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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 . I p& Z1 D6 ^: B+ F1 t ?; g民用航空词典 # K# O( P3 F' m; r; k! U/ _波音商用飞机集团 6 u1 V, H/ u& x- C ` C4 KBOEING COMMERCIAL AIRPLANE GROUP * I. H* w4 k1 T- A# [英汉对照民用航空词典B OEING+ m5 P2 p" _# B. _ TECHNICAL DICTIONARY 1 * {! _3 k7 B' {1 r, r* U5 z+ OA( u' ~- C. q! m; B) Y ABEAM (ABM), Beside: An aircraft is abeam a station: o' j/ u) e# \, C2 S2 h. ? when that station is 90° to the right or left of the track of5 h5 N! v, g; N$ y* X) q9 h the aircraft." g# Y" \4 m/ @6 s* o0 F9 u ABSOLUTE ALTITUDE, The actual distance the aircraft + Q3 V4 z5 P2 d5 T* S# L+ Zis above the ground. ! R! }8 e8 o- }& N% pABSOLUTE PRESSURE, Pressure of a liquid or gas % v& v F6 M) }8 Tmeasured relative to a vacuum.+ f8 W2 \8 L% {( z& m0 |' m$ c ACARS, SEE - AIRCRAFT (OR ARINC) REPORTING6 X0 j& W: U1 S. p9 E J ADDRESSING AND COMMUNICATION SYSTEM $ G1 `/ [1 R/ x/ w+ z+ z& VACCELERATION, The rate of change in velocity with/ q8 x1 Y9 x6 ^& U# _! U respect to time. ( o2 ]- l. ?( Z$ }ACCESSORY GEARBOX, A part of the engine, + }! p3 P, X$ ~9 g2 Pmechanically driven by a compressor or an angle( [7 b& m; b+ ]/ p H2 [ gearbox, for driving components necessary for engine1 ?; n4 d8 O% [4 y3 w 正切, + y5 n1 a% w+ N* v7 E0 `and airplane operations. @3 @( i2 B( H6 Y& w: }$ x2 A5 `' \当电台在飞机左侧或右侧方与航迹成90 度时,飞机正 " i- Q- T* M2 R* T0 c) i切电台。- I, I8 m! f- O* @% s7 k3 R5 T 绝对高度, , ?; T6 U: F! X. i4 O' T8 I: R3 x/ U飞机离地面的实际距离。* d/ T+ W8 x( x. a/ h 绝对压力, + s+ l8 W `( f( T5 h相对于真空(无压力)测得的液体或气体的压力。, o- N1 V9 L( l# q8 b" R 飞机通信寻址和报告系统, , D& s6 H) O' _: ^7 E见Aircraft(or ARINC)Reporting Addressing and& T8 g3 T7 K H/ } c Communication System.9 Q: J2 \3 O ~8 ` 加速度, # r/ S" m; C, s随时间变化的速度改变率。4 @. I& L8 j+ ^3 v7 U* n$ K8 D 附件齿轮箱, 1 O1 v ^# r1 L5 J发动机的一部份,由压气机或伞齿轮箱带动,用来驱动/ v4 c1 y' F) o" i8 |9 g6 P 一些使发动机和飞机工作的部件, f: K# {5 X- n! P! Z$ L& w4 S+ @ 英汉对照民用航空词典B OEING 4 }. ~ N6 e6 }TECHNICAL DICTIONARY 2 $ W7 h3 {! n4 a' T0 Q1 l5 D- @ACCUMULATOR (NO. 1), A container with hydraulic8 e( u. H* X5 r6 K ts when normal hydraulic supply is not. M- e1 b2 _6 S vailable. ! T. a, j+ Q, j) sCCUMULATOR (NO. 2), In a computer, a special# S3 Y% ~! E( m torage register associated with the arithmetic logic unit,$ l. B6 S% K g& l olding the results of a computation or data 1 r5 k) h* z3 R: F& m" b& HACTUATOR, A mechanical device operated electrically,! x/ Q- w, w0 U hydraulically, pneumatically or mechanically for 2 M4 O3 n9 g6 W i- Stransmitting motion between components. - U7 \- }0 g z% {ADC, SEE - AIR DATA COMPUTER) j# D& E) ?, H, o' x; s; Q ADF, SEE - AUTOMATIC DIRECTION FINDER 6 e1 F6 U, b8 n& xADI, Attitude Direction Indicator, An electronic display of $ }6 ~% o) Y+ G* p/ a qairplane attitude information in pitch and roll.7 e) w S$ W% B& } 蓄压器(NO.1), / e$ V. j, R8 U* s) h% s+ L含有靠干燥空气或氮气增压的液压油的容器。当没有正+ d& r7 e: i( C. F, j& P7 g 常的液压源可用时,该容器可用以驱动部件。 % x, [1 G7 F4 `0 i, y存储器(NO.2),0 v4 v9 r. o v0 M! S 计算机中,一种与算术逻辑组件有关系的特别存储寄存 9 [! }( Z0 \+ u) _; Z- V6 ?7 S器,用来存放运算结果或数据传输。: C; @& Y- `% B1 r$ z* i 飞机状态监控系统, 7 a) _& t- c$ I3 S7 P见Aircraft Condition Monitoring System5 n# k" j% n/ s1 y5 A fluid pressurized by dry air or nitrogen for operation of6 J/ F" ~/ h, g- V2 _* g componen 5 V2 e4 q0 B& Q& B( `* W" `0 aa$ ^4 [- d% S0 m1 C A6 V( [3 I" J+ b2 l- g3 L. |; e3 A/ R s ( X- ]0 m# j* i' U: r. k& mused for h# f L1 j' ]9 [0 w9 y transfer.$ q( I/ i, f' ^0 K$ K; L ACMS, SEE - AIRCRAFT CONDITION MONITORING" U) |& P+ J5 Q SYSTEM .+ o; ?9 v. x( N/ U) i: [ L" g8 k3 c 作动筒," i3 f6 E: ?1 \; u 由电,液压,气源或机械驱动的机械装置,用于传送部 / A3 ^* E% K( X* S! t) d件之间的运动。" D6 v; I7 O6 s" l 大气数据计算机,' c s3 `. i3 g 见Air Data Computer. % _. R9 s7 L0 \5 i$ p2 d自动定向仪, . I( K {- P$ _% g) m) S见Automatic Direction Finder. 5 d0 F% F; K4 _8 @+ |$ E4 k姿态指引仪,7 k$ s: K4 Z2 G! m 用来显示飞机的俯仰姿态和坡度的电子显示。 " c5 y+ l- E# \7 n. B* s英汉对照民用航空词典B OEING $ Q. ?- V% M. m' n0 xTECHNICAL DICTIONARY 3) h# w, l0 s5 H AERONAUTICAL RADIO INCORPORATED, ARINC is4 w% f4 t- Q& V9 ~3 O) S0 n b# H ,5 ~3 i/ a4 ~( h+ M) i nufacturers, and foreign flag airlines. ARINC( x% D) `0 I9 \) w' o1 X evelops and publishes standards for electronic ; `* n* z) ]1 w+ E% I9 xquipment and systems. 4 _) e2 R r+ \) B/ {/ l X* tGILITY TUNING, The capability of the DME to ! a& v3 M; x H' W7 u$ Clternately tune between two different DME stations in / D) J6 E9 }8 y1 N+ f yrder to get two distance readings from one. e5 V0 W6 l; m8 [5 @/ Q terrogator. . z3 ~) w# k4 _ge6 K t& l" }8 i+ t2 V ILERON FORCE LIMITER, An electro-mechanical 8 U! Z. d+ p: x" G1 {IR CLEANER, A component in the pneumatic system' Q; b) z/ ^. f) C upply to the air* g3 D9 Z' D( B0 w5 G onditioning system. - e# `& \2 U& _; b3 V! B; s" Z订并出版" b5 M- o. Z' z 子设备和系统的规范。7 Z* F. T8 Q1 L 快速调谐,$ Y2 x7 N2 D5 M% x& C5 ]- \$ c 机载DME通过交替调谐两部地面DME电台以测得来自4 V7 n. C8 u, T$ j( ]( v! g7 N+ Z 同一台询问机的两个距离数据的能力。& |6 ~% j) g4 Z. M3 M- R. N+ H 翼操纵力限制器, $ J# y, Y( Z! K3 c装置。在自动驾驶工作期间,用来限制驾驶盘, c) @* ~8 [* p; S- h7 H' U 气清洁器,, r: u( j6 c4 h( u' c9 J1 O 部件。用于去除供空调系统使用的发 2 q, X4 Z5 n! T$ M: l+ Ha corporation whose principal stockholders are United/ A, q4 }* s" `" f7 W! X9 L% I States scheduled airlines, air transport companies+ t: o8 {' _( n+ H aircraft ma " B+ |. K5 Z: @1 o7 o- Zd2 O' {/ _; V# k: J4 X e 4 Y1 y- m; B3 H" h6 \" O9 P1 rA0 p% Z/ u: I1 ^# } a . n9 f) n3 g' M6 s8 So 8 }# B! I$ ~: y# Ain' i0 V; ^2 t; t" e$ g AILERON, A hinged moveable part on the trailing ed2 W2 ~5 M1 b. d: a! a6 m3 J of each wing for airplane roll (wing up and wing down)4 M- p. B7 r) G3 e4 | control.0 G6 c! }( K5 c- u; E8 @ A 4 y3 ~. ^; [* u- bdevice for limiting the control wheel movement by the7 {! Z( v, h5 ]7 l- I6 Q) ~6 V autopilot during autopilot operation.+ ?! g9 ~7 Z: p. T5 Y6 N* D( v2 p A : L+ i3 `7 d1 Nfor removing dirt from the engine air s. I1 t Y4 a! M% J4 E: i% V c; l6 h4 B$ Y4 _+ x7 w- O" E# h4 \; I 航空无线电公司, & u1 ?/ v ^1 v1 J1 T q主要股东为美国定期的航空公司、航空运输公司、飞机 + V" M) h( e+ s* [# r制造厂和外国领队航空公司的组织。其目的是制9 S7 X% x) G6 l+ E. Y2 H: Y. `6 H" \# D+ s- T3 k+ e' X( o4 _& m; S 副翼, + J' K U/ l5 u9 Y, Q( l9 _铰连在每个机翼后缘的可动部件,用于控制飞机的滚转/ c+ l% _( P$ I3 E% K4 x, x (机翼向上和向下)。+ x/ T( n: [8 i* d a) ^8 G& X/ H9 f1 G$ I 一种机电 7 m/ N7 h4 l. N; m的动作量。& K+ r3 ~2 b+ ]' v0 O$ ?( V O0 p: p' I* Y0 y7 [ 气源系统里的一个 ; B: y7 x* W! D1 O- ^动机引气中的灰尘。 0 V: |, R5 m' r$ @- v" b英汉对照民用航空词典B OEING5 _, `1 N) A1 T0 ]9 G TECHNICAL DICTIONARY 45 {( E) e6 f/ S4 ? AIRPORT ELEVATION/FIELD ELEVATION, The1 o, q# `* K$ u highest point of an airport's usable runways measured( ^1 P3 L8 _# h in feet from mean sea level. In a few countries, the3 z4 }$ N. O) M airport elevation is determined at the airport reference 3 c: h, n- t3 _; w5 ^+ h9 cpoint. ; C& f8 m. D3 ]0 E0 ~AIR ROUTE TRAFFIC CONTROL CENTER (ARTCC),- p9 Y2 @$ D; q2 |% |5 X ervice P& t3 I6 ~4 ]# v7 O ase of & p7 p2 ~# I3 J& Mus flow of air traffic. 2 v) J1 G! c& F# ~& k: X7 ^IR CYCLE MACHINE, A compressor and turbine on a 5 I9 y3 [+ F* h" W |8 ?2 ]' ^ommon shaft for cooling the air in an air conditioning : L; T- \8 P1 Pystem. The air is cooled by expansion from high to low* p: B- i4 f3 I ressure across the turbine. The compressor is driven/ r9 R# ]3 }* l y the turbine. [9 y J" { q: T; f# U! D) \$ [ 中航路交通管制中心(ARTCC), 1 e- A. O6 w& R: B& S$ j0 |域范围内使用仪表飞行规则飞行的飞机提3 q' O% v$ ]5 n+ C) A9 T# f& K 管制(ATC),) x; E! I& V$ F9 {* I0 V u 涡轮冷却器, $ a: g' o& ]* e/ \6 L9 E& R9 s是装在同一的压气机和涡轮,用于冷却空调系 " Z3 @! V$ s5 f统中的空气。气经压气机压缩后,由热交换器移去热量, 5 V8 ?; |1 L( V然后经过涡轮令涡轮带动压气机。通过涡轮之空气,温+ m: b0 _) P& J ^/ h$ G8 S1 b/ F: q 度下降。 + I6 n4 |4 ?0 \/ N: I( W& {A facility established to provide air traffic control s 3 ~* M! _1 n7 Y. e k, k) oto aircraft operating on IFR flight plans within controlled . ~6 f+ H& G3 Y8 N' I7 tairspace and principally during the enroute ph! G' G$ B( V- k% e flight. $ W' J+ D" t2 l P% R% y ]6 oAIR TRAFFIC CONTROL (ATC), A service operated by 2 Z0 ]3 S& y6 ~, N2 W+ _appropriate authority to promote the safe, orderly and2 X5 U0 u. i: ^) G expeditio5 I/ z9 h" J& X A: X( @$ x3 @, k! S! G0 j c ! A/ v! u9 n' Bs 8 }( e9 _2 |' l) e% ~p- P- N6 J8 W1 F" B( U% _$ Y b0 h0 j5 G) {# R: i/ I) H( A. O3 c 机场标高, ; \8 E6 \6 i/ }& m" U指海平面与机场可用跑道最高点之间的距离,单位是英 : ?+ _4 E& I+ G& B7 A1 A尺。有几个国家的机场标高是由机场基准点而决定的。 ( ]( ]7 H$ s* R( n5 q% y) i' A7 S6 v& f( Y 给在控制空 # u/ g" `% j/ Y- o6 W9 u9 H供空中交通管制服务的站台。 ' I2 ~2 M% i4 T6 E空中交通2 Y+ \: W8 C: ~0 N* \: F) z 由有关当局管理,旨在促进安全,秩序,和效率的空中0 u: [+ T5 k9 T8 w% c7 s. T8 P( y" v7 h 交通服务。0 W0 z( b' O/ ^1 f; H 根转轴上$ {2 w1 B. {# C: ^$ C$ `" y1 V6 x( ~9 Z% d+ _! k B2 D, q# v& C% H 英汉对照民用航空词典B OEING 1 N3 {: m: ?" U& Q2 T) Z+ \6 ^TECHNICAL DICTIONARY 5

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发表于 2008-12-24 21:36:52 |只看该作者
AIR DATA COMPUTER, A computer which produc4 U4 O- a, J( w data information, such as altitude and airspeed, based 7 g8 }6 M/ s+ K& g& |on pressure and temperature measurements. q6 F+ ?7 V y0 H1 y0 Y1 C4 j es air% z6 t- L8 l0 `2 O! O* m IR TRAFFIC CONTROL, A system comprised of , |) E7 c, [7 Bround and airborne components used to identify, track( h; d% s- m3 _! ?8 H: f, m OUND SENSOR, An electrical device operated7 T$ m* I3 J' w. w2 W, f0 v" z* d2 J A, y y the landing gear, which transmits on ground/in air9 e9 d" T- K* u( ]. r formation for system operation in flight or on the( b2 x0 _$ J9 O. c round.# i, c. W+ j: S/ Z IRBORNE VIBRATION MONITOR, The AVM takes0 ~: H. b$ k9 Z; v e signal from the engine mounted accelerometer and- V6 n7 e; v9 O7 h alculates the vibration on that engine.& c% S) y4 V1 e- m0 ? corridor equipped with radio navigation- e# B: V; }+ }2 R; G/ Y$ \- ]6 u! Q aids. 8 F. G0 g- @5 RAIRCRAFT (or ARINC) COMMUNICATIONS3 w( z. M" g3 C5 S ADDRESSING AND REPORTING SYSTEM, An " n- w0 m3 b$ G5 h O2 baddressable digital data link system which permits the ! `5 u6 l- f6 |0 qexchange of data and messages between an aircraft + Z# V+ K+ \5 b) U3 xand a ground-based operations center over a radio 0 v: l ~" z- s: O: Jnetwork. : `& T$ j$ d. g% ?( IAIRCRAFT CONDITION MONITORING SYSTEM, A 4 r1 v6 }5 D7 t0 m6 usystem of sensors and recorders to monitor various. j. l* O" f. x( p; N9 } k airplane systems' performance and status. + b) o I5 ~% A ^- X机, - a5 ^6 {2 c# v ]4 G中交通管制, e. N+ b" [, }: C. E 一个由地面设备和机载设备组成的系统。用来对飞机进 d2 ?3 x- i& B地传感器,& c- }$ N d b8 v+ K 一个由起落架操作的电气装置。用于给空中或地面的飞+ ^! b, p1 W! T% H( |2 i 系统运作传输地面/空中信息。(有些系统只能在地面 ) d8 S7 ^" G9 |' C用)8 u7 j( a3 Y# i& ~4 W' S3 t 载振动监测器(AVM), X9 f7 _- D! Z/ e1 `8 M4 {6 T AVM从装在发动机上的加速器取得信号后计算出该发4 ?0 z3 V8 U- w& G0 N7 Z6 H* o, T4 U 机上的振动。) C% {% ]3 u( Y, r( y8 q 式建立的控制区域,内有无线电导航设备。5 z' ^" |; W! n) n" e: O 飞机通讯寻址和报告系统,' a* R+ o* O- i, _7 Z( l/ X 有种可寻址的数据通讯系统。利用该系统可使飞机与地7 h7 Y2 r/ k7 b. u/ P; n- s/ L/ h9 Q& h9 d 面操作中心通过无线电网络进行数据和信息的交换。 O; P- ]9 M7 V" X$ s 飞机状态监控系统,& w+ ^5 _) v% X9 v3 ~; W 一个利用传感器和记录仪对各种飞机系统的性能以及( X% y% r8 C6 R* n+ G 状态进行监控的系统。 1 w" }! t9 Z! H+ E, K6 ~A, m7 U% p8 p1 M: `# S( a g) @7 b$ I7 z* a and locate aircraft. a/ n+ k" U3 W. N AIR/GR 5 `+ F* O$ s( ~& J9 c% gb. f2 j7 U {) k in & S' x3 y" {4 b) U- O& bg6 \9 c S7 O# v6 y" o A$ b) X m% ^' k* V7 y2 u, | th 3 g, Z6 I/ x! L5 |1 H9 @, ^c 3 o- W# j) K" s. W% I V) aAIR WAY, A control area or portion thereof established % ?, `1 y4 }4 B' T. ~* j& }in the form of a . U. C S5 E$ o1 K# k: O大气数据计算) j! V6 i4 X! Q9 \ 根据量取压力和温度而产生大气数据资料(高度、空速 % m u: p4 P% d等)的计算机。 / q* e5 b D, F# N& k- y' K) c$ y& p1 {6 s% T/ f( E' _行识别,跟踪和定位。% A7 C9 S! }' J+ v8 W4 P$ Z' C" C4 a' e! }: w' R: B8 [# O. `3 H* T& k# N5 I; k( D使 - d" u0 q& ~5 w6 K# J7 `9 U s' l) V* r i* b, H/ x' J8 o. b航线,$ M" o9 T* B0 z" K 以走廊形. E; C$ b, O1 u2 F5 X! ^6 ] 英汉对照民用航空词典B OEING' i9 v/ g+ p* T; t0 q4 r. u o TECHNICAL DICTIONARY 6 k& v# d- a$ R, [3 |: l9 |AIRFOIL, A surface designed to obtain a useful reaction, 3 U% b( _8 E" }" H3 h9 q/ { gsuch as lift, from the air through which it moves. Wings, 4 N6 m; K* H' c7 _% hstabilizers and control surfaces are airfoils. 4 p+ s+ N. d8 K B( |4 `AIRSPEED (IDS, TDS), The speed of the airplane + P6 A8 c( e" }$ B2 @# Grough the air.% r5 G+ ^9 d# C5 R D INDEX, An adjustable pointer on the 6 u4 }' O! T0 {3 m2 p1 ^$ d8 Eirspeed indicator.* N4 [/ k: [* J( T# G) s and legal ability - l5 m% T9 l( Dfly.+ r7 I: r5 j- v$ Z0 f m, for example, the procedure for finding the " K# K9 E. s: xquare root of a number. - J8 r2 r& N. W6 L. Z6 h3 ?y o/ H5 l- F( r! l) D" T' H7 | re, wind, ! g- H4 s, }4 s7 j. b8 yand aircraft flap setting. : R" C3 w n% t是翼面。( P4 M1 D0 h7 l8 ?1 G R. { 速, 8 F, x' O- D, o飞机在空气中运动的速度。" M) s( t2 @' N) l+ h9 D3 e4 g$ v g 在空速表上可以调整的指针。& G1 L0 n" l2 _1 b: K9 h 机械飞行能力、和合法性的飞机状态。$ E$ z- A9 d& ^( Q, J" u 一步一步的解题方法。例如,计算一个数的平方根的步1 E5 d* i' Q' s* `' [. p! J4 ]7 n ^5 U8 |& F4 c: `9 i$ Y% s& c7 Y. m1 p: X( o; @ 资料的法定文件。4 Q3 H6 R$ k" P9 N' l8 u 翼位置成函数关系。 * M, d: |# P$ D( i1 N( Ath & {- I2 E3 k$ s1 ^AIRSPEE5 a4 b3 [; Y7 G7 Z a8 C" Z2 S* y, z" j% B( C AIRWORTHINESS, The condition of the aircraft with 7 |& Q( f* k+ X) ]9 C2 ^" u; brespect to its aerodynamic, mechanical, }3 I, G3 @! f% K" Y! M9 M* Rto! Y. g! a, @: b& a) m ALGORITHM, A step-by-step procedure for solving a # K1 e2 s* L& {* ]" f, O+ Cproble 2 d6 ?+ F8 _5 i! b. g1 Ss 3 g7 e; `3 ?/ j* i4 b& j' a5 r% KAIRPLANE FLIGHT MANUAL (AFM), The legal 0 e7 f5 w) f4 K: j4 Ldocument containing performance and operating limits, + {0 P7 ^0 f8 v; p1 Poperating procedures, and takeoff and landing5 K- W# `9 k* b$ D! [+ u performance. o. @. q. {- |5 u AIRPORT ANALYSIS, A comprehensive set of takeoff, e6 a4 E# ]& v, I weight limitations for a given airport runway, generall1 r; g! G; A: Q9 ^5 C presented as a function of airport temperatu" b' S1 W3 c! l" z% M# }" m 翼面,: y2 n j8 B y; \6 H& I 用以从气流中获得反作用力(如升力)的表面。机翼, ! u+ i' m% ~, d安定面和操纵面都4 E. }+ N" ?. T9 x1 [/ T& C v' F ` h7 a- m0 C6 ` 空速指标. b# w0 g- w$ p 适航性, 3 J+ N7 b/ _9 n8 k+ }# W有关气动能力、9 ]% x* K/ D y E3 m# ?+ { 演算法, ' u+ z3 O1 X$ H$ V( X# l) h, [7 _' r4 Z1 O3 x1 K2 G飞机飞行手册(AFM),$ H8 L/ X, o6 E: B. o4 d 包合性能极限,操作极限,操作程序,起飞和着陆性) F7 \3 t. _9 z" ~0 o. o& X" V6 Q1 _" R5 b 机场分析,2 g9 A5 E; ]# _+ F# D, ? 一套针对给定的机场跑道的详细重量限制资料。通常与! _. F$ |! s5 U L7 e T 机场温度、风、和飞机襟: I, a% E2 y: I7 S, p, ^. u 英汉对照民用航空词典B OEING! w$ w0 a; r9 g# E1 ~ TECHNICAL DICTIONARY 70 R' G0 ~2 N5 Q AIRSPEED BUGS, Adjustable pointers on the airspeed. A& s4 h' Z0 I indicator. 4 s1 ~3 _2 ?- {" Y+ m' eALLOY, A mixture of a basic metal and small amounts' k' i& v& H2 G. `' a. n f other metals to change the properties of the basic - ~) b9 e3 Y1 p$ M5 Oetal. ! O4 ]$ n* H" kMinimum airplane speed.( ~8 @; Y/ `% y. C) z2 j3 g! d e of8 B1 W3 x$ i! o itting airplane angle relative to. d8 i7 D# p3 P2 @3 c irstream for the stall warning system." ~9 h3 H& D. _3 [6 s3 w another. & O1 F: x# _: b% uLTERNATE , An additional airport selected during0 T. f* m2 C5 s( E: h( L8 @! @/ ~& C6 r: R3 _合金,$ T& E7 y: z5 V" a' O% [7 D- m 在金属中加人少量其他金属,而改变其性质的一种金属& \' g4 f' j% a0 e 合物。 6 O" v* A: A" m0 y# R; D$ s2 S [飞机的最小速度。, y/ V O1 w! S 速警告系统传输飞机对 ) K z, q9 M1 x; n! Z. c流的相对角度。1 C4 [7 |" V; ^ 由一个状况改换到另一个。 9 C* D/ ]; f( ]$ K+ W4 N7 u降场,+ g+ `' ~, p9 T& O 划时,除了目标机场之外,所选的另一个机* c. f/ q/ p7 v* R% [* b/ K o0 f$ y3 ^. Y" a% W' r m! _0 b- t5 Z, _; O6 P# { ALPHA SPEED,0 m* F9 J0 ~/ \+ i5 R ALPHA VANE, A small moveable airfoil on the sid& i6 K5 o) V: x q( x, o% X the fuselage transm T+ J; x6 D% _# U" j* T. ~+ _8 t/ l( W: F a + u, q3 M: v- F# ^1 JALTERNATE, To change from one condition to/ S# G3 \, o/ h+ z6 r' L! z( g A $ L* F4 X, f2 R5 yflight planning, usually near the destination airport, to be ! D: t) `5 X6 x/ ?& b9 vused when it is desirable to divert from the original U0 ]( h, l) j( a2 ldestination airport.9 N0 u0 P+ {. p/ x" ^% D 空速游标' U Z: P( Q! b, F( g& L' x 空速表上的可调指标。 + S+ C# L* E; e8 V6 b2 d' q; f4 y+ d7 O. @- p 迎角速度, m2 M5 _. p. M3 F迎角叶片, 3 W; x3 ] v8 p! l; V' Z& K位于机身侧的可动小翼面。为失+ X+ ^8 j8 d5 `1 D( }: ^6 P9 \% [+ S 交替,+ X, ^$ W ]: s3 O. @8 r4 D. u7 r. f( O$ m, r8 W( A7 P; v* i+ s 制订飞行计 # @+ U, [9 H) {& ^% v O, |/ i% X& I场。通常在目标机场附近,以备不去目标机场时,改降之! s; W- I" C: {! I# ^ D! ~) T 用。 * ~9 n! l6 V# D. r英汉对照民用航空词典B OEING : R) r2 K% d; ^5 Y$ [' W! Q$ T3 DTECHNICAL DICTIONARY 89 f8 g( ?. s0 @( \9 j: J ALTERNATE AERODROME, An aerodrome to which ' ?: W5 O7 F& f0 {6 l7 y/ kan aircraft may proceed when it becomes either8 m8 a( u; l; K% ]& U7 b possible or inadvisable to proceed to or land at the p4 d" {# E4 N0 w0 c3 d. k$ I erodrome of intended landing.. Y R5 |+ Q- {: a L T, E6 j TER SETTING, The adjustment of the altimeter ! \1 ^5 F5 I) ~, u" Iaccount for local variations in atmospheric pressure./ p9 h& Y$ Y7 C* ^& Q LTITUDE ACQUIRE, A digital flight control system+ o" v. }$ f. A5 e+ w" x7 N+ B ode to transition from climb (or descend) to level flight.' i( Q- |# E) r! {% ~ LTITUDE ALERT, A flight deck alert occuring when the% |$ K% `- x: x& x irplane approaches or departs a selected altitude.) U; ]% z" |' P0 Z LTITUDE CAPABILITY, The maximum altitude at2 D0 g; L, r$ ]) T hich the airplane can be flown at for a given thrust,9 w) T: A" A" ~! Q7 L( r; a peed and atmosphere condition. $ Q9 a& e+ G$ _9 G& V# ZLTITUDE HOLD (ALT HOLD), A mode of the autopilot / ~& M4 F$ s! j: \* ^% fr flight director to maintain a selected altitude.! S' N* b) e: T+ W7 B: s irplane's altitude during VNAV operation. 0 j: r, x8 m/ M, X: i7 P& U# K机场着陆时,可作着陆使用的 + J0 e; v9 L( z( g# e1 v; H8 l场。 ; Z0 s- `- W0 l" U- {1 Q$ [- w( S( r0 f* C根据当地大气压力变化而对高度表所做的调整。 8 L' N+ N1 l7 u+ H. X一种数字式飞行操纵系统,从爬升(或下降)改平的模 ! Q" U# [ g3 E) W# A, n9 P( v3 [- K( x' { s度警告, % G3 [, J7 {% J8 C2 Z当飞机接近或偏离选定高度时,所出现的驾驶舱警告。 7 _% g0 f# ]/ T# L. s/ b- T高度能力, % O) a6 x! v* L& ~ P9 v在给定的推力,速度和大气状况下,飞机能飞达的最大4 o9 [9 T& B/ M$ d0 | 高度。 * w+ e1 W. z [# H! Y高度保持(ALT HOLD), 0 v0 n. R# f( N! b- h自动驾驶仪或飞行指引仪保持在选定高度的一种方式。 0 w7 m; Z: r' j4 T2 C h& B: J, V: A, w+ L! b3 G$ M 员对飞行高度的控制。 ! Y4 Z8 f1 h% O" p4 ~! I* z/ Kim # K# @: p/ R+ q' m( d' }" oa * B) j0 s4 a- e, ~7 F8 FALTIME ! s* \ P0 Q6 Z: @+ B( ~+ Kto# Y7 k4 ]& E& d1 H0 H A9 w2 X1 h" Z& N& q) H& M& K m5 G4 b$ }+ j: V' M) P A 3 P' p% Y$ j8 M' E; u" F" T! Da , Y6 R4 w6 G: a' MA0 e8 Y3 o$ e+ r; _7 d* S7 {. _ w8 P# Z+ p& ]2 M4 E s3 x+ o4 |6 u2 t$ L+ x! p( f- K A 2 g# Z% i. `6 N1 p# L' xo 4 }; Q4 k W7 @5 I: JALTITUDE INTERVENTION, Pilot control of the1 I' e$ f* g) g a * F7 Q4 P0 D& [+ _( uAMBIENT, The surrounding atmosphere. 6 E: x5 H) \/ n" K2 c6 @备用机场,6 {, ]/ y8 E0 J U5 @: ^1 s 当不可能或不适宜在预选 3 C. D1 ^# q ~& J% s; }: X( _. I2 U" B2 e% n8 b 高度表设定 # \! \+ \7 k0 x8 K# `% t高度截获, ; R$ V" S& F+ ^% C& F: w( C* _2 S$ w9 e6 d( e; x4 y6 h, O" z( f( H高度干预& d q% d% Q! y8 [# n 在垂直导航工作过程中,飞行4 p5 s. M4 F- N! x 周围环境(地面气层),: @- ~7 g5 J; U 物体周围的环境(特别指大气)。7 N6 U+ c. ]. b1 [' I! ~3 F 英汉对照民用航空词典B OEING * w5 @+ L/ Y1 O0 F9 \' G0 [1 ]* KTECHNICAL DICTIONARY 9" _* N8 v, ^5 M2 \7 ~) e AMBIENT PRESSURE, Pressure of air surrounding an& A/ X2 g+ s' k object, measured in pounds per square inch (psi) .. D8 N# A( @$ Z3 l# S7 y7 l MBIENT TEMPERATURE, Temperature of air" m$ U" s/ A3 `- E2 c mpere.& f, K4 z# I! ]5 |! y9 a urrent waveform.! \1 t+ b! q. l. o g an0 u |. `# c' c* P# ~2 [) N nalog signal to a digital signal. , y. C% |% h: u! k ^+ ?, ?ore inputs [9 M" D5 S2 V2 \: Af binary digital information and one output. The output! p! j+ Q" a6 i' y3 S 1 only when all of the inputs are 1. The output is 0# O) |; L( y* D# Y8 U' | hen any one or more inputs are 0.& |- `* G/ y" \$ Y6 Y! [ 面气压), % d* q6 g9 `# E7 d {7 i1 s' Z' ]境温度, $ h) B% X5 C& N' ], Z气温度,用摄氏度(°C)或华氏(°F)来 ; ?' ~) `* z. X+ e% O( `3 p, @( u4 k; h5 `. j4 D- w. ~6 U 电压或电流波形的幅度。 & A0 j& o. z7 q0 G性变化的信号来工作,或产生连续性变化的信号8 V. w# `+ l- R4 s1 R 统。 * V+ u! e+ w2 v7 a; ~9 D将模拟式信号,转换成数值式。 . l2 y7 x6 o& x一种有两个或两个以上的二进位数字信息输人,一个输 7 H% _9 D# x: a7 o的装置或电路。当所有输人为1,输出为1。当任何一个9 d" ^5 O' X0 l% S8 q) q B- r! W 一个以上的输人为0时,输出为0。 0 D* F- t! F; S2 G9 LA4 V/ w. l* u u. B) T8 ^4 @ surrounding an object, measured in degrees Celsius+ ?! t# i) g& F% V6 a3 x (°C)or degrees Fahrenheit (°F). ( x3 M1 @0 J% B, m$ B1 pAMPERE, A unit of electrical current. One volt across7 T" q2 \0 W( p+ a1 o% k one ohm of resistance causes current flow of one; a, d' [5 v+ @8 F, s, b J& ? a ! w& b/ H/ k* F$ ~3 {AMPLITUDE, The size or magnitude of a voltage or, x% Y1 ~9 |9 M6 E8 G3 Y c9 H. X9 G4 ]4 j5 V; `4 n: v7 n ANALOG, Quantities or representations that are8 ^1 l; a, H4 M7 s$ V& i6 a variable over a continuous range.( ^: B7 X& f+ [/ W ANALOG-TO-DIGITAL, The process of convertin6 W! z2 O% N r% U, j$ O: i+ y' B a 1 @- Q1 A$ C- X* bAND GATE, A device or circuit with two or m 3 W$ b1 n. Y- Y9 \* {o$ `5 ~ Q# j* O2 |8 s9 F is $ Z; j- Z7 p/ P$ lw9 J7 [1 s$ T- K1 b 环境压力(地, ?6 x5 D$ j+ X) t+ X7 F8 x$ f$ I 物体周围的空气压力,用每平方英寸多少磅(psi)来 ; C e) y, V& f, k4 n/ `/ J4 D1 ]度量。! r4 r8 O" c/ w3 k L! r1 e4 c P8 J9 j 物体周围的空- g# e6 U) M9 ~- M4 a/ V4 @ 度量。3 P3 j' R0 q; d; ]; `1 c& G 安培, ( I( G1 Z( c9 v$ A/ Q电流的单位。 B0 [3 N& X, w! R$ \1 ?. e1伏电压在1欧姆的电阻上所产生的电流为 ; o- J1 E6 m9 ]4 d/ m3 _8 q* B1安培 : |& Y# V) }& R( a& m* O振幅, * k' ]1 |( A I) {8 y模拟式,# x; D8 s3 n4 E/ P; U 用连续1 r' F9 z/ o: r" J" d- Y/ a* T9 z& m 从模拟式到数字式,4 [" j: n6 ^5 q G/ G 与门, ! `4 ^4 f* M. S( O: i; u( o: u' m% g w9 t8 Z! G, M3 @0 a9 S! F! g+ Q4 b英汉对照民用航空词典B OEING - a& ^/ O4 k3 u% W8 C0 [! qTECHNICAL DICTIONARY 10 & u9 r ^; ? k$ xANEROID, A sealed flexible device containing air at low 6 Z, t% f3 r; X% y- e& u5 Cpressure, which expands or contracts during change of e- H6 ^# k) g0 {ressure outside the device. , j, ?, y0 {: x/ H! @) Sically 7 k$ r- w8 v8 k; @r changing the direction 7 b' T+ N; C9 G& ?, T q: Xf drive. ) }: S& A* |( I. u# M6 ^8 Cof the wing chord in : E5 Q: V# F/ `: ?8 r0 X: xlation to the free stream airflow as it moves forward7 t+ d. L1 Q3 O% @2 V2 f rough the air." G9 \4 o( m1 R al axis of the . d' z' {8 g2 gaircraft.2 z" W( j% o8 q9 ^, I 胀或收缩。% F; [2 Y. o* s e3 I+ a: U6 t1 k 箱。是改变驱动方向的机械装置。 8 K* T: K3 V3 X: j- I7 Z3 {7 W5 k机翼翼弦在空气中向前运动时与自由气流之间的夹角。! P* g5 Z* r/ r. n/ M1 Z9 ~8 O* ^1 A0 j1 k p 3 J8 v& H c' n- DANGLE GEARBOX, A part of an engine, mechan + V" j$ p4 f4 ~0 G: udriven by the compressor, which drives the accessory" h. U* U( I2 A# A% E gearbox. A mechanical device fo- |5 d6 m4 |1 ?8 i2 @2 ? o. N! [0 ]+ P4 U" @- l0 W E, g0 S" E3 w ANGLE OF ATTACK, The angle , B' T+ |6 q: y/ Tre 3 o! ~- T3 l& c2 X4 {6 V+ ]th, x, Z$ [6 `5 {0 ]/ h s! b$ G ANGLE OF INCIDENCE, The acute angle which the, b+ e0 ~) e8 w' O, P) O wing chord makes with the longitudin0 I: f: O ^; ]7 c1 x; u 膜盒, # J( n( c2 h0 d内含低压空气的密封弹性装置。当它周围的压力变化" h' N2 i0 j j7 @+ M0 n! R3 L* ~ 时,会膨, f( y! H1 X+ k0 Z9 ^0 O' Q 伞齿轮箱,- e* X- d: Y. w5 G, j" ^# [ 发动机的一部分。被压气机以机械方式驱动,然后驱动% l; A; z* k* @ 附件齿轮 8 i7 m+ X4 f9 H" I0 M迎角,, k6 O6 n8 j& o* V/ ? 安装角, ! e! I0 x" s( {飞机的纵轴与机翼弦线所形成的锐角 ! Y# b: u1 t# `! G英汉对照民用航空词典B OEING 2 C! u) m# k8 ~TECHNICAL DICTIONARY 11& O& E! Y' j7 d5 \" d1 k U7 Q ANNUNCIATIONS, Audio or visual indications used to : t4 S& Y9 C- m9 D) jcall attention to an event that has taken place.. |1 T4 p+ d0 t, x. f& t ANNUNCIATOR, A visual device consisting of a number 6 i x6 D8 ]3 q, l5 qly. / ?7 ?( p8 v- k3 LANODE, The element toward which the principal stream * i/ i8 d' Q: u8 jof electrons flows.0 ?$ q5 N" f6 B) S7 Z ANOMALY, Not normal.- B) o2 a* f3 T/ Q! O ANTENNA, A device which, used in conjunction with a& j. p5 P& H1 Q6 W. W- W% ^; |. o transmitter or receiver, is used for radiating or receiving& x- Z4 @8 C0 b2 l$ {- w radio waves.. x8 T' R$ p# | NTI-ICING, A method of preventing ice formation on # y8 {7 t6 p8 ]& }0 m! [e wing leading edges and engine nacelles.; W8 L$ l0 k9 Q6 f5 D, C# s! @2 i2 T' W NTI-SKID, A system for providing maximum braking 2 Y" B2 M) U- z. @6 Jithout skidding for any runway condition. Anti-skid0 p& ^) H* T+ r; X& u# r5 S" b0 R% h omponents are part of the brake system. " O+ l3 K6 @' V" ^5 {+ d/ ]1 b! ^告, # o' w; r6 x5 d d! Q! s当发生事件时,以声音或目视指示形成的提示信号。 ' A6 q5 g8 ]- F6 b" H与之有关的电路的现有情况或已存在的 * O! h$ t4 V+ m3 C$ \8 ?' o! f' V' J4 l0 J1 C正极,( q5 [- D. E5 f- N 主电子流向的极位。+ U! `$ n' M1 a, q) ~0 @ 异常, P! C' F+ ?" O7 b0 Q不正常。/ X1 ~" c, f d- W. c9 {- C7 G 天线, / C6 m0 Z8 {) ~/ j一种与发射机或接收机共同工作来发射或接收无线电 9 ?) L W w) l9 g, L波的装置。 $ X$ |( _, q. P( B% o' @冰, , _7 a$ q* p5 l4 I* x" S+ L& b! k防滑系统,; S( R+ [, B+ w% [9 t 一种在任何跑道状况下,都能提供最大的刹车能力而不 / i) B$ d$ S V/ u! ~# l2 r使轮胎打滑的系统。防滑部件是刹车系统的一部分。; c8 ]: l% ?% ~! a5 @! I' t of lights. Each light indicates the condition which exists% z3 M( X0 s. E/ I& X( n- m or has existed in an associated circuit and is labeled- h% i6 ?+ n" |1 ^! u$ r! }! \- U' S6 [ according ' F' |! L' [3 R" [* M! IA 9 o+ H2 ^3 P- H9 W0 x, P) Uth: o. f( C, X; O9 S A : ?# S3 f5 K I& f! `/ _1 uw 9 Q! N0 E, i# e4 d; k% |c . Z _. W3 o+ M# F% w" n$ f f* W/ A5 L) U( w4 T 信号牌, 2 C# A& \8 b( `7 f) R由一系列指示灯组成的目视装置。每个指示灯都有相应* ?% [# \$ e7 O5 p2 f; J 的标记,用来显示* T6 A9 ?" Y! r4 P! i; ~% l$ g( Y/ F) a# A, t9 P0 w防止机翼前沿和发动机短舱结冰的一种方法。 [4 v+ d3 P& p/ g5 ?$ m& u7 P英汉对照民用航空词典B OEING % {1 n3 S9 f: i& l0 A% [* vTECHNICAL DICTIONARY 12 0 _' f( ?4 J" w+ `$ ]) h# T" sAPPENDIX, A supplement to the Airplane Flight Manual . w3 t `- l9 h5 I* Jtained in the basic manual. A ! {* X6 W: }* n' U. t1 z D5 }ollection of supplementary material at the end of a & F; x4 }/ M# zook. 5 c& [$ I0 u! @; d2 r# n7 aof the- A, ]0 J( ?; q) Z; k n4 [+ a rsion link on the landing gear. " H6 _) F- i. b* O7 w) zAPPROACH MODE, An autopilot/flight director mode# L9 G: S$ ~3 X which is a combination of localizer for roll control and # o, E$ \9 h7 s+ s6 H& gglide slope for pitch control. This mode is used when full & |, _6 L) G4 w0 s6 D, binstrument landing system is available. 7 S6 M* y" @ L5 L! ^1 pAPU, SEE - AUXILIARY POWER UNIT. l2 J/ S+ u& J3 W5 r/ d ARINC, SEE - AERONAUTICAL RADIO ! z) W: Q8 p/ B1 @' tINCORPORATED $ l B* T- w* D% [ARM, To make ready for operation. # p$ z2 r% B' c: ~8 l+ h4 [附录, & X6 e5 @7 [. x! M# ?6 {飞机飞行手册的附件,包含基本手册中未提到的飞机形 5 ?( q6 _* P% E' c; M4 E* b( M3 s态的其他性能。是附在手册末的补充材料。& _" X5 \* I$ ~5 ]: c5 S/ ~$ j! l 顶销, ( C+ k0 O' p' z8 ?/ h用于连接起落架扭力臂两部份的销子。" u. u* f4 R! A6 o! ?+ c( Z2 W* L 进近方式, + g3 C1 R7 U) n0 L一种综合了控制横侧的航道信号和控制俯仰下滑信号- ?1 ?1 l: J; z9 t) d 的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系( F9 W v" X! a8 {+ ^# a 统正常时才使用。 * b2 U8 b" h& r$ l6 j辅助动力装置,3 d3 Q& ~' R" \0 F6 I' g7 j; k3 E' U 见Auxiliary Power Unit$ q6 m( i$ q7 I R: [; a/ n U/ N containing additional performance for aircraft$ Q& Q" Y. `1 Z$ [& X" S* x configurations not con; V4 O8 P |7 w. S* u: S2 f c 7 Z8 b- G5 l, T# n6 n/ k' jb - n6 d% k& z- x5 c: F; A' ^APEX PIN, A pin for joining the two sections; a; K# H% F2 h$ P; a7 g to# ]$ e* \/ Z z- B7 O: o' B6 |8 J8 E; S/ A% ?4 n9 ~3 k2 M 航空无线电公司, ( O. v) `. t* M, P! E0 f B见Aeronautical Radio Incorporated. e0 i3 J; y1 \1 \! D& ` 预位,# J; v1 `% v8 ]9 F1 Q, I1 E' L 部件可以开始工作的状态。 5 d" l) @8 Y( E w: M0 [英汉对照民用航空词典B OEING 6 F( W9 O5 j" P1 j. {: a |% f# eTECHNICAL DICTIONARY 138 a5 m' g( N/ v/ s' ~; M ARC, The curved track over the ground of an aircraft8 g+ z z' X1 _: ] flying at a constant distance from a measuring& z- I, |- x C N( |( y a8 m equipment (DME).3 m: t2 t7 _2 J2 C. I9 F2 H in the limits of self-contained system 6 w: R0 a8 x; [; W4 \# capability. % C4 R" A2 o' y" ]7 ~" X$ P1 ctem for opposing or restricting 9 b& ]/ F0 y. v+ ^! D4 G$ Sovement. & F, e+ Y; h7 _. R& tSPIRATED TAT PROBE, A sensor that measures total 0 d1 j+ K' L* n& \9 o$ @8 Pir temperature when the airplane is in the air and that$ H: |/ K3 S2 d3 @" I+ L8 T* b easures outside air temperature when the airplane is 2 j" Y) n# r: _ u. }n the ground. The outside air temperature is measured0 n1 P( b4 X% n5 {: \3 L SSEMBLY, The fitting together of a complete structure) C* h: f9 ?& d9 ^2 u SSUMED TEMPERATURE REDUCED THRUST, The O. z) G d: h0 j3 j8 a, w) B ATC, SEE - AIR TRAFFIC CONTROL - l7 D3 E$ w3 n) A+ ]) W% V) }- p7 b' D- }* F; V 系统中所产生的一种用以抗拒$ G+ R/ o, r6 p+ L8 ^& l' f: q 作或限制动作的力。' L F' x: Q( c7 g" ^5 `$ q+ B$ d 头, ; r$ `9 {" ?; _: J+ L用来测量飞机在空中时的总大气温度和在地面时的外: ~; c2 I% Z/ z- H2 g6 J 温度。地面外界温度的测量是利用引气将外界空气吸入 6 a1 S8 p) ?2 g+ T, }9 ?头,以达到测量的目的。 # I, O1 D0 g5 s配,+ E5 Q; g& P1 j- b* m9 h2 r 一个完整的结构或组件的过程。! ]% J! T3 R) M1 Z; n4 B 假设温度而得的减推力,$ G C& J2 _* Q, g8 l. {8 i) Q' J 推力设定值时,假定一个比实际外界空气温6 n- v+ m' ^8 l6 L 空中交通管制," W8 u) S$ E1 q" ]/ v 见Air Traffic Control7 i! b4 }( c! d AREA NAVIGATION/RNAV, A method of navigation2 u3 x: Q' O- ]2 o# m! B: ?, R! Z that permits aircraft operations on any desired course, M% }4 z3 G% ]" R( G1 n4 g4 l1 b within the coverage of station-referenced navigation ' U& U) p5 Y/ O3 w% n# g1 `( A K1 Dsignals or with $ r% M3 w9 K$ J( sc, ~* T$ V; s# f% r ARTIFICIAL FEEL, A force developed in the flight0 f% P1 M7 ^/ |9 m9 B3 S8 M control or brake sys! \+ P* T$ y+ {8 t G& S$ K: I# [ m4 ?* z5 X3 a- T Q9 }; M$ ` A , f, }/ s8 W+ z1 pa* E4 G$ q q4 H5 w: L m 0 w& [7 S- q5 a, m8 J: a& H3 G {o" G }$ ~0 y! ]$ n8 j: L( { by using bleed air to draw ambient air through the 8 S+ N& {6 w/ D7 osensor when the airplane is not moving. " ?+ N' {/ I: U5 ~; P4 [0 RA 5 u' T) u& U) x5 `* Qor unit.3 c( E/ r# X8 w% G/ V% p( I A. D% K9 \$ M3 E' W% H lower thrust obtained by setting a higher than actual b) d w0 D4 I# b5 ^ Outside Air Temperature (OAT). " ^$ ~! a' q$ Y弧线, ( N0 P# @( ]/ a7 x+ Z% v飞机在围绕DME台等距飞行时的弧形航迹。 8 q% G" w, l9 t区域导航,; ^6 Y2 X) v, ] z. D8 b" G8 b 容许飞机飞行在有电台参考的导航信号或自备系统能 ) S m) G4 ~( Y; z9 k! W$ W力极限范围内,飞行任何预定航线的一种导航方法。 8 }7 S! L% P Z模拟感觉 ! h& T( [* S" h: K& x在飞行操纵系统或刹车2 U/ N2 r; z* v) n9 l5 F9 e* N# A" Q- p3 U$ p7 J 吸气式总温探 8 \# s7 F$ V/ t5 t6 q- k: v; ]! {- p4 C2 S& z/ {8 O$ o" D$ P" O. E7 Y4 E2 f/ O) s+ m+ m 组合成9 S! d1 t5 c4 }5 _3 t7 I6 I* J$ k' b$ E2 j在选择起飞 8 {0 v4 T1 f6 c- T2 @度高的温度而得到的推力。用这种方法可以减少发动机的 ) ]2 g z6 ]/ p7 n7 p6 v; W5 |2 `磨损和维护费用。6 {) l1 y& P$ d8 i) j Y/ t. m p3 ^) W 英汉对照民用航空词典B OEING! H! r- _* L' N+ q# V) Z: e4 @ TECHNICAL DICTIONARY 143 K6 {2 c O6 j# e8 m8 ` ATE, SEE - AUTOMATIC TEST EQUIPMENT H: I6 R; Q* u$ N ATMOSPHERIC PRESSURE, Pressure of air due to the9 F# {* o0 S4 {. _& ?+ p% U, k1 y arth's atmosphere, expressed in pounds per square 9 K" F1 v) c' \$ f4 ych (psi) or inches of mercury (in Hg) or millibars (mB). : B8 C7 n1 K5 H, A# o5 ~" G* E) YTTITUDE, The relative orientation of the airplane with , s$ \; [" ^9 f: c. m- jspect to pitch, roll, and yaw.3 R- f2 {. j% F( x( e2 j8 ]# e( R UDIO CONTROUSELECTOR PANEL, The panel in, n2 u z9 v) B; T( g) S e airplane which controls and selects the routing of + z8 q6 H/ n) u7 L6 r' y( Vudio.5 L( g1 e" T0 {/ f, t, g UTOLAND, Automatic landing using the Digital Flight! W' l0 f" Q S' P2 A ontrol System. : e$ J( m2 i% _2 P- P/ \n.3 V) U) ?$ A2 f+ H M, A system! C `0 Y" z% p- ~: q omposed of all necessary subsystems needed to guide+ G1 n' s6 T+ _7 m$ ~- x) w s | e flight of an airplane.3 Q0 y% i; |0 F9 v EQUIPMENT, System test ) Z/ w& c* u9 y3 I$ ~quipment that operates under computer control.4 P: j5 ? ?% m9 ?6 X# E! g 装置,

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e ( G6 }1 ?) m* l0 P# j9 w9 Win 9 @, t, M2 Y* L/ L( c7 i3 N9 wA9 d7 ~) d: y* A% ~, k re 1 m, u$ l7 |/ D( D3 f# @A 8 _8 x+ ?8 E5 Y, Z. B/ Nth 4 n1 F" \8 W9 J6 u l: g0 h' ba3 X) F# Y) R* D' z A % T2 i" Q" O1 @$ Q2 vC / Z* y+ X' g: F: vAUTOMATIC DIRECTION FINDER, A system which# V5 \3 {" O& O1 o/ }3 k determines the direction of a radio statio/ [1 `$ @7 A2 }, O0 O AUTOMATIC FLIGHT CONTROL SYSTE 9 g, s [2 r8 d! _1 Pc 2 l S3 O, L3 u+ Gth( ?8 _- L& N4 K* q2 V" z AUTOMATIC TEST ; z9 ]+ l7 O3 B+ v' L8 T( Be! C' z6 T. [, Q: [ 自动测试& l7 ?% X$ P' F+ j 见Automatic Test Equipment. , z0 x2 H' L! W' Z4 r大气压力,% A5 S& G. x0 ]+ b& ` 由于地球周围的大气而产生的空气压力,以每平方寸多 ' y3 A/ Y' j% H- y/ i4 p& X磅(psi)或多少寸高水银柱(in Hg)或毫巴(mB)来- d! O9 K5 G8 q# P* }5 u 示。( f, L$ U4 Q0 |4 L# i 飞机姿态," h) Y& t% g5 o" Y, Z0 v 飞机与俯仰,坡度,和偏航有关的相对方向。 & R5 w' U- x6 }, y* \# z! G音频选择面板, % } V+ z8 M# j飞机内用来控制和选择音频通路的面板。 / E8 G, y) T- o5 {8 g自动着陆,3 u4 Q$ h& Z8 r# R' J( y 使用数字式飞行操作系统来进行自动着陆。4 n) s( Q4 ]6 j- F! {; }1 y7 D" a- D 的系统。 6 c1 k) `4 f+ z5 d. O! f; [) t X6 [! b" ` 系统所组成的一个系统。 ) } G7 K2 S( x# R) O在计算机控制下运作的系统测试装置。 : m4 Z# C0 @" t7 G) u V) D- d3 q8 M5 H% g6 I4 Q! h! n( f% A# [; R4 U自动定向仪(ADF),, Z, `+ p9 @" y5 ^ 确定无线电台方向4 n3 I2 C/ h/ \, K: n 自动飞行控制系统& t/ C* e4 ?: F! O 由所有能引导飞机飞行的子% V2 P6 E. E/ i' j3 o 自动测试装置, 2 t5 B+ x h4 x) |. R2 C英汉对照民用航空词典B OEING9 r& x7 T- ~' o& a; l- Q TECHNICAL DICTIONARY 154 A2 m: ^1 J: h/ { AUTOPILOT, A system which automatically controls 0 E3 y, I6 `" k7 ? ]+ |# @and guides the flight of an airplane." \4 E1 C B4 c AUTOPILOT FLIGHT DIRECTOR SYSTEM, An - l' G- m0 |7 w; ?; jtor5 j( c( y& i# O- D, ]7 ]% a UTOTHROTTLE, A system which automatically' Q5 M' D) X9 d& r ontrols the throttles of an airplane. $ s, v" I. Z# g3 r7 IPOWER UNIT, A small turbine engine in : s* j. m9 W! qe airplane for supplying electrical and pneumatic ; u. Z3 n$ v$ nower for systems operation on the ground or in flight. 1 ?" Q% N0 m6 ]2 s& O& _VM, SEE - AIRBORNE VIBRATION MONITOR& e. a* [9 [' g" S6 [4 x XIAL FLOW COMPRESSOR, A type of compressor& ^% B# _& v# I" _ sed in a gas turbine engine in which air passes through ) m. W' o! W- K8 X' PXIS, An imaginary straight line or an actual physical# N% u: ]' o9 ` X! { omponent (such as an axle) around which a body can * l1 y+ w- e) f6 a1 G1 |8 ]2 Atate.5 w2 J3 H$ x) d* L 仪,9 B3 e$ _ O5 J [/ K1 G2 }. T( b! H- x 自动驾驶飞行指引系统,4 M- B2 e8 O, q3 ]3 D$ c 动驾驶和飞行指引功能的系统。 . d/ [8 x& i) m& ?+ C- e* [动油门, 0 K( k1 l' f8 _+ \. P7 w自动控制飞机油门的系统。7 g: e# o; H. y V' t 是飞机内的小涡轮发动机,在地面或空中给各系统提供 / ^/ e, d! ^& M+ J% z, O( W* {* A% {源和气源。; W8 L5 c4 k; h) u5 N 称。 ! R/ ~) n8 N0 X) Q5 f$ H3 u" L* e载振动监视器,& X2 v' W0 {8 o5 ^ 见Airborne Vibration Monitor 2 N* ?2 \6 y0 }+ m+ I5 Qintegrated system containing autopilot and flight direc 4 n7 Z* {6 j9 M1 B S+ q B, Kfunctions.3 f+ C1 i# b: u( | |3 b A : x5 R5 r5 s6 m; fc ( }' t/ o8 I9 E7 b8 V- RAUXILIARY8 A y+ o7 O9 R4 b) r C th $ Y4 w9 ^& Q }& kp 8 k. P" u8 a/ _: s; A6 l. z8 p% |AVIONICS, An acronym designating the field of aviation |* |" a# w J; v8 s8 p electronics.3 c( J: Q4 p7 c A : u4 @: `" \- o" r: QA) p% j v! k5 t# X# F/ Y2 o# e u & ~- O' [; o% f w" p: Sthe compressor in a straight flow, front to rear./ ^7 T6 E8 `7 b) F- H: p A # |3 @) X( c2 ]8 C' Ic # q8 L& a# M" T. X: D; Tro $ |* L. @6 J" V自动驾驶 $ v: e: f. ~: N3 o+ c动操纵和引导飞机飞行的系统。 - n' s5 C: |7 J3 I1 |一个综合自6 N: G3 a/ M, @9 @2 p7 {% q4 Y! H5 _( d% \" y( ]) h7 @ 辅助动力装置,, U1 ~: V2 B* D2 ?+ {, c/ r x; [) a8 t- m 航空电子学, : W3 Q0 _# s2 c是航空电子领域的一特有名: y9 V- V% v/ [5 ?$ o, U' p. E( P" L h; W# y7 k! y7 [; c# ^$ J/ F, b 流压缩机,$ R( q8 _- \- k: J 一种用于燃气涡轮发动机内的压气机。空气由发动机的! v- C5 ], j8 q) `% t 部流出。4 ]5 Q: o/ R, D# p$ X- r: f1 A! c3 s 线, & A) L7 |: r; v* m% J, A2 o可让物体围绕着作旋转运动的一个想像的直线或实际/ o+ T' Q* D, f: [ N 在的部件(如轴)。6 j9 S+ ^' x S; Y ~$ ~4 ] {* [8 ]4 N' J2 m o前部轴向流人,压缩后,由后 ) k; T5 D& m, {& m7 [8 I9 ~, X1 o4 k1 i1 U0 F6 x) t/ }6 ~. X# C$ i$ \! M# N [4 O8 D3 X英汉对照民用航空词典B OEING % @4 C$ A0 a# rTECHNICAL DICTIONARY 16 ; P5 `$ l1 @; {+ D5 gB - U, C% O# ?7 A1 R7 DACKCOURSE APPROACH, An approach to a runway " {4 q0 J2 Q( s3 u1 s& |' B3 tversed. $ O$ O; B9 v& {; [) O" H- _own on the EFIS that1 h2 ?- c2 R; m- c' F oes not readily change, for example, navigational aids.+ P5 O4 j1 c4 Q8 ]" {1 u vement in the tank or reservoir.) w \; M7 V5 R4 Q$ T0 @% n5 O8 _ ALANCE TAB, A small hinged moveable part on the5 q) H7 \3 n7 f ailing edge of a control surface (aileron, elevator,0 G2 W3 q# m7 s2 h6 @; A% d 航道进近, ! I {4 ?# @* ~; P' O相反的进近方向。当反航道进近时,无下滑1 O/ X3 i4 c3 p9 M 显示在电子飞行仪表系统上不经常改变的数据。例如:9 k W( d& N# y% t1 p3 i+ ?0 B& N 航设备。9 W9 F; Z( C5 {: R. i 在燃油箱或滑油箱内阻止液体流动的隔板。 5 E- b8 x. e$ E$ |0 `, h动补偿片, 3 x1 e$ k1 k' g5 M% |5 V% s0 O铰接在操纵面后缘(副翼,方向舵,升降舵)的可动部。9 x- b O+ C9 K* {! Q/ Q( a _ 与操纵面相反,以帮助操纵面运 9 j7 O* A1 X, A9 A( s" M% c8 Y& iB 4 p( ^& P& X3 K8 }5 Owhich is opposite the normal approach. For a& [7 V) g* \# Y* P backcourse approach, glide slope signals are not6 i6 {/ e- N$ q6 P6 U8 c available and the sense of localizer signals must be 4 Y! E/ K% w- d% Ure! u9 F( ]& T6 ? BACKGROUND DATA, Data sh 9 C# {; b3 [) g9 l' Td1 ?7 S4 S1 A3 g/ T+ A BAFFLE, A partition in a tank or reservoir to prevent & e2 F0 E) X: S Xfluid mo$ ^( T+ A& |, v2 ^2 ^# L4 i B # P1 C1 D0 k% ~7 u5 ctr 6 L$ N# N) U1 q- M7 Frudder).The tab moves in an opposite direction to the) o; F! {/ ~' x7 ?" P- \ d- B0 w control surface for assisting movement of the control & B" ^, E, X% [$ v, C9 nsurface. 9 W4 Q! C1 B2 f3 k+ r& w% m6 e. B: F3 g' Y! S$ W- c% p9 p% E与正常进近2 E7 ? _' K4 K* w& H! ~ 道信号并且航道信号也必须逆反。 5 F0 U, I( e0 k' U背景数据,7 E* [& L( [+ O' c$ Z }1 y# u" Z- G' \/ n( Z+ m( O5 O _ 缓冲隔板," m g7 R) v! X- f9 W& x$ O* B* b' _- p C7 D# Y 随动补偿片的动作方向& }( `: A& h% y8 c4 b C5 w 动,减小操纵力。 X- }4 o5 H. Q英汉对照民用航空词典B OEING 4 R# E9 O j5 a3 HTECHNICAL DICTIONARY 172 ~6 x2 T" B8 n [ BALANCED FIELD LENGTH, The field length4 e& C# x# U; m associated with optimum aircraft performance when * X5 Q6 b. ^% L2 }: H7 {# F' Hbstacles are not a constraint. In this case, after engine$ z$ y, h4 N) X- J: n0 f ilure at V1, the distance required to accelerate, takeoff 1 y! x U! S2 C2 U' h# ]/ E, cnd reach a height of 35 feet is equal to the distance8 W* o/ T- D7 _& E U: K ALLAST, A weight installed in an aircraft to maintain $ X0 ]3 x$ E& u. {ALL NUT, A fixed spherical nut driven by the; O( _0 @' b$ c& t AR OUT OF VIEW, A signal used to remove the flight" q5 q9 a: p0 W8 A1 g* { AROMETRIC PRESSURE, The pressure of air above9 A3 r5 B! A* g$ V0 O g) or4 f9 L% C# l1 N millibars (MB). 0 C$ z0 t3 ^" i8 x8 j: C9 OATTERY, An electrical device for changing stored % D! G$ F# U7 i1 p2 O. ]性能的场长。在此1 V0 v3 {; `% Z, S 况下,V1时发动机故障,要完成加速、起飞、离地35 * N' Z4 [- b% i9 F& X ~9 D尺所需距离等于相同速度下完成全停所需的距离。# ~ ~5 e3 @$ n; f# a! m0 _ 舱物, / H' v' u( M" Z; t) A+ z重心在许可范围内面装载的配重物。 1 T0 t4 ^6 O0 {* @9 A/ U形螺母, " q% W: U* l" l. K* X5 d的固定的球形螺母,用以使襟翼和水平" l0 w' _% p% ] 引杆消失, 4 V; h2 `5 Y0 a5 y& Z/ z! d指引杆的信号。 . |6 k* U% b2 O; D压,, w5 ]: B3 x; V. W3 j 压力。通常以多少寸高水银柱(in 9 ]1 Y; R& W6 u( v瓶,% h$ A% {, n/ x5 A# W/ I! [ 的化学能转变为直流电的电气装置。 ( S. x6 |- k( Y$ {o5 m; \/ U a3 \6 d& d! | fa ) x$ Q% }* D4 z; H; y. \a & d9 B/ ?- Y4 {% \" Z; z8 nrequired to stop from the same speed. ! Q' h, T- M- q" rB % m5 D; |9 R" F8 d, h7 Dthe center of gravity within allowable limits.- y+ J( P0 D p. n+ f h* o B 7 }0 `/ P6 O( i2 {. w4 a/ M; i1 a' Fjackscrew for flap and stabilizer movement.7 O8 s, R8 U V% G, |# x B " x! P" ~; b; A# P( Sdirector command bar(s). 8 f. w# D& ?. G2 D0 L9 K% Z9 D. {B 5 W1 A+ i7 `( ?* u/ Dzero pressure measured in inches of mercury (in H # b& u8 Y9 r' g6 E7 e! Min0 F/ `5 o. m0 r0 |- Y BASE METAL, The underlining metal to which alloying& `- e* ~* S0 \ g s3 } agents or metals are added. . G4 d( F% }6 I3 i' nB0 u! u& ?1 c' A- M5 e$ P! E chemical energy into direct electric current. - h. K8 d: v2 A$ {1 i* I平衡场长,' j) q0 t- p$ t" h& ] 当障碍物非限制因素使飞机达到最佳7 \6 ~2 P% v$ n6 y p, L2 O, n4 p9 b7 A% h. q e i# `6 I0 X0 q# ` G! S* Y/ z3 o为保持飞机. _0 C, u6 b8 x" N/ M/ @" C. U# P ] P4 \6 l! _( d由粗重螺杆驱动 . W1 W/ K0 {; }* l6 N { {安定面运动。 3 Y) U4 m6 _& J% x( a$ P+ n! ~. m1 R+ w3 o- B: d: p 用于除去飞行 F) _6 ?+ ?1 u, D. A1 N( b' T# E- X: O$ h% a& I5 {' `/ e; a. h 零压力以上的空气 5 `* J) O6 t$ A+ }0 f0 JHg)或毫巴(MB)来表示。 R6 y+ S3 A. @0 N3 \# U6 t基底金属, 4 F6 L0 ^) O5 {+ P ^ P1 Z+ e指合金中的主要金属成份。 ; V1 n( j( R( J* n6 Q) Q1 j$ X0 u6 Z9 C. K: P! z 将储蓄' ]2 q, U( K: v0 e7 f 英汉对照民用航空词典B OEING $ U( L/ L5 u$ MTECHNICAL DICTIONARY 18- V3 ? M+ f6 ^2 G BATTER 0 \/ \; ~+ [# T; rdirect cu ( W' {) M* e- U' u: D! T, P# Fpower su1 D7 N; b/ s0 ^) c7 t9 X Y BUS, An electrical conductor supplied with 6 c( H& }/ k) V7 V. n( krrent from the battery or transformer-rectifier for 8 U- a2 g9 ^3 K5 P3 f- e& j5 H! {. ypply to operating components.% ^; ~" W$ V$ H5 m# S' ^2 G CHARGER, An electrical device supplied 6 D' p/ o c9 l! ?9 W" Jith alternating current, which produces a direct current; p" H8 V' l& A+ H4 L; W utput for charging the battery on the airplane.$ ^- F) V8 B9 w7 k8 j4 _+ @4 A AY, A compartment in the airplane structure.: k# Q# L8 \8 h" A& M CD, SEE - BINARY CODED DECIMAL6 e+ s2 G, g% P5 V+ n EACON, A device which emits a signal for use as a: S/ A+ ?2 l: u/ \- v" G/ L uidance or warning aid. 4 S+ O; z9 j! Y3 {0 R7 BBEARING (NO. 2), The direction from an airplane to a$ w% u$ t! X3 n( X ground station.# ?6 {0 u* q) d 瓶汇流条, z& T# {4 b+ E# U 将从电瓶或变压整流器来的直流电供给工作部件的导9 ?& v" @1 w+ A. l4 z9 Y 体。 3 u; Q; ^7 `: a: f. \瓶充电器, + d, Q1 q8 o+ s7 }用交流电向飞机内电瓶充电的电气装置。带有交流电的 3 C9 \3 i; }, w3 `1 c6 W气装置,该装置产生直流电向飞机上的电瓶充电。9 Q9 f1 z" R3 J" r 舱,7 a* J, [3 _5 ]% v; Q 飞机结构中分隔的空间。) Y7 f& K x a! f' _0 _ 二进制编码,, B9 F9 F2 z2 Z9 c6 P' ~/ j* Y 见Binary Coded Decimal 7 J2 | _* i( D* K2 U4 n. Y& R" nBATTERY d8 F- z, {2 w9 D$ C$ Z w & B' ]1 k& x, jo 0 i. V9 s9 T. DB * G! @9 @& h6 a! Z! OB " f; A; X. O4 b5 f+ }2 B+ _1 sB/ E6 c2 \" u y g8 ?1 H6 S) F _ BEARING (NO. 1), A surface that supports a moving 0 j& `1 q( Y/ L( r/ G/ zpart and reduces friction between the two. % _; x4 E0 v0 s6 n# v0 s9 ~* t! P9 Y" L7 d$ [3 Z$ z; L1 }$ n( Z' L. F; i/ Q5 D; Q: k* X" I" U: S2 @: @3 K- f3 m9 y. J7 b( B( h! R. P5 s v$ C3 C+ G/ R" m# _7 @, C$ L信标, ! y5 l3 ^- \+ N$ F2 D发射引导或警告用信号的装置。 3 M2 q- F. z" V' E8 S" T. o方位(NO.2),; f) W4 A5 o% O& T2 i! g 从一架飞机到地面台的方向。7 h. F+ R9 S, A" z 轴承(NO.1), 0 u! y" y1 m5 Z1 c. S$ t# I用于减轻机械转动磨擦的机械装置。 \4 o! Q* P) o( F" O1 q: {英汉对照民用航空词典B OEING4 ]2 P& s5 o9 {. L TECHNICAL DICTIONARY 19 6 }) a* A/ C) X% D; k" sBELLCRANK, A double lever in the control syst* q$ w( D C \. p% K" c2 A changing direction of motion.7 h3 ~, r7 q+ a6 d I$ s em for 7 i2 n9 j7 j0 r7 c8 Mct in the1 e8 Y7 c) V2 F9 A: _ neumatic system for absorbing expansion of duct due + j/ q; j6 c. V* Q9 @heat. - _. z8 e j1 R6 B( j- TELLOWS (NO. 2), Corrugated folded or pleated9 L3 {9 A( w3 ~7 ?0 Q ontainer or compartment used to measure pressure.. P# A4 _8 b& P3 N1 ~) _ EZEL, The part of an instrument case for locking the& I# h w% K! w( ?; w4 C5 j lass.: }& Y3 x& V' p* C: x IAS, The potential difference applied between two8 E0 {1 `3 H' G+ \: j5 h! x% T oints for controlling a circuit. 1 P' P; w9 l+ R1 V( k/ C. dBILGE, The lowest part of an aircraft fuselage. A place ; S1 E/ G- R* s* Wwhere water, dirt and other contaminants collect. ! Z& C! F0 |9 Y) ~气源系统内提供管道热胀冷缩所需要的余地的波状 0 X" ]* u. Q8 V% B轫管。! A5 ~6 \" s9 {# A0 l; o( L 空膜盒, 0 J4 o9 ?6 l# D一种具有波状表面的容器。用于量测气压。& \1 k. d9 W, @, z r& \ 嵌沟缘, 8 A3 T* h5 E* h! c2 j将表面玻璃固定在仪表上的圈状零件。 ! l( M& K2 t* g; C& Q1 p, z压,0 P J8 v6 ~: y- q/ _ 在控制电路的两点之间的电位差。 * {' ]/ j& ~7 B' U( h机身腹部,5 P( C+ e, Q( E4 s$ Z- b/ ^ 机身的最底部,通常水,脏物,和其他外来物集存于此。% K4 e1 T9 O: r$ ~% l BELLOWS (NO. 1), A corrugated flexible du 6 [( q# p: v W1 _& \p7 t3 T) z2 U& D# v( B' U, m ^8 a to 4 ^" V/ O0 a6 M# E" E. rB9 M) }* U' p5 q: C c ( ^" w* d; n% D7 dB6 k* q, O* f( v }! ]7 s9 V: ]0 {5 d" r g- c1 ` S+ Z3 I B ; m' z5 L" n e; x( E$ h$ Qp/ D; y! Q# w9 S* u ^# ? 直角摇臂, ) c; F& j T9 k e在操纵系统中改变运动方向用的双臂摇臂。' H1 _' Z4 \6 t 波纹管, : n; A, U6 T x5 i: `! [4 R& E' I- U. a( m3 [- J2 n) I: N' n& q' ^3 k' Y, ^) ?7 f" E& {0 Y& W+ u" N4 n' O( T/ b# g) ]1 z7 b: ]" z英汉对照民用航空词典B OEING) k3 E7 ]3 g; N4 ^2 ]: [( { TECHNICAL DICTIONARY 20, s: K; j, h$ o# z+ e BINARY CODED DECIMAL, A system of coding each) `' N* J3 Q( q1 F- Z digit in a decimal number using the binary equivalent.+ a+ y5 L9 G+ c. z0 i BINARY NUMBER SYSTEM, A number system using " y: h% z' \+ U. k$ Os0 b! f1 z! z( v( i4 @ IT, In the binary number system, the smallest unit of1 I+ n ?% e( p( Q* o' t& e formation, consisting of a 0 or a 1.+ R5 m# `0 m3 z) }/ u/ g+ [* V ITE, SEE - BUILT-IN TEST EQUIPMENT , d f5 j0 B. R+ x; E* Q5 gLANK DISPLAY, A display that does not have any K" z) H: e% @4 ^! Q dications, normally due to failure. . a; W. E$ A& `; q, ^. _LACK BOX, A container for electronic circuits to record 8 I; ^, b* u5 D8 e, p. b, G- Sight data. & e; J: A7 {- A$ K/ H+ e+ DLEED AIR, Air taken from the engine to power various. E8 ` i. ?9 }% q4 q ircraft accessories.( O! W# l; m) h& s8 U A valve in the pneumatic system for air) i: B$ J0 g" c6 k7 p# q; {+ X. ` supply from the engine or auxiliary power unit to the8 q$ J0 x7 Y% @) F pneumatic manifold. A valve on the engine for reducing & m! _+ v: S" C6 m& h: ipressure in the compressor section. N. {; E! T8 b0 o4 x进制, * G) h" P5 ]6 [% V( M& i/ X: o9 B进制,( b5 z: R) u+ V1 H! a b5 ~: m' J 一般用0和1)和2为底的数字系统。' N9 u; B: H+ e; d. I' C 特(二进位数),5 K( k G4 R$ H8 Q0 ] 二进制中的最小信息单位,包括0或1。, Q K1 ^1 r+ o4 K) V4 g5 V' s6 s 内自测系统, , d8 b: L# h5 B" j. ^4 ]; }6 Y) X见Built-in Test Equipment& h. h! Z" O# p5 _- N/ s two symbols (usually denoted 0 and 1) and having 2 a& q2 e8 [' `( J* T0 k' r) K- f its base. - Y, U9 R \, _B 1 t" P4 F0 o% Z& o+ \0 L& ein, q5 s+ {" v3 ~1 y% h5 K- A B ; a6 z3 D; r C. {* CB6 E' A) |* v% [% v" r' j7 k$ T$ T in; P% O7 |6 p: @5 h# O5 v/ L B 1 S4 P! P0 K" ~# g; c4 ofl7 \9 T5 d7 x4 P! R: [2 P$ `2 H B* |/ w W J. W5 ^! E a9 r D; N. x1 {3 N& d BLEED VALVE, 3 z+ ^; O& c$ ]& X& Y# k) _二进制编码的十( C0 b v' o3 e 一种编码系统。用等效二进制位数编译十进位数的每一 4 B! N* v9 H7 k9 P+ B( |位。) I ~2 R' j- k) U$ N3 d5 G: e! A9 x2 ^# M6 M- T4 K. a% q 以两个符号(5 ]8 f7 s' U& G# f- @, B+ J7 r s9 [+ k$ E$ P% f! V6 S7 W$ {& ?8 D3 ~# d. * |1 b4 W5 s1 ^/ w白显示, " }( I! r! G" H# \% v6 u通常因故障而造成的显示器上没有任何指示。 ( m2 F& n$ x) H$ H# f! Q. m匣子, ) g5 U7 E/ e2 z. K装有用于记录飞行数据的电路系统的容器。# w! G, b4 s5 t* q7 \+ L$ I' M 气,4 x+ e L2 T e" [ 取自发动机而用以驱动飞机上之各种附件的空气。( N2 F* {# r! L4 v 气源系统内,使来自发动机或辅助动力装置的空气进人 # \/ A& P: Q8 P) _7 C气源支管的活门。发动机上,用来降低压气机压力的活门。 F7 w: R+ P( u1 Y4 s, H3 R. t3 x1 k) d1 T" w6 `6 a& v. ?3 K! B; d% {: b" K: q, r, z/ R8 ]1 D3 j3 d引气活门, ; B2 R) b& G0 [6 Y( F5 N# n英汉对照民用航空词典B OEING) h' J$ W+ U* r9 z+ A TECHNICAL DICTIONARY 216 G, o- e7 }* C# G# n+ v BLOCKER DOOR, A device on the engine for blocking 9 y: r) n/ S; o/ c, ~the normal airflow during thrust reverser operation.. g1 R& p' k6 }* e LOWER, An electrically operated fan for circulating air. ( _, I% e0 K) R3 G$ F! u+ xLOWOUT PANEL, A panel in the structure between $ x& y1 g! N) M! p" o Uo compartments that opens to equalize pressure in " e2 `( u) m7 u5 B; G* le compartments. ' m5 j5 X+ ^9 J5 xODY GEAR, The landing gear attached to the 8 m$ Z% L- v9 Y. B, b, E! A% {3 r+ ^grounding. # \0 ?3 r2 R3 }1 o9 c' p1 p5 {0 l正常的0 h& E' O1 S% V 气流。2 }% e2 T) o+ j! n1 ` 鼓风机, 8 s0 s! a$ b' D! l t用来使空气循环的电动风扇。 6 N+ m. V3 U1 o& W压口盖,3 B/ O' t4 F& O5 D 两个隔舱之间的口盖,打开后可使两舱压力相等。( D, k7 b: q1 j4 d 身起落架, : M4 i. P* v2 E( l4 e身构架上的起落架。 2 B5 {9 M$ T" Y& BB% ~% Y p8 X2 e9 ~5 X7 X B! _( e. n! N& E7 e) }1 X tw# m- S0 x. T: {; T: C) k( [* R$ Y th - E8 t. p- q! tB 6 b+ R; B+ i! b3 G/ Wfuselage structure. 3 ~$ ^* v$ K& B. C3 X8 O5 `BONDING JUMPER, An electrical connection between - u1 k8 a* c9 [- S I( Ka component and airplane structure for electrical ) k0 ^7 l( ]1 x7 v" G阻流门,* l% C8 q) J8 g1 K 发动机上的一个装置。在反推工作时用于阻挡 : A% N+ W, N; J1 D/ x- ]; ~/ u( M4 Y8 N$ ^/ {1 ^6 A6 `9 k3 n7 a( P* |( E装在机 % \* K6 H! n( Y) k搭接片,. ~& T- S: \, q3 z 连接某个部件与飞机结构以形成接地的电接头。7 q& y3 C8 L' `, p$ }$ D" _" o 英汉对照民用航空词典B OEING! c1 r2 e1 O! c& v. C/ S TECHNICAL DICTIONARY 22& }) q6 S$ \5 v2 Z+ v- `; r BOOLEAN ALGEBRA, A mathematical system for , b( N" D; b0 K6 [, `writing combinations of logical statements." f# Z' B% }5 ]: \3 N. [ BOOST PUMP, An electrically operated fuel pump for" g9 Y1 [! v; u/ F# v" H7 i fuel supply from the airplane fuel tank to the fuel + q; b& P8 v$ {9 lmanifold.% ^) q2 {& ~* y* e0 e BORESCOPE, An electro-optical device for looking at ' I( J' }- ^( N! J$ n9 f; Iternal parts of an engine through holes in the engine. # G4 H+ w( `4 Q, Q0 }orescope ports)5 _/ R0 o' c& m OURDON TUBE, A curved flat tube in a pressure gage% M# x7 {/ L$ \$ r0 Z# t* O r moving the pointer when pressure changes inside # i$ N4 A5 Q+ m( j/ x b4 Con the ability of the brakes to $ i) H- o" `2 J7 J/ M3 o$ Cbsorb a predetermined amount of energy during a ! |% H/ F8 w& Y( `! ~/ r. gjected takeoff. b) W' k3 X7 M! G 用于通过发动机内的孔(孔探口)观察发动机内部件的, _5 u1 G- J* t* h, A 光设备。6 Z1 j0 p% p% s& n5 F 端管, . D: t$ H4 d1 _, Q( h测压计内的弯曲扁管,管内压力的变化时它使指针移 0 E' a/ {, s3 L/ s" j# S力。 9 n( b" Z+ y/ W H/ d极限重量,% o+ N- b/ K' q. M9 v! o! D" {2 _ D$ k) ~7 q起飞重量。* }1 P# j5 ^( O6 H1 q' |4 j 发动机滑油系统与大气相通的通气口。, u j0 p& J+ [ in R! U) z: {7 }1 F(b+ U R _) i) k% S# \1 t$ v B; d6 g4 _( K q fo1 b$ |# h5 [- \6 v7 n+ H G the tube. + |0 W/ f$ y- R6 kBRACKET, To enclose or surround. ! K" G5 R% w8 o5 ~2 ^! W3 N' B5 GBRAKE ENERGY LIMIT WEIGHT, The maximum 3 O3 t0 _' |5 w1 B, x- t- e7 vtakeoff weight based) W+ v! E1 D; B4 G7 t. Z a6 [$ ^' H q3 r/ k& [ re# O9 [2 x9 L" W" `2 V BREATHER, A vent to ambient of the engine oil system. 9 |; R8 J' } o9 q布尔代数,* R: Q2 s& O# K3 q9 C. N 一种用于编写复合逻辑命题的数学系统。9 X; Q! T) ^, \8 f* G. u 增压泵, 4 m/ h! f; w( B; k- ]从飞机油箱向总油管提供燃油的电动泵。5 x4 M4 o" U3 X8 t/ Y$ }" K 孔探仪, 8 \, E# Y" F. a P5 W8 ]$ j6 E: i |) A- F" z6 l' Z) }7 I 动,以指示压5 i" G: I r+ K5 d; ~. h8 { 托架,1 J( Y" E0 _2 A+ W3 w6 i6 Z 用于作支撑、装托、或围绕之用。; A, `! y* s1 p 刹车能量 ' G$ I& ] R; m中断起飞过程中,取决于刹车吸收预定能量之能力的 ) z: w8 L" @! p3 n9 }0 B- ~: X6 L* D4 T 通气装置, # f+ n- w4 Z% {* k" o英汉对照民用航空词典B OEING 1 k4 Z1 e- Q$ q- J4 o) STECHNICAL DICTIONARY 23# r! v) e" ~5 t/ A BUFFET, Vibration of the wings and airframe resulting . l2 J9 g, x8 L: S9 Sfrom unsteady airflow over the wing; caused when 3 ~/ L( E4 e6 _airspeed is too slow, the bank angle is too steep, or9 K9 I* E& a+ u- m irspeed is too fast. / l; J5 P# I! H X' Z1 ~9 L5 YUILT-IN TEST EQUIPMENT, Equipment installed on ! f; t* W: [# \2 p2 Y5 Xe airplane and in airplane systems to test the systems % R/ ?4 [! U- n. \" v& a' [. ^ithout external test equipment." `3 q# q3 d2 I: \. \+ M( ?6 Z* m3 X# a UFFET MARGIN, The amount of residual maneuver( X m ~& ]/ V3 C2 l; P apability present before the onset of buffet. . l" u9 B/ B5 v9 \! c5 R( JUG SPEED, A preselecteed speed to be observed + c, I- c- t& m) L8 v9 f) a: Hnding sequence." r# B9 T0 o' @8 J9 o k8 v J e: R$ C& F! r ng landing gear operation. ' i! I% d) @! g) h速度太慢或太快,坡度太大,均会引起抖振。 " J' C- C* S' h \自检设备, ' x6 a: s2 A+ E2 f安装在飞机和飞机系统中,在无外接检测设备情况下, 0 W3 j2 Q, }" A$ s' x5 X1 A \% w用于检测系统的设备。 ! |! e% Y# P/ i5 s4 o5 E2 X& {6 h抖振裕度," |8 o( ?" d, K 飞机在遭遇抖振之前,剩余机动能力的大小。9 r7 S2 z* j/ X% B 标速度, + k3 y+ W/ B$ H/ Q2 [在某些机动飞行过程中,特别是在进近和着陆时,飞机1 M: J9 G( m5 W) f) s$ R8 p 预定速度。 " n: m) V; Z A& M" {% V" ?. c) |力装置,! W |( E& ~5 X 架工作的一种机械设备(弹簧或减震器)。 * z8 X, ]7 v7 W: c/ [. p流条, . i1 H8 H4 g1 s) o. r, g在部件或组件之间传输电、数据、或定时的单一电线或2 O1 ^) e2 y0 k9 p5 z a % h% c- G1 H5 X% l5 WB 9 E1 a* ^9 o0 {th . Z, o3 ~, p/ Q3 i8 l U# Qw 0 o; g. Y! L3 I4 ?* [; aB 7 J X* V8 T3 m2 p$ W2 b+ _% `c$ ?* R4 B* Z0 W# ~: T B " `/ \8 A* n7 y' s5 U# eduring certain maneuvers, particularly the approach and 9 b! a& C S( {& l0 r0 r& rla , @" [8 p+ ~4 c3 EBULKHEAD, A structural partition in the fuselage or! q' s5 m# i" _ {, s* m3 Y wing. 5 ~& y6 O$ w+ \+ \6 S+ v b8 GBUNGEE, A mechanical device (spring or a shoc" F0 R8 i u2 x# e absorber) for assisti, Y5 {. Z+ o0 b# } ]9 `( m! Y BUS, A single wire or group of wires which transfers0 X9 r1 _0 ?& k$ r+ @1 T$ ~ power, data, or timing between several units or ) Z6 D4 n7 g; Q- M: i! Zmodules. 3 R. l. R# i4 Q7 U4 D, u% U+ Y5 D% r抖振, 0 M3 Z& N7 | a2 d; h2 J由于机翼上表面的不稳定气流引起的机翼和机体的振$ A; d T7 k9 i4 l7 |/ Z 动。飞行9 i4 e* t; M$ l7 x$ e, y; Q0 Q- z/ Z: U! [, n6 i+ X+ M所应保持的 4 l& o# c' I% W3 y% y# \/ \, t壁板式隔框,8 U/ A$ |6 ?3 G& l$ ^! }0 c 机身或机翼内一种结构隔板。 1 O8 r. b5 ^% W9 q4 Z) y5 |' Z% N/ u用于协助起落 & Z8 U% H. ?$ l! I4 R! J0 {% o( g- F' c1 u9 E ?+ c电线组。 - c: p2 G9 k% p9 K# B( d英汉对照民用航空词典B OEING ! J# H" \9 E& E, G- d$ W/ s* d, ~' n$ Y: vTECHNICAL DICTIONARY 24

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BUS DRUM, A mechanical connection with pulleys 8 r8 z. g: f4 G3 t; r# M& p$ ~2 Fcables in the control system.6 d/ Z. E* e! y& Z- t/ S7 a and : F3 \0 s1 ]; |. D( v cl circuits for control and protection of ) i7 A! F) z ~/ b# O2 V! l7 vlectrical alternating current supply to the airplane. + C I. [! W0 Xduct for closing and opening the duct- p* r3 H" v% n8 y; H) @ assage. * \2 _ M) s* T$ L4 p9 Y: pUTTOCK LINE, A vertical reference plane along the ' A6 y+ Y: f' Z9 I* Hselage for horizontal measurements of the airplane. 4 h' X+ `" \* F" R接。 7 A! c% ^' t& {; d6 k组件,内含控制和保护飞机交流电源的电 ) h8 T9 G' B+ J) {# L H# Z* y) z- d7 ?1 `作动简控制的转动装置。用来关闭和 I( d, h) H9 w2 |+ \+ I 启管道。* b' \2 a6 D1 H5 j. s: L 沿机身走向的垂直参考面,用于飞机的水平测量。3 ^/ [- O% M$ V' U1 o9 o; ~ BUS PROTECTION PANEL, A module (black box)" j2 Y4 `+ v7 |" U containing electrica0 q2 g" ~( i9 V& U e 1 o6 E. Q8 e" l0 FBUTTERFLY VALVE, An actuator-operated, rotating 2 }9 Y" R/ r& R+ H, adevice in a : J6 H. q4 C8 _: ?6 J! a: [# o; cp 7 W Q: }: y( {, \B8 d. l1 f, Y' G# d( ?( z fu # r7 f! S# X) B" R转动鼓轮,$ U2 J; x1 @4 x 在操纵系统中,具有滑轮和钢索的机械式连5 u1 b; M/ r3 y- |9 W 汇流条防护板,3 W4 O) R" S( M2 Q6 {; K) x1 v4 g$ g 黑匣子式的: w: n* L- o. n) s5 H( ?4 V; G# J. `) u9 F1 D% \蝶形活门,8 N1 Y4 B3 T# q 是一个在管道中由% {+ W' {& A3 r* y* D# y5 Z' W _纵剖线, 0 G+ b* {) G, M& J8 L8 J英汉对照民用航空词典B OEING. q- \" A) j1 X" O6 D TECHNICAL DICTIONARY 25$ V) b- J0 a! d7 k' q' ~ BYPASS VALVE, A valve through which air or fluid will) r. [2 f! {9 v; x1 S! G flow if the normal flow path is blocked.0 h# w$ I& S0 X& ^. D" q. D, W BYTE, A group or string of binary digits. A byte is 7 J8 ]" N+ J/ Y7 B4 D/ Lsually eight bits long.: N9 H& z& T2 V+ \# G ABIN ALTITUDE, Atmospheric pressure maintained: r' T6 X/ B z& ] ithin the cabin, indicated in terms of feet above sea# t% V% L1 }& |' M ALIBRATE, To repair, adjust, fix or correct the 9 W) u: t* c+ Y" h" g% G# Oeasuring capabilities of a measuring device. 8 t9 u% b; v% _. `ALIBRATED AIRSPEED (CAS), Indicated airspeed ; f3 ^, l& H' R; dAS) corrected for position error.7 g# x1 L8 h( ~3 \2 ]0 v. q% j nical * _# U" P% g) ~1 y6 Romponents.: f. ~" Z5 i! ]* H' U6 U) R# j1 w+ G3 S9 t& o: c( p 节,: o+ n) D$ z6 u) d 一组或一列二进制数。通常一个字节长8位。 + T( R0 r7 I2 t2 J1 U) v舱高度, & ?0 K: X- N( I, @& o4 M座舱内保持的空气压力,以海拔多少英尺表示。7 i- x3 J2 g; T( v. A: A 准,7 H) z" s+ m. F" P 修理,调整,定位或改正测量装置的测量功能。 ) P) O# M- z) S5 [- k2 ?正空速(CAS),. y* @8 k0 f k* [ 在修正了位置误差之后的指示空速(IAS)。 `4 m4 m5 m( O2 @1 _ 用来移动机件的一种转动装置。8 U! n% p% ^4 H! J' g u ; ?! O& j2 }# cC * h) ~. j, A4 R" YC & A4 z/ d, k% B! [: c. N4 Vw ' i$ \/ c* u* K [level.2 y* \4 D# m# L- A/ H C. V I7 X& A: j- _. y- [ m: U! v, S7 _2 Z0 V C# _9 T9 y+ c# E6 G9 V% G! r (I $ i# e( t& K5 o9 TCAM, A rotating device for movement of mecha ! m7 A7 W* T7 I' `, }, }9 bC9 }5 A! G5 K! h 旁通活门 , _9 l$ v8 A1 e" z气流或液流在正常通道阻塞时所经过的活门。 ( f% \- b; B! u' J( h) P! l; I3 v+ D8 v6 i( F! G/ x1 c. F P7 o# h9 ] J* A+ ], w G+ E T' {4 x! V4 n0 W 凸轮, & U7 [2 U$ u v: J4 H* R2 u5 ]英汉对照民用航空词典B + x# Y4 W6 I+ x! qCAM-OUT, An autopilot condition in which the actuator' i5 r8 y1 u& W detent piston is overridden, either manually or by the, X) `' [ s8 e) o ther autopilot actuator.# X9 @( |4 [& S* ^3 j AP, SEE - CAPTURE 0 @' M9 u8 f8 S7 U& }0 Z+ PAPACITANCE, The measurement of electrical energy( P/ h3 U9 ]& O; I- |# l tored in a capacitor (condenser). ) l" C9 k! h4 k. XAPACITOR, An electrical component of two metal1 a9 T, i1 ]5 P* K" r# u1 {! y lates separated by a dielectric material, for storing % n3 w6 O1 Z1 p0 c7 Klectrical energy.- Q7 P3 W* S4 F7 F CAPTURE, An autopilot or flight director function to" Z6 a- y1 o# Y4 I4 t acquire a selected mode. % a1 R3 B8 X3 g0 O* K2 Z+ OCARD FILE, A container on the airplane for printed * P8 y$ J- l" i* Tcircuit cards.0 Y3 y* o4 {+ X; N1 B 一自 4 z: Y$ V! g5 v! n1 a# S, Z# ?动驾驶舵机所超控。 , D+ K. y- y: m1 M& l& u( R截获,0 S$ l B% Y0 R 见Capture* v% L+ V( O. C1 B" @ o 4 _: r. [6 w1 n0 U( z0 oC% t$ f" F. Q2 i2 S C 1 [' N* Z. U" t" qs4 R- g5 t' R0 O0 C) ~ C 6 {8 I. a' W6 l, `* U0 O5 r" vp ' B2 _, z4 w% q; G) xe0 [# g$ N# H5 T: g! | 凸轮不工作,4 T* M0 ~, j% p( ^+ N" b# z/ S Z 一种自动驾驶状态。此时舵机锁定活塞被人工或另0 C+ T8 Y9 L$ T" R4 c. l$ ^' [! v% ~8 D2 { 电容量,; k6 N1 }% B# N. c) \. n 电容器内所储存的电能的量度。! u1 S- U. r3 S$ A( {- K$ K 容器,$ r! G5 u& A; q/ [ 两片金属中间用绝缘材料隔开的电器。用以储存电能。 ! [' P" v7 R7 ]! A) M. C* p1 s$ B截获(CAP),8 k. Y" Q) {* q 自动驾驶仪或飞行指引仪的获取选定方式的功能。 8 {+ a, B" }' _4 l* E线路板盒,! C( v3 ^, d& K, D; H$ v 飞机上安装印刷线路板的容器。 # {+ d( b- H; a- p" m4 |! C) h7 q( g/ s+ _ OEING* r9 F/ D6 O' q. [0 { TECHNICAL DICTIONARY 262 L Q$ |. h( {7 |( S* a+ t3 o9 q 英汉对照民用航空词典B OEING0 K4 z* e" ^9 s9 `& v2 b TECHNICAL DICTIONARY 27 8 R5 v) x1 }$ p( l7 [ m/ }$ r! i; NCASCADE, Two or more similar circuits or amplifying! e/ N N) i* f; D4 E stages in which the output of one circuit provides the - i* G) ?" d! u0 {( G0 \. _" pput of the next. $ M' ~% s* m: G5 m) yASCADE VANE, A vane for turning the engine airflow , I5 {# s- d: i ?. ?$ w! W: y |uring operation of thrust reverser.; F4 f$ \/ X. e: B: Q/ }. I3 h3 T ASE DRAIN, A drain carrying lubricating and cooling( ~5 ~/ o" P, m- k: L$ P uid from a hydraulic pump. 3 m4 J$ X3 r' Q KATHODE, The element from which the principal; ?+ c7 I" d6 S2 V7 V; d tream of electrons flows.$ S' K! E+ Y' D$ g; J$ | ATHODE RAY TUBE, An evacuated glass tube with a6 o X7 r& q9 g# O. W) R% j CEILING, The height above the ground or water of the! x4 S s3 @) M4 \ base of the lowest layer of cloud below 6000 meters9 \+ D7 }+ V# C4 h& \ (20,000 feet) covering more than half the sky. % r% C4 b8 B% z' C9 Q: }; ?程。该 . k/ c8 P1 Z( F8 f) ?程中,一个电路的输出为下一个电路的输人。3 O5 t. ?8 e& U5 a) Z+ [& Y4 r 叶栅叶片, 3 O% M: W( m; A7 W在反推工作时,使发动机气流向相反方向流动的叶片。! A5 Y+ ?# M. K( x# z4 m 匣余油管, g1 |- x6 n. |0 _1 b液压泵多余的润滑液及冷却液的排放口。3 e6 a' p/ _) q, y" u! F; S 极,$ p0 o1 h/ f( P/ o, \3 M7 w 电子流流出的极位。# J$ i+ o! _/ O1 Z$ V% w 极射线管, & Q+ K" f, e' {* E; p有显象屏幕的真空玻璃管。用于显示信息。 8 d+ h2 e" v* D" a) ]8 l云高(云底高), $ h5 |* \! T$ B5 S8 w* {4 I/ H6000米(20,000英尺)以下已覆盖一半以上天空的最* f( t9 E# I D; G 低云层底距离地面或水面的高度。$ A. |8 x- Q" t4 {1 k$ _$ p& ? in 9 |* R" [& I1 J# ]' o5 O1 j! u8 eC ' w' N% R" X- x' f+ Z pd , A$ i5 ^" i( ~" Z$ N2 iC " j) p6 w, T9 mfl* Q. T6 c$ H7 A7 G* p8 z5 p C! f" P- e+ b' R0 A& ?" M2 I s8 L" k7 v7 c: `* v' E7 a9 ` C$ M4 J: C3 `. b4 t4 ?6 L viewing screen, used for displaying information. . s9 i6 j! ~1 ^级联,4 o" Q: T% O0 K9 g* M4 ~0 q 两个或两个以上的类似电路的逐级连接或放大过 5 Q; ^; x; h! H D/ C4 N; Q* ], l. Z | Q; h' m* W4 C- V- Y1 }5 Q0 v/ o. k% M. {! x6 U" L4 b0 ]& B8 ~; O/ s9 e# r/ G* j一个具0 k |+ E, j! ^+ O/ F. v% L 英汉对照民用航空词典B OEING# ?/ l6 e' q% ^8 a7 J) W) B TECHNICAL DICTIONARY 28 4 u$ L: b: s7 {& t. Q! R' Q5 eCELSIUS, A temperature scale in which zero is the( B5 q$ }) q$ _9 @& W; Q" Q freezing point of water and 100 is the boiling point of * n/ x. D* j2 Swater. " N: v1 @$ V* v& F! ]CENTER OF GRAVITY, The balance point of an object. `8 e6 B5 ^% E- f7 Y* `( Y r rigid structure expressed in terms of percent Mean# U" R/ |2 z) b erodynamic Chord or in inches from a reference point. 1 T- F9 K, V4 vENTERING CAM, A cam for moving a mechanism to a. X0 B0 F2 e3 b: s& d2 |4 I) I eutral position. . E3 N) w0 b: V- XIGURATION, A configuration of the: g8 }+ T( T4 A7 a4 {9 S# ` ircraft approved for operation by the local governing/ \) m! Q/ S# s gency.. z" S. U5 A/ A ENTRAL PROCESSING UNIT, In a computer or2 `+ q2 K9 k5 R5 m, F0 @6 @. { igital circuit, the section containing the arithmetic and4 l ^" L* u/ `& H' | gic,control, and internal memory circuits. * U& q! u8 j- v w cENTRIFUGAL FLOW COMPRESSOR, A type of 6 E6 o# t& M/ p8 V1 I5 l5 W/ d2 l/ \ompressor in which air is taken into the center of the ) U8 S9 d* W7 Y3 l+ C vpeller and is slung outward centrifugally into a diffuser , f, \0 c1 y8 Y. |4 vhere it is slowed and pressure is increased., `6 i& U6 P- u- R _ CG, SEE - CENTER OF GRAVITY' C) T; G. _: Y# M 构的平衡点,以平均气动力弦的百分比或9 `) N' ~" |8 C" u, ?7 L 某一参考点若干英寸来表示。% I! a8 f3 z! L7 x' p3 R& u 中凸轮,$ l8 Q1 i/ ]9 A 将机构移向中立位置的凸轮。/ y- ~+ R5 B! m" i 格的装机状态,2 E- t D+ m4 h- {8 h& J0 ] 由当地主管单位批准使用的飞机装机状态。4 O2 w( z2 n% r* ~0 [ 中央处理器, . k6 E0 S5 d$ j. C, @计算机或数字电路中含有运算,逻辑,控制和内部存 5 \! z: A/ Q$ W" Q+ x储电路的部分。 * y. Z, \* C$ o' s5 q1 l4 d& \心式压气机,9 [/ q; N% J/ H; E 压气机的一种。当进气到达叶轮中心时,被叶轮离心抛; H, F; `1 A0 i 进人扩散器。在扩散器中气体流速减慢,压力增加。5 b% w$ p J- \8 I7 Z. o 重心, 4 _* Z% e% _5 p3 J$ M1 u4 P见Center of Gravity1 a. u/ x* c! p! w% s o : |( `9 Z1 [$ |/ bA # T: K! J" L9 ] ^1 d, jC2 |7 P! Y! k) f- y1 {8 K- v n z0 q% P a( p. H- X/ N- Z' T( wCERTIFIED CONF6 S+ o, c. D0 h& n1 ` a 5 {( `+ @1 v' Ma # r, |; E. m6 w* ~& l- }1 kC ) f! e4 U; ]3 S7 Nd 4 t% n9 D8 I* l! X8 ilo) P1 u9 R: o+ R C 8 Z8 u. Q3 O0 fc* n; O1 r3 r* Z8 y im # d) _: p9 t1 \2 mw! |. e) @5 i7 H* T7 U 摄氏度(°C), + O$ d6 G! x8 q4 R% H( K$ T温度的度量单位。在此单位中,0°C表示水的冰点, 1 V2 p) O* l! J4 y* m100°C表示沸点。 ( k4 l& V1 \4 p. u* x重心 $ W2 C1 C& O* A& Q1 a3 H物体或刚性结 9 Q9 K: `2 ~+ E L+ f i) e4 I9 Z7 B( w3 r9 d; z7 e1 c i8 R' O+ P3 H9 V8 |4 K; {/ `6 ?1 n4 f2 M4 `; {; b; O; Y6 o2 {+ ^4 N. I* g5 f" o9 q. ~% [1 _; H英汉对照民用航空词典B OEING ' J8 T2 j$ R( z, jTECHNICAL DICTIONARY 29 ) s' x C( {% aCHANGEOVER, Conversion from one mode to another. 5 r4 l9 s$ M9 L! R* PHARGING VALVE, A valve for supplying air or fluid to. O9 [$ }* z0 n9 h/ q% m HECK VALVE, A valve allowing flow in only one - n7 s2 F( e9 k7 ?irection. See Non-Return Valve.$ {" K! \/ |1 ]. c HECKSUM, In a computer, a summation of digits or4 J: R6 N& J7 t- M& C N its which are primarily used for error detection. # O2 k0 ]6 X# f5 ZHIP DETECTOR, A magnetic plug in sumps of# D) T, }+ ]8 x5 v: l bricated components for detection of internal failure of% Q7 {& f# W8 p2 n e component. ; W/ _: t I( L2 RHORD, A structural component of spars or frames. 2 o' Q6 p- e( X* Q+ {' j3 a添活门,/ c' V- B8 U4 w7 ~ 器充气或加液的活门。 5 [4 {9 `3 N% q7 F0 n% w单向活门, ) C5 }5 Z, u5 P1 h8 ~: a; }仅容许单向流动的活门。见Non-Return Valve

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发表于 2008-12-24 21:38:05 |只看该作者
C. H8 j8 M; D# {: A/ e+ l9 D1 s* R a reservoir. - G9 C: a% }: q3 h4 ]9 `) @C- L6 `+ Q# j C% q% P d ; ?+ @) }3 c j5 PC3 y; Z" M6 h d+ b) G2 }9 | b6 B* h W( o, T% q: w+ [ C- T1 N, T' W( W. m* I lu/ T; k; S' u2 W' Z th ! {/ n" Y/ H* QC : v/ p' T+ i1 C8 E+ s转换, 1 L4 }; y9 i: L+ @1 n由一个方式转换到另一个方式。2 \ M' z I5 p( ` C3 G% w! l1 p$ G 用来向储存, F# r9 |; m+ f4 v* R! P# ^' ?( l8 t" v3 P0 Z 总和校验, 2 K& l1 ~. V* `$ \: Z. q计算机中,把那些用来探错误的数宇或位数的总和进1 `5 O, W$ k2 U' E/ k. ^" r2 b# C 求和计算。! U4 V( ?/ l& d0 A 属碎屑探测器, ; \# K0 W1 x3 r: e5 X! g装在被润滑的部件滑油回油管路上的磁性塞子。用来探, u: R' Y" ?; F$ g2 W$ B% { 部件内部有无损坏。 7 Y ^5 l( n: X& ?+ |5 m弦,9 z: z2 ?* x8 B3 l 梁或框架的结构部件。 / ^$ t% V0 O6 i. ?" Q& f; U: j$ p" Q8 V7 e c& |+ N# K0 k- \6 {' a5 Y6 o6 c& g! N" V8 r. P$ w% P( Z1 b5 p2 ~3 F$ x: b% f9 W) K9 L, [0 v& K3 |, L5 d, P: a w% b/ L: k) k英汉对照民用航空词典B OEING, v6 o4 c3 p7 E TECHNICAL DICTIONARY 30 1 \% `0 c# H# A; C, [4 S9 p8 Y3 ZCIRCUIT, A closed path through which current flows* p7 w+ V+ D: Z( E ource.1 t- s) r2 y: j6 x" l2 H6 Y IRCUIT BREAKER, A device that automatically 0 j( a6 Z( c( I9 O6 Heactivate the system.. w' \- l$ t# Q) U8 m7 X lear of all non-frangible objects which k b% R r* B6 F ay be used as takeoff distance available when ) D+ ?% W# x# e/ balculating a takeoff weight.! D0 ]9 P% g' Y8 t6 t: L r water under the control of the appropriate2 Y0 T! s' M* L3 Z/ k uthority,selected or prepared as a suitable area over : O$ v8 m i0 s4 nhich an aeroplane may make a portion of its initial & a' B, v. Q) \2 B9 |* ^limb to a specified height.8 c3 O; L2 A F" W: c6 _ increasing.% G: O7 u4 h& S! x6 P) X4 w sed 2 o/ v4 k/ B& ?( ~( O: yLOCK SIGNAL, A continuous string of pulses used for" ], a& ~! S" B 开关,( f4 F9 ?6 h' @! Z+ K& h& K! J 故障情况下自动中断电流以保护线路不受过电损 " N- J2 U1 ?4 m; N0 G9 ?体障碍物的区域。在计 : A/ l. G$ x( M8 w. V/ G9 ~起飞重量时该区域可作为可用起飞距离。 . C9 e* i# U* R( [+ ]- @5 e是在有关当局管辖的地面或水域内一个界限明确的长/ ]7 B1 n) a& [4 \8 T& \5 _ 形区域。在这个选定的合适区域内,飞机可完成初始爬 9 z7 W( ^" {' _& m的一部分,上升到一个指定高度。, p$ C T8 t* Q; u+ i% J4 ~2 ^0 i 飞机高度不断增加的飞行阶段。 2 @; k9 g& h; b, p3 n钟脉冲,0 _0 Y: k$ W" R, @ 步的连续脉冲信号串。% @7 `& M" c% C- I: J; C. T5 p from a source, through various components, and back3 k7 b8 @ m/ B+ a! c- N to the s 1 m5 T0 K% ?( |1 E/ ?4 x3 ^C! a* R) S$ ]8 a- O& \: K2 l5 V interrupts the flow of electricity (current) during fault : e9 a9 J6 R" s% u y4 ccondition to protect wiring from excess current. Circuit9 _+ E) I j! H" c0 K4 r7 g8 j# _ breakers are also used as a means to manually+ i( t1 W3 N* h. N [5 y8 z8 v0 u d ' d" y6 v- M/ M Y$ VCLEARWAY 1, An area beyond the takeoff end of the 5 i& R, i0 _9 r* |# [2 K8 ~; Erunway which is c2 s3 D: L5 ~7 A! ~ m * w* X; l0 Y: W# V' P) _c& m3 L2 t& b: B) s; B) T3 W CLEARWAY 2, A defined rectangular area on the . {: y6 j5 ], I' X, z. g% Yground o ( e8 a- I* i. |9 ?5 E) g! ua 1 G( ^1 \4 \3 w6 Q) Aw ! T3 ~( L& c0 {* N$ k: L% Qc# p5 `* \& {8 u" D) f- l CLIMB, Phase of flight where the altitude is6 C+ j e# s3 k' C$ c% G9 U1 F CLIMB LIMIT WEIGHT, Maximum takeoff weight ba7 r8 p- O/ `- C' ^7 |2 i on a minimum climb gradient with one engine# r' p( W7 d0 k; \* I8 @ inoperative.8 l3 @5 o8 l! t C ' D$ M5 f7 m3 n+ t5 j& s8 `1 rsynchronization., a! G+ Y2 m, `+ u+ o 电路, ' u9 b8 z/ @5 @& |. P9 d一个闭合的回路。电流由源头流出,经过各个元件流回) N4 ^+ f( X$ s9 P- d& z 源头。 - W" G( u6 @5 _7 F" W- q$ t; V& z0 J1 Q: S$ ?, R, v. { 能在% c* S0 d* a8 }) U% N: _. e 坏的装置。跳开关也可用于人工使系统无效。 - ]- u2 \; }5 d! i# s. D3 c {) x. q一号净空道,* ~+ u/ V, N, h 是跑道起飞端以外,不含任何刚: v/ f6 o) A+ E. J, ]. Q4 T0 x1 C1 I' p 二号净空道, * s% E/ [+ V; @2 p2 U* G+ S" \: P: q/ y) p6 ?$ J+ g; X$ F. v( }4 O7 ~( V# I) \ 爬升, * i( [, t0 T* g4 \; k爬升限重, 2 Z$ p0 R O) H- Z取决于由一台发动机工作时的最低爬升梯度的最大起7 b( S: t- M2 g" { 飞重量。 / [: U) [/ ]/ {' x. q, ^) @6 q: x用于同 . d K8 {- P7 e: j" M英汉对照民用航空词典B OEING - z5 p+ K3 {* O& A3 M9 sTECHNICAL DICTIONARY 31 . P2 D& C0 H. w) c7 ^ C2 qCOALESCER, A device in the water separator for , H5 _7 E$ z- {+ g2 N" j. Yollecting moisture from the cold air. 3 s% e. p* C* L8 \, a& Gn antenna with a receiver or transmitter. ; y5 E( T7 z0 Q0 Ihe cable has an inner conductor and an outer : d, M1 B- b. c( z4 I4 Krounded shield. * `+ a, P3 W$ z; `& W, Bting one inside the* f) _1 }! }" k6 N$ c ther for rotating the low and high pressure( @' I. F" n D3 H' h) [" T7 Z ompressors by the low and high pressure engine$ q& j7 Z$ @% @( ?- P# B rbines. % L2 ]$ |: a7 O" \2 HOMBUSTION CHAMBER, A part of an engine for$ `* o( P1 Z# w% s urning fuel in the air supplied by the compressor." u8 V. v! `6 s" @' u+ `/ k 置。! M' s: H: { Y2 M 射机的电缆。电缆 8 h7 ?' h2 [& ~$ c% u a1 q中心导体和外层的屏蔽所组成。 , Q4 [3 c k4 O两个套在一起旋转的轴。用于使发动机低压和高压涡轮4 p$ H% S/ q k) H' g8 t) R 别带动低压和高压压气机。9 f, `8 D" Y# v+ B" s 烧室, ( M4 m5 {; G7 n% ~$ I发动机的一部分。用来使燃油和压气机所提供的空气相$ N9 N7 D2 G6 ~6 h5 ~ 合而燃烧。

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发表于 2008-12-24 21:38:35 |只看该作者
c + p0 S l k8 ^! K* G) dCOAXIAL CABLE, An electrical cable usually $ O( [2 K/ V" S% E+ G5 Lconnecting a" u% b* G' F B; n A" I T3 ?% V! F6 _* C: R1 R/ ` g! _' u/ a& z) {& z+ A# i COAXIAL SHAFT, Two shafts rota+ c+ E4 t8 R8 p5 x2 z0 a1 H2 p o9 A2 u, k; D0 p# S c 6 S9 q0 X4 g9 p/ ntu ) Z6 ~$ ]4 Z5 v5 UC2 `# q' K, Y' `& \" ~ b' c& f; a8 r* S; f* _0 n7 o 凝聚器, % I$ Y. {( r) a4 j5 o6 H3 g6 G水分离器内收集冷空气中水份的装 8 P) D5 }+ B& o4 I t. |( q同轴电缆, & c$ Y4 K4 x- @一种通常用来联接天线与接收机或发( Q; ]! Z4 L/ w/ N. o( Y E7 ]2 Q; `8 a$ E( L 同心轴,$ d9 ?6 `7 O, o" ~& G D- D, }% m5 X' N$ R5 s# s: K" L8 H5 t: F8 ^2 H/ _% j' g' r8 L/ q 英汉对照民用航空词典B OEING ) u( P# a- k% D+ j( x+ eTECHNICAL DICTIONARY 32 ' B1 Y3 l5 [) f5 v- lCOMMAND BAR, A flight director pitch or roll comman " _- e. v' S5 w; Y2 c7 Mindication.! B& l+ |" m- I' D d" e& j& p% q p' f OMPANY ROUTE, A route flown by the airplane2 R6 e3 W. [& J' T OMPASS LOCATOR, A low power, low or medium' ~2 ~/ s* V+ R' s7 G equency (L/MF) radio beacon usually installed in8 n& g5 p# Q2 S2 K1 e2 Y4 H0 U onjunction with the outer or middle marker of an 1 h6 A, p: Y7 F( a. rtor (LOM), A compass3 u( Z, h: t0 i* o locator installed in conjunction with the outer( l$ e5 g" _; f9 U marker of an instrument landing system. 5 B: Z F. a% \! [$ H Xss ) z* J8 D- q* a3 _0 N) [le ; ~: L& g" \, }0 y7 }OMPENSATION, To offset, balance, or counteract. / A/ F+ n' w5 j- \% yOMPENSATOR, A dual capacitor for changing the fuel % `0 Y. d; C |* k2 faging circuit capacitance due to changes in fuel" C: P4 i* ?7 @ ensity. 4 f. q0 h/ w( F, ^' m3 x' e& KOMPOSITE MATERIALS, Non-metallic materials used . X0 s3 w; r" w; xr airplane construction. Fiberglass, Nomex, Kevlar,5 T4 k: ^. [: ]( k0 Q raphite Epoxy are composite materials.' Y% N2 q. x- R/ Q; I 司航路,9 d. I+ n9 i+ ~ 在飞行管理计算机数据库内由航空公司飞行! b% A/ P3 O* c2 \3 m 盘定位台,9 A0 c- R, V' T/ s 与仪表着陆进近系统的远距或中距指点标配套安装的 ! {- k; x- l u9 t# s9 ^" x) h功率、低频、或中频无线电信标装置(低功率NDB台)。. F x/ p$ L" [: K8 L: ` 程序中用来导航。 ; c! z, h0 C( {1 [1.远台, 0 v9 Y5 M+ j1 {: D6 J与仪表着陆进近系统的远指点标配套安装的罗4 t/ C' C) X! |% J 盘信标台(NDB)。 1 o/ N5 Y4 |9 S2 ?: y+ g- Y偿,1 C4 V& \) U' r+ J6 K) w+ o 抵消、平衡、或中和。4 n4 C3 w8 e6 W& R/ Z% R 偿器, 4 d/ A& c' u& `3 a在燃油计量电路中,用来改变电路上的电容,以与燃9 {: G/ F; N9 Z- A1 j( I; T 密度改变所引起的电容改变相抗衡的双电容器。 2 ~: g6 m9 G: m f( R合材料,& {, F4 M4 P3 W4 h$ j5 R 用于飞机制造的非金属材料。如纤维玻璃,Nomex, " x2 y& F. T% \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 6 u7 v5 y% n8 A/ ~; g f7 boperator that is normally stored in the flight3 j% H7 e* ]) Q management computer's data base." ?) H! j6 X3 T$ F; [ T' u C: ]7 ]% J4 c5 [( o* H, ? fr J4 v3 H6 b; c+ zc 5 A( y+ T9 q( N5 S* a7 |instrument landing system (ILS). It can be used for4 P0 i/ y6 P- s7 Q4 G, W! k navigation as authorized in the approach procedure." ?' V" ~" e/ m; Z 1. Outer Compass Loca ( c) J8 b; X$ p$ G X1 F, R. |2. Middle Compass Locator (LMM), A compa / k, A5 B% y z) S; o2 Elocator installed in conjunction with the midd9 r$ ^& i9 x& F3 t marker of an instrument landing system. 3 K! U0 T7 x3 e1 o8 A0 {6 o; H6 DC K) Q, u" A% R+ w+ kC4 [0 s+ i$ z, n8 c* e( L) [/ k g& m7 t; g l8 r% q d8 E2 F( R* e9 z- ^% P' f' ~* @ C 4 ^7 X; |' [+ @$ x }8 hfo! M; b& s- s) v, V2 m5 @5 z! E( E g . }* ?1 \" G* Y# e6 E. l指令杆, 1 H4 P# W9 D+ X( p+ p* i飞行指引仪俯仰或坡度的指令显示。8 Y( K8 x% f. f5 q5 C4 g! B+ c8 ^6 N- H! j/ b1 h 通常储存 + j# e* n9 X4 U2 g/ X的航路。4 R; q7 p' n( ~7 i5 P7 q# S8 y2 Q7 e( x6 n- T Z# P. I& ?3 ^' w/ n+ Q经认可后在进近9 L c. O. E s* h6 R# h# H! b1 H 2.中台,0 W* K1 I |9 W& o 与仪表着陆进近系统的中指点标配套安装的罗 ( y- Q' l# J/ l) }) }0 T- n1 \盘定位台(NDB)。) j7 w8 u6 i. y8 @- x$ ]- [% m9 K p& B# E' P' v, ^2 U, G- ]5 m6 G/ z1 Z, X [& n; S6 q8 S' F; h2 N" F+ J* g) c7 n& ] K + r3 {4 _7 p# h! x+ |英汉对照民用航空词典B OEING 0 K! f: l5 y$ k% @* tTECHNICAL DICTIONARY 33 5 B: S9 u& Q7 Kby, O2 K7 U5 W, ]% G- [ or increasing air 9 u; x0 @1 Y5 x$ C: dressure and temperature before the air enters the 7 m0 f/ O0 d. c/ r; e. l: xombustion chamber, Low pressure compressor - front8 n+ o7 e, c: g% k N* e) w ection of compressor, High pressure compressor- rear& g) z# ]9 I1 g4 z. g OMPRESSOR STALL, An event that occurs when3 s! I- X( ]) _7 Q- { ~ ere is a complete stoppage of air or reversal of air flow8 G1 N1 u" l1 J M! k5 I COMPRESSOR SURGE, SEE - COMPRESSOR ) n i ^% E9 \ VSTALL COMPUTED AIRSPEED, Indicated airspeed, y W) [/ v; s; p. @ corrected for the static source error. - M6 {5 T3 I7 ~( W2 p+ b" u的机械轴来驱 % X) _& r9 F' M" S# },用来增加吸进空气之压力和温度,以供燃烧室使用。 , V" P: `3 m2 B- D8 n9 G压压气机—压气机的前段,高压压气机—压气机的后; O2 s( k5 W) q7 a! v! [: k; J6 I, q& _# t气机失速, 5 p4 x8 N: y' n! h. T当气流完全停止或通过压气机时气流方向逆反的一种7 W2 u: W. G$ V5 ?2 B 压气机喘振, % h+ \' Q9 J3 y0 P9 s7 V) i见Compressor Stall1 e9 i, K% u" w+ C" z) m2 l COMPRESSOR, A rotating part of an engine driven V" g; W1 r# ma mechanical shaft from the turbines f" ?4 R$ Z# J# } { p" l% y- H0 h+ [4 {- a7 v% l. U0 d c / k" z* S0 _$ q* S( X4 hs 6 t4 l7 i( Z }4 _section of compressor. $ m+ @; |! O+ [( e# @3 X, oC 0 A' \6 H# c' ]$ y- Oth6 ^' Z$ [' \: B R: g through the compressor. " u1 L( x- u5 ~" ^9 ~压气机,8 Q u$ J4 x' m1 V7 i( d; Z 发动机内的一个旋转部件。由与涡轮相连5 T+ l v4 u' h/ {9 B* ?3 v/ I+ `! {$ c8 B6 i5 L% Z- ^& ^$ y$ K" A/ `, q% @2 ]% m' c1 l. \# ^, D7 S现象。 7 d1 r; g* Z- f% v' o+ x% b4 x0 L/ m& a 计算空速, ( m# b- s$ n5 P8 \4 H修正了静态源误差后的指示空速。) R: |' N; p+ u; a0 a3 x J 英汉对照民用航空词典B OEING8 u5 a1 P0 J' G; \' I TECHNICAL DICTIONARY 34

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发表于 2008-12-24 21:39:27 |只看该作者
COMPUTER, A device that performs arithmetic$ c% p! _, D5 L3 S x2 | operations, manipulates data, and makes decisions. ) h* L _. v2 F! U) g0 T7 `$ @( nditioning2 r. u( d* T* y/ C: E9 ?% w the air and the0 J Z% ^# U6 W6 [ frigerant or moisture vapor is changed into a liquid.! ~) ]/ Z3 F/ L: e: K ine! m2 t, _ h: v3 c ONFIGURATION, The position of flight controls,6 J4 y9 a- a, ? missing which) l) X5 p) a9 Z* u may affect the aerodynamic performance of the* \( b/ J( [) }* K1 u { airplane.1 s }& x4 g9 q) t! y 置。 3 i1 a/ g& U+ _! U中能使热能散发到空气中,以及使冷冻剂或湿& S* \4 s' \# ~& W% ~& n 转变为液体的部件。5 i7 p& U; W+ x, v7 Q8 J 连接到飞机结构上。 ; {2 S: s. z- ~- n, N) D- k态, 5 d3 f; U, E/ P& P8 h7 L& V/ Q0 P定飞行阶段中,飞行操纵面,起落架等的位置。 - g: [8 [. g$ g, z5 z8 G), 3 }2 Y% K8 u( r0 j& U受到影响。 4 i. X: O; u: w6 m: a5 S ^. iCONDENSER, The component in an air con5 H! `3 V& q3 ]1 `' R; z system where heat energy is given to / [% w: e, Z( E9 ~& Sre0 W' O" \3 x6 g$ Z CONE BOLT, A bolt in the shape of a cone for eng 7 t) n0 q% A: s1 Tattachment to the airplane structure.+ }! i1 s' T! T) {+ x: c; g% J C9 {5 s% J1 [# m6 p5 [- Q+ [- v. A landing gear, etc., for a particular phase of flight, e.g.,, w$ g9 ^: _2 D. E' N Takeoff Configuration, Landing Configuration, etc.! Y* o8 ^7 J+ \+ f: j' I CONFIGURATION DEVIATION LIST (CDL), Appendix X3 i" ^! {+ J; Y+ D6 A in the Airplane Flight Manual (AFM) allowing operation1 r. }* T4 Q6 C$ t! C& a D of the airplane with certain airframe parts ( |+ f5 Y( D3 K7 K: S/ V% G计算机, . g6 r/ o9 R/ d- @4 R. _能作算数运算,数据操纵,和决策的装 1 d1 U$ [1 r A: q冷凝器,! M7 m* x" e' P3 c, { 空调系统2 A7 B- R9 j2 Z. U* B. H" P+ @1 F# K3 l) ^* M" X- R! t锥形螺栓, & v0 O; G* K; K外形是锥形的螺栓,用以将发动机' Z. r n4 p7 |9 Q9 e) O. ^& b" [) X) W0 d 在某一特 , G5 k2 h- z! G6 b* n/ ?如起飞形态,着陆形态等。 1 H) w0 I/ y$ B5 J缺件单(CDL& ]0 ?- l5 V1 v3 c: F 飞机飞行手册的附录所开列的飞机上某些零件的清单。 2 }7 w4 n/ v7 u' U1 {在缺少这类零件时,可以飞行但气动性能可能 . i/ B* R( E0 \% f$ K8 a英汉对照民用航空词典B OEING" O5 C; j7 b1 P- B; h 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; {- d4 F$ R' ]4 I1 R component for changing variable engine gearbox speed% C. X d5 g: t ONTROL AXES, The three axes of the airplane which + L4 j% b# ^$ T4 f9 Z6 z. O& wre perpendicular to each other and pass through the( {7 K/ T- X5 P" g3 n enter of gravity of the airplane.9 q2 b5 d) a$ \, m, e Pitch axis - Horizontal or lateral axis, passes through; D3 N. E/ ^* l: [( N the airplane from one side to the other - ' @* s) H6 g7 {8 C unose up and nose down control is by " r1 {& h! W5 D% Y& E2 Melevators (and stabilizer for trim). & Y" `2 I4 F0 y( }: G. N6 Q2 ?Roll axis - Longitudinal axis, passes through the 8 a9 Z* O, I8 M- D- Qairplane from front to rear - wing up and , x3 s* |0 w4 ]" H' I* Vwing down control is by ailerons and2 g! [) d8 s/ p2 @ flight spoilers. & b, P$ K1 ?# t" u0 l% y8 u0 FYaw axis - Vertical axis, passes through the% N. J* l+ H; }, _ airplane from top to bottom - left and 2 T5 O: g" H% O' y: z6 Bright control is by rudder.1 P& M& m4 Q8 Q4 E% } 置, * v/ Y3 S8 d, ?6 S' O) ~6 G* Z制轴," L# g- ^1 E) X& I 通过飞机重心互相垂直的三个轴。 % k: U9 T5 O: n0 U/ X, d* Z% s俯仰轴—又称水平轴或横轴。由飞机的一侧通向另 . ^; n2 n% A& l- _' y6 m2 P- y侧。飞机绕此轴转动即造成机首的俯与仰 ) E1 u9 K% q1 I0 r) F俯仰控制是由升降舵来达成的,水平安定 / r& o, Y/ Q* \4 q则为配平之用。4 Q! g. j* B. Y7 o% [9 c, M 横滚轴—又称纵轴。由飞机的前部通向后部。机翼 & S3 U3 }; l; [* N( z0 p下运动由副翼和飞行扰流板控制。, F& G/ D `4 Z4 o* N& I7 Y# K 偏航轴—又称垂直轴。由机身上方通向下方。飞机7 x4 p. F( k) Q! F5 j 此轴转动即造成机首之左右运动,此一运 ! A4 ^4 S4 [1 ]1 u由方向舵控制。 : X/ s) F( N! o9 X0 Q8 T" Hto constant speed to drive the electrical power.7 e) ?; y, j) E4 B C Q# a4 S/ t" ba + \+ K3 @/ G, [9 wc( _* t1 g. ?$ {, b# x5 @/ H 恒速驱动装: `+ d/ G6 W; u% S 将发动机齿轮箱的可变转速转变为恒速以驱动电源的- J3 Y* P n6 `4 ?, E' w& Z 液压机械式部件。 - ~7 z3 C0 g* Q8 V F# r+ ]7 D1 ^% b+ J: _" I) w1 K6 [& A) l* d( D/ R& m x7 ?( j6 k4 E# v1 O. T; c' F% E1 |9 X( y9 b0 l) B: ^/ S# P7 q8 p% ~! B' z# O a9 A! ]) k5 u2 r! I" h9 _% U 英汉对照民用航空词典B OEING 6 S b* E. l; \* T& p8 Z6 m* KTECHNICAL DICTIONARY 36 % _/ S0 g, f& K6 S* y, \CONTROL COLUMN, A mechanical component used2 K( g; T" K1 S. K rs 0 n6 p0 ?* T6 H( w# C- @nd elevators.- l+ |6 x& L9 H# v% ^8 N2 N ONTROL SURFACE, Moveable panels on wings and 9 e! i9 e6 y8 s( o* bil for movement of airplane on pitch, roll and yaw axes.$ Y: \ ]+ X. r$ L7 \/ Z# b3 r ONTROL TAB, SEE - BALANCE TAB 1 t1 I* s' {. D, X9 `0 X: CONTROL AREA, A controlled airspace extending! a+ y: j" O. I" L5 a" T. x9 @9 t pwards from a specified limit above the earth.: p$ x$ d; |: S ONTROL ZONE, A controlled airspace extending5 ~0 U% L' B6 B9 [6 R: T7 c" H pwards from the surface of the earth to a specified) B |. |% \4 t. Q+ `/ s pper limit.6 {* X; r( N+ A0 h is : F/ ]) S2 |! W' } _/ Jo IFR flights and to VFR flights in accordance- ?" Y; [1 j, B6 f5 w1 I: Z8 t% _ with the airspace classification. : [. c- H1 Y/ o' ?机械部 , K- _( [4 @3 [* W# e; R% [4 J0 _6 e+ C3 J5 l, ^ 操纵面, : z. I( Z7 r2 ?5 F5 v机翼和机尾上的可动面板,用以操纵飞机俯仰,坡度, ; G7 u, S* B4 Y* s& l7 w和偏航运动。 c# e4 r: m& m$ J) _# e4 T; T操纵片,$ g; f/ c" l% n" S3 K1 B 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 spoile9 k+ A" ?6 u, \: o; m% g2 } a6 y) I9 ]* U x) a3 s8 x2 _9 h) g C a# p6 ]- ?2 [6 f1 Qta" r1 t7 C! y# J/ N4 b C ( t' j9 W9 Z# WC6 `# m9 @. ]0 }/ { u# e/ W: V3 y' K( s2 | C- J5 T2 \; U+ _. r( R+ h u . p/ }7 t1 }) ?- E' C. S9 s5 l8 x7 Gu7 n( C @( \) b3 M" }! g CONTROLLED AIRSPACE, An airspace of defined 3 L* K9 V# |7 S- X, F' {" Pdimensions within which air traffic control service9 |: S# J. _: W$ C provided t 6 J f- W2 v( u, w) Z+ Z4 n驾驶杆,. n9 D( P$ c* D1 h 飞行员用来操纵副翼、飞行扰流板和升降舵的 , Q+ U1 Q; v! e) e3 |) u- }8 g" p! Z+ o: f+ N. V, v6 i1 } 管制区域,+ w" t9 g0 }& m( k 高于地面的指定极限以上的受管制的空域。 " z1 V: |9 P; ~$ t- G# n: n制范围, # x. {4 N6 S4 j! X1 u由地面到指定的高度以内的受管制的空域。 6 @" m! M! b/ ]& |6 d一个范围明确的空域。在该空域内,仪表飞行规则飞行 X( q& v \3 y* S; I 和目视飞行规则飞行有空中交通管制服务。- ?1 T$ f" D q1 q( M/ H) r) h9 a [$ C 受管制空域, ' v3 H, D# X: ?) c英汉对照民用航空词典B OEING * }9 e5 U/ ~: _* F# p+ HTECHNICAL DICTIONARY 374 M+ X, c5 P, b CONVERSION, To change into another form.3 i0 M8 J8 n/ j! C6 _ COORDINATES, The intersection of lines of reference, 5 T2 S0 W# d6 e; u( V6 d( xsually expressed in degrees/minutes/tenths of minutes7 H. x6 n4 W2 \8 @8 c4 e" L$ K f latitude and longitude, used to determine position or3 x7 A5 I3 Z/ l CO - o, v0 {+ v# O7 d1 ]destruction of th * k. [4 _- K& w! |, e. hchemical conta ! M* f3 g( {5 V& vCOWL, A remo ' w, ]: w6 c4 P; a( W" I! ^3 J3 Qfor access to th + _- ~. P J1 iFa $ Z- m& f/ F- U* K& zNose Cowl - Front section of the nacelle for air inlet 7 d% H$ q$ M* t' k x# R4 W4 Sto the engine./ w/ a/ w9 e# B, d4 @ M, i1 l$ \ Side Cowl - Cover around the sides of the engine. 8 O3 J! u1 z( M/ ^Thrust Reverser Cowl - Cover around the core: ~+ `8 u9 S* R: t section. / ^0 b/ V: `+ {, L' } v6 ]/ _/ ?Translating Cowl -The moveable outer portion of the1 y2 s2 A8 c: L5 D( ]2 j0 a. Q thrust reverser cowl which is+ ?7 Q7 x$ ?: N* [% u operated during reverse thrust.7 ]2 v$ m8 q Q0 |5 A0 {/ } 标, . \' N) X. K$ z基准线的相交点。一般以经纬度的度/分/十分之一分4 X) u9 f: }2 }( r! y+ [4 }2 @ 读数来确定位置和方位。8 D2 l: a7 N9 P. p1 u( H/ F 腐蚀+ R2 ?% G' J& s v3 ]- E. { 动机外部可拆除的罩子。发动机上的构件必须要取下 3 R1 D1 e- t% c6 I流罩后,才能够到。5 }8 n1 ^: H# v$ o* u0 Z( I+ b9 j) W7 O; W7 ]机的短舱的前段。) t1 a! U) I' A+ n: Y2 H 侧整流罩一发动机两侧的罩子。 S, `; k0 [% n1 O/ V* U, n5 i反推整流罩一发动机主体外的罩子。 7 N& d( I! S+ c( \ |% K1 n移动整流罩一反推整流罩外可移动的部份,在反推工 / _; x0 p/ w* F4 N' X5 m( o9 S; _- X作时使用。1 ~* z! Y( o; x; f5 G u 2 n0 [( Z, _& U# Y9 f$ t6 S+ wo8 P- O: q0 {$ Y location.' w9 H' q# R) s RROSION, A chemical action which causes gradual9 u8 B2 K7 Y% o, O e surface of a metal by oxidation or & Y( n( U' A0 w- vmination.$ ~2 d0 w( f% S0 T vable cover around the engine sections# ^ Z4 C! q r! R6 t e components on the engine.* T) D3 b S$ c) } n Cowl - Cover around the fan section.3 b1 f- E: W5 y7 h 转换, % Y& q4 q/ ?- p {# s改换到另一个方式。. i S1 Z% g& p, i1 u5 {5 a+ c4 m. P a; u' \& D- Z% Y/ y4 N) m" V. y5 z8 ?4 p( ^8 n* j 氧化或化学污染造成金属表面逐渐破坏的化学反应。 " v: \; v/ e% u. y0 ]发动机整流罩,1 i0 h+ W" Z7 ^& [4 `) A9 u( h {2 v( f( k% q. o% t# R& c0 t) W" Q2 H! R 扇整流罩一风扇外围的罩子。 1 Z: a0 M% X3 f, G: C6 y2 |前整流罩一引导空气进人发动$ a5 n; X5 v( N \4 f! [ 英汉对照民用航空词典B OEING: H) [9 d5 [4 v! _* C( Q3 J TECHNICAL DICTIONARY 38 ) g9 Y' [( h W! s4 ]CPU, SEE - CENTRAL PROCESSING UNIT 7 J" o% Q5 s' [CROSS TRACK, At 90 degrees from the desired track+ k f4 F# Y, ?; | Y f the airplane. For example, cross track distance is the, |& k7 `" p! L$ Y, }( v! i3 t istance from the desired track measured 90 degrees" ]4 b; y* L% `, L7 W/ K* T om the desired track. " t. b, X/ R \9 W! }0 J2 w. o- NROSS-CHANNEL, Electrical wire(s) connected from + u7 x# [( }3 l; v0 F$ bne system to another like system, for example, FCC 9 h7 H0 B: x0 c, O- T2 |% s3 L1 M+ [" to FCC "B". * C6 u" p+ ^5 j: y+ Bn adjacent engine or one on the other side.* K% q8 e4 s) r l crossfeed ; T' T& l& j- ?6 {: i2 Ianifold for fuel flow from one side of the airplane to the9 ]. U3 A* y, t! [ l- `7 Z6 _9 q ther side. & f4 X5 e- ~, r5 |4 f. W) w/ t# nre% f7 n8 G) @" g# c8 \ RUISE ALTITUDE, An altitude or flight level5 L# c) _$ ~, r1 l* p1 f% A g! f o ! {) X+ m/ k5 ed0 \/ r- {0 e7 Y* A: a6 f# p1 N4 n fr1 q8 Y5 `3 J& g7 V6 r3 i/ t1 D( ~ C- u+ x5 ~5 b M f* S0 ^ o& i" x, c# d" {; T "A 8 o; ~2 V2 S; N! J+ E' \: R% r& h0 TCROSSFEED, An interconnection between fuel : O: u5 s, Z# r* M. D4 V, S2 M. rmanifolds for fuel flow from one side of the airplane to& f7 ]* ]% Q! i; J! e a ' }" H8 A7 N4 `3 _+ k9 mCROSSFEED VALVE, A valve in the fue+ r! b3 G, B b, F m+ ?; y! d: x% ?. j2 X- [ o# K1 X3 p" W b4 b( t) ^$ R5 X CRT, SEE - CATHODE RAY TUBE ! h4 T: I% p: T' u0 N! g2 uCRUISE, Phase of flight where altitude and speed a ! {, k! d ~. {* Pbasically constant.$ x5 E% X' d5 F% b, l4 A C( f7 y6 B, c, r( A& }4 N; ]# W- _ maintained during enroute level flight. + B% h. n1 K% ]) `2 b4 \8 {+ e中央处理器0 S( ^% ^+ c, ?" Y' q* K+ _* s+ ^ 见Central Processing Unit. ) w% H& t7 `! I0 f9 n" c7 N交叉航迹(XTK),& p) W- ` R8 L( w 与飞机预计航迹成90°角的航迹。例如,交叉航迹距离, p: }5 e2 G U. C$ k% D" x 是用与预计航迹成90°角量取的到预计航迹的距离。/ l5 C# N) ?$ \* K# ]3 B% J+ W 通道跨接,+ W% u2 o; k% b9 d2 _8 ]/ y 电线由一个系统接到另一个类似系统。例如:由FCC0 {8 M5 l$ o% P' D- a; ] “A” + {; U* P( B5 q0 r1 m, m接到FCC“B”.. m/ e/ T0 u% e6 `4 D 机身另一侧的发动机。 0 F) Z! m v/ X' J1 v+ B于使燃油从飞机的一侧 # @0 Z1 f1 k; H6 J% P8 R向另一侧。# X2 A% s0 Y6 U6 K+ V6 A' Q& q# X 见Cathode Ray Tube ) t- I9 {' ~ W5 p( I+ {交输,, w5 A* Z/ r. q 燃油支管之间的交连设备。可使燃油从飞机一侧流向邻+ k5 A0 `0 e9 l6 Z+ i+ Y 近的发动机或在 $ T! ?0 Z" }8 z/ z/ {8 l交输活门, + T4 f- u. J' W0 g! f" c燃油交输支管内的一个活门。用; f- I9 D/ M" d7 ^: U3 |- i: T/ P c- _ 阴极射线管, 8 |: p" z7 d, _.! i: F3 H2 y0 g- J5 } 阶段。 # f& z& D! h% s. {3 m航高度,+ ]4 _, H( n4 ^+ v! f$ X 飞行期间,飞机所保持的高度或飞行高/ s! M3 }+ `1 [4 q 巡航, + Q; {' F( K- P! q飞机的高度和速度基本上没有什么变化的飞行) F+ o9 S" w9 v1 [9 w6 k5 \) t, T: m, M; k) k; b 在航线上水平 0 R' n% D1 z W K度层。9 B7 \' {/ M3 U( r) F7 W 英汉对照民用航空词典B OEING& u- h( w3 ~* \6 a( b3 j" O TECHNICAL DICTIONARY 39 ! p5 {; y6 `7 b; e+ @- @7 `0 b' PCSD, SEE - CONSTANT SPEED DRIVE 9 t4 y3 F9 F9 m. d' ]1 ?CURE, A chemical change which takes place in a resin6 A# v6 L8 Z. I4 o5 K% D and fiber based component causing it to solidify., M4 o8 g1 }) _ CYCLE, A complete series of events that take place1 `/ T; d( I4 V0 G" [! y gularly normally in a continual sequence.# G3 ~( [. q0 _7 F, Y# d AMPER, A device for slowing down or limiting # C; z1 d t; DDASHPOT A mechanical damper for slowing down 3 j* ^' p4 a& D5 U1 J0 P2 h1 |ovement by restricting fluid flow.# y( j, t' R% |0 Q D 5 F& P; h0 y- T+ [2 Z8 VATA BASE, Stored information which is used as the2 H7 d! R/ U$ Q# Y1 ] ba 3 ~& `* e- G" D4 F& ]- a% [7 kDATA BUS, A conductor over which digital data is .1 q1 s; U' t* w6 H9 f transmitted. & N* F6 E1 |" rDECELERATION, To decrease in velocity.8 ?1 c( Q1 ^1 s 装置, ) N: N+ w* }) e8 z- t4 arive4 [3 Y1 S4 A2 o7 v$ t re( ~/ ~* a( w5 Q: | D . n t: T B- Z2 a* @! AD1 @8 S- ~: m# S1 Y. P movement.4 m3 Y7 J& ?$ d' a8 U" v m0 U' |& J/ o6 L3 @( }- l0 V* o ATA, Another name for information. - c+ v$ Q' K$ o' c; {/ C" tD ) ^# n5 j$ p- Bsis for computation. , u$ i X9 v4 P- P ?恒速驱动3 Y8 b6 F* ]- C 见Constant Speed D .* G; p8 d# `: c2 E3 l2 G9 N0 T) G 期,: V+ `- c4 i* s; ^ 不断重复发生的事件的一个完整系列。 % Q8 g: z/ D0 ~- z0 v! o尼器,0 j! B5 ]. n) u; y5 t% z2 G 慢的一种机构。 5 M' a, k+ w4 n3 V) e$ F1 x e7 ]' Y& e0 H$ u* a 用限制液体流动的方法以减慢物体运动的机械式阻6 O, e0 x4 ~. ]3 h' ?7 o! D. Q1 m. P, m: w7 T) j* K% O# X9 A; O) M 料的另一名称。 f6 t/ F* b7 `" C {3 f( H 据库, , q# x2 {" V2 o k, [* p- n数据总线, y) Y9 P% q" c) x5 c6 ~一条或一对导线,用来传输数字信息的通道。8 y) {1 V3 ]: F, R 减速,1 l6 g4 d( K7 G+ g- V9 _# O {: w) @ 速度随时间的递减量。' v4 g9 W( w1 E; T& `& u( s 固化,& w, ?8 T) I# ?6 ^ 树脂和纤维部件内化学反应使之成为固体的变化过程。# n" y2 P: S$ [3 T9 y* d2 y6 l5 c; e( R$ f C7 g" w; M4 n3 B' V- \ 用来使运动减/ K t: I7 y3 ] 冲器, 1 a% O$ q; w: }" `' U器。 + a$ D6 g* s, i' E6 R( E$ U据, 2 E4 o8 E5 d5 [, D5 i$ b: s4 R, r% n4 D8 O3 p) `$ |( K储存起来以便在计算时使用的资料。8 B8 {& i4 K x) r% w 英汉对照民用航空词典B OEING + q& S. F) v# W; lTECHNICAL DICTIONARY 40 % g7 P- l3 K5 gDECIBEL (db), A unit of gain derived by computing the3 |# m$ R( g z tio of input power to output power.3 \8 A3 ^6 R" }% I ECISION ALTITUDE/HEIGHT (DA/H), A specified/ `/ g1 F9 b% U7 Y+ g, V ltitude or height (A/H) in the precision approach at8 W- V& G! X. C hich a missed approach must be initiated if the7 [. f, K& v! V, L ECISION HEIGHT (DH) 1, With respect to the * Z/ r P- G1 A+ I' n! ~, \proach or ], f3 k1 V) x pexecute a missed approach. ' s, D l1 s' F6 O" C- G5 i& wproach to trigger the decision of either 3 F6 ?( `1 i( l* }; Y1 K7 f4 e7 Znding or go-around.( s2 g0 e ], W* l) Q9 x& P ECOMPRESSION, The loss of internal aircraft air) [- C d& r! {2 Z s ressure. 5 ?! M5 X* W. I8 ~E-ENERGIZE, To turn off or cause to not operate.. q2 [( o. Q$ _. C$ M' X K rom the tanks 4 }: g5 i3 M* H$ eusing airplane fuel pumps or external suction. ) U; M$ X3 x5 L X f# t( S算的一个增量单位。分贝 {, W, v, I Z5 o 常表示两个声音信号或电力信号在功率或强度方面的) i5 k* |' v4 {% S: X8 \2 x 对差别的单位,相当于两个水平的比率的常用对数的十5 q6 D+ w5 [$ t 断高度/高(DA/H),& X4 B1 F: d9 `6 R 在继续进近必需的目视参考没有建立的情况下开始复- D0 }3 d3 K" a9 U 的精密进近中的一个指定高度或高(A/H)。 ; T1 f0 g1 e# T断高(DH)1, # _+ q K+ J7 c( O; N! B操纵而论,指在使用仪表着陆系统或精密着陆雷2 W2 F* _( \7 ^; c, b# J/ g# \- t8 a 生继续着陆还是复飞决定的高。 0 t# V9 p3 w7 y' S% G2 p飞机失去内部空气压力。 : b. R: [& c# {, k: a1 W开,3 V- Q; r3 I4 w- H4 E% d! t' ] 关断或使不工作。 ' M. p1 f! n* p- I: o3 @机的油泵或外部的吸油装置将燃油从燃油箱排1 y' e* j& ~! {' c& j5 [3 H5 [ r 出的方法。1 D- }+ V1 S- X" D ra+ }, A4 m- |2 Q6 f D % I3 e3 g: |' h$ d2 Ha* ?) |& [/ t% G( N; v% s w" `1 P7 p) Q' z1 S8 l! W6 | required visual reference to continue the approach has( ?2 ]4 i; I# x# v not been established. ! P% c, d, u, D9 ^9 n( n4 DD 1 {$ `. E3 Q# Y3 ^operation of aircraft, means the height at which a * a* D: g" K( j6 q mdecision must be made, during an ILS or PAR3 C, j, D8 A# P0 F. @" G7 T2 P instrument approach, to either continue the ap 0 g: ^6 w; {; }& g; l4 h; Wto ' R: |* B- p6 _" \DECISION HEIGHT (DH) 2, An altitude used during a! x! s8 m3 b; |6 J# ] precision ap$ \9 |& M' u; Q5 z+ @. N la ' O5 B M/ n4 U9 f. YD; A9 q$ Q) D+ |& C p * c+ s6 c7 ^9 t1 vD 2 \0 f1 W5 w9 l) |& s1 fDEFUEL, A method for removing fuel f4 Y3 L- }+ B5 m* X+ V- j 分贝, 5 \' e* u6 M* \' o以输人与输出功率的比率来推 ' p7 ]0 x% U- G* \, R: w6 a; ]8 a8 U" R% g( ~6 `/ G+ X# ~# K+ @. ^3 }+ T, J, r5 s8 T6 S3 f' c6 G0 i4 l- e6 m L0 P; j) P0 w" V2 u' Z0 P/ g" |* r5 A( s( W+ o, p* i/ k. ~) Y 就飞机 . x% Z* _* d' T% W6 n6 [& h达引导进近时,必须要作出的是继续进近,还是中断进场$ j5 `! x0 q' p7 x) o4 Y, [! y 复飞决定时的高。 / h0 r) a1 x! }5 Z! l决断高(DH)2, " U. ^$ `: ?8 B, f, J+ F; k' |; ]精密进近时产 l( K1 v0 l3 |3 u9 I: ^失压, , J+ G) G8 G9 s9 M# B" q/ M# u$ r7 f& g' ]& g+ ?排油,# w% [( I' C6 @ 用飞: ]0 Q; c5 Y5 L4 U) L6 W 英汉对照民用航空词典B OEING # }; D/ P+ y4 I; q2 q# gTECHNICAL DICTIONARY 41' H! j$ W* z+ m" U3 b DEFUELING VALVE, A valve in the fuel system for 1 E0 s8 J: |8 o1 x4 D: ~" r* |" Oefueling the tanks and for transferring fuel between the ! M% Q+ G1 k; WE-ICING, Removing ice after it has formed on aircraft.7 U& }$ `( t, x+ o Change or difference.# K4 a5 Z j, h, ~* e- b. N EPARTURE CONTROL, A function of an approach% U# |9 K0 @; L# ~0 d/ } ontrol facility providing air traffic control service for) F+ l( ^1 r, d* {+ p eparting IFR and, under certain conditions, VFR4 T B; t' R/ c5 W; M EMODULATION, The process of retrieving information- E! {3 S/ d0 m carrier voltage. % ~ o+ x1 L1 ~" J$ A) yation./ P1 t3 l+ T( |! g lic * f7 C$ E a" l1 h; p8 hcreasing hydraulic reservoir air pressure to2 ~. @- y' Z K3 @% x, r mbient pressure. ' I2 U- x0 l4 G6 M: p箱排油和在燃油箱之间2 W1 g/ z4 p8 M) Y% B: o4 u 送燃油。 4 q7 v; o' h5 l, [. M- d7 Y6 x冰,0 o. W- ^' @9 y$ L- [) p) ` 除去已凝结在飞机上的冰。 ! U6 Y! w" ?4 q( P+ H& J删去或取消。 6 A, [1 Q9 U2 b8 |$ h量, * d% X. a+ w" i3 \0 W, C变化或差异。$ [3 M" u: L7 Q* | 场控制, / U: R# e4 N2 I `& I+ D给用仪表飞行规则离场,和在某种情况下用目视飞行 . C7 l% {. U6 ^1 O1 g5 H则离场的飞机提供空中交通管制服务的进近管制设施 ' A% s1 i; n9 L! w1 R$ o9 w0 U0 ]4 r$ m- w 调, : v; h1 L+ t; Q0 [电压中获得调制电压的处理过程。" P1 W# |0 V( v 环境2 Y$ b* b! ^# Z: ? 力相同的活门。2 R, F: i/ Z: L/ I; q1 i, G' W7 q d ( a3 O8 c% T6 I4 ]* ctanks.* R) t% r. P8 |, ` D * O1 K0 w* J8 e8 rDELETE, To remove or cancel. + G, X& w! L. K) e9 Q$ B# PDELTA,( v; j6 p$ N- T. C% p2 \1 u, h D * k$ S( B3 U# J: \/ wc* Q `( R2 b& k& G0 W/ e" F d 9 s- k8 _1 U5 L6 `aircraft. * {3 N2 h' W% o* PD9 s! J) {: }) x7 b (modulation) voltage from a modulated # T% H3 b/ c( C5 M' s! [DEMODULATOR, A device or circuit which performs , M2 l1 J, W0 r7 Z! `/ s1 wthe process of demodul + h* s+ \9 ]) H5 y- zDEPRESSURIZATION VALVE, A valve in the hydrau, ^/ \& O% R3 p! |0 A- r system for de - W& p5 g8 C" V" s! t! n3 r5 z4 Ka7 _5 C! Q3 D4 C0 {2 R3 q 排油活门,: G- w5 Z% s0 ^" d6 _ 燃油系统中的活门。用以为燃油$ c2 d# f A b+ N7 ?; h# V) d. o3 U+ Q! i8 r$ \. J) q/ p6 F删除, 4 v4 O1 X* C4 o4 o0 g' E9 P J) U5 `8 k8 R- e6 \5 I V+ w4 y0 ]" n7 `7 r9 \- D9 }, ~% B3 i) h) Q" F. c# Z% ]' i, ^的一种功能 - L9 Q# K$ K7 g6 a. G2 O/ U: D3 K5 E% i+ B( V& l- P从载波 2 ~" ~; A1 O% F解调器,$ j5 U* x* y/ C 完成解调过程的装置或电路。 + {, i' |3 a F% b2 @" \减压阀, 8 c, W% v$ S; |: T9 K& k9 Q9 Q在液压系统中,将液压油箱空气压力减至与周围/ i; @8 j1 u8 W1 R: m9 Y; `2 z) w# s 英汉对照民用航空词典B OEING 6 i$ Y1 \% V2 {" B5 K6 \TECHNICAL DICTIONARY 42* o- W( z" E* L1 u! e% V: ^ DESCENT, Phase of flight where altitude is decreasing. 8 o, q: W" r6 }5 G& Z# u, YETAILED FLIGHT PLANNING, The calculation of fuel " ?$ p4 O( c1 s2 j5 dnd required for a trip by considering each phase of " S/ u! T S3 @2 u9 ^8 C0 y" Uight (climb, cruise, descent, reserves).8 V4 y4 @% L* Q. N al or1 \# {) M* E; U! h+ { ETENT SOLENOID, An electrical solenoid used for1 u! K# t+ t3 h/ } F t.9 q& t `7 P' `, ? specified course or, x4 X- S' e' Q* ~5 Z4 J. m rocedure. + U! f4 Y) N0 Z! j5 }( D1 se.* i1 z9 f U {/ h9 |% W5 b* X 飞行计划, + j4 h$ c6 h: ~. Q* }) Q将航班中的每个阶段(如爬升,巡航,下降,备降)都 ! v! @* e& f r- } K4 L' M人考虑,来计算该航班所需要的燃油量。6 j$ { u% Q7 ]& e |; U$ H8 T 用来感应情况之正常与否的电气装置。 ! F/ q) l* C( g1 ^1 ?定电磁线圈, " p7 Z5 B* O5 Q Y9 e4 X- g+ ~, C出接通的电磁线圈。 4 \; Q4 C8 n; Y1 ~/ F! S. ~) A2 s* q差, 1 e* `3 P8 r# B与指定的航道或程序之差。 V/ x$ K2 ?8 R6 h8 I6 d( E, Y 用气压或液压操作的活门机构中的柔性部件。. ]( c5 m" l" Y' s- u; M- v+ B5 F D, j2 M8 y7 V& G4 W a ' B* @" m \. |6 ?4 ^% e Rfl 4 X3 V; J4 n8 @- H% W. kDETECTOR, An electrical device for sensing norm+ T# @6 | m0 E; l+ Q abnormal conditions. 2 g8 G3 F0 w+ U! i1 nD% I! Q9 Y& m: i% J, g: u controlling the engagement of the actuator outpu , h; x6 {0 G( N) I" c; V9 p8 @DEVIATION, To change from a 8 C, c# N" X3 V) u- g |- }( Lp: E5 \) p) h7 I# { DIAPHRAGM, A flexible part for operating a valve/ |3 D" s: N @' Q5 j8 { mechanism by pressur % g4 D+ p, ^- W8 d9 l* C下降, , y* u0 c8 p$ k6 p6 x飞机高度不断降低的飞行阶段。 : \, o" `# i1 A) J+ D) p" G w详细' h6 X& e& U" l/ a+ |- _. J' X6 h: B6 \- r' R3 S探测器,6 W3 A9 b/ O% @! [$ o/ V9 r1 F1 ?. X1 o/ s6 [7 ?7 t$ n$ H0 ^1 B" C用于控制作动器输! _& m7 |( ]8 R. [$ v0 |* A6 L% D! z' A$ {, Q9 a 隔膜,* d* V: J3 B3 C. H- R 英汉对照民用航空词典B OEING # S& j1 b9 X) ~0 j! |TECHNICAL DICTIONARY 43 4 N6 o% X/ R( r. w( PDIELECTRIC, A material which does not conduct 5 c5 p9 O; y2 T. selectricity and used between the plates of a capacitor+ @% S6 w8 P! J8 b5 Q (condenser). 7 l+ h+ v; j$ A) t" _ |nother pressure in the same system, measured in " [2 y/ k+ S& Z) x6 |4 Kounds per square inch differential (psid).& w% Y0 M* }) p6 h+ U) r IFFUSER, A part of an engine between the - V0 Y) j4 A. {+ Bompressor and combustion chamber for reducing the 9 N0 n7 s2 a! v G) Bair pressure., {( \* ]1 @6 V* p) o igh # X R" P6 i' E* C* jpulses.( E2 h. Q3 F# k' u! E ignal that is a close approximation of the original * N" r+ {8 a" T' J5 O) Tignal.; ]4 G, ~8 g+ K6 Z* t* S IHEDRAL, The angle between the wing reference, E3 x# M& L% o+ j4 _. j* w lane and water line. 0 b0 X( }/ U( E' W. K的压力,以每平方英寸4 B* N) _/ P; V 少磅压差计算(psid)。& n7 G5 ~. O% e$ w9 v, q3 l& q9 i5 n) Z1 E 散器, 6 H% Q8 C) {1 V. U* E2 e发动机内压气机和燃烧室间的一个部件,用来降低空 2 \" W, S3 W% H& ?0 B. y" x! N$ s增高空气压力。 / }3 C! _6 u5 r9 e, h+ X% g换, @5 i; u% g! i- H7 i* K 的连续可 3 J* X+ t0 N8 l2 S1 k(模拟)信号的处理过程。 P' a, C& G9 @; ?( h- ? 反角,( Q/ I! e, u% @3 U 机翼基准面与水线之间的夹角。 $ C+ I# a& H4 H" d% r: ]! XDIFFERENTIAL PRESSURE, Pressure relative to5 b% i* F2 n7 ~ a ' K* F3 `* N- Dp* t/ K7 }- A2 a' d ^( d D% O* P5 v" A5 [8 w c! J" N0 S, g0 B( X$ i' n/ E airflow speed and increasing the& x2 l& q7 T- A* f1 w% e( z. i DIGITAL, Digital refers to a signal whose amplitude+ s7 u @9 ~) Z6 p8 U5 C remains constant for a finite period of time. Digital4 z0 f6 S' v9 Y2 `# v+ K signals are commonly represented as a series of h $ B7 v6 Q$ R# R( \! hand low3 y5 c# `$ e1 O; O4 e/ o6 }, ^ DIGITAL-TO-ANALOG, The process of converting a& l# E5 x6 q- T. ] J' i- F: i1 |( D digital signal (binary) to a continuously variable (analog) ! A, r: [: u1 j0 |s7 m) b& v. [# v4 t- I! L, j s% B# Q* {! ~+ ` D 1 ?+ Y, t9 f3 Y" g% ^: ^4 Cp + p; l/ N. v U% s. H& Q3 Q! [电介质, 9 X1 {" G/ M. E# j# [一种用于电容器板之间的不导电的材料。 ! ~4 R6 q$ T$ J: N0 Z; v, K- C压差,7 ^0 k6 T/ Q0 D _0 ]- K1 S 相对于同一系统内另一个压力 q. { H5 A. a2 c: i$ g; v: o# J, r, R! k& Y1 c2 d. o. ? 气流速并1 F( r( w5 B6 d( b; j h 数字式,% z0 _( {( s8 V 指一种信号。该信号在一定的时间内,振幅保持不变。; }7 D2 a! i! i) m2 r9 [9 {1 Q 通常由一系列的高低脉冲表示。$ q1 V9 j& Z+ @ 数一模转9 Y- K) J9 C7 ?8 }9 V$ Z 将数字信号(二进制)转换成与原信号相似- h2 d! ~" F. f) G [0 A4 w' _. T8 r* f j5 l5 o Q. v$ b$ l" m, L/ q3 s英汉对照民用航空词典B OEING 5 p3 r9 j c' Z' q) FTECHNICAL DICTIONARY 444 c# k5 q' V w$ K9 Z8 G DILUTER DEMAND REGULATOR, A component in the : h) h% [6 P! z9 dcrew oxygen system which mixes air and oxygen and 0 ?0 G6 M- _$ R& I1 b. Y. R0 ~upplies constant oxygen pressure even if there are 2 N, C; x; k- b6 u. a- p) j0 _hanges in ambient cockpit pressure.! O1 A8 @8 }2 U7 e' P IM, A word value of light. For light control devices - dim6 | N, D) f4 i5 Q. f4 c7 { the opposite of bright.# t4 A5 y8 g: ~% i R0 c! e- ~ IODE, A device which allows electronic current to flow" z1 t: }) d& ~* o9 D* Q only one direction 4 E1 l* I! }# Cuid in a reservoir.) G B& _8 h9 T( O% c! I3 ]5 ?0 G DIRECT, Straight line flight between two navigational' T/ }+ { G9 S8 _% k3 P: _" e aids, fixes, points or any combination thereof. When , \; I) ], @4 B) aused by pilots in describing off-airway routes, points ! X" ^$ u3 Y$ g& Udefining direct route segments become compulsory 8 X1 G, h0 [" W0 P( Z5 F& ereporting points unless the aircraft is under radar 6 i# [8 ], t% Ocontrol.( Q0 t9 l/ s* S0 Q- h 节器, 9 t: }0 H/ Q3 ^3 Y+ \9 n0 q将空气和氧气混合, 3 O( U. w/ A F- j8 _4 m: ^使驾驶舱环境压力改变,它也能提供恒定的氧气压力。 ; z$ l' r) ]% L9 Q/ K/ Z+ b0 ?3 v. ^- _9 z: W. ~% Q1 ~' {3 @一个形容光线亮度的词。对于灯光控制装置,暗的反9 \2 d# N! u8 J4 T! h9 P& i v 词是亮。8 s, C# f& `: Q$ S+ C: @ 极管,- W1 U9 s! }6 o 只允许电流向一个方向流动的电子装置。 F9 Q9 ]. b6 y+ } A' n) v" y. R器内液体的量。' ]. M3 {* |4 @: x+ S" F } 直飞,- j% X# Q. k- m8 d- { 两个导航台,定位点,导航点,或任何的组合之间的直5 X3 k/ L7 C3 K2 A& R) ` g/ I F 线飞行。在被飞行员用于描述偏置航路时,除了在雷达控1 _" P# `5 p" } 制的情况下,确定直线航段的导航点成为必报点。0 j/ q, Y3 J9 g s 1 o, _: k# G$ s. R. Pc6 v9 K/ [7 \; _: u; b' U% u2 v D 0 o- ]' G& K+ I, N1 mis3 s$ @0 r* ~* M0 ^; i D 4 F5 d; s) ]( Min) Q" m. w$ s$ O0 F- X' ?6 M+ t DIPSTICK, A calibrated rod or stick for measuring a( F+ X( O3 h4 v; j quantity of fl" ^8 i3 ?+ j) a% G# B( q0 Q 稀释氧调: `( [+ |% _* ~ D8 S. e; ` 驾驶舱氧气系统中的一个部件,它 + a! _: r$ C- q8 P: L+ O5 l! y, s. m' p# h# W+ ]( Z$ H( W( w. [7 B' D2 i3 W" Y+ V5 t! e* y2 P) O0 J7 E d量尺,1 Y m5 U6 t: i5 M7 c$ I. P8 Z 校准过的棒或尺,用于测定蓄液 N9 o( C4 J: h" M7 T英汉对照民用航空词典B OEING, `! U7 h4 `, M, _ TECHNICAL DICTIONARY 45

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