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: 7629|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6 S& N; Z% Z- G. a; Y5 ? 民用航空词典# r) X; i. w5 W/ s 波音商用飞机集团 - ~ E& b( c" P" h4 OBOEING COMMERCIAL AIRPLANE GROUP; C* f% N4 i d4 Q 英汉对照民用航空词典B OEING 8 z5 b( k. h1 k' V, ITECHNICAL DICTIONARY 1 : D5 z5 D( p* f9 y9 HA/ r6 w# ], y3 `) o4 `3 c8 S! t! u ABEAM (ABM), Beside: An aircraft is abeam a station 0 h( Z; _6 N4 h; z8 S' Zwhen that station is 90° to the right or left of the track of- w2 N3 _& k. m' g the aircraft." ^# x. J J! A9 _1 U ABSOLUTE ALTITUDE, The actual distance the aircraft3 M6 h# V4 l" ]9 e. h5 ^7 t* I is above the ground.$ h8 i# n a% V1 b2 l ABSOLUTE PRESSURE, Pressure of a liquid or gas 3 M" Q( h$ e, Xmeasured relative to a vacuum.* ^+ q3 w+ @* P K1 k ACARS, SEE - AIRCRAFT (OR ARINC) REPORTING 5 k+ P: C; h# r2 S+ v5 J7 C0 mADDRESSING AND COMMUNICATION SYSTEM3 y9 g/ B: e* I& X& p, m" m ACCELERATION, The rate of change in velocity with$ B5 q# o0 c. F: M8 s+ \8 o respect to time. : {' ~2 V! Z% q' `: J1 Z. XACCESSORY GEARBOX, A part of the engine, 5 w m0 I& Z3 x+ P( Y# ^7 Emechanically driven by a compressor or an angle# B- S, |& g, q/ A0 \ ^ gearbox, for driving components necessary for engine# y# ]& I, O) S4 J z6 W 正切, " K# k2 P8 p* F% [and airplane operations. ( w+ z$ J* {$ H! D7 J( I" j/ r当电台在飞机左侧或右侧方与航迹成90 度时,飞机正' h0 ?" D0 n- A! E: m) c2 Z: ` 切电台。# n* ~$ w1 ?2 F7 `9 U5 L 绝对高度,2 x$ y4 x3 E# @* A' l! u% q3 z 飞机离地面的实际距离。( s4 Z9 A" x3 r 绝对压力,8 ]; F* l1 R0 |/ e+ T: r- A5 R5 | 相对于真空(无压力)测得的液体或气体的压力。5 y6 o/ ~# s: D& s4 m* g! B 飞机通信寻址和报告系统, % V. |0 |2 W3 }" I, [' m, Y见Aircraft(or ARINC)Reporting Addressing and ) o$ Q( {+ f: @8 PCommunication System. ( O5 p) z" r3 ~% f& K加速度,% @# `7 i/ o2 O 随时间变化的速度改变率。- Z4 g+ _/ z0 w 附件齿轮箱, 8 C: q( r# @1 [% P" R发动机的一部份,由压气机或伞齿轮箱带动,用来驱动1 {# `; O/ G) v( J 一些使发动机和飞机工作的部件 , O. T$ g- z6 G* x9 `: g' G! A4 E0 p英汉对照民用航空词典B OEING - Q8 P; y; G$ G) D8 U ]TECHNICAL DICTIONARY 2 0 N& L* Q( l0 \( I1 h! E0 {; HACCUMULATOR (NO. 1), A container with hydraulic! A5 \5 n8 X q5 U6 a# K: M3 K ts when normal hydraulic supply is not1 R7 n) q. {5 P" T: m) ^( P: K vailable.7 }( { e8 t5 Y8 @- R0 s CCUMULATOR (NO. 2), In a computer, a special% r. v( i; E, Y+ p6 G torage register associated with the arithmetic logic unit, : e6 X, D: ~* C$ Y9 G% Solding the results of a computation or data. @% O1 T+ p- J# |1 j# y4 s$ U ACTUATOR, A mechanical device operated electrically, & X0 ~1 i& T) o: W2 h( M) O4 V+ }7 chydraulically, pneumatically or mechanically for9 W; g; [) @0 z, y transmitting motion between components.- J6 K" X( I9 Y9 D# D% E ADC, SEE - AIR DATA COMPUTER O% ]% y4 _: f. F ADF, SEE - AUTOMATIC DIRECTION FINDER+ _4 A7 |: v7 ~0 L' h' L ADI, Attitude Direction Indicator, An electronic display of ' J. X) ~$ O& f5 fairplane attitude information in pitch and roll./ a$ d7 O# r, ?1 i2 B" O! g: o 蓄压器(NO.1),4 m0 s+ g( M9 g ?& n 含有靠干燥空气或氮气增压的液压油的容器。当没有正 4 B" {2 }) z. w, s& q8 Q常的液压源可用时,该容器可用以驱动部件。& T, a$ O( t% \* O% @6 O* B 存储器(NO.2), % Y% q7 V9 ?# g7 v& g5 A计算机中,一种与算术逻辑组件有关系的特别存储寄存+ r3 @8 B: b6 B& F7 K8 f 器,用来存放运算结果或数据传输。 8 H% O/ r* O2 n( g4 I0 E' V飞机状态监控系统, 7 D8 Y7 d& v. h9 X见Aircraft Condition Monitoring System/ ~- t* g1 ?4 L fluid pressurized by dry air or nitrogen for operation of; b5 s* ]/ ? C5 ]( K componen+ D* ^' y, d% j a 3 {' w7 ]4 [0 X, D# n9 ]A1 d4 d9 B& d5 L" d0 @ s/ D1 b7 _$ L5 g& H: O used for h ' ~$ t/ F/ o" J3 V1 X$ B; v7 htransfer. 7 A& J# {: {4 j; k. kACMS, SEE - AIRCRAFT CONDITION MONITORING4 H+ ?- g; _/ w6 D: M' M$ p# l+ W SYSTEM . 4 c9 Y- @' k$ d# R! }! D8 |作动筒,% V# @$ A, s5 \1 B+ N$ L 由电,液压,气源或机械驱动的机械装置,用于传送部8 e( X( {8 p5 B 件之间的运动。- w/ t( F }7 m$ t 大气数据计算机,7 I/ s4 F3 Q5 b1 T3 K* w3 n+ k$ ~ 见Air Data Computer.0 n3 J7 N" Q; [( V! f 自动定向仪, : P6 v$ m% H2 ? \% ~% u见Automatic Direction Finder. ; g+ @% Q2 K) j/ t' P. c# P, ]9 h2 X姿态指引仪, ! `6 R& w3 i) F用来显示飞机的俯仰姿态和坡度的电子显示。+ [+ c# s8 h0 ~ 英汉对照民用航空词典B OEING / v/ g' E% T# X; f; aTECHNICAL DICTIONARY 3 # Y+ t/ o% E$ PAERONAUTICAL RADIO INCORPORATED, ARINC is , H6 j- V4 G- L* y u1 Q. J( ?5 j, , F8 i2 a, D0 X: V4 R% K9 O. ^# ynufacturers, and foreign flag airlines. ARINC: M/ x6 M" N) x! R1 ? P3 y- ` evelops and publishes standards for electronic# [7 p% \$ H) O v* K2 A% Q quipment and systems. : a6 L& t) F, ~8 I9 S1 z5 {) YGILITY TUNING, The capability of the DME to 9 Y h0 Z% C3 h( N' ?lternately tune between two different DME stations in 9 t# b7 e! s) T1 f, Grder to get two distance readings from one % {4 m8 {' }1 e2 t; Z7 Oterrogator. ! L/ ^/ y. ` Z6 D; [7 ege 1 N5 O3 T& O! YILERON FORCE LIMITER, An electro-mechanical# X% t% q- Z8 A) C4 G. l IR CLEANER, A component in the pneumatic system 9 S/ u+ A4 E1 U7 W3 x& A0 v, x( Kupply to the air8 ^; R8 k( Z" }# t) q8 W onditioning system. 1 V* Q' ]- y/ T5 W$ z# H4 O订并出版 * z( O g' I6 `子设备和系统的规范。8 A5 F9 N9 P* V0 W- i$ g# _6 L 快速调谐, ( k* W- @ h9 A" x0 G机载DME通过交替调谐两部地面DME电台以测得来自! S8 |+ ?! y2 L: `/ e/ |( a- h1 x! t 同一台询问机的两个距离数据的能力。 7 L) Y" c! `4 F; d6 B- g翼操纵力限制器, : a" q4 m! ^/ D4 k) Z4 s' [/ d装置。在自动驾驶工作期间,用来限制驾驶盘 - x1 v, l4 l, }( h7 Z* C" {5 x4 z气清洁器, 4 `- R6 o1 T) o部件。用于去除供空调系统使用的发 , f8 p- W' Y; ]+ J+ H; fa corporation whose principal stockholders are United - B3 s) X& E5 V7 VStates scheduled airlines, air transport companies1 _" G# }* [( S* g aircraft ma ' G: T1 u* \; td r+ M3 k9 [/ Q. q) ^ e ! G8 M* h' i# d0 M. oA 8 e( M j1 P; ?6 p: @! ga; @" ?- s/ F0 `3 M. [$ q o5 A4 H* C) l- ~ o in / [# c, j4 w7 V' Y# g. w' gAILERON, A hinged moveable part on the trailing ed: Y4 _# S8 o3 n* X; f of each wing for airplane roll (wing up and wing down)/ H# G/ i$ v% B) P$ M. P control.; W L; P2 `- Y A S2 k/ K; A; V4 p ]device for limiting the control wheel movement by the 0 c" n- U. R$ k) P' q+ Wautopilot during autopilot operation.% R' U3 e- x% w" b7 r( _! j A * J2 Q' v& W; e l; p9 Ffor removing dirt from the engine air s ) N) i; y" \8 m8 {) Lc % U* \: N' w; ?' G! P; v4 R航空无线电公司,& x+ D5 j4 L% @+ S9 d 主要股东为美国定期的航空公司、航空运输公司、飞机 ' X) A3 w6 r) C: u- T制造厂和外国领队航空公司的组织。其目的是制 * |+ o: m: O# i! [8 T7 {: w6 W9 d0 I5 o+ q 副翼,4 [# ~/ s5 Y# y, t9 x 铰连在每个机翼后缘的可动部件,用于控制飞机的滚转 " {7 o n$ S; \& l$ M" h(机翼向上和向下)。 ; A7 m+ Q2 m+ L' K; a$ D* P0 U ]1 V: ~7 A! ]) Z7 n一种机电 ' x' T- {# x6 _4 S5 a. ?) {的动作量。4 E8 Z( ~9 c: a2 t+ L. _! V' N' {5 ^4 i( ]气源系统里的一个! m, n' r# S5 l 动机引气中的灰尘。8 d! o0 G J8 {- G6 K5 @% q- \ 英汉对照民用航空词典B OEING 6 ~: P! w) v/ |8 C9 KTECHNICAL DICTIONARY 47 p) {! S5 B1 N6 {% S" l0 j, q' e AIRPORT ELEVATION/FIELD ELEVATION, The0 u2 r, Z% w; }& S, v2 A# f highest point of an airport's usable runways measured7 B& i: {. H# s: J& x* @* {9 _ in feet from mean sea level. In a few countries, the$ F: h7 u& F2 W airport elevation is determined at the airport reference* i0 A6 n5 A2 l9 n point.( j! c8 S( @. }$ q+ N" ?3 o AIR ROUTE TRAFFIC CONTROL CENTER (ARTCC), / ^ W& f( u* \3 Pervice5 Q5 F. E/ {9 U+ m7 t0 M4 { ase of/ F4 ?4 `& T1 B us flow of air traffic.! P! C& @, E, t' Q" _2 T- e _- Z IR CYCLE MACHINE, A compressor and turbine on a5 M6 R/ r2 f/ K+ u/ i: @2 ?, E ommon shaft for cooling the air in an air conditioning8 }9 r2 y$ j" T8 S2 E ystem. The air is cooled by expansion from high to low , r, M, }. x. `7 ?6 {ressure across the turbine. The compressor is driven 7 C* ?9 ]1 ?) ]+ m+ }* j7 B3 R: ?y the turbine. $ ~; W, l5 I: j5 X% a中航路交通管制中心(ARTCC), 1 T# u7 d5 t0 R域范围内使用仪表飞行规则飞行的飞机提4 A, k# _3 B9 x$ G 管制(ATC),# k, [5 k) I8 a3 I) I6 o2 d 涡轮冷却器,, O% _6 v+ y" `' q 是装在同一的压气机和涡轮,用于冷却空调系 ; k" ^8 i! N+ p( s' b统中的空气。气经压气机压缩后,由热交换器移去热量, B( e$ u. L9 F0 P1 ~+ ]然后经过涡轮令涡轮带动压气机。通过涡轮之空气,温 " @7 Q; S0 _4 N, [3 {' b# d度下降。: B2 b% O: \0 l9 Q1 k A facility established to provide air traffic control s : w4 F* P) g* y6 y% u+ j7 Oto aircraft operating on IFR flight plans within controlled/ c1 b8 m; V* d; G% q7 j! g! w' m airspace and principally during the enroute ph- f" E" _: Z" ?$ b: b4 p$ ^ flight.' ~- B6 o' e. k% c. X1 v" g AIR TRAFFIC CONTROL (ATC), A service operated by. X @5 e! S( [: t; C appropriate authority to promote the safe, orderly and * a( ^. ^* B9 M. V0 ~: Dexpeditio . c( n0 s, ~+ v, @; N( ^A! p1 S, A7 W- ~+ i! F! Z c / Z }, f* L5 \. v. Ys 1 @, ], p o0 t0 j! A$ ~9 Hp - M; o) k9 v3 ?$ tb. e- q( o1 O$ B 机场标高,) J1 [+ Y2 t' w3 }( D 指海平面与机场可用跑道最高点之间的距离,单位是英 " C: P. D+ Z( Y尺。有几个国家的机场标高是由机场基准点而决定的。# c3 \4 z8 \7 T7 h0 \5 F% G: [% z+ \% N z( O 给在控制空 $ {$ j8 ]; L# i( ?' l+ }7 C( e供空中交通管制服务的站台。- G# J @2 T% C5 r+ \$ d 空中交通 3 j3 l% C/ x" J K; d! e) v由有关当局管理,旨在促进安全,秩序,和效率的空中* U- v+ s/ [8 w8 e9 D 交通服务。 6 H/ v) n) Q) m% _, D7 J, Z根转轴上4 q e' N5 Z! N/ u" m2 g* `- Z( z& b \6 l6 i+ {3 { P英汉对照民用航空词典B OEING2 }9 {/ K% { X c 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 $ y, n8 \/ }1 H' _data information, such as altitude and airspeed, based / W, X2 T4 D0 |4 I" hon pressure and temperature measurements.: Z( A" N# ^( U# B9 n es air% W6 h& D3 T; y6 U IR TRAFFIC CONTROL, A system comprised of ( U+ D/ v X3 z& }round and airborne components used to identify, track 6 ^" t4 e+ Z' E- L4 m" WOUND SENSOR, An electrical device operated4 h* T3 W# c% { y the landing gear, which transmits on ground/in air 4 v3 h4 ~) e6 w. g# jformation for system operation in flight or on the, t" S+ c- l5 g. P' F4 Z* ^# W round. 4 ~! K- }5 \2 e9 e2 w0 ?0 N2 }IRBORNE VIBRATION MONITOR, The AVM takes * i0 ^# w( o# g9 me signal from the engine mounted accelerometer and% g" P* m' A; g _8 E; E+ k" J alculates the vibration on that engine.( a& @3 @3 W. ^0 K. D, { corridor equipped with radio navigation 8 s5 O; z2 L" `2 ~6 @5 ]aids.! c' u. s! x- B. g6 k AIRCRAFT (or ARINC) COMMUNICATIONS + ^: N( U2 f' _/ p- Z& HADDRESSING AND REPORTING SYSTEM, An - y8 F' b) q" m! |3 raddressable digital data link system which permits the8 P0 u: |' ~: { G exchange of data and messages between an aircraft - I: w* t( O9 K2 M, N4 C; _and a ground-based operations center over a radio$ A( i! f* l) ] network. $ @5 I4 Y8 t: ]AIRCRAFT CONDITION MONITORING SYSTEM, A4 r% c) R' E; f% ?5 c system of sensors and recorders to monitor various2 z9 F9 B Z$ D; G$ u+ J airplane systems' performance and status.6 v& \, t u' d3 C' p- T 机, 6 m- y9 m! ?* s0 V+ @中交通管制, : E( J, w. r- Q1 a) ^: N/ Z一个由地面设备和机载设备组成的系统。用来对飞机进 , R+ }# t/ r( ^$ d地传感器,/ p0 k! V3 Q& j5 y2 S& [ w 一个由起落架操作的电气装置。用于给空中或地面的飞: X' H2 Z* l7 H: g2 U, k7 K+ j 系统运作传输地面/空中信息。(有些系统只能在地面 ' c. b8 ]3 H7 J: i5 R用)2 T) w+ a4 d8 n$ d T" k: g6 S 载振动监测器(AVM), , ?, t5 h5 X+ m" n; TAVM从装在发动机上的加速器取得信号后计算出该发. t$ x6 N8 E+ s" H% I) K6 v+ a 机上的振动。4 ~0 l, g& h+ Z' r 式建立的控制区域,内有无线电导航设备。6 T# S7 |3 K! _$ e& E 飞机通讯寻址和报告系统,. z. o/ q ~# e- J( p" a 有种可寻址的数据通讯系统。利用该系统可使飞机与地 8 {1 S) Q3 C# D. Q- W3 i1 m) J3 K面操作中心通过无线电网络进行数据和信息的交换。 . q" x; W9 i0 N8 h飞机状态监控系统, u/ ]9 E, V5 ^% ?$ y A- H+ w 一个利用传感器和记录仪对各种飞机系统的性能以及 . s2 ?/ S+ z5 K2 R* H状态进行监控的系统。3 O# C% S E; k A * c3 J) a' Y- j* ~g ) |7 y8 K) E. M, j2 R; E5 mand locate aircraft. 3 Z4 F! X9 ~# ~' R1 g& PAIR/GR d$ v, O8 e- I0 Z; e2 {b# |' W0 j% ?5 ~ u/ c! L! o' j in7 C# A. l2 i& Q g " w s# x9 W4 {- ^- c. U1 W) Y: \, mA( G% X: \# }4 V* z2 W' c4 C th9 X! y8 r" d# ^6 n c $ i ^; ?5 `) C' ]$ J! H3 ]- xAIR WAY, A control area or portion thereof established & X0 ?" g5 o6 ?/ Y" q/ Hin the form of a + I, K! p& @" _1 Q' o- P大气数据计算3 ?" c# @! N, M1 Q& Z; ]5 m' }9 I 根据量取压力和温度而产生大气数据资料(高度、空速 9 n/ O2 h# F; z等)的计算机。7 {7 Z) \$ Q* P6 o4 A- S7 m8 s1 e( U( b+ B7 s$ y2 T: e行识别,跟踪和定位。 ! ~: o* S$ P) p0 h1 Y% e3 w+ t) }1 A; k2 o! y: u* c1 Y! S1 g1 N" y% c" @4 G: i使 + r+ a' a, X& q A9 b$ G' Y1 K7 o6 [$ p2 x; q3 ?. j0 ~4 t! z航线,* y7 ]" f$ f, b$ w- r: } 以走廊形 ; Y% G/ w0 _$ U/ c英汉对照民用航空词典B OEING P4 N) Z; o/ v TECHNICAL DICTIONARY 6 3 l& \% k; |7 N: p/ p% FAIRFOIL, A surface designed to obtain a useful reaction, 8 P! r) L6 G3 ]( n6 Y/ U* ]7 zsuch as lift, from the air through which it moves. Wings,2 e4 P C1 r; t# B4 i* f# W stabilizers and control surfaces are airfoils. - M5 [" g9 `6 |; R; u: g7 BAIRSPEED (IDS, TDS), The speed of the airplane5 b4 i7 c. W3 h8 u# @/ Q4 B- b& T. S rough the air.: z5 Y" F3 V+ W# i' G0 M& W- B1 ^ D INDEX, An adjustable pointer on the & `5 k" ~ ~& r. c( O4 rirspeed indicator. " G1 @+ E: ]0 h& P. q1 nand legal ability % T- K; @3 z D6 K, X) `: a0 qfly. + g! v/ l+ n/ n5 u% D6 zm, for example, the procedure for finding the 2 x: D- y/ N' l9 G9 x7 n \1 Pquare root of a number. - O6 @% e; ]9 B* P9 g2 \y( N9 h$ d* H0 `7 \ re, wind, ; X- x! j' M; ^9 d, Y8 ?and aircraft flap setting. ) g! _1 d3 o9 _; _1 e' k5 K0 S是翼面。! O6 u) T" b7 [! w; K+ x 速,4 {" }0 x7 ~# H 飞机在空气中运动的速度。 / M8 f: K8 L1 |* V( J! V* a6 u9 E2 A8 o, R% Q; O/ ], | 在空速表上可以调整的指针。 ' [; M. b6 p* J8 s机械飞行能力、和合法性的飞机状态。6 w# j7 Q$ F; ?6 i: n 一步一步的解题方法。例如,计算一个数的平方根的步 8 h' o I: \5 m) D$ d- U8 i5 m* R5 M4 {7 {$ V9 T7 e- ?9 M; s8 b f" ?* D6 Q& x 资料的法定文件。% R8 F! H" w' X4 ]9 \ 翼位置成函数关系。 & q) M+ x H1 O1 ^th/ I. |& a. w8 ^" m( P, T AIRSPEE$ @! J2 u4 d: v a # F: P K+ M9 y3 KAIRWORTHINESS, The condition of the aircraft with% J5 e; m6 x. A. b& q. P respect to its aerodynamic, mechanical, 6 E4 @1 }9 l6 D8 A$ w# Y# |% s: j: hto K& E* w |2 @, ?ALGORITHM, A step-by-step procedure for solving a" O: u4 Q" T2 `9 {/ n proble' {, _) O; x2 } Q- N s) p6 Q- C- p* f AIRPLANE FLIGHT MANUAL (AFM), The legal $ p$ |8 K' L7 r. W. C% {document containing performance and operating limits,: u2 ^9 F5 V, x" w% B operating procedures, and takeoff and landing) j! _ s- k0 K! t4 R performance.8 S, ^( p2 C2 N- h. i9 Z AIRPORT ANALYSIS, A comprehensive set of takeoff' u1 N A/ K& a1 @, o* ^9 N weight limitations for a given airport runway, generall $ T% u2 I; p: o& b4 J3 apresented as a function of airport temperatu / C0 g8 U2 X' {+ r翼面, 8 F" C. x* u- \% i: o0 K7 m2 G( o4 N) Y用以从气流中获得反作用力(如升力)的表面。机翼,; o: h3 K8 g7 j5 Z3 t 安定面和操纵面都 & T! K' O& n: s1 n' D( V3 a3 k+ \* ?9 e8 f 空速指标 - s* }% W% ?" ~+ O N适航性,- e% V! y% u* l, E) X& N 有关气动能力、 & s2 {! i- X5 C" }7 }7 M演算法,2 _8 _4 @! n, E) u6 B6 O$ h2 J. e8 F! q, _5 B& a1 {8 i7 ~ 飞机飞行手册(AFM), 3 s: O6 B: m+ e/ D包合性能极限,操作极限,操作程序,起飞和着陆性# l: T1 D2 K( L* v7 ] Y* y) k5 F/ O2 l/ x& X机场分析, 0 N0 n6 n1 A3 z% y4 s' U一套针对给定的机场跑道的详细重量限制资料。通常与6 P6 C ]8 v, z6 H, o 机场温度、风、和飞机襟 8 q6 M5 C1 C6 O) K6 a2 s! S; X7 i5 h英汉对照民用航空词典B OEING7 ?, b5 a( L# n( o3 n' }. e TECHNICAL DICTIONARY 7$ m# D1 }1 J4 S5 H; G; l& R4 u AIRSPEED BUGS, Adjustable pointers on the airspeed8 t7 V) L5 F" q% H; B' l3 A. Q indicator. / S) T/ B2 G0 P& \- e5 ?ALLOY, A mixture of a basic metal and small amounts & f$ g7 `- m7 ^ w+ E' v% vf other metals to change the properties of the basic 4 _+ }! A) b2 D5 A# u; y" eetal.8 |6 D. ^) [2 k( {+ Z& _( ^! A Minimum airplane speed.: z9 C8 B) a& B2 |1 f$ J+ N e of2 ~3 ?7 K9 [% O) I, J itting airplane angle relative to% Z3 u" h' Q: `, K O) X) J irstream for the stall warning system.) F0 b& Y, v, j/ f* D ?( V: a another. 2 B( X& h; N2 |6 O) w8 X `LTERNATE , An additional airport selected during2 F- H0 u, ?/ d1 H4 v- {2 d9 B: J- @ 合金, " @3 G' t& |; l% P( x1 H在金属中加人少量其他金属,而改变其性质的一种金属/ { c1 W9 ~' Z1 B K# \" M 合物。 7 ?4 V% H6 a6 S, `飞机的最小速度。/ @& ~" Z$ I, k3 D6 ? 速警告系统传输飞机对0 \2 ^6 b& {% O4 |& T 流的相对角度。 ) p- J0 r, V. b$ q由一个状况改换到另一个。$ T" Q+ f6 i9 d) K& } 降场,2 m. A' t% i9 w/ W 划时,除了目标机场之外,所选的另一个机, A; P, ?$ o. z) W: w; V0 r! V o 6 ^ a, _& ]: B( @7 F, Tm3 \0 ~! F/ x' w4 \ C) i7 g% Z6 `1 b' X ALPHA SPEED, 2 ?8 a# F. z$ t& F9 gALPHA VANE, A small moveable airfoil on the sid 2 `) h# K( f% ^6 F. D9 v+ N5 \the fuselage transm4 a7 K, q/ z2 i a2 J$ l" i! t2 @; K$ T0 j, ?0 A ALTERNATE, To change from one condition to- n4 h% t# T( D F1 K A ! D. h0 M# \' @' A2 h Kflight planning, usually near the destination airport, to be, W1 r6 I4 o! [/ c% X9 [) [/ i used when it is desirable to divert from the original f6 c9 v& D8 U) Z! L destination airport.: Y, D R" k5 J% G ` 空速游标$ \ I* ~. t4 }; b- u) }/ n 空速表上的可调指标。, d! z3 g9 ]: b. c" h% R9 G% Z) a9 w) Q9 [* W迎角速度,0 L% b, O% ~% I! W _6 N8 x 迎角叶片, 0 O7 r7 z% p! P; R位于机身侧的可动小翼面。为失 ' l* {* I9 x0 |$ M& L5 \9 E" O: j+ R% x9 J1 o交替, 0 {2 m5 D# Y3 C) _9 ], v5 K# @/ U2 k2 d3 x" T 制订飞行计 $ Z$ T' q2 A$ x场。通常在目标机场附近,以备不去目标机场时,改降之 0 E2 x/ j: O/ o, J& e5 m用。 - C/ T8 u/ U8 F5 I英汉对照民用航空词典B OEING : {4 _& r/ C; \% \6 w/ g1 CTECHNICAL DICTIONARY 85 E) M0 \# t0 j9 v5 n ALTERNATE AERODROME, An aerodrome to which$ C8 C) x; [, \+ I0 U, L an aircraft may proceed when it becomes either 6 }0 Y8 `/ ^1 ?/ i4 B1 gpossible or inadvisable to proceed to or land at the 1 {: g, S% h. k8 serodrome of intended landing. " D" E' h+ z% r5 O" \TER SETTING, The adjustment of the altimeter 4 q& O) P/ t; j& c3 haccount for local variations in atmospheric pressure. - r8 o0 v5 I( T* ?LTITUDE ACQUIRE, A digital flight control system % O1 R1 X2 J: ]+ l/ Z# e8 wode to transition from climb (or descend) to level flight.* F" b- Z1 O+ [7 R LTITUDE ALERT, A flight deck alert occuring when the5 b' y n; R8 S& L irplane approaches or departs a selected altitude. ) K: K! g5 r; G1 ELTITUDE CAPABILITY, The maximum altitude at % f% d1 h0 V! M* |$ Rhich the airplane can be flown at for a given thrust,( b, P3 J- ?( k! ]0 _ peed and atmosphere condition.: C$ t( @' t8 a9 v LTITUDE HOLD (ALT HOLD), A mode of the autopilot7 z- A4 @4 N6 ?1 o! A1 S. ~; u8 W3 J r flight director to maintain a selected altitude.* ]8 f' Y2 \5 L# P, X { irplane's altitude during VNAV operation.9 G; N# T& `! ~ 机场着陆时,可作着陆使用的 n* O& a/ _9 n4 c5 u- ` 场。$ o9 t J+ {+ M% z" C+ }% `8 G" x5 i3 A+ v7 [ 根据当地大气压力变化而对高度表所做的调整。 ) `2 J+ @7 c% W+ F一种数字式飞行操纵系统,从爬升(或下降)改平的模. l: y3 s4 N/ p c$ i# ^" i" @ |! A1 Y2 _5 A 度警告, $ A& Y! L! w* b9 ~! d当飞机接近或偏离选定高度时,所出现的驾驶舱警告。+ |/ p. P$ i0 }$ F } 高度能力, 9 J3 V/ S$ _! i0 q) w在给定的推力,速度和大气状况下,飞机能飞达的最大 ' P! U( W* J! h. T0 i- k高度。 2 I+ X. E0 D" W3 X高度保持(ALT HOLD),5 \1 M0 s# [) P) S+ i2 ` 自动驾驶仪或飞行指引仪保持在选定高度的一种方式。 2 w4 T3 P1 L' [: I0 B5 {. ^" H8 `$ P" W5 A$ g) q 员对飞行高度的控制。1 [3 l) d3 U+ j9 ] im; T: ^9 \/ c9 }4 a9 x9 \ a [- A; M# j6 u' x# FALTIME6 ]7 n2 D* [+ k1 n( d to' }$ r. J5 h: d& B8 E: k9 q: X A. \* y. Z0 {2 d4 T% @ m; g4 r' u e2 z1 z6 x! o A # |3 G7 w U% z! R1 m1 @a6 M6 N: O f/ v A( p: X: G! e$ U% E% a! j% P7 \ w! W0 ^2 W0 z& U7 v( Q s% A/ Q) A- D+ U, w A " n& q% v8 x I! \$ s8 X& K# ao. q+ A- ^' }& G! k8 E$ i ALTITUDE INTERVENTION, Pilot control of the4 a, Y# d6 H" l* c9 \. ?% f a* m6 M( ^5 X3 n+ J3 |% V AMBIENT, The surrounding atmosphere./ j4 V& N1 i- v& O 备用机场, 1 A$ d: @8 R: @$ H; O, x当不可能或不适宜在预选 ) A& Q5 I, @" s0 T4 R! d0 w- ?- e9 v8 X) f% S高度表设定 ( {: T% ~, a( [% P$ }2 d! ~1 b; g高度截获, $ F. A/ |" y$ t; K8 |2 ^4 ?0 C! d9 a) Y* H7 ?% k* v8 K9 ]/ R9 {/ L( [) A; R r \ 高度干预3 t$ X- Y7 L- B5 m4 b/ V 在垂直导航工作过程中,飞行 ; e, p) [! Q$ ?& W2 G周围环境(地面气层),1 s$ ~+ ~: H9 h8 V; z/ ?/ H5 Z4 O! L 物体周围的环境(特别指大气)。8 ]( ?" N7 i( U" x/ N5 b4 ~ 英汉对照民用航空词典B OEING |/ [ h6 U8 O& bTECHNICAL DICTIONARY 9 ( w, A% r4 \. T$ }AMBIENT PRESSURE, Pressure of air surrounding an 2 S: F! t( s/ X9 H- e! Zobject, measured in pounds per square inch (psi) .$ U0 A9 P4 a6 a5 ^ MBIENT TEMPERATURE, Temperature of air ; r# R; C+ i% c3 g1 mmpere." u/ p* ]* B* X: {* n8 C! K9 @ urrent waveform. & Y9 W1 R5 V' e/ F* jg an: |4 Z) c. @) n3 C& K: y7 ? nalog signal to a digital signal. * S8 B" R9 H' oore inputs ! P6 R( l' l* t) g9 x( l8 Df binary digital information and one output. The output9 G7 l9 @5 P, |0 |7 |5 Z) X; c 1 only when all of the inputs are 1. The output is 0" |$ l) S" O! }) b0 G3 Z4 C' s1 D, i hen any one or more inputs are 0./ Y6 W2 ? D$ G7 H: D, { 面气压), ^, E- O4 W7 s1 F% F4 ?! J$ @5 | 境温度,7 Y+ v) m' i2 `$ i# k' M2 q' O 气温度,用摄氏度(°C)或华氏(°F)来 0 S0 k7 D" Y3 U$ k7 u8 \3 ^' J; L* ^ o" F6 M `( d电压或电流波形的幅度。/ d- I& b: h- t! ]0 a$ c- ]9 g; l s# S$ j 性变化的信号来工作,或产生连续性变化的信号 3 |; n4 V0 t2 U, {# f! I统。# A! ]) O0 d! Q) d! r' ` 将模拟式信号,转换成数值式。 3 [- j5 \, j* U2 k: J, c V% |/ L4 w一种有两个或两个以上的二进位数字信息输人,一个输 . k0 B( X' \( q1 U) @的装置或电路。当所有输人为1,输出为1。当任何一个7 C; f& i# }6 j 一个以上的输人为0时,输出为0。) _" N, N) G0 P# h A& e: P( u. A9 ^ W surrounding an object, measured in degrees Celsius [$ b/ n0 u& [7 |) f# O2 c(°C)or degrees Fahrenheit (°F).! W/ a7 w. w/ C' u3 s" U$ }! ^ AMPERE, A unit of electrical current. One volt across ~9 [ v$ N3 @$ d one ohm of resistance causes current flow of one0 g: J* S* r" {. I, `7 N a 2 E/ T/ B1 m8 X' K: ^; X' _! ]7 ^AMPLITUDE, The size or magnitude of a voltage or# n0 K. j' w+ S A. Q! |: u# C c9 G. L8 ]: |, g' R ANALOG, Quantities or representations that are6 N; _% A, |) | C0 Y variable over a continuous range. 7 y9 m, o% i" h/ K$ UANALOG-TO-DIGITAL, The process of convertin' t9 L9 ]! o9 T/ q a% l) G4 g/ Q" F AND GATE, A device or circuit with two or m $ _( v/ [! ]" G/ y2 Mo ) x8 y3 [; i$ B+ a% w3 Fis8 g3 S2 }3 S, ~8 b3 r w1 k8 \0 U* Q0 L X$ |& P1 t, F 环境压力(地 E9 g9 \% C+ r9 j 物体周围的空气压力,用每平方英寸多少磅(psi)来& n. q) ~. Z; V9 w/ R 度量。 , T1 Q* x0 t1 r: Z2 p5 d2 F% r; S# ]# ]' B$ M/ E物体周围的空 & @% x A0 x; Z/ i度量。 5 C4 ]6 I, j' U. Z: t9 W安培, # _% ]9 e5 W9 E3 }6 t$ X电流的单位。 $ E2 T T% T' [1伏电压在1欧姆的电阻上所产生的电流为4 K' [% b; G: x8 @% o' x, y1 N4 v! F 1安培 1 K9 e) `6 f! W- v& ]振幅, 7 X4 r0 X" K3 j$ _3 J5 b7 k模拟式, 5 Q! ~! d0 t) O+ ]8 U- f5 w用连续) T0 A% @& Z6 x+ A4 |5 e& O5 i% V9 ^2 g( u从模拟式到数字式,3 [, u8 r u! q g' @& m 与门, $ M, V% \& n' j, w' R( q; O. |1 G" w3 q! U6 h2 ?; Z3 A% A/ I8 a3 V( H, y英汉对照民用航空词典B OEING / Y3 h0 X$ M# E3 L0 STECHNICAL DICTIONARY 101 X' ^, r. }1 d' p& p7 [5 q* ~ ANEROID, A sealed flexible device containing air at low ( O( D& Z2 i' Q: X: h. t" Tpressure, which expands or contracts during change of 2 ~% k o& L7 F& Pressure outside the device.5 @% M, L; D. P% p z$ x ically$ w" K$ q3 I8 j: X4 Y* q& T" Q. V, g, a% r r changing the direction 5 n; q/ g# ~' S) q, xf drive. 3 |( b' e3 n2 T! b9 q% Dof the wing chord in( }! ]1 J' {$ V: }5 R3 D( b. @ lation to the free stream airflow as it moves forward 9 d e# z8 k3 g, orough the air. 0 V) [+ U7 V& M- t7 V$ ual axis of the " a2 a1 M+ a: Y! {) A( x4 A- waircraft.' M, ~- N# {0 m- n5 \8 k2 i, x 胀或收缩。 # X- `- T: P. ^& e7 q7 c6 T箱。是改变驱动方向的机械装置。 C; K% X ]: G# w 机翼翼弦在空气中向前运动时与自由气流之间的夹角。 , y( R4 A% }% H' b+ l; V% |; S: d9 f7 w- _0 F4 n6 {6 H p 1 z O( v4 ^% q/ U$ ~; iANGLE GEARBOX, A part of an engine, mechan 2 T9 }0 B4 c! m. ~/ M% Ndriven by the compressor, which drives the accessory8 @# `( `2 k# D ^7 n gearbox. A mechanical device fo3 r! G/ b' h9 E7 t9 Z7 s1 y o& l% m# n4 H8 |7 E ANGLE OF ATTACK, The angle 6 o- i8 A8 m; f* Vre * y, Z6 z- X5 `3 `( W9 @th * g6 {3 |- j' N& X; B) p% IANGLE OF INCIDENCE, The acute angle which the' g- _2 \8 f' e A7 X& A* W wing chord makes with the longitudin Y4 P4 ~7 m1 }; n膜盒, - K' U' O! G, j0 T S2 R& b7 Q内含低压空气的密封弹性装置。当它周围的压力变化, o: \7 S5 t6 [# ^0 B3 j0 X5 c 时,会膨 ) {* X* q, x/ ~) ^# ]: q- ^伞齿轮箱, V6 K1 V, ^& _4 P6 f U$ y( j& ? 发动机的一部分。被压气机以机械方式驱动,然后驱动 9 H( ^8 n7 n, ^+ g9 n6 I T附件齿轮0 @, T" ], N6 i 迎角,0 t/ s/ I6 \/ _8 i) ` 安装角,/ ]" x2 ^+ F0 E) T: C 飞机的纵轴与机翼弦线所形成的锐角 9 e$ X8 n" h' y+ c5 _. @1 u2 c英汉对照民用航空词典B OEING 8 V: C T- Y5 f- u/ CTECHNICAL DICTIONARY 112 u z0 _& N9 Y6 o, x% z& ], Q, w ANNUNCIATIONS, Audio or visual indications used to! W* u4 h: V* u) |5 a t call attention to an event that has taken place. + c: B: B7 C8 X/ M( t$ Y5 Z1 s: w: ^ANNUNCIATOR, A visual device consisting of a number " u: M0 r ~- X5 N$ f" h0 Lly. 8 T9 x2 E! }2 G6 i8 H; a0 V6 zANODE, The element toward which the principal stream3 j( |& D# N9 Z- K# x of electrons flows. M. A4 D$ B5 J B: d$ L ANOMALY, Not normal.0 T& ^( ]. q2 I- [ ANTENNA, A device which, used in conjunction with a ) X* H0 o3 h2 n, m' ?, Btransmitter or receiver, is used for radiating or receiving - ]3 t( u3 r# Z0 h! i# wradio waves.( V; S/ d" l" X& C NTI-ICING, A method of preventing ice formation on 5 o" r# @# n- R- x9 k0 ~e wing leading edges and engine nacelles.8 m: M: {! Z; r7 } NTI-SKID, A system for providing maximum braking& G. x/ A; @4 ^& Y0 D2 S8 b R ithout skidding for any runway condition. Anti-skid % [! t$ l0 `9 |) p x0 i, Momponents are part of the brake system. 3 M! c4 m8 X. ~/ ~" P% c告, . @, Y4 W$ K( K当发生事件时,以声音或目视指示形成的提示信号。* o/ M7 Q) n! ?1 E( |( f. {1 X( w 与之有关的电路的现有情况或已存在的 s. i/ q9 V! s. E' G, w5 }. X. u& ]- g 正极,1 Z5 A9 I; k8 v% _ 主电子流向的极位。& D+ z% Z8 H* [ 异常, ! }/ G9 h o" k: g4 K) n不正常。 ! n7 f+ |/ W4 R) E5 N& t4 u9 L天线," W, r8 g! L5 N5 m3 A& e/ N 一种与发射机或接收机共同工作来发射或接收无线电' {9 y P% k- Z4 |: g 波的装置。, T8 Z6 J# y0 z" l0 M! x 冰, + p* @/ J b; ]2 u% k0 z防滑系统, " b5 x* E. Y% x, `8 o& `- z一种在任何跑道状况下,都能提供最大的刹车能力而不 9 r5 ?6 v7 L( i6 P1 I使轮胎打滑的系统。防滑部件是刹车系统的一部分。- H; o$ m9 O8 C2 G of lights. Each light indicates the condition which exists 0 c) j% f' ]9 l" T1 j2 J! _or has existed in an associated circuit and is labeled 6 }# }, p* E* g% U% Y# taccording 6 U4 b4 ~( ?0 k- a, w0 w% H1 W& ?A + j {1 n+ Q9 O/ W( mth2 r' p: k$ Q% X+ |. J5 g' P3 P A ' [; ^, R8 j: h' E8 pw7 U. t7 t, ^ S% _0 F c1 p, \ F) I0 n9 a+ P2 C, b) K" H& Q, n- e5 t/ C) ]% ]: T6 t0 v, G: _* Y. I p 信号牌, 6 v# G$ `" g/ g9 s9 Z7 f4 W由一系列指示灯组成的目视装置。每个指示灯都有相应 - Z, l, k, b2 P7 ^6 `的标记,用来显示 X% b8 W0 a; I8 a9 w4 W* V/ Q3 E3 T4 w7 P' b7 G5 t0 e) f3 ^$ W6 I/ E防止机翼前沿和发动机短舱结冰的一种方法。8 ^. F4 Q4 r! y5 W 英汉对照民用航空词典B OEING ) _ a, Y+ c% a4 B6 m0 FTECHNICAL DICTIONARY 12& j# \& T9 | I! d2 n/ w APPENDIX, A supplement to the Airplane Flight Manual 1 P/ z% s2 v* D% ^tained in the basic manual. A 1 `+ l$ E) q+ Gollection of supplementary material at the end of a+ u& l, u% i t% n) a; e" C) P$ w& h ook. 0 ~' I! F: D" s7 _- Bof the ; | z: X2 i2 ]: Z$ h: {* Srsion link on the landing gear.6 u: C" J3 J$ f1 c APPROACH MODE, An autopilot/flight director mode ' A; b! J, z" R8 Mwhich is a combination of localizer for roll control and * n/ ]" x' g! T! K' L8 _/ Vglide slope for pitch control. This mode is used when full! R# C1 p, {3 t2 z* s5 ]. f4 l9 E instrument landing system is available.6 s+ m$ e% e: y& l/ w APU, SEE - AUXILIARY POWER UNIT 3 I4 e4 c( D+ _8 h I# @ARINC, SEE - AERONAUTICAL RADIO: {: J5 W& @+ f$ _ INCORPORATED( L2 D8 u! \5 b) h3 Z ARM, To make ready for operation. 9 ?8 z- Z. v4 H3 S附录, + u: i0 q- P8 W$ L6 w: N飞机飞行手册的附件,包含基本手册中未提到的飞机形 5 u5 J: f( y/ K6 W7 o态的其他性能。是附在手册末的补充材料。 # \% Q3 V* L9 z8 r. V顶销,4 n2 D& O% X6 K: h$ _7 c; k+ j& _# w 用于连接起落架扭力臂两部份的销子。 6 P8 w* h$ P Y; A! ~/ O8 r1 s进近方式, " L7 B% ^+ d3 d一种综合了控制横侧的航道信号和控制俯仰下滑信号$ |, p2 W* \2 _ 的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系6 R1 A6 d- z0 w# f: Z T3 k 统正常时才使用。 6 S) T o3 {+ m辅助动力装置, F: S/ d" s1 l7 M/ q+ Q% F T7 W- J见Auxiliary Power Unit2 w* J: f; e2 m% B) n containing additional performance for aircraft8 n( h) w. B! Q7 ~& P% u configurations not con- [0 u# S! g) t+ p) ^8 \( ^$ V c 7 E { R$ l' k& G3 \9 Db ( T$ E ]6 e1 _; g# EAPEX PIN, A pin for joining the two sections 1 k; E2 C, r# T+ \to: z5 _+ [1 Q7 k& J% N$ V$ R0 H0 [2 @* S航空无线电公司, 7 M t& a+ [0 z9 N5 t见Aeronautical Radio Incorporated. & w. W7 w6 I p6 c& Q预位,. ?6 }9 c" ]6 C5 \( j, i$ i. B 部件可以开始工作的状态。 " d& K% ]; Y/ W' b英汉对照民用航空词典B OEING ! q$ f8 y. L8 M0 ~' I* Z9 j' Q uTECHNICAL DICTIONARY 132 c2 C4 Z6 C1 I) j# N ARC, The curved track over the ground of an aircraft, Z3 f- [% L* N! t flying at a constant distance from a measuring ) a) E) e5 Y/ \equipment (DME).+ a0 ^- D9 U% ^$ I4 i6 l1 @- s in the limits of self-contained system / G% k: ?/ S' g4 [, gapability. 2 O- ^! v4 k$ Utem for opposing or restricting: p9 Q9 }7 C0 D9 r& ~1 a% O, a ovement.0 m6 w6 @- T' Q SPIRATED TAT PROBE, A sensor that measures total * i9 n" E" l( k$ vir temperature when the airplane is in the air and that * U7 y$ [4 n5 _ Reasures outside air temperature when the airplane is; y% a* j t' F! v$ C' p8 n2 e0 r n the ground. The outside air temperature is measured2 R: h- O; z* W) V SSEMBLY, The fitting together of a complete structure& }6 Q0 {9 \, i4 L& s7 ]& g SSUMED TEMPERATURE REDUCED THRUST, The 7 y( ~+ h! O& R; Z) `0 SATC, SEE - AIR TRAFFIC CONTROL 6 ]8 X. K. Z% h8 V7 U) a8 ~! [9 w/ g- _8 e5 x3 ^7 R$ }5 o4 x S 系统中所产生的一种用以抗拒 ! n! @7 h) L$ K: Z7 j作或限制动作的力。 8 M- p+ a% ~4 d' K头,) W& n9 |# _: {8 c 用来测量飞机在空中时的总大气温度和在地面时的外 2 D( e5 c1 Y- v2 y温度。地面外界温度的测量是利用引气将外界空气吸入 - j6 U5 J* C9 P' f头,以达到测量的目的。6 k, Q1 O# C5 \( N 配,' ^' } w3 q5 [0 W/ T 一个完整的结构或组件的过程。 % n& f4 S3 |" x, S8 i4 V& `假设温度而得的减推力, ; {8 S/ r2 j3 e/ B推力设定值时,假定一个比实际外界空气温 + }; z- ]% L$ m空中交通管制," ^0 _ Y* z& B7 V5 Z8 L7 L4 c 见Air Traffic Control $ N# y) W) v6 G( MAREA NAVIGATION/RNAV, A method of navigation 1 f. ?, [) Q9 ^5 X6 I( G# Hthat permits aircraft operations on any desired course # A' U G' w/ n) P, |% ewithin the coverage of station-referenced navigation8 w2 Y5 o9 b9 G$ M2 ]9 } signals or with1 V) q+ N' W: H c $ X; a4 \& q% J' W4 g6 bARTIFICIAL FEEL, A force developed in the flight' y- Z5 k% a" K; ^ control or brake sys# _1 z8 b* H# M9 V) F" k m ' `+ L& M3 n I) I/ l- s7 DA( u3 u# e7 v- ? Y* s7 l a7 @5 h5 T N& K5 M+ J m " }! F4 h/ L$ p! x4 Z. Mo 4 \+ K* t8 I6 m0 L0 Jby using bleed air to draw ambient air through the % o$ ]3 y2 Z3 r9 y9 U5 Vsensor when the airplane is not moving.& m. ]* j- W8 @ A+ e: B% `& b+ Y9 h! G- h or unit.% W0 c, X, ~# h$ `- |; u A ) F: w6 _% d5 V) x) B: {) wlower thrust obtained by setting a higher than actual! W+ j& q+ @& _( D$ X Outside Air Temperature (OAT). ! q* ]+ Z' O, R( q. G+ u8 E弧线,+ t1 P) C) p; ], g' H/ A2 R 飞机在围绕DME台等距飞行时的弧形航迹。% q1 B$ w0 @* {. l 区域导航,3 H2 J6 B Y: H' ?, j 容许飞机飞行在有电台参考的导航信号或自备系统能 ! ], K X9 \# I. X7 }2 Q( I$ [力极限范围内,飞行任何预定航线的一种导航方法。6 F6 {2 @1 x. V 模拟感觉 ! F2 n7 v4 C A/ \6 T在飞行操纵系统或刹车9 I( B' w' T T: R" N6 ~9 F. i& j' L4 d% g! m- h 吸气式总温探% ^9 h- @$ p$ A/ X" ?7 h2 C! S: e- @2 e, U3 d: H- ]' g% A- ?5 D4 S( j% s2 m2 d w2 X3 s i组合成 3 U U1 p: W) d& r. y' K1 N, h! s, s# h) E' L在选择起飞 4 u# p1 D; A8 q( x* L/ Z度高的温度而得到的推力。用这种方法可以减少发动机的 1 U' |8 }; t& d! |' g4 g6 o6 p6 e磨损和维护费用。 $ Y3 k* ^# ^; ]7 e: v& Q* R2 `; \2 q2 J 英汉对照民用航空词典B OEING- e1 ]$ J9 w3 r6 Y- P$ k" ^1 h TECHNICAL DICTIONARY 14. I O! l4 Q5 ~1 ?9 A7 O ATE, SEE - AUTOMATIC TEST EQUIPMENT$ z' o; q9 A' ]% J) d1 z/ L ATMOSPHERIC PRESSURE, Pressure of air due to the. b. X+ _) y" C5 A& M* @ arth's atmosphere, expressed in pounds per square * E( L( k* S* r9 Xch (psi) or inches of mercury (in Hg) or millibars (mB).2 e3 A) X2 P& L TTITUDE, The relative orientation of the airplane with ) K% l9 d P3 A% q! A$ l2 G Aspect to pitch, roll, and yaw. 2 p. z* R7 |7 B* X- A/ l6 QUDIO CONTROUSELECTOR PANEL, The panel in % I: u: f$ u6 g1 Y# R, ~. E; c9 Ne airplane which controls and selects the routing of4 K9 {9 s. d* v( `- c udio.+ p7 K4 e2 A+ Q/ h6 c: B. o) x& v r UTOLAND, Automatic landing using the Digital Flight 1 V# G) G: \' F( f' aontrol System.6 n3 K$ \" ` P5 E8 _2 T2 C- _ n. 2 G5 E. F& x Q2 p* e- o7 O. tM, A system 7 U- j" J# d( ]5 [omposed of all necessary subsystems needed to guide W7 e8 D+ k2 w# w/ g" d* q e flight of an airplane.7 b0 V E8 ^' `6 z; A EQUIPMENT, System test 4 ~1 D2 N# J" {/ qquipment that operates under computer control. 7 ?8 ~6 @; _+ O4 O/ U装置,

使用道具 举报

Rank: 9Rank: 9Rank: 9

3#
发表于 2008-12-24 21:37:12 |只看该作者
e $ e, v: b* ]2 ^/ M5 |in ; L" X# B; ^7 a7 m# E4 k' ^% _A . ~, P( D/ m% w& m- Y2 K- d5 ore 1 H) `' P8 V; l& K. Z1 `A9 K/ R* X* Q% r3 `. R th % Q/ n+ l2 p3 N& D2 O# M9 m8 X0 Na . t: W9 @3 Q+ ^9 k7 L- `! zA ( [/ U. a) P# M, yC! O5 @1 O. j: n5 z9 Y. O) @: ^ AUTOMATIC DIRECTION FINDER, A system which6 ~0 _ {0 x3 c2 j2 Q# c: U) E determines the direction of a radio statio 2 z- h }! M' p3 H1 R7 P& M' Y$ hAUTOMATIC FLIGHT CONTROL SYSTE( G5 {9 N ?; J$ z. { c ! S; D* s7 I8 cth" z( I* Q5 q5 U9 O7 W$ X4 u/ z AUTOMATIC TEST+ n- Z: `% W1 H) m) A* v e 5 r- A" I; `$ I1 ^. X) N自动测试 R; C' U, _7 |: y8 d见Automatic Test Equipment.0 ^; |' D0 a& r8 ]+ U/ [% P; z/ O 大气压力,( Z) k" M; h) {1 a* y- B+ F 由于地球周围的大气而产生的空气压力,以每平方寸多 z; @) a& T; [, F& b 磅(psi)或多少寸高水银柱(in Hg)或毫巴(mB)来 1 W7 a# Q! i( x; T示。 # V1 |! `& w% l" U0 _: Z- x飞机姿态, ( t4 X$ s9 W* N2 S8 S$ j飞机与俯仰,坡度,和偏航有关的相对方向。 " i" n9 x' R8 C3 U/ L6 v音频选择面板, 0 D9 [5 v8 ^ C飞机内用来控制和选择音频通路的面板。$ A3 a3 }* v( X0 G5 e, z 自动着陆, ) i$ O0 ]! I0 ?# ^/ k使用数字式飞行操作系统来进行自动着陆。2 [. M3 p, _) ?- ]( O# h/ W6 i# z 的系统。 $ I9 Z5 M4 f7 T9 `" a4 e" R7 h* ~ ^. | r. D c6 ^ 系统所组成的一个系统。9 @( o# A' |4 s7 V+ {$ ` 在计算机控制下运作的系统测试装置。 9 v" _+ T& K5 s" R: n6 Q9 W8 O# {; Y# n1 l r+ e T' p& I 自动定向仪(ADF),9 B& V/ N# J3 k% V3 [9 I 确定无线电台方向8 s' k9 ~, q- I* v( B8 o1 B z 自动飞行控制系统) L7 J# n. b2 }: M8 A0 {2 s; { 由所有能引导飞机飞行的子 $ ?0 {8 g; D) c9 Z! `自动测试装置,2 K% X7 u( J$ X# Z ` 英汉对照民用航空词典B OEING7 H: Z8 i1 C+ i TECHNICAL DICTIONARY 15 + B$ q5 X' P- S0 I+ ]! EAUTOPILOT, A system which automatically controls! z8 P) ]2 g, Q- } and guides the flight of an airplane.# O! C- f' X6 F# E AUTOPILOT FLIGHT DIRECTOR SYSTEM, An 6 P6 `& N3 e$ t' E3 I- `. Ptor & B7 N9 F3 K$ n7 P( _UTOTHROTTLE, A system which automatically " J5 }$ w" B' ?6 W7 D$ G1 Qontrols the throttles of an airplane. . a- \; S9 n# L, n* A; m1 JPOWER UNIT, A small turbine engine in, |; F7 [3 q" x! Y$ q2 p/ ? e airplane for supplying electrical and pneumatic ) K8 E7 E- Q5 q7 n+ M( zower for systems operation on the ground or in flight. 3 t! f& F8 K( A5 G& J5 z# q# n+ uVM, SEE - AIRBORNE VIBRATION MONITOR - N0 ^0 ] U7 ^) J" [XIAL FLOW COMPRESSOR, A type of compressor; h# O& o9 H! m" q! l5 t# o sed in a gas turbine engine in which air passes through- J) ]9 c. A" d' r4 p% E u) H XIS, An imaginary straight line or an actual physical0 v1 O3 r1 N; ^, M+ N2 ? omponent (such as an axle) around which a body can8 a: m- I2 T0 a7 d- i* l tate. $ e6 T2 n: m3 I9 U仪,) ~. r# N/ {. O' h; W; E H. B/ s1 o$ P* t' u 自动驾驶飞行指引系统, * j$ J% o5 L2 L1 g9 v- Z动驾驶和飞行指引功能的系统。/ g: B2 g$ \" I8 c/ l 动油门, * b3 D; V( x) T+ w自动控制飞机油门的系统。 / `" i' q% ~% D& `% T8 F是飞机内的小涡轮发动机,在地面或空中给各系统提供3 T+ P5 K7 `0 `, J 源和气源。 6 F& e8 P _; t. `7 E* S6 H \称。* P7 Y7 o& k1 G+ J9 u% ]" f 载振动监视器, 5 n' A' Y' J, ]( {# w6 S见Airborne Vibration Monitor* m. D4 Z$ Z$ M3 @6 m/ {! Y, Q integrated system containing autopilot and flight direc! E0 B" z2 W! G( D& g, a functions. " D; ~5 _! Q0 K" Z% gA% O; z* _. B. j c 6 f# O; ]3 \( g. \$ Z( lAUXILIARY 0 p: X/ P; G2 K. Xth % ?6 k. ]! _% |. ~. t' m* L( Bp / }# r3 \) A: v' Q9 o9 hAVIONICS, An acronym designating the field of aviation* X3 R/ ?3 E! u$ g$ K) J' b electronics.$ V8 h7 q4 m8 L. T) b( W A 9 r/ H. x, e7 `/ a' G, o& LA 8 ^+ X1 O5 r ~% \3 @: _u ; I1 `# u1 z0 p$ pthe compressor in a straight flow, front to rear. k0 d K0 l2 e4 w0 X4 n A- n+ W, @8 g$ N6 m% J c! y& Y) J4 R, _ K( t6 w" v ro % Z: m- J+ w- {9 T3 D; ^自动驾驶 . a0 c. O$ j6 g7 J0 k动操纵和引导飞机飞行的系统。- X! n" L! e; o n: {+ D% z% d 一个综合自; y1 Q" |; X+ w }4 s, _1 y0 a8 [: \& b5 v8 O 辅助动力装置, 2 q3 y1 q; {) F5 v2 A% Y# Q7 q7 E4 ~ 航空电子学,6 N& V8 h1 k/ p 是航空电子领域的一特有名 # U1 x9 l- r- V5 Y6 c% E; @; y4 y% B/ c/ w! Y9 l; }9 H- v7 q3 J7 `流压缩机, : |; j) e7 B% i8 a6 P9 X& S一种用于燃气涡轮发动机内的压气机。空气由发动机的1 a1 i# Y, T7 B+ k 部流出。- ^& s4 \9 Q& j4 K; e8 O; v# ` 线,+ n {! e7 j' Q2 |' B% G% j. T 可让物体围绕着作旋转运动的一个想像的直线或实际 @2 R' B7 M- N; m9 c, H* E 在的部件(如轴)。 5 L$ u4 R/ | n8 u6 p1 g( y g' M8 [3 C& O前部轴向流人,压缩后,由后 6 F) N8 V. u, N! L! u: Y. C( c5 B( }' F, E( `! M5 @, m' y, p+ B6 ^* G% Q/ \英汉对照民用航空词典B OEING ' y5 q* m- p! T, ~) |TECHNICAL DICTIONARY 16 3 q8 c; L& I2 ~+ h5 q# MB2 }& x# P* |# N4 f1 F/ T5 J! j ACKCOURSE APPROACH, An approach to a runway; k# H* Q- P9 h6 S4 E versed.* h! k, g, s' w own on the EFIS that" A. w: i8 L. i6 E oes not readily change, for example, navigational aids. # [" O5 y. [+ j/ }+ `1 P. M. Hvement in the tank or reservoir. * _- f- [/ d V; YALANCE TAB, A small hinged moveable part on the % {$ X- L' _6 _3 T2 i2 Eailing edge of a control surface (aileron, elevator, # N. C% H' E* D8 J' w航道进近,7 l6 \( L& g6 U+ e 相反的进近方向。当反航道进近时,无下滑 - r0 h, W; J" M5 {: n% r% E显示在电子飞行仪表系统上不经常改变的数据。例如:) L( M0 n& ~1 L) M' M 航设备。' ~9 [* V8 f# i# t" z' A* V 在燃油箱或滑油箱内阻止液体流动的隔板。 8 L2 L. T0 Z! q, m动补偿片, $ \( \6 g4 `7 T# S! T7 ~铰接在操纵面后缘(副翼,方向舵,升降舵)的可动部。! D# A+ f9 S6 o) b 与操纵面相反,以帮助操纵面运 6 S1 U7 v; {$ M. ?B$ n, }4 p' f0 V+ Z( g which is opposite the normal approach. For a! [8 j+ Z5 D# o. I2 V6 A backcourse approach, glide slope signals are not: K' @5 K: e7 K8 Z8 l available and the sense of localizer signals must be ' g, n' V( U- U. n+ m( Fre ; E/ }8 w* d! U7 h4 ]6 I V2 q8 f: sBACKGROUND DATA, Data sh! ~- D( Q9 ^ C d. _+ s9 T% c# \8 g0 N0 | BAFFLE, A partition in a tank or reservoir to prevent * t3 K; g+ u+ _% Ofluid mo $ C8 r+ m& ? [% E8 A T( FB" g5 p8 t1 h E q5 K tr 6 E1 K1 B8 Q3 J! b5 m* Xrudder).The tab moves in an opposite direction to the ; r4 k$ p7 ?3 Pcontrol surface for assisting movement of the control 5 f6 D) T" b7 a- O: P) e& Z3 osurface. + A8 p; \; r% |' L/ Z% g( w- v. \: C \ 与正常进近8 Y/ X. V2 |; W7 z" Q! [' W8 c 道信号并且航道信号也必须逆反。 6 k& ?& x+ ~, N背景数据, 5 s+ i" X$ l! t! H9 X' v8 {4 ]" h1 @5 ?缓冲隔板, ; p4 t% d) _# F) A$ a& f6 d+ O% v" {% G! T4 k' { 随动补偿片的动作方向, w9 i4 r/ O* z% `* C; P& V 动,减小操纵力。 . p$ l& ~+ z/ F$ y0 a* b K$ S英汉对照民用航空词典B OEING& |' H4 }" t+ Z TECHNICAL DICTIONARY 17. ^! E5 M9 S- H$ ~5 x BALANCED FIELD LENGTH, The field length$ m/ f' ~7 W; @, C( d, F2 m associated with optimum aircraft performance when 8 T. ^) D. @" A& @/ r( ibstacles are not a constraint. In this case, after engine 2 {2 s1 K- q+ t$ B8 [* bilure at V1, the distance required to accelerate, takeoff8 Z/ Z: r' {' C- [2 M- r- j* h( B nd reach a height of 35 feet is equal to the distance8 p3 M7 m/ j! J0 I2 g% E* J! S, I ALLAST, A weight installed in an aircraft to maintain \& m% u' Z, Q9 X# S$ J0 s A. | ALL NUT, A fixed spherical nut driven by the # A* L- A+ H3 VAR OUT OF VIEW, A signal used to remove the flight% T2 _# Y5 t8 Q2 u" n& i AROMETRIC PRESSURE, The pressure of air above9 P5 c3 {. j, L% D5 O g) or 6 n8 j- m; N1 O& V9 I1 umillibars (MB). 2 z9 N7 ^9 E9 ^8 U2 ]# D" mATTERY, An electrical device for changing stored. L8 f0 b* U" r" ]2 d' F; B$ L 性能的场长。在此 7 J2 I& Z/ |$ z况下,V1时发动机故障,要完成加速、起飞、离地35 g' M8 O1 P) H6 t* N 尺所需距离等于相同速度下完成全停所需的距离。 ; l+ D5 a1 s# L1 v3 a$ x舱物, 5 n9 k0 e3 d7 [0 h- R$ z- ?重心在许可范围内面装载的配重物。 5 z! c' s4 v% T形螺母,; p3 l6 s) A4 j' |1 j! e 的固定的球形螺母,用以使襟翼和水平1 k: A9 r0 P3 [! K& \) G' c! S" D 引杆消失, / [, b; D. R" Q" Z' E4 f3 q3 d& @指引杆的信号。 ; S( V0 l6 L7 \压,' a% |/ L4 t- ]5 v# K$ `4 m 压力。通常以多少寸高水银柱(in8 I# a2 W1 v, `' W, Q/ a 瓶,# }0 D6 J3 ~" z$ I# E( g' g 的化学能转变为直流电的电气装置。& h/ y! }6 ]# D. u1 P5 [ o 1 \7 q& `& m3 W) o9 A8 z& D6 g* \fa1 |- V) g5 ]8 K0 u& P( }; Y" u9 K a ; F' L& Q$ v0 prequired to stop from the same speed. # p, Z% v, T! X/ w, Y) ZB 2 k+ e8 b0 m& p) d5 N5 P7 H/ wthe center of gravity within allowable limits. ! g& g3 V' Q8 S+ F, c/ z+ X9 hB 8 F% f: k1 N! J8 U! F) g: N8 Z$ Gjackscrew for flap and stabilizer movement.. g7 W3 N; d( C& K. t B( ?9 k9 ] g3 g: N h% [, l& w director command bar(s). " m( G6 s- ~" M% C( w6 P! nB9 Z6 S+ t W$ w zero pressure measured in inches of mercury (in H8 y; F* [ n# g0 W% I9 n6 s in 7 C* P) Z& G2 A- aBASE METAL, The underlining metal to which alloying. r1 C* i' Z8 \; t2 i+ E$ m: U7 Z agents or metals are added. 0 Q `$ A& {: n8 CB . W9 w$ K6 U# h/ m4 Wchemical energy into direct electric current. / s6 f0 t% C |" K: t. y平衡场长, # k* |. K9 O. S) x当障碍物非限制因素使飞机达到最佳 # c! Z- T% n/ o. E2 p3 i: z) L4 P8 b6 s- ^3 U5 t" L% _# i* g* S% }+ A, A. X: q- G, X" M6 Z3 U* s8 z; z* v2 p, L1 \为保持飞机 5 k# Z3 S& {2 ] T8 A+ A! }' z7 E" B3 A( F2 H p3 n由粗重螺杆驱动 ; B3 `2 ^& B; \, A( m安定面运动。' `9 D6 n0 K$ @4 Z% Y4 [* f! H$ ^3 D' E. g0 O. s2 _用于除去飞行/ a- G" S) [' I/ t; S" {* a1 U% z ^+ f. u( }零压力以上的空气 n; N. J% }& P4 j. Y! X7 gHg)或毫巴(MB)来表示。 6 ^1 ~- f1 _% w基底金属, , z/ f0 Z0 D$ W指合金中的主要金属成份。" ^# ^6 H9 p: J& U" B# Y9 ~% o! k9 N1 ?将储蓄 : W" E% O" M, j# Q0 i% w# ^1 f) n& x英汉对照民用航空词典B OEING * F' p! F- E% H5 r6 L1 n" Z5 j% ~TECHNICAL DICTIONARY 18 p( C; R8 A. I2 i7 L5 U BATTER 7 S& G8 | Y8 Q6 h+ n2 C1 rdirect cu / c6 q) d. z' N [1 I: m4 }+ zpower su/ ]' q; e3 \* n; B$ }9 S4 g1 w Y BUS, An electrical conductor supplied with 7 @2 L% K6 @( _. b& A. E; ]0 |3 Rrrent from the battery or transformer-rectifier for ) v# I* I; T! l$ c5 c# O2 upply to operating components. ! r) ~/ q1 a/ Z TCHARGER, An electrical device supplied% j5 N" e2 Z1 Z+ o* F1 n6 O ith alternating current, which produces a direct current3 `1 e- t0 N. ]7 N. v utput for charging the battery on the airplane. ( @5 ]! M$ h. ?0 s, mAY, A compartment in the airplane structure.* M7 }: ^+ g2 q CD, SEE - BINARY CODED DECIMAL . U/ |7 u! A$ Z [* WEACON, A device which emits a signal for use as a- g, c4 ?3 O) d uidance or warning aid.' i2 S4 v( }2 E) O+ ? BEARING (NO. 2), The direction from an airplane to a& Z8 a6 n: J4 D- w8 ^ ground station. 1 h) u5 U7 Q7 q8 t瓶汇流条,. ?& B# `* Z5 V5 z! K 将从电瓶或变压整流器来的直流电供给工作部件的导0 {7 Z/ k' d5 q0 N4 M 体。 + m. u4 m- c4 Y9 l8 s$ {0 v瓶充电器,0 @0 p9 Y# Q% F8 T3 m; y1 A 用交流电向飞机内电瓶充电的电气装置。带有交流电的) @ U, [$ m+ m$ H# s 气装置,该装置产生直流电向飞机上的电瓶充电。: f* m5 f' R% o( L/ D0 ~: s 舱, 8 _* x7 s+ ^$ X; C% `& B$ z Z飞机结构中分隔的空间。 5 D# ]% Q9 i4 M2 H6 v% O q c二进制编码, $ h# s4 K+ W2 K见Binary Coded Decimal 6 n" `) |6 u: c0 B& tBATTERY ) }5 v& m" u( l' o$ p# v5 H7 iw " h0 l: u* z( R) b- s, g2 G0 Oo6 a& q3 k4 ?+ q. ~4 U9 {& B B " E7 ~% g @3 r5 MB 6 R& m! f: m1 ]+ }7 t6 L! @B/ e$ x; K: i" z2 g. Y5 q0 r8 n g# I+ S2 c+ g0 o5 ^; L+ B$ a BEARING (NO. 1), A surface that supports a moving 5 Q- P" V7 \/ g& I) ]part and reduces friction between the two./ g1 n" ]3 j! J4 ]9 N3 O6 A4 e* i1 F1 }) h0 r0 O8 w3 }$ X" v" B e* J, C' ^ _1 f) U8 k% {& c8 r8 }& `* T2 @& K5 w( S/ X! S" ^% O; ^; \1 O$ I( _1 }: S& R 信标, : ]7 _8 I$ ^( R4 X% c7 i5 e发射引导或警告用信号的装置。/ T( H/ n Z% u' n0 j# w. v 方位(NO.2), l: U. x r7 w" P" ~ L 从一架飞机到地面台的方向。 - g& G; d$ c& I$ {$ o# I轴承(NO.1), ! r% H3 o% @. H3 w6 T, S4 O* d用于减轻机械转动磨擦的机械装置。9 V8 _) m J6 | 英汉对照民用航空词典B OEING & J0 e% Y' f( x5 yTECHNICAL DICTIONARY 19 H% j& T' P$ M7 JBELLCRANK, A double lever in the control syst" |% a9 [0 M w3 k( z F, g, w* e changing direction of motion.6 E# N# e* b: U0 c* p& U em for ) h$ j* g3 B6 W" Y/ b* d7 b/ [ct in the3 @) k- y0 @ F' ~& I, w2 p neumatic system for absorbing expansion of duct due. C2 k b T% g# V6 m5 ? heat." }# q3 o) N; o6 c: t) U8 L) n ELLOWS (NO. 2), Corrugated folded or pleated : K- I$ z1 N: J% A; U: lontainer or compartment used to measure pressure. ) Y% A' ?6 {% s8 j8 U8 M8 \EZEL, The part of an instrument case for locking the ) M2 x U* r8 e0 p( t6 E) Klass. 6 N0 H! j2 `, H8 h4 k3 ~# u3 Z) pIAS, The potential difference applied between two1 o6 }2 ^: z6 v oints for controlling a circuit.* q5 D0 Z" c& b' _3 Z BILGE, The lowest part of an aircraft fuselage. A place 7 v3 r9 K9 T- n* B" i( _5 S* \# g9 Bwhere water, dirt and other contaminants collect. , R" M; c+ K" \' W& H6 J气源系统内提供管道热胀冷缩所需要的余地的波状1 i" \4 ]9 r- R+ ~+ A 轫管。! Y) r% u: A$ [) q; y0 B/ f% o0 n 空膜盒, 1 f: r k* I. |; r" p一种具有波状表面的容器。用于量测气压。7 }* u( Z# V7 s) O8 L 嵌沟缘,# F' V' g6 V" G$ B) H 将表面玻璃固定在仪表上的圈状零件。" C7 T, S# d* J 压," k& H( _- `% @9 q 在控制电路的两点之间的电位差。 6 ^, t% v4 B6 D2 {& Z+ ^% `" X机身腹部, 6 a% h% t, M2 J: u$ r机身的最底部,通常水,脏物,和其他外来物集存于此。2 y; c- v. Y& i4 N4 l# z& M" E8 ] BELLOWS (NO. 1), A corrugated flexible du. ] f/ ]: p7 }! F. g5 { Y5 n p - x" j. @/ W, O9 }3 Z' d& A' Jto# @! N. s, n) X B, T. Q/ F, O w, U7 E% r4 q% U c 2 |* Z: a, W3 Z7 EB + J6 @6 D$ l( f; W3 w: X' tg& \% R5 k N2 _# J( L* k B" @5 w- ]5 B1 ?: g, }" ~ p( p, ^: s m( j- X 直角摇臂,! s9 G6 G( h4 B$ j" ? P0 e 在操纵系统中改变运动方向用的双臂摇臂。 - l* T! ~) H, A. X! L: P波纹管,4 P. R/ Z0 X) I& e$ }5 j, Z1 U6 u- Y4 [4 |& c% O4 L" R3 N7 u# ^5 m- X* D& [$ ?( ?) W6 T" c9 y* X0 W" c8 n4 {英汉对照民用航空词典B OEING + v# v6 K; K, R! S2 QTECHNICAL DICTIONARY 20 / b/ h$ \+ {' ^BINARY CODED DECIMAL, A system of coding each# f# Y, ~* [5 K2 I; M1 J- d. h5 u, G( N digit in a decimal number using the binary equivalent. ' s2 a$ U7 C/ E9 M) gBINARY NUMBER SYSTEM, A number system using + V: P* z5 I- Y/ u7 Hs/ c) S7 ? m# z! P$ A$ k IT, In the binary number system, the smallest unit of # G0 A: V" d+ G6 n- a$ lformation, consisting of a 0 or a 1. ' f# i7 n2 S6 e6 a" tITE, SEE - BUILT-IN TEST EQUIPMENT ( r2 X- N/ h+ m1 P& W- M* sLANK DISPLAY, A display that does not have any2 s+ U% q, J) W% I7 r) k( @ dications, normally due to failure. $ Y& N, s! a' G# e* l" ^LACK BOX, A container for electronic circuits to record' j" Y2 ^% {1 e( c' v' s ight data. 7 k8 D X, c( {6 N/ g5 sLEED AIR, Air taken from the engine to power various0 T. x' S. i3 T# y ircraft accessories.& z+ z) L; d1 i1 P; [ A valve in the pneumatic system for air/ u1 V- q1 l' R2 B$ {- J" u supply from the engine or auxiliary power unit to the ' ]2 }3 Y9 x7 \* k% `% ipneumatic manifold. A valve on the engine for reducing6 q7 a6 T8 ] z6 U' z pressure in the compressor section. 0 _( i8 `! o+ H" c0 A' \进制, , T/ ?) O5 w8 @& E5 M0 \+ |进制, ( h0 J' j& h3 [' n9 u* }一般用0和1)和2为底的数字系统。 l8 p. c6 T5 f; c) e# O. s' G5 M 特(二进位数),8 J) S3 H& ~8 M! q4 } 二进制中的最小信息单位,包括0或1。 0 i2 V) z4 f% S6 {: c0 m内自测系统,/ ~& s0 D& z! i- e7 n4 h' j1 } 见Built-in Test Equipment / t: M+ p# x: h( Atwo symbols (usually denoted 0 and 1) and having 2 a , y8 {! O; Q- M8 U( C7 O. e1 O, \its base., N7 i8 ]) b( s5 \3 `& Y, z B1 r; p: }; E% R* @" [4 t in# K, c1 R0 P" E8 N2 R( d B . O2 i+ R& O- T6 G% b5 xB, E$ G& f- W, i( C9 T$ W" o in , I, R& [# @' ?' NB0 x7 u5 R0 e$ }! P$ U* W1 R7 L/ j fl 9 Y, k0 X* F4 f5 sB0 I h8 S% w* y/ j( g9 z. r a4 {+ M/ j+ f) ~: F4 Y BLEED VALVE,. _! h1 I1 J, B. p7 a6 h# n 二进制编码的十 1 G, W6 e% C& a d- k4 b3 M6 l一种编码系统。用等效二进制位数编译十进位数的每一( _9 d' Y( E) e 位。 " F* S) ~6 I: _8 D" ~7 c3 B( Z" Z1 ?+ O7 Q$ D" \- ?$ A. ~以两个符号($ \. G4 M& L G8 s2 F, X: [% M" \/ m/ S M$ \) L0 q. u.0 F3 G6 h3 b) O; ^$ n; W/ F( C 白显示,4 `/ t- o7 Q* ]: P) D; _ ] 通常因故障而造成的显示器上没有任何指示。 $ c. b: M8 S! r/ D5 S n, F2 ~/ x匣子,) y6 N& b% F" ]7 i6 r 装有用于记录飞行数据的电路系统的容器。 3 Y! @! f& u o3 |气,( v, _0 y( v; x8 {0 L+ P 取自发动机而用以驱动飞机上之各种附件的空气。 & v2 g) }1 c+ N' m( H9 \$ n7 E" d, F气源系统内,使来自发动机或辅助动力装置的空气进人6 O2 n2 g) N8 R, d$ a 气源支管的活门。发动机上,用来降低压气机压力的活门。' t) N# N, G9 y+ S1 N/ y6 b7 j2 f" \: w/ Z+ M3 I- _% c& p5 _1 K) g/ z7 T0 P7 {! Y: z引气活门, 9 l* _! B0 y7 Q3 Q6 z9 G" v英汉对照民用航空词典B OEING7 k" }9 }. Q" h; ?. q, ~% y TECHNICAL DICTIONARY 21- v+ A4 @) n) F x2 E BLOCKER DOOR, A device on the engine for blocking1 H3 f, q+ M: Y- m! e the normal airflow during thrust reverser operation.0 \" I) p" J9 V% m1 ]+ p! i4 { LOWER, An electrically operated fan for circulating air. ; S& Y% z# ^) j7 V) P- w5 \0 R4 TLOWOUT PANEL, A panel in the structure between 3 |& K. q! V6 mo compartments that opens to equalize pressure in ) O; D) H1 p! B* I! n7 Ve compartments. ; y" ~/ `$ u( X* [+ D& NODY GEAR, The landing gear attached to the 1 D8 M6 V: R' l. _6 Sgrounding. . C- i) l( T8 c3 ~正常的& K Y! L# G1 W' {( u 气流。# r4 M) z- u, p; q; L3 @ 鼓风机,$ [+ }! h9 [- }3 n/ @- b 用来使空气循环的电动风扇。 + Q3 V* h" L2 z) `8 g6 w压口盖, % R$ g+ c; s0 ?/ p两个隔舱之间的口盖,打开后可使两舱压力相等。 ) s5 o$ G( G3 q) {身起落架,9 C' ^+ W3 A' i! H' n$ l 身构架上的起落架。5 t6 l2 g9 l/ E. v B' X { _: L% ^* a% o B / P% V; a9 u- n Wtw4 q0 N1 R) V) F6 z2 g; C) I0 ^' n th. n: ~4 F) [. J1 E6 x9 X7 p& k B6 j3 f% o& Q. ~9 A8 y fuselage structure.$ ~$ h. ?: |2 x: d! I B2 b! ?1 @ BONDING JUMPER, An electrical connection between " u0 L) o/ i3 u- A4 ha component and airplane structure for electrical) c6 Z, F G$ j( t5 h+ c4 c 阻流门,7 }9 f! B* M3 S# }- y U9 I 发动机上的一个装置。在反推工作时用于阻挡* {4 D* r. h% g T' w0 I5 f) U6 ~; D. |8 b- K, Y! ?! Z; j) q 装在机 9 _2 V1 _. `$ [* G搭接片,/ H% }1 t; L+ `. A! A" J# _ 连接某个部件与飞机结构以形成接地的电接头。! D5 F3 C ?" A& u0 F 英汉对照民用航空词典B OEING1 A$ P E. b8 h( E3 p TECHNICAL DICTIONARY 22) X1 C7 ?$ w4 ^( N0 d+ K( ? BOOLEAN ALGEBRA, A mathematical system for3 e' I; D8 c8 v7 F writing combinations of logical statements. 2 [) B0 w" q' E. ^8 YBOOST PUMP, An electrically operated fuel pump for 8 z( W& S* z, X7 h7 a+ d! c5 `: afuel supply from the airplane fuel tank to the fuel5 p$ }9 l8 G/ X( X manifold.2 b" X$ v+ G- @ BORESCOPE, An electro-optical device for looking at5 l7 S) J' S3 [5 B7 Z: W# T ternal parts of an engine through holes in the engine. ! E% Z; n9 O$ e% |orescope ports)0 k& n, @/ T2 ?3 z+ f* W0 x9 r OURDON TUBE, A curved flat tube in a pressure gage7 w t f b6 k r moving the pointer when pressure changes inside : {" p2 z; C, u+ O, ^8 gon the ability of the brakes to5 [3 H; }5 X$ N4 t0 E9 w bsorb a predetermined amount of energy during a 0 j7 R# f# U: C, K0 u4 d2 Bjected takeoff.! X8 w2 }; A1 d: o9 |2 n 用于通过发动机内的孔(孔探口)观察发动机内部件的 0 D) }) T; o: W$ Y; [5 {, K6 @- U% r0 d光设备。 9 u' N" q Z0 O! f0 L# y" ~端管, - u, |. I1 h# q% }& Z2 s- V- u, v/ [测压计内的弯曲扁管,管内压力的变化时它使指针移8 } D* S5 ~8 J' Z 力。 , C% f1 m' \: M+ |极限重量, & K! v S( d6 G" M0 V, |6 S: U4 P: c) `& Y# O5 X 起飞重量。 + ?4 V) A- c0 K$ C% a+ f0 X发动机滑油系统与大气相通的通气口。% {, [) S8 L! {* _ in* _* }+ K3 C( v3 ~' y* F$ |5 ? (b: Y- D' ^& M v" L/ x B ! K; F \& U" m. L( a6 lfo% u- i! y9 G! @9 ^/ s the tube.( Q6 ~: N( T- l- k" Z& | BRACKET, To enclose or surround. " F: j) `8 n& a9 I' S6 qBRAKE ENERGY LIMIT WEIGHT, The maximum 0 C- @$ A% r( itakeoff weight based& n& ^" F( l* r! a7 d$ E a* K1 A& x: d! ^3 V M re4 y/ K. r# l9 Y BREATHER, A vent to ambient of the engine oil system. v, ]* t/ q9 c, o4 i; m 布尔代数, : q$ C1 f+ H9 F, U* N; Y, Z, B. U一种用于编写复合逻辑命题的数学系统。 / s% D* w R2 K. C: n增压泵,8 N& ?4 O2 ]0 b$ j 从飞机油箱向总油管提供燃油的电动泵。$ a: a* Z7 C: F8 a. X( K) X0 ]% U 孔探仪, ) z7 ?. O; H5 B" L- }+ K e* f8 e ?) `$ b; n b6 G: D% ~6 Y' T" I- j% t. w 动,以指示压: U8 P/ N. W$ C, S( { | 托架,- a. u- q: g& p N% @/ n! L8 B 用于作支撑、装托、或围绕之用。 " D0 t$ L! m, A1 x刹车能量 % y4 m5 S# e6 I, J7 q7 \/ E- G中断起飞过程中,取决于刹车吸收预定能量之能力的' G& A6 l4 B! f9 M# `6 ]2 u, P1 f% J, n) |$ u; c( p8 j 通气装置, 5 a& m+ [( ]5 X6 O2 F" K, K英汉对照民用航空词典B OEING3 ~/ l0 P7 \8 G; i TECHNICAL DICTIONARY 23" {' _& o, X4 u& [. d8 {4 |- y BUFFET, Vibration of the wings and airframe resulting3 b( ~4 Z* p: k from unsteady airflow over the wing; caused when) D' _9 y- R8 a& c5 }/ C airspeed is too slow, the bank angle is too steep, or & a6 a7 w5 x* Z5 b& oirspeed is too fast.% f- t9 V1 [# n I+ b, X0 ? UILT-IN TEST EQUIPMENT, Equipment installed on+ I8 G4 I* G7 o" u, o7 M e airplane and in airplane systems to test the systems $ k- A' B: m& |ithout external test equipment. 8 C- H5 S. W8 p+ Y( F. GUFFET MARGIN, The amount of residual maneuver + Q+ @) @; R3 z) w6 v# v1 gapability present before the onset of buffet.4 t$ i1 M$ O7 d: w! ^9 P UG SPEED, A preselecteed speed to be observed1 W: J/ Z4 Z! Q& \ x nding sequence.( ?( Y1 E$ R. ?5 S3 ~ k# [5 T" b) ?% n. v# x1 ]* d ng landing gear operation. & O" `% T+ `" j0 w5 G$ u* g速度太慢或太快,坡度太大,均会引起抖振。 & L e; R* ^# ]+ V3 k自检设备,3 X8 U# [- z) y2 {. K7 P 安装在飞机和飞机系统中,在无外接检测设备情况下, . G1 D4 }; S/ W) }9 ?用于检测系统的设备。 8 n; |& `8 v+ B0 ]5 n) c2 N% H抖振裕度, + X+ ~! z; y0 E: z0 _飞机在遭遇抖振之前,剩余机动能力的大小。2 ]: ^$ F) M/ n5 k; P 标速度, m0 e' w$ j2 |1 n% I8 h4 C- o在某些机动飞行过程中,特别是在进近和着陆时,飞机 ' [1 H* x. ~+ u* ^4 W6 ]+ `& |) ?预定速度。 , `9 m' t8 ?# u力装置, 3 W! w, i0 G' `1 ]: b架工作的一种机械设备(弹簧或减震器)。5 C! u/ b7 e( g) N0 ~7 q 流条, 0 l, f, n1 y7 `6 j) J s9 J- V6 W在部件或组件之间传输电、数据、或定时的单一电线或- {. c5 P% z, d7 S, r a. x, \3 M) F& M( X6 Q j" y* j( { B! x: F- F9 j# ~& D6 u& ^. s th) Q' Y5 l& f# \& S4 f4 ]+ ~" h9 O i w 9 l. }/ C1 m* K( R5 [0 O3 R. IB , o- k8 h' U( M8 _3 v* Q' w) O9 A3 ]c% f, f) L( F1 [4 ]3 @ B# r" o! ~% E' N* w; ^5 [) V: f/ N during certain maneuvers, particularly the approach and, N2 W& v; i* f' s7 ` la5 V' z8 E: a2 f* V6 V' ]' D' M; r BULKHEAD, A structural partition in the fuselage or 5 d/ a! Z2 t0 ~' h I5 N+ ^' Kwing. , k) j) K0 C. I3 s) F& i# t2 dBUNGEE, A mechanical device (spring or a shoc8 a- n( @# `4 W& W& k6 e absorber) for assisti . ? _- V/ z' o3 V; K6 o7 k9 gBUS, A single wire or group of wires which transfers9 L0 m' M$ G' O: P power, data, or timing between several units or# P4 Y$ {: W4 ^9 c) a- z* @' P modules. ) f0 y& u( y$ \" @5 o3 H抖振,6 ]$ v0 v( M$ {& @4 d8 o 由于机翼上表面的不稳定气流引起的机翼和机体的振 . n! z/ P0 T# w4 U k# H( J动。飞行* T. Q1 w: u% h$ e4 D w& F" o- o0 Y; o' Y0 {/ `% ~3 F# l8 m所应保持的1 O! W" P% V$ R) V2 f- i 壁板式隔框, . E( X- R: m# B0 @. I0 c机身或机翼内一种结构隔板。* D* F# P" p! f) m" c( I# J6 i4 f9 I" j$ S! d' a6 q用于协助起落, m, j. ^% j4 v6 F- i7 F) a, p7 Z v! n( V# ^电线组。' I7 n/ p, K! M9 D1 t2 } 英汉对照民用航空词典B OEING 5 P8 L. F6 ^% t. I- PTECHNICAL DICTIONARY 24

使用道具 举报

Rank: 9Rank: 9Rank: 9

4#
发表于 2008-12-24 21:37:30 |只看该作者
BUS DRUM, A mechanical connection with pulleys& g$ ^. g* g# ?: T& i cables in the control system. 2 f, @! d5 ^3 x* Dand1 m) _9 ~* K- h+ S l circuits for control and protection of 2 c; R% f4 ?1 X; u4 e: B+ wlectrical alternating current supply to the airplane. ) K/ J4 }- g9 K. @: O0 L& Hduct for closing and opening the duct0 d% Q: q9 L9 u- C: p assage./ A5 Q( k" T1 a+ s; G UTTOCK LINE, A vertical reference plane along the , s( E% O; e* Y3 u* X7 zselage for horizontal measurements of the airplane. 2 t+ m' x$ B) J6 l3 B& x3 z接。5 y M- `1 h/ F1 _0 T5 K 组件,内含控制和保护飞机交流电源的电 3 P/ f+ U& R" C9 x0 k6 t# \/ }* m# }& S作动简控制的转动装置。用来关闭和& z+ d% J" Y- Z/ b0 S/ {- T H: p 启管道。1 B. T! D8 |, p2 P' Z: p 沿机身走向的垂直参考面,用于飞机的水平测量。0 E0 j% |& X5 U$ m BUS PROTECTION PANEL, A module (black box) * G* z& S& j" O7 N3 s/ x6 g: a. ccontaining electrica 1 v3 o* z: m' I# ge 2 q& D) d& r! SBUTTERFLY VALVE, An actuator-operated, rotating+ c; B* J5 F) I/ u& q& ~; W) x1 J2 C6 N device in a ' |9 i3 Y' F1 r+ c1 bp: b5 t) ` L( l5 h8 O B% l `8 c6 N" C8 _9 u fu' `' K: V7 P0 m/ _* \* }. w2 o+ V 转动鼓轮, . `% R% ~9 h8 F6 T( }) U在操纵系统中,具有滑轮和钢索的机械式连 ' _# K3 I, z/ l5 t3 B6 j汇流条防护板,/ T+ C9 }3 _- p. u 黑匣子式的1 d. Q# m, O+ o \( X4 h+ [3 k0 F% A* g2 [ C- w+ o' `! z; U9 w2 L4 m4 o 蝶形活门, b8 x* g6 K* f; K) B- m 是一个在管道中由7 g" G. J7 [0 }' Z( c: m2 V: o' r 纵剖线, 7 K) |# _3 w8 ~& l; o英汉对照民用航空词典B OEING 8 U9 a6 K7 W: y% xTECHNICAL DICTIONARY 25 7 Z! @+ D1 U2 x2 x! O) v, G4 S' SBYPASS VALVE, A valve through which air or fluid will 5 F9 Z2 ]! {) l9 Pflow if the normal flow path is blocked.( y! F: d, `2 _8 ~4 J BYTE, A group or string of binary digits. A byte is ( f0 X" w' Z d* }sually eight bits long. & b- _# H7 a ]$ V4 c& P- TABIN ALTITUDE, Atmospheric pressure maintained& q: N7 X8 T- F' _+ s ithin the cabin, indicated in terms of feet above sea- o! \4 d" B: B% b I) E* Z ALIBRATE, To repair, adjust, fix or correct the, q: n; @/ p, u easuring capabilities of a measuring device.& M. R* E9 Z1 T3 K ALIBRATED AIRSPEED (CAS), Indicated airspeed8 D+ p, a$ R# q' R5 S2 @7 K/ E; j AS) corrected for position error. " k m* P; q. q$ ]+ k0 N) qnical6 q) O. J& E+ T. h- ~7 _6 b omponents.0 r. d Y3 W( _4 {: k3 C1 G8 V6 z5 \1 { 节,/ q# m' B# d* Q; p9 ^& }6 \0 F 一组或一列二进制数。通常一个字节长8位。 " h/ C5 ~6 A2 Q舱高度, ' R/ ~. K7 N e9 W: J4 p% X座舱内保持的空气压力,以海拔多少英尺表示。 7 L; \8 [4 \, ]/ `8 F7 U准,8 }, d: ?: Z& ]5 l 修理,调整,定位或改正测量装置的测量功能。( I, x, f- E) F [ 正空速(CAS),9 @7 G8 X7 I$ b4 g, [" j 在修正了位置误差之后的指示空速(IAS)。8 t& u P( G9 E/ X! g& i, M0 c 用来移动机件的一种转动装置。 7 g+ e0 s" M' q( D" Xu, ^' ^3 p. U) R' Z$ K0 E C 5 e3 p0 D& h; {C7 l% a) w) b8 D w- c# k& w8 `6 p- a level. 8 W* Z, A/ A- s9 D6 ZC6 H! l# T! y, K; v- U! K m4 C B, g. w! x! A; \! j C- y, [( B/ o% }: v, O (I) `/ C. i* ]6 h! _3 Y, Y* l7 u CAM, A rotating device for movement of mecha % I- Z5 {: f! ~1 kC + S: j) ]# c* ?) I旁通活门 + N! Y. D+ }) U/ U& J气流或液流在正常通道阻塞时所经过的活门。 % u i/ k; g7 H# M3 I4 n1 _9 g7 H" t% a, a; y# z0 V$ v4 c9 r/ J+ i3 z2 G+ S3 r; {8 C: B u9 m1 N' g* f" W0 ]凸轮, - Q! o2 n" g, o) [% \( ~$ `* m2 B/ m英汉对照民用航空词典B , o# p3 B- i- E2 Y9 ^CAM-OUT, An autopilot condition in which the actuator4 L! T# `# Q$ t! f detent piston is overridden, either manually or by the3 t6 ?) h: g; b1 b7 C ther autopilot actuator.4 T2 f! W, L1 K7 L AP, SEE - CAPTURE ; \; z8 [- Z. b; j+ mAPACITANCE, The measurement of electrical energy3 C+ l- k6 w; |% i( F7 J tored in a capacitor (condenser).! e% |1 @( s4 G! U. y$ B! p APACITOR, An electrical component of two metal! f& R' E$ D6 [! F lates separated by a dielectric material, for storing ' L9 }( B7 z1 x/ |- Rlectrical energy.) J- X* E" j7 W1 C5 ?( X! z CAPTURE, An autopilot or flight director function to1 v4 `4 P' ^9 M! T! }! o) k acquire a selected mode. 0 N/ |; X$ Y$ Z) d% ~CARD FILE, A container on the airplane for printed/ C- ^% }* B w% n* F- C. T circuit cards. & r: ^4 q. m" s9 T8 f一自 " U; o. K L# \! U. B动驾驶舵机所超控。 % ]4 }( ^, }+ O/ T* @, v截获, 5 d% q; h# `( x1 W$ W见Capture 0 Y3 |$ O; `& Y5 M5 P2 t) ho k6 i3 t3 [7 A& W- W; t# d- ?C' ?) T' d$ k; K* t f C: D2 a, }; G' p% s s5 Q4 N! u: k7 p& Y+ R& t" U& g C 4 O2 M" J1 ~& _' x2 ]( I r: C+ yp) }; N( J- }/ {) U& Y& z e0 K) s/ q* I G6 d* B: | 凸轮不工作, 7 v: D, _9 n3 v) V4 d9 S1 t一种自动驾驶状态。此时舵机锁定活塞被人工或另6 Z$ ]4 ]5 K; r! @' D) c& v7 P8 Z( ~9 S6 B; e7 i电容量, " }' a( ]: |$ F# `电容器内所储存的电能的量度。6 i g+ x+ E% ?' n 容器, " I* U8 `$ f7 x两片金属中间用绝缘材料隔开的电器。用以储存电能。 % T9 T ^4 L9 c7 K0 c( N3 C截获(CAP), 1 B, r* s/ ?# G1 L! r. o* K! W( E自动驾驶仪或飞行指引仪的获取选定方式的功能。 % g T! N; H/ d& A! Y线路板盒,9 G4 K# s* F% |; ^% R$ F4 m, c2 H/ ? 飞机上安装印刷线路板的容器。 + g+ p$ v3 f ?# V; g6 w/ l: S$ [- I; ~* ?$ L B* ^1 d6 XOEING 8 `; r6 a% Y+ I8 g8 R: G0 tTECHNICAL DICTIONARY 26 1 \# E, ]$ Z4 X. k# d' n; U英汉对照民用航空词典B OEING / D1 a0 H# E! b( J S1 O7 `1 k' bTECHNICAL DICTIONARY 27% S7 e, N/ k0 q0 M# W4 ~ CASCADE, Two or more similar circuits or amplifying 9 k% n3 {, p2 ~- e& X. istages in which the output of one circuit provides the ! ^: O* k, _( c! B0 I" j jput of the next. : y6 B w) `( c& k+ c1 n! `# GASCADE VANE, A vane for turning the engine airflow , K' T. f ?7 K2 q9 j) n( huring operation of thrust reverser.5 E1 S4 n& }5 c ASE DRAIN, A drain carrying lubricating and cooling 5 h: ~9 z: G: H& }; z, buid from a hydraulic pump.7 B. L* H2 N" j* [& a2 w( ^ ATHODE, The element from which the principal) M3 G9 h0 B7 I8 w tream of electrons flows. 4 n: k- F3 u2 E3 O" ]6 rATHODE RAY TUBE, An evacuated glass tube with a% j& \+ u/ u1 z* `, ~ CEILING, The height above the ground or water of the ' l9 U& n: ?+ O3 J( O' rbase of the lowest layer of cloud below 6000 meters 5 R, `% a7 Z' s% T' i9 X(20,000 feet) covering more than half the sky. - j w9 T3 Y. k+ k; l! m程。该0 J& a1 N: ]* ^% b! A* [" M 程中,一个电路的输出为下一个电路的输人。2 W ^, M- L9 W2 P- G% _ 叶栅叶片, 0 U. a1 y3 b0 b$ P& N4 F在反推工作时,使发动机气流向相反方向流动的叶片。& D! ^% R) A) r' u) s- k* `0 { 匣余油管, # e, V7 Y5 ]. o, a液压泵多余的润滑液及冷却液的排放口。$ W3 [7 h6 @7 X 极, _$ N- J# S/ D$ h" w 电子流流出的极位。 C. b- x5 q, F" X 极射线管, ' i- N- V! B% b x. H( _9 @有显象屏幕的真空玻璃管。用于显示信息。 5 B5 Z3 B9 [5 t) _4 T云高(云底高),5 }) A3 A- h" V2 o [/ e 6000米(20,000英尺)以下已覆盖一半以上天空的最0 M9 ~% p' L6 x7 K. w 低云层底距离地面或水面的高度。! x6 j: }" M5 J) b: Z- u" I! l in! g# d$ B% @4 ^5 l5 G& A( F; K8 ?1 {1 j C. I0 C. p/ O! V0 Y" k" A* t d: t: V& v0 x4 A S C! _8 [5 f& c5 \1 m* d1 N fl 6 [8 S7 a( d I/ t; w+ jC8 f. C: }: Q: y! h; D s - d9 E2 E. s3 F7 x9 c% ~! {C4 a& e7 W. H# |: k0 P6 p2 \1 @7 O viewing screen, used for displaying information. 0 u( ^! w$ y# e4 r, v7 n( `级联,1 T9 e O7 b' d9 p+ w 两个或两个以上的类似电路的逐级连接或放大过 \2 W5 d% t- f' A! ~/ Q# W5 _7 h$ f. Q: `1 C. r) |+ {/ @5 T7 d$ G( d$ p2 g: J$ k3 ~* D& [1 X9 B2 u一个具 & Q& M2 f1 X; r+ x英汉对照民用航空词典B OEING + v+ ~5 `9 h1 c" p1 Z" p5 h; `TECHNICAL DICTIONARY 28+ p8 b5 e+ G* k2 |3 r$ X ~ CELSIUS, A temperature scale in which zero is the $ u; c' P0 P& k+ ofreezing point of water and 100 is the boiling point of; D8 c8 }. c4 z$ m) a( p water. 8 E# W* e1 D' K; R- ZCENTER OF GRAVITY, The balance point of an object # C$ P% h3 L& L+ xr rigid structure expressed in terms of percent Mean O, a. Z* h! E+ z2 A1 _ erodynamic Chord or in inches from a reference point. + A, f/ T; W SENTERING CAM, A cam for moving a mechanism to a& H" k- ~/ p/ k5 P. L eutral position.6 z9 i# Y1 u" p2 u IGURATION, A configuration of the7 m) }9 m8 H" z' f ircraft approved for operation by the local governing8 J3 R/ d0 J; K, [ gency. ) S/ I) J G0 n$ W; gENTRAL PROCESSING UNIT, In a computer or& h7 b$ O8 E0 }; k) ?0 J, q igital circuit, the section containing the arithmetic and 2 v" `$ Z/ P2 t- s0 jgic,control, and internal memory circuits. + n$ G( P$ n- s A4 z* OENTRIFUGAL FLOW COMPRESSOR, A type of, N* T- w9 N7 [( g/ c. d ompressor in which air is taken into the center of the 9 J: x+ g* U# q0 I7 f5 V& }/ Tpeller and is slung outward centrifugally into a diffuser # V5 A; K- ~2 ]' {here it is slowed and pressure is increased.$ \" Z. F+ r p/ Q CG, SEE - CENTER OF GRAVITY3 _4 m1 W, ~/ b! P9 _1 y" c7 R 构的平衡点,以平均气动力弦的百分比或 e9 X4 D7 \- {6 | 某一参考点若干英寸来表示。 " m5 o- M0 ~6 p5 e中凸轮, $ @: q4 z' x! ]2 r' S3 @& g将机构移向中立位置的凸轮。 / c7 D7 r, p, i8 h: |" n格的装机状态,5 ?; q( F9 ?. P( A 由当地主管单位批准使用的飞机装机状态。 Y: S; w4 i3 R1 X, Q% b中央处理器, " h& E! |, _$ _: b计算机或数字电路中含有运算,逻辑,控制和内部存; E1 {, A$ `# [ 储电路的部分。 1 k' ]) B! A$ l, ?8 b4 P心式压气机,% u8 ]1 |: B, a. y& W; ?1 } 压气机的一种。当进气到达叶轮中心时,被叶轮离心抛5 A$ j' k' B" v, e 进人扩散器。在扩散器中气体流速减慢,压力增加。 ' H5 t$ Y. p) [0 J& S4 K, r7 u0 B重心,/ R' x6 X p* h0 U5 F9 p# U 见Center of Gravity 8 o# R" t% t4 M! B) [, Ro " I0 I# [# z( s$ G! uA $ h2 U- w4 V& d I/ U3 W0 f- ^1 oC" r- V$ D6 O; h( b" h n % H7 J: f5 Z4 w, P8 P" ]5 XCERTIFIED CONF3 ^- q" L4 u- Z+ a9 t f. T a) F3 s, O5 }5 F, q- r, R3 }" f a) w v' \4 @# O3 m9 M4 z1 U9 z" | C 8 {" b7 Q4 q- i5 yd * o% b3 S8 M- e/ ]+ N; ~9 ^lo8 T: r' Z6 x0 y& c7 r6 ] C / h) Q1 i* _: E& Ec e5 y u( N3 C: o0 U( f4 tim 8 v, u4 f3 Q$ U1 h, g- i/ Aw ~$ `, h' L6 F3 B2 [摄氏度(°C),0 q- F2 j7 I0 H( }. y7 x, Z1 o7 W 温度的度量单位。在此单位中,0°C表示水的冰点, $ y3 b4 f* w5 V( P/ T100°C表示沸点。 S9 C, |( y2 n重心" s9 Z& Z9 D; ?7 U7 J4 K- c 物体或刚性结 ' C$ K0 c/ l% S1 I/ q. v5 q# @) l6 _2 v; k: ^$ j8 I' {3 t) W; h% } ?2 ^. Z$ i- v1 }8 r+ d5 w4 R( h* H2 x: Q; I0 I0 t7 K7 X) n7 t! T2 u( x! b$ z3 }. m* e2 t- w英汉对照民用航空词典B OEING & P8 X$ r t8 q4 }3 K" U1 |TECHNICAL DICTIONARY 29 3 z5 Q$ \5 u. }. |; c) j3 XCHANGEOVER, Conversion from one mode to another.2 Q9 q" F& J: I9 H( X H Q HARGING VALVE, A valve for supplying air or fluid to/ d. E# y }- E3 B- p HECK VALVE, A valve allowing flow in only one0 t2 y" f. s6 C$ d irection. See Non-Return Valve. 2 X+ I: T+ F4 y+ DHECKSUM, In a computer, a summation of digits or u, S5 r/ Z5 y% W/ O E+ I9 Y- r its which are primarily used for error detection. x& Q& ?0 I- E& K( n0 g v. | HIP DETECTOR, A magnetic plug in sumps of 5 S1 Z" d( w; P m/ Vbricated components for detection of internal failure of ( A! U m# Y% oe component. : v$ P g. Y( p5 w4 hHORD, A structural component of spars or frames. ( p1 @2 a3 _4 u7 F) Z0 [8 ]0 D! l添活门,# ^8 Z+ [( s) P4 ~, s, g- w 器充气或加液的活门。5 ]' h* ?9 y4 @" ]% q 单向活门, $ y3 v5 b' D4 v6 L4 i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' B( i1 F5 B7 c2 z S, L7 p a reservoir. * J5 v) L; Z+ a" E2 KC6 t8 A; l2 j! H4 T3 p d0 q! R7 M. A0 H( d. `+ y7 \ C 4 i) ?. I0 n" x7 `% b- Rb: Q4 k- I: t& Y0 g" i; T: B/ W C: r& z! W1 J- q- U8 C lu % A0 | |* O& F/ Pth* ~5 H( l; J- E) @9 N9 L" R C1 k, P$ `) w: ` 转换, # x+ k' }( X: Z5 G( u9 g由一个方式转换到另一个方式。6 m: r: M' ]( S9 E8 o$ c" U0 ~ Z% G/ D. r8 `2 b8 @用来向储存7 w! u% x& p& Q6 }8 n5 [' q. I1 E3 p6 Y8 c, w% h K9 T总和校验, ; Q/ C- u( Q$ x" V5 e# i5 A' H7 a计算机中,把那些用来探错误的数宇或位数的总和进 - ]& A4 l3 Q5 H/ j- Y; F求和计算。/ X- D1 R _0 x 属碎屑探测器,2 D% R0 Z: \6 ^( Q 装在被润滑的部件滑油回油管路上的磁性塞子。用来探 - n) W3 w A* W1 s- G4 ^- q8 |部件内部有无损坏。 / I- H4 [5 _) A, S- g" T5 J$ ?弦,: Q4 p: X6 v* @5 @. m) @" ^" ^( B+ C 梁或框架的结构部件。 2 s! O+ e, @# y; a' E& J" {: h; i: F/ L3 `0 o5 k2 w5 f( F6 ?3 m( l5 A1 ^% ^, M% I7 u% E/ K* g1 ~2 x! H. P+ G. A6 l) n& f' _- P9 y+ d9 D( Q% r/ w英汉对照民用航空词典B OEING , M& \4 o4 x. M- JTECHNICAL DICTIONARY 30& Q2 \& q# E: Z/ c# S; G CIRCUIT, A closed path through which current flows! V' n( I( H4 M! }! m9 m% M ource. " W* P# F7 X# TIRCUIT BREAKER, A device that automatically+ a; R3 t9 ?( Q3 D eactivate the system.. `8 v3 _4 T; E9 H; `& v lear of all non-frangible objects which0 _ \) R+ v( _- v ay be used as takeoff distance available when5 U% w8 Q. r' c alculating a takeoff weight. 3 O5 A, c6 f) a- e8 D. Pr water under the control of the appropriate- T" S$ c# T0 t" J( e5 O* ? uthority,selected or prepared as a suitable area over - K, Y: g% a# h$ shich an aeroplane may make a portion of its initial # i) a2 P$ ] K' slimb to a specified height. 0 ~3 {) P$ N$ I4 O! L+ Qincreasing. : m3 F& j9 w* c* b4 d3 Q+ S" Msed : }: o3 |8 [: p! PLOCK SIGNAL, A continuous string of pulses used for 0 j, W% O" A) d& J9 \开关," P% |3 S; x) ^$ N 故障情况下自动中断电流以保护线路不受过电损, f4 D* a+ U1 u: `/ ~ 体障碍物的区域。在计 9 I i3 r$ C2 _' e- p& ^" B" G% |, j起飞重量时该区域可作为可用起飞距离。 . `* T/ [1 G! d2 h3 a6 K+ F是在有关当局管辖的地面或水域内一个界限明确的长 1 F4 k. h( I' \$ u+ T7 Z形区域。在这个选定的合适区域内,飞机可完成初始爬 ! l% Y% n! v/ t+ y' N* y9 N" i* V的一部分,上升到一个指定高度。7 ]) h% n9 [7 ^ 飞机高度不断增加的飞行阶段。3 e$ N! L4 O: _5 ^) E' j 钟脉冲,/ ]- g" s9 H# O# v/ }2 `# O. m 步的连续脉冲信号串。 0 v) l. r' W* T) ]from a source, through various components, and back ( U9 m$ W4 j1 F1 y% q8 ~8 b( jto the s- o/ ~" U2 V2 m7 A% Y% q* B7 I C 3 p1 S6 C7 }& J* Linterrupts the flow of electricity (current) during fault7 y( Z0 |! {% X5 o# F! _$ U \3 R condition to protect wiring from excess current. Circuit. }! W! o* [( |, l2 X breakers are also used as a means to manually - G" d) N8 ?. f* L1 id , J. ?! D" c" d* z# r" YCLEARWAY 1, An area beyond the takeoff end of the: ?8 o0 x+ d+ R8 K2 A9 X runway which is c0 F p- k+ H' n$ C( H m " Y) }4 ^1 P, N* \$ uc6 l. V& C1 U0 n' d& l' A3 C CLEARWAY 2, A defined rectangular area on the6 u6 Q* Y0 k, e& |/ g7 M/ v+ ~0 z9 a ground o! v6 {4 ^3 f9 ~ @* ^ V8 R$ z; s a ' _, C& G7 j% `0 M( Y4 G: `w 0 g8 [* e+ P7 S* V9 ?9 ^c7 k, _/ q3 t8 S! m# b. ]5 o, c CLIMB, Phase of flight where the altitude is3 _8 ]1 W( b' Y CLIMB LIMIT WEIGHT, Maximum takeoff weight ba , K, D! u( h) @' K; Kon a minimum climb gradient with one engine # ]& M5 d9 C7 A4 r* Ginoperative.9 q6 z& t0 D5 B C# \: A& }, ]. j synchronization.* C# p g* B* F* n 电路, " X- M/ y1 G2 ], F一个闭合的回路。电流由源头流出,经过各个元件流回 6 B$ P1 y" T3 o源头。 1 K% ~' D& z' [/ l: n0 |( k( w# a. k1 B. \; N! U7 ?能在 . h9 W9 x* ?. q( d0 L坏的装置。跳开关也可用于人工使系统无效。 $ x( }% O3 ~% o/ ~" E一号净空道,0 i% M7 [9 }& x* a2 F; m8 o 是跑道起飞端以外,不含任何刚9 u& K5 w' ]& Y1 D0 |9 r6 Y' j9 E/ L! Y/ e$ m1 O% R 二号净空道, ) g3 [: m1 D6 W5 X! d. D: `9 R2 Y! m+ _; q! ~- w- _$ R1 A5 j/ a% [$ B 爬升, # M- M' e, V8 y2 w w爬升限重, H* B# ^" g& f6 w 取决于由一台发动机工作时的最低爬升梯度的最大起0 E6 m4 y$ a9 }2 V+ P- m 飞重量。- O: L5 a( T% ` P: S% G% n8 V3 n9 [# `6 ? T$ i用于同# |& t4 m: t$ l% { 英汉对照民用航空词典B OEING. J0 U1 |2 K9 f { TECHNICAL DICTIONARY 31 0 a* H9 l, @. A' DCOALESCER, A device in the water separator for2 ?5 @6 ~4 Z. W8 V* u* o/ R! _ ollecting moisture from the cold air. + b9 I- `& L+ Yn antenna with a receiver or transmitter. ! t" ]- m m6 [" h$ ]: nhe cable has an inner conductor and an outer1 |5 b) ~0 h! ^3 c* d rounded shield. # X0 c- y5 v. lting one inside the# v$ x0 T6 }' c5 A ther for rotating the low and high pressure' ~; v7 K, y7 h6 B7 H- ?' s ompressors by the low and high pressure engine 6 z6 y* m8 \+ e8 yrbines. , B& u' x- k& K6 X9 |1 uOMBUSTION CHAMBER, A part of an engine for' G! ^6 f! @8 } urning fuel in the air supplied by the compressor.0 {" ^$ W7 q0 Q/ Y5 Z# o* [9 j3 @ 置。) i! N9 _: J+ p( S$ \" H \ 射机的电缆。电缆6 v+ W# c0 K; G+ X 中心导体和外层的屏蔽所组成。9 k+ V7 n. J) C8 K L6 ^5 D 两个套在一起旋转的轴。用于使发动机低压和高压涡轮3 b% O5 ?( f/ _& w 别带动低压和高压压气机。 2 M3 L( I3 [; }) h+ |烧室,( Y6 S' C' L' a- P- ?' y 发动机的一部分。用来使燃油和压气机所提供的空气相% n- s* ^9 ?& u( O/ `/ T' }/ ` 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 / J. }& a: r+ o" z3 g9 MCOAXIAL CABLE, An electrical cable usually$ G+ b/ ]' N; Z$ h- A connecting a; I8 I) I+ D; r) ~$ k T ; s, Z- n: m6 n& V( J- {7 d4 Cg3 _. k; }3 d1 H6 G3 C COAXIAL SHAFT, Two shafts rota # f) @0 f9 H9 N6 z6 B% Eo, S: z+ p. z; N& ]( J. Y c7 z7 e% v H" J5 v! x tu ; Q& R$ I% h0 \& t) F: N" ^9 Z8 YC( E; a! I# F# t; J+ M b& A X, k: s1 p! C& b7 i7 ^+ y 凝聚器,: I( p1 U& L. c: `! f+ R 水分离器内收集冷空气中水份的装, w! N3 ]- L3 Y 同轴电缆, 1 Q1 o- p# l2 G/ c, _* H一种通常用来联接天线与接收机或发" i& k0 p# |+ Q9 b: H; Q+ ~9 K7 o 同心轴,* Q( } k4 s: A. a: t7 k7 I+ H4 L! w7 @+ y0 d8 A& ]1 c5 R9 F% l" {0 F. \( m! m7 D" R9 s, m2 \- o6 Z# M英汉对照民用航空词典B OEING # F# ?. U/ |2 C( e" b! zTECHNICAL DICTIONARY 32 5 M: f+ r9 ` [$ m9 w0 SCOMMAND BAR, A flight director pitch or roll comman 8 {2 Y/ m# C* ]3 H+ Windication.' K; j. o9 Z; n, l; Z6 t4 M d# b$ o* U% [* N( |7 @ OMPANY ROUTE, A route flown by the airplane ' F+ {, l m" t5 v x) MOMPASS LOCATOR, A low power, low or medium + @0 Q: k+ v6 ~" q$ j6 ]7 Yequency (L/MF) radio beacon usually installed in 1 {* U; I N0 d' aonjunction with the outer or middle marker of an, s4 q5 @; g$ R' T# o9 \ tor (LOM), A compass / G& ]# x( V$ o0 M4 dlocator installed in conjunction with the outer5 K. X0 ]$ A+ H( M marker of an instrument landing system. 3 ^( f7 B1 Q( R+ L7 xss( d! g4 b0 J2 w) l le; \& k1 _7 I4 H OMPENSATION, To offset, balance, or counteract.3 |* [( P. J2 N( f* C OMPENSATOR, A dual capacitor for changing the fuel' a' z9 L: V; ^ aging circuit capacitance due to changes in fuel * S2 Y+ n* j7 z& a: }' rensity.: @2 h# _+ n# Q) V OMPOSITE MATERIALS, Non-metallic materials used O. y- Z7 W$ [( Q+ `( o& ]r airplane construction. Fiberglass, Nomex, Kevlar,; f- A* h Y* K; H7 X+ r, p raphite Epoxy are composite materials. - c: x( y4 a# z4 Z司航路, # g: z# U8 V' _, G2 a8 N3 w6 [在飞行管理计算机数据库内由航空公司飞行; G- e% S/ m/ S2 e8 h 盘定位台,: B3 e/ R2 k$ h$ L4 W# F$ }% g( K, T# \ 与仪表着陆进近系统的远距或中距指点标配套安装的 ( B% {- o; x' W) Y" K9 i( _6 Q功率、低频、或中频无线电信标装置(低功率NDB台)。! t- Q/ V$ f( I+ R 程序中用来导航。8 `) z# M/ J3 P p4 M 1.远台, 7 O& i' W" \# o1 j" o" d+ f3 h7 [与仪表着陆进近系统的远指点标配套安装的罗: o* G' ]) Y$ x( }+ X* x 盘信标台(NDB)。; [9 n# t! \' g+ Z' [ 偿, ! J. c: l. u0 R; k抵消、平衡、或中和。; A& Q- a3 v( ] e% Q! t% n9 j5 o | 偿器, & m- `7 V4 n1 z6 Y在燃油计量电路中,用来改变电路上的电容,以与燃 5 r* ~ f) Z, w: E5 \. E0 s, E+ c密度改变所引起的电容改变相抗衡的双电容器。 & J$ x0 K4 Z1 }& `合材料, 0 }/ s; j0 T+ H& y+ P" t7 O用于飞机制造的非金属材料。如纤维玻璃,Nomex, 3 O6 }( I$ v$ P/ T% Uevlar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 % D# q7 l K$ |% H/ D: Xoperator that is normally stored in the flight 5 w/ k( W7 V/ ymanagement computer's data base. & m3 `* K3 I' G) R7 @) oC, a+ ]$ z' s: l! m' h# t( |$ ~ fr1 E7 d6 ]4 d8 v, A$ F c$ U0 E2 ~5 w4 m5 O! b& \8 `) f instrument landing system (ILS). It can be used for6 k" V8 d$ `: W, s+ n: a navigation as authorized in the approach procedure. : Z# l4 {6 r- B3 g+ I3 Q1. Outer Compass Loca; E* r6 G9 V1 U8 {# h# Y6 k 2. Middle Compass Locator (LMM), A compa 5 J" c+ b7 g$ dlocator installed in conjunction with the midd ' M4 g, }9 Z, a4 b; imarker of an instrument landing system.$ i. n5 K0 ^ z; } C . g5 o1 o' y0 L8 E2 n8 w! [C6 X1 [) v1 s6 x+ a1 w# {6 w1 i- l g . G1 M2 n& v0 x' }' G% id% O. S" s/ a" k9 l+ ] K9 k0 } F C . i. u# S: s7 s" O! o# e% Afo * q7 V) I! |% t9 o4 Xg% d# M0 u$ |" [: S. m3 v 指令杆,7 ^0 i+ L- `4 e 飞行指引仪俯仰或坡度的指令显示。& F4 D, I. e" m Z9 q; a2 N! c* X# D: X- E. P: V$ b通常储存 [( M6 H' A. I 的航路。. n( e1 ]7 e1 y& g: d& a; Q7 d" }+ F& o! I P* h# N4 G$ Z% N( x# b m i 经认可后在进近/ M" c, D# u. p4 X) K9 I 2.中台,3 w9 @, p; _# }* x* e) L 与仪表着陆进近系统的中指点标配套安装的罗 1 z$ ]9 h( t( c& ~盘定位台(NDB)。- x8 Z) P" e8 I4 z3 T! A4 _- z7 t9 T/ c) y5 \$ s- v: U& q& m8 s/ B- ?6 u9 A% n' M+ J4 v: q0 X8 [1 H: S! e9 Q: ^K2 q( L E& M8 Y 英汉对照民用航空词典B OEING 2 k4 t& [0 Y9 X$ x- nTECHNICAL DICTIONARY 33 1 `! M$ ~2 j% q- C" Hby / x5 C5 @6 D9 ? a$ Y! _or increasing air ) N4 B& y N& k4 _9 Uressure and temperature before the air enters the# Y& B; w f- t1 @7 `/ e ombustion chamber, Low pressure compressor - front# D) Y3 G- h; R6 v ection of compressor, High pressure compressor- rear4 k1 B# C' N3 J4 t- R OMPRESSOR STALL, An event that occurs when / T3 g0 t: Y( E& t. Bere is a complete stoppage of air or reversal of air flow- h! f. y4 V) x/ [2 O% g COMPRESSOR SURGE, SEE - COMPRESSOR& m$ X5 a! w2 l+ C. u STALL COMPUTED AIRSPEED, Indicated airspeed" M$ ~# [3 l( k# H3 f5 K/ d! w corrected for the static source error.' i+ R! U/ E; d5 b# N 的机械轴来驱 A3 C# h2 D5 H K1 k,用来增加吸进空气之压力和温度,以供燃烧室使用。 0 d0 L+ ]* o+ P$ y; u$ n9 d压压气机—压气机的前段,高压压气机—压气机的后0 V9 _8 X: z: } J, F1 b, l, b5 A2 v$ R! v/ d 气机失速,& \) d; Z- W5 I. I4 U+ L ` ] 当气流完全停止或通过压气机时气流方向逆反的一种 ! n& R9 J5 }' W! U: U压气机喘振," S& m9 j. u3 E& U, c* H& ^ 见Compressor Stall 9 ]& R) L+ m, |- \6 wCOMPRESSOR, A rotating part of an engine driven 2 o3 C1 Z- o# ]9 L2 |a mechanical shaft from the turbines f ; Y' P- B2 z6 l9 }! Op % H( T: h% }* Qc 3 @5 g1 M5 V* G, a7 ]s : i% f4 b: G2 s' g( t9 d) lsection of compressor. 1 d R% Q3 O9 O9 c' PC , e/ K) k' M7 X9 c u( S' \th5 E# q0 a/ [" X* g, h* t through the compressor. 5 Z( I3 A# U) }$ e4 Q" M压气机, 5 X5 W2 i( J3 Y% d发动机内的一个旋转部件。由与涡轮相连 3 |* _2 Y0 e4 i& N( h, ^; r; a R5 f0 A. g7 P; ~5 F) L* n# \: ?1 p' W* V- W6 P. z8 r. p+ |& R1 k+ c# ^1 w3 Q" O; o) \$ o# H/ l( m9 |1 V' b( U 现象。 / x( m+ J. p, v& c* j- V. T8 F l: Z$ F* `9 ^# o9 n& v, t/ n% p+ L2 ?1 O4 H2 I计算空速, & F0 Q- m% V% Q! i O$ p F修正了静态源误差后的指示空速。 0 @7 x; a/ R5 q英汉对照民用航空词典B OEING' G+ x2 S' V3 f: R" j4 \ TECHNICAL DICTIONARY 34

使用道具 举报

Rank: 9Rank: 9Rank: 9

8#
发表于 2008-12-24 21:39:27 |只看该作者
COMPUTER, A device that performs arithmetic + P8 _' r: P& K& Loperations, manipulates data, and makes decisions.% Z7 l! m; Z+ i! z" [ ditioning- t9 r2 D$ O6 T2 X; ]! Q the air and the& N/ ~3 ^$ N& H frigerant or moisture vapor is changed into a liquid.! G2 J! D4 P1 ~! `! V5 v- O' o) r% S ine* } h4 v6 q' E$ F, e( G ONFIGURATION, The position of flight controls,9 B0 c3 s1 S* r5 K2 Z* { missing which 6 c5 \5 \( ]) y# Y! Pmay affect the aerodynamic performance of the ( ~$ s# r: O# j; R4 X, m; pairplane. 8 L; r# @2 c: W/ b0 V& W3 L, C* _置。 . o R/ ^: |' ^( L% [& u. ?中能使热能散发到空气中,以及使冷冻剂或湿; z) |, f0 Y. G$ Q3 M2 k* }5 } 转变为液体的部件。& W4 L3 N. G% @# m: t* W% M) @ 连接到飞机结构上。 0 K1 M: ^0 l2 n态,2 L: u" u; w. m/ S* N) z 定飞行阶段中,飞行操纵面,起落架等的位置。7 E- F X+ L8 q ),& w/ @5 Y6 v7 q( k- j0 C 受到影响。 7 S+ b" o# A- |, k8 TCONDENSER, The component in an air con S$ a5 C7 y! r& q4 |3 s; g system where heat energy is given to& F9 ]# x# I! m re ' H) f4 x' z/ l+ E& ]; jCONE BOLT, A bolt in the shape of a cone for eng4 o# q. l- O, _" g attachment to the airplane structure. $ b% L" U2 A8 Y! e7 M# \6 yC0 r1 r; f8 E/ J$ P7 [ K landing gear, etc., for a particular phase of flight, e.g.,3 W5 N L4 C4 \ Takeoff Configuration, Landing Configuration, etc.( e; w& [. _4 z9 |3 s7 h CONFIGURATION DEVIATION LIST (CDL), Appendix ) T5 m2 ?7 n; c6 Cin the Airplane Flight Manual (AFM) allowing operation3 u& ]! @! r( W2 k of the airplane with certain airframe parts % r7 Z7 r' J$ R# i0 \计算机,7 g$ J7 Y8 P1 `) r/ G$ U( V 能作算数运算,数据操纵,和决策的装 " M6 q7 }7 f" \9 w$ W6 P冷凝器, # A- f3 k9 F+ o, Q: F, t( c空调系统 & r( T+ g0 A& z8 s; q+ C9 C- C, I; R1 e 锥形螺栓, b* Y' Y" C3 y, I6 _2 r5 i2 C9 @( Q 外形是锥形的螺栓,用以将发动机 2 g6 f0 T3 Z% m, g0 E8 v* V8 T! C, e" w( ~( M2 B7 e; \/ Z1 R r l3 o在某一特 ) {3 y1 R [- s1 H如起飞形态,着陆形态等。 $ x& L. r8 o, K" s缺件单(CDL ; B5 m/ K$ s( {$ M: n4 [! G; O6 g飞机飞行手册的附录所开列的飞机上某些零件的清单。 7 B! k% I+ ~4 l% P在缺少这类零件时,可以飞行但气动性能可能7 E1 A4 S; f3 h+ e$ J/ ` 英汉对照民用航空词典B OEING 5 g8 \0 K2 z+ X {$ eTECHNICAL 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 ! n5 V7 U6 J' Y- D' y" U! Rcomponent for changing variable engine gearbox speed% L* {; a- ~. D3 w2 P ONTROL AXES, The three axes of the airplane which 1 h6 |8 r8 j- g; Yre perpendicular to each other and pass through the3 T% n% y! C+ j enter of gravity of the airplane.7 }- R' j: k! G2 c1 T Pitch axis - Horizontal or lateral axis, passes through4 s! Q" J$ Z7 q& F the airplane from one side to the other - " v2 N( v# k6 z) F9 R+ ?; p& Unose up and nose down control is by 8 u& O; L+ x6 B$ Aelevators (and stabilizer for trim).9 b7 ^6 m3 L$ O- [/ D Roll axis - Longitudinal axis, passes through the D: n9 h! Y8 }airplane from front to rear - wing up and% @. u7 o4 S1 n- X0 U wing down control is by ailerons and + c0 N: F# R2 E; dflight spoilers.$ {7 H2 P* Q$ ?/ `, r* ?5 _" N2 F. e Yaw axis - Vertical axis, passes through the4 ^7 Z0 m; B, S# K0 y$ h* L airplane from top to bottom - left and 0 \1 H) W! Z, k. N8 @- G% Oright control is by rudder. R- i6 C0 Z6 n3 b! O6 ?置,5 d* U3 H+ T6 P) I: Q6 n7 S 制轴,: T! i8 n1 [0 H0 v! [* { 通过飞机重心互相垂直的三个轴。) F1 I9 ]. ] j4 Q E" v6 T 俯仰轴—又称水平轴或横轴。由飞机的一侧通向另; G9 j, w' d0 Y0 l; T 侧。飞机绕此轴转动即造成机首的俯与仰 : q+ a4 ~. h! W3 [1 \俯仰控制是由升降舵来达成的,水平安定 8 @" H8 @$ i8 c E则为配平之用。 : d; p0 c- W j+ K横滚轴—又称纵轴。由飞机的前部通向后部。机翼 ! X2 C5 D) X9 Y9 [# `# n下运动由副翼和飞行扰流板控制。 @2 x3 p& n9 W% | 偏航轴—又称垂直轴。由机身上方通向下方。飞机) ~0 u& z! Y2 A% ~* U: D 此轴转动即造成机首之左右运动,此一运 2 ~5 N+ u+ `5 y+ I6 @由方向舵控制。 & y2 z( \5 K* Pto constant speed to drive the electrical power.+ I5 M; i, s: A! j4 [6 ] C6 j: y8 q \4 p W a& U9 i; _3 d6 g: M: L9 B' H c 3 ]6 M* ~ n) w9 ? K+ M恒速驱动装 , M$ ?) |6 x# Z8 k将发动机齿轮箱的可变转速转变为恒速以驱动电源的 ( Q# E' V" P/ q+ ?液压机械式部件。 " L1 E; x2 [! L u+ Y' U2 r) D- Q, z" K |. J. g( J6 d& S3 E3 _# Z: B: H0 @6 h+ f" _; q$ F c) V$ s4 p$ U2 X) s% T7 j6 _2 _) Z( n* ?/ h0 q0 f H( n! d' ^9 R+ _/ x/ z3 o& e" Z4 P英汉对照民用航空词典B OEING 3 R, b( Q" H& W) D" y2 xTECHNICAL DICTIONARY 36 - t7 X' i8 ]- t% Z; LCONTROL COLUMN, A mechanical component used ' G1 ^; |5 z' y: brs 2 `5 Q! Z1 x) n m' U0 j* R3 \- qnd elevators. + c R0 r/ z& I# n& n/ {ONTROL SURFACE, Moveable panels on wings and' ]) |5 z; x, y- \ il for movement of airplane on pitch, roll and yaw axes. " q* O3 P5 x3 z( A, Z [6 zONTROL TAB, SEE - BALANCE TAB 5 Z0 H, Q4 `! RONTROL AREA, A controlled airspace extending / `& H( e9 t5 |; ]3 S0 {pwards from a specified limit above the earth. $ E* C4 Q) |: j6 Z: I0 gONTROL ZONE, A controlled airspace extending 2 L. l6 S. |! f6 [" S- H! Cpwards from the surface of the earth to a specified 0 v6 _5 X" e( K8 cpper limit.1 E9 q' u2 H, R4 @9 B$ | is9 ^6 K! r/ b: q- k. N o IFR flights and to VFR flights in accordance : X$ G( Z( ]9 Lwith the airspace classification. 2 m! M+ d# z/ e! P' c; H3 j/ H机械部 / @$ {& E! Z1 M0 I$ b e3 y$ I# T/ ?% ?1 ?操纵面, ; J& E4 R" ?2 M I# L机翼和机尾上的可动面板,用以操纵飞机俯仰,坡度, ; |" @5 Q! f+ T0 {和偏航运动。 9 _; J9 a& l) q操纵片, % h* J. h/ R' l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& }* [$ E8 }* j, {# j0 P1 g9 N4 g a 6 C+ H$ o1 F/ S+ CC : u/ o# G( X+ L, s- D( Cta8 B0 }4 W5 P" c0 U" F( e' M C2 O2 j9 A+ j c0 c! g- e" W C ( I; O$ H0 \+ v# R" W0 @) `u / J% S+ \* Q7 M# B! E! k- y. IC & R' F/ x' {+ ?+ H. m# M! W% z7 s+ X% C4 Qu2 f, S4 m; n$ K" h, w _ u$ |; J5 J o0 `! ^ CONTROLLED AIRSPACE, An airspace of defined # F: ^ s- r8 a( ?; l8 `! `dimensions within which air traffic control service( T& Q2 L/ _) c4 [8 Z% _ provided t, U# Q6 F. l) D% w& } 驾驶杆,7 |2 L3 ~5 ]) E/ c9 s+ J0 I' Z 飞行员用来操纵副翼、飞行扰流板和升降舵的' V' g o; _1 l+ T; H8 |0 S" L" Y9 t. \ r/ I. |" ~ r) j# p- S$ U7 o; n! S管制区域," t: X/ P5 R# L8 X) A- ~6 K 高于地面的指定极限以上的受管制的空域。* e T, ^0 _9 V% B 制范围, 3 g" u( w' r4 ] o, n5 Q由地面到指定的高度以内的受管制的空域。 , U6 G- U0 s7 j一个范围明确的空域。在该空域内,仪表飞行规则飞行7 a, @: Z; K$ T* G3 o9 |/ i) Y 和目视飞行规则飞行有空中交通管制服务。 : V7 `9 c {& Z6 s# ~$ @2 y9 e* ]9 g受管制空域, * r' ~* ?: |4 k, g: ~" K英汉对照民用航空词典B OEING 3 Z* k$ o" t* X6 s2 W1 WTECHNICAL DICTIONARY 37# S1 q; @+ F e* d6 M# S+ ` CONVERSION, To change into another form.7 {" K/ U6 l, \: q( ^0 N+ E COORDINATES, The intersection of lines of reference, : a3 A5 l7 L# q8 Qsually expressed in degrees/minutes/tenths of minutes& X [6 s! ~$ m- k: e3 s1 P- `% P f latitude and longitude, used to determine position or0 B7 f. N# u( ~* w$ ?. K1 W( ~2 w* R CO( R! x( x4 u2 P% X- `( o destruction of th) m$ _8 _$ A( f& C chemical conta 8 |: B/ b, T# W, b f# u$ B* {/ ?COWL, A remo + Z) l6 S' i% s, b5 Z, | Lfor access to th3 Q5 t$ A: N. z8 {. [6 h" j Fa. R9 H: N: `+ e Nose Cowl - Front section of the nacelle for air inlet' \. m) `. R1 N9 c' x* ]) H to the engine. ( y( E, ]" x9 v vSide Cowl - Cover around the sides of the engine. 8 c% S1 C: l7 N; OThrust Reverser Cowl - Cover around the core ( N$ {8 j/ b9 B2 H5 J; dsection." _: }9 r2 q( y Translating Cowl -The moveable outer portion of the2 W- ~, a- t+ h2 \. _ thrust reverser cowl which is$ O' n- m: W; s ] operated during reverse thrust.! ]* @9 d. u8 [) s 标, $ \5 F" w% f) G基准线的相交点。一般以经纬度的度/分/十分之一分! G' t% E* @: @. _9 j5 u 读数来确定位置和方位。 & C3 H3 C O1 l- b8 {/ ~腐蚀3 R& Z4 Q9 Z7 Z4 x L( B 动机外部可拆除的罩子。发动机上的构件必须要取下 9 W1 o) q% r& i: a流罩后,才能够到。 * q; M# _" k- N! H- p5 m1 ~+ u3 Z: u/ p% \5 n( A& R 机的短舱的前段。6 T8 R2 T! k w, h3 V; b! i 侧整流罩一发动机两侧的罩子。 4 q3 @6 Q( z5 k8 T" A5 T反推整流罩一发动机主体外的罩子。# a, @9 F4 G7 R" Q! T1 p6 p$ G- o 移动整流罩一反推整流罩外可移动的部份,在反推工4 u4 H( D0 W' s# i( b. O; @ 作时使用。 5 z4 O5 c3 u& \9 w% ku3 |- C! }1 B3 _) j, r! a6 Z- d1 P o. @- f) D4 Z: ] location.6 I5 a/ i3 @* |, P: U: x. X RROSION, A chemical action which causes gradual # _9 R" e9 N( E3 te surface of a metal by oxidation or. ~4 W) Q$ S. x mination., g8 G) e% f# y" H) y+ G( K5 c vable cover around the engine sections @+ [6 S* V" z, z* _) D& @ e components on the engine., w0 A" B: x# C1 d( s O n Cowl - Cover around the fan section. 0 [2 y: }" e _% e# y转换, 7 N/ O, S* W8 p. Q, G' L改换到另一个方式。 _ G# `8 Y3 z- G1 {* i$ }4 U: O0 ?4 F# J' h2 j& H: Y( O8 |* T7 t r2 J6 ~, n# g( B, V氧化或化学污染造成金属表面逐渐破坏的化学反应。 * e! W: l1 B* v# T! r- I& p发动机整流罩,( |* i% L% y( ?6 w! _8 H, p+ o) G3 O1 M9 s, B+ ~6 ?/ `( i) Z1 S# Z' s$ {扇整流罩一风扇外围的罩子。 0 J* k2 M, v5 q. V9 Y: C4 \4 w前整流罩一引导空气进人发动2 ?" \; u. t( i( V 英汉对照民用航空词典B OEING : ~3 B1 M; y2 w! \/ p, n$ M5 w/ @TECHNICAL DICTIONARY 38 " a v' h- |8 P1 ]8 _CPU, SEE - CENTRAL PROCESSING UNIT . X8 L9 Q6 g! OCROSS TRACK, At 90 degrees from the desired track * a4 O0 u9 F1 U& zf the airplane. For example, cross track distance is the' ?/ ~# M& A) V1 l istance from the desired track measured 90 degrees + h3 {. V( @7 C" ?4 L, R% v* rom the desired track. & _+ O6 X4 b8 Z' B1 qROSS-CHANNEL, Electrical wire(s) connected from 3 Q+ r4 m- c& X/ w. S8 Kne system to another like system, for example, FCC 0 q, S9 h% t# G' ]; g1 z. q. \" to FCC "B".3 |4 e. Z* {. x! o/ Q- k6 K) r n adjacent engine or one on the other side.9 `. N$ z- i# O7 \. w3 T3 D l crossfeed ! ~: y! B# S; `$ J4 Kanifold for fuel flow from one side of the airplane to the 5 a4 \2 @- V; g! e) Rther side. ) f4 U: t w% z& x2 Vre 4 \' `" V3 {0 n! @! t5 jRUISE ALTITUDE, An altitude or flight level - B0 I8 }# q _+ Y) J: b# q. C a; A1 |# c7 i- M' C o & D! x( l# x$ t p0 d {2 G7 b7 qd 7 _3 [% M5 S. c! {- [1 Sfr 4 G% [/ \3 i. S+ V+ K5 PC 8 J \+ ~4 U. B4 k1 oo / d2 \. A) U$ t, L- F6 {8 C"A0 h4 h, ]2 q$ f0 i* X CROSSFEED, An interconnection between fuel' Z5 O: x* G# v3 w- \& J. _: Y manifolds for fuel flow from one side of the airplane to 7 K! b6 m& G3 r7 z* v* ?: ^; o0 Ja 2 M& b y# Y0 a4 a+ C3 `CROSSFEED VALVE, A valve in the fue / ?1 T, T6 O, D- |# e6 |0 Mm; c8 x$ d. O# D6 i* ` o: P% X1 { o9 M& p$ A! Y0 }, Q. p! e: C CRT, SEE - CATHODE RAY TUBE8 T4 o8 r! q* [ CRUISE, Phase of flight where altitude and speed a# J3 t# u0 ~) D6 h! r. P basically constant.8 e' {" D$ e# i" p C 0 F8 M$ s9 a6 ?* S7 m5 o/ j4 ?maintained during enroute level flight. 5 [9 Q; C# x+ _4 k中央处理器6 d) I; M1 k" g* O2 N, ] 见Central Processing Unit. 5 i/ G L0 K2 C' S2 R6 P" n+ T交叉航迹(XTK), ' t; u9 \& J# E9 g! i5 S. |- m. p与飞机预计航迹成90°角的航迹。例如,交叉航迹距离 ; J4 M# W4 {# r5 H9 y" K5 Z是用与预计航迹成90°角量取的到预计航迹的距离。+ r3 M% f9 a+ P9 `+ x1 O" ?" t 通道跨接, " L {& d1 N% v5 Y/ r9 w电线由一个系统接到另一个类似系统。例如:由FCC - E( @* ?& D! l* Y/ [' n“A”% }+ k; z; ?# |5 w9 _8 N* E 接到FCC“B”. 3 X% J9 Z: b5 U3 c" ?" X! l; G机身另一侧的发动机。 - T' n( K; L8 o3 g( |0 U于使燃油从飞机的一侧/ a! s! h- T' p) \ 向另一侧。 $ k6 A5 z5 c- f" [. c/ t$ ?" ~' N' i见Cathode Ray Tube1 H3 @; n6 H, ? 交输, - z s- u: N p6 l燃油支管之间的交连设备。可使燃油从飞机一侧流向邻3 x/ t) T. V) ]4 K) ^/ [ 近的发动机或在8 p7 Y2 U3 x& w2 l+ H 交输活门, & H( B6 L% |# y' S$ }/ z: d9 E燃油交输支管内的一个活门。用2 {7 F: y" j% p2 O3 A: q( u. y+ ?+ A8 r6 Z, J# ]. G* B r3 D2 C阴极射线管, 4 _+ ~2 P+ s1 a3 J4 f0 D: X% f" o., E! Y# N1 d* o8 I 阶段。/ q0 U; F1 T M) S" s 航高度,( M; A$ q2 ]* c* v- u& ? 飞行期间,飞机所保持的高度或飞行高* f- G, P# h9 Z% G! ?% V9 E5 H. t1 j 巡航, $ w3 k& Q4 K& N n9 d飞机的高度和速度基本上没有什么变化的飞行 " }5 B3 l4 p9 B" d$ F. V! i1 j' y5 ~) Q 在航线上水平$ X1 m9 D0 o$ @0 u8 D 度层。 ! I9 ^8 O, e8 { l3 x, |英汉对照民用航空词典B OEING 2 e) e3 [( o4 I$ Y. R" I& d* F6 E* yTECHNICAL DICTIONARY 39 : G8 K* A: p, R* {% cCSD, SEE - CONSTANT SPEED DRIVE * N' K5 }# [: J I8 U1 eCURE, A chemical change which takes place in a resin4 d0 r1 B8 V" J( C and fiber based component causing it to solidify.) V/ J/ Z" \4 K5 ` CYCLE, A complete series of events that take place7 k! a2 b( F3 ~& N s gularly normally in a continual sequence. ; _' f8 s; o! u+ Z6 K4 y- hAMPER, A device for slowing down or limiting ) w0 _+ z* o& {: ?9 U+ u% RDASHPOT A mechanical damper for slowing down3 ]# x" _: p, p" v ovement by restricting fluid flow. % [1 _( n* Y4 g' r7 k) D' y+ tD' X0 \: v3 Q$ g+ c' W# _! F; ]+ z ATA BASE, Stored information which is used as the . \2 w5 T0 }, [3 g: eba7 M' h8 U' F8 h6 Y DATA BUS, A conductor over which digital data is . # b$ [3 b! C [! H; F8 Z1 Rtransmitted." _/ B/ U) R6 v- k; W* t0 K DECELERATION, To decrease in velocity.: P# x. s5 S: q+ ?: k. U 装置,$ h* u2 V$ k6 M/ @) _- B rive 8 a, c( r1 e( hre! r6 W% o, x5 U D! m1 m/ S6 O; z' X2 s% ? D9 Z9 E6 Y+ A* ]; Q2 e& i movement. 8 K" f P* G$ ~+ f- @m & Q6 U+ }% \# }9 @" P- xATA, Another name for information.; q& Y% E! ?* p, Y# W: A0 x6 s D & u2 h8 i. @+ R, Usis for computation. 9 K* y, G/ [3 X9 t% Z恒速驱动 # ?5 j6 a# C% p/ h: k见Constant Speed D . , ?1 h, p" u" g- ]9 W! d m期, # v3 f9 Y* W5 t/ A& I4 ^) c, k不断重复发生的事件的一个完整系列。, B& M+ e k r" l4 v 尼器,$ p, }4 ]3 T: J# G) a5 w2 J 慢的一种机构。/ \' q% i- L# ?* q8 q4 d3 X n0 a$ @: _ 用限制液体流动的方法以减慢物体运动的机械式阻' J c7 j8 ?# f' z/ A# p- L# }# b) V$ R7 }( L9 i& A, ~8 f: b9 O; `- _9 A8 a7 F+ |' W2 M# o料的另一名称。+ c/ Z* v# N% t2 I! ^ 据库, - f7 o' D f0 Y. I. o/ q数据总线, 0 e3 b8 X# E. B# _1 F! ~一条或一对导线,用来传输数字信息的通道。' V$ ]# B0 y) v4 V3 }+ R" D 减速, ' K6 a8 D. I H! b9 M速度随时间的递减量。2 Y6 d4 q6 |, s4 ~8 Y+ f P4 H v: r* U 固化,2 B! g' k# r4 @0 @, t/ N1 e+ ]6 K 树脂和纤维部件内化学反应使之成为固体的变化过程。- {% V! Q: [) O7 A# Z2 l8 E1 ~( C4 {3 y6 p# `0 _) {& X, z用来使运动减' u3 \" K$ k6 g/ t* M% S0 u 冲器,5 W8 U$ X/ K' S9 k/ y 器。 2 X2 h' v& [% J* ?3 m3 @据, ' U& X" y! U# S$ u! r! j- t) _+ k, U( p, _- o5 r9 _. \! H) p 储存起来以便在计算时使用的资料。$ b z q8 Q$ F) m( }1 G 英汉对照民用航空词典B OEING 9 U! X: |. }& e G- ~. K) wTECHNICAL DICTIONARY 407 m; J; ~9 T" h2 T, B; f DECIBEL (db), A unit of gain derived by computing the 7 q V" Y: F6 j, C9 ~ K1 x% G' Vtio of input power to output power. 6 Q2 R; ?6 O! K; a4 M6 W5 M! jECISION ALTITUDE/HEIGHT (DA/H), A specified$ s) P% J' I) Q: p7 h ltitude or height (A/H) in the precision approach at- z7 A7 H- z' Z4 [/ H hich a missed approach must be initiated if the. m- K& e. C" B8 E ECISION HEIGHT (DH) 1, With respect to the6 }% l2 z* r8 z0 u3 ]* U: z @ proach or" Q; I; D% L6 h2 P Q( u6 c execute a missed approach. 3 A* Y. i! w H" g( i- \proach to trigger the decision of either / t, E E" y& y$ ]5 _2 Hnding or go-around. * C6 m% B$ K/ x8 ?- eECOMPRESSION, The loss of internal aircraft air * F! Q4 l/ T% L, s* Z( F' O+ zressure. * }$ C% y& V3 ]3 y: _' {E-ENERGIZE, To turn off or cause to not operate. ; P; I8 L5 `& A v" xrom the tanks ' \# B6 C: |; [using airplane fuel pumps or external suction. 2 ]3 ^8 |" e2 d4 S算的一个增量单位。分贝 _3 {% O0 G" \0 s# e# Y; ^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# e. H I" m6 _ 对差别的单位,相当于两个水平的比率的常用对数的十 & X' {# ]8 m, e* V8 {4 Y断高度/高(DA/H),8 ?$ G3 q1 I4 g# Q5 m! y 在继续进近必需的目视参考没有建立的情况下开始复 , `/ E* g" n3 |1 C的精密进近中的一个指定高度或高(A/H)。/ K8 n3 Q) Z# r6 N 断高(DH)1,/ ^* _+ l" i l1 { 操纵而论,指在使用仪表着陆系统或精密着陆雷 - B. o+ X& m1 q i1 @+ `生继续着陆还是复飞决定的高。$ l" l' `8 {, J t 飞机失去内部空气压力。! I' P: i5 `' _; x% I2 ^' A 开,% g+ Y$ T: P5 z: v3 p 关断或使不工作。 ; T7 {" T/ Q3 d- n% O2 w6 w机的油泵或外部的吸油装置将燃油从燃油箱排 ' W- n/ t. f! x; P8 W9 y* a4 z9 c出的方法。3 G" z3 w3 H, o9 d: |+ K. | ra! o% i$ Q; {- b. ~ D 2 e1 L) Q* f& Da) A& ?- }8 O" R% I7 } e5 h6 o w : ?: }: L1 P* @7 U+ R$ Orequired visual reference to continue the approach has5 ^% I1 O7 ^% [5 d) q) S+ j not been established." V: G% O8 Z0 `) m% `, r D # a% D- m( f6 `% o H* toperation of aircraft, means the height at which a 9 L4 h& G, n) J& k% a$ F2 b' ]8 pdecision must be made, during an ILS or PAR% I3 k% Z$ _" l& Q1 e instrument approach, to either continue the ap 3 l2 j* P2 q1 F3 X+ S+ Oto5 \8 V' z8 ]: F4 A. x3 B* G DECISION HEIGHT (DH) 2, An altitude used during a 9 ]8 K. s8 d9 @% o. f0 ~4 tprecision ap 6 t6 T* Y6 h+ `' U# x& l, v) Tla0 M1 X+ o+ X& N, X# S( H D 0 y2 `. G" R- D2 b# O; N" {p4 P* ^4 n) f, j0 Q0 J$ ^ D4 }+ B/ j- h) b: Q DEFUEL, A method for removing fuel f; W H" Z5 }! u/ G2 G6 B7 g t; y) R 分贝, 4 H; S6 m3 j7 d$ {$ g. ]$ a以输人与输出功率的比率来推7 z0 g+ s$ J" d2 O4 m. r# c4 m5 A, N$ W: P2 }/ ?, _9 U& U+ P k; K1 t: Z9 v1 H. e8 Y1 q2 {# c$ i- t+ G- [1 h) I; b1 a0 w2 L+ u- F g0 O5 h% L+ R7 x* R# R就飞机 9 o. C1 I1 z2 a" B8 B达引导进近时,必须要作出的是继续进近,还是中断进场 " S2 j) P* l* B" a复飞决定时的高。 5 @: A! E& f* ]! a3 F; C. D7 S" W决断高(DH)2,8 l$ m% z O/ b7 g 精密进近时产- k3 Q+ a/ I N8 Q9 M. v, u 失压,# u( N9 ]. a3 @% O9 R! J5 p" _/ x+ R8 V& g& l" E排油,: c& V/ a9 K) J 用飞! Y! v+ j4 v4 T+ l$ C 英汉对照民用航空词典B OEING/ r; e: f0 n' P X+ n; z TECHNICAL DICTIONARY 41 & t, A) Q2 r" t7 V( h. |* XDEFUELING VALVE, A valve in the fuel system for 5 [5 O4 q5 _% n2 H( F4 Uefueling the tanks and for transferring fuel between the1 w5 z4 V8 y! y7 g' l. ?( q) Y E-ICING, Removing ice after it has formed on aircraft.0 o% P. b0 P4 A }* o Change or difference.7 S2 r6 w6 ]) z+ z, z* U3 \ EPARTURE CONTROL, A function of an approach) y! u: O- y/ h& t7 F2 A. G+ Z. p# t- Z ontrol facility providing air traffic control service for. X: O3 _6 I$ T$ D* `% I eparting IFR and, under certain conditions, VFR , j# e1 ?0 X5 o+ R- c9 n9 |4 ~/ ]EMODULATION, The process of retrieving information + c3 I$ H/ Q# q6 A p. gcarrier voltage., D) l1 N6 b5 t X ation.. V2 p/ V: C l4 t) u2 l, W, i lic0 @) \4 ?% C& d* s creasing hydraulic reservoir air pressure to W$ [) [ I9 N mbient pressure. ( t# }9 x' e2 I6 d' L箱排油和在燃油箱之间 # R: S ]. p$ n1 P2 _, |+ u! f, i- v7 O送燃油。4 C# x1 a9 I$ h0 v4 } 冰,. N5 e6 p' t8 t$ \/ J$ g. X' A1 M& t 除去已凝结在飞机上的冰。 # I8 D7 R4 f% s* I$ [- I删去或取消。 ; z1 }+ _. ]9 z9 x5 n量, ! D2 s9 A: _- E* X6 n变化或差异。 ' w' g" v+ Q- g场控制, : g7 B4 ~4 N% k& W! `给用仪表飞行规则离场,和在某种情况下用目视飞行 " w* K2 R/ z1 ?则离场的飞机提供空中交通管制服务的进近管制设施 , U: N2 Y1 @% M% ]6 o5 P* Q* ^% r0 K) @0 L& @& Q 调,' w; b* v9 a- O* T 电压中获得调制电压的处理过程。 ; u! R) m/ h/ U: I5 C环境: {/ Z% G6 P. g( i1 m/ \1 e: [ 力相同的活门。 3 i% K, t! W) k7 C: n( N; Jd/ ] X4 y: [) v7 F- }7 ? tanks.: j/ ]9 N: D9 {. h& l: I$ q! [ D . ~7 ^9 c" z! f2 ^DELETE, To remove or cancel. 2 N2 }" A1 j7 `5 P0 z9 N/ zDELTA, - {9 h J# A9 B/ Y. F' ^D V5 R/ M. k5 P, t8 E0 V c6 \6 ]) r6 |5 |1 G3 ]3 i. g d% E; S; g% y' L+ b0 v0 ^ aircraft.$ z1 P& b5 G8 C: z D# T; Y8 z9 W, R- X1 x* C6 Z (modulation) voltage from a modulated * v* N6 b0 p f" p9 EDEMODULATOR, A device or circuit which performs6 B% s; `* {3 L5 @2 d the process of demodul) K2 T! z5 A! s8 j3 y DEPRESSURIZATION VALVE, A valve in the hydrau3 v- Z( l5 R& O/ c7 O/ D system for de 5 `4 p: |: V6 W' K3 `* k5 G& i3 za& O; e' |' k2 R# Z) W" B$ X 排油活门,# J7 v. q& R' W* E& ~ 燃油系统中的活门。用以为燃油9 [. V' X4 i" x5 U3 k" [* j1 Y7 s+ v* S" m+ l& b+ P$ F+ X5 o$ Z+ T9 F) B7 u删除,4 W+ e$ p! p$ B$ m% T$ Z6 A0 |# L6 n) ]. J4 h& P+ a% K% ]. [: A3 f3 u& O8 D0 n% Z! o的一种功能 $ d5 G# M0 }& K e4 T# o6 ?3 i% @% s" P4 f$ p( b: y I6 B 从载波 5 H# F4 }+ h) z. I9 O. n% O# H解调器,! D, W! V/ o8 H/ ~' o0 X 完成解调过程的装置或电路。 0 W, Y5 a3 C3 x, C# T减压阀, / z M8 p" M$ j6 Q2 E( @" C在液压系统中,将液压油箱空气压力减至与周围0 {! {, b, ?) }9 G, I5 j5 r6 k 英汉对照民用航空词典B OEING ) p! \) W+ f1 U) v! O6 }/ I$ bTECHNICAL DICTIONARY 42" A& \2 Q( o) z! m DESCENT, Phase of flight where altitude is decreasing.1 ^: M' z, P8 u6 O ETAILED FLIGHT PLANNING, The calculation of fuel: Q* k6 X0 k( @3 m nd required for a trip by considering each phase of* H# c# t# K0 J, _& T$ A" ` w ight (climb, cruise, descent, reserves)." c# w* Y9 R, c al or; @- X1 c0 c! C ETENT SOLENOID, An electrical solenoid used for / ~+ E$ Z* E, b; It.* W# ~! f6 J3 { specified course or * _7 B3 h% d, B0 p( ~, Yrocedure. 1 @5 I+ ? m% i( Fe. 7 V$ }6 O o2 ^# N. V5 p飞行计划,5 o: ^7 y+ Q9 Y$ e 将航班中的每个阶段(如爬升,巡航,下降,备降)都: g, c( i+ m$ x$ @ 人考虑,来计算该航班所需要的燃油量。4 U6 v, V! v( O) g6 D& n3 B' {: k 用来感应情况之正常与否的电气装置。5 I1 J% `2 q3 U4 L. R$ y 定电磁线圈, + G+ Z1 P9 H7 {) Y出接通的电磁线圈。* d! ^% b; U" } 差, / ~9 }6 x @, R* k2 p( {与指定的航道或程序之差。! D H( v1 W' v: t J7 L 用气压或液压操作的活门机构中的柔性部件。- t8 K" T; ^) t* f5 k D* [1 B7 G s o5 _8 `7 P( g a+ G, ?, o4 g$ m' M( u9 a fl , q! N: h- g/ E3 ?+ _DETECTOR, An electrical device for sensing norm0 v }4 q2 |1 u- N" k abnormal conditions.; R( h) l. ?% w( S& N D/ Q9 F0 N! O" ^% \ controlling the engagement of the actuator outpu& N( S. d9 g# B! V/ x$ X2 e( w- @9 M DEVIATION, To change from a# F# n/ L: ]. ]! M! A$ r p3 L) r% a8 A: E0 E DIAPHRAGM, A flexible part for operating a valve ; r" f7 [' x% |# n( amechanism by pressur. B! }7 `3 f P- _7 e; Z 下降,5 O8 r/ p( b5 C& z7 ]! c 飞机高度不断降低的飞行阶段。: Y0 u. K1 ~) j5 k. E- P2 f 详细9 b1 i" H1 S% T, [$ N$ \! f: E% f$ z探测器, ( M. o4 k; U; {7 f! m& n5 [9 M& ~* N 用于控制作动器输6 j, }- G0 y( k) ?2 o$ s* f- a4 L) u# V& }: N2 |) s 隔膜,! r& J% Y) G* }- z; f- c: G, k 英汉对照民用航空词典B OEING 4 D& U" i; @7 {/ t& e, F$ |, hTECHNICAL DICTIONARY 43) K# p( M+ _2 c4 K% {4 L9 {5 T5 e DIELECTRIC, A material which does not conduct 5 N( R# k# i% t+ C" d2 ^electricity and used between the plates of a capacitor $ U1 X5 U# @4 A8 r$ ^(condenser). * y+ a5 ^) l" |3 @0 C% hnother pressure in the same system, measured in! `6 f3 o9 m. N4 w' U% S ounds per square inch differential (psid). O, q) `1 F u( m5 f9 pIFFUSER, A part of an engine between the " H. W) m# @# fompressor and combustion chamber for reducing the 2 M8 l& X/ I" _; K L6 Xair pressure. ( D! C4 C2 v1 l4 figh 9 ~ s2 y1 }$ K$ f1 W& fpulses.$ U; N% f: i, {8 y* e4 }$ P' z: J ignal that is a close approximation of the original & W9 ~- r# {9 d6 S# f# _ mignal. ' C. n5 G4 [/ z9 tIHEDRAL, The angle between the wing reference# H7 F! c% |* Z1 A7 Y# T# s/ G lane and water line." t% r# u* M5 J' [% f) I 的压力,以每平方英寸/ j% r! U$ t A: w3 N/ R 少磅压差计算(psid)。 8 n: x/ U" i }: H8 i( U散器, 7 u. @& G, ]/ u! F4 j发动机内压气机和燃烧室间的一个部件,用来降低空 1 n. Y% j/ V! q5 c1 T: t* @增高空气压力。, b# i. l. i2 m 换, $ \+ ` U; ?3 Z的连续可 ! U. n B% o; S. {(模拟)信号的处理过程。: I4 b& ~" V. M( S1 U9 W- n; }' Y 反角,* L, m5 j# c7 D 机翼基准面与水线之间的夹角。, @: U. R7 a9 U0 X( q9 l DIFFERENTIAL PRESSURE, Pressure relative to8 Q, R* |2 L0 v$ [" Z0 Y# @ a/ G [% X' a& ?* M8 f p & p4 w% |( S2 ]: X( g9 UD1 V% P5 x5 H4 I, J5 } H: B$ l c ?7 a' J8 O1 s airflow speed and increasing the; Q' ?! J: h2 D; C1 l% H DIGITAL, Digital refers to a signal whose amplitude5 G/ p, _9 Z2 n) ]: p1 A remains constant for a finite period of time. Digital1 X9 h" y$ j2 u5 Z/ k signals are commonly represented as a series of h4 B( x6 }7 V+ K' H5 V* A" a6 R and low 3 h, [- D9 r1 r& I A) O8 ADIGITAL-TO-ANALOG, The process of converting a ; Z/ g8 V8 U' {9 Adigital signal (binary) to a continuously variable (analog); J% R: p0 ?, f6 j: r s+ C5 `1 v) D" D# | s / G* S5 ^& `# C: i5 q2 U* X# Z4 xD9 a" J7 P& g# Q p ! E( N1 |/ F6 A电介质, ) e. `; |& k9 x* c$ x* ^( @: n' w一种用于电容器板之间的不导电的材料。8 V" T5 ~: I, D* [8 n 压差,- ]6 x- ?9 j$ {& Z- V 相对于同一系统内另一个压力 6 S; R; t9 A4 ?4 C4 @) R+ y- f/ n: g& s# P- b1 z4 ?: z1 H& ?- \: _6 k8 [; }! \1 _/ x, }! Q 气流速并: p8 k( f5 M6 \ B1 ] 数字式,9 Q3 t, z5 f3 }4 N 指一种信号。该信号在一定的时间内,振幅保持不变。- |6 L1 B% p8 s* H5 s 通常由一系列的高低脉冲表示。 G# D0 n# ?; ?9 A 数一模转 ; ?$ m+ R. I# T将数字信号(二进制)转换成与原信号相似8 L0 p% p& H! R* r6 H3 _( C0 _( t# M% \6 `& {0 _8 }2 p9 L9 g9 j' h/ v英汉对照民用航空词典B OEING / H3 } X% c5 \4 I8 p1 @TECHNICAL DICTIONARY 44% @: z; b; a3 s9 g2 u DILUTER DEMAND REGULATOR, A component in the( J; ^( r8 c$ D8 D% J' G crew oxygen system which mixes air and oxygen and , n. M: P8 k: K2 aupplies constant oxygen pressure even if there are " {- X) H" X% r' w4 N0 vhanges in ambient cockpit pressure.7 n7 S2 Z, g L2 g p4 ^0 k8 [% c IM, A word value of light. For light control devices - dim ) p: k: F( M! G& _9 q- W* J/ G# Athe opposite of bright., a9 q9 @' x: m IODE, A device which allows electronic current to flow0 O! ~5 A" S. A& q2 |7 g3 g! M only one direction ( M% J8 z3 Z5 N* \4 J3 U6 u' puid in a reservoir. . ~+ ^# G( d! z& E& BDIRECT, Straight line flight between two navigational! D- ]- ?7 @7 d) a6 @' X5 c: a aids, fixes, points or any combination thereof. When ( L T+ R& s. _0 uused by pilots in describing off-airway routes, points# d/ K% L) r2 l defining direct route segments become compulsory 3 i! g' W0 X% d: A6 Treporting points unless the aircraft is under radar( ?3 S( _* M0 t, W control.6 v' @' C) F, Q" h2 M$ r3 m# s- @- x 节器,; F$ B. a/ `9 y1 M0 [ 将空气和氧气混合,5 b9 `, S6 J- }4 G, r: `& Z; s 使驾驶舱环境压力改变,它也能提供恒定的氧气压力。 : B$ B+ A+ B+ U" S* {( P+ j& W& T9 l; i j; f6 j5 e 一个形容光线亮度的词。对于灯光控制装置,暗的反1 u# n" O9 _$ u 词是亮。! ]5 Z' Y. k7 e, R% Q3 M5 j 极管, , P E; M/ r1 b5 ?1 I3 g9 N X只允许电流向一个方向流动的电子装置。8 H8 L G* {$ A, W7 @1 c; @0 }. w 器内液体的量。9 C0 I5 A* i" C+ n z( d- C! b 直飞, 1 \3 C9 B1 o1 ?' F- Z; v7 o' A两个导航台,定位点,导航点,或任何的组合之间的直$ ^& l1 B1 i! F B" Q 线飞行。在被飞行员用于描述偏置航路时,除了在雷达控5 J1 F+ x+ W3 C' V& J, D 制的情况下,确定直线航段的导航点成为必报点。/ ]8 Y' p. ~ e/ n& K' u( ?8 E3 z6 \ s * I" p: {- C, b# ~- Y4 A8 Fc 1 ]/ [4 r# N H, S$ Z3 [D! t! R; e1 X% {& W is7 K: i# g" N# `. C& R D C V! @2 z+ b. l8 w0 \in O7 t. \9 h7 K d% J& P& ZDIPSTICK, A calibrated rod or stick for measuring a6 u9 Y. y* h9 E+ J+ h) _ quantity of fl/ H) J8 A, t- ?8 n5 F, z 稀释氧调6 J5 l* A b. ~+ M' ^# r 驾驶舱氧气系统中的一个部件,它 2 w3 g x2 P. f; t9 R6 u1 |* j8 @- S0 p* H$ Q" \) @ [2 [" _5 O% E4 Q' a) {- h3 B/ K6 `, w5 a6 s+ s+ V, |9 G6 h量尺,: j. z' _4 ?8 N( U* w 校准过的棒或尺,用于测定蓄液 4 p G4 H! I: W3 _; t/ U' [9 p英汉对照民用航空词典B OEING & e$ G6 Y# B/ m9 w( c' @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, 2025-10-12 07:28 , Processed in 0.053003 second(s), 10 queries .

Powered by Discuz! X2

© 2001-2011 MinHang.CC.

回顶部