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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) r$ d1 C, w, x2 J* v6 G 民用航空词典; A: z* N" y. H+ e$ @2 j4 x5 B 波音商用飞机集团 ) C. R' O x5 Z% h7 t. R- nBOEING COMMERCIAL AIRPLANE GROUP! h r8 L" j( `1 t, ^) c" e0 T u 英汉对照民用航空词典B OEING + u" z; d+ b; [TECHNICAL DICTIONARY 12 o5 y1 q5 M+ o- i5 Q4 f3 R0 ` A) y7 s0 J- o" m/ X0 ], d ABEAM (ABM), Beside: An aircraft is abeam a station( k4 Z8 k8 K l" q8 V# s7 u when that station is 90° to the right or left of the track of # e! ~# T; U4 X7 `* uthe aircraft. ( H; k% y F4 q/ `. e% I0 U! ~ABSOLUTE ALTITUDE, The actual distance the aircraft : i6 t" p7 { w+ ~( ~# vis above the ground.2 |" z1 N+ y) a F8 B- ^/ ]1 K ABSOLUTE PRESSURE, Pressure of a liquid or gas" w: D$ m5 g# J4 j measured relative to a vacuum.1 C; n) [# m: k- A ACARS, SEE - AIRCRAFT (OR ARINC) REPORTING 9 L9 Y. E* o g* k5 ^% `. e' C. dADDRESSING AND COMMUNICATION SYSTEM 5 V! B- |" Y2 r, _8 J' o' ZACCELERATION, The rate of change in velocity with2 ~, ?7 D7 K/ S' _* w- l respect to time.0 u* j8 V, b% B! Z8 s1 Y ACCESSORY GEARBOX, A part of the engine, $ l& n9 ?( C9 b, j. @mechanically driven by a compressor or an angle$ @1 n* N. ^; T6 {: Q/ z gearbox, for driving components necessary for engine3 Z4 {6 z! k m" k$ K, Z 正切,# [, a# K+ e( e. U" m and airplane operations. $ n# w+ T5 D3 c2 e2 [( c当电台在飞机左侧或右侧方与航迹成90 度时,飞机正 1 T: Q5 d6 h0 R1 L, s切电台。5 |9 e* M7 p | 绝对高度, 5 |8 V1 k2 D9 H/ _飞机离地面的实际距离。, T0 k, V4 v2 o) Q9 p8 i9 q& ` 绝对压力,' }: P0 c( N7 X2 p3 b 相对于真空(无压力)测得的液体或气体的压力。0 S, P* c/ T: {& g 飞机通信寻址和报告系统,7 l& a) [2 `( u! S/ | 见Aircraft(or ARINC)Reporting Addressing and ; O2 f4 p1 L! [Communication System.# ^; t: N0 Q/ Q1 u M: f 加速度, 5 E. j. `( `9 p& {9 y: |# v随时间变化的速度改变率。 / C. e3 z" V1 F* w, \9 x \7 i附件齿轮箱,3 t' \6 e* _4 f4 J 发动机的一部份,由压气机或伞齿轮箱带动,用来驱动 0 A7 z" V" l4 `+ }, d一些使发动机和飞机工作的部件 d6 e6 M) C- l+ s英汉对照民用航空词典B OEING" r8 V$ r5 c& N! b( w TECHNICAL DICTIONARY 2- q9 b* _: D e( P# m5 G# C5 V ACCUMULATOR (NO. 1), A container with hydraulic 6 N& h) N& p: J) D& z7 fts when normal hydraulic supply is not 1 l) E3 O1 d* S7 w# zvailable. @8 F% i- O/ N/ }/ yCCUMULATOR (NO. 2), In a computer, a special : x. m4 o6 w8 @, M- ctorage register associated with the arithmetic logic unit, d' D# G7 g; N olding the results of a computation or data + F8 O$ M% t! b& E: K4 m4 ~' YACTUATOR, A mechanical device operated electrically, 2 O+ O: |# N2 a+ vhydraulically, pneumatically or mechanically for ( e }# n% U/ m. V, A1 Stransmitting motion between components. 0 e# R* B/ k& J+ n% BADC, SEE - AIR DATA COMPUTER2 ^0 ^) l- A, Y" r# L0 u$ K! G3 B ADF, SEE - AUTOMATIC DIRECTION FINDER; D j- Z2 g! W6 U0 ~ ADI, Attitude Direction Indicator, An electronic display of y7 U: O( A6 \9 X8 T' T. H airplane attitude information in pitch and roll. 7 E+ l$ p; @+ Z& G蓄压器(NO.1), & h3 \# p3 K& [# U8 O& K+ m: W含有靠干燥空气或氮气增压的液压油的容器。当没有正( \3 Z$ U, M6 i( U! e3 S 常的液压源可用时,该容器可用以驱动部件。( @) B- D, Q( E* L8 v9 l 存储器(NO.2),( b% [' b: D6 O' o, D, w 计算机中,一种与算术逻辑组件有关系的特别存储寄存 * C' B0 J; `! B% Q, l2 y器,用来存放运算结果或数据传输。" y( \, @5 r& w0 n, J. M, A 飞机状态监控系统,# r+ G# g- |4 F: y 见Aircraft Condition Monitoring System$ e$ ?' b) Y' z- ]7 P fluid pressurized by dry air or nitrogen for operation of / |( q) d& `( z# ^: u; U1 Acomponen8 I g }9 O+ m [. ]# z6 k a, I/ |6 g2 l9 D A : }: \) f. Q6 @9 e }8 Zs3 _9 E+ i/ g5 J" E" N+ [ used for h) ^( U* I G$ w7 b transfer.! V8 O1 K: w D) ]+ V, i ACMS, SEE - AIRCRAFT CONDITION MONITORING( s+ k0 w9 c: K) r1 H SYSTEM . 5 B x7 \2 u/ ?* a& w8 ]; o0 P作动筒,5 i; a/ X9 J$ K# I 由电,液压,气源或机械驱动的机械装置,用于传送部- h$ Z& I; o" w% e+ N 件之间的运动。0 \# g$ f& A: I5 E0 I7 @# x! k 大气数据计算机, & z" g# u3 j0 m/ W见Air Data Computer.. G: Y, t* t: X& Y' {) g- L 自动定向仪, ! f/ S$ m3 w% p# k见Automatic Direction Finder.* C: x+ e( \( j/ j 姿态指引仪, 5 K7 j, c2 ^ U( X; u v3 U用来显示飞机的俯仰姿态和坡度的电子显示。 ) D2 ^; E0 N! P: D' p英汉对照民用航空词典B OEING1 ~' f' X6 m$ ~, E: R5 B TECHNICAL DICTIONARY 3 r; |1 _! T7 R2 Q1 n AERONAUTICAL RADIO INCORPORATED, ARINC is/ W: \ W1 w P ,5 j6 _) y7 g: e8 {0 p+ ] nufacturers, and foreign flag airlines. ARINC . d8 |) x2 ]0 N) q3 I/ Q Fevelops and publishes standards for electronic0 R: f5 |8 p {# l' w" {" Z' d) g: ] quipment and systems., M2 A$ q& g" Z w" p4 W( j GILITY TUNING, The capability of the DME to, _1 z. J! F+ {+ y lternately tune between two different DME stations in# H0 l, `) H5 @' g4 E" Z rder to get two distance readings from one ! h. B8 @) X ~; pterrogator. 0 l- i* `' b& n' j/ Mge* g* J( \$ p$ b* d2 X8 g3 M ILERON FORCE LIMITER, An electro-mechanical6 u$ P& F/ I' \4 _5 } IR CLEANER, A component in the pneumatic system9 k5 f. }: T' z: p1 W1 U# n& J upply to the air% u$ p: {5 ?9 D8 [$ h onditioning system. 7 H* T1 b, P5 F0 {2 e订并出版 + Y! I0 }2 Z; v- c9 @0 c+ w3 E子设备和系统的规范。! Y+ a7 D/ K K0 F8 n 快速调谐, 7 _( h* ]* C3 a$ y2 |9 v0 q# k机载DME通过交替调谐两部地面DME电台以测得来自 3 Q3 b& r# l5 ~8 N同一台询问机的两个距离数据的能力。5 J/ c0 E; F+ O0 D9 d% ? 翼操纵力限制器,: c4 \4 F% C/ d% S 装置。在自动驾驶工作期间,用来限制驾驶盘$ }1 X8 Z; w- c- Q& G 气清洁器, : q/ a$ o% i9 u1 [/ n! Y4 [部件。用于去除供空调系统使用的发 . L l- q# u+ k8 S6 ~" C' c' Ya corporation whose principal stockholders are United ( w: w. w: R7 W2 P2 IStates scheduled airlines, air transport companies/ C" ~& Z: C: E aircraft ma8 L, q- Q2 X; F8 k: b d , p4 @5 Z3 l( X3 v; @e # [* C$ o$ n" F3 T4 iA A2 _# _1 I! @' ^4 N: I) i a ) S2 D4 [+ D+ K uo& }$ A; _' x7 e: K" ] in4 e9 q0 C$ b7 P& o) j. I( p8 F AILERON, A hinged moveable part on the trailing ed 1 e. s" L8 Q2 _of each wing for airplane roll (wing up and wing down)* h8 C) J, H- ]6 p control." S1 x6 ?! c6 e1 }' B# @ A4 g6 a1 Z" v+ s( l. C. Q4 c0 v device for limiting the control wheel movement by the8 x/ N( ?' }* Z' U5 E; |& Z3 X* v* z autopilot during autopilot operation.! v6 _3 u- Q/ S' w$ N4 `: ] A % H& n+ Y% D( X1 [8 i# \for removing dirt from the engine air s7 i9 d' C; W h c " t. g7 s1 d% Q4 W L& y航空无线电公司,3 r: B7 Z) K! w: }5 V 主要股东为美国定期的航空公司、航空运输公司、飞机( x0 ]7 c7 l' k6 ^8 X7 C! I% t& n 制造厂和外国领队航空公司的组织。其目的是制& s4 k& S( {/ b5 P3 d. c" G/ P8 ]. w( ~" z副翼,& `$ v- B2 o: O: A! W1 S 铰连在每个机翼后缘的可动部件,用于控制飞机的滚转% p( \7 h) z6 X8 r (机翼向上和向下)。5 _8 Q3 c" E1 m9 d, A' K7 h# }" x X9 n* g 一种机电 ! A/ X2 ?% P9 K* z7 E4 A- I$ u的动作量。+ S6 y) ?+ h) c$ L5 d- N. K, v7 b- P+ P0 C5 c) B 气源系统里的一个 - d2 r+ Y9 p- R1 q动机引气中的灰尘。" x4 F# `' p) ~ 英汉对照民用航空词典B OEING - W- j; R: F& O @TECHNICAL DICTIONARY 4 . e) _5 Q$ U6 K' XAIRPORT ELEVATION/FIELD ELEVATION, The & @0 r( d6 O( u0 Uhighest point of an airport's usable runways measured$ ?2 i) u r7 D' [ e$ u: L in feet from mean sea level. In a few countries, the 8 S5 R! ]5 o& J) ]) Gairport elevation is determined at the airport reference4 y3 r, @# ^/ ~% p: W point. ; @0 e$ D0 J) Z4 jAIR ROUTE TRAFFIC CONTROL CENTER (ARTCC), - `8 I) [: g1 E; A0 `/ r1 P2 }ervice # e4 v7 {0 L$ z! X- fase of 5 Y f) Y3 D/ N ?3 L$ eus flow of air traffic. $ I! t) C% E4 u; o4 z) z7 r6 BIR CYCLE MACHINE, A compressor and turbine on a2 {2 b% C' O: Z% P ommon shaft for cooling the air in an air conditioning * c: }* I6 _ e0 w1 B( ^ystem. The air is cooled by expansion from high to low ' n' O! [" F0 Jressure across the turbine. The compressor is driven 3 x0 ?' i$ S; P: l q9 {: M' hy the turbine.( t- Y. U3 a% O: H: h/ s" I 中航路交通管制中心(ARTCC), 2 v9 y. X( D) D; V) C+ e域范围内使用仪表飞行规则飞行的飞机提) d% V/ ]8 k5 C 管制(ATC), & K/ l6 q; F; \7 l$ p& o涡轮冷却器,* s4 {$ j4 L' t 是装在同一的压气机和涡轮,用于冷却空调系: Z0 D1 z& U F7 j/ b/ u2 v 统中的空气。气经压气机压缩后,由热交换器移去热量,4 B9 Y( b/ u4 k0 f$ u7 u8 ]) w6 K 然后经过涡轮令涡轮带动压气机。通过涡轮之空气,温" E0 ?) r! p" B) E0 V! O 度下降。 3 V4 o. r1 Q+ f) IA facility established to provide air traffic control s6 \1 }! Q5 N0 |. H, F9 a3 b to aircraft operating on IFR flight plans within controlled ! M& s7 a S$ g8 `! a0 o/ D$ Z6 ]6 g. Lairspace and principally during the enroute ph: y, S0 o: a! }# [7 W4 p% b4 n9 ` flight. 6 _# e" A9 {$ U/ N1 y2 n- ?AIR TRAFFIC CONTROL (ATC), A service operated by& M$ H. d' c1 c y0 S0 R- O9 f, V appropriate authority to promote the safe, orderly and( {( x+ J& }. a& e& N: G" h expeditio 8 ?$ g/ E* [0 _; m; K6 nA, j/ o Q! O+ y0 j c/ [* V7 h7 H r2 t! Q s 0 W0 U6 ~9 k. z zp 7 \" n, p# R5 G1 S( \0 @' D( \, {$ Kb3 ^6 w" S2 j3 V) Y 机场标高,% `3 k! B. b% e' }/ y3 I: v$ c 指海平面与机场可用跑道最高点之间的距离,单位是英+ j O" o& x' o, v. a9 I! s 尺。有几个国家的机场标高是由机场基准点而决定的。9 n! y" a% P# k" Z6 p/ h. ^2 G5 ?3 h, c0 |. x% s 给在控制空 : j3 ^/ @3 T& ~7 U供空中交通管制服务的站台。9 y; y- z0 M1 A- b/ [8 S 空中交通 + T/ \9 O: W9 L( N3 A) c由有关当局管理,旨在促进安全,秩序,和效率的空中 5 k3 X; h2 L0 C' V/ Z交通服务。 : i/ }8 e1 Z3 B& W# D% G4 {根转轴上8 Y. t) d6 N& h! C; z1 C4 B1 b2 J9 h }- _, G& g7 m1 L8 b5 U# |: V6 A' t* e1 @5 I 英汉对照民用航空词典B OEING& x& x- h, @( k. x w TECHNICAL DICTIONARY 5

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发表于 2008-12-24 21:36:52 |只看该作者
AIR DATA COMPUTER, A computer which produc ' S {% W O! c) O$ z2 d, `; Z: }, _data information, such as altitude and airspeed, based9 {7 S4 J% U! ] S$ R on pressure and temperature measurements. 0 k- I$ \3 u+ O* o5 bes air * h3 b& A7 m3 D9 j- ^3 b3 Z' V wIR TRAFFIC CONTROL, A system comprised of# l9 c. B) ]5 ? round and airborne components used to identify, track + S/ X; _. }" F8 n5 @ sOUND SENSOR, An electrical device operated% s7 e' K! V9 @# g% W y the landing gear, which transmits on ground/in air 5 e3 X" z2 J4 a. G. E9 ?8 Q: Bformation for system operation in flight or on the ) b# V" P! e. n- f8 A6 p6 o$ _round., P: p5 c% f. b IRBORNE VIBRATION MONITOR, The AVM takes* K7 k) W+ Y& [) E e signal from the engine mounted accelerometer and 3 o" T: s2 ?) r3 palculates the vibration on that engine. 9 s2 ~# m. i1 i' U4 _7 i& D |corridor equipped with radio navigation" G4 q7 d. G/ W0 m- v0 ^# [ aids.3 o! u$ W! N2 P, a7 @ AIRCRAFT (or ARINC) COMMUNICATIONS1 E- G: t+ {+ J4 q; o- ] ADDRESSING AND REPORTING SYSTEM, An9 u: N* Q7 p1 d- i' `! F addressable digital data link system which permits the7 V2 z3 @) h. J exchange of data and messages between an aircraft1 Y* ^$ l! Q# [: J& C and a ground-based operations center over a radio/ i# Q+ m# i0 W, y8 E' X network.& {5 L5 d" D- c4 g$ G6 T/ M AIRCRAFT CONDITION MONITORING SYSTEM, A : d5 N2 E7 h0 ?system of sensors and recorders to monitor various8 |% \; U) c2 a7 j+ v y airplane systems' performance and status.( `% }1 O& I! W" { q# e8 m 机,7 d9 n+ h. z+ R1 b8 C* m3 S 中交通管制, * t0 e9 d5 D6 M- p$ X8 b* o一个由地面设备和机载设备组成的系统。用来对飞机进 % l3 G- g7 R, ^4 _地传感器, 1 Z. c, H: p9 D一个由起落架操作的电气装置。用于给空中或地面的飞 $ Q4 S3 T4 q, @' ]1 {- ^) O- T系统运作传输地面/空中信息。(有些系统只能在地面 # @7 ]- K% c. J9 }/ t用) 3 z* w- }5 p6 o. K8 j: |) E载振动监测器(AVM), 9 \6 L' g! G. u: L1 Y1 ?0 h5 PAVM从装在发动机上的加速器取得信号后计算出该发 % R. M- S" N* ~0 V7 q, }4 T机上的振动。 5 @. d2 c3 C' [, ?0 K式建立的控制区域,内有无线电导航设备。4 X( p+ `; r6 r9 P' i 飞机通讯寻址和报告系统,% F7 e+ K5 r9 @5 S l8 Z4 z 有种可寻址的数据通讯系统。利用该系统可使飞机与地 ' p- ~8 s: b8 K- D" Y面操作中心通过无线电网络进行数据和信息的交换。 $ ?. f* s9 Z1 ?4 T% Y' x0 V) ~8 @飞机状态监控系统, - K3 i) [# F9 f2 o: e& X一个利用传感器和记录仪对各种飞机系统的性能以及+ R: R& ]8 B, l& Z) w) Y 状态进行监控的系统。8 y: i6 w! y9 M' G8 p' P6 x$ a A 0 {: E6 v2 m1 P1 O" w" Eg : Y% Y; d) r; v! Qand locate aircraft. X. \0 R& J+ N$ AAIR/GR+ h% \) m2 I8 k8 V* G0 a. N b # R/ d5 ], I5 Qin1 G& ^; X1 z2 ` s g' a. C3 q4 \% u- { A$ y0 p- M2 b; h th 6 c4 q9 t5 u; t; W+ Nc 7 [3 f& P. J3 \7 \6 BAIR WAY, A control area or portion thereof established7 {) g+ J+ d9 @4 l in the form of a8 f; X: E/ C% m* | 大气数据计算 + w F3 C$ o; n5 r1 {1 d, s4 C根据量取压力和温度而产生大气数据资料(高度、空速 , X7 l' M8 Y: }6 s y! O% x( v- j等)的计算机。" s$ v x2 s. i. q+ U, v7 d: ]4 {' b' ^8 U* ]3 E- P行识别,跟踪和定位。 ' i5 [% \* ~( r: K7 T7 H* v! X) h! l! e& G { n6 o9 h: E I2 ?* X. `7 V使 2 x" H" Z) }& k4 j' b4 P& K8 n9 P2 A8 i. O, w3 C% M" T, S3 {. G 航线, 5 `2 B) U! l* v; D4 X+ a I以走廊形 ( V# ? ?' R+ J+ V% @4 o英汉对照民用航空词典B OEING: B. p$ D" _1 Y9 E* J! N7 U TECHNICAL DICTIONARY 6! r" c$ Q6 L2 e; D* A AIRFOIL, A surface designed to obtain a useful reaction, - o6 L( b# a# @8 y1 [. {" ]such as lift, from the air through which it moves. Wings,, H" u0 B' N9 m! P stabilizers and control surfaces are airfoils.: n; [" n5 n2 B, m# E3 H/ ?* n- g AIRSPEED (IDS, TDS), The speed of the airplane: ~% j: E, V5 W% U7 }( R rough the air.: T! L+ @0 }& U5 _ D INDEX, An adjustable pointer on the : @' G8 ?! R4 T" X7 xirspeed indicator.: A- H7 t( f, K/ U. }9 X6 ] and legal ability, |; l0 X$ p7 E2 F6 t7 b fly.$ s/ N# M2 S6 g2 r4 y s, T9 j m, for example, the procedure for finding the9 G+ x2 B, A0 X& D. H quare root of a number. 8 N2 z* d2 {2 H" k0 Zy* a/ C/ J% o. W# s7 a) y0 C. y# w& o. f re, wind, 0 \* C$ n2 b- w7 t. sand aircraft flap setting. `3 {) c# j7 W0 R$ G2 m. L( _( A 是翼面。% `' h$ g" O6 F* }! ^$ @& T 速, ; S& p" v6 w0 h飞机在空气中运动的速度。 * q5 Y4 y0 q, B3 H. f) h0 }0 F( x6 [7 K/ L2 Z. x在空速表上可以调整的指针。& `4 ]: v$ E/ r' u! @ 机械飞行能力、和合法性的飞机状态。 9 p( q) ?, Z- ]2 B; a一步一步的解题方法。例如,计算一个数的平方根的步 3 e9 b! H; J% Q- v! R, C* r+ G0 h' l! ~$ ~& T, c, u' O0 B9 U" P5 W% Z& s7 R, m 资料的法定文件。1 D2 ^ d, q u 翼位置成函数关系。 ( E2 z N- a) X5 S; q: kth $ v% x0 B0 z* hAIRSPEE & J# e5 ^0 }; O- S6 ra4 z* F6 u2 o- x+ Z6 m AIRWORTHINESS, The condition of the aircraft with ; {$ @# R5 o- X, Trespect to its aerodynamic, mechanical, 2 S% Z% m/ y' C" O$ h) q4 |- _to 2 J: Q8 ]; @* M8 oALGORITHM, A step-by-step procedure for solving a 3 l' M3 l8 k% o5 ]. s. W1 @2 E5 @proble4 s; t9 x: h+ v8 f. N; v s6 E% Z, f1 ]( S) e! j AIRPLANE FLIGHT MANUAL (AFM), The legal . ?2 ~" v: I- T8 odocument containing performance and operating limits, 1 e' H; \7 b$ s2 G3 q" Z) ]operating procedures, and takeoff and landing ) D1 L$ E" b/ W' a! c7 Uperformance.9 C3 H" U6 _* G4 ^1 k& Q AIRPORT ANALYSIS, A comprehensive set of takeoff 0 N0 k& n, k; p3 m( x+ G2 n& Uweight limitations for a given airport runway, generall ) }4 t1 ~# B) q/ Gpresented as a function of airport temperatu. Q& _: y I, K 翼面, " ~: W g" d4 p$ R用以从气流中获得反作用力(如升力)的表面。机翼,- `* ?. c7 d9 b- ]- r 安定面和操纵面都1 ~; @9 z" V, Q$ R$ S4 e; v5 l" I 空速指标* b: n0 x( [4 f5 x" k6 Q 适航性, ( \% h$ i+ ?) e) l% T有关气动能力、/ m3 U% A0 b6 D: s0 g 演算法," u* k* D/ W$ f8 K5 x+ d- w. a- [) r; P; f 飞机飞行手册(AFM),( ?0 I j; i7 Z; l7 L6 j 包合性能极限,操作极限,操作程序,起飞和着陆性 & I6 h# A$ V \) d! z+ a" N% i6 t# c+ u机场分析, 4 E* f- l2 J y. X; M/ P h一套针对给定的机场跑道的详细重量限制资料。通常与 2 k4 x! E; S8 \' C机场温度、风、和飞机襟8 J ^" |6 j$ T0 g# M% }, ] 英汉对照民用航空词典B OEING 2 F/ ^" w4 ^4 [$ K! Z0 mTECHNICAL DICTIONARY 7 ! T; b8 A1 z1 T. ~$ o1 F8 JAIRSPEED BUGS, Adjustable pointers on the airspeed9 d+ u; K7 n; A- B indicator.0 J$ N' t! M" i, O8 H( z, t ALLOY, A mixture of a basic metal and small amounts6 u5 \8 M% A. v4 y; x f other metals to change the properties of the basic " T$ `+ H) c5 |" ~% a* S8 yetal. 3 W# t( S/ o+ WMinimum airplane speed. 2 s0 S0 b# ^! w+ Y9 \e of & s) F5 @1 R+ h0 \" I( R5 H1 xitting airplane angle relative to & {! c) M8 q3 h: s: u: M# j0 Virstream for the stall warning system.% Y) q* D- S* }. S3 Q* G" t7 S another. ' y9 f' @$ u: vLTERNATE , An additional airport selected during1 y9 u. ^) a" x6 c0 |$ S& s! a1 [5 e/ W合金, 5 k! Y: k/ B% p* M* g) d: a/ b5 x/ a在金属中加人少量其他金属,而改变其性质的一种金属* J# S5 U9 n' k5 V4 K 合物。 + I8 d9 W( B6 Y, y6 Y7 Z2 c4 b+ A飞机的最小速度。 0 V; C( u; E h/ c速警告系统传输飞机对5 J% k: a r4 i0 ` 流的相对角度。 4 ?9 ^& m# x3 z由一个状况改换到另一个。! v9 B4 S5 A: {7 g) C3 t 降场,8 Y3 |/ V& N( |/ h. A- g! t 划时,除了目标机场之外,所选的另一个机 ( w# J; k* }4 j& So % ^9 S/ X' F. L# N7 Km I+ T$ T5 m& t0 s% S: }' o" _. wALPHA SPEED,* M7 A2 b0 P1 A% z6 T: M7 w2 p0 s ALPHA VANE, A small moveable airfoil on the sid; k' B ]% E& R, L the fuselage transm $ Q+ |+ f; c# }0 J6 M/ L. ha 0 [# k: k/ D/ KALTERNATE, To change from one condition to) }* P5 t5 @: G A( n" v- T1 m) ? flight planning, usually near the destination airport, to be ' o+ t |6 p+ I9 M- Y( Pused when it is desirable to divert from the original1 e6 Z* l/ L. ]- b$ F destination airport. S1 a, |+ x0 L1 W0 f+ ?空速游标* ^6 j4 }" Y C9 e5 F5 \1 R/ ? 空速表上的可调指标。 : H- H+ P9 c; t: o, W: K. @6 b3 `. r$ l7 ?6 K6 K& V7 t4 n: v迎角速度,2 L: R" p" |7 E. Z& g 迎角叶片, - s* Q! I' P) W. W4 r9 D位于机身侧的可动小翼面。为失 - A) z1 i8 B1 i2 L0 x& ?) ]+ o' `- F6 M" O1 |9 F% K& s. g5 J 交替,. N' @1 e6 d, _4 L; [* q8 C7 J, t3 |$ X- }: u制订飞行计7 v9 q- A2 Z* g- h( ~# J7 W 场。通常在目标机场附近,以备不去目标机场时,改降之 8 d- {* M% d+ D! N用。 % b! _4 Q, C+ O' ^英汉对照民用航空词典B OEING # h( i' r# N7 B2 [TECHNICAL DICTIONARY 8 ( ^( M2 ]3 J* ` WALTERNATE AERODROME, An aerodrome to which . ^/ `3 _4 S4 c( N" \an aircraft may proceed when it becomes either0 q+ ]7 N1 X% K% _- q" G possible or inadvisable to proceed to or land at the ' e7 T! |4 N7 V1 V1 ?8 l- _erodrome of intended landing. + e3 Q" `/ a0 d4 u6 Z( ?+ ETER SETTING, The adjustment of the altimeter* @- P8 Y0 ]- F9 H5 b1 R1 i- I account for local variations in atmospheric pressure. 9 Q3 |( I( K! U( m& P% G3 TLTITUDE ACQUIRE, A digital flight control system 0 u! E) n% _& `0 B. vode to transition from climb (or descend) to level flight.. s& I( s8 i0 i: O LTITUDE ALERT, A flight deck alert occuring when the2 Q9 f) q3 O! g% R( ^ irplane approaches or departs a selected altitude. h' S) ~( R! R2 J1 o LTITUDE CAPABILITY, The maximum altitude at! p' f+ W0 y% r& W: E+ Y" y hich the airplane can be flown at for a given thrust, + @' q# f G- e) M6 d$ D% ?. Z" \$ bpeed and atmosphere condition.+ @1 A: l! Y D LTITUDE HOLD (ALT HOLD), A mode of the autopilot 8 D7 k$ s( P3 g1 c. H3 s5 ?) Pr flight director to maintain a selected altitude.9 X H* X. N4 `& D, \% m4 J irplane's altitude during VNAV operation. # {) P7 R. `% B6 O A机场着陆时,可作着陆使用的 " W' d% m! e0 f$ G7 k场。 4 G1 ^' E$ \# U/ c$ l, g# R, u2 R; E/ u/ o; {7 p j; Z# E 根据当地大气压力变化而对高度表所做的调整。1 \# U$ S+ K; l( X m 一种数字式飞行操纵系统,从爬升(或下降)改平的模 # k7 s4 R. v/ e/ U1 y% a5 {/ v/ y; ?" v 度警告,' w/ s/ o9 ~; s; k 当飞机接近或偏离选定高度时,所出现的驾驶舱警告。3 P2 E$ k3 w& b- l 高度能力, 8 z7 X7 J( H0 b: w4 D1 V$ L A1 F在给定的推力,速度和大气状况下,飞机能飞达的最大 2 ?) N6 V; U/ Q0 u! {2 V/ }高度。6 N, k* y8 ~; p, `- C1 I3 f 高度保持(ALT HOLD), 3 H3 F! ~1 N: C% Q自动驾驶仪或飞行指引仪保持在选定高度的一种方式。" Z' P, O& S4 w, z: w9 l7 r) w$ X4 ^3 @& w" L7 Q员对飞行高度的控制。 $ Z8 @ g; B4 ?0 E% Zim0 p% G E3 [8 N/ r9 c! h5 s a 8 D- ^" r& w+ C4 W& n- uALTIME * s* N; ?1 }" B( b$ o; [3 s5 jto ( b; Z+ B5 g ]- ]4 tA0 _( b9 K3 _- W. d* x m. u5 m" f# _8 ?8 b4 o5 G A 1 |2 V3 F$ R: o9 E( aa. Z) c# Z8 e4 _# E1 I0 I A9 O \2 ?6 ?# D4 l q# F; G w $ }7 Q5 _) i+ M! D* S* ~s6 b$ q4 {3 r0 m4 H* g8 \ A : X0 @9 N% b% zo 0 C$ F( K# _* A& r XALTITUDE INTERVENTION, Pilot control of the 2 y3 ?* n/ |# q- s; _* N4 Za" _" Q3 o% r8 d7 Y o, a1 x AMBIENT, The surrounding atmosphere. 1 A+ w5 z0 Y. O' V% C: ^: v备用机场,* Y/ i' j/ |8 [$ T. [! q 当不可能或不适宜在预选5 U; u! V- \/ ^* [- Z D0 s2 o2 \" a& g2 s0 l; ?; v/ ` 高度表设定% E. X: @" A( N5 a5 v4 m9 a 高度截获,1 p$ c9 r H$ l. D6 d7 i3 d* c( Z- c0 s# x* @9 ^3 S1 T( o0 {( A! C0 |+ p高度干预 , B! A6 U% r. Z3 R. i- C0 H' o$ C, z在垂直导航工作过程中,飞行 # Y8 r# M! E" r3 |9 s) H周围环境(地面气层), 4 l* ^" m; A1 J, e/ Z物体周围的环境(特别指大气)。- s7 c/ Q! R3 Z% V7 [5 \ 英汉对照民用航空词典B OEING2 T0 f- N; h; X+ L1 b TECHNICAL DICTIONARY 90 |2 N- O4 `9 C5 r f- w& M" i AMBIENT PRESSURE, Pressure of air surrounding an ( f/ q: G3 S d# Qobject, measured in pounds per square inch (psi) . 7 ?1 ]. u, T0 D# q$ B0 I! nMBIENT TEMPERATURE, Temperature of air # D/ J" B1 a; v5 q( Rmpere.) l) ]) _ N3 X1 B- O# X8 k" X urrent waveform.- w+ N) v, S8 z( N2 J2 U g an: ^+ K8 U9 b' \# t. ]5 k2 ]! M nalog signal to a digital signal.8 k. m R# o( O+ C5 Z! Z ore inputs , J3 i3 A* M% P( J, H; wf binary digital information and one output. The output ) |! p, N) N6 v8 O" z5 X/ `' j1 only when all of the inputs are 1. The output is 0 1 j8 M3 {3 ]# A {6 d) s8 Lhen any one or more inputs are 0. ( C" b4 b$ i) H* \' V面气压),% B9 V% ~6 M _3 _* ]! v* y 境温度,% I8 l# T4 f3 x% Q5 f+ p5 j 气温度,用摄氏度(°C)或华氏(°F)来 ^" }: D, {; D, q2 Y7 C8 L6 j* C( @' D$ s" S Y电压或电流波形的幅度。 # _2 |+ {) n: _1 k性变化的信号来工作,或产生连续性变化的信号- I, n }; T7 d! Q 统。! g; Y2 Q* W# y6 u" H, I 将模拟式信号,转换成数值式。 y2 c" b* s, ^9 Y, k7 C 一种有两个或两个以上的二进位数字信息输人,一个输 ) G' I! `. i4 i7 B; `& D# V的装置或电路。当所有输人为1,输出为1。当任何一个9 L, {0 f4 k, U5 w% R 一个以上的输人为0时,输出为0。 ( V. o5 ?0 o0 L& VA / M" E; E1 I" M! V9 X u* csurrounding an object, measured in degrees Celsius + @# a: `8 W/ g+ U(°C)or degrees Fahrenheit (°F). 2 w* A" R6 F- ~6 IAMPERE, A unit of electrical current. One volt across. L2 H! t9 x5 b$ z+ | one ohm of resistance causes current flow of one5 @) K0 U$ a3 p7 F( E6 D6 K% D a' z+ V, B* `- n2 R, ] AMPLITUDE, The size or magnitude of a voltage or: O5 _ a6 G n c" L: }, i" M E" a6 m9 [- x ANALOG, Quantities or representations that are6 D3 j# S8 \; J& D2 ` variable over a continuous range. # y$ d( t% `3 d8 U% GANALOG-TO-DIGITAL, The process of convertin 6 Z2 F9 ^0 Y3 ?6 M' Na* V2 r2 K$ i6 s7 P; e% N AND GATE, A device or circuit with two or m( G! h/ Y% L) \5 |. ] o. A0 l y2 c9 n is ( T+ x. D# o6 e! t5 c2 `# o3 lw 3 L. Z" j3 C1 z' D环境压力(地* s! x9 \9 H' N/ I# ?$ Z' T 物体周围的空气压力,用每平方英寸多少磅(psi)来) C; A) M5 J! M$ j. L3 q! M 度量。 6 o' c; y- m- c8 b) W, [/ r; o# n1 b- | 物体周围的空 9 n e1 l9 W _! |5 W0 `( k7 q度量。/ o @ [# C) {. N* K n7 ?8 | 安培, T+ s$ y: V# D! C. J' f. f电流的单位。- }2 ~4 w5 _( H* P @ 1伏电压在1欧姆的电阻上所产生的电流为3 {% A/ ~2 {2 ?) J 1安培, z5 `" `6 m4 t' w0 a# q+ n" u 振幅,, s8 X& j' q6 }/ o& u 模拟式,& x& I a S2 @$ S7 k 用连续 - L4 Z W5 M+ i, k/ X+ x1 B& S$ r 从模拟式到数字式,# Z* B1 r& G5 v) g$ s 与门,3 n1 T& |* z( L: K; r' l4 L, J. E& e; t- p, a6 P# v. t6 e9 C+ f英汉对照民用航空词典B OEING + m6 `4 V! C9 j. _: Z5 @6 uTECHNICAL DICTIONARY 107 m$ C" C9 E; o ANEROID, A sealed flexible device containing air at low# b. J; t4 P1 | pressure, which expands or contracts during change of * _# J. C0 q. Y b5 Nressure outside the device. - ?$ E% b* h9 B& y Dically 5 ?4 |% w' G7 w0 O8 {r changing the direction1 |) \+ I' H3 o: O9 p f drive.& Y3 ]0 J$ N; Z+ c4 j of the wing chord in 3 ]( m( Z y8 G" v ]( ilation to the free stream airflow as it moves forward4 I6 V5 m! l0 N rough the air.& Y* g" D: [. g" T( q. R al axis of the 6 r: z+ P z8 Uaircraft.! R ^( N0 p% [# z 胀或收缩。 * ?1 B9 u s. K7 ~, [箱。是改变驱动方向的机械装置。& d! p4 ^2 J" C5 @ 机翼翼弦在空气中向前运动时与自由气流之间的夹角。" J9 S4 Q$ o1 ~4 G. E' ^( g* {/ P$ D# a6 C; v p! X4 Q. a2 O" N! K* F2 Q4 ?$ j* K0 {8 Y ANGLE GEARBOX, A part of an engine, mechan * Q! m, T, r6 Y2 j: sdriven by the compressor, which drives the accessory ! s! u l. p# C1 agearbox. A mechanical device fo ( j1 M+ J* B So3 Z3 q0 q: u3 A+ a3 r) { ANGLE OF ATTACK, The angle ; ^- f' |+ j6 v8 _% C2 l$ Rre/ i) g, U* j8 u$ q th+ T0 I- v4 ^( b1 W- o, j ANGLE OF INCIDENCE, The acute angle which the # Y, T: S' e" s) _9 ywing chord makes with the longitudin ; H! u, ?( G+ r膜盒,$ ^- @1 B' T2 e 内含低压空气的密封弹性装置。当它周围的压力变化 ( f! U' |+ \( {/ Y' @时,会膨 5 E: a+ u x/ A, E- P6 o9 V P7 e+ |伞齿轮箱, & } K8 Y: I8 w" q w发动机的一部分。被压气机以机械方式驱动,然后驱动. t6 i) I/ B$ j! m. n- ` 附件齿轮 $ |( y H1 O, R' D0 v迎角,! {6 s0 b9 A* z6 \1 S 安装角,& Y+ R5 B; l/ v2 X0 R2 Z) I. } 飞机的纵轴与机翼弦线所形成的锐角 - d- d6 K- _7 B( O$ m# p$ W英汉对照民用航空词典B OEING) K6 N4 s1 N0 l6 }2 l+ X TECHNICAL DICTIONARY 11 1 O% |/ X8 _: Z [/ H8 sANNUNCIATIONS, Audio or visual indications used to+ l1 A! M+ d4 c! U, Z! H: A' |' {/ a call attention to an event that has taken place. 8 Z9 m6 ^) O, e; E5 N( F- yANNUNCIATOR, A visual device consisting of a number: d. P# C. i% j$ O6 S l( W: C- A ly. l1 F) S5 |1 q q; l) W% cANODE, The element toward which the principal stream% U: s( d' R; @ of electrons flows.) G) F: Y+ c6 }* \* I' d: ^ ANOMALY, Not normal.( [# z+ c; g! F! N ANTENNA, A device which, used in conjunction with a1 d4 }" Q" b6 K8 y$ S transmitter or receiver, is used for radiating or receiving / U* [, n/ g# Qradio waves.. A B, X' H" x t" B2 a NTI-ICING, A method of preventing ice formation on5 G( A; [2 ~( J" x( ^( u e wing leading edges and engine nacelles.. {( D4 _# D2 A, G* u6 _" ` NTI-SKID, A system for providing maximum braking6 ~3 K: l. Z# N( {# @ ithout skidding for any runway condition. Anti-skid: o; A* w+ `! X1 b- L2 } omponents are part of the brake system.7 s% G0 `8 N7 q; R4 M 告, : c! E# }$ I7 r2 G& U- W当发生事件时,以声音或目视指示形成的提示信号。3 Q8 q* Y- r, f* U3 r 与之有关的电路的现有情况或已存在的 ! C [. W$ p2 j& F+ D- m% S& j8 c1 z9 L6 {$ a+ U正极,5 o; j, E3 S# @/ l( B 主电子流向的极位。9 @' ]7 {* u2 Z# D 异常,! M0 V E. V9 }# e' V# ~ 不正常。 ! Y/ X ~- l( t天线, ) J; a% P6 y0 c$ M6 g: p一种与发射机或接收机共同工作来发射或接收无线电 ' U3 n& V# @/ l2 B! T6 L4 P- ~波的装置。 ! t" D2 i5 ]9 o' f+ d# G6 M; F- E冰,2 O$ k$ b! O9 P% b 防滑系统,: u) X7 V$ Z; r3 p7 F4 F- T4 B 一种在任何跑道状况下,都能提供最大的刹车能力而不1 T2 u" ~1 \$ @* Q7 z 使轮胎打滑的系统。防滑部件是刹车系统的一部分。& u0 J/ t; u1 m3 T" L7 m2 J3 ` of lights. Each light indicates the condition which exists " I0 F3 F7 E" O2 F& V- P$ gor has existed in an associated circuit and is labeled 9 V& ~5 n6 B% A9 L4 @# q6 q- u" Vaccording $ G/ ]! g( `; W$ M E6 vA ( W. B; A, \; F: N# [0 O" @& G1 Sth 0 n2 M6 m" Y! `5 D; dA5 ?: i9 V. W$ J3 [ w v/ ~0 g% | X c" q n) v1 u6 P) t M6 |: M" J q, C5 O$ L5 t4 g+ W5 `" U& `信号牌, / i! \; p8 c. {1 x由一系列指示灯组成的目视装置。每个指示灯都有相应. C4 P/ V. Z% z9 u5 c4 ^ 的标记,用来显示( A: A! `* m& r' x3 P/ U1 T$ y: p8 c; z# W* |4 b8 ?* N* B+ r- B0 t! j防止机翼前沿和发动机短舱结冰的一种方法。" F* Q; X {1 V' n- E; h 英汉对照民用航空词典B OEING; O/ @ E6 x1 d5 j' B( V0 \ TECHNICAL DICTIONARY 12 9 Q) {) M2 k1 A4 b) c. CAPPENDIX, A supplement to the Airplane Flight Manual% I) |- J2 _( {: w tained in the basic manual. A9 G# G0 z/ d, \) c6 g+ d ollection of supplementary material at the end of a - e. y( }$ ]; L6 Iook.# [4 |8 H b R9 ~- h1 _9 B of the r: r+ {: p0 \, i, } rsion link on the landing gear. 0 }; {( _) g: HAPPROACH MODE, An autopilot/flight director mode 2 j( f4 d" k; v* zwhich is a combination of localizer for roll control and) _+ ^2 U0 V. c- B glide slope for pitch control. This mode is used when full, V8 u1 l6 G" S instrument landing system is available. 1 O& H- h$ g9 ^2 a5 m+ K! `1 I2 t, YAPU, SEE - AUXILIARY POWER UNIT 4 w5 h2 g& |' E3 i! K6 @ARINC, SEE - AERONAUTICAL RADIO" C, S$ |6 p$ k% P$ ] INCORPORATED ! k( m% g/ Z+ }& t3 f; v# ZARM, To make ready for operation.$ j8 j6 A6 m% u, @7 M# L" K 附录, " i2 O- }$ n i% T飞机飞行手册的附件,包含基本手册中未提到的飞机形/ D- U7 w- D9 w* t* | 态的其他性能。是附在手册末的补充材料。" o* |% X( b3 w, w: K$ ? ?7 S 顶销, % Y1 l7 D" l d6 `/ W8 ^7 V! I9 m用于连接起落架扭力臂两部份的销子。- y W h! G. C. b 进近方式,2 E( d8 |, s2 Q( O5 {& e7 H 一种综合了控制横侧的航道信号和控制俯仰下滑信号 * y" S7 Q* W! K的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系' X2 c }% `) Q& T 统正常时才使用。1 \$ C8 k. f# X 辅助动力装置,4 E6 v# K( u4 U o5 l0 s" l# p 见Auxiliary Power Unit0 q# A$ m2 k5 }0 h containing additional performance for aircraft " x7 t/ Q# Y0 Q: Sconfigurations not con7 d5 g- f* `5 P. p& M9 g c/ J3 C; s2 K( X. v. _ b0 u0 F- _' h0 [: x1 Z0 } APEX PIN, A pin for joining the two sections : q6 `3 r% y5 Ito4 N1 z! ?: Z$ k. \: ^9 U; a1 O M5 U! I5 | X7 _ 航空无线电公司,' _& c& m; L0 W 见Aeronautical Radio Incorporated.: d# S3 [$ S! O% ? 预位, 7 y: f4 ^- a5 e0 O* V& K& _$ Y) H部件可以开始工作的状态。 1 |( X& }. u7 q- O英汉对照民用航空词典B OEING % F0 K: _. y# `TECHNICAL DICTIONARY 13 " Q) F) Z, v7 [ARC, The curved track over the ground of an aircraft ) G7 c5 _% w0 q# \7 Iflying at a constant distance from a measuring V5 v, x4 [0 C) Z6 n equipment (DME). 6 g7 S( \8 ?; }' T* P, ^2 l6 b6 rin the limits of self-contained system 8 U/ j# t. ?2 r% z7 T+ g) o, ?: Wapability. ; O9 L1 d" s2 y5 @/ T2 t8 Ctem for opposing or restricting! X( s, P" J( ]! H4 u ovement.0 c9 ~9 p A/ E. P" ]' a5 _6 i SPIRATED TAT PROBE, A sensor that measures total & V6 O( E! p5 X! B$ a# Mir temperature when the airplane is in the air and that , L# b0 V; @2 A! v: p9 Teasures outside air temperature when the airplane is* I( g7 g5 U5 o& u: G4 i% S n the ground. The outside air temperature is measured ; c0 @7 R, S6 Y" m2 x3 @SSEMBLY, The fitting together of a complete structure 2 _& \3 X+ B: F3 l' h& H, iSSUMED TEMPERATURE REDUCED THRUST, The 0 q; i% ^' x( f- [8 Q8 UATC, SEE - AIR TRAFFIC CONTROL+ n# y. \- Q) T; J+ s0 d7 V P. r4 D* p系统中所产生的一种用以抗拒 2 a' q/ r6 u& ?4 p; \. f \0 Q作或限制动作的力。 8 _9 ?" N3 x% `0 O# z5 o头,/ m! S: ?) a/ X+ @- p! ~$ o 用来测量飞机在空中时的总大气温度和在地面时的外 J, T* b# B3 Q5 N1 ?2 c6 h 温度。地面外界温度的测量是利用引气将外界空气吸入: x5 k4 d3 t4 Z/ V5 N m 头,以达到测量的目的。 $ ~1 b. U( y! R+ V+ [: q& Y! \! \配,$ i! k* K2 R% V U8 k 一个完整的结构或组件的过程。* |1 y# q) [% y$ } 假设温度而得的减推力, 3 V! I" b, c2 ^0 @推力设定值时,假定一个比实际外界空气温 , |4 ^+ v4 i% X* m f. C* F空中交通管制, 7 g* r9 {- P, [8 D% Z4 Q' w$ {见Air Traffic Control, O" o7 P0 V; }! e1 ^+ d2 X7 W AREA NAVIGATION/RNAV, A method of navigation: ? E' _ [8 @1 D- g( x5 w that permits aircraft operations on any desired course8 I( j" v# [& W+ r4 M, y# W2 J2 @2 E within the coverage of station-referenced navigation 9 c3 Z! H$ h$ ?signals or with + X5 X+ Z, I! B- k9 P0 q" C4 y# B0 @c+ \3 \+ ?7 C* A# C2 F4 d7 L# h ARTIFICIAL FEEL, A force developed in the flight ; C9 K! X/ c* z2 tcontrol or brake sys8 m& @7 g7 b* E" F8 N; C) ~ m . Q* v+ |1 W; B6 _- X* xA % m1 g3 U* a0 X7 ya/ P3 l. a. ?* J, v: B6 z m+ V: u! U5 X1 @8 V4 {. i o9 U! k- [: _, u! G+ \1 _/ }( B by using bleed air to draw ambient air through the" J, L8 z5 v& g4 A( U8 x& R- x sensor when the airplane is not moving. $ X! \3 _ A# K: W8 ]: uA 7 u' `- b; {, O& e4 C& B" C& Q* Bor unit.1 M0 y+ |6 s- J c A 1 }5 J! j) c9 N0 [5 alower thrust obtained by setting a higher than actual: @! x6 |1 f- F9 b0 b9 ?" r Outside Air Temperature (OAT).: G- R, y& O8 ]1 Q. _. G 弧线,4 Z) G" r+ }5 b& n U& r 飞机在围绕DME台等距飞行时的弧形航迹。 , m! _6 m9 l) S+ K区域导航, ; ^! z9 a h* @* i容许飞机飞行在有电台参考的导航信号或自备系统能 ) G- M6 C. t" ?力极限范围内,飞行任何预定航线的一种导航方法。 * F& _; x) X+ L1 b模拟感觉 $ P1 l) k6 ], ~* Z3 N在飞行操纵系统或刹车 1 s% ^- g! F+ ^: [9 D, c+ L e* q: o8 }( z& N$ h/ U7 N 吸气式总温探 + v# b1 T& y2 i' r0 A* k2 p' |! u4 I8 }) b. K( C: _$ y( ?# s8 j& {/ K+ o7 ?. f0 [2 k3 V0 Y& T! d( D组合成. f. {# Q& m9 P6 ^0 E* }0 \5 C5 s* W( U5 ]( z, K 在选择起飞 3 c; q- u- c: m1 W度高的温度而得到的推力。用这种方法可以减少发动机的 5 i* ]' Y6 l; {8 }6 t' x# W磨损和维护费用。 g9 a* b' V. r3 k& \6 @: Z' u: w [1 }+ |/ M9 G 英汉对照民用航空词典B OEING 7 A- \ s8 |. J+ v4 \TECHNICAL DICTIONARY 14, H, q( o8 |& {6 g: i ATE, SEE - AUTOMATIC TEST EQUIPMENT$ q2 y, v" v0 \& U4 _3 J ATMOSPHERIC PRESSURE, Pressure of air due to the 6 Y/ l2 Q# Y+ |1 Warth's atmosphere, expressed in pounds per square& ?) w- K' Y. ?' T$ k ch (psi) or inches of mercury (in Hg) or millibars (mB). 4 U0 k1 G6 K p# eTTITUDE, The relative orientation of the airplane with; a2 z2 H7 {: K% u spect to pitch, roll, and yaw.- F- _) E: V- F2 O, ?1 _ UDIO CONTROUSELECTOR PANEL, The panel in " e7 `/ [. J+ w+ C5 Ne airplane which controls and selects the routing of / M, C+ S/ V+ W9 Q. d- P, kudio. . O$ |7 Y2 z9 X8 Q% B2 ]5 h; sUTOLAND, Automatic landing using the Digital Flight # E0 {% i& f$ d4 i5 a H k8 U/ ~ontrol System.% g8 n2 {& I& \9 G n. : S( r n" N" a1 g/ }7 {M, A system/ C, D, M7 }6 V$ {' M, V1 g omposed of all necessary subsystems needed to guide ; F) X) e Q: i3 R& X& H. ?e flight of an airplane.7 T' g& a9 ] e- d9 T6 } EQUIPMENT, System test : `4 c. y2 V6 z( Kquipment that operates under computer control. 9 p: ]& ^* g# G0 g0 g7 M2 L; {装置,

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e! p$ o- u8 d8 D# s7 W in/ U2 w8 [* s3 ?. m8 s* Y2 s1 O- U. q A& I1 p3 y5 W" g+ D E7 b3 f; Q& K re3 U2 n' B; a. l- D( K A& e8 ~+ U& W1 \: g$ |- i th$ O$ k6 G9 P- D% J" U a4 `) e. ~6 A2 c2 O! C U% T8 c A # Q( G) @5 x2 zC9 S. E* C; \5 r% D ]: t AUTOMATIC DIRECTION FINDER, A system which 9 k& f% O! `6 Y" u9 {1 Wdetermines the direction of a radio statio) y; K* j3 o% L7 G! m AUTOMATIC FLIGHT CONTROL SYSTE ! j) H- g/ j A7 { Yc! E: v' A6 A r4 @) V) ^ th* c: c, K' ^% _/ A; O, _. J AUTOMATIC TEST : p# O& G* Y8 F) W+ I! Y3 i E$ Te ; f4 e [1 ~0 f0 w自动测试% U% F/ i; M6 R& r4 W2 ` 见Automatic Test Equipment.& o# [9 _% A; y& U 大气压力, ( p2 E# R$ i/ v, \! X4 `/ _由于地球周围的大气而产生的空气压力,以每平方寸多 9 ]( d" n. t. p% B磅(psi)或多少寸高水银柱(in Hg)或毫巴(mB)来9 _% z+ C% a. e1 z2 d% \9 ? 示。 5 G% a8 n! p! C飞机姿态,& o; H: [9 A5 c ?& C6 a6 D' ]; r 飞机与俯仰,坡度,和偏航有关的相对方向。0 O9 T4 d2 f' `% S6 s% N( S. c 音频选择面板, 9 r( _& G) Z( H飞机内用来控制和选择音频通路的面板。6 t( q; M$ g1 ~( f( f4 z+ H' I 自动着陆,' e/ w1 e$ Z/ b. j+ e1 r 使用数字式飞行操作系统来进行自动着陆。. L* x- Y9 Q8 g' h/ z, q/ a G3 [- U 的系统。 [) ]8 ^0 }/ j- [# R. U3 U" i( v- g9 k# s' C# x" c- U6 U, G6 J 系统所组成的一个系统。 9 [) u4 \* ~" y) R. I, o' s! ~在计算机控制下运作的系统测试装置。 # W2 ]) n3 Y& c, _. p2 p5 H3 C) k0 P* }. k# W" J8 G _8 c. ` 自动定向仪(ADF),2 O2 Y8 e1 w- j. [" { 确定无线电台方向 1 s# i* T8 Y: \1 a( |) m" l自动飞行控制系统 : d) ~ W* e. H" J% e由所有能引导飞机飞行的子1 V4 d4 H8 S" X4 O 自动测试装置,* d _3 Y' K* q5 u 英汉对照民用航空词典B OEING5 t2 F' J! e, U/ @0 U( j TECHNICAL DICTIONARY 15' u% H3 X. [8 X" a; n AUTOPILOT, A system which automatically controls+ v/ S% a& U2 }& \7 ?: d4 H8 y4 F and guides the flight of an airplane.* u6 C$ Z, V) w) D& j AUTOPILOT FLIGHT DIRECTOR SYSTEM, An " f4 x& x9 _5 }% xtor - t2 H; L) k! z' @UTOTHROTTLE, A system which automatically " [7 l, n/ x& P' y/ y% T% [1 Tontrols the throttles of an airplane.7 G& ]2 K$ n! M/ [( Z/ G! R$ h% L POWER UNIT, A small turbine engine in ) u' z) D. G. \9 v$ a8 z2 We airplane for supplying electrical and pneumatic- M/ _% B5 t6 \% S ower for systems operation on the ground or in flight. & I8 z7 ]4 X$ QVM, SEE - AIRBORNE VIBRATION MONITOR q" m; I8 Q2 x) v% q* U$ i& P0 |XIAL FLOW COMPRESSOR, A type of compressor 7 A4 G3 M% ~/ C9 f) dsed in a gas turbine engine in which air passes through- T1 X7 C0 }1 a1 f/ h XIS, An imaginary straight line or an actual physical* v; a1 g x! M' N. T omponent (such as an axle) around which a body can 9 f. D0 m% s& q- e1 rtate. # {5 S. t, n2 p( M' w3 K: n仪, 9 s% F* E u- u* J# g t: M! S( z' ` s4 o9 s! p 自动驾驶飞行指引系统, 0 s2 Q# \) ?& u* `* _, Q动驾驶和飞行指引功能的系统。7 r% ]; }3 l. z, [# {, T 动油门,8 N% a5 H6 j8 @5 B1 ?6 [6 L+ n# H 自动控制飞机油门的系统。 ; W T+ |0 L+ ~* b# J$ z是飞机内的小涡轮发动机,在地面或空中给各系统提供 ( Q7 z) ]" o% T- c" H5 C& f% [+ h% U, T源和气源。 ( f% T4 {- ]% K! R- V称。 ; G& O3 Z$ K- [5 p载振动监视器, : O2 g( `2 e/ ^9 |, W a见Airborne Vibration Monitor) r) w6 N+ y9 C; D, V1 b# C integrated system containing autopilot and flight direc # ]% f0 r; k, a" a3 L) k9 \functions. I7 N/ s+ S/ }1 A' H A+ V& j6 F4 C" w$ Y c ' I1 w* M: l# x& vAUXILIARY 5 A$ p/ ~4 G$ Pth6 A m S3 {( @5 C& B2 x p % Y5 h# E3 `7 Y ZAVIONICS, An acronym designating the field of aviation% Q7 h# U" \) d# A- S) ~* l2 D electronics. ; S8 X3 ^6 r$ Z) \- r) mA 2 T; S9 q% _ Z, f) p+ g- w0 QA0 v7 ~* @% ~4 u9 Y; m6 z u" P" F6 M- e, I8 i6 Q" Y the compressor in a straight flow, front to rear. ( x+ D; Y) o% W0 g# b% `A . ^' V4 O1 i- y* i% a% Fc / M& w& a' d' Hro' o1 P- {$ _+ U4 U* D 自动驾驶 ! @9 ^9 y( k% }2 R动操纵和引导飞机飞行的系统。 & \% L+ D5 F6 d一个综合自: I) K/ I- O S) h/ w8 m `& z: h1 Y辅助动力装置,7 N5 f% y+ e2 O `$ g, j' x. s% v8 | ]$ y) N6 l: ]航空电子学," ?+ N* ]( u; K: u, V4 a 是航空电子领域的一特有名 : B9 j7 g% |1 D5 T; h# @% e8 G ^( N t; D: k/ {( t3 ^+ I2 C( j流压缩机, / m2 x: d% `6 K一种用于燃气涡轮发动机内的压气机。空气由发动机的 7 {& X# O* M ~4 Y$ x5 L部流出。 + W3 M3 D8 H. ]% ~+ o线,6 O: J# Q# ]( j3 x7 d% e `) C 可让物体围绕着作旋转运动的一个想像的直线或实际 6 k/ E' s6 v; _( b5 ~; C f; a在的部件(如轴)。 2 B+ m# y |: R, P6 ?& V7 z8 N" J* x3 _前部轴向流人,压缩后,由后 _0 C3 E( D7 }$ U: o) D- `6 Q4 ]/ L4 d. z/ c0 A% L. C8 E" r0 _# [3 w) { 英汉对照民用航空词典B OEING , r6 I+ M0 {( x! @1 X0 h( ~TECHNICAL DICTIONARY 16 ! d* y, {/ c1 u3 e. ~: @0 t& R& KB ; o$ U. |' m5 SACKCOURSE APPROACH, An approach to a runway 5 d$ X( }' J5 W/ vversed.# n+ L+ e2 E7 h/ \* x9 n) X own on the EFIS that 7 f# s+ r2 q3 w% x* \oes not readily change, for example, navigational aids.- O# X8 P& Q; r3 C vement in the tank or reservoir.5 i% R% t+ L0 Y7 E ?$ Z ALANCE TAB, A small hinged moveable part on the) ^7 @- _; a* |9 c+ T/ e ailing edge of a control surface (aileron, elevator,0 ?: M. i2 q- F. j3 U+ \5 p 航道进近, - H. I' p8 S5 ]% g# }3 S! A; n相反的进近方向。当反航道进近时,无下滑8 P+ h9 G# R7 }% \) b 显示在电子飞行仪表系统上不经常改变的数据。例如: # c# D% T7 @: ^航设备。3 I' O6 i ~& _; ?1 W! P 在燃油箱或滑油箱内阻止液体流动的隔板。# `5 Q: n! g4 F5 Q7 _! E5 L 动补偿片,, W8 P3 v; q" ~' F 铰接在操纵面后缘(副翼,方向舵,升降舵)的可动部。% s* }1 e9 E- ~, `0 l& q 与操纵面相反,以帮助操纵面运# E' J* E' K E0 F, L3 c) q B, K% i0 [& ~9 d; e. e which is opposite the normal approach. For a& e' k [0 f8 {, s9 K, a7 E% S+ S backcourse approach, glide slope signals are not , F7 K3 y. [$ Davailable and the sense of localizer signals must be5 S# y$ h% J% U5 n( N* \! t re0 u. `6 E/ d$ G# n- @ BACKGROUND DATA, Data sh * d, A5 n3 x1 fd U4 \+ ^5 F9 Z/ |6 q BAFFLE, A partition in a tank or reservoir to prevent+ ^, ^* F) `7 x: o; z# U fluid mo 4 t& o! u R3 YB- l, f; D3 t+ C: v$ D% O* n/ q tr% B0 g- c% D" u/ }8 K rudder).The tab moves in an opposite direction to the9 b8 S! w9 a6 L' P0 p: w control surface for assisting movement of the control . g! [/ s& |/ Zsurface.3 x' \$ f9 Y2 ~" G3 E7 e& a2 o* k8 E5 a6 u3 M与正常进近% i0 z9 ^4 ?" ~/ [' S! Z 道信号并且航道信号也必须逆反。; ]1 |0 z7 d/ D4 I 背景数据, # z$ B8 g) h% {( o- \. B k3 V r( K4 x0 u2 j缓冲隔板, 9 p* h! U$ D# ]: d) }# }2 F$ h' o [6 r5 z% [+ [! n1 G 随动补偿片的动作方向 ( ]: X e6 q3 J3 W" W# I2 F动,减小操纵力。 4 E9 a* B4 J- I4 \' z英汉对照民用航空词典B OEING4 M" i" r5 d5 W) \# q5 R: x TECHNICAL DICTIONARY 17 $ e% Z% q5 r | gBALANCED FIELD LENGTH, The field length8 e3 v. g. w- Y S8 ^4 k: ~$ e associated with optimum aircraft performance when" `- R8 O p, E$ R' r7 r3 W bstacles are not a constraint. In this case, after engine " c1 o4 m, t( z% o. |' M' ~ilure at V1, the distance required to accelerate, takeoff/ k( a9 ~, q1 y! G- E6 L nd reach a height of 35 feet is equal to the distance 9 N- \" w% T1 E# N$ Z; i: v3 F! @- JALLAST, A weight installed in an aircraft to maintain 8 L) T, {* j* L4 Z. }" p' HALL NUT, A fixed spherical nut driven by the 8 O$ |( @$ p/ i5 ^- b0 Q6 o. CAR OUT OF VIEW, A signal used to remove the flight+ l; s! t: Q% g- i( Q3 U& x AROMETRIC PRESSURE, The pressure of air above * e2 a5 b4 @ s: P; Gg) or ! ?0 O5 t0 v* C+ i- V; Xmillibars (MB). # P6 m/ Y! d- U9 T4 ~& q2 ~ATTERY, An electrical device for changing stored6 F! b8 d* n# t: j( M+ A 性能的场长。在此$ {: e) h( {. i* @, G 况下,V1时发动机故障,要完成加速、起飞、离地353 Q+ j5 m" V. G' Z. B+ @/ b 尺所需距离等于相同速度下完成全停所需的距离。1 K3 C; d$ b3 }6 e1 K 舱物, ; j1 }0 i" P$ Q" ]! w& Q" Q重心在许可范围内面装载的配重物。 / C8 L8 S1 B% M1 b5 P) n形螺母, ) L7 ]; n ^ W1 z* g9 M5 e. Y的固定的球形螺母,用以使襟翼和水平- W# x2 _6 y1 t( c 引杆消失, 4 G8 L6 ]: ^5 ?( o: C# ^1 z指引杆的信号。 ! } @4 ]) |2 T U# K/ \压, 2 L7 ]4 [5 i1 U" F) l压力。通常以多少寸高水银柱(in9 _6 p2 S$ q' Y1 Q8 h( V 瓶,( t/ j, z6 B8 C+ n" D! ^# z0 H* S$ N 的化学能转变为直流电的电气装置。* v1 `* L( x6 y( o/ s( H: S- N o* w( x \3 O9 N9 B0 H) B: e fa& D n" C6 g$ I: J" I/ L a6 I) k& w4 }0 i3 h | required to stop from the same speed. 8 ]4 e2 T3 P7 G2 J, s7 jB; p" |. b9 ^) ] the center of gravity within allowable limits.' _" v6 [- g( P3 j B + `" B3 M6 K$ \/ i# E1 djackscrew for flap and stabilizer movement. * L1 h% e/ U) E& N4 dB0 L% V+ H7 c# }) Y director command bar(s). ( `- h; H3 w; ?% O( _, |B1 `; V" g w/ j/ E9 ? zero pressure measured in inches of mercury (in H U1 R3 }! J8 f" d" ~- q6 u( S. Y in& L4 H+ w. K/ c# o3 D$ c) a BASE METAL, The underlining metal to which alloying ) K8 v9 Y$ L& X% h9 cagents or metals are added. . H+ B: x- @# v" ]B - H4 @& G9 k) Echemical energy into direct electric current.: O" q6 S# \/ }3 ~" X 平衡场长, 5 @# y0 _! u y- g9 n5 W当障碍物非限制因素使飞机达到最佳) P0 C6 M, W! k3 G, v" j/ j, ^# r- L \- J0 Q' Z5 j9 d8 [( X7 S# ]$ d; \8 N2 N8 s+ i' X5 v9 y5 H为保持飞机# I" X: `+ o3 Q; Y- E' o: f4 D( Q/ L5 b0 \9 W' ^由粗重螺杆驱动 # [6 l; b. ]1 D" \. s安定面运动。 8 C; }" F) k, [# ^/ J4 i4 q+ H( o 用于除去飞行( P( I v; V" b" L Z' M. {( N5 b( p零压力以上的空气 5 a2 I; S3 X/ n5 @Hg)或毫巴(MB)来表示。 " Z- @) O3 O4 w- D基底金属,6 z- J; ?: c+ O- S! C 指合金中的主要金属成份。 ( W0 d: t2 k6 }5 Z- T/ g8 o1 `) D; N. g) M+ e3 q$ p i将储蓄% q) G% l/ B/ ^- T, t1 L$ O 英汉对照民用航空词典B OEING 5 }0 T( w( y s: J, {TECHNICAL DICTIONARY 18 ( J2 ?9 Z9 i6 m( EBATTER! \# B4 @& o: y h9 v. g/ M direct cu' y: q- S- o% y, c" Q+ r; u power su( h6 G( w$ A9 ^8 d8 u- r Y BUS, An electrical conductor supplied with # G, Y8 [" B% M1 h7 s' P! errent from the battery or transformer-rectifier for4 d8 c7 C( V/ \* z2 V6 N! A, U: [ pply to operating components. 6 d$ ^' | B# E% lCHARGER, An electrical device supplied & ?7 ^0 @# @+ o3 C4 b' U, u5 Pith alternating current, which produces a direct current7 W4 M% @" ? P$ P utput for charging the battery on the airplane.) ?! F' Y, R: z( e3 C AY, A compartment in the airplane structure. 3 z. P0 _4 d- Q# _/ D5 P( m& o" v3 e& n% MCD, SEE - BINARY CODED DECIMAL0 |' v# u9 ^- q9 ?7 ^* |3 r EACON, A device which emits a signal for use as a2 Y# c6 Y/ k5 m& {/ {6 E uidance or warning aid. 1 a* O) ?! D( K$ i; x- j5 K* mBEARING (NO. 2), The direction from an airplane to a 7 Z0 ?) t5 h4 lground station. 8 b2 ?9 O2 V$ w瓶汇流条,6 A* ^9 Y: M; U6 S8 g$ L 将从电瓶或变压整流器来的直流电供给工作部件的导% [( L; T' p" e3 i 体。# M4 m% N4 W' T" Q 瓶充电器, $ z9 V. L, x1 U/ {3 q0 n用交流电向飞机内电瓶充电的电气装置。带有交流电的 ! W0 u1 n. F. I' { y气装置,该装置产生直流电向飞机上的电瓶充电。 & W* f0 b2 g% r: \! R$ x0 i舱, 5 F. E; y" k D, o' N飞机结构中分隔的空间。& B% `7 S6 \) U1 |8 l; b4 D 二进制编码, 2 o4 {* x g5 k) m4 }7 I见Binary Coded Decimal % U- A& s1 m) N4 j# K# c/ vBATTERY9 B( N, c" p) u( E+ i; w6 y4 S w w, G0 z r+ e$ Q+ oo + G% w$ X8 J& r: x) e+ O$ z" d4 n7 lB " Y- I. z* g) K2 T. m- ]& {B9 b4 W- I9 J/ `% y, @& r# z B - ?7 R5 w$ S9 V6 f+ S* Ig: X { m5 I- N6 Z: o0 B# ] BEARING (NO. 1), A surface that supports a moving . p2 O* f/ k, K5 w5 Jpart and reduces friction between the two.8 [0 S: x- X" k' [( S3 P% t% v, @' c1 |" s$ O: K6 N: [4 V" z% O8 k7 c3 h. P/ E' B( ~; j! l; f! G6 `! F$ |/ M0 M0 o/ ~# C0 S) Y q% s2 u% R4 F7 P- B6 i( x- S. U A, i% w 信标, " u6 s" U! P% I( S" Z发射引导或警告用信号的装置。- B8 x# l* M: ? 方位(NO.2), / i$ R8 i3 h5 j4 f$ P从一架飞机到地面台的方向。# o) Q, j( R! ` J# c* G N g' `: F 轴承(NO.1), ! V, o% u& z' w6 k( U4 q! d& [3 k用于减轻机械转动磨擦的机械装置。 $ _' K/ h" Q7 [7 N8 k英汉对照民用航空词典B OEING : N: l$ J) ?2 w6 [* JTECHNICAL DICTIONARY 19 % {2 _) S3 W) x |% eBELLCRANK, A double lever in the control syst 7 P9 c$ a/ u8 h# {. ^. n- lchanging direction of motion.) ~, B0 k2 Y' d2 W1 {) R em for 1 r/ {! n- E @+ W( ict in the8 b& o" a: L7 T. E9 @: y4 z neumatic system for absorbing expansion of duct due & V5 I' P' ^) I5 X9 Kheat.$ K! ^( G7 q: `( d ELLOWS (NO. 2), Corrugated folded or pleated 1 N6 n) `4 [, @9 @+ K g9 Uontainer or compartment used to measure pressure.$ L$ i. [8 ^: ~8 k. \ EZEL, The part of an instrument case for locking the4 T/ ^4 x. X+ p G; a) N y8 G lass. ' q# d6 \0 p+ q( X0 b' |IAS, The potential difference applied between two . i1 H, {; p4 q: @$ P; P2 }* U9 doints for controlling a circuit. N! M5 k; _8 N+ t9 j BILGE, The lowest part of an aircraft fuselage. A place ! P* U9 {. ?7 swhere water, dirt and other contaminants collect. ; c, Y! Q9 @1 l# ?气源系统内提供管道热胀冷缩所需要的余地的波状3 u% L; t* e9 D 轫管。 . W/ m2 l/ q3 C- z5 S8 }空膜盒," t2 d, l. d# ?9 p% I/ j 一种具有波状表面的容器。用于量测气压。 % V3 b6 C) A; L$ z6 w* r% [嵌沟缘, 4 X3 ~# g' v9 P8 e将表面玻璃固定在仪表上的圈状零件。 ; {- k9 G0 n7 _" v- Q0 u. o" y压,# U1 G9 ?6 K* Y6 y+ R8 x ^ 在控制电路的两点之间的电位差。1 ?1 Y6 G' I4 J, y6 T! Q; ] 机身腹部, - u. G# V A& X机身的最底部,通常水,脏物,和其他外来物集存于此。- d/ d: ^' M4 z3 R5 G G! X2 K BELLOWS (NO. 1), A corrugated flexible du ; @" M* G( ~1 d8 `' g! }5 Pp 4 H q. i/ @. u3 {! j9 Qto1 k9 z( p5 I5 i B " J5 O" |8 L5 T' c# S6 Pc- K; e. f2 l* K7 f9 i B ; M3 a j5 x1 c9 f# x! c, _2 @g6 a. V) E; ?) H B + t/ Z5 I4 }4 b- |% x5 f1 X: }p& ` V( u" H3 p9 b 直角摇臂, , S# i& K3 d! u+ S8 s4 z- h在操纵系统中改变运动方向用的双臂摇臂。! x5 O W2 C5 T 波纹管,& k5 w$ U& W. D) m. _& Z4 f% d- c6 y: I L- r: z b" ~$ g8 S% q E$ a; z$ L, K, d# I1 ^" w5 m/ ?" ^5 S$ U2 \英汉对照民用航空词典B OEING6 H0 o6 x* h6 E5 q- r TECHNICAL DICTIONARY 20 g& ^0 V% _/ P% x7 L8 P" PBINARY CODED DECIMAL, A system of coding each+ s- x/ U% H) @) f1 S. ~ digit in a decimal number using the binary equivalent.0 K" C) q m/ @ BINARY NUMBER SYSTEM, A number system using + Z9 S" k1 Z; f% o3 gs6 G: Z5 _% h4 F" q IT, In the binary number system, the smallest unit of: o& Y/ F9 z9 O" Y0 t" G formation, consisting of a 0 or a 1.6 o4 ?1 f( c2 {0 K4 n- i ITE, SEE - BUILT-IN TEST EQUIPMENT( D9 g& J7 M% v/ Y LANK DISPLAY, A display that does not have any1 t: J5 M7 Q1 e O; O4 {( Q+ g dications, normally due to failure.) V& Y: c& k2 j. ?7 F. Q0 ^ LACK BOX, A container for electronic circuits to record. @1 ?" Z$ \0 m; W ight data., W) U+ {! q6 z8 @ LEED AIR, Air taken from the engine to power various. o6 Z9 H5 v" H; a: F x- n* m ircraft accessories.1 A9 d- Q+ m7 L B: h A valve in the pneumatic system for air9 y; T: s ] U8 F7 o8 }/ n supply from the engine or auxiliary power unit to the4 U" u, N8 I. V! _ pneumatic manifold. A valve on the engine for reducing: I$ q; o* N" {4 R, I pressure in the compressor section. 1 F) f& R5 j" O5 D9 J4 ~进制,3 i# @. m/ Y% e% D! Z3 m- r1 U 进制,7 p; T: v- a1 b9 u. @+ K) ~: w 一般用0和1)和2为底的数字系统。 8 \5 x. B; p& J特(二进位数),% R" i4 r' K0 t1 y8 u 二进制中的最小信息单位,包括0或1。 : k7 z; ?3 d, {& x- N1 [内自测系统, 2 U P9 y" N. Y( I/ h) D见Built-in Test Equipment9 j/ O1 o& c: G( T) {" m- ^ H two symbols (usually denoted 0 and 1) and having 2 a " X0 J& i& D e% d" `+ Uits base. * }: N: a7 E# G' }3 F; C& z7 o0 u7 [! }$ `B # P2 ~& \ u+ ?9 x6 Lin 0 U+ ]6 Q; Q u6 j- _9 UB7 l3 F$ I$ B: v2 M3 y1 q$ t) I B/ f* T" N' V0 J/ Z' R+ p in: F& F; t. P1 H n$ n! H! `8 D* q- v B I) Y' M+ \, g1 V' K; Q fl* n0 m! b1 x, K U" q6 s3 W B- I" P* W. A4 R( o; n. H9 h1 ` a* o: n( S0 |& _ BLEED VALVE,1 D8 u! h" h8 l8 C! m; \ 二进制编码的十) L9 _& N6 W t3 D7 V' H 一种编码系统。用等效二进制位数编译十进位数的每一8 t; ~# O3 X. }$ X; c9 C 位。+ H4 X' \0 A/ t& Z2 k0 R: H E. a! ^/ \3 E* H. B$ S以两个符号(2 J* D h; C5 E9 \. [* z& o4 @# m' i7 o* V2 ]8 _/ o; L: t _- x. E" R) u .2 _4 W) V! ^: n8 i. O) { 白显示, ! d' E: t- A1 e: {6 ?9 m. R4 k通常因故障而造成的显示器上没有任何指示。 # \! Z7 V' \, [( }5 ~2 a8 a8 |匣子, # F! Q' K3 r; ~' L9 V3 l装有用于记录飞行数据的电路系统的容器。% f: a: \2 S& {4 i" N& [ 气,: Z. V1 I' |, Y7 x: t 取自发动机而用以驱动飞机上之各种附件的空气。 1 e m6 E. p" H# D气源系统内,使来自发动机或辅助动力装置的空气进人1 c, Z6 ^3 r) Q 气源支管的活门。发动机上,用来降低压气机压力的活门。 % ?8 j$ B8 v; I4 q5 W/ Y# D% P8 @4 s) G1 p* P, W$ I( ~" ^& @6 m. n( e1 S2 h9 W: ?: V/ i引气活门, $ Y5 f' U- o" v C: z英汉对照民用航空词典B OEING # |3 f* p( l' }8 `3 b4 g/ X/ |1 tTECHNICAL DICTIONARY 21. N* s/ R- s6 I+ M& ^: }, o BLOCKER DOOR, A device on the engine for blocking 1 p9 E1 E( z+ T% ~! z$ `the normal airflow during thrust reverser operation. ( V7 `6 g% Z+ ULOWER, An electrically operated fan for circulating air. # b1 G5 Z3 z1 k! i- L; gLOWOUT PANEL, A panel in the structure between 4 F1 H/ X1 z1 W- W B, ?* A$ Mo compartments that opens to equalize pressure in % x. v0 a4 u+ P/ q" @e compartments.9 t5 l# o) L- O$ @3 e7 a, D; n ODY GEAR, The landing gear attached to the7 Q0 |) f% \* n, m grounding.* Y' u( `4 H% ^; |+ {" ~# \5 w 正常的 3 y( @* m4 X) c" C# A* p- V% D气流。 % {: t. ~( b7 Y! O鼓风机," K& l' r% y1 E) T& Q- } 用来使空气循环的电动风扇。 " O. q8 v$ A# G压口盖, 4 A( r" I) P8 L J0 i* c两个隔舱之间的口盖,打开后可使两舱压力相等。 ; i( ?% j6 {! b# d身起落架,1 i8 W& O" ~, k; Y% O8 k& _ 身构架上的起落架。. I$ A- E: Z+ b. q r& e# P B @1 P+ b3 d3 Q3 a4 YB7 A* Q4 D: `7 w/ n- G, @2 }; u tw! w$ D+ a. [3 O+ H8 T) ~ th / l/ {7 j4 s& ]% _: qB9 |" s) c" F; l( I$ D fuselage structure. 7 `7 H0 V% `3 l: T$ vBONDING JUMPER, An electrical connection between 2 \! [4 A$ Z3 W3 n* a. `* c% sa component and airplane structure for electrical5 k2 w* J% q6 B6 V! G2 U! T& E 阻流门,' r+ p; A5 {3 x$ } 发动机上的一个装置。在反推工作时用于阻挡 9 j) | n( `+ E# _. b6 j, E. Q3 L8 Z3 o! l! \) \' q% I* ^. z$ r0 ?4 W9 H 装在机 + i; B) n7 W, y/ e! f# {搭接片,: r, Y1 a1 P5 R$ g 连接某个部件与飞机结构以形成接地的电接头。 0 h+ y a9 @5 r& \5 t1 Y- H英汉对照民用航空词典B OEING + ?% d2 b& a1 y& sTECHNICAL DICTIONARY 22 5 Y6 W! {3 n$ z0 cBOOLEAN ALGEBRA, A mathematical system for 5 g0 ^4 j# S _9 r8 q3 d9 O1 O, k1 dwriting combinations of logical statements. ' U+ [2 J5 }" C; YBOOST PUMP, An electrically operated fuel pump for& n% }: v0 j' A B3 a7 A3 l8 m fuel supply from the airplane fuel tank to the fuel$ |+ j9 U. H' V. C* _6 \; l manifold." M! e' T! g4 f BORESCOPE, An electro-optical device for looking at 4 I5 S; y7 k" `+ d- C s/ }ternal parts of an engine through holes in the engine. 2 B5 Q- Y" C5 ^orescope ports) 3 A4 U8 E! k) Y% z7 a3 DOURDON TUBE, A curved flat tube in a pressure gage4 u4 |9 F! _. R* T r moving the pointer when pressure changes inside0 E2 K, E T. o& w$ n/ [. \ x on the ability of the brakes to! b. h6 D4 j8 X* @) w- y9 Z bsorb a predetermined amount of energy during a1 y6 O! t2 R' a7 c" Z0 U jected takeoff.& R0 Z4 H L3 I9 R. p% x+ k4 P 用于通过发动机内的孔(孔探口)观察发动机内部件的8 r v- q6 K7 c, P. Q1 M+ f3 j% Z, r 光设备。! {+ V0 x7 H% U- O) `) G; n: u 端管, 1 A+ \9 M! e9 o1 L6 N1 T) |测压计内的弯曲扁管,管内压力的变化时它使指针移6 F' V# T$ J7 f) X8 y 力。 5 |& r9 G1 o- {" M/ u: t极限重量, 0 Z3 z) _7 @) \ M' A6 w5 @/ [7 U+ ~0 W0 y2 T, l9 S7 c* M. _起飞重量。 - [' x0 U" G6 n/ z! I& l) w发动机滑油系统与大气相通的通气口。 1 t; Z" ^) F6 j1 u9 ?; D ]in , i* a. O+ v( Z) z3 E0 V! d(b ! _% {7 U7 _! N& t9 x1 e5 n: S; JB + I1 b3 J% S, o5 Pfo# I* ]9 Z0 j b- _4 R the tube.2 _3 O O0 s' L$ m* s0 @" r4 k BRACKET, To enclose or surround.0 w ]! t! g) |% v7 h9 v BRAKE ENERGY LIMIT WEIGHT, The maximum; c' Y! N0 G* u+ k0 x: _ takeoff weight based ; m- {2 L3 X+ D; B; n$ L- La& w9 U/ r* S5 o& U5 q* m2 g re# F6 T# h; T6 k+ n: t# j. L4 `3 n6 Q BREATHER, A vent to ambient of the engine oil system., `2 f9 ~& l; @7 U 布尔代数,. `" F0 p( `6 O: ~" ?! p9 h- i 一种用于编写复合逻辑命题的数学系统。 , m# `' c, ^( i增压泵, 1 E9 h' G. H4 @5 q6 o3 M4 D从飞机油箱向总油管提供燃油的电动泵。1 ^) U3 s0 E, v2 J( R/ @. ? 孔探仪, 6 r0 C* Z% @- @( H2 d; _# o& q S% c2 d* g! t2 M9 Q; E3 t( z# h4 k 动,以指示压# F6 J( r2 y5 p! r) E4 b1 S 托架, 9 O, ?. b% q: }9 i2 T# Q% v z& t用于作支撑、装托、或围绕之用。% J$ h& X! p' L! ?" N& b 刹车能量 ( U& w6 i7 t7 k3 T5 f9 f! v中断起飞过程中,取决于刹车吸收预定能量之能力的 & h: w$ o; _( W5 q4 U0 |; j4 t( x1 H- w! i% {9 U0 x v通气装置, + c% y- Z: ]) u9 ]( C英汉对照民用航空词典B OEING. x# A( a$ F/ u TECHNICAL DICTIONARY 23" o# K9 P- C5 C; q5 f# v BUFFET, Vibration of the wings and airframe resulting # r) M9 l! f0 f% |- `from unsteady airflow over the wing; caused when . F1 g4 z& H, F6 M) |% x; A! Eairspeed is too slow, the bank angle is too steep, or* s( r! o) Y4 o* A4 t irspeed is too fast. * V& {9 ~1 Y$ B0 GUILT-IN TEST EQUIPMENT, Equipment installed on/ B5 I5 X) N, B' q# Z, z( ~) X" f e airplane and in airplane systems to test the systems6 Y! X, n% R! x6 Q+ l ithout external test equipment.% E5 W) s& ], z6 j2 p- W7 S' P UFFET MARGIN, The amount of residual maneuver ?; Q& t$ J, m# p- L& X% ?: ~apability present before the onset of buffet.7 |/ L9 r) y$ d* Q4 L: E; E UG SPEED, A preselecteed speed to be observed / V; D4 H5 P& b- j6 y6 D# ?7 P; Gnding sequence." R- }, L& }! s. ` k 7 J5 Y' l7 q5 s" y/ }! \3 b% Hng landing gear operation. * e. v9 J) {( z2 [速度太慢或太快,坡度太大,均会引起抖振。9 Z, J1 M( ^7 g1 ]- X 自检设备, ) D8 `; Y( r3 j; l4 b) |0 T7 {( Z安装在飞机和飞机系统中,在无外接检测设备情况下, # u" K- k! {. t# H7 D用于检测系统的设备。 # Q2 P& X" A% x s6 S' H抖振裕度, * g3 ~" U* X0 ?. h/ v. J8 S) i飞机在遭遇抖振之前,剩余机动能力的大小。 ; |$ {6 r3 P& N+ G标速度,, K4 z1 |- R3 G0 b* C2 Q0 g 在某些机动飞行过程中,特别是在进近和着陆时,飞机1 u4 k _8 e% ]' ?. j' Q 预定速度。6 Q: z- I0 R g$ C3 w 力装置, ' k$ |7 {4 a# {: O9 F( I8 d架工作的一种机械设备(弹簧或减震器)。' s% R; R- F8 R5 s' y5 j* |9 O 流条,: y6 w6 l5 m# c. p7 _7 F2 @: a 在部件或组件之间传输电、数据、或定时的单一电线或% i1 m) l; T* y# M- p a 6 |4 H* e( `8 A9 R4 _B2 @1 b$ M; Z$ p B4 ?7 ?3 a th + K& [; K$ B- q4 |w% ?/ X* C. }+ U6 ?2 f" i B 8 W$ O$ q M* }. r9 G& i" z/ j$ Ic $ M8 k4 |5 b, }3 r" xB 2 F0 K& g$ H" ~5 Nduring certain maneuvers, particularly the approach and1 t e: ^% C9 X' v' W la ' ]* M6 K1 s5 A/ wBULKHEAD, A structural partition in the fuselage or 8 a# e6 }& N+ J, I3 Kwing. / i, N4 j+ j+ gBUNGEE, A mechanical device (spring or a shoc: T t- H- i/ l g1 G absorber) for assisti . c e: x/ s; i8 q# q. }5 HBUS, A single wire or group of wires which transfers " `5 u( Q& S# g9 q" E) Spower, data, or timing between several units or : L# E3 g3 X4 Z( O" }modules.: W0 m( Q& F3 t4 b0 |2 x 抖振,8 Q2 y* E# X, z8 h 由于机翼上表面的不稳定气流引起的机翼和机体的振 9 _; x. N$ V, _! E* Q7 z! a3 m动。飞行% y9 o4 X. G: ~ Q- ~$ Z" o$ W' v: s4 u" F 所应保持的 ; r& t+ v2 p' u壁板式隔框,% X( ?6 N( |0 j; `5 W 机身或机翼内一种结构隔板。) l- W+ I% @. Q* E) S: [2 z1 M3 A3 G) B+ @9 P用于协助起落. S5 e b0 X: ]: V& H+ m* g- p$ Q$ N; e$ Q2 m1 i! t 电线组。 / x2 |4 U7 g/ H( g' M英汉对照民用航空词典B OEING 6 [: z/ L! y3 C8 t+ _TECHNICAL DICTIONARY 24

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BUS DRUM, A mechanical connection with pulleys : }% a- a6 F# Bcables in the control system. 7 g5 P. W* u9 K1 P4 uand* N+ C( L2 f* v l circuits for control and protection of 4 R% b# t. a* o Nlectrical alternating current supply to the airplane. ! a2 p4 J* ]+ K8 Fduct for closing and opening the duct ' z; Y2 r6 |4 T) |: O( |( Rassage. 3 `( \' N+ Q. O- ^) sUTTOCK LINE, A vertical reference plane along the " y- P( T, _4 r" ~selage for horizontal measurements of the airplane.7 s6 f+ C7 K! a0 z. f% | 接。 4 V' x3 _" b; U4 e& s; t5 z组件,内含控制和保护飞机交流电源的电* t% X+ X& c7 E3 @3 [& H- B" {* I6 G: Y [作动简控制的转动装置。用来关闭和 2 ?5 M6 Z* G, p8 H" c启管道。 / S$ q$ P0 a4 f! P$ }* X6 U沿机身走向的垂直参考面,用于飞机的水平测量。3 D* J3 e1 t: P3 x3 m# Z8 _; U BUS PROTECTION PANEL, A module (black box) - T- T5 b( c5 o4 O- Ycontaining electrica1 ?. i+ p% b0 k4 c) \2 o e ( `" B& e" m4 ~BUTTERFLY VALVE, An actuator-operated, rotating" y0 M; D+ `* G% U* U device in a$ F8 y: {' W# | p ' _+ K7 L% W4 SB5 v5 m1 N! z3 ^8 F fu" f* c c! g0 }( {4 I 转动鼓轮, 6 A [( {' S) g/ h# G在操纵系统中,具有滑轮和钢索的机械式连/ D+ \; l- e, I 汇流条防护板,' G0 M) k" g9 J9 e 黑匣子式的 , t& T# y* l3 k8 e; t& z! Q/ K5 R% H) y: I, F+ m 蝶形活门,9 ]6 m3 k+ V; F W5 ` 是一个在管道中由$ [- }- s+ D+ C6 s0 F3 Y: i. I& g9 P+ |% ]/ B% I4 Q 纵剖线,2 \8 {$ k4 a" K0 p' X+ w 英汉对照民用航空词典B OEING) P+ A0 J5 e, Y+ ~6 y3 F TECHNICAL DICTIONARY 25& c2 l4 q. E; s BYPASS VALVE, A valve through which air or fluid will 1 ]0 y2 ^* Y- `flow if the normal flow path is blocked. $ @0 [" ?. P' h. x5 d$ pBYTE, A group or string of binary digits. A byte is 5 p; g& ` o: ^8 Msually eight bits long. # n4 `, v- g A* ~' m% } r, ?3 jABIN ALTITUDE, Atmospheric pressure maintained+ M, a: ^$ i! t% l; Q* J# ^ ithin the cabin, indicated in terms of feet above sea# p# y7 j1 s3 p% y& p( N7 ` ALIBRATE, To repair, adjust, fix or correct the \( V- T; t4 B; y+ j/ i easuring capabilities of a measuring device.+ O8 O3 M7 K) n- n/ s% r5 o$ X ALIBRATED AIRSPEED (CAS), Indicated airspeed 5 b7 ?0 {7 }, a7 lAS) corrected for position error.7 G) V) f4 `$ _ nical * k, G3 l: a- h$ d# C) komponents. # {0 Y- j; p5 X+ y$ ? J$ k7 |7 S% `$ W+ `! E/ S节,8 c: B4 A, b0 C- \ M0 }6 U0 Q 一组或一列二进制数。通常一个字节长8位。. f. x9 [! s) v' ^' ^ 舱高度, 5 D( L9 U( ?( }: d/ F" H8 N座舱内保持的空气压力,以海拔多少英尺表示。) i7 u- C5 @% ]) m1 S- T 准, * s' C3 E8 Z" r" O q+ U6 O修理,调整,定位或改正测量装置的测量功能。9 A6 f$ P! S: R 正空速(CAS),4 ^) j) _* n- C* ~5 d" Y* z! f 在修正了位置误差之后的指示空速(IAS)。0 R7 L% ~. ^/ ^* w5 B3 m% j6 H 用来移动机件的一种转动装置。 d1 N+ }: D' V$ q6 a9 L u $ g" w; X7 Y+ wC ) t8 l k4 L" a7 E7 QC 5 W7 |! c2 S1 ~* cw+ f. {: s7 J0 z' {- u8 N7 g3 b3 m* p level. l/ Q- n% H: b$ j C, j5 y \0 A7 l4 O# @1 N m 4 o9 A1 [7 E" E) E7 V- VC* u0 r+ h8 D2 B Y1 p( D' g! \& h7 [ (I0 b4 v5 e+ }' _$ e1 c" c CAM, A rotating device for movement of mecha 9 I" ^! }( d2 P+ j$ bC ( |% R/ `! z: L' o旁通活门 . y1 K- X" C8 ?气流或液流在正常通道阻塞时所经过的活门。 8 b: O; `5 d& G: m }! U- \) D5 u O3 v0 ]) Y: X( B% y' p- t: |; x, s3 o( }/ R. ~) q8 O" b% ?3 f( O" M9 ^% @8 ], k 凸轮,4 B; V( I- v. u3 `' U( v- _ 英汉对照民用航空词典B . y3 a) [, d9 m! GCAM-OUT, An autopilot condition in which the actuator " u! c4 `& d5 d2 i# I. s, tdetent piston is overridden, either manually or by the 5 {' j$ P; ]" X: n1 k4 i& ?, hther autopilot actuator.. x6 P" E, L+ L4 i' g- s! Y2 n AP, SEE - CAPTURE " q- L% Q1 G3 u* I; K) `7 }# [6 [. Y# vAPACITANCE, The measurement of electrical energy , Q; L# \; ^) j9 x, @0 u8 {tored in a capacitor (condenser). - f) H7 n2 n) [$ } `5 R" kAPACITOR, An electrical component of two metal# m) u* e9 O. }( I7 T* R6 Q lates separated by a dielectric material, for storing+ n9 Q- W$ P, K" y lectrical energy. 9 j( l9 T- i% r8 v/ z( cCAPTURE, An autopilot or flight director function to, d" b7 `, P+ O; t( m( C acquire a selected mode.$ H; T, S# y. p4 y6 L" [ CARD FILE, A container on the airplane for printed 9 ^ [- d) b7 g% l4 v) N% g$ F) Z$ ecircuit cards. 0 Z9 W3 v8 n$ b1 m. ^+ O一自 7 l& f' B; N! i' y动驾驶舵机所超控。 8 U: n/ Q) M1 V- {; d9 T5 ]截获, ' L5 l4 j& v1 T4 j见Capture0 N8 a- j0 _/ ~8 D, J- W) T' Y o % S( F+ Y% x F2 KC6 w: o5 ?! e# l, n u3 ^ C4 }' e8 [8 Z3 \% v+ S# q4 Y s1 z& e, g( X% }( `; R( { C ; n( G# ^! C4 P9 C& b. u+ Q1 _# o, V) dp # K- y& q) E. r# ?& p- K7 T3 E( Ge% e, |. R- _: _' O6 c, I 凸轮不工作,6 W9 M# |$ I4 M, X7 V! `& ^: e 一种自动驾驶状态。此时舵机锁定活塞被人工或另+ _* N( t8 Y4 n. n. N( R# J, q8 {: o t A8 y3 g" p9 R 电容量,. ~2 E% n" }( F) |/ h5 Q/ Z 电容器内所储存的电能的量度。 ! t2 I, }0 j3 i- P7 d' `% l. G' X+ l容器,: M1 J9 F# ?$ s2 s5 o 两片金属中间用绝缘材料隔开的电器。用以储存电能。; I3 t4 q n: \( [8 L: C 截获(CAP), ' D, N+ Y& W* q2 {自动驾驶仪或飞行指引仪的获取选定方式的功能。 ! j2 S: ^* K# c线路板盒,; }. ~ _9 \1 e6 q& \8 o2 _5 z' I' i 飞机上安装印刷线路板的容器。 5 a" d! c0 M6 J/ k9 a0 [0 m) v1 t4 G+ }- F$ }% ^" X# ^ OEING# b/ T/ }4 H5 |+ F# m TECHNICAL DICTIONARY 26 - E9 A" L7 z+ ?- k' G" o7 }英汉对照民用航空词典B OEING 3 E3 a: {6 p* H6 nTECHNICAL DICTIONARY 27 : l j& r* k, W2 m; M! `CASCADE, Two or more similar circuits or amplifying 5 w V" v& M& ~6 I8 w& a+ ^! z5 _stages in which the output of one circuit provides the5 D R/ Y- z/ X& K' h put of the next. `3 M2 ]5 x5 G ASCADE VANE, A vane for turning the engine airflow & w5 u4 u8 u' iuring operation of thrust reverser.$ q" ^% ]. r) U+ W" x' F ASE DRAIN, A drain carrying lubricating and cooling( |( n V. q h& B uid from a hydraulic pump. " f2 N/ j5 i- k; ^3 IATHODE, The element from which the principal * j% A) z3 }& f) P) d" l3 Vtream of electrons flows. 2 v3 g/ m" _4 I2 \9 M1 e! c$ [ATHODE RAY TUBE, An evacuated glass tube with a 0 }; y9 {" U& v7 g) KCEILING, The height above the ground or water of the3 ^, X! X& l$ U3 s4 y base of the lowest layer of cloud below 6000 meters+ _- J, D. f1 J2 i& q3 w (20,000 feet) covering more than half the sky.2 s6 Q, o+ e2 W6 F/ T2 s 程。该 ! u' J5 Z& Y/ S% m2 _. K程中,一个电路的输出为下一个电路的输人。 9 {4 z; b/ U6 X) ]7 j5 `叶栅叶片,. ~5 L' Z! Z* y" m) P 在反推工作时,使发动机气流向相反方向流动的叶片。3 Z, o4 d- \. p 匣余油管,3 g" Q l+ a/ `5 J: V5 Z 液压泵多余的润滑液及冷却液的排放口。( y- `& r: [( m4 s 极, ' S6 @0 b% z' z+ X2 l电子流流出的极位。 4 v( z) M. t$ X0 [4 b极射线管, ! z+ r. ?& \" `. v* |' K" c, Q有显象屏幕的真空玻璃管。用于显示信息。 % P6 U% _! J; `9 O' b i云高(云底高),) ?% Y6 t( a( k 6000米(20,000英尺)以下已覆盖一半以上天空的最 7 S0 @. D2 D- Y) Z4 y低云层底距离地面或水面的高度。 ( j" C' C1 p' `* V& F3 p! h9 E1 i) `in6 \" A3 e$ `3 l% T C 0 L- \0 o6 h1 m0 m6 ~3 h! Xd$ f& e4 T9 A1 K& a! } C 1 o7 l3 ?; N% e' F. b) hfl4 Q6 W' j) J4 i5 O C 4 q, [! U0 v I# Q# x) K# Ds2 D( ~0 z. g4 [( N3 s C# e7 d0 }' j" Z/ \; K: l, S! C viewing screen, used for displaying information.4 b! a3 X- ^; ]. h4 t 级联,% | p& M( l$ ?$ D! _0 g 两个或两个以上的类似电路的逐级连接或放大过" t% L- a& X3 |5 ^) X3 z2 q2 X8 r! U' ]9 i: P1 D2 n3 t+ s* Q' K4 i- A" f$ x8 v" E% f3 G- {: y W# ~5 b 一个具 8 W1 {: X& T P3 [9 D/ Z英汉对照民用航空词典B OEING- ~6 V+ Y/ x0 T1 |- a TECHNICAL DICTIONARY 28 Q- K, o# P: X( ]: ~! F, p! ^ CELSIUS, A temperature scale in which zero is the# i2 w& e% }$ w; i: F, ]' Z5 f5 f freezing point of water and 100 is the boiling point of3 ]; R# }# l" Y. N: } water. - @/ n& j5 H5 ]$ F. yCENTER OF GRAVITY, The balance point of an object3 |5 ^" L9 e0 s2 ^4 V7 o r rigid structure expressed in terms of percent Mean ; q2 L6 _5 \0 N7 t) {7 ?erodynamic Chord or in inches from a reference point. . K% O# [; I6 b: |' p1 r8 Y6 M3 nENTERING CAM, A cam for moving a mechanism to a - w9 u) y- ]6 l) `' [' s, aeutral position.8 \ P F ?5 a. j: s7 F$ H0 r IGURATION, A configuration of the ( M# p* M5 m4 H$ M i xircraft approved for operation by the local governing $ W/ g- E$ W a4 j& n/ q. Sgency. 1 G2 K7 u5 ]& xENTRAL PROCESSING UNIT, In a computer or/ ~5 T: `1 w; w: Z igital circuit, the section containing the arithmetic and: e6 U- w% y7 J- f, o/ ?8 O. m gic,control, and internal memory circuits.. H. s# O- F# `1 Z" E ENTRIFUGAL FLOW COMPRESSOR, A type of5 B# |* v2 f& k ompressor in which air is taken into the center of the. T2 n+ x. e7 ? peller and is slung outward centrifugally into a diffuser * C9 J0 F# P; z- zhere it is slowed and pressure is increased.$ Y* R6 S. _8 Y1 C CG, SEE - CENTER OF GRAVITY+ b6 `, O! S: }$ |# X: Q+ S 构的平衡点,以平均气动力弦的百分比或 2 x2 r7 f: T2 x9 [" T某一参考点若干英寸来表示。 , J% L. E2 k2 F- ]+ S! a中凸轮, & N' W& G# d5 v+ X将机构移向中立位置的凸轮。 + S, F- I3 z5 L1 ~4 d+ S格的装机状态, ; q2 \. c3 g- ^: Z' E由当地主管单位批准使用的飞机装机状态。2 h( m0 R* w" H2 `0 l 中央处理器,1 ~( i- m: K9 s, T 计算机或数字电路中含有运算,逻辑,控制和内部存9 m! k6 Q0 {% Q. R% a; C# y% C 储电路的部分。0 |- ^. Q) ~& O" h4 B8 `4 F 心式压气机,9 Q& J( O8 s& c. Y, B 压气机的一种。当进气到达叶轮中心时,被叶轮离心抛# l8 x: ^+ N/ J4 g( z( d; F 进人扩散器。在扩散器中气体流速减慢,压力增加。 $ x/ Q' y H Z( u重心, ! l( S* L r; |# h, ]: W. `见Center of Gravity; a M' N2 {- i( ?& J5 w3 K, r o 1 K4 u- q! H W4 {A 5 W7 o; K. [, B0 I; ?C- X# \1 I: J3 O# @; e n7 Z! M/ z4 _0 J2 B, K) V% e CERTIFIED CONF8 V: x' j7 j3 d a# [& c4 k: y, H( l8 A a" b) z- d, H' ]/ ?' r C* k! |& f2 Y3 M. Q9 T. C d 1 B3 { x" b7 M4 A) r* X" wlo) K5 f& R, V3 u6 k C: x5 N( @& z5 c c 5 _1 a' |/ w7 h; j R$ Mim 6 A3 U0 s0 t* J; a6 q9 s7 ~* W ?w . A' |4 _6 {" g' s/ f8 b! I0 {摄氏度(°C), - C8 k2 E2 }/ o温度的度量单位。在此单位中,0°C表示水的冰点,' [3 y& a: L/ t; G1 u1 V 100°C表示沸点。; l1 ^/ K& v' q; [; s* m 重心 " p, d6 [' j( E& c/ h物体或刚性结 ' u% d+ v) q0 v) _; m* ~5 Z- r: k' B% h& F8 @4 g( d* v8 @0 g0 t/ X E8 e. T5 |+ j, A3 X0 s7 h8 v7 }0 I/ n( k) e, o) G q+ W% m/ d3 ^ b 英汉对照民用航空词典B OEING# I' k( Z) A/ e( c0 p TECHNICAL DICTIONARY 294 P+ [0 n. k! X* }2 W* {. X CHANGEOVER, Conversion from one mode to another. ( q& ^# f* s) q7 IHARGING VALVE, A valve for supplying air or fluid to 0 [8 z) O8 Z! X9 D" {6 CHECK VALVE, A valve allowing flow in only one / k! t3 ?' T8 e# ?; `irection. See Non-Return Valve.5 D6 t) ]3 y4 U' h" C HECKSUM, In a computer, a summation of digits or2 B! M, g i- z) R7 N& v' f3 W" E its which are primarily used for error detection. ! A1 X$ d0 H, }$ M) m4 ZHIP DETECTOR, A magnetic plug in sumps of) h3 Y, A8 b/ [4 [ bricated components for detection of internal failure of, C' S; D7 f( v2 r. q4 s6 Z e component.' u" N8 |- g9 l: q HORD, A structural component of spars or frames.. d- y% L2 A: X, X+ y3 U, k/ R8 P 添活门, + t' a/ W) F h/ V: u3 z7 a器充气或加液的活门。7 f. Y- F3 q0 z: x 单向活门,' X7 {! |# k+ p' h. u, n' j$ W 仅容许单向流动的活门。见Non-Return Valve

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发表于 2008-12-24 21:38:05 |只看该作者
C/ U- ]' @8 E' w( M* W( r% ` a reservoir., t9 j" V" _. g# N. p3 S C, P2 Q# W7 c% ~0 w1 T d ' f; u* [: Y/ j- |" U# V4 Q. jC ) _4 g3 s$ g# g5 r6 p( ~' ]b 6 A" ]' f9 [! Q6 N4 D* OC9 O+ j ^8 r' C# ?1 T6 W2 G0 E lu: c4 N% t4 @2 J( O6 T# u8 A# c* S+ @ th ; J4 h4 B4 f+ y' KC 5 E* e) \- O, f, B. m1 ]& x转换,) a# T9 k% u: V' u' C8 t 由一个方式转换到另一个方式。, c1 i! R: m5 f1 D* b8 N" g0 B+ U- V' ?/ D' q 用来向储存 , c9 m0 e, `" _- h1 W) D1 T9 y$ V% U. G( h& o 总和校验,0 i: ^! [4 b% O" n 计算机中,把那些用来探错误的数宇或位数的总和进 * G, r, M; b- B求和计算。 , ~2 G" ^3 d! [0 P1 m4 G属碎屑探测器, ( F( P# Y2 j4 |) l; V# O装在被润滑的部件滑油回油管路上的磁性塞子。用来探1 e. h7 y1 b& S0 t& _' D5 g5 P 部件内部有无损坏。1 I* B0 i3 _7 G. g 弦, 0 u& U" B/ K7 Y( p9 M3 P" i, q梁或框架的结构部件。 8 B6 w# a( H# Z9 u) U8 l8 Z0 P8 I7 r M* W* _: s% s: y( N& W( a! h" R7 c* h) F' z" j }# T9 I! @1 E' P0 m9 y* H# `- h$ b, \9 a 英汉对照民用航空词典B OEING. K& M6 Z% K1 N5 |" Y$ ?2 f9 g TECHNICAL DICTIONARY 30 1 `5 X8 |) K2 t$ |CIRCUIT, A closed path through which current flows + \' a, G3 @$ S# y1 `1 s# aource.5 I4 G- Z5 X+ E: q) i. F IRCUIT BREAKER, A device that automatically % K. w( Y' M) Q" l* B. `eactivate the system. * i" Q* c& m @2 t0 L; I4 p; Hlear of all non-frangible objects which ' `/ m \0 ]6 e# Day be used as takeoff distance available when 6 y* `! \3 W* A8 I3 A$ x2 K6 k. galculating a takeoff weight. ' b0 z7 Z. X: a% u0 G3 Dr water under the control of the appropriate: R& x% x; [" I& X uthority,selected or prepared as a suitable area over- q3 Q! n( d) F, n# l9 ?) S hich an aeroplane may make a portion of its initial- o* p7 \( k+ J. |. c, `5 u; E limb to a specified height. 4 q# U- E; z2 _ d' l. Mincreasing. ( _( j* c, b3 ]0 ~+ Wsed: N" @$ _& a; s LOCK SIGNAL, A continuous string of pulses used for$ F- H$ E# b* p 开关,5 V* s" F) r2 I4 J# V! @6 W, j 故障情况下自动中断电流以保护线路不受过电损 - o9 Y5 s* u( L体障碍物的区域。在计* v/ G' l/ c* u5 ?; p5 D2 y 起飞重量时该区域可作为可用起飞距离。3 d4 q( H; \4 p: s9 \2 g# n; S 是在有关当局管辖的地面或水域内一个界限明确的长 * n0 ~" Z9 f+ h% O" U% }形区域。在这个选定的合适区域内,飞机可完成初始爬 $ D8 E( J0 |1 A$ N5 o5 P的一部分,上升到一个指定高度。" p( ^/ j; h. I: [ 飞机高度不断增加的飞行阶段。" F# \% P# z- s 钟脉冲,$ H: J3 r! q6 e6 P( \/ G! t' @ 步的连续脉冲信号串。 , G: M& K! J9 W$ {from a source, through various components, and back0 Z9 W5 R" Y) A3 F1 W. o to the s6 {2 s0 O( M L$ O1 _* n C1 `& f% C( O6 n# H% h interrupts the flow of electricity (current) during fault/ [8 S- @8 x- F& ~, B* h' M! _, D# p condition to protect wiring from excess current. Circuit1 W& J/ {, ?" a! @ d* i breakers are also used as a means to manually ( S' s' o2 @8 {0 N6 qd $ Y; l( {. q% g. WCLEARWAY 1, An area beyond the takeoff end of the % n- g6 x" A' h3 M# }* I( J- drunway which is c' Q: G( h, X- D8 ] m : `, C* f: O/ m) [+ M! lc & R* R1 N$ e' D( U U5 b% T- UCLEARWAY 2, A defined rectangular area on the1 u7 i3 P; O5 P0 n; S0 k3 @ ground o; e0 ]& r* m2 J% s) M, a a * R6 F( {# Z0 R* Z" S: lw + F9 H+ G+ n( Uc9 Q; i8 \" ]" A5 R" r CLIMB, Phase of flight where the altitude is " n' P9 |+ E& [; j( d+ ^CLIMB LIMIT WEIGHT, Maximum takeoff weight ba " S: D: N. }( R% K4 kon a minimum climb gradient with one engine 3 Q8 ]( `8 z; \9 g, uinoperative. - u% U' j$ m3 v. s6 {C3 s" G& n: ]# j( ^, {& P' C synchronization. . Y2 O" Y7 E* u6 V! B电路,/ t6 S1 ~" k* v; D9 { 一个闭合的回路。电流由源头流出,经过各个元件流回 5 c' s1 T$ F+ H+ m源头。 1 A; e9 \2 Q6 k- i$ d. |3 n% k, @* r$ k- K能在 4 _( I2 q. J: ]" e) E坏的装置。跳开关也可用于人工使系统无效。 # d9 `& ] o, g( F5 Y一号净空道, 4 e. B, M, y' O$ ?) \" N! M是跑道起飞端以外,不含任何刚 : h; u" V. ?( x U/ ~% J0 F; t% J7 P' q+ x' R二号净空道,& l" n9 P/ u& A7 p6 A6 v. b! ~3 L O1 t$ f1 Y8 [3 v# |% D5 S- q$ T2 q. S; n爬升,0 i o- y7 v. l$ J2 Z* D 爬升限重, 8 L; m* U: I9 T8 D# |取决于由一台发动机工作时的最低爬升梯度的最大起 ; e i1 a; N2 v* S飞重量。 : ~% I1 N: z6 w |$ F& F% T/ \; R% {& o) {; a0 a0 R% E用于同 * g/ q5 K" P% _, i& F' ?" s0 G- F英汉对照民用航空词典B OEING: e9 t0 _$ O, A& C TECHNICAL DICTIONARY 31 6 v" N- k* [. G& |COALESCER, A device in the water separator for# p# H1 j1 Y) k& Y; a ollecting moisture from the cold air.# k+ Y! i/ R4 J# E0 w3 d5 Z' B9 D n antenna with a receiver or transmitter. $ d. }9 ~. K% B1 dhe cable has an inner conductor and an outer/ p+ C1 a" Y8 k7 C/ R5 k! Y rounded shield.4 \% y: ~: u, o# A3 p& U ting one inside the; H. ^, Z8 v. w7 M ther for rotating the low and high pressure+ n5 J9 ^0 H* K2 n" K ompressors by the low and high pressure engine: O2 v1 f/ M" ]0 x: P4 u8 ~ rbines. / O, u& b% _! B1 o# i9 |" NOMBUSTION CHAMBER, A part of an engine for- X. a8 g, k, \* f1 S) g urning fuel in the air supplied by the compressor. ) y! B( U( |; o7 e4 @2 B6 ~( c- F置。4 O4 z$ l, g# N- | 射机的电缆。电缆 ; A; }0 X) N* M$ g8 J中心导体和外层的屏蔽所组成。9 O z I! _4 V2 k 两个套在一起旋转的轴。用于使发动机低压和高压涡轮 . p# {3 ^$ c4 ?$ v: s U别带动低压和高压压气机。 + q0 [# A C& L$ j7 P5 e7 m烧室,# g8 p/ d0 ~! ]/ x2 x. S 发动机的一部分。用来使燃油和压气机所提供的空气相& U9 o4 R. I, A8 ?6 v$ u, A, W 合而燃烧。

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发表于 2008-12-24 21:38:35 |只看该作者
c* j; q8 d3 `+ G& g! i2 E COAXIAL CABLE, An electrical cable usually ) C. w8 K5 \2 T5 @. X$ i4 H$ @* oconnecting a 2 A1 z% y; e5 h" @# R3 U: V# CT 2 J4 D6 M; p( k- V q, K1 y* Zg% ], ]# x c3 |2 g( [ l COAXIAL SHAFT, Two shafts rota, w6 m# Z/ _8 c- j% G% m o) {2 o/ z2 ]2 S# a8 y c , }$ r$ s( u' A: xtu$ e8 b$ o6 ^- n2 }' Z C6 U# _' A( V, g6 C8 p" B3 n' V b: j- N! K& X/ x+ E, I/ m 凝聚器,/ A2 E! y Q% j" j4 `3 b2 e" c 水分离器内收集冷空气中水份的装 $ C1 y1 e- Q( e! s; S; ]2 P5 y同轴电缆, 6 f8 s) t# ^% Y5 e) G+ S& `一种通常用来联接天线与接收机或发 5 S; u7 i" q7 U( U P4 H7 H; N+ k' N 同心轴,+ D9 U( ?4 s+ ~0 o* U' Y5 O3 K% N5 j; {& A" `% r9 e: |) A3 R" Z. O; X4 y2 e- @- l) r3 K+ v 英汉对照民用航空词典B OEING8 Y. Y) ^$ X( G7 q# r6 v } TECHNICAL DICTIONARY 32 9 x$ }% c+ p/ e$ V, |COMMAND BAR, A flight director pitch or roll comman6 s- { J# E, O3 s) F6 N; P- r indication., R5 |4 l& z1 H d - r' _/ N6 d4 q& C- |- g. u4 @OMPANY ROUTE, A route flown by the airplane $ E$ x. \) }3 ~& a8 BOMPASS LOCATOR, A low power, low or medium% V, R$ K8 g$ K( V0 l4 t: K equency (L/MF) radio beacon usually installed in# r2 C- G3 O# e' ^/ v% E- P onjunction with the outer or middle marker of an + s4 O; Y7 |8 q8 A# X! utor (LOM), A compass ( ^# \+ \: H% \ k8 F9 f3 a. V1 N5 Clocator installed in conjunction with the outer0 N! r% ~4 s4 H: N! t. k, F. } marker of an instrument landing system. , X7 ?: E* F* s: Wss2 O8 S- O' o/ L8 V le 4 z/ R$ [! c' r' g7 G. Y0 aOMPENSATION, To offset, balance, or counteract.; o) F1 S- v5 h OMPENSATOR, A dual capacitor for changing the fuel % H' y; G" Y' w* k" Kaging circuit capacitance due to changes in fuel - e6 f8 t0 W9 @( l8 Z% g9 w4 vensity.8 h. v; ~- z# l/ f" h2 a OMPOSITE MATERIALS, Non-metallic materials used ( d R$ K6 G ]0 P' q. br airplane construction. Fiberglass, Nomex, Kevlar,, _& b3 j& a; O, @9 A; |" @ raphite Epoxy are composite materials.! y( j# q3 M6 [& ~( L* N: M 司航路, / L6 p; m ?9 `/ C1 n在飞行管理计算机数据库内由航空公司飞行0 |$ Q& [9 J% [' |6 G& H m 盘定位台,1 h7 `! h. z, F8 ~9 X! v6 ?3 K 与仪表着陆进近系统的远距或中距指点标配套安装的7 V7 x" |7 D6 l8 { 功率、低频、或中频无线电信标装置(低功率NDB台)。 % Q' E! g" f: {) ~8 _7 J) E程序中用来导航。! p# F: M. h, z. B3 D) | 1.远台,2 C- Y2 W2 Z. D+ a+ s 与仪表着陆进近系统的远指点标配套安装的罗 , `3 F6 v4 Q. Q2 e$ v盘信标台(NDB)。 / V9 y$ r* j# U& F偿,1 E: T* y" r3 ~: }% g5 B8 F. J1 o 抵消、平衡、或中和。7 l: }+ S- X1 ~! u1 ]! f% U 偿器, - S* V* k8 Y1 S: _% _" R. i在燃油计量电路中,用来改变电路上的电容,以与燃9 U" w& H: j- |2 F 密度改变所引起的电容改变相抗衡的双电容器。9 u! ]! t8 ~/ x! z 合材料,* g) w) M, }+ v, |" ~. Q 用于飞机制造的非金属材料。如纤维玻璃,Nomex, 0 c8 e Z3 d) E% x/ 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' i! N3 w5 {" X2 r operator that is normally stored in the flight! H5 K! F1 d m% V- m3 V management computer's data base. 9 n$ h7 N8 a+ R1 JC1 g* e% r, q5 X fr& m. K# F! y4 c' U6 W c # b* t) S- e; }) R6 q4 [instrument landing system (ILS). It can be used for ( A6 V2 I% _, L4 ?navigation as authorized in the approach procedure.) p0 t6 I- {4 f5 X$ |% U9 U 1. Outer Compass Loca! E, D" V/ ?2 M% u 2. Middle Compass Locator (LMM), A compa 8 g9 U# E6 c; q8 t& ^0 H+ i+ olocator installed in conjunction with the midd9 t: C h# Y* E- u* ^* M marker of an instrument landing system.# i) A5 X1 D, k0 [& l. `) \4 }/ E C& d6 ]/ F8 N- `. z C1 Y4 c7 j7 `0 o) @ B0 i1 y% h g. r' v4 X }; l. o$ w" g- q, Z d8 y* J3 C4 r4 g; ? `/ ^" q C - b. d( b0 s( G6 O) ?) Vfo0 R: }3 a- j# i+ A1 ? g/ ]8 U; ?+ E) D# f 指令杆, # T* o( x& Q- X; |1 N# \飞行指引仪俯仰或坡度的指令显示。 1 m0 @# x" X' ^' p5 j2 o8 i. H 通常储存 % _2 A+ C4 |) e* Y; q) [1 }$ r; W的航路。" _: X2 Z2 k8 R) ?+ a b5 r4 b6 s5 _1 [) k. a9 v4 u+ ?: t. v o" `* W7 G经认可后在进近 8 n3 C) N* N! y6 V- r2.中台, ' |' X5 F r j与仪表着陆进近系统的中指点标配套安装的罗/ H+ Y. x/ B$ R& n' f0 d 盘定位台(NDB)。 ; u' M2 K+ u# n' V* }, |: @/ i i" C0 }, _0 S# L' T0 Y( V; q" c' ^ f7 D0 h8 J/ w: Q: N# v4 ^# `% m% {& R; I S5 ?K7 Y0 |6 z. e7 d9 U/ v) K 英汉对照民用航空词典B OEING4 h9 C H, H# F9 p" m( {9 B TECHNICAL DICTIONARY 33* T4 W5 d6 _' H s$ j0 K! \ by 3 t3 j- O- m2 |" }0 N4 Hor increasing air ( V. }" g! ~ r# G4 J6 V7 Zressure and temperature before the air enters the1 a' F9 T# G- q$ g# I: @ ombustion chamber, Low pressure compressor - front " o2 F; b' R! W: P1 {2 v1 Zection of compressor, High pressure compressor- rear( q2 s% F1 P) N5 q( e OMPRESSOR STALL, An event that occurs when * W# w; a6 a o# T( H7 y! @ere is a complete stoppage of air or reversal of air flow( ^9 b$ y2 y6 E. N1 h7 z/ g COMPRESSOR SURGE, SEE - COMPRESSOR; f1 b- ? w, S$ p5 M STALL COMPUTED AIRSPEED, Indicated airspeed ! U8 ^. e& N5 L% ?3 acorrected for the static source error.+ f) P, {2 ^: C- o: w 的机械轴来驱 S! `9 B' {" S5 P8 Q; P) h$ G3 v! |,用来增加吸进空气之压力和温度,以供燃烧室使用。 % c4 T$ ~6 a4 e' }- v压压气机—压气机的前段,高压压气机—压气机的后 " e2 |0 E1 p% O. z# p5 Q& V4 ^, Z9 O/ K J) k气机失速, 1 |- y, v0 o/ ?$ K当气流完全停止或通过压气机时气流方向逆反的一种9 i. ?! J) N2 ? 压气机喘振, + c) g! p% z8 R" Z; l见Compressor Stall . E! U5 A) f6 \2 e/ c: B$ X- C: JCOMPRESSOR, A rotating part of an engine driven. q. Y, y' W3 g1 P9 d. R R( Q a mechanical shaft from the turbines f 8 S- b8 w# J4 y0 H/ o; Vp 1 b# T) t# X$ H6 Lc + R9 X L+ _6 u$ R6 J) Ys( F+ ]/ q l e8 Y9 o section of compressor.0 b; U( M5 b4 }* y+ }/ j/ y, J C. H: O! c/ n/ Y* [ th3 Z! F6 C i: k; H through the compressor.* u3 z) e: x7 q: @: ` Z/ M+ k& o 压气机,+ H( \* N, t1 D6 W6 t" o! g 发动机内的一个旋转部件。由与涡轮相连: S; ?$ z2 F( O* V( k/ Q( P! ]' { o# Z- C% |$ o7 R' a- d* W5 h! P4 A, ]. n( u* Q0 d. g0 @3 k4 U: N9 h t6 r% Q 现象。+ J4 n6 v q' x6 j% T9 T$ t" e( p" F# _# L) }. H( ` 计算空速, ( S) B# _: F9 M6 Z修正了静态源误差后的指示空速。 6 D- P% T/ t$ x- o- U N+ w. ~( @英汉对照民用航空词典B OEING, G+ ^; J! t4 k 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 + r4 ~. R' d3 z2 aoperations, manipulates data, and makes decisions. 6 C& c+ y+ R, G6 [9 o ?) u6 H u! Qditioning ( K0 B9 Y- {. J( C0 }) C1 kthe air and the7 {! ^; M) I5 P frigerant or moisture vapor is changed into a liquid.3 }$ b, P( X- H1 b" A# t ine % t1 ?' |$ f& ?ONFIGURATION, The position of flight controls, 9 P7 x* e& r% J6 I [missing which 6 e& x; k* R* U, h* E S- E6 R7 fmay affect the aerodynamic performance of the ! a, p# h. ^: j5 K, t$ M8 _% pairplane. / C0 u! f3 z7 v+ x( J置。3 A) }) Y# l1 c) V 中能使热能散发到空气中,以及使冷冻剂或湿* Y- q1 c$ F; H/ o6 J5 Y& d 转变为液体的部件。! x1 _; y7 a& Q( _/ { 连接到飞机结构上。 4 _ @ R/ B% s0 b! L7 J态, 8 A" D# Z+ D _* F. X/ B6 k定飞行阶段中,飞行操纵面,起落架等的位置。 " k& R8 E+ O/ t4 S% J( y3 x1 w; v),. U0 Q0 E- B& F5 h- @ 受到影响。4 o, G# R5 N/ |! O. p: ]6 H7 B4 ? CONDENSER, The component in an air con3 }! x: o( m" X6 Y" F system where heat energy is given to' z$ c$ T. _% Y2 B7 h* K re B0 H, W6 b5 D9 {9 q/ R1 ?/ h CONE BOLT, A bolt in the shape of a cone for eng/ m3 _, x( b; O# b& W attachment to the airplane structure.' _3 O* l2 t1 B5 r- A! p$ u" Z1 l C& [( _; T: y2 }- ~ landing gear, etc., for a particular phase of flight, e.g.,; o6 S# ^% @, A, t: b Takeoff Configuration, Landing Configuration, etc.8 w- E3 |% }9 K) n7 h1 @ CONFIGURATION DEVIATION LIST (CDL), Appendix! }( `2 @* f# } in the Airplane Flight Manual (AFM) allowing operation. t! `% y/ g4 v of the airplane with certain airframe parts1 g' R; ^5 z: z2 a 计算机,4 E9 Z% `7 e% P 能作算数运算,数据操纵,和决策的装 & K4 L% \ Q- e1 ~6 _( w7 [5 [冷凝器, 1 t, Y; |/ t7 L+ V A) B' z空调系统 ! }2 K D- S; e* O, {; v+ |+ H7 [4 V% [) M( K& \锥形螺栓, 9 g8 X; c3 x6 V6 p" F i外形是锥形的螺栓,用以将发动机. p1 x! {4 A& i' f; X1 v! h4 {6 l: |1 d# J在某一特& R" F# ^+ i( {9 k 如起飞形态,着陆形态等。/ v- R6 ^$ A$ C K; C 缺件单(CDL( E, L0 x( I K* Z8 v: C1 i; h 飞机飞行手册的附录所开列的飞机上某些零件的清单。 W' f, @0 P- |6 V, r+ c在缺少这类零件时,可以飞行但气动性能可能 , e5 W7 V! Z9 i, i( A* u6 H% T) e英汉对照民用航空词典B OEING/ T2 y$ q7 E" w8 a% Y TECHNICAL DICTIONARY 35

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发表于 2008-12-24 21:39:49 |只看该作者
CONSTANT SPEED DRIVE, A hydro-mechanical ; E! z8 D& ^9 T& dcomponent for changing variable engine gearbox speed 9 u9 @- M+ s4 \$ tONTROL AXES, The three axes of the airplane which% d; c: A5 U% A( R$ ] re perpendicular to each other and pass through the ; i" @. R$ W1 w3 ]enter of gravity of the airplane. - M* h4 R- Y& i# x( zPitch axis - Horizontal or lateral axis, passes through& ]* ~/ G! p0 W! {! A! t the airplane from one side to the other - ; H+ p) t+ c# onose up and nose down control is by ; k2 q. O) @6 Celevators (and stabilizer for trim). 3 x F: t/ v% _: Q5 j0 i2 tRoll axis - Longitudinal axis, passes through the' @1 Z% R M0 O3 Y& b7 o4 B5 c airplane from front to rear - wing up and# a1 A q j) v: O+ Q wing down control is by ailerons and5 \5 ?2 Q \) m9 y, E' W% ~) T2 a) v flight spoilers. " K( B- n2 ?1 ?3 d# Q+ bYaw axis - Vertical axis, passes through the , _! X A7 F& R8 ]airplane from top to bottom - left and 0 n$ |7 I2 V7 z& w& E; dright control is by rudder.9 X2 g+ s3 ^& E: b( m 置, h6 n( a8 ]6 Z' Z3 O" F制轴,2 L- \! V- \7 ?9 F$ G# e 通过飞机重心互相垂直的三个轴。; ^; U6 M I/ k) z 俯仰轴—又称水平轴或横轴。由飞机的一侧通向另4 e# Z7 o+ V) Y8 B+ g9 l- N# r2 k& B 侧。飞机绕此轴转动即造成机首的俯与仰 7 U1 V9 x9 q- p: |( @俯仰控制是由升降舵来达成的,水平安定 2 }( P2 y% n2 w8 M# _ I则为配平之用。' p; A6 m& J7 ^. z 横滚轴—又称纵轴。由飞机的前部通向后部。机翼. e; i* a: Q) i& j$ c2 M+ E2 G 下运动由副翼和飞行扰流板控制。0 a/ l# N% H, q9 a 偏航轴—又称垂直轴。由机身上方通向下方。飞机 * b' P6 X; |( u7 F7 z v: ]& k此轴转动即造成机首之左右运动,此一运; \. v! ?" h4 D8 _" i' v 由方向舵控制。6 C0 w8 v% ^" _! `- a' b0 k to constant speed to drive the electrical power.5 y* s6 N; p3 H! Z C 6 n( V2 W- l/ {1 G. ka b4 O5 u! I, ~& c4 D# E5 {5 g1 ` l c * N4 S/ s) B, B$ t) y恒速驱动装 # x0 t9 s1 U6 {; s3 N0 W( `将发动机齿轮箱的可变转速转变为恒速以驱动电源的- K# I* ?/ P7 @! I 液压机械式部件。7 i% y' {9 z: p' H1 T( m0 I0 M' J5 ?, V- M* z; x; |1 |7 \5 h5 l1 b! ?( I4 c& a4 P3 u( t) ]9 w/ f, y8 J; {+ o' x. k: X W b, x& ?# r7 q( D2 S( Y8 S$ O" L: ] P$ u" _# k' b* e1 u; Y4 d0 v- d英汉对照民用航空词典B OEING % f; G& Y- ^6 E# pTECHNICAL DICTIONARY 36+ |. M, X& w) h& h* Z! I CONTROL COLUMN, A mechanical component used8 g. J# w3 |5 J- O/ t7 q rs . k- A7 J; V0 [/ ~4 |' dnd elevators. # l* T: L9 N! Z$ Y6 j5 R' w2 jONTROL SURFACE, Moveable panels on wings and : ]( l6 d/ I& e; A# Y( Y( L! ^il for movement of airplane on pitch, roll and yaw axes.* g/ L- h5 ~* S3 n9 D8 r2 c ONTROL TAB, SEE - BALANCE TAB ; t; m( J. ]7 ^6 i: C' d w# `ONTROL AREA, A controlled airspace extending 2 P0 p& ~$ [' o3 _% a% v+ E" v8 @pwards from a specified limit above the earth. * t: F: z3 w' \. J: Y% [ONTROL ZONE, A controlled airspace extending ( a' y& _! v, j) [# |6 D1 b) v# cpwards from the surface of the earth to a specified 7 |# V6 B/ i/ p; Opper limit.( q) @* _8 ~( z+ | is) V; K& X2 {. G3 q7 _, p" d. [8 A o IFR flights and to VFR flights in accordance2 m4 ]! z$ d2 M# O. u with the airspace classification.& ], d9 m9 |) G+ y 机械部' }3 v; t6 M% W f7 X4 l/ b$ g8 t" ] 操纵面,# y3 N7 ~, L3 G& z( | 机翼和机尾上的可动面板,用以操纵飞机俯仰,坡度, 9 L7 K5 j3 I. O$ Z和偏航运动。8 m7 r {' Q9 N3 b6 ^ 操纵片," w( O6 s+ f1 ~. k4 B" `- Y6 i 见“平衡片”Balance Tab

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10#
发表于 2008-12-24 21:40:09 |只看该作者
by the flight crew for operation of ailerons, flight spoile _- g/ f6 l# Q Y+ g a / j- @! B+ C0 d( {9 I: T9 l. H2 uC . I% L( `9 Z# u7 X6 E5 Y' wta ' a" y1 I! M/ F& c1 UC ) g3 i& S, s+ q1 bC $ Z6 F, \ e2 Y* D0 o. l! Du ! F) j7 `# W4 O; o/ _: V# VC ( S9 h+ t5 g* e, Vu- F/ u9 v* l# @' }3 n. t4 w u: C6 q2 F8 D1 F; O% x$ F$ i4 L7 v" ^ CONTROLLED AIRSPACE, An airspace of defined2 _6 n2 \, j! p3 ^1 ?- u( X5 m. ` dimensions within which air traffic control service! W/ E. S0 W8 n& ]4 H" G3 D" m$ f# Y provided t ( @: v6 c! { D0 P( J7 s驾驶杆," d) X4 P# {/ e+ D" q1 k 飞行员用来操纵副翼、飞行扰流板和升降舵的 + X# H2 U7 V- N; f4 Q: ]7 b2 n% }" _3 Y) D2 U2 [% k. A6 K& `; n管制区域,1 |: K; T) L* q9 \; Y$ ^' w& M 高于地面的指定极限以上的受管制的空域。 8 I: x p' H! c* f制范围, - @" I7 N: ]2 g( d1 Z: b) n/ J由地面到指定的高度以内的受管制的空域。" ^8 e" N6 w6 A% F1 B* r 一个范围明确的空域。在该空域内,仪表飞行规则飞行: x/ o4 X0 `7 x5 J 和目视飞行规则飞行有空中交通管制服务。2 B5 a1 O* f1 \& n$ f5 H6 q1 t# L/ g) j% d: h受管制空域, $ x7 s+ n+ B6 P+ g" L英汉对照民用航空词典B OEING) {) j+ U- ]( i7 |) Z; T, ~ TECHNICAL DICTIONARY 37 5 @4 S4 f$ |( ECONVERSION, To change into another form.; ?1 @* g( I0 E/ s3 Q8 Q7 p COORDINATES, The intersection of lines of reference, 9 k; K! M" C5 bsually expressed in degrees/minutes/tenths of minutes& s" v) P' z: @1 K7 @ f latitude and longitude, used to determine position or 3 R; d, c4 T- v# ]/ \* ZCO - w$ h. f4 o7 x. i* Jdestruction of th1 p: h0 t1 y! s6 p chemical conta- K; t1 i+ q# {( [: P2 h8 @ COWL, A remo5 ^( [$ J! J- V6 F3 _, [+ f for access to th 5 `+ W" [: z( J& S4 `Fa 2 ^ C9 _7 W0 C) W9 eNose Cowl - Front section of the nacelle for air inlet7 K% a- z9 Y7 U4 \/ s" g5 H to the engine. - A/ ~4 C( @1 m) ?Side Cowl - Cover around the sides of the engine.. s& y- S4 @4 R0 L! V Thrust Reverser Cowl - Cover around the core / z/ Y! H$ x ]1 ~, m/ Msection.2 L# l2 [4 U! Q; _& l5 p Translating Cowl -The moveable outer portion of the3 Y+ x1 L) N; r0 o. [4 k thrust reverser cowl which is 2 x5 _- _5 M3 ]: d x# Koperated during reverse thrust. ( ?; o' @! f8 u) C- x' K* v标,' P: q% P- g$ Q: p. k 基准线的相交点。一般以经纬度的度/分/十分之一分 / j. Q% a& U8 v6 e! i3 A读数来确定位置和方位。- Q' M% K) R" G& h& r 腐蚀7 e) C1 E# k2 n& s( T" | 动机外部可拆除的罩子。发动机上的构件必须要取下 4 d, B+ f& Z% C4 w流罩后,才能够到。 ( g2 X5 c6 i& Q# F( `0 z2 O. y6 {& m/ V5 f% W* r4 s/ b0 S 机的短舱的前段。 ! |! z( F8 T6 h* M4 I& ]' q% E侧整流罩一发动机两侧的罩子。 , I2 N; L6 B T7 G反推整流罩一发动机主体外的罩子。 * P) w$ A- s7 n% w1 ]) y; `; s: A" Y移动整流罩一反推整流罩外可移动的部份,在反推工7 m" X% ]' j3 V3 O9 T. b 作时使用。 0 s) W9 E6 O: T' a- ~u+ d0 d6 m0 S% B, v o8 ~; w. h- p3 T5 k u4 v location.1 p+ ]" [+ u5 u RROSION, A chemical action which causes gradual, f' \# T. _$ X' Q2 l e surface of a metal by oxidation or p# s9 p, h' T$ f7 N& Nmination. . A: y7 {; q- G% G! T' z- {vable cover around the engine sections6 h1 Y! {) N4 ]3 f8 @2 V e components on the engine. * @6 U: ^7 V$ y% Ln Cowl - Cover around the fan section.+ X+ v% J# w" E; ]- P# ?6 i! V 转换,' t: S4 r6 Q8 _6 M. U1 x2 U7 l 改换到另一个方式。6 i! Q+ S5 E2 |8 `7 V& d! Y8 E) u" \) G( W% V- i2 S" o3 Y* f' S) ^2 }7 v2 k: o6 Z% J+ ?% B0 n' Z 氧化或化学污染造成金属表面逐渐破坏的化学反应。/ m! K* I6 f5 y" o7 T* @# P" [ 发动机整流罩, 4 p* c: C2 S0 _" W' a+ x; X- }4 Y# n( U$ o% x, f% \, _1 ~$ u* `4 S0 \8 n: O" l/ D 扇整流罩一风扇外围的罩子。 t7 G( p2 R9 U% z0 W 前整流罩一引导空气进人发动 - k& t; x: o$ {# m2 p英汉对照民用航空词典B OEING2 V$ F' S8 e7 G4 B8 A# F% f( ]3 t TECHNICAL DICTIONARY 38 7 Y7 I0 x4 B" } `& z# M4 wCPU, SEE - CENTRAL PROCESSING UNIT- C8 ?, X7 t2 r# I; E CROSS TRACK, At 90 degrees from the desired track 9 {! g- v p) J/ ?; l1 C( @. v& J, [f the airplane. For example, cross track distance is the. m- }! N, _# c7 ~! z/ q0 H istance from the desired track measured 90 degrees9 \7 l) ~' M( j7 \6 w om the desired track.4 i+ l( S5 R% } ROSS-CHANNEL, Electrical wire(s) connected from1 P8 O) \/ s2 L8 E& ^/ u ne system to another like system, for example, FCC ) W4 t6 }) l& t( b" to FCC "B". / v* f3 a3 d) ^) T8 f) Q) F* mn adjacent engine or one on the other side.' I8 z4 V- q- t+ X, b+ n8 M1 x l crossfeed 6 t! f$ x( j( [! S5 @anifold for fuel flow from one side of the airplane to the ) e x4 g6 q ~- a G) a0 @ther side. s. r: @; d. }; ]# ]5 ] re* ~% u1 ^% M* D4 t. o7 s RUISE ALTITUDE, An altitude or flight level ! G; w+ I" `" f; q+ K0 r |- \0 W* g5 T o & X( i# }. t, Vd9 g5 k7 C1 k! s0 e: | fr 1 e ~: b/ v% M% m) g: oC ( D' P: y$ A. R0 U4 z( ]: V7 c, Q% jo " B9 T1 ]! I9 N8 l5 }2 P* J"A- t2 K6 q* d4 N0 c CROSSFEED, An interconnection between fuel6 p7 M7 ?9 S3 @- B% C/ t# h' U) B3 N9 e/ V manifolds for fuel flow from one side of the airplane to: P0 S) `$ F& `1 g8 N4 I, J a 1 W+ d# D0 k9 k! d( xCROSSFEED VALVE, A valve in the fue" h6 J, U/ _4 H' \; W& e% ^ m * [. Q' {8 s# e' Z* A4 ro ! j2 U; @0 C) P9 [$ e8 v- rCRT, SEE - CATHODE RAY TUBE6 @$ w# \- t. m P3 p" ] CRUISE, Phase of flight where altitude and speed a- A4 s0 Y$ L/ e+ P7 y% y' E basically constant. 5 @) T' K- K$ x* A" f2 r8 {# I8 rC1 ^. B1 a2 |) C. @# z% f( E maintained during enroute level flight. ' B4 w' z; B; C$ T6 `中央处理器 ' G: U4 P7 L- U! M" L" V; h0 d6 k见Central Processing Unit.& Q* o, o/ Y# h4 a 交叉航迹(XTK), p9 ?- l; y0 ^与飞机预计航迹成90°角的航迹。例如,交叉航迹距离# M+ b- o: C9 [ 是用与预计航迹成90°角量取的到预计航迹的距离。2 w$ b8 n9 a4 N+ _- D' b" v 通道跨接, & d- j" x- v! n4 T7 H, Q# J: Q电线由一个系统接到另一个类似系统。例如:由FCC 0 _6 l" c4 f5 L$ O“A”% ] c) c# i% `2 `! W! u7 o 接到FCC“B”.: `$ Z ~4 g2 O 机身另一侧的发动机。 : o/ b: J. o2 }于使燃油从飞机的一侧 - q4 S; }: m h4 Q) R向另一侧。# \ j/ Y4 T! D* L3 G 见Cathode Ray Tube2 v, ~/ m0 g8 d1 ~& |& } 交输,% w6 B$ l( {5 f$ y2 ~; i 燃油支管之间的交连设备。可使燃油从飞机一侧流向邻 ( G7 i) b. `6 c近的发动机或在8 U: U) H3 n; N7 N8 ? 交输活门,: ] n0 s% I: u2 H# N0 \ @4 V7 l: Z 燃油交输支管内的一个活门。用 0 W; K9 u2 t1 K2 `* a# k+ Y& H+ u1 a0 b3 r6 l, l$ o+ r 阴极射线管, 7 a$ F& a: A r8 H9 U! i6 ~) O' A.# p3 y/ k3 V3 D& t) H 阶段。( }) g6 _ j4 g- V( l 航高度,! V: v0 J s8 t: e, k( v 飞行期间,飞机所保持的高度或飞行高3 X! X' h8 A+ U7 C# [# x& m- C/ b 巡航,& g$ L% t( m! Q 飞机的高度和速度基本上没有什么变化的飞行% }2 H( _ a3 M/ _- }, q' B/ ]; ~ n- A; }& v 在航线上水平. R. `1 @0 K$ Z% [9 n& Y: ^ 度层。 r H$ u& V5 f/ m: {2 o. u( f英汉对照民用航空词典B OEING Z7 Y3 _/ H- WTECHNICAL DICTIONARY 397 g# l; l. k+ X% a; d CSD, SEE - CONSTANT SPEED DRIVE- } I7 ~$ b& _" b6 Y% S9 ^ CURE, A chemical change which takes place in a resin9 Y% o0 L- R% Q- i and fiber based component causing it to solidify. 9 S2 v& H- V9 l) wCYCLE, A complete series of events that take place 2 R. d7 z" ~* P' b+ O- p9 a0 Cgularly normally in a continual sequence.; ^% B7 ~) I: b AMPER, A device for slowing down or limiting. f& w, t9 |% s4 h/ E DASHPOT A mechanical damper for slowing down 6 Q4 K# }! d' _7 r, v' fovement by restricting fluid flow.! h9 N2 _5 O- c! q) o6 B D ( p" t b) c; V* C9 p# r. w3 }: aATA BASE, Stored information which is used as the# A1 W- i2 f( x$ y6 M; r, o$ y8 n2 R ba2 o! d4 ?# X- _& Q/ X1 K DATA BUS, A conductor over which digital data is . * u/ s5 G* W% P; jtransmitted. # U$ h9 o* W4 T, ]6 V: VDECELERATION, To decrease in velocity.2 M0 s% J3 P) x j 装置,6 d: [+ V) H! c$ ^* [. M5 F rive ( M0 L/ `9 \+ Ere$ v T. i* I: B2 u; C- ? D 7 } r/ f. @4 C! d. uD4 s1 I% j8 f4 o' h9 p movement. # ]2 p8 e7 @( E lm, w: P) `: H- i7 }/ j1 z- L& o. R1 @ ATA, Another name for information. 6 F" e5 @( Z g! S J" S. s$ eD" U6 P! i) q0 @1 S8 D% m sis for computation." F, M! g$ z4 C% U( ]( x4 C 恒速驱动 # s5 z6 N# `( S5 Q# T见Constant Speed D . ' d L6 _( C- r; ?期, 6 M9 A. B, x* h N1 K9 B不断重复发生的事件的一个完整系列。 - a6 N" `8 r P$ `. z F9 p尼器, 8 F' H3 s- j' i) I6 ?4 {慢的一种机构。 ; o6 L( ^0 ]0 O' C5 ]4 U$ Q8 s3 M0 P; g8 p6 W I' x 用限制液体流动的方法以减慢物体运动的机械式阻4 n: I# J) i; l2 V! @6 Z8 Q& W# N/ E4 b {, J/ ~9 c# }8 j1 o" u0 } 料的另一名称。 $ a3 p# o6 \7 R" y) L9 @据库, 7 i( q& M( c l% I数据总线, & \: Z# r1 i) o) ?. |9 D一条或一对导线,用来传输数字信息的通道。 2 a( K' U5 q& t# ~( q减速, + @. b6 `0 ?6 ]. b速度随时间的递减量。 ! V( T7 [- l' L8 ]" ~: {$ z* h$ x固化, ; X( c) e0 ]+ \# O1 j树脂和纤维部件内化学反应使之成为固体的变化过程。9 Y8 m3 `" a$ U: a8 i, ~% Q5 V9 T. J5 n! {" s4 k% `5 X" X( G @8 p: \3 U7 J" r7 ] I I 用来使运动减 9 `5 X+ `+ R4 z6 b" ^4 I x# U冲器, / `% Z5 l. u3 h: ?0 @1 I* _器。 + `* x3 O( B. o8 ^据, * @- b) i' F$ t" x* H5 t6 Z7 N" W! }) e) s3 h7 k' e! z8 ^( q9 _$ I# C% M6 v R" R 储存起来以便在计算时使用的资料。$ [4 z* \9 I! ~- F3 D 英汉对照民用航空词典B OEING 5 u" Q+ M5 L# w+ ~+ c5 v% NTECHNICAL DICTIONARY 40: z' x& {/ c% @) P7 t! r5 k DECIBEL (db), A unit of gain derived by computing the' X1 W: t# _4 G/ q$ Z) h tio of input power to output power.+ Q. b6 A+ b: V) w3 T ECISION ALTITUDE/HEIGHT (DA/H), A specified ' ~8 p- J6 M# I o* Fltitude or height (A/H) in the precision approach at1 Q$ `- K, _% e, q Y% N hich a missed approach must be initiated if the) v7 R/ k5 j7 S$ R7 k ECISION HEIGHT (DH) 1, With respect to the ^ `1 |( ?1 G proach or / o7 o k' U% S! q4 T( @2 Nexecute a missed approach. 8 m2 s6 k6 d* Q7 {8 \proach to trigger the decision of either 5 d( N% E$ G2 Cnding or go-around., H3 r# Z8 @$ ]& q6 y# ~ ECOMPRESSION, The loss of internal aircraft air7 W+ c/ n- C3 k6 L3 Q" ^ ressure.7 q1 A/ j. M' Y: D E-ENERGIZE, To turn off or cause to not operate.6 l" X6 |+ A* _( W6 L rom the tanks " m) b. |6 E1 C7 m8 a- b, susing airplane fuel pumps or external suction. ) G* ^: n" V2 h/ _算的一个增量单位。分贝 . y, B& U& p) d/ t! _常表示两个声音信号或电力信号在功率或强度方面的6 r* f s2 W) Y! Q# W- R0 z 对差别的单位,相当于两个水平的比率的常用对数的十 / ?6 {( ]8 q/ I, b0 j+ M6 b断高度/高(DA/H),8 z: p1 W; `0 w6 ` 在继续进近必需的目视参考没有建立的情况下开始复 $ e5 u7 {6 e$ J7 ~- H9 j的精密进近中的一个指定高度或高(A/H)。 6 k7 w2 w* u/ Q, A6 O断高(DH)1,% d/ J6 o( Y! \0 c) _7 T 操纵而论,指在使用仪表着陆系统或精密着陆雷( I0 q x' H! a1 A3 s( y3 A: |, ^ 生继续着陆还是复飞决定的高。 , ]* S( V" _ G6 {# k飞机失去内部空气压力。6 Y. X6 D3 e5 C6 d( \ 开, 2 `7 `8 c$ S/ F9 i, ]$ c( g+ O3 u关断或使不工作。8 p+ U* x. T' s7 c0 w- j 机的油泵或外部的吸油装置将燃油从燃油箱排 7 x% ?: z$ [- Y# U1 s9 x4 R- ]出的方法。 4 h* {# K8 f: n$ {ra8 O( s. K! o. a0 ~7 T6 P D8 \, c4 C {/ _/ g# c: f! G) O a& v8 |$ i4 t0 G: p, |2 a F( j% A w ! p/ F1 E0 y" I' f# ?required visual reference to continue the approach has 4 P; l+ G+ Y# l) \! W" mnot been established. 0 ~/ T6 b+ J- y W9 f2 ^. u, X1 |* CD1 H5 q: Q4 j/ X5 Q; D operation of aircraft, means the height at which a F/ Y& c2 ]- C% W# C: [- c& C9 Ddecision must be made, during an ILS or PAR - D1 n9 O, g4 S9 C+ ~ dinstrument approach, to either continue the ap 8 H$ r: F8 d7 P- N" }1 ]% ~to # p( {. Z' v ~9 KDECISION HEIGHT (DH) 2, An altitude used during a ! b5 U& |/ v5 l8 Cprecision ap " l. a) ?5 V- B. ?0 sla 9 y. b3 U' q, N0 S7 L$ W3 {) \D : ~: ~2 H7 U" v8 o. pp 5 e) i! i, J! X# w& l, E* WD / k$ }) Q+ G& O0 V6 B9 `- i) ~DEFUEL, A method for removing fuel f0 d2 S& X* N% J: h: W, E8 R 分贝, % w! t5 A# {/ `3 i6 W7 G以输人与输出功率的比率来推 ( Z# y ^+ |# m9 `' U" d" i& }. t5 p3 ~: x; U$ U0 b( O( D4 _* @0 E# A! b3 A* m1 g) b @+ H+ q' w) }" N! G, Q9 v) [$ e* t0 h9 C; A v) [0 y ~( ]( V% @+ P# f+ c+ b就飞机 0 m- Z, {" O# W, U达引导进近时,必须要作出的是继续进近,还是中断进场 8 x' A/ I1 z; r' e% V, Z复飞决定时的高。" J+ x8 `2 y5 u: i+ i- ] 决断高(DH)2, " O a6 Q+ F$ A2 A+ D, j' x6 n8 `4 O精密进近时产# p0 c. _6 B, q9 p) W' c 失压," C3 }, i* C1 z$ x; U; W) |; g7 o/ h3 e7 g! W. J; |- y4 \排油, & X9 l) ]4 C ^ l" f用飞 . H# x; ~, c( l) R英汉对照民用航空词典B OEING 8 h/ [6 A" q2 H4 t; C2 j8 x# hTECHNICAL DICTIONARY 41 2 _2 S& E" C- }' G8 n* b4 T7 yDEFUELING VALVE, A valve in the fuel system for 3 J' Y3 p$ Q/ t* n0 |efueling the tanks and for transferring fuel between the- [, A; f8 n% \( h6 b0 Q' Q0 P E-ICING, Removing ice after it has formed on aircraft.5 Z0 O. J& n5 R- y Change or difference.- }4 Y" u5 W$ x6 {7 c$ r9 M/ b4 O7 O EPARTURE CONTROL, A function of an approach& o) c" Y6 e# s) |2 W ontrol facility providing air traffic control service for k+ T* p! O8 P! X- `eparting IFR and, under certain conditions, VFR * O; M* X# S6 m4 ]1 ]EMODULATION, The process of retrieving information 6 O- Z( c7 w4 w9 x4 e' wcarrier voltage.' J S% I1 K K3 [& v! X ation.# B5 Q* L' y t* { lic 8 e/ y" Z/ E/ d+ M- |& D5 O8 Screasing hydraulic reservoir air pressure to 7 g" R, r$ X5 ^# l( kmbient pressure.1 I) D1 ^/ e, E' | z. C1 f 箱排油和在燃油箱之间 - h2 |8 e5 `/ S. \送燃油。3 t: P$ O$ i2 Y. | 冰,! u% ~. j+ M( |8 I4 o/ Q 除去已凝结在飞机上的冰。 6 x( P: V2 y0 y7 w( ^( u M删去或取消。1 p4 H7 x# b7 C) c+ ]) d0 x; b- h 量,! F; X! J" }' p 变化或差异。- O9 p( e* ]! O! K- B9 J( ~9 m 场控制, 6 D8 @) `0 C: D: @- v/ L9 ^给用仪表飞行规则离场,和在某种情况下用目视飞行 ; i& V. J) q/ O" S5 v) P则离场的飞机提供空中交通管制服务的进近管制设施$ F. k$ V5 p$ j. Y* s' O, ]+ d& m6 N# h调,' ~5 A+ t9 V; w9 Q- m 电压中获得调制电压的处理过程。 + S, u3 z# Z/ v3 q) j; E5 \8 c环境! Q& X& ` O: H9 i! k' c B 力相同的活门。' o. R- D; I( Y' e9 z" | d' n) Q, |0 v d: p* B tanks.) w0 o" M& r! X4 M. i D6 W$ h# u; A3 }$ F* V: i DELETE, To remove or cancel. - G8 f% z3 W% [7 @DELTA,0 ~1 O3 T! k& a N4 W: X D! q9 B$ A( H8 W# c% {& P c 4 _. }! H' J$ e5 _3 [d7 I: C! H, |# ?% e aircraft.. R8 |3 B2 _( x D# r/ X- v: u1 s, g (modulation) voltage from a modulated 7 }+ e, M- L: }DEMODULATOR, A device or circuit which performs& V& l9 Q1 c" g; z/ a the process of demodul ( W3 ~) h* t: T! h2 S0 w5 ?DEPRESSURIZATION VALVE, A valve in the hydrau , L6 N8 d, I* ~+ {system for de% k: r) O) l( W2 O" L& t. n5 v# a a 2 J, f& X0 h( I: I: N排油活门,% ?) D# P% d9 z2 z* E 燃油系统中的活门。用以为燃油! ~0 N6 B! E! I2 j& B: }- y0 z4 L% X/ F0 T' @$ D( ~5 u% H$ u% L删除,3 U! [( F9 q) b6 t0 w: _& i$ X' i$ \3 {/ b. x( {$ G6 g; p& b+ E8 O" W/ h. x. K2 P0 G$ H2 w4 i+ u/ B. u" e% d7 X8 n/ r的一种功能 * _, C5 y: T Q6 ~- j8 l1 y/ E# c1 `' L9 [6 [! I) Z2 z7 u从载波2 l5 X2 A2 \+ s0 A- B& l 解调器, : L/ B3 ~8 }( T ]* |1 p完成解调过程的装置或电路。 " |8 A% g! T* K$ J2 I减压阀, ) _8 b' i# S; q0 O% X$ I在液压系统中,将液压油箱空气压力减至与周围 - n1 i, X8 b( J/ _* `! }% W6 I" L o7 o& E2 B英汉对照民用航空词典B OEING ' V& k0 ]7 u0 u, QTECHNICAL DICTIONARY 42( {# s# ]* H) B) @ DESCENT, Phase of flight where altitude is decreasing./ t9 S$ ~$ C' ]" } ETAILED FLIGHT PLANNING, The calculation of fuel- U6 `! [6 W% p. G: d nd required for a trip by considering each phase of: C" [. y- h5 r) w' L5 h- o9 ~ ight (climb, cruise, descent, reserves).8 ^1 o1 J- A0 K; w al or+ }( l5 Q! c. u4 x0 f% g ETENT SOLENOID, An electrical solenoid used for & |4 `7 F1 O0 u* s, Q/ q* Vt. % m8 V* S& B- }3 i' xspecified course or : [' W% s; R& w$ U$ \- U% G* j$ frocedure.( c x% }3 O) J$ _0 R& }# _ e. t, c* }. ^3 Z! B+ o飞行计划,* N, P* Y4 w6 a9 b0 Q 将航班中的每个阶段(如爬升,巡航,下降,备降)都: U6 @& }, z/ \1 }7 D) E7 W 人考虑,来计算该航班所需要的燃油量。 - B B+ t- z( P9 {4 v# ^用来感应情况之正常与否的电气装置。 4 y& S9 b+ e, D1 y! V定电磁线圈,& w9 y# U. @. w# s3 m! E( k 出接通的电磁线圈。% u5 F! t) q6 [: G, p2 t' f 差, " @7 ?) v. J8 y. `与指定的航道或程序之差。 6 G E) D# E! b( Z) A0 p/ s! J用气压或液压操作的活门机构中的柔性部件。$ C, C' }8 w1 O7 B! X* F1 ?% x0 Q D% _& P9 e3 K! @0 ^% T+ h a3 ^3 @4 P( G/ U& V' ~) _0 O fl / W+ a* b# X/ V6 h. HDETECTOR, An electrical device for sensing norm - b5 c; h8 V/ f7 W/ kabnormal conditions. : t. e7 L3 x* v, A2 x4 r: s7 [* mD 1 j) y/ ~+ J5 @- _) t n0 t; econtrolling the engagement of the actuator outpu' B8 ^& r. y% M+ m DEVIATION, To change from a 7 `8 m. ~0 x$ D. c1 \. Zp : N8 ]# ~. G3 A( ?DIAPHRAGM, A flexible part for operating a valve$ b. |5 C9 w, x( R1 `7 q mechanism by pressur& ~" T" E- f& o; b. f; C! u 下降, ) {) Y' m" K& Y飞机高度不断降低的飞行阶段。" z) }4 W. s7 R- r- p b% Z 详细' N: M3 [3 A8 a& d/ L4 z @/ f7 u2 s) ~& ~探测器, C) N4 D' G. J) L. g% ^2 [ M$ O- _$ r, l( @9 O/ G3 o 用于控制作动器输/ D# I2 }3 |/ M& x( c- W# @5 j1 g/ w% F" q% {8 f# ?: z隔膜, 2 s$ d6 u8 v, z0 `1 B英汉对照民用航空词典B OEING' ?! W4 v5 s3 x TECHNICAL DICTIONARY 43 W1 Z+ M8 j* P% E5 B2 S. ? DIELECTRIC, A material which does not conduct 2 x; |; i' Z+ `9 `- lelectricity and used between the plates of a capacitor 9 ^* V0 D1 }; d. Z; t h, y(condenser).* W: u! ~& G" k) v/ m* z nother pressure in the same system, measured in0 q u! M- s M2 H ounds per square inch differential (psid). ' f7 S+ u. j# t% \5 cIFFUSER, A part of an engine between the C0 L9 ]+ M9 j2 I* q* [5 C ompressor and combustion chamber for reducing the8 U U3 e# z* W# P& U8 C4 l air pressure.$ |8 a d {# {2 Z2 o, {$ D igh+ n4 |9 x) V9 ^' X X( O pulses. 0 ?* X1 `6 E \& e/ O3 v. @- x! yignal that is a close approximation of the original $ K6 k" h" W; g- i* Wignal. 4 Q0 f8 y% I' c3 \: P; IIHEDRAL, The angle between the wing reference ( U3 M; \% j" V7 M3 clane and water line. $ x0 G& {3 {& S# R4 O的压力,以每平方英寸 7 o8 e/ ^2 @, Y& T% R少磅压差计算(psid)。4 c1 ]2 Y; ^! ^- f% c 散器,4 H( s# {2 g: ~* I2 \8 D7 L# g 发动机内压气机和燃烧室间的一个部件,用来降低空) J* @0 k$ F1 A, J; @# g8 r 增高空气压力。 $ U3 S+ K. H& b; j换, 3 \5 W q1 H: }( W$ M的连续可: [( A! l; c8 B; I5 t% i- Z (模拟)信号的处理过程。3 v8 \( p+ |+ g" q3 W 反角,1 w& `+ A' _% G* I1 p& U3 f8 s 机翼基准面与水线之间的夹角。 8 c/ f+ n; O/ |4 G8 W6 rDIFFERENTIAL PRESSURE, Pressure relative to 5 _/ @, D- t" q' ^. V' S9 j Q5 s1 za0 ?3 m- L9 H" p3 ]: z p; K7 R% I8 q7 V, W2 q D* l, }, q2 U6 u# k: S0 k" f) @+ B c4 T6 ?" M% \# L e airflow speed and increasing the 4 |0 I6 t7 L) hDIGITAL, Digital refers to a signal whose amplitude 6 I' C4 u% M- sremains constant for a finite period of time. Digital- H$ U: n/ T( T% s D! Y2 D( c+ Z signals are commonly represented as a series of h0 d' E+ j2 W9 q, }% W% S7 H; L- [ and low $ e& ]) Z( R" Y0 s: s5 FDIGITAL-TO-ANALOG, The process of converting a1 g7 V. c5 {$ p! ^. C5 U3 \7 w digital signal (binary) to a continuously variable (analog) . h2 X- o( m; {' X( H: P4 }s & s' x% {: R; v2 \4 L9 h# S; C) {/ zs6 Y. h" ]9 d' L g3 q+ C D' |; p/ v K( _% j O" M# ^0 h p, ?" [$ H# c/ O 电介质, 5 `$ x; [2 P" r0 a6 T7 n+ P# m一种用于电容器板之间的不导电的材料。+ [. Y1 W# V1 ^' S4 l 压差, * d# T: a6 h7 U3 f" [& O) y相对于同一系统内另一个压力3 k1 ?% I ?! @. O' C7 N3 Y3 a6 Y; U C: V( k, S3 B; Z8 A% E3 ?: b# T1 n/ p/ B气流速并- @/ M2 v( U. l! {6 d8 J/ Z 数字式, 5 q8 S- v" Y# P( i! m5 a d3 x V/ i6 N指一种信号。该信号在一定的时间内,振幅保持不变。3 c( g+ @# C# C9 X: Z$ e6 E 通常由一系列的高低脉冲表示。& T# x0 i) V; P; F2 @2 @ 数一模转' e! ^ p j) Y 将数字信号(二进制)转换成与原信号相似 4 F+ k! K- n u9 [/ W. ?8 E$ c3 ]8 c( U5 \8 o. g8 @( ^+ S0 `2 N Y s5 s 英汉对照民用航空词典B OEING k5 ?1 d3 c% a: L/ L' {4 ?TECHNICAL DICTIONARY 44 ; o2 ~% P( }- _DILUTER DEMAND REGULATOR, A component in the # C. h3 p, O' {- ]crew oxygen system which mixes air and oxygen and0 w: L' v. D3 q$ Y6 P% z upplies constant oxygen pressure even if there are : c7 L2 a2 S7 D$ A- `hanges in ambient cockpit pressure. 2 i1 T+ y5 q3 O, k4 ^IM, A word value of light. For light control devices - dim + E2 ]: S3 Q& u' Kthe opposite of bright. : G C8 B) x3 B4 b# x/ bIODE, A device which allows electronic current to flow* ^# P% f' @. H4 P, l1 G0 Q only one direction $ C: O& D0 ]2 r9 }" Puid in a reservoir. 8 y" n* _& K: v4 Y' BDIRECT, Straight line flight between two navigational 6 K" G4 W/ T) T1 ~aids, fixes, points or any combination thereof. When8 m& U+ U0 Q7 Y6 O* L$ Z used by pilots in describing off-airway routes, points 6 S: k9 S8 N! e {defining direct route segments become compulsory# i- i4 d# [4 @% `# k2 W, b3 t0 k reporting points unless the aircraft is under radar * f8 h1 @; O- Econtrol. 9 R# @1 i- l. C$ K5 d" C% N4 g! v8 n9 }+ y节器, 0 R; K5 P1 N9 w8 K( G6 E- B将空气和氧气混合,) n9 n8 l$ J3 m, J 使驾驶舱环境压力改变,它也能提供恒定的氧气压力。 # l( U& f, N+ \/ l0 _+ L. Z5 |' a8 s) F) @( T, R" ]1 J一个形容光线亮度的词。对于灯光控制装置,暗的反 ) K: v. Q. }$ R; N0 [2 J( p* K词是亮。 s( L [1 O( K极管,, x; t6 B; c) W* f8 X: ~ 只允许电流向一个方向流动的电子装置。 ) {+ m% N* B0 x6 W9 E0 P器内液体的量。2 x8 a4 z" }% }* e* r1 N2 @7 @ 直飞, ! \# d9 C. `, Q; V% U4 Q; Y V+ N两个导航台,定位点,导航点,或任何的组合之间的直 1 X% m# I3 Q, c* G- w( z3 K线飞行。在被飞行员用于描述偏置航路时,除了在雷达控 0 ^ y' Y: ~) w: o) q9 w: B制的情况下,确定直线航段的导航点成为必报点。 ; o& g6 J# u) |- G M( `s 7 ~; c t6 X: p0 |9 b" t6 T$ Q6 \5 Tc4 ?, U* ]8 n0 f: ^ D . O# k6 `' g* m% C* E9 |) Ris7 V# E) N. z$ f% o/ Y) F+ H# i D8 z8 z* A! _% |8 `( C9 k- f# D in % W8 Y6 b/ u2 u8 F( rDIPSTICK, A calibrated rod or stick for measuring a8 C9 `, e. @- i4 H6 \! a quantity of fl% a' P) O, B( ^ [ 稀释氧调' W( j0 C) X0 m 驾驶舱氧气系统中的一个部件,它 " r9 I! B3 W4 x' l% Z7 R1 ], J& q6 b, C0 x+ W1 W+ V, j$ |# V! w+ P! m( Y# ]% K- z4 L. F9 [4 |3 A) U2 R& a6 D3 y 量尺,% v) {6 L; m Z1 ?+ j" O 校准过的棒或尺,用于测定蓄液7 B( m/ X& _: } 英汉对照民用航空词典B OEING * N. i! R' a8 R0 Z2 LTECHNICAL DICTIONARY 45

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