 V9 v(°C)or degrees Fahrenheit (°F). 7 o# E- \1 [3 M! K2 N% ~5 EAMPERE, A unit of electrical current. One volt across: A6 z. ^ j8 ~: a9 Z one ohm of resistance causes current flow of one 2 i+ I( S- Q# e* p3 j/ \a " }4 k. C2 h- g0 HAMPLITUDE, The size or magnitude of a voltage or ! j! ?$ A1 p3 ]5 h6 Jc + Q$ G3 o' ]6 D# {/ QANALOG, Quantities or representations that are 5 j) J$ z" @. N7 i7 G: f# Qvariable over a continuous range.6 ^( d# O/ w2 D9 y: b8 y# e5 M ANALOG-TO-DIGITAL, The process of convertin0 }- E& b, R/ u. q8 ~ a 9 B8 u4 U6 q# N: c! w3 {9 uAND GATE, A device or circuit with two or m% u- f/ a6 i6 Q, F3 h% ] o ' c: C7 g6 Y! Ris$ Z: j. Z0 w0 @+ x w / m( E4 p2 T( w7 o& @环境压力(地 9 H; }# ?3 a. u7 Y: f) G物体周围的空气压力,用每平方英寸多少磅(psi)来5 I) t: Z$ Z; d& x/ }, O 度量。 / I/ q% A+ y2 a! O; \/ l# B9 `( G6 {" B/ M物体周围的空. f" q% S1 V1 f4 d3 E' C, P4 r 度量。' u: `5 X, e) i2 H5 `7 V" g# p( I 安培, 2 k( o, [( v" [7 A4 y) {: }+ P电流的单位。 ' `' j. f* D6 ^' {, p3 c1伏电压在1欧姆的电阻上所产生的电流为 ) F% V2 ^3 K4 R2 r# `; ^7 l1安培 * g8 Z) e) ~' M8 i5 M. m振幅,9 U1 B$ K. C: _' ^* X% ]" A+ o 模拟式, + ^% B: n) @, |- y6 B1 x用连续 7 Z3 T4 `& i% C2 X {6 E- f& ?) Y6 K7 l: }' y1 ~9 A! K 从模拟式到数字式,- T, s4 n7 a2 N8 j5 c! ]9 d 与门,% Z6 u' ^+ r) @( S: K' D7 X+ L0 D2 u. f0 }8 y! C" E: V# {0 v$ r) r. b英汉对照民用航空词典B OEING- ]3 V# b1 D' @) X TECHNICAL DICTIONARY 10" L, \3 x4 n9 _4 l1 S ANEROID, A sealed flexible device containing air at low # H2 f4 _ x* m$ j% _0 y: Dpressure, which expands or contracts during change of % }0 j3 P8 N8 Y: B, iressure outside the device. ! d( e( ]$ X4 N; Q5 Nically% S, P! h: o8 O2 ^: I r changing the direction 4 f0 @9 ?9 F, f8 Z, \9 _7 zf drive. % l( |1 E1 p8 V9 p( ]of the wing chord in 2 n9 V9 n$ e: Xlation to the free stream airflow as it moves forward 3 M4 P. o! I+ vrough the air. I4 u# Q5 w! S) E+ K4 qal axis of the+ \6 b: x. e0 g5 u aircraft.) @" X* R% u; I' g% e } 胀或收缩。 ' ]+ u s' |8 ]( m& _7 X- w# L箱。是改变驱动方向的机械装置。' k9 w2 A1 I* ]* p6 X 机翼翼弦在空气中向前运动时与自由气流之间的夹角。 E* _8 u# t( g0 q1 }* `$ N+ [" u8 b/ g7 ?p+ _- R F- ~* \3 I ANGLE GEARBOX, A part of an engine, mechan # {, a7 x: a% f7 udriven by the compressor, which drives the accessory; c/ [- t- P* V+ y% \* d gearbox. A mechanical device fo3 X. ^; I! n& x/ W/ Y9 U, Y o5 L! X q, K$ h5 M6 |# ]' N ANGLE OF ATTACK, The angle # }2 i3 l7 m; P/ {4 Y; Are# L7 l! I9 y: l+ f9 {! a; H th M* ?" `. n( S8 r( T- A: H. v* W ANGLE OF INCIDENCE, The acute angle which the d! P# Y( I% A4 [$ X) s; q( S wing chord makes with the longitudin 4 K& w. c: N! t0 p( W$ a9 i膜盒, # s) }6 _) a0 K C4 \内含低压空气的密封弹性装置。当它周围的压力变化 2 j4 V+ y" c8 o5 V时,会膨 4 [. W% e8 t5 S- _3 l( q: h伞齿轮箱, ; S/ b% {, L$ q. z发动机的一部分。被压气机以机械方式驱动,然后驱动' @( K) D) \- m$ o( d) D1 } 附件齿轮 0 r1 s% v8 d; ~% @( \ }迎角,7 A8 @' g6 K! r4 y4 x 安装角, + Q9 ?2 r( z7 ^5 ?5 N! M( W: t8 o飞机的纵轴与机翼弦线所形成的锐角 $ c( G4 g( Y3 v英汉对照民用航空词典B OEING + I, M/ e( h: B# c0 k$ f- Y0 A+ _TECHNICAL DICTIONARY 11 / h2 K5 a5 V2 z! r7 }ANNUNCIATIONS, Audio or visual indications used to ! d5 k0 O2 Z8 i, p. u* Hcall attention to an event that has taken place. 1 i7 F# r$ t5 [- o* B" C: C5 s! aANNUNCIATOR, A visual device consisting of a number 6 K7 [' ^- b( v k" Ply.6 d# V: K( E6 M8 X2 H ANODE, The element toward which the principal stream$ J2 Q. L. S" z0 ` W. K of electrons flows. $ ~6 `, _6 w7 TANOMALY, Not normal. + Z& N2 S' y9 yANTENNA, A device which, used in conjunction with a 0 c9 J% K& j p% A9 @ btransmitter or receiver, is used for radiating or receiving" F( @6 M; u* x& e3 f radio waves." Y0 {" N5 W/ F \4 ` NTI-ICING, A method of preventing ice formation on 1 j$ w5 Z9 Z* h: n; Ae wing leading edges and engine nacelles. $ q9 E& M5 }# ` ~8 _2 v. S8 QNTI-SKID, A system for providing maximum braking% q0 Z/ | d. H b$ Y3 O ithout skidding for any runway condition. Anti-skid U; H8 W6 B3 k8 `& s7 Uomponents are part of the brake system. 4 s. A0 f! s/ K0 N告, / N) ~* k# F7 I8 r当发生事件时,以声音或目视指示形成的提示信号。5 d' q$ P- y Z4 S/ @ 与之有关的电路的现有情况或已存在的 $ Y5 y" a. {! n8 i' d* F7 t3 `, P. u, Y- p( H* w$ A正极,( H1 u0 F2 v! ~+ D n( u 主电子流向的极位。 8 y0 R1 R; Q+ v% B. g异常,% M$ A! ?( Q1 [9 O( Q% P 不正常。, ?2 M) A1 X/ ~+ n, [3 i 天线,, d( }2 w( e% g" \- G+ x" c( v5 K! S 一种与发射机或接收机共同工作来发射或接收无线电6 [- G4 C! Z6 O* O 波的装置。* s u' W* E4 r: K 冰, , w3 e# `' Y3 q1 R _3 a防滑系统,2 S! a5 j6 U& }$ H 一种在任何跑道状况下,都能提供最大的刹车能力而不) L2 U3 U: Y$ n* ^4 [! L 使轮胎打滑的系统。防滑部件是刹车系统的一部分。& ^" A5 y; k R% u4 Q3 a of lights. Each light indicates the condition which exists ( _ \1 k3 Y4 Z( @7 D9 P% Qor has existed in an associated circuit and is labeled# ~; B# W9 ~. D- S0 |* B$ b' [ according / U r. u8 S7 u' |6 Y6 kA. a9 ^1 O1 Y6 J6 y- l( Q( h th/ @& h3 p$ `0 n* {3 ^ A1 n1 D4 X1 i7 H, V" Z9 r9 v w' I; [# l( R( N* d c/ a! U u0 c! ]/ M U. g! k9 `; [. i信号牌,' n& I+ g( u% x, S+ @ 由一系列指示灯组成的目视装置。每个指示灯都有相应 9 b8 K$ X. C- f/ r的标记,用来显示 6 j$ x- \( e3 D A0 e' A) |- ]+ D; P0 ]) U0 n+ ?" s0 C6 z! c( P" K) j1 c$ N u 防止机翼前沿和发动机短舱结冰的一种方法。* h h) L+ s/ V- M' {$ R5 j0 a% R& ?" [ 英汉对照民用航空词典B OEING8 e0 L' N+ P5 v, \0 v! B TECHNICAL DICTIONARY 12 " ^2 y5 z L R3 N3 G l) kAPPENDIX, A supplement to the Airplane Flight Manual 0 ]4 d' X' }1 ]6 n- X, Ctained in the basic manual. A$ \/ A$ \* h" c7 N ollection of supplementary material at the end of a 0 e7 L$ P: b) t, Zook.* b: B1 z; b/ s4 { t7 }3 W+ `6 Q4 G of the+ H' B) V) \# G; v ~ rsion link on the landing gear. & [% R, _0 A6 q) u9 H; t& b3 YAPPROACH MODE, An autopilot/flight director mode# b7 q9 ^% p2 C: x5 @& A: } which is a combination of localizer for roll control and : n3 E$ K% o- p. Z9 eglide slope for pitch control. This mode is used when full, T* R( V2 u$ _- ] instrument landing system is available. , c1 V% k- a; J2 Z% G& BAPU, SEE - AUXILIARY POWER UNIT' w! w+ z1 w! A6 K4 b0 {' b0 z ARINC, SEE - AERONAUTICAL RADIO 9 s2 u# l$ n( \9 t3 e! ~; }$ a+ W' a% uINCORPORATED0 B4 H! i% }* y) _& {" | ARM, To make ready for operation.5 B, O6 N0 T5 Z* p 附录, 3 {1 V% s# Q' [' H P- H飞机飞行手册的附件,包含基本手册中未提到的飞机形 % I1 m! g0 l- d7 j" F2 v6 N态的其他性能。是附在手册末的补充材料。 ' j" M% Q+ K1 p+ }* u; g2 ]" b顶销,2 L* G1 [! h% J 用于连接起落架扭力臂两部份的销子。 - L5 t6 K6 a# A5 u- f进近方式, - D) \ Q; V5 O# w- m一种综合了控制横侧的航道信号和控制俯仰下滑信号 0 e) V: ^) E8 k的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系 8 {: ~% O8 M# i统正常时才使用。 : s- J4 u: L* G, ?; u8 a8 Y辅助动力装置, % Z @: M" c' l3 O9 }& s& Y, T0 T/ o见Auxiliary Power Unit ! u1 P5 \6 g6 Z, U8 Dcontaining additional performance for aircraft9 n: G4 W3 b% e configurations not con R$ f: s& x8 V& qc4 M8 X8 X" `" `; \1 I b6 e8 {+ u! V/ m9 @* j# v; e$ W APEX PIN, A pin for joining the two sections 6 Z9 q% S' P2 d+ Jto k T0 _6 ~8 H0 O& s T& k' e7 b* X/ w) u& ~ 航空无线电公司,9 g" y9 `2 F- T ` 见Aeronautical Radio Incorporated.8 q9 t- _! X) U! N! ~, t0 r 预位,; y9 n4 O' L* g 部件可以开始工作的状态。 % { l' ^5 \2 h( c* Q; R英汉对照民用航空词典B OEING5 e' Q/ \4 A* J4 ?3 [+ T, V TECHNICAL DICTIONARY 13( i$ y8 @! z, V& r4 b# l ARC, The curved track over the ground of an aircraft. u; c4 T# _' X7 M/ S- p4 | flying at a constant distance from a measuring+ T: d' t b# s) l z equipment (DME).7 |8 \: h% I; p+ g9 z in the limits of self-contained system / K7 R3 l) c% p. L7 l/ Sapability.5 W) I6 x$ O' |# I" R% Q% `% k tem for opposing or restricting V6 p& m/ d6 l# w+ K6 j2 Q ovement.$ ~ B; ]3 ^1 |$ P SPIRATED TAT PROBE, A sensor that measures total- p! P) u( r" H1 @1 L$ x& R5 W ir temperature when the airplane is in the air and that! i# O% M3 S% Z- ~1 n0 I5 n+ M1 `( q easures outside air temperature when the airplane is Y- l% A' O- H5 J0 z; w0 ~n the ground. The outside air temperature is measured% E2 u& G5 s3 H' n7 L$ v6 U SSEMBLY, The fitting together of a complete structure ) w* K c! Q, o6 p7 t6 BSSUMED TEMPERATURE REDUCED THRUST, The2 r$ J3 A2 b# N2 [ ATC, SEE - AIR TRAFFIC CONTROL0 Z/ t6 E) V' n) s) v1 x6 R/ [0 B% ?. S. l& Z4 f- N( i 系统中所产生的一种用以抗拒 . z9 w' D# J- d4 `( Y( H9 b& _作或限制动作的力。 u& H, V: L1 o头, 1 n: X5 d4 D' A s5 f用来测量飞机在空中时的总大气温度和在地面时的外 # c: c, F) m% r9 h g温度。地面外界温度的测量是利用引气将外界空气吸入 & }, m. h. O! O1 P头,以达到测量的目的。 $ ^$ C2 ~) `3 g9 \ G% m2 A7 z配, / G6 S5 z& b! w! ]一个完整的结构或组件的过程。! [# @3 Z; x/ R2 I6 E( J+ m y2 N4 H 假设温度而得的减推力,! [* W3 X( R& n' Q 推力设定值时,假定一个比实际外界空气温6 m V, J1 N. t5 C( Z" ` 空中交通管制, 2 t. q D. u/ W) x. c. t) y见Air Traffic Control % A: m$ R/ ^$ v5 ZAREA NAVIGATION/RNAV, A method of navigation* x3 K& a+ i& }& O4 Y# |2 v+ K that permits aircraft operations on any desired course; c4 _7 M0 R$ g within the coverage of station-referenced navigation* j' Y+ t" h4 j/ }# e signals or with! P E6 b; C7 {" e. A c & f3 G- N* E' Y; @! g' o4 UARTIFICIAL FEEL, A force developed in the flight & \9 k: [, z' o0 Scontrol or brake sys6 T1 }9 T2 M+ f, e+ n" e% l m , k: ]: _3 S# |! W$ P: j0 \A* X& c* D1 Q' }- M! Z a8 f6 H* v5 o$ d, ^9 p# ]9 I! Q m 6 k ~. m/ a( r! jo) a" x: b! I7 E' X; u/ a by using bleed air to draw ambient air through the* G! b3 b; U5 x3 ^6 d! e; f sensor when the airplane is not moving. $ X8 V) w* C( i% Z+ G! W) _& jA8 N" R5 K3 w+ s0 F or unit. ! c9 T T& `4 @8 `$ B, c0 W% ?A 5 M# I: ]+ {) Rlower thrust obtained by setting a higher than actual 1 W$ M+ N- [9 s# BOutside Air Temperature (OAT). 5 q' y, n2 V* S弧线, : w9 H5 _$ U" f: E7 u8 T飞机在围绕DME台等距飞行时的弧形航迹。 ' X' Y- v- f/ i y& t5 E4 n区域导航, ; t$ _/ n) J5 m9 b* h, B容许飞机飞行在有电台参考的导航信号或自备系统能; n4 Q2 ]" G$ x# {7 t 力极限范围内,飞行任何预定航线的一种导航方法。 ' t+ q) ~- w' S模拟感觉 % N6 X$ C' \ E' F# b) w! _, s6 I在飞行操纵系统或刹车 $ b9 R$ S9 m' p. A% z: N8 c* G! q/ C, z吸气式总温探 Z3 _( Y' D R5 j+ d& C5 `$ J. |: c9 E" B! ?- h& t" c( t+ [" Q: U4 X, V! Y# T$ V组合成 # z. b. N1 n# D1 j: z' c1 m1 x3 u% J: Y; G 在选择起飞 ' Q- ~0 H5 M% |# `度高的温度而得到的推力。用这种方法可以减少发动机的7 x }/ a& ~( U3 }8 @. B! ` 磨损和维护费用。9 V P7 `" l& g" H7 T& e% }) T- j: n& y英汉对照民用航空词典B OEING; j% f' `+ c+ w. R. p TECHNICAL DICTIONARY 142 {% M% k h1 s7 O5 e( a9 i9 ? ATE, SEE - AUTOMATIC TEST EQUIPMENT5 c8 r- ]7 l1 ~! J ATMOSPHERIC PRESSURE, Pressure of air due to the ) d4 R* C- G. X% b# Zarth's atmosphere, expressed in pounds per square . W% b2 p. E! x/ sch (psi) or inches of mercury (in Hg) or millibars (mB). ! p3 `! I3 D1 C+ G: ATTITUDE, The relative orientation of the airplane with" _ l' H3 a# [. ~# ^/ \. f spect to pitch, roll, and yaw. * H9 Z. Q% e! D* yUDIO CONTROUSELECTOR PANEL, The panel in' v* f8 N, d! Q; s9 l e airplane which controls and selects the routing of* s$ D" k# d- Z6 l. x; F3 B6 N udio.' v8 j- r! Y6 L# c& k6 o UTOLAND, Automatic landing using the Digital Flight . Y# o# f: O+ E& Fontrol System.! B' ]4 x0 C/ B) r% o n.1 D* r. a% n: Q. n% p7 `4 x M, A system 7 q1 P: k6 D" k. i. m& ^omposed of all necessary subsystems needed to guide7 q, Q7 A4 j6 q5 A9 @# U; G0 B6 ? e flight of an airplane.- x1 G) x+ J! \ EQUIPMENT, System test' _# ~; T, X8 j& L4 D- k0 M quipment that operates under computer control. / P5 [, c4 G, M, m I, a* h8 w装置,

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e : A- M7 I* D% s6 o: t% oin + r9 r9 m$ h1 J) @. wA 3 d2 I6 e6 E6 v3 S. v/ c7 j" Xre # G* Q- X. A, Y& S1 E$ w5 x! [A0 V1 @& y7 s7 o9 O+ i th& r, E( h' O! W* }5 w" L0 T" i a" l: _' M2 s$ A' P& H A: L* ]. b" J# m C 6 e3 y% h, G6 G6 d$ NAUTOMATIC DIRECTION FINDER, A system which/ T7 i L) M1 w6 q; e determines the direction of a radio statio% _9 v1 T$ Q& U% {, X AUTOMATIC FLIGHT CONTROL SYSTE$ e+ _. u( b# s& d6 G c $ o4 I! t, [, ?& s4 {# g; Lth & B% R3 w6 m* U5 [: R9 N: r: Z }AUTOMATIC TEST, z. w4 }2 x+ r; F1 {0 N5 r9 T e 4 b* X6 ]2 R" Q4 X- m& C7 ?自动测试% g- d. H0 M- E8 ` v" ?' M0 V 见Automatic Test Equipment. * E/ r( d# u! a. f2 a2 |% j C) P; j大气压力, 0 P; o/ j" Z1 ^* a9 |) r由于地球周围的大气而产生的空气压力,以每平方寸多 * z- l u; f; g L: \磅(psi)或多少寸高水银柱(in Hg)或毫巴(mB)来 ; v( j, ?- j* @; k3 x示。 2 y) d" l6 L6 z飞机姿态, t/ J! W! \& x' M! _ j 飞机与俯仰,坡度,和偏航有关的相对方向。4 t# S" ?; g/ k r$ Y3 [5 @9 K 音频选择面板, / `. L! z3 n5 r5 h* T2 U D. q飞机内用来控制和选择音频通路的面板。 . `6 z7 k" t4 W4 T: H6 ~- B8 @自动着陆,( |. Y: `8 n2 |; m0 p7 l$ f | 使用数字式飞行操作系统来进行自动着陆。 1 c. u+ q. S- y的系统。% Y! {4 n) U- [0 W6 F( b* ^% d: h$ G5 L2 y& I 系统所组成的一个系统。9 O1 H+ j# }4 s9 ^8 \ 在计算机控制下运作的系统测试装置。 . z+ ?8 \4 B6 Q( r6 `1 U) F, Y+ t+ I; ]) [) S+ M3 P5 m: I) V! ~! X8 f+ `自动定向仪(ADF), : W) {% _2 e! u! V* {确定无线电台方向 9 Q& m+ w) q( c1 l5 j; D自动飞行控制系统1 @% ~) F7 A- |- j4 u" d+ ?2 j0 V: L 由所有能引导飞机飞行的子3 P1 K. X( ]. G( _ 自动测试装置, - j' G3 J- c5 p- n$ e- Q英汉对照民用航空词典B OEING4 ?) n. t" r2 g5 _6 ] TECHNICAL DICTIONARY 15 , U. n" @. _4 WAUTOPILOT, A system which automatically controls 9 ~1 k5 \ K% N8 g: x: \* Iand guides the flight of an airplane. 3 @; B% ]/ v" F8 |AUTOPILOT FLIGHT DIRECTOR SYSTEM, An( ~5 W, ~4 U1 D% G. O1 q tor& W2 R2 x _0 O UTOTHROTTLE, A system which automatically4 C% B1 n6 C9 Y ontrols the throttles of an airplane. 3 F1 ]: K" F2 {# W' p: B4 mPOWER UNIT, A small turbine engine in' e7 N4 v4 ^# K }; z6 \ e airplane for supplying electrical and pneumatic * F) ]0 m: D" x$ e/ Hower for systems operation on the ground or in flight.* u7 x& {# m5 f0 `- I VM, SEE - AIRBORNE VIBRATION MONITOR 3 ?4 c' m6 W5 U/ ~( b9 S m7 \ M9 sXIAL FLOW COMPRESSOR, A type of compressor " x; t$ s8 D2 t6 _, Hsed in a gas turbine engine in which air passes through K: N5 Q6 |8 n$ M$ d XIS, An imaginary straight line or an actual physical* r" z: _! \& ~2 @ omponent (such as an axle) around which a body can4 z( I: X9 \) Y/ C3 X. W8 Z tate. " o% N) x# ^6 v+ X' Y. Q仪,; t( S4 t4 N M6 w, g1 O# k! \$ C! r4 _9 K: q. Z自动驾驶飞行指引系统, ) X6 W+ O% {% |7 F+ Q动驾驶和飞行指引功能的系统。8 K" P* V. F2 P3 d6 m$ `9 x6 I; ] 动油门,2 ~- ^% |. s/ y+ C4 M! g; S9 W 自动控制飞机油门的系统。9 l9 x3 P, _% G 是飞机内的小涡轮发动机,在地面或空中给各系统提供 5 B9 V* R0 ~( A源和气源。 ) A) b4 M/ j( @8 |+ \8 U- h称。- H$ q' z8 Y( ^/ t 载振动监视器, % O9 @' }4 C( K. W见Airborne Vibration Monitor5 X8 W2 t$ j3 ^; P integrated system containing autopilot and flight direc' _, M, N n* ?. o functions.+ z% i/ u! N2 q+ p5 f A G [2 ]6 k' X4 Y; t c 5 b* A. [! v& ]2 o4 Y8 q( rAUXILIARY3 x$ W% g# Z i! `. G' S th, E/ ^" R- O% Z5 A$ i! \ p5 f+ `. j" r3 \4 r! g AVIONICS, An acronym designating the field of aviation9 }; w0 H- ?& j* A& k& H electronics.8 ?5 m! I; J( ]- ^0 y/ V) n5 T A 2 r2 ~2 U/ t) }. vA3 y) A t" C- I% ]& ?& b u' A/ k5 }1 V d5 H* g the compressor in a straight flow, front to rear." B0 |# g. g- @6 z, t% B) r A }! P' B( v4 F7 c c3 _9 X3 M$ o6 ]1 g2 c* V/ y& C& `( F ro 5 {: u) q6 O; ?/ H自动驾驶 - u2 _, C" ]! a" i动操纵和引导飞机飞行的系统。 H4 Z/ P7 U7 A, k0 L4 z: M 一个综合自 * j3 E$ {7 c9 S! |8 {6 W I/ b- @4 Q6 s2 ]- l0 Y辅助动力装置, ! u' J1 ~: K2 e; b6 S% J) Q6 J+ c# }5 V" R2 V5 C" u航空电子学, / K/ A9 q3 M. f1 u" }/ _8 n是航空电子领域的一特有名2 E/ W# ?/ w6 e8 [# [" k* y; X3 f! A4 j" l Y! G0 M- {; A流压缩机, 4 l' J$ \6 M* E8 R一种用于燃气涡轮发动机内的压气机。空气由发动机的/ g7 E# H' F$ B6 ?; _9 e! Q 部流出。 - ^5 R; Y: x! d" {. L& \3 P线, ~: E( W; V6 U( L 可让物体围绕着作旋转运动的一个想像的直线或实际4 _/ u* \' p$ {/ t 在的部件(如轴)。2 x& D: W; d% d: S6 |, H2 a% S$ D/ o' j# z# K$ C 前部轴向流人,压缩后,由后) M- v a5 v- b [% p2 o, h! V a- H: k1 S& W* D* J' p9 ?/ k" m* F( t4 P) O 英汉对照民用航空词典B OEING . [8 w3 f0 r8 C# N, B9 Y8 |# VTECHNICAL DICTIONARY 16 & b; N2 [$ V2 C7 m3 H" tB ; e" J' P1 ` }1 p! Z) M, iACKCOURSE APPROACH, An approach to a runway) J5 T( {$ A) U9 S8 \# }+ p versed. 3 r1 K. p2 w" Xown on the EFIS that " m. Z+ i6 x4 y& @3 L$ zoes not readily change, for example, navigational aids. $ n( [4 J; ]* f* X) {, }vement in the tank or reservoir. : E% e k# K$ `8 \. lALANCE TAB, A small hinged moveable part on the8 o3 y1 L- \! {! J6 ^2 L+ L ailing edge of a control surface (aileron, elevator,) x; d9 s$ b- ~ 航道进近, 0 ~- i+ W( o# H" s @9 {" r相反的进近方向。当反航道进近时,无下滑8 _1 c' L) S% U. ^" i6 e 显示在电子飞行仪表系统上不经常改变的数据。例如: : A% [, d8 Z5 w1 a航设备。( M- C0 J7 Q. l/ ] 在燃油箱或滑油箱内阻止液体流动的隔板。" N/ g; \8 z8 z$ N; }7 ]0 b 动补偿片,1 `9 u2 e" x+ H" l( X 铰接在操纵面后缘(副翼,方向舵,升降舵)的可动部。* o4 g: I8 N' J( K1 U 与操纵面相反,以帮助操纵面运 0 |" d5 {& q( e) y f+ s' q) pB: z1 d8 N: [3 K5 l1 A5 B' w# \ which is opposite the normal approach. For a + r& V9 R7 e" W8 b! K& |4 xbackcourse approach, glide slope signals are not; Q- K9 g5 c4 P* D! F) y% A* @, n available and the sense of localizer signals must be 5 P- }9 y9 y4 @8 P0 Sre 7 { z2 i/ |/ R; w: W$ {BACKGROUND DATA, Data sh % n9 P- u7 @' A5 x, Od 3 {3 j' u8 b% d9 P% J4 @BAFFLE, A partition in a tank or reservoir to prevent3 v( x5 H& @0 z* s* Q9 F' B0 g4 ] fluid mo; K( D r/ ]1 Y. P2 ?/ N B 3 Z# U) r4 D/ Htr 6 N6 {: ~5 `1 lrudder).The tab moves in an opposite direction to the9 p5 F* n: w1 l3 `+ ^ control surface for assisting movement of the control 6 ]2 B; z; H7 |# o6 d1 [% @surface. 7 g; A$ K- i* l; o* n$ n# z- p$ l) B' W, v: Z( g与正常进近' ?3 ^2 K: g' B 道信号并且航道信号也必须逆反。1 F& D* E: x- R4 G3 z. a1 W, W 背景数据,! E9 Q$ L6 t' w: _. A" j3 ` g& a3 L3 _+ i缓冲隔板,6 G& [6 x+ A3 h3 k9 h% z5 Y& }) R. x$ `随动补偿片的动作方向9 ^6 I- Y9 d7 {8 y+ M 动,减小操纵力。 , {1 H: G- d& v0 {7 x& I英汉对照民用航空词典B OEING7 {& V- b! I& G4 K9 ]3 Z TECHNICAL DICTIONARY 17: B: g! J( \- y w; U+ W! d8 B# A BALANCED FIELD LENGTH, The field length# U0 _* F# b G2 w# w4 k associated with optimum aircraft performance when6 ^6 f- I+ @1 ]( r/ v, ] bstacles are not a constraint. In this case, after engine 6 m" f8 b* u7 E# j2 P$ M; ~ilure at V1, the distance required to accelerate, takeoff 1 t4 F2 \+ g( W! d3 Tnd reach a height of 35 feet is equal to the distance ) D6 i: [2 ^& k" r# Q# O! }ALLAST, A weight installed in an aircraft to maintain, v$ Q2 e( e7 o& K- q ALL NUT, A fixed spherical nut driven by the 8 @2 D- L L8 o( ]AR OUT OF VIEW, A signal used to remove the flight " w. o* W6 e1 d5 y G4 nAROMETRIC PRESSURE, The pressure of air above 3 U" t; F2 I6 l; e% O6 V& r- ng) or , L: R7 L k0 P- M j" Y3 H! {millibars (MB). & v) t) Q- M+ e# }& g1 \2 ~1 w5 dATTERY, An electrical device for changing stored 1 Y, r' C& I/ m: S. V. h- ]性能的场长。在此8 P$ C0 h1 B* P8 R, R* V 况下,V1时发动机故障,要完成加速、起飞、离地35: t5 d* x$ W ~( D% u$ w6 y 尺所需距离等于相同速度下完成全停所需的距离。/ R& ?8 {/ w2 D$ i+ h3 } 舱物, % ?7 H- W5 d9 t: t4 S重心在许可范围内面装载的配重物。- J* P; g6 K2 {; G 形螺母, 0 v, `8 J/ n6 e% S的固定的球形螺母,用以使襟翼和水平 ; ?: F5 Z3 ]+ e2 x; u" d引杆消失,8 C( n. l4 K2 C, P4 M' L 指引杆的信号。. F w% }+ V. j0 v 压, 9 A" C0 Y) Y8 L( `- {压力。通常以多少寸高水银柱(in , m2 d. Q6 l w' j1 N0 f2 ~瓶," U/ H/ E1 J& D! }: m8 R1 P( j4 K 的化学能转变为直流电的电气装置。: _0 Z U- d; A7 `! }: g; ~& M o 0 A; S4 f! B0 A& W% a/ Nfa. K3 k4 J- u$ m1 B% R: N a ! ?- c6 b( X* c+ D) m! K# Krequired to stop from the same speed. ' g& u8 M! D; |: G1 i- T* G Q3 vB . V" ?8 ~' \3 n% L; K# S& ]# rthe center of gravity within allowable limits." C4 i2 U" a% I& q, i6 ?. e B- Y9 o& l( s" R+ e jackscrew for flap and stabilizer movement. + J4 w$ |' G1 ?B4 z6 W) h( `$ F: u" D2 b" Q6 N% d director command bar(s).! Y% Y* ~* R9 s4 [6 ~- Z B , U: `3 p3 P: G5 y- bzero pressure measured in inches of mercury (in H8 c- t# u; M8 \) V; v in . x# z& E2 u' oBASE METAL, The underlining metal to which alloying1 U8 f; I! x( Q! V: y agents or metals are added. * e4 p- G' V& ?- i N: @) F8 D! jB( O/ I* F9 V3 s2 T' f7 |+ ] chemical energy into direct electric current.; x4 i( R6 C" e2 s7 N 平衡场长, & Z& R( s1 z, K. S6 [! N2 ^当障碍物非限制因素使飞机达到最佳 2 I# R6 a" K# I* @. e; s0 E" R) N" g( U2 g1 f% D1 n& q0 J6 j' n) A3 }. M8 L, p! d8 l7 V8 V) |' b为保持飞机 H, ~5 b, L! ?" U$ W3 j$ U* X5 t' }9 _; Q3 | 由粗重螺杆驱动0 t- j. F6 v# a! H1 C! S 安定面运动。1 j/ E: ?, _: d" j- Z" p" Q* m0 T! N5 l! [; p- P4 I: \ 用于除去飞行# B, F! a6 }" M& |1 \3 ~' }# s- v$ P! U- r' G, X5 D5 g零压力以上的空气: S4 m" [( Q6 L8 b; @) U6 q% r$ h Hg)或毫巴(MB)来表示。 * D: H# v R' c0 `* Z9 X8 _基底金属,$ f) p: C5 `! P# I- G 指合金中的主要金属成份。 : u7 d4 w* V N; G8 }- |: U" @# X+ M1 |, f 将储蓄7 N: ]8 A3 r/ j; h6 s- B. _ 英汉对照民用航空词典B OEING' y% B- i L) T( h- r TECHNICAL DICTIONARY 181 L6 L! C+ a+ z BATTER, \3 {% }1 u! p4 m2 N' x# N) j9 b1 i2 w direct cu( c6 r# x% e9 {2 M! L: E0 C% \ power su; M! U8 R$ n1 j0 D Y BUS, An electrical conductor supplied with ' b/ t* a- {4 G7 p+ f' Y& e" crrent from the battery or transformer-rectifier for 7 ^2 Q) X0 U1 D8 L4 ^pply to operating components. ' c7 Q+ n' v2 _0 ^" |) XCHARGER, An electrical device supplied w# U! I: I0 x; E ith alternating current, which produces a direct current8 V. A) j- F' j; \. Z# h utput for charging the battery on the airplane. , M5 \3 h- ]3 EAY, A compartment in the airplane structure.. i7 w( }8 @) D: Y0 ]8 I2 R% P CD, SEE - BINARY CODED DECIMAL: X, z# K+ ]9 r: K# e* K3 Z* ` e EACON, A device which emits a signal for use as a1 P" e9 X7 y6 l8 y3 J uidance or warning aid. 4 U- I+ ?* U+ u/ LBEARING (NO. 2), The direction from an airplane to a( h$ M8 Y3 G) c- C! R$ h; j$ S ground station.' V9 U7 {, d) Y' I" O4 n( s 瓶汇流条,, t2 ^' _. c3 p$ E. [! k+ ] 将从电瓶或变压整流器来的直流电供给工作部件的导" h2 U6 k- G! x8 [7 Z4 G 体。 ! d. b, x# |7 R' B: \* y: k瓶充电器, 7 x6 {! `( u" [8 H. T1 I1 n5 d用交流电向飞机内电瓶充电的电气装置。带有交流电的 2 V1 N) C. r1 N/ u6 b9 v/ X, C气装置,该装置产生直流电向飞机上的电瓶充电。 9 W. t7 h- L* K) Q* h! D舱,1 {- Z2 A; f5 I4 d0 X 飞机结构中分隔的空间。 ! S5 \$ r" e" \" l9 _二进制编码, # Y+ ~3 `3 v9 J) n见Binary Coded Decimal 6 b3 G! j, G( u1 IBATTERY7 w7 i# r9 v9 f) h- f+ H" o% j* F w . i2 r( R9 ?; m: M8 @3 Oo, A% }" A {3 z- s2 S( J! O B9 ~+ s7 l- y4 T* |5 M/ u3 J B8 ]1 f; [ i: M0 t" ]- n B : o* b( Z: \; s U9 Pg0 P4 s6 f5 }2 x BEARING (NO. 1), A surface that supports a moving " R/ ~2 D+ O6 ~4 Upart and reduces friction between the two. & ^ N |% z& G3 H2 |" H$ n3 z6 Q& X5 Z$ O) e1 f$ ~! L9 D% _* W) r9 n9 G8 S3 _% M$ q9 Y9 A& O" j9 T" U: i+ D5 b1 O4 W" j; ?* V; C# ]$ P# D, `6 |5 X3 |5 P/ A. g. o) i; o+ r8 o- X+ C u+ r% D+ R 信标,4 n) L; s2 B% H- Q2 B" F2 m 发射引导或警告用信号的装置。 1 U' h' `; ?. |2 }) A! ?方位(NO.2),5 J# F) t2 P4 [" Y- y& E 从一架飞机到地面台的方向。; f# _/ A; J# q' d8 ^& D0 K 轴承(NO.1),& h! k) u' p, m1 s8 ]1 G: K% r x( j 用于减轻机械转动磨擦的机械装置。0 [2 t; B2 k5 \9 ?* { 英汉对照民用航空词典B OEING. n/ b0 w( k) Y* r/ C TECHNICAL DICTIONARY 19) V8 A: Z L7 E BELLCRANK, A double lever in the control syst 1 j/ ~9 E" d6 Z4 Q( @$ Qchanging direction of motion. 1 f6 R, ?* J' O# v6 K" Y! a& [* Z$ lem for5 K+ w" Q6 ?. o ct in the! |( v; s+ W. i& y" m P) w neumatic system for absorbing expansion of duct due 9 Z$ k7 g5 u; A9 W) qheat.0 q" V0 q( H8 }8 N# X, N$ } ELLOWS (NO. 2), Corrugated folded or pleated % H# f! s9 D" `, ?8 Lontainer or compartment used to measure pressure. * |: d/ v& ?( ?/ SEZEL, The part of an instrument case for locking the3 [% ^7 y6 `# k lass.) b/ {$ _, R$ j3 d+ [ IAS, The potential difference applied between two 4 J5 c% R% H; J/ ?9 M/ j9 Woints for controlling a circuit. . t! i; {5 A1 t" G y* H/ m5 [! lBILGE, The lowest part of an aircraft fuselage. A place 2 Z6 M4 A2 Y p7 F; mwhere water, dirt and other contaminants collect.8 G$ x( N9 ?+ k+ z9 O" H 气源系统内提供管道热胀冷缩所需要的余地的波状 {) l4 L* @$ j ~% l8 y 轫管。5 J! B9 s! C6 M# V4 o6 L 空膜盒, ( ]& R1 l0 B$ N1 H一种具有波状表面的容器。用于量测气压。. L; n9 g- K. U4 j; S" A. H* b 嵌沟缘, 5 Q/ a. ^& s+ n: H5 f5 X; W将表面玻璃固定在仪表上的圈状零件。 # _; |& M# x2 I+ z+ R压, 1 A7 V; R; M8 m2 M, b- t在控制电路的两点之间的电位差。 ( M) V3 i- ?3 e5 F; U9 i% L机身腹部,. c, i* Z0 S/ R/ g 机身的最底部,通常水,脏物,和其他外来物集存于此。 % ~% M) H% I8 |9 F' ]1 C1 Y1 UBELLOWS (NO. 1), A corrugated flexible du* t- B3 I. @0 X, M2 h p; N3 T3 C6 i) E& I7 t to$ k0 z9 L |- d' u B 1 [, m! o1 ]+ f Zc % B/ ^4 c7 A4 v- S: d% I! J4 r) `- L& TB , @* o2 Z2 U, W- f0 Vg7 O y! S; K# u( W B# j) V1 A# D3 p% v1 X p ! X: b; q, Y: c3 D( e+ f: V( X* i直角摇臂,( c7 ^7 W0 p: R# \9 | 在操纵系统中改变运动方向用的双臂摇臂。* k) W& R/ d) x. w 波纹管,* F8 y1 h* k$ N. v( Y Q# Q& U1 j4 T" q+ H" b4 T" g* E) h7 n; f4 I1 U1 k! h# m$ _' A2 z: [, X9 y$ a1 w, \ ~' q3 L( [) X9 s英汉对照民用航空词典B OEING, ]" G9 w: T) @5 ~ TECHNICAL DICTIONARY 20 / M% s+ ~. o8 O. Z9 H0 Q+ i" EBINARY CODED DECIMAL, A system of coding each) ^" V. K* @8 V$ O3 b8 F | digit in a decimal number using the binary equivalent. & R1 f' ], [; H! p' HBINARY NUMBER SYSTEM, A number system using - F7 T1 ~4 _/ C7 p* f0 ^7 p" y4 @8 ss1 H9 m/ i5 j0 ? IT, In the binary number system, the smallest unit of ( y; x1 t0 e$ a, t3 q E* |7 d( R+ aformation, consisting of a 0 or a 1.' U6 X# E* ^* r9 U) @% F& s ITE, SEE - BUILT-IN TEST EQUIPMENT& V, `, ~6 T+ T LANK DISPLAY, A display that does not have any 3 W( ^% r2 A3 ~: P4 U# q6 t6 I$ X- Hdications, normally due to failure.3 }" X7 l) O* o5 p1 b2 m LACK BOX, A container for electronic circuits to record4 G/ P* n( _8 ?7 i Z) I+ H1 p# B ight data.2 N9 i4 z" _+ t; V LEED AIR, Air taken from the engine to power various% r8 n1 `7 z. Z2 I4 s: p1 L ircraft accessories. : K2 H/ `5 S8 F! q p0 t2 kA valve in the pneumatic system for air% Z5 I3 p1 T" h$ k! L6 x supply from the engine or auxiliary power unit to the7 ~# R, K* L# z- d8 c pneumatic manifold. A valve on the engine for reducing* W! H2 U: K9 y( l v8 n" l- D( u pressure in the compressor section. ; p, J( h' B5 X* }- A% w进制,. b+ ]# l# A( m5 b4 S9 J" K 进制, # V* C4 e9 e" ~4 H6 q一般用0和1)和2为底的数字系统。5 I! k- m, h; O3 J7 B 特(二进位数), 2 l3 g) Q. O3 Z二进制中的最小信息单位,包括0或1。 2 P2 x5 b. e v& N$ G内自测系统,% A: R- U( f, j4 y- \+ i 见Built-in Test Equipment 2 x( e0 X: f( ^. ztwo symbols (usually denoted 0 and 1) and having 2 a 6 P% l# }. o" o& M7 A Gits base.# Y; i% |3 a# e' c& ~ B 9 p: O" x( M& Q1 U e/ ]% Vin - Y! C5 e8 L( b& bB2 Z6 i1 D. l+ z$ l" x B- B% a* u0 J& @( z4 ~$ I; [ in , k0 y4 K" i0 k* s, A. {7 UB6 |3 R0 {* |2 `4 ~ fl2 G' a i; H% e* h; F$ }0 |4 Z B0 I0 q' r0 [* q3 O a! ^3 B4 p g+ c2 b9 c# j, l6 X BLEED VALVE, & b9 E+ t0 v% Q$ I4 n二进制编码的十 9 l; E2 o4 x' c4 @5 z8 G一种编码系统。用等效二进制位数编译十进位数的每一 $ b) d; W8 a" {位。$ K, n8 s: Q6 i2 e( J2 u" ~( F# J0 l0 Q6 L7 W- m! G& P2 q( V以两个符号( 2 p4 o: R2 ?# Y) n/ b, I& \5 @6 `6 D" K- u2 z$ h' l' C, s3 o/ ]# K.. C/ Z7 R& C! ~% F- [) f- U 白显示, : H5 S0 c W' o( n( Q& }通常因故障而造成的显示器上没有任何指示。 # T4 E! n: ]) n% @) a* ~, ~# Y匣子,: c v# K- |, c2 Y' K' P" x7 M 装有用于记录飞行数据的电路系统的容器。0 E" Y! E- g* ~4 z% ~6 c* | 气,9 r9 S# J& d/ G/ h, H 取自发动机而用以驱动飞机上之各种附件的空气。 * `5 l8 E( S2 z' F! q气源系统内,使来自发动机或辅助动力装置的空气进人 7 w" o6 R9 z$ d气源支管的活门。发动机上,用来降低压气机压力的活门。/ a/ d6 M% ~ I( `1 o1 \9 n3 H. J8 @7 G4 A1 b1 d1 e. S7 x& [: E3 ~: t% F8 G; B$ ?4 }% f$ Z U8 ]引气活门,' r/ @1 V9 g0 v; B 英汉对照民用航空词典B OEING % U& A8 g) E: A. gTECHNICAL DICTIONARY 21- I4 y) y `2 G: N3 \- ` BLOCKER DOOR, A device on the engine for blocking7 R( S- c% H' D# _2 S9 i the normal airflow during thrust reverser operation. * Z% d9 T) N# ~LOWER, An electrically operated fan for circulating air. , j. V7 s( G: H) p& hLOWOUT PANEL, A panel in the structure between' b; x$ C; T+ X, J+ c, _- ]% R o compartments that opens to equalize pressure in , h1 w5 f' |7 ?' [e compartments. / B3 g: P5 ^$ G7 F9 s/ j" XODY GEAR, The landing gear attached to the G$ F, ]* j0 l# d+ D grounding.4 Z5 K4 R! B) T' n! b \- [2 | 正常的# b8 j, l/ z/ Q' _8 A5 M- O, u 气流。3 Z% }- ~4 F5 r) T+ R9 j 鼓风机,! @) {: {) l# X$ r 用来使空气循环的电动风扇。* ]( `; b; V# |$ b' E% I 压口盖, 4 `' n O8 a9 }$ U7 E {6 B, @) Q- j两个隔舱之间的口盖,打开后可使两舱压力相等。* v- ?: L n7 X 身起落架,1 [1 }) i. e/ o 身构架上的起落架。. z5 D5 i; t- |2 r# k- \& C B ( ^7 k9 G$ p3 L; sB & h; n! ]1 Z/ d( ^) [tw; q5 N$ X" H" x: s& Z. U th+ T* F0 f) Y, I, S$ H B 5 w, U; v6 e) a9 E8 c' ]fuselage structure.7 H: V6 A0 |3 x2 ^& v5 Z BONDING JUMPER, An electrical connection between; i0 U5 X5 y' C8 \# J a component and airplane structure for electrical + w4 @3 r) u" n! i% e阻流门,0 y) j& _# `2 b" H I! r* J 发动机上的一个装置。在反推工作时用于阻挡 ! O9 A" e* r% t9 y' f; k3 A; |+ {) l7 n5 c/ x U% M! b8 y+ t, A, D装在机 . ]2 s5 }. e* C- H% P2 Q# c搭接片, 6 ], V7 @( V$ J% X& [5 G. Y" x+ U连接某个部件与飞机结构以形成接地的电接头。& H, `$ M0 m& K; s 英汉对照民用航空词典B OEING 2 C3 i0 G: G: G6 n( ?, [/ yTECHNICAL DICTIONARY 22 $ r- g+ H6 Q( G4 ]BOOLEAN ALGEBRA, A mathematical system for! V# ?/ ^( K [% W/ n5 } writing combinations of logical statements. 5 C) K5 s: V! L$ N( ]BOOST PUMP, An electrically operated fuel pump for 8 S z: w6 R$ J. d* ^1 ^fuel supply from the airplane fuel tank to the fuel7 M" a+ S* U" u& i4 j manifold.- d' r) C, r; B: r6 d2 a BORESCOPE, An electro-optical device for looking at - Y' F( `0 X- f r8 p% }ternal parts of an engine through holes in the engine.9 n) a6 h/ x& e b2 H' w% j orescope ports) & x/ I+ {4 j6 I/ O; c R& e9 iOURDON TUBE, A curved flat tube in a pressure gage9 W; T. k: w2 w7 N r moving the pointer when pressure changes inside 8 I) P" a6 D. g$ D5 {4 B$ Oon the ability of the brakes to" p/ \9 E' F# E4 ]+ R( R bsorb a predetermined amount of energy during a' y9 w$ o; S v" g. T) I jected takeoff. , M. n- D$ A) y- q用于通过发动机内的孔(孔探口)观察发动机内部件的* O3 V+ S# l6 _& L1 N9 k" d 光设备。 , [. s! i( U$ {) ?3 b端管, `3 P% X8 H( U, e' B; F8 | 测压计内的弯曲扁管,管内压力的变化时它使指针移 1 e+ ^* W% y( s& J力。* `# C/ E, [/ ^' T! o t" x1 s' c 极限重量, : }% s: T0 S. v* m. J/ `0 Q6 Y# o; u6 r" W起飞重量。 4 n0 W6 }5 x! |, V2 y发动机滑油系统与大气相通的通气口。2 B. o0 f" n2 X8 l$ n in ) [* N k' Y: _" X! ](b( T7 H) q9 s4 ]$ y' w3 T B * N w1 Y8 a" x; F% g9 ~ o( S0 Lfo 2 ?* Y$ X3 j5 q% a3 D/ Kthe tube.% I7 U9 v- t! D BRACKET, To enclose or surround.: T' C. c B6 E0 d; |* J BRAKE ENERGY LIMIT WEIGHT, The maximum- i- |7 m" P/ |% o; r takeoff weight based" ~+ M9 M+ ]1 `9 ` a, p+ m2 f9 a1 v1 m9 ^ re # b8 M/ h. G- s( \( FBREATHER, A vent to ambient of the engine oil system. . P1 u0 H% K+ {1 f [% |1 N0 l3 a布尔代数,' E$ d4 w: z$ T9 ` 一种用于编写复合逻辑命题的数学系统。 + g- O2 M* l$ a( o增压泵, 7 X2 `" _/ G$ \* M* K" m" w! P- J& D从飞机油箱向总油管提供燃油的电动泵。* g* W1 g6 j( x8 M 孔探仪, - d" X( M8 S# T, `3 Y0 L' j) i/ `4 p! f4 B4 r# L, r t* s. K( a$ ?! P0 T& e! y动,以指示压 9 W; y) ~5 U9 R* }2 Y6 m托架,( c8 W0 K: k/ n( X! I 用于作支撑、装托、或围绕之用。 ' w. ~% p: K k' g& }刹车能量 , R4 Z$ E8 e+ ~; f. W- _5 m R中断起飞过程中,取决于刹车吸收预定能量之能力的0 b5 D( H2 M* s, Z, {* t6 y8 `9 z; B9 A5 h0 k* Q5 ? 通气装置, / ^0 K X# g. E8 \1 ]英汉对照民用航空词典B OEING& W" l1 [! F( o7 e TECHNICAL DICTIONARY 23 % X; v4 S ^, \& X! S; _. }BUFFET, Vibration of the wings and airframe resulting * @( w$ u1 z; N2 wfrom unsteady airflow over the wing; caused when 7 E7 L/ s- X+ V7 gairspeed is too slow, the bank angle is too steep, or7 ?7 B: m. Q: S) N/ \ irspeed is too fast.5 p0 h# A# \; G- j6 _" g, f UILT-IN TEST EQUIPMENT, Equipment installed on 9 |- o# f8 o1 ]4 l ^' o2 N/ r: Le airplane and in airplane systems to test the systems+ u- ^' Z( _, J9 } ithout external test equipment. ' [; w5 F+ Y' h* x( gUFFET MARGIN, The amount of residual maneuver ! u" Z3 P& M9 J3 i; N* L: tapability present before the onset of buffet. 5 r8 g k3 h( c( S! J/ gUG SPEED, A preselecteed speed to be observed 0 d m! z0 q/ a4 N/ p; Ynding sequence. 9 n0 M: `( [- t5 K4 ?: ]) ~k, s) ?% z# O3 R% B* ] ng landing gear operation. 0 d8 P5 h$ g8 |- E速度太慢或太快,坡度太大,均会引起抖振。3 J7 w- m2 r& \6 ?% o6 x/ b& e6 a 自检设备, , e' M2 W3 y; p! }0 @4 S% X$ X3 m安装在飞机和飞机系统中,在无外接检测设备情况下,2 T* c$ F; Q: d" h% `2 A 用于检测系统的设备。; l+ U3 a } x 抖振裕度,( U: h1 `) i K4 U3 G% b 飞机在遭遇抖振之前,剩余机动能力的大小。. O/ o) E# \$ D 标速度, 9 L3 u+ k, h% { o在某些机动飞行过程中,特别是在进近和着陆时,飞机 / Q% M9 v0 D3 c+ s预定速度。 6 _2 W6 s' z9 ]1 W+ Y$ m! U' E力装置,* W5 a5 R+ D: `. ?$ r; G V 架工作的一种机械设备(弹簧或减震器)。 . U! X) n9 W+ E6 z' s' ]流条,5 E# k+ ?9 f7 g5 L/ P- m. N 在部件或组件之间传输电、数据、或定时的单一电线或2 V# Y1 B' V3 P( A: @3 ~2 S a0 n0 o" V2 \. t, b: P B' H3 Y' I* g" z& v0 f. [3 h$ B th! t9 g, z; @2 n5 @% d1 m w 2 }* S: U% J/ o4 [' {B0 m8 r. y: i: z, ]2 b/ d2 X3 q c 9 d; p6 B4 a2 l; WB + T0 b4 o: `% {( P) D: rduring certain maneuvers, particularly the approach and 9 v: _9 S9 s6 dla3 E* p- G4 V8 T: k BULKHEAD, A structural partition in the fuselage or % v4 h7 J% o& G! U( {" j% Owing. 6 n0 D! f( g% m7 h% Z9 }8 PBUNGEE, A mechanical device (spring or a shoc 1 K6 ~4 _7 p1 |. V& g8 ]1 Sabsorber) for assisti$ L0 R. N U. L# A( E3 p- z; M g BUS, A single wire or group of wires which transfers- U$ I- s6 f$ {- b5 L* v7 h power, data, or timing between several units or+ Q+ e4 O" O s; t i' R modules.6 I8 m/ E" C1 k4 }# T+ p( t) k 抖振,8 L6 W$ ] v6 l 由于机翼上表面的不稳定气流引起的机翼和机体的振% Z) k0 n$ _' y6 I3 T/ W& f! b 动。飞行2 C7 R! K W2 F: d6 S- _6 u6 A$ ?9 C. y7 T0 ~3 `+ ^% u, e所应保持的 - N, y5 D. x7 ~ g/ f: I6 G壁板式隔框,7 b: p0 I; v4 n1 t& | 机身或机翼内一种结构隔板。; A6 i# L& [3 E1 Q- V% X1 G7 s! \& q4 F7 S4 n7 f用于协助起落' o! g' s: s8 d( v: I% f: F5 G1 t* \$ K1 E电线组。& o" V2 n# r) ]2 K0 g& x 英汉对照民用航空词典B OEING$ N* w' p1 f$ z1 q( ]: t# ^" q TECHNICAL DICTIONARY 24

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BUS DRUM, A mechanical connection with pulleys( X4 M7 E+ u" F+ t& } cables in the control system.1 Z* C2 \; Y- B8 ` and ! O! R( _" `) w& t8 Y+ fl circuits for control and protection of3 x# f- e! _( y+ I) E lectrical alternating current supply to the airplane.3 w# C6 d+ r9 A1 P# h0 ~ duct for closing and opening the duct * l+ f+ X. t2 _0 @! K' l0 uassage. ) `7 ]0 \* g/ _2 [2 [5 Y& CUTTOCK LINE, A vertical reference plane along the / A7 r0 @ d% y+ n7 Aselage for horizontal measurements of the airplane. ; Y! ?3 a" R/ a) s+ m接。 h9 \/ t q7 Y- p0 V 组件,内含控制和保护飞机交流电源的电 3 r* \5 H3 {+ ~. [5 _0 F& S/ E+ L e9 u作动简控制的转动装置。用来关闭和 " u* F! r& a7 a5 o2 w& [启管道。 ) l+ L" N( k; L, Y3 e5 D沿机身走向的垂直参考面,用于飞机的水平测量。7 P7 G. J5 p/ V- a. g" O& d BUS PROTECTION PANEL, A module (black box) * j+ N5 h7 q, A( K: Ccontaining electrica; ], L7 R# O( k# I. B1 n& M e # y+ N% J' d* _( ~ mBUTTERFLY VALVE, An actuator-operated, rotating ' z* J) s: V: Pdevice in a. o: |/ O: \ ^# z p # @+ G/ k; X- N, s: ?! s& F$ nB . u# E4 y. E" `fu 8 X# O7 b7 E' y# d# N$ ~9 b转动鼓轮,3 z- D4 ]9 M0 Y& Y5 U% ` 在操纵系统中,具有滑轮和钢索的机械式连 8 g' n7 y8 V. d汇流条防护板, * H6 P& p; y5 i1 j% [' A2 e黑匣子式的 5 k! Y" z: B, U% d% m' E- E6 x0 J H蝶形活门,* b; S2 P6 t2 W 是一个在管道中由; i" i4 s4 Q& P1 `. _' a3 t( A i9 D, E 纵剖线, ( X+ C( Z. G% ^6 Z y% X$ a英汉对照民用航空词典B OEING % e8 {; _* w8 t0 o) {+ P, TTECHNICAL DICTIONARY 259 Y8 I* E/ t% B4 p BYPASS VALVE, A valve through which air or fluid will6 `& v0 w* s4 ^+ c" n6 v flow if the normal flow path is blocked. 8 f ?& E* x$ ?, n* [7 fBYTE, A group or string of binary digits. A byte is( O/ g* Q3 }, ~) | sually eight bits long./ ~3 A" w! O- l" y6 k% B7 e ABIN ALTITUDE, Atmospheric pressure maintained1 K# c- U) |! J) x/ e8 Y8 r* I ithin the cabin, indicated in terms of feet above sea - [6 D& Q# X9 D# wALIBRATE, To repair, adjust, fix or correct the/ U0 b: }; ~+ c5 H easuring capabilities of a measuring device.% f7 i8 M) H9 `4 ^8 O ALIBRATED AIRSPEED (CAS), Indicated airspeed& y9 W. n1 y( Q3 D+ R- d8 e3 V AS) corrected for position error.0 D4 ~6 \+ p& e: k7 G! v s9 ?# u6 k nical: G5 I) R, ~. @3 h$ k: L% Y omponents.: P+ `* t$ B0 F" L1 \$ [* m8 {5 _% v, C6 e9 i 节, / J! N0 s9 d8 E. x& e V Q; D一组或一列二进制数。通常一个字节长8位。 ; \7 P P+ a: U% B舱高度,# g" Z2 E' R7 d) x' C 座舱内保持的空气压力,以海拔多少英尺表示。 ! U0 U+ X- a1 K准, 4 k7 j$ s! y. ?& P5 k修理,调整,定位或改正测量装置的测量功能。; P e6 k8 \0 n; N7 Q 正空速(CAS), . \$ _; V, |* I- Y' A在修正了位置误差之后的指示空速(IAS)。9 v; h+ f8 h' }1 D0 v) Y 用来移动机件的一种转动装置。 9 Y4 z$ U G1 O6 vu 5 ^* Q/ J" I4 ^. j3 G/ ~; w0 hC& T, e7 J0 J8 l( ] C3 a: L2 X% L9 ]( T! z w ) c7 o. t" W) W9 zlevel. ( `1 B' W& `) MC( m" J1 F2 h8 B: E m$ ~% c3 e2 o$ H& Q C e! \# \/ m8 O' D4 _. T5 m(I# t: c. [3 M2 a- [( }, Z CAM, A rotating device for movement of mecha& [3 Z- Y' T+ c4 c# V C p. O, ~2 ?& m; G) A3 M旁通活门5 o7 S: A& g- C' l9 S5 v! p 气流或液流在正常通道阻塞时所经过的活门。, s8 t+ Y) f3 r! T9 p" M- e! |' g% J; d; z5 \* s' |) T7 N1 I# E+ m7 [* p/ R, F8 ?3 p$ m3 B+ P+ f0 F7 r9 M/ o 凸轮,, h9 n4 D7 g p: ]0 z0 y( z+ P 英汉对照民用航空词典B2 ^5 s$ w4 I: i$ E4 M" Q CAM-OUT, An autopilot condition in which the actuator, D. J+ D$ z/ K# ~/ L detent piston is overridden, either manually or by the & W2 F; L9 H3 kther autopilot actuator.9 D$ j( i( z. a; W5 w& _% R AP, SEE - CAPTURE D" k* e5 i4 Q APACITANCE, The measurement of electrical energy 8 y& n9 _) R( T# b c7 [! P/ ptored in a capacitor (condenser). ; T8 K X0 O; X+ ~( B) ~* }- mAPACITOR, An electrical component of two metal 1 [0 q" o+ u6 o: m, C: U% elates separated by a dielectric material, for storing . k$ [4 E5 B r$ j7 llectrical energy. U4 Q' \ l0 |* ^( j; e CAPTURE, An autopilot or flight director function to V4 p. w: ]* i8 N) M6 t; q" k! |acquire a selected mode. ; d& q) }4 f5 Z! SCARD FILE, A container on the airplane for printed 3 g9 \; q; N+ B! @9 ^2 \; D; ?circuit cards.0 Y1 K( d) b) x# r 一自5 X- M- Y4 h- h1 ?7 b5 [ 动驾驶舵机所超控。 2 j7 H. N8 F- t' N截获,9 E9 G# x( x% s. a& T7 e t 见Capture . o0 N) m; x! t$ U. d. R5 R! k% do- f1 v/ v$ u+ I% H C9 g5 K7 q2 W6 c" P; _+ }5 i; x C ! T. r' J- ^4 Q+ V" I1 qs F( S' P6 f$ ^6 ZC$ ~6 ]5 ]. q2 \8 v- b p( Y) e J8 ~3 H6 } e 3 X& d/ z( M$ Z: w b凸轮不工作,! N- t- J! S: [7 X 一种自动驾驶状态。此时舵机锁定活塞被人工或另9 }7 H/ W. H' x8 W! r2 d7 o# \" O* X R/ ^" x3 I. K# Y6 J# S3 h电容量,8 f: ^4 s6 P; |) u" f 电容器内所储存的电能的量度。 , M+ d! h6 q \8 y0 J' ^容器, : P- E" F! | y- G& {8 c% F两片金属中间用绝缘材料隔开的电器。用以储存电能。 6 w0 A6 `, c: e; s" K" D截获(CAP),/ R3 o# r6 H. B' b1 Y 自动驾驶仪或飞行指引仪的获取选定方式的功能。8 \; [; A" B4 h8 j4 A, P 线路板盒, % Z9 v9 G( C. Y' i1 K飞机上安装印刷线路板的容器。 7 K1 s5 \1 h% v( f) \2 L: o$ y: `2 a, h% H, N: F- D4 qOEING 2 H8 ]# H2 I; b& e9 L, a; `TECHNICAL DICTIONARY 26& i4 X" g" q& s, ^% T( [9 C! E0 H" D 英汉对照民用航空词典B OEING! E: ^6 X7 A" [ R' p+ v ^" q TECHNICAL DICTIONARY 27 / f0 O. p( @, J+ {6 D G# p" XCASCADE, Two or more similar circuits or amplifying( |; c! \1 ?# a6 J T3 ~ stages in which the output of one circuit provides the 5 f; C, G% H2 g4 R1 q% L$ t$ _1 Vput of the next. 4 x6 }2 w& ~2 \% ~5 I2 G. Q% iASCADE VANE, A vane for turning the engine airflow6 h1 j b9 L7 b" q uring operation of thrust reverser./ p4 D9 k, E# X4 ~' f8 N5 y0 U5 U ASE DRAIN, A drain carrying lubricating and cooling * b% | U$ `2 b& B$ [9 p, ]uid from a hydraulic pump.3 u7 n; b9 R9 u* K% X ATHODE, The element from which the principal 1 H4 m; j: N. }2 r. otream of electrons flows." A/ A( L! n& }+ S2 n ATHODE RAY TUBE, An evacuated glass tube with a , [2 a8 m& }$ MCEILING, The height above the ground or water of the 4 ^+ g* L* z, B" R( Cbase of the lowest layer of cloud below 6000 meters 3 V- l! A+ w. n' t. h(20,000 feet) covering more than half the sky.! _! {5 M2 z3 K. j 程。该, o9 M" T8 L Z9 o; T, }5 o$ i" I$ N 程中,一个电路的输出为下一个电路的输人。& N3 Q% Z0 r1 k- B0 ?0 | 叶栅叶片,) W X1 T! J- q9 Y9 P2 G 在反推工作时,使发动机气流向相反方向流动的叶片。 - I; z) z8 R7 H: x# I匣余油管, # P7 U: K; P* ^4 Z液压泵多余的润滑液及冷却液的排放口。' I, l6 w+ E3 q 极, # y/ \4 A8 }( a' O' Z" t电子流流出的极位。 8 a# w7 r: |* b. ^/ R$ W极射线管,5 r! z M4 O% T& _* @& B 有显象屏幕的真空玻璃管。用于显示信息。 & \7 b) N) I' `1 }# i3 C$ P云高(云底高), / Z- J1 b/ v, o! s! i2 x6000米(20,000英尺)以下已覆盖一半以上天空的最 % p6 l. N+ F5 `3 Q+ b低云层底距离地面或水面的高度。 R5 f/ ^1 M5 m8 ]2 g in3 G, h$ u- r6 _( |( Z b, S3 h/ b C 8 T/ n2 e8 P) Q+ Rd: | c/ g8 S2 ~7 N6 f2 _& _- q C a3 ~2 k* U& {# q6 l fl . i: S* G0 g' u! S4 F! YC$ H9 F( I0 g+ y) o* B2 J s+ M8 {7 z( Y& \- {( j( Z C2 `" q& Q2 M* A! @* }0 k. D8 l* m viewing screen, used for displaying information.. r# N9 n- b( j$ d: b1 E 级联,# ~5 J$ i8 ]- M# u 两个或两个以上的类似电路的逐级连接或放大过( E7 @- `" }. [4 ^4 T* z! ^% L, j' b. j2 `1 |+ T- D! ~2 b2 `8 z# U' G+ z$ S' s0 S- s% D0 C, q$ y1 ?/ z* G a+ ?; u; d 一个具 / w0 y! o( R0 ?+ H, F英汉对照民用航空词典B OEING5 @, J& _9 s+ g, G- h TECHNICAL DICTIONARY 28 a3 M& \; z7 N5 p& b. J CELSIUS, A temperature scale in which zero is the7 ^: C5 S7 Z( t+ w' @8 h freezing point of water and 100 is the boiling point of : O, Z: j* m7 @1 R% Q Xwater.' e+ f# X8 y" R- `# B2 d CENTER OF GRAVITY, The balance point of an object & v9 A2 [5 z8 y1 d% Z; or rigid structure expressed in terms of percent Mean + d; E& h& D0 D) p( [erodynamic Chord or in inches from a reference point.) H6 |4 _& G* d/ f/ ^% K! W ENTERING CAM, A cam for moving a mechanism to a) d2 e. o f* T [4 R3 y* c eutral position./ S6 V& V: ?+ H3 [' J IGURATION, A configuration of the( K$ x Z( B3 v: F: ^. k6 Q& k ircraft approved for operation by the local governing ) q. @4 x' Z6 @5 Y) dgency.9 t6 w4 O5 n& ~+ {6 | ENTRAL PROCESSING UNIT, In a computer or # K: S2 i5 \: Y& |; D: migital circuit, the section containing the arithmetic and ( B: j- V7 j, Cgic,control, and internal memory circuits.! c! f$ R6 O0 v% ?% t# ~ ENTRIFUGAL FLOW COMPRESSOR, A type of3 m$ P! x/ b" h; R" r8 P+ Y ompressor in which air is taken into the center of the 0 T: `+ l6 S3 m- q! p( R) F* apeller and is slung outward centrifugally into a diffuser9 d, v6 D+ L5 |/ f9 K here it is slowed and pressure is increased.$ [# Z3 a6 Z4 A. H& a$ ~ CG, SEE - CENTER OF GRAVITY+ U9 R) V: M( i! w8 o' N. N 构的平衡点,以平均气动力弦的百分比或 2 M, `/ J- y4 X/ n; Q某一参考点若干英寸来表示。 w. v3 n' e* `7 e* \4 U I: U) ^ 中凸轮,, h8 c4 K ?. F& W: Q 将机构移向中立位置的凸轮。 : _/ u S5 b* k p; C格的装机状态,# r$ v8 X3 t6 g) c/ T/ m/ _3 j" p 由当地主管单位批准使用的飞机装机状态。 $ B2 C! u& T( n" o, D$ {, e中央处理器, ! k0 x: s$ H) M) P计算机或数字电路中含有运算,逻辑,控制和内部存 - D0 V) D/ _$ ~8 C& f* P3 [* g储电路的部分。8 I& a( n/ q' V& U 心式压气机,: z5 O* R9 d7 Y% N5 Y0 V 压气机的一种。当进气到达叶轮中心时,被叶轮离心抛! O. J* L0 V, `% F 进人扩散器。在扩散器中气体流速减慢,压力增加。' F2 `5 Y$ ]5 h: {3 H 重心,' x& {/ V! s& g$ r+ o6 r/ u$ x- s+ i 见Center of Gravity4 ]5 \# a1 p& Z) i' Y' b o+ j4 v+ w( q5 P+ e1 `% T A1 w% t& `9 {$ U% }! p2 O C * Q" ?. M p' yn ! m8 E+ r) { b: E/ k- F4 nCERTIFIED CONF L6 ?: X& n) I4 qa 3 n& w) e5 |( H( Q" ~6 G# Ea. l! z- w% F I& i C $ g$ z. ~; T( U$ F, N8 Id- j- u6 o0 D" n lo ' J# T. q6 \3 X& zC6 [2 g: {; V8 f1 {: H c) G. d/ P# w$ { S im : v' n3 l2 D8 E. }w" v L" Z0 P4 R( r* a+ ~# z! J+ t 摄氏度(°C)," v% t3 g% M1 } I 温度的度量单位。在此单位中,0°C表示水的冰点, ) X* N2 ~9 P, B* F8 M6 k d100°C表示沸点。 8 B; @' L; K% i' c( \1 B- K- ]; C重心% w) q" i: h; |& F3 K; |1 U0 R2 g; l 物体或刚性结/ M' Q v y1 t1 R. K. O4 O* w* }. A/ X- ^4 o# c! k" @- U) I# ?9 Z6 i: ^6 H1 Z, @1 s: W' ]6 {7 L& a+ S3 B4 o% c& U9 c( s6 Q$ o* P6 J$ V$ ~$ w英汉对照民用航空词典B OEING $ h) L6 F) g9 [& Q" g* s/ v3 f! L: e1 CTECHNICAL DICTIONARY 29 ]+ ?; {8 O. G# j# r5 B mCHANGEOVER, Conversion from one mode to another. ( [# I) I6 ]; }3 J9 {( o4 B9 DHARGING VALVE, A valve for supplying air or fluid to / `- f {7 \. C3 b" E; xHECK VALVE, A valve allowing flow in only one ) |+ T% j7 r$ J4 T; D5 r& F( Zirection. See Non-Return Valve. ' a- E" l* N' U+ k @% Z# W# tHECKSUM, In a computer, a summation of digits or 5 X$ I4 l+ p9 o# i* B/ ^its which are primarily used for error detection. 8 ?4 q( n) Y( \$ B2 S, e) R/ t0 K# `HIP DETECTOR, A magnetic plug in sumps of P2 n# r, y ?# ]$ A# n" S' B0 Fbricated components for detection of internal failure of" {3 u+ I) I- A: n6 d6 L: v" h e component.& {& |9 N0 Z# |: E" s2 m# Z } HORD, A structural component of spars or frames. # V8 V1 b2 |$ F1 m添活门,/ A3 |+ N/ p; k- h$ u 器充气或加液的活门。 # ^" s0 [4 P9 b& {; f单向活门,8 B5 m; T# Q4 e* R- `! {. U( A7 ? 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
C4 C$ _5 N( U5 \- u% e8 Q( [ a reservoir.) J. C. H& S+ U: I, u C ( f. {* w- F% |" xd 8 x: b; b% d, F7 j/ P; FC2 o( g+ p: V( p" ^ b! H, f' W6 J8 ?- y C " M; t) O* z! U D! w7 `0 Slu1 m/ ` S# J/ A) I' t. e th7 A Z9 I. k& \$ S# m C5 D9 {# d; ]9 t5 W/ d* E/ q3 X 转换, ?7 G4 C* \. K6 P$ z+ o7 O 由一个方式转换到另一个方式。 ! D: f; {/ |9 O8 j% R' d$ S7 W8 f2 u6 f3 f+ N: w. R4 X0 N% c2 U用来向储存8 j& Y5 |4 i4 U. d+ a) h" Y( Q; a+ M& H! B! N 总和校验,6 s! I; _( N, L% M6 U7 { ?, Z 计算机中,把那些用来探错误的数宇或位数的总和进 ; w9 I" H3 U$ t求和计算。 8 |2 n0 _$ U3 M0 S) ^9 _属碎屑探测器,9 l$ H) X8 N1 e+ A' e. f/ D 装在被润滑的部件滑油回油管路上的磁性塞子。用来探 5 w! A$ X) D8 Q8 b: _, X7 ]+ i7 k部件内部有无损坏。 0 \2 L$ }& _4 X4 x6 P弦, % E7 A2 h( Y! \7 g! b梁或框架的结构部件。' F8 f0 ]1 r) v% }+ B: _9 E+ t: y5 L( |: s/ X2 _$ o4 X. y% M, T- ?3 i# v2 S* r& c/ C1 E4 P5 e) v q) V6 \7 J5 R! T+ r/ K英汉对照民用航空词典B OEING, @' ~4 {6 {! B$ S* N) i" ~, [ TECHNICAL DICTIONARY 30" Q( v; g+ x. U' V2 y9 q CIRCUIT, A closed path through which current flows }0 f- w2 r4 v7 h! w ource. 8 U: N( x" \6 B# s- K tIRCUIT BREAKER, A device that automatically1 D* A- F- ]# B* D eactivate the system. ) x0 c. h+ N) ?/ g# ^$ q1 H9 _5 P; m- E5 ^) Slear of all non-frangible objects which % f" v. ^& h/ Y6 _7 say be used as takeoff distance available when2 s( w" B; o! n1 A, P( g$ A alculating a takeoff weight. 7 E- p& I, L& |) A5 P5 g2 n% jr water under the control of the appropriate; q; G# d6 C. F1 k. g uthority,selected or prepared as a suitable area over [/ k3 A2 |! dhich an aeroplane may make a portion of its initial6 l3 ~+ J0 B* h! K' f; f+ X limb to a specified height. G0 _- r, ^* Yincreasing.% R, O/ R& o [0 z' R sed u/ m6 j& z7 [+ T9 a/ e LOCK SIGNAL, A continuous string of pulses used for9 v/ x' ?3 ^. ?8 _- t 开关, 5 Y4 I7 l1 C& w7 f( m% n故障情况下自动中断电流以保护线路不受过电损 0 i9 o6 F' _/ \9 z体障碍物的区域。在计 . J; A7 n! y- N8 r6 H起飞重量时该区域可作为可用起飞距离。, J9 D( J S4 k( @ 是在有关当局管辖的地面或水域内一个界限明确的长 - [3 u5 ^/ x) q! u$ k; Q形区域。在这个选定的合适区域内,飞机可完成初始爬' M$ _2 o% t* I* o, _; H 的一部分,上升到一个指定高度。 ' O) W/ Y6 y' z; c飞机高度不断增加的飞行阶段。 8 j5 `& m, {# m: f2 r# g钟脉冲,7 f3 K) ~2 Y& Z4 {# t& U 步的连续脉冲信号串。 9 b' d3 Z% n4 c& kfrom a source, through various components, and back. T8 Z$ j3 {# V$ I8 Y; D to the s * H1 B7 Q* k) g% x: FC / {3 \8 n% W7 tinterrupts the flow of electricity (current) during fault- z# h) `& |/ t condition to protect wiring from excess current. Circuit2 a# c7 ^1 U6 y. h# Z6 @ breakers are also used as a means to manually T9 V) q) k: D4 Qd8 Q" w+ \, q2 X9 [8 j ` CLEARWAY 1, An area beyond the takeoff end of the % o4 ?; w" b. [) u; prunway which is c 8 k |/ [5 ]7 N1 x1 J0 Pm) v9 p% k; H. z" N c4 N: W/ n/ n& y- \8 f5 z. \% W CLEARWAY 2, A defined rectangular area on the& A5 _3 z2 `6 `/ `# F! z* c( X ground o $ n; N& W( }/ d) Q W2 Xa# u1 C( C. U$ r7 T+ ]5 a s w3 X9 C5 J1 G3 V c / W2 r+ v9 r+ m2 y% HCLIMB, Phase of flight where the altitude is " D% |& K( Q+ lCLIMB LIMIT WEIGHT, Maximum takeoff weight ba" t1 ~/ |/ z7 p9 S on a minimum climb gradient with one engine3 G& p/ _' A8 o; Y# Q6 d2 s. ~ inoperative. 7 _. x9 ^- y3 D$ jC1 G/ p9 h8 J$ J4 M' Y synchronization.* o/ w( \0 [7 M7 I7 { 电路,2 S" c+ M: A y& F$ ^7 t8 G 一个闭合的回路。电流由源头流出,经过各个元件流回 " I3 Q9 a# W2 E( @. D9 T. }源头。 8 i( ^+ ?% q# n2 @7 l6 {7 z4 Q" t5 C4 ?& [6 B1 O0 e 能在 1 h$ M' |0 v8 P( K8 V4 H坏的装置。跳开关也可用于人工使系统无效。 / E" N% y! P: O: o3 _3 A一号净空道,. ]: r* z' P. n j$ }" i 是跑道起飞端以外,不含任何刚 / j) W9 X0 N; z% m A6 x3 H3 y, S. u" V, O5 L二号净空道,6 s/ ^. |& r/ v: }. k/ \! f( ]; u5 r9 w, ?# h& f c3 P% c# r1 x) \4 G, b 爬升,8 q$ k* m8 w1 v/ l* G( t) a& M+ Q 爬升限重, 4 s1 g( B/ L. ~0 G. n$ A8 S, X7 @取决于由一台发动机工作时的最低爬升梯度的最大起 i u# p& s2 O( u/ @$ E飞重量。5 v0 f$ i& p# ^9 x' C {8 e& B# f1 i# |$ I3 Z. Z2 s 用于同0 w$ S: [$ W3 B8 P+ R! u/ t 英汉对照民用航空词典B OEING. u2 |2 {1 P! } TECHNICAL DICTIONARY 31 . \8 y8 Y1 A! p0 d8 m& _% M2 CCOALESCER, A device in the water separator for+ S% j" p* \- j; X# B3 y/ v ollecting moisture from the cold air. . T9 e) u: G$ bn antenna with a receiver or transmitter. 7 ^, t4 ^& f1 @& ~ whe cable has an inner conductor and an outer: E2 Q, C* o; t+ G# l: j8 I9 E rounded shield. 6 \" ~' F/ X' \: u4 p: Cting one inside the . g( e5 P4 Q- j. h1 @# fther for rotating the low and high pressure0 g# K3 {& u! @5 O ompressors by the low and high pressure engine ; f! i0 o% D* ]/ srbines. ' L- n8 ~ j6 P6 EOMBUSTION CHAMBER, A part of an engine for ' U1 D1 \" l* i5 p2 J# O& Q0 Iurning fuel in the air supplied by the compressor.3 S; y" D8 n* m' k7 } 置。 ) ~! o6 l' |$ Y! F* L5 `* s& c射机的电缆。电缆- M+ u) G7 W, J' o7 } 中心导体和外层的屏蔽所组成。 2 n/ R2 L* B, ^1 R两个套在一起旋转的轴。用于使发动机低压和高压涡轮 / P$ s, Q0 ]' a1 q2 S1 L别带动低压和高压压气机。 + V. l, _* q" c# b$ i; e, @. h烧室, 6 @" k- W3 |. J" u5 ?& S+ v7 Z+ V发动机的一部分。用来使燃油和压气机所提供的空气相 5 @3 E8 C0 M2 D4 F+ W合而燃烧。

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发表于 2008-12-24 21:38:35 |只看该作者
c$ S* k) H6 T; B: i7 w( C! ? COAXIAL CABLE, An electrical cable usually 3 @( \7 b6 q d0 i: vconnecting a 9 b/ V3 L/ J; `$ _9 [# wT0 l! @. O7 `! _/ T7 z3 K g ; r' b8 s; l [9 N( `9 ^9 JCOAXIAL SHAFT, Two shafts rota) l2 g2 X8 Z# p- } o 6 ]. q$ v _; g: {c, J) K7 H/ ]9 w tu ; i9 d9 {- W1 L4 k# W9 LC , W" G) Q8 o X5 Ob % b! p5 e7 B# Z凝聚器, 8 I& k" Z+ q: r# S( ^5 n水分离器内收集冷空气中水份的装9 j" d" R2 u! w$ F 同轴电缆, ' d5 |/ ]6 {8 k n一种通常用来联接天线与接收机或发- B9 F* c1 h3 L+ I/ T% a- x& m* ~: g. C) C! S4 [8 t; E& f同心轴,2 U8 D8 P0 u: L* }1 \. J% o3 ?( ]. N9 d& w& o1 [% U& `9 Y! U) D2 t% t6 P- K9 O% b0 y, }英汉对照民用航空词典B OEING1 L: l; U' v; g1 ?/ U6 z TECHNICAL DICTIONARY 32, B+ r' a$ B3 t COMMAND BAR, A flight director pitch or roll comman# W' r# l( }5 }5 j# V* G( C6 B0 d- D indication. # q, ^- G* I, e6 w6 h( ud6 w, B* X( C5 ?7 B4 w OMPANY ROUTE, A route flown by the airplane 7 y9 q: p1 l" `2 l8 Z2 ~OMPASS LOCATOR, A low power, low or medium 6 g' [9 n u6 V6 j8 Qequency (L/MF) radio beacon usually installed in + ?+ S; v a3 V4 u9 C$ m& n% J& fonjunction with the outer or middle marker of an 0 L4 U+ l& V3 X4 J1 F7 R X- {tor (LOM), A compass # p9 i+ b3 }, flocator installed in conjunction with the outer1 p1 f/ F6 [0 _ marker of an instrument landing system. 6 P- O! [& E4 F6 V. h; Pss % w F: U1 U- J3 n" G0 Y1 Ble( E" n1 n- P( [: s OMPENSATION, To offset, balance, or counteract.4 K$ C, B5 D% e4 u+ T! X1 N( Q OMPENSATOR, A dual capacitor for changing the fuel 0 K3 H% m( h+ v0 A$ Maging circuit capacitance due to changes in fuel : D) g, `8 f1 E Pensity.! o& g7 t" [, T/ D, U) u OMPOSITE MATERIALS, Non-metallic materials used ( a; f( X! b5 z- F2 x5 xr airplane construction. Fiberglass, Nomex, Kevlar, & ?" I, f: F4 Y& `+ D2 ~raphite Epoxy are composite materials.* s, h Z0 k( g# Y 司航路,& O: \, K: ^5 `0 _ 在飞行管理计算机数据库内由航空公司飞行& g+ O6 [ h2 v! \/ L. i( h5 t 盘定位台,& ~, S) y* t6 V1 q 与仪表着陆进近系统的远距或中距指点标配套安装的 0 `/ }. S; {0 K+ [功率、低频、或中频无线电信标装置(低功率NDB台)。 7 @- M4 P* K' [. c7 |8 G. F程序中用来导航。; ^4 @# n5 T" a, R4 }# H 1.远台, + g* y8 l: f( ]与仪表着陆进近系统的远指点标配套安装的罗) ?% m# E9 V- B- P2 Q 盘信标台(NDB)。 3 s& H$ u, L; O+ |4 F5 K; U+ d, U$ a1 m偿, ; k* `: c. f" s' }- z抵消、平衡、或中和。 \6 A8 u8 L' F; c偿器, 5 H5 R9 `3 c% x8 P. y在燃油计量电路中,用来改变电路上的电容,以与燃 # Y; x1 ]- J% i# @ b$ Q密度改变所引起的电容改变相抗衡的双电容器。1 ?3 M0 L9 z* T* y 合材料, ! j: x7 I- e X6 K用于飞机制造的非金属材料。如纤维玻璃,Nomex, $ ]$ o9 R& z5 G& r% Mevlar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 * i8 b Y/ J) q, _" v" m. ^; ?0 Ioperator that is normally stored in the flight# z# ^" e. D) M8 p management computer's data base. 5 w( ^% D: e+ m3 aC * s8 }9 A) L1 i2 f7 @fr & `" F. W0 q* F# T5 F, Kc3 U) x. z4 w8 X/ p instrument landing system (ILS). It can be used for 1 u+ C# S) q% y# |navigation as authorized in the approach procedure. J5 I' w1 p7 R& q' Z6 Q* A" {3 Z1. Outer Compass Loca! d; i; _' q+ D+ ^7 b: Q 2. Middle Compass Locator (LMM), A compa 7 b+ q( Y- `4 s' c) Zlocator installed in conjunction with the midd * G" T# u5 d! i6 h% s* lmarker of an instrument landing system.. C/ o; W* Q8 d* {9 W! F* |/ A C ! n8 a& p( {% w2 d" j* i( S |C; e9 @; R+ L; t" f6 l% ^ g# f3 C* p( u- \, n$ ? d# ?8 D' [) k# `6 k: \, v C4 W- y8 c# m* j fo8 w% z1 @. i+ h- o, k; B g8 v1 p3 W$ ]* Z" D" Y3 V" e8 z 指令杆, " f1 N! r0 o; c, h6 x8 g飞行指引仪俯仰或坡度的指令显示。, g6 k4 h" g- w3 \2 R+ Z& C. f! |. q& S, V$ O通常储存" x+ R% t3 h- t+ g 的航路。 / Z$ L( J: }5 f" i8 U; A7 B. Q/ D- Q9 o: A3 I t0 S$ T6 U# b/ L# A, w& d8 N0 ^7 V, B- m 经认可后在进近* M$ Q3 K3 }) q 2.中台, ) W4 p/ @: O5 j. t5 ?与仪表着陆进近系统的中指点标配套安装的罗1 y! g$ L2 s6 x 盘定位台(NDB)。 " }4 y1 l+ a! r, v0 W/ Z2 o- p, b4 D# Z z1 T: ?8 A9 E1 Q: c0 a4 X% u! T3 f5 c& m4 ~% W9 v8 F2 u, F* ~: l- k1 X+ u* x K $ z8 e1 ]5 p2 |7 j- n/ g英汉对照民用航空词典B OEING & M1 F( a. O. N0 m: ATECHNICAL DICTIONARY 33. T8 K$ U9 W8 T0 Z by0 P9 n: O* h& |: r0 L9 U or increasing air % k9 l) C8 [- d- r6 }ressure and temperature before the air enters the 7 w+ |5 z) U2 Z" _. f1 R" q& w' mombustion chamber, Low pressure compressor - front8 [0 m5 b5 ^, C2 [" y ection of compressor, High pressure compressor- rear9 @ R2 L9 g( l8 H/ p O OMPRESSOR STALL, An event that occurs when * Y4 y' h) l8 m+ J; U# b! oere is a complete stoppage of air or reversal of air flow0 _! F6 V% ~4 I: L COMPRESSOR SURGE, SEE - COMPRESSOR ! [! h+ h% r9 w! s! i7 ~5 ?STALL COMPUTED AIRSPEED, Indicated airspeed + E$ _4 s& F) Mcorrected for the static source error./ e& o/ h- m" P& b) E, _4 ] 的机械轴来驱* `- V( R" E0 ^6 f3 o: G+ [8 W: y* A ,用来增加吸进空气之压力和温度,以供燃烧室使用。! t) e* t; G' [: m 压压气机—压气机的前段,高压压气机—压气机的后1 e7 x; B- u5 @. C2 B* p* ? a8 k' G( Y 气机失速, 6 i/ t( |; B/ S( ~当气流完全停止或通过压气机时气流方向逆反的一种 : e0 G$ R# ?+ Q1 y. _5 e. k# M压气机喘振, 4 O! g$ ~' e( J" L见Compressor Stall4 M3 i1 ]( r) D/ n0 M& H8 K) \ COMPRESSOR, A rotating part of an engine driven - E7 `! G' Y$ Y) q3 J' fa mechanical shaft from the turbines f ; P2 U6 O5 L2 A' V# Yp - R1 P" b& ?( }' Tc * O) o: ?0 e. a7 k8 [7 a0 K! E+ m! ms 6 L2 T9 M( c5 W2 [section of compressor. ) D8 _3 _) b+ W6 f/ _ FC " _' e8 { D1 b$ e/ a; ]th ; p' j* O/ w. _3 {# ?9 K6 Zthrough the compressor. & L$ s: B& ~# t- X压气机, / c; l# ?% u6 C7 N3 K发动机内的一个旋转部件。由与涡轮相连 4 a% W x( A+ X; W! f9 a. m* R+ k" R3 f- h6 S1 E0 e1 @$ c+ O; M" ~, W$ z% _( W: J' q6 u( \- S% o8 m# j; A5 N: S' M 现象。 " ~- j% y# d1 _# l, ~6 L$ _+ W* \9 v' q 计算空速, 0 K/ s& {5 N2 e修正了静态源误差后的指示空速。 ; \% F M$ I. p) a4 H英汉对照民用航空词典B OEING ( X7 L) a* B7 X+ f4 FTECHNICAL 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 7 N8 K# ~) l$ t! c) Q noperations, manipulates data, and makes decisions. 0 R% k1 Q' P9 j+ T- cditioning3 O; H! M9 L% h; [0 q, h4 o O' \; G the air and the * O9 L" i v$ A* x; ]; o9 Pfrigerant or moisture vapor is changed into a liquid.* j$ E" n s. U' e# W+ r6 q# L ine * X, H2 x; ~. P1 V0 Q2 k1 h+ aONFIGURATION, The position of flight controls,; a1 S4 l% R- b" b# C missing which! b$ m% R8 \7 ?+ g3 Z% [8 e0 W may affect the aerodynamic performance of the% a0 b5 ~; |+ D+ w7 D) J airplane.% L' J4 Y. k/ t; z. m 置。2 g( u; d8 X4 r6 ? 中能使热能散发到空气中,以及使冷冻剂或湿 7 [5 W5 P4 t% U0 G2 l% h" o6 i4 ]转变为液体的部件。9 c0 z7 e! R2 L a8 i0 o# M, {* f 连接到飞机结构上。 / |; k' w9 e" U; @3 N态, w" C/ `8 r) W8 }9 k, t 定飞行阶段中,飞行操纵面,起落架等的位置。. T. t2 l& f9 l( Y2 I/ g ),$ @; X+ C( Z# [ _3 v" p$ u* u 受到影响。 ! H3 @& i3 F$ nCONDENSER, The component in an air con - W. w# W) M; ^) ]( ~system where heat energy is given to 0 Z/ i1 J* c! }4 N* Y- Xre & r% \- a- Z* a: C( v: G YCONE BOLT, A bolt in the shape of a cone for eng , f! B0 [) W7 g1 F* K: r& }attachment to the airplane structure. % \$ Q& ~$ s! b; eC, R1 L2 B i: ?, N# r3 g landing gear, etc., for a particular phase of flight, e.g.,0 x2 W1 y# q- A+ ~0 n* D- f5 D Takeoff Configuration, Landing Configuration, etc. ( p" ^2 D. d oCONFIGURATION DEVIATION LIST (CDL), Appendix0 I/ l) ~ I; t+ Z" H8 S in the Airplane Flight Manual (AFM) allowing operation : u6 y; X( a# d2 bof the airplane with certain airframe parts 3 g) e' m7 A- T+ H% f' L计算机,/ f- L* s/ M9 { 能作算数运算,数据操纵,和决策的装 ; `; }" L/ @/ C2 K% j+ U冷凝器,5 E7 d' s9 j. Q 空调系统 7 z+ ^7 |3 O+ m4 D$ D7 g( g' B2 h- [* ~9 Z$ f 锥形螺栓, 0 s+ U' ~/ s7 [4 m外形是锥形的螺栓,用以将发动机 5 w# c7 C5 ?" F2 W H2 r& {9 f8 O! V) Q# J) ? 在某一特 : r2 e, G' S+ u# |1 i+ K如起飞形态,着陆形态等。1 c/ C2 |. T7 N* q: ? 缺件单(CDL ( B9 f D- B" A$ P飞机飞行手册的附录所开列的飞机上某些零件的清单。 2 M) A" j' L* h4 x, O9 f在缺少这类零件时,可以飞行但气动性能可能 - J. [& E9 y9 G6 n; S' w) |英汉对照民用航空词典B OEING" b f% }/ k+ p3 e+ y 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$ J" A6 w* Z; j" e component for changing variable engine gearbox speed8 m# G8 ~4 ?+ ] ONTROL AXES, The three axes of the airplane which 2 H+ m- R O4 e" S" u8 @ u% Are perpendicular to each other and pass through the4 C8 O/ z( ^& P2 ~0 Q9 [% K enter of gravity of the airplane.1 c1 {) z& C% W/ ?( t Pitch axis - Horizontal or lateral axis, passes through , F! b* q u% v0 c) Kthe airplane from one side to the other -( z% a9 s. T$ h/ a- E2 K- k* k nose up and nose down control is by, D z. g6 O2 K elevators (and stabilizer for trim). # a1 b1 F; t" ~! b) [ T; lRoll axis - Longitudinal axis, passes through the7 M. @( B8 l% ^3 o1 ^; g airplane from front to rear - wing up and ! D' I6 _& z) S/ jwing down control is by ailerons and1 b g5 o. P% o* t: [$ I. x flight spoilers. ; K( n4 f% W4 {9 l: b4 d0 mYaw axis - Vertical axis, passes through the 8 K( w$ i$ L6 @7 Z# b( X5 ^* Z3 \1 q8 @airplane from top to bottom - left and4 a2 u2 L/ S* i7 Q2 a& `) {4 i. w right control is by rudder.( v. l' U" j) C# | 置, * [6 w, r- | H/ T9 O制轴, - ~' z4 U( V3 u通过飞机重心互相垂直的三个轴。( B- P9 z! _ p8 s 俯仰轴—又称水平轴或横轴。由飞机的一侧通向另3 i# ~, k& ?1 S; L* m 侧。飞机绕此轴转动即造成机首的俯与仰$ |3 D# n. t9 z4 U8 T 俯仰控制是由升降舵来达成的,水平安定3 q# V# |4 y) {2 z- }/ y 则为配平之用。 - X. O- K& l* S4 i8 m. T" W# p横滚轴—又称纵轴。由飞机的前部通向后部。机翼 4 |7 `8 e$ p* d2 W" n, r9 f下运动由副翼和飞行扰流板控制。 + D+ n# ]' n7 @& l+ T偏航轴—又称垂直轴。由机身上方通向下方。飞机 3 H. ], A- u9 [此轴转动即造成机首之左右运动,此一运 q& e4 d/ h; ]) r& t9 N 由方向舵控制。5 D+ I; T j$ T$ X) N to constant speed to drive the electrical power.7 C. e, k( r; h. K0 a C% ~- i, o) T* K# n! C' I! D$ o/ _ a 1 ~3 s7 w/ S# ^# e* T0 k! v5 jc5 `# m7 v2 i2 @8 P+ ^: V6 r 恒速驱动装 ; [- {: f0 d+ g' d' k将发动机齿轮箱的可变转速转变为恒速以驱动电源的 * n( S6 W3 m) [' J- T+ p液压机械式部件。 9 E7 l3 v( I! x. N( @6 k S& [! f; A/ R3 P9 B ]' K0 R7 N7 z, w7 v; c, [- L1 Y! g& Y3 g- j: `/ B6 P/ O3 s6 P9 M- q9 P! q! |8 g5 H* z' ~8 w$ H, w) \8 v0 V" J8 L* {- H8 g英汉对照民用航空词典B OEING* z2 F: ]5 @+ K) f" x# ? TECHNICAL DICTIONARY 36+ X$ F# H5 [- n CONTROL COLUMN, A mechanical component used c$ Q2 D3 f$ D+ [ Yrs9 \) {, l; B+ P8 B1 K$ p nd elevators. 6 r" {0 v# A0 v9 A, t4 Q& bONTROL SURFACE, Moveable panels on wings and & n, F$ m. |: Y! [il for movement of airplane on pitch, roll and yaw axes.% O. P# p9 j( u- ` i; m ONTROL TAB, SEE - BALANCE TAB! a5 Q" _# g& a- W ONTROL AREA, A controlled airspace extending ! G8 @3 w+ l8 [8 @pwards from a specified limit above the earth.5 j& Q! R6 J0 A# B ONTROL ZONE, A controlled airspace extending . g2 e! u2 T: j8 Z- E& p! jpwards from the surface of the earth to a specified" L* Q- F% A; N* z pper limit., j, P" U! a' A8 N is , e6 j: K9 U/ u; O6 b7 |o IFR flights and to VFR flights in accordance0 m: Z% p! r# P9 |8 Z; m with the airspace classification.& o! q/ x+ T6 s w* W+ g' k 机械部7 e& T9 C3 k3 y# E* c1 z6 E, r4 y& L2 J7 [操纵面,, k, E' d+ C/ E) Q& K. m 机翼和机尾上的可动面板,用以操纵飞机俯仰,坡度, 0 h" q# _ L* F. j) x @和偏航运动。3 p+ b: ?7 a8 |" s- }2 x4 }$ \+ p 操纵片, ) T3 q% a ^0 o& b; d' l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( m8 S' x6 {) T# x! {- q a 2 v, J; @- o: `! c/ Z. O$ b5 g& uC / B4 l3 u; t- H: @( ^ta1 s5 `! Z* r& ^ t! E C % d/ p9 A. ~) l% |3 K. }+ WC5 Z/ g- R: [9 g2 u' Z, e u # F6 B! ~5 B9 s$ ]7 u/ l/ f3 _" {. yC; a4 M9 |& L9 w u % z. k" o6 }0 n0 _u 5 |3 i( X9 }' }/ g( d XCONTROLLED AIRSPACE, An airspace of defined 8 [$ [* O4 y# q6 ^dimensions within which air traffic control service 5 |" P' L( q f: h4 ]provided t 5 Q9 \1 z# e9 |2 s+ E& b驾驶杆, ' u- X2 s/ e. P0 v9 q9 e飞行员用来操纵副翼、飞行扰流板和升降舵的 7 O7 J2 M! X$ ?0 [- p; C5 V% y1 k% X1 I% n- G( j# e! h4 M+ [' j. j; t" g 管制区域, 7 R5 n) K& r7 W. @; I, B高于地面的指定极限以上的受管制的空域。 " n& L, G0 Q6 F) W9 q制范围, ; g4 b" G4 b% |由地面到指定的高度以内的受管制的空域。 8 a" G( x/ L% j9 T# {+ _一个范围明确的空域。在该空域内,仪表飞行规则飞行 7 i- ]" S. F" s) |' V* o! I和目视飞行规则飞行有空中交通管制服务。( `3 E" l6 Y6 V" k+ x' s0 H2 v3 ~: I6 C 受管制空域,5 m$ X- j. }0 ]( t2 z 英汉对照民用航空词典B OEING $ O( N+ e$ i% U* ^( aTECHNICAL DICTIONARY 37! }8 d, ? J. w CONVERSION, To change into another form.3 X' g5 W0 N' r- c2 P# P COORDINATES, The intersection of lines of reference, 5 T$ y ]3 p }sually expressed in degrees/minutes/tenths of minutes - b6 j& x8 |9 \& W/ C$ T7 r9 Tf latitude and longitude, used to determine position or / ]/ V+ h( D/ `8 t- O) c, hCO / ^7 E4 {/ I6 M2 edestruction of th 3 j' U; E: ?9 f; vchemical conta / Y. _5 e: v" O( L+ [COWL, A remo7 `& ?' ]2 o# z3 C, I for access to th ) ^' U3 o5 h6 T( u; CFa6 y @* o5 N' B$ r; ], q" W- _ Nose Cowl - Front section of the nacelle for air inlet& X) ]2 P5 L j$ D* I" u to the engine. ! {4 v9 Z# d; }" K/ d& M) Z0 rSide Cowl - Cover around the sides of the engine. , H9 N7 ^% f; k: yThrust Reverser Cowl - Cover around the core , U: O: M" M, ^: Vsection./ R3 ]$ G! H5 |# z8 A5 S& L$ c Translating Cowl -The moveable outer portion of the . k2 y% n6 f, _ }9 s; p7 Xthrust reverser cowl which is + o+ e! [# }- v7 ? y: O% i7 ooperated during reverse thrust.6 g* ~7 e6 o# A. Y8 n$ ^! L# {; K 标, # h9 B2 v3 l4 j# }+ ]5 u" ~基准线的相交点。一般以经纬度的度/分/十分之一分 % b& W; g0 X/ F7 v读数来确定位置和方位。 : t3 E/ }/ l! w腐蚀" T9 x; v8 k" m7 F 动机外部可拆除的罩子。发动机上的构件必须要取下- x5 u/ ]* @0 `; M4 m4 Q0 h 流罩后,才能够到。7 Q" x. J$ h0 s! T* t8 u* k1 P. C, B* _9 ?0 u1 Z- R 机的短舱的前段。 - w6 a" C3 p4 d* h0 [" c B n. u* `; r侧整流罩一发动机两侧的罩子。 7 U G$ q1 ] K反推整流罩一发动机主体外的罩子。/ w' P( g: x8 y 移动整流罩一反推整流罩外可移动的部份,在反推工 + j0 u& y, Z7 z2 l9 s3 x作时使用。 8 l1 z1 b3 a& x; Xu+ E& p% }$ _. @ o7 D/ @2 i0 s. M Q8 I6 B5 q/ b location.9 ~4 H7 {$ E$ m; d2 K% R RROSION, A chemical action which causes gradual : l% B5 G( C1 ]0 R4 F( G2 X6 y- `e surface of a metal by oxidation or * s' S; J6 `" Mmination.1 p7 k. Q2 D! u6 v vable cover around the engine sections1 V! E3 L! Z8 y' ^' G4 v! A e components on the engine., h) h, R; f, {7 n1 ] n Cowl - Cover around the fan section. 2 w* n) ^) Z; n1 |: }转换, P0 ~( k0 M! F# c改换到另一个方式。! g6 k' m+ T( o& Q! Y$ ]8 N+ z. v4 H2 Z$ \# a9 s! E2 O$ {3 Q$ {' C, y% D- H1 L2 Q) O; V2 Z2 r5 G 氧化或化学污染造成金属表面逐渐破坏的化学反应。6 I, Y' r" \/ Q5 d/ O$ D2 H7 M 发动机整流罩, , H a$ Y/ t3 L8 } }& _9 @8 n2 P% A' j, M5 i; i$ ]4 p9 C( e/ K3 K3 O( n4 k扇整流罩一风扇外围的罩子。8 ]+ Z0 s% R( ^ 前整流罩一引导空气进人发动 3 B- r5 R* O0 p6 g7 Z英汉对照民用航空词典B OEING 8 c+ F6 Q0 s; r O4 ? h# aTECHNICAL DICTIONARY 38 0 y! [+ w7 a g. p5 JCPU, SEE - CENTRAL PROCESSING UNIT5 I$ f9 d2 p% p" y' ?& k% w7 l CROSS TRACK, At 90 degrees from the desired track' n% r( s5 ~0 V) Q f the airplane. For example, cross track distance is the9 q& _+ |* g+ X: I0 k- b3 W7 l: F! } istance from the desired track measured 90 degrees - m5 q! s* T7 q( [: zom the desired track. - r' `+ n7 {/ y) p0 S6 FROSS-CHANNEL, Electrical wire(s) connected from - D; q D) w: `' Une system to another like system, for example, FCC ( u1 ^6 p3 [. K: b5 q' p- n" to FCC "B".: L& P0 M/ R% H" {! T, T& q. y* n n adjacent engine or one on the other side. % M* }, |3 `0 i9 V `l crossfeed& ^: G" p# z9 _' h anifold for fuel flow from one side of the airplane to the 0 R, S, e/ _: M% m1 ]ther side.. ^/ o' {+ i$ V0 [4 c* O re. w% j& i9 I7 ^$ f- |- y+ @- l RUISE ALTITUDE, An altitude or flight level " [5 S& }; u: \) W8 |" F5 p2 [- a0 j `/ w5 V o3 a4 s' ^1 Z- [; g+ Z d( J0 e j B# }5 }# t' K' D fr + S6 C/ S$ h: X3 |4 H y$ B! TC , H6 s. j: x7 \* i& uo 5 M W) E( X! h6 L2 H) o H"A# A, [, y& e& u1 {* d) J CROSSFEED, An interconnection between fuel3 M$ [7 W1 n( J2 h9 H, Q manifolds for fuel flow from one side of the airplane to& i4 v2 |, \; e a 2 f- u* v8 n# Q" ~# P4 lCROSSFEED VALVE, A valve in the fue p* b0 t" ^# A$ N3 p. a m% T4 v* ^& Y" {) }& } o* P8 r' j# E9 Y1 r# m5 T CRT, SEE - CATHODE RAY TUBE# D: O* I' n. j0 q CRUISE, Phase of flight where altitude and speed a / I* ]8 E* O! Gbasically constant.' ?7 N) H; U( F& x' u C + S: H9 U. x2 k4 U# I$ \: tmaintained during enroute level flight. + | s# {, s4 R' b" u! a" i中央处理器) V5 O/ K6 c' p5 H 见Central Processing Unit.+ T8 g+ a8 w8 m; n/ Y 交叉航迹(XTK), 5 f. J& h% Y( R# r4 n与飞机预计航迹成90°角的航迹。例如,交叉航迹距离 ! |3 {" n- y: Z) P4 u是用与预计航迹成90°角量取的到预计航迹的距离。. y" D4 { z1 j 通道跨接,8 p |8 j P% t 电线由一个系统接到另一个类似系统。例如:由FCC 8 x6 J; `3 a" s" e0 ?1 ^* B7 U( w“A” 3 |1 d4 a: Z! v! `& R! v, Y/ x接到FCC“B”. o. ~9 b5 w: q0 X% ? 机身另一侧的发动机。 E E7 w z; h5 a于使燃油从飞机的一侧 / c" h( h' _6 t E9 R向另一侧。" h+ c d& I3 Q- X6 k4 d 见Cathode Ray Tube7 ]& a3 `4 n( [ S7 P% f 交输, 3 ^! d; @# M2 [% `* b) I5 c燃油支管之间的交连设备。可使燃油从飞机一侧流向邻 3 k) O" |6 R& F( F! A% A近的发动机或在3 b6 L( t: K" W7 I 交输活门,1 ?1 `4 `% n- d7 t 燃油交输支管内的一个活门。用 ! a/ @$ f6 S6 m, y( ~, \: x% w4 X- W3 _/ e. }阴极射线管, ! ]2 ?1 ^. U. r9 {, p0 l+ k. - ?2 p1 ]# I$ c! s5 O* U# b阶段。) P' G/ ^/ D$ Q 航高度,9 N* Y( c5 M) `. A 飞行期间,飞机所保持的高度或飞行高& g. | X# J/ \* ~ 巡航,( \7 L3 R+ [( }" k( T 飞机的高度和速度基本上没有什么变化的飞行( A2 x4 B# t/ e0 W' Y# \& O& d' v! |9 B2 j( Y* `1 M# G( x6 S 在航线上水平3 G3 L2 z; ^& p1 g) t 度层。 1 u, a7 [9 Z! N2 w# e% W$ g1 p英汉对照民用航空词典B OEING 4 |% b% T! d$ Y" R8 m* o9 hTECHNICAL DICTIONARY 394 O$ t5 O Y& H$ S; R CSD, SEE - CONSTANT SPEED DRIVE 4 f7 O0 q5 E; x9 UCURE, A chemical change which takes place in a resin, Y) ]4 w. ?) y: b and fiber based component causing it to solidify. + \% N6 l5 E' O4 k9 q4 ZCYCLE, A complete series of events that take place U) t' e: ^' r" k0 f% u& r$ g# x+ }gularly normally in a continual sequence. ( }1 H# K3 z ]) o/ B! tAMPER, A device for slowing down or limiting1 Y w& O8 I8 }6 {% q8 K) H0 S3 w DASHPOT A mechanical damper for slowing down 3 [+ @" Z, |( c: l L- qovement by restricting fluid flow.8 {" u, U5 J4 g6 S8 y6 Y D 2 o1 |" I, N2 Q. R1 ~! [9 X) yATA BASE, Stored information which is used as the 1 O8 l6 [* ` v- Zba0 ?2 f; v* d+ [ c DATA BUS, A conductor over which digital data is . 8 v: w" A. B( m+ j7 Vtransmitted. ! @; s; ~" p/ x H1 p4 z. NDECELERATION, To decrease in velocity. 6 S, P5 f3 \ q* H装置,8 ~$ L( p( c7 \" D! Y v rive/ D( E$ \+ L6 v1 F$ ?8 Y% n re + G/ G; g/ Q& h Y6 z' }, J) WD ) E4 }& m' p1 WD- T6 [; H3 A9 d8 v" J8 o0 I movement.' j3 F! K+ ]3 J( s, C m 0 f8 W* P& U6 ~& Y; h8 F2 vATA, Another name for information.& P# _! l5 e O) f D / n5 v2 @1 v" [! U* isis for computation. 5 C w: W% @# a1 f1 R' K恒速驱动# ^! z1 R: l& T 见Constant Speed D .8 o1 t% Q* _( _2 y4 P( W 期, G% A' Q. n9 Z) p& x不断重复发生的事件的一个完整系列。 4 \% u% `' q0 I: v* _! g1 A8 g( s$ Z尼器, 7 L% ]! ^! O, \" \' Z6 s7 @) R慢的一种机构。+ j( G/ U7 X& [+ |( z' @% n$ i! _9 ^, r1 y用限制液体流动的方法以减慢物体运动的机械式阻7 l3 U- B4 r. g( J' j; @3 ~+ C# A/ P* _ N- X0 L. y) _% }! y7 `$ B; i; T 料的另一名称。+ \5 f( S1 K- y0 Q 据库,6 J4 D$ K/ ^, P3 t8 Q 数据总线, 9 U( u G9 P. [( y- m; \4 p- r一条或一对导线,用来传输数字信息的通道。7 F- y5 s" G2 C& j$ e2 D; a8 F" D/ B 减速, 5 M9 G9 f, C p) R/ q! t$ ]+ Q: ^速度随时间的递减量。' g. L9 }5 }" j9 }* A! E: {3 B; ^ 固化," y0 R! `) T6 C. K1 F+ \ 树脂和纤维部件内化学反应使之成为固体的变化过程。 ! `' H" Z& f( x8 Z+ }6 H2 p* c. R. w6 } a+ y D. X" M& K; g: \$ ^ 用来使运动减" O1 }+ Q1 B9 Z5 r 冲器, + U" r- n1 E7 \1 E器。 : p4 N4 u; e9 C0 d& X' Q3 y, L% P据,5 p, H: ~; U2 U% G6 S7 m, I5 k0 k3 N; s1 M1 M* N! F" d: g8 k5 R$ ^; V0 o4 V储存起来以便在计算时使用的资料。 ; e* C& O8 x/ r& S% T英汉对照民用航空词典B OEING 2 q/ j2 R3 S6 q' X4 I$ xTECHNICAL DICTIONARY 40+ H3 L* J9 J, K DECIBEL (db), A unit of gain derived by computing the 3 B$ w( \: [6 M0 G3 Ltio of input power to output power.5 m. }8 |7 j9 f) z( w! ~8 i ECISION ALTITUDE/HEIGHT (DA/H), A specified 3 Q. ^+ Z; Q6 g! a8 ^. }( J, oltitude or height (A/H) in the precision approach at 6 A7 r7 b/ B- P% _3 {) [+ phich a missed approach must be initiated if the % u: ?3 m( a+ r& x# qECISION HEIGHT (DH) 1, With respect to the6 g! Y6 }( ~0 `& p! R* { proach or F7 l9 T+ |) a0 [( ?, ` execute a missed approach. - {9 N1 X- E" t6 Dproach to trigger the decision of either ) F: c- {# N pnding or go-around. ! i; A E7 ^. R5 R8 @8 IECOMPRESSION, The loss of internal aircraft air " b) _# y! u7 h+ r1 J* H9 M4 @ressure. ' S( e5 R1 ~: O, F6 \8 NE-ENERGIZE, To turn off or cause to not operate. ( Q+ S; [* g* t1 B" i" {rom the tanks5 ?0 D/ O) |5 a. H+ \- G/ ? using airplane fuel pumps or external suction.9 I& n9 _) j* f1 _4 J; Y 算的一个增量单位。分贝: p" j3 l& y* g 常表示两个声音信号或电力信号在功率或强度方面的4 `# j7 w6 e6 F; Y1 g9 s1 k 对差别的单位,相当于两个水平的比率的常用对数的十 . x) A0 ?5 d. s5 h) R _, g& i/ E8 c断高度/高(DA/H),2 i, u8 Q# m6 B& D4 m2 {% c 在继续进近必需的目视参考没有建立的情况下开始复 4 e% Z# c: Y4 B9 C) m$ K的精密进近中的一个指定高度或高(A/H)。 7 o/ r2 b! t# ]% k3 b断高(DH)1, / W) T. p" ^& t% f操纵而论,指在使用仪表着陆系统或精密着陆雷' p+ E* g7 z& L i f4 g$ l 生继续着陆还是复飞决定的高。4 Y+ z9 {& [4 w* M: [( m; l% [ 飞机失去内部空气压力。 ' T; C$ Y& q L m; {开,) d; c* y8 K1 l4 w 关断或使不工作。 ' |2 X5 v8 o; F6 L机的油泵或外部的吸油装置将燃油从燃油箱排4 y) m @, w% S& e 出的方法。 1 g" r# T, z' r9 Y- k8 dra 3 U' _0 K& d9 |D , q! ?6 @$ g2 C$ d' }$ Ma3 X3 M* H3 E& g& o w' R5 ~: J, e0 e/ X, x* v$ F( T& O required visual reference to continue the approach has, c9 F) Q# H( Q- ]( K- }% V not been established.9 W# P1 |+ G1 T7 Y! \: N6 O D8 W8 v# V4 ]( a' d operation of aircraft, means the height at which a7 a& T- M5 b( r9 x/ q! w1 K decision must be made, during an ILS or PAR6 p4 T# T( J% Y/ |" ^ instrument approach, to either continue the ap # [8 x0 d1 R- c) K3 Dto/ B) W" O! ]& W. [* y- P' w: ^8 X DECISION HEIGHT (DH) 2, An altitude used during a . _* D4 e3 @- F! z, Eprecision ap) e8 b! @. k* J6 I3 H+ x5 h la" C5 R! K4 [; g D! j8 g( Q N* _3 p1 y3 \( q/ z) @ p2 G: K- R1 W4 f& L; S4 d D 4 g" S% z+ ?" s4 I v O# L( w6 S# Z# {" eDEFUEL, A method for removing fuel f ! N8 K# C9 J/ z% k* X2 d' l; o分贝,) T$ X: H; }, Y; @4 R 以输人与输出功率的比率来推; z- C6 ~! j. `2 X. X+ c, z2 N7 a% e# n: r6 O! y3 x/ U. G7 O: _( n" o0 ?' R0 ]$ `8 B; ^3 P) ?& W7 A7 }# O" e" q; _9 F$ @6 S2 Z4 |- L7 ?% M, N( Q 就飞机8 N" {# @# t* H$ C7 \ 达引导进近时,必须要作出的是继续进近,还是中断进场( F* g2 k! }/ A2 U 复飞决定时的高。( G, `9 Z" W$ P9 c3 C 决断高(DH)2, 1 K' [; z. N6 k4 K精密进近时产 ) n6 j0 b3 |: F* s4 _+ o- V5 g失压, 8 r3 I* ~- T! E, T# m. V% U9 u" ?& Q9 f0 E排油, / ?. V4 i' C. R# x1 }- r. c3 y. n* p用飞 ; R2 A' q* C/ r0 ]! Z1 M4 x英汉对照民用航空词典B OEING 0 T0 j3 e/ L3 o+ a2 ^$ HTECHNICAL DICTIONARY 41 * \4 m3 X: }! Z' d% `% i- r6 a, BDEFUELING VALVE, A valve in the fuel system for , E G. d: c0 G4 p3 hefueling the tanks and for transferring fuel between the6 [9 q2 S/ v; k+ F0 R1 F6 Z6 ^1 V E-ICING, Removing ice after it has formed on aircraft. f$ d# S1 v# i! XChange or difference.; K v; L$ q. I- e. Y9 [: {* h$ w EPARTURE CONTROL, A function of an approach " R$ @/ d1 ?5 E, {ontrol facility providing air traffic control service for 3 v& c9 L' v2 i5 \- Neparting IFR and, under certain conditions, VFR1 I9 h# W1 v. } EMODULATION, The process of retrieving information' A- O+ B r6 i* ~5 Q/ D) |7 b) p5 P carrier voltage. / V; q' z: \1 z( U0 Qation.6 M4 ~; ^/ I. |! l c lic6 D' q2 Q. }$ K creasing hydraulic reservoir air pressure to# y5 T" k" o' K mbient pressure. ; e& `# ?6 R5 g/ m5 x箱排油和在燃油箱之间 ! t6 j! G# n4 o+ z! o: i/ r送燃油。 z- a: T ~1 e9 h冰,4 @! y6 q0 ?2 P' v 除去已凝结在飞机上的冰。# k7 t4 k8 ]/ S4 b; v3 P) u7 \ 删去或取消。 , b" N. ^5 |1 k! |5 P! Y. Y量,+ y# w# u! [7 A 变化或差异。 M1 A2 |7 _9 A+ J- z 场控制,4 h( I# t4 g. j 给用仪表飞行规则离场,和在某种情况下用目视飞行 : G/ K, k+ w- }9 n- f2 M3 Y则离场的飞机提供空中交通管制服务的进近管制设施 ) Z# J6 ?1 B: T: K6 X G. A8 H& x2 w* z( s5 X' g1 | 调, % P. [; d0 b$ M: v. i电压中获得调制电压的处理过程。 + ?1 `, C4 t! g2 T2 C {. W6 O环境( q0 f% t* L% b 力相同的活门。' ^) _! V! T7 k* a8 Z5 Z8 u4 A d, b9 I* ]/ u! y4 | tanks.0 h$ u9 X6 k% a; b: ~8 N: k$ \ D ; D& o V0 f; e7 ]DELETE, To remove or cancel.- V' ?% a$ r4 S+ b( Y6 | DELTA,* E! {# j7 f7 l+ I# _* K/ O D5 e% ]- I) W9 a c0 Q5 s2 j1 Y9 X- a4 M8 D1 \ d _# j. e( c' W3 g raircraft.5 ]9 V( a2 ^4 U4 | D ]5 f' }0 l0 x2 ]5 \ (modulation) voltage from a modulated, V2 f) i0 f' Q7 L4 b, x+ M* W DEMODULATOR, A device or circuit which performs! F4 n* E! i# W) D3 F the process of demodul 8 F9 R' t5 X( s) ]3 KDEPRESSURIZATION VALVE, A valve in the hydrau. J$ ]4 Z5 R+ R/ ^1 j2 @' o* u7 x system for de 8 i# R/ J v" @6 p! S1 ^0 e0 J2 S$ ]a0 W! r$ c- Y/ a/ |/ s1 H( U! |8 _# q 排油活门, $ x$ `* V9 f/ b) ~4 }燃油系统中的活门。用以为燃油 . i/ {9 o, J' |7 J2 q- F2 w! b' ~4 X+ x J( V" E2 Q0 ~7 q! Q, z5 f5 ~4 l6 u5 J0 g1 Q; m 删除,' g6 z5 k2 y% h6 d0 i% ?& b {! F! A: l; W; w& ?) v. _- k+ U! ~8 E6 @+ {% P3 r3 \- Y 的一种功能 ' ]8 k3 Y% q2 U& D& S! H6 h& |0 K6 g" ^( W2 q: U 从载波$ h7 L- B2 r+ r8 r$ L3 \ 解调器, 5 M0 C b: u) R9 V' e6 C2 @完成解调过程的装置或电路。 % g E, N" A% J6 M8 P2 R0 q x减压阀, - U' m9 c# C; N7 B) F% O" G在液压系统中,将液压油箱空气压力减至与周围 - I- L8 m1 _0 }* C. C; k. M# Q$ T& I2 E$ V* |英汉对照民用航空词典B OEING6 A$ @+ w ~4 f TECHNICAL DICTIONARY 42 8 V2 X: [7 |& r @7 ]6 w* KDESCENT, Phase of flight where altitude is decreasing. . u# q! K6 N5 P# METAILED FLIGHT PLANNING, The calculation of fuel' r; H# j: y- U3 P nd required for a trip by considering each phase of: y: n; _# L+ R4 ~% o ight (climb, cruise, descent, reserves). 7 E: z1 _' a* A3 \6 o% eal or8 O# Y& f* U: i o( V! X$ x3 p0 S7 ? ETENT SOLENOID, An electrical solenoid used for 6 R5 j2 D% ^' b W" H) F' H3 ~. Lt. 0 T# A8 o$ {7 y8 [specified course or% N+ z1 @( ^% G) L- b* [ rocedure.& e0 [" y+ K; M1 v1 i( C- ~" ^ e.$ q: z+ E3 W& l; j 飞行计划,0 ^7 J$ {' b0 P9 x( ]0 U* ^ 将航班中的每个阶段(如爬升,巡航,下降,备降)都8 J# c% h9 Q# @$ o# ~% ^4 B 人考虑,来计算该航班所需要的燃油量。 : h+ A4 E" \- ^2 Q用来感应情况之正常与否的电气装置。3 Y( c' x+ g0 H3 K6 ? Q) W 定电磁线圈, % M! k7 f$ P2 |9 y1 R: c. w出接通的电磁线圈。 ( a; Z2 F$ y+ p2 f4 S1 I1 H4 }9 q+ o差, : [5 G) P, t9 z6 `与指定的航道或程序之差。 3 _! e: ?" D# L8 Z Y4 h6 e+ }用气压或液压操作的活门机构中的柔性部件。1 U2 F5 z5 p8 U( ^$ H( S- l5 J D ) n0 P2 l: o/ B ^7 z: k# E% n, `a ! q2 P2 T: F2 J/ F! ?" \. l0 d' Ufl ( [5 j( Y8 Q7 x% m$ r9 dDETECTOR, An electrical device for sensing norm * [0 }/ Q1 E/ c; cabnormal conditions.6 M& q) \! N! r$ @9 X4 `7 E- C D6 E& O# h+ c1 k controlling the engagement of the actuator outpu 0 a# D7 D) W8 x9 }DEVIATION, To change from a% B5 E3 L- n0 \7 w8 M9 y3 W) v8 p p# J# H u; Y! u; H! _ d- U6 P4 s DIAPHRAGM, A flexible part for operating a valve / V* v$ ?! f7 V2 p, Qmechanism by pressur- c6 N/ R8 J7 M; Q# r 下降,; F" _/ s& N/ O# ^- T3 a! } 飞机高度不断降低的飞行阶段。! H3 v# z- M e" E5 O# G" | 详细 * g; ?/ m+ V7 l1 A4 i# Q$ o" N( `, T- U+ ^& x* D" Y5 H; g 探测器, 2 a8 ]7 M9 A$ h' D" t2 U& @# j9 i2 c* n# M0 ]' k用于控制作动器输3 f* I3 h. F" B) l6 j7 m- w' Q' T' |* F; _8 R隔膜,6 ?% y7 j, z4 {1 @0 L 英汉对照民用航空词典B OEING9 A3 a0 V: ]4 Z" t/ o TECHNICAL DICTIONARY 43 ' i9 C# k) D! l9 YDIELECTRIC, A material which does not conduct+ e3 ]0 K( M! F" n1 o4 t electricity and used between the plates of a capacitor 7 p- _5 G. G, y7 S; v0 a(condenser).5 t/ p7 c8 |+ o) a, k) I- w nother pressure in the same system, measured in6 ]- A+ r0 I9 r) E5 S ounds per square inch differential (psid). $ t. u5 k& a2 YIFFUSER, A part of an engine between the/ P3 G; `0 v- O& u5 y6 r1 f ompressor and combustion chamber for reducing the: m8 j- i$ z* P& g$ b air pressure. 2 h/ G" |+ a! a1 C; Kigh2 G5 u) T9 s! w" C pulses.! P$ \ ?) D9 h& w$ Y, D7 M ignal that is a close approximation of the original* t/ \% g& C$ ?+ u ignal. ) _# t' I5 o/ y) P3 iIHEDRAL, The angle between the wing reference g, w A8 U/ e( p4 ~ lane and water line.( C4 ?$ _- V( p2 `, Q 的压力,以每平方英寸7 V8 ]" o) s8 e5 f0 {) f( k1 G& ^ 少磅压差计算(psid)。" o, `* M7 U" P* T4 W7 r% { 散器,- |- w& V# e$ q! q/ F8 u 发动机内压气机和燃烧室间的一个部件,用来降低空$ j1 x; q- j3 f L% b1 \6 E 增高空气压力。 5 m0 N, K' s6 o+ `8 I换, 6 i5 [" q1 v' R4 d$ {的连续可; X; A, X5 a' L2 Z( y; Z (模拟)信号的处理过程。 1 z5 ]& _( j8 {) A反角, + u1 e! b, m( A机翼基准面与水线之间的夹角。 e! i+ h `9 }. r m DIFFERENTIAL PRESSURE, Pressure relative to % w; P \: E* wa " u5 H; W2 i8 W: Up8 m1 H) G% v+ V& p D* u* s# ?! @2 N. E1 Y c * w$ j3 S+ m' i8 z- \8 @airflow speed and increasing the- G7 R% M6 U: M$ a6 \: X DIGITAL, Digital refers to a signal whose amplitude 1 O% ~! r7 ^6 o3 P, Q0 J8 h! kremains constant for a finite period of time. Digital) E9 V' A. u" k% I signals are commonly represented as a series of h 8 A/ m- E! ]% j# r8 r1 o, e5 Fand low L q9 q3 U j DIGITAL-TO-ANALOG, The process of converting a% `6 m; T* N* |( R digital signal (binary) to a continuously variable (analog) 7 J0 ]; }% _) u" _4 @s9 w# F# u$ V7 Y, z s 2 @& g, { \4 o, yD 1 Q' r. `8 [$ E8 K1 |* Mp! r& j& _" i) m4 b" ?5 V6 H 电介质,$ L! x* J" D3 u6 Q; } 一种用于电容器板之间的不导电的材料。 : y5 x! l) ~! B+ ^& `压差,: `3 Q/ M* u" Q3 \9 x 相对于同一系统内另一个压力6 O( e) y9 C- s, L6 Y/ J' U8 E% b2 ^! I3 A7 v7 s( t- F4 r4 r5 |8 B$ ^ 气流速并 / k0 m( R5 ^6 I数字式,7 h2 s. |( r! h! j4 F+ @9 _3 f 指一种信号。该信号在一定的时间内,振幅保持不变。 ; Y/ F2 ~) i1 m5 [9 V- F通常由一系列的高低脉冲表示。 ( O8 t2 m" n! L; N6 N数一模转- S+ z) T, T: g+ I0 \ C5 K 将数字信号(二进制)转换成与原信号相似6 u6 [1 y6 B9 O l( y8 Q( x5 o/ i6 p( s6 { e. q. h% T$ p- C6 x/ }英汉对照民用航空词典B OEING 0 s3 h1 g- e& ?2 r+ _# q/ E, d" d% gTECHNICAL DICTIONARY 44+ q! n3 s$ z- U$ B$ X% P; ^ DILUTER DEMAND REGULATOR, A component in the # J$ p9 U0 R+ ]crew oxygen system which mixes air and oxygen and ) i4 g$ x+ E% A w1 c, B+ Y! ?upplies constant oxygen pressure even if there are' U8 g" Q1 L5 l; f0 g/ _) v9 I hanges in ambient cockpit pressure. ( D; C9 w1 k9 f. x7 L9 AIM, A word value of light. For light control devices - dim 5 T, j* v3 T4 a7 g' wthe opposite of bright." |5 @8 w7 A; ~% G IODE, A device which allows electronic current to flow ! T4 e7 ? t6 d7 R2 }) a1 u* ionly one direction2 i+ m" m6 x$ p& H/ O uid in a reservoir.: x3 r3 M" _ {1 p; [/ e D7 s DIRECT, Straight line flight between two navigational 9 _ c) D4 Y9 Q8 Raids, fixes, points or any combination thereof. When0 w" u) Y+ c+ N* O& S" J3 a used by pilots in describing off-airway routes, points 5 I8 u6 S- {# _& Z) J4 c1 Xdefining direct route segments become compulsory ^) c) {& \4 | A7 x reporting points unless the aircraft is under radar6 O* q3 W1 h: _" j) z6 g control. 7 x8 ^3 s9 f4 J# Z8 w5 C, u H节器, / a$ G* [" X) ^7 |( f( ^) P7 @: z将空气和氧气混合,% |% @6 S7 X+ h# ^ v: ]: I, A9 a; k; [ 使驾驶舱环境压力改变,它也能提供恒定的氧气压力。 5 s8 j" e. K7 x! Q5 E3 o e2 R# f0 f8 D9 e1 o r2 l; ^一个形容光线亮度的词。对于灯光控制装置,暗的反 8 w% q5 Z' u6 f/ q" ~6 S) ~词是亮。4 l+ F! q& L/ \ V1 t& ~6 @ 极管,$ h- Z, L4 \# N* y0 A 只允许电流向一个方向流动的电子装置。 ; R! J* E! m+ Y2 C器内液体的量。 ' b- ]7 s* L9 @4 M7 @! R直飞, 8 o: F1 C. U X L: K' \9 c9 U两个导航台,定位点,导航点,或任何的组合之间的直 H) s; ] z- c 线飞行。在被飞行员用于描述偏置航路时,除了在雷达控 ' I, R) f7 T C: I0 k制的情况下,确定直线航段的导航点成为必报点。 ) j& J) ?: A) n8 K5 Ls 1 J }* q, L3 R6 ac) H. z( ?4 {4 C6 E D . b9 V' b/ N& Dis! I1 p% x9 n* i( `( @ D2 q2 }( k4 K! M in( c! ]. m# q3 x. T/ a DIPSTICK, A calibrated rod or stick for measuring a o% j2 O5 i; [ quantity of fl 8 y$ v3 a" }8 d% w' ^; ~, e8 R稀释氧调* [/ N# h8 K# u6 X1 Z* j 驾驶舱氧气系统中的一个部件,它 6 @; y. j- o8 \1 n, D$ i3 s; X1 d: N" i. l, n" U, V/ T( S) A3 M8 Z, H" C! u {+ b' l& x* M" r& j& B- }, E9 p' x量尺, 9 Q$ K. H, _$ H; E' C% L- H0 ?校准过的棒或尺,用于测定蓄液 6 l K* a7 ?) B _. n英汉对照民用航空词典B OEING) U" r# R8 E& T1 ? U& l TECHNICAL DICTIONARY 45

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