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: 6811|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 ( d! c* C5 k1 P民用航空词典 6 P8 H2 p* W+ A* u. W! d2 u波音商用飞机集团 ; |: _* E' K* V$ [- [6 H3 @) q1 H! pBOEING COMMERCIAL AIRPLANE GROUP+ n+ k) n& Z. w7 u+ @0 y6 j( U/ o 英汉对照民用航空词典B OEING3 q* j% e; h# [8 }5 `( g- I+ w TECHNICAL DICTIONARY 1; s- }* x3 R) x A! J$ ]1 U6 O3 m# z6 _/ h, X& d ABEAM (ABM), Beside: An aircraft is abeam a station) @# w9 X+ b/ t7 H, O when that station is 90° to the right or left of the track of 4 v: u2 y7 n; k, o: J fthe aircraft.1 |& x0 m$ m* |) X ABSOLUTE ALTITUDE, The actual distance the aircraft . x; i! W9 b7 C0 b" d) n2 h4 X. K2 }/ xis above the ground. # r% o+ R& [7 F% _# ~ABSOLUTE PRESSURE, Pressure of a liquid or gas ! S3 g- R# c% P, g1 w1 tmeasured relative to a vacuum. 8 C/ P3 ^: W! yACARS, SEE - AIRCRAFT (OR ARINC) REPORTING ) Z- N5 s( w, I. r8 v4 I0 B2 iADDRESSING AND COMMUNICATION SYSTEM 3 u* Y$ [ R' u0 z& p IACCELERATION, The rate of change in velocity with6 x- b. m" c, p9 d/ | respect to time. 9 S$ W+ v0 M4 P! `( Z8 G' pACCESSORY GEARBOX, A part of the engine,$ b- p6 J$ P, f mechanically driven by a compressor or an angle, H4 p' O* L+ T$ {# z7 ? gearbox, for driving components necessary for engine 2 a- h0 G2 X% A8 {4 a1 G: U7 N正切,: z9 K I3 {& H3 D* A0 l# [$ h" l and airplane operations.# c$ a. r6 w- s3 K1 Y3 Q 当电台在飞机左侧或右侧方与航迹成90 度时,飞机正 2 Q( ~- z8 E, _4 W# u3 ]( |3 w切电台。* y7 _' b' Z5 x/ G/ j 绝对高度, ) J" P9 O }" j9 O; ^* g2 c5 n飞机离地面的实际距离。2 t4 j# X$ Q% F6 [3 Z* s 绝对压力, - ^0 v, T6 u- y相对于真空(无压力)测得的液体或气体的压力。 4 K% \7 e# u' o# W& F7 n飞机通信寻址和报告系统,! j8 x5 | [) h5 X+ X9 [ 见Aircraft(or ARINC)Reporting Addressing and 5 i4 N$ y; C6 k( A1 l; `* O* U! @2 HCommunication System. $ M1 Q, ~6 O, |9 c3 M7 S加速度, 4 t& B' E; D0 K2 n/ r+ N随时间变化的速度改变率。6 Y y6 D1 f0 s h3 u. ?( y9 V 附件齿轮箱,7 @% a+ ~* b9 z; } 发动机的一部份,由压气机或伞齿轮箱带动,用来驱动+ O9 X; M# m5 ~2 i# } 一些使发动机和飞机工作的部件 # `. l0 H0 ? g1 W- Z英汉对照民用航空词典B OEING$ X0 X. @ e0 R' k7 y' Z6 J TECHNICAL DICTIONARY 2 ! S' T k2 o# J1 hACCUMULATOR (NO. 1), A container with hydraulic5 V t" |9 Z8 }& g$ v ts when normal hydraulic supply is not ( R- B+ Q3 Q6 hvailable. ' I6 V7 b+ z( E( y/ rCCUMULATOR (NO. 2), In a computer, a special 8 B( Y5 t+ q. htorage register associated with the arithmetic logic unit, + D0 f0 z, C9 ?" |) D A! Y3 W! Polding the results of a computation or data 4 r( R- [/ @0 p- ?ACTUATOR, A mechanical device operated electrically,/ P# x) A# O4 c5 W# Z" ^ hydraulically, pneumatically or mechanically for + e0 A, k7 J9 _' C1 [transmitting motion between components.& N" l1 p2 C9 }5 P ADC, SEE - AIR DATA COMPUTER 4 L( J0 g! n/ v: C2 CADF, SEE - AUTOMATIC DIRECTION FINDER% B: V d! B& r! ~1 B6 b, z/ }; G _ ADI, Attitude Direction Indicator, An electronic display of ) e3 `0 O/ o" ]2 { Q+ N6 qairplane attitude information in pitch and roll. : {( x; J+ C) D% l S: O. B% b蓄压器(NO.1),( E4 H2 e2 L3 f 含有靠干燥空气或氮气增压的液压油的容器。当没有正5 \; ]5 f# u0 K" \; W 常的液压源可用时,该容器可用以驱动部件。4 P+ L+ n1 \! a+ s: I. W5 r 存储器(NO.2), , i; `7 s4 n! f$ v" ]. u计算机中,一种与算术逻辑组件有关系的特别存储寄存 4 y {% |: n# |3 l# q器,用来存放运算结果或数据传输。 + y4 O: ]- K; `5 h2 n4 c) H飞机状态监控系统, : }. }5 `/ G! ?见Aircraft Condition Monitoring System$ ~' u8 Q% @% C" J fluid pressurized by dry air or nitrogen for operation of/ T. n3 e G4 W( c1 R' f( N1 F* h componen" ~! X5 D2 _8 e7 @, | a( [# k+ o9 l% t! c/ H A P% ?/ R1 \- O& l5 g$ b' W( Gs $ |/ B2 V( l( h3 y u9 dused for h8 g* N0 ~7 }3 n. r0 Y" s, O8 Q- s transfer.1 i9 i6 i7 T% p5 ] ACMS, SEE - AIRCRAFT CONDITION MONITORING . u0 N3 m0 L LSYSTEM . , l# F) n! z" X作动筒, + L4 P3 u' M2 D' f由电,液压,气源或机械驱动的机械装置,用于传送部 7 h* j8 @+ I$ K' s5 X件之间的运动。 3 C8 L7 {( L3 y# _! |1 R大气数据计算机, 3 X) b# s2 X( W* [6 m' T+ |+ W# u见Air Data Computer.5 c. O8 E$ ^ a3 N+ F# X4 X6 E$ v 自动定向仪,. j0 }( M/ v' m7 m; S# X6 r 见Automatic Direction Finder.2 Y8 ]0 C. g8 d7 \" }$ k, J 姿态指引仪,6 @/ r0 [2 @/ M1 K5 ] f+ e 用来显示飞机的俯仰姿态和坡度的电子显示。 6 p) I, }$ g2 ^, h英汉对照民用航空词典B OEING 4 B+ T' I) u. J6 p, RTECHNICAL DICTIONARY 3 ( P1 m/ T5 `' g8 }4 cAERONAUTICAL RADIO INCORPORATED, ARINC is / g5 {4 w' s5 \6 e, ^2 @, 5 ]# d$ j1 g4 [nufacturers, and foreign flag airlines. ARINC; o4 t. ~# K/ {6 M E3 I3 y evelops and publishes standards for electronic 7 J6 q" C" ` i. L: I, Q# ?quipment and systems. 5 e3 j! Z: l* k FGILITY TUNING, The capability of the DME to/ _; b; v3 M ~7 f. j7 E lternately tune between two different DME stations in 2 \. U, x! T" {( D6 W0 p" N: C- N3 krder to get two distance readings from one' Q, X* @6 a3 N* ^ terrogator.: a" I5 _% \3 [" Q I4 @# s ge & R% Q! S: t- l: o0 \' x' `/ u: _ILERON FORCE LIMITER, An electro-mechanical , t& U! l* p4 f$ {IR CLEANER, A component in the pneumatic system' X7 D/ Z) ~8 g8 M upply to the air9 ]; P6 A9 p8 j onditioning system. # G1 N# a. l- g6 D5 N1 Q& s订并出版* U# @2 ]0 r) W/ }. x3 ]# A 子设备和系统的规范。 + j1 E; ?0 X' b: `" d& E快速调谐,; J! U. n3 k; L, v8 Q ` 机载DME通过交替调谐两部地面DME电台以测得来自 8 A, D1 \: Q' e$ J同一台询问机的两个距离数据的能力。 . o+ E: i- @' r( l9 A3 O翼操纵力限制器,9 s/ U& v7 d# ^( K: P 装置。在自动驾驶工作期间,用来限制驾驶盘% |6 r2 N6 k- K) P; f! Y- ]' R 气清洁器, 0 g' t0 t+ f1 A+ k; b5 h$ ?+ {部件。用于去除供空调系统使用的发 ; E/ S2 p7 m2 Xa corporation whose principal stockholders are United' g0 H8 N2 i( S1 m States scheduled airlines, air transport companies7 K* s2 O+ v) v- ]0 n& x+ U aircraft ma# { r: n* q3 _% t d / z9 ~% ]. S$ t! i0 {+ We9 _& u6 A2 |* X; M4 B A0 x, t' w( P8 G a( e! `& J- m. t* ?) W: f o) l1 W) W# j/ e7 z& K T5 z in2 o3 ^7 Y; r! h R" M3 `4 G. i AILERON, A hinged moveable part on the trailing ed' F! f. e ^# D, h of each wing for airplane roll (wing up and wing down) f7 h3 _ ~2 J# A1 [control.: p- y& Q- |6 C o: N A , }1 z8 ]" J! J% |device for limiting the control wheel movement by the( m2 @* X$ |1 J# s; H autopilot during autopilot operation." j" R Z( S+ y. I5 v' V A ; p- ~/ j# |+ C- g3 D2 w* |: Zfor removing dirt from the engine air s. g2 c7 O* u7 ~' W5 a X# M c 4 w% G6 T, |1 r1 ?/ x航空无线电公司,9 B1 N' s2 w% {$ f+ R 主要股东为美国定期的航空公司、航空运输公司、飞机5 \) X- y* Z$ S8 K1 D 制造厂和外国领队航空公司的组织。其目的是制6 }, |# w; \/ a. j5 S3 q9 y) ^4 |8 m+ l 副翼, 1 V; a$ I- m# J6 a铰连在每个机翼后缘的可动部件,用于控制飞机的滚转" T: _! S# B# N9 P2 C (机翼向上和向下)。 : l E! Q7 g$ S$ J4 [! X6 Y# |6 T D 一种机电" F1 t* h' E( N5 Q4 l 的动作量。 ) I, x' }# {$ A" ]$ j# `) Z+ @ B) f. H4 ?3 @% Y: E' I气源系统里的一个; w8 l6 k4 e! h+ b" G6 w0 ` 动机引气中的灰尘。 ' r# ~7 E; M8 C; V/ B; }英汉对照民用航空词典B OEING ; Q# ?& Y* w0 c, r) T& O3 N- ITECHNICAL DICTIONARY 4, L4 m9 g6 {8 c, v% ]* m AIRPORT ELEVATION/FIELD ELEVATION, The- w0 a6 w2 f3 x8 |6 G+ Q highest point of an airport's usable runways measured & ?& T: ?, d/ m1 u2 Ein feet from mean sea level. In a few countries, the& }7 t4 l* S! B8 k airport elevation is determined at the airport reference( T: H3 X$ y/ n& J4 ^8 M7 q# q- j point. 5 o+ Z3 ]& k9 J5 ?AIR ROUTE TRAFFIC CONTROL CENTER (ARTCC), - U; e8 r' @ ^7 K, p8 a. rervice * b& _0 g7 s; j1 \- Mase of: j) G1 R A) g, d& x us flow of air traffic.+ i/ x% P- P; k" D" ]: z IR CYCLE MACHINE, A compressor and turbine on a 6 v7 G5 V4 e) T: aommon shaft for cooling the air in an air conditioning 8 P) p, W& B7 J }! T1 @0 mystem. The air is cooled by expansion from high to low6 s) y2 g4 K( {' k ressure across the turbine. The compressor is driven# L0 r- S' i4 x/ y9 G; K% _ y the turbine. 6 w5 T8 k' W9 P6 k2 @中航路交通管制中心(ARTCC),- w9 d+ z. W8 [8 B6 G 域范围内使用仪表飞行规则飞行的飞机提 C1 z+ l: d9 z7 p. j管制(ATC),+ Y9 ]/ F! ~' {! M' t 涡轮冷却器, T( g" k; M7 ?是装在同一的压气机和涡轮,用于冷却空调系 , D4 w; {+ _, S, V% }2 c+ z统中的空气。气经压气机压缩后,由热交换器移去热量,& U5 W# e7 G! d1 j( _) ^) b 然后经过涡轮令涡轮带动压气机。通过涡轮之空气,温' H0 d* m7 V+ B3 V) X0 m+ J8 q7 W 度下降。 2 N6 R* g; I( f; H$ XA facility established to provide air traffic control s b$ i& {+ y% s$ {! O+ M4 ~5 h to aircraft operating on IFR flight plans within controlled4 T3 F/ K4 p' U2 _# n airspace and principally during the enroute ph- }& S4 E+ E# z% L) ?, f" a flight.1 W" o, D7 |" P% Z7 q% D7 k1 f AIR TRAFFIC CONTROL (ATC), A service operated by ( [( D) ?$ y1 `$ u. Mappropriate authority to promote the safe, orderly and; S$ O& A" e# |* j6 z+ h expeditio & e! ^& O! ^* X( KA 0 o; w I9 m0 w& q# }( Pc * F7 y, {. b- T( k9 i c: j, bs 0 J8 y* K" ]- G4 s. Hp1 d; o, S. D& f! `4 g' d b 8 J' t/ n8 V- P1 n* z机场标高, 4 U- }+ E1 m4 u" [& d, ?指海平面与机场可用跑道最高点之间的距离,单位是英% H! Y) Z$ q x% r8 G9 t2 _ 尺。有几个国家的机场标高是由机场基准点而决定的。 . h+ ?5 |" P6 h. M1 D: u c6 O4 K- M' \ o- g) S/ h 给在控制空! g2 g, x7 c( I; G 供空中交通管制服务的站台。1 {3 b% F. G# i, J# V% _ 空中交通! m$ G2 T/ H- Y9 z/ N3 `5 |# K4 j 由有关当局管理,旨在促进安全,秩序,和效率的空中 9 M+ ~0 Z/ ]# N交通服务。 ) \( i# t0 W7 c& H根转轴上/ ~ C2 ` H$ H6 D; g7 w9 H/ ^ e8 a$ I0 f4 }$ i- J: Q! ^" q; {3 `, F* U( J0 |' G+ t英汉对照民用航空词典B OEING. m) x c8 K* v1 C9 T 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 $ @) k3 V- l( d. Y: ?data information, such as altitude and airspeed, based & |0 O0 J/ N& s4 d4 E3 `on pressure and temperature measurements.* J( U4 }/ g, G& C* G) b% X2 y es air # C( I$ J: O: pIR TRAFFIC CONTROL, A system comprised of 6 S/ N% G: k1 W1 i* O7 fround and airborne components used to identify, track0 Y3 _! U6 `/ ~* ~1 U OUND SENSOR, An electrical device operated # K% t3 b. L8 o( h% m. d3 J" Ky the landing gear, which transmits on ground/in air& G* i2 x8 ]' L- e formation for system operation in flight or on the ' j6 O6 m c2 tround. , v$ }/ T7 {' R9 a3 KIRBORNE VIBRATION MONITOR, The AVM takes5 x, V% k, c3 |5 m e signal from the engine mounted accelerometer and ( s/ X/ F. K% M+ f9 {6 ?" t6 ]alculates the vibration on that engine. * f Z' l8 f+ K( A' Xcorridor equipped with radio navigation, s6 J8 {1 K0 p# ]. Z# p7 k( n aids. 9 n; G ?: G6 ]- D3 Y# [AIRCRAFT (or ARINC) COMMUNICATIONS & J# H% c! t! g" @" _5 O ZADDRESSING AND REPORTING SYSTEM, An( y% X9 k8 h! z/ O, ]" @- H7 l( ? addressable digital data link system which permits the ; d8 C" h9 l& _3 B, Texchange of data and messages between an aircraft! G) p+ Y/ z+ h and a ground-based operations center over a radio 0 u& q3 C1 m9 D% ^) u7 e3 P( \& Mnetwork. " X* u3 o' f& a+ y' x! L5 FAIRCRAFT CONDITION MONITORING SYSTEM, A ! ~* |; L/ Q/ N: q0 c, usystem of sensors and recorders to monitor various/ e2 O) d) C- z% u) ~2 O9 Q airplane systems' performance and status. " O C g2 P% n1 o机,$ L2 y8 h6 N3 N7 {5 ~% i 中交通管制,' K$ N7 _- i+ X/ }; s. V3 e$ j 一个由地面设备和机载设备组成的系统。用来对飞机进 ; V+ f; \2 B$ {5 i) G) h地传感器," R2 ? I% n8 g% Q4 ^7 o( q. o 一个由起落架操作的电气装置。用于给空中或地面的飞 ! w Q8 D0 o1 H) `( `! x( _( ~系统运作传输地面/空中信息。(有些系统只能在地面 , E+ t# V* c+ [9 o用)/ d4 V% |3 \0 r7 ?: G 载振动监测器(AVM), J r% c# \$ i) j: CAVM从装在发动机上的加速器取得信号后计算出该发 5 m& r9 g( ^3 w, C' }9 S; a& R/ B机上的振动。* ?8 N% O8 w8 n+ } z X6 W 式建立的控制区域,内有无线电导航设备。 9 a0 H- O9 U6 w飞机通讯寻址和报告系统,+ [# e7 J( V& S& t; P9 g( S 有种可寻址的数据通讯系统。利用该系统可使飞机与地+ d2 x: @: @/ Y3 ~9 p. [1 M3 a9 a 面操作中心通过无线电网络进行数据和信息的交换。2 z) t3 o" f: L5 {5 ?' b5 F3 Z 飞机状态监控系统,7 _% z6 e& X# l2 ] 一个利用传感器和记录仪对各种飞机系统的性能以及 9 g% `- r1 o/ M! ?- \5 ?! C状态进行监控的系统。) B6 t4 y0 \% C6 `( i2 [ A 7 {6 E. o2 v# z& jg' {$ E' t, h& h/ U: O and locate aircraft. 5 m% r# d" Z" `; q" f% r! h3 H3 cAIR/GR- G' D+ O0 i/ T b7 m, G. w1 ]* m4 f7 Q in5 Y' w# G0 n" v0 j* {+ e g ' P5 x" U/ u( U9 o7 K, Z' VA , S4 I y C3 y' H* c7 `0 p+ Q) a* cth ! f. l! ?/ Q% D9 ]$ V2 Yc . y0 s+ Q1 \5 Y* N$ q3 l0 CAIR WAY, A control area or portion thereof established / ?9 W b. j# h& G0 H0 jin the form of a + Q! m" J; G# z6 C* P! b( J& ?3 A大气数据计算 " o) ^) G t7 @5 X, F2 P1 a根据量取压力和温度而产生大气数据资料(高度、空速9 z: S O; M* p( i& ] 等)的计算机。 & r4 ?! I, R0 A, [' d8 g' x* [. z x4 P& k行识别,跟踪和定位。 # L0 t( p& V H" O# x2 _2 c/ h) i7 J) S @9 Q4 q7 h* K6 [+ K# ~7 y; H: z0 C3 v; M0 Z5 }8 @使 ' S& B+ s- N" N4 w! o) R9 \+ y( V! ?5 l1 Y: Z% M/ r: H# H3 ]& y" O" k8 C 航线,5 [( T) J' X1 U8 A% H# Y" j 以走廊形 $ E V( {, @4 D8 ^/ k, I英汉对照民用航空词典B OEING 2 E' u! d0 ~7 G2 `. S1 m6 F% mTECHNICAL DICTIONARY 6 + Q: e$ x7 R% m' V( fAIRFOIL, A surface designed to obtain a useful reaction, 7 x) h9 |8 b" _' p8 r3 W2 dsuch as lift, from the air through which it moves. Wings, 5 `+ V4 F5 x. H' E1 e7 Istabilizers and control surfaces are airfoils.' ^8 O3 h5 K' T% D8 G, b AIRSPEED (IDS, TDS), The speed of the airplane ; T* t; I5 ^* Crough the air.# ~" B W3 o t7 a! v" c1 ^9 e D INDEX, An adjustable pointer on the " @/ B1 X& J d3 w# oirspeed indicator.5 g3 i- s3 S9 F( s and legal ability ! r8 U+ L" O) [% U" lfly.* |, D8 ]5 }$ T7 E m, for example, the procedure for finding the 7 W: E# @, \8 }; ^quare root of a number.4 j* a0 y' `: J5 R: }* s" P y . ], a. _( y6 O1 h1 \re, wind, `1 ?; _* u' R# Gand aircraft flap setting.. _: k2 O( l- Y. N+ U9 F; u; O 是翼面。 + T+ r3 ?6 V& a速,2 I) m; w! h) J) }" d* | A5 N 飞机在空气中运动的速度。 ( l j+ f+ H- i) Y4 M) Y" U/ n. V1 l1 A: H, d7 n在空速表上可以调整的指针。" y5 s6 I$ C0 l. B0 e2 ` 机械飞行能力、和合法性的飞机状态。 & B$ j! x- T t6 Z, _一步一步的解题方法。例如,计算一个数的平方根的步 5 ~- ?4 o, g, }7 z+ W% x* Q p# v, j" c. w) P) ?5 ]- G2 b- D 资料的法定文件。9 V0 j: C4 D5 V' N$ {1 p- b 翼位置成函数关系。 2 |" E c) y5 p- g. U3 e$ O& Oth + v8 S/ I4 q% p( A$ UAIRSPEE / e- {* k0 y# V6 C( ?a3 ]( g t! h) g6 _) G AIRWORTHINESS, The condition of the aircraft with- J3 `7 [6 x: P0 f' {, T, W respect to its aerodynamic, mechanical,$ m: b, ? z8 G to4 i" T [! b& B/ Z6 ^ ALGORITHM, A step-by-step procedure for solving a , s, u3 w0 Y1 `8 U( D, R Vproble/ O0 Z& q& j6 V% A1 f/ [. e. c s * C/ w/ ]- N$ S/ m/ UAIRPLANE FLIGHT MANUAL (AFM), The legal & z7 z$ K7 b5 c7 `document containing performance and operating limits, 1 Q* {- e1 M2 o, Hoperating procedures, and takeoff and landing- F9 n1 f1 S1 ]# z. J; J* Y) w performance. / k/ A9 `% Q" e+ J6 x( W2 `AIRPORT ANALYSIS, A comprehensive set of takeoff. O" x& M U+ G6 _0 n/ ]0 c6 ~9 A weight limitations for a given airport runway, generall A Q. @, `0 i3 Y* |, V: R" ypresented as a function of airport temperatu7 E/ u& V6 g9 P 翼面, 4 r# \) s$ d$ I用以从气流中获得反作用力(如升力)的表面。机翼,* ^* e+ I, X+ h" K4 y! R 安定面和操纵面都$ T) V" C/ P" h" A) O; u+ a- A% ?: l+ q7 Q) X8 X. I2 E 空速指标 7 D$ ?" G1 |# P5 _& w2 F适航性,1 {+ j. F4 O3 K* C R6 O% \1 [: q 有关气动能力、 . y! v. Q* y. k8 b演算法, " i' T6 G7 K+ q0 P5 G2 K" b$ a$ e+ C飞机飞行手册(AFM),7 k/ x k1 }' Y" s, f! ] 包合性能极限,操作极限,操作程序,起飞和着陆性* D' [) J1 U: f, M: D* {4 ?& r j/ M 机场分析,0 |- z8 o1 ?8 K% l1 S 一套针对给定的机场跑道的详细重量限制资料。通常与 9 M* g. f$ t0 v V _0 u7 N机场温度、风、和飞机襟0 b u7 K! n; R4 j7 ` 英汉对照民用航空词典B OEING % Y: g* Q# }( WTECHNICAL DICTIONARY 7 ! ~* L8 G" D- j$ c/ rAIRSPEED BUGS, Adjustable pointers on the airspeed! f! k6 G9 z2 M; r7 ?% M% ~' r indicator.& E8 e1 W, n$ U1 t& b ALLOY, A mixture of a basic metal and small amounts, m3 V" l$ s2 w' c! B/ n$ | f other metals to change the properties of the basic/ T) Y" x1 L* y+ v+ `* N etal.; E* ?+ c0 j, g4 B Minimum airplane speed.0 D- c" A7 T- U& R l e of7 e/ ]. X$ |+ j: q8 r' ` itting airplane angle relative to 9 B0 P) o; O* C# C, W1 ?, Qirstream for the stall warning system." N9 w, `+ Y. a. l! l" K another.- h' n- _7 D0 K' ~( t. o; e LTERNATE , An additional airport selected during 4 F( P; M, [9 {" H' Q4 A& A1 q6 V4 g _1 p( W L- b合金,# Z7 H; ^8 z2 X5 L8 m7 i 在金属中加人少量其他金属,而改变其性质的一种金属! \& m( H. x7 _5 b) [+ x: i0 K 合物。 ( x- N. I: O3 ^) p飞机的最小速度。 + _- ^( {2 |5 R$ b) F. j' o: e" M速警告系统传输飞机对 ! b+ ^) j, ^# F) L$ O& {2 E流的相对角度。 1 X/ z4 Z2 I# {3 L: C由一个状况改换到另一个。5 N" ?" P. B8 e) l, R- D, I 降场,4 L. N) W* L( _+ T8 } 划时,除了目标机场之外,所选的另一个机& \* l( t) U4 s( F o# Z/ C$ M* I4 _ m# N; Z0 ?5 Y2 B9 s, | ALPHA SPEED, ' B {" J5 c7 K; e' kALPHA VANE, A small moveable airfoil on the sid . U; B8 x, E1 u+ @! gthe fuselage transm9 x- Y5 |5 A) L a $ n8 f- G) D# M. r Q, X( u6 wALTERNATE, To change from one condition to * y7 u% d& f- V4 q( k) ~0 f* QA # E- Z0 X# F t2 [8 t8 ~, ?flight planning, usually near the destination airport, to be 9 Z7 t8 z' V$ x6 h# X! Kused when it is desirable to divert from the original" X* ?# M. h4 r( L+ K% m destination airport.! @, x7 h9 R2 [1 D% j* | 空速游标 ! H/ B+ o4 |* l0 J空速表上的可调指标。 3 X/ A* t/ @/ W% j# l% n/ S6 s$ m5 F [! j6 K( |( N 迎角速度,$ i" ?8 h5 z+ z7 @( b* j2 x& N# V1 B 迎角叶片, 7 j) s/ k8 y+ f位于机身侧的可动小翼面。为失6 ?9 u+ {/ G2 H K1 l& R. i r) ]0 J: y7 a0 e. A/ O$ L4 O) O交替," V9 l2 a1 Y ^. @4 k0 c" W" b: W3 s* J2 K, p% @8 `; h 制订飞行计 4 T; C+ U; l" F1 Y$ e' B4 }' q. N场。通常在目标机场附近,以备不去目标机场时,改降之9 x; ]2 t3 }: r! k 用。+ ^: T) s- s2 }/ s h: z. z4 z2 t 英汉对照民用航空词典B OEING P$ c# i" q# y; i* K. c TECHNICAL DICTIONARY 8 0 \$ b6 M8 a. t! {: _ALTERNATE AERODROME, An aerodrome to which . D% R# j$ c9 M5 M% p4 X. Zan aircraft may proceed when it becomes either( l9 ?- o" M8 p* N1 S possible or inadvisable to proceed to or land at the" d9 u: T) T* z' n erodrome of intended landing.! Z) r8 P$ m% X" d TER SETTING, The adjustment of the altimeter! P- T( Y$ y9 W6 W3 q [ account for local variations in atmospheric pressure. - u% P1 H- L$ @. `/ K% ULTITUDE ACQUIRE, A digital flight control system7 e1 L* Z9 p% W3 s# S0 ?$ [ ode to transition from climb (or descend) to level flight.; I' ]2 u6 Y& K. u1 N9 S( ^" t LTITUDE ALERT, A flight deck alert occuring when the # l# K$ B) M0 P5 l' sirplane approaches or departs a selected altitude. @6 q& J j0 HLTITUDE CAPABILITY, The maximum altitude at : P- T# z- |5 d# D4 q3 K: |4 thich the airplane can be flown at for a given thrust,& x- I1 ] T% K/ Y& A# D peed and atmosphere condition.9 ]* T9 J1 f9 Q: a LTITUDE HOLD (ALT HOLD), A mode of the autopilot) |. w, X* K: }" ~( w r flight director to maintain a selected altitude. [2 b2 G* s" I: U6 a( ?8 v/ dirplane's altitude during VNAV operation.- q' o: ~: w8 {) c$ m 机场着陆时,可作着陆使用的! k" {4 H& y/ h- }: V" I m& w4 f 场。 , d$ j$ u! n- q0 T. o1 S6 q6 Q. V# a 根据当地大气压力变化而对高度表所做的调整。 + V2 \# M, ?/ ?6 N: E/ p9 e, a一种数字式飞行操纵系统,从爬升(或下降)改平的模 $ O' S. a5 w! O% G' J# {+ x% ]8 g4 D8 U. i度警告,- _# D5 W# z; f: g A 当飞机接近或偏离选定高度时,所出现的驾驶舱警告。 : q: L5 N$ F% x Q5 S高度能力,$ I0 O; y; _2 i0 g! D8 K+ V6 ` 在给定的推力,速度和大气状况下,飞机能飞达的最大4 S' m5 n6 s5 w ]1 c5 a 高度。 W. N) g8 U! {: z6 _' C4 q 高度保持(ALT HOLD), ( ^0 ~# @/ L, x: i8 y自动驾驶仪或飞行指引仪保持在选定高度的一种方式。 : h5 W3 T- x; b, G: j6 |6 I1 a' w3 R! t 员对飞行高度的控制。' X% t2 b2 _/ ]- ?6 l* F3 e/ w+ } im+ k1 h+ {2 L& Y/ `) h4 S3 i; Q a + U: D$ U+ w# s2 hALTIME8 C: W7 O4 \, E% i& x8 {6 L to* B+ |; W. {; u% {; a. G! K, ^( l( o A* ^: a/ g3 V* b6 F2 j3 Z m 0 r) c1 ^9 G8 C4 W& {& d1 f1 |$ bA' x# G9 a4 V* \0 Q: W, {1 ] a 7 {! G+ z, D2 Z$ q; rA) n0 u& J/ r6 l P w/ o% u, g/ Q3 ?9 l ?$ G s" I1 z X9 {' _( F5 T; u A0 e+ h9 V. a# d- ^! @: C0 J o 9 i6 a2 G u( g9 ]' U9 \8 SALTITUDE INTERVENTION, Pilot control of the # ~+ w- l( y4 K$ n* o/ U* za1 `, H( c) Y1 \! j* F% M AMBIENT, The surrounding atmosphere.# H2 r: ]9 E5 r! y& f5 u6 U( f7 X 备用机场,/ t7 v# V% {5 k" h# B1 E 当不可能或不适宜在预选 " `8 f- g/ N9 ^- q) i4 b% P* V3 H. J; q( U2 n 高度表设定 - _; K4 q0 d+ T4 _- ]: ^高度截获,6 f$ j7 `! _% T* W8 M O1 B B* o0 Y$ A$ h4 U% r1 F2 Z7 X4 ?* J2 W, k$ o' r2 a 高度干预! j+ y7 ^ \, O. q 在垂直导航工作过程中,飞行 ! e$ L n* p. u* \% X1 U+ Y2 J周围环境(地面气层), # `' z0 I8 I% E% W# V物体周围的环境(特别指大气)。 2 ]4 F6 h5 C# Z1 w8 s: q英汉对照民用航空词典B OEING" ~5 Q( t, y& C5 N% f) z TECHNICAL DICTIONARY 9 . P( g* q- T7 X2 \9 zAMBIENT PRESSURE, Pressure of air surrounding an. N; `6 c7 d+ d1 @ object, measured in pounds per square inch (psi) . 2 _+ b% R8 r% t; l% j4 ~MBIENT TEMPERATURE, Temperature of air ; s: L1 I* R& f2 C3 ompere. 3 O2 f1 [% s4 E/ E% ~urrent waveform.8 `/ c) o+ f: G8 n5 g- K- _7 Y# F g an , ~8 b0 i1 [/ knalog signal to a digital signal. " v8 H" E9 Y3 pore inputs / v: s" w' `$ | U2 x* Wf binary digital information and one output. The output( ?7 N1 r0 F0 T# N 1 only when all of the inputs are 1. The output is 0! Y% _( \ c) O: Q( e3 x4 S hen any one or more inputs are 0. 2 f" L& v+ }1 _" x+ U8 Y面气压),* R; W$ ]/ {% V1 y1 `+ _) q( g 境温度, ! m; c" e, l0 J8 Y. G气温度,用摄氏度(°C)或华氏(°F)来 . O' L( c: ^2 l) m& J4 ^, O A- z% A2 G3 @7 e2 `/ P+ a( a 电压或电流波形的幅度。7 W/ @& l7 j* V3 A3 X 性变化的信号来工作,或产生连续性变化的信号) j: Q7 u( j9 p: e) F 统。 * K8 z: l- p9 t将模拟式信号,转换成数值式。 & I. O8 ]5 ^1 j4 n一种有两个或两个以上的二进位数字信息输人,一个输3 d K' r: N w6 f4 F 的装置或电路。当所有输人为1,输出为1。当任何一个& ^- `! d2 ~' f+ N& s% v9 D- p 一个以上的输人为0时,输出为0。' j" T0 w, Q) { A + a) W2 {$ T3 _surrounding an object, measured in degrees Celsius8 m9 G8 O* D, t# z (°C)or degrees Fahrenheit (°F).+ I3 o, Q, {! B$ v3 c5 e4 q AMPERE, A unit of electrical current. One volt across+ y ~- e2 {$ }& {) Q one ohm of resistance causes current flow of one; z& _( V* {5 S a 7 `" S& O% o5 u* z* v; KAMPLITUDE, The size or magnitude of a voltage or- t6 I$ C1 X9 w9 ?3 Y c & b+ J4 f! K: b' f% x# U/ AANALOG, Quantities or representations that are8 m6 r% l: E! m8 g) u+ L% g9 |( o; E variable over a continuous range.) ~- [4 p Z8 [# h ANALOG-TO-DIGITAL, The process of convertin& Y1 F5 A. W1 Y* W- E4 H4 ] a6 Y7 a( n$ L4 x) U4 V AND GATE, A device or circuit with two or m + I( k1 y1 M/ s' c2 _# K, Yo + u2 ?; s- J$ a. }" b1 b; qis" a0 \& r% R* S7 L$ Y w1 v, }' N! G. y/ d1 G 环境压力(地& g; `9 V& M0 k1 d3 B* J1 E 物体周围的空气压力,用每平方英寸多少磅(psi)来, h/ R4 I, r V" X% e: q, d" ]( k 度量。- F8 j0 Y5 [9 X8 u" e1 z1 w5 j1 S4 a6 T7 U5 n 物体周围的空 9 |) y2 m2 t3 b6 B度量。2 ^/ D: l) @" s9 l. u1 U: i 安培, 4 f. \* I! j. A& T7 H9 }' m5 ^( K电流的单位。 : k0 I& \6 O6 h! F1伏电压在1欧姆的电阻上所产生的电流为 8 _. `" T5 f; }3 P' T1 V* X: ^1 ]/ r1安培& e& S! F) O5 y) I7 F2 L& J! _0 D 振幅,. g( \/ o, H7 q* h4 T. J 模拟式, 0 N6 \9 ]/ f9 l+ n U5 B+ `用连续 5 c3 ?! m6 f0 |; H. ]4 E. _ ?+ i# L1 o( } 从模拟式到数字式,& _9 m7 C! e$ z 与门, $ {' p0 t" p# C! y8 J' ~ o- P) X" w0 z) d+ a+ z; O/ g( z, W1 r: v: p2 R1 _ 英汉对照民用航空词典B OEING" o- A" Y' r) T/ g$ d w! V# ? TECHNICAL DICTIONARY 10# I! e# X- I4 K; t( W6 H ANEROID, A sealed flexible device containing air at low" h8 q6 u$ s' d7 i7 R* J pressure, which expands or contracts during change of& Z0 Y6 u/ @5 ~; U# Z3 r ressure outside the device.2 i4 m! E' k1 D) M, N ically $ H7 @! F; A$ q: pr changing the direction8 O! a6 v f6 N2 O B f drive.- j: \, X, c% ?* \ of the wing chord in" h V U# ?& ~2 ~3 T) q3 s lation to the free stream airflow as it moves forward3 B+ s* ]7 o& }" B; D6 p# Q# L rough the air. - y' N6 O2 O1 `al axis of the9 T$ k& {# f* E1 Z' g6 ~' o aircraft.9 Q$ `# T$ |1 N0 k5 e 胀或收缩。 . _/ i0 C6 C) Y* S6 J箱。是改变驱动方向的机械装置。8 F& `8 R, M! d 机翼翼弦在空气中向前运动时与自由气流之间的夹角。, o% K3 B0 v* e; m4 F4 e1 V/ l( i, r5 ^/ A& D3 `: Jp, l8 {+ E# L* n2 K ANGLE GEARBOX, A part of an engine, mechan + m7 X) |' x9 ldriven by the compressor, which drives the accessory! o9 A! y7 G3 X+ W6 z gearbox. A mechanical device fo o; ]' z/ o ^7 P7 h1 J$ Y) e, Go' w4 q. d1 A( t ANGLE OF ATTACK, The angle. p) }$ o: t+ O4 S re7 @; P+ q5 r+ G+ i1 x- n th) Z; d, b' t# {; S f2 V ANGLE OF INCIDENCE, The acute angle which the3 G4 X2 n+ |) ?. ~) Y% U! `+ |( C! Z wing chord makes with the longitudin) L K5 x8 c w' y; X: @/ R! ~ 膜盒,, H. ` {, L' y- d ^1 Y 内含低压空气的密封弹性装置。当它周围的压力变化' V: `3 t, f; s4 \ 时,会膨 j* ?: l# @: i% X$ t% c 伞齿轮箱, * B4 s- \/ e" e% I/ q/ Z发动机的一部分。被压气机以机械方式驱动,然后驱动 # a/ s5 u, N- O! b附件齿轮 6 z! i5 T3 i6 {: M2 B迎角,, ?- a% {3 z$ j' y+ l# }3 g9 ] 安装角, 6 B" S2 l `: V, {飞机的纵轴与机翼弦线所形成的锐角6 |2 T7 B) c) U& L9 B; g 英汉对照民用航空词典B OEING! I h9 i- ^8 ~7 E" c TECHNICAL DICTIONARY 11 ! `9 Q" T, s& D6 X8 `1 M# o7 H- B9 E/ n$ ^ANNUNCIATIONS, Audio or visual indications used to/ ~ y t* @ K6 N call attention to an event that has taken place.$ C, i6 g9 Z& h" O0 ?! ` ANNUNCIATOR, A visual device consisting of a number 1 \7 z% l' ^1 v2 R# e) Wly. : z0 I- U9 W6 } ~ANODE, The element toward which the principal stream , }% S7 N! l, Q- e8 z. jof electrons flows.: d7 N2 k- j8 D0 L" i5 O ANOMALY, Not normal. 8 b. C) s; y% q, EANTENNA, A device which, used in conjunction with a % `9 d$ Z- g9 _8 Q$ N& Atransmitter or receiver, is used for radiating or receiving* I; S1 ]# r, T4 \% D radio waves. * q6 G1 @2 r( I; e& \5 ~. @NTI-ICING, A method of preventing ice formation on' _9 {" }& n- o/ q4 ? e wing leading edges and engine nacelles.3 P0 N+ g5 w1 o% @) G5 {0 Y3 ^; p- W NTI-SKID, A system for providing maximum braking. }( t' A$ q& \" i) G7 K% _ ithout skidding for any runway condition. Anti-skid8 R( X; g, ?- }9 p- Y+ ^) ^* n omponents are part of the brake system. 5 h3 K! U& x+ s) ^告, & H1 x9 f6 z( C: e9 \当发生事件时,以声音或目视指示形成的提示信号。; u1 Z( `' a N# E$ }4 ? 与之有关的电路的现有情况或已存在的 7 B* d8 r9 o d8 r1 p" e2 E5 u. I! n% L- X( `( A- x 正极,+ b. g D4 J+ L9 ]. @$ D6 } d 主电子流向的极位。. ` l+ Z0 x1 _" G 异常, & k! I: Z3 { E" d% h: j- `不正常。 / ?, Z) e3 ]7 M! i- I: W天线, " G1 u! P7 y) S; N4 T一种与发射机或接收机共同工作来发射或接收无线电 * X2 |* o' M( Y) J% I' Q波的装置。 % S" A8 H3 s' c2 v) a L3 x冰,+ ~/ K+ `7 m- b( n/ A. ~ 防滑系统,( h5 F$ [# B8 R 一种在任何跑道状况下,都能提供最大的刹车能力而不" Q1 H; d' `9 u2 b! W 使轮胎打滑的系统。防滑部件是刹车系统的一部分。5 {" h/ t: k, ^8 \# k8 A3 i' M of lights. Each light indicates the condition which exists$ \2 I6 ^! B: D or has existed in an associated circuit and is labeled: j+ T) s/ v" p) } G according! t' k0 C* |% _. J' z' }) O A& d' D1 R: Q9 I th. G* c% }" Y- D A ! G: N- p# {0 Q/ q. W, c6 ~( nw/ x' P1 W0 @- i0 y c 6 a i/ q) w3 D6 y6 l1 i8 s% k: b8 b: n 信号牌, # P n1 l) F; y" s! ~0 ]. d% Z, [由一系列指示灯组成的目视装置。每个指示灯都有相应+ K) d; y& V6 F7 e* F: Q 的标记,用来显示 ! \. h( I8 _% k. L7 n$ n' K7 B$ @2 m7 X$ }8 a( S) ]: f, B! I0 M$ h9 y: T& I, m: w* z防止机翼前沿和发动机短舱结冰的一种方法。9 O: I" `* x* W* Z6 o6 }& x' c( H 英汉对照民用航空词典B OEING H) k# [" z! r1 E2 j1 ^TECHNICAL DICTIONARY 12 / ?5 E) t7 w( D- SAPPENDIX, A supplement to the Airplane Flight Manual 2 k) w3 w0 M; x# W. f2 y5 F- ttained in the basic manual. A ! A: p' s8 r4 sollection of supplementary material at the end of a! p2 @) J2 r. I% T* } ook. 2 f5 D* }/ r3 ~of the' \* A# O7 t! n( j) I# v+ ?7 E* ^0 r rsion link on the landing gear.( g- E! K2 U0 j! j APPROACH MODE, An autopilot/flight director mode - [- e- M4 R4 r* F5 l) L( Dwhich is a combination of localizer for roll control and 2 [) O. c, ^( G5 e3 F/ ^+ j/ Dglide slope for pitch control. This mode is used when full/ b9 W0 ]0 B3 o' w, [ instrument landing system is available.1 ~' T9 S/ u/ ]( D) X! P. o6 w: [$ i APU, SEE - AUXILIARY POWER UNIT 5 `+ f3 `' z i% T* Z- d. PARINC, SEE - AERONAUTICAL RADIO# ~/ _5 _4 l& r- z# ]' G INCORPORATED : T$ ^+ }: r% P4 ?' B, `ARM, To make ready for operation. ( e. B5 ~3 N3 `, ^, r1 B+ i附录, 3 m8 K9 X8 T2 a% _# P- g飞机飞行手册的附件,包含基本手册中未提到的飞机形( W' F' h N! U% B# f9 D 态的其他性能。是附在手册末的补充材料。% \* ~" h/ m- x* c5 U 顶销,- q( f/ G- |0 |+ |. ]8 ` 用于连接起落架扭力臂两部份的销子。 ; b! R9 ?, w4 G8 W0 Z, i进近方式, ( s" {0 T* N+ p. u一种综合了控制横侧的航道信号和控制俯仰下滑信号9 Y# A& z" ~# {6 _+ {& B 的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系 / e3 P* P. w$ O统正常时才使用。; R1 J1 y, X! b: q7 s1 } 辅助动力装置, . z' y( g" S/ T见Auxiliary Power Unit$ j* F; f5 H& J" k containing additional performance for aircraft( \; c$ ^+ J7 K configurations not con 0 [2 _2 ^2 Q7 x5 _! I. \' ?4 I9 Q% D9 Lc & |; s- G4 \! U& M3 i9 |b D9 o/ Y) ?: sAPEX PIN, A pin for joining the two sections % D1 e) P; O6 v2 D' xto/ \8 i! J: Y: t9 w8 k9 @8 a4 m4 i8 Q1 P2 W/ e( V/ I 航空无线电公司, : P* _6 B. j) W; b见Aeronautical Radio Incorporated. : z# a, c7 ~, v2 C! Z2 z预位, 4 u9 _8 X C! [& y部件可以开始工作的状态。 O+ o( O# _6 ?/ E7 h, c* K英汉对照民用航空词典B OEING " i, e0 C l; W; p2 f0 }! \TECHNICAL DICTIONARY 13# V( ~! J' M" ]3 c/ O ARC, The curved track over the ground of an aircraft: U; X/ m) L" B$ d3 m) Y flying at a constant distance from a measuring % d4 o* D2 C8 L, V! ^# u# V: Jequipment (DME). - G4 h0 y7 N R6 X2 P1 sin the limits of self-contained system ; [$ b2 i) e/ |: Aapability. 0 i# g* W' j, {2 j. a. _ Btem for opposing or restricting* ^5 `6 e" T, p! m8 i ovement. ' m3 [7 j+ @3 f3 L5 eSPIRATED TAT PROBE, A sensor that measures total( C$ M# |& q. H6 Z ir temperature when the airplane is in the air and that 5 O9 F) e3 g7 A+ F; Feasures outside air temperature when the airplane is ) `+ s2 P1 m6 O5 S3 Z7 bn the ground. The outside air temperature is measured% x G+ U$ m S7 C SSEMBLY, The fitting together of a complete structure 4 ?/ B7 f# _1 ~* L' Z0 c% sSSUMED TEMPERATURE REDUCED THRUST, The) }( |, u) t8 G2 l `* y$ T) Y0 u ATC, SEE - AIR TRAFFIC CONTROL: B; n) {+ J8 \8 ~( v7 u& c9 F+ k# n# U( |/ h" Z. e8 f q系统中所产生的一种用以抗拒6 `* K o* b, j, g/ s8 v' r1 q 作或限制动作的力。+ }3 s4 ^, J2 r' q. L 头,; j/ Q+ b I& w% Y! r1 l& h 用来测量飞机在空中时的总大气温度和在地面时的外 + W% G1 |7 R5 D# V温度。地面外界温度的测量是利用引气将外界空气吸入6 Q; `# u& Y$ ?( @ 头,以达到测量的目的。 & E" e% { D+ O; _2 t0 p& g配, Y2 A E; N1 z/ p 一个完整的结构或组件的过程。; r0 `% C& |! R9 G 假设温度而得的减推力,- K& p9 ^/ @9 k/ w 推力设定值时,假定一个比实际外界空气温( o: ?, I- _5 l/ {6 s7 g" X$ y3 W 空中交通管制, % F! [! a2 J( k4 p* J9 t$ p见Air Traffic Control 3 ]5 u2 e2 E6 ?4 x1 @2 dAREA NAVIGATION/RNAV, A method of navigation % s; N, [* t! p# Athat permits aircraft operations on any desired course" [% N1 L1 s2 |' V- D7 {) I within the coverage of station-referenced navigation5 F* ]4 Y9 w0 ]7 @) D8 ~( _' u signals or with7 m6 {/ t" N: Z, V9 g2 Q( B c& ~8 }. T' f% H1 m ARTIFICIAL FEEL, A force developed in the flight0 v8 \2 x8 G2 [0 e control or brake sys k: K4 q1 x' q5 T0 o8 b m 9 G S1 Y8 ~# c- {/ V/ pA , f3 v$ A O. Ba / q3 C$ @/ U8 V9 Z$ ]m8 W3 u4 X( C7 v' c( ^ o8 y& `( [- v- V0 J) D C by using bleed air to draw ambient air through the) H4 ~2 n- O6 Q sensor when the airplane is not moving. - \) n1 H" [& L9 h- A2 @A% M0 k3 P0 v* H" O p+ }: W' I7 \ or unit. * ]3 A2 I% ~' d& E9 m" b4 oA . {- k! f2 E6 o# {lower thrust obtained by setting a higher than actual( C2 ?$ E+ `9 j& p; a Outside Air Temperature (OAT). $ a; u) m' M N弧线, + ~5 \8 w; O! K飞机在围绕DME台等距飞行时的弧形航迹。 j$ I h! |% _) _. q. n U 区域导航, 6 z. B' U8 `, @9 t! z' ~9 o容许飞机飞行在有电台参考的导航信号或自备系统能 6 a8 \8 x. [+ U力极限范围内,飞行任何预定航线的一种导航方法。 9 u; ^3 R: h. y( G模拟感觉 ! I9 \ I- I) f7 j. b在飞行操纵系统或刹车1 w+ B: @$ c2 E: ^6 }, {( b5 o# W& H4 E# F1 \7 P吸气式总温探6 U1 S" d! {: S1 f: k. v( F. @7 a" p, i7 v8 C9 \: ]3 X# h- q. d r' N; I5 q! n! e. }% M7 L8 z4 m( i 组合成; c$ \4 ? _8 j4 n) a' S6 c. p* V: E- @. F2 q 在选择起飞 ' m3 X% U; m! z0 S/ ]度高的温度而得到的推力。用这种方法可以减少发动机的5 E* g& K' N( ^0 C0 }1 z3 M$ T6 x5 | 磨损和维护费用。' k! _; ]2 Y9 x) \# V! Z' {# x) s$ I7 v" e- s& x5 p' }- B英汉对照民用航空词典B OEING# r% X/ Z0 {4 v' A TECHNICAL DICTIONARY 14 $ J/ V5 M$ Q1 ^ATE, SEE - AUTOMATIC TEST EQUIPMENT 2 D' x" v2 w8 k, |% B5 ^+ dATMOSPHERIC PRESSURE, Pressure of air due to the % W. l! Q5 o9 t9 D! n6 oarth's atmosphere, expressed in pounds per square 1 B9 d. n7 T. i2 @4 F& R# B, n2 q" wch (psi) or inches of mercury (in Hg) or millibars (mB).1 l- ^9 \: x7 G# R' L. k" E% X7 n TTITUDE, The relative orientation of the airplane with N# ^, @2 p7 y) a# T. m spect to pitch, roll, and yaw. ' U1 k m. A* l8 J: r+ K4 WUDIO CONTROUSELECTOR PANEL, The panel in - b. z @! R# }# [& P& re airplane which controls and selects the routing of: X) ~4 b# p1 w( `* O udio. ( W8 F0 a/ n7 I7 k* O/ ?UTOLAND, Automatic landing using the Digital Flight. r. e+ J6 ] C/ ^) u& w7 Z% q ontrol System., ]! g: C3 ~, r9 z/ f) J" {$ g7 y0 i n.1 V) H& I" m1 ^- B M, A system / R5 s* l, M$ S4 R) qomposed of all necessary subsystems needed to guide % u7 _ p r9 Q5 d1 U8 |e flight of an airplane. ) f4 s& B% |0 a1 P" o4 ^& lEQUIPMENT, System test! o. l9 K8 C$ Q- ] quipment that operates under computer control. ) t7 r8 h2 f9 K* h/ k1 R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, a& d& q6 \, x$ g" d in # C7 J$ r Y( uA , y1 W& m/ P. H0 R- f2 v5 B: B$ ~re7 l5 M. N/ Q: }1 A; D A ( {( q ~% E( [: _th " C7 Z n# w+ U p3 \a ! j! O0 e3 N& s6 V$ z: t6 c8 NA( b* g+ [/ G2 g1 k4 F C% r K( A) r4 G9 b AUTOMATIC DIRECTION FINDER, A system which) ?. W3 m' }6 c( `0 A determines the direction of a radio statio/ Y) S0 d9 |/ ], j+ r d AUTOMATIC FLIGHT CONTROL SYSTE3 B$ S. a& K H* \/ ]0 {+ |0 H, A c ) M6 D) A- e, `6 bth2 E3 Z( L# j( z2 Y6 F# a AUTOMATIC TEST % N/ d( t7 d0 [" o7 C: [1 _e : L8 n% G3 T9 E1 M$ y6 R) w自动测试 4 z) h; B8 D$ Y见Automatic Test Equipment.2 A7 m9 L* y: }; m( G3 Z; U 大气压力, ) C3 f2 X. W# j8 A0 C: R由于地球周围的大气而产生的空气压力,以每平方寸多* h& ~" W9 u! `$ M 磅(psi)或多少寸高水银柱(in Hg)或毫巴(mB)来" w# T8 j! O* \ 示。 t C3 I5 v. O- H S+ ?) ? 飞机姿态,0 }% Y! }6 k. E B$ H 飞机与俯仰,坡度,和偏航有关的相对方向。 0 T+ n* y. P& o5 V: d# q音频选择面板, 1 E5 W- y2 p6 u: d, r" Y/ H/ t$ ?5 Q: z飞机内用来控制和选择音频通路的面板。5 B" ?* ? D9 X2 ] 自动着陆, . P: S$ I4 t( ` E; w使用数字式飞行操作系统来进行自动着陆。 8 u" H+ K7 [; H% S的系统。 * Z/ ^$ D4 }+ d" h. ^3 g) [/ T. O) H0 I3 ^( _4 [# ^2 L 系统所组成的一个系统。 & F8 n5 e8 f- b3 {: P9 {* F- Q在计算机控制下运作的系统测试装置。 3 D# W4 L$ R* z& F) F/ I8 f& m) c& e3 ?# o( u& K" u2 L4 K2 \自动定向仪(ADF), / n7 H( g5 N I1 e2 E确定无线电台方向' ^* g! r8 R s% M 自动飞行控制系统 3 I' Y8 X8 C8 z3 z6 ~' v0 W由所有能引导飞机飞行的子 / ~! m& N: R1 ^4 K! Y自动测试装置,' p: }9 [8 O; b( N0 X' H 英汉对照民用航空词典B OEING , k7 y3 O9 `4 t- e, l% N5 }, QTECHNICAL DICTIONARY 15 I! o3 j- y, {+ EAUTOPILOT, A system which automatically controls2 x0 R" y F5 A& q( w# e% z0 J and guides the flight of an airplane. + a; U+ w# B5 u- s- DAUTOPILOT FLIGHT DIRECTOR SYSTEM, An4 y$ N7 j1 J* I3 c9 q$ X% \; w W tor , C: z; M7 s$ i% ^' `% UUTOTHROTTLE, A system which automatically- M1 I8 u# I( Q ontrols the throttles of an airplane., |3 ]( R7 M% M! g! r& C POWER UNIT, A small turbine engine in+ \* O; d$ h5 L/ x% q3 c e airplane for supplying electrical and pneumatic& c* k9 N, t9 k" V6 ?) x- q( a ower for systems operation on the ground or in flight. |8 R W& R( u. y/ c% ?9 ]- \' |2 _7 wVM, SEE - AIRBORNE VIBRATION MONITOR, i7 ?0 F: {, {& } W: g a, o XIAL FLOW COMPRESSOR, A type of compressor + e2 g- s/ J, k' \8 W, a+ ^5 s; qsed in a gas turbine engine in which air passes through + q( M# n! ]2 }# E( T# q4 aXIS, An imaginary straight line or an actual physical; P9 C. k: r! c- V7 s omponent (such as an axle) around which a body can9 |3 R+ @- @& O% E5 j, A tate. q; e$ v* r3 E' D, E. i# u仪, % n3 P& ^4 b9 ~3 E; E7 ^' y5 s+ U7 K: j2 f3 N8 U5 ? {自动驾驶飞行指引系统,9 P: \) ^5 Y$ A/ u- U 动驾驶和飞行指引功能的系统。 3 K5 q6 Q9 g+ X, O2 L% a0 X5 l动油门, 2 V; x. ~8 h( T: n2 t自动控制飞机油门的系统。 9 J+ s, [3 n% G u是飞机内的小涡轮发动机,在地面或空中给各系统提供 ) d- H Q" W+ I( b; G* d& {源和气源。6 W3 }6 L- B8 p4 C* p! d 称。 # `8 r! W$ P& y D0 ]& n& Z载振动监视器, ! h& z" o# `6 w4 O; I& q e$ S/ M2 }见Airborne Vibration Monitor. M1 I0 [2 t" [ integrated system containing autopilot and flight direc! u$ V* D# E# {$ I functions.) B/ E, ]5 G1 z. I3 U5 o. W A4 @! k, [% Z5 X- R$ n8 @* J- F c4 v% y8 I {4 {& x AUXILIARY 3 ?/ Q# [2 y/ lth, _# H% a# ^- O p 1 D; o& t% z2 X1 u( L* w5 QAVIONICS, An acronym designating the field of aviation9 x/ H& p" N% e# ^# Z1 W W2 ? electronics. # A; h% d% e( P1 `A 0 G9 W: o% _$ ^7 B" O0 c/ fA / Q) ]6 i {9 Bu b# ]) O2 s. D% Y5 E- Q the compressor in a straight flow, front to rear. ' A+ D A3 C) y( C4 {2 u7 q0 B( v0 f) EA! W2 M. S5 `' L) v3 p c 3 _/ o$ @; |. dro ! v) H$ j- T6 p自动驾驶! G, r) K+ m1 U5 | 动操纵和引导飞机飞行的系统。7 X0 _2 N7 E9 Q4 h 一个综合自 * q. h# Y7 x( B. K+ d/ @* i- n% H5 F. y- O: x/ M' E辅助动力装置,8 m$ d& t/ _8 q Y1 W! K! V% ]- J! v) ~- G, ?9 e 航空电子学, ) J+ J8 s O o$ o. @+ |4 n+ H5 W是航空电子领域的一特有名6 ^% `% b4 D! a) a! q3 M3 f# F+ i, ?1 F# e* D5 u8 y! R2 H" Q! |1 Q9 K6 ?7 h# c. ?2 B 流压缩机,: D4 A- X; D1 K, h" o/ Z6 u5 z 一种用于燃气涡轮发动机内的压气机。空气由发动机的 6 N" U! K$ w2 }( [* n1 ~部流出。9 `- F/ {. p' Q( ]/ P9 |' u9 R+ Y& W 线, 7 p) a0 C9 i7 |, U7 O4 O4 j( S可让物体围绕着作旋转运动的一个想像的直线或实际 , P# R3 e$ D! w. R) B+ P0 G Z在的部件(如轴)。 $ V; d+ B% o# Y9 c* S: |" ?' b e* i4 u. C+ H" W! O 前部轴向流人,压缩后,由后6 i5 y0 b q( c5 i: I; q( k5 A2 s& G# h( b5 o4 ^( B2 F+ U! S+ p英汉对照民用航空词典B OEING! ?# h/ j" F) G& O/ h( a- o TECHNICAL DICTIONARY 16& B9 O/ C9 v' Y" x: D9 u8 ~% b B + Q+ p* E- N# ?7 OACKCOURSE APPROACH, An approach to a runway 5 f p0 U( b9 |" c+ mversed. . t. ]6 H* ^) o; f) A d& jown on the EFIS that; R, v3 {: ~" j$ F- J( B* r oes not readily change, for example, navigational aids. 0 u! t) b6 J+ Y Wvement in the tank or reservoir. , M6 q9 D& t% X# V( z1 }6 ^ALANCE TAB, A small hinged moveable part on the2 m+ N) b% a5 J2 X" a: ^ ailing edge of a control surface (aileron, elevator,, v, M" [9 |5 }6 G/ X 航道进近, % `3 Y( p6 K! U0 y4 g相反的进近方向。当反航道进近时,无下滑 7 H" R. |# k! \* t" i显示在电子飞行仪表系统上不经常改变的数据。例如: 8 q) ]9 F" d$ d1 T6 h. ^航设备。 ( u( ^; v+ r) i在燃油箱或滑油箱内阻止液体流动的隔板。 * G) g3 W6 M$ |! m动补偿片,* ]7 w9 }% A+ y' {0 f* J. d. ?0 K 铰接在操纵面后缘(副翼,方向舵,升降舵)的可动部。3 n6 W! ~8 L$ ~1 ]; s& D$ ` s 与操纵面相反,以帮助操纵面运+ t! b( O: ]7 d* e B ) ^/ C2 ]8 w h! }6 p- i" G7 fwhich is opposite the normal approach. For a 3 j1 v! U4 q4 A: @backcourse approach, glide slope signals are not4 d& p7 A/ r( u' z; G0 v; c! q7 O available and the sense of localizer signals must be $ t# l! O- N4 P& kre( l4 C% {( `2 X3 t: d3 M5 i, x) q BACKGROUND DATA, Data sh8 k9 z U4 i+ {8 @5 R d ! ]3 p5 S& w g. a+ V* LBAFFLE, A partition in a tank or reservoir to prevent , C8 ~2 k; `! ~) d7 Qfluid mo" ?* ]- h6 V$ M. | B ' U/ P) @, z& Ftr. `2 }, V* {7 S+ T, p rudder).The tab moves in an opposite direction to the - J7 y# r5 c$ V0 z3 D3 ccontrol surface for assisting movement of the control# \- ` o, W# b/ w8 u surface.5 ]2 d# G- e5 k2 E( n3 A; \% g- F( }4 P: K. v5 f 与正常进近* V9 A6 w7 ?, i7 n4 Z 道信号并且航道信号也必须逆反。 8 H8 S* B: T8 m2 ^ z5 d9 s) a背景数据, ! p6 V7 x5 D) |4 l5 b% M* W7 P- ?. g- V% D w! p5 V/ f 缓冲隔板,% e' F/ C' v4 u- K8 y; M! k. Q, j4 p! S9 Z/ }0 h7 O e9 N8 @ 随动补偿片的动作方向 [5 S; P( f4 |6 S9 r6 e动,减小操纵力。# B! E' u) T* ]1 t# p- A8 \3 R" m 英汉对照民用航空词典B OEING6 p8 W2 ]' ~( L% \ TECHNICAL DICTIONARY 17 ' B- X# J) M) J8 nBALANCED FIELD LENGTH, The field length( c* ?# c! `7 q associated with optimum aircraft performance when; A# F* [6 L% ~9 g% ^1 H- J bstacles are not a constraint. In this case, after engine * T4 ^ b1 ?+ f$ [% O( @7 x- Silure at V1, the distance required to accelerate, takeoff/ z' |" D1 _( D( c9 Q |7 ` nd reach a height of 35 feet is equal to the distance( ?4 `4 z2 d( v! ? ALLAST, A weight installed in an aircraft to maintain 2 w5 `, ?$ c; O+ ?ALL NUT, A fixed spherical nut driven by the 1 c+ |; ]. K- g/ S( V+ x: S. tAR OUT OF VIEW, A signal used to remove the flight * R. Z+ Q: L7 `: p V; C6 hAROMETRIC PRESSURE, The pressure of air above1 X1 i, C: H" H! P9 [9 m! s. S g) or! d" c' a' q; A( f G- D millibars (MB). ) i& E) Z# b, s6 ~+ V8 h5 n2 c& \ATTERY, An electrical device for changing stored 8 r; V2 F. w0 t/ A' D性能的场长。在此7 t% s: g# I& d0 u# E) n 况下,V1时发动机故障,要完成加速、起飞、离地35 # e" \0 s- o$ q! m( M尺所需距离等于相同速度下完成全停所需的距离。 \4 e" P: u8 A( O7 ~1 }. M' X6 D: [) \舱物, * h2 E; A" }: W+ z重心在许可范围内面装载的配重物。/ K) }) F ?: c9 Q _, } 形螺母, - i# x3 ?" h' D7 {6 T的固定的球形螺母,用以使襟翼和水平 1 I* u5 F4 j7 z" I* W引杆消失,6 V1 B- b% r L6 H9 m w" p 指引杆的信号。 ) j, M4 M4 _ T2 p压,0 X* e" Z9 K: F8 [: }3 K9 y( Q* w 压力。通常以多少寸高水银柱(in ) P/ B5 R0 T- m. _瓶, ' w% k0 N- B% Y6 x的化学能转变为直流电的电气装置。6 i$ D& S' s5 s# k o , Z2 l( K& N& s" Yfa* I5 r8 l0 I* g7 Y, w+ V a9 B0 w6 A/ q. g! S* v required to stop from the same speed. 8 n. _2 C! K0 @2 ~ ]; ], J9 e, JB . K- x0 Z! T. m# M N; A. m% `% lthe center of gravity within allowable limits.7 T _. c, l2 Q, M5 j B- Q: b" W1 ?! q" X jackscrew for flap and stabilizer movement.* W$ R9 g: e; y" @+ p2 o! U% V B 6 E( [" u- n! I( K1 o) cdirector command bar(s). & \$ e5 n/ I+ g1 W2 u* r, U! pB5 A$ {3 c9 r- @ zero pressure measured in inches of mercury (in H( R# {9 R3 _* \ in " I, `1 i+ A, ]' @# H0 _' oBASE METAL, The underlining metal to which alloying " Q- r+ E" _+ ~; M. B cagents or metals are added. 4 I6 B8 O$ a; D( |/ jB 1 T: U, a+ ]+ wchemical energy into direct electric current. 8 C* f" {1 F! M6 G: k- J/ h2 @* b平衡场长, 6 m; ^6 R% N8 O当障碍物非限制因素使飞机达到最佳, r7 D" \+ F7 P6 I6 i6 {, n# v9 N/ K5 r$ r X' a9 B0 t* g0 z0 `4 b, }0 b5 y/ T- ?' q. T H. O为保持飞机 8 q% w/ w+ k5 [& O9 t/ p- a. N: ]0 K 由粗重螺杆驱动2 o9 Q( V2 v# F; u 安定面运动。 : {+ T9 Q B7 l( c& J5 J' G( D. h( X- Q! X! r用于除去飞行 1 X5 s S' }0 W! L; j" c7 q3 D. a/ [! k a 零压力以上的空气 " z; H; |5 _( E+ ]% g; fHg)或毫巴(MB)来表示。 9 h6 s# [ @. z& q) R基底金属," T2 I# l0 v/ e7 ^ 指合金中的主要金属成份。" h! r+ Z$ }+ U8 n3 u3 D$ e* T# c9 x$ p! F 将储蓄 # [$ Q" }! Q6 Y4 W% M; G英汉对照民用航空词典B OEING* n$ m/ M5 c' ?9 {& q+ m TECHNICAL DICTIONARY 18 3 ^& C/ M$ H% R9 v6 [+ nBATTER3 P. A6 N7 |, b/ v: ] direct cu / U# f- l* b' ]; X4 V% c9 t- Kpower su) x8 d% a6 s0 f0 K) H& Q; S Y BUS, An electrical conductor supplied with ; ~2 E9 H3 ~4 Prrent from the battery or transformer-rectifier for) c3 U; X1 u& N c pply to operating components.! ~( \' K# n. A: B% o2 _ CHARGER, An electrical device supplied- y0 b0 r0 N4 S0 R ith alternating current, which produces a direct current / S$ K+ d9 H; B# ?- Uutput for charging the battery on the airplane.# t1 \' u3 j, `/ v4 E3 F AY, A compartment in the airplane structure. ; E5 t/ e' p! g# T* nCD, SEE - BINARY CODED DECIMAL % g! W0 h, j9 Y. U) vEACON, A device which emits a signal for use as a , _1 [% W8 b. O! l Q7 u2 _$ vuidance or warning aid.* @. U8 Y9 @8 t) x% t$ K7 M! h- y BEARING (NO. 2), The direction from an airplane to a ) w; y. W: [1 n, x' h* bground station./ x# l& `, O' c: e$ N. O9 q 瓶汇流条,! ]" p! |: n& [$ x! S 将从电瓶或变压整流器来的直流电供给工作部件的导& C# i0 z! y. W Q: V& D 体。/ ^8 B6 D/ l8 \) a8 | 瓶充电器,$ L8 h$ ?- _2 [8 e 用交流电向飞机内电瓶充电的电气装置。带有交流电的, L& r) j# a5 L% G# |8 r0 |, _ 气装置,该装置产生直流电向飞机上的电瓶充电。/ v/ H3 O! y& D1 a 舱,: h3 d. Q$ }' E. S 飞机结构中分隔的空间。5 i7 i4 s! t9 Z, B2 o 二进制编码, # ]9 g. _" M7 M( m- y8 X+ d: O. ?见Binary Coded Decimal / i9 `# D5 f5 i: l6 w# yBATTERY 5 [# ]/ C8 O/ ^! F C$ E5 nw( M. P [3 ^0 ^ o6 G. W/ g/ r. a& g4 `: C B+ j* m( V; `- x2 a B0 k% _+ n: P+ l6 s/ Q B9 X( `" `" ]0 }% f2 m g( o4 ~) i, j2 G1 W& H0 K) |$ l BEARING (NO. 1), A surface that supports a moving % y$ Z8 O, H1 J' Q: a' q% Z, C' ppart and reduces friction between the two. 3 h# _5 R( _1 d$ b& N/ _0 Q2 P* n$ z8 e" P# T4 I# g6 w h8 y) E7 d5 l- [- t% I( D( U: P' a% R. Z6 P+ z% Y: G5 D: G. K% F" ^5 K0 v) n% d+ d/ l# Y8 W7 w1 O% ~ w# {/ ~8 l, l8 X9 t: T$ s1 s3 N信标,5 j2 f1 a: {6 I* a 发射引导或警告用信号的装置。 / m" K. d, f0 x方位(NO.2),; c6 u: r' L; L" i! E/ ]+ A8 J 从一架飞机到地面台的方向。" Z9 x4 P( l% B/ c 轴承(NO.1), $ _6 _# [, `) e) e用于减轻机械转动磨擦的机械装置。 5 K/ c! {+ X. X2 v! `; [4 d英汉对照民用航空词典B OEING' z; G* d8 e( Y' p TECHNICAL DICTIONARY 19 * }) R1 i- h* `5 n& s) KBELLCRANK, A double lever in the control syst 3 A% l& v2 G: j& ` uchanging direction of motion.% n& B# F% Q/ I- G. R/ I em for) w- S+ ~4 x3 g: X$ k# ^0 W+ V ct in the8 U' H* a( R/ G( K, \ neumatic system for absorbing expansion of duct due" H8 w8 @% L( ^, T3 [ heat.; S$ l" V: d4 r7 g9 y+ o1 e9 N ELLOWS (NO. 2), Corrugated folded or pleated% `! D2 G. |* r, \3 y9 X ontainer or compartment used to measure pressure. 0 l& x! `% |/ M9 S. IEZEL, The part of an instrument case for locking the 1 s' V, Y8 A1 ], llass., ^$ j8 [0 o$ U& A3 M IAS, The potential difference applied between two/ S# B+ A: j, D: K! x: r oints for controlling a circuit. # _+ Q4 c6 Y; a ?BILGE, The lowest part of an aircraft fuselage. A place , H' `1 U" B1 Y" cwhere water, dirt and other contaminants collect. ) R* I! ?. A9 A# Q! k' I气源系统内提供管道热胀冷缩所需要的余地的波状+ l* T: C6 [/ {1 {! b% }# b" P 轫管。 ( k! u; ?& O+ F" E y5 u( n2 w; \1 Y空膜盒,! P) \+ I) W+ }$ T. V h# v+ q 一种具有波状表面的容器。用于量测气压。, K0 v- N+ [! T8 s! B 嵌沟缘, 4 s( R& U1 W& Q8 U8 W将表面玻璃固定在仪表上的圈状零件。 : y, r5 w' V& X7 s压, : T1 P% {$ w: |8 A在控制电路的两点之间的电位差。; V" l a1 N2 u9 m* d v 机身腹部,9 \3 w9 _; U( E9 s6 `. j' w* ] 机身的最底部,通常水,脏物,和其他外来物集存于此。 - Z8 v' L" q: I! sBELLOWS (NO. 1), A corrugated flexible du : @% s' r a6 M# ~/ Jp, d4 R1 C" a2 ^4 S9 P to , a6 q% Y: @" M _2 JB3 ~3 d$ s5 R, o, i c + E5 i& J0 q! c) K+ u+ QB + p5 J o5 T/ l0 W7 }g 1 \; H8 Z/ {- @ W' JB' F% r; ?) C$ j6 a p ! {1 i4 @1 d/ C" h. @直角摇臂,. n7 A3 x) h+ \# e" i7 d 在操纵系统中改变运动方向用的双臂摇臂。 ; U4 `: j7 E* i波纹管,3 j U: \* E1 ?$ W) R* p5 m& ^7 `- M+ ^5 J- }5 B% \9 Q& m' P1 C6 U/ q b& q+ T" E3 Y* t, D/ E& ^' _$ G. m: X 英汉对照民用航空词典B OEING 4 q% r, f- c0 ~+ p1 VTECHNICAL DICTIONARY 20; S: U7 L/ C+ X$ U9 \ D BINARY CODED DECIMAL, A system of coding each# E# ?/ s/ g' `+ h7 p) ] digit in a decimal number using the binary equivalent. 9 Z4 y: y- p( V# }BINARY NUMBER SYSTEM, A number system using 0 X2 @4 U+ i; @) ?4 us " e. i" y% c4 B6 Z% L7 b6 v9 vIT, In the binary number system, the smallest unit of 1 j- J9 E2 {$ fformation, consisting of a 0 or a 1.1 a1 q0 h$ D2 Z* B7 N: \+ G7 p ITE, SEE - BUILT-IN TEST EQUIPMENT 5 ~# P3 y+ }/ y# ~$ t2 HLANK DISPLAY, A display that does not have any * X3 i3 K* S; r, Q. [# |# [dications, normally due to failure.3 b: N: O, A0 W2 T% V: ~ LACK BOX, A container for electronic circuits to record7 Z" I4 `, v; K0 L ight data. . y8 B, P& v% E7 A# jLEED AIR, Air taken from the engine to power various E& e6 u6 E* [ d- q( Z) |ircraft accessories./ t& Y6 _1 p% ?: | F3 Y A valve in the pneumatic system for air' K5 s& G0 z$ d7 W2 l8 R; p supply from the engine or auxiliary power unit to the4 C$ o- s& z! O; y* a4 N, A% |8 M2 L l pneumatic manifold. A valve on the engine for reducing. P3 ] u5 O; J! f" C! T6 u3 S) Q pressure in the compressor section. ; _: h9 R d8 p+ J/ s进制, Y. T) z+ m2 J/ z6 R$ S 进制, $ Y* F; y/ J' a+ ^一般用0和1)和2为底的数字系统。 0 F9 @' f0 t+ T1 i特(二进位数),$ s% o" P% z. d6 z4 S. J0 v 二进制中的最小信息单位,包括0或1。( t0 p' W' N6 S$ ^ 内自测系统, ( b! Y2 @( O8 h. J见Built-in Test Equipment8 Z5 j( b' V% N2 ^4 x% [ z0 t0 K two symbols (usually denoted 0 and 1) and having 2 a6 J& u( D* P( m& o1 [4 `# p0 V its base.) V8 a+ Q+ A" d+ }4 X) U B8 a$ ]/ O+ ]( e7 W+ [ in , T( P, J) m4 r$ iB . @+ y9 B0 T7 i1 e; |4 l1 rB4 o; x$ D# D3 V% K! @4 r& a/ I w7 P in 6 Q7 t' `/ x+ m: @& ~B 9 z& O1 ^/ X# \! I& z& ofl' g$ |' w9 V% E' w3 u8 P B5 s$ I3 A5 e( q q a 7 G* w# d1 N1 E; d; d( ^* tBLEED VALVE,7 @5 D+ h/ u6 g6 l; v7 K 二进制编码的十 : E% p- H" N# Y- h ~一种编码系统。用等效二进制位数编译十进位数的每一 ) ~& m$ I% B9 ]2 E2 @; ]- U位。 " n$ T, `8 Q% v, O7 g" M! O" ?' |! I# S& ` {以两个符号( 7 g$ G U& O3 n9 N: o6 g8 c" I% q. U: n) I y1 \& ]' n9 |3 b, K7 x- r. @. 0 y3 e8 g1 I3 N- N: V白显示, . f. p. r+ Q2 }. q通常因故障而造成的显示器上没有任何指示。* n, K, I" Z( j6 ?4 S) c# q6 ~9 h: d 匣子, 7 l1 E- j( @( _: t S% U装有用于记录飞行数据的电路系统的容器。5 f9 h. H+ {4 j. g4 Y- L 气, ; \- v" k# M. ?/ o+ M取自发动机而用以驱动飞机上之各种附件的空气。+ J1 u, f; S# J" Z# f% r 气源系统内,使来自发动机或辅助动力装置的空气进人5 f6 X1 F& p4 b1 ^; k/ D 气源支管的活门。发动机上,用来降低压气机压力的活门。0 E1 o1 |: U: L; r+ M1 D1 `0 u# }" h- }2 V/ r2 O& u7 O6 B4 b4 w3 x& ~/ s. P% E% r( X b5 L, i4 j! x 引气活门,6 c, B" u/ I. F 英汉对照民用航空词典B OEING3 D! e7 b6 {5 G6 S TECHNICAL DICTIONARY 21 ; R& b3 m+ }5 vBLOCKER DOOR, A device on the engine for blocking , L' k8 P* z, r0 `the normal airflow during thrust reverser operation.& w2 L6 B+ I% X1 D LOWER, An electrically operated fan for circulating air. 2 n2 T( ~& o! xLOWOUT PANEL, A panel in the structure between' {2 t1 A7 ^/ L- X. B o compartments that opens to equalize pressure in 5 W8 @9 C/ w* q8 y3 O! e: s9 }8 [e compartments. ) B5 |6 q. Y( Y6 x, I1 cODY GEAR, The landing gear attached to the. C3 N9 A) t8 m1 F grounding. 4 b! Y& z" b- c7 ?: Y9 `正常的: d# R3 C3 c5 M4 t2 y 气流。1 }. P- M) ~; S" C9 k! S9 L- {7 R 鼓风机, 6 F" z$ W& i+ |用来使空气循环的电动风扇。 " ^3 l w. f) Q+ E$ [+ C0 g压口盖,0 ^. c+ Y$ Z/ h3 v' D8 E. f 两个隔舱之间的口盖,打开后可使两舱压力相等。 # b5 B( d7 {% G0 g5 h" u身起落架,1 _! @# @9 L& _: Q. A0 E" [ 身构架上的起落架。 , J2 B9 K! \% E- W$ x( b6 h0 b& WB, S, B; S$ i! q: v T B ! F, \: h8 j9 Ttw5 E2 F/ D% G/ _7 Z# F4 D th 6 b" ~& m9 e, V, g: aB # w. }8 U5 m4 |+ Tfuselage structure.2 {7 B' W9 n; L0 i; m' F8 K BONDING JUMPER, An electrical connection between+ ]* w9 _/ ^5 a3 J- _ a component and airplane structure for electrical; X- v i& M) x2 |8 F) t) \! r+ Q 阻流门,; E7 q) l2 W' |& _! j3 g: C, o 发动机上的一个装置。在反推工作时用于阻挡! B4 |1 C, f* l9 J9 Z6 U$ I4 `8 k5 t; t! E) ~/ [3 i9 M0 S- e |8 U- m 装在机3 G/ Z9 s; \! {7 q$ O 搭接片,9 k& r p7 K0 N# {% M0 o; e 连接某个部件与飞机结构以形成接地的电接头。" l4 _! ^. p2 x 英汉对照民用航空词典B OEING ! C/ M4 ] V0 D w, lTECHNICAL DICTIONARY 225 s ]' k. |* j1 R8 ]' g0 D- ] BOOLEAN ALGEBRA, A mathematical system for6 n0 d1 A- j# z+ Y' w" I writing combinations of logical statements./ J! Y; ^$ U3 Z: b- T. u- H BOOST PUMP, An electrically operated fuel pump for 3 U& P( K' D) n$ Pfuel supply from the airplane fuel tank to the fuel8 v6 W8 G& J7 S1 K manifold. ( g& E9 ?5 n; x! e- fBORESCOPE, An electro-optical device for looking at 6 a: o% y6 G+ _; k5 k9 Cternal parts of an engine through holes in the engine.6 j+ n1 X% M0 @" p/ M; ~% J8 i orescope ports) 7 q/ O# f& s8 R+ H0 hOURDON TUBE, A curved flat tube in a pressure gage & d: l4 q. v( N* T$ F s) i3 M; o% Ar moving the pointer when pressure changes inside# i3 V$ Q. a2 d. V on the ability of the brakes to / ~2 c, q" K% A9 Y6 W8 Z) y4 ~bsorb a predetermined amount of energy during a! P/ H! H6 @5 ?1 I h4 J, y jected takeoff./ l; K& n) j; k! o4 @ 用于通过发动机内的孔(孔探口)观察发动机内部件的, V8 Z7 J, ?) T7 S9 ^ 光设备。 & ]3 ^/ ^* U! T2 x5 F$ @- k端管, / a/ ]; U6 G! ?( z1 r% S测压计内的弯曲扁管,管内压力的变化时它使指针移+ ?1 }& J5 r3 {( r 力。 % I+ A% G" X/ b0 h Y极限重量, 6 f% `. I3 g0 R9 S" V2 ^9 b; _3 y; p0 w T* Q 起飞重量。 5 t( h! t) j& G# V' {+ a1 e1 t发动机滑油系统与大气相通的通气口。. W4 P2 ~7 }" o h in: X) c% n4 w" X7 R7 a6 |) t1 l (b" K# ]* m* C1 w y B ! l7 n9 D. i$ _; N3 h9 g3 @fo ; b B: @4 j! t4 c) P& H( G3 Tthe tube. 7 f. S% L0 C/ p, jBRACKET, To enclose or surround. 2 r+ C6 B0 V+ W+ q/ j. OBRAKE ENERGY LIMIT WEIGHT, The maximum( u2 Q, t) ^1 G takeoff weight based3 s1 G! ~/ I5 F$ J6 ^! [' {9 N: x* ~ a% v7 Z. C. z0 f) B2 I re - s4 M$ _5 p% @, iBREATHER, A vent to ambient of the engine oil system. 6 Q8 q2 g- O* {% }7 d布尔代数,& U ~8 m: w! K+ O( @" | 一种用于编写复合逻辑命题的数学系统。2 X8 @3 u4 c0 O" r5 R 增压泵,& B+ Z. N9 K: z# f9 q, _ 从飞机油箱向总油管提供燃油的电动泵。: H% F: T* A& _$ b j7 f1 J3 e# O- _ 孔探仪,2 k- c4 Q4 t) Z$ ]( U4 i0 K' ?9 D9 C! D6 Q3 X' A2 s: H* {- c( [- V) @! j& I 动,以指示压1 P1 G `! K1 N% E 托架, . L7 T1 ?4 ?8 I3 r# m8 n用于作支撑、装托、或围绕之用。5 w; F9 z* u P% u: u! J" G3 b 刹车能量 . e! J+ V* z% k3 D7 R中断起飞过程中,取决于刹车吸收预定能量之能力的 + q7 B4 S3 M# N5 x- ]" j8 A, H# f, A3 n8 H6 q0 E1 k" p% M 通气装置, ) S. [) V [* s' o/ z英汉对照民用航空词典B OEING , q5 v+ @ ^, q8 v! K7 J! X0 RTECHNICAL DICTIONARY 234 x" H7 y. y% h BUFFET, Vibration of the wings and airframe resulting0 \) a1 X2 |. A from unsteady airflow over the wing; caused when1 _" a2 Y0 L- b$ ^6 A9 f airspeed is too slow, the bank angle is too steep, or & c% c% K( g2 B: W8 Q1 virspeed is too fast.7 L) s0 n5 c6 U- k9 ]6 a+ h UILT-IN TEST EQUIPMENT, Equipment installed on " o" {" L% E1 C$ d$ Ie airplane and in airplane systems to test the systems8 i' m& b& T. s ]3 ]) [ ithout external test equipment. 4 s* Y/ W5 m. YUFFET MARGIN, The amount of residual maneuver + t% N, p& b9 L! t4 v: t% kapability present before the onset of buffet. ' m0 y' `" Y: W- @UG SPEED, A preselecteed speed to be observed1 F# X& Y7 o* K1 l nding sequence. 5 x/ `1 E* @; U; mk4 B$ w: F' i1 B7 P: T ng landing gear operation.) M$ ~% D& b) L" O" k 速度太慢或太快,坡度太大,均会引起抖振。 / V3 h( g; m) A2 m- d4 @# ^7 C& R自检设备, u- E$ L4 a/ \9 K" ]7 g安装在飞机和飞机系统中,在无外接检测设备情况下,; j. f5 S3 ^* W8 W 用于检测系统的设备。 0 I: ]8 g# M" P4 ?抖振裕度, ( F& S- g2 U, E' _7 ?# n1 H5 `飞机在遭遇抖振之前,剩余机动能力的大小。 ; H' }! t4 Q$ a4 T1 J9 i2 q' U" u1 \! P- w标速度, : q& W9 }2 N( O- y+ T0 Y5 O在某些机动飞行过程中,特别是在进近和着陆时,飞机% a3 i( A$ p9 ~ K9 V6 Y' f* i1 o 预定速度。/ B- n$ f! [1 l- ]5 c 力装置, $ f1 O+ L- V2 o5 Q$ _# d1 {架工作的一种机械设备(弹簧或减震器)。+ |. O6 K5 z9 D* V$ Z 流条,. i( I6 s3 S9 H) c% D1 M* d 在部件或组件之间传输电、数据、或定时的单一电线或* `' u: _8 k7 r A# W: V a2 C5 I. N* [! a- _7 h$ D' \& v* ~ B 4 a1 b; Z, h Cth ! p* e) o' D; e; Mw 0 {4 U# n4 z6 V! k9 qB ; ~ v3 _. L: ?3 q$ l' Gc6 A S: l, e: R B 2 S( n, o. |; M; h kduring certain maneuvers, particularly the approach and 3 @& u& h1 h# X! |la 9 ?5 d9 z. ~; z0 o5 u" }# B; oBULKHEAD, A structural partition in the fuselage or 0 P8 n* i3 }- ~) P1 u' ~# g3 S: Swing. ( b6 i6 E: ~. v- g; V( d, x- iBUNGEE, A mechanical device (spring or a shoc: R' J: k5 }2 b absorber) for assisti0 F2 i' [+ ~' ?5 [5 @" v% M BUS, A single wire or group of wires which transfers. V+ t2 @, N; D/ l) H5 A power, data, or timing between several units or. O- Z( p, ^' n. I; Z0 t modules.% f B) i9 G: M2 T4 m b 抖振,3 J+ ?* R& b p1 M7 W8 k 由于机翼上表面的不稳定气流引起的机翼和机体的振 . \ n* J. V" W, E3 g动。飞行0 e) t* @$ ] M' i5 @: t6 U" ?! m% | z! @ 所应保持的 - ]6 K, o* U9 Z8 C ^壁板式隔框, 0 _8 y9 Q) H6 s机身或机翼内一种结构隔板。( s) L" S: A2 y4 J$ w6 T7 `9 M% e0 L: k用于协助起落. B, ~+ D- o& l0 a3 M* j6 N% |/ }- B+ ]; \! A 电线组。 2 r2 c' ]5 v1 t5 `; ]7 \英汉对照民用航空词典B OEING % B/ ^, Q. |1 r% C& }+ w1 Q# xTECHNICAL 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( H" B+ ]% } cables in the control system.* e4 t8 C! C5 ^6 M$ i5 M& w& n and2 X6 V5 R9 t1 o9 E l circuits for control and protection of " k2 N1 Y; f1 z" s) c; o: llectrical alternating current supply to the airplane., P9 [/ C5 u! }; h duct for closing and opening the duct # {$ U s3 d1 r+ _assage.: t( a1 \. {1 D' G UTTOCK LINE, A vertical reference plane along the 5 h: B/ }: b& aselage for horizontal measurements of the airplane.! z. V) r6 Z2 |& Y) ] h# p; R 接。 : b! P, L0 H3 u' g) C组件,内含控制和保护飞机交流电源的电 ' u8 U- n- M4 O i$ w& ?6 c- Q3 p) `; k8 |) [% J! C9 z) Z" i, m 作动简控制的转动装置。用来关闭和/ N2 ~% @/ v' e# k 启管道。 ( u0 L$ C5 c" O( a1 Q2 @沿机身走向的垂直参考面,用于飞机的水平测量。: R1 a* l! j! m1 c( |0 R- s BUS PROTECTION PANEL, A module (black box) : G- F* V( ?& ~. p+ e/ O2 ]! U2 ^containing electrica ) l) `( A$ q( @2 ~9 O+ E, ge5 E; B- H! R; z3 W BUTTERFLY VALVE, An actuator-operated, rotating n5 h! W" D# Q! q8 J" Jdevice in a " M3 B% W, _% H# \, U/ u! I. Ip# ~: ]8 F7 O3 H" P3 g" |# q* H F B, X# y _7 I8 k% ]8 s8 b+ }6 K fu 7 y6 d( R+ E2 z转动鼓轮,- Z. P6 \& s8 k O" T3 Q( S% O) S 在操纵系统中,具有滑轮和钢索的机械式连' [* ]+ L; G6 F( `" j N 汇流条防护板,& ` ?1 \5 R$ Z6 |$ N8 n; J 黑匣子式的 ; P+ E/ b; c% I7 T0 O" M, H% k) n% ~& i5 X; U7 }+ X 蝶形活门,# p# }# `, D" X* }" s 是一个在管道中由( ?! U4 p" H( |3 b U, O) h) O, ^! Y! O" r. {% ~& f# u; A纵剖线, * M% N' T- P4 g- R英汉对照民用航空词典B OEING1 C3 K( j1 |' U0 s1 A# y2 v TECHNICAL DICTIONARY 25 z% s7 w5 t4 Y0 E: bBYPASS VALVE, A valve through which air or fluid will ! a9 O% r# ]/ D% N C3 ]- Sflow if the normal flow path is blocked.' r" Z( Q2 y& C5 B& G) k+ q BYTE, A group or string of binary digits. A byte is 4 o- f6 v5 N3 s6 G9 k( isually eight bits long.; M: |- y, s0 ^4 E/ ^# p/ F ABIN ALTITUDE, Atmospheric pressure maintained + y+ d* T7 z1 L& K) Qithin the cabin, indicated in terms of feet above sea # m" U+ e3 a# Q5 rALIBRATE, To repair, adjust, fix or correct the9 ^3 K+ \ H: u0 j7 W easuring capabilities of a measuring device. + R% e# i7 b" p8 U0 jALIBRATED AIRSPEED (CAS), Indicated airspeed9 t4 z2 O# `' W8 d' l: y AS) corrected for position error.' z1 ~$ ` t2 _5 J: U9 ` nical % z/ t+ R& w* `4 Uomponents.9 ~2 r H9 ^" d) z: _) @, L& a) T d0 u* i0 j0 ^1 M* n5 i' Y+ P节,/ v0 e& D6 b( K* ~6 g 一组或一列二进制数。通常一个字节长8位。, C1 ?1 D" M8 W 舱高度, : R6 b ]; B* H. a ^: Q4 U( V座舱内保持的空气压力,以海拔多少英尺表示。 3 z! D! z) L' S& L准,9 x1 v5 g2 o/ M V 修理,调整,定位或改正测量装置的测量功能。 5 I5 c5 ^. i( h/ C# L正空速(CAS),: W4 b4 l% p' D, y3 R( D 在修正了位置误差之后的指示空速(IAS)。 " \- J8 B, }0 j. B3 ~9 ]! R% x- `用来移动机件的一种转动装置。 & I1 \3 m( \* f/ Zu Q' v- [+ m, r5 f* t C 0 { `$ x0 L. X4 }C 5 X/ E* ?* `3 d W2 Yw0 `- Z3 L% c ]- ~ level. 3 k( M" z' L! Y, rC7 w3 w& v6 b/ \. w: c m8 s9 g) d" r; q% Z* S C # u3 i/ ]/ w, D. b3 r4 q6 x4 I(I1 o+ f1 o% v9 [) s* j. H CAM, A rotating device for movement of mecha2 H; p& z- Y- `! y9 h. V7 ^ C# i- k/ d' q; ]1 @ 旁通活门 & H1 ]' [7 _( ~气流或液流在正常通道阻塞时所经过的活门。 # g5 S2 \; V+ A7 t. q, U2 _( S' H( `+ t# \$ [0 P8 D) u$ U# |( f" L/ O6 [2 p% A" H" Z+ G" Z9 u" ~9 [7 [- d, U( w! n# x& d w/ n 凸轮,5 e; Q f5 E) h* J8 ^ 英汉对照民用航空词典B % A8 ?8 x+ X# X7 d2 B( q! F; WCAM-OUT, An autopilot condition in which the actuator1 F! \- m) x# Y2 L detent piston is overridden, either manually or by the * H$ _+ S+ Z% a: j7 l5 ather autopilot actuator.7 d& H/ p, W& a6 n% |9 z0 `+ N+ L: i AP, SEE - CAPTURE 2 I, A7 S, ~. wAPACITANCE, The measurement of electrical energy , ~3 l" i6 F' p7 C: K9 wtored in a capacitor (condenser). / q1 o( S" N8 k7 K! yAPACITOR, An electrical component of two metal / u- j$ j# f8 ?2 nlates separated by a dielectric material, for storing 3 Z1 r6 X3 {" I2 |4 c2 _% p3 vlectrical energy.' Y1 w3 }4 J5 \, l6 P& r CAPTURE, An autopilot or flight director function to " y0 i5 d. R# l$ ]' ?/ U" O+ Wacquire a selected mode. " D* C |3 x9 u) Y' }8 l# eCARD FILE, A container on the airplane for printed 2 T8 Q) W8 ~" w2 q) h- m6 n8 [circuit cards. 4 g* e) @$ P) _- i$ r' ?5 Q1 V" f一自 / f- v0 a2 @8 h4 s动驾驶舵机所超控。% ?' S6 y2 G( E$ Z+ s6 L 截获, ( F& w) H: [8 b见Capture $ _. v0 r5 p% Y1 S1 J/ Ao) r7 }. k3 [- y& s @. k C+ d6 X8 Q5 F1 Y) F# M( G; ? C 5 ~. P& k& c- [3 B' X: Z. vs - w4 {5 M2 D- z5 E8 r" SC4 T% k" M" n4 d4 i p" i( P+ Q: V! ]; L. q e $ _& E# V0 ]8 `凸轮不工作,; D3 S" w& x4 S( m% u 一种自动驾驶状态。此时舵机锁定活塞被人工或另 % b6 P" G7 V1 D' ^" Q- ]+ ~) A! K U( [& f' @4 n- ^! _电容量, ( o; R0 |4 V- [/ [% I- [7 _3 I电容器内所储存的电能的量度。 ' I6 E/ H* y0 M$ b4 M) Q! m* r容器, 6 R: [, l4 Z Y) W% _. _7 l两片金属中间用绝缘材料隔开的电器。用以储存电能。/ o, ~# J& L1 y! F 截获(CAP), & {' n/ W, [/ S/ F自动驾驶仪或飞行指引仪的获取选定方式的功能。 # O4 G: R7 v$ V2 H线路板盒," _% b+ U8 \3 d3 [ 飞机上安装印刷线路板的容器。! I) p) U$ T( w$ s3 ]6 ~6 c, r1 U* v- V OEING3 M' x6 [5 F- N# Z2 A$ U TECHNICAL DICTIONARY 26 $ q* Y! N0 \7 {9 z* I( w# R英汉对照民用航空词典B OEING9 N, F( J4 K( m% K- _ TECHNICAL DICTIONARY 27( \, E. h2 @- z' {0 A3 b _ CASCADE, Two or more similar circuits or amplifying( t5 v _% i5 T$ v8 Z stages in which the output of one circuit provides the% W( {1 |& M$ Y( f& u) O put of the next." k* p" M8 \: z" F0 d" \ v ASCADE VANE, A vane for turning the engine airflow N. M C& M6 {! C) a& o uring operation of thrust reverser." |6 d. \. R8 h/ _/ @ } ASE DRAIN, A drain carrying lubricating and cooling k5 m- r l2 X( h# o1 G uid from a hydraulic pump. * k9 c: ]+ q9 X2 d( o4 ~) x2 zATHODE, The element from which the principal ) ^/ c5 H. ?! ~' Wtream of electrons flows.( C" F% L- B/ t1 F- u ATHODE RAY TUBE, An evacuated glass tube with a1 w E* G$ L# Q# o( ^/ V) W$ P CEILING, The height above the ground or water of the% P7 I$ e, D, S9 [) l7 E$ G base of the lowest layer of cloud below 6000 meters ( i' O+ U9 _$ U(20,000 feet) covering more than half the sky. ! g0 W% K/ p, D: Z( F6 i程。该- V$ k& p x, H 程中,一个电路的输出为下一个电路的输人。 6 R" z; P" p0 Q' A4 t+ U叶栅叶片,1 j' D% a+ z7 u# ^0 [* H 在反推工作时,使发动机气流向相反方向流动的叶片。& F& P7 f+ @, N& J' p 匣余油管, 1 _/ L) {0 N& J" R6 S* d4 R液压泵多余的润滑液及冷却液的排放口。 + L- [% t2 L- e' b# [, p极,0 l4 J7 F3 {, ?1 N4 j$ ~: ]: J 电子流流出的极位。 6 g+ \2 a F# h# V; T7 V. {! q极射线管, ' o. u* V {; a& J; N% w/ _有显象屏幕的真空玻璃管。用于显示信息。' q3 p/ J: @8 d4 o 云高(云底高),2 i' P& ^$ l& m. {4 L6 g& a2 S) c 6000米(20,000英尺)以下已覆盖一半以上天空的最9 }% Q! Q, t: j) K( D$ v, T0 T4 a 低云层底距离地面或水面的高度。 9 M9 e( E, S) @/ P% Min ! l1 H' I; P* k1 gC 4 U- @( i2 m5 p( M6 [d* e, ?- d t" ? C+ A+ L4 V& ^& b' t fl . `& `1 X. B( m$ @$ b) dC 2 l& {5 m$ R* [, ~( h6 Es8 r2 C* B5 H; r6 f( ^. Y3 B C9 k% Y; G2 m8 A4 l5 z9 C! k viewing screen, used for displaying information.8 H, D8 c$ D/ A; g* a( g 级联, 8 W/ U& I+ Z/ u: _两个或两个以上的类似电路的逐级连接或放大过 ) `- v/ y' |5 a: B2 x/ T ~5 w: R6 x0 Z( i `1 o/ [7 C) a; ], T4 L& Y& u9 J1 Z6 M, {/ ?1 o' K3 W! b% o$ d0 }8 P 一个具 + K! R( \% O6 o" W, E6 m h英汉对照民用航空词典B OEING ; g6 w0 T( P$ d0 @* V7 e: |5 kTECHNICAL DICTIONARY 28) B6 X, D6 P" f CELSIUS, A temperature scale in which zero is the 4 X# O% ~) j7 h; ffreezing point of water and 100 is the boiling point of, Z4 } ]) M& e( C: v water. ) c( Q, _2 H+ Q2 S6 n$ h" _4 tCENTER OF GRAVITY, The balance point of an object ; r3 U) G! O. \* {+ Ir rigid structure expressed in terms of percent Mean % j+ C% u& O3 V) j! o. f: }erodynamic Chord or in inches from a reference point.0 m2 d9 j; ] W3 Y ENTERING CAM, A cam for moving a mechanism to a6 i* V7 E" n4 X/ ~) ]' F2 c eutral position.( i5 g% v H+ ?4 j IGURATION, A configuration of the + m, U. V' S% nircraft approved for operation by the local governing: }% x/ d0 c. Y( x gency., P: V$ w# \& f4 Y7 I X ENTRAL PROCESSING UNIT, In a computer or" ]3 y2 p+ Y2 A* G igital circuit, the section containing the arithmetic and) w$ g' M6 F" V& K; u- k7 Y gic,control, and internal memory circuits. - X) q1 u1 g$ X! I: QENTRIFUGAL FLOW COMPRESSOR, A type of / g9 @5 y+ _4 W8 f7 B) L! @, Aompressor in which air is taken into the center of the 0 R; q `! @3 m% v$ \6 apeller and is slung outward centrifugally into a diffuser, U* r J: n: I, X, n x here it is slowed and pressure is increased. ) r' Q; l r3 ~/ Q1 K4 k) ~( vCG, SEE - CENTER OF GRAVITY: G L3 P e+ N1 ~' E% | 构的平衡点,以平均气动力弦的百分比或 . H% r- Z7 F. q: C- K' p( g9 y某一参考点若干英寸来表示。' B3 |7 y& S1 q Y# X+ j5 B 中凸轮, {6 o; s% i; i/ B0 d将机构移向中立位置的凸轮。: d) q n% {* ]. o- m, v& S- Z 格的装机状态,1 B' F! B$ @. Z* Z+ v5 P4 K5 }2 M# L 由当地主管单位批准使用的飞机装机状态。9 g* U. [. A( w: g# I 中央处理器,( c/ h; w6 h4 z* t7 a- x4 E 计算机或数字电路中含有运算,逻辑,控制和内部存+ u1 q7 U- U5 n. O: w( g* S$ e. P 储电路的部分。 . u+ x! e0 M1 N2 b' y心式压气机,$ t( p. E* v7 s 压气机的一种。当进气到达叶轮中心时,被叶轮离心抛* x- S: v% t- c2 m$ m: Y9 a+ D6 E 进人扩散器。在扩散器中气体流速减慢,压力增加。' T& [3 h% J/ ^( j2 e 重心,$ T! c( o9 N; A* \0 r 见Center of Gravity ~. k8 ]0 F' ~- p0 Io 1 S2 `2 B3 V3 c: Z4 SA0 I4 b, `+ x. o6 G" {6 Z C & U& C# V8 m" L1 ]+ pn # }* w* E0 n7 L- jCERTIFIED CONF % _$ A) `2 d: s, ~, da, L: i0 {3 O5 [# p8 p a 7 r0 E4 |$ Z1 s* B8 Q8 x8 k- ]4 _C* s$ o B9 j, S4 |8 F# q d % G1 @3 y! x, |: z2 r7 D/ H" ~lo+ t/ t) v: v/ g! E C # d! C3 U4 l: N4 j4 w' x) @. |5 f' cc+ A/ U* `: E8 A! U3 @4 w6 q im8 T u: i% I1 r" S& m# | w1 a8 t7 o( h1 @5 u5 G5 I' [ 摄氏度(°C),- e8 F& g+ c5 Z; J: I3 r 温度的度量单位。在此单位中,0°C表示水的冰点,. T! N; d* C2 w# w* G' I, x& _ 100°C表示沸点。. v) o& |& c2 a5 C6 {5 y. ?. a2 ?3 b& | 重心8 Z8 w5 m i( m& i& D. I 物体或刚性结/ K0 k- o8 m* m, y% s$ I s- s! j: [2 ^+ Q9 K, x. m+ \& N% @) @8 t0 ~0 D* s+ ]2 J7 e- d5 H( G+ G7 {; Z9 i6 T9 O/ ?; f3 P% H 英汉对照民用航空词典B OEING5 p/ m [0 X: R9 q6 \+ N# R; U: H- p ^. ^ TECHNICAL DICTIONARY 29 1 Y( }/ ?& [+ e% n& w/ X& Z xCHANGEOVER, Conversion from one mode to another.1 ^. R$ i" ]* k$ d& q, F HARGING VALVE, A valve for supplying air or fluid to! r7 J$ a! q5 u1 O( j4 T4 n) v& J HECK VALVE, A valve allowing flow in only one + ~& V$ P5 Z+ Sirection. See Non-Return Valve.2 C Q$ ~3 P# s' C* K2 H HECKSUM, In a computer, a summation of digits or z: U5 q3 `0 r' H its which are primarily used for error detection.. R. o* x4 f" }& X5 D HIP DETECTOR, A magnetic plug in sumps of ) A- d5 G" h6 Q6 [2 Gbricated components for detection of internal failure of$ `0 `6 k2 O# m# F( H* I e component.+ z+ b! Z- C1 [+ H9 q: k2 E& J6 F HORD, A structural component of spars or frames.9 A3 H A# l) [) H: \. P$ I: c 添活门,) @3 I5 H5 k5 e9 J9 M 器充气或加液的活门。6 P5 N" h# s# S) j 单向活门, ' Q R; Z0 B/ S; Q* s6 O i" C3 K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/ c' @# ~: v' \+ B X( ` a reservoir. . b% p! o3 s, S/ ?8 p& PC . r8 k5 H7 X8 d1 V- I8 k/ Od . D: v U4 I9 d8 D. q0 b0 {& CC $ ]' U6 c) r0 k! D7 ^ ~0 T# g7 `7 l4 Mb2 C; _$ i" s5 c* C# D6 ]( [4 C! I: _/ v C % T1 z# v$ c' F. d( _. k, mlu 2 `% G: |( u( @5 f% fth , f" R! \/ p" B, SC 0 x1 j6 u; b8 g$ X& I0 }* {转换,( h& |& b: w8 V/ E$ u& `* T( P 由一个方式转换到另一个方式。, ?: X3 n; T9 s# I( O) i3 p2 h+ F, Y# h0 {: p; K8 e用来向储存 : L6 {- W# I/ w- y* Y4 W0 {2 X* L, r: v0 \ 总和校验, 1 c! ~ h, T+ u. Y计算机中,把那些用来探错误的数宇或位数的总和进2 q, h, A. u! r2 O2 ]- t& J5 V- | 求和计算。0 w" v& A, y+ X8 y 属碎屑探测器,4 B( i# c; N7 @' D# s1 j! l7 [ 装在被润滑的部件滑油回油管路上的磁性塞子。用来探 : Z4 ^) [+ b( x6 Y部件内部有无损坏。9 b. W+ H3 _( q! H: V8 ~/ S# ~8 C 弦, ' h- U6 b; m. v: z4 f3 i; D3 c梁或框架的结构部件。* c, I) f; i8 Y, O7 t8 F* \& v+ ? {/ n7 ?/ g% Q5 s. r: }! I; F( v2 \& Y) J, E N8 E8 W; I, T" Z: ]) A! ] q/ H( E2 ~6 |+ d& b2 Z& _. Y. O# l1 A0 z 英汉对照民用航空词典B OEING ! W% l( z2 c8 q4 E2 Z; XTECHNICAL DICTIONARY 30& m# K2 P& x; u CIRCUIT, A closed path through which current flows( _* m+ g( k4 d" R ource. 9 l) U5 Q. s/ C3 ]7 [% N7 G$ tIRCUIT BREAKER, A device that automatically; A( Y! V, r' r' A eactivate the system. " n& {" K: R3 P, B, ]/ flear of all non-frangible objects which 9 \) s# ~) J8 r- S+ f& z( s: Jay be used as takeoff distance available when 8 N* t- E- s1 ?$ {; o6 n" F0 r7 Walculating a takeoff weight.1 ]. r% O1 `8 p3 a! ^! z2 L' D r water under the control of the appropriate5 F. T1 D4 l c. W$ ?/ T/ X, u" \ uthority,selected or prepared as a suitable area over8 v6 k' o) v8 F. s) E! @: f9 C hich an aeroplane may make a portion of its initial # B# ~' |1 W0 K2 ]3 x9 [limb to a specified height. & Y: X5 ?0 T# a0 Y$ R9 a% S4 T1 gincreasing. 3 H& z5 z+ \# Q# c6 m6 ?8 o; H. dsed 8 }% U/ `/ f# S. S9 c8 c( SLOCK SIGNAL, A continuous string of pulses used for 8 ]# r1 |# H6 } v5 d6 f( R开关,; j+ P4 X( U0 ~8 f. O- h 故障情况下自动中断电流以保护线路不受过电损 - g9 ?1 V/ U+ o5 e! k' ~5 s体障碍物的区域。在计% C$ p& G: V4 j' b! i 起飞重量时该区域可作为可用起飞距离。: n, v- k% Z' m* a 是在有关当局管辖的地面或水域内一个界限明确的长 7 ]& a, ~/ ~- \$ ]2 E7 F形区域。在这个选定的合适区域内,飞机可完成初始爬5 u! g* m. X: F7 a5 _- b9 P* B/ [2 ? 的一部分,上升到一个指定高度。 ) Z" Z6 s% J) d* U4 Y8 ?飞机高度不断增加的飞行阶段。) W9 y# K& H. `2 x1 Y( u$ M$ O$ ~ 钟脉冲,( @1 R+ q( C; }5 ]$ m2 n+ f9 k" A 步的连续脉冲信号串。 ! D( j0 `4 y4 M3 X9 U; M0 yfrom a source, through various components, and back7 v! F* H$ J& q# p! N to the s 3 P$ }: D' B! o. _4 SC ) e& S$ C# T! n5 N) R5 j' `4 einterrupts the flow of electricity (current) during fault 7 S! i' f5 d _condition to protect wiring from excess current. Circuit 8 G+ e$ y3 @& x: v/ `* @- a nbreakers are also used as a means to manually6 |1 W& A) `6 y/ ] d3 |$ c% A: t6 a3 a CLEARWAY 1, An area beyond the takeoff end of the * k( `6 U, Z5 R: n4 ~2 zrunway which is c 8 D1 s K c7 m; V8 m0 h* gm $ b4 A3 r0 i& Oc. ?6 F% e' m6 t CLEARWAY 2, A defined rectangular area on the 9 c4 _& y1 ^9 r! a) xground o ) P: I5 }$ o0 N* ya 6 P4 _/ C. b9 y; l* R7 b- ew 6 |- i) |6 H# Vc6 l1 O& ]7 F& V: l. z2 } CLIMB, Phase of flight where the altitude is6 \$ g( F! w! k1 u4 e CLIMB LIMIT WEIGHT, Maximum takeoff weight ba5 j9 K- C8 m7 ~- R# S3 \: j# Z& K, J on a minimum climb gradient with one engine7 s9 l4 Z9 [/ v$ m3 o# r3 l inoperative.$ I1 B+ Q" Z0 @' r" g4 R( `/ R C" W1 y4 |& q& _ Z( v8 A6 w2 M) E synchronization. / L C! I4 w3 g6 y电路, . a/ e- E0 P' H+ C f; `一个闭合的回路。电流由源头流出,经过各个元件流回6 h; E1 v- G& z# T6 f7 P 源头。 * e, Y1 L4 n" [) q. V; q( I, V" E3 ^0 ] n) I- I 能在 . }# `- F5 m: a' P3 v+ [坏的装置。跳开关也可用于人工使系统无效。 3 a8 D( k# E) a6 i一号净空道, 9 t- H7 L% ~ X4 h是跑道起飞端以外,不含任何刚4 S/ m8 m$ `) ], X- ~: B. m2 U" e6 Y( O/ X, @5 ?' W7 Q二号净空道, " K, ]; O# i# V$ N# U' p7 M. I) ^8 a. @, `9 d/ ]! F/ o8 C, v/ w1 b+ N- g 爬升,4 P+ g$ x$ I# v& O 爬升限重,; ?8 J( G# s+ w 取决于由一台发动机工作时的最低爬升梯度的最大起$ [( y# T( m+ G" y 飞重量。 2 m/ m6 p' n% T- E5 q6 b. i: g1 P5 x% K 用于同 / ]/ z3 v) q+ n英汉对照民用航空词典B OEING! P# X7 l6 T+ o TECHNICAL DICTIONARY 31 ) [/ V% |1 G) z1 N+ s9 g8 x; uCOALESCER, A device in the water separator for 1 A$ N+ {: a( J; r; b0 T6 aollecting moisture from the cold air. - H+ M" `+ F" H( Cn antenna with a receiver or transmitter. 8 }4 B, n* p8 P$ yhe cable has an inner conductor and an outer( f! R! X: w! i& L+ B- b* f2 f rounded shield.2 W. I+ ^' w# x1 W5 R ting one inside the ! e/ I0 \* t1 w2 e) I6 Wther for rotating the low and high pressure0 l6 _% t7 P( ]5 l1 ` ompressors by the low and high pressure engine0 X# X# n0 T0 W rbines. b. L+ ]0 E& X; T$ u# n( J8 E, P OMBUSTION CHAMBER, A part of an engine for" V: V, o Q' C7 H* y) h urning fuel in the air supplied by the compressor. $ U3 m% U/ \1 O置。8 u& b9 p6 C t- W, Q' a 射机的电缆。电缆 ' M4 X8 T" g- ?; x中心导体和外层的屏蔽所组成。 7 s/ o- P' B1 a$ z6 B两个套在一起旋转的轴。用于使发动机低压和高压涡轮 ( C1 A; B1 p. D: w别带动低压和高压压气机。 ! Z7 J7 m; B0 @/ z( G* h烧室,5 U" i- x" a' t( W4 [ 发动机的一部分。用来使燃油和压气机所提供的空气相% e$ v% ]2 X0 @. b! [6 v 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 * c! ` f! i1 k% @2 kCOAXIAL CABLE, An electrical cable usually% _' Y9 Q7 B2 z% i connecting a . T% n( Y+ k. [$ B2 P7 FT ( l! ?/ Q2 l: d4 a4 X; _/ Mg 6 d9 L! T4 Z7 _/ B# w" D2 r, B5 LCOAXIAL SHAFT, Two shafts rota$ U$ K( Q) @4 P# N o 6 w9 Q n: J7 b( Q& ^c ( O7 d/ }* Z& R2 t& w; {$ x, C ]tu - |, h4 s5 t; N n7 SC$ ]! C7 A; }9 I8 b# r/ t% ] b& `1 f: d( Z/ B3 z 凝聚器, % s- }2 z/ z/ S; k* m% u: I水分离器内收集冷空气中水份的装 * ^5 @# b4 f+ h* W* V! t2 d/ |同轴电缆, * r1 {% j- V: b& f* i6 ?+ L' T1 w一种通常用来联接天线与接收机或发$ E2 D2 z5 ~, R( ]2 d; `) }+ U8 f 同心轴, ) ]/ V* c: X3 C; m8 a5 ^9 M9 @* G, {& m0 m# y: O% U' A! K/ M: a4 g3 S9 F# ?6 |6 U# {& k 英汉对照民用航空词典B OEING ' _9 P: @7 ~2 VTECHNICAL DICTIONARY 32 4 } H( s* h3 M- K: \1 V4 bCOMMAND BAR, A flight director pitch or roll comman+ l3 n: i3 c8 ]4 f! Q indication. * r; ?1 E0 ~& \7 o) o! Bd1 s f( L& _% ^, W: d. m OMPANY ROUTE, A route flown by the airplane' ?: x; [/ E1 ?' h& k+ i! F OMPASS LOCATOR, A low power, low or medium7 o: c2 Z" k) R) @& W' d9 n equency (L/MF) radio beacon usually installed in 5 D) C: b- f* c+ w' lonjunction with the outer or middle marker of an8 R/ u4 u3 V# B" z tor (LOM), A compass 9 G7 g9 J8 d! G5 s4 R3 D/ jlocator installed in conjunction with the outer+ O* c3 g0 a4 y marker of an instrument landing system. ; e: `) M# J; V5 i1 Gss , I& U1 ?2 j8 n; l7 d* ?- Dle , Q4 T5 B' C+ B* ^1 e( jOMPENSATION, To offset, balance, or counteract. - [% h. T% V6 yOMPENSATOR, A dual capacitor for changing the fuel" U U* J' p1 b4 ` aging circuit capacitance due to changes in fuel5 D* m& }! ^0 f# G) n& `" J. i/ b$ z ensity.. s1 v R3 x( p5 q# ] OMPOSITE MATERIALS, Non-metallic materials used ; M. g P. `+ D' tr airplane construction. Fiberglass, Nomex, Kevlar, " I; S( k7 F( ]! }4 p8 Araphite Epoxy are composite materials. * C, C( S/ V! J0 c0 |* D9 W2 H/ k司航路,+ Y8 y& V- u0 @4 ~( i 在飞行管理计算机数据库内由航空公司飞行; ?5 n0 J. q0 N" \# x 盘定位台,$ } z( z3 v1 g. o3 p# k 与仪表着陆进近系统的远距或中距指点标配套安装的 0 c @7 B9 x+ z9 [( r( C/ K3 j1 b3 @功率、低频、或中频无线电信标装置(低功率NDB台)。 " U% ~7 S+ F! Y) ^7 ]9 L2 x0 G程序中用来导航。6 F; ^4 {# a1 ~1 G* R 1.远台,) A1 P1 l$ I% `; ]0 {- o# u7 l3 ^9 r 与仪表着陆进近系统的远指点标配套安装的罗, K& }: ]+ U& ^2 r2 A" j5 n5 P) | 盘信标台(NDB)。 1 p( p! ^" V0 [" \" D偿, . s9 G! D& g9 Z抵消、平衡、或中和。 ' }$ Z% A8 w: w8 N偿器," X: t. K+ w: `+ ?9 b 在燃油计量电路中,用来改变电路上的电容,以与燃 % D' n3 O D5 x) ^6 u密度改变所引起的电容改变相抗衡的双电容器。1 }. A) F( c& \. `6 [4 u# a) @; d: h 合材料, , G5 E% X& x8 N5 E用于飞机制造的非金属材料。如纤维玻璃,Nomex, . A4 k- L* `4 revlar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 ( \3 ?+ {/ F3 {% P3 `% koperator that is normally stored in the flight 6 z+ T- P9 o p$ ^3 k$ Rmanagement computer's data base. $ e+ O! E; e- Y) mC8 J' a( f, F) H! L: B9 `5 u fr6 u5 K. z4 L0 d c @- P) `# E' v# G$ W instrument landing system (ILS). It can be used for2 D7 e9 ?* a3 \. }4 h$ j# C2 t* K9 g navigation as authorized in the approach procedure.) L1 G q" ? ^5 ?4 W8 \% s 1. Outer Compass Loca : P$ R& _$ p" j( ]% W7 Z2. Middle Compass Locator (LMM), A compa. u& Q# ^3 t0 a2 j$ q) p locator installed in conjunction with the midd% l- n4 B3 _9 \( | X marker of an instrument landing system.! F" N# U7 B/ c7 W; {3 m$ p0 Q$ J$ K C : _$ p0 v5 l; r. ]8 HC 7 G2 \8 f1 O) J& v2 \g , e* G3 {! g6 v9 U# R9 O3 p2 Zd " B! h2 _+ y$ V% c0 IC: D4 ?( r' b" I8 F. w9 E8 _/ ?9 Z fo" p0 s0 G$ a. K( O& m1 O; [2 c* Z0 S7 u g( T S) h/ ~6 m. b 指令杆, ' e8 r" v {1 L! u o/ d飞行指引仪俯仰或坡度的指令显示。 + A! P7 |$ w1 L+ w7 T* a$ p$ O! a* q" J 通常储存 q" `7 ?, k) O5 U) ~; v的航路。 " i7 p1 E0 ^( n! O; O1 L" \# ?3 d: n( r$ x; w* m2 S C; M9 @. ?' h2 y! F# F F经认可后在进近 % _/ K; S% P( L* T4 l2.中台, , u5 V, m4 |8 \' Y" [9 Q, i% k* }与仪表着陆进近系统的中指点标配套安装的罗 $ s5 _7 K1 y" X l盘定位台(NDB)。 8 M$ {0 n6 V7 @! m2 ~% C5 z/ S2 ~6 c" V Q7 d+ g* t. M% e9 P7 ], N) R8 S4 a/ f& r& L( x, V% a4 i1 X! |: }% p K 0 N2 w7 G/ z* O* y/ G英汉对照民用航空词典B OEING0 H' A% e8 @& b TECHNICAL DICTIONARY 33 + q% X4 |' M. G$ B5 w6 E1 V; f1 }by f# n/ N7 F* P6 g9 S* t- m! Xor increasing air - T' @# t# J1 o$ mressure and temperature before the air enters the4 K6 z, x$ Z* k) V7 Y4 S ombustion chamber, Low pressure compressor - front6 h: s3 o5 d4 S7 n5 T ection of compressor, High pressure compressor- rear - j" y" ^6 S6 r" h: MOMPRESSOR STALL, An event that occurs when- c$ b; v% p- v& x6 I ere is a complete stoppage of air or reversal of air flow. F [& j9 H0 S/ b8 t3 E0 X, K COMPRESSOR SURGE, SEE - COMPRESSOR0 K3 ~+ D0 J' u) o STALL COMPUTED AIRSPEED, Indicated airspeed X% u7 i1 u$ S' O5 U3 Y& \% ` corrected for the static source error. 8 u; X) J, O( C8 P- r+ A% @的机械轴来驱+ ~ `* ?) i: }2 X. L ,用来增加吸进空气之压力和温度,以供燃烧室使用。4 H% q6 S4 O5 O( S 压压气机—压气机的前段,高压压气机—压气机的后 5 B6 O/ z7 p4 z* P' q: F$ X4 U5 P) @0 S3 J* t 气机失速,( f- F1 R1 O$ t! r# X* q: d2 c 当气流完全停止或通过压气机时气流方向逆反的一种 4 M. u: o4 ?! d: F" D5 u: @压气机喘振, 9 M% k) S- G' I: O见Compressor Stall , @! U4 Y1 c: a UCOMPRESSOR, A rotating part of an engine driven; a" [7 e( V' M) [ o a mechanical shaft from the turbines f O$ q0 {, s- P' ~ p% \2 N% Y8 L! I c, y$ ~. f: w Y# i$ H+ ? ] s " w* Z( L* E/ \; ksection of compressor./ q3 ^1 d: s9 [ C8 t: _: h! B) P4 S0 W* `4 Z2 P th! P; |, }: c& r- W& N through the compressor.2 F% i W! K7 L% z 压气机, 9 m5 G5 z5 U9 Z- i' q% \发动机内的一个旋转部件。由与涡轮相连0 X& b1 |% U) V: ^, X S: H0 G& [, Y. l- y3 K8 b5 V; W, I' J7 U5 u% a' d# f1 e, L8 m4 v. @' {& S/ S0 c; h( p 现象。/ |3 R# p( M& _1 l( @, l4 w6 u+ g. x计算空速, $ E, [* @2 D) I修正了静态源误差后的指示空速。 ; J+ h1 c ?' r/ _" L2 h8 L |英汉对照民用航空词典B OEING @( k3 ]& j* e* Q5 Y- R5 qTECHNICAL 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 + k; e# w/ j: G. L: v% h, Coperations, manipulates data, and makes decisions. , T8 a7 z+ r- vditioning9 I! E: C& D& t" i: Z, k5 D: P the air and the 2 U/ x1 T5 M! d: E- ?frigerant or moisture vapor is changed into a liquid. 5 _0 m% f1 o3 Rine5 N" H3 Q/ _1 W, @$ Q2 N" f ONFIGURATION, The position of flight controls,3 N: N# ]$ a# b2 [( A( Z missing which " D9 {& x$ y7 `0 g2 Kmay affect the aerodynamic performance of the t/ [/ @$ G, T) [: p airplane. - l/ q7 A5 C: I* ^' t! y置。: {/ R5 v$ x, U: y7 ] 中能使热能散发到空气中,以及使冷冻剂或湿8 ?% |9 e4 W0 I' e' l 转变为液体的部件。5 B& K/ p& T- s# Q( V/ x% s/ E 连接到飞机结构上。: }* ~8 C$ k3 m2 x9 o, v 态,/ k6 l5 C! `( I) P( t 定飞行阶段中,飞行操纵面,起落架等的位置。 6 C) ]2 ?# ~, |1 V; q), * F2 P3 ^$ M# N5 f) G受到影响。 $ g. }8 q# }! z7 cCONDENSER, The component in an air con % Y0 U! ^# m) w8 y, p! |4 J0 Esystem where heat energy is given to . C% r+ x" ~ [% }re ! F0 u( g( @4 T* y3 C- h6 @CONE BOLT, A bolt in the shape of a cone for eng + J0 U' [# K/ M* n- S; Sattachment to the airplane structure. 3 K+ G. O. p# Y5 K8 D8 H. j* j0 ~5 ~$ wC+ D/ t3 B5 t0 _. ^- ~; z1 I& w* } landing gear, etc., for a particular phase of flight, e.g.,# K6 n1 f7 H; T( J$ F2 `9 u Takeoff Configuration, Landing Configuration, etc.) j+ n9 ?* M/ m8 F- R4 m" z4 j CONFIGURATION DEVIATION LIST (CDL), Appendix2 T, M4 ?8 ^6 D7 L" D in the Airplane Flight Manual (AFM) allowing operation% q6 g: S5 Y; r; g$ o! r' w. A of the airplane with certain airframe parts4 n% e# s6 e9 Y) a* J% ]" y 计算机,- P- O9 ], c6 M8 ]/ D 能作算数运算,数据操纵,和决策的装8 E2 ]- H8 M; }' O0 z! u3 S 冷凝器, h4 I' V0 D3 H! m& U* q空调系统6 d% L! A' f; ?9 X5 q) T# U. O; s+ N; K# B# Z9 }' d3 y 锥形螺栓,+ C- _; x8 K3 I; {* x3 o 外形是锥形的螺栓,用以将发动机 % U0 y& J% D, ~2 @$ r/ x' i$ L, a5 M: X在某一特. Z6 l/ z( i+ d( U% K% U 如起飞形态,着陆形态等。 4 k# d P0 b! F) Z* V4 Y: F缺件单(CDL 9 R" Z) d; E' ~4 u飞机飞行手册的附录所开列的飞机上某些零件的清单。$ X& H, a! h1 D ^7 g7 n: Z 在缺少这类零件时,可以飞行但气动性能可能 / g0 j7 u9 O. O* u" v' k0 `英汉对照民用航空词典B OEING: n' |' p+ v% J. E% H TECHNICAL 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) N) c' X# u% H0 R! q+ e! ?2 m9 N component for changing variable engine gearbox speed a) i: i1 V" c8 I$ f8 I1 FONTROL AXES, The three axes of the airplane which3 S& m* R$ b! e* k9 U re perpendicular to each other and pass through the k3 N: Q9 b" e# N# B enter of gravity of the airplane. / s7 P) G. K! P% u4 wPitch axis - Horizontal or lateral axis, passes through' e3 `0 i% W' Q4 W$ q+ U% D" U K& W- D the airplane from one side to the other -6 ^% I, ]$ T$ p$ z- C, l nose up and nose down control is by - ~* W5 A: O+ y; e2 [elevators (and stabilizer for trim)., t# a+ ]: f3 V' U$ }" e Roll axis - Longitudinal axis, passes through the3 R. N, x: W5 X airplane from front to rear - wing up and( U$ ^: U2 ^& t$ |9 J1 T# R wing down control is by ailerons and/ ^6 s) f2 C6 W0 H$ j3 e flight spoilers. " s. u0 x! x- R+ _ l, h9 k" u7 |Yaw axis - Vertical axis, passes through the 7 f2 x' o* {& N- m: ~. n+ G2 Bairplane from top to bottom - left and+ x- G, o+ R r5 V0 g) X right control is by rudder. & t7 O F, y3 R4 ^6 A9 g置,: t( [) O S4 a 制轴, ( ~% p9 y" `2 B f通过飞机重心互相垂直的三个轴。 7 M0 X. l L9 a" [+ k俯仰轴—又称水平轴或横轴。由飞机的一侧通向另4 t# N2 P4 Q6 x: H2 k$ O7 O. U3 H% |9 z 侧。飞机绕此轴转动即造成机首的俯与仰 ' ^1 O: p2 F5 c3 j# ?; e) N俯仰控制是由升降舵来达成的,水平安定( F% M: B. E$ M) m 则为配平之用。 % k7 ]; `0 J& O1 R8 E7 a, {横滚轴—又称纵轴。由飞机的前部通向后部。机翼 4 M" o, d. l* G5 w* G j/ C9 v下运动由副翼和飞行扰流板控制。 ) c) X O. Z0 \偏航轴—又称垂直轴。由机身上方通向下方。飞机 & Q1 j7 z3 J" Z7 Z/ d( ^1 v此轴转动即造成机首之左右运动,此一运 ; m! }2 r& s& f9 N! S4 A由方向舵控制。+ @, D* d4 S7 M7 a) W) t to constant speed to drive the electrical power.4 o2 p( b3 O5 L3 B8 X; e' Q, ^1 { C# r- q+ v! v4 P1 z# J a1 N( ~3 ^# X9 e( K F0 h/ t c 9 c% m, c/ |, _恒速驱动装$ R0 F' u6 e4 |( O! G! f 将发动机齿轮箱的可变转速转变为恒速以驱动电源的0 c, k& K; Y6 a/ l 液压机械式部件。; b# i5 E; @- c" y* ?+ l1 z, {0 l! ?& v7 l+ z/ Z4 A' T+ w4 y6 U- V! f& n. j2 Y6 p" ~2 A; }4 r: z5 v- a Q$ A2 Q* ], A0 U8 R$ b: V- I: Z( G/ c$ J# a6 x2 `0 d6 S0 i) \1 s- m1 ?+ W f英汉对照民用航空词典B OEING 9 b2 u, E3 J! STECHNICAL DICTIONARY 36" Y$ n7 A" \- C5 S/ z( ~: i CONTROL COLUMN, A mechanical component used; Y# w, q/ g! @6 K rs & E6 L, r, A, j% Lnd elevators. $ U9 {$ _! q9 u! R, L& x" y, c& P- mONTROL SURFACE, Moveable panels on wings and) z; }7 i6 u, B- N' K l: ~& A il for movement of airplane on pitch, roll and yaw axes.7 f8 C% H% @$ u3 c( g: b& S. ~4 b% j ONTROL TAB, SEE - BALANCE TAB 8 @- B' Q* E, S) Q* e( ~ONTROL AREA, A controlled airspace extending( F: ?( ^3 ~. ~3 n3 e* ]' { pwards from a specified limit above the earth. . k5 x+ C) k9 p& [ONTROL ZONE, A controlled airspace extending0 t B- W/ _, B" n' e- R+ K pwards from the surface of the earth to a specified 0 r% @! o# \. Rpper limit. ( v4 `1 E. F& z M. V* lis; q1 w* r9 _6 P+ y1 H4 u a( f o IFR flights and to VFR flights in accordance. k9 }- ]& K4 h! y8 A& X) k with the airspace classification.5 h* @/ ~$ ]5 J6 z' u; V 机械部 6 }( F2 C( r9 D: ^; U! A) J5 @) r操纵面, 8 W; G1 n' F% T机翼和机尾上的可动面板,用以操纵飞机俯仰,坡度, 4 A* g9 U. `4 S# _和偏航运动。, ^; e$ i) t x 操纵片,1 @. X' f' u1 ] 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 5 y* w' z/ [5 \ xa4 I9 i: U9 e3 o2 h. {, @% _7 D C. W, N6 G: t7 m' V# C ta+ m' w, W. {( E6 N! J/ f2 u% ] C1 ^' g5 u' x- U5 F7 M' ^( j C; k" @( ^, ^% n u t; z6 d; n0 X: q; SC7 v) b" P! h$ f5 S4 h& J! H u + u/ `: j c; }' \; mu$ u3 W/ }% Z @ CONTROLLED AIRSPACE, An airspace of defined' d X; l5 G/ y6 Y9 V dimensions within which air traffic control service $ d8 n# h4 A3 u# f' n4 e! X: Jprovided t! I' l8 F8 b1 K2 \+ v 驾驶杆, + m7 Y0 t. l* x7 y' |飞行员用来操纵副翼、飞行扰流板和升降舵的 ! b8 K) \+ y* P( C# \/ K/ S X/ a4 X+ v4 n, ^! \' b+ J! i7 b4 w1 U0 V0 [5 a 管制区域,1 p$ n- F1 F2 _, B- T, O 高于地面的指定极限以上的受管制的空域。 : E9 c" n/ B/ M9 l4 Y制范围, - P% ]( i- Q9 Y. R, j; J& `由地面到指定的高度以内的受管制的空域。) ?* t" ]+ L" {$ Y 一个范围明确的空域。在该空域内,仪表飞行规则飞行 / ]" p2 L; }" t* H1 }0 O4 F和目视飞行规则飞行有空中交通管制服务。, a! r- T8 H/ i& _/ _+ Q5 o: o* X, c, o: | 受管制空域,& d) f1 H( P/ b6 Y5 h/ A 英汉对照民用航空词典B OEING0 @# g' W0 }+ u5 T: H TECHNICAL DICTIONARY 376 }) h8 f) v: ` CONVERSION, To change into another form." Y, x8 x5 b1 E; H, I- j COORDINATES, The intersection of lines of reference, % [1 P3 L" T% M7 P: o# usually expressed in degrees/minutes/tenths of minutes - g3 r+ N# ~8 ]) Q1 H/ Yf latitude and longitude, used to determine position or/ `) T2 }$ L, ^* C% X CO 5 W% R# Z$ {1 r/ j. ^destruction of th2 V: m/ E$ T% P8 ~( H0 r chemical conta 7 \9 f9 a2 q8 B1 ~6 O$ J8 lCOWL, A remo 7 s& U L. V! T9 m' p# K/ o9 ffor access to th L; o- U' j2 eFa : V5 o$ M: }. U6 I( hNose Cowl - Front section of the nacelle for air inlet % m7 F! {0 J7 a2 T! I' X/ @to the engine.. ~* x2 A' a& z2 r% L Side Cowl - Cover around the sides of the engine./ B& Q# w& g" x Thrust Reverser Cowl - Cover around the core P: G/ \0 R1 E5 U6 N r6 ? section. & N( t" B6 n( a, l, J+ R7 \Translating Cowl -The moveable outer portion of the ' L1 [9 k6 M; W- y* G6 Pthrust reverser cowl which is 1 L" D* i4 J! [& A' Zoperated during reverse thrust.9 E/ n- o$ ~7 z. R7 N2 r+ T 标,- _9 n& {* c4 U2 o" t3 } 基准线的相交点。一般以经纬度的度/分/十分之一分2 ?5 }6 L. G7 b/ v 读数来确定位置和方位。) v& J. P e$ W5 W$ M3 D 腐蚀: v0 g4 l3 k# {0 T/ `. ~ 动机外部可拆除的罩子。发动机上的构件必须要取下8 o! a1 {# a* S _% }* o 流罩后,才能够到。% W2 ]: F2 v1 i# N9 e# N: L1 Y1 y. A+ i$ }: F2 V 机的短舱的前段。 ' `* `, Z& n5 z# Q侧整流罩一发动机两侧的罩子。 & o. Z* q# R8 q" h( q反推整流罩一发动机主体外的罩子。 p+ i, [5 T1 j9 r- [移动整流罩一反推整流罩外可移动的部份,在反推工+ k. E& B+ i8 g F* b6 L 作时使用。8 |8 p0 S6 q* z; l: A u ( o6 u1 n( d. J% F5 {2 S3 }o : v/ K# a; U0 Mlocation.- n' H% O5 q. D" Y* [ RROSION, A chemical action which causes gradual & R$ f% ?2 f( k R1 re surface of a metal by oxidation or; m8 K; k! F* W. ]( Y5 \- a mination.* l5 S' q( J6 h2 I1 S* N8 L vable cover around the engine sections1 R D! z$ T. t5 x# e8 M( V4 @ { e components on the engine. + _+ B' ^- G- U( }: \; \n Cowl - Cover around the fan section. % m' I. {! W2 V2 G转换, # K* o: e( B$ l5 O6 X9 y- a2 `改换到另一个方式。 ( L5 |3 } l8 j* j( @ D- [* R( v B% r, _# D# v4 u, P7 K, Y* q) h/ g/ M$ x" o0 e# M1 z1 p8 Z5 j7 u5 N* R氧化或化学污染造成金属表面逐渐破坏的化学反应。 ' l3 `. |1 s8 o发动机整流罩, - N% H4 G3 s8 p+ L, |" t7 l9 O; A* o( j2 W% q- P0 K" `5 e7 B" F5 K8 Q( M& K扇整流罩一风扇外围的罩子。 " _7 Q6 O. k8 C- M8 v前整流罩一引导空气进人发动7 _. i! k" G z6 r 英汉对照民用航空词典B OEING2 f5 I6 V, ]6 j- C: e% c TECHNICAL DICTIONARY 38' n; e0 C& i9 B: u/ Q CPU, SEE - CENTRAL PROCESSING UNIT $ q( u {! X3 s0 G7 WCROSS TRACK, At 90 degrees from the desired track 1 F+ v5 \7 g) I: E6 I# x1 Af the airplane. For example, cross track distance is the t6 C5 B- W% l) O5 z( E istance from the desired track measured 90 degrees , I; ^( |- w2 [6 M" |% r$ som the desired track. % `( s" }& [) ^+ KROSS-CHANNEL, Electrical wire(s) connected from ) T2 O5 B+ Q3 a' f$ k/ ^ne system to another like system, for example, FCC' U8 q' I* {6 T& i+ X) W" a " to FCC "B".1 Q6 W/ H/ }9 ^ n adjacent engine or one on the other side.6 ]. J6 d0 ?6 k# D l crossfeed 7 y: S4 V% Z9 V( zanifold for fuel flow from one side of the airplane to the " D" w2 L8 Z- L# Jther side. - I# V3 \! r; v5 {* Wre + }0 C5 \& [" L* uRUISE ALTITUDE, An altitude or flight level7 ^; C2 j: m6 _4 Y( x5 J' b" {# }/ T9 \: M T' P7 xo# S$ j+ X g+ n6 {) \ d& v" R ?8 P1 k, J fr* f# v O1 v$ ?, r- w C ' ~5 P+ ^" f% V6 H8 A8 V [7 t3 A6 Vo$ ^4 N/ y* i8 Y) t( k, _3 U "A; @4 T( l- S. g1 [ CROSSFEED, An interconnection between fuel ; q& [7 D6 C3 Z7 |& H6 hmanifolds for fuel flow from one side of the airplane to % r P' H% x. M" i" N0 e% Aa , s. P3 K1 R' mCROSSFEED VALVE, A valve in the fue% \2 T& E7 }& w m 6 f% c6 |' H) Y6 ho - X; c$ u" L) R( v: X! E0 N$ S' _CRT, SEE - CATHODE RAY TUBE ' v% ]& F/ Z5 P9 [; T( O2 bCRUISE, Phase of flight where altitude and speed a + i" W- A+ w0 I+ r2 e mbasically constant. ' }' n% L9 x" e' G7 R! I# P, U- lC 9 y8 a! }/ A: q5 T! t' Hmaintained during enroute level flight.( J. Z+ Z h; n3 }( R+ n; a! M 中央处理器1 S% j1 \# i0 [. j. ~ 见Central Processing Unit. b+ ^9 g7 c# ^+ J/ S" G 交叉航迹(XTK), 2 ?8 D% F9 j* _3 j1 P; s6 s i9 d与飞机预计航迹成90°角的航迹。例如,交叉航迹距离 & e0 ^- i, ~1 V. Z9 d是用与预计航迹成90°角量取的到预计航迹的距离。 ; x s. g4 R1 t F# A3 }% `/ l* [通道跨接,5 m" S; G$ X- Z3 z 电线由一个系统接到另一个类似系统。例如:由FCC ( I0 \: I- Y( M: G“A” : B( n: B: p$ E/ z$ w接到FCC“B”.* K& p7 F' g6 _0 Y% f. J- X 机身另一侧的发动机。' D/ h, o% x% |% V/ H 于使燃油从飞机的一侧 & Q" z+ y! J; a$ V1 p s. P向另一侧。 * l7 Z& v( m3 O/ |6 [; T见Cathode Ray Tube / Q8 U; Z4 o3 s交输,: G9 h( O3 j+ R: @5 T+ v 燃油支管之间的交连设备。可使燃油从飞机一侧流向邻 ' n, F H! R# w& M1 B近的发动机或在5 P& S4 X( d( e$ k. k* f7 p0 ]* E 交输活门, * q9 _5 i* W5 n S- K' Z燃油交输支管内的一个活门。用# t- d4 }# Z& L8 S) h- W% V/ F9 d, l2 i" R 阴极射线管, ! ^0 ]# |9 ^7 X. . V% ^6 H- @ \3 `2 z! B' i8 G阶段。2 j5 v5 U/ M8 d9 \ 航高度, 5 Z8 T' i5 a1 w5 M$ @9 s& N飞行期间,飞机所保持的高度或飞行高 ( h! F3 A0 i z$ U& A; F* r巡航,& P, O( a/ J$ }& B 飞机的高度和速度基本上没有什么变化的飞行9 a" I- y& l9 E) z0 K3 X+ I6 `9 r8 O* u$ _7 _ 在航线上水平 {" \- U$ E( ~& u$ d3 k x 度层。 4 ^ ^: b/ i+ @: Q9 N) e: x* S' h英汉对照民用航空词典B OEING( a- i b% m4 |4 C! M; p: s6 Q TECHNICAL DICTIONARY 39 ! I/ E, p' N& q) L6 B' f' }* WCSD, SEE - CONSTANT SPEED DRIVE) e' F% i# S6 [$ b* {; B7 E CURE, A chemical change which takes place in a resin $ Z! _$ B: Z4 ?% e2 y3 dand fiber based component causing it to solidify., d! i4 Q3 P0 O CYCLE, A complete series of events that take place ! A7 }: w: E2 c/ b% pgularly normally in a continual sequence.6 U' L5 L) n/ @7 \$ r; I AMPER, A device for slowing down or limiting, I" c! P& n" R h$ j- }, a DASHPOT A mechanical damper for slowing down/ @8 d, K0 d+ y7 d0 f4 R3 P ovement by restricting fluid flow.5 H. F( U) A4 R. n) i, x5 n D2 @0 ^7 [ N7 \1 c7 u2 h! c0 F ATA BASE, Stored information which is used as the ( F8 h& M8 n5 T1 j3 X+ }ba 6 r9 K) _% j7 v7 LDATA BUS, A conductor over which digital data is . 1 v$ [) @5 z9 R- E _7 B( Itransmitted. ( L1 \! ?8 l% y1 O5 E6 M$ J: _5 FDECELERATION, To decrease in velocity.! J6 g, O9 M& z" r! f9 Z 装置,- d. X! P/ `5 l4 I rive # a, U/ T, n7 j7 h3 r2 bre* a4 m# C e. D5 k" Z1 t$ Q3 \# h9 }$ o D . d" P2 B7 O7 h! R4 x" PD ! T9 w6 B% c/ H( Y4 A6 Jmovement.1 C7 L0 j7 c% @% M/ a3 } m , p3 m5 H" N9 g. ^7 \ATA, Another name for information.7 V1 `5 u% g: G; Z0 a; b5 L D : v1 R; t7 d7 T2 C' j# Fsis for computation.- h* P: ^" |1 n 恒速驱动3 R% Q+ U1 y0 ?2 y 见Constant Speed D . ' b$ R% k' p Z" c- Y期,' G* I9 j i1 } G& K 不断重复发生的事件的一个完整系列。 - {' B9 I8 W5 X# q2 p% b8 I0 ]" `尼器, & ]0 f# m. B* w8 S6 I慢的一种机构。1 a" H% _. F5 d- o2 h6 P3 _2 t7 {, o; C; K6 g: c6 z用限制液体流动的方法以减慢物体运动的机械式阻( W8 `3 v' ?5 x" l% N6 I7 o+ a9 h4 P" T8 s! _; q7 M- a1 E. _1 ^, F2 H' C1 {; D$ \ 料的另一名称。4 b. b/ P8 Q1 K! B5 X 据库,6 f4 q3 Z3 Y; _* m: m- }$ F5 F( ? 数据总线, 0 ]- Q3 G1 O7 n6 t* M1 s: m一条或一对导线,用来传输数字信息的通道。2 D9 k. `3 E" H- H- Y3 x 减速,$ Q( m0 g) ?7 }5 A6 R4 S 速度随时间的递减量。9 d. ?4 s+ s3 G/ e5 e' S7 ]1 a 固化, 2 [0 }: o3 j% `' I# ]) P+ [1 c% |1 A树脂和纤维部件内化学反应使之成为固体的变化过程。6 I- w8 r( t- x9 `, u0 D) D" M2 a1 Z9 b2 W: T; d5 F$ t+ f+ K( l2 y/ f o! b& k1 W用来使运动减 . u8 n2 s& R# @0 x5 V5 \' s/ k" L冲器,) e, Q. o: P I. E) s 器。 # v( S- {+ L! _据,7 y4 X7 W8 j1 Q' v. \# O% ?; R. m6 B3 j2 K O- q1 j' S3 T) G" L/ z( F 储存起来以便在计算时使用的资料。 ' W5 U: c, b+ h* M! V# w1 e英汉对照民用航空词典B OEING 2 S( L2 U+ B' t J3 Q$ o" |TECHNICAL DICTIONARY 40' W0 k: Q- }( }! s5 b2 }! Y DECIBEL (db), A unit of gain derived by computing the . N* E# ]% G: A0 X; E' htio of input power to output power. 5 E8 _* z2 h+ |, `ECISION ALTITUDE/HEIGHT (DA/H), A specified 1 m$ X: N/ {/ \4 ^ltitude or height (A/H) in the precision approach at 8 G# C+ l+ i. khich a missed approach must be initiated if the, `6 s, E6 z+ J+ }3 c0 J6 l Q ECISION HEIGHT (DH) 1, With respect to the $ C+ C3 ?9 d, F H+ ^proach or * O6 y; n) H) eexecute a missed approach. % M- T$ g( A0 `: [" n% Wproach to trigger the decision of either . f1 W! _' e- [. o3 T2 wnding or go-around. : O! I: i; `6 p" L2 i# SECOMPRESSION, The loss of internal aircraft air 8 c5 @6 @ T5 l7 |5 Z J# D- e9 uressure. 7 y9 V$ f7 i% e% W3 H2 hE-ENERGIZE, To turn off or cause to not operate. ! H: i$ @ K2 q2 r3 h$ I* b% Jrom the tanks * l% E* c2 H+ P/ {" Fusing airplane fuel pumps or external suction. R6 c" z3 I7 n4 M, T 算的一个增量单位。分贝# Q. L0 T) a+ H, }- u' T 常表示两个声音信号或电力信号在功率或强度方面的 5 t) a7 g1 j6 r3 L1 _5 r' T对差别的单位,相当于两个水平的比率的常用对数的十3 G9 }# p5 z% |" x 断高度/高(DA/H), ; J( u5 A1 G* |+ r7 v在继续进近必需的目视参考没有建立的情况下开始复 & \# F- `# {0 {. Z; w的精密进近中的一个指定高度或高(A/H)。 2 @7 u, W5 m! x. @* [) U断高(DH)1, : d' T9 p, v4 _, }, \7 Y操纵而论,指在使用仪表着陆系统或精密着陆雷1 x. z; z3 k/ `% t 生继续着陆还是复飞决定的高。 E) L& z* u" G( v4 Q1 x 飞机失去内部空气压力。5 l# z( P7 M# b- \* \ 开,, b& {' b' x3 j5 a$ D 关断或使不工作。 : j) x! g( h3 `' u5 x机的油泵或外部的吸油装置将燃油从燃油箱排 ) i( Q4 u) d+ W0 v( M$ A出的方法。0 D3 F ?( p7 T$ I ra: R0 y5 G! o3 Q5 ?8 } D ( l; w0 m: Q$ \2 W8 V6 ca+ p8 v; \" T+ ~/ ~% E w 1 R2 _9 [+ ]2 m# r9 crequired visual reference to continue the approach has # [5 m8 E F; ]5 x: o" g5 Snot been established.. F# ] m4 A" E, g0 W+ T5 ` D / g" K9 t5 p0 P" W2 D: coperation of aircraft, means the height at which a3 O. q4 s( Z! L decision must be made, during an ILS or PAR& Q6 h4 L* }, H9 d8 L7 ~ instrument approach, to either continue the ap' A5 e& P3 |4 q/ p$ G3 m to; U1 e7 X, y$ {6 Z& d4 |' | DECISION HEIGHT (DH) 2, An altitude used during a4 W. s- p8 J' U6 e; R6 ^ precision ap / v6 e4 l( ^3 c+ u2 |* r; r( ola* v5 n8 e( C/ V, E: j; k: R6 | D 0 x9 ^: Y( M" I' Q8 Y# Hp2 I0 |# q% e; P S7 x/ |5 F0 o D% {: R, s' \# B1 T" A/ ]7 U& j; \! }" Y DEFUEL, A method for removing fuel f4 @8 T5 T8 Q6 Z; W3 y8 W 分贝,9 b& l: G9 {0 C: p+ h; v 以输人与输出功率的比率来推7 X' T3 P; S7 j, d$ z' p& ], _$ d# G! n' L6 F% W( |: j+ ~" ]! f! D- L+ n" e: x/ X8 |8 v& p I, t9 t+ K2 y) [; O) K- f S+ G6 M6 z9 r% p0 g4 z$ V7 U- D- u1 M7 P B' Y) K2 T% w+ v" E! V. G3 y* j9 ~* _; j: r就飞机 ) j5 e% |+ h4 g达引导进近时,必须要作出的是继续进近,还是中断进场 2 ~) W n8 q- N* A复飞决定时的高。' l& t0 T) c, n2 ` 决断高(DH)2, : y' K! R5 K2 {( j( }2 e精密进近时产 : C* |8 ?, J; T* @8 N$ }失压, 2 Y) q& t' \: d6 ~8 z" N; G- o/ @! } 排油, 8 ^' ^0 F: n0 U+ `) B6 D+ }. ^# t用飞: C. I. D, Z) _' F6 d 英汉对照民用航空词典B OEING - B# `+ w. Z* [; h2 n$ R$ ]7 X$ ^TECHNICAL DICTIONARY 41* I2 t( _$ H0 u9 e6 A DEFUELING VALVE, A valve in the fuel system for5 K% o3 n; G3 h5 Y efueling the tanks and for transferring fuel between the * G9 \+ c$ v+ P( w2 a' `& T0 |E-ICING, Removing ice after it has formed on aircraft. 4 a: C5 J6 z( C1 K, FChange or difference. o. r: V6 V' f; ]( L: g/ S: ?EPARTURE CONTROL, A function of an approach$ O" a- b v& d/ M$ | ontrol facility providing air traffic control service for $ s6 D" l7 t& H- X/ ?eparting IFR and, under certain conditions, VFR 5 p: J5 ?5 c, vEMODULATION, The process of retrieving information ; a2 o8 E& ]4 \$ h- Rcarrier voltage. + c3 r. z& E: m5 W' ^ation.5 `- a8 s2 i$ F4 C7 o" R3 @ lic% E& ] X+ c. e- }6 ]& ^/ I$ r B creasing hydraulic reservoir air pressure to / M8 L' t( p/ @+ H+ V5 ^0 X& c; Bmbient pressure. 8 Y, m: y/ Z& l7 y$ n7 D7 \箱排油和在燃油箱之间8 t- k& l Y' S; J& r5 M; D2 f 送燃油。 * p' F( d4 \) H: u! w冰,$ o! r( L( }7 n 除去已凝结在飞机上的冰。 ' F2 p; K1 D4 _% O( Z- r% J. E删去或取消。 ' `) i% t) y; X1 ]" L g/ m量,) L2 ~, U8 b3 `1 X0 ^ 变化或差异。 & }3 T+ P; o& V场控制,* t2 a) E9 z" k' X. _ M 给用仪表飞行规则离场,和在某种情况下用目视飞行 k. E' C# D* N! d' ?0 T$ [ 则离场的飞机提供空中交通管制服务的进近管制设施/ ]2 d" l4 G: d6 k6 H1 H$ g0 U& _ R# O$ K3 m9 g 调, & m1 G6 T6 M L8 x: ^电压中获得调制电压的处理过程。3 S+ |! |2 k7 ^+ Y5 o4 R* t+ f; A 环境 2 P1 L/ ^0 p! x. x力相同的活门。 % Z3 k7 U9 [; P0 O' yd3 a; Q% h% H9 w T* k8 l1 g tanks. + n ~( \+ q+ \, Z9 T3 iD& k5 q, K5 r, B r0 M DELETE, To remove or cancel. 4 S( R$ d6 {/ N( mDELTA,; u6 W; C( A1 K& l D M- v5 D( B# [9 w+ m c 9 a) n+ I5 {' k2 x+ H9 Vd; n: {8 S0 B8 T. X* E0 y5 ]( u aircraft.1 M7 B9 F; }4 c9 y D . _7 E0 F/ q4 d0 @* f0 |8 Q. l. T(modulation) voltage from a modulated# i0 ?- B4 I2 g; j) T; m; ?4 B DEMODULATOR, A device or circuit which performs 1 ` b) g8 j# ?) Q& c$ uthe process of demodul! w8 B. ]1 R+ Z, Q. k# [ DEPRESSURIZATION VALVE, A valve in the hydrau 0 B. m7 U/ u( N* C8 v2 M4 F& j( {system for de ' \! T7 x/ m) V0 Qa 0 _, \( ]3 O- `+ F% y排油活门, ! d/ X$ d J N燃油系统中的活门。用以为燃油 1 c% g. E# c) a9 Y8 E' } z. R* V0 X7 f) e! D, |1 ^4 {0 b5 C. X, T8 c r 删除,* {+ }$ b- c' j9 h0 g q1 C( a$ c5 L; `, e% R ?! f, ~" E# ]* g) N7 \" J3 F' `5 V8 R! G& t! `* H8 i! ^. i9 S+ r的一种功能6 x# n( d- F# p ~: {7 [+ Z8 D. C从载波 8 ?1 W% o0 H9 r解调器, 4 z* ~& {) b7 [& ~" L完成解调过程的装置或电路。1 h7 ~3 v) Q# Z# Y* M& c! B3 | 减压阀, 5 A' O b5 J; e$ y1 S在液压系统中,将液压油箱空气压力减至与周围1 C9 D3 W/ I& L4 I. B1 |5 k; u6 G8 Y4 X/ \1 Z: c; O {0 G英汉对照民用航空词典B OEING: T ~. `& ]6 k. |; W TECHNICAL DICTIONARY 42: f! r1 X/ }6 P DESCENT, Phase of flight where altitude is decreasing.: `* M- ]3 Q) @7 ^# r: z3 L8 \+ w ETAILED FLIGHT PLANNING, The calculation of fuel 8 c A8 }" }7 Q5 }0 A" _; |4 N4 @nd required for a trip by considering each phase of0 [# l0 M. {! Y4 d ight (climb, cruise, descent, reserves).7 q# G' Z& Z- j al or" C; e8 U# e; J7 N" k0 r3 E ETENT SOLENOID, An electrical solenoid used for3 G5 {7 O: J- L7 l( h t.. q- @% x7 D7 X# q8 C* g specified course or- Y7 H4 L, Y g3 z8 |# \8 Q+ I& b rocedure. ; U9 s9 J& z# Me. 1 r, Y: K; q4 S- Z& `: V飞行计划,7 m( ?2 H; a7 L8 ^9 c! E 将航班中的每个阶段(如爬升,巡航,下降,备降)都 ' h/ Z. z' Z- ?# p" N人考虑,来计算该航班所需要的燃油量。 / p! A, q4 c& _; o L用来感应情况之正常与否的电气装置。 ) C+ O% Z) U4 r- E; B' q, m2 k定电磁线圈, ) @% [% l# ~4 N- T3 M出接通的电磁线圈。! y# u' |" H! b: V7 d: i 差, + a; Z- y* v9 b* Q与指定的航道或程序之差。9 _! Y- R3 k5 D7 T# Y* \. Q 用气压或液压操作的活门机构中的柔性部件。 1 R* E6 n& |) P9 l6 A0 L" k+ q3 WD 2 R2 b$ k; _# g& {( pa / f0 A* c% _ d! h% D( C+ L+ K! xfl* e$ ?1 Z6 o0 @/ y1 n DETECTOR, An electrical device for sensing norm# A* x r& B3 t, S% J( n0 o abnormal conditions. - o4 N0 d6 D) a* k0 P: cD 4 k! X0 L1 w2 f- m3 bcontrolling the engagement of the actuator outpu. c! b9 E0 o |, L* q5 r DEVIATION, To change from a2 ? d1 x5 A! j/ z; Z' u) s9 N p! P+ `, ?' x9 V5 |+ I+ d L DIAPHRAGM, A flexible part for operating a valve . I& x; t: }, r' Zmechanism by pressur( J" Z/ t3 L2 L: I 下降,5 z; B! p7 ]) z9 Z; g k J 飞机高度不断降低的飞行阶段。 ' e) J% O' k' s8 @* _2 D详细0 R5 \. Z- y' d0 Y' F; i# b: _( R8 j$ Y! n2 c ~2 r 探测器, 8 _. f5 ~1 d4 t1 J6 \( L2 o% P5 o- {( Y7 R 用于控制作动器输 5 [6 n' Y d6 m1 W" P( t9 F) r( G) c 隔膜, . P" u$ o( u8 e6 K/ m6 V! D0 H英汉对照民用航空词典B OEING6 R, E- z: v& W& t TECHNICAL DICTIONARY 439 g o7 g9 L+ I& ~$ @8 j DIELECTRIC, A material which does not conduct 2 q/ m" d; ~( F( zelectricity and used between the plates of a capacitor 3 r c x* y) Z(condenser).4 q/ S) w, \- R# m- C5 E nother pressure in the same system, measured in1 o8 R8 r6 G) |* Z$ D* f& }/ B ounds per square inch differential (psid). 6 b( S l; d, Q* |/ E* bIFFUSER, A part of an engine between the / f7 F4 V; d( Nompressor and combustion chamber for reducing the+ e3 X4 V& W! n$ F& B air pressure. ) a" d# \$ b t! ?igh * }6 i8 K4 d3 m1 y+ j* }pulses. - O5 f+ j) N; [$ P2 |ignal that is a close approximation of the original 7 {6 E- H/ {' jignal. 8 u+ ~2 {' {2 |IHEDRAL, The angle between the wing reference' B" Q( F: U* V- \/ e" K2 H* M' W lane and water line. N: `! |3 I1 `6 V! `) ], _! c. Z# a& O9 f的压力,以每平方英寸+ {, S3 A8 \1 ]3 J' D 少磅压差计算(psid)。 0 _/ u- h. s$ e散器,+ D- s5 w5 U5 p3 ?, O4 c 发动机内压气机和燃烧室间的一个部件,用来降低空 7 l/ }" e, M' l" U/ `9 n增高空气压力。! l+ [0 }" }4 P+ o 换,% q9 h$ n i& P5 l. Y 的连续可 , b4 R4 r1 H) P+ A(模拟)信号的处理过程。, z4 F% s0 K; o. G0 m" L 反角, 2 M) q0 M! H7 j/ i! p0 b机翼基准面与水线之间的夹角。) B+ j* U w% i5 |6 _1 o) X DIFFERENTIAL PRESSURE, Pressure relative to * n- O5 m0 Q- va $ i# o! I/ m {p# \" y5 x+ |% P" M+ A6 b D7 @* i6 `6 T! m* y4 Z2 G1 ]; ^ c( I' O5 n& e$ z7 Z( W5 [0 t airflow speed and increasing the ! O" U! i: M" g9 p( X/ _DIGITAL, Digital refers to a signal whose amplitude- _- R- C9 j5 j( _- E remains constant for a finite period of time. Digital ; F, R3 R$ o4 [" {signals are commonly represented as a series of h4 r. @2 F" k0 d. l and low & E! }( i- j( ]( ~7 f- tDIGITAL-TO-ANALOG, The process of converting a: {9 t1 M1 }) `8 |% O+ t: C( D4 Y digital signal (binary) to a continuously variable (analog) ; Q2 ^* T, `+ U2 s! ?s' U# R& X. r$ f! A s . M& [ s) N% @& {: |3 gD 5 E6 Q# O+ c2 ip % W- [, S- P8 c3 a, s1 q电介质, 2 }* g4 g' B' v$ t& I一种用于电容器板之间的不导电的材料。 5 c0 m ?0 m, |* k压差, B* n4 A; Y1 H0 j: ~6 n* @相对于同一系统内另一个压力 1 ]: U8 p/ o' }+ f7 A3 C! w* v3 Z9 L# n0 f* J5 |' l: N* ?气流速并% x" v9 ^, _$ Q6 d6 f 数字式,% G& l5 X. N$ i$ ]! I/ E* J: }6 I 指一种信号。该信号在一定的时间内,振幅保持不变。; {3 M4 J3 ?2 B# V# j 通常由一系列的高低脉冲表示。 ; Q: H# Y8 \8 o( r# \数一模转 V4 E( W. J% N将数字信号(二进制)转换成与原信号相似 0 I% e, E3 H* B: S( ` b& |' {; H) A h: ]6 W3 H+ }7 X: i% X* r' J& W: u: L 英汉对照民用航空词典B OEING( O, N" u& g, O K! S3 C TECHNICAL DICTIONARY 44 0 r ~/ z/ Z: F3 {" k; Z# ~DILUTER DEMAND REGULATOR, A component in the# }" q) |6 K r# x, Q crew oxygen system which mixes air and oxygen and 2 Z! z" e0 N) Qupplies constant oxygen pressure even if there are9 J0 _- ^1 h: ?9 S4 d, V hanges in ambient cockpit pressure.! p1 ?9 l# Y$ h5 t; u/ t0 r IM, A word value of light. For light control devices - dim + v8 j- u1 C# z/ U5 l6 g( lthe opposite of bright. # i4 |( g" z/ R7 ]. f" u' B6 HIODE, A device which allows electronic current to flow* w s5 g0 H4 B& F; E) s- J only one direction - u3 `' m) F. o3 V: J1 }( yuid in a reservoir. , `" _0 F g% h2 f/ f6 `DIRECT, Straight line flight between two navigational; B" P# c6 L3 w; t aids, fixes, points or any combination thereof. When ! F" x# ^9 O/ C; ?4 hused by pilots in describing off-airway routes, points* g# ` w7 R1 f8 y( S defining direct route segments become compulsory 1 i2 f0 u1 Z% y5 q/ x+ M6 W/ preporting points unless the aircraft is under radar; x3 P( P3 K# N3 r Y control.0 E; k' t/ W! E9 t7 m/ c 节器,) j1 ?- S3 ?; s; B7 T 将空气和氧气混合, 8 Y: P1 t0 @1 r% Q: }使驾驶舱环境压力改变,它也能提供恒定的氧气压力。 , |& k1 e& g+ y' V( s o: j7 O) \) F% [7 ? 一个形容光线亮度的词。对于灯光控制装置,暗的反 , m/ m3 ? W/ D' x' R9 G6 w词是亮。: Y3 _& s/ u+ l8 i; W 极管, 6 k- y( M o, ]$ |7 R2 C只允许电流向一个方向流动的电子装置。7 D+ I' e+ c6 ^! _$ ^- ?# Q 器内液体的量。* B) ?/ K5 ~. k' } 直飞, 2 K& n( f8 i& V" g两个导航台,定位点,导航点,或任何的组合之间的直 + q& v) L2 B! j- u6 v+ \) W线飞行。在被飞行员用于描述偏置航路时,除了在雷达控 / c4 l. c' E9 t- a& R; c9 ?, I" d1 p制的情况下,确定直线航段的导航点成为必报点。 6 `9 Q; v+ H3 C) Z5 K ?3 h* xs9 k! k5 o$ y* Z @8 r0 D3 ~ c! g# P: v- r# q- A; F D ( B Z t0 Y" |0 tis& Y$ u2 D" F1 ]; ~+ _. ~ D # s4 |/ ?) L) _! e9 \5 ain- b, u) y- F2 i m3 T$ p DIPSTICK, A calibrated rod or stick for measuring a 3 C3 ~# _" q$ h( G/ Mquantity of fl6 K9 w9 R, W6 G; c2 y 稀释氧调: q* u- F; l. s5 N( ^, M/ O( R 驾驶舱氧气系统中的一个部件,它 & `5 |7 o- I5 a. A1 M2 _$ c$ w# A( `( D0 C9 T7 [+ l' B- |1 D, ?! X: n! m- G0 B6 Z4 {2 c* t- }1 t量尺,$ y5 R% ~4 Y2 f( P" `9 b: E 校准过的棒或尺,用于测定蓄液. L. _5 R" t( Y 英汉对照民用航空词典B OEING ' U0 L% ~* `6 B# r7 pTECHNICAL DICTIONARY 45

使用道具 举报

您需要登录后才可以回帖 登录 | 注册


Archiver|航空论坛 ( 渝ICP备10008336号 )

GMT+8, 2024-11-22 04:13 , Processed in 0.056003 second(s), 9 queries .

Powered by Discuz! X2

© 2001-2011 MinHang.CC.

回顶部