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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 " q' g: E, U3 N# ~% v' T! |% u4 v民用航空词典 # K$ N8 z" Z6 S+ I波音商用飞机集团& Y" p1 N! d5 {: ]3 { BOEING COMMERCIAL AIRPLANE GROUP5 m# f& V9 [% b' z 英汉对照民用航空词典B OEING 6 N ]: ^' Z& n/ E% BTECHNICAL DICTIONARY 1 2 g& u3 i& D4 R- r+ o, K' k4 B. H0 ^, |A3 m' z% B7 N4 ?1 s ABEAM (ABM), Beside: An aircraft is abeam a station; B! Z- V7 J" w when that station is 90° to the right or left of the track of 1 R) t! ?$ J, g1 ]; _+ i/ ?the aircraft. 8 D4 ]5 L1 `- NABSOLUTE ALTITUDE, The actual distance the aircraft6 W6 d& E, \/ c6 p$ r& \ is above the ground.; z- `' K1 I! I. W; a+ @+ N ABSOLUTE PRESSURE, Pressure of a liquid or gas9 J% r0 W6 g- E) ?9 H4 d4 W& |, v measured relative to a vacuum.1 Q& q* R5 Z9 a" J; q ACARS, SEE - AIRCRAFT (OR ARINC) REPORTING6 v/ ` k9 | N7 \; K. X$ M N ADDRESSING AND COMMUNICATION SYSTEM % {: G) j; }8 B1 b, V% OACCELERATION, The rate of change in velocity with( z0 o( I* }5 N3 @ respect to time. / `5 k2 k2 n+ r7 d2 bACCESSORY GEARBOX, A part of the engine,- z" e9 \- P# I; e mechanically driven by a compressor or an angle t8 R6 b0 ~0 {$ ^0 Kgearbox, for driving components necessary for engine$ O( \7 ~7 Z9 c: d6 @# [( [5 y 正切, _% r- Y. Q- w; n, C s6 M4 ~( O and airplane operations." j" {1 `- f/ d) s6 B* u' Z 当电台在飞机左侧或右侧方与航迹成90 度时,飞机正) M7 I/ \3 h2 T, O: S: g 切电台。 , a9 a) S4 v% U. {* I绝对高度," y) S3 X& J# l; E 飞机离地面的实际距离。 $ C# A$ ~& G* J8 s绝对压力,7 ^5 Y1 R# ~* M6 h 相对于真空(无压力)测得的液体或气体的压力。 , P B5 a w5 j% f! c; ]7 g5 ~6 ?飞机通信寻址和报告系统,6 o1 E- ~8 t7 g6 T 见Aircraft(or ARINC)Reporting Addressing and0 r7 Z1 f' g n' R: | Communication System. , S0 ~# g8 _! { m, w8 a. r8 q" z加速度, ' H, @1 `! y8 D% z) P, k6 w* K随时间变化的速度改变率。 % M4 b/ L. S: U0 n附件齿轮箱, 0 }6 D) B9 j' }2 u! a, [发动机的一部份,由压气机或伞齿轮箱带动,用来驱动 2 f. X7 J% M) u7 m一些使发动机和飞机工作的部件 . Y+ I. d1 X# k$ K0 Y) y1 T英汉对照民用航空词典B OEING, h: j$ b& l3 N1 r q TECHNICAL DICTIONARY 2/ ?. }- D3 {) n3 ` ACCUMULATOR (NO. 1), A container with hydraulic ! k y* ^4 J& p, o9 e* dts when normal hydraulic supply is not$ W' o( k% j* g2 ^2 H vailable. ) a' m: R% @! y* b: a% ^/ sCCUMULATOR (NO. 2), In a computer, a special , W" w0 @$ H( y1 D" } ltorage register associated with the arithmetic logic unit,5 d9 l: J6 x3 f0 W4 [, o olding the results of a computation or data ; W3 i7 P% }# t( z5 P% N9 c; {6 SACTUATOR, A mechanical device operated electrically,8 P! y$ S: a$ a$ c4 W+ d hydraulically, pneumatically or mechanically for( j5 B& ^7 m6 A5 d' W# w0 b transmitting motion between components.' q* v$ j- |9 n9 ]6 q% }5 F4 F5 @ ADC, SEE - AIR DATA COMPUTER 6 c% j/ a3 C/ u" L9 N8 ?3 J9 GADF, SEE - AUTOMATIC DIRECTION FINDER # @. o# f0 e2 n( dADI, Attitude Direction Indicator, An electronic display of- Y) r2 X7 D3 y) @5 M* `) C: v. N airplane attitude information in pitch and roll. / z; o& W8 Y3 m% p1 f4 q) R* a蓄压器(NO.1),0 L1 C" t, K- f 含有靠干燥空气或氮气增压的液压油的容器。当没有正" v0 G- U# }9 o 常的液压源可用时,该容器可用以驱动部件。 ?; Z$ K9 q/ v0 W" [存储器(NO.2),2 P& I# S3 @; _, A8 h. K" O5 ]/ |6 ? 计算机中,一种与算术逻辑组件有关系的特别存储寄存 9 s! y5 U- z! a; g器,用来存放运算结果或数据传输。/ U% q: u" i6 x) ^! `1 U" Z' C& V 飞机状态监控系统, $ [" r5 P* I( ]见Aircraft Condition Monitoring System# i0 E/ r: n# h2 N0 n) y3 R1 p fluid pressurized by dry air or nitrogen for operation of " s: ^* d# y2 a5 A8 Ocomponen$ d4 X" z: c2 L5 @! N$ ] a# H" U# x$ E6 }; { A" O1 ]7 P9 }/ ^& ] h& Y" N s, V8 u D& v) B; Z0 y9 |: C6 F* y3 V used for h/ l' H H6 z& m/ M# S transfer.3 m5 a3 [. N g ACMS, SEE - AIRCRAFT CONDITION MONITORING 0 t$ L5 Z1 q/ z4 aSYSTEM .3 [' [" T3 e: n. `3 l; ]$ F 作动筒, ) m. r) w( k% p- v* t+ Z9 i由电,液压,气源或机械驱动的机械装置,用于传送部 $ L6 Q; Z' G6 l件之间的运动。9 ~' c: s) \7 i, ~4 c7 M6 F 大气数据计算机, - N" d p! H2 z$ `见Air Data Computer.( e4 P; U. ^, B7 ~& K9 w) ]6 v3 I 自动定向仪, ( T7 k" H8 Y. ?! D$ |7 ^见Automatic Direction Finder. * t; S% ?" g2 v/ w姿态指引仪,# M: r/ K' V v( p$ ]9 P3 [$ n 用来显示飞机的俯仰姿态和坡度的电子显示。" N' Q+ Y/ ]( W9 ?: m. \. o 英汉对照民用航空词典B OEING- }4 Z6 M$ y' c* ]' i TECHNICAL DICTIONARY 3* G4 n9 v6 B( q+ h AERONAUTICAL RADIO INCORPORATED, ARINC is * Y+ ] _6 y8 e! N V6 W9 S ],' t5 S4 n5 g: R4 z9 n0 S5 Q8 { nufacturers, and foreign flag airlines. ARINC P5 ]( T) ~# R5 R7 g% b) L evelops and publishes standards for electronic' u$ [+ K2 |8 V- ~ quipment and systems." a7 k* l0 v% c3 i5 H GILITY TUNING, The capability of the DME to * x1 R0 J8 r( s, o4 j( @lternately tune between two different DME stations in , q! ^3 B4 s9 U+ Erder to get two distance readings from one1 V9 _, c ?& f$ F, V K terrogator.4 L2 Z" z- b0 Q( B1 f$ { ge/ Q" M0 \5 P; L7 M7 _3 X. l+ S ILERON FORCE LIMITER, An electro-mechanical / I5 ~2 i& m0 IIR CLEANER, A component in the pneumatic system# K/ k. m# u9 ~7 V7 }4 q! } upply to the air : R1 a, f- i4 K2 U' ?0 {* Q1 Ronditioning system. ; K6 T1 h& | T6 s) y: T% Y订并出版$ {5 U5 t# J* l 子设备和系统的规范。 & ^/ v, ]% F- @% M3 e快速调谐, & n4 b9 |5 |1 c$ M1 B+ d机载DME通过交替调谐两部地面DME电台以测得来自$ q9 O$ z4 R# K* B 同一台询问机的两个距离数据的能力。1 [ ]/ P) S' X9 e9 d# p3 z* W 翼操纵力限制器, / ~! K! s0 s+ m7 W$ n- n2 v7 v装置。在自动驾驶工作期间,用来限制驾驶盘# c8 P; k# U+ Z6 d 气清洁器,6 e% g* Y: D# _ b1 m 部件。用于去除供空调系统使用的发: f: G; f/ x$ D0 b, ~* z! e4 v% E a corporation whose principal stockholders are United / p4 u; o6 n: \/ `States scheduled airlines, air transport companies & H7 F: j$ G4 G% r1 T% w* uaircraft ma 6 |( [! Y3 ^1 U1 `d1 _9 L; H( E( m6 l e: P k+ z: {! j A3 m- p) w5 x% V7 q a 9 \ \0 U8 o- J. E4 d" ]/ Eo( ?5 I8 D% p; G& @5 n$ k in3 r8 p4 N/ c, I' k0 S$ V P* N AILERON, A hinged moveable part on the trailing ed4 b4 r' b% [2 k6 M+ R8 Z8 B of each wing for airplane roll (wing up and wing down)- L/ s ?2 f5 Q7 ^$ F control.8 N7 m ~- a( \8 z5 g# i. u1 S A . I7 q/ ?* |- G& F( Hdevice for limiting the control wheel movement by the4 m( G1 T9 }' N1 B$ } autopilot during autopilot operation. , c9 ?. y, J( G: I8 OA; B1 l" e, x- O: s/ G for removing dirt from the engine air s % n6 m( o( z' }! U$ Wc 2 t' m: w" c& s' R& {. ^' _6 [航空无线电公司, + u2 ~4 K& }! `' R2 ?( r( j7 l3 f主要股东为美国定期的航空公司、航空运输公司、飞机# |' O5 W1 `1 x) f' u; D: C 制造厂和外国领队航空公司的组织。其目的是制 - ]$ d# [% s, c3 s) J5 ~& j6 B5 p! x. T3 B2 F2 X副翼, 6 [/ P; U! a# E& E1 M* j铰连在每个机翼后缘的可动部件,用于控制飞机的滚转0 u( O$ e! P$ A5 Q- @+ P (机翼向上和向下)。 " d. j8 A4 R( V! S+ f0 K; r. o4 w+ O4 e& d/ O% C 一种机电 * r/ [: q! j7 {7 v/ B" @的动作量。 - i5 v8 j6 K/ ^% x' n4 E9 Y( _# W% E2 o* K 气源系统里的一个( S, u6 j$ w: F5 k* ?' W0 H 动机引气中的灰尘。( d; K! j/ B3 c( u+ g2 H9 T 英汉对照民用航空词典B OEING j+ r C6 f6 m- E% T* e7 B TECHNICAL DICTIONARY 4* j7 F8 Q4 g8 |0 L8 c( z" q AIRPORT ELEVATION/FIELD ELEVATION, The8 m( a% e; _8 u- P highest point of an airport's usable runways measured ( @* |3 G- M) Q" A! J* n- v* [* Kin feet from mean sea level. In a few countries, the 0 Q- U% Y; |+ a) ~airport elevation is determined at the airport reference* @* k" \: }# A t) s% Q6 k. ?7 ? point.2 }/ B/ T$ N% L; T) m; m- E AIR ROUTE TRAFFIC CONTROL CENTER (ARTCC),7 B5 {5 n- V) s5 D ervice " Y5 e% R) ^9 [7 ~# `; rase of ! n6 P4 |, H/ ~( Nus flow of air traffic. , {' C/ G6 r* h, _% G% }IR CYCLE MACHINE, A compressor and turbine on a& y5 Y" i( G) M ommon shaft for cooling the air in an air conditioning $ S3 _2 [6 e6 @ ~ iystem. The air is cooled by expansion from high to low 2 v, X& H- S! }9 z4 Yressure across the turbine. The compressor is driven( ]) L% ]$ w* r) H y the turbine.6 \: @ z1 ?. y, Y1 f 中航路交通管制中心(ARTCC),& ^: I4 w0 r$ O: T, p, N: k 域范围内使用仪表飞行规则飞行的飞机提 $ u4 E: ^, X7 m7 R4 n' \$ H管制(ATC), " X4 {1 j; w3 ^- j4 j; S) r0 \6 q涡轮冷却器, 7 N- k; H+ M. o1 c3 \是装在同一的压气机和涡轮,用于冷却空调系 0 H( k8 n e/ h9 f" D' Y% F3 g4 A统中的空气。气经压气机压缩后,由热交换器移去热量, 7 }0 {; F' O* W1 q) D& a+ z然后经过涡轮令涡轮带动压气机。通过涡轮之空气,温 1 B( s; @- P- ]5 ~度下降。 % M$ m& d& f8 ^' H& u/ M: N% bA facility established to provide air traffic control s1 q9 f) N' O" O0 z4 c9 T to aircraft operating on IFR flight plans within controlled % b: C+ g& I9 n$ Hairspace and principally during the enroute ph7 Y& T; @3 L% d O- W flight. ) K' p0 P6 w8 h: J' dAIR TRAFFIC CONTROL (ATC), A service operated by & L( D3 \1 f( K! q9 `" C' o: Zappropriate authority to promote the safe, orderly and 9 u" R& [; H* o+ t$ Gexpeditio0 L k8 L1 y5 J2 [1 }0 } A& M( c" t. `3 C" E2 \! ], W* p c 6 e0 ~. B) ~! \( }s8 u# y$ L' V; k, F* m p ! P5 {+ O9 V2 u$ G# v0 @4 g$ tb6 F" O( e( p3 e# v7 v 机场标高, 6 Z% E$ V0 x6 I. z; c ~/ f/ ~指海平面与机场可用跑道最高点之间的距离,单位是英 8 l. f% G" i# W9 k尺。有几个国家的机场标高是由机场基准点而决定的。. k. i! g) h/ p9 ]/ [( T$ e* x* A4 Q6 ]" Z3 u5 D给在控制空0 K2 k. X' m1 w6 u) r$ V; o 供空中交通管制服务的站台。* {. ~( o" R9 c2 m! B$ E 空中交通/ a" S* Y: S! U7 N6 [* a( Z 由有关当局管理,旨在促进安全,秩序,和效率的空中$ I0 E" [5 U% i 交通服务。1 C5 P& N# D7 E8 E A. A* ? \ 根转轴上 + B! G& L" V; l! b" N, T$ g% g* D( K3 V; D3 i9 A- T0 m5 u6 F9 }1 J: j英汉对照民用航空词典B OEING $ h: n' i/ Q7 N+ g: N9 STECHNICAL 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 , `( z, Q0 z: U1 udata information, such as altitude and airspeed, based 9 e: O, _1 x( b" w, ton pressure and temperature measurements. 2 _9 N2 P" S) C0 @4 K' [0 Oes air/ Z @5 t" C) i IR TRAFFIC CONTROL, A system comprised of9 w: n; [- A) M) h' k round and airborne components used to identify, track/ C( Z2 g) H+ H8 v" D y OUND SENSOR, An electrical device operated0 q5 ]; d$ J4 j1 A5 s+ C6 C y the landing gear, which transmits on ground/in air$ J1 T- r7 p+ r& L formation for system operation in flight or on the 3 I0 ? z4 p" m5 iround.- R7 K: G2 v: v) T IRBORNE VIBRATION MONITOR, The AVM takes( `( P# N$ m5 d8 P, ]" j3 ] e signal from the engine mounted accelerometer and4 q- i0 w! r8 }4 w3 M J# [ alculates the vibration on that engine.9 f; W# Z T( Y6 T! j corridor equipped with radio navigation% h. v: W1 W7 H6 x aids.' l# b& z# |* u9 r! g0 t% O: | AIRCRAFT (or ARINC) COMMUNICATIONS 0 v2 I0 d4 `+ M# r$ R6 u+ nADDRESSING AND REPORTING SYSTEM, An 9 a; \( ~ L# y: N7 _9 Zaddressable digital data link system which permits the 2 W- g* ]$ V( C' b, |exchange of data and messages between an aircraft: O% R$ w X* c5 J: r+ T and a ground-based operations center over a radio 2 y' I& F5 o7 F5 z! i/ Q4 ]network." q. i, j g2 H! A2 t2 D# P, O AIRCRAFT CONDITION MONITORING SYSTEM, A% |" \/ s& K3 j# @6 e$ x6 G system of sensors and recorders to monitor various) p* v3 a" u0 K. c' n( g3 C airplane systems' performance and status. + p2 h9 v& _( r/ B7 m6 ^7 |机,! {/ v% `" I0 L. e 中交通管制, 8 t$ Q+ I8 L/ j5 {& F& b一个由地面设备和机载设备组成的系统。用来对飞机进 ; T, ^! i8 O! ]7 v/ [1 s# b5 g! ~地传感器,* j( Z5 d9 u1 u; |$ G+ t4 m( u8 r* A 一个由起落架操作的电气装置。用于给空中或地面的飞) S5 w; K: D) S6 u 系统运作传输地面/空中信息。(有些系统只能在地面* \+ Y/ B% `6 u8 V 用) ' Q; c# a4 G. }5 s; m; [) V5 R5 |载振动监测器(AVM), 7 h! o5 z7 Y7 U" D" s, v0 g# eAVM从装在发动机上的加速器取得信号后计算出该发0 y3 u0 @& t0 B l 机上的振动。 ) z1 {% R. W, K7 K% W式建立的控制区域,内有无线电导航设备。) ^0 |4 N2 ^0 O [ 飞机通讯寻址和报告系统,: p! j! K- a5 R, e 有种可寻址的数据通讯系统。利用该系统可使飞机与地 * I s; s+ |8 p3 S N; @$ H, _% E* t面操作中心通过无线电网络进行数据和信息的交换。* I; R, ?/ E) i1 m 飞机状态监控系统,( p/ U2 o4 E. ?' [/ j+ h 一个利用传感器和记录仪对各种飞机系统的性能以及' H; Q" e8 {, U. s 状态进行监控的系统。, T5 b- r% W( Y4 a; ]& Y# N A + T: e4 d/ k! O. d1 p1 X( @# N' ?g5 N% X+ z0 \! l8 S* @6 p2 ^# G4 h2 O: A and locate aircraft. , e! B& m4 }2 K; }AIR/GR 4 Z3 R1 B: F9 y: wb1 L6 C3 i/ U% X9 j$ w in2 }" g- W, f# ]% _7 D" F& M6 j g 0 i- D `- d6 w; J4 zA; n8 _4 ]; ]5 D7 w7 f* Q th( y1 G# Q2 `6 W" t* T6 N, [ c3 f8 W: g: v" @$ j/ v# a+ ]( Y: O2 F# z AIR WAY, A control area or portion thereof established) f; [6 C/ i5 o" ^$ w( U6 o3 j in the form of a & r, N9 o- }, @2 V大气数据计算( m2 c+ h ~4 k+ ]6 s 根据量取压力和温度而产生大气数据资料(高度、空速1 W- N( N" `! `1 y 等)的计算机。 + X8 g8 }. C7 s( y0 V; H' H* V/ }) E( i! h1 M行识别,跟踪和定位。 / d6 Z& i% O2 v8 N. r! F# J# C9 A; @ A c& J7 d# N% E& r* j. ?9 N& a, f0 @ 使 ' S& j( X1 ]' B- n+ F$ T0 S/ O% r. q1 R! j: {, a. A, ^) J+ y" ~; S航线, * p; J# W- L b以走廊形 7 V( q" Z n5 X' \7 y英汉对照民用航空词典B OEING( ?5 j. l4 u# S( Q% s% z TECHNICAL DICTIONARY 6* A( L0 H( ?% b6 V, D* U0 H& p% F AIRFOIL, A surface designed to obtain a useful reaction,' G) O, D+ a6 R: _ w$ [ such as lift, from the air through which it moves. Wings, . e5 A: i, b) E4 b- rstabilizers and control surfaces are airfoils.) W: c6 W8 V1 U) U9 a AIRSPEED (IDS, TDS), The speed of the airplane 7 e7 g4 y) m9 s: L _1 Z1 ]rough the air. # Y) E+ d. {' K5 g. R" n [D INDEX, An adjustable pointer on the - F" f2 P: k5 R/ kirspeed indicator. 0 i2 [8 s. z" `7 w9 ^5 Yand legal ability) F9 h3 p0 P1 B1 s: M fly. 0 K. R. s3 m8 F- @: }5 Rm, for example, the procedure for finding the / P0 e% ]( Z3 i) z" N% B6 \2 C) Qquare root of a number.% j9 S# D5 y0 m y! i! |9 }+ x, D re, wind,3 {( [' J `: F+ r2 a' _ and aircraft flap setting.9 C; \; B7 V3 X. K 是翼面。 0 Q! c8 }2 H8 P速,; r4 t. A0 y: g* V- G' s- M/ V2 c8 q 飞机在空气中运动的速度。 % i# Z) {4 G3 G- m- A9 x3 l8 w在空速表上可以调整的指针。0 g) Y9 E: Q \/ \, T# d, Z 机械飞行能力、和合法性的飞机状态。 " }' ]0 C+ u; N) ~4 T# T! d, C- p一步一步的解题方法。例如,计算一个数的平方根的步 - L! Y1 R) J; i. G3 l% u5 r3 c8 N9 T: ^2 F; u; W8 j# {2 h n! q! ^% u4 m) H/ x资料的法定文件。 6 C1 N8 E- i4 C5 x1 \. j翼位置成函数关系。 + ?3 E$ D. f v3 z) H* Hth$ r k, B0 {1 M; `) J AIRSPEE ; M3 j( O6 O6 Ia $ l8 c \1 N8 bAIRWORTHINESS, The condition of the aircraft with, S! {+ k8 u" T! ]9 L1 k respect to its aerodynamic, mechanical, % s+ p( D) D d) \to , c% v4 O7 [! B/ [) u% UALGORITHM, A step-by-step procedure for solving a' b' U7 A, Y# ? e7 t3 k# c proble. t3 Q( I: ?# s( L( d9 t s * G/ E/ m7 h3 X$ Q- Y( \3 h$ L7 W* OAIRPLANE FLIGHT MANUAL (AFM), The legal $ ~# e; a: ]' V* m+ `document containing performance and operating limits,1 Q; y- t/ C d! l& s1 @5 c operating procedures, and takeoff and landing - ?) C# M1 D. ~performance. & @1 S9 s6 H# E" u8 a- t& TAIRPORT ANALYSIS, A comprehensive set of takeoff( C6 e9 u: q8 o# p$ X0 c: G weight limitations for a given airport runway, generall' A& V! p- V1 j$ z presented as a function of airport temperatu 6 q# D* g$ F: d+ m b翼面,. _2 \% c% z, r' T0 X# s 用以从气流中获得反作用力(如升力)的表面。机翼, d* k% G, ?# y& i! M4 _4 q( ? 安定面和操纵面都 + p+ d, \& ~5 U, V% b4 n2 i u7 {0 |) `+ d' t) c. I: x! j2 P0 L- b空速指标; V/ `. F4 n+ k m9 j 适航性, % r6 l! Q( g0 e& t; p有关气动能力、6 e& R) W+ v) \% h7 [7 I 演算法,: r9 D/ l; N0 S- ]! t, d9 n9 E, M: k5 u 飞机飞行手册(AFM), m" m) D7 j( K3 _包合性能极限,操作极限,操作程序,起飞和着陆性: a* s, r, M/ A% b, `' ~: i; k' e* @! j" s$ B2 Z9 h机场分析, ' J4 l' m8 K" Y6 u一套针对给定的机场跑道的详细重量限制资料。通常与* M4 |9 ], M) U# P/ z2 w0 ~& e 机场温度、风、和飞机襟 7 s9 ~3 e( }! {英汉对照民用航空词典B OEING ( V! l/ m; Y6 C5 XTECHNICAL DICTIONARY 72 K" X& k1 Z1 z5 d AIRSPEED BUGS, Adjustable pointers on the airspeed + h' o0 }. P0 I; p1 c6 Eindicator. 6 p. L% x5 |: `. p( X3 a/ |0 t9 ]: IALLOY, A mixture of a basic metal and small amounts0 }% r' P6 ~8 | f other metals to change the properties of the basic 2 ^9 Q5 @- F+ p" l6 Hetal.. a# ]; z* H7 r, s" ` Minimum airplane speed. . w1 F2 K" }, U0 x3 @ he of & u! L7 c6 h. T1 D" J# Citting airplane angle relative to $ b# I8 e5 }+ s& |1 t& ]) i4 tirstream for the stall warning system.. ?: U5 F: a! p) ] another. 8 s, @$ N' J1 J! O; {LTERNATE , An additional airport selected during 8 R" N5 {+ V0 Q8 @3 Y6 }% e9 \5 f% m1 S( g2 C' Q f1 W合金,0 d" i- g0 q4 ~* W' a0 O 在金属中加人少量其他金属,而改变其性质的一种金属 - [! F3 ^4 `: A# ]合物。) u- J! x r# m! R( _ 飞机的最小速度。 3 G' I+ g& a; ^8 A速警告系统传输飞机对1 f5 \# N! L' V J 流的相对角度。 : M( n6 r' \. w" K* {% ]/ j1 T3 r, ^# X由一个状况改换到另一个。5 L3 }+ P# z- S' c5 e6 s3 F! s 降场,9 D% I2 h" p+ S* L& N* | 划时,除了目标机场之外,所选的另一个机. @ Q: j7 H- ^- [ o) [/ J+ O( T, Q/ ^! ]1 o m ; e# C1 q' u" KALPHA SPEED, " R8 G, |9 c3 D8 [' R& R4 S7 }ALPHA VANE, A small moveable airfoil on the sid B; d) V6 O/ ^8 u% o& F' Ithe fuselage transm ) O6 ?7 V. g: A da 8 L9 ^" Y$ R3 P7 j6 PALTERNATE, To change from one condition to 8 v. D: Q7 l4 q0 VA - U8 T7 O9 n& b# Iflight planning, usually near the destination airport, to be( I5 q% k$ ?3 f* I4 I& M used when it is desirable to divert from the original: W% g+ c1 a3 f( Y! { destination airport.! k( o; b4 L5 A0 j+ e7 ~5 b& G% }$ K 空速游标 7 e% I. B, b9 }& Y: g' O空速表上的可调指标。 ; @; A: R' C; n. u" }2 q) D U8 S& ^2 `- v+ d 迎角速度, % f3 M8 c4 @1 q6 `0 t' U7 t迎角叶片,$ f0 X7 a8 ~4 K' o 位于机身侧的可动小翼面。为失% i, ~7 Y2 B3 D' O' B, u; a( Q; t3 Q& d% h1 m8 x2 t交替, : o2 W$ z8 t! y/ r* v# X& U7 ^ v& h9 ~* x; V 制订飞行计( [% M1 N! b$ l 场。通常在目标机场附近,以备不去目标机场时,改降之; T9 \! f, W9 A7 P; Q 用。 6 @* ]! w3 Z v- k# O- R; K1 Q英汉对照民用航空词典B OEING3 p2 r: M9 a6 N" b; H" p" f0 m TECHNICAL DICTIONARY 8 & s# H5 T. c) Z+ B! x( r" GALTERNATE AERODROME, An aerodrome to which! l4 z+ Q$ B& j; |% B3 q an aircraft may proceed when it becomes either- ?% d% v1 E4 k1 y# s1 G9 G: I* ? possible or inadvisable to proceed to or land at the 5 ~" ^) {+ z. k5 \- J7 {erodrome of intended landing.! \1 n2 u. ]- U. l# M4 }, q3 a TER SETTING, The adjustment of the altimeter9 w/ W o* h$ ] account for local variations in atmospheric pressure., `; D/ Y5 ~0 i5 L6 q! ^& j- P LTITUDE ACQUIRE, A digital flight control system% Y$ G! x% W3 J7 D/ h) U ode to transition from climb (or descend) to level flight. ) s' r! }8 Y4 E5 |# `8 C2 _' k! U4 l6 f5 w) PLTITUDE ALERT, A flight deck alert occuring when the . B7 B; [9 J4 V- `! Eirplane approaches or departs a selected altitude. 5 e1 u8 V! H3 F9 A0 t3 [- f# _2 xLTITUDE CAPABILITY, The maximum altitude at & j& t+ p' H o4 Qhich the airplane can be flown at for a given thrust,3 i) |# S' K6 s/ N# z peed and atmosphere condition.$ N# i' Y4 T4 R. | LTITUDE HOLD (ALT HOLD), A mode of the autopilot+ O' Y) R2 {+ x r flight director to maintain a selected altitude.4 [5 o) {0 f7 y5 _5 b: j irplane's altitude during VNAV operation. # b3 y1 I$ O: m0 z+ q机场着陆时,可作着陆使用的 5 _: D6 r0 f, X8 S5 z1 o1 _场。: x% ]% M1 ^* W5 t$ D# S* ]4 i; D6 n7 y& a" h根据当地大气压力变化而对高度表所做的调整。# `& m& T, y- Y+ F" t$ ^ o 一种数字式飞行操纵系统,从爬升(或下降)改平的模0 a, b& _$ U* v2 k/ M( I1 ]! t9 z' Z" s6 Z: \度警告,+ ~" {( T0 a( L5 y* q& s 当飞机接近或偏离选定高度时,所出现的驾驶舱警告。 ( V% W- t$ f6 E" i) y1 J高度能力, 3 t+ {4 _4 v- J; U, V在给定的推力,速度和大气状况下,飞机能飞达的最大 0 T8 Z$ K1 ^3 A' ?+ N. }, [高度。3 A9 j% ?* ~9 s 高度保持(ALT HOLD),( K0 X) t7 m+ N% @ D: w4 i 自动驾驶仪或飞行指引仪保持在选定高度的一种方式。 ' f, e2 ]2 z8 W/ S- h4 b) }0 [% U. |* P" H6 \2 O# p员对飞行高度的控制。8 ?6 [8 J: @9 |+ | im 9 s3 X- d. `! }9 {# @a 4 X4 G- r9 f& {$ UALTIME1 d8 ?2 Y, ~6 s- o7 x* [ to! N, k& y6 E, ?- P( O A 0 t+ }5 e7 w# o! |% S4 B w8 l$ }1 sm ) p# C, N7 D$ y' I/ Z! tA ( ]3 S) f7 _, ?) T/ za + o5 \0 }0 U4 S3 n* u- TA 8 U& p$ A7 v" D9 o- U- Vw 0 i& v4 b |4 ]4 os/ c5 X, w5 g9 F2 n7 h A1 L( I+ k; O0 i) Z) \7 t7 B$ y o1 `# O1 Q. r. d, o0 @1 t1 u ALTITUDE INTERVENTION, Pilot control of the ! V2 H5 {# n+ ^% A& w# Qa- s4 H8 q; F |0 [& O. X0 Z( ? AMBIENT, The surrounding atmosphere./ M/ W3 `2 _# f7 U5 w 备用机场, i& ~( e+ [/ r$ A4 G8 @7 j; e当不可能或不适宜在预选 - _7 t3 z3 j; {: t7 e5 E; _) l: r+ ~# w; E0 E 高度表设定$ {; J; a2 t6 z( v) Q3 M5 P 高度截获, , J3 e) u! T, Y {& [6 m' ?/ a5 v" e. }* _% }( h! E0 b9 i5 i% c4 H0 D& ?& L 高度干预 9 i" T7 Y6 ?. X( M在垂直导航工作过程中,飞行 ) X9 j' M0 P0 P F; Q5 B周围环境(地面气层), # g5 w1 l; q& {, ^' g& H1 r% x物体周围的环境(特别指大气)。/ P# o* m1 | s3 Z' }9 k4 [8 P8 N 英汉对照民用航空词典B OEING 6 g7 }& d4 k) o T# n( [: `% UTECHNICAL DICTIONARY 99 P4 `/ T1 {) O$ Z AMBIENT PRESSURE, Pressure of air surrounding an f' n& ?$ B9 ^3 f! m+ }3 I, B object, measured in pounds per square inch (psi) . 5 e* N2 ~" h: y! _. N2 r2 qMBIENT TEMPERATURE, Temperature of air 9 L& ]2 l) x; _2 H! Rmpere. ! H, _! `8 K; K1 C" }2 T/ f- N, lurrent waveform.1 c. \& p* I. G! p g an ) ~, B5 _0 b# L- @nalog signal to a digital signal.+ J/ M# Q& d2 W; M4 M ore inputs+ y2 f: C& W% J6 s# C% z& X f binary digital information and one output. The output. J4 f6 W+ r8 T7 M 1 only when all of the inputs are 1. The output is 0' L3 d: }- q. d& i) M hen any one or more inputs are 0.4 w* Y& J1 b1 v2 t/ E' \ 面气压), ! x( ]$ |7 J% J N境温度, ! C- A, y; x! }/ c3 @气温度,用摄氏度(°C)或华氏(°F)来 ( B0 L* x, e- J' q+ u$ g/ `3 {+ L- U8 x- J2 Z! `7 g 电压或电流波形的幅度。- I1 c! v; y* F8 }0 ~# [& T( R1 ?& A 性变化的信号来工作,或产生连续性变化的信号6 ]$ F( S. i% m$ ]9 E# s 统。$ `( T+ x5 F: D1 e: k9 @ 将模拟式信号,转换成数值式。* ]' R6 f$ P/ q6 v 一种有两个或两个以上的二进位数字信息输人,一个输 # a8 y& E' h8 q( d, h( N的装置或电路。当所有输人为1,输出为1。当任何一个( r+ `8 E6 u; k( x& a& W 一个以上的输人为0时,输出为0。 % ~9 `- N3 g1 m+ i4 g* AA7 w7 [$ B& \1 }% ^* ? surrounding an object, measured in degrees Celsius R# e% ^" ~* T6 [5 x5 ^5 c) s (°C)or degrees Fahrenheit (°F).0 f/ k3 c- Q0 c9 w$ @! W AMPERE, A unit of electrical current. One volt across $ }' A; v/ T6 hone ohm of resistance causes current flow of one' ]5 R; W1 E& P& M% @% P0 T8 { a ) C& `9 J% Y' nAMPLITUDE, The size or magnitude of a voltage or , a( k0 Y5 q1 u0 Yc+ n' J! ?2 ]2 U. ~8 [0 n ANALOG, Quantities or representations that are . k1 Z' ~" W# f- f7 [variable over a continuous range. / ?) k# D5 P2 W8 { bANALOG-TO-DIGITAL, The process of convertin + e1 ~' h8 E% X/ ca P4 R' \3 d# b3 ]- x; d) u9 K AND GATE, A device or circuit with two or m1 G! |# F, i# Z |0 Z o) x1 ^: R* {& D) h: o3 a3 x+ ~( L is: r: N1 y; W$ H1 o+ k, W0 R w ) ^# a' g! r; N- H: Q" G% u/ c环境压力(地 0 ?, ^$ M! g/ A5 f& w+ o物体周围的空气压力,用每平方英寸多少磅(psi)来& h! F0 I! l" P4 f; S8 B 度量。7 u# z3 K. O4 m4 K$ l8 D+ K9 l# `- V- D4 ~5 ^物体周围的空/ x- T g* C* Q# M% i7 V( \ 度量。 - F6 |9 [/ x5 W0 [0 x) {安培, 8 q6 u+ _' n4 A% o: q电流的单位。- J4 v1 f: N8 b" r; L 1伏电压在1欧姆的电阻上所产生的电流为, \ b; m x/ Y, X 1安培 ! Q+ s5 S" H! d) H振幅, U+ d( q: V" P1 _% z模拟式, + ?4 g% Y% h/ K8 ~# m5 }用连续 5 @- c6 V, C7 V0 E$ f4 l/ H6 |$ a4 ] 从模拟式到数字式, . P5 O4 J1 e; `: f# Z& K与门, 1 N8 M3 f+ p! i; j; n/ r4 j$ Q- J- e6 T% @3 ]/ l, k% W' T8 q+ W9 ^( T) r1 y0 \8 P" ^( I 英汉对照民用航空词典B OEING- j7 y& H3 N( _% p: J3 m h TECHNICAL DICTIONARY 105 d7 \2 A- g. N9 ? f* ?! q1 v* I/ n ANEROID, A sealed flexible device containing air at low% G& S8 X( q7 a8 e pressure, which expands or contracts during change of3 C O/ p2 X" o& ^0 U) G, p8 R; s# s V ressure outside the device.6 s8 I* m; [+ L3 m6 F ically 3 C# K) V3 \# R5 t% z- E3 mr changing the direction 0 ~0 D% v/ p7 W! E+ z0 \5 \f drive. , h! H5 f2 L8 p+ }9 aof the wing chord in! X2 D7 b. U$ D2 `- i lation to the free stream airflow as it moves forward + g! } m! i4 t. C3 D4 T2 lrough the air.4 b' t& G, o- G$ M3 O al axis of the5 ^- y7 U; X j3 ?: }; w* j! } aircraft. 2 g& {( l9 ]2 o5 C/ c) f胀或收缩。 9 F* Q( |: u0 j# p3 ^5 a5 T7 A6 i- D箱。是改变驱动方向的机械装置。 % o# I Q. j8 C* p4 t& W% K机翼翼弦在空气中向前运动时与自由气流之间的夹角。 ! u. s1 e& ~4 G9 B, J8 O% {, {+ B$ r! g# c p ; }( n" n+ f3 j# p0 J BANGLE GEARBOX, A part of an engine, mechan y [$ Z6 h& G D driven by the compressor, which drives the accessory: y" B0 }- D) w gearbox. A mechanical device fo) B# {0 @3 x9 T" r; C' Y o9 J$ y& x0 @- t: X* _' c4 k6 Y8 l, |8 c( D ANGLE OF ATTACK, The angle 2 C6 k! m% I" [( @, y3 cre8 s. }& H3 G2 i y! b th* e4 G6 i1 a# ~7 t! \" A ANGLE OF INCIDENCE, The acute angle which the 0 J0 X0 V# S+ L7 rwing chord makes with the longitudin " u& d) _9 |+ J8 {膜盒," M# n' [$ H( r! H) I+ v 内含低压空气的密封弹性装置。当它周围的压力变化+ _9 |) g( @7 ~3 u+ { x 时,会膨# Y1 i1 H: `+ @' ~# W 伞齿轮箱, * P) o. L5 c& k- Y+ H发动机的一部分。被压气机以机械方式驱动,然后驱动2 u' A* Q& T& `0 }6 | 附件齿轮6 S" [9 G6 p1 A/ ^6 w+ H 迎角, . j% E; a' l3 A/ ^8 n5 m ~安装角, ' d+ l! `- P8 s* N: l飞机的纵轴与机翼弦线所形成的锐角 ; W& d! t' L, S- p' \/ D英汉对照民用航空词典B OEING) ^5 ~, H! \5 h TECHNICAL DICTIONARY 11! Y! N: d3 S" s; Q- e% j# L ANNUNCIATIONS, Audio or visual indications used to U7 L8 }. C9 G0 z2 k" w9 X! b call attention to an event that has taken place. 9 S2 j; Y/ e( _6 HANNUNCIATOR, A visual device consisting of a number5 F5 f# f! o P ly. - c% N+ z- g! X7 Z2 vANODE, The element toward which the principal stream # D. C, w8 X @5 P0 ?& T6 c; zof electrons flows.1 T3 c/ @9 Q1 a ANOMALY, Not normal.2 Z! N1 S3 C. X- e ANTENNA, A device which, used in conjunction with a " f# m$ t R5 B( T% d9 ltransmitter or receiver, is used for radiating or receiving* ~6 C2 m7 `# y4 z, k1 ~ radio waves. 1 [/ N+ t7 t1 x8 g* ^NTI-ICING, A method of preventing ice formation on 2 \# H- L) _% ]$ ]e wing leading edges and engine nacelles. . C( b d. p+ V' U, B4 kNTI-SKID, A system for providing maximum braking % V( P( c' Y+ o; F4 [' Lithout skidding for any runway condition. Anti-skid " L) N' Z$ p. M/ S0 U! A* B, `omponents are part of the brake system. % y* `3 N4 ~/ } b告,$ b# G3 c2 k# n+ S6 s- N7 W5 i; _2 O- l 当发生事件时,以声音或目视指示形成的提示信号。 3 z- h r4 ~9 k {" Q0 O与之有关的电路的现有情况或已存在的 0 } p" Q( E2 B- e e1 b* B4 S; a2 T6 ?$ I 正极, ' _: I* R( v* n, v4 s! d% P$ N主电子流向的极位。 6 Z! i; {0 [& c$ V9 A1 ]异常,3 M# z$ y3 f8 |! I, r, d* G: k 不正常。 / C. f- U' `# Q9 Z% J' H天线, . Q+ a8 x& \5 D1 K) W一种与发射机或接收机共同工作来发射或接收无线电5 }5 b" o! Y# I/ ~9 ]% w 波的装置。& S8 U6 F, v9 F( p$ ~. X 冰,: V0 ]2 \/ H. B- u# I% D, J% g 防滑系统, ; G' Y3 u* I: A; E. a一种在任何跑道状况下,都能提供最大的刹车能力而不 $ r( |3 Z. s' g9 z' @1 ?6 n* k! B+ l使轮胎打滑的系统。防滑部件是刹车系统的一部分。 7 W7 C; Y4 C: ]+ Nof lights. Each light indicates the condition which exists( L/ ^ o1 T* ~ J or has existed in an associated circuit and is labeled+ N5 @' E) P( A: f( M, Y. \ according C/ M+ b* s$ PA; }) A5 U) ^3 v! t9 D g th: j, C8 `! C$ a6 g E A , {# X# R, v; N- |9 H) Cw ( j: Y( |& l+ ]0 L) o- L5 {c 7 b4 p2 A8 y8 {9 T' z: n+ `: u1 F4 _* @- \) Q' k+ W9 W信号牌,! r1 h" f5 \# l; G8 X$ R& w 由一系列指示灯组成的目视装置。每个指示灯都有相应) ^* i @4 Y' q' K { 的标记,用来显示 * p8 ^/ h3 G: n! G) q6 V2 q+ n ~4 k6 A+ Q& x4 s$ a* g$ n2 A D$ a 防止机翼前沿和发动机短舱结冰的一种方法。 1 [# v, w3 \, Z英汉对照民用航空词典B OEING ) c, n- L9 z( m0 ~1 B+ i0 |TECHNICAL DICTIONARY 12 2 ]* O5 u/ b: FAPPENDIX, A supplement to the Airplane Flight Manual * `1 C" R3 |$ x# t3 v( ktained in the basic manual. A . W. p4 J8 f9 R: I3 c* C/ \ollection of supplementary material at the end of a ! L2 v- ^+ e j9 z: n9 P/ ]ook. * H+ b; P0 n0 k. }, \, [" J/ hof the j \( u! N( m7 v5 k9 Rrsion link on the landing gear. # _6 T" }* j$ Q: Z0 @: YAPPROACH MODE, An autopilot/flight director mode3 d% K8 ]" n4 D. N& e which is a combination of localizer for roll control and 0 g, C* a, h0 O Cglide slope for pitch control. This mode is used when full" }* S( j2 F! [! b instrument landing system is available.( }% p4 k; _" A% n APU, SEE - AUXILIARY POWER UNIT/ c9 n6 j) _! z ARINC, SEE - AERONAUTICAL RADIO 9 i" w8 V3 X' u' ?* bINCORPORATED 0 V8 C% N( U8 I8 ~% n' ~ARM, To make ready for operation. # L. V7 J5 \7 X' k8 ?( F3 |附录,& Q u$ A3 I; y; \: m7 u- k 飞机飞行手册的附件,包含基本手册中未提到的飞机形7 }5 z# k0 Z; V! }) e! u. | 态的其他性能。是附在手册末的补充材料。 0 U4 ?1 g) ^) q3 X! ]; q顶销,8 P# z( i) `5 L 用于连接起落架扭力臂两部份的销子。 ! o: w! t/ @; y6 a" Y3 Z进近方式,) u' f' y4 y0 N8 _ 一种综合了控制横侧的航道信号和控制俯仰下滑信号 y3 i, c- Z# t, l" @5 {& s' F6 g的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系 Z+ B" w# q9 h1 B+ g% K5 e 统正常时才使用。 c; H& o5 i! s/ W! }, ?( u& u 辅助动力装置, ! t& S! E2 Y& }) o8 E: r见Auxiliary Power Unit & a F C4 e7 a8 u- Z" v2 acontaining additional performance for aircraft . F; F' o4 c$ E pconfigurations not con ) `+ V# w* |+ D# f" E( ~c+ R& Y4 _ ?% G) Y' \ b# o: N* e3 w- E* P4 y4 `, ^ APEX PIN, A pin for joining the two sections- k0 O% p. {5 e. \4 V( ]( [' H to( v( |; y5 U2 J. d+ w+ U1 C+ ?0 }- z6 ]1 @- ] 航空无线电公司,7 x# c$ U* y% {" m* P 见Aeronautical Radio Incorporated. 2 ~8 e; e1 l6 @6 f- e预位,- A( L0 p" R; [5 } 部件可以开始工作的状态。3 G% R' U3 L4 X4 M" k8 d. x 英汉对照民用航空词典B OEING 3 W+ b/ _; |7 \' fTECHNICAL DICTIONARY 13 : p$ o. T o8 tARC, The curved track over the ground of an aircraft : [9 M' H. M2 p5 q) Tflying at a constant distance from a measuring - u( ?0 Z' {$ r* L. \% J0 Qequipment (DME).5 T, g. ^* }0 T- p; x in the limits of self-contained system # l) d( F" z6 z& C& Fapability.) F* f) |, I8 I6 J/ S& D8 I, Y tem for opposing or restricting8 d- ]: m" V8 e5 S& J8 w ovement.& }: @& ~; J- m4 L( H/ X SPIRATED TAT PROBE, A sensor that measures total / h. ?/ Z/ I+ a3 M9 ]0 ?8 }$ xir temperature when the airplane is in the air and that ' W4 u) J1 E) {, E/ R3 f8 Aeasures outside air temperature when the airplane is ( M" J( D& ^& K4 yn the ground. The outside air temperature is measured7 p m' J* C0 H; I8 n A SSEMBLY, The fitting together of a complete structure ; J9 K/ o' y. Q d3 W) F( _SSUMED TEMPERATURE REDUCED THRUST, The 2 M# d: d# `1 {, `4 ~0 pATC, SEE - AIR TRAFFIC CONTROL) T7 V5 z2 W4 x7 x) k0 `! g7 }0 T; s# f- I 系统中所产生的一种用以抗拒 / ^! O. z* i x6 C8 G! E- c; q作或限制动作的力。/ M2 @* p+ \; \1 Q 头, ' b7 f' R, B& z% I7 l3 c; K- ?用来测量飞机在空中时的总大气温度和在地面时的外6 d% F9 m2 [# ^ X3 Z$ M E& _' d 温度。地面外界温度的测量是利用引气将外界空气吸入2 F0 Q d+ {! D! u' @) B; r o& g1 W 头,以达到测量的目的。 8 m5 \, t+ E' ~1 B配,, @2 B0 m7 q# B1 f5 W3 z3 s4 ~+ s 一个完整的结构或组件的过程。1 C. S; c$ D4 Z3 f) x8 Z 假设温度而得的减推力, ' m) I) E, ]% s7 K* q推力设定值时,假定一个比实际外界空气温8 }2 [( C7 V3 I; k# R- j 空中交通管制, 5 ~9 }9 Y( P H$ R5 y9 ]4 b/ l0 P见Air Traffic Control ) d+ O; A* L" w9 ^3 _6 a& GAREA NAVIGATION/RNAV, A method of navigation 6 L7 {! Q& L2 a' m0 v8 I+ S/ Ithat permits aircraft operations on any desired course 3 W- [. I A- P% h: j$ s; c! V" ewithin the coverage of station-referenced navigation 8 n0 A# J2 u; k. j; w+ }* F# |( Vsignals or with i `0 W# c, r: t5 P* y c+ T' J) q% w6 R- B( T* O% u ARTIFICIAL FEEL, A force developed in the flight- W( ?4 E' v7 b) |/ @ control or brake sys+ a5 P' S9 s) @ m! w+ V2 W/ X8 V1 v A3 l0 t* w* K1 @* j ~! R0 i a # f" O$ \% {+ J% r5 ?3 V7 ]m" x4 V6 O+ `3 Y% B% z' N6 F6 f& h* N o / O1 _2 z8 W7 Fby using bleed air to draw ambient air through the . c/ x- a, Y- i+ ~4 F$ z' ~8 Usensor when the airplane is not moving.& X; I1 S4 g& d0 m6 q0 _0 \ A) N4 F0 y) ^; U3 I or unit. . A9 ^" Y! }7 V* h8 x: ^A . @% j$ _9 W# K9 Blower thrust obtained by setting a higher than actual. t; V: N8 G5 D# b2 N# u Outside Air Temperature (OAT). H- f {. O5 X, Y7 }$ B 弧线,$ ?8 ?, Z5 h7 M1 k6 \. r) m5 Z 飞机在围绕DME台等距飞行时的弧形航迹。 ; S% J- f; ~+ F: g& {2 p# ]区域导航, ! A* Y) B4 l1 @2 T容许飞机飞行在有电台参考的导航信号或自备系统能 / Y* S& i5 \ o. `6 J力极限范围内,飞行任何预定航线的一种导航方法。 1 |) |) e, C; }+ K模拟感觉 * i/ r% x# u. n: e$ a5 {6 [, Q在飞行操纵系统或刹车 - ~# V2 x/ p6 Y6 t: {: q5 B" A/ Y, l, \7 u$ a# x% p3 P吸气式总温探. Z( R$ ?; ~+ K( Y( Y! |* n/ h: ^9 M/ a) {+ B2 Q# e- a s# C" W8 B7 l1 y( r8 Y2 F; N$ c组合成 ' Q% J; c l% n3 p- n$ l; a8 c/ a! n/ }/ Y- ]4 D! u在选择起飞 3 B/ s4 n, O! a. t" Y度高的温度而得到的推力。用这种方法可以减少发动机的* d, o( Z/ P1 K4 I 磨损和维护费用。 - }' P$ p; h+ w+ ^- `; b" c. F# O6 j& }3 x: N英汉对照民用航空词典B OEING; T6 @/ p! D% u6 E" P TECHNICAL DICTIONARY 14/ I% P- P6 o- O: P, a- I- ~. k ATE, SEE - AUTOMATIC TEST EQUIPMENT/ p# c" J/ \3 t- f1 K ATMOSPHERIC PRESSURE, Pressure of air due to the0 w& } e" @$ C2 X3 F arth's atmosphere, expressed in pounds per square ( c3 s/ G. l+ J1 P) sch (psi) or inches of mercury (in Hg) or millibars (mB).$ |( o+ q4 n/ D j* L6 ^9 r" N TTITUDE, The relative orientation of the airplane with" z8 J8 E/ @2 X" V- A spect to pitch, roll, and yaw. & s# I F! j) b! q: NUDIO CONTROUSELECTOR PANEL, The panel in* G- ]0 g! u5 d4 t8 s5 A. m e airplane which controls and selects the routing of " v2 w6 G' g! N! ^8 o e+ V0 Gudio.) g) a+ J2 V# }7 W- G! D, _ UTOLAND, Automatic landing using the Digital Flight : @' [; E6 d. V* ~4 _; control System.$ G/ D0 K9 q& A3 _, i n. 8 F% X- k% a4 {# _$ |M, A system+ Q" _1 O# }6 n$ V# c, F omposed of all necessary subsystems needed to guide7 c( Y4 @; x6 B6 B7 f. \6 e3 J e flight of an airplane.+ Z0 [5 Y8 `- F+ }$ t EQUIPMENT, System test 7 |% {$ Z- o: {) k, o' J# @- @3 Uquipment that operates under computer control.) Q* h, m6 ]* m* J! D$ ^ 装置,

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e2 C$ X6 n+ e6 B2 O in " P# O& w D. q6 j- h* |A$ ?" J' z' x, |! u A0 @' F re ( |5 \+ z# }( J- Q4 f! L1 LA ( A- m' x" W( K( _! R4 W8 ~* Dth9 }7 \3 w9 s3 H/ @ a 8 o( w6 @' z! D3 T0 j4 _2 v: dA6 V4 Z3 S- a0 ^: g' x! j/ { C0 [. I8 B7 O( t AUTOMATIC DIRECTION FINDER, A system which 0 m7 q O: p3 j) J2 {) p5 mdetermines the direction of a radio statio9 Z, I% P5 E% a0 x: k AUTOMATIC FLIGHT CONTROL SYSTE % X6 P; i5 W/ O) y8 }4 b" ]$ D2 l/ vc $ k' O: u# T/ I7 R; q oth + Y5 L5 D% G& ~$ rAUTOMATIC TEST4 }+ V9 k7 |8 G, B e* x. o, |6 @( i, L, s* ` 自动测试2 g0 }8 d8 e$ q( z) r4 P 见Automatic Test Equipment. : Z# S. r. `. X, F5 @大气压力, + O1 V ]$ Z# x) R由于地球周围的大气而产生的空气压力,以每平方寸多3 X8 ~# @+ ~, n; }" x. G 磅(psi)或多少寸高水银柱(in Hg)或毫巴(mB)来 # n m. T3 W" \( X5 t* E3 x* O示。 * A0 ?6 f* j3 }' ^9 R飞机姿态, 8 K- V+ p* w' T- J* A& r4 ]7 D飞机与俯仰,坡度,和偏航有关的相对方向。 . Z$ \# J+ v& E# G音频选择面板,! |# m3 V [1 R# W: | 飞机内用来控制和选择音频通路的面板。 $ b8 a$ L! D) U' G: M2 i$ p自动着陆, ) r& p. }9 P: O0 @/ b5 C7 q使用数字式飞行操作系统来进行自动着陆。 * d" v1 J. E; G+ R; b的系统。 2 H. q0 h6 b& e$ z9 q W% z8 {' @! w' n$ ]" G 系统所组成的一个系统。' j: z3 i% Y* t4 ?: m 在计算机控制下运作的系统测试装置。 3 t N2 a. d4 [6 s- i* ^0 V; m& [- K4 z$ |+ v% ]( j0 U! w) ?1 u! H& X5 u4 `$ Q自动定向仪(ADF),- I c1 G& P \$ C# i7 P( A 确定无线电台方向9 p/ a8 w% p0 O& Z$ o 自动飞行控制系统/ Y$ }* j4 I4 E- f8 R4 ~ 由所有能引导飞机飞行的子 ; J8 u, L7 s+ Q4 w' D( g# f自动测试装置, ) n9 ]) i+ ~& G( o! t3 C英汉对照民用航空词典B OEING7 y3 J, X" L" ?9 x* ?) n* _2 w3 O TECHNICAL DICTIONARY 15& y' K( f M- N. z4 t) v AUTOPILOT, A system which automatically controls ; N. z1 |) G7 n, |2 x, C( s; gand guides the flight of an airplane. 1 `! A! y9 }4 D1 g) }& p# Q, LAUTOPILOT FLIGHT DIRECTOR SYSTEM, An5 o" w T- u$ e tor / f: ]" R" n, a/ k4 u* }, t, d" ]UTOTHROTTLE, A system which automatically% c; f- w& a9 Q# u ontrols the throttles of an airplane. 3 Q* p, W% C: j/ VPOWER UNIT, A small turbine engine in + T& l. Q, F8 p8 P! W; ?3 qe airplane for supplying electrical and pneumatic+ A2 V$ i) E6 }' u ower for systems operation on the ground or in flight. 2 N6 B% L% N7 wVM, SEE - AIRBORNE VIBRATION MONITOR0 `: g- c6 m% }& X6 m# C+ E3 M! K XIAL FLOW COMPRESSOR, A type of compressor 2 p3 i8 V- l- c# j! l; Hsed in a gas turbine engine in which air passes through9 ~2 w0 X1 {( d- C7 U: M& t2 P XIS, An imaginary straight line or an actual physical, T& Q+ N" L3 ?% t% p: b1 n omponent (such as an axle) around which a body can- N! R; _* ~2 Q- \5 E6 `2 l8 d! b tate. # J" a5 [6 E$ B仪, 4 B. f/ Z5 Y5 L |5 h4 g3 ^. [/ x; a( d' R% u9 v 自动驾驶飞行指引系统, + F& V* [/ `. S8 V8 g9 E: V8 t动驾驶和飞行指引功能的系统。 1 _2 W2 ]1 y& G2 F动油门,* e/ {5 ^0 p' B& P& A { 自动控制飞机油门的系统。 2 N% U% C' B+ {3 O% E F1 K是飞机内的小涡轮发动机,在地面或空中给各系统提供 * m5 l7 X- @& C+ F/ V3 s' S" {源和气源。+ ^4 u5 `- a. v' g0 _4 p 称。 / d- _+ A; _( r4 C1 C" h6 I载振动监视器,6 x8 n" _$ W/ K3 d" s4 c0 R7 r' H) u$ w 见Airborne Vibration Monitor 2 {: q+ a& j" _. B0 g* Aintegrated system containing autopilot and flight direc7 m0 D8 z- m3 |$ k; H/ v$ g functions.$ d V2 Z2 k9 o; B# i6 f9 Y A1 }8 _ A 0 Q# L" g+ w; V. C1 vc , r- J5 _0 L- L! D2 B. n$ ]7 qAUXILIARY ( g# r4 k) x; X$ l1 vth+ ?2 z: A+ P' r, \ p , M X4 F) D9 p' ~' }' @AVIONICS, An acronym designating the field of aviation* V2 T2 Y( z8 u) \5 } electronics. 8 M4 J8 \( g2 |4 L' jA j" @) |" w% Q4 {9 ^ J5 p( vA, l6 a0 b, }5 _$ [5 b2 X# g/ { u: N* L5 L) g* w Y8 h6 {- S the compressor in a straight flow, front to rear.; Q3 Q, \. X* y( C! p; Z A 1 a4 a1 ?! O7 y; x0 kc, ^% E! U' L% x/ i ro s$ ^5 E P% A# m 自动驾驶% T" ?! }* Z. @' C+ B, O 动操纵和引导飞机飞行的系统。/ @; P( K1 k9 l3 | 一个综合自' v: Z1 ?: d! K; F$ P" {8 } S+ A3 d9 O0 Y1 T4 X 辅助动力装置,5 O$ d3 X4 y" u2 M) c6 q# j9 I! O% Y Y, E, g& e航空电子学, : h: y& F+ q- V是航空电子领域的一特有名$ \5 R C3 D5 e$ g4 s9 Z( @: @% C+ L+ V5 J- f. Q, x* z7 @8 c1 s! p4 X8 Y; U流压缩机,2 o1 D7 K$ }& }7 r 一种用于燃气涡轮发动机内的压气机。空气由发动机的 6 k7 n* m! H, t# y% @8 S部流出。 9 y2 D) X8 d' T线, m9 N# d5 u; x; ]7 \* e 可让物体围绕着作旋转运动的一个想像的直线或实际7 U4 E- Q" _4 j& r4 b 在的部件(如轴)。 & s# ~: g# T0 g+ o, q* A$ |" V0 A. c# W$ [5 `前部轴向流人,压缩后,由后 4 x% s5 ]* ^, Q1 c& Y1 B+ V9 y J5 d" O& I9 u+ I0 [) r$ s0 t' a4 G( j6 L0 t0 @* M$ D; x' n) @- ^: B 英汉对照民用航空词典B OEING ; s5 U( G4 l5 e lTECHNICAL DICTIONARY 16* y* Y e7 e$ a6 O; K! p B/ J: ^5 q$ ]! { ACKCOURSE APPROACH, An approach to a runway 4 S/ d1 u7 M6 J2 N, P( Wversed. : ? p4 }5 g4 w$ X& Y7 g" R$ N# }; I1 \& Uown on the EFIS that9 G& s( K0 ]9 ]$ m oes not readily change, for example, navigational aids. ' M0 e+ @# M. j& r. Y. @5 f% q0 Tvement in the tank or reservoir.) m9 f7 Y4 h5 X. c ALANCE TAB, A small hinged moveable part on the; [. ^9 G z2 l% i+ ~ A4 U ailing edge of a control surface (aileron, elevator,9 P K- V* L+ ^9 M8 F4 D& j" Q 航道进近,& @4 W+ ]; i! O, Z3 N4 P E; q9 Q 相反的进近方向。当反航道进近时,无下滑& Q5 p q b0 m! ^! @4 f 显示在电子飞行仪表系统上不经常改变的数据。例如:; _8 M& C! B3 W5 O: W9 }( } 航设备。- s/ S* n7 A2 p" H7 | 在燃油箱或滑油箱内阻止液体流动的隔板。) W% M5 [1 @; p" \ 动补偿片,- h8 N2 |( h; T2 _: g( ?$ @+ | 铰接在操纵面后缘(副翼,方向舵,升降舵)的可动部。& x% ]) P- J5 l- H0 ^4 z+ [ 与操纵面相反,以帮助操纵面运, P6 Q% n" R* D7 r B 8 r9 F5 Z4 M8 q( B4 p. B' J8 [( swhich is opposite the normal approach. For a) C* \4 G8 S0 q1 p( q; \1 L. _8 r. J backcourse approach, glide slope signals are not " y3 E" v& i) ]available and the sense of localizer signals must be' M2 _$ m7 Y7 Q' B. f" V re 8 _4 ]* E+ v, Z' @) B" LBACKGROUND DATA, Data sh! \- Q- k# v$ N# _2 V+ @& L d% L, ?" G; S0 K" y7 K: l5 x' Z BAFFLE, A partition in a tank or reservoir to prevent* T) s& d/ w+ j) J- T fluid mo7 k5 }( ^$ B' B8 W' B1 q- P4 r B ( \; } b- O/ L$ W. q3 }6 O5 X2 F1 gtr( Y+ a4 L/ c5 c& @$ W0 T. }& e3 I rudder).The tab moves in an opposite direction to the! G8 m! _, K! Z, |% ?$ i6 V, ? control surface for assisting movement of the control & E8 a$ i+ J) D- {1 B/ zsurface. " w9 `) ^5 o* u! d3 ]' M% J* z4 S与正常进近. z: z- ^2 h. p# O4 M" ` 道信号并且航道信号也必须逆反。 6 G6 a8 K2 S# i& u# o背景数据,7 _2 p- w/ J; u, F) h8 c. n9 T3 I3 K: I1 u+ i" t缓冲隔板,8 N. i8 J3 s" [# @$ f }6 b: o0 W ~! D7 F1 F随动补偿片的动作方向 & L" Z S$ m, l. ]3 _4 j! L+ y! s. p动,减小操纵力。' F W* P7 N; }8 w% d' ^) E: L6 y2 Q& u 英汉对照民用航空词典B OEING ' } W! a5 d# I) rTECHNICAL DICTIONARY 17 - I) ~( P! n5 ]0 g2 }* F& ^' P& EBALANCED FIELD LENGTH, The field length/ t4 F/ i8 I4 s {% t3 x9 B3 M' d; w associated with optimum aircraft performance when9 P. r, ]5 R5 F/ t- s% { bstacles are not a constraint. In this case, after engine ; q9 z2 I/ r% b4 \* A Rilure at V1, the distance required to accelerate, takeoff5 H) i, Z1 [9 X nd reach a height of 35 feet is equal to the distance2 Q- f* z9 A2 V1 ~) O: s ALLAST, A weight installed in an aircraft to maintain9 L/ B. d( l8 |/ g' W# ?" ` ALL NUT, A fixed spherical nut driven by the. G2 r! U1 i# k5 D AR OUT OF VIEW, A signal used to remove the flight6 E* q* s8 K& x& o8 ~- \2 K8 R* f AROMETRIC PRESSURE, The pressure of air above/ Z; p( R7 [6 c, r5 {0 i' F g) or 7 D3 ^7 {: K3 H6 L" s1 Amillibars (MB). 3 Q7 A" _: @, f ]' u" b( i ~ATTERY, An electrical device for changing stored/ {* q) g' ]+ o/ {9 \ 性能的场长。在此 * n' b3 U. q7 [# L, K' I/ _况下,V1时发动机故障,要完成加速、起飞、离地357 L# s( B* r% g0 a( `5 M 尺所需距离等于相同速度下完成全停所需的距离。5 i2 S7 W4 [7 M: l; |) T 舱物,9 |+ z1 w; D+ V5 C) L* F- ?4 f 重心在许可范围内面装载的配重物。. c9 t1 a" A; l3 f$ C/ _5 a 形螺母, 7 |4 h' i$ ]8 ~1 g% Y+ K% S' m( ~# s: Y的固定的球形螺母,用以使襟翼和水平3 f9 F) }4 C+ u: P! u3 r0 N! g 引杆消失,# X* |+ O- c$ ]2 J 指引杆的信号。5 U, e( ]) @/ j/ [ 压, . o% k$ e; r8 i. Y2 s/ {压力。通常以多少寸高水银柱(in 6 j- T3 b9 F4 r% |0 k4 q1 a. Z* P瓶,+ P3 n7 h. w8 r8 r x 的化学能转变为直流电的电气装置。2 U; G" a5 r8 b4 P7 p- ]$ d! g2 P o; r+ z3 d( c' K h! o! O9 T3 o! t fa) ~+ B# x9 z# ?; v9 a3 N9 _4 J. j a 0 R7 z9 [7 K0 S5 o# `0 @required to stop from the same speed. * @1 \7 [# i$ p8 P. \8 h! ~ PB 4 v" N ]3 R8 l2 f; E+ ?6 s) Jthe center of gravity within allowable limits. % z: w# P; h6 ^& t. F: i$ ]B$ Z$ y' k5 u# | jackscrew for flap and stabilizer movement.( J9 N( d% u' a* a7 F B + K; S/ }0 l7 _' M4 p+ Pdirector command bar(s). 8 c N+ C2 I! [B+ S* F- \: R, X! G/ N zero pressure measured in inches of mercury (in H9 m( t6 X+ V: Y) R# L' q in2 T3 H1 ?4 O( W9 P" y3 }: i BASE METAL, The underlining metal to which alloying* S9 u: R1 J+ ^ agents or metals are added.4 j3 M7 O/ \/ _. w6 e! t B , p) w8 y/ j2 _( Z, h7 U0 I* Pchemical energy into direct electric current. 3 ]. P/ h) a) Z/ J平衡场长,' W( a( [+ d1 y( Y7 @( s* s 当障碍物非限制因素使飞机达到最佳 2 W9 s/ @; l* O3 X, ^/ s- Y8 D$ {% U' b: }% I' g; M1 \; }4 b/ g- C- H) v( k0 ~为保持飞机 , e) Q. T+ f. C& l& l) D: h" B! g5 C由粗重螺杆驱动 8 t7 E9 D$ g3 z5 O6 c安定面运动。7 a* K6 P; }0 v( j& U" X9 ?7 R6 q+ w7 w+ z 用于除去飞行" U% C4 t0 O3 _4 ~& z2 N6 z, d" g# n' R* d 零压力以上的空气 2 ]! n7 V; q- d6 x+ g0 _Hg)或毫巴(MB)来表示。# `+ Y+ S4 C9 N) m1 g( H) C6 O% S( k 基底金属,. c9 B ^% w3 t 指合金中的主要金属成份。& p& a( M, |5 ~3 ^: N3 a; B( i' m$ O; I5 R; i- k将储蓄 ! [/ B* W" v2 }# J英汉对照民用航空词典B OEING 7 f& k. x7 r+ |" N( a: F6 TTECHNICAL DICTIONARY 18 7 d. z) m; v) H, \% ~BATTER . J s1 r- ?, Udirect cu & T. C( f/ X0 Ipower su' \3 M! {0 ]( e2 }- R0 Z Y BUS, An electrical conductor supplied with % a A2 S. Y4 X2 Orrent from the battery or transformer-rectifier for . ?* S. @' @1 k1 wpply to operating components. / J: U# e q3 U0 L7 u5 l3 S- YCHARGER, An electrical device supplied7 _3 s' Q- l! K; @" D t& h. K ith alternating current, which produces a direct current * e5 R' P2 H9 ^1 R3 Output for charging the battery on the airplane.- t+ B. v t: S9 g( a AY, A compartment in the airplane structure.# D' ^7 q/ ]# k z; Z f CD, SEE - BINARY CODED DECIMAL2 G& ^/ n9 L7 v& g2 `1 y EACON, A device which emits a signal for use as a ]: M" Q4 u6 z/ tuidance or warning aid.% h j3 E/ x* y1 ~ BEARING (NO. 2), The direction from an airplane to a$ K( U0 M1 u) b" m9 Z' M ground station. 4 b/ A; R% p7 d7 \) I瓶汇流条,& L/ g5 Y$ Y! Y6 R6 F T 将从电瓶或变压整流器来的直流电供给工作部件的导 2 [- H) W( E8 x& n2 t体。* S# m1 i6 ?9 \; y' G4 p 瓶充电器, . \2 w p8 c7 D0 c) U$ D" i用交流电向飞机内电瓶充电的电气装置。带有交流电的 ) ?! a% p* {$ N* N( ~. t4 |* d气装置,该装置产生直流电向飞机上的电瓶充电。1 X. V/ s" Q* _ 舱,; `* U( R* D! L6 d2 z9 R 飞机结构中分隔的空间。5 k3 c! f: W- }% w2 P$ ~; w+ [ 二进制编码,( n1 O0 N+ @' P+ O 见Binary Coded Decimal( f& G2 f; p8 ? BATTERY / `! r5 T# n1 J8 j/ x8 M* \7 Nw: q# v! l, q/ P& j4 p o4 Z8 B2 N4 j+ ^ B% I+ a i( e- T B. M# {; D& T4 m B* y5 q1 q( e+ s g : e% M1 c5 h+ _( \, h4 kBEARING (NO. 1), A surface that supports a moving 4 b) ]. S4 ~! O% t$ [& y- gpart and reduces friction between the two.& D8 t o! X. W3 n. b; [/ R4 }; u: f& I C7 B; X$ g! F4 U, q7 [' @5 f& q* g7 q" @; [5 L: e8 ^9 k6 A- k6 V# W) D6 c) k% k8 ]& ~ L1 A. {& p6 Z2 U9 z ?$ J7 d/ z3 |# U6 G5 }+ ?- T' i& T+ \; Z 信标,! }; @7 D( {- C' L6 T' i% j 发射引导或警告用信号的装置。 ! T C$ @4 U" p) Y( J8 j* }" { t方位(NO.2),5 v0 s* K8 R; C 从一架飞机到地面台的方向。 $ E8 n8 z+ p" R% d/ _) {轴承(NO.1), 0 F/ T. u) e+ W' `9 x6 V' B用于减轻机械转动磨擦的机械装置。4 A8 M8 S/ u) m' r! R! l 英汉对照民用航空词典B OEING % M A O: O7 `+ _5 W# Z" z4 [TECHNICAL DICTIONARY 19 6 H2 Y4 T( T& \, m C/ O1 ]. bBELLCRANK, A double lever in the control syst + g- ^. D' Z3 t; Y. schanging direction of motion.8 I o% E9 i7 b em for; ^1 {% j* j: ` I; z ct in the* V+ j% U( \9 U( |1 S neumatic system for absorbing expansion of duct due 4 I; n$ q$ V$ l& oheat.6 p, C: \5 x. f6 H& d5 \ ELLOWS (NO. 2), Corrugated folded or pleated ) k! k' d/ O/ `" A0 }0 Hontainer or compartment used to measure pressure.0 D# R" s) r" v& a3 N$ W, Y EZEL, The part of an instrument case for locking the 6 t! K# e G. O0 _& ?9 k7 V+ elass. , k5 R7 U" H ^# m) ?IAS, The potential difference applied between two; _' y* S8 ?5 B oints for controlling a circuit. q5 |* w8 N- PBILGE, The lowest part of an aircraft fuselage. A place * w8 q/ Z" O; Zwhere water, dirt and other contaminants collect.) _) \( o+ m. h8 M& y- s 气源系统内提供管道热胀冷缩所需要的余地的波状& y4 x) z5 c {+ U 轫管。9 H) Z. `4 @) {) }1 k- @( f( Q 空膜盒, 9 d; X7 J% `' e- ^一种具有波状表面的容器。用于量测气压。 ; U. M. f9 [, ]7 B6 g' `嵌沟缘,! ~; b1 g2 p. \: i8 f 将表面玻璃固定在仪表上的圈状零件。& P) Y- u, @ \ 压, $ M* T# t' d) S& p, X4 y在控制电路的两点之间的电位差。4 |+ S+ ~% R! S9 y& Z( T1 U6 b 机身腹部,+ v8 @2 x9 Q# A$ U3 D2 y 机身的最底部,通常水,脏物,和其他外来物集存于此。, d# P& E" l3 j$ B* U V9 D2 A- n BELLOWS (NO. 1), A corrugated flexible du1 c- a) r4 d; {7 `# }, @) T. Z- ` p 4 N( u1 G% m% i' b8 }to* ~' N3 y" s7 H. o& g B- L# X& W& d6 N# X- V- F2 X- X6 H c7 I; g, X( H! {" k& V B 8 X+ a4 I3 o' }$ p8 Vg* t$ O: S. @5 r( c- j7 D3 f" p B5 \& w7 z0 W# Q% [; i p: @& A. u, ? i) Y+ u1 G m 直角摇臂, ; k. M I& Y6 q& ?在操纵系统中改变运动方向用的双臂摇臂。( O! v" `* G5 h9 w 波纹管,7 m$ I& R6 y2 Y* E1 H# K6 B3 w- ^$ C& Y. s0 I9 s0 g6 r* g, j6 H6 k' C- }* _$ T+ C! F& b; _5 ^% u, ^* `, z2 Z/ o' r* H6 \- L/ D 英汉对照民用航空词典B OEING % w0 S7 l8 ?+ X8 v* ~TECHNICAL DICTIONARY 20& H# \/ S4 p u9 ?1 c BINARY CODED DECIMAL, A system of coding each ; J3 [0 F+ M$ M3 Idigit in a decimal number using the binary equivalent. , @/ I6 P2 k+ W2 c5 B" KBINARY NUMBER SYSTEM, A number system using 6 l5 f" H; @1 ]$ Y" T2 ls _4 d5 G3 k/ `+ X5 P3 t E8 rIT, In the binary number system, the smallest unit of1 C2 ~/ c# p( o3 v formation, consisting of a 0 or a 1.1 R' O# c; M6 n) ~6 |" M ITE, SEE - BUILT-IN TEST EQUIPMENT8 g% b. S1 x' a8 R8 _3 x7 P; [! J LANK DISPLAY, A display that does not have any% U9 U! j/ Q% N3 _. @+ V; j dications, normally due to failure. 7 y$ g: E; }; i- A9 R `, x1 wLACK BOX, A container for electronic circuits to record/ o( O+ z) x* t7 S$ N1 ~ ight data. 9 t6 G6 j' t+ E; c1 qLEED AIR, Air taken from the engine to power various & ^7 `6 X# Q7 y" s4 y) J: iircraft accessories. $ F5 T0 h9 ^8 t1 E- j) _" WA valve in the pneumatic system for air7 g/ g, g0 v5 P0 {" b supply from the engine or auxiliary power unit to the3 z% g0 H! P1 I( E8 m1 d pneumatic manifold. A valve on the engine for reducing0 e: ], Q& f( ~' u( B5 R6 |6 l pressure in the compressor section.3 H: R0 Z8 n/ }6 B/ G) j" j 进制,) ~: [% N% C; J2 {* Y/ m 进制,& f' }8 W" ?4 }, ~9 K# K 一般用0和1)和2为底的数字系统。 6 d" q" Z% t$ V0 k" d# v/ p特(二进位数), 7 x }& l& G5 X9 k% \9 R+ [, B$ Z二进制中的最小信息单位,包括0或1。 " `% \! l4 J9 |; k内自测系统, & j `: k6 l# w' q7 Z$ S. B见Built-in Test Equipment g" v6 D/ Y! { two symbols (usually denoted 0 and 1) and having 2 a$ ?' J* `* d9 L, x- K4 z# j# W its base. ' C5 [( C# D/ ^* i) s0 IB ' j9 c' L' c' y4 |5 | t9 Win$ u: g6 k7 x! R+ G* i1 G- c& ~ B W* [0 g( d; S& @( X- A B - E9 g! n- B% cin; h1 F8 x" [9 H4 G( F" O B . I- q7 {" w* A; ^/ w- Y! A0 Q: s Ufl $ x; D8 D# g9 lB " v. }: T1 @7 t, Q4 \4 i* Aa 1 U- [! f7 l/ G+ j% F0 K9 B+ ZBLEED VALVE, - ?- E1 J6 {, A! `% j二进制编码的十7 I) _3 l3 N9 u9 i1 \4 g6 X" v- V, R0 p 一种编码系统。用等效二进制位数编译十进位数的每一 ! Z, V9 v: |9 R- }位。 ^' \$ I6 Z5 V; U9 r0 k I* i! P6 r 以两个符号( 2 L) {1 I0 b/ h. t/ u4 j3 G' w: O3 q1 O; `0 @& O7 A( w7 o, r) n. a' Z& g# m/ m8 s6 ~! I 白显示, & J& l2 E7 F' [" z通常因故障而造成的显示器上没有任何指示。1 J8 e( N C2 [8 |5 f. [% } 匣子,0 {* U0 g" B) S, F' Q* H 装有用于记录飞行数据的电路系统的容器。 . N7 ~0 v4 \* W6 r( |气,0 c+ [) F* x$ `* z) J. v1 m, r 取自发动机而用以驱动飞机上之各种附件的空气。( r- a0 u+ j/ x8 J# ~ 气源系统内,使来自发动机或辅助动力装置的空气进人" p, w- O7 N0 _. a! U 气源支管的活门。发动机上,用来降低压气机压力的活门。 # r. ]" d$ L" Y& D0 X2 L8 u0 [, Q" A$ s7 k0 e) w: j7 ]3 G' [3 ^' }+ f! x+ g6 ^' x) q3 ]+ ]- U引气活门,0 f( Q$ Y) f0 P* E$ ^ M5 m 英汉对照民用航空词典B OEING) O3 A* f. W* b TECHNICAL DICTIONARY 21 8 h" R) n6 ]" {9 BBLOCKER DOOR, A device on the engine for blocking 1 V, w9 D) e/ S/ G1 Y0 S7 `" ]) j1 \the normal airflow during thrust reverser operation.9 t, t7 b! ~$ j# e' d* ? LOWER, An electrically operated fan for circulating air. ; u' ~/ Z. J2 \" }LOWOUT PANEL, A panel in the structure between; b/ K7 B9 N1 R" U4 r1 s" b( W o compartments that opens to equalize pressure in " ]) f: C2 r0 B% a) y) [4 he compartments. & `$ x$ l9 ~! n7 G6 PODY GEAR, The landing gear attached to the 3 A4 @% R: l) l& K& C9 b8 T1 Sgrounding.! d/ m' N; u9 [; p, M- x* H" _4 Z1 R 正常的6 R; u; N& i8 v2 _" q 气流。 4 c$ p$ b: X8 P8 Z% }: {+ }鼓风机,- s, L0 o7 q1 d 用来使空气循环的电动风扇。1 x. |0 ^7 @, F. }, e& V 压口盖, : f* E2 s' k( v& e5 O Y! r- w& P+ x4 e两个隔舱之间的口盖,打开后可使两舱压力相等。 $ o' [1 v* t! E! w: c. S' I身起落架, ) `. K( s" J8 g7 u( K7 {身构架上的起落架。3 D- M; M: P2 e; [ B " e5 s! u$ A0 t( _5 I4 p( t6 NB 9 \% O/ K0 ^2 t, a" A1 Ftw - T- [. u, A: L# c7 ]& `- B9 kth " r1 ^; Z d- c9 \9 }; I: g. iB , i' j2 `. O( I6 ffuselage structure.6 ~. n5 p% b9 }5 ^! S BONDING JUMPER, An electrical connection between # o5 V5 m* k. H& H1 h7 `a component and airplane structure for electrical7 v5 Q1 c8 `, i& L 阻流门, $ K% t4 B9 u8 j0 P6 Z( _ Q发动机上的一个装置。在反推工作时用于阻挡% D( o0 y" m# V* t1 K3 b, x2 d$ E5 L3 b$ W3 f/ o' q: @1 N$ P- o( I J, D3 m装在机9 G- ?. c+ I% v: D9 @# ~ 搭接片, / A o& _6 A I1 k& m连接某个部件与飞机结构以形成接地的电接头。 9 F+ g* g j9 k# ~# Z英汉对照民用航空词典B OEING$ T2 w9 ]! z' ~: [ TECHNICAL DICTIONARY 22) z* T4 X) ^& h6 m& B/ s F: d BOOLEAN ALGEBRA, A mathematical system for 2 v& X; m- X$ N1 ?8 ?writing combinations of logical statements.0 G5 K( O# J- ?) o BOOST PUMP, An electrically operated fuel pump for% k8 h: E; o( x3 } fuel supply from the airplane fuel tank to the fuel5 g" S3 S' R- D) D, j, E9 l' X manifold. : d% e1 m5 L' w8 rBORESCOPE, An electro-optical device for looking at4 u& B$ H! X: H, Z/ l* s0 H/ { ternal parts of an engine through holes in the engine. 1 ^' i9 g5 v3 O% worescope ports) " V! ^* e6 K+ J0 mOURDON TUBE, A curved flat tube in a pressure gage ) {( d* R) P, ~4 rr moving the pointer when pressure changes inside / P0 D& p2 Q- @; von the ability of the brakes to 6 ? A7 i" b1 E* Qbsorb a predetermined amount of energy during a 9 ^5 q* m( t' v/ {' |) ljected takeoff.7 L4 f# Q. ^( B) a 用于通过发动机内的孔(孔探口)观察发动机内部件的5 e4 O* d. ]" A9 H% W9 |( z1 S 光设备。2 a% S, l. w7 E1 J7 M6 ? 端管, 9 C- q' M) K0 c6 F8 A0 D测压计内的弯曲扁管,管内压力的变化时它使指针移0 e8 g8 Y. t* c8 e/ w7 `/ Z" p 力。& S+ `: O- n5 N0 \& b 极限重量,( G+ M& Q: @* B( H& [6 E+ x8 e& S: @1 s0 U1 s( t( M L0 R! d7 r 起飞重量。 3 m+ b: L! l: v V发动机滑油系统与大气相通的通气口。/ z4 E* R' N6 h8 r in) `3 R' R1 S/ L9 w! Q: u (b, S* S8 B3 z5 t2 E B" r. T) i3 z! D/ f fo5 o! ^- J% C p the tube.$ s- J5 G9 o* x7 o0 q: Q) |1 s BRACKET, To enclose or surround. 0 r$ h* W( Y* X7 F- `BRAKE ENERGY LIMIT WEIGHT, The maximum + r5 y/ E D' c' \+ O; _9 _takeoff weight based. i# o- ]4 d* i" c a 1 O0 x0 E0 m+ K' w7 x1 Qre 1 O1 S7 ^! x* _1 Z, I# I! m7 {BREATHER, A vent to ambient of the engine oil system.- `& n' G7 e- U7 c' `7 S+ y: d 布尔代数, & S: x7 X% L/ F' f7 r& m% w一种用于编写复合逻辑命题的数学系统。- n% m# h, n. J5 g& p- J* \ 增压泵, + m7 i* q2 _ I( D& v从飞机油箱向总油管提供燃油的电动泵。 + U* H9 J3 P1 \" `+ A M孔探仪, + V+ @9 q& Y* g/ ~, j/ R) N+ p! U8 N+ [+ t1 ?3 A- X( g$ b/ Z2 E3 w7 t) q# C 动,以指示压0 @: d" d: ^9 v- j* G 托架,' k6 i+ w& x' J8 h 用于作支撑、装托、或围绕之用。& _7 Q2 ^- g5 F w; c6 F. Y0 ~! T 刹车能量' y) O+ k6 f9 s* |6 i8 W4 X Q2 Y 中断起飞过程中,取决于刹车吸收预定能量之能力的7 Z [1 J8 w) r! [: }6 ?. B! H( Q+ `* b6 u! C3 a 通气装置, $ Z; _! m) a8 `0 X英汉对照民用航空词典B OEING + p/ `% y: V3 {2 D: z, D- ~TECHNICAL DICTIONARY 23' e0 |$ N! G4 ^- _( n; B BUFFET, Vibration of the wings and airframe resulting5 Q3 B$ G% x# E% a from unsteady airflow over the wing; caused when , Q6 Z: V/ b' S1 D3 Oairspeed is too slow, the bank angle is too steep, or0 K a8 A- Q, X' t3 b irspeed is too fast.3 u5 [: C2 ~" Z: e UILT-IN TEST EQUIPMENT, Equipment installed on % M6 V1 }8 V+ o q: He airplane and in airplane systems to test the systems 4 R) Z$ P9 V# j |% Xithout external test equipment.7 `3 k% F$ b. U/ i0 e UFFET MARGIN, The amount of residual maneuver 6 v5 |2 L+ t' J" i' fapability present before the onset of buffet.! e6 K/ {. X8 C, }1 Q UG SPEED, A preselecteed speed to be observed ' a) H# @$ V& z9 [& e+ t+ u, |nding sequence. , r, G0 @; \) ~+ s! \7 ]# ok8 B/ ~# ^! ~4 I, c ng landing gear operation., b+ I0 X% m2 a8 J( R k6 @ 速度太慢或太快,坡度太大,均会引起抖振。 3 z+ g! O% F- B1 {: g. G0 J自检设备, 6 h3 L x+ M; ]3 a5 S4 Y安装在飞机和飞机系统中,在无外接检测设备情况下, 6 |' [' e4 V& U% [用于检测系统的设备。7 u( [" Z9 f* u# C9 m$ m 抖振裕度, 0 ^2 X& I( w9 S% k8 ~飞机在遭遇抖振之前,剩余机动能力的大小。 4 D, E) Z0 V* ? \. U8 i2 r+ [ y标速度, : g, _& z: s2 p& K) H# z- ~9 q在某些机动飞行过程中,特别是在进近和着陆时,飞机3 j: w9 P5 L3 S) i% N9 U( j+ K: { 预定速度。) [' E' n& z5 _: z, M6 n# m 力装置,: P' |; M6 q8 V. Q5 n5 s 架工作的一种机械设备(弹簧或减震器)。 * K& z: J$ G4 C: L流条, . S& h; Y4 _& Z" v( {在部件或组件之间传输电、数据、或定时的单一电线或 b S6 U7 F. Q3 V* C a f5 ~, y' L- t. z5 DB9 _% j4 H9 q' }1 o. J- i1 N$ s th' U9 B9 C$ b1 C# ?; N- @. Z w ; s! T N. H; Q; ^9 Z3 l6 k; WB+ Y; ~# t& K$ n. F9 \& F c* `/ {% r+ b. S B. [' _3 g- B# P/ m J during certain maneuvers, particularly the approach and + [% l) @2 o: z3 K z" x# E6 mla0 q) t; Q- e y) p' v BULKHEAD, A structural partition in the fuselage or ) F9 e8 o$ B1 b) i. A% R: _4 ?9 jwing. - V; l( O; k2 v) x+ Q2 e% qBUNGEE, A mechanical device (spring or a shoc' o+ Z5 ?3 H# | absorber) for assisti: g- [% k* a+ [ BUS, A single wire or group of wires which transfers + ^# Q0 H1 U5 j9 i# Epower, data, or timing between several units or' p) v& o# ^$ r% G! S- i modules.8 Z3 d0 M9 J0 } 抖振,0 C! L& Y5 T6 y$ q 由于机翼上表面的不稳定气流引起的机翼和机体的振' g' x& z K2 p" A3 n( o$ B3 D 动。飞行, k! x6 D9 v* Y G6 I3 I6 D( ^# z- A" F所应保持的 . V6 H [2 R4 k$ v$ y9 y9 f壁板式隔框, 4 E* k3 m/ u& M( q! ~9 J y: f$ O) Y机身或机翼内一种结构隔板。$ n4 x7 ?% f k* T8 R0 k* e8 {* G) e' E" w9 f 用于协助起落+ A0 C" w5 ]1 Z1 l: G' i9 y Y1 K( J4 H$ B% P1 k4 r# A电线组。 6 ^4 H( s+ G6 Z5 L- B$ r7 E英汉对照民用航空词典B OEING: |% [9 W2 n3 `; V2 D9 A# | TECHNICAL DICTIONARY 24

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BUS DRUM, A mechanical connection with pulleys ( i8 h @6 U. |1 scables in the control system.1 A+ v7 L' |1 ]1 ?4 A and& a% D U' }$ e; ~$ ^6 e! H l circuits for control and protection of3 G1 D; p m- \1 j1 d lectrical alternating current supply to the airplane.' f7 d4 Q$ \, c" K$ s duct for closing and opening the duct " L1 @# \$ ^) [* |1 d0 o- y+ Wassage.1 R* y2 E. v) B" ^2 b* Y UTTOCK LINE, A vertical reference plane along the: z1 u5 J0 ~, e. C. x# A selage for horizontal measurements of the airplane. " A! B6 N1 ~* q6 T接。 / y) T, J8 v; L7 }组件,内含控制和保护飞机交流电源的电: w: L) X1 d; P+ v, R3 z5 B/ l$ O' ] ^5 O8 x1 r: J+ G( j作动简控制的转动装置。用来关闭和 $ g) r0 P/ q: \* D启管道。 2 P' P3 Y- h* k- @$ T沿机身走向的垂直参考面,用于飞机的水平测量。 - o2 c( t1 X G* z* CBUS PROTECTION PANEL, A module (black box)3 x/ K/ _. u7 T containing electrica. n$ a* Y' `6 J1 Q$ K e4 m G6 U' ?! ?0 N& O5 h7 J, A BUTTERFLY VALVE, An actuator-operated, rotating ( x9 u' }& k, E' T7 }device in a . B" o! s6 V! Bp & `9 N1 B8 ^/ D, O! T: GB 8 S( S, A8 Z. G" l' O8 J5 ufu2 | k' _% F) m+ v7 H, t1 C 转动鼓轮,4 V8 W7 x! e$ O( F 在操纵系统中,具有滑轮和钢索的机械式连 4 y& C1 j( z5 f' r, M汇流条防护板, 8 z [* U" p* M黑匣子式的 9 n. @- y! ~, ^' ]5 c, g# E3 p& Y5 y! e蝶形活门,. q, ~! g' M; ?( R 是一个在管道中由5 U5 Y0 j1 U2 W! u+ F A+ L" K# ]. Q! Z 纵剖线,, x1 C. c+ q7 `% Y4 W6 K5 ? 英汉对照民用航空词典B OEING% V# s# M$ x; C M$ w% v TECHNICAL DICTIONARY 25 " w) _# ^% O& ]* c+ mBYPASS VALVE, A valve through which air or fluid will# N; L o, s( f flow if the normal flow path is blocked.3 T# w5 a4 ^8 X% d0 D BYTE, A group or string of binary digits. A byte is u" T+ N9 w$ b2 H sually eight bits long.4 z' L6 k5 ^# v% S( r- Q ABIN ALTITUDE, Atmospheric pressure maintained 0 C, q. d4 g% {* Z& uithin the cabin, indicated in terms of feet above sea . w5 f+ l& \$ x. o4 M0 @ALIBRATE, To repair, adjust, fix or correct the4 U0 y$ P( U g2 @& ]- Q% \( Q easuring capabilities of a measuring device. : m7 ^1 e7 l- f1 z+ D; rALIBRATED AIRSPEED (CAS), Indicated airspeed / V7 Y- {+ E' z1 Z# iAS) corrected for position error. 3 C1 k `$ z( [) b# g# D- ]nical5 `9 E7 X- Y t; Z* L omponents. & a$ \0 v: E( R- S0 B) s/ [' i/ K: j' C节, 9 W: j& y/ a( N3 m0 K一组或一列二进制数。通常一个字节长8位。 0 i# a( n5 _" [- T5 a. ]7 G& p舱高度, , ^9 u7 [* F$ t. t% A! V座舱内保持的空气压力,以海拔多少英尺表示。 , V. ~0 F% t" Z+ `* F准,7 I' H# ~: e. _' E# Z4 y+ C j" ~$ [ 修理,调整,定位或改正测量装置的测量功能。 ( {- ~6 q" o) V X- Q正空速(CAS),/ c: D- K! Q* I9 B$ F7 p) Y9 w. o+ l 在修正了位置误差之后的指示空速(IAS)。 ) I' P. T7 r: q; I4 d* z2 P$ S用来移动机件的一种转动装置。 5 e+ I, O [. H7 Y& p0 n. Uu 8 @# J& p) M0 a wC5 m+ P. G6 a) `, p# P: ^6 Q# Y6 A C: ~, b5 X) |( d( v9 Y% r! w( ~ w6 z* t7 ]. b& @, B( V# k5 D level.. ?2 Y( A( t7 |& X C0 |8 X% x$ z, M9 ?4 u! M3 G# c5 l. O m 5 h8 V6 i. H& o& w3 pC : ?% n6 {; o& u- t# T(I; `2 y' M$ F/ I( a1 B9 K5 d CAM, A rotating device for movement of mecha1 Y, `0 x$ ?6 b% p0 K C 1 V6 \! X- i8 P/ _旁通活门 ( B, F) R2 M* r" j0 Z气流或液流在正常通道阻塞时所经过的活门。# U! a- s1 C, Z6 b5 J7 r; R7 j5 A' P$ |: D% z" Y8 m: y+ V Z9 }* G+ n5 y) i% G- {* d. b& W2 p; ~/ [) V( }( T0 Y* _ 凸轮, r7 o! L# @# j, P5 ~# a+ w/ y 英汉对照民用航空词典B : `& a0 e: h$ n) {& wCAM-OUT, An autopilot condition in which the actuator 8 t: `6 x! A0 b( |detent piston is overridden, either manually or by the0 p$ V4 _# Z( t ther autopilot actuator. 8 q+ Y. ]" X! }& k6 O: vAP, SEE - CAPTURE! z, Z* c- q/ K APACITANCE, The measurement of electrical energy * \) ~! h! S! Vtored in a capacitor (condenser).! @% v; m% I3 j! Q3 v APACITOR, An electrical component of two metal5 A, ^; w9 _4 D# e8 @, \6 w lates separated by a dielectric material, for storing 7 Z; h- s% I) e- tlectrical energy.' x4 T& ?# d$ P5 M8 C! M CAPTURE, An autopilot or flight director function to \9 u/ c5 e# t2 I' _5 ] w acquire a selected mode. % B; m- n5 V) tCARD FILE, A container on the airplane for printed8 j( \0 |. F4 e circuit cards. * F- ]6 L1 w( F$ [' S一自 " ^( }' K2 |# B$ ^动驾驶舵机所超控。 ; w2 _5 i) z2 x) f( u0 d/ D截获,0 u5 s/ `* N& ~6 i7 F* d 见Capture $ ~+ E1 A I" x( R; [o * F" H4 ^% |$ I' l) p U7 B. r1 VC0 ~+ j. Y5 v6 B+ b C ' {& \+ J! H. K4 Cs 7 k* C( d7 k) i% {0 u* GC3 D# m' I' p; ]4 T( V p' k- g4 e h/ H% t e) c, L5 F6 @$ v 凸轮不工作,: R! K! H* h- K+ Q! r9 V2 Z0 M 一种自动驾驶状态。此时舵机锁定活塞被人工或另 * c. o4 t# a) U, p' ~3 _; a% b& t! X2 z) P' `6 q; O# V: i电容量, 6 N3 c' U- y" r5 y: G7 W6 A电容器内所储存的电能的量度。 ; [! W" b& k E% f" J1 i. W- w4 w7 K容器,# X/ K0 A3 k: E- H7 C! l D/ h5 u 两片金属中间用绝缘材料隔开的电器。用以储存电能。0 W3 L. y) q3 d% F+ Z2 t( D 截获(CAP),6 l5 q, c. J3 p! v( K0 Q4 _ 自动驾驶仪或飞行指引仪的获取选定方式的功能。 & K/ K3 [8 g1 J5 g线路板盒, 4 _" C7 w' e8 Y# J3 \) Z' Z$ Q* V1 }飞机上安装印刷线路板的容器。 x1 \" [+ X" F! G! I; w& D2 e) c: {5 i% Z7 Y& n2 u OEING 9 m& [0 h' T" D4 w/ oTECHNICAL DICTIONARY 26 # q4 W2 B0 a5 a9 s8 X6 ?1 a; O英汉对照民用航空词典B OEING. G p# A1 A0 J: X2 L' v6 Z TECHNICAL DICTIONARY 27) ^7 o% t5 [# Y* t& U0 | CASCADE, Two or more similar circuits or amplifying, U/ ~% p9 ~; N stages in which the output of one circuit provides the* J. ^- V- N L3 j7 F5 A put of the next. + b; O) m+ i, |- E* @ASCADE VANE, A vane for turning the engine airflow5 A! q5 x5 Y2 D: ~) A4 F uring operation of thrust reverser. " O8 @2 T1 q* w sASE DRAIN, A drain carrying lubricating and cooling " a$ Y9 l* K. j# O# p- Suid from a hydraulic pump.& N3 {0 u, u0 r ATHODE, The element from which the principal ' x6 w: b& K* O% Q0 G7 utream of electrons flows.) G: b$ q/ d: I ATHODE RAY TUBE, An evacuated glass tube with a 2 c0 O: x: S* L" \! e CCEILING, The height above the ground or water of the ; ^ Q+ e0 h: ~4 s4 U. z" Jbase of the lowest layer of cloud below 6000 meters ! A3 P: `$ v+ o5 u7 X* E(20,000 feet) covering more than half the sky.$ v( h& h" P: B+ ? B 程。该 2 F' x/ R x" G9 N( s7 D5 A程中,一个电路的输出为下一个电路的输人。7 t% F4 z$ j0 g% h( t: H 叶栅叶片,/ y) A2 m* g; e9 g C# \ 在反推工作时,使发动机气流向相反方向流动的叶片。/ Z5 F6 | U8 t6 }/ @7 v+ _ 匣余油管, 9 B& m; V2 l* G( t/ x+ s9 _液压泵多余的润滑液及冷却液的排放口。 9 I+ ~, _: y9 c; ]; K5 e3 n. m7 S& c极, ( ]( O M: V. l7 ?) T& ^" c电子流流出的极位。/ _* B( i2 r# `8 W 极射线管,& t; J) R+ e! U0 M$ w 有显象屏幕的真空玻璃管。用于显示信息。 # t; g% J" Q. q7 N% I: C7 r云高(云底高), 1 M, n z) q, H( f. R( \$ f6000米(20,000英尺)以下已覆盖一半以上天空的最% b: C1 q: s3 L8 s0 i 低云层底距离地面或水面的高度。 ; G6 A5 ?/ w B/ G. u3 t- yin8 E" ~: L- v( m! T! `/ q2 M% o$ o( ] C & p4 e3 j1 R: c5 |# fd ; F& g' k& Z3 G, D. z" SC4 w+ {, z' m5 q/ V3 p* K fl" y% I! I% f0 j- \' R+ q! W# \* o1 r0 | C , K' k- }8 ~/ S1 w& b: D2 s- cs; h* l8 O' \; J; X K3 t C 7 S% }6 Z, {( A/ U1 ]viewing screen, used for displaying information. & m- _6 N5 F! D2 Z级联, " [5 a/ O8 Z( {9 q两个或两个以上的类似电路的逐级连接或放大过 % \0 s* D1 Q/ m. C/ j( ~4 v2 y/ J Y* Y/ a# Z. ?" S0 r" d: P; A1 w1 V/ B& v7 U" |6 i1 z4 a8 m3 s. F9 A/ _3 v4 K/ F- r$ V一个具+ _6 n# F+ g Y/ J5 u4 i/ d, x 英汉对照民用航空词典B OEING % p- ?; q( O/ R/ e$ MTECHNICAL DICTIONARY 28& N" z% g1 V! s' u: S2 J, f) U3 Q CELSIUS, A temperature scale in which zero is the: O* o+ f) s" ?5 x+ F; U freezing point of water and 100 is the boiling point of 3 M+ N' |& T. K& d) j: L2 K0 @water. + x, N5 y7 A: Z( q4 h+ u& y8 \/ k8 nCENTER OF GRAVITY, The balance point of an object & m/ w9 R- X4 t" V9 t6 k5 B4 H; n2 Rr rigid structure expressed in terms of percent Mean. N/ q7 v+ w1 o% g. b/ W erodynamic Chord or in inches from a reference point.7 c6 c5 f0 [4 c: {- g6 X+ |$ y ENTERING CAM, A cam for moving a mechanism to a . X9 z9 a) |( `8 T" f) Reutral position. ! D3 Z8 K3 w- k6 RIGURATION, A configuration of the $ y" j1 G2 s' C6 k! U( }5 qircraft approved for operation by the local governing z% Q3 r3 P1 m: r. Kgency. , G9 \8 E+ [5 n# E5 h- fENTRAL PROCESSING UNIT, In a computer or& j% A4 A. B8 z; O. W1 n igital circuit, the section containing the arithmetic and 7 J G8 P& _% C" b+ kgic,control, and internal memory circuits. 6 O+ @- v0 M2 {, O# qENTRIFUGAL FLOW COMPRESSOR, A type of6 H! \, y: ^8 I, K1 ?/ Z ompressor in which air is taken into the center of the$ O8 O" ?! Y6 b; v' o: l peller and is slung outward centrifugally into a diffuser - f A" A$ m* B2 ghere it is slowed and pressure is increased.6 @. k8 R9 Q6 k% D6 `: L) b CG, SEE - CENTER OF GRAVITY8 F: d& }9 x5 V! ?4 O1 e 构的平衡点,以平均气动力弦的百分比或- W1 N5 @9 U, _! | 某一参考点若干英寸来表示。; J1 ]/ f- H3 o0 Y! {& W e1 H) Z 中凸轮, / S7 z' J! }1 s1 A5 [将机构移向中立位置的凸轮。 9 G* `. n8 o, F+ F \格的装机状态,1 r- l8 p" ?9 e* [ 由当地主管单位批准使用的飞机装机状态。 " @: x4 d4 a$ R+ }中央处理器,( A: l' }. I: N8 H$ R- A$ b 计算机或数字电路中含有运算,逻辑,控制和内部存 5 J' F! R) L5 Y1 L储电路的部分。 $ T+ Q8 C9 |, e; M心式压气机, / \/ [( C: {6 [) S压气机的一种。当进气到达叶轮中心时,被叶轮离心抛- H0 L n' }4 `8 z 进人扩散器。在扩散器中气体流速减慢,压力增加。 1 ~" M$ z3 }6 E v重心,# \, [3 c. P* c2 _3 n s" S 见Center of Gravity3 m* ^; I l& C& D4 M! R7 k8 s* O) o o * |# F& \' Y1 s3 CA * Z! h1 b5 D" m( W. g; XC : B7 x& {0 z/ Un ! G- x$ k, {/ l# f+ V& HCERTIFIED CONF$ z) k3 ^8 Q1 q/ a+ q3 L a 1 o/ E# H! l: l$ H# Wa " L6 M' I- a8 H& a$ a5 F$ c/ yC 7 ]7 x* }+ U9 o" r3 zd 9 ?0 h; w9 [9 E: g- ilo c$ j$ v* S% h0 r- f, kC! M1 |) | \; ]% j c+ L5 V' a3 G2 W6 k im+ b4 l. \1 C$ F1 g* k* ^ w6 u z) v% F) X6 }+ X6 u% e 摄氏度(°C), 1 G/ A! m& |7 |* c9 ]5 Z温度的度量单位。在此单位中,0°C表示水的冰点, ! s) I3 t) @- A& P" x100°C表示沸点。 * J2 d, A5 [# N: I8 L重心1 v0 q; V3 @( {, N. A5 m: R 物体或刚性结! @; m4 l0 l7 [2 M, W2 P" G6 n" H' s# @# B" M* c, n& p0 U: l" B/ [+ G# J7 t! z( s d1 K. a* b: D$ U8 {2 V4 v3 D4 U% U. `0 w; k/ w3 w- g" E e, S英汉对照民用航空词典B OEING9 W0 o. j# `6 S; { TECHNICAL DICTIONARY 295 x3 K0 A+ z9 o5 W CHANGEOVER, Conversion from one mode to another. 1 Z! o5 _8 a9 {HARGING VALVE, A valve for supplying air or fluid to6 r! @; l$ I9 }" p9 A2 p HECK VALVE, A valve allowing flow in only one J w% X/ D( u% c* Sirection. See Non-Return Valve. 0 J# Z4 r% e; Q) r7 |3 e9 ~# u: NHECKSUM, In a computer, a summation of digits or; n& A$ c; @, Y- w! s( C its which are primarily used for error detection. " | L' @1 s) C6 q( ZHIP DETECTOR, A magnetic plug in sumps of : \1 d$ X3 Z- e" Z+ c: v3 Abricated components for detection of internal failure of; u' b: k* R8 D2 Y: v7 x e component. ( |( {2 z5 J$ K8 `: gHORD, A structural component of spars or frames., Z1 L( m3 h7 N9 v& [ 添活门, _) J) t2 n l; y$ _* B 器充气或加液的活门。4 v9 |) y3 o1 K7 ]- _# r: t& L, A 单向活门,# _. a) u, o( W% Z" d+ s 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
C3 Z$ s$ m! ^. c- o, a$ `, G1 T4 B a reservoir. 8 S- }$ i& u7 ?( BC ; Z$ ]9 Y/ T! ]d9 ^8 Y8 y+ B" B- z- B% j% w6 _ C a) q1 E. K% Eb * e" v, l/ {/ {! J. yC0 F" L: T1 ]* H lu: `5 I1 r4 I9 L' a th ! G' p5 B0 m* P/ Z, p4 B& {. X6 kC' V1 x( J5 a: p# M5 m' ? 转换, 1 J7 T) Z+ c; d$ p5 a- _由一个方式转换到另一个方式。4 `( S) U! l3 G: Y8 D3 ]0 R5 G% u ]/ [' k/ O- S7 ^+ Z( \# V# `0 q 用来向储存. n- U3 A3 q6 o! }# X! x! o7 u- d7 e0 S总和校验, 4 X) u F2 s& b6 U; d$ g: v9 |计算机中,把那些用来探错误的数宇或位数的总和进 & N8 \ c& U. M e; b4 v求和计算。* G; n& L3 g* t0 I% D 属碎屑探测器,9 V: X0 |$ F* t5 _! C. O) A 装在被润滑的部件滑油回油管路上的磁性塞子。用来探 e" M% V& L: Y& |& z0 D" e& o 部件内部有无损坏。- K( j) W8 F q 弦, - |8 T8 {& e b% A; m4 } l& A* ]梁或框架的结构部件。; I6 x1 d$ u9 E* Z6 I8 G Q/ D* u( E6 n% L: ]2 _$ e& y! l- {5 {* u6 S4 }! J6 a0 l C; @% p' x8 f7 |8 @7 F' R4 c3 k4 Y( Y5 u& ^! o3 a5 H9 b6 X( r+ } S* l3 R9 P( c) G 英汉对照民用航空词典B OEING0 z; W F# l. q2 X+ w# @, P% } TECHNICAL DICTIONARY 30 , c2 k7 r& o/ j9 N' m( c$ r, jCIRCUIT, A closed path through which current flows # N8 w2 i! @/ o. L& \! ~ tource. * A' M7 m0 a0 R! @& S, c$ bIRCUIT BREAKER, A device that automatically1 V+ S' w2 [5 u# J- W4 K, w7 N* _ eactivate the system.+ g7 E6 C- N- U lear of all non-frangible objects which $ x) N7 O6 E: M1 W! ^ay be used as takeoff distance available when 9 T$ S$ k5 r" i4 U3 d+ q P/ \alculating a takeoff weight. 2 e4 Y. v/ m( _+ r4 [r water under the control of the appropriate 4 D* O# z }6 Z4 m, a! `+ guthority,selected or prepared as a suitable area over 6 z1 Q8 E r5 q6 q+ O# {8 chich an aeroplane may make a portion of its initial2 c9 o- w- K4 U& t) e; @ limb to a specified height. # J, u9 W! k6 J1 I8 j) ]increasing.) T, h% ?! A( J sed & }1 r l7 e; r; uLOCK SIGNAL, A continuous string of pulses used for - ]8 V; b0 v. s3 p& i7 _! ^. a) h: U开关,* g* r1 }) H. S: C0 ^ 故障情况下自动中断电流以保护线路不受过电损3 N9 N. U" O$ L6 B! [9 M h 体障碍物的区域。在计 , F9 C$ M& k& M$ q% N4 Z起飞重量时该区域可作为可用起飞距离。; m5 u4 J0 D7 v( O+ k# ^ 是在有关当局管辖的地面或水域内一个界限明确的长0 U* v3 y( ~5 l0 i 形区域。在这个选定的合适区域内,飞机可完成初始爬( P; c8 E. L7 d 的一部分,上升到一个指定高度。 / z) m0 L4 a5 |9 |) l1 `# z; N. |2 Z飞机高度不断增加的飞行阶段。& Z" P4 i: O& m" i& V8 Y 钟脉冲,/ b3 H: j: q6 E2 D! b0 o3 a3 W! P6 f5 w 步的连续脉冲信号串。 ; Z$ m% n* z& V8 q# i! Z9 Ofrom a source, through various components, and back! l$ u5 r6 d8 G. U& Q to the s : J' V) t" E% FC - M; s/ u" O( ^- S( Iinterrupts the flow of electricity (current) during fault4 k8 C# k$ w7 M condition to protect wiring from excess current. Circuit + a3 C2 E/ F3 I5 Xbreakers are also used as a means to manually 0 Z5 O( t6 |/ Z- f, J+ D8 od ( @3 l6 `4 N+ e7 S8 LCLEARWAY 1, An area beyond the takeoff end of the [2 x6 i, ` h& k6 mrunway which is c . z" |' D: g$ ^1 D! tm0 N/ r* S$ S9 c9 v+ e c , k, O3 w; H- C8 E! m- c* ACLEARWAY 2, A defined rectangular area on the D; h+ z+ m l ground o / X' K6 h5 M. q5 ^( Ya 2 Q7 U! a6 t) l( S9 ]' H* a; Aw1 _7 d, u0 W1 m* ~9 y3 t: t c o# j# X) r- u6 A3 Y6 N0 M* fCLIMB, Phase of flight where the altitude is . `9 y# ?" Y! GCLIMB LIMIT WEIGHT, Maximum takeoff weight ba ( Q4 n% @/ S2 ^* xon a minimum climb gradient with one engine 7 m G" x, d d, \ R+ tinoperative.1 T# w1 D. [7 H) u0 D+ u C, j# G3 h3 G4 F. S3 {: X& { synchronization. # J: _% X0 {$ o O( H4 ]/ c' @电路,5 Z# R5 i0 f' |$ t 一个闭合的回路。电流由源头流出,经过各个元件流回; k0 P) K/ B+ ]" B, d; c1 E 源头。# M. O0 B( i' y/ B7 f- N0 c0 F# I# E3 }: X+ C' d7 L- C6 l能在( P( ]! W1 v* g1 }& ] 坏的装置。跳开关也可用于人工使系统无效。 , g- ^+ n2 @ s X* h一号净空道,1 v* f1 A( j( |$ D 是跑道起飞端以外,不含任何刚 4 j1 | A$ w1 ?2 H5 ]4 C5 u, o$ ]二号净空道,2 B5 S. B$ ]( z4 p& C2 D1 C# x* Q) Q. w- O$ X9 Y' {- ^; F e$ r: j6 K. f* B8 t爬升, 1 H8 p8 O* V/ D5 \* U9 q爬升限重, # c8 f# K9 K+ w- G取决于由一台发动机工作时的最低爬升梯度的最大起 ! f/ v/ ~$ v7 _+ `飞重量。 0 p3 R6 s& R4 Q* h" U5 @. z4 X' D" x0 h# r8 Q1 F, y$ M 用于同5 Z+ S& `6 E2 ?7 ~1 K: l 英汉对照民用航空词典B OEING1 f2 p3 X5 j5 _6 d1 R% w TECHNICAL DICTIONARY 31 % J) x% a" Z8 [3 L6 S1 Y; y' wCOALESCER, A device in the water separator for' c# D1 q+ H& |+ A ollecting moisture from the cold air.) p( A$ o. t; A2 I n antenna with a receiver or transmitter.: t1 W( v4 y8 T# j) q* `7 X he cable has an inner conductor and an outer) j3 } `* U1 J% v( q0 M' [. O rounded shield. 1 o( x4 W! ^$ R; n% g9 @ting one inside the + m1 [/ r; v1 E G2 kther for rotating the low and high pressure( Y& @" t( _3 y5 ^! R6 | ompressors by the low and high pressure engine2 t2 @- A: Q8 R: r8 y. J, `9 k rbines. 7 @* M$ m9 r$ \8 h6 IOMBUSTION CHAMBER, A part of an engine for2 y5 q* ?2 d* I+ ^8 | urning fuel in the air supplied by the compressor.$ V" q/ s# v4 P) e( F, p 置。 5 x8 R/ L6 V# B# f4 `6 n+ L射机的电缆。电缆2 G, e3 Q" s0 B3 T$ r/ Q8 P+ ^, g; n- M 中心导体和外层的屏蔽所组成。 {- e/ ^# T/ \ 两个套在一起旋转的轴。用于使发动机低压和高压涡轮7 Z% r5 p6 h& V2 k) `+ T 别带动低压和高压压气机。 , J+ H q9 V& Y8 j烧室, % S, ?3 H: C0 G8 p8 M* S ^8 a发动机的一部分。用来使燃油和压气机所提供的空气相+ F5 {0 _' N+ ^4 Z; N) | 合而燃烧。

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发表于 2008-12-24 21:38:35 |只看该作者
c% R; b. t+ D" T1 C COAXIAL CABLE, An electrical cable usually. [; f- J; u8 `6 v( ? connecting a+ O6 t9 b" K: v T * U4 C6 c3 ^5 G7 z* Fg ; Z1 {# L7 p- Y! h/ mCOAXIAL SHAFT, Two shafts rota $ n) N1 [* D7 ko1 q+ a1 ^/ u' u/ l* @ c $ L r" u% _+ [( ftu7 {6 o! V# x2 D C " M4 b N: K. mb 7 z' K6 K5 ?9 M6 R凝聚器, ( X2 ]1 G/ o/ E' u- a水分离器内收集冷空气中水份的装 ) B6 @8 f7 X. Z* }3 w0 _1 p同轴电缆, 0 d' Q0 S: R1 @; m( v一种通常用来联接天线与接收机或发 7 z4 N# b1 C; k8 b, E/ e! D. R0 ?# H5 w$ a 同心轴,9 Q% ?8 O8 h5 N! s1 M; v: x4 g" T" F, l# {" A9 {1 k- _0 J1 I; g; ?% m7 Y$ J8 k, Y) ~6 R- X4 E* ^+ b" Z 英汉对照民用航空词典B OEING2 E1 C6 ]5 l6 q; n% G. e; H TECHNICAL DICTIONARY 32$ _5 P R, W* H. X6 f COMMAND BAR, A flight director pitch or roll comman ' S0 U4 ^" y0 ]& i$ d- ]% J( j5 M% Uindication. . r0 u' C0 h, j7 Kd4 @( \4 L; m$ u- _7 Z( x OMPANY ROUTE, A route flown by the airplane" r8 X# G8 m/ ]+ X7 v OMPASS LOCATOR, A low power, low or medium! T8 R5 O2 h1 A1 f0 _8 w, o) B' T6 L equency (L/MF) radio beacon usually installed in0 s3 B `' N b) l2 o/ h onjunction with the outer or middle marker of an8 z) P& `1 ]8 M) A tor (LOM), A compass 5 v! V9 F8 Q" U9 l" U" Plocator installed in conjunction with the outer ) S b0 Z* C& N/ ~9 |marker of an instrument landing system. {( K/ |# E" L! h ss8 u6 X/ |) u0 ~ le , V$ Y9 R" @5 DOMPENSATION, To offset, balance, or counteract.) v+ R0 h3 A) Z" ~& d z1 j OMPENSATOR, A dual capacitor for changing the fuel/ t9 h! T! h1 M) B, F" G+ V aging circuit capacitance due to changes in fuel 7 A$ H4 F( d# x0 e% l! b- M* ~ensity. 4 O' k1 a: K" g8 m# ~* }OMPOSITE MATERIALS, Non-metallic materials used ; U5 P0 H5 s) |r airplane construction. Fiberglass, Nomex, Kevlar,+ E# ~8 g) ?4 W' h3 O4 l raphite Epoxy are composite materials.; i' ]" o# k& g P# e; J' N! d 司航路,# H' H9 c" r+ n: Z 在飞行管理计算机数据库内由航空公司飞行7 G8 b& A3 b9 l* H. y T& g 盘定位台, * V& }) {4 N6 U! x与仪表着陆进近系统的远距或中距指点标配套安装的6 x9 q& B% ?! m: Y: ^- C9 ^ 功率、低频、或中频无线电信标装置(低功率NDB台)。 % Q1 ~# Z& |* C; d0 R2 S1 q* A程序中用来导航。/ f4 B0 M9 \4 _4 ~8 x# y 1.远台, 3 C' n$ v; f1 [7 Q与仪表着陆进近系统的远指点标配套安装的罗) p$ q' U1 l9 d& C 盘信标台(NDB)。 * g( V' o f) w" Z# A U3 f# J偿,0 K. T+ [( u3 H: i' \4 N) y. |/ p 抵消、平衡、或中和。 f* H" B' v6 {9 w 偿器,9 X; H% Q7 U' K1 e# _* k 在燃油计量电路中,用来改变电路上的电容,以与燃" T! s6 t1 W" ` 密度改变所引起的电容改变相抗衡的双电容器。- z5 v. g e- W0 ? 合材料,/ q. V0 x* s7 d- R- b! _ 用于飞机制造的非金属材料。如纤维玻璃,Nomex, ; N, Z5 W3 ^: y4 }0 nevlar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 1 G: J! o# ?( [3 `* q4 Boperator that is normally stored in the flight9 z) j# y u. Y5 Z; S% C1 } management computer's data base.5 y: Y! h6 G5 H4 o C ) b8 s1 w3 F4 P+ f: X, sfr9 L2 K' E* H6 P# S: K c , ?( H; U" R8 d) W' K* winstrument landing system (ILS). It can be used for 5 c# }& X) \( j5 q7 _ cnavigation as authorized in the approach procedure. c- |7 @2 ^% Z9 a/ n/ X: N1. Outer Compass Loca ( O( W& b0 V/ f. @+ o6 q2 r2. Middle Compass Locator (LMM), A compa * n6 v" s) N1 g2 D- glocator installed in conjunction with the midd$ k4 p$ h. ?# v* k marker of an instrument landing system. ; Q5 h& _+ L9 {+ b }6 ^C 7 F5 }4 f+ P. ^ v; k" oC % v# ?# R: D! z% A! D1 Q' l2 xg! n$ [3 {) D, g- H( ?- Y. o d8 u* o2 z) F- k1 f& ]- o C' P S6 W& n& _9 m fo 6 i! Z! r- c2 l% d6 n) D9 Dg2 {, L8 o# A. i$ z 指令杆, S9 q/ ?. q. S2 }" Z 飞行指引仪俯仰或坡度的指令显示。 % _" y6 E6 y( U0 f3 E, N" m6 d- w& H* e9 w. r# [$ s8 i 通常储存 + Y2 z; _# f i. T* T的航路。 + e, O" S2 l3 Y8 q# d# Y! F4 U& o5 i# m$ u) B- Z0 Z6 q" I( h& h. L- i) X m' w经认可后在进近 4 [# z+ C1 h4 |, [: I2.中台, 7 e: }! |. t$ R0 N8 ~与仪表着陆进近系统的中指点标配套安装的罗 8 C: Q+ i6 V6 q+ O盘定位台(NDB)。 + F3 P, F- b) n2 z3 M) `# p b& C5 @2 o! U5 H! d- h9 s, {: |0 A# D% D$ S# s! v1 x5 J. x2 ?' V1 U# C! R' K h0 S2 r7 hK # Q; z$ `7 E: G# o% p8 v/ _英汉对照民用航空词典B OEING . O$ u+ m; h6 V- H# t0 N' ^* OTECHNICAL DICTIONARY 33: }# \7 y/ S, m" C by : I5 `4 }- g- E- i. P3 U# ?or increasing air2 s( j/ _6 d. B- T5 J+ X0 P ressure and temperature before the air enters the4 a/ m9 h0 S+ Y% x% M: \3 ^8 X ombustion chamber, Low pressure compressor - front0 A* m6 i( s+ S ection of compressor, High pressure compressor- rear. |. a; n; f' S* [5 Z) o5 E OMPRESSOR STALL, An event that occurs when7 E: a' }% O* i" Y# } ere is a complete stoppage of air or reversal of air flow ! H* c8 b- R1 s" ^4 ?& ECOMPRESSOR SURGE, SEE - COMPRESSOR* K) @9 D. n" Q# Z" W$ B STALL COMPUTED AIRSPEED, Indicated airspeed4 a3 j- N, W4 U! O corrected for the static source error. 8 a( u7 t M* Y! T0 ]/ X4 F的机械轴来驱 1 j. [- I" `( X* {( N,用来增加吸进空气之压力和温度,以供燃烧室使用。 7 }9 u3 b; G/ \8 c压压气机—压气机的前段,高压压气机—压气机的后: x+ R* c% U8 |3 |1 W6 ~$ a1 ?8 ]* B" t; l8 @气机失速,7 w+ E0 Y- w# ?* g! o4 M' @3 ~ 当气流完全停止或通过压气机时气流方向逆反的一种 Q j, {1 m. I- w8 i压气机喘振, ^8 O2 A0 p3 [0 U# |+ c9 M" M$ k 见Compressor Stall 7 k- k) O$ B4 H* u& \COMPRESSOR, A rotating part of an engine driven $ W( c% p& A& _& h# T0 U0 ea mechanical shaft from the turbines f 6 f6 q& n6 y2 C' U8 F* [( S: f$ _p l6 z9 i8 p% S c ( m' Z1 k( q9 Gs5 p( _* G; w8 k# a: [8 l. D. x section of compressor.+ ^( }% n8 @ g k1 ]% o; W2 E C' l: R! A9 ?1 t6 H th % {: f; f- y! O, G) }# ~through the compressor. $ Z5 y) d/ f0 b% |+ J压气机, 5 N$ `! w! p2 f/ `' F发动机内的一个旋转部件。由与涡轮相连 3 d# X4 X' u2 ?$ u' [& ]3 B8 N1 |+ r& q3 Q* F! K9 |6 v5 L. g! _3 ~/ f' ~5 X( r1 B2 w6 M, l2 V0 V4 W9 f 现象。, a# z. j0 [' _; R$ r6 `6 k# g* x8 h0 A 计算空速, + p& K* \/ E9 U) s& `' H- @修正了静态源误差后的指示空速。 , F* o T# G, |英汉对照民用航空词典B OEING- [: i7 b `. ^5 Q m TECHNICAL DICTIONARY 34

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发表于 2008-12-24 21:39:27 |只看该作者
COMPUTER, A device that performs arithmetic , x1 R" S( x& w' r$ p/ G; O0 ooperations, manipulates data, and makes decisions.1 L* x* x+ i( b# U; [& P _$ u ditioning 1 X$ t) g) |. tthe air and the' e0 s% b/ O% j' Q+ W8 q frigerant or moisture vapor is changed into a liquid. / }2 a! y- _* _& B' |0 Gine: K' v% W, L8 o$ O! k' t2 e+ ~ ONFIGURATION, The position of flight controls, - |! ~& U3 g, L" s3 g2 Z: T! Vmissing which3 e( R5 W s. Y/ ?) X& E9 o may affect the aerodynamic performance of the( [8 Z+ o( G# _: C0 j airplane.9 I2 ~. t \! R4 L 置。7 Z% u6 Y7 f/ V 中能使热能散发到空气中,以及使冷冻剂或湿3 g: k- ?; k' i0 O- G 转变为液体的部件。 , q+ v# n9 I- |连接到飞机结构上。+ c8 l5 u: d# G! p 态, ! t% ]# g5 B3 R& Z: g! S6 h% L定飞行阶段中,飞行操纵面,起落架等的位置。+ X& i7 D! j4 A1 j5 e ), / @$ B! z! g, |6 G* t, Z受到影响。# J" L: t3 o2 x( Q* u- }2 o CONDENSER, The component in an air con 1 P; h9 `) x* A qsystem where heat energy is given to/ R% C5 w# D9 F1 g0 K1 M( F# @ re0 z- i; u( G8 q$ w( c, P6 T* b CONE BOLT, A bolt in the shape of a cone for eng : i7 h0 R* S. n% k8 aattachment to the airplane structure. ; g; H0 g6 m2 R% lC 5 m9 v( d9 m; N% J! qlanding gear, etc., for a particular phase of flight, e.g.,* E1 l' W/ n& I/ L/ C Takeoff Configuration, Landing Configuration, etc. " \) H: G# u; k9 oCONFIGURATION DEVIATION LIST (CDL), Appendix # N# k- a S3 i$ W" B3 |in the Airplane Flight Manual (AFM) allowing operation- G, k3 z1 q+ z" x' H( b! f of the airplane with certain airframe parts % a0 M4 b3 N" h& ]1 O计算机, , o4 d8 N2 _6 t* g" G. T能作算数运算,数据操纵,和决策的装! L0 I8 f$ X: G; m 冷凝器, . A( U5 \+ @2 I, w2 d" g9 F空调系统 1 w# w7 V' V3 H" b1 T# S, r2 K+ a! J1 { 锥形螺栓," a8 I* q( U: D: k" Y8 ^2 u8 j 外形是锥形的螺栓,用以将发动机: |* c. D) s3 h3 {# Z: D4 L0 |0 { }) ^3 T1 c! ]: j/ H在某一特 - r1 r4 X" C' E如起飞形态,着陆形态等。 ; E/ I9 ^7 T) @( K# X: \缺件单(CDL ) u( H7 J _" [! l4 ]! D飞机飞行手册的附录所开列的飞机上某些零件的清单。! p/ n. M: [* ^' b2 v% b 在缺少这类零件时,可以飞行但气动性能可能 6 b9 }1 f3 G- K* L7 c英汉对照民用航空词典B OEING7 `' c8 }7 O: }( L" a: E/ W 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: ~3 o( d/ L0 x* o+ `" q5 G component for changing variable engine gearbox speed& K" }1 x+ Z$ g3 Z ONTROL AXES, The three axes of the airplane which, E3 l: Y0 d$ ?+ P1 a& i4 W1 q re perpendicular to each other and pass through the v" f# ^) ~# @' [ enter of gravity of the airplane. 1 P; u( y3 I+ u3 X6 Q- T( L. fPitch axis - Horizontal or lateral axis, passes through% ^: c9 S" T! o) X3 A1 R the airplane from one side to the other - , l& D( k( H/ ^% Ynose up and nose down control is by : T4 K+ G5 @: I9 c1 M$ Gelevators (and stabilizer for trim). 2 g v0 r2 C/ q& c+ a0 uRoll axis - Longitudinal axis, passes through the # u6 P; G! }" o# h, m0 |6 q0 Iairplane from front to rear - wing up and 5 P/ p! P7 q9 I: O, M2 {wing down control is by ailerons and 2 }! c8 G% Z; `flight spoilers.' z0 `/ @/ q3 O. [ Yaw axis - Vertical axis, passes through the2 s4 L! e4 y4 U) {4 _5 n* @ airplane from top to bottom - left and 2 w9 f/ j' Z5 d* }6 M( W- i# `1 tright control is by rudder. $ N# P% {2 E5 b% V2 f置,6 Z5 ?5 q& D$ ^: ^$ g, C 制轴, 6 X- |) D. S D4 n! h& K通过飞机重心互相垂直的三个轴。 $ r! y0 P: j: j6 i2 ^0 E7 H俯仰轴—又称水平轴或横轴。由飞机的一侧通向另 ( e/ `2 l4 i9 B8 q" G$ m; ~/ ?侧。飞机绕此轴转动即造成机首的俯与仰. ?8 {0 A; J8 X" m& o+ n 俯仰控制是由升降舵来达成的,水平安定 6 m$ X# I0 ~/ g7 @则为配平之用。 5 r6 q$ \1 j6 @1 b. P7 _7 n横滚轴—又称纵轴。由飞机的前部通向后部。机翼6 p0 X8 a& m" L! u5 Z4 @ 下运动由副翼和飞行扰流板控制。5 R+ D# b7 u" F! `& J, s 偏航轴—又称垂直轴。由机身上方通向下方。飞机7 X$ V3 H8 K0 t" k 此轴转动即造成机首之左右运动,此一运2 u. ~" G0 J$ q8 T$ {0 w 由方向舵控制。 ) G1 L- g; \( x% C, q+ Dto constant speed to drive the electrical power.! j. e. ~* Q( n+ A% {6 X4 |* X+ o C* ?, @' Z2 F" f+ A$ l, h a( W9 ^4 S# ^7 A; x$ [ c * a$ ~7 ~* W2 T) C) G6 }恒速驱动装 ' v: x5 ^4 E9 O7 w$ U将发动机齿轮箱的可变转速转变为恒速以驱动电源的6 A7 h0 H3 s5 V' o 液压机械式部件。$ \% v; S# ^) `3 ~5 R9 D1 T$ r' n) z+ a* [4 b- G3 d3 Z8 N4 @9 a* W+ k5 \0 W4 R8 n8 L* v: c1 [6 } L5 i/ a; h7 o1 z% ]' j& {. ~' ?' A* d& s! l9 ?1 S. v/ `2 y ^) s, l1 t8 {& P" K英汉对照民用航空词典B OEING8 i% Z3 B* v4 @! z TECHNICAL DICTIONARY 369 q V5 i. \' \5 E+ y6 i CONTROL COLUMN, A mechanical component used 1 o8 c; J- E+ G* ^+ G: U' x+ ars3 ?- o, D1 x/ |$ l4 }% Q5 A3 a nd elevators.7 G4 K) C. {: ~1 O" D ONTROL SURFACE, Moveable panels on wings and. v) p* e- [% h/ w il for movement of airplane on pitch, roll and yaw axes.* G1 P2 y; H' h- p9 D2 ^ ONTROL TAB, SEE - BALANCE TAB ( `4 V \# P6 t1 NONTROL AREA, A controlled airspace extending$ O5 J/ K5 S% ?# V pwards from a specified limit above the earth. q7 Y+ d: a: M m( W9 ZONTROL ZONE, A controlled airspace extending ; ?1 @9 a0 n% e c2 o; K- zpwards from the surface of the earth to a specified I2 ?$ b6 F4 z, R pper limit.% x( G% G8 f9 O0 F0 `3 q6 h is ! g& v4 N3 U# I* C* L2 ~o IFR flights and to VFR flights in accordance- m! ~: }- P0 |: a e0 i- I with the airspace classification. 8 T& X& l4 W f5 h" A机械部 7 b# l" v. w0 a$ }7 b4 Z+ U$ m0 X: p' o `! F' @9 {. m2 K 操纵面, ) v( r4 _, R/ i; e( e! T' p, H机翼和机尾上的可动面板,用以操纵飞机俯仰,坡度,: L5 P0 b! O" S# h/ |+ A$ Z 和偏航运动。 2 D$ ^9 f6 S0 t# O2 i操纵片,: u0 M0 B i$ E/ T& O, s+ y 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 spoile0 j% m5 I4 z7 p2 W, E! s3 V8 x. R2 E a% k" i. ?% W. {+ j0 b5 r9 }) b& C" n C ( H7 ]. o8 @. H: c4 w/ e Pta% _+ C- S) W. q- w8 q C( ]% d* o* d1 N C8 ?9 W% @/ G0 Z% G4 Z q6 _6 A u0 U# @1 |$ C2 X( ~ C" I' m0 R6 {" G5 _: r u& ^& H/ o, i4 P. r# ?& z9 p8 B% P u 7 J$ \0 b$ ?2 b0 J! e+ wCONTROLLED AIRSPACE, An airspace of defined 6 O& s3 x" ]# t5 m \' Ndimensions within which air traffic control service % G6 T# U c5 g+ Z- t! k) L' r U+ ~4 W* kprovided t ! b5 |& H# o# t( g5 f5 a驾驶杆,6 | B4 A$ o- d! { 飞行员用来操纵副翼、飞行扰流板和升降舵的 " s4 n5 q. _6 t. k$ M0 A3 R& r N- N" Z i5 q. ?! ~% `0 e1 o7 R管制区域,8 T1 u" H2 Y9 c S8 A 高于地面的指定极限以上的受管制的空域。 ; p7 X7 q0 D8 }6 B3 b$ F! |) W' L$ F制范围, $ x% d+ q- v. q2 T; E1 c由地面到指定的高度以内的受管制的空域。. ?. |1 h, Y* |$ w6 ] 一个范围明确的空域。在该空域内,仪表飞行规则飞行# a( |0 g6 l2 P 和目视飞行规则飞行有空中交通管制服务。' A( b2 ~6 E/ Q4 i% ^ X, n9 R3 e9 J5 K. W2 ]! ]. K5 \( |5 [0 |受管制空域,8 n* R3 a: R) E4 Q( p9 n7 P. ` 英汉对照民用航空词典B OEING9 W; \% T( }7 `' t2 ]- f TECHNICAL DICTIONARY 379 j7 Y2 }9 H" |2 s9 T- N) u CONVERSION, To change into another form. ! p. M1 `% w, |2 a, NCOORDINATES, The intersection of lines of reference, " U$ n, [0 U& e- g- ksually expressed in degrees/minutes/tenths of minutes: E$ T) J2 ]; R0 G f latitude and longitude, used to determine position or ' \8 e1 H* Z# x; O$ v* kCO . |/ C* K0 B) Y8 n) ~destruction of th + h) S5 f2 A2 k1 c) U" y# gchemical conta " R: z5 c4 R& [COWL, A remo/ ~( V4 h3 U5 c, L for access to th " G6 I. w$ V7 `- [Fa 7 q* Z4 g" M# }: ~% ?Nose Cowl - Front section of the nacelle for air inlet% I9 B# ^8 H" P4 v+ D to the engine. 4 Z8 Y- u4 A8 I2 x z' E6 ISide Cowl - Cover around the sides of the engine. 8 O( x, C( z- p$ T2 Q, U2 S5 x. nThrust Reverser Cowl - Cover around the core & X$ ^ D1 d1 s u6 f( `$ ~! g* n0 wsection.) _% \4 j8 \5 `: g Translating Cowl -The moveable outer portion of the0 O' p1 k( Y! ^6 `& F& Z1 s thrust reverser cowl which is , L3 s+ ^% m; T6 Z2 Y1 J) j- _operated during reverse thrust.7 C+ \1 N. y3 A6 u 标, 6 D, ~! o' ^+ X. r B- ]基准线的相交点。一般以经纬度的度/分/十分之一分 $ X: a5 ], l+ @: d读数来确定位置和方位。' j, t. {+ ~2 _& V1 s- F d 腐蚀. V" G8 Q8 u/ _3 E" e' g/ ^% W 动机外部可拆除的罩子。发动机上的构件必须要取下9 a) F2 _6 D* `1 Q1 v) J4 H3 x. S 流罩后,才能够到。 ) c6 [3 G1 n B) d1 m* T5 C8 W6 F1 x9 h机的短舱的前段。 3 k. L7 x$ @- y C# R. z7 o/ R% q侧整流罩一发动机两侧的罩子。 % N. \" O7 O7 d反推整流罩一发动机主体外的罩子。$ A Z' q p, c4 O 移动整流罩一反推整流罩外可移动的部份,在反推工 * a: b7 L+ i" X- s7 Y: e2 F- r作时使用。 1 M, x) j' z% i; ^' z2 `% B3 qu & c5 J& ^" y4 e8 L3 G! L* Go ) B: m3 e* }$ w' `1 o1 klocation.8 t) K- d. U) B8 z! C5 ^ RROSION, A chemical action which causes gradual * E# G) E" |+ F0 Q, Y; Re surface of a metal by oxidation or( J3 n" P+ R! T3 B( X mination.7 m" y6 `/ v( z2 B, ~3 @8 u vable cover around the engine sections0 N# C- I+ B9 x0 K* V e components on the engine.6 d6 v$ K& ?* k+ K4 q: D n Cowl - Cover around the fan section.5 G2 q* i) d: \, U s* t/ b+ G 转换, * e+ x9 x) h5 t0 u+ Z1 y! l改换到另一个方式。 ' m" k* H* ` x6 C# X; f5 k, V0 M0 V2 T: c% B. y: W7 [: p' ^! g/ j A6 v0 m6 U! @$ v1 L; H氧化或化学污染造成金属表面逐渐破坏的化学反应。) Q9 M* ]# }& K3 _4 I$ J 发动机整流罩, 5 U+ f' V8 K' D0 C/ {6 Q1 T$ t( U' [( u' o ?6 l) k8 z" z/ ^! o# W8 h8 Q% \. z0 T1 O扇整流罩一风扇外围的罩子。 % w' c) U0 s7 o! D' J前整流罩一引导空气进人发动 % x1 H3 s" c4 @% }& x0 P; B) ^6 g英汉对照民用航空词典B OEING- {( _; k8 I& {! j TECHNICAL DICTIONARY 381 N) U e8 h) _+ P0 F k6 l CPU, SEE - CENTRAL PROCESSING UNIT " d" Q {8 i& @7 h$ b0 ]6 w0 [/ t6 MCROSS TRACK, At 90 degrees from the desired track% R- G( [! N- H) L/ J f the airplane. For example, cross track distance is the 7 V& E) W3 G6 ]% L8 f. Uistance from the desired track measured 90 degrees " Q5 p3 o9 E5 }om the desired track. 3 b- M( u: c" G8 ` |ROSS-CHANNEL, Electrical wire(s) connected from s. D5 j$ D _7 ^, t) R6 Q6 A% E6 U ne system to another like system, for example, FCC ! w O! b4 B4 o+ _" to FCC "B". % x' D F- l% K; e+ M4 q, ~n adjacent engine or one on the other side.% K0 @: H x* D, [ l crossfeed5 s- W. @8 p0 o* J- T% l anifold for fuel flow from one side of the airplane to the 0 I) m% F4 E) \5 S2 H0 ether side.: Y7 U" Y+ R! G' ~0 j1 P re2 d/ j1 U$ M) W* y RUISE ALTITUDE, An altitude or flight level ; P# i- X- }+ G7 t! N+ \9 S/ N" r5 a' v2 v6 u) _ o( h( A+ R/ M$ r. ?, p d# M4 Z* I7 Q5 y! g: Y fr ) e# i) c! ?5 {# b' B) p3 HC5 S5 m1 l0 k- C o ( Y+ b1 W" Q! d8 [- Y# r& J8 \ [2 \"A# j8 a1 d1 ]' ?6 Q4 P: |+ r4 n CROSSFEED, An interconnection between fuel/ y( L, ]5 i/ o9 S2 {) `3 @ manifolds for fuel flow from one side of the airplane to # P* Q' p7 f; G% u4 i+ k& f1 Ya ) E4 q, s9 z: _- B$ S N& ZCROSSFEED VALVE, A valve in the fue 0 i; }0 a) T6 o( C" Q: h+ Bm 8 o% a: i" d2 [( Ko( x7 t5 q6 F# W, K7 V7 ` CRT, SEE - CATHODE RAY TUBE$ W4 Z; e8 p4 ^8 J4 {1 S, Q CRUISE, Phase of flight where altitude and speed a 1 s; E! {. F7 I+ P9 Lbasically constant.$ P* l+ x; L f2 h, o: T% _" D C - R- y" |0 Y* X2 L8 rmaintained during enroute level flight.+ ]1 ]& H" r9 ?5 t9 H- ~ 中央处理器 ! [7 y5 ~, l2 f& Q见Central Processing Unit. 7 ]5 h, Q' a2 r+ P1 e/ W交叉航迹(XTK), 9 u. m* y, V& r5 }4 G0 Q3 p与飞机预计航迹成90°角的航迹。例如,交叉航迹距离% p: b. W* w% B 是用与预计航迹成90°角量取的到预计航迹的距离。; B! c/ y6 U7 G) |- L# z/ A 通道跨接, + L+ z0 R( v( [7 ]/ H/ v电线由一个系统接到另一个类似系统。例如:由FCC% r. T3 T* E! p8 c" ^ “A” $ l t; R( n# j9 ?" j; x接到FCC“B”.$ h% N, c5 {( Z0 d* V8 ? 机身另一侧的发动机。 ) t- Y5 v- Y) o d1 ^- c" k于使燃油从飞机的一侧 $ Z$ w. E+ h5 [( P H向另一侧。 9 ^3 Z. E# j. Y见Cathode Ray Tube 9 _1 ~8 e# L( m, G& A5 P交输, 0 v" i7 C: O* S燃油支管之间的交连设备。可使燃油从飞机一侧流向邻) \$ s% d" \; f! {7 O* f 近的发动机或在/ H; T' I- b2 V* w6 c) G 交输活门, " W \- ^& k8 M% _9 f3 d燃油交输支管内的一个活门。用 : [7 T# `! h5 ~. V1 X" u1 y9 ] V/ `! _" | 阴极射线管, 0 |2 J2 J7 P0 G.# G- f/ R! I& z6 Y! ^ 阶段。 0 N: O' ?$ d( w2 s$ v# L7 s航高度, 2 P. b% @, T Y飞行期间,飞机所保持的高度或飞行高$ g% i. t( ^7 ^$ H7 I 巡航, 1 I: M. l: }3 K飞机的高度和速度基本上没有什么变化的飞行! m9 ?3 N8 Q. E7 J1 x, P8 R* T( ~3 ], f" t+ f# T7 g, `% \, Q4 n在航线上水平6 A0 Q6 }6 y" W. F+ A1 D. u 度层。8 G2 T9 i. H; F1 N1 R: f 英汉对照民用航空词典B OEING9 n& Q: ?4 P4 g) x TECHNICAL DICTIONARY 39 3 y& p+ |2 b: m/ w9 UCSD, SEE - CONSTANT SPEED DRIVE4 R' x& q/ @& p; U$ R# C) P CURE, A chemical change which takes place in a resin9 D$ D$ p- ~7 d5 G. m and fiber based component causing it to solidify.# g) d* h' e! ` CYCLE, A complete series of events that take place: Y0 e, M! c7 ^- R& U+ ` gularly normally in a continual sequence.7 l O5 N; x: g, q AMPER, A device for slowing down or limiting 1 h; g2 C4 Q( j9 Y1 y" ODASHPOT A mechanical damper for slowing down! r6 I" D* |( e ovement by restricting fluid flow. % ^6 R. W; l; n/ ~0 \5 U8 SD - h* O1 w$ }( L! S, n( g3 U9 SATA BASE, Stored information which is used as the + V- `, G. d# u, Hba* e8 z9 m9 l8 {6 m7 J DATA BUS, A conductor over which digital data is .* Y [2 T! ~2 x0 d+ n0 ^; I transmitted.* J2 N$ H' l8 d- V% q# l6 D DECELERATION, To decrease in velocity. * M0 S2 ]; k) s1 f- U: L# b/ L装置,/ X! f' Y: n2 U' f9 X rive5 V: `. c4 D6 Z( s( w re 6 G9 z; z9 u6 q# O/ ?6 BD' v) f% l3 Q; P2 t3 g- s D7 r- l% M; r- x, `. i movement. 2 V+ J2 _1 m5 i& [m, v* Q7 J' R/ p8 c/ G5 f ATA, Another name for information.* f. y. |3 `' n3 e1 ^ D ! F) C2 ]. C/ N- zsis for computation.& c1 u% V! n* M/ b. I 恒速驱动- M2 q; I) d9 `) I9 ?9 r% ]3 h: j 见Constant Speed D . 8 a) b# ~# t1 E6 A期, + K$ s8 T( o; R7 @不断重复发生的事件的一个完整系列。 3 [ l: H7 j% S尼器,' I0 q6 U Y$ `# m+ p 慢的一种机构。 2 |5 H( m% j& O& J2 A. N. O+ P) x+ C8 b3 ~$ }9 T用限制液体流动的方法以减慢物体运动的机械式阻 4 B! F2 t( F+ i! _1 W& ~( Y7 L" o, G$ q1 d* E: y/ \- h8 }料的另一名称。& L' m4 v* n6 j 据库, N7 L) n3 s1 `3 H' O+ }4 Y e8 Y 数据总线, 6 s9 B/ l' a N9 {一条或一对导线,用来传输数字信息的通道。 & u, M, U9 f+ \- U* g# G减速,/ v0 f. [. R0 h2 F! B 速度随时间的递减量。 ; o- C0 ?5 b8 A固化, 4 ~8 b- b% I: y1 W' i C2 h- u树脂和纤维部件内化学反应使之成为固体的变化过程。: O( F. {/ F0 U/ [' ]7 r/ X5 M3 n1 R6 U: h8 R9 O! i) ?5 B6 M6 y 用来使运动减 + W. O! o7 s/ h8 n* Z- {冲器,2 V( b+ a' a! g9 Y* q1 @0 V 器。9 \; o& Y' \6 } h. G. j9 l 据, ! H( x$ N# G5 b& e5 ~3 s9 t4 Q5 B" c- V/ L7 O1 ]: ]2 y: i' e& I ]; l8 c) K D9 j储存起来以便在计算时使用的资料。9 b4 W! Z/ |5 C! i7 z, G5 K 英汉对照民用航空词典B OEING0 Q8 Y8 T. I+ t/ {$ p' X6 x" j) l TECHNICAL DICTIONARY 40/ B; C# [3 `" Z DECIBEL (db), A unit of gain derived by computing the& g% I4 g$ F& J/ m9 o tio of input power to output power. ( T4 V1 B7 X2 MECISION ALTITUDE/HEIGHT (DA/H), A specified - T* t+ ~" K8 {ltitude or height (A/H) in the precision approach at 0 Y; D" I+ A7 E, a( uhich a missed approach must be initiated if the 9 O/ G+ ]! @; V- ]ECISION HEIGHT (DH) 1, With respect to the9 c6 p! W1 W+ G1 _, d proach or 0 s! k2 k T0 v+ ]: f) dexecute a missed approach.7 C& S& n, t& d$ b) y* X# x# a4 K proach to trigger the decision of either5 @9 V# ^( g/ E2 T# ? nding or go-around.6 F6 j: `5 ~2 T3 `" Y+ W& m2 H0 C ECOMPRESSION, The loss of internal aircraft air& x+ N* n0 o6 u6 `- D ressure.$ s, F3 b! a0 n E-ENERGIZE, To turn off or cause to not operate. # ?% n- m7 |- @* T! l3 d( F ]rom the tanks 5 c2 a+ E( t9 L! ]9 g- Jusing airplane fuel pumps or external suction. . \; P3 |* E9 f2 b算的一个增量单位。分贝0 r8 C$ _5 W. d9 G 常表示两个声音信号或电力信号在功率或强度方面的5 S$ s( ^* w- _8 l) ]2 R! R 对差别的单位,相当于两个水平的比率的常用对数的十 0 d& D1 F+ u9 k断高度/高(DA/H),& `( S- S5 q0 r2 o 在继续进近必需的目视参考没有建立的情况下开始复0 b0 d" }( D1 L 的精密进近中的一个指定高度或高(A/H)。8 C& k2 s' D" T5 Z* ^ 断高(DH)1, ) x- b$ I: d9 l3 D, \: p操纵而论,指在使用仪表着陆系统或精密着陆雷 $ H6 I' B7 Z* V" i生继续着陆还是复飞决定的高。 ! ]4 A7 l6 S; {2 u" v* i飞机失去内部空气压力。" }$ p$ Y- B) z$ j1 W 开,1 \! r1 z4 A: M: g) { 关断或使不工作。 * P) z/ M Q2 ]! n- o4 C机的油泵或外部的吸油装置将燃油从燃油箱排' G# t! w5 }6 K1 d2 H 出的方法。) m; I( d. u1 P/ H/ B1 j% J ra 1 f* q: }* d) I& l) vD" c; K& q- H: u) t; F/ q1 o a+ {( s% W" k6 ^ w( `1 I/ R3 Z/ X0 O& \) v N required visual reference to continue the approach has ]7 G6 d: y$ g& } not been established.. ]7 w( ]# j' _0 a0 A& F D0 h9 K" h5 X# N; { operation of aircraft, means the height at which a1 Q8 X; A$ \: @8 A decision must be made, during an ILS or PAR" t9 o7 x% I% w0 B' E B) z. O instrument approach, to either continue the ap 6 b, V5 J+ @3 z {' fto 2 a' e5 f. G' e* f1 {DECISION HEIGHT (DH) 2, An altitude used during a& e. p$ e( R6 w( Z& x: k1 U precision ap # y) U& k& I1 H* s- |la - A% q8 S' @. P; X8 O" i6 B2 `D & x: b# A: x0 m% u. Jp& E# }+ E d/ s: J+ |% f2 y% Q, g+ R D! @& t* U! Z' A4 C! Z* g: a5 z DEFUEL, A method for removing fuel f+ h5 g2 @6 w/ k4 Q* ~ 分贝,% ?4 L& }0 U2 n0 x9 W 以输人与输出功率的比率来推 * c7 A6 U0 G, H6 C6 \' o9 ?) v. ]. \. _/ E4 d' s6 N: M7 G" w7 l7 f1 F7 @: K5 Z/ B9 J: v/ x0 n. L: S" e3 W+ X3 }8 [! ]! u" I- W! R' }% L' P$ {; x8 g6 `" v/ z. B5 F3 o# Z: B8 e% I7 b+ z 就飞机 6 P) E' ~1 R8 Z$ s3 } L6 h! }9 O达引导进近时,必须要作出的是继续进近,还是中断进场 + V9 U/ N+ H/ `. ~; k" @复飞决定时的高。 + Y: c& } F8 K8 [: C8 w/ f v9 p决断高(DH)2,: i6 J+ h/ F5 ]7 S. y* d 精密进近时产 + R1 Y( O2 Z% m! E1 F4 ^$ M9 L失压,/ E6 N# V, x4 L$ B A) w1 _ v* n. x! O! i3 q$ I4 \6 `排油, ) O( X) o$ @, W+ ]$ p用飞 $ ]3 c1 H! W5 ]* |' M( D8 ^( B英汉对照民用航空词典B OEING. n, b4 n8 L; G: P, z$ d TECHNICAL DICTIONARY 41 8 l: c# q; R( }' f* wDEFUELING VALVE, A valve in the fuel system for7 C7 w1 U. u1 _5 K efueling the tanks and for transferring fuel between the. s R& R6 r% |% ^. x3 r E-ICING, Removing ice after it has formed on aircraft. - g& b; a# N6 a' L7 VChange or difference.2 m: e) f: t; ^! I/ A( P EPARTURE CONTROL, A function of an approach ?2 Q! @! ?, I3 x- @7 ~) L+ gontrol facility providing air traffic control service for# a) P8 c+ s. F5 n% R3 n- j$ g eparting IFR and, under certain conditions, VFR# n, z* R5 d4 P( F+ b EMODULATION, The process of retrieving information 5 i% Q6 N3 ~- `8 y. e- pcarrier voltage. & V# h3 C3 Y# o/ J4 {/ G- C) oation. b5 X$ \& h/ f1 X lic$ }* @9 d2 k# Y6 p1 g creasing hydraulic reservoir air pressure to 6 w9 \$ i! r+ }3 q, b5 l% Vmbient pressure. ' f( ?5 l; H8 U% v: X箱排油和在燃油箱之间1 j7 C4 ~% {( F8 A/ Z8 `9 c0 O 送燃油。 , L1 }9 |* w$ \+ F6 u. G. }3 A! s5 }冰, ; A7 ] N- p4 ^除去已凝结在飞机上的冰。' U1 d) }) {$ ^3 } 删去或取消。 ]/ q6 ], {) L( a; @$ w 量, ( V- E, ]- q: R' D ^/ ?/ u变化或差异。 & W3 V5 B2 \" { ^4 k5 a场控制, * K ~+ z1 n& n, u* E9 n给用仪表飞行规则离场,和在某种情况下用目视飞行( |" }/ r _2 n1 d' o0 M 则离场的飞机提供空中交通管制服务的进近管制设施 8 f" g& p# I% C. f$ G- x: I9 u% y! X, `0 V2 D/ q1 `" D调, 2 \4 [7 ]$ [2 m& _7 h) B" G8 A电压中获得调制电压的处理过程。 ! i# U5 J) C; E环境8 x+ j# E# N) }/ i# y4 K8 t6 J 力相同的活门。 0 F/ s& ] [+ u5 L9 w+ ed " K) c0 ~, T9 Ytanks.9 {, Y0 x$ d; C9 w1 [" N3 N4 k7 o, g D7 A9 u& V6 ?! ` DELETE, To remove or cancel.; Q1 W: c) v, [ a4 T4 Y) D DELTA, 0 V+ }* M J7 G1 tD9 g1 `3 p& t0 S: G! v c - o, Z2 e! D8 e: S4 vd 0 z6 a! g6 r% N! _+ B' U) o( T& Zaircraft. , R( v1 N6 f9 o7 J" HD8 c- T, z" P2 r (modulation) voltage from a modulated % D2 |0 ^% x+ K7 MDEMODULATOR, A device or circuit which performs$ b" e7 c; a; ^6 J7 | the process of demodul8 ?9 B, d# I E! _) d) | DEPRESSURIZATION VALVE, A valve in the hydrau 2 U/ i! |7 [# [) |- }4 Usystem for de ' m) _7 ]4 x! X) s1 T5 l3 h/ M! wa - Z' J* c) ~+ z) R排油活门, ) f/ j4 _8 H5 ?$ c: s" u燃油系统中的活门。用以为燃油 3 t8 w' c- v/ k- }; W4 P! j0 P% V" @0 L7 W5 ?: P' E( K9 H- T0 J' W$ o0 Z3 L& F删除,; H3 P# g. F. B& c" C. O6 c# Q4 @0 I( s1 A6 F1 F% T- F9 d. m) _! }) f9 b的一种功能2 U& A; @' s3 C- K! p+ }8 x/ N& A* \ 从载波. |' f9 M; _$ F1 f& O9 d 解调器,( z3 t. }; T/ L) I7 c8 f 完成解调过程的装置或电路。: H }+ P" {1 V, X% v9 P 减压阀,3 r+ o2 q* i& |$ K6 U 在液压系统中,将液压油箱空气压力减至与周围 # `6 d! |; c k* ~( l% H. H+ t! n/ S+ a英汉对照民用航空词典B OEING; R _, L% z) k& f TECHNICAL DICTIONARY 42 2 v# G q: V7 [! z3 \DESCENT, Phase of flight where altitude is decreasing. 1 e% ?5 y: w% x! Z. cETAILED FLIGHT PLANNING, The calculation of fuel ' E, Y" y0 o% z: }% gnd required for a trip by considering each phase of ( `! t5 x7 O# e0 O' T! \' z. V4 ^ight (climb, cruise, descent, reserves).$ m: O8 I9 n$ Q" G' j4 Z al or! }3 u; ~5 S! ^: H! r4 c( O ETENT SOLENOID, An electrical solenoid used for ! ]2 p, e J, ]1 a, ]* Vt. 2 W% I+ E% z7 x; E/ n( Cspecified course or ' J: x* M0 p8 G; procedure. * I% M) G" m: [( a9 S$ H; ~e.' u3 x0 ]7 d4 Q+ A6 C/ p3 z 飞行计划,, b" ?4 O2 @: R' c& _" B 将航班中的每个阶段(如爬升,巡航,下降,备降)都 : \7 p4 X1 ?9 L8 u J人考虑,来计算该航班所需要的燃油量。 ' |1 t2 @* A/ D; K用来感应情况之正常与否的电气装置。+ b( T8 x) S: c! _7 A. X2 s; K# L! o 定电磁线圈,% C' R$ W4 i" _+ Q# i 出接通的电磁线圈。4 l7 ~1 |' X0 z3 W 差,! U% M6 E; h3 B( x 与指定的航道或程序之差。 $ m) r5 ~% \( T: r用气压或液压操作的活门机构中的柔性部件。8 N X9 ]% d/ N2 Z* p' I# b) G D3 v* S+ d- N8 N k! x1 K$ E a " _5 v% F; u4 T$ B( J" @; P8 _; Ffl( r' x" H- D4 L7 b. e: F# h1 I DETECTOR, An electrical device for sensing norm 1 G L! G% @* Q2 Xabnormal conditions.) K. `# `( k7 e0 I. O! I) V D# N2 d& h) n* A( ~& [& p5 p1 Y controlling the engagement of the actuator outpu 8 i4 z! I9 z) a2 W' W. ^% q3 {DEVIATION, To change from a @0 T! X. i$ `$ S+ d3 ^5 l0 `# T, wp2 M3 z& i. n: X; { DIAPHRAGM, A flexible part for operating a valve 4 a4 e: t# W( e- K& |mechanism by pressur- X. p7 s' i. W$ w; r. @ 下降, 3 L* ^) H( c5 H4 B1 U% P( a+ i1 a2 k飞机高度不断降低的飞行阶段。 0 x! b' O* D. ]: L详细/ s% s& z0 K3 ?# H% | o2 k3 E) O4 U2 z, _/ W 探测器,; V5 C' C9 ~2 |* Z; s/ _2 O( h: |* z9 y" A$ {3 I0 ]) i3 V* k用于控制作动器输 2 _) c" I; s5 q& }& c; K/ ], f) C4 N- _8 k4 E, C0 G6 D隔膜,3 P9 q# x9 \) l v X7 h 英汉对照民用航空词典B OEING & c, m' E6 Y8 f; |0 ?TECHNICAL DICTIONARY 43$ [( e. N9 ~7 D DIELECTRIC, A material which does not conduct / j4 M- x% g1 U* d$ M) ?electricity and used between the plates of a capacitor2 M( v2 h1 V" u6 _3 ^1 Z5 t9 q* W' N (condenser). 4 h# ?, y& j7 Q" X( i4 q8 tnother pressure in the same system, measured in# P7 A* ?5 t0 k) h+ d" i# J8 E ounds per square inch differential (psid). 0 c9 L5 j) i0 S+ N9 R5 R8 vIFFUSER, A part of an engine between the5 _: `5 F, e A) x& v ompressor and combustion chamber for reducing the! s9 q1 S( {2 |0 h/ C7 k5 u+ r air pressure. * I1 K: r6 f8 g, G7 j; `; P9 {, ^igh9 N+ O1 e- A2 m7 Z pulses. 1 W/ p) o" T. F$ A1 @/ ], A( d" Lignal that is a close approximation of the original ( } l3 `+ Q; t8 V4 D1 Hignal.$ g/ r, {+ K/ X" e, n' s a) e IHEDRAL, The angle between the wing reference! U: C! M2 T4 _% |1 q i/ M1 w lane and water line.+ ?: k2 }* s9 }) P, I: Q# ^ 的压力,以每平方英寸) E' S) x# j0 m( l) m4 m 少磅压差计算(psid)。 ! R1 I3 A4 w o散器, ( p6 p5 f( Z% b' d- k6 K8 @: e发动机内压气机和燃烧室间的一个部件,用来降低空 % l8 I# B# A$ G: f) y5 v4 w增高空气压力。 : q1 K z, |' r+ Y换,1 ?' ?) b- s5 n* B! L* z 的连续可1 e& y+ F J% q& G+ z# f (模拟)信号的处理过程。 ^0 Q F$ T. l. E5 o5 ` 反角, / t$ J" J. ]( p# {$ T1 f5 g机翼基准面与水线之间的夹角。% {- B1 Q) g0 x7 e) V( J8 }3 Y DIFFERENTIAL PRESSURE, Pressure relative to ) A/ d3 ^9 |+ N/ M# ]a L2 j. x7 u$ B" }2 M8 k7 Qp8 }) _+ u, M+ j! q D . ~' A0 k; _/ vc - |6 [3 m- Y$ H5 Hairflow speed and increasing the " I3 {' D8 W7 F0 Z& X0 ADIGITAL, Digital refers to a signal whose amplitude * @/ ^5 x0 R: q$ H# ?2 qremains constant for a finite period of time. Digital- x6 ]6 G) L; D- E/ a& h/ Z# y signals are commonly represented as a series of h9 W$ u) i+ I9 [6 B6 o and low( K+ K1 \6 ~- N2 L DIGITAL-TO-ANALOG, The process of converting a) \* v! b7 `: p; ^! \5 W S( o digital signal (binary) to a continuously variable (analog) , U8 k. O! @* Ls 6 \+ N8 N3 X; Fs ) u% Y5 e7 L6 l: P# C& MD * }, z, Y/ I1 Kp+ i& H+ k6 [+ i- G 电介质, 5 f1 c: }1 B7 w- i一种用于电容器板之间的不导电的材料。. w* U2 {" t5 U2 f" g1 ?' O: d. c: g 压差,0 Z8 M- Z$ H4 H9 I 相对于同一系统内另一个压力 ; K2 U( y! l% L7 b: \" a5 t# u: ?/ A7 d5 W4 n5 q' M, z8 ]; ^9 ^# ^* r气流速并+ [* q; P% P$ k 数字式,; I. \4 I& C" L& R5 Y& N0 b 指一种信号。该信号在一定的时间内,振幅保持不变。 " d ]4 u- u0 w* q8 V" s+ l' c通常由一系列的高低脉冲表示。: X* X _! X" k5 z, U2 z2 N/ q 数一模转& R+ b y& T; b9 Y9 I4 S 将数字信号(二进制)转换成与原信号相似) l6 {* J7 q# r* q3 O) s, |( D2 V$ b1 j$ y- k- `4 g2 z6 \英汉对照民用航空词典B OEING" M/ h0 Y; x! ?& d& v' d5 l TECHNICAL DICTIONARY 44 $ R; E5 r% h- G3 r2 wDILUTER DEMAND REGULATOR, A component in the 9 Y5 ~8 a, i, b; Bcrew oxygen system which mixes air and oxygen and* K6 n& ]% b* X7 B n6 Z upplies constant oxygen pressure even if there are0 A4 u; n% X2 Y, X hanges in ambient cockpit pressure. - g9 x2 D$ {2 B0 eIM, A word value of light. For light control devices - dim 4 A6 J4 B2 y# a; r7 C3 y1 F- K8 Ithe opposite of bright.& t+ j* p9 ]/ }+ ]. l, l. w7 X IODE, A device which allows electronic current to flow& F5 S2 p: M" E' D8 E only one direction5 z* p( X# V* [9 \# g1 G$ W uid in a reservoir. 9 k! E" d3 @' A: E! a1 ~6 zDIRECT, Straight line flight between two navigational . F0 j/ Q7 q% Z9 Z! i! [7 paids, fixes, points or any combination thereof. When 1 q* W. i9 S! p9 b$ V. Wused by pilots in describing off-airway routes, points# z* i& K& \; {$ T& H0 k defining direct route segments become compulsory ) I, `6 w6 ?" s; W4 Wreporting points unless the aircraft is under radar 2 k) ~9 z" _& ^: b8 D, j O& xcontrol. . ]* W! I5 u" E- w. D& |节器,: c( Z0 E) c7 E# [; a 将空气和氧气混合, ( d# i7 |# m \* C5 E( s使驾驶舱环境压力改变,它也能提供恒定的氧气压力。 0 L3 A# h+ g$ ^( d0 M5 |7 Z* G; R9 y) J 一个形容光线亮度的词。对于灯光控制装置,暗的反 / e8 _0 o; ?9 J2 @$ Q5 |4 X词是亮。3 P* P6 g2 C) x0 T 极管, ; {: }0 V C/ P5 d只允许电流向一个方向流动的电子装置。 $ y+ n& \, V1 ]: L3 L' V5 _器内液体的量。$ X. O8 S! ?1 g# Q% i% r0 t 直飞, 2 [) @' s5 o# L7 M. [ I两个导航台,定位点,导航点,或任何的组合之间的直1 I/ {# A) o# Y4 Z& q5 v, f 线飞行。在被飞行员用于描述偏置航路时,除了在雷达控2 J. Z$ D4 d% ~0 X; k 制的情况下,确定直线航段的导航点成为必报点。9 a6 d6 a9 S& N- q s ! \# V( w( ] h. Z8 M/ M+ cc . u- E. p; O* b1 o5 `( f' D# @D( s& J9 d! i+ P* B' C" u F5 n- r is4 P3 Q3 [7 _: J D1 u Q9 p- T: R/ g/ @ in ) ^) [# v( S6 o- ]3 f. cDIPSTICK, A calibrated rod or stick for measuring a ( N+ y- j: e) I: @/ S% \; aquantity of fl + B* v; J4 k/ m4 a2 u- W稀释氧调9 a: P! G3 h1 x( F8 T 驾驶舱氧气系统中的一个部件,它 ( q4 K4 L! X/ b* |% l- p! c. D' w# e0 P8 {- O3 M7 F; G7 l$ u' g) ^8 B; E" Z5 n1 t8 \/ B; B! u! K+ |: {7 C/ r. Y7 u) G量尺,1 S3 {$ C }: O2 h q. r1 v 校准过的棒或尺,用于测定蓄液 1 X7 M1 ?- w8 a) _! f: m6 x: Q" Y2 I英汉对照民用航空词典B OEING % W. c& v# j' l4 o2 C( N! z9 GTECHNICAL DICTIONARY 45

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