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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 & U' p! ]5 p. C$ R. C! H民用航空词典# ^. f+ A4 ]4 x: c1 I 波音商用飞机集团 0 n5 p* C, w" ?: a) YBOEING COMMERCIAL AIRPLANE GROUP & U& G0 s* V8 N6 G/ Z$ R$ g英汉对照民用航空词典B OEING0 G( H6 ^6 { o {2 F TECHNICAL DICTIONARY 1 : y7 N2 Q5 X, _, [1 n1 PA- U9 o9 o r- D1 J) P ABEAM (ABM), Beside: An aircraft is abeam a station7 n* C$ ` r! O8 i* E( ^ when that station is 90° to the right or left of the track of 5 I, V5 W) a2 d% }the aircraft.; d. D+ b0 v6 U ABSOLUTE ALTITUDE, The actual distance the aircraft/ q: {2 N5 p$ i% E is above the ground. A# [" q" ~/ `% { ABSOLUTE PRESSURE, Pressure of a liquid or gas & L+ ?* \5 i: l' w3 Z$ t% l6 cmeasured relative to a vacuum.8 B0 Q2 \( j. M+ }# F ACARS, SEE - AIRCRAFT (OR ARINC) REPORTING, V: }& p9 d) U3 J" P8 v. O ADDRESSING AND COMMUNICATION SYSTEM ! ^& `% n, E; e% oACCELERATION, The rate of change in velocity with $ T3 k5 F7 U) M: K, m+ k" Irespect to time. 5 l/ q* z# Z, K& ?5 e+ ~ACCESSORY GEARBOX, A part of the engine,& \+ S# \4 ^$ A5 m mechanically driven by a compressor or an angle . S/ d: q) r) b- \4 ^gearbox, for driving components necessary for engine ) b/ X. O- y* l/ E4 @正切, 1 `, g3 t$ |) c& C+ G4 Iand airplane operations. # N# u" F4 i7 D" V当电台在飞机左侧或右侧方与航迹成90 度时,飞机正6 ?7 I/ P) V4 ?( [ 切电台。- D; p/ r. E4 X; _/ r- p) @ 绝对高度, 6 i( l3 D* |! R/ ^+ f飞机离地面的实际距离。6 B; t# I, I: m 绝对压力, " ^9 \8 n$ c6 Y# ^相对于真空(无压力)测得的液体或气体的压力。 ! c; `6 t& ~. B0 t; n: Q3 @* }飞机通信寻址和报告系统,& E1 Q* y; u: \! t9 C8 J 见Aircraft(or ARINC)Reporting Addressing and" n% A) o. T# `/ q. p8 ~) l Communication System. 1 V; b" }% T5 u3 ~2 l' U+ t加速度, ) ]2 ^' v" ~& s; }随时间变化的速度改变率。0 _- r4 a, r1 K7 Z4 I 附件齿轮箱,9 s, U" x! | B' f. t; E3 C 发动机的一部份,由压气机或伞齿轮箱带动,用来驱动! l. u4 m- o& o: K P 一些使发动机和飞机工作的部件 * B3 H/ b% h# U) g+ j$ X$ T英汉对照民用航空词典B OEING/ x5 i# r/ N: x% n TECHNICAL DICTIONARY 28 E+ t0 \- e: S# C- ^7 I& u ACCUMULATOR (NO. 1), A container with hydraulic ( u: S* p( Q. yts when normal hydraulic supply is not + b' l5 ]2 D7 r- \vailable.5 x9 W2 d8 t$ }. w CCUMULATOR (NO. 2), In a computer, a special' ]/ A5 y+ [8 l! F torage register associated with the arithmetic logic unit, " C. i6 |3 R" A" K+ c/ m0 c' e( aolding the results of a computation or data ) U( X7 g& ]& E# Y4 w0 N3 GACTUATOR, A mechanical device operated electrically,! p# m- |4 y9 b- O7 T9 A hydraulically, pneumatically or mechanically for * f% K, o, P) I$ N% ~transmitting motion between components. 0 n# g4 b2 D1 c% z6 D2 cADC, SEE - AIR DATA COMPUTER 8 S( ?; b" c8 b, K& }5 N3 |3 lADF, SEE - AUTOMATIC DIRECTION FINDER: |0 H& ?* V$ \% m( w3 S+ U' h1 l/ F ADI, Attitude Direction Indicator, An electronic display of: Q1 i) D/ B! U6 U airplane attitude information in pitch and roll.8 L, c+ _7 `) W$ a2 U 蓄压器(NO.1),9 p1 R5 P* @5 M8 m4 o2 d1 O9 m 含有靠干燥空气或氮气增压的液压油的容器。当没有正 3 ~9 @! ]/ [4 H6 q常的液压源可用时,该容器可用以驱动部件。* U( a: z: e; |- D) B2 {) }% G 存储器(NO.2),' \- A9 s/ S% O/ ]3 Q 计算机中,一种与算术逻辑组件有关系的特别存储寄存 1 H) {6 \" p0 @1 k/ s* Q2 \器,用来存放运算结果或数据传输。 , _: A% F( }, l5 W( L8 Y飞机状态监控系统,7 V- e4 S( Z8 l9 d0 o, K" I/ W 见Aircraft Condition Monitoring System 1 B; A% q5 M! f$ C! S% A5 lfluid pressurized by dry air or nitrogen for operation of 9 i/ c @6 C# p# V* Z, [componen ) v4 _6 U- p9 q8 n- I4 a& Na! F7 a* W* _9 ?, T7 N A % {( p/ T& Q" L4 l5 Z. rs, ?8 _* U4 A+ Z+ Z7 ] used for h) A, K- |& B7 U/ t+ U" M transfer.0 ?8 u. v1 q7 u o' ?1 ^ ACMS, SEE - AIRCRAFT CONDITION MONITORING. x& o2 \: X/ R SYSTEM . : @* ~1 B+ n# _0 b: `- W作动筒,4 A+ q- m" o: ?$ ] 由电,液压,气源或机械驱动的机械装置,用于传送部8 X4 A1 c# Q2 Z+ x 件之间的运动。" U; H" U! c: m) \8 m* d' ? 大气数据计算机, 4 t0 a7 w+ Y( r, h6 A4 x* d见Air Data Computer. # n: i$ m% s, i; R6 k( @& w自动定向仪,+ F7 ^% c8 w' P/ Y 见Automatic Direction Finder. $ W7 D# H2 \ B6 `7 m. Q- d姿态指引仪, # n, B( t7 c S% q, U用来显示飞机的俯仰姿态和坡度的电子显示。 & J- H2 s ^- w& B# Z5 J英汉对照民用航空词典B OEING ( n( V# N% M: S; X6 C2 o) dTECHNICAL DICTIONARY 3 1 p l/ T" b; T. w0 _5 X% r8 I! L% D1 x3 SAERONAUTICAL RADIO INCORPORATED, ARINC is 2 f1 G- k0 W" g( q,2 X+ U3 y! o; Z4 j/ z) c nufacturers, and foreign flag airlines. ARINC ; v% L$ \8 c. D* U: W5 G- N! n$ Zevelops and publishes standards for electronic : R/ L/ Q- Z6 u9 p5 q1 nquipment and systems. [" X1 f$ Q0 Y' NGILITY TUNING, The capability of the DME to " a; n3 U- Y0 K) i" Klternately tune between two different DME stations in* b" N: V1 z& W rder to get two distance readings from one% U& [2 ^* w7 C terrogator. ; v+ q* N) J4 x2 Vge4 p" o% a8 P( N& u. Z ILERON FORCE LIMITER, An electro-mechanical% B# h0 R2 a2 \2 y+ E IR CLEANER, A component in the pneumatic system Q/ c6 L6 X5 q! ]" Q6 K9 b upply to the air! f$ v- k/ d8 n1 o+ E onditioning system. 9 d( ?% F6 a" j订并出版8 I+ X5 ^7 q% c6 B/ a 子设备和系统的规范。. K8 S. I3 ^, N7 t 快速调谐,) d% F8 u' G2 I* d+ M1 x& V 机载DME通过交替调谐两部地面DME电台以测得来自 " |# U1 R1 \0 a/ m同一台询问机的两个距离数据的能力。 e- T6 u9 Q D翼操纵力限制器,) u* `5 q& m5 \; W3 x- h* x 装置。在自动驾驶工作期间,用来限制驾驶盘 ! H5 `! d. E9 k* M5 [" G气清洁器,! v6 c- y5 }1 u& ~& H1 I0 j 部件。用于去除供空调系统使用的发 % b4 l% p( t! J, W. Ta corporation whose principal stockholders are United3 C0 t- c6 i9 k States scheduled airlines, air transport companies1 n+ Z: y( z# L; G1 ^ aircraft ma * A! Y, J1 z0 v% }, x( V# ud " m* z8 \- |& f6 Xe 4 D- K* K. G' l1 z3 ]1 H7 \5 a# [$ p& }A 1 b9 z3 K- G! E2 M# x# H, m1 xa ) ]0 a. w- t0 Z; ?- f/ Wo7 Q3 J1 Y1 y! Y; X- G3 v- B" s in6 k. H- O/ `2 R( t0 B AILERON, A hinged moveable part on the trailing ed7 G2 T& X9 B( l4 L2 a9 L% n of each wing for airplane roll (wing up and wing down)2 {2 P7 k8 J' X5 b8 V4 i. ?" p- A5 \0 n control. " [. R; x% D6 f s% t" b9 gA 8 Q" @5 R, P, o3 rdevice for limiting the control wheel movement by the$ h3 n( {, e* n c5 a+ W autopilot during autopilot operation.0 ]9 }5 @2 K8 H+ }& _8 \ A; D1 \" H8 W" ?. `! a9 B for removing dirt from the engine air s " J9 e+ G8 l* Q! K$ v4 T" o9 {c 9 g% Y+ K* w( m% Z, M! O航空无线电公司,1 k2 d/ C, e% a* R% D 主要股东为美国定期的航空公司、航空运输公司、飞机* v+ o/ j' p; T6 c; e: Z: \1 v 制造厂和外国领队航空公司的组织。其目的是制 5 I. t* r v9 h, g; M. G# c8 |, \% m& L+ h 副翼, - l k7 y9 c5 i1 U铰连在每个机翼后缘的可动部件,用于控制飞机的滚转: `0 x, }8 k6 ?* S$ r0 y (机翼向上和向下)。 9 ]/ k1 q8 p+ [5 t# z& E0 E; w, g5 v3 ^一种机电/ W A; B; K/ o8 x( D' X 的动作量。 - X/ l, M( ?9 P1 H3 F. a! p, N) r% y; m K2 l! n 气源系统里的一个- y2 z+ i9 Q2 `% _% e5 b! q7 t) p6 z0 ^ 动机引气中的灰尘。7 O/ F6 d* g4 [/ s; N, ]5 ] 英汉对照民用航空词典B OEING # Y+ Z" J6 T% l6 CTECHNICAL DICTIONARY 49 A6 G" h1 B: l- Q) i* N) l AIRPORT ELEVATION/FIELD ELEVATION, The9 I1 q! Z. t7 e m+ C, K5 }4 \ highest point of an airport's usable runways measured( l7 J* N+ G8 w) c1 K in feet from mean sea level. In a few countries, the, E' q" f; w- D/ [' X8 S airport elevation is determined at the airport reference9 D1 F8 P8 H5 t4 D point." T0 o6 s: b7 N- k V3 {% i" W2 V0 m AIR ROUTE TRAFFIC CONTROL CENTER (ARTCC),4 M# R4 p, J6 q0 d ervice ) `$ \; |. s6 C# m# Hase of $ O9 o9 \- @$ L% Mus flow of air traffic. $ m9 d& B" r6 p" l2 GIR CYCLE MACHINE, A compressor and turbine on a ' t @: m, q0 n/ E" G& R$ p, fommon shaft for cooling the air in an air conditioning & C/ P0 X! n& P' J$ Y( s! rystem. The air is cooled by expansion from high to low7 Z0 l3 [, w2 k ressure across the turbine. The compressor is driven ) S4 X. T7 Z5 l e6 c; I9 py the turbine. ) m% T* p( L! `& R8 H4 c6 l中航路交通管制中心(ARTCC)," J' V" T- P5 ]1 a* U 域范围内使用仪表飞行规则飞行的飞机提" B. Q$ R# _4 i; D* l) ^8 P4 I9 O 管制(ATC), Y( [. ~( v5 w+ v6 k 涡轮冷却器,0 G: v- `9 a1 p: I' b, h 是装在同一的压气机和涡轮,用于冷却空调系4 D0 {. y4 T: L+ l9 F 统中的空气。气经压气机压缩后,由热交换器移去热量, ; I& J& A# V5 C0 }5 j' y8 X9 Y然后经过涡轮令涡轮带动压气机。通过涡轮之空气,温# P* [+ j# q. j! ^7 |& E" c$ j O! a 度下降。% C8 P# {0 y1 k2 A! j% h6 ] A facility established to provide air traffic control s' S e2 L; ~7 `+ T to aircraft operating on IFR flight plans within controlled1 Y* s- Z# P& ^" V airspace and principally during the enroute ph % U% X, j, G$ r* C, q7 U# Q, F& nflight./ S. f" C" V6 }1 }& r, M. B AIR TRAFFIC CONTROL (ATC), A service operated by 6 F) ^" r; {6 V3 x/ happropriate authority to promote the safe, orderly and $ r+ O" ^) C# i6 eexpeditio7 G8 h) ~9 Q; O. R- K$ j$ k A + ` E% ^+ P; P; zc ( g6 d2 v7 x/ is , a/ u" R' R$ ?7 ?+ y# Bp ( @$ A5 x! {1 R H6 H, w, Ob 3 t2 P2 m5 X1 b* _. L& A机场标高,( \- L8 t# Z0 v% K) g+ M& y' W2 a( b 指海平面与机场可用跑道最高点之间的距离,单位是英 ( i, F- G3 h n0 r4 c# _/ R% N尺。有几个国家的机场标高是由机场基准点而决定的。 3 z5 g c2 H! z9 S: M9 t' o# O' N7 o" ?1 r 给在控制空2 ?3 j2 S( k* c! D3 F 供空中交通管制服务的站台。 " R2 |0 [1 q. o( _# A* o# z空中交通 ( v+ \, r ^/ }/ [1 q2 i6 X; G7 Y由有关当局管理,旨在促进安全,秩序,和效率的空中 4 t8 @" a& Z) R交通服务。. A5 b8 `& z9 [5 P3 d 根转轴上0 T- M3 w+ A7 i+ Y& c) f# x# I" Q9 Q+ x3 M+ c2 x0 v& k+ M9 B# S: S |! T 英汉对照民用航空词典B OEING $ b, Q2 D0 s; r( W% qTECHNICAL 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 produc/ I- d, w* _9 O* O( G) U data information, such as altitude and airspeed, based# B% T m5 |5 n, q; n9 J on pressure and temperature measurements. 9 S" ^- o: [2 i& i3 F- E+ Pes air' I/ J3 G9 k3 q7 q5 B" m. m$ A* W IR TRAFFIC CONTROL, A system comprised of3 p+ n5 i. _7 f, ` round and airborne components used to identify, track6 s# B2 M& C( l/ e) f9 Q OUND SENSOR, An electrical device operated. `, b2 i: v/ T" g. z/ X. ] y the landing gear, which transmits on ground/in air 5 |7 p7 F& {. |* wformation for system operation in flight or on the ' [9 [* H1 o9 S% i! V, sround. 1 A ` Z. |+ y8 ~0 p5 `2 xIRBORNE VIBRATION MONITOR, The AVM takes% Q. w1 u/ W5 `1 X& Q8 j6 C+ [ e signal from the engine mounted accelerometer and # J! y' N3 G, R1 Balculates the vibration on that engine. 9 V+ x! H& f2 X/ B( fcorridor equipped with radio navigation! G; V# ^/ \2 l aids.( n7 L: V' O% P$ y+ [, |0 I$ j: B# b* n AIRCRAFT (or ARINC) COMMUNICATIONS* H, W; H: A8 O5 N9 b; | ADDRESSING AND REPORTING SYSTEM, An1 M$ u& T- C4 e( Z7 k6 n/ i addressable digital data link system which permits the 1 k& |4 ?/ O& E- f1 H9 nexchange of data and messages between an aircraft7 }6 g& H9 V, C/ B, a and a ground-based operations center over a radio ; K5 A; x$ [" m" c5 { o% b7 `network.: f/ _( _' x: W$ V AIRCRAFT CONDITION MONITORING SYSTEM, A- [5 z- x" A: {6 M$ [" |' i system of sensors and recorders to monitor various1 U- T9 \ ~: K& z3 q6 {5 f' h" l airplane systems' performance and status.5 M4 d& Y! l0 i ]4 W 机,/ N. Z3 R- C" Q0 M 中交通管制, + K' G$ L) m+ u @一个由地面设备和机载设备组成的系统。用来对飞机进1 E5 K7 L1 }. n2 M 地传感器, ! A( ^9 N z- Y一个由起落架操作的电气装置。用于给空中或地面的飞 2 r- `& D* f( p- F' c7 M系统运作传输地面/空中信息。(有些系统只能在地面2 {* V6 O1 J3 d' Z/ m2 ]. x+ o 用) . E8 Y! k5 \1 s& ?% D载振动监测器(AVM),& K/ U) \) C! Q: B2 V" X$ [- _ AVM从装在发动机上的加速器取得信号后计算出该发 & H( O* c: C* b机上的振动。 ' N- X* ~5 i9 e1 Y' n4 }式建立的控制区域,内有无线电导航设备。 " z! l; X8 ]: x; W' ?% Z1 ]飞机通讯寻址和报告系统, : Q5 u3 e. `. x有种可寻址的数据通讯系统。利用该系统可使飞机与地5 p" P- B2 ^ J! g& R 面操作中心通过无线电网络进行数据和信息的交换。 + h# Q. E- i4 N" S, O# V0 K' N# I飞机状态监控系统, ) H0 e& |' G2 K S$ a( W6 L9 h" g( I一个利用传感器和记录仪对各种飞机系统的性能以及% Z1 N2 |* q0 e 状态进行监控的系统。 7 I! r. m* l0 Y/ |# M# c+ pA# |; f1 q2 |; Z# m' k! |" U8 B g / Y" Y2 A" D5 `. C( C4 V! J' Q, Vand locate aircraft.* X& x' V9 J2 u: ]$ r% l0 ] AIR/GR 2 B8 k4 i" M4 Z; l9 Jb 6 V0 z x, `' g" F4 ~$ Win 2 Y4 S% G/ R/ A9 T' O* w- P2 m( vg- Z# u6 F* M2 }: `/ s+ f) ~9 B, @# l A * ~. G0 _2 ^7 {* Yth+ M/ V6 u) v5 h. v* W. P; ?' j c9 N, U( G, N) I AIR WAY, A control area or portion thereof established q# M& Z/ i5 C$ u in the form of a5 J `8 P: M; O% j( A, V& e 大气数据计算, T' i& x& V% Q* U 根据量取压力和温度而产生大气数据资料(高度、空速5 h. a# [, }$ n 等)的计算机。 0 J' D T/ O5 H: v$ t/ x4 w/ S$ z9 |6 x# P) H' v+ Y( t" @: v9 x 行识别,跟踪和定位。, ^; o1 m/ I' R2 z; L$ i+ U$ x6 E9 r% x& s2 R3 G0 Q' e! z$ t1 m ? 使 $ a' E/ D4 f) T0 u' ~; B# s) @$ i- l6 L3 m! I1 P7 s- f! p1 v ~4 i 航线, - Q) [( ]* I4 H3 U+ J" J以走廊形5 Y( M: z6 H' e! j2 F1 s6 v, S 英汉对照民用航空词典B OEING & U8 h1 [) n- xTECHNICAL DICTIONARY 6% {7 Q/ q. b; O4 V* ^3 x( g+ U AIRFOIL, A surface designed to obtain a useful reaction,; k7 D1 n7 C4 u% c such as lift, from the air through which it moves. Wings,& J- w1 H5 w7 k stabilizers and control surfaces are airfoils. L; p- y5 h* k# a- @7 g AIRSPEED (IDS, TDS), The speed of the airplane1 j6 T. p" a/ s8 G U. i rough the air. 6 |" g% d$ B: V1 ?& w) B: W8 M" d oD INDEX, An adjustable pointer on the " Z0 h& }6 r; r+ A7 |- |# `irspeed indicator. ; C. i* a& o. `3 K, Z1 Cand legal ability/ U+ X/ W+ I6 _ fly.' k: N8 {5 G( [* l) u: w0 c3 t m, for example, the procedure for finding the . C' p9 n8 F1 b) dquare root of a number. 2 J. i0 G$ g2 S( ~# r v2 o- cy * G' Z; u4 v& p9 Q) C* d0 X4 cre, wind,9 I- `, N; ~3 J9 S and aircraft flap setting.2 A8 L; _" B% `. u 是翼面。4 ~) _( c# K9 n* g) M) D 速, ( I7 Z7 s+ }# F! F0 e$ h0 e0 H0 [飞机在空气中运动的速度。2 l; S: a' G! n& T, z5 b7 v' b/ [' o4 F, F& I' h 在空速表上可以调整的指针。 & u3 W$ {3 _! C$ z9 s& H1 z机械飞行能力、和合法性的飞机状态。7 R x+ m1 Z Z! R 一步一步的解题方法。例如,计算一个数的平方根的步 1 D3 @* C7 T4 K) I9 V/ |5 Y6 n, ~$ l9 i. w, O; t9 N" D3 t6 ~7 m( N& u$ b Q$ R( e 资料的法定文件。 ( |8 W O: e3 {7 D2 c翼位置成函数关系。7 q5 e* v0 d6 Z. N) m th 5 r: u% f' t: EAIRSPEE & J2 X0 M/ G4 c9 ~; Ba 3 N9 D% ?6 d8 U# A2 C# @, ]; { q5 WAIRWORTHINESS, The condition of the aircraft with' x( S/ w+ j& E% ^ respect to its aerodynamic, mechanical, V* }; ^& N5 v( D- z to + @' r2 x# M' z# JALGORITHM, A step-by-step procedure for solving a # Y+ b$ Y0 l! p0 e3 N" Mproble& @, L; H- n A3 C; {' D& b s 0 r1 R0 m8 m/ l: d+ M, ^$ k qAIRPLANE FLIGHT MANUAL (AFM), The legal" R2 B% y# U! N2 k5 ? l3 H document containing performance and operating limits, 7 p' M3 T# Z. G/ ^1 s- A) p$ Noperating procedures, and takeoff and landing2 s( B# |3 l9 V performance.# q9 `# m6 m8 Y5 }# N7 f4 J, e AIRPORT ANALYSIS, A comprehensive set of takeoff $ c4 ?1 M. j! Pweight limitations for a given airport runway, generall & k; Y1 k2 R R0 q. Qpresented as a function of airport temperatu 9 k: S; y( a2 r0 k/ U! Z K翼面,8 D' Z/ T& q; z+ u. E 用以从气流中获得反作用力(如升力)的表面。机翼,& R% m; K, b z: J5 O3 T- b9 g 安定面和操纵面都 2 E* R) m& A% \6 \$ B# Z/ `& K. O' b8 ~ B( D ] P 空速指标/ n6 M5 D3 b" Y# z9 b8 C" o 适航性, ( Y: _5 W3 Y7 N8 a# ]; i1 h有关气动能力、& E; `5 `4 \0 D5 F/ C! ] 演算法,' i; N9 ?, B9 R+ d6 _8 J3 W9 |3 u. H0 ]6 X( E飞机飞行手册(AFM), ! F# _0 p4 z$ M/ T包合性能极限,操作极限,操作程序,起飞和着陆性 : g# |& ~/ j: Z2 M) g, b5 E' U. C6 P( f. Q, R- d7 Y 机场分析, ! {+ h% v' b0 ]; s4 e一套针对给定的机场跑道的详细重量限制资料。通常与 % Y/ L( h6 q7 |$ n机场温度、风、和飞机襟 ; I6 [3 H& m7 D' D9 \英汉对照民用航空词典B OEING% y# G. C; {% @) g: @& v% v TECHNICAL DICTIONARY 7 ! |* Z$ r% z5 J9 l1 @) l; O- u0 Y5 hAIRSPEED BUGS, Adjustable pointers on the airspeed( v6 p6 K# d/ f% L% W( Z2 @ indicator.* w4 t z J0 z" o) H ALLOY, A mixture of a basic metal and small amounts # L1 m% y, B' U6 h: _( S- Cf other metals to change the properties of the basic ' C2 c: G L# ~& k& E8 wetal.) c& o1 a# Y, Z0 W, F Minimum airplane speed., V! Y3 j! r! ?! ^ h& l% z e of8 k0 c7 D3 c! G2 k9 D itting airplane angle relative to3 n! j1 l; o2 U1 j, P6 q, r+ q2 h! P irstream for the stall warning system. 8 G! @5 s, z0 j) L% ganother. / y- S( I; |6 V9 bLTERNATE , An additional airport selected during ( Y! c. f# k/ i+ n0 K& r' T0 \6 e( P6 D% h# ^6 I; ? 合金,# Z7 `6 ^. c! p2 m' b7 d) f3 e+ K 在金属中加人少量其他金属,而改变其性质的一种金属 ( v5 r: x8 {$ p8 i5 L% y6 S; v合物。0 u% j. H' r2 d/ [6 E5 K+ ~ 飞机的最小速度。/ a( u- V; j& R$ j$ G% w/ T 速警告系统传输飞机对$ S2 L, F/ Y+ P! L5 X 流的相对角度。( a" S8 `9 W& I 由一个状况改换到另一个。) t- ^8 ~+ G; l5 I* T 降场, ; h& B& z; i9 M l2 ?划时,除了目标机场之外,所选的另一个机 " H* y U4 L' U: h/ r1 R7 p- m* Xo & e$ `+ w9 S8 P$ w C1 Mm2 }* }$ G: W: j) D( i ALPHA SPEED,! Z, I) V/ }; ~* Y4 M; o& w ALPHA VANE, A small moveable airfoil on the sid 5 R8 j8 T+ @/ k7 kthe fuselage transm + w- W; o& ~ D) a9 va' J7 I. Z# d3 t; Q4 J; C ALTERNATE, To change from one condition to 3 d9 O! J, L( g7 ?- ?- eA# R& w) g% W1 t9 Q: O5 | flight planning, usually near the destination airport, to be " ~3 T1 _1 [( N2 X7 h$ lused when it is desirable to divert from the original8 l5 f+ ]* M2 J L destination airport. ! T. E) o7 x! L2 u( y1 z1 D空速游标6 O3 T+ z/ n( b8 K 空速表上的可调指标。 0 @. S2 t. o( z0 F9 s- e) k0 @( [+ d0 d5 }1 `( m 迎角速度,/ z3 u* v, U! j/ v 迎角叶片, ! Q+ z' f& }: E. \0 |: @; E位于机身侧的可动小翼面。为失% p$ b( o6 W/ R" U" ^ W! @& r" j+ l( {. W/ u; P1 g5 K交替, & D/ z! R0 _' l* D0 P6 u$ R1 V* R4 w _- X! e. d5 f 制订飞行计/ c( a4 U* b% ~) n( t" C 场。通常在目标机场附近,以备不去目标机场时,改降之 7 R, [3 Z/ n. @/ [+ k用。4 Q! O& v3 Y0 m) m7 P- E0 W 英汉对照民用航空词典B OEING 2 }) D1 Q+ _4 B% @4 S4 LTECHNICAL DICTIONARY 8 % O+ C: u. _' `* y7 B. vALTERNATE AERODROME, An aerodrome to which . v8 I: c1 ]7 ^( m' V" Nan aircraft may proceed when it becomes either 0 v8 A' x# B. G2 T) ipossible or inadvisable to proceed to or land at the5 {! g& o- U3 F erodrome of intended landing. " q* r5 d) p6 m' c$ d5 e* ^TER SETTING, The adjustment of the altimeter ' x; D) c, F$ Xaccount for local variations in atmospheric pressure.. e9 e6 ]* N9 `' g! ]# M+ [8 E/ F LTITUDE ACQUIRE, A digital flight control system # A4 N, p, Q/ dode to transition from climb (or descend) to level flight., m" O2 V- E M LTITUDE ALERT, A flight deck alert occuring when the 0 j3 L3 [' F7 f# l- i; Virplane approaches or departs a selected altitude. 0 a) f0 t* v* y5 _- jLTITUDE CAPABILITY, The maximum altitude at$ s& f* s# F5 K# b0 W) q hich the airplane can be flown at for a given thrust,- h- l! B6 [& _9 M$ q F/ }, v peed and atmosphere condition. ! P, I! a& f/ q. @* nLTITUDE HOLD (ALT HOLD), A mode of the autopilot- @* v2 F3 Z: ~% Z r flight director to maintain a selected altitude. + x9 q5 ^1 g% w% Z! {$ ^' {; G- {2 wirplane's altitude during VNAV operation. 2 G& c% B+ C! ~1 C7 H机场着陆时,可作着陆使用的 ) ^8 r. S' T8 c$ Y! Z# z场。! R9 k7 A s3 j/ s2 q% }. W& R2 }3 J根据当地大气压力变化而对高度表所做的调整。 3 Y$ G6 h% f z( v& e; ?% z& f& K6 B一种数字式飞行操纵系统,从爬升(或下降)改平的模 $ [3 I' a# \9 @: _8 ]3 L+ P8 U) i9 i$ x3 d: b! S# Q 度警告, ( Y# j6 _! ` ~: A( P当飞机接近或偏离选定高度时,所出现的驾驶舱警告。 , ]& S# q. t0 l9 ~7 H0 ~% V高度能力,# ^, f9 R) q1 W& s" e 在给定的推力,速度和大气状况下,飞机能飞达的最大 ! B4 z8 v; P: `$ k高度。 ) i0 V* J3 D& i& u+ Y) X高度保持(ALT HOLD),4 }; t7 H- }5 \: s, F5 }& b0 j" [1 d; m 自动驾驶仪或飞行指引仪保持在选定高度的一种方式。 + y& n% s7 B( [4 f& L% |# S: E0 }" A% N 员对飞行高度的控制。 3 \ ?# ?& ]: Y7 Q: U9 U7 i Z# Vim ' m/ R) C, b; g5 K9 Va$ R" h* }& S$ h: B0 m" o/ c ALTIME ) F# Y6 l. D6 l: a7 pto , E y/ |; `+ l5 i# IA' z R/ E8 U5 d, K& A+ F m " l9 I1 _8 k/ ` V' k6 A3 o/ X# OA! d& Y- V8 ^* D6 A) U# \ a$ z, D9 z/ G$ y0 ^ A" g% y9 d$ ?8 ^ D" r4 k w " P7 C& r5 D2 m" }, }s + O( V6 D Z& K0 k9 {7 e6 mA* c+ g8 K7 w7 O& G6 Y; @ o ) A' H: D) r; W, P g& ^( C& yALTITUDE INTERVENTION, Pilot control of the * C: J$ M/ F6 v; Z4 F( q a; y- s* La7 Q3 A' `$ D& d0 d# }& v* U AMBIENT, The surrounding atmosphere.2 C4 c0 P+ Z4 C5 c+ E+ E 备用机场, , e/ H( ^$ }0 a# m6 o当不可能或不适宜在预选 * V; X- _- Y# k8 z& E* \7 t: m$ A( d, a& {- K- Y- ]$ d: }高度表设定& f7 t& d7 I' |) J% Q 高度截获, 2 ]0 L' C0 j4 u) ?; D3 X3 H! C. i6 h q" O/ d; w8 t5 U( b( L7 g( a高度干预+ B% \% ~ g+ f6 Z# f6 ~ 在垂直导航工作过程中,飞行, J$ q5 D, U' b! _ 周围环境(地面气层), ; _$ [. m. n: j* V3 c- z物体周围的环境(特别指大气)。/ v" d2 A- l0 s" b 英汉对照民用航空词典B OEING 3 G" r/ \& U* }' U! MTECHNICAL DICTIONARY 9 ( Y) G- |% O. K0 k k& I/ F% m/ CAMBIENT PRESSURE, Pressure of air surrounding an ! u( x# e6 s* `* P3 g' c! J6 R, {object, measured in pounds per square inch (psi) .1 g! w `, V* ^ Q! V MBIENT TEMPERATURE, Temperature of air % Y0 a% q1 _; E( F* C0 ompere. ' i* c$ a6 u2 n/ eurrent waveform.* g* U- N; a+ \# \ g an 7 y7 M( o3 H: y* g$ u0 Pnalog signal to a digital signal. * b7 _9 j9 g$ Q- r) e; p. }ore inputs ) d4 I. f! N) Wf binary digital information and one output. The output, C* @/ h9 a! n4 u9 T* H 1 only when all of the inputs are 1. The output is 0 1 y& Z- z- {5 G4 Khen any one or more inputs are 0. # n' y7 G# X/ g8 k面气压),( f- C4 G" {" f 境温度, 7 e2 p0 l& }/ d, D- E气温度,用摄氏度(°C)或华氏(°F)来 0 G3 [$ k6 d- n) R- t {8 ?( Q- X# z$ ~# a电压或电流波形的幅度。! f1 j" s: \' Y% ?4 v 性变化的信号来工作,或产生连续性变化的信号 A' S5 Y1 B+ O/ B2 C3 x4 a 统。 ) A) M8 C1 _+ ?将模拟式信号,转换成数值式。 8 W, ]! |# T# ?2 g一种有两个或两个以上的二进位数字信息输人,一个输 ) k3 d5 f2 s2 _2 r- Q6 @; U( b的装置或电路。当所有输人为1,输出为1。当任何一个+ V* p6 h' G' `0 U0 r, c 一个以上的输人为0时,输出为0。. W" d. ?8 ~- q/ A A, ~7 ~" ~+ Y! s- N surrounding an object, measured in degrees Celsius 9 _! D% X2 [- u& d$ z6 X(°C)or degrees Fahrenheit (°F)." E) W" A; |$ Y$ m4 c {2 b AMPERE, A unit of electrical current. One volt across ) u- W8 p" y( k' V; oone ohm of resistance causes current flow of one* t% q/ J& _ }0 F, F; L a 6 g& ~" E. n4 K, M$ Z; x o+ kAMPLITUDE, The size or magnitude of a voltage or - T, C$ f9 T" [5 \+ ]c7 R9 Z l- S" _& a ANALOG, Quantities or representations that are 6 T, k4 [1 L" o1 N/ S* Yvariable over a continuous range. ! M& Q) y! \1 L% G0 ^2 j, w; bANALOG-TO-DIGITAL, The process of convertin & h) [7 n \! s7 F% k( @a / V( o6 k: Q6 W# N: f4 K; W) H& XAND GATE, A device or circuit with two or m ! Q7 a0 f- }! Q9 I: K) d5 U* Co : v9 m9 F% b# Y1 ?4 h `is# M, F7 s5 }2 r9 i w& F, M v1 C3 V1 ^6 l# n5 m 环境压力(地8 V5 a1 _# v/ @ 物体周围的空气压力,用每平方英寸多少磅(psi)来/ x7 y! c6 C F3 T- E8 D 度量。 / x( y# ~7 x5 Y& L/ Y2 X& ?& u. [4 o B 物体周围的空" B; y" |7 V3 x. x3 [% N0 O 度量。2 a+ h) ~# h0 F3 S2 T1 l 安培,2 D- _' k6 d* i7 B% H, s4 z 电流的单位。8 Y( Z0 d. g' X G6 t L 1伏电压在1欧姆的电阻上所产生的电流为. N3 T! @' c1 e# _2 t2 G q 1安培 4 P+ [1 A+ c. g9 j- k# `振幅, ' W4 _* l% a: r3 k. K: e# V模拟式,% I; ~: Q1 p$ e, z4 }" U; ^( O 用连续 ; ~* B5 K! M- p- F3 r& k; i6 W: [! N6 t# v' t& U从模拟式到数字式,: b4 E! ~3 h' s 与门, ) r2 ]+ `$ X% K( a9 t8 A% U$ W- g! o6 ]! h0 n2 p" h& @8 i* X5 A7 u1 E( h 英汉对照民用航空词典B OEING+ M' I5 K2 [# c% K! G3 R6 { TECHNICAL DICTIONARY 10( y) F$ R1 H4 r" k. _, X ANEROID, A sealed flexible device containing air at low0 _/ ^% n: c- W6 E( C# K9 u pressure, which expands or contracts during change of8 \+ W! O" W1 e, ?% a+ |/ R) ~: M- Q ressure outside the device. $ Y9 p# V+ C1 o% cically+ r# E% P! E2 [ V r changing the direction$ c5 z& p, d4 z) y8 Z+ T- x% w f drive.1 D* }" d. q2 { M of the wing chord in * E/ j. P( ]( ?lation to the free stream airflow as it moves forward8 I: Z( v( l5 |( ?3 C rough the air.6 H- S- B- y \ al axis of the 4 t J: I% L5 b4 \5 O# |: M' ]aircraft. , C. D* V3 H4 ?胀或收缩。 3 B$ }# C6 `, ]( g; I$ o3 F& a箱。是改变驱动方向的机械装置。 * d( n! O( c+ k# g% ^机翼翼弦在空气中向前运动时与自由气流之间的夹角。0 Z" N* L `9 V# @/ U/ W: n" r$ D' V* u* X4 g" X p " C# }& k% i& y# M5 pANGLE GEARBOX, A part of an engine, mechan* J# _% s- a% P6 {" r3 d driven by the compressor, which drives the accessory : `# s, }1 l) f; Sgearbox. A mechanical device fo , K, i a& L; U( H( M5 `4 `o6 N: {$ V f7 O- b3 r3 N7 e ANGLE OF ATTACK, The angle $ b0 F' i5 n7 A( Qre8 F7 i6 { A5 C# e( v th ) i1 O1 |3 m9 {# @6 mANGLE OF INCIDENCE, The acute angle which the+ d. l# R" r n1 `- o! [4 n wing chord makes with the longitudin / y7 N n/ x" W膜盒,; ~# l6 ]# v Z9 [; { 内含低压空气的密封弹性装置。当它周围的压力变化' r3 ?; d8 Q) R" q. {: Q4 f 时,会膨0 S& B% W( x, J& _" X9 Y 伞齿轮箱,+ {! T+ C$ L. P# | 发动机的一部分。被压气机以机械方式驱动,然后驱动 , p. G* t% t: x7 D& S附件齿轮 I* }* e% A' y. ^& {迎角,1 I( g9 Y( V* `) Y 安装角, # V) t# i: Y( q飞机的纵轴与机翼弦线所形成的锐角 ' U! E% z$ q4 e8 B英汉对照民用航空词典B OEING9 a% k- c t) S+ N/ G5 G TECHNICAL DICTIONARY 11 6 W( ?# H2 B. M0 H NANNUNCIATIONS, Audio or visual indications used to9 O9 J3 Y7 E! ]/ \" S call attention to an event that has taken place.! T) @) i: V/ d, \ ANNUNCIATOR, A visual device consisting of a number * A, o w9 z0 J0 Z# C% s3 kly.' i4 Q( O, D: U2 W ANODE, The element toward which the principal stream' V# o- U2 r: ]$ V/ I of electrons flows. # X, j' n- @ x1 a2 ]3 F ~ANOMALY, Not normal.; J2 {5 l$ M0 J* z8 M ANTENNA, A device which, used in conjunction with a ) T. |0 u# N& y! w. ]5 x$ Otransmitter or receiver, is used for radiating or receiving) [- T& w- B2 R radio waves. # p# K1 |$ q: F' BNTI-ICING, A method of preventing ice formation on' |9 @% g0 q- J& t e wing leading edges and engine nacelles. - u2 u6 [+ U' {2 U* R. q" f7 jNTI-SKID, A system for providing maximum braking 2 \7 o' H3 \+ u4 _/ n H( G' b" rithout skidding for any runway condition. Anti-skid3 ]+ [. f1 ~1 M5 J2 e, l( _ omponents are part of the brake system. ; Z: Y* R' x1 ~3 c: L: F: A9 {& X告,) _* a) V) y) m4 O0 G7 | 当发生事件时,以声音或目视指示形成的提示信号。 . Y' L+ ~6 c" R9 k; s. Z4 T与之有关的电路的现有情况或已存在的# Z- D4 {3 P4 c7 D4 R* H) f7 o, q3 Y- `" ]正极, ! n: V6 i$ d. n0 z; [6 }主电子流向的极位。 8 R/ v: x6 r+ g3 k) l9 a异常, ) W8 C# g4 f% F$ B6 Y- c, l8 C4 r不正常。- g2 @( W5 F0 h% N4 t) B, \ 天线, * U B& G; e; d& Y; p一种与发射机或接收机共同工作来发射或接收无线电+ F" I; J5 Y; P1 X 波的装置。9 r% g# ?7 s# M1 ^7 R7 q 冰, 4 r# O+ G; }! n, {( y3 [7 n: S3 C防滑系统, 3 E- w3 Z* T( a9 I1 [" [* ?! ^一种在任何跑道状况下,都能提供最大的刹车能力而不7 ]4 Q* H! o+ C! E1 r% G( w4 V5 U 使轮胎打滑的系统。防滑部件是刹车系统的一部分。 . g+ w' D4 l! w/ q6 P$ Eof lights. Each light indicates the condition which exists* z; N9 I# \( j8 ^. K or has existed in an associated circuit and is labeled 9 W/ a1 V9 J4 W5 h6 i, Baccording* v1 W! m! _- C+ H5 ?! u+ L A ^5 y( F t! l. I- l; }9 rth / _5 \/ Y. n3 a |" cA 3 j% G/ O9 B; ?+ x. ]8 d) hw % J+ Z8 l" u- {0 s8 |0 uc 9 h; y; Q9 j0 v \. [( l3 G$ H6 E" ^7 r* H, ?信号牌, + R. T. y8 u' m1 g5 h9 ~2 M* _由一系列指示灯组成的目视装置。每个指示灯都有相应 ( C- W R1 z2 c+ j5 h的标记,用来显示 3 Q) A! |! z4 }) V( K2 m2 ^- ?/ W. D* x2 i- @& ?/ D) _1 h7 _. D! Z 防止机翼前沿和发动机短舱结冰的一种方法。. f, n u" n% b0 n/ K+ r1 h 英汉对照民用航空词典B OEING/ P1 F( ?2 i! f! n- `/ X TECHNICAL DICTIONARY 125 j( l! ~/ z; I APPENDIX, A supplement to the Airplane Flight Manual - M, D6 e1 b+ E. D7 rtained in the basic manual. A ( ]$ D8 [ b/ q7 `, tollection of supplementary material at the end of a & p# N: C8 y3 X8 Vook. ' y% H/ ?& O2 @4 R; vof the ( `" z) s B' d) Jrsion link on the landing gear. 2 G! S% R1 _2 H( e8 h" vAPPROACH MODE, An autopilot/flight director mode) v1 }: Q8 ^8 n2 m2 ~# g; ~ which is a combination of localizer for roll control and / F# F' N. r5 G0 U" ^& E5 @glide slope for pitch control. This mode is used when full $ o1 |" n5 O/ \! Finstrument landing system is available.% m6 v2 s5 [. L1 l4 X h9 ?1 H APU, SEE - AUXILIARY POWER UNIT ( n, ]- c. p& e+ W" CARINC, SEE - AERONAUTICAL RADIO * Q/ K+ w3 U0 tINCORPORATED4 A, H. z1 T, q8 j& ]- O* ]3 s ARM, To make ready for operation. ' _0 O0 |+ j* v) g: v附录,- j6 W6 r {) k9 g 飞机飞行手册的附件,包含基本手册中未提到的飞机形 h/ v" i% x1 K {2 K6 x态的其他性能。是附在手册末的补充材料。' Q; C$ G. I: R" Y! t9 C2 t. N 顶销, . J* T* e1 t( l: O用于连接起落架扭力臂两部份的销子。3 ?4 p' A* ?, |- q/ I/ ]1 s 进近方式, . n, g+ V+ a) E- O# x4 `/ `9 p# P一种综合了控制横侧的航道信号和控制俯仰下滑信号 : W2 n/ Q' I# Q7 {* h. \' X- J+ r的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系 & S- B( i4 p' @2 r统正常时才使用。! {- p* r0 V$ P6 | 辅助动力装置, 1 c7 I0 W# o6 x- Q" H. h; o8 ~2 s见Auxiliary Power Unit # l1 o5 m( w4 v. ucontaining additional performance for aircraft 0 x' g0 x; [6 {$ \4 Bconfigurations not con 3 h2 W+ T7 }- D) \3 Gc$ C- C9 r" X6 y3 U' R6 p* t% J2 k S b $ K* T8 P) g/ G. c- ?" pAPEX PIN, A pin for joining the two sections : a; q* c- ]$ S/ [" Wto* R8 G& h8 k9 p7 B+ u; T8 [, d% K0 K! t# o4 C f 航空无线电公司,6 I7 {% n8 |% G9 l6 Z% N 见Aeronautical Radio Incorporated. 0 P$ E5 W H" {0 W8 L5 w预位,! ]# L' f& m5 o4 F3 f7 u 部件可以开始工作的状态。 / e' O6 K3 M! P4 ?% M7 q4 l英汉对照民用航空词典B OEING ( {) ?; Y+ I& q( k% v( rTECHNICAL DICTIONARY 131 T8 U. U4 k/ A& s2 ^- @" r) O" p ARC, The curved track over the ground of an aircraft1 A0 c5 k+ A5 b; R* z4 n: G flying at a constant distance from a measuring ; C V( m8 x& [7 \equipment (DME). , |* o7 {: `: N: o( b9 oin the limits of self-contained system # R" [* D e/ ~; p9 }apability." J4 q# P" `0 T) N tem for opposing or restricting 4 l1 D1 Q$ r; u- V, povement. 3 O4 u, `3 ]' tSPIRATED TAT PROBE, A sensor that measures total- A& d! H) K: o" a9 M0 u/ E ir temperature when the airplane is in the air and that % ~# m g% s; M& @9 c9 k% {) D/ Oeasures outside air temperature when the airplane is9 d& o5 v# L# z* L; n2 ]) o n the ground. The outside air temperature is measured " L4 J P/ B/ i' n, N: U3 _SSEMBLY, The fitting together of a complete structure. @# d4 Q' r, x. A+ a SSUMED TEMPERATURE REDUCED THRUST, The4 r) c% Q) w) v; n7 ?, z5 L0 c/ v ATC, SEE - AIR TRAFFIC CONTROL* [* [7 p7 S* T D, ~; M7 [9 Z& ]3 F: o, R% I: _3 }系统中所产生的一种用以抗拒 1 X8 D' M$ S* \- L) _" @ ]$ e作或限制动作的力。 ( H# [" t; \" p4 s. h( T头, 4 x( b8 N4 I0 Q+ g: z( u用来测量飞机在空中时的总大气温度和在地面时的外 ) C9 s' k& t4 i; I/ a6 [温度。地面外界温度的测量是利用引气将外界空气吸入- Y& e6 L' g4 |: y" {/ H 头,以达到测量的目的。% ^1 m' V8 M3 A/ Q' } 配, 2 k9 z* {2 B/ _$ ?8 c8 ]一个完整的结构或组件的过程。 / B, d( T3 j: K6 ] M z8 q假设温度而得的减推力, 7 k. y2 n1 V8 g2 E9 Z/ y, X推力设定值时,假定一个比实际外界空气温 T! o6 P5 r% v空中交通管制, 8 a8 L, F4 n$ u8 g* Q见Air Traffic Control& E- U+ f9 o: ~- ]0 S* } AREA NAVIGATION/RNAV, A method of navigation6 [) ]1 ~/ a( r8 ^1 B; h that permits aircraft operations on any desired course1 t* p" ^( ?5 k+ e+ m within the coverage of station-referenced navigation ; ~0 w7 G9 t& T) Y8 msignals or with * I# w' I& @& T" m* r1 @c& r a% {# w# X O ARTIFICIAL FEEL, A force developed in the flight( n& V! l% ^% B, r* k control or brake sys 8 m% A$ \& h$ om * D- f, o" W# J4 ~& cA ' n) J7 T! U* O. @5 ~a7 P/ B# e2 o! L1 L m% |# a9 B% K6 V: P8 f$ D+ C5 n o 1 ~7 \: e) ~3 d- e b- Nby using bleed air to draw ambient air through the + K; V& I% W V# ]: p' h2 Jsensor when the airplane is not moving. + N' p7 W! |; r+ _$ ?1 M0 KA! x' u" s/ Z- k4 y8 F or unit. 4 R! v. |1 R3 G% V' J( ^1 n7 cA' z5 t5 A* B& N# j# Q f2 U lower thrust obtained by setting a higher than actual + e" O- u( n5 e& HOutside Air Temperature (OAT). 3 I# A7 R" K3 q& y- `弧线, p" ]- B3 k [! X) k/ }+ z 飞机在围绕DME台等距飞行时的弧形航迹。 ; p$ i8 R+ E3 q" c" k) {: n# v5 a8 H区域导航, 5 F8 ?- a* d/ z% y容许飞机飞行在有电台参考的导航信号或自备系统能 ! s$ \4 t1 L- r: k力极限范围内,飞行任何预定航线的一种导航方法。 ! L# t o8 c7 P" N模拟感觉) V1 L4 ^0 m, x 在飞行操纵系统或刹车5 I" l2 k+ s6 F6 V- t5 t5 ^9 x7 \: Z8 S% ^4 B B' t 吸气式总温探' i% E! f3 H& E% N7 o7 Z; r$ H; \7 j- f, F) c+ A' T: n$ L, |4 ^; |* L' G4 _/ V7 |$ P$ Y- _ 组合成 / ^5 m0 I# r$ P$ S% x( E9 S/ C4 _( E" J2 s- }; @在选择起飞! U% { i: f& e( V6 P 度高的温度而得到的推力。用这种方法可以减少发动机的 ' I% j+ K6 G( G# O磨损和维护费用。1 a# s' L4 i$ r9 m# ]4 H% t) ~6 E/ t9 ~8 y英汉对照民用航空词典B OEING) l5 x f& d( @+ v% T5 y TECHNICAL DICTIONARY 143 }3 ^& [9 T4 x+ L+ G ATE, SEE - AUTOMATIC TEST EQUIPMENT G- g% t. X4 j' g8 {- P0 K) A4 wATMOSPHERIC PRESSURE, Pressure of air due to the $ K- r y, [3 e. T8 v" f1 Tarth's atmosphere, expressed in pounds per square & Z0 w3 Z: i$ y3 A% G0 C$ pch (psi) or inches of mercury (in Hg) or millibars (mB).4 I. `0 l% a8 n: F TTITUDE, The relative orientation of the airplane with 0 g" r. @8 f$ t* `/ Gspect to pitch, roll, and yaw.( m3 p! R+ g# J* Y# @% F4 I7 w UDIO CONTROUSELECTOR PANEL, The panel in' E1 R; @9 Q& \* M a; _ e airplane which controls and selects the routing of 8 K' E$ r% `+ c; n! Sudio.' d6 R, ^3 P w& D" Z: J& g UTOLAND, Automatic landing using the Digital Flight- e4 ?( U" |, z+ p ontrol System. " H/ V% r, q. xn.3 ~* X( o: m5 G0 u* c) `+ k M, A system5 F' m# S# X7 p5 v, b& @2 R8 b! { omposed of all necessary subsystems needed to guide2 r4 A6 _) f2 h% Z* W( d e flight of an airplane. . m8 J/ g$ p h1 P. {" r9 v/ I5 dEQUIPMENT, System test & X$ t. \# X( ?, H* e* K+ squipment that operates under computer control. / v( w5 x" N# |# c! V V* K/ j' M装置,

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e : h. f: h+ t0 O$ c) qin # V3 m5 Z1 ]2 f+ l5 V! j" pA! ^/ S7 a' l: m, I6 z/ c re, s- t4 Y3 [' O J0 o: } A) c0 ~' ~% t/ | V# f3 { th0 _% E4 B0 O# f9 [, P; x! X a) p* M4 @/ B/ U- j( I) x `. L A , d: z3 s! J3 ?5 O2 RC+ q: ~9 [, u- W AUTOMATIC DIRECTION FINDER, A system which 0 o) c, P& d! N7 M# U7 [, |) edetermines the direction of a radio statio) K: b! O- v y9 y! R- H7 I) @ AUTOMATIC FLIGHT CONTROL SYSTE : y- p6 f. ~& Z$ {. f. _5 e3 lc ( m# [4 a5 M2 Kth 5 G# t+ ~9 e( C9 e3 F+ |. jAUTOMATIC TEST 0 _# z' ]% Y7 H6 Oe: J2 C$ x* Z9 v* d 自动测试. P1 R9 n4 C6 n( V 见Automatic Test Equipment. . F/ k! j1 M2 J% T, W2 K$ ]大气压力,! w) E1 X7 i* u5 V 由于地球周围的大气而产生的空气压力,以每平方寸多) K) s6 V2 r# m# W* Q ^ 磅(psi)或多少寸高水银柱(in Hg)或毫巴(mB)来 " X+ z7 M, u$ ^$ E ?# n示。 8 L- t( ?/ s$ M( f, f z2 E飞机姿态, : o1 w' L! h! Q, D8 s飞机与俯仰,坡度,和偏航有关的相对方向。* g; Y. {" \5 @( Z% t 音频选择面板, / H, }7 C; S- ^9 S% k4 }飞机内用来控制和选择音频通路的面板。2 @/ D* `8 J2 v& i1 _ 自动着陆, $ x: [- U: y: M v* k使用数字式飞行操作系统来进行自动着陆。5 A: M9 p$ \+ b% y 的系统。 + a7 h2 p ~1 F# X- l7 q! z% I5 I1 Q* @系统所组成的一个系统。5 f0 t+ U7 T3 h" L- [ 在计算机控制下运作的系统测试装置。0 {# K5 H6 _* m f X% r0 U- S5 W% [0 `9 U( x s% }- [" k9 ]! d, m- z$ Q1 q9 z自动定向仪(ADF), 1 x* U* Z' |$ q, w m确定无线电台方向 0 n p! R$ J9 b! I2 ^ O( W自动飞行控制系统. \5 F, N& h+ d% ^ 由所有能引导飞机飞行的子 : W9 F- X6 d' |自动测试装置, % @+ Q6 l- U% x5 \英汉对照民用航空词典B OEING # I) n9 s3 |4 r$ eTECHNICAL DICTIONARY 15 2 w" D- {! K; `& NAUTOPILOT, A system which automatically controls# Q% ~3 h; s1 ]1 l3 I and guides the flight of an airplane. 0 ^5 g0 \% m: y( IAUTOPILOT FLIGHT DIRECTOR SYSTEM, An $ @# x9 O4 f( f) v Rtor . h5 q' T4 ]8 X+ r7 C& uUTOTHROTTLE, A system which automatically) L* v! r% x) Z* K ontrols the throttles of an airplane./ k9 D7 D7 o# k3 G POWER UNIT, A small turbine engine in( `0 b" h3 b" x8 {6 h e airplane for supplying electrical and pneumatic- h$ g! Z% r! \ ower for systems operation on the ground or in flight. 8 m6 V0 c: |/ l! LVM, SEE - AIRBORNE VIBRATION MONITOR/ ^* }7 ~- V i XIAL FLOW COMPRESSOR, A type of compressor: i( C% W( [- J' d sed in a gas turbine engine in which air passes through 8 V [/ B4 b9 S( z( q( hXIS, An imaginary straight line or an actual physical 4 k9 A" @6 r$ ~; nomponent (such as an axle) around which a body can' A) V" ?# _7 w! o+ G# m tate.) r2 I/ a8 X" ^: F 仪,6 R) Z' C4 P; |6 d: K8 ?' G0 A3 A" |- ^6 |7 N自动驾驶飞行指引系统, 7 G5 t8 a7 a) s: i J A3 i, g动驾驶和飞行指引功能的系统。 ' a B2 w% u# G动油门,8 J* V `0 M2 L3 [* I7 W0 k+ a8 H 自动控制飞机油门的系统。$ a' R5 n% _" s 是飞机内的小涡轮发动机,在地面或空中给各系统提供# w2 R0 R2 H2 t, H2 W G 源和气源。 & M/ B! C) v8 y- x3 W2 t称。7 }0 H; B& o$ L% f$ {% H 载振动监视器," x/ ^- M' Z/ q1 `9 l 见Airborne Vibration Monitor 6 x1 w G8 T" B6 e; kintegrated system containing autopilot and flight direc 9 x6 M3 v0 M" @; s C( I, rfunctions.8 e+ [; T" ?4 d5 Q" {& z4 o# Q, Q! ] A . }) j' m+ z1 N8 S, B8 u# ]c6 Y) }9 D* C1 b; z4 `9 } AUXILIARY $ v9 ~4 r' v1 Z+ ^0 Tth* U9 ^3 F5 ~$ z0 |( \- v9 v/ L p) P) Z: P0 a6 f" L/ o AVIONICS, An acronym designating the field of aviation: {0 _' L$ P! ]# V electronics./ T7 x' Y+ o& v8 N& Y/ N A( q2 Y8 N: t6 @4 U; j. W) ? A% ?4 p/ R' a8 K9 ?( N u 3 R! \4 K# P0 r$ u$ mthe compressor in a straight flow, front to rear. 9 B2 ]( \3 |! uA 7 X; v5 n7 \/ ~; |. x% Uc- b! l2 d# X2 Z$ s ro: R. ], h7 Q2 l 自动驾驶. m+ c, F+ o+ P: p( N8 G 动操纵和引导飞机飞行的系统。 1 s5 Q7 ~3 L U- p3 U一个综合自, a ?7 ~: v! C" R, {# v- Y( X" Q" l3 b" H9 b/ S! r辅助动力装置, % E z1 }) \% K' I1 \2 {. a. _& _- A$ z. t 航空电子学,& }3 r$ |4 X: }, H 是航空电子领域的一特有名' `4 M; q- i. d% [$ ~7 b0 ~9 y/ t* W$ v- A; z4 y* K, g& ^3 ^: @' N- Q% U: W7 u1 a流压缩机,5 e0 R% g+ A& \- T+ } 一种用于燃气涡轮发动机内的压气机。空气由发动机的 ; X. {- A& q4 J7 a. J* f部流出。 6 Y% Z& H, k0 v3 m$ F n线,* E' e, T! }" Y6 L; _ 可让物体围绕着作旋转运动的一个想像的直线或实际 " V9 U4 ^2 a: O在的部件(如轴)。1 f/ ?( G ?- i. F" y2 O8 `. F& R7 P A p 前部轴向流人,压缩后,由后6 N: X4 C; r' R" \ i" A8 v7 y) k0 u5 Z: ]1 u$ N. N3 G P! ?0 f+ i" T3 E& ^8 K英汉对照民用航空词典B OEING 1 p$ c, K" t6 L3 _6 b- GTECHNICAL DICTIONARY 16- }2 a; G' M8 |4 b9 ] B - X Q! m& `0 a* ] @ACKCOURSE APPROACH, An approach to a runway 4 |5 X+ a/ o3 y. Q8 G0 n9 d# Aversed. , r! D# M: R' e0 ?' @own on the EFIS that / u6 n5 [4 Y/ F' V6 ioes not readily change, for example, navigational aids. ! ^# n8 o+ H& m' q# b, p. v: Dvement in the tank or reservoir. 6 i% f0 J2 b1 U* F! _0 G/ LALANCE TAB, A small hinged moveable part on the ; F L. A; \) w1 tailing edge of a control surface (aileron, elevator,0 g0 D; f2 T2 D. f. w/ J+ u( [9 v 航道进近, ( K5 ?) ]) V6 v9 J; l0 b相反的进近方向。当反航道进近时,无下滑 # X7 B! L3 C) Q3 q1 n: C3 I' J& B显示在电子飞行仪表系统上不经常改变的数据。例如: 2 Z! t- f! k% B) Q航设备。 " J$ j: R4 s1 e0 @+ ^. ~4 X% ]) N9 N在燃油箱或滑油箱内阻止液体流动的隔板。' w- S0 m b* ^# @3 u 动补偿片, 5 R$ \4 F& y' L5 W铰接在操纵面后缘(副翼,方向舵,升降舵)的可动部。2 A! H ~9 }- q5 s, z' u 与操纵面相反,以帮助操纵面运 0 o* {) n8 o! b% c9 c7 c* XB + u h& l; l: k, E S% E% jwhich is opposite the normal approach. For a 9 H! A# m- U4 z' ^; Mbackcourse approach, glide slope signals are not " m1 e7 m8 Y: Javailable and the sense of localizer signals must be: [! L$ J$ |2 ~/ B* M9 B5 O re7 C0 d! D7 L0 R% f! F BACKGROUND DATA, Data sh" H) s( w5 W$ m) f d* f$ ]1 n9 i7 ~+ |4 A3 ^1 y BAFFLE, A partition in a tank or reservoir to prevent8 q/ |- D x' L; T( h fluid mo * r0 O$ C7 t( y* ~/ J4 I, t) FB/ h2 m1 f2 V! ?+ F! O5 S tr# A& W$ s P6 l( Z rudder).The tab moves in an opposite direction to the # Q8 d/ O! X+ L$ Rcontrol surface for assisting movement of the control 2 y ?/ X' v& {surface. + A- ` z( e, u8 x9 k" \& l' f4 S9 c! K与正常进近 2 n; n9 `% t$ r4 U6 K: f道信号并且航道信号也必须逆反。( S- L# Q5 s! Y1 Q. d 背景数据, ! X. I( ?$ N& E4 N; m0 e8 R O- K 缓冲隔板, " J/ g6 E3 k/ J0 n) b- _) [# P; _: c* ~4 M, a5 R 随动补偿片的动作方向 # r P. ~ m+ T' m7 g动,减小操纵力。6 J/ ]) F* c% M3 ~) m0 w2 B 英汉对照民用航空词典B OEING' K' I# _( t# \0 Z: E) h- U& Y Z Y* q TECHNICAL DICTIONARY 17/ G; z4 _/ F7 }* [ Z" [ B9 k BALANCED FIELD LENGTH, The field length ! B; m" s f' ?. @3 nassociated with optimum aircraft performance when 5 W4 @6 ~; x( ?9 y8 A$ _bstacles are not a constraint. In this case, after engine% k8 a' c: Z% K' n: o( ]5 \ ilure at V1, the distance required to accelerate, takeoff! }: x" |$ u0 p( a' _2 r2 T nd reach a height of 35 feet is equal to the distance , V# M0 Z, s/ a- T$ M4 I: `ALLAST, A weight installed in an aircraft to maintain : T" U4 @2 U/ MALL NUT, A fixed spherical nut driven by the . S% n# J ~) X- r1 P+ }AR OUT OF VIEW, A signal used to remove the flight 6 q. j n. U" y+ U$ i- JAROMETRIC PRESSURE, The pressure of air above * ?6 R2 e8 [7 y% Z/ e7 ~g) or # r" Y6 [( y0 v5 _% W, x3 E4 smillibars (MB).0 G8 R/ m- \- p ATTERY, An electrical device for changing stored- |; M7 N& t* ?5 A% h2 C5 a% R 性能的场长。在此* `+ d- R( P0 z- {. c1 ]' z# z 况下,V1时发动机故障,要完成加速、起飞、离地35 ( ~% K8 m$ q8 C尺所需距离等于相同速度下完成全停所需的距离。 5 B% F; L6 R0 p _0 n+ ?舱物, # D$ |% l: F8 ^重心在许可范围内面装载的配重物。 t9 ~5 w$ v1 g; @0 s 形螺母, 6 O" l/ r0 b1 q$ N$ m8 Y的固定的球形螺母,用以使襟翼和水平% M9 Q, |. a4 G2 W/ e1 J) k. y 引杆消失,$ K' P) f' K; o. j3 C3 \ 指引杆的信号。 8 s, W, }+ [/ m! v N" i压,' S0 D- I6 A; e% o4 ]! N% L 压力。通常以多少寸高水银柱(in : S- h8 c ^) N" a0 M瓶,3 K& T% w' p4 j+ a1 P! o 的化学能转变为直流电的电气装置。' o+ H# ~9 Q+ ^* } o: `8 }2 S! N$ o+ G2 o fa ' c& A2 ^( i0 p5 s9 Wa 0 S1 O; J3 R; ^$ x$ Rrequired to stop from the same speed. & a7 q7 G h" [) x: qB 1 w' e, d8 P! N: F% I8 q4 \the center of gravity within allowable limits. ; v& G/ l6 G2 A. F8 Q! lB & e$ a$ ]) }" u" \; ` Yjackscrew for flap and stabilizer movement., W1 j- l* y! J" j# R6 M& Q" i: ]' h B : H6 {8 B$ a9 h. Xdirector command bar(s)./ |, {6 ]4 _6 W" s B3 h" X# k p6 z9 Z+ c: D zero pressure measured in inches of mercury (in H % C5 F0 @- h$ k) n' a/ ^9 qin # m, z9 y$ X: t* ^8 H: vBASE METAL, The underlining metal to which alloying % V6 v' C) W: y6 V, Gagents or metals are added. 0 t( _4 O+ ]4 DB6 T' b' A y- m: u% J. r2 `1 {( ` chemical energy into direct electric current. . P+ O' ?8 b: f6 |7 c& r$ o2 Z平衡场长, $ ~' |" e& b* Q$ \当障碍物非限制因素使飞机达到最佳6 E% v" M3 C: A/ [$ d; \8 S. r) p# A+ r+ `+ u4 O; e8 N; A; J9 I$ T$ F- V" n3 I- ~! Z; y8 d" S: Y9 i$ q为保持飞机' E g6 S! v ^! t* Z5 ^% p/ q, f8 ]* F, N& {9 @, P由粗重螺杆驱动 3 ^! K6 R3 L* p2 ]9 @( E( G安定面运动。 2 e1 Q8 T9 H" d% s6 _3 n3 } z5 }9 p" G" {* R. U7 {. a7 p. p 用于除去飞行$ w* S! n5 B5 \ U) [! j( a+ g; ?) C 零压力以上的空气 9 ~- E$ X5 D* ]1 P d q- ~Hg)或毫巴(MB)来表示。 / g1 r. i9 s: `8 w3 P% D基底金属, ( H0 A G: q! i+ ^指合金中的主要金属成份。 ) N% o4 H8 s) p& ]- y' \& M3 _6 Z 将储蓄; |4 o+ M9 k4 U) J" b2 a' T 英汉对照民用航空词典B OEING* T1 G( k6 S) j6 `! [$ k TECHNICAL DICTIONARY 18) \& a: z! U& A8 M- ?$ Y BATTER % y: h: a8 V% c+ |direct cu: c- ^8 O7 \, R2 o/ [; i power su 8 F" Q; ^2 q- \8 pY BUS, An electrical conductor supplied with1 \8 h! v- W6 R; T' j rrent from the battery or transformer-rectifier for( [- K3 }) D4 `6 N pply to operating components. 2 t8 r7 ^% k x& n) b( FCHARGER, An electrical device supplied6 T# J8 V( A0 t& D" r& l: j/ q ith alternating current, which produces a direct current* G/ r( o6 g, r. Z5 a4 l+ J utput for charging the battery on the airplane.- c9 D- {* g& U0 L AY, A compartment in the airplane structure. 2 Y" b4 _ Q( M" ^) R1 s8 W# s1 n% rCD, SEE - BINARY CODED DECIMAL $ `( Q8 [* X Y/ `2 u4 qEACON, A device which emits a signal for use as a& d \$ ~ I- n( j3 _9 H uidance or warning aid. % X _+ P' t: F- t; G4 \BEARING (NO. 2), The direction from an airplane to a% }" q# M4 m" a q/ |, g; f ground station. + k: e: n& x2 t8 b1 I瓶汇流条," t* f: G5 {7 l( u' \1 X5 @ 将从电瓶或变压整流器来的直流电供给工作部件的导 # z. y, ?& C- V% X$ |4 ^6 ?1 N体。: o9 o! W7 c" F, X3 W0 c& M 瓶充电器,7 S) Y9 w- G( Y: J# V+ M4 ~2 c 用交流电向飞机内电瓶充电的电气装置。带有交流电的; X7 O' b$ q. h% i+ l 气装置,该装置产生直流电向飞机上的电瓶充电。 - V" b, c: M' E/ D舱,) G* M# o; c) ~6 g1 G 飞机结构中分隔的空间。6 B% v* q/ ^% _$ F: ~& M! |7 G4 ] 二进制编码, 9 Y4 V* Y8 Y( p! i# P% L见Binary Coded Decimal$ f" }0 @- ^2 d4 z0 J% j% M, e; f BATTERY 1 }% F) t/ R+ n. w" X- h1 Qw $ t/ R! L+ `4 v4 B% b, P+ Jo1 G" ?# }/ g4 x4 X' W0 C0 t B1 m. J: A$ w5 E. a' S0 t5 L B( z) D1 m2 P& y, q1 O2 i" T B / o Q6 T! P; A1 [6 Jg + X& u3 c! {" z9 w6 I; z1 c _BEARING (NO. 1), A surface that supports a moving $ \# V. @+ |6 r+ Vpart and reduces friction between the two. 9 j0 M! @1 w9 d% C& P8 z2 R5 b* X* w i% u0 H1 J+ L0 m. l1 [* Y9 a* B! q0 L; v: }: S. P0 U3 F, `$ g$ u% s% ]- J5 X0 V+ O2 E1 C% v5 G* X+ q 信标, 1 F. a5 z9 ?% z0 C发射引导或警告用信号的装置。 1 J0 P: o2 T t; }! m方位(NO.2)," w5 [8 }7 P, I# R 从一架飞机到地面台的方向。" }6 e+ g0 a! ]* T; b0 o9 { 轴承(NO.1),! U5 ~ L8 o/ V0 t0 a# O 用于减轻机械转动磨擦的机械装置。7 p" [7 z! k' x; G" ]- n8 h 英汉对照民用航空词典B OEING 7 y2 M7 n0 g& l, g6 m4 Z. J qTECHNICAL DICTIONARY 197 ]; V( Y) L( p3 \( T4 E BELLCRANK, A double lever in the control syst 6 W: t/ b" K6 q( v; a* }9 x" S# dchanging direction of motion. ; U6 ^( t& T8 ]& b$ oem for" V+ s a6 }8 m% j ct in the & { E* o. b& o4 U; r4 i$ jneumatic system for absorbing expansion of duct due + _* h4 L; K2 R( o3 _; m7 xheat.! X4 [+ t; ?' L ELLOWS (NO. 2), Corrugated folded or pleated3 [4 `: M7 y& q6 Z/ L ontainer or compartment used to measure pressure. , v6 X; o; ]/ S3 \ kEZEL, The part of an instrument case for locking the) e8 x. x; c- M+ o' e( ]4 ` lass. 1 }- R( m0 R* g4 ?5 g, B& `IAS, The potential difference applied between two5 }6 G+ j. n+ x. O* k* ~7 } oints for controlling a circuit.) L& z, {+ B; \# T8 H, | BILGE, The lowest part of an aircraft fuselage. A place # d( [$ W% A3 U( d* a' D5 Z; j4 J4 Dwhere water, dirt and other contaminants collect.# D3 m$ S" a; I- ^( t+ ]( h6 t 气源系统内提供管道热胀冷缩所需要的余地的波状 2 P) [1 K) x. t9 A5 O9 F1 {轫管。 9 F* P0 j5 c$ s. k空膜盒,3 y7 R/ ?6 O3 V/ Y 一种具有波状表面的容器。用于量测气压。( b; b: }. c6 p$ q# p# m 嵌沟缘, 6 d: \+ ?2 f& [* W- ~将表面玻璃固定在仪表上的圈状零件。 " {: P+ c9 K! |' ?% w9 e压, % J* ?1 u' A% t z在控制电路的两点之间的电位差。5 p" i! M; N$ w# x9 W 机身腹部,5 h% ?+ _8 j9 a; H) d9 C, O 机身的最底部,通常水,脏物,和其他外来物集存于此。 # s9 D! c; N% L+ NBELLOWS (NO. 1), A corrugated flexible du' B& t# G/ W/ M p" q: w8 x: X a* q4 V5 ~% z z to8 r; r4 d. U# c" C B6 P( E5 j) O. r$ o4 R- }. p c [3 |1 J2 l% H. b) z& v* k/ n+ t B- d' Z5 K: o- o& v g - V$ }# B# e2 \$ ^B% E1 F* I- c6 q: {+ X p 6 W6 ^! e0 _+ u$ A& C直角摇臂,4 K9 ^( b3 {2 ` 在操纵系统中改变运动方向用的双臂摇臂。! g+ ?2 k. W3 b+ k 波纹管,% ?! {% U9 i0 D) B' m6 u5 t9 z! {: u' X9 Y i F- u: h2 U; \ C2 D' e) X! L+ P& g$ F5 a8 H$ C3 Y8 ^+ x6 } 英汉对照民用航空词典B OEING) s' {1 d9 Z& {; V" t# \7 M1 q TECHNICAL DICTIONARY 205 h; m( J5 G' }0 U+ M BINARY CODED DECIMAL, A system of coding each" I% e) W# {# ^7 z$ H' h digit in a decimal number using the binary equivalent. 7 k9 ]2 A( g; F4 J2 V& ^; C: lBINARY NUMBER SYSTEM, A number system using4 m z; `9 ^* Z- ]: ] s , b6 n. q, G2 S3 |2 W" dIT, In the binary number system, the smallest unit of8 Z n1 b/ ^) I% S2 d `" [ formation, consisting of a 0 or a 1. 6 _( q3 [& A; |0 }# [) x1 r/ W$ aITE, SEE - BUILT-IN TEST EQUIPMENT; \, q- P: {" w* ^ LANK DISPLAY, A display that does not have any% [$ l1 r1 J$ q; t% e7 G- j7 v dications, normally due to failure. 9 t/ {# R! \9 T* t* R1 ELACK BOX, A container for electronic circuits to record 5 K/ I% J0 h- m' Oight data. K9 `; u- G2 W" U1 sLEED AIR, Air taken from the engine to power various9 a8 h8 W. K& E1 y" _0 u1 A( q# } ircraft accessories.% X( h* x- n3 p" s4 t$ |: s A valve in the pneumatic system for air - c) j# H/ x. T4 R) @% S- a* ?1 w8 r- Gsupply from the engine or auxiliary power unit to the. R8 }3 o- g2 E# y* [- R. E5 j pneumatic manifold. A valve on the engine for reducing - \ j& S5 N! E# q9 |" q) N6 K: \pressure in the compressor section. 6 u8 F/ S3 N6 A进制,8 O! v) ~. J G 进制, + v F' u. {' v# q6 h一般用0和1)和2为底的数字系统。 Q- B) L6 {+ {" Q, R* w: H% J0 i 特(二进位数),5 ?% g6 \4 f4 d: s! j 二进制中的最小信息单位,包括0或1。 3 C @; E9 N8 t4 ^7 Z. M+ V内自测系统,4 g9 R1 x; }' z& j4 r) i 见Built-in Test Equipment# d+ H& R4 \$ u8 h3 D# Z7 M two symbols (usually denoted 0 and 1) and having 2 a . J |7 L/ h aits base.* q# Z4 j4 o; i4 ]! k: x8 o; O; a* s B 4 S( c$ e3 V( Xin* @, V- p. K4 ~0 e% m- H B7 B( v' f4 H% E% b m B 2 g0 X$ G6 U' X8 W; M2 {in 0 ^; s' d+ q% ^7 e0 mB' p: h' [( x) D fl- Q/ H( {) M! J' j1 d6 P3 L3 I2 H B& J* t& Z" ^$ m a ! S- H+ T2 m' |7 k+ oBLEED VALVE, . O" G& c( ?3 q二进制编码的十 3 Z t, [2 Q( m* _一种编码系统。用等效二进制位数编译十进位数的每一 ; X4 y$ e; H& D+ D6 G3 G位。 - A6 r9 Z1 c& L6 W y% M6 X( }! a7 m/ l. |1 C以两个符号(, P% a$ v6 a4 f2 _0 |/ q, W# K3 | ?4 x: G( m/ Z. |0 h$ P6 _- H8 K* p) M5 U . " t# k& P/ U* }9 B/ E1 e白显示, ! Y Z) G6 X; ?) m1 t通常因故障而造成的显示器上没有任何指示。 ) v( u B! U" }; }4 l- u" d- f匣子,9 r Y) L, l* g& {2 k H 装有用于记录飞行数据的电路系统的容器。& d7 t' Q/ H d9 a8 t/ h2 y 气, , ~4 R+ c/ i% o( D4 J取自发动机而用以驱动飞机上之各种附件的空气。- r, S4 f2 J; ~9 H5 e/ _% b 气源系统内,使来自发动机或辅助动力装置的空气进人 ; x4 B4 A+ t0 O- d0 B气源支管的活门。发动机上,用来降低压气机压力的活门。 ( j; Y- Y3 C; S8 n4 o; G) |/ o/ B9 a9 H3 |9 u$ \+ H" A( V7 L/ f. z- w4 V1 l2 n* n* \1 B; d3 e3 Z引气活门,& H4 `& c- P9 v/ @' ~ 英汉对照民用航空词典B OEING 6 ~4 G5 T2 R1 m. B. BTECHNICAL DICTIONARY 21 ( L! ^. x4 j% L. Z) f8 }BLOCKER DOOR, A device on the engine for blocking* P+ o% g8 _ R: [( c, a! m ~- E+ r the normal airflow during thrust reverser operation.4 W; G R! F3 ]8 v9 _ LOWER, An electrically operated fan for circulating air.* f+ [) S6 d9 {3 X/ z7 ?" t LOWOUT PANEL, A panel in the structure between 1 z P* d1 \ h- R" Z$ Ro compartments that opens to equalize pressure in ' w; k: }, G# ne compartments. * Y, h! l' h$ ~6 v( Y+ t DODY GEAR, The landing gear attached to the2 P9 r9 O+ ?8 [ grounding. ; W/ }+ P' M- i' A& I- W( w正常的 2 D+ V( W$ l/ g! A+ ~气流。 + r; O7 B! P: u# `$ R鼓风机, 2 r/ ] B. x0 m% i: s4 M9 Q用来使空气循环的电动风扇。 7 R/ Q# P$ e- }8 E- s压口盖, " l) G7 d& c. z* @" n* ]两个隔舱之间的口盖,打开后可使两舱压力相等。 1 j, Q W* I. n! K# \身起落架, 9 {( _; h9 L, h& t身构架上的起落架。; b+ H7 r4 U* w' D6 n7 V4 u B" P7 i& H- P7 u2 b) c- {* ~ B1 @7 Z1 C3 W" c+ K! L! { tw ! Z) Q" A+ A8 ^. x3 vth 7 M' S9 L+ p2 U! v4 c' ^/ iB ) s( c- `& r* I$ U5 C) h# c/ b3 nfuselage structure., c0 S8 k; T/ j0 j1 p BONDING JUMPER, An electrical connection between 4 g) \# ~" T, h( f2 ]4 n' Za component and airplane structure for electrical ' \& W! K# _3 O3 i4 X2 S阻流门,6 J' z* a" ?( F4 Y 发动机上的一个装置。在反推工作时用于阻挡 9 y0 X! ?7 w& ]/ H7 g5 o6 O% P- K" }- y+ Z Y- s1 Z& w& {1 ]' z9 g4 K/ v' B# H装在机5 N; {( T) a; d6 q1 U) S1 ?. G; i2 T 搭接片,! r' `4 f% l! P% c3 h4 U 连接某个部件与飞机结构以形成接地的电接头。 / _0 t$ b& N0 Q7 b英汉对照民用航空词典B OEING 5 }, [6 Z1 @3 A! o, J4 @3 yTECHNICAL DICTIONARY 22( t& f4 F7 F3 b' ~& V BOOLEAN ALGEBRA, A mathematical system for% e3 @$ t% J' f: }: o writing combinations of logical statements.3 N: U; ]9 A S, c- A6 B BOOST PUMP, An electrically operated fuel pump for ) T' e: Z# ?+ e& q: T. pfuel supply from the airplane fuel tank to the fuel1 m) q. l2 c3 D P9 u manifold. ' `! c* R$ o/ M* f4 kBORESCOPE, An electro-optical device for looking at 3 U; a5 [3 N% Mternal parts of an engine through holes in the engine. - v; G8 r N/ e0 i4 sorescope ports)% U- ~8 w0 N* G3 N7 f OURDON TUBE, A curved flat tube in a pressure gage& ?; X" ^1 Y U, |! M1 A& g0 ^! G r moving the pointer when pressure changes inside) _- V) M6 L% p3 T6 A% C0 ? on the ability of the brakes to 7 s1 C/ V* a2 r/ l6 kbsorb a predetermined amount of energy during a 9 E% w0 N, K- njected takeoff.+ r2 E$ ]% u- ^, N K1 R 用于通过发动机内的孔(孔探口)观察发动机内部件的! k! J% K: a) ~/ ]& K$ ^8 b 光设备。! j; _/ {& G6 F' g5 [- _ 端管, d! I- j1 v& `; l: l测压计内的弯曲扁管,管内压力的变化时它使指针移5 O" ]; f, r# c 力。 , C# {% e" h+ K, M2 l0 W9 ?极限重量,4 h9 d6 L/ U" j" H( P; k9 k: `) b/ f, z8 z4 z, ]; A 起飞重量。 & _* y7 L( M% ?/ e# C发动机滑油系统与大气相通的通气口。 % ]0 c; {0 u% S* n% C# o/ Win3 \9 g3 K* X& z2 a- O& S% O (b $ f8 S* @! i5 f% N; kB 7 l( A3 F I4 x( v1 bfo ( @ q7 t4 J% i7 f% j( q) H2 Athe tube. 3 f J4 y7 N$ R- T/ NBRACKET, To enclose or surround.9 u. j! X4 U7 l% L BRAKE ENERGY LIMIT WEIGHT, The maximum 0 N/ _% D' T5 otakeoff weight based - n/ U5 |& H& o, sa % w( I' J' D, T, c6 m. }3 lre4 D- L2 c1 C# o. \$ Q BREATHER, A vent to ambient of the engine oil system.& Z# P, Z5 O$ ]0 Y$ D: |/ O 布尔代数,/ _1 u* h4 n1 \1 x8 ~' f 一种用于编写复合逻辑命题的数学系统。 : v5 X4 N: p/ K5 G5 `3 |增压泵, " v% |6 r' h8 \" y/ \& s从飞机油箱向总油管提供燃油的电动泵。' k) J7 j4 o6 r 孔探仪, |: @) G7 K5 z/ g) ^' l/ @; Y# h- `* M' |" v% H. k: _: H4 P# X7 I动,以指示压 6 s6 ~. u8 a# i. H托架, 7 E! ~) m* z8 m用于作支撑、装托、或围绕之用。0 p1 u5 E) l$ A. @ 刹车能量 1 Q7 p1 i- Z9 e0 P" ]中断起飞过程中,取决于刹车吸收预定能量之能力的 * E/ \1 ?0 W( g. y0 ]& S" I. v- F 通气装置,8 \, v/ l, V9 X2 K& g5 c/ D! s( _ 英汉对照民用航空词典B OEING4 F. I' I8 ^( `2 i3 q' L2 z( V TECHNICAL DICTIONARY 23 - J% |. V2 k% k0 X" ^: u! aBUFFET, Vibration of the wings and airframe resulting* _, p3 N) Q% N. K; \* N6 N1 P$ T4 P from unsteady airflow over the wing; caused when5 u8 F* ~1 ^. H f+ L2 P( ` airspeed is too slow, the bank angle is too steep, or 6 P" L. u7 C/ Z0 Iirspeed is too fast.5 Y" E+ s. `( J- _ UILT-IN TEST EQUIPMENT, Equipment installed on # d- T5 r4 V% j+ R$ Fe airplane and in airplane systems to test the systems( V3 D6 Y8 h! z5 r! l( U* d ithout external test equipment. 3 a8 J! e/ I2 g( |UFFET MARGIN, The amount of residual maneuver ! B4 Q: e0 j$ M3 }6 V- P6 j japability present before the onset of buffet. ! b d" i) L* y, a: c; R1 z$ AUG SPEED, A preselecteed speed to be observed 9 a' K; z' x- z4 A Y. Inding sequence. # w+ T' _/ W; V5 C$ Zk 0 \9 t/ e! ^( Kng landing gear operation. 3 V( T. O1 o* p- Z {4 p, Q速度太慢或太快,坡度太大,均会引起抖振。 6 I. p# E8 m8 C. |$ Q0 C+ M自检设备, 1 q! z$ W* @$ \' A安装在飞机和飞机系统中,在无外接检测设备情况下,% G9 g6 x9 K' Y 用于检测系统的设备。7 `$ S. z' m" z) R. b7 A p 抖振裕度, / D) U a8 P3 d. p; z: f飞机在遭遇抖振之前,剩余机动能力的大小。3 [5 [7 g1 r& Y& W( k) l I 标速度, ; W3 m: H9 w T+ Y( w0 n在某些机动飞行过程中,特别是在进近和着陆时,飞机 & x$ {9 |/ b) S/ a2 ]预定速度。 ' b; c8 r$ m& c- \; D力装置,' f1 P ]0 j' W 架工作的一种机械设备(弹簧或减震器)。 & X3 R' q) ]6 g/ B5 V流条,7 e5 v+ O6 F8 J' [ 在部件或组件之间传输电、数据、或定时的单一电线或 ) }; R h. z2 C/ ]1 A' e5 \, g ja _# K: S4 d% H1 H( p4 A: WB , k# U1 f; z! B# [( N2 O9 f. p% h1 pth 2 w3 k: R& V: e' ^5 sw 6 A( @/ E& D, [1 n) JB3 O' J. J9 y( x. I5 R/ {1 ?0 W6 v c3 [# C! C y2 E( U3 q2 l B ! U8 c( D, W- o& Y% h6 xduring certain maneuvers, particularly the approach and. o z8 e2 ^; @ la 5 Q' M) A6 y! R) z1 ~8 I: CBULKHEAD, A structural partition in the fuselage or4 g1 W8 C- r* v" C wing. 5 R) Q+ A8 T" T6 m/ ^BUNGEE, A mechanical device (spring or a shoc) Q0 e3 U1 G# h/ ^; P7 e+ j absorber) for assisti4 O2 P, Y5 {/ T ]3 o$ `4 l ` BUS, A single wire or group of wires which transfers9 [' }: U2 J1 d8 |& g! q0 D power, data, or timing between several units or 1 k+ k/ _6 {: h6 X! `- rmodules. ) O) y& A' U8 ]+ R; k2 \& C抖振, 5 g0 g( D+ B5 H' [3 h2 b6 o由于机翼上表面的不稳定气流引起的机翼和机体的振% s* w- {1 W, B, q4 _1 O 动。飞行 5 R; ?. w! G: D x3 Z. E0 t; B, Q. p. z: I: n+ t. l所应保持的 * }& v$ N9 M& o* [壁板式隔框, 1 w. k/ w0 p7 ?: U机身或机翼内一种结构隔板。 8 a3 O# V) q- U, z J$ |0 X! U* O) k' r/ A3 \6 f8 m q' i+ t用于协助起落, P" C4 g$ q' O6 c- Z7 U" g& p$ b. e* P ?电线组。 " T9 a0 h+ c' o- n英汉对照民用航空词典B OEING2 ]% ]+ x) n+ s0 o+ |! W TECHNICAL DICTIONARY 24

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BUS DRUM, A mechanical connection with pulleys $ }4 n7 o* R$ @6 y* g' Ocables in the control system.* U1 W- _' K. c and( l/ P9 R- g0 ~; I ] l circuits for control and protection of 8 C, W9 D2 J& K/ H& m% Dlectrical alternating current supply to the airplane. 0 ]1 }* j3 N6 \+ N& T2 ^duct for closing and opening the duct $ }5 t/ p% \; w* kassage. ) k& \! u1 ]2 H: O0 I$ HUTTOCK LINE, A vertical reference plane along the 8 b3 i, i& f4 w9 xselage for horizontal measurements of the airplane.4 L* ~2 h( [+ U 接。 0 i) a1 R% j# G组件,内含控制和保护飞机交流电源的电2 H; r( F7 o0 @, L# q& ~: F' y- N+ q2 W: Q9 @9 S( N" g7 Z 作动简控制的转动装置。用来关闭和 : L% k$ {, J, `% `# S启管道。 8 f, w' Z) o. S% F" l8 Y' {0 `沿机身走向的垂直参考面,用于飞机的水平测量。 - R# h0 `# q- P0 p! Q+ JBUS PROTECTION PANEL, A module (black box)5 X5 f. l! N2 D7 [2 q containing electrica $ l* `& M1 }2 O, r% Pe & _6 f+ \" v6 N" Q( q. l1 ]5 `) f) SBUTTERFLY VALVE, An actuator-operated, rotating& o8 g& I/ n6 t' T% z: { device in a 6 o- x7 L3 T; x# y4 i/ yp $ t. q1 V7 @9 Y7 G+ S; ?B 7 m( s' k/ H/ w' Y" x- ofu ) `' ?( _3 O6 ?+ ?转动鼓轮,) |2 J& B a- Z% s# \ 在操纵系统中,具有滑轮和钢索的机械式连 r) Z5 G- U* }, ?汇流条防护板, ; h: k. Y3 i4 p( L; E黑匣子式的 8 i& S4 `7 }6 y' o4 n" \% N3 ^8 r8 ^$ }1 Q* K0 K5 a/ V" ~6 r; G `9 q/ }蝶形活门, 6 }5 }! q5 z& R D [0 Z4 s/ g是一个在管道中由 5 X* ?; l/ ~7 Z8 d3 l( {+ e0 ]1 J% V; a+ t4 E 纵剖线,& n, y7 Y+ i6 z 英汉对照民用航空词典B OEING ! E$ G- X3 \3 o/ RTECHNICAL DICTIONARY 25 1 w8 y, y$ } p8 r0 y- `BYPASS VALVE, A valve through which air or fluid will" T1 T, D9 M$ S$ J2 O6 A( F8 K3 E9 H flow if the normal flow path is blocked. ! ?! ^% W: `$ R7 X+ zBYTE, A group or string of binary digits. A byte is$ ^1 S9 E8 \1 V( ~; f5 h sually eight bits long. 7 k, p5 L+ R* ]3 U" a9 J) Z# m. o$ [) dABIN ALTITUDE, Atmospheric pressure maintained- O4 ^0 {: K: L0 \9 l! u3 H ithin the cabin, indicated in terms of feet above sea# A; C2 y3 S3 |# |4 S' N ALIBRATE, To repair, adjust, fix or correct the c: q! ?& H0 R/ U, g7 Z8 m Q easuring capabilities of a measuring device. 6 g$ _' ]; K: OALIBRATED AIRSPEED (CAS), Indicated airspeed # y! k3 F7 Z" Z8 J3 `3 h4 E( uAS) corrected for position error.1 {& g& g# x# A+ O# q7 ] nical 2 `$ W0 k; E2 y/ Zomponents.$ i- e u$ O7 \# p3 u& @/ B% g6 g3 o) q; t! h6 a2 d节,& C" \. E! L# }; u+ G) W 一组或一列二进制数。通常一个字节长8位。 * m* j: _' q4 h1 q; J舱高度,* f2 _5 z# l% X( X8 k 座舱内保持的空气压力,以海拔多少英尺表示。 1 Z5 Q" T: x: C' U2 |准, 4 r$ Q) }' M& K4 S" j修理,调整,定位或改正测量装置的测量功能。1 V7 |$ p) z, K+ B2 t 正空速(CAS), " `1 F/ t" y+ F- T在修正了位置误差之后的指示空速(IAS)。 $ `' {: V4 }9 b( l" n0 K0 M0 O用来移动机件的一种转动装置。 % R( ^" J8 K/ ^% a! n- cu - ?4 D2 y; q' I9 Y8 gC; g" y& a- G( z5 I* A1 P0 a( j C 9 S: C& w! J$ k+ I1 B2 Iw7 N X9 V6 o) W+ \) q8 h* L, l level.# x9 y5 H; X7 T. O' k5 D C' ?" }1 f# k, A: F( f/ n m $ A( m4 Q1 x# Y6 h" RC 1 x: ?; m8 R' r8 g9 n9 U9 Q& \(I J% J* a( a' l7 h FCAM, A rotating device for movement of mecha 8 n. J0 H$ ? \% m# EC - l9 a P4 K# ?. S6 ?. C旁通活门) i8 e ~) Y/ r; V) y# _ 气流或液流在正常通道阻塞时所经过的活门。7 N" t3 t C; v: p M: k# ?4 _$ e7 i" x# m; K$ ~. H( p& U+ L/ E! ], N3 i5 Q% ]) X' f( b, m+ T8 ^' [4 G2 s) [7 `1 q- [8 f2 m凸轮, * D0 y, s% R! G5 b% ?8 b英汉对照民用航空词典B * _$ a1 g9 W$ ]0 p% QCAM-OUT, An autopilot condition in which the actuator : P8 O& d6 m7 J9 e4 x1 G8 |detent piston is overridden, either manually or by the# e/ x$ p8 a1 D4 [8 T) g' `+ u ther autopilot actuator. 4 R# |2 ^7 n- }1 oAP, SEE - CAPTURE 6 t2 U/ ]. ~8 V. Q* SAPACITANCE, The measurement of electrical energy ! D# ~. ^3 [+ { j; b/ z7 e* ztored in a capacitor (condenser).7 k, D; o3 L$ f5 N APACITOR, An electrical component of two metal% O/ A7 _9 h, i [4 l5 M, w! r: X& ~ lates separated by a dielectric material, for storing1 I! p: Z# ?, j6 `; X! q5 |1 G lectrical energy. " D$ [# L. v3 q; U: A) _( SCAPTURE, An autopilot or flight director function to ( \% {. {1 ^2 t+ Y+ W% y* e, wacquire a selected mode.& v/ X# ~2 F2 r8 q0 Y+ y) { CARD FILE, A container on the airplane for printed ( O! ?7 h ]( F. G7 ]circuit cards.! I- t2 s) i" |8 P6 e 一自* L0 }0 o2 N! B( ?; v 动驾驶舵机所超控。 + e$ D0 @4 l7 ]" b7 h9 J+ o截获,1 S3 f9 L" a$ D* B, A7 { 见Capture$ G" V3 ?& G$ ~8 H. z8 M7 h o & C7 M' o/ a. |2 p" }0 h; N* W; }C! u* f/ c# c5 M/ } C 8 S: @6 e( X: b7 I% @5 M! N8 Ys 8 z6 [) a0 a) H% g* n: a( i; X. HC) N+ o1 {7 R0 w1 t p& J2 |: t1 y7 f6 Z, O e- Y% f5 K6 q F 凸轮不工作,+ Q2 P5 \& H/ q! B& ?7 [2 X2 q* k 一种自动驾驶状态。此时舵机锁定活塞被人工或另 : M5 {8 H3 w+ D" t' x8 k5 |( X6 e' h e3 u1 y3 \ 电容量, ; |, O& I) A% b/ j6 O电容器内所储存的电能的量度。 $ A9 J: }1 P* }" o( n/ S容器,8 {# ~' l) x9 W3 `3 T 两片金属中间用绝缘材料隔开的电器。用以储存电能。 & h( Y, h+ Q4 V( K截获(CAP),+ }/ L$ [3 A, N# A* O* Q) c# K! {- q( F 自动驾驶仪或飞行指引仪的获取选定方式的功能。3 M* y5 S* r. Z/ w2 ^2 r 线路板盒, , g6 c7 F$ @) o- R" B+ I, Y$ X w! P飞机上安装印刷线路板的容器。0 z" j- J8 N1 |* \" u7 ^+ Y) ~* ?6 S) P% g7 jOEING ! ]1 P. z! }8 |* gTECHNICAL DICTIONARY 26 9 f5 Y; `3 C6 T; C" M英汉对照民用航空词典B OEING5 c0 r' Z% ~ O0 f) ` o, p3 t TECHNICAL DICTIONARY 279 v0 `3 k x: E CASCADE, Two or more similar circuits or amplifying - R& m8 e7 F d( [0 Estages in which the output of one circuit provides the: c( k" L7 W% a' h put of the next. , s& W, P: J5 m+ BASCADE VANE, A vane for turning the engine airflow9 A N6 c/ n8 Q6 ^" ^1 d1 Q! ~ uring operation of thrust reverser. / F+ b- b/ m# X2 ^& P. Z2 UASE DRAIN, A drain carrying lubricating and cooling ' ~( c( p- Y# E9 Guid from a hydraulic pump.$ ?! |; g* h% i- I4 F: { ATHODE, The element from which the principal , V7 C$ E1 ~9 j# Q$ ~tream of electrons flows. , i- Z5 m0 ?$ lATHODE RAY TUBE, An evacuated glass tube with a" J" U. x: m! v' ]2 H9 [- } CEILING, The height above the ground or water of the ) ?4 c" I0 v1 T2 Tbase of the lowest layer of cloud below 6000 meters4 ~+ D: {' k0 ]3 ]) | m# W (20,000 feet) covering more than half the sky. 5 J" v6 t$ b/ b% {. o4 W( [( I9 P程。该; W5 |( p2 o! [+ g% c. O) S6 Z 程中,一个电路的输出为下一个电路的输人。; I, N2 N. {8 r 叶栅叶片,: ?# y# T' b% I0 `. L 在反推工作时,使发动机气流向相反方向流动的叶片。5 M" d4 l; Q$ l( c3 H 匣余油管,9 K( g2 I! Y$ W0 j Z6 b 液压泵多余的润滑液及冷却液的排放口。 / e: E1 w5 G7 L4 k4 N: D/ D- O极, ( R! O6 i! ?: L2 C$ d+ G电子流流出的极位。/ y; G1 i" Q# X, f7 R# p, C 极射线管, # F. x/ Q$ i$ h- z4 e/ Y) e* {有显象屏幕的真空玻璃管。用于显示信息。 ( S. k! X; n( B7 _) X' ]云高(云底高),* }, v: P. \3 r) v( b: V# \1 y 6000米(20,000英尺)以下已覆盖一半以上天空的最4 K J2 @4 W9 V7 R3 R/ ~! k$ z 低云层底距离地面或水面的高度。 - }: L% Z, n" E, U1 r: @! Sin9 h! C5 U4 |+ {. x C 9 P5 y5 U9 E* f- }9 ^d- d5 I, G6 h4 _6 _6 N4 O C 8 G1 P+ \- h' @# p/ L, lfl* W9 u' T; A1 S# V7 J; I( M( F C( L2 ]' ~2 F4 k J# I s/ B, w! h! v' ? C5 j9 O3 R! x7 y3 y7 k viewing screen, used for displaying information. 2 C, L; O, d8 \5 E级联,$ i7 Q1 V! Y: ]- y( f 两个或两个以上的类似电路的逐级连接或放大过 W* }8 `' i5 G0 F/ i, L& w. K2 p8 `; q/ Z. X1 M3 E8 {" e/ s/ a, a. q6 s+ C1 B4 y. k* e" x1 ` P% ~; N6 v1 Q X1 I' Q$ { 一个具 ! E: N1 [9 {4 I, l( [5 Q9 C英汉对照民用航空词典B OEING 0 L7 G3 P3 E4 ^- c; f( p9 wTECHNICAL DICTIONARY 28 ' i, V& D# @: A" R# Y% WCELSIUS, A temperature scale in which zero is the& L1 O( q% U" O freezing point of water and 100 is the boiling point of- W% O$ [$ X( C7 J7 t water.: }+ F( @$ `( \7 H9 { CENTER OF GRAVITY, The balance point of an object / Q0 o! y* K$ R: Wr rigid structure expressed in terms of percent Mean) y% {4 D) Z5 I3 r9 s. H4 C) Y3 T erodynamic Chord or in inches from a reference point., ^/ K W0 I% w. ]2 h3 @& _, p ENTERING CAM, A cam for moving a mechanism to a8 I; X M4 J7 M0 n: d6 |! [ eutral position. 0 U, W4 `: Q# X% n9 U1 I J# IIGURATION, A configuration of the 5 X3 C3 }& ~. m k; k: Pircraft approved for operation by the local governing 8 b+ W8 k" H/ S: u( ? Igency.; L5 p% p J! c9 W! C* ~6 H5 C ENTRAL PROCESSING UNIT, In a computer or 7 W* Q8 h! y6 u: @8 v, B: ]igital circuit, the section containing the arithmetic and , b# I( ~/ a X0 L% Mgic,control, and internal memory circuits. ; \$ a( N' V3 X" hENTRIFUGAL FLOW COMPRESSOR, A type of + q H6 n2 w% p/ v% _6 o. d7 hompressor in which air is taken into the center of the* |4 k I. [: Y) y7 c peller and is slung outward centrifugally into a diffuser & _7 g/ K" M: |0 chere it is slowed and pressure is increased. # B7 \3 f- S. d7 a* lCG, SEE - CENTER OF GRAVITY / Q9 }2 |5 l8 s- Z, \构的平衡点,以平均气动力弦的百分比或 5 o6 ~5 C+ H5 q某一参考点若干英寸来表示。 # y3 B( B7 n1 ?中凸轮,& c) w" B9 Z6 g 将机构移向中立位置的凸轮。 $ S6 e( G9 ~4 x* Q7 w. B格的装机状态, ; j" k4 s; ^2 j, ^& y5 E9 l5 l3 O由当地主管单位批准使用的飞机装机状态。* S2 C; E: q ]! F5 B. D 中央处理器,& s: a, Z) o5 F8 k, N! L 计算机或数字电路中含有运算,逻辑,控制和内部存 / e/ x) ?! V0 |7 H, a5 e9 E$ v储电路的部分。% f3 N0 w* S9 m 心式压气机,' j! B5 h+ ?3 W" M9 L e 压气机的一种。当进气到达叶轮中心时,被叶轮离心抛( o) w1 j( e3 R) f 进人扩散器。在扩散器中气体流速减慢,压力增加。 : q$ a/ t; b8 s+ f. R4 r4 l3 B重心, 8 f+ f O. n0 p* p% z7 r9 M见Center of Gravity : B: n+ s) F/ b* G: ?. Jo ; X0 P# h2 q4 R6 L2 U" {9 zA w/ h2 s5 v$ i9 `2 O- QC 8 V- B+ Q+ }" g4 a9 [; F# Bn; L6 `5 |; o: s) _+ | CERTIFIED CONF, ^9 G0 s8 y% `. f0 i6 g1 l a' s6 ~+ f" T$ E3 a: m a ! x% e$ L0 b0 HC2 j: q4 f* i; y' V6 G' Q d ! j: i8 G+ ^6 U7 l2 _$ G" R4 `lo / L4 a: X: H, }( U6 x) r- B) A+ @C7 m6 _0 F8 A& ?: g( u c * Q5 O- S3 V; }5 uim c) u; L8 e. j, P% |w, v7 g$ Q4 U" C 摄氏度(°C),# c% t8 w" D7 n 温度的度量单位。在此单位中,0°C表示水的冰点,- q F$ q: @+ s7 M$ H7 e7 k 100°C表示沸点。 ( l8 f5 C, y2 H5 n4 I- u重心 # o) P# f" v+ w) b物体或刚性结 & j: N, f$ B) ?9 Q9 ?* O. q% h( |% I, W& J4 X8 c/ z3 a7 s5 C: |" H; q6 j; K8 I+ G+ f( I! r5 }1 Q! Z$ t$ n' t& t! \5 \9 I5 `; |/ z( o, H6 H" {英汉对照民用航空词典B OEING( d6 T3 ?( j/ O+ N TECHNICAL DICTIONARY 29 $ n/ c8 u2 ^9 l5 I- [& `8 RCHANGEOVER, Conversion from one mode to another.% W6 V3 S& f ?8 f z2 X% L, q9 J HARGING VALVE, A valve for supplying air or fluid to. R2 H. Y' O7 [ HECK VALVE, A valve allowing flow in only one 2 | ~$ @* o9 N6 }irection. See Non-Return Valve. $ W" j: A& ~/ A# k8 {HECKSUM, In a computer, a summation of digits or# }/ X3 P3 @( A( I( F: ^8 P7 S3 d its which are primarily used for error detection." L! @: Y, x w: A$ ] HIP DETECTOR, A magnetic plug in sumps of) b9 _4 h0 W2 U6 ]! ] bricated components for detection of internal failure of * d/ \, w( s( o' x& y he component. 0 ~ }- Y# n2 A/ ]1 b2 n& i! Z- WHORD, A structural component of spars or frames./ S9 f. ]& Q2 \( Z' F; d 添活门, 9 u/ J' @+ _) N. D器充气或加液的活门。 D$ S& f8 e& a单向活门, 9 g. I1 U- P- T, O- t" U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; X' g2 Z2 G1 x" Y7 E a reservoir. # k. G8 }( j2 r+ b5 aC & b; ~ C4 \: o8 K0 [9 h% Z( r3 yd ' N! P3 }# \5 s5 IC $ v( T0 c# U1 p8 P( d& Tb, @' L: F$ a- ~ C ; `* u, o5 W* t4 ylu 0 e# c% q2 ~# o0 Ath B4 W; W( N2 g& q8 l C 3 D" A2 D0 G* g: y. F转换,5 X% {5 D) |# e6 U 由一个方式转换到另一个方式。1 o% ^. M, K; r6 T9 _3 f/ @( |$ h. r( d# l5 ]9 Z 用来向储存 ' }0 l3 Z+ [5 S K( r" \# G5 d4 C# Q# {9 I) l' R8 \/ w S6 M0 }% k总和校验,! W: T9 t$ N- w6 O, \4 J 计算机中,把那些用来探错误的数宇或位数的总和进 6 S# e" a: {7 J4 X6 V7 A5 ^求和计算。3 j7 J2 P' P6 t) Q 属碎屑探测器,+ C+ K$ N0 o, E1 A2 b 装在被润滑的部件滑油回油管路上的磁性塞子。用来探& w |# i8 [6 n3 y3 n- v 部件内部有无损坏。 , h) O0 v+ n8 c9 a U4 |4 |, g6 q弦,* _- v* J9 Y8 q: z _; a6 _& v 梁或框架的结构部件。 3 p1 L% b8 J6 e/ C" K% C v/ U V+ n- ^- u T- T/ p8 h; }9 _! g$ W" V0 d T6 O% q" \- y9 W) I% } v8 O+ F) Z6 |8 W; D: a* l5 Z. Z4 d Z英汉对照民用航空词典B OEING* O ^# ^2 r! a1 r TECHNICAL DICTIONARY 30% Z9 d* H- d- { CIRCUIT, A closed path through which current flows: T+ E8 B M3 X( W5 y) Q( r2 a' x ource. 4 e# b/ F. H2 F+ n' b* {0 hIRCUIT BREAKER, A device that automatically0 Q0 @% y7 B% R) g( F: q: H2 i* f& f eactivate the system. 2 D/ P, ?. O$ e( G `7 ^6 K0 ulear of all non-frangible objects which ( |- F k% I* Tay be used as takeoff distance available when & d+ E4 _3 z2 ~8 {$ K. I; D( |alculating a takeoff weight. , w8 a; c% c8 r9 ]& P0 mr water under the control of the appropriate . \8 [8 @8 Y% w" E6 N, Kuthority,selected or prepared as a suitable area over& E0 N z$ M. T5 E: C hich an aeroplane may make a portion of its initial, x5 t' m v( L limb to a specified height.5 k, u' X. z/ ~1 Z5 I3 _ increasing. + _" m" V5 T0 Bsed: c* y4 f' f+ U& c LOCK SIGNAL, A continuous string of pulses used for 6 p. m8 x$ p/ \# E+ O开关,7 J5 p. s. i6 L9 G& [0 u 故障情况下自动中断电流以保护线路不受过电损" {4 p5 w+ H+ r 体障碍物的区域。在计 : {: x* ?' X; c* s: x9 ?起飞重量时该区域可作为可用起飞距离。 ( Q: y) f6 \- l M# H$ e是在有关当局管辖的地面或水域内一个界限明确的长: m/ g4 x- h8 N5 [" E/ R6 O 形区域。在这个选定的合适区域内,飞机可完成初始爬/ G8 ^& z1 s$ k- C( C C 的一部分,上升到一个指定高度。5 y6 z! n! H+ T( y7 J6 U% B 飞机高度不断增加的飞行阶段。; o6 _4 l1 E- P4 F: g 钟脉冲, ) V0 i4 V: e! t/ H步的连续脉冲信号串。 * |6 H! J) P5 G$ n. l" k3 t# |4 K7 N$ Cfrom a source, through various components, and back0 U( I5 P7 y' y to the s& i! q% Z0 U* Y2 g1 c C 5 E. t7 S* U0 Z, w6 xinterrupts the flow of electricity (current) during fault: D5 K, p- n$ V/ S condition to protect wiring from excess current. Circuit0 Q& a1 R# U' H8 E breakers are also used as a means to manually. [4 S1 u4 A4 k2 g; r# l- P1 r D8 Z d : ~$ `5 L, W# C. XCLEARWAY 1, An area beyond the takeoff end of the ; V P+ A6 j0 _( j9 qrunway which is c 5 }4 m! z" d5 gm0 k7 o' M* N% v) I( X+ ~ c : `" a% E# u+ }) jCLEARWAY 2, A defined rectangular area on the # S# C! t9 v9 E( [/ c6 w9 w" lground o( I7 ^1 e2 S1 S% c- Q7 Y2 d8 c2 K a. |9 a3 k/ F B9 E4 ~0 j w ' |7 z; l- O; E) Lc! L0 n* P* y9 r; j CLIMB, Phase of flight where the altitude is/ ]) a; X; t6 [! |" s2 I) x CLIMB LIMIT WEIGHT, Maximum takeoff weight ba 7 R5 l+ g8 K; y, H+ [. M+ Won a minimum climb gradient with one engine + T0 x# m6 d6 s! H. b+ qinoperative. 3 l2 u R+ Y6 @: ^$ n3 GC( M* c9 u1 R' X' p* e# R: q+ H( } synchronization. \* U+ A5 K! p- \1 D电路,+ {; D- V) l( S1 _. A5 @% w! @ 一个闭合的回路。电流由源头流出,经过各个元件流回 , x. O+ K- O2 g% }+ ?* _1 F源头。 ! E' \/ ?- H6 M& t" U* \1 T7 j6 s) h# V$ S. _ 能在 - j) B7 g4 C9 W坏的装置。跳开关也可用于人工使系统无效。 9 A! L. G* J# o" E( ]! D6 j一号净空道, . t, `7 n5 B; d5 \! n是跑道起飞端以外,不含任何刚 & K2 s6 {' O- s" j# Y/ Q& e/ w( {% m6 ]2 z# h5 t 二号净空道,5 Q# A! S( L# S6 K# H1 n$ m3 q9 `% x) e, A3 x; F/ _6 I- w3 { D0 i9 P8 }爬升, 1 P7 Y' a9 L9 N l. O2 n; t爬升限重, Z$ N; t/ k) ^+ i: {取决于由一台发动机工作时的最低爬升梯度的最大起 $ @) @9 d, k8 ^; I$ K$ ]飞重量。 1 `+ H3 _( }8 D8 k7 w( Q3 l( e# H4 l! b* R( k2 x" G' |; K) P4 j+ [8 {5 S用于同: G/ z: r: A; k7 E" b+ v5 ~ y 英汉对照民用航空词典B OEING 5 Y5 Z9 c1 [9 s9 G, T: w% ~9 eTECHNICAL DICTIONARY 316 m* A) q% X9 G( e. d COALESCER, A device in the water separator for* D6 b) W- K) L6 ]# N i ollecting moisture from the cold air." z$ M4 T, t3 h2 u& s% N; w. Z n antenna with a receiver or transmitter. 5 [* X+ c& ?+ T5 y% Che cable has an inner conductor and an outer 4 F5 `% X3 l P q+ A8 p+ q/ Frounded shield.* U; |) F" W; Z1 }7 l/ i3 c" ] ting one inside the 2 d7 a* K/ W" R4 k+ H! xther for rotating the low and high pressure - c' W3 {! @( O$ j7 M7 P. Nompressors by the low and high pressure engine " X7 ?3 I2 y9 w0 D( Q$ Brbines. $ {( m$ p/ H2 P& I( \( aOMBUSTION CHAMBER, A part of an engine for ( F5 X G' O9 kurning fuel in the air supplied by the compressor.5 l0 m0 G3 M5 V0 G2 l' F, R3 y y& n6 k 置。 " G9 u9 _/ M! E. t: i射机的电缆。电缆 g" |2 q, U" J0 G4 |( J 中心导体和外层的屏蔽所组成。 2 y6 y8 k* R* Z两个套在一起旋转的轴。用于使发动机低压和高压涡轮+ J# F9 X! N( p) b0 R; L. ] 别带动低压和高压压气机。: [ \- ]* }0 W' y. O 烧室, 4 U, L0 D/ C9 }6 z$ u- g& P发动机的一部分。用来使燃油和压气机所提供的空气相 ' h6 o( ]; L5 ^合而燃烧。

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发表于 2008-12-24 21:38:35 |只看该作者
c; M2 X* u: B8 N' P, T COAXIAL CABLE, An electrical cable usually . _# z+ y- h4 n3 Hconnecting a % M* R1 W1 d( k& S% `T ; h. ?/ d- q: W* [& @. x$ V2 T5 q7 ag+ U( w* N! _8 A' H COAXIAL SHAFT, Two shafts rota5 @& w# }2 I- u3 [+ z1 A/ r o5 L& V1 ~( h% f; Q' l' M: C$ N c ^1 R0 y. g& Z' p4 Q* Ptu. @! G; R; X7 C5 @$ i9 [ C6 C9 B* O2 h: D0 J' i+ @ b4 K8 j5 o$ i9 t9 d* H! t 凝聚器,% u0 r! c3 |* [* G" ` 水分离器内收集冷空气中水份的装' M1 K0 \1 H0 E) i( f7 b 同轴电缆, . @' S# G( k3 F0 }, |$ @$ s! E一种通常用来联接天线与接收机或发 " G) O; p# \. B6 D4 v. r9 d$ c9 u' T3 z 同心轴, 9 @8 j( p) `) g' j' E- u+ S h8 J5 [ V9 h1 Z* x8 m& }- B I3 F& E2 P$ O1 K. z& x, s 英汉对照民用航空词典B OEING' }1 P; J; Z! p& k5 w TECHNICAL DICTIONARY 32 - q1 A/ H) V6 sCOMMAND BAR, A flight director pitch or roll comman6 S- n% U V2 g) h/ {0 K indication.5 y: a: n% p: Y7 H d / K$ N# @! P& F8 P" `$ M" V* qOMPANY ROUTE, A route flown by the airplane % y* |3 J; A$ T1 t5 c9 }OMPASS LOCATOR, A low power, low or medium/ y' y% I: R8 a5 @. z; K* Z) i equency (L/MF) radio beacon usually installed in ( h) c3 I) O' w% X% Y m8 r; S5 Oonjunction with the outer or middle marker of an 5 o% b6 G! m5 f# K* e9 v# Ktor (LOM), A compass , E* h, Q) Q4 Z k# ]' F9 ]locator installed in conjunction with the outer/ \ q) O* e7 L# R9 s. ?5 | marker of an instrument landing system. 0 p1 ]; u3 e; y" _# k+ |* ]ss$ y: S8 T- k V8 p6 f le ; ?" z" a( ?) g. E% p6 LOMPENSATION, To offset, balance, or counteract./ B4 t5 f% U$ q9 q5 X" x# o( K, J OMPENSATOR, A dual capacitor for changing the fuel ; Y" C9 D; V& C/ G! uaging circuit capacitance due to changes in fuel + A5 U0 \3 Z4 Q9 [ensity.: p1 U2 d; d7 M6 Z9 Z* @ OMPOSITE MATERIALS, Non-metallic materials used * p* i/ z( p1 n. c9 r& q Vr airplane construction. Fiberglass, Nomex, Kevlar,( E7 C: g* L" _9 V3 V( b' u raphite Epoxy are composite materials.+ ^* F1 Q8 K- J4 `# Y2 Z 司航路, / j: L) | C3 o0 C/ B在飞行管理计算机数据库内由航空公司飞行! r: ?6 S7 S& @* q/ ] 盘定位台, - N: h1 J( k$ W/ \2 z1 }与仪表着陆进近系统的远距或中距指点标配套安装的9 {3 r8 y& c7 ^ E8 L9 v( |, h 功率、低频、或中频无线电信标装置(低功率NDB台)。 3 Z- `) g& ?3 \2 ~1 a程序中用来导航。* ]5 Q' [9 x* f( ^: S 1.远台,0 U; O) b z' x: {$ f5 ~1 E 与仪表着陆进近系统的远指点标配套安装的罗 / z. |9 x4 D# Z) ~* W0 Y盘信标台(NDB)。7 X3 d2 M u2 j' }& j, V% Q( \ 偿, 0 }% f% F( l* i抵消、平衡、或中和。/ e3 A* T6 p: G! m$ @) J 偿器,1 u9 J- k6 G2 F4 S4 T( s5 I) ? 在燃油计量电路中,用来改变电路上的电容,以与燃7 r3 q* W0 X4 N; h# Y 密度改变所引起的电容改变相抗衡的双电容器。 + P# |6 |9 E+ Y) Y合材料,- M. P6 O& [& X4 I 用于飞机制造的非金属材料。如纤维玻璃,Nomex, % U, k9 ]& ~2 yevlar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% P' g* ?$ I5 m: X2 W operator that is normally stored in the flight) P* g, S& ^) Y) S7 O* n3 l management computer's data base. 3 t' @1 e% |9 a/ Y1 GC- |, }" X4 a+ ~# P# \# d fr 6 `8 f- X6 ?4 @c 0 s$ _8 D# b0 X" minstrument landing system (ILS). It can be used for7 X/ t" U% O- n3 M2 O navigation as authorized in the approach procedure.' i% a+ t) b) C9 y' E6 P 1. Outer Compass Loca/ k L+ b/ u9 ~( a2 { w2 l 2. Middle Compass Locator (LMM), A compa# i4 ]+ b- V+ P4 H2 _ G locator installed in conjunction with the midd & C3 T5 R2 ~; f2 @' Cmarker of an instrument landing system. & e' r: w. S3 S7 s: h8 U" J6 cC $ h. G- D1 k: B$ q9 EC2 m6 s% ~' s% M4 c g: R2 d# Q; o# u# a0 L) |- g d# W3 k6 i, A2 z$ ? C% i1 J/ S4 l4 {" }* b" h5 ?; { C fo ! s/ a9 I0 C: B, \3 |1 A9 I; Tg 6 Q( O& S' F$ G' _指令杆, 0 E6 u5 _" ^( d6 K1 n2 ~1 [飞行指引仪俯仰或坡度的指令显示。& e- @; g( E/ P" R5 U* r7 V& n4 }) R5 p3 g4 j8 o 通常储存2 O3 ]+ K( C& S. |: J0 P k 的航路。 & s! x/ x1 {2 h4 o! Q2 j, g+ v. P8 @: ?0 Z4 h8 c7 I9 R8 e7 } 经认可后在进近6 P8 w: i& h9 |' a2 E% K 2.中台, 9 ?5 Z0 w+ Z# M" {2 |与仪表着陆进近系统的中指点标配套安装的罗, g( E/ ?& z% N# u 盘定位台(NDB)。 1 O3 a& r/ K! i4 I2 }9 a* v+ p" a# m% l9 }) @2 A9 Q/ i2 D! q. k/ G- H( i8 g3 P4 h$ i% ?+ K( @1 m$ E( S) I/ {2 Z/ r! D% S4 Q* G4 G, d, u3 UK3 E4 _5 \; f5 i8 j7 u6 v6 W5 K 英汉对照民用航空词典B OEING( R8 G) \, c9 O0 Z5 x! [* V# ]- c TECHNICAL DICTIONARY 330 T T* l! f2 j: a* q" L" n6 E) t) G by8 b* S9 a* C! ~: V8 d, }- Y( E, f or increasing air 5 T! Q: g1 |( D+ bressure and temperature before the air enters the & P I& \: f8 J* P* hombustion chamber, Low pressure compressor - front: D/ J( g3 Q4 X" _! x) N ection of compressor, High pressure compressor- rear% @8 q+ M' i4 A h1 I OMPRESSOR STALL, An event that occurs when ) y0 e8 u: X! aere is a complete stoppage of air or reversal of air flow! \$ s$ V9 `- |% s3 }* {7 v COMPRESSOR SURGE, SEE - COMPRESSOR+ t' C6 C( v2 H* _- T M, z8 N( x& \ STALL COMPUTED AIRSPEED, Indicated airspeed) }; ?" c% l; } corrected for the static source error.# O& j6 U( K8 H% k( F8 t, i" a 的机械轴来驱 # B2 W8 c3 K; U,用来增加吸进空气之压力和温度,以供燃烧室使用。 . o! Y# U1 D3 I- k& M压压气机—压气机的前段,高压压气机—压气机的后+ T: O2 O1 @* d7 n( Z6 K. ?8 \- j( n A& | 气机失速, " m! G7 \2 t! G4 _; l# X$ t当气流完全停止或通过压气机时气流方向逆反的一种$ [" i9 _) t7 @; N. m/ f6 q 压气机喘振,0 X: ?* @1 v" M: {. p w9 T9 _ 见Compressor Stall$ j' a/ m3 J) X COMPRESSOR, A rotating part of an engine driven 3 z: k- J0 C) K" s3 ~. q: ia mechanical shaft from the turbines f" M' o# H+ E4 B. s! i p% t3 {" d: N% X% h c" B) I4 g- z' Z8 N0 H7 m s ! j! l7 L) U- C* r' p9 m% tsection of compressor. c* M# J9 e9 ?6 k* I% `1 Z/ }! wC . |/ u" j- m. B5 {2 q( Vth0 k8 O4 S5 |- r' J! K; Z3 M- T through the compressor. ?+ p' ~( D5 C压气机, - N; J5 }% J/ s发动机内的一个旋转部件。由与涡轮相连. H* e5 Y8 G" t( p1 X: }2 R2 b2 s7 A0 Q- P5 @) X; a/ v- S! B3 |4 o1 B4 y4 h5 q* [) G1 m- H7 l现象。& S( A, r/ Z' t" `. r! e" }; L# e# P 计算空速,! w8 g' x$ M' T& A0 Z/ M& N0 `- B: i* [ 修正了静态源误差后的指示空速。: U6 }. z9 i# A 英汉对照民用航空词典B OEING6 I7 b! i% q9 f" P 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 arithmetic2 D3 c9 A. V. E& { operations, manipulates data, and makes decisions.- q5 N4 R W: h9 v9 D$ ^$ n* j ditioning0 b* M3 @) g% l& E; Y% B9 t the air and the1 O& Y& l z) J& l! \3 W frigerant or moisture vapor is changed into a liquid.6 e Z7 |8 z" H( M2 U1 O: r ine & O, z9 }* ^3 T U- yONFIGURATION, The position of flight controls, 8 B# q8 A2 O4 ~+ qmissing which ; M, N4 E9 J% l8 O3 F" \may affect the aerodynamic performance of the 8 `5 V: p6 I6 f% ]" _7 |airplane. % u9 q) q3 A6 n' T& A置。 - \* u" P& y) `6 I c5 q3 K9 O中能使热能散发到空气中,以及使冷冻剂或湿 ' ]& @: |) w5 g6 \* U转变为液体的部件。! x( j6 a: U; v/ u" f5 C g 连接到飞机结构上。 2 }- A" ?( @: ?1 Y! M+ D% _态, ' m7 i/ T# V* q" ~7 O2 S" N' W/ r定飞行阶段中,飞行操纵面,起落架等的位置。 ; R% u& d h. I3 O), 6 f- Q% ]6 X# M( B受到影响。 ) I# C$ i- h+ j uCONDENSER, The component in an air con - {5 u, s1 ~$ N- v6 E3 R- Dsystem where heat energy is given to * M/ z! ]- B5 o/ Bre' i# N) R4 n8 I m CONE BOLT, A bolt in the shape of a cone for eng . g+ o0 C7 K: _; q' Vattachment to the airplane structure. 9 w8 C; J# W d# A) @C ' \+ H& X% v0 Q& q# \2 X( t1 Blanding gear, etc., for a particular phase of flight, e.g., : k- d1 |- A& Y' ~2 [Takeoff Configuration, Landing Configuration, etc.+ e! q' \) X, U; Q) F; {/ P" X8 y CONFIGURATION DEVIATION LIST (CDL), Appendix - Y/ ]$ a# q0 f* w& Ein the Airplane Flight Manual (AFM) allowing operation$ j) [( K; r6 ~! P+ X of the airplane with certain airframe parts8 s: Y7 w# [$ _1 d8 a 计算机, 0 K( r2 Y& d$ G1 m; M( H+ K/ N& A能作算数运算,数据操纵,和决策的装 3 X6 M* v2 ~ L: k冷凝器, 9 ~- l+ L. M8 T' Y) r空调系统$ {# w& ~; Z& V+ n# T# O0 j; f. h0 L9 ?* [- U: _" a- |" a锥形螺栓, " z, z4 l) C8 v |* @( p# w' D, P外形是锥形的螺栓,用以将发动机, j) W& \, {, n( n7 O. C1 {- P+ d. K/ X) Q2 }8 l 在某一特0 B4 O0 A7 W# q+ }4 c 如起飞形态,着陆形态等。 # h. H% x' J2 F# P& D5 Q9 x缺件单(CDL. I; Y& z0 K; ?7 A 飞机飞行手册的附录所开列的飞机上某些零件的清单。5 M3 O# K: V1 B' b 在缺少这类零件时,可以飞行但气动性能可能4 ~# I7 r* b; V- ?( r 英汉对照民用航空词典B OEING " y0 y" v0 ?( l5 B$ z8 j VTECHNICAL DICTIONARY 35

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9#
发表于 2008-12-24 21:39:49 |只看该作者
CONSTANT SPEED DRIVE, A hydro-mechanical* j' v- ^3 z% {9 t component for changing variable engine gearbox speed- k' M8 v. q) z t6 X ONTROL AXES, The three axes of the airplane which/ u6 M8 T* f3 |1 l: S0 o; | re perpendicular to each other and pass through the 8 ~+ e2 y& J5 renter of gravity of the airplane.2 p e/ R9 n5 `5 o# P Pitch axis - Horizontal or lateral axis, passes through- h* u9 ?5 ~: M& R' x. f the airplane from one side to the other - + V4 w# \: j+ n5 Pnose up and nose down control is by & l: S3 q4 Z0 k+ o, y+ Selevators (and stabilizer for trim). % k. l7 D9 b! ~; f6 \. JRoll axis - Longitudinal axis, passes through the! ] i) g' Z4 @8 T/ I8 o; ~/ e airplane from front to rear - wing up and * M2 B! a6 H/ [2 s, Z/ twing down control is by ailerons and 4 q. G/ I: d4 n4 v" oflight spoilers. $ G' T. h) J; I1 [* J$ tYaw axis - Vertical axis, passes through the9 I% c e" M3 a4 f: Q! m+ K airplane from top to bottom - left and ) P) T: t- Q- w0 Xright control is by rudder.0 t' n# a* S H, t; y. p 置," B4 x ^+ A! O: B, x 制轴,: x1 H7 g) ~7 W' u" |. ~" v 通过飞机重心互相垂直的三个轴。: ]& N' q$ B% U" X' Z 俯仰轴—又称水平轴或横轴。由飞机的一侧通向另4 E2 H. ]4 t( a. i' f2 H; r4 s 侧。飞机绕此轴转动即造成机首的俯与仰5 L* g C8 s, b* @ 俯仰控制是由升降舵来达成的,水平安定 , x& t: h. S7 J& J3 c( c5 N则为配平之用。 7 r( J: u' ^! q" ?" B. S* Z横滚轴—又称纵轴。由飞机的前部通向后部。机翼, o6 x3 X2 m. Q+ `; v 下运动由副翼和飞行扰流板控制。, H4 G8 g' E( N$ P' d+ {" ] 偏航轴—又称垂直轴。由机身上方通向下方。飞机( c+ X5 j, p5 \+ T* [ 此轴转动即造成机首之左右运动,此一运 D& M: }9 B' h0 C+ M6 A 由方向舵控制。) C& x2 M% I/ M6 e* b) Z7 _ to constant speed to drive the electrical power. 9 O3 Q6 U8 w7 Y, l$ B* wC ; Q& |6 a# D+ u1 d$ ~& D' `a- {. A7 V7 l+ f4 @# W& u6 x c ! e7 }% L+ g' c3 m a+ }9 S恒速驱动装 % ?5 m, {/ n2 E1 }, T9 I. o将发动机齿轮箱的可变转速转变为恒速以驱动电源的3 x% v: k/ A3 I* _ 液压机械式部件。8 V3 s1 m9 n6 B+ V$ u& o2 c3 V8 ?' J3 z, L! l6 T2 W+ r+ m+ w R4 p7 Z! D% a& }9 Y. ?) o: \, W( p1 J9 i4 l4 a% n H2 K# f6 q7 P" g0 E" X. {) k+ L4 b0 r ^) C; o+ r; Y& ^英汉对照民用航空词典B OEING ) V7 D' }' R( B% }- T/ Y$ yTECHNICAL DICTIONARY 36 * D- t/ A0 N) h4 L$ i% d) ~CONTROL COLUMN, A mechanical component used ! f& ~9 g' _6 k2 ^* T* M4 d5 f$ Q# ors% D) z% T0 `$ i$ x$ n6 K9 p9 F9 \ nd elevators.4 {" _- |9 k5 @ q ONTROL SURFACE, Moveable panels on wings and # A. l4 h1 c6 Q! E. Eil for movement of airplane on pitch, roll and yaw axes. - q* \: D& T+ _) L6 OONTROL TAB, SEE - BALANCE TAB 2 j9 u7 [# C8 t( d& YONTROL AREA, A controlled airspace extending & n; G Y* n1 r3 x+ bpwards from a specified limit above the earth. ; H# j! h) @# N, b9 XONTROL ZONE, A controlled airspace extending: m6 [: n4 N" a k- |/ O pwards from the surface of the earth to a specified 8 O+ z7 Z5 I, o# V2 N) upper limit. 6 ~2 K& q' O1 Y! pis 0 `8 T8 G# s6 `4 _) }o IFR flights and to VFR flights in accordance6 |& s# a$ S7 N- p with the airspace classification. g# `8 _& g# o% a, b; }机械部! _& ]2 x1 k0 a. M" T( O1 {% }, _ 操纵面, # ?# V, Y$ K% v7 m机翼和机尾上的可动面板,用以操纵飞机俯仰,坡度, . T+ h) j H0 S2 w7 n0 r% J& B6 z和偏航运动。- c: ]9 Y& @; ^ 操纵片,4 x& S! A6 f+ k8 u. u" w, @7 { 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. V8 f/ V/ Z. A3 p6 R a I E' ~5 D, i6 e/ NC # h4 p1 O( Z! t) Qta# D! w9 P- [6 j T C) u, g$ B; h; l$ v3 H6 D C * ^8 m* ~: M+ T2 Fu2 G' d1 X3 K, [' x6 q9 s/ j C 9 Z) R$ B+ J+ n1 Su2 h: `6 ]5 P6 {) g2 z# ^5 Q5 b: t7 e u / p3 Y/ B) v& g8 i1 lCONTROLLED AIRSPACE, An airspace of defined# v8 M( A9 R" ~0 J- p/ O s dimensions within which air traffic control service % V0 F; x* J5 E3 m/ z7 ]provided t/ R# e1 ]2 [' a# R 驾驶杆,/ E; i& I" H- i5 t 飞行员用来操纵副翼、飞行扰流板和升降舵的 E1 |9 u; p& c4 Y7 e4 U Q% o' L6 Q. `4 U3 A4 i5 o, B) I+ I. C0 N管制区域,- A( i' B' R+ t* w 高于地面的指定极限以上的受管制的空域。8 H3 _$ u& {2 r# z7 q& K P7 N 制范围,+ K; c" ]# u$ D 由地面到指定的高度以内的受管制的空域。( p3 ?( ~1 l, B' j0 _ 一个范围明确的空域。在该空域内,仪表飞行规则飞行1 Q2 r, y& C6 [3 C7 N9 S7 z# y 和目视飞行规则飞行有空中交通管制服务。1 s! O8 ?" |- ~) O" G7 i E' |( }- S7 G. b% h9 U 受管制空域, # k6 ~, V/ j7 y. T) t& ^: x3 y英汉对照民用航空词典B OEING6 B% _: p+ f( v. z# ^* A- h TECHNICAL DICTIONARY 37 - | w5 C4 p$ |CONVERSION, To change into another form. W- T' Z% I. q# [; T3 T: f' hCOORDINATES, The intersection of lines of reference, ' _* e6 H/ [; B" xsually expressed in degrees/minutes/tenths of minutes9 G' ^+ K. j3 }0 Y+ {% @# R f latitude and longitude, used to determine position or % B0 J1 n3 l3 gCO4 w9 U- Q8 V' R. c( w3 A3 \ destruction of th 6 f. Z s. m# M+ _& r3 Bchemical conta ' N; J; S- P; r3 m+ K7 z( ?COWL, A remo, t G# z$ H) | for access to th* j" g, F! J5 \0 H1 @! ? Fa ; p+ h# @. S& ]& b# n! F! d: tNose Cowl - Front section of the nacelle for air inlet % d% ]" r. k- @" }- \to the engine.; i( ?: Y0 ]$ f: L2 z Side Cowl - Cover around the sides of the engine.' ]& O, |5 w* [! e* B5 @; [ r Thrust Reverser Cowl - Cover around the core/ e7 D2 ?. Z+ |' ^ section. 9 m7 B- O6 ]/ R+ [1 G+ ITranslating Cowl -The moveable outer portion of the " d5 G" V% U( @thrust reverser cowl which is# P ]# n2 u# Q' Y* l& ~ operated during reverse thrust. % I; X8 s- l+ P3 R2 j5 S' C9 j) e标,' ^3 D0 w( q1 u' M 基准线的相交点。一般以经纬度的度/分/十分之一分( j. J5 R; q5 y4 F 读数来确定位置和方位。 7 Y6 g* Z) B' j5 i8 B& J, j腐蚀, V! s' `) {2 {# z 动机外部可拆除的罩子。发动机上的构件必须要取下+ X* B; G0 V. L" f5 ] 流罩后,才能够到。 ) h7 ~6 C E5 ~" `; N% Y# L* U1 W! S# X6 p' H8 | x 机的短舱的前段。5 o z- _ X3 S 侧整流罩一发动机两侧的罩子。 9 p$ ?, N: a7 o; w; V1 Z反推整流罩一发动机主体外的罩子。( e& k; e; E4 g/ N) S, v 移动整流罩一反推整流罩外可移动的部份,在反推工 , L a+ i% ?, H作时使用。$ S0 U4 z; A" \ u - U: i5 N2 \+ X( S0 T# v8 v5 ^8 l; @o, J4 y: ~- T' z* \3 V# T. N location.4 |0 f* A/ w4 i0 z( N RROSION, A chemical action which causes gradual, D8 T. F% ]) v1 q: } e surface of a metal by oxidation or! i* O1 o( E% C mination. r# ~' x1 w# Q7 f' cvable cover around the engine sections( t; r! F8 x2 ?6 w e components on the engine. 5 V! \6 A* O" b M* X$ {! y3 In Cowl - Cover around the fan section. : A3 U+ ?7 t6 d& _转换, ) l" u5 }& f) {2 F* h) z改换到另一个方式。 * M2 u0 T. V9 z# _, C* o8 V5 |5 _. d& Z8 t/ x8 }4 ~* q2 ^. i/ I# C: |9 x7 e2 q& C3 m/ u0 u4 J$ i 氧化或化学污染造成金属表面逐渐破坏的化学反应。7 q/ m8 S: K/ Y/ U5 ]$ G 发动机整流罩, ; }! U* n0 M: e S* M) ]6 m1 T# }, b8 \+ z7 r8 L1 w/ C# U. H2 q% W; l4 M" s 扇整流罩一风扇外围的罩子。 : L8 c: ~" T3 i# h2 p前整流罩一引导空气进人发动7 H, O$ b, s; X, x2 V# O 英汉对照民用航空词典B OEING 3 l: n5 c1 U$ v8 a9 F( }TECHNICAL DICTIONARY 38 9 }! O$ o) G# Z6 J! [CPU, SEE - CENTRAL PROCESSING UNIT : T; F8 _6 x8 t9 F4 r# cCROSS TRACK, At 90 degrees from the desired track 1 N% s& K) [. d7 f- q. ^) cf the airplane. For example, cross track distance is the* k5 S" m8 R! r3 k( [$ ?* T9 J, H istance from the desired track measured 90 degrees0 ] h* ?# D+ L5 e( s- y, U A2 E om the desired track. * p- S9 L# ^. B% m! |( D- Z' kROSS-CHANNEL, Electrical wire(s) connected from$ ^ E2 F7 ? s2 y2 C4 D; a( P ne system to another like system, for example, FCC2 Q4 ^ t+ y: {0 z0 T8 a " to FCC "B".. _/ H6 `! ]# l n adjacent engine or one on the other side. 1 T2 ^, U0 r w2 C4 g: k4 Il crossfeed # T S4 x7 Z# A% M$ D; s" Hanifold for fuel flow from one side of the airplane to the / w" z* m: o; K2 n; g) a+ sther side.- x; f8 j6 |8 k: o% J re* M7 L6 o1 ~0 X RUISE ALTITUDE, An altitude or flight level! ~6 T4 O% t; k) x6 N2 Z: |: n* J g. x3 ?* l, u) ~( W% c7 z ? o - V [( A/ `& P( L$ s7 Z' U& ]d % n& e$ D- T+ a% H3 Mfr 1 U' f9 e/ C3 n1 \/ KC X) P) s4 A X8 co6 c% k7 @& V2 |& e2 J7 r) Y "A5 V' w/ u b7 v9 z3 }1 | CROSSFEED, An interconnection between fuel 9 o9 a4 N6 X. D( J! cmanifolds for fuel flow from one side of the airplane to- s1 t5 @6 t$ G; M! P# C4 q/ v; e* G a: D% `9 O+ e; I0 z: f2 ^ ^ CROSSFEED VALVE, A valve in the fue: X _9 m I# U) w m3 u+ w/ C0 e/ K. I& J o p9 W- S5 s8 v( ~8 k% BCRT, SEE - CATHODE RAY TUBE- S6 |9 ~0 R z! T9 F$ V; J CRUISE, Phase of flight where altitude and speed a8 F; r" M1 e3 Q w0 v basically constant.' F7 [* Y, K$ V. @% n# `6 s9 x C7 c s) {1 d, H maintained during enroute level flight. $ F: ` L/ W6 U1 a中央处理器. N: j/ a1 s9 i+ D$ Y 见Central Processing Unit. ; U3 M' S2 K ^; j" g交叉航迹(XTK)," `4 m& S0 ]( K8 V/ H 与飞机预计航迹成90°角的航迹。例如,交叉航迹距离 : O- v$ S. ^3 Y( c是用与预计航迹成90°角量取的到预计航迹的距离。 ' c% p) I3 u! ~5 l0 A通道跨接,; r6 u$ y* P% V4 o- `. F/ A. @: H 电线由一个系统接到另一个类似系统。例如:由FCC9 A. F) ?7 V$ t5 U# m/ I" ~ “A” 7 W: c! v1 p% J4 W接到FCC“B”. - x: |# i- R6 G, ~$ r6 O7 R7 r机身另一侧的发动机。 7 e% t- @2 U, k# m. K0 ^于使燃油从飞机的一侧 @. ^/ d2 c3 t 向另一侧。 " ~4 Z7 Y {3 Q3 N! o$ p见Cathode Ray Tube+ e9 S* ~) J; i/ G 交输, / Z$ P, H+ s" x6 K' v燃油支管之间的交连设备。可使燃油从飞机一侧流向邻/ p( B- {% N+ M3 V) { 近的发动机或在 4 U, v1 q$ Y7 l2 X, K交输活门,- X( n( H0 C0 L: u& l 燃油交输支管内的一个活门。用( m& F f/ _' e3 ~$ }% {- l+ m# Z, U5 |; @ 阴极射线管,0 Y2 p4 y0 a+ R2 W9 U .! F( u/ ?' w2 a M4 b/ K) l 阶段。 : Y9 j+ o% D& S& A航高度,! G+ }( ~+ j( ?/ M6 ^# Y# n+ n7 L 飞行期间,飞机所保持的高度或飞行高* x) M p( m& @! H! o7 P 巡航, ! B. h* F) C7 T( h9 N, N; D) A飞机的高度和速度基本上没有什么变化的飞行) M% @# \& o/ H. U; q B: i1 t M8 D9 l3 A4 T! W1 N& ~2 n. f在航线上水平$ G" P) j9 ^! N9 W 度层。 J! p- x) W3 O2 m! t: p英汉对照民用航空词典B OEING. k/ l4 K# v9 r+ c TECHNICAL DICTIONARY 39 + y; ?0 _/ P+ y. d" [% R# y! r7 eCSD, SEE - CONSTANT SPEED DRIVE2 V- S4 ?5 j& n; g CURE, A chemical change which takes place in a resin # u( @, Z G& i6 w: tand fiber based component causing it to solidify.( M/ e! ^% G5 y CYCLE, A complete series of events that take place ; y4 V" W; j3 W( u) fgularly normally in a continual sequence.5 G3 {: L2 O# D' M3 P+ ? AMPER, A device for slowing down or limiting # m2 M# b- S, q2 `DASHPOT A mechanical damper for slowing down 0 j+ E8 R i K! S1 a9 Eovement by restricting fluid flow.; G* z& r* }9 T4 `" p0 i. K3 H/ i6 c D - m! F* w0 e1 l8 U7 I: N2 V9 g* V& N7 XATA BASE, Stored information which is used as the ' T% i! { {+ B8 X0 k" qba8 U: {2 z' v Q+ X: T9 v: q, ^1 Y DATA BUS, A conductor over which digital data is . 8 u5 o* P+ W5 J j6 Mtransmitted. " O/ C0 m8 V) b* o BDECELERATION, To decrease in velocity. 7 M2 {8 i8 e! X装置,7 B3 X) z' k3 v f5 O* A rive& _- r- T( q% y$ S4 w3 H re . P3 d" @0 z U, Y1 h4 ~) GD 7 l3 B8 l* s) pD8 b1 D; a' P4 Q movement.+ S4 J2 I7 o0 r; ~& M2 r. {) ] m- t' B* A3 a; D/ @# y9 }! a ATA, Another name for information. ' ^3 U% u% F. C0 `D# p7 @- e! k5 s# Q4 z sis for computation. 4 F' i1 U1 \+ b5 }恒速驱动 % C1 w* g# ~, F/ Z6 p, y9 x见Constant Speed D .( _) g8 A8 {/ n) @/ b" z 期, 1 v ?; ]# M! B: t/ l) a% H不断重复发生的事件的一个完整系列。 4 N7 l7 g6 K" z% ^尼器,+ f0 y2 ~8 e: s/ h4 B- u0 j 慢的一种机构。 " b- G# ~- Z$ A9 D F! t9 a+ F; {; H0 t 用限制液体流动的方法以减慢物体运动的机械式阻 % u$ K r3 \ x" ^+ j( H- S; \5 [% \/ R3 p0 G; q6 n, `- K4 L% m$ T- X( k- b6 q( o料的另一名称。 R( Z9 {2 D" n% C9 \1 L据库, 3 Y7 x9 y" ]6 {: q. u+ Y数据总线,2 A6 U! l7 I3 L ?, p 一条或一对导线,用来传输数字信息的通道。 4 T+ K$ }$ [" B0 M( I8 ^ z/ J减速, ' Q7 F/ ]- y! \2 P1 A3 a" c速度随时间的递减量。) b! ~, ^1 k$ h/ O( A- w 固化,1 `! D) ]# U: \9 Q 树脂和纤维部件内化学反应使之成为固体的变化过程。( d e; w' w7 D# f/ m Z8 U5 V0 i0 b. h1 E. w6 C0 j t* _$ ^9 a3 H 用来使运动减 9 C+ b- E( H, Z冲器,- N4 k2 V% |& Z6 i S( Q8 T0 O 器。 ) c; K' g$ K* ]9 Z( j5 d据, . o) T# X3 y: E: N: i( H$ g, W+ |5 [& ?( v8 _$ ?, J$ ~1 Q1 A$ @& G3 W% q储存起来以便在计算时使用的资料。7 ^; g2 y* ]! d" b 英汉对照民用航空词典B OEING0 ?2 J9 z" N. h: B) M TECHNICAL DICTIONARY 406 P. X3 c! Q, n# B6 C7 ^" `' U0 o DECIBEL (db), A unit of gain derived by computing the : t0 \$ w3 a7 ^tio of input power to output power.$ t+ b' H+ _2 U4 `$ j; p$ O ECISION ALTITUDE/HEIGHT (DA/H), A specified. G& r; y! a4 g8 b* n ltitude or height (A/H) in the precision approach at: a s2 j: h0 z# I: X/ Y5 b hich a missed approach must be initiated if the8 ]. b2 n; Z, u1 w& r ECISION HEIGHT (DH) 1, With respect to the 6 X. ~3 L+ N; a3 rproach or& t9 r: \* v9 ]2 c# Q execute a missed approach. 4 S( d2 C( F) H6 \" Q* u# xproach to trigger the decision of either% L* F' V& t* K# K7 T, k nding or go-around. 5 R/ L# F7 V D# m3 DECOMPRESSION, The loss of internal aircraft air% I* N3 a" ]9 O2 m- m! E$ T ressure. & s% {& w% {" H& n7 e) _E-ENERGIZE, To turn off or cause to not operate.4 | }7 B0 O5 l* }: k4 b9 C rom the tanks# H7 l* @6 U& i& d2 U using airplane fuel pumps or external suction.1 Q1 e% u* ]& O- B" g6 E4 j 算的一个增量单位。分贝: A/ E" x% g/ C& I3 {1 a+ n5 k2 v 常表示两个声音信号或电力信号在功率或强度方面的 1 y" S$ {: m/ Z a+ n对差别的单位,相当于两个水平的比率的常用对数的十* I7 }7 t7 {9 }3 F 断高度/高(DA/H), 4 d0 o) C: b, A0 M; x% M在继续进近必需的目视参考没有建立的情况下开始复3 a3 P8 C$ F" T8 P4 F. W 的精密进近中的一个指定高度或高(A/H)。 7 C) _: q+ _- j: }断高(DH)1,4 `+ h) {- f6 q+ D+ o- q$ a 操纵而论,指在使用仪表着陆系统或精密着陆雷9 g6 C( k, }$ J* c3 p; d 生继续着陆还是复飞决定的高。 $ s9 x! @- f: e3 \3 q8 Y飞机失去内部空气压力。 - u& G' S$ H6 O: n开, % Z( q7 Y% S% ~4 C, o+ e关断或使不工作。 2 R& c- |+ }* o! N+ y3 |9 K机的油泵或外部的吸油装置将燃油从燃油箱排 & U% X d* d: s出的方法。! n( V- ?: K6 |$ @* Z( M+ S ra 2 ~" U0 W% D2 J% I; ?8 LD6 y2 b, i0 `) q. d ]' S a/ y" Y- j# W" _/ `1 u; t w# _' T$ p# m0 n }1 A) o' j required visual reference to continue the approach has " }# s9 v% n5 H1 T& @, ~! ~not been established.$ ~2 _* j+ E: o* {8 X7 H/ K( u9 S D ! Z" C( E% o" \' W3 Y* Ioperation of aircraft, means the height at which a( }* m$ G5 ^; B4 |" U/ V" v$ H decision must be made, during an ILS or PAR % v+ ~: e; m& binstrument approach, to either continue the ap + a4 M k/ D* v3 k' Nto $ [7 |% B1 E0 T) Z3 N! j& X2 lDECISION HEIGHT (DH) 2, An altitude used during a * X# g6 r9 [5 b( W+ x% \( nprecision ap% p I5 @7 O0 ?% z/ z) O6 a la9 v5 X7 |1 A; {. z" z: ^* X/ q# o D0 ` I3 j3 _* R u8 ?1 Z p' ^" ?$ `' a% w3 e6 d D 1 B) y; B+ s5 `% Y! ~+ aDEFUEL, A method for removing fuel f 7 J" K5 D/ p4 }8 @0 {, E$ `+ G分贝, ( O5 u P% f+ a a* S' r" {以输人与输出功率的比率来推9 U/ k0 t( ]3 Q2 l+ w# P+ U8 D3 R5 m- l2 H: p: u; Q5 B, L6 C7 J' M/ [3 t; A9 U( x/ i3 v# W W0 {5 ?0 M X' N4 E) s3 c: ?: c1 `3 |; N. O+ e5 `+ s* M0 `( m: S" m) f, Y就飞机" @! i. R& j* x: m, x% I9 m 达引导进近时,必须要作出的是继续进近,还是中断进场% `& a# H# X R 复飞决定时的高。6 D; g5 k2 X5 m# d4 |; [' l/ X m 决断高(DH)2, \8 w$ d7 X4 |+ A( V2 r! M9 S& ~3 e: L精密进近时产 $ I& g8 L- p9 X7 r. H失压, - e; v2 b# U T- g; D0 @& Q3 M0 ?4 d9 D. U" ]' R7 _( V 排油," c+ |2 s1 J" v 用飞 1 g3 @! A! ^' x$ H/ l英汉对照民用航空词典B OEING J! V' r' F0 J0 B TECHNICAL DICTIONARY 41! s2 H+ [' N- B4 c, r* M( ~. t* d DEFUELING VALVE, A valve in the fuel system for+ v; k& }/ d8 T }9 J* E efueling the tanks and for transferring fuel between the 8 U" {: y1 ~* P* PE-ICING, Removing ice after it has formed on aircraft. ; j6 ]" C1 {% z: h( xChange or difference. & {1 n3 g. t5 j6 M* o' U! nEPARTURE CONTROL, A function of an approach3 j1 x, f% ^9 C; m ontrol facility providing air traffic control service for2 U, i/ x% k# j$ ?* T6 k+ f5 Y! F eparting IFR and, under certain conditions, VFR 2 c1 t3 G: e3 B8 H( R: vEMODULATION, The process of retrieving information5 Y7 X& f9 B$ O& a+ T carrier voltage.- }0 m' g0 U" V% r9 U, a: T5 T* g$ b0 R ation.% D& O* W( ^. w lic # X( \1 V6 i% p, i4 ncreasing hydraulic reservoir air pressure to) h, K$ ^5 H& y1 N0 Q5 [, `' k mbient pressure.* \4 a3 B6 p v9 G 箱排油和在燃油箱之间 ' X: g: W. N+ A$ s) _送燃油。 * m6 o2 O7 s2 A8 _; U/ R& o冰, , i" W+ Y& P' w. g) w) y4 K除去已凝结在飞机上的冰。/ J$ D3 i6 R: X. p5 s 删去或取消。 # {" T8 K0 L; z. P0 d量, - u6 }- T9 R* @! y, z* N o& O变化或差异。! M/ m$ j. ]0 d& G& t } 场控制, 1 h# P7 G) ^# Y7 W0 g* m给用仪表飞行规则离场,和在某种情况下用目视飞行 3 l2 x# m |0 o2 r3 z则离场的飞机提供空中交通管制服务的进近管制设施 3 U2 G* Q J& C; p3 ?& F; }. [6 T" U调, 4 b7 U6 z4 \# J6 y: k: k电压中获得调制电压的处理过程。 7 O, @& J, U0 t1 X环境* \7 L/ F' N; [0 W 力相同的活门。" W5 `; b; ?( p; @5 O d , M4 A7 F% ^3 f: S/ Xtanks.* G* U9 I$ X4 ]' K2 V( ]; Q D, j |% }3 ]$ i9 E. ]8 { DELETE, To remove or cancel. - W h" @0 Y$ v1 X5 W4 tDELTA,9 y$ ?) q" \8 r D ; P. f9 Q8 J3 E$ b4 }" `0 O4 Oc 4 f. A0 z ?& x ad 3 C6 ^, g- y$ laircraft. 9 ?, F A; S9 K. {0 Q( QD; n. P5 l1 `2 w1 m (modulation) voltage from a modulated 4 K9 q' S/ w2 `' B! l% NDEMODULATOR, A device or circuit which performs : ]" p2 R/ A! a: s p* A& h$ E, athe process of demodul / N( K0 W+ L) Z& ZDEPRESSURIZATION VALVE, A valve in the hydrau4 H1 A/ c% L/ v! Y" q system for de: ^- W' P. F0 Z4 R5 g0 P, @ a' b5 L! T: \, p' d! R% r' y7 p 排油活门, * C3 i1 B2 s. S2 m# v1 T) E7 V燃油系统中的活门。用以为燃油 ( _5 P- u) F- L% e9 T) n/ e/ {$ g; v: l( v: I* e3 R' I- g 删除,. Q; t6 P. w0 [ Z* ~- Q% E9 r" H$ l$ N9 M2 G0 v! k/ B3 r' F$ \) S. b- q" V% _; ^, F! d 的一种功能+ ~4 K: J& N7 E5 p( u( a1 A2 B. C* D) \& T9 C3 s3 J% |* z( f 从载波: [, ?' x2 @4 v% ]* ? 解调器, ; S Z/ F. V/ {. L完成解调过程的装置或电路。! [5 m4 D* r( {" ]7 w: Q9 B 减压阀,3 X9 c+ \) g3 c1 R( [, g3 T; v 在液压系统中,将液压油箱空气压力减至与周围 " W8 i# O. N/ J! R( N2 V7 d: Z0 O9 {英汉对照民用航空词典B OEING 5 e2 g1 h. y) WTECHNICAL DICTIONARY 42* {6 F0 e9 T! i! ?% r5 V7 O8 | DESCENT, Phase of flight where altitude is decreasing. ! }# M6 D/ Z' Y- c) TETAILED FLIGHT PLANNING, The calculation of fuel0 x2 V1 e! n! r- @$ q nd required for a trip by considering each phase of : g0 D2 a4 j. J \9 a1 ]2 b" k; Might (climb, cruise, descent, reserves). : n: H# p8 h* Q. Q4 Xal or& {; g; b" ]3 g% `' _ ETENT SOLENOID, An electrical solenoid used for8 T$ i! x, E4 [# m% k: \4 s t.$ j) ]( ]5 i" t$ O specified course or 1 V0 |# |" L1 S& w: B3 mrocedure. 7 N6 ^: a2 ?- f- q2 I0 oe.0 b2 @" Y6 d; \" T8 |9 F4 W 飞行计划, : ?( K" r, _; J9 ~将航班中的每个阶段(如爬升,巡航,下降,备降)都 U/ \1 W" N/ B* l) o! T% m人考虑,来计算该航班所需要的燃油量。 * m- }' V6 X6 i) f4 d. Q; ~用来感应情况之正常与否的电气装置。& L" J( M& g. X) ?- F2 @ l6 m 定电磁线圈,3 ]3 K J+ ^* h! w8 G# ^5 A% Q 出接通的电磁线圈。 ' O" w8 m% \3 q8 [$ B5 Z& ?差,) g! q" }. B+ ^& [- ~0 y! |7 v 与指定的航道或程序之差。 . k6 _( y8 n \! p3 v& K& v用气压或液压操作的活门机构中的柔性部件。 . @8 }! l: N) O' p1 ~D ! E' d! c, h4 ]: Pa 7 d4 @, X" y1 O; G9 h9 R& w& Ufl # Z" u( {" \+ Y3 B9 e2 A6 b* WDETECTOR, An electrical device for sensing norm 5 Z8 r4 y& f7 P' j, y4 [abnormal conditions.: d2 U7 { B' z+ F- g; {2 s D+ O# {1 Y; d$ L controlling the engagement of the actuator outpu5 P0 ?' e1 y' b7 s4 f DEVIATION, To change from a . Y* Z! M- {* E! M* np5 f$ c& z+ Q2 ^( H* [* ] k$ `' |* i( X DIAPHRAGM, A flexible part for operating a valve c0 v4 Z( \5 E8 H! O. J9 _" C mechanism by pressur; N) k# f( J% e$ ?; ]6 t 下降, # m8 m0 I# W: Z) u/ c; @ T飞机高度不断降低的飞行阶段。$ o; Z5 [ z$ N1 }/ A 详细' P5 v7 n2 w; a' h+ W: w& k0 O1 a) Q6 ]; ~探测器,/ `: N8 X6 p$ o. H4 Q3 _$ z" H0 b4 c# Z2 H- x9 {5 A 用于控制作动器输# z: I" K( P3 P* Z4 s7 ? u5 }3 M1 @, L; H, X 隔膜,4 I; v* h" q9 [& L- B$ Y/ C/ w- u 英汉对照民用航空词典B OEING , s* A8 m+ D* r* X4 L& F fTECHNICAL DICTIONARY 43 % D( M* J$ U( ~9 R. qDIELECTRIC, A material which does not conduct& C& Z" v: Q6 ]3 @, W/ k+ ~. r electricity and used between the plates of a capacitor - a+ m9 T h6 o3 d" a8 k9 g(condenser). 6 v9 ?6 w: p/ X; vnother pressure in the same system, measured in: l1 a3 o& R" Z0 ~$ U; j ounds per square inch differential (psid).9 O7 P0 N, {' B; `# ] IFFUSER, A part of an engine between the) n0 w5 Q& c& |, N7 h ompressor and combustion chamber for reducing the - Q5 Y( @8 D4 W$ T4 v, M2 ^air pressure. 6 s/ w9 q& r- c2 s: eigh, w2 T1 ~5 ~. t3 w8 E pulses., p1 C0 }! |1 P+ w. z! h# m ignal that is a close approximation of the original+ Z2 k: t( I4 t! |7 r# |# [5 O: P- l ignal.! X) C% J* H0 T' n9 R* U IHEDRAL, The angle between the wing reference + M/ @) s3 @& y6 ]. o4 dlane and water line.- J# `) f1 u5 Z& k, h) [. Z 的压力,以每平方英寸: t9 @7 U4 n' b' t 少磅压差计算(psid)。 7 G7 W3 ~% C4 j4 J8 P1 h# J散器,! j4 P& z( {: r. {2 M 发动机内压气机和燃烧室间的一个部件,用来降低空7 ?; W1 X2 A% A- j, o. z. S- B 增高空气压力。* f+ g0 J0 [ _6 l" P 换,2 \) e- c. C! V0 k O 的连续可 0 J; X; B3 l0 G g(模拟)信号的处理过程。6 c: T& c2 V( R: _4 Y: |7 Z 反角,+ |. A1 G4 Z1 j; I9 `0 c$ x( P 机翼基准面与水线之间的夹角。 * i, ^: i. y8 I9 u8 a7 ^1 O. HDIFFERENTIAL PRESSURE, Pressure relative to 3 L$ W2 @ c7 {3 q* I5 I' aa 8 D2 U( P% B% O4 V2 b Ep# m/ w6 o4 t, [1 o' g* u! w1 ~8 u D- G2 C- _" C1 ?* } c# v* C/ K; Q. q1 \/ v) c/ U airflow speed and increasing the ( w4 e% R1 y6 {DIGITAL, Digital refers to a signal whose amplitude * _ L( H4 }1 I/ tremains constant for a finite period of time. Digital+ ]! m- I* N) z9 T, b$ t4 F: E signals are commonly represented as a series of h" n/ ^- L- k" z; j and low0 X% P8 E/ \# W d b: ]0 t DIGITAL-TO-ANALOG, The process of converting a+ p) }* d. l% ~: [& }. d digital signal (binary) to a continuously variable (analog); ]: s- C |- t/ M* S, r4 q* o+ v s9 o5 f, z5 @$ }' X7 ^ s $ L) A, ]6 D1 U2 Y5 F- ND9 U6 O; s8 i {# K. C( Q% M7 Y1 N& m p+ a- H/ k% f3 \3 U3 { 电介质,1 J+ H1 f6 ^9 w' T* ?3 z0 z 一种用于电容器板之间的不导电的材料。- |) x5 I( F. E4 } 压差, . o" H G" ]$ H! o$ m) x. U相对于同一系统内另一个压力 6 y0 T4 V" y; |5 v/ t: L' {" i: Z! p l% D, G' X/ A1 o' ~+ q, u# U( `6 j, g7 J 气流速并 " c: [+ A: P6 k- W5 u数字式,1 b* m( C0 [. g/ { 指一种信号。该信号在一定的时间内,振幅保持不变。/ ]1 |( H9 e: R- G L 通常由一系列的高低脉冲表示。3 x- k& J: `+ v9 J! w/ b! @7 Y 数一模转7 O# ]+ N; ?3 O$ X3 A: I 将数字信号(二进制)转换成与原信号相似& ?0 X4 P5 C6 H" Q' W9 S) ~0 J3 _. S3 a, V M/ X! [! o, I; f* M+ T) f9 O- F$ [+ \英汉对照民用航空词典B OEING. X, f- _7 Y3 |+ B, Y1 a TECHNICAL DICTIONARY 44 ) T S$ c, P" ^# DDILUTER DEMAND REGULATOR, A component in the 5 e9 d4 K T! b+ r, Pcrew oxygen system which mixes air and oxygen and , s1 G; w( {8 P% U3 Rupplies constant oxygen pressure even if there are/ Y; r1 z- W, b" U' Y# u hanges in ambient cockpit pressure.$ O0 R$ u- n7 Z+ q- K$ O IM, A word value of light. For light control devices - dim . D, E3 }! L( m3 u6 ?the opposite of bright., w, g( I8 x# v8 C4 S IODE, A device which allows electronic current to flow/ T" |, R9 h; u9 x* R& x( l- x+ X& Z only one direction 7 q5 h1 h: S0 luid in a reservoir. - B e8 {% Z0 i6 o( ]2 PDIRECT, Straight line flight between two navigational & w& S6 Y. l/ Naids, fixes, points or any combination thereof. When- o- L4 ]! Z* I& r used by pilots in describing off-airway routes, points* B+ g+ B/ F3 k2 w+ Z, q2 W defining direct route segments become compulsory , Q( u0 g& A. X6 L" d. }- |# dreporting points unless the aircraft is under radar ( K3 P6 ~. _" p" l& H/ f |4 Kcontrol.: N5 V w- l' ~6 ~ 节器, $ t" E3 c# h- u/ j* d9 k2 z! ?将空气和氧气混合, ; b; P( j) H# t+ M6 C& l3 [9 f+ \6 p9 `使驾驶舱环境压力改变,它也能提供恒定的氧气压力。+ Z7 k: j, T, E3 B2 _1 Z2 }: R$ B/ y0 K 一个形容光线亮度的词。对于灯光控制装置,暗的反- ?' Y' {9 ~/ K5 m$ t 词是亮。 6 `6 V) }) ^# h; N! J/ w极管,- e5 Q7 _4 M) Z; b V 只允许电流向一个方向流动的电子装置。3 d9 c, |% {$ D 器内液体的量。9 s/ k( w4 L+ \" i& C6 |# m1 F 直飞,8 `2 @2 v( \) e1 w! h 两个导航台,定位点,导航点,或任何的组合之间的直/ ~' Y) b2 _4 y, l. L 线飞行。在被飞行员用于描述偏置航路时,除了在雷达控 : l: f# |9 @. y4 s" k制的情况下,确定直线航段的导航点成为必报点。 ; f* @9 J r) x6 b& zs. E5 J4 u: v+ A8 ^9 T0 w c " ~$ x W k/ J4 C; ~ {D 3 q# I* a: M; ]4 l8 ~is2 d! q' b6 i$ A( V& Z8 e/ x D' g: G" U0 [8 [ in % V" t& a4 L& Y& b! }$ B% EDIPSTICK, A calibrated rod or stick for measuring a 6 y: c1 ~3 }' W1 _% l1 Nquantity of fl `; [4 O, Z& n, c* l$ d 稀释氧调 6 s$ y0 i3 n! ~; a6 c' l2 D* [& M驾驶舱氧气系统中的一个部件,它1 V' I5 }, E5 u2 p r$ v! S) p, n9 N, w$ w3 l" s( C8 J; P; z, i, R" Z( H4 ?' M$ \ W, m+ \. w$ i+ F# t: |3 u- D1 Z8 b" O U量尺, ; p3 d; i1 v* K7 z' Q0 P: [. _) D7 y校准过的棒或尺,用于测定蓄液1 V& Y% q0 _' ~3 K% d# u! n! F6 y 英汉对照民用航空词典B OEING ) Y/ H4 \; ]# e. G9 R8 cTECHNICAL DICTIONARY 45

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