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: 6817|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% N* [! Z: U' [1 n. Q 民用航空词典. W8 J% ^* n9 ^7 l% m 波音商用飞机集团/ G+ |: q1 C0 Q4 B9 @+ ] BOEING COMMERCIAL AIRPLANE GROUP 0 Q6 }' ?" N* A9 [英汉对照民用航空词典B OEING9 Z( h' ]# Q& Z: `$ o TECHNICAL DICTIONARY 1( b1 V$ K0 X( b8 Z* U- Z9 D; t6 U A 1 h. j# o$ k5 x% j: s0 OABEAM (ABM), Beside: An aircraft is abeam a station : n: l, j4 d) S) |7 @- ]% gwhen that station is 90° to the right or left of the track of' v; }. c) q+ \7 w0 b- Z the aircraft. " v( i C9 \, x4 [; JABSOLUTE ALTITUDE, The actual distance the aircraft) W" X, R4 V9 ~9 N( Y is above the ground. P6 X; J2 y+ D0 C. \ jABSOLUTE PRESSURE, Pressure of a liquid or gas 8 t6 \7 `: I3 s- Dmeasured relative to a vacuum.0 _" x+ m( r) P9 m* Q: C ACARS, SEE - AIRCRAFT (OR ARINC) REPORTING0 B$ B0 s, i/ d* z ADDRESSING AND COMMUNICATION SYSTEM ) X x z' V4 M! |. vACCELERATION, The rate of change in velocity with( q! D% {' U$ v; T respect to time.( C @* ~' w' D3 }3 \+ L ACCESSORY GEARBOX, A part of the engine,6 i3 `: s+ r/ t/ P: }: _; L# V mechanically driven by a compressor or an angle- ]. v8 s# c( F% \ gearbox, for driving components necessary for engine * K( j# Y [0 V/ k; T9 ^, K正切,, U( `5 N& T1 [* Y7 Z* Y" _ and airplane operations. + R: B `# P, Y5 |当电台在飞机左侧或右侧方与航迹成90 度时,飞机正9 `7 g, S+ i; B5 U3 s 切电台。 ! N6 U) I" V! u+ C6 H( c绝对高度, / D% j1 }1 y7 n" [: x0 Z飞机离地面的实际距离。' }% O) E9 O" j& [2 n 绝对压力,% I5 U- W; F6 | 相对于真空(无压力)测得的液体或气体的压力。 8 O" s+ k$ j7 V- ~/ b! r飞机通信寻址和报告系统, & w( @3 F9 {- z3 V7 q2 Y+ q- [+ T见Aircraft(or ARINC)Reporting Addressing and ' H2 @! I2 L: z" X6 g, cCommunication System. : W# q- y& d. L$ c9 i加速度, 0 s( \( X/ H" k7 z) Q5 H( F3 \随时间变化的速度改变率。 ) j; {/ e2 h5 n, Q附件齿轮箱, 9 u0 F4 [$ q1 C4 }发动机的一部份,由压气机或伞齿轮箱带动,用来驱动: h$ c: J! c& B. m( B" n( b1 u' M 一些使发动机和飞机工作的部件3 s: L# P3 u7 B& w* s" y3 L! d. ]( F 英汉对照民用航空词典B OEING ( ~( x% ^* b2 |; @TECHNICAL DICTIONARY 2 5 p' `* X" V! m0 W9 `+ a- oACCUMULATOR (NO. 1), A container with hydraulic % I" @4 O7 ~( j2 f) r Nts when normal hydraulic supply is not- S9 `0 u, L/ [% |& d vailable. " h+ W3 y0 k7 C. hCCUMULATOR (NO. 2), In a computer, a special3 l; a: }2 ^( h) N2 L8 T: u4 v torage register associated with the arithmetic logic unit, ! y4 c Z6 I: F& e" K6 K9 o" _% ?olding the results of a computation or data , q' ?6 }8 Y2 D }( e% TACTUATOR, A mechanical device operated electrically,8 ]+ I) a+ B. y; U2 }, u hydraulically, pneumatically or mechanically for 8 ^6 j/ }2 K; W& T+ }transmitting motion between components. a/ w$ M/ d; {* c8 Z! fADC, SEE - AIR DATA COMPUTER $ w- x: ^0 W) b% N- X& B0 cADF, SEE - AUTOMATIC DIRECTION FINDER - U# t5 v* Y$ N( J) Q! f5 EADI, Attitude Direction Indicator, An electronic display of v& ?; \' R& i! X8 } m+ C airplane attitude information in pitch and roll.( @4 J# [ X$ A& j) O 蓄压器(NO.1), # h( p. K( x- `, u9 q- I含有靠干燥空气或氮气增压的液压油的容器。当没有正 * o3 t9 e/ ] m, L) Z: i常的液压源可用时,该容器可用以驱动部件。 8 g0 t- a0 F6 V% `7 S存储器(NO.2), 9 W4 v' M+ K) h2 Q& t* T计算机中,一种与算术逻辑组件有关系的特别存储寄存 $ Y: z% A" q+ [5 o% F5 P器,用来存放运算结果或数据传输。2 j( d$ P$ o1 ]" i. \' O0 `' Q) b 飞机状态监控系统,; x7 F6 O: c; C% P3 H& }$ m, M 见Aircraft Condition Monitoring System: q5 Y5 t X2 u' k3 w1 f, P fluid pressurized by dry air or nitrogen for operation of , ]1 Z# v( T2 j1 `) Q: tcomponen, ]7 [) ~5 A/ d3 G4 |) y0 G5 n. ~" E9 N* t a7 d9 i# V! b$ z0 T5 `" {$ M A , o1 H) R8 Y( l. R% J% D( r+ Ws : h. T0 Z4 ?2 b- C& eused for h 5 Z2 [$ \, G/ M; V8 `9 x, F1 c, \transfer.4 |% |8 C, i8 ]8 a# Q+ x! V ACMS, SEE - AIRCRAFT CONDITION MONITORING6 `) ]5 ^( ^. @4 r. e; d SYSTEM . 3 r9 F4 b+ O9 N% B( G作动筒, ' R( i/ y) O4 g由电,液压,气源或机械驱动的机械装置,用于传送部" ~, [# Q1 m. ? 件之间的运动。 1 ~0 O' R$ L L" L大气数据计算机, 9 P" k, _3 ]7 _8 D见Air Data Computer., o3 m8 L4 m i3 Q6 _ 自动定向仪, & S8 b( n M$ Y& a3 a" w见Automatic Direction Finder." ^3 e _( ^2 m 姿态指引仪, f+ y# n1 \9 a0 ?( K- O6 g 用来显示飞机的俯仰姿态和坡度的电子显示。 1 N- G! X2 W1 R" P/ B M9 r2 z英汉对照民用航空词典B OEING8 Z1 v+ e# M7 R6 Z! O# t1 a" ^ TECHNICAL DICTIONARY 3 % @9 u, R$ E& k+ K9 KAERONAUTICAL RADIO INCORPORATED, ARINC is 2 ~: r" K7 \ \* h, 2 y$ \1 ?, ]5 ~, d/ pnufacturers, and foreign flag airlines. ARINC 3 a9 N# E% z& s# i7 {# E, J5 Pevelops and publishes standards for electronic# L3 R; x! u# ~) { quipment and systems.* v0 J1 U" {5 @$ \0 G GILITY TUNING, The capability of the DME to1 B# }" G. I! i lternately tune between two different DME stations in 5 I3 U5 A8 N: krder to get two distance readings from one # G" [$ a/ [9 y, U; Hterrogator.; T; ~0 u2 H. M- T" h5 o2 Q+ u ge $ h; ?. b/ }5 d( iILERON FORCE LIMITER, An electro-mechanical# C; m' i) J) `$ n# d: @9 E" y* j; P IR CLEANER, A component in the pneumatic system1 _ Z6 r- t. V% z# v upply to the air& D2 x2 D$ n0 _% n$ d onditioning system. m, P2 h3 C/ L8 Y/ G 订并出版4 t/ @6 X G( `& L) D$ l$ T 子设备和系统的规范。 , r, x! @- T# \" d6 C r' I# \6 u快速调谐, 3 o7 r+ j4 e5 \3 h X1 X: _4 N机载DME通过交替调谐两部地面DME电台以测得来自 & H" Q" [3 B; K( b5 \, I同一台询问机的两个距离数据的能力。 + D3 b: j' M% z( U翼操纵力限制器, 9 k; d! b& l E8 E( p# f. [5 r8 r# V9 o装置。在自动驾驶工作期间,用来限制驾驶盘& ~* j4 r4 p; @ 气清洁器,! e$ S) V4 d0 L3 i7 J 部件。用于去除供空调系统使用的发9 y3 D+ D, ~+ V) ~6 Z) t6 x3 S2 w a corporation whose principal stockholders are United 5 ]9 ]/ l' a( y5 Z+ A& ~( ZStates scheduled airlines, air transport companies! G% ?7 t9 ?- c7 n. d$ a aircraft ma6 p, Z' M6 [# t; V d 0 J: u8 \' x, O( Y& g0 De $ V. g$ c- c' I% F- f8 tA1 {/ V4 b" ^( M U' N% ]' @# S7 E8 a! \ a" _' e. G! y b: ?9 w! l! F5 X o 2 |$ f' K; F0 ]( M3 _6 Ein" c+ j: ]$ ?3 a/ Y F AILERON, A hinged moveable part on the trailing ed ! W( b- ^, q& A9 @of each wing for airplane roll (wing up and wing down)% Z7 F3 b8 f$ f1 x/ [9 ^# U. s5 @ control.5 B. M# E& p m2 m# K; D A: |# x3 \* |1 [ device for limiting the control wheel movement by the" y1 `+ H p8 {7 o* S2 B% _ autopilot during autopilot operation.& f$ z$ Z% C- `% @+ t' w) K5 S A h$ `2 p" c% z+ G8 O6 T; ?for removing dirt from the engine air s7 b# Q5 i% o- T# [7 Z/ `7 ? c : _1 m2 U# ]; `& x/ A航空无线电公司, - P5 l5 k- X. P4 j主要股东为美国定期的航空公司、航空运输公司、飞机( X0 y; o" M9 N. z5 L 制造厂和外国领队航空公司的组织。其目的是制- Z" V% c9 B1 r, ^/ i% E& w% Y$ w+ D副翼, * v3 I* G, _$ G# k' w9 x铰连在每个机翼后缘的可动部件,用于控制飞机的滚转 ' H+ Q8 Y& i( U; n( v j, l(机翼向上和向下)。7 b+ N4 {5 i, K4 n- e8 z. @; b, @6 e( y+ H- R; G! O3 e一种机电 + w2 `1 z- D/ v的动作量。 / U2 S6 X- A, B" G7 h' r1 I& [( g+ A4 N% I8 W/ S) X 气源系统里的一个 ' C0 u4 L7 P6 M' v% T动机引气中的灰尘。 , C7 h$ @& x9 o/ O! ^* K英汉对照民用航空词典B OEING8 Z: B3 W* K$ { TECHNICAL DICTIONARY 4/ h; B( t2 W, ]' l; {2 G AIRPORT ELEVATION/FIELD ELEVATION, The) P \+ F- Q2 [* @+ m( F3 U: i" Q highest point of an airport's usable runways measured S" R8 T6 s; p0 X% uin feet from mean sea level. In a few countries, the+ Y/ L* S" z: U' @' U0 i airport elevation is determined at the airport reference ; U" u' `/ f7 x7 ypoint. / A' J; q+ S) iAIR ROUTE TRAFFIC CONTROL CENTER (ARTCC), + C1 ` E- U5 i, nervice 5 J( z6 d: z- ]# d8 m( G9 Sase of ) L9 v9 ?+ J% s) R+ \- `; }# [us flow of air traffic.1 d( M; N1 S U: U4 E IR CYCLE MACHINE, A compressor and turbine on a. x" G9 ^8 S1 k ?* h ommon shaft for cooling the air in an air conditioning8 s2 F* h& @7 }/ l7 \* r ystem. The air is cooled by expansion from high to low 0 R9 P& X9 \+ [8 \$ h# Qressure across the turbine. The compressor is driven 6 p5 u3 M. ^0 U- Y; ~y the turbine. * d1 J, l! L) ~5 @( R4 N5 t中航路交通管制中心(ARTCC), + W- p' u7 f1 ]. Y/ s( b4 n; G域范围内使用仪表飞行规则飞行的飞机提6 x6 K" w& j+ {8 L 管制(ATC), 3 z, K) K$ n$ Y7 s+ C涡轮冷却器, . x6 T$ X5 k2 {" W# j0 t是装在同一的压气机和涡轮,用于冷却空调系2 [, B- I1 ~7 ]4 p7 `. t1 \3 n 统中的空气。气经压气机压缩后,由热交换器移去热量, " T$ j: C/ U) G* R然后经过涡轮令涡轮带动压气机。通过涡轮之空气,温 - I$ p- H$ _/ N4 s D' z& g度下降。 ; j% E6 r J$ {* ]/ P$ Q! UA facility established to provide air traffic control s/ O% p+ K: p" x/ R to aircraft operating on IFR flight plans within controlled * D* |/ Q/ p4 B, z' eairspace and principally during the enroute ph " J# V. r1 H4 a) |3 Nflight. : a" i8 x# l3 l3 |9 |AIR TRAFFIC CONTROL (ATC), A service operated by 0 L Z. b* v5 R% T: J7 p; Vappropriate authority to promote the safe, orderly and # L$ h( s k$ c8 L5 j5 |) | a" u; iexpeditio " c' M0 i4 O% z; i( G% ]A0 E/ q1 ^: E( h; Z$ c c7 q* u0 P) i9 e V+ Z; p s ; W4 q3 D8 @7 _# R' qp. c5 F; M, N: Q3 i" K; E$ E b1 A/ f/ ~& N. j, x% T- ?2 H 机场标高,# {3 W/ l& L/ W8 a9 F" H! a8 S; ~/ i 指海平面与机场可用跑道最高点之间的距离,单位是英+ g9 [6 b! L; z- H$ L; d 尺。有几个国家的机场标高是由机场基准点而决定的。7 c- K% x3 m8 U9 W+ ^) @/ u4 D' F5 W( \5 v' A* O- ^给在控制空7 {, c+ W- i& u% j% O$ M _! s# a* } 供空中交通管制服务的站台。 3 b4 r+ V0 ?/ V" n- [4 N空中交通 7 |; {/ p, g# r" S. Y由有关当局管理,旨在促进安全,秩序,和效率的空中 ' a& p. ^: [9 U1 D& ~0 P& c3 U交通服务。 9 b0 m, C( ~* }. |4 W# G2 L; l根转轴上 D: Z- q4 e S" ?- F+ ]$ n" O) _3 m5 h9 n: X! c; ~ M3 p" I7 ~/ O: E& ]# l: Z英汉对照民用航空词典B OEING; N$ P) i! C& {; A: h 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 5 h9 L8 S% W, ?# i6 ^4 _data information, such as altitude and airspeed, based& N8 I6 X5 Z4 w on pressure and temperature measurements. + n4 Y* c. E: p: Wes air # K1 c m. C l; F1 vIR TRAFFIC CONTROL, A system comprised of$ G. H7 {( B9 v, e5 }7 }7 M+ F round and airborne components used to identify, track 5 d& D) @+ X" R6 VOUND SENSOR, An electrical device operated 3 t/ K$ ^( s$ N7 H0 a% A$ {y the landing gear, which transmits on ground/in air ' f3 X0 B- j0 M o! G3 tformation for system operation in flight or on the, q; Q2 B/ ~! J( f round. 1 Z' S' P& c8 X: n+ J) TIRBORNE VIBRATION MONITOR, The AVM takes, K& L' }; `- p# [ e signal from the engine mounted accelerometer and0 W- q k! N9 r$ R alculates the vibration on that engine. # {, l1 h9 [' q, r/ rcorridor equipped with radio navigation7 I' ^* l% O3 o: @ aids. ]' M! h$ [: E- L* Z5 E& D5 gAIRCRAFT (or ARINC) COMMUNICATIONS 2 c$ Q2 P8 H& _! x) j7 Z5 PADDRESSING AND REPORTING SYSTEM, An6 `4 V( v: X2 [2 G addressable digital data link system which permits the" `% c. H6 A0 E# M5 @( U. | exchange of data and messages between an aircraft7 p6 I A5 Z1 D! R& P" n0 h5 s and a ground-based operations center over a radio/ a. b# Z8 ^% _, \, D3 V network. ' _+ b8 l; \! o* V5 m3 j6 T' S# VAIRCRAFT CONDITION MONITORING SYSTEM, A : w7 s+ q$ X6 H7 [* usystem of sensors and recorders to monitor various7 F) c, D8 j: M8 ]$ M airplane systems' performance and status.9 A) |8 x$ {) b 机,1 y: Y' r9 b0 n7 ^; b3 \5 X 中交通管制, 5 q% s8 D/ L. D' q一个由地面设备和机载设备组成的系统。用来对飞机进2 {) m5 l: ^$ y5 t 地传感器,& B/ T) K' k$ D, A1 |: b 一个由起落架操作的电气装置。用于给空中或地面的飞 / U- n0 F3 s* ~% R系统运作传输地面/空中信息。(有些系统只能在地面 $ `% h/ t0 o1 [6 m用)* `! X8 Y5 q" _7 G6 C& I- i) t 载振动监测器(AVM), * K$ q6 ~. ^, ]0 x6 a1 JAVM从装在发动机上的加速器取得信号后计算出该发* l4 ^1 K A4 b/ V9 f/ l 机上的振动。5 G/ ~ W: X( z. Z B! w) ]5 f) g/ U) g 式建立的控制区域,内有无线电导航设备。4 W1 z, ~3 w: i 飞机通讯寻址和报告系统,: D4 X. }, h) I) R) u" P 有种可寻址的数据通讯系统。利用该系统可使飞机与地 & _, L7 A0 \! x面操作中心通过无线电网络进行数据和信息的交换。9 D9 ~) W4 h- T 飞机状态监控系统,% I+ e# k, K5 v4 W% L% G' d 一个利用传感器和记录仪对各种飞机系统的性能以及% G8 ^7 `2 C j* Y( m 状态进行监控的系统。1 E0 ]$ ?; T9 ?& [; Q: J0 V A. [& I0 y1 Q. r" Y9 B0 w1 b g 1 }" ^+ f& i, I) @1 I- T9 rand locate aircraft.& j0 w9 r6 m$ V: h AIR/GR 2 U. t7 r: |3 t5 b& w) C, ?& [& E; ?b" ^. S$ d! J6 {' m4 @3 } in " T0 \3 \' P9 s* `g 0 P& R: D9 a. C+ gA * Q/ P+ l# g) J7 mth 4 @ V& h6 w9 }c \5 E0 [: P) J1 K3 I AIR WAY, A control area or portion thereof established $ B0 A( s- O/ Zin the form of a+ A `5 w2 e1 s) o4 J3 [ 大气数据计算 . n* N- T7 Q0 [根据量取压力和温度而产生大气数据资料(高度、空速 ; H: h/ f7 F0 s# |/ I8 X等)的计算机。 " U" U p% y* G4 |; k z# Q; j4 O$ a* E4 [行识别,跟踪和定位。4 z H; r) X: ?# j' p. f9 G1 y6 i$ j S- x4 Q* m' b' @8 P! n/ q' F 使5 o9 |- x6 D9 a0 e3 K( j/ L3 v( L7 F/ ?& s* F# @% y4 e- M3 N航线, # @" }4 I1 _; d以走廊形 ( d7 a& d( P6 V% Y& e w英汉对照民用航空词典B OEING ( A) r0 t8 U4 M* ^TECHNICAL DICTIONARY 6 / d2 A/ v' ]* ^) T4 [9 H L5 DAIRFOIL, A surface designed to obtain a useful reaction,( J8 S& k% `- d, D% B such as lift, from the air through which it moves. Wings, 7 G x& V) I, S$ i5 Q# v3 rstabilizers and control surfaces are airfoils.# t# e5 x5 F+ P9 P" { AIRSPEED (IDS, TDS), The speed of the airplane ! i( I! R/ e$ g/ R& Y; [rough the air. ! z- G, a) a7 {- H P9 ]D INDEX, An adjustable pointer on the4 m/ n7 H( \& f6 F: ~ H irspeed indicator.0 f; V; u; D+ b9 S- w6 A and legal ability ; a$ d' s, t+ l- R. J0 R: Mfly. % H/ {& `9 }0 p# |- a4 Tm, for example, the procedure for finding the . a: C' \* d, m5 vquare root of a number. ! l0 x: h5 f* by & x; i8 T8 L9 J/ f/ [+ p; Ire, wind,2 Z* ?! ]5 Q) ?- z and aircraft flap setting./ c; D3 ]2 T3 c- x# P 是翼面。) n9 M! f0 K- o1 f! X 速, 6 n. ?" P, n2 T' Y! q8 q- W飞机在空气中运动的速度。 ( x0 g! B7 x& Y% X& M/ f, U) ?/ y$ ] m# I# S9 F/ h 在空速表上可以调整的指针。- r9 i( }1 a0 T% L( v- H# [ 机械飞行能力、和合法性的飞机状态。: p6 p% L. M ] 一步一步的解题方法。例如,计算一个数的平方根的步7 n, O5 v* ~ G5 b5 k- Z6 y/ O2 s x- L) A% s1 h0 f' I6 t& M8 Q9 c5 J 资料的法定文件。 - K& e# j% _. O) Z翼位置成函数关系。5 O1 z' Z/ G! ?3 G( h; b" i th + t2 r3 ^! F1 i' x. X1 dAIRSPEE 1 y0 T. x. c1 a% o& e0 v/ n$ Xa" v. ^) U$ Y/ W% \/ _ AIRWORTHINESS, The condition of the aircraft with7 }! T1 p" k2 `/ v0 o; w% p respect to its aerodynamic, mechanical, V5 u& H; f! ?0 @6 h0 sto ' j; n, E; ?8 @* x! FALGORITHM, A step-by-step procedure for solving a; Y4 T( e0 g, \ proble % {3 \9 U4 M' Ss6 z: d# T7 h* k( `, v8 S0 Q) h AIRPLANE FLIGHT MANUAL (AFM), The legal7 J$ T( O Y8 d, t8 Z0 T! _ document containing performance and operating limits, 3 S" X/ E; I0 N. P: ]+ Aoperating procedures, and takeoff and landing 0 k+ Y. ]5 p% A T5 Hperformance. 4 @; i/ L) s0 s' z) DAIRPORT ANALYSIS, A comprehensive set of takeoff $ G! V4 ~, m* c: j" Bweight limitations for a given airport runway, generall 0 r; p* M! o# n0 l; ]# ppresented as a function of airport temperatu9 n$ d% s6 c7 L d* W, s7 ~ 翼面, w& j, a n* \5 `+ {- d, \% J4 S6 T用以从气流中获得反作用力(如升力)的表面。机翼,' {5 s% ?) t# a! Z 安定面和操纵面都 1 {( U/ q s% z9 ?5 t9 k% q! Z" S- F/ ^& Y! w! Z空速指标6 D4 `% A- N! h" ^! q& y/ Y 适航性, ! }: j X5 m A有关气动能力、! Q$ q! s; P @0 Y- \4 K* b- R 演算法, , p2 i: `# K( q: L& {7 i, z3 A" [& w飞机飞行手册(AFM),( L! Q" u2 r# \8 X0 s 包合性能极限,操作极限,操作程序,起飞和着陆性' q6 v! L: ^0 r, L4 v* T3 s# R- W: t; w, j/ C& U& Z机场分析, : R+ [+ h: M3 w: t一套针对给定的机场跑道的详细重量限制资料。通常与; p5 e7 E. Y4 Q 机场温度、风、和飞机襟1 B0 Y# P1 s6 ], `: n0 F 英汉对照民用航空词典B OEING% L4 n; ^& x+ G- w7 V; b# x TECHNICAL DICTIONARY 7' A0 i }6 N- B AIRSPEED BUGS, Adjustable pointers on the airspeed/ y0 w1 g1 U" a8 b; r indicator. 1 Z' [; K! z$ c% F6 N6 K5 R/ WALLOY, A mixture of a basic metal and small amounts 8 T8 V! ?! Y# w. y+ _2 C4 v5 P+ Kf other metals to change the properties of the basic " ]9 Y h! Z9 l E; Tetal. / ~9 K% |5 c+ W7 I* Q: _* \/ ~Minimum airplane speed.* ^ s& S+ _3 Z e of$ r4 m) y* _% h e itting airplane angle relative to8 ]# U7 c8 Y% z2 f: C$ V& q irstream for the stall warning system.0 }( n2 }$ ?3 z6 y' Y: _8 O another.0 [% r. ]1 T0 u8 w5 a LTERNATE , An additional airport selected during - `! G1 I/ l8 q6 [. K+ d6 _9 G! g! Y6 Z合金, / \ n, i, y+ S7 Q( T9 b在金属中加人少量其他金属,而改变其性质的一种金属1 X6 E9 X. ^" r1 W0 U) C 合物。+ ]/ Z6 P2 N1 F3 Z$ J$ G/ Q) e 飞机的最小速度。 * Z4 J* k6 w- N) J- e速警告系统传输飞机对 ) e' Y" Z. m. K; Z! E' n1 A流的相对角度。 , Z' b* V Y3 k' V. |; ~由一个状况改换到另一个。7 y3 b. P, G5 p1 h' ^ 降场,3 ] V/ ~, U, S" t, S 划时,除了目标机场之外,所选的另一个机. u: B1 f6 K2 Z" z: [( u- r0 ^ o , I. S& n1 \ N9 ]8 P5 q. bm# W( I6 G5 D* |7 Q ALPHA SPEED,; r$ E2 P1 A. l5 p" { ALPHA VANE, A small moveable airfoil on the sid ! f) a$ g. M; w; }the fuselage transm3 j9 N& L$ \0 {, q a 4 Q0 j! ]" L2 {) O' }ALTERNATE, To change from one condition to! Z/ S9 X( p8 y" C) d: n4 H/ _ A * {1 i: X! D6 u% Z2 |flight planning, usually near the destination airport, to be% q( E i: w* O( J, p9 } used when it is desirable to divert from the original 2 C( S) V) q9 `5 L/ mdestination airport. ( s8 N7 E; s, u( w. F空速游标; h/ d) p X1 J6 G 空速表上的可调指标。 8 m, I) O2 @$ _, x# s' K; Q8 Y" X& o k8 k7 |* w& _6 G! {迎角速度,7 a. n8 Y- F% J# ^! k 迎角叶片, 8 z4 b+ _, y5 k/ s2 Q/ I位于机身侧的可动小翼面。为失9 ^& l {2 K: O- H( ]1 B1 X! K* O 交替,: [; i7 Z: g9 T3 }. z' r) J0 r! C, t" s2 _2 H" [制订飞行计. v$ y7 j# u* J+ ]4 t, h9 m0 F' [ 场。通常在目标机场附近,以备不去目标机场时,改降之! D0 n+ Q' i9 U% r4 |8 L2 a* S 用。 ! q$ i$ K6 Z4 h& x1 u英汉对照民用航空词典B OEING 0 F" w+ c7 X8 {; Z* l5 ?1 f# J3 VTECHNICAL DICTIONARY 8 0 u8 ?3 {5 M% d0 A9 F C+ N3 {ALTERNATE AERODROME, An aerodrome to which$ {" F; K( }' Z! p an aircraft may proceed when it becomes either ' B9 V3 f Q( Bpossible or inadvisable to proceed to or land at the ; q& v, L6 s; n9 ~8 H. h$ lerodrome of intended landing. + v0 Y! s$ W" M8 ETER SETTING, The adjustment of the altimeter & ~, o0 g6 M# Y/ j# n) q% Uaccount for local variations in atmospheric pressure.! L7 l0 h1 w* s9 D: Q LTITUDE ACQUIRE, A digital flight control system9 S% O! v) ?; f( i5 {: @+ e7 v6 X ode to transition from climb (or descend) to level flight.) M2 V+ v P! V5 A3 R X1 i LTITUDE ALERT, A flight deck alert occuring when the , i( J/ y! R" J& ^$ p" Airplane approaches or departs a selected altitude. & A# h5 V/ {) g% f) E; _LTITUDE CAPABILITY, The maximum altitude at N+ ~' I/ Q- z& b7 H! { hich the airplane can be flown at for a given thrust,/ |$ _; Y( K' b( L2 h' i" U* ~8 h& H peed and atmosphere condition.) S" \( v8 {6 A% j# q' ~0 L: l LTITUDE HOLD (ALT HOLD), A mode of the autopilot" k, }" }3 G0 ?7 t2 i r flight director to maintain a selected altitude. $ s$ G ?4 f1 I4 R3 Oirplane's altitude during VNAV operation.* T c) o' ~, y; _" U4 V 机场着陆时,可作着陆使用的 7 a' S8 U& N% j% W! T4 s9 T场。 3 p5 Y- A) M4 H* V% b! D4 J! K+ D6 @ 根据当地大气压力变化而对高度表所做的调整。 ; _' z' Y, V1 l2 J9 n) \一种数字式飞行操纵系统,从爬升(或下降)改平的模 & W t! J$ q& w5 L( z7 O" s( k2 }+ Q" I! @- p- u度警告, 0 n4 ]% n' \$ f3 a" Y# f当飞机接近或偏离选定高度时,所出现的驾驶舱警告。 * T( m6 @8 X7 e- Y) v8 a2 i5 @+ J高度能力, k6 I9 |( Z+ }9 O在给定的推力,速度和大气状况下,飞机能飞达的最大% n2 G' V% H( h9 P1 G& J+ S1 @ 高度。4 e) u j6 h% q" w" o7 Q 高度保持(ALT HOLD), ' l7 S! x$ _2 r* i3 a自动驾驶仪或飞行指引仪保持在选定高度的一种方式。$ I9 D& s0 }; S7 \( h0 `6 i! Y4 y" m& P员对飞行高度的控制。 0 d! `/ N. G( Zim , o3 W# q9 ~* N. W/ ]1 ]) Da ' ]; g; r0 ^. R1 U6 ?ALTIME ( I B/ i% P& | B+ K3 qto: G* R. N) r8 i A# I f% ^5 t* h9 X m1 v, e6 K/ [2 j2 }! a! Y( y' s A' v! l+ J* T7 c' c$ g E a7 v9 `, { e/ P; @, t0 e A 2 c% C2 R! r. C4 e5 e1 t. Uw ) d, p% c8 W( w- As" j$ K2 l& T8 h2 L. A! L3 h- w A& u S( Q! c% w' k7 S+ C! i o ) c4 E, S) P' I: {2 fALTITUDE INTERVENTION, Pilot control of the - ?, X0 W4 D) K/ c2 w ?a - L" \% R& m' ]$ SAMBIENT, The surrounding atmosphere. ' O# R( Y: [% s9 W/ d备用机场, 9 m( s6 q" |/ a2 j& N1 ^9 g* j* @ K6 J当不可能或不适宜在预选 ; I6 p; A8 S# i, ^, H) Y5 O" ]/ X6 y6 v _3 O7 q/ g 高度表设定 ^2 r" ]/ f) L! C 高度截获,! a% U6 ^$ M" Z' E% t5 N0 `( P/ c5 G+ P; X# Z5 j5 X9 T7 ^8 r- {. Z x/ \, a6 D# I 高度干预 & C) B3 g# v" u$ F" ~在垂直导航工作过程中,飞行# j1 J- V( F- H, w) k$ u5 U 周围环境(地面气层), s) V3 F) U/ E" I物体周围的环境(特别指大气)。 7 R9 E* t9 I/ x6 W: f' @英汉对照民用航空词典B OEING$ c" q! @% ^* g; y- R' _ TECHNICAL DICTIONARY 9/ W1 ^. c2 S4 z7 e4 P4 ^ AMBIENT PRESSURE, Pressure of air surrounding an 8 q6 h6 |# J' ?( hobject, measured in pounds per square inch (psi) . $ Z5 \! B3 e6 b% n/ MMBIENT TEMPERATURE, Temperature of air 9 L1 d0 \/ m1 Z! l+ H7 g, Wmpere. ; v' s4 I, ?9 _- Gurrent waveform. $ m4 k4 m+ j- U7 n/ ]3 \2 s/ Mg an! z$ ~" A/ x$ }% `% y) K z nalog signal to a digital signal./ e% }+ z$ P* ? e- ] ore inputs p5 r1 z* d d f binary digital information and one output. The output 8 f) o1 H* S! H9 V4 t! o1 only when all of the inputs are 1. The output is 08 X7 \' J8 ~ U9 I' k hen any one or more inputs are 0.- C5 [) h( K& P 面气压),0 z6 q# Y2 ] E/ R" [1 a 境温度, ! h/ {: x( E$ ]3 n/ `# F; @1 X气温度,用摄氏度(°C)或华氏(°F)来9 y6 u% N: z. C* s# @& p* H4 E0 Z- ^% b7 p- Y& t" U( L 电压或电流波形的幅度。- h) G& ], h, K 性变化的信号来工作,或产生连续性变化的信号# ?: Z3 C/ J% _1 R5 b& ^ 统。( Q5 M" T' l( d# X! D 将模拟式信号,转换成数值式。( i3 J) ]* f6 ?7 M 一种有两个或两个以上的二进位数字信息输人,一个输7 Y% B6 g k( I* b 的装置或电路。当所有输人为1,输出为1。当任何一个 1 w9 V, L! K) n5 N一个以上的输人为0时,输出为0。 ( v2 Q8 a# @8 ^" o/ m: { q: r5 h+ Q LA , Z' n& E8 j, Y' ^, d) Msurrounding an object, measured in degrees Celsius8 M& r f) J) [ (°C)or degrees Fahrenheit (°F). 8 i& L! R+ ]. z# EAMPERE, A unit of electrical current. One volt across ' y) H% t( P- lone ohm of resistance causes current flow of one) E4 a3 t3 s8 S9 R4 m- B$ R. [ a : ]8 _# N ^5 RAMPLITUDE, The size or magnitude of a voltage or 1 m h6 f# N% V7 x7 jc $ c/ ~) n6 n aANALOG, Quantities or representations that are$ P8 t1 x. a8 E3 A- S7 T9 W% U% }7 h- P variable over a continuous range.. Y) M* Z& P3 e/ ~ ANALOG-TO-DIGITAL, The process of convertin4 ^7 Y+ }9 h5 E- U6 `' o) ~7 } a' B6 ]9 k0 b, F1 V2 S$ F AND GATE, A device or circuit with two or m ; }. R9 C' n! o# \3 P- f- Fo( {$ f; }$ D1 D$ _ is; @3 K: x. ?7 Z; i# @# o* d2 |9 _2 q6 X w N* } O% [, Q( V; @环境压力(地 2 X% {. G5 {& l- s. R' E: f6 N% u3 e N物体周围的空气压力,用每平方英寸多少磅(psi)来 # E0 Z C9 F# c/ x' y度量。 % I$ t/ m5 e5 M6 }7 j" K7 E9 P& V& k. T0 f7 h q% i物体周围的空9 X* j8 L7 G O! z0 n y& X+ V 度量。 / ^6 O& @6 {" o2 G! c* B. A: O安培, & }; O5 W! L% v* x! c电流的单位。 , M$ \! U, P& a5 O# r* F3 e) `9 y1伏电压在1欧姆的电阻上所产生的电流为% b* n- r g4 |4 U 1安培$ k6 L7 {+ L: O 振幅, $ }$ C Z# E! u# Z* z; C模拟式, 3 P* T. A6 ?, I8 }用连续! [; ~9 {" l' U: T# ^5 S e/ j& S8 J! a2 u% I从模拟式到数字式, 1 f6 z, c0 b% o与门,9 A7 t5 |: g7 l7 {) D/ }0 U4 |3 e( `7 `& |$ k, G4 ^, l4 K4 D: b1 W/ x0 j+ F5 X 英汉对照民用航空词典B OEING/ Y- [9 A7 K( [" x$ q TECHNICAL DICTIONARY 10 1 H8 V% o" k( B B# vANEROID, A sealed flexible device containing air at low l1 @# j, Z) ^# H7 S5 {pressure, which expands or contracts during change of1 ?; Y% @( l1 v- t ressure outside the device. 9 y% f# T0 I: y f! L# h1 D/ }ically# B4 b1 e: j. V+ O6 J. n r changing the direction3 _; \' H" m* O; e3 }) z f drive.$ e! K9 h: T3 Z2 C: r/ b of the wing chord in$ t; }# W% a4 @) t/ d lation to the free stream airflow as it moves forward 6 U( `8 W$ o, r; m* T. mrough the air. 1 N! r! A* g+ i) b$ S- J Fal axis of the 1 ^! f1 x. H$ w% W! T2 H/ Maircraft.6 d; @- E% _% H( n4 x- P$ B 胀或收缩。% l3 C5 A7 P& c% `' W" B 箱。是改变驱动方向的机械装置。5 j+ U) i4 F/ a3 h' Z 机翼翼弦在空气中向前运动时与自由气流之间的夹角。 $ U6 p4 ^4 Z' h9 q Q- ^6 v) j% U5 I; h& G8 e& d+ U4 r p J& x& q' a$ d* f! y+ dANGLE GEARBOX, A part of an engine, mechan . H" s" N d) I0 ddriven by the compressor, which drives the accessory 3 Z& |2 R# n7 W6 b Tgearbox. A mechanical device fo 9 s$ d7 g7 u: T6 e/ K0 l8 S0 g* lo & P: Q8 T+ Z X/ c8 F- d4 YANGLE OF ATTACK, The angle " U0 i, I3 i9 V1 Qre , w3 b) z Q0 vth) x& F6 b9 m. M3 q" b ANGLE OF INCIDENCE, The acute angle which the ( P0 b8 c! {, b7 G! m' Jwing chord makes with the longitudin$ ]7 f8 V- R: }8 q 膜盒,% p3 `) T3 v( l9 F, K 内含低压空气的密封弹性装置。当它周围的压力变化 ; W& P3 K& j, q, f8 b, j( ]* D时,会膨 0 T @# Z5 |) {. t8 e伞齿轮箱,' n4 l. W8 B( J! T 发动机的一部分。被压气机以机械方式驱动,然后驱动" H' D3 Q1 \3 {! B, C; J 附件齿轮! r9 n! h% m! \+ W$ _ 迎角, # P! f: G$ M/ o6 [5 _& {安装角, : D" |/ Y- v+ y* P8 ]3 h飞机的纵轴与机翼弦线所形成的锐角 1 A' ?5 t8 z# ?- C ?英汉对照民用航空词典B OEING ! s4 [" {: p2 M0 ?) [ W, ]TECHNICAL DICTIONARY 11 * v1 [ A# u1 T3 ~! I n' kANNUNCIATIONS, Audio or visual indications used to9 ^+ i1 h' Q9 V6 B2 j C1 { call attention to an event that has taken place.5 j2 x' t+ {% I, d( \ ANNUNCIATOR, A visual device consisting of a number% e ?# c1 p( f- a, N. ~/ K ly. . [+ |6 w# V. m r% W) b8 BANODE, The element toward which the principal stream0 F( @# ~! k0 M* ]$ ]1 K of electrons flows./ g' h' s4 ^$ P% X3 a* x$ E ANOMALY, Not normal. ( z9 J* {( z$ {8 m8 `$ K6 JANTENNA, A device which, used in conjunction with a , i+ b' a) G, Z, R1 atransmitter or receiver, is used for radiating or receiving / L" I C! p/ n8 t- I. j2 U9 Jradio waves.' c) ]3 h7 m2 { \" ` NTI-ICING, A method of preventing ice formation on $ i M- a4 Z: }* Je wing leading edges and engine nacelles.7 P: m) t' T9 D4 q8 O# P' I NTI-SKID, A system for providing maximum braking5 ]0 M& f# m3 t9 B* s0 o# k, E2 m ithout skidding for any runway condition. Anti-skid % Z8 F6 y$ H w' Q8 {omponents are part of the brake system. ^# T f8 h N3 R0 q告, 1 y6 [; W: w8 `6 S& n当发生事件时,以声音或目视指示形成的提示信号。 * p8 N' Z% L! [0 t与之有关的电路的现有情况或已存在的 & ^. I& h. V( t0 X5 v8 O" E: h$ o' q0 {. e9 ~ 正极, }4 v" V9 s7 O 主电子流向的极位。 H0 v& O( l9 @' g( n) x6 ^ 异常,; o L/ `" G( y 不正常。 - ], \, J2 H, N+ j( ]天线,: C0 u1 g @( V) B; W' D9 B 一种与发射机或接收机共同工作来发射或接收无线电6 R4 M: a+ L7 S4 d" V, [7 Y6 x 波的装置。4 {0 b# t) O% P+ l0 h 冰, " w2 g! v$ t5 _0 ?防滑系统,) {5 X5 A; R6 d 一种在任何跑道状况下,都能提供最大的刹车能力而不 6 r( h9 E' J& z使轮胎打滑的系统。防滑部件是刹车系统的一部分。* q9 F7 s! {$ l: u of lights. Each light indicates the condition which exists 5 y' Q4 X/ J# t% r& b, Hor has existed in an associated circuit and is labeled ! U" c5 H+ m) M9 ^$ [0 o- n* c2 paccording ( m/ C3 ?. }! P" YA : D0 S! y+ w" J! K m% \3 M. Q: o) rth; O1 t" q( u9 y" `8 o3 u' \& T" u( J A) u5 c# T- H. e: H) _: v/ Q) b w , k8 W( G& d1 v6 E3 ic & l4 F5 K, Z0 {9 n$ H, r4 G1 h& h2 A$ V- s; q3 _+ n- [ 信号牌, $ d5 P% d }' m% }+ a: s! B# A7 A由一系列指示灯组成的目视装置。每个指示灯都有相应 5 z% `& o% ^8 C" z的标记,用来显示! M+ v Y# k' A$ _% i4 V, e( r N/ @, O0 j3 G) `9 Z3 I6 T) Y' o2 `6 j+ y" M防止机翼前沿和发动机短舱结冰的一种方法。) s5 Z' f7 ?7 E( H 英汉对照民用航空词典B OEING ' L3 J/ [- ?2 l, Z" f rTECHNICAL DICTIONARY 12 " B1 Y/ I, @4 F4 B0 M. zAPPENDIX, A supplement to the Airplane Flight Manual; ^1 ~4 s# k0 k' u- U* B tained in the basic manual. A$ H; x+ n4 T a( k) Q ollection of supplementary material at the end of a + t. N1 @, o$ Q J: Wook./ p5 `3 _' R) | of the C9 V$ S/ l5 j4 L8 p* b rsion link on the landing gear. ! H% h$ h9 s7 ^APPROACH MODE, An autopilot/flight director mode ' k# ^1 w# ~1 X* G9 w0 l3 G- Fwhich is a combination of localizer for roll control and 7 S/ W$ R0 j, ~5 w/ u8 {glide slope for pitch control. This mode is used when full7 Q1 @3 O4 A& h( ` instrument landing system is available.* m( \( J" B8 k. o% l9 j APU, SEE - AUXILIARY POWER UNIT( ]2 r( S$ j! s6 G; f% T6 m ARINC, SEE - AERONAUTICAL RADIO. k* {/ S; F; |3 g INCORPORATED- z5 l# v7 e8 T. h4 R ARM, To make ready for operation.$ j* h* U X8 d. v- D# v* Y [% H 附录,. T1 P1 l7 R6 x9 | 飞机飞行手册的附件,包含基本手册中未提到的飞机形 ( }2 Y5 ^6 c* u9 g态的其他性能。是附在手册末的补充材料。 + d" P* ]3 _% P# ?9 ]顶销,2 Z3 H* W- o6 e2 s 用于连接起落架扭力臂两部份的销子。 5 T3 M/ S8 m7 w2 [; B8 c- [进近方式,4 U2 q+ ]7 |" g1 Z" a0 L4 K 一种综合了控制横侧的航道信号和控制俯仰下滑信号 ; g. f% X$ O& [* V; K4 I的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系 / ^! x8 p' C/ R/ K5 g B% t0 [- }统正常时才使用。: x8 z J! T% U7 Q- X& u 辅助动力装置," T8 w9 z0 M( B0 E' B 见Auxiliary Power Unit: M+ U0 w& M. a( p containing additional performance for aircraft3 F0 X V; x5 {7 O# [) x0 q configurations not con4 o# t! k- i+ {) t c0 S$ r! M8 w/ q4 R+ W6 q" [2 @7 ^ b " \8 {2 D% [, @/ x" x; |* {" v' @APEX PIN, A pin for joining the two sections- W* I2 t! Q- Q* p to) S7 A/ H( t8 r5 u [) x7 t& w' t6 s3 P% p7 r' q3 J& r; F7 {' v, y' l 航空无线电公司, # w: \* B9 }. \) d3 r% R见Aeronautical Radio Incorporated.8 a2 Y$ O Q# A* h" u4 X, M 预位,8 F- {- ]5 c( @; ] 部件可以开始工作的状态。 / P1 W9 J6 Q2 ] }英汉对照民用航空词典B OEING; c! d4 j/ u; c- W TECHNICAL DICTIONARY 13% V: d$ y% f2 t. h! `3 ^ ARC, The curved track over the ground of an aircraft ' D; I4 } w7 G5 D D# Bflying at a constant distance from a measuring+ M4 s0 M$ E3 H+ E' U5 m equipment (DME). ! t, S/ I3 n# E% _$ e2 cin the limits of self-contained system3 x* `/ R% T0 z7 h% L apability. + w* B& u' E( I/ k: Z' Q1 utem for opposing or restricting3 p/ C& U- A0 F( E, |- m ovement.4 d) I5 b0 I* I7 s1 z/ L/ Y7 T SPIRATED TAT PROBE, A sensor that measures total 3 H; v! ]5 Y+ F, J6 c3 u7 Y' X9 X% `1 Xir temperature when the airplane is in the air and that# v4 ]9 l4 Z" E3 U$ @ easures outside air temperature when the airplane is& ~) \( _" T8 E* ]. ~2 J* h n the ground. The outside air temperature is measured& U/ b' p( P" l: C7 {# _- E SSEMBLY, The fitting together of a complete structure 3 J3 \7 |. U; Z' PSSUMED TEMPERATURE REDUCED THRUST, The; a+ r$ L7 C; p! S' D7 t' N ATC, SEE - AIR TRAFFIC CONTROL . I1 f8 W J. c& S' `% A* ^; k v 系统中所产生的一种用以抗拒 * T) O3 w7 ~" O- p, f1 S0 ]& V0 V作或限制动作的力。 1 k, F% {5 L' ~( |头,* Q/ \, @/ w8 F 用来测量飞机在空中时的总大气温度和在地面时的外0 t. a6 z$ Y- O1 ]$ X2 I$ d 温度。地面外界温度的测量是利用引气将外界空气吸入 1 M$ Q6 m8 @. o% I头,以达到测量的目的。 3 Z y% V' [) K) K: {配,+ k. m$ ^2 p9 C# I9 o 一个完整的结构或组件的过程。 ' l* ?; K. e$ K) u8 h假设温度而得的减推力, 0 T1 f3 W N0 l* X+ Z5 ~0 U推力设定值时,假定一个比实际外界空气温 ) \0 f. h' [9 {2 C空中交通管制,. b0 B( r, y. ^- b3 H& t* X 见Air Traffic Control9 @" M# Q) X8 @; L7 D AREA NAVIGATION/RNAV, A method of navigation: s2 ^. a7 q7 S6 O. S that permits aircraft operations on any desired course % W4 a1 o- s! _0 a' n" Nwithin the coverage of station-referenced navigation; q$ _3 N; G H' F z f9 t* ?3 C signals or with 7 W# R/ F$ U! W* r) Tc* d) V7 |( B" V! o+ r0 z! a ARTIFICIAL FEEL, A force developed in the flight, Q% f$ G' B m+ j7 z control or brake sys; \4 \' ]. n9 M7 f) X0 a! B2 Q/ D0 f m & ^' K- \7 @7 `A % |6 ?7 {+ c/ ua# C& @, k; f) g1 m m5 d; F! `# j L o6 m, D' l6 c v9 o( J( ~/ s8 U8 _( F1 Z by using bleed air to draw ambient air through the. s' g/ [ G8 E+ H# k' y w) g! \ sensor when the airplane is not moving.4 Z& B( U; s1 ] A ( S( W w6 I# W/ h& ~2 c' wor unit.! S' l5 C# b* ?; M0 ~7 g0 D+ d8 V A/ t- l9 j4 E) P: k* ]; v% `; ^ lower thrust obtained by setting a higher than actual 6 f: F+ r# m" ]6 H% zOutside Air Temperature (OAT).7 m% ~: B* N; W0 X' w4 Q$ Z 弧线,& @2 N6 D5 Q. K2 v! x 飞机在围绕DME台等距飞行时的弧形航迹。( p) G+ w+ I" C6 g5 A7 b$ N8 { 区域导航, + T {; S& Q$ l# x' C |容许飞机飞行在有电台参考的导航信号或自备系统能 + [4 @; L% s5 h, G力极限范围内,飞行任何预定航线的一种导航方法。 # B1 B) C9 N) N+ [, Q模拟感觉 2 ]1 C: [) L) N9 p# U! y/ F在飞行操纵系统或刹车 : o1 Y; D# v# _ o, c4 v0 ~; V. |# v3 n% U/ B吸气式总温探" P, V1 r9 y* j+ V9 ]& s* L" j8 r* ~0 w# J2 q1 v0 E1 g% E- C. _; {. P/ S5 J7 J1 w" E! `5 E组合成 8 i# i/ x$ ]* e" ~9 D' F+ g' d) X! ? Q 在选择起飞 0 r. p+ T# {- B( T度高的温度而得到的推力。用这种方法可以减少发动机的 . I' }- }- o" {9 L# \& U2 ^- V磨损和维护费用。 % G7 W/ p: H0 C+ S: D ]# |" H+ _6 ~# j; w* ~英汉对照民用航空词典B OEING X4 `9 p- j& t& KTECHNICAL DICTIONARY 14/ i2 C0 J. H- ~) l ATE, SEE - AUTOMATIC TEST EQUIPMENT # ~$ @$ |0 _ gATMOSPHERIC PRESSURE, Pressure of air due to the 2 g& ?+ z$ I$ {9 p4 m" Zarth's atmosphere, expressed in pounds per square & B2 [" _) |2 v: P6 dch (psi) or inches of mercury (in Hg) or millibars (mB).2 h- a8 \. w. P( ~6 V6 f TTITUDE, The relative orientation of the airplane with. j. X/ }+ u4 T( X1 U0 e spect to pitch, roll, and yaw.# S- O; j b# u UDIO CONTROUSELECTOR PANEL, The panel in4 z' w0 y8 ~2 s- C# g4 E; r& z) x e airplane which controls and selects the routing of# B! K' d+ o. g, B udio.1 x# [9 B# A9 ^4 P2 T8 L: p+ J UTOLAND, Automatic landing using the Digital Flight ; G/ u6 T$ t" ?7 ~! f ~( }ontrol System.7 V& f6 m' E. B" a n.: J0 C2 ^& ]* [, g M, A system( G. f+ m$ w- T2 d" C2 ]' t1 X omposed of all necessary subsystems needed to guide ; [: [8 i- M. ge flight of an airplane.! e; |: e3 i# f; V: Q# D* L! s EQUIPMENT, System test; z, k, Q6 A1 D; a6 b# H, G/ ]/ h quipment that operates under computer control./ V' ]5 M8 g- q, g 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 , z5 h/ B1 q( z# {1 K/ zin ) x" a* ^, g- ^8 u2 T! U: m/ ?A4 h& H. [, E P9 M re, h" B' Q n4 C5 G7 J- m' \ A & h2 J3 l: y) }# Lth - v. w1 c! I7 y- ya8 X* ]6 G1 ~ e, L A; B5 ]% s0 a: k C 2 b: l% ]( I( J! W; }% M5 w1 |& @6 fAUTOMATIC DIRECTION FINDER, A system which ) x, l5 y4 I- R! tdetermines the direction of a radio statio & W, G0 b" F9 s9 I" [6 dAUTOMATIC FLIGHT CONTROL SYSTE6 L( z0 f8 n8 Q5 i c 5 E& M0 L! M1 C& {' @/ ~th " f4 Z, c# v0 `6 |AUTOMATIC TEST / s/ B* V$ \9 re! T7 E. o' O/ a; r& h0 v& M$ ^9 B 自动测试8 y, K& I% Q$ G6 C; M7 d 见Automatic Test Equipment.1 E( h. U# P/ t$ b( h 大气压力, 0 j7 b% J( o( a1 @/ {/ `. S* c: K% Q由于地球周围的大气而产生的空气压力,以每平方寸多8 Z% c$ W, B+ M* e! s- s X' g) o2 A 磅(psi)或多少寸高水银柱(in Hg)或毫巴(mB)来 6 l# d5 }; n8 o) p6 H示。 5 `# C( i( o3 k- F& ^飞机姿态,8 Y) `, H$ }+ U; L2 X 飞机与俯仰,坡度,和偏航有关的相对方向。 - F7 S2 \2 [/ s$ y2 ^, h/ ` d音频选择面板,' i7 h/ T+ Z" C; K- A 飞机内用来控制和选择音频通路的面板。 + L) f6 {4 O: v6 |自动着陆, ) Q5 H* X8 ?, u, m5 x$ Q使用数字式飞行操作系统来进行自动着陆。 6 r0 Y; y6 k; G+ {. e% H' z的系统。 ! G0 C' t3 V" w: l/ A: F- P- f) r% q3 k# Z 系统所组成的一个系统。 % K' x3 \( u) i在计算机控制下运作的系统测试装置。3 {5 B) q1 j1 ^: w, P: r( i4 l# \% C3 F! E0 T s自动定向仪(ADF), 3 {0 a9 E3 R) r$ h确定无线电台方向 ' x9 \9 w w6 p" q* U" n自动飞行控制系统 4 l* Z+ q$ _: `5 S由所有能引导飞机飞行的子' d! t1 [: W; |; v1 r! y. v 自动测试装置, 2 d2 M( j$ [4 f/ A2 G& U英汉对照民用航空词典B OEING( H2 A1 ^, @) b0 c3 p. H- n TECHNICAL DICTIONARY 15 * a" E8 U8 _' j r; ?8 s# A4 `AUTOPILOT, A system which automatically controls1 Q0 ^8 @; O; f0 a' O- n and guides the flight of an airplane. . F" I) v* e6 V2 i! _6 S0 E+ ?AUTOPILOT FLIGHT DIRECTOR SYSTEM, An 5 o+ Y, C. T$ I! [. t& S/ Gtor: t5 C- n# y8 w, v5 B' @5 A4 v UTOTHROTTLE, A system which automatically 9 @5 F& h& W' h( A8 W* q& Tontrols the throttles of an airplane.; v9 A Q9 x% _3 i( A POWER UNIT, A small turbine engine in . X2 V7 Y, |* O- De airplane for supplying electrical and pneumatic3 s; ^, p7 I# i: {" c ower for systems operation on the ground or in flight. , g3 [' C9 Q% v. t" UVM, SEE - AIRBORNE VIBRATION MONITOR 3 Q; e3 G9 Q$ i3 _5 nXIAL FLOW COMPRESSOR, A type of compressor. E" J6 S- O2 Y! g; j sed in a gas turbine engine in which air passes through$ a) G2 N, e4 G$ k XIS, An imaginary straight line or an actual physical2 I9 s2 h9 f5 l/ y; |' r Y8 r5 l, i- n omponent (such as an axle) around which a body can# J* X- V* L1 j" f0 H# I tate.: ^( i8 E( a( ?( [6 S C 仪,( h B5 P( W- J" \ B* M# J% B( b- f Q 自动驾驶飞行指引系统,; n1 K' l* \' h7 Y 动驾驶和飞行指引功能的系统。 K0 |. d4 ]0 Y. R1 C9 e9 T4 D' [ 动油门,- ^. A9 |% [' V) f n 自动控制飞机油门的系统。- J. A( H& j* W 是飞机内的小涡轮发动机,在地面或空中给各系统提供 ! V: G8 Q1 F; e: M) ~源和气源。) f* K8 D4 @0 `2 f! l 称。9 U, b7 r6 ~$ y9 [) s B) Z 载振动监视器,) ?* ]& `( ^& R$ r- T0 \ 见Airborne Vibration Monitor6 k# j A _! j& ?0 |* R integrated system containing autopilot and flight direc9 n( E( _, e$ m! r8 P, L functions. * i( ]. d% c& j3 r( S4 u" iA" \1 z; b! ^1 n+ O3 W c ' f8 w ]' N6 T& v, n& C3 u' A/ SAUXILIARY - p {; O" ?) n7 z$ a+ }- jth A1 l5 p7 }& d# S' z p , {* a* V( b4 IAVIONICS, An acronym designating the field of aviation 7 Z0 F1 Y2 Z8 H9 s, v8 @+ aelectronics. + \6 i K) J1 c: V7 YA }: F+ v" b- \ A+ y- U% H1 K8 } f u ( E! Z/ a- r8 G5 M$ w! Rthe compressor in a straight flow, front to rear. 3 d9 q3 H. X1 v# [A - q& _) K9 D; jc: |; Q; m D# k: B7 T9 B1 d ro % |3 F8 b' K2 `自动驾驶 ( f1 h' t$ a7 ?' d. M/ G动操纵和引导飞机飞行的系统。 , O' ~1 q6 N% K+ J& Y一个综合自; O) j) n0 @3 N9 K! T' E- y, S' V) Y2 s; V辅助动力装置, 7 F8 Z5 v1 j0 k; q- g' E6 z1 f* h9 t$ k7 _0 B& T% f& j' k航空电子学,$ b$ w" C4 K' U& \0 f 是航空电子领域的一特有名 . Q$ Z4 W. o; d4 s2 d9 Q7 f, v: ?# R; Y) h# J( v$ s9 y, K3 o {" H 流压缩机, % i u5 @1 t% a3 \$ V一种用于燃气涡轮发动机内的压气机。空气由发动机的 / h- S( w% L$ n; G- d部流出。 9 i% V! j! D. T线, 6 Q# Z6 m+ h. C% m, C k, C可让物体围绕着作旋转运动的一个想像的直线或实际 ) @ t* ] s6 f在的部件(如轴)。# K3 E# u4 G e0 e% ^- x [$ h) {$ j 前部轴向流人,压缩后,由后$ Y* Y0 G" _8 |2 i1 c8 [+ u& V4 I+ P) T1 ]( ~2 y) ]2 e2 [" Z5 e1 w2 j: l 英汉对照民用航空词典B OEING [/ d4 k% O( C, c1 s5 l! w2 j TECHNICAL DICTIONARY 166 P u. b; K$ i6 X B % D( e: g( l P$ W4 w4 EACKCOURSE APPROACH, An approach to a runway' p0 c5 a0 g. M versed. ( K9 v [, s! vown on the EFIS that . p0 {3 J2 m2 }# Goes not readily change, for example, navigational aids. ) G% J3 k! ~; `, @vement in the tank or reservoir. / S3 v% k/ X! C/ w2 KALANCE TAB, A small hinged moveable part on the; y8 ~' s8 R- a7 U ailing edge of a control surface (aileron, elevator, 1 }' B a! q8 j- _' [% H航道进近, h8 r4 P; `* l8 e- y 相反的进近方向。当反航道进近时,无下滑% F! K, ?( @$ p0 r, R 显示在电子飞行仪表系统上不经常改变的数据。例如:5 g6 T) }4 Q% o 航设备。 ~3 ]3 T; t7 [, c 在燃油箱或滑油箱内阻止液体流动的隔板。5 ~8 S: Y. N& J7 R! d 动补偿片,) z, _; d/ m3 {3 j' A 铰接在操纵面后缘(副翼,方向舵,升降舵)的可动部。 / b: L0 b& q) E$ X: x与操纵面相反,以帮助操纵面运& I" |0 \8 n8 g |) d2 H B) A: m# P$ i6 w7 j* p% F% R which is opposite the normal approach. For a ; ?; v, x* i7 ]backcourse approach, glide slope signals are not + \" u: O( G j2 E: @& Yavailable and the sense of localizer signals must be5 b8 z; H- |& U re6 E' [& T$ X* n O- Y9 s9 L BACKGROUND DATA, Data sh 9 `$ K9 e0 h8 o$ d" F" F+ Y8 zd- b1 c' L; K, [. s! B/ t( S BAFFLE, A partition in a tank or reservoir to prevent - @ U1 _2 ~& d# Xfluid mo : L ~- }3 t' Q2 u% u0 h) d4 }B% `& x9 v7 b6 x0 X' O) W tr; q+ H! l9 S6 j: ]5 z+ f, M% ` rudder).The tab moves in an opposite direction to the * B8 a# X' d7 U9 ?control surface for assisting movement of the control+ w) I- z7 y; @ surface.% g) \, R, n/ ]8 K( E/ Q: \% _- C) e4 q! n, u" Y 与正常进近2 O# C6 S' d7 d; e4 o 道信号并且航道信号也必须逆反。& j/ `. D- D M+ t+ O 背景数据, 6 k' V) ]$ K5 h& L5 [# e5 x6 G5 `% n; Z" g/ r, N! l 缓冲隔板,$ x) c; |3 h" g" t1 U& L; a2 j/ i( B7 N/ q0 U: J. | 随动补偿片的动作方向, _9 M8 d7 w, [' a; l7 B: [8 @ 动,减小操纵力。4 _$ g. U# ]1 H, q# q& U 英汉对照民用航空词典B OEING 3 V% F* Y! K W$ r; Y. TTECHNICAL DICTIONARY 171 \ P- O u5 J7 G- n BALANCED FIELD LENGTH, The field length( G" B3 C s& U& [8 i associated with optimum aircraft performance when - }9 T+ q% ~# z2 A/ H' r& Lbstacles are not a constraint. In this case, after engine% k+ Q: R9 h& t$ d0 F9 | ilure at V1, the distance required to accelerate, takeoff Q0 r0 t# W& N: X, d' Qnd reach a height of 35 feet is equal to the distance : N( R8 a% r* C* |8 q9 MALLAST, A weight installed in an aircraft to maintain . t0 E1 B$ f, y1 ?# W& J' f. v8 bALL NUT, A fixed spherical nut driven by the $ M* M3 u$ F1 O& Z4 e( PAR OUT OF VIEW, A signal used to remove the flight2 v1 @' S$ B( z& R/ Z AROMETRIC PRESSURE, The pressure of air above3 F# R I! F; B& C g) or% F& p; k& C5 y3 ]" H9 _, @% W millibars (MB).6 H& H! M2 R- h8 T ATTERY, An electrical device for changing stored , y: A0 ]8 Q5 ]; D4 S性能的场长。在此; h& S9 J0 {; A6 ~ 况下,V1时发动机故障,要完成加速、起飞、离地35 ( j4 J7 n: k% E# P O5 r尺所需距离等于相同速度下完成全停所需的距离。 - I0 |8 m: @0 p m6 c2 W4 c0 c舱物, 2 ^3 E8 Q0 l9 | m" l重心在许可范围内面装载的配重物。 / G" {$ ~: O/ _' g, d8 _; l形螺母, . V ?+ V2 n2 a! M的固定的球形螺母,用以使襟翼和水平 G; L$ f9 [! W; }( @; p3 W0 U+ b 引杆消失, ; W+ G: N4 ~# Y指引杆的信号。 # ?) r N. l O4 G% g/ _0 m q4 H压,. J; z2 _3 |' O9 I* ^2 w 压力。通常以多少寸高水银柱(in& U& x/ P; K% Z2 J: R" j3 \+ ` 瓶,9 O6 q( r* ^! U/ Q# {9 r6 ] 的化学能转变为直流电的电气装置。 5 S$ l- x% Q( jo: ~; d; m/ j) |" W fa % b- @* m7 g( E4 f" F1 C0 A. L& j, ]" \a7 y( e5 d: E3 h0 v5 y' q required to stop from the same speed.2 T; e$ R3 O3 r& ~4 c B5 _% Z: L- M( |- ]6 t* n the center of gravity within allowable limits. ; a& Z& K; {2 {' n3 G xB6 ~$ K, m0 `5 T- F' M# U* b# q; i$ e' k jackscrew for flap and stabilizer movement. 2 J4 A9 E: a/ v z; i% G" ] K, QB 2 H7 G+ R7 Z9 c i4 q7 e% sdirector command bar(s). 8 V& S) a: z* t: i& @$ O8 vB 8 ?2 h5 F. i9 Tzero pressure measured in inches of mercury (in H6 ?; ~) P2 L; @: P9 G0 A- @: W in1 j6 N" w1 \& I* O BASE METAL, The underlining metal to which alloying / }# ?# r' I0 I4 q. e( ragents or metals are added.+ P' ], p0 P) [/ l. t B0 F- w3 v7 T4 U7 p% c0 v7 M chemical energy into direct electric current.' `7 v0 B3 m4 O2 s 平衡场长, ) T& W' L5 j0 N当障碍物非限制因素使飞机达到最佳! g( y( t' }) Q9 K8 K8 N, [! }, T( N8 F( N) K) p8 W9 l, d- n$ C$ e: K; \ V! G6 b# h2 Y' T% C) ~# }2 X, _! F. b" q% S 为保持飞机& W1 ?1 q) ?# Q4 R4 D( S% `0 t; [8 S. G. Q$ }8 R% ^" _, u/ a由粗重螺杆驱动 ) K j0 z; G" ^2 w( [1 F% I( I安定面运动。! w' Z( y1 K2 Y6 U) J& H5 V% B: C$ k: ^" I用于除去飞行 ; j3 T7 Y/ T2 }" R- D% h% E' w' f( U3 t0 X零压力以上的空气4 a" y: ~' [* e) ?& A# G Hg)或毫巴(MB)来表示。& A% ?5 `3 D# V7 ` 基底金属,( k5 `* w0 g; n4 K0 Q 指合金中的主要金属成份。 1 x- k) {: p/ L2 \: N' U0 _# I$ s. U6 n5 X, q8 \# D6 Q# U 将储蓄 B# M& E4 V2 I+ J: S s' \0 y英汉对照民用航空词典B OEING+ {/ s% ~. n! K6 V$ R. M3 W H TECHNICAL DICTIONARY 18 7 S9 ~& V4 f/ @( l7 ABATTER ; s3 D* l1 B# I* k7 Udirect cu& K$ O0 Y d `" ^2 D9 Q4 w power su ! F/ V T0 L ]* z( a. Y) Z* OY BUS, An electrical conductor supplied with+ \3 D* t3 y8 V/ C) o! e) U( b rrent from the battery or transformer-rectifier for 4 n0 K' u/ u* q! lpply to operating components.# B! r. a! S' |2 { CHARGER, An electrical device supplied3 n. T" f" X1 x. u0 \8 R ith alternating current, which produces a direct current : F* C# a! ]1 o4 H$ [: Output for charging the battery on the airplane. 4 s4 ?1 g& m* t6 y Z: l, v! wAY, A compartment in the airplane structure.5 u; W8 ^. U6 r6 ~ CD, SEE - BINARY CODED DECIMAL: z6 M& a3 S- v" K6 H) a& i EACON, A device which emits a signal for use as a : K* I# B* E, f! _uidance or warning aid. % K! J4 W7 T5 g% K2 y) uBEARING (NO. 2), The direction from an airplane to a4 W) }6 z1 K6 a- \) m# d4 z/ @ ground station.2 t: i, X4 [+ Q. I 瓶汇流条,5 Z: e) j+ s; J: B6 J 将从电瓶或变压整流器来的直流电供给工作部件的导 & W1 ~' _# v! ]% o' z* i体。( Q, h8 B* j; T! ^ 瓶充电器,) Y: }' \, c! I: v9 v: E# z1 I6 x 用交流电向飞机内电瓶充电的电气装置。带有交流电的 _+ }6 g1 b) q: C' ` 气装置,该装置产生直流电向飞机上的电瓶充电。 9 W d' x4 r2 L s5 u( T! B# K9 X舱,8 h1 x( O. A6 ]* e7 `$ W) X 飞机结构中分隔的空间。$ r4 t% s' G2 M9 A3 \: b 二进制编码, & ^$ M8 `" K+ J# Q7 p见Binary Coded Decimal ) B8 S9 ~& ^" ^5 R2 j$ g" UBATTERY . R* `% u- h) H7 rw # O" Z; |) U; C, z' E9 ?+ g! Xo0 p- R S0 H- y/ d2 P: R+ i2 E B - n# n( ^6 l/ R8 l: |B . O, z: F4 B3 U$ zB # i* V. E7 N0 }3 r2 Fg. P' d- L; d5 o; N) R& B BEARING (NO. 1), A surface that supports a moving - k) o9 r3 G' T2 p0 s+ Hpart and reduces friction between the two.& D! t F7 d. T* g& o6 ]; f: {$ e- Z& C/ ]/ P' M5 B6 \: O+ Q1 V3 W) F. f/ J/ m, Y" r6 F4 y: s4 T9 \9 p! n% [2 K/ ~ t; o) `+ v( H4 X/ P& A3 ~% g' l6 V/ ~$ H/ g$ E: u" n+ R8 `* f4 u信标,5 f5 O$ p! J, D; n/ S 发射引导或警告用信号的装置。8 {. |* G7 Y) l R 方位(NO.2),' v! n% K6 j. n8 C. [ 从一架飞机到地面台的方向。 8 m: I6 f- M4 f" @; d- M. a轴承(NO.1),1 `" e, f) b- M- S" A; D6 d- h% B 用于减轻机械转动磨擦的机械装置。1 c' F- ?& o9 S g 英汉对照民用航空词典B OEING' G) U& I% r& R TECHNICAL DICTIONARY 19 0 X! }6 j* v3 \3 ~BELLCRANK, A double lever in the control syst " H& T* Y0 x8 z+ M* |) O4 Ychanging direction of motion. & {4 f( L5 U1 B* F$ mem for, C( N9 L0 z- v$ q, J ct in the : e, w% G3 {6 x4 y6 fneumatic system for absorbing expansion of duct due: R. Z! ]3 U7 N) b: ] heat.2 Q( B: y% `8 z L ELLOWS (NO. 2), Corrugated folded or pleated 4 X: T* \+ K4 y a9 _+ }ontainer or compartment used to measure pressure.8 ~- y9 W- l% {" a5 G EZEL, The part of an instrument case for locking the- g F) D0 o6 _+ H lass. ' y5 x1 E. j- B) D; ~IAS, The potential difference applied between two ) p& ~/ J) Y0 U& Q$ noints for controlling a circuit.2 r7 [3 z6 R2 f8 U& h% T BILGE, The lowest part of an aircraft fuselage. A place4 b& p& g# T( D: b; H: F where water, dirt and other contaminants collect.6 s! O7 _+ t& C7 X8 f 气源系统内提供管道热胀冷缩所需要的余地的波状7 ?, L( v' O% i 轫管。& S+ [( @2 F( W5 d. B 空膜盒, " a+ R* x5 E3 j0 U, _/ l. e一种具有波状表面的容器。用于量测气压。 0 L. l9 y: [5 y7 y0 m嵌沟缘,7 e2 ?9 K4 p! T9 m5 ], P( T* v5 W 将表面玻璃固定在仪表上的圈状零件。 + B. R1 y) E# ]9 V% @: ^0 d压,* R7 t+ a2 v8 z 在控制电路的两点之间的电位差。2 y) X$ U# d/ Z+ P& N. L4 U# l 机身腹部,- Z1 x: y. y0 J3 A6 l" ` 机身的最底部,通常水,脏物,和其他外来物集存于此。 6 K; p( F, N/ a4 e$ }" B$ `6 JBELLOWS (NO. 1), A corrugated flexible du& Z; G: G, j/ R3 B p6 {) \$ G! f5 @6 s3 G to! h1 `* `: X& j! }4 } B 6 y: z# K1 Z/ ^) T: @9 u- Kc / u* H8 v0 }. A+ g2 {9 oB$ U/ I8 ~$ W, }6 V" D g # A/ D3 T c/ {2 m; v9 AB# N( v& q; b5 I6 n1 g" c F+ w3 _, D p 7 b8 g3 S; L+ x3 Y# K: E" k直角摇臂, " O( k: x4 a+ `9 O, j5 b在操纵系统中改变运动方向用的双臂摇臂。 6 T- _; E0 r9 Z, A' e波纹管,/ ~* _- y9 _% E" D$ n1 ~, l% w6 J; T: ]0 I4 c1 f4 |: I% r5 i8 i9 _- A) l* a8 I2 t: d) K; R4 o, h% M) Z9 G( S o$ n5 G- `2 `英汉对照民用航空词典B OEING : B, f N- z4 T& @4 l, s' D9 FTECHNICAL DICTIONARY 20 ! d2 J: F1 ]- a! gBINARY CODED DECIMAL, A system of coding each ) q9 S+ H% O) n, z [1 q+ L2 adigit in a decimal number using the binary equivalent.6 I3 M% q$ a7 p i BINARY NUMBER SYSTEM, A number system using( z3 |, T& a7 }* z1 W s 8 R6 m9 y2 f9 N; t0 s4 {) m' mIT, In the binary number system, the smallest unit of " x1 J6 ^# }/ m) nformation, consisting of a 0 or a 1., V8 y2 ]) c" g- M5 N# I ITE, SEE - BUILT-IN TEST EQUIPMENT " \2 P* X) ?- z e& I* J3 DLANK DISPLAY, A display that does not have any" m' ?9 u& X1 `( e dications, normally due to failure. : \, ], g7 {8 v' s" ILACK BOX, A container for electronic circuits to record , v8 }+ n5 n/ R) X- k: k" o! Yight data.% A: T# U9 s( f' y, }4 ~8 z7 I. G2 S LEED AIR, Air taken from the engine to power various $ ~1 f: p# B. P- c! I) eircraft accessories.2 B. h9 b j, K; S0 E" Y A valve in the pneumatic system for air " @2 y! Q6 g- S) G9 @7 G' @/ _supply from the engine or auxiliary power unit to the1 q1 ?8 y) |/ f/ t- U0 d: y7 ]7 S pneumatic manifold. A valve on the engine for reducing M, u' G7 Q$ v% f7 i A) w pressure in the compressor section. 7 o* X' f: `' a$ U G进制, 8 _3 x* M2 _5 Q+ K3 O进制, & s+ ]' ^, X& i9 {9 ~一般用0和1)和2为底的数字系统。 ' K7 l0 O+ T5 g& u% D特(二进位数),* o8 _( O0 t; V+ y 二进制中的最小信息单位,包括0或1。 ' R/ h! U# K8 W) |" W3 K4 b内自测系统, ; ^: t; X# X& P+ S见Built-in Test Equipment* u5 n; A% s, i$ j$ U- @. J two symbols (usually denoted 0 and 1) and having 2 a0 h3 _7 s. y- {% a7 m1 o its base.$ ]1 [" L0 t, {4 D B ( N9 m& f1 E8 |4 u9 B+ fin ' p6 S1 I, w, o/ UB4 D6 w( J/ e/ V [ B 2 c! P* u& k; F2 d6 din - ~6 n/ J- ~1 j/ N' t1 V! D/ L! f; NB) t! |, P1 x* p fl; d' m1 |, x# O( y B6 z! h' m6 c' n' J- @$ e0 b a: F9 Q* g8 D8 x$ H+ V2 g, q- b BLEED VALVE, 3 _0 q& O( d* h G+ E- f1 H8 [二进制编码的十! V w7 ^' Y' o# l4 I- { 一种编码系统。用等效二进制位数编译十进位数的每一 ' u" s# r% Y( F& `& [位。 ; b" W; z* z, _; e& e+ Y+ ?+ E* W4 K. x' n/ R% v8 W* Z以两个符号(2 l4 J! I m" U4 G" [# ]# Y* g( q0 k! L* S# U b3 k' h: H& P, l$ ^! C% e8 R- M0 I( I! n.6 } N! T4 W: C( z, C 白显示,3 S. o3 @6 p+ ~6 ^ 通常因故障而造成的显示器上没有任何指示。* D# J [2 ], @; \4 Q& I 匣子, ! a! J7 `+ M+ e, F# R装有用于记录飞行数据的电路系统的容器。 7 `8 v$ X" Y! M气,. j4 _& ?7 n, B6 \ O% o 取自发动机而用以驱动飞机上之各种附件的空气。 - T8 }& |3 G$ A; d气源系统内,使来自发动机或辅助动力装置的空气进人0 C$ S3 U" S1 c+ u 气源支管的活门。发动机上,用来降低压气机压力的活门。 3 H7 u0 a+ @; _9 S, i* m9 ~, b. k6 `% o7 i! ]4 `! Y5 O o) i! |8 t" e, m. v* X) B 引气活门, & ^# U6 v. R9 k& D/ c; X' F; i" ?英汉对照民用航空词典B OEING. I* |# u+ f; ?4 U: U ^0 D TECHNICAL DICTIONARY 21( |6 |; T' K: ]( e* }: O. G BLOCKER DOOR, A device on the engine for blocking 2 o# [* K8 O: C! J" n; Y( Ythe normal airflow during thrust reverser operation.6 z' k/ B8 R/ o n) c* v4 M- @: { LOWER, An electrically operated fan for circulating air. ?7 P# A% Y. S/ J% e9 t LOWOUT PANEL, A panel in the structure between2 m; m9 P# @* Q/ w% T) o: K o compartments that opens to equalize pressure in 1 p- S! D# ^& N: C& e+ Ae compartments.# |' y# C/ v& ?* }1 L ODY GEAR, The landing gear attached to the / S/ ^7 s; m# h( Z7 w, E; Agrounding., g) T# ^( r5 x- @ 正常的 9 n' D* _, F2 j/ P Z7 p( }气流。4 L1 `* |# R( q9 E 鼓风机, 4 H- p) L+ j/ ^1 n8 J) k用来使空气循环的电动风扇。& j8 o. A3 W; F# d* } 压口盖,1 q( H" o# Y$ g* [7 @# P0 h0 B 两个隔舱之间的口盖,打开后可使两舱压力相等。 4 L: ~- i9 p" _; V$ T3 S身起落架, : e. g. R" [. [5 d8 z9 M% n0 Z& k( o身构架上的起落架。* t; ~& g' y, h/ y B 6 p. _$ t: o* H: Q" y# {5 NB6 Y- U1 |$ |, a" L5 S% C1 p tw * \# l1 W2 O2 t4 ~' O, Eth 5 R; \+ c" }$ p, `B 0 H0 v1 [( V! ?2 `2 Pfuselage structure.$ Y) W3 E4 l# p3 I+ {- o, B BONDING JUMPER, An electrical connection between 2 Y" ?4 Q- V4 k" j* la component and airplane structure for electrical : J+ V/ ^# Z7 i2 e9 W3 `7 F7 j. r! n6 x( K0 |阻流门,; c5 _4 t" x) c3 t) ^. k 发动机上的一个装置。在反推工作时用于阻挡; O% r* e+ z7 ?$ E0 ^1 u y, D& K6 D6 }$ ]8 P. `7 L- a' z+ E, E3 Y装在机 ' ]+ Q& g! O/ h# T) b J+ L搭接片, + I( s/ o/ H% |; A+ j* K连接某个部件与飞机结构以形成接地的电接头。 . K: F1 z' j% J英汉对照民用航空词典B OEING - z3 p6 l9 p; O7 r' q! XTECHNICAL DICTIONARY 22; g8 @/ k9 j5 j% ]! ~2 v! b BOOLEAN ALGEBRA, A mathematical system for 2 t: v! y" K! w8 h" X8 }writing combinations of logical statements. # x9 Q& Z, T1 B) o' c, jBOOST PUMP, An electrically operated fuel pump for: j) o1 b1 q3 y+ M, O7 p fuel supply from the airplane fuel tank to the fuel / a/ W& Q0 E& L. `* x9 u: r7 W0 imanifold./ S2 F' a; S' v7 R* t P: H8 R BORESCOPE, An electro-optical device for looking at ; j( v5 i6 i9 V1 i1 @. Z6 tternal parts of an engine through holes in the engine. & b% V3 d# {0 X( s' eorescope ports) R M& t- f1 ?( t' |" Q$ T8 t OURDON TUBE, A curved flat tube in a pressure gage % J+ d6 t) `' g6 a6 e: ^r moving the pointer when pressure changes inside % s; I3 Q$ F% }" w( Aon the ability of the brakes to 5 S; t" l' P8 p' M3 t: r5 Obsorb a predetermined amount of energy during a2 d1 X$ |; a/ s& M. B! M3 w jected takeoff. & C9 D4 I* u& z; F* V0 W用于通过发动机内的孔(孔探口)观察发动机内部件的 ! n# u1 A; M; f+ c9 O光设备。' W0 E+ Q3 y L/ a 端管, % u, r; D3 b8 R) Y s测压计内的弯曲扁管,管内压力的变化时它使指针移! g) [* K8 {# K 力。1 h5 U) r) {1 A% r* l0 i 极限重量,: ~6 t: F, [) B( X& k% n; T4 i! m) i7 [起飞重量。 2 E+ O) Y& J) e' J发动机滑油系统与大气相通的通气口。 ; q6 F% l! L- w: m% ~in ) e, |, B- K( v, F+ m- j(b ( ^# _5 A& l& p5 TB; v& k, `" X2 `6 s& q* @ fo4 L h5 t" ]4 F0 D3 ~/ e the tube.+ d& S8 t( c! Y# q J3 x BRACKET, To enclose or surround. $ V1 }* r7 E3 e* D3 vBRAKE ENERGY LIMIT WEIGHT, The maximum ]. {$ ~! V. P3 f9 V; T' K* u$ x takeoff weight based, W# Q( @' Z' S# A a & g: j5 e0 c& B$ {, Tre t& Q. W% O3 O" \8 M9 Z BREATHER, A vent to ambient of the engine oil system.8 p( | s. y& J U" @ l( p% T 布尔代数, * ^7 _ b5 ~6 j一种用于编写复合逻辑命题的数学系统。 & }1 A3 {- {- _3 w: @增压泵,+ m( T8 {$ Z b g5 H 从飞机油箱向总油管提供燃油的电动泵。 ' ^7 Y5 s/ B" [% w1 O7 X孔探仪,( _# c8 b2 S4 ?* n1 j$ [) ]( @# L. S G6 k9 g2 [/ u) ~2 a2 v: ?& N动,以指示压* w, F: H& r2 C( j' B6 I7 @ 托架, ) t3 j9 k; H: C. _4 w用于作支撑、装托、或围绕之用。& t. D0 c9 z/ J7 ?. R$ L! } 刹车能量 ! [# f9 c& z9 {/ ~中断起飞过程中,取决于刹车吸收预定能量之能力的4 _* h7 R4 c, W( }: R1 o+ r! L% D# j2 S7 V) ?" \" q2 T( d% B通气装置,) g N: Z$ @, Q; ^' ]% V/ T' ^* E 英汉对照民用航空词典B OEING 0 K2 B& K* i7 Y% z9 [TECHNICAL DICTIONARY 23 : b+ a+ Z, b# R3 R2 J- r5 yBUFFET, Vibration of the wings and airframe resulting) e8 j8 ^ | c% u% y) S from unsteady airflow over the wing; caused when6 n! o6 r! g& y8 G0 I- A' S airspeed is too slow, the bank angle is too steep, or , e$ e/ I r8 G# dirspeed is too fast. - K7 b7 h, S0 i1 q6 Z, UUILT-IN TEST EQUIPMENT, Equipment installed on 2 {# {7 m% z- v9 Z/ W je airplane and in airplane systems to test the systems % ?* a$ h: f r# G8 T+ Xithout external test equipment. - e% }# ?% i0 f5 zUFFET MARGIN, The amount of residual maneuver" E# t a9 X7 i; h3 X6 R( g apability present before the onset of buffet.* ~7 g F0 z# y/ c% b UG SPEED, A preselecteed speed to be observed 3 q7 D7 u! X& k2 Dnding sequence.4 S7 m1 |' j0 {2 h+ O% ~$ K, h k2 P: Z% E, e/ A ng landing gear operation.- H- u9 l \3 U' Y- \) T 速度太慢或太快,坡度太大,均会引起抖振。 9 _$ B; A! H1 E9 X3 y+ _自检设备,7 k0 G) R1 s% ^% l3 t! H5 X5 f2 A0 D 安装在飞机和飞机系统中,在无外接检测设备情况下," Z3 E: m8 |) z2 s 用于检测系统的设备。9 d: r# U5 K2 a3 A 抖振裕度, - ^/ `2 ~; j w; d飞机在遭遇抖振之前,剩余机动能力的大小。 : J# f$ q; K2 Y# O' s6 G标速度, ( X/ r+ r8 Y' R3 n' m在某些机动飞行过程中,特别是在进近和着陆时,飞机 2 {( K8 _5 \) Q* {6 T预定速度。7 p3 L8 G& \4 m9 Z! ?9 E 力装置,7 t- p* E" h6 {4 \/ I8 }" I: M 架工作的一种机械设备(弹簧或减震器)。% K6 l) K. M* r7 l7 Z) n- E 流条, $ Y% Z+ M& z# I在部件或组件之间传输电、数据、或定时的单一电线或. L$ l4 q( o; z* s/ W& [ a # j* x8 [) C' y2 K1 dB # @! e. Y6 g" r+ [. u" q) mth 8 a; m M$ i; W- f# v7 b0 H- Lw / s. `) _- } W: n: j/ n% SB6 U f, e( d1 {/ w3 u2 ~ f- y c* N Z1 Y5 @: d1 P1 l+ E B4 s0 e; F: I- N. f- ], s% O during certain maneuvers, particularly the approach and ) x' o) }( F# Z/ e/ ola 4 n) C) M/ S# _- sBULKHEAD, A structural partition in the fuselage or 3 k2 W1 U1 A+ s( S: Q; Vwing.0 q) @$ w: ]# e BUNGEE, A mechanical device (spring or a shoc3 t6 h( r; O7 U# y3 o absorber) for assisti 7 y! b/ c% E) K6 l9 T, }BUS, A single wire or group of wires which transfers0 s. `) f/ G3 H5 V power, data, or timing between several units or- _( h$ v( P \; g5 p c) f modules.9 C7 v3 ~6 |9 B) c 抖振, $ P" {& I, O& l: e" E. P' Y由于机翼上表面的不稳定气流引起的机翼和机体的振 ' s% \- @* r+ [/ @- ^2 W4 }$ B动。飞行 0 d$ O: K. I! N3 A' y& i6 ^ I! Y5 E3 r所应保持的 " Y. s, E' U3 P: C2 ?! U7 e壁板式隔框, 1 _$ S# h; M }# R1 |机身或机翼内一种结构隔板。 ) o% f8 G: e E3 _( @/ \4 I0 @7 E% C4 H4 t5 J( M! Z& ?& a用于协助起落 6 C4 o( J+ t( e# j8 @ s4 Q; G: B8 o& z9 m1 g) @电线组。 % B1 W# |( ]' w d" y英汉对照民用航空词典B OEING9 S! ]' D) W6 Y/ s5 z; W 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 pulleys1 t' U$ U6 }3 V: o0 y6 O3 T, d cables in the control system.- G3 C( O" n( H/ c/ @+ d9 Y2 q3 w! ` and/ ]! _3 z1 h6 A3 ~# r; X( d5 K l circuits for control and protection of, J9 l* i# Y( D$ F lectrical alternating current supply to the airplane.2 y& m9 X& I7 t' N$ y3 |/ @! A duct for closing and opening the duct/ b, w# f' I0 }1 J8 `3 k- ~ assage.0 h: [' M1 L. a( l( N UTTOCK LINE, A vertical reference plane along the5 m/ S& X& e. @* S% D# M2 g# M selage for horizontal measurements of the airplane. ( Q9 @* d' k. k( ?! J' d8 X, u接。 % i, A6 o8 }( e0 [* g6 J组件,内含控制和保护飞机交流电源的电 5 M, h! y1 E! b# O+ i: i* O/ L3 l% a: i0 m作动简控制的转动装置。用来关闭和: @3 g8 h, {6 d5 P- B/ t/ F9 Z 启管道。 6 }" c; S0 i- V0 b8 @% { a( t沿机身走向的垂直参考面,用于飞机的水平测量。 2 O- H$ b; C0 y& X0 m5 N, `BUS PROTECTION PANEL, A module (black box) 4 q9 a) X9 |2 A2 l/ b; hcontaining electrica 1 |4 [& }0 Z- ^' D4 {+ ce, u2 g$ Q% c& H! `% l BUTTERFLY VALVE, An actuator-operated, rotating) B9 ?1 M0 u' L; N4 H; d4 z6 x C8 x device in a8 I5 R: r' k4 L$ `+ Y% ]# h! ~ p # T. G/ _- w" W8 l% SB ! k$ h [2 K: }' X+ G1 hfu9 [, c8 ]2 p5 k: n: R 转动鼓轮,2 a9 p8 s& y3 j/ i: G* Y3 E) p. ~ 在操纵系统中,具有滑轮和钢索的机械式连 B" S. U& g+ D! O+ j汇流条防护板,/ I: x; j0 z3 N& f 黑匣子式的 8 ]; F2 A4 b9 y; O6 T( J1 d4 O) N+ O7 b+ T# x8 l 蝶形活门, * \, ^6 |7 D$ y8 e/ H1 T是一个在管道中由6 P" F% x. Q1 F- w' c+ x D# v2 J% H l+ s, ]3 I$ H 纵剖线, 1 N8 Z( V3 B @! x1 @英汉对照民用航空词典B OEING" }: {% d' ^1 `. { TECHNICAL DICTIONARY 25 - a0 n/ P" T; x tBYPASS VALVE, A valve through which air or fluid will2 K9 ^/ p. u C3 b flow if the normal flow path is blocked.: [' d6 S: S) x; M, m, m BYTE, A group or string of binary digits. A byte is. U! L1 L$ V! ~ sually eight bits long. $ h( e6 w% F7 f) C4 m1 j l, dABIN ALTITUDE, Atmospheric pressure maintained& Y. V7 i r+ F' E$ r ithin the cabin, indicated in terms of feet above sea5 t5 Q/ Q% W3 M( Q, ]( C ALIBRATE, To repair, adjust, fix or correct the % K# [9 e. v6 ?easuring capabilities of a measuring device. - }# L d: j: z# @7 x7 V4 n. p% eALIBRATED AIRSPEED (CAS), Indicated airspeed: }' t, S. O' _ AS) corrected for position error.) B8 n7 U% A6 l( y5 U3 L nical4 ` w+ d0 r# m) N; F/ R- {: [ omponents.+ c+ k9 o8 L1 v ]- o, T' V! ]; r, A. m% o: q1 c6 G9 s5 Z5 e 节, / ^) v* o5 I, p) O6 T一组或一列二进制数。通常一个字节长8位。 . ~; a/ r9 W7 K+ q舱高度,4 }8 g. s1 j2 P; G 座舱内保持的空气压力,以海拔多少英尺表示。 ' u4 R6 t5 x9 ^准,1 c7 D* {) ~( O) m: o0 U 修理,调整,定位或改正测量装置的测量功能。* C9 G( {2 R: y' P& O4 G 正空速(CAS), ; S$ v! q! U8 Z/ [% W在修正了位置误差之后的指示空速(IAS)。 + `9 S& x2 w) l) ~" i2 _用来移动机件的一种转动装置。 / w% n( B* L3 `1 Cu9 W4 X8 L& Y& N: v$ B4 E C 3 Q5 U t8 E& y! P: W4 [C9 F! j' R# t9 N' j( b! _/ q w i, b$ z/ i9 v# Y% @3 xlevel. $ @! `5 V3 r2 R9 h& U& ~C ( ~0 X8 _* { M |0 I7 Em1 f( @: \+ C) h& y q3 X C# S2 w- J$ b L (I6 L9 F* R: Q" m! h CAM, A rotating device for movement of mecha0 Z8 k3 I" X0 k1 F C ! S7 p& {0 e) _旁通活门 N& t; W/ G w9 t% m; l 气流或液流在正常通道阻塞时所经过的活门。 $ O- c% ~' b3 k7 u" _3 z' \+ \1 \3 m: W& `* z; y# P& n+ `, J! Q) Y& `) U- `- z( X8 A) N2 x; m: f, z; B* X3 A+ T$ w z1 Q% r D- ]' \! ?# Q; b" l- m 凸轮, F, x0 g$ W' o 英汉对照民用航空词典B . o$ V' }- v1 ?$ ?" m" h/ H1 fCAM-OUT, An autopilot condition in which the actuator z' y0 \5 n ]' q. V5 n, J% S detent piston is overridden, either manually or by the 1 E$ c& X/ j; v% ?ther autopilot actuator. 2 q" \# }$ e9 ]' L9 NAP, SEE - CAPTURE! m3 s. b( a! [3 {, _7 y APACITANCE, The measurement of electrical energy . k4 V p1 ]; E( b7 k& d- w, X, o4 Atored in a capacitor (condenser). 9 q q b1 `9 T" a+ n( MAPACITOR, An electrical component of two metal 9 N$ Q& A4 I3 I' T9 n" |lates separated by a dielectric material, for storing" s. [2 R) I7 ] lectrical energy. 4 m" V1 P' H# n: E: X5 sCAPTURE, An autopilot or flight director function to9 F0 d$ ?* @/ m9 n! L3 {3 M acquire a selected mode.. k( u: U5 ~" n' O, A, v CARD FILE, A container on the airplane for printed" z5 O8 r$ E; @+ \ circuit cards.4 [/ b& o: l, X, M; x$ P' { 一自) Z6 R w. p: k/ o, U f 动驾驶舵机所超控。 L3 C" m+ F" p( g 截获, & o# s. V3 A- U" b见Capture ( p+ X! i/ x$ m% r% s, zo $ C$ S5 E o2 ?8 tC, K4 ~! l/ p. e* g! b+ @ C/ {( `3 q! _% W1 A$ Y* Q5 o/ F7 n s2 P9 @6 l! e" {+ V! h C9 Z2 Q3 t$ W0 @+ ? p 6 c5 J( `: N9 K, t+ ue( R2 M ^& x. q& G+ ~ 凸轮不工作,: s4 R; Z% Q7 G$ O9 N 一种自动驾驶状态。此时舵机锁定活塞被人工或另 C% P3 v7 x8 W+ q4 p$ R) i v$ ?9 ]/ P- S& \: t7 j电容量, , x! n; l6 m4 D8 @电容器内所储存的电能的量度。 * q' L: R! d/ \容器,& p; k9 P* g, R% @( r 两片金属中间用绝缘材料隔开的电器。用以储存电能。8 j2 P6 p( Z7 u' {" ^" o' J2 T 截获(CAP), G w `: A p) V自动驾驶仪或飞行指引仪的获取选定方式的功能。 5 F! S) ^, H& C' t6 ]7 i* ?9 \+ K" r线路板盒, 4 \2 W9 ? z7 y; Q# b飞机上安装印刷线路板的容器。 8 a6 }* M/ T. C) e, D6 T% @# K) Q/ E/ k; U, T L) w; a9 OOEING 7 V7 y* `0 p9 Y) R) NTECHNICAL DICTIONARY 26 + ^* p' v: Q" P3 [5 o英汉对照民用航空词典B OEING/ p, s1 e8 t z% V4 O$ a" b5 ]0 P TECHNICAL DICTIONARY 274 T$ I; k& N/ ?5 t5 G3 L* G8 T3 U CASCADE, Two or more similar circuits or amplifying 0 e, R2 ^% o O% f9 O3 G/ \stages in which the output of one circuit provides the 2 C( ]$ j" \" W$ N+ @put of the next. 2 I4 B/ m6 V7 bASCADE VANE, A vane for turning the engine airflow 5 \* o* m: D! d8 I8 e9 V; [uring operation of thrust reverser. ( \2 B+ I) a2 Q* XASE DRAIN, A drain carrying lubricating and cooling 8 [$ z$ X8 g+ H/ P6 o8 B: nuid from a hydraulic pump. j, B) c8 s$ k3 f- zATHODE, The element from which the principal1 R# U& }* T% O) ?) l) Y3 h7 h tream of electrons flows. , A5 F+ v6 Y* h1 u; \ATHODE RAY TUBE, An evacuated glass tube with a 7 U; t- q2 G$ ~4 kCEILING, The height above the ground or water of the, c! `: j6 ]$ r7 j9 o base of the lowest layer of cloud below 6000 meters/ }. y; k8 b0 f' R5 x9 ]9 f Q2 C, X (20,000 feet) covering more than half the sky.- ^2 m5 m8 c! ^$ m. H% I3 N% U 程。该 % a+ M4 \3 Z5 v7 M- F; I程中,一个电路的输出为下一个电路的输人。 ! f( \$ s- ?4 N4 K! ?0 b! W& K叶栅叶片,% v R3 l, ?1 i4 h* J* M 在反推工作时,使发动机气流向相反方向流动的叶片。; f9 W; g( Q; w6 D 匣余油管,5 N& [$ f& g, r/ ` Y0 o 液压泵多余的润滑液及冷却液的排放口。6 Q0 u+ p" N9 ?+ Z: ? 极,- f- _8 b$ Z; S1 e1 G# o 电子流流出的极位。5 K$ F _0 }. ^% E% X 极射线管, 1 y" u( h# d: H( N有显象屏幕的真空玻璃管。用于显示信息。 & D" X. n% L6 a7 \! U4 M3 {云高(云底高),( H( N: d6 j$ V0 X4 d- X; y 6000米(20,000英尺)以下已覆盖一半以上天空的最 7 k% A) c, A; V- ^% ]7 n低云层底距离地面或水面的高度。' z; a. ?7 |7 U& T! r! N/ P" S in ' }8 o+ g5 s' P# O& _% GC' q/ _7 ~! i" j! `3 `- E- D d # \) Z" k) ?* P6 {C ; a( E3 E7 t: H# nfl* E* K3 M! m" r9 C/ }; y C 3 w& I0 n( C, b9 Bs( g L+ I3 N9 V0 F( i9 O* o; g C3 z- b* s& F n- P3 ~ viewing screen, used for displaying information. ) A# e+ b+ }: b9 F* d级联, 7 {/ P/ ]# ?" i% }% d两个或两个以上的类似电路的逐级连接或放大过9 t, @* h+ |8 v/ Q- s$ S P* C& [. \! d$ H" U4 q5 E! _. f3 u; ` e% {2 y3 w/ t9 O1 y5 v+ J: b: C% V+ J9 M& L9 k 一个具 0 a# E' _: Y1 b3 e英汉对照民用航空词典B OEING0 I* {( N% y0 l2 [0 f I TECHNICAL DICTIONARY 28& N6 t" L8 K7 M7 C" _0 R A CELSIUS, A temperature scale in which zero is the . }0 s, j. t3 Q# X# H. _freezing point of water and 100 is the boiling point of0 p ~0 M, D& R; P) N3 @ water. + H& Z/ i# P" G; q, E4 [CENTER OF GRAVITY, The balance point of an object/ t. Q. \: C* p6 _+ R9 O r rigid structure expressed in terms of percent Mean+ M. L: F" G0 F& S, v5 i erodynamic Chord or in inches from a reference point.# l& W x2 |$ ?; Z8 `( Q" r ENTERING CAM, A cam for moving a mechanism to a0 e d8 Z2 F" E' r eutral position. 3 z& l- S$ \* G! f& P) o+ _IGURATION, A configuration of the+ E# `9 N- h; v3 h" S ircraft approved for operation by the local governing4 M" s% T( h) Q5 w gency. o: @' v9 o- T ENTRAL PROCESSING UNIT, In a computer or, j' ]: F. x+ A M5 \& R igital circuit, the section containing the arithmetic and# m# D' C6 W% Q9 P gic,control, and internal memory circuits.5 L, m5 }. h* _/ k. x4 @0 P ENTRIFUGAL FLOW COMPRESSOR, A type of6 S% `1 `7 o3 q; Y ompressor in which air is taken into the center of the5 U( g/ U+ U+ `/ _+ E7 t peller and is slung outward centrifugally into a diffuser " q2 B% [: [. C7 X8 _here it is slowed and pressure is increased. ! Z9 B, P1 M- b# ?6 P- fCG, SEE - CENTER OF GRAVITY: b. m$ M4 g @" @; a; q( q 构的平衡点,以平均气动力弦的百分比或 3 W1 y; g( g5 n. y7 s6 l某一参考点若干英寸来表示。 : W8 D4 l4 t/ W m4 U$ ~; x中凸轮, ( @4 m" S: N9 O* \, P/ G, T将机构移向中立位置的凸轮。6 {: G8 c+ Z6 \: p: R 格的装机状态, j. b- a7 a3 L 由当地主管单位批准使用的飞机装机状态。3 C% m) I- V0 m* e6 i1 _ 中央处理器,+ U, |, Z x* A* x; G 计算机或数字电路中含有运算,逻辑,控制和内部存 m1 l! R" d2 X1 J' ^6 ~储电路的部分。 2 ^& h8 v9 Q+ m+ G, W心式压气机,( ?8 f1 N9 a! P/ P8 ~ X 压气机的一种。当进气到达叶轮中心时,被叶轮离心抛4 g; h) n$ d2 m' ^3 S# b7 n 进人扩散器。在扩散器中气体流速减慢,压力增加。 4 G# b. G% `! G7 p重心,1 _0 |+ B: a3 Y" m0 j 见Center of Gravity w; s, A8 z) W. h# `, a" L: m: |( ~o & `% |' u! D$ b, r; b8 nA- {. I1 q5 ^) Y. Z# K C% a9 V5 x6 i9 Z n/ u7 S" Q+ U% C( a/ z; j, \ CERTIFIED CONF 1 ]! A8 w* k* X3 b1 pa $ ^- [5 p; P& l$ Q- [0 d. j# ra + y" l W6 ?# P4 zC/ |2 l* a8 d; r* b$ ~5 k d/ e5 r) S- B1 a lo8 a: l% f3 R% b1 C" `% Q7 R C 6 o( G5 S- k, |9 X% ~* }, i. ?1 Zc* O! U& t: z; V7 T7 e" G$ u5 _ im 1 |1 L: P* K3 t6 Mw 1 J ]$ B( F4 p3 E6 S4 W2 z摄氏度(°C),3 _3 ]% H7 I6 j# U8 ~! S* @ 温度的度量单位。在此单位中,0°C表示水的冰点,4 d( M$ D5 @) ?8 ^* W O 100°C表示沸点。 - G0 \& z3 w/ J2 N+ o重心$ a' K; p6 X0 e2 \3 J0 H 物体或刚性结 & ?6 ?: z* W1 b) z0 f4 H% A( D; @2 r2 N7 H1 s/ g* Z4 y! j) V6 Q1 O3 _/ w4 S- K6 t, W i$ K- E* N6 x+ x' w7 q9 ]$ m+ {8 z! y* a2 y+ c5 @5 Y5 c% S( V% B g( t6 E 英汉对照民用航空词典B OEING1 ~8 ]$ o9 r9 H" q TECHNICAL DICTIONARY 297 V( K' A5 h5 \4 Q CHANGEOVER, Conversion from one mode to another. 7 D6 _* o1 `- y& t7 B- [4 ~HARGING VALVE, A valve for supplying air or fluid to 6 C. e6 M( F/ p) w- VHECK VALVE, A valve allowing flow in only one 5 y, Q8 g1 G& b, A, e3 `1 Oirection. See Non-Return Valve. 1 [& g, N1 ]* p3 Y( D5 [5 o4 @HECKSUM, In a computer, a summation of digits or 1 p# X: x4 g2 k$ i0 q' ~its which are primarily used for error detection. ' C" N' n+ h2 N! V- N1 ~. e- JHIP DETECTOR, A magnetic plug in sumps of/ Z0 o6 T9 k0 r0 e" \ bricated components for detection of internal failure of 7 I( Q. r D) n% q3 e6 G7 de component./ `' i' g1 `% p: }! p HORD, A structural component of spars or frames.$ ?; c- h, j6 e' m 添活门, $ K+ F. e# _, m* w器充气或加液的活门。2 B V' U, L$ T3 v/ L 单向活门, ( o* f u$ Y2 O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
C $ K* [' A3 ?' e8 v8 xa reservoir.0 c& Z5 m8 j' l8 s C ; k. B F+ I( ed: q$ @5 @0 j( n# d L C 7 }2 K1 Q+ S L* z% mb4 `3 p. {! H! a3 J3 u C; e- a3 U' @. q) K, Y: G; t# M lu 9 p+ O& T& M% M7 j) m5 H ith , Y; l4 Q, T+ C w4 D4 RC . f- B9 o1 }" n$ N/ v0 S转换,5 I9 _5 c+ r3 B 由一个方式转换到另一个方式。, | o7 X* N, @- Z' s; ^4 @2 D& `3 g; z9 W/ d; E 用来向储存* q2 V) X/ {9 M$ `/ ^8 T6 Q+ M8 F1 s! U4 L) C9 q1 u2 q 总和校验, ; V1 u! q; R2 m$ k1 W, ?3 K2 k+ n$ `计算机中,把那些用来探错误的数宇或位数的总和进0 H2 X1 F! Y' `- o4 P 求和计算。8 d+ O9 _- y1 I+ B0 Q 属碎屑探测器, 8 l: X9 v6 n) y8 t5 Y装在被润滑的部件滑油回油管路上的磁性塞子。用来探% h2 h7 y. R1 n 部件内部有无损坏。, V0 J! I4 Q+ S9 [ 弦, / c$ t" y+ }; l# D4 Z$ H- [: W梁或框架的结构部件。 3 \* j2 P4 w% ?. c$ ?# [2 Q+ W: T ]8 _# H3 k6 u: Z m: D' K) X5 R+ k" A; D7 U* ~9 p5 M/ {& x9 r8 G$ B; `! i$ w8 J; @* q F* q3 k9 h: M! O" x8 q英汉对照民用航空词典B OEING * M0 l! ~$ C7 z0 H" TTECHNICAL DICTIONARY 30# u3 R+ s8 \( \% W: j7 |/ C CIRCUIT, A closed path through which current flows ! S) M) _" k- R! ^. Q- [ource. ; J6 l% m. V: b2 ~$ r! o0 GIRCUIT BREAKER, A device that automatically - k2 b4 n3 Z+ V: e" V+ K. _- Y7 leactivate the system.2 Y: B% }& V% B2 @9 q+ b lear of all non-frangible objects which5 U8 r" _5 o7 K3 c1 q: g6 l0 l7 i) U ay be used as takeoff distance available when 7 X8 T/ _4 c9 t2 B/ V7 galculating a takeoff weight.# A* J9 i. w$ h. m5 m- u: ~ r water under the control of the appropriate$ O& M& O5 z, P" q uthority,selected or prepared as a suitable area over. P4 Y: G, g; n$ L/ ^( W; d0 v0 T hich an aeroplane may make a portion of its initial }4 ?# f* e/ v- S/ `- blimb to a specified height. ; C" S! y; c; W k& @increasing./ J' p. R. C: ^ R2 v sed; N4 ] }/ M* a$ X2 U LOCK SIGNAL, A continuous string of pulses used for 6 i }$ i4 J" f. e: G/ L开关,0 y" b9 t$ }- }, t% H 故障情况下自动中断电流以保护线路不受过电损, w \1 e% _+ R$ S- l% u4 z+ ` 体障碍物的区域。在计$ n! `5 {7 u. m9 H7 w( w 起飞重量时该区域可作为可用起飞距离。 6 ~0 y8 S- t& ]( k" {是在有关当局管辖的地面或水域内一个界限明确的长 ' V2 j$ J: R, ~( n2 Y- N( E形区域。在这个选定的合适区域内,飞机可完成初始爬 + v; _7 g7 e: u3 @的一部分,上升到一个指定高度。8 F2 I& v V( j9 L3 g 飞机高度不断增加的飞行阶段。 , Q# k& `9 x) |9 \) F- B钟脉冲, 1 c, S {; f. c+ k! l4 z6 d步的连续脉冲信号串。3 n0 E; F/ \8 @: g- A, Y! K from a source, through various components, and back 8 k8 x* A& r" l+ v. Dto the s) l1 U% W: `' M) q6 I6 T( o C 6 l+ j7 y S# F& dinterrupts the flow of electricity (current) during fault( A* N+ @7 q3 G, E, _ condition to protect wiring from excess current. Circuit ! b+ Z6 e0 h" N, ~3 t; Ebreakers are also used as a means to manually6 X) }* h$ \; f8 _2 S" w3 E d; I# z* B9 c) T+ T0 b) r CLEARWAY 1, An area beyond the takeoff end of the ( @/ n8 i {5 q/ |7 \" A* srunway which is c& u' w( x% j9 J0 W0 [ m N! S( I& L1 h9 L* q- t2 M$ I: `c % e8 J2 E) [/ ]4 m7 C8 cCLEARWAY 2, A defined rectangular area on the * x: o7 G1 ]! C0 a, Y* jground o I$ f8 w: }! @: T Ja + p; z# q8 h, u$ uw2 V9 |' D& r U. F c # V+ F6 t& n' j) r9 p) sCLIMB, Phase of flight where the altitude is / L+ _1 {4 J5 y5 b' d: l! YCLIMB LIMIT WEIGHT, Maximum takeoff weight ba ) T; C0 P8 V G, son a minimum climb gradient with one engine 3 T) H v- E! G- ^5 Ginoperative.0 V7 v& w$ d8 U C + K, d, ~) `4 |# ~6 t1 l) D* C/ |" Rsynchronization.: m6 X: J( c5 B' C ^! g8 ~ 电路, 4 @' K8 e6 C* \一个闭合的回路。电流由源头流出,经过各个元件流回9 I5 i X+ `+ R( ?/ x 源头。2 P# W* P9 s$ @3 t+ ]* r; m1 p1 o" g- E0 A0 ?8 E能在% ~ U$ j$ m# h; Y! c$ z2 B$ t 坏的装置。跳开关也可用于人工使系统无效。 ) }% ]! m: j/ L$ U Q一号净空道,. Q+ f2 C( Q, b$ Q 是跑道起飞端以外,不含任何刚 # ^- i# t8 y) f4 B2 J, E) h8 _ b" U6 K2 \6 y! I7 I 二号净空道, ' S- f/ r& L- ]7 s3 Z( c8 M9 K) G6 o8 i/ _. z& [ x0 S: S: V+ Q, x, _4 _9 l; I9 k# U- H 爬升, 3 [7 N. C" z, v2 @爬升限重, 9 y6 ?$ O6 R% X8 _取决于由一台发动机工作时的最低爬升梯度的最大起8 ~' @9 N# p! F' Z 飞重量。; _# U3 J7 Z$ C$ C* V& G8 ^4 |$ U' G/ j5 x j' l2 m! `( e用于同. k( d- V8 }! Y% u/ d7 I 英汉对照民用航空词典B OEING 5 M o$ |: p2 u' k- ATECHNICAL DICTIONARY 31% u0 y7 K& `0 u' L& k& r! b COALESCER, A device in the water separator for ]$ P: F0 w i& w, Q" q6 H ollecting moisture from the cold air.* t2 J/ M9 g; X: f n antenna with a receiver or transmitter. H U& d, O' k- r: hhe cable has an inner conductor and an outer* E' Y2 B5 r# Q1 s rounded shield.. p; N! [# u7 H: { ting one inside the 5 z' _9 i/ V U' o$ `8 P- ~$ }ther for rotating the low and high pressure , m9 [3 X7 E. Y7 vompressors by the low and high pressure engine ' Y- [4 X9 _3 P. ?* [- Yrbines. x: v# d. s: F8 {% Y# M+ e/ j OMBUSTION CHAMBER, A part of an engine for p' y4 U( t b2 ?) Z0 | urning fuel in the air supplied by the compressor.* d+ `# K4 Y: h5 V+ [5 g4 Z 置。' Z* h% ]) _+ P( g0 m6 ? 射机的电缆。电缆* ~. x' P2 F4 G 中心导体和外层的屏蔽所组成。 % w( {3 H$ q/ M/ d2 U. ^两个套在一起旋转的轴。用于使发动机低压和高压涡轮! P$ _2 @9 t* X, C 别带动低压和高压压气机。3 N3 @9 ?' S' ]1 \1 j 烧室, , p$ o6 X4 a( d; \1 o1 t发动机的一部分。用来使燃油和压气机所提供的空气相 + t# Q" E' g, Q+ s0 h+ H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" S, r! z) Q. h COAXIAL CABLE, An electrical cable usually+ y% V( K! x3 _5 A2 W: H, e connecting a$ A! e& A1 U. |' P- c T% j: y6 [; Y! Q5 ^: M. w g 3 T1 y( Y6 u; oCOAXIAL SHAFT, Two shafts rota 7 @! K) j) O) Z6 r1 \2 w6 ho , h1 i" d; Z! i; l. i9 R/ p( H3 tc# w1 J7 y/ o' X3 j' s8 h- A. ? tu3 J8 ^: M: a4 p! P. }+ N4 q2 B C & S8 _) p+ o; v' wb " [- g; e0 D. u5 m! G6 U' ?/ |- {凝聚器,: V; p3 Y: B ^! b8 p" b" G% ?& V. e 水分离器内收集冷空气中水份的装/ @# d% ~ d' W3 ~5 I 同轴电缆, ( \/ N3 ]) ^5 ^6 I: S* A& }一种通常用来联接天线与接收机或发: o6 |, u2 n6 B+ X/ E2 w1 r0 ~# a! l @同心轴, 6 y4 s: c: N0 |( }' @0 ?0 \" [ x. S4 A1 R, t) Y4 w7 S& \& Q/ ~# {$ i' \. |# V# v0 S9 {0 A英汉对照民用航空词典B OEING " _* [3 l" q. F# ~9 ]: ~TECHNICAL DICTIONARY 32, Y1 x4 B& N5 v5 x- L1 M COMMAND BAR, A flight director pitch or roll comman $ j4 v" x4 `; kindication.* E9 K$ J1 n; f! |) B d+ J+ u: E' M- c$ C9 ^2 g OMPANY ROUTE, A route flown by the airplane ! }, Q6 k- a! E8 K4 g+ qOMPASS LOCATOR, A low power, low or medium' ^+ J! o7 i6 o8 _8 m/ z7 Y equency (L/MF) radio beacon usually installed in 0 Y. D8 m2 n9 \3 W; qonjunction with the outer or middle marker of an f: y# i& b. G ~ tor (LOM), A compass % E) h% ]3 c i% I; Qlocator installed in conjunction with the outer5 U7 v; O) I4 x, m4 z: r6 }; P marker of an instrument landing system. V; |. R6 d7 E6 E7 e( Jss3 v/ N3 x4 O7 i) z0 n( m6 V) l4 F le! h/ }, U) B' b4 y0 A OMPENSATION, To offset, balance, or counteract.7 F, I. y! |; v) s OMPENSATOR, A dual capacitor for changing the fuel 9 }& M6 N7 E r; b3 A w$ g3 Paging circuit capacitance due to changes in fuel 8 u* k. Y6 a7 A8 I5 j/ Qensity.# P1 d! N( z* W; ^8 A+ b8 S) O OMPOSITE MATERIALS, Non-metallic materials used 9 a; C3 M! T4 ] L2 lr airplane construction. Fiberglass, Nomex, Kevlar, K, J3 c# W* mraphite Epoxy are composite materials. , t& ]2 p( J N% `1 w司航路, 1 |- k8 ^: V2 ?5 s6 v# j在飞行管理计算机数据库内由航空公司飞行 + a* m5 y' U' v( [2 l' I盘定位台, $ X+ G; p" j5 \0 H2 J- \8 M与仪表着陆进近系统的远距或中距指点标配套安装的, N" `7 K! D* l2 R6 ~ 功率、低频、或中频无线电信标装置(低功率NDB台)。( W* R$ S/ H/ a8 H; W4 w! g 程序中用来导航。$ g& g5 w& P/ G$ ^6 n 1.远台, 4 E: x9 O% M+ C* z# R与仪表着陆进近系统的远指点标配套安装的罗 5 R+ ^5 u& b. l5 ^盘信标台(NDB)。 5 ]' a0 v7 ~! u- n$ U; s& k偿, 9 _+ W. p! t+ I) B/ v抵消、平衡、或中和。 ! W" h$ {4 T, h0 G; E+ u偿器, . { ]7 ]. s& L# s4 V在燃油计量电路中,用来改变电路上的电容,以与燃% X2 l6 u8 C5 j6 q5 w3 c 密度改变所引起的电容改变相抗衡的双电容器。 8 N$ F5 N h/ }% E* ^+ \6 X合材料,1 w* R- X6 u/ e# k0 {6 I 用于飞机制造的非金属材料。如纤维玻璃,Nomex,( n1 s- h/ O' }* J$ M evlar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
C / X/ z- x* p7 O& Coperator that is normally stored in the flight- D* |+ z& x( @. R. _. x9 N management computer's data base.9 P! g$ X8 [; L( v t+ g C ) I% E# R# ?! |& K9 Z4 B+ F( g3 Y8 Ufr 9 ?; j1 O5 f r' qc0 w9 m. N' b L, d instrument landing system (ILS). It can be used for ( l2 ]+ `* i. r K, hnavigation as authorized in the approach procedure.; C+ z: f! V! i2 m: ^# Z" p 1. Outer Compass Loca( d4 P# t" C; j/ F$ h* E 2. Middle Compass Locator (LMM), A compa( X& i& U2 p, F. d locator installed in conjunction with the midd 3 r* R0 Q% L2 z3 zmarker of an instrument landing system. . X h4 r6 f. ? R" _- {C . w" X1 o/ N1 V1 e0 r1 }C 2 }8 Y: M" l' `0 M7 e! zg4 q$ j' ?& \+ v5 Q* S' o2 e d 0 B% l* @$ I nC }- d4 V R0 i( d Y fo7 M* q! }6 |0 X, Y$ ^6 K g6 |: G* k! t& o, n$ Z9 K# u) e 指令杆, ' j Y8 N: K2 R: s0 P0 o$ U# t飞行指引仪俯仰或坡度的指令显示。- o0 A4 I- L/ z( j! P, l+ g4 I6 |7 |% _7 M. c 通常储存" l8 ~8 \. M. f7 _/ } 的航路。9 p$ j# W! \2 b5 u7 z0 ^; r& U) w5 Y/ q- Z- V1 I5 z# |) X! Y- c: u) O" F! s 经认可后在进近% \3 {3 t7 x6 G& R2 r/ i 2.中台, 2 H$ Y( ~8 K$ a* _# f与仪表着陆进近系统的中指点标配套安装的罗% A7 c% m" f( g/ l 盘定位台(NDB)。; K3 x* I9 u# H1 u) \6 O+ E8 p9 {4 a6 d& p# \- C2 \# v$ ~, W2 d" P9 u0 q& X% i t5 A8 s' T- D0 F' e2 ^# n& [- ~ K! T4 s/ N. ?$ l6 y) y; w 英汉对照民用航空词典B OEING ' A1 W3 b6 V# p) q7 K3 f5 yTECHNICAL DICTIONARY 33 ' D" p, a7 b8 P7 t9 }# Zby8 K& O- y3 W1 b4 z5 Z: v or increasing air 4 ?( R8 H3 ^% j0 a+ Jressure and temperature before the air enters the . C& ~; n1 k: O: L3 q; u, ?5 xombustion chamber, Low pressure compressor - front ! k' o8 `1 _* \5 H& `ection of compressor, High pressure compressor- rear; L7 B8 P& q0 x3 r# t8 a OMPRESSOR STALL, An event that occurs when 6 r- n; i. Q) ?+ b' u- Bere is a complete stoppage of air or reversal of air flow3 k8 D& V3 J. H% p; u) I$ E COMPRESSOR SURGE, SEE - COMPRESSOR3 G9 d. z5 P+ a! Q1 J STALL COMPUTED AIRSPEED, Indicated airspeed 0 a+ C9 |1 U$ D8 l7 q$ u# E0 _corrected for the static source error. q! A# P: ^* u3 ?/ B! }的机械轴来驱 9 [# Y* a V3 U6 [8 n$ l,用来增加吸进空气之压力和温度,以供燃烧室使用。 V0 U* x' S7 B1 F' l1 |; E 压压气机—压气机的前段,高压压气机—压气机的后) V* w, U& L" B) t1 y+ m( v( L, z k# b气机失速, 9 ^4 x9 f D5 }. L8 j当气流完全停止或通过压气机时气流方向逆反的一种2 {+ F/ C, k& q4 ^% v7 ^- s1 `" b0 ~ 压气机喘振, . s' v( u; M: n- K" \% E! |1 _见Compressor Stall 9 c! |7 Q+ a+ q/ ?+ S4 Y8 XCOMPRESSOR, A rotating part of an engine driven* m# A3 M) L4 K% `" [ a mechanical shaft from the turbines f! t% _) e6 z# l3 v7 Q9 o3 D4 Q B. r p& k2 |& Z. K2 b$ N c ; d+ H4 C8 E: Ss 8 n1 ? {* D. c, Vsection of compressor. ' }8 B$ @0 ^/ D1 AC ( A+ R6 y" v$ c# Z7 Fth / T0 C5 l8 V0 B4 v0 l9 Ithrough the compressor.3 w4 Z1 s* o. S# g 压气机, / A2 U0 ?# l2 e3 E; D8 v& c$ c7 G发动机内的一个旋转部件。由与涡轮相连1 i" G- D: t/ D8 G% Y" I3 u; w$ u* b; w( W/ P1 A" A7 H [$ g, g! i/ G; m/ D" m q4 {* P$ y& y# ^# X4 x) g+ G; P; b, H2 B; X现象。 , e' o X+ ]. x/ _0 _* _7 W, u# h' ~1 I+ T% j! k计算空速," K1 s3 U, H' A0 V. Q- h 修正了静态源误差后的指示空速。& c% R( S( B, [ 英汉对照民用航空词典B OEING. L7 Y7 w6 R: d6 L7 @/ @0 o( E3 ? 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 arithmetic3 l: J% Q6 ^( ?2 A4 ]: a. i operations, manipulates data, and makes decisions. ; U! m, M# x# y# E- ~ o8 A. xditioning; F5 `- B3 ^4 t {! E+ o8 n$ s the air and the & Y' O2 I- Y9 k. Z8 y- Hfrigerant or moisture vapor is changed into a liquid.( F: d/ D8 L% Q" D* d! }* s* P% x& j ine0 x5 m# U3 l1 y% E& o0 |" Q ONFIGURATION, The position of flight controls, 3 k' o8 M5 Z) A& hmissing which 9 p+ B, A, I8 y8 c8 [may affect the aerodynamic performance of the - [7 `5 G. N( _2 {. P; eairplane. % W2 @5 r$ k9 u置。% j1 k M2 J7 w* M" t) [: X 中能使热能散发到空气中,以及使冷冻剂或湿 4 m1 {/ A' q* E2 c1 y4 m; b转变为液体的部件。 8 A U1 y. n% w连接到飞机结构上。; Q1 o! k3 I' y m( ]$ R r+ d5 y 态, 7 o: ~. [& @3 C$ i: Y定飞行阶段中,飞行操纵面,起落架等的位置。" c8 i; z* D( |, J ), 8 D. e6 q: M! M1 ]% A受到影响。 " W$ O! E0 C4 K' [) WCONDENSER, The component in an air con( K) C* G x2 `+ e, q3 }6 o% J system where heat energy is given to ) P8 A& r/ N! \1 O3 @re ; D. F. W( ]2 D1 m8 JCONE BOLT, A bolt in the shape of a cone for eng - z3 k8 m- |7 g- nattachment to the airplane structure. % C- d$ G" W7 W, ]( g$ p/ VC$ _/ H/ i4 a( M" U& E landing gear, etc., for a particular phase of flight, e.g.,- ?! t" q3 {5 W3 T Takeoff Configuration, Landing Configuration, etc.* g9 R# S4 ^1 s T' G2 P2 o/ u; c CONFIGURATION DEVIATION LIST (CDL), Appendix* y4 m: \- w8 |6 w$ U% S1 `7 A in the Airplane Flight Manual (AFM) allowing operation+ Q. v7 B$ l0 [; i' N/ \ of the airplane with certain airframe parts : @$ h2 V8 H4 J- L3 B计算机, ) w' W1 S7 y* q能作算数运算,数据操纵,和决策的装/ a& |. ^2 v& R- V, _ 冷凝器,+ t: z% c7 _( g0 X; G 空调系统% u; ?+ u( M# O3 S1 ] T- @; l2 ? O* t3 O* j锥形螺栓,9 \; C8 U. J. Q( q. J 外形是锥形的螺栓,用以将发动机/ A; |- f4 O4 ~/ d: E& W' Z! o! q' [7 g 在某一特9 d0 z: t- d, \9 D: j1 @ 如起飞形态,着陆形态等。 - b. N' m6 G" N' y5 X1 [缺件单(CDL* \5 k; ~& s" Y, M u 飞机飞行手册的附录所开列的飞机上某些零件的清单。 & M" f& ]7 e3 j在缺少这类零件时,可以飞行但气动性能可能; b/ w, Z0 r; H9 z/ h 英汉对照民用航空词典B OEING " x5 h8 w4 d: CTECHNICAL 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! \; t M5 Q" i9 g9 p$ U @ component for changing variable engine gearbox speed 0 p/ {' X# D+ v8 K2 {" }' zONTROL AXES, The three axes of the airplane which ( v- N- h0 S4 i( j T+ qre perpendicular to each other and pass through the Y! r0 k3 a0 E' L) [, Renter of gravity of the airplane.( s2 j# ^7 R- a9 d8 m5 |' w Pitch axis - Horizontal or lateral axis, passes through $ d, e6 ?& I' h* rthe airplane from one side to the other -* m/ [: t" A- E+ [9 q. y' T nose up and nose down control is by" c) z) y, `3 R; i) _; E. ?/ \8 t6 K elevators (and stabilizer for trim). ( T2 n' V# f, F7 M9 z3 l BRoll axis - Longitudinal axis, passes through the ! S7 T) x1 J4 e, ^' Jairplane from front to rear - wing up and & f4 D8 }# B+ y' a5 Uwing down control is by ailerons and * T5 z9 P2 e2 R& h0 B4 vflight spoilers.1 u" y9 l) \ U( ?0 L Yaw axis - Vertical axis, passes through the/ ^) m: Z- s4 I& N! y8 c airplane from top to bottom - left and * [1 s3 g6 L4 u3 G$ Eright control is by rudder.0 N& v' ]; i6 `+ Z U' z1 U0 X. R/ c 置,6 \# R) k' c0 z+ n- H8 V 制轴, % n0 G" {. }- m3 b, T8 N通过飞机重心互相垂直的三个轴。+ H0 x" [1 n- ^3 K) ~ 俯仰轴—又称水平轴或横轴。由飞机的一侧通向另 , P7 i3 \; J% q) R侧。飞机绕此轴转动即造成机首的俯与仰 ) ]6 |; @* j% ]( h俯仰控制是由升降舵来达成的,水平安定4 _% T9 N) U9 o2 M5 P* r: z 则为配平之用。; m7 s7 ?' g4 c( A+ g# w9 y 横滚轴—又称纵轴。由飞机的前部通向后部。机翼- M- L2 Q/ s1 K, g 下运动由副翼和飞行扰流板控制。 r2 j R L/ u' K' a+ w) f偏航轴—又称垂直轴。由机身上方通向下方。飞机 , i' H" }3 C8 m# R& U此轴转动即造成机首之左右运动,此一运( |+ T! L2 d" F2 ? 由方向舵控制。 % q2 M2 q' O, [( ~2 d4 Oto constant speed to drive the electrical power.' x0 n; h4 h$ K7 y% C: P C: \5 B3 L% h/ |( Q8 K! D a5 s4 l' C: Z4 g8 z' u1 A; N5 Q/ R c4 h; w+ W9 P( }, Z: W4 I 恒速驱动装 8 _6 [3 i2 `3 d( @* K将发动机齿轮箱的可变转速转变为恒速以驱动电源的4 P" K5 Y, m& h* u* w8 ^: H2 y 液压机械式部件。 / c$ G4 V4 W$ v2 U0 G% P( g( T: b9 c2 \$ F% V, [9 _8 f' y+ v% g4 y# h9 R3 u8 A' b/ O, L/ M8 C9 d5 Q" s. N" l; F7 R7 U: J0 m9 P! M. Q" G9 W, G) g/ ]' S; E: X7 N8 f" H; G* M) N6 u) d4 M1 r# z) V* l英汉对照民用航空词典B OEING 1 z/ L. ]8 z. v. w2 t. KTECHNICAL DICTIONARY 36+ p* W' D% d Z0 b) v) _+ H8 U CONTROL COLUMN, A mechanical component used G( S( v% }# R" A, U3 ^; X rs& e8 f0 v' R3 }( s. W2 X nd elevators.. {$ L( h$ J- h! ^ ONTROL SURFACE, Moveable panels on wings and' m" ~. _9 Y' d; F9 Y% j S6 b. t0 ], O il for movement of airplane on pitch, roll and yaw axes. 6 |( Q( d; _) G1 ^/ \6 HONTROL TAB, SEE - BALANCE TAB1 F* N4 q3 V2 q; p) e) c ONTROL AREA, A controlled airspace extending( Q/ E. g% a$ p& F% I% [5 f pwards from a specified limit above the earth.+ i4 C" ?* Z6 }' j1 _6 U ONTROL ZONE, A controlled airspace extending / ^# V5 D. J' S, j3 x R; E- G( ?pwards from the surface of the earth to a specified* d" u1 D; z3 ?, v( G& g* ^ pper limit.' V; s+ J0 ]: m7 ~6 J6 S is5 u8 Z* K$ Q) l e O( v% Y o IFR flights and to VFR flights in accordance , ~; o1 M: G9 ~5 s0 o% owith the airspace classification. 9 m3 r1 Y, G$ A机械部 4 v) E8 C U' W1 x! u3 n R4 n$ _) M' t" K, Q+ I# h. D* s& {' x. r操纵面, 4 `/ I4 q6 M/ g9 @5 c/ Q; H- X机翼和机尾上的可动面板,用以操纵飞机俯仰,坡度, . p: ~/ {7 ]) c j和偏航运动。 1 R3 c+ u$ ~5 X& _ f$ S操纵片, 2 ^3 ?( z+ p+ \. d- x) _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 " B3 U W+ C( I3 s/ v/ u9 x9 Ia 9 `6 a! p% H% RC , H& u G9 t. j E$ k" h rta 5 L* J0 v5 R8 b9 }1 f5 rC 9 ~: }# J, I5 y( `# m) _( W/ MC , J4 C- z- c; k8 y+ x& d/ ^) eu0 z l1 Z6 v/ M% R& t. A C # n& W* u9 [$ a( Bu2 p+ N, N9 X$ h u 1 ^3 p# H0 B/ `CONTROLLED AIRSPACE, An airspace of defined ) Z' r# f9 o; J) `dimensions within which air traffic control service, y' T# M4 n0 C/ C l7 w provided t* @5 E+ Y6 c! a& w2 P 驾驶杆,9 L m# o- P4 w G$ W 飞行员用来操纵副翼、飞行扰流板和升降舵的 7 D, q, ]# Z2 f. D; w2 N8 y ~6 p2 A i2 i) \. v% y* y7 p' J0 s `! ?- P+ v管制区域,$ v0 t4 c2 m$ U 高于地面的指定极限以上的受管制的空域。 : A- W& f" E& M" }% U制范围,7 i! ~! ~2 ?; I3 ] 由地面到指定的高度以内的受管制的空域。 # G9 Q4 V9 {- o/ a* h一个范围明确的空域。在该空域内,仪表飞行规则飞行 L8 I. D f: e# s; |和目视飞行规则飞行有空中交通管制服务。 X5 S# t2 j) l/ d1 o* P# j! Z G7 y1 G9 [ G6 ^ 受管制空域,8 z! q# x" A+ q# B: e# K5 O6 }" F 英汉对照民用航空词典B OEING' A8 G* O. |) A TECHNICAL DICTIONARY 377 i0 Y; G/ V0 j' p. s CONVERSION, To change into another form., P% t# ], J$ w* G" o, o COORDINATES, The intersection of lines of reference, 0 \1 r3 L+ k) w0 ^6 I; _sually expressed in degrees/minutes/tenths of minutes4 ]' I6 D5 v# X. h9 [ f latitude and longitude, used to determine position or1 y2 H6 w) Q* O5 ^ CO1 H/ g: G7 L+ l) i9 S9 e& [% y destruction of th+ x8 W- n; @! y3 y chemical conta 3 _( Y% s" u2 z" D6 h$ h `COWL, A remo 0 x- z, v' M$ I, L$ I) B' Qfor access to th+ A' A2 u/ O, N1 z, Q# a) [) r Fa 7 A* `9 A2 e3 F' c0 K: g4 _Nose Cowl - Front section of the nacelle for air inlet' g$ G x4 H6 Z0 Q9 [ to the engine.& o% g! o' c8 N, {5 |- v Side Cowl - Cover around the sides of the engine.: {' U, I" G, ^3 @% Q6 Q Thrust Reverser Cowl - Cover around the core : A: e1 \+ ~ R& h" lsection. 6 x$ V$ t$ |# R0 @Translating Cowl -The moveable outer portion of the' Y; F' D% N- F7 @! k+ c+ q thrust reverser cowl which is ; I/ [( C% u: d7 m. R! q. @operated during reverse thrust. 9 |8 F* o8 ^( T标,$ P. G6 S: Y9 P, y8 A 基准线的相交点。一般以经纬度的度/分/十分之一分/ }0 ~- F. Z* R. j$ m( x* r+ x2 ` 读数来确定位置和方位。 ; _- A( Z. v2 |1 w$ z+ g* W k腐蚀 $ \$ o: v6 l# b8 g6 s# r8 M动机外部可拆除的罩子。发动机上的构件必须要取下 & h9 ^/ z* Y% K. ?流罩后,才能够到。 3 l. M; u0 o5 v! p! f2 n7 o+ ~" p" S% y机的短舱的前段。/ r W$ P: }3 X- z* Q 侧整流罩一发动机两侧的罩子。 0 c: Y% H2 A0 Z" ^反推整流罩一发动机主体外的罩子。) r/ ?: Z1 j# K, E& H 移动整流罩一反推整流罩外可移动的部份,在反推工) L. Y4 B' D! L* i0 y 作时使用。/ V4 S: j% N, |7 Q7 x u4 |9 O5 p8 c7 [) H o 0 o- y& w0 |6 o4 G* Ylocation. * a- a) o. v; V6 oRROSION, A chemical action which causes gradual: T6 C* p2 }, H' B: Y/ S8 p; {$ N4 x" x e surface of a metal by oxidation or) F! H5 P3 h& R4 C D+ C7 K5 t mination.8 B- f, O5 Z* ?, L2 U! \1 f1 x vable cover around the engine sections 7 _, t5 v0 K- ee components on the engine. 2 A) t% i( [& v! u& H2 _n Cowl - Cover around the fan section.; s" J7 Q/ l! {. A- \$ A2 | 转换, 8 }& s& H# o# Y; w% r3 R- A9 w改换到另一个方式。 3 n# b# S! J. J- \8 v: D; H& ~) g6 ^. G/ O$ s$ e0 u- P6 m. ]* j- d& p# F+ \, j; }/ k& c. S6 l x- L- R! _氧化或化学污染造成金属表面逐渐破坏的化学反应。5 u& k; C* D& A; o- ~( a" m 发动机整流罩, b4 _3 g A. y- ~4 S! b% @% I& c# Y8 I8 q+ u- X- w- ]' n3 T2 `, q) y* J7 G" n扇整流罩一风扇外围的罩子。( @1 ~* }$ c6 k' d1 s, J 前整流罩一引导空气进人发动: E( v/ R' _ {# L4 a4 F 英汉对照民用航空词典B OEING. Y* y* b3 H* e; z. a TECHNICAL DICTIONARY 386 ~2 }: A) Z6 v+ J5 T9 Y. E$ x CPU, SEE - CENTRAL PROCESSING UNIT ( a( Z8 H( H/ [. `CROSS TRACK, At 90 degrees from the desired track% F# s0 u' `3 u f the airplane. For example, cross track distance is the 0 i7 H, [. p6 f7 l, x/ F; @istance from the desired track measured 90 degrees: ^5 l3 T7 x8 l+ d) ]& _3 o' t/ f om the desired track. , \# z# q, y/ y% L+ wROSS-CHANNEL, Electrical wire(s) connected from% U, v" R- Y2 `( V ne system to another like system, for example, FCC( b& u% |0 l3 r& h " to FCC "B".4 ]/ f! W: O, a7 N& m n adjacent engine or one on the other side. ) V5 ^7 W# \" h9 V" Ol crossfeed 5 N6 G3 M% J! t1 T5 ]: aanifold for fuel flow from one side of the airplane to the8 a! m, U8 L& D2 c- F( r ther side. 7 n+ O% H( Y- s+ Qre 2 Z& W$ v; F! [2 L' l7 i! qRUISE ALTITUDE, An altitude or flight level ' X+ C9 `4 [, A& E: T( J: \: E: S2 e3 p2 x& F o6 D- j( d( l8 B3 T/ f d3 s h1 r9 o/ h$ P: g" V) B7 ^ F fr. r5 v. T* [* `4 k. t, ? C* z% U' y8 R- n' R) L1 h( z o ! Y% y9 B2 M' r0 N5 w3 P0 c B5 t"A7 W5 n6 v- ^* @) F; ]5 D+ H7 @$ N: A5 M3 n CROSSFEED, An interconnection between fuel 0 f1 z+ z* ?% \. [8 Kmanifolds for fuel flow from one side of the airplane to# x7 T. c6 h3 i- n a 7 ^! x: ~3 k6 C4 H3 |3 wCROSSFEED VALVE, A valve in the fue , O# q) j3 |5 J/ _& X `; bm ! L* j- f! z. j$ }/ T7 l) do \ ]+ ?1 c% c* P: \% ]CRT, SEE - CATHODE RAY TUBE1 u0 Y, f2 S: V5 F CRUISE, Phase of flight where altitude and speed a & u' q% k6 _ O$ o5 fbasically constant.0 O, o- d3 d4 l8 H2 S C; B4 P1 P: t" |7 ? n. t maintained during enroute level flight.# J6 M) ?+ R0 x* w" f! l 中央处理器 / b/ r5 {; Q, {见Central Processing Unit. 3 A6 z; _8 g/ ?% k; v! N, Z交叉航迹(XTK),1 x) s: K( o; J! { 与飞机预计航迹成90°角的航迹。例如,交叉航迹距离6 e1 n3 T2 q$ M( l! L 是用与预计航迹成90°角量取的到预计航迹的距离。4 z; I& V# i% C 通道跨接, 5 X a- W! u7 C& s; N2 l7 R电线由一个系统接到另一个类似系统。例如:由FCC ! J8 z2 j( H6 x7 d$ ]2 |“A” 0 h& S- R2 z3 w接到FCC“B”. $ t: n& w+ S. s机身另一侧的发动机。 8 G. z. p' B- f; i, f! X于使燃油从飞机的一侧 * |1 i: S6 Y8 P) l1 ?( v4 f9 {向另一侧。 , j' B! c, g* P) h' t. h见Cathode Ray Tube- m% [# ^( U: r# J9 M' ~* ^9 O0 h! ? 交输, V3 N8 l% x" Q9 b0 }$ X( v" p 燃油支管之间的交连设备。可使燃油从飞机一侧流向邻9 _) k$ @5 `4 ~+ a 近的发动机或在 " |! O5 I. ^" O) X! e: X交输活门, $ a& E+ I, u9 I) c* Y7 z燃油交输支管内的一个活门。用 6 ~! h1 ?2 e- \5 N, O: S! b& f0 r+ l: r$ ]4 D. B6 n 阴极射线管,6 w6 K+ I' ?* w; y; Z .; H; h5 D. R" l" B2 R+ a, w 阶段。 8 D; r2 c4 d8 g! X6 E! ^航高度, o# w1 v, b* ^+ P8 x& I 飞行期间,飞机所保持的高度或飞行高2 S( ~& G, f, I 巡航, . c8 |6 X" T8 V7 m飞机的高度和速度基本上没有什么变化的飞行- S: M, }8 t5 q# K4 w+ K8 V) j2 s4 u! B. y7 \在航线上水平8 P; [ {. b4 y# B 度层。 + W0 A0 j$ V: ]4 h9 o% }/ C( r0 M/ p* b* _英汉对照民用航空词典B OEING $ ^# B0 {% o. T, GTECHNICAL DICTIONARY 39 & P# F9 m% N$ @6 H9 I8 u8 @) iCSD, SEE - CONSTANT SPEED DRIVE% a; P8 x/ K/ D1 ? CURE, A chemical change which takes place in a resin 8 h7 S& ?3 h: s( b, t! c4 K9 Fand fiber based component causing it to solidify. : Q9 y# z0 N. ]CYCLE, A complete series of events that take place j; J8 n! \( y" `8 \gularly normally in a continual sequence. # i* {0 b8 s& \" e: @, pAMPER, A device for slowing down or limiting 0 J4 }. u! T, k6 r5 @; EDASHPOT A mechanical damper for slowing down 7 ?2 M. ~% I/ Q$ h3 X7 s7 W( y8 tovement by restricting fluid flow.; v8 w" D( U$ z1 y2 q+ \4 K D 6 x* q. Y9 |; i mATA BASE, Stored information which is used as the . c/ m f4 ^4 s' R5 g$ ~7 Zba 4 E. r1 W b6 ?& y* H3 gDATA BUS, A conductor over which digital data is .& q, g$ n6 P" w transmitted.: C' Y1 q4 w% l! Q/ ^8 T DECELERATION, To decrease in velocity. " Y# p0 A8 t( ^4 T/ c$ R' F装置,, F, ^( \* O k M* g" i8 U rive 2 l. k" i9 ]$ [7 Nre" w: a* E2 ]" G+ N" p& O8 e) w D/ q6 g7 m- j$ ]4 T Q$ Y2 @ D; b2 c: H# V3 q) Y& Z' ` movement.8 a& ^6 d6 c. T( \* ~: U m. Q- ~! x7 w3 U8 n) J7 L; w ATA, Another name for information.6 g! v' P" X k4 V D# n/ F: R: ]. d2 E+ Y sis for computation. ; j% K" H' Y: p3 D9 Q: Z/ G- `# d恒速驱动 2 L! \! o& J- t' Y, u8 w$ k见Constant Speed D .) u0 N4 L3 B o6 U7 M$ u* t4 q 期,8 Y+ l( _+ x$ y* b9 o3 }2 r" f 不断重复发生的事件的一个完整系列。% N N, A- `, Z/ H6 q0 | 尼器, 7 l2 b7 h- K+ A" X5 s0 P慢的一种机构。 * v" Y- q' @% t# J/ }" u, q- j! T5 ^' M9 z1 y. f 用限制液体流动的方法以减慢物体运动的机械式阻 8 [$ t8 E3 ]. y% ?/ z' D# p& o2 U; M7 r4 D9 u/ j4 N& A& L2 G 料的另一名称。9 J7 {$ K6 y: F3 q5 R* O! c& I) X 据库,* y3 S& ~( G% |) W) W 数据总线,5 x+ Z+ @) c) ?/ E# @# |" S 一条或一对导线,用来传输数字信息的通道。 + ^3 R, Y3 Q$ `6 f7 \减速,# x1 h$ \0 p# n4 `+ n' K: E% j. l/ J 速度随时间的递减量。5 T2 s7 L& A/ |. { 固化,5 m3 V6 U9 c6 P" e* }+ a0 _. x V 树脂和纤维部件内化学反应使之成为固体的变化过程。- O9 \+ ^ G/ R- L. x* H$ g; J; }5 m5 y, c# o" i% R1 R! s* p 用来使运动减 " z/ s3 e+ g; f冲器, ; B/ Y8 e: @* ~! r器。 , e9 X/ F$ g3 N* G( \" p" _5 }据,+ E* l1 R4 C# ^9 X( N: P& R2 b- A; a' R3 c0 s" f+ D+ K* s2 [" @6 R 储存起来以便在计算时使用的资料。 5 n% J( p* R8 W2 t" U英汉对照民用航空词典B OEING 8 p" ~) q+ j/ R# l+ OTECHNICAL DICTIONARY 40 * }3 B. Q. Z6 ] @* ]9 V4 d, C: w- }9 BDECIBEL (db), A unit of gain derived by computing the * ]. Y$ H$ O/ p- S+ b' N0 j, }tio of input power to output power. & N- z% ^( U& l) xECISION ALTITUDE/HEIGHT (DA/H), A specified. O+ y& T! O3 Y8 E! w( c$ G2 |4 a ltitude or height (A/H) in the precision approach at% Z0 b- [2 G! z hich a missed approach must be initiated if the 1 {/ M" B. x- x4 D! N4 OECISION HEIGHT (DH) 1, With respect to the 2 D8 h' ]' _+ {0 s! ~/ b6 P: E$ @proach or 3 ~1 Y6 V- \% d& j0 ^1 \( gexecute a missed approach. 5 \3 I; }' E# @3 o8 gproach to trigger the decision of either6 j7 x5 F* } r& k' T* m nding or go-around.1 e, U& T" p, n1 b/ r. T" F8 h ECOMPRESSION, The loss of internal aircraft air 5 B' Z7 s8 ^- R) }/ dressure.3 X- i) U" d. r; B3 j E-ENERGIZE, To turn off or cause to not operate.7 J. l$ B" t4 O8 U8 _* [3 b rom the tanks 4 T( n' P. y" Z7 \4 lusing airplane fuel pumps or external suction.- G$ T3 K; Z1 H, {, O& T2 j 算的一个增量单位。分贝 / U8 @. o. h" v$ U* g! K常表示两个声音信号或电力信号在功率或强度方面的% W- t: H f% r; K 对差别的单位,相当于两个水平的比率的常用对数的十3 S& O0 l/ d+ Y$ X- k9 i+ e 断高度/高(DA/H), / ?% j5 c6 l: m5 u6 Y7 a2 V在继续进近必需的目视参考没有建立的情况下开始复 ! w8 |, e# U. e8 b的精密进近中的一个指定高度或高(A/H)。- H" P1 ^# S% b- x5 {7 t 断高(DH)1,) l6 X7 ~6 ~; B# g' _" | K 操纵而论,指在使用仪表着陆系统或精密着陆雷 , p* E* Y0 w( K# N9 B1 A, Z8 _生继续着陆还是复飞决定的高。 8 e# \1 B+ U. b- t- a2 B/ V5 ?飞机失去内部空气压力。1 D& V7 O3 @( R; O 开, " P K7 M- _( v7 G3 e+ ~3 l关断或使不工作。 8 B" l: Q& A4 T4 W3 O$ n. x机的油泵或外部的吸油装置将燃油从燃油箱排 : K$ P& u$ R, v2 u: W8 I8 V出的方法。 ) Y7 b/ H0 q% j) _# S g3 tra 5 n3 J4 l- C4 d% y# A$ WD ( C( T' L% t. |a 8 |, B# J: c- |, Mw: p) y& P8 F' @ required visual reference to continue the approach has * i. i" {1 s' J5 Onot been established. + |& o, H# F* Y& ]9 hD$ n$ m. n/ A& L4 @! z) `/ q operation of aircraft, means the height at which a$ ]1 u: w5 L. E2 X8 I+ [ decision must be made, during an ILS or PAR+ c. N( A0 g8 S# X instrument approach, to either continue the ap/ q% w$ Z2 T+ v. T to 6 g" X/ w( P9 W4 ]% i/ z) c+ ?7 TDECISION HEIGHT (DH) 2, An altitude used during a5 _, W4 A2 D/ a9 w; L4 h precision ap ( w9 W# ~; k4 W& y% U# t: d0 i9 E9 g8 hla. Z. L; f* E' P2 A, T& p) j: Z/ Y D # ?; z+ ?0 H. Y3 K: jp . _: w( I6 p; z4 d8 R! A- h8 T. BD8 x# {; o# D% F4 u DEFUEL, A method for removing fuel f + z3 f# M/ X( H, W分贝," C0 |8 Y* C X1 H* b" m, N 以输人与输出功率的比率来推 ( X, p+ T# l. j( r4 U* i6 ~- s% n$ D; s' w" G0 k& o9 V, Y. d' z- p- m, z C( Z5 R) r0 Z% o7 j) |7 a8 Z. a7 y! l" r$ Z1 a+ ]( d8 c ^( e7 [) t- n& t% s1 _, J5 o0 \1 m( X7 I. I就飞机 d, u9 Y6 y( q' u- a, ]. C" i达引导进近时,必须要作出的是继续进近,还是中断进场7 @, G& A3 F9 s 复飞决定时的高。' I! {) q/ M: S$ J: z/ } 决断高(DH)2, % u& c( w5 s# Q& L- e# r. ?$ p精密进近时产+ J" i5 t! o" w" { 失压, 1 i: n" B4 C4 N& |; A" N) e2 Q/ `- _, [1 g 排油,* f2 v" c, Y' V' y. E' [8 U 用飞3 K) x$ T8 Z, K! |% ~2 e7 A 英汉对照民用航空词典B OEING 9 x3 Y5 [. p) j0 q7 m: HTECHNICAL DICTIONARY 41 ' \% I1 ]) p2 v3 r9 WDEFUELING VALVE, A valve in the fuel system for f7 A1 X" Y. z8 q efueling the tanks and for transferring fuel between the5 M- |4 h. Z' G' K9 i7 X E-ICING, Removing ice after it has formed on aircraft.( S9 b0 X) T+ `, [" b7 t' L Change or difference. 9 q5 p' O- L3 s: QEPARTURE CONTROL, A function of an approach , G; r# d: E0 j i6 D4 p* o/ gontrol facility providing air traffic control service for) n$ L3 Y. K) q eparting IFR and, under certain conditions, VFR) K1 |% ~ H1 F EMODULATION, The process of retrieving information, o5 ^" d7 {# a7 i9 Z, q carrier voltage. ) r5 ~) {7 z4 q# d( C9 Fation.9 B. I3 `5 J. G* Z% t lic, S6 D9 H/ {/ Y" l% J8 m F7 e+ U creasing hydraulic reservoir air pressure to & c2 P! B3 Q, u6 d4 p6 ~4 [0 ~; I- mmbient pressure.& o7 U! E9 D. Y, K! M; ~# z 箱排油和在燃油箱之间 % z( u' b9 W* ]4 o送燃油。, J0 [' W& a' E, L 冰, . I1 u5 v6 K# K2 P- U除去已凝结在飞机上的冰。 : z% e7 z; {3 \: G* x" }0 v/ j删去或取消。 ; W$ F! k: P( z量, % g& {9 ~ W# x变化或差异。( W# l. x+ o* X0 S7 f* G2 ]9 P 场控制, ( ^# W" b6 g! x. i& O. ^+ J给用仪表飞行规则离场,和在某种情况下用目视飞行 7 M( U7 | Q: W8 \则离场的飞机提供空中交通管制服务的进近管制设施 ) t9 X8 F: K" N8 o8 {, y4 L; z3 P8 G. ^" |. z2 _* `# l 调,: P/ s" h8 {3 H- j! \ 电压中获得调制电压的处理过程。 3 S' M( L+ Q3 ^* S# h& ~3 I0 h环境 % }. z1 x3 {, {; w* |% j8 |力相同的活门。- W8 F- \; _8 { s d2 T7 Z8 {% T$ C3 C* ~$ P tanks. 8 [/ d! R# k2 e, P3 v# ]+ nD' f- K5 Y6 J7 u9 n9 { DELETE, To remove or cancel.# ]) K7 G, v2 o! v; U2 O+ U0 S# ? DELTA, 7 a6 l, o1 k" F! JD1 {. x1 X! A5 L( g3 i) u0 q c - N0 |) H; e3 g" `d7 [6 h% X" I$ i5 ?( x( t aircraft. : e0 B6 M+ X7 I: n9 z- m: FD+ d& r1 \- A* b5 s9 T (modulation) voltage from a modulated" @3 R* @* U d9 R4 }" T0 s DEMODULATOR, A device or circuit which performs/ \( i8 U- {; _ the process of demodul1 z, o) O1 `! c2 b5 t9 f& W DEPRESSURIZATION VALVE, A valve in the hydrau$ Q. Q) M3 i" {. h. Z* y system for de 7 U2 |7 p: H' K% f+ Wa" \% `/ E5 U ?) ~( o4 @! L 排油活门, # h( }/ X4 I. q% N# u9 K) {燃油系统中的活门。用以为燃油 N3 u" `' ^& M" C% P2 {6 w4 U0 E" L1 R% y, s' Y3 P! x" J0 s3 i0 X' k6 n" M删除, 8 p6 L, i; e, h: P; A: _! U8 X* f+ s8 P/ S9 Z( E* S: ~$ B5 c( |& g& i" O" z: v* I7 u, J+ W 的一种功能 $ k- l: B7 O; R# }6 i% X$ h ~5 \& O从载波 8 [# _$ G- y+ h3 Y解调器, / g& J8 z! E- N完成解调过程的装置或电路。8 |- O9 T+ z! y) ]) l 减压阀, W! ^+ t5 {" U2 a* _% k/ `在液压系统中,将液压油箱空气压力减至与周围1 {9 ^1 r6 G( B/ ?& v$ w2 w7 L" }% N" L# T( X( l. N 英汉对照民用航空词典B OEING * e- F1 Z% a6 bTECHNICAL DICTIONARY 42 % C1 l F& R5 ~* T6 ^! pDESCENT, Phase of flight where altitude is decreasing.. H1 l1 k6 z9 g8 |8 O ETAILED FLIGHT PLANNING, The calculation of fuel- R+ S* j$ u/ | nd required for a trip by considering each phase of7 S" \% N) e0 E ight (climb, cruise, descent, reserves).; H- V, r4 [, i8 r. Z al or . T: y7 M( B) Z$ i6 T3 ~- [ETENT SOLENOID, An electrical solenoid used for $ L6 Z9 }: q9 V1 H) t& b* ct. 2 Z& u5 }5 q c9 _# k8 \specified course or $ X! ]* Y7 Q) [5 u: Q- ~& N: K% Drocedure. " F! P6 X; f, H* X# L7 {e.0 ^5 t P% N! N1 O; Y5 M* | 飞行计划,, a9 ~0 I: } V9 B8 M5 i) p- s 将航班中的每个阶段(如爬升,巡航,下降,备降)都 ) Z# R/ M/ w+ }% X' G5 R. x人考虑,来计算该航班所需要的燃油量。 ; z% c4 q- ~ n- ^" T# c! U8 u6 s用来感应情况之正常与否的电气装置。 * P/ d6 U& h" Y$ H7 J定电磁线圈,( @# r( k3 d# f 出接通的电磁线圈。) \" q: K! r4 ?% B4 n0 Z 差, F; I. G w% c, c) |与指定的航道或程序之差。 ' ~# s3 p* }1 b# O6 Y/ Z2 i用气压或液压操作的活门机构中的柔性部件。 ! ~: V8 @4 e/ _; fD , Y+ T& Y: h2 Z; y% J. T% ]a' a! J2 e, d8 {5 n fl! w8 ?! z0 B, T& _7 g. e o DETECTOR, An electrical device for sensing norm # H$ l; Y) W4 C- e0 eabnormal conditions.7 u' O* |% T1 d7 v. @. q% |6 x D . ]/ Q) Y5 {, b/ R) m4 U# B0 Mcontrolling the engagement of the actuator outpu . i* o8 B( ~( \1 }0 k G# T2 TDEVIATION, To change from a O; _6 v9 V I p' T5 X8 M( L$ @3 o. d DIAPHRAGM, A flexible part for operating a valve2 w: h6 K ~% H mechanism by pressur8 r) K* r* P* o5 a2 C4 n 下降,9 K& B! E4 n5 p* Q 飞机高度不断降低的飞行阶段。4 G a) L3 a8 p. z8 V& l, e 详细 ) ]# O& Q- m# D( K c& K: d# R8 `0 z* c d P2 v1 u G+ R5 A 探测器, , x) A2 a; ~7 N, e1 ?0 F1 M8 Z4 q) ?& i* q- W. ~" B3 H2 {% n! v 用于控制作动器输8 U8 U. R0 f. Z9 E' S& w$ k( N2 E5 e; b. b 隔膜,, Y& ]$ X) W( w3 r* o" u 英汉对照民用航空词典B OEING ) K8 O& n/ z6 Q8 _& |TECHNICAL DICTIONARY 43 + H' `& Z" p G* gDIELECTRIC, A material which does not conduct/ g) ~ u5 h2 _4 u2 E electricity and used between the plates of a capacitor, V3 N: C- g _+ Z! x (condenser).5 g5 d/ O' h; W) @6 P! @ nother pressure in the same system, measured in # C' t' \6 t' f0 Uounds per square inch differential (psid). - I, U3 u( V7 C* e* f, GIFFUSER, A part of an engine between the+ P" j8 m% G4 o+ G4 G ompressor and combustion chamber for reducing the7 n+ B: N$ }0 S& |8 m" o9 W air pressure.# K* U$ G: p, N! T7 m igh " c7 e0 |2 w; \5 b7 X# @/ Mpulses.1 q F1 B# B# }5 D ignal that is a close approximation of the original' _6 B1 Y# N$ e* R1 R6 z ignal.! U3 b) Q0 B: N( F0 F/ v5 X IHEDRAL, The angle between the wing reference 2 X+ W: H( S: A4 R, n- elane and water line. " _! f. |0 x3 D# y B* Y的压力,以每平方英寸 ; [; R7 q1 @' K- |; \, ~- G少磅压差计算(psid)。1 r& I9 y& f8 H% X" r4 H 散器,; t$ L5 C1 G* s2 a! D) K/ m 发动机内压气机和燃烧室间的一个部件,用来降低空$ _* o' m$ {; \6 C: L# G, P1 z+ V 增高空气压力。$ @' y, N& s7 U+ T 换, 0 P3 i7 N! q+ }! {的连续可 ; Y) Z8 @' {8 t(模拟)信号的处理过程。 7 H+ R! [! X- L+ x反角, , r0 K w/ C8 j( H/ C8 `7 _8 R机翼基准面与水线之间的夹角。; J8 n" L- i; E% g DIFFERENTIAL PRESSURE, Pressure relative to 8 E+ ]) G( y: L) ga' |' z: R: s! P. B$ z p1 R3 p V- O9 ~' J9 |, \! j D9 W( D& p2 \0 \' B/ C2 u5 B c , b R. J( t A2 ~, Kairflow speed and increasing the . T$ F) t$ \) O1 o" S* RDIGITAL, Digital refers to a signal whose amplitude 9 O& N. X. h7 J7 h% G$ U6 Vremains constant for a finite period of time. Digital$ M0 z8 A$ C" ]. o' v3 O4 L9 @ signals are commonly represented as a series of h6 C7 `% ~" [' N' x2 f and low4 h2 [0 H% _* }; X' V+ }5 Q# Q DIGITAL-TO-ANALOG, The process of converting a ! T5 ~: X0 r. N' {* K( J! m) W7 \digital signal (binary) to a continuously variable (analog)- j* X" V1 n( t- X9 g( X s$ d+ ]( H5 M3 T& Q8 n s * ?( ]9 v2 @% X& WD2 w* q: X5 O/ j6 g9 g2 z4 ^6 h( E' ~ p # l& i; Z. @& s& t0 J8 s电介质, z# [1 V% f) l" _' c- z8 l 一种用于电容器板之间的不导电的材料。% x- m! D& Q9 E; s' o } 压差, ; P+ Y% v6 A' {% T相对于同一系统内另一个压力6 q% _( b1 n7 H# F& B" [* i7 \, g7 J- M6 D1 [$ n# P' z7 P$ G( Z% [9 t; {4 u7 R 气流速并; a: Y* z0 C; Z3 S$ Z 数字式, p8 O& k% r1 x9 q% D6 E1 M3 f4 Z指一种信号。该信号在一定的时间内,振幅保持不变。 * O. ~: _0 p8 R3 X0 j' d" ^* c通常由一系列的高低脉冲表示。 7 e1 R4 `: U. {+ L6 ^数一模转 * `# ^ b$ }. x& `将数字信号(二进制)转换成与原信号相似7 M) f( V/ A/ S3 |6 j+ W# i7 Q4 v! _) F, }. O' w0 K" d2 D/ o2 }: B英汉对照民用航空词典B OEING9 ~+ ?' I8 m e2 D- s2 Z5 G TECHNICAL DICTIONARY 44: ?' z6 j( S4 f/ v( O DILUTER DEMAND REGULATOR, A component in the $ `! Z1 z: a( j" H6 L9 T" c4 A" r( Ucrew oxygen system which mixes air and oxygen and, p5 }) N/ k* k( m4 ?. F8 D' `& u upplies constant oxygen pressure even if there are6 X( ~6 a0 n1 p/ {; ?, b hanges in ambient cockpit pressure. 3 W" m M% F9 a9 @2 }) FIM, A word value of light. For light control devices - dim G' @# d* I4 A) q0 ^1 {# ` the opposite of bright.3 ~, z9 |8 m. d4 h) x IODE, A device which allows electronic current to flow: O, o! {* g! `9 E# f7 X only one direction! U) E3 o4 l1 `3 W) ~ uid in a reservoir.9 N: T M* R! v/ g DIRECT, Straight line flight between two navigational # I: m- ?) v& L/ {aids, fixes, points or any combination thereof. When ; [6 t( E7 C9 I. ^' ]0 hused by pilots in describing off-airway routes, points- t( Q( O) |% T+ m$ Z+ S defining direct route segments become compulsory+ ~7 X% H7 f: K reporting points unless the aircraft is under radar 9 B. a8 F6 A% ~6 o- Q, a1 n/ j9 Ocontrol. # g# H$ C! _6 h3 g1 L节器,7 J0 \# T! p, p( J7 A 将空气和氧气混合,- Y' P# t+ h3 p+ c2 P1 Z 使驾驶舱环境压力改变,它也能提供恒定的氧气压力。: D( Q& {$ m! f* {* N' @ `6 Y. W: e 一个形容光线亮度的词。对于灯光控制装置,暗的反$ \& z( H, w4 X2 l9 l 词是亮。# G& O% `' n0 r, S' V$ E 极管, $ _7 ~2 z& o* H" i7 u+ B只允许电流向一个方向流动的电子装置。" G7 _- _0 r3 w, ` 器内液体的量。 ; b0 N* ^7 o5 j" s T: I直飞, ' H' E* x" V1 R) j- y两个导航台,定位点,导航点,或任何的组合之间的直( ?2 l/ Y3 R. K1 E$ E 线飞行。在被飞行员用于描述偏置航路时,除了在雷达控 3 ~+ m0 I4 H/ v制的情况下,确定直线航段的导航点成为必报点。6 E/ q6 Q) m! v5 z s . [! W8 z' I( g4 l N% xc! }6 h! b( u/ S% m/ w/ P& P D ) o6 G+ ~& k* z. e3 [' Q( Zis) V5 Q2 L. b. U- v D6 B8 V+ r% x; c' y8 ~ in3 P4 N6 P) Q1 s% A DIPSTICK, A calibrated rod or stick for measuring a( l- p( c2 V* _( G. \$ t7 p quantity of fl " C5 N4 c! a q7 N' M3 P% R H8 D3 C! I L8 {稀释氧调0 w- J1 }( _. C- q 驾驶舱氧气系统中的一个部件,它/ b( C, f8 J, ?/ r* M' {1 j9 l( N) k. }+ _' i" T# M" S" M) M- j0 U- ]- h4 o. C# Y9 E6 _" G5 [7 V* R* k; F" O" a$ s$ t; F& r/ x 量尺, 9 J7 S, X8 P/ M+ Z8 A) y4 ]校准过的棒或尺,用于测定蓄液 , Q& Z2 [) f0 s/ C+ e* E英汉对照民用航空词典B OEING. U% r4 |& o: w$ q1 y TECHNICAL 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, 2024-11-22 09:15 , Processed in 0.057003 second(s), 9 queries .

Powered by Discuz! X2

© 2001-2011 MinHang.CC.

回顶部