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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 ' V8 ^5 u9 n1 Y6 X/ U& i$ {' r% E! _ _, W民用航空词典 3 Q, O* @' _% c3 C, @波音商用飞机集团 , |; k2 _! k* d; ~* f2 f6 KBOEING COMMERCIAL AIRPLANE GROUP 5 |% ?( b0 l( R9 D英汉对照民用航空词典B OEING/ V7 ?# s3 @: O1 g2 ^ TECHNICAL DICTIONARY 18 o/ ?7 }( a4 @+ R$ v3 m A# v3 ]2 l3 k1 w8 ~" c: e3 B1 r ABEAM (ABM), Beside: An aircraft is abeam a station k2 L, W& T: \- a" M4 d when that station is 90° to the right or left of the track of ( F8 j- m- {, v" b. }the aircraft. # h- `0 n* h# S5 ^8 W, oABSOLUTE ALTITUDE, The actual distance the aircraft # ?& M# e1 i2 y1 t! O# } C; I Nis above the ground.& R+ z* e) S' V- Z+ I& b ABSOLUTE PRESSURE, Pressure of a liquid or gas ' s* m: E y% Bmeasured relative to a vacuum.! _# c# j( y2 N$ C* u! G( V5 q- g ACARS, SEE - AIRCRAFT (OR ARINC) REPORTING / \+ O0 m9 E7 f1 F6 L" fADDRESSING AND COMMUNICATION SYSTEM 0 c+ i# H7 B; N+ hACCELERATION, The rate of change in velocity with9 g- t: I- A$ F( g! e respect to time.! A, G& @4 D f: a8 H) b/ B" W ACCESSORY GEARBOX, A part of the engine,, h& d4 z; X& G' e1 U mechanically driven by a compressor or an angle- t5 j) G) Q6 a/ R2 q gearbox, for driving components necessary for engine , j v7 N8 z6 `! G, ]9 G& x正切, 4 _% |& ^6 a! R& m2 o0 W8 [and airplane operations.( q E/ M! I) Y% E8 ^1 f2 ]3 e( K) X 当电台在飞机左侧或右侧方与航迹成90 度时,飞机正! T |% T9 ^; N0 M" D4 l* l 切电台。1 h9 ^& s0 U& n# Y6 V( S' u' M1 Y/ [ 绝对高度, 1 t: a4 E/ b& P: P3 s* D% N飞机离地面的实际距离。 . E Y3 U. c( o6 Q. |8 n; `# w, q* a绝对压力,7 X1 O: `! ^4 ]! s# v 相对于真空(无压力)测得的液体或气体的压力。" l7 t3 ]1 e0 m+ k! i 飞机通信寻址和报告系统, " }# ^! L6 c: R( m: R6 @: F见Aircraft(or ARINC)Reporting Addressing and , ]! ^ \: Q5 w( L5 E6 ^) RCommunication System. 6 Z! }' ^* f! X& S加速度,0 o- `4 Y+ i% K: V 随时间变化的速度改变率。 ; [" z! p# V( h' K附件齿轮箱,# u7 P, Q, y% D4 c2 P 发动机的一部份,由压气机或伞齿轮箱带动,用来驱动1 w9 i6 X4 a2 X% B: o* h( z 一些使发动机和飞机工作的部件 - h+ o1 c: \7 y1 M4 B$ F. K! A& s英汉对照民用航空词典B OEING1 t Q2 T0 S$ ^# `: V2 ~ TECHNICAL DICTIONARY 2- S$ L+ O9 t3 c2 \. |' c ACCUMULATOR (NO. 1), A container with hydraulic ) P2 w* u, L! e6 m' Q! Ots when normal hydraulic supply is not ! h6 d$ _/ ]: v3 r5 Uvailable.& Z: M3 U7 K' U8 ^: z7 J6 y; a CCUMULATOR (NO. 2), In a computer, a special ! [- ^. R W# ^8 {2 @, m9 Otorage register associated with the arithmetic logic unit,$ `' J. E* S( Q. O olding the results of a computation or data 5 a) Z. h& |7 Y& ~- f& _ACTUATOR, A mechanical device operated electrically, * X' c p' t, Q% R/ phydraulically, pneumatically or mechanically for$ f0 a1 y; Q: H6 E; X8 p0 N7 N' e transmitting motion between components. 6 r6 ]- ?) n' i' S4 {% `- Q/ RADC, SEE - AIR DATA COMPUTER 6 z6 u$ M# N# a \8 x9 GADF, SEE - AUTOMATIC DIRECTION FINDER d1 T: g" ?9 y. N8 I7 A( ]" iADI, Attitude Direction Indicator, An electronic display of) ?6 ]- D6 G- P" K airplane attitude information in pitch and roll. - n l6 D4 y5 c. I- m蓄压器(NO.1),6 N" z- B& k! t% T1 K 含有靠干燥空气或氮气增压的液压油的容器。当没有正. V) x" l3 D6 T( p5 X 常的液压源可用时,该容器可用以驱动部件。 ; @3 V5 [- L) P% x6 ?8 u! n) V存储器(NO.2),6 o, s* c5 m$ N M' C0 t 计算机中,一种与算术逻辑组件有关系的特别存储寄存 0 x1 w, I, x+ Q! j9 w2 D器,用来存放运算结果或数据传输。 - K( c$ x* a: p飞机状态监控系统,' U6 _' W# I H1 u, M, d 见Aircraft Condition Monitoring System 3 R" a: F O" t! Gfluid pressurized by dry air or nitrogen for operation of+ U/ ]: d- j ]' v$ R& `" a componen 6 s) V0 x2 ?0 s& O0 e, ka/ U; s) P" R; A3 G4 a* ? A 5 ~* q# K5 K, i: Z2 v0 d, @ |s8 O% U# F+ ~7 ]+ V used for h / e @+ I2 a& ^! Qtransfer. - B" u/ V1 l8 i; w/ B; iACMS, SEE - AIRCRAFT CONDITION MONITORING+ Z* a5 M; J' h: B/ L% \ SYSTEM ./ e/ b: ^2 ?1 w7 m0 v 作动筒,2 h7 S# s. w* @1 _8 V+ E* _ 由电,液压,气源或机械驱动的机械装置,用于传送部$ e d- k# f5 M5 b4 G 件之间的运动。 ; Q% J+ n+ O6 l& A& {大气数据计算机,# T* l# m+ y8 c3 c 见Air Data Computer.7 E' W" H% u1 W$ r4 C 自动定向仪,) P5 F% |4 M3 F9 s# p, n- U2 W 见Automatic Direction Finder. 5 g1 H! R7 w* X姿态指引仪,# C: C. o! H/ R; C# g 用来显示飞机的俯仰姿态和坡度的电子显示。 1 ]& a8 ?3 l9 s/ ?, x/ l英汉对照民用航空词典B OEING f: L1 q/ ~+ r6 d2 [! q- a( WTECHNICAL DICTIONARY 3; W& R3 n! i0 h0 i" y AERONAUTICAL RADIO INCORPORATED, ARINC is , d5 J; @; {8 x+ A/ p1 h2 j! C,3 _9 Z/ H b" }9 Z7 B nufacturers, and foreign flag airlines. ARINC ! N, |- e$ f4 X- o" z# qevelops and publishes standards for electronic & o' U% l& @! v3 z7 Q" T# y, k8 Rquipment and systems.6 U4 Y' f' E7 t# k GILITY TUNING, The capability of the DME to / ] H& a8 ^6 m. }# a# a, p+ B1 Ulternately tune between two different DME stations in 6 n, B5 y% j# e' Z6 H' E' n; Grder to get two distance readings from one 9 A. f- z6 `1 p, V% pterrogator. 1 c" W* g2 n9 E9 O/ [+ B! Uge- Y4 L( S: S0 g, a C- J ILERON FORCE LIMITER, An electro-mechanical & ~8 { L0 Z4 lIR CLEANER, A component in the pneumatic system ) M. @& T/ W- b. u" eupply to the air! d& n' `) m+ ~ onditioning system.( E* n3 R( e1 [+ |* i9 v* v2 P' @ 订并出版 ( v% a. ~5 B4 B: w# L9 u子设备和系统的规范。 5 [: b/ V# d" i5 C/ |快速调谐, |. l( g8 F$ _- r" A机载DME通过交替调谐两部地面DME电台以测得来自! h, }3 W3 v3 J6 C3 r; ?: j 同一台询问机的两个距离数据的能力。 ' B$ ~; R" f" ~% t5 L5 w+ a翼操纵力限制器,. O) ?" | F3 d4 M( N 装置。在自动驾驶工作期间,用来限制驾驶盘6 O: ]; e$ C* l& L 气清洁器, & S0 @5 F3 L _3 V' z/ F部件。用于去除供空调系统使用的发# S3 q$ a& _6 G& ?+ |: V! u; j# i a corporation whose principal stockholders are United + ?' \+ h( j2 g% A/ d5 p8 E; OStates scheduled airlines, air transport companies( n$ K B4 u4 t. i( U aircraft ma. j2 w2 ]# j* d0 F9 q* L d , R; z2 t9 F& q+ J3 Re7 y5 ^$ k/ x/ @ A / Z7 y0 y& m. q$ O1 ^8 f: O1 C$ r6 Xa 5 U3 x h8 d. f/ ]3 A3 o* a% `o0 t6 ^; g, W: @ in' l _) f) f/ x# J; R$ }8 D AILERON, A hinged moveable part on the trailing ed # t" X r7 ?. [: x2 c8 ^. ?7 aof each wing for airplane roll (wing up and wing down)4 W- Q8 W; |/ v" t control.# {0 ~3 w" E% j7 O; J% U A9 |' a+ Q* l0 I* U+ e device for limiting the control wheel movement by the $ w* ~% s' [8 b7 Uautopilot during autopilot operation.- y3 g7 U# G2 C2 w' V' L1 N A1 y" \- m- r) x for removing dirt from the engine air s' {/ S3 }7 Q% K% ] c 0 J6 m; K1 s7 @! ]$ \% n# n9 L航空无线电公司, . h* h2 J4 J0 ]3 |5 ]6 g9 U4 O主要股东为美国定期的航空公司、航空运输公司、飞机 * |" X, w z4 T+ }制造厂和外国领队航空公司的组织。其目的是制 ; A, ]; k" V6 I# ?1 w( E$ j% S# }# f0 }3 C% H; `& L 副翼,- ~5 p1 k7 c7 W* Y% q 铰连在每个机翼后缘的可动部件,用于控制飞机的滚转 , [7 q) O$ ~6 T4 I) \& V(机翼向上和向下)。# @( a: h9 v0 d+ G5 T5 `6 J& G1 r& ^. |- t+ x3 n 一种机电* }$ x- ]. Y8 Y4 H3 R+ q* y 的动作量。 ( ]0 [5 C. k9 c' ^. ]+ e2 ]5 B0 r9 M H% T& Z0 i/ i# C气源系统里的一个 ) \4 A+ e4 W5 Z6 ]动机引气中的灰尘。 7 z7 L4 D) Z$ {英汉对照民用航空词典B OEING& ]6 r$ G% [& u" I$ e$ z TECHNICAL DICTIONARY 4 / N* R& k% G" v- |; w6 xAIRPORT ELEVATION/FIELD ELEVATION, The5 R5 |9 d/ Z. _" C5 c j0 Q highest point of an airport's usable runways measured 5 o: N4 n& l( P0 Kin feet from mean sea level. In a few countries, the. E% r5 Z7 g. C7 m6 j4 G3 B4 E; u airport elevation is determined at the airport reference: J! `" U. K3 ?) l* ]: N point. * R, F$ _8 J9 l! X! E) bAIR ROUTE TRAFFIC CONTROL CENTER (ARTCC), 1 t7 w2 o+ b5 _5 ]& @- y2 l4 {" R8 service - F% m& x# P; m5 W* Yase of) ^$ @+ P6 V; u5 F% ~7 ^ us flow of air traffic.6 Q# F6 `2 i7 G4 Q0 L1 k IR CYCLE MACHINE, A compressor and turbine on a 0 ^! ]) M3 \: uommon shaft for cooling the air in an air conditioning) d, I$ J: m v! I ystem. The air is cooled by expansion from high to low+ R( K1 u4 Z5 b. `5 Q ressure across the turbine. The compressor is driven - e l8 |9 \8 Z/ z* f* Ry the turbine. 9 Y% s" f$ A* M& Y( c+ `) l4 {中航路交通管制中心(ARTCC), $ g4 z* S: W \8 _0 h域范围内使用仪表飞行规则飞行的飞机提 . v3 f6 z) }8 n' c9 q管制(ATC), % y( x, z, ]5 u! ]/ D4 X0 y2 W. g: l涡轮冷却器,1 ~/ _: ~+ R/ @/ v$ H, s0 H 是装在同一的压气机和涡轮,用于冷却空调系 $ m5 I3 d# v8 N4 o统中的空气。气经压气机压缩后,由热交换器移去热量, ! G) F V% V* D! S$ t- y$ P然后经过涡轮令涡轮带动压气机。通过涡轮之空气,温) j3 V+ [4 E T 度下降。 5 n- P7 @! q5 Y$ zA facility established to provide air traffic control s' z Z$ ~- c0 K- S( Q+ Q4 W4 ^ to aircraft operating on IFR flight plans within controlled$ [8 W5 O, S' H+ ~* h5 N( n( ] airspace and principally during the enroute ph3 i! u# `0 N$ D4 P r( x: O flight. 6 ^" e- J9 [: g- ^* c- Z, X/ KAIR TRAFFIC CONTROL (ATC), A service operated by 5 r; S0 P) C& z4 a/ C& I! Oappropriate authority to promote the safe, orderly and2 H g3 n- Y! I# ?- W: F& j expeditio9 k# [7 Z o# v4 ~ A # I3 ]& b8 T; l; C$ }c 1 U+ D' {" C' e7 Bs# G7 ?% J2 ` E' ]& I; P; Y p & h) Z( d; B# O j: Jb7 t5 h7 J- w4 s 机场标高,& Q- J. V; f r1 F- s 指海平面与机场可用跑道最高点之间的距离,单位是英 , u s! y1 s0 {- n尺。有几个国家的机场标高是由机场基准点而决定的。 ! X! _0 O$ W/ L5 T9 ]8 K% O6 r- `* ~5 u3 b" c- J 给在控制空2 L+ {4 ~: W; M, s 供空中交通管制服务的站台。 * M N! x7 d( o% U空中交通+ X' `& ]; R) C. E; l( U 由有关当局管理,旨在促进安全,秩序,和效率的空中 6 V: b6 d3 S8 Z' z( g+ l8 t交通服务。4 g, |/ l; \1 e6 d( L8 T 根转轴上 9 \, D! W* h# q! Y7 Z# ]+ i( j3 V+ y" f7 |4 ^/ @& d1 @! B ^' Q 英汉对照民用航空词典B OEING ! G) F4 y5 M5 q1 z& l, L1 l; @: u& yTECHNICAL 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 produc7 F, d. ?, F) L9 _; U' A4 D5 a6 H data information, such as altitude and airspeed, based 4 \- g+ ^& C- r; ~on pressure and temperature measurements.5 [6 R% K3 k3 E" \4 d! Y es air. s, i V% X, z! W2 y d& V7 q IR TRAFFIC CONTROL, A system comprised of $ {4 a5 K3 f9 \5 r6 v5 c/ Xround and airborne components used to identify, track. ?- z4 g& C" D1 @# B) m; z OUND SENSOR, An electrical device operated$ q! x' O c; H Q y the landing gear, which transmits on ground/in air) {. J) W5 [2 m% |% X formation for system operation in flight or on the E, v; U. T8 ?9 _ round. 1 }# s9 i! A \* l* h: c, ZIRBORNE VIBRATION MONITOR, The AVM takes # G/ ]9 R; w. t8 A* r. A4 ye signal from the engine mounted accelerometer and # c# D& I$ |- c% K9 G$ ualculates the vibration on that engine. # g8 T$ [+ @7 c$ W# ]3 {corridor equipped with radio navigation5 K- @4 K) y% W8 ]* v9 g* y aids. 0 e. k' f) F! ^6 z: oAIRCRAFT (or ARINC) COMMUNICATIONS 4 d k5 g$ U) L; f2 \) dADDRESSING AND REPORTING SYSTEM, An 8 H. F. Z# r9 W7 Maddressable digital data link system which permits the ) l% Q2 ]$ Q: k: |! Vexchange of data and messages between an aircraft , z2 W0 T# r" y7 K7 l. c, |and a ground-based operations center over a radio6 r- W/ E4 Q9 j& N network.+ N+ z( ]) _; `! t( M. @# D AIRCRAFT CONDITION MONITORING SYSTEM, A/ a8 W$ Z* ?1 s! X5 s8 W system of sensors and recorders to monitor various % n; c) X& R2 i6 eairplane systems' performance and status.: C! e" `0 {+ H- U 机, 0 {) r @5 v, n: m4 @中交通管制,; K! d$ V. E* Y! z ^! l7 e 一个由地面设备和机载设备组成的系统。用来对飞机进 ! y! m+ z: T* J地传感器, 2 c9 h: P& U7 ]7 w- j一个由起落架操作的电气装置。用于给空中或地面的飞& p$ u2 E, C# S+ V: y' L" p% x8 z 系统运作传输地面/空中信息。(有些系统只能在地面 2 C$ R- M2 I6 e! u用)9 ~; F. S! h8 O2 V" e 载振动监测器(AVM),$ Y) t; O0 P6 S* R, t8 C& u AVM从装在发动机上的加速器取得信号后计算出该发& _! w E7 ~# a b* B, t 机上的振动。: w+ A3 W% t2 C+ X5 d 式建立的控制区域,内有无线电导航设备。4 E+ y/ k6 I! W7 @& B" s* F 飞机通讯寻址和报告系统,3 [: N5 {, N q" M" W9 H9 [8 F: p2 A 有种可寻址的数据通讯系统。利用该系统可使飞机与地 $ Q/ f& h' _9 f& e4 s3 W面操作中心通过无线电网络进行数据和信息的交换。) [+ ~9 w! Z& z! I 飞机状态监控系统, 4 N8 `5 g- u* P1 o8 n- f% v一个利用传感器和记录仪对各种飞机系统的性能以及5 n0 g7 x, K! Q 状态进行监控的系统。5 ?6 F3 g# Z$ e4 U A% K5 D& x) B: i g/ P t6 Q' g: y' o and locate aircraft.+ I' \6 C& B9 F AIR/GR 1 i3 K+ f: t$ F& j0 g* Eb # G; R' s$ y/ Q8 v- h$ a, t2 ^in - A9 l8 ?% `. h% lg 5 e+ G! M1 r9 b8 w( J& N6 y6 O9 MA b/ \/ \! X8 J' lth- o3 X. M) ]3 [. h( u# c c $ U3 w6 t) e' `9 r# B6 ~' Y5 F9 WAIR WAY, A control area or portion thereof established ' M: ~6 Y1 e! ]in the form of a / \# q( S5 C# P/ M大气数据计算9 [( `1 W$ b0 _( T s 根据量取压力和温度而产生大气数据资料(高度、空速 2 Q1 e. D! F# q! O等)的计算机。# Y, U: P2 C x4 E+ v" K) F: c' h8 i7 o0 V% m 行识别,跟踪和定位。+ J3 P- H; o4 X! H: ^: @& H7 c N+ y* |; T! w5 z# u3 u5 u& L' w: L使 8 a! ?1 Z6 u1 `% P7 b9 w# {" L, X y' |) U0 q5 j# F4 j) J2 [. g7 a8 a- V航线,9 b/ D5 I! w- ]6 `% d. _ 以走廊形# q- h1 d$ W7 l- s) ~$ w 英汉对照民用航空词典B OEING) U0 y5 f) x7 A/ F9 S1 w1 _ TECHNICAL DICTIONARY 6 ! K/ n# O$ C' H8 Y9 \AIRFOIL, A surface designed to obtain a useful reaction,7 u8 M* r4 k; G3 U1 [+ u such as lift, from the air through which it moves. Wings, - V% ?( e# x2 tstabilizers and control surfaces are airfoils. 7 q& M+ ]# A; T; EAIRSPEED (IDS, TDS), The speed of the airplane 5 p' i( p) q6 arough the air. u4 t/ ~( j8 u0 KD INDEX, An adjustable pointer on the ; t; i# f" H0 M% U3 N8 {2 Uirspeed indicator.8 z& B3 S3 \* y and legal ability" a. K) k' V$ E, y; } _& C fly.6 ?" w9 \* n/ e" c% O; X. F% o m, for example, the procedure for finding the% i3 r% h* d% J( J: i quare root of a number. " v9 B V/ C+ A' N6 q! u" b& y& K0 Py 8 x3 d9 i l# A" ^# i) C" Are, wind,% V' `$ \( Q. x and aircraft flap setting.! I* p8 C" X. @ 是翼面。 $ U# |) @; w: Y/ N8 @5 v速, 0 n/ ~% h) H7 `$ [& E飞机在空气中运动的速度。 ! s0 H/ {* u0 @9 z- i% V9 n- Y% k# h/ V0 ~1 R 在空速表上可以调整的指针。7 m2 i T" @" \$ |- T0 q% ~ 机械飞行能力、和合法性的飞机状态。 ' Q) P3 ^$ X1 r }& L7 k6 m一步一步的解题方法。例如,计算一个数的平方根的步/ ^# H' r$ _4 ~7 c+ m. O) ~* N9 O& J9 X. g. k) E- O/ O* L" l' f 资料的法定文件。 $ C# d* R$ O/ q6 q/ ?翼位置成函数关系。 1 D Q) J+ Z6 N+ \+ K; @9 Hth0 I4 {- c3 b/ z- Q AIRSPEE ! u; F2 c" r( `& M5 i+ N8 i' i4 ?6 ^a 7 | ^8 D8 D4 W& J# E! jAIRWORTHINESS, The condition of the aircraft with$ A5 o9 E: Y1 f. T+ j& Q respect to its aerodynamic, mechanical, ; T i# `" D5 U# i; X2 s6 F, B* oto + e, U6 Q$ f6 ^6 EALGORITHM, A step-by-step procedure for solving a 9 k( L4 Q8 z- b) gproble. M# i( O4 @* x3 r) `( E, d s a# ^ ?4 `5 `5 |+ J* W AIRPLANE FLIGHT MANUAL (AFM), The legal' j9 c! d# S, K, m) p: ] document containing performance and operating limits, ) C! e$ H! G$ a" Doperating procedures, and takeoff and landing5 W L8 \, J9 `1 ]; Z: ?5 q performance. , q; h; p2 c8 h+ R" n5 f7 JAIRPORT ANALYSIS, A comprehensive set of takeoff* [$ e* w4 |$ v1 z weight limitations for a given airport runway, generall $ o L1 I4 n3 n, m" k: Wpresented as a function of airport temperatu 1 X# K% J; o& @0 P% o翼面, 0 ]" f' h; V# p2 R- u+ ~2 Y用以从气流中获得反作用力(如升力)的表面。机翼, $ g- D# W* ?6 e, n安定面和操纵面都: a) }( i$ L G3 L; N R7 t6 D: M' U7 C) e/ S/ b/ B 空速指标8 ]- ?, `9 r+ g6 P% \8 X 适航性,! R8 ~6 I" k0 i$ j( S9 ? 有关气动能力、9 \, m4 a' h% s 演算法,: w# A+ g. p. A4 g3 R# _) X' ?# v3 K" u }+ I4 o; k飞机飞行手册(AFM), ( W( g+ _1 J% o0 _包合性能极限,操作极限,操作程序,起飞和着陆性 % `' ?6 h4 A) |, o: m" d& a' z" f& G6 S, J8 F* p E机场分析, 3 M( h" V1 }' b& z一套针对给定的机场跑道的详细重量限制资料。通常与 ) _# q& D/ [; i( H! @% h: @! S: z机场温度、风、和飞机襟. H9 i% k* G6 _; S, m1 | 英汉对照民用航空词典B OEING3 m( ?7 S# V) e. { TECHNICAL DICTIONARY 7 3 ?( b6 v& p1 D6 a! a$ S, ~AIRSPEED BUGS, Adjustable pointers on the airspeed 3 ~: h9 f0 P c$ L# Bindicator. * `! ?: j6 u p; U6 M3 `ALLOY, A mixture of a basic metal and small amounts & G) T9 F: q" H% T) ]f other metals to change the properties of the basic0 R, P9 E' y' U etal.. u* |* N: k0 ? Minimum airplane speed.- n; d+ b% v) N, J9 h e of 5 t9 f' g8 k: U# H/ litting airplane angle relative to( @' h8 A1 X2 M0 w irstream for the stall warning system.& {' L: L3 _! [* \! R8 J- M another.( R! I: b- u" ]2 J. I9 f LTERNATE , An additional airport selected during * ]* v$ j B: G6 t7 M H7 G+ K/ J' P5 u0 C" D7 e, e合金, : o7 l9 M, I1 c% k在金属中加人少量其他金属,而改变其性质的一种金属 7 A' e- v8 e; F: O' Q6 [1 z, u5 p _合物。 7 w9 R7 H8 ~8 b# K飞机的最小速度。 ( Z! J- W3 c- z9 f速警告系统传输飞机对3 [2 Q1 R6 a7 u# m 流的相对角度。- k/ i( w: D% M( { J1 g 由一个状况改换到另一个。 % u; n& P* F( G- n7 X降场, : B$ ]- r- _3 c" @9 [5 V划时,除了目标机场之外,所选的另一个机8 l" N4 d1 Y/ Z+ |. ]4 E* j0 M3 d o$ K/ R6 W% C7 x6 D7 Z$ r m # p4 z; ^' ?3 b1 w9 ?ALPHA SPEED, p6 B! x6 d+ }6 M6 {" D9 | ALPHA VANE, A small moveable airfoil on the sid. ]4 y6 ^+ Z" q- I' e% s the fuselage transm 2 @* O2 e& i1 O8 _a + ]# ^3 A% y/ [4 C) j3 A% _: [ALTERNATE, To change from one condition to+ _) D& M0 c p; Y" U4 V# A$ B A 7 |" W7 S( b9 D) Y( }flight planning, usually near the destination airport, to be: x: G, n) q/ S! i9 h used when it is desirable to divert from the original/ u* q5 G2 L. `! N, ^ destination airport.% |) e" q2 a1 N3 w) v 空速游标7 T1 ?2 @3 P) L' \ 空速表上的可调指标。; G9 _8 w; A9 f6 A. I; V/ b9 H' \: R- L! k迎角速度,# Z* a& X o5 g2 L6 C 迎角叶片, 7 v1 K2 z) x/ q- r+ V位于机身侧的可动小翼面。为失 4 c: t# {/ W9 T/ w: u* w% P" g! c: k: g" J4 W1 g 交替, - l" h* v. Y/ ?4 X8 F9 z3 u- ]) f$ q, ?制订飞行计; e" E( e1 @" Z m 场。通常在目标机场附近,以备不去目标机场时,改降之 ( r$ G" ?0 e# g1 N# j, Q用。& w! _0 ?3 [# _' H" j, ` 英汉对照民用航空词典B OEING* {! J2 c+ N5 I+ \" P6 T TECHNICAL DICTIONARY 8 ; P5 L# ~* L6 |1 L0 @" l7 o1 SALTERNATE AERODROME, An aerodrome to which 3 u7 L$ p- c0 [ Uan aircraft may proceed when it becomes either0 ?! h# l. S% h possible or inadvisable to proceed to or land at the$ K! F/ ?+ C9 T% R& Y+ ] erodrome of intended landing. 6 P4 O" g6 f2 k3 M" jTER SETTING, The adjustment of the altimeter7 J) s# y- c9 D1 t( O account for local variations in atmospheric pressure.' H9 {4 n. S4 u# ]; y8 o/ D LTITUDE ACQUIRE, A digital flight control system1 A! V% s' w) c6 h' _- e' E# T/ V ode to transition from climb (or descend) to level flight. ' q% }) x' A6 w+ w+ c. r+ Z$ xLTITUDE ALERT, A flight deck alert occuring when the, p4 b5 @1 r, m$ |, p/ D6 l irplane approaches or departs a selected altitude. : p* f6 q9 G( Q% \* P0 e& OLTITUDE CAPABILITY, The maximum altitude at4 M1 q" P3 p* d8 N% J {# g: r" Z hich the airplane can be flown at for a given thrust,2 z. Z: g8 h0 w5 t+ o' d" E peed and atmosphere condition., v4 E: f# V+ F% s7 T LTITUDE HOLD (ALT HOLD), A mode of the autopilot3 x, ^$ V d/ r/ F' R r flight director to maintain a selected altitude.; @3 w7 F) {8 i& }" c irplane's altitude during VNAV operation. / y/ {8 ^' c C3 u6 t机场着陆时,可作着陆使用的 ( V# M" F9 e9 D$ }: K N- |场。9 T% ^* L2 |( U0 U, O* W7 e4 i& X( B- m 根据当地大气压力变化而对高度表所做的调整。, D" ~1 T: w" y* S 一种数字式飞行操纵系统,从爬升(或下降)改平的模 ! v4 E+ I# z1 @5 \5 r( a( M4 U: f A8 j! i3 F& }9 a. q6 h 度警告,0 y0 F* f X# ]/ K2 _0 Y 当飞机接近或偏离选定高度时,所出现的驾驶舱警告。2 a; i' t. |6 G3 k$ _; u 高度能力,5 X( w% |' A& U( e& o8 j8 p 在给定的推力,速度和大气状况下,飞机能飞达的最大 & c( O( k7 D* f; \高度。6 U! Y$ ]) w3 j. e! ~ 高度保持(ALT HOLD), l1 B0 L# u8 J; Q" ]) B# m; l+ f 自动驾驶仪或飞行指引仪保持在选定高度的一种方式。 - ]7 u8 S) b& W% i1 N7 o& n1 @! b$ j/ ?2 D4 g( r员对飞行高度的控制。+ r0 r" J! @1 a: `) P. \5 Y) P; R8 n im ! i9 Q4 v: s/ r% g( @/ e [a # B0 _9 w: N; q" F# W& b( uALTIME) g2 O% ]" \& Y/ A( b to4 |( h. a/ G4 y A . U0 D) e7 J. H' bm % M% W1 T; y4 j0 t: m* y8 PA 9 E1 |6 R8 S E3 [1 x6 C$ j7 \a ' b* ]8 I4 a$ [7 d9 f# T' ?A 5 s3 x L- k; |, h3 ]% iw$ G6 Q1 c. X/ f# e4 D s# H/ K1 T0 R! x: E: A! V( w A! @, X' w$ y+ B. o, P o 0 S6 r1 ]9 O; r2 p9 IALTITUDE INTERVENTION, Pilot control of the* s$ r$ Y: j2 V* b- D+ w a F; h+ k* u9 Z" R: y% K, @AMBIENT, The surrounding atmosphere. & t2 z/ l% b. } l4 |/ r备用机场, 3 t% b/ V( I4 R6 M$ R. j# }当不可能或不适宜在预选5 a6 R8 Y+ t3 ]+ h# g7 B' J: k+ \4 r 高度表设定 : B2 c$ [* Q/ \. ~4 c高度截获,, ~6 E4 j$ w; U/ Q# T* J9 P U* N# c1 c0 f7 j2 V- }/ v- R+ C7 }3 I% `9 d! ^高度干预2 Y! I9 Q8 a: E9 X4 b! Y' }4 A) G 在垂直导航工作过程中,飞行 x$ k! i/ m- J' @5 r# a 周围环境(地面气层), , B$ S# I$ J7 ^: @% C- h% I7 ]4 O物体周围的环境(特别指大气)。/ T$ c) v$ f _+ Q! B; ` 英汉对照民用航空词典B OEING0 Y5 u. j1 q$ l# B7 m( Y& r$ a TECHNICAL DICTIONARY 9 6 L. h! f) A0 mAMBIENT PRESSURE, Pressure of air surrounding an 1 F2 K6 b8 \* K$ U% Eobject, measured in pounds per square inch (psi) . N( [1 |& J( ~! m6 {6 LMBIENT TEMPERATURE, Temperature of air" G1 ~/ @& x* [3 k8 f mpere.5 `2 E1 D4 Q. V$ C6 q+ w urrent waveform. / [' V" P( \& E2 v& @+ yg an 0 |; m" _" t" W6 o q& X7 Y" Bnalog signal to a digital signal. 6 v4 @" k3 T. vore inputs! S) M p2 c( s. }% b f binary digital information and one output. The output % J" a0 [$ j4 x( u/ m# K6 h1 only when all of the inputs are 1. The output is 08 G4 H$ Z; [$ m4 ]7 y. T hen any one or more inputs are 0. ! C$ R; `7 R5 Z面气压),6 P2 O, P2 A: G5 ?6 k" Y* Q 境温度,' Y1 H2 ?, M! _# s* a6 n; @$ D6 V 气温度,用摄氏度(°C)或华氏(°F)来3 _0 @! K. G) ~5 k; V6 y) \1 o0 B7 n4 I$ A3 ]2 x4 a电压或电流波形的幅度。6 q+ j/ U6 N" j& B& p' t 性变化的信号来工作,或产生连续性变化的信号 . ^9 p" o% z9 a" ^ [4 C统。 0 c8 w; i, L4 C将模拟式信号,转换成数值式。 5 I( G+ Y' C. V4 u1 r一种有两个或两个以上的二进位数字信息输人,一个输# D! e# c8 Q- S. q8 Z( Z$ Z7 U 的装置或电路。当所有输人为1,输出为1。当任何一个 4 r) e- X0 Q0 |# H一个以上的输人为0时,输出为0。, z9 p5 ~9 p3 k/ x& j$ N A 6 L! h2 p. i( F) v. g* X/ A! c7 [surrounding an object, measured in degrees Celsius , K4 G# a0 J; n9 b# G+ J0 E g(°C)or degrees Fahrenheit (°F).9 |7 Z Q5 H* c; ~* e) P6 t" Z AMPERE, A unit of electrical current. One volt across ' Q1 ^* ~2 R5 v/ i, Qone ohm of resistance causes current flow of one: d7 h( u( D# T a & J7 x' x# ~0 G& KAMPLITUDE, The size or magnitude of a voltage or " g: {5 r% y4 L" o$ _+ Jc ! D; o5 m* g7 G" P9 _: P x+ rANALOG, Quantities or representations that are5 u7 D+ }# D* n# N variable over a continuous range. # m( ? f3 X1 u; j& q8 W0 O) P' BANALOG-TO-DIGITAL, The process of convertin * P0 y& ?4 g2 I/ f r0 n. p) X/ N# da + `# [# T, W; d+ ^6 A# AAND GATE, A device or circuit with two or m # N' b4 z+ L' a# q& [& B* Yo 8 V$ _) U7 H# @( ~; \! a0 s2 Uis 8 [2 o: p6 c4 Q E4 C( nw1 H- D# Z2 j. c" r 环境压力(地7 M9 c, @# s1 ~; _% O 物体周围的空气压力,用每平方英寸多少磅(psi)来 5 `) n1 Q5 e( o+ Q9 ^9 j" l, ^; J度量。 + H4 f3 z1 A1 w9 `- n, F( U# L P: U& U; ~. N! M 物体周围的空9 [2 B. M# H" w* L, S) S- \1 W 度量。) K/ z0 F7 F6 `' c7 A 安培,. M3 |( Z9 ~) R0 x. u: M4 ^ 电流的单位。9 z9 \+ E4 x9 z- n 1伏电压在1欧姆的电阻上所产生的电流为 - j1 D4 `& {! v$ t7 q1安培 8 ~" \* p1 @7 X* P& H0 G振幅, - c0 d! l/ \0 w7 w模拟式, $ A; H- k7 \# Y" M8 t8 r4 O用连续; j5 v3 ]1 V& P7 u: \+ j4 ]2 U% u4 r9 r$ @ e* w! m$ v 从模拟式到数字式, ' p* A \& Z* k# v与门, ; W# S5 V& X# W) m5 E- n- g2 o& h) E5 ?" i- ?! Q- _5 U# o+ Q" S3 ?3 F9 f# a英汉对照民用航空词典B OEING ) t$ q: Z- p; a3 TTECHNICAL DICTIONARY 10 ! R# |! E3 u* \) eANEROID, A sealed flexible device containing air at low X _6 G& }: A, f! ~% l3 U1 _pressure, which expands or contracts during change of) X4 [) `4 S' y% a ressure outside the device. g8 i0 G3 n& {) n& b' u ically # M1 n( M% b0 v! K6 R3 b: i* \1 Kr changing the direction 7 f4 {$ Z# W w2 P% @- uf drive. 3 G y1 o2 g5 S/ w/ K+ }( |of the wing chord in # H" B4 y/ u- ~" B- Dlation to the free stream airflow as it moves forward 5 Y9 H. U/ ~' b1 ^! Prough the air. ; e+ j: ?# b- I7 f$ r E9 b1 val axis of the& h* |8 E4 w5 X% t3 |1 u1 H0 f aircraft. h6 F/ a- ^3 I$ K0 T' _ 胀或收缩。 3 G# a2 o& M y) F* G; q箱。是改变驱动方向的机械装置。 ; k8 t h8 L1 V* W# t机翼翼弦在空气中向前运动时与自由气流之间的夹角。! O" s- A- R; P# V( u( C/ V& u6 `% m1 v( o( [. U4 ?8 ] p , R& M# ? f- w: y0 pANGLE GEARBOX, A part of an engine, mechan% Q6 q9 \1 w1 i8 W6 p5 x% ^0 E- i# ^ driven by the compressor, which drives the accessory 5 y2 I0 h7 [8 [* @# _gearbox. A mechanical device fo 4 w8 X8 S) M3 a0 no 8 {1 {. w- z! Y c `ANGLE OF ATTACK, The angle/ @1 a/ F$ ]& K- ]( |9 N9 c7 z re: O+ C7 `' I* U8 T; ^; y9 o6 | th" L) {# G# w% w/ S: I6 r ANGLE OF INCIDENCE, The acute angle which the : p+ j! }9 b" jwing chord makes with the longitudin( j, t- r! I! S1 f 膜盒, $ d9 ^5 P) V$ ^4 e9 F" l; r9 ^内含低压空气的密封弹性装置。当它周围的压力变化 - R: b- o1 Z0 C/ f3 v3 u; q, r% i时,会膨 ' B; T* U6 K2 ~8 Q, ~1 x伞齿轮箱, 6 ~ B2 u9 V7 \/ j8 d M, P发动机的一部分。被压气机以机械方式驱动,然后驱动: ]* F w/ H7 T4 h1 d- C4 f 附件齿轮 : o: O2 t- @3 |1 ]# K' p+ G- x迎角,5 m, v% {, J1 c 安装角,0 ~/ y' W- p% W) L- l 飞机的纵轴与机翼弦线所形成的锐角 ) S9 ]+ O1 _9 i6 g7 H* [英汉对照民用航空词典B OEING 9 O; r: b9 }" l+ m- b7 W# hTECHNICAL DICTIONARY 112 c3 _6 g2 a5 `! v! O9 i ANNUNCIATIONS, Audio or visual indications used to# V# B1 [' f: ~ call attention to an event that has taken place.! J- \2 N( M# ^/ J! r ANNUNCIATOR, A visual device consisting of a number1 L, N$ b% @: o, A& N) E ly.2 p: }2 h% Z) ~; d0 k ANODE, The element toward which the principal stream9 u+ X7 Z. @0 I. \4 C P8 H. s1 l of electrons flows. 8 [' Y# `. m5 C3 V, u0 cANOMALY, Not normal. + x w3 Z# x0 A* o8 EANTENNA, A device which, used in conjunction with a, t5 Z" I% @* q transmitter or receiver, is used for radiating or receiving 5 v4 I$ |/ E' s5 F* ~4 K& m+ Fradio waves.9 G y$ L4 @$ d$ g NTI-ICING, A method of preventing ice formation on ; w, D+ G0 Z: @+ Ve wing leading edges and engine nacelles. . `5 s$ c# P7 h1 C+ s$ e: qNTI-SKID, A system for providing maximum braking 6 t1 P/ j7 ~- J; O9 h {ithout skidding for any runway condition. Anti-skid9 J k( q Q- J6 _: p omponents are part of the brake system., T& `8 Q* \9 a% w! `+ W5 z 告,+ `/ Y) x/ v% k) g3 r' ~! c: S 当发生事件时,以声音或目视指示形成的提示信号。 1 v3 J G0 `4 W5 l: Y) w与之有关的电路的现有情况或已存在的 + K& s4 Y3 A X3 k; F* n6 R, V9 N4 o& y2 [; H 正极, ) o# O$ r/ ?4 K: q( v; T/ n主电子流向的极位。 ' W2 i( f _# b异常, - l. x' |: s' |. y不正常。 ; Q) f9 k1 y# }- C天线, ) N/ i# Y+ H' @* p7 G: Y7 j一种与发射机或接收机共同工作来发射或接收无线电 5 s% @' x Y- y: V波的装置。8 l; g% {5 `% b2 ? 冰,/ i& Y. K: U9 b 防滑系统,. T$ o6 }3 q! X( W, q% C 一种在任何跑道状况下,都能提供最大的刹车能力而不6 f' u9 d6 O5 H 使轮胎打滑的系统。防滑部件是刹车系统的一部分。( `% y4 M q+ q( d* q! Z+ | of lights. Each light indicates the condition which exists% D: ~/ f1 Z, B' ?+ a6 X or has existed in an associated circuit and is labeled# L; c# k, E) a1 g+ x# y according5 W( J% r% q) K A+ B2 J& o' u4 t8 b: L k! M th 3 `! i4 j3 j) r) q' e# ~3 l$ |A1 |6 X/ j: M5 t z/ W w' Z& |7 Q" m- x/ T c 7 o- i! e& S% x5 O* v2 k' P# e! G3 \0 p3 A. g+ Z. W, \- a 信号牌,( R3 m6 l0 i2 _' a; W 由一系列指示灯组成的目视装置。每个指示灯都有相应2 y0 g' z6 r& }$ c( l- M o 的标记,用来显示 8 ]1 o5 h8 p. V. h- j5 b M/ e4 i0 G! @. Q4 W2 y0 J' c. B) f+ A" Z/ M防止机翼前沿和发动机短舱结冰的一种方法。 + y6 \; }5 I% ?6 J8 S) q! U英汉对照民用航空词典B OEING9 ?" D# H9 A0 a [$ P# b( _* @ TECHNICAL DICTIONARY 122 y g6 w: y r& ?. P* C" i( T9 F" |/ u APPENDIX, A supplement to the Airplane Flight Manual5 Z1 V% c q2 T' i+ g tained in the basic manual. A7 ?. \- e, |: I% F6 ?( g `0 _ ollection of supplementary material at the end of a1 t& H; ?5 `! x ook. 1 A6 ^3 ?" x* U0 \& B% p; k- sof the 6 h9 y* Q0 \3 X/ E+ prsion link on the landing gear. 5 U) k1 {) ~; S$ @" G. O$ d" UAPPROACH MODE, An autopilot/flight director mode& n. G" i/ B6 |2 X# ]$ R which is a combination of localizer for roll control and * |; m# L; d, e4 c9 I* c2 gglide slope for pitch control. This mode is used when full% S0 Z- |6 I) W; y/ ^ instrument landing system is available.$ \5 \. B, {& C; Y0 r8 p* s APU, SEE - AUXILIARY POWER UNIT i; Z9 r2 V7 }ARINC, SEE - AERONAUTICAL RADIO8 F9 E" j* D2 u0 ~+ D3 H INCORPORATED/ [" Z2 c9 Q. M s2 h7 x0 b ARM, To make ready for operation.1 M8 X! F! d8 a. b 附录, & n. o. K. |) }$ h5 D4 M# t) X飞机飞行手册的附件,包含基本手册中未提到的飞机形 5 T# n& g/ Y/ y" n4 l9 _态的其他性能。是附在手册末的补充材料。 , t* A: m1 ] }+ j顶销, . x0 W, {* U! T+ |用于连接起落架扭力臂两部份的销子。 5 i9 {' k, U$ k7 S0 I: D! }进近方式,* W8 ^# a+ L) z% N2 d* s r; b( I 一种综合了控制横侧的航道信号和控制俯仰下滑信号 V9 I7 o/ z$ b* C7 w 的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系 8 Y3 k+ {: {! C D; ?3 q$ J统正常时才使用。 . u ]# T$ u0 i+ r% `( H- n+ T辅助动力装置, 5 t# M: a7 s+ [* u$ _见Auxiliary Power Unit) N6 S* H) x X containing additional performance for aircraft0 ~" J" B2 Y* h4 Q configurations not con. V: V# f$ M8 Y; d! L c1 ^! y( J( s+ E k; x% K: i2 P b 3 l7 c9 i9 c3 p! _APEX PIN, A pin for joining the two sections$ w8 |2 A9 l+ I2 Z to& ^( D( s0 _+ k. Q+ [; `' l1 x$ D! p |# q. f4 s" h4 i 航空无线电公司, " L) Y6 c! \1 x6 d& }* o5 k. y见Aeronautical Radio Incorporated. ' y0 _) N) `" p3 n u1 }预位, : q% K: {+ C* G5 d+ t部件可以开始工作的状态。8 y) p m+ Z- [! R) p. L 英汉对照民用航空词典B OEING {+ ?0 ^5 K5 p I# n8 ? TECHNICAL DICTIONARY 13 $ d/ E0 ~* n2 rARC, The curved track over the ground of an aircraft / W a$ {! K# { g" |. U/ Uflying at a constant distance from a measuring ; Y, L' q0 C1 b$ }7 |7 Xequipment (DME).3 p7 v+ F" i, a in the limits of self-contained system8 ^) N; M- Z4 ]+ F# e- K apability.1 f3 x6 T' @& L; r8 g2 M( s tem for opposing or restricting! w, i8 x4 y6 h' H, @ ovement. 9 Y8 c+ W' C% l6 H1 p8 L. v# T9 fSPIRATED TAT PROBE, A sensor that measures total ; p1 I) D9 s3 Qir temperature when the airplane is in the air and that - u4 o* I: o* G9 X9 c9 ^2 xeasures outside air temperature when the airplane is5 A5 F) [; W6 y! \( w n the ground. The outside air temperature is measured9 n. ~% _! W3 X& Y6 ~ L+ e* Y+ k4 _ SSEMBLY, The fitting together of a complete structure 0 O7 c( h; i! H7 \, N# L# x4 A# r& uSSUMED TEMPERATURE REDUCED THRUST, The- i. F" L# j h) _& M& K9 j ATC, SEE - AIR TRAFFIC CONTROL9 }0 n, J/ i- ^5 Q" V8 ]2 F% P$ v9 e$ f$ L6 M& w$ Z! f系统中所产生的一种用以抗拒 & ]1 ^2 f) M( [! j5 h0 f4 Z( A作或限制动作的力。/ r! x" Y' h. q' ] 头,; v8 d; }3 j2 b7 B. C7 T 用来测量飞机在空中时的总大气温度和在地面时的外" {0 n9 s4 a# S. b/ F 温度。地面外界温度的测量是利用引气将外界空气吸入, x) s7 P- N. |) p# @% ~, v; | 头,以达到测量的目的。 " Q2 S3 g3 B( ]) h& Y配, 3 r) b9 r( o8 C* f j一个完整的结构或组件的过程。 , @, w5 {4 O ~! K5 b* A1 u; {+ E假设温度而得的减推力, $ ?! n& Y$ u- r2 R i: n1 ^9 E推力设定值时,假定一个比实际外界空气温/ k. K8 }5 s6 { k# f9 v9 h 空中交通管制, . u2 Q! s$ Y) _) J: z( s/ m5 y7 L) W见Air Traffic Control + Q' v- b; O1 n# }6 HAREA NAVIGATION/RNAV, A method of navigation % H T6 A1 k, Z) O5 Kthat permits aircraft operations on any desired course( c8 B- J1 d. t within the coverage of station-referenced navigation ( E4 @0 A- e1 I2 L. t0 u& ~. v' |signals or with 0 |+ |% h* o" M# ^. tc 4 Y' {: Q/ S9 }- zARTIFICIAL FEEL, A force developed in the flight 8 \/ b s1 R' R6 K* V Bcontrol or brake sys3 e. L8 H) M! a m , w0 Q1 N* n7 A, t) J) JA& ~' l/ F9 Z* Q! e9 q a& ?' j" K7 L# }* U5 p m" R0 }( w4 q# I. q o 4 e% E9 Z, K; ^# U3 O: v9 T1 R+ sby using bleed air to draw ambient air through the+ u0 p! A9 V9 Z& g; E/ P7 q sensor when the airplane is not moving. . F, f9 t$ B* b$ D2 \# M0 s* SA" I2 U* B) u! Z or unit. # _8 E3 o: I6 L# o5 M/ { \! `A" F# O; O/ p2 u lower thrust obtained by setting a higher than actual# }# O1 T- I* }& h& c Outside Air Temperature (OAT).) Y/ f% n4 k' C: z. E8 ] 弧线, ( |% d9 x$ t6 B+ `6 ~飞机在围绕DME台等距飞行时的弧形航迹。* d5 y j7 m+ t1 O! |" M 区域导航,4 s, `; @- [+ e+ H3 c7 D8 w 容许飞机飞行在有电台参考的导航信号或自备系统能 6 V/ [$ ?. v) [0 |) c力极限范围内,飞行任何预定航线的一种导航方法。$ {- D, c' s/ i) O" x) r1 U 模拟感觉5 x/ x+ N9 `. M# I! f" n' {2 O' H 在飞行操纵系统或刹车+ Z, L# F8 {# ~4 u5 @7 y) w9 e) |, k. ^' [吸气式总温探 & {! J4 g3 _7 z9 s& O2 H' f* N" C+ w5 C1 ^0 N# o9 V! z; |. K1 c" X8 ~& e& C {" W( i组合成 9 ]& |* R2 E( B7 |# m0 i0 E/ L1 X. [3 K2 Z 在选择起飞 8 u1 [: u+ f, C2 P9 S& v9 `6 {度高的温度而得到的推力。用这种方法可以减少发动机的& d+ {. m' v* ]" v; M 磨损和维护费用。. G( d# ]& Q1 f" o8 F, j* s' w+ t8 p* l/ u: O 英汉对照民用航空词典B OEING # u" m' h+ H4 y% {$ _+ q$ X% R$ [TECHNICAL DICTIONARY 14- m h; n' Z8 L# u ATE, SEE - AUTOMATIC TEST EQUIPMENT ( h6 s4 l6 o& L2 `: t3 dATMOSPHERIC PRESSURE, Pressure of air due to the % m0 K* t* F' C% ~arth's atmosphere, expressed in pounds per square / i& \1 H( H" H4 i8 bch (psi) or inches of mercury (in Hg) or millibars (mB).5 v; D& p( Y0 p8 ~1 A* R4 z# v TTITUDE, The relative orientation of the airplane with, Q- J4 e' {2 T8 z+ h- a0 @ spect to pitch, roll, and yaw.; i2 K$ J4 R- [2 v( }% U UDIO CONTROUSELECTOR PANEL, The panel in 4 s: q7 N! A! w# q# X; w9 i \e airplane which controls and selects the routing of# F* X6 }4 s* B: V udio.' `% r! s! p0 {2 E: _; W6 {3 | UTOLAND, Automatic landing using the Digital Flight 9 x6 i \ G& Sontrol System. 2 G8 b+ O. G7 I$ a0 R% f4 Yn.% U! X% k$ E) \; h5 ] M, A system0 W. ~# _7 J) G: H. E' D2 W7 x omposed of all necessary subsystems needed to guide' p( U# m1 @$ U9 `4 z e flight of an airplane. 3 w7 X( T3 O/ bEQUIPMENT, System test6 T# N0 @6 N, y3 n5 j/ h- m quipment that operates under computer control.) q: U: C0 @" l. J+ N 装置,

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e 6 o9 k! C: l% x6 Hin* x! F% W, w' R8 w; q4 g A# r; H1 F, g- ?2 }' H& W re1 t4 J4 E6 \3 F A* k0 G$ p! H' Q th * W. b- `0 S! B9 _9 f7 Ra) f8 R( E, h @, I A # m$ T/ z/ g7 q9 M" cC( U% I! e0 w/ Q0 A# v AUTOMATIC DIRECTION FINDER, A system which . n4 R! N) V! D; G1 adetermines the direction of a radio statio 0 i. D3 u+ h1 K' f% X- e0 y% VAUTOMATIC FLIGHT CONTROL SYSTE , K) |& [+ V. Q% F5 c; j! hc 4 a# q( p- B! b0 y6 oth 0 R: f. W- ^0 p- E/ \% [AUTOMATIC TEST * E; Q& w+ i. E- n/ u( N1 T6 qe0 k# \& b+ }# c7 }. j 自动测试 0 ^; x, A t# H7 C见Automatic Test Equipment.2 k7 Q* m: i d; A! K0 T4 W 大气压力, _/ P/ W! t3 v% w i1 V" x/ u 由于地球周围的大气而产生的空气压力,以每平方寸多7 R# \6 Z, h7 M# z- W- e 磅(psi)或多少寸高水银柱(in Hg)或毫巴(mB)来 & d7 K/ F1 O. G- e示。: t8 j" t ]; }" r( W% u+ G3 ~ 飞机姿态, : m# j5 u& o; q6 ]. P. {5 z1 i飞机与俯仰,坡度,和偏航有关的相对方向。. x# _! Q/ j- m 音频选择面板,- i% X% R' Z$ Y4 U6 q 飞机内用来控制和选择音频通路的面板。 # v- k7 r; L' X D4 W% Z自动着陆,+ c* s* l \5 x 使用数字式飞行操作系统来进行自动着陆。4 L* K4 p( o% i% f3 S3 { 的系统。 8 m& E8 J1 I3 E- R6 c% W" [3 p: X& Q5 `# f系统所组成的一个系统。 1 \! a4 |9 d- n7 g在计算机控制下运作的系统测试装置。 0 C. ]9 t# N6 { u$ v7 Z; x6 B$ E- G2 a- u% o9 A H5 \: Z3 Z& F3 c; }3 ~( s" I G/ o 自动定向仪(ADF),0 S) z6 W# a; p( k% G" @5 p$ N 确定无线电台方向- C5 Y# c E8 q2 @ 自动飞行控制系统6 D3 J8 Q) l! ]7 p3 w$ M 由所有能引导飞机飞行的子 ( S$ X4 ^/ l! p; x: O自动测试装置,# B `3 i- I2 l5 R, ^' B* p 英汉对照民用航空词典B OEING . O' e5 N Q b8 eTECHNICAL DICTIONARY 15 % z( q& E E8 k. W" J4 w& YAUTOPILOT, A system which automatically controls- k, f _3 l8 ? and guides the flight of an airplane.4 Y" I [- L, b- b" j1 ], t AUTOPILOT FLIGHT DIRECTOR SYSTEM, An' w6 N+ n6 v" M, m" A5 Z0 n* {- l tor* d/ w; ^/ {0 T UTOTHROTTLE, A system which automatically 8 e. p' q& A/ Q/ m lontrols the throttles of an airplane. 8 S n" V: _9 wPOWER UNIT, A small turbine engine in 3 n/ }# _. y' ?. }$ h; V; v @e airplane for supplying electrical and pneumatic " n5 P& X6 F( `$ X9 dower for systems operation on the ground or in flight. 2 {* k( |* r' `7 F: K: NVM, SEE - AIRBORNE VIBRATION MONITOR # R1 o- A) F& JXIAL FLOW COMPRESSOR, A type of compressor A( b, ?# r6 ~- P6 j! j) c7 rsed in a gas turbine engine in which air passes through9 _ a2 s: n6 W* v6 ~" z5 \4 y$ a XIS, An imaginary straight line or an actual physical5 z3 Q3 O! m5 X5 E- [+ ~- S1 B# ? omponent (such as an axle) around which a body can , ]+ g( `6 ~5 l, [4 ?8 ^; O. C$ otate.! ?$ B6 z' D* z1 t+ v6 Z: D 仪,* L3 j, G( j+ M7 A: L. p" b+ b0 o3 O6 I+ e$ O+ M自动驾驶飞行指引系统, / c. `8 X) w) d6 \2 ^; N* Y动驾驶和飞行指引功能的系统。 % B' a& w& K$ l p动油门, $ i9 |0 U; w G6 @4 S5 t* R自动控制飞机油门的系统。$ f+ H* H$ K2 z5 A! _ 是飞机内的小涡轮发动机,在地面或空中给各系统提供5 T5 N; Q J2 d5 P1 Z+ j# Q5 n 源和气源。3 Y9 @& F! @2 C# d+ ?7 P- q 称。 2 T# V% n% L: T& @载振动监视器,' H4 i3 d! p% {5 ?- _4 }. ` 见Airborne Vibration Monitor4 S# C) `. V4 J& |" n- D2 l4 R5 x/ ]% u integrated system containing autopilot and flight direc 6 B+ v; _# O! P+ n* Z! pfunctions.) s4 r$ F* [0 |0 Q: v# t9 s A* w9 p1 b, W4 t6 K- S c 8 o$ ~, @5 w1 z1 m5 ]7 IAUXILIARY 3 x3 P: e3 H, K) e1 l' ath $ B3 W. Z$ e/ m' \/ M: up 5 j" R+ e" k- x- `) AAVIONICS, An acronym designating the field of aviation: ~ C; _0 Z0 K" N( v electronics. 9 }% c) K) F" I# w4 k: u6 _A; ~- ?# @8 |% K! [ A ; u- L* a g ou 6 g5 e& W% c) f) Z6 k z4 a8 mthe compressor in a straight flow, front to rear. 4 \; w' I. z* B' E- H% w1 \1 i; ?A 5 E/ R# s: |& T6 n s3 ?4 }+ A7 Ic/ s2 {4 f/ [& D ro & S0 K& T; c p/ \% t" Y2 P自动驾驶! @( v4 c( \7 h6 [ u% k+ o: | 动操纵和引导飞机飞行的系统。 6 v" ? k8 H3 |4 M一个综合自 & ?3 Z6 @: k6 P( N( ?; _- D4 d2 ]/ w) Q 辅助动力装置, 3 S |7 x2 J# w2 k; S2 F, `6 t* h, b9 l- Z% z8 z5 i4 r( N; O 航空电子学, 0 {2 y+ T; k i0 k5 b是航空电子领域的一特有名 3 s5 Q$ T. L4 _6 G. ~9 R4 E! d7 Q( X) d' C8 \4 X' i' i3 P! \$ K 流压缩机, 5 f9 t! P' U* v' k8 _* s一种用于燃气涡轮发动机内的压气机。空气由发动机的 & e0 k! u" H$ ~# p$ g) }+ F( l) f部流出。 9 v3 n0 T3 d; _# U* G% o线, / C) ]$ c+ k1 e( A, r可让物体围绕着作旋转运动的一个想像的直线或实际 - T2 V/ `& N4 P5 H+ k, |在的部件(如轴)。 : Y; R# `& g: z7 u8 }) j8 i& \) S+ y* S! V 前部轴向流人,压缩后,由后1 x/ _% I7 Y6 o4 }3 h+ |( {( k5 b2 E7 p) e# l4 |, r5 A 英汉对照民用航空词典B OEING1 T$ P1 ^0 m r) I! }- s TECHNICAL DICTIONARY 16 q+ T2 G0 c: ^9 [+ F+ jB6 l( {" Q, L( l8 u ACKCOURSE APPROACH, An approach to a runway5 [+ a/ D# X3 ^. r) H versed./ L0 L& q, P2 l" H; q. `# j own on the EFIS that 1 C: o* W, _) a0 N2 t" x& Woes not readily change, for example, navigational aids. % F. J6 g4 j, { C5 m7 F+ Zvement in the tank or reservoir.& |3 ]: ~7 m9 v( }0 o. c6 a ALANCE TAB, A small hinged moveable part on the* }& L$ p+ u' i! C ailing edge of a control surface (aileron, elevator, , e* W8 K9 r% l) o4 S" J3 ]4 H航道进近, ' ]- T: ^' U, f6 v+ c6 k K相反的进近方向。当反航道进近时,无下滑 4 N* z. d* ~0 i2 L' V显示在电子飞行仪表系统上不经常改变的数据。例如:5 N# [6 h5 k8 J+ i4 s5 _, O 航设备。 / B) g$ I2 A0 A9 u0 ?在燃油箱或滑油箱内阻止液体流动的隔板。 ( o- p8 `- \$ S1 f6 k% i# X5 p% e. c动补偿片, t3 S5 u" K8 g2 {. b 铰接在操纵面后缘(副翼,方向舵,升降舵)的可动部。& q- y7 m/ O: w: `1 k 与操纵面相反,以帮助操纵面运& ?1 D0 l3 E# P6 E, n/ _ B 5 Y; I* o/ L0 xwhich is opposite the normal approach. For a 0 @3 T4 w6 ], o7 v4 I" [backcourse approach, glide slope signals are not8 V/ ^. a. Q R2 m8 F" K W available and the sense of localizer signals must be, \7 {4 ^( ~8 l re # Q% k4 p: O4 j0 L$ SBACKGROUND DATA, Data sh) p% l+ P4 d% J' g d ' c# n; O' [' c$ k5 [BAFFLE, A partition in a tank or reservoir to prevent! H$ N$ X8 W7 J- U3 K5 o) | w fluid mo- u' C- N9 k# T B% \0 G: Y, Y& P4 W4 H. z0 r0 a ^ tr % ~9 h+ n- Q6 r3 ?9 h( G7 E8 S$ w& erudder).The tab moves in an opposite direction to the d" A, e$ j/ _# v# `* T" D control surface for assisting movement of the control5 @2 \# L* r: g! j( R surface. 4 @9 S8 o j& F$ f6 M- J: n+ C! u7 i8 q% ], V( x9 f6 O3 V7 Q. j与正常进近 4 K* u. \* V3 H道信号并且航道信号也必须逆反。1 N- q) [% A4 l& T$ K 背景数据, Z' Z- [% @* s- T. D7 ^5 [2 i( R% G: F缓冲隔板,7 t" m3 g" E$ g. ]- X% B; a! O3 E. R& k5 D随动补偿片的动作方向( g0 E. c1 m7 u. n 动,减小操纵力。 6 } u8 H" u8 B# u/ y英汉对照民用航空词典B OEING # Z$ V: `3 {2 N! V- ^" Q* C1 jTECHNICAL DICTIONARY 17 H g, }% D4 `1 v BALANCED FIELD LENGTH, The field length # y3 u7 P2 l9 R6 j% o/ Eassociated with optimum aircraft performance when9 _- f. |( @% ^7 g bstacles are not a constraint. In this case, after engine ' t8 v9 I+ t o$ Ailure at V1, the distance required to accelerate, takeoff % X. H7 h U8 qnd reach a height of 35 feet is equal to the distance " V0 G4 R5 }7 q C. j: ~ALLAST, A weight installed in an aircraft to maintain K# z5 I% h0 q" [5 m/ w: c5 J/ @ ALL NUT, A fixed spherical nut driven by the % T1 \6 d+ x# ?' RAR OUT OF VIEW, A signal used to remove the flight : t% ^6 |- h! |2 B/ i. R& O1 U* fAROMETRIC PRESSURE, The pressure of air above ) Y( x6 T6 ~3 z& L7 Y$ Ag) or6 l2 O$ }5 X6 v" m3 L. V6 G5 Z+ w millibars (MB). 5 |0 J- |" V) Y' ~$ c/ N, pATTERY, An electrical device for changing stored 0 e3 N9 E7 P5 O( }; T' ~! M6 v! q: ?性能的场长。在此 3 @6 |" C ?( P8 G; B3 E# y况下,V1时发动机故障,要完成加速、起飞、离地35 ' G( L7 I$ H: V) Y1 J1 t尺所需距离等于相同速度下完成全停所需的距离。 5 ]* n( \. a# w- j, o舱物, 4 \6 f0 {4 ?5 x% c$ u2 q/ k重心在许可范围内面装载的配重物。2 U% G" Z3 m6 l! M |) Q. v' A; t 形螺母,* g/ W7 c2 ~, l- q! S+ ~0 L 的固定的球形螺母,用以使襟翼和水平% K t M* u6 {2 U 引杆消失,! x! E% \, Z, W/ R1 k2 I* F* P' H 指引杆的信号。0 _2 p" ^; {; ~" l' l% v+ D" ?/ |$ S 压, # O5 F9 n+ F% K' @1 E% I8 B7 B压力。通常以多少寸高水银柱(in ; g( m0 Y& w0 U3 q0 ~0 h瓶,1 `1 E1 ]8 X# Y5 _& l k( ^ 的化学能转变为直流电的电气装置。 / |: w/ K/ e2 i. zo 6 }8 p* W7 S/ A2 c8 U: kfa( b6 L# ^$ D0 M( d$ f a 9 j- V+ p3 T( rrequired to stop from the same speed. 4 M" B8 W, q( g" aB2 R7 \ ~+ n4 ^- h; K) K1 i0 U7 { the center of gravity within allowable limits.. h; T% A2 F! H5 M B # ]0 F1 {. R2 T" Yjackscrew for flap and stabilizer movement. ! s7 ~9 O9 h M y( Q1 [- j) vB) N' l- w4 p3 M8 v* J! ?/ W2 X7 _( N director command bar(s). 2 a1 n+ q1 J: v. ^) uB' w* C+ P6 z5 W# _. q. ` zero pressure measured in inches of mercury (in H; T: ]% e4 T( G1 H+ U! v in W& ]5 ?$ [+ o# S+ F) P" zBASE METAL, The underlining metal to which alloying; E3 S$ H" X; P) n! @3 U agents or metals are added. 2 _" T) ~8 F7 LB / r8 A2 v9 f* Pchemical energy into direct electric current.$ N2 {9 @7 A, y( i. T& N 平衡场长,/ R# d. `, z# A: i 当障碍物非限制因素使飞机达到最佳 % x( ]! B) e1 I$ T- i) k; x4 {0 w8 I) @& L& U. B' O& P) @, V( R) D* h( N; V' x8 ~- W5 Y为保持飞机) A% k" u1 ^) a, Z, N& A, K/ P6 f( o7 e2 t3 q) \2 d/ z; U 由粗重螺杆驱动 " F( y4 T0 ^8 A( l" g2 Z安定面运动。 " c5 A. T) \3 O5 C- S$ K# B2 n; U0 Q0 w, M" i* Y用于除去飞行9 J3 S3 U7 |! _3 I: V5 x' J+ b+ n! d& W- ^# |3 b零压力以上的空气 ( F; L9 t8 J) a8 `4 ~# ^2 @3 QHg)或毫巴(MB)来表示。 + {4 U1 p6 U) U" s基底金属, , f9 B- R( ]; @- f, i# u* }8 [指合金中的主要金属成份。 : g9 ?. w) n+ `3 n8 A' h8 z7 O' G% ? 将储蓄 5 h! H. `0 `8 i# h英汉对照民用航空词典B OEING . _+ M& J0 y Y7 T. C. ]( x9 ATECHNICAL DICTIONARY 18 5 U: f) F$ E, D3 |! b/ G" ?! mBATTER' M) D7 C/ w/ i# u direct cu, ^0 G" v8 y" m% y power su/ p' ~- q2 r1 m( S4 L% B Y BUS, An electrical conductor supplied with; D5 H# T3 }* M7 ?9 O3 m rrent from the battery or transformer-rectifier for- T' P2 Q r1 R- H: _& d pply to operating components.$ R" a8 j. k' C CHARGER, An electrical device supplied 0 n$ L4 L" i6 S8 ?1 a+ uith alternating current, which produces a direct current+ w w$ @: B' \; I& {" J+ o utput for charging the battery on the airplane. & k8 S* p1 P @& I" G$ b# QAY, A compartment in the airplane structure. 1 [1 o2 {% U% `) vCD, SEE - BINARY CODED DECIMAL* {4 r T1 _# O1 V2 V EACON, A device which emits a signal for use as a % t- w) ?7 p7 ^7 s& Juidance or warning aid.% v0 f {3 [6 m9 R/ }6 v# I BEARING (NO. 2), The direction from an airplane to a / l) r2 P! Z3 g/ D* y( N3 h7 j/ nground station. ( q( G5 a, b2 k) m6 R% C3 S瓶汇流条, 7 d4 W9 [ E" D6 a" d: Y将从电瓶或变压整流器来的直流电供给工作部件的导& @( J0 g W+ Q% a, f( g- Z% i 体。4 A$ `7 i# x7 B& C2 L: j' d* r# T 瓶充电器,) d- O" L8 \+ q1 u0 ?+ M 用交流电向飞机内电瓶充电的电气装置。带有交流电的1 Z( ~- _0 q, w! W9 v4 x' M# Y 气装置,该装置产生直流电向飞机上的电瓶充电。 * f) b' I; l7 P, V1 M8 x" _& u K4 K8 w舱, $ J0 T8 P! X- U; c5 X" I飞机结构中分隔的空间。# h- G% J, V* C$ v. l5 Q 二进制编码, 9 A" D7 u! C- G. ?" _6 I/ P" u+ y见Binary Coded Decimal, ?$ W U0 i) p( ^/ o BATTERY% X+ v5 B$ i: g7 l4 l w" p' v! l0 x( R& a o ( ?% ~6 x/ v- j. I5 rB 4 a. w+ q; Z& H0 S6 N" `( `6 NB 1 a9 Z* k/ ~8 O- X! b1 o& V& WB ) J3 [4 h( c1 D1 Z" l$ kg5 F' S: V& _; ^- I" o% L4 E7 X BEARING (NO. 1), A surface that supports a moving ' x( @/ ^/ ~6 T# `part and reduces friction between the two." ?# f: h0 l- o. O4 r" J1 n3 V9 w$ _2 e/ `) j9 [% c" e- u: K$ P& a+ M/ |8 K0 O' \+ e# l: K3 o7 H1 Y) i; _$ q/ X; `) J4 _7 }7 B/ R' @. w3 I4 r+ V% @ P% T- A8 N( p 信标,( O$ V; s) V/ h0 N2 z+ _4 u3 g 发射引导或警告用信号的装置。 y0 Q! l) J0 b$ j' [ 方位(NO.2), * F* e1 d; I5 {6 x3 t: t1 Y3 p5 k4 a从一架飞机到地面台的方向。$ T" l( r* e! K. i! l 轴承(NO.1),5 l' Q; U+ X: c5 H 用于减轻机械转动磨擦的机械装置。$ L$ m9 i4 H' c' }, G7 ], ? 英汉对照民用航空词典B OEING 2 I6 d" J. x. y6 KTECHNICAL DICTIONARY 19 / ~! h$ z& c% z, ]3 [! A/ D& hBELLCRANK, A double lever in the control syst& ]. ]( |8 J/ N4 c* {) e changing direction of motion.8 ?& ^5 R8 @) B: z& k, G em for5 n6 D* ^3 c$ w8 z ct in the/ A7 j |% I) A6 T: o& t5 ^ neumatic system for absorbing expansion of duct due 3 V w4 X. Q0 F9 J3 |+ f1 Aheat.6 Y) P: I9 P4 \; p, m5 P# v7 _ ELLOWS (NO. 2), Corrugated folded or pleated * U9 Y8 W" q9 L8 dontainer or compartment used to measure pressure.% A |7 n! \# C5 _& W* R EZEL, The part of an instrument case for locking the : J; [5 T8 w1 N; Plass. 5 M& @; b0 j Q0 B+ CIAS, The potential difference applied between two ; q* K5 \ Q. V1 ^oints for controlling a circuit.5 L* Q& E$ H3 Z BILGE, The lowest part of an aircraft fuselage. A place / j9 r7 p: J' ]% w# f! }" Ywhere water, dirt and other contaminants collect. 3 H' ]. Q/ A! l, T2 ~$ u4 L& t气源系统内提供管道热胀冷缩所需要的余地的波状, h* p' B" t! e3 j! Z- u. |$ | 轫管。 2 u. H. _, a L$ W( m空膜盒,+ y* L/ U' v& n1 _ 一种具有波状表面的容器。用于量测气压。, @$ t2 c0 F/ ^ 嵌沟缘, ' z+ R. \7 P3 V1 L将表面玻璃固定在仪表上的圈状零件。 / v' o/ v: k( G4 }9 ?1 R% Y) r压,+ [) n8 v4 {0 v' n, y* y 在控制电路的两点之间的电位差。' Z; h9 M, ^0 F1 F; v" ]" x4 L) ~2 w 机身腹部,* ^! B5 ] H& I9 h6 n 机身的最底部,通常水,脏物,和其他外来物集存于此。3 G* p( ~, N) {1 U* f BELLOWS (NO. 1), A corrugated flexible du & R2 i5 F0 u+ Pp1 Q0 W; M0 g& p# _! ?/ S- ^) o. o to$ F" A1 x; T7 J2 I( q- ^, s B 9 G; L3 t8 z% O5 ~ Uc / g% i) k6 o) d& U: z; zB% T- {! D8 [4 @0 j3 @ g. u Q/ l1 H m4 N4 j B: m) a+ y1 ^& m4 @. ?, I p # X* W% h3 y3 D' @- `直角摇臂, , Y6 E+ b. L7 O* [: a在操纵系统中改变运动方向用的双臂摇臂。 ( b( b6 R, B- q1 {+ ~波纹管,, D9 \5 D/ |% r g9 J. N/ Q/ t3 Y$ ~$ V' r$ Z/ q) y# C9 l y" }0 O0 g) m# \, _( V0 B( X. W; y, g" f# y2 ]! R9 ?$ a0 l- F& u英汉对照民用航空词典B OEING * v, E% E% e( z1 p% ~# c# BTECHNICAL DICTIONARY 209 M9 T; M9 t0 Z9 H7 M% Q' z: T BINARY CODED DECIMAL, A system of coding each ) K; V/ L, x# g$ {4 P7 }digit in a decimal number using the binary equivalent. : Q9 G( ^: z- j# p" QBINARY NUMBER SYSTEM, A number system using : m( t% j9 k! ?! r1 `4 C9 x; Ds - ]7 ^7 }! Y: x3 a, F6 MIT, In the binary number system, the smallest unit of # c, [& \) b( p) rformation, consisting of a 0 or a 1. - D6 v" E# y9 {1 A# X; `0 f! XITE, SEE - BUILT-IN TEST EQUIPMENT 8 @7 F6 d8 O' pLANK DISPLAY, A display that does not have any * b7 c/ G5 E+ E8 {7 z c( \dications, normally due to failure.6 O2 ]) m" O9 Y- g+ J# h( E0 n LACK BOX, A container for electronic circuits to record, [& V# |: n9 _$ @ ight data. * N' j; F2 E- e! J' nLEED AIR, Air taken from the engine to power various" s4 d! I( J y4 @4 y ircraft accessories. _3 u) T1 M; B; M* KA valve in the pneumatic system for air ! c h, v- Z8 V8 ~9 m$ S$ F5 C B+ Msupply from the engine or auxiliary power unit to the 7 `$ I" W6 U5 \3 [pneumatic manifold. A valve on the engine for reducing D. w- _, a9 D8 `- | pressure in the compressor section. + S9 o, J& S& i+ G! Z6 r$ G进制,% g/ v( x) n; C* x+ t 进制,: P9 P: a! u4 R, |8 x# s 一般用0和1)和2为底的数字系统。& L* d8 H$ `, e- s6 a% q& U 特(二进位数), , i8 P' U/ m( W9 \1 Y二进制中的最小信息单位,包括0或1。- x2 E0 x2 J7 Q3 @- o" ^) O 内自测系统,2 B0 e# P5 ?: _- B 见Built-in Test Equipment; R# i/ K5 E y, e: M two symbols (usually denoted 0 and 1) and having 2 a7 F" z5 V: f' V1 c1 @ its base.8 k6 w) _/ r7 M3 y# t6 R B2 Q1 Z. q4 N3 r) S# ?2 N# X in & h: M$ f) U/ eB1 D5 q% K; B: i8 b B : d% W1 ?- F6 Y' v+ }1 E& oin4 K+ H6 Q0 D2 M: @ B! \, ]4 E* i" d$ m8 f fl9 Q6 ~+ m7 m0 R( ] B ( ]! T0 P Y6 M* m; {% ya: @9 V0 S- A& {4 F) |" n& Q BLEED VALVE,. _" L4 a) c: i6 S5 s: t. l 二进制编码的十 # I: ^- h4 B* z, d) [! t, g一种编码系统。用等效二进制位数编译十进位数的每一2 N7 G$ R) r4 F! Y- W8 g$ | 位。8 `* Z. y7 W P c8 c: g9 @& M w. d' O1 g7 v! q 以两个符号( * O- J6 m+ N- [2 F. {3 Y' i2 N" G# U% ] k. Q3 J/ _$ u& g* b1 r" ] .! [/ }& t5 \' Y 白显示, ; Y- s& E1 F, E; ^6 ^通常因故障而造成的显示器上没有任何指示。 T+ W/ h* n* B* q7 E; Z匣子,7 z. `$ k. Y. } 装有用于记录飞行数据的电路系统的容器。 + [* q8 z) Q2 r3 d% {' L2 B气, 6 y% J# X: k; W F8 r取自发动机而用以驱动飞机上之各种附件的空气。 ) b" |3 d& s/ c& j气源系统内,使来自发动机或辅助动力装置的空气进人 $ o% v9 W Y) i) B7 e) l气源支管的活门。发动机上,用来降低压气机压力的活门。+ t! N& k. w5 m9 M0 y8 B. ~; M( k: g* `) b N6 A3 M& B+ n% K! f. h* n. ]# g* Q& X& G. { D4 `+ R 引气活门, 8 M9 W" M" {! a6 @2 ]英汉对照民用航空词典B OEING 1 p$ K, Y7 t6 |# D9 aTECHNICAL DICTIONARY 21- e* }$ _: c d& P) F; V BLOCKER DOOR, A device on the engine for blocking, R$ t( R, Y7 J; ^% Q" L the normal airflow during thrust reverser operation.- u) g/ M/ O: } LOWER, An electrically operated fan for circulating air. ! Y8 [! O- W8 ^, i% _, H% gLOWOUT PANEL, A panel in the structure between ; r% c9 ]( r( N# x( V. ]) I( Ho compartments that opens to equalize pressure in% [8 D# m+ x: [7 F e compartments. ; E; e0 y& E0 m8 b# gODY GEAR, The landing gear attached to the 5 Y) I6 t# x4 F. y5 a- O" jgrounding. 3 [9 X* p0 A5 Q: u7 z正常的4 w2 m0 n. I4 c, a% U/ d9 t$ g2 c 气流。 * k" A# E! T( s6 M鼓风机,4 \5 V5 [+ ~7 p4 A 用来使空气循环的电动风扇。 * P3 d- s9 C6 G* A; w, S压口盖,, n$ v; B5 W* F+ m7 Q9 f 两个隔舱之间的口盖,打开后可使两舱压力相等。; [6 X* V; ~$ _) o 身起落架, . h+ y& I! y. W. S# W身构架上的起落架。 * Y+ s5 z. u( u3 a5 C7 gB% l# t: `+ L" g% E0 }7 K B) `+ c, U) c, w; p! Y: G tw2 z7 |5 L& T( ~$ M" U! a th 5 W) ?; k, w" _9 O4 PB( G, @3 o# M& t* x1 x; v fuselage structure. 8 g% J. \0 H. ]% EBONDING JUMPER, An electrical connection between; f4 r E% C8 v1 A3 r, `$ F a component and airplane structure for electrical" W# V' J; y% O 阻流门,8 _5 `& `, Z2 l) v 发动机上的一个装置。在反推工作时用于阻挡 ) Q# e/ ]9 I! E: T5 p: L' l7 r8 @ Z" r) b3 w* Z s; ?! W0 V3 I! A/ y& F5 I1 R装在机 ' l) J, y) C& p$ @- s! T搭接片,9 E' B4 {! B$ Y, l 连接某个部件与飞机结构以形成接地的电接头。 9 ^" c7 a) [5 H英汉对照民用航空词典B OEING6 D- K. l' p) T1 L: Y# ` TECHNICAL DICTIONARY 223 _: |& U3 m5 N1 {0 l" a+ z: ]# \ BOOLEAN ALGEBRA, A mathematical system for' M* ?7 b% @0 T5 H% x9 X writing combinations of logical statements. 2 B) F% r6 E2 }( dBOOST PUMP, An electrically operated fuel pump for @, Y/ F/ S9 d: C) Y) M0 Q+ G fuel supply from the airplane fuel tank to the fuel5 u% E3 @5 F3 _ manifold. & D% B, `7 s1 @BORESCOPE, An electro-optical device for looking at g0 t4 ^0 M. Oternal parts of an engine through holes in the engine., @+ i( `0 q0 Y( [0 C orescope ports)' k: u/ i% q6 Q# R" C OURDON TUBE, A curved flat tube in a pressure gage$ J2 H9 t! D7 q" d) X r moving the pointer when pressure changes inside ( c: A( f- F/ W2 h9 R# U% [on the ability of the brakes to 7 V1 f' |7 g2 q( [ S0 T9 R* gbsorb a predetermined amount of energy during a 1 h7 O V0 o1 X1 O g3 mjected takeoff. , b3 v3 S" s# E( P/ W& F用于通过发动机内的孔(孔探口)观察发动机内部件的- L3 D# y3 i5 r( ?( F7 U3 } 光设备。. D' w9 K8 P% K2 _2 i9 I$ L 端管, , ^5 u0 [$ \2 x4 M测压计内的弯曲扁管,管内压力的变化时它使指针移3 t9 }- {! |# b( r( Q2 c9 O 力。3 o( W) H# Z* ?9 Q1 t0 r% w 极限重量,9 P! _5 I( E, S# q$ d. G# J E 起飞重量。 ' i" g# N: J9 Q3 m发动机滑油系统与大气相通的通气口。 , H6 G3 S$ ~: N9 c, {0 b$ f! e+ x; Z+ Din+ L* o8 e2 X( z (b8 x0 J' A- u5 o, W4 W5 ? B * |* I" ^; \7 ^$ R- G) ~fo0 B3 Q& n* M3 f& S the tube.8 s ^8 ~# ^! n% X3 |8 q BRACKET, To enclose or surround.5 b L" x9 q; h) M BRAKE ENERGY LIMIT WEIGHT, The maximum- z9 R0 u- Q8 R takeoff weight based/ @& |/ o& L8 Q a ; e7 U" M9 w8 `5 _& [& B& cre ; @6 f: U$ r. t+ t VBREATHER, A vent to ambient of the engine oil system." `3 W/ v1 j0 H- b1 q 布尔代数, M5 Q0 {, o8 c3 P9 U2 l; G0 u7 ^一种用于编写复合逻辑命题的数学系统。- Y7 e9 V8 o( B# O, S 增压泵, 9 k: m) x3 Q. w! p+ T6 p( @ e从飞机油箱向总油管提供燃油的电动泵。 - `. u/ R# |3 ]孔探仪, " R6 d! |6 n$ k. E. g7 L1 g/ j. B/ D, ^# r, d% r' s) v: |9 I6 _0 v4 v 动,以指示压 - h& ?, l8 i, N托架,8 E8 B% } G' {; o 用于作支撑、装托、或围绕之用。 * b. U: \$ c5 V7 {刹车能量0 S% [4 k8 w/ Y0 n5 k( [" A 中断起飞过程中,取决于刹车吸收预定能量之能力的 : T5 F' \% Y, i' |% e) k+ G$ K7 K* N' A( B通气装置, 2 x- ]8 J4 i* S) A英汉对照民用航空词典B OEING) f- u5 Z+ _5 p* f! B. c; k TECHNICAL DICTIONARY 23 3 b# C' @- T, M' q3 s' c) nBUFFET, Vibration of the wings and airframe resulting . Y% V# ^; P' W, ~from unsteady airflow over the wing; caused when1 q } ~4 L; O airspeed is too slow, the bank angle is too steep, or ' s. {' Y1 {/ d# K6 B, { \8 firspeed is too fast.* |8 T0 t7 o, ~) ~7 @/ P UILT-IN TEST EQUIPMENT, Equipment installed on; w# |* E+ m# B( @ e airplane and in airplane systems to test the systems0 i" u x+ i& ] ithout external test equipment.. Q) d' _9 R1 ~: s) W9 [ UFFET MARGIN, The amount of residual maneuver W: s+ \$ h N4 t$ h0 n apability present before the onset of buffet. ' ?* E a7 t( [7 @6 NUG SPEED, A preselecteed speed to be observed 7 p3 t7 m3 k8 i1 ending sequence. & L) g1 R( {3 sk" U* e: Q6 Q4 R( y ng landing gear operation. 7 a+ s9 A7 f J6 ~速度太慢或太快,坡度太大,均会引起抖振。 ' j6 ?3 V& y; W$ R自检设备, 5 Y% |& {; p# ?" ^5 v2 f- I5 E' V安装在飞机和飞机系统中,在无外接检测设备情况下," T9 R2 A5 h" z1 a, f: V( p) M 用于检测系统的设备。 ( L& t- ?) X5 a1 z# r( u. O( u抖振裕度, 5 D3 m+ Y+ y9 t7 S. S+ v, Z飞机在遭遇抖振之前,剩余机动能力的大小。& K0 m, U4 r1 {6 D2 { 标速度,6 u& R+ P% K& s 在某些机动飞行过程中,特别是在进近和着陆时,飞机1 ?& j: ^3 K6 n) y& |5 z 预定速度。 $ c2 ] Q+ f' _3 v4 P力装置, ) v# {1 _& y4 X* j架工作的一种机械设备(弹簧或减震器)。% V" I7 g* T) Y$ h) ~4 H1 |5 c 流条,* [& G! V4 Q1 X3 z# w* A6 {; h 在部件或组件之间传输电、数据、或定时的单一电线或 / C5 t9 q: F# k) `# Ha 0 L! T. o8 ^7 T5 J8 _1 _& d4 aB 1 u* e) W) [2 ~+ mth + g- _2 H( l) C: K, Rw # z( x, W$ R& u" dB9 S/ P! m: n% m+ W c , t3 \% g. J9 [$ V. C. \6 l: yB9 f4 e% M p/ ^- X Q! d: m during certain maneuvers, particularly the approach and : n' _0 U1 i. mla2 W& k) H' t: s+ D& O V) | BULKHEAD, A structural partition in the fuselage or ' m% k2 [: m% X8 Z/ T$ J* qwing. ; z* W" @5 x; m# A. T qBUNGEE, A mechanical device (spring or a shoc 3 L' Z2 G) ^6 Iabsorber) for assisti' d6 M) e* B, C" U2 h" g BUS, A single wire or group of wires which transfers8 g$ j! R$ s5 B( ~- E power, data, or timing between several units or$ g: z$ H+ E- g* z/ l; B9 D modules. , {, g R9 K. B; ?9 |: L& B抖振, . q7 B; i$ n3 ]7 d* e( h+ k由于机翼上表面的不稳定气流引起的机翼和机体的振6 H3 c1 t+ L" V, h) C 动。飞行) X* O' q7 |8 E1 B' c5 _- n7 k6 }% {5 | F* f+ k# V/ O所应保持的+ ]! Q& W/ }: F# n( F+ D 壁板式隔框, 8 E J7 l+ `1 d3 g) @机身或机翼内一种结构隔板。 4 L s% w Y) p% _5 G! r2 z% P$ _* f5 Y! ]( g) J" r, O 用于协助起落2 c7 k, h, [5 h/ H% e+ [0 l$ G* L: r3 z+ d7 M( X# A# q 电线组。 , O8 \# x+ r k/ R英汉对照民用航空词典B OEING. I8 |, L: |7 V2 G TECHNICAL DICTIONARY 24

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BUS DRUM, A mechanical connection with pulleys 2 {7 { l+ n2 m) g% Y: q1 kcables in the control system.% ^* L1 u; C- e* y and2 u$ _$ O- P4 f% g* f, k l circuits for control and protection of 4 T/ y/ ?; T H; m# |# y* E! m2 P& rlectrical alternating current supply to the airplane." u0 {8 H6 b* X4 r9 q5 X0 V# X duct for closing and opening the duct0 j" Z$ I o: R2 O. H3 N assage. / u7 s+ m+ c" ]UTTOCK LINE, A vertical reference plane along the - Z$ ?) k+ t4 `+ u0 eselage for horizontal measurements of the airplane. % G8 e+ J% T' w3 D4 s+ |( J; f接。 + X" I5 ]1 i6 P, w& D/ P3 Q组件,内含控制和保护飞机交流电源的电) N5 z$ b6 o c7 m% c& C; i& @ m* R2 }( [3 n作动简控制的转动装置。用来关闭和% h( f0 f F* Y/ Z3 a0 d 启管道。6 G X. s# @. y1 i1 g6 {( i$ W 沿机身走向的垂直参考面,用于飞机的水平测量。9 C& I# L0 m6 [5 s3 U5 m BUS PROTECTION PANEL, A module (black box) 5 h# C" J: x2 I/ Icontaining electrica, J8 y9 R- s6 d& n6 P; l e f' v6 F6 ^* y# v% J* d8 X BUTTERFLY VALVE, An actuator-operated, rotating " \+ e5 C5 L" n( d2 T& P+ u6 Vdevice in a 5 |& h2 X* _0 `p+ ], m7 j/ Y+ Y B 3 [& h" ?: I& d. Cfu 1 k- U( n' d* S4 b转动鼓轮,0 v$ d/ `- I- M* g+ l' Q 在操纵系统中,具有滑轮和钢索的机械式连' y& k) _% b/ Y$ I; [- k( K1 I 汇流条防护板, 5 E/ U$ V E; }) j黑匣子式的 ) v% j1 J% n! ?9 j9 d# v* C% V }9 s7 \" ~! }, @蝶形活门,, k2 i8 |2 Z# ~5 Q o# o 是一个在管道中由 " ?* L$ \( Y5 Y# R7 I; q/ [. k8 P+ f6 ]# k* U0 q3 ?) n纵剖线,$ K% ~6 }' |& J, Z7 c6 @) }0 P5 ? 英汉对照民用航空词典B OEING ! o7 _ ^! G+ h6 q9 aTECHNICAL DICTIONARY 25 & b2 B" k& j& f7 H: LBYPASS VALVE, A valve through which air or fluid will " _ Y8 @: [( Z$ k$ _" F+ L) Nflow if the normal flow path is blocked.0 p, W5 j& i( a1 h8 P, X BYTE, A group or string of binary digits. A byte is* S' f1 h9 r: o4 [! p6 d1 v' n sually eight bits long. 9 D8 k' M' r: P+ zABIN ALTITUDE, Atmospheric pressure maintained 7 e# v# H7 R5 q0 }ithin the cabin, indicated in terms of feet above sea, P# b+ {! ]" ~ ALIBRATE, To repair, adjust, fix or correct the0 B8 x3 `$ _7 j# a easuring capabilities of a measuring device./ E; b# s% e9 f& B ALIBRATED AIRSPEED (CAS), Indicated airspeed 0 v) Z& F# G+ e n$ b' u, I; MAS) corrected for position error. : h* O! b5 `5 A8 ~" e) jnical" [' E% t4 c! C1 n5 |5 Z omponents. ' w0 ?+ {' C) M' w" i2 Z( w b/ U- ?: k1 j 节, % E7 y2 ?9 ^0 @1 n一组或一列二进制数。通常一个字节长8位。 / ^& X& v1 R3 D8 L! Y舱高度,2 V& d# ]5 d- @ @ 座舱内保持的空气压力,以海拔多少英尺表示。. j8 p8 v; ?( d6 X$ [ 准,7 W6 O& P6 k: ^* s0 d: i2 s 修理,调整,定位或改正测量装置的测量功能。( U9 Y/ `; t/ k# {4 W; Z: z \ 正空速(CAS), % q- D. ^$ L, w h+ r- T在修正了位置误差之后的指示空速(IAS)。3 a! X0 A) r" J6 o 用来移动机件的一种转动装置。' W/ [! s9 F) G/ o- l u* b6 k# X8 [" B1 Y G& @ C: n' N; q( w' t4 \5 [$ T$ u C6 T. K' R1 x: `: @& [+ u+ K- e w ; Q" X+ t* k+ V" c7 O$ ilevel., M; N. z' P- j( x( Z- @& s# C; f C + V0 ]+ K) D1 x8 T- k5 mm8 {, v( O* j1 a) V9 l/ _" ? C9 S e m# J2 Q (I' i) I0 q B K3 Y) K6 o' f0 S CAM, A rotating device for movement of mecha: A' H8 X3 i7 Q! U8 h C 9 M2 M b5 H7 \ l, \# Q$ @1 f. U旁通活门 # ?) c! l! F; {! [% n气流或液流在正常通道阻塞时所经过的活门。/ p% H" V1 }% _1 F' s4 b4 S2 n4 O( t# W' Q |4 @1 I2 E# ?# j; {7 ~ L. s& e6 z& J. z( F, N' D0 o* J/ t. _8 F 凸轮,' u- }. a. P. Y8 h 英汉对照民用航空词典B; K5 t i# k4 r8 w1 }' Q0 ^ CAM-OUT, An autopilot condition in which the actuator0 F' V0 @/ m8 T3 P9 |3 D$ Y9 H3 [ detent piston is overridden, either manually or by the7 {: ]5 z$ \9 V ther autopilot actuator.. f& Y3 v; J: L AP, SEE - CAPTURE- o2 T- s) g- z0 P1 t" p APACITANCE, The measurement of electrical energy 6 e& J! ^0 I$ @* L% ^( ^0 _% y6 w$ Jtored in a capacitor (condenser). * J; D1 f* ~. h0 c7 SAPACITOR, An electrical component of two metal 8 s- S* Q9 h, _$ [4 R$ B9 l1 ulates separated by a dielectric material, for storing* G4 _! ~, N% a% D lectrical energy.: }, x, X! s' O# r: Q CAPTURE, An autopilot or flight director function to 4 V" w6 ^5 i, P/ facquire a selected mode. * P0 l$ Q1 `$ \$ O: j! TCARD FILE, A container on the airplane for printed 1 D" {$ k" _# k# lcircuit cards.; z* e" s" T) k7 P8 P7 [ 一自; J( U" w0 y% e2 ~; Y- }* a 动驾驶舵机所超控。4 ^7 f& f( p+ v* E& Y$ O 截获, U# s. x$ o2 |' r 见Capture 8 O* d0 L/ C7 h7 }o 7 v5 U" z5 I$ q9 UC ! i0 }( z4 L: Z* t5 kC# Q0 e2 j9 K e" Z$ u s9 K5 Z( f9 R+ `- m5 `; `/ N' J C 5 \+ I) j% T% S3 k3 ]: tp, s" z# R1 q7 c U d6 U: _ e ( u3 X- r, n% r凸轮不工作, 7 n' y, c7 i* _" X& f7 d, ~0 i一种自动驾驶状态。此时舵机锁定活塞被人工或另: d) \5 {& E- a$ V/ T O0 v- p8 B$ A4 N3 E7 v& y( B 电容量,9 y8 v q- W( b) U. V 电容器内所储存的电能的量度。 ; M. n n( g+ ]* ?容器, 0 [$ r! z$ r, T! K' [* k两片金属中间用绝缘材料隔开的电器。用以储存电能。 : K( g& m6 H5 a* u# c截获(CAP), ( I0 R% S& f6 _! S1 H7 H自动驾驶仪或飞行指引仪的获取选定方式的功能。$ o" s6 s3 i$ Y0 p+ l0 H) h2 t2 O 线路板盒,* Z6 Q0 a$ B) Y% X* K2 O F 飞机上安装印刷线路板的容器。 & q6 _, ^7 m4 l( \6 j0 X$ X( M3 k$ P- n6 y6 n3 @' }5 T% xOEING 8 z# _3 j) U1 Z$ f/ nTECHNICAL DICTIONARY 26! s; F8 @0 m, m% ^ 英汉对照民用航空词典B OEING. j1 N" B& m- `+ q1 z/ ^+ {9 q TECHNICAL DICTIONARY 277 A& m# j) ?; {4 S) @/ b CASCADE, Two or more similar circuits or amplifying: Y' u$ g- W- E/ e0 \ stages in which the output of one circuit provides the , L' A" X$ b& Y8 { g0 m7 G& a Wput of the next. - b8 d3 E+ |& T; \ASCADE VANE, A vane for turning the engine airflow; m6 v% G1 U& K- `% X uring operation of thrust reverser.8 I* P7 k" ?: Y* U7 L- ~ ASE DRAIN, A drain carrying lubricating and cooling5 {; k5 c" } M* a$ x uid from a hydraulic pump. ' [; x- c: d- G2 eATHODE, The element from which the principal - ~5 P0 W& p* {: xtream of electrons flows. . Z' N5 B; r7 TATHODE RAY TUBE, An evacuated glass tube with a ; R# ~5 ?+ k) W4 a1 L+ cCEILING, The height above the ground or water of the C( o r$ ?* s2 I- Q base of the lowest layer of cloud below 6000 meters $ m) ]2 a1 i' l$ ^4 g; t" {(20,000 feet) covering more than half the sky. : Z0 i$ X1 j0 q. C5 D程。该5 ^% n/ t' R; J4 ~9 R, M 程中,一个电路的输出为下一个电路的输人。 % [# h W: C u4 Y5 w2 w叶栅叶片,; l; \) N7 Y& J+ U 在反推工作时,使发动机气流向相反方向流动的叶片。 0 G/ s0 J; Q( [2 j* n# ]- }+ _匣余油管,$ p% r( w: }& R$ L' d4 O 液压泵多余的润滑液及冷却液的排放口。 # X$ o: T7 `1 Y) U6 R/ {8 j极,7 y$ M: ]" S( p% D 电子流流出的极位。 3 }! T9 L% Z5 ^& e0 P1 c5 Z* s7 m极射线管, ) v2 f1 C0 v F9 l o) K2 a有显象屏幕的真空玻璃管。用于显示信息。: Q$ o0 v" J+ H7 x4 x' O+ X, d 云高(云底高), . S6 w" l& S; Z& |* K: D. s6000米(20,000英尺)以下已覆盖一半以上天空的最" Z# m0 j9 _ k; } 低云层底距离地面或水面的高度。8 U! A7 \' s4 c2 g in - } b* b' b3 c& M% gC4 F4 U" B0 z U+ H) V8 B) j d% J* F/ ~2 o f+ Q C ]5 z: c( h6 l2 z fl $ Q$ p6 W: `# a; p$ f0 R( NC! K8 |* c$ v9 } ~. Z) K s2 @: W1 F9 F1 z9 J% z/ L C $ K: O2 L9 J/ n3 [$ E0 \viewing screen, used for displaying information.+ V* q: x* m: p/ K. p 级联, 6 t6 Z1 }, O- ~, G0 L* Z- Q两个或两个以上的类似电路的逐级连接或放大过 , d; n3 K3 o, d3 k% [: o$ Z7 [9 u, A( V* ~7 i5 V0 N# Y6 t4 E! {2 G$ I. @3 B% m' k* a8 d. u. r% y( N1 T$ |" V- c! @7 l* R9 n6 B& A 一个具 / } h6 |- }. ~$ s2 D英汉对照民用航空词典B OEING 6 r3 D# t+ @6 `; X1 A! L- K( ^+ dTECHNICAL DICTIONARY 28 . W/ M; A- o$ G/ R2 Q( cCELSIUS, A temperature scale in which zero is the7 r3 w/ @6 x( m- W" ^- @1 L freezing point of water and 100 is the boiling point of % D/ |- D2 s. g$ Swater. 2 k2 p! d A2 K2 W1 KCENTER OF GRAVITY, The balance point of an object 7 a1 [: Z& k5 t0 B9 a& v& V4 l( W9 {r rigid structure expressed in terms of percent Mean! X" _/ x" f7 q G5 o1 [ erodynamic Chord or in inches from a reference point.% N {/ i) H+ E! p* ` ENTERING CAM, A cam for moving a mechanism to a ! c$ W% b$ [3 geutral position.& J' ^9 u( e4 A+ ~& \ IGURATION, A configuration of the( d7 O6 \6 E% n3 w; O3 {) O ircraft approved for operation by the local governing $ W/ A$ E; Q6 vgency.6 X/ ^) K2 z- L ? ENTRAL PROCESSING UNIT, In a computer or3 }7 x; Z: s8 l, r igital circuit, the section containing the arithmetic and2 T2 j1 {, a+ C9 U3 r gic,control, and internal memory circuits. " N; X! Q( e0 d8 HENTRIFUGAL FLOW COMPRESSOR, A type of' ]) u0 ?# c9 O: A2 c ompressor in which air is taken into the center of the4 F+ l- }1 o6 Z peller and is slung outward centrifugally into a diffuser " ]' E. Z+ W) ~- H3 {here it is slowed and pressure is increased., `, s* B9 b0 m$ ?( z CG, SEE - CENTER OF GRAVITY7 J+ U, X1 A2 m' [ 构的平衡点,以平均气动力弦的百分比或- U. t- ?! T+ W- u. r 某一参考点若干英寸来表示。 7 f' {7 ?; @% l. E, I: ^中凸轮, / `" A- p; \2 j2 U- q" F将机构移向中立位置的凸轮。$ z# T/ r; W! a, h6 a9 d' u 格的装机状态, 4 t8 C* n \9 s* i0 _7 L2 _7 ^由当地主管单位批准使用的飞机装机状态。7 s( W% P0 j# @* [8 v: u 中央处理器,1 h5 ^/ X: n, E X 计算机或数字电路中含有运算,逻辑,控制和内部存 ; p/ f4 ?) C" _, G6 L! V+ `3 X g储电路的部分。$ h' G% g: a2 @7 H6 O7 B6 M 心式压气机,: l3 K# o! R- c* K3 D, P. u 压气机的一种。当进气到达叶轮中心时,被叶轮离心抛$ u* L& Z5 L1 ~ 进人扩散器。在扩散器中气体流速减慢,压力增加。9 K+ I: h" |7 G* h* u 重心, . A! C- Q% r7 Z- s/ K见Center of Gravity % D. d0 s: k0 O1 Bo: Q* s% q" K, {- f: u A+ L% c; ^+ ?: n* X7 Z1 @ C 1 v3 Y P) \* P; K; t+ a* R8 @+ t2 Ln6 q0 v, z5 [3 D1 \8 g5 x+ B CERTIFIED CONF 5 g& z, e" I; V1 i3 G5 X4 J9 y- va ( ^6 R3 E/ K9 g! ]. }0 i. r0 e$ xa " r* V9 k9 Z9 X: k0 y! nC 2 }7 [7 e% [" r$ jd0 G q" r6 D9 T" ?4 F5 V3 s0 ~ lo8 l+ V& z8 B' E3 ~ C! Q; `: g6 N. y5 x2 ` c 1 C% O2 e& \3 R. z% Xim ' g' W# ]! k9 G4 ew ( e" w8 ?' i2 N摄氏度(°C),9 S3 ]$ M* K8 R- I 温度的度量单位。在此单位中,0°C表示水的冰点,) H* Z- `' M* e' _- n1 j! F4 s 100°C表示沸点。 2 I4 R7 d$ N5 A4 u1 G9 Y4 F7 I. P9 H重心 # l. S O% J5 i! r: h2 ]( W物体或刚性结6 |/ u, R& c& j8 a) W$ ]# b. ~% K' C8 [# \4 @9 e( C# A n( `$ L' D, F; c0 z! b" O8 ]$ i [ A' F) d7 R9 B. `2 ~8 }. J' F. ~% D& S* A5 w G英汉对照民用航空词典B OEING- i- s, R. h2 ]2 E. J7 O5 t TECHNICAL DICTIONARY 292 w4 c* g4 ]. w, H CHANGEOVER, Conversion from one mode to another.' x) i; y/ p, y; |7 x* V( E+ N HARGING VALVE, A valve for supplying air or fluid to 9 Z+ o, c! @7 O' z* V4 w( @9 _HECK VALVE, A valve allowing flow in only one3 ^; l* e! t( N# P irection. See Non-Return Valve. R( T7 z5 D% sHECKSUM, In a computer, a summation of digits or9 N2 {) l) h* C1 t u8 Z" _ its which are primarily used for error detection.- \$ E/ Y5 I0 B. O8 U$ y9 I: z HIP DETECTOR, A magnetic plug in sumps of + R% P) f' z6 f1 v6 ?; ^( p! N! abricated components for detection of internal failure of ) y0 v9 Y" J3 Y. H9 O9 ge component.- {$ B3 @" F- h( P: a5 d HORD, A structural component of spars or frames.4 q0 _7 L4 K) U$ |1 X 添活门, + {' ]& C) [/ z$ I4 h: m" {4 W器充气或加液的活门。 : l# a6 t. |$ \% Z: z单向活门,% Q1 P( Z$ A& y! u/ V+ { 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
C4 u# g5 ^. o8 L$ Q a reservoir.+ u9 k7 p' u0 R9 y, e" c C, s( k7 T# o3 ^ S( M: T5 ~! f d 2 f) ]# s+ g0 oC+ Y# w. a j6 `7 | L b 5 F& w0 f. [/ w9 G) H; PC: `% m9 H3 a) w- u$ A+ | lu2 E/ P$ V1 j; J th & f. j5 ~1 O h, N& M7 m. W, ~; oC8 n+ ]; i) c3 m0 u 转换, 0 O. @2 _. H1 l由一个方式转换到另一个方式。2 c* O4 N% i5 N! d8 b7 B; I& k# C; q. M3 h( Y用来向储存9 `' A# o# z$ ?, m0 j( p: W3 e, G$ ?$ |8 _& R, S4 k$ ^9 \4 b总和校验, 7 W0 y9 y! Q3 N* p r# M计算机中,把那些用来探错误的数宇或位数的总和进) r/ O, X% ^! X( k+ y 求和计算。/ i; h& T. m s, W& N" |* k2 ^; P* ~ 属碎屑探测器,; i* n7 k8 p) Q+ [- O9 X 装在被润滑的部件滑油回油管路上的磁性塞子。用来探: j* P8 d, O( O. N; \% ^ 部件内部有无损坏。# b( N/ s. \8 A, x- A, a! {) z5 Z 弦, # ~; u q4 J( k# {' [梁或框架的结构部件。, G; H7 @5 X9 T5 y1 e" N1 B/ @9 g' e" p. b4 n& I" M. s. O. v0 S9 a: Q# m5 b. o* z5 i1 R! w2 b+ b& M% H, O: N; E( ?: \; G: x0 G6 Y 英汉对照民用航空词典B OEING: a/ d( O5 g$ V, u8 s TECHNICAL DICTIONARY 30 % ?* c% C, A4 j- d1 }; b# ?CIRCUIT, A closed path through which current flows, j5 C4 [& Z# i& S$ z/ a, M" {! H ource. 4 u% }- b5 K, T8 k8 ^, W( PIRCUIT BREAKER, A device that automatically ; r4 i, N3 V5 s3 Q+ g% ?' qeactivate the system. / n$ B6 T: O1 M! G Olear of all non-frangible objects which1 d4 |) i% M. L ay be used as takeoff distance available when ( K$ J5 u& H- G& ]5 h" _. D. z( Xalculating a takeoff weight.& M) e& [0 C. ?3 l6 ], r3 S5 Q r water under the control of the appropriate . g. @& X7 h& x; m1 }uthority,selected or prepared as a suitable area over5 e5 B1 L0 E3 ?* r- n# q3 O hich an aeroplane may make a portion of its initial $ d7 K2 z0 H U( Xlimb to a specified height.1 M" o% ? l5 F0 B4 a e increasing. 9 u6 e# R2 I9 b, H2 psed, g- b$ w, F. w2 C8 e LOCK SIGNAL, A continuous string of pulses used for 7 W# J0 v2 ~4 j& f; s" ^! A开关,+ R* ~, O8 f$ G6 \5 A, C/ S1 P+ T 故障情况下自动中断电流以保护线路不受过电损 5 b0 |/ C- K* m; G. z, f% _, q体障碍物的区域。在计/ X! `7 {) ^% _" ~# H' d1 c- ?) C- G 起飞重量时该区域可作为可用起飞距离。 ^9 G# e0 ]6 [: l |! v5 A" K是在有关当局管辖的地面或水域内一个界限明确的长 3 j( \' D! s( a0 y) Y, _+ `形区域。在这个选定的合适区域内,飞机可完成初始爬& N' J7 @3 U) s- ?/ R2 M 的一部分,上升到一个指定高度。) T7 `0 z) |' ? 飞机高度不断增加的飞行阶段。( T ]$ U! P0 R6 w. P# i 钟脉冲,! k9 k5 m* a+ [9 l5 X) Q 步的连续脉冲信号串。$ L) x% j# \' \; B from a source, through various components, and back2 o) O: t# A F. n* p. F* ~ to the s * q( a6 l/ V3 WC ) a9 X- y! v# ~6 L; Yinterrupts the flow of electricity (current) during fault 4 d4 v1 c* F7 pcondition to protect wiring from excess current. Circuit % d% p0 w5 p! [( qbreakers are also used as a means to manually ! G) Z* c0 b8 [/ v1 f, d* z! Qd8 j+ d4 ~1 t. j: J" n CLEARWAY 1, An area beyond the takeoff end of the1 W/ W3 U/ g. L) u runway which is c9 `2 c$ Y+ @ ?% @+ G. [+ j" } m+ w+ I. M9 x+ G) ]$ o3 b/ H c6 h9 z$ [" H( |( v CLEARWAY 2, A defined rectangular area on the * T6 u$ f+ E; g$ e ^- pground o/ A ~0 T4 r7 i) I% ]7 \ a% c% s, I/ M0 N5 B' R w & F- u l5 G- \$ e$ O, X" ?c% {7 G9 n( T) v, m3 c1 K! q. W+ D CLIMB, Phase of flight where the altitude is ) N" \1 y4 O9 q* t# oCLIMB LIMIT WEIGHT, Maximum takeoff weight ba% W+ q7 {1 l. n+ q* k- U on a minimum climb gradient with one engine, j2 _: o5 F7 [; x inoperative. 6 M2 {) f: b! G4 F& kC ! i) K8 A N' \synchronization.$ N1 q* ]) J1 e$ j 电路, $ \. R8 j* X* @( T# D% E3 G一个闭合的回路。电流由源头流出,经过各个元件流回3 i' e3 k9 [& I. S m/ D. z 源头。 # U& H& s/ o8 z4 C# v4 \5 {" Y6 J; A7 Y7 S! Z 能在 4 w1 H8 b# W9 N- }坏的装置。跳开关也可用于人工使系统无效。) N) K/ Q( c$ S# v0 h z- Z 一号净空道, % A$ @. w. T. W/ f3 a8 d是跑道起飞端以外,不含任何刚 . z8 s {8 _# V; s, e8 h f5 D5 \8 Q# O$ s+ S/ R二号净空道, # Z' x! U# w3 Q3 o$ p" F% [& U y" }6 |9 ^7 x2 u; z0 A( c- \4 L" Y爬升, ! y& @+ P. \7 @, B* H7 t3 {爬升限重,$ y4 ]8 G) s x; Q5 M( G6 x$ F 取决于由一台发动机工作时的最低爬升梯度的最大起 2 T: D& o$ Y* D# c1 y$ h飞重量。' o4 Y9 ~7 G8 M0 s1 ^/ }( U: V( k! g7 X用于同- y% R2 ]7 ]0 u8 e6 B! g- K 英汉对照民用航空词典B OEING. m( N% b* q: t, N- E$ N7 B TECHNICAL DICTIONARY 31 - C& h! P! j7 B. }COALESCER, A device in the water separator for / e3 A% ]4 R8 T; Qollecting moisture from the cold air.1 _& F7 P9 P" M. Y n antenna with a receiver or transmitter. 3 e- J; M* n* k( Z9 u: L) W6 L# Bhe cable has an inner conductor and an outer5 f& r9 K" t4 j: R1 ? rounded shield.) F6 C% a8 C$ X- j' [7 l1 C& n; i E* ] ting one inside the& l4 _5 W* f7 E2 ^1 Y ther for rotating the low and high pressure 9 d x$ {' p+ o5 N6 X% g% jompressors by the low and high pressure engine8 m2 G& B4 R% p rbines.: B+ Z5 g" @3 [% l OMBUSTION CHAMBER, A part of an engine for* ?1 b# F+ K4 P- l, A urning fuel in the air supplied by the compressor. , y: |( [" l6 j' x9 \& I置。: U# J6 X, S6 S! `1 b 射机的电缆。电缆5 R* u& O9 I1 h& T 中心导体和外层的屏蔽所组成。 1 c* _) Z! }3 x, R两个套在一起旋转的轴。用于使发动机低压和高压涡轮7 _9 r$ P$ Y( }# D L 别带动低压和高压压气机。 3 x7 T- K/ M2 i6 N烧室, - n U/ O* n4 w: P) C }发动机的一部分。用来使燃油和压气机所提供的空气相 1 T+ O1 ^7 @) t `8 d+ s合而燃烧。

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发表于 2008-12-24 21:38:35 |只看该作者
c / P& I/ z& }( F9 w. ^. J3 nCOAXIAL CABLE, An electrical cable usually# ~9 q. c6 l! T connecting a/ d3 k7 h: t5 W* Q, k; K# R# W' m: U T % U/ r* k2 _2 w2 u3 ~0 K0 ~g2 q8 i! ^3 _1 K( \1 c2 f COAXIAL SHAFT, Two shafts rota; V7 Q8 n+ q% D' c# I/ u) u o 0 c3 [2 n1 {; M6 H. V; S( Z Wc5 ^ n& x, B, ~ C( r$ F+ ? tu 1 o2 F/ }1 n* F9 ~C3 i, D! g: }+ ?$ L) @8 Y b; E5 A! G' S5 w 凝聚器,5 w5 X: j9 X5 T; D; ]6 y 水分离器内收集冷空气中水份的装 0 u+ M5 g1 e6 @% Q# |同轴电缆, ! {5 x0 W0 l% Q9 W$ e# h$ M* a, i一种通常用来联接天线与接收机或发" |+ @! i3 u- W+ q$ S9 j8 p. S. g" e/ }! O1 G 同心轴,2 h' o- R* J7 e" U: B- y& N; S T' b/ q- ^: ]( @8 l3 i' T* r8 H0 E U& S7 n# V2 Y4 `; A) D5 x0 w5 q7 O% c) {! e 英汉对照民用航空词典B OEING + v" n5 [- K! _; ]6 @ jTECHNICAL DICTIONARY 32# Z1 }) s' B+ u! R8 V' t( a$ V COMMAND BAR, A flight director pitch or roll comman ( k. e! C v! b0 a* [$ ~/ Mindication.$ }: \5 @7 o1 t( _1 }& f; J d & c" B( z8 S# v) g3 U: g0 rOMPANY ROUTE, A route flown by the airplane / u: o& E# u0 y, @: \5 fOMPASS LOCATOR, A low power, low or medium' U1 n6 K. F. v- D0 D equency (L/MF) radio beacon usually installed in # K" Y! B! ]" W9 r5 ^onjunction with the outer or middle marker of an5 t/ \) I+ E$ r* ?$ n n: q tor (LOM), A compass 4 _+ o: V6 w3 Y9 Ulocator installed in conjunction with the outer7 @7 e" Q/ S) s marker of an instrument landing system. 8 `( f/ l y. N; p% oss ; y/ ]' {* z0 B& E) T3 A kle C+ Z# S" [$ {. e* h- F0 j9 y# gOMPENSATION, To offset, balance, or counteract. % y) Y6 v# e1 m2 J1 {2 Z& jOMPENSATOR, A dual capacitor for changing the fuel " A# e" {- }. ?+ u3 q; q2 |9 Taging circuit capacitance due to changes in fuel4 m& T+ Q7 w" g! G ensity. / \& e6 J8 Y+ R6 XOMPOSITE MATERIALS, Non-metallic materials used0 D" n9 c2 A" p+ e6 U r airplane construction. Fiberglass, Nomex, Kevlar, 7 D3 i3 t4 y- traphite Epoxy are composite materials.# t: U# K! ^ ~7 W 司航路,. z) i' {) a2 Z 在飞行管理计算机数据库内由航空公司飞行 ) A; U% T6 l% \; R8 I盘定位台, 0 a" }! B( 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- f W: k2 a# Y& t5 G2 ?( | 功率、低频、或中频无线电信标装置(低功率NDB台)。 * L8 P6 T j) X! f, G程序中用来导航。6 L& C' C& N( e6 w 1.远台,3 _% G4 X2 B, |6 j. ~, C8 K 与仪表着陆进近系统的远指点标配套安装的罗 % F% U" t2 E( T H9 W. ~# O盘信标台(NDB)。 . d% v$ y' Y" ?3 e8 ]3 h偿,: l' U7 d7 k9 ~# m 抵消、平衡、或中和。9 R* _# I( B6 y 偿器, ) {- p9 h z$ ~" V9 O- ^- b" A在燃油计量电路中,用来改变电路上的电容,以与燃0 e% t4 O- D" Z3 B1 v/ b! W" P3 i 密度改变所引起的电容改变相抗衡的双电容器。 & g0 h4 I, h. w合材料, & E4 U8 o3 }# g8 ~& N用于飞机制造的非金属材料。如纤维玻璃,Nomex,( i- H: O0 b/ ~* P! r% K" j evlar及石墨环氧树脂等,都是复合材料。

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发表于 2008-12-24 21:39:01 |只看该作者
C; r/ Y6 e+ \: |7 C Q" \0 F2 u operator that is normally stored in the flight$ ~ r* r1 O; q9 g# ^6 w% [3 C management computer's data base. # `$ f5 x! I& U5 FC + M8 ]3 u. y7 x6 I! a6 Bfr & v+ c% y/ w# p' D- Kc" Q. f0 V9 S M1 U9 p& U" a: ? instrument landing system (ILS). It can be used for& D! H# {% z! {' W navigation as authorized in the approach procedure.4 y" M% ^$ z( p2 n! o: P 1. Outer Compass Loca 8 Z5 E* j( u. b+ i2. Middle Compass Locator (LMM), A compa & ~. H$ U/ m; x% P) q/ n! G& i! flocator installed in conjunction with the midd3 \! S8 h/ a, ]# h: F) G8 G' w marker of an instrument landing system. : j( d( o9 K$ E8 zC7 s$ A: y& Y% f y( d2 I5 ] C B5 m( L+ @( `2 @# X$ Z g! E% e, Q) Q, T2 E6 M4 f6 P6 Q; h d) c3 k" S7 t% F8 i: M C $ y2 [0 ^$ J f7 K3 `; t8 y6 v! o: }1 rfo 4 I v. i' z6 e' K4 Dg 6 A2 K, h F: `# r) }& m指令杆, B( M" D3 G/ I6 A# ~ 飞行指引仪俯仰或坡度的指令显示。 ) n: k3 I: |1 y8 L* h: S! B0 B* t& G2 j% r" l! ] 通常储存1 J# Z- y- }; G: I" a* n3 G 的航路。 0 K3 n% w% M8 w% F: D: u7 O* u0 _+ e5 Y( Z7 n+ {" \2 I! r' j' ~ {/ j1 w+ D# M 经认可后在进近- u& ?; l! X+ r% D. x# k 2.中台, 2 z4 L; I& m0 M5 W与仪表着陆进近系统的中指点标配套安装的罗 % L1 Y- X: Y# P盘定位台(NDB)。 " } E) c% J0 b$ {% o4 J1 y( q1 ]0 c* ?% L# ^5 t9 l4 j+ O* F; g: `# K. m7 W" o) l' Y3 C8 Y! X4 h1 `# ]" |4 H" Q1 ^+ O6 A8 c' ]1 U$ RK5 Q8 ^- v% z' C4 t. O 英汉对照民用航空词典B OEING4 f/ J5 G W; Y5 h/ S& j6 A TECHNICAL DICTIONARY 332 h& Z2 ^5 v6 E/ h2 d6 ^# W- B by 6 _# Z# o, h! L6 I; P. \6 T: N$ nor increasing air0 F6 z6 Z" d5 g2 y( n ressure and temperature before the air enters the 5 a" ?* o" _4 [3 _, W* tombustion chamber, Low pressure compressor - front " r9 e) t+ N, I8 o6 T( Rection of compressor, High pressure compressor- rear 4 a+ }; q" W/ ?4 O+ c3 q# UOMPRESSOR STALL, An event that occurs when / q& S& ~7 k- z# R- A' Fere is a complete stoppage of air or reversal of air flow# `8 \; @/ e8 R4 | COMPRESSOR SURGE, SEE - COMPRESSOR, g8 Y) l. b5 s1 P STALL COMPUTED AIRSPEED, Indicated airspeed 2 j1 T1 i# ]) a7 m% Z) ~corrected for the static source error. * z- e. A% ^! x3 l" P的机械轴来驱9 Y0 e$ X& V1 k% o- S9 B6 L& R ,用来增加吸进空气之压力和温度,以供燃烧室使用。. t P$ i8 s. K, q, a 压压气机—压气机的前段,高压压气机—压气机的后$ |( Z8 K# u) _! I8 s$ V. `& h4 u# M; l 气机失速,/ W* M1 z }& Z0 A" ~( y# Q 当气流完全停止或通过压气机时气流方向逆反的一种# g' J6 _2 K; T3 E) i 压气机喘振,- d1 M3 c4 J: S* l1 i0 f8 E 见Compressor Stall: t$ e8 F D& i5 ?0 W3 A COMPRESSOR, A rotating part of an engine driven , }, V: o: S7 qa mechanical shaft from the turbines f# H, b$ L1 h6 K0 g2 M, N2 W' k p$ q% g! ?0 X* M# F' W+ [, @( G" b3 X) o c : [' G0 A, }& l0 R. Q& us . U5 ?5 [9 m. U: ~0 Xsection of compressor.3 F7 ]' y! ^; X/ T6 Z' E C. ?, z; w) {( i6 b8 F' e th 8 z' P# T K& I* ~5 ythrough the compressor. 4 f" p0 l# o0 X) f压气机, 4 I/ Z2 l( V6 v发动机内的一个旋转部件。由与涡轮相连: P. y* F/ G* C @/ V& u6 P' d9 B% R" h: d% Q7 E) X1 v: J2 p' B5 B* F7 g5 f$ J3 j/ U/ x! K7 }/ x( R- n" T现象。* c# N0 ^: J+ M" ^6 _, I5 r+ ~8 p计算空速,# U% i( i9 b0 e 修正了静态源误差后的指示空速。 # w- I# @/ Z3 p/ @1 X% k% D5 D1 ?* e英汉对照民用航空词典B OEING6 I, ^! q% q0 z- ~) _ TECHNICAL DICTIONARY 34

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发表于 2008-12-24 21:39:27 |只看该作者
COMPUTER, A device that performs arithmetic " H' e# q7 {0 g" doperations, manipulates data, and makes decisions.( E# G2 `4 c1 P+ e: o/ ~" X ditioning 0 p! z/ ?# O8 O# {the air and the # O1 M! n5 Y, hfrigerant or moisture vapor is changed into a liquid. ( [2 i2 ]1 Y9 X- z, p: oine % I: e# C: T7 Q- G* |3 }1 b% @; T6 xONFIGURATION, The position of flight controls,/ W' e% P1 g- ? missing which ; h0 Z9 {5 e9 x Umay affect the aerodynamic performance of the5 V, ` }8 Z( J' E airplane. / H: y0 I5 i/ @, n) i3 m置。 ( C6 n/ g& K- ^" V# X6 |) F. l中能使热能散发到空气中,以及使冷冻剂或湿* G w/ H- D, \( g! p( m 转变为液体的部件。 2 G# P" u: D* a1 [9 Z" v4 c# S5 z连接到飞机结构上。 0 l2 D3 ^" [( h. U# n, R态, ( n+ U7 ^/ D4 l: e4 S6 i( e" J3 G定飞行阶段中,飞行操纵面,起落架等的位置。4 v( C( ~) r) s ),+ `9 Q5 g8 ]0 b( h0 O 受到影响。 , J; u9 M D! N$ ?" MCONDENSER, The component in an air con- R/ \# a3 R1 D. F+ z6 O4 } system where heat energy is given to ) w" k" D% U/ |! j' _. nre : x8 b5 h& X9 ` y1 [$ v/ _; wCONE BOLT, A bolt in the shape of a cone for eng/ e( Q1 V2 h$ ^% o+ b3 e4 C attachment to the airplane structure. 8 {: W A7 [' L0 G: V9 f1 \C ! w3 r' Z- y( K j1 [landing gear, etc., for a particular phase of flight, e.g.,# [5 a9 R) K5 Y Takeoff Configuration, Landing Configuration, etc. 4 }) M+ d% o$ @& ?CONFIGURATION DEVIATION LIST (CDL), Appendix 6 s' ^9 i8 ?# R; C1 f8 `4 Cin the Airplane Flight Manual (AFM) allowing operation' J/ @$ Y X& A8 m of the airplane with certain airframe parts( B. s) u/ L& j5 \2 ~ 计算机,- a$ Q# U2 ~4 ~2 T6 w 能作算数运算,数据操纵,和决策的装- @& U7 I/ _) ?; P9 O 冷凝器, 1 `% A* T t2 R空调系统 S% \: P4 q9 K7 Q5 D* U4 t& I; A6 r, `* }1 O& Q3 U 锥形螺栓, $ `4 z7 C3 r6 ?( i# S% [3 V) R外形是锥形的螺栓,用以将发动机 * W- Q- I& T2 T( ~2 A) W& h4 J7 J/ d+ V/ |& I( } 在某一特 9 t" \. U; h3 c2 Y: N! Q如起飞形态,着陆形态等。 ( A$ ?: k/ F5 T$ r% {0 `# m+ \缺件单(CDL : G. ~ N9 c# J. ^0 P5 D飞机飞行手册的附录所开列的飞机上某些零件的清单。 F; j' D, V5 A& i! s在缺少这类零件时,可以飞行但气动性能可能 ! \0 l+ J+ n6 R; R& n& L; f英汉对照民用航空词典B OEING1 U6 F! w% I$ y& z% V% v4 K 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% H. i2 ?3 j$ h- k9 t component for changing variable engine gearbox speed + L V0 _1 A& \; b3 MONTROL AXES, The three axes of the airplane which 9 l% h" r. c6 ~; k# _- W# qre perpendicular to each other and pass through the4 {! `6 Y5 Y( X enter of gravity of the airplane.- V2 `1 Y- m* r9 J4 d Pitch axis - Horizontal or lateral axis, passes through; J2 W8 o$ u8 y3 G! z) \- t8 n the airplane from one side to the other - - U/ r `$ M) u: n9 y& jnose up and nose down control is by- X5 y2 S, L! g2 \( G/ e' ? elevators (and stabilizer for trim). ; d, e/ G0 q6 y( h! m2 CRoll axis - Longitudinal axis, passes through the8 h; V" |% j5 e0 O3 s9 m airplane from front to rear - wing up and& g: a) D) y+ X$ c7 \, q% D wing down control is by ailerons and5 {' b( t ] W- y/ ? flight spoilers.' t0 V$ U* F5 R E C0 f Yaw axis - Vertical axis, passes through the 4 l7 t: N- H1 X+ {; lairplane from top to bottom - left and 5 R5 K) f+ n2 B7 [right control is by rudder.6 `5 k$ }) I0 e0 i/ b 置,5 I& R0 E4 e0 O- ] 制轴,( R' g( Z$ a6 C2 ] 通过飞机重心互相垂直的三个轴。 : T) I& Y; a4 E俯仰轴—又称水平轴或横轴。由飞机的一侧通向另 5 k# Z& a G- o侧。飞机绕此轴转动即造成机首的俯与仰% e- C* a4 s% m- [; l8 y 俯仰控制是由升降舵来达成的,水平安定: d; F& ?+ B% z 则为配平之用。 ; \/ T$ A, }' r2 ~9 h* h横滚轴—又称纵轴。由飞机的前部通向后部。机翼 9 A. N" V; t7 F p" H; Z下运动由副翼和飞行扰流板控制。 : u# u3 c" }+ U0 s偏航轴—又称垂直轴。由机身上方通向下方。飞机 ! z7 R/ _! V1 F此轴转动即造成机首之左右运动,此一运 : m: K- T4 [8 G由方向舵控制。" T6 c4 d% s+ E9 T& k* H% }0 ] to constant speed to drive the electrical power. - Y D7 Z- [/ b$ _& f, b/ iC ; P; K0 G/ [/ I( f- U4 Q6 m, @a0 O) b3 L' v9 u/ x. ? c9 G$ p, @) V7 T& l! U 恒速驱动装 g2 p1 Y( O) d9 {, B3 n- j 将发动机齿轮箱的可变转速转变为恒速以驱动电源的& A# g) o) _3 z3 n$ A1 G& z/ d 液压机械式部件。 5 Z9 a6 Z+ K+ O' m0 w0 A a" d$ i( s4 g: I2 a% N" Y+ w' ? b* }8 E+ y- K+ w9 N* I( q2 e5 C5 h' w1 K/ w$ h8 Y3 P7 Q4 z6 L/ T! O1 d9 H/ e6 Q# e7 A6 H: ?7 B3 h- G- X5 e8 R+ K英汉对照民用航空词典B OEING+ }4 y1 S( z6 J% m9 K9 ^# e/ k( z TECHNICAL DICTIONARY 36& `/ I/ J" }$ P$ V CONTROL COLUMN, A mechanical component used 9 V" n, u4 y! e: ors! p7 p r- B4 q$ u2 t nd elevators.0 M- D2 _# ~! a( H! p ONTROL SURFACE, Moveable panels on wings and1 |/ ?, z5 k- `& p il for movement of airplane on pitch, roll and yaw axes. : [3 Z5 D% a' {3 x4 DONTROL TAB, SEE - BALANCE TAB+ i& H% C8 b' [7 Z" p' p4 U8 G- w ONTROL AREA, A controlled airspace extending5 X w3 \) M- N; o! N' F) k pwards from a specified limit above the earth. - ?/ H/ Z0 ^5 I4 E* `- D, YONTROL ZONE, A controlled airspace extending3 b$ A% R P6 x6 b* V pwards from the surface of the earth to a specified : f& @, h! ^, c8 X+ ?& D7 Hpper limit. , e( H5 U. U$ e8 J( z3 X+ G8 ~is 0 g% |+ C# O; K& t) eo IFR flights and to VFR flights in accordance0 l5 Q( k4 G7 N @3 o with the airspace classification.# R7 p( `5 W Z) w o& _6 g0 z 机械部+ J6 o' X: x) r( O$ k# y+ Z' c2 |& Z7 l+ R( [ 操纵面,- p; \- ^% Y; T) ]% i 机翼和机尾上的可动面板,用以操纵飞机俯仰,坡度, i* N% v; @) K+ x- G' P; Z 和偏航运动。 / K! b& O) j( V" }操纵片,( S' M; e. ^+ R% }, s 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% Q$ P: K, q9 z' ]3 V+ F a . o5 I: l$ p! e( X7 b. Q& VC 0 {: f: b+ z* X& o7 n7 ]ta 6 E2 C% d4 p" {- h3 }C 6 F) Z, `1 ~! x% fC # |. Q) ^) I% [7 vu; H. r! m* k4 D, k0 ? C3 ]) ^/ s B- p4 t u 5 g# b1 C/ g* h- Xu5 ~! t& Z" Z/ O& G) N+ z CONTROLLED AIRSPACE, An airspace of defined - D. R) e$ p4 b% t; R' F0 y; Odimensions within which air traffic control service / j8 H. |+ k8 {provided t e5 C' m; F$ ~$ g$ G* _9 y驾驶杆,+ K, v9 j* V* I8 Y- F# m 飞行员用来操纵副翼、飞行扰流板和升降舵的 8 h6 A, ^7 d3 Q; a- y! `5 L* T8 x5 w4 p H1 ^0 T U0 @* D6 F' c) ?, r. [( C" H8 w0 W4 |, Z管制区域, + l. U, k0 N3 ?% L I8 R高于地面的指定极限以上的受管制的空域。 8 P0 o* t0 v; Y5 a- n制范围, G+ H8 {$ C$ A: a. h; K 由地面到指定的高度以内的受管制的空域。 ! `. F7 }7 S4 q0 t$ @5 R: |! ~1 i一个范围明确的空域。在该空域内,仪表飞行规则飞行. v& r6 k* ^6 a" @ 和目视飞行规则飞行有空中交通管制服务。 " o7 t# ~( f9 [4 G* R2 e# S% V- V4 f! k) |) b+ }0 `& z 受管制空域,; }" b3 j9 }6 @! b ~ 英汉对照民用航空词典B OEING U) A' b) w+ i" g' fTECHNICAL DICTIONARY 37+ h0 [8 G8 K2 I3 K. p; U CONVERSION, To change into another form.1 j: P, K- p/ `3 c" k* f: ~5 d4 y COORDINATES, The intersection of lines of reference,9 `- j% m- i! F sually expressed in degrees/minutes/tenths of minutes 9 H$ ^, l& M" \9 Wf latitude and longitude, used to determine position or/ f N7 s) V1 P3 R7 l CO- w) F# T2 x9 x+ y destruction of th 5 o2 h b6 A J+ B" b) i9 Echemical conta 3 d/ @8 w8 M" E+ R' p9 U; yCOWL, A remo 0 F" n8 k. W" f/ ?3 [; F% ~. z; Tfor access to th 4 X- @( Y' w, b& ?6 dFa 3 I t* f- D' u& p7 F& wNose Cowl - Front section of the nacelle for air inlet ' F# r# ]8 N ~to the engine.4 p K( S* D9 {: m5 v0 A: F! C& b Side Cowl - Cover around the sides of the engine. 5 W5 B! G2 b* Z2 OThrust Reverser Cowl - Cover around the core 6 W0 h2 I& {* _; \section.0 x; n: U3 F' r5 r1 u Translating Cowl -The moveable outer portion of the N5 |7 M u0 ~0 K) `! r, c# L" x thrust reverser cowl which is0 M ^, N+ o+ P1 n5 O5 H+ _ operated during reverse thrust.1 o" U/ W7 G" E, _3 f 标,7 T3 S2 z$ Q, d4 C 基准线的相交点。一般以经纬度的度/分/十分之一分 ; _+ H0 Z1 O& O5 Q5 h2 \0 \3 O读数来确定位置和方位。! [* O$ j2 U( N 腐蚀% G9 f" G$ g2 m! @9 t+ f1 O' R 动机外部可拆除的罩子。发动机上的构件必须要取下0 \% @- S: L2 [4 }5 L 流罩后,才能够到。 1 H' ?" g8 Y) U4 E. g& u- @, p" `5 q' s: _- J 机的短舱的前段。 ) s6 _+ { z& T: p% h6 U Z( e% ? ?侧整流罩一发动机两侧的罩子。 ! X! B, n1 d' S! a+ ?反推整流罩一发动机主体外的罩子。* m( c L, k6 B 移动整流罩一反推整流罩外可移动的部份,在反推工- o0 r! m- _, r- z8 Y# b* S" } 作时使用。" z( v- s1 n; n6 m: _- o2 e5 i$ ~ u 6 n* y9 ?6 a/ i$ r" d* J& No" \- }2 q N+ k6 ?7 e location. $ Z, W( o8 l6 \. y. G' ~, ORROSION, A chemical action which causes gradual 4 G. t- I1 w% ^2 he surface of a metal by oxidation or 1 G+ o. q/ C6 K& c2 e2 b/ \- Amination. : p4 h$ d+ z# K5 G+ ]' u q$ s3 ]2 Pvable cover around the engine sections 2 Z, v8 x! ]7 G; x2 r$ ge components on the engine.0 N6 f: v# t% Q! ~* ~- ^& X n Cowl - Cover around the fan section. , T% }2 ?. g. e5 _# V. n转换, % L6 d \' D* N: B7 m9 o2 f改换到另一个方式。 d3 O- [+ K, I b6 B+ s9 p T+ ~( i$ v2 p* ]5 P% m$ m0 q- U3 p6 G" |! U; @$ `$ O# L, N$ ?5 e氧化或化学污染造成金属表面逐渐破坏的化学反应。 , c& U" \" {- w" P% {! ^; _发动机整流罩, 6 Z* y. r- L! N1 J/ Q) i& u- ]+ `8 y( W' V8 K8 v2 Q7 _* N0 K; h扇整流罩一风扇外围的罩子。 + W; L; m( F8 T) F4 J前整流罩一引导空气进人发动 l! O% R: [# O x2 ]英汉对照民用航空词典B OEING + x8 I+ Q' d; C/ Q8 e5 I& zTECHNICAL DICTIONARY 38 . u5 o, T' {1 QCPU, SEE - CENTRAL PROCESSING UNIT6 p) r/ o1 g7 i8 @7 U& I CROSS TRACK, At 90 degrees from the desired track 6 Z$ f t+ h& y3 W0 }f the airplane. For example, cross track distance is the! ` M* E; O2 D, Y0 ~; m* L. E istance from the desired track measured 90 degrees Q$ ^; D/ x$ U- @! {om the desired track. 5 K' P* Z$ |7 O, X6 pROSS-CHANNEL, Electrical wire(s) connected from. Z0 l5 l4 r" H5 W ne system to another like system, for example, FCC 8 o- Y' f( \6 _8 ?- w1 W9 e" to FCC "B"." Y9 C1 j! N: {7 m9 A M( n- @ n adjacent engine or one on the other side. U0 ~0 C+ w; jl crossfeed7 _; T- A( N ]0 D; }$ F anifold for fuel flow from one side of the airplane to the : H. {' L: s7 P4 P1 f% Y$ f3 hther side.! K# A9 ?/ g& n4 m# W re: @) H& `( E7 s* {3 } RUISE ALTITUDE, An altitude or flight level " D1 v7 f% H9 Q3 b$ ]6 }( q2 S# l# i( wo$ v# s. d/ f$ A: ~1 y6 n d3 c, P Q/ W, z( ` fr0 X$ z& Q( x7 n2 V2 B. b% L: J C * q- o( ^' d4 n' s0 po 1 ?/ e8 G8 I Y6 a' r"A + x8 l/ R* ?$ T4 ?/ VCROSSFEED, An interconnection between fuel . ~- Y# e: I I" tmanifolds for fuel flow from one side of the airplane to + g; h. V/ A/ qa& b' n) j: Q! n$ ` CROSSFEED VALVE, A valve in the fue( k' m/ r* `( t/ G4 I m' h, e- y' V3 z9 {3 `7 g2 ], G( A o 5 A% r: j# A3 E8 u& H# @CRT, SEE - CATHODE RAY TUBE % F5 H9 [1 a# W( j RCRUISE, Phase of flight where altitude and speed a, l. U* h1 E) E basically constant.+ Y% w+ y" n; W7 r& m/ L2 C3 ]; p6 b C/ t! ]) S; }* M' L maintained during enroute level flight. 1 }6 r- R. p( l* ^中央处理器- y, l: S+ | f, e U/ p# D 见Central Processing Unit. 8 g+ M1 |& w6 u- w5 a1 ]. l交叉航迹(XTK), 2 C4 s- G. }2 U# e与飞机预计航迹成90°角的航迹。例如,交叉航迹距离) V8 [5 N( Z( f# u9 s1 g 是用与预计航迹成90°角量取的到预计航迹的距离。 + S' A" p! h: o; }' o通道跨接, 8 m. d2 a+ }! u- S" b电线由一个系统接到另一个类似系统。例如:由FCC / P3 [6 [4 S& Z# A; g6 c t0 R9 h“A”5 `$ h& F$ s9 p( q) w+ a) |1 D 接到FCC“B”.3 |% W, T6 F0 C: {* r" Q: e ^- ] 机身另一侧的发动机。 2 u1 }6 n: ?! e$ z* h) r7 ]& d# M于使燃油从飞机的一侧( Z/ m/ c( o' _& o" v1 b5 u 向另一侧。 , ?6 I3 ^/ R/ Z* E( n$ M, `0 d见Cathode Ray Tube' a) G4 M2 v" D& F) G k5 u 交输, " }6 Z( ^* _0 h2 ~燃油支管之间的交连设备。可使燃油从飞机一侧流向邻$ F& z& u- z! o$ l 近的发动机或在8 X8 C: n* y" Q$ `; d# J/ W) @2 s 交输活门,7 i7 i7 p- K ~" f7 O$ ] 燃油交输支管内的一个活门。用 ; L; H, {! S' i/ n- M1 @& O7 A3 C) Y0 K) F# I) Q- N阴极射线管, ( `& E. J' Z6 r.$ k7 A* |% s: s D; N. Y 阶段。 " P, w- g' r, k航高度, ; q( e9 l3 o0 g( f! S+ u飞行期间,飞机所保持的高度或飞行高 9 q+ \2 Q, G9 C) }巡航, ! g$ B s5 J5 G. k飞机的高度和速度基本上没有什么变化的飞行4 l8 y: x, W4 x( J- z+ X- y: V4 a- |) l 在航线上水平 $ b2 z6 `8 G* u: A& W( h* l度层。 + U B0 c6 ?3 a) d, Q; Y1 H英汉对照民用航空词典B OEING 4 R) L, ]8 f+ j" M% M, _0 Z7 sTECHNICAL DICTIONARY 39 1 R7 U0 z# v2 W0 ?$ d1 JCSD, SEE - CONSTANT SPEED DRIVE5 t8 z( d3 h! d& }5 k8 A# L& B# k CURE, A chemical change which takes place in a resin 7 p% N6 C' G& Z# @% [4 Z( Pand fiber based component causing it to solidify.+ J4 T& v, ]' g* q CYCLE, A complete series of events that take place 3 z& N X3 t3 ]0 P" v' M: \$ l( xgularly normally in a continual sequence. $ \$ Z8 S+ j5 ]( O+ p j) \: WAMPER, A device for slowing down or limiting5 r7 q2 n& J3 {2 P) r& @* W1 U DASHPOT A mechanical damper for slowing down & y6 Y: g6 Q% \8 iovement by restricting fluid flow.% d( a: X$ u2 D! F# A+ K D / P! p5 o+ k& S9 H* Z' W+ t9 [ATA BASE, Stored information which is used as the ) P1 c- a/ {8 L8 E+ E Tba ! C; y( o( h/ m5 f: A2 KDATA BUS, A conductor over which digital data is . " z$ f! c8 N8 [" H1 r# dtransmitted., B/ v t1 _& Z/ N2 B) H+ M DECELERATION, To decrease in velocity.: \# z5 K8 d% H 装置, 8 G$ [! J8 Y' nrive 0 ?: S( x. v3 x9 cre : |, G5 s: i& C4 X6 q/ yD , B& l7 K* u" a3 L/ {' aD9 w. [! E, D$ H1 I3 g' [2 R+ i2 L movement. $ d) ~5 }( \5 S! J4 i: E Im$ R7 ^: s, P5 v$ A9 n9 k+ U ATA, Another name for information. 5 o0 x; V# |- c: c( CD" ~/ W5 ]& M6 d D sis for computation. 4 i4 k0 @2 [5 K4 g( ~; o8 h; u恒速驱动- _; z3 b2 |1 a$ k 见Constant Speed D . 4 h0 U7 y% O3 r+ O7 K9 A4 N* r期, % L. }' y( `- A1 J! x' C不断重复发生的事件的一个完整系列。 ! U! Q7 p' ~2 E' y3 q. k, F" p2 ]尼器,: h. s+ h$ d$ s, U; K; m 慢的一种机构。& v3 y" \$ ^/ {; }1 v2 }- B; o1 n8 D# q# t$ d! `5 c( ]% O7 u r用限制液体流动的方法以减慢物体运动的机械式阻 ' E7 v7 f6 n9 s9 D/ i( r$ N; j8 n4 M! q ~6 G* ^$ u. [* P9 a/ V3 a' [8 P料的另一名称。4 n' c3 j6 n) ~1 l) C& z/ x 据库,% P' ?0 o, l" O, e& k2 F( S% e: E 数据总线,- b/ r2 ~3 d3 r" x9 J' h" f$ n 一条或一对导线,用来传输数字信息的通道。- W Y+ D1 ]+ r% r' U. L# ? 减速, # p+ W5 H2 u) I; v! D% E' z' @速度随时间的递减量。 8 C, n% x- z4 ]/ M+ I固化, 4 a! g% o( W7 G7 v树脂和纤维部件内化学反应使之成为固体的变化过程。 " x/ R' b9 p0 B/ }. y" _. r7 E1 ]) u% K7 ~, D8 b+ j 用来使运动减- \1 }$ L7 T; |( v) ~7 o 冲器,$ f; q( c2 `" z2 `3 W Q7 p 器。 + J+ }' ~, y/ S& }$ ]+ I g据, / A- w, u& u1 k0 i/ Y, A! ?; M4 `! ]' d8 P6 T" b/ n" I3 }8 W/ N. C) g: t( V储存起来以便在计算时使用的资料。% r0 X% X% D' ]+ P, t; J 英汉对照民用航空词典B OEING 6 w/ O4 H+ P9 w xTECHNICAL DICTIONARY 40* @1 d8 n+ k7 k, F DECIBEL (db), A unit of gain derived by computing the( A. R- W0 O; y! ? tio of input power to output power.9 N- g5 ~" n( v& @ ECISION ALTITUDE/HEIGHT (DA/H), A specified * Y( I7 E8 A! Y% _ltitude or height (A/H) in the precision approach at . [) \- W$ i6 F' d' A, z; Ohich a missed approach must be initiated if the 2 n" m2 M% s5 ]) R. hECISION HEIGHT (DH) 1, With respect to the ( ^% u$ S+ C1 ]0 u/ z& ]proach or6 d4 l$ u( l5 Y. ~* C execute a missed approach.9 e5 v- N1 c; S+ V proach to trigger the decision of either - q6 s- s; B$ `8 } Snding or go-around. & X$ [+ t& z! D7 @ECOMPRESSION, The loss of internal aircraft air, _% \& V% i4 q" j4 M ressure. 9 n1 H i9 O, c: aE-ENERGIZE, To turn off or cause to not operate. + O5 g' C( N& {9 Qrom the tanks " n8 z% G8 I2 N+ E: q9 fusing airplane fuel pumps or external suction. / M- P! n& |+ H/ v \算的一个增量单位。分贝# ~# _( R N! B, R, L 常表示两个声音信号或电力信号在功率或强度方面的8 G! J3 H; a/ C/ F$ s2 L 对差别的单位,相当于两个水平的比率的常用对数的十9 G) @0 G7 f' i5 A6 s/ Y 断高度/高(DA/H),9 V, x" j* f4 k# D: o U# z6 w$ F2 i 在继续进近必需的目视参考没有建立的情况下开始复* q4 b4 `+ w* O0 A 的精密进近中的一个指定高度或高(A/H)。* U" b1 N) D l3 F( r 断高(DH)1,$ G# u# a' o: c( I; Z& ^ 操纵而论,指在使用仪表着陆系统或精密着陆雷 3 I, i" S' n G3 h生继续着陆还是复飞决定的高。 5 [+ S+ h; X& l' @: {2 k飞机失去内部空气压力。 # i. E2 F' D6 [: t1 `) ]! O开, 7 U: O2 c/ Y7 p& E* _4 [关断或使不工作。 0 z% |/ z- p+ O2 w9 } M4 H% h机的油泵或外部的吸油装置将燃油从燃油箱排& M% q$ R' y8 L' C 出的方法。 % J& ]- M) c" w# C! Vra$ H. |: T4 O& M D 9 u9 B8 V' }6 E) r2 w0 @6 Ya( l# T' h3 l0 I7 U) k- H w; T1 s2 E* h x" u9 i required visual reference to continue the approach has( q* {) \8 n$ s not been established. 1 {5 @5 L* Y ]" BD, J0 g7 _5 o& W' q1 Z% h! E+ h operation of aircraft, means the height at which a # u& @: e# x3 w' u2 Hdecision must be made, during an ILS or PAR ; }$ j* k; _% w6 x4 p" c: tinstrument approach, to either continue the ap + Y- b6 X0 d" o: D; x% Tto 1 D- @! G# }. l; b7 ]DECISION HEIGHT (DH) 2, An altitude used during a- a9 v' b: W* v, C9 r precision ap % h6 @" [9 a1 w. J6 z+ Xla 3 F0 `( p# D0 A h, N gD 4 B0 C/ k O% k) t2 C5 {2 Pp' ?' |0 B3 e r D" E+ v- R5 I$ G7 N* I) ] DEFUEL, A method for removing fuel f 4 r4 u9 e& a% m& {: f分贝, : u$ O5 O6 O; u: L! I8 R8 U以输人与输出功率的比率来推 / u+ d4 [: u& H& [4 p6 W% P2 \4 Y7 K4 H; B/ T( ~! n2 G9 d9 v0 G3 e! r- Y6 p9 d) _$ w+ a6 S4 x0 n0 k, n. f0 [& O! p% l+ }1 U4 c就飞机 . h+ E% c! r6 X) O1 G达引导进近时,必须要作出的是继续进近,还是中断进场" I- L' [/ o, E+ P f. J* k 复飞决定时的高。 ! n: ?' C& s2 h6 N5 I: \7 D决断高(DH)2, . z2 V0 U% `; F; \! J1 o9 q3 D* r1 D0 s精密进近时产0 J" i- F& u0 o9 b/ o5 Y 失压,) c) L+ y$ x! r% M: z% P! @" X/ R6 o7 h* F+ s排油,7 R7 q* o0 `- ]& Z8 G 用飞 1 ?$ m# A; A4 W' ~' [英汉对照民用航空词典B OEING2 Q- \* Z: f$ P8 \( Q* x x TECHNICAL DICTIONARY 41, F* w$ R, W. Z$ h DEFUELING VALVE, A valve in the fuel system for & d, O1 ^, K9 i1 P# e% v* t" qefueling the tanks and for transferring fuel between the / B& B8 u8 r0 T& d2 uE-ICING, Removing ice after it has formed on aircraft. 6 g1 H( ?# x& JChange or difference. 6 Z1 s! s# r( Q: c7 j& u: WEPARTURE CONTROL, A function of an approach : y% @7 ]: l; o" ~ontrol facility providing air traffic control service for - u ?. M2 X0 ]5 R* u5 Q- E9 leparting IFR and, under certain conditions, VFR 3 D5 }8 V0 c# y0 u/ Z! kEMODULATION, The process of retrieving information : E, q) `, k* gcarrier voltage. : P; v4 O' t8 ~2 f" [ation.( C7 y. v" N( x lic 7 N' `; _$ h* `creasing hydraulic reservoir air pressure to , {/ o$ {3 \& r1 C# Gmbient pressure.! D+ F8 _9 S9 @3 a; ]* ]" K7 E7 O 箱排油和在燃油箱之间 - } Y4 ] y8 g# w. N9 `送燃油。 , a" y2 C5 z/ |0 c" b$ M9 v冰, 8 c0 N! N% Y: X5 {# z除去已凝结在飞机上的冰。( a" S4 ?) R9 f# K5 g+ t 删去或取消。 ) J& A3 r6 D4 D* t. Y3 T% }量,* F3 x$ o: ~( c, w$ V8 w- O 变化或差异。: C0 e+ l- A' P9 R3 Z* a& I 场控制, $ k Y. s( r, [给用仪表飞行规则离场,和在某种情况下用目视飞行 2 y- ~) T' u# K7 y/ h/ N! {, y. x则离场的飞机提供空中交通管制服务的进近管制设施 1 Y4 |/ \" g. Y" i c0 m* R: C, z0 L; B, n" @调,. m+ ~; T8 D4 A 电压中获得调制电压的处理过程。6 p7 ?+ y" g# }! w( p 环境 4 ?2 Y0 D" X4 O- [" e力相同的活门。 2 \+ s" M, J, }/ d+ Z* H5 |. Ad 4 B& I7 W# k. otanks.9 o$ o' a& F! [/ p6 M+ I6 I D $ W7 [1 v( j Q/ L7 g& s6 }- CDELETE, To remove or cancel. ) ^" }. @. y9 o$ N- \DELTA, 4 ]: {- `7 @3 l$ W" A0 y2 xD 5 w. b" { y& L+ J- ~6 f& o9 hc( ~! U0 t4 M; D d 7 U( u' v4 H$ i: T: Gaircraft.2 U K3 a' C4 A0 @. [ D * B7 `' c3 f/ j) \" m7 d# f, a- e(modulation) voltage from a modulated ! O2 }* r5 ?5 ?* vDEMODULATOR, A device or circuit which performs1 @3 @. n7 t1 D5 j5 E! b8 D the process of demodul, s3 M" r7 q# v' [/ U4 H DEPRESSURIZATION VALVE, A valve in the hydrau * |9 B8 W/ G3 |7 e9 l( R Fsystem for de+ X1 A& }+ K- X0 `& E a1 _* \) \1 j% ~8 @* Q0 ? 排油活门, 3 C3 R' r/ R$ A9 P燃油系统中的活门。用以为燃油 ! N8 G' O& l; Q. c4 V+ y) L) `5 H* T+ n6 g3 R* T6 p! \5 L! x& G: y5 W4 b2 v1 n7 a 删除, * `; y& k: A- }9 m" h X! l% O8 ~+ @; n% Q* l" t0 Q3 D) o1 y* W. I7 W1 s- |/ x+ I" W; S2 Y. z1 ]6 b0 |9 ^的一种功能 & h+ T% ~( J8 f" r6 W* o) v5 q: k" }( U从载波 1 `% q7 R0 n! `6 d解调器, $ k2 s9 |' a6 p完成解调过程的装置或电路。 ; t% e2 f. k5 C% X- i- V9 m减压阀,3 }, c$ J9 g$ W 在液压系统中,将液压油箱空气压力减至与周围: T8 Z, R3 v/ |7 H" U& D5 E$ ^7 }: k4 s6 b) Q* F- u2 t; i 英汉对照民用航空词典B OEING 3 c, n" J& b/ u' l) W9 rTECHNICAL DICTIONARY 42 4 `1 N3 Q- Y/ w8 GDESCENT, Phase of flight where altitude is decreasing. $ w& P% U8 ?; y' z5 tETAILED FLIGHT PLANNING, The calculation of fuel 1 {& {* M$ Q; Y' Z8 Hnd required for a trip by considering each phase of ; ^4 O* O1 ?7 k8 l0 s3 @( {! gight (climb, cruise, descent, reserves). 9 ]' p& p- u0 ]0 T6 E1 Fal or 3 u) p5 b2 f# cETENT SOLENOID, An electrical solenoid used for 0 p% |5 Y: m) r$ Y4 o' u9 St. $ U2 s3 z, W# H) ~8 `. k; W1 |specified course or 8 {$ O `4 k/ R! _4 U) i# erocedure. , S; `. u5 B4 p* G% ne. $ F3 Q n' l. D+ r, d6 d飞行计划, + @% b! o) b0 {; f将航班中的每个阶段(如爬升,巡航,下降,备降)都 * S5 Y) ^4 Z5 ^. q! ~+ [! e! z人考虑,来计算该航班所需要的燃油量。 $ n5 i# B/ Z- z用来感应情况之正常与否的电气装置。# [) j4 N2 U2 c+ ^ 定电磁线圈, " O! I7 g' J8 e0 e4 Q6 c1 _出接通的电磁线圈。6 b& c7 z L! [8 t 差,! A, M s. h& E3 Q 与指定的航道或程序之差。& |/ p/ K* l% V" O" e3 U, m: b2 i 用气压或液压操作的活门机构中的柔性部件。 4 X: U, \5 ~2 q: CD" ~- U) @1 O7 C1 ?" e J8 }+ \& B a+ d/ ~+ {/ @+ C5 J& L fl 9 q2 U2 l! i1 S+ y# eDETECTOR, An electrical device for sensing norm: A' h- c( |0 \5 A, z abnormal conditions.) J3 X" {+ L2 o: J, I7 u D6 e6 O% r5 `; D$ t! R- s controlling the engagement of the actuator outpu8 w# Y! k5 I; p/ \7 H% e DEVIATION, To change from a! @$ E' p9 {0 l" l p0 ]( L8 y8 J2 ~; ` DIAPHRAGM, A flexible part for operating a valve+ x# e4 l3 ~$ y- N' f mechanism by pressur ( U; y& K) \. @! w. u下降,: Z* I$ g+ L* d% T4 U6 F 飞机高度不断降低的飞行阶段。 5 n, C% d2 l1 x$ O! A$ m. o详细2 x3 W! V4 Z, }+ ]1 V2 {/ x7 n- f8 g1 z, J 探测器, 7 ^" D) }, V- s8 O, h4 x! {$ p4 F. Y0 l: P 用于控制作动器输 / d& F" S7 l6 M! E& ]7 m6 m2 C 隔膜,0 B: i- N8 s% y# o; o 英汉对照民用航空词典B OEING 1 Y: D/ I& T- V7 E0 _TECHNICAL DICTIONARY 43 C( v: g( Y3 O' B; `4 o" z' m DIELECTRIC, A material which does not conduct : E; g" v2 `1 u- H/ ~2 B Belectricity and used between the plates of a capacitor4 S7 j+ }6 f7 f: _3 K6 O0 t (condenser). # M. T7 _2 L! ^# S9 P% u; p5 tnother pressure in the same system, measured in * {* F( p' s: o. \; \# @* ]ounds per square inch differential (psid). 0 K) v& y% L; M3 u) }IFFUSER, A part of an engine between the4 I- k' F. N: Z* v ompressor and combustion chamber for reducing the/ m: J) |* _# q' ~3 F8 B3 u, S air pressure.0 v+ W" @) P9 k5 |4 I3 R6 _+ t8 g# Z igh # d; U# P' w: J0 G- z9 R* v+ ?pulses.9 d* w% S, w% r; X+ k1 p ignal that is a close approximation of the original 0 B, g; b. Z3 z& q: oignal. ' l! K( O `2 H0 R" J$ XIHEDRAL, The angle between the wing reference # G# n3 s: N9 K# Z" z, j9 Xlane and water line.3 `: S7 b8 F- v! P- y2 Y1 z3 n' W 的压力,以每平方英寸 6 Y- X" u( {' X少磅压差计算(psid)。" e3 f, i$ S+ \- _2 c9 S8 Q% ^ 散器, 5 O0 @4 ?- V4 x" }' i0 p: h6 N发动机内压气机和燃烧室间的一个部件,用来降低空 N& m0 a9 \( y0 V, |5 g* I增高空气压力。2 N; c+ d1 n6 @4 F; V1 q. G 换, 8 A; Y$ H( ?5 u1 e8 x$ v的连续可" r: m/ n0 C9 W (模拟)信号的处理过程。3 ?( `5 a2 o% F2 ]7 g* D$ ? 反角, ! e" J Q/ O& [. M机翼基准面与水线之间的夹角。 3 Y/ [) }4 i. E0 N2 W: ZDIFFERENTIAL PRESSURE, Pressure relative to) P5 Q: Z+ A, ]4 K# X a% ]2 {2 p* v9 j* l) O6 e p4 f4 Z- [* g+ R* R7 m' Q+ c9 q) w. C D ! a- W u( K; ac ' J! ]- l, q; x! mairflow speed and increasing the6 V& C* k) z7 o% n) k- f DIGITAL, Digital refers to a signal whose amplitude & A7 P+ m) d. x5 l# oremains constant for a finite period of time. Digital- v: i5 H% `1 n% L- ? signals are commonly represented as a series of h . w Z7 x- i$ g, mand low 7 @# s5 C# Q9 K9 G0 MDIGITAL-TO-ANALOG, The process of converting a 4 m" L: D0 H; v/ s, S' Wdigital signal (binary) to a continuously variable (analog) y7 @7 y. H7 N8 ?3 Y s % T9 j C1 L7 e, v. a+ hs " w9 p/ \# z* S: P; y4 g- ~3 ~, @D q" V+ |8 D2 J0 J3 a p 0 |5 O P7 S& N+ f; c4 j电介质,7 ]. f$ J' l8 h* o: Z 一种用于电容器板之间的不导电的材料。 4 x5 E) j3 O& I: ~压差,! ^: x- ~, i6 u! C7 Q7 t 相对于同一系统内另一个压力4 ? q6 d) @& W0 e' i. D* y1 a; {. f" c0 ^9 c% f6 P) u8 T# k气流速并: i! p% J* w0 k 数字式,& [! r: N% _( o& j ~6 k$ \8 Z 指一种信号。该信号在一定的时间内,振幅保持不变。 , ^9 ?& W/ a& y- t通常由一系列的高低脉冲表示。 + {; P* `4 q$ d/ M0 k) |' g数一模转 ' M3 W' j$ W7 K+ D0 V将数字信号(二进制)转换成与原信号相似 1 M2 ?7 v7 X) L3 ?/ j$ @2 v, k8 J5 y/ g% E: _6 y7 O 英汉对照民用航空词典B OEING) ^% K. b: J t/ t; N5 S: ` TECHNICAL DICTIONARY 44 ( `3 \# `" X0 K e& P( aDILUTER DEMAND REGULATOR, A component in the* J+ y' f1 q x4 x5 c( o crew oxygen system which mixes air and oxygen and1 b9 C" \3 V& d0 j7 i/ u upplies constant oxygen pressure even if there are 9 R7 W% P$ t- D' Mhanges in ambient cockpit pressure.8 n1 k; Q/ K% w4 D) J# T. q) r. ? IM, A word value of light. For light control devices - dim6 `1 c1 N% r. H( T3 ]4 x e the opposite of bright.3 g3 e# W) R7 y( d! Z IODE, A device which allows electronic current to flow8 v T% N+ s; \$ J4 O% o5 e$ S only one direction- n* Z% ?& H& u/ N' y9 p' Q uid in a reservoir.5 e4 C# f" L0 r2 Z+ X9 K6 u DIRECT, Straight line flight between two navigational ( {% r1 B# ~+ \) y9 G! \aids, fixes, points or any combination thereof. When * m" s a1 A s: r, H! |4 |used by pilots in describing off-airway routes, points; c {% f5 i' Z# f+ ` defining direct route segments become compulsory7 u/ a. E5 W1 a' e! ] reporting points unless the aircraft is under radar* F8 p- N2 ^) D9 r2 a q% ? control. " m6 f( i! s x节器, - T7 c! i b4 J5 p* J将空气和氧气混合, # E: X9 h! @: T1 g5 P5 R& h; ]3 W使驾驶舱环境压力改变,它也能提供恒定的氧气压力。2 n/ O! R1 r! X% K" b1 Z0 V! M j( X/ O9 \0 l5 w. u2 e一个形容光线亮度的词。对于灯光控制装置,暗的反2 y" m: Z( b3 |) U0 M 词是亮。 4 @5 M$ `" F" C+ t' q) D9 ~2 K极管, 4 e3 j+ U( ?: |1 z4 e3 A3 i只允许电流向一个方向流动的电子装置。 1 ~5 P3 z# ], o S9 C, j1 o器内液体的量。# j m3 n, c* b9 A8 I 直飞,2 p( h) t5 b- w+ J, o9 ]$ A& I 两个导航台,定位点,导航点,或任何的组合之间的直 }9 z: T+ q, R. r6 z线飞行。在被飞行员用于描述偏置航路时,除了在雷达控 3 }& J" O! c7 J, n制的情况下,确定直线航段的导航点成为必报点。6 a/ f1 Z8 T8 ?0 v: q s / O: X4 M$ P: j+ F% v( yc! {! {2 G8 \. R/ d D " H& f( R+ e. M& f `' n) G& Mis8 d9 w& F2 `/ r5 c& N; V( ` D4 ]; y$ s/ M2 Z in5 v# G- h2 X4 A9 u DIPSTICK, A calibrated rod or stick for measuring a ' v$ E& l6 a5 V" S5 K! K4 P7 Squantity of fl ( A- Q& v5 d2 a5 |稀释氧调 6 `' G+ m6 U8 E; c- M% d, l驾驶舱氧气系统中的一个部件,它 ! E( ~/ y. ^3 g: T, y1 b: _; ]) X9 H$ N2 }; A" O. x, }4 C$ s/ O3 o0 s0 u1 P0 S8 Z9 T. B& O0 t# T+ |1 @5 m! Q0 v: ]4 W/ f$ Z% V- R7 s量尺, " q$ [( L, ]/ m7 d1 Z" ^校准过的棒或尺,用于测定蓄液 2 ?! a6 r/ C: J9 ^# v英汉对照民用航空词典B OEING3 O6 [5 M! O4 } TECHNICAL DICTIONARY 45

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