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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 8 J5 K. b8 L* r% q0 `民用航空词典7 c9 W& B) W8 ^ 波音商用飞机集团 & W" ]8 ?( U; U7 i" c0 E$ sBOEING COMMERCIAL AIRPLANE GROUP 7 {; ~3 w" ^: o英汉对照民用航空词典B OEING ; V% n4 _: t4 q) b0 E: iTECHNICAL DICTIONARY 1 , |& L I( V! }' Y; N& c9 sA5 \2 F' f6 p3 N7 \ ABEAM (ABM), Beside: An aircraft is abeam a station1 B Z" @$ r$ C' B1 G6 H, s& \ when that station is 90° to the right or left of the track of $ N7 T. M7 U) G" f- C dthe aircraft.$ y; @; z+ X0 R2 x1 @6 D ABSOLUTE ALTITUDE, The actual distance the aircraft 6 u; F5 r {: y, v( o0 }is above the ground.6 q, q {# [- j/ X ABSOLUTE PRESSURE, Pressure of a liquid or gas ) M7 H) G/ B& Z7 P( g; {measured relative to a vacuum. ) _+ E5 v( \: n+ n- SACARS, SEE - AIRCRAFT (OR ARINC) REPORTING1 ]& F/ k* s9 R/ W2 n ADDRESSING AND COMMUNICATION SYSTEM- {6 e$ X j \7 S ACCELERATION, The rate of change in velocity with% P) [5 {6 y; ^- I% M4 n& s5 ^. b respect to time. 1 O9 q/ M3 A9 A6 ~1 ?ACCESSORY GEARBOX, A part of the engine,% [' j$ Z* T, `5 O. ` mechanically driven by a compressor or an angle3 Y8 |" g7 _/ _ gearbox, for driving components necessary for engine: a4 |) ], P1 f- H$ ?' c 正切,! h% n; l/ S& q, O$ T! T" ] and airplane operations. ' O# P R3 U. c& f4 p& B/ d当电台在飞机左侧或右侧方与航迹成90 度时,飞机正 % }( v: E6 y y, R4 w切电台。 * N- N) F# X+ x' l8 u绝对高度,: e: j. v+ f; m- w% k- {! G( r& j 飞机离地面的实际距离。4 d0 J# c& }; s8 |8 m! @ 绝对压力,* x+ g; p0 p1 w9 m& Z1 ^2 L; e# `4 V 相对于真空(无压力)测得的液体或气体的压力。4 f2 [- v! a; ^' n6 ` 飞机通信寻址和报告系统, @9 l# A1 [4 @" W3 N& m8 k* f 见Aircraft(or ARINC)Reporting Addressing and7 s) o' W- X" y& c, _- O Communication System. 5 b8 b( O9 A* h/ j+ s% S) V. ^加速度,$ ^% F+ G" |; _. I Z4 J 随时间变化的速度改变率。3 V4 E5 _- R) B 附件齿轮箱, 5 U/ Q$ b5 U' \) O) J6 f* l$ J发动机的一部份,由压气机或伞齿轮箱带动,用来驱动) ?% l# c, B/ u D 一些使发动机和飞机工作的部件0 |0 W( r7 ^/ k 英汉对照民用航空词典B OEING 1 ]- H9 ~+ p% O. @TECHNICAL DICTIONARY 2# j$ P; J7 b V ACCUMULATOR (NO. 1), A container with hydraulic0 O" u% T+ L. P6 N" K- b ts when normal hydraulic supply is not 9 a- F8 N+ v6 I5 y+ }$ t. U1 J W$ v" `2 svailable.$ S* B! f: {1 q8 P1 ?$ d CCUMULATOR (NO. 2), In a computer, a special1 @0 Q! m0 O* k: {( q, c0 @ torage register associated with the arithmetic logic unit,1 I+ i- H- o; h9 `! ` olding the results of a computation or data$ G. L- a, l Y* T ACTUATOR, A mechanical device operated electrically,& K; M n" |! Q, W' `1 i hydraulically, pneumatically or mechanically for * N( ~) P8 e5 K$ |$ t- e+ H& ctransmitting motion between components.: X9 F' P6 l3 I7 z8 a# { ADC, SEE - AIR DATA COMPUTER( b( I+ _' z ]4 O ADF, SEE - AUTOMATIC DIRECTION FINDER) P% G) E( y1 p, X" p; v* Y ADI, Attitude Direction Indicator, An electronic display of7 [ o* J8 j$ _. l- I2 d# n airplane attitude information in pitch and roll. 9 }3 [) R& I ]- E蓄压器(NO.1), 0 Y% q& ~+ b& n1 B' J含有靠干燥空气或氮气增压的液压油的容器。当没有正 M& n% P7 f/ F5 a- z常的液压源可用时,该容器可用以驱动部件。 * W; C2 i; i; h5 t% k4 e- l存储器(NO.2),( W0 I& m8 E( V! M1 h" T 计算机中,一种与算术逻辑组件有关系的特别存储寄存6 k4 I) V& l9 h4 @" T7 [1 V2 W 器,用来存放运算结果或数据传输。 # }: u) N" K, l, K# C飞机状态监控系统,5 U! j! Q! R) c8 i' [0 K 见Aircraft Condition Monitoring System 5 n- J: O& `2 H, {fluid pressurized by dry air or nitrogen for operation of 6 a3 v5 l0 O7 t' P: icomponen; A8 Y `8 Y3 V9 t9 |. v/ Y a 2 ^/ O9 ~# i, A2 d, @A2 F4 E# l; U+ n: A( W( r s8 v3 y2 M4 i( y0 ] used for h , B0 @$ f' J. V O7 C7 Z$ Gtransfer. " e( p6 }* x3 d. _7 hACMS, SEE - AIRCRAFT CONDITION MONITORING 4 z& ?* D4 ^& o8 zSYSTEM . ; m$ G* [; v- D6 m6 {9 E作动筒,$ F9 [ ~# ^0 W' g6 y' E 由电,液压,气源或机械驱动的机械装置,用于传送部7 i' p2 _" q6 C& Q 件之间的运动。 & ]1 V/ x; |) R# I大气数据计算机, , `4 A4 X- C% z$ j' E: u4 w见Air Data Computer. n1 w$ b9 h- L0 R4 c- o; q 自动定向仪,' j( g$ j$ P1 T% \( X 见Automatic Direction Finder. # d [! i( ]- m1 w姿态指引仪, ! Q$ Q! `2 f6 ]; {6 i; G用来显示飞机的俯仰姿态和坡度的电子显示。 / A. Z+ s0 Q3 M5 Q3 t$ z英汉对照民用航空词典B OEING. W G9 M, m/ l) T TECHNICAL DICTIONARY 32 a# w5 M5 }; E8 O0 M AERONAUTICAL RADIO INCORPORATED, ARINC is0 U8 }; _* A& S6 ?" G0 v, T ,/ Z* `3 y+ o3 u+ A; s nufacturers, and foreign flag airlines. ARINC" u' b' j9 J5 g% } evelops and publishes standards for electronic2 W! m P( I, j4 I1 j$ @9 H quipment and systems. * s0 @' f3 N9 m+ n+ i! pGILITY TUNING, The capability of the DME to ! {. {) y" I$ z, xlternately tune between two different DME stations in 8 V" o) t1 ^2 K: I) ?rder to get two distance readings from one. q4 k& s5 y2 d3 n F8 E! k terrogator.# R2 ~. x) h" y9 W2 G# m ge 1 ]: S4 z4 r: t1 g! e; t" hILERON FORCE LIMITER, An electro-mechanical : o( r4 C9 A! L' A9 xIR CLEANER, A component in the pneumatic system' e; D9 L3 _0 D) ~7 C' N5 s- S upply to the air$ l5 d6 y) Y7 a$ n onditioning system. ! f: [" a+ A# y5 @ W7 R. u订并出版: F% @) X7 P* g/ L- c, K# p 子设备和系统的规范。 9 h W! Q! E! Z) l: K& M3 ?% E+ Q快速调谐, 9 W& |% r/ U5 b3 Q j6 r: i, J9 G机载DME通过交替调谐两部地面DME电台以测得来自/ _; Z/ V! j; h: q 同一台询问机的两个距离数据的能力。( c/ o/ ^; ]* G1 L9 o 翼操纵力限制器, 7 ]7 d* h4 y4 y$ S; |6 [装置。在自动驾驶工作期间,用来限制驾驶盘) [0 I# |1 q* J' T" r% w 气清洁器, $ t9 V- R: e% `部件。用于去除供空调系统使用的发4 T1 a) }! ]# G, [ a corporation whose principal stockholders are United 3 p8 m2 K# ]% d4 w' {& U1 mStates scheduled airlines, air transport companies0 O' |& k4 p( K" g2 r aircraft ma & h' T% m9 U- u4 Q+ u; k! r7 Rd # P. u$ g- P+ B# f- d$ {e, i7 H& E% I. Q A 0 P# m8 n! n: d. p2 _9 ?6 ca ; R* z9 Z% W' K; z/ H" e" Qo q2 ^. h# I8 p! h2 L2 ]2 H3 E in ; {/ |* Y) q7 N- }. l9 g4 g8 {2 _AILERON, A hinged moveable part on the trailing ed& d& z0 j7 v/ I, e of each wing for airplane roll (wing up and wing down) ; O5 ~5 e( e1 Wcontrol.% P3 w8 z: v1 { L9 a, |, J, E A 7 Q+ g5 u! {* Hdevice for limiting the control wheel movement by the: C- J o& s B0 ^7 G autopilot during autopilot operation. 8 u9 q: P1 ], M# q- rA " V# ]4 I: U( gfor removing dirt from the engine air s! k5 ?& j* [$ \ c 0 N! L1 t- e, C; P: {7 q航空无线电公司,) W* B1 u' M. _! N! H. U) K3 R$ e+ V 主要股东为美国定期的航空公司、航空运输公司、飞机& k/ t7 q: ]" f! H7 ` 制造厂和外国领队航空公司的组织。其目的是制 % z: G7 j5 h$ q' p. E6 y- ?! [3 L1 u% v+ J" W4 x: K: z副翼,- `3 e3 G+ [& Z0 y4 \/ d 铰连在每个机翼后缘的可动部件,用于控制飞机的滚转 8 X5 {7 P6 U5 L5 m5 {: t4 x. j(机翼向上和向下)。, d0 l$ |4 P E# n! s3 x: |( F) _# L9 h7 c/ n 一种机电, F' T* V, l4 W6 [/ Y 的动作量。 ) K5 b1 v' Z1 B( [( j% }9 Z+ L/ N0 J& G1 o/ l- `: U" b 气源系统里的一个 ) {- g/ d8 J3 U8 Y! p2 ?1 H动机引气中的灰尘。- e; n' u& D( Y 英汉对照民用航空词典B OEING3 {5 N: @8 y! ?2 C: `& ] TECHNICAL DICTIONARY 4" \9 a |+ o! \9 S1 l/ g AIRPORT ELEVATION/FIELD ELEVATION, The 3 \: _5 L& h7 }1 C2 A$ O2 w& vhighest point of an airport's usable runways measured ! e) s0 B* M2 C+ O9 q3 Y4 G3 d* c+ x/ tin feet from mean sea level. In a few countries, the , W; K6 s O0 }1 v0 R; ? ^& n( tairport elevation is determined at the airport reference6 V% y4 a1 \' t/ r/ S point. * H0 C, c" k) m2 _1 a! }& ~AIR ROUTE TRAFFIC CONTROL CENTER (ARTCC), ) h" E! R6 A6 R: ^ervice |/ {+ T5 X0 ]9 s3 G4 ?% B; m ase of ) s' s. h) i Q1 R, hus flow of air traffic.$ p; V6 f4 J2 D5 V6 s0 s IR CYCLE MACHINE, A compressor and turbine on a ! j+ Y) z/ {5 F8 e* jommon shaft for cooling the air in an air conditioning ?5 L/ Z' E9 n0 Q$ i( b+ y# L- K2 P ystem. The air is cooled by expansion from high to low6 V: G: L+ j* K* w' r ressure across the turbine. The compressor is driven8 U: `. _0 k( p y the turbine./ p" s5 q, I$ M( Y) j3 U E, b 中航路交通管制中心(ARTCC), ) W# `" q2 Y, V* U域范围内使用仪表飞行规则飞行的飞机提 ( w" [9 U" c6 |管制(ATC), : d& ]* w9 Z, p涡轮冷却器,+ I8 H0 C3 A# V j& n- J 是装在同一的压气机和涡轮,用于冷却空调系 y' }6 r3 F/ ^& J5 m( A6 H 统中的空气。气经压气机压缩后,由热交换器移去热量,6 u' N6 ~ ~1 x3 c! H% g% H0 H 然后经过涡轮令涡轮带动压气机。通过涡轮之空气,温! _6 }9 U- g( Y7 b5 j9 b) v 度下降。: ?$ r/ P* W8 ?7 Q; @) y A facility established to provide air traffic control s $ W5 g9 X; f+ Yto aircraft operating on IFR flight plans within controlled( k7 x$ A3 V7 ~+ y0 @& g airspace and principally during the enroute ph : V5 W( C# O* p7 a0 Bflight.7 d1 p1 a& ~. K7 _$ T$ ? AIR TRAFFIC CONTROL (ATC), A service operated by : v: T1 s9 O: [9 m; G Jappropriate authority to promote the safe, orderly and" B: a6 z1 P+ D5 X% B expeditio; [8 T$ f/ S) D, k A 4 n8 f0 r6 [4 p( vc Z) v- R0 m' {s & {. e! c7 O6 l7 T& Ap" }4 P, e$ i" g b0 h; L" }. J1 o- V! c X) l0 H 机场标高, : B9 s' v3 [2 c/ c. h指海平面与机场可用跑道最高点之间的距离,单位是英8 Y9 p) {/ A) r' x5 o 尺。有几个国家的机场标高是由机场基准点而决定的。 9 f# Q& s3 h. t* P$ L& B! T" U& t0 L9 [4 f! D( ^给在控制空7 Q9 P p8 u8 Q: T 供空中交通管制服务的站台。 1 N6 Z! \, X' b* O" b空中交通% S% q) k0 G `6 v% x8 t 由有关当局管理,旨在促进安全,秩序,和效率的空中7 ?& t4 E, I7 L 交通服务。) e1 V# u: t/ ]* E& H0 p! A 根转轴上 5 c! S& h8 l+ ^+ C! W2 ]" F% ~8 |5 w" b, \7 c; E3 J# B+ H! ~1 v英汉对照民用航空词典B OEING : b% ~- r& W: e, Z( xTECHNICAL 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 ) ]& e+ A5 [1 i! f7 \data information, such as altitude and airspeed, based - V" s+ b/ Q( B- Q5 w- ~on pressure and temperature measurements. * V+ M" Y4 l, \5 g8 zes air/ U* U4 s% t# |1 s( F IR TRAFFIC CONTROL, A system comprised of : o9 t" o4 f4 N) [round and airborne components used to identify, track( W/ g! h8 b3 {$ e6 E OUND SENSOR, An electrical device operated 1 Y* I4 t7 Y' I& a. r. Ty the landing gear, which transmits on ground/in air: [) V. o, w* V5 d. q! l/ t formation for system operation in flight or on the1 X( [( _1 d1 M2 z round.! L2 q& U0 u: Y. p, u$ o' ^, \ IRBORNE VIBRATION MONITOR, The AVM takes 8 e, D2 P# F* w5 ^e signal from the engine mounted accelerometer and $ @8 M' D: ?# r! s+ jalculates the vibration on that engine. 4 K$ R6 a( s0 H6 O) i+ Gcorridor equipped with radio navigation ! I) u/ R+ d8 N6 qaids.! E) X: f0 a2 ~% }# I AIRCRAFT (or ARINC) COMMUNICATIONS % I3 W s: V+ G E: X; k! e7 eADDRESSING AND REPORTING SYSTEM, An , ~1 v) j1 Z" x, o" i. ^6 T0 i7 [addressable digital data link system which permits the! b4 F& [# L j2 i8 c1 M# ` exchange of data and messages between an aircraft1 m- B/ l9 T: {3 c3 M" w) Z5 t and a ground-based operations center over a radio+ U$ k/ }; u# Z+ P% m- v' J network. ; g4 c, B/ V' p* rAIRCRAFT CONDITION MONITORING SYSTEM, A ' o, O+ h3 r8 `5 H! Y. lsystem of sensors and recorders to monitor various' g, r3 a6 c* U2 H3 c airplane systems' performance and status. " f5 e$ u7 J3 N5 D) z8 x3 n机,0 q- `4 O2 `: R! ?8 G9 ~2 q 中交通管制,) l$ r2 ^) p" B) c 一个由地面设备和机载设备组成的系统。用来对飞机进- E2 P; w* |. F6 ]3 {$ |. } 地传感器, O8 G' G" F6 f+ P& C* c" e* R* T一个由起落架操作的电气装置。用于给空中或地面的飞( o: X# q1 s) E) F8 v, X 系统运作传输地面/空中信息。(有些系统只能在地面& R2 e/ ~7 N: f3 D) f# o* Y+ }9 a 用)9 A7 _: c7 a& `0 x 载振动监测器(AVM), 6 d' k9 v* V$ }( o/ \AVM从装在发动机上的加速器取得信号后计算出该发 ; t* Z( n% o6 W机上的振动。, _- _6 B6 H$ E/ ^/ Y7 r 式建立的控制区域,内有无线电导航设备。 2 O" n- |7 ^4 N& y" c; k9 j) h飞机通讯寻址和报告系统,; ~+ D- |3 |( v, O 有种可寻址的数据通讯系统。利用该系统可使飞机与地 ' o6 S2 _! t1 g( m" `面操作中心通过无线电网络进行数据和信息的交换。1 C1 D9 _2 x' C" ~, X1 Y. {8 x 飞机状态监控系统, B2 @4 A! c8 ]( j 一个利用传感器和记录仪对各种飞机系统的性能以及$ F; f2 A/ R' D( J0 I2 L 状态进行监控的系统。& E6 M b1 [ @7 b" u5 M A , l: w, D( S, X$ r4 A# t" m6 \5 Rg / {3 h5 r9 k; xand locate aircraft.# |) n$ T& Y" G AIR/GR 2 R6 I0 W& N( Zb9 \6 K) x2 k% k# n0 q4 X in 6 F/ T5 Y3 W+ r/ [g ' Z5 g* O/ M& S! A, a; m, h. ~! ?A + A( |' D) V7 y" U8 D" f% f3 kth 8 t* d5 k& }# B3 J# ic8 B' W+ p" ~% {8 F& L0 w8 ]: K AIR WAY, A control area or portion thereof established - l3 [. M& A2 l$ a- din the form of a9 ]. ? [0 R, J/ V( q 大气数据计算* i2 r2 e3 S3 y0 y8 S! _4 O7 }. z9 Y/ a 根据量取压力和温度而产生大气数据资料(高度、空速# K9 E2 }" |9 a4 A 等)的计算机。0 r# o7 A b1 `4 v" w$ W9 b S: g+ \行识别,跟踪和定位。8 o2 N; [4 x. U0 @; Y, c% ?: R& ]' _% \1 U0 u7 `' ~, H- I1 a P Z: [/ a使 6 F* \3 R2 e0 T' T u2 T% \7 ^( K( {' s& w* e- Y# N3 |2 {/ ?1 T- Y$ Z* ?* p 航线, ' J% G2 h) S, U" H ~以走廊形 - D3 a" E: F" v# `) x8 e' X2 Y2 z英汉对照民用航空词典B OEING* J; v" Z* Z( T3 v# j" u8 W" V TECHNICAL DICTIONARY 6; ^& Y) C h4 k: V- c0 c( p, h! H AIRFOIL, A surface designed to obtain a useful reaction, & R5 {& S w' I5 g3 g. T* T. U: Zsuch as lift, from the air through which it moves. Wings,# }0 p. s& N b stabilizers and control surfaces are airfoils. 3 M4 ?+ s0 w+ u1 U6 L( y5 j6 yAIRSPEED (IDS, TDS), The speed of the airplane) L3 O7 q F- L0 a1 B' T1 |, @ rough the air. . h, S. F4 D. J. ]# iD INDEX, An adjustable pointer on the ' e" s! t0 o, o/ U) Iirspeed indicator.0 N) h% x E1 u and legal ability2 N5 n- x: p; l7 o, v# t fly.& I, a3 [. D: s, f m, for example, the procedure for finding the: ?- J4 T, ]" ~3 c( O quare root of a number., S8 P4 K7 ?* A2 @) Z; R- A y & g9 u0 x/ v! o4 K4 pre, wind,, A' q6 G5 @& X @& J1 M and aircraft flap setting.% I$ b7 I3 a; z( P! z 是翼面。+ d4 E& H$ \2 ^# V& q 速, D# {. u9 }# ~3 c3 ?3 o 飞机在空气中运动的速度。( I$ ~( J+ j& E" t& E* u+ d2 y: C4 V0 k在空速表上可以调整的指针。9 V8 @7 R$ K( i/ F5 E" k+ q 机械飞行能力、和合法性的飞机状态。 ( i& `) B- w! y8 y! J! n一步一步的解题方法。例如,计算一个数的平方根的步 ], n7 i8 @2 q8 z* G7 L/ ]/ P: m& \) }6 s5 J1 d7 A! F% i9 b2 A0 e8 v 资料的法定文件。 & |4 C! K1 t6 U" [翼位置成函数关系。 - \# O I9 X: { X0 W! ^9 P( Zth 6 K3 [5 s' d9 O( ~) p9 cAIRSPEE" {0 h* r9 ?1 e( c9 G9 g a * q% i) J- {3 ?8 G6 m3 G* t1 ?# VAIRWORTHINESS, The condition of the aircraft with" ^ L" N( H) S* N& |, x4 y respect to its aerodynamic, mechanical, : }! U, `1 ^8 {) j! X0 eto 6 u- y. {. B6 W1 s4 `ALGORITHM, A step-by-step procedure for solving a ) I2 r: D5 _$ _( x3 ^* J- g% Qproble9 l* r' R& w* q. U s+ n4 F7 a$ o D5 {; U: t( z, f AIRPLANE FLIGHT MANUAL (AFM), The legal. K5 C/ L9 Z3 K& W6 c: L. ` document containing performance and operating limits, ' n' x- U6 m. M& E4 ]operating procedures, and takeoff and landing ( W: r P9 J7 hperformance. 1 W6 V& G( J( b0 y ] g5 C x! fAIRPORT ANALYSIS, A comprehensive set of takeoff 0 s$ X! P: L9 p+ s2 |/ B5 i1 Zweight limitations for a given airport runway, generall & V. \( D) p3 u! S& q, Zpresented as a function of airport temperatu # b8 _+ t( F, R翼面,0 F( e! Z. ], Z2 _# g; k# s5 T- W 用以从气流中获得反作用力(如升力)的表面。机翼,! H5 W4 w8 U# @! {9 D$ S$ y 安定面和操纵面都3 d! ^6 y1 ]/ D, I b% ?) \) |/ J9 v空速指标. S* e5 q8 S+ P 适航性,6 f. Z8 r" W6 w8 F) f0 P 有关气动能力、; C+ k1 @: h! S- G, V1 \ u 演算法, # z- s' r) e- f; p5 M2 v7 h% H6 F' Y" R9 D, @- b 飞机飞行手册(AFM),3 L. D7 _: s7 |4 ~4 U. U 包合性能极限,操作极限,操作程序,起飞和着陆性 + A% V0 H9 |: n& K/ K3 N+ d7 b) B* C) w机场分析, O% U7 d1 F1 M' p 一套针对给定的机场跑道的详细重量限制资料。通常与7 p8 E. J% k( p 机场温度、风、和飞机襟4 {# w, z# M. G5 K4 P% f: Y 英汉对照民用航空词典B OEING * y* m6 [5 |* H* J* rTECHNICAL DICTIONARY 7 " A4 K& m: \" ~. V6 J8 ]6 C, aAIRSPEED BUGS, Adjustable pointers on the airspeed ! J4 t+ ~3 o- Z+ v4 j- R$ P2 O' eindicator. 6 }' ^6 V; n3 A; V7 p0 ]ALLOY, A mixture of a basic metal and small amounts* A# s h) Z" X. t7 H; j0 g( B f other metals to change the properties of the basic : J) G9 z! \: retal.7 ^( u6 r _& I: ?& L Minimum airplane speed.' s$ [+ Z% } {! b! s" `7 v e of 1 u c( x, E7 v; r' v+ B5 w/ _# Hitting airplane angle relative to + h5 d1 F* q! X& u1 dirstream for the stall warning system. ; r/ L0 v# [( b/ ~another. % q" C) Y# r$ e6 }* D3 A* ]LTERNATE , An additional airport selected during/ K. r5 v7 I8 u* W/ R- [9 P1 Z: L1 K1 Y, _2 W V& j; n3 B( d合金,3 B" ~1 c' ^; [# i4 m 在金属中加人少量其他金属,而改变其性质的一种金属! l1 K# D. E: k! J! m9 I7 x* G" ]3 w 合物。 7 b! a5 y& [7 P0 g! n5 N飞机的最小速度。 ! d% `5 q/ n/ M5 l$ N" a速警告系统传输飞机对/ ]$ j2 u# Z9 L* b4 C 流的相对角度。3 h& b$ T" [) x 由一个状况改换到另一个。- e4 d0 z( z! \' m# s 降场, + Q& q Y3 q. W$ M: V% [6 f6 W" H划时,除了目标机场之外,所选的另一个机- i' q' _) z7 J6 |5 m! W: V l% m o : w# _$ z; b( G! q# |% N0 `+ o; Ym 8 U! a5 t: d3 i( ?( i6 _ALPHA SPEED,* f) k2 e, ^% j" {, \3 D ALPHA VANE, A small moveable airfoil on the sid & n) P- j" o4 ithe fuselage transm $ F) D- B6 Y7 G+ sa V& e' \( B! h1 {ALTERNATE, To change from one condition to . s @. P: |' } S, UA7 k9 u6 V; }/ D% n7 k/ [( x$ @& W flight planning, usually near the destination airport, to be 2 t/ i( x/ ?- [; n( D2 i# [used when it is desirable to divert from the original % g l) ] {/ h" ?destination airport. . F) t3 M) M( U- H$ B空速游标 1 Y- h3 y9 S6 l空速表上的可调指标。/ `5 x5 ^4 \! i6 F8 [( B# I) z% g/ c# o! r; J3 A3 @ 迎角速度,% _: d: @$ l: \6 L 迎角叶片,# f l; A7 [/ J k m# r/ t- b7 n 位于机身侧的可动小翼面。为失 " M. ^' C6 R8 u% t2 T L( E/ f s$ W9 B+ C( G: A4 ]% g 交替,/ E) I* W2 C/ W0 J9 y) k! {9 z' N6 R& E! \4 K( S制订飞行计) M7 I& n- f6 ?& G' I5 @ 场。通常在目标机场附近,以备不去目标机场时,改降之6 U, ^7 M$ R2 H D' J3 @8 w M$ V2 m 用。* L9 @+ F; S' B# u I. X 英汉对照民用航空词典B OEING 3 `; F' R( p" f0 F! _2 x% m) \TECHNICAL DICTIONARY 84 A! c X1 i) _& n) Z- O$ @ ALTERNATE AERODROME, An aerodrome to which1 w1 s; v' ?! q an aircraft may proceed when it becomes either$ P0 S2 C2 a- p% r" v" u" [/ Q possible or inadvisable to proceed to or land at the1 ~2 k8 W; d6 S9 t7 F; O( i2 U erodrome of intended landing. n' B% @8 p7 Q( X% D1 i TER SETTING, The adjustment of the altimeter 5 ]: `- L- w4 ^- R1 J0 Taccount for local variations in atmospheric pressure. ]+ c) Y5 J' h. v. T! Q+ t LTITUDE ACQUIRE, A digital flight control system ) }: n& w" v$ I7 ~; x* Jode to transition from climb (or descend) to level flight.1 a' Y0 E- e/ j8 R2 M. M LTITUDE ALERT, A flight deck alert occuring when the5 {# a" {$ E! q3 b$ R. L3 A irplane approaches or departs a selected altitude.1 x- t ?' ]2 j# t) f, b; p9 n LTITUDE CAPABILITY, The maximum altitude at* N& j: g* _& O1 L' X4 b& ] hich the airplane can be flown at for a given thrust,1 c% J5 n( { n peed and atmosphere condition. / `% N5 o7 i5 C0 u( [ @5 zLTITUDE HOLD (ALT HOLD), A mode of the autopilot ( K% X' g L% B/ Q; t5 Rr flight director to maintain a selected altitude.* N0 b' O3 g% Z6 ^- ]4 \ irplane's altitude during VNAV operation. 1 h. k, o3 n# O+ w T1 ^* f" _ l机场着陆时,可作着陆使用的. l* ~+ v1 u9 `9 P5 y% V* V 场。( p) M. A* h+ V9 N) U) H5 w5 X8 L: m# d0 }* h3 Q2 j根据当地大气压力变化而对高度表所做的调整。) M) i. \9 c7 o3 F" K2 p$ A9 J: E 一种数字式飞行操纵系统,从爬升(或下降)改平的模 ( h1 _& ?, y" y: V; S. d- n; b1 @. ]; h度警告,. v( J2 ^% ^, I/ Y& v5 N r 当飞机接近或偏离选定高度时,所出现的驾驶舱警告。& w* H* m/ v# v/ L) h/ P; A 高度能力, * i: l7 N) v; a9 Q+ y# e- i在给定的推力,速度和大气状况下,飞机能飞达的最大1 n( D" I( r% Z3 ~& J! h& `$ c 高度。4 J! W" {" A) o2 `4 ] 高度保持(ALT HOLD), 9 [2 w6 l; U9 Z N自动驾驶仪或飞行指引仪保持在选定高度的一种方式。( x, U3 }7 B( A+ \) k* x% Y) _3 Q$ ^$ T$ U$ J8 E员对飞行高度的控制。 3 A4 Y! V! X% Y5 ]( Iim ) i" k! {) G; J. `a! p# V# V* P0 a; Q8 t ALTIME # a# ~) o' ~. J& Bto; H- G) p+ e6 a- I A" \5 ^+ r4 y) _% Y- O m8 y8 l- M! V' R A , V4 G. t; f8 b4 Za ; b& B( M9 }! t# r; t* tA! J* H# P1 H3 ~) C w ' [! @4 N+ n2 [4 T5 gs * z# {' F1 L! q3 w; X1 ?% c* PA 0 `; p- S8 ~1 h6 C! lo ( s2 I* a* w# C# J+ W4 a5 M5 qALTITUDE INTERVENTION, Pilot control of the 2 d+ f$ x9 t4 Va( h3 C( H3 k/ Y( Y: Q" N# m$ k AMBIENT, The surrounding atmosphere.. J0 ~( L7 r/ ^ 备用机场,2 E; I" i) s0 Y" U7 L 当不可能或不适宜在预选 ; b. ~. ^# C9 m8 r3 b. ` }# N, G) k! D5 l) O4 ~高度表设定 9 ~( _$ I4 o, Z( m) d3 |# O高度截获,2 P$ G+ _. S( M" H. J: C* \' |: G* H6 Q; D1 t0 u+ U; G$ G6 T1 G5 _. a+ x- b, Z 高度干预 3 G$ t+ d6 x: K$ Z6 ~2 R2 ^在垂直导航工作过程中,飞行/ e5 i% j3 }4 U, o9 R* c* ~ 周围环境(地面气层), 6 i; x' {8 ^, [! M6 [0 E3 i* f/ Y9 P3 X物体周围的环境(特别指大气)。 3 e. S9 {1 O/ W) Z英汉对照民用航空词典B OEING 3 r1 Y2 [" f( W X& M2 pTECHNICAL DICTIONARY 9 ) B9 y( c( Y$ z* OAMBIENT PRESSURE, Pressure of air surrounding an " e( u5 v3 i G" A% K: n/ K: N2 lobject, measured in pounds per square inch (psi) . " n! ^' i8 p% EMBIENT TEMPERATURE, Temperature of air- w/ d* ~5 x: ]7 N; X. _ mpere." E( `0 e0 x0 _; d urrent waveform. 3 f5 s; i/ a& @# Hg an) v9 [: {" @! B, C. Y nalog signal to a digital signal. 5 |7 Q6 Y: e) R/ j2 Tore inputs : K& L( L% y+ O4 |: a, _! ]f binary digital information and one output. The output # D/ ^+ D: E5 s8 s0 H$ ^) k1 only when all of the inputs are 1. The output is 0 % ]7 O) T- C' h2 W7 ^6 @6 |hen any one or more inputs are 0.! e8 j4 ~. m) i* p 面气压),; ^" S& ^/ k4 M9 r9 J 境温度,3 ~3 i2 q" a( D4 p/ [ 气温度,用摄氏度(°C)或华氏(°F)来 ! s5 F( z/ _" K6 Z$ U: X0 ~6 S+ D' a9 V电压或电流波形的幅度。 : l3 D8 k- ], @! _5 n9 w性变化的信号来工作,或产生连续性变化的信号7 J) G, S3 e; t$ U+ y9 p 统。 : n: o2 } x* L& R! ^将模拟式信号,转换成数值式。& t. e8 ~$ n8 @9 _7 W- L z5 ~( }. ? 一种有两个或两个以上的二进位数字信息输人,一个输 9 _9 Q) X y4 l w! i. c' i4 p8 G# o2 N的装置或电路。当所有输人为1,输出为1。当任何一个" I* Q, d" [' g4 u! {2 w 一个以上的输人为0时,输出为0。 , }* ~) J& k$ ~! m. G6 kA ; R! M9 Y. {& r- ?) \1 Msurrounding an object, measured in degrees Celsius# j6 F: w# p8 o& X$ S, l2 {% s (°C)or degrees Fahrenheit (°F).8 e: g: A& q8 k! S AMPERE, A unit of electrical current. One volt across 0 [5 e/ ?7 u# K- Mone ohm of resistance causes current flow of one+ @: ^5 ~) _7 K9 U6 b- P$ `1 U a 8 K' r3 H# i9 O$ F. o1 qAMPLITUDE, The size or magnitude of a voltage or ; r: G- f" s( F9 N% ?1 P/ T7 mc F6 }8 U; f; K( ]- {2 B ANALOG, Quantities or representations that are ! `# z, f" v3 ?1 E: i3 A1 @variable over a continuous range.3 z& V# D! |+ l# S3 ?5 Z+ a ANALOG-TO-DIGITAL, The process of convertin0 }, D- g0 ]9 S( f9 o a 9 v! j/ [6 W) O D: A% @AND GATE, A device or circuit with two or m0 N: @1 D @6 N o % G5 o* i! `, [% pis ' g8 m' k" C; p# ?3 z0 ~# }2 cw 9 B6 e/ G! z+ P3 I环境压力(地5 Y( x& Y1 g2 l) s 物体周围的空气压力,用每平方英寸多少磅(psi)来 ) Y( m( T$ m0 Q. V; u5 p" Q度量。 + k) Y; z% I" R6 F( X$ T8 N/ m# F, h4 Q9 p物体周围的空 # Y$ R8 g% x3 Q/ |# y度量。3 v) M: c8 ^# O* G) n 安培, * `! Q# `6 f& |4 i& o" }电流的单位。 $ G6 J9 G3 R% D- h/ C/ n( ^' S1伏电压在1欧姆的电阻上所产生的电流为 2 l4 `3 f3 u" N$ _1安培 5 R( N% I G( i振幅,: p: n0 H' I b& W3 p 模拟式, - D/ C% K5 R, T; P; e8 X5 V- O用连续 5 v5 g% A- W/ A5 D1 _1 E+ h" H0 e, A2 a# ]! g从模拟式到数字式, 4 M# {- \2 }, ~6 l" x8 y/ b与门,9 G1 h! ?4 g7 D$ P- C" O7 G7 L g% Q( B2 }8 Z! p; P4 X+ T" y$ k( T0 ^9 u英汉对照民用航空词典B OEING: }9 j9 {7 e0 c TECHNICAL DICTIONARY 10+ Z n' W" j9 x! j. D ANEROID, A sealed flexible device containing air at low/ h& V. C$ V l pressure, which expands or contracts during change of - z# `5 }4 X0 x* c( I |" N( E" Gressure outside the device. # z' @% f7 e, L) b4 t/ iically1 m- `' z" C1 q0 Q0 M- s r changing the direction5 j$ M/ m, s$ d9 Q. C f drive. # U/ s1 p; t$ D9 I7 |of the wing chord in9 a4 u$ J' L& [% ^" ~5 X lation to the free stream airflow as it moves forward $ c, B2 t# ]; jrough the air., `6 L9 R: M+ x+ Z al axis of the# D$ p+ _+ _' h: a/ f- ]3 x: G aircraft.0 `! ]2 u3 _7 ]1 {; O 胀或收缩。 " m' P# f& f% Z7 d& U, e% u' y箱。是改变驱动方向的机械装置。 / Q. Y9 ? P- d1 _机翼翼弦在空气中向前运动时与自由气流之间的夹角。9 K2 U7 A1 Y; S/ a; b2 h- K- h7 m6 t4 F0 L p , @+ ?, x$ B3 \) c1 _ANGLE GEARBOX, A part of an engine, mechan 9 V: I4 j+ ]; {driven by the compressor, which drives the accessory8 u. h6 l' F! E8 ?" Q6 C! Q+ m7 c; [ gearbox. A mechanical device fo 7 m# k' z$ o( J: d+ v7 X( S. Po 2 R! g, r; @* F# D% Y1 }ANGLE OF ATTACK, The angle$ S# k8 ^1 t- O: g. k ^ j re5 h9 a* P* b/ n+ }9 e6 b th 4 o9 H; M+ S" U% a( k* iANGLE OF INCIDENCE, The acute angle which the! G% W* f- Y7 c; w! k wing chord makes with the longitudin # }, A7 @, c: I; X膜盒, 8 _9 s. y. A# T; w& b内含低压空气的密封弹性装置。当它周围的压力变化8 @7 w# F0 N) j( G 时,会膨2 k- M g; A$ P2 d, m& ^ 伞齿轮箱, ) V6 Q w, s- \# _( }发动机的一部分。被压气机以机械方式驱动,然后驱动 7 L- c- s6 c: z6 i2 h附件齿轮4 @- n" F# ?3 e! `* B6 f 迎角, : n5 M4 w# I4 {% t, R3 ~1 f/ l安装角,8 c: t* ^* u$ T9 R 飞机的纵轴与机翼弦线所形成的锐角+ l& C+ H& l7 Z1 v 英汉对照民用航空词典B OEING/ \) }7 a; F' r+ L2 k TECHNICAL DICTIONARY 11 5 }" ^7 x6 h: P2 ~4 Z) B6 mANNUNCIATIONS, Audio or visual indications used to : G3 \; ?, [2 h- F% o: P; n1 tcall attention to an event that has taken place.( }9 \6 ^) p, k% M$ o; v( A8 } ANNUNCIATOR, A visual device consisting of a number1 X8 D3 G. I, i5 [! `; O* t, ?+ U ly. 8 ^- ^1 s! x/ {/ c% U& gANODE, The element toward which the principal stream; P/ j: O% b5 B* m( Z of electrons flows.6 }9 Q- h/ v( x! M" K3 m ANOMALY, Not normal. + u+ s$ J# x" pANTENNA, A device which, used in conjunction with a 5 t( G, L4 L( H) ~' \2 m ]transmitter or receiver, is used for radiating or receiving ; X% b4 O% T/ ], |5 o/ n- vradio waves.2 Y# \1 p( n9 P3 b" m" g+ Z8 { NTI-ICING, A method of preventing ice formation on . b5 p6 ` Q( x. Pe wing leading edges and engine nacelles. - k9 d8 D$ I4 z* [7 i/ yNTI-SKID, A system for providing maximum braking% m0 V" X3 i" a7 @' m5 g2 o5 O$ b ithout skidding for any runway condition. Anti-skid * m& d' y% @4 Z* \; ] _omponents are part of the brake system.+ M9 [9 T5 d; L6 O+ U0 T 告, ) v: j" K4 @1 N; ?6 s Y当发生事件时,以声音或目视指示形成的提示信号。 * Y8 K. f( \; U5 O. N6 m与之有关的电路的现有情况或已存在的5 t5 e/ }3 |" W8 l& u! I+ r$ N5 }2 i 正极, . K* X0 k% p% J7 a( [6 N8 ?1 h0 ^主电子流向的极位。 - l: T9 l" I7 L3 v3 C& F异常,' O6 \4 u3 D1 l5 K0 {6 b 不正常。 1 E/ T0 J# T y% v$ u" c$ J7 b天线, 9 m* }; f, {3 ]+ E9 i一种与发射机或接收机共同工作来发射或接收无线电8 B* ^, Q9 U% Z3 E; U( Z2 x 波的装置。) L% T' Q6 w2 e/ Q; H% A$ L) Y 冰, p) F1 ^5 i0 i! e; r: L防滑系统,. a+ n" j5 V% q) D5 o/ D7 A 一种在任何跑道状况下,都能提供最大的刹车能力而不' S$ [% r& v f 使轮胎打滑的系统。防滑部件是刹车系统的一部分。# x, H! {- @+ e8 T& M of lights. Each light indicates the condition which exists 4 `& \) A# R. j/ i! Z0 v' a* e+ Eor has existed in an associated circuit and is labeled9 Q+ I; P# h& f) ~5 E. P according. F4 |7 i) U. a& ~& [; C; t. E A 6 o, O/ y( p- v- v3 Qth% A7 W: ^/ X c. o% a* V A & @* e8 O i, Z: G$ ^! Tw 2 c# _$ o; H: ]7 W5 Oc 5 l/ O& w) J$ `1 a0 L+ k, A2 }# U; A2 L$ b2 Q; a信号牌,4 k! Y8 f. p& [, H6 i 由一系列指示灯组成的目视装置。每个指示灯都有相应$ D1 Z$ y0 m8 O( s; |) l; q 的标记,用来显示 2 J H9 @6 M: g3 g* b; m6 |( R8 V& U* e7 p8 c" J: S; m* [0 C# E 防止机翼前沿和发动机短舱结冰的一种方法。) j6 Y k' L; {& ~' ?4 N 英汉对照民用航空词典B OEING % n8 n% H+ B9 C dTECHNICAL DICTIONARY 12 1 {$ q5 I1 v( T& m) d( p. w/ IAPPENDIX, A supplement to the Airplane Flight Manual 4 A! W! E/ o1 W) z% n1 }& X$ otained in the basic manual. A ) B' A" |1 @$ _9 j- u/ p rollection of supplementary material at the end of a4 j1 W7 F0 o) f6 _7 b ook. 6 d3 I$ A" t+ x3 [! v6 g9 vof the9 s, P( ?/ |7 M' _9 L rsion link on the landing gear.' }* x/ S6 Z& B6 D APPROACH MODE, An autopilot/flight director mode + k& X" H' l/ b" @8 Iwhich is a combination of localizer for roll control and5 \( B! X+ u8 H) L) d glide slope for pitch control. This mode is used when full : w; c3 N3 B0 } J4 [( tinstrument landing system is available.9 |3 C8 i: J8 r* k( o APU, SEE - AUXILIARY POWER UNIT ) l/ b) N9 f+ ?5 y/ JARINC, SEE - AERONAUTICAL RADIO7 n+ s. e) T$ _! |" Z INCORPORATED& e/ h" w7 D6 { ARM, To make ready for operation./ @, q4 {9 b9 y+ d$ j 附录, ! V5 a& W7 B( x; ^; \: v飞机飞行手册的附件,包含基本手册中未提到的飞机形- Y% ]" M0 V' s! S" S/ h 态的其他性能。是附在手册末的补充材料。 4 V0 @' {0 t7 _0 T" W/ r" f顶销, 9 g w8 r9 x6 s0 \9 j2 {; n用于连接起落架扭力臂两部份的销子。: A9 U" c$ p- s0 q% m* ^, f1 Y$ ] 进近方式, ) L; o, l9 u) D( N5 Q" c: y: H一种综合了控制横侧的航道信号和控制俯仰下滑信号 & n# n2 U# W# U m9 j* w的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系 $ _, F4 r# {* m7 z) Z% R1 r统正常时才使用。$ W1 v6 a% e* V& q 辅助动力装置,7 [8 e5 H; H/ Q; M# s3 J: N9 b- W 见Auxiliary Power Unit - t4 D, R% {3 U2 Y( H. B8 lcontaining additional performance for aircraft# _ |* q7 f4 X+ g2 |& { configurations not con 4 j4 W1 C0 Z# _% [9 n& P3 o- Fc 0 B- ?" C+ u' l& S; D4 s" @ eb a/ q. `& c3 F8 @6 a6 w6 dAPEX PIN, A pin for joining the two sections0 t" z! v3 h0 {: I5 h/ v0 N& Q to Q# I, p9 j8 \! E5 b! e# R) K5 B& p3 e 航空无线电公司,8 u$ A8 I, }& q x+ ? \8 t5 k5 V 见Aeronautical Radio Incorporated. ; o$ |4 f: S% k1 L; a3 }+ e预位, ' d6 h, ]8 O; W0 \9 T, V部件可以开始工作的状态。 " ?* p' p3 R2 ~) Q0 r8 c4 s5 ^: E& s英汉对照民用航空词典B OEING # ~1 d# t$ H2 K5 i! m' j- c2 m) ~TECHNICAL DICTIONARY 13 : P2 R7 ^: w; t; V+ b4 zARC, The curved track over the ground of an aircraft a5 r! B. D6 F+ g6 tflying at a constant distance from a measuring* S9 q7 w- {0 K& N2 Z equipment (DME).8 n. ?3 g1 P8 _8 K in the limits of self-contained system) A7 L L @& y: B+ L; Z apability. / `/ e3 Q) k/ s) b J, Ptem for opposing or restricting1 m9 }: O }" y8 L8 B6 f* P. ~8 O. U; ? ovement. . B* k/ T. k( k* B3 R+ hSPIRATED TAT PROBE, A sensor that measures total 0 o; t5 U9 p4 x4 t6 ^! E9 ?) Oir temperature when the airplane is in the air and that # u: X+ M/ i3 f: v& W1 j% seasures outside air temperature when the airplane is . T6 c. B7 {( E) \2 On the ground. The outside air temperature is measured 3 k! g0 F# p( i5 Q' jSSEMBLY, The fitting together of a complete structure1 P" p- W' V* u1 M7 y4 q9 S6 | SSUMED TEMPERATURE REDUCED THRUST, The6 N, N g) s: i2 }% s' | ATC, SEE - AIR TRAFFIC CONTROL6 H6 f8 @4 G5 E5 J% C/ A9 F1 M# \+ x1 l 系统中所产生的一种用以抗拒- B V2 f4 d$ _1 C 作或限制动作的力。 0 Z; S2 V' V: j2 ^4 n头,3 c2 l& j9 ^( p& G/ B, v' O 用来测量飞机在空中时的总大气温度和在地面时的外 " X7 }" T* p1 k# h7 a9 I2 O温度。地面外界温度的测量是利用引气将外界空气吸入3 K7 S% ?) \5 k 头,以达到测量的目的。1 x3 ^9 F* a' o! v2 g7 A$ ]1 p+ \ 配,& T- x9 c3 j9 B5 w: B) ` 一个完整的结构或组件的过程。 7 f- ]8 g* i' f1 g W7 B假设温度而得的减推力, 8 T; I8 B6 u3 Z D/ f, D推力设定值时,假定一个比实际外界空气温 ; M2 e, Y, E4 O$ G( _3 I空中交通管制,# b [8 q6 D1 I 见Air Traffic Control 8 S* R8 J# ^: G+ D3 l) xAREA NAVIGATION/RNAV, A method of navigation 4 A/ T$ Y. _' P' W ]that permits aircraft operations on any desired course # G* J$ R/ {# D0 f' T3 w, lwithin the coverage of station-referenced navigation8 Y) Q4 F: l& _+ K7 o signals or with& Q' T$ j: E7 Q A- d c 8 H7 C0 o' p0 {# \1 {0 l$ `ARTIFICIAL FEEL, A force developed in the flight! L( J4 ]& N, }- D; O control or brake sys, U9 m' {( P1 W2 j' a m9 x- P3 T b* E+ e A 7 e: C$ e$ w, T7 u" e$ p! {6 R( {a $ |( n# H. Y" D9 C' g5 C- U3 Um! h, Q; J: @, W$ w/ v' u# j) c o / V# _4 Q) C" q; H* \" Qby using bleed air to draw ambient air through the$ u/ _6 ]# @! e& \; ` sensor when the airplane is not moving.. |- e! Q+ J) |8 a5 t8 ]' y A& J9 M% j, u. C4 b or unit.( H4 G k: g3 Z5 h% Y7 _8 w" V2 i A% T3 I/ e2 T6 v" G lower thrust obtained by setting a higher than actual) ~$ r0 N, ^. @1 e$ Q, L# _ Outside Air Temperature (OAT).$ y0 @ R6 w5 f 弧线,& f; u8 c6 q" \6 J' K# Q* Y1 N' p 飞机在围绕DME台等距飞行时的弧形航迹。' D: K8 F v# h# b# D A1 Y) P% C 区域导航,, k7 j% p3 I) `2 x0 n( I 容许飞机飞行在有电台参考的导航信号或自备系统能 4 l" w- y* u5 w1 x力极限范围内,飞行任何预定航线的一种导航方法。 1 D! r7 A4 B! i1 |0 m模拟感觉: h8 r" m' ?" [) f# W9 u+ \6 f 在飞行操纵系统或刹车+ K1 x3 r) ]6 f# L" {2 M( }8 _, x# r 吸气式总温探# G$ _& r) E" r# J& k9 `7 w. v! [! C) i/ F# y- }7 N" i: ^' g8 x" q* I1 q& w; K# V% H6 i/ ~) \组合成% n& O/ f0 v. a+ |& w6 S/ C, ^! M: j 在选择起飞0 }3 q& }, F% o! _- K, ]" V 度高的温度而得到的推力。用这种方法可以减少发动机的& k$ Q0 V& d7 g/ L# d. m 磨损和维护费用。 ) A, u3 P9 E4 j, q" z# G& q- O7 n$ y& w 英汉对照民用航空词典B OEING . u4 H, E/ e* l2 p; H% n, NTECHNICAL DICTIONARY 14' ]! v4 q6 y( v! t" n ATE, SEE - AUTOMATIC TEST EQUIPMENT `) r9 V" v2 M8 `2 Y" D" b. JATMOSPHERIC PRESSURE, Pressure of air due to the' Q+ @9 @2 y. j3 Q5 u6 [8 T# S arth's atmosphere, expressed in pounds per square . I+ z# S0 Q! m [& kch (psi) or inches of mercury (in Hg) or millibars (mB). 8 a! m& o1 i2 u4 X8 HTTITUDE, The relative orientation of the airplane with J; `: |" F: `) p1 yspect to pitch, roll, and yaw.* w. L0 }" b c2 c2 l( j+ R$ C$ h UDIO CONTROUSELECTOR PANEL, The panel in9 F3 |4 A7 y" y+ n8 o7 Y e airplane which controls and selects the routing of4 ~! t+ c X- ~9 B udio. 9 ~* W% M% N7 p. J0 B+ \UTOLAND, Automatic landing using the Digital Flight / |+ ^+ z. r/ U9 F$ Z \; sontrol System. 2 I2 ^ ~' P: L) an. . u/ `# J" J5 ZM, A system4 s+ i: J6 H- T; A2 b( { omposed of all necessary subsystems needed to guide $ U' d$ |: q0 Ie flight of an airplane.4 V' N& L- h" {. e3 v8 L( M EQUIPMENT, System test* S' S% s! z6 f1 u: T3 Y& i quipment that operates under computer control. / i: Z9 g X: a5 I装置,

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e& w8 I6 H2 ]3 f( ^8 V0 ` j in ) g) l" ~& U) b3 g+ b1 S0 r' O2 aA+ }- o0 V! J% J5 H5 ` re 7 x' c' T7 b& }- J/ X0 L( WA 6 ~: G6 R1 T2 w0 ]1 b- Nth ' l9 J& Q+ N, w7 ua, O7 D* }4 R5 S, B, B( o. J A1 i2 ~# U1 E& T, T8 C! z- Z* C C' L: J K( B/ t AUTOMATIC DIRECTION FINDER, A system which , e f5 q8 w/ k: }determines the direction of a radio statio* R- ] C5 r2 Q$ `' c AUTOMATIC FLIGHT CONTROL SYSTE, d7 e1 f6 L: t- O& e- s c - M5 P8 [$ y) _ a* Sth ' B) u# C3 |+ s* h8 wAUTOMATIC TEST+ Q+ _% P% X) _( z3 H) D e 8 p1 P3 O! J% D% {1 Q, W" o自动测试0 J. v$ ?- C. g$ S 见Automatic Test Equipment. ) k* Q+ ]7 O; J' ?5 G) V+ e大气压力,1 P% w! W, \3 z! L- B1 c& L 由于地球周围的大气而产生的空气压力,以每平方寸多 9 d/ ?/ q$ N) E3 t6 R6 b+ z磅(psi)或多少寸高水银柱(in Hg)或毫巴(mB)来& Q3 c! I5 f1 z& v% | 示。 1 D9 Z$ q) m- E2 e+ a) g3 I飞机姿态,1 _+ Q+ L* Q! ?5 c$ M8 w 飞机与俯仰,坡度,和偏航有关的相对方向。9 Q k& o: z' V6 r( t2 F2 F7 Y( x% s. G 音频选择面板,1 T1 D6 k; T) x1 Y 飞机内用来控制和选择音频通路的面板。 ( R$ q* }$ Y0 S, r$ D0 q自动着陆,5 H6 l4 T+ h3 U6 ~, p 使用数字式飞行操作系统来进行自动着陆。 5 d$ i; Q7 a. O+ Y& d; L% Z的系统。 ; I5 ~8 j# j7 \+ H# d- `; g9 v9 O* Q7 E. {- K2 }6 r 系统所组成的一个系统。8 }" V3 D, i) K 在计算机控制下运作的系统测试装置。2 X9 s, Q0 g# k( T! Q6 f- N. q+ I; t& d1 b0 v' y$ q4 A: k9 c0 U7 t$ v% j5 q2 J 自动定向仪(ADF),+ q. Y+ d% c2 [4 H) `* y: G1 H* t+ K 确定无线电台方向 + `2 \) v% l, c自动飞行控制系统 2 u5 r- j6 {" O7 G4 p4 S5 R1 M由所有能引导飞机飞行的子 5 e# Q" ?) J& l自动测试装置,% P6 o; \# ~* `2 p. e# Y 英汉对照民用航空词典B OEING 4 i$ F' o, `) K C0 |) p" N PTECHNICAL DICTIONARY 15 ! G9 D8 O e% d Z& f+ e. L P) HAUTOPILOT, A system which automatically controls9 |/ L4 L: V9 B6 k- X7 E K* a and guides the flight of an airplane. ) O- J) V8 M( j* qAUTOPILOT FLIGHT DIRECTOR SYSTEM, An; ]( E7 H" y, O5 {' g tor 0 ?) c0 j& t$ P6 rUTOTHROTTLE, A system which automatically " @* Y0 }) `& G5 B1 O3 G) j+ bontrols the throttles of an airplane. * B! _8 B% W9 V _- U" `2 GPOWER UNIT, A small turbine engine in& ?- Q5 F. s! T5 T e airplane for supplying electrical and pneumatic & u* |1 @! V5 q; C1 [ower for systems operation on the ground or in flight.. b7 W1 ]# [$ I! b! ^- R VM, SEE - AIRBORNE VIBRATION MONITOR 7 q7 U5 `! l2 W2 s. dXIAL FLOW COMPRESSOR, A type of compressor ' g, \7 }, m! I, M0 gsed in a gas turbine engine in which air passes through # D4 b0 L. A. ?5 Z% `, |XIS, An imaginary straight line or an actual physical 4 _3 } y- O3 z6 somponent (such as an axle) around which a body can / s/ ?6 w2 s5 f$ rtate./ t+ f0 r; S' K. \8 K. r 仪,2 Q) t2 W' \+ @6 p3 }6 \$ m+ c; o9 d6 e' c4 s# o C) W 自动驾驶飞行指引系统, & R. v$ I3 E3 d# n8 ]动驾驶和飞行指引功能的系统。 * Z- y( M4 c( L- V动油门, : W: v7 Q4 |" B1 i- x0 l9 R自动控制飞机油门的系统。 5 r4 }$ \9 x$ I0 i9 J是飞机内的小涡轮发动机,在地面或空中给各系统提供 9 V" [: t+ k, ?3 a4 ~源和气源。8 O3 P7 K9 z( E3 d# p ~$ x 称。/ L& O6 F& u( j Y u' I 载振动监视器, * c1 j9 m) e4 Y1 @! g见Airborne Vibration Monitor 6 S' |; j- X- w- O8 r9 b; Aintegrated system containing autopilot and flight direc 6 j3 ~) e! n& l! C' [functions.+ B, P% A; e1 u+ C: \ A 6 D9 f! S1 T, `: e! y* oc # _2 w, z% ^0 t4 k0 V/ b1 {6 D( @; mAUXILIARY " F5 [9 U6 C2 |6 O2 e# h- pth$ `# N2 f; b4 d# x1 J) @. t* k5 T p, x- f! K; c7 E" K AVIONICS, An acronym designating the field of aviation 8 J% A4 u* z% o* M3 Jelectronics.; J( L/ z* S* v) c/ h/ R A6 [& F7 X0 ^/ b. W: V A ; p0 n" i' L0 d+ B# Uu+ h3 n2 c, Z9 \" l8 z" J the compressor in a straight flow, front to rear.7 k! Z/ {: }1 c' J6 U4 Q7 e; l3 u A ' z8 v% e$ s: P# N6 ~3 ec; K' `, X7 N5 ]# ]9 G8 W ro * Z# f+ X" m& V5 _; Z) W4 J自动驾驶 & Y" s$ ^+ A% a9 Q5 \动操纵和引导飞机飞行的系统。3 o3 x4 [; K( m+ ` ~ 一个综合自 " Q' k* a# Z6 ^* [0 c O% u( B3 _" ~' ~辅助动力装置,& R% O* H$ Y6 s( B8 C& R/ t, E/ r* i航空电子学,7 S7 V# {5 e: N0 U5 @ 是航空电子领域的一特有名 ) i G- l4 _$ u$ H( u$ k1 Y- m2 h( p* q( Z# ~! k: n. ]9 ]) G; P0 z2 o0 m# o流压缩机,8 A! T2 t: J/ g+ K 一种用于燃气涡轮发动机内的压气机。空气由发动机的1 \$ a: f2 x% m4 {2 i( ~ 部流出。' `$ g" @- Z6 P) c# Q 线,& @5 @/ b4 Y+ g/ H1 e5 P' U3 t* K- E 可让物体围绕着作旋转运动的一个想像的直线或实际0 i Q0 @) R' F4 G2 L- I; | 在的部件(如轴)。 4 \! l8 f8 P/ M7 ]5 _# m9 q. a& p' t+ }$ I {# W) \) G) Q. c前部轴向流人,压缩后,由后, x p4 R: j2 Q3 B% g' `8 c+ a5 t' X4 D1 e X: p9 N( i8 J% B- U英汉对照民用航空词典B OEING # \# _# I3 P M7 O& i9 HTECHNICAL DICTIONARY 16 . E; i, a) T& e$ x1 dB% s/ v3 t; b" {: e ACKCOURSE APPROACH, An approach to a runway 8 f2 X' R8 t% _) T0 r' Pversed. , c" V) b! P$ zown on the EFIS that 2 \6 d" ?4 O8 h8 V% S, ?" koes not readily change, for example, navigational aids. ! q5 v! K; x: C9 V4 W6 |vement in the tank or reservoir.. u6 ^6 L5 B4 l( v: A ALANCE TAB, A small hinged moveable part on the2 D6 v2 k( F. Q6 A8 L ailing edge of a control surface (aileron, elevator, * k& V2 a+ M! L航道进近,; ` V9 z4 W9 O9 ~ 相反的进近方向。当反航道进近时,无下滑 w: n. |: W) v* C1 ^& G+ |$ }' y 显示在电子飞行仪表系统上不经常改变的数据。例如:2 [4 d9 {* B" N/ N ]6 F8 r 航设备。 U8 u6 H' M" v6 V在燃油箱或滑油箱内阻止液体流动的隔板。7 t! E6 i& i; P 动补偿片, ; U d6 @% E6 j3 t铰接在操纵面后缘(副翼,方向舵,升降舵)的可动部。 7 N. b9 _3 J. J" F与操纵面相反,以帮助操纵面运2 m0 z# x7 k \ B 2 @- ^; @; }" |% swhich is opposite the normal approach. For a 8 `' i4 N$ Y: t6 Mbackcourse approach, glide slope signals are not 4 f9 N, O; r# x( c, H8 aavailable and the sense of localizer signals must be ) F& z3 o x3 h& j3 N% ]re . W' ~6 \" {, yBACKGROUND DATA, Data sh $ h0 \5 R7 g" E: [$ A# |d" o2 {3 c0 a( y BAFFLE, A partition in a tank or reservoir to prevent ' F% u7 E9 K. k/ A+ L6 Yfluid mo ' h$ z; Z& F- k6 k, ^B + D# D' J& v% C7 N. y. t' mtr0 l: g4 J3 z5 I5 d) q' H. y( c rudder).The tab moves in an opposite direction to the ) o0 Z/ @( H7 C% C; l+ |0 |control surface for assisting movement of the control* d$ R2 `2 f7 W, g7 P5 p. Y) N8 h surface. : O4 u% g* S* [* _2 _8 {: h& w$ `6 i9 B与正常进近( ^( ^; S3 g5 Q 道信号并且航道信号也必须逆反。 ) z% d- Y. [+ B3 b' Y背景数据,6 W. J7 ?8 p5 b! w! P7 y; k$ j; h( u缓冲隔板,* S1 q4 U" s* @1 p% h+ E+ @2 c' ]! B+ q3 D5 F1 ^! y随动补偿片的动作方向% r& g+ o, W4 x! z/ c 动,减小操纵力。+ { O! H! o* g7 X 英汉对照民用航空词典B OEING6 g/ h) g* t6 ^* e' U; L TECHNICAL DICTIONARY 178 L0 ^0 O: i$ L BALANCED FIELD LENGTH, The field length. q; v8 ]' l c- X5 y/ L associated with optimum aircraft performance when 2 K, E4 Y; ~$ \$ e! dbstacles are not a constraint. In this case, after engine 0 J$ n# O* p/ ~7 p1 Uilure at V1, the distance required to accelerate, takeoff 1 S' b/ C; x ~7 C6 l# V# rnd reach a height of 35 feet is equal to the distance 0 w( }: A4 ~' @5 xALLAST, A weight installed in an aircraft to maintain 8 q9 |" q" q- p& VALL NUT, A fixed spherical nut driven by the( |2 K8 M: j: q4 ?: B1 f AR OUT OF VIEW, A signal used to remove the flight ! Z ~% d& {- ?; ^8 f6 f EAROMETRIC PRESSURE, The pressure of air above 2 e; E8 d4 I% C9 l- J8 rg) or 3 z5 o& c" j0 ~# B8 ?7 f+ Mmillibars (MB). + Q$ W: ?- u ^5 O( E$ YATTERY, An electrical device for changing stored& e* X3 q; O: A U- A& |" p3 I 性能的场长。在此 - x7 W1 s; E1 D- _2 a2 q9 i5 B况下,V1时发动机故障,要完成加速、起飞、离地35 ! Z$ U. _$ C ]: }/ m尺所需距离等于相同速度下完成全停所需的距离。 ' t2 t; Z0 G6 R2 A% p j舱物, ; m6 @1 y% Y% o# V重心在许可范围内面装载的配重物。 * z. y y+ [8 q, L0 o) y8 ?) P, m形螺母, ! q& \8 T$ M' c$ `, m& z# |的固定的球形螺母,用以使襟翼和水平- |9 q3 e% b4 O# o, W- W% n- p 引杆消失, y) z0 k6 x& {" u' z6 [指引杆的信号。& W! p# ?7 ^5 v' T$ O$ U& d 压,. h; T' D h# t/ E7 b& B, G& O/ Y 压力。通常以多少寸高水银柱(in; h8 r! t2 f g# B- k 瓶, " v! x) y. S4 M& k+ d/ R2 H的化学能转变为直流电的电气装置。 9 t4 N+ s, g, {% F$ Go ) v5 v! S" y1 h3 h: m" S& ?+ @9 G ~( ~( \fa! E) |5 N0 x9 Z! x4 @ a3 f/ N9 {. T& |1 l* T required to stop from the same speed. / ~, N( R8 H m! g. D- M# k. x, oB 0 c0 O9 z2 R2 j6 _* t! x4 \! Ythe center of gravity within allowable limits.8 R( L( i P7 i- L2 m B " s" i$ \2 ^% ^jackscrew for flap and stabilizer movement.' D* _4 @, r& d( {1 x0 [2 s0 ^2 {. T, n B ) r k$ x# R7 Edirector command bar(s). 0 g/ `( s" q" E* o: G. dB - X; V# p' i/ V! c7 Dzero pressure measured in inches of mercury (in H 3 Y; v% k4 j; u6 m. [7 {in" T4 O/ }3 O. r7 I9 u. {6 L0 | BASE METAL, The underlining metal to which alloying7 ~3 V' i( E& X* ?8 p8 y agents or metals are added. 2 ]; d$ z5 m7 `3 X- U1 YB ~) K" \" Y8 v6 a" Achemical energy into direct electric current.$ E6 w3 |+ U" F7 V 平衡场长, ( z' P0 e7 N( D) N) L0 l v1 A3 Y当障碍物非限制因素使飞机达到最佳7 w+ |5 Q: Q% p6 E% } @8 Y8 J. e$ e3 x& _3 R/ J3 A6 p3 W& n0 T1 x5 r7 w; \2 }- f9 J. l, w- G+ t: Y" u6 F7 B& X' a为保持飞机# d1 r# }" c2 c: C, y& ?- V% z+ N3 j9 l. y; b由粗重螺杆驱动 + E1 X& \( u$ H7 O2 L/ Y安定面运动。 ( t5 F0 ]$ t4 y% N+ e- p3 Q( R% T! K( Q |- x; q. S 用于除去飞行 7 j% ~& b" Z: i8 f! e3 v# Y7 h; `7 F; A- I" S t" n零压力以上的空气 % C& J1 z. d2 L- xHg)或毫巴(MB)来表示。 8 f4 x1 C7 l% m5 ]基底金属,2 a4 W9 h( Q3 A7 ^& F 指合金中的主要金属成份。 " E& l6 z% a! m2 f# t3 X/ r2 [2 R; B0 O9 R2 I* S$ B# _ H( i8 w 将储蓄 * Z0 p* `. p" E; h英汉对照民用航空词典B OEING 0 @) F1 X( D; m/ X; ]5 uTECHNICAL DICTIONARY 18- z. ?. w7 _% W8 O! \: s7 I BATTER( W5 t% S4 _$ A* S& [: b direct cu Z: B5 a7 \, h4 I" A! S% U: Rpower su 7 n# [3 p. q. W' j" J3 o. e$ [9 r( AY BUS, An electrical conductor supplied with9 h6 V5 W$ h0 B" c" w' }5 p rrent from the battery or transformer-rectifier for / d4 h' N* S! ~2 t: ^1 I, Lpply to operating components.+ K0 k9 N# O0 f, R: _ CHARGER, An electrical device supplied - v9 [ N# R( ?( @0 C" bith alternating current, which produces a direct current 8 R4 Y1 K3 v- w. f! c1 l1 H: [utput for charging the battery on the airplane.% J5 u& g& l/ i9 `9 T; f; J AY, A compartment in the airplane structure.- l7 Q! q9 e, l5 r: V! K( a7 L, s CD, SEE - BINARY CODED DECIMAL1 `$ f4 s q, \! K# @- l EACON, A device which emits a signal for use as a - E* ^1 J) U" T3 l, t. J1 }uidance or warning aid. . E+ M/ C S( m: \& k; [BEARING (NO. 2), The direction from an airplane to a 0 X2 f* E" F4 h: V/ L/ t& @ground station. * @: u; {8 U8 T& I7 z! A N1 a- y瓶汇流条, 1 K, A6 \3 Z5 a6 j; z9 R" z4 f5 C将从电瓶或变压整流器来的直流电供给工作部件的导 ! c7 n, u/ m0 [4 p1 M; S; ^体。 & j2 t, Z. |/ c% W5 x( e) J# W瓶充电器, D1 [3 j, _$ I( S" y* b6 X. C 用交流电向飞机内电瓶充电的电气装置。带有交流电的1 `' k$ e- f3 I+ S# } 气装置,该装置产生直流电向飞机上的电瓶充电。3 E3 i# E$ H* ^/ _ 舱,6 g4 x0 J9 e* q 飞机结构中分隔的空间。 + \: v4 w8 |) n" C$ W0 y1 d7 a二进制编码,/ i; k8 ~% X9 l+ B, Q- |8 a$ s 见Binary Coded Decimal- M4 p% m4 t0 b* v1 w# N BATTERY% T3 V: a( f0 a w s4 g% e5 a( \o2 B) G3 g& M# c1 c& R4 x6 Y; H( B B, D# o5 y% g1 l2 g' R$ M, H% O B 1 L* X& G8 I# PB 7 O$ m4 E* d' B. E* ]g- m; X2 W( d7 @! m$ y. S' E BEARING (NO. 1), A surface that supports a moving * _0 Y: \" e1 }part and reduces friction between the two. - v. i0 P0 [" W; M3 C& a) B4 \1 @; ?( N( Z1 u' S# r5 d/ {9 v9 b4 [! h; f; R! X# w" b9 u& n) p8 Y$ s3 V5 U% I% T; u' h( Q, i; I4 x6 m( D1 T4 ^9 g3 {4 x" k& }( @ k& E 信标,8 P2 e, J+ W4 H" x 发射引导或警告用信号的装置。 0 q" I8 S+ ~1 U3 }+ S8 G: A/ h方位(NO.2),! m$ O- U4 H! L+ _. A: A 从一架飞机到地面台的方向。; l7 s/ k6 U/ }' p 轴承(NO.1),/ f. ^! B& [" X+ X 用于减轻机械转动磨擦的机械装置。, x0 R" d/ m6 h$ { 英汉对照民用航空词典B OEING% a! f: z6 z/ C: @2 S TECHNICAL DICTIONARY 19: f7 O% a: f) ?5 T BELLCRANK, A double lever in the control syst- C; m( T G* B h) n& x changing direction of motion. ; Y+ |9 H4 {+ t" f# e/ E$ S# i9 K- w+ Eem for 6 F! P6 f: s8 _ F1 H4 Fct in the ( h/ @5 y) Y. R! U/ k- l& hneumatic system for absorbing expansion of duct due 3 |: V* s+ Z5 Z, c3 Hheat.- {& X5 ?/ `/ X1 n0 j \ ELLOWS (NO. 2), Corrugated folded or pleated / A# W# b* E9 _8 z4 s7 o, \ontainer or compartment used to measure pressure. " W' Q' l9 J" ^$ p0 V7 aEZEL, The part of an instrument case for locking the 7 m$ K5 U' ?4 @* Z& p0 Q/ Rlass.6 s$ Z5 m% C9 P IAS, The potential difference applied between two - e" t5 f9 r* O# L K7 Xoints for controlling a circuit. 9 r1 y6 [: y5 \1 z- F5 ^) _BILGE, The lowest part of an aircraft fuselage. A place# j7 S) r' z, S3 _5 J; A: x/ u where water, dirt and other contaminants collect.4 T2 {/ W2 m- U0 D- r) ]- b4 T 气源系统内提供管道热胀冷缩所需要的余地的波状 * ~+ x5 Y' X V2 p0 W轫管。8 n( T5 L4 o; [& b0 n) ^8 p 空膜盒,. @; t8 W7 |+ Y# N6 B+ j 一种具有波状表面的容器。用于量测气压。& l% t, S7 ^. x 嵌沟缘,5 z6 k. L( i1 \ 将表面玻璃固定在仪表上的圈状零件。" ^1 [6 J5 Q: z2 O 压,# w& |* j. b& S( h6 C7 E) S 在控制电路的两点之间的电位差。- Y$ T! t. w' S7 {3 K 机身腹部, : q# B2 A% v$ z2 ~机身的最底部,通常水,脏物,和其他外来物集存于此。' {9 U* A" j& e0 U! ^ BELLOWS (NO. 1), A corrugated flexible du X0 C5 {$ h+ ~9 {) h p: G" t1 b: D0 j; ?5 k' g, | to 4 p8 Q' `- T* s* IB " u) B" ]% R: I3 E( Ec * b- f0 X8 Z7 X1 U& Q7 c( MB5 G+ v# t4 u6 D) `$ ?5 U g 4 q: D; f0 f1 V2 kB 2 o! M: f4 N- U2 [p I/ D1 X$ ^4 e* w6 e直角摇臂," d: S$ [; |2 c- N7 X# m: k- K1 _ 在操纵系统中改变运动方向用的双臂摇臂。+ m% o7 h* {/ }/ Q* g$ q 波纹管,! G6 m. N2 u9 i0 r- d2 z, u7 s6 H: x ]$ W& ~- T5 \9 D4 B# e* \4 ~, G( T; J5 S- \' s5 f7 |5 s" d1 N3 p4 @! \5 L2 t, y2 ?4 ], u1 u: \2 ^: \: A英汉对照民用航空词典B OEING* A9 H3 [& r2 h/ g8 H+ ?" Q TECHNICAL DICTIONARY 20 ( B, Q2 p) F+ ^* D5 NBINARY CODED DECIMAL, A system of coding each 6 u% E, x5 y0 xdigit in a decimal number using the binary equivalent. ; @* Y/ u2 a) p0 I- u" u; hBINARY NUMBER SYSTEM, A number system using " K3 u& M" n' k$ I/ H. Ws: Q5 U' ^6 K% x0 p' x2 u IT, In the binary number system, the smallest unit of P. h, d3 _ t0 sformation, consisting of a 0 or a 1. 0 s; W& K. p7 r$ s( D5 A# OITE, SEE - BUILT-IN TEST EQUIPMENT h2 O9 s ~) n, N% N# U" G LANK DISPLAY, A display that does not have any# _/ x1 o6 n5 a6 b) a6 w1 h+ R5 t dications, normally due to failure.5 W' ?8 _9 S' G& T' \1 K, Q LACK BOX, A container for electronic circuits to record ) |# p& E9 F' M, N. n9 E5 Xight data.5 s2 V( H2 E0 ~! h3 C2 s. \) k LEED AIR, Air taken from the engine to power various, c* r! w/ Q) U/ {0 L6 u( {! J1 | ircraft accessories.( W' @5 r6 o H, M: V2 U% `4 _. L A valve in the pneumatic system for air; D; U" W3 {# H2 S" i. [" n( M supply from the engine or auxiliary power unit to the ! k+ N6 O; ?4 i; L1 ?pneumatic manifold. A valve on the engine for reducing $ z( t" u9 I/ N$ z3 Apressure in the compressor section.$ ~2 ?! E' ^+ Z5 f& O 进制,1 G+ E3 ^6 N7 F) V% ` 进制,5 i' J: x5 T1 h: q8 Z 一般用0和1)和2为底的数字系统。& s8 x5 u; v5 \7 X. d 特(二进位数), / Y1 V. j v, E3 F0 q; h/ w二进制中的最小信息单位,包括0或1。( }- ?. ?- I, A0 d( C" ^ 内自测系统, 8 ?- q& H8 X" X4 O( Z! I: v见Built-in Test Equipment, v( }- k$ c. n two symbols (usually denoted 0 and 1) and having 2 a- r: V/ P" _1 ]6 w, l2 B% W its base. $ ~ V& t7 L, [$ oB ( Q9 X! k9 E2 }1 _1 ~% b; Y* Win5 N- H3 y( V% Q% t/ @/ k B t, J: E& A- h1 ~9 e B 8 j. L" a1 c+ R- T4 Q1 Nin 1 A ]4 h6 J6 X8 `B" k+ t! n0 E# R0 ?; E fl9 s# z- _3 `; \/ [ B ' }1 k% y! w( A( ]1 Ma , c7 O' p4 |1 pBLEED VALVE, & w7 X* U8 o2 v6 a+ r5 u- f二进制编码的十+ ^0 d. Y: K4 Q$ U. J [ 一种编码系统。用等效二进制位数编译十进位数的每一3 `1 e6 Z% Z( ], M& i9 f 位。 , ~. r/ L4 {5 Y( i) g" T1 N- G- f3 B7 V& t5 i' ?, k以两个符号(" z1 {% Y: B8 E0 g1 I! p, ~3 F4 N$ j; q$ ?% S: X( o# W2 S.( X ]$ e7 a0 i( m6 X: `7 J8 L 白显示,4 P; x6 p) a- V 通常因故障而造成的显示器上没有任何指示。 $ }; I& p& I+ m匣子,0 O/ k: C8 r$ ]: i7 N 装有用于记录飞行数据的电路系统的容器。( Q4 j$ m9 [( v& h/ [$ v( X4 f 气,& i" x1 J& h& S8 z5 ]6 I 取自发动机而用以驱动飞机上之各种附件的空气。 9 F' u$ A' A+ N4 K% W气源系统内,使来自发动机或辅助动力装置的空气进人 " H8 m O0 s9 o% l" ^气源支管的活门。发动机上,用来降低压气机压力的活门。. s* [6 f3 P' ^' \- f0 K8 `# M5 ?. F" X0 V W$ G6 P; ?8 j& R6 w. {0 n0 T- x1 J. t8 L4 O4 ^6 }8 [9 F& I( R/ [& Q7 x1 b5 w引气活门,! a5 R# O* V6 d/ G: S 英汉对照民用航空词典B OEING 7 g. @, u# N* s8 K1 yTECHNICAL DICTIONARY 21 ) k/ s: Z2 e6 l) w" @% G1 E! \BLOCKER DOOR, A device on the engine for blocking& C9 x+ p$ t$ ~ H" @2 b1 g! h the normal airflow during thrust reverser operation.' ^+ O7 E) Y* I+ D" @8 [* b/ j LOWER, An electrically operated fan for circulating air.9 e! B& h3 y! Z3 |2 ?$ l LOWOUT PANEL, A panel in the structure between - @8 p3 n2 K2 Eo compartments that opens to equalize pressure in3 i3 C/ n/ Y5 P1 @+ ~5 W e compartments.1 L* }* ?) ~; C2 U ODY GEAR, The landing gear attached to the 7 @, P8 \! Q% n/ hgrounding.0 a2 t0 {! k' p4 `- T/ X 正常的 8 Y. n' i2 H$ Y气流。 & ?# f1 L8 A$ \% ~1 p6 D3 j鼓风机,9 s: O! k3 @' d# @; R7 S- L 用来使空气循环的电动风扇。7 T# ~2 X3 M0 E; S 压口盖,' J2 O+ Y4 Y9 n* V6 {& W 两个隔舱之间的口盖,打开后可使两舱压力相等。 8 D, O3 d1 v- {9 ~! G5 a身起落架,' f7 H$ D- E" k M& v 身构架上的起落架。 ( U1 i# R: K: |' \$ t; I* }B 2 L5 j/ b# P+ |2 n J- ~B) M; w7 ^: B# ~$ n( x; s tw1 k, q1 h1 h5 r. K9 o3 a& c th8 @& O( ~, [& f. p M! X B/ \# X Q4 C: G- d9 Q fuselage structure. 3 L+ O# q( U2 L2 t8 _2 cBONDING JUMPER, An electrical connection between + k) f4 z# z/ f" R/ l w; xa component and airplane structure for electrical1 E' e: e) E9 L$ n* }$ E 阻流门, + |1 p" B' {8 H' _6 W# c发动机上的一个装置。在反推工作时用于阻挡 ' `3 g3 K0 j" j1 ], T. @7 f% j0 v/ M# s F2 D6 F% o6 x) \1 v, [3 M" o装在机9 I* m6 s0 z9 n7 r0 D4 q G0 d 搭接片,) V- H) o/ G9 S# ]4 c 连接某个部件与飞机结构以形成接地的电接头。 3 E: N1 D) W) s英汉对照民用航空词典B OEING - c9 }" |: F' b* \. R7 K% Y0 `1 t; ] WTECHNICAL DICTIONARY 22 5 l1 ~2 K2 E; kBOOLEAN ALGEBRA, A mathematical system for0 j' s6 `6 R6 p# ~ writing combinations of logical statements. $ d S0 @' q$ n% E) c2 {5 \BOOST PUMP, An electrically operated fuel pump for % `' T4 K: I. \$ y) Kfuel supply from the airplane fuel tank to the fuel( r5 T% v9 @7 Y6 y" l manifold.2 K! d+ W! A0 x BORESCOPE, An electro-optical device for looking at 6 O4 c! o5 ~% j9 f& K7 Fternal parts of an engine through holes in the engine.2 o6 W. K0 r0 E. L4 d/ R orescope ports) ! T/ s- N; |9 o- GOURDON TUBE, A curved flat tube in a pressure gage + J7 \- z. y6 O1 h) Z* _8 xr moving the pointer when pressure changes inside % H/ R. C& |8 [8 d" X! Ron the ability of the brakes to/ p/ y' M# ?9 [, L; _& x bsorb a predetermined amount of energy during a% J; i x; J4 ?& U jected takeoff. 0 V9 w8 x% @2 T& G$ R用于通过发动机内的孔(孔探口)观察发动机内部件的 ! e3 ?" `! v, R3 i! O$ l光设备。& _9 h* O% p! l9 p$ Q @( |9 } 端管,' m& W+ q2 y0 V4 \8 X 测压计内的弯曲扁管,管内压力的变化时它使指针移 + m$ j% J/ t, N0 k3 ^- o力。 8 u/ k# k$ u( Y9 ]极限重量,) i( w0 d Y( r. n. c/ x- k/ O5 |, \, M) \% L6 u起飞重量。 + b6 x3 A. a: w7 U, f* A发动机滑油系统与大气相通的通气口。 & W# r- P% s, r! [0 O6 C" U( Ein# I' {9 s+ D+ o (b+ S+ u: A9 u: l# r# J. k B 9 J" E# }/ x/ W, G8 O- m1 h6 Ffo : b9 M1 h. W4 P5 ythe tube.5 S8 ^5 y# a# m8 G+ A4 R- | BRACKET, To enclose or surround.9 w5 p& A, y1 R: e5 j% ~8 c BRAKE ENERGY LIMIT WEIGHT, The maximum + E% N0 R! n" C; U, c5 X" jtakeoff weight based ' ^- n" k8 j8 u+ g' ra# h# b7 U( \0 ?+ [' _) N: k6 E re 7 z. @& {% a+ B7 Q+ H8 BBREATHER, A vent to ambient of the engine oil system.5 {0 }# u/ g- p, Z& y 布尔代数, 7 X( k7 _" ?7 i+ {一种用于编写复合逻辑命题的数学系统。4 Q( O% k; e3 K' F! i* C3 D0 X 增压泵, " Z$ t5 J7 K2 S3 d5 j5 ~从飞机油箱向总油管提供燃油的电动泵。 ; @1 F8 Z3 ]; I. x" R# e: z2 q孔探仪, % B' L+ a; f' G% V+ Y6 e9 z4 i- ?; {: E/ }) i ?3 S K% E6 r q1 R6 t, D. B" M动,以指示压1 O7 y# R9 v6 e3 }% o 托架,+ e2 }" @/ j7 c4 b 用于作支撑、装托、或围绕之用。 7 D% b% y2 D9 t1 l" }' A M刹车能量4 u1 H% T/ g5 ~5 s3 j 中断起飞过程中,取决于刹车吸收预定能量之能力的) B! l' M4 E! P5 A+ H0 O& j" A, u% K9 G3 y9 B" u+ ]; V0 J$ Y6 S2 N* X通气装置,- S( U T, \ o1 x4 y% C 英汉对照民用航空词典B OEING$ P) O8 e( G) S" n TECHNICAL DICTIONARY 23 6 }3 U6 S9 w9 E! z5 y6 ]9 [) lBUFFET, Vibration of the wings and airframe resulting ( c% C/ c0 x) Z3 b6 ifrom unsteady airflow over the wing; caused when 3 d2 q5 Z3 z; e! _, L, Fairspeed is too slow, the bank angle is too steep, or+ Q' e$ R8 R) I" [% ` irspeed is too fast. & ]$ n0 e* Z/ T8 g v* h, a0 tUILT-IN TEST EQUIPMENT, Equipment installed on B8 t) \6 a! ?; G e airplane and in airplane systems to test the systems 7 s4 _' g6 I! v, g! ~' z' f$ E3 ^* {ithout external test equipment. y' I7 B$ o S T T UFFET MARGIN, The amount of residual maneuver% @" [* Z b. w) t apability present before the onset of buffet. . e$ v0 E1 V! F9 C! i/ w* G ~( ]UG SPEED, A preselecteed speed to be observed. Y6 n) R. z+ ^' v; I' g nding sequence. 5 {$ z/ D2 X- q" c; lk# Z- U! w, V. l! D7 I0 F2 k! C ng landing gear operation. ; Q& c/ c2 J. z* _; U/ K: R* [3 G2 f速度太慢或太快,坡度太大,均会引起抖振。& e3 k2 C5 o) x- d: B7 s8 \ 自检设备,+ Q: a" `, m# f* u 安装在飞机和飞机系统中,在无外接检测设备情况下, / o* n- X: x3 L用于检测系统的设备。4 G& S. D6 m: s- I2 A$ }5 Y4 c1 T 抖振裕度,3 Z# v" Z \! Z: n9 z 飞机在遭遇抖振之前,剩余机动能力的大小。 $ Z( H5 x# U9 F, z! I. R) w标速度, 0 K9 F* c, g! M! U+ d7 c) ~4 t在某些机动飞行过程中,特别是在进近和着陆时,飞机; z. ^2 @6 l+ ?) @" |: _- l& [/ S 预定速度。' m, z+ G' ]& l3 w 力装置, 2 n8 H9 V, o3 e架工作的一种机械设备(弹簧或减震器)。 # G: t; I: A6 l; A, l6 c* ~流条,6 \) g0 C4 i) N: H& T5 o 在部件或组件之间传输电、数据、或定时的单一电线或 ! s$ s: S/ J6 a& Va 4 e3 R' p4 b1 B. v; T8 u' GB $ b% W U# G8 |8 Ath- F2 j" x" H! U" m w2 j& I, a4 c" p# @9 L B$ d; h& w# ]" F c) Z- N, B5 n* `2 j' j/ U6 A1 e B * c/ N _7 }; [% Q" N* M gduring certain maneuvers, particularly the approach and ; I& o) k, M# Y; t: K8 x- Gla3 i7 i6 c1 E' k0 [6 ?3 t' m BULKHEAD, A structural partition in the fuselage or: i6 o' D0 `: T$ F* A. a9 ~ wing.* v1 }7 z7 _# `) }5 {# F$ u4 j BUNGEE, A mechanical device (spring or a shoc ) G1 u Z6 D1 ?% H# Y, w1 jabsorber) for assisti 3 j& Z! n$ U7 I- A9 S0 N; Y- r! `BUS, A single wire or group of wires which transfers9 o3 X; A, q0 z; r! F: U power, data, or timing between several units or: m* x+ U2 z, P6 h" L9 u1 ?4 d modules. 6 @! J$ a! Y: |% \7 J抖振, : h) n4 X# ]8 h$ g$ o) |" r) [由于机翼上表面的不稳定气流引起的机翼和机体的振 ) i" h: _0 ~' {9 n, D. V动。飞行 6 P6 b: I; B r" Q, q/ \' q& @ n5 Z0 E$ A; S 所应保持的2 P2 F0 m; D6 u2 X; O+ @ 壁板式隔框, . L1 i# N- g% f8 V+ c& ?+ x机身或机翼内一种结构隔板。& B, D9 ?: e5 v- y# o2 J5 f$ M# W; }6 F: l" H 用于协助起落5 e6 i$ n# K* N) @8 X1 ^) `9 q! M2 R& t* x$ ]电线组。. `. C7 t" M0 p8 a, g 英汉对照民用航空词典B OEING! I8 V' _& }6 n TECHNICAL DICTIONARY 24

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BUS DRUM, A mechanical connection with pulleys 7 ^* n/ _% P* F3 S2 ~3 Ecables in the control system.3 C/ ^+ B5 V( U$ ?6 T and : g) [0 j% {8 p! Q- y7 E4 Fl circuits for control and protection of , i+ i5 [. x* O4 C( klectrical alternating current supply to the airplane.; h5 {" i4 o: p- H* H duct for closing and opening the duct 0 G3 ?! a a7 { Iassage. $ ] Y5 \7 M9 [/ l; q, `UTTOCK LINE, A vertical reference plane along the. u7 A2 }9 h' V selage for horizontal measurements of the airplane. + ~6 p) _ B! z4 g接。4 i" `4 |' G4 J( R' W 组件,内含控制和保护飞机交流电源的电 6 U) H2 z" l: }' P4 B, o6 T7 F; |% r4 _( Y9 O' B作动简控制的转动装置。用来关闭和" L ~ [; y* k* k9 ^+ p. ~ 启管道。) G* o" H3 h& }+ D8 Z+ v; d 沿机身走向的垂直参考面,用于飞机的水平测量。) v2 }! {* f/ {, b* |- p- J BUS PROTECTION PANEL, A module (black box)0 ?) I& J* }- A6 \2 ? containing electrica2 l3 f6 H& O C& E e" T- o* |! @. R/ H- f% k BUTTERFLY VALVE, An actuator-operated, rotating! S# }/ p8 T9 B- ^ device in a$ s) l* K* o' |1 i' Q6 o* ?1 a& B p1 Z/ L, R! W. e4 }( A9 i) Z B % C N% ^( _( [ K9 Sfu9 }$ X" N* {/ [' E/ [ 转动鼓轮,, d% h% U I1 ~% }. N 在操纵系统中,具有滑轮和钢索的机械式连 7 a: D8 O& U6 Q3 N3 g8 b汇流条防护板,) ^5 z+ y3 h/ i! ^1 l1 | 黑匣子式的 6 P1 B; A2 T2 {. u! O4 y2 Y9 P/ q% M5 s 蝶形活门, + J0 I" \ v! b- [1 O是一个在管道中由5 k% t$ Z' ]- h; o7 H9 L" Y3 |# G& i5 x- |% ~6 e8 A纵剖线, , }6 p+ f1 Q. l英汉对照民用航空词典B OEING , w6 | _% u( X; S: ~TECHNICAL DICTIONARY 25 # C0 \' C; J4 KBYPASS VALVE, A valve through which air or fluid will 6 {% G+ [5 D$ Q. s7 i" F2 K3 _flow if the normal flow path is blocked. 6 X* R( X$ y+ i' R' f2 r; LBYTE, A group or string of binary digits. A byte is # W" M2 _, ^# v2 z. b# H) ^sually eight bits long.& J: S b, P8 t+ Y. \ ABIN ALTITUDE, Atmospheric pressure maintained+ V+ B6 A4 N! T2 d ithin the cabin, indicated in terms of feet above sea 5 }4 B- p \: CALIBRATE, To repair, adjust, fix or correct the ' ?' }* w, Y: {easuring capabilities of a measuring device. / A% B+ q- H: B5 [ALIBRATED AIRSPEED (CAS), Indicated airspeed * t: T' c$ f" E" V8 x) Y8 N9 yAS) corrected for position error. ' N; h5 \7 d! qnical8 a A; G$ u2 N4 _# i omponents. + ]7 p; |+ x8 }2 Z$ o1 p# C, m; a& p& A- l 节, " W1 r: D- O0 V" r/ ~7 L一组或一列二进制数。通常一个字节长8位。 . _* P7 S" h8 W o2 C舱高度, & \# I7 [/ E# o$ O# d5 E! a) E座舱内保持的空气压力,以海拔多少英尺表示。) x# s! m0 d- _/ ]7 O 准,0 h: g; x7 Y# c( S4 s 修理,调整,定位或改正测量装置的测量功能。 7 E; t# ?$ F! w- n+ c, `0 R/ l正空速(CAS),) E: B" n& g% k+ U6 R 在修正了位置误差之后的指示空速(IAS)。0 f. ~7 z, M( {4 B' V. ? 用来移动机件的一种转动装置。 % Y7 F w/ L7 w& l# Au( H8 f2 W0 X9 M C8 U) _% J8 b5 [3 M C , D `0 J# \8 v" z/ _$ f9 `( a3 ?w- E3 r/ [1 a7 x7 w1 o/ z4 | level.4 }1 P. b% |& N7 @ C- v$ _4 A/ v9 e& E0 ]/ [' |, w m 7 y* Y9 O; {2 J( b$ n+ d! t, uC 9 f5 c2 z" d- K0 W(I9 H# G6 n7 B, K, k CAM, A rotating device for movement of mecha 8 G, ]9 R/ H" j) m' ~C* g1 Z; G9 I2 R3 W0 X& G4 L6 I. Y 旁通活门. r$ e( D* T5 d" B 气流或液流在正常通道阻塞时所经过的活门。* H- t% _: Y, Y2 u; C. c8 b' S1 I( [, A" `/ [% ~5 n( u* n0 H7 o5 b/ F. s- G7 y; O2 r2 I5 W& |" A7 W: V& K" |3 M9 P0 }" j: R! C凸轮, ( d( h3 R2 j z( i英汉对照民用航空词典B . Q, ~. e4 d, o. j8 W6 Q# QCAM-OUT, An autopilot condition in which the actuator v1 g5 \ {/ g9 E2 t detent piston is overridden, either manually or by the 4 x |' h5 Q, f* gther autopilot actuator. 5 Z5 _/ o ~4 [5 V3 ^ s, W1 w+ _6 \AP, SEE - CAPTURE S9 j$ s. U- D- t' W' Z' i' C APACITANCE, The measurement of electrical energy8 `( U( ^7 n0 Y) X tored in a capacitor (condenser). 7 ?! Y5 p. V- O4 GAPACITOR, An electrical component of two metal" x6 l3 L- Z% l, ]' d lates separated by a dielectric material, for storing 3 r7 b! i: d- h- {" Flectrical energy. 2 ~* g6 W6 o5 G( |( |6 @/ z+ uCAPTURE, An autopilot or flight director function to4 e; w& A7 h! j5 u9 K9 ] acquire a selected mode. % v6 P' S! `- oCARD FILE, A container on the airplane for printed ; d0 _& b/ R0 N9 Y( Vcircuit cards. 7 h! Y8 i' x0 K) r `6 F) z一自 $ u2 a4 c/ z% w& `; d2 d B, H& M动驾驶舵机所超控。 / i7 d9 s/ R4 F7 B6 n; g截获, 2 u6 G' S* V# J$ f见Capture 6 V7 G. X1 c0 ]! @- yo- f4 l2 y: W& y C & B! R" t Y, UC2 u$ T2 `: b5 @/ y: E s 3 {2 |( d) W, z! Y7 c2 |* SC% L4 I3 t. k8 {8 {# w, B p8 Q" F5 K) i- ?8 F1 } e* c9 q$ ]& z) U- {! n5 z 凸轮不工作, * V, S% e! [- ?% ~一种自动驾驶状态。此时舵机锁定活塞被人工或另 t' ~" r! K$ E, G$ T; u3 L) w0 I. b, v; u 电容量,7 m' M8 i/ k; v: N1 {- Y: Z( _. ]% M 电容器内所储存的电能的量度。/ W& s$ r6 m. ?) r& r) _ 容器,# N8 f* @7 k6 v! W1 m2 J/ U0 X+ N 两片金属中间用绝缘材料隔开的电器。用以储存电能。( O! p, M0 c: @$ q0 ? 截获(CAP),: X# m2 D4 A8 N! B |. L2 X. V5 N0 F 自动驾驶仪或飞行指引仪的获取选定方式的功能。6 r6 |: m" R3 O 线路板盒, # V2 T, s' Y2 A( o5 {飞机上安装印刷线路板的容器。- \, n( k! ^5 p* b* D7 ?& D4 {# A" ~ OEING8 L6 s5 t5 Z: j, [4 w4 z8 Z- G TECHNICAL DICTIONARY 263 @+ R4 G9 q5 a( S6 x. G 英汉对照民用航空词典B OEING& D- c# M) G$ \ TECHNICAL DICTIONARY 27) u7 s" [# Q! j CASCADE, Two or more similar circuits or amplifying , V# g. C6 L7 \8 gstages in which the output of one circuit provides the3 V' y% ]% R# a; q& p, F' B* c I ~ put of the next.5 H. S. I X; x3 M% M ASCADE VANE, A vane for turning the engine airflow " b' Q7 o' F) D* w% R3 [uring operation of thrust reverser.4 f6 L: F: z3 b; K8 y9 c" ]4 q ASE DRAIN, A drain carrying lubricating and cooling . m" l' S$ P- f' o3 Q9 quid from a hydraulic pump. $ f$ ] B0 t+ c& nATHODE, The element from which the principal5 I' P: N/ u% B# Y9 K tream of electrons flows. ! M" o. o. j2 ]( u& FATHODE RAY TUBE, An evacuated glass tube with a+ o/ T( i, Z) P! x" h2 X CEILING, The height above the ground or water of the $ J6 S# a1 A6 O; I1 p, abase of the lowest layer of cloud below 6000 meters, L8 w$ H0 p4 P0 L (20,000 feet) covering more than half the sky./ h+ C* h$ c6 q& R 程。该 # s j/ b# q) `$ x" {: V2 N9 S程中,一个电路的输出为下一个电路的输人。$ W& ~+ k2 f+ r 叶栅叶片,) u2 U2 F% S" ?$ W* U 在反推工作时,使发动机气流向相反方向流动的叶片。 : i. c/ p& R2 G9 T匣余油管,+ f, S; Q7 J. ^- B+ ?4 I 液压泵多余的润滑液及冷却液的排放口。# @- a: y/ ^) V4 @& D9 c7 I 极, ) J7 P! R" m0 Z- i3 r9 h( S4 G电子流流出的极位。 ?2 T% e% \. f/ h 极射线管, ]' K4 o$ v8 _6 Y: T有显象屏幕的真空玻璃管。用于显示信息。 2 _& G5 L3 _3 m7 b* T9 P" G云高(云底高), 8 Z7 t% _5 S- H, K% G+ `( @6000米(20,000英尺)以下已覆盖一半以上天空的最 6 T: t8 o7 A* Y9 n* c2 s4 e低云层底距离地面或水面的高度。 # }2 x( R) y2 c4 Q0 Din $ Z6 T1 r+ i9 C4 A' DC, M: z$ S, M, ~ d 2 E7 q3 r$ h7 N: Q+ FC & t3 h- n# _: S. q1 N& Afl# x6 p$ K" H. m C( `7 Z$ T2 m! {0 ?$ r s ' u3 {% m+ y0 t/ m: s }" QC) ?* Z. o) F% R" i viewing screen, used for displaying information. / ^3 b/ x; A8 d& e8 h8 S( x级联, - h% k6 a% ?, R# h, ^# T% q( P" f+ K两个或两个以上的类似电路的逐级连接或放大过' ~7 k! r/ n. Z( a/ R3 d) j/ I" b2 E+ Q: x1 q" |( m6 w% E9 l7 u0 C2 M% c, u+ X) t0 m: o8 }: J) L. C- p6 K一个具 - O* t5 e) z7 m% M英汉对照民用航空词典B OEING7 i s7 M6 v# W/ B" o! f TECHNICAL DICTIONARY 28 : j$ n% G( n# SCELSIUS, A temperature scale in which zero is the/ C) S8 [ b' |! Z- }, y freezing point of water and 100 is the boiling point of - E6 D& x; G" i! N. g! i1 n5 jwater.- e4 ^8 ?+ U7 m+ r; ?; M CENTER OF GRAVITY, The balance point of an object, ?: b2 Z$ M2 u l r rigid structure expressed in terms of percent Mean 5 R2 _ b F2 c: G+ S7 u' Nerodynamic Chord or in inches from a reference point. * f$ U& k e. ]. b5 |0 l5 ^: oENTERING CAM, A cam for moving a mechanism to a ' X& D" J( W8 G' ~eutral position. s' s1 F* L6 Q$ L+ G. |IGURATION, A configuration of the# P. a6 ] z& ` ircraft approved for operation by the local governing3 s0 y% a; ^1 f8 S( u4 J gency. # Z# }. j: n e) r8 p$ g L5 RENTRAL PROCESSING UNIT, In a computer or& |5 C% `) l( e7 z0 h+ q3 N6 ^ igital circuit, the section containing the arithmetic and( Q6 }) B6 B+ p# f9 j: ^ gic,control, and internal memory circuits.; r8 I. |) ?2 v3 Z# n) ~ ENTRIFUGAL FLOW COMPRESSOR, A type of # i1 N1 w1 P" b0 W( p/ K& Wompressor in which air is taken into the center of the $ ] w9 x' e6 jpeller and is slung outward centrifugally into a diffuser 3 m" V: l4 p+ E. D3 K9 q1 @! H) xhere it is slowed and pressure is increased./ ]8 H6 q0 P: \) V, q! o9 x0 x CG, SEE - CENTER OF GRAVITY ( @1 W, V e' Z/ i$ E) H. W, h构的平衡点,以平均气动力弦的百分比或 * L6 X- H6 q k某一参考点若干英寸来表示。7 u# z$ s. p8 Y* D1 I 中凸轮,7 I4 ?1 G1 B: D 将机构移向中立位置的凸轮。 * F6 B; Y F/ M: m% v$ w格的装机状态, / ~. X* z/ D$ @5 u由当地主管单位批准使用的飞机装机状态。 ' O# d m3 E+ g; Q5 I2 r) o中央处理器,$ N; ?! U- V7 Z 计算机或数字电路中含有运算,逻辑,控制和内部存# F1 Q8 Y/ E% k9 o' \& A 储电路的部分。6 |& F: t8 Q3 q7 R# W 心式压气机,6 ?+ e5 l4 [3 m7 b 压气机的一种。当进气到达叶轮中心时,被叶轮离心抛 4 F- L" w9 o7 ?9 d0 q4 y进人扩散器。在扩散器中气体流速减慢,压力增加。* f5 m% i2 J9 f8 P/ I5 H* Y5 { 重心, * z! u- I4 A* v见Center of Gravity ) v* H' A! e( }3 _/ E: Z( r. oo5 k$ X( V9 n9 S% t$ W8 W- } A 5 d7 K9 m5 N& }( O! V5 G, }# UC 6 Y$ h1 l" Q0 R3 qn' Z1 l9 h0 j+ a( e5 h0 o CERTIFIED CONF# Q2 X3 A# W7 I- J, s7 q( ~ a* q4 v, a, Q8 ~: b/ r0 u% r a& Q9 A0 t/ i$ @6 i3 `4 j8 J3 @3 u) _ C& d" G) I1 I5 B$ ? d* p5 c M( J* W: E lo6 x- m; ~( T; g# } C" O8 |9 G7 G# b' p# u) Q c; `" ~/ {. {4 M7 Y im/ ^) T* s! x" j8 {' h: _8 t. m w0 y4 D% V7 F; s) l 摄氏度(°C),6 J# ~ E: z* U' K6 e, v6 }3 \ 温度的度量单位。在此单位中,0°C表示水的冰点,* l f B! D" y' C t 100°C表示沸点。 ) \+ {# F: v+ Y7 r- M: W重心 - Q9 t, C# c: w* J! F物体或刚性结 : H& [8 m1 [6 N/ r+ E- z9 {+ k* k% o/ D6 a. A2 f+ f( U* v& i2 n) M; H. p7 S8 M7 j0 T; n1 n: ~# j% o4 m7 b. Z8 T; Q) _; @0 _: i8 J2 q. S9 F0 G英汉对照民用航空词典B OEING 4 S1 T- }! s5 Y$ S7 [- TTECHNICAL DICTIONARY 29( ^' Y& l) j. M9 ]3 s7 X CHANGEOVER, Conversion from one mode to another. 5 Y! V- m/ k# d! m: uHARGING VALVE, A valve for supplying air or fluid to - x( _: _2 j8 cHECK VALVE, A valve allowing flow in only one % z! Z6 D% |6 g6 xirection. See Non-Return Valve.) v) i. L. g6 L6 L- O3 l. @ HECKSUM, In a computer, a summation of digits or . m$ B/ S$ |2 N, @) D# hits which are primarily used for error detection. ) a8 v7 `' j- D. wHIP DETECTOR, A magnetic plug in sumps of2 g5 e1 N1 M% U4 X% C bricated components for detection of internal failure of ( k: W6 _- J" M& U0 Qe component.2 y$ O" H* n2 `* a/ N5 o e HORD, A structural component of spars or frames.9 d+ l* B& r9 I3 |# U 添活门, ' ~+ M' x9 g" _! b9 ?器充气或加液的活门。" G5 g& O# ~; W$ R/ Q3 M# X 单向活门, 8 {! I) D$ l, A6 y9 ?* S% X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 7 c/ O2 |5 B" e& {: u& Ma reservoir. 3 {: L* G# S; ^' V0 J L4 I# @( ZC 3 t' l& d; ]; o8 A* k# ^8 R6 ed8 j- }9 G% W- Z. { C 5 {( b/ o; x2 [8 Db & V* G. _) J n4 u1 I9 d1 RC8 ?7 f8 P1 |8 A" J/ M/ b! m lu# `) y" R) f: H5 K3 }! [ th* e" _* A; m" h1 Y2 ] C( I2 }0 C+ e; Q3 T& M 转换, ( G2 W1 F% K* j+ R; i+ }: O9 J由一个方式转换到另一个方式。1 I+ p. }# N! J6 g* j# ~% ?# P8 c E$ S- d6 l2 L8 C用来向储存 + m6 j4 X6 N3 J/ o$ d# Y. Z4 j# z, y4 |, A; f& i/ L总和校验, 3 t/ O1 ?) ~& x8 K( Y: _计算机中,把那些用来探错误的数宇或位数的总和进' p& Z4 U- q, `1 I+ ]; x. t/ ^ 求和计算。, {; e% j7 E, K; M 属碎屑探测器,6 U' b- B8 }$ B8 Y8 P9 j 装在被润滑的部件滑油回油管路上的磁性塞子。用来探 5 q3 H, a7 E8 e! N! ~/ {部件内部有无损坏。2 p6 X+ ~) ]; H) `$ F; `5 \/ i 弦, 1 H1 G! S3 b$ L: A梁或框架的结构部件。+ I% n2 S+ ^% ?: {5 N% Y; Z5 m E2 F9 n9 q. j! w7 ^! J* y# G# L( z( r' G c; Y$ z1 w: Y" r* y3 W& n8 L Y( Q, Z2 j# W3 h1 X% {$ m2 c W9 P6 x) f; i2 D3 f 英汉对照民用航空词典B OEING + w7 A& U$ c1 E y5 w) a% ITECHNICAL DICTIONARY 304 F0 E: U6 v1 u( }6 f# D CIRCUIT, A closed path through which current flows$ r% k" f4 c' h; A1 O9 a ource.- C' L1 J* Y+ m$ e5 h/ k/ m; q IRCUIT BREAKER, A device that automatically " ~% n* y2 a4 I; {1 w- ceactivate the system.8 J, F1 l) F9 p4 j$ }$ z5 R lear of all non-frangible objects which9 }1 `7 O& z5 W5 d ay be used as takeoff distance available when ; V, o+ l1 A5 ~$ v8 w1 ~0 X, i. Ralculating a takeoff weight. # D \7 R. r3 wr water under the control of the appropriate5 J( e& w4 h2 R uthority,selected or prepared as a suitable area over 3 z) S5 T' @8 @- @hich an aeroplane may make a portion of its initial- R2 |( U" d* ~8 l' ?8 G6 R limb to a specified height. * w. A- Y; A2 p9 v" ~( @4 Q1 Vincreasing. % F0 y* U" b: Dsed5 W3 x1 I- `0 ^) x/ T/ V' X% i LOCK SIGNAL, A continuous string of pulses used for $ d6 o) z1 W7 h' S开关, : N0 }, q' o# h+ M故障情况下自动中断电流以保护线路不受过电损: j. ~+ I4 _+ }/ B9 u; V 体障碍物的区域。在计 / y8 \, m9 J- _5 M起飞重量时该区域可作为可用起飞距离。! Z" ?& I2 A/ w, R 是在有关当局管辖的地面或水域内一个界限明确的长. C! S7 V7 P+ z6 B9 b) W2 u 形区域。在这个选定的合适区域内,飞机可完成初始爬 9 a9 C. r( k/ R的一部分,上升到一个指定高度。& N2 F$ s c& e- \/ Z) O 飞机高度不断增加的飞行阶段。# A- J1 l# @8 ~; O 钟脉冲,6 K$ {8 S" x' E+ I/ S 步的连续脉冲信号串。 * ^4 z, W, `* Y! D2 mfrom a source, through various components, and back # h5 y- a. y W' ^0 w1 rto the s 1 Z2 h2 N5 G% f8 UC }, X4 z' e" M# C. ? interrupts the flow of electricity (current) during fault # `& w1 D; w/ wcondition to protect wiring from excess current. Circuit* _0 X" N" J/ N9 `: R% N. N breakers are also used as a means to manually 2 I2 W8 \" o9 r* ]3 @d ( W7 J0 d9 K" {/ q }0 u& ^. k9 X/ _CLEARWAY 1, An area beyond the takeoff end of the! m6 y, D8 y) f m$ h runway which is c : G& [. H/ A+ _, h& km ; r9 ]) m# _# D" A& C: W- N: ec; q+ R& v" U3 L7 J CLEARWAY 2, A defined rectangular area on the ) y0 m! V. @2 h" W# Qground o % P- v( }6 x4 _6 na5 K! A+ a3 ^% g5 h8 P# G* X1 Z w0 t( h. ?4 Z$ U! t: D# i5 g! s c 4 F" J' t3 C" s0 S' D' oCLIMB, Phase of flight where the altitude is 6 D" s' O" B" \: A( h/ [CLIMB LIMIT WEIGHT, Maximum takeoff weight ba 6 s" g/ M7 ?3 i! A) Y- @$ Zon a minimum climb gradient with one engine % x. u, {7 q f+ i$ pinoperative. ( e0 q C+ W1 ], S7 A/ `C0 i$ L0 L: f C0 a, T synchronization. ( ~5 k: `8 J8 l+ M! B# l电路,( z1 |: b/ S5 v! s9 p 一个闭合的回路。电流由源头流出,经过各个元件流回 3 r7 Y, l# j4 ^' ~/ p! ^% I9 x0 m源头。+ Z8 }/ t& M9 A, `& T: P `4 r K7 i. }$ X( a能在 " v' t- `( n$ s( V# y, Y. M坏的装置。跳开关也可用于人工使系统无效。0 D9 K' J* y/ F7 `5 I 一号净空道,) T2 j" \* {: P8 W! k3 F3 a 是跑道起飞端以外,不含任何刚 : ?- d( e5 K+ M9 Z/ i- s5 d Q/ K1 m二号净空道,7 `2 G4 o8 n2 S; U: T u" n8 T( S/ [' B8 v3 ]: u4 h2 n& b4 R. t- @0 J" y; `+ d* t/ }: C, P爬升, ( {- |1 ~; T- I1 l爬升限重, 6 M) Q* u/ |( I* |( p取决于由一台发动机工作时的最低爬升梯度的最大起8 J. B2 Q8 g: K% V$ q 飞重量。8 j# U6 f! M* h8 b3 q. b! K6 F' x4 i用于同 & S* d! j$ ?* t0 ?. u" k英汉对照民用航空词典B OEING4 t9 n' D9 A( x3 b7 w) m- H: | TECHNICAL DICTIONARY 315 T' [8 p- e1 m9 W$ U6 Y COALESCER, A device in the water separator for 0 K- b3 W4 N$ ^( e! ?. c$ m+ zollecting moisture from the cold air.0 g9 p0 m$ T" b n antenna with a receiver or transmitter. " p" r. g _- g# N f0 m5 Jhe cable has an inner conductor and an outer ! r e0 Y, j- z7 H8 vrounded shield. - O: M* j- d: p( L0 N' zting one inside the3 l5 ^/ F _% ~7 `% `4 g, c$ c9 z c ther for rotating the low and high pressure2 C8 B" V1 R- ? ompressors by the low and high pressure engine- u) E4 |* X( D rbines.' p, b' V" W" W9 B, [! h8 L OMBUSTION CHAMBER, A part of an engine for- j1 z0 s+ G5 d' D, D, C% t- v, E urning fuel in the air supplied by the compressor. % e# w. N E9 a置。 E4 s8 S" O+ E8 E6 C9 H6 F射机的电缆。电缆 $ p& g& A5 y9 I/ s1 d3 b, J9 X$ K中心导体和外层的屏蔽所组成。0 C6 Q# k H+ l" m# G' o 两个套在一起旋转的轴。用于使发动机低压和高压涡轮 # l9 U8 Y2 S5 ^* T) ^" q& h别带动低压和高压压气机。2 v5 M" C. S/ J$ L& x' y0 U1 h4 x 烧室, ) X, W! K( x% L+ h# I- x" Z发动机的一部分。用来使燃油和压气机所提供的空气相0 H0 f1 u h. |' ~: T- h7 r 合而燃烧。

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发表于 2008-12-24 21:38:35 |只看该作者
c( I% O" ^! G- k# N2 f4 V3 T COAXIAL CABLE, An electrical cable usually * ~$ x/ g9 D4 v% t, b- j# Sconnecting a % B. L1 f. }. H, lT# [+ _# N) z j7 P+ k6 Z: a, q( K/ e9 F. a g # G: e7 p8 ^9 m: j6 b# l5 u# ^1 q5 \COAXIAL SHAFT, Two shafts rota 3 M3 X8 Z. u0 E- Yo6 t+ ]6 w! `2 L6 Z; U( w9 }- ] i c1 c. T4 J$ |2 R, d/ f* o( D# j+ p v tu$ n2 E. a [- p/ F, d/ J C. u+ w3 C9 s! o8 M+ K# g+ Q5 U b7 U: V7 m" C' {1 C3 z 凝聚器, 3 c7 s) `$ }& z" h; V- O$ z+ L水分离器内收集冷空气中水份的装0 x5 n/ N9 l/ Z; F- E 同轴电缆,. v7 T. m8 B8 Q! E+ n# r 一种通常用来联接天线与接收机或发3 r* \. a6 Y& V3 g. T- N! N5 S! ^) s, H: a5 A/ y. k$ ]同心轴, / S2 x' @0 B, b6 }6 k( _7 r2 Q+ {! K2 V2 T; ~: j, ^1 o/ @ x- C# p% _' r: {4 o) e4 M3 N& W9 s# w5 k! a4 e% J英汉对照民用航空词典B OEING& l; K- A' j3 { TECHNICAL DICTIONARY 326 Q8 w0 a& a/ f% k9 `. B J- A4 f! W) j COMMAND BAR, A flight director pitch or roll comman' t* {7 |) l. U7 B0 G a indication. 8 J3 n3 O3 [( j9 W- Zd ; {& {) x. N3 R6 u4 Y4 DOMPANY ROUTE, A route flown by the airplane 2 C4 `. _9 O: C/ F4 eOMPASS LOCATOR, A low power, low or medium 7 z7 S1 C5 u* Y- u1 xequency (L/MF) radio beacon usually installed in$ \& V& @/ }% B( A' P; ], f onjunction with the outer or middle marker of an: q) Q! |* [% L tor (LOM), A compass # K- m4 L$ z* K9 Mlocator installed in conjunction with the outer 4 r# p. g! U+ u8 k. x- ^+ hmarker of an instrument landing system.* |% c; l+ c6 P0 U% g ss : ?- j' M3 d7 Z) H* Gle8 c' ]) O+ ]$ \% z+ B. Z: a6 L OMPENSATION, To offset, balance, or counteract. 4 s4 L( w( G5 L1 N( VOMPENSATOR, A dual capacitor for changing the fuel, [* o" ~% Y7 f0 h aging circuit capacitance due to changes in fuel $ A. U0 E/ E8 O! c2 `* A: _ensity.' b) ?8 r8 o+ P1 b OMPOSITE MATERIALS, Non-metallic materials used, t% [: \, p4 \1 u8 x# { r airplane construction. Fiberglass, Nomex, Kevlar,/ e1 f* x* Z8 }- T/ |- F3 @: a raphite Epoxy are composite materials. % R7 d) B: |- a司航路,& I. }0 _7 B: c6 W( A j q 在飞行管理计算机数据库内由航空公司飞行 ) _, |' ^( A- j* ]( O2 G5 s" `6 r盘定位台,: d& {3 A* }0 n! I 与仪表着陆进近系统的远距或中距指点标配套安装的 0 h! D6 m9 ~! |' M* [2 D7 @功率、低频、或中频无线电信标装置(低功率NDB台)。4 e0 u, h3 r3 T8 U 程序中用来导航。 2 P! E8 Z8 l6 p9 A; }* z, Q$ e6 f1.远台, % D( q: h. M2 o0 G与仪表着陆进近系统的远指点标配套安装的罗0 j# R+ X: {) W 盘信标台(NDB)。/ J5 q3 \" R$ H a' `/ n8 a2 A 偿, * L: Y# f! k/ q, h抵消、平衡、或中和。 x% r% d: C! B 偿器, 0 p5 u, D% h$ r% Y- B在燃油计量电路中,用来改变电路上的电容,以与燃3 G& P4 K" F' Q' c3 n& u/ A 密度改变所引起的电容改变相抗衡的双电容器。 # c& W! T, z' ]合材料, # S9 }9 n r0 i% ~; j, E, N& `用于飞机制造的非金属材料。如纤维玻璃,Nomex, 0 C% W4 i( R; o6 B: a8 e$ Tevlar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% D+ `7 U7 o7 f4 W1 n operator that is normally stored in the flight3 L% H/ ]. b8 d management computer's data base. " s& o, ]) ~+ T6 O% A! ^# RC% {2 d+ A( y1 a5 z0 q3 C fr $ S* ^+ h7 A& Ac) q, c& f6 U" ~7 k instrument landing system (ILS). It can be used for 1 T/ ]$ n! F9 {4 Dnavigation as authorized in the approach procedure.% M* d! o* ?. M1 X5 N6 S7 D$ z 1. Outer Compass Loca+ z4 q* n4 \' Y$ |0 T0 [ 2. Middle Compass Locator (LMM), A compa ; H3 Z7 U4 M% i- C% o9 F7 flocator installed in conjunction with the midd ; k7 ^/ h( X7 }) q e0 G' E* Y. @" Omarker of an instrument landing system., }* A P! K! ]0 R C $ P f0 n4 U5 E/ vC9 s0 I6 g2 W( h) P g " W8 T' ?* H7 [d+ I* |5 W2 @- v* j' T- x C( F. O7 C4 X, f% m( l fo 1 t: d+ M/ B1 C2 rg # j3 T: i8 Z' F2 G/ |指令杆,* { V1 T8 T5 O4 ]5 ?" ] 飞行指引仪俯仰或坡度的指令显示。2 U o' {4 @- s2 F& G9 p! F. D4 Q' I( l7 h6 s" c通常储存5 b" D. Y4 W# `' {: F* o% [ 的航路。 " F: m- }& l) ^+ _, ^/ ~" x% d% X7 X3 x4 R: R8 B5 r! g/ S% S7 O! [# y9 J经认可后在进近 + h3 @! ]) L2 t3 c* W$ S2.中台, 5 n$ w* l' c+ V: y8 p1 U! l与仪表着陆进近系统的中指点标配套安装的罗 + q, P, s) `4 d' I$ \2 ^2 H盘定位台(NDB)。 % O% E6 E+ N3 j: k. T' _' j, X, w* l3 ~1 L# v( E q4 C# |! H. W& G& A5 Z1 o" [: z3 [, @+ K% V) |' V- q2 i* L3 u1 ?, U' b s9 W$ @$ i: _& o+ C) EK( \9 O# N2 ]' X1 M3 l 英汉对照民用航空词典B OEING9 v$ U' e+ @3 w2 Q5 s! i. ^ TECHNICAL DICTIONARY 33 3 V( F6 Z# v- ?6 Vby 4 r0 H. }* t4 r, k, z! Vor increasing air ?9 ~- j$ ~$ l0 f* y' f- {ressure and temperature before the air enters the $ N, L { ]- [) X2 ~7 D& t5 P- nombustion chamber, Low pressure compressor - front 4 f4 @. S$ u8 ]! d0 J6 gection of compressor, High pressure compressor- rear 9 j9 a; L4 u2 hOMPRESSOR STALL, An event that occurs when& ?3 a3 c: B. g0 A( _3 l ere is a complete stoppage of air or reversal of air flow3 h8 B0 F3 H% z# Z COMPRESSOR SURGE, SEE - COMPRESSOR 5 ~, Z3 D& S- ^$ G+ g! K/ I9 CSTALL COMPUTED AIRSPEED, Indicated airspeed0 v |3 ?( X, o0 T corrected for the static source error. ) J2 _% P' ?$ e9 E V0 y的机械轴来驱 ! a2 @9 s/ x7 M$ V5 r1 [' z,用来增加吸进空气之压力和温度,以供燃烧室使用。5 H0 L! D# y+ L/ J4 g) E' k) v 压压气机—压气机的前段,高压压气机—压气机的后 ( P- B7 i9 B' z U) M) W# R+ `: M1 C: [6 @ 气机失速,( [* A; ~/ R; ~6 j1 F 当气流完全停止或通过压气机时气流方向逆反的一种& F1 m! W8 d5 j7 w+ r8 Z 压气机喘振, 8 ?1 s9 W% @3 |# e- B( z- D* p见Compressor Stall ) O9 I- y+ U3 S# HCOMPRESSOR, A rotating part of an engine driven 5 s8 g( D" @5 t+ w& y/ ia mechanical shaft from the turbines f/ a1 H5 ]; M. U8 H6 G9 t p ' D' n g$ `2 Ic " `3 J! Z# n: |' s% ?+ C0 g+ {s & d" f8 a- U1 Y8 S7 N: |% Lsection of compressor.1 P4 E4 Y1 q9 p! u C 1 P- E; t& j( X. t+ n* ^0 uth9 J R2 n) q, M) L% x+ M through the compressor. / O; T4 L/ v# B* }8 B7 D7 }0 ]压气机, 8 j1 i* u6 z2 }! b* u发动机内的一个旋转部件。由与涡轮相连2 s+ U9 ~0 x7 J! n# J# g, n7 C' A6 `; b; @: T- e3 l9 n7 _/ ?+ h' s7 ], G1 D( K) a+ \ f3 a; ]0 m2 U- M2 m9 F$ C- T3 r) {: i 现象。: F% i) T& K" I! Q, T4 Z- U5 ?/ L+ a2 M' f2 f计算空速,$ i! V4 I# o( F% L E) i' b6 J 修正了静态源误差后的指示空速。 7 x- e4 b; p7 _英汉对照民用航空词典B OEING 1 z, `4 B9 `2 E+ P* h0 u5 fTECHNICAL 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$ ?+ n/ N! C3 V/ f: ` operations, manipulates data, and makes decisions. d2 W7 G7 ?/ ~0 m( bditioning0 C0 A( H( Y. H the air and the, ~6 _8 S6 U% z5 f3 T frigerant or moisture vapor is changed into a liquid., b! z ^- Y* Q ine* h, Z! ]1 h: F& i8 B$ T ONFIGURATION, The position of flight controls, # R% B% c% b' ^missing which + t. @6 S( B# z% M0 Omay affect the aerodynamic performance of the 4 c; f- D/ q2 A2 V1 Dairplane. ; b2 L( P- t6 I置。1 [, r+ ]+ E- N7 f 中能使热能散发到空气中,以及使冷冻剂或湿7 G) `3 A" O& b: ^+ v9 x 转变为液体的部件。% h m/ l) B2 y* u& d! ` 连接到飞机结构上。9 t9 h: |8 ?7 ^9 L 态,' Z# B+ @! t2 s S2 Z, J" r 定飞行阶段中,飞行操纵面,起落架等的位置。* \3 |7 x- d+ Y1 \ ), 8 E4 M, A: C g+ w受到影响。1 E0 t6 S( }0 d; @3 } CONDENSER, The component in an air con, p8 E" |3 d, L0 F" W system where heat energy is given to+ u l( H) ^. t5 q: I+ P$ O' D re * }& }# i) E: [3 v B$ k8 _9 CCONE BOLT, A bolt in the shape of a cone for eng& T. {# M7 L! F( G* P9 u# w! N: Y attachment to the airplane structure. $ M. ?( z' ]2 C7 S# uC) ]: b- C0 B$ _ u% H- a9 v landing gear, etc., for a particular phase of flight, e.g., 0 A- k m. h3 S& G9 V+ V. P% m6 `Takeoff Configuration, Landing Configuration, etc. % C4 W2 S" h$ n* b5 |. cCONFIGURATION DEVIATION LIST (CDL), Appendix4 L8 v% K5 b( Y- z in the Airplane Flight Manual (AFM) allowing operation6 i1 v0 m6 l% v3 ^" F of the airplane with certain airframe parts; _2 w$ a+ r; n/ X' F" {+ ~ 计算机,2 I9 |- _$ t2 X6 \5 [- g7 M 能作算数运算,数据操纵,和决策的装 2 M- p. y2 e/ e y3 S% ~冷凝器, ; f0 y+ ^6 j+ V8 x' }+ Z空调系统 " j6 r7 m1 S* L* R8 O; f8 J5 s B9 q5 g" P+ f锥形螺栓, ( M ^7 }3 Y, M. C外形是锥形的螺栓,用以将发动机 6 Q3 `, K; _) v' i+ ] G1 j, u1 ~; i5 N+ H& ?6 H% ^" C/ _9 q在某一特: C1 U! E4 a& e ^; o5 Q* W 如起飞形态,着陆形态等。/ }! l% g+ Q& a( j* O$ q 缺件单(CDL9 ^1 Y& R/ y7 E9 _, a2 T# V 飞机飞行手册的附录所开列的飞机上某些零件的清单。9 M" X$ F9 a; U: Z6 E: I 在缺少这类零件时,可以飞行但气动性能可能7 W, |! b6 n6 v 英汉对照民用航空词典B OEING + @+ l; u5 G, I2 f a' J/ ]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- d' U+ A4 X2 g* l- P component for changing variable engine gearbox speed D7 g" ?2 f p1 d6 f% @ONTROL AXES, The three axes of the airplane which 7 `2 _5 j, a4 p6 Qre perpendicular to each other and pass through the 0 \+ U# W8 x& g% [* Q5 S* `4 oenter of gravity of the airplane. ( T" k! ^6 f: K6 L$ ^; [# t5 tPitch axis - Horizontal or lateral axis, passes through : E2 ^3 C& y! C* Ethe airplane from one side to the other - . P, e+ V5 Z7 l# f* Unose up and nose down control is by" l q7 m) D# t2 E/ B' ?4 L elevators (and stabilizer for trim).* E. T8 G K. A' T: c' p/ I9 u& a Roll axis - Longitudinal axis, passes through the ) \: V6 @0 u5 ]( m( S7 t, \ ~airplane from front to rear - wing up and7 U& }2 g4 z3 w wing down control is by ailerons and# y+ h8 ^0 W4 D x2 g flight spoilers.* @. A4 M6 i* F2 j L4 U) ~ Yaw axis - Vertical axis, passes through the 8 U6 ], D H$ R; Z+ F. Qairplane from top to bottom - left and. e. r* S5 F1 L; c( `8 J right control is by rudder. T/ a# R% X4 X. ?# P% S9 P; k ^置, ) Y& S+ ^1 [' f A制轴, ( v" f) j% {) U' r( ?7 e0 E通过飞机重心互相垂直的三个轴。; D5 w- E( O3 ]/ A8 s+ I8 U" o 俯仰轴—又称水平轴或横轴。由飞机的一侧通向另 , L0 s5 v7 n' N6 c7 y: C侧。飞机绕此轴转动即造成机首的俯与仰 1 H, H0 S+ [# W- u( M' F. U俯仰控制是由升降舵来达成的,水平安定3 D5 A, \& p- K 则为配平之用。 ; \ T" R& g1 {' Y/ B横滚轴—又称纵轴。由飞机的前部通向后部。机翼5 A2 q* ~- ~% |5 P 下运动由副翼和飞行扰流板控制。 8 r1 N5 l- d3 b* C9 Q7 S偏航轴—又称垂直轴。由机身上方通向下方。飞机8 C1 v8 N9 c5 |8 e 此轴转动即造成机首之左右运动,此一运 ( K9 N+ M, ~, W2 O; Y# c由方向舵控制。, Y7 F' R: q( E0 |) V) j( J to constant speed to drive the electrical power.. k' I3 f8 N+ {- Q2 B8 V6 v# w/ H C2 n5 Y! C! Z0 k" Q! v0 ` a * C+ D% G9 R' |% jc: s$ F# _) H) Y7 V 恒速驱动装 ( p* M9 Q/ D$ U2 L: [将发动机齿轮箱的可变转速转变为恒速以驱动电源的, X! | N& ~. U 液压机械式部件。 8 r8 ?! N+ j' ^# r: O8 X4 Z2 C3 d# h+ ?* s+ T* w! \7 g' M( O: K8 p9 h6 S0 H# l+ \9 \+ F) X' S' ~, |& d8 y2 A1 Y3 q7 k3 \. A4 ^ j, s# `: n7 M; ?! [2 Z9 `8 n6 B- c7 K7 {! K$ v2 {+ Z英汉对照民用航空词典B OEING ( b a+ t2 S" z. }9 xTECHNICAL DICTIONARY 36& _' |9 x& n( N0 ? CONTROL COLUMN, A mechanical component used( }- e+ `2 R/ t" H rs6 k4 e7 u( y" Y9 J. ?' @ nd elevators.5 l1 c! S5 d$ U9 B2 S1 K ONTROL SURFACE, Moveable panels on wings and6 D' b. h1 p" I& Z/ `! Q il for movement of airplane on pitch, roll and yaw axes. % R: |, w5 x6 Z* LONTROL TAB, SEE - BALANCE TAB. i& t2 s% v/ M$ W# T: } ONTROL AREA, A controlled airspace extending * W2 P" }9 ~% Gpwards from a specified limit above the earth. ! c: w4 _9 b/ AONTROL ZONE, A controlled airspace extending, z7 e, _7 e5 u+ r, K6 E- x pwards from the surface of the earth to a specified $ [; w' {/ j. U% zpper limit.5 @; K# [4 t# S is+ Q% q2 {- X4 m! \2 g P5 l o IFR flights and to VFR flights in accordance # `' b7 U0 y' M2 l. G+ Twith the airspace classification. 2 y) A4 a2 [! L$ s& q$ |$ q" D机械部 9 {; D+ o* b% D+ c5 t* A+ ]9 x: q: F+ L# I# }# h 操纵面," _' |; e# u& t; h" k 机翼和机尾上的可动面板,用以操纵飞机俯仰,坡度,4 r6 n' I5 W, {2 \3 Y$ h, ~2 K 和偏航运动。 8 s+ Y0 d: [' q2 `& A操纵片, , Q9 |4 s% L- V) f3 d$ z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 ( M$ g9 f% ?) Da % P7 K! V5 X4 w/ yC# E- S$ }# @6 m* _& D ta ! g* ?( V( F* R+ y2 ?2 `9 FC 7 `/ D! r4 |" H- I# q: s6 W* G0 JC5 M( Q7 ^" h' Z! m u ) o0 E. H1 D- NC' X0 M% K! f; L. } u7 h6 i! h8 N" f; K% b: w3 B( h9 i. | u( Z! t! g2 J3 ~ |8 u CONTROLLED AIRSPACE, An airspace of defined 3 Y8 a# W; C" ?' C4 m- k9 xdimensions within which air traffic control service ) x4 J6 @! w( i' Sprovided t6 q# @- g# {& o* J 驾驶杆, : D- K$ w+ _* u3 A8 o. L飞行员用来操纵副翼、飞行扰流板和升降舵的) s4 H2 \' J& D- e8 H* Q6 A" Z1 d) B8 ?0 j3 V+ a6 C* C8 w管制区域, ( O9 W. y5 L4 d3 j1 x: S高于地面的指定极限以上的受管制的空域。 # m, n0 c: b' j制范围, 3 ^- N/ p- i% b: v- m0 {& g' w由地面到指定的高度以内的受管制的空域。, H! M/ }( t6 G( y" O, L3 ]$ H2 X 一个范围明确的空域。在该空域内,仪表飞行规则飞行 " q# y$ O, d/ O* Q和目视飞行规则飞行有空中交通管制服务。 8 t* @, @4 H# w( i9 K" h6 O: t# w. P- S1 ~受管制空域,% l4 z. o) P% t7 Q) Y0 K1 t7 ? 英汉对照民用航空词典B OEING 8 H7 U) e4 x$ @3 kTECHNICAL DICTIONARY 370 j) G7 ~9 g7 v" E CONVERSION, To change into another form.9 X! t+ a% O6 R, r/ J3 p COORDINATES, The intersection of lines of reference, ) z$ U! w9 }+ _3 U, qsually expressed in degrees/minutes/tenths of minutes0 o' h) i" I* D% {" H* A/ [ f latitude and longitude, used to determine position or. r' h$ h9 j- o! o: m+ H+ l CO # o: r* e/ g0 S' M) M* V! x1 fdestruction of th8 J/ z5 {, e5 u Q& ?5 F9 A chemical conta : b* t4 Z- J, A; QCOWL, A remo O6 N/ y" q7 q3 {" \" kfor access to th ( z4 E* f5 G/ H9 C7 i* A/ e& nFa# w$ Y. v6 T) s; ~2 b Nose Cowl - Front section of the nacelle for air inlet t; _) y* f+ E/ M/ h# I# ^( v! Z1 ]to the engine., f g7 b, c; K( W" q Side Cowl - Cover around the sides of the engine.1 u$ B& z" ?- W Thrust Reverser Cowl - Cover around the core ; Q: @' A5 m8 w" i% F. a& ]section. 5 R3 H5 L3 l; F* p% s# sTranslating Cowl -The moveable outer portion of the ' G8 `& p+ d5 y0 Qthrust reverser cowl which is $ _; ^2 e9 N! o1 X. toperated during reverse thrust. 1 _+ t! E3 r* O标, e# ]0 x: Q% v' t4 t7 i+ q基准线的相交点。一般以经纬度的度/分/十分之一分 ) \" P/ s" ]4 g( v. N: E& u1 j& y读数来确定位置和方位。& S! [' C. C- x, M/ L/ p% r 腐蚀7 ]7 K6 B' L! ~- l2 e$ Y- N 动机外部可拆除的罩子。发动机上的构件必须要取下 6 ~5 P8 v8 E8 ]; q- I" j流罩后,才能够到。 6 J4 h0 z( |* m# F: m1 K1 R8 k' g- m# g1 |( O 机的短舱的前段。. K9 s2 G5 \( i7 d' b, M+ e9 [. f 侧整流罩一发动机两侧的罩子。 ' ?, j" L/ ]4 t- d+ g2 o反推整流罩一发动机主体外的罩子。 ' r, ?1 @- g$ d. ^+ `移动整流罩一反推整流罩外可移动的部份,在反推工 3 ~$ p) Y; t R4 X" V作时使用。 3 N% E( Q" O5 u2 Pu; |" _0 }0 Z- Q; X7 W: F# I o 4 `7 M2 T, |* W% ?location. ( B `: W( R- r5 q6 KRROSION, A chemical action which causes gradual # f# c$ X( l% d0 L( m/ O+ E" ue surface of a metal by oxidation or ) p& `1 w; l$ c$ J- h" pmination. 2 u0 F0 ]$ D; e' Y* z/ pvable cover around the engine sections- C4 A" u, B+ P' v9 J0 | e components on the engine.# X4 {: h9 v/ r k# W$ v0 b9 W2 q2 v2 ^ n Cowl - Cover around the fan section.( n4 I3 h5 u$ e) F 转换,1 g6 E9 j0 F8 G2 _ 改换到另一个方式。 - p3 o& d4 y& R1 X8 b% j' V& x6 {: E/ l8 N+ ~2 w, \ Q1 t& P: V+ v# I! o |7 k( n( V氧化或化学污染造成金属表面逐渐破坏的化学反应。 5 J$ X+ j8 }/ b2 m' o& _发动机整流罩,2 v! P5 T# Z2 h) w* f; E% j5 H) t1 a) A6 t, J" a! N1 n5 x1 N$ F5 N/ i8 H- w- ]扇整流罩一风扇外围的罩子。4 s& m) C+ P( b4 d& T G: q 前整流罩一引导空气进人发动# Q2 @7 T% T3 T7 s( S8 G4 |3 l 英汉对照民用航空词典B OEING # ~$ q- y7 `) g; FTECHNICAL DICTIONARY 38 ( U4 s0 x/ f; ?% Z( \" f5 ]% {CPU, SEE - CENTRAL PROCESSING UNIT : J4 o9 G; m9 l+ Q# DCROSS TRACK, At 90 degrees from the desired track! d( v% |* J. I, [& \4 [) g f the airplane. For example, cross track distance is the: g( i; u9 \9 ]4 b; X; ] istance from the desired track measured 90 degrees& m: R0 b4 B$ e' ? om the desired track.6 P Q% Z: u1 l$ \- C ROSS-CHANNEL, Electrical wire(s) connected from( U! ?' R$ D) G8 C$ u ne system to another like system, for example, FCC + L8 n3 Y$ u9 ]' E* Y% |" to FCC "B". E, R( s: p1 M% X) H( H9 ~ n adjacent engine or one on the other side. 8 @7 Y6 |5 F& v& jl crossfeed! D7 D% L5 P' H S! W anifold for fuel flow from one side of the airplane to the e5 K) x* R$ o& _0 i9 j. Rther side.& K1 S( M# d$ i$ `% H re7 f. U% H, w, e% H, W$ ?$ R RUISE ALTITUDE, An altitude or flight level ) S( n8 C4 T' K4 g- O; A1 C, ?4 y/ X4 j2 o+ A" E+ r6 F9 \( L1 u o3 Y9 N& A! l4 `) O" v& S$ q, U2 \ d # f! b, n8 a6 y$ q/ o5 }fr 7 x6 U2 t! e0 C; EC 2 U) t( d- K9 ]2 _! C4 a6 W9 Ao; t8 i& U! w* D8 Q "A 3 l8 m1 I# B# j0 h; l6 pCROSSFEED, An interconnection between fuel1 Y% L3 s$ t: f manifolds for fuel flow from one side of the airplane to ( A4 M- D! N# ^4 |+ s. R/ Va : h4 r* b6 B3 A8 d/ f% d: DCROSSFEED VALVE, A valve in the fue+ |& f4 H$ j6 n2 K- I( h m- f, t! l7 V/ _ o8 ^5 z8 ?2 Y) t0 d CRT, SEE - CATHODE RAY TUBE + a1 z W0 T8 i( W/ a+ dCRUISE, Phase of flight where altitude and speed a/ d; I2 Z& L( I* M) H) S basically constant.- T. x) g1 I8 _ {1 M [ C m" S, [% l' w, Z9 l6 S1 \2 N8 z maintained during enroute level flight.8 F: a) M8 ]( \. m; R. _, e 中央处理器 2 o6 {( `# e m/ a9 H- ~见Central Processing Unit.3 ]; O2 \8 W# Q- k9 t 交叉航迹(XTK),9 g' _8 @7 }/ a3 a7 F 与飞机预计航迹成90°角的航迹。例如,交叉航迹距离 % m, J# S+ ~) \! J是用与预计航迹成90°角量取的到预计航迹的距离。 . c# d' w3 s3 D通道跨接, ; ?# V- ]) Z8 ?电线由一个系统接到另一个类似系统。例如:由FCC0 E8 B1 \- g& M “A”' D) D1 Z% E! a! ]( o8 v% V* ? 接到FCC“B”." k# N" c2 @. s" Q+ [7 W 机身另一侧的发动机。8 Z6 e. Z0 w8 d5 c) Y* a 于使燃油从飞机的一侧 + S- ?3 ]5 \: x( [$ m9 |# m, [: b3 G5 `向另一侧。* f1 d, l0 m% s2 Q$ Y 见Cathode Ray Tube* K2 U* s H2 D 交输,1 h/ D3 p; H1 r5 _ 燃油支管之间的交连设备。可使燃油从飞机一侧流向邻0 R# X) _( V7 e$ k 近的发动机或在6 ^8 m$ y- ]9 T. E- B 交输活门, ; C0 ^' i7 E2 }燃油交输支管内的一个活门。用' V% w, `6 R9 Y! z f1 q* E! H0 u2 a阴极射线管, , @+ I/ W* c+ w4 W( @.' c4 L* \! z1 o) N 阶段。 % d# G0 O3 Y0 D! l+ j A航高度, ~3 A$ {* I9 J! t飞行期间,飞机所保持的高度或飞行高, r+ d+ W* z4 I- J 巡航, 7 x* U$ ^: D2 _! L: f$ d飞机的高度和速度基本上没有什么变化的飞行7 x: I- T, U% ^8 J0 a( k$ j% K" j( Q/ O: y, u 在航线上水平 - L) t% V# j1 d( q. O度层。+ ^/ b( l+ C: @5 G8 B/ K/ C+ N0 @ 英汉对照民用航空词典B OEING( t. G. i4 F* [8 i TECHNICAL DICTIONARY 396 W$ E8 G7 ^8 Q$ U, N6 x, I! N CSD, SEE - CONSTANT SPEED DRIVE ' r$ Q' Z7 ?0 ICURE, A chemical change which takes place in a resin) E4 c" O, G( Q: e4 h' K% ~1 P and fiber based component causing it to solidify. 8 E- J r7 {9 f0 C% u( ?1 g ]CYCLE, A complete series of events that take place" H( r& K& k$ q& f. ?! d gularly normally in a continual sequence.- X: I/ d/ ?6 q, J' j- c AMPER, A device for slowing down or limiting 8 L% ?+ B( `0 B. ~0 t% ^( x6 dDASHPOT A mechanical damper for slowing down ; Z( T* c& g+ \0 j3 {ovement by restricting fluid flow. . d5 r ~% G2 q6 F1 W ^D; r$ c% e: U, q3 t3 z9 O% q6 M ATA BASE, Stored information which is used as the5 J9 w! }9 _1 I ba 8 h/ v7 S1 a0 T9 g8 ^DATA BUS, A conductor over which digital data is . + U3 H" D$ @3 C& H3 \6 xtransmitted. " V* `% P6 n/ g6 C! f/ [DECELERATION, To decrease in velocity.! _9 E/ A) a6 T( y1 A0 r, g, X 装置, 4 B' v, [1 q. I% [1 ]rive' k ^( y& K _4 j re9 c, v0 ]4 y2 F/ F% h0 Q- E- Y D' Q; F, v5 Y; K D e m+ f7 \. w- ^3 M movement. ) Z$ ]: Y/ }7 O6 ~4 Rm$ K, C8 p2 E( Y# Z( _ ATA, Another name for information. / W2 w/ s0 n* b: R3 v( m4 @/ ^D# x8 s* d6 s8 n: v$ T8 x7 R% ~ sis for computation.$ I& `" v3 E- c! [; Y2 D 恒速驱动 ; j2 J) }: P0 w见Constant Speed D .9 s* A: z9 M2 s 期, - r5 c7 [6 j1 @! |; U不断重复发生的事件的一个完整系列。 * o0 m: H N) H2 W; D! J; n尼器,$ |, Y9 c B. {6 d 慢的一种机构。 ' t7 T: I. F' q6 H/ e" r* | ]1 c1 d' c! m. W( {用限制液体流动的方法以减慢物体运动的机械式阻 0 y2 [2 B" Q8 F$ U4 H5 [% f+ |: u' l* v! T7 |& b. h2 W( c$ v# w- {# [, D0 J料的另一名称。 5 _# W! S0 h# ~据库, 6 ?/ d: f' U4 l* m5 J* G& \9 e数据总线, 1 p: S) n# Y1 z! {5 X" N一条或一对导线,用来传输数字信息的通道。 # r0 o3 R' `; K7 S* e$ Z3 E! F, F- i$ f减速,9 u$ k' b7 H9 a, H& } 速度随时间的递减量。 $ O8 V/ f% z; M9 g/ L( w( W0 K2 z8 u固化,6 a0 g* S& D$ p% o+ J& u* [ 树脂和纤维部件内化学反应使之成为固体的变化过程。0 W0 x8 a4 h& ]3 o, S9 A' }, g# O* C# r* L% {7 v5 C3 Y* K/ Q6 }& j用来使运动减 # k4 }1 \2 y& G3 t冲器,+ ^4 Y3 ~: o0 B; b 器。: _( i' e0 e( ~7 F5 y8 F+ V& o: i 据, ; d: A8 [5 A a* V7 |: U( Y! m; f }$ U$ k5 F: ^* j o/ t+ p; N0 T+ \- h5 }1 h储存起来以便在计算时使用的资料。% w; z7 m. o: z2 ]9 o 英汉对照民用航空词典B OEING # @( S/ ~$ Z9 V0 P9 Z% \& lTECHNICAL DICTIONARY 407 n7 {7 [( a; [: z+ G5 p7 y DECIBEL (db), A unit of gain derived by computing the 9 [- O8 F q5 a9 Q& @2 E& ptio of input power to output power.! \+ X. g3 J& ]9 e; q; a0 | ECISION ALTITUDE/HEIGHT (DA/H), A specified# O. [6 K( j }0 g! A( | ltitude or height (A/H) in the precision approach at & e: s6 c& q! x/ bhich a missed approach must be initiated if the" x2 r v+ J. \9 O- u2 ?4 L ECISION HEIGHT (DH) 1, With respect to the ) y4 S/ @: i" y, ]9 Hproach or, ]# L1 i5 C( e: H! M execute a missed approach. ( ]& C3 A2 h4 ]5 ?proach to trigger the decision of either 1 K5 w* Z4 h2 ~$ G. R( j$ w6 xnding or go-around. ; R7 |8 c0 B) _! qECOMPRESSION, The loss of internal aircraft air # ^( q9 s* X' K2 g$ N1 kressure.7 D( O" Q8 B! q4 z9 s3 ? E-ENERGIZE, To turn off or cause to not operate. 1 V9 e* p. {0 T) q' t% brom the tanks % D+ l, i M* }6 s5 Lusing airplane fuel pumps or external suction.5 K" c" g$ ~0 W& X 算的一个增量单位。分贝+ @3 W/ W8 g$ J/ y 常表示两个声音信号或电力信号在功率或强度方面的& r2 G0 t( u( V1 O3 P y6 k 对差别的单位,相当于两个水平的比率的常用对数的十; p" }1 R: V( s) y9 M6 `8 o 断高度/高(DA/H),2 X' k Z9 ^1 r! | 在继续进近必需的目视参考没有建立的情况下开始复9 L$ j6 }" w/ w 的精密进近中的一个指定高度或高(A/H)。8 {) S7 r" w/ V9 q. ]* C 断高(DH)1,# l$ x# }; P; }0 h; {# R- ~4 g 操纵而论,指在使用仪表着陆系统或精密着陆雷 ( b& b j8 \) }8 X生继续着陆还是复飞决定的高。 $ C/ r" Z4 l* F' [飞机失去内部空气压力。 5 ~% @ m0 ^* }+ A开,- F# t7 t, v6 x 关断或使不工作。4 m$ J) q, M1 ? 机的油泵或外部的吸油装置将燃油从燃油箱排 5 }/ G$ M: T1 ^6 t8 i/ \% _出的方法。. f8 V5 J/ v+ M- W; j; e/ y ra ) q$ b0 V" f* R8 ~! TD1 }" C1 O; [- h- O9 J a1 b4 e' \: O7 G w0 b! a M4 D. U required visual reference to continue the approach has. x/ A8 r; w' ]( {9 R not been established.' r8 M$ |$ S+ k! x/ K+ d! ^/ H3 L D. o( S0 j$ |& V J/ |, ] operation of aircraft, means the height at which a 7 J. ?" d, ]6 K Jdecision must be made, during an ILS or PAR 6 o& O4 Z& }/ yinstrument approach, to either continue the ap$ E- H, ?" V* Y$ D6 w to % Z2 X9 b$ q7 g9 ^/ \( p) sDECISION HEIGHT (DH) 2, An altitude used during a* H% \$ ?+ |5 F- u* A. h precision ap2 J4 W8 l( z7 h+ }& h$ M la $ _* z( G6 t- b8 c lD2 |/ F1 p; F" u& k) q p + y. B8 n( D& P( }2 R1 W8 v: nD& u1 ]* K+ U2 B) K5 }' `, w5 @ DEFUEL, A method for removing fuel f , b# s! N4 j( K! N& c分贝, , T0 z6 S. s# e+ G以输人与输出功率的比率来推! f: p- w- T5 N) z' }: ?$ y/ X% A/ ?1 o+ P- u+ D. D4 F* j. b" W: ?$ y' q9 a3 w& D6 I, h$ d7 h: R& R3 H0 M g& W# R0 A, n1 N' _5 ]$ F/ y1 [8 p8 _& u2 c7 b) b) u# G1 V. U, o- i; k" r7 F. ~' q0 h5 ~ 就飞机! x$ l" u; D# @1 I' k+ A1 j 达引导进近时,必须要作出的是继续进近,还是中断进场. s+ n8 S7 r3 Y 复飞决定时的高。 0 h& y1 R" ~! Z E p3 ~- E决断高(DH)2, 1 L( W8 F6 I$ j9 s/ j/ ~. X- o精密进近时产 * ~, m; ~3 r, b失压,+ L! X- ^# y1 ~) g @2 |& f# T# ~$ `; |8 C排油, ! h* B9 s* j- M& ?( {用飞7 ^/ v' D! q5 V" D; h- `& Y 英汉对照民用航空词典B OEING' ~1 \+ Q/ F+ v# D. K- ^$ i2 a TECHNICAL DICTIONARY 41 - ~1 t) y7 a# u5 BDEFUELING VALVE, A valve in the fuel system for5 [6 c4 h: V% V+ ?" f W! { efueling the tanks and for transferring fuel between the ! }4 @" N" @; E6 KE-ICING, Removing ice after it has formed on aircraft. 6 l& s: E: [3 f- ^; o& Z3 ?Change or difference. / D: t" b: w- d! H/ mEPARTURE CONTROL, A function of an approach + ?6 w* c6 e0 P5 P. Q9 hontrol facility providing air traffic control service for' f; e* e! l" P/ x+ M eparting IFR and, under certain conditions, VFR 8 k4 u# B; J$ G6 gEMODULATION, The process of retrieving information( u5 d9 [. g1 V8 q0 L carrier voltage. r8 i7 v6 v. j- U ation.! t0 N a9 d! ^ lic4 v+ h: W$ I0 t' V" y creasing hydraulic reservoir air pressure to- J7 y2 S a+ k, \, a0 X mbient pressure. - z2 @' v h! k% Y箱排油和在燃油箱之间( h7 C! I0 Q% H/ ? 送燃油。 " b4 ^ d3 l. E& F冰,9 r5 N2 p6 s8 ^* X( h 除去已凝结在飞机上的冰。 4 m9 u# G& h6 [" l' D, m删去或取消。 4 X+ M" r9 l6 B, ]4 |8 j3 Y量, , [1 a! j4 G; |; y4 M变化或差异。4 i2 n% ?7 ~7 t 场控制,/ j) C' h2 z( K6 G1 J Y 给用仪表飞行规则离场,和在某种情况下用目视飞行 $ I* O3 l! y# m9 o+ J$ S则离场的飞机提供空中交通管制服务的进近管制设施 ' z. O/ _) E7 \7 R3 x6 F9 k$ g& |- o" @% w( e, B. B& y调,: o$ C# x% X8 M4 d3 F9 G7 \; Q% B$ \ 电压中获得调制电压的处理过程。% z2 k* b( \* f3 u* d( A 环境3 P* e# x+ ^0 k) G; ~. ]) Q8 ^& m6 O 力相同的活门。' a1 Y1 m( f- e, `7 b5 R4 y9 h d3 u+ a! v& a% F0 z tanks.: `" V* e% H# E7 b( w' m D + A; ^6 J7 l+ MDELETE, To remove or cancel. 1 e4 b0 o+ \& b% I1 \* dDELTA, 2 |1 G" c; f6 C: r; M+ U! ZD 2 @+ j! P* X# C7 y. A7 O0 {" }c # ^ `0 ]) K$ {; s9 s* V0 md5 O0 V/ n1 d$ Z- @0 O% t2 c; e1 m aircraft.2 L6 U8 U% K# v D ! t1 M# H/ T' z) _4 }6 C, S(modulation) voltage from a modulated9 l7 |# @, U, p! T! n' Z DEMODULATOR, A device or circuit which performs; T0 w( ^7 [# C7 p5 @& ]3 I8 F, T! R the process of demodul9 m& K$ X! l! ~+ v. e. r DEPRESSURIZATION VALVE, A valve in the hydrau 7 c0 p( k% P a6 x5 s8 f; _system for de / O' o7 C$ f( P8 I8 c+ X+ Ya " J$ X# T8 E7 [2 s f% w0 C排油活门, 2 F8 r' f3 {5 A1 S$ q燃油系统中的活门。用以为燃油* D2 ^% a; a; ^! L* H R/ y& ?& M$ H% v" h! ~) H# z$ q: Z8 R5 u5 D+ \& z+ e4 f 删除, 9 @: A* q9 w2 r( D. e* `# h9 ?7 w; Q/ m0 {- g n J5 V% `9 J9 s7 `, f4 U* z0 F7 x% q( o6 P8 _6 P! e. Z+ r- h8 a的一种功能) o" @! a& W$ @8 ]# Y* n* r8 T E+ [: d6 c6 E2 R1 L从载波 0 A' p: l1 b R( t7 S! Q解调器,6 Z* j( ^! s1 @2 w; f/ Z- u0 u+ { 完成解调过程的装置或电路。0 ` R( r+ D9 p3 g5 L9 U* X1 n% j: v$ { 减压阀,6 T" |8 }% N. ~, ~5 x 在液压系统中,将液压油箱空气压力减至与周围0 w, f% }4 i+ _: \* h, t8 f$ K# N+ z l z 英汉对照民用航空词典B OEING 9 I# u2 q) R |# b* _5 w6 \TECHNICAL DICTIONARY 429 D. x$ |# S+ o! Q5 c) y DESCENT, Phase of flight where altitude is decreasing. ' Z+ Q u/ T: }% J% z- Z( HETAILED FLIGHT PLANNING, The calculation of fuel8 l0 D" G0 o; t' D' Q; x- ^) ^; Z nd required for a trip by considering each phase of 8 X0 ]* N- e! `" n0 H" r8 z7 Qight (climb, cruise, descent, reserves).8 h' v. t- ~) b al or / I' z7 K3 l& U8 R5 uETENT SOLENOID, An electrical solenoid used for5 X* N1 i8 b- b# ^+ p- M t. ( k: C0 g- z7 t# Aspecified course or 5 u% x2 ^: E, mrocedure. : u. ^$ H! C! Be. - D" w* J3 v" x p4 x1 K, @/ w飞行计划, 9 k" I8 O" v% V- _2 h" n* g R! F- R将航班中的每个阶段(如爬升,巡航,下降,备降)都 w0 {# w, n! f- Q8 f1 N( G 人考虑,来计算该航班所需要的燃油量。6 d% i/ n- ~! G. G9 }. k/ h 用来感应情况之正常与否的电气装置。" o6 v) U% P4 K2 H- g 定电磁线圈, ) \* T# `- {. j4 L% X出接通的电磁线圈。 : n' q) [2 k1 Q# O) C' n6 S) g差,: U W: [, O9 |5 Z; ~' R* T' U 与指定的航道或程序之差。 4 r8 A n+ r; O+ O" T2 y5 Q. @用气压或液压操作的活门机构中的柔性部件。 8 P( I2 q% b7 N4 P* kD+ U, {* O; S$ `" z, [ a 7 `) C' ~/ F* I$ M6 s ]fl: `: ]9 L2 j! u, ~$ h DETECTOR, An electrical device for sensing norm 2 T. ?/ N. ]( t+ I8 n; Iabnormal conditions.2 [/ m- V6 d# F0 r D* Y. P; \; ]! `" Z0 h6 J0 }: ~# i9 J" [ controlling the engagement of the actuator outpu9 @( \3 F) u1 A& l( i DEVIATION, To change from a 0 S i' r# R, _9 m1 Vp% T7 @# g- m) X% H: k$ K DIAPHRAGM, A flexible part for operating a valve 3 C$ p: t5 |8 m6 Smechanism by pressur4 z+ v- Z( y" G6 m+ [ 下降,; v0 K) O8 P$ n: j' t( {' P 飞机高度不断降低的飞行阶段。 - C+ _( y* C) K1 o+ V详细 0 A/ b3 g# M; [# L; V/ q4 ^( q9 e3 u2 I- d3 C& |6 T/ k探测器,+ E# u) X8 ?6 J/ w) \1 R8 n6 M9 g3 e) ` 用于控制作动器输 . |$ j) D! A) z) Y9 Z- p# S* r z, ?# ?隔膜, % m( \5 R1 E/ ]8 u6 ~; l* W' V英汉对照民用航空词典B OEING/ Y/ n2 j+ l( J" N$ k TECHNICAL DICTIONARY 43( Z1 O/ _( i; [7 V2 c0 [/ |0 U DIELECTRIC, A material which does not conduct+ P$ ~5 l3 L: z/ w$ i0 \6 L electricity and used between the plates of a capacitor ( ^4 D. y. s/ s4 L0 N(condenser).! e2 v, R/ k* E nother pressure in the same system, measured in & [, p8 T( G$ e: f! v2 oounds per square inch differential (psid).0 O% }; M9 @" L2 ^) a, W, r, S* D; b! n IFFUSER, A part of an engine between the ( M/ f0 ^( K) p( e) w l2 sompressor and combustion chamber for reducing the 5 V P; F4 h* L: \2 y' ^" D% Uair pressure.2 y3 n- k& |% V9 _ igh3 W4 U- ]1 q5 p' N5 D/ j, ]: O! O pulses.3 Q, }; N, J9 _1 | d ignal that is a close approximation of the original % f! D$ u' h4 Y# p9 h; m0 G* k4 signal. 5 }( N# P m/ w# c- m* NIHEDRAL, The angle between the wing reference5 R: y. r2 ^4 y4 e lane and water line.) a+ j! F7 X( U, B/ R 的压力,以每平方英寸0 k F' h/ c5 ^" M' P: \ 少磅压差计算(psid)。- `7 d5 Q; s; K* h0 B8 P 散器, & L1 R4 [* ?( K% t( X发动机内压气机和燃烧室间的一个部件,用来降低空 4 S5 M. O1 V$ Z4 j& Z: }' g6 p增高空气压力。* t9 F6 b* \- @$ R) y3 A ] 换,% b0 \/ x1 W' U1 | 的连续可 9 s$ _1 ~ U/ ?7 u5 a( M: x(模拟)信号的处理过程。# z# ^* E7 Y! E7 \. V2 T$ S: U 反角, \7 F o' M' N- Q 机翼基准面与水线之间的夹角。, }- T+ G6 X$ d L3 H3 D" f3 F DIFFERENTIAL PRESSURE, Pressure relative to 8 ^$ F( a n; S: t0 t' p0 Da . }9 w b$ c5 O' |% F: `' Np 6 w1 U( z/ K0 `4 n; m1 ED& K- p. F2 B% ~- @0 i6 ]% ` c) S; @4 G" f- ~5 J3 L" r# b airflow speed and increasing the 2 ~5 f' `9 w y, ? Y+ A# jDIGITAL, Digital refers to a signal whose amplitude- e/ ^+ L0 S+ M7 \4 n$ Q4 A remains constant for a finite period of time. Digital # ?" {: S% u. H& \4 R- bsignals are commonly represented as a series of h 6 r( k: ^" D+ qand low( E( A, Y4 R! h1 e, ?& [: @9 v5 I* K; ] DIGITAL-TO-ANALOG, The process of converting a4 ]: M" t; p8 }. ?+ i* y, Q digital signal (binary) to a continuously variable (analog) 2 t- P* m* }1 `/ z, C4 `s 1 j- R. n4 F; P9 M4 S `8 Fs ) Q- A2 s/ S1 V; S( Q/ G8 l9 [/ t _D ; l) J; ]* Y) n c* f9 Bp; J3 {: q1 ]& n+ g: @ 电介质, ' l Q! f2 j: d" z& O5 _1 B8 q2 U6 t一种用于电容器板之间的不导电的材料。4 b% b1 q* T+ }/ ?+ f8 e 压差,, J( Q6 ?3 S' F- E 相对于同一系统内另一个压力4 j5 B* _$ B% v* n! V2 u) g9 e7 p4 g+ N I8 R7 ^, ]; z* f8 B/ y# m气流速并$ t3 P" E% A7 g" T3 q4 z- L; ? 数字式,( g" \2 @) D9 x; g+ U x 指一种信号。该信号在一定的时间内,振幅保持不变。 u6 L; M, c+ g, d 通常由一系列的高低脉冲表示。 . t% g1 l5 N$ h( s3 K数一模转 7 F# b" ?2 T3 a将数字信号(二进制)转换成与原信号相似 2 m6 e5 n1 m# H5 k; @2 h6 p. Z: u3 `$ }/ g2 D! ~. A' m' o英汉对照民用航空词典B OEING 9 @7 M2 k# j: yTECHNICAL DICTIONARY 44 . Q' r# n3 s/ W7 l! ~DILUTER DEMAND REGULATOR, A component in the / h- l5 S/ I2 S0 K" @) ncrew oxygen system which mixes air and oxygen and# e6 o6 p. Q$ [8 V h9 r upplies constant oxygen pressure even if there are! s0 ]/ I: T& b% W6 b- A, e hanges in ambient cockpit pressure. ) i' [, _$ E ~* W9 v# ~IM, A word value of light. For light control devices - dim" R/ i! e" Q" d/ L+ n; q the opposite of bright. 8 O' N4 W0 x. l1 Q: O6 u3 R% f+ q' ?IODE, A device which allows electronic current to flow; b+ A# c" Y: l. H5 N1 g/ ]6 V only one direction' ], X, D7 r* |) n/ s0 A6 [ uid in a reservoir. , A5 o# S7 Z9 VDIRECT, Straight line flight between two navigational " d3 B( R. \& J7 W6 s9 R" k, t4 G9 Haids, fixes, points or any combination thereof. When3 e- G+ ? t" z/ w used by pilots in describing off-airway routes, points" R3 N# }# [) C defining direct route segments become compulsory0 ]! `: L2 W" P- e reporting points unless the aircraft is under radar - e! E) v4 k9 v& Q! Jcontrol.3 k3 i& z! m" A 节器,# V! v& m4 P9 S2 l 将空气和氧气混合,( R8 D1 Y2 C7 f* e/ ^9 g3 q0 u 使驾驶舱环境压力改变,它也能提供恒定的氧气压力。 # L" d+ M1 x1 S9 J' n: ]. y' u' |, _一个形容光线亮度的词。对于灯光控制装置,暗的反 9 g6 w/ v5 P5 E- O词是亮。! p0 j: \1 v- q( ^+ a" @' T/ Q5 R 极管, 2 P! z2 @2 c2 Z v, @2 Q只允许电流向一个方向流动的电子装置。 ! k; U. i8 U) F器内液体的量。 y5 e: ]; S0 ]4 H1 O p7 A直飞,, _1 w; E! z* R6 t, C! h- f 两个导航台,定位点,导航点,或任何的组合之间的直3 `' v7 ^: ^; G3 _6 Z 线飞行。在被飞行员用于描述偏置航路时,除了在雷达控* g" a; i8 S1 P- K8 s 制的情况下,确定直线航段的导航点成为必报点。 + R C9 _! E% k7 Qs$ w7 f, }4 g5 H c ' ~" P+ X2 W: O" _$ OD" X' `. O- a. B3 x# E Z is/ P" N# c# ~* }3 m D7 r+ O+ c# a9 k* }% C* t. {+ k in; U/ M% p4 j7 A% ` DIPSTICK, A calibrated rod or stick for measuring a$ j* L" ? ^" L( x" a$ v quantity of fl3 l$ x0 E. E+ Z' h5 k 稀释氧调 1 D. u: t! `( H驾驶舱氧气系统中的一个部件,它 7 r4 f- z) X. t/ o" a" E6 R8 t, T% P* J* o! M% B1 h; Z: u" q7 c- M# g4 P8 J# e8 R( @1 Y9 V9 x4 c/ |; Q/ g; Z1 k( w# c* U 量尺, 8 c( L0 p* D8 L校准过的棒或尺,用于测定蓄液 " ]# i. e/ y1 \/ r7 _( J英汉对照民用航空词典B OEING \' I3 z& w; P1 S( STECHNICAL DICTIONARY 45

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