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英汉对照民用航空词典 [复制链接]

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发表于 2008-12-24 21:35:01 |只看该作者 |倒序浏览
英汉对照 ) a8 V$ X' r! m( u) f( k3 Y" j民用航空词典 4 c7 i3 V7 v; r, }( y5 ?波音商用飞机集团 7 d) ], u3 L; ^0 ]) G* k% m CBOEING COMMERCIAL AIRPLANE GROUP ! V4 W, ]$ U7 E; y# C( l- |英汉对照民用航空词典B OEING2 Z2 G: h+ M9 A2 s- x8 G% R TECHNICAL DICTIONARY 1 : f) p: C+ h8 w/ Y8 dA+ x2 v p" J1 h5 L# N3 O8 @9 y ABEAM (ABM), Beside: An aircraft is abeam a station- u/ Y U) x3 ] when that station is 90° to the right or left of the track of' l0 ^6 k8 |* C( Y$ d6 Y; t4 ] the aircraft.0 o: E% j( ] m3 G+ w ABSOLUTE ALTITUDE, The actual distance the aircraft- z/ U; n6 U; h is above the ground. . o7 t- C4 Y+ d0 IABSOLUTE PRESSURE, Pressure of a liquid or gas 4 S1 |4 A4 f0 @measured relative to a vacuum.( k$ \# n& ]+ q% c( s ACARS, SEE - AIRCRAFT (OR ARINC) REPORTING& Z/ D; i- ^1 p) q, L# _9 v5 z. w ADDRESSING AND COMMUNICATION SYSTEM5 v6 [+ M2 h3 ?6 u+ d7 I, }2 C ACCELERATION, The rate of change in velocity with+ M* q/ T* W* M* N8 V @3 N# i respect to time. 4 T& x7 H7 i; i! b, [. z7 G( ZACCESSORY GEARBOX, A part of the engine,( V0 B5 C- w7 U9 z* I1 V mechanically driven by a compressor or an angle- }, H9 ?' R" F/ u7 t gearbox, for driving components necessary for engine ' G" }! R5 i9 W7 _( {正切, 4 c* a# q. f* ]! u1 { wand airplane operations.# v) b8 q" I# W4 h0 _/ L, Z 当电台在飞机左侧或右侧方与航迹成90 度时,飞机正 . b6 z4 N2 n! x2 o切电台。 # Q0 r% r- h& J a绝对高度, r, A5 A+ b2 R. D) c 飞机离地面的实际距离。 8 S7 D' L; V6 u+ n0 V绝对压力, 5 g1 r, P7 C( M/ @相对于真空(无压力)测得的液体或气体的压力。( H$ Q0 { t+ G9 N 飞机通信寻址和报告系统, ) @2 N' K+ L0 ?8 L: Z见Aircraft(or ARINC)Reporting Addressing and/ ]8 j- D) y! N Communication System.: f3 a5 N( N5 e! {9 X! D 加速度, 7 s4 v/ T0 z& ^随时间变化的速度改变率。 4 a) L( o0 Y- W0 j1 m) P附件齿轮箱, 7 k7 {: O/ ^ l @发动机的一部份,由压气机或伞齿轮箱带动,用来驱动 . b* I( H4 C4 m- X9 T$ s5 f* V一些使发动机和飞机工作的部件% t5 B- r7 t) W9 w 英汉对照民用航空词典B OEING a+ d! c" z! L. X: S0 [5 r& } TECHNICAL DICTIONARY 25 H* V3 V2 V# z ACCUMULATOR (NO. 1), A container with hydraulic . C! h% O# q5 x R( @ts when normal hydraulic supply is not5 H, ?! \' V# _/ i J) N vailable.- R2 G7 k$ p4 O" K0 _$ P CCUMULATOR (NO. 2), In a computer, a special0 f$ k; D/ E$ B2 n& P4 ^1 q torage register associated with the arithmetic logic unit, : x X5 E/ h5 Y6 G' xolding the results of a computation or data# @' v( `+ v0 Q5 }5 b( ^ ACTUATOR, A mechanical device operated electrically,1 f0 Y; z0 o% i( ^. I0 H hydraulically, pneumatically or mechanically for8 c- S7 w2 I7 ?* ]. U8 ^ transmitting motion between components.. {: K# Q5 p7 w ADC, SEE - AIR DATA COMPUTER ; i3 U5 z5 q5 c( ~2 kADF, SEE - AUTOMATIC DIRECTION FINDER: p" q" o. {1 a0 N ADI, Attitude Direction Indicator, An electronic display of 4 C6 l3 g: L- aairplane attitude information in pitch and roll.# ~# J8 j& c8 ?, l Z1 o 蓄压器(NO.1), ( t# {! o- }) _: v含有靠干燥空气或氮气增压的液压油的容器。当没有正 1 E5 ], ^0 W) x4 b常的液压源可用时,该容器可用以驱动部件。 $ J1 q+ X0 m+ B" ~存储器(NO.2),4 C% m& l7 w- D3 R 计算机中,一种与算术逻辑组件有关系的特别存储寄存 " }: e1 f, T: t; z器,用来存放运算结果或数据传输。 0 v* }2 Y2 I7 b- J' H% R- n. B飞机状态监控系统, a; n; o/ T: p% h1 n. C n 见Aircraft Condition Monitoring System 5 g0 K1 v" c+ I$ o7 wfluid pressurized by dry air or nitrogen for operation of- G; O& ~% v, b1 i7 o: [4 _ componen 7 z1 o w4 d/ ?# m& r/ R+ xa , R' s. M* q" g% K/ k! H5 NA 0 w4 B3 ~ L. d8 M" J( [s 8 f" Q$ x+ C( R6 |2 A% C3 xused for h 3 j# ?+ s5 L0 p$ V* I. Ktransfer. . m& ]+ b' c# @8 W5 D# IACMS, SEE - AIRCRAFT CONDITION MONITORING2 K i$ t, x6 A+ R u2 C6 b5 [: i SYSTEM . ' ~, y' [: A7 d" M: d; X1 N0 R作动筒, 7 V w7 k' q4 \3 n, U由电,液压,气源或机械驱动的机械装置,用于传送部) V% i1 D) g# a! j 件之间的运动。1 a4 E$ ]( W- \0 c7 W P: c 大气数据计算机, 4 h' n- P3 u, J; P见Air Data Computer.9 C# I6 Q) S5 c- M! I 自动定向仪, / s( P! \, [4 y$ s( n见Automatic Direction Finder.6 r- Y! w' D q2 z9 j. v 姿态指引仪,% t# R& |+ ^: S, H 用来显示飞机的俯仰姿态和坡度的电子显示。% C3 R! L1 R' n' ~4 g 英汉对照民用航空词典B OEING 4 v: p. j' A5 a6 U5 zTECHNICAL DICTIONARY 3 & a. l" r: V# ~. G/ lAERONAUTICAL RADIO INCORPORATED, ARINC is7 L8 b4 t. K6 t: R4 t6 Y% ^ ,; m2 t# J& x C ^8 P7 p4 w7 d$ z6 ^ nufacturers, and foreign flag airlines. ARINC ( y% t) I$ D8 Z$ `& Revelops and publishes standards for electronic" E' [) `& r9 f4 ^ quipment and systems.+ A- ], R! O, V' T7 h GILITY TUNING, The capability of the DME to 3 U7 e$ ]" m8 Elternately tune between two different DME stations in / I6 ] Y7 d) G( P% O! t1 yrder to get two distance readings from one ! N# u3 f/ Z" l: l. Y! z3 uterrogator.! o+ _' z9 y; R+ T6 _$ G ge Q e1 ?* Y8 G/ |8 k" r- o2 ` ILERON FORCE LIMITER, An electro-mechanical( {9 I. Y/ u" o% e! d$ x5 \ IR CLEANER, A component in the pneumatic system6 r+ i- r$ ^. Y3 U5 M upply to the air; I. z- p; }8 K4 F! P& s! _9 c' k8 V onditioning system. ' ~1 q9 g4 u. F" `1 ?订并出版 . x! F4 B/ D4 P, F子设备和系统的规范。( G1 A9 O4 Z* Z* D/ B 快速调谐,/ f3 W5 I; K; {& ]) A' f" x1 ?* V 机载DME通过交替调谐两部地面DME电台以测得来自 / ?' _) U4 [& t( ~3 n6 ]. K同一台询问机的两个距离数据的能力。 - ~7 p. q- W) c4 H# b翼操纵力限制器,3 T: ?' O. F2 k0 A# E- q& X. v 装置。在自动驾驶工作期间,用来限制驾驶盘 $ J/ @" D; b$ z* b/ O: E气清洁器,0 o) }( `/ ?9 o) ?9 n, d8 z& R 部件。用于去除供空调系统使用的发 $ z; p) u3 ?7 b. h$ Z6 ~a corporation whose principal stockholders are United 9 l- W E0 i- c& Q' s) jStates scheduled airlines, air transport companies; {6 J- u6 u( z6 U/ p aircraft ma" Q2 [2 U9 T: M5 N9 O7 q0 X d 8 e) g. B& x$ N8 O* d( oe 5 R f, }8 G* vA 8 ~9 H; h, C( c3 w( ha v- w; T* O/ @$ C) lo C3 F/ t# z; F( y% u7 nin! R4 [$ B6 l7 b; U4 \: J! V AILERON, A hinged moveable part on the trailing ed. Z- J! J2 l& O- E0 [2 ], T: ~+ { of each wing for airplane roll (wing up and wing down)) N* O& {' |% Q; w0 `2 n control.: O+ ~' G/ M) i) q0 ?6 k A ' B8 |$ p. O: Z1 x; ddevice for limiting the control wheel movement by the9 N; h) x. _: U' U7 ] autopilot during autopilot operation. 3 K+ X4 |" }4 h# x; ? Y- x XA5 J3 D0 S. \6 A/ w+ e for removing dirt from the engine air s/ z0 s8 i: g- r c* G6 ~1 d' M" Q# @' | 航空无线电公司,6 Q0 k8 k+ k8 K8 ` 主要股东为美国定期的航空公司、航空运输公司、飞机 ' }* ~! w% a; }- E; E" q) z制造厂和外国领队航空公司的组织。其目的是制 0 L$ O7 y& p& K3 ]3 H/ l$ Z/ g: b2 \" J. F副翼, ; ^. I; ?6 n% L7 u铰连在每个机翼后缘的可动部件,用于控制飞机的滚转 % \- J3 N% N0 T6 v0 I(机翼向上和向下)。 9 I8 {/ H8 H: j& B5 q) Q* o% e0 a; i. {# j: v, W/ `一种机电0 W' B ^3 T6 a3 D8 S 的动作量。0 f- v1 V6 ?9 v& m+ S. N1 R$ w" |* M q6 ~3 ]( H! E1 @ 气源系统里的一个 + z! k; M5 `/ V7 t7 w; P动机引气中的灰尘。9 V( _0 `7 S4 o/ z( o* e! s 英汉对照民用航空词典B OEING 8 P& o" a, M9 t" o/ m/ ?TECHNICAL DICTIONARY 4 ) g. o, Z8 G# A4 ZAIRPORT ELEVATION/FIELD ELEVATION, The! |8 F6 i0 v- [2 a' E, { highest point of an airport's usable runways measured 1 g# n, b& F) n. J2 f) s0 oin feet from mean sea level. In a few countries, the7 h. F, @! C* N; F" S& f V. V airport elevation is determined at the airport reference- u4 t1 ^' Y% t/ W0 O point.2 { v; U5 p: {1 L4 `$ D0 q AIR ROUTE TRAFFIC CONTROL CENTER (ARTCC),: B2 s/ A' I% ?* o( h" t ervice- F( j8 x+ P a. r' C ase of 0 B0 R( E, P$ b; b( qus flow of air traffic. 0 V, k% ^' o `0 d2 `IR CYCLE MACHINE, A compressor and turbine on a% M& \$ p: q- @- f& P K; s ommon shaft for cooling the air in an air conditioning : z) ^; P3 C$ M, hystem. The air is cooled by expansion from high to low4 N% o2 ]- I6 e' x& F4 C. m+ P ressure across the turbine. The compressor is driven 7 Z) B* @! h1 P# r' i, B, O7 jy the turbine., { q! {, T A7 e! x( G5 S 中航路交通管制中心(ARTCC), 2 b% c+ S8 l F7 W/ o3 f域范围内使用仪表飞行规则飞行的飞机提0 L* t R* K; H; [ 管制(ATC), ) U" o! U+ b1 ~ l4 x8 W3 G涡轮冷却器, # N. `! ^7 V% K0 E/ S U是装在同一的压气机和涡轮,用于冷却空调系2 H& V+ z. x2 P) d' \) d6 Z 统中的空气。气经压气机压缩后,由热交换器移去热量, * j3 C* X! r- r1 i然后经过涡轮令涡轮带动压气机。通过涡轮之空气,温* y; T# z" [' D7 Y* {: A& j# Y 度下降。 8 \; q$ s9 q! z9 f% ~: }A facility established to provide air traffic control s - L" {0 c7 C) [; ?& k( f/ ?$ xto aircraft operating on IFR flight plans within controlled! F+ p( ?) P2 I; H" |9 D, @ airspace and principally during the enroute ph" u0 ]4 ^ P# H$ j. \& y flight.# o7 a: a! s7 l$ v8 g$ e/ @ AIR TRAFFIC CONTROL (ATC), A service operated by( N$ {$ c! d O appropriate authority to promote the safe, orderly and) G6 i; D8 ` f2 Q9 u, s expeditio 8 D/ t% D1 E0 }/ v. m8 R. IA [$ a% `" t) v% ?' X* p1 Dc + u8 j# ]: y: M( k5 K7 z6 F% Hs# r; P: o& Q4 X5 T f p+ F: X/ n9 S; a E6 R9 r- u4 v b ; f( K: R# o c2 C4 G机场标高,, C% Z! Z1 w$ D0 H; u* v& a0 k 指海平面与机场可用跑道最高点之间的距离,单位是英) _& R9 H- ~* d* ?4 Z 尺。有几个国家的机场标高是由机场基准点而决定的。 ; L9 u5 a3 i# d# @1 m" t* @0 X, S1 z% s/ ~, P5 J" h 给在控制空% {9 z1 u3 }4 } 供空中交通管制服务的站台。% q2 u# S7 c8 D2 f" U0 x 空中交通 , ]" v, U9 @2 Y& M6 @9 f由有关当局管理,旨在促进安全,秩序,和效率的空中 . v) N3 n5 n) M1 t9 G交通服务。 $ p$ H; M3 X! R5 k根转轴上 4 y7 k+ J; `6 F# l% k( C/ w$ v6 f' ` m Z5 }1 J3 R& |" B' q2 w/ o8 N6 P) u! X英汉对照民用航空词典B OEING# u0 x) w- F2 }, `) b+ F TECHNICAL DICTIONARY 5

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发表于 2008-12-24 21:36:52 |只看该作者
AIR DATA COMPUTER, A computer which produc3 ]* m X! E7 G& G5 B data information, such as altitude and airspeed, based ( L6 n% W N0 _* Y6 I( yon pressure and temperature measurements.# f8 Z6 k( g$ s, F$ Y8 K3 h3 Z es air3 E6 L: B+ C) H" C" {, {# N- m IR TRAFFIC CONTROL, A system comprised of# ], G$ F8 J6 o; F: e$ c8 ?- k9 L round and airborne components used to identify, track5 g1 o$ s4 X" Q' m OUND SENSOR, An electrical device operated 8 g6 k/ L' n# S: o% ny the landing gear, which transmits on ground/in air O# d. G: p5 b, C$ P formation for system operation in flight or on the 2 Z5 f# a4 p; ]0 N8 Around. 7 |; [* ~" ~8 S' v- `8 E5 hIRBORNE VIBRATION MONITOR, The AVM takes 1 _, l+ R2 Y1 K Q: d4 Ne signal from the engine mounted accelerometer and& _/ i9 F" y8 t6 E" ?% ~- D alculates the vibration on that engine.- ^7 G! V) U0 k o I4 O- ^ corridor equipped with radio navigation 6 |+ E* f: B8 a. F6 Xaids.9 {: a0 A9 e2 @ @ AIRCRAFT (or ARINC) COMMUNICATIONS0 @6 Z' ^9 ]! f; T ADDRESSING AND REPORTING SYSTEM, An 8 M7 @: Q! T: X) ]2 Waddressable digital data link system which permits the 7 H6 ~; _0 W7 g4 M5 }) B) Q, @exchange of data and messages between an aircraft . A8 d( P" f% a [) {3 yand a ground-based operations center over a radio " m W0 Z" z. M; ]network.1 c; T$ x' h/ | AIRCRAFT CONDITION MONITORING SYSTEM, A e! s% R" g1 l% A* }$ k+ Csystem of sensors and recorders to monitor various* |9 `2 ^7 ?7 ^: Y6 ?# ?4 p airplane systems' performance and status. ; G3 Y& Y) M2 b( W% _$ J m2 E机, " {: h: G7 ]( U, r* o* g" q0 @中交通管制, 7 z. n6 S# e9 B( M2 o" G一个由地面设备和机载设备组成的系统。用来对飞机进 . P1 u+ A' j. J( [4 C地传感器, 8 P7 B$ Y" ~$ O' B3 c% R一个由起落架操作的电气装置。用于给空中或地面的飞% @3 w- I7 e! L- c- |3 g 系统运作传输地面/空中信息。(有些系统只能在地面 H5 X# q1 M, a7 c 用): r* S0 M4 c( N5 b1 q 载振动监测器(AVM), 7 m3 |6 o- \. L. n: E+ ]9 VAVM从装在发动机上的加速器取得信号后计算出该发 4 T3 K8 \* D) R机上的振动。1 }% f9 W' f7 Y0 B 式建立的控制区域,内有无线电导航设备。. F& O& W( U) z$ d. B 飞机通讯寻址和报告系统,* B4 l3 |% n5 }. X- P 有种可寻址的数据通讯系统。利用该系统可使飞机与地) y. A: [! M8 g1 o# } 面操作中心通过无线电网络进行数据和信息的交换。 # m4 A L h, ]3 z飞机状态监控系统, - p' X V8 J8 g: Q: \3 c: J# W4 ?一个利用传感器和记录仪对各种飞机系统的性能以及 1 o# [: c! i1 M: r- Y/ E4 i, I状态进行监控的系统。9 K/ v1 G3 b) N+ i A& A" a& t% a8 K g ' A2 P+ g W: l7 @8 b; iand locate aircraft. ; I8 g, H. R: PAIR/GR : ?$ L0 f6 r+ X$ U, ]b % p. r! E% }% z+ y) M) h. y/ f7 zin ! c0 g' [9 M' b r$ ^5 eg, m3 [& u1 v' H& t+ f+ r# U! a9 J A) \9 a! @% u& ]. |1 v th $ T2 i, t* c4 `6 Ec 7 q+ J4 e$ H0 |! j- P- `AIR WAY, A control area or portion thereof established 7 I1 q! Z. l$ g$ Z B3 }in the form of a A+ ?$ [) g! I8 `5 y+ R' t2 h& m0 ~大气数据计算 3 m' b5 G: f: x: T根据量取压力和温度而产生大气数据资料(高度、空速 , w/ b+ T5 K0 v, M3 M等)的计算机。 3 a8 b' _/ K, y8 ~8 P( @6 D+ s+ V3 E4 m3 O行识别,跟踪和定位。# [ l! ~( _, z1 {0 ?2 o& t6 x/ F+ Y% P0 j# e: t& j6 s6 Z1 o% `/ b5 B0 X 使7 _: @/ H. z; w0 ]* P7 R5 }, P8 P5 |7 e3 C4 y" T# U" A 航线, # t0 j: ~! A' k0 Q以走廊形 & q1 G, O4 l, T! i& ]英汉对照民用航空词典B OEING( c) d1 i- o4 C3 O( g TECHNICAL DICTIONARY 6 9 w% f/ V% p% UAIRFOIL, A surface designed to obtain a useful reaction,$ L0 g: W7 d' ]% ^: e g such as lift, from the air through which it moves. Wings, / _, l$ b: v) \/ P' wstabilizers and control surfaces are airfoils. $ {* y$ C, `5 Z& `AIRSPEED (IDS, TDS), The speed of the airplane3 a# m' Z5 |$ r( m/ H rough the air. ! r# M3 K7 M' o+ N" j5 t5 xD INDEX, An adjustable pointer on the & X Q; `/ L: t, wirspeed indicator. $ r5 ]5 X8 u' {' R/ A! _and legal ability6 c' z" g. \' r& E/ J0 ^( C: Q fly. + A, [. W0 c& o9 C& u5 [+ Lm, for example, the procedure for finding the 3 y" q7 x0 f6 I8 p! E% bquare root of a number.& O. e* N% d; v- E7 ?8 D+ e& I; E y+ b: `6 C0 q" R3 c( l" L re, wind,8 R4 d" |3 T- ]6 ?4 x, D and aircraft flap setting. - R! v |% A3 y是翼面。% v& s5 D3 d, Y; @# j 速, ; t; v" P5 {& ^" s) u, C飞机在空气中运动的速度。 . p" k! _, _' p, v. x5 @1 W7 S在空速表上可以调整的指针。2 d/ r, [$ @* p4 q0 p1 I 机械飞行能力、和合法性的飞机状态。, _* y3 t+ n0 M, Q# Q, {: B% t 一步一步的解题方法。例如,计算一个数的平方根的步 / k8 s" E3 ~8 f5 h- F( [# q3 Y+ y. I% D0 C% P" r9 X. R+ [) T; W+ f; X& U" C资料的法定文件。 ! S8 w+ c* v; ?; [3 w翼位置成函数关系。9 u$ S) A9 l! R3 Y0 I% [ th 5 Z; r& G; O& {0 j. G% XAIRSPEE$ f/ Y: x. w& [6 i2 v+ T) R a6 N% p0 @9 u4 y6 @ AIRWORTHINESS, The condition of the aircraft with }( Y1 L7 P/ q% [respect to its aerodynamic, mechanical, ( z" m" c, A4 T( n3 o4 \to( @, j Q6 B, w( \) R9 X0 y ALGORITHM, A step-by-step procedure for solving a + O% p# t, J8 l0 m3 n; }proble 9 V2 I8 x9 D# w( n# w# ?s/ ^+ W$ S. Y1 N- ?, B AIRPLANE FLIGHT MANUAL (AFM), The legal8 R) |/ a+ ~, e1 V6 z) E document containing performance and operating limits,! b3 N1 M# {$ g# J. `/ e! E2 k operating procedures, and takeoff and landing * G& k3 ~% J6 iperformance. ) o( q: `2 d9 a$ {7 F3 s8 JAIRPORT ANALYSIS, A comprehensive set of takeoff * x+ ^4 a* W7 {! e; ~& n( p7 Q8 Sweight limitations for a given airport runway, generall ! ~; [( p2 X K3 L3 jpresented as a function of airport temperatu ( D k# i' t2 C( |" d翼面, . V; W5 j3 s$ ^, T8 c4 ~0 y7 `用以从气流中获得反作用力(如升力)的表面。机翼,2 R9 X% L! d1 Y4 d 安定面和操纵面都 2 _' T0 I9 I; I# X6 t7 J; i7 T( X9 A8 q1 m& X- h* g# A9 G空速指标& S) i: |# T# T3 J) E5 ?( r 适航性,6 t) n- M+ @3 Y: q M1 a: G5 a 有关气动能力、 3 `' t9 S0 f' ^7 }/ t; W1 d/ Y' X$ p演算法,2 h K6 B5 L3 a) m( A: ?7 }5 ~5 X. e7 Y( L; t0 ~0 V W 飞机飞行手册(AFM),4 z$ B! {9 y d 包合性能极限,操作极限,操作程序,起飞和着陆性 , Q4 y; f* G3 R4 G& \6 U# T1 m3 a! g7 g' B( t机场分析, e* Q$ J6 X! J) C一套针对给定的机场跑道的详细重量限制资料。通常与1 ~( Y8 `4 B* _; i S6 q* Q8 v 机场温度、风、和飞机襟$ X3 g8 L" I8 a% j6 [; e 英汉对照民用航空词典B OEING 5 g# z* P$ @- h. u$ q$ K* MTECHNICAL DICTIONARY 7# U* K: [- m) H' e4 |, f, I AIRSPEED BUGS, Adjustable pointers on the airspeed& |+ v' L8 o$ E indicator.! [( p$ }/ f) _0 q" e ALLOY, A mixture of a basic metal and small amounts 8 p8 V% Y& ^& ?6 ]% yf other metals to change the properties of the basic ; ?% G; r" u* x1 g h& ~# `$ Aetal.7 P" `+ D3 l( l$ c' i Minimum airplane speed. 2 T' @1 S! Y% Q( I9 o" t5 y( Ne of5 Q5 b; E* n) C) ]. D5 C3 G itting airplane angle relative to2 W; B! R& T! s, a; Y/ R irstream for the stall warning system.. E' b) Z( a- b8 P/ @ another.; O* x+ x( Q& t% L& ]' r LTERNATE , An additional airport selected during $ _0 ~6 @5 b9 B* Z9 s5 O) B3 a0 v' ?8 Q8 F合金, * s6 H$ N% U$ w/ t在金属中加人少量其他金属,而改变其性质的一种金属 . l! j6 F# @! Y6 k q9 W( n合物。 ! y1 O4 s7 }% ~3 k飞机的最小速度。( x) y! X% R0 c# F G7 J 速警告系统传输飞机对1 W' a# ]. A7 M/ e/ G/ q% @& c 流的相对角度。 8 g' j/ Z6 k& T% [' V由一个状况改换到另一个。- n$ U: c" F* w+ `. G8 Y- C! Y 降场, 9 ]3 h& v' r: E9 n划时,除了目标机场之外,所选的另一个机 & e% H. \$ }+ j/ g5 L, Lo % ?# w3 @( q5 }* G* ~1 D4 W* `m / ]4 n, K( p0 A# pALPHA SPEED,1 p; P( A% r& G7 E5 |/ i ALPHA VANE, A small moveable airfoil on the sid ( z8 b" j4 m2 {. m( W+ }# [: Tthe fuselage transm / H! a4 F. r/ B9 n* Ea& g, U1 I+ G/ c8 c1 f5 K ALTERNATE, To change from one condition to8 c) ^$ G8 `! h" K% n- F A- K; K5 T: p- y, [6 v! Y flight planning, usually near the destination airport, to be6 V$ z3 y& i6 D9 _1 T used when it is desirable to divert from the original - g7 t* s! V% M. p4 C" L2 H' Pdestination airport. ^0 U6 u+ H. n- H, L空速游标8 C- D% x/ d9 w# ?8 F 空速表上的可调指标。5 s% ?) H6 F# j& A+ [' ~; R) ~+ i5 ^& q8 Y 迎角速度,4 B0 q( B# u3 y1 ` 迎角叶片, + ?1 s; v5 }5 q+ }& i' b- H位于机身侧的可动小翼面。为失: J% }$ o. h) D4 |, M. b4 \7 t4 g" W# K# d$ u交替, ) L1 S u+ p* \+ y# l+ s$ Z ~; ]- L2 Y; C! A( K制订飞行计& _8 v6 A& M2 u2 n" x& z6 E1 p6 ? 场。通常在目标机场附近,以备不去目标机场时,改降之/ \3 F- c$ e) j* r 用。 6 N* H% Q# }3 @. ^& a/ `. f. a3 q英汉对照民用航空词典B OEING + \6 M/ |1 [% f( B5 J) uTECHNICAL DICTIONARY 8 1 Q8 p; R8 T9 P+ zALTERNATE AERODROME, An aerodrome to which, T; S" X0 K i. ^ an aircraft may proceed when it becomes either: v" z) t, I+ D" P# o possible or inadvisable to proceed to or land at the # P$ R$ W( t; ^2 V+ serodrome of intended landing. ; ~; S( h' k; N+ u# w8 hTER SETTING, The adjustment of the altimeter $ N5 J) \6 j8 Uaccount for local variations in atmospheric pressure.* ]# z! R1 V% c2 }+ N! \ LTITUDE ACQUIRE, A digital flight control system 2 X" }7 N" K' c' N w1 tode to transition from climb (or descend) to level flight. t) w1 c# w1 n7 O. Q4 k! H2 }* @LTITUDE ALERT, A flight deck alert occuring when the$ W; e3 f% S& I irplane approaches or departs a selected altitude. ' {. N8 [* o9 I3 J2 N# G9 L- r: w+ B9 tLTITUDE CAPABILITY, The maximum altitude at6 g* D) F- @2 g" p0 y( [ hich the airplane can be flown at for a given thrust,& c% Q& }! B, |9 |& X peed and atmosphere condition./ e; \- g5 _% S LTITUDE HOLD (ALT HOLD), A mode of the autopilot0 j+ I6 u p5 s F5 @- L. a$ z r flight director to maintain a selected altitude. 4 W3 M3 H/ O4 L+ p+ J% Y# yirplane's altitude during VNAV operation. 6 F/ _! t) ~+ p+ q r- a1 f# p机场着陆时,可作着陆使用的 + V! `" h7 U0 ^& x8 w$ d, t8 b场。; K8 K7 G. \; J8 g; ~' V6 E1 }- g" M! l1 S 根据当地大气压力变化而对高度表所做的调整。) P# }7 h8 U# v) i2 x+ U 一种数字式飞行操纵系统,从爬升(或下降)改平的模 / ]+ K& J: y. m# ~' b! i/ {* ^3 q3 P( i) q3 @0 R度警告, * R( | C' `2 G R7 a- q5 b* B! }当飞机接近或偏离选定高度时,所出现的驾驶舱警告。 t/ o7 k6 x9 L M# v8 _( A } 高度能力,# L; I( K2 n7 g 在给定的推力,速度和大气状况下,飞机能飞达的最大 1 A6 F U( \& A, T7 i0 x高度。 ( j9 d, w2 e7 d% C& O: H高度保持(ALT HOLD), ( q: J" J. m, l, \" N8 [) ?自动驾驶仪或飞行指引仪保持在选定高度的一种方式。 ; [) q5 x! X& z( r! w8 S9 J, f! r, M# T; _/ u7 Q# ^! ^3 |) E1 K 员对飞行高度的控制。" y2 i, a0 f; f- O im 7 r6 u, y- R, Ja6 `( ?- B: @4 Q3 O ALTIME / i5 T7 l# O9 j+ L$ Fto 3 x. G. V5 g# k$ |7 R; r5 x* fA5 F' }9 C* ?( y/ u/ [! S m : C0 N$ Q7 b. g+ N0 vA, I7 V* G" U3 h a 1 [4 x% R! y/ r; o' Z2 e5 EA0 K. }! Q w9 \3 m+ t w + a$ r) n% L1 K- ?+ T9 {5 Es3 {; X$ {. }# I+ Q5 Z' c A @3 l- W5 X/ ~. E o ; I" ?$ k0 q) L. t4 @ALTITUDE INTERVENTION, Pilot control of the 1 n u0 e. l' Ma 8 `. @3 J9 }) n2 \! K% B9 LAMBIENT, The surrounding atmosphere. 9 I0 d! Z- M* A3 d( n( N备用机场, 7 l& d1 n3 s+ E) c( F当不可能或不适宜在预选 # m! i% {% J) m% x z ], F4 h% d. l2 n8 l高度表设定! W3 S2 Z, Z" u. M5 \ 高度截获, ; ]. R( }" w8 Z5 \5 e, O- }' h& b/ Z# d) w. m! V5 E; Y. u& K9 u5 k9 o高度干预; N- o- n8 r4 o 在垂直导航工作过程中,飞行 - n+ h V# u. ^3 Z周围环境(地面气层), ' \7 Y. V/ f" N4 W, c3 ]2 L* ]( D4 Q物体周围的环境(特别指大气)。 # L# o1 s, g0 J5 B英汉对照民用航空词典B OEING # W6 {3 v& b+ ]2 z* \9 y# W5 tTECHNICAL DICTIONARY 9 & T- V3 T) V1 m9 g5 C% `' h5 y. y1 lAMBIENT PRESSURE, Pressure of air surrounding an& j5 g0 v, n1 t7 r; j* @ object, measured in pounds per square inch (psi) .9 |6 ^. k: _# X$ I1 r, p; ^# T MBIENT TEMPERATURE, Temperature of air0 \" u* W! a) d( i mpere.9 Y3 ]0 C5 |! _. f) w urrent waveform. * P. w& f( c2 `g an # ?- ?" d# w* r8 Gnalog signal to a digital signal. " c$ g- a! \. h, Qore inputs1 F; I. w& ]& H9 a$ p# ?% u7 u; g f binary digital information and one output. The output ; k4 L& b8 T* K1 only when all of the inputs are 1. The output is 0 . a8 T7 j8 u3 D% }5 ohen any one or more inputs are 0.6 m. U: w$ A. ]) y0 r 面气压),& n% g5 P0 Z; ], g# [ 境温度, 8 i3 l* c$ d8 t5 [2 g( y. v气温度,用摄氏度(°C)或华氏(°F)来 1 {: m+ ^' I$ c- m4 o) [. P: W- f& E' D( r& I! \电压或电流波形的幅度。( n) ?! p* X' H! D X, Y0 f 性变化的信号来工作,或产生连续性变化的信号* |7 w5 {! Q3 z( x4 Y 统。$ a1 b1 L- o3 P! \$ A 将模拟式信号,转换成数值式。 & a9 U9 e. z( U一种有两个或两个以上的二进位数字信息输人,一个输 % e1 @- {3 Q; _的装置或电路。当所有输人为1,输出为1。当任何一个 # a+ p- w: p; C- z7 c# ~# V5 ^一个以上的输人为0时,输出为0。 - X y7 [4 i1 z2 z0 \( q; E% [A/ b! {% t2 U- _% U4 P4 b4 ^ surrounding an object, measured in degrees Celsius$ q0 x1 _; Z6 H( E l. v. p (°C)or degrees Fahrenheit (°F). 8 ]4 _6 ? W- k5 r8 zAMPERE, A unit of electrical current. One volt across 7 Y5 i( K* a4 b4 \* d* i; done ohm of resistance causes current flow of one ) A: d$ i; I$ S5 _' A7 va1 m/ u/ |, V% D% w0 @' u AMPLITUDE, The size or magnitude of a voltage or + y9 B. R- a9 z, B: z8 q; Ec, j9 {6 m5 @9 E ANALOG, Quantities or representations that are 6 S- ~5 j( O* x" |* T( @variable over a continuous range. 4 D7 L" a w" l8 \; n- `8 BANALOG-TO-DIGITAL, The process of convertin+ r1 d% |2 X. M ?9 I a ( W* n [; ]$ }5 m9 t. |" b [AND GATE, A device or circuit with two or m # q) r( o% `5 ^o" g% P" f# z3 y is! g) z; I1 n5 I# t( P$ ~2 a w0 \. d! c2 y0 x- s# _4 [ 环境压力(地1 L: ~0 g5 S9 c 物体周围的空气压力,用每平方英寸多少磅(psi)来% {4 s j+ D. M" a 度量。 6 E! s: o8 N: i/ _( l {' E" p; Q7 H' F" ?4 q) k( [$ A 物体周围的空+ O& |( e5 s0 ~: I6 I! j 度量。! Q2 \$ `4 q# \ 安培,2 f9 J$ T4 ?0 b0 z( E; @ 电流的单位。 7 E/ ^' B. u# x1伏电压在1欧姆的电阻上所产生的电流为: e$ o# E3 S Z 1安培* Y5 k ~3 D! s6 N( ] 振幅, % u# R% g" a8 Q模拟式,* S0 ~, v- U' L+ X f+ V' d 用连续* y$ s' E' G! @; i1 s5 d3 o I* c7 r" C3 w/ d8 @! Q& G 从模拟式到数字式,0 I: H/ Z1 l* a6 ?" k3 N 与门, + Y% ~% e2 X$ `+ c; Z5 q( f. i) S+ f6 r" G7 E$ r& R英汉对照民用航空词典B OEING 8 L2 k9 ~- y4 X! ~+ K' t. cTECHNICAL DICTIONARY 109 h% R- {& \9 c( S$ a7 N" O$ F: `, r ANEROID, A sealed flexible device containing air at low 6 K0 B" h* \, ~( M* V2 Mpressure, which expands or contracts during change of f! L: x2 \* Kressure outside the device." d: r+ T% K; G, s/ n; e ically $ p+ Z' L/ {0 Y, Xr changing the direction - C! ?* u% w' a4 k/ }f drive.- `% L6 b( }9 R- }7 j: H6 g of the wing chord in . W* h9 p9 R, z& Z" _1 ]lation to the free stream airflow as it moves forward, w8 y6 J1 d8 Z1 D* t+ p4 ?. ^, r rough the air.. [- W! l6 z( L0 j# |4 O al axis of the ! L6 ]6 q: H& F4 G; xaircraft., ^1 ~( i0 T' t5 K' e 胀或收缩。 + v* h$ C5 b8 m" a4 s箱。是改变驱动方向的机械装置。 & T0 a; S3 @0 w7 z机翼翼弦在空气中向前运动时与自由气流之间的夹角。 ; S$ b: N7 i8 n% l3 T. g; {+ X4 h4 R9 A' W. ? p1 h) j' }7 y6 k ANGLE GEARBOX, A part of an engine, mechan . S, \7 S+ M' ]- Ndriven by the compressor, which drives the accessory 5 ~8 j6 z f# g) R l1 M$ @gearbox. A mechanical device fo, K# i. s: q& c, k4 n" R o3 M: ~8 P5 N# ?+ S ANGLE OF ATTACK, The angle# \3 ]- m) G8 G0 \ re 5 p- Y$ N2 e) } P/ o" C# u( z/ Rth 5 x- P+ T2 \% m. {4 |0 |! l. QANGLE OF INCIDENCE, The acute angle which the 3 q' U0 C, u0 Y; D/ awing chord makes with the longitudin. r( ~. S9 P9 |' U% ]5 L. y7 J; k6 O 膜盒, & g* D6 e# r' H7 V0 t! ~4 J内含低压空气的密封弹性装置。当它周围的压力变化4 Y( Z4 a+ u1 _. l0 r 时,会膨 s6 r& {, ]/ B$ p# {' g* M 伞齿轮箱,7 v+ T N4 ] Q 发动机的一部分。被压气机以机械方式驱动,然后驱动, U8 Z6 c% I4 K7 ~ 附件齿轮- d9 k& E7 j& ^1 O1 {2 { 迎角, . _. m4 |! i$ ^; q1 b安装角, + k8 X6 |" }5 i1 T$ C: o飞机的纵轴与机翼弦线所形成的锐角 0 m$ A4 R' B8 [0 S! V6 [0 p英汉对照民用航空词典B OEING8 l) A. D# f& l6 w3 ]: G9 k* g/ H, Z* y TECHNICAL DICTIONARY 11' Y$ m6 Y" F; d9 |( w7 ?" I. G7 n6 e ANNUNCIATIONS, Audio or visual indications used to 8 E3 s& ]( Y7 n5 `1 P3 u0 H! Fcall attention to an event that has taken place. 0 l Q5 a9 j1 V) c, ^0 KANNUNCIATOR, A visual device consisting of a number ( d6 x. y. _5 B2 E7 a6 ely.. R' u: t/ t- t* n8 M ANODE, The element toward which the principal stream " A7 ]2 d% Y1 b* Qof electrons flows. $ v# |) Y% x+ aANOMALY, Not normal. # k( e! H \+ M' y" mANTENNA, A device which, used in conjunction with a 5 Q$ Q7 e. ~+ d/ {5 ktransmitter or receiver, is used for radiating or receiving# ]+ B2 Y; O6 b6 n/ e3 P n radio waves." c4 {3 B0 y5 R) d' l5 H! z NTI-ICING, A method of preventing ice formation on " X+ e+ h/ W( D% u6 c/ V4 l7 }e wing leading edges and engine nacelles. 8 `9 f5 a+ I, fNTI-SKID, A system for providing maximum braking1 D+ g, O- p8 J0 _( b: O ithout skidding for any runway condition. Anti-skid8 H6 f" }: r$ Z% Q4 c! x G: w- p8 g omponents are part of the brake system. . k* N4 z6 a5 D告, `8 b6 y" {5 U1 } 当发生事件时,以声音或目视指示形成的提示信号。 7 u$ ]. ? o3 z5 Q' [8 _1 _与之有关的电路的现有情况或已存在的 6 H: k9 Z- @' Y' u2 \0 g" p+ S, h1 w 正极, 2 X' E8 J6 w4 N主电子流向的极位。 % y1 ?# ~: A6 B0 z异常,0 x( t8 d/ I+ G4 G8 t7 z* C 不正常。. L9 q& e2 K) |6 y+ Z: @ 天线,5 P% y& x: B4 ]* s4 | 一种与发射机或接收机共同工作来发射或接收无线电4 h/ H! l p) Y: A* @4 ] 波的装置。 ) z4 e# F9 a: n' r冰,4 F1 ?: e0 @7 R5 E# F6 B( H0 V 防滑系统, ) _* t5 H( m3 x" V6 A9 F! }, y一种在任何跑道状况下,都能提供最大的刹车能力而不# O; a. x H/ m; _+ f 使轮胎打滑的系统。防滑部件是刹车系统的一部分。0 F/ F2 ]7 @1 M" c6 ` of lights. Each light indicates the condition which exists# w( j) U4 n: L3 a H) ~ or has existed in an associated circuit and is labeled' q8 I" @- S" F2 v& f& y according- W- |: J% D' t* ? A; Y6 S( D$ L2 U4 Z0 B* ] th3 ?5 _% k A7 a A, n! ]8 r& M8 h6 C6 E w ( A6 e2 {4 N$ Dc3 W" T! G" ]4 Y/ Q% L$ G/ M# ?1 U, B& U 信号牌,4 S5 T- G& r9 l; r+ x, l0 O 由一系列指示灯组成的目视装置。每个指示灯都有相应9 H- V8 v# o. C' k' A( b 的标记,用来显示 + n; i% {% u, J4 b$ m' x2 v* e- ~6 n1 ^1 ~# N, h7 i" q8 a6 }! d j, W 防止机翼前沿和发动机短舱结冰的一种方法。! {( n1 r7 @2 ^ 英汉对照民用航空词典B OEING5 N: _! ]. D" V: u. I" z' _ TECHNICAL DICTIONARY 12. R3 I* y' R% ^2 d8 {' o) \* q APPENDIX, A supplement to the Airplane Flight Manual * y$ L+ n; \1 c8 F+ S, i: }: O) Ftained in the basic manual. A4 Z5 s( n1 P- \2 F. J0 n1 Q ollection of supplementary material at the end of a- K8 `$ H8 q* z$ w- _. X ook.7 q7 H) V$ g! Q% h4 {5 s* A; ~' }" W/ C of the. r; o- m8 _( A( l" V' q) d% C2 f rsion link on the landing gear.: S- Q6 D& s9 E, C R) d7 l/ i0 l APPROACH MODE, An autopilot/flight director mode6 f' d2 n# o: w1 Q, Y6 ~3 \ which is a combination of localizer for roll control and( |; n( ~9 W" n" q2 v" b glide slope for pitch control. This mode is used when full# w2 |- x& p; ^; |3 w! D0 @ instrument landing system is available.1 j, F2 e# j4 o( q0 {6 n0 B APU, SEE - AUXILIARY POWER UNIT( H: u/ e0 J: D) I; y) ^ ARINC, SEE - AERONAUTICAL RADIO% P+ V, _# n- b7 s INCORPORATED - b9 `( [8 [& @0 kARM, To make ready for operation.1 H4 Z0 t4 p* y/ Q1 ]6 b# @7 d. Q/ V 附录,# y! A, }0 {( D( Y# [+ S% D' m 飞机飞行手册的附件,包含基本手册中未提到的飞机形 2 t+ @& B, Z; F* @; U& h2 {- A态的其他性能。是附在手册末的补充材料。' Z3 Y9 E; h1 Z# m ` 顶销, 5 R* C( B5 S$ M用于连接起落架扭力臂两部份的销子。- a& M0 D6 K" e; y; h 进近方式, $ U) @ v2 x# T) { P一种综合了控制横侧的航道信号和控制俯仰下滑信号 3 p1 p$ p6 z/ ]% j+ O' c的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系 ; L# [1 m+ B9 @, m0 e统正常时才使用。/ W+ [& h, W8 \) b0 a) _) Y! w! ?5 e 辅助动力装置, 0 q' |; v# x7 E8 h, k见Auxiliary Power Unit1 T1 A: E2 _& X2 F containing additional performance for aircraft) F4 v: G4 L2 }3 v configurations not con $ g: d" T5 i; g1 ~/ Q& U1 s9 oc0 u" w$ ^4 c/ O1 A; P% p b7 e& S7 h% ~, P* E APEX PIN, A pin for joining the two sections% j" l5 W2 G$ p0 A( p Z4 S to0 [* k- w, l4 G; s I% I9 D6 n. }9 q1 w$ e4 J% T# ?航空无线电公司, + R8 Y8 ]" ]; W( \; k见Aeronautical Radio Incorporated. : K8 o8 f9 ?+ Y: P: P7 h6 o' E4 r1 b预位,7 J6 Q# g+ L. `- K 部件可以开始工作的状态。2 @' f2 d$ k4 Y 英汉对照民用航空词典B OEING % r& ?- w% `+ zTECHNICAL DICTIONARY 13' Q3 s7 d0 ~' C7 p ARC, The curved track over the ground of an aircraft1 v: V8 `' K' v( x* w$ N9 C/ w8 B flying at a constant distance from a measuring% ~9 w0 I$ S, T6 A( V equipment (DME).1 m3 m, W9 [) S. F4 b3 F" ^& Y in the limits of self-contained system* w9 [% ]9 e, T" D apability.) H5 H; D& E5 a3 U9 Z" \/ T/ q tem for opposing or restricting! G; R% ]5 L8 |% C+ e) d3 q ovement. 4 q* f! }; r% v. G- j6 z8 G% MSPIRATED TAT PROBE, A sensor that measures total / H. Z8 r1 z1 }5 L; Y* `/ u! ^) Jir temperature when the airplane is in the air and that $ h9 b5 b; y$ M, Z9 ^easures outside air temperature when the airplane is ! @. \0 x U! Q3 yn the ground. The outside air temperature is measured " t2 u4 P6 j0 iSSEMBLY, The fitting together of a complete structure & \, i7 \7 |1 K9 XSSUMED TEMPERATURE REDUCED THRUST, The/ H1 F1 ~4 k& f6 ^ ATC, SEE - AIR TRAFFIC CONTROL 0 T# K. i' V6 Z' s/ A7 \/ }# R* D1 y7 K, x t6 e系统中所产生的一种用以抗拒0 L- Y2 v0 C9 x( D. q 作或限制动作的力。 ; G$ \" \, t1 x/ N& K4 O头, + ?0 y r) U8 `7 m) ]; j. d7 U; `* h用来测量飞机在空中时的总大气温度和在地面时的外 , x& r0 @; y/ U X5 ~' W0 M温度。地面外界温度的测量是利用引气将外界空气吸入& T6 u% n6 ?! \ 头,以达到测量的目的。 $ J) ?6 B2 v# _配, # d0 N. a. G! X. u" t9 N一个完整的结构或组件的过程。1 ^: }% V8 O2 I+ r 假设温度而得的减推力,4 `$ A: d: ^8 M2 z& Q' l, }" I" U 推力设定值时,假定一个比实际外界空气温( p% K; v8 i2 j& p 空中交通管制,( }* V/ L1 o. U3 s; ? ]0 y 见Air Traffic Control . ]' i% A; ~) M ?AREA NAVIGATION/RNAV, A method of navigation0 d* X2 s, v) `. ~! f4 E6 a that permits aircraft operations on any desired course & c: Y9 p9 A% m4 Jwithin the coverage of station-referenced navigation * v0 I% U) B: [1 ]5 ^signals or with+ b% S9 g7 |* {% R. W7 G* U c; @& a+ I0 {6 H* t* K ARTIFICIAL FEEL, A force developed in the flight, N; x0 S- a. H* g) Y2 H control or brake sys) {' K- A9 T" @3 q/ P m , ^7 q2 w! ?' y" U- G7 j# ?# B) x% `A 0 K! A2 S! }' e9 k q" N: Za 6 V) ]1 I; @9 l# w. N+ x) ym* R5 O% I) n3 T$ |( f o) H; O8 u. }. r1 M by using bleed air to draw ambient air through the - c% N* C) N- H" o/ Xsensor when the airplane is not moving.- ?. S! j) b" Z/ x A # b( a) `; o. e. ror unit. . \, D( R& G" d/ `3 y5 k6 KA / u! T1 z8 d7 |$ ?" glower thrust obtained by setting a higher than actual 3 f9 V+ H( q I- c5 _: R. COutside Air Temperature (OAT). 3 U6 s1 A5 q# I2 d; X' M: o! ]弧线, * v" A. d+ p& P$ U" E飞机在围绕DME台等距飞行时的弧形航迹。 6 L0 X; O9 r" U) a' B区域导航,7 M: m5 E& N4 W z 容许飞机飞行在有电台参考的导航信号或自备系统能( d/ Z% u7 `: b 力极限范围内,飞行任何预定航线的一种导航方法。" ]! p/ S2 H4 O8 t 模拟感觉 9 B& Y: S2 N8 S% }在飞行操纵系统或刹车 % V& r9 A- R2 E* k0 i7 l* B ]- Y, `: d吸气式总温探 1 l5 U5 c0 g+ b6 M5 g) \6 l( \3 r9 Q& |8 }9 u( \+ o" ^) ~& }0 D* {1 i* S6 _- P& a8 C$ P# l$ k+ b1 a 组合成3 F; L0 u H$ v6 g f m. u3 ?+ B! O% d! E v0 R 在选择起飞 % g. N4 ~) K' @9 V0 _: @度高的温度而得到的推力。用这种方法可以减少发动机的 + n8 {6 W6 ^) P: } G磨损和维护费用。 4 g: R+ l/ q7 R# u. V5 j7 G* b+ e0 }9 C英汉对照民用航空词典B OEING . ?, ^9 a0 N# G# gTECHNICAL DICTIONARY 145 x" R ^6 n- x" [5 X ATE, SEE - AUTOMATIC TEST EQUIPMENT 1 Y1 `8 {7 N" m! VATMOSPHERIC PRESSURE, Pressure of air due to the % e4 ?. X# z1 }. x- varth's atmosphere, expressed in pounds per square / u' x9 b0 F Lch (psi) or inches of mercury (in Hg) or millibars (mB).2 ~% y8 D6 G/ m0 Z' O+ `, w TTITUDE, The relative orientation of the airplane with! B6 g+ e. N7 \ N' W spect to pitch, roll, and yaw. ' W) v7 N$ F* d. S$ ^; R) Z JUDIO CONTROUSELECTOR PANEL, The panel in # J$ Y: d8 T4 `% H) j) ^9 h2 f2 G1 oe airplane which controls and selects the routing of: \! _1 O1 @' q7 {/ P: g& A udio.! R; Q" q) m/ u8 p UTOLAND, Automatic landing using the Digital Flight: ]1 j% I( |* M8 {- m1 p2 r& R4 | ontrol System.+ ^6 Y; k7 G4 @6 c8 [; { n., S- j8 u6 V. M5 M7 V M, A system8 Q8 ?% a" e( R0 D) g8 [ omposed of all necessary subsystems needed to guide! [5 j& U9 h# d3 E e flight of an airplane. 0 X( Q+ g2 Y( VEQUIPMENT, System test 5 ]2 |) t6 \; _2 r. fquipment that operates under computer control. 6 p: S( z$ f1 {, v: a' k+ }& v8 h' Y装置,

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e5 m/ J2 c" X8 F5 j) m k* Y in/ E) j) U @' x& w( S A% a- b' {" P- n/ C, K re 4 t5 L* c9 m0 R1 fA ! B L- ^$ M3 r, X$ M1 kth , x' [; l2 @0 C: P; ra6 ?* E* [$ f. q3 I0 ~' L2 c' z8 t A; h' b$ z# p" n5 A7 d, ~) S C: T8 S% g& b, w! `8 L, ^7 U( F AUTOMATIC DIRECTION FINDER, A system which * s! _- \! y/ `/ j, N1 O+ s) Hdetermines the direction of a radio statio * I: {" G6 E! PAUTOMATIC FLIGHT CONTROL SYSTE, w, j( g4 z- H) M( ~* l c7 r$ N( b& i. }$ @* Q1 p7 ~ B" ? th . E, c' |1 F2 k* y# Q" o' ^AUTOMATIC TEST- H% }( z! u0 S8 C. m- T/ w z1 L* z( s e; `, e$ D# y6 Q0 c6 Z 自动测试 / i0 E g9 L! U8 f. M见Automatic Test Equipment.5 A0 _; J/ q: R$ c1 r! r 大气压力,* h) w9 o& o$ p) a4 l 由于地球周围的大气而产生的空气压力,以每平方寸多4 E5 t9 \9 B$ l1 J7 j 磅(psi)或多少寸高水银柱(in Hg)或毫巴(mB)来 o- \5 S3 T, H$ A1 h2 y1 L8 m. `示。 + Q* C6 H: P3 }3 p. k飞机姿态, 8 P- `- Q( t: b2 ]2 z* ]' ?3 f& a) d8 }飞机与俯仰,坡度,和偏航有关的相对方向。 ' y& f: \. v* J音频选择面板,* V7 ]7 k* ^( H' b+ s4 S 飞机内用来控制和选择音频通路的面板。0 y, i) W6 a8 h* B2 H 自动着陆,/ Q4 C' ~9 e* \ 使用数字式飞行操作系统来进行自动着陆。* Z& U8 ]( n# e( D! _! t 的系统。 $ s: F: s, k6 Y7 a0 k" j; m! U$ M; X7 [4 g系统所组成的一个系统。+ A. K* W' S! h& T9 P 在计算机控制下运作的系统测试装置。 5 O c, E$ J, [6 v/ x" W- `6 y: z; j" K; g5 `" `* w' Q" Q0 | 自动定向仪(ADF), : w7 W0 |$ Y# ~ j# `# S9 J' k确定无线电台方向! x$ Q1 |+ I2 Q" T: {- u0 ` 自动飞行控制系统1 [# k. |3 E0 n( T+ ]1 e 由所有能引导飞机飞行的子 + y8 _. Z. L* U, v( J自动测试装置, 5 T9 l" ^& P& z( g9 W, P英汉对照民用航空词典B OEING ) n( _( W& C% J* ?" c" u; h8 pTECHNICAL DICTIONARY 15# R/ z; \1 F- s& o# r7 J AUTOPILOT, A system which automatically controls ; {' m: D; \" `$ {# d2 G4 uand guides the flight of an airplane. 0 r$ L \. ^: H, b# lAUTOPILOT FLIGHT DIRECTOR SYSTEM, An 4 n G; Q# _3 G; Y8 \; h. A" h: Etor5 u+ }* C8 k, w% Y. g UTOTHROTTLE, A system which automatically 9 Q w; e# }- q/ F4 D3 K1 M3 Rontrols the throttles of an airplane.* Z+ B4 ^% z$ u9 z$ N) W$ g+ [7 ~$ N POWER UNIT, A small turbine engine in: G7 s3 K% ^( c* [' C6 {9 j e airplane for supplying electrical and pneumatic + [* n- d: m9 C+ oower for systems operation on the ground or in flight. . {$ x0 b1 ]$ [, G2 AVM, SEE - AIRBORNE VIBRATION MONITOR . i( d% p5 C/ q* x: H0 u+ ?! aXIAL FLOW COMPRESSOR, A type of compressor , s! \& t s; G# {& qsed in a gas turbine engine in which air passes through& q& v0 F: b" D8 ]$ R" S XIS, An imaginary straight line or an actual physical & S7 B, g- S& @omponent (such as an axle) around which a body can& W: V; b& B% s$ B6 I: n# X! e. r( D tate.( F5 Z V5 C6 l7 e- L- x 仪, B$ q6 Y' n( V' `9 @0 H+ v. k& i2 F0 A h4 L2 ~% F自动驾驶飞行指引系统,- b, t# R" Y* R2 ?8 M4 g/ G, _4 G 动驾驶和飞行指引功能的系统。; f; x$ h5 X7 W6 l% Z. x 动油门, ) a, ~( m2 h5 k( A# e自动控制飞机油门的系统。( f0 j# ?6 m d 是飞机内的小涡轮发动机,在地面或空中给各系统提供 2 Y6 @4 `6 b( X$ @7 e3 A源和气源。. }: [- ^' Q8 F! }. b$ z5 l 称。0 Y9 U/ S+ F( G2 T 载振动监视器, " g/ L) u: K# ?$ ]见Airborne Vibration Monitor " `' L% d; V7 J# Iintegrated system containing autopilot and flight direc , Y5 x L2 T3 wfunctions.0 @1 E+ P2 m! ~# C A" H0 I# ?6 a1 b c : l' m% O4 A: F$ t6 v( k0 p9 RAUXILIARY + P% T; `2 }$ H+ ? Eth9 r$ o' P1 O3 L p/ Y! |, _. w' R$ W4 j AVIONICS, An acronym designating the field of aviation ' D5 f: q$ t' `. d7 G( delectronics. + a$ G R2 d+ C3 kA1 t! X+ _2 ` S: ? A ( |, k2 J* t% q( S- ` P, Vu/ i3 A. W5 Q) n the compressor in a straight flow, front to rear." R* A1 @2 c$ | A 2 d3 {7 c/ _9 Y2 }; vc B2 d# v% W+ R; s9 ~/ ^ro ' p* x/ w, P) `" f# w3 P自动驾驶' W) I/ d9 x8 }8 h0 Y. B 动操纵和引导飞机飞行的系统。/ S: q2 W6 \, N9 O! g2 y 一个综合自% o% v$ _- ~; O* g3 C" X* J E! }4 x辅助动力装置,0 R! A4 q3 X2 }+ \: ^2 J$ K$ Z- W* T, M1 R& y 航空电子学,, D/ `& H6 l i1 Z9 n 是航空电子领域的一特有名 ; S. @- u- m2 K3 S4 b# {' o- b! J# }& h7 p) T9 S) `, V6 Z: s3 Y" x流压缩机, , U6 A: ~- ^1 U% s; F4 H! |一种用于燃气涡轮发动机内的压气机。空气由发动机的; X& m( ?. [( Q% v& C5 _ 部流出。 A0 W t1 G v# H/ s 线,, W* H# a1 i7 l- T7 [& ]4 ] 可让物体围绕着作旋转运动的一个想像的直线或实际 ' U1 }! {- y& t在的部件(如轴)。 0 P. H$ L+ j# o% v. y2 ]% M8 G! l, }. Y0 n; a7 t" X 前部轴向流人,压缩后,由后! T, [/ n; A" ]# @. J: {% o# L0 z- \( e) f, A( V7 H3 A: }& a! o: i' V英汉对照民用航空词典B OEING) w" x7 l& D% @1 \! h TECHNICAL DICTIONARY 16* }% C/ @1 Z \. y& J B 5 _) M! E* t: ^/ G- f9 ]ACKCOURSE APPROACH, An approach to a runway 3 p# r% g8 w% ?2 M2 d9 b, Aversed.9 g5 f5 w+ V* h/ p1 P own on the EFIS that . e1 q* n8 q2 k: Q& q$ D6 o# l7 r, }% does not readily change, for example, navigational aids. 7 i; ?3 b5 N. l0 B4 ^# ]vement in the tank or reservoir.& s c, S" J' D2 R L ALANCE TAB, A small hinged moveable part on the , W* m$ H3 W, k2 q$ T# o$ xailing edge of a control surface (aileron, elevator, . ^* R( ? m/ v2 D2 x, R5 W- B航道进近,% c; O: G0 f& |: j 相反的进近方向。当反航道进近时,无下滑 : y' q# ^! g2 f6 P a显示在电子飞行仪表系统上不经常改变的数据。例如: 8 s: s1 U/ C" `; v6 s$ T0 |2 G航设备。 0 e, G, ~2 c& G/ ^& e在燃油箱或滑油箱内阻止液体流动的隔板。 5 a% G9 M. o3 ^4 j( ~; Q' d动补偿片,3 m/ G" Z; K1 A+ O 铰接在操纵面后缘(副翼,方向舵,升降舵)的可动部。. u6 `8 D7 {4 K- r4 w) ?( I6 H8 s 与操纵面相反,以帮助操纵面运8 f' r5 t( R1 z' S8 ^! w' D! z% M. S B' [& b3 [/ V; k8 h which is opposite the normal approach. For a+ t. @: E& N( s: l backcourse approach, glide slope signals are not 5 ?/ C. M d* d; oavailable and the sense of localizer signals must be, V: U8 n6 X$ t: H O re - |+ w8 Y9 o+ u4 ], v( E2 fBACKGROUND DATA, Data sh # [& P. D, _, y9 ]# }. gd! v) s+ x3 U0 n5 Y; I BAFFLE, A partition in a tank or reservoir to prevent + a9 i# O n p6 Hfluid mo $ J' z1 ?! u/ x* CB- P$ `2 n9 e' v j+ @. W tr 7 o5 u; t, @2 {+ C% Urudder).The tab moves in an opposite direction to the( g- b: }6 f+ H+ d control surface for assisting movement of the control 5 T& Y0 Z3 n5 R2 n9 {4 zsurface. 5 v3 j* v5 \3 k5 c+ H1 X) N6 Q: w# G$ m: I$ K% K与正常进近 - M3 s, ~5 t: O5 e% c道信号并且航道信号也必须逆反。# s6 i9 B8 W) ?% W9 F, i% ? 背景数据,; l4 n# P: p: @# Z6 D0 h( C% C8 E7 v' J. l1 H 缓冲隔板,( R9 L1 T1 p9 w5 O/ E1 f% R. F' ^3 T( _* y随动补偿片的动作方向4 ]8 O8 g4 i0 I: f* c 动,减小操纵力。 * z8 O$ G- o. O3 B5 z- e6 g英汉对照民用航空词典B OEING' Q" b$ F) l4 d# I- s! F) f TECHNICAL DICTIONARY 17" l4 o7 H. g# B, {$ r: \/ s* B BALANCED FIELD LENGTH, The field length |' x3 M" E; d- V0 Hassociated with optimum aircraft performance when" a, @/ v& d/ T4 |6 ~. s3 i bstacles are not a constraint. In this case, after engine 7 M; @5 Q$ {- u5 x* ?ilure at V1, the distance required to accelerate, takeoff ; f! Q. r: {5 S" r; v9 pnd reach a height of 35 feet is equal to the distance 9 ]) m0 p$ _5 Y) _/ e9 hALLAST, A weight installed in an aircraft to maintain ) F3 m* h: E3 ]1 [ALL NUT, A fixed spherical nut driven by the - n" `5 N+ F+ `. \2 i* A! r3 hAR OUT OF VIEW, A signal used to remove the flight 9 V* H- i* u# K9 n+ _) E% uAROMETRIC PRESSURE, The pressure of air above * S. }8 T! V( t' x3 lg) or 6 o0 d2 P# R4 D4 S$ o' e7 fmillibars (MB).% f r1 b% Q- N* Q' Z$ h( \: B ATTERY, An electrical device for changing stored6 Z5 G6 g3 M! `: F- I" |) P6 J 性能的场长。在此- y# x0 D7 w- @) M; o9 r 况下,V1时发动机故障,要完成加速、起飞、离地35 # ~+ ~7 ? `, E8 I尺所需距离等于相同速度下完成全停所需的距离。% T t8 |: u0 E& Q0 H 舱物, 7 j4 y9 Q; c4 z/ j重心在许可范围内面装载的配重物。 ! Q. e9 c3 c% h) U形螺母, 5 D2 W6 E4 D4 m- [/ ]/ y/ `" C的固定的球形螺母,用以使襟翼和水平2 G0 `. W p" M 引杆消失,. k7 h) B; ?# w0 R8 Z3 q 指引杆的信号。 : ?4 ^7 @- y3 d0 P1 y: Y压,; U" B0 T8 Q: [, D 压力。通常以多少寸高水银柱(in0 Q s v: s/ s: S' n 瓶, 1 w9 b2 W2 h% B B7 B9 @的化学能转变为直流电的电气装置。3 H& ?' z! p" U o / o, c' P# @0 Y- w0 F% S3 pfa 0 Z. d' a4 J7 ~/ A5 D# ta! u2 O3 f1 o, K/ X4 e required to stop from the same speed. + Y/ p0 f$ [. t. B! J% R7 C) P& [6 {B3 G2 \3 U+ S' l( I the center of gravity within allowable limits./ F( K9 w% x Q B % o6 k, C: \! ~3 R2 D! q. ~6 djackscrew for flap and stabilizer movement.9 ^7 D' Q& `9 I/ z) C6 C& Z8 @ B3 N* @9 @+ ]/ @% n director command bar(s)." D a1 {8 M. ~/ }8 r/ o B 4 Y% `* D" t0 z. K( [6 W) uzero pressure measured in inches of mercury (in H # } s" s, k) C) J& j- V7 }in ! l8 `4 U( e& a+ F/ t6 yBASE METAL, The underlining metal to which alloying! S4 X7 }% r0 m5 ? agents or metals are added. , X! d7 k: ]* [' C4 AB+ Y8 }* S) d8 u ?1 C chemical energy into direct electric current. ! i: y( ?1 H( D. i! `7 Q平衡场长,3 z& m8 y& \. `3 O" ?8 h 当障碍物非限制因素使飞机达到最佳 , C m+ ~3 i u5 w. T5 C4 S7 \& b ~( q: l' a& @. w# O, g' H( v; R8 V6 W7 n# x* G 为保持飞机 1 @* Y5 l- s1 v# i- W/ ^7 U# c% u9 u; `, L/ @. W# L- u0 U由粗重螺杆驱动 ' o$ l' S: F. c* ~1 T8 e5 O+ H. O( F安定面运动。 0 u. F# K2 E" ~1 _. o# I9 Y9 A9 \' q- i7 A: g3 z* N 用于除去飞行 + W+ E8 D) c3 G# H( g8 ?" n: Z; m) x 零压力以上的空气 " q: T, ^& n7 M" X/ G5 X2 UHg)或毫巴(MB)来表示。0 |/ Q7 E$ @( W0 A 基底金属,3 d: s `5 |: v: c/ n- A 指合金中的主要金属成份。 * y2 |. ^$ O. e: U4 A9 }' o4 n5 w) o+ Y# d0 {$ m( l将储蓄 9 y0 k8 j8 Q) v英汉对照民用航空词典B OEING 1 D+ q7 ] \7 f& ZTECHNICAL DICTIONARY 18 ' p5 ~* A) o0 k3 R5 b5 z" R# |BATTER4 |2 h) [6 O: _. q' O6 R direct cu" z3 C# p8 S3 B, K I power su" ^1 W( v$ [# D7 N Y BUS, An electrical conductor supplied with, n# ]9 t. X/ R* f& |% W7 ] rrent from the battery or transformer-rectifier for . g( K l8 ^# q! Mpply to operating components. 7 X3 [: E( m" oCHARGER, An electrical device supplied/ F) n# x" {3 ]8 L# [ ~4 j ith alternating current, which produces a direct current $ e0 G3 W' _; uutput for charging the battery on the airplane. q7 ]4 I$ ]: t$ R1 x. P) S6 j. AAY, A compartment in the airplane structure.7 e+ P9 V: s$ U7 ^! H CD, SEE - BINARY CODED DECIMAL / v: p& P6 Q( u0 lEACON, A device which emits a signal for use as a 4 x/ }. M: V$ d @/ b9 Kuidance or warning aid.8 J( L& u1 w t% c8 d1 d. G2 k l) b BEARING (NO. 2), The direction from an airplane to a1 T0 E# @1 p6 j; T" D ground station.: i6 B# c, _2 a: g7 _& H8 i 瓶汇流条, 8 S2 C) H, D7 b0 o" K O/ s将从电瓶或变压整流器来的直流电供给工作部件的导 % \! m( h9 w2 K: d# P体。2 k* u! B* ?! ~* ^ 瓶充电器,8 [3 Z3 o0 g+ G7 [! k 用交流电向飞机内电瓶充电的电气装置。带有交流电的 + U$ L* v( d8 }气装置,该装置产生直流电向飞机上的电瓶充电。 6 U1 b1 y6 y/ A+ c% w舱, 4 O' A1 I6 g& K飞机结构中分隔的空间。 3 E. ^0 x( d" h P" o( ^* d: m/ _二进制编码, 9 `* ^. L: N8 O7 ~见Binary Coded Decimal 3 N4 k* X, j% W2 z5 k2 bBATTERY + M9 W& V) V0 v+ s1 D% ~# g- [* ?w* g7 g) i/ X$ _! b7 L" k o' [2 Z7 S4 ~) b7 S B ( h; J6 K4 [. f! w% B( z" nB; ~: R3 t/ @3 l# [1 I# [3 G6 { B/ H5 u+ c9 N$ O8 r2 O# L, \5 z g) Z0 p5 `. g2 g: ~" e- u9 y BEARING (NO. 1), A surface that supports a moving/ `6 ^/ U3 o8 E! k7 r4 T- j ]0 u part and reduces friction between the two. ( P/ L1 o" |8 x8 s4 _" v1 c; N7 {3 ^; P% t4 F% `% W$ w# K, K$ F! X6 X/ ~8 D5 N! p/ M% \7 h5 ]5 m( v( V: K* Q+ y! ~3 B% r, z: ]: z" P% h% w: Q7 A( T& n 信标,. k* [0 v5 Y) S1 C; [ `( L 发射引导或警告用信号的装置。! H, \4 y9 k/ S$ ~ 方位(NO.2),0 `0 N6 z1 g4 g9 J7 X" S 从一架飞机到地面台的方向。/ V* y6 h- j! u 轴承(NO.1),# R5 B1 \ X, O+ _- W* s; K1 \( e 用于减轻机械转动磨擦的机械装置。" k0 X, C. E' K* v6 m1 Y7 q 英汉对照民用航空词典B OEING 0 j& O) g9 H2 T9 a3 O9 `& CTECHNICAL DICTIONARY 19 ! Z. d4 w1 y4 _/ QBELLCRANK, A double lever in the control syst ]2 ]$ G1 k" Y5 ? changing direction of motion. x/ b0 W( x i4 \* z em for " o: T- }! N/ X1 h: lct in the8 O' R: r( i; T7 Y1 p" o+ ~ neumatic system for absorbing expansion of duct due1 b5 Q2 @+ {# L! j heat.1 o) Y; |3 S% [ ELLOWS (NO. 2), Corrugated folded or pleated 4 r2 R9 p/ V- d* G" D B" l7 u6 m1 p7 tontainer or compartment used to measure pressure. " r% H/ \& v/ W. X& w* fEZEL, The part of an instrument case for locking the' w8 |+ R& T/ r! }) k+ {/ c lass. P1 z: f' W9 Y7 } IAS, The potential difference applied between two # Q$ _# j, O0 G9 \* ~+ Qoints for controlling a circuit. 8 p4 j* Z' S- E T: {BILGE, The lowest part of an aircraft fuselage. A place) R u* y4 [& L" ]" Q3 R3 V where water, dirt and other contaminants collect.5 G* s @5 Y/ J 气源系统内提供管道热胀冷缩所需要的余地的波状0 `0 v. n0 Q6 M5 q! G' X 轫管。! J* ^) |. F2 o& ~$ N! W 空膜盒, % F6 R# V% V5 U& o% Y- C一种具有波状表面的容器。用于量测气压。3 q O3 k) f t* [/ ] 嵌沟缘, 1 N8 N1 }( z' c+ b+ K5 e1 z! q将表面玻璃固定在仪表上的圈状零件。# k2 x8 Q. Q/ T; A/ o' ]6 Z. ?) K& d 压, ) j8 g/ S1 X: T& A) e3 Z2 S- O8 u$ P在控制电路的两点之间的电位差。$ M' L. S0 f6 h# o 机身腹部,( Z t4 h0 W* s 机身的最底部,通常水,脏物,和其他外来物集存于此。 3 u& X$ N: ~6 k5 Z6 NBELLOWS (NO. 1), A corrugated flexible du ) Y' s& d. i$ S4 M8 L* |- v# v0 Gp6 { [% F0 |1 ~: x1 ?9 Q3 W2 m to3 p6 F+ ], f+ R4 g4 }# E: Z B# R" k6 [. z2 U c 2 S% D. G( u7 S3 V0 CB7 {2 N2 B6 p# u; M& J g % A; c& T: J& P8 y8 PB, ^0 n# P/ u" k/ v; b* | p7 O. w0 y& O) k8 r/ F, @ 直角摇臂,- ~- A/ L4 f7 @% u/ l# X! R 在操纵系统中改变运动方向用的双臂摇臂。9 v7 l" g. {* z 波纹管,3 ^; Q; h2 y3 G) X0 n. w+ P! H9 D, f6 B5 x3 I! b2 q5 i# v5 W0 O* @5 {/ a x. G! W7 }* y8 P/ a, F5 T8 J! r& v" t2 K0 l h 英汉对照民用航空词典B OEING" u7 F, v. S) k4 ?9 |) F% h TECHNICAL DICTIONARY 20 * v% Y m# `2 H, p# q; MBINARY CODED DECIMAL, A system of coding each / f: R6 ~% K0 cdigit in a decimal number using the binary equivalent. ( O* ?( ~; `$ z2 Q8 ^# e nBINARY NUMBER SYSTEM, A number system using4 B+ s5 s2 Q7 D$ U s0 L# I- i* |- |- O8 x: J7 \ IT, In the binary number system, the smallest unit of) @. ^7 m, B4 S( J$ e3 r" \+ y8 H, h8 O formation, consisting of a 0 or a 1. ( E- G! g6 T6 B. N# D6 _& CITE, SEE - BUILT-IN TEST EQUIPMENT 4 y, Y: E+ G0 l0 LLANK DISPLAY, A display that does not have any ! n8 y S) i+ S, T2 R: pdications, normally due to failure.0 }4 W2 M$ N5 h4 @7 ] LACK BOX, A container for electronic circuits to record/ h/ z5 D( D7 _% Z# E1 j ight data., E4 \, f# z$ E# f. y0 Y LEED AIR, Air taken from the engine to power various) F* T, ~2 u6 I; ? ircraft accessories. . B" b& W2 E% `+ R7 XA valve in the pneumatic system for air8 ~' ?- G6 `7 Y! y9 X/ x- B supply from the engine or auxiliary power unit to the$ g8 }* n* H1 X; }2 V4 x6 v pneumatic manifold. A valve on the engine for reducing . l! O, W$ d1 T! Opressure in the compressor section. ( E% S" @2 p# ?# t8 [2 s$ F. v C进制,, H8 [; a0 u8 V' b3 d2 j+ d 进制, 9 G3 B E& P- g一般用0和1)和2为底的数字系统。 5 W4 X1 a* ^9 _( a: m, |特(二进位数), |' h0 Y" {$ u' t 二进制中的最小信息单位,包括0或1。 * Y( X: B, Y2 ^0 a. u内自测系统, 6 C- x) x4 f8 {/ N% T. k' }1 J见Built-in Test Equipment / }! q1 K/ |2 [- Etwo symbols (usually denoted 0 and 1) and having 2 a 4 z$ ~3 c4 w" {; ]8 Q! Lits base. ! ~2 n# i7 W* F, D' b- y( XB2 h/ B$ F5 A H* \: t in 1 K' b* g& I' C6 t c' yB$ U( Q9 {- `0 \! U" _/ |$ b5 k B5 z# g3 X7 J6 x! p% m in 6 Y8 I* H: k( VB " z4 X, K# V+ _5 w8 ofl$ e5 T! D+ i: X! l" A- N) L6 T% a& w B " u: f% {# R* Y3 ^# k7 @( E5 Ia 3 o" u9 E1 c% ?4 g& n# sBLEED VALVE," _( t1 V3 }4 O1 B 二进制编码的十0 _: n- T; @* n" m% h 一种编码系统。用等效二进制位数编译十进位数的每一 7 q0 a2 E% F% T位。! N: X. n( I: Y" c/ q# [( R1 X- ^9 G; @ 以两个符号( H0 U, |9 c/ r. L. e6 K0 {( z5 b3 p& X) N8 }2 y4 K, W; _0 L2 R, j" k# ~& B+ B: q& |. G .: M9 P7 z1 D9 @# a! q1 T 白显示, & O' Y% ]+ h) y+ [9 M通常因故障而造成的显示器上没有任何指示。' G7 l( M! D. d# d% z' t 匣子, " y g7 z8 |: K0 D. L! O* d l装有用于记录飞行数据的电路系统的容器。/ r5 Z$ K: T& ^: F- I; D/ D3 Q0 q# O 气,( B4 @; ~+ }1 P( P: N/ V( A L; W 取自发动机而用以驱动飞机上之各种附件的空气。 % C! m& q* p1 E2 U/ H4 B$ c1 B* {气源系统内,使来自发动机或辅助动力装置的空气进人 $ P# r2 C% Y3 q! g气源支管的活门。发动机上,用来降低压气机压力的活门。 / |9 y$ F% v: q3 I g' {9 i8 F2 o3 B- ?! D2 {7 O% P6 U q) z2 f( J, U引气活门, * b9 }9 D2 R) d5 h英汉对照民用航空词典B OEING W( e N/ D; M' [7 q8 X* D" ~TECHNICAL DICTIONARY 21 ( ]0 y# E+ c5 C8 ] TBLOCKER DOOR, A device on the engine for blocking , g7 l, _* D: c0 R( O7 cthe normal airflow during thrust reverser operation. : E+ r( w% s! n5 I- PLOWER, An electrically operated fan for circulating air. * u3 ` z( r7 F8 L! mLOWOUT PANEL, A panel in the structure between 2 D1 H8 a G4 o! |. r2 R# jo compartments that opens to equalize pressure in * M/ B) G7 F; ~, K$ p+ n: Z' @e compartments. & _1 \, z% _8 n& WODY GEAR, The landing gear attached to the- ]( f4 V* E+ S, Z grounding.! H2 z' V9 d7 h: o' A9 Y 正常的 ! P X7 n* Z+ [" u+ R气流。! U2 L, B) G8 Z5 u W# `- w 鼓风机,1 s8 V: L" T7 y0 J% |) r 用来使空气循环的电动风扇。; R0 j7 n: C0 [2 f 压口盖, : z- W( b7 H$ ~" y) X两个隔舱之间的口盖,打开后可使两舱压力相等。 ; b3 }& p/ X5 T6 g" Z2 U身起落架, 3 h$ I! s7 P9 m. b2 h. ^* R身构架上的起落架。 6 @; |# w- U7 _2 q qB % c; k' M) f+ t: n( c2 [" IB% p& _3 V$ X( c2 [5 w tw: @1 M/ X3 k/ A1 o( S q3 u th3 B" E1 |& D. U1 z" D1 s ~: Z F B ) J) B9 Y+ x) F# M2 x" B# h( [/ k# tfuselage structure., j* `$ V0 u9 b" h BONDING JUMPER, An electrical connection between" M3 i7 A: C5 e) K+ I) t8 @+ \ a component and airplane structure for electrical' \+ W& S& Y6 @% y1 Q6 H Y 阻流门, ) x* r* K+ a+ b1 T- V' m发动机上的一个装置。在反推工作时用于阻挡 ' B; x9 j8 _$ Z: W/ ?! ]' ^ c2 o$ Y' o k: z* c( ]' B- u. X d3 ?. t: @ 装在机4 }) S' z, f. ~- g2 O 搭接片, 8 ]/ Y, `' A: x; A连接某个部件与飞机结构以形成接地的电接头。, ]; v) Y) {$ `7 Z$ U% z 英汉对照民用航空词典B OEING0 y; y# G( g" I3 o- p4 i TECHNICAL DICTIONARY 22 . _/ l% ^ d: v# CBOOLEAN ALGEBRA, A mathematical system for# s3 Y; U0 @" l% P* _: H! [ writing combinations of logical statements. 4 F: \+ C# m# @4 y6 q; F$ gBOOST PUMP, An electrically operated fuel pump for3 O' O) v. X+ z7 E; g- f) J fuel supply from the airplane fuel tank to the fuel3 X! C* k- q: a: b$ h( k- l; p# @ manifold. + K- N+ N* G( y% y+ Z+ [" LBORESCOPE, An electro-optical device for looking at ; _' c: J; `+ e3 w3 O- A( Wternal parts of an engine through holes in the engine.0 t: F" O8 y" G8 k* b orescope ports) : W. H: M& Y/ u% ]$ v2 F/ r) hOURDON TUBE, A curved flat tube in a pressure gage) b% n" r+ _" C3 y r moving the pointer when pressure changes inside ' H' g+ l% M8 \0 Lon the ability of the brakes to+ E- p0 D0 `. H% l bsorb a predetermined amount of energy during a4 a( x3 Y! x1 }7 ?9 Z0 { jected takeoff. - p: @/ ?' r$ y/ u用于通过发动机内的孔(孔探口)观察发动机内部件的 ; z$ N% w1 \3 M% t* @光设备。 1 c; k/ H t7 J1 R' C- h端管,& y$ p i/ {2 p3 C 测压计内的弯曲扁管,管内压力的变化时它使指针移 & n0 U) A: {$ V力。 2 c5 n2 j7 c5 e' |! h* W极限重量, " k: z- A: m* c7 Y8 U/ L! l! d! }! H 起飞重量。 2 {4 U, e# X* ]8 }8 y发动机滑油系统与大气相通的通气口。, a# S' u; {9 S+ @0 u1 m in6 F! A m" B4 X8 G/ ^3 m+ X: S7 W (b & v) P/ q+ `4 L- B6 D4 U2 ^7 W: G. mB - P+ ^0 A/ V) s+ Efo y5 O; w2 t o2 }( c+ }0 X+ v8 { the tube. 9 h/ [, ?5 R+ O8 T1 _/ o! IBRACKET, To enclose or surround.- T$ Z3 X0 o9 J6 k) H BRAKE ENERGY LIMIT WEIGHT, The maximum# Y$ e( G3 o4 e9 H takeoff weight based. V7 [7 M1 S9 F a 4 P G) w) _4 t+ @9 pre8 N1 y/ s+ ^9 o9 t3 t1 H# i BREATHER, A vent to ambient of the engine oil system. u5 b" ^5 v& }) n 布尔代数,) X8 M0 ?8 K! O9 | 一种用于编写复合逻辑命题的数学系统。 7 t% Q. A. K/ U% D6 r增压泵, & p$ k3 x5 H: h8 L: }从飞机油箱向总油管提供燃油的电动泵。! ]/ h; {0 }! E1 D# w' \ 孔探仪,3 B8 c' ]+ L; V: n# m( Q' ~9 h% w& N) h) ]) v" d' D1 f9 o' K+ ?% G3 _$ B m p 动,以指示压4 j1 [& K: f6 o 托架, 3 x# k' g) Z: G. K' _/ `4 l W用于作支撑、装托、或围绕之用。, h: a& s5 m! u3 o" P 刹车能量. c0 J7 _, X, y% K. C 中断起飞过程中,取决于刹车吸收预定能量之能力的5 q- S1 t/ K/ v/ [( _! ]' E" g5 L$ x% E! i3 G) M通气装置, U/ h s- x3 Y3 _: Z 英汉对照民用航空词典B OEING1 Q8 ^! T Q. ]' `$ j0 i3 e TECHNICAL DICTIONARY 232 r( t9 |) K( s7 E4 q' k5 g+ x( d BUFFET, Vibration of the wings and airframe resulting 9 L# t$ C+ x4 I, [( q& F& lfrom unsteady airflow over the wing; caused when: Q. b: y3 f1 |: a airspeed is too slow, the bank angle is too steep, or $ [* @( ^5 ^( E7 V% k$ K! `0 Jirspeed is too fast./ [& ~8 \2 b/ ?2 }; X: K1 d6 ] UILT-IN TEST EQUIPMENT, Equipment installed on, P4 L: @& s4 X5 R e airplane and in airplane systems to test the systems+ c, a" Y8 n6 \. h ?: ^' c ithout external test equipment.) v+ s# Y$ T9 O! a" k5 L UFFET MARGIN, The amount of residual maneuver - ^) {7 W" C7 _# u/ sapability present before the onset of buffet. 8 l( V3 ]! b+ [5 L2 ]. j S- F4 EUG SPEED, A preselecteed speed to be observed - y6 x3 t2 @* X3 d) F1 d9 s, ]( Knding sequence.' d, n5 p) N3 T! c$ |( P/ W9 p. R k ) Q( p7 y* Y+ ?2 u4 ung landing gear operation.5 J9 T/ t7 n# t 速度太慢或太快,坡度太大,均会引起抖振。 ( _0 X2 y& U0 h; s自检设备, % a8 W+ D2 B" S* d) t安装在飞机和飞机系统中,在无外接检测设备情况下, , A. M) i n* A3 X2 R0 u/ z用于检测系统的设备。 8 V, z5 p! \$ {+ t: Z6 z, @( Y) a抖振裕度, " u5 {3 L* F; j6 x+ z( y: Z飞机在遭遇抖振之前,剩余机动能力的大小。2 i5 ~# B4 w6 C$ Y% H9 H+ V 标速度,( B) T( F# V9 g+ ~% [ 在某些机动飞行过程中,特别是在进近和着陆时,飞机 ! t0 y+ J ~/ z9 w* I1 [4 ^0 \预定速度。& c; U# t6 J6 v5 q- R 力装置,1 v7 w; D/ p+ o, |$ t 架工作的一种机械设备(弹簧或减震器)。 . k" }2 g: U X, F# F; }流条, * G7 i6 H3 \( u" K$ a& B在部件或组件之间传输电、数据、或定时的单一电线或6 U! a" e$ x+ i! X a ) g& u; k1 Q% I+ s! b, `2 [B 3 d$ k8 n7 G" F: Q9 T, \th 7 v* e0 K' N% P8 Ow 5 J+ a! r9 J9 L0 RB . S% g; p: y" ~6 o' s6 p7 pc: P5 X: t& |9 T5 s5 F B' L1 f6 y; q+ ~* L. B( P2 }. e/ S J during certain maneuvers, particularly the approach and5 Q' R" j n3 t' Q0 M( q la % W. c1 k. L9 x) {" z* p. JBULKHEAD, A structural partition in the fuselage or e0 d1 {" m' y6 L2 E' T/ ~/ awing. 8 B4 p. C! |# aBUNGEE, A mechanical device (spring or a shoc# F- N* q9 ]9 X absorber) for assisti, t6 q5 j& l" h* ^% _ P BUS, A single wire or group of wires which transfers ! D7 b" i/ F6 l- ?( `; s4 Bpower, data, or timing between several units or ) @9 q+ M$ F8 k% @0 _& B- a1 _8 y" wmodules., v. Q: z" ^& k' g 抖振, - ]. J1 X: w. N) U- p/ P由于机翼上表面的不稳定气流引起的机翼和机体的振 9 v8 @: A, m2 \9 q7 \* I% J动。飞行, H: G: K! T: ^+ g# I, [7 m6 S2 i2 U0 T! H 所应保持的! H) T; t* E# ^ 壁板式隔框, 5 V7 o9 P$ D8 ?1 V机身或机翼内一种结构隔板。% P. r2 K% n# ^0 J/ J6 u8 |& y8 H, a v9 q' ^, H4 S 用于协助起落 - T5 y6 X0 W; o3 h4 X0 h M7 y K$ L7 z; z) n 电线组。2 m# ^ P" \" u. j8 j" n 英汉对照民用航空词典B OEING 6 Q1 q% E4 |& P2 p; S0 |TECHNICAL DICTIONARY 24

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BUS DRUM, A mechanical connection with pulleys9 R5 L$ c1 N/ d0 Q8 r) q/ z4 ] cables in the control system. 7 V$ |8 {, S: O$ aand! @! f6 S: }6 Z' d l circuits for control and protection of4 `' J/ K7 f4 `& H lectrical alternating current supply to the airplane./ q& y0 n7 s7 U" [+ }4 V* ]& O duct for closing and opening the duct 0 e# \- S4 T* [$ O6 W3 D/ t5 xassage./ j# e$ f! g- A& u UTTOCK LINE, A vertical reference plane along the & n. @. H: L$ O0 Rselage for horizontal measurements of the airplane. & ~0 m% S" L8 V. s接。0 e& d: s4 g1 I; i+ q7 z$ h 组件,内含控制和保护飞机交流电源的电% V: b i& ~1 `/ b0 d& X8 B6 C7 q, t6 d8 A) z6 N9 v- |. N# y G作动简控制的转动装置。用来关闭和* t1 R. v# E4 Y' u 启管道。, q. K- R' s+ O$ x& R 沿机身走向的垂直参考面,用于飞机的水平测量。 ( V6 x2 @' x" v! M ]* w2 n( JBUS PROTECTION PANEL, A module (black box)+ }+ B7 H7 Q7 q- p5 T5 z containing electrica ) h8 R+ r: j' fe f" H' {6 z9 x) m, V) z BUTTERFLY VALVE, An actuator-operated, rotating * I4 }. S5 \+ y0 o) ndevice in a: V8 P! b; M- x3 Z p) ~6 Z7 k: G5 }, R9 N# c) e B 7 L; B9 T9 C" S. Q2 w& k! K+ }fu" N4 X- }! g/ n1 \3 F" z 转动鼓轮, 0 j# h' E6 A% c在操纵系统中,具有滑轮和钢索的机械式连 ( \* A' C- r, B, y! C7 [' h# d汇流条防护板, 6 O/ [8 u4 b7 d' s% \( N黑匣子式的, Z/ t) w0 C$ l8 _& r/ u& ~8 y1 K! O) X9 N5 n& ?2 A9 _) J蝶形活门,1 F8 J% I9 N$ ?" t# j1 T1 m; i 是一个在管道中由) Q, D7 p `$ I+ L9 R: `1 N7 K; m" a 纵剖线, " T; V, l% h# D) P" V2 Q英汉对照民用航空词典B OEING & h% c4 w" h. ?. O/ OTECHNICAL DICTIONARY 256 w7 c0 v" h, t, D" b BYPASS VALVE, A valve through which air or fluid will 1 C9 t& G1 ]$ b: l1 J0 o: Eflow if the normal flow path is blocked.8 c7 _, Q" `; s6 ~. P* O9 I& f BYTE, A group or string of binary digits. A byte is ( m7 f) x; ^: R* R. ~! tsually eight bits long. & |! B; \! S: y7 {9 F+ uABIN ALTITUDE, Atmospheric pressure maintained. b1 k6 z- T9 t( b ithin the cabin, indicated in terms of feet above sea) ?" V- T9 d7 I' R8 ~ ALIBRATE, To repair, adjust, fix or correct the" y/ m3 J& @3 t( W& u( i6 b easuring capabilities of a measuring device. ! v3 W: U3 ], c1 b% fALIBRATED AIRSPEED (CAS), Indicated airspeed- \ C0 a w; j: I) ] AS) corrected for position error. 3 [% j8 B5 s2 Tnical $ ]8 ~2 @5 @2 t0 W% Zomponents. F2 X! z" G3 C2 A- Y2 _+ s8 f, E# \: }5 ~! j! H5 S节,4 T4 L" \5 U3 ^% N 一组或一列二进制数。通常一个字节长8位。 3 R) `/ J' b! Y2 v0 [0 F舱高度, 4 ?2 V5 Y6 G" E座舱内保持的空气压力,以海拔多少英尺表示。8 P* R- l3 o5 {# p0 d/ \5 f2 e 准,( G0 l9 C7 P1 ^ 修理,调整,定位或改正测量装置的测量功能。. c2 B! G2 M0 n$ f 正空速(CAS), $ f, R9 G- P7 A在修正了位置误差之后的指示空速(IAS)。& U: E1 H* Z8 J5 I$ C2 _) i 用来移动机件的一种转动装置。2 g% c' @ ^: o1 w. n( K8 ] u 8 C/ B4 K& i) P$ z/ KC 4 @8 G% }+ d! ]' L" r) oC5 F' P3 p8 x# X; s9 A4 i. x w 1 U; f( a$ r0 B, b( z" blevel. ! U8 v0 i ~( EC & c% M: s+ x0 ]- i" mm9 u0 j6 g. y. `- `- } C |' q% K3 [% ]$ d& C(I/ v- E! ~ M$ h' |" C% `- f; L7 [ CAM, A rotating device for movement of mecha - d' F; a+ e; a+ w. AC. U4 c2 @9 F" }5 k- |8 Q- D! T 旁通活门& H% U; B# ?, r4 ~2 c. R. B 气流或液流在正常通道阻塞时所经过的活门。) ~) Q( p1 Q* ?/ c! y( C; z, e/ d4 w. b8 E0 P0 N+ k' T/ L+ ~( ?- p; `3 P/ J- e5 i5 R* h. E: e4 [6 @9 y# R2 g) J凸轮,6 M8 b$ P9 F9 B% V$ W 英汉对照民用航空词典B. G7 L" w% [0 R: Z$ }+ l CAM-OUT, An autopilot condition in which the actuator0 Z6 |+ P& m: Q0 L detent piston is overridden, either manually or by the . \* t9 c0 o+ V: P9 ]ther autopilot actuator. 7 K4 r. J% @$ pAP, SEE - CAPTURE/ D" b3 M! f$ o APACITANCE, The measurement of electrical energy + z" l. x; d1 o. \; {5 ^: k. Y4 e6 E- Ptored in a capacitor (condenser). . D6 ^8 E; E. ~1 j7 |" uAPACITOR, An electrical component of two metal 3 C$ }, r$ U0 B5 X: l( O% glates separated by a dielectric material, for storing 2 M. H* a2 |& A$ ^lectrical energy.! U. h/ x% Y5 v3 K CAPTURE, An autopilot or flight director function to& D ^" b7 |7 u acquire a selected mode. 9 s8 _" g( g4 W# F0 U1 {8 t$ MCARD FILE, A container on the airplane for printed) B# t1 t- p, X7 x& V5 D% X circuit cards. ; F9 O6 T& [/ P一自 5 k( U# m% U3 f1 u/ g% D动驾驶舵机所超控。" G) F: ]" B# f+ n# Y4 \ 截获,6 [3 L" Q }+ M7 ^4 [ 见Capture 4 `* _7 \* ]9 { no , p8 Q% @3 B9 RC % o4 v7 u* X# w( W5 n2 y8 jC" A3 P6 k% q. U4 h; L s 7 a4 E% D# S- L7 KC , x* t! x+ ]% j( T) ^) A5 {3 f' ]- _! J0 kp - h9 ?; Q; S7 z$ K: e4 n) n' \e Q/ y' e6 p/ t8 Z' W* x) j5 }凸轮不工作,% h" f7 Q/ G1 r 一种自动驾驶状态。此时舵机锁定活塞被人工或另 . W# F& n- r7 N7 o/ ~6 n6 Y# S& J- Y) I; x电容量, ' d/ a) P- o8 S( u+ S4 ^1 F电容器内所储存的电能的量度。 4 _ _% F$ ~# {( T& V5 H7 `* T容器,; p0 V: l$ p4 ?8 @8 O5 | 两片金属中间用绝缘材料隔开的电器。用以储存电能。: L0 N( m! `& i3 l4 X 截获(CAP),1 Q. m& H+ U/ i 自动驾驶仪或飞行指引仪的获取选定方式的功能。 8 V* ?! f' m( _, r$ R, p线路板盒, 5 d9 h( C! R& V/ ^1 c飞机上安装印刷线路板的容器。 * k" Y0 m( A9 Z5 h% V2 y( K _! X# A5 J; H OEING- P- J' T# p" N& ~' s TECHNICAL DICTIONARY 26) S# k$ y! C* e 英汉对照民用航空词典B OEING1 V6 q5 P2 U) T3 G2 } A TECHNICAL DICTIONARY 273 W7 P: [0 U/ M/ w0 L CASCADE, Two or more similar circuits or amplifying 8 L0 |' X/ H$ I2 T0 \stages in which the output of one circuit provides the 0 ^ E# V1 M' }$ g" Z& Zput of the next. ' Z0 m! B* N3 J3 v7 _+ aASCADE VANE, A vane for turning the engine airflow9 N0 Y% b. n% B ~, `& ^ uring operation of thrust reverser. * p* Y& ^" m; q/ g. i" X6 KASE DRAIN, A drain carrying lubricating and cooling + E A: F: L q/ y, ]uid from a hydraulic pump. # D4 n1 q3 ~. q7 b6 LATHODE, The element from which the principal( b* ~7 N4 ` L5 ?+ H* o tream of electrons flows.3 v$ l$ ?4 N: R4 g1 M7 [ ATHODE RAY TUBE, An evacuated glass tube with a 6 Y u7 x8 ~$ o' eCEILING, The height above the ground or water of the$ W/ K6 E( a; d( E+ c' L base of the lowest layer of cloud below 6000 meters 2 j4 o; D. { N/ O+ L: u(20,000 feet) covering more than half the sky. 2 P, T& i0 |+ f+ a; C! u a程。该 0 ~# b" z/ u; U) e程中,一个电路的输出为下一个电路的输人。* g" N2 j+ ]3 a, B2 c- Y* m 叶栅叶片,+ O" j9 a k. t" j' ?4 M 在反推工作时,使发动机气流向相反方向流动的叶片。 - c; a- f0 [7 Y3 O匣余油管,9 h+ l; L! }# r3 O 液压泵多余的润滑液及冷却液的排放口。8 ^( X" S% @$ i2 V4 @ 极, : T5 P T( C! c% p: Z2 Z# C电子流流出的极位。8 u- I1 l. c: S' ~& Z9 ?8 l* ?8 b 极射线管,0 d8 R' P3 T5 @: Z- m 有显象屏幕的真空玻璃管。用于显示信息。 * k% v9 O X( F) s云高(云底高), - ?+ i% q: q% h6000米(20,000英尺)以下已覆盖一半以上天空的最& i j0 Z: a$ A8 i% y4 P 低云层底距离地面或水面的高度。. s) j. C6 @2 z6 Z) @ in8 e, [9 [6 a% H C 2 b# g) M6 u4 E# _5 G# p( pd& K. X9 ~ ]. s: ]( W C; ?6 T6 W2 u' A" k" Y fl 2 H0 w3 b4 E* QC - Q; m+ F9 C: ]s9 e# D! o7 d% t$ M& n& o) ] C) d+ c; q* @2 _1 _5 W$ u( I viewing screen, used for displaying information.0 p- b5 e" A* O2 k( J+ k+ N 级联,: e/ D+ G* s' b8 r% w! y 两个或两个以上的类似电路的逐级连接或放大过 , ~# G* T6 d' |( P, G" j. o M9 G' y+ s& W1 a* b9 N7 O; {, e, E( u v% z' k: e" I9 g" E4 w9 L1 t; ^$ d8 C* L% {5 Q. H2 ]' x. w3 Q" {$ D8 @0 J! F3 `/ @一个具 " e9 y) ?3 \2 C0 t英汉对照民用航空词典B OEING 6 J0 c; T/ i3 n7 qTECHNICAL DICTIONARY 289 ~7 X5 T2 L8 ~( B) }+ |; @) Q: h; f CELSIUS, A temperature scale in which zero is the 5 P: `4 j% M! |4 X+ _; mfreezing point of water and 100 is the boiling point of& B8 M* j C: v& J; H% B water. , d" t* f; h+ f$ v4 NCENTER OF GRAVITY, The balance point of an object 7 H8 W. ~# b+ S+ a7 d/ T. Cr rigid structure expressed in terms of percent Mean $ _3 ?: {0 _% d8 D* P/ |. F6 l0 zerodynamic Chord or in inches from a reference point. - D# ]+ j' U) P9 F8 z8 v! |4 VENTERING CAM, A cam for moving a mechanism to a $ l8 g4 Y: M: A0 U* A* C. t* h+ Veutral position.5 K3 O W- V$ `8 q, U- Q' L IGURATION, A configuration of the* W8 g% z) ~7 _ ircraft approved for operation by the local governing# a5 r5 @3 X. C gency. , }* z# s% u, R: T: N G( Z6 U' JENTRAL PROCESSING UNIT, In a computer or : I* }( A7 [ Sigital circuit, the section containing the arithmetic and # K/ u; C. X7 D1 [3 G. Fgic,control, and internal memory circuits. ' y; }2 s! Q3 U2 @$ C( {ENTRIFUGAL FLOW COMPRESSOR, A type of , a9 A% B" d5 w. P0 h) gompressor in which air is taken into the center of the& w: d! J# ^! P$ k/ c: a) p1 u peller and is slung outward centrifugally into a diffuser1 l4 C1 t1 T% |, M+ z here it is slowed and pressure is increased. # S6 M' e: p5 C; i+ _% YCG, SEE - CENTER OF GRAVITY, u/ z8 Y$ [- X( D* E5 n% ] 构的平衡点,以平均气动力弦的百分比或9 C0 Z7 [% R6 T. }3 ^ 某一参考点若干英寸来表示。 0 w, U" [' @9 u! j1 x% k5 C中凸轮, 6 R9 M: y: L% G! ]. X1 t( P将机构移向中立位置的凸轮。 9 G: }2 H& {1 Y) D4 G: V格的装机状态, ! U+ s* V0 o8 }由当地主管单位批准使用的飞机装机状态。 1 {* w9 L$ n. i# F$ N# T中央处理器,% N& H% B( u" W7 O _; z! A 计算机或数字电路中含有运算,逻辑,控制和内部存 + s. ]% P# N4 G( l; V& ?/ ^储电路的部分。% V& D5 w: b9 U+ D- R4 D 心式压气机, , a0 U0 P: F! J压气机的一种。当进气到达叶轮中心时,被叶轮离心抛 : ~# L5 U6 R6 |, t进人扩散器。在扩散器中气体流速减慢,压力增加。 4 H; T5 }" S# H9 \, [9 Z重心, * C4 ~) N7 O6 v见Center of Gravity 4 K6 i% K8 z) v1 D& O$ w) wo4 {& ^8 [" {' h: V A $ M& s3 w1 Y, [9 t5 pC * E* T) `- y; r2 V5 H! qn 1 P' F1 I- T9 g/ \6 `CERTIFIED CONF , m$ x8 N! n& E' { ta1 [- |+ G7 v8 W. L: U a * [. n$ n5 s7 `( U- R. x; ?. i iC - n" d; X* H, @0 ^. Y sd' [6 C, |# u2 Z8 j7 U lo4 Z# |% p. y3 S# h3 [& N" ` C 4 d; N$ i8 l" z0 l: w0 }. X" Jc * A0 h1 C P. t: e- eim, X" `; Y/ I' Z0 x9 w w @! O! j& N. B1 S9 W" y 摄氏度(°C), . z5 Q B/ A6 W' q( G$ M温度的度量单位。在此单位中,0°C表示水的冰点,% q% p j" p2 C) \4 k4 A/ J 100°C表示沸点。( c I8 h" D+ U: J( m 重心 + g: i7 A1 }! w; T7 v# n# @6 E" Q物体或刚性结# T9 w- M" ? X$ }+ C4 u) D" x! I U4 y* z9 F9 c5 _( S0 q% B$ V U! u8 q: n) p1 c) Q5 j+ t5 U" k# G: G7 z. ~6 D1 V9 J$ C# T& i0 P6 S, j6 q6 g英汉对照民用航空词典B OEING- q' b( ]. P k$ W TECHNICAL DICTIONARY 29& X! C1 A8 z6 {4 i0 T* R) @' ~ CHANGEOVER, Conversion from one mode to another.4 I; ~* U2 u& p4 A: G5 @ HARGING VALVE, A valve for supplying air or fluid to- p6 J `- {9 O) v k: R# g7 E HECK VALVE, A valve allowing flow in only one& t3 J! W6 p9 Q* o& R& @ irection. See Non-Return Valve.; j+ N( c: X6 }+ P HECKSUM, In a computer, a summation of digits or* B" U: |$ O4 f" }4 _. z its which are primarily used for error detection. " t/ o2 n# U( X+ C. [: tHIP DETECTOR, A magnetic plug in sumps of 7 q% i- V# r* }; W/ n% X1 Ebricated components for detection of internal failure of 1 C9 k/ L2 [3 i, Ve component. 6 w( }% y6 o* Y- o( dHORD, A structural component of spars or frames.' v7 c N/ d6 P I 添活门,9 z- J9 b7 `$ C; t6 y8 Z 器充气或加液的活门。 % S' q) n2 s2 V/ r& n8 j9 M/ X单向活门,; H" q7 W& u& o: s 仅容许单向流动的活门。见Non-Return Valve

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发表于 2008-12-24 21:38:05 |只看该作者
C) }- z# m: o4 s* s) g9 U1 h a reservoir.* |' M5 g7 F R4 m& d C 2 a( F+ ]- T- {1 g, Q6 ~" kd 6 [; l. n* C- |' d9 l OC1 j4 X( n* p4 ~0 u( e b " Z V# m1 b, ^9 zC8 o, q7 d% O2 T; I% K! P( }' o lu 2 D4 P1 y x' \% s4 i' eth @9 }5 o3 U9 } V) D' X* W! cC ' d8 k% E: h! n: w# o转换, % A6 K- K! f( }- c- o9 g由一个方式转换到另一个方式。 - e% I; m, D, I, E, K8 A" D+ K2 W' P5 h' V2 ^ 用来向储存) ^) K2 Q' `: J5 Q: }: q# {; c0 B- l3 P+ i! B$ G 总和校验,8 ?7 @( G6 r) ?; U; b$ E2 i) h 计算机中,把那些用来探错误的数宇或位数的总和进 / Z! e, G$ C, z& I4 {% s( ^$ J% I9 u求和计算。# u! v* Y9 D p& g 属碎屑探测器, 5 H x% }1 {; |5 S+ x$ N; C装在被润滑的部件滑油回油管路上的磁性塞子。用来探 2 A! y: M3 v: _, {4 Y3 r i9 `部件内部有无损坏。1 b3 w. |$ Q5 G 弦, # _1 z) z% X' k$ ^* Z2 q* W梁或框架的结构部件。! j2 V5 G8 L O; r5 p9 P; q+ i3 E$ O! a+ W5 B. S1 h% c5 @7 r6 Q; h$ a4 b% a2 `( m! j! ]- c2 F) z0 \' d4 g }9 x& g% B' a; p! M- }英汉对照民用航空词典B OEING! d5 B! j K2 { X5 ] TECHNICAL DICTIONARY 308 A5 T2 H k2 u3 t0 e6 E$ M) H CIRCUIT, A closed path through which current flows% {/ B' X1 ^4 F8 b1 V- g ource.0 V, O( m3 L5 Z! @. ^; J6 \ C: k IRCUIT BREAKER, A device that automatically' h4 l0 x/ a; V3 m eactivate the system.+ \+ k& E- f: \! U: m lear of all non-frangible objects which ' k3 y2 F, p% t' ^7 iay be used as takeoff distance available when 0 d: P1 g( g% Dalculating a takeoff weight.9 n; ]& Z, W( ] r water under the control of the appropriate * U! @5 r; d& A: Authority,selected or prepared as a suitable area over N) ^6 z2 ?" U; {5 k* N G hich an aeroplane may make a portion of its initial c' K) B! F. O limb to a specified height.$ f# x% E( r" e# O increasing.0 I+ r$ z- L, p3 F* H sed & C/ @2 U z' `2 ?LOCK SIGNAL, A continuous string of pulses used for8 u7 i: v2 g; Y+ e9 K1 ? 开关, * g4 S, ^8 v/ L; m# \, Q故障情况下自动中断电流以保护线路不受过电损 - j( M% g8 d2 h3 F8 Y, d体障碍物的区域。在计 : }$ |3 E* t/ o起飞重量时该区域可作为可用起飞距离。! a: G% M: W7 S' `5 Z: t. u( k- ~0 V9 J 是在有关当局管辖的地面或水域内一个界限明确的长, ~0 l2 a, Q, T6 | 形区域。在这个选定的合适区域内,飞机可完成初始爬5 V* u0 P2 |7 o& x# x: b 的一部分,上升到一个指定高度。7 T" D) |2 S# v9 l+ @2 t 飞机高度不断增加的飞行阶段。+ k$ Y0 V: a% H) Q$ ]6 s 钟脉冲,+ c% h8 R; r# ~ 步的连续脉冲信号串。# m( f& Y. r# \* L1 W0 \& D# c from a source, through various components, and back ; s6 i0 [* y# z( E# e. Sto the s4 `0 j& g& H+ N G& Z. F C, {: ?8 m. g+ k2 e: b interrupts the flow of electricity (current) during fault0 a. k: r( s" R% C. y" `8 k condition to protect wiring from excess current. Circuit ! L: o- S' h z% k7 P7 H: obreakers are also used as a means to manually 9 }8 w+ C4 a9 y1 p* G) `2 D: x- M9 yd , E+ p/ S6 Z- B6 i5 V; dCLEARWAY 1, An area beyond the takeoff end of the* A% F! P0 C- s6 @ runway which is c. R+ F0 [! ]6 W$ i! _0 e6 j m( k3 H! ]$ `' s* g0 F& k6 h/ M c6 I8 ?$ W0 o F) \: K2 r CLEARWAY 2, A defined rectangular area on the$ o7 B' N; \8 G; F( x9 w- | ground o 4 m) q" Y" @6 }0 Ja % p u- F3 `0 E6 jw2 u& _& b1 m0 r c& ~" _6 k) f4 y# u& Z8 I G3 z, ~. n CLIMB, Phase of flight where the altitude is 8 F! g* c9 \, l$ {CLIMB LIMIT WEIGHT, Maximum takeoff weight ba) m7 t! p/ A ]( h8 ?! \. j) P) T on a minimum climb gradient with one engine 1 Y' ?/ D- O, N# [% Ainoperative.8 B. s8 a Q: G; S( J, `- ` C + h9 ~+ x! m x. {# \8 Nsynchronization.& C+ t# S, R2 @ 电路,; U* i2 v& A& |1 r6 h0 h7 A! C 一个闭合的回路。电流由源头流出,经过各个元件流回 ) S/ a H' L# G0 C7 ?源头。: y, Z( }2 M6 ?+ y. V2 a4 k5 ?9 p4 K5 o1 Z 能在 [! C- T/ o" y坏的装置。跳开关也可用于人工使系统无效。4 L# l( w# h' v5 p+ C; r9 r: |( q 一号净空道, 5 O m4 O; P# H是跑道起飞端以外,不含任何刚" M! C2 N/ ^; h" x" H% p* |, m7 t& H' a" C& O3 S+ i 二号净空道, 3 w3 V* r$ @0 w1 _- P3 n5 k7 ]% n! j% W( Q8 |: l P5 Z( M% `" H) h5 h6 f9 Y( U4 O 爬升,, @# l* t1 O; i: Q0 t' t 爬升限重,2 @2 ?" T' r& l4 g6 y& Y1 k 取决于由一台发动机工作时的最低爬升梯度的最大起 $ k: w _/ O% N飞重量。; S$ \' x$ j, {! U( _% w" U: k- }9 e q2 O( c4 A 用于同0 h, D" p9 P9 Q& | 英汉对照民用航空词典B OEING# S. e' P* q9 T* P TECHNICAL DICTIONARY 31& Z2 _. G! c- W+ b5 X COALESCER, A device in the water separator for1 ^2 J/ {( L& G \4 ` ollecting moisture from the cold air., _6 z. s% h. B! J' R; q* U n antenna with a receiver or transmitter.0 d: ^! Q9 \0 e) x he cable has an inner conductor and an outer1 |0 r, x. R& C3 G& K n rounded shield.7 U/ }6 x. v) a! K ting one inside the 4 ?$ @0 D, s* K2 ^ther for rotating the low and high pressure ; X1 r4 Z1 ~5 xompressors by the low and high pressure engine6 I( ^! W4 v7 p* o rbines.7 k* H9 [8 V$ Z OMBUSTION CHAMBER, A part of an engine for5 f4 _3 G/ \( `0 r urning fuel in the air supplied by the compressor.5 g2 ~! f. `0 b0 P/ t3 K 置。 * E. e; C( _; y& y射机的电缆。电缆 , ~( y5 |4 p; h- J9 ^中心导体和外层的屏蔽所组成。 * _9 h& [2 n) m! @; k两个套在一起旋转的轴。用于使发动机低压和高压涡轮+ Z9 A) P" x; X/ l+ ?$ A/ ^1 @ 别带动低压和高压压气机。# c9 u- y* Q% x 烧室,4 N* {- y7 p r7 } 发动机的一部分。用来使燃油和压气机所提供的空气相 e/ z0 |+ R% c9 F$ m- a合而燃烧。

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发表于 2008-12-24 21:38:35 |只看该作者
c) b- g9 X3 F0 s4 B: I COAXIAL CABLE, An electrical cable usually $ ^4 T1 J9 s! {) R, U: N5 cconnecting a. Y* w1 T1 L4 n& m T 9 j0 J& d/ m4 D$ y' d3 Ig- y' y+ h8 p2 P" [# ^! t5 U COAXIAL SHAFT, Two shafts rota * [ i& x& V" w# E2 O" O" p/ Ho q5 a- [0 v( M6 tc : D% a( \. O' _9 ctu & g8 G7 w L5 GC+ b3 y: ^" Z* K4 x P b $ a3 E; ?$ h L |+ w* O凝聚器, ' B* B' u, U. `/ p$ ?1 D1 I水分离器内收集冷空气中水份的装; z' y4 B0 _, b4 G: B h' J) ` 同轴电缆, : G8 p$ D9 \! J5 u一种通常用来联接天线与接收机或发 ) V. V$ C4 ~" S: t0 ~0 K8 l8 |9 C% t: t/ l7 h2 x同心轴, , j' ?! [# C' h5 z$ W4 a( v0 q2 E$ g2 Z8 }$ V( t, S1 M) d1 s& B* S: A' U* z. v) w: n$ K( n, G5 X0 Z6 c" J4 ~6 x I 英汉对照民用航空词典B OEING " D: u1 b. w- }% G2 o# _TECHNICAL DICTIONARY 32+ S3 c) N" Z! m a+ G, e; M+ ~4 l COMMAND BAR, A flight director pitch or roll comman7 X1 B$ e# B# n, V- N* D4 J; { indication. # w) A- n1 J( c* L* R4 ]7 Fd 4 A6 @) e! X( \6 HOMPANY ROUTE, A route flown by the airplane; T. c$ M+ ]% L4 s% p OMPASS LOCATOR, A low power, low or medium7 a8 D4 E/ J2 C5 j$ e# h5 \ equency (L/MF) radio beacon usually installed in / N, D" U' @# O4 D$ C3 j9 E2 vonjunction with the outer or middle marker of an _% B2 k7 x0 g* Y3 etor (LOM), A compass : y! P2 m" O) ?; U4 ?locator installed in conjunction with the outer/ r7 [3 x! ?7 d* {" r [2 |; B" b marker of an instrument landing system.0 L: t: A; W+ K ss : W' i- ^. x3 {- \! m$ cle3 ]% h* A+ {) e% Y) l3 ? S0 r2 [ OMPENSATION, To offset, balance, or counteract. % H+ \3 {) c+ |# lOMPENSATOR, A dual capacitor for changing the fuel7 [5 Z! J$ M r1 O# `2 O g$ G aging circuit capacitance due to changes in fuel( Y% a' Q0 \) c. x( r, c0 i3 V ensity. 3 W+ C; s2 {8 q3 L+ C3 BOMPOSITE MATERIALS, Non-metallic materials used ' @% u6 i6 \' Vr airplane construction. Fiberglass, Nomex, Kevlar, 0 f9 A3 l- d) W1 s1 Rraphite Epoxy are composite materials. : \% u7 h" g" X; g5 O) ~( J司航路, 0 L/ h2 i! J" N( } w在飞行管理计算机数据库内由航空公司飞行 0 G6 S$ q: ^# H, L* H0 u盘定位台, ' q* C0 u5 w7 B' M$ L/ X与仪表着陆进近系统的远距或中距指点标配套安装的! I0 d+ G0 x, [: D( [. g 功率、低频、或中频无线电信标装置(低功率NDB台)。. N5 u) {+ M7 @ 程序中用来导航。 . G) P' G) f L! F% R% p; M1.远台, . |. T( T! x& h* c与仪表着陆进近系统的远指点标配套安装的罗 7 O( z' t0 H* c8 a盘信标台(NDB)。 ) b) `* [4 \% k* K偿, 7 t' @9 `- S% I% F' D# w; X1 G% P抵消、平衡、或中和。 ' Q/ q* s# i( |8 S偿器,- d# r7 a- E) B% p 在燃油计量电路中,用来改变电路上的电容,以与燃3 Q( k& ^+ j: | 密度改变所引起的电容改变相抗衡的双电容器。 # `) ~* a$ Q! w! J" ^- q合材料,9 Q2 X: d" G8 L. H8 y. ?. y [' j 用于飞机制造的非金属材料。如纤维玻璃,Nomex, + B* y/ r! F0 m3 f9 c" ?evlar及石墨环氧树脂等,都是复合材料。

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发表于 2008-12-24 21:39:01 |只看该作者
C* g2 z0 [0 b, [7 s2 F! G+ S. }' } operator that is normally stored in the flight ! e! Q- q. j+ @. b# |- jmanagement computer's data base. " e/ m) i% z* u% a0 |* ZC, V$ U4 D; Z" d" R" n* T! z fr 7 w$ f! D; b& X; x$ d, gc( t( U* O0 N8 q3 Z( R& k: [ instrument landing system (ILS). It can be used for 9 e K) |; O8 Q. Y8 s: Inavigation as authorized in the approach procedure.5 \: }8 ~7 M- }4 w3 d! H 1. Outer Compass Loca" E! e0 M5 y8 s R 2. Middle Compass Locator (LMM), A compa : C. |# I" J/ b% g, Dlocator installed in conjunction with the midd - m E/ ^/ W6 s/ _8 @marker of an instrument landing system. $ b& b" o0 ?' f L0 ]1 V" X; PC: d/ s1 R0 L& r; f- M% g C c' b: @+ v" I$ qg$ i& w3 @/ I+ @( n3 M5 l4 J d, l/ n& {" ?5 ~; z: ?6 G C* d% N7 @$ Z: X; I" k9 g fo$ |4 L9 [0 l1 Z, O g" ~) ]2 ^. O) _, B) H 指令杆, ! u+ Y* t7 _( _5 q飞行指引仪俯仰或坡度的指令显示。: n: P$ }: R" B! u6 n8 w" N1 ]% b+ f4 t 通常储存 ! }. W! K6 N# S, ?6 p的航路。) }0 E% A Y, y2 n) S+ p2 b& I( ^& D' I. x( F/ ]: X3 N G3 q* D7 @* V" h8 f" l) v 经认可后在进近 7 Z! M2 Q4 j1 j. m4 v# d' h2.中台, * v4 Y9 J! b% j0 @' |" P与仪表着陆进近系统的中指点标配套安装的罗2 g( ]6 s& S+ w+ F( H; S) ? 盘定位台(NDB)。3 Q9 `- w1 S/ G( E" {% T4 J+ W, s6 v( u" u' S3 n9 n" O2 N7 ?. _$ z, D+ e. D7 Z' {2 t3 U: y, d' J& C5 ~* c8 F0 m2 }1 d0 Z K # I/ l! y$ {2 B$ f英汉对照民用航空词典B OEING- \8 X; a& Y9 ~3 ]3 V TECHNICAL DICTIONARY 33 $ D/ M& I3 C5 Yby - K) q0 ^% ^$ @8 o9 `. bor increasing air4 d/ b0 ?( ]& o. k3 T1 m- ] ressure and temperature before the air enters the# P$ t( L8 ~% a- Z% }7 w5 {' n2 P ombustion chamber, Low pressure compressor - front- h! ?. l, s5 O* i! {) S, [/ u ection of compressor, High pressure compressor- rear 4 V* N- T3 F$ m( }8 dOMPRESSOR STALL, An event that occurs when/ r: y. X& Y6 h7 X" E9 X! O ere is a complete stoppage of air or reversal of air flow ' R; j' M, _8 g; w' iCOMPRESSOR SURGE, SEE - COMPRESSOR9 a+ e; ]6 ~. X! a( `( B STALL COMPUTED AIRSPEED, Indicated airspeed2 Q4 @- {9 B4 S- d8 c" j corrected for the static source error. 3 B7 G% p/ u- ?1 ]* O$ U/ o5 F: V的机械轴来驱/ f7 ^) q4 v2 X9 e ,用来增加吸进空气之压力和温度,以供燃烧室使用。 d2 i- I- J- ~5 f: ?; J# M5 J: P压压气机—压气机的前段,高压压气机—压气机的后# v. Z/ e# |! B2 {7 p$ z+ X- @* V M& [- F- V* h% s) A- r# k& c# _9 M 气机失速,6 l M' C9 R) z4 w 当气流完全停止或通过压气机时气流方向逆反的一种 9 J( u4 ~% D0 L' k5 p T; Z压气机喘振, 2 f3 ~; \& f- {6 U# l5 \4 y见Compressor Stall# _+ S0 X2 x! W; V' m2 _ COMPRESSOR, A rotating part of an engine driven' P" ?: U5 ]2 ?# A0 O( O4 ` a mechanical shaft from the turbines f 8 @6 E3 e- u, p1 @p $ T. }% H) b2 j, f: R/ [. ^3 x) a. _# Ec 1 h/ ]0 [+ K+ F# B) p; Ps % r& T* F) L" t7 F* Bsection of compressor. ) B; l/ G6 ^0 ^3 p" Y. I2 cC, ~+ k8 w. D6 p8 G. l( A! @ th $ F7 M" P" t8 h; ~through the compressor.2 d+ ~. l/ X2 C 压气机, 2 f0 x/ Z( U& d发动机内的一个旋转部件。由与涡轮相连 y9 g; \) v3 J* D; p* `2 d- {' H, @% ]0 j' T n3 I( h" _( m: p9 i9 I: z5 J2 s: `- W6 y! O s1 v. j现象。 0 d, b6 `' ~4 b) h, E$ h2 S6 u: \) m* _8 t& x计算空速, 5 B1 |4 ]- |; @1 \: \# Q: E修正了静态源误差后的指示空速。, X. d9 d9 |" y" S) Q% I 英汉对照民用航空词典B OEING3 m& Z- a2 G- o1 w+ q TECHNICAL DICTIONARY 34

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发表于 2008-12-24 21:39:27 |只看该作者
COMPUTER, A device that performs arithmetic $ @& d E7 q* p+ B) Zoperations, manipulates data, and makes decisions. 3 m# {; T' y1 c tditioning 0 O* A) x9 n: w; Ythe air and the . D# R* d/ I# }( B, ]frigerant or moisture vapor is changed into a liquid.. s+ a# P6 |' Y0 H ine 6 v9 ]- \* w5 P. lONFIGURATION, The position of flight controls,, I$ c& ~8 o8 z1 y. q9 X missing which & O$ c9 o+ A- n: k- Dmay affect the aerodynamic performance of the- ^2 h4 r( M$ a6 [8 K airplane.5 n4 [1 p$ C9 F9 S2 j2 C 置。 ! [( L, H. E7 ~2 q* |# @3 E9 Z中能使热能散发到空气中,以及使冷冻剂或湿+ b1 y9 }# U/ B: R 转变为液体的部件。2 f% b. D) d4 t% [7 w* V 连接到飞机结构上。 # h9 g$ A$ E1 \& } ~2 g- f5 ?态, $ q0 d1 _. Z) X定飞行阶段中,飞行操纵面,起落架等的位置。7 ?# B! d( s- i ~) K7 s, g ), 9 S/ ?7 _9 }' m受到影响。; z/ |2 H; e: X" [ L: z" y" _. r CONDENSER, The component in an air con/ ^1 Z/ v3 s1 p1 _6 Z8 N system where heat energy is given to2 [8 Y9 I5 n7 |" O3 [: ] re d; U9 i9 }/ F9 o CONE BOLT, A bolt in the shape of a cone for eng . _; B: t& a# e# wattachment to the airplane structure. 0 ]( V' F/ R6 L+ \; }C ' W. o; }# ^! _+ Jlanding gear, etc., for a particular phase of flight, e.g.,) b' g0 l( @ W$ o; l) i' L+ A) ? Takeoff Configuration, Landing Configuration, etc. 4 z& r ?* f7 t" xCONFIGURATION DEVIATION LIST (CDL), Appendix ' M8 X7 p4 Z m# \4 j$ rin the Airplane Flight Manual (AFM) allowing operation : r8 a* ?. v/ m( \, b- Bof the airplane with certain airframe parts # }, a5 B! t/ D+ h$ t计算机, f# ~- T$ _9 B 能作算数运算,数据操纵,和决策的装* G$ t/ w P M! R, {4 F( G5 q( m; Z 冷凝器,7 B/ c6 p) b- ^6 A$ \: b6 ~5 G 空调系统" n8 i3 k& w R$ r( d+ k/ S, C+ a9 k% {1 y& a4 C 锥形螺栓, }3 o; l& e) o 外形是锥形的螺栓,用以将发动机; Y7 j# B# C! f2 T# }9 ^1 P n+ I, W2 z/ H1 j 在某一特 " H; _' V$ x$ V0 v9 s如起飞形态,着陆形态等。 3 _; {% @' Q" p, n3 z; ~6 M, r7 D缺件单(CDL" q- Y- ~: r' N# [6 |+ p 飞机飞行手册的附录所开列的飞机上某些零件的清单。+ X: ]: N% v+ n. G0 I4 w 在缺少这类零件时,可以飞行但气动性能可能 7 \( V9 ?# f# l* a N英汉对照民用航空词典B OEING3 ~ u9 h: J" D TECHNICAL DICTIONARY 35

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发表于 2008-12-24 21:39:49 |只看该作者
CONSTANT SPEED DRIVE, A hydro-mechanical4 r' h! P* Z* Y component for changing variable engine gearbox speed $ X0 f' g2 o1 _: z9 y6 _ONTROL AXES, The three axes of the airplane which9 \- S. Q( v$ i/ L* S# q re perpendicular to each other and pass through the : Z% _7 }3 l% C( @6 Tenter of gravity of the airplane.5 k) ?/ G( a' D! E" @, J Pitch axis - Horizontal or lateral axis, passes through 4 @3 i' G; ` [. h5 }9 ]the airplane from one side to the other - ; H8 Z( i9 R1 ?nose up and nose down control is by; ~0 P( w) o! m) H3 C0 b elevators (and stabilizer for trim). 3 E' X: A7 S( z# H$ h) oRoll axis - Longitudinal axis, passes through the 6 r, L; @# N3 k& z9 w/ L& Zairplane from front to rear - wing up and# |' j3 x4 H; q5 F1 V, }- ^, { wing down control is by ailerons and 6 f7 R9 ~) }" Y9 uflight spoilers.. O8 O% a% n/ Y7 v* H Yaw axis - Vertical axis, passes through the 1 q& T0 h# \1 b0 W% G% E) Y4 xairplane from top to bottom - left and: F5 T0 {0 U/ K! n8 [- o' V right control is by rudder. / z: {3 P8 {# H" S- y- v5 x置, ) b1 R' w" v- v制轴,8 i1 P0 `( C& m( u2 U 通过飞机重心互相垂直的三个轴。# E. r8 D1 H' U* l! H# |+ c( X' N 俯仰轴—又称水平轴或横轴。由飞机的一侧通向另 & d6 ]& x, K# E/ p侧。飞机绕此轴转动即造成机首的俯与仰" r4 t& Q, }# S8 R) [, h 俯仰控制是由升降舵来达成的,水平安定 3 |/ h8 B8 O$ v w6 R, w: W4 I0 u/ f则为配平之用。 6 b# L; Q2 C, O. D$ H横滚轴—又称纵轴。由飞机的前部通向后部。机翼. G2 h1 Z6 y& v- H" _* u 下运动由副翼和飞行扰流板控制。 2 p( p- ]/ G5 [& Z* ~3 o# [3 s偏航轴—又称垂直轴。由机身上方通向下方。飞机 ) J e9 q7 H3 r1 W; X8 Q) t此轴转动即造成机首之左右运动,此一运( k. x- _7 }) O 由方向舵控制。 ' v. o6 l' h9 H j/ k+ E2 }0 ~to constant speed to drive the electrical power.5 Q$ L6 Y4 x! g: f$ W3 s1 b* x C 7 E B, \: N V' i/ B: ^a% q9 t6 n8 L9 l. ~' G2 z4 R/ g c % {. v9 ^% H, P, m恒速驱动装 # `" u& Y% A! }; x& o) `0 M将发动机齿轮箱的可变转速转变为恒速以驱动电源的 5 {+ w# L+ Z/ ^: A: w( o, Y* O ~液压机械式部件。 3 y$ _1 |, S) u# ]8 N3 P) L, F9 r; h2 Q9 r/ Q7 B6 _# z$ J) I% l0 u3 H7 p" D) Y& q J- S9 P2 y9 @% _( E6 V* \/ C+ @. R$ F7 E6 ?+ i6 F- ?% e; b* C/ B$ I! `; \( L. a& b- H4 [, v' }, G: u& r英汉对照民用航空词典B OEING9 D$ a; w9 F0 D3 k TECHNICAL DICTIONARY 36/ S2 D% M u& o7 i3 l- E CONTROL COLUMN, A mechanical component used1 Q; J+ q& v: C7 [4 [ rs9 Y- K# L5 W& {6 O9 z/ F: Q: U nd elevators.- v! Y$ F/ H' |' U! l$ i9 E) M j9 c ONTROL SURFACE, Moveable panels on wings and, @; L; O9 N6 K/ {( T! u il for movement of airplane on pitch, roll and yaw axes. + c8 W4 P3 K' ]" u# [2 W: |ONTROL TAB, SEE - BALANCE TAB$ q& r. l# K b4 s# [ ONTROL AREA, A controlled airspace extending $ _7 Q1 I4 y5 f' a8 k9 B( _# Zpwards from a specified limit above the earth. ( E+ w0 j" Q; F) q$ D* ? QONTROL ZONE, A controlled airspace extending% F5 M% w. ^( V7 B/ l+ \: Z% ^5 A+ o& J: K pwards from the surface of the earth to a specified 6 r9 [$ @$ s. J; zpper limit. + m- O5 D) J, V- y1 E7 v, ^is% |+ Q1 ~, R3 P o IFR flights and to VFR flights in accordance " U6 a i9 Z) {: n2 `' D; Bwith the airspace classification. . b; J) [; ^2 d$ \4 y4 p+ D机械部 " O) v' Y6 Z% E% S, |1 W4 {# T7 _+ ^ 操纵面,3 }* n, L) u1 a) | 机翼和机尾上的可动面板,用以操纵飞机俯仰,坡度, & X+ C. X/ {! r% ]$ _+ ^和偏航运动。. M! T! V: F8 \) j8 E0 Z+ N 操纵片, 8 c& A1 j- T8 X+ R( l见“平衡片”Balance Tab

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10#
发表于 2008-12-24 21:40:09 |只看该作者
by the flight crew for operation of ailerons, flight spoile , E; ]. {! n3 U7 oa 6 c+ r3 @( Z: M# I2 V. {; A7 RC % Z0 W6 ^( w+ {( c( Hta 7 U9 l. i) b' z8 @3 P: w9 u& ?8 H) p' \C % `% E( V1 l# `0 b9 r; D5 kC 0 V+ J5 ?& g5 k/ v# [u0 B2 j ?2 {" e. R' ^' [" [) k C2 N. q$ w% M" U u " p }; g u% S' m; M0 U! Fu) b* ~, e) W3 \/ n9 L2 K7 Q CONTROLLED AIRSPACE, An airspace of defined9 e# v: b4 Y4 i$ h- J8 l. I$ x dimensions within which air traffic control service( ]4 z( \4 d5 d T) t provided t5 v! _3 e! q7 M: ~ ?# c2 [3 u 驾驶杆,6 n) D8 Y7 M1 v( R* R0 {* u. m* ] 飞行员用来操纵副翼、飞行扰流板和升降舵的 ( O+ O0 \( O4 J2 O5 A. n% R1 l0 h* t7 x. y9 m! ~. Z, i2 g8 d8 t( w- B9 H; E) {管制区域, 4 _1 x# v8 n; ^# g. ?6 l高于地面的指定极限以上的受管制的空域。 1 r. Z" O" R- l- m! A制范围, 3 _* f7 Y& k& v0 K/ j) V由地面到指定的高度以内的受管制的空域。 & K( b1 Z1 b- `) b- x- }一个范围明确的空域。在该空域内,仪表飞行规则飞行. P! V+ X( m4 G8 j9 I Q 和目视飞行规则飞行有空中交通管制服务。, e$ q! G+ s; r! O7 @1 _- y% ]. J0 u4 b! G3 Q+ z- ^" @) {( k 受管制空域, 6 m8 n& e3 }6 F7 N' l英汉对照民用航空词典B OEING+ w4 _- d$ X7 R u TECHNICAL DICTIONARY 37 3 g9 \. K8 I7 ?% O# _! g( f2 MCONVERSION, To change into another form.! W9 P t, f0 N. r COORDINATES, The intersection of lines of reference, , `" h: r; _( s& [* p* L4 fsually expressed in degrees/minutes/tenths of minutes' r8 d4 f% {( Q2 Q; i+ M' D. ~/ y f latitude and longitude, used to determine position or ; u: a1 n; T1 p. M: }CO+ D& l$ |% }7 c1 ]: i0 U& V destruction of th 5 g6 k" X8 V2 A1 S$ G0 m% b: vchemical conta% ]/ q1 ?- K* b1 X COWL, A remo 7 |- b( i5 C! ]/ h a& _. ffor access to th0 x0 y5 X+ a2 C* ^+ f- A ] Fa0 q% Z9 G4 ?4 O8 C+ | Nose Cowl - Front section of the nacelle for air inlet. b3 M5 `) C0 ? to the engine.& k9 `% a" L2 A' H Side Cowl - Cover around the sides of the engine. 2 Z4 u" t1 o9 VThrust Reverser Cowl - Cover around the core O6 _, I: W3 d( Y section.: H: a4 o+ k/ C+ Y9 D+ }! ? Translating Cowl -The moveable outer portion of the % `) \2 R. j, @2 @. Rthrust reverser cowl which is2 ~9 e/ E, }: {# V8 L/ _ operated during reverse thrust. ! o9 h% v! j) B% o& h# x标, $ w4 o8 N: _* E3 |基准线的相交点。一般以经纬度的度/分/十分之一分 ' U8 m( e" ~! }# [! \读数来确定位置和方位。* h$ P" E1 Q; v 腐蚀 ~1 M& T) o5 [1 W, \ 动机外部可拆除的罩子。发动机上的构件必须要取下+ D) m' E' W2 p 流罩后,才能够到。 ( Y& i3 G d; \4 K1 z7 q9 r: @7 `& U; j1 o2 B0 n) [机的短舱的前段。' w: s) Z& X1 N" M$ D 侧整流罩一发动机两侧的罩子。 $ Q+ i; G# T0 m+ \/ \1 m% u A反推整流罩一发动机主体外的罩子。: y7 j& Z- e7 g2 f& M) J r. A 移动整流罩一反推整流罩外可移动的部份,在反推工1 p4 X, L$ M. A8 ]+ L! R' N7 m 作时使用。 9 ^' M- } i5 G N- {u2 O# h$ }1 p# o: o o 0 W7 k% f4 V. p# ~7 ?9 v. Jlocation.! j: m; X1 u' l p RROSION, A chemical action which causes gradual 2 F& m4 j$ P- E; E1 ye surface of a metal by oxidation or$ f, h4 y+ }2 l mination. ( T! M( f0 Q6 L% Jvable cover around the engine sections5 s, [/ a+ t d' S4 m( I e components on the engine.1 s* O, {) O& Z( L& U2 | n Cowl - Cover around the fan section.4 @) ^2 ?0 ?0 I) o9 Q8 A; Z7 s 转换, Z4 C6 _1 ]; M$ F7 D# f 改换到另一个方式。# S) o- U! X8 J1 e/ }/ `2 m U& t- z- f6 [* T5 Q. o: B# V, k1 i2 P6 M; k/ ~, t3 V: \6 D氧化或化学污染造成金属表面逐渐破坏的化学反应。& Y) R2 p0 W! Q" s) N, y* a 发动机整流罩, 0 I% X9 v, g) i4 f: A8 p t3 i' `3 K- A% C; C% g: C! \ r1 W* {: I3 p+ f$ W, Q/ b' E扇整流罩一风扇外围的罩子。6 b# L" d3 V& [ 前整流罩一引导空气进人发动 , k3 x/ J+ y+ h7 o英汉对照民用航空词典B OEING! W8 O }7 X5 [ ? TECHNICAL DICTIONARY 38 ! {5 u& d9 w" g( M0 ?* X# ~CPU, SEE - CENTRAL PROCESSING UNIT' V o* F( n; n* u& B- d CROSS TRACK, At 90 degrees from the desired track + @: ^0 U( K$ B; j Mf the airplane. For example, cross track distance is the # I5 ^6 s) l7 X1 G: s8 D; \: Fistance from the desired track measured 90 degrees 7 j `# R" s6 ]2 d: r; kom the desired track.. @+ m2 ?( J# _* m# C1 U ROSS-CHANNEL, Electrical wire(s) connected from+ w' j+ f f) R8 J ne system to another like system, for example, FCC 9 }0 @6 ?; a8 c5 G1 e" to FCC "B". " L! |* q9 d# {/ B# rn adjacent engine or one on the other side.2 R$ f% r8 `7 e" N' {/ F l crossfeed 1 t3 g, F. @8 E G5 Tanifold for fuel flow from one side of the airplane to the : |( B! i5 V6 _; }+ mther side. & b7 x2 Z0 @- ^re & n- b2 n! X# o% W) t ~! jRUISE ALTITUDE, An altitude or flight level % `7 ^- J* D+ Y& i0 m/ H. ~$ o4 M& }; g1 o9 H- v9 m( B o3 i/ ^" `; h. J, r/ s, V d 9 q1 V, u: o. @ T& s" s7 pfr , m( @1 y/ s) D0 YC ( N" c4 t' ]& q. b: d! xo / R" t$ W- x7 _"A- m6 c, y) J5 r( M7 T% W CROSSFEED, An interconnection between fuel* W# z- _8 B/ c manifolds for fuel flow from one side of the airplane to $ K, j5 ?' m( G1 e- J2 aa( l- s0 K, W+ Z. W; B& r" a CROSSFEED VALVE, A valve in the fue5 t6 e- z2 c* \& W m0 |, N5 {& J. v1 ^8 G* Q o1 u* E: E- O" s4 [ CRT, SEE - CATHODE RAY TUBE ) f( ^6 k% T5 Y4 ^CRUISE, Phase of flight where altitude and speed a- F9 t! t' P- k! ~ basically constant.9 M' @7 P( ?/ \5 Z2 i' ^ C1 v2 i/ i5 v: _: w% I5 | maintained during enroute level flight. : s3 ]- E' h) q8 k! g) H! r3 s中央处理器 * ~, \9 Y- s% n1 l8 K/ q见Central Processing Unit. `: c3 j7 {! C6 j 交叉航迹(XTK),+ l; O# u3 s0 G/ K$ z 与飞机预计航迹成90°角的航迹。例如,交叉航迹距离4 B# I/ r% u: ?4 s 是用与预计航迹成90°角量取的到预计航迹的距离。- t1 T: J7 ^6 E; I9 Q 通道跨接, + J/ b5 v$ |7 [- `) @& x: J电线由一个系统接到另一个类似系统。例如:由FCC: x5 c! w1 K; f% R2 e5 F “A”8 V9 m9 O9 n; _0 h 接到FCC“B”. $ f% R5 L! `' r0 H! c) t机身另一侧的发动机。8 u3 p! i" ]4 K2 M 于使燃油从飞机的一侧# k9 {. l2 [+ C o+ C# P8 V. t9 r p 向另一侧。1 o- Y% H3 w$ `5 g) o# r 见Cathode Ray Tube) B, T$ {% D( f. y2 s. q; s5 a 交输,' `/ |% y; U2 [/ n8 J 燃油支管之间的交连设备。可使燃油从飞机一侧流向邻# o- W: E+ b, x$ S, L8 z 近的发动机或在 6 i3 E. @* t, p8 L0 j2 s: h交输活门,* S8 @) J( P% o% _ 燃油交输支管内的一个活门。用/ w0 q. [* W. Y6 [; S: ~( s' g4 M0 H$ R 阴极射线管, 7 R. [# w3 a; b! b; h: r; t5 Y# m. ; Q$ L. n. o$ V! D1 C5 N) w阶段。 2 D3 v2 C) A; C5 N) g" c航高度,9 L' h8 O( S8 p7 k A. M 飞行期间,飞机所保持的高度或飞行高 2 v K4 l" p0 J1 w$ s5 ?. K) t4 l巡航, 7 B1 j* F, Y: @: e8 i. H. M& T飞机的高度和速度基本上没有什么变化的飞行 ) W4 b2 }. X# E1 D" \# M6 _4 Y' p 在航线上水平7 s9 i7 G( T0 R4 P9 b 度层。* ~: G3 |" d/ I2 S& E: J- v 英汉对照民用航空词典B OEING + F: M: L0 }8 s9 w% h5 ^, e& BTECHNICAL DICTIONARY 39 # v" w0 m1 q9 @. sCSD, SEE - CONSTANT SPEED DRIVE M2 L) N+ ~/ r0 p- Y CURE, A chemical change which takes place in a resin3 t/ p Q, |: b/ A9 v# J and fiber based component causing it to solidify. . m8 ~5 N/ U; T: ^CYCLE, A complete series of events that take place$ I0 j& ^# B! D6 a gularly normally in a continual sequence. $ |) {1 d- g5 i- V+ V5 i4 x3 rAMPER, A device for slowing down or limiting. D$ P/ Q6 @$ Z DASHPOT A mechanical damper for slowing down % C0 d! x' j2 [ L: b! [' oovement by restricting fluid flow.0 e) | g Y3 \ D; b. L. |, P! ] ATA BASE, Stored information which is used as the6 U% R' n: r2 S' M2 y ba9 T+ n# N& d( ] DATA BUS, A conductor over which digital data is . , I. m$ O: B* ]% Q8 t+ ftransmitted.* [* L5 O! q, h. f, [ DECELERATION, To decrease in velocity. , W) z- ~' @% D* F# a$ k% F装置,2 M1 r( B r) C$ F+ n/ J$ E, v rive . [3 k- R( u# B5 T. X9 C# m& Pre - R u m- [' u4 R+ R' f( YD ) B# ]3 a7 }- x1 ^& F; ]$ }3 G' p( LD 5 l% p5 N* X6 P. [' S kmovement. 3 D) t0 C* @5 Nm 7 R# Z+ I* y1 CATA, Another name for information.0 v/ U& z* U) c5 T, I0 a D ' v$ z6 ^+ O/ ~% ?sis for computation. 9 `# K2 t: n) b: i4 o恒速驱动 7 F* ?, g& D/ [* s$ F- B) {& j见Constant Speed D . r; P/ Y) W. K, Y期, $ b$ d. l3 X1 }不断重复发生的事件的一个完整系列。- G, ]% P/ u: o8 w$ T8 U 尼器,* T- D! x2 L. E$ o' k( c- p ^ 慢的一种机构。, ~8 ]' R, p% ~" I; ^+ M- T' {" b' O( s 用限制液体流动的方法以减慢物体运动的机械式阻+ o0 a' `$ M) h& ^% K* Y) X7 }7 ^8 H+ R- w& t" D4 B0 n7 n. g; ^# M2 m料的另一名称。 ; E% U/ | v0 \- ?据库,3 y. ]% B0 S H k& v2 R8 q6 ` m7 c 数据总线,3 y: V2 P: |; e& W( U x7 m# j 一条或一对导线,用来传输数字信息的通道。 ( J. I& c0 l: R2 ~5 U减速, # ]/ R4 F, Q4 U" R7 H速度随时间的递减量。 3 V, t% k+ D t1 s9 i- {' R- d+ _固化,# H+ `9 m" D/ q" D. T, B9 X 树脂和纤维部件内化学反应使之成为固体的变化过程。 ; _7 r/ P/ e) @, y4 p' Q7 |3 Q" U0 q6 D" r; T0 L: ^- b" u6 @ B用来使运动减 ; i1 i8 ]0 Z+ y3 _冲器," x; l1 K' E. ]' K" J' D, @' M 器。% |( c% h, u: i) ? 据,0 ]/ p% C+ W8 a+ A) Q2 O4 h' P% N% Q2 o) F3 {) m; w: _( a储存起来以便在计算时使用的资料。 N' U! ^( ]' f5 `, f英汉对照民用航空词典B OEING8 Z( o# A, l1 Q r TECHNICAL DICTIONARY 40' Y1 k) q. a' }9 d, L DECIBEL (db), A unit of gain derived by computing the # B) q; A2 E9 Ctio of input power to output power. $ k# k/ `1 z! B- R& dECISION ALTITUDE/HEIGHT (DA/H), A specified# K4 s- h- Q* K/ m' _1 M ltitude or height (A/H) in the precision approach at 4 m6 ~2 s4 q, R4 ghich a missed approach must be initiated if the( E9 S, U; H# L7 D* o1 g& T ECISION HEIGHT (DH) 1, With respect to the* x/ U7 L3 l1 @+ d8 u. ]0 c) c proach or & L( @7 H/ M. |" G* Mexecute a missed approach. 1 G" g5 I* B8 F9 t6 X2 N; S2 ~# uproach to trigger the decision of either % L7 w" C7 l% Y4 {( [nding or go-around. $ x7 R" @* Q; h" n7 o; _ECOMPRESSION, The loss of internal aircraft air1 L. E% t8 S# m G5 o2 b3 M/ ` ressure. 5 F E6 q$ [& e6 E- l ?E-ENERGIZE, To turn off or cause to not operate.- h( V5 Z5 _3 G# j. {. p7 ]6 \ rom the tanks 5 ^2 ~9 K/ J" x# _( ^1 Kusing airplane fuel pumps or external suction." B1 j E; i8 y3 k 算的一个增量单位。分贝 4 E0 {1 A' t& W6 ?0 W常表示两个声音信号或电力信号在功率或强度方面的 8 X' I# l, }& u" L4 X( h8 X对差别的单位,相当于两个水平的比率的常用对数的十 $ Q9 P' R4 J* l, Q |' w断高度/高(DA/H)," D/ m! X& ?$ Z 在继续进近必需的目视参考没有建立的情况下开始复 V/ m8 q5 g1 m3 J. m" `( g 的精密进近中的一个指定高度或高(A/H)。 ) b. {( D* S, ^$ b8 C$ C断高(DH)1, 2 d# u, \: O4 Y. e操纵而论,指在使用仪表着陆系统或精密着陆雷 / N& x# u* \) m. J0 N, \4 W生继续着陆还是复飞决定的高。' g j6 |7 h' ~5 i& h8 ~3 N d1 ]' t 飞机失去内部空气压力。' h- L; ~2 G6 ` 开,& h) m1 U8 ~5 B0 C 关断或使不工作。 & i* F" p, l" o5 h3 G. L; {机的油泵或外部的吸油装置将燃油从燃油箱排 : f! x p/ j0 B! o: X8 h出的方法。$ R9 n$ S$ ^' @5 S0 D0 U$ F) u ra0 k' f X. h; A. j/ \ D 7 J9 Q$ X) P$ M, X& D: q$ b/ [a6 h6 O: r; p* H w ' ]7 H2 T# q% p- N5 h' c6 Jrequired visual reference to continue the approach has! ]: r! B; H3 I# ^ not been established.0 A1 D0 C$ y* S5 a3 g: ~- K* T D - j7 \5 H2 t2 y! v5 u) t) z- Ioperation of aircraft, means the height at which a 6 m" f2 t; h# D( [decision must be made, during an ILS or PAR . e9 A; z. m: G$ \( ~instrument approach, to either continue the ap, E4 \: @% V2 z5 k1 H' _( Y0 _ to 6 U+ @% S* y% _9 Z# oDECISION HEIGHT (DH) 2, An altitude used during a / ~) }8 e7 C- C) t9 kprecision ap. W7 E6 O2 f* ?5 H7 O$ h, {, D' ~% s I la 8 l- c/ |: p0 I+ [D ) J0 A# e/ L3 A" l: ]p- X! @4 a' `# \3 C' b! s3 c Y D7 C& p7 v. T* ]' G DEFUEL, A method for removing fuel f 9 i! z5 X/ O. Y0 w2 M分贝,7 w6 _8 r0 T4 E0 L' J+ d5 f( s! c6 U" H- s 以输人与输出功率的比率来推: R/ n# a; P+ N, @* {+ E# [: M# b5 y7 U0 k( s' b: q, [ @: V! f, k% V! D3 x, d& [3 [ a% @. a3 ~) H' J5 w$ n& W# R2 o0 S1 G3 Y9 s! `7 K" E" P: A( M" v! U! j2 V+ T9 e5 c; b8 A! T2 ], J" G5 G: D就飞机 ( g/ J4 k2 k2 O i9 z4 n% L" l达引导进近时,必须要作出的是继续进近,还是中断进场3 g6 o1 c! b4 S4 x 复飞决定时的高。 & o) D4 W: ~* V. n% `1 ]5 X决断高(DH)2, 9 v% |+ ~/ U( h) `) I' U5 A( C: E精密进近时产! l) [7 F0 j5 S8 c3 a 失压, 0 E" a7 h7 h+ L3 {8 q/ {8 ]# p% d m# k7 X. n q! M" d, J ?* p( ~; g排油, 5 s/ D) Z2 T1 k+ |; K用飞 . J" q ], [% x8 P k8 [英汉对照民用航空词典B OEING ; W& s; ^0 G$ Y- |. z. T) nTECHNICAL DICTIONARY 416 v5 F6 p: N) g8 a) S# f DEFUELING VALVE, A valve in the fuel system for $ N$ Y7 e: z6 {3 Q$ @* G$ }6 zefueling the tanks and for transferring fuel between the, _4 @3 o% J- w# I% D. j E-ICING, Removing ice after it has formed on aircraft. # m0 Z+ T$ n4 L% {Change or difference.+ h. l$ z: E s/ k6 p EPARTURE CONTROL, A function of an approach $ n9 A; ~0 a" R& q0 xontrol facility providing air traffic control service for ' M& V; u& |* W* y6 l7 ueparting IFR and, under certain conditions, VFR ' e& j: f& j* z3 e# BEMODULATION, The process of retrieving information2 e6 A* v9 w* b4 O S carrier voltage. 2 W1 ^, v. b. Y( Pation. $ ?' K, _6 w; c: L; Blic T7 J0 u" ^/ E! `1 h creasing hydraulic reservoir air pressure to 6 g d9 y7 A4 ` \2 X% Q6 pmbient pressure.+ a0 |. j) p2 F 箱排油和在燃油箱之间 / O6 N7 l* V6 N" g送燃油。( g7 p+ D+ g0 c& \ 冰,9 m9 ~) [7 W8 E ~ 除去已凝结在飞机上的冰。5 k9 P* C1 d& Y9 B' y8 p- t9 a2 R 删去或取消。- v2 z8 p: r: P$ v, c4 c! ^ 量,7 s2 L0 Z2 U" A( w3 ~ 变化或差异。 : J1 | m1 ^+ {' d8 H+ D场控制, / W8 v' i. j6 V0 G7 N" X* J6 _! h$ C给用仪表飞行规则离场,和在某种情况下用目视飞行$ Z# b* r/ _2 O4 Q" i) E 则离场的飞机提供空中交通管制服务的进近管制设施 8 Z2 r+ `9 b/ x. f( V9 i3 s3 H# P8 @& k( x 调,; Z$ C6 F4 `' N& o" s 电压中获得调制电压的处理过程。 0 _6 `/ c) o. ?- v; S环境4 C" K0 u! q- r( H; Y' A 力相同的活门。 . T6 d% K0 L3 h; w2 M/ vd & N; [7 K; g/ n% q! ^& i9 Ctanks.4 y3 T$ K9 W: t% W; K* ^- v1 Q D" Q* k* p) l/ M V5 Q DELETE, To remove or cancel. ( M# H5 ^" g% aDELTA, * y* @2 }$ ^- b1 HD : l2 |* }% Q ]c6 |* M/ X4 j |9 w" T d/ U, J. `) k$ j7 { aircraft. # e" g. G+ p# ED; }7 [6 Z* X6 l( M! q5 s1 f (modulation) voltage from a modulated# J$ N0 i( Q4 b3 \0 E/ }5 t DEMODULATOR, A device or circuit which performs 8 {4 e$ U$ K( q v# o i8 Z7 vthe process of demodul8 g' B1 u* Y3 T4 d DEPRESSURIZATION VALVE, A valve in the hydrau # g# m* I# W+ j4 {system for de6 V) r3 M, f5 n, |. j# Z a( u9 x8 H. ^, T. _* [( H- l* F 排油活门, ) F" k+ o8 @$ s燃油系统中的活门。用以为燃油 . C: H x, U+ {- R( h- z' G5 N! J( O5 \- Z9 {+ Z7 \: y5 l8 `, z; s ~/ K8 H, R. A( w删除,. L2 Y, N! k# h3 s6 |& g/ m ~7 p3 X" v5 |6 H* v6 P3 {& K; w8 P" g/ C* F: k3 u/ A& K6 u+ y, I2 N* H- G的一种功能, j! j, `3 I) e+ ?5 [# `! `" ]1 p从载波* g, U& L5 r( E V9 f. E 解调器,+ K- ~5 y. J, p( d+ u 完成解调过程的装置或电路。 - @7 M# O7 \2 O" ^# ~4 Q减压阀, ' h* }# H; x" V6 i- B在液压系统中,将液压油箱空气压力减至与周围# C% p9 P- j% c! W8 r3 U* ^9 i; ^ @0 x: S! s 英汉对照民用航空词典B OEING: M' K% s( q* E! K$ U TECHNICAL DICTIONARY 42 5 f) U( G9 i# k6 ` K% b7 ]DESCENT, Phase of flight where altitude is decreasing. & M7 `4 c+ \2 K0 a& a- PETAILED FLIGHT PLANNING, The calculation of fuel 0 s5 B; l" J; w. G" Z" E, Und required for a trip by considering each phase of1 G- C" H5 V8 _; D ight (climb, cruise, descent, reserves). p6 [8 I. i5 P1 }: hal or ~. o4 O! Q C, gETENT SOLENOID, An electrical solenoid used for7 a' p% Q# u1 d& E$ f t. $ Y" W4 R7 `, Z% q% C. ^specified course or # L) |" h2 d5 @! i u6 crocedure. . M8 b2 I9 {, E# o! V# S/ g1 ge. , J) V. U0 C, b3 a7 t4 u飞行计划,4 ` L! W! v2 n9 A, V9 a" U+ \" w 将航班中的每个阶段(如爬升,巡航,下降,备降)都 8 R6 C0 C0 V$ e; b# ?人考虑,来计算该航班所需要的燃油量。 4 q$ ]% T- A; b7 ~: W( O/ ?用来感应情况之正常与否的电气装置。, |# P3 [4 N" x- Q* y/ O! L 定电磁线圈, ' _& }/ A3 {; X, C% {出接通的电磁线圈。/ J. W! w- H; w! [, b3 K* \ 差,# [. F7 H. E- U& T6 @ 与指定的航道或程序之差。 7 p0 `2 F& p+ O3 b2 _用气压或液压操作的活门机构中的柔性部件。& i5 {9 E& q) d0 m* l D , `8 T& D% Z1 Z1 d; n5 la , T; X- m9 H2 q- bfl8 v1 K0 y! E) q- f2 P% [ DETECTOR, An electrical device for sensing norm/ k! ~" K6 ^, }- [/ { abnormal conditions.! n. _, c# g6 o0 w8 M2 u0 ?/ y" } D 1 y8 M1 l# R$ k# G- j2 G' Ycontrolling the engagement of the actuator outpu , o4 M2 r- A( G( f9 p3 m9 G9 J/ kDEVIATION, To change from a % z' S; Q) Z' i1 ^5 Wp( ^5 [' T' u i$ S- e# R DIAPHRAGM, A flexible part for operating a valve 0 [' ]3 m; O) t! l+ U# M5 smechanism by pressur' v+ A6 M9 n" Z% j5 D+ Q 下降, 6 C, b/ u" A8 }0 q/ g2 p飞机高度不断降低的飞行阶段。; Q5 W7 R! [ l. @ 详细 ; O ?* z& i0 U4 ?& z1 g* t) |. y4 P' Y+ E* e探测器,0 s9 o/ j( Z' O( f+ C" I4 W! U# }7 n用于控制作动器输 / x, x# C+ M3 Q: u9 L7 U o' d" r; M) ]! A+ C 隔膜,6 q* C, X5 u2 f L1 Q, E 英汉对照民用航空词典B OEING1 r6 z* {3 J6 i$ N- g0 O+ m TECHNICAL DICTIONARY 433 H) Z/ p- e2 @; l DIELECTRIC, A material which does not conduct " N4 g$ v# a4 t! D. S) |electricity and used between the plates of a capacitor) x6 h+ z2 q7 y( ] E2 w (condenser).6 k6 E d$ q3 P6 L$ q! k/ y nother pressure in the same system, measured in$ P7 _, d4 t$ v3 R8 U' P ounds per square inch differential (psid). + b3 a0 R8 {5 m& W4 YIFFUSER, A part of an engine between the3 N) Q+ N0 W- a0 y2 F: s7 x ompressor and combustion chamber for reducing the' T" U3 h L4 J6 E air pressure. 9 `) j& a W& Tigh / v2 H' M7 K7 }. s$ m p9 {5 Bpulses. 9 X! @, J! I' r5 f8 Iignal that is a close approximation of the original % p$ v# y7 u+ V# _8 _ignal. 7 a. c+ B+ n, T6 G- UIHEDRAL, The angle between the wing reference ; g/ y4 Q! A9 S5 ]; D: j$ b9 y4 h+ Alane and water line.0 ~7 Z1 L+ Z# I9 A 的压力,以每平方英寸) {. V) d6 ~5 s' a' n 少磅压差计算(psid)。, a4 g& i( f1 Y* S; Y) ^ 散器,& A' ^! i9 Y" z- W5 T+ B" G- E- \ 发动机内压气机和燃烧室间的一个部件,用来降低空 % X$ o1 S3 E. [1 w, h增高空气压力。 , g' ^; P% m6 S' Z6 L6 p换, 5 g) b2 y7 a2 h7 `" R C的连续可1 [ A! T0 e3 q: P1 l' n (模拟)信号的处理过程。* e( V3 u8 v+ m: o) G$ e- d 反角, " e2 X% W- k2 s8 t6 r/ n机翼基准面与水线之间的夹角。 o7 _' l; _9 n; u" _1 b" ?; { DIFFERENTIAL PRESSURE, Pressure relative to( H0 i4 {; t0 O9 V a ! Q4 f$ R+ |" c" I" l4 Sp $ `8 Z; Q# Q& U3 P9 Q4 X: s* VD H, o' l8 v8 s* W* I1 b5 @& { c; `3 ?+ g5 S" S/ Y, p% n airflow speed and increasing the; x, L& T% L; L0 i" e0 i* ` DIGITAL, Digital refers to a signal whose amplitude 8 _ _ y/ }* [* a7 [' wremains constant for a finite period of time. Digital * r" K6 {( a; @. Z. i6 ]- Zsignals are commonly represented as a series of h 1 o( Q& i/ C$ z0 z$ zand low # J/ e& y" g% M3 EDIGITAL-TO-ANALOG, The process of converting a0 j* ?. w$ d+ r* ^4 R" H& t; M digital signal (binary) to a continuously variable (analog)$ z3 N' o. V' @# z5 K- j s: U" V" _5 a; t J6 K s1 m* R6 V4 J/ a; ` D 3 O6 `; ?3 O |/ s2 B* jp 3 S5 _0 }3 \ t, h5 M9 T7 q电介质, $ t3 \1 c; ]! D6 ?一种用于电容器板之间的不导电的材料。 8 d% |; I4 E: Y: Q0 k压差, r2 y' N. U! J, W- w3 C" ]+ \. e 相对于同一系统内另一个压力+ s5 H- W. I6 v. \* f8 ~, k; m& H1 G1 Q9 m0 x3 d9 B* Q6 r9 T气流速并4 V" N6 R3 P+ L0 [1 D 数字式, , f" v$ K/ S- J% m2 h5 x* P指一种信号。该信号在一定的时间内,振幅保持不变。8 \8 c* f" R( X' ?# f 通常由一系列的高低脉冲表示。 + {( ~, m# L4 X- C. j数一模转 $ r7 k O/ o3 p# l. U/ E将数字信号(二进制)转换成与原信号相似 5 @! g: x' _+ g0 Y1 Z$ \( Q# q F( D6 z# u, k5 l1 v3 Y: t( t: Z英汉对照民用航空词典B OEING % `8 O$ W g$ vTECHNICAL DICTIONARY 44% F S( p/ r0 R, _9 u DILUTER DEMAND REGULATOR, A component in the ( Z! z5 `, M5 r u0 y5 {3 Ucrew oxygen system which mixes air and oxygen and 6 x0 X7 b3 \- U# ~" a Y1 uupplies constant oxygen pressure even if there are $ w0 M+ o J" H b8 t% l" Whanges in ambient cockpit pressure. ) Z2 Z* w( o M3 b( J5 s( DIM, A word value of light. For light control devices - dim% z% l% n9 A, X- a7 Y _% R the opposite of bright. + m) V; |. u) w" kIODE, A device which allows electronic current to flow0 t3 o% w1 n* E' z# X$ M$ [ only one direction8 g ]% G9 Q* t" B/ V$ m" K9 T uid in a reservoir. ) n' N) m- A/ n& m. K5 GDIRECT, Straight line flight between two navigational% @% W' J- V7 D* [- R0 j aids, fixes, points or any combination thereof. When - W2 r$ K+ U% [, `8 Q. zused by pilots in describing off-airway routes, points1 ^. }# ?6 o! C9 v: |, C3 p defining direct route segments become compulsory k; f2 W) Y/ Z# R reporting points unless the aircraft is under radar$ s( v4 q4 q8 b# e4 | control. 7 M/ v, N& ^, \/ A* G( i; g4 J) j. Q节器,$ ~: _. P2 c w- F* L" c 将空气和氧气混合,( @4 E- C7 A0 @: [ 使驾驶舱环境压力改变,它也能提供恒定的氧气压力。8 L" _( F' P: d) \6 u: p+ ~+ |( [2 v$ o+ n! k. C 一个形容光线亮度的词。对于灯光控制装置,暗的反9 \& `+ d$ E V* {6 {- Z% m6 n 词是亮。 / w% _2 }+ X* q1 Q: F7 f( Y% O8 ?极管, 3 {, [9 ]0 V# E9 j5 K0 q7 N只允许电流向一个方向流动的电子装置。 8 f1 l7 K8 B4 o- P! W' S3 z器内液体的量。 $ v/ W4 j0 s: p2 v3 {" q' @1 d直飞,; |/ c0 b5 x. d7 p- W5 F 两个导航台,定位点,导航点,或任何的组合之间的直 1 Q' A4 Y8 v3 h* M- p( s线飞行。在被飞行员用于描述偏置航路时,除了在雷达控, a! C a* E7 z' I& x 制的情况下,确定直线航段的导航点成为必报点。 2 x" I( h1 }; o7 b1 p7 @8 _s 9 z1 n( c1 B$ w; K9 Qc) I! G7 p- R! U9 A D , K7 m. c0 U3 zis 1 r6 J, Z1 l6 K+ L/ i, FD 4 L" g" m" f Fin 0 a7 N5 }' a* ~7 p0 pDIPSTICK, A calibrated rod or stick for measuring a8 m4 V6 F! H" e& |' V1 q" X1 b quantity of fl6 |" |4 u! c$ C4 H k 稀释氧调) c4 i& o& \1 k7 O9 o' o 驾驶舱氧气系统中的一个部件,它 ^- ?& M" p+ p/ O% @7 n) M% s% i& O+ _# A c" Y* F! w: `0 Q; K8 ^3 m. z! p$ _# V: ?$ B) C量尺, . |( j) s' `/ B! b; _9 H1 i, r校准过的棒或尺,用于测定蓄液 . y1 |8 `! p2 {- W; I英汉对照民用航空词典B OEING5 a" c+ G7 }/ j; N) ~* u& S TECHNICAL DICTIONARY 45

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