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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1 z: W! |) Q5 I" L, c: ^& A* _ 民用航空词典 , G* v& d2 _; T k. k波音商用飞机集团2 F2 O. ~4 X* k' U, ~! K% X& }, q6 \' \ BOEING COMMERCIAL AIRPLANE GROUP 9 `& \8 M$ c4 @1 T英汉对照民用航空词典B OEING9 D: ~7 F) N$ c: K1 u9 O" O TECHNICAL DICTIONARY 17 N5 Q1 L) C2 o* l( b" a A# }$ o- o+ n5 K2 E. }- K ABEAM (ABM), Beside: An aircraft is abeam a station9 d8 [/ P" D* @ when that station is 90° to the right or left of the track of , F' L+ L+ s% q* }; e7 hthe aircraft.6 P; E$ G( V4 |6 P ABSOLUTE ALTITUDE, The actual distance the aircraft h, ^2 B$ [6 h; X/ K is above the ground. 4 x4 T. _3 I+ k+ i! AABSOLUTE PRESSURE, Pressure of a liquid or gas 1 Q7 h& ^4 e4 c4 Y) o* Z$ B6 D/ Dmeasured relative to a vacuum.) x; u3 s( ]) G$ `0 j6 D ACARS, SEE - AIRCRAFT (OR ARINC) REPORTING 1 I! ^. {" ~4 X$ oADDRESSING AND COMMUNICATION SYSTEM+ u/ B; M# n5 ~0 V9 I8 q% }% w5 p ACCELERATION, The rate of change in velocity with " L% q7 M5 u0 s4 T |0 irespect to time. 4 [3 N0 y2 ?6 ~8 V# s lACCESSORY GEARBOX, A part of the engine, 9 o/ e2 L7 F7 j4 _8 Kmechanically driven by a compressor or an angle % T7 {( ?5 ?' D0 I1 xgearbox, for driving components necessary for engine 0 U* z2 s1 y+ S( o正切,$ H7 g( |' [' ] and airplane operations. / A6 b) v2 ]& z- A% [3 l/ B当电台在飞机左侧或右侧方与航迹成90 度时,飞机正 5 B) Q7 r! `: f0 Z1 l切电台。 ' z8 @. J2 Y% @# B% j绝对高度, / Q& E' u4 P6 m4 d. h4 |( J飞机离地面的实际距离。6 c; G# y0 |% W2 i. E' O 绝对压力,' A U6 _' x1 H5 ] 相对于真空(无压力)测得的液体或气体的压力。 % q1 \# W7 B) r( C飞机通信寻址和报告系统,: a! Y2 C0 o7 o 见Aircraft(or ARINC)Reporting Addressing and6 T" l( ?4 j9 v Communication System.$ T' X/ V7 A. D% I5 s# J 加速度,, Q; Z6 \* o: ?! }! Q 随时间变化的速度改变率。( i: l% f! x7 R7 Z" E2 ? 附件齿轮箱,6 c2 }2 I, a3 _; y& \* q- I 发动机的一部份,由压气机或伞齿轮箱带动,用来驱动% m' \6 Q2 d% I1 T- g- ? 一些使发动机和飞机工作的部件 E8 P8 b6 P' c/ ]3 q英汉对照民用航空词典B OEING , j( M1 ?; v" R% \* NTECHNICAL DICTIONARY 2$ A0 E; ?( [6 |- f6 a ACCUMULATOR (NO. 1), A container with hydraulic9 E5 T9 L! _- a1 [$ l ts when normal hydraulic supply is not 2 x8 ]- D3 Y1 C" Kvailable. ) l! v& G" F* a* u( e/ FCCUMULATOR (NO. 2), In a computer, a special$ t# u5 A3 F- m& ]/ a; j$ a. G torage register associated with the arithmetic logic unit,2 @# [! Z- A1 z3 C2 ? olding the results of a computation or data: ^7 w9 {2 U& Q" d ACTUATOR, A mechanical device operated electrically,4 T6 G( M/ @, M4 E" G5 i3 ` hydraulically, pneumatically or mechanically for; k5 |8 G @& I7 V transmitting motion between components.5 R. n, R9 c/ p2 ]: E* e ADC, SEE - AIR DATA COMPUTER( g# L" L1 Y( H ADF, SEE - AUTOMATIC DIRECTION FINDER $ p. T1 @4 c& ~ADI, Attitude Direction Indicator, An electronic display of, f0 E$ e1 e, ], I. Q" F2 g5 L e airplane attitude information in pitch and roll.+ ^: F5 P; ?% o$ F3 Q: M9 u+ ?% y4 G 蓄压器(NO.1),- k' Y4 V L/ G5 T( X4 J" F6 L 含有靠干燥空气或氮气增压的液压油的容器。当没有正3 N& e# ]& }: e& I1 t n: G 常的液压源可用时,该容器可用以驱动部件。 4 _* e0 K; z- ]8 ^& x! H7 ^0 V存储器(NO.2),1 f* I$ a9 M0 _ 计算机中,一种与算术逻辑组件有关系的特别存储寄存 ) K& `) K" A7 A+ n4 f% x r器,用来存放运算结果或数据传输。7 i2 S9 s( y0 O' i; | 飞机状态监控系统, 7 z- }4 A+ R) k4 H见Aircraft Condition Monitoring System8 _& `" w; C/ X3 J- `# C fluid pressurized by dry air or nitrogen for operation of& ~) y/ f b* G0 k8 a$ h( _ componen % T/ m+ |0 [! i+ h- Q9 f$ ma2 P' C z: ?! ]" j! t' Q) \& ]7 I" h9 ^ A l0 N7 h( u/ T1 \8 h+ Ps 5 E" J9 B5 P1 Q- Pused for h/ K5 B k0 }7 B: ~ transfer. ( J7 L- q; G8 R2 G; BACMS, SEE - AIRCRAFT CONDITION MONITORING * u; v$ c3 A' S8 [. t% i, cSYSTEM .# G3 h3 k- s1 X+ j: | 作动筒, ( ^' Y+ w( c6 F# a$ X* c+ V由电,液压,气源或机械驱动的机械装置,用于传送部 ! [/ k. l2 R: ?. W件之间的运动。 * a) R% I! x, W1 o, n大气数据计算机,8 r" ]8 i Y X" ^7 e0 q 见Air Data Computer." ~8 E, G. Z u# ]2 F6 V, B 自动定向仪, e1 ]. f2 D) Z 见Automatic Direction Finder. . m! F! P% U7 U) l7 H0 k姿态指引仪, 8 Q6 }# S b" m5 k用来显示飞机的俯仰姿态和坡度的电子显示。* q5 \ q6 H" ` 英汉对照民用航空词典B OEING 1 d0 A) p' D! L+ QTECHNICAL DICTIONARY 33 S z: _6 y4 R" R# W5 \( T AERONAUTICAL RADIO INCORPORATED, ARINC is : d0 a6 E: i! @8 _, , u: S& C, _! [# x5 T' m$ P& m! Znufacturers, and foreign flag airlines. ARINC0 ^6 X& W( Q; N+ m" `$ a( R evelops and publishes standards for electronic 2 R6 c1 s& T+ f6 Oquipment and systems.) j% b, S3 U2 _( G+ X5 j, v GILITY TUNING, The capability of the DME to 6 P/ o5 t* [; b5 w. flternately tune between two different DME stations in 0 n5 v' { @7 erder to get two distance readings from one ) Q b/ ?; L' `5 s- X- ]5 P, fterrogator.6 B* l c1 n$ S; F& {7 H2 k& v ge 3 Z' R! X; e" J0 B& L6 n& D( MILERON FORCE LIMITER, An electro-mechanical # U4 K: i$ V! ?5 }& j1 eIR CLEANER, A component in the pneumatic system: e. Z9 n6 ]& b2 { upply to the air 0 B u: R' ~' [$ Z- x0 yonditioning system. ! G& f7 Q$ F5 I% T1 H6 |订并出版+ y4 D, B5 R9 Z; e- h. {4 T8 Q 子设备和系统的规范。 9 V( P; U. w- \* e4 n9 N! h7 W6 P快速调谐,/ s3 a1 T' l& R4 X& ?8 u 机载DME通过交替调谐两部地面DME电台以测得来自 : w& ^8 x2 q$ M8 E2 h" l9 E! A2 ^同一台询问机的两个距离数据的能力。 ( U- G i, J+ p1 P! D翼操纵力限制器, 1 Y P5 t. n& k* m, L% |装置。在自动驾驶工作期间,用来限制驾驶盘: R$ Y0 ]" t# O5 X2 | 气清洁器, z% x- H" O: O+ T2 b- Y% ]- M部件。用于去除供空调系统使用的发 - P' N+ |& N) t0 ~/ }# D: Ha corporation whose principal stockholders are United 5 ?; J) \8 x( c1 e F4 }- e mStates scheduled airlines, air transport companies : D6 e; o0 O* t4 N% t8 Z+ Oaircraft ma / y' j3 g/ y: ]/ l1 t* C6 s) t$ wd 8 c6 i% e- ?7 c# He+ m) n' t- |% E6 _2 }! g) C A* f( T- b6 S2 D) ]5 g {: t a 2 n4 t0 B0 H: Y6 L- g* A( t/ I' Ko- l6 j+ R6 R# |5 G) V; U% u in ^$ D7 }9 V7 o* c. {% n4 n! JAILERON, A hinged moveable part on the trailing ed) `$ U9 ~4 P1 P. J4 C% |1 @ of each wing for airplane roll (wing up and wing down) & n3 B* I7 {& k) r4 \$ O4 {7 a, |4 ycontrol. s- |1 g6 h% kA . [; y8 F( d& q* Fdevice for limiting the control wheel movement by the- Z5 R9 o% X7 B" V+ V: M5 d autopilot during autopilot operation.! Q+ N8 ?% Y3 Z" J; D7 r2 X: } A' Q8 X" P- K7 h1 F/ w8 Y- {' z9 W for removing dirt from the engine air s 0 T7 {2 I. r4 ]" H4 F3 e8 Dc 2 q' I3 S! ^$ l3 |航空无线电公司, ) [1 V4 d1 M- n, h2 [6 d, i! P主要股东为美国定期的航空公司、航空运输公司、飞机 * m! ]6 T8 f% p# i. _制造厂和外国领队航空公司的组织。其目的是制 * g% T- b0 q0 q* G- z* L5 x+ I. k8 c* L2 o4 U# p9 | 副翼,+ p. E1 s; S# G2 y3 }5 C% y6 n 铰连在每个机翼后缘的可动部件,用于控制飞机的滚转0 r& V# D- ]8 [+ U3 M (机翼向上和向下)。: T0 Q) G2 f7 N# w/ K, S7 U7 m( k/ x Z一种机电# [. h; b9 ]9 o 的动作量。/ {( A$ |; {6 F9 | m" @& p" \9 [) e* E4 z- t9 @, D2 k气源系统里的一个" ~+ Y$ ^ j1 t 动机引气中的灰尘。 z0 Z4 Q2 ^& l/ M9 s" C- k 英汉对照民用航空词典B OEING 5 _! J7 Z0 V- Y( v& XTECHNICAL DICTIONARY 4- G+ F. Q6 `2 @% b AIRPORT ELEVATION/FIELD ELEVATION, The+ e N$ F/ a' J; i) H highest point of an airport's usable runways measured* u6 `1 z5 `; v: @& Y in feet from mean sea level. In a few countries, the : J H8 \7 v5 K8 w0 xairport elevation is determined at the airport reference; v* k. k+ X: y+ Q point. / l% D. m+ _4 b8 xAIR ROUTE TRAFFIC CONTROL CENTER (ARTCC), $ t [+ C3 @/ h, [/ u1 @ervice3 C) ?5 ~8 W& T3 r ase of; x& D+ z: O, A+ o us flow of air traffic./ U# X8 f1 @' f IR CYCLE MACHINE, A compressor and turbine on a+ X- p; e8 Z* z- G8 M+ k ommon shaft for cooling the air in an air conditioning1 C0 ]# g9 @! _; ^ ystem. The air is cooled by expansion from high to low E! O* u' u& e ] {ressure across the turbine. The compressor is driven - g; L& ^3 }; n4 g5 [1 e6 r" r( yy the turbine. ; p- a- F: t2 o; [中航路交通管制中心(ARTCC),8 M$ G1 J6 L: I5 S% b 域范围内使用仪表飞行规则飞行的飞机提& W/ H: ?, U# h$ W# F4 w/ O8 z 管制(ATC),7 I; J$ u9 P, k) R# ]' k, \6 o 涡轮冷却器, 5 p/ o1 F' b# I' X' Q; C是装在同一的压气机和涡轮,用于冷却空调系9 x6 _( l# f- _) E% s* |, c 统中的空气。气经压气机压缩后,由热交换器移去热量, 5 P9 G j2 P* r! u' {/ d% v2 i然后经过涡轮令涡轮带动压气机。通过涡轮之空气,温# s' I0 R) I7 v, q+ K 度下降。; b4 u5 m1 b5 G$ M: u A facility established to provide air traffic control s ; \* M$ S( h9 g# Z7 p! z9 m" ~to aircraft operating on IFR flight plans within controlled 3 M% v) G/ e7 Q6 s5 G& I2 K$ m7 |5 K% F' Eairspace and principally during the enroute ph $ A* v2 T3 Q2 ]flight. * G9 L. P9 K- K' @4 d) y) mAIR TRAFFIC CONTROL (ATC), A service operated by 2 d, o% m/ z; Zappropriate authority to promote the safe, orderly and6 \6 {4 w# T8 a expeditio 6 c. N+ V; h1 s! l. Y) ?2 }5 N6 c6 l) v( N) KA4 }+ K- C0 D8 B V) q0 b3 i c4 K3 T% b% U5 J/ f" O4 a s& j( h$ G/ s7 I6 x5 {! z1 G p: z9 P( N; e# s4 H0 ?1 t; J7 g" ?2 r b( `. h/ d) p2 C+ { 机场标高,; i( O2 n$ s% O l 指海平面与机场可用跑道最高点之间的距离,单位是英 + |5 i) i* G% j+ J尺。有几个国家的机场标高是由机场基准点而决定的。3 g" J% |: ]- ^2 @. b- R8 \% o; x4 h9 k; D' K给在控制空 " P5 H; Z: K* V5 F供空中交通管制服务的站台。8 K! [$ y! t: ^" d3 L$ C 空中交通; {# j6 y5 c, q" H 由有关当局管理,旨在促进安全,秩序,和效率的空中 ~$ i; K* K5 M# w7 q交通服务。9 @/ y/ h7 B1 Y" ^" p; Z 根转轴上' `4 |/ `% x! v/ [' } \1 a: U& C- @/ ^% t& u. G7 _, I% L1 l$ H) z6 T. b" W# h英汉对照民用航空词典B OEING - j$ m3 b7 Q' K! E0 ^: N" Q1 u& sTECHNICAL DICTIONARY 5

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发表于 2008-12-24 21:36:52 |只看该作者
AIR DATA COMPUTER, A computer which produc; @4 W1 B4 V1 K; W7 y data information, such as altitude and airspeed, based 1 |/ x& M0 Q1 ]% n9 \4 Oon pressure and temperature measurements. 1 D% \/ h4 M& k% {8 Pes air 9 Y2 T$ C: i$ bIR TRAFFIC CONTROL, A system comprised of" @8 N: s$ o5 c# W" L round and airborne components used to identify, track5 [$ V$ w( `- e1 ?9 F% F: l OUND SENSOR, An electrical device operated 1 g) n! a* ]; ?, B0 m& Sy the landing gear, which transmits on ground/in air2 I" V8 A8 R2 n! P5 B( t* } formation for system operation in flight or on the 4 i' d( S, t6 E& [( mround. + q4 n' N1 H+ M2 _IRBORNE VIBRATION MONITOR, The AVM takes - q6 b" D$ l% ]e signal from the engine mounted accelerometer and + c D: b; D+ U ]8 U ]alculates the vibration on that engine.- ~9 d( d2 |" w$ P2 Q- U9 N; P# @ corridor equipped with radio navigation 1 P! R; Z2 V# K1 }' gaids. : R# z2 i% v |AIRCRAFT (or ARINC) COMMUNICATIONS # n5 h6 @7 Z. \3 }( a" EADDRESSING AND REPORTING SYSTEM, An , ~1 d( Y9 ~- m- C7 y7 \addressable digital data link system which permits the$ v5 h6 x( ]. w# \ exchange of data and messages between an aircraft% ]1 e/ v% d" B- V and a ground-based operations center over a radio# K# i0 L) o& e' _% G& {! G network. 1 m$ \, w7 B0 \% O4 R' W3 OAIRCRAFT CONDITION MONITORING SYSTEM, A% U4 @' T6 v+ Y( v' E5 J system of sensors and recorders to monitor various 5 b e; L4 i1 h" V1 Mairplane systems' performance and status. M0 w7 |+ K) D" Y% U2 O, _0 ` 机,) f# ?; n% x& E6 i% F* t 中交通管制, ! Q1 @' ^% e7 v" B% c& u一个由地面设备和机载设备组成的系统。用来对飞机进 ! l. \& e! j$ [! a地传感器, % {! d8 s/ R/ |+ n5 n4 X一个由起落架操作的电气装置。用于给空中或地面的飞+ g0 T1 ]# q2 \& S5 L 系统运作传输地面/空中信息。(有些系统只能在地面 $ j# ? E& A( A用)% D1 [' y, z2 D 载振动监测器(AVM), % X& {" U# F7 ]8 OAVM从装在发动机上的加速器取得信号后计算出该发* s5 Y, F% r2 T: S 机上的振动。+ `) o. V& {. j% w 式建立的控制区域,内有无线电导航设备。* o. [. q& \6 p7 K 飞机通讯寻址和报告系统,7 S" B$ z0 T8 _, j5 X 有种可寻址的数据通讯系统。利用该系统可使飞机与地& u3 V+ K5 l2 K( s8 b8 p" _* n# S 面操作中心通过无线电网络进行数据和信息的交换。* x4 e- }, `3 _$ I8 ^( z t- E/ |$ h 飞机状态监控系统,( c1 L, Y, q; D/ V6 y+ T 一个利用传感器和记录仪对各种飞机系统的性能以及 # T, E9 F: s% Z状态进行监控的系统。' f% ^% o Z) j6 T A5 E. R5 B# i# g, @0 |# E1 N g + V* F( s5 E$ X" `6 ~! R& Xand locate aircraft. 4 H$ a4 [" r& _8 NAIR/GR & _( _! c" U0 y3 T+ H5 g: _b * O& d w) v) u( Y! Yin( x% o0 c5 Q: T* y8 F g6 n$ b) {) [3 m& {! N, F3 f- O" [ A 7 H P( h0 Q( M7 I; c; uth ; z5 A( A( v" N; w2 F- ]$ |c ! f& \, d' J. mAIR WAY, A control area or portion thereof established$ u6 l3 p; z8 E, x4 y5 V) o u in the form of a . h( \) ~9 a: U# n q% m大气数据计算/ W' d% v7 R8 g: a$ }% b 根据量取压力和温度而产生大气数据资料(高度、空速 ) O; z. B" K0 c$ c/ K2 x% `0 C等)的计算机。 8 T0 l' _/ X0 ^9 q( J' [! ?8 _: t7 f: o7 I 行识别,跟踪和定位。 : C& ~$ u) @' F! ?2 v5 [: p* e K& N8 M, G$ ?; X" d* q$ I' d( M4 N 使. k& G* ^, E/ }) k+ u! m, z7 }- _! f" O9 z7 @+ R3 Q! k 航线,2 S2 ]9 v+ k: l. C0 } 以走廊形- e. R- j4 M: A8 {/ ^! { 英汉对照民用航空词典B OEING; v3 T9 U5 v% ^7 `2 f4 T7 D TECHNICAL DICTIONARY 6 & C# j" ~0 K% F& hAIRFOIL, A surface designed to obtain a useful reaction, & ~9 ?7 R- p+ Ksuch as lift, from the air through which it moves. Wings, / x; J6 P7 i, K/ F* A' [2 jstabilizers and control surfaces are airfoils.) u8 W: ? \) J9 v AIRSPEED (IDS, TDS), The speed of the airplane9 ^; v' R) ?& j- j2 ? rough the air.) B. a2 i/ g# ?5 f$ h% v D INDEX, An adjustable pointer on the # Q7 w |" S- b/ L( ~+ |* }irspeed indicator.% I- {4 n- E2 A7 J8 T* H3 D and legal ability. S8 J' {0 o) |2 D" t fly. ! R3 P6 O# C# ~7 x( um, for example, the procedure for finding the6 @! f7 L9 K& x quare root of a number.5 w) J5 a- m( f. s' {' { y* n# v% [5 e2 ~9 d, J re, wind, 1 a3 D; m$ G J1 gand aircraft flap setting.9 a; l6 A8 t# q8 q 是翼面。 9 }, G/ |" w, n9 K7 o速, : B7 j2 y$ t5 N飞机在空气中运动的速度。, B& } w) a2 K+ p& w% A: \; Y7 j( H( N0 Q+ e7 l在空速表上可以调整的指针。 ; T3 s% B6 V+ |1 X机械飞行能力、和合法性的飞机状态。 " B1 ?5 b7 @) o& r一步一步的解题方法。例如,计算一个数的平方根的步2 C3 S5 ]# w7 E" \6 ]3 c! X1 t! _9 X9 K' c0 n- y# z$ A2 @! o {( T9 @ 资料的法定文件。! f/ ^# h0 D) Y0 B( f 翼位置成函数关系。 $ v' u4 w" V; ^9 r' _th0 I9 M; d/ _, K3 z3 [ AIRSPEE ' n( Y/ W% O0 S, }' ua- w% e: Z Z% {. _ AIRWORTHINESS, The condition of the aircraft with) q( U; J0 M) _! n7 ^" J! h respect to its aerodynamic, mechanical,3 [' w3 O, s" y A& a8 P9 V to * h3 M. g+ z9 J6 }" L' H+ V8 HALGORITHM, A step-by-step procedure for solving a1 [" m7 B1 H& n# e/ U proble ) a% r! C2 U k7 x" K$ P% M+ P4 bs/ ?: x# i+ S/ H9 w. P, ~* I' K4 O AIRPLANE FLIGHT MANUAL (AFM), The legal , s9 w1 W% J8 V3 M) Fdocument containing performance and operating limits, % T1 L4 C( C3 ]# Y' eoperating procedures, and takeoff and landing 3 |% ^8 Z( B" f3 Cperformance.- ?8 Z; U- |+ i. T6 ]9 l AIRPORT ANALYSIS, A comprehensive set of takeoff 9 y1 M! @* w$ u8 O0 eweight limitations for a given airport runway, generall : Z7 ?6 ~& H$ e/ x& q8 `. Rpresented as a function of airport temperatu ' G6 x: }1 |5 |7 e; h6 S翼面, 8 H' t: W% J) x8 M用以从气流中获得反作用力(如升力)的表面。机翼,; o9 q5 C, i3 b3 Z 安定面和操纵面都 : {; H$ z3 E7 i: L. q9 o" ~ ^+ E5 t; f% k+ Q f+ `4 h空速指标( e' \ S, f1 r( ?9 N% M% L 适航性, / G- m8 z6 z+ H9 k3 I有关气动能力、+ `" a/ x2 j1 d$ t 演算法,; [6 F# Y2 S& F% b8 v6 X1 n) K2 c5 d u, ` 飞机飞行手册(AFM), f8 V% m; Y5 ^, g- A5 ^* i6 E: i B 包合性能极限,操作极限,操作程序,起飞和着陆性- r1 V4 q- h c5 a7 V$ {; ]* w+ J4 @* A0 ~* M机场分析, 0 D* L( x: t% s$ V# W- k0 a一套针对给定的机场跑道的详细重量限制资料。通常与 # O1 T- c; y" [机场温度、风、和飞机襟 4 k" X: [: F/ ~$ H6 v英汉对照民用航空词典B OEING 7 G: l, q* d% p$ OTECHNICAL DICTIONARY 74 J7 ]5 E- h7 ]* u# w AIRSPEED BUGS, Adjustable pointers on the airspeed 2 S6 d! X0 X3 s4 \ Bindicator.# D, U. Y- C% E8 v1 s0 b7 ~ ALLOY, A mixture of a basic metal and small amounts % t" {" U+ ]2 I8 H, ?# y' ef other metals to change the properties of the basic " _3 `0 R1 r/ n( W& Jetal., x: A. C7 a( }/ k Minimum airplane speed. $ Y! O6 K. [8 e+ O0 G% V% X3 e4 a# @e of 8 [, D. N4 q$ c; c. N) s; Y gitting airplane angle relative to! z. h5 J& k' g! R5 G7 [5 v irstream for the stall warning system. ; G5 p" }6 P7 P! a* R4 b- Kanother. - f6 w/ L: G( p, V: H% M' F; g! dLTERNATE , An additional airport selected during 3 h5 x! P' D4 P5 J& _+ V5 X: i' \! Y2 T5 Q/ b 合金,* e; k( V/ W, K {2 y0 ~/ Z) t. M 在金属中加人少量其他金属,而改变其性质的一种金属2 B4 `& n# i |9 g( d4 V8 ?5 ] 合物。 Y" q5 o/ [0 b& n% `# {5 ^4 g飞机的最小速度。) ?, n6 m* n. n6 y+ h9 O 速警告系统传输飞机对& l$ N& |6 [0 C6 ~ 流的相对角度。" r: j- m7 W( y( e 由一个状况改换到另一个。5 ~: S6 i$ F- \; ^, p 降场,3 Y$ |7 Y9 O: Y5 M8 r! ]: ] 划时,除了目标机场之外,所选的另一个机% s# e& o w7 \! x1 P o ( {1 z* V; B6 x6 N+ zm 8 H# A; e8 k* x, kALPHA SPEED,. q8 f2 j7 I( N5 b. A. h& C ALPHA VANE, A small moveable airfoil on the sid ! D3 g7 x- v3 E: S! n V; U7 Rthe fuselage transm W$ q- G: h( k1 K1 ha 3 X0 ?# k: ]/ U# f9 zALTERNATE, To change from one condition to$ s, Y9 h6 D* k% ^ A5 h6 t7 z7 ~( j! f: e; Q9 \ flight planning, usually near the destination airport, to be 4 x: g( h& r) d' `! x) k' v: cused when it is desirable to divert from the original* U; W# v2 V3 t' x1 U9 v# P destination airport.& {+ k; F8 F) g) S 空速游标' ^2 L' x3 s3 E& R2 @ 空速表上的可调指标。/ x) \: i. t+ L9 q- U6 H2 n9 b. |1 P0 ^# |9 C迎角速度,' o W/ M" b' E. D4 P 迎角叶片,9 k( n6 z5 Q' K7 K$ n8 {/ a 位于机身侧的可动小翼面。为失 R- W2 x9 i( W+ N e: T2 m0 M& f `5 D2 F 交替,+ Z- a3 k* y0 j& |2 v `7 _. ?( f& a, ]! `, ^ 制订飞行计 8 F+ S6 U8 T2 j场。通常在目标机场附近,以备不去目标机场时,改降之 " V% {% ^8 u4 ]5 @3 H用。 3 s- }5 x* }( H0 h) N9 b+ }* h% P英汉对照民用航空词典B OEING ! t5 c2 \; v& CTECHNICAL DICTIONARY 8: {3 V& [3 Z& f6 t5 C ALTERNATE AERODROME, An aerodrome to which7 H3 @7 n2 N/ e; j/ G) g( i8 G an aircraft may proceed when it becomes either 2 C7 ?0 y5 y+ M' ~7 K0 tpossible or inadvisable to proceed to or land at the. i& M' Q) h& K$ [. k6 d erodrome of intended landing.3 d. J8 r4 c; d3 B: v. A TER SETTING, The adjustment of the altimeter: V& Q [5 y' W0 {& O7 ~& i. h# K# w account for local variations in atmospheric pressure. 9 v# e) S; C+ r& cLTITUDE ACQUIRE, A digital flight control system ; ^# A { a0 V' Qode to transition from climb (or descend) to level flight.) L0 ?/ i' P% [4 W LTITUDE ALERT, A flight deck alert occuring when the+ f- D& C# W7 R* {" ? irplane approaches or departs a selected altitude. 7 c5 c/ i' x6 I. ?LTITUDE CAPABILITY, The maximum altitude at * v4 D! l; Z; M& B9 [! i5 v- _hich the airplane can be flown at for a given thrust, . h0 g! Y8 N- Speed and atmosphere condition. 2 P3 b9 J% i/ R) uLTITUDE HOLD (ALT HOLD), A mode of the autopilot * p [6 U& i6 u2 j2 ^, h+ Ar flight director to maintain a selected altitude.( N O! H+ l5 N5 n irplane's altitude during VNAV operation.* @& e' S. g3 s4 W7 d6 o0 X& g 机场着陆时,可作着陆使用的8 m. V8 V% D# k% U% d- ? 场。. J1 v8 g9 Q8 S) f0 ?6 s+ G" ?0 y. D* _9 R% A% O, N+ ~ 根据当地大气压力变化而对高度表所做的调整。 $ g3 k+ _1 ]) n4 k一种数字式飞行操纵系统,从爬升(或下降)改平的模 ) |# g# w2 _" E' \7 X( E+ D. d; g, V1 I. E0 i度警告, # _! o* P7 h* n; x. E0 `当飞机接近或偏离选定高度时,所出现的驾驶舱警告。, _ k8 ^ z8 u3 Y3 u" ?6 E- ~ 高度能力,/ n1 y( m- V9 b1 @ 在给定的推力,速度和大气状况下,飞机能飞达的最大 v3 U, p0 s; ]1 Z2 ?" C/ K9 m) q2 F高度。. x1 t' B0 H; `. B 高度保持(ALT HOLD), ) V# g0 Q! @, F$ a% R0 B& ]! `自动驾驶仪或飞行指引仪保持在选定高度的一种方式。+ E/ ~ L; z7 \9 h" M. q/ c' W3 a. E4 K. C, J/ Y 员对飞行高度的控制。 - w# q' l& c Y; g4 m) g& sim * G8 c; h7 G! P/ x; _a 5 T) J- ~( A) }3 `ALTIME ; e7 q/ @$ g1 }0 S" N% wto$ ]* _9 u, j% i7 V2 w" D A9 h. h) ~1 D! d m / |0 ^9 k- V' C: }8 E; z" O7 OA o8 S: e; _0 I* T/ S5 R a( s% e1 U% G. m% |; R A( v% {8 q. T# y, P1 |* R! e w; P: I( I, ^1 } s - i7 b. s0 A4 A& S! U- B6 gA0 e. @, m. x b o: Y4 \. `2 R; v- c ALTITUDE INTERVENTION, Pilot control of the * p g2 S/ u0 v7 R0 x' f% sa 6 D( _, F( ]1 |8 N2 SAMBIENT, The surrounding atmosphere. 0 e+ e# h ]8 h) S, R备用机场, - N# T7 W" y+ _0 z+ ]; L/ O当不可能或不适宜在预选 ; B$ ^9 ]. n2 r1 K- D2 x2 |: C' K/ L$ h 高度表设定* Q# X1 l2 `1 s2 A) f( b1 p& m 高度截获,1 F) ^+ I/ l9 }! {2 R& r% G- C, J2 p& Q4 S# }- @' X% A$ R J9 K. O/ q 高度干预 / u8 R) ^3 Z- t; O在垂直导航工作过程中,飞行 4 z% Z. M( `5 @周围环境(地面气层),/ D' v! X6 Y- W2 ]/ n, j 物体周围的环境(特别指大气)。 ' [% S. c J, j4 [) N4 F英汉对照民用航空词典B OEING/ c# a2 ~3 V7 \: k/ L# C TECHNICAL DICTIONARY 96 j2 C+ d [# X) ^ AMBIENT PRESSURE, Pressure of air surrounding an X/ e$ y1 d4 m- W; z7 H object, measured in pounds per square inch (psi) . 1 t4 f% {# E2 C/ ~% H' o( z6 ?MBIENT TEMPERATURE, Temperature of air, |* @- o9 [$ Y2 ]- W9 ] mpere., S4 z8 f( a) o4 u( [. G+ z urrent waveform.1 C( P+ C. ~3 R0 }& ? g an' {, U6 Y( N( C E: `& q nalog signal to a digital signal.& z/ g1 x: r8 b; e& ^0 Y+ ` ore inputs: ~; m; `( T* [) G f binary digital information and one output. The output & Q3 q1 I& K r; |/ p1 only when all of the inputs are 1. The output is 0; G. f' j- v* { hen any one or more inputs are 0. ' O$ ^; U& k) S+ ]8 t* d! p面气压), 6 R F/ @0 W/ _境温度,5 J6 \7 b) F8 I3 @ 气温度,用摄氏度(°C)或华氏(°F)来 0 `0 O3 k& z. R& k3 Q# z& v! `6 N1 o5 T9 r b3 G' |, v电压或电流波形的幅度。 ' T( }3 q8 v' n性变化的信号来工作,或产生连续性变化的信号 & P+ ^: E; Y/ }! y! h6 c1 r统。 9 r7 }/ V7 P' s: h% o3 E将模拟式信号,转换成数值式。( K- I/ G! g3 @/ z* [ 一种有两个或两个以上的二进位数字信息输人,一个输 7 _$ ?% k3 `5 ^7 o9 T6 r( x的装置或电路。当所有输人为1,输出为1。当任何一个 1 \( w. B2 x* Q: o* E一个以上的输人为0时,输出为0。 1 K2 c; m) \1 n' ~+ |A 6 q7 {, u; a' p5 [4 P' n' usurrounding an object, measured in degrees Celsius 2 q: \2 U K0 u* r5 ](°C)or degrees Fahrenheit (°F). 7 v& t6 }# S9 e& K8 uAMPERE, A unit of electrical current. One volt across ' x2 v' m% q+ \one ohm of resistance causes current flow of one $ B. p+ d+ ?, F. x/ G G$ ka & z. h& ] l( T, B& p% }+ |AMPLITUDE, The size or magnitude of a voltage or$ ~0 m) B. m$ A c ; `" h0 d% L) aANALOG, Quantities or representations that are 2 F g: R& I- ^9 G6 w% Ovariable over a continuous range.+ J ?( u5 O# h0 U$ L ANALOG-TO-DIGITAL, The process of convertin; M4 V) L5 W* g, y0 K a 7 a K- ~, s# D! Q: C. E1 r$ q5 \AND GATE, A device or circuit with two or m 4 Q1 L; c! h) i) D, ?o * ], b9 h2 G0 W+ w3 N) fis5 n; Q' ]4 P7 X. Q w 2 v' T- v$ x' R环境压力(地- E4 \% ?, ]: b. p2 L 物体周围的空气压力,用每平方英寸多少磅(psi)来 ' ^9 s7 v ~ R2 y度量。! i4 ~: S) ^5 E& T+ W4 x% u+ M; V物体周围的空- \7 l7 o; _, L. D9 Y8 A& u 度量。 C1 k3 y1 `0 [( ^1 K安培,& l! I( O( H0 T! a 电流的单位。6 O7 u8 Z* p& ~$ ~% f; E 1伏电压在1欧姆的电阻上所产生的电流为 $ x" x% Q. a2 L- J1安培2 p P5 |& |# Q1 e* M) { 振幅, 8 K, u% T+ y0 @0 X9 C; @模拟式,, l, o7 F5 ^6 U+ s% B+ d 用连续 4 b' o% v: d$ p- l4 N3 O/ R O& ^: W0 ?, \- i7 i 从模拟式到数字式, + `$ [! c( N8 t! A4 B与门,8 Z2 z9 |) m; X1 i3 x/ N8 x5 M9 H: V" L' y- C% J, s b& M0 i+ V9 r7 }0 U& @ 英汉对照民用航空词典B OEING # U( H! ]7 h+ ]( ?8 x" n* d2 v2 f$ aTECHNICAL DICTIONARY 10' W$ H; X# Y" L S. u0 S ANEROID, A sealed flexible device containing air at low$ O7 I; d4 U7 Y6 } pressure, which expands or contracts during change of , y: \/ L# L8 h6 e6 S# T) Pressure outside the device.) C# U. W+ q) S2 d$ J3 K ically % b3 `8 M4 v7 ?# gr changing the direction 7 q4 r2 s n4 ~( P9 T' ?9 {f drive.: C3 ?: c4 i% y. ^4 I! W of the wing chord in $ F- M5 a9 Z, K/ Y5 v( u klation to the free stream airflow as it moves forward / b$ p, N: F8 K3 F* R8 G+ trough the air. ; P% R) `$ Z7 I+ m, _al axis of the : a& J, k% t; Paircraft. ! I# i0 g% q6 y( `+ B( E- n5 M8 T胀或收缩。& |5 E, S/ D* h% h! Y 箱。是改变驱动方向的机械装置。% Z. z$ ?" t2 U& O 机翼翼弦在空气中向前运动时与自由气流之间的夹角。# Z* H( M8 N. N# I# B9 t- L9 m+ ?/ J8 ]7 n9 N0 w$ qp7 f1 s7 p+ v% q- f ANGLE GEARBOX, A part of an engine, mechan, l) A4 X; s9 U driven by the compressor, which drives the accessory + B4 E. o. [# j7 X* A& Z" o) J: w) Qgearbox. A mechanical device fo 4 S |0 M5 p/ v1 fo 6 {8 K7 F. P. y+ i. yANGLE OF ATTACK, The angle% n6 R4 v+ l9 o( ` |5 W re& S r% }: h# d8 Z: A: @/ u th+ _' G" \1 E6 N5 ` ANGLE OF INCIDENCE, The acute angle which the ( y1 b8 g- _4 Z7 {8 z/ Swing chord makes with the longitudin ! T& K6 r" E" p- k- J膜盒," N- z, b$ {5 @& @! |" e$ _8 ~ 内含低压空气的密封弹性装置。当它周围的压力变化 # v6 _# _9 M: T6 ^时,会膨4 a: I6 Z2 o6 l) e# q b8 w 伞齿轮箱,7 A: O- U% G/ `/ Q* }: z. a$ p 发动机的一部分。被压气机以机械方式驱动,然后驱动 7 M; x2 {7 H- U }$ [( I附件齿轮 7 D7 {+ h- x6 P0 T2 P& y1 d' x迎角,1 S* Z0 R9 z0 y$ b 安装角,8 {& @. s( J3 S- A; G0 b 飞机的纵轴与机翼弦线所形成的锐角 $ ]- W& |+ ?) \5 C/ k% A, [英汉对照民用航空词典B OEING2 Z# V+ G; R2 e$ l7 d: P- J7 r TECHNICAL DICTIONARY 11( Z- ~0 ^0 |, ~ ANNUNCIATIONS, Audio or visual indications used to 0 p) C% C) j$ }6 I @0 j+ jcall attention to an event that has taken place.4 K* U$ m# d, W) [ ANNUNCIATOR, A visual device consisting of a number 7 B6 a9 C, \5 n: I: \ly./ N" C6 X7 P2 E ANODE, The element toward which the principal stream/ y6 Y% J% u$ q! N8 B) J" X of electrons flows.5 a! B* D9 B$ |; T& h) G) j ANOMALY, Not normal.8 C. a6 e# e& c" C ANTENNA, A device which, used in conjunction with a ; j! [: N0 h& D9 Stransmitter or receiver, is used for radiating or receiving6 A" z# N! F8 c" X. p6 I radio waves. & u6 a; P3 `: sNTI-ICING, A method of preventing ice formation on 3 `+ k( d1 w" h3 e; [ we wing leading edges and engine nacelles.1 y+ ~ B5 h+ ~/ y. s" m" A NTI-SKID, A system for providing maximum braking2 C* n+ J8 n) }7 E; l1 F ithout skidding for any runway condition. Anti-skid, w' \. d; V' W& ]7 ^$ a omponents are part of the brake system.2 X1 ]2 v# g' C6 q7 N 告, + [* C' e# v, G8 |( c当发生事件时,以声音或目视指示形成的提示信号。 / B; q2 u, e- W8 W6 f2 U与之有关的电路的现有情况或已存在的9 Y" x! I6 Z0 o+ L6 W5 y* \2 g" s- S- Y7 S( A8 B 正极,; v- ^) i6 h1 J4 f& E 主电子流向的极位。' @) @; f+ j- a9 [) j! k: u 异常,1 q. c( N$ p) D- `( C' r 不正常。1 a* A6 V$ ?) K& t" h& b- ^) k 天线, * B$ l" Z2 f6 `5 n一种与发射机或接收机共同工作来发射或接收无线电$ K9 F# Q& p' T) z: m1 T0 v 波的装置。 3 u$ w4 f: W$ ?( f5 B冰,& u' ^! c5 ]9 l 防滑系统,3 W3 ^4 e* q( v+ E+ G' c5 k 一种在任何跑道状况下,都能提供最大的刹车能力而不 - L, C; b0 F" b使轮胎打滑的系统。防滑部件是刹车系统的一部分。 9 b; z( A- c1 [: _1 R f: ]of lights. Each light indicates the condition which exists5 \- N. D6 k4 [* o& {% ?/ }+ J% l q or has existed in an associated circuit and is labeled! \5 X$ L8 l) D; Z, `+ E. ?3 d b according( i7 x- H5 @/ G A# n: {5 d: D( M- ~ th / @. z3 n% O5 R: F! @. S5 RA + {% |- l0 x8 C7 a( G4 Dw 8 |( }* u: E2 n9 ?2 `/ R Cc ! X& ~. V- |( ^; u5 Y$ n! I! k6 _1 Q5 i: a& J5 e3 [, A) ~信号牌, # w4 D4 A% m0 D& ^由一系列指示灯组成的目视装置。每个指示灯都有相应 `2 M1 h1 ~. F5 `: A/ b3 X 的标记,用来显示 % y+ }6 \0 z$ r6 O( T1 d* M( E& y" N. I7 Q8 B$ ^9 {+ ?2 O( O( t3 O. X; q 防止机翼前沿和发动机短舱结冰的一种方法。, [/ i( P8 B7 T/ h2 D0 V) J1 @8 P 英汉对照民用航空词典B OEING 7 C2 V/ E6 g2 c$ NTECHNICAL DICTIONARY 12 . b; z' I( n8 \/ uAPPENDIX, A supplement to the Airplane Flight Manual 3 m; \) X5 K1 u) Y& l2 |tained in the basic manual. A $ v. ]% J1 o3 L6 N" q! Nollection of supplementary material at the end of a {& ?7 A+ U9 \3 N, v1 Dook." M5 S8 ]) ?# \) u- K. K of the. d* E3 G k2 g( D& V6 w rsion link on the landing gear.- z" k, i- V+ M) V6 q/ k+ p8 |) ^ APPROACH MODE, An autopilot/flight director mode * |1 r3 N- T. Uwhich is a combination of localizer for roll control and: v, X' w5 `( r: z2 _: n" X- w glide slope for pitch control. This mode is used when full; ^. j- r \- ?% O; E. M instrument landing system is available. + d9 T0 J- Z; A- Z) cAPU, SEE - AUXILIARY POWER UNIT ' R/ n% J8 f6 {" YARINC, SEE - AERONAUTICAL RADIO ; k3 Z" m* a# c6 BINCORPORATED2 O* _( O6 g0 S3 C, X# ` ARM, To make ready for operation., U% V0 s9 }- R6 ~, m* R 附录,0 B. k* X; V) e$ V Z5 n3 b6 [' c, V 飞机飞行手册的附件,包含基本手册中未提到的飞机形. J2 q. B: ~& J1 _8 } 态的其他性能。是附在手册末的补充材料。 / a4 m% w/ w; T顶销,* u+ {# \* W0 {+ \3 v7 O 用于连接起落架扭力臂两部份的销子。 $ f1 v% g3 O- t3 x" M进近方式,* s( }7 ~8 [6 B 一种综合了控制横侧的航道信号和控制俯仰下滑信号7 E8 m. @1 U J) \! 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 & w' A! ], i$ q( Z \统正常时才使用。( W- ]4 Y7 {0 X* q% [ 辅助动力装置,7 j m" E& h0 U' d 见Auxiliary Power Unit + U9 X4 J) `1 t% b+ w, wcontaining additional performance for aircraft/ G8 q4 m' w7 g N6 U! b configurations not con1 z: g( @3 F' s: R8 A' S c* M- l. U: z( C1 Q. x2 y2 u9 w4 ` b2 P4 q* l4 X; l) S4 g3 c APEX PIN, A pin for joining the two sections7 A1 q. ?* b9 R- t/ B5 X$ z to ) C. a9 v, W4 K# |, j) i* A+ ?1 I航空无线电公司,- m6 }! ?, E& X& J$ ~5 k# u6 l 见Aeronautical Radio Incorporated. 8 M7 Y; o, ]% `9 `& P1 {3 }* [3 n9 S预位, : D; c4 j2 |2 G3 P, N$ s& W8 b$ n部件可以开始工作的状态。4 {3 q1 A* `* q% M9 i8 l 英汉对照民用航空词典B OEING2 T* Z8 p d2 s/ ~5 m+ h TECHNICAL DICTIONARY 13; b: ~; o9 I [ ARC, The curved track over the ground of an aircraft9 }3 |& n5 c/ g. E0 q6 p2 a flying at a constant distance from a measuring " }) ?) B6 B% q- }equipment (DME).; R% O' D# R1 \* m* v1 F in the limits of self-contained system; L9 i( Q8 l2 T: Y apability. J" V2 J$ e8 L7 f tem for opposing or restricting8 N! S# J2 q: ^/ Y; s! } ovement.% k; K6 G, N7 ?; ^; Q SPIRATED TAT PROBE, A sensor that measures total* v: F2 V: w. M9 Z8 G! c$ G ir temperature when the airplane is in the air and that ~' W/ F$ i+ J- Y1 ~$ H easures outside air temperature when the airplane is $ t& D1 }0 m* `8 k" {n the ground. The outside air temperature is measured& v W! l' Y. h- U/ ~0 n+ N4 G SSEMBLY, The fitting together of a complete structure) a- N3 J# P) t8 z K) A" h# d SSUMED TEMPERATURE REDUCED THRUST, The & _3 E" Y8 E& U/ P' h DATC, SEE - AIR TRAFFIC CONTROL 8 I9 X* O3 O }- j' ^$ R1 `- t$ o7 S 系统中所产生的一种用以抗拒 9 d: f; H+ o6 N z0 h作或限制动作的力。 . _ \) y3 ]: K. b& `头, @) g- n: d0 \ 用来测量飞机在空中时的总大气温度和在地面时的外 ) J% g% T! Z9 F. T- |% G温度。地面外界温度的测量是利用引气将外界空气吸入 0 S! a/ i: D- b# @头,以达到测量的目的。2 X1 P, p' ?9 E) {; x3 x 配, . ^5 [6 D7 p. r& z. e$ M' w9 n. B一个完整的结构或组件的过程。 ! j8 E6 Y- f% I+ P0 a% O假设温度而得的减推力, 9 @& r+ q; \( u _4 K$ Y推力设定值时,假定一个比实际外界空气温6 s+ _& m' d4 g7 K, c 空中交通管制," Z- Z% z& n3 \3 F! V4 ^! L/ } 见Air Traffic Control 1 }3 \. y" U$ u+ tAREA NAVIGATION/RNAV, A method of navigation ( G2 ^: }: h5 E0 \2 N0 Lthat permits aircraft operations on any desired course `9 F6 T* R8 A7 pwithin the coverage of station-referenced navigation% p' I4 ^2 g& q1 j6 K( t signals or with. y! c% X. e* c" o, Y" \( G7 K. m c 9 }5 d2 j7 ]" y3 i7 iARTIFICIAL FEEL, A force developed in the flight5 A D' V8 S7 q7 j1 f+ w- `& r control or brake sys v/ I( E; O% |1 t5 | m / h, j% E% o# N( m: XA1 S( ?. S1 \/ _2 Q- K ]) g a0 U, f( t7 |: {; S% S- N, ] m 2 K/ t- K) ^0 p1 [* ^o! [0 E9 b9 V1 ? by using bleed air to draw ambient air through the 8 n) C8 e+ Z" R" V/ d( d5 i6 d _sensor when the airplane is not moving. % x/ e5 S* a( K6 y/ a4 r: y& ?A5 [0 p2 y0 X3 ~ or unit. ( D0 P' o% |. DA( w2 h1 p& X" D, P8 E3 C1 ~ lower thrust obtained by setting a higher than actual - z' X; v1 k5 L" P$ xOutside Air Temperature (OAT)." ]8 L$ x+ J6 A* L 弧线,. S6 |% W4 j' | 飞机在围绕DME台等距飞行时的弧形航迹。" z3 |0 A8 | j7 D1 [) [& ? 区域导航,# c. h. i$ E" r1 n$ H0 X3 [ 容许飞机飞行在有电台参考的导航信号或自备系统能- o" }7 M4 Y" `! ~3 Y2 G3 \ 力极限范围内,飞行任何预定航线的一种导航方法。, }8 \# ~3 V2 y/ c5 s 模拟感觉 , a$ F6 }2 k/ _. h在飞行操纵系统或刹车 ( a- T! i9 U( c7 r C# g: ~4 Q4 M6 D1 E: A 吸气式总温探. S2 X- [1 n% U" e" H; ~4 U7 |+ d# V* W9 c# q. _; ~/ n0 G ^ ]4 x7 D& c9 v2 k, ]组合成 ! t- D" a5 ?8 y/ t# g* G, i& A% f, F在选择起飞 - ?/ B' S" `. Y/ P度高的温度而得到的推力。用这种方法可以减少发动机的 2 U' J0 i+ [3 ^' _( p7 I( z0 m磨损和维护费用。 # a |/ ?1 z" n5 V% A- G3 l0 t2 |$ X% j) Y9 [ 英汉对照民用航空词典B OEING0 Y6 ]% O6 g3 ~* s! i+ \$ w) S3 I. g TECHNICAL DICTIONARY 146 d; Q$ B5 U1 m, d N% |# o( n ATE, SEE - AUTOMATIC TEST EQUIPMENT; {' I" m$ @, J5 h+ n: W: ` ATMOSPHERIC PRESSURE, Pressure of air due to the1 e. R* _) @$ E7 y# S arth's atmosphere, expressed in pounds per square+ H# |6 N' _) F% G. n3 t% [ ch (psi) or inches of mercury (in Hg) or millibars (mB). 1 w! e. T3 W p# @* V- YTTITUDE, The relative orientation of the airplane with # ~. |) R; ?. Q \+ E$ T- G6 t# Gspect to pitch, roll, and yaw.' E" Z. g, }. ?4 I1 w UDIO CONTROUSELECTOR PANEL, The panel in 7 j+ `; Y4 k; C8 V8 pe airplane which controls and selects the routing of ( z) N0 {* p6 ~% E& P* Q6 M& pudio. 4 S0 g0 ?* i$ \/ F8 A: I: J2 @" SUTOLAND, Automatic landing using the Digital Flight* w3 u! }9 ], b3 l p0 \: @6 j ontrol System.9 `6 _1 c8 w4 A2 V n. - ?# Y$ _9 k5 [# @M, A system w0 @+ c; p) e0 O* r0 k, Q8 h omposed of all necessary subsystems needed to guide7 K" S/ H, r. K: w. k e flight of an airplane. : a2 X* J8 K$ q' Q% Z% P+ [EQUIPMENT, System test* K6 a; s7 B/ x! y6 S quipment that operates under computer control.8 J. E& W; y' m6 @( B 装置,

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e $ z; T% O6 f: i* p( C; k: C6 ?5 [5 tin( X( z3 ~! b5 [9 D w( \- D) v1 u A & S/ f! R" x6 P2 S. Rre ( E* U. u9 p4 P5 YA3 M5 D8 Z8 s" c/ I1 _ th# l; q p. ]- V! Y2 E! P O) X, ` a 1 [9 A" _' @5 x/ _, A( DA # y V% e% A' w1 Q0 \+ T1 Q' MC . T' d5 m/ T3 t/ J# t! EAUTOMATIC DIRECTION FINDER, A system which % k2 F p! X/ t* _+ ]5 L5 V. Rdetermines the direction of a radio statio . K# f* B5 V. y* _. n+ A0 w( tAUTOMATIC FLIGHT CONTROL SYSTE 2 O9 ^) `" R0 ^0 z3 b$ jc * r$ c( P8 E+ p+ B; W8 Nth 0 T. R7 d$ `& F: _* v# iAUTOMATIC TEST * C- ?$ ^4 ~9 je 5 r5 j- K2 M+ x' Y" c( |( J自动测试 ; a$ P7 n- e( g0 C: m$ D% r" O见Automatic Test Equipment. : }) Z, `# }! J' Z. d大气压力, S7 c# }# S! w) x! o6 n \由于地球周围的大气而产生的空气压力,以每平方寸多, r7 Z7 G) R1 h! z5 H 磅(psi)或多少寸高水银柱(in Hg)或毫巴(mB)来 - U% j: i! N; b示。 $ ^% Q! D* j4 o: G- \: c5 X飞机姿态,0 \. M% `% ]9 z7 P9 [2 B 飞机与俯仰,坡度,和偏航有关的相对方向。' ~# ~" ^9 v1 p4 Q 音频选择面板,: t, T# X# N; s7 p 飞机内用来控制和选择音频通路的面板。3 _* A. {. X8 c: B 自动着陆, : o, Z2 v: V% j! t0 d1 b0 ~9 n, J使用数字式飞行操作系统来进行自动着陆。' j' \7 m* K& | X 的系统。 9 J4 G8 ^7 a C4 C. L+ @$ M( J7 p; l4 P系统所组成的一个系统。! Z; T" k% g* G; Z 在计算机控制下运作的系统测试装置。% m6 g# Y7 V9 m L2 q5 i3 A' p6 o1 h# ^0 e; b T; @& I% u! r0 |4 v* I 自动定向仪(ADF),8 l" Y, }+ ]& U 确定无线电台方向 2 O4 g- Z0 ^. T" F5 X: ^& K) h; w# A5 a自动飞行控制系统& v5 e: y/ C1 i+ A% I3 D& M 由所有能引导飞机飞行的子 / s P6 f0 D6 ?) W6 |0 S2 m自动测试装置, ; I; m' N9 z! w# y英汉对照民用航空词典B OEING! c) J" ]' c: L% K( ^! [5 {; { TECHNICAL DICTIONARY 15' U, }5 O3 K9 k* s" h+ t% j h6 u AUTOPILOT, A system which automatically controls & `" Q1 V9 D4 M$ {, Aand guides the flight of an airplane. ) `0 w7 u# O1 gAUTOPILOT FLIGHT DIRECTOR SYSTEM, An + ?, W6 v I5 _/ h9 s1 mtor 0 G1 V" ]" P/ r, U3 fUTOTHROTTLE, A system which automatically 0 |" n, M7 ?. c2 U% Wontrols the throttles of an airplane.. `4 h: F! B! b2 @ POWER UNIT, A small turbine engine in) H m. z& g( a( s( I3 i1 u8 [; N e airplane for supplying electrical and pneumatic 4 Q" ^& H! _( a7 ^0 L. jower for systems operation on the ground or in flight. / ?: ?2 x' B& p' H8 {. c5 r) oVM, SEE - AIRBORNE VIBRATION MONITOR& z, U% N9 I: O! z7 R X) f XIAL FLOW COMPRESSOR, A type of compressor7 R; \; U* i+ E. |2 g! w2 _# I sed in a gas turbine engine in which air passes through* p* a# B6 B; n XIS, An imaginary straight line or an actual physical 9 s( `' G) y* J$ d2 U, F! [ U Y b$ \omponent (such as an axle) around which a body can ( G' v* D2 C" T' _. \tate.1 r$ T1 A& b9 u. t' l 仪, 1 K; _* G8 p4 R5 z. {$ G% w4 g) G& b2 y6 {# w0 P自动驾驶飞行指引系统,* }% n! l2 u5 |* p 动驾驶和飞行指引功能的系统。 8 X8 Y$ p: T0 s8 Y, q4 I7 @动油门, ) f U7 J. V" R& u" w6 Z" R自动控制飞机油门的系统。 ' k( s5 ]2 _9 f! ^+ s是飞机内的小涡轮发动机,在地面或空中给各系统提供, D$ f1 O, e' u" _% x. P( m 源和气源。 X) E% I' A* F" S, G 称。 ) _; k- E/ E. V$ p; d, F7 L" U载振动监视器, 4 R: @, l6 P; _0 k" J5 W! V o见Airborne Vibration Monitor! c' s! u3 m$ J integrated system containing autopilot and flight direc+ s" t2 e( j T2 U functions. + c+ ]# p3 u r8 `+ JA; e/ J9 W! W$ j2 M8 ~ c 2 }1 Y( U* f; ]6 ^% ? e4 QAUXILIARY , ?% G! x9 N5 _& Vth9 p5 t6 U' L( U p% f+ h5 E4 s( I, L1 X0 R AVIONICS, An acronym designating the field of aviation5 a, Z) |1 A+ Y0 S electronics. v) y' s$ Q; q2 H7 I- _A : A, W4 P; r9 s- S* P( \6 {/ |' VA! @8 U+ K, T6 D6 X& v u 2 v7 _+ f# c5 h# Mthe compressor in a straight flow, front to rear.: g$ [4 b3 w- e( s1 d1 |2 a A 2 U9 I! ?6 i! S1 I. {c& U: M/ R& \ p% B9 N' i+ G x2 G ro0 j0 A5 B. P4 d$ x+ Y, }: [. N 自动驾驶1 `: F$ ~! }+ D" i7 }! Z- S 动操纵和引导飞机飞行的系统。 # w! J. X- H }, U; t! } e一个综合自* c6 _% r( n2 N. f1 ]: o2 x$ {3 u7 q% }5 R, M( r" \ 辅助动力装置,! Z; ]" T! X N9 _9 Q' c" ?7 g$ g) B1 `# n航空电子学, % x) R6 E. @* O5 T3 j1 L是航空电子领域的一特有名 ! T4 G) ~& d7 V1 l7 g: q8 a e/ | \2 l: j, s4 e1 L. X5 E2 H2 K3 h& U& I流压缩机,8 m! {8 S* i- X9 s; J2 n 一种用于燃气涡轮发动机内的压气机。空气由发动机的 + k' q Q; `( y: d部流出。 & Y: |: C# K: W$ Y5 M6 g$ r3 N线, ! p5 t; j5 C, S# V! M* c# ^可让物体围绕着作旋转运动的一个想像的直线或实际: E& [# a3 W( G, b6 w 在的部件(如轴)。- v5 @0 w/ w, B; P6 d: Q2 z0 e, `4 \" V n/ k- c2 T! X* e 前部轴向流人,压缩后,由后/ |( C u4 ?; U; G& y5 N9 Z: d/ k9 X! y; {$ E0 ^' d( y; _' E& i英汉对照民用航空词典B OEING $ }6 Y: m( |9 K$ p+ ?" KTECHNICAL DICTIONARY 16) [% W8 p- N* l B ( F3 p; d' w; H: ^' j" r1 iACKCOURSE APPROACH, An approach to a runway ) n2 d; [) Z) R) ?9 ^* G& {versed.3 {7 D |0 Z9 Z7 w. n# L4 A, }- b! E; | own on the EFIS that ) D# ]& X* m" o2 n2 `+ R# l; J; }oes not readily change, for example, navigational aids.. }9 w! z* o9 N& e7 H: ? vement in the tank or reservoir.7 q" M5 l7 E! D( O' [# V ALANCE TAB, A small hinged moveable part on the ( v% r. h8 \( C" B6 mailing edge of a control surface (aileron, elevator, ; w2 F( W+ o; g3 v: ?& z8 t" v# y航道进近, $ q4 e+ ]9 |: F% M H相反的进近方向。当反航道进近时,无下滑 6 g5 S' j% ^3 }0 k9 ]显示在电子飞行仪表系统上不经常改变的数据。例如:# \. {0 w! O7 B& Z3 [6 e 航设备。 / `. p( L- X* ?$ `. A2 X& W V在燃油箱或滑油箱内阻止液体流动的隔板。 8 }' S' C( e6 e动补偿片, % O2 a" O7 i' M0 R* A铰接在操纵面后缘(副翼,方向舵,升降舵)的可动部。0 t* u- E# T8 j: Q 与操纵面相反,以帮助操纵面运' A7 {* Q; ?5 B' d( P& N B ) X2 ~* P1 ^' F3 Wwhich is opposite the normal approach. For a * N( D& b6 y* m) _backcourse approach, glide slope signals are not . p: p" S& j3 b, T0 V' F/ N/ _available and the sense of localizer signals must be * p* e+ |) m1 C: |; Vre 9 @* D2 F$ b9 Y5 m9 CBACKGROUND DATA, Data sh 2 v+ q7 p# G4 l0 A0 K0 Wd ) ?/ x2 X# A& f* Q0 ?7 VBAFFLE, A partition in a tank or reservoir to prevent# ] ^# R" B/ o" s8 N) e* k fluid mo* Q% s1 _; `) B4 q B0 t) t# P% R3 }4 S/ ~ tr( C$ d9 ]9 R$ O A- ` rudder).The tab moves in an opposite direction to the 7 D) G( l$ p" vcontrol surface for assisting movement of the control 2 }6 R5 }% A* h9 m( lsurface.- h" B$ _) k& `" \5 x: P2 k" E0 }* l) n: o7 a( r& d, ~, Q" d与正常进近 $ ~7 f; d/ }5 q# b0 P6 C! U6 j, J道信号并且航道信号也必须逆反。' V$ E5 T' ~' r* U+ z W+ s9 W 背景数据,7 O5 N- N) x: a% |! |& {8 m9 M# x/ E, z- | 缓冲隔板,, h5 X+ y5 r8 Q Z$ U" L* ?6 {. A' j J* L0 I随动补偿片的动作方向 ( e' G5 Q! r1 \9 ^5 `动,减小操纵力。 4 P: \2 H8 A2 P O" x9 e1 k英汉对照民用航空词典B OEING, e( }1 \5 a/ J l8 y TECHNICAL DICTIONARY 17 1 k( y8 ~5 D' G2 X( ]% c7 xBALANCED FIELD LENGTH, The field length 3 V8 p8 V6 k2 R2 F* m0 L9 Tassociated with optimum aircraft performance when0 \8 Y1 r% \3 b/ ]2 r I6 S bstacles are not a constraint. In this case, after engine r/ s. y* b, p# E$ _$ k$ q( U2 D0 L5 } ilure at V1, the distance required to accelerate, takeoff& F& d, }6 p) w3 u nd reach a height of 35 feet is equal to the distance- m3 G' X* X$ \! E* ]: Q ALLAST, A weight installed in an aircraft to maintain 8 V$ L/ }$ _7 {2 O( F2 KALL NUT, A fixed spherical nut driven by the5 B7 `; b& q( d( C' c. W/ O1 t AR OUT OF VIEW, A signal used to remove the flight- Y0 {: C2 _# G' @" E4 W AROMETRIC PRESSURE, The pressure of air above . C3 L8 Y* w, H" Z( v9 p: Gg) or $ }) h, a# l8 Vmillibars (MB). $ S$ q' h7 R" n2 j4 @ATTERY, An electrical device for changing stored/ C( K$ T) ~) k 性能的场长。在此 $ B, l8 U" y8 w \: P3 I; N. A况下,V1时发动机故障,要完成加速、起飞、离地35 * M1 J& R- Z7 |, v5 ?. t- _尺所需距离等于相同速度下完成全停所需的距离。 ; |7 b8 e- F( O2 B舱物, d8 R- T' W" R7 Y% m, U5 x6 M重心在许可范围内面装载的配重物。 2 ?% b0 W: T: o3 z) R5 p形螺母, , y8 M- w2 m$ c! ^0 ?* f的固定的球形螺母,用以使襟翼和水平 * P: o2 ~- s/ X1 B% V# B2 m- W; L引杆消失,0 l7 z4 | q C" `* b- ` 指引杆的信号。 ( E& _2 w/ K0 {8 U0 U* h# [" A+ v x压, 0 J6 l; M2 x/ ^) v: c0 D' g- c. R: n压力。通常以多少寸高水银柱(in* s4 \5 ]$ D' b# q$ y( y* _ 瓶," H) X# x- s0 G8 ?2 Z9 b. C 的化学能转变为直流电的电气装置。 ' V1 \6 y1 }8 q9 j+ S2 u; `o ( i- b( H" ? I: ufa - m! d$ g" H+ r) \0 }2 ]a. S. |& K8 x; `2 l, b* { required to stop from the same speed.. c- P% q: b3 | B , D' P) d2 w$ \. C; bthe center of gravity within allowable limits.& U2 k! [' z8 L& C B# w b/ x+ |0 B/ Q' b( T jackscrew for flap and stabilizer movement. v( v& B# y' q5 H" M( T0 AB9 W# ~3 D4 S$ u2 a. h director command bar(s). ! r; F2 L, `1 {, ^4 `, L j" D6 mB 1 h. t) S1 c* v9 ~3 tzero pressure measured in inches of mercury (in H * M& j" p1 t5 u0 E& Bin' \/ u/ L5 a4 ~ BASE METAL, The underlining metal to which alloying / l/ H( K& \3 t# A$ ragents or metals are added. , c$ ?+ W, z) F# V* e' oB; n. V' r& [1 F chemical energy into direct electric current. : S! i4 O3 ]0 r" F) }平衡场长,. j [ R1 G( q: n3 g$ ? 当障碍物非限制因素使飞机达到最佳 . h7 a6 _) ?) I- r4 |( J6 Y: C* E6 D" w4 n7 T$ V, S' B7 G4 u7 Y2 }4 z6 L8 a8 w% z2 H/ X' `1 C j" v) V为保持飞机 ! g/ d! M' B% _! }! E; p m- w5 D; D 由粗重螺杆驱动 ( i# V# D0 N( L) R! ]3 g: z8 G安定面运动。5 w% ]9 f1 _$ `; j+ T4 m# x/ J9 d0 _. r7 ?# C& ?# w1 O用于除去飞行 % j& x+ ]% H9 R7 E( `6 h4 v+ E0 v& j$ Q8 z7 x零压力以上的空气, l# e, |2 m) b2 c! X& Z- C Hg)或毫巴(MB)来表示。1 L9 N$ G: T: \- A- U- D 基底金属, 9 X0 w( N$ I7 P* Z% D+ Q* R指合金中的主要金属成份。4 Z7 m, [* `% y# W3 e& ~+ B$ _* u; u将储蓄 - `3 _2 l8 |# _- d2 H4 f7 f4 R英汉对照民用航空词典B OEING - x$ V4 [% }1 n6 _* `) _+ pTECHNICAL DICTIONARY 18 % {, G: A8 J$ XBATTER1 B5 S0 p6 W6 R$ R! s C/ g; _ direct cu* V2 l3 i" A; K. p7 s" X, x' ~ power su# t) f) n8 `& E. u* a Y BUS, An electrical conductor supplied with - C) {! Z- z! K& E3 qrrent from the battery or transformer-rectifier for, Z+ i" ^' ?% R1 \- o: V: R: a pply to operating components. * a% j. N$ _/ a9 n4 E4 mCHARGER, An electrical device supplied $ B$ n5 J2 y( B7 j: P8 D) kith alternating current, which produces a direct current. P |9 e) ]- } utput for charging the battery on the airplane. 1 a; l# B- z5 I6 l/ GAY, A compartment in the airplane structure.2 O% x V P. P5 P F: _ CD, SEE - BINARY CODED DECIMAL 4 a& \! s9 i1 R( G, I# }9 PEACON, A device which emits a signal for use as a 5 D( a) T. h6 I- q: Nuidance or warning aid. : s% Q/ j+ b; j0 g& Q4 xBEARING (NO. 2), The direction from an airplane to a , x8 S2 k6 v1 f' Q* L2 O: Hground station." |* U& T G: r$ E2 K1 s- M% { 瓶汇流条, $ z0 U" k8 ~5 d6 \( k% x: `将从电瓶或变压整流器来的直流电供给工作部件的导( N' @& Q4 z$ Q3 _% Z2 J2 D, v4 v 体。 G* V5 P1 E0 b6 ?" _" C 瓶充电器, 5 E. v% W$ M1 q' m- G$ o, n用交流电向飞机内电瓶充电的电气装置。带有交流电的+ b. q8 H, O7 N& t! u! c+ s 气装置,该装置产生直流电向飞机上的电瓶充电。 & @, C1 B. x( `( g舱,( O! f, o( G" ?7 _* o 飞机结构中分隔的空间。1 X8 `: G3 W( C# S2 T7 ] 二进制编码, 9 A8 |1 ?1 j* Z- Q1 u/ F7 ^" P见Binary Coded Decimal% B; F4 e* j- ? BATTERY& d) I, F2 ?$ y5 e: R' S( F, T2 f w ; I) t6 {2 q" h4 j. l' fo ( \, s$ Q' O9 P; _* @B 1 w8 b# |6 q, b$ T( F& G5 j# uB. p/ i7 H E& q- \) Y$ ? B* W, T) Y; j R- U Q: O; t* L; B8 K g & `5 v1 f- X. s% \* e# x3 L$ S9 `) UBEARING (NO. 1), A surface that supports a moving . u1 O- q4 `! xpart and reduces friction between the two. 9 H& E' T7 f Q0 T' ?( F! q' o {5 K8 f8 c3 p/ O3 l* ^- D. f4 L m) i4 m3 U1 ]9 [- v/ s2 F9 Y: W3 d) L( M4 F! k8 Z/ ]2 Q. u0 I h: R, a: B( q- W+ v. d" v/ ~+ `: R 信标, ; U( E# g6 Q4 E* G3 g发射引导或警告用信号的装置。( K) f0 ]) M2 e, ~6 ] 方位(NO.2), . V, `" }8 r# U: i从一架飞机到地面台的方向。9 D& c+ N+ j8 r! | 轴承(NO.1),$ u4 D. p7 e$ n1 C/ v% z3 F 用于减轻机械转动磨擦的机械装置。 - u; \& m O+ Z$ G. C. f8 s英汉对照民用航空词典B OEING' N+ P( e1 z' c: _/ z9 f TECHNICAL DICTIONARY 19& c4 N. b" I0 n S' T- ]8 P( x9 N BELLCRANK, A double lever in the control syst2 X1 H3 H6 ^8 I3 K& z- Q$ p0 f changing direction of motion. $ r4 l) |+ ^: ~. ~3 l5 Y: Gem for: e! L# ^6 S" x9 ?" N9 X9 \* j0 _ ct in the $ W- _3 c/ {& _ D. dneumatic system for absorbing expansion of duct due" J7 q$ o; g& a3 V+ X$ H& H heat. ( l' g5 v9 { P0 q- k/ p( uELLOWS (NO. 2), Corrugated folded or pleated7 d+ {) P" j$ k/ r- X ontainer or compartment used to measure pressure. 1 t. Q8 S4 ^9 s8 G [0 oEZEL, The part of an instrument case for locking the 0 V4 d; z3 F% ~1 Nlass.. B$ @" e* n8 T6 [9 ?4 f IAS, The potential difference applied between two1 P; E8 }5 h% s9 z& j oints for controlling a circuit.! c8 k8 X. Q4 {( i/ L0 ^/ z BILGE, The lowest part of an aircraft fuselage. A place 9 X- B% a; y% Ywhere water, dirt and other contaminants collect. 4 p0 N7 Q P* X5 S5 X$ R: _气源系统内提供管道热胀冷缩所需要的余地的波状 / w1 G) J( [8 M9 h* S轫管。 3 ^( s! J1 t6 D& }1 P9 @& ]空膜盒,2 ?4 @! a7 D" u) D 一种具有波状表面的容器。用于量测气压。 j }* o* f% A* d嵌沟缘,( R2 T# f5 @9 w, Q, J 将表面玻璃固定在仪表上的圈状零件。 A) B9 X$ |, A& n 压, , W& _- u$ Y& m; Z' b8 b% U在控制电路的两点之间的电位差。 ; `' @0 @ ~* b: {- l% a机身腹部,; i: d5 {' u$ r& g1 b5 y 机身的最底部,通常水,脏物,和其他外来物集存于此。; g# j1 {, B. P BELLOWS (NO. 1), A corrugated flexible du; E5 p( T" h9 U9 y" |% b3 R- r& J p! m% m3 ~1 d4 w' p' b, |6 s1 M to4 D1 n5 ]. i; u8 Q B- p7 a% [2 J, ^- B3 ^ c: ^4 R& L2 _6 A" e* T B% ?) K9 f' o4 h0 B+ i' {( g8 y9 I g8 _, b6 ~' u; b' s9 \' b7 S& T. q8 p; Z B + S. G7 j1 N5 n$ Dp0 H2 F$ i6 @+ p4 k; F 直角摇臂, 3 t/ W! u: G. ]5 b) y" A& H; z在操纵系统中改变运动方向用的双臂摇臂。) @# ^$ P+ }2 y5 S' L) o+ @1 S 波纹管,6 n) t: b7 e F( @1 v1 }$ l% c/ e5 l7 G( P: I+ N* C/ L3 A/ m) t; F! G. b0 G5 b) x8 g! {4 e* Y0 w$ O1 |" q7 O: x. d英汉对照民用航空词典B OEING4 r \# a' l1 u% _- v9 W) P TECHNICAL DICTIONARY 20 ' U' y: j1 x4 p* \+ gBINARY CODED DECIMAL, A system of coding each( F5 l7 m" } K- @) l digit in a decimal number using the binary equivalent.: ^9 \7 {' A% y" h( J BINARY NUMBER SYSTEM, A number system using. R) a$ v9 ~/ T6 q# v2 r s% |0 w) h, F+ U5 v IT, In the binary number system, the smallest unit of . U8 W/ h- Y5 k: ]; mformation, consisting of a 0 or a 1.2 q& _) Y" N; H1 l& p ITE, SEE - BUILT-IN TEST EQUIPMENT - }9 R+ c6 I/ KLANK DISPLAY, A display that does not have any, m) t0 q/ t2 M+ y dications, normally due to failure.0 X" t+ C# V0 `, M LACK BOX, A container for electronic circuits to record 4 r) V! F9 y4 h( Hight data.2 t& H/ o+ D% P$ K6 P LEED AIR, Air taken from the engine to power various1 _, t( [ q% _& E ircraft accessories.1 j# j8 L& j; X7 E( Z( l' V+ E/ ] A valve in the pneumatic system for air$ k. P- A6 D- _4 G! D supply from the engine or auxiliary power unit to the# @( U0 j0 [' v pneumatic manifold. A valve on the engine for reducing ; B2 `8 t! o5 B2 |* U: Dpressure in the compressor section. 5 f1 Q9 W& Q0 u8 k6 ^进制,, g$ j# z/ B1 {# v R- U5 J: i( t 进制, ) t. z9 a! @3 P- _% F& {一般用0和1)和2为底的数字系统。7 U% c4 [; T, y: D8 o! A) ?2 Z 特(二进位数), ; S& I" b! C8 M2 E+ c二进制中的最小信息单位,包括0或1。 % U- t* e! i k/ [% G内自测系统, 0 O* c" @& o& M1 L+ u见Built-in Test Equipment % Q: c9 B. L( d$ L! l; I/ m/ O$ Otwo symbols (usually denoted 0 and 1) and having 2 a& J7 Z1 P/ c; @3 N I its base. 9 ?1 O2 ]* A0 X2 U- S3 GB' j/ I6 P4 k7 M6 d in* `, z7 Z9 N, l% h$ k B' \ C) u3 h9 D- [" g( ? B1 l5 _* ?; x7 A Y* k* f# ] in0 S( z5 A2 {, G2 i# s+ E8 @ B+ P/ V4 f8 T( J d5 C1 d6 a. d0 q fl % [: B6 P0 g: R7 Y* h/ G+ @- fB - H7 S9 \, _ `, l5 L, p: l# Oa4 }+ t1 q6 U' X. U5 t! ] BLEED VALVE,3 q+ A* ^" { _ 二进制编码的十 ) | L$ Z" R3 c* F一种编码系统。用等效二进制位数编译十进位数的每一 , o5 J% Y, U2 d4 m位。* P9 o/ t: y3 ~/ L( D. _' ^ l& l: h9 J8 ^, ?% e) `# J9 O5 G以两个符号(* k/ M# ~8 H. g8 l3 b, G% r( T. b x+ `- p& v) i.8 ^4 E7 j% X0 G- D7 F' g2 a 白显示, 5 E) |7 y: c) {- L0 ^通常因故障而造成的显示器上没有任何指示。 9 U" O% y* D9 S* D$ v# T匣子, q1 x8 G* L' I. L' H9 Z3 s 装有用于记录飞行数据的电路系统的容器。 , e# |; Y. w) T; A. u气, 4 w8 ]3 ^, x3 q2 B" ^ ~# X取自发动机而用以驱动飞机上之各种附件的空气。 ' X E* b0 y$ q+ }/ Y6 Y, Y3 w气源系统内,使来自发动机或辅助动力装置的空气进人 4 N0 D7 R; a, d" ~; F. P5 P7 h! r# v气源支管的活门。发动机上,用来降低压气机压力的活门。 B/ r) L8 e: u& i. [9 C' e1 p2 a. b7 i8 e) l ^5 x( }7 |1 @& h( ?5 D7 D* L1 r引气活门, # ?5 D* _4 }* [7 W英汉对照民用航空词典B OEING3 _/ `$ D7 ?+ ` TECHNICAL DICTIONARY 21: {* S* K5 R" P! u( c BLOCKER DOOR, A device on the engine for blocking- ~6 m4 z# `4 B- u- A. y the normal airflow during thrust reverser operation. 1 p/ C6 b6 C6 W' z5 P1 S- X; ?LOWER, An electrically operated fan for circulating air.- u3 G' p, f" A( C LOWOUT PANEL, A panel in the structure between9 L* t2 |. `. O o compartments that opens to equalize pressure in R; n& ~" ]0 C L$ x; J e compartments.) ^& p3 \; t3 k9 R, `8 ~ ODY GEAR, The landing gear attached to the+ l5 y7 m/ Y9 A grounding. + H4 A# d) J- f1 C* E( V1 v% b正常的 7 \) V$ W' G. G6 s气流。 ( D- L4 {6 S& D6 X. r8 \鼓风机, % U8 S+ e2 K+ J3 f7 H: o用来使空气循环的电动风扇。# j% V/ a0 d, q! o 压口盖,* w; S& l* R9 P2 U0 \ 两个隔舱之间的口盖,打开后可使两舱压力相等。 + _5 d" L4 B9 \4 k. N身起落架,4 H1 m2 D) [4 G7 U 身构架上的起落架。) L W6 b& o5 v B& d5 @1 d' |; X B. Q- ?7 j1 _/ j0 n tw ; f# N/ m0 I& n2 d4 k( {* x3 Zth ) B9 J0 x. {* t) x* ]. q# X( `B: z! D/ E$ l, R1 ~. M& e5 l; p fuselage structure. k: d% ]1 @4 L& b% f$ r3 z4 q BONDING JUMPER, An electrical connection between 9 A; d# ]" m2 c- b: h3 v3 V( ~a component and airplane structure for electrical' m4 R& L7 }/ K$ N 阻流门,6 |/ g; g1 G, I* i8 s 发动机上的一个装置。在反推工作时用于阻挡 " K' |% ~- U( u) m7 Q; {3 V1 l- A& U4 Z" }) ^, G* {( }: V* o! v9 r 装在机" w' N3 v9 s1 |" | 搭接片, ; l* s6 o3 Y1 G, f, M+ _& o& i连接某个部件与飞机结构以形成接地的电接头。 $ l; q/ U8 c; |0 ?# e2 s英汉对照民用航空词典B OEING0 k# |" @6 C& n0 U, [7 G @2 p TECHNICAL DICTIONARY 22+ N% v7 a: \( Z8 o1 W4 m$ A BOOLEAN ALGEBRA, A mathematical system for 5 u) V" u, v* Z* t5 Gwriting combinations of logical statements., S7 _# v' x4 m. _# [3 B& U BOOST PUMP, An electrically operated fuel pump for; {2 e9 w3 X7 b) O/ t# S fuel supply from the airplane fuel tank to the fuel ' e& w- A0 i. ~) Z* V- h+ Dmanifold.# r7 u3 |3 T' U BORESCOPE, An electro-optical device for looking at 2 V) P( `3 i4 @2 z5 n* N1 Gternal parts of an engine through holes in the engine.- v8 i1 O) y; O orescope ports)# \$ M& m5 T5 G+ i' \2 r OURDON TUBE, A curved flat tube in a pressure gage * b5 \$ p& p9 ~3 Nr moving the pointer when pressure changes inside $ o5 k4 g9 C, m& A/ R& a3 Ion the ability of the brakes to # z4 A0 e" M$ Nbsorb a predetermined amount of energy during a 8 `* E4 {2 a0 [6 S/ J3 Njected takeoff.8 q" X; i2 {) d$ m 用于通过发动机内的孔(孔探口)观察发动机内部件的 8 X, o& j J) r/ [% T$ k光设备。 l; K" K2 i( H7 D [: l7 X 端管, $ S0 }, o6 j1 V2 S$ h" K% v# q2 ~测压计内的弯曲扁管,管内压力的变化时它使指针移 # n* [, o1 G4 u8 a) \0 ^' a* q力。 ) R. R- g9 _/ D( F- I+ l4 z) j! A5 e极限重量, 8 h* j( d) _3 U3 j/ [- d* H! V) ?! y0 s0 H' b 起飞重量。* t! V5 L2 b1 S* f# N1 ? 发动机滑油系统与大气相通的通气口。& d8 M w) [( E* n q4 M( m in % x2 g) [$ n2 i0 p! n) Y$ a(b2 ^+ B) L: @+ `% t( l- t B o* H- n: g$ y$ R! k fo! R* R% I+ s* M" Z# {$ Z! G the tube. 4 r j9 k3 U$ p) P1 d+ nBRACKET, To enclose or surround. 3 x/ V" N* h) \7 B1 F! ABRAKE ENERGY LIMIT WEIGHT, The maximum9 \, o: @; |; r h takeoff weight based : _' ^, W& n' w$ P6 oa . v8 x7 ] y4 z2 m: W5 are 7 m. I6 U& u4 tBREATHER, A vent to ambient of the engine oil system.% X1 W5 J2 m0 g4 w/ c% i( d 布尔代数, , ^" r+ G6 l, |* Q+ A一种用于编写复合逻辑命题的数学系统。/ H& c, b( \" F 增压泵, ; \/ X0 j- s Y# ~5 \) e2 v! R从飞机油箱向总油管提供燃油的电动泵。2 G) o2 j4 I* J- t7 X2 c 孔探仪, 7 k9 |6 g5 N: D8 B9 Y+ B! B) U' `, a8 x: r2 p! O" \' f7 e, {1 Y, e: [ 动,以指示压 ' v8 s6 n: g3 q* b% ]1 B托架,; D" u Y6 r O n+ X" @% g8 H 用于作支撑、装托、或围绕之用。 6 h1 O! X$ `3 {& H h" H4 ?刹车能量 " s1 H# A7 _; g& @; k2 @中断起飞过程中,取决于刹车吸收预定能量之能力的6 G' P% _! ]: b; e% I* w/ @7 }) w/ z通气装置, + i7 c& e( r: p. d$ e英汉对照民用航空词典B OEING & w2 f' ~% v# aTECHNICAL DICTIONARY 23( e- I9 R) E, Y9 Q$ t# V! q BUFFET, Vibration of the wings and airframe resulting : p" n* b/ N H( ?+ E5 Wfrom unsteady airflow over the wing; caused when 9 N& L+ U' F+ i* @7 V/ Q, Zairspeed is too slow, the bank angle is too steep, or # y! z: s- w6 Z5 x& U& ?8 [- V; iirspeed is too fast.9 z/ M* _5 W$ F UILT-IN TEST EQUIPMENT, Equipment installed on " e5 W- W! V( L' Ye airplane and in airplane systems to test the systems! o! @. U* y( F$ r1 w! I ithout external test equipment.) \% d; G% Z+ W UFFET MARGIN, The amount of residual maneuver % T* z- f0 s; dapability present before the onset of buffet. 0 d# }. I# n/ H L& q) ?+ IUG SPEED, A preselecteed speed to be observed6 `# Z$ W+ H, X; U nding sequence.- i' L: X" v: q5 N k 1 N; L8 V `: q% g% i( i2 A7 ?; }ng landing gear operation. 7 f1 y! P/ j# y+ l/ _速度太慢或太快,坡度太大,均会引起抖振。8 L8 J* u: j8 s* M# I 自检设备,8 o( e, J7 o/ j" z; p6 ~- e( l; v 安装在飞机和飞机系统中,在无外接检测设备情况下,6 V8 I1 r0 m% L) Y; Z 用于检测系统的设备。 , {! X% h+ M7 c5 B抖振裕度, 8 b. o. f' n1 B. L/ P b: T飞机在遭遇抖振之前,剩余机动能力的大小。 ' X* c/ o4 w% M6 W2 E9 P% r- \标速度,8 L* h t, z# m$ g6 \& T. A 在某些机动飞行过程中,特别是在进近和着陆时,飞机 7 s6 H% l* x6 n, _" ?+ s& {" C# P$ X预定速度。 + p1 k% O' p6 W. h, Y) m力装置, + \9 L7 a6 b/ W9 ?5 K架工作的一种机械设备(弹簧或减震器)。8 E- v5 W. x5 H) u 流条,8 |* t8 n: m/ ]9 Y2 O0 v& N 在部件或组件之间传输电、数据、或定时的单一电线或: N$ E% k0 |; A" W! k) @( ^- Q a$ z- z: p9 {9 R, ^! v$ B B $ r; J0 _! u7 cth 4 }# ?: o5 m- o+ u" Gw & A" }) |% N" q0 Q3 O+ EB ( R' I4 u$ c; b: K. fc6 @( o" B; D( U6 I# Q B 0 M5 i) K2 N t0 |during certain maneuvers, particularly the approach and # n- m- T4 ~+ [+ Vla 6 ?" h- d2 h9 S \BULKHEAD, A structural partition in the fuselage or 3 {+ H: K1 g" W5 m/ ]wing.5 T p0 L, L) I* l4 p$ @+ w% u3 c$ @8 b BUNGEE, A mechanical device (spring or a shoc / h- E/ i- e0 a( v2 \8 M7 nabsorber) for assisti4 O, B @+ h/ e, p% l BUS, A single wire or group of wires which transfers ! h% \; p2 Z( \( wpower, data, or timing between several units or0 w7 W4 n, r: G f* U/ R* u8 V modules. 4 I+ T; r5 e! a抖振, ! n4 g/ r0 O& R* e8 ~! |) M/ K$ h由于机翼上表面的不稳定气流引起的机翼和机体的振+ l( y& V& B+ U3 f* Y* X7 | 动。飞行( U- {3 G$ W' p, W/ F1 s' q. K8 ?0 T 所应保持的 / M, q* A. N$ S* P1 `) d( J壁板式隔框,, l p- n6 _. K 机身或机翼内一种结构隔板。 - s8 O' Z8 j) H5 S S6 O% ?. ~5 _) H. O3 T用于协助起落 d! E% ]# I* L* ]9 O7 D. R+ T9 M! t: a! h) a8 o% }9 `" q 电线组。+ a- P3 j2 A/ {3 r5 x0 ~ 英汉对照民用航空词典B OEING + N3 \0 f& h/ i) J dTECHNICAL DICTIONARY 24

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BUS DRUM, A mechanical connection with pulleys 2 C; ]1 O" v" I1 \cables in the control system.! m/ p) [3 E! d+ d+ {) m6 o and P5 D- J) r$ C: V* q. B# } l circuits for control and protection of" q! r2 Y" h0 y6 F( K s lectrical alternating current supply to the airplane., R, F6 Z, w Y( E5 u* H" `0 c duct for closing and opening the duct( z9 \/ |/ |5 z0 t, R e assage.+ p& E( y+ J W" u# _/ X UTTOCK LINE, A vertical reference plane along the& G* m# P/ c# i$ h5 e selage for horizontal measurements of the airplane. ( O- n' c+ b$ T. G @: o接。/ b9 s# w8 A* Z 组件,内含控制和保护飞机交流电源的电 9 o8 l$ {- A6 m# d" H/ P4 w0 B5 ?; Z 作动简控制的转动装置。用来关闭和 + L) T0 ~. p+ Z8 b1 Z0 m2 O启管道。7 M- g4 t) T7 j) k/ K 沿机身走向的垂直参考面,用于飞机的水平测量。 : d+ u+ x- s9 \# ^1 HBUS PROTECTION PANEL, A module (black box) ' s& n, w: O( e5 M; ~containing electrica j9 w, l8 X6 _; z4 ] e - q8 W+ Y% _+ GBUTTERFLY VALVE, An actuator-operated, rotating ( X) V9 X8 Z. B1 l) a! n% L b% Hdevice in a : i- ]) i* H1 p1 v5 Tp $ M; ~; g: w; D# n9 J2 ?$ _B0 `6 E) A% E& l( F& Q& a; K fu 8 ^. J6 m: Z: Q$ q0 [# R转动鼓轮, " R# S* D# z. A2 [" Y0 n5 ]在操纵系统中,具有滑轮和钢索的机械式连8 h# M6 m! M- a2 W8 E1 i u1 Y$ } 汇流条防护板,1 z7 l5 S) X) M$ Q5 r2 o+ p 黑匣子式的# Z) [5 h' f7 P) P1 F* J! T) B. L% J; T8 } 蝶形活门,. I. ?, C2 q" I 是一个在管道中由3 s4 ~' A* N L: r6 m' Q @1 y, O' g0 \: f# _% z2 _ 纵剖线, + c9 \% I5 A% `$ z英汉对照民用航空词典B OEING4 k* p; a- O% x6 i6 H TECHNICAL DICTIONARY 25( C3 D$ s1 z2 ~1 }8 g BYPASS VALVE, A valve through which air or fluid will 7 j. s1 S# ~, M$ Yflow if the normal flow path is blocked. , L/ H9 t5 u3 _' B( p7 JBYTE, A group or string of binary digits. A byte is' F2 m; J* s9 f1 S1 c2 r sually eight bits long. ) }$ O# X3 k' V% p& PABIN ALTITUDE, Atmospheric pressure maintained8 X P% p" r- y. V ithin the cabin, indicated in terms of feet above sea 9 g; G m3 B/ c* HALIBRATE, To repair, adjust, fix or correct the) o0 S1 F( O* S' F; e" n easuring capabilities of a measuring device. 3 Y" y7 e) F) BALIBRATED AIRSPEED (CAS), Indicated airspeed1 V5 M3 O& Q0 T$ i" n AS) corrected for position error.: Q* n4 `) Q( F+ w3 f* s! e nical$ P. K8 w w- x+ K4 j omponents. 1 z" f: l% n( X" g& G# D" Z! Z节,5 D( U H7 W% @ 一组或一列二进制数。通常一个字节长8位。 1 \% _5 z: b7 d+ I舱高度, 0 y" K/ G+ L& B1 H座舱内保持的空气压力,以海拔多少英尺表示。 & `! x$ d Z1 s+ x准," W6 K' d/ L! w' W4 L4 l9 e ^ 修理,调整,定位或改正测量装置的测量功能。 . R4 v) l' Y. \; Z* l& h5 l正空速(CAS),# ^( t7 b/ Z, N1 a1 g. E 在修正了位置误差之后的指示空速(IAS)。 4 H. v5 w5 Q7 I( x1 @! g6 f用来移动机件的一种转动装置。 $ _( k! s Y0 _& y4 L" e fu7 T# E/ m( t: [0 `+ N7 l( A6 O C9 b& s, O) `5 `- u3 \ C7 Q# B/ A$ ]- b X* } {; m2 g" ` [ w ( v2 q& e' r/ _level.3 G" t2 z- s, X4 U* x* Q, U C3 L% u' p1 O( O m $ i1 c' K1 O; `6 f# k* _3 @: G3 _C( K# h6 m) M+ t5 _ (I" L" N! Y( f; o CAM, A rotating device for movement of mecha0 ?% D) C2 g0 Q/ \ C# Y: n2 j0 E. j3 [3 Z) v% Y( p" ` 旁通活门 , X. ]: Y4 e1 f气流或液流在正常通道阻塞时所经过的活门。. w3 n! k% I; _& l, w; U X" E: k7 h0 u# ~8 O: G- T X# h8 b3 H( g* N1 i7 D% `6 X: U8 B k, Z, X1 Y0 F, A凸轮,% P. _9 i" s r4 n 英汉对照民用航空词典B3 o) @7 h% `) V7 A CAM-OUT, An autopilot condition in which the actuator0 n: m5 X7 H7 n' I: h- T7 A detent piston is overridden, either manually or by the R/ R4 R J, y8 W, h# Q5 K ther autopilot actuator. }8 h8 ?7 b2 nAP, SEE - CAPTURE+ u* v2 w& |( I/ Y8 [/ H! p APACITANCE, The measurement of electrical energy" |) k; r* p. e$ w3 y3 G1 o tored in a capacitor (condenser). / M" Y6 o" Z \, c# iAPACITOR, An electrical component of two metal" ]3 H; a* X5 S5 B/ w0 O lates separated by a dielectric material, for storing9 f# Z% |4 D( C' _ lectrical energy. ! c6 o+ O9 u/ }# x2 W! N0 Q+ uCAPTURE, An autopilot or flight director function to ' s3 k8 T- l& Q1 uacquire a selected mode. * o# d3 ?2 G! k" BCARD FILE, A container on the airplane for printed / I" {$ i0 ~) m' ]( q& A+ Qcircuit cards. / E1 z7 b1 j9 h6 p/ r一自 6 o1 S; N3 {4 _" a$ @ J6 r+ H6 w- w动驾驶舵机所超控。 5 h' V8 N; }- x+ S2 L截获,% j- _- v3 c9 E: {5 i1 e 见Capture! t- m5 H, s( s, {- O3 \7 N o $ k3 C2 W& N; b5 W; @, p% J' Z+ l/ pC ; i3 E4 m% ^; |& j5 }7 @/ t9 \! B, rC 6 e+ k7 r' B: j( v5 q3 A& Ds6 o) y; S* |- B) p. n6 q C 9 S- n1 T4 V- n6 Q0 Ep1 `+ ~; W2 b( E" Z/ d e . q5 [( y; x w' X凸轮不工作, & y. `, y1 m p* l, f8 N0 m一种自动驾驶状态。此时舵机锁定活塞被人工或另3 R5 l8 }3 y- z2 C9 C! p, o( V! i/ G1 q电容量, 7 S/ W$ N- B8 }) g9 d电容器内所储存的电能的量度。 5 \7 ~, O( V; @9 s容器, 2 e1 d, s/ J5 @: {5 T两片金属中间用绝缘材料隔开的电器。用以储存电能。 5 a5 Y o- n. f* p* [+ a" D截获(CAP), ; {# I' @! g1 A自动驾驶仪或飞行指引仪的获取选定方式的功能。/ y& |3 ~% Y) z! k# o) O2 z 线路板盒,( F0 y8 H9 k4 S' p 飞机上安装印刷线路板的容器。 : Z. _/ D E7 v+ B3 f! Q& S" o9 B' d! XOEING ; K: Y) T% H: j3 vTECHNICAL DICTIONARY 269 B; m# k" }8 M9 y7 o. C 英汉对照民用航空词典B OEING4 \* ^$ `; t3 m! w8 @! n4 c8 ^ TECHNICAL DICTIONARY 27 1 e9 h3 ^6 o8 A9 W4 XCASCADE, Two or more similar circuits or amplifying d G$ n4 K7 A% u& s( Q3 Y* u stages in which the output of one circuit provides the 6 `. k. ~% j; W( aput of the next. # F4 ]$ I: s: W6 H5 U" Q5 YASCADE VANE, A vane for turning the engine airflow# J( g6 Y% G3 u uring operation of thrust reverser.7 B, w0 R: R! Z1 X9 ^; J1 O ASE DRAIN, A drain carrying lubricating and cooling % F% J; t' O8 q0 a/ j; Euid from a hydraulic pump.3 [/ C) d) B* u( m: C) _9 } ATHODE, The element from which the principal , { E1 l7 s/ m& ptream of electrons flows. 5 u: Q0 c! b& ?: N6 _ATHODE RAY TUBE, An evacuated glass tube with a' g' C# x0 o3 D" L1 ] CEILING, The height above the ground or water of the$ p0 T& P9 v; ~3 `2 e base of the lowest layer of cloud below 6000 meters 6 u0 S& i# R5 B7 v(20,000 feet) covering more than half the sky.; R) d* D; O5 I, A+ M 程。该' O4 t- m2 E7 S+ R 程中,一个电路的输出为下一个电路的输人。' d/ {2 v, n8 n' _$ i: y4 @8 K, Q 叶栅叶片, 1 S7 f9 e$ B l; T/ }在反推工作时,使发动机气流向相反方向流动的叶片。 / @3 u3 q3 J4 A/ I$ U* t匣余油管,# Z; [4 s5 R$ T$ y7 m6 i 液压泵多余的润滑液及冷却液的排放口。 7 Z7 R: L3 `& p. _8 O5 w& B极, * T: F8 B3 w# B$ H; C9 N电子流流出的极位。 : O* f6 \/ q& ~7 `8 |极射线管,# d/ I# X$ h" y 有显象屏幕的真空玻璃管。用于显示信息。 ( e3 q& F7 q6 Q云高(云底高), - K: I" w- z W% E* ], R& y: F' w6000米(20,000英尺)以下已覆盖一半以上天空的最 1 g7 F$ b+ g) X! w6 P3 h低云层底距离地面或水面的高度。! j {9 b$ i8 n- p R in8 s4 q: z" ^7 }0 z( b v+ g C ; \8 D. M: |3 L& fd * o4 D7 l1 O/ C" u# ?C 8 h! B9 M$ V& x: v4 E# Wfl + S) T1 Z* q& _4 @* d9 A9 c! VC) m8 B/ ?1 _% n* P3 |: v4 ~) c s$ g* K3 J Y6 r K' z2 y7 H C . n: N& u6 g- z0 @6 dviewing screen, used for displaying information. 2 [% P* n$ Q: m级联, " }& w# Y8 S1 W5 E+ h/ B4 ]) ^- U0 r两个或两个以上的类似电路的逐级连接或放大过 - N* ]: J+ ?# Z. I3 [1 z: J4 k, I0 n2 A5 o I/ `' C' l0 p( U6 N$ E+ h2 r4 b9 `: w) |; n) j$ n1 ]$ `5 d3 ~# @3 Q" \! o 一个具 " k( n! L( Y7 }$ m) |英汉对照民用航空词典B OEING, W. X; e* Z, ^, J' C: j TECHNICAL DICTIONARY 285 H; q% _) Z+ d CELSIUS, A temperature scale in which zero is the 5 {3 z- A8 J& {' y9 i Bfreezing point of water and 100 is the boiling point of0 Z# F* t1 |" p; ?2 W water.# }, G. ~8 S- [# ] CENTER OF GRAVITY, The balance point of an object 1 P. h( ?+ Z; ~) A1 i! Ar rigid structure expressed in terms of percent Mean, @8 |* ?* n8 m erodynamic Chord or in inches from a reference point." B: j; x5 g8 W4 z( f ENTERING CAM, A cam for moving a mechanism to a 8 z. V' w1 G; Feutral position., e& B Z7 T/ l: _) G IGURATION, A configuration of the& S( i! ]* J- e6 ~) { ircraft approved for operation by the local governing ' L+ K" `: c8 S6 Hgency. - o5 v6 X# s. Q0 U3 IENTRAL PROCESSING UNIT, In a computer or 7 r7 p' B0 H' G0 m( t8 qigital circuit, the section containing the arithmetic and f& u$ o* B# q! P, C% E. Xgic,control, and internal memory circuits.# o) j" S# S& V5 K- `$ {" M ENTRIFUGAL FLOW COMPRESSOR, A type of4 _( C1 {: }7 v2 `5 |- k' a% d ompressor in which air is taken into the center of the ( x" W! N8 h6 d; w/ wpeller and is slung outward centrifugally into a diffuser 5 F9 |5 c6 N$ `- ]* Chere it is slowed and pressure is increased. L. y# c6 N* x7 G7 K( C& E# |& D: ZCG, SEE - CENTER OF GRAVITY) e4 e& p8 z1 ]& r+ ` 构的平衡点,以平均气动力弦的百分比或# L' `; c8 l9 B$ f9 X4 C5 b 某一参考点若干英寸来表示。) {: Y9 C [. Q6 R* w 中凸轮, 1 o- P1 ?( x" g9 }+ E$ j; a/ X将机构移向中立位置的凸轮。 + S, N7 A9 H9 n! o2 o q F格的装机状态, " I, v* U1 b. a4 b$ H" C由当地主管单位批准使用的飞机装机状态。 0 j, x1 _( i$ Z* C) {中央处理器,+ X, L X0 N5 Y# B% `8 ] 计算机或数字电路中含有运算,逻辑,控制和内部存 3 P' f# Y. x w4 s% h; P5 O储电路的部分。2 T8 g. x3 Z: V' F- F* e+ q 心式压气机, ; A+ A6 t1 }1 U4 ~压气机的一种。当进气到达叶轮中心时,被叶轮离心抛 3 R% Q- S7 G* A( T3 e p- ?% P) N, X进人扩散器。在扩散器中气体流速减慢,压力增加。 & E( ^% D6 E4 {1 @9 F重心, ( ?" J+ {) F* A ~1 y& F见Center of Gravity$ p' b2 J3 e; @4 m o ( d" o% M/ D0 S4 JA' k) E3 K6 U N8 M f* A; ]% x C 6 q% K0 Y( l& y7 }! O, Kn; L1 C- W7 D9 \ CERTIFIED CONF ; K4 k7 Z9 V( qa ' L/ W* C0 G/ x1 l5 x) \a7 X6 G; k8 G7 h: T1 | C: s% V% Q) y, s) w: l d : i2 \, q5 B7 @5 z( s zlo , s3 k/ \, {) z% W' Q- H' j& |C . X/ I7 v, j% p, v, f3 i8 S, s, Ic5 c5 L/ o. r' d) Z, m; N im6 N# E1 d+ P" v1 S! H; q; B- v w + ~0 [- T/ R% ] e: o( j' \摄氏度(°C), * _1 ]; f; A2 }3 {: Z温度的度量单位。在此单位中,0°C表示水的冰点, % K; O% M. n3 }& @* m100°C表示沸点。 . [- i8 d a. ]. i ]6 u重心% C4 M, `, C9 l0 [- r 物体或刚性结 ) @8 @: n2 J! I* N& F& D$ K& Q- y5 \6 c, }! k1 K! }; H$ I! C2 v8 I- ?, D9 a7 l8 Q7 M; z! l0 B4 S ^% X- P6 }0 a0 w* y& G! Q3 `8 B. V6 G x/ u 英汉对照民用航空词典B OEING # |) h) N) r- j% L. f$ R! QTECHNICAL DICTIONARY 29, S* i) g# l% g CHANGEOVER, Conversion from one mode to another., \2 S, L- Q! q) {( p HARGING VALVE, A valve for supplying air or fluid to8 _' g2 s$ A! J% c4 q9 z HECK VALVE, A valve allowing flow in only one # Y$ I. A3 i; }& b! E/ g4 N% Z, girection. See Non-Return Valve. 8 A5 g8 ^$ s5 w& Q1 S% OHECKSUM, In a computer, a summation of digits or * q) _, }5 J: t6 Q0 s5 ^# dits which are primarily used for error detection. * p5 G/ [* y1 @7 g' H3 O# U2 rHIP DETECTOR, A magnetic plug in sumps of - ~! i1 U, W0 y" d, d6 e+ O& j9 o, obricated components for detection of internal failure of / }' L7 f E$ R2 le component.* X1 n0 d% \4 D6 \ HORD, A structural component of spars or frames. % P! U6 M. [' G1 z9 `添活门,: O+ u y, k0 s/ S8 n5 U B. J+ g1 W 器充气或加液的活门。 2 x0 V; G+ X$ F* B. t% ]单向活门, ! `) p8 ]+ [5 M. S仅容许单向流动的活门。见Non-Return Valve

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发表于 2008-12-24 21:38:05 |只看该作者
C. R9 L0 Y q& K. B: Q( u a reservoir./ G" a$ H+ t8 B& E C $ K, l9 ?+ L9 [" md0 S% |' ^& J. x$ ]! c, L C 1 d. i- A/ ]+ Z8 Y* }b , i3 J( t8 m8 @" I) k7 |- N" eC ) x# Y" d- M" e8 Q& i6 a j l( \+ ?; ulu 3 {7 o, Z7 w8 O* S* T5 v+ ]0 D5 yth; }, s* A2 f0 l C+ v! u7 n L- C 转换,& c, s# w3 ~) e4 u: o6 W( } 由一个方式转换到另一个方式。- [& i, T* a5 l8 ^" `# ~3 @2 b$ _( C: F 用来向储存 4 Z( {& P/ C6 S( h) `3 G, _& t2 _5 R9 s6 x' j9 f- y J总和校验, . i- D; Z" ~6 A8 m5 L/ R计算机中,把那些用来探错误的数宇或位数的总和进 4 n I* F; |& g( D- b+ C$ A& C. A. k求和计算。, n/ I* w" J$ D: E% i' o9 |# B 属碎屑探测器,# \' b/ N1 ?% e& I+ ` 装在被润滑的部件滑油回油管路上的磁性塞子。用来探 8 f, @. q: G( r1 e; @$ b1 K1 P- }1 n部件内部有无损坏。 - u( t! _/ s, C& @) P* @弦,( L8 q/ [3 E6 p, ^ G# }+ v7 X8 j 梁或框架的结构部件。& G6 E# U1 D6 E- m( S. G" X6 {8 S' `# V" [$ f7 V7 B! l) x& W+ ^$ }/ E- ?% R( \3 J" P, ^9 K j" j7 ?( m# x7 y9 w; g1 W( t+ a: q( |4 s% l' \! `英汉对照民用航空词典B OEING2 o: |" O1 s4 { TECHNICAL DICTIONARY 30 ; Q1 z3 e3 m+ |CIRCUIT, A closed path through which current flows % q6 s2 J }, b9 J% X7 W; G0 A5 L7 }ource. # j# W. N$ o6 x8 `, Y& e) @- BIRCUIT BREAKER, A device that automatically' ~4 |% L& U5 Z1 |& w; W/ K' _ eactivate the system. $ y7 ^3 K- h0 s' M* plear of all non-frangible objects which & M$ r6 T i& \" @$ i3 yay be used as takeoff distance available when + H( {3 l/ l5 D. palculating a takeoff weight. ' {. }* C9 Q1 F% Y( s K' hr water under the control of the appropriate& u6 ^8 U! ~3 A% A5 O/ P% i3 a uthority,selected or prepared as a suitable area over, w4 M2 f; s6 M) x a hich an aeroplane may make a portion of its initial5 e2 u! e; t; t/ f" `* { limb to a specified height./ a& q L4 i( _ increasing. 4 a6 E# A& `; vsed ( r) D% y* N3 B9 Y6 E0 n+ dLOCK SIGNAL, A continuous string of pulses used for- b' y4 Q$ W/ c2 o# N 开关,/ m, z& g1 O: E! U$ {& p* e 故障情况下自动中断电流以保护线路不受过电损 9 A+ N+ S4 T4 F6 r体障碍物的区域。在计 7 h4 n8 Q8 X5 K4 u% X+ _! n# A3 p起飞重量时该区域可作为可用起飞距离。 1 N% K6 M7 E0 E2 I% a是在有关当局管辖的地面或水域内一个界限明确的长 3 |' z. ^; W2 I1 @形区域。在这个选定的合适区域内,飞机可完成初始爬' ?- ?" ^& H# ]' N) \7 U 的一部分,上升到一个指定高度。# @& O5 I2 h! }+ x6 w 飞机高度不断增加的飞行阶段。 " @; T7 H- w) x, `/ e+ b$ L% Y钟脉冲, 1 I# ^5 ]1 \" ~* v步的连续脉冲信号串。; d3 U1 i' H5 k from a source, through various components, and back# j$ X6 x$ r( L6 O* G to the s& Z) j, m5 z! j: i$ O3 w3 U- ^ C 1 m! ?. J7 ~. i: C0 ]7 E- ]interrupts the flow of electricity (current) during fault4 z+ h4 q! s7 E5 g condition to protect wiring from excess current. Circuit4 G$ o# \( u, W0 Z3 b breakers are also used as a means to manually+ U* A# U2 B/ c- J1 j- I0 t' t d! a$ p" J9 u0 O; \& `. |" z2 T4 M+ @ CLEARWAY 1, An area beyond the takeoff end of the/ \% `% R( `, V; h; L runway which is c( v0 Y& `; A) n0 [2 W3 a, D m ) q! |- A# F0 qc 9 I8 J: f; r* e, ZCLEARWAY 2, A defined rectangular area on the 5 Q* M6 h. A+ b" W( s1 D& Aground o 3 d2 k. {+ g" x1 W+ D% [a$ D8 @9 ~) _' d' i* `+ Y) ^ w2 T6 R7 u. w* l c ' }0 b* _( J6 ~' cCLIMB, Phase of flight where the altitude is) \4 ?; Y1 D% i CLIMB LIMIT WEIGHT, Maximum takeoff weight ba 1 L2 q" y7 y* U+ ~2 l8 a* kon a minimum climb gradient with one engine; Z9 R5 J/ L. _, Q, Y7 d inoperative.$ O5 P2 p& w/ ]& h C: T' H. w1 l( n I6 ^ synchronization. y( L. v5 x- I7 Z; e, ~ 电路,3 H6 Z8 |2 @! t0 L 一个闭合的回路。电流由源头流出,经过各个元件流回 6 R& G) f U1 y: _源头。4 D6 W# B) |: }# U4 u6 M. }. M. p0 o( U5 [; O3 t: m3 S7 a 能在 & F+ H+ G2 U: z3 [& Z坏的装置。跳开关也可用于人工使系统无效。* R* Y J. L( D1 ]7 @* @ 一号净空道, 8 {2 F/ V1 e. [ a5 }是跑道起飞端以外,不含任何刚. [5 G2 h- N- r8 D& Y. B( |8 J0 {& ^3 _/ V3 i 二号净空道,* C3 j: T0 f \( [& F- a8 {: P( p' {* D. k/ k6 w& c$ H) t9 U V+ M: T爬升, y' `; E1 z$ U( E8 n. F 爬升限重, ! |! R8 {- d: T8 e, P/ {取决于由一台发动机工作时的最低爬升梯度的最大起 ) w7 I/ f8 R Q& l3 |2 y飞重量。 9 \, @3 \9 D# K. r1 W* q I( P. ]) P( K 用于同 ; ^9 [5 J1 O2 ], f+ c英汉对照民用航空词典B OEING$ J2 P# j/ s4 G5 K TECHNICAL DICTIONARY 31 R; p# d! ]0 B; j3 uCOALESCER, A device in the water separator for 5 W2 A9 l1 @5 v- U w1 U) _ollecting moisture from the cold air. . w+ O; F- N. @- Z% xn antenna with a receiver or transmitter.7 q& X( ^/ M& y6 M7 o( p he cable has an inner conductor and an outer 0 Z2 R( Z4 _" A( \7 Erounded shield. 1 \0 L- i) C! ^3 C4 yting one inside the , J* |& W8 G- J7 |# ?( hther for rotating the low and high pressure8 t Z* M' P" X) c9 P1 {6 T ompressors by the low and high pressure engine + t' ?8 L9 a* U/ J+ g$ f+ drbines.7 W5 h! O& m' I) T3 } OMBUSTION CHAMBER, A part of an engine for ) V+ g) ]/ `6 a, vurning fuel in the air supplied by the compressor.8 I& O/ \4 Q9 L2 \: [ K# x' R$ F 置。 2 W5 u# T- e6 E7 {5 L射机的电缆。电缆% @3 j7 K9 n6 H3 n 中心导体和外层的屏蔽所组成。5 D/ v: P; f$ |; { 两个套在一起旋转的轴。用于使发动机低压和高压涡轮 - s0 |3 z) S: V+ K5 o' G! }9 i1 Q别带动低压和高压压气机。 |# J( h9 `& e' f- d& P$ F2 [0 l烧室,2 f* O" l5 w) Y7 O8 n/ C, e 发动机的一部分。用来使燃油和压气机所提供的空气相 8 Q. C9 R4 z& L4 D% R合而燃烧。

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发表于 2008-12-24 21:38:35 |只看该作者
c 3 @3 A4 W7 c1 B6 ~( `COAXIAL CABLE, An electrical cable usually4 i8 T9 q2 }5 E9 K: T connecting a- _4 }8 B _0 t7 A& B1 { T2 ~# F. i1 R5 l g & Q2 q; @5 A4 k3 e" ACOAXIAL SHAFT, Two shafts rota0 v. L* _0 x1 K; b) c" K o + P; ?4 \2 n$ P3 I r9 qc 6 L' c3 l' W m8 x, btu & Q9 Z+ W" H- Y3 ^# yC5 |- h8 c# Q5 T; M R# Q b 7 l; l2 Z3 L1 O$ v2 }凝聚器, / l5 X# P* b+ b0 a Q) J( n" s7 H% ~水分离器内收集冷空气中水份的装# I9 {1 Z! ?- N0 t" [$ B+ V 同轴电缆,4 K- Q3 F4 w4 b, r& s1 c 一种通常用来联接天线与接收机或发 : Y- q% |* V/ s2 W- ]2 g6 ~8 P5 }+ O; P同心轴,1 F8 P1 g8 a$ _5 I7 D+ k2 w* V+ ~! N ?# p. u. i4 r5 p3 V. k# Y- M8 [" A Y) M5 r2 {( I9 P) |7 y英汉对照民用航空词典B OEING 3 o. f7 P* M, ^, lTECHNICAL DICTIONARY 32# d7 m6 c6 n) K1 z COMMAND BAR, A flight director pitch or roll comman2 R, H1 V5 J l" O! {/ w" Z o+ S indication., ?0 J/ U& B/ h& x# [4 q3 E0 E& B d + n ]0 Z; P! L* \5 ^* a3 A; tOMPANY ROUTE, A route flown by the airplane8 l, g; V! p( H* d8 P OMPASS LOCATOR, A low power, low or medium* _- g9 \; Y5 W: s/ ? equency (L/MF) radio beacon usually installed in 9 E# m$ t+ a& s4 Conjunction with the outer or middle marker of an+ K c" {8 O$ P7 t$ j tor (LOM), A compass: [6 `9 i2 `% {$ u4 H0 s2 A4 T locator installed in conjunction with the outer1 W, K3 x+ T& |" K* T1 u. P1 Y ] marker of an instrument landing system. ) V6 F R# I! H [ss 5 f- _4 h5 z! ~1 Ple ; c* }3 g/ g! w9 T0 EOMPENSATION, To offset, balance, or counteract.5 g, \* _7 k$ B) ] w5 C" m. Z8 d5 g OMPENSATOR, A dual capacitor for changing the fuel7 z, T" k! D( x [4 d8 h3 Z aging circuit capacitance due to changes in fuel$ }( ^6 ~0 O- K; F; f: f ensity. ( @/ n4 [7 j v# q4 ?# ~5 h/ f! \OMPOSITE MATERIALS, Non-metallic materials used 3 Q" N" l4 g2 G; B3 Or airplane construction. Fiberglass, Nomex, Kevlar,( T/ I. w; i2 ^& T# f0 E raphite Epoxy are composite materials.& Y) m" S' h; w$ R: Z* |9 b9 Z2 Z k 司航路,+ V) f% a8 c6 M w( m; J5 w) n; v 在飞行管理计算机数据库内由航空公司飞行, h4 I. e3 n) R9 \2 M( x; D 盘定位台, 3 Q* {. |7 B2 m2 j1 u与仪表着陆进近系统的远距或中距指点标配套安装的2 C- q3 N! q0 ~5 E% k4 {: G 功率、低频、或中频无线电信标装置(低功率NDB台)。 1 n- X+ z, `4 l2 z( N7 u6 }3 z程序中用来导航。* \, }$ T3 _8 U# R' u 1.远台,: Y2 o. y) X) E5 R8 M5 o; ] 与仪表着陆进近系统的远指点标配套安装的罗# G, j7 l* S. D 盘信标台(NDB)。 : \" ~" \0 ~. a4 M偿, $ W! U/ `* f" b% i抵消、平衡、或中和。4 \+ ^2 B8 {+ \" n# ~ 偿器,4 l q) r- a6 h# O& j3 ^2 Q 在燃油计量电路中,用来改变电路上的电容,以与燃# ?9 D- W& C5 x% @, ~4 _ 密度改变所引起的电容改变相抗衡的双电容器。 - ~) o) T+ O9 { C! T合材料,5 O, g/ `/ v- n, X$ S 用于飞机制造的非金属材料。如纤维玻璃,Nomex,! A+ V& I/ x( n ?- b" d, J6 `$ A 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, w# _* Q, B- B' g0 }! w2 S operator that is normally stored in the flight7 U" c, A* b. t# X- A0 W management computer's data base.! _% A- a. ^: f' V/ r5 i* \* ? C : G: M2 H5 |/ Z& e% A7 Pfr& f' F0 `; j/ ~/ ^) i$ V) r+ D5 O c + P2 R( o: P) T. S" tinstrument landing system (ILS). It can be used for - u7 P4 \0 y5 r0 V- _navigation as authorized in the approach procedure. . d4 Q! R5 e$ p$ q" K' r1. Outer Compass Loca |& n+ ~. e/ \2. Middle Compass Locator (LMM), A compa5 ~0 L% D& J2 z! A- w) K+ T locator installed in conjunction with the midd + o9 s# x! _6 U0 m, ^marker of an instrument landing system. * b7 `; X3 o4 YC " S% j2 N/ Z0 {8 AC- ]' a" `9 t. E5 @2 F g9 r: A+ L- |; |3 g' Q d- m( V) ~0 E. D3 E/ Z C . W1 R% n8 m7 w7 X, c( B, h: `fo# h2 \' h# F+ I6 i2 C3 q, F& [ g; J: i0 ]6 h! w6 }4 W 指令杆, ; {" ?+ k+ o* j3 I+ T飞行指引仪俯仰或坡度的指令显示。& c0 v6 J; o7 e, i7 |% e5 `. C2 ]) U5 Z& m8 ], m" p通常储存1 E7 p3 ^( t, D5 H! i) C( u 的航路。+ e2 d1 s" y* U4 L" b+ h9 ]! n/ H, e3 Q9 Q8 e. n1 k3 I; S8 c" f' g& i" @/ N$ z& _# s经认可后在进近 " `* w* }, G3 N* W: ~2 \7 W2.中台, # Q) d+ L- L) r. C! ~: N与仪表着陆进近系统的中指点标配套安装的罗; q. z) U/ V3 S7 F! [7 ?: a0 ]. { 盘定位台(NDB)。 & G+ u; ~6 w4 b/ ?8 X1 K- B) B+ @' w+ D# \9 c- P& P$ E0 a- }. g' B( Y- A( c K5 Z- I/ E5 l3 q' @: J3 o- S2 d ] j9 h! {/ `0 q# u# E( M1 T$ {K$ Q. R0 h) \9 j0 i8 w 英汉对照民用航空词典B OEING' R6 I6 ]. u. k! G8 g TECHNICAL DICTIONARY 33 1 {# y/ z0 S+ T2 L+ Y/ p2 ~( J, p5 Nby ; y( W4 p- l1 i! m( f$ dor increasing air 7 k, [. S/ R) v1 t4 rressure and temperature before the air enters the" H2 J$ g, Z0 k* A% N0 ^) r ombustion chamber, Low pressure compressor - front& ?) Z& s, t8 d+ H' b( r8 _$ u/ e6 E6 @ ection of compressor, High pressure compressor- rear 6 Q' D: e& x7 }- |OMPRESSOR STALL, An event that occurs when ) `* E" }" p) ~! c: y9 w# s2 Iere is a complete stoppage of air or reversal of air flow7 x# s" l/ j- x COMPRESSOR SURGE, SEE - COMPRESSOR / }) K4 m; P8 |; w+ V& i L5 FSTALL COMPUTED AIRSPEED, Indicated airspeed ; o8 A/ V& o: f: P! B) y" Dcorrected for the static source error.5 v$ |( d; Q' Q$ X6 d 的机械轴来驱 1 e! o5 I6 u7 Q6 d. G; R,用来增加吸进空气之压力和温度,以供燃烧室使用。3 {' }8 B) ^3 _: ~' e 压压气机—压气机的前段,高压压气机—压气机的后' R' _% l; [1 F8 P0 k; n8 I2 {5 H( X9 Y气机失速, 2 C" p3 L( E- o当气流完全停止或通过压气机时气流方向逆反的一种 & t, n- C, w5 o压气机喘振, 5 I( p" f5 _. M见Compressor Stall 1 G6 g2 f, \0 \# E0 Y0 E( \2 GCOMPRESSOR, A rotating part of an engine driven$ e- _, A5 B) a0 w a mechanical shaft from the turbines f$ F0 r0 t3 S: m" l3 m( r4 ~ p$ |% M" S! ^) v7 ] c" C* x" L% w0 U0 \ s ! n- R* y: A+ ]" Esection of compressor. : v; v1 ^! U7 r6 E# |! ^$ o s9 B2 q2 GC 2 [ f( B: J: z7 G" a8 F% z9 vth+ C8 Z- l2 J) d j: e through the compressor./ k0 N$ S6 P: {0 b+ z! C+ W' u; P 压气机, ) r+ {9 S, R5 B& [* B" b" {发动机内的一个旋转部件。由与涡轮相连9 r ?) L% C% Z/ g' T( e+ A1 O' i1 k9 w" ~0 x8 k N( }) ~: {/ R. `* v/ v3 a: i8 T2 @% g; k3 T4 U U, V+ k9 i* s4 ` 现象。) B% W2 O- P$ P) D; M1 z+ D2 _7 r( r5 m9 }计算空速, ! ^9 B, [3 S$ H7 U. \. v. p5 G修正了静态源误差后的指示空速。 0 a a& B6 s% o( N% Z# k5 C8 i英汉对照民用航空词典B OEING 0 r7 x# O; I( D* K1 S) r- qTECHNICAL DICTIONARY 34

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发表于 2008-12-24 21:39:27 |只看该作者
COMPUTER, A device that performs arithmetic$ G. v5 W8 f ?1 I# r/ @ operations, manipulates data, and makes decisions." g3 O3 j) p" l w2 g( s" N ditioning - V' v3 o0 f" w" l% X5 D1 wthe air and the% ?, L I! \) c# w9 V frigerant or moisture vapor is changed into a liquid. 4 t0 ^9 q* ]' O' a; y& uine3 a+ b( L* L* C ONFIGURATION, The position of flight controls,' p; C p+ E ~6 u( j( ~( o4 K missing which - x4 e! X' F: C& c3 X: \7 S! omay affect the aerodynamic performance of the: z& a% C+ Z- [4 O airplane. * v N( x7 y4 |7 ^$ i6 S置。! R- X: |- f5 Q 中能使热能散发到空气中,以及使冷冻剂或湿 . E( B% `, `4 w% ~4 m转变为液体的部件。% ]; y) l# `5 e 连接到飞机结构上。! h5 [4 c/ n) M3 T$ t 态, 8 T. ]& L! f. B; j定飞行阶段中,飞行操纵面,起落架等的位置。/ B9 Q* t9 H" j) p" T/ x9 T- H, D ), . g( D4 o) k2 `: V7 Z受到影响。 4 O0 g8 o- v/ TCONDENSER, The component in an air con 8 o# y% s) T& P/ L. c0 }system where heat energy is given to & {( F9 O: a, Ere * E; R9 ^/ }* I7 WCONE BOLT, A bolt in the shape of a cone for eng. W/ ]! m; m! v8 l" |+ [ attachment to the airplane structure.: m% ]& T! V, V' y/ u C - h v/ |; C) \; G! z, ilanding gear, etc., for a particular phase of flight, e.g., ) I4 v/ s; g9 A7 w' ~, |7 Y9 XTakeoff Configuration, Landing Configuration, etc. 6 [( v$ ?3 S; C. C; N' u) u+ aCONFIGURATION DEVIATION LIST (CDL), Appendix 0 L& K& G6 c2 A: ~; `8 g) bin the Airplane Flight Manual (AFM) allowing operation; b! x2 X5 }4 w1 y of the airplane with certain airframe parts # u% f$ h, R6 U* p* N+ O. }8 O+ l计算机, , v0 H4 @! C, Q6 F) Z) G! K; A4 Z能作算数运算,数据操纵,和决策的装 9 B% k3 ]7 G( }0 {- m5 z冷凝器,# E; o+ O( y$ p3 t1 Z4 H* J! z! F 空调系统- q& O+ w$ i, y8 w) s* W! ]% D. j, B# i9 G. P锥形螺栓,5 k8 j L: j5 ?" {- x2 X/ j 外形是锥形的螺栓,用以将发动机 $ C) C0 _7 b/ [3 |; U. g( t) s. D* v. K! v B* J在某一特 . {* |7 W# }$ ~3 }- p' G" G# H, K如起飞形态,着陆形态等。 + x4 r0 i- U! B% Z' {2 O7 Z缺件单(CDL 4 G! `0 T2 G7 ^' o飞机飞行手册的附录所开列的飞机上某些零件的清单。7 Q" ` O8 Q8 }6 K 在缺少这类零件时,可以飞行但气动性能可能 7 F6 c, Q( G% [. j2 l英汉对照民用航空词典B OEING( S6 P& u2 i' s" Y TECHNICAL DICTIONARY 35

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发表于 2008-12-24 21:39:49 |只看该作者
CONSTANT SPEED DRIVE, A hydro-mechanical * q8 x- f9 N8 n4 Ocomponent for changing variable engine gearbox speed : G) G4 f+ i; YONTROL AXES, The three axes of the airplane which 9 D0 `5 Z. L+ x$ `% f- R5 sre perpendicular to each other and pass through the 1 G" G- a) f v3 renter of gravity of the airplane. ^: w% p/ r4 n Pitch axis - Horizontal or lateral axis, passes through . Q! I: j: S& r1 s, tthe airplane from one side to the other - 2 l# D. W/ {# o0 ~nose up and nose down control is by4 J' D9 G: h k, @7 k& n elevators (and stabilizer for trim)." y3 m0 _9 A. y# ]5 H/ t" {$ H Roll axis - Longitudinal axis, passes through the8 s w9 M( Z% g8 c- I5 q( Z* F airplane from front to rear - wing up and2 f$ r+ H+ m& X! {3 w- A wing down control is by ailerons and2 e. g6 w& D6 H# W flight spoilers. 1 c5 ]% p' t$ g S8 `; PYaw axis - Vertical axis, passes through the ) t6 _) A* S9 hairplane from top to bottom - left and# u0 D: k# S% _8 s) p, T0 ?/ n0 A) \ right control is by rudder.1 B/ j5 e, S5 \* Y9 o! p 置, - F& U* F/ o; G- N; x4 A制轴, u# @& R8 k- S, g* u通过飞机重心互相垂直的三个轴。 T! \0 L& M7 d2 J5 F/ d 俯仰轴—又称水平轴或横轴。由飞机的一侧通向另: q$ u6 \; e( t" e2 S6 u5 q 侧。飞机绕此轴转动即造成机首的俯与仰4 i& B. Q, e/ A0 |/ l* M0 g6 L! I 俯仰控制是由升降舵来达成的,水平安定 7 p2 P' K- B1 }/ Y则为配平之用。, F0 M1 s6 d/ S# W7 E 横滚轴—又称纵轴。由飞机的前部通向后部。机翼 * g, Y$ Z$ ?" s( T下运动由副翼和飞行扰流板控制。; A2 N. T; w$ u1 m 偏航轴—又称垂直轴。由机身上方通向下方。飞机$ i2 V, s/ ?' b; u' E/ u8 a3 l 此轴转动即造成机首之左右运动,此一运 9 L1 a X( \9 r( x9 }6 M3 \由方向舵控制。; e& u5 a6 t- K8 F to constant speed to drive the electrical power.! i+ w( @. g* a2 U; o) F C $ |7 L" ?+ B; b" S" }a , Q+ v1 L N8 K. Q! ^9 @9 }) N7 ac , ]1 z$ \' ^) E9 K. m恒速驱动装 f9 r0 a, \0 D- Q 将发动机齿轮箱的可变转速转变为恒速以驱动电源的 % c" t. o, F' X( [7 r液压机械式部件。0 J5 ~) q: p; q$ S7 Y( \" J2 u% `9 M$ ~( E9 Y# J3 @- R+ a: Q7 E p" u7 j; V$ f- g* t% Z$ S0 f S3 x5 \2 G+ A& @' `( |3 X: U7 d% z: g9 s0 S1 K0 X" R8 k( Z0 P; E% s* j9 F# Z& B. P! s7 ?( V英汉对照民用航空词典B OEING4 |' e: O9 s7 \! F TECHNICAL DICTIONARY 36& X3 p1 l/ Z, b5 ~. X; V, M6 S CONTROL COLUMN, A mechanical component used/ H! S" ^: O- Y* C8 c0 j rs$ K) k% S( g% L' ~ nd elevators.) Q" m/ b8 ^8 Y* l ONTROL SURFACE, Moveable panels on wings and & V& {, Q2 j! Q2 {1 a' F! Qil for movement of airplane on pitch, roll and yaw axes. % g( ?/ q$ l0 TONTROL TAB, SEE - BALANCE TAB4 z) E' b- y2 ]1 E: S5 x# E& j ONTROL AREA, A controlled airspace extending' S6 v6 z. Y7 i8 N/ F) _. @ pwards from a specified limit above the earth. ; M1 v; `5 E0 Q9 l3 jONTROL ZONE, A controlled airspace extending ! r; d" }5 V, Lpwards from the surface of the earth to a specified' k5 U+ \ o/ C. K5 D I pper limit. 7 A1 v9 K6 \/ i l, [8 q1 O8 J5 Gis 3 r7 f* P1 D: w) io IFR flights and to VFR flights in accordance & a% T( `6 }2 pwith the airspace classification. 3 H& ?* t' j; B; l y机械部0 I! H4 x0 _8 M+ E9 @0 K( K1 r" R4 A |7 q操纵面,/ s# e7 {/ j% c6 z3 X0 Z, H; p9 Q" n, p 机翼和机尾上的可动面板,用以操纵飞机俯仰,坡度, ' \5 I$ `0 Y5 p) v+ a和偏航运动。 / E9 r/ C; J' M操纵片,/ m; G$ j( s( i, j. f2 R* { 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. l- `/ }% L* D2 l. W5 e6 i- N' \5 t a 6 b2 C; g6 w, o# I* V* |C 9 G. L. r& ~% Qta2 G( {! v0 h3 |# o4 N C 2 {) l# {4 W# G, ?# `( [C 2 n& Q0 p+ e- T' K$ W; d/ ?u: @4 O& @6 a, ~; \" x. Z' L$ ] C & H6 w _& Z7 M$ ] Mu ) R0 h7 @* X! Uu , o6 P; J- i9 L' RCONTROLLED AIRSPACE, An airspace of defined, c4 r( N' }7 M9 ` dimensions within which air traffic control service # b, \. [9 Z X: R: B. tprovided t& @9 x, L6 I% \3 e 驾驶杆,6 F( b" Y7 h* t& \2 Z0 z( ^ 飞行员用来操纵副翼、飞行扰流板和升降舵的 ) b/ ^" I$ v& B3 t: }4 d+ K6 P' |5 V8 y; e$ `2 ~6 H; E$ {! S% |: c 管制区域,- ^- r6 h3 f9 U7 t 高于地面的指定极限以上的受管制的空域。4 h6 U4 ?- Q$ {; V* m 制范围, 8 |0 X5 \) F( \; p1 c! C由地面到指定的高度以内的受管制的空域。 # E8 N$ U9 d6 @6 Z. q' h一个范围明确的空域。在该空域内,仪表飞行规则飞行: m) W9 c9 k4 T( |& r: l8 d6 J 和目视飞行规则飞行有空中交通管制服务。 " C3 `* B/ m# b& J% }( f# p$ v- Z+ S4 x, M0 ^. S- S受管制空域,! Z% ]9 ^6 S- X1 z 英汉对照民用航空词典B OEING ! K/ V: K4 ~# Z, {- X/ JTECHNICAL DICTIONARY 375 H! M" i- H5 z2 m CONVERSION, To change into another form.$ i$ K1 C/ J5 p4 J+ N COORDINATES, The intersection of lines of reference, + g+ j! O! o5 q) rsually expressed in degrees/minutes/tenths of minutes5 M. |3 x: }6 I2 l" Y f latitude and longitude, used to determine position or. V% _% U+ a- Z4 q* P" \ CO) ^ q: L6 p5 W destruction of th " J1 a* W" L7 s3 r2 G$ m$ P8 X6 h* Bchemical conta& U7 D# I5 w) {% q, Z3 S: s COWL, A remo 0 `+ {. I9 k+ B6 h- Hfor access to th * R; q+ c |0 l* CFa5 Q7 @1 m$ S# d, W Nose Cowl - Front section of the nacelle for air inlet ! e. j$ _4 \0 V: A. {; s7 dto the engine.- Y+ G& a( c7 _/ E) g) U; b Side Cowl - Cover around the sides of the engine. N( }* `( o6 C9 z+ B/ b6 ^Thrust Reverser Cowl - Cover around the core 1 B& `2 G8 v2 r- a8 p6 Q" Asection. : S6 ]* F3 E, v8 P) `) N( k0 }Translating Cowl -The moveable outer portion of the# ^& z& S, J( O6 U0 X" h thrust reverser cowl which is " Y3 w7 i/ h) c0 i3 coperated during reverse thrust. , J* ~& V/ W/ V5 n; }5 C( v标, 5 j/ c3 R9 ^* a- v5 d' Z/ P基准线的相交点。一般以经纬度的度/分/十分之一分 7 V# Q+ B1 Y; D3 _读数来确定位置和方位。 ' |' z! ^7 N9 M, v( }: i: i, j腐蚀 6 B8 u, f; Z2 Q1 _% f动机外部可拆除的罩子。发动机上的构件必须要取下 4 O" Q A3 k! g# s: n9 E8 ]流罩后,才能够到。" [+ L8 q8 s* y* W" R; v) A7 P2 m6 v. C1 X机的短舱的前段。 . e1 Z$ @( t# D1 P; K; _侧整流罩一发动机两侧的罩子。 ' \. }+ d5 Z D4 w# h: \反推整流罩一发动机主体外的罩子。 0 p+ V/ z# d6 l ~移动整流罩一反推整流罩外可移动的部份,在反推工& \% L+ `# w. E _2 y 作时使用。. `, ?" R; Z/ m% P# D u " ?4 [$ P5 g( g6 P0 x- X' Zo4 O8 G, ~+ ?# D5 N4 U" i; T location. ( l3 J- e, O. h" rRROSION, A chemical action which causes gradual % U! d) @9 I8 M. D6 R5 d% ne surface of a metal by oxidation or- n$ M, H$ D0 {( @; ?- A mination.- r; T/ ]3 F& K$ L4 P vable cover around the engine sections * |5 q+ Q9 C7 y! Ke components on the engine.. f3 i! \0 j# K4 H1 [+ ] n Cowl - Cover around the fan section. . x( ~9 ?& a/ J# _- e转换,! S+ x& H# m" K/ T/ c 改换到另一个方式。8 C& y5 i: P) g$ L3 R6 ]; Q: @- [% _$ h/ d4 ]* i5 b! d( a/ @' ^2 B9 h* e1 S- B v* Q5 } 氧化或化学污染造成金属表面逐渐破坏的化学反应。 i+ u0 C/ |7 l2 r% @: Y3 ^. Q( P5 }发动机整流罩, . ?! Q+ e9 ^" v1 V2 O0 ?3 `3 q4 k: W3 c1 V& B% \+ F. b9 q4 ? r4 u, Q" h- v" w8 _6 z {, b' r 扇整流罩一风扇外围的罩子。 ' h Z# W+ v. t0 R前整流罩一引导空气进人发动 ; V# s7 ?* s6 }8 z: `, ]; [( X英汉对照民用航空词典B OEING ' o& |1 g: a* s) C9 V# J4 nTECHNICAL DICTIONARY 38- ^- z) z& y% w; |4 z8 Y CPU, SEE - CENTRAL PROCESSING UNIT8 j, P) z/ E7 B1 I& F& \! C9 I CROSS TRACK, At 90 degrees from the desired track7 p9 R* i7 m8 P f the airplane. For example, cross track distance is the 3 D2 y$ W% G' s& ^7 Q* a3 Fistance from the desired track measured 90 degrees/ t& [7 S& J) C! U: D om the desired track.6 v, }; J0 f' F) y7 S ROSS-CHANNEL, Electrical wire(s) connected from 7 z G L' g2 a A6 h0 H8 ene system to another like system, for example, FCC+ B( D4 d' q# H4 b' u8 g& Q " to FCC "B". # G+ v8 y& J3 Q: p, u On adjacent engine or one on the other side.. x. E0 d4 h% W+ z6 Y: e3 k6 d2 O l crossfeed" m+ s _# @+ b5 D+ W6 j) h$ G anifold for fuel flow from one side of the airplane to the 1 W7 Y7 `/ D) ?" e. V9 W- z5 Y0 bther side. ! ?0 j8 E( p: h% s. m5 fre 1 Q+ [* U5 l5 CRUISE ALTITUDE, An altitude or flight level , p$ B7 v. P s3 C- Z( H3 j. q6 j+ c. n0 S- M+ X6 o o & v9 m( J( P4 T o- ]+ L. ^0 Q0 Hd! V0 @" q1 d. ?: `1 t fr" i$ O6 D( x; P3 {( F/ C( W0 ?) Z C 5 }) t. L- n; Q1 Z. I* z# y& vo 2 e) N& r, P. |/ R1 G( ^6 O# `2 m"A 4 o: d8 F# v& w1 K) _- y) b) P7 xCROSSFEED, An interconnection between fuel 4 U7 _) p( E. X# r; K: O4 u+ rmanifolds for fuel flow from one side of the airplane to 5 M6 I/ \ A* f& o1 R: P/ }2 Ua+ G" M4 P3 I5 J: ^" K5 ]* a1 a CROSSFEED VALVE, A valve in the fue7 I/ y7 C; Y3 X% y0 |. D0 j m / t G( j% n1 ?. ]) xo & Z$ b; v0 T, J( W: S& E3 RCRT, SEE - CATHODE RAY TUBE : n1 ?! x/ Z0 e5 @& ~ Y# TCRUISE, Phase of flight where altitude and speed a5 N; K- d" d5 Z5 M6 j: ] basically constant.2 t! Z+ C7 V( a4 z( H9 a C0 Q, n* ?% ^, c3 L3 M9 W' t maintained during enroute level flight./ ?7 R. n% b& h& k. s 中央处理器 " u) W- Y& F4 v6 g9 H$ ?: y见Central Processing Unit.2 `- Q# i! @' W% [ 交叉航迹(XTK),9 ~- i% q4 L; ~4 n% K; N3 W$ q5 z& A4 x 与飞机预计航迹成90°角的航迹。例如,交叉航迹距离! c3 \' V. y% V 是用与预计航迹成90°角量取的到预计航迹的距离。 ( z1 I1 _7 `" l5 D) h. p2 ?2 x通道跨接, 4 O" @/ T1 Y, R9 `; n6 Q* I, {电线由一个系统接到另一个类似系统。例如:由FCC + i' S0 V! n" X* S* t“A”1 f4 n5 N5 d2 |( H9 ] 接到FCC“B”. 2 I$ w6 x/ j( l+ q* @: l机身另一侧的发动机。 ( t: K& _/ K, N于使燃油从飞机的一侧 ( {9 M. x; W% S( m# p F向另一侧。 ! |; K' N; G. P/ E3 p* x; T; ~见Cathode Ray Tube 0 }9 a- E% ?3 f% O8 k2 y交输, R8 H8 t. @: c' h, I 燃油支管之间的交连设备。可使燃油从飞机一侧流向邻: W, x- G6 N% i8 v- u+ O$ K/ } 近的发动机或在1 r/ `9 N" m; ~8 ` 交输活门,# }! h) I0 k2 x 燃油交输支管内的一个活门。用3 t# Y9 P* y8 ?* Y r- r* h( _, w* D; B& Q! [阴极射线管,$ N% B- c" g/ E" H6 _! ~$ v$ P .1 C9 H3 b+ A! b4 `2 h. B6 w) Y; R 阶段。 3 T) P: q, n% r9 Q D航高度, ' T, F% ]2 {. E3 A+ t6 d# N飞行期间,飞机所保持的高度或飞行高2 t5 M) d9 V" x* X9 k9 k0 ~ 巡航, * k y5 v3 s' r+ H9 t1 x飞机的高度和速度基本上没有什么变化的飞行 & M" ]- ^1 O% ^5 R. {; h# l# E7 e; H0 R在航线上水平 / B5 ~2 P5 d# s% B; b( v8 Q4 I4 Z度层。) U% z% v- {+ y1 i9 ] 英汉对照民用航空词典B OEING$ \0 V# B6 j0 \5 c7 u TECHNICAL DICTIONARY 397 I$ ?/ I4 b Y7 }/ a* o CSD, SEE - CONSTANT SPEED DRIVE 2 i9 |' l! d6 F" y% \0 m! y1 O! sCURE, A chemical change which takes place in a resin - z1 D; X9 T, n$ kand fiber based component causing it to solidify. 1 n3 ?" I( ~6 F: }/ O: y- uCYCLE, A complete series of events that take place {) M" H2 Q. k% V% y' I5 k gularly normally in a continual sequence.' k. h( p4 T; M! I) Y AMPER, A device for slowing down or limiting1 ]. D @- x0 Q. ?+ |! }/ D) [ DASHPOT A mechanical damper for slowing down $ s; E( o/ A3 F7 _ovement by restricting fluid flow. ' u1 T; M0 l# z7 s8 p5 o! `/ JD " {2 b8 `% g1 _' q: ~9 @2 KATA BASE, Stored information which is used as the 2 D/ V+ v6 J2 R( cba * Z5 n/ L5 \& s3 X6 bDATA BUS, A conductor over which digital data is . ! A% Z4 ^4 v" {transmitted.1 M& w% W& w# i# k9 N# ? DECELERATION, To decrease in velocity. z( }3 I4 K! {9 N 装置, 7 ]$ |% b% a6 I+ o) Jrive$ w2 }6 W' g/ f4 Q re 5 f" F3 k7 F/ qD% m3 K) o( K) W' [7 A D* M. P0 z+ ]( W ~1 ^ movement.* { l; e( J& e# d, i* K& K m3 Z. H: m6 S- a3 J6 ^; l ATA, Another name for information.( h! M# _8 Z8 ] D ' c0 w9 e0 k1 d1 t9 E/ ]# H: psis for computation. 3 `! u8 b/ ^/ Z3 y* F- ^% V8 @9 \恒速驱动 - c1 j7 O6 Z$ z N" [ j1 t" `( T见Constant Speed D . 2 e+ D! Y$ @3 e* ] [. |期,6 Y( y2 |, b9 |2 M2 A! B V 不断重复发生的事件的一个完整系列。 N7 P0 G4 A1 L: {9 f4 r尼器,1 h# U4 K6 b% j; W 慢的一种机构。& \% z5 C8 b4 W* @+ u Z5 J9 v% c/ X' j$ f, B. S 用限制液体流动的方法以减慢物体运动的机械式阻+ ^: v6 B6 H, |1 B* k. D/ c. r) y8 p! }0 W3 R( I: T' ?% t% @' B料的另一名称。) V; P2 D$ S& o& x0 O 据库,# W4 y) U4 ?9 f$ i& t8 G& H3 @9 O 数据总线, ! N+ ?8 q0 @2 J) V! ^8 l, W一条或一对导线,用来传输数字信息的通道。 # ]5 E1 T0 m( V3 N7 g减速, 5 j7 Z( Y4 Q( u. k1 k4 [. L/ `速度随时间的递减量。 4 \9 n m* @$ F, Z' {8 g6 e固化, 9 {3 y0 V* r+ ~! D4 H4 P0 K树脂和纤维部件内化学反应使之成为固体的变化过程。 / F: X( `1 P' g% ~: {( S0 v* Y1 Z& m" Y8 y. a# [9 G8 b2 y+ h: g8 [! C用来使运动减* n" h6 z4 K0 `4 W 冲器, 0 A+ I! ^. h" r/ y& F: Z% H器。 5 u3 H9 @3 M0 T* k# S, k- d2 P据,% x; V4 N0 k4 F7 `; V3 E$ O5 v! l* L4 y0 _- _$ Q% b4 }8 K 储存起来以便在计算时使用的资料。 1 g6 I$ ~& p1 M$ }6 r( F% d; Y英汉对照民用航空词典B OEING . z) s. f, N, t4 G7 F: ^TECHNICAL DICTIONARY 403 M/ j4 h: j' a# a DECIBEL (db), A unit of gain derived by computing the " R6 [+ [- U. x( Rtio of input power to output power. 6 c) T g; m9 `2 R6 BECISION ALTITUDE/HEIGHT (DA/H), A specified ( g8 C2 c3 K/ ?* H' fltitude or height (A/H) in the precision approach at& s K2 `$ z+ N9 O hich a missed approach must be initiated if the2 ?8 B( v2 u9 b$ R4 [ ECISION HEIGHT (DH) 1, With respect to the+ i& d v Q. g' l proach or . A- W* f- F" N& G/ gexecute a missed approach. 5 S& S8 W4 B% M6 nproach to trigger the decision of either $ ^5 y1 T8 g% Z" E7 e2 bnding or go-around. ' j% d, D7 m3 ?, |+ iECOMPRESSION, The loss of internal aircraft air* j6 P& t4 u! g5 l$ d, e ressure. 5 u6 I/ t5 n" |: K* \# DE-ENERGIZE, To turn off or cause to not operate." Q; g4 K9 I3 Z+ P8 C, d$ V3 A rom the tanks* n" _; b6 a& B! m3 d, M using airplane fuel pumps or external suction.$ f2 B Z. `' \5 {1 ? 算的一个增量单位。分贝 ! \3 B& h, N( v5 e' l常表示两个声音信号或电力信号在功率或强度方面的) _( g Y1 H3 M x9 M8 A 对差别的单位,相当于两个水平的比率的常用对数的十 5 S/ ]- X- c& {. g5 _6 _断高度/高(DA/H), 4 b( _8 H2 w0 B- R0 I- d L( D在继续进近必需的目视参考没有建立的情况下开始复9 ]6 M; @. j6 R S$ D 的精密进近中的一个指定高度或高(A/H)。 9 @' S! u. G0 Y( T断高(DH)1, ) F5 R9 N$ ~* k& L操纵而论,指在使用仪表着陆系统或精密着陆雷: g& n p4 x. I% u8 b, H5 l 生继续着陆还是复飞决定的高。. R& m8 h. u4 O1 J& |$ ~/ g 飞机失去内部空气压力。 ' M6 p# H$ k1 U开," k) n7 I8 n# d 关断或使不工作。 0 u! g7 Q9 C, I* f机的油泵或外部的吸油装置将燃油从燃油箱排 7 G F/ z5 |5 t出的方法。 ) q1 ?/ J& x L0 B( C2 p5 zra. M3 [' J6 q/ J) T; K+ c2 n! `' A( e- P D 2 L' Q9 }; s; h1 T) p* v. u5 fa, ]# M5 I8 v8 V9 `3 Y6 X w7 q3 a/ m2 @* y: R' ?$ z required visual reference to continue the approach has7 ^3 v$ `/ o; l$ u( g3 [: N not been established.! `" O* L p% f6 o) S D & q$ Q9 {+ w* e: R b% ooperation of aircraft, means the height at which a5 v% p- u, R s; ]# l decision must be made, during an ILS or PAR. m. e2 ~) z6 L+ i+ { instrument approach, to either continue the ap ; a9 V' S3 e" [5 S M: pto5 _& C5 x! s) w) k3 _8 g# Q DECISION HEIGHT (DH) 2, An altitude used during a - Y9 N. A i/ n/ w6 J) ^/ gprecision ap! T& ~3 j+ o S/ V3 t/ e+ b la) ^" {9 j* m% Z D, j, c" b. V3 ]: ~' W; _ p $ e4 R$ i9 W5 P. V: BD B5 m" i, P O: q2 nDEFUEL, A method for removing fuel f 0 @0 z) C6 X. t+ h) K- L3 f7 Z' }分贝, 5 B. u% \. C& S- a8 }以输人与输出功率的比率来推1 B! E T6 [4 E/ j1 `, a3 y% x9 z- y& ~$ q3 @. ?: {" L$ |5 D b% L) L8 u; a$ C. L; ^6 b- g) m3 ]9 H' I% F; X7 a) {* M% b/ F3 _* f- N* N( I. Q" A4 x r. \! Z; Y( | 就飞机( F% s3 X8 q+ x 达引导进近时,必须要作出的是继续进近,还是中断进场 - q7 \2 d( _2 m; M7 _复飞决定时的高。6 h5 \ @& t# e$ B0 }, o 决断高(DH)2,$ h; q6 [! ]2 k% n, U 精密进近时产 + m+ Q& r. x6 J9 `" Y$ P失压, ! E) Z' }8 h2 c3 ]3 h$ ]% u- J+ _( z1 L* l5 H# P/ G4 g; r# v排油, 5 F b% j* S' j* @0 e* s5 K用飞# l. m5 F0 c" z& \/ o+ f# n* Q 英汉对照民用航空词典B OEING + D) L" L, I- d" x" ETECHNICAL DICTIONARY 41. D( s2 g+ Q% U- f# {# e% |* `9 `5 S DEFUELING VALVE, A valve in the fuel system for ) |$ X3 @3 ^% F4 ^( l' j: x* e: Defueling the tanks and for transferring fuel between the* }+ r8 i9 w0 g/ I9 E' R1 [ E-ICING, Removing ice after it has formed on aircraft. & f$ X( w {' bChange or difference. , k: u8 y3 @7 i; \6 xEPARTURE CONTROL, A function of an approach & ^. Q4 B$ q3 W0 {ontrol facility providing air traffic control service for' ]8 T7 [7 P" f# a5 }# ]) L eparting IFR and, under certain conditions, VFR 4 L6 W" a7 K8 k0 n2 ]EMODULATION, The process of retrieving information) }0 t: u8 \3 r7 e2 { a carrier voltage.6 y: Y9 j- s; }# I ation.) Q4 T! G& C& g) X lic3 i% J/ k& F" H: k. K# p0 @( k creasing hydraulic reservoir air pressure to : W' c& u4 d0 n' w- e+ Z$ u/ @$ Qmbient pressure. u6 d3 d- d% P+ B6 E2 t 箱排油和在燃油箱之间) Q9 f: s/ Y+ J% S 送燃油。/ w; O6 i m' J$ M5 y5 T- V$ f4 ~1 B 冰,2 Q! z1 c; k; t# Z/ [" T+ ? 除去已凝结在飞机上的冰。8 h, O: b7 L9 ?8 b& O, a( ^ 删去或取消。 ( }$ [+ }$ b: O/ W6 e量,. ?$ j3 N' S( X4 T/ x' j 变化或差异。4 R: H' c; V1 r$ Y/ G/ ? 场控制, P5 R8 Y7 w3 `" s3 C 给用仪表飞行规则离场,和在某种情况下用目视飞行 / f2 T" G* b* K% I! G/ z q( E则离场的飞机提供空中交通管制服务的进近管制设施 0 ?' _5 e1 L7 G% k% g4 D# O0 E( G1 X( K2 v2 p/ D调,; C/ q: a# s ? 电压中获得调制电压的处理过程。& A; z1 N) }/ `$ h! V3 g$ ]5 z0 T 环境 % P8 @ n' R/ b力相同的活门。 1 M$ A s3 P; y$ Y: R8 rd$ D/ I8 u5 F4 n/ V, G# Q# _ tanks. 5 O$ V- ^, s" N: e. A# w) U! HD9 T: e4 r- _& X DELETE, To remove or cancel.. t8 k+ F5 A+ o# S1 { DELTA, & ~5 N; {4 x- m( {+ C6 l+ ] [- \D ) y# ?: y7 s/ Nc & j5 I6 U! W; ?8 K( Kd( E$ C4 Q' a! B8 a6 \6 x aircraft. 3 y5 \; A$ @; Y! s, M: B* N& ^" lD 3 l" k$ a4 Y4 F(modulation) voltage from a modulated & e) E/ V K$ e" Y+ H) gDEMODULATOR, A device or circuit which performs - u9 d' O) j! wthe process of demodul . q; } n8 K5 p6 H# E4 o5 GDEPRESSURIZATION VALVE, A valve in the hydrau # `" R: }; f, k2 x, o4 }/ Z" M% \% rsystem for de . \* W( k+ S( G2 }) c! _0 aa ! t7 M4 `7 R1 U* q排油活门, ; a3 \$ u: k. I9 P0 b, I燃油系统中的活门。用以为燃油4 ^( f" U3 o0 z( I9 b2 Y+ Q5 X0 q7 R9 z$ s) V# V( b/ ^1 M* e/ G+ `) b' N2 V删除, 9 F5 W# c. E3 F" R4 {9 R' c$ r- [6 u/ |8 s, ?# P; E3 k- Z$ D& q) B9 r/ C. X# w8 X1 y7 g 的一种功能 3 C: W- e/ w0 F+ w/ x; [: W: k. A- Q3 J 从载波 : y* U7 `, g# t" I解调器,5 a: m0 T9 h2 d, q/ P9 ~ u 完成解调过程的装置或电路。 3 h# N3 p4 `3 b5 g减压阀,7 Z/ Z1 f9 t- Y0 J+ L3 D& [! o 在液压系统中,将液压油箱空气压力减至与周围 7 e) F& I4 x) F+ u! ?& Q$ ~. s* J! J3 f6 ` 英汉对照民用航空词典B OEING % N+ m% A1 [) X5 bTECHNICAL DICTIONARY 42" L7 ^" K: S! m, x DESCENT, Phase of flight where altitude is decreasing. . d5 |/ L; [/ W/ ]* [ETAILED FLIGHT PLANNING, The calculation of fuel ! _9 Z( \8 ~' `. R( bnd required for a trip by considering each phase of/ ^7 ~) o- s5 D* Y C ight (climb, cruise, descent, reserves).) H2 X' k7 c. S7 O9 a al or" w# r3 k9 y$ @ B# K, @! D2 o ETENT SOLENOID, An electrical solenoid used for& ^' ` j" H2 _1 D t. o% D9 n$ f' Bspecified course or 4 x7 E: i X. d) V6 P. B. grocedure. 1 ~$ r5 ^! s4 @; Ye.+ P- k6 K7 T; h1 u2 P r3 ]- Q 飞行计划, 1 U9 \ R) l" R: u5 T将航班中的每个阶段(如爬升,巡航,下降,备降)都+ x$ h0 w! G! h! x7 J 人考虑,来计算该航班所需要的燃油量。 b: m! a+ v2 O! {$ A2 q用来感应情况之正常与否的电气装置。) K. @" u F# z$ B7 A 定电磁线圈, ! D E8 Y8 O: \7 u7 t出接通的电磁线圈。 2 e; ~1 U0 a% H5 H- a9 M9 k差, ' N t( T0 N! y& j% R- ^# E7 T% c与指定的航道或程序之差。 3 d3 W; U9 E7 `. l, L6 D用气压或液压操作的活门机构中的柔性部件。% b: j: Y! ~5 S# Y$ B D ) ~+ V- A( j3 va+ K, P7 @( U( E9 f' C fl& U6 s" C2 H, p X DETECTOR, An electrical device for sensing norm w7 z0 C( m9 V: r: P abnormal conditions. 6 a- T8 {9 n% O- h7 }D8 E( r9 {- |, x controlling the engagement of the actuator outpu h. L1 b# ~- h+ }1 [+ ~ DEVIATION, To change from a* @/ P" Q% j6 u" m7 F$ A p3 N* d9 e4 L# j& e& ~# V DIAPHRAGM, A flexible part for operating a valve * ^( _- ^- m* R3 Z/ `4 o+ ~mechanism by pressur : ^. b4 T+ m6 w* b0 R: q下降, - c& X$ k. g8 `' Z) D/ ?飞机高度不断降低的飞行阶段。 @! x; Y2 \' A1 M4 X" s详细* n6 r: Q! ?3 G: M' R1 {1 ~6 |# c9 `. y6 P# j 探测器,; E0 Q6 m6 F k4 q6 S& k# n. m1 `( t4 F9 R" ?用于控制作动器输 % @# N7 M$ A) h( W( N+ Z3 d6 @& |$ X6 r$ }4 U* o- `$ H隔膜, - K: g4 F$ I( Y6 s0 n( T英汉对照民用航空词典B OEING 3 f- n1 q; U, d$ BTECHNICAL DICTIONARY 43) M# ?% }1 b/ P5 m. S: I DIELECTRIC, A material which does not conduct# E1 P1 M) m' r, d G) T: v" l electricity and used between the plates of a capacitor( ] K+ `- ]2 K8 z9 ^8 Y (condenser).9 r; w' Y+ J; u0 x/ t nother pressure in the same system, measured in5 m8 Y0 ]( t5 l. `0 h6 U ounds per square inch differential (psid). 2 Q" ?) B) d% J1 ]' CIFFUSER, A part of an engine between the; o6 H% ]6 d, S# [1 X ompressor and combustion chamber for reducing the 1 l* t0 B% b6 s' x( Yair pressure. 8 i {1 m4 C$ q9 W- q* high 4 l# n+ U. I- K% Upulses.5 V2 |- b/ q: c; |1 x( ` ignal that is a close approximation of the original- g+ ]6 a) f* e+ @: y7 t ignal. : p; F: Q" f* X- @. Z" p1 F' h6 hIHEDRAL, The angle between the wing reference % D" X# a9 K7 jlane and water line.5 F$ P ~* a- }$ f 的压力,以每平方英寸/ J# t# q* s7 r% e8 z: `; T 少磅压差计算(psid)。 - {/ A+ \7 V; ^* T- a. ?/ g1 t ]散器, J; j# A" v3 c4 u' `: }( L 发动机内压气机和燃烧室间的一个部件,用来降低空 c% h4 {. i+ i7 M2 N' ]* C1 Q 增高空气压力。 ' I8 a- Y; z/ g$ Y换,: e! E. k: l @6 n 的连续可 & \2 P! J: ^: z2 r) b(模拟)信号的处理过程。 6 z% f2 w. x! |7 z* O) r d% V反角, / Y0 ^3 M# V2 }4 M8 x7 z机翼基准面与水线之间的夹角。 ) x, X, n( T( l4 L5 e. X: l8 f5 aDIFFERENTIAL PRESSURE, Pressure relative to& f" S& L& t/ O* |7 U7 o" f3 \ a * N, O0 `+ C- Q: v0 O4 Np $ C7 N) C9 N+ \6 l8 v- `( {D: {4 O9 R; A# |7 Q8 r c 9 @' f. T' `9 yairflow speed and increasing the ( h) e; N6 a2 C( FDIGITAL, Digital refers to a signal whose amplitude4 j/ C6 [: a3 k remains constant for a finite period of time. Digital ; j8 }/ v1 ^( j2 H0 Qsignals are commonly represented as a series of h : ^7 g8 T8 k' @( Iand low1 R- b/ e: G# b6 g3 ~ @! _ DIGITAL-TO-ANALOG, The process of converting a/ i- v) K: V% w4 `2 j) t3 c7 w digital signal (binary) to a continuously variable (analog) . j @0 c" G: ks4 M N2 D( S: o" D s : n. |) I' {1 k) Q9 k2 U9 TD$ W- v% V% b4 y O! M: ^ p " ~7 V0 ~# i$ `5 ?2 @3 z- }电介质,4 P/ ]9 M; C8 Z 一种用于电容器板之间的不导电的材料。9 d6 L5 J7 A+ ?" h* |& D) i 压差, ; o: l5 K- a( V9 K' F相对于同一系统内另一个压力 2 U8 T* O- v+ M# F8 K/ [ F" B! d, _ C" ^$ G+ V! d+ L, U3 s5 n4 l1 x* }* K气流速并 $ T) q, y2 Y) B2 n- B数字式, $ S% c6 t' Z; k& @! h指一种信号。该信号在一定的时间内,振幅保持不变。( s/ }6 x* x; m4 U& z 通常由一系列的高低脉冲表示。8 J( G/ V5 M, r& f: ? 数一模转 % w. `! t! M/ @9 g# e: t8 Y将数字信号(二进制)转换成与原信号相似 & Z {, D5 s9 r( S6 z! Y6 {2 P6 |) y7 E F+ \4 T. G) c1 V& u4 X/ o英汉对照民用航空词典B OEING ( N' D% {, G2 t ]) yTECHNICAL DICTIONARY 44 * A) e* V$ g: |3 bDILUTER DEMAND REGULATOR, A component in the 7 i6 m$ V. d* b/ a, K$ N( Ycrew oxygen system which mixes air and oxygen and 6 b4 y* ]5 ~; u' c7 Supplies constant oxygen pressure even if there are : i+ c" H: {! J5 d& o$ d0 [8 \# m4 Vhanges in ambient cockpit pressure. # n- P$ U- \! J: D; H, r0 [4 l+ b HIM, A word value of light. For light control devices - dim$ |% `' ~0 P$ t/ s6 `. ? the opposite of bright. + `, j/ h% l: S/ c6 t% b! [) i+ aIODE, A device which allows electronic current to flow9 q* Q7 F j7 m1 M% K only one direction- J# [, U& D. s9 i) _ uid in a reservoir.2 X; L4 |& `& X2 v- K/ A# R) f5 } DIRECT, Straight line flight between two navigational3 q9 _# P/ Q- E% d+ m5 Z aids, fixes, points or any combination thereof. When) V/ V. X8 Y- n9 j% z) K used by pilots in describing off-airway routes, points 5 r2 _, |* t6 n; t; k/ `$ e: Kdefining direct route segments become compulsory ) S2 t: u8 c- P1 }8 t# \reporting points unless the aircraft is under radar5 T5 X' S/ ^9 ]& b/ H7 h( I( G control.1 f. w& [6 o3 s 节器,; P1 b2 ^& I# E9 Q* k 将空气和氧气混合,/ M- n" O" \! o2 P6 [: v k* W, p 使驾驶舱环境压力改变,它也能提供恒定的氧气压力。' `- {( j2 t1 o- Q( B$ A! d7 w$ y; y0 B6 v/ C, l; l( K! P一个形容光线亮度的词。对于灯光控制装置,暗的反 4 `+ I) f/ i0 {( `) g7 ~词是亮。 / l* E+ o8 C& Q; c4 D极管,0 k1 d* k, Y3 o% j8 T- |( p6 m 只允许电流向一个方向流动的电子装置。 ; E/ o& c& S6 M/ H0 U: a4 x器内液体的量。8 P E- b8 w* z# a7 h3 z& h, b! t- B3 k 直飞,+ N1 K( }$ W2 K6 w8 _* l! T D 两个导航台,定位点,导航点,或任何的组合之间的直0 v, x7 H: x( ~7 \ 线飞行。在被飞行员用于描述偏置航路时,除了在雷达控 : s+ L& `' b# F制的情况下,确定直线航段的导航点成为必报点。- _5 } \4 G& D1 j, Q. ^3 _7 K! a& }% H+ d s : {& ^, |, s2 |, ^! e# n) nc # V' O$ A4 u1 Q: J6 C; S% w6 |- B% iD/ V9 `" d: }7 f! b! k8 M. _ is . c6 s. a& U6 @ Z% mD ) l9 C0 M/ @: @$ B% ?in % _( C+ k1 R# MDIPSTICK, A calibrated rod or stick for measuring a / w* G3 X* X# {; a5 A& M+ W. xquantity of fl; @4 {) G7 y& @ L5 c9 B; [" A 稀释氧调 L b3 {& F" Q7 G( i/ T驾驶舱氧气系统中的一个部件,它) m+ l* M1 k8 ]1 p e/ A* ~, H, l% O! M. A' E/ i" Q4 z: q) p1 d! T! s- Y; T! C, n5 K4 W" q" }/ K3 R$ v8 }9 |, c( q量尺, ' _" K" f$ |5 l( j. p* n校准过的棒或尺,用于测定蓄液 : e" B' p4 A7 ^6 K. K英汉对照民用航空词典B OEING ! g/ T% V; L8 z; uTECHNICAL DICTIONARY 45

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