航空论坛_航空翻译_民航英语翻译_飞行翻译

 找回密码
 注册
搜索
查看: 6934|回复: 22
打印 上一主题 下一主题

英汉对照民用航空词典 [复制链接]

Rank: 9Rank: 9Rank: 9

跳转到指定楼层
1#
发表于 2008-12-24 21:35:01 |只看该作者 |倒序浏览
英汉对照 9 U, [# ^! Y4 F6 [民用航空词典 ; \* m* t9 Y" x波音商用飞机集团 # }4 j! H s: lBOEING COMMERCIAL AIRPLANE GROUP0 v% c6 q) W$ z3 |0 ` 英汉对照民用航空词典B OEING5 R$ f5 ~7 I. I# R) F TECHNICAL DICTIONARY 1! T f5 D X% ?6 U3 S A2 K8 y# N3 R! R/ h! L$ W, s' J ABEAM (ABM), Beside: An aircraft is abeam a station ; m: F. N' L( B! Wwhen that station is 90° to the right or left of the track of " \, Y' A6 C* X8 l- Mthe aircraft.2 N" j7 H* r. \/ ?; |5 v7 N ABSOLUTE ALTITUDE, The actual distance the aircraft! S6 R" U9 S$ N# L- s2 p9 M# Y5 f is above the ground. * p7 X: z2 A# J& nABSOLUTE PRESSURE, Pressure of a liquid or gas 1 @9 ~5 q P* ^" I2 \measured relative to a vacuum.7 o' X. G0 A( _# k) z- V X ACARS, SEE - AIRCRAFT (OR ARINC) REPORTING " U' t! P- C+ t* C' s n; JADDRESSING AND COMMUNICATION SYSTEM / S" r1 c3 a/ E2 u D, OACCELERATION, The rate of change in velocity with 2 i% z/ f* l+ }2 Prespect to time. ' U- ]* @6 I6 E" w* lACCESSORY GEARBOX, A part of the engine, 4 }/ s9 M2 {2 L ?mechanically driven by a compressor or an angle 4 z/ _5 L' j9 N+ Mgearbox, for driving components necessary for engine 9 g& {/ b4 m- Y% [1 |正切, 0 r' V* U6 y! A/ c0 D7 X! e% |and airplane operations.; O. t/ p }9 f 当电台在飞机左侧或右侧方与航迹成90 度时,飞机正 ' [0 P4 E2 j- I1 a* c- Q, M1 h切电台。 , U3 o9 s" j6 L, a9 t! y绝对高度,8 a; q# `" T" S) i$ ~2 Z 飞机离地面的实际距离。 9 M0 v) |7 Y, W绝对压力, . p$ E% W) X1 A O/ D0 d8 J- ?$ l相对于真空(无压力)测得的液体或气体的压力。4 r! u+ P$ Z* t 飞机通信寻址和报告系统, : e# C( \& {4 ?# w! V! g/ f% r见Aircraft(or ARINC)Reporting Addressing and 1 I6 g* e: b" r8 b8 RCommunication System. 0 w/ U4 f7 O' j2 J0 T. Z' W+ K! J加速度,/ y9 q* Z1 S; T4 R 随时间变化的速度改变率。* N* Q3 e4 j- C: Y! C- B 附件齿轮箱, ?$ |/ j7 z# o0 a* v) A9 s发动机的一部份,由压气机或伞齿轮箱带动,用来驱动 ! h) ^: ~; p& o. _5 G" m' G; f一些使发动机和飞机工作的部件/ D2 H! e5 U5 A0 {' h 英汉对照民用航空词典B OEING0 ~. k0 }2 Q- B$ Q2 P: H TECHNICAL DICTIONARY 2 2 z$ `3 `) K! N; h8 O. L/ G0 k5 h8 hACCUMULATOR (NO. 1), A container with hydraulic ' a- E! @ A6 u) @, f; fts when normal hydraulic supply is not9 |5 G* @+ v! k8 S0 B7 ]# K vailable." N- A! i: \, N* k& h. P; U7 D) L; d CCUMULATOR (NO. 2), In a computer, a special , @% B4 W; c }2 J$ vtorage register associated with the arithmetic logic unit,& R* z# r8 _, Q ~5 Y6 {! w/ @ olding the results of a computation or data 6 h5 ]+ f. c* e# W, }$ m3 n3 f rACTUATOR, A mechanical device operated electrically, 5 @9 n( g" Y4 y8 D2 g2 a ]hydraulically, pneumatically or mechanically for" l: D. H+ M1 }; g/ I' H0 @- w: b transmitting motion between components. 5 z) [1 }! y* C3 y0 t" _ADC, SEE - AIR DATA COMPUTER + ` H, g' Q1 }+ OADF, SEE - AUTOMATIC DIRECTION FINDER - b L- q% Q1 N2 v4 L' ZADI, Attitude Direction Indicator, An electronic display of! u% ^) a: Z& k airplane attitude information in pitch and roll.% k0 F! \ g! J. ] 蓄压器(NO.1), ( y8 l) Y; v6 D含有靠干燥空气或氮气增压的液压油的容器。当没有正1 a9 I% W+ z$ Z% K 常的液压源可用时,该容器可用以驱动部件。 * u+ P9 F2 |* c- T3 i J存储器(NO.2), ( B7 f2 M5 y0 }% u计算机中,一种与算术逻辑组件有关系的特别存储寄存3 ^) j0 D1 O9 u1 b6 }0 p% K 器,用来存放运算结果或数据传输。 $ k4 W0 }1 D, U$ c- a" J+ l2 ~飞机状态监控系统,* `) l* [7 c/ i4 x# L$ _3 T$ K# [# @ 见Aircraft Condition Monitoring System5 T% p _6 \; W- l6 ?- i0 j X fluid pressurized by dry air or nitrogen for operation of3 _4 T% C+ \+ m* ~( p0 i; | componen: M! [& ~. |4 ?* @7 X! } a: x m' `6 U. c0 G1 [' x+ H' J A5 j8 a" X; g9 X V) D0 B2 K s / B% c! k; ?1 m) J/ \! j; ?used for h9 a2 ?- z2 M; z6 c d transfer.) E2 n* W: q! @" r# o( d; {& R ACMS, SEE - AIRCRAFT CONDITION MONITORING 0 `+ e( v; {4 k u! {9 X0 qSYSTEM .2 {. z! [/ A# C: s: `# e/ K0 j& P 作动筒, - z5 U; s7 k) D! \/ O8 r6 L由电,液压,气源或机械驱动的机械装置,用于传送部/ L/ T/ R4 Z3 P* ^ 件之间的运动。& s7 k: d# E6 o$ {0 m 大气数据计算机,1 q& Z2 _* O9 x1 N1 W 见Air Data Computer.: N. E- |% h5 b; ~, _6 I: g% _" ^ 自动定向仪, 6 `! z6 |8 V3 ~/ G+ b+ s6 r见Automatic Direction Finder. ( P L& M& B' p3 V姿态指引仪,; O4 u& R) s/ O% y9 [3 ] 用来显示飞机的俯仰姿态和坡度的电子显示。' y7 N% l: k* n: s s 英汉对照民用航空词典B OEING: L3 w2 {' m; b( [ TECHNICAL DICTIONARY 32 l, c& I9 n) E j0 B+ v; @ AERONAUTICAL RADIO INCORPORATED, ARINC is: f* V+ K0 P5 b% O0 K u6 T" R) ^7 W ,; e* n2 {( E3 v v) ~0 B/ u% ^/ k nufacturers, and foreign flag airlines. ARINC7 |, d8 x7 ?' \$ Z# F4 I* P! q evelops and publishes standards for electronic/ \! O1 `* U8 s( |( u% G quipment and systems.. b5 _, O q7 M8 k GILITY TUNING, The capability of the DME to - ~0 }4 |7 p* J) i: qlternately tune between two different DME stations in 1 K$ A/ N" ~# h6 g/ v9 u6 d' K: Order to get two distance readings from one! h) R" Y" }. e. E9 I7 y terrogator.. U# u6 t8 x, X3 k: h! U ge 0 |9 [$ e9 L F* r% R! h& bILERON FORCE LIMITER, An electro-mechanical; Y1 r# w' V f3 J- R3 _- j. U IR CLEANER, A component in the pneumatic system r; `) T& L; \- \upply to the air9 a$ L7 S$ D% a; ? x. d/ q onditioning system. " G# ^; k2 l% r& _- t J订并出版 ( ?' l- d2 u4 v# [$ Q子设备和系统的规范。$ H9 _6 |' ]# h1 e0 n8 @$ i' Q 快速调谐, K$ V' [; E% `; q' T$ E" V 机载DME通过交替调谐两部地面DME电台以测得来自" t/ Q. M0 t" w. Y- `. ^( r, x8 t 同一台询问机的两个距离数据的能力。 2 d- p5 k8 r. j. U' S5 x4 y翼操纵力限制器,. k$ ?5 _0 I& L( m 装置。在自动驾驶工作期间,用来限制驾驶盘% |0 P0 | l# x+ ] 气清洁器,; Q( B1 h4 b8 b: L2 y4 ?' o" O 部件。用于去除供空调系统使用的发9 m2 T# j# n; I. t6 q4 [ a corporation whose principal stockholders are United6 R$ W9 b* v& A$ q0 Z States scheduled airlines, air transport companies - e2 S0 s. ?3 maircraft ma: f: f3 }, c' O" Q' f& l+ F d8 E# Z$ e, k3 ^" H e % W( `# C, a; }) o8 xA1 k8 [0 _, z2 d! T1 t9 e1 ^ a2 h' b. q \5 f( C o+ o( ~8 f3 q7 d& Y in 2 n6 u) `( g0 r% v/ {$ AAILERON, A hinged moveable part on the trailing ed # D, q" {3 d& r4 F# L& ]of each wing for airplane roll (wing up and wing down) 5 }! W! X. i3 f9 ^control.1 m+ a- ]$ S. E- { A ; }& |" l$ P0 F. g7 z' }device for limiting the control wheel movement by the % G- i7 e2 y6 nautopilot during autopilot operation.+ [/ d8 ]( B7 T A0 z3 F) f a! Q6 ]( v7 p for removing dirt from the engine air s0 @9 J$ |8 l+ r! n' f. ~* A c4 d4 s' `) C7 g+ W2 h8 x$ f" R( S 航空无线电公司, 8 S8 C# L/ P0 ]! ~% Q( w) [" V主要股东为美国定期的航空公司、航空运输公司、飞机 % r! {$ J3 ]6 [* I' Z4 t( S6 b制造厂和外国领队航空公司的组织。其目的是制8 w' G* B# E3 T5 N5 j, ^, t! F; `: {9 W4 k副翼,, @; n5 l. I& t6 g 铰连在每个机翼后缘的可动部件,用于控制飞机的滚转 , h% l X: v9 v) M1 m0 z' o(机翼向上和向下)。 1 G2 U; s; @: {) F3 E' E6 K7 U- `1 V7 A( Y& d 一种机电 6 w! A q+ a( l9 t的动作量。 $ u$ @7 l9 `8 V5 ]3 Q9 h9 ?/ V9 P: @! S, H气源系统里的一个 ( v( ~7 Z! Y, {7 g7 k+ x( Z动机引气中的灰尘。0 g& V2 c& A1 [& G 英汉对照民用航空词典B OEING+ _. O3 }& u% [. j' s( ^; L TECHNICAL DICTIONARY 4 + G0 |( M* Y+ y" _% wAIRPORT ELEVATION/FIELD ELEVATION, The $ ~% n- L4 c5 t* Q8 e: Ghighest point of an airport's usable runways measured & w3 Q5 u4 ^! Hin feet from mean sea level. In a few countries, the: w4 s* W( C5 ]- K; {/ Q airport elevation is determined at the airport reference P4 Z, o2 A, }5 Vpoint. + y3 P& _" i. ~' R: AAIR ROUTE TRAFFIC CONTROL CENTER (ARTCC), $ O: I+ I" q: o2 ^% t: T2 }/ tervice i) M% i( O/ S: M5 ~ase of 5 B8 |2 ]$ g! P7 s1 cus flow of air traffic. . `0 k# E. P' c# \: wIR CYCLE MACHINE, A compressor and turbine on a; k5 A2 b t! L$ Z+ ]6 I ommon shaft for cooling the air in an air conditioning . j0 i, ]! A8 b0 mystem. The air is cooled by expansion from high to low 7 n* \, }3 c! q0 L% _! Tressure across the turbine. The compressor is driven" s& s. E0 L& {" Z y the turbine. 6 t8 p `7 l% P中航路交通管制中心(ARTCC), $ Q6 A8 S. `5 ~ S& C+ a$ ?域范围内使用仪表飞行规则飞行的飞机提 . N9 G/ c9 R* T管制(ATC),) e. M6 x8 [) N' f0 n; I% O! F 涡轮冷却器, ! B& q3 j9 w b$ @- R是装在同一的压气机和涡轮,用于冷却空调系 z" c3 W' b, p9 \, H4 Y 统中的空气。气经压气机压缩后,由热交换器移去热量,, X7 ]6 p* N3 b6 P A) y, S 然后经过涡轮令涡轮带动压气机。通过涡轮之空气,温& a% W: |2 I2 H4 t 度下降。9 l; M" b1 n2 N" R% N; g0 d+ I A facility established to provide air traffic control s ! P8 I8 A+ c4 y; s7 ^8 J7 h/ c) yto aircraft operating on IFR flight plans within controlled& ^0 g, a: o% \' c% I airspace and principally during the enroute ph / L, X( U5 Y$ d( T! n5 `" Uflight.$ }* _2 u% ?2 @" ^ AIR TRAFFIC CONTROL (ATC), A service operated by ; o+ v* S! ?8 A' u$ B. N0 Happropriate authority to promote the safe, orderly and& |9 X# L9 u2 | expeditio , h4 ]' Y X% M5 ]A / O. G8 q" _3 y5 y5 Hc 4 j+ c. `+ D5 P1 d+ ws 9 f. K5 _4 \2 ip( V! K4 [ }# O- V3 f7 B b ) L; C4 a+ J4 B% d9 ^$ q+ j. o机场标高,, w. }: F" v! W4 E 指海平面与机场可用跑道最高点之间的距离,单位是英# Q; t8 A* j, I+ X" G% \ 尺。有几个国家的机场标高是由机场基准点而决定的。 ! }6 X% V, R" c% r3 H1 c1 g$ R6 {* Z5 f+ Q: _) L. K给在控制空0 Q2 Z3 }$ i0 K6 l$ G 供空中交通管制服务的站台。' \* B5 o( d: E0 V5 h, M' Q- I 空中交通. a6 D" i8 x7 s" e 由有关当局管理,旨在促进安全,秩序,和效率的空中 ( D4 F3 u. c7 H: J# y- k交通服务。/ h7 r! I6 a( E7 h( U0 H9 H 根转轴上 ) \ L, q0 H7 h8 }: }, |6 d* e# l" O2 K% i; C8 z; Z# p7 T1 I+ M英汉对照民用航空词典B OEING5 ]! D3 @# Y% ?+ I% y* p+ p, J! x TECHNICAL DICTIONARY 5

Rank: 9Rank: 9Rank: 9

2#
发表于 2008-12-24 21:36:52 |只看该作者
AIR DATA COMPUTER, A computer which produc ( o. f1 L7 j9 `& _: j# ~data information, such as altitude and airspeed, based/ `; P0 g3 D% Y7 Y on pressure and temperature measurements.) M9 ~2 p2 b& n! z es air 3 j4 n1 I6 d8 K% ]; _0 U, ~3 IIR TRAFFIC CONTROL, A system comprised of5 d F" j- s- Q' [3 A7 s round and airborne components used to identify, track 8 ^) _9 D4 U- D) V. y' [4 ~7 QOUND SENSOR, An electrical device operated0 J$ a6 F) R$ \% ?# j# W7 b* A y the landing gear, which transmits on ground/in air 3 [5 }0 ?# {+ |0 Z% W: Q* Kformation for system operation in flight or on the( H- s% ]+ r! T# S round.2 S; e. T/ Z% e9 P. a) a5 v9 ^, q IRBORNE VIBRATION MONITOR, The AVM takes 3 @4 v1 ` N0 h) F0 q; ~ de signal from the engine mounted accelerometer and * r6 K% F9 O! I Falculates the vibration on that engine. ; A9 {1 F, W9 L/ Rcorridor equipped with radio navigation & ?0 n! J& A( ]aids. {& B) V# k( p0 v0 r AIRCRAFT (or ARINC) COMMUNICATIONS+ t+ E1 q c$ O" ~& H. W ADDRESSING AND REPORTING SYSTEM, An' L, N7 P( o9 L" T1 Q7 o! ]3 P4 c; [4 d addressable digital data link system which permits the8 _3 y. p" M, H0 ~1 H exchange of data and messages between an aircraft# @7 H8 Y6 L1 y4 }4 |: \# l* A and a ground-based operations center over a radio- A- K9 [6 C/ c2 ^/ z0 }( v6 s network.% Y' K# V; d; d AIRCRAFT CONDITION MONITORING SYSTEM, A # Y' b* u. V# G+ u: Nsystem of sensors and recorders to monitor various 0 j' j X& l6 \& Nairplane systems' performance and status.% l) h, i- g& j 机, - Y3 z- z! I; ]$ \中交通管制, * j. I. I! Y8 Z( b X一个由地面设备和机载设备组成的系统。用来对飞机进 + ]+ o! ]0 u$ Y地传感器, 3 S" U- {: D1 L0 w# U# z2 `- h一个由起落架操作的电气装置。用于给空中或地面的飞 5 ^9 m) E, f- x1 a! Q$ z* J _系统运作传输地面/空中信息。(有些系统只能在地面 2 c ~& u3 ?" _( f) s8 m9 \用). Q6 G4 X! A1 p& u6 Y 载振动监测器(AVM), ~- ?2 y. n9 z: u& zAVM从装在发动机上的加速器取得信号后计算出该发; u- K! A- x% F. K 机上的振动。 * X; f( g4 {- N) M9 @# H- G式建立的控制区域,内有无线电导航设备。 - o8 I- C4 |, D5 H% W- q# s飞机通讯寻址和报告系统,% i0 B8 `- N$ _8 _& `; a 有种可寻址的数据通讯系统。利用该系统可使飞机与地 ; i4 h* q( o" c) f. O& c面操作中心通过无线电网络进行数据和信息的交换。4 c8 J) C" k _& ?: F 飞机状态监控系统, " O; r+ G: _" p9 h一个利用传感器和记录仪对各种飞机系统的性能以及 & m. N/ Y- O" A" m7 r2 T状态进行监控的系统。3 j' G5 l2 q5 D4 A: Z- Z; M A 5 g/ P2 G6 a; \g 1 ^- F- g+ M2 u- T7 l! t$ u% Tand locate aircraft.! m: _+ ^7 A0 C$ N, ^0 r- {, j AIR/GR 3 T/ u2 c8 W/ M$ ]" P1 b: ob ' w! j e: a; M8 U9 ^* Ein9 ~. W# O* S1 l2 Q$ D g! l$ H# D( b" x" } A 7 v4 ~, ]1 S( i; e$ ]th 7 P' I, O1 f( \% {* [c 2 C7 i( [/ I6 \AIR WAY, A control area or portion thereof established & J0 ^" d: M) u& s$ B; pin the form of a , _, }3 [* I' K- T大气数据计算 - t; h3 g% M7 N( s: O9 p根据量取压力和温度而产生大气数据资料(高度、空速$ o3 S0 a4 @, \0 ]. Z' E/ T 等)的计算机。4 @2 H2 ^6 |2 f: O5 b% c7 E" w: c( h0 T. V行识别,跟踪和定位。8 M- u/ ?3 H( T9 }; ~8 w6 X9 p, o4 {- X2 _- f7 }- ?$ n0 J/ ? 使 0 _7 h0 _ D/ w) e* m7 Y5 Y# |- C( ~! H: n j3 E( x! \5 S0 P. @4 w# k+ e航线, # C8 t9 g0 w' r4 w) B6 ?以走廊形; v* |( _- G8 v% I9 X; s+ A) C 英汉对照民用航空词典B OEING0 e! `' }% q4 c" a. z0 h TECHNICAL DICTIONARY 6; z2 K( e- A* M/ k/ V AIRFOIL, A surface designed to obtain a useful reaction, * l3 G1 v6 R O; s: s+ g$ ~+ Esuch as lift, from the air through which it moves. Wings, / Y8 z" D0 G) u, ^4 E8 l9 X) {+ Zstabilizers and control surfaces are airfoils. : x0 S3 g4 _. `, y( i2 G/ m) BAIRSPEED (IDS, TDS), The speed of the airplane) X4 u0 Z& Y$ t rough the air. 4 B" O3 n) a ^. k6 f% e% rD INDEX, An adjustable pointer on the; \' [9 F9 k$ z$ O+ ?- y irspeed indicator.% M, Q! S) h2 |3 q and legal ability6 }- v6 S) F$ k& g- c6 n fly.7 l7 C& w& t. E& e* M8 q+ \ m, for example, the procedure for finding the: q4 h2 \9 \) s; s# [; @ quare root of a number., q7 p% t& l f/ F* w y - ]0 [6 G! ^* r }) k2 Q1 C% t9 ]re, wind, 5 J9 X* p! M, O1 |! Oand aircraft flap setting.5 _- k& I% Q3 M% l1 H/ ]0 \# b 是翼面。. e) n0 S; D, o% V4 b 速,* \% ^, b5 v; s8 I3 D 飞机在空气中运动的速度。 b/ C/ t8 h& _1 F" k0 ? h% h; r. n8 ]% ` U( \( U 在空速表上可以调整的指针。 7 a# R4 ]4 j# N) X) C机械飞行能力、和合法性的飞机状态。' S5 z3 H+ r1 h w. m8 p 一步一步的解题方法。例如,计算一个数的平方根的步 0 ?* o4 U9 x" V2 O- y; p- \% u2 m' A4 U# w3 g5 B" H- }& K: H! ^5 a- j资料的法定文件。3 M- q$ S: V* Z7 m' L0 b' R- g4 I 翼位置成函数关系。' m6 s) S+ |0 }% [ th " Q3 \/ \3 v* @9 H6 U$ x# FAIRSPEE" ^$ f8 v! y' Y0 l, [3 b1 u4 [8 M I a; T3 j, o# _+ ~6 {! J AIRWORTHINESS, The condition of the aircraft with; v6 }) [/ X9 @" H- T* p respect to its aerodynamic, mechanical, " F% w$ S1 @& O6 H& y; ]0 Oto, F2 {2 O5 i! ?+ r( ~5 p9 `2 \ ALGORITHM, A step-by-step procedure for solving a 1 y7 J8 f" P+ L6 Xproble% d9 {8 o( B7 k) b8 C# \7 } s & T8 q* a i4 f9 a' K$ @AIRPLANE FLIGHT MANUAL (AFM), The legal1 P4 t$ A2 Q% Z4 l8 ] document containing performance and operating limits,. h9 t( p" j e operating procedures, and takeoff and landing+ j; x6 v$ F# d, ]% U6 | performance. $ q% \, g3 l9 j1 ]AIRPORT ANALYSIS, A comprehensive set of takeoff! b# A1 X: j* M1 Q weight limitations for a given airport runway, generall : s! n. }8 |. B- ]4 `presented as a function of airport temperatu0 X3 G* v1 {1 d, c2 V 翼面,8 y4 L& I* F" g$ t 用以从气流中获得反作用力(如升力)的表面。机翼, 8 |" [% F- O$ E1 l4 B i* j! m安定面和操纵面都# d. n2 D0 P3 _$ M5 q! w' _# [; T a! C: W- y0 x 空速指标/ o( ^5 w( I+ C% }: U) @ 适航性,% }& X% k* R: f9 B. q8 S$ F 有关气动能力、 8 S3 D& k8 h* u! X& P! q演算法,) F) L' Q9 ~: Y3 p6 F% o$ Q# `+ f4 a& C飞机飞行手册(AFM)," k; {1 s | \5 @/ T; J8 [9 N 包合性能极限,操作极限,操作程序,起飞和着陆性4 \9 s% j+ v: O; Z/ S! k1 \2 S: Q$ e4 R5 C, u 机场分析,/ X, [# m) R' w3 b" B( D! p$ J, b 一套针对给定的机场跑道的详细重量限制资料。通常与- ^/ ~% B4 ~) ? 机场温度、风、和飞机襟! s7 I0 `, l" {$ c3 |5 @+ c 英汉对照民用航空词典B OEING. h, T [$ _: h9 w3 c! Y TECHNICAL DICTIONARY 7, d9 E. P" r8 V s5 _8 O$ d9 d AIRSPEED BUGS, Adjustable pointers on the airspeed; o# A5 g4 o; D indicator.4 d% X! ^$ V1 d H, m# O ALLOY, A mixture of a basic metal and small amounts, Q# o& X1 z2 C" _9 v f other metals to change the properties of the basic# E8 w" a; y5 L etal. 2 J/ F$ \- M& ?7 vMinimum airplane speed.& \+ t0 a& N( a! r% R e of % `/ Y7 Z! }2 {itting airplane angle relative to# W0 W# W% o/ k irstream for the stall warning system.$ o! e; @1 x/ T another.% S* ~+ D5 X+ S LTERNATE , An additional airport selected during/ S3 Z6 ~0 b' ]0 C0 \: b/ j d/ U( \) W# n 合金,6 q- h( C3 D5 C8 r. _2 v8 y 在金属中加人少量其他金属,而改变其性质的一种金属 & j5 I- b/ p2 V+ U2 k4 E合物。+ h4 K& G! |7 v2 u3 T% ]5 c0 y3 Z 飞机的最小速度。 ) Z% e1 }& n2 }! h速警告系统传输飞机对* m3 F& f" [! f( y( ^ 流的相对角度。, K. r% ?5 a& J( ]' q2 C 由一个状况改换到另一个。6 k$ y5 Y9 t- S 降场, ; e/ b! W% u% B% F8 q6 v划时,除了目标机场之外,所选的另一个机 9 Y2 n0 Q( C% N- {o . \) a; a" M( s& w) n9 Wm 7 Y9 q+ C0 d0 E8 b1 J8 ~' ^ALPHA SPEED," y) }) {: d& { ALPHA VANE, A small moveable airfoil on the sid 0 @' z; P0 _0 I9 u7 }% Kthe fuselage transm: h+ o! i4 v! h3 Y) ?, a" B4 f. t$ r a8 p* t9 M6 I! l* s8 I) a0 t R8 v/ \. I ALTERNATE, To change from one condition to) T' U0 }6 I4 b9 w, T' n& b A ! U* o A( W. D( A* Mflight planning, usually near the destination airport, to be0 ^1 p; k# S" x- U used when it is desirable to divert from the original) V1 j! [* b1 O) @ destination airport.$ O( s/ r8 X( }. V& {1 [& M7 w 空速游标 6 z" t' y$ r) ?8 R空速表上的可调指标。 ) h, c" |: \- ]7 m1 S* f# [; r) Q0 Z0 ?7 j8 m- S% _' p* b/ t迎角速度,$ x0 `. I* @' p: ?6 R2 u9 I% }2 N 迎角叶片,* u1 S# H, T+ f 位于机身侧的可动小翼面。为失4 H- C ]7 \" t+ ]3 \( N4 p! A# T; z) U$ n! y 交替, # b& }$ C w ]2 Z1 t, I, }1 ]& k# N: y* d 制订飞行计 # C4 \8 H/ }; @# [3 E场。通常在目标机场附近,以备不去目标机场时,改降之6 k) X2 b7 n5 W' @- D) Y 用。, {% {- _1 b9 u, \6 m2 y2 V; g 英汉对照民用航空词典B OEING : I2 ?1 [; O+ n& LTECHNICAL DICTIONARY 8 * I/ J5 a6 C& `8 x) mALTERNATE AERODROME, An aerodrome to which / |7 t2 \; }* F6 uan aircraft may proceed when it becomes either : I$ g# Y+ e1 Spossible or inadvisable to proceed to or land at the: \# \/ c2 z" o5 t) C3 i erodrome of intended landing.; V; V. u% j f TER SETTING, The adjustment of the altimeter 8 e& r0 j4 R# xaccount for local variations in atmospheric pressure.+ [3 C* n% O, Y4 T0 g: n LTITUDE ACQUIRE, A digital flight control system + a* |- Y% W. ?% x7 Sode to transition from climb (or descend) to level flight. 1 f( H1 v# u7 f) U+ y1 J6 o& ]8 ]LTITUDE ALERT, A flight deck alert occuring when the' D5 T8 h2 a/ [6 G: o3 h& k3 W irplane approaches or departs a selected altitude. . T2 C) a% y; G8 a; S* oLTITUDE CAPABILITY, The maximum altitude at8 W: J, X, @* U hich the airplane can be flown at for a given thrust, 3 w# d6 Z7 ], G. w8 e5 N9 A( Dpeed and atmosphere condition.+ q3 u; K8 B9 d z8 p u; N) n LTITUDE HOLD (ALT HOLD), A mode of the autopilot 6 A. }* v; x+ O, v/ B9 E8 Yr flight director to maintain a selected altitude.% Q3 w1 V5 d4 ? irplane's altitude during VNAV operation. ' i$ H+ |! c/ o, i }* p机场着陆时,可作着陆使用的: X$ c' | k; ^; X+ v, ?" g 场。& B2 ~1 L9 B! g. H( S5 I" Y3 R; F9 O5 W根据当地大气压力变化而对高度表所做的调整。 5 [ o! R( r l一种数字式飞行操纵系统,从爬升(或下降)改平的模 * k, y. ^& U0 F% _) a, x2 G( e$ ^ q5 `4 ~度警告, ! A& l: e9 ?+ y' d& |9 B& l# ^当飞机接近或偏离选定高度时,所出现的驾驶舱警告。 / J/ H" W# K* C8 Y8 ^( d高度能力, ' |7 c0 i+ F1 I0 c# R/ n3 t在给定的推力,速度和大气状况下,飞机能飞达的最大8 \1 E0 S$ O$ I$ |( W4 H( W 高度。 ) K$ V8 h- _1 t' j2 `7 B) y$ k高度保持(ALT HOLD), " L1 {& _- Q! X0 f6 p9 `自动驾驶仪或飞行指引仪保持在选定高度的一种方式。9 T* ]% e! O6 \8 ]" H ~. v X7 i& _- z6 |( W/ d3 T 员对飞行高度的控制。( ]3 P" Q1 l& Q7 D- D* a im % w! Z* _6 S- t& \a 5 H7 p. Y5 v# U0 W9 p! JALTIME* k) n1 n* j& G( k0 T. c to 1 d2 S! g' M8 G2 fA& \; k( t6 U4 t1 D2 C3 C1 \ m 2 Q. H& |( {3 uA8 r4 T4 a$ ]& l# s7 [1 m0 Y: F; ~ a " `" `( G3 I' S# f3 O9 s2 _% S- K: K5 uA+ C, t7 ?* g- U# ]0 Q w1 {2 Y& ^$ [4 x( V. u* Y s 0 X9 ~' K! K' K3 xA; s5 S8 Q A+ r' P/ T3 b9 h E4 W o3 n5 q. E( j! A ALTITUDE INTERVENTION, Pilot control of the * H1 Y$ o- \6 E8 T& c; }! R9 |a . z9 T( C) g+ A8 ~8 }AMBIENT, The surrounding atmosphere.% o, l: Z6 Z: Q4 t 备用机场, # B4 ?# `* @$ ^% z3 a# ~当不可能或不适宜在预选! r9 ~5 g1 y2 U" {' V3 N+ c9 |+ ?3 ` 高度表设定 $ Q* L$ `1 b; P/ b. g0 e高度截获,; z4 n+ h4 h5 Z& D- K% [3 m }/ n: x l$ \) L6 V | K4 @高度干预 . z) c1 p3 V. P/ h- J7 x在垂直导航工作过程中,飞行: M" U% V0 Q* E a% S 周围环境(地面气层),$ F0 P" Q( B+ B4 r 物体周围的环境(特别指大气)。+ o0 j6 K1 A& P8 i4 w 英汉对照民用航空词典B OEING D# M+ b/ L9 u! p2 [+ t: `; \ TECHNICAL DICTIONARY 9* a. N/ }! P X AMBIENT PRESSURE, Pressure of air surrounding an. r( T" O. T( x% M! O object, measured in pounds per square inch (psi) .0 P& b7 I" A& L1 q% W9 U MBIENT TEMPERATURE, Temperature of air) b: s0 D$ w* h+ m- v mpere. ! W G5 c/ X4 B2 ^% {urrent waveform.3 Y/ a2 c% `; d g an % [5 |% a; i, ?3 O( P" ^2 z7 p. Hnalog signal to a digital signal. `7 j# L% U' W( Y4 j* j( {- ] Z( g ore inputs 6 P9 G. Q" W- E5 d" Gf binary digital information and one output. The output! {( e/ q! k. N( W9 H E1 f6 E 1 only when all of the inputs are 1. The output is 09 ~1 ]7 {7 @, c hen any one or more inputs are 0. Y6 A- ?7 y- {1 _* n4 T; G& J# @ 面气压),- h2 \# `# n) A$ ` 境温度, ! a) R6 D. W3 p, K/ K气温度,用摄氏度(°C)或华氏(°F)来7 U/ c+ h# X2 D/ n. A! t) ~: I$ `2 r) F; @! O+ g& X电压或电流波形的幅度。 ( J$ e6 Y7 O' i0 ^5 k: i7 e7 m$ C& f性变化的信号来工作,或产生连续性变化的信号 . Q) s ]& M; ~9 a统。( Q8 v$ p( d2 k$ u. Z6 l 将模拟式信号,转换成数值式。+ T- p, |* @3 t E8 y 一种有两个或两个以上的二进位数字信息输人,一个输1 k, c' f: k9 N \# Q! e* h/ h- P4 ]; l 的装置或电路。当所有输人为1,输出为1。当任何一个 5 S: R% N8 o" `+ q) A0 @2 _3 @一个以上的输人为0时,输出为0。" }( F5 I, o8 _- O2 j2 T A: N1 E. C9 f6 T% Q8 v; }+ Z% m9 Z surrounding an object, measured in degrees Celsius 2 B+ G6 m9 d2 E2 B, x$ N+ y# q9 F }3 _(°C)or degrees Fahrenheit (°F). + V7 o2 `! u- b+ f7 z/ ~( yAMPERE, A unit of electrical current. One volt across. ?% N. }- s7 g8 f one ohm of resistance causes current flow of one 7 l7 Y% g8 p- D* d, S/ Z) Ja ) s% i. p7 k6 f: p. @$ ]AMPLITUDE, The size or magnitude of a voltage or / y1 J2 x3 v2 ac ' s! D. j6 V; d W* GANALOG, Quantities or representations that are) W$ {7 q& w6 H' O4 B variable over a continuous range.) v3 ^" R2 m$ t y8 a8 n ANALOG-TO-DIGITAL, The process of convertin * M. z' c; o0 M& j/ ]a % r9 x/ X$ t5 K/ H, `# t, l1 X( SAND GATE, A device or circuit with two or m " x$ l7 g9 q% U) j: o* A+ ~o a( ^. ~8 R2 ]is* ?' P0 i3 F2 d# n, ^ w * q) p( j9 t9 E U0 {环境压力(地 0 y4 i' A0 N* s& n6 `, D0 {# R物体周围的空气压力,用每平方英寸多少磅(psi)来9 X+ `. h a; D: S4 v) p" d 度量。: n0 s% S, r j \4 z8 ~2 X5 Y Z% }- {+ ~物体周围的空 * H7 x- h; _" l度量。 ( z$ n6 O1 \8 q6 Q9 C o7 ?$ r$ t安培,, M; T% C8 Y2 L# v 电流的单位。/ a, i" S+ r, y) l 1伏电压在1欧姆的电阻上所产生的电流为$ E* I Y2 h7 j 1安培2 G2 B) ]) W3 J" X9 c 振幅, / G7 g k4 U. z: W! D& L e模拟式,- P0 g. y" a/ K6 Z4 Z/ u0 k 用连续 : r9 \% Q4 j7 O$ ]/ ~1 F: y- [" m+ K9 E& B: M: Y 从模拟式到数字式, 9 ^/ J! S( `9 l: Z' n$ M与门, 5 D% q/ j( O- v: C5 p2 j# w9 @# x) d: m* J p) t( z- i! M3 I+ O英汉对照民用航空词典B OEING: Q# i1 ]* w0 f3 W9 t TECHNICAL DICTIONARY 101 z/ n3 O/ I d- @* j' i: I ANEROID, A sealed flexible device containing air at low ! X% P1 D- `8 ^& opressure, which expands or contracts during change of $ B* {: M2 U1 b `; ]ressure outside the device. ( v8 O" ?! t" o: ]! Vically - [% v- ?1 A3 } Y1 i5 Zr changing the direction ]/ q, L+ l X' L2 h3 Af drive. ; u$ T$ d/ ?0 J: ]( D, G5 E/ _of the wing chord in 4 P9 \; i ~! X1 e3 Jlation to the free stream airflow as it moves forward % C+ H$ |7 P7 Rrough the air. 5 q+ q4 |8 D, B% _al axis of the 6 W+ x, c) O Gaircraft. t0 G, P0 v, u% w$ i% e* n0 D 胀或收缩。8 k0 V' f; i7 { 箱。是改变驱动方向的机械装置。 % @8 q+ i( V' B% s, b机翼翼弦在空气中向前运动时与自由气流之间的夹角。 ) d& D+ C: S2 Z+ n2 f+ }2 x0 ~( ~% P$ K) ]2 U9 k' lp: L& P1 Q5 I) E ANGLE GEARBOX, A part of an engine, mechan " \6 ]/ `& P* p! K7 u9 Adriven by the compressor, which drives the accessory1 o, t9 e7 }* S \- ^4 q+ P- U$ T gearbox. A mechanical device fo % I% W$ q) x# }" r# n+ Zo ) y" }2 }8 D" L9 ~! ~ANGLE OF ATTACK, The angle + A! k2 O8 }' N$ F6 s: p# U& }re 9 p5 B( ~- I' Jth0 j! a2 H6 [; k9 H5 N ANGLE OF INCIDENCE, The acute angle which the 8 e( `$ ?0 l. D8 U/ i# D5 e0 hwing chord makes with the longitudin+ \1 R4 h7 b3 n. i* k- [& Q 膜盒, U7 y4 `/ {7 s3 [5 o内含低压空气的密封弹性装置。当它周围的压力变化 : R. c0 q) g, C- j; o/ R时,会膨 ! q. P3 T* t5 c" F6 _9 d/ s伞齿轮箱, % k' b8 [1 X# V" q/ ~9 ]+ P V发动机的一部分。被压气机以机械方式驱动,然后驱动 ; [: R+ ~$ I) h M附件齿轮 + z# ^. D8 U7 ?5 M! {8 K. {* Q迎角,6 g2 ^1 }. K! r% g$ p2 E 安装角,* M9 a; @5 k2 R0 z _4 Q8 ` 飞机的纵轴与机翼弦线所形成的锐角1 c* w1 @* U0 f6 P$ x; u 英汉对照民用航空词典B OEING/ b# w( P5 f4 N* f TECHNICAL DICTIONARY 11# K+ N/ J+ z a1 e$ [9 ]* j ANNUNCIATIONS, Audio or visual indications used to ' U5 @* w( D- f, ^3 ucall attention to an event that has taken place. - W$ S7 _# s- b1 c" @4 kANNUNCIATOR, A visual device consisting of a number 3 y* K/ H6 E0 a# q5 Yly.1 k4 Q! U: Q; c" w; g( k ANODE, The element toward which the principal stream . z- i( X# c& z: l4 y8 d9 nof electrons flows. ! i! A3 C; B& ?1 m6 YANOMALY, Not normal.- E9 j. t, w2 \; ]. \/ q- p0 M ANTENNA, A device which, used in conjunction with a( T/ z4 V0 [0 u2 S+ V) s transmitter or receiver, is used for radiating or receiving$ L* O1 w# n9 ^# R& X radio waves. D' P: w" _" Z9 W* tNTI-ICING, A method of preventing ice formation on ' v& b0 Q9 @: q& x7 x8 z8 Ae wing leading edges and engine nacelles. , i) C; L' M) uNTI-SKID, A system for providing maximum braking5 a; `2 f& Z) g% N ithout skidding for any runway condition. Anti-skid * y/ M! \9 e. N momponents are part of the brake system. ( G! x# V1 x0 d6 y6 X2 ~告," Q1 T) _; K4 [$ |$ [ 当发生事件时,以声音或目视指示形成的提示信号。 5 d$ D) v" j7 K/ z与之有关的电路的现有情况或已存在的6 y8 H. g4 `- g) N! l7 G" M' g2 F! n7 |1 W5 s. o 正极,5 _: u8 C% P) d v. L1 S( @3 R 主电子流向的极位。; k" D7 M3 g, K2 m; A 异常, ) T* `& m1 P: h; a7 ]不正常。 , E$ H4 [( r/ d. Z, A天线,% ]! l+ U& m: ]6 G6 F& L 一种与发射机或接收机共同工作来发射或接收无线电. X) R: y8 x+ V+ G2 J 波的装置。1 C! Y$ N/ q5 C- v, {6 D( Q 冰, / L! V, ~) S `0 z- Q4 X, _防滑系统,1 p7 {' ]! W6 j# D8 l' | 一种在任何跑道状况下,都能提供最大的刹车能力而不( N( f, R' E2 b* R- E7 n. Y: m V 使轮胎打滑的系统。防滑部件是刹车系统的一部分。 # S3 O; c8 \- _. D- oof lights. Each light indicates the condition which exists" {' B2 H! Y2 ]% T* y or has existed in an associated circuit and is labeled 2 T$ e- j1 W" T1 O- A, A$ t0 x% Gaccording " I2 _9 n- [+ A0 y6 e5 vA, J" k4 A! u! v* i: r! _ th 3 g+ d! x+ O9 ]! ^" e" l1 qA / _$ U1 K: @8 }! @' j/ ^w ( _- P3 z( H5 x6 |c $ I) N7 F: X' S9 m2 V7 O' p7 o+ A, s; a& m信号牌,. A5 x" O- j" b4 K* p* g3 h 由一系列指示灯组成的目视装置。每个指示灯都有相应 7 V9 I. p8 r: e L5 w+ v2 W! y9 P* _的标记,用来显示! t" e L, b; b. o- d: [9 N6 \: C' z5 D& s2 A8 \' E g& o7 f Y 防止机翼前沿和发动机短舱结冰的一种方法。 & S. e9 z) k+ \- j英汉对照民用航空词典B OEING 4 ~* l, a; W; f( b+ ]TECHNICAL DICTIONARY 12 $ E# L/ B7 _. g1 {2 B# bAPPENDIX, A supplement to the Airplane Flight Manual4 P: i: x. p, J+ B p+ H. u tained in the basic manual. A ) D* ]; [+ O5 f& u" k! l) j, c* ]ollection of supplementary material at the end of a& \* b3 E: j5 ~& s% M: ?/ D ook. 2 I2 a8 I5 `6 {- ]of the- t+ K/ B4 n T# B. X rsion link on the landing gear.+ o6 B; ~6 a; ~+ e* c1 o! B APPROACH MODE, An autopilot/flight director mode3 _5 ^3 }* n# N" V! f' d which is a combination of localizer for roll control and 5 y7 {7 \' N1 T# Oglide slope for pitch control. This mode is used when full 0 k/ m5 `% K, {9 B+ z# u0 ?$ |instrument landing system is available.4 i# J. e& V4 F* M8 Z APU, SEE - AUXILIARY POWER UNIT' P7 K) Y& b E. R6 a2 B6 h2 C ARINC, SEE - AERONAUTICAL RADIO' H# A+ }. P5 p* g, G INCORPORATED 6 s: a$ K; K1 s% g1 Y" t' P8 E. i6 ~ARM, To make ready for operation.1 k g$ b/ O M' \ 附录,* Y8 B( w( Z" C/ ^ 飞机飞行手册的附件,包含基本手册中未提到的飞机形 8 H0 d3 G' Z7 s& T x态的其他性能。是附在手册末的补充材料。 6 ?% u/ ^& V7 H7 a' L顶销, : K3 w& C* Y' ]( E用于连接起落架扭力臂两部份的销子。 9 Z6 D+ L1 |8 P5 E; j2 t6 W% k$ a) s进近方式,3 W0 I! U+ q1 _3 W9 V 一种综合了控制横侧的航道信号和控制俯仰下滑信号 ( D! N* v0 F r( m4 M1 v, j0 U, q的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系. n% T* l8 l1 t. |# F 统正常时才使用。 & a5 v4 j7 F) I! r$ ?% Q辅助动力装置, : k' Q6 D6 W, M' Y6 j* X; h见Auxiliary Power Unit " d. G( R" g7 ^/ Lcontaining additional performance for aircraft 4 N$ |( H3 \8 T* g$ yconfigurations not con8 y G5 m1 P6 f& \ c$ J5 [0 A" s4 B b % Y i% {; ~$ Y! S1 |+ }" CAPEX PIN, A pin for joining the two sections 0 z0 X+ S, n( N, y) \6 c: V. fto" ?' ^. b$ g' C4 t$ q4 T; w7 {! Z" M, @) D航空无线电公司,! h- H7 Q9 P- m" N3 A 见Aeronautical Radio Incorporated.: a7 e% @! B6 L 预位, + Z& @ D0 y1 t5 Q7 y' J部件可以开始工作的状态。* G# U4 X. V6 f 英汉对照民用航空词典B OEING ]* _5 M4 i9 F5 {0 L TECHNICAL DICTIONARY 13! ^' G1 h. Q5 G( L0 x% d; i ARC, The curved track over the ground of an aircraft4 [. p+ T1 [! i7 M flying at a constant distance from a measuring; [: \& [9 h# |1 S7 h4 I8 S' ^- I equipment (DME).$ O9 E6 S- B3 l6 X+ ^% D l' w- I in the limits of self-contained system9 t& t7 j g, H, F: L; Z apability.; [7 i# ~4 t- K- ^! f( t4 U4 | tem for opposing or restricting - g0 f, S! y* L3 Uovement.2 K. i7 c/ s% q. u1 q/ F- P SPIRATED TAT PROBE, A sensor that measures total. s& ~; T- ?' R5 \0 V v) F* c1 k8 H ir temperature when the airplane is in the air and that , l! d; f/ ^8 h, g$ veasures outside air temperature when the airplane is/ e3 R5 f0 N* R/ l4 u2 a$ A n the ground. The outside air temperature is measured 3 A$ D0 J' |% G- I$ D- e0 F" E) G8 QSSEMBLY, The fitting together of a complete structure; D2 h2 [1 ^1 F5 c& X SSUMED TEMPERATURE REDUCED THRUST, The) r8 h2 o& r8 L7 f4 O ATC, SEE - AIR TRAFFIC CONTROL, h3 q2 J4 |# e2 A/ m, b" u% Y0 a# T/ c1 P9 {% s 系统中所产生的一种用以抗拒 9 e0 x5 x! O# ^8 j作或限制动作的力。) P- E7 n5 ~0 g- {+ L6 u) Q7 i. \ 头, 5 D4 u3 w: J, g' F+ }用来测量飞机在空中时的总大气温度和在地面时的外& X! J# }; S; X2 F0 n/ r 温度。地面外界温度的测量是利用引气将外界空气吸入 3 f. q4 w( M* |- Y- w: ^# v头,以达到测量的目的。) `$ w0 K, Y- `) ~; a: C 配,8 T; X2 q; n3 y5 N% b+ C 一个完整的结构或组件的过程。 2 w' m9 |5 E9 @8 O2 ]假设温度而得的减推力,9 Q) |6 z* T! C+ p& K% F 推力设定值时,假定一个比实际外界空气温( c" E/ W4 H6 I 空中交通管制,+ j& p6 V4 s7 [+ D 见Air Traffic Control 6 O2 r4 i( ^9 U& e% u2 m& jAREA NAVIGATION/RNAV, A method of navigation . ]# n+ t, t% u' Rthat permits aircraft operations on any desired course V. Q( y: `2 U, {, Dwithin the coverage of station-referenced navigation + j/ P8 J. r/ _# Dsignals or with % l5 V( ]* c3 i8 b" b. v, o) o% qc + c6 t, k6 X! @8 @5 L) F) HARTIFICIAL FEEL, A force developed in the flight 2 \3 S9 Q9 Z/ ~ m9 q4 A- \4 hcontrol or brake sys/ F$ A" M- S7 x0 ?3 E$ m! c/ x m . L7 T' x6 |6 }1 FA/ `. Z, g% n0 m( r5 } a a* c8 V# o+ ?5 X9 d1 C& ~+ l m $ f" S1 p, v& W$ ~" Zo 8 Y1 V, F8 x" `0 ^+ |! Yby using bleed air to draw ambient air through the X+ y. t# y6 K1 Dsensor when the airplane is not moving.) r0 I: v. p9 N. T8 U A5 C& L& g2 q& m0 i/ b8 S or unit. c q% Q3 m6 K+ I; k# h1 F! u A ( _# A% K0 l; v" i5 ?lower thrust obtained by setting a higher than actual1 _& `+ z9 A! t7 Y Outside Air Temperature (OAT).1 k) d; k) ^0 R& K0 c 弧线, p, ?! s, u) p! |+ c 飞机在围绕DME台等距飞行时的弧形航迹。2 C/ U& ~! C% K1 _& ~+ E& d 区域导航,' ] T. m+ A, f5 }, v% e! V, b 容许飞机飞行在有电台参考的导航信号或自备系统能 ' ]+ E) u% m) t0 L S- r- C力极限范围内,飞行任何预定航线的一种导航方法。 8 _/ y, T4 \" y6 h模拟感觉( e* p) B4 V6 W& G 在飞行操纵系统或刹车 ; \& j; E1 d( t# N3 u1 V& v9 N: W# m) o' H 吸气式总温探8 a" V& o+ C9 |8 F5 F, i3 D5 g1 r3 L! y3 a! k* t+ G: v6 t( w) g' {6 y; J; R# {9 P; B9 u( i2 {5 x组合成 * N% e% ^$ J; v" j: ~' c4 s% b5 A3 A" m: L. y 在选择起飞8 U. k6 A; A8 r( O 度高的温度而得到的推力。用这种方法可以减少发动机的 4 |; }1 v1 W1 F4 X8 T* }磨损和维护费用。. Z. Q X+ P! Y" [5 Z% O) t& `. u( }, d: {/ m英汉对照民用航空词典B OEING $ P- g# G9 z$ H) |TECHNICAL DICTIONARY 14 ; d7 n. n8 y4 b) L/ S' z+ {ATE, SEE - AUTOMATIC TEST EQUIPMENT/ o# M% p5 U- x ATMOSPHERIC PRESSURE, Pressure of air due to the, m& ?) w+ s/ A4 ~% L arth's atmosphere, expressed in pounds per square 0 c6 H& n6 a9 Y/ @9 ]ch (psi) or inches of mercury (in Hg) or millibars (mB). / n( C* N) O. v$ l2 m5 `- hTTITUDE, The relative orientation of the airplane with6 K+ T: i* P5 @8 b8 f) T( } spect to pitch, roll, and yaw. # B3 X9 M. O" e7 \( ]. F! O* PUDIO CONTROUSELECTOR PANEL, The panel in5 A2 q( \ G0 Q' |. N$ a e airplane which controls and selects the routing of ]8 o4 ]9 h! H( zudio.( f* x, b6 P" P8 ]% T& O0 C/ f/ z. C) Q UTOLAND, Automatic landing using the Digital Flight # m% T; ^& k- J; @6 ]$ Yontrol System.# ~$ S# r7 B ]0 E+ M5 m3 l n. ! r2 I( t' Y; I+ R5 _. g( kM, A system ! u( i% c/ h3 c! }3 e) womposed of all necessary subsystems needed to guide 5 _1 Z- L+ x4 e1 G- P) ?e flight of an airplane.5 G: W3 k6 q( }) i/ j# N/ ^ EQUIPMENT, System test " c" a: W$ ]$ Z5 Cquipment that operates under computer control. 2 z& Y, W2 U7 t2 T0 }( [/ H/ J; u装置,

使用道具 举报

Rank: 9Rank: 9Rank: 9

3#
发表于 2008-12-24 21:37:12 |只看该作者
e 8 z/ g8 X% o/ l8 W4 ^+ |) G, Nin 4 w# W2 e+ L+ K3 dA$ P( x/ j; N# R E re ( t3 v! {* f- Z& [( }+ YA " ~9 \) Z. E, D4 e# Eth0 u5 S' s9 l6 }6 E& _ a " B, g1 }. h b8 |% O; H. fA 9 o8 f# I& T. s' U, N% i8 F/ BC ) r6 x6 ]0 G; b9 uAUTOMATIC DIRECTION FINDER, A system which& G. |- k# j5 \) u determines the direction of a radio statio- ]6 J% O/ Z/ L" B3 s! C0 g AUTOMATIC FLIGHT CONTROL SYSTE * s/ j- U1 O$ e1 n# Kc 8 k2 R% N, C4 E/ u2 F) [! fth % K8 E4 S% ^9 h% y. [7 f8 T% fAUTOMATIC TEST& S7 K0 M% O2 b2 g" ? e 9 O! ~! s$ f* p- F- i- L# D自动测试 # V1 ?. Y( {" H- p见Automatic Test Equipment.$ X* Y4 z9 p+ Z4 l0 E: W% y4 | 大气压力,+ R" G: k T0 @1 Y; y1 ^& o 由于地球周围的大气而产生的空气压力,以每平方寸多" u0 m; V; D4 J q% j5 V5 q( H1 t 磅(psi)或多少寸高水银柱(in Hg)或毫巴(mB)来' Q3 ~6 W8 w: U1 P1 u2 N2 ~8 T 示。 : _) y/ f1 _# ?飞机姿态,4 ?* R1 Z/ P: ^$ ~- l$ x 飞机与俯仰,坡度,和偏航有关的相对方向。 - Q' z6 m# y' j! J! M* n. `8 S音频选择面板,, Z7 Y' y9 Y+ y/ C8 E6 N1 g 飞机内用来控制和选择音频通路的面板。 5 t4 \; j' h' i8 _2 ~自动着陆, % S( u( V8 ]1 {9 w7 E+ L u使用数字式飞行操作系统来进行自动着陆。 c; ~" H) ~0 C" U& Y2 l' m1 c 的系统。 . K- d9 A+ ^% x! @7 H4 W8 o8 i7 u0 r4 v4 ]) n 系统所组成的一个系统。+ @0 k& X. z* @& | 在计算机控制下运作的系统测试装置。 0 ]7 f; t3 A3 ^% T: E/ Z; t% |& ?0 h7 W9 z2 {. A- n6 I$ |8 U自动定向仪(ADF),: H; q! n! k v% h' h7 s 确定无线电台方向2 p% Z1 c, x# `0 }- K* H3 U' x 自动飞行控制系统! x# P9 _- r" @ 由所有能引导飞机飞行的子3 U W- @! ^- [2 e 自动测试装置,3 l9 V. @# s8 U" ] 英汉对照民用航空词典B OEING4 a. Z7 Q% U' E' e TECHNICAL DICTIONARY 15" x" W9 u0 `* J% t AUTOPILOT, A system which automatically controls" _2 T( a1 F7 U# y5 r and guides the flight of an airplane. ) x7 Z O/ N7 Z* AAUTOPILOT FLIGHT DIRECTOR SYSTEM, An8 U: G! f, l( k+ ` b. ~# @ tor' Z( T) Q K' K UTOTHROTTLE, A system which automatically' h H/ K8 k( d# ]- |. i! o ontrols the throttles of an airplane. # U( E; O- Q/ d0 M. r- Z$ J$ RPOWER UNIT, A small turbine engine in6 A1 o$ D$ R) J* _. b0 d e airplane for supplying electrical and pneumatic 2 _3 F5 R& h9 p3 Z0 P9 s4 uower for systems operation on the ground or in flight.1 C8 p! i+ s" ]3 @8 b' ^ VM, SEE - AIRBORNE VIBRATION MONITOR : h: b0 L" Q# }3 L9 Q. L& Y; E: dXIAL FLOW COMPRESSOR, A type of compressor ; R% ?. C% V. A/ U1 R" P" ?sed in a gas turbine engine in which air passes through, g) W/ }+ z- W/ D- J3 ^1 ] ~! N XIS, An imaginary straight line or an actual physical4 {% u g7 ]) @( Y omponent (such as an axle) around which a body can6 W. Z- Z, u4 n/ f9 D3 v tate.) X) X' ]& p8 ~& f 仪, 3 Q; d" |4 u2 ]& \9 |( P/ S' Y- j n, W7 b @7 y# _" v: x自动驾驶飞行指引系统, 5 X* q$ i( h) [动驾驶和飞行指引功能的系统。 0 u5 q) ~* b. ]+ }: q q* b3 M动油门,0 v; r+ Q/ `& z0 ]/ B6 w. Z 自动控制飞机油门的系统。 6 O3 v/ y5 f+ ?9 k8 D4 ^* ~是飞机内的小涡轮发动机,在地面或空中给各系统提供! ]; v) X+ B1 E2 R* p4 r& U 源和气源。 2 A! {8 T2 }2 ^" _称。 " j# U1 i: p9 {载振动监视器, ?" ~% F& _- S2 b& U! U/ D 见Airborne Vibration Monitor O$ f0 y( U. i+ J, D) d: |6 j8 | integrated system containing autopilot and flight direc4 x) d4 ]& x5 y- Y2 O1 n& v functions.# p5 {. `$ u# Z8 k3 `' g/ }0 F A & d) G" {; Z; b, Cc9 C5 X) Z% t5 M2 F8 A AUXILIARY8 Z. c! A$ ^! o8 r& T; j th + I7 T9 C2 N5 j; \p , H. Y2 x) C/ S, K9 s' X9 Y# zAVIONICS, An acronym designating the field of aviation : {+ a" I5 M* u2 r! o8 Oelectronics. 1 F3 P6 L, ^. ]# i( hA( y' U. q4 p# | A ! E9 i" Y: R0 {1 ~4 W4 z3 fu . u3 J! ^2 c) j) D5 G$ Rthe compressor in a straight flow, front to rear.4 K9 E" A1 B7 h8 q6 I7 g* E1 U A( f7 X2 ]( X! C* G& b+ f! K, M c s3 z* a3 R9 E0 u2 P D) \# |ro ; I- w+ a& m' }3 B! g6 s4 {2 e自动驾驶: r( i& U: x, D3 I3 I9 f 动操纵和引导飞机飞行的系统。4 y8 H3 _6 E! U+ F 一个综合自 & O+ s5 X* v& S( U/ g( W8 S3 e$ x5 \: j% v7 e% u9 e辅助动力装置, " n- C& @0 @8 U+ S$ |- \: A: b% C0 i! }# z; n5 s3 m航空电子学, ! ~: I# K5 \, u+ y9 {, I是航空电子领域的一特有名 3 ?0 D$ K2 `6 @3 K' b0 b* q- a1 i3 U5 b$ u; ^" h. K% c; i" A. c$ Q U/ t3 D流压缩机, / Y* S0 t( W* A6 X. Y+ _一种用于燃气涡轮发动机内的压气机。空气由发动机的 - B/ t& [2 @- b, t" `* f/ Y部流出。) b" O, a" @# }7 B& p9 T- M 线,7 i/ g$ A( o0 k5 u 可让物体围绕着作旋转运动的一个想像的直线或实际1 K' k h' I; ?/ o$ r% X 在的部件(如轴)。4 e. ~6 s; w G5 \ b* S1 Z6 V% ~' }前部轴向流人,压缩后,由后* M) y6 B, ~3 a% |. {5 o3 O1 v# S. G C, J) @5 |. Y5 e! P& n- S1 O& q# u6 E+ w/ s 英汉对照民用航空词典B OEING ) S" Z# h t- ~7 Z9 zTECHNICAL DICTIONARY 16' p0 `* A% i) s3 G1 } B ! M3 m4 N* k$ H: _ACKCOURSE APPROACH, An approach to a runway% s. J1 I+ {, L' B versed. 0 Q& |8 j0 j; B$ }own on the EFIS that 5 \, z3 E# a* k# g C/ [. aoes not readily change, for example, navigational aids.( Q6 W8 Z& ?7 c' s vement in the tank or reservoir. 6 Y: j' V2 t' I( m' e' S, ^ALANCE TAB, A small hinged moveable part on the% }& N4 O5 m# [5 h5 f) A$ \4 | ailing edge of a control surface (aileron, elevator, ( E8 x. |* P6 P0 p3 k! [航道进近, & i& {6 i u/ b, L) J# N K; s0 }相反的进近方向。当反航道进近时,无下滑 0 F; E, @7 V1 I显示在电子飞行仪表系统上不经常改变的数据。例如:% o8 t8 G/ @% ~. K4 u0 ?) R 航设备。- b c& z+ ]5 o# N- w 在燃油箱或滑油箱内阻止液体流动的隔板。! w4 o4 c8 V+ P/ W# | 动补偿片,# e/ s$ w! S1 L8 M/ U7 v 铰接在操纵面后缘(副翼,方向舵,升降舵)的可动部。& w4 h8 U: Q( f4 R* r3 l. H 与操纵面相反,以帮助操纵面运% K8 S* p/ w, q: l3 Y; L$ b B* P2 S- k: x2 O: r7 H which is opposite the normal approach. For a & J0 C/ p7 z* O# o& ] Bbackcourse approach, glide slope signals are not7 J7 _0 h) Y: ~; { available and the sense of localizer signals must be ) [ b8 T- O" J4 i5 n3 v: A2 u0 sre* ?! j) m/ ~$ Z6 T8 E BACKGROUND DATA, Data sh- b1 ~$ i+ k+ C d 0 \6 n: e6 ]7 ?, IBAFFLE, A partition in a tank or reservoir to prevent6 r2 h3 D1 U4 e( z fluid mo ; q. w" A4 i4 `2 `9 ^+ E/ W4 WB 8 a+ L4 U; @# i0 C$ e8 |6 ltr4 {" M+ K3 K, l( y# T7 z5 d' } rudder).The tab moves in an opposite direction to the ! x5 }" ]4 \5 b! P Z8 W& Kcontrol surface for assisting movement of the control ! Z ]. s; N/ `9 Q9 _surface. 7 R: T. Y! @- k! o; a( G6 U L8 F$ Y% v. ?/ i0 Q) P 与正常进近; N: W0 y* `; M) p( c! [ 道信号并且航道信号也必须逆反。 , ?3 o1 T3 A5 n2 w8 T X: r \7 T背景数据, + a- I7 e: t4 s/ m. _* Q; H' p+ \9 q+ k" I- b# [7 O+ D 缓冲隔板,8 X" y% L4 }# h7 k) {+ Z. W$ R/ I) f& o! k 随动补偿片的动作方向5 o2 \) O" k3 Y* _% Z. ]- d 动,减小操纵力。 ) f! k9 q8 u2 ~6 t英汉对照民用航空词典B OEING) }/ P" ~. n4 n$ M/ H: q* }3 o TECHNICAL DICTIONARY 17) w3 z. f% N: s( s0 l* G+ Y BALANCED FIELD LENGTH, The field length3 `' q6 R: p7 m7 D7 j0 o- r/ Y associated with optimum aircraft performance when2 y( l# `" o+ I7 |. k8 R) B bstacles are not a constraint. In this case, after engine 4 t* c# e. S; k W" g# Qilure at V1, the distance required to accelerate, takeoff& }& l% q$ }! N- y nd reach a height of 35 feet is equal to the distance ( H8 n. j) [1 T; u6 @ALLAST, A weight installed in an aircraft to maintain( X$ U& r6 _, Y- }7 `/ x ALL NUT, A fixed spherical nut driven by the: A- @2 w: t) Z: l" D0 B; f; ] AR OUT OF VIEW, A signal used to remove the flight 8 v* R" J: ?3 l. H/ K DAROMETRIC PRESSURE, The pressure of air above 9 u3 D& \' I0 V8 @- _4 C$ {g) or + {5 ]$ ], m1 mmillibars (MB). ' L' E8 j& D+ `8 \ATTERY, An electrical device for changing stored 1 g8 e) _ g; }$ p/ M性能的场长。在此0 ~$ _, ?$ q- U" r3 a. H 况下,V1时发动机故障,要完成加速、起飞、离地35" @: `( [. _4 I) H a" _ 尺所需距离等于相同速度下完成全停所需的距离。 7 |7 t" ~* |* N& r+ V2 |舱物," ~3 u* r$ q# T; p- \7 d 重心在许可范围内面装载的配重物。4 u4 k7 `) G5 e* ~ 形螺母, ' X3 F; C8 f5 ]" ]* g1 e5 S的固定的球形螺母,用以使襟翼和水平 ; ? F, H+ |( n+ m引杆消失, . t/ m' S$ P; y4 {% C5 u指引杆的信号。' J/ I: m5 B& y' z4 [) R 压, 0 H5 l0 r7 s& j; W* [: ^压力。通常以多少寸高水银柱(in! q5 }+ ]. F7 r& a5 q 瓶, % e- |- o9 v# _0 J2 d的化学能转变为直流电的电气装置。 ) a) K! G2 X; Co : b3 t7 B" Y; {! yfa% N+ b$ |% c9 h+ F3 `, k a # W. G& t* M( Z$ w6 j, trequired to stop from the same speed.* Z, n; U0 D0 s7 s0 y8 @) j B4 g8 c. t- F/ f3 Y# k' U2 c9 o' e the center of gravity within allowable limits.9 W8 ]" M- G2 F' h% _ B / _; Y( R4 i/ D; c [% Zjackscrew for flap and stabilizer movement.6 T& P. R& l: Z) L3 M/ G/ ^ B Y0 X4 y/ A" l' I+ }1 e director command bar(s).. ~6 a. M! ^7 T; X+ q B9 `. T& c. o+ l: E d( ? zero pressure measured in inches of mercury (in H 6 q: j8 A1 ^ J3 U1 C- m5 din8 j& v6 R/ I" V* t$ ] BASE METAL, The underlining metal to which alloying0 f; B7 @ ^6 y7 \8 m& O agents or metals are added.- q' ?, C# h2 }2 T( }- L# r8 s# | B ) _; ]$ Z1 |* ^# R1 P+ Lchemical energy into direct electric current.' v! Y7 R& s4 @. F+ N) a2 D 平衡场长, ! N. Y. L/ r3 H当障碍物非限制因素使飞机达到最佳1 W& }5 M; H" k- n3 C5 K+ _' V0 s+ `6 x4 N; m- R+ k7 w# [6 k, B) d3 Z3 `( ~% o- Y/ ]6 b S5 x为保持飞机 8 t: X5 H# V6 r$ f3 {; B& ?1 x' I6 [5 q+ N) y1 Z8 r l由粗重螺杆驱动' U. c+ R* a% W! ^$ b 安定面运动。, p8 x0 z4 _: }% F/ K0 J! d' u3 h7 O# h- Y9 _$ \8 x# r& l 用于除去飞行 6 p) k" G$ r; Z2 {( n4 ]3 Y% B: |6 W) c: w7 ]0 U4 H; s; f- Z零压力以上的空气) ]5 l" |# W& t% ?7 |2 T1 r6 f Hg)或毫巴(MB)来表示。 9 F4 t- H( n2 W3 K基底金属,' f# g- l. G4 P# `% _ 指合金中的主要金属成份。0 Y! w! }9 f6 C2 F- U* L! X. O2 p' W- y. o$ T" X# `* v 将储蓄 X: ]* |. c) ^# j 英汉对照民用航空词典B OEING1 A* y9 m. ]' }, A TECHNICAL DICTIONARY 18$ A6 r; E# U) G/ v/ h5 j BATTER $ C& |6 u' z1 ~direct cu' f/ S) }- r/ Y0 D5 i power su , Z( f' \3 w R; V' T7 QY BUS, An electrical conductor supplied with 9 X" b( a# x& S- i1 Orrent from the battery or transformer-rectifier for 3 O+ b! L+ U; A/ Gpply to operating components. 3 o, t0 _! T1 K+ g+ t/ V! sCHARGER, An electrical device supplied% W! G- z9 V' G7 _) @+ R- Z/ T5 B ith alternating current, which produces a direct current 9 @5 G4 L( p6 L$ L& W2 Output for charging the battery on the airplane. * O* l6 m9 Y4 n, z# sAY, A compartment in the airplane structure. : k2 C ^9 g4 V9 s1 MCD, SEE - BINARY CODED DECIMAL* c% z N+ F. l9 V1 T$ x EACON, A device which emits a signal for use as a) D2 P3 H" Y: U, S, |/ ?- r uidance or warning aid. 3 t6 o; m( i d: SBEARING (NO. 2), The direction from an airplane to a " d; q( Y0 a3 Xground station. - }+ n$ V6 U* a" K+ ^瓶汇流条, 5 w6 _- ^% a& \将从电瓶或变压整流器来的直流电供给工作部件的导 K' y( A" m. L- A, @ 体。/ c) N8 I0 j6 M/ ?( G/ o$ h- D 瓶充电器,# x7 |3 k# W6 r$ v# M4 J5 H 用交流电向飞机内电瓶充电的电气装置。带有交流电的 7 A. h6 }. X- H: \9 {气装置,该装置产生直流电向飞机上的电瓶充电。+ u9 v& @( @7 y7 v% B$ l/ i7 K% t 舱, # d' S5 z; m# P( X1 `- q& C飞机结构中分隔的空间。 / N% P6 |8 R$ X# G9 l* C二进制编码,* |' C. z% Y) W0 n 见Binary Coded Decimal3 |4 O/ q- C+ o BATTERY3 _( i$ [; ^* s7 ~% j2 H w# H5 O, @. {1 j2 M k/ } o5 y5 g9 j7 k$ E* s; A B ' _7 D, c" W* b1 {7 [' {B. n2 I: v0 ?, g) [& T8 a3 B; | B 0 Z. A6 r( |' F* i6 Zg 2 n- F4 e8 ~/ `" H2 B3 C1 PBEARING (NO. 1), A surface that supports a moving 6 v; t+ h$ k0 V& S, p' qpart and reduces friction between the two.( U: v" b6 j! Y$ C6 P! t. J3 a6 D7 v Y9 h5 C3 b0 R5 F- z; L" X- M5 i) w4 R" U% i: y! u# o) z# ~( R6 I5 n8 A, i \! `2 ?1 ^; M i m9 ^& y3 K6 X+ ^/ M$ K5 b" s9 @6 t" I. M& d% b1 p& }信标, " ^+ w# {. Q; ]发射引导或警告用信号的装置。 % v6 |* {% K, v, U方位(NO.2),, V9 N; @% ]6 w/ g e( d 从一架飞机到地面台的方向。- }1 G) t) p+ b+ k$ j 轴承(NO.1),1 w8 O3 W; g7 S" }5 D$ u/ s1 R; L 用于减轻机械转动磨擦的机械装置。) Q1 ?* p v, C- g 英汉对照民用航空词典B OEING( ~( x' H2 s7 D7 h) c u2 K TECHNICAL DICTIONARY 19# s2 s$ ?. s1 V N# E- V1 q BELLCRANK, A double lever in the control syst, w3 ?, i* [: |2 e1 k changing direction of motion./ S6 a8 |& b( ^( }, P em for/ h2 r* ?* U* z3 h7 Y, R# N) q ct in the 3 M. ` W. ?2 g3 |; B; n, qneumatic system for absorbing expansion of duct due0 z# h0 A; v6 ^# S heat.4 J: {6 G6 e ^- Q' l0 v( ~* v ELLOWS (NO. 2), Corrugated folded or pleated5 x y' B2 J0 L5 { i ontainer or compartment used to measure pressure.% G' F+ N+ G( l' L/ I, j EZEL, The part of an instrument case for locking the 4 ~5 B/ i/ e/ class. : m" @" Z5 ~# B0 }# K& WIAS, The potential difference applied between two8 T/ X7 Y2 o+ `1 B4 A oints for controlling a circuit. 5 ~! B/ T' w4 `BILGE, The lowest part of an aircraft fuselage. A place: I. \. t' v) R1 L' m! o8 y! K where water, dirt and other contaminants collect. . u, R) M) a5 C1 K5 \气源系统内提供管道热胀冷缩所需要的余地的波状 ; s' q4 V+ z* N( U% ]* }轫管。. E* `% x+ U% U2 j4 H 空膜盒, ' M7 \3 H8 J& X2 Q4 k一种具有波状表面的容器。用于量测气压。 + j- ~6 u9 {6 \6 [2 o. J嵌沟缘, 6 k4 Z7 b6 _6 G. s+ {, O( H. j将表面玻璃固定在仪表上的圈状零件。4 k( v& d9 n% b/ z; a+ N; L 压,+ S0 M- q' W- b" t- \3 L! L 在控制电路的两点之间的电位差。 / G6 d0 X b" |( `* q! z9 z机身腹部,' G: b# I' W6 M" Q 机身的最底部,通常水,脏物,和其他外来物集存于此。 % w; `# F5 k/ }- e$ X% P" UBELLOWS (NO. 1), A corrugated flexible du 3 B& a) {% i& c6 E4 f8 j5 q* [p' T! m2 a# P' \) a5 x to, d7 _6 o/ _! c6 k1 @ B/ m3 V8 X8 V- o$ q a c0 v* g1 D3 y6 K B & z( x1 B) F4 H! P. F) E- Dg 3 G! f0 B3 f7 L3 ]+ y# ?1 H( q5 e1 c @B9 A3 W( Y4 @, H5 y$ V p 1 E% _0 T! F) r( T `直角摇臂,! m& ?( b d* q" Q; Y1 m, w! b 在操纵系统中改变运动方向用的双臂摇臂。 " n' U$ V; y ~8 n; H波纹管, ) Z5 i/ b6 Q( n' L. E8 ?: }. S8 z; Q' o5 l, ]' I5 O" q/ @8 C7 c# p2 @, M0 \ z4 j# q1 N) Q; y/ b, \: P6 z 英汉对照民用航空词典B OEING 0 M( A8 o X; A# k0 k) H* gTECHNICAL DICTIONARY 20( q. u1 j% d2 o9 Y- u BINARY CODED DECIMAL, A system of coding each8 N2 e2 n2 M, C9 r A& d2 N digit in a decimal number using the binary equivalent.+ e- b0 \4 p: S# R) F8 u BINARY NUMBER SYSTEM, A number system using+ d7 }0 P; p( \5 C9 V) V( p0 {" s8 d s {- P/ J0 L; A: i0 s4 ZIT, In the binary number system, the smallest unit of 5 h3 @) z" \5 O& Z/ lformation, consisting of a 0 or a 1.% v% U5 g$ }+ C/ q2 _$ A J ITE, SEE - BUILT-IN TEST EQUIPMENT / h8 p4 @7 @. w6 O4 W; m8 V: @LANK DISPLAY, A display that does not have any: f2 T/ S# y1 j! a& T9 i! Q. ~/ f dications, normally due to failure.. @6 j7 K$ D( g. Y6 ~( P LACK BOX, A container for electronic circuits to record ! M7 P. a! [8 w' h+ S& oight data./ t- Z' q3 z' j" D7 i2 s+ a+ \ LEED AIR, Air taken from the engine to power various % }5 l6 U7 o. A/ c( T& qircraft accessories.7 H7 L6 w9 `9 Y5 @7 g, t A valve in the pneumatic system for air % a8 P0 P5 \3 K$ H) ?! C2 m, Bsupply from the engine or auxiliary power unit to the 2 Z2 v" P8 }. I8 jpneumatic manifold. A valve on the engine for reducing6 q$ F0 B: J- p# p pressure in the compressor section.7 h8 Q3 b1 a+ \: U 进制,. [7 J$ g" @+ Z( b 进制,5 j% Y f- p/ A& F; z/ K( t 一般用0和1)和2为底的数字系统。$ A& ?, D, i# O2 U) {# w 特(二进位数), 1 T% Q/ W* O1 P% b二进制中的最小信息单位,包括0或1。 3 N: F" s. }! p! h) e内自测系统,4 Y4 H) _8 m$ W& ]( h 见Built-in Test Equipment8 d, E4 P5 O8 ]8 E two symbols (usually denoted 0 and 1) and having 2 a : c; p" B4 o! i; x) D( |its base. - |1 m0 X I8 P( iB ) e6 K G" F1 ?in $ Y6 Q( T. P. _- g7 j# h1 j# n3 A3 aB, r, u+ T3 \* N B 1 e$ j* S6 K$ j6 @in& w$ ?7 u! s0 e# R5 g0 t$ _5 k B0 U7 q% ?3 }; K! b fl. z D/ u5 ~+ H: L B9 S. L' r/ @. T0 s9 S5 a6 k/ e a ( p) P0 y- L; A6 Z- mBLEED VALVE, - ^5 m1 H' k' l二进制编码的十( `6 H) ~ P0 V! u& w; } 一种编码系统。用等效二进制位数编译十进位数的每一 ( C/ k- N$ \5 u- X$ ]- B1 D- D位。% f( H3 Z* [* x! Q# K' |+ C: y 以两个符号( 1 F: {( N8 n- i+ e; d$ j3 X! e8 Z3 k& `3 f5 d9 A1 I( e) t# d$ _- j$ p, O1 e. 7 w" \7 l: s! ]5 }白显示, 9 ]( s4 t# X' l8 }通常因故障而造成的显示器上没有任何指示。 1 Z" C" a! J! N# Y9 K8 s匣子,: g. Y$ C& S' g$ s0 K2 e1 @/ n 装有用于记录飞行数据的电路系统的容器。! ~2 a0 r d t9 C( X) \2 \ 气, + G! v; M# X' Z7 X. E( Q取自发动机而用以驱动飞机上之各种附件的空气。4 h4 i& I+ c9 Y7 U$ N 气源系统内,使来自发动机或辅助动力装置的空气进人 4 E4 g& r# T% Q3 G* x气源支管的活门。发动机上,用来降低压气机压力的活门。1 q' o) }) N7 u: U$ W7 e8 I7 a& k# ]" O4 z( T3 p, ^; g3 B! \- {8 k; [! q1 n* I! z引气活门, 5 ~5 @, k* {' r. }# v" r英汉对照民用航空词典B OEING 3 D/ p+ C2 S+ d; S- ETECHNICAL DICTIONARY 21; }2 m1 I0 C5 n8 X2 j BLOCKER DOOR, A device on the engine for blocking 6 [# p; g/ p7 t" a' t# [the normal airflow during thrust reverser operation.- n" |6 F% i l) @8 Z" a$ q LOWER, An electrically operated fan for circulating air.) {% P% h) W7 D( r+ Y LOWOUT PANEL, A panel in the structure between, I0 ?3 P6 ^- u6 [- R& N1 M o compartments that opens to equalize pressure in " A: }7 H# @% Ae compartments. + ~& `3 V) m6 P& H' |ODY GEAR, The landing gear attached to the1 \9 ^, z: W" a# {% W8 e grounding.2 B% E* |2 \: ~( @ 正常的/ @, [ S% s u1 D0 Q 气流。 ]4 [6 }& V% W 鼓风机, , y( P: c( L6 A用来使空气循环的电动风扇。 " ~4 M" u) e( {4 f+ A压口盖,1 S& l& W9 k( D4 t! g5 ] 两个隔舱之间的口盖,打开后可使两舱压力相等。 % x/ X& e: j" `( O) f( {9 j0 u5 [身起落架,2 X" s5 w. s5 H$ z Y 身构架上的起落架。# M4 L- ^$ G4 W3 `; m$ h: S& f' B B0 l9 u8 _* x9 d M8 U! O1 x B # F9 O# [9 W8 U* Gtw1 M. ]) J1 {5 P3 z2 P th / B9 {) v% i5 `1 o6 J6 G0 p5 cB " s; b1 P! `" _% q' }fuselage structure.$ |: R5 Q3 z( t# L& A1 [ BONDING JUMPER, An electrical connection between ' J% |3 W7 y3 r# Ra component and airplane structure for electrical & B$ W3 m5 m0 d' D- _. U阻流门,5 s7 Z$ |8 M( F9 P7 A 发动机上的一个装置。在反推工作时用于阻挡 0 Q; W% k# f& J) |" ~1 W( E3 T& ]4 m8 s% l6 C u4 ^! J/ T7 Y& n 装在机' Z' ^+ {! }# t7 y# b" |; I 搭接片, 1 Q, t7 p- J4 E连接某个部件与飞机结构以形成接地的电接头。 8 u- o* a5 D. V: c英汉对照民用航空词典B OEING% e- G: U/ |) L- ?& b TECHNICAL DICTIONARY 22 * w( `7 X! a2 l3 i ]BOOLEAN ALGEBRA, A mathematical system for : E0 w/ _' v2 S/ M0 M9 G& hwriting combinations of logical statements. 0 ^& a1 i( x' }7 E' ` gBOOST PUMP, An electrically operated fuel pump for+ {2 X' a1 \+ |$ o5 f fuel supply from the airplane fuel tank to the fuel; ]7 z S! y2 Y. }( V manifold.9 o; q$ \$ `' `0 U BORESCOPE, An electro-optical device for looking at: n9 T3 ?" ~! }: F ternal parts of an engine through holes in the engine.6 S' i1 p4 r7 y: B' q orescope ports)* v5 z2 S* E/ u6 X% ^% L- z OURDON TUBE, A curved flat tube in a pressure gage0 Y4 p4 h5 K1 V* f+ Y r moving the pointer when pressure changes inside ' C4 [7 v% j7 Von the ability of the brakes to3 n* U) I% n1 f9 y! N/ F& z; \- y bsorb a predetermined amount of energy during a ; A" a0 a K9 t* ujected takeoff. 1 A6 @0 J3 I9 R0 X' a* r5 \用于通过发动机内的孔(孔探口)观察发动机内部件的 ) E5 l3 q1 v- |8 }' a' T光设备。 ' b: s- F% n- q- v9 C端管," w* a$ _+ u0 F1 t 测压计内的弯曲扁管,管内压力的变化时它使指针移 2 M( W8 c1 ~, o8 D) F" i0 ^力。# ?) z+ M/ O3 \$ ^6 z9 u, ~ 极限重量, / p1 T# ?$ Q2 O+ t& H) g4 W* y# m. Y- Q 起飞重量。" R J7 m3 Q3 i* O7 d- _ 发动机滑油系统与大气相通的通气口。 5 l* M4 w& [+ k+ Iin ' M2 j& G* V h. y, h(b% w% x, t+ m: s; `) N6 r B ) L6 C: W6 L: x9 C$ e; s( xfo% \" E9 V, Z# d9 {' ?! |; I8 J the tube.1 G4 R; \" Y. }/ ^! N( u2 `' ~0 p BRACKET, To enclose or surround.4 h+ e+ X1 H6 i BRAKE ENERGY LIMIT WEIGHT, The maximum + \+ ^( H# R6 d" stakeoff weight based % _& G. q' C6 G7 C& r. Qa 8 Z1 ~ t4 }% `. |) xre 5 d9 p9 b7 | J& u h% U7 aBREATHER, A vent to ambient of the engine oil system.5 q% V" C, K9 @+ N$ P2 R 布尔代数,5 ~: ~% h# G6 O0 G& g# R4 E) k6 H 一种用于编写复合逻辑命题的数学系统。" }. d' r1 n& l 增压泵, & c- b6 d, h! {2 V K从飞机油箱向总油管提供燃油的电动泵。 # N5 O; M6 }7 X+ o Y孔探仪, 2 s. s/ v9 t6 b, s+ h' ^. H h9 e7 f- E. J' C; K! h' x( n1 e3 c4 N+ r: s( M! i1 [ 动,以指示压3 E' g; R, Y% z 托架, 0 T/ p$ P( v/ o/ E0 M" R, y2 W用于作支撑、装托、或围绕之用。, K& V0 V5 R4 {" S4 o" g 刹车能量1 A2 w" V+ E7 l0 e& ]3 c% T 中断起飞过程中,取决于刹车吸收预定能量之能力的% F! g" f, E: C& r, o. K: |- A5 W0 E x$ R5 b 通气装置,. _2 C$ d0 f* U( Y( j 英汉对照民用航空词典B OEING , _( n8 F) Q+ {; X/ LTECHNICAL DICTIONARY 23 ) L1 }4 i d) a; I# \ f& nBUFFET, Vibration of the wings and airframe resulting 6 ]5 @/ T$ D6 H: T( B9 H0 vfrom unsteady airflow over the wing; caused when5 E1 W" g6 X) V* M/ d& X" w: M airspeed is too slow, the bank angle is too steep, or $ x9 P$ Q" K7 m y+ D" u6 J1 qirspeed is too fast. % Y9 M4 g; ?- t, f) k; Z! r$ UUILT-IN TEST EQUIPMENT, Equipment installed on; Z5 U& g" |+ R/ e( f) | e airplane and in airplane systems to test the systems 4 I8 e) T. h1 q& e+ j3 r& ?ithout external test equipment. ; Q l _* L0 G( e5 NUFFET MARGIN, The amount of residual maneuver, R0 \& l7 x4 D% e7 X) L. m+ a apability present before the onset of buffet.6 c$ P$ ~! v4 L* B* j6 S UG SPEED, A preselecteed speed to be observed3 F) O8 y. q7 i& [4 k nding sequence. 6 x! d6 E! B* k' r3 j; z2 pk2 }5 M" e# B' U$ R/ R, I0 ] ng landing gear operation.; T9 T' Q+ q! ^- R4 p5 l% v1 @ 速度太慢或太快,坡度太大,均会引起抖振。" ?5 j, W5 I' B2 A) B 自检设备,+ a O. m0 P% o$ s! B [9 s 安装在飞机和飞机系统中,在无外接检测设备情况下," y) l; d& I+ C' o) ^$ \: `# l) l 用于检测系统的设备。( }$ H0 M9 q% }" n& k# ]. { 抖振裕度, - B# W& a E9 N9 Q3 ?) H飞机在遭遇抖振之前,剩余机动能力的大小。 ; Q) h9 s; {: @; \- B标速度, 6 E- P9 h# q2 J2 M' ~在某些机动飞行过程中,特别是在进近和着陆时,飞机! ^' [3 o" S g% a0 P 预定速度。 & O! {) d$ L7 L力装置, ) l2 e6 O- x2 |: a/ Q架工作的一种机械设备(弹簧或减震器)。 $ q7 ?- Q; E6 {& J! d: v流条,7 V+ a9 @. C0 { 在部件或组件之间传输电、数据、或定时的单一电线或) L& k4 J+ i* B5 [8 G a: h+ U# e$ X3 M( Q0 |# r" U B ' H r0 ~3 H# a4 W8 Jth - Y0 C9 _ B* `w $ k. | G8 v% J/ EB 8 p, H: s: P8 R! {, Fc # f8 h7 @% c7 |6 h# Z$ K4 Q" F! cB5 t- E' N" X4 f during certain maneuvers, particularly the approach and n2 h2 R+ {" X) ^, b la ]7 v5 f* g* L* @% r" Y% @ BULKHEAD, A structural partition in the fuselage or2 ?* J. L+ a7 c+ `. { wing. * J- p: x# h. m+ w, ]6 dBUNGEE, A mechanical device (spring or a shoc 7 c# |& b2 T/ S1 Aabsorber) for assisti # e4 p& ^9 [" `6 T. ^- nBUS, A single wire or group of wires which transfers* V! C9 W: Y; A' q3 r# ? power, data, or timing between several units or( K! g6 `) W& D$ m H$ @" @: E modules. : _$ {. _5 i# J# c' ]. j抖振,' C+ J6 I) L: c5 h3 N7 W$ H4 T 由于机翼上表面的不稳定气流引起的机翼和机体的振3 c/ O6 x' a0 L) u 动。飞行 / z( Y9 g" ~# M' c1 f# K; k- [& x. |% G7 `8 j9 s# V) z( f所应保持的 / c5 [! T8 G1 _壁板式隔框, 7 f- I/ s4 t( B机身或机翼内一种结构隔板。1 M% `, }& A! h! P$ p1 H: ~% f- g9 Y/ Q( r4 ?0 S/ R, E# O用于协助起落: A0 e" |! w1 Z3 ^4 w& [. `3 v) ?+ l. \/ [电线组。 3 o0 K+ U- S* i. {3 W; T英汉对照民用航空词典B OEING& ?) F$ ?; R+ _8 f9 B) R TECHNICAL DICTIONARY 24

使用道具 举报

Rank: 9Rank: 9Rank: 9

4#
发表于 2008-12-24 21:37:30 |只看该作者
BUS DRUM, A mechanical connection with pulleys ; W5 n8 ?; w# A6 \ x# o: A7 I. Ncables in the control system. . O( ^3 p- a/ `' e7 n8 @# }and$ O( X# R3 K( {5 r" b/ n' D l circuits for control and protection of) N7 Q" Q1 A Q' p# t+ o lectrical alternating current supply to the airplane.: J5 m- a6 f* z3 A' {4 P duct for closing and opening the duct 4 {- L* E$ ^ N8 eassage.- `" E) q5 Y7 _, V1 h UTTOCK LINE, A vertical reference plane along the- J$ O3 p, i+ \; q7 S4 |# D selage for horizontal measurements of the airplane. 5 l, E" _0 m; q! j- G2 J接。 ( s' V s! \* y+ T+ N. S组件,内含控制和保护飞机交流电源的电 - |1 Q/ S# ~; j# {5 d3 j2 C9 ~' r( }9 g8 ^6 c4 F3 { 作动简控制的转动装置。用来关闭和 9 p, j- B9 |$ F启管道。- z5 k8 L/ M) O" h: T4 q* b 沿机身走向的垂直参考面,用于飞机的水平测量。 2 m& D! _" E( g$ X3 WBUS PROTECTION PANEL, A module (black box)7 {7 R1 a2 w& p/ G; q G" T- R7 `* ] containing electrica/ l) ^: V/ F, L" Z; t4 ]% o0 N% ?9 A e7 w: I0 H: ~& F% @" @% A" I BUTTERFLY VALVE, An actuator-operated, rotating1 k# B) l/ f2 q0 ]& F; I) e; o T b- ] device in a2 g' Q1 P2 g3 g. r p0 D& C& @& z. W. c" k/ \6 z B e: r( s7 g/ u5 n0 U/ k& I) }9 z fu4 w+ q( k4 U9 b) |# t7 J$ { 转动鼓轮,3 f+ @- D9 Y. b- n, S; X4 V 在操纵系统中,具有滑轮和钢索的机械式连 + b* X2 m2 U: Z n e2 k4 V) r9 K汇流条防护板, 4 m: D* P; r) P' F黑匣子式的 v3 Y0 Y' i3 [, V1 b8 i) J" ^: s9 Y2 u- _蝶形活门,2 \2 L9 b9 i# s% Z/ M- y- R. W8 I 是一个在管道中由 / E. c6 F( K$ m/ W& T0 z1 w' z& T3 Q 纵剖线, 8 w- @* Y2 P6 ~ c& V" i. f0 P5 ~英汉对照民用航空词典B OEING . I8 Q5 \* u2 w' [6 JTECHNICAL DICTIONARY 25 & i7 z7 D! T6 j+ e3 n8 WBYPASS VALVE, A valve through which air or fluid will% X" V; ~$ J q1 J flow if the normal flow path is blocked. + @; t! |3 Y& K- s$ |6 w W! DBYTE, A group or string of binary digits. A byte is / _; p: M) f( d6 l0 X' _sually eight bits long. ! o, R3 {* S. x% [ABIN ALTITUDE, Atmospheric pressure maintained7 f3 {& _) X, v x; S ithin the cabin, indicated in terms of feet above sea ( B5 B2 b# z) V8 \! d, P% jALIBRATE, To repair, adjust, fix or correct the ) j% |! h F r0 N) ~ D7 E2 I% N4 o! Xeasuring capabilities of a measuring device. % T; t" ~+ [- p" U$ J, PALIBRATED AIRSPEED (CAS), Indicated airspeed5 f% J t: I- O% N4 f0 a AS) corrected for position error. , @- V8 d+ v2 P |) q% L/ Znical! v6 B8 i! J$ j+ i) j omponents./ Y# }% ]" y; A+ O* ~% I# w7 `- M" Y& A% L" Q4 K' i5 Y节, ! x3 h/ S; w2 M5 I r8 z% D7 m, C: Q一组或一列二进制数。通常一个字节长8位。 3 U" t/ O; O+ E舱高度, % W2 |0 J& S' x% }4 ]座舱内保持的空气压力,以海拔多少英尺表示。 " g1 l5 Q, \& _9 R3 c7 d准, - E, s6 g+ U: \/ B' N! p* @1 m修理,调整,定位或改正测量装置的测量功能。: O& P$ w4 G' g 正空速(CAS),2 f, ^4 v% O9 p& Z 在修正了位置误差之后的指示空速(IAS)。 8 b" _% f% d0 u用来移动机件的一种转动装置。 " T7 Q% ^$ P5 T. a6 @1 E; @u& A5 ?& r v9 G" X1 O6 c C + T5 r' N9 P+ f0 L, j7 V, r! Y- DC% t/ L0 m8 K) |9 x6 z( O w ) ]( N- c' p$ U+ Hlevel. 7 c- e* j# _' i( O, @6 J- M" JC Z: x' o" r& F( S- F( km ) m& }, z( U% kC + ^5 v6 s/ v! {5 t4 H' P) p(I * ]5 x, g/ r' ?CAM, A rotating device for movement of mecha& W8 m: g% c5 u+ J3 }1 i4 J C 2 Q+ w2 d/ c/ B1 s9 ^% l旁通活门% L- j2 a- G$ N$ B, V2 z. m! F3 { 气流或液流在正常通道阻塞时所经过的活门。0 S# f$ }, d) _ a6 h* {) k! m _$ j9 F+ M- Y |" M: K) F3 H( r' A9 L1 [+ t* g7 w, G R) F, y/ q; H) ?: {7 r. Y" m& l凸轮, 7 u( A8 l/ Q- G4 a! l9 X5 d英汉对照民用航空词典B' _ j+ O9 G2 u$ e: H CAM-OUT, An autopilot condition in which the actuator/ ]# O1 ^: V2 N% p detent piston is overridden, either manually or by the + A N$ ]2 F* P7 x. Tther autopilot actuator.7 b# S- i1 M3 F' f: R. G" Z AP, SEE - CAPTURE* W& f) O: d7 |7 W APACITANCE, The measurement of electrical energy # e$ h* j7 O6 G* {( n; l; ztored in a capacitor (condenser).' M- K% V' i$ B% X0 p APACITOR, An electrical component of two metal. c9 c* l- r* V. l) y& v lates separated by a dielectric material, for storing s" d, T* Z+ _5 g0 `/ Q3 s% V9 h lectrical energy." n, A2 x1 e2 c, ^0 b CAPTURE, An autopilot or flight director function to 4 c; T; s8 C, ~7 u; }2 y: \. ]9 wacquire a selected mode.9 r. ^* U- Z: @/ e% H9 ]% n, m f; C CARD FILE, A container on the airplane for printed6 O! ~! Z; I+ {/ y: j9 P3 f circuit cards.$ L+ t" R2 i6 O6 M4 e7 o) Q 一自 4 h b0 p1 j9 [1 ^动驾驶舵机所超控。" }8 M9 q" u+ T' {8 n4 s 截获,9 |: Q. R% I- L) v6 R2 f 见Capture4 ~' J4 N2 V* [: h7 [( L o; `3 a4 T! S" L6 d0 l C 7 E* S& q, `. z& IC . O+ X7 C. s3 X$ h( X% R- Ps' x/ G: R/ ^ l; }6 v, \3 t C0 k& K* w$ O; j4 @7 [: M8 R2 { p * E: g5 n7 z4 g# ke) X" o3 X3 ~% ^: G' C( h$ z 凸轮不工作, 7 W7 d1 @9 q, V9 V& B, W1 |一种自动驾驶状态。此时舵机锁定活塞被人工或另 . f' V5 u) Z$ g E) a! T9 k# G4 o3 H: s. a 电容量, . h" Q8 j8 n( o. d& L+ ~电容器内所储存的电能的量度。 ' d9 K. b1 n, S5 G6 j8 w( G. O容器,6 H7 C8 K* \/ `* q 两片金属中间用绝缘材料隔开的电器。用以储存电能。/ `. Z) s6 N" I0 b2 H: I8 U 截获(CAP), * x q$ S" D |0 ~: u自动驾驶仪或飞行指引仪的获取选定方式的功能。 . f$ r$ V% p. O线路板盒,5 v+ @$ I8 M% i9 R1 n2 C 飞机上安装印刷线路板的容器。6 h- b" Y( J2 k( v7 e0 C' N% O- z5 |2 y0 i. Q7 y& B8 G OEING4 n, Z, t' f% | TECHNICAL DICTIONARY 26 # `- Y7 n) W, X5 E# ~7 j2 N, }( U6 }英汉对照民用航空词典B OEING/ A3 T f! K9 x1 {" [% C8 e TECHNICAL DICTIONARY 27- N0 r8 ]" ^/ F- V CASCADE, Two or more similar circuits or amplifying G3 \% _) ?, P- p stages in which the output of one circuit provides the8 h+ M5 I7 x# [# K% p2 p& ^/ S0 B8 j put of the next. 3 u5 @* O" w. T, l5 A( V4 v" XASCADE VANE, A vane for turning the engine airflow9 N, H& i. g, x; }; ^1 Q( x uring operation of thrust reverser.2 W4 z. M- ~0 ~( `, v; W N ASE DRAIN, A drain carrying lubricating and cooling( [! x( G3 u- g6 Q2 X3 w uid from a hydraulic pump.* a5 l( U# L( p- l; F# | ATHODE, The element from which the principal! W4 R- q9 m5 ]1 b8 B% I" V tream of electrons flows. 5 l7 [ t; L/ L. ?6 q' A/ |ATHODE RAY TUBE, An evacuated glass tube with a / _) x$ V' f" G+ o/ ECEILING, The height above the ground or water of the : X T8 s$ g6 Q" H* H& g' Sbase of the lowest layer of cloud below 6000 meters+ t; [) T& R3 Z+ e; D! a (20,000 feet) covering more than half the sky.9 {' h8 e+ p- T! ~ 程。该/ {- W4 i) p9 M1 c3 Q 程中,一个电路的输出为下一个电路的输人。; C/ }- }' ]$ c9 m* g' n& ^0 C* M 叶栅叶片, 7 ~& L# x2 l# [" Y7 \6 }0 {( u在反推工作时,使发动机气流向相反方向流动的叶片。 ( ]5 Q+ ~0 a' k; W% T4 w匣余油管, * ~* w* p) l j; U. @) C液压泵多余的润滑液及冷却液的排放口。9 b; |2 m, H8 F4 U 极,+ T( `9 Q1 K: ~, p1 B 电子流流出的极位。 ; o2 A0 p8 {! j9 p# m极射线管, - p* k! L9 u7 m/ v& l7 U! z有显象屏幕的真空玻璃管。用于显示信息。 4 |& E s7 J8 c云高(云底高),* i' k% _: [/ o# N( s 6000米(20,000英尺)以下已覆盖一半以上天空的最 0 W3 q# Q- d g; R' X% w低云层底距离地面或水面的高度。8 |* z5 c) s# w7 H+ Z in & g, @$ g) S( ]; g0 @C 8 w) [, K$ x# j# rd8 a: {% @( a7 t6 W: N) ^ C7 T! R7 ?% C, |8 B& ~4 a fl4 R9 t- B% a! }7 q7 Y C$ d. ]) N3 N% W! q( L) J s 5 C8 ^% p+ Y* o+ P# ~0 v YC" Z6 S5 ^- p+ d* d' \5 Z$ g viewing screen, used for displaying information., {$ @6 m5 ~: c- H' F 级联, , L! h6 {) {, N3 |, w两个或两个以上的类似电路的逐级连接或放大过 v$ a* |' `# u7 H* k7 _" a& H ~$ k& t% I8 `3 `: R1 |+ x8 m9 t+ G7 A) Z" }: z2 Z+ L& n$ A. y7 I2 ?8 ^8 y; w7 F( G2 ^1 Q9 t; C7 B一个具& c4 _" o2 F4 z z8 D1 Z/ i 英汉对照民用航空词典B OEING* R. R2 j+ S) H8 N TECHNICAL DICTIONARY 28 ( X s* F+ [) q, t- \CELSIUS, A temperature scale in which zero is the+ ], Z' ]) x; _7 Q9 _ freezing point of water and 100 is the boiling point of4 C+ g) C8 |8 T0 y water.7 o1 ^# [ U+ Q3 ~" P5 C/ ^" U CENTER OF GRAVITY, The balance point of an object: w2 [3 J5 T6 r r rigid structure expressed in terms of percent Mean; D! m4 j1 l( }5 {% b) d erodynamic Chord or in inches from a reference point. * }+ E( A4 v- v7 O% m2 l% uENTERING CAM, A cam for moving a mechanism to a5 O/ k4 f) j" [ eutral position. $ V" _9 { Q9 C- MIGURATION, A configuration of the B$ P2 l/ A1 U6 S) C: S- }' l" V Q ircraft approved for operation by the local governing % @3 U% U# H' l7 J% k; Ngency.9 W5 ^8 w# r! B1 a) E ENTRAL PROCESSING UNIT, In a computer or$ L8 k4 n- y* a4 [6 `. O igital circuit, the section containing the arithmetic and- {1 [1 d! o: } gic,control, and internal memory circuits. l B( I. ?, P. F7 e+ X) rENTRIFUGAL FLOW COMPRESSOR, A type of % F" A0 [* z4 z# \- Compressor in which air is taken into the center of the2 S) O$ L2 f. @9 P peller and is slung outward centrifugally into a diffuser w/ `2 w; ^: ^1 Y here it is slowed and pressure is increased.- R/ Y5 c1 r5 q6 P CG, SEE - CENTER OF GRAVITY % Z! `, O7 B$ x7 S& R构的平衡点,以平均气动力弦的百分比或 / W2 w: B& l2 x某一参考点若干英寸来表示。$ |7 t* v) J. e) ~# X 中凸轮,; q( q0 ]3 R+ X/ o$ A 将机构移向中立位置的凸轮。 6 W& p) t8 h1 h( [- |/ \格的装机状态, ) |. R( z4 r5 A由当地主管单位批准使用的飞机装机状态。$ q0 o' W* A) L 中央处理器,* K4 j6 N( H3 Q" B 计算机或数字电路中含有运算,逻辑,控制和内部存 3 p6 R$ q! Z+ B. k储电路的部分。( F1 C0 k+ f1 y5 P 心式压气机, $ h. s+ ^. O" b- E压气机的一种。当进气到达叶轮中心时,被叶轮离心抛. w- }7 N* Y# L% G# @9 i 进人扩散器。在扩散器中气体流速减慢,压力增加。$ A% m2 M1 c; ]: y3 d. k8 W 重心,, w0 E0 ]& I. h8 ^3 N& K 见Center of Gravity% ~+ D5 h# ^ |; M: g o 9 [6 [ l) o0 }8 O2 `- ^A; V1 _' I5 m( c1 T C [% h. a/ `1 S4 B+ _$ en* k/ P. d& h/ y$ o: o2 D CERTIFIED CONF; `, m z* h. a ?+ I a6 F( C2 d# \$ X6 |( r* G0 A a6 B: O+ ]- J) L* m7 n C ! R4 h, T0 u1 l" u3 S& q0 `d- b0 }) d F2 f( _ lo $ i0 t! `" ^8 c$ s5 RC 2 B3 g- b2 A! v! P1 t& J8 zc9 t* b1 o) t# L im ; q/ Q0 A" U! P. m6 D+ J0 D a' g' f+ fw+ o* ] @/ ]' f( ]$ Q 摄氏度(°C), ( b1 p; _) `0 g( K! ]( ~6 S' J5 k/ J) ?温度的度量单位。在此单位中,0°C表示水的冰点, " O/ s8 q: u4 P# ?100°C表示沸点。 - ~- o2 Y9 }8 M8 V8 F* ~# i& h! h重心 7 {. U5 D4 `3 R1 C物体或刚性结7 ]- _7 H* p/ e+ L/ t2 N9 _' w+ ~! U1 M. c" K5 x D2 `4 ?6 n. O% M8 e2 ^; i; I' v9 ?6 A9 @4 m L/ T1 h* p& k4 I+ a n) W5 `, H! a& O 英汉对照民用航空词典B OEING% f1 L* g" M" T' w. U1 d+ i TECHNICAL DICTIONARY 29, B# w9 t2 h) c5 p% c" h$ q4 X CHANGEOVER, Conversion from one mode to another. 5 z. g5 {7 Z2 X* f6 y) y; D, sHARGING VALVE, A valve for supplying air or fluid to" ]9 S6 \1 i# ? HECK VALVE, A valve allowing flow in only one 7 b+ K" G+ r" ~, J* Yirection. See Non-Return Valve. ; Q% ^! e2 f" G0 r7 G, W1 kHECKSUM, In a computer, a summation of digits or & S2 R S# m! e: c1 k4 L# [its which are primarily used for error detection. - G, v3 P0 `: @! YHIP DETECTOR, A magnetic plug in sumps of/ G6 {" f; z" t- A; ]7 j1 S bricated components for detection of internal failure of + B/ D( a+ k2 l8 f" ^e component. 1 L0 S! w2 K* O9 @HORD, A structural component of spars or frames.8 z/ T# {* f* o E8 ^ 添活门, ! Y+ X- Y4 e+ m5 K器充气或加液的活门。/ A( X9 g4 z7 Q; p 单向活门, . n Z, U- h5 E- l. P" Z7 B仅容许单向流动的活门。见Non-Return Valve

使用道具 举报

Rank: 9Rank: 9Rank: 9

5#
发表于 2008-12-24 21:38:05 |只看该作者
C6 g1 h6 m& b+ L a reservoir.& m9 U$ U9 u' A) t$ g+ _' P C . R- ~. N3 A7 ~, t9 t/ Bd $ o u+ @9 U9 d4 eC . x' L! a# [2 s* e& O" h! T& fb ) w+ d- h8 l+ P) W2 ?1 OC) f: j# @* T$ j$ M; r: P$ [ lu5 u" v( T1 P: I1 }& m# Z: n. o th 8 l# Q) G# @8 ], b* KC- O; _. i- G. ~# w* @: v2 z6 [4 n 转换,$ Q( W% a$ G7 n/ q! ^/ \5 @ q 由一个方式转换到另一个方式。+ E1 o S9 @1 O8 j/ l; h! J! |( G. l7 z2 e) D用来向储存 0 q& `. v7 Z) p* `, B) l W$ ?' `8 B8 d0 T% n5 N" K8 a& c总和校验, % ?$ C+ ^. c( K0 i3 k4 r( h计算机中,把那些用来探错误的数宇或位数的总和进 : h" c( y& t3 z4 g4 A( k4 W" k求和计算。 : m' f) _. x7 K* o. O- h: t& b属碎屑探测器, 7 g5 d4 n* }2 S装在被润滑的部件滑油回油管路上的磁性塞子。用来探 * V( W& D5 B* h部件内部有无损坏。* O* Q* \7 B$ |* I/ I+ d' A: B7 b: b+ T 弦,! Y% Y0 F3 g( S/ X+ ?( u: e 梁或框架的结构部件。3 v7 f2 J1 k4 c8 m7 b" J5 o6 ]+ U9 ?; [: d5 `6 l! x/ x8 Y/ T- ]5 r, \- }8 z$ h: `* E3 j; _! {9 s) Q6 I% R. u2 Z- K- ~( l) P# ~& M英汉对照民用航空词典B OEING 0 _ }4 g7 _; ETECHNICAL DICTIONARY 30 - J2 G8 Y. B. h& |" eCIRCUIT, A closed path through which current flows ! }1 }; q9 k/ m2 C$ f! |6 Yource. ) l; N. |" o2 WIRCUIT BREAKER, A device that automatically5 i7 S9 C8 t. K+ t. z eactivate the system. 3 n$ k/ a9 T! V. e* ?lear of all non-frangible objects which i/ T( O; T C0 b$ Y: Hay be used as takeoff distance available when 7 {7 g, Q- v- H( Q5 B5 ~" c# talculating a takeoff weight. % H4 z" ^2 ?2 Vr water under the control of the appropriate 2 p* {' N1 e+ m3 t: ^( juthority,selected or prepared as a suitable area over h2 d; G, J' ^, q4 D) o hich an aeroplane may make a portion of its initial. K" ]* F3 V. ^- @ limb to a specified height./ S& l' q% _7 J% W" o+ A# k% |2 [ increasing.* u! w, r9 h5 ^- y9 x H sed8 P% K4 m8 B- R+ W- U- s/ ~! a4 t& M LOCK SIGNAL, A continuous string of pulses used for - |) M2 i1 O3 Y( Q3 j- N# x开关,2 H3 l' C' s/ f 故障情况下自动中断电流以保护线路不受过电损 # e/ L7 U: S1 n$ |( g- g6 G体障碍物的区域。在计 9 J5 Y. ?; R8 \0 t起飞重量时该区域可作为可用起飞距离。 5 q2 I" q8 G g( D `! T- e是在有关当局管辖的地面或水域内一个界限明确的长 m/ P. u: a' ~形区域。在这个选定的合适区域内,飞机可完成初始爬/ B, ^1 C) }/ Z1 k 的一部分,上升到一个指定高度。 9 w' l' }+ ^1 S% i2 @飞机高度不断增加的飞行阶段。) @9 ]0 @- O& H4 h5 T$ W' E7 L 钟脉冲, " ~6 d3 p: B" E' w i2 \6 J, S步的连续脉冲信号串。 # `5 P6 N! M% C% {8 k, ?from a source, through various components, and back ) V( d) c' M0 f' {, Gto the s ' r, c& e9 E1 D2 J p. v4 k8 `( j4 N3 xC/ ^0 m/ m0 M+ B( U1 ? interrupts the flow of electricity (current) during fault6 u' u5 H9 r6 r/ T1 r/ h A condition to protect wiring from excess current. Circuit . k" E0 U0 J" o5 M9 p9 kbreakers are also used as a means to manually; _1 V" r* v }6 Z# E d ) a& R" @3 J+ A7 cCLEARWAY 1, An area beyond the takeoff end of the2 M6 H z5 r+ @2 | runway which is c6 m% p' S7 b! o* A6 H) _ m 7 k7 Q' i7 y0 D" ]- j. hc # x3 h! b8 h1 }- t% SCLEARWAY 2, A defined rectangular area on the + d2 C* t5 x. `1 J) \8 a0 ~. hground o ; r# X8 a# X4 pa6 H0 s% A: q) H1 z7 ^* u# _ w: F# G0 L; r$ P% q: m: h; l7 l c' H; [8 M; k# L% [5 v CLIMB, Phase of flight where the altitude is) p1 b4 P4 m1 d7 j' p CLIMB LIMIT WEIGHT, Maximum takeoff weight ba' T7 B2 V5 E8 w( K, d/ M2 _ on a minimum climb gradient with one engine 4 z( U6 U% Y% q" ~' x: Ninoperative.' Z0 d7 }4 J) {" K C1 N o, @7 Y5 E: c4 [9 ^ synchronization.0 D: z$ o: m1 n- [/ i* c5 B0 ?, ~, f 电路, 4 p. ?+ ~0 G! l! z- x, k一个闭合的回路。电流由源头流出,经过各个元件流回 - P4 {7 @% G+ [4 _源头。 $ q% I# u7 v+ L- [2 X+ }5 R6 N* ?1 h. z能在, E4 y! d5 j3 F% p4 t$ V: V 坏的装置。跳开关也可用于人工使系统无效。 8 F+ Q) V1 k+ Z* x: r一号净空道,8 s2 }) ~" ?4 B4 t% v 是跑道起飞端以外,不含任何刚3 b0 G3 d5 Q( }$ J( K8 R# q D# ~( p r8 m8 N+ j: } 二号净空道,! B. l3 S8 Q% ^! F* R, E, T( e( R3 o8 A6 D: F* \. P- j, z" d+ `# x7 k | 爬升, - s. _+ [/ S7 P5 ?7 e$ P" e爬升限重,* A9 I( B2 I1 J: f- r# j 取决于由一台发动机工作时的最低爬升梯度的最大起 / ~6 B% k T4 V: n( c6 o飞重量。1 ]1 s3 K! P' m7 Q6 m8 L, D* `: e用于同 & M& l y1 _/ J英汉对照民用航空词典B OEING 2 ?( Z5 b) o% E, T$ L1 P5 R3 Y% [TECHNICAL DICTIONARY 31 ! Q( O& L* n* ~4 K/ |COALESCER, A device in the water separator for& a/ x4 b3 k* s ollecting moisture from the cold air.6 l9 _& X; A, L1 L' n n antenna with a receiver or transmitter. ! N% ^6 G9 g0 {: }) O7 |he cable has an inner conductor and an outer# a! B) P/ A& _; ` rounded shield. , W7 M7 i$ p. [" e( xting one inside the , g7 }' C- ]* ~2 L$ n; Q8 Other for rotating the low and high pressure1 D2 S* U5 a7 r* s- G8 O' y; p ompressors by the low and high pressure engine . v7 s$ L: q# \* h, frbines.! `% v4 `: B' [ OMBUSTION CHAMBER, A part of an engine for0 s! I- ]6 a/ m$ | ^. D urning fuel in the air supplied by the compressor. ( h$ W' N$ }. o% o3 q置。 O# Q1 D9 R/ c9 t$ o 射机的电缆。电缆 2 q/ y9 J0 [5 I9 H. E中心导体和外层的屏蔽所组成。 ' i m2 s' _! J1 ?4 N- N& c5 K1 D7 z两个套在一起旋转的轴。用于使发动机低压和高压涡轮 K1 h l1 l! t" d: V 别带动低压和高压压气机。 3 ^: ^8 T/ w) r5 u, p烧室, u d) z" R+ K% W发动机的一部分。用来使燃油和压气机所提供的空气相3 |7 ], \7 Z* v6 v e% n' C6 ? 合而燃烧。

使用道具 举报

Rank: 9Rank: 9Rank: 9

6#
发表于 2008-12-24 21:38:35 |只看该作者
c ' q$ _1 m2 d8 }, b5 d" ?; P+ \COAXIAL CABLE, An electrical cable usually5 t+ i I! l2 L, R L8 ? connecting a 8 @6 U5 Q7 W6 `( [6 a7 q4 NT ' m# O6 m: P- I9 _g ) o& v! I" ^7 Q+ Z0 xCOAXIAL SHAFT, Two shafts rota % e! ^$ R' C9 z& o. l& oo 8 Q2 c3 a3 t/ O( y) Uc" U; i" O j' Q tu- F( |6 q' }$ V# n+ a3 G# [% Y; c C G1 s- o' m8 m- e1 Q" v4 xb; U( H; K% P, ^( @' w. Z 凝聚器,3 q3 v' ?2 T3 V' q5 L' ^ 水分离器内收集冷空气中水份的装3 e+ v4 @( W; ^" Z' J 同轴电缆, 3 F- |" r$ O' |; }0 C/ T$ Y; u; I一种通常用来联接天线与接收机或发 5 D: a. E$ l# ^2 m. y3 c8 P: b T' u- O" w% e3 A' |同心轴,( m2 j- z4 i1 k Q0 l' `/ A: x1 ~; j1 [0 V; D! T6 w c* g! R% R% g) p2 d. n( [) _ N英汉对照民用航空词典B OEING: A8 H- f" M' H& |+ ^; s+ w- t TECHNICAL DICTIONARY 32 # b% c5 A4 O2 Z9 ECOMMAND BAR, A flight director pitch or roll comman & z, P" n: Z, Nindication. . f5 l1 v7 E6 h3 _d6 Y/ V# y, B4 F x* T OMPANY ROUTE, A route flown by the airplane! @" a6 C/ m3 g3 S" z8 g OMPASS LOCATOR, A low power, low or medium 2 R3 s% ^2 g; ~equency (L/MF) radio beacon usually installed in % s- ^7 F3 V2 `( Bonjunction with the outer or middle marker of an $ b: z7 U d& d$ @tor (LOM), A compass & P7 a: _4 V5 o. K% Hlocator installed in conjunction with the outer 8 R5 }" I- a. F' w( h/ d" H1 ?marker of an instrument landing system.1 t N* v, D3 w ss ! X" r/ m+ z. P6 X1 {$ Ple 9 M5 w; ^% v, I4 U5 Q8 [3 F' `OMPENSATION, To offset, balance, or counteract.8 X* j$ U; s+ d- }# K OMPENSATOR, A dual capacitor for changing the fuel: i" H O& N) n# K/ {3 C aging circuit capacitance due to changes in fuel4 x' s) t) p. M$ A) E3 s4 t4 h ensity. / s- i7 x; g7 X5 n" p$ Z( @OMPOSITE MATERIALS, Non-metallic materials used ) e( c) b3 W' a, n9 ~. vr airplane construction. Fiberglass, Nomex, Kevlar,7 D' O# ?0 G4 D7 @ raphite Epoxy are composite materials.7 T; z1 g( U, t0 O, q3 W 司航路, . `. I9 `5 f: L, j7 c在飞行管理计算机数据库内由航空公司飞行 & ?# d5 D" Z3 f" }: }4 }! D9 f盘定位台,6 r" l4 q2 \2 _6 V v" n 与仪表着陆进近系统的远距或中距指点标配套安装的2 ~& a) Y$ {# m- r 功率、低频、或中频无线电信标装置(低功率NDB台)。 ( L1 M* O+ u0 J; C程序中用来导航。 6 e( Q6 g: w1 V! o; @1.远台, 7 W/ N: G( d- F9 ?* w. x与仪表着陆进近系统的远指点标配套安装的罗4 e/ g1 R# c; y2 ^" ] 盘信标台(NDB)。 1 ]% d3 O% G/ v! |' E- F偿,' X9 g0 E1 u5 Y. A5 o' A) c( W 抵消、平衡、或中和。, D( V% }! A% E 偿器, 9 u5 P0 \) z! M5 ^: N1 `$ \$ z在燃油计量电路中,用来改变电路上的电容,以与燃 ; V' w: P- }3 y, f( ?; z+ T密度改变所引起的电容改变相抗衡的双电容器。 % P3 c* R( Y1 M! G7 u: | b$ R r合材料, - i' Z3 l! f" Y9 f) {用于飞机制造的非金属材料。如纤维玻璃,Nomex, / z) I8 \$ K' ?# a$ aevlar及石墨环氧树脂等,都是复合材料。

使用道具 举报

Rank: 9Rank: 9Rank: 9

7#
发表于 2008-12-24 21:39:01 |只看该作者
C6 _! r5 H( ]2 q0 D! F! H3 } operator that is normally stored in the flight % R* }& ^& b' q% {) ~7 \% M2 Smanagement computer's data base. r/ o% c7 p- r* _3 pC + b1 `2 x% O7 d1 x! C1 ifr& l ?- g" t7 v) p9 }1 P c ' H7 s9 M" k2 m* ?( {* zinstrument landing system (ILS). It can be used for; R. x4 i6 @2 z navigation as authorized in the approach procedure.* R7 [! j3 {% f 1. Outer Compass Loca - v N2 q# ?$ @3 {2. Middle Compass Locator (LMM), A compa) X# [5 R' F3 |2 y, r* f locator installed in conjunction with the midd: ]5 N2 u2 x8 o) e+ p2 Q marker of an instrument landing system. , \0 I9 b* f$ n% l4 ?* cC; Y6 Z5 F# ^/ N. s1 g. z d8 J C ( s# S. U/ ]$ rg ( S% |# D8 x( v% S( cd% l* D' ~: W. d" o: ?4 i C 8 b% H$ k, y8 N- \% z7 _fo- s' }% Q3 W: s9 \, q8 w g9 l! R% J" H# |% @ \ 指令杆,7 E- R3 A7 Y! d% R( ] 飞行指引仪俯仰或坡度的指令显示。 4 H9 y) y! G. h5 f) ?5 _5 Y- u: u, H: @5 t c通常储存# A( m) o, [: p8 U 的航路。% J4 O8 K% m( N3 M7 @9 x+ B: F9 g- L6 j9 M# B: N$ Z8 q' a) D8 Z$ k1 f$ ?* ^: {5 c经认可后在进近 9 |1 o" T! T( w) c- O2.中台, 6 |* b8 s+ {0 b1 ~) k+ u! B- `7 m与仪表着陆进近系统的中指点标配套安装的罗: _5 A3 K- S) j! t0 j 盘定位台(NDB)。 $ X: V7 m/ s0 ~ K" H, x8 ~# x& Z! b* P8 l! |( r+ I! O, T1 {# w: x, o: u' f3 I+ a0 ?6 Z. S* i n& S# G- Z3 }2 B% J# B" H8 bK 3 ] @4 z3 a: e1 b) ~" [$ P英汉对照民用航空词典B OEING9 _! v! d, V2 T! Q. U TECHNICAL DICTIONARY 33' t A2 q( j; f2 J$ S5 S( v7 K by# j4 \% P+ b) l; K- w$ I3 V or increasing air 9 g% G) X6 U* J' o% B# v- Jressure and temperature before the air enters the% f( g! y; ^9 Z3 G5 A ombustion chamber, Low pressure compressor - front - T, @; G" y9 G3 E% v7 tection of compressor, High pressure compressor- rear0 Z/ ?8 k' p- I' f' m OMPRESSOR STALL, An event that occurs when" V5 B# B ?- W9 g; U ere is a complete stoppage of air or reversal of air flow 2 B7 i, z- |$ Z8 y% b. }1 i# \COMPRESSOR SURGE, SEE - COMPRESSOR; f- s1 s8 M% k3 P8 u+ a STALL COMPUTED AIRSPEED, Indicated airspeed' B3 f3 H! o2 G/ L8 C corrected for the static source error. , f4 L% J" p7 M/ }$ l7 H% k的机械轴来驱+ \. ~% D3 C; B' N- c; F# y; M- X, V ,用来增加吸进空气之压力和温度,以供燃烧室使用。 $ O1 P1 S' ?, g; `/ ~压压气机—压气机的前段,高压压气机—压气机的后/ A, [/ D( R" T/ ^+ y& V# f3 l4 ?& k( f, H$ l气机失速,& J/ B, _9 f. r7 N. y 当气流完全停止或通过压气机时气流方向逆反的一种% E3 y) t2 z. D B4 E 压气机喘振,' @! [: r7 u) _0 w& J0 H5 } 见Compressor Stall 7 {$ G) h+ Z2 d: J4 RCOMPRESSOR, A rotating part of an engine driven $ j5 }' T; N% ^5 D5 C/ sa mechanical shaft from the turbines f 8 P- Y$ y% K- ]8 _p& F( |/ d" P. b$ z c9 B1 w( t5 |" ?& y* c0 i s / T" f3 K3 n9 D% B- Xsection of compressor. ; u! b( o* ?' d! HC, W& k3 K8 ?( g: H* b th1 G3 U$ h' J& s; c through the compressor.8 D3 u0 w% s4 f# F" N$ X' ?; x' P 压气机, 8 p6 S4 |2 a7 m) H) p Z5 O6 N' H发动机内的一个旋转部件。由与涡轮相连 ! d8 I" ]- ~; V* h% n" y/ r( G8 {: W) V! O5 h) y* @+ k9 A" A' {7 q4 a! J4 Y: q( g) k( O8 [8 V: o# @5 n4 N7 @( R3 ~! o2 H" p现象。 8 Y5 M$ w1 @2 A- o1 m( q; q6 b9 m2 [' \4 V0 ~. o4 V 计算空速,+ s$ l2 V9 G( u 修正了静态源误差后的指示空速。 6 Q2 _6 q$ \! K& l* Y英汉对照民用航空词典B OEING [+ }7 p7 q7 L& Q! ]4 z TECHNICAL DICTIONARY 34

使用道具 举报

Rank: 9Rank: 9Rank: 9

8#
发表于 2008-12-24 21:39:27 |只看该作者
COMPUTER, A device that performs arithmetic $ J9 j% x+ R* E" g3 s! y3 k" voperations, manipulates data, and makes decisions.3 w1 K+ I2 [0 u" K* f ditioning9 M8 S9 ]$ c% j the air and the0 T% Q3 r, T, H0 t7 Z frigerant or moisture vapor is changed into a liquid. ; g; h3 B* s1 o3 e2 X" f' |( Wine. q% |. O' h$ H/ b; [ ONFIGURATION, The position of flight controls, $ ?+ L4 Z# k: @7 N" S6 Umissing which 7 I6 a0 B+ M% T# m; }) Imay affect the aerodynamic performance of the 0 ], K; B1 B* ?0 ~5 }! q: I% r1 Wairplane. " s' w0 Q7 W1 z* @置。" l4 o a: ~* C7 D, d 中能使热能散发到空气中,以及使冷冻剂或湿3 W# m; t6 d+ }- Z! L1 n 转变为液体的部件。0 {) l( R5 c a6 J- g+ k 连接到飞机结构上。4 I! y6 k5 C7 m3 ` 态,. ^5 y$ z9 Y6 @ 定飞行阶段中,飞行操纵面,起落架等的位置。 2 P/ D7 k0 f2 ^6 \), " _& W, `$ c/ M; L* v3 @受到影响。 ! L- S; y7 S- a/ ?( M' }CONDENSER, The component in an air con6 D' s* ?+ N3 G; D) y$ g system where heat energy is given to. |0 t+ Y) Q7 Y( Y% M re 7 q" T+ j$ g+ a7 x+ F( bCONE BOLT, A bolt in the shape of a cone for eng; I3 n7 A. h V6 c attachment to the airplane structure. 9 c4 Y9 t4 |1 a4 c' @" X1 I5 D1 dC 8 x6 D+ {! M! y- h4 flanding gear, etc., for a particular phase of flight, e.g., q2 {1 o8 I8 }' r Takeoff Configuration, Landing Configuration, etc. 4 D9 x6 [8 f2 I) k$ Z- qCONFIGURATION DEVIATION LIST (CDL), Appendix$ V5 @& X& _) t0 d in the Airplane Flight Manual (AFM) allowing operation3 L$ B: `: i3 _# i/ Z of the airplane with certain airframe parts 2 @5 F, x+ T/ Q/ D计算机, + Q$ o$ T/ T4 D能作算数运算,数据操纵,和决策的装: X2 `( l% A8 l& \4 v. F 冷凝器,% E# N @- ^( Y) n; N" @ 空调系统# b& E# ]6 j1 w- x) z- R5 a1 l: E8 b; q9 G2 M/ E1 f5 H# u锥形螺栓, g) k3 M7 k$ v0 u7 t4 E' ` 外形是锥形的螺栓,用以将发动机4 G7 u0 R2 B w; g6 V" d6 Z0 u% t' I7 _ _6 b 在某一特( r- F! a( Z! Z/ o9 ?- ^ 如起飞形态,着陆形态等。 $ d. \9 n* ^( J3 y T% o3 j7 l缺件单(CDL " H+ A2 Z. l& T# L飞机飞行手册的附录所开列的飞机上某些零件的清单。 : F. l" L/ t p- A) H' x) D在缺少这类零件时,可以飞行但气动性能可能 ( g$ i0 p- v- m英汉对照民用航空词典B OEING 8 N% i9 \, `# V! r, T& `" E2 lTECHNICAL DICTIONARY 35

使用道具 举报

Rank: 9Rank: 9Rank: 9

9#
发表于 2008-12-24 21:39:49 |只看该作者
CONSTANT SPEED DRIVE, A hydro-mechanical . m( J0 Z# v% M& v, fcomponent for changing variable engine gearbox speed# J1 |# s* @. N! f2 q ONTROL AXES, The three axes of the airplane which* m! W9 B" L2 m3 p re perpendicular to each other and pass through the/ A' `# j% @8 t7 D/ B% c0 _) @+ o enter of gravity of the airplane. 9 K2 B, h/ s0 z2 nPitch axis - Horizontal or lateral axis, passes through ; w6 H2 [" b# ~5 Z: I1 e: @the airplane from one side to the other - ( _4 h- k3 U0 ]nose up and nose down control is by ' ?% Q w! a$ a* N, {elevators (and stabilizer for trim). 6 l* M7 m" C5 eRoll axis - Longitudinal axis, passes through the % X) L b( `. v3 y$ I; z3 F' I1 Mairplane from front to rear - wing up and' Z6 M! e, ^6 c wing down control is by ailerons and E- E6 X; ?9 Q h8 d c flight spoilers. + @6 V; U6 B, V8 U( sYaw axis - Vertical axis, passes through the- M/ d- W2 T7 ~# {( X airplane from top to bottom - left and- J; [% v0 v; e$ b7 c5 y( U right control is by rudder.) V! k; l. l9 N$ \; [ M% H6 q 置, ~" t2 @ I3 i# |制轴,/ m6 Y# o f. M, q6 R. L6 \# c- ]4 p 通过飞机重心互相垂直的三个轴。+ F- ~* v0 ]& l 俯仰轴—又称水平轴或横轴。由飞机的一侧通向另 ) y3 W7 L4 a! a6 S& K9 h侧。飞机绕此轴转动即造成机首的俯与仰( Q: V/ e; C( l3 |2 w b/ r1 ] 俯仰控制是由升降舵来达成的,水平安定% d& P7 ~3 ^$ {8 }% i 则为配平之用。 ' _3 L; z1 k1 f+ B. d. s) ~( z横滚轴—又称纵轴。由飞机的前部通向后部。机翼 " r0 p; H* Y0 D g9 j2 Q( u' G8 W下运动由副翼和飞行扰流板控制。 - f' S t% r) u6 @* o偏航轴—又称垂直轴。由机身上方通向下方。飞机 ( l+ ^8 g5 n- R2 O' ?此轴转动即造成机首之左右运动,此一运 * w; u8 a0 }4 s5 U/ o由方向舵控制。 # J% j$ F: Y) }( @* }* Yto constant speed to drive the electrical power.0 _9 V% |' ?4 D; f# Z8 ? C ( {& s2 w% V! M9 }8 Ia . W8 f0 E6 b5 X: E* d3 B( M# ^c % a$ E& j1 Y* V+ y3 \; c恒速驱动装$ i) ]7 s* I! ]1 j 将发动机齿轮箱的可变转速转变为恒速以驱动电源的1 `) q: {+ `) @0 P3 p3 X 液压机械式部件。 & Y. x/ g4 @" s5 i7 u2 a% M3 S0 D$ o/ o1 ?' \9 Z6 ~( ?$ I" { _1 H5 O+ a9 L! Z1 h1 T/ d, b. ^- ~5 Z6 X% H9 _7 \) }/ E' h9 [ F0 s; Z! V9 c. W( c9 f0 S3 u" |. V/ D6 o8 |% o5 G4 k3 Q; N1 F% L% D- Y* Y( d0 I5 {! m英汉对照民用航空词典B OEING& M% b/ i6 ~5 b% @& u& Q( b* c TECHNICAL DICTIONARY 36 " M- Z) b) C6 `! F, }7 GCONTROL COLUMN, A mechanical component used * Y! O) G G+ V! a/ t8 }- mrs$ s% n9 p* L3 a& B nd elevators. , p. s: }, a+ h- p- Z/ HONTROL SURFACE, Moveable panels on wings and) g4 b/ ^! ? j& y8 [) ]2 |: J% j il for movement of airplane on pitch, roll and yaw axes. # t3 P0 k0 O2 H7 T( O0 jONTROL TAB, SEE - BALANCE TAB / `" n" F/ R' p) IONTROL AREA, A controlled airspace extending) O* G' Q0 Z6 z* g, \ pwards from a specified limit above the earth.: w* E6 Q! c0 g" j1 v k ONTROL ZONE, A controlled airspace extending8 A! i1 C5 m" ^ R" K) x pwards from the surface of the earth to a specified , i. H1 C% f3 N5 h. Lpper limit.& v' Z" S/ d& ~% D is 5 e* W6 \# f) vo IFR flights and to VFR flights in accordance w. t- U% H6 v8 c) G+ w3 }5 xwith the airspace classification. ' h- N/ Q# T3 Q* H7 G5 U, a机械部/ D% J( W6 I! r& o: d8 S Q: k# c: O" z* `% L3 E, |; U8 x操纵面,- X4 B i. a. u. i2 R/ e 机翼和机尾上的可动面板,用以操纵飞机俯仰,坡度,/ v. l) `: B0 ~8 ^7 x 和偏航运动。2 z( G, p! Y1 o! X% _ 操纵片,, r S% r# ^3 p g 见“平衡片”Balance Tab

使用道具 举报

Rank: 9Rank: 9Rank: 9

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 , o/ }) f9 z) [# Ta O" M' U, M3 W! D C . Z4 K6 G @0 x2 u) O0 ~ta 1 w$ J" ^! ] Y3 e* c: BC # h& L2 w3 q7 f6 t* I7 E0 q) nC2 |6 m) ?1 m7 H# q% @6 @2 h u% F4 m2 m$ [% }3 X' \& a C % t# w# C* M9 k; o# lu% p: v8 V1 z* \) Y$ r) ~ u! ^1 c4 Z* [! C. F CONTROLLED AIRSPACE, An airspace of defined* O9 ~5 ?$ b# {+ c3 x: O' c dimensions within which air traffic control service5 M1 k! z9 ?( X! b" x" R provided t 5 S9 Q/ t3 h. b1 ]9 B驾驶杆,1 `7 Y4 A% M6 R' q9 S6 c7 }; D 飞行员用来操纵副翼、飞行扰流板和升降舵的1 r; v! o! i0 c" [ c3 ?) h) p4 y* U p( M% R7 U3 H# R+ k$ D R; T! k1 r+ |% s; y 管制区域,$ j" C6 v4 |0 c 高于地面的指定极限以上的受管制的空域。 ' D% X3 O% C0 M/ d3 b$ y& n制范围,7 p. m6 U L0 Y, G! L# o% U: \ 由地面到指定的高度以内的受管制的空域。 4 q& Q' M! e/ V一个范围明确的空域。在该空域内,仪表飞行规则飞行3 s1 I$ t# m0 Z 和目视飞行规则飞行有空中交通管制服务。5 u. f8 E2 y/ {. m! J2 @" \$ J. s( V0 h% a3 h( w k# C 受管制空域,# N* H: V7 g. m3 E( x 英汉对照民用航空词典B OEING8 p- d1 O4 M8 v9 Q TECHNICAL DICTIONARY 37 / O1 ]& w, o* J+ y% fCONVERSION, To change into another form. ( p# }) a5 G2 p3 T- @' W! v; Y% A7 jCOORDINATES, The intersection of lines of reference, ! t* `# r# m) W) `% P/ V$ Z6 xsually expressed in degrees/minutes/tenths of minutes+ p' X2 _% a1 i7 S; s f latitude and longitude, used to determine position or 4 Z( n2 N/ ^; A- K4 p* B8 M+ j! Z. hCO/ @7 ^; o: X, \ \- \" t* q& O destruction of th ! G+ G, n2 v( {. ~& t8 S; nchemical conta% D0 D) X) P& E: m6 s# x COWL, A remo0 I2 S" Y) q$ n7 `9 ` for access to th 0 }1 { L6 _6 `$ {! gFa b+ ], g% M0 g Nose Cowl - Front section of the nacelle for air inlet' F; `/ \( c" ?% q9 v: l to the engine.0 L3 @7 V4 Q0 s# C# w' ] Side Cowl - Cover around the sides of the engine. 0 n l* }% ?* V. q2 m- s EThrust Reverser Cowl - Cover around the core1 x! b; P' f+ I section.# \! T. `- L* v' x: i* g Y( t Translating Cowl -The moveable outer portion of the & M7 i1 @" x8 g4 ]thrust reverser cowl which is * W" [1 e B. Hoperated during reverse thrust. ( a% Q- f2 _7 X0 _5 g: {* l0 A标, 7 H/ E& h9 o+ c' u基准线的相交点。一般以经纬度的度/分/十分之一分 + x) n) i6 |( z读数来确定位置和方位。 & Z+ S5 c5 [" y& C- t) q, T腐蚀: _3 {" O7 v' _" M. Z! p* l 动机外部可拆除的罩子。发动机上的构件必须要取下 E2 O1 ?( q- J6 i& P5 E5 }1 h流罩后,才能够到。 : V/ M: g$ g) @& S4 H# d* S0 H 机的短舱的前段。! k a& z4 N3 l* Q7 u/ M) S 侧整流罩一发动机两侧的罩子。! S* L U- W I3 ~; d4 E 反推整流罩一发动机主体外的罩子。- H& U9 ]$ ?. V( e) |! B 移动整流罩一反推整流罩外可移动的部份,在反推工 ( h4 u S* Z; h ]% f1 B, b: j1 |作时使用。 # D! k+ n6 K" i4 d5 Y6 k! ]- `1 Hu % W" Z: Q0 ]0 T0 O7 Co, A0 C$ Z: k) g7 h location.7 F* `) O3 B$ h9 a RROSION, A chemical action which causes gradual 8 S, S! a) J$ ^* v8 I: He surface of a metal by oxidation or5 f: P5 w$ B& H% ]6 U mination.0 W' u8 l4 t% m% N! B vable cover around the engine sections & X x+ C5 G1 L4 k; k6 a t* je components on the engine. * ] Y z. k, D# Un Cowl - Cover around the fan section.3 G7 b8 h. @3 F5 W) Y 转换, 4 t; l( j& }$ K改换到另一个方式。: i. }" e6 [- {5 R3 Y0 q, P% i' ] }: ^1 d: t" W! a# o. u$ e8 ?/ `8 S# E' B3 S+ u% y# w Z3 O+ ?- f- u5 r; H7 }0 ] 氧化或化学污染造成金属表面逐渐破坏的化学反应。# O9 _- i) O6 d1 c2 T2 n 发动机整流罩, 4 ~. h) `" w3 ~3 U; m+ Z- |( C5 D* m' @1 O7 Y/ ^, s0 C" X9 y- `! f' e( k6 t9 B" B 扇整流罩一风扇外围的罩子。+ K3 p6 z, d) ~" w7 ?, `& O6 i 前整流罩一引导空气进人发动( J! Z8 X, K. s. D1 ^ 英汉对照民用航空词典B OEING / v0 o9 V1 w' b m4 ^. u. v% r8 rTECHNICAL DICTIONARY 38 " {8 g$ O3 K' ECPU, SEE - CENTRAL PROCESSING UNIT, t5 n8 S0 r' u CROSS TRACK, At 90 degrees from the desired track 0 W4 _ I: u$ v1 ?. |5 vf the airplane. For example, cross track distance is the0 D. J* P1 v) _9 [8 I- R; B9 _ istance from the desired track measured 90 degrees G) y8 I9 L' }! \! A* l/ {& Z om the desired track.) R' W) a% N5 x- A6 O ROSS-CHANNEL, Electrical wire(s) connected from7 @) V+ W, _# V0 Z: j ne system to another like system, for example, FCC# q: l* D$ Y* ]. U( @6 ~: Q " to FCC "B". ! G% e4 [' w+ P. An adjacent engine or one on the other side. 3 i: g! l% m U) ?" I0 e; G1 c+ ~l crossfeed, J t2 ]& Y/ a; m anifold for fuel flow from one side of the airplane to the " Y2 l4 I- k; k( {$ Ether side.; ?2 u* W- W0 g" ^3 V# x6 L re " b% H" U. E% m8 ~/ lRUISE ALTITUDE, An altitude or flight level& X, z" C5 R" p5 o8 V K# B# `+ D% B& ~( b* c o3 Z' y( J9 _! r5 `- _ d. ?# R2 q# u% b. }' f) P; j fr; E, w$ Z% S9 | C9 p1 ]8 k( s/ D% B$ w2 X o 4 |; ?* ^( Z0 f+ s% d"A 5 V- h2 K' Y8 n: L( G: B% ACROSSFEED, An interconnection between fuel$ t; N. N5 Z; D& G. G- i, v1 b/ I manifolds for fuel flow from one side of the airplane to + f4 C, w, c1 N+ ma 1 p5 S) C3 @0 v) m g2 s- Z# mCROSSFEED VALVE, A valve in the fue % S N) b; }! K$ f0 g) x! p. qm& `& T- r! ~/ w o $ \- ~* Z9 V! ZCRT, SEE - CATHODE RAY TUBE 7 r# u1 b, q0 }* q# i) s6 y; jCRUISE, Phase of flight where altitude and speed a0 b+ p. _/ q; l9 o6 J basically constant. $ [1 [9 P) {$ ?9 e$ pC, |6 u0 I" M! i0 { maintained during enroute level flight. $ c) e( U- R& c& g( K6 I/ r中央处理器/ @' N0 {& M3 n; q: @4 s c) `0 ` 见Central Processing Unit. ( V( I4 d M+ A# J- |交叉航迹(XTK), 1 L9 ~* N0 z3 I- v* r" b5 h与飞机预计航迹成90°角的航迹。例如,交叉航迹距离 " v. ~1 V, f6 N; d6 o: v0 h+ G# b是用与预计航迹成90°角量取的到预计航迹的距离。: ?" ]6 a& n, q% v8 u+ v2 q 通道跨接, ' X: v# O) T0 l: v4 y" a& ^0 ^电线由一个系统接到另一个类似系统。例如:由FCC + `5 i; B' |/ {5 X“A” : m6 i3 M4 v& b$ S! i接到FCC“B”. / Q$ a0 P* [: C- j, B机身另一侧的发动机。 - \2 f T1 n% Z7 k# G# }7 D% Y! {于使燃油从飞机的一侧 " S+ x/ F- m; _% H$ z向另一侧。 + B$ U7 _6 p. q4 r见Cathode Ray Tube ; {4 G8 C& _. {' D+ C0 N; j3 L交输,3 K; }9 F0 P, ~& T. j# E: O* \& D 燃油支管之间的交连设备。可使燃油从飞机一侧流向邻* ?0 N& K" [5 d7 L& Z 近的发动机或在5 b" ^0 z. k' B; P9 p 交输活门,& Z/ Y+ {4 i) Y& K6 T7 |; g) L6 J 燃油交输支管内的一个活门。用 1 |$ F1 p4 ~. y: C) Q/ E: B' P# L% g* g- f$ q# y" n" N! R阴极射线管,9 O, M! R( G6 U ., Z& M/ i$ N8 g, E9 E: J 阶段。 ' }4 q$ Q' M9 Y" R" I航高度,! b l3 C! a9 D; j1 s$ u1 T/ N# g 飞行期间,飞机所保持的高度或飞行高 / ?/ _* l6 Y$ j4 p3 Q3 A6 {巡航, 6 i- e1 y4 H, h; |" \2 p! K" U飞机的高度和速度基本上没有什么变化的飞行' h+ G; K1 A D; m K; S" x6 K. x1 N, D在航线上水平 7 n8 f% b/ {- u% v7 Q5 e6 A0 o$ w度层。! e: K5 ?7 s9 B# M0 } 英汉对照民用航空词典B OEING * J7 }0 D2 u$ I& ?6 ]1 rTECHNICAL DICTIONARY 39+ P+ Z ?3 H9 w+ l1 \ CSD, SEE - CONSTANT SPEED DRIVE, b5 m6 l' i0 |2 \" v: P* ]$ @ CURE, A chemical change which takes place in a resin/ X( ~- k" d' {8 ~ E2 N/ ` and fiber based component causing it to solidify. " a( D) W6 f4 \. O8 vCYCLE, A complete series of events that take place % |4 v. M* W9 \gularly normally in a continual sequence. 9 C0 D/ Z$ m3 V2 kAMPER, A device for slowing down or limiting4 z) K) {; G6 s, l1 _ s: H DASHPOT A mechanical damper for slowing down 2 n2 H, P) u* p1 B7 Aovement by restricting fluid flow.! m T) \0 Z8 T3 K5 e D- D$ P1 S* i, y# [: g& j; G; X- F ATA BASE, Stored information which is used as the 0 H* Q+ @& i& ^- B7 z% [+ dba' [. L7 d8 h0 D" R% S DATA BUS, A conductor over which digital data is . 4 n. O6 L: d0 ]: K3 e0 btransmitted. " X8 |! E5 N( `0 |DECELERATION, To decrease in velocity. + W, l& g, u+ E, i$ f3 w) T( x% T% Q. _装置,; N: @0 Y7 Z* q& d+ O3 p x( V5 ` rive3 n+ Y+ r$ O0 C: I! y re' C& m! _4 Z, @7 ^) {3 m D6 I' C$ ^6 J( h2 \2 ^: w. i: w i D# e0 Y" ?6 W3 P: S" Y( H movement.9 W% [) Q1 A1 g" Z: D m1 g/ P! E( z I4 G( @ ATA, Another name for information. / K; V/ ^: D( D+ `8 HD ! `; `$ |0 I V# Msis for computation.8 {) u2 G2 |; @' H" ? 恒速驱动. g4 W" A$ w' F. i+ C. f) \ 见Constant Speed D . , t2 s) g V+ |期, 6 u ^( T5 K% n) V9 P不断重复发生的事件的一个完整系列。9 E2 ^ q+ @( n6 m5 ~( k, W. }! l( j* J* I 尼器, ' _/ X. {% M/ o慢的一种机构。 0 _/ K3 N3 @ J: s0 u# X( v4 R! u$ M/ `; u用限制液体流动的方法以减慢物体运动的机械式阻 E# r, }0 H0 {0 q0 [6 H$ t4 P) i9 P- M+ R, z! T; `9 z. Y4 `6 P- Y+ R料的另一名称。* a3 R0 k; o( |3 r$ ] 据库,- s* `' w ?3 `# ^3 s/ h 数据总线,% B$ S+ M( [ [% s6 W 一条或一对导线,用来传输数字信息的通道。$ K7 E9 m" a1 Y9 t 减速,9 |5 R1 m& }8 R. e, t8 B 速度随时间的递减量。 1 ]6 h8 L& L8 F C5 L3 F固化, 3 p* f8 `2 V$ ^* A3 Q2 E+ {树脂和纤维部件内化学反应使之成为固体的变化过程。 ' f/ {/ L7 {, H1 x0 A8 _+ j% b( Z+ G1 B% J& a% ^6 [( m9 Z- q- u1 ?, @: {: M用来使运动减 - T. a2 e' N% k5 L冲器, & I* b! g' b c) {4 S4 t器。. H+ ?, t* n; S 据,/ c3 l& l* @2 y+ U" d$ W: i8 `4 W, `3 O0 y5 P" Z' z9 G) n$ @% X6 W- H( ?3 m储存起来以便在计算时使用的资料。 2 x# N+ m1 @1 [5 N英汉对照民用航空词典B OEING + C4 s% A% E/ JTECHNICAL DICTIONARY 40 $ s$ Y& w9 A$ @7 \ pDECIBEL (db), A unit of gain derived by computing the" \ L; d+ ^3 |; T) B# n- u8 L tio of input power to output power. 3 s6 u7 V$ }+ y7 k7 b1 @6 S* rECISION ALTITUDE/HEIGHT (DA/H), A specified7 K0 w5 U$ B/ \) G ltitude or height (A/H) in the precision approach at2 P8 h9 j% g$ W) R: L! q hich a missed approach must be initiated if the2 _4 b4 b1 ?2 |3 j3 l2 Z- V ECISION HEIGHT (DH) 1, With respect to the % Q( N1 d, L$ V3 n- `proach or * M; N# H# X# d0 uexecute a missed approach. 2 ?+ x! \5 }' ?8 Uproach to trigger the decision of either. z D3 K$ w$ p- f$ L nding or go-around. 9 p' n% t: M7 M h9 z7 zECOMPRESSION, The loss of internal aircraft air! M3 r) [: }( Y ressure. + i! y4 J3 e q3 h. A- ]E-ENERGIZE, To turn off or cause to not operate.) R7 ]3 i- G( C1 h: ~) A rom the tanks " I5 ?# E: @% u5 n( o+ `! E3 X: yusing airplane fuel pumps or external suction. % y- E7 Q+ _2 L3 w算的一个增量单位。分贝( @7 W4 H1 T4 K6 `! N$ O( Y 常表示两个声音信号或电力信号在功率或强度方面的 : N! y7 @$ Q( D2 S6 k& a( O; X对差别的单位,相当于两个水平的比率的常用对数的十 % j( f; Z5 s) _# [断高度/高(DA/H), 7 V/ O$ X) P5 I r在继续进近必需的目视参考没有建立的情况下开始复 & R+ Y1 j% K! ~% L' _, T4 X- u的精密进近中的一个指定高度或高(A/H)。 3 B4 U p* j X! U6 g% T1 ^, G5 ]断高(DH)1, I8 c- {3 Y& R7 E* a操纵而论,指在使用仪表着陆系统或精密着陆雷4 s0 {# F6 K4 J+ Q: g$ `# @ 生继续着陆还是复飞决定的高。. B- x2 V. F6 G7 r$ b% U' U) N; z 飞机失去内部空气压力。1 F3 r) n' [- X. {2 r. p9 Q' ^ 开,, ^& Y1 i) L6 u) P, G% f* n8 M8 S4 ] 关断或使不工作。 4 U3 E$ }0 {# Q5 b z0 S机的油泵或外部的吸油装置将燃油从燃油箱排 * t0 L6 M% F9 R% J出的方法。 4 ^' w! n, P- Y. Yra( }2 Y0 z) c& G$ p: k4 G$ |3 r3 N4 h D! C3 p* u; p h+ L a . T6 E6 p% V' }w ' d7 Y8 w9 ~9 Z- drequired visual reference to continue the approach has& b! Q4 O+ X' X; U not been established.. ~! t$ L9 C+ K D/ i" k( u0 d# s( {, g+ ~ operation of aircraft, means the height at which a ! m1 N- S3 r- C* cdecision must be made, during an ILS or PAR # d2 X5 E8 P# Ninstrument approach, to either continue the ap - d S, u3 V |: X. mto- T/ h% Q: Z% J R/ @ DECISION HEIGHT (DH) 2, An altitude used during a $ q, d9 ]3 A0 m3 m @precision ap9 r3 k0 Z$ s. C la- r; n& q ~5 u; b5 }. s D1 p4 K7 g$ N8 Z5 M! w, G p2 w- T( p) ^( h2 S) z: ~ D3 i/ k/ t2 U5 u! r0 Y: ~$ V4 N DEFUEL, A method for removing fuel f& g( X" [1 {. a# e6 y; W+ v! C' ? 分贝, E* x6 o4 | |& S% z4 m$ L! ?以输人与输出功率的比率来推 ; @* u( K" l0 y& c! W! E% `2 V0 d k: Y8 k* d' K7 u: e+ c2 x' E0 _9 t4 R/ Q2 i9 j4 h) `5 H0 W+ W& O7 ~- K* f3 x2 `, i& T V0 L% c, I5 f2 Y. @: J 就飞机9 P% W& l0 z; N9 `7 [& j 达引导进近时,必须要作出的是继续进近,还是中断进场 ! e/ r- e0 e% M9 R; f复飞决定时的高。) C6 a' C0 W8 E, G ~ 决断高(DH)2,( H# w! x/ I) A( }$ {- e) r 精密进近时产 ' U7 v% @6 m( B失压, + t5 ^; T' @: _3 O2 e( F* R+ `3 v+ x# g3 s排油, I! H# H0 k8 H3 G用飞7 w7 s# X, F# J) ^ 英汉对照民用航空词典B OEING, F- O1 m/ H; n: b5 Z' p TECHNICAL DICTIONARY 41 ' @1 a' v$ l' S, s$ K/ k) Z# YDEFUELING VALVE, A valve in the fuel system for2 ^$ G8 S0 x/ Q efueling the tanks and for transferring fuel between the ! C0 B1 u6 e/ R: m9 ]1 ^( }6 v* f% nE-ICING, Removing ice after it has formed on aircraft. $ W8 r: L0 h4 F }: W7 Z9 `9 TChange or difference.- ?0 \3 I: ^. a" L EPARTURE CONTROL, A function of an approach. t2 T- [0 @: X, x% ? ontrol facility providing air traffic control service for / Z% _+ {1 `9 B2 j3 ?2 P3 Leparting IFR and, under certain conditions, VFR+ L5 C3 z; ^) X EMODULATION, The process of retrieving information : }/ K! Z, D' X( Icarrier voltage. ' ~) B$ b& M6 T$ uation. E) Q! b7 _: I9 b" A8 _ lic / U& z) s" V; _. N P$ Gcreasing hydraulic reservoir air pressure to 0 H0 z% p2 P) M2 u7 `) Pmbient pressure. # z# d* U8 [9 U5 V% x+ e箱排油和在燃油箱之间 * G w! h! W4 I8 M送燃油。/ O' N. h. b5 v 冰,0 u* c5 D9 {/ x6 M! `. a7 h 除去已凝结在飞机上的冰。' }, |1 x! H$ v( b6 c 删去或取消。' r7 m% D1 k' W7 h1 L1 v4 E 量, + y; Q7 M' |0 J% m% L变化或差异。0 c" h' x2 a$ G0 O# N: ]9 d4 U+ { 场控制,% A" f8 ^# X% B 给用仪表飞行规则离场,和在某种情况下用目视飞行4 O& y+ B; ?- W+ F2 X% _. F+ W* J 则离场的飞机提供空中交通管制服务的进近管制设施 , X* [) P# v3 K/ R- I& S$ ?2 [1 |/ u$ F2 g调, % z( q4 Z8 ^0 r电压中获得调制电压的处理过程。 {! z' \1 p8 J X" J环境: N0 w& w3 b0 y 力相同的活门。 & y% G7 d% X9 K& @d - D3 N( M1 a: wtanks. * ?4 f+ D& K# ~% N- OD+ L H- T1 [9 Z, u DELETE, To remove or cancel., _. B$ O4 @, K, @% U% E DELTA,4 `( e8 N( ]( C6 Z D 1 v, x& g. C2 K# K$ Wc % G7 K V. }( P$ Qd 2 B" `$ t7 j! ~aircraft. # H' e. v8 u1 q( G# oD % k+ I- h4 h. V+ i! {(modulation) voltage from a modulated 8 c; b1 o3 j+ U9 }' p" F: XDEMODULATOR, A device or circuit which performs. G9 j; w% e. b+ y" s' S the process of demodul* g" Z: ^7 P) V: m9 e' [' M DEPRESSURIZATION VALVE, A valve in the hydrau * s' h2 d7 n& gsystem for de1 p6 O+ S3 x; E0 F a/ `( M5 R* k- E+ b- ^) j9 J9 c 排油活门,& U+ e3 [1 ?2 s5 @0 W 燃油系统中的活门。用以为燃油1 L C5 v s6 h0 F; Y$ A, E0 o& g# P7 H# G. h3 @/ e3 x' G0 [# o! ?, Z8 D- r0 B& H) I 删除,3 U# P, G4 k9 l: g$ l9 u$ \4 [/ Q, H6 w8 R5 Q2 D8 q1 G' _' K8 U h" R$ Q3 Y0 F9 z2 C( \; f 的一种功能; z( _3 c- E" A( r3 x' ~3 u* d' H3 W3 \$ N 从载波 1 _; i1 H# A& l7 u解调器, 0 @& N: W9 F! @6 ^+ n完成解调过程的装置或电路。 1 x1 l% y$ K f$ g$ d$ X减压阀, % z- [$ L& e4 @0 ?: e在液压系统中,将液压油箱空气压力减至与周围% f% W9 W8 L# y9 ~- o8 T& j# L" [5 E- o# J* t# X 英汉对照民用航空词典B OEING4 h) v8 F, y3 ^: A: j+ |7 S, t TECHNICAL DICTIONARY 422 c5 q- P5 W7 e9 g/ | DESCENT, Phase of flight where altitude is decreasing. , m+ ]( f. @% r/ METAILED FLIGHT PLANNING, The calculation of fuel1 P x5 @. ^4 o [ nd required for a trip by considering each phase of+ [" E* n( E3 n" p3 q+ y; c ight (climb, cruise, descent, reserves). - e! J( u v/ U9 q, y, h8 ^al or & X8 G. Y: m2 H5 K7 Y& y6 X+ vETENT SOLENOID, An electrical solenoid used for # D V2 H' H* S8 E& ut. 5 P) U/ _: C. N5 Sspecified course or. v0 g/ a6 X; m4 L/ B rocedure., \* o7 _+ _) J @# f e. % ]+ v, s: e' r4 ~& Z飞行计划, % z7 j+ k+ ?/ c3 n将航班中的每个阶段(如爬升,巡航,下降,备降)都. |% E% b2 w" A- u9 | t V: \ 人考虑,来计算该航班所需要的燃油量。1 n- Z) @8 ?: J( ]+ Q- @* L 用来感应情况之正常与否的电气装置。 6 j- g4 \3 v1 }$ W! F定电磁线圈, 9 \1 K; \/ J/ l1 L# f( s出接通的电磁线圈。 6 l- W1 h, S5 ]- W+ X差,+ p$ e2 [- }' _" u! x8 V i; c" T 与指定的航道或程序之差。3 t# }) m% n# J- ]- U w 用气压或液压操作的活门机构中的柔性部件。 7 X6 W( n5 L& j* u r5 L! ?D: N5 m e& r& V2 s, n a# B# J! c# p0 _9 y fl6 j u. r/ ?0 ` DETECTOR, An electrical device for sensing norm / ]* K. x9 n0 Iabnormal conditions.( o* | r! k, P D . P8 K0 B+ I: n$ pcontrolling the engagement of the actuator outpu : w* `$ m f) c7 Q, QDEVIATION, To change from a 4 h: @- H) s7 j6 x$ J Ep ; z) v+ A5 g l4 ODIAPHRAGM, A flexible part for operating a valve 0 b% H' u& z: Lmechanism by pressur ], [( K" g: L/ p下降," f' v$ d7 M4 W( a1 t2 x 飞机高度不断降低的飞行阶段。 8 h4 \. y! C# m7 g% Y( d9 z0 I详细 " l' o+ y, b. n! a, `& K. Z6 O! S; I 探测器,4 Z: N/ ^( x+ D4 }+ u1 Q- K3 ?: a5 j2 A9 a 用于控制作动器输/ W% G- A) l+ b" `; Y- D7 e. y3 x$ F6 }& \. u 隔膜, ' x* a0 ?) E4 Z6 ~! |英汉对照民用航空词典B OEING- I& \4 b7 J0 T' Y* W$ @& h TECHNICAL DICTIONARY 43 ( i* i6 [0 T7 C" nDIELECTRIC, A material which does not conduct1 a: i i5 y* C) b; D electricity and used between the plates of a capacitor 2 f; G- S7 W5 r* a Q. y3 B(condenser).' V9 M4 g. \/ r9 C1 X; b+ ? nother pressure in the same system, measured in5 I: ]4 `" @: e- \* D& z ounds per square inch differential (psid)./ O7 G4 Y' I1 v+ X+ s i% W IFFUSER, A part of an engine between the. Y$ V5 @* s9 z% ` u, { ompressor and combustion chamber for reducing the 3 `( d# D; K: Y# z8 K) nair pressure. 2 @9 j0 @7 r7 K6 [2 T8 F" uigh + O8 y- y5 k+ z8 v8 |- a# A8 X$ F3 e0 Upulses.2 B1 p3 A+ l$ o/ h9 A' ] ignal that is a close approximation of the original # [& @: |7 c4 signal." _2 `& K( u6 ~& h; F' _ IHEDRAL, The angle between the wing reference9 ~6 q9 m/ |! g) L m lane and water line. ' m: b. X- d6 O: H) R+ `的压力,以每平方英寸 : |" Q* P j; K少磅压差计算(psid)。 9 H1 } p' Q) z1 D+ a散器, 5 n- M" c& U5 I+ J3 r/ d/ f# }0 P发动机内压气机和燃烧室间的一个部件,用来降低空+ E; r$ P9 G' o. f 增高空气压力。; ?( p( ~. Y/ G* \* G3 { 换, 0 M' E. r0 s0 j3 V* b的连续可1 p, p' V2 G6 A' C( v2 ? (模拟)信号的处理过程。' l0 G1 n& e, ?5 |9 y" D 反角, & |5 T* @, i5 A% D机翼基准面与水线之间的夹角。! } @# I, i8 z DIFFERENTIAL PRESSURE, Pressure relative to ) s7 i: ]" s9 |; ~4 g2 Ra . ?5 y. z8 ^3 x0 t# S( c. X) Tp5 q4 I; U: Y9 N D; H) \0 H; V2 h4 S; |2 [$ O' a7 J% y c8 s# b0 B/ Q L& ^1 f3 M airflow speed and increasing the 6 L+ @7 O+ a+ \# Z9 h/ W5 VDIGITAL, Digital refers to a signal whose amplitude 9 H% ^5 m; e; t4 ]0 G8 xremains constant for a finite period of time. Digital' D- F; A0 w: G9 T# m+ V( E( A, Z5 E signals are commonly represented as a series of h+ u, z7 C* R% ]+ @ and low , H, _$ W2 T* d8 H0 t: oDIGITAL-TO-ANALOG, The process of converting a/ D+ G8 J. u6 d6 O digital signal (binary) to a continuously variable (analog) 8 ~5 b! `' w, O! g0 ?5 j; t3 fs 7 k! D. s1 Q, s; xs 5 X- v+ m! ?/ N& c2 u7 ED! t: S0 v& z- x) q: }2 p p4 Z' T8 c8 F( i( | 电介质,) A0 V' t Q. u1 L" L& Z* J 一种用于电容器板之间的不导电的材料。 / \3 x' m1 ]& O0 v( K压差, , y, k: h& I$ I A( Q; O1 u4 B相对于同一系统内另一个压力 / X j7 N# z i3 L/ |1 q2 k/ K1 t& ?) u9 |" O0 v% R7 p 气流速并$ F" N* `1 p2 S- A1 `. N 数字式,* D3 V3 j4 e: |$ S; `# a% E Y 指一种信号。该信号在一定的时间内,振幅保持不变。 . o- O0 m n5 E4 ~) Z+ ?. v通常由一系列的高低脉冲表示。" b% \# V3 j$ e6 q& l1 {- s 数一模转 3 {9 ]; H. S+ y将数字信号(二进制)转换成与原信号相似" w Y/ z, b6 _- P9 j& j* m+ ~* T8 V- O: ]# R: z1 w" y) f, q9 P% J) l. p) {3 S' C4 U% X英汉对照民用航空词典B OEING - ~% a6 P. l- E0 G( z* o6 x7 E4 JTECHNICAL DICTIONARY 44 ; K# D: ^0 Z9 |' E; UDILUTER DEMAND REGULATOR, A component in the# Z5 k; @7 `- e crew oxygen system which mixes air and oxygen and3 h n. v9 ~5 O3 o3 [& F$ j2 v+ Y! g upplies constant oxygen pressure even if there are " U% w' R" @( k. R+ Q7 ehanges in ambient cockpit pressure. , A) A" u# k3 n6 L& ^: MIM, A word value of light. For light control devices - dim + s+ J: r, M3 o Gthe opposite of bright.* R9 ^$ T, s% R% w IODE, A device which allows electronic current to flow # c5 }6 ?( S9 \$ q6 w3 fonly one direction7 |: F; }/ l/ n uid in a reservoir.' G2 K' W* l0 {7 _) Y+ ] DIRECT, Straight line flight between two navigational% ^* ^4 I! q% n/ Z$ i; Y) y aids, fixes, points or any combination thereof. When. e2 m h; Q% `" u7 c$ n8 D used by pilots in describing off-airway routes, points1 I% |$ [6 f) b' X defining direct route segments become compulsory; C8 Z' W, c1 X% a5 [8 w reporting points unless the aircraft is under radar" p; E2 ?- b- R control., g3 s$ A( A3 }6 x! S 节器," {+ g7 [7 u! c4 `# U 将空气和氧气混合,5 x" J8 w! I8 @, h& P$ D 使驾驶舱环境压力改变,它也能提供恒定的氧气压力。, I" k6 R7 B& a6 q( Q. W9 v' ~ 一个形容光线亮度的词。对于灯光控制装置,暗的反 5 d) ~* z5 `$ B9 X5 e+ L4 O词是亮。$ M( ]! `7 i- _3 p" A 极管," e1 P+ V, z6 M! q* b, N) e 只允许电流向一个方向流动的电子装置。" n% b. h6 u4 i 器内液体的量。- [3 z8 i. ] U- J1 f 直飞, ; j# h9 `5 z F# d! a# E" r% m Q两个导航台,定位点,导航点,或任何的组合之间的直& a# j8 k7 F1 W ^, w 线飞行。在被飞行员用于描述偏置航路时,除了在雷达控 ! Q" W9 ?6 p+ D# E' c0 q- V制的情况下,确定直线航段的导航点成为必报点。 ; d( I6 R, r) Q2 h. O& [# p& v! Es- ?% X! X& M, W) x, N+ Z c6 B t9 a$ C* m D4 l* W4 I7 J' _9 p% F is ( y. c2 I" H, w S1 XD) e8 H; m+ X, l) \3 a! p in & l( y* [+ m4 Q. K2 QDIPSTICK, A calibrated rod or stick for measuring a0 P# U6 q' z. `5 B5 p0 H% i3 C. ? quantity of fl. ?' o. I3 n u) J# ~, I& f 稀释氧调 . N+ \5 [; E4 a/ L/ i- Q驾驶舱氧气系统中的一个部件,它% t8 t0 a+ @( f0 i3 s! a1 y; V; |! i# h5 L# Q& J# _, n1 M3 ^/ F" A2 s t# U* T: W% {! |' B3 v% o0 [7 K. j1 r量尺,4 `; i) c' [9 k# Z5 a8 E 校准过的棒或尺,用于测定蓄液 8 m; J# D( \% Q; U# a英汉对照民用航空词典B OEING ( c( ^1 U- _+ w: uTECHNICAL DICTIONARY 45

使用道具 举报

您需要登录后才可以回帖 登录 | 注册


Archiver|航空论坛 ( 渝ICP备10008336号 )

GMT+8, 2025-2-23 05:25 , Processed in 0.057004 second(s), 9 queries .

Powered by Discuz! X2

© 2001-2011 MinHang.CC.

回顶部