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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 ; |. z( g" t F4 b民用航空词典 / t2 N" p4 q( s0 x波音商用飞机集团 , z# }, S# U3 D8 Q: x9 dBOEING COMMERCIAL AIRPLANE GROUP3 k8 z$ A u4 U2 q4 w" A' Z 英汉对照民用航空词典B OEING. _+ P& B4 {' x TECHNICAL DICTIONARY 1 , g1 r2 w; q2 ]* l; J: p+ I$ jA! Y0 n4 _0 d W8 a5 } ABEAM (ABM), Beside: An aircraft is abeam a station$ s' y+ Q. N+ v. B. a! M4 n when that station is 90° to the right or left of the track of5 F1 e, [! I, m+ o ~( E the aircraft.1 E' p. [: }. V$ e- f6 q& N ABSOLUTE ALTITUDE, The actual distance the aircraft, f$ I2 Z9 z* t* x1 S( U% ?! g: L is above the ground. - @) X; r6 t: v" sABSOLUTE PRESSURE, Pressure of a liquid or gas : H$ N+ F H3 q7 g% {' hmeasured relative to a vacuum.5 b% O0 G0 i; j+ p# j ACARS, SEE - AIRCRAFT (OR ARINC) REPORTING; a- a5 h$ ?3 U g+ W, L) D, g ADDRESSING AND COMMUNICATION SYSTEM4 P" D4 m7 n1 B; M" x ACCELERATION, The rate of change in velocity with$ p4 P$ q; b1 E7 v2 W2 o5 C4 F+ c- C respect to time. ' _- h/ ~# `9 EACCESSORY GEARBOX, A part of the engine,0 F( P8 R: c$ s. \! J6 v mechanically driven by a compressor or an angle2 @! n/ f# B9 G2 ~. J! _1 x+ j gearbox, for driving components necessary for engine' c" n: l9 F. O5 Y" v( P* W4 a 正切, : z9 i* V" [ Q- F+ z; Cand airplane operations.3 r8 O$ O) _, i8 G t; E' R 当电台在飞机左侧或右侧方与航迹成90 度时,飞机正 $ F Y5 q; N8 e/ X; A9 ]: G/ p切电台。 9 K5 o6 U; H) s. @7 f) Y2 G3 l3 w) i绝对高度,! ^" d. P# ^% i. l 飞机离地面的实际距离。 ; l% }# ?* [! a% t2 d绝对压力,0 n9 S8 j( F! |/ E7 p 相对于真空(无压力)测得的液体或气体的压力。% P `( n1 i7 j; _ 飞机通信寻址和报告系统,: e. V. s z/ k% Y: Y9 X) ]9 G8 E 见Aircraft(or ARINC)Reporting Addressing and ) @3 `% U2 C& X( h& y' PCommunication System. . H+ o2 B, l% v& n/ b2 \6 p& q加速度, 3 y9 d7 M! d& p9 i7 r+ U9 }随时间变化的速度改变率。 * v# k: s6 X& d" b' g1 e附件齿轮箱, 1 q2 D1 Y1 z2 z- h3 Q发动机的一部份,由压气机或伞齿轮箱带动,用来驱动& ` _; o T: \0 N+ U 一些使发动机和飞机工作的部件0 N' ~$ c- W- ^' v# O 英汉对照民用航空词典B OEING ?3 F% s b3 Z7 rTECHNICAL DICTIONARY 2 6 `9 }6 d+ P2 |; ^/ N6 wACCUMULATOR (NO. 1), A container with hydraulic 8 b" N4 P b4 x) R i& zts when normal hydraulic supply is not8 c" J0 Y6 D1 ~: w3 V# B, X vailable. ! x9 _/ k Z* ?8 [CCUMULATOR (NO. 2), In a computer, a special9 `4 U- S! o1 j, D- F$ | torage register associated with the arithmetic logic unit,2 Z8 @# k9 k) s# M8 ^% Z olding the results of a computation or data+ |, A5 o3 D* \ ACTUATOR, A mechanical device operated electrically, 8 v6 n" V9 }4 m& m- [hydraulically, pneumatically or mechanically for 3 z3 Q. ]3 f% I5 Q% Wtransmitting motion between components.* }" K) Z( `& d ADC, SEE - AIR DATA COMPUTER : c- e( D+ ]3 i8 Z3 M3 D) ]ADF, SEE - AUTOMATIC DIRECTION FINDER ' l; E3 A" @- YADI, Attitude Direction Indicator, An electronic display of5 j8 h( v9 M& O6 q airplane attitude information in pitch and roll.8 _1 y2 {8 H9 D. D# q 蓄压器(NO.1), 1 i% n/ k( S9 A8 ~0 E" D- N" }含有靠干燥空气或氮气增压的液压油的容器。当没有正5 N2 ?+ F4 M" `, M) N# x7 `/ ^ 常的液压源可用时,该容器可用以驱动部件。 9 X" C. ?, s" g- a6 O4 O( |存储器(NO.2), 7 Q' p3 a+ `3 d7 p) H3 x. s计算机中,一种与算术逻辑组件有关系的特别存储寄存 # G7 A8 m# T, f: k3 i$ w5 k; |器,用来存放运算结果或数据传输。7 D# z" Y; m& Y6 A: M 飞机状态监控系统,3 Z- o, W8 ?0 T+ W& I8 U* ~ 见Aircraft Condition Monitoring System, R5 ^' \* E7 h j( p$ Q# R3 d fluid pressurized by dry air or nitrogen for operation of * j% l1 {! ]' O! {! ncomponen & |8 \* B+ y7 {% z+ Qa7 M0 q$ T1 H5 |4 ^7 r A 4 ]8 {, n! z: W9 k5 rs , u* e5 H* \6 w$ ~used for h $ o. A8 O ~9 l+ btransfer.0 A. W% Z2 y7 z; ~3 |$ a5 o ACMS, SEE - AIRCRAFT CONDITION MONITORING5 N6 _0 T9 l, \, a. | SYSTEM .9 B8 E$ ?! @$ o2 J: C 作动筒,2 X$ N$ Y- \7 _5 R 由电,液压,气源或机械驱动的机械装置,用于传送部 c: e) U# e+ t" R) Y+ V1 ]7 o' Q件之间的运动。. G1 T: Z5 M1 ]& x 大气数据计算机, ; v g0 V( \# }, S0 {' h7 O见Air Data Computer.* c8 L, }: y% v/ \) a7 s# u# f 自动定向仪,/ _9 T; h8 J3 { 见Automatic Direction Finder. 7 f- a9 P4 f1 X: L5 V# T5 s2 P姿态指引仪,+ W: o, D: `; g" D 用来显示飞机的俯仰姿态和坡度的电子显示。 7 V" Y* h" M, K$ Q! u英汉对照民用航空词典B OEING$ b7 D* g0 U: o% F& ? TECHNICAL DICTIONARY 3 |) T2 K0 Y3 ]' H* i& e. W f$ c0 M& zAERONAUTICAL RADIO INCORPORATED, ARINC is , [- _7 C0 ^4 v& `( p# n, 5 X K! F: b; mnufacturers, and foreign flag airlines. ARINC4 }7 S. h9 L- T: P: h evelops and publishes standards for electronic8 Z) V; h# |: \ ~, g) m9 Y quipment and systems.( \5 F# z9 u) ~, s" ] GILITY TUNING, The capability of the DME to 7 u) r+ g/ _/ G6 Ylternately tune between two different DME stations in7 T8 i: b0 y- o rder to get two distance readings from one 2 f5 r; q E6 tterrogator. 8 L! q) e I) Vge2 K5 g6 N" U+ L7 d ILERON FORCE LIMITER, An electro-mechanical$ V& u+ `+ W5 R. {) |8 m# y) o IR CLEANER, A component in the pneumatic system9 Q" e. J$ c# ?3 a% t K upply to the air" ?7 w+ T5 e1 d* _8 X onditioning system. _: X" m5 m5 P1 ~3 c! ]订并出版 5 ]6 B/ ~- U" j* G$ G; p: E* W子设备和系统的规范。% S" p* R) _0 _ 快速调谐, % y- p7 L& K4 z8 t机载DME通过交替调谐两部地面DME电台以测得来自' _* W7 a: k$ e 同一台询问机的两个距离数据的能力。 / X: P$ F8 |- A8 k4 i翼操纵力限制器,5 Q' I) V G8 k" `. g 装置。在自动驾驶工作期间,用来限制驾驶盘 # K) s6 v+ N7 @# Y气清洁器, # A v( w# z: P- d) t! L部件。用于去除供空调系统使用的发 6 W0 A9 K, r, B! m( z w1 o8 ta corporation whose principal stockholders are United 8 H% G" t5 u) J$ ?2 {( iStates scheduled airlines, air transport companies 1 G0 m2 ^1 ~8 K F9 B4 ^" ]1 {aircraft ma @% i9 M" ~! Q! E$ e2 f d& J: z% q& P! h e c3 q* u; b$ E3 K# A( hA* a7 {2 P% Z: o: @9 c3 B& \' ` a4 _6 s0 O2 J a, W6 D o# g( ? ?& y5 a# ~ e$ J* T# f/ p6 [( J in# g, R. h! ~) f5 d3 n( g0 b! R AILERON, A hinged moveable part on the trailing ed 5 Y% K6 e$ ^' i! _* n3 ~4 nof each wing for airplane roll (wing up and wing down) : [9 d, q9 t2 \; scontrol.8 O( F& j4 Y; b9 `* b+ J. E A3 O4 D6 P: `: s( I. q, i7 F. y device for limiting the control wheel movement by the L6 m: V- R' e' vautopilot during autopilot operation. ! c, C/ E% ?3 d( Z; n% `! yA: B5 J7 L5 }/ t' h5 P/ V. A/ M' b for removing dirt from the engine air s , q& \# X0 x' }8 A- V- L) gc " Y, Y- r2 y: _( h! Q航空无线电公司,6 k& v: w6 v2 L! O6 i a) d 主要股东为美国定期的航空公司、航空运输公司、飞机 ; h2 o& @) ?# Y% b7 M- y9 @制造厂和外国领队航空公司的组织。其目的是制! ~# U; ^! j, y# g: J7 \, j$ W+ R/ a副翼, 4 g+ D! j5 X* D F0 b3 ?铰连在每个机翼后缘的可动部件,用于控制飞机的滚转( q& d& q" V% Q; N* Z6 R/ l (机翼向上和向下)。8 G8 P# X+ S, d. D0 ?4 f& I8 h+ }4 M- S& C4 M一种机电 & }/ l* P& ^$ B8 \7 Y的动作量。 ; f9 `& t7 p& k( s3 N; }9 X6 N, [! i8 g# O, c4 `& }) ?气源系统里的一个# o( G& R( R; C1 y2 \ 动机引气中的灰尘。) M& `/ j$ E+ l 英汉对照民用航空词典B OEING6 C( ?% S' \' Z! K TECHNICAL DICTIONARY 4 3 L9 L( p' I8 G: A5 A5 vAIRPORT ELEVATION/FIELD ELEVATION, The 0 D2 r/ K+ r0 q5 i6 {highest point of an airport's usable runways measured ! a2 d: N8 V9 ~8 J2 Vin feet from mean sea level. In a few countries, the7 ]1 D* i$ q& C( k9 s5 e airport elevation is determined at the airport reference - g6 Q9 C3 J5 Q8 T1 q# Upoint.' P- k2 Q; f" i- O" \( ~ AIR ROUTE TRAFFIC CONTROL CENTER (ARTCC), / \% S, _' L# T# T2 n# I9 r Oervice ! |( Q; o3 {; t: Sase of ; r O5 m# h0 m% eus flow of air traffic.4 M0 h Y- V; w* R8 s- s IR CYCLE MACHINE, A compressor and turbine on a( F: C( \3 p+ G( m& U" c' q2 B ommon shaft for cooling the air in an air conditioning6 X7 Q9 `5 X# f+ I! }/ }' o d ystem. The air is cooled by expansion from high to low ! G: j' g. Z4 t8 I' Mressure across the turbine. The compressor is driven , t2 J8 I* N' [, s) W9 \! wy the turbine.4 P% e/ t5 _, s2 f 中航路交通管制中心(ARTCC)," p6 ~0 W, M3 k8 H) ~1 o 域范围内使用仪表飞行规则飞行的飞机提 3 `( Z5 a5 v5 g* Y! q4 u' d9 } A管制(ATC),/ P2 {( u7 y: q. Q 涡轮冷却器,& G! ?( @+ q, P6 d8 k 是装在同一的压气机和涡轮,用于冷却空调系 3 U G# v0 J& M0 l统中的空气。气经压气机压缩后,由热交换器移去热量,/ j" B3 H$ P; Z 然后经过涡轮令涡轮带动压气机。通过涡轮之空气,温 o- e/ w" h. A/ `, T5 t' ^. ^" x 度下降。) I5 q7 ~$ R k% ?! K+ b A facility established to provide air traffic control s% A( X7 Z1 Z1 }2 j0 i to aircraft operating on IFR flight plans within controlled* D7 F8 w. a7 i6 R/ r0 h& V0 Z airspace and principally during the enroute ph; R$ J j$ n1 B5 y& c6 X0 s! \ flight.7 K0 ?& L6 r1 X% B8 c+ c3 Z AIR TRAFFIC CONTROL (ATC), A service operated by ! w w. `4 ~+ c; E; O5 ], ]appropriate authority to promote the safe, orderly and7 X/ U( I8 ~/ M5 ^; {2 P5 G. A expeditio 5 [& H1 Q" e0 P; i; vA8 C- f, K# |7 U6 S9 o5 ^ c& n" C8 \0 u y3 a s ( m1 l3 v2 ]3 Vp! ~$ y3 v f( v6 e. @/ ` b H/ n6 n5 e! T `+ b( D) t 机场标高,% k+ Z: ?6 A# L; C1 m0 E8 k 指海平面与机场可用跑道最高点之间的距离,单位是英! j+ P. ?$ G& \' D) r, } 尺。有几个国家的机场标高是由机场基准点而决定的。4 ^) |: Y9 w7 b/ X1 u& i2 x' g# W+ B9 c 给在控制空3 m$ J% l e9 S$ c/ T4 W 供空中交通管制服务的站台。' n# d: }) h i7 U5 r 空中交通2 v' h& s5 j: e: l 由有关当局管理,旨在促进安全,秩序,和效率的空中# P. @/ O4 d& o, v _# q 交通服务。; p5 S+ B4 S& K' U) k& a0 b 根转轴上 # R) r) O, I1 N; c/ x2 i. g5 @0 S. ?6 O( ]3 f: T! \" ~0 y1 d7 D. m- g, p; f 英汉对照民用航空词典B OEING 9 I, r% w. Z1 M0 s) r, hTECHNICAL 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% v b+ w" p( Z2 z data information, such as altitude and airspeed, based3 W3 e @+ r' U3 e, b, L on pressure and temperature measurements.6 a; t+ D/ e& `$ c' i {0 P8 b es air& t e/ N# A0 ? IR TRAFFIC CONTROL, A system comprised of ]6 Z# ?- n& @% j/ wround and airborne components used to identify, track4 F8 Y" r1 [1 r+ Z: w1 I( [$ _9 T6 }5 ~ OUND SENSOR, An electrical device operated . B0 L3 X" g' k" ^, Py the landing gear, which transmits on ground/in air- D" @' Q7 @2 X formation for system operation in flight or on the : ^7 ^( |4 w! v; eround. 7 p3 U$ T9 x, J6 D, M6 `: vIRBORNE VIBRATION MONITOR, The AVM takes - f( f9 ?- u5 }& g9 M' Y2 m/ x8 `, `e signal from the engine mounted accelerometer and 9 _2 A0 Y* p I* E" Zalculates the vibration on that engine.3 g4 Y0 Z" g3 D corridor equipped with radio navigation 3 v; V2 Q4 ^: n) g4 `* uaids.& Y2 n: g! j$ i- s$ ? AIRCRAFT (or ARINC) COMMUNICATIONS7 P3 Q' m2 k, W0 T ADDRESSING AND REPORTING SYSTEM, An % I3 Z% y6 L+ K8 v+ r2 Gaddressable digital data link system which permits the ' O3 s( l( {% v! t0 V* R( [. G( x5 zexchange of data and messages between an aircraft 9 h9 }. F1 N" M0 r0 e. Yand a ground-based operations center over a radio) W: ?8 p+ B; |9 [& w7 x4 a network.: M0 Y# C$ T. m, V5 G: \ AIRCRAFT CONDITION MONITORING SYSTEM, A \6 g3 T0 h8 }system of sensors and recorders to monitor various ' v4 E, ]3 h6 H/ O$ x5 ~airplane systems' performance and status. 4 j! H) k* z2 X& a [! m& \: `机, 4 f% H- I8 w' W8 C0 e# x中交通管制,4 H" \, ~9 T4 ]- g4 E( G; L5 I( F' { 一个由地面设备和机载设备组成的系统。用来对飞机进# j5 k5 t0 s2 i 地传感器, 0 ^' `) X% x) q+ j9 U一个由起落架操作的电气装置。用于给空中或地面的飞 8 R' [" X$ G* L+ K/ @系统运作传输地面/空中信息。(有些系统只能在地面" o, o- d( o9 B. r" z" g0 U 用) 5 }" v# P* Z0 `载振动监测器(AVM),/ u0 T2 ?) l+ |3 w9 S AVM从装在发动机上的加速器取得信号后计算出该发/ x; S) C: f5 L! u' R& q) t 机上的振动。0 a* _$ K7 c9 u- r6 N% n) \& r 式建立的控制区域,内有无线电导航设备。 " x; U6 P/ @+ p q, U飞机通讯寻址和报告系统,7 r$ A) C# b' x+ z. ]* b 有种可寻址的数据通讯系统。利用该系统可使飞机与地, ?/ w" o% U% Z4 ]: m& P/ y! K 面操作中心通过无线电网络进行数据和信息的交换。- i$ N; [- _ ~! I 飞机状态监控系统,! M' O S% C; d1 L8 P6 k* ` 一个利用传感器和记录仪对各种飞机系统的性能以及 x$ q% y% [3 j" u( t+ R状态进行监控的系统。" B0 V3 |" P q+ J& V; Q) |( x3 { A 8 Z y$ M& }6 g9 c/ u- g. X0 Cg 3 w9 l( z) _# l. @and locate aircraft.( k/ o" S& G8 f! s, d/ N, H AIR/GR ( c4 F4 L- x" Mb, q- |( o& q/ O s9 ]0 u5 z+ a% G in- g. w( C/ z3 t g7 z# r, W/ O3 ~ | A ) t4 O& J& e6 L& Hth3 h& B) I* N" v; e. m8 D9 r0 j) q c 1 s4 s% k. ?' y& P9 u) @' c) @1 M; WAIR WAY, A control area or portion thereof established & ?3 ?* G @* u, Rin the form of a m3 O* U( q9 Z7 Q 大气数据计算 - P% i, f5 n# k$ @& J根据量取压力和温度而产生大气数据资料(高度、空速4 w& f; v8 H: e: {) e( f1 p 等)的计算机。0 M. n P2 \: V n6 x: R8 H2 w/ ]1 w* s- o( J* Q行识别,跟踪和定位。 % i# G. T6 Y1 m( j" B8 j" B/ w9 r0 U$ x9 _' e; J/ C% i. V3 n- q" k. s8 A: `; s使! B8 v. Q3 e+ p7 a. t: Y5 s5 f* Q: {5 T( d3 Y. r) _+ I3 _5 B. _0 m3 t3 \- {1 _# H航线, : h. D- w V8 l; Y以走廊形, G4 z/ F7 q$ ~: y% V* ~ 英汉对照民用航空词典B OEING 6 M# r- S# l; {1 T6 TTECHNICAL DICTIONARY 6 - g, b: {% R7 ?: N: lAIRFOIL, A surface designed to obtain a useful reaction, / W9 a3 u) |9 Zsuch as lift, from the air through which it moves. Wings, + c% B _0 J* D; P, [+ T. ?4 Astabilizers and control surfaces are airfoils.0 ]- A( ]/ f8 l. z6 h5 v AIRSPEED (IDS, TDS), The speed of the airplane ?3 b6 }$ t4 k+ k$ _rough the air.5 G" G: E# S( s7 C) G D INDEX, An adjustable pointer on the $ p5 @' X Q& \: O5 }4 D# Yirspeed indicator. , r# t& J6 n7 N2 `3 I: Rand legal ability: j! G' W! R7 T( `4 T fly. 6 K: [" w. k" Q$ c5 km, for example, the procedure for finding the : N8 L( a3 ] @1 s3 \quare root of a number. 6 A/ l6 z7 G/ Z! G! o1 m1 K" L% yy5 g8 ?9 v: Z) i( N/ y3 O re, wind, 1 e: \/ b% G6 o# P6 a( Zand aircraft flap setting. - E# [8 L2 W0 N$ o是翼面。 . v3 m ~. o5 K6 y' b- h% J, d; v$ f速, 2 b3 E$ _: `2 F0 i1 n. u! _8 N飞机在空气中运动的速度。 2 _1 ]% J* _1 M# ~9 h6 ?6 J$ {0 d' d$ W" J4 @2 S w 在空速表上可以调整的指针。 + z& K6 W; ^, n机械飞行能力、和合法性的飞机状态。 , E; z" c. x8 l- @# k一步一步的解题方法。例如,计算一个数的平方根的步 5 `: c3 ]2 x5 n, t& Y! {/ Q+ }( X. ~. X, r( s) }$ k7 |# ~/ A$ }- L' [6 c 资料的法定文件。 5 h+ i4 _3 J5 j& a1 e翼位置成函数关系。 2 C7 H# @4 ^* m1 I/ A' w2 N* Fth ; T0 x0 x9 ?( nAIRSPEE # i! \/ g+ ` K5 g' U3 i( ]% _a' f% r! |5 R; H9 q3 }8 ~ P AIRWORTHINESS, The condition of the aircraft with , B, g# l. p' z0 H0 krespect to its aerodynamic, mechanical, 1 v; B" B. m( rto 6 A- C u9 A1 LALGORITHM, A step-by-step procedure for solving a 1 s. O7 `* J: Y$ R$ t7 I, qproble& K' _- c1 @5 n4 m- W: k5 o- ^: i s 8 `* P& z0 Y" v2 J# CAIRPLANE FLIGHT MANUAL (AFM), The legal4 e% X7 J C, Q7 u' g document containing performance and operating limits,2 X; O& N3 ], D( l operating procedures, and takeoff and landing 4 s" Q: T4 P$ B* w# ]performance.$ q5 |* a6 }( r. G AIRPORT ANALYSIS, A comprehensive set of takeoff/ R: o& m5 R; G/ W2 A, O" ~ weight limitations for a given airport runway, generall 3 p' B4 V% c; Y" r/ M; p- A) Bpresented as a function of airport temperatu3 c, c# P# D+ z$ N* N 翼面, " y; S4 ]8 J0 H/ G! l用以从气流中获得反作用力(如升力)的表面。机翼,2 z' y6 k3 _' R2 s) ~1 B 安定面和操纵面都' F" O! G- t* J) p6 ]& |3 i) b2 K2 b- }0 ?( u8 \. [ 空速指标/ c" Z4 Q( O* B/ ^: v8 R; n7 T 适航性,4 W" x1 k' R8 W# n2 ^6 g 有关气动能力、 ! Q1 m6 X! N3 a5 v8 @) f% D演算法, ' m2 ^6 @1 _5 T* n: G* V8 H- r7 t+ M' { 飞机飞行手册(AFM), 9 _+ Z c" G. S& u包合性能极限,操作极限,操作程序,起飞和着陆性 + o1 P) V' _8 ~9 b: {' X' s9 r) h, t, R5 b 机场分析,# B9 G0 ^7 q3 W8 ?: Y) I% V2 d 一套针对给定的机场跑道的详细重量限制资料。通常与 ! ?. }3 z* u, y3 U |* g/ |机场温度、风、和飞机襟" ~# P& k, Y. J* X5 k6 R8 `0 A 英汉对照民用航空词典B OEING5 ?% b# I1 `9 [. Q$ e+ u {$ ? TECHNICAL DICTIONARY 7 / \0 @8 ~1 F& v/ b+ u/ lAIRSPEED BUGS, Adjustable pointers on the airspeed 3 D( P% |3 N9 m2 j" uindicator. 3 I1 K* q2 y6 n, n. hALLOY, A mixture of a basic metal and small amounts " q+ [. E+ @* D! E8 Vf other metals to change the properties of the basic 4 l" M' f" Y& c( K, m }etal. " t; R% d3 D2 m0 U- g& X% A; J! ^Minimum airplane speed.- e, P; n( P$ i: I5 w3 e% B e of; V, M+ R6 o* k1 B itting airplane angle relative to& A# S/ x4 q+ {9 O irstream for the stall warning system. : l# P2 m# O5 W2 v" R& aanother.8 [0 e( e0 |+ o& j; E: ~& k LTERNATE , An additional airport selected during( r+ |2 U+ P- d' K# y) Z6 k0 }3 m! I) _( ^% U 合金, : U: c" x2 U$ P; Q) G在金属中加人少量其他金属,而改变其性质的一种金属 6 a+ t6 T$ I0 ^! a' q# j* n+ g合物。: K, X2 l# e! T3 C u- T# s 飞机的最小速度。+ d' N# m& c+ j3 x7 A 速警告系统传输飞机对 & o! _2 V. N) z" x+ ~5 h! \! S" r: q流的相对角度。0 @7 p: C) P, Z; Y7 u* ~$ q 由一个状况改换到另一个。 ; _7 q$ y- y) h' z1 { o+ I. e降场,$ T, p/ s4 Q. N# o 划时,除了目标机场之外,所选的另一个机 ! L# v' C4 U+ Z" y& B# G7 uo 6 \& m9 M4 e0 L$ Y+ e8 am . k# M; O2 `7 |7 |% |ALPHA SPEED, 4 _% J) s d @' P8 YALPHA VANE, A small moveable airfoil on the sid 7 A, m7 a5 N( c2 `' F- C/ bthe fuselage transm ( h/ n) x- D4 x/ m/ a" o3 f. Y8 A \a ; ]6 w! K( J3 ~( o- z# VALTERNATE, To change from one condition to 3 {2 g( X: z; O( y8 S" y/ s! hA y7 E7 D, ^! W% j& b1 t7 h& aflight planning, usually near the destination airport, to be' U# a/ u2 D) u8 m9 V used when it is desirable to divert from the original4 B) }5 n7 R. u/ `$ G destination airport.3 Q) O0 E! T$ e0 i 空速游标 0 U; q% s" F. D' [, R4 f$ I1 d; w空速表上的可调指标。 / O* w6 G: b9 h- x2 N" N( h4 J1 V C- ~+ i: b迎角速度,* u' O4 z+ e8 d; X! i 迎角叶片,: W4 } F3 V) R @ 位于机身侧的可动小翼面。为失2 ], `8 Q8 W) V- A$ |: N4 }/ M; v5 w- h% m0 a3 I" k 交替,0 L& z6 v5 F6 e' L" ?, c( j9 e. x* I" q( \% g 制订飞行计 * S$ n0 _- m! V! f" G, g2 t% F场。通常在目标机场附近,以备不去目标机场时,改降之 6 y, u; Q/ J2 x' Q s用。* n) v8 G: C5 ~& b# W. Z9 T 英汉对照民用航空词典B OEING L: P0 X+ \8 U1 B# _ TECHNICAL DICTIONARY 8- H) [$ m* S; q' p2 s# j/ E/ t ALTERNATE AERODROME, An aerodrome to which 5 S1 x9 i0 u7 ]6 X# \an aircraft may proceed when it becomes either ( k/ E6 m' i Y x& tpossible or inadvisable to proceed to or land at the D: \- {9 @/ cerodrome of intended landing.9 C+ D$ h" f7 X+ m TER SETTING, The adjustment of the altimeter x3 c7 {& T' B2 P( L4 Y( s) z6 Aaccount for local variations in atmospheric pressure.6 s3 n. J- b' l0 X$ D! c+ x LTITUDE ACQUIRE, A digital flight control system9 q5 k" A% }2 P# B. B; @ R- X; Y6 ` ode to transition from climb (or descend) to level flight. 8 @, {$ A) e: t5 v0 s$ R$ sLTITUDE ALERT, A flight deck alert occuring when the- Q. l. o9 ?7 b( o7 n; M0 H irplane approaches or departs a selected altitude.5 [7 t( `, A7 `8 }% D LTITUDE CAPABILITY, The maximum altitude at5 p" P: s- O% M2 L* F hich the airplane can be flown at for a given thrust, " r! k: R( `. O. Cpeed and atmosphere condition. ' E" H1 r& i; _: a3 K: G% O3 |1 OLTITUDE HOLD (ALT HOLD), A mode of the autopilot . ]' }) T L8 Z3 qr flight director to maintain a selected altitude. ' R& `7 B8 j# m8 Virplane's altitude during VNAV operation. & H* g$ `6 Q& x机场着陆时,可作着陆使用的4 X" S( u( K% a5 c& l5 y+ b) u; E 场。; _9 x* M1 G% b% P# p- K6 I* d# Y( h3 M5 Q; D- q 根据当地大气压力变化而对高度表所做的调整。 # X9 A1 n) b$ ]8 S: ^6 A一种数字式飞行操纵系统,从爬升(或下降)改平的模) F0 _7 { L8 r9 m1 f% F4 W5 _+ H6 F$ J0 \" W% c6 Q5 y度警告, - P( `' ~6 I8 K9 [( u& J当飞机接近或偏离选定高度时,所出现的驾驶舱警告。, x) Y, Q) D- c/ k" w 高度能力,: @5 ?, ]- U' d7 G5 y% |" a/ Q$ A4 P 在给定的推力,速度和大气状况下,飞机能飞达的最大 5 N: T& z; Y; I9 V2 O. F; @7 D高度。* }% V+ B7 e% G( E 高度保持(ALT HOLD), 6 L) N4 u* @7 a. w自动驾驶仪或飞行指引仪保持在选定高度的一种方式。 b- o7 T4 J1 A6 Z( G( [/ X, }/ \3 O! b5 n, k3 v员对飞行高度的控制。& T/ J+ j8 \1 S; M9 Y im0 d* v& X1 R5 n$ I2 }* x a , B* k) `# ~, l, W, UALTIME 8 ^( X0 L: C, ]* ~( {' D% sto 7 r0 _" |4 X f) uA $ N$ s9 a" d) lm ' h: H, I0 m* x' Z+ ]A ; K' K1 T/ _/ \& m/ \, oa 4 D+ R+ l* b' x. p! G9 ]& l3 QA " p! V4 U- l+ N8 v$ q+ h: Hw & h2 F. V i4 k1 U1 q9 Fs 0 D+ Q6 N3 |1 m+ j6 ]+ r/ ]" MA. w N; g5 ~' Y0 ]" A; i o6 b! }9 D1 v& }9 N- K! S' C3 C ALTITUDE INTERVENTION, Pilot control of the f; R; W U. j+ Q. ha * J0 H, k) s$ Q; L( ]$ d+ ?! rAMBIENT, The surrounding atmosphere.- h& J; A. F6 \% A' l! h1 X k3 ]. e 备用机场,. `9 U: U3 f8 ~2 t& C, w1 X- b0 P 当不可能或不适宜在预选1 e" P7 U$ w$ O7 o9 w- k3 n9 p {3 C2 P1 l/ A& t, } W 高度表设定$ R$ }. ~% }, f* P 高度截获,) l l3 v+ E; B' `/ {2 m+ ^' n K9 T1 r' n+ j' ^" O- R 高度干预 2 [' L( w- r* X& s- d6 c在垂直导航工作过程中,飞行 ) ~: e a2 c3 D& O9 H, x周围环境(地面气层), f: e1 r( e5 i# X: G# k物体周围的环境(特别指大气)。& l7 Y! w! ? ]6 T. q. a( o& m 英汉对照民用航空词典B OEING ( c; s. r: n& g# sTECHNICAL DICTIONARY 9 0 X; s3 ?- X: X5 p$ kAMBIENT PRESSURE, Pressure of air surrounding an3 r: @$ y; ^& a. _" P" A object, measured in pounds per square inch (psi) . ) w( U- }1 M/ Z: i# U# `MBIENT TEMPERATURE, Temperature of air9 D( O8 T" O0 p0 a6 j# ^( h+ Y2 P9 H mpere. 3 w f* z: n0 e# murrent waveform.0 m: |/ J9 s' C" P4 x- y6 E g an , C2 H% S3 i' e: c8 J0 I N% \nalog signal to a digital signal. " e$ u7 P9 X1 S$ U2 fore inputs ; l2 g; A4 ~4 \9 @1 n0 @* w. Vf binary digital information and one output. The output% } L2 N* {2 }: L- B& w( g: p2 o 1 only when all of the inputs are 1. The output is 0 ' ]* r, s7 ~4 e" K3 [4 nhen any one or more inputs are 0.5 e/ w3 [8 b- x7 ]" D2 R 面气压)," C- c1 y8 P) X t0 | 境温度, 6 V2 ^9 J2 G* y% {气温度,用摄氏度(°C)或华氏(°F)来 1 I/ x/ h# X, g, A) p- b& k5 M7 J2 c+ f: O$ l电压或电流波形的幅度。 6 e) V3 F! A% _* ?# E性变化的信号来工作,或产生连续性变化的信号& k0 R3 _6 n& p 统。- o$ N4 |% r7 z( \, J3 u6 F' o 将模拟式信号,转换成数值式。 % W4 m2 r U0 C' L一种有两个或两个以上的二进位数字信息输人,一个输 7 d* z- I' U f% P的装置或电路。当所有输人为1,输出为1。当任何一个5 M- c8 ~( |( M& ^* ` 一个以上的输人为0时,输出为0。3 `2 r, F6 y! b A + R5 ^: B6 ^; Y/ N& lsurrounding an object, measured in degrees Celsius " m8 R" c3 M5 W9 ](°C)or degrees Fahrenheit (°F). : ?) O8 d" K, y; dAMPERE, A unit of electrical current. One volt across+ R* d9 w+ N9 H- c. X. M one ohm of resistance causes current flow of one7 o4 }5 ]! ?" A0 |4 {- C& J a, J0 x0 V. [1 Y# a7 l AMPLITUDE, The size or magnitude of a voltage or / T9 x2 d" n' [, @% r2 e3 `7 N& Gc! Y: O# Y# `) r3 L% ^4 l5 f ANALOG, Quantities or representations that are $ B4 E0 ?( f1 X* k8 S+ ~7 Kvariable over a continuous range. 2 P* R+ \$ q6 BANALOG-TO-DIGITAL, The process of convertin ) ~$ m3 Y8 {7 va 0 i% u J. H8 X2 N0 `% |AND GATE, A device or circuit with two or m : F* a o; a8 `4 T1 Yo 0 e5 ]# j3 ]# I" ]' Eis ; _/ n& G5 b5 R1 r0 k$ L0 {4 vw 0 x' {7 X% \( t, u/ k8 }6 w& I x% D环境压力(地 , [: ?% h- S' v1 i9 Q物体周围的空气压力,用每平方英寸多少磅(psi)来 2 X# |) c! r$ ]- O) ?% T6 s度量。3 |" d7 C4 S1 a) a, r% w* t! a6 \# T _* f, d) q 物体周围的空 - Z7 |0 o% L- t- f* u1 u1 q2 r度量。 / ~8 r- g6 i) Z- Z1 v* i5 f安培, + G6 E: g+ `9 ~" o电流的单位。 ) D/ {5 S2 z$ j' [1伏电压在1欧姆的电阻上所产生的电流为 3 q0 w4 E6 E$ T1 y' P$ Z1安培 1 Q+ c' V. _! f5 V3 Q. ^" ^7 b$ b振幅, H. a1 Q( m5 c2 a. p" J( Q模拟式, / T0 L. j9 K8 ^* V( b( o- E$ H. a, N用连续$ B' u) A) E- K, [9 a3 @6 n: }2 m% e' R% ^( |: ^% P s从模拟式到数字式, v3 f5 i1 M. w# y/ f6 ]1 v% C 与门, 3 A" [; E. m7 Z. D1 h3 L- x& k7 N, ?0 L. K+ w# }) q/ k' `! S英汉对照民用航空词典B OEING ) n+ g2 X I, V8 K. Q) aTECHNICAL DICTIONARY 10+ J0 h& l4 j. \% u5 m ANEROID, A sealed flexible device containing air at low 3 s/ w2 {/ W& v) R% d; Tpressure, which expands or contracts during change of2 p W+ ]; S2 l& s! ]% k ressure outside the device. ! S7 `. L; ~0 ~7 G& ?7 Y( ~. Y3 C8 eically) Q5 j% e* J: X, ~% G N r changing the direction . ], B* ?3 \5 r: vf drive. / l) }7 ~- B5 W9 L7 t- W# B# Dof the wing chord in* \6 g* Y3 G G% C lation to the free stream airflow as it moves forward5 }% A, M+ f# |0 G2 y rough the air.$ Z& q, ^' q$ b2 C7 F al axis of the ' \$ @; c. I0 Taircraft. , s6 \8 E7 W6 |4 U. D* H胀或收缩。( |7 D" W& V t | Z' U 箱。是改变驱动方向的机械装置。 . Q: E" m4 d+ E7 C! h: L( D机翼翼弦在空气中向前运动时与自由气流之间的夹角。! u3 s! \. d8 N, C& _- r' N* [7 G M/ C# g; z p ( P; `1 M$ L$ i: ~1 D; J+ ?; nANGLE GEARBOX, A part of an engine, mechan . O& H/ [, l6 ]8 u& [# U$ r, xdriven by the compressor, which drives the accessory # { T3 V# |! L5 w$ e3 r: `gearbox. A mechanical device fo + G- q; A- L: S6 v3 x' qo7 t5 |( @* R: t4 n5 ]7 d+ V ANGLE OF ATTACK, The angle ' |% L; k: j8 [re0 g/ f* h* x* H; T! d5 C th, {- g& x2 H) w; A3 S; `- {& o ANGLE OF INCIDENCE, The acute angle which the ) ?& m& t7 Q) ]& `1 Mwing chord makes with the longitudin! R) o0 u; d. G* @: E 膜盒,8 I a" c5 k7 H 内含低压空气的密封弹性装置。当它周围的压力变化 1 L% P& g y5 E- H' O% {时,会膨 0 f# }% \5 j* j/ F+ B6 O伞齿轮箱,( T% M9 |$ a5 ?* ]4 ^5 ` 发动机的一部分。被压气机以机械方式驱动,然后驱动+ k* T3 O' f/ N1 ^ 附件齿轮) ] @, k$ P7 E+ j1 p* R( h 迎角,% f$ S3 Q/ r- |" M- ] 安装角,5 @! M$ ^$ f7 z$ V1 v% a 飞机的纵轴与机翼弦线所形成的锐角 . w0 M% Y+ K% v1 Y6 j E英汉对照民用航空词典B OEING; l* n/ E" m; j5 @. O8 o TECHNICAL DICTIONARY 11 ; y+ \! }1 q& I0 KANNUNCIATIONS, Audio or visual indications used to( |2 F$ q. q* k8 R3 @, w call attention to an event that has taken place. 1 m" t. X/ X- i7 t! x" [( XANNUNCIATOR, A visual device consisting of a number8 B* ~% M4 t" P2 H; c ly.$ L) ~ m/ v7 c/ g S0 u& ?9 r# R/ W1 ] ANODE, The element toward which the principal stream/ k8 p/ e" ^1 W" B of electrons flows. & S5 d, x9 X8 b' z7 s2 ~/ ^8 IANOMALY, Not normal. " b2 C( [9 j3 E2 f KANTENNA, A device which, used in conjunction with a % X7 v$ t! J6 N7 a( F7 a! otransmitter or receiver, is used for radiating or receiving3 ^/ u! N! ?, h& q7 ] radio waves. 1 Y: H( D5 M) q" ^: @NTI-ICING, A method of preventing ice formation on9 f9 a) M5 C: J M3 G$ Q) z0 S; J e wing leading edges and engine nacelles. \) m8 `$ l% MNTI-SKID, A system for providing maximum braking$ ]) ?2 u4 K2 ^; z* ?$ j5 C. d& V ithout skidding for any runway condition. Anti-skid! M( M8 | k# O omponents are part of the brake system. ( Y% ?9 O; h. ]6 W& @3 f告, ( o* L- Z! y! |7 F当发生事件时,以声音或目视指示形成的提示信号。 7 O. A2 D) O) }" p) n3 A- t与之有关的电路的现有情况或已存在的 : [. y& W. J" P: N! }! O: w2 |9 o6 N \+ y! u4 m) O, D 正极,% E* u8 E6 F J0 S3 Q2 Y 主电子流向的极位。 9 }" N! Y' B9 g* M异常,9 M. q6 Q! t$ R% h( G: G' F 不正常。 \# Z8 C1 m* m* n$ W 天线,/ S) \) j/ i% Q3 ~- [* _6 m 一种与发射机或接收机共同工作来发射或接收无线电 ; z, ?, v. e) z7 C波的装置。 ; k0 V" @4 \$ S! Q冰,; D4 A* T4 D( P# [5 k& R4 F/ ? O 防滑系统, " R U3 B2 a3 S9 _9 R0 }4 X& i* z一种在任何跑道状况下,都能提供最大的刹车能力而不 B% x+ V3 b9 i8 w5 @3 n2 p 使轮胎打滑的系统。防滑部件是刹车系统的一部分。 3 C$ H V3 a9 _! b4 _5 aof lights. Each light indicates the condition which exists 6 G( p; B& Q3 i" L$ |or has existed in an associated circuit and is labeled 6 q! }6 k) `: daccording ' L1 O# u, J( u+ T' i6 h* @A- g% |5 S$ j6 d th ! ~/ y7 U/ D4 t' J* x+ _( VA ) |9 _4 D6 u7 k! q9 F* Zw # H' B# l8 m" C; C7 i# ^c- @ M+ k& B7 n5 G' z3 k; j0 T+ J8 S 信号牌, * G. O6 k& [" K7 U/ M* T/ X由一系列指示灯组成的目视装置。每个指示灯都有相应9 g$ e Q1 j# c- ~) G! q5 S7 ^" \ 的标记,用来显示 8 O6 A$ Z& m$ s: q/ t2 Z# p0 @8 ^. a6 E+ v8 x. m7 n+ _/ s2 B& \' Q" j防止机翼前沿和发动机短舱结冰的一种方法。 , {0 _7 ?4 D$ O2 G2 u4 g' @& ]英汉对照民用航空词典B OEING 4 q _* l/ z7 R3 ATECHNICAL DICTIONARY 12 $ p W! Q B2 g5 [0 e/ L5 S7 zAPPENDIX, A supplement to the Airplane Flight Manual7 O9 _( E- Y3 b" X) e$ L tained in the basic manual. A) ]0 _7 i* `0 z; g, `- u9 G- o# @ ollection of supplementary material at the end of a! @- j$ z$ H" T: y1 h* K* O2 e ook.- D" m, w! _; T of the ^7 Q" u: u7 n5 x/ l rsion link on the landing gear. : A7 D. A! z7 Q. _2 NAPPROACH MODE, An autopilot/flight director mode" b7 m. v8 m8 U" K, p which is a combination of localizer for roll control and/ j) N, F, R4 q9 g3 s glide slope for pitch control. This mode is used when full 4 P9 n4 u6 t8 ]instrument landing system is available. ! E4 L5 R+ Y( [2 z# p1 T& j; i( GAPU, SEE - AUXILIARY POWER UNIT 7 k" W5 p* m( E5 N# E! QARINC, SEE - AERONAUTICAL RADIO / R, i$ ^6 Q9 YINCORPORATED. s5 E7 T. K1 M" I& R ARM, To make ready for operation./ E2 h% H* |- W. s' k9 u; w. C 附录, : m n9 Z8 F9 i9 w飞机飞行手册的附件,包含基本手册中未提到的飞机形& N; d: \$ D& @% P9 z7 m7 S 态的其他性能。是附在手册末的补充材料。! E( g$ [, y% T9 c 顶销, * Y) [" i' Y: p9 R$ ^2 e, k用于连接起落架扭力臂两部份的销子。1 [5 u4 l ] A4 s* J0 M- q 进近方式, ; v8 q8 \: {) q+ t6 O/ I2 _一种综合了控制横侧的航道信号和控制俯仰下滑信号 : _; P4 y Q9 T0 Z X' _; o# X N; ]的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系 7 }1 R2 s4 I+ u* b5 p+ r. O+ R) Z统正常时才使用。 " e* {5 a9 a o& d' }) `9 J辅助动力装置,, p. s- b9 c1 ]% R" I3 j. R( K d 见Auxiliary Power Unit 2 x9 z; l, a/ w* k5 i( M' f/ Wcontaining additional performance for aircraft$ v$ ^. X" I3 a6 ~ configurations not con- y2 B0 @1 y, n6 W9 X2 D3 {8 S6 b c; s. C8 P- m7 ] b9 H- `5 t8 |9 J# p6 }3 n APEX PIN, A pin for joining the two sections& u: M8 g) C5 ]/ T# M& w to' l6 {% X+ X# t6 D: I, Y6 j* r6 ~' S) }5 G& | 航空无线电公司, 6 Z' f1 J1 T0 |( K- k7 T; F见Aeronautical Radio Incorporated.3 }0 v6 p( j; ?( S/ y7 Q, f1 B 预位,' K6 j( M, X" ?6 u 部件可以开始工作的状态。# a5 J6 l' E& ?: l5 x6 h6 k2 M- T 英汉对照民用航空词典B OEING " a5 x6 r* M& F: qTECHNICAL DICTIONARY 13. @9 C; B5 w9 b( r G ARC, The curved track over the ground of an aircraft ) \7 A0 u( P% c4 B! d! `' Qflying at a constant distance from a measuring5 b$ g% [& c0 v6 ~+ q* Z6 M equipment (DME). - G: k0 K$ B0 c1 P. _( E9 Fin the limits of self-contained system 1 s7 X, a% x P% z4 X9 [% `! kapability. % I6 j% b/ W7 w6 G$ ttem for opposing or restricting 1 R4 t9 f0 U0 `+ N2 o! h6 }ovement. 9 c h1 \0 r6 c0 O- NSPIRATED TAT PROBE, A sensor that measures total8 P T( j& n' d1 Y( y( B# z ir temperature when the airplane is in the air and that: |& D7 J& F" s' ]# S5 E easures outside air temperature when the airplane is( k& Z) ?6 s& b( c- J } n the ground. The outside air temperature is measured 5 b. G0 i% |' K G' W6 T& Z" K5 |SSEMBLY, The fitting together of a complete structure 1 z- e5 C& m$ k' M: b, b, h- `3 W3 g0 [SSUMED TEMPERATURE REDUCED THRUST, The 9 D6 d( s! D$ ] B/ `' }6 f( WATC, SEE - AIR TRAFFIC CONTROL u4 Q, Q p6 F( S, \7 u. S( q/ Q2 G `: j( K* s7 ?/ U9 `4 C 系统中所产生的一种用以抗拒( M. w0 E0 c/ y+ ~# q 作或限制动作的力。- H) s4 d8 J' W/ z8 Y3 L 头, C: k; J& m( m- u7 }1 B3 M用来测量飞机在空中时的总大气温度和在地面时的外6 \; N2 U$ z2 G# [/ S& ] 温度。地面外界温度的测量是利用引气将外界空气吸入 8 m( r- W1 X# n: s: O, Y9 Z/ g头,以达到测量的目的。 4 k& ]( I6 }: A5 L' u* F配, : O. R( v' _7 K0 d% B) k: K$ u一个完整的结构或组件的过程。 4 }9 i% Y1 K$ }# o! ]' E假设温度而得的减推力,4 @/ c1 l: ]& N2 B5 v4 b 推力设定值时,假定一个比实际外界空气温 ( E& z2 S. `3 E e空中交通管制, , b0 u1 b) W5 r$ j( Z% _6 G见Air Traffic Control; y; z- @' c, G/ [' y+ `" B AREA NAVIGATION/RNAV, A method of navigation 2 k2 m: _+ W, K) J+ E- k$ {& othat permits aircraft operations on any desired course 2 ]0 L( p, G! S5 n. _. Wwithin the coverage of station-referenced navigation 2 I7 A4 S$ |4 ?5 ]# t, Esignals or with }% c* a& B/ }: X, H! uc+ Q3 F3 F& f& q. F1 R0 b# R ARTIFICIAL FEEL, A force developed in the flight U. k7 L5 x) Ycontrol or brake sys $ e4 |, j. }" |( x- M1 `9 p y1 ym 4 t3 h) B0 m/ x3 o9 S& t+ hA5 G- l! A/ R' S a4 Z0 m1 f$ ]7 F* G# b m+ n* J6 p" E% W+ \0 X+ H; L o7 ~, ~* I1 \) Q# t/ W: G, G3 n0 Y by using bleed air to draw ambient air through the / f/ f/ i. }4 ?0 Msensor when the airplane is not moving.; O( r( K1 ?- L$ l2 W' W% F0 u A & l' I7 Q$ x" y/ L: O0 m0 B5 ?* S- hor unit." |$ I% J; N: k A * @/ v/ N+ w& y5 _; x- r- ilower thrust obtained by setting a higher than actual 1 Q; C: M7 ?/ a) y1 q* rOutside Air Temperature (OAT).* q% V: O4 c" R; w8 t, H {# m% P$ l 弧线,8 R4 r% k2 }9 q' R 飞机在围绕DME台等距飞行时的弧形航迹。! a/ r1 j9 s- Z( c* P 区域导航,1 `% Z2 x) Y, b$ d. k" Z4 S 容许飞机飞行在有电台参考的导航信号或自备系统能3 P2 h4 K9 E& k( T 力极限范围内,飞行任何预定航线的一种导航方法。 : W3 O# D# v6 N$ l& L. @ J模拟感觉1 W" A9 h. r5 D9 F, ~7 h 在飞行操纵系统或刹车- ~0 f; |. W! O! a# q0 O$ Y0 f! f" n/ K4 Z吸气式总温探7 v) K m W9 D5 U0 l* S4 O$ Z/ K$ |' j, ^% |7 b7 p H; N. \$ M& s* ]5 u- S( d' v. Z0 W2 V8 H: M' i2 m% l$ n2 J 组合成 7 P- B$ `2 w4 ~6 d$ `# K6 @; {( {6 g ~% v4 f @在选择起飞 . m+ g8 i3 b+ X' w' M2 s+ v度高的温度而得到的推力。用这种方法可以减少发动机的 7 c5 D9 O) c& D; h$ G磨损和维护费用。& f- s; h U; l0 Z. H0 S4 I c/ c# {0 a* F3 s6 s$ {% y 英汉对照民用航空词典B OEING0 b8 v/ \! c. g/ h TECHNICAL DICTIONARY 14 # a6 L5 w3 d$ G) g0 eATE, SEE - AUTOMATIC TEST EQUIPMENT. [- _' b4 w$ N$ W ATMOSPHERIC PRESSURE, Pressure of air due to the 4 |3 f; L3 I+ r: X; oarth's atmosphere, expressed in pounds per square# U* W2 Q" S0 _- J0 A$ m7 q4 R6 f ch (psi) or inches of mercury (in Hg) or millibars (mB). 7 Y9 K$ {* J, Q" s1 N% N' CTTITUDE, The relative orientation of the airplane with ' I6 O3 g9 I" N) r" L( Q6 ispect to pitch, roll, and yaw.3 b5 O5 z' E7 }, J q UDIO CONTROUSELECTOR PANEL, The panel in 9 }5 Q! @" Q8 [; Z+ O! w" de airplane which controls and selects the routing of 5 f8 C ?3 f/ V/ `3 Xudio.# M0 z; A2 \8 c2 s$ r' T9 b# p! ^ UTOLAND, Automatic landing using the Digital Flight : E! C6 k! f4 P0 M0 W3 R, oontrol System. ' F9 ~4 W: P& |" C% sn. 6 y8 a. h2 S& k: K0 g2 mM, A system ; {# [& n- v; ?5 A+ e3 Y7 [% T/ zomposed of all necessary subsystems needed to guide 4 w' u9 I2 M0 C8 a4 E7 B5 l Ue flight of an airplane.5 q( B6 c4 n4 M EQUIPMENT, System test 0 h( S: v6 m. F# Y u! r, Vquipment that operates under computer control. * r. r( w. r/ d: M7 r装置,

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e - ?$ W. k3 ^. V7 ein ( \5 M$ O, X& |9 I* xA - e3 w( o& ~7 f) f) k ]re6 s$ V2 P* o. f7 }) D* u2 M2 z7 M A$ n3 ~7 o. W! g, m' F+ R* Y. D th+ m' Q7 E2 L, J a% l' M- k8 `; \* P& i$ @* { A 2 A y2 t# i4 K7 O5 dC 7 z- U& r7 e& wAUTOMATIC DIRECTION FINDER, A system which/ d' o5 r5 D+ c! j9 m" w% G4 l0 x6 m determines the direction of a radio statio. ]8 k! P" W& w5 T2 u& n% t AUTOMATIC FLIGHT CONTROL SYSTE 5 j3 p2 q6 L0 e% p$ A+ xc $ L. H" D ^& eth 4 e$ n! i! P) B4 b, CAUTOMATIC TEST/ W! Z( v. I, Y$ t8 [0 I! ] e 9 G* d( Y/ J5 d; K5 L自动测试 5 ]/ D: ?6 M; @9 I0 D0 E见Automatic Test Equipment.2 s- O1 a5 W& O5 [7 D' P 大气压力, 5 T8 c: B7 U" |6 m) K; J( f, e由于地球周围的大气而产生的空气压力,以每平方寸多3 b) Q2 n: i: w) K) G) k* V 磅(psi)或多少寸高水银柱(in Hg)或毫巴(mB)来 ! O7 o$ e; H, H u0 g示。 l9 _# P$ F1 d. x" Z, t 飞机姿态, ' w% U/ a2 J4 O8 P; i' O N飞机与俯仰,坡度,和偏航有关的相对方向。 1 f I( Y3 V7 L; f9 k( o% Q7 H9 _音频选择面板,- S: n& f7 D- v2 H! [* r 飞机内用来控制和选择音频通路的面板。+ [3 F* }5 N1 V1 i 自动着陆,7 V8 e l/ a& t, V 使用数字式飞行操作系统来进行自动着陆。+ u2 Q) G1 Q3 u% `; Z/ U2 n( D 的系统。+ |* Q$ k N. ]+ ?2 w- g |; C4 }* r5 q6 X系统所组成的一个系统。" P2 u }8 f( K( T6 x6 d: t+ x 在计算机控制下运作的系统测试装置。 4 A; i \8 h; s# Q% K T$ D; J+ K2 j- m$ k& E! k l1 K自动定向仪(ADF), ! U* [3 M+ p' x1 d) G& _确定无线电台方向 : c3 K+ k6 x; _* A$ U3 n自动飞行控制系统 8 O& ~* L' q. k! k由所有能引导飞机飞行的子 , [$ I) h' i- S0 t2 H! {& Q自动测试装置, - h# O2 D# u% a* B3 n0 ^# A! z% _& y英汉对照民用航空词典B OEING. ?# b2 i% Q" Q5 M2 C: x1 w TECHNICAL DICTIONARY 15! o7 S1 w5 a+ ~2 l% l, n* X AUTOPILOT, A system which automatically controls 4 Q% u/ J* }3 U" E( j" {( rand guides the flight of an airplane. . e6 S/ K5 ]0 P' `. S R* QAUTOPILOT FLIGHT DIRECTOR SYSTEM, An 0 ~7 @" ~) f# t8 H2 {) Otor + y" f; _) w3 u: wUTOTHROTTLE, A system which automatically Z% [& ?: o4 B3 `6 @ontrols the throttles of an airplane.& r: t& ?2 p' b% g POWER UNIT, A small turbine engine in2 O4 I! T; c `+ u e airplane for supplying electrical and pneumatic ' y/ M8 O* v& Q2 E4 bower for systems operation on the ground or in flight. 4 g$ \ r! S& QVM, SEE - AIRBORNE VIBRATION MONITOR 8 f5 y B' p* ~1 lXIAL FLOW COMPRESSOR, A type of compressor; I: _9 p+ V5 q# S/ u sed in a gas turbine engine in which air passes through Q7 Z; i1 C) y- p) O XIS, An imaginary straight line or an actual physical . Q2 a7 a4 i( ^6 p9 C: komponent (such as an axle) around which a body can$ F: U; p+ y( g9 t+ A3 A1 k tate.' Y! {; M2 t8 s+ y 仪, # z/ Y" ?$ |/ B( i9 o+ {% C9 W0 g" g/ B* A4 h自动驾驶飞行指引系统,: N( A* W% e9 b; j5 e. k 动驾驶和飞行指引功能的系统。3 T7 H/ t+ I( K& Y/ N l 动油门, 0 w& A# e* N! W- r: T# m自动控制飞机油门的系统。. H* Y* U# K" ^, _5 E( s 是飞机内的小涡轮发动机,在地面或空中给各系统提供 ; W" b! @( D" L& |源和气源。* Y( j- K- E x9 O- s& V 称。 - S) B5 H5 ?. J6 ]8 s. O( B载振动监视器, # K7 ~1 l7 M/ \. d- Y8 s4 F* g5 t见Airborne Vibration Monitor ( {) Z6 M ~9 D, n+ d" fintegrated system containing autopilot and flight direc I U( d) [8 F functions.: ]2 M7 d9 K# _* F( G8 L* \ A & D+ w& y: @: O4 {c & r3 q5 }7 I! @- uAUXILIARY$ Y" e( B" d; y, V/ }. T1 D th # x# x, l3 e( k! p# Z e& o, f- R! ]p6 m5 H' M/ X5 Z# f, w9 [- a AVIONICS, An acronym designating the field of aviation# m4 t) r+ w( Q; C$ ^3 _ electronics.* w- D3 s8 F' ~ q6 [; E' l( ~! a A! e% ~) B- {% L: l3 o j) k A- L# B: ~& ?4 o; h u% |9 S$ n6 U% x5 A# t. C- M' j the compressor in a straight flow, front to rear., U$ B9 x+ r, r$ L* c7 d7 ` A% M6 l1 a- W/ b: a8 i" X2 w. Q c& o9 b/ s% ?8 a ro 2 b$ f0 y& h& G% t" G5 _6 U. e+ M自动驾驶( P1 }1 [; T/ I# N$ X/ l" y+ ] 动操纵和引导飞机飞行的系统。 ! s) k# c. |3 X! e& u0 }0 r1 k一个综合自 / m. z- i- e. c9 M- P2 w5 G1 ~" P6 \* F' Z' N5 G A/ v辅助动力装置,6 K) P" H; j! D& b0 O; v8 R8 K6 U- r 航空电子学, \ a+ |5 `0 o4 M$ ?: R是航空电子领域的一特有名! `. q' E9 z! B O- Z7 A8 i( U$ A, ?1 v, ^2 t( p* M8 d$ e( b7 p$ F, Z2 O1 J% B流压缩机, 3 L) U* q& J# h: _& Q4 Z& M一种用于燃气涡轮发动机内的压气机。空气由发动机的3 |+ u2 B9 Y, L- d. D5 D9 p' U g6 Q1 d 部流出。 2 ^- o, s! G+ t# F' l线,/ d/ u |, ~% s7 N8 ?/ ^ 可让物体围绕着作旋转运动的一个想像的直线或实际0 i- o+ B2 U- J1 ?1 A' k 在的部件(如轴)。) s- H/ }0 v2 E0 b+ w" n! I/ C3 ?! v: x2 t前部轴向流人,压缩后,由后% Y& g: S8 u* } K6 I( _& ^* d7 A+ i; ^% ^5 N9 B3 T) j" I- m3 d4 q 英汉对照民用航空词典B OEING7 B3 o+ F/ c5 {6 s9 P TECHNICAL DICTIONARY 16# N) r' |# w( F( u B ! T: Z" H5 k; S0 ?8 D' _( G9 C2 sACKCOURSE APPROACH, An approach to a runway ( H, N% P3 r& Z4 Iversed., [, ~% N) r) g0 X. n own on the EFIS that$ O4 D4 H, i e' B oes not readily change, for example, navigational aids.9 ~* E: z7 w$ F$ X; G vement in the tank or reservoir.$ f: J( [$ | V1 K9 ] c ALANCE TAB, A small hinged moveable part on the5 m( J1 f g/ S2 D, p6 v ailing edge of a control surface (aileron, elevator, , Y. \. a7 X' E @1 j航道进近, * C x" H$ x# z s* j" e相反的进近方向。当反航道进近时,无下滑- j7 k( l7 ^; D9 g! B8 h$ a 显示在电子飞行仪表系统上不经常改变的数据。例如: 7 n. i# Y* L+ Y) W航设备。 ) u) n3 b2 ?* L在燃油箱或滑油箱内阻止液体流动的隔板。% O( I$ K: Y3 J: ~9 W 动补偿片, * ~# m4 V0 R7 T# j6 ]) T7 N+ R铰接在操纵面后缘(副翼,方向舵,升降舵)的可动部。 6 t6 m, z* H: _与操纵面相反,以帮助操纵面运 8 h2 @& k4 n7 Z8 g+ sB " D# f) N* W& F" s: J. m) T7 Dwhich is opposite the normal approach. For a2 \3 [7 C( y! B6 u backcourse approach, glide slope signals are not / \( d) M z8 k+ i2 b8 r9 `- navailable and the sense of localizer signals must be7 `9 _5 \; C0 \ re % Y( ~9 B3 w: |( GBACKGROUND DATA, Data sh & Y" p& l8 O3 q- _. ?d$ S; Q% h* Z" p) {+ W' w BAFFLE, A partition in a tank or reservoir to prevent , R! I2 m+ o% U4 N$ w/ c8 d7 J5 qfluid mo |3 q3 [+ V$ uB1 {7 j9 d. B7 V0 o3 F, F" @ tr9 \9 `* ^, `5 B2 ]8 j rudder).The tab moves in an opposite direction to the5 A( I# U1 V% K! ` control surface for assisting movement of the control6 A% Q0 Z8 F6 D: @& T surface.# h7 v3 U% E) d% U; T6 @ q7 H( p E2 M% N: b- A与正常进近 6 a( B" Y# A9 y6 L( g k. f道信号并且航道信号也必须逆反。 1 l$ g8 c3 P0 w d+ [背景数据,1 F; G6 J( @7 r |$ `# ^: D5 j# ^ m5 @6 V) C2 n O缓冲隔板, ) h7 V6 ?+ V- P0 {6 u+ u$ P( R6 o$ q 随动补偿片的动作方向 . p! p7 X3 N2 U% }7 G动,减小操纵力。8 c/ I! t/ W4 V% o t, T8 ? 英汉对照民用航空词典B OEING - F4 P- x: U% V7 @' pTECHNICAL DICTIONARY 17) _5 y0 t- x! m5 c" i' l6 G BALANCED FIELD LENGTH, The field length: ^" O7 L& q5 b; }& M1 h associated with optimum aircraft performance when V+ h! c/ j2 n: gbstacles are not a constraint. In this case, after engine + N+ x7 w% e- h- z, K" t; wilure at V1, the distance required to accelerate, takeoff : Z, r1 Q& b0 j- l# Dnd reach a height of 35 feet is equal to the distance1 X* g/ W. c8 C4 J6 s6 a ALLAST, A weight installed in an aircraft to maintain5 ?1 V; u* {$ V" Q8 Y ALL NUT, A fixed spherical nut driven by the& A# t* ^ ~1 u7 E* e8 ~) S6 c AR OUT OF VIEW, A signal used to remove the flight* t# X8 e) m4 e- P" t AROMETRIC PRESSURE, The pressure of air above # Y, y0 S7 ?2 O S! F' E9 Yg) or E/ x, q3 j. }3 zmillibars (MB).* E3 Y& S. K# T* ~ ATTERY, An electrical device for changing stored) N! C8 \8 g" |' {4 k/ A- v5 B 性能的场长。在此 8 y( s0 w8 j+ y5 T& ~% W- Y况下,V1时发动机故障,要完成加速、起飞、离地35) v! v+ F) R. z. g7 b0 C; O! ~+ \# B4 A- K 尺所需距离等于相同速度下完成全停所需的距离。 1 N$ b1 j2 b1 _4 H. e8 z& Y, z舱物,- n, k! @2 ]& L3 V1 c 重心在许可范围内面装载的配重物。* e* m$ ?3 [1 Q, ^' E5 ` 形螺母,+ Y! E8 P N$ B% n4 D' p$ ], s 的固定的球形螺母,用以使襟翼和水平 ( D% g5 x8 N4 o, l. C0 n引杆消失, / k1 M3 s3 {2 G/ a3 Z& ^4 M, R6 r指引杆的信号。 8 o$ X8 O/ m4 l# y, L压,, d3 ]- m3 ]5 D4 q 压力。通常以多少寸高水银柱(in h6 X8 c) H4 S% l瓶, F+ H- L3 G" @3 h1 r% q9 I的化学能转变为直流电的电气装置。: f" ]/ ]/ J: m5 y o 5 p5 |7 s, u- r8 f: u# k5 ~# Q) Ffa9 x* y* D7 a7 i/ W a ^9 G' _+ r, w+ S1 n# K0 q$ wrequired to stop from the same speed.) w! ]. X4 Z, I1 l) d B 4 a- E; z* m7 _- Sthe center of gravity within allowable limits.: y7 x* ?! J5 i/ H4 _; x B/ |: P1 s! ]% \- H' A jackscrew for flap and stabilizer movement. " I: `. P* I1 I \1 O( [, m" LB: W% a+ q4 \3 z9 Q director command bar(s).( a8 W1 _$ x0 S# l/ j3 j y B ' s6 ]4 u0 r5 mzero pressure measured in inches of mercury (in H + W& ?& i7 z1 i1 e9 ain " e% v) ?$ ?1 A0 W4 SBASE METAL, The underlining metal to which alloying * K$ d- w8 }- J' Iagents or metals are added.! Y' I2 c( u9 D: [0 r% a B , H: q( T; v5 bchemical energy into direct electric current. ; W7 j: U3 }; a- [5 @平衡场长, ; x* r; K* ]& N0 d! K当障碍物非限制因素使飞机达到最佳2 S3 w: B8 g8 L3 Q$ T: q# r" i( f" J5 s0 ` k! \7 o, A' q( b* F$ G) Q. |" ?, E/ \$ m, k) d4 F& l3 U8 G 为保持飞机 2 l5 h5 b7 {4 d8 f. `* |5 }& F( O# n! [9 ~: d由粗重螺杆驱动3 k. n1 L. a2 T' h 安定面运动。) @5 F' m7 O5 ~! W6 J# i" y7 Y8 J# \) w o+ d' _$ `2 p用于除去飞行 % A+ a2 l6 e7 f1 b" U$ z2 z' t4 d; v$ `2 q# m零压力以上的空气# t: Q/ |2 O0 i/ R/ | Hg)或毫巴(MB)来表示。 2 U' ]& |! L" L7 a基底金属, 5 {# m/ O$ i7 J3 V指合金中的主要金属成份。 ! z, E8 T( u. K$ f" w1 i. w5 E( X. D# l! j. F 将储蓄 * O; y- ~7 J1 _4 ?8 H英汉对照民用航空词典B OEING0 F6 J& y- [$ S* Y% }# w TECHNICAL DICTIONARY 18 % y) d' I- w- \" f' hBATTER F/ g3 e. [7 K1 z% Qdirect cu - j" | n9 ~8 T# l c" |/ X! Ipower su ; Y c1 }! t6 C/ d( ?6 j2 ]' SY BUS, An electrical conductor supplied with 2 I0 A$ ?4 k; ~2 v5 `7 Qrrent from the battery or transformer-rectifier for 9 l3 c3 j& C/ F4 i. z, Ypply to operating components. , m* D5 Q7 x" U# v0 HCHARGER, An electrical device supplied3 F; f) a1 c' C ith alternating current, which produces a direct current 2 j/ S% Q8 j/ s8 yutput for charging the battery on the airplane.2 k4 K9 g+ Y. e* G$ A% U/ a" M AY, A compartment in the airplane structure. 8 C+ S0 z' } g+ t) Q: ~CD, SEE - BINARY CODED DECIMAL ! j4 X0 j% I0 y' d" C' [EACON, A device which emits a signal for use as a % i1 R7 `/ `9 C2 o1 u1 _2 x( D P' z' Kuidance or warning aid. % b# o9 c2 y& T5 u8 a5 p5 L& tBEARING (NO. 2), The direction from an airplane to a 0 j9 F1 P1 j# {% b) J7 _" x6 gground station.8 w" P) d: n4 S; e8 E3 V) E 瓶汇流条, % q. v$ h# p* ]% s5 M将从电瓶或变压整流器来的直流电供给工作部件的导5 }: l* R. J* r# c. Q 体。4 s/ P# |* A7 I( U$ r/ J 瓶充电器, 8 x; A. D @7 X用交流电向飞机内电瓶充电的电气装置。带有交流电的 & y1 V; g- P2 U7 b6 S ?5 D$ ^气装置,该装置产生直流电向飞机上的电瓶充电。3 g+ w( c5 W( h% Z3 f3 x8 X 舱,& Z- d3 g4 E8 H 飞机结构中分隔的空间。 7 N" J$ t/ T9 w2 z! H* N二进制编码, * V3 h# |5 A8 A c+ r见Binary Coded Decimal1 k+ n9 L- p- l6 D0 o% P1 _: L BATTERY . t1 h, j. Q5 T; w& C1 a. I5 yw / [9 M2 U% } b0 ko 5 D6 a9 S# D$ J l% e6 s' ~+ E9 N5 [B & |/ s) T1 E# N. V2 I- IB : v9 [5 C- Y# X& IB , p! _& @9 C, a: U' B' X9 F6 N/ I. `g / z! D9 f4 _# r. ~, L$ WBEARING (NO. 1), A surface that supports a moving 4 K/ \5 n( ~+ ipart and reduces friction between the two., h9 ~) S. P9 F2 `: l' d5 _) U! W' t: R+ k& T" D4 `/ r# n: w- R! l: w" j- `8 W" W* i: |9 o9 Q* M6 X7 J* x7 k5 m6 Z& Z: Y8 R1 D" J+ Y6 f/ C, U: Y- R" u5 i& i 信标,9 V* @! M; [% f* W 发射引导或警告用信号的装置。 3 h4 F; K9 U l方位(NO.2), 5 V7 ]* f% Z* z) h/ {$ d从一架飞机到地面台的方向。# D/ B, Y) o `7 n9 p 轴承(NO.1),4 h' Q0 _7 J) @1 W& [! f$ o 用于减轻机械转动磨擦的机械装置。 ; [. o7 [6 G) s3 K& G4 \6 `英汉对照民用航空词典B OEING/ u4 @+ A+ J$ k TECHNICAL DICTIONARY 19 3 t; y5 Z2 s8 W; XBELLCRANK, A double lever in the control syst. q1 T0 \* A& A. I9 C; M changing direction of motion.* \) f P- W: ?4 {- U& x8 E em for/ _7 t( t8 m% H7 p S0 ^ ct in the ! y2 `8 N+ W: d5 n6 i& Pneumatic system for absorbing expansion of duct due / m7 f: |) A9 A$ C) M& wheat.6 _; L% Q8 _' S1 R ELLOWS (NO. 2), Corrugated folded or pleated9 i8 B1 D' e- e U9 u4 j! \ ontainer or compartment used to measure pressure.1 K2 Y% B c2 M EZEL, The part of an instrument case for locking the - h* v4 G$ J4 x) nlass. ! b3 ?6 u4 e9 [* I+ T$ XIAS, The potential difference applied between two; i4 Q4 W: w6 a; a oints for controlling a circuit." ]& {# B% [4 m3 Z/ {6 {- { BILGE, The lowest part of an aircraft fuselage. A place8 X% w/ W& z% d0 s0 R- O% W where water, dirt and other contaminants collect. 3 o4 e9 K0 c9 k气源系统内提供管道热胀冷缩所需要的余地的波状 2 v; }# v% _( l; n/ a轫管。 6 I C# p: q! l; f+ U! p空膜盒, 9 Z( E1 F ]) h! q* P, Z! M一种具有波状表面的容器。用于量测气压。 - t6 g9 m# L, o; K0 E+ P4 x嵌沟缘, . m9 w r" ]" v% ]! n将表面玻璃固定在仪表上的圈状零件。 $ T% u+ a4 w0 {" [压, ( `4 Q& f0 `* e/ b- \6 _ O在控制电路的两点之间的电位差。4 r, s# N$ g& q! d {5 I! q 机身腹部, , ~2 F+ A7 \6 q2 ~, M机身的最底部,通常水,脏物,和其他外来物集存于此。' w) a! l7 k8 N9 J1 J4 v# B BELLOWS (NO. 1), A corrugated flexible du 4 _ e3 S2 H( } k3 F; tp % x3 F9 I6 O5 I0 G; ^) Bto9 v9 w4 Q' T/ K6 o, q' \ B & z% X |8 ^7 t- I% o- Lc 0 {' D+ }4 c9 [* U' zB, z! E/ l8 D4 q$ T g* L* y3 f+ J' J- y B 4 x+ t+ f7 c( F9 @4 \) w8 k- }p9 }) Z3 ?/ ]) S6 L; d 直角摇臂, 3 }5 D; l' O* \% y1 H在操纵系统中改变运动方向用的双臂摇臂。; R5 R# U) S3 z5 I4 Z 波纹管, - c, I# \7 F' W+ F# n( g9 m$ _; m2 |% Q) x2 l; r2 B% c3 W, F( v1 Y' v4 e% \7 N. Z% F2 ]# x7 p0 E5 w2 H; Z$ o+ |" l# H# s* L m+ f# m4 N3 e英汉对照民用航空词典B OEING + Q' O( N7 Z* u" ?TECHNICAL DICTIONARY 20 : o$ ?+ q) Y$ ^( {+ f7 n9 JBINARY CODED DECIMAL, A system of coding each ; t x E- v1 x T# M5 v. o9 {7 I Hdigit in a decimal number using the binary equivalent. 1 U! B8 P( B# s/ ? G- SBINARY NUMBER SYSTEM, A number system using / {2 y8 O& ]- ?2 D: C3 b( M9 U% fs1 j @. N8 i: d. ?- f4 Q; m4 A IT, In the binary number system, the smallest unit of* I2 j: @/ A& w: b formation, consisting of a 0 or a 1./ o" ~9 I2 {0 ] ITE, SEE - BUILT-IN TEST EQUIPMENT 1 ]9 I& P; @- T7 u$ P! R( LLANK DISPLAY, A display that does not have any3 g5 @: ]* l, N+ W# S/ f2 u dications, normally due to failure.4 n( ]7 [1 B [8 G9 B& Q3 i4 e LACK BOX, A container for electronic circuits to record% M) ?9 M E1 ]0 H ight data.3 K6 {. w/ ]9 p5 @ LEED AIR, Air taken from the engine to power various ) u7 H9 c2 i0 i9 r% y+ kircraft accessories.7 R5 ]/ w8 D$ l: J" v6 b; U" J A valve in the pneumatic system for air' R6 t) g5 a! ~. } supply from the engine or auxiliary power unit to the 1 M) [' @; m) D( w# B+ \" xpneumatic manifold. A valve on the engine for reducing K! [# G4 B* _2 g7 i5 P2 k+ d" a pressure in the compressor section. . ^; W5 r! [, H* E0 z进制,- T* c2 [5 m3 K% J4 E* V. k 进制,1 _. c! k) [% Z6 X F/ v 一般用0和1)和2为底的数字系统。 4 R( ?( j# n7 R0 l2 V6 r特(二进位数), - e# |2 k$ V8 q* W5 v二进制中的最小信息单位,包括0或1。 Q f3 H! [6 w内自测系统,0 `2 o8 g6 P, z* r W 见Built-in Test Equipment y: F$ L0 F6 V C; Ktwo symbols (usually denoted 0 and 1) and having 2 a0 k$ f8 }! V r/ ?8 S( ~5 P its base. " T( }& x) L; q0 y! x' cB + s# z7 |+ S& G' _7 i7 X/ s$ `6 sin" y+ G. n( h- @) z7 R) ]' ?' v( j( Q B % G& W( K9 f' x) OB 0 I) o! e. W# W6 M; U$ gin 7 _- N3 L7 e- V& _B ( m- N2 v8 j- }fl* y$ Q7 r6 W' G B. @" l' J- t. b& ] a% @3 A+ K- T$ H; J; s5 i: V$ m* E# s BLEED VALVE, , H3 S' \3 K& d; H5 T2 p" Q二进制编码的十 0 x2 [7 X; N9 l7 R一种编码系统。用等效二进制位数编译十进位数的每一 5 I- v1 `9 q. W# l# L; P位。 % L( H: Q. I' M! E; f w' e/ ]$ F' ]6 S( Z以两个符号( 4 `6 c5 `: r1 T! D% s7 W2 v$ ?8 y: Q! p, ^) x: |. v& S3 d2 E- s* E0 {2 a ., }4 q; @. G2 q8 e6 T) s 白显示,% w0 b- g+ i K, v4 }4 H* n5 w7 K 通常因故障而造成的显示器上没有任何指示。 % _$ N& a1 k0 U( l* G0 d匣子, 5 @6 B4 V3 y# `( o- Z! [装有用于记录飞行数据的电路系统的容器。 8 `( U) s5 O7 }, Z1 b气,' Z+ M5 M6 K0 j) I% v; } 取自发动机而用以驱动飞机上之各种附件的空气。3 a% S( ]- [+ o$ G6 b4 [% B2 x2 B+ \ 气源系统内,使来自发动机或辅助动力装置的空气进人 5 }" U, Z0 A7 o8 T8 M- A' P! R8 P气源支管的活门。发动机上,用来降低压气机压力的活门。' i" [+ G! w* W# d5 n/ Y6 J7 ^( W, h: U+ g" ?. u0 `/ @; l( T! X0 `& i7 o K0 a; M9 U2 \ 引气活门, ; [0 ~7 K( M! f% Y/ [: ^英汉对照民用航空词典B OEING- ]: s0 k& \, _! J TECHNICAL DICTIONARY 21 7 z# ~; l& o9 \' E9 L8 _* A/ b! GBLOCKER DOOR, A device on the engine for blocking/ E0 m$ p9 M! q" o& J) t6 F the normal airflow during thrust reverser operation.$ x! c+ Y! Y3 I8 ]' b# Q' w& h0 d LOWER, An electrically operated fan for circulating air. 5 n! J) B" V$ a% l; gLOWOUT PANEL, A panel in the structure between0 o+ F" s8 g P/ W3 S x o compartments that opens to equalize pressure in7 a+ m) n9 Q) @# [1 f- Q1 x e compartments." Q; m- y2 J/ b2 r2 K/ v ODY GEAR, The landing gear attached to the 9 D% g, S$ J) J, B& D# Ugrounding. " D3 d0 K/ |4 W3 l正常的" K( V7 ]: |" h& l! t! Y9 x9 h 气流。3 h ^8 ]# ]$ v; c* c; Z 鼓风机, " Z- U5 N. v/ z3 K用来使空气循环的电动风扇。 ) ]) a! o5 y8 y! H5 I压口盖, 8 U0 D/ L: L) M3 W3 c两个隔舱之间的口盖,打开后可使两舱压力相等。 ; k. T: v, X& F- Z/ b. r身起落架, 5 e1 h+ x& l' S& I! h' h8 Z身构架上的起落架。 $ X( g8 G5 }: w. OB \+ p+ @+ O+ n0 \4 V# X6 K0 C1 iB, z2 c9 f5 m, D: O9 f4 Q tw " d' H, K" ~$ Z$ i) Cth! D( T" W" I, T4 A1 U4 x B+ U B 4 }2 W# ^" F. Z7 O; w5 P. H% e( Zfuselage structure. / a0 t' N4 f" G h! NBONDING JUMPER, An electrical connection between & Z' u* K7 K6 ba component and airplane structure for electrical " R% a+ ^$ k- w1 x8 D阻流门,; z4 _ t- v2 p" Y2 U4 v5 J 发动机上的一个装置。在反推工作时用于阻挡, D7 s( n: ?2 r3 y: V) H* K) v+ B- [7 ?1 \/ D F" D3 F, t+ S/ H- n 装在机 : Z9 B, J, }7 v2 V9 E& G搭接片,+ H. k( ]& s3 m 连接某个部件与飞机结构以形成接地的电接头。 l+ F) B2 s, r: N3 S- j英汉对照民用航空词典B OEING $ ^/ _9 Y" h" u/ f4 fTECHNICAL DICTIONARY 22, {+ `8 L9 |* y& {8 @" j, y# W6 B BOOLEAN ALGEBRA, A mathematical system for 0 E; B4 \6 H3 R: D% {. u |! swriting combinations of logical statements.' W* o$ q3 g* L BOOST PUMP, An electrically operated fuel pump for' I, @# G$ u- S5 u fuel supply from the airplane fuel tank to the fuel * y7 N& U% g, T7 ^9 k9 B$ A1 Vmanifold. $ C7 d: x2 ^/ PBORESCOPE, An electro-optical device for looking at/ P9 L; y6 I7 C1 U3 ~3 _ ternal parts of an engine through holes in the engine., ?' @ y; i# a orescope ports) % h k, L; O4 {3 U# cOURDON TUBE, A curved flat tube in a pressure gage% y- J7 J) k+ o% d# r# e: b r moving the pointer when pressure changes inside S9 |, i; \6 P! Z& y; j* gon the ability of the brakes to$ y* U1 F" h- r9 O# J& x bsorb a predetermined amount of energy during a2 n0 `( B% o Q& F) H jected takeoff. - }0 h. J& F$ ~6 A* d( A9 G( N+ V+ T用于通过发动机内的孔(孔探口)观察发动机内部件的+ a X( ]. b- q3 S0 C3 c; J/ w) i 光设备。% D* U! y- V2 k4 ?8 Z6 d: M/ o 端管,; i: t9 O, V& `/ W6 g' a 测压计内的弯曲扁管,管内压力的变化时它使指针移 $ Y+ k }6 a4 h( O- U力。, |8 M- m+ O. Z* g; H7 _+ S% O6 n 极限重量,% P4 O$ ?; t& M5 y2 Z: \5 P5 t1 U1 [8 s4 f6 c$ K 起飞重量。) p) u1 a. r0 v$ r* U: P" n$ K/ X 发动机滑油系统与大气相通的通气口。& P: J2 y' m) G* V in3 y W7 s! l6 D1 S$ S& ^1 L1 c (b $ G E s, H3 w. DB7 _8 X0 J6 ^) E3 [1 @# U2 I fo- p5 A% y- I& i8 I7 e9 h4 z' G6 h. o the tube.' u) m! ~3 A. W' Q% H BRACKET, To enclose or surround.* l- K6 n- n. O3 i' ]: Y; }/ I7 O3 n BRAKE ENERGY LIMIT WEIGHT, The maximum % x- Q+ q& H* h+ o$ f6 g; h9 vtakeoff weight based 1 M, E% W0 K! {. u' x9 ia( b8 l) H6 Y6 o q" N re + j: y3 H" g- V9 D4 A4 d8 M4 mBREATHER, A vent to ambient of the engine oil system.( t5 k3 m% p3 Y) f5 O 布尔代数,# [& U3 Z/ J0 y& k1 y5 [ 一种用于编写复合逻辑命题的数学系统。 3 ]6 l. _0 H% B0 k8 P0 v! H增压泵,0 T( U( M7 @# j/ y 从飞机油箱向总油管提供燃油的电动泵。7 u1 U" D& F1 t0 _. v) L! A' C 孔探仪, + z H' V/ e6 u1 e3 g( p3 V7 f6 b2 Q: h; E; I2 I) V2 u% h1 {5 p) C2 ?9 g: q/ t) W 动,以指示压 - y+ j. \7 H: i" C/ _! ^3 a托架,4 P$ l: M e/ G* V 用于作支撑、装托、或围绕之用。 ; m3 N1 e* }( [" @: Q( A8 s! [刹车能量8 Q! R" M. ^' {6 ~2 R 中断起飞过程中,取决于刹车吸收预定能量之能力的5 m) r, I: y+ n( g) ]$ k# j* Q9 N* [* j通气装置, ; x3 D! m8 X* \+ T$ `英汉对照民用航空词典B OEING3 G+ L! \/ l! ]0 s TECHNICAL DICTIONARY 23 + c" P [. U( R$ ]0 JBUFFET, Vibration of the wings and airframe resulting# N; y* H' I9 z1 I' k5 v$ I from unsteady airflow over the wing; caused when 3 @/ u; R7 r+ d# c5 J) Aairspeed is too slow, the bank angle is too steep, or 6 z: s8 k4 Q. P7 Z$ ~+ G' Oirspeed is too fast.- x, g7 C$ n' Y# [" |$ L UILT-IN TEST EQUIPMENT, Equipment installed on- d5 q* o2 t* h' N% ` e airplane and in airplane systems to test the systems 0 F) n1 [0 m( A8 pithout external test equipment.* q7 L2 R$ y& t& J5 H' @( R' n0 O# j1 m UFFET MARGIN, The amount of residual maneuver - b, ?% s+ {3 q, m$ w/ hapability present before the onset of buffet. $ U) z' ?& X7 pUG SPEED, A preselecteed speed to be observed 7 p, v+ `0 u) I( e; B* X' m, {5 r4 ] Inding sequence.4 m; v ~! e2 n0 D k& X, w, ^: V4 n/ n; s9 P, N Q ng landing gear operation. / B' m# }( h6 V9 z2 e速度太慢或太快,坡度太大,均会引起抖振。 6 m: x. o( e. [- _3 z自检设备, 4 J" c" } N& b, s7 ]. ]安装在飞机和飞机系统中,在无外接检测设备情况下,2 C: L+ u+ H- _8 f9 d# s7 M 用于检测系统的设备。 , |* p% ]- ^1 M d3 i% d抖振裕度, 0 u5 l S5 u/ s8 p' c! I$ g飞机在遭遇抖振之前,剩余机动能力的大小。 g8 n; v& J) W Y3 t. }标速度,! ^- @ }$ U% f& V& w. C2 o 在某些机动飞行过程中,特别是在进近和着陆时,飞机 + _6 m4 {$ S; ~6 B# h预定速度。( Y. [* d7 T4 \/ L9 p, m 力装置,( |# d3 `0 ?0 f" j6 B" }- R3 i 架工作的一种机械设备(弹簧或减震器)。" Z& J& S, J8 f2 G: s 流条,* |8 ?4 E. {4 ^: f3 _; d; Z 在部件或组件之间传输电、数据、或定时的单一电线或 . r, s( u) o7 Y! ]9 j& l& La; E" b* v( L9 W+ ? l1 z B 7 k# Q3 W, y. M# B5 rth3 F1 V0 q7 V2 ?- r8 p$ O w 2 y+ i: X3 S6 p' k$ ~. o6 ]7 cB 5 W5 T( o, z* j% |# cc# y+ ]5 X1 W# Y9 C0 y B 2 G2 N8 M& W2 H' A$ P2 i/ V5 ~during certain maneuvers, particularly the approach and6 b) d% f" f) |& T la 2 Y- o, b4 e* ^& S' g9 nBULKHEAD, A structural partition in the fuselage or$ [( O+ N) g# A2 ` wing. 5 N! F9 v0 n# gBUNGEE, A mechanical device (spring or a shoc4 ~7 Z. H0 w" ]. V* z4 d absorber) for assisti 0 P$ D% ^6 V; N; C+ ^. _8 pBUS, A single wire or group of wires which transfers- K6 B# f6 r2 l. r1 f power, data, or timing between several units or3 q" l2 m4 ?3 ]7 L* Z% U, u modules. : s) r' h8 O: j5 F H& j1 J/ p抖振,1 @6 j( t5 f1 j% | 由于机翼上表面的不稳定气流引起的机翼和机体的振 . Y2 k. S8 C# c9 @: M动。飞行 & U, V; x$ f# Q$ v: Y3 _9 Q' W3 r0 ^' V9 ~0 i7 ~# K所应保持的! E. @4 m0 u2 h0 L 壁板式隔框,- f' T7 ~! V S4 O 机身或机翼内一种结构隔板。 0 u6 I$ F6 U5 I( C# y- q) J O' c: w( W- C7 E" _用于协助起落 3 U r4 _1 O0 K) ?! S$ }+ j0 w3 C' D- n电线组。% J7 N3 T( }! L+ [ V Z 英汉对照民用航空词典B OEING ; A2 X+ ]; d: I+ V' N( ATECHNICAL DICTIONARY 24

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BUS DRUM, A mechanical connection with pulleys/ k) v7 S( z/ v _6 U% X cables in the control system.5 Y( |+ I0 T- R0 o7 e7 S- r3 r' F# Z and% i+ i9 N# i4 a2 I5 g( r l circuits for control and protection of ! Z8 G% J2 O5 @5 j: |0 u3 olectrical alternating current supply to the airplane.: J8 k6 E o- G, R duct for closing and opening the duct 4 V, q+ v5 r, K! x( H9 `assage. 4 V! ? H- r! a3 I) hUTTOCK LINE, A vertical reference plane along the & ~. L* C5 w: j# F9 Wselage for horizontal measurements of the airplane. " c, h# U% Q- C9 r接。) v0 k/ K- D$ [, p2 J" i 组件,内含控制和保护飞机交流电源的电& o% i" z5 p6 ~! K! d) m1 S* Z& g; A s0 Q4 P: L作动简控制的转动装置。用来关闭和 6 ^2 f1 d; O# E0 u! `! G- @: Q启管道。( v4 a. Y& }0 Q2 f) _/ w2 s 沿机身走向的垂直参考面,用于飞机的水平测量。 5 u- G9 w3 @# Q% }2 K, f$ QBUS PROTECTION PANEL, A module (black box) 1 p9 ^& v4 c% |+ |containing electrica 4 J' q/ H7 g; e1 Oe7 m" c+ j, Z3 P# T- W% } BUTTERFLY VALVE, An actuator-operated, rotating1 J# z7 a5 {5 w$ Y device in a# @' ]7 |9 |7 G* K: l) ~) t6 w p) u: O/ s% G( G8 {6 c' l) D( `8 d8 h% i; t B+ D* m W$ u/ x" z* H fu+ h7 M% |4 B2 d" G& m 转动鼓轮,' o- P+ E/ v! M& k3 } 在操纵系统中,具有滑轮和钢索的机械式连/ v. T; A% \4 l- L 汇流条防护板, ( S1 {1 u4 d* R4 S# u2 c) r黑匣子式的 / O* Y; ^! f: b3 k2 [1 l( T' \. B. `0 _+ ?1 J) [6 ]蝶形活门, i) m6 q( N" K/ @4 T1 v9 [5 I是一个在管道中由( k: S- |' @ ?. g& x, S. Q9 B% Y& n9 m$ I( U+ @ 纵剖线,& T9 m- n8 J y( }+ T0 r2 @ 英汉对照民用航空词典B OEING 3 ~/ T7 q0 V! Z% v' K6 I9 z1 kTECHNICAL DICTIONARY 254 Y3 I) i2 T4 E+ D BYPASS VALVE, A valve through which air or fluid will * ]7 ?( S& O" f z* ^ D- a& L% Wflow if the normal flow path is blocked.0 p+ f6 b( f7 b$ O BYTE, A group or string of binary digits. A byte is , U5 d; w$ ~' [) e+ esually eight bits long.! Y) C% n& U& z ABIN ALTITUDE, Atmospheric pressure maintained 8 u! U# W- V& ^: q1 F0 T, J- Fithin the cabin, indicated in terms of feet above sea ) r8 i4 m( j4 B4 E LALIBRATE, To repair, adjust, fix or correct the - ^: q8 ~: I/ m6 N0 ?% Weasuring capabilities of a measuring device. 8 x# j. F# j3 P/ FALIBRATED AIRSPEED (CAS), Indicated airspeed$ `4 P; m8 c2 ^& r A0 _$ V AS) corrected for position error. ' z4 v4 Z" z5 W; \nical 5 }3 |! o' c3 z) a8 R/ S$ Components. % Z. k, }$ Z" P% @% ^6 d! c# G2 b, l5 _1 P4 q g1 ]( m3 {- k 节, . S) @; U5 J; d. G一组或一列二进制数。通常一个字节长8位。+ _* M/ A2 r+ ~! _9 ^ 舱高度,2 y& _. ]' _- _. Z 座舱内保持的空气压力,以海拔多少英尺表示。 9 c. w- H* O5 A* W准,; E2 ]6 j2 q* C( C9 A* p" g0 o 修理,调整,定位或改正测量装置的测量功能。' C9 a, J% B8 P6 J# {1 p! B' o4 \- ^ 正空速(CAS),& a5 j3 m$ n' Q8 E# [1 S! H 在修正了位置误差之后的指示空速(IAS)。! o) K$ C8 Z* x: b) \( J 用来移动机件的一种转动装置。 Z+ j- M! o2 j O$ w5 T2 g& r u0 U4 P7 w7 H5 e8 v2 T7 p, l9 T C1 Y" s0 L2 c/ A0 [2 x% k: Y C: u3 I- @6 K# N' M W9 e4 M w 1 c% \% s* Q2 c& S4 clevel.' ~7 V c- T' K; S( { C ) t( l/ @. C! G$ N4 k; B7 sm ! G1 b4 ]! M, O9 M1 vC0 }4 I; c/ i$ S& I/ D4 p (I : M8 y# y* C+ N$ }CAM, A rotating device for movement of mecha 8 ~9 T( j( a- _C ) q+ j& F2 e9 Y旁通活门 4 @3 M; J' f0 w- ^/ O9 I$ W; t- u气流或液流在正常通道阻塞时所经过的活门。5 ~) }8 m6 `! F2 f- E* f- R. F: J s# K. D2 }+ s( \) s+ B$ f- R% I5 k# a, ?, z/ B( d/ A2 A) K& N" D8 t7 K4 ], b* Q+ b凸轮,% C$ M5 s0 M- d7 U7 V3 Z% l( m 英汉对照民用航空词典B $ y' Q; Y4 {- B# PCAM-OUT, An autopilot condition in which the actuator' t. a4 g- l7 F( u- _ detent piston is overridden, either manually or by the / v3 {! b# a& j( A Z6 N' Bther autopilot actuator. - D7 j+ `1 t& u. p- ] qAP, SEE - CAPTURE; O6 `; [0 s4 m+ C0 p+ G+ y6 d APACITANCE, The measurement of electrical energy1 _- a1 @2 q, P tored in a capacitor (condenser). * [' b9 V3 f; t1 z$ L! W' aAPACITOR, An electrical component of two metal E9 U& }9 J/ R _7 n" {; X8 z& Flates separated by a dielectric material, for storing, X% O8 C; h2 [. \$ a( v lectrical energy.+ V- L6 q7 [, q CAPTURE, An autopilot or flight director function to , A/ L1 X; x; S8 Q% L' S" Y; U! wacquire a selected mode." t* |- f7 i8 T# f CARD FILE, A container on the airplane for printed8 h- r5 G4 l; n circuit cards. ' N& L+ U5 \# t6 c+ Q' j- f9 h一自# K+ O4 X5 Q- {+ y& F% L 动驾驶舵机所超控。 " z+ E5 |1 a$ @截获, . y6 K4 M! i0 a$ n5 p见Capture : O* g/ B. r( E. s( c8 {) T: E5 Eo( B1 a: F4 {7 X; L8 X( t C; X A: H5 H$ I- r. C3 h* l* c3 h C# t) j2 o0 y. [/ B. o1 a s- ~3 D7 O K' O+ V6 }" Y C 4 [, Y5 h b* q5 V' Pp 2 L& m# }! x; w8 D1 I* ae : @* ~( C, S4 e2 Y7 q凸轮不工作, ' r& S2 w- X5 B" h2 Y& o2 W5 G. L一种自动驾驶状态。此时舵机锁定活塞被人工或另 ; L' Q0 b/ J, E s3 P6 q* M' |1 [2 `6 N; W 电容量, ( V* U3 L% @' H* E4 R电容器内所储存的电能的量度。 # i/ Q9 T8 e8 {4 e: ^" v容器, 5 L# M; x" z& y3 J, {0 l两片金属中间用绝缘材料隔开的电器。用以储存电能。* `* L/ l$ c% Z7 Q3 K9 N! F/ B 截获(CAP), ( K8 u& f% e4 H8 Y. ^自动驾驶仪或飞行指引仪的获取选定方式的功能。 4 g6 p2 w2 N) V/ H' R线路板盒," w, t! B: ^6 v _/ u 飞机上安装印刷线路板的容器。 ; B7 M5 a! C5 z# p. i3 K8 [; E0 A6 s7 \ OEING 1 c4 q* F/ t' Q$ }9 k4 qTECHNICAL DICTIONARY 26 0 ]1 i7 t9 l1 ^5 S9 V( V6 P英汉对照民用航空词典B OEING . v, W. r1 ?7 ETECHNICAL DICTIONARY 271 Z8 A& A8 L. n( I- c" m5 V2 w3 v1 m: W CASCADE, Two or more similar circuits or amplifying 8 P2 Y6 {* \! q& t G# m5 a& Dstages in which the output of one circuit provides the: I! V" n; N. Y put of the next.- n7 O: d' H' Z N2 g5 ^ ASCADE VANE, A vane for turning the engine airflow 5 }7 @! x n7 guring operation of thrust reverser. 6 w/ Q' X2 Y9 rASE DRAIN, A drain carrying lubricating and cooling) f" ^4 C5 c: G7 V uid from a hydraulic pump. ; K& \1 F' P7 }; h4 z9 L# u* FATHODE, The element from which the principal7 k) O9 ?* S4 Y) R) _- U tream of electrons flows. , @6 ~) x- O3 VATHODE RAY TUBE, An evacuated glass tube with a5 `: t# P$ ?2 F CEILING, The height above the ground or water of the . O _, w8 [& E4 u$ a# V! kbase of the lowest layer of cloud below 6000 meters! f" s, @4 Y) j0 \4 k0 k; o (20,000 feet) covering more than half the sky.3 P, @8 x) \$ k$ ^( W, X7 V 程。该 , ?" j& d0 i$ E e/ {% \) m程中,一个电路的输出为下一个电路的输人。' k. E; [: a# i1 { 叶栅叶片,# B& N/ B: G* {$ s9 ^ 在反推工作时,使发动机气流向相反方向流动的叶片。 * t4 C) E9 ?7 C匣余油管, . K2 d' f: @) J$ O! \6 L6 z4 |液压泵多余的润滑液及冷却液的排放口。 7 H. E/ O6 x' u2 k0 m极, 3 c3 v6 ]: o0 P# @. H5 }/ Y3 ^* i电子流流出的极位。, h% u, g- k N3 K J 极射线管, |2 A/ ]* T/ p' V) Q7 } 有显象屏幕的真空玻璃管。用于显示信息。+ e2 ~+ Y0 Z$ d, u/ |# v 云高(云底高), 3 i! `$ i9 D( t( h2 w# F6000米(20,000英尺)以下已覆盖一半以上天空的最9 m& M0 d$ Z8 u. D( y 低云层底距离地面或水面的高度。 7 M- [% i* I3 d7 j* B3 ]& tin0 B! D4 O- @/ D8 S C5 |5 t& _( [7 ?( y& P# G d$ v0 e4 f, z4 w2 t+ g5 R, c C+ `) i4 i/ y) ]8 |! F fl , F, S2 }) u+ R$ N, K( k5 @C ! {2 T4 ^, C% j- vs$ r; w' }5 B5 P' h" p4 O C # C Z. }* W% i: e" Wviewing screen, used for displaying information.) `% {$ |! K" R/ j+ Z 级联,: B5 ]- M' T( @( Q, e9 B# D3 i8 q 两个或两个以上的类似电路的逐级连接或放大过% Y3 p4 L+ Q, b1 z6 |4 d9 x* v8 y3 F0 j8 J& i. c5 k# K5 E7 w. _5 x# K# n: K0 ?: i/ S ?4 p* m+ Z6 R& y. D* P5 D' i+ T& y5 L 一个具; F3 }& M R' u3 W) V 英汉对照民用航空词典B OEING' |' p8 Y7 W+ i! s# I$ b: G TECHNICAL DICTIONARY 282 Q+ M" O( E" {7 } CELSIUS, A temperature scale in which zero is the . X# b3 G; r9 ?) L! h8 [freezing point of water and 100 is the boiling point of& Y: K( [* {+ t$ N: O8 D/ g9 W. z J& \ water. ! ?- b7 S. H: N1 x5 [8 p3 RCENTER OF GRAVITY, The balance point of an object $ T y6 `5 ` D3 c# \( }* Br rigid structure expressed in terms of percent Mean 2 i4 @. v. K' F2 c1 X0 xerodynamic Chord or in inches from a reference point.$ l4 X* O- s6 ? a" X( y: H' a" \" t ENTERING CAM, A cam for moving a mechanism to a 3 ^3 Z2 r+ t5 l9 R/ `eutral position., X& j J0 F+ k2 o Y8 @3 W2 [ IGURATION, A configuration of the * v3 Q( l( Q& w2 p( t* x6 X# M0 {5 wircraft approved for operation by the local governing, y- y5 o7 ^( q B; q" a7 p E gency., O' F1 _! R1 R3 n' F+ D ENTRAL PROCESSING UNIT, In a computer or+ G/ Y9 s {/ O1 e! K E: | igital circuit, the section containing the arithmetic and 5 W* t. H- A! ~# x1 k! y+ O! zgic,control, and internal memory circuits. ! _2 M: m' x" ]* jENTRIFUGAL FLOW COMPRESSOR, A type of 7 ~9 ~1 H1 k# |' W0 T; p: b; rompressor in which air is taken into the center of the' a6 @0 c5 @0 M6 O) m peller and is slung outward centrifugally into a diffuser( y; F, l( j3 ?, Y7 V here it is slowed and pressure is increased. 4 y# D' R& _6 @CG, SEE - CENTER OF GRAVITY* }! x( k! ~' g k3 v j 构的平衡点,以平均气动力弦的百分比或: s- I% `% u! V4 B5 H 某一参考点若干英寸来表示。 ( x0 A$ j K2 l& j T中凸轮,' G0 b" G& k, \& @; r* ^2 c/ c 将机构移向中立位置的凸轮。7 \% U$ r' z) g( }0 L# D/ ? 格的装机状态, 4 G# x) x2 q2 [* b- m由当地主管单位批准使用的飞机装机状态。 " W: `( }2 o8 ~# C& N中央处理器, 5 b& |2 P# R* W2 p1 [; k3 ^计算机或数字电路中含有运算,逻辑,控制和内部存" _, E9 _% ?% U4 L, Q 储电路的部分。. H+ Z0 r; E& m 心式压气机,3 _! G- @. K- {. ]6 | 压气机的一种。当进气到达叶轮中心时,被叶轮离心抛. P" P* }/ Z. o4 G& v 进人扩散器。在扩散器中气体流速减慢,压力增加。 " R. Z y1 [2 a$ C1 C. A重心,7 B) M! |( R* u& v$ ?; `' _ 见Center of Gravity ! g" Q0 i9 i0 G0 l' z" J9 c# C% g9 fo " @% f/ s; j j. q4 eA $ I% k \6 P0 Z; k OC 8 f9 F/ d, W' p( Z% V; O, u3 {$ c8 Fn 0 A3 s. k5 V) r3 @0 f! G: SCERTIFIED CONF . s& z7 a7 `1 v3 U! S- F2 ~' Na9 I% ^- g" k, Y: Y a: _3 w2 e1 n' A C2 s- m0 P7 C+ t& a8 K! M d - @* d9 V9 r3 j. V: _' Clo 7 ` M, P: x* t4 y" S/ ~! iC7 \- w1 i) v) u1 k c$ O$ G7 i0 P# j% Q9 \ im- P4 ?$ Z1 y" w9 N3 _0 { w 4 r; `+ s" g' _5 G摄氏度(°C),2 U- T! ]. y! C 温度的度量单位。在此单位中,0°C表示水的冰点, 6 U2 b" \& X& t5 c2 @100°C表示沸点。 0 z/ s2 T* j5 ]" X重心 + M8 o- e( l2 q% ]+ L. U物体或刚性结& h2 M1 Q0 p, C( G7 [- [% ~5 G$ t& V7 `& p- M8 d5 ]. J) X/ p3 C7 k* D' Q" ?- f* ]. {! S& j9 B$ m9 P% M; W1 F: U+ M; J# g- b& i- N4 W# v [英汉对照民用航空词典B OEING 0 F9 v5 e1 t+ d( d* ]TECHNICAL DICTIONARY 29 % ?; J4 A; k- B" i* VCHANGEOVER, Conversion from one mode to another.4 _* \: L1 D; ~& `' n HARGING VALVE, A valve for supplying air or fluid to1 s* j* R4 N+ K5 x i9 p9 Q1 \ HECK VALVE, A valve allowing flow in only one$ ?0 P- g: H& f2 R" e, w irection. See Non-Return Valve. 1 G5 o: @1 e6 R2 g: v) lHECKSUM, In a computer, a summation of digits or 0 ?* s8 R8 H C E N& O+ wits which are primarily used for error detection.' R% s; Z9 X3 s* b# o! `7 N HIP DETECTOR, A magnetic plug in sumps of 9 S& F& Q, T( C4 o8 K4 pbricated components for detection of internal failure of # L/ |7 R. v: D, | |# n( e1 Ye component. * k) j, }0 j; Q; R( \, ? V" lHORD, A structural component of spars or frames. ! U4 f2 B s L( K0 r添活门,5 a/ M0 o# s: P2 ~ 器充气或加液的活门。7 l) D8 u8 `; j9 p- [3 s 单向活门,& w7 r0 F6 v. i) |6 s' H4 r 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 " A$ l& b! Z2 \2 ma reservoir. ; e( l( c6 x6 w6 |C% Y I( ? Y6 C. l% \* p: _ d 6 P" q. M8 G! `3 } H1 r$ a, i; NC. g" i: N7 \ C b+ {! X! w* E8 Y# I C % t6 _4 r! ^6 I8 Xlu - J4 k4 y, Y2 R# c& d' kth & e4 O3 _3 T3 P7 r9 u* h; fC ) q& a8 ?) |& ]: F7 K/ D9 v1 @转换,. T- I5 w; y- K. | 由一个方式转换到另一个方式。 4 W/ ]# U: ~7 ?3 _% t/ i, f8 W& z. S" v 用来向储存4 y/ A2 T) J: {! A+ ^; {# q0 K6 _/ |* H, j; K总和校验, # ~9 R# ~8 n y$ n" C3 W$ k计算机中,把那些用来探错误的数宇或位数的总和进0 o$ L3 T R" [ 求和计算。 4 P2 H/ F+ z) O7 p属碎屑探测器, 2 w8 C& C+ \" m3 a7 `装在被润滑的部件滑油回油管路上的磁性塞子。用来探% {" g2 b/ k) w% T Z 部件内部有无损坏。9 t( B3 \# z" W0 y 弦, 2 C2 Y4 F4 l5 R2 H梁或框架的结构部件。! D% b G& j" |2 G$ q- `6 @% B9 D$ |. v) y% c2 Q( K8 q6 k' f7 o" X, G7 H& p( v: d) F G+ b4 ]+ \( [: Y, O1 V, w% s: I) }2 T; S$ F5 ^2 Q( q; _9 a) R# r4 R& P. Q" q英汉对照民用航空词典B OEING & S: ]- j1 c) _: H. F/ ^1 @; PTECHNICAL DICTIONARY 30 5 N0 X. R3 Z( { vCIRCUIT, A closed path through which current flows ! n) }4 n0 f t% cource.4 X, x) g. m6 z0 G IRCUIT BREAKER, A device that automatically; f ?$ h# S4 y3 O9 u6 {" K0 } eactivate the system. 3 P: W9 A2 @" y+ v1 zlear of all non-frangible objects which 7 R x! {2 O; E! c& x. F" [5 bay be used as takeoff distance available when' d( C+ O" M: d; g alculating a takeoff weight. 7 c0 N6 v# x& nr water under the control of the appropriate ! m. c& [8 ^, ^/ i5 \& [: ~uthority,selected or prepared as a suitable area over: t; e$ j8 V0 I. d hich an aeroplane may make a portion of its initial. @' Y: o& x) l0 d8 ]1 l6 ? limb to a specified height. + D* U4 [8 H5 V/ eincreasing. 4 i" I+ Z$ I2 H# V. l8 Q) g- \sed" Y" G- S% n. |/ f% ~ LOCK SIGNAL, A continuous string of pulses used for ( s5 b% c c V8 _& k开关, : z( F" \& G; j/ A. O2 {& A故障情况下自动中断电流以保护线路不受过电损, a( L- Y8 G0 b1 V 体障碍物的区域。在计- U( y" X1 T. g G( ?7 u. n+ z+ [ 起飞重量时该区域可作为可用起飞距离。( [2 b3 p3 B* W; g* q8 L" d' V' b7 ~ 是在有关当局管辖的地面或水域内一个界限明确的长 8 F- U; { w9 t; [9 H" D, Y0 G形区域。在这个选定的合适区域内,飞机可完成初始爬 _0 S5 c% T, R& n: L7 R/ {的一部分,上升到一个指定高度。3 C5 p( S8 V9 C* D* H 飞机高度不断增加的飞行阶段。 % D- x9 p& r: _钟脉冲,5 n8 W3 p7 d( X$ e& Q6 A 步的连续脉冲信号串。# Y! v3 K7 e8 j3 W% ?, i from a source, through various components, and back ( G6 C( Z! D5 s7 Pto the s, L% x/ @8 e) h C; d& I* ~! J' z6 X: G6 Q interrupts the flow of electricity (current) during fault! \( ?0 @3 h6 G! J4 Y/ o( i) R condition to protect wiring from excess current. Circuit2 @( K' U ?4 R# K, F9 l# Q breakers are also used as a means to manually$ t3 e1 g1 J( o d7 Z" h, A9 v( N CLEARWAY 1, An area beyond the takeoff end of the 7 }! Y2 l& C2 n- Orunway which is c * a3 P+ z: b+ `8 W& s5 xm & j; j) E* U9 pc7 r( N& Y/ Q4 P! I! U; f/ s7 l CLEARWAY 2, A defined rectangular area on the& U1 K+ q9 [/ v8 x. ]' H ground o , @8 b z, J+ @* o! q& c# ka 8 x3 E, [6 x; [w ' q. W. S' |, \# Vc ! S( _9 l7 {, lCLIMB, Phase of flight where the altitude is3 F4 B3 X. K1 Y" C CLIMB LIMIT WEIGHT, Maximum takeoff weight ba 5 r3 O$ F& W) U4 ]8 P" i, v6 {on a minimum climb gradient with one engine1 U; d6 D# d+ z& u inoperative. C4 B* {# E I! {, `1 m% n' v6 vC% \, j+ V2 R, g synchronization.5 y+ ?- o9 n7 d( @: c2 S0 p+ S+ i! Q 电路,9 J+ M7 }2 @" j' V' j7 V 一个闭合的回路。电流由源头流出,经过各个元件流回7 P4 G2 i" P; G4 V+ p8 o) g: a 源头。! ]* C0 t& n$ V8 ~ t O4 w# i `6 I/ d' d/ J2 r; A 能在. S8 @: N$ R! `; J1 q! l 坏的装置。跳开关也可用于人工使系统无效。- D0 s+ H" Z$ V( A r; c 一号净空道,; ]; K1 b6 w' J& W 是跑道起飞端以外,不含任何刚* z- Y1 N. W8 e# {$ C! X+ N; E( b+ V3 o- B. I3 Z& d 二号净空道,9 q H5 l4 X; H# ~ `) N) a+ O( N* b1 l' a" T: i1 L. l5 s9 s# {3 ~4 }0 E# r爬升,/ w3 k. W% x1 F9 h0 Y* | 爬升限重, 5 \2 Y7 x; k# ], x2 V取决于由一台发动机工作时的最低爬升梯度的最大起0 E" w9 E" v9 A; R+ o 飞重量。& w- K( l5 L5 v8 g. X# g7 g, d* k' l2 F. v$ s3 h' k3 M 用于同 0 v/ y) H4 i1 k1 [% R英汉对照民用航空词典B OEING' W1 U7 w4 r0 ^' |% ~ TECHNICAL DICTIONARY 31( X; p" h) F, S COALESCER, A device in the water separator for, u* T" E. U2 i! b4 Q8 F' D9 ^ ollecting moisture from the cold air. 8 S7 T4 T& d1 r( b9 [$ Bn antenna with a receiver or transmitter. $ L- {* `% O% Y, \: ehe cable has an inner conductor and an outer : \/ s! f( {8 T, L+ o( y4 prounded shield. v5 r! m1 q+ o% v3 a/ W e. Wting one inside the6 N/ \! s) I5 t( ~& B ther for rotating the low and high pressure 3 @2 k) e2 m3 [. s/ C7 yompressors by the low and high pressure engine 2 H4 x5 e4 p* @, D, @( {7 trbines.+ ]( \, a" z$ D" k6 M OMBUSTION CHAMBER, A part of an engine for ' h+ N0 S. @5 T9 U. k* Eurning fuel in the air supplied by the compressor. 6 M* `: p0 `; _置。+ [0 S& a& u$ E 射机的电缆。电缆 $ p6 N. a1 G, l, d: O- v7 I+ s# g中心导体和外层的屏蔽所组成。( q' M; s1 J7 s( x0 B 两个套在一起旋转的轴。用于使发动机低压和高压涡轮9 M' [$ N% y" l7 |0 U 别带动低压和高压压气机。 ' {0 p& q X2 {/ y烧室,' e L, ?! S; x% N. A 发动机的一部分。用来使燃油和压气机所提供的空气相" I! ]- x. W& B9 N$ Y 合而燃烧。

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发表于 2008-12-24 21:38:35 |只看该作者
c 7 w% }0 L! o4 H9 LCOAXIAL CABLE, An electrical cable usually * C1 J$ y& O* E( V: F0 g0 yconnecting a8 e5 O& x. X/ g8 I/ K3 Q T 1 j" z$ B o' R( ]9 f" `' j; yg 9 h8 C$ f+ f/ T, t/ `6 \; \COAXIAL SHAFT, Two shafts rota0 L0 j( H& @0 W9 ~ o / v" a) X5 u: qc! d8 j' Z7 p: e+ ^$ S tu, s% B& @6 R4 d! J0 p5 j% I- X C% Y0 |% m% O5 [" c b% |5 E. L' N" @6 P) k 凝聚器,! l H( J& H+ g: } 水分离器内收集冷空气中水份的装& G' Y: Q q/ _; a) ?' G 同轴电缆, 2 ^& m' U* w2 g1 c1 u一种通常用来联接天线与接收机或发5 s# y: ~' S2 e, p4 i7 `5 O. D( x9 N/ S2 A; R同心轴,* J2 ?) J- e8 ?( | h7 o+ q9 t2 s8 N/ ^. B9 ^2 F1 ~6 K* |5 M2 Y0 ^# G; z q ~: W% t4 x1 I 英汉对照民用航空词典B OEING " W9 t7 P% _$ N9 V6 z/ w: u, TTECHNICAL DICTIONARY 32 . l' ]: s: c& uCOMMAND BAR, A flight director pitch or roll comman + ?5 c; D9 g) ~( T8 w2 nindication. - R) g P1 q3 x; M1 sd 0 b z( F% b3 I7 o( IOMPANY ROUTE, A route flown by the airplane * J1 W6 x5 _2 e- b; T" C Z3 ^OMPASS LOCATOR, A low power, low or medium) `4 ` x& m* c) [. f- T7 Q equency (L/MF) radio beacon usually installed in % v) B/ P% K8 e9 N7 uonjunction with the outer or middle marker of an1 z, H) J8 g9 Q6 k; D tor (LOM), A compass r) i% t1 U+ Y. d+ Z7 i+ X4 ?locator installed in conjunction with the outer; y; L! t' I& |9 z3 ~" E" E4 d marker of an instrument landing system.: G. P: o9 M1 H8 g4 d7 p& v ss/ R" l6 |1 o. a le5 V. T) t" m9 _" u& l8 S OMPENSATION, To offset, balance, or counteract.' Y. k) N4 W% v- n2 E OMPENSATOR, A dual capacitor for changing the fuel9 K2 z( F6 S% A3 q* e5 Y } aging circuit capacitance due to changes in fuel7 _" H( e( C- E4 [+ I6 ` ensity.4 K Q0 ^1 i1 L1 C3 }. y OMPOSITE MATERIALS, Non-metallic materials used % `+ l5 e, e! c9 P/ K0 Vr airplane construction. Fiberglass, Nomex, Kevlar, 2 @, Q/ F: ^7 u; @! T1 }raphite Epoxy are composite materials.& d1 w: U' S5 V1 J2 N 司航路, 4 F% Q I `# @6 a8 u- A9 o在飞行管理计算机数据库内由航空公司飞行 ( p% R9 ]6 {" f8 ^盘定位台,: m p6 |8 Z7 W, p& V% p 与仪表着陆进近系统的远距或中距指点标配套安装的 4 Y9 o, t! I2 W8 y$ b功率、低频、或中频无线电信标装置(低功率NDB台)。' s! Y7 `7 O; u3 ^* J 程序中用来导航。# V4 I* W9 O5 I3 P9 \4 p 1.远台,+ H; G- ~; ]3 }# l 与仪表着陆进近系统的远指点标配套安装的罗3 |' e# O3 b% \, o; o 盘信标台(NDB)。1 R$ V8 G* B6 U- b 偿, ( n- }3 T$ Q. Y( T: t& R抵消、平衡、或中和。; D2 X9 ~! N$ O2 h' g5 r. O 偿器, 6 u" l8 l& P# c& v' R% t在燃油计量电路中,用来改变电路上的电容,以与燃" V+ @' Q* D' I4 }. | 密度改变所引起的电容改变相抗衡的双电容器。' P: ]) v: q% } 合材料, ( D' I2 R2 t, P0 t* C; ~用于飞机制造的非金属材料。如纤维玻璃,Nomex, $ ], |, U5 Y1 D0 d9 Z4 U' Hevlar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
C5 ^- u! z) L2 c% l# W& {, Q. Q operator that is normally stored in the flight $ L. J3 V* Q3 k% I" ?9 dmanagement computer's data base. ; r9 |0 V7 D: n- _/ QC/ `# N9 [% z1 C) s% _- [ fr / f" e8 c% W( ~& ^2 Zc% H2 |; K. L8 a- K instrument landing system (ILS). It can be used for Y! R4 k+ T6 N; v' J4 anavigation as authorized in the approach procedure.; V1 h6 E& o8 P6 `& v6 ]9 _/ v 1. Outer Compass Loca# O& E% T- L$ r" f 2. Middle Compass Locator (LMM), A compa + `) ^% i- [, f j; Clocator installed in conjunction with the midd 8 p4 P! N5 i4 a" {marker of an instrument landing system.4 m9 q$ r E# p4 W C- E) a1 M. Q2 a. Z$ u. N' `$ q! I C' k/ Q& a* f- r% _( z7 d g( |/ A9 @& A- J d5 T0 e: Y) j# {3 q& C1 u: U. \ C$ Z( `+ A, u { fo7 w! U9 b( i, Q# _1 ]! X7 V; y g% e" Z* ?$ e: y; u% e 指令杆, $ D- f5 j( ?% q飞行指引仪俯仰或坡度的指令显示。# [% y) T- U5 t: C" V2 H. H8 F4 S0 O* s- B8 k/ E/ Z! h通常储存 ; t4 j1 Z4 W1 p7 g的航路。0 L: B0 ?/ y4 c9 ]' V: w' o) k4 p9 o2 S0 l) G$ o* n$ s% I4 I+ H* @7 z3 L5 B1 z" t经认可后在进近8 G& E' {! \) u; J 2.中台, , j c- E# E- X9 t9 a与仪表着陆进近系统的中指点标配套安装的罗, L4 J6 Z; S# _: f8 c8 \ 盘定位台(NDB)。 9 \! e2 B/ q, ?0 n- I7 e ] z$ w8 t" \: d4 `% f! s7 }. F5 a( R' ]! S8 ]' o; w$ H2 H9 ^/ Y* _& w! A K ! v0 z9 w: ]+ F4 l& N& Q# q4 u英汉对照民用航空词典B OEING 1 \/ h8 N: S5 d/ T* p! _& cTECHNICAL DICTIONARY 33& z( [% n8 R& J* ? by6 b9 K& m8 [4 K% e$ q# l0 q% q or increasing air ' H+ r2 |5 c1 g: W: w* A$ Pressure and temperature before the air enters the ; S( T9 s' T3 }4 {ombustion chamber, Low pressure compressor - front ! {- a/ W. H7 f, V/ Qection of compressor, High pressure compressor- rear8 E# u) R7 @) A$ \/ ?, I! Y, s$ C9 [9 x) H OMPRESSOR STALL, An event that occurs when! m. T4 ], D4 _; { ere is a complete stoppage of air or reversal of air flow 4 b; r3 F$ W% R2 ]- RCOMPRESSOR SURGE, SEE - COMPRESSOR( C& F+ l7 n2 V9 |0 F! k+ j STALL COMPUTED AIRSPEED, Indicated airspeed( e" V" s4 y6 j2 A corrected for the static source error.1 E# l# y1 Y4 I9 a 的机械轴来驱8 @$ I2 x+ W2 h7 P" r ,用来增加吸进空气之压力和温度,以供燃烧室使用。8 }9 C. J J% d$ x# h 压压气机—压气机的前段,高压压气机—压气机的后 9 e9 k+ t3 E; ?$ x# T4 K" t T' P& j+ ]; c 气机失速, * U3 s! V* N' J- [7 e+ Z当气流完全停止或通过压气机时气流方向逆反的一种) a# T, E6 r6 h/ F8 v 压气机喘振, & L7 C7 X- R: n. r见Compressor Stall3 p! O- [( S7 K7 B6 E& d5 B COMPRESSOR, A rotating part of an engine driven 5 r, O! H% j: w) u, O- ^6 q+ @; ua mechanical shaft from the turbines f % J' o# o$ K5 F; `, i: z# b( Dp ' I" U1 [4 p" a+ Z4 fc & e: L3 ?+ @& Y$ @+ P+ B9 u- {& Rs* \- T( S) _% [/ O M section of compressor. & Q! l1 {& I& ~- ]4 X$ C$ iC0 W# E) R1 S$ Y* h" a+ r+ v0 v0 g th 4 W' \5 W1 Z3 L' _through the compressor. 9 r3 ]2 \, M3 `( Q! l+ e* B. P. P压气机,' O+ V z4 c, O( a+ a 发动机内的一个旋转部件。由与涡轮相连" R# i2 }, i4 D3 O" h/ C3 \. s8 \8 W) F0 f1 m3 G' U# G: ^0 J; w5 \4 s' l- n$ n$ `( P3 ~) @* a2 \" [4 ?, p2 V现象。& a) A8 [/ J7 y( ?5 r1 X3 K/ O, T2 ]7 ]! P' y6 u0 y( C4 A计算空速,6 O- u, }+ s, Z 修正了静态源误差后的指示空速。0 {; [8 Y2 m5 ~5 |; P) x* r) J 英汉对照民用航空词典B OEING ! Z, n' b; D p2 a$ CTECHNICAL DICTIONARY 34

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发表于 2008-12-24 21:39:27 |只看该作者
COMPUTER, A device that performs arithmetic) j# q* E0 C# M( U operations, manipulates data, and makes decisions.- b5 M* S! Q- u) _ ditioning1 `2 Z/ g0 [9 U H8 z4 q the air and the ) k* R" ?; w* ]1 H8 j6 z2 V! j" tfrigerant or moisture vapor is changed into a liquid. ) s# V+ t2 B3 a' T! f& Pine ! @* [7 d" K& T9 h: ~ONFIGURATION, The position of flight controls, ( q7 s" e/ X9 i3 J' }7 hmissing which 4 b( H7 ^$ X! `! D7 Amay affect the aerodynamic performance of the$ u2 ?2 i4 n) p airplane. 9 |- M: B! e2 [置。: ]& E A# r5 B/ P9 c1 S 中能使热能散发到空气中,以及使冷冻剂或湿 ( X6 {8 c, v3 S转变为液体的部件。+ Z8 U9 @. i, z( S! O ~+ P$ }2 ?( q 连接到飞机结构上。 $ c( w3 I) k7 {2 T态,$ p, G" m- o: M 定飞行阶段中,飞行操纵面,起落架等的位置。 6 E$ J: U. |! M3 w. W; ?" b0 G), . P9 x9 @" p. ]) t1 r受到影响。 6 Y4 z1 P# }) t0 m9 }- VCONDENSER, The component in an air con 1 ]* N; L, Y6 ?7 X5 Esystem where heat energy is given to% u) E7 V. J. r y re 3 |% ?: M% P5 ~9 E% wCONE BOLT, A bolt in the shape of a cone for eng 7 y1 B: U2 v/ l9 Q' E( f" hattachment to the airplane structure.( h& j ?& S: S% T0 m6 N2 a4 F' r C: I0 ^/ Q: ~% D( O# x A1 B landing gear, etc., for a particular phase of flight, e.g.,$ \! w a( D' ?$ z9 c6 C# w Takeoff Configuration, Landing Configuration, etc. 2 E* X! g& P5 S4 k% {CONFIGURATION DEVIATION LIST (CDL), Appendix * N; `0 }) N9 N9 X! m6 n5 ^in the Airplane Flight Manual (AFM) allowing operation 8 X; y5 p* k$ q) q! r& yof the airplane with certain airframe parts( n1 D5 }9 U+ i 计算机," R2 ]) t T% C% c 能作算数运算,数据操纵,和决策的装; E# S" R% ~; o4 [% Z# S 冷凝器,6 @( @8 x1 d4 F0 \% K; ~ 空调系统9 l" T* W g ~8 Q. w. Q/ I3 D( A; Z% F# Z5 D( w: t5 P: d9 |& D( r8 t. F2 O 锥形螺栓,3 _1 X4 Q& \1 m 外形是锥形的螺栓,用以将发动机 , E" U+ e) y ?' P% k8 d- V0 x- j2 w( r8 u$ g; D& o/ d1 x( C在某一特 ( S/ V% {3 I" r如起飞形态,着陆形态等。 ; t5 _5 [, o% {7 }: b" h* n9 @, j缺件单(CDL 6 j, A) P! X1 `飞机飞行手册的附录所开列的飞机上某些零件的清单。3 d) _6 F# A# W5 [ 在缺少这类零件时,可以飞行但气动性能可能+ ]9 W( ~: }* o7 x& h 英汉对照民用航空词典B OEING - g8 r1 R; X0 @( s& OTECHNICAL DICTIONARY 35

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发表于 2008-12-24 21:39:49 |只看该作者
CONSTANT SPEED DRIVE, A hydro-mechanical . K: q7 a: k l: u0 Lcomponent for changing variable engine gearbox speed 4 `9 D8 r. |* P0 `* Q- bONTROL AXES, The three axes of the airplane which + p8 h7 z# w# x! U9 ?' gre perpendicular to each other and pass through the $ S, _7 H) ^& [enter of gravity of the airplane.1 l* ]8 P5 J4 Q* V Pitch axis - Horizontal or lateral axis, passes through4 B' T6 h% V; c9 F k the airplane from one side to the other - 3 D; d3 u; C+ N& g$ k: H. E' y; o9 i: hnose up and nose down control is by 2 m5 ^6 U# T& o/ F( }, aelevators (and stabilizer for trim). ' P( t: j" B: F: dRoll axis - Longitudinal axis, passes through the ; ?7 @6 \' {( K4 I5 ^airplane from front to rear - wing up and1 I# G! ?/ N# N6 d wing down control is by ailerons and8 p# F# T+ T/ x9 s) Q flight spoilers.4 ?5 t' Q4 ?' w; M* C l Yaw axis - Vertical axis, passes through the 6 a0 }+ R' u9 R! P5 p% cairplane from top to bottom - left and ! w# F7 C) o; j0 g$ O9 \right control is by rudder. # `7 l4 w" A6 @; F置," s8 V$ J# p0 @5 E. ]( h X 制轴,& t5 M) u7 L0 a( i; b 通过飞机重心互相垂直的三个轴。' U7 ?) d" L- B( |' t6 C 俯仰轴—又称水平轴或横轴。由飞机的一侧通向另 ' N7 I& @- N% Q# u/ }& J侧。飞机绕此轴转动即造成机首的俯与仰# U9 x) ^6 R/ d" o' f# e$ Z Y 俯仰控制是由升降舵来达成的,水平安定 + n6 d. T( m+ ]0 R: b则为配平之用。- S3 U5 D9 f* ]# [ p2 g% w 横滚轴—又称纵轴。由飞机的前部通向后部。机翼" K3 D2 i! c q2 Y b, D( A 下运动由副翼和飞行扰流板控制。1 e/ V' R8 v* a% Z 偏航轴—又称垂直轴。由机身上方通向下方。飞机 4 t. ^0 p& R j: F( F此轴转动即造成机首之左右运动,此一运# v: Q% j" Y2 S. v) k' s 由方向舵控制。* y5 W6 ]0 c7 I+ ~& W5 j- g to constant speed to drive the electrical power. ) e; i! t9 Z2 oC5 ` j8 G, c4 C: a6 o a $ L5 B& J2 x* e, w+ I7 @* J1 yc* u* d- S' B/ u8 i* f3 o. J 恒速驱动装4 g y6 D' {' H$ j( O2 F4 n7 [ 将发动机齿轮箱的可变转速转变为恒速以驱动电源的 x4 N6 M+ L/ S$ m0 Y# x8 j液压机械式部件。 , W! H$ p6 R0 v! R; z' K+ c9 W, ~/ b2 j& X9 a: ~1 L- j. q8 a9 N0 U- j- r4 R, _' K: g/ v# e+ o v& S, S% Y: _& G, L" M7 G" S4 O! T1 C5 D8 O( A4 b" n7 m& x* v/ S/ d8 M3 e7 F, B, q! q7 Z0 y3 K O, {# Z% ?英汉对照民用航空词典B OEING 0 t0 I/ K9 c) [# V. NTECHNICAL DICTIONARY 36 3 x8 u& y4 U. p2 F" V( C Y" e# Y) yCONTROL COLUMN, A mechanical component used+ ?# q3 {7 @: U) B0 W% z6 d* v rs + @* ~- Y4 f) `; \" l6 y, r; rnd elevators.- p1 z; Z: Q( H. j ONTROL SURFACE, Moveable panels on wings and 0 Y* _* i% \0 Zil for movement of airplane on pitch, roll and yaw axes. + {* w* B1 J2 i3 W& zONTROL TAB, SEE - BALANCE TAB i' ?4 M$ B9 m0 C& y6 ~' `ONTROL AREA, A controlled airspace extending3 B0 K/ ^) O" ?3 g o pwards from a specified limit above the earth. 3 s/ _# {# x6 rONTROL ZONE, A controlled airspace extending/ A2 I- K( ]& X# G pwards from the surface of the earth to a specified 4 u A9 a% c; U. K8 u+ tpper limit.3 X! {5 C9 q; q: c is : m( y5 O2 r: X6 Z, ?4 x1 Vo IFR flights and to VFR flights in accordance / @. w4 g5 O: d. Q; S% [% Twith the airspace classification.& I- T; u; k: m 机械部, {" G R( W8 c8 |/ A$ `9 @, k0 ^$ v: F7 P! A6 _ X- ^操纵面,+ b: k2 V% \2 E) K" s 机翼和机尾上的可动面板,用以操纵飞机俯仰,坡度, 7 o4 R5 @! }* ?( L `: o# h# B和偏航运动。& q* @+ {( _- F, X+ m/ P1 v2 r 操纵片, ' H( y4 |6 a/ v2 d1 h; c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$ f- e, l: H% `, { a / W; `* y- l% L- w1 l9 VC! T2 h, I3 N+ d* D ta4 h1 m+ ?7 T9 z0 R! t) S C ) o/ ?* c$ w a7 Z6 X+ uC 5 e" E! J- m7 X6 a3 Z9 iu3 L: q8 T+ T# M1 w4 t C% U2 ~6 e5 @3 |/ T9 e0 m5 L+ f u+ C: l# @ }; E u' W! U! c8 `( M& ]1 ?1 ? z CONTROLLED AIRSPACE, An airspace of defined ( w$ c* U# d; M+ W1 c8 {' \3 Bdimensions within which air traffic control service 9 f2 K# X9 d. w6 Y, a" \, o: gprovided t : i o0 h* j8 y2 E+ }& V驾驶杆,0 Z; l5 ^, [" h1 T( V- V- W 飞行员用来操纵副翼、飞行扰流板和升降舵的% s4 B$ H W5 g( L5 h2 G6 a) k; @7 p" |, N( ?5 X5 c0 M+ m5 g. U# j8 X管制区域, 5 [4 _ Q M4 I1 L$ n4 P |高于地面的指定极限以上的受管制的空域。 6 M# H/ f4 L: j$ ]& j3 {制范围, 3 a& {: T# s2 G( j- A3 o8 U由地面到指定的高度以内的受管制的空域。 4 [+ o) \) V( r* s7 H一个范围明确的空域。在该空域内,仪表飞行规则飞行8 f4 Z T' ^* ]& K9 Y, D/ \/ n7 S 和目视飞行规则飞行有空中交通管制服务。. D) J& z b- f& `& a1 ~2 A- Q, F 受管制空域, 9 ~* ~! H4 x- R9 I/ i英汉对照民用航空词典B OEING! q$ T0 R$ Q8 u! r0 o TECHNICAL DICTIONARY 37 * _2 \' L$ n6 D) [, w8 BCONVERSION, To change into another form.% Y! B- Z9 t0 Y0 V( e$ `2 d COORDINATES, The intersection of lines of reference,0 S- Y& r) T6 a sually expressed in degrees/minutes/tenths of minutes ' [( T/ e8 z( O: D0 Ef latitude and longitude, used to determine position or * g0 F) z7 {" @* f% N* q; RCO - U- `. W$ C* Z+ a/ [( ]& x" b' gdestruction of th: z; Z. N; a1 @, ?% z/ Z chemical conta + W5 w7 F6 x1 H1 b( ?$ Z- _$ BCOWL, A remo( ?/ h7 z a. y$ @, r7 O1 J0 P( O for access to th/ ^4 R7 B, H [/ |' t5 X! A Fa y7 I7 l0 |! }! Q' D7 T1 ~9 y: R6 r Nose Cowl - Front section of the nacelle for air inlet ; {3 u! o1 j; A$ P. A3 y2 Z2 R8 eto the engine. 9 `5 q1 O9 g* |* E' ySide Cowl - Cover around the sides of the engine.2 S0 y; F/ g5 U; S. Z3 n9 R Thrust Reverser Cowl - Cover around the core / X$ k0 j) m8 a+ V/ j2 {- q- fsection. $ D2 X+ f' ?! _. K! d( i4 k+ YTranslating Cowl -The moveable outer portion of the 5 t, N, b! G& G! g$ m, ythrust reverser cowl which is q9 |# l( T' f- g2 g" Q& x& ` operated during reverse thrust.& `0 c& w; Z4 } 标,% d' V+ k% k, C0 C. M$ l 基准线的相交点。一般以经纬度的度/分/十分之一分 : z5 z% S. y; \5 ?3 G; x2 z读数来确定位置和方位。 % j9 S+ B3 |' |8 Y3 g" a腐蚀 * R* V- C' T+ d8 c9 x动机外部可拆除的罩子。发动机上的构件必须要取下5 [ f3 o) \/ x1 O, @7 Y$ R: h' s 流罩后,才能够到。: o+ S* W/ D+ i. n" o t; V' @) T5 e# ]机的短舱的前段。& j$ K$ p; z. c3 W: J 侧整流罩一发动机两侧的罩子。3 k2 W0 U5 m9 ]7 L0 e 反推整流罩一发动机主体外的罩子。 % W6 Z" s$ A0 ]8 \& k s k! p移动整流罩一反推整流罩外可移动的部份,在反推工: Z# B# [7 G& w# A: C7 E4 a9 x 作时使用。7 q- I, R5 I# `* |3 S u * I/ v' M# b0 E8 q Co: x+ K* l: P2 g8 j. x% Y- {, v. J location.! b/ Q$ I$ ^3 V" l' o0 e RROSION, A chemical action which causes gradual . l1 H( b" t t9 O' ae surface of a metal by oxidation or ! p% p2 L% o0 u" d( vmination. 3 ~9 k8 F$ c. Vvable cover around the engine sections4 P; [( h2 s" k1 O. C e components on the engine. 6 `5 P( _6 B# j2 D3 W) xn Cowl - Cover around the fan section. 9 R( n7 V$ |: T4 X: Y3 u转换, ! U6 y3 S: i) b2 ?7 k9 N: Z改换到另一个方式。/ [$ H! R; Y* ?) ^* _" f- r: o) N2 E- [: I/ D4 u( U0 ?7 g0 t% u, e8 [! G# _ V" d4 H% C: @+ Z' L氧化或化学污染造成金属表面逐渐破坏的化学反应。8 Y8 g& A% J* O {/ | 发动机整流罩,( }8 l$ L9 K9 `8 j2 M7 D- r b, `1 }5 F4 j* I* ] u' }% @3 |$ V. e. |$ k$ F扇整流罩一风扇外围的罩子。; [' k! K0 m5 T$ _) s) B/ |8 v 前整流罩一引导空气进人发动( V L5 g7 ~3 }. i r9 l4 }& `/ M- v 英汉对照民用航空词典B OEING / n+ U& J- V* j, r8 P8 @TECHNICAL DICTIONARY 38 1 N4 i* l, u) WCPU, SEE - CENTRAL PROCESSING UNIT ) {, ~# H1 |$ @% B* h# r( F% TCROSS TRACK, At 90 degrees from the desired track* M3 T/ R1 c, c$ K3 ~ f the airplane. For example, cross track distance is the , Q3 q, n" J- {! q& w) wistance from the desired track measured 90 degrees " @- x2 f: H' r' Q8 M! a! vom the desired track. 4 a) e& I& |! V; L& L9 S( jROSS-CHANNEL, Electrical wire(s) connected from 3 ^8 J% B& F8 o/ Z; @% Vne system to another like system, for example, FCC : |* R2 O/ \9 s+ `+ o% h3 t" to FCC "B".- z" S4 H1 Q8 A9 ~ n adjacent engine or one on the other side. 9 O+ V( p3 Y' Z8 il crossfeed' w' a% k8 b3 @4 T! |( ?! v anifold for fuel flow from one side of the airplane to the( E$ `0 K9 G% c: J- A8 M; ]" a ther side. . l* |% d- E' Q; `$ |) x6 C1 Ure $ S, L8 [0 u6 _- F' b5 d4 ZRUISE ALTITUDE, An altitude or flight level . b( D, B( L6 M4 ?) U7 d2 Q* p8 t$ b# K: m" X: ?9 G+ ?9 W o 9 \2 f( c. L; Jd8 \. ?( T- T! m; q fr 2 l" v# e( E8 c$ c0 r& a6 LC. ?3 l3 |$ M4 v o / C( D' A* [( \7 k"A5 g2 W/ ?8 @0 W; T, b! E0 e; E- } CROSSFEED, An interconnection between fuel 7 A) ]1 C$ H7 O8 t- [ Emanifolds for fuel flow from one side of the airplane to. U6 J- v" K) V5 z, ^4 ]4 A a- v: L" A, [) M9 P- d CROSSFEED VALVE, A valve in the fue # i2 x3 M9 F& Nm# M( |# U, z7 i+ O1 ^) x o 3 m/ g4 q6 [5 c+ | K% CCRT, SEE - CATHODE RAY TUBE" V! }# `1 s" s CRUISE, Phase of flight where altitude and speed a$ a' X9 h. ^4 F( H% b basically constant. 7 t. I7 F: b" A8 [* _1 VC 2 w: z4 ?. K0 l3 f! dmaintained during enroute level flight. $ w7 _3 r4 W; t& A9 ~中央处理器- G, Z6 k) u) o6 { 见Central Processing Unit.; R; V: X Z) p# P 交叉航迹(XTK), ) M* v# k2 U- t/ T' G( I3 I与飞机预计航迹成90°角的航迹。例如,交叉航迹距离 2 f0 q; A/ Q9 [1 E7 v$ E7 }0 { y* u5 P是用与预计航迹成90°角量取的到预计航迹的距离。: I/ j% z2 `5 y8 b* y+ S# b 通道跨接,8 P- G' b ~- M- C8 ^/ z 电线由一个系统接到另一个类似系统。例如:由FCC 9 X' l0 ^- x: G4 D5 {% F“A”7 V8 m# `# ~7 \( f 接到FCC“B”.4 Z3 _8 q0 Y& I6 e$ }3 R; T 机身另一侧的发动机。" x- ^& f1 h5 E- M8 f 于使燃油从飞机的一侧 8 k8 B W5 j0 }9 Z$ X) L. `& ^向另一侧。. J1 N& V, {3 Y& r4 }0 L! G- N; q 见Cathode Ray Tube3 p( I# ~1 E: f! I) N& A 交输,: ]& C' B6 _& d. V- j! @ 燃油支管之间的交连设备。可使燃油从飞机一侧流向邻; f$ q+ @, ?! k% f% E1 k4 d+ ^ 近的发动机或在 j& E0 ]; u$ q4 a* n( l交输活门, ; l& B8 `2 _3 u3 L: M燃油交输支管内的一个活门。用 * q& N' l# L5 ]8 x9 f5 H/ w8 w5 ?" U% N+ Q4 S: I3 D' ^7 Y 阴极射线管, ) {. v, S( u. {2 |$ P' W.3 G+ L/ M9 r/ S8 }" |1 E 阶段。 0 X4 } n; }9 ~( Q航高度,+ A7 B7 V7 e! X" l6 O0 U 飞行期间,飞机所保持的高度或飞行高 * t. o' f8 u$ C" m0 h5 E巡航, 5 \3 r6 u& P5 u) ~3 z飞机的高度和速度基本上没有什么变化的飞行& B6 Y! J& L8 @8 C3 w* p# ]8 @7 ]/ T. X 在航线上水平- E: g$ Y) Z" P P 度层。2 q6 o5 C* P, T9 { 英汉对照民用航空词典B OEING. a: t2 A2 ^5 o* g. k2 w TECHNICAL DICTIONARY 395 `. G) D( z0 X0 k3 u2 J+ _: P CSD, SEE - CONSTANT SPEED DRIVE 9 W+ E8 d7 s: P |! L* n: \( j5 s" j& JCURE, A chemical change which takes place in a resin v5 V2 g: s: [6 y# S& F9 v+ U and fiber based component causing it to solidify. % C& ]3 g# r/ N4 p CCYCLE, A complete series of events that take place + A# n5 r }& H) E( z2 igularly normally in a continual sequence.1 K6 R. B5 _2 j" H AMPER, A device for slowing down or limiting8 r- W2 k* Q- M' C" w: c DASHPOT A mechanical damper for slowing down$ S* o+ ~6 O/ { ovement by restricting fluid flow.+ m, f: S1 [4 e4 H# `$ b: q D ( B. m- U, y5 R Y$ ]! l! E7 hATA BASE, Stored information which is used as the 0 K9 C' A# l& l6 k, p+ Fba8 ]& v" j8 w9 _! J6 ^# S9 S DATA BUS, A conductor over which digital data is .* C( Q' o3 o7 r transmitted. ; a1 ~' s, v( Q4 P* W3 o5 vDECELERATION, To decrease in velocity.. ~' P+ H" n% M9 G1 ]1 ~ y; K 装置, , R/ j- z% v, Q9 {: T3 ~rive8 U5 ^" e, L0 T% e! Q- `& d6 d re" X* A2 P. s' e; V D 2 B5 Z/ M0 W% MD/ N. S' T* P+ }7 T: k movement.9 H: m q, U3 s' n7 \2 a, U m ; h# o9 D1 L) CATA, Another name for information. 8 d3 d' a4 X& B, | q5 PD 2 j: R. S' w6 R; c2 }; e' qsis for computation. 4 G# v8 r: Y: t/ c3 {6 J. K4 G& e) t5 y! k恒速驱动4 _1 ^: z3 K( a 见Constant Speed D . 2 m& q' y! K8 ]期, * a" T5 L) @, [& a不断重复发生的事件的一个完整系列。 4 H/ ?" f# n/ N: o4 ^尼器, 4 j8 h* b) M% `* j6 {. @% G( c5 K慢的一种机构。* I- m# o: N% x, A; L2 k6 E) V( ^7 A( Q" J% i& R' L- e 用限制液体流动的方法以减慢物体运动的机械式阻7 y) Z" B7 v F1 o; |8 I! z! c; m" r. a" }$ B% D2 c' s0 B% ^+ d9 Q* ?2 J$ [: |5 i9 c% M 料的另一名称。 $ V: d r1 J: R8 b# q; P据库, d5 n/ R$ f( s6 r2 _% x 数据总线,0 h, A6 d, A8 e; ^; H 一条或一对导线,用来传输数字信息的通道。) @5 j: O* H, C+ d# u1 D1 { 减速, ! M! d! f" C0 q- `9 G5 q: E) Z" ?# G速度随时间的递减量。 5 u' s( Y# Q" v5 n& M& i固化, + l9 Y* n( s3 `3 z9 o+ f! s树脂和纤维部件内化学反应使之成为固体的变化过程。 & G& ~( t0 ?" C: a- I: j; p1 N$ F- F# x, w* l& b! k. d用来使运动减- y/ |+ l; J1 o* c 冲器, 7 H9 f! K1 h- r% j& B" G$ d v器。- O8 @+ k; F, S: d2 J) \' w 据,: `& c+ {- g* W: i0 O' `9 z' y# [4 Y" `8 O' i# Q7 _) I4 n+ k7 @5 J# O- V. t) b7 z/ R 储存起来以便在计算时使用的资料。: L& [* [" U$ t" P+ Q6 ^; m0 O' w 英汉对照民用航空词典B OEING ( m/ a$ n! `. r. k" ~/ [- yTECHNICAL DICTIONARY 40 4 v4 a( k) a4 o( \- DDECIBEL (db), A unit of gain derived by computing the8 M% L: k! `3 k8 v" B* C) e tio of input power to output power. 7 ?+ ~- P: j7 cECISION ALTITUDE/HEIGHT (DA/H), A specified# K* h! U2 p5 R* r4 @) N ltitude or height (A/H) in the precision approach at $ R6 N+ w! R8 Q/ k1 i [) M! ghich a missed approach must be initiated if the* i, M7 i1 x% k9 G$ o ECISION HEIGHT (DH) 1, With respect to the 5 I: X( U( R$ ^2 w( e( ^proach or3 F" b' @, n7 n; E7 N: M$ Q6 H execute a missed approach./ h: E A6 c* G* K- w4 L" d) z proach to trigger the decision of either * j0 }& }" ^1 \5 k- K1 nnding or go-around.9 R0 W7 r# t- [& u8 k ECOMPRESSION, The loss of internal aircraft air) d$ d5 h4 W& Q& Q( U" } ressure. h# ?7 o# Q; K/ q) R& I E-ENERGIZE, To turn off or cause to not operate. 7 T, J% S6 Q' m+ }rom the tanks" ^9 ], Q2 j) s using airplane fuel pumps or external suction.7 @, l i t7 g 算的一个增量单位。分贝* f) X! X6 H- q; J# f! F' a 常表示两个声音信号或电力信号在功率或强度方面的 # x9 u- S* T, g8 V7 i% N8 K2 V, t对差别的单位,相当于两个水平的比率的常用对数的十 5 t- r. a: t3 d( g断高度/高(DA/H), 0 [1 O" v! N; l5 W ~) S* q7 d在继续进近必需的目视参考没有建立的情况下开始复 ' p: `7 D$ O5 L4 }. h$ y的精密进近中的一个指定高度或高(A/H)。 e- m) f* {2 H6 G; ] 断高(DH)1,& n$ V. n( Q2 L3 U, L 操纵而论,指在使用仪表着陆系统或精密着陆雷 3 H2 t; n, x+ y; B: J" `, b生继续着陆还是复飞决定的高。6 c! d9 _+ j W/ v 飞机失去内部空气压力。7 H1 L- x) E! q. b 开, + ~) z2 J2 f/ v关断或使不工作。 8 F4 t# H6 Q$ G, w c# W* C+ o( T机的油泵或外部的吸油装置将燃油从燃油箱排 7 |) e/ z0 P+ \5 k$ ~! F4 {出的方法。 & O" Q0 I7 G i4 B* vra 9 o p! e3 g; ]8 p7 k. JD 7 i! L3 c/ i' T; o% Pa S! D4 z+ M) I( u* s% S! Aw ) [# ~9 R; B9 q1 }; N4 |$ wrequired visual reference to continue the approach has) D& d4 l( i5 L/ ]# S not been established. 2 z0 s6 E0 v7 SD % [ r1 s5 t2 h1 O/ H+ |operation of aircraft, means the height at which a % i c. P/ g) ~4 \) `decision must be made, during an ILS or PAR7 @ ?6 m4 R3 T" q" S6 H instrument approach, to either continue the ap & x( W1 n0 f# ?9 [to * v8 b( {( m1 S( H1 w+ \( ODECISION HEIGHT (DH) 2, An altitude used during a " k1 k7 s0 c$ Z r, ~precision ap1 J% U9 F, U0 Y1 v5 H la : v( s5 g$ y0 ]0 m% T% WD5 D# n: h. ^# ]5 d$ g4 ], { p 6 \$ q, F. b x* Y+ g( W/ iD1 k6 D# c# l2 Y) I+ Z7 }2 @ DEFUEL, A method for removing fuel f - N M" O/ J3 b; z' g, d$ P; o分贝, 2 ?0 e- S; o8 A/ K( ?, z以输人与输出功率的比率来推 : ` T( D2 V+ V. M+ a4 F, O$ P/ }9 l( g( J, { `1 M- m8 a; b2 N0 `* A# h6 y- u+ o" M' C, m4 T( M" A T0 s, X7 _$ u; X _& l! h" n* A) Z/ ^- E M/ |7 w, F5 J( v9 _' O- F/ O1 a" L- ~) B 就飞机 * }$ V& I9 B3 _- ~2 y6 r达引导进近时,必须要作出的是继续进近,还是中断进场 M9 `& }6 f; O# n复飞决定时的高。- I( `4 r9 a/ \" g! X 决断高(DH)2, - u2 z% G! y, h+ Z5 z: s9 s精密进近时产 8 C8 k6 E' V5 P2 p" [失压, , N$ { e6 Q1 }# y$ V! ]1 i o% P) k: K1 |& J 排油, - a+ R& O9 L8 l9 D! ~, q. B8 p" G用飞 `' @- I! @: \& V$ T 英汉对照民用航空词典B OEING . d6 D, [& l) f" x4 {1 A. e- bTECHNICAL DICTIONARY 412 }/ C% p6 n+ G8 Y! ?: y DEFUELING VALVE, A valve in the fuel system for 7 `2 B$ Y l( @, y6 t& Vefueling the tanks and for transferring fuel between the 0 ^3 d4 w; C* D2 Q! }9 X6 eE-ICING, Removing ice after it has formed on aircraft.- G9 N. D4 R: \: {& g& _, A Change or difference.* I* }3 H& Y/ m7 [1 B8 F EPARTURE CONTROL, A function of an approach' I$ Z3 C- B& y ontrol facility providing air traffic control service for 4 n4 y u' Q) r4 c4 Beparting IFR and, under certain conditions, VFR 6 m# P' F2 o. LEMODULATION, The process of retrieving information / M9 t- h" T% Y& ^0 Dcarrier voltage. $ h5 Q% s8 F w7 t: Q1 r8 Bation. 3 d* Y) w( B' t# O0 ?lic: _1 T$ y' Y( N" n* N9 a creasing hydraulic reservoir air pressure to 9 ]9 W% _- V* pmbient pressure. # g( Z. J* \( v. f箱排油和在燃油箱之间 % c, n0 Q- p" x- {' N- ^送燃油。( N+ E# @1 v( A; Q6 s: V2 r/ e2 E 冰,# Z m P$ q5 D' v, M/ K 除去已凝结在飞机上的冰。 - F9 A7 p, R9 Q; `: h" U" s) d6 O删去或取消。 # ], N% F x% T量,) p+ t7 S$ g1 s1 h3 ~% n$ A 变化或差异。) @- S9 q( S7 P) i1 ?- [ 场控制,1 W0 ?9 Y/ \; k+ A! Z' W; Z u 给用仪表飞行规则离场,和在某种情况下用目视飞行 ( Z0 L; w9 s9 n3 g8 }* Q$ f则离场的飞机提供空中交通管制服务的进近管制设施 : I6 H3 K6 U# o+ t; `& ?+ s2 w5 Y5 j7 s! O' ~) ~ M; z% k 调,8 |9 }+ z& Z0 [- ]8 V4 g 电压中获得调制电压的处理过程。 & _) A% t/ z/ _环境 $ H1 k6 I/ X! A$ u, d力相同的活门。/ i; O" E) z7 v5 y4 f* G d( J& R$ p8 i) D; H+ E6 w tanks. + o Y0 N0 g VD' M5 ^" `' [: v- t' {! e0 d DELETE, To remove or cancel.7 ?: r! R2 k1 z/ {0 h3 n DELTA, 3 E ?- d# [" yD " K$ q0 u3 U Ic % I5 q) h6 L, j: ~2 Y5 M" H; Fd, q" \8 I8 t$ _: I2 y7 k$ |7 j aircraft. & G+ `+ e5 P3 e( ]D# X7 b$ T# w: D. O6 G; D0 C& e (modulation) voltage from a modulated l' ? \/ G# `6 o DEMODULATOR, A device or circuit which performs 3 U2 Z A K' {8 e( T) Hthe process of demodul ' ~+ y7 c+ u* h/ W7 n. rDEPRESSURIZATION VALVE, A valve in the hydrau % V: Q- F! ]+ z, \ Psystem for de 7 R% {; `( ?) G& H4 L: Ja . R0 P- C T. W0 ]排油活门,9 @! J/ S( b7 [0 U4 G5 S 燃油系统中的活门。用以为燃油) m0 B3 Q. @# R r6 R S- h% s: L' L' `% P' j. |: g: T& t$ Y* J4 t& u9 `0 @/ ^+ n8 _ 删除,; R7 Y( R* }$ w5 g- `7 Y( I: `3 O: R6 v P; N& y3 h# p/ C! d Q m. X. M% j, F* R5 t$ y$ g" g9 @' U/ N: B9 r- `的一种功能8 i& U) O6 r' e' |8 ?, B* ?3 _+ e2 x8 D3 E% ?" `* A' Y( _9 e 从载波 . G/ h0 T c$ E' Y解调器, . W# E, a4 P, t完成解调过程的装置或电路。! {1 Y% ?' M- H 减压阀, `( d7 J6 Y' ^+ t8 H在液压系统中,将液压油箱空气压力减至与周围% r: p! `# V: X0 W5 }1 M+ f5 t: m. e: s. p. B) }+ Y# P. q 英汉对照民用航空词典B OEING. O; H* A) w& F; z: K! ~% } TECHNICAL DICTIONARY 42+ p( R$ @. A# W* l) z# R! E DESCENT, Phase of flight where altitude is decreasing. C/ I2 l( i& [0 a% O) jETAILED FLIGHT PLANNING, The calculation of fuel: ~4 ]# r, B# Q nd required for a trip by considering each phase of; k4 P3 E4 [' X( _1 t ight (climb, cruise, descent, reserves). 8 r: {" g. J6 h. zal or x6 G; \6 ~, _1 c( T2 W ETENT SOLENOID, An electrical solenoid used for; `3 Y+ q+ Z0 w; e7 j9 z- o t. 2 y2 Q- {/ T" Especified course or6 {! Z+ z6 R# ]1 t rocedure. % _0 Q: C1 P8 c$ u& xe.: ?7 N; G' N: ?% V 飞行计划,; S. Q: V1 ~4 w' s 将航班中的每个阶段(如爬升,巡航,下降,备降)都 - [0 n# q1 o' i9 t% W: b人考虑,来计算该航班所需要的燃油量。$ d1 F6 C- ], @6 X: ] 用来感应情况之正常与否的电气装置。( @ w. {( p) ]4 V1 T& H 定电磁线圈,. Y1 M. F1 ?" J( ] 出接通的电磁线圈。% f9 T9 [( A6 d9 b 差,( n7 n. o9 W1 T" d 与指定的航道或程序之差。 9 q" j0 K, @$ {3 k用气压或液压操作的活门机构中的柔性部件。6 w3 D2 j6 I5 P$ D D2 r4 ~3 u8 m# n2 k a4 k; ]4 q; ?+ `+ L' h# g+ r fl 1 L: l. A1 ~: A2 pDETECTOR, An electrical device for sensing norm, ^; W& n2 J' i abnormal conditions. 8 J7 R& m; |) o6 a. wD8 W9 t Y, ^9 T# t controlling the engagement of the actuator outpu ' b; [) s) z/ n2 Y- \; oDEVIATION, To change from a 0 V1 p* g7 S% k+ j% @p% J& ]/ |2 Y( R J7 k( l DIAPHRAGM, A flexible part for operating a valve ' f( }5 G% p6 U( {. Y7 Emechanism by pressur5 w- t% y# K4 R% V. ^. \ 下降,- G! s6 p0 P2 P# P 飞机高度不断降低的飞行阶段。3 d7 U2 C f* ]! p Z& d8 f9 a 详细1 Z( a# P2 _0 Q, E6 `8 x8 j. E2 M* T r% ~& l/ k; V探测器,* g/ a, C. P1 r3 E6 j, V U& L5 Z. ?9 E/ }: G$ Z 用于控制作动器输 9 o; ]6 C/ V' |6 i2 m2 |9 D0 t! Z/ t, b6 J 隔膜,( E$ j( N) G5 Y 英汉对照民用航空词典B OEING " q+ C7 k! @* I7 |TECHNICAL DICTIONARY 43 & C5 U5 i* p& [( ~, \: WDIELECTRIC, A material which does not conduct' S# }$ R" u6 o8 D electricity and used between the plates of a capacitor) j! @3 X/ K' o (condenser). 2 {, C# u! s; znother pressure in the same system, measured in 4 l# N( t6 I- E, E# M- f# t1 nounds per square inch differential (psid). 8 j. U! B% E, y) @3 J8 s8 d$ zIFFUSER, A part of an engine between the2 X Q3 S6 F( } ompressor and combustion chamber for reducing the) J, x a. V, ^1 I air pressure.& l" H! V& E" z5 v2 C igh ( P k4 N4 f3 u! A% f1 B- M# f2 cpulses.- r% p9 M! I' f6 H$ Z# y2 b9 L ignal that is a close approximation of the original" n# M5 }5 E0 t& N! H' p4 _ ignal. ; z' s7 `* z9 ^IHEDRAL, The angle between the wing reference 2 o6 i5 _0 T! T2 F" r5 X1 @lane and water line. ' H) y8 h# K; S' o9 P$ F: _的压力,以每平方英寸& M) r& P; `( w9 Z5 A' S& T6 v% Y 少磅压差计算(psid)。+ U/ E Y6 i! z* ^! \) D. K- a9 H: Y 散器,; }6 l0 \2 X' W2 _3 Y9 i, E! | 发动机内压气机和燃烧室间的一个部件,用来降低空9 b2 P+ |: i" B# F ~ 增高空气压力。 ( S$ {, m l' A) z5 E! Q换,6 O" x4 w: A4 x2 p# }% @7 r" \ 的连续可 " l$ G" B$ ^0 ?% k1 X5 y(模拟)信号的处理过程。 % h: v. d) v _反角, # c& H/ V; W* ~' k0 o3 M机翼基准面与水线之间的夹角。8 a7 p: X7 z5 `! O, p0 N DIFFERENTIAL PRESSURE, Pressure relative to ' m# q& h( p, O4 aa4 ? }0 s7 F. G9 I; ` p 0 S" u/ P {1 h3 [9 a# f: o- S3 ED* O- f+ E& b" w- j, k) Y* X c' z4 d; ], x& J' ~9 c( K- D airflow speed and increasing the . P' e& g* n/ `- I# [: y7 \' ^DIGITAL, Digital refers to a signal whose amplitude % h& [& ^ @$ Y z) y9 }, Xremains constant for a finite period of time. Digital ' [4 ?! {# F$ o# [- {$ w1 L$ q! Csignals are commonly represented as a series of h, t0 U; ^0 Z2 i, n3 p' m+ m and low& P: g, ?" n: M DIGITAL-TO-ANALOG, The process of converting a4 Z. M7 Q* q1 \+ ^9 n digital signal (binary) to a continuously variable (analog)! l0 i3 t% O. G, _6 m5 K. I s# Q, h( A7 L; h. ^! F! ~& L1 N s 0 g- `- {" D4 WD$ R4 u) @* S! `5 {( }' k& k1 e p& A6 y/ D) J# d 电介质, ! g0 l7 t# k7 V一种用于电容器板之间的不导电的材料。 ! L( f& ~. s7 g压差,6 G6 P D( M# S' K 相对于同一系统内另一个压力 , {2 b" O. h! T' c. Y7 T* z' D& x5 f* g3 m& M$ {% ] a w$ G 气流速并 ' N% w% y H% V; ~3 |数字式,$ j/ b+ r' j0 `" s" | 指一种信号。该信号在一定的时间内,振幅保持不变。" l. B! G$ B. I V 通常由一系列的高低脉冲表示。5 F, I1 |8 f! h, B/ I4 \ 数一模转 Z! s; G2 E; }# [0 m. P6 D4 R Y) X3 _ 将数字信号(二进制)转换成与原信号相似+ F) w% L% a+ z v; A8 N0 i7 U* _- Z1 b6 Z ~4 w6 [& o: `& |$ a; l- z' g1 w" J T7 r英汉对照民用航空词典B OEING 1 S; _) Z6 t! Q* h! h0 DTECHNICAL DICTIONARY 44, y a# v% r1 {" `" U- `2 G DILUTER DEMAND REGULATOR, A component in the * W3 s m: t1 ~9 ~+ C" |( vcrew oxygen system which mixes air and oxygen and 4 J( {$ M& @5 wupplies constant oxygen pressure even if there are , D4 ]6 d6 ?5 R+ Q B/ [: shanges in ambient cockpit pressure.9 D5 |- a: ?- _% b" d, b IM, A word value of light. For light control devices - dim 3 K& Z! O# }/ d" U% Z0 ythe opposite of bright. , P' F$ }; X# t# c$ S }IODE, A device which allows electronic current to flow# r# u% S& `8 k: Z& G' O J only one direction 3 E7 V+ _" P3 J3 L8 U7 nuid in a reservoir.# F1 ^/ u& I' {5 V6 ] DIRECT, Straight line flight between two navigational' Z! z! ]! R9 X0 P; n6 r aids, fixes, points or any combination thereof. When6 {0 M; f6 D1 w9 B# g4 w3 P used by pilots in describing off-airway routes, points5 V$ y7 M) v2 f9 R$ N defining direct route segments become compulsory . i0 [; P# I: T" C, f, D8 d6 Y, greporting points unless the aircraft is under radar " |' r( ~- P3 s2 rcontrol.$ c& S% ^8 a! I- L" ? 节器,0 K0 B+ i6 e- o8 J( K 将空气和氧气混合, / R; Z% i$ x6 J- q使驾驶舱环境压力改变,它也能提供恒定的氧气压力。 - G- u, U; {4 j9 h( m3 c6 C! ^! c5 b9 Y" d+ \+ l3 a 一个形容光线亮度的词。对于灯光控制装置,暗的反/ n, }8 Y+ B% P4 T 词是亮。3 w, y+ Z. U8 f& U/ l. A1 L 极管,) r! M/ |( S) H" a( n1 u 只允许电流向一个方向流动的电子装置。 4 h2 r% `! o- [/ e. O器内液体的量。4 {: K. \, r- n' q4 B# j: [ 直飞, v9 T% N' W0 @ u: K& b 两个导航台,定位点,导航点,或任何的组合之间的直& a3 S F! E3 h( z) R& r 线飞行。在被飞行员用于描述偏置航路时,除了在雷达控 3 r; B' k" c1 j制的情况下,确定直线航段的导航点成为必报点。 4 s9 s3 y0 e9 M9 p/ k2 Es 8 X& n+ B; n/ [6 y! ~c 3 C2 S2 s4 x7 u9 fD0 S* ]$ l$ t$ h2 \9 s! d is : D$ E+ V( N; \- ND M$ C' h u" D1 a$ M, Z in ) v1 B9 H4 g8 i5 ]$ v3 w: t# PDIPSTICK, A calibrated rod or stick for measuring a+ Z6 P# H) S' c# w. {, m quantity of fl7 a) I: {. U4 d$ r5 c, A 稀释氧调7 i$ K" p; Y' ]( e3 j% M% H3 [ 驾驶舱氧气系统中的一个部件,它' R) J% H; {6 F3 P* Q" V1 t. h9 U* Z9 C0 b5 o4 \* ?( p2 n+ r3 d* H1 |0 V c; ?5 O6 E% x1 B$ m9 | r3 |) E& p- L* F量尺,, U: s- u# F8 I4 N4 h8 s+ ? 校准过的棒或尺,用于测定蓄液 , I: D( G" M$ d F- [8 L! o英汉对照民用航空词典B OEING 4 L, |: y6 `% bTECHNICAL DICTIONARY 45

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