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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( H$ r i+ }/ w5 [ 民用航空词典 & ^8 x/ G9 Y `+ I" a9 p. Z( T波音商用飞机集团5 Z$ r$ r0 m- T. M* i5 i BOEING COMMERCIAL AIRPLANE GROUP: U5 z4 i% m8 e ? 英汉对照民用航空词典B OEING- J; _: h1 [2 q- [& ?6 [ TECHNICAL DICTIONARY 12 U& J" [9 W5 U y5 j A( T+ b4 u$ i$ v9 \/ H' j ABEAM (ABM), Beside: An aircraft is abeam a station 8 W$ o- ~* J4 \. C$ X6 bwhen that station is 90° to the right or left of the track of2 @: t+ I4 A5 ~4 F j the aircraft.' P, _5 v! v3 ~ L7 S ]) H7 x+ A ABSOLUTE ALTITUDE, The actual distance the aircraft , I6 H9 ]/ m: u2 E2 W, ~is above the ground.0 f# ]2 E# M" U* o) K ABSOLUTE PRESSURE, Pressure of a liquid or gas ' R- H1 {! Y1 p0 l0 ?measured relative to a vacuum.. Z( u {6 q" i- }. z$ L- d ACARS, SEE - AIRCRAFT (OR ARINC) REPORTING 2 W/ X" Y2 L8 F% Q9 h8 \9 {5 |. aADDRESSING AND COMMUNICATION SYSTEM3 `7 T. u+ R) W& s8 D! h( P& S. V ACCELERATION, The rate of change in velocity with! T8 l2 B) f7 k' b8 o3 o' L- \+ n0 S. q respect to time. 4 C2 W6 Z2 \4 {" Y6 ]7 h) wACCESSORY GEARBOX, A part of the engine, 5 g+ t5 j# J. L8 [' m9 A0 omechanically driven by a compressor or an angle, W) b1 O/ R- }, m' `, v2 v4 g gearbox, for driving components necessary for engine 1 u; X' L, ]1 D) S; O I) ?; _正切,& P" h5 q) p5 |- G/ T! ] and airplane operations. , o \1 H: Y# s; r当电台在飞机左侧或右侧方与航迹成90 度时,飞机正3 r0 t$ I. Q5 _ 切电台。 7 {7 `. E, [7 |/ a I绝对高度, # z- N8 w8 V& C7 M* b飞机离地面的实际距离。5 s9 o! ?1 t3 W' _! I+ p. r. p3 C 绝对压力,1 `; M/ [: i6 t2 r6 w 相对于真空(无压力)测得的液体或气体的压力。 ( K' z3 a1 r/ I! {4 I4 e6 e飞机通信寻址和报告系统,: a# O* Z7 t2 J6 I" T5 a$ P1 x 见Aircraft(or ARINC)Reporting Addressing and3 y p- R' [; N% J Communication System.1 ~! A/ f6 \8 G% k8 @" [ 加速度, : `0 S. h, C7 Q' _随时间变化的速度改变率。" H* R- k% e8 J5 J) u 附件齿轮箱, ) p2 P4 x* ]" u发动机的一部份,由压气机或伞齿轮箱带动,用来驱动 $ P( E8 z @% u一些使发动机和飞机工作的部件" l: q2 s3 ~+ c 英汉对照民用航空词典B OEING: a7 ?- W. @) g. e/ Q9 |$ R- E" S TECHNICAL DICTIONARY 2 4 S% m0 h9 s) u1 T& n* [ACCUMULATOR (NO. 1), A container with hydraulic& y: n' r' [7 [$ c4 V: S ts when normal hydraulic supply is not0 C! C9 o0 h9 J) b+ O/ H3 w vailable.* P; T% Q; ^& A+ d1 ]8 W CCUMULATOR (NO. 2), In a computer, a special : N9 h4 t3 k5 R! U5 [torage register associated with the arithmetic logic unit,1 ^' B! P- s1 m; K: b3 b! z; f olding the results of a computation or data ' h7 `4 v! l% K' _- q2 d& iACTUATOR, A mechanical device operated electrically,8 q0 U+ M% s( C8 x, j7 l hydraulically, pneumatically or mechanically for 7 A. u" M/ j( ~* S. K" I6 {$ S8 _transmitting motion between components. + b7 h4 t5 \. F4 A. G( p# y0 zADC, SEE - AIR DATA COMPUTER" g) q) y0 | v* M5 ~) D ADF, SEE - AUTOMATIC DIRECTION FINDER j3 g0 A8 N ]* i% P ADI, Attitude Direction Indicator, An electronic display of # c" h; {' T( P) @. r# sairplane attitude information in pitch and roll.- P' n9 [4 t5 E% O& L& c3 ~* g 蓄压器(NO.1),$ j0 d' Y! f8 L. M, C k) x' M 含有靠干燥空气或氮气增压的液压油的容器。当没有正 * X% W' m9 Q$ J) X. d. X常的液压源可用时,该容器可用以驱动部件。: G0 r8 K3 J4 x) }6 G% q: c" | 存储器(NO.2), {: q T4 A- d/ {计算机中,一种与算术逻辑组件有关系的特别存储寄存5 M& ]9 I: s7 {) j8 Y- i" P 器,用来存放运算结果或数据传输。' ?4 g) c8 b5 C! w' W 飞机状态监控系统,' x$ e, ]3 t( X3 d5 t4 W3 A+ s 见Aircraft Condition Monitoring System2 C9 C( c: y3 U fluid pressurized by dry air or nitrogen for operation of1 S& K/ |0 F3 c- n" i, S6 [1 ~) b componen5 ^( O- ^& X9 q0 L a , i5 f8 A( p8 }7 }' w9 gA ! a' ]3 b( g9 T0 l1 Fs4 R( P# _( r. f. P3 r" p9 l used for h6 q8 D4 W8 j7 l( W. d4 L( v transfer. ( G; {/ ]% X7 x; T) R4 O; H/ {$ w+ N/ dACMS, SEE - AIRCRAFT CONDITION MONITORING6 G' i( n- K: v8 m3 X) o; P SYSTEM . ( l. | s P2 R) Z7 A; n2 b作动筒,7 l8 U9 [9 ]) Y |7 @& l9 Z9 D 由电,液压,气源或机械驱动的机械装置,用于传送部 + z2 m0 A/ _1 b" \$ ]件之间的运动。* q* w) B2 j* r: Y' B* M 大气数据计算机, m3 B" Y; o# x7 y0 f: ]& j 见Air Data Computer.( c+ O) Z9 {" w0 `( I( T& M 自动定向仪,! ~# \/ J% L! U/ @4 ~2 i; t X/ i2 u- S# S 见Automatic Direction Finder. 5 c0 s) S8 j6 ~. g: j7 j1 Z" |/ d姿态指引仪, 1 ~9 I- c7 G$ P7 B用来显示飞机的俯仰姿态和坡度的电子显示。 3 Y+ k2 N+ J+ _1 b% B _英汉对照民用航空词典B OEING% @" B2 A5 y/ ^8 }1 u TECHNICAL DICTIONARY 3 # e$ a/ H: d8 p, {' eAERONAUTICAL RADIO INCORPORATED, ARINC is - e! Y$ U. Y% ^* h) J: { v3 w7 v, ' Z5 z4 C x$ U1 U/ G( Z4 _nufacturers, and foreign flag airlines. ARINC4 F# ]" c$ F: _( }* z; v evelops and publishes standards for electronic. i9 n! L& f& Y# R quipment and systems. 2 ^# O1 p% h3 u! \; B6 tGILITY TUNING, The capability of the DME to! e8 E# L$ q+ ]4 o( U lternately tune between two different DME stations in # X: Y F( u, _0 u, s, ]rder to get two distance readings from one 6 [4 m9 ], l4 t8 c$ hterrogator. 3 d9 ^+ ~7 @; R# {, U' hge. [1 \# l! H$ D ILERON FORCE LIMITER, An electro-mechanical+ C9 a! U1 }8 ^ X1 y% c) A IR CLEANER, A component in the pneumatic system+ i+ o c# ~( O4 T upply to the air 5 N8 u" X8 X( P1 sonditioning system.( p. F( L8 x* u; _, V: [ 订并出版% F) a/ r9 U* }. F% Z 子设备和系统的规范。 9 c9 C8 Y, z# B快速调谐,5 e2 o& \* p8 C6 o 机载DME通过交替调谐两部地面DME电台以测得来自 & I i7 c+ G3 ]" b同一台询问机的两个距离数据的能力。 $ d$ H5 o5 {% b, C) i9 ~, P& T翼操纵力限制器, # z/ e* f, L1 O- \( a6 b装置。在自动驾驶工作期间,用来限制驾驶盘 3 e$ Y) }, u1 S, D) Z# @3 G/ A! p( e气清洁器, . U* {! g+ h m/ c6 W部件。用于去除供空调系统使用的发1 W% h$ E' q3 a4 ]+ L a corporation whose principal stockholders are United: }3 ` C% O7 r9 w States scheduled airlines, air transport companies4 ~7 ]; a" q1 M& \- u* _$ o/ T aircraft ma: k0 L E- U/ n6 D; a5 H' [, A d; _ v) M7 q1 o8 J e 1 E1 \- K# [, l% t) k+ S9 Q& _A0 ^8 O' s" B3 ~6 `' |2 } a 2 g/ I( a' E% p/ T8 I" qo1 o5 I' V# b0 }. A( I2 _: S in 7 X" X2 C- I7 a" X( BAILERON, A hinged moveable part on the trailing ed 8 Q/ {/ K7 `# l& n* L6 o2 J+ fof each wing for airplane roll (wing up and wing down)6 m6 f) r1 F2 o8 ^# O. G9 h6 L control.5 b8 C$ o! t O! d A ! f: B& S8 r6 L1 @3 x% S" ndevice for limiting the control wheel movement by the B/ c$ g$ c$ U9 L9 Y8 o( O autopilot during autopilot operation.+ P+ f/ |" k8 k" Z( B: a A0 ~- }" e. [9 W& Y1 j( S# n for removing dirt from the engine air s$ x& ^; c. s! k% M c . v% I* n% x2 B7 K航空无线电公司, " n) Y/ {' V( U5 I' `* k/ e) M主要股东为美国定期的航空公司、航空运输公司、飞机9 `' |( a6 T% w: v 制造厂和外国领队航空公司的组织。其目的是制 6 @8 _7 G6 M* j X0 F1 \9 \9 ^" q; ~" } n& ~4 c0 Z副翼,% k( l/ [ B, |+ i5 Q7 D4 D 铰连在每个机翼后缘的可动部件,用于控制飞机的滚转8 a9 f1 t9 L- `2 P. D (机翼向上和向下)。 a& j, U, ~6 M% _$ }/ J. R" e. V: N& [; N5 ]( _* @一种机电 . R! c2 Y7 H# ^/ Q的动作量。! y0 q6 P! O$ j0 A7 [ y6 \, P+ A( ]* T$ W) D0 m气源系统里的一个 : @5 N3 ~: m- u5 L/ ~动机引气中的灰尘。% s" E% E& @$ u# @# V0 m# ?0 D 英汉对照民用航空词典B OEING . {/ J, o0 U' GTECHNICAL DICTIONARY 4 8 d1 ^ ~( O. \AIRPORT ELEVATION/FIELD ELEVATION, The $ i2 U) b+ m; N" yhighest point of an airport's usable runways measured( m& ~5 f& a" X9 @ in feet from mean sea level. In a few countries, the 7 {& G3 [5 j2 i/ ~$ e7 m* w4 u9 J+ qairport elevation is determined at the airport reference9 n, R+ ^( y9 h9 T point.6 ?+ b6 R0 `) J AIR ROUTE TRAFFIC CONTROL CENTER (ARTCC), 3 {8 R2 r/ l1 l9 Nervice* [4 n5 j* A2 G1 R- c ase of+ ?# Q) F% ?3 ^ us flow of air traffic. ' \& E' a' r. D. l& ~IR CYCLE MACHINE, A compressor and turbine on a 8 P1 i- o% P/ s, d) Oommon shaft for cooling the air in an air conditioning' a$ T# l2 g8 P0 F0 x* a/ K$ f. v: u ystem. The air is cooled by expansion from high to low7 T& Q# I; j7 X- O- Z+ u6 I ressure across the turbine. The compressor is driven( g8 R' \/ x7 I3 M: e8 G5 r- L y the turbine. 0 W1 @& x- z+ F/ X+ F: n中航路交通管制中心(ARTCC),! m( b) j4 W$ C W9 |) ? 域范围内使用仪表飞行规则飞行的飞机提 - m" Z5 M" h f% g4 o+ y/ Z% B5 D管制(ATC), , `! B( o. p; g+ Y涡轮冷却器,7 @/ W/ w2 E+ P 是装在同一的压气机和涡轮,用于冷却空调系 8 f, Y4 j$ R- ~. y a统中的空气。气经压气机压缩后,由热交换器移去热量, 5 ]' Q" j, A7 `% N( J, T$ C7 S然后经过涡轮令涡轮带动压气机。通过涡轮之空气,温" _5 Q/ N, p& w 度下降。 : j& I7 D9 w1 ^6 ^; h2 R6 S- cA facility established to provide air traffic control s5 C/ k g) t) Z2 g! X+ D8 N% e to aircraft operating on IFR flight plans within controlled 9 @9 R$ `+ a9 w3 ^. B' ]# P% hairspace and principally during the enroute ph; ?% H% D8 P! c& X* G: ? flight. {( K8 t+ _7 l AIR TRAFFIC CONTROL (ATC), A service operated by 0 _& I) o9 H( f- ]1 tappropriate authority to promote the safe, orderly and 2 F. u8 K0 c4 T" rexpeditio 1 V' Z5 y4 o4 [( e) B; p1 g# jA" y$ i9 I9 h/ l- [2 G c! R% R- Y- B- B3 e* p9 D2 s2 H4 [ s - R, Y4 d: B' V# s( j! @7 _p( \9 p: P- W, h# K' k: k2 L' ~ b 8 L6 d0 g1 _5 J0 l* p& I' V* T机场标高, + G$ {# J# o# p U' `指海平面与机场可用跑道最高点之间的距离,单位是英 ( i8 e0 h7 l4 c$ v$ r$ @! X尺。有几个国家的机场标高是由机场基准点而决定的。 % @2 ^- R7 i, ]" i/ [8 u' }. Y# H% b0 P; ?, ]给在控制空$ Z. S0 d! P* X7 Q 供空中交通管制服务的站台。/ ]# i( X& T, }& y3 j 空中交通 % S# g1 k# V* _4 ]由有关当局管理,旨在促进安全,秩序,和效率的空中6 s$ p, ^9 H/ q7 U$ k9 d$ z( ?* s 交通服务。 ; B9 u/ s. X6 k; n* e根转轴上 7 l& i% g# s8 x% r, ^$ I+ M4 M/ z5 C; e" v* Y+ Z3 A5 _$ R9 _ 英汉对照民用航空词典B OEING/ X4 q2 u; d$ k Q7 L TECHNICAL DICTIONARY 5

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发表于 2008-12-24 21:36:52 |只看该作者
AIR DATA COMPUTER, A computer which produc1 Z& y& `! y0 }) z4 D data information, such as altitude and airspeed, based0 r& P+ M, a3 h/ q( E on pressure and temperature measurements. ! K. K# t6 j/ Y, j# [ C! xes air; t% f/ `* p' A S/ o% N IR TRAFFIC CONTROL, A system comprised of # i5 i5 y7 ?2 Wround and airborne components used to identify, track ! s- U. t/ G) e5 i* r# BOUND SENSOR, An electrical device operated0 g4 z4 a! }5 U( O$ ^1 f- A y the landing gear, which transmits on ground/in air + v4 X# H. \3 u1 Q$ _5 gformation for system operation in flight or on the' y5 ?4 L4 O2 K/ P9 E! n round., G, r& a4 r2 E3 D& w IRBORNE VIBRATION MONITOR, The AVM takes( W5 M$ [. T( D' r9 e( W' r. [& D e signal from the engine mounted accelerometer and 2 y' `9 f& r7 M9 j! e8 ?: oalculates the vibration on that engine.% V5 j- O; H/ ?0 V+ [ corridor equipped with radio navigation 1 T0 b% H+ i( D7 r0 j, maids. + z0 Y6 A' r* T( B+ T0 O$ p# uAIRCRAFT (or ARINC) COMMUNICATIONS ) \. P8 J* ~. n6 a! [ADDRESSING AND REPORTING SYSTEM, An' o- \8 s9 K4 n7 E% y3 k addressable digital data link system which permits the7 ~ t' }2 E0 G1 s: b" h( G; k! X exchange of data and messages between an aircraft' Y* T& H! D) R) w6 Q+ P and a ground-based operations center over a radio1 c) N1 |8 ]* Y9 X) a2 X network./ N8 @) ]% q7 P8 B- j+ w AIRCRAFT CONDITION MONITORING SYSTEM, A6 J/ j% P0 a/ X system of sensors and recorders to monitor various; o6 a( n0 Y1 u. B& U: H. M airplane systems' performance and status.) q1 E, t S: M4 W( Y 机, " C, I1 w3 N( a中交通管制,1 @! h+ A( Z- s7 J 一个由地面设备和机载设备组成的系统。用来对飞机进( [ a" [: L2 {( d" u* U$ X 地传感器, 2 g5 H* t; H9 W* w% Y一个由起落架操作的电气装置。用于给空中或地面的飞 6 \4 { @) M2 h系统运作传输地面/空中信息。(有些系统只能在地面0 y, q. ~9 K+ ? 用) $ w6 v" r, D# W& w, D5 S载振动监测器(AVM), a* u# w% x9 [( m: y) TAVM从装在发动机上的加速器取得信号后计算出该发3 z6 b* g# _" {5 ^ 机上的振动。2 A7 M( z' F$ {+ P9 C: c! [ 式建立的控制区域,内有无线电导航设备。' [2 b8 a7 g6 T 飞机通讯寻址和报告系统, 2 @* y7 u9 R& T' Z9 G* A4 R# q* H0 S有种可寻址的数据通讯系统。利用该系统可使飞机与地 . N! f! P2 P& l2 D1 f1 R/ h面操作中心通过无线电网络进行数据和信息的交换。, s; o/ `. O. I 飞机状态监控系统, P% K% B* {3 ?) G4 w3 @8 v C 一个利用传感器和记录仪对各种飞机系统的性能以及 8 Y9 _7 [% U' F" O( W状态进行监控的系统。9 z2 C, v( l1 q' _ A9 {6 t0 ]4 d' ^( | Q! f g 9 ~, ?7 r5 g2 P" G" d7 n$ I' Uand locate aircraft.' x. V3 A" N- l! ^0 e+ G. l AIR/GR4 ~1 ~! L5 l1 v: t4 }" ?: w b1 `; T9 @4 \3 V4 d in 1 l0 I% q2 E: F7 j1 b- Sg ! D$ n& S$ f' |3 N5 e: KA : A! I( q! k" W' G( |th ) }+ v! f2 L# }- @c - K! n$ W0 d; c% U0 JAIR WAY, A control area or portion thereof established; l, A. W Q% _) b2 J, {' l in the form of a# d8 _& I: Y1 ]6 G! H4 k 大气数据计算 9 Q8 R( i9 R8 |, V& x根据量取压力和温度而产生大气数据资料(高度、空速 . O, h" A( | a等)的计算机。0 p$ d) z* ^5 y+ @ Z0 `% q0 ^1 l1 G$ g) m行识别,跟踪和定位。2 H* g; L" p4 F$ i2 t1 w) ]6 A! ^3 a2 X( t. a/ g8 q L. |- I0 r: V' T使$ V! x* N) a0 i" Y4 P* _8 p5 C! A( x. p% _* T6 Y/ g# B" N! U, L7 C航线,- _/ f! A* ^/ x# V R8 t+ m 以走廊形 : x3 I) z8 o- H* n) d英汉对照民用航空词典B OEING' t9 @% O' B9 b3 I1 {$ k TECHNICAL DICTIONARY 68 B5 W: I' @6 N5 t6 F1 c5 P- b k9 N AIRFOIL, A surface designed to obtain a useful reaction, ) V2 U! ]- e! r4 m' A3 M, ~such as lift, from the air through which it moves. Wings, \: @3 \1 ?. x7 Z+ U3 w8 Pstabilizers and control surfaces are airfoils. q. T0 [8 j% J/ |$ ^; l AIRSPEED (IDS, TDS), The speed of the airplane 2 b' \1 W% V1 ~rough the air. 8 ~9 m* W# R7 e" k2 wD INDEX, An adjustable pointer on the 8 }% z0 p8 s+ F3 o' H, _# Oirspeed indicator.: @: O6 x$ Z4 `& ^; A6 F4 P and legal ability) o8 M, C' w0 Y fly. ( F, B# W, @' G, fm, for example, the procedure for finding the 4 |8 j" D1 B mquare root of a number. D/ s% O) a) P; p+ A7 v$ S- ^ y + a9 R% } ~; x1 ore, wind, : {& Y. c8 m! m- o4 {! F( sand aircraft flap setting. l2 N9 Z1 `8 h3 r& h$ ^# g 是翼面。2 ^5 e$ }& O7 T1 p 速, 6 p' ?4 ]) V U% h6 b* j8 G/ a飞机在空气中运动的速度。 2 a3 |0 w' j2 j2 H$ H& }5 Z$ o$ S+ ?/ U! F7 C在空速表上可以调整的指针。8 h( r: u; e' U 机械飞行能力、和合法性的飞机状态。 7 c+ K4 B( [0 T8 D! P一步一步的解题方法。例如,计算一个数的平方根的步6 \. E" v+ E# n% x2 F# G! @6 q5 c f4 T/ B m* G7 t4 F& n资料的法定文件。: l( s# @1 q: S' g& X 翼位置成函数关系。+ j W" N/ ~5 F; A8 ? th4 d/ j1 e, z" ] AIRSPEE 6 ~( t+ k m+ X$ ba ( ~) m' G+ w6 d8 c8 k9 v/ p7 HAIRWORTHINESS, The condition of the aircraft with 1 Q2 @' S$ H2 h3 Vrespect to its aerodynamic, mechanical,! ^4 F5 S6 l2 J3 v) t" u& |, b5 D to, E- Z( A7 {; `( c ALGORITHM, A step-by-step procedure for solving a 9 b9 g& ?, P: w& Qproble 8 S0 r- l0 c5 z* Is6 v8 {2 T) o+ U. Q: D% A' k$ ] AIRPLANE FLIGHT MANUAL (AFM), The legal& @) L- ^& n& {) U: Q, M document containing performance and operating limits, 4 d: Q0 a) r% h7 j1 K5 B1 Eoperating procedures, and takeoff and landing& t0 w" ^4 ~6 y. d% q) L( j$ a performance.: D7 f: }) d$ h& t! f4 j, C AIRPORT ANALYSIS, A comprehensive set of takeoff * l+ b: [; N. m9 v fweight limitations for a given airport runway, generall* m& T( |# @7 z) A) ^% c+ n+ j presented as a function of airport temperatu) K# m8 N! ~0 _; l! e! X 翼面, 9 T$ u- i+ y8 i$ T. n0 c7 C; [* V Q用以从气流中获得反作用力(如升力)的表面。机翼,2 @) i# w. w4 e [- z 安定面和操纵面都 9 c' s% L; d( F, m# M" u' O$ R9 [5 d& H1 v/ x6 w5 Y空速指标" u. }2 D) K# A Z3 T, J+ {8 e g6 K 适航性, * J" ^( A6 ~0 B* `; e9 d有关气动能力、2 t4 I% o9 ^, ~# j' R2 |8 B' X 演算法,& M: ?2 y0 G" F; h0 h5 u; X4 y& g. v. e# u 飞机飞行手册(AFM), 4 E1 ?) F9 b( l( }3 n/ {包合性能极限,操作极限,操作程序,起飞和着陆性, l' y- ^! `+ _) o4 S) k% w: J; c! Z+ C8 P9 T) o, E/ J7 v8 W# Y$ P 机场分析,# d5 q% w4 h( l 一套针对给定的机场跑道的详细重量限制资料。通常与/ S4 I# }' a8 c9 G. y 机场温度、风、和飞机襟" }0 h' t7 O$ J; r 英汉对照民用航空词典B OEING 7 a( D$ j6 t! }% O6 u* B0 L! fTECHNICAL DICTIONARY 7 8 n2 p( E/ p! t3 h' B/ H2 ~7 PAIRSPEED BUGS, Adjustable pointers on the airspeed 0 \, d7 X& C% l, k5 k5 p* O: Jindicator.6 Y' U# [1 @0 ^ ALLOY, A mixture of a basic metal and small amounts/ M, P7 W7 `* {' B7 E; W: J f other metals to change the properties of the basic/ c! G; l: H& } etal. 5 r! Z7 Z3 J/ B$ y% CMinimum airplane speed. ^* s+ f/ p/ g7 u e of: U7 }* O/ C8 y9 I. _/ y3 T' t itting airplane angle relative to! l& G$ g* t0 i# J. Q E irstream for the stall warning system.! E, a( Q: p5 P9 k5 b! v another. / I2 \; @) {$ u3 vLTERNATE , An additional airport selected during$ ~4 u5 U Q& z# W) E& i* g- d' L# j$ f+ Q4 y合金,' l. B% }! l% D* Q: S) k. z9 t: E 在金属中加人少量其他金属,而改变其性质的一种金属 ( E, u9 q% B6 r$ }& X合物。 5 k# K4 o+ B" v飞机的最小速度。 8 e1 p* X- f% Q9 `1 c速警告系统传输飞机对 & R0 [8 F5 L3 v流的相对角度。 / b+ \! V# C0 z5 B9 H8 y由一个状况改换到另一个。) p' ?* V7 `! L 降场,1 m- k+ M- i' w5 }. I" D9 G 划时,除了目标机场之外,所选的另一个机0 ]2 i# R [. a h b% R l o $ g0 l H3 I* P9 g8 S2 Lm/ I' X# P7 V; d0 w ALPHA SPEED, , `# _4 _& E! Z# i8 aALPHA VANE, A small moveable airfoil on the sid' g% J* I3 s& N' J) t- |" y( s+ e the fuselage transm ; T& R& C8 q* S8 La; x4 {+ N9 [( g4 h' A* G4 f9 l5 r ALTERNATE, To change from one condition to5 u6 U& T! U9 c+ y A $ Z; V) ]$ ]9 N" t: I/ Eflight planning, usually near the destination airport, to be1 m& t, H' k8 w! n used when it is desirable to divert from the original - z% T- f* p* M* i! Xdestination airport.8 \$ \( w! X- g. f/ W0 ~ 空速游标 , X, [. F5 s3 d6 Z9 p* s/ q6 |空速表上的可调指标。! t" G: T, Z, j3 u( y1 a$ I, l7 Z) C1 G' g$ t9 `9 t迎角速度, # X' R. h% j' V9 t# |迎角叶片, : t6 L# W, i6 P/ {- N: Z4 @' z位于机身侧的可动小翼面。为失 , S% k# ~& T* g" Q; x* h( \" v1 D R& z5 p' R# M* ?! Q; u2 v, q 交替,% k2 H0 E1 I, P6 M, n l* q" K l2 l: ~3 z% N制订飞行计 ; W0 z& y6 f; u0 @场。通常在目标机场附近,以备不去目标机场时,改降之3 o; ~" I$ c/ r0 T8 ]8 {- J 用。0 o5 }* l/ m. F& b 英汉对照民用航空词典B OEING " }$ x5 z0 P8 |. d3 ]9 U8 h7 STECHNICAL DICTIONARY 86 h( `+ T) u4 L9 J' F0 k* u) r ALTERNATE AERODROME, An aerodrome to which # x1 g( G6 X! O/ b% ?* l% San aircraft may proceed when it becomes either : o1 q; R2 d% i3 Z" p. ]' npossible or inadvisable to proceed to or land at the : \' D: Y. S7 \, h4 aerodrome of intended landing.- N3 s9 x1 o5 w- t+ u: x- D TER SETTING, The adjustment of the altimeter ) `; p- [$ b# w8 f) B: _! T; haccount for local variations in atmospheric pressure.6 w5 c1 S1 @; z5 q LTITUDE ACQUIRE, A digital flight control system 3 ^6 k; y8 r' X$ b. vode to transition from climb (or descend) to level flight.$ T q, i8 Z1 H LTITUDE ALERT, A flight deck alert occuring when the) E9 a; y- V% H: Z' s7 G( C. g1 W irplane approaches or departs a selected altitude.2 S: Z5 U/ r& \0 d LTITUDE CAPABILITY, The maximum altitude at3 C, z6 j- E+ I$ F) [ @ hich the airplane can be flown at for a given thrust, / |# p, ~5 L8 E2 p s+ Qpeed and atmosphere condition.3 [( O$ I% A# p1 `+ ]: z1 z LTITUDE HOLD (ALT HOLD), A mode of the autopilot; }, Q! U' L2 ~# _3 u7 q' L/ F r flight director to maintain a selected altitude. 4 w3 D1 L2 w. W- Jirplane's altitude during VNAV operation. 1 t* ?; N4 k! C) x6 f机场着陆时,可作着陆使用的/ d6 w5 }4 \% Z' D: x/ X 场。) g9 b" E; [( G6 Q7 W V. s$ R4 l. t. X5 Y4 M x; o根据当地大气压力变化而对高度表所做的调整。 1 {+ }: u) z4 ^! r! ^1 Q一种数字式飞行操纵系统,从爬升(或下降)改平的模 % t0 ~$ |: ^& A6 U/ o* [1 l2 q2 c 度警告,8 D6 c2 c% t, x* c( C4 b" N: {( S 当飞机接近或偏离选定高度时,所出现的驾驶舱警告。$ H2 C! F& R7 g3 q 高度能力, ! ?, G) ?; I6 C* O0 ~在给定的推力,速度和大气状况下,飞机能飞达的最大( M8 X& j% l+ C; {6 o 高度。3 R8 _2 S* _- I$ _0 I n 高度保持(ALT HOLD),9 F( N/ J$ j7 X( t `6 _1 m 自动驾驶仪或飞行指引仪保持在选定高度的一种方式。 6 s+ j$ g" k- @7 N5 ~& q' X$ T* I. w7 D4 B! Y; y 员对飞行高度的控制。, e% g+ E+ C0 g0 P* m2 z$ B* N im 2 c X5 Y7 d+ r4 w/ U8 Wa # K& S+ X/ V- W: C X2 K- GALTIME - [0 W7 C P, y v* A+ R2 R# Ito( ]6 e# P& w% F% a. K9 ` A Y0 Y5 L: ^: K) m( @0 n) sm , G$ ^- E9 z; nA - q. A8 y4 h: ^- O7 h2 za $ i+ C1 m# o6 H5 @A: w( h( B( a; q; e4 Z4 y w2 Q s. Z+ W1 ^/ ` s ) u9 }' F9 y& K) r0 x9 t6 J0 IA 1 h6 ?% c* v/ N ao ! i4 L" e; c1 U/ Q; x& u# y$ |ALTITUDE INTERVENTION, Pilot control of the 1 d. P& |( ]1 `9 w: ~' [8 Za : q7 x1 S2 o4 a# K9 MAMBIENT, The surrounding atmosphere.7 K' n( H* {1 ]2 G9 V0 m. P7 C 备用机场,5 l0 Z7 L6 Q2 A @- C% k 当不可能或不适宜在预选+ O f8 N9 `: ]- m$ Y3 O% C _/ o7 o9 D4 B. h- y7 ~) g5 k/ Z高度表设定8 _& r/ C- y& g- L 高度截获, " m! \' j& m( R6 W! ~; _ x& {2 [, x3 A* \$ r' d/ ~3 f8 J% N7 b/ f" y7 `+ @高度干预 + q4 ?7 m0 Y* G1 l1 ^& _在垂直导航工作过程中,飞行" D9 Y- W, W* Q: d+ g 周围环境(地面气层), f* R2 B5 E& I+ M 物体周围的环境(特别指大气)。 3 U) `+ H, t- w \3 b6 X英汉对照民用航空词典B OEING& Z2 A+ c# Z& b: m$ V TECHNICAL DICTIONARY 9" ?& Y* F3 c7 Q; a/ Z) g AMBIENT PRESSURE, Pressure of air surrounding an 1 y, D$ e# x/ T9 iobject, measured in pounds per square inch (psi) .* i: {& n& {0 U$ r MBIENT TEMPERATURE, Temperature of air % s z7 b; Q6 _7 r) Nmpere. + P7 v3 a/ @, p; c8 gurrent waveform.' k" }8 {# y! Q$ X+ ]$ m" i g an) M2 x x% q/ |' Z I$ q" C nalog signal to a digital signal. 0 n6 r- z' j# U G% h- @ore inputs/ q. S% p9 T# v4 @2 [ f binary digital information and one output. The output* }7 E& ?/ F9 T- I" T 1 only when all of the inputs are 1. The output is 0% P2 [9 P# \4 r7 ]. a/ B hen any one or more inputs are 0.; o" N- y j) u 面气压),: ]& E# Z7 l+ y0 L 境温度,' J+ h& O1 @! A6 }. t" A$ y 气温度,用摄氏度(°C)或华氏(°F)来: g. \- P% ~) B; v* a+ z9 ^- Q8 x8 i6 ]$ C4 i% e电压或电流波形的幅度。 1 O Q8 e' |2 m性变化的信号来工作,或产生连续性变化的信号; _( ~3 |; ?8 U1 P 统。 ) l j4 S5 x/ O6 l$ d6 i将模拟式信号,转换成数值式。 ; h1 o. m* j' \/ F一种有两个或两个以上的二进位数字信息输人,一个输 & V3 u( }* E" D$ {6 v/ f; y的装置或电路。当所有输人为1,输出为1。当任何一个- @* D/ l9 q5 d8 _, p# ` 一个以上的输人为0时,输出为0。& L& i. a2 W9 c3 B A 4 b7 e6 Y: Z( B/ j; q5 usurrounding an object, measured in degrees Celsius 7 T7 I1 q! v8 R; O# e% b. Z(°C)or degrees Fahrenheit (°F).% U/ `1 Y: p8 b+ L4 K R' L AMPERE, A unit of electrical current. One volt across ' j5 k1 W7 o* v; qone ohm of resistance causes current flow of one% u: W l/ u+ b9 h, U; E a4 y4 L+ B- v# z, s6 d: ]/ O AMPLITUDE, The size or magnitude of a voltage or 3 ~: a& X3 Q4 M) Z2 b; `$ [c7 r, k. Q8 P& R, B ANALOG, Quantities or representations that are ) N6 T e; J8 \0 w+ K# a' B, |variable over a continuous range., |8 u% ]! F( T8 c' \& r2 a ANALOG-TO-DIGITAL, The process of convertin1 w6 e3 X2 {+ i8 B4 V1 N2 C a" x+ M6 N- v( o1 c! R AND GATE, A device or circuit with two or m g: l9 t# p c1 Po 4 x! w; U v, K) F& pis . |: g! h$ j# Z. O) Q* fw# V5 p* a+ ^/ ]/ y 环境压力(地 * W5 Q# y) `4 _( ~& z物体周围的空气压力,用每平方英寸多少磅(psi)来% k1 A) q+ N0 r4 X' w 度量。# u# v6 `+ r# {" M! S( W/ S" S9 h! V物体周围的空+ S: g* w% L( [ 度量。 f- K) r: W2 D* F( k% H& G 安培, * {+ j% L- o( I% E1 k& h5 H$ t电流的单位。 + M7 Y* `6 z3 n6 p4 f& [2 P* Z1伏电压在1欧姆的电阻上所产生的电流为9 G* a7 n3 H! Z! H 1安培 + C* z( g9 k* z/ r- e& F) c振幅,' z& t/ w$ g: g+ x 模拟式,0 I* s4 W- x! H: M( f& V 用连续% o5 d: c% j: L3 h4 K6 a# e3 U# b$ ~) p. R" D7 i" U F从模拟式到数字式, ; X4 ^& x4 x+ ?! C! n与门, 2 p$ e' @$ c, L/ p- L5 m( ^- s) r, e( a( d( H) |/ I! s 英汉对照民用航空词典B OEING $ f4 z6 r! v7 ]+ e5 Z5 j( b5 L0 ^TECHNICAL DICTIONARY 102 B8 K4 s8 w3 k ANEROID, A sealed flexible device containing air at low1 M, n) ?0 [' g+ q: Y, D pressure, which expands or contracts during change of 3 D7 ]1 i- T8 X: K+ i/ C; }ressure outside the device.5 g0 G9 T. i; ^2 ^8 ` ically 0 i5 h# ?& [: Fr changing the direction 2 v5 L5 O% x5 ^$ y* N! Zf drive. i) `! b3 i% R' m! z0 g; Zof the wing chord in; u( z1 Z; w9 C& ] lation to the free stream airflow as it moves forward / M' U+ a: t" d" M; ^9 Zrough the air.6 o9 ]' j2 f# `7 V al axis of the0 @5 x4 V1 V i# H% P( t aircraft.4 G4 M1 O+ w$ @/ x 胀或收缩。9 `5 B# {( @' e. _ ~& H 箱。是改变驱动方向的机械装置。8 f- X3 @/ L( t x$ R( Y( R9 @ 机翼翼弦在空气中向前运动时与自由气流之间的夹角。 ( D% ^. H& g" J7 H% @. z5 ~+ B7 @. qp * E* v' B8 M K# G. }ANGLE GEARBOX, A part of an engine, mechan 8 ^' s% G) t! c* Pdriven by the compressor, which drives the accessory 6 W7 Y1 Q, L7 j t4 h& o5 Pgearbox. A mechanical device fo0 t% N7 u' L/ M: D" m. W- d o % C: N3 `. m( N$ g% K5 VANGLE OF ATTACK, The angle 2 F" ^: F! J$ [2 p8 Tre * g; C' }- v9 k e; V6 mth 7 j, z7 W1 h8 K p, O4 [ANGLE OF INCIDENCE, The acute angle which the 4 V) `- \. G* i' M% T3 l+ nwing chord makes with the longitudin * i) X$ k! N9 D$ a* |膜盒, 6 o5 q! t, E2 ~2 H, m2 c' x, U/ M内含低压空气的密封弹性装置。当它周围的压力变化 2 A$ P: ~# G% y: ~( y时,会膨% N$ v' J7 L& w+ r( R+ U- _7 T 伞齿轮箱,8 T5 _9 g- k4 k; o+ o- k 发动机的一部分。被压气机以机械方式驱动,然后驱动& u# Q. G2 M) i% b% @ 附件齿轮 ! V+ y7 F _3 r0 u5 p迎角, * Q! i9 B z$ l# a' T5 o1 v安装角, , h0 }5 W- C6 Z& j( ^# o飞机的纵轴与机翼弦线所形成的锐角 ) o0 D, i& i: E: c( h" g英汉对照民用航空词典B OEING ' E3 T! X2 y: ]: h' n8 L, ?TECHNICAL DICTIONARY 117 Z7 c" X. R0 |7 _. l, } ANNUNCIATIONS, Audio or visual indications used to9 u( d2 F9 p3 h/ F call attention to an event that has taken place. + _ `" b W$ qANNUNCIATOR, A visual device consisting of a number % _9 E8 z/ \9 c% n6 Lly.6 h: P/ f5 O' b0 B ANODE, The element toward which the principal stream & r' J- D9 \- ?5 x" n) J' W2 z! Nof electrons flows. 3 P4 m. o# t6 H0 V4 V, m; o3 }5 uANOMALY, Not normal.% P+ m1 t' J; u u, C/ f0 ?" E ANTENNA, A device which, used in conjunction with a& M' _: `* P9 K& u3 Q9 W. \ transmitter or receiver, is used for radiating or receiving5 u+ _3 h' V$ i0 T/ _$ [ radio waves. : U* b8 w9 Y4 ^NTI-ICING, A method of preventing ice formation on # i |: K% R1 i+ F4 se wing leading edges and engine nacelles.6 l0 W) T. \; d' \ NTI-SKID, A system for providing maximum braking3 K8 |, Q1 Q- V( z) X ithout skidding for any runway condition. Anti-skid1 E7 i3 U' r# g omponents are part of the brake system.; M( Z& y" o- u 告, ; M0 Q3 W$ g/ |2 B3 h当发生事件时,以声音或目视指示形成的提示信号。, k! o% ^* e3 i0 w/ n' Q. u 与之有关的电路的现有情况或已存在的. L b, @3 N' f' ?' }0 \& k4 c5 U$ r: Z$ l; T" e$ K% E1 f 正极, ( T: h& Z& B2 L0 n# a. C主电子流向的极位。7 Q; i3 N6 ^1 O, U4 W 异常,6 x1 h k4 L) U7 N' E; t 不正常。. @" b; j. u, b 天线,1 p7 _7 N; N6 x7 v5 y 一种与发射机或接收机共同工作来发射或接收无线电 ) l, |) n0 G* X) A7 f波的装置。2 D5 o8 q) a9 I( ~7 g 冰, M2 F O0 v) ]+ t 防滑系统, 3 X; i$ C4 ?( S# S* `一种在任何跑道状况下,都能提供最大的刹车能力而不 8 W! d# b4 n9 \- p& V! n m使轮胎打滑的系统。防滑部件是刹车系统的一部分。 / s' c5 @8 Z1 u. Gof lights. Each light indicates the condition which exists 6 [1 y6 i9 {9 i0 F: Z9 P( por has existed in an associated circuit and is labeled9 m' U6 W6 `$ j5 {8 d' ]4 }$ [ according 2 E5 ]# q, w3 G- pA 0 r# X, A4 G$ [& Fth2 e) n$ z- g i/ S. V/ f' ^ A) o1 K5 h0 y* V/ k* P: Q w 0 ~3 C4 L6 j3 u- T k6 Z8 wc ' m; _% D" @$ Y2 T7 \ N8 N5 r% i H1 b- t1 T5 c% C$ S* X* X 信号牌, 8 M' @* ]8 _- Q; d1 L% O5 o' b# R由一系列指示灯组成的目视装置。每个指示灯都有相应 3 n+ y F& [5 L3 |: a的标记,用来显示 * c: q4 _/ t6 g- o9 {+ @' V( p! S" f: W# P( c4 @4 f9 {, D6 t) P/ X& \5 K 防止机翼前沿和发动机短舱结冰的一种方法。 ! K5 k# O. C6 N4 v; F! h英汉对照民用航空词典B OEING : E% m; F# V# z* r5 I5 t4 TTECHNICAL DICTIONARY 12 . g( l0 o% S1 p1 fAPPENDIX, A supplement to the Airplane Flight Manual 2 E3 G, j8 d: z. Y% O9 q; V5 ]4 ctained in the basic manual. A . P7 l8 o6 D/ J1 g& p+ Nollection of supplementary material at the end of a; D) e$ y* O- @" {% t ook., p! d6 U, [- A, W, Q of the# O% ]: T* D$ m! r5 n& K2 q# ~( e rsion link on the landing gear., n: L/ y3 Q) ]7 {# T+ c7 B6 L# u APPROACH MODE, An autopilot/flight director mode1 ? C+ A. w; P- J d( k which is a combination of localizer for roll control and ' U9 ], j: T- }# \. iglide slope for pitch control. This mode is used when full , n$ q0 l( H$ x; N; _. vinstrument landing system is available.: ^: O2 J. \" t r x* ]( w, \ APU, SEE - AUXILIARY POWER UNIT* ]. n9 o! C* A6 h% j ARINC, SEE - AERONAUTICAL RADIO: i) H7 l' A, Q% e; Q7 I INCORPORATED, H6 A. `# Y7 a( @6 o3 o" _4 N( ? ARM, To make ready for operation.9 g& ?, T1 _# J' E5 { 附录,9 E% U: f2 X" A5 I! F& k- T( {! H! f 飞机飞行手册的附件,包含基本手册中未提到的飞机形# y. T) c8 D; I. k6 M) V 态的其他性能。是附在手册末的补充材料。 . M6 x) n& j4 n' i# C6 v7 E' B顶销,* z8 Z% v) v4 }1 c; o 用于连接起落架扭力臂两部份的销子。+ ^+ h5 j0 |+ u2 |2 w% |1 w 进近方式, ( S0 Y! d3 d; k9 U- a7 @. ^5 Q' D一种综合了控制横侧的航道信号和控制俯仰下滑信号1 q: @2 B& G6 u' n" S& J: ~5 o( D 的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系' v/ |; O4 i/ F o2 V+ D/ G 统正常时才使用。 5 i } C1 V" `, P* d! ]# I辅助动力装置, 2 }! O, k* s' O4 `见Auxiliary Power Unit3 z( M* _: z: j9 @2 ] containing additional performance for aircraft # L$ w m& y1 X- n6 [configurations not con ( `- V* C' o5 C$ U+ M' F8 Yc : G# D* }/ ^, s3 N/ O. q; D1 e7 _b 2 W: ^5 Q5 w) ]. HAPEX PIN, A pin for joining the two sections. N# N# P2 I Q4 g q to# T5 P+ B- e& A" \* |& }, H; O1 _! T1 v: l8 B! @7 d7 @$ R4 O 航空无线电公司,5 Y0 b$ k( `* Y 见Aeronautical Radio Incorporated. 1 y. c; J1 @) |; x预位, 9 z$ ^% a& a' h& u9 m6 ~6 d& f部件可以开始工作的状态。 # `3 @6 t8 |, N% X- Z$ w英汉对照民用航空词典B OEING$ `$ B9 q" C J/ v$ [1 Z$ @# y$ R TECHNICAL DICTIONARY 13 9 [( ^$ k2 @5 s$ S9 b5 \2 e- m2 KARC, The curved track over the ground of an aircraft0 F/ S2 D* z# {; W+ _7 c5 c2 A flying at a constant distance from a measuring, u% g4 E: |( u% }! O equipment (DME). ( g2 l/ F5 k8 r* |0 Gin the limits of self-contained system % H( t- t: | r% aapability. 7 @. \; B4 X3 V* xtem for opposing or restricting; v6 p+ @2 G1 U% B* Y ovement. , {3 c, R- c' r2 [/ c2 `8 d9 TSPIRATED TAT PROBE, A sensor that measures total9 x% N8 U; e) E- b6 L" X$ z ir temperature when the airplane is in the air and that , F+ t u& C, x8 `) heasures outside air temperature when the airplane is & l* _0 F5 Y+ |0 b3 Fn the ground. The outside air temperature is measured H1 Q5 Y- [ B4 WSSEMBLY, The fitting together of a complete structure3 H; a* s. g' s- @% V; d |9 w* g SSUMED TEMPERATURE REDUCED THRUST, The! g/ W! A( O: x; |; a ATC, SEE - AIR TRAFFIC CONTROL 1 x( v- V% ^5 ^5 i% t% o2 F8 w3 q. W% q/ ^$ _, q9 q: J 系统中所产生的一种用以抗拒0 z- N% p- a2 ^! Y" [- O0 }' a! s 作或限制动作的力。 & Q- O1 }+ m" d头, $ o9 G2 K+ k" e0 ]4 L! i+ R5 V用来测量飞机在空中时的总大气温度和在地面时的外 ) J# A# p- D5 k+ c! |温度。地面外界温度的测量是利用引气将外界空气吸入( U# C' [# Y5 p3 |) G3 b/ K! x 头,以达到测量的目的。; v5 f7 z, S. s% I2 E, ]; ~ l, W 配, M0 ?) y ]; w4 a: a( _# ] 一个完整的结构或组件的过程。7 q" w+ @$ {0 l 假设温度而得的减推力, + @2 T1 ~- D: |+ _7 c推力设定值时,假定一个比实际外界空气温 5 g) J- a {' b; F k3 E空中交通管制, 6 l' l; @) W2 V; G O+ D9 Y% B见Air Traffic Control & h. O% P5 t. @$ sAREA NAVIGATION/RNAV, A method of navigation 2 B Z3 [, m+ K, fthat permits aircraft operations on any desired course ) S' `$ N6 p& v ewithin the coverage of station-referenced navigation S' B4 @8 K# g signals or with , R1 j% `* k2 t/ M2 [( {, lc+ I& q$ ?( F5 b Q, Q ARTIFICIAL FEEL, A force developed in the flight( x0 r# {6 `( y0 x5 Z. P control or brake sys, L! u1 o! P3 k; f9 T$ R, f% \* | w m$ p* ~7 E0 [! P9 \! @/ g A: }: m1 g" o( ?/ z& q" O a5 ^+ c% P- l6 }- f7 `2 s# D: a m : ], ?9 W- o# `- l+ Y& Qo # [+ [; J9 J/ _by using bleed air to draw ambient air through the 1 F. q/ N" {2 o7 W6 L: q% }6 [sensor when the airplane is not moving. + H: T) x- V* w9 B3 b1 TA8 ~: W9 [( t; A, Z& B$ G- P or unit.2 Z2 }( g$ e) @, `6 a) G A- Y4 u( @$ v2 O, } lower thrust obtained by setting a higher than actual) B- p% v3 N+ w$ h0 v% O Outside Air Temperature (OAT). c7 J; [; A4 _: n+ {" P! f R5 p G/ B# c8 g 弧线, 7 Q: a. N$ z0 c( l飞机在围绕DME台等距飞行时的弧形航迹。& ?8 A8 |- n& N( p 区域导航,' G3 r4 k4 S, k! A: y* o 容许飞机飞行在有电台参考的导航信号或自备系统能+ x* b7 w( o6 h) H$ b: t 力极限范围内,飞行任何预定航线的一种导航方法。 1 j7 \2 B1 D3 u; @2 m模拟感觉 : j- H$ ^! V2 ^在飞行操纵系统或刹车 1 r+ H" y6 U; C% p+ Y7 n! y2 g; x' Q) I- q. S) O吸气式总温探 , Y" G3 i- d: D/ z3 L/ K3 Y/ N. \2 f5 _: d6 P, d" J! |0 W7 D6 o/ C2 a8 {& C8 `! m4 u- Z% B7 _; V1 ~9 l 组合成 A ^& L% J H2 f4 Y$ B2 a/ C# Q, Q0 W0 Z+ f2 U6 O在选择起飞$ p& O' T d! O5 j 度高的温度而得到的推力。用这种方法可以减少发动机的3 r3 g- c& m+ } 磨损和维护费用。 - ^1 S+ L+ ^2 R5 n- i X; [/ {- d# W# J: v* p% V- i: @英汉对照民用航空词典B OEING * J6 w# R7 L4 FTECHNICAL DICTIONARY 143 i2 a# q8 ~0 {) v7 C9 b* j ATE, SEE - AUTOMATIC TEST EQUIPMENT 3 @ ?8 b) g6 J* z5 TATMOSPHERIC PRESSURE, Pressure of air due to the8 q& }2 i0 z6 [ arth's atmosphere, expressed in pounds per square% j1 X; Z7 v+ j- V5 H9 ^" w3 l) q ch (psi) or inches of mercury (in Hg) or millibars (mB). : s# D. t# S( l0 Q XTTITUDE, The relative orientation of the airplane with6 ~. W% ^' R& I! c8 ?8 z) z spect to pitch, roll, and yaw. 1 |3 b4 {1 z/ @0 Y" Q' qUDIO CONTROUSELECTOR PANEL, The panel in3 Y6 o7 r* X7 Y1 S2 v9 ~5 z/ H; E e airplane which controls and selects the routing of' f% b8 @# {* `9 l* q udio. * K1 N* J, E7 Q, P3 N7 o- v) C( FUTOLAND, Automatic landing using the Digital Flight 8 g$ X# v! \8 g) y+ sontrol System. 2 s g. R1 E& i6 I9 Wn.* ^& l/ v9 V% r2 \& @, [/ Q* x M, A system 5 _% @3 `8 }. V+ M: J9 `: y: Jomposed of all necessary subsystems needed to guide3 N8 N5 S8 U8 W; s) m e flight of an airplane. - ?0 _5 O2 A i& _) eEQUIPMENT, System test 2 `$ `6 ^0 z2 f% g2 D3 equipment that operates under computer control.0 Z! ]2 R4 ^# L$ } 装置,

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e 2 R. D" @& W. d* m- bin 5 k: V4 {3 _# L2 [+ J% w; R* H# Y+ RA! U2 J! Q% H E1 {3 M re% [8 }- U9 J' j* f3 U# I A8 @/ U" _2 [8 q; Q th, o6 |. g, T. i$ w. Z8 J; o a + z5 x; Q F1 F' UA% T. x$ B8 [4 ? G7 u% { C/ \& h8 V2 M% ?9 P AUTOMATIC DIRECTION FINDER, A system which * s3 t5 t$ U4 ydetermines the direction of a radio statio) a. N8 E7 n1 E/ Y& d0 F, H7 B9 F AUTOMATIC FLIGHT CONTROL SYSTE - F7 _* ]0 X6 B! g5 Q9 Xc i! I. h" D [& w) G3 ]! e. i* ]7 I th ) \8 x2 D+ B# t9 N9 Y- c; QAUTOMATIC TEST ) Q" }% O8 H: B; E0 `6 q( Ye0 y; u/ W% P- _& q7 K 自动测试& ^3 c) j2 @. r: o; _ 见Automatic Test Equipment. ! k) h* Y8 P# P+ s大气压力, , k* C. q9 x& k7 E' n由于地球周围的大气而产生的空气压力,以每平方寸多 6 \6 J6 C- M& `; l磅(psi)或多少寸高水银柱(in Hg)或毫巴(mB)来 4 V4 e0 z7 |3 [( p" H0 n( o* C示。 / w- Z' @9 q- L4 Z" ~' j飞机姿态, * ~, q, c8 E+ W7 g- W* d8 y# i. D飞机与俯仰,坡度,和偏航有关的相对方向。 ! t+ C3 ^2 e% e( @" y) B, ~8 p音频选择面板, & S. c) e9 b% w4 Q6 w* r飞机内用来控制和选择音频通路的面板。 ) ~ g( y% Q" e" w) A9 F自动着陆,- p- A/ |1 V9 W/ d+ v& B, s 使用数字式飞行操作系统来进行自动着陆。5 h4 M& J. x5 c: B( o 的系统。 I3 \0 y+ r4 s& Q+ z% o' V( k8 y- D8 K8 B 系统所组成的一个系统。 4 g9 y4 m! ~& _0 J在计算机控制下运作的系统测试装置。3 d7 m% R9 S0 q* r: T3 j5 l: z' i! G. V1 o9 A/ C# q$ U( ^( K4 H0 Q/ q自动定向仪(ADF),4 N$ \% R. C4 h# { 确定无线电台方向 # j8 P- F" e3 K: D% k自动飞行控制系统$ t) T5 w6 T9 O* }) Z 由所有能引导飞机飞行的子: j& K4 l9 f2 \# O+ U 自动测试装置,8 ^' F, s" b( T& @' q 英汉对照民用航空词典B OEING2 P, F: o4 |/ k% \ TECHNICAL DICTIONARY 15( G( }, J7 P. [& D0 F% l AUTOPILOT, A system which automatically controls' ?( N6 N% `6 E" q- d4 z and guides the flight of an airplane. 6 ~+ T: C5 E7 U, Z/ Z8 D( L( dAUTOPILOT FLIGHT DIRECTOR SYSTEM, An& m+ H# X1 d, d' z+ `1 ` tor , \1 _) D: i" k" a% f% u5 RUTOTHROTTLE, A system which automatically 1 p) `2 Y: T; G1 Controls the throttles of an airplane.0 J+ z& H5 Z. v0 s+ h$ p1 \ POWER UNIT, A small turbine engine in) O0 d2 Q# [; Z: B4 |1 T e e airplane for supplying electrical and pneumatic9 s( c3 e% p+ H: D8 O ower for systems operation on the ground or in flight. 6 y/ r: V( D% C) s0 TVM, SEE - AIRBORNE VIBRATION MONITOR0 [! U" p) q2 h/ ~3 |4 g" ` XIAL FLOW COMPRESSOR, A type of compressor: @2 Y* J- N3 ` sed in a gas turbine engine in which air passes through 3 J1 P8 g0 \7 Q3 a( xXIS, An imaginary straight line or an actual physical# x; L( a* g: _% m# X) | omponent (such as an axle) around which a body can ' ?' w/ T% j+ c0 q- w b& Ctate. 2 X/ ~) ?+ ]5 |. \8 I) g0 |仪,; u+ {4 s# {( |( a6 w) W# e% J' C, v3 E) n7 k/ \; s/ k2 {6 N8 y9 @ 自动驾驶飞行指引系统, $ q9 m8 ]+ l2 z动驾驶和飞行指引功能的系统。7 F1 W9 q) S" E0 p6 {6 ?) X5 T- G) @! |. X 动油门,/ T! K! D3 z5 i( n& P/ n 自动控制飞机油门的系统。 ! a$ [6 k; q Q0 Y" O2 N是飞机内的小涡轮发动机,在地面或空中给各系统提供! h: H' @9 F5 u( j |( J4 L% X 源和气源。! |6 I* ~1 f' ]0 o' b0 q 称。 5 M d1 V, h! x9 i# Y载振动监视器,& |" x+ y1 R4 P% ~0 a( X0 d( k4 j 见Airborne Vibration Monitor - p' T: n6 b$ [% \* w' Aintegrated system containing autopilot and flight direc' C- S9 e# B& o9 |3 W5 g6 Y* b; p functions.2 h) t8 |* ~4 I A/ W- L% r$ z( T c . \3 k" G# z) f8 M; T U+ LAUXILIARY + b6 e; o+ ^5 U% hth; H- o; ~4 L, N, y/ G. {$ _ p , O& I5 R% M+ B" J! F; eAVIONICS, An acronym designating the field of aviation 6 j6 ^6 F. \& a3 X: `$ n- Oelectronics.0 Q1 g8 f3 d; I4 K A 1 K; T6 }/ ? T9 ?A( t* j- t) Q# u# Q3 v/ W u( ?9 F# k( e2 G1 S& [5 e4 S1 V7 C the compressor in a straight flow, front to rear. * P5 N! K8 Q2 q' x; RA 7 l t$ I5 X$ d* n3 ]c0 D+ \4 e9 N0 d+ J ro # \; @0 a4 w5 B! k自动驾驶 1 N2 f p5 p' F" `动操纵和引导飞机飞行的系统。 Q, N) x! V; z# {9 j5 Y 一个综合自) O" ~" h: ]5 \! P8 u, l. n5 b; P0 e# [ 辅助动力装置, : H. n! z$ L* o0 r. D: e" {0 F4 u3 \ 航空电子学, ( z0 f. i( _1 }4 q3 h! C是航空电子领域的一特有名 - M2 V$ y7 F3 e. l: S: c3 v9 L6 z, [% A0 C* Y. @% q6 t0 C0 |8 V1 N+ G 流压缩机,* M0 N8 ~, ], t) H/ G3 d5 e: { 一种用于燃气涡轮发动机内的压气机。空气由发动机的 0 J, D- h8 i4 u: E" }4 y部流出。 - N' v5 z# X7 _0 r+ _ w线, 5 u/ J# z+ j- D6 G* i; L- g6 t可让物体围绕着作旋转运动的一个想像的直线或实际; D8 o( P% C9 k4 D* s% T" f+ L+ C" \ 在的部件(如轴)。 & ^ r: D0 ~/ Y/ ?7 x1 k/ j, x. |5 A. ? 前部轴向流人,压缩后,由后4 E$ W3 L9 {$ h4 [2 A& U1 L! @+ b% q; p1 i/ E# g, c$ p0 ^( v9 g) c! y# N; ` 英汉对照民用航空词典B OEING2 k6 I8 g! z9 B& T8 ^5 z) F TECHNICAL DICTIONARY 16 + k A, z' `; G& jB: v' c! C- U# q! q ACKCOURSE APPROACH, An approach to a runway % e, d& O, p0 J" `* Z; C) c+ uversed. 6 u+ n3 T6 x+ T3 A+ S6 D- sown on the EFIS that . o5 r3 \% ~* S8 |/ ~2 j/ Foes not readily change, for example, navigational aids. $ S0 D, V1 z% B$ ?7 Kvement in the tank or reservoir.2 B$ ^5 u: ]" n ALANCE TAB, A small hinged moveable part on the: U6 [9 R# d8 t8 ] ailing edge of a control surface (aileron, elevator, , W' {( `% c' Y" b5 f8 z! q航道进近, . \$ S6 S! u: P4 c7 `相反的进近方向。当反航道进近时,无下滑! ]$ F: \! V7 ~$ M. ?4 W) Y, x. m 显示在电子飞行仪表系统上不经常改变的数据。例如: # b; P1 \4 d) ]3 x; I2 G4 O3 ]航设备。# s3 R u; e6 X7 x8 u6 d. v 在燃油箱或滑油箱内阻止液体流动的隔板。, i( \/ S, `. X 动补偿片, 4 s$ s4 B; @/ y1 ]$ w" n/ h铰接在操纵面后缘(副翼,方向舵,升降舵)的可动部。 : f7 {: \- \0 r P5 H与操纵面相反,以帮助操纵面运 % E1 h3 I/ q: q' S& D9 y8 u1 _B" ?$ {( L" i' [: E7 E which is opposite the normal approach. For a$ s; Y! P, ?. v backcourse approach, glide slope signals are not + t+ J9 Z- I' I& W8 F! P% Wavailable and the sense of localizer signals must be 8 H- m, l! c- m# z" Z. Ure3 j& _( |, D b. ?, u( m3 D BACKGROUND DATA, Data sh ( o' Y! F9 Z* U5 N) ?d - n+ S; T" D8 a" uBAFFLE, A partition in a tank or reservoir to prevent! Q' `3 }& q/ a" C. ^2 g" y fluid mo * ?6 \; K! h3 a7 V$ {( uB 4 _) b5 U" [' Y; H+ L1 |tr' m! z7 }, H9 ]+ [. _ rudder).The tab moves in an opposite direction to the/ |1 m# ~( H; }0 a! D/ P control surface for assisting movement of the control7 D/ o4 ]4 s' P* I surface. " Y" E& q! _6 B; J, j8 Q1 N+ v2 U, I; y. U7 v 与正常进近 8 n9 h P+ o* p2 X8 h& y1 L道信号并且航道信号也必须逆反。* ~. N* y* i9 ~/ p 背景数据,/ n0 \5 a$ H7 k+ e( d* R: V) r0 [/ V4 u) l/ i n: r7 l缓冲隔板, ; a: r: V" A( `! l% F$ j9 j7 k: `* V& [ \8 T P. U 随动补偿片的动作方向2 ~, W( E' G, [; Z. I+ ^ 动,减小操纵力。7 S4 G9 _- d; H) Y# P! X: L- | 英汉对照民用航空词典B OEING# Q! I7 p% X' F TECHNICAL DICTIONARY 17 5 B0 L! D! M8 a. l1 C9 ABALANCED FIELD LENGTH, The field length! z0 Y6 ]. Y* s9 M! @0 P+ ^ associated with optimum aircraft performance when + Q. ^) l7 l5 o% G% T3 c7 sbstacles are not a constraint. In this case, after engine2 x) h3 c3 Q" U! ?9 ^ v: d! \ ilure at V1, the distance required to accelerate, takeoff' s: u. t0 n/ S4 V8 L& o nd reach a height of 35 feet is equal to the distance $ w# }2 L) R; W; p6 PALLAST, A weight installed in an aircraft to maintain9 E. r" N; ~9 J7 B: Q4 [ ALL NUT, A fixed spherical nut driven by the 5 v0 [, ?5 g0 ^5 m' v( BAR OUT OF VIEW, A signal used to remove the flight , q3 }- Q4 |* ?1 j$ U# jAROMETRIC PRESSURE, The pressure of air above% D) P$ Y4 A( L2 q g) or0 y0 Z& u5 i. S& N; Y millibars (MB).9 l0 H9 n5 F6 k. f; U ATTERY, An electrical device for changing stored& Z* R8 C. |+ X$ i 性能的场长。在此 ) Y* O5 Q* j ?况下,V1时发动机故障,要完成加速、起飞、离地35: B$ p; N7 C t3 I6 R 尺所需距离等于相同速度下完成全停所需的距离。 1 ^: ?# D# s }0 V舱物,4 p j' l8 i. i4 d1 } q( i! }9 {% D 重心在许可范围内面装载的配重物。 ' o" J/ F: C/ B2 D, e4 q" o+ \4 ]形螺母,5 ]; j7 H1 K* x/ ?2 S4 {' }% W 的固定的球形螺母,用以使襟翼和水平 - O9 C; B$ ]4 @, y* N7 P引杆消失,/ | z6 Z& s) l7 N' ~1 g1 q 指引杆的信号。$ D" c: U' `* P5 k6 I 压, 2 T9 ?4 v/ C( r4 u- g S" R. ]压力。通常以多少寸高水银柱(in( g3 ?4 M8 |0 W2 {4 T 瓶,3 J) c% D, p, ~ 的化学能转变为直流电的电气装置。 4 a1 k" q! e* m2 h; N) yo6 P9 b! F% @: i0 L fa ! Y( Y% s* @& Ea3 n& i) f3 O* g; g/ Y required to stop from the same speed. ! z9 M8 S) _& E `B6 \- C4 ?9 a3 r; [& ` the center of gravity within allowable limits. # P) `5 J4 P0 l6 WB2 ~5 b t. [9 j0 u% Q jackscrew for flap and stabilizer movement.! u( G4 n8 P$ \; ` B& Y; V5 k9 b. e8 X( s; c" g9 T director command bar(s).' [ P: b' l: w; e$ D B 2 e# f0 b3 F# Y* r) Kzero pressure measured in inches of mercury (in H % [# a/ L- O3 p" Kin* L% p4 k, J6 f- [ BASE METAL, The underlining metal to which alloying ; j# F$ x7 Z& J7 I, L& Jagents or metals are added. 5 M' _. A! i" }9 h& m3 d3 I* _% jB7 u y" H8 o0 s) e+ A" `4 L chemical energy into direct electric current.) C4 }4 w; D) d6 U! s 平衡场长,6 M/ e' G5 N0 v3 Q$ T- }7 t 当障碍物非限制因素使飞机达到最佳 * w4 ]3 N3 }8 w6 e" X" S1 D4 E: d, X# t# S9 D6 |6 `6 `% p% N8 [2 a+ q Z6 v- T' k# a4 E K$ b为保持飞机 0 Q1 {" W9 [ m0 S# B# D# `! }2 [3 e p1 |由粗重螺杆驱动 * p$ c1 h: Y3 U r安定面运动。% b- `% ?4 W& ~0 k* G7 |" a d; g [, w7 @用于除去飞行 0 p5 p; P1 o8 X1 C2 Q& q9 R9 \! ^5 p5 N4 E& {; [3 l" `( t零压力以上的空气9 {( _( B9 ~& m+ v: G Hg)或毫巴(MB)来表示。( q5 v1 ?$ S1 A2 [4 B+ V 基底金属,: z/ k6 |6 N' m U. U( `/ u7 a, M B 指合金中的主要金属成份。 $ h* b' |; q7 e3 A: x7 ?0 o% } q* ^2 R/ O: W' k将储蓄 $ j h+ y% O9 g- W, R7 d英汉对照民用航空词典B OEING5 m0 l& h. i O& r/ e TECHNICAL DICTIONARY 182 {& |" ]! D4 e) T5 B) A& p BATTER' R8 L: w4 }/ Q; R direct cu ]/ B8 p& B L5 a power su4 f+ M( ^& o) X. U2 e Y BUS, An electrical conductor supplied with 0 h& b% s+ V0 W' u) l: prrent from the battery or transformer-rectifier for 5 E0 q6 R# B1 p. Epply to operating components.+ k" w: g4 ~3 h1 w+ B/ ? CHARGER, An electrical device supplied# D' G6 w2 C! n ith alternating current, which produces a direct current, A6 `# F: _+ n7 s) n! V: f5 h2 S utput for charging the battery on the airplane.- a% U+ L! P2 p: W: } AY, A compartment in the airplane structure. ( u% F+ z7 B; V/ w$ w0 N8 ZCD, SEE - BINARY CODED DECIMAL ' V1 A# H' o& |0 fEACON, A device which emits a signal for use as a . l0 K. q: j! v- b+ Tuidance or warning aid.1 N" E7 @5 v: d2 K# P2 w& q9 f BEARING (NO. 2), The direction from an airplane to a3 A- z9 H0 A% i- r; D ground station. 8 _" t4 ?! `- G* ]- R# @! K1 P/ ^瓶汇流条,7 y" o6 b- {1 D 将从电瓶或变压整流器来的直流电供给工作部件的导 1 H. K% V8 c. t% X! R e体。 6 w3 O4 n% ^+ V# I瓶充电器, 3 Z+ h' u3 m* K' K用交流电向飞机内电瓶充电的电气装置。带有交流电的 % O& o3 e! P% x4 c& c气装置,该装置产生直流电向飞机上的电瓶充电。% }4 t; W3 K& m4 d 舱,/ z1 a+ J) {. ~9 N8 t 飞机结构中分隔的空间。6 y! V5 ^1 A7 p5 U! G9 ? r 二进制编码,. `3 u: Q, p' s) z0 E. R/ R0 ^& h 见Binary Coded Decimal6 i7 ^$ R- y! h* E BATTERY 0 e' k4 e9 {& W5 E4 j) F Gw 9 Q8 G' s# j- ?o ( N- E Y" o5 ?; l, r' rB: b+ d2 Z9 U9 G* F; D) T B D8 f; _& {2 j. ] [, xB# e% `: |7 z. Z* n2 ] g 7 D% {" Q, J3 `# t) @+ Y5 YBEARING (NO. 1), A surface that supports a moving / o* H. ~5 y/ v; T. Lpart and reduces friction between the two.1 H( M% i L0 B$ c- y, Y5 D# Q* O5 j+ O$ U5 M. X, ?! }) ]! u7 Y- a. ]$ t4 x. j7 k k% M" y& r) G' O$ A5 V/ ~$ e+ O, ]+ ^5 f/ t8 l y, }) |$ y$ ^7 u+ y 信标,( R8 ^5 a4 M6 b \6 m! } 发射引导或警告用信号的装置。 % }8 L! A) L3 y/ ~7 @方位(NO.2), ) ?, d0 P1 f3 m: M% u. \3 b% ~从一架飞机到地面台的方向。 6 H6 ^: ^& A, ^" b$ L; U轴承(NO.1),6 L8 Y% m0 {1 [ ^, V 用于减轻机械转动磨擦的机械装置。" h: H; P' R; Q$ n 英汉对照民用航空词典B OEING 1 e! U6 z# n2 @' JTECHNICAL DICTIONARY 19* X% g# u& x8 ~ BELLCRANK, A double lever in the control syst % l8 j$ w! h6 E F6 M4 \changing direction of motion.( j0 o& A! X) }) Q' J, P em for / k' H: O @5 f& Oct in the$ M9 f* p9 I# p( \( ^9 m neumatic system for absorbing expansion of duct due ; h4 d( ~3 |8 t7 B& }$ s% oheat. B. ^+ a# Q) lELLOWS (NO. 2), Corrugated folded or pleated! h/ o, E" J t' } ontainer or compartment used to measure pressure., w0 t3 o( n3 s9 |+ b1 K5 A; `, m EZEL, The part of an instrument case for locking the. j; l+ _' z! i$ l% C lass.9 V: `0 p, B' o- g( H; J IAS, The potential difference applied between two 0 O8 U) O1 @7 ~- toints for controlling a circuit.: e3 ?6 ]2 @; h1 } BILGE, The lowest part of an aircraft fuselage. A place3 L& M0 j* d2 f4 ^ where water, dirt and other contaminants collect. ; e0 G- `2 p+ D$ p6 ?气源系统内提供管道热胀冷缩所需要的余地的波状" X$ u+ P4 D1 P) B% i9 x+ V 轫管。" c8 ^. \) E/ c. M; I6 H' z8 _ 空膜盒, * I4 a, v4 V3 z7 Q一种具有波状表面的容器。用于量测气压。# M4 k8 ?& \# s' [4 G% Y2 x 嵌沟缘, L+ K% q3 u4 F+ F将表面玻璃固定在仪表上的圈状零件。2 W1 o }0 c4 y" F1 s# q( M 压,( Y4 W& O1 _/ E8 z$ V: @ 在控制电路的两点之间的电位差。+ i) `/ h( C' C 机身腹部,- z% S, N/ B% @) T, o5 e 机身的最底部,通常水,脏物,和其他外来物集存于此。& t5 b: ]# Y) ?# t7 l- E! N9 Q BELLOWS (NO. 1), A corrugated flexible du 8 {# K. n# C+ ^$ x8 ~. ` T) s, Rp8 G C7 q) i# y* |! \7 q to% U% ~ h1 E4 q9 }1 _ B* {7 i) e3 Z# a4 j* M c 0 a/ P3 z6 T: V1 s+ e" f8 n: AB) [* O8 i" m/ a# \ g" R5 [' f, m# r9 x1 h/ v, e% X B# a; M. C6 p# f$ v# K( N p 5 I( q, M0 w! g L, m! M直角摇臂, 4 R* m' m. F* p在操纵系统中改变运动方向用的双臂摇臂。: M+ J! K4 c' [! H 波纹管,/ [5 p2 \5 G% \; P* g1 x0 t5 L' M/ q- Z: S' Y- v: m" `3 _0 c/ l# B: T% Q( v* G5 r- `+ a' M; z2 \% F) o. b# E8 {, r0 T% E4 e 英汉对照民用航空词典B OEING 5 x; c4 B: {9 r& z3 ZTECHNICAL DICTIONARY 208 R4 h( c, {1 V8 H" g+ ? BINARY CODED DECIMAL, A system of coding each- e6 G& O$ U7 I- m3 r' I$ Q& F digit in a decimal number using the binary equivalent. " L. f7 R& d" ~6 l: P8 V. y5 }: iBINARY NUMBER SYSTEM, A number system using ; J0 D! N. B7 m7 Q* l2 [s ! F! [5 I, t$ G2 P! R% FIT, In the binary number system, the smallest unit of: j) L1 C a B# o' j formation, consisting of a 0 or a 1. ' x& c- H# x9 x$ D Z* T( Y" CITE, SEE - BUILT-IN TEST EQUIPMENT - }8 H {0 ~/ S& s9 B: ]" }LANK DISPLAY, A display that does not have any# D7 [. a C& J9 h' o' e dications, normally due to failure. 6 C. D- O$ k, U) \( O/ i' j: ?7 kLACK BOX, A container for electronic circuits to record* m, r/ P6 A( z& f9 d E" z ight data. 2 S7 A2 r' }& f0 fLEED AIR, Air taken from the engine to power various5 |2 t+ _& m. c9 h$ U ircraft accessories. 0 |. Y1 i* E9 q5 ?A valve in the pneumatic system for air! t4 ]3 {" b5 g2 @ E2 {, U supply from the engine or auxiliary power unit to the ! {* P+ p" E- o) T3 R5 I' Opneumatic manifold. A valve on the engine for reducing 9 n# y/ _5 z- M" |5 w: }pressure in the compressor section. + F2 j0 r1 ~* H) P进制, 1 z& s! `. { V1 T% Y2 N- M+ X进制,; ^- Q( l. F; c! d* S8 N) H+ D 一般用0和1)和2为底的数字系统。 4 `9 ^; g% K1 m3 Q特(二进位数),+ D' g4 Q2 \; C+ S 二进制中的最小信息单位,包括0或1。 8 v: Y% M9 n9 \2 e- s: A/ r内自测系统, . ^. p" l: g5 }% G- z8 e: C见Built-in Test Equipment ; K4 M4 ~2 l- Otwo symbols (usually denoted 0 and 1) and having 2 a5 C) q7 w- |' ^9 @4 N# Y7 Z its base.8 l# n( M$ ~" d7 n3 Q* ^( w B7 r8 W2 ~2 Z- p! E' A/ w' p" o+ R in 2 U p" `% D. d0 m1 m. A* `B 0 X! k+ l9 ~# U! Z; q oB- c% Q% u9 y, T! R in 4 C) e% z% S3 R4 F4 ?7 qB 8 {5 {2 u+ y) {2 |" f$ R# ]fl$ K V2 C/ ?1 r5 l/ W0 z B ! N* r* q) ?, V; {; Y7 X: Ka# u( e7 E* Q4 S' }; @ BLEED VALVE,- ~8 ?, U4 C: X4 p" Z5 \# I5 N 二进制编码的十 1 x4 w% J8 O, _# G p一种编码系统。用等效二进制位数编译十进位数的每一 / ]* a- ~* l5 ^3 r( Y' U位。2 T5 R. {+ \3 ~! T% l+ B" O1 R. s& ] 以两个符号(5 K9 L Q6 f( r9 Y2 z5 u7 `: [* B* t4 K! A! X& p) K$ `" e# i+ T' v. l7 q! D .3 f* v' b) s% q/ _8 c6 n D0 {3 K 白显示, ; r9 P5 f0 o7 V) r通常因故障而造成的显示器上没有任何指示。 + F8 X& O* U8 W# z; B9 V# G匣子,( k$ P K, f, X; y 装有用于记录飞行数据的电路系统的容器。2 Y2 A0 d" K: u! @1 n) |6 F 气, 9 e( t% p0 m' `: X+ b取自发动机而用以驱动飞机上之各种附件的空气。5 P" R9 m9 e" O | 气源系统内,使来自发动机或辅助动力装置的空气进人! o) o/ W' F* s 气源支管的活门。发动机上,用来降低压气机压力的活门。7 |7 i" b) g$ j% X. U+ w& D" J- Q2 I) x! |* V8 A9 m' B+ Y/ Q" C2 r& u9 \2 f7 H/ ?6 W; F' N* E$ A$ d引气活门,! P1 \3 |. i# S 英汉对照民用航空词典B OEING ( q9 L$ ]7 X& T+ e+ e S& gTECHNICAL DICTIONARY 21; B% ]) M7 l4 c& t" A8 m! g BLOCKER DOOR, A device on the engine for blocking6 S2 A% h7 t: v) e }0 S the normal airflow during thrust reverser operation.+ N2 Q4 R' X" V7 j( k+ ]2 f LOWER, An electrically operated fan for circulating air.! p1 `. e5 f, r LOWOUT PANEL, A panel in the structure between # x0 w8 U' \! m4 m. K, eo compartments that opens to equalize pressure in3 Y& U9 U6 ~5 A1 q3 ]/ J9 F e compartments. B$ w+ K I! ~ODY GEAR, The landing gear attached to the% | j* [0 O. S+ k( O grounding. ' ^: h4 R& `- f( @/ i! [0 T正常的9 A9 e4 C+ Y2 c 气流。 * `, ]3 a* d: j& \: T0 R9 r5 w鼓风机, ' b9 @# ?% m+ e( ?# e' m用来使空气循环的电动风扇。 3 B3 D& A+ Q M- c' D压口盖, : f" A$ N Q( i( v9 D两个隔舱之间的口盖,打开后可使两舱压力相等。$ n8 m$ a, C# q7 m 身起落架,. U, O! a+ j& a- u, G. A 身构架上的起落架。 # s! k; _& T2 L+ lB' g3 d; H* N* @5 w0 X+ t B- ?7 Y: Y$ G$ w/ z# \ tw & x. |3 }3 j$ k* i& }! Rth4 l' e6 W% j, d B & O+ H: J' N3 l ?& X) A& Afuselage structure. & U$ G3 ?# ^) g. U7 W* UBONDING JUMPER, An electrical connection between6 A1 p) ~6 L. s0 \) g1 k# {5 V9 v a component and airplane structure for electrical+ C a1 y$ h, p3 Y5 ]0 f 阻流门,+ P8 {! f; l, |0 {; v5 u' f z 发动机上的一个装置。在反推工作时用于阻挡4 P7 H% S Q e. L7 J8 O' v8 z# H: r5 H( m. M' z. ?; K: z* g( H& K, N- P1 u+ a 装在机 + ?! g, P6 j; q4 Q* L搭接片, $ r* x" x; K3 R& g9 n7 j {连接某个部件与飞机结构以形成接地的电接头。 ; L' m' s4 p" d% W' G- w/ d. a英汉对照民用航空词典B OEING- p# x4 e W4 R* i TECHNICAL DICTIONARY 22 " Y( p2 A( l; E! P2 c3 kBOOLEAN ALGEBRA, A mathematical system for/ M1 Q' g) c7 g) [ writing combinations of logical statements. z! ~& W1 K5 y9 [ BOOST PUMP, An electrically operated fuel pump for0 Z% _: P$ j. r; } fuel supply from the airplane fuel tank to the fuel& a/ B1 t5 X+ L manifold. 5 Z1 ]9 w- v4 ~: q: l8 t. N) A7 sBORESCOPE, An electro-optical device for looking at , A) [- g8 D; k7 iternal parts of an engine through holes in the engine.. S; a: h V3 W$ u orescope ports) 6 R5 N; C1 n# Y" {OURDON TUBE, A curved flat tube in a pressure gage8 \' L. x. ^5 i5 a: f: n5 k) y6 I3 g r moving the pointer when pressure changes inside ' W% O6 h& e1 `- ron the ability of the brakes to 7 L2 l: ?# _: v ]/ n. Xbsorb a predetermined amount of energy during a5 l5 Y1 t# {* y jected takeoff.0 i2 e4 C! d3 S. S 用于通过发动机内的孔(孔探口)观察发动机内部件的 X: R6 x: t; E. _光设备。 4 t* ?0 l1 u; {0 Y) {7 I/ t3 D! I端管,! J8 D' `+ B2 E' u! d% A z 测压计内的弯曲扁管,管内压力的变化时它使指针移6 {, m$ F- S A0 S/ Y) t# n) n 力。 $ C& R/ c3 ^9 [1 Y- u) c# p极限重量, # {: ]6 R% n5 ^3 k% V d- ^8 _$ m9 M _- g6 D0 D 起飞重量。" E1 D' Q, ], Z" U& u 发动机滑油系统与大气相通的通气口。2 b0 n, _2 q J$ B8 k6 o: R Z in 4 ?- `9 M+ v8 d. N2 e% O(b ! [; u# x8 a1 b; VB9 H. [2 _ D& M' z" p- a fo % N$ U$ }2 I- Gthe tube. ' H7 d2 {2 H5 u# C* oBRACKET, To enclose or surround.* j/ z) }! N/ ?- b# j# q1 w BRAKE ENERGY LIMIT WEIGHT, The maximum 9 B1 S8 ^' I6 g* R G$ Ctakeoff weight based6 d( X! R: k) J+ R; J$ `, F n a ; u2 }, |" ]7 M- |re) y: r# _( _* _ BREATHER, A vent to ambient of the engine oil system. 4 N% K5 I' @% t) O/ Y( L6 S; e布尔代数, ! }3 E! O- u/ S& N0 x# A$ Q一种用于编写复合逻辑命题的数学系统。3 P$ i- {9 s$ |- @$ G% F0 N 增压泵,. }6 M. o( B* ]& o3 I3 i5 d& ?. K 从飞机油箱向总油管提供燃油的电动泵。3 ~. w" h* k) y& o4 ? 孔探仪,% `# X& V% c, h, G6 e( b+ G5 _' K2 ]1 P6 ^) I' z* P, |! K6 a" @6 G7 ]; L动,以指示压 1 k) o- i1 ^5 A托架, {- f! N' Z; \+ B6 o 用于作支撑、装托、或围绕之用。' _2 l! i3 Z9 | 刹车能量( L9 k b3 M) T8 O G 中断起飞过程中,取决于刹车吸收预定能量之能力的$ @# h/ q* M K" C4 y5 P8 p1 L! Q2 |+ Q" `3 {通气装置, / Z5 P: i! e) e& ^+ B* z英汉对照民用航空词典B OEING ) V3 {3 G/ {7 _# P& _ gTECHNICAL DICTIONARY 23 " o2 d3 H m5 P1 n3 ^) QBUFFET, Vibration of the wings and airframe resulting( n8 E) ?* x* h from unsteady airflow over the wing; caused when . N1 Y5 Q' Q7 c. |2 H/ Iairspeed is too slow, the bank angle is too steep, or 8 A) p' V$ @# W. Jirspeed is too fast.1 n/ m. b P3 u. [* C% \% d UILT-IN TEST EQUIPMENT, Equipment installed on 2 f, |4 `4 K1 K" A |# A# K7 Oe airplane and in airplane systems to test the systems9 x9 b6 o# O8 T( c, w! @ ithout external test equipment. ( U- G' a0 u+ w- oUFFET MARGIN, The amount of residual maneuver4 a3 ?4 l+ z$ n% m8 _ apability present before the onset of buffet. f9 J! J# k: @5 S+ T6 Q; ~. \ UG SPEED, A preselecteed speed to be observed7 P4 j3 _+ s+ H8 A7 J8 o/ e nding sequence.7 o m3 U; m1 p4 X" j& g# i O k! A2 f6 u' X" K ng landing gear operation. 8 p9 H- {0 e" N1 |( q+ D速度太慢或太快,坡度太大,均会引起抖振。5 i e! S% P/ v* j8 o' v 自检设备,6 Q3 ~) O1 D) M 安装在飞机和飞机系统中,在无外接检测设备情况下, 0 M' t) @/ h; S. \/ `3 w1 c1 F用于检测系统的设备。; a% \3 k* Q; O. K 抖振裕度,' m+ ], A7 M5 V- |2 s+ L 飞机在遭遇抖振之前,剩余机动能力的大小。) i1 ]! `4 b7 j' e' F 标速度, & y/ U5 J; ?3 W s P9 J7 y在某些机动飞行过程中,特别是在进近和着陆时,飞机" f9 c- \1 d% O" l 预定速度。 6 t7 S5 y. _8 S* z$ h' P, e; k力装置, ' Y! r- N( j9 _2 I' H( D架工作的一种机械设备(弹簧或减震器)。" l8 T" I3 q& z9 a 流条,: N2 L k3 s3 V: S% O 在部件或组件之间传输电、数据、或定时的单一电线或 ! a' Q; t3 {8 G% @" l) T+ wa / ~5 X+ y# Y% g7 H8 S; E/ LB7 l6 T2 v l9 }+ W2 a/ h& ` th ; m2 R# Q A; \9 `# Cw0 O: }4 Q3 b. N( e, R B 6 }; `- G$ x' p @0 ~c : Z W; T; U* |, h( q) o: eB e' X; v/ k( e7 h0 T4 x during certain maneuvers, particularly the approach and 4 S6 J0 [ f0 q2 P! |, M3 Tla " z! m+ {0 ^8 z9 l0 [* q/ eBULKHEAD, A structural partition in the fuselage or7 ]* E1 m& x& Y% e$ m wing. 5 ], E; l3 L+ C5 F% {BUNGEE, A mechanical device (spring or a shoc( q4 r) k) ?1 |9 H# J8 c! `) W absorber) for assisti$ U2 l" M9 E3 \7 L3 \# l. r. y8 M BUS, A single wire or group of wires which transfers ; w# M9 ~ x3 U$ u2 ^% ~- zpower, data, or timing between several units or 2 U. ~2 f" Z2 _! e2 R+ c( s1 v, |# emodules.: p& L7 y% { ^ I& i% n: P% \' w 抖振,# K) G# W. ^: [( y/ Z0 V8 f 由于机翼上表面的不稳定气流引起的机翼和机体的振* g) X9 Y* O' D0 }. o 动。飞行 0 f* ~- `- i3 K7 K* y8 o! n3 M% ~' Q% S& B5 L/ ~. a所应保持的 / @! a( q5 x/ [9 v ?& z6 f4 s. ~壁板式隔框,9 L' g, \. V) P- x* o6 I 机身或机翼内一种结构隔板。! D6 l5 _- T5 A6 B. v$ D* e; Y2 q' } 用于协助起落8 L( X8 K1 O; L! N' M. p7 t* k7 S( {, K电线组。 K' P/ ^. O* R$ G3 c英汉对照民用航空词典B OEING3 u, J$ b" V! D4 y# @ TECHNICAL DICTIONARY 24

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BUS DRUM, A mechanical connection with pulleys5 R2 o9 [ Y! [; i# D2 K8 L1 e cables in the control system. H6 @& @7 R- z! e' d+ w3 e Wand: z; ~/ g8 Q0 }, G. I9 u1 x l circuits for control and protection of: E4 B, W: E1 y+ i3 S lectrical alternating current supply to the airplane.! n' a: S8 H4 ^9 p% H duct for closing and opening the duct2 v% {1 F4 h* Q+ \ assage. 6 S& E$ L/ a+ k3 ^+ k i; jUTTOCK LINE, A vertical reference plane along the . e A. N6 S0 t/ p9 C' d5 {selage for horizontal measurements of the airplane.4 R, b0 O" U# F/ g# l 接。 7 V. R* X% C: g0 ?; b组件,内含控制和保护飞机交流电源的电 * D. P/ \5 [2 w* q* c3 [4 {( ]: l- ~0 B5 Y6 Y9 W2 k作动简控制的转动装置。用来关闭和1 N4 N( Z, @. D% m5 C 启管道。0 m9 X6 ]: F, s% Q8 B5 q 沿机身走向的垂直参考面,用于飞机的水平测量。4 d) {6 q* ]2 Y* J1 _ K# l BUS PROTECTION PANEL, A module (black box) " o* b8 n& Q" p2 x. z/ kcontaining electrica$ b: c7 C. B2 H& V3 F. P0 \# t e $ k+ q' o# K% Q" ~ ~# c6 D' n& E, nBUTTERFLY VALVE, An actuator-operated, rotating! C( r8 h+ d5 M% v3 ] device in a. t; y3 v- N+ a' Q0 ^ p * v0 {6 R9 H; |( {9 _B3 m9 H' I0 `: }( N/ G# e$ ?! a& I3 w7 V fu & k* B1 J1 V* J/ W转动鼓轮,- x2 A/ s) ^ Y+ r5 k 在操纵系统中,具有滑轮和钢索的机械式连0 n2 T, i9 ^) Z8 r7 e 汇流条防护板, + N1 a; b- a+ U/ k黑匣子式的 + Q" L$ U" m- ?9 e& U, ^7 Q1 v$ X$ M; ~$ V+ [蝶形活门,; `, m- x4 S3 ~: O, j, M6 @. n 是一个在管道中由0 y2 g3 d$ T& s8 U) H: q) o1 o6 u6 Y- T) p 纵剖线,+ ]/ {# p4 ?0 {* k% `5 f& J 英汉对照民用航空词典B OEING : x( b/ p% W. T" U- w+ TTECHNICAL DICTIONARY 259 @- n0 a, N+ n7 b BYPASS VALVE, A valve through which air or fluid will ' ?: X$ ?# V2 j% z" Gflow if the normal flow path is blocked. ) x% q: Q5 y8 N9 L- {) lBYTE, A group or string of binary digits. A byte is- @8 N2 i- R& a6 X" l3 X sually eight bits long.5 S8 |# |) q" J& V5 E; M# n ABIN ALTITUDE, Atmospheric pressure maintained 2 N1 e7 [5 _/ y& U9 jithin the cabin, indicated in terms of feet above sea7 B: j, ?! l' m; m. [& C0 f6 M ALIBRATE, To repair, adjust, fix or correct the4 k' r+ l1 W/ [0 B3 z7 X easuring capabilities of a measuring device. ' k; e* c- h. ]ALIBRATED AIRSPEED (CAS), Indicated airspeed 7 B* b. A& X* l5 l1 ^/ D/ vAS) corrected for position error. / o: y! @7 O- \- ~+ X, `; Y1 j1 D4 ?nical / M0 S. H, C& ]7 d9 Domponents. 7 x) S/ P7 Y5 f1 {4 p% f; v8 w" \ ]( L. D$ P 节, , K+ \6 k+ Y' a. n一组或一列二进制数。通常一个字节长8位。 . I2 n) a" k8 I( T) ~5 F% G舱高度,1 J8 f ^3 u% Q& @* Y0 N2 a 座舱内保持的空气压力,以海拔多少英尺表示。) r( P/ A4 t$ U 准, 3 }& R/ V! `& `7 }0 {4 `, {修理,调整,定位或改正测量装置的测量功能。 * N) ~# a) T8 V2 `* ?* j7 l正空速(CAS),2 F9 B. T. d2 }; N1 z' R 在修正了位置误差之后的指示空速(IAS)。 2 M& K: F, ]3 z! }6 ~用来移动机件的一种转动装置。% ?+ R; S2 U$ t+ C7 R1 Z u ( g4 _) a' Q" B- E0 C) E s9 h" r0 ~C i% k+ u# M0 ?2 M* XC1 T5 X* X0 E( E# F- \ y+ ^; N w " i* _- M1 k- B, ilevel.2 j9 t' s: v' ~& B$ t4 B C 6 V3 R0 ~5 M# ?9 Hm * V1 S4 C1 _6 y( J7 U$ EC 1 g9 M7 l" ]! U! G(I: s* O* K# X8 P CAM, A rotating device for movement of mecha. c, l6 |2 E5 D5 h) X; B* H# ? C 8 R* b6 j x, F& H旁通活门 4 ]' ?% @; p. I& u1 s6 @* a气流或液流在正常通道阻塞时所经过的活门。 ' h; m$ P! X; l" H. @7 S# n% |8 r" g" k! C) A5 N$ z8 q% |$ T6 {/ c. B" ^: j5 p) I* c& n. q' D# l! A1 W! H/ `% C# b/ X) j凸轮,0 w' g9 v" A$ X6 y 英汉对照民用航空词典B9 d, ~3 Q. r9 s; j CAM-OUT, An autopilot condition in which the actuator & U. a- k: U3 `: y( rdetent piston is overridden, either manually or by the 3 ^ i! c! g3 r8 B6 l, ether autopilot actuator.2 w/ Y- s9 {# r0 P [" I AP, SEE - CAPTURE6 r I N6 _7 K3 i; Q APACITANCE, The measurement of electrical energy! ?# \( }2 [1 U# `, q0 _8 G tored in a capacitor (condenser). & @* n. m4 q) o/ N$ d' k# HAPACITOR, An electrical component of two metal 7 D* J5 y0 M+ w8 _; v, i& Plates separated by a dielectric material, for storing- O. z8 M; T+ e2 ~) c8 g( R5 ] lectrical energy.$ p3 M. e, m5 A/ F( b2 m CAPTURE, An autopilot or flight director function to ! d' T. c T9 B* d+ oacquire a selected mode. ( ], f8 x0 F4 x# K( C! [CARD FILE, A container on the airplane for printed / D- c7 \0 u! g: B$ C# ycircuit cards.+ t' V+ H1 w3 B7 p0 c* ^1 K 一自 ! l$ ^7 [) X' i/ b" t- ^动驾驶舵机所超控。 9 J1 }; }; o4 c9 A8 v; V截获,2 H5 r7 M; j; c2 c5 W$ _& h 见Capture6 }+ f0 `: B/ ?: |) H0 t4 E o- d, Q4 y1 V* F( R t' L C# r- Q5 `; j: s" G& M C # M6 I- a; W& ]/ zs$ O) b1 T9 B& {, s C+ A5 p& Z3 N) b3 P: Y' x: O p! `3 |3 f# f2 l$ e e% ^; J! w! n% ~6 x7 A$ f+ J9 J 凸轮不工作,1 T' O e+ q6 v1 B! W& H 一种自动驾驶状态。此时舵机锁定活塞被人工或另 , n* p* I) J& |+ U6 Z( w z/ P& X7 J, k: Y 电容量, 2 n+ ~8 |8 f/ |. e+ Q电容器内所储存的电能的量度。* y% Q( x1 e: x. `3 y/ y 容器,$ b7 O+ L) n& @; w V& L 两片金属中间用绝缘材料隔开的电器。用以储存电能。0 z1 \$ I: ]1 [" d b5 v4 } 截获(CAP), 0 p: Y' u; Q; T- R' E2 J, [自动驾驶仪或飞行指引仪的获取选定方式的功能。, b# p* _9 U, a9 M4 ]' [3 c 线路板盒,# u' y# A* d6 n- J0 g4 M0 N 飞机上安装印刷线路板的容器。 & d% c3 Q2 u2 [8 u6 l$ {, B" D5 Y: @' n9 v OEING1 K& r4 g: r) S TECHNICAL DICTIONARY 26 % E/ K# `. `/ @2 A英汉对照民用航空词典B OEING) ^6 P5 v2 F$ L& ?2 A7 V TECHNICAL DICTIONARY 274 {5 x W0 s# m# z- K, U6 T; c: J CASCADE, Two or more similar circuits or amplifying 4 x9 ~7 l3 w8 P/ X4 r- \% K3 Sstages in which the output of one circuit provides the 5 {5 g' O4 V( P6 V7 F3 e$ |put of the next.3 }6 N# C6 P! k ASCADE VANE, A vane for turning the engine airflow 1 o0 S% U' Z& _7 u! h7 @uring operation of thrust reverser. ! C, L. H# E, J' |% pASE DRAIN, A drain carrying lubricating and cooling; u4 C. M. y& P uid from a hydraulic pump. / Y! \8 ~, l8 ?4 FATHODE, The element from which the principal A5 j! M7 A: q R1 }+ Y+ Y/ Jtream of electrons flows. N7 O6 y- t: ? ATHODE RAY TUBE, An evacuated glass tube with a * n% w& Z0 _9 @# l; F$ mCEILING, The height above the ground or water of the0 U; s8 f8 w4 {/ x* w* X* Z base of the lowest layer of cloud below 6000 meters - j5 B4 F2 r" h" P0 W8 _( h(20,000 feet) covering more than half the sky., S' {! X, L$ a& Z( h/ M4 s; D, l2 q 程。该 ! g5 i' u& t1 H, ?" K程中,一个电路的输出为下一个电路的输人。 ; U) d1 }' _$ p5 q# k3 ?叶栅叶片, 6 Y- f2 |" c. L, `3 ?" R在反推工作时,使发动机气流向相反方向流动的叶片。% d* B: H q& H* T: R& r 匣余油管, & t, G- o- M" A+ F2 H液压泵多余的润滑液及冷却液的排放口。 " g8 r& f! z' A极, ! ]8 f7 _9 }( z1 U电子流流出的极位。 , Q/ h& I- N/ m极射线管,# }, p. P( O' D: }' F 有显象屏幕的真空玻璃管。用于显示信息。: V I7 x$ q1 c' d 云高(云底高),& ~3 @1 q5 ~5 P' g 6000米(20,000英尺)以下已覆盖一半以上天空的最 ' E+ ~0 d4 a: a5 H; }0 [& \/ f; f- k低云层底距离地面或水面的高度。2 W6 @4 d! W" \" ^8 ^; X in( g1 j$ y. f+ f* K( t1 J C 6 J* w/ U( |' y+ d1 ?* x4 K8 Cd : c2 r5 a R- U: t* P2 PC/ z, ^1 T( M8 q m8 w. @' J0 \ fl . H5 d, }8 I) J4 nC ; {, P! }% V& Ns5 b) Q" {1 d# \1 z% h9 a C 3 Q$ z, p8 P) i" a* D& |viewing screen, used for displaying information. & h4 q+ x0 P& _/ b8 R7 ^( ]级联,( P7 O' p1 m8 T T5 W) z 两个或两个以上的类似电路的逐级连接或放大过 : T- p( ^: c6 h0 S% L% {5 `6 Q( n. L& j+ p% J) ^1 ~5 b, g* E1 P) f& |; S: M3 F2 }4 m2 I7 r一个具4 s) L( I9 L8 I- u" j7 F5 J 英汉对照民用航空词典B OEING! Q: Q% M8 @) |( S& \6 ~ TECHNICAL DICTIONARY 28. z% z& b1 L6 f6 u8 f CELSIUS, A temperature scale in which zero is the . T) U/ [8 X+ ?. L' Cfreezing point of water and 100 is the boiling point of4 q0 V0 b1 k) Z- v9 O ?3 Y% V water. % y' l/ Y ~/ ~0 Y( R3 h( cCENTER OF GRAVITY, The balance point of an object8 Y6 N% n$ C% T6 x1 y. x1 M! S, A r rigid structure expressed in terms of percent Mean0 ` z: G1 X/ ]4 k: r' I erodynamic Chord or in inches from a reference point.1 f: F9 J7 r# o6 g$ ~ ENTERING CAM, A cam for moving a mechanism to a5 A0 T7 i; [1 G eutral position. . B3 ^" z$ Z" l SIGURATION, A configuration of the0 }% q! o m) Y( u ircraft approved for operation by the local governing+ d% A7 @. l# n' r gency. 1 C; Q2 ], ?1 [4 u" TENTRAL PROCESSING UNIT, In a computer or' Z2 N% `1 f3 A5 m* l# o& V igital circuit, the section containing the arithmetic and( q z& G9 }6 h4 W: Q- Z( }1 [ gic,control, and internal memory circuits. y- u. a$ A% J4 w: y ENTRIFUGAL FLOW COMPRESSOR, A type of - j* j1 g; A: P/ L' e& Iompressor in which air is taken into the center of the# Q0 V- m9 d/ p5 T) t peller and is slung outward centrifugally into a diffuser # Q2 R9 J+ K0 d- Qhere it is slowed and pressure is increased. , i# h8 t, O- L7 a. C; ECG, SEE - CENTER OF GRAVITY5 b4 w3 r; j& v1 \9 w/ w5 g 构的平衡点,以平均气动力弦的百分比或, A. ~" g( F+ ], V4 u- h 某一参考点若干英寸来表示。. ?. x* J- C# G: E 中凸轮,# e+ B: X% c" D! l 将机构移向中立位置的凸轮。' e% X; |- _+ I7 @. O8 Z 格的装机状态, 2 a2 _; [( ] s8 t% u2 |由当地主管单位批准使用的飞机装机状态。+ r5 E7 l" t, v; V B2 R 中央处理器,! B( q$ G* b* X- m% v9 P" | 计算机或数字电路中含有运算,逻辑,控制和内部存 2 [. X4 q; O: x! }3 Q储电路的部分。 6 h- c2 P- q# i, ?* H" ~/ Z心式压气机,. f/ A1 ~ w8 S3 L1 Y& v2 I 压气机的一种。当进气到达叶轮中心时,被叶轮离心抛 & m; F- D* O6 O2 J# ?! a: o9 H进人扩散器。在扩散器中气体流速减慢,压力增加。& A, `" G) T7 \6 K 重心,8 ]- q7 D6 d9 w 见Center of Gravity & d: A* u" t# _2 ^% G8 n4 No) A$ Z0 V. C' Q# x* g% _/ C- ?3 \7 C A 3 Q9 _! G& t( AC 9 L* ~2 k, y& ?% }; C, jn % w- b2 t3 C+ |! U( W+ q$ c( wCERTIFIED CONF 3 ?5 \: V0 V/ N% W' |3 Z2 Sa 7 t1 g' V6 s& J3 Fa' i( z. ~8 t: H4 k C- o8 F; v9 d2 H9 V3 P6 w d 8 Z% C$ W, |- N5 j* t1 j T* N2 ~" clo 1 [; a" i9 w K! t8 H6 HC" X- e+ Y. X- \# \# h' f) ~ c ; ~$ R0 M/ x, xim8 D6 E: d J7 C2 P/ g w , ~7 W/ U8 ?( T) u+ M# J; M摄氏度(°C), + l7 _& Z5 w H& M' k' k温度的度量单位。在此单位中,0°C表示水的冰点, F( X0 ~; l% x7 s$ o100°C表示沸点。 3 i7 p5 R# g2 `重心" H* q, X4 Z. V; L; p' k) ^ 物体或刚性结& I* [; F. E( g' r* k& k% h9 J# R Y- c9 J* d. j8 y3 ^! o* j2 }1 g6 t, K9 [4 k" l# ?- T3 V/ W* M6 l+ ?5 k5 l# l) E6 q8 a% C* P0 B# q. ~ 英汉对照民用航空词典B OEING ( w9 f/ ]* n+ {9 CTECHNICAL DICTIONARY 29* }5 x. S6 Y2 v5 J" ^- A CHANGEOVER, Conversion from one mode to another.: J7 d4 k2 M; W' y3 |- I# F# @ HARGING VALVE, A valve for supplying air or fluid to) K, ~7 Z2 l) ?6 I" B HECK VALVE, A valve allowing flow in only one 2 K6 \0 m# A7 [$ F( T2 `, G/ F1 Direction. See Non-Return Valve.. ]0 l2 P4 F2 ^8 c$ c8 v, A, k HECKSUM, In a computer, a summation of digits or. }& E$ L n$ a its which are primarily used for error detection.: E. ?9 W* {! R6 ?' ^" `* R HIP DETECTOR, A magnetic plug in sumps of ! v% i n& h# L2 x' U# c0 ]) R, r) Dbricated components for detection of internal failure of % M! w" O* G: D& j4 @( pe component.9 B3 t9 _/ I x0 H8 J HORD, A structural component of spars or frames. ! b! W3 Z! d4 ^$ }8 G7 w添活门, 3 W( @& u7 G; d! j C器充气或加液的活门。 ( Z8 G& @/ U, L* D% ]' h8 p& t单向活门, ( u9 _! Q" R. l0 `9 B! P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 2 P( D8 e4 Y* x4 a# \a reservoir.5 a- Z" O' u! `" w C( V, V- |$ E; ?* U/ X d # D' N. c; z8 o7 CC/ U7 o9 R. _2 {) j/ }, w. ^ b3 q& ~1 [. c+ m3 a% ?9 s4 p3 j7 c* B C( n( Y4 B3 |1 W. l lu & W) a7 I2 F( t( J% \0 Xth( I% }1 r$ O& V' z8 z C 7 @# O+ P7 ^; e) a2 c( o' ~! ?转换,+ O" e/ Q J6 p' T' ]5 s2 Z 由一个方式转换到另一个方式。1 [. X! b! v* H; A/ M% @& L. X1 X 用来向储存2 ?, F2 g5 s, b9 @. v6 p" v3 v$ x. l8 O. k- t7 U 总和校验,9 b3 ?4 o' h, n% g V' R- o 计算机中,把那些用来探错误的数宇或位数的总和进 ! F. R# V2 T) p7 Q3 W1 Q4 V求和计算。$ v2 V* Z/ m/ _7 I+ H! e7 K) y. x8 ` 属碎屑探测器,4 m$ F2 r4 M6 \7 Q" |/ y 装在被润滑的部件滑油回油管路上的磁性塞子。用来探# ]* L; h, L- i2 V 部件内部有无损坏。 ; o) p3 @3 G+ f# r; D# D( U3 z弦, * P- P& B: o6 c梁或框架的结构部件。5 m- w5 C9 r1 y+ N7 S- q& u2 [6 h0 B, B. e8 o6 [+ c& A- @) X/ Q' K" G9 E V9 y: } s) o; p# D- a1 a. U5 r1 C* W% b1 B) F' |. W& J. @5 ~英汉对照民用航空词典B OEING- v) D5 C W& ~ V TECHNICAL DICTIONARY 30: x# c D) U: q3 F M, H CIRCUIT, A closed path through which current flows ' f; C# f( |$ u% n7 nource. + z" z- i$ ^" m& g: ]* P4 f7 TIRCUIT BREAKER, A device that automatically ( e0 Y& q E3 Q/ [( Xeactivate the system.2 @2 x1 [# p5 G lear of all non-frangible objects which ! T8 J/ z8 ]. b: m; ?/ J+ Y! ]5 iay be used as takeoff distance available when 2 @4 Y0 _0 g0 P8 f) Kalculating a takeoff weight. * h4 H# U0 E$ p! N. S1 ir water under the control of the appropriate2 F! |1 G9 Z s9 ], q& q& T uthority,selected or prepared as a suitable area over, A `6 `, u% ^" f4 g hich an aeroplane may make a portion of its initial ; D2 p& r% B* w x' n0 Ilimb to a specified height.8 a2 Z% F% ?7 u" ]# W* h, Y* ~ increasing.' g) `/ V, P( ]" r' S- Y sed / z7 e, a9 O5 y) l9 t! RLOCK SIGNAL, A continuous string of pulses used for 7 y( O; M# d; x! r% F$ U0 [开关,+ S1 o8 l$ V# \, U, |2 O 故障情况下自动中断电流以保护线路不受过电损; U9 z8 L! O7 m- X( E7 W* H 体障碍物的区域。在计- R" l2 q! c( h1 ~ w: D 起飞重量时该区域可作为可用起飞距离。3 K$ C, {5 W1 ~5 X6 l }- M8 x4 h) N 是在有关当局管辖的地面或水域内一个界限明确的长 8 M7 f' Z8 C1 i0 h: K& p形区域。在这个选定的合适区域内,飞机可完成初始爬 - I1 p4 L" ~6 Y( _$ V4 n的一部分,上升到一个指定高度。 7 @0 ?2 E* l9 `* C3 [飞机高度不断增加的飞行阶段。 ; w. z4 Z# V# l2 m, q& k钟脉冲, , [' m o$ v. y1 k% M- p7 b& J4 w' i, Y步的连续脉冲信号串。 8 U# [0 x2 }1 `8 J3 sfrom a source, through various components, and back ! w! ]1 X- h0 W) vto the s ( L( W0 x' |& ?" UC$ a9 P+ M& O% O0 Z+ B interrupts the flow of electricity (current) during fault $ h3 \( Y2 ~' F! \8 L, Z! lcondition to protect wiring from excess current. Circuit 9 y- P- I4 X; E6 L, `( e- Q5 Pbreakers are also used as a means to manually 4 J, `2 S8 _( ? j4 o4 x; X& e7 s/ sd) k; B1 I( u; ~+ E. Q: F( j K CLEARWAY 1, An area beyond the takeoff end of the. f, y8 T+ m, @2 C8 f* Q* E: w runway which is c 5 {; u9 e+ Q$ F; l2 Tm + g2 {6 L7 k. h7 \2 J) d3 Lc / ]1 i. U& _; `CLEARWAY 2, A defined rectangular area on the 4 H( a f. \6 w/ Xground o( l4 Z8 F" Y" A/ I. c) k a 3 e0 X, }; i* m+ b1 ^: p W$ T. q- hw % q; o& n. I& z, u/ s& ^) W6 q! Hc( z5 l3 X( T* i% ]2 U' D1 u CLIMB, Phase of flight where the altitude is( y4 j+ R6 n+ P7 ^; ^ CLIMB LIMIT WEIGHT, Maximum takeoff weight ba g4 Z2 k. P9 L- ~4 S4 O; Zon a minimum climb gradient with one engine * j4 z, b# K0 |0 f4 i( Finoperative.! @* X9 k$ \5 K5 S) F C , K$ L) ^* R; _, Isynchronization. 1 p* j; s& l' ~5 n# _电路,4 j/ I5 h5 h3 ^2 p6 m4 o 一个闭合的回路。电流由源头流出,经过各个元件流回4 g9 F g( `1 M2 f" |- j9 H4 | 源头。' L, }, C: L- ^! |( v5 g/ d# |) V U5 R! w! I2 F- T能在 ( h( m: o' O5 X坏的装置。跳开关也可用于人工使系统无效。. U" y3 [9 F5 s8 C 一号净空道,5 g8 `+ w, r5 x/ d! t* M! W$ G 是跑道起飞端以外,不含任何刚1 U ?8 m) Q, C+ y9 z0 G- n" n. U, A! T5 d( `# L二号净空道, ( ]) U+ J3 k) h2 c0 l* K: }; |' G; U- u$ m$ q( d5 o3 q0 o! r7 h+ z. o- m1 y, M 爬升,! t- T$ `5 ^" B9 B* `, H7 Z 爬升限重, / v/ \( D/ p) L# p) t取决于由一台发动机工作时的最低爬升梯度的最大起 # Q* H5 C8 H% i' t飞重量。 ' _- c x0 p% l u- X6 T- S( z/ E' a( H/ ?0 H用于同. O9 x2 r* ?5 N5 U& G- [ 英汉对照民用航空词典B OEING4 p' Z% r/ B$ f: E2 F, ?: _ d TECHNICAL DICTIONARY 31 1 M+ y3 k1 N" K) [COALESCER, A device in the water separator for % ?8 ]' Q2 P% n0 z/ D* \2 u' Wollecting moisture from the cold air./ m. s0 H- |9 i9 _+ @9 p! T8 x n antenna with a receiver or transmitter. 4 ]$ O" a7 A# z, {9 E8 rhe cable has an inner conductor and an outer d+ q" `0 A% w6 P rounded shield.% ~. J4 p* e u1 ~3 s ting one inside the ( i3 h8 f, x) L1 t0 yther for rotating the low and high pressure2 U \; T1 ]4 i' L% l7 |( t1 h ompressors by the low and high pressure engine ' j# r! \0 g7 \$ s# v m2 u( ~$ lrbines. ( H0 A& Q; q0 oOMBUSTION CHAMBER, A part of an engine for Y* k5 @( w3 J* V2 W! q8 hurning fuel in the air supplied by the compressor.- n! j( u& p, C# Y u5 a) H9 {, b 置。7 S5 m7 O3 u' g- V5 e# B$ Q+ b! w 射机的电缆。电缆 # m: z1 L7 e- C# J中心导体和外层的屏蔽所组成。( ^' r* N( B* {9 L 两个套在一起旋转的轴。用于使发动机低压和高压涡轮; b5 B$ ^, D- ^- M# i! f 别带动低压和高压压气机。! k% \2 Z7 J' S' f1 q 烧室, # c' L, `5 a- {5 V# ^发动机的一部分。用来使燃油和压气机所提供的空气相 4 {. H! M2 M% B1 C6 m合而燃烧。

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发表于 2008-12-24 21:38:35 |只看该作者
c 2 X* o$ @' P% K Z! S3 ~8 MCOAXIAL CABLE, An electrical cable usually 7 H; z9 C% H) S( {2 Dconnecting a + M# |3 q9 l. y" j$ V2 u4 d. F/ JT( i5 W y5 s) H- z1 t1 ? g " F2 m5 P: N2 \ {4 I- I( J% A. ]COAXIAL SHAFT, Two shafts rota1 C$ |7 {5 y# H v o 1 Y% {, M7 u1 ~, `# K4 W) X, nc 3 _) o! B( N+ x2 v$ o6 r& ^tu 0 G5 f v' ?5 ?7 iC % c3 R, Z6 s2 v tb 0 d. J8 c! X8 P凝聚器,; l/ F& N0 g. a7 q& W 水分离器内收集冷空气中水份的装 6 n: M) P& y. ] P- s j同轴电缆,/ k' ]- F, i/ A1 q. t6 V9 x/ Q 一种通常用来联接天线与接收机或发 7 ^7 J O; [& e! P& x9 a/ y" Y9 l; Z$ Y/ b$ q& X" M% [! | T 同心轴,$ S' `8 d, Y8 T9 O( c e) l2 z. x, n6 Z' i4 t9 e* j1 d( H2 n+ p! G% r3 G: q3 t) {# w: M7 |3 p英汉对照民用航空词典B OEING 2 l; t6 s% l3 j0 l9 [+ L# P/ }TECHNICAL DICTIONARY 32 - H1 m; A3 l6 ?) E" ]- C% rCOMMAND BAR, A flight director pitch or roll comman, D0 v1 o& q* U indication.: |9 A! A5 j2 U d - t( M: s2 s$ R9 WOMPANY ROUTE, A route flown by the airplane7 I, m% g/ M) K" i8 P& [+ ] OMPASS LOCATOR, A low power, low or medium ! A3 N [; i. \ S" h/ Dequency (L/MF) radio beacon usually installed in , b# Q+ y1 l& a; Conjunction with the outer or middle marker of an7 |1 z- v. M5 ]# O& v tor (LOM), A compass 9 H% M+ R+ z* T$ n4 [5 tlocator installed in conjunction with the outer 6 ?1 {% T8 U" J a: Kmarker of an instrument landing system." A0 r5 N/ c7 _9 M ss / h; u+ H6 e" Y8 a3 jle# J4 h; q& O. b- ]4 h1 ^ OMPENSATION, To offset, balance, or counteract.6 u- P% h, A5 z8 m OMPENSATOR, A dual capacitor for changing the fuel/ {" t& }3 i. Y; o1 X* i# p aging circuit capacitance due to changes in fuel 8 ~2 @( Z- x- q5 g/ q) Uensity.5 X5 X8 W- n9 S0 V OMPOSITE MATERIALS, Non-metallic materials used9 ^! O' r* l6 l r airplane construction. Fiberglass, Nomex, Kevlar,& }! k3 A* Q1 J% g9 ] raphite Epoxy are composite materials. + t" `3 R( e# C1 N6 k司航路,# A6 g9 `5 E2 d$ Y, U( v% F+ B, G 在飞行管理计算机数据库内由航空公司飞行# e; \% v2 C2 E 盘定位台, ' {( u# E! i- h( {- U. v与仪表着陆进近系统的远距或中距指点标配套安装的1 r$ q& o& l$ A k: J 功率、低频、或中频无线电信标装置(低功率NDB台)。1 M; r3 N5 |) f7 r& j: k; ~6 K 程序中用来导航。 3 g5 E1 z* L; Y3 ?+ \# J6 b1.远台,% e' P1 s+ H3 r 与仪表着陆进近系统的远指点标配套安装的罗 ( |6 ?6 R$ G0 h6 n0 Y5 e盘信标台(NDB)。8 O w( r+ ]- N 偿,) T: b4 u& p( S( W2 e4 P0 f+ c 抵消、平衡、或中和。 ! `* n7 w' s6 @" H5 |$ T偿器,5 B& r( R$ Y" D' T1 k3 Q1 T 在燃油计量电路中,用来改变电路上的电容,以与燃 5 y0 t( \ j$ m8 H3 u密度改变所引起的电容改变相抗衡的双电容器。0 x* Y4 L1 T0 J8 _3 B& }% p" r5 } 合材料, 4 v7 `9 K' x d6 z3 r5 G/ f用于飞机制造的非金属材料。如纤维玻璃,Nomex,; G% l' v# i) H( Y7 D/ g3 P( J evlar及石墨环氧树脂等,都是复合材料。

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发表于 2008-12-24 21:39:01 |只看该作者
C. c" ~% o. z8 Z3 L7 \5 ^6 Y operator that is normally stored in the flight % d$ P+ i: x1 P+ e5 I% n2 imanagement computer's data base.3 Z) s) J- _; G5 H, S% X C + j7 @0 c: i! y) r4 ^6 J$ [5 s! Sfr2 Z8 w3 B+ W3 l: J y c , E8 m9 i6 t' I1 I2 ~instrument landing system (ILS). It can be used for : p0 g' m# K R+ V( I# E3 S$ mnavigation as authorized in the approach procedure.2 M7 {) {+ Z4 c3 Y/ y6 d* d3 Q' L 1. Outer Compass Loca: q) w5 J! _2 _5 H 2. Middle Compass Locator (LMM), A compa+ b/ z5 _5 {+ L: @8 U( w: v locator installed in conjunction with the midd 4 ]3 C8 q/ N9 Y. K9 Gmarker of an instrument landing system. ! @3 E& J0 P! H# nC' [8 R* ]; C( v C , E8 M4 r& _& t1 o% R2 X Qg 3 I7 z6 r% e: n0 C! Y+ jd/ s/ _& Y/ B, _& w% { C3 F+ u' o' K5 u: P- x" z fo : ?/ i7 [. \0 E' ^g& n. J. A1 W& R 指令杆,; H% u/ z5 |: ]$ {" S5 f 飞行指引仪俯仰或坡度的指令显示。 . Z! Z" v6 J- ]+ [# F9 L7 q9 V$ e) R K- w! }7 @通常储存# @. r9 x7 j, E; Z/ Y 的航路。 $ z+ R1 o$ z \- ~' ? [; B( s7 a9 N* j8 |0 h" H! j: m" M7 t5 B# w S0 o- E2 J# t. j* Z 经认可后在进近 ' b& {( m9 B! g+ q5 ^2.中台, " B. C; s; \1 w0 |" G; e& ?与仪表着陆进近系统的中指点标配套安装的罗 ; Z4 x K# t) j+ T- i8 }8 G盘定位台(NDB)。7 w+ q+ ]( n% Y# J1 X* Y; S$ l1 G" l$ {6 Z; G: m; b% V8 {/ c3 d8 L5 Q4 D v, m0 s7 f' c8 t8 w' i( V* _8 z# A$ T) R3 ?) T; t; |- m" DK 2 l1 S6 O, z8 _: r7 w' d英汉对照民用航空词典B OEING ( B8 [0 f$ |& ]1 ITECHNICAL DICTIONARY 337 Z& h) b8 {6 C2 B1 h! t# ^) c7 U by p n, b; V" ?6 ~5 u or increasing air 5 ?. e" Q$ H! P: b9 oressure and temperature before the air enters the2 H, w, E2 G# B: O ombustion chamber, Low pressure compressor - front 1 s9 ?1 {& g4 L6 ^6 Pection of compressor, High pressure compressor- rear( Q: ~ q# e7 s) V! Y8 ]' b9 F OMPRESSOR STALL, An event that occurs when+ c6 w$ s" p! e5 K; S% n ere is a complete stoppage of air or reversal of air flow( u! c0 Z; i# A- p% C4 R9 O+ } COMPRESSOR SURGE, SEE - COMPRESSOR* i3 c9 D! R; ], ?% N4 X- I STALL COMPUTED AIRSPEED, Indicated airspeed% b- _4 V+ E% z+ Q& { corrected for the static source error. 5 s! B9 C" d0 m+ [0 d1 ?的机械轴来驱 8 n$ y$ s! a; W5 ^/ f,用来增加吸进空气之压力和温度,以供燃烧室使用。9 E F" r$ N8 _6 b I& ? {6 ?3 J; L 压压气机—压气机的前段,高压压气机—压气机的后$ ?9 I7 N+ {* l& M+ n4 B/ H) U& G& ^/ D气机失速, 8 U: \1 p8 a& s1 F i7 C4 V当气流完全停止或通过压气机时气流方向逆反的一种9 {" |( u4 R$ `. E1 T. s 压气机喘振, a1 V7 g( Y9 P' ~7 E5 c见Compressor Stall* d: S/ |" J, r( V6 I0 v COMPRESSOR, A rotating part of an engine driven% g4 u. l1 R* l, S: a a mechanical shaft from the turbines f " O0 `7 @9 W* F8 tp 0 g. W+ ~# A7 M3 xc & e/ I7 I. K! Xs * f) _0 t4 F q0 S8 gsection of compressor.% |5 f9 A& t: V& q( N' Q( F9 K C d$ v8 S9 C. H, l0 U th( Z2 W9 A; s* N through the compressor.2 J/ w: w3 o5 ~* x- d) r& V% K/ g 压气机,! \% }& `' F1 s, Q, u 发动机内的一个旋转部件。由与涡轮相连9 |: q4 [7 t2 G( \# k0 z3 s( V; a2 L" n R( |- d: j3 k7 ?9 `$ v: N7 n0 x5 }- C3 U1 E; [( E- m. \/ |+ }& _5 f8 [) q- G+ o现象。# s& o7 M0 ^0 g& \) h! f% w) Q& F* h& P# g4 |1 F3 ~计算空速,3 x9 j; ?6 u' T6 U3 d/ d; f 修正了静态源误差后的指示空速。 6 k. u8 r% l( z/ Q+ K英汉对照民用航空词典B OEING6 {2 U U3 x7 M$ U- s4 Y" I TECHNICAL DICTIONARY 34

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发表于 2008-12-24 21:39:27 |只看该作者
COMPUTER, A device that performs arithmetic0 N8 E% A) }/ D9 n8 V' N" r* e) | operations, manipulates data, and makes decisions. 3 e3 Q/ b7 u9 Z6 t6 }8 yditioning V8 i7 o2 W4 ]! l the air and the ! G3 O) `; h2 t7 Zfrigerant or moisture vapor is changed into a liquid. / e2 {5 d y; a- M8 Fine ! i2 x7 Q0 J, mONFIGURATION, The position of flight controls,2 \7 J* w7 m( R+ l( W" ] missing which ) \) y7 m. |. C7 ~3 G" _% M3 pmay affect the aerodynamic performance of the 9 u: I& M& H" X' E7 g; D9 ]airplane.; r5 D y6 B0 w3 |# K- U 置。2 V# ^. r" W5 W- p 中能使热能散发到空气中,以及使冷冻剂或湿 ! ]- w9 c- c/ D D- H. ?. F1 ~( U转变为液体的部件。 * o. ~8 }, v3 \/ Z; `连接到飞机结构上。 9 l: g5 d( J- P @/ p8 r4 D& T态, m" J' F2 d" Z& `, F" z9 ^! f定飞行阶段中,飞行操纵面,起落架等的位置。 3 @* x/ V: r: t6 H( j L)," z& D. s9 i( l1 L* W1 j 受到影响。$ J5 x' M3 P; g9 B, d6 } CONDENSER, The component in an air con 0 S! d* C$ u2 Qsystem where heat energy is given to. i4 l, C8 Y% e9 a5 m) b& \ re . N# ?8 m$ Q8 t! j9 S3 FCONE BOLT, A bolt in the shape of a cone for eng & ?, i* P+ Y% I2 N. S7 x" n& W3 pattachment to the airplane structure. + X( p$ c! \) ^( g% f' {3 IC' q) H9 J7 J( V7 Q landing gear, etc., for a particular phase of flight, e.g.," W. k0 x+ @* j Takeoff Configuration, Landing Configuration, etc. - i( R& q" ~! s* ]CONFIGURATION DEVIATION LIST (CDL), Appendix 5 P8 Q8 b* ~4 E6 f( {, Ein the Airplane Flight Manual (AFM) allowing operation1 s4 d& p3 C" I. Z/ h0 Z of the airplane with certain airframe parts 5 ~7 ^- s6 ]6 Z# X5 a9 O( o$ _% E计算机,4 p0 U1 i2 U3 j; N 能作算数运算,数据操纵,和决策的装 # V$ W1 @/ H4 s; R/ M+ x冷凝器,4 P5 e" q, U l7 N1 q: I 空调系统 ( L% l/ t" F, u6 l3 E/ V% ~+ n/ A- S6 Q @3 t: p4 M 锥形螺栓,9 C% ^9 W8 F" \7 A0 c 外形是锥形的螺栓,用以将发动机 9 K* p$ b& X- \6 c- j8 r0 ~6 a. Y7 d: b( ^4 V5 ?, d在某一特 % d9 s. j. V# D; v+ L$ I' a如起飞形态,着陆形态等。 / G q9 g: A5 s' I4 w) |缺件单(CDL; V W3 x% }% Z7 K8 u 飞机飞行手册的附录所开列的飞机上某些零件的清单。& n- O. N* s2 v( ~% P 在缺少这类零件时,可以飞行但气动性能可能 ' N" l! o0 W+ h* K0 l英汉对照民用航空词典B OEING : E9 }; t; Q8 e' Q$ e( C" zTECHNICAL 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$ R5 A( R- ?- N0 T5 a/ \2 I component for changing variable engine gearbox speed9 y4 p$ v! u9 ` ONTROL AXES, The three axes of the airplane which5 ~ c) C# y* G" J, x7 M re perpendicular to each other and pass through the ' \: Z; `+ K/ @$ Lenter of gravity of the airplane.8 O/ `/ L' w9 L. y" ]; D# v5 x Pitch axis - Horizontal or lateral axis, passes through " N: y0 n7 S1 i6 y- m3 Ithe airplane from one side to the other -; i/ b# T2 `5 N7 n8 D" g2 L nose up and nose down control is by6 a2 F, h3 W2 X; I- \! s! Q( ` elevators (and stabilizer for trim). $ q5 V! `- i5 b+ e! P3 c9 C+ WRoll axis - Longitudinal axis, passes through the 5 W) l( L, H( T8 j L. K9 Tairplane from front to rear - wing up and + X! H0 W& |6 J: j# _% Awing down control is by ailerons and - k& P: c' v; Tflight spoilers. 6 q+ T0 c. M( C L6 z! K1 YYaw axis - Vertical axis, passes through the : k% `! R8 M. B" s' Eairplane from top to bottom - left and ' i3 Y( N X9 Z& pright control is by rudder. % ~! j5 D, u% m8 F. o- J' S T5 ?置, ! ^. Y1 Y+ {8 g8 s/ z+ P制轴, " g' d4 `6 b& _" x通过飞机重心互相垂直的三个轴。 8 \" j ~' Y' L, T) q$ C3 Y; Z俯仰轴—又称水平轴或横轴。由飞机的一侧通向另 $ y) f# D$ l: W3 Z8 v侧。飞机绕此轴转动即造成机首的俯与仰 + R& T2 z% C/ x. a俯仰控制是由升降舵来达成的,水平安定 A3 K7 S a7 s9 G则为配平之用。 + |2 L' N/ v) r/ R; {- m( e横滚轴—又称纵轴。由飞机的前部通向后部。机翼 2 q3 X3 h+ N. W2 f4 G6 N下运动由副翼和飞行扰流板控制。0 _# g6 y. ^0 O$ o" J 偏航轴—又称垂直轴。由机身上方通向下方。飞机0 I& K* `/ q4 H/ \! o 此轴转动即造成机首之左右运动,此一运 3 @2 ?9 ]# g0 f. Q, e" F由方向舵控制。 3 z a4 ]! T. X8 Q# h# bto constant speed to drive the electrical power.$ |+ @4 h. `% ~ C( i7 F0 K' l0 D4 P3 k a1 f$ {* @, u: N2 h3 g' O K c2 G6 N- _' M6 v9 d8 a7 z8 g& J 恒速驱动装! D8 G& `% V+ J e+ H) Y 将发动机齿轮箱的可变转速转变为恒速以驱动电源的8 S! }! B1 ]- U x: ~9 Z3 l, y1 j 液压机械式部件。$ V9 A3 y5 I& E" M" @0 I1 ?" F* y: C- M) i% l9 K) `* d( C9 I- @" U: Z1 O2 k& D8 n" w% o" t) }: n1 V3 I9 A3 `) l, J! d. o! i G: W! f% x! I/ {. |5 p5 S0 T' y7 G+ O8 G r: z% m5 I1 n( [+ S7 H 英汉对照民用航空词典B OEING7 b6 w( A2 S3 \' n* {6 ], V TECHNICAL DICTIONARY 36 6 v) c( h7 D1 w! n3 r, d& xCONTROL COLUMN, A mechanical component used9 F$ x2 B& Q7 v1 R# Q- K3 v rs 0 f! C* @* T3 }& `5 F; ]% Tnd elevators.3 `( O# p `! B6 j" v' q" ^$ K6 O ONTROL SURFACE, Moveable panels on wings and5 r9 T* Y. y+ ]! M3 `0 o7 O! y il for movement of airplane on pitch, roll and yaw axes.3 E5 t) W/ [5 ] ONTROL TAB, SEE - BALANCE TAB . S n, u" X0 e$ E, V7 J2 tONTROL AREA, A controlled airspace extending 9 W7 X9 |* J s9 fpwards from a specified limit above the earth. - O' L9 }; c6 r( n; r2 ^ONTROL ZONE, A controlled airspace extending6 c' ]* T# D. Z pwards from the surface of the earth to a specified* K5 O8 t! d9 {4 c" P pper limit.# n- v) {; M, ~8 L is ; L% J7 M, H* Jo IFR flights and to VFR flights in accordance * A+ S7 ^' K5 i% Z2 M N2 ~with the airspace classification. % E3 @0 Z( t( ^3 V8 L机械部% m0 `9 N) ]2 `1 N1 j0 a9 i5 q: {3 ]# f S 操纵面,* }- \% \* J5 u. d 机翼和机尾上的可动面板,用以操纵飞机俯仰,坡度,0 l9 H- x: }+ {1 v: a: t 和偏航运动。 $ s+ ^9 ?$ ~# Y% e4 M; p3 F! t! n操纵片, 7 i. }& E) ^" b6 c. l1 s5 C# M: D+ K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 ; Q1 B$ h8 q' w. K' i: c+ Ia 3 B/ o" p3 G0 B% v. B$ g; yC* G/ X! n& v( R* B; v ta / |( O' P/ ]* s- AC * o& X' l: E: E5 s, {7 MC) E% g; ^0 \- ]( r u * g) E7 p( @$ S: _C+ z a1 T% g) M' i; t1 b u& m0 t4 v6 }$ S2 d; E2 x# } u / I/ f9 c% q5 l( X+ F* a3 oCONTROLLED AIRSPACE, An airspace of defined 5 X& r/ \# `: N' V4 c" Z udimensions within which air traffic control service & F l; T6 F3 x( T- c/ h! oprovided t 1 [1 `4 X3 {% Q% _1 U6 v8 a5 O驾驶杆,; i- L: v' b3 T: ?' m# N( g! R 飞行员用来操纵副翼、飞行扰流板和升降舵的+ S/ R5 C! x3 w& _& _7 I6 G; n1 R2 w! K! a( J& R0 b3 t! ^+ a1 O5 X 管制区域, i$ V! M' K' ?/ ] 高于地面的指定极限以上的受管制的空域。 3 v% p: Q8 ~6 H0 m4 C制范围, 3 K1 q4 F1 _! x由地面到指定的高度以内的受管制的空域。 2 W- j; ~% ]" R一个范围明确的空域。在该空域内,仪表飞行规则飞行 # n1 W5 O$ t; L) x和目视飞行规则飞行有空中交通管制服务。 / a; Z+ n" x# ~; a2 q/ G, L" l, {/ v. N& N1 e$ Y 受管制空域, % c u- Q% I) j* T9 b英汉对照民用航空词典B OEING' [$ w7 j6 J1 B& N TECHNICAL DICTIONARY 37 # g. w) a; Q6 s B, _' HCONVERSION, To change into another form. 3 q9 U( z! M$ `. d) W0 F5 HCOORDINATES, The intersection of lines of reference,$ u6 `& G! `7 a) L+ } sually expressed in degrees/minutes/tenths of minutes% ^( ] ~- K3 I: m% t" L- ^ f latitude and longitude, used to determine position or Y$ K0 H. V& W, {! c% Y- KCO ( O6 U+ g9 `4 Z8 jdestruction of th: C9 W6 u$ b5 ^ chemical conta5 w3 W. b q6 Y$ s# K COWL, A remo- p t/ K7 h; J for access to th $ r' P/ M: p* I! vFa. C' X ]$ {# D Nose Cowl - Front section of the nacelle for air inlet # B: l0 _5 A* |' H0 ^% mto the engine.9 I2 S8 F8 r7 E0 y; u& C" n. ~ Side Cowl - Cover around the sides of the engine./ f/ `: |( E3 h Thrust Reverser Cowl - Cover around the core 5 C* i3 Z' |6 O$ n% c+ X0 Ysection. 4 a3 O. t6 K# e5 O7 ~ M1 _) XTranslating Cowl -The moveable outer portion of the y8 Z) }3 A l& ~9 V thrust reverser cowl which is! A) a; s3 q$ I$ c" @8 N# O5 a operated during reverse thrust.1 D+ z9 ~8 W5 J" M; x1 j% e( P 标,& U4 v2 |: c+ {1 Q7 ? 基准线的相交点。一般以经纬度的度/分/十分之一分, M b# {; p8 z* Q" s 读数来确定位置和方位。$ E$ ?/ E7 H; |0 s' ~! u9 d 腐蚀 7 P; H' p% @; Y8 b r$ V动机外部可拆除的罩子。发动机上的构件必须要取下' t4 p9 Y# u2 h% C' X 流罩后,才能够到。4 u( Z) C0 s m% q- x; a# K# Y9 C( f/ f7 M$ S 机的短舱的前段。( o% w# m. T$ {) W1 }4 o9 } 侧整流罩一发动机两侧的罩子。 2 k1 E) j3 q2 ]' T+ H反推整流罩一发动机主体外的罩子。, Y8 w4 {" x0 b5 U! L 移动整流罩一反推整流罩外可移动的部份,在反推工 # i k4 N# }0 B. Z# N! x$ f作时使用。0 D; d: b* g1 H; l u 4 h5 v/ F! p' K0 m j, Lo ) F0 A4 M! Y8 ]6 Glocation. 5 @( J/ g6 r+ ]1 E. r3 m7 l# lRROSION, A chemical action which causes gradual + W& X2 m- j; o* ]% P% je surface of a metal by oxidation or: [2 a1 c$ m- [ mination.( g# N' E7 e3 K: T$ W( Z) G vable cover around the engine sections o: h q: a# W. c5 |e components on the engine.9 U( G+ ~3 ^. W' F6 | n Cowl - Cover around the fan section. ) L: p. v7 K, z3 C3 `6 u( [转换, " ]( j9 R1 B7 z' g: b& D# j改换到另一个方式。 % B0 c- j, t7 b% @; b2 P/ C, \3 X7 @4 g/ t2 B5 Z2 Q+ \: ^$ M" B1 e' r0 ]+ Z6 K2 d7 Z1 s/ D氧化或化学污染造成金属表面逐渐破坏的化学反应。 - A- C: ^! U+ v发动机整流罩, 4 n5 Z1 r7 R# i3 |& @4 k* C. d& q0 Y! d7 n$ ?0 F6 y: @7 P1 ^8 R8 g) _* R 扇整流罩一风扇外围的罩子。3 z5 m& w% @% `" \ 前整流罩一引导空气进人发动 - T" x% s3 o( F% F* \0 y英汉对照民用航空词典B OEING ' E4 b* f5 v) [; M. p8 JTECHNICAL DICTIONARY 38 # x3 ] Q6 X W% P, p* ^0 hCPU, SEE - CENTRAL PROCESSING UNIT( I2 c( W, U2 M) e CROSS TRACK, At 90 degrees from the desired track7 _' n- k( C1 `+ v, o9 H2 y f the airplane. For example, cross track distance is the. w1 S+ u i- d. k3 l2 C C* A# H istance from the desired track measured 90 degrees & p! V0 i, z' R% \7 Z/ Aom the desired track. 7 i0 `: i5 @; L0 P7 P* xROSS-CHANNEL, Electrical wire(s) connected from 4 t/ d4 R8 J+ j' yne system to another like system, for example, FCC f. [9 Q. M9 I" to FCC "B".0 M, b9 T4 K. @; G9 w1 d n adjacent engine or one on the other side.5 a( w: `- C+ i5 h* F4 B5 ~ l crossfeed# {# j" R; [: d% j; J anifold for fuel flow from one side of the airplane to the ( I/ k. n$ U m& S& F7 p3 jther side. # m1 K# | v& V0 k2 w) k2 x3 f- sre v7 }0 v* O# m; w% V) XRUISE ALTITUDE, An altitude or flight level 6 Z4 n, ] k& X- f9 \" y7 r& O+ O) O# J9 z o) c3 N' oo* z2 \; L1 Q5 g c d / i8 k# K! ]6 h) Mfr - d5 y% F. B' w: A4 w2 u' k9 sC/ n9 Y1 A* T3 \5 M# }$ U" X x o- p+ B% D9 N$ g* H% Q! c' H "A $ t+ K7 l8 B+ J& b. H2 yCROSSFEED, An interconnection between fuel/ L c- o' @- }) g$ b; e manifolds for fuel flow from one side of the airplane to 1 v8 R2 [# ~/ \/ w% oa " a( U9 I& Y$ i" E5 G2 Q( t3 QCROSSFEED VALVE, A valve in the fue: X, j( k! T# V8 y3 S m , i5 E" Q9 Y' g2 i0 U. {o * g; q3 o5 I1 S) @CRT, SEE - CATHODE RAY TUBE , Z+ f7 G* ]; j5 p" \CRUISE, Phase of flight where altitude and speed a( |4 e; m; s7 o basically constant.! K' N' O; d9 V1 x% t+ A- N8 C C( V7 e1 p- v: p, b5 j9 [% L maintained during enroute level flight.5 O+ a6 C: }7 U, a 中央处理器9 Y9 J$ G* n; `) ^8 V6 j$ G 见Central Processing Unit.2 a/ t* A/ R2 Y" V; Z0 ^ 交叉航迹(XTK), / B+ f! E: |" Q+ m与飞机预计航迹成90°角的航迹。例如,交叉航迹距离4 T- e) K3 p* {) R& m0 ] 是用与预计航迹成90°角量取的到预计航迹的距离。 % W6 o/ h7 W- Y% p/ p& s通道跨接," a( B5 P& t; `4 f+ g. j' ? 电线由一个系统接到另一个类似系统。例如:由FCC$ K& z3 r/ V2 J A- D7 Y% i “A” $ Y/ z) d3 z% y; s( W: P接到FCC“B”. 6 R, H6 L. W2 z* F$ [* B机身另一侧的发动机。 3 K' b9 p* \/ Q4 p于使燃油从飞机的一侧; _* j& y# _) U" s% N* Z 向另一侧。 . f3 T4 g. L1 g2 h0 I$ {见Cathode Ray Tube ~2 L, J1 N8 w( G/ i交输, ; ]6 C5 q5 s# C# J1 x3 k4 W燃油支管之间的交连设备。可使燃油从飞机一侧流向邻 5 U8 A$ D0 X: q6 u3 P近的发动机或在$ H' m2 W3 @7 ]" z, J 交输活门, + {+ }- V5 G7 i+ u# l* c燃油交输支管内的一个活门。用: K- L4 Q$ X$ G! v8 N# l' C& V5 N# M6 N: T i 阴极射线管,( ?. E! G; |1 q& }2 J .7 k! Y0 W) @6 Q3 k 阶段。 0 D- ~/ H- p, B. G" q航高度,/ A1 N7 X+ U. d( { { 飞行期间,飞机所保持的高度或飞行高 0 \0 ?; q2 J; t; E9 v! k8 ~4 S巡航,$ ~* L1 Y& l9 X/ j& U7 b' x& U 飞机的高度和速度基本上没有什么变化的飞行 . [% ?' D1 _5 |6 n. z' G, V8 O+ q3 \- L ]( z在航线上水平 & `/ E5 i- y) }8 e- I% j; m度层。0 P' j$ n4 \4 F- e& d9 }% H 英汉对照民用航空词典B OEING 5 p7 I! g$ T9 _6 [4 }TECHNICAL DICTIONARY 39$ _, b- ]+ z- d+ N3 z6 r# k CSD, SEE - CONSTANT SPEED DRIVE* t$ q- _+ f. G) a CURE, A chemical change which takes place in a resin- }4 O0 F; `5 b& y9 F' j and fiber based component causing it to solidify.+ V2 S) s- @9 ]; T$ y* k CYCLE, A complete series of events that take place/ X' J. c- S H0 O6 H/ ^ gularly normally in a continual sequence.! a+ c6 ~ {0 W: W2 O6 @ AMPER, A device for slowing down or limiting 6 F/ |+ }: R$ O; m* zDASHPOT A mechanical damper for slowing down, P1 k+ e: g1 V* u9 ^/ ~ ovement by restricting fluid flow./ I. H4 R+ ~! m( C% s) M$ P3 A D * }4 n+ Q) G" r d& K! ZATA BASE, Stored information which is used as the1 F5 k! t( _: D5 A5 g) l ba # A t* `* \3 H+ ]( a3 A& o: oDATA BUS, A conductor over which digital data is .; i! a0 Y0 k/ i! A6 |+ h: A0 D transmitted. 7 h( s h0 m( Z" o5 a& nDECELERATION, To decrease in velocity./ n$ n, [. {2 o) _; A/ w: A 装置,: }; m. F1 w$ ~2 T2 [0 [0 w( F rive 8 p' o+ b3 d) }, J, w$ rre 0 |+ r K5 u9 n8 d2 ~ ND: u# O3 R0 ^4 t, z D 1 M! @( k- F3 A2 jmovement. ! t+ ?% Y" p2 h( o. [m. z/ B$ a- w Z- ]4 ]* x ATA, Another name for information./ _+ S9 y, h1 J. _' c- E+ k D$ F5 P& g" b' |/ k' X3 z sis for computation.* x8 y+ S4 {& W 恒速驱动 " X4 l: o" J" l; V. O! f见Constant Speed D .: {5 n2 X6 Z" n, p$ l& t! Q. | 期, . z" Z2 A" o6 a! a不断重复发生的事件的一个完整系列。% Z4 h( q% D" P1 _, d 尼器, 8 g. v7 W+ d0 A! ]) M慢的一种机构。. y+ [. z5 @1 j: ~/ E( [1 G- F: u9 S. p7 Y 用限制液体流动的方法以减慢物体运动的机械式阻. P* r1 u$ C' Z9 T( ^" `% B3 V* S B# R0 K" h, v5 R# P: H7 ^! p( u, ]" g 料的另一名称。 1 T6 a6 \7 c1 F4 Z+ o% v. N据库,$ J' p- J* m' r1 l$ G 数据总线, * {- y. t2 l4 I一条或一对导线,用来传输数字信息的通道。 r: q8 X/ C t& h+ z减速, 0 \' E5 p0 u* x( d, O1 b速度随时间的递减量。 . q. V! ^6 T8 ~4 Q6 k6 q固化, $ n+ X' z) v- i5 s树脂和纤维部件内化学反应使之成为固体的变化过程。+ r" f% C" _0 O- D. K& _! f! i7 m; J8 ]# U. S; i5 {, I6 K+ l* H I2 P) i) e1 H0 f用来使运动减. d) ?- A: h5 D 冲器,7 Y w* [0 ?& r. ~2 z7 L 器。 ) x) n: R7 x, c) ]! ]/ q据, , x6 A; ]" r3 y& V2 ^! m, s0 C' Z# k8 I* _! B5 K) |( q: M+ g 储存起来以便在计算时使用的资料。 % l1 G7 Y* M$ {, \' w英汉对照民用航空词典B OEING7 U3 n' K: J! N TECHNICAL DICTIONARY 40# Y1 I! g( k5 W5 c9 O DECIBEL (db), A unit of gain derived by computing the 8 I& V1 J! P( F9 O7 Ctio of input power to output power. ) i- D1 ~, Q& TECISION ALTITUDE/HEIGHT (DA/H), A specified! n9 z: W, m( [9 ` ltitude or height (A/H) in the precision approach at$ L4 b0 }' X+ W9 _ hich a missed approach must be initiated if the$ d' Q8 ~5 [- I% w) F, | ECISION HEIGHT (DH) 1, With respect to the / n- t0 `7 v3 g8 V' Q+ qproach or 5 f* E7 B m( V3 I9 [execute a missed approach. 4 i- h3 U1 u; t& ?+ H- @2 S% M3 rproach to trigger the decision of either" n- t6 C' f1 a nding or go-around. " r( G, N) K& w' K( ~/ }* ~/ HECOMPRESSION, The loss of internal aircraft air + P7 Z% b# J y- @; wressure. / y) K. L& H- k. HE-ENERGIZE, To turn off or cause to not operate. . c( Z- B c2 _+ z R6 Erom the tanks" r; Q+ c$ {, ~9 i& p; c using airplane fuel pumps or external suction.6 B8 X; [- }4 Z6 Y M 算的一个增量单位。分贝; c4 ]: P; E/ v7 b8 r% ^1 R1 E 常表示两个声音信号或电力信号在功率或强度方面的( x& X0 y( @5 c3 Y9 p 对差别的单位,相当于两个水平的比率的常用对数的十' s- [' |7 ^& W1 K 断高度/高(DA/H), x: a5 u+ l# S n! L7 }在继续进近必需的目视参考没有建立的情况下开始复8 U5 {% J" y. T% `# W2 w! J; Q 的精密进近中的一个指定高度或高(A/H)。0 [9 }6 a7 q+ d% V( T 断高(DH)1,6 O/ f$ b$ j" w- q+ w; q 操纵而论,指在使用仪表着陆系统或精密着陆雷 + n; J0 r7 Y, p* j) g. t生继续着陆还是复飞决定的高。+ ?* G# |: J" @# F/ i 飞机失去内部空气压力。( @2 @3 ?3 D9 o5 V7 J* o 开, 9 v1 l. y- z! K关断或使不工作。1 H/ {3 G' X& m0 L 机的油泵或外部的吸油装置将燃油从燃油箱排 1 N r3 f0 s1 G出的方法。 $ t! ?# I6 b0 M) i' ?ra0 ~- u9 K2 g& G0 j# b D $ L& ]2 @+ P% k& e; p) n( R$ E+ Ia0 s0 X# e8 N, [& n* }; L* o w $ a# G4 U( v2 l( y$ E# Grequired visual reference to continue the approach has 4 q: U1 E( C( Q4 _( N" b+ Gnot been established.+ n1 Z1 k2 Q( J- `5 h1 }( A5 e3 C D ) g/ |' e+ {' Z' Woperation of aircraft, means the height at which a + H" i% {* h7 A( @, {/ adecision must be made, during an ILS or PAR / r" |' }. |$ G7 G0 Yinstrument approach, to either continue the ap 3 P f! p4 o4 I/ Cto , [9 K; E2 E( z. D4 gDECISION HEIGHT (DH) 2, An altitude used during a2 E; P- V& X: l, U4 |7 R/ G precision ap 5 |- B3 V# X. A$ J4 ela g$ F* t/ l/ C7 G# u3 H0 oD* C0 c, v' B, Z3 a. N" x p5 ^* |8 d: M1 r2 M* \, b D - G; M# p; o8 V5 JDEFUEL, A method for removing fuel f! t B0 R* B" u 分贝,0 b) c8 U$ Q8 U# k) o! p 以输人与输出功率的比率来推 0 \: ~/ n3 @9 u2 ~/ x3 e3 {, j, E$ q, e2 P6 i: X" [1 e9 @8 Q: H$ v6 ?+ C4 _0 j$ c" G" M- U; G! E, j. o, x+ t1 I6 a1 A' `3 u- j$ Q' X- K* k M0 w. w! R- e: R7 Z 就飞机1 \+ o" F2 s" G 达引导进近时,必须要作出的是继续进近,还是中断进场 , a0 S9 o; w" _! e# w% J; ]( h复飞决定时的高。 9 n5 O# h5 P- H3 \" Q决断高(DH)2, & ?5 Z# R, k. l: K: b+ W2 d& P. C精密进近时产+ l/ X: ?# p( Y5 v/ c 失压," n+ k" E4 Z% i$ A' ~4 R$ e$ T Q; k4 n8 q$ Y) ^9 H) C1 t排油,3 L) ], e: P/ j: d 用飞. L4 j2 ~. M! I( y, h) x 英汉对照民用航空词典B OEING' P1 Y4 @( W; k+ W! H0 _& j- u6 J TECHNICAL DICTIONARY 41# P3 W4 A& m! ^ DEFUELING VALVE, A valve in the fuel system for ; o E8 b! L: [) o; `+ d! F/ eefueling the tanks and for transferring fuel between the" ^/ z5 }4 H; Q E-ICING, Removing ice after it has formed on aircraft.. i4 v) B: K: a+ k0 k Change or difference.* [$ B3 m6 b0 b% Y( o EPARTURE CONTROL, A function of an approach. L, q+ c. M% y ontrol facility providing air traffic control service for+ v D2 W# m0 T8 n6 }: }* h, @6 T eparting IFR and, under certain conditions, VFR - q9 g8 h; n) \2 V# L8 HEMODULATION, The process of retrieving information : M% B, h; H3 Ncarrier voltage.5 w- d5 U5 i# Z2 O2 b ation. . ]! t H" j( e: w" j6 zlic # g5 E- C' }- {- U8 [$ s2 U) Vcreasing hydraulic reservoir air pressure to 4 [# K$ b9 P9 |+ Cmbient pressure. 5 s; B& Z* ]# t6 [" z& d箱排油和在燃油箱之间4 U- r8 z6 h, [9 w2 s% s 送燃油。6 _! U5 j8 k$ U G/ m0 y 冰, , }- _4 M; j* y* t除去已凝结在飞机上的冰。 # A% X) H7 X6 p/ _6 c1 i1 a$ L删去或取消。 2 d! _4 ^$ W+ B3 [4 [量,4 W. I" V+ Q0 g 变化或差异。 - m- F' F! V0 f- g" z, C) x" j" @场控制, * o7 T, t. \( i( B给用仪表飞行规则离场,和在某种情况下用目视飞行; j& M0 J. y8 M( Z 则离场的飞机提供空中交通管制服务的进近管制设施 6 T+ L6 ^( M" U% r/ s- e; C: l6 }2 E5 a0 l- n7 c) {6 I0 Z 调, e O: _1 P% ]8 |4 c 电压中获得调制电压的处理过程。 . _* k8 B0 G4 W7 m1 ?+ Q- g# z环境* w3 |1 `$ w2 a5 h 力相同的活门。1 e' B, j7 G3 `/ J7 V1 Q: N d( c8 o+ T( X3 a3 Y/ @5 ` tanks." T. k; n m2 s2 Q D 7 i$ ^4 E. {# xDELETE, To remove or cancel.2 V" B' ~$ Y o1 a0 g DELTA,: j6 T/ W4 @* E/ k( c D u2 m. |- U+ `; e. h. L$ sc w0 s9 X( m, n2 h* Q! _0 J C d & D( F8 |# |* {! y1 H9 V/ A) Maircraft., ^/ u+ o1 C8 R+ F+ }6 F2 |& V D* W, m% ~4 [3 p (modulation) voltage from a modulated : h$ E+ G$ K) q3 z N' ~* z, H3 KDEMODULATOR, A device or circuit which performs 9 x# H; E5 D0 K& H0 ?% o( mthe process of demodul1 G+ N4 m$ V( T4 h DEPRESSURIZATION VALVE, A valve in the hydrau . Q6 B! e9 b; x3 b% y9 r7 l8 M# Zsystem for de ) f; M* G/ C! z5 s4 W, u4 @: n1 ka , w ]( e) G1 I4 w: \7 d0 f排油活门, u" r8 ~6 ?9 C( l燃油系统中的活门。用以为燃油 ( U2 f+ J9 o9 s0 R8 c& e: M G/ x' c K5 n& q& w4 J4 b4 d5 ]9 n; C6 r$ ?3 a+ T0 k0 j- M 删除,- L; Q/ h7 L1 e4 f% X7 v3 X; c4 A- u! ?$ Z. D+ i! h/ K1 W% e" z0 u$ |' E1 _: A" s9 v$ E0 j' f, w8 r4 J! r的一种功能" H& w$ Q- e" {: \& m2 I) R" n9 M% b6 ? 从载波3 o1 C- I8 a$ T0 v4 A 解调器,* } m7 X1 G/ T( G# z9 P 完成解调过程的装置或电路。( r; M& E+ S) o( K 减压阀,; e h, S8 i# o9 w4 E* Y 在液压系统中,将液压油箱空气压力减至与周围9 i# E! ~, @+ l7 n: j* A) W0 d0 e; Y, v! t. y6 m$ [ 英汉对照民用航空词典B OEING / I* K; V# o: t) p) x) g6 K7 wTECHNICAL DICTIONARY 42/ Y5 s3 P/ H6 \$ n' g DESCENT, Phase of flight where altitude is decreasing.& S3 }3 L( |* u* X ETAILED FLIGHT PLANNING, The calculation of fuel C- v' V- H. R. C, \8 l" N$ M! M" D nd required for a trip by considering each phase of2 t+ K5 X: r" N& e8 A3 z4 E, ? ight (climb, cruise, descent, reserves). 1 S7 b6 E2 h. p3 l5 Zal or, R2 M* u1 w, V& L6 l5 s& D& e/ I! D ETENT SOLENOID, An electrical solenoid used for& O! e& ?0 s$ g7 [ t.- N* o: w, g. c, Y5 K specified course or) K% G @( {% | rocedure. & P7 h5 `2 @- l9 N# ke. 7 ^$ H: m/ t1 I飞行计划, % x9 d+ }: G1 ]将航班中的每个阶段(如爬升,巡航,下降,备降)都 `4 g1 g# g. G人考虑,来计算该航班所需要的燃油量。' s3 T7 ^3 Q$ n7 ]6 |1 b 用来感应情况之正常与否的电气装置。 1 X" Z. x# o( n- s5 G- ?7 Y; V5 V定电磁线圈," f0 `; O! W3 t 出接通的电磁线圈。 2 @2 a' |+ o# F* x& }差,1 Y( K, A* U3 n 与指定的航道或程序之差。 6 d& i2 ?, r: v5 n" j用气压或液压操作的活门机构中的柔性部件。 . R; l6 V* J! t2 [D0 m1 U& C) v! y$ S: i$ U. N+ D0 z a * ~7 \: ~ @& afl$ B/ V- G/ b+ L/ }/ e DETECTOR, An electrical device for sensing norm$ T3 f' T& J/ q8 j abnormal conditions. : R2 T: q! [7 N! [4 \& @* D0 y" QD1 P7 ` w% z! w5 \$ D8 l% h* l- O controlling the engagement of the actuator outpu 0 B6 m/ [8 R: H8 n) RDEVIATION, To change from a. ]7 [4 p x5 S% @3 j/ e) F p 7 v+ M8 n7 \' A; E5 y3 a! o" t1 EDIAPHRAGM, A flexible part for operating a valve 1 c8 o$ ~- F7 g7 mmechanism by pressur 4 j3 ? L! B: z8 v4 N下降, 0 [. t( |- ?) \0 ^ V% C+ K# P3 F飞机高度不断降低的飞行阶段。 % z. l. Z/ o4 f( i' r详细5 I% a. U F4 C5 k9 ?1 b# [; j- o9 y, f. I探测器,- X& s; {! z) A! B# t5 S5 }8 r$ n0 [8 ~0 _用于控制作动器输 : \, } N" j* s# W+ |" Y. z/ n& Q; c隔膜,' D4 _6 Q! J, i 英汉对照民用航空词典B OEING3 A9 w" t3 O% X O! q. n TECHNICAL DICTIONARY 43 - k4 K( X' e0 s$ [) uDIELECTRIC, A material which does not conduct 9 w: y4 N: x# \/ o8 \0 V2 Z7 Jelectricity and used between the plates of a capacitor7 Q6 }$ _! ]/ q4 C4 g3 Z7 M (condenser). . W: J& c8 f- b1 Y6 Hnother pressure in the same system, measured in [& d' Y9 e- \5 v. k ounds per square inch differential (psid). 4 c; p2 L+ q3 D) p/ M" r9 s) F9 {IFFUSER, A part of an engine between the 9 s9 C' W& y# lompressor and combustion chamber for reducing the , I- V# S+ E, oair pressure.7 @( |; c( O9 c! H7 Y/ G0 g igh! k3 \5 V+ g2 k( W& Q; ? pulses." _- p/ M$ O- S ignal that is a close approximation of the original 3 }! v" G" W6 D: h% _ignal.2 Z6 o. k2 s x" y& C8 u9 V4 ]7 w IHEDRAL, The angle between the wing reference 4 ~1 W, I- [1 { E2 U7 y! p' I- T: Jlane and water line.) p3 y. Y" D+ |) |; N; V" _6 C 的压力,以每平方英寸* q. t7 b5 a/ I& K' B: X0 @ 少磅压差计算(psid)。 A9 N* D/ v$ q; [* e. T, [ 散器, ! S1 q; o: d# p发动机内压气机和燃烧室间的一个部件,用来降低空 + ?+ \/ }1 G2 u1 A增高空气压力。( c$ z2 m& I4 B 换, 0 S- I4 P0 I C7 I7 o的连续可% k; K3 x' \4 } K0 p6 q7 t (模拟)信号的处理过程。7 T& l& S# m/ d0 U+ V 反角, ; {3 ]6 Q1 v! S" R机翼基准面与水线之间的夹角。& m, b+ D: {# N5 F: _6 C/ z g DIFFERENTIAL PRESSURE, Pressure relative to1 @( Q" v. E) ?) g' G, @ a* K! O. J- b0 @0 M) s p 1 z5 T0 c3 }+ w6 ]& v nD 6 {- [6 p& }+ d8 Rc / J6 G+ _$ A9 @airflow speed and increasing the 3 b+ S c( l# K: jDIGITAL, Digital refers to a signal whose amplitude+ E1 b2 I/ V' {* p+ N- ?+ F8 k remains constant for a finite period of time. Digital( a. m" r; K4 V) l4 J; W: X! J: k signals are commonly represented as a series of h * B) P$ x0 b7 g* J8 u0 X! vand low ' x% A! h& M N0 l$ wDIGITAL-TO-ANALOG, The process of converting a, b: H6 n6 E; ?6 J digital signal (binary) to a continuously variable (analog) # V# R6 A7 a7 is% G/ [ R+ X, A. [ s , x8 w% H) e- D, ?/ ` x$ ^0 ~D : }+ U: c: c* G5 ]) gp2 o" @1 J* q/ w8 b, Q3 F* U 电介质, # z0 m* m9 S& Q) @% G# h) _一种用于电容器板之间的不导电的材料。 4 v- _2 Q# c0 g1 ~1 T7 E) q压差,7 A u+ }$ m$ ^. ?/ }1 O) F% F 相对于同一系统内另一个压力 + E& i1 o% d' K* ^& \* m/ D% H! v1 F, l% p- F# b( b' G3 b: @# [0 f, H {5 g气流速并; C a" A+ l8 Q& @+ n 数字式,6 `9 a" I7 H: H- K 指一种信号。该信号在一定的时间内,振幅保持不变。2 b1 M/ i) N3 a0 f+ d4 y 通常由一系列的高低脉冲表示。 / L3 O( {! d: K8 {数一模转' m1 R; n5 \/ m% V; l% ?5 P 将数字信号(二进制)转换成与原信号相似5 a n1 r9 m3 q7 x6 a( H7 g" W1 J2 E4 e" ]( u/ z D6 Q, q7 P* l* o% u( c, {! T3 I英汉对照民用航空词典B OEING ! Y, ^% e+ R. O4 t# P% _TECHNICAL DICTIONARY 44; V) V: r& l3 _5 k DILUTER DEMAND REGULATOR, A component in the * w: B6 D: m1 p; ^0 Zcrew oxygen system which mixes air and oxygen and ) _! j% ] \+ H1 tupplies constant oxygen pressure even if there are 1 q$ d6 t, T6 _ H2 Q4 b) r+ K4 [hanges in ambient cockpit pressure." R% ?6 l: z4 r9 @; d }) L2 ? IM, A word value of light. For light control devices - dim 0 b9 u7 R9 B4 @! Q d0 _the opposite of bright. " t2 u! E6 h5 J. R0 f: t: oIODE, A device which allows electronic current to flow$ u- e; L4 ~2 z; W only one direction6 k; L. @! Y5 N6 ?5 U8 I6 f% ~ uid in a reservoir. ! C6 F3 V( e" {0 F6 |3 r( UDIRECT, Straight line flight between two navigational3 l; z9 J: w" F0 t% x, o( H6 |5 z4 f aids, fixes, points or any combination thereof. When $ v3 n g- o! ?; {: A6 H7 hused by pilots in describing off-airway routes, points 2 }- d+ }! S% X V& Z3 j* Tdefining direct route segments become compulsory& K- \/ k) q1 I. o, \# i7 v reporting points unless the aircraft is under radar4 T9 C% l% Z! h, v7 a% C control. A" F7 L4 t/ c/ p( k* d节器,- ?# \! ?' \/ q' @$ f. X( Z 将空气和氧气混合,% w8 W U) d) E 使驾驶舱环境压力改变,它也能提供恒定的氧气压力。 9 x1 ^& u2 {+ X/ [4 C- z5 M7 o: I9 D1 G9 ` t4 b一个形容光线亮度的词。对于灯光控制装置,暗的反 8 A9 t5 N7 |# O2 O0 D1 S5 x词是亮。 2 T5 h0 w" L3 |2 F& H3 s" V, `9 ~极管,0 Y' i n. Q& q! ]( l6 } 只允许电流向一个方向流动的电子装置。 : x" z! r5 [: g7 O7 d( [# l0 _器内液体的量。7 v) O1 o% B7 i9 X/ R3 t% F6 _) E4 H# S- u 直飞,; j3 W+ c3 W4 W- y' w 两个导航台,定位点,导航点,或任何的组合之间的直 & B+ M$ ^, ]; X+ X) a线飞行。在被飞行员用于描述偏置航路时,除了在雷达控* F S3 ?/ \6 }( `; r4 ^ 制的情况下,确定直线航段的导航点成为必报点。# m' }2 O" q% [: a" z4 ^ s ' h2 \( r2 w! p/ Wc& z& G1 T$ R4 l3 i: H D/ `+ |2 D% n& u4 M+ g is * E9 }1 D4 O! O! g2 ]; gD K) [0 E* ^' w: uin" D: R- G7 I) w+ k DIPSTICK, A calibrated rod or stick for measuring a0 v; X( ~+ j% G& Q quantity of fl 9 B% O9 w" w6 C/ O. S* D4 c5 f稀释氧调- W- B1 d0 ]1 j Q+ {/ U 驾驶舱氧气系统中的一个部件,它 ( o" `' T7 g" u6 F, w4 s, I% _6 _, n4 b" O2 ?. a5 N. @1 @+ z7 z& t9 F1 r. K' D4 Z: q/ F. z/ u8 _3 s" O# s% [: w 量尺, % { k8 q \" T- M: x& Q* U+ ]+ v校准过的棒或尺,用于测定蓄液7 k8 m% G# [+ u1 j& H, \ 英汉对照民用航空词典B OEING 1 m6 j+ G% @) Z/ ] Y8 X! |! }TECHNICAL DICTIONARY 45

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