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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( E: H) r/ J0 j, J: S 民用航空词典 5 a( t( n0 U ?& X6 u# e波音商用飞机集团 5 m! \. f3 f# u! b& ]% f% kBOEING COMMERCIAL AIRPLANE GROUP : Z: n; |0 x% m) @英汉对照民用航空词典B OEING $ _7 [5 L- Y" h, mTECHNICAL DICTIONARY 1 4 g% _( p f6 m# IA5 A% T- `. H8 c C' L/ \) \ ABEAM (ABM), Beside: An aircraft is abeam a station( A+ @! b5 {9 A when that station is 90° to the right or left of the track of9 z# Z" ~& O+ k the aircraft.% B- g& C) Y6 Z! P6 N ABSOLUTE ALTITUDE, The actual distance the aircraft! O; H: m9 f& z0 z6 Z. f' P/ Q is above the ground.$ q: J$ A& a0 H# M! l; D% G/ \ ABSOLUTE PRESSURE, Pressure of a liquid or gas2 i1 m9 D8 r0 k. ]: S2 a& l) \# u measured relative to a vacuum. . B$ W& l+ m+ W: D! t9 m5 fACARS, SEE - AIRCRAFT (OR ARINC) REPORTING- C. a& Z: @# U# V ADDRESSING AND COMMUNICATION SYSTEM6 `! S: z7 ^- {0 E8 n8 x2 R3 y+ m ACCELERATION, The rate of change in velocity with3 f6 x" b j' d) T$ R# u: k respect to time. 6 `, [' O& B1 J% L \& ?0 i1 Y& oACCESSORY GEARBOX, A part of the engine, 2 y p( V& t1 K. k: Xmechanically driven by a compressor or an angle E2 e9 i& ^( w, P9 A2 wgearbox, for driving components necessary for engine . q$ H5 E( a+ @5 j' Q. U- \正切, ! Y8 a% d- T2 v1 j5 m8 g1 Wand airplane operations. ' Q+ m, v1 L6 N- t* a* n0 b当电台在飞机左侧或右侧方与航迹成90 度时,飞机正 : ]$ [( T' A) Z( \9 n% k+ x' v+ r, Y切电台。+ f! {+ x, M( ` 绝对高度,8 J2 a0 m, a q1 U& Z 飞机离地面的实际距离。 2 I/ m5 j1 ^+ `. T' T( k6 R绝对压力,+ h9 J+ y r# V9 O( `: N4 k2 {; B- E 相对于真空(无压力)测得的液体或气体的压力。; r0 u0 j7 n$ ?/ Z; v 飞机通信寻址和报告系统,# k" R" g5 i1 G, O0 W O' s8 q1 i 见Aircraft(or ARINC)Reporting Addressing and# d# U- q+ ^0 z Communication System. 1 j3 m% g7 G. q/ S5 Y4 C加速度, 6 T2 x% |! V- |+ H( O随时间变化的速度改变率。 Q8 u6 n# c( F# \: C% d 附件齿轮箱, : Z! ?3 a" |1 x% R2 O) Y8 y发动机的一部份,由压气机或伞齿轮箱带动,用来驱动$ J- A# }9 g7 p5 X8 h3 | 一些使发动机和飞机工作的部件, e9 A: B: U0 g7 `2 t 英汉对照民用航空词典B OEING; M% F: s0 u1 d! m) b TECHNICAL DICTIONARY 2; _/ C) h" J/ O6 W4 A7 K* J0 \ ACCUMULATOR (NO. 1), A container with hydraulic 5 J0 Y' S7 Z6 F9 kts when normal hydraulic supply is not * Y/ L- Q- m" P! z8 E" i/ Kvailable. - y9 ]2 C4 L7 t1 P; MCCUMULATOR (NO. 2), In a computer, a special ( A4 K& s. R6 f1 U6 C7 ptorage register associated with the arithmetic logic unit,& I1 f: n6 ^0 C olding the results of a computation or data ( X* S- q) |2 c5 y0 d" sACTUATOR, A mechanical device operated electrically, * V0 h) s! N. a: ohydraulically, pneumatically or mechanically for, j" \2 N. S$ O, _ transmitting motion between components.! R9 L7 R3 |8 O ADC, SEE - AIR DATA COMPUTER7 E: K) u& _ P" ~- U: a, f ADF, SEE - AUTOMATIC DIRECTION FINDER1 y# s+ f6 W1 D; h3 H8 H& X ADI, Attitude Direction Indicator, An electronic display of $ r+ ^* q4 @% v* N2 a9 tairplane attitude information in pitch and roll.9 O" O4 ?& R2 A) u6 w 蓄压器(NO.1),; X: U% o: ]3 B" f/ S 含有靠干燥空气或氮气增压的液压油的容器。当没有正 0 n2 I- M% }+ M H- x. k# q常的液压源可用时,该容器可用以驱动部件。/ k. ~' T& I: A0 u- |8 C 存储器(NO.2), 4 u, {2 H/ z8 k* h计算机中,一种与算术逻辑组件有关系的特别存储寄存 ' v4 p' I( g% P# l% z0 U8 _器,用来存放运算结果或数据传输。 , }# y" @+ t; u飞机状态监控系统, : u+ J, l$ s4 A& f3 l8 k% y见Aircraft Condition Monitoring System / i' j& W6 s3 E) F. P2 sfluid pressurized by dry air or nitrogen for operation of 0 R0 E" T* Y$ b' s5 dcomponen & c% H: {1 W# ` q! Ta& h& Y* F1 z P# p A : i- C/ p8 g8 h0 r+ u: os: X V- {$ L1 w1 P- O used for h # {( T3 n; x2 O, p8 K) G; Ytransfer.; L, o( q; k9 V6 ~) Z ACMS, SEE - AIRCRAFT CONDITION MONITORING 0 `0 _! H' c% p+ Y R- R; s0 uSYSTEM .* i& F6 V7 G* n/ j% q 作动筒,* d$ I, H& `/ d7 {1 X- I 由电,液压,气源或机械驱动的机械装置,用于传送部2 i& ], Q, U J7 F' O 件之间的运动。 - U$ P2 B% _. g大气数据计算机,. Y& [; ^ l! D! l& [# ^: j, _ 见Air Data Computer. 3 \; W; X' S2 [8 t; ~3 S自动定向仪, ; K' |" \3 ?# a8 g1 D) w见Automatic Direction Finder.3 q# w2 ~! M" w. W: z 姿态指引仪,5 t, ]- s% I5 K( _ 用来显示飞机的俯仰姿态和坡度的电子显示。6 |. p) h9 E& X) M 英汉对照民用航空词典B OEING4 V7 _' F7 z1 @- a5 A TECHNICAL DICTIONARY 32 @9 R( U4 b" N$ q AERONAUTICAL RADIO INCORPORATED, ARINC is4 R. W. [2 n' C, j$ }# H , & C# \$ T/ V( k! ` @: _nufacturers, and foreign flag airlines. ARINC" F: j; O' [% Y1 Q evelops and publishes standards for electronic1 s+ x z# y s9 C) Q5 B) b1 w quipment and systems. 6 f; k1 ~ x8 ^6 E" s5 [GILITY TUNING, The capability of the DME to 4 W. @; G3 P {* l; F' H) Clternately tune between two different DME stations in ( G+ U6 T: P+ D$ l: r, @rder to get two distance readings from one" K' m6 ]+ Q2 ]$ c5 n terrogator./ j' E( m" I) m5 \* ^ ge" w. }* d, K9 ?" |" w! G ILERON FORCE LIMITER, An electro-mechanical% `9 A8 K# U. l# p% R% a, [+ j IR CLEANER, A component in the pneumatic system0 Z3 I- V% F5 |1 D- g upply to the air 1 A5 P3 ?- p6 `- Z0 z8 i! Y$ E* a( Monditioning system." n4 a8 i3 S2 ~4 R9 _ 订并出版 F* J* I& F6 c7 T* m o( Y子设备和系统的规范。8 f9 ~4 S) C6 j/ x4 ` 快速调谐, ' |$ {1 H8 O4 H机载DME通过交替调谐两部地面DME电台以测得来自 0 K/ w$ M! v+ ^3 m# X* B* s同一台询问机的两个距离数据的能力。 i( H3 J8 ]" q3 P: a 翼操纵力限制器, X3 q* \0 E- [8 \装置。在自动驾驶工作期间,用来限制驾驶盘 ; P3 ?% t0 I2 J气清洁器,9 B7 ?5 Z( S6 y0 P( O W 部件。用于去除供空调系统使用的发6 Z$ _' K3 _0 Y8 k/ p0 g3 h/ ?( D a corporation whose principal stockholders are United6 i/ M2 Z* ]7 V States scheduled airlines, air transport companies ' `' D- ~0 `& M5 U: M' d8 aaircraft ma 1 ~# Y' u% P& }; T' A4 yd# ], H. P/ I- L2 [ e 5 |. N4 T2 q" ~1 ~5 e7 SA , d; d2 J L4 \; q( C v5 Wa 3 T+ C3 s2 ~9 X9 u, z9 co 0 }7 M3 z' B+ z: hin' J) c9 p% ^# a+ e2 y. w# C AILERON, A hinged moveable part on the trailing ed8 j: @7 ^% G( ]9 \. _4 \/ \$ P of each wing for airplane roll (wing up and wing down). ? e/ `4 e( n0 p control. 2 j* m9 P5 }. Z7 d! X/ GA* a6 {0 x( O, z8 C3 u9 W w device for limiting the control wheel movement by the) w% L+ n8 [' p/ r- g ?' f autopilot during autopilot operation. % H c; { F4 @) N5 qA 8 E$ v/ N( |4 ?, bfor removing dirt from the engine air s+ D" V% e/ h, R c . E/ C% ?( Y; i9 O# X航空无线电公司," F' L. \9 [+ O8 w6 O6 z H: }( k 主要股东为美国定期的航空公司、航空运输公司、飞机, Q' G5 F" _* a" [, i; s" u 制造厂和外国领队航空公司的组织。其目的是制! |# \- Y+ E, _6 [ X+ Z6 k4 Y0 |& G }4 h* k副翼, + g. S4 [1 l% [ n+ O铰连在每个机翼后缘的可动部件,用于控制飞机的滚转+ Y w5 a! r$ K+ l/ Z/ Z0 F4 B/ v4 M+ G (机翼向上和向下)。( s# E5 N6 `$ m7 a. o! \7 c- B, _! v d一种机电 / S7 ?0 [* E4 V1 z; ]的动作量。' J X, F& r. h$ e& l- n: m( @) L: W! b5 i4 G- e% ^ 气源系统里的一个 * l) h3 ~% w( T- J, T, p8 Z动机引气中的灰尘。 ) U: E8 ?! J R6 S. r英汉对照民用航空词典B OEING ( @/ `. A$ R/ {& t6 y' v* v' GTECHNICAL DICTIONARY 4( h# @- Z# ]0 R' c' C AIRPORT ELEVATION/FIELD ELEVATION, The # v/ W0 _( u9 j9 ^4 Ghighest point of an airport's usable runways measured' W4 B6 J0 }! b) m in feet from mean sea level. In a few countries, the, Q. C" ~5 O/ g% y airport elevation is determined at the airport reference 5 l, j/ s9 b( R/ Q' lpoint.# n; }& g6 E$ f AIR ROUTE TRAFFIC CONTROL CENTER (ARTCC), $ c6 |' M0 W' m3 d5 [) h7 dervice 6 O* F$ ^9 B) i, O/ Tase of ) b1 _ E+ W9 ?% ~us flow of air traffic. 7 @- N: m$ D1 KIR CYCLE MACHINE, A compressor and turbine on a & B9 l6 Z% _# \7 Kommon shaft for cooling the air in an air conditioning( ?/ O, x0 |7 y' f' C ystem. The air is cooled by expansion from high to low1 O$ f! h A! e, _7 d% t+ Z: E/ Q ressure across the turbine. The compressor is driven / u/ z7 M* t. s5 }y the turbine.8 b' a% W$ I$ f; z8 ?' L 中航路交通管制中心(ARTCC),5 C. H4 U# s, a% }% a2 A5 i 域范围内使用仪表飞行规则飞行的飞机提 - |- {$ ^6 _' v& o管制(ATC), 7 H: l0 B. s& {1 ]7 M. v- z涡轮冷却器, , i4 S. g6 @6 Y# @; V, _2 X是装在同一的压气机和涡轮,用于冷却空调系5 r6 u9 `9 u+ D/ w+ a- X2 z 统中的空气。气经压气机压缩后,由热交换器移去热量,' R; a: z; V- r! Z% O, Y! | 然后经过涡轮令涡轮带动压气机。通过涡轮之空气,温 ' Z" u, { Q7 ?! {6 j, G5 q6 T$ o度下降。4 y! D: b" j* s v5 |0 D, C A facility established to provide air traffic control s' z2 C" `+ |5 q: s* G7 A to aircraft operating on IFR flight plans within controlled 1 w2 S8 }; z4 F2 t0 T! m3 Gairspace and principally during the enroute ph9 l9 s+ i8 q, l- r: M5 n flight. E% ^' n. i1 KAIR TRAFFIC CONTROL (ATC), A service operated by4 i7 z6 u7 f& b& A% C6 z, i appropriate authority to promote the safe, orderly and - o. x( {, G: O" W6 j9 qexpeditio; R I4 [( |2 ~) I4 @1 K# _ A 1 O( S" g" u- b4 K1 h+ H E* a; Fc w% |7 p* H4 M) r0 |3 O! Ts+ A7 _* |* \5 F9 n; P. O6 p p 2 Q9 A/ x5 R9 B( C3 w0 hb8 @+ V5 N9 N9 _* e 机场标高,0 i/ Z" `0 z: r. Z: t: { 指海平面与机场可用跑道最高点之间的距离,单位是英. \; y) j8 P7 s) I% ^ 尺。有几个国家的机场标高是由机场基准点而决定的。 / x! Z; T0 @) T9 i0 U( L# V: G- X! T7 x7 Z X% p% @给在控制空+ \' x A( w$ t6 a6 k( r 供空中交通管制服务的站台。, `8 X) N" Z# h& t7 H1 K7 X4 h 空中交通 # P3 P6 q3 b& _5 _! c; G由有关当局管理,旨在促进安全,秩序,和效率的空中 3 y" [* i9 Y$ X% Q: {/ _& [交通服务。) J7 w7 V8 h5 |! ^ 根转轴上# Z- l0 {- o+ k' E# A/ p7 r6 M$ t; Q1 S! N6 D0 j3 y" g4 R5 [6 f3 D' l0 z9 M" d 英汉对照民用航空词典B OEING' w1 J3 a b) j, [! S 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 produc) O# n: H8 P( `7 Y. ]" D data information, such as altitude and airspeed, based % k8 O6 i/ o: z1 r+ W6 }on pressure and temperature measurements.( p5 @ R! w% Z" C! P! @ es air. c- j+ [0 }! Z; K IR TRAFFIC CONTROL, A system comprised of1 h! Q; N9 q1 N9 g" K3 Z round and airborne components used to identify, track 0 o2 K/ T5 E2 J B; P# _1 i$ R: }OUND SENSOR, An electrical device operated ' X# e N* t* I& Qy the landing gear, which transmits on ground/in air # v8 q; M4 D$ `5 {formation for system operation in flight or on the 7 i) Q6 `* i! i5 S4 vround.0 a: X( z5 I8 s2 y2 y' K/ @ IRBORNE VIBRATION MONITOR, The AVM takes% c4 n0 t! s% ^1 p e signal from the engine mounted accelerometer and & O7 B; F$ j7 M7 f# s3 ^# K; d# Z+ Jalculates the vibration on that engine.0 D y5 L4 e$ D7 Y1 j9 k corridor equipped with radio navigation % d* t; |/ t2 K% Xaids. 6 G8 _ l# k8 j& E0 {& JAIRCRAFT (or ARINC) COMMUNICATIONS 7 i! ?0 L& U- I% |. N9 J. aADDRESSING AND REPORTING SYSTEM, An# `4 x1 _ D- i% y# E3 a3 C addressable digital data link system which permits the) P' S) I% S) k! N2 w- n8 o exchange of data and messages between an aircraft( z3 }' }2 v9 N8 q% b- r and a ground-based operations center over a radio * I# r. T( m4 ?5 \1 I( enetwork.! }/ f& T# G$ J- W8 k/ ^ AIRCRAFT CONDITION MONITORING SYSTEM, A 5 Q* {' `1 _; Psystem of sensors and recorders to monitor various ! l0 H d/ _4 W1 d. M9 jairplane systems' performance and status. " ~% p7 R7 v$ p+ m3 J. W! e机,: x: `- ~7 J1 \0 s 中交通管制, Q6 w+ K) t/ x- F" P 一个由地面设备和机载设备组成的系统。用来对飞机进 ' F% }0 [( f3 V" g0 G Y地传感器,- b: q2 o; w$ r2 j) N& W( i 一个由起落架操作的电气装置。用于给空中或地面的飞3 V3 h% \% U5 f/ M 系统运作传输地面/空中信息。(有些系统只能在地面! r4 D8 F: A" L9 j$ n3 F% m 用)% K$ K! h. s0 C( o, C# j$ n4 N 载振动监测器(AVM), ; q2 ^! w. h/ b& W) u2 qAVM从装在发动机上的加速器取得信号后计算出该发! X6 W, m2 D$ a. f$ ^6 F7 ` 机上的振动。 1 \# j' X: m2 g式建立的控制区域,内有无线电导航设备。/ H) \9 G7 T& v D$ e/ G9 g 飞机通讯寻址和报告系统, / ]" E% g2 }* P* m! d+ L! g5 G有种可寻址的数据通讯系统。利用该系统可使飞机与地* U1 e) G; O1 k5 Q 面操作中心通过无线电网络进行数据和信息的交换。3 |. R/ l8 f: `4 ~ 飞机状态监控系统,5 _% Q3 x! {& N# Y* p 一个利用传感器和记录仪对各种飞机系统的性能以及 |! A; U: g; E" G: b! N 状态进行监控的系统。+ e0 G4 h4 A- o) `" z A5 l. Q7 S4 ]+ h7 Q4 B g & }0 u4 c1 `2 W/ Wand locate aircraft. B$ W/ ]9 q0 M2 `& f& N" t; j AIR/GR . k, n* }% h4 R+ [0 rb 2 C5 z/ v2 J& j% jin ) b7 q! D# n3 j, U5 Dg 4 S ?6 I+ o h+ LA : T/ K% r. i$ M, z ? m6 o- dth . H, H B! H% p& n8 e; |9 m9 K4 Hc! ^* F5 T& d) [9 {5 _ {4 y AIR WAY, A control area or portion thereof established # W" P4 @# K* q4 G: [! ~3 X6 fin the form of a 3 M6 ^0 V0 e1 _3 U6 K2 k$ e大气数据计算 + T- \" ?3 Y6 `6 F/ a7 w根据量取压力和温度而产生大气数据资料(高度、空速$ D J: D8 x2 K' |) q 等)的计算机。 2 U+ {6 Q0 _$ [" ~) C k% g! n( Z$ @( ?5 w- M: W$ Q* ` }0 B行识别,跟踪和定位。 & N/ D4 ^1 u! m' P# j6 j6 ^: d% {$ ^0 m, L; R/ g; U' [& W! r4 a4 f& s } 使 3 Y/ a8 x" h0 \; L$ e! @' w/ Z( k$ L5 x3 D. y1 y& ~' R; ~/ E& | t" A- w6 Q 航线, ; ?9 y8 V- J8 A5 Q) |. ]$ }: `, f/ G, [以走廊形" i1 O1 p: p$ b; a+ j5 V6 A 英汉对照民用航空词典B OEING# g8 g6 [% H' U$ q3 S! ] TECHNICAL DICTIONARY 6 * D c7 k3 V1 [AIRFOIL, A surface designed to obtain a useful reaction,/ W5 S& G4 D6 x! A; U; t such as lift, from the air through which it moves. Wings,( x7 D5 k5 e7 T+ a stabilizers and control surfaces are airfoils. 8 @/ H j. \4 ]AIRSPEED (IDS, TDS), The speed of the airplane5 o" b4 a( `& e# ?8 ] rough the air.& A5 Z; `! R+ }+ U: |' w D INDEX, An adjustable pointer on the0 P F; |* J% `7 ^- `5 q; p irspeed indicator. 9 E8 P, R4 x5 X7 ~and legal ability4 M9 @" d/ @8 m ` fly./ P2 |: U4 m! U m, for example, the procedure for finding the + f. |+ H' P3 X7 H8 n- jquare root of a number. . J) v3 z9 ~. e. q0 _, [- X( Ly* k" c' k* y& b/ t* @$ J! l re, wind, 3 B W# g3 f1 p" w/ Qand aircraft flap setting.# k0 Z0 k" O7 e! b1 ?5 U 是翼面。6 n" k; X; u7 N6 G: p6 y' r 速, ; D2 |, U7 O6 F+ {- A7 C/ C飞机在空气中运动的速度。4 D9 e8 s* B, h! P3 A: g& i+ K( V3 x9 H/ P6 \: x+ b- Y7 @, J0 ~ 在空速表上可以调整的指针。 - y6 s% z9 {- A o" g( Y( m机械飞行能力、和合法性的飞机状态。- t0 h. q4 ~6 c: B( O1 T 一步一步的解题方法。例如,计算一个数的平方根的步/ L8 M4 z/ Z. \& c5 |+ K( t b4 `- w4 ^4 R- w4 Y5 a- R5 z8 ` 资料的法定文件。5 l: z% k) C! a8 f8 e 翼位置成函数关系。 & K. x' W l) s1 x2 xth. _+ c; W' s Z! h( q AIRSPEE n6 n- f" @+ `6 w. P+ Ea2 \- B6 t3 e k1 V AIRWORTHINESS, The condition of the aircraft with2 d( N* a" F: W5 G respect to its aerodynamic, mechanical, # F9 S4 z- w* Z) zto : D( F" G% ]$ kALGORITHM, A step-by-step procedure for solving a8 Y u2 ] V. ?! @$ v. M proble u' g1 Q( V4 W8 l! s, h% N9 Y' ` s6 T0 r) L' u$ P% a3 b6 Q; Q9 l AIRPLANE FLIGHT MANUAL (AFM), The legal , ?; ~8 ]* j6 D! m% wdocument containing performance and operating limits,% L; m" e, B* e ?' j% n" y! f/ E# B1 X: [ operating procedures, and takeoff and landing7 a# J; i* s. ?! w% ?8 F) N# {" I performance.5 r# S9 k8 ]$ U% J AIRPORT ANALYSIS, A comprehensive set of takeoff! ~1 w6 a* {; U( P weight limitations for a given airport runway, generall 7 g+ t* [% S) t4 K+ |: ^presented as a function of airport temperatu & s: b) p R6 ?! ] l c) ?翼面, 1 d: B ]$ j9 W4 V# r- P( T用以从气流中获得反作用力(如升力)的表面。机翼, 0 `9 {. u* _2 F4 d3 [9 k+ \1 l安定面和操纵面都 . j8 O2 x& a6 p$ x" ?7 S9 W% u) X- [8 q0 B7 H4 Z空速指标 + {4 t( H' O' z) }适航性, 7 K2 b5 `3 _7 `0 W有关气动能力、 ) `5 C) C% v' C- A0 {演算法, ( M! Z: u% w* x% L+ L4 B1 g" T. K* f5 [- v% b$ q 飞机飞行手册(AFM), & r0 R6 K3 e4 t2 x6 ~6 j4 t+ y% z包合性能极限,操作极限,操作程序,起飞和着陆性 , F9 S4 t* I& L) @; Z1 Y9 X$ B; F8 B9 B8 {3 R7 t机场分析,1 C% G& G! m/ s9 W9 _ 一套针对给定的机场跑道的详细重量限制资料。通常与 " l' X6 V0 `7 x6 l, f B机场温度、风、和飞机襟6 P" W1 d' Y( W 英汉对照民用航空词典B OEING 1 r9 ?; d3 x* y M* h- \TECHNICAL DICTIONARY 75 t8 i' v) Y6 C4 d T0 `# A9 S AIRSPEED BUGS, Adjustable pointers on the airspeed3 W5 L$ P& R9 B4 f' l indicator. 4 h5 v7 m+ e0 l4 E% OALLOY, A mixture of a basic metal and small amounts ! u. Y, F' y( V# @' Y( N' j, uf other metals to change the properties of the basic , r4 ^ m ?- n" |, a% F( Aetal. 5 p! K; C. L/ {2 G* T, QMinimum airplane speed.9 \, d; M' V* d3 m7 U/ j! P e of {) X# p1 u+ w$ h% ? itting airplane angle relative to) D$ N% ^3 C! ^' @+ d irstream for the stall warning system. : P. J# o# l3 n. ^another. $ N6 O2 m0 U6 x3 m* _+ q XLTERNATE , An additional airport selected during 8 e/ Q8 E4 V# T. @" m% z) e; y& g, h; F: |8 J+ S6 N 合金, 5 t: M \1 l3 @6 j在金属中加人少量其他金属,而改变其性质的一种金属 ! z: A- a4 a9 m- ?% F- d5 x0 D合物。 5 i8 Q K) O# K- L8 t飞机的最小速度。5 k a' a. W. N 速警告系统传输飞机对% S1 T# ]" i7 S7 ?$ A( M+ G9 G) ? 流的相对角度。7 }, a# d- t* o3 B; \ 由一个状况改换到另一个。 ! o: @ Q0 _# b g4 g- D" l9 f% T% a* j降场,& v% Q6 ?7 P8 K' J- B 划时,除了目标机场之外,所选的另一个机 % F# ~) s) M# w7 w; po % f- Z0 q/ q1 H$ m# N: d \m , h& w5 f0 K2 b! G% ~ALPHA SPEED,: C! n6 z t1 X6 O4 O# G ALPHA VANE, A small moveable airfoil on the sid2 i8 x! }. P! | the fuselage transm - w5 y! L' Y4 R G- h5 Ra5 B; L$ W6 I$ z- B! {/ Q/ G4 Z# ~ ALTERNATE, To change from one condition to ( A. e" J k3 fA , S. ]- l% ~- aflight planning, usually near the destination airport, to be6 L8 L) V v3 X, K; M, w% q used when it is desirable to divert from the original* G5 B8 Y( a0 Y4 R* c! Q6 D+ E8 V! I destination airport. ! h, K6 w2 r+ @$ b) _% z4 |空速游标 ) d, w% t" P' O: G9 ^* _; y# q! d9 V空速表上的可调指标。 9 o5 n7 P- h; e& Q( x" }4 J1 l. J 迎角速度,& v# ^- {0 A1 N1 b" s: Z. @ 迎角叶片, 7 \! J' e9 `0 h, @- ~& H% ]位于机身侧的可动小翼面。为失; u. G' w; S5 A3 l8 t0 s. V9 c0 g- z- n { \交替, " @; k1 J4 F. G, A+ V$ V5 D) [3 E, m: P" X 制订飞行计: r, n" V9 ?( X$ a, b5 ` 场。通常在目标机场附近,以备不去目标机场时,改降之4 S+ k+ R- M+ ?- ^ 用。 * a1 u1 ]. \+ f英汉对照民用航空词典B OEING ' H3 f4 N1 j! @: qTECHNICAL DICTIONARY 8! l$ w* B: i$ }0 H ALTERNATE AERODROME, An aerodrome to which 2 j8 N( b. n& }5 l7 han aircraft may proceed when it becomes either6 Y& ~) ]& V( H# G possible or inadvisable to proceed to or land at the 5 N% T6 C0 b+ B d4 derodrome of intended landing. ' a3 Y5 q. B, R h5 T9 C) UTER SETTING, The adjustment of the altimeter ! {8 y1 c$ i5 q' j! K+ ~6 Iaccount for local variations in atmospheric pressure. ) G( u( D( N. c& N% \, i& jLTITUDE ACQUIRE, A digital flight control system6 m6 {$ s8 E$ y7 J ode to transition from climb (or descend) to level flight.: F6 M. g2 i( ]' `$ G% U LTITUDE ALERT, A flight deck alert occuring when the7 A5 `( \9 J. ` irplane approaches or departs a selected altitude.* m( h/ {9 j! L* D. L: t( w. _ LTITUDE CAPABILITY, The maximum altitude at 5 n- C8 ]2 i+ l# Y! U7 Dhich the airplane can be flown at for a given thrust,1 J9 J; s1 h) w' d6 ^& A4 L" D" K( V peed and atmosphere condition. 6 }2 M7 p" W, ?LTITUDE HOLD (ALT HOLD), A mode of the autopilot $ f2 @ ~$ [# G) U. vr flight director to maintain a selected altitude.: Q" T: W4 ~( J, i" r4 R% J3 L* s irplane's altitude during VNAV operation.* {* R* Z+ _9 O( K 机场着陆时,可作着陆使用的2 {6 d/ P8 q% {* _) S2 C 场。 : m" {" P2 h/ t7 K3 Z* H. j8 G; G9 z$ W) [8 @: Z- A6 {根据当地大气压力变化而对高度表所做的调整。 0 m; | V5 s1 {: H3 h# K8 @* K一种数字式飞行操纵系统,从爬升(或下降)改平的模7 A6 K+ z( x6 s* y. T# Q8 ?3 D0 y8 i7 |度警告, ! _+ v2 T- R" k当飞机接近或偏离选定高度时,所出现的驾驶舱警告。 ( @$ n2 R ^6 G高度能力, : M8 R& d: M/ {/ g6 c& O9 P在给定的推力,速度和大气状况下,飞机能飞达的最大" C# @: H# b( F8 G C2 P$ a: @ w, s 高度。 6 Z. e/ e1 |2 n8 l N高度保持(ALT HOLD),7 M0 E; a3 s* H 自动驾驶仪或飞行指引仪保持在选定高度的一种方式。+ T) D0 D2 ~* _3 ?, K) v' |$ {; a# @5 M/ Y* a员对飞行高度的控制。% X. L7 I0 ~* C/ z: @, [ ^+ k im1 o+ k" y+ E$ k5 E; ]5 ^ a9 _/ \+ S. S+ W ALTIME , Q: z# A7 W c: H0 `/ a: A4 nto ; M7 J" J/ J# H, ~4 w$ ?. mA( z& x: L7 G7 L1 i9 r) x& M m * g: B6 \- m& t2 QA 6 i+ c) U, N+ N' I+ J5 ?a : s2 C. O2 \9 x1 \' W3 V, _A1 a3 |; A3 ]1 |; p% J d w : o% g, j1 ?) F P. c) v; ks 3 h2 }6 C. G- X; {! ~1 ]A / G+ f* w, Q. ~" |o # {8 g( u) s) c/ b4 o$ @2 @3 AALTITUDE INTERVENTION, Pilot control of the- f- O( x/ E: ^' f8 |* D/ n6 F a i. t5 h$ o) oAMBIENT, The surrounding atmosphere.# O: X* X% @( r; t: b2 k 备用机场,2 O1 G/ H' B" T0 v- g( w9 { 当不可能或不适宜在预选 . w/ g% H, V7 S8 i9 g& p: h$ q/ s$ E4 Y' k高度表设定; H3 F) I4 ~, X; r5 G' u( b b 高度截获,4 l( T2 Y% N2 Y" ]( i- s6 }; D" s. |' ?7 s& e; ]; I) | 高度干预 $ h* c/ d3 J! g5 D4 T在垂直导航工作过程中,飞行7 U- Q4 M( k* b6 P; B 周围环境(地面气层),* P' g0 q, o) o8 s% e. F$ s0 X 物体周围的环境(特别指大气)。 2 i+ V$ {$ G2 \+ l英汉对照民用航空词典B OEING a; V/ S1 N/ ]; H! C" KTECHNICAL DICTIONARY 9% k, m' I( f0 U* f# D& R$ V! B AMBIENT PRESSURE, Pressure of air surrounding an # w+ J/ r! c1 }& hobject, measured in pounds per square inch (psi) .; m6 r5 k5 x" U0 f MBIENT TEMPERATURE, Temperature of air0 G8 A( U6 K6 e! _/ |) e: | mpere. ' u7 J- J# f% E; Y6 h9 burrent waveform.; D& j1 y5 c8 l5 T, f& a g an 4 F& H+ J8 W7 _0 a/ F* T7 e2 snalog signal to a digital signal.! c* K, h/ x) p: Y( v( [: N1 L ore inputs: D; N! `$ I2 S; p* p f binary digital information and one output. The output) p' Q$ J/ p3 c" m 1 only when all of the inputs are 1. The output is 0 % u1 `3 @& ~5 X& Vhen any one or more inputs are 0. & E8 m! m1 G5 p( Q面气压),7 a2 m7 U+ f! t% D. r: g' ? 境温度,. |. U, J7 s% Q5 M! M" A 气温度,用摄氏度(°C)或华氏(°F)来$ Q5 k; ]" C0 ^- d' g. F! g4 b4 e$ x& {( H& M0 l电压或电流波形的幅度。+ W0 @7 M' ?1 y 性变化的信号来工作,或产生连续性变化的信号1 x: m3 v# K8 a 统。$ N" m9 m; E2 b2 ^ 将模拟式信号,转换成数值式。& C: B+ U4 Q( _; F- g5 H 一种有两个或两个以上的二进位数字信息输人,一个输8 X* l7 d$ T7 ^5 S+ @* h" \ 的装置或电路。当所有输人为1,输出为1。当任何一个 : f2 ]& B" V6 z' B6 `8 E$ n一个以上的输人为0时,输出为0。* J* F2 i0 l# h. m A : B+ m0 l2 o" p0 I7 G' j) msurrounding an object, measured in degrees Celsius1 M0 c, k5 F2 ~! x$ v2 T. H (°C)or degrees Fahrenheit (°F).5 P! n& s; j! Z AMPERE, A unit of electrical current. One volt across+ s' b" [. m u9 C* ~ one ohm of resistance causes current flow of one ! K( @; ]4 u3 @% u; W' ?. [a 9 O. S/ B2 Z/ `7 f: FAMPLITUDE, The size or magnitude of a voltage or' | D/ }$ y+ ^ c 2 i8 w. B. ]( @6 TANALOG, Quantities or representations that are 2 @- z3 y! H- R7 D; m, c1 ]variable over a continuous range. 1 M+ a% w* X1 u7 q0 ?/ lANALOG-TO-DIGITAL, The process of convertin' E( M: }1 [7 \ a" V, n% n/ M) f* Z AND GATE, A device or circuit with two or m* U. w ~7 U, Y& d9 l o1 j5 D& r; o6 Y' K- Z( I is. f, a; j! B: j5 v3 o J' W( S w1 u1 ]- ~. F6 d% s' c. L& d 环境压力(地 + }! S$ F" v5 e+ ?1 h物体周围的空气压力,用每平方英寸多少磅(psi)来 * M3 v$ n7 T5 o9 U: P9 ^度量。 / O; p- g4 k, @/ ^1 X0 _. U: Q. K2 O7 j% r 物体周围的空 5 I5 }' W! q7 ?/ {度量。! f i$ ?% w6 d* I# V6 _7 k 安培,8 j; ]7 f3 E! @( D2 s- O7 ~7 H: o+ V 电流的单位。 7 @7 o$ A# @7 d/ B/ ]4 _; e6 J+ t) s5 s1伏电压在1欧姆的电阻上所产生的电流为 % {: {% F9 u V1 T1安培& u6 s8 v' L: ?$ M5 c. { 振幅, A. u6 b+ u4 g1 J" m8 @4 j模拟式,+ w1 }5 s8 S. H8 C; F" W 用连续! `# k4 {9 g7 G- h$ P" G7 g9 }' s7 S8 v( P$ a8 v* f从模拟式到数字式,% }* `) h' ?, q5 G' r4 g 与门,$ c: Z8 J, r6 |+ Z1 _. P) Y* {( P2 t) f9 \! S. Y7 x. h( i) I+ |: E8 W, f英汉对照民用航空词典B OEING9 N: X4 ?3 P, I" |( d TECHNICAL DICTIONARY 10' B) W7 Z) l& z- I6 q2 Y ANEROID, A sealed flexible device containing air at low 7 h7 O9 N4 V) n/ z- D/ ]" P1 Cpressure, which expands or contracts during change of 1 d7 r) `* @4 U/ f: l% `! E- Y) h( Vressure outside the device.4 \4 k2 V# {5 Q# O" V7 d+ _ ically j; H j, F {8 v; n2 g r changing the direction ! h/ P7 h0 w5 O( a$ D6 If drive. , ~$ p2 M' O4 G8 k3 U0 e7 Oof the wing chord in; k& ]8 X/ A5 r5 s6 i! _ lation to the free stream airflow as it moves forward8 S9 [: t- R ]7 P% F( O2 | rough the air. + P/ M! u9 F3 }' T$ U; G8 \al axis of the; ?3 `2 z- B% p( P$ |+ e aircraft. 6 @) }0 |8 n& `. d& N8 u0 ^4 |% T- L胀或收缩。 3 B. P. x4 n5 {: i箱。是改变驱动方向的机械装置。5 g7 A) J0 p e" C& w 机翼翼弦在空气中向前运动时与自由气流之间的夹角。 ( m' s8 G8 a H& I* X9 s7 H+ T& G4 N' qp ) m$ H% J" j; O- A4 \3 L. f! V5 vANGLE GEARBOX, A part of an engine, mechan! Z1 }! e0 L3 \0 d driven by the compressor, which drives the accessory 3 A+ p4 h! n7 _/ L4 q1 Jgearbox. A mechanical device fo % h& ?) U; j/ L V* R" d) ]& Oo * O8 [% H1 v) H, hANGLE OF ATTACK, The angle ; Q. g1 w) [7 Cre ) B% z A0 G* dth : P) ^1 K$ }/ PANGLE OF INCIDENCE, The acute angle which the7 q% F$ T% m: B! s) v* C: A wing chord makes with the longitudin 9 G; L3 s8 \% Z5 D e' g0 D/ |膜盒, , x! P) v {2 C- M! l) ~' u; h内含低压空气的密封弹性装置。当它周围的压力变化6 w7 K$ w4 S7 G4 G4 ?2 ^* R 时,会膨 9 w, ^' ?# J& d6 a1 U" |伞齿轮箱,0 ]3 F6 o9 M2 k7 \ 发动机的一部分。被压气机以机械方式驱动,然后驱动; b+ K. r1 Z! ] 附件齿轮8 i- { G. O2 c( U* U# [ 迎角, 9 W' B+ X7 u( n% U9 B3 b$ X安装角,- K) l; j: b e$ c) U1 n# { 飞机的纵轴与机翼弦线所形成的锐角( F* R( Z% Z8 F& w 英汉对照民用航空词典B OEING . O+ P" v1 g7 J0 yTECHNICAL DICTIONARY 11' `' n3 i+ i3 v5 `3 \& g0 d: d8 d ANNUNCIATIONS, Audio or visual indications used to/ Y( [; |( [: i call attention to an event that has taken place.8 E: j* \+ ~6 x% s5 _ W! k6 Y! [ ANNUNCIATOR, A visual device consisting of a number, q0 K2 ? Z b" Z5 _# a# E ly. - e7 @; ?6 G2 g# |ANODE, The element toward which the principal stream0 i1 n0 A7 B9 E3 n; X- L of electrons flows. % `- |3 a" K% F* L/ n4 S; P4 \ANOMALY, Not normal.( F) ~6 F! r4 S8 r- l ANTENNA, A device which, used in conjunction with a " |* h6 \' d& K; p7 m' W* Ytransmitter or receiver, is used for radiating or receiving 0 x$ |' a# |# m) lradio waves." c3 N; g& x% [' c* J; j, [6 W NTI-ICING, A method of preventing ice formation on , V s# t1 F6 r7 e! }6 d9 ~e wing leading edges and engine nacelles. + B# C2 O% r+ H+ ]& |8 P, YNTI-SKID, A system for providing maximum braking5 u) ` Q6 m. x. n ithout skidding for any runway condition. Anti-skid) v, _& }% r9 e% k2 z; C omponents are part of the brake system.7 [9 h$ i. p( R) @! n, p 告,6 d1 t9 O" c3 u4 l 当发生事件时,以声音或目视指示形成的提示信号。! t2 v! {8 B& u# ^9 z 与之有关的电路的现有情况或已存在的3 V$ f* v! T$ \2 x# F8 a9 _& ?8 a0 U' Q0 B, ^ 正极," P1 C- E6 k+ d0 _) J 主电子流向的极位。3 w% A5 {* u! e6 k0 S6 e; m9 B! [ 异常," f5 _+ a: A2 q% [: x$ h 不正常。5 t# K) ^- D$ F+ F 天线,: I" Q; g' h1 M. A9 ` 一种与发射机或接收机共同工作来发射或接收无线电* R; `; ~& Y8 l4 t" B+ U' o6 i/ e 波的装置。 j* R7 I6 }% D 冰, 3 p9 k/ K3 z. \! b3 A2 W& ]- K防滑系统,2 B' f* O, |9 i. P5 g 一种在任何跑道状况下,都能提供最大的刹车能力而不! N m8 e% n! ]& I$ k 使轮胎打滑的系统。防滑部件是刹车系统的一部分。 3 m$ H. C% i$ L0 t- ~0 u4 H0 Y* Gof lights. Each light indicates the condition which exists 0 T% |: x& b. a$ G. r' t, ror has existed in an associated circuit and is labeled 7 h8 |* u- b, b" Iaccording : @- i8 g, d9 W; b& GA, p) a; |5 _& o$ q' y* b0 w) t th - }4 }& y, C- B( e/ ]. b# ]2 BA' `5 l4 _) G* ?, d5 j* \ w $ ~8 n4 n1 k3 `6 S, ~c1 M7 d1 a6 A" [9 e! j4 b. j; k3 ?+ C3 B' ~( B信号牌, E" V4 J( S3 z+ H4 N/ `由一系列指示灯组成的目视装置。每个指示灯都有相应' K5 I4 k9 W2 F- d6 W- m 的标记,用来显示 & i7 e, O8 v) d4 q" e' A5 [7 j# |% F7 o" O6 u! L4 k0 Q: e" G' H5 O# A' K 防止机翼前沿和发动机短舱结冰的一种方法。 9 m" L- N' P( q1 C- \英汉对照民用航空词典B OEING1 i$ k) a' y7 c- F2 ?3 z& P5 o TECHNICAL DICTIONARY 123 N) R* X( O; ?3 h/ E APPENDIX, A supplement to the Airplane Flight Manual( h7 g1 \6 G9 D% ` tained in the basic manual. A L/ }- j9 j* C* [2 J m. |7 @5 `ollection of supplementary material at the end of a 3 A) [; ?5 @8 P' R. N/ ~ook.+ x7 I! u) J: t( h; Z of the& i6 d) ]2 z' R; ?& C# U rsion link on the landing gear.7 ~1 Y& p9 E0 i) [ F' z0 q: @ APPROACH MODE, An autopilot/flight director mode% m9 w8 ]# ]* K3 D which is a combination of localizer for roll control and 4 Q3 {, D" d2 ~% @3 q% n, k/ N& tglide slope for pitch control. This mode is used when full% f5 K! }* O9 m instrument landing system is available.+ P/ X! h& s2 k- P: F/ M7 ^! `. \0 ` APU, SEE - AUXILIARY POWER UNIT ) y: u4 N, u/ R# b/ T4 u3 gARINC, SEE - AERONAUTICAL RADIO0 J" e# a8 _$ m9 G7 d INCORPORATED# z' r. V) T ? G# Y ARM, To make ready for operation.2 k% Z. S! Z# T+ R4 ] 附录, 2 _8 ]0 W2 O0 l* h飞机飞行手册的附件,包含基本手册中未提到的飞机形 3 a, C$ P6 T/ M4 j2 u态的其他性能。是附在手册末的补充材料。 q7 P7 Q/ d/ w6 K( Z* ~4 m$ e0 _ 顶销,* v! Q O# p, r3 X, W+ D T 用于连接起落架扭力臂两部份的销子。) N4 @# R1 v- M2 c5 p& _4 [ 进近方式, , U* H- e# y ]9 I7 m一种综合了控制横侧的航道信号和控制俯仰下滑信号 5 P4 C- N# _7 C& I1 f的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系 9 D r i J& d" V: U: z统正常时才使用。 2 {3 R" ?) i5 p$ ?辅助动力装置, + ~% j3 Z4 X8 u U" k7 q* o9 L见Auxiliary Power Unit # p2 s4 l+ }& {; ?( kcontaining additional performance for aircraft) k/ s/ C' v- I8 S2 ~2 C configurations not con 8 i% C3 [* O* Ac - K% U* }2 U$ M2 D3 Yb( }8 r8 ?: s/ D3 B# n/ t9 a! k APEX PIN, A pin for joining the two sections S- T7 V1 z0 y to & ~, R0 B7 w% x9 i. @7 _6 g c, ^8 A% z航空无线电公司, ; k# x+ ?2 t5 J% q2 K见Aeronautical Radio Incorporated./ a5 z( k$ a" D0 h 预位," h4 ?7 j% s3 o 部件可以开始工作的状态。 4 a+ H x: u% n+ }* N& T英汉对照民用航空词典B OEING* w: @' w1 N9 ^9 T0 {% s TECHNICAL DICTIONARY 13 ( z8 y( g* u8 \5 {2 A f+ z2 ]8 VARC, The curved track over the ground of an aircraft( D# e; ~8 s" F, x+ k' V3 w flying at a constant distance from a measuring - @3 W6 y# q) c5 S" F: iequipment (DME).5 X9 ]+ A2 }9 ?' L in the limits of self-contained system 2 x, e" e Z- V! G% b! I( lapability. 8 E1 P* f! j" j+ stem for opposing or restricting 0 n/ P( @; B$ S3 ]. R% Povement. - e! }& S4 p: ^9 c: DSPIRATED TAT PROBE, A sensor that measures total ) M# n) i/ }5 Cir temperature when the airplane is in the air and that% U1 [, h: s4 y) G; _+ `& D4 R easures outside air temperature when the airplane is 7 F- U" J# v& r5 \n the ground. The outside air temperature is measured( p) A% H! s) X- k% E i/ r$ T SSEMBLY, The fitting together of a complete structure + P* D. O; y; P- q- sSSUMED TEMPERATURE REDUCED THRUST, The5 X. K4 O3 l; N! T. N' \- { ATC, SEE - AIR TRAFFIC CONTROL# W) N6 u4 Y1 E; a* h# j% z* s$ m/ h9 q! K5 W- J \系统中所产生的一种用以抗拒 8 x: h4 j6 U1 C# E* B; ]作或限制动作的力。9 t8 {! }& a) c) W- G6 W* w 头, * \! b- n+ q% R* y' k; b用来测量飞机在空中时的总大气温度和在地面时的外 " v2 r3 |3 Q: ?0 T$ e温度。地面外界温度的测量是利用引气将外界空气吸入 - H B( o; b$ F+ ^头,以达到测量的目的。% N6 g& s4 }* b3 J* _% d# X 配, $ O% }) P( z( }' Q( p, Z一个完整的结构或组件的过程。 , R/ L. A/ u [; P+ w5 J( b假设温度而得的减推力, " |- S* e' X- I8 o: A$ t- N推力设定值时,假定一个比实际外界空气温 ( Y5 _" D+ k+ G1 M* k9 d" j空中交通管制, ) J4 M0 q5 v5 o见Air Traffic Control4 M b1 v9 E. L- U2 k% G, L- { AREA NAVIGATION/RNAV, A method of navigation * d1 D0 _* A3 ]that permits aircraft operations on any desired course 2 S, x' G6 h6 Q3 c& _8 twithin the coverage of station-referenced navigation 0 q) f% I, P; ? c# t" Ysignals or with # o K% v `4 Bc! W& P4 ~/ m u+ F3 B' t, X$ a ARTIFICIAL FEEL, A force developed in the flight3 w: |5 u: ^1 o control or brake sys% q" I$ G* T; u" d1 W: l m) k6 `( U3 |1 K9 Y) O# P4 @# k) u A 6 z- F% ~! t! ]$ b' f. Ya 3 U. K$ E& e* ?& e6 b; i g, ^- Gm& C# X5 Q; k. e- E o 7 C# Y! r6 w4 [ Wby using bleed air to draw ambient air through the" h6 v0 h5 U' r c/ a2 [' [# M' O sensor when the airplane is not moving. 7 y5 {7 q) {; F7 p3 tA9 W% {- ^+ G) E2 |% W2 M or unit.: g N. y: l& G4 X( @: S) q A ! V; @9 R+ ]1 k: T3 V5 Nlower thrust obtained by setting a higher than actual " m; `; [7 L" i i' lOutside Air Temperature (OAT). Y% J+ v$ n, K- p8 C& U$ C% v 弧线,, m+ n* }+ K, l& m3 d3 @- G 飞机在围绕DME台等距飞行时的弧形航迹。# {& [) X) i( P( L$ I 区域导航, 1 a8 _8 z: T/ \; Y" h容许飞机飞行在有电台参考的导航信号或自备系统能 " Q7 p5 d6 c4 p/ {6 N( R/ x力极限范围内,飞行任何预定航线的一种导航方法。" G$ `# D, ?6 m! A' }, E2 {- Q 模拟感觉- f, R. u& ^& Q7 i; n9 m 在飞行操纵系统或刹车9 w+ }, C, q3 t1 z q! F0 G. G$ t# G2 w$ g/ p1 C) h# P' Y吸气式总温探 ! q+ Z( Z2 ?' z! t9 M1 t" \' V+ J6 H3 F9 i2 {6 |/ ~, D# V* _: |, }% `; N6 `0 _' A8 Z. F1 K 组合成( J4 n0 I" p% K9 _7 s, }" H0 @5 `在选择起飞6 k. o' S$ |0 | 度高的温度而得到的推力。用这种方法可以减少发动机的 ) F4 A( |2 g# M7 y磨损和维护费用。 3 ~! {8 `9 ?+ {+ Z! Z& u9 B1 W0 r* y( O7 f: S) ~; \5 r! Z 英汉对照民用航空词典B OEING J, c! ]! h9 lTECHNICAL DICTIONARY 14 # G7 r$ L n) j( s6 h; v7 bATE, SEE - AUTOMATIC TEST EQUIPMENT % A/ K/ l" a; r* k X4 vATMOSPHERIC PRESSURE, Pressure of air due to the; q, u3 _' |8 R; i arth's atmosphere, expressed in pounds per square $ |% r+ H8 Y: \ch (psi) or inches of mercury (in Hg) or millibars (mB). , [$ @ Q( v3 I; c- K$ hTTITUDE, The relative orientation of the airplane with1 g* x u7 K% f% a* F# v1 d7 z spect to pitch, roll, and yaw.0 E1 R% J8 h4 f$ O: ` UDIO CONTROUSELECTOR PANEL, The panel in T! a# C9 s! J5 k3 O! i% M0 we airplane which controls and selects the routing of" }6 h- d9 U; e( ` udio. ( O; Y u) M, @7 KUTOLAND, Automatic landing using the Digital Flight: o) B, P* Y1 _4 b$ c: q9 H ontrol System. 6 J0 P( X& O9 K, e" \6 {: t; Cn.( J- n8 E' F% N3 x. C M, A system7 {, \' F- y3 d4 q0 r$ i omposed of all necessary subsystems needed to guide* x1 K4 {) P p8 Y; c& G, n e flight of an airplane. ! W$ `* d' |/ Y: O' _- ]EQUIPMENT, System test) y' Q8 l! [; t+ s" W quipment that operates under computer control. * J: N1 p4 i' f装置,

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e ( J, G/ M: j$ ]% vin9 E( O( q( L! ^% { A 2 J" b/ V( k( jre ~. H4 _% y, e A 8 Z+ Q. `. s0 w3 l" U7 w6 o4 [th; F+ f9 S* z5 p a, t' p8 M$ L; Q A / `0 |; U7 a5 v! ?" y1 NC 5 C1 f' V; { s5 LAUTOMATIC DIRECTION FINDER, A system which$ S7 ^; {+ P) v; Y1 Q1 B determines the direction of a radio statio ) m3 R6 t4 h5 \! FAUTOMATIC FLIGHT CONTROL SYSTE! w0 A9 E: C) K. o c) u5 y( j. x; n* I, \- C0 n th" D2 T* j" `) g& K, k0 K AUTOMATIC TEST 4 S: o8 @# ~9 I+ e$ re - E4 d3 K4 D. F7 i自动测试5 n+ ~; v( [8 e; o/ B8 J 见Automatic Test Equipment. ' {/ g6 e0 B4 D8 Q大气压力, # R9 n7 i# }- [3 D. w$ u) x$ _! `由于地球周围的大气而产生的空气压力,以每平方寸多7 x& E5 b' [; N# X! p: o 磅(psi)或多少寸高水银柱(in Hg)或毫巴(mB)来 T% ]/ g, Y. k; K% [% d示。 3 ~' b/ K+ p; ?& X! }5 b1 u飞机姿态, % H& a# a" N( ^* o- N飞机与俯仰,坡度,和偏航有关的相对方向。 * F) }. W+ c1 G3 ]音频选择面板, 4 `7 {0 E" S9 v3 z/ @( r飞机内用来控制和选择音频通路的面板。 ( V* @/ h9 k1 C0 C9 c自动着陆, 3 |! H6 H' c' ~ L8 f% v9 _使用数字式飞行操作系统来进行自动着陆。! [2 c+ \. E) g0 F 的系统。" N& V5 j0 r5 [; ?. |) W9 X" E- f! \4 M, U l, y( X2 C 系统所组成的一个系统。 : s8 l; S1 c8 }; u+ ]( M在计算机控制下运作的系统测试装置。 ' o2 e+ D: O! p# X- l, r% w* _* F5 i, y4 ~$ e. x# R, C6 x" x/ ? 自动定向仪(ADF),. X6 p4 ?& s' \/ F& S( e1 [ 确定无线电台方向5 m4 W$ K* @- K! G 自动飞行控制系统3 _( {+ h/ J1 @% b6 ^8 }/ B 由所有能引导飞机飞行的子; T+ z3 R' g2 Q4 ~( ` 自动测试装置,' o' X% s( i ~( f* s2 L 英汉对照民用航空词典B OEING " D5 r- x. T" W2 c% Z o! t. tTECHNICAL DICTIONARY 15 2 W7 W+ g. s/ b! HAUTOPILOT, A system which automatically controls ( ^& s9 y5 O3 r, k( B0 z% E! Zand guides the flight of an airplane. ) O. n: B \" d) ^! [) @% N% _+ SAUTOPILOT FLIGHT DIRECTOR SYSTEM, An! g# O0 }8 {9 G5 ] tor $ `' x% d- {7 ?UTOTHROTTLE, A system which automatically 1 @% s) ]) Y1 c& hontrols the throttles of an airplane. * Q6 y: A* w$ D5 \4 pPOWER UNIT, A small turbine engine in& b6 r% \5 N% A e airplane for supplying electrical and pneumatic " F; W. M5 m+ W" d$ H! Power for systems operation on the ground or in flight.' {* |& N. w; ?5 R* u. W* } VM, SEE - AIRBORNE VIBRATION MONITOR ) u( s% d8 o+ [. J" uXIAL FLOW COMPRESSOR, A type of compressor 7 Z- M3 F( j, H; O3 Esed in a gas turbine engine in which air passes through& Y( a# P7 q" |- e$ ^) ] XIS, An imaginary straight line or an actual physical$ z. _) s9 Q3 Z omponent (such as an axle) around which a body can & t1 v4 [7 b% U& v+ Y2 ltate.; H& ?& e4 G9 u8 O. y 仪,1 V. a' j+ M& y3 d2 m0 m# u1 Q6 M, r3 }' B( t5 _" @7 Z 自动驾驶飞行指引系统, 3 ~- ]) P& ?/ C动驾驶和飞行指引功能的系统。 4 v( o. i; E# r @动油门, , [9 B) p1 a8 u* y7 L! _# ^7 h自动控制飞机油门的系统。 $ ~! x+ F) Q4 j; l S3 q- _是飞机内的小涡轮发动机,在地面或空中给各系统提供1 G: t$ r- k, J% V, J 源和气源。 3 t6 v5 p$ u9 @9 a称。 / d, F' x+ Q' A! u载振动监视器, Y0 C6 ]& B! U' P 见Airborne Vibration Monitor% O- r" l: f* n! ?4 E0 F% b# \ integrated system containing autopilot and flight direc + N6 A; m- A1 @9 Wfunctions. % g9 [; u. V& Y* J( S) K9 k) [ o2 fA ( `$ q3 _- Y% P. H. @c/ m5 l0 k/ r% J$ T, M" w AUXILIARY5 N/ l& j/ v3 i+ v th 0 P; C. X% l0 k4 z. s- \p1 |# v4 `6 ~: g0 n2 I( K/ t AVIONICS, An acronym designating the field of aviation 7 b( {' B% j6 P$ @: l, d. Kelectronics.& K" z: I, J0 e$ N v( n3 p A& S# G. ?; |8 G- n( M A ( W$ q8 d: v6 g& i4 I, Gu% u1 [8 e8 @8 n3 M the compressor in a straight flow, front to rear. ! F; m) X$ `6 OA " v7 J' f) u4 c9 P( D2 P2 D3 `c. Y0 o# R5 I x' j" X& R6 t ro% F! J' W) }6 r% U( Q: R 自动驾驶4 C, t5 |+ W+ t9 l# J 动操纵和引导飞机飞行的系统。# A0 m3 h2 r& a9 e v 一个综合自 % o- }$ O- c3 U9 K! T. M# X' ]% u* Z/ v( U+ {% @0 d7 l辅助动力装置, * } g2 j A6 ~, W5 c9 M* e0 V) ]' q h2 \- k; v! }% q5 _ 航空电子学, * E& W8 _7 z ~+ E' m5 Y是航空电子领域的一特有名* v& w4 S1 _( m4 _$ y8 d3 g1 t! Z8 q% O" L2 ~& l& n1 \" Y) E) ^/ ^# L4 v流压缩机,. f- p8 |0 p/ |: Q 一种用于燃气涡轮发动机内的压气机。空气由发动机的 : k/ g" F: K/ @! T% |( Y部流出。6 L3 N }. l3 ]/ t. J; v8 r 线,/ \" Z8 s, |& \9 O( {# k1 j 可让物体围绕着作旋转运动的一个想像的直线或实际. u! n1 B4 t6 T9 ]1 h 在的部件(如轴)。& |7 u8 t3 f, z. V3 O' t9 S+ |& [) F/ j5 `1 n3 ] 前部轴向流人,压缩后,由后( s7 k4 K: g! P" _9 N# y5 ?1 k! n. M+ K! U$ u2 Z9 D% R; B; E) {1 n 英汉对照民用航空词典B OEING . L. T, R) R1 ^6 H/ PTECHNICAL DICTIONARY 161 b* n0 p) v& D d1 J- k3 v1 p' N B$ i6 j3 M: G! M ACKCOURSE APPROACH, An approach to a runway ( h4 f% H& l; y7 v5 ~. }: v Oversed.7 a, [. v) s( K, S {6 D+ B* s own on the EFIS that ' k& n3 y2 C- w w! R. moes not readily change, for example, navigational aids. 5 ` D* y% G' s6 b3 Y- cvement in the tank or reservoir.! O) j# [: u: {% Y0 Q( f0 c8 x# K ALANCE TAB, A small hinged moveable part on the) w! [6 k2 p! C2 n3 b ailing edge of a control surface (aileron, elevator, / m5 I' p; \" J/ s# u# S航道进近, 4 }2 q8 ^: k1 @) F( f7 n相反的进近方向。当反航道进近时,无下滑 2 O5 o; j! M5 G+ k# [显示在电子飞行仪表系统上不经常改变的数据。例如:# K3 k/ |+ R/ V/ N5 s 航设备。 5 \/ n% v! ?3 v% Q$ D# C在燃油箱或滑油箱内阻止液体流动的隔板。 6 f$ R# d1 ?* @( y4 b动补偿片, ; g, m6 ^6 {2 m, I- m铰接在操纵面后缘(副翼,方向舵,升降舵)的可动部。 V; ^3 O& C5 u5 { 与操纵面相反,以帮助操纵面运: \+ I/ K" w" T7 |7 X$ r" A B ' w) A# N% Q$ U8 Lwhich is opposite the normal approach. For a 6 |, z( k% C# @4 G+ Xbackcourse approach, glide slope signals are not & t# {* i0 f& e( r; q. Eavailable and the sense of localizer signals must be ' o! I( g9 ^' |2 ?re ) u8 j6 G/ A: R% R) qBACKGROUND DATA, Data sh ; y9 S+ n- q6 }$ I, [3 b% Qd " I9 | \9 {$ P. NBAFFLE, A partition in a tank or reservoir to prevent , S9 ~8 _& u: h% [fluid mo' E9 e0 b; D1 g* O0 B B2 G. D8 G3 Y# D# e tr. X/ V( N/ U' u) A+ v" l1 b rudder).The tab moves in an opposite direction to the . a- c/ x$ w0 c& L# J( k3 v, ~control surface for assisting movement of the control - h3 x0 k8 C/ fsurface.3 R( g* ?0 K( `* v/ p5 _& F. z* d( T* R4 n4 d- ~3 F 与正常进近 " b( j; n- b0 s! E% R- V道信号并且航道信号也必须逆反。! r5 b7 S# g# x" \% ^. X& e F$ u0 m3 o 背景数据,& W8 I) Z3 i6 h; h0 d0 J, r* f9 ]* U/ O 缓冲隔板, ! V) B6 b d# x. I2 y8 u& _" ?# D随动补偿片的动作方向; r, Z" z; F0 l. T% z! Z$ e L 动,减小操纵力。7 z! l/ ?% ]) Z2 S1 x$ E$ p) s 英汉对照民用航空词典B OEING : M7 G( Z8 c) j) y& W XTECHNICAL DICTIONARY 174 {; A! j. | E5 H5 f% l7 m BALANCED FIELD LENGTH, The field length2 N7 O2 M% J! H associated with optimum aircraft performance when " v/ ~+ q0 `$ o1 ]' y* P7 obstacles are not a constraint. In this case, after engine; H7 T) _ v z ilure at V1, the distance required to accelerate, takeoff( p y& I% C d* F L* X nd reach a height of 35 feet is equal to the distance. @+ P! A( f1 @5 U' o; y ALLAST, A weight installed in an aircraft to maintain) H3 t1 M% M1 D# } ALL NUT, A fixed spherical nut driven by the4 Z+ S* O8 w7 l AR OUT OF VIEW, A signal used to remove the flight . K: O) n" U& M; q" q w! f" f& N# xAROMETRIC PRESSURE, The pressure of air above: a* o) _4 L) g5 U# c4 R g) or" F! f" S3 W6 T+ Y5 ^4 C millibars (MB). " C4 |. B0 w2 A) P. m8 vATTERY, An electrical device for changing stored* \9 N9 e+ R" F; ] 性能的场长。在此+ @1 A j! U* O8 F5 t 况下,V1时发动机故障,要完成加速、起飞、离地35 2 n7 _! o1 i* J+ c' m, k) y尺所需距离等于相同速度下完成全停所需的距离。& ^8 Q8 f3 _4 |# G$ ?8 h- {# i) R* i 舱物,. r" e' c$ E) A) D6 ` 重心在许可范围内面装载的配重物。9 V- T/ I, g+ | 形螺母, 4 j2 _+ |! b( g. Z* x2 F% E8 C的固定的球形螺母,用以使襟翼和水平6 C5 }9 a2 N( Y# Q( A2 P/ O 引杆消失, # j8 r( V1 V2 R6 ?3 M指引杆的信号。 . n9 _. ]8 N! {$ i+ `" O3 c压,( x9 O% Q+ n0 g/ N& v7 [# n 压力。通常以多少寸高水银柱(in- q7 f4 D4 z1 F, I$ z/ D 瓶,( @+ H; O! F/ d9 j s! ~3 j! Z( Y x 的化学能转变为直流电的电气装置。; m6 F3 V+ b* N: q0 K4 Z o u* C/ p: w! J3 m$ o fa , D/ q4 r/ B9 |0 U6 s9 f% Ua ! Q' Q& F/ z3 Z1 F! mrequired to stop from the same speed. ) w, n) b" U" LB! J: \( F) _( K% C* L the center of gravity within allowable limits. ' K" M3 v' d. S4 l( dB" T. f+ X6 ~. z4 d# | h9 t3 S' v jackscrew for flap and stabilizer movement. " y( I8 X8 h( s( k" ~B& m3 f; `$ r$ V. H5 ]0 u/ Z# r1 s& F director command bar(s). 7 x7 f9 C7 e& Y3 M# f/ D" vB * A8 A- \: ^* ^zero pressure measured in inches of mercury (in H. `, J9 \# x8 \0 `$ i# i in ' o w# Y) q0 wBASE METAL, The underlining metal to which alloying ( G0 p% ?' v* _8 i. Q3 S; eagents or metals are added. 8 c: G) f* y3 R: B! F. `B ' ^# k' m4 l. y$ [! Zchemical energy into direct electric current.5 R7 w6 T' O6 U% H9 e 平衡场长,% S* Z8 F- V6 S" ~- f# O) M 当障碍物非限制因素使飞机达到最佳 2 k! j* K6 V$ v7 J! D, S' A* s4 [3 S8 _" o& n& k8 j& Q' A5 Z, }7 Z& x( {: z) U5 P! [) d9 o. M+ o! H& ] 为保持飞机' }) ?9 x8 s5 Q. b" I9 U# o q% W 由粗重螺杆驱动 4 P- ]" q4 \+ z: a3 Y& z1 `安定面运动。" U7 q9 V( G: ]8 C( h2 [3 a- Q! P: @$ R; n' \. S5 ^用于除去飞行 3 h# Z8 ?1 X$ o8 c/ u# ?: k( ]0 B: D8 p+ L8 V3 f4 `4 m$ T零压力以上的空气 & d: m4 q( v/ H9 J4 j) YHg)或毫巴(MB)来表示。 ; g) k" X* [8 q基底金属, 5 X- j* o' z3 h- s, Y4 c指合金中的主要金属成份。 0 s1 Z3 {0 x2 ~2 r1 ^/ Q$ x# J2 d8 o# c9 z8 o6 l7 |+ E& X" p将储蓄 7 F g& H" J6 [1 m0 @英汉对照民用航空词典B OEING9 \8 n1 U# \3 i$ b& e* B) X TECHNICAL DICTIONARY 18 / m. H' Y! t+ h' }) NBATTER7 a* i5 q w/ E direct cu 1 U/ y: e" f9 k$ g4 z) j7 ppower su 6 }% d2 n& X# C J- y" s) y& GY BUS, An electrical conductor supplied with 9 y( k5 D) ]# \0 R8 Orrent from the battery or transformer-rectifier for ) Y1 o: }& A/ Y# V% Zpply to operating components. + a& V9 x3 r7 Q$ z4 t6 ]CHARGER, An electrical device supplied7 b8 Q: x) _' Q' @+ P ith alternating current, which produces a direct current 6 {4 X: c1 d- [7 Z# yutput for charging the battery on the airplane. + |; E! Z& }$ A+ O7 o& v# ^AY, A compartment in the airplane structure., ]/ e- ^ m7 j" n CD, SEE - BINARY CODED DECIMAL % N9 O0 `9 C `4 ~$ MEACON, A device which emits a signal for use as a: C- a" c5 I! R# s1 Z4 R5 U uidance or warning aid. : T7 a$ u) C! p+ qBEARING (NO. 2), The direction from an airplane to a" J# X) N, F% |, m8 R% H! z4 c( m ground station. 5 ^* o. C: Y. q瓶汇流条,7 h" v8 D% R, W- V; h 将从电瓶或变压整流器来的直流电供给工作部件的导 7 ^7 }$ f: X( t- b/ Y1 O8 E体。' Q3 y0 C( Z8 q2 d8 W! R 瓶充电器, 9 O: [8 m$ U4 [6 o: G5 O+ v: a+ N用交流电向飞机内电瓶充电的电气装置。带有交流电的+ [+ M; k0 ?9 C- \8 e 气装置,该装置产生直流电向飞机上的电瓶充电。 2 G1 [" ^. a+ i5 Z* P6 s0 A5 G舱,& _! }9 e! y, S0 o8 j( X 飞机结构中分隔的空间。; P! T8 x& C, a$ W 二进制编码, , T; \2 G9 w- Y& h- d见Binary Coded Decimal, W( ]; U7 z0 C Z2 X BATTERY) ^7 H7 U& d8 E) U: W w , k1 r D) @: ?$ j, qo 0 u% I' c0 [' fB 1 p6 H3 x9 ]6 e4 y0 u+ d% HB - M6 ~4 n" v; G! S5 [+ wB0 J4 W8 Q# ]4 v: Z; |2 n0 n3 G$ y g 8 C" T; y5 n% g9 ^, X! XBEARING (NO. 1), A surface that supports a moving ( Y' E' J$ J" H9 y9 |8 }5 d2 ^. S3 Cpart and reduces friction between the two.7 d& M: Y( m9 |' D4 s( d" f. t; k7 O/ ^, w m6 ~& i* X% n2 h$ C5 z2 K7 j* M/ \( z! z' p) O: k Q8 J m7 Y0 g9 ]; X) a, h/ e# F( _( S c( R0 ?. j4 E+ k 信标,3 Q6 `( c: q3 h- `' D1 L' [ 发射引导或警告用信号的装置。: Y& t( N- ]9 @9 a, ?& w% _ 方位(NO.2), ) u; w z, W. P" g9 X* }& U5 b从一架飞机到地面台的方向。 / Q! K( o# P* M+ _& Z1 L轴承(NO.1),% j5 p2 q$ B% U) F- L 用于减轻机械转动磨擦的机械装置。- i3 ^# E& I- s8 T7 X+ ?0 P) [+ \6 [ 英汉对照民用航空词典B OEING" B& E0 l) ?; O8 ? G% F TECHNICAL DICTIONARY 19* q. O, W% K* Q$ s% v BELLCRANK, A double lever in the control syst% n9 H( `% q8 U8 K9 f3 y changing direction of motion.+ J$ t/ z7 A9 z% ]( u$ v! _4 n em for : Y. Q0 ^. p3 v, o1 F$ x& r; Rct in the O3 J ?6 h6 A) V neumatic system for absorbing expansion of duct due \' W4 d0 H# \8 `1 j* sheat. 3 a" C/ J3 o- x6 @" @6 DELLOWS (NO. 2), Corrugated folded or pleated 4 A0 T7 } ~& `' `ontainer or compartment used to measure pressure.0 R7 q: \. Y1 w- R% [" W2 V EZEL, The part of an instrument case for locking the% j' f( G- w* P, k( P0 O lass. / R3 t& t* ~& f3 `IAS, The potential difference applied between two 5 x1 g/ | O3 r7 Doints for controlling a circuit.8 S7 ~, E2 B% a( c BILGE, The lowest part of an aircraft fuselage. A place ' y0 a6 h5 |. O+ n( O( lwhere water, dirt and other contaminants collect. 8 ?7 |. `: z6 [4 F( y气源系统内提供管道热胀冷缩所需要的余地的波状4 p) a/ F1 C! p4 B( d t/ ~ 轫管。2 A$ w7 {% o3 _, J! a3 c, {$ |% D 空膜盒, & E; w( q/ F1 p4 w" b一种具有波状表面的容器。用于量测气压。% x9 b7 c6 o5 q; p( z1 Z7 K, b 嵌沟缘, ( K. z9 P; L/ @* D1 Q将表面玻璃固定在仪表上的圈状零件。! K4 k2 \, r W% G 压, y0 u' {+ B# L9 A* c+ W. t 在控制电路的两点之间的电位差。% ^8 e* q2 W7 T 机身腹部, $ _8 K2 {. s0 M& f4 D" D机身的最底部,通常水,脏物,和其他外来物集存于此。$ L; y7 ?! r5 a) z) d# l5 {: ~$ }7 y BELLOWS (NO. 1), A corrugated flexible du : }. |3 c( `6 wp8 {) R7 M7 ^- r to , |, {% y/ ^5 j ?+ SB 5 U7 {9 ^: w1 h4 a# Hc ( W1 h1 {* j8 @9 d9 eB ; I& K9 O" l9 mg2 l. Z: _% C& E! z2 S: ^1 J B" E, R0 ^/ v& v9 e9 f5 z p9 u! j. f3 G0 W5 ~, X' L* C4 g! o" V u 直角摇臂,, ~9 I0 }7 f) Z# q& T 在操纵系统中改变运动方向用的双臂摇臂。/ W! c7 H2 m; f/ W% s, X1 Q4 m" O) | 波纹管,( n( p# W- k8 X- Z5 X% C# s6 ~) h+ d$ q- V- z/ `6 ~4 m5 F+ e- g% [8 D0 w5 V5 x8 U n" [) {! l0 d l4 ]: i5 x K6 k% e. d A( U" O, v3 z; c9 P( o# C 英汉对照民用航空词典B OEING , S5 J: `4 `, j" oTECHNICAL DICTIONARY 20 9 _) u, J1 t1 PBINARY CODED DECIMAL, A system of coding each % i' O2 @8 u) f; u" k/ Sdigit in a decimal number using the binary equivalent. 4 Y1 P$ m& D) P6 Q8 R+ n8 d" RBINARY NUMBER SYSTEM, A number system using* p' S) c, ~! p$ h0 r, Q s/ x. y# P5 L' u/ u9 | r& f2 C IT, In the binary number system, the smallest unit of* H' o r1 O" ]; K, E3 M formation, consisting of a 0 or a 1. 4 Y& B' ?! Q3 BITE, SEE - BUILT-IN TEST EQUIPMENT . G' W3 w6 ?! {! }; U; dLANK DISPLAY, A display that does not have any+ ~6 V% a6 t9 P" S, { dications, normally due to failure.2 C/ H' F5 d. `2 m) `( d! M) M; F LACK BOX, A container for electronic circuits to record ; \5 |* o& p: X. {) Aight data.+ p$ h6 C- m4 x- v' b: {! E LEED AIR, Air taken from the engine to power various# L! [1 Q1 A x2 z. o ircraft accessories. 9 G1 b1 A" D* w5 b# mA valve in the pneumatic system for air: s6 B" v/ {) q2 a7 i7 ^( D& t# R supply from the engine or auxiliary power unit to the. N% J4 \ z+ ^3 T9 }1 [& H% [ pneumatic manifold. A valve on the engine for reducing 9 E3 ~ n, f2 i9 t* epressure in the compressor section. , u! P4 P/ y' W/ l进制, ( x1 W; q8 X$ k! ^, B4 G进制,+ v3 X/ O4 A/ G5 d0 K4 D, m& h' U 一般用0和1)和2为底的数字系统。- @9 B6 K# p2 s( o9 f+ C0 x6 Y5 U! I7 E 特(二进位数), F, ?; i, P* E: }+ l" a6 j 二进制中的最小信息单位,包括0或1。 9 \2 t, O) ]- u/ ^$ F+ p; f内自测系统,2 a" x5 P% n# H& I$ {- y+ O8 Y 见Built-in Test Equipment 5 g F; O' c" j1 n" H1 f0 Q$ Otwo symbols (usually denoted 0 and 1) and having 2 a) U+ t8 G x/ e its base.) l3 w/ W( p7 q! A7 `; S" ? B & r+ j# [4 M7 X0 O! min . g* j3 K8 p; v x5 h" l: BB/ T0 o. w/ P0 |: f B + j: R r& S7 z s1 ?9 Ain ! O- V s) w# ^B: I/ {$ @8 V& E8 E- d4 L, j0 t1 G fl " g/ k. w* x! O( p+ lB8 G- t5 G8 C5 c3 ?% \9 E# S1 |$ b a T8 N) X* I( w' t8 [$ ~& | BLEED VALVE,5 K7 A( G9 ^$ e. V7 X1 \9 V 二进制编码的十 1 ~% Z' W2 r2 h% n! |( S' Q一种编码系统。用等效二进制位数编译十进位数的每一! Q' H, ~" A- c& P% j 位。' L* u" \) w6 k" P1 I( ?0 U6 P2 X4 M1 h; X4 s9 K 以两个符号(+ y) r+ p; b( G4 \6 ]# J4 Y% o( j ?( F' ^1 u/ t. y- O6 n7 D . $ k: y+ T! A, O' M1 G( o7 r8 \白显示, : v- ]& z( H4 G5 }' ]+ A+ ~6 ^通常因故障而造成的显示器上没有任何指示。- {8 t1 i W3 C1 |( p8 S 匣子,0 m" D6 E/ D3 x/ r; p' B 装有用于记录飞行数据的电路系统的容器。 B; Z1 |( h' `. \& N9 W气,. O n# I$ _; } g; h 取自发动机而用以驱动飞机上之各种附件的空气。 : N9 P+ \& _; c1 h O6 d- c气源系统内,使来自发动机或辅助动力装置的空气进人: `+ P8 O/ k; t# G Q- e9 I 气源支管的活门。发动机上,用来降低压气机压力的活门。* @( D0 t3 v9 ^9 [5 y- H6 b! {* W8 x2 K; o) i4 }" W* j+ e( n$ Y1 b4 [, L. b! R( S. {; n7 Y: ]引气活门, U4 K: f5 E$ {4 a* Z英汉对照民用航空词典B OEING # ~* g6 W1 }2 }+ g# lTECHNICAL DICTIONARY 21 z+ U2 ] b% R4 k" Z4 X; DBLOCKER DOOR, A device on the engine for blocking0 _9 |/ v6 C8 ]& h8 K1 f the normal airflow during thrust reverser operation.: B! H+ C3 {& k* I+ U) e# c% t$ U LOWER, An electrically operated fan for circulating air." s# ~" H& y( O LOWOUT PANEL, A panel in the structure between0 D: y& g% T3 { o compartments that opens to equalize pressure in1 {+ f6 m3 s5 [* Y" n8 V, y; U e compartments. 8 v v: Q0 j/ R& w4 pODY GEAR, The landing gear attached to the 0 q) ^/ _- _& b p) ~/ ^grounding.. R1 j- o9 {3 z7 i 正常的 ! F G3 N4 ~2 v) `3 |气流。 ; }" t, |& `" c- ^鼓风机,5 m9 `% q0 y2 Z# N h4 r' ?1 ~ 用来使空气循环的电动风扇。7 C2 V9 g( B" {1 t2 }8 u 压口盖, + J. [' O; N& Y) ^- ?0 B$ y两个隔舱之间的口盖,打开后可使两舱压力相等。 ( q! a" r) J5 ]: ]; l% j身起落架,; l7 _# y6 @! `, _" ]; L 身构架上的起落架。' R, O2 I" d$ j B8 t$ E6 r4 c* _1 f. C9 j B" u* U$ i- J' D tw $ x6 j% |1 Z( w' `3 \th / W% i3 G! {, H. i p' d6 j1 p1 G4 dB ) p' x% V- _: L2 F7 }fuselage structure. ' }- u4 x- J0 CBONDING JUMPER, An electrical connection between. ^* r3 c: }' m' Z ^& e" v& P a component and airplane structure for electrical ; F+ n8 [+ U% \) O1 d, V阻流门,: \1 y- p& `) u5 q4 W( H e& E, U& R 发动机上的一个装置。在反推工作时用于阻挡 ' ^0 l0 i- a3 i/ B! Y5 c+ I6 |" @& _, B0 s" A1 K M" W6 D t 装在机2 {6 C4 K9 Q) `& n 搭接片, 0 T8 L( {! W- W% q连接某个部件与飞机结构以形成接地的电接头。 $ J9 {' x' `# W1 p0 E0 e! p8 C" K英汉对照民用航空词典B OEING % b e' Z; s3 Z4 D1 l' W1 nTECHNICAL DICTIONARY 22 ' i" I% N- X, o. ~& {" j7 uBOOLEAN ALGEBRA, A mathematical system for 0 o$ n9 Q$ b* _$ t& N# Mwriting combinations of logical statements.6 Q+ m* ^, Y( S5 }2 d BOOST PUMP, An electrically operated fuel pump for' g: K" p7 ]- j2 y0 ] fuel supply from the airplane fuel tank to the fuel: @% K$ C4 d3 I) x" U) ` manifold.8 f+ K6 j& @: z0 W" D3 R3 d, [ BORESCOPE, An electro-optical device for looking at7 R2 e. `, N9 S0 h ternal parts of an engine through holes in the engine. # v9 T/ f" Q/ y& aorescope ports) . {& N/ p! V8 R5 a( H; u. q' XOURDON TUBE, A curved flat tube in a pressure gage: J, O5 `3 n x; S r moving the pointer when pressure changes inside, |$ {. q% m9 g on the ability of the brakes to ^& \8 [( i1 Y9 }/ `" {9 m! t1 M bsorb a predetermined amount of energy during a % b8 N. q% p" a- n& Y* [6 w& Njected takeoff. 9 J2 J: f" c+ ~- |用于通过发动机内的孔(孔探口)观察发动机内部件的- M( a0 W7 w; A. F 光设备。+ ]. m1 H; ~* d! |6 ^1 _3 g0 |% M0 I 端管, P# H) v/ i6 H E0 y测压计内的弯曲扁管,管内压力的变化时它使指针移; E2 b3 Z1 l# I W0 a) B. p 力。 , r4 f$ H, @2 P( \. J, j& n/ U极限重量, 6 d- A# K/ u8 o0 n. C+ G* o( q3 P' J2 j/ z起飞重量。 0 Y9 E# s( d- t* F发动机滑油系统与大气相通的通气口。, s4 ?1 s# {( z6 z: u* l5 ^ in 9 Y& j2 g; `7 n" G6 V(b7 p, K4 a" l5 M0 _: m: e& t B/ Z; C) U2 l) E5 G fo& Q3 C/ F8 q3 l7 F the tube. 3 T' j1 v5 C X i1 \8 VBRACKET, To enclose or surround. : ~1 W( t5 o0 k2 QBRAKE ENERGY LIMIT WEIGHT, The maximum ( p" U- k6 v* g# d& D/ gtakeoff weight based' j' B$ {) y( a a) \& i4 p7 N- D! {& u3 g3 p' T re7 R1 q4 G( k [% Z BREATHER, A vent to ambient of the engine oil system., P b- Y9 S8 X* \, | 布尔代数,6 D" N% i3 _& L5 N 一种用于编写复合逻辑命题的数学系统。$ [+ T9 u% R# v& a 增压泵, # t+ l6 `) x/ ?, R从飞机油箱向总油管提供燃油的电动泵。9 s! S$ M, L' F t6 x& N: u8 O 孔探仪, 2 T, C7 I% a9 {) S; \! \& Y5 ]4 j. q8 K' @% p' x' }; Y# r6 A动,以指示压 e! Z: u, n# x7 p8 p 托架, # w) N2 \# X2 D6 L# _5 Y用于作支撑、装托、或围绕之用。6 W9 E8 b# b/ c7 y 刹车能量 . h: d' Y' D k! K中断起飞过程中,取决于刹车吸收预定能量之能力的) y I/ @3 b+ w. I" `0 e! Z0 q. m6 o$ W: P& i 通气装置, * q/ P0 P7 V( _7 ~* X英汉对照民用航空词典B OEING % _$ T2 E" O3 S6 B. I$ zTECHNICAL DICTIONARY 23! \) w) o% e2 ^( \! [ BUFFET, Vibration of the wings and airframe resulting . {& A. d m1 P6 r1 tfrom unsteady airflow over the wing; caused when 2 h6 W* L; \; t; f! U! Q! eairspeed is too slow, the bank angle is too steep, or. j8 M+ Z3 s# Y% a3 o irspeed is too fast. / b8 x" T! s1 s% V# _8 f) A- ` s$ HUILT-IN TEST EQUIPMENT, Equipment installed on 9 o' A- { I+ G/ Qe airplane and in airplane systems to test the systems 5 y6 V3 h9 x1 S! y7 xithout external test equipment.1 a# K7 T% L+ ~9 o, ?3 S$ z UFFET MARGIN, The amount of residual maneuver. E G- |5 d* O2 e- U$ N5 A apability present before the onset of buffet.4 @+ _0 N9 o) B' s9 ?8 |# _9 }# S UG SPEED, A preselecteed speed to be observed2 l( z9 h: q, w/ | nding sequence. ) e" Q k* d/ ?2 w' pk 2 I* s1 o' H% S" M, w+ Y5 P7 sng landing gear operation.1 F7 c- u* W3 D. n 速度太慢或太快,坡度太大,均会引起抖振。 $ L0 {' c8 X' @, T4 j5 \自检设备, 5 n/ s& Y& J& }, X) J+ x4 \7 W安装在飞机和飞机系统中,在无外接检测设备情况下, + ~& s. g3 ~$ P1 g% j4 ~用于检测系统的设备。& T7 i+ U1 ]5 d 抖振裕度,. K1 M( {% F% q) Y( g' Y X# \ 飞机在遭遇抖振之前,剩余机动能力的大小。0 L+ R6 b: j- a5 O2 ] u 标速度,/ K/ y, ?6 w8 H+ ^# w% f 在某些机动飞行过程中,特别是在进近和着陆时,飞机- W% s3 E3 R8 Y# S( D7 R 预定速度。9 @) [9 s* I3 {8 \7 A+ A C 力装置,* L) n8 W& K: i. _7 A# M 架工作的一种机械设备(弹簧或减震器)。! m+ r" a, C+ F0 r1 K Q 流条,7 Y! N; Z$ `1 t) H# q3 D 在部件或组件之间传输电、数据、或定时的单一电线或) P( j, l- P/ J8 W0 K6 {" ]& s a: h h/ |3 x. E, Q B ; G* _+ p T/ sth6 c+ q9 V) u9 L. z w: P% I3 P$ I g. e% f; x B+ K& P; _0 z4 O c % [0 X, W ^3 E' I! L7 DB 0 e* [2 i( p/ a' fduring certain maneuvers, particularly the approach and8 E! B4 \; j `& A% Y$ n& z+ r la & t G' g: ?. R6 ^BULKHEAD, A structural partition in the fuselage or 4 x* t+ X: ^- Gwing. ) e7 y( R" R* {9 fBUNGEE, A mechanical device (spring or a shoc 3 Z& {8 {4 c% ^9 `$ G" I9 K: u1 dabsorber) for assisti4 w S/ @7 h2 D& h$ d( H. v BUS, A single wire or group of wires which transfers1 {& G9 v* `+ R, f9 J+ y power, data, or timing between several units or $ o0 V0 V& }! l& B; Smodules. 0 V' C/ b" }# @' U抖振, l& L* F6 A% M t由于机翼上表面的不稳定气流引起的机翼和机体的振6 I6 W( q8 ]7 K% ?5 T6 k 动。飞行 1 S2 I9 G2 y2 s9 Y. o! r9 d' } y& r- W% Z6 i 所应保持的5 t0 a( O4 @1 L% ?2 `% Q 壁板式隔框, 8 G3 s7 X0 n$ `8 Z1 a+ I机身或机翼内一种结构隔板。 3 ^0 Q- ~6 @9 F: F9 t$ |2 o' d) f |, E( o* f) ]用于协助起落 " z' ~% I. c1 p) k+ ]2 z& [2 \4 @& g. G8 }' `) _' R电线组。; R2 I/ m& j ~5 g9 L7 \8 l" s) f' C 英汉对照民用航空词典B OEING 8 g5 S8 G/ H* VTECHNICAL DICTIONARY 24

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BUS DRUM, A mechanical connection with pulleys6 Q* o% B1 ~- c' y/ ?, Z1 f cables in the control system. # H+ s1 Z# f; ?4 J0 D# t5 y$ O5 z! q: Rand 4 N5 S$ c T% c& @l circuits for control and protection of Y. [2 T) X) U! I9 i, [: N- l& Ulectrical alternating current supply to the airplane.1 X+ V" X! ~! y7 Q, P+ N8 v; C duct for closing and opening the duct2 a- \" ]. {% ?. e S, Y8 d assage.$ v% y% O( |: Y UTTOCK LINE, A vertical reference plane along the/ Q, P; B$ r/ e: q selage for horizontal measurements of the airplane." `( G2 J3 e0 M+ Z# C. h0 b* q: b 接。; L Y8 a3 l! l 组件,内含控制和保护飞机交流电源的电2 [: B2 h* J& |. G( V6 a9 i# j4 w8 S" i2 r' O9 b/ G# W: V) O 作动简控制的转动装置。用来关闭和% c% e3 U/ y9 @8 x" ` 启管道。 ) g( p& i5 t2 a( h+ D5 W沿机身走向的垂直参考面,用于飞机的水平测量。) g) E4 x0 y0 A1 }; m BUS PROTECTION PANEL, A module (black box)# U6 L- n; ^' U* } containing electrica $ @& T" Q5 k( b! y Q+ `e% Q* @/ j: S, |1 L5 Z7 B! N! ~; X BUTTERFLY VALVE, An actuator-operated, rotating* G. m! F. ^( k9 p5 S/ e) q device in a3 `7 G8 y) g' M7 I6 C$ d0 D p ) z8 f& ~0 c3 ~8 w+ UB; ?$ F: m- U3 p L2 C* y, `4 u) }$ L fu 8 }6 x/ g w$ F( L4 K: ?转动鼓轮,, ?* Z! X _( F 在操纵系统中,具有滑轮和钢索的机械式连 7 {# a% u# B- Q2 q# P B4 Y汇流条防护板, - [5 @, B0 z* w. `+ ?/ j黑匣子式的 + p, T3 E* f* q6 ~% i% g0 W" e8 F" h$ Q蝶形活门, / X, x" ~) f5 b% V3 A是一个在管道中由3 h8 `( |- O7 e/ V6 n# i+ T0 h" s. G; w* r1 ?- ~纵剖线,* W F# D o8 @ q 英汉对照民用航空词典B OEING * ]& r6 T, e! ^# b' X \2 f1 M+ fTECHNICAL DICTIONARY 25 ; s- ]# @, b7 ~8 \* bBYPASS VALVE, A valve through which air or fluid will $ v4 d( g* {8 E9 U6 C2 z a! gflow if the normal flow path is blocked. 7 X$ Q' O0 \2 I; VBYTE, A group or string of binary digits. A byte is + B, t4 ^) k6 L6 I: A" H5 |( Usually eight bits long. . ?& [: g) R) e0 ~ABIN ALTITUDE, Atmospheric pressure maintained- e5 A9 n3 _ d9 q5 [8 u ithin the cabin, indicated in terms of feet above sea " o, b9 X. g: g' KALIBRATE, To repair, adjust, fix or correct the4 w* y& v1 t* s0 }# E' F- I easuring capabilities of a measuring device.: I! m/ y7 H, u5 S0 R/ ? ALIBRATED AIRSPEED (CAS), Indicated airspeed/ q; F" h( O% J' t AS) corrected for position error. : c' h" N% Z- {! X; lnical ; g* P2 [) Q6 M' x) Xomponents. : x) m# |3 R2 r- j) w& J1 z' x! D) J, I节, 4 f5 D( U8 r! f4 \一组或一列二进制数。通常一个字节长8位。 6 F& c: a8 }5 g舱高度,. J; c' U2 D( {# Z3 y 座舱内保持的空气压力,以海拔多少英尺表示。( D2 V+ C/ |1 o$ e5 u 准, $ z& H4 P' {( _. V6 R1 G修理,调整,定位或改正测量装置的测量功能。# i' }# ?* ?, g/ [/ f 正空速(CAS), 3 F& k4 c7 w% M1 }2 H, @' _在修正了位置误差之后的指示空速(IAS)。3 U( J2 Z+ ~$ _/ H6 C! x+ O2 i 用来移动机件的一种转动装置。 + t: }; K/ T- T! m" V: \u) ?$ k( k0 x: i o5 d* o% s C 2 O+ Y: N8 l9 m" h5 ?C# e( v6 [: E/ K- K- q w$ O; o7 u) g+ _" Q$ j; v$ I+ w level. / `' c5 l, k0 o6 ~3 L0 q RC . \; Q* O8 F% ]5 u1 S- s# Dm - h, Y% u4 X! HC 4 c" T3 R6 P- @ [8 X(I1 Y" c/ l# \) ^ CAM, A rotating device for movement of mecha 6 I5 E# M! j! b3 p2 NC : l! N5 I7 e t! y1 K旁通活门 - v% a+ n/ U; I' k- R) x9 b8 e气流或液流在正常通道阻塞时所经过的活门。$ O. R2 e) f" n9 I4 n4 n6 k1 T, I' q* t) |& k5 w$ v8 T. V% j8 J' X' D8 h' Z- ~9 I# Z2 C6 A# a% s8 h, @: g凸轮, 7 Y0 `& A' v7 o) w8 ~英汉对照民用航空词典B& Z, P J J& [4 j CAM-OUT, An autopilot condition in which the actuator 6 p& |* ^& D, e) k) n9 E `( b& Ldetent piston is overridden, either manually or by the * h6 f& a; e+ X( s% O7 R% }8 j3 S# }ther autopilot actuator. : W$ O' P/ U z- b/ K% A0 |AP, SEE - CAPTURE 0 I) O& e5 V) F; w+ \6 h7 oAPACITANCE, The measurement of electrical energy 6 U! S- t3 ]: z4 Xtored in a capacitor (condenser). # H8 i$ [& Y2 S9 t2 T0 y: iAPACITOR, An electrical component of two metal / T& ]' I( v* R6 c' K! Olates separated by a dielectric material, for storing 3 u: M+ j% T; `" P1 ^* c+ R% Mlectrical energy.3 f. `% D# P- P. h' }( c CAPTURE, An autopilot or flight director function to( j7 U% i) U* D; e acquire a selected mode. % y2 y! c" S7 r8 {4 |CARD FILE, A container on the airplane for printed " |% ` m2 X/ ^7 kcircuit cards. 9 s k6 Y: J; B+ N$ ~1 B一自 / Z, J& E4 I% n% T+ X; }动驾驶舵机所超控。4 } H/ [! E9 |6 Q; D/ r/ f 截获, & c4 o; d4 }0 Y见Capture ' l' {& d. A; X2 r8 \1 Jo ( y4 h" _. G. l Q$ K6 Q8 kC# {" y) K* _4 i C* P" p3 e* g* D1 B s/ x% [( F$ @$ Y/ u5 G C 0 I# v" H& ]6 w/ N5 e; Fp- F- R& f" a, v; ?2 {4 K3 H {5 P e, H. |- B4 l. ^% Y# g 凸轮不工作,: H* o G6 W; k2 ]+ O+ B 一种自动驾驶状态。此时舵机锁定活塞被人工或另 ' u5 ~7 z9 r1 n2 |' n3 j& o$ }7 V0 |0 Z1 @电容量,% m# l& s C3 m% o0 e n 电容器内所储存的电能的量度。 8 [& V% s. N/ C. n0 a# P# A容器, ' j" D' O }/ Y5 L, J. X两片金属中间用绝缘材料隔开的电器。用以储存电能。+ b/ @6 c. F" x+ B- E 截获(CAP), f2 z* w% [+ U. X" U+ R5 `自动驾驶仪或飞行指引仪的获取选定方式的功能。 ( `2 O- Z* u7 E( g线路板盒,3 f3 J3 u" M7 |1 N$ [8 S! ] 飞机上安装印刷线路板的容器。0 a0 }; ^* U7 J! [+ U; ^3 |4 A& D: A8 `9 ]( ?( H5 h, w% U OEING $ o- |3 `2 u$ J5 JTECHNICAL DICTIONARY 26 B5 t: ~- q: e英汉对照民用航空词典B OEING5 i' ]6 X0 h" X TECHNICAL DICTIONARY 27/ ?. ~4 D- z7 f* [& g1 ? CASCADE, Two or more similar circuits or amplifying ( V' ^2 J! S4 H$ g1 gstages in which the output of one circuit provides the' b0 I; U" ~. k9 ?: U6 o4 p put of the next. % y+ ^6 h2 l9 g2 M# CASCADE VANE, A vane for turning the engine airflow ' ]4 x: m" Y+ Ouring operation of thrust reverser. 1 @7 Q5 k. Y. l3 {9 I' w/ ?ASE DRAIN, A drain carrying lubricating and cooling & F N/ s) F( _& Wuid from a hydraulic pump.6 b3 a' A, [+ U" c/ v ATHODE, The element from which the principal! d- S) b' m4 A3 T/ w: A1 j tream of electrons flows.1 ^) W- ?5 m# n8 H1 f ATHODE RAY TUBE, An evacuated glass tube with a0 D# O7 O* I2 _1 I# l, K CEILING, The height above the ground or water of the( D# P- t c' M3 O4 y% g. p1 d base of the lowest layer of cloud below 6000 meters E9 N* j" s+ y& O" n2 i- U; K0 x% @: d(20,000 feet) covering more than half the sky. 3 L2 |7 E5 }) r9 L程。该 7 f. y4 C! O% c! d5 D* P, I程中,一个电路的输出为下一个电路的输人。 : ]6 C$ U$ T7 F5 L叶栅叶片, ( o% h' L/ v. C- A! M z. K在反推工作时,使发动机气流向相反方向流动的叶片。 4 y; ~( `5 o: R$ _$ C) `' b" w匣余油管, m( t6 O9 f0 f( [/ {: o& L0 I 液压泵多余的润滑液及冷却液的排放口。6 t' U1 q0 y1 Q2 k5 a" p/ V 极, " ?& ~6 B* N: Y; z0 \" D2 y, s电子流流出的极位。 ' s7 r, _+ k1 [: g) @; K; o! u$ S; P极射线管, : N$ x. D+ C3 C* z* R" m- f有显象屏幕的真空玻璃管。用于显示信息。 " h1 R0 M+ q- A, H! l! a云高(云底高), ; O0 A: Y7 h# L- F8 g2 v1 L/ I6000米(20,000英尺)以下已覆盖一半以上天空的最 . R6 {' `8 v/ B低云层底距离地面或水面的高度。 7 F9 e/ k1 y0 |; Z( tin * p; E) f0 t! R5 l3 c7 HC/ m% q1 Q! D6 Q/ ?4 L3 |( B+ P3 E' [2 [ d' P& N1 q- i6 j C ) i8 ~- w8 q& E% d i' Vfl* M8 v2 ?# C2 Y/ {8 G9 a3 P2 { C 7 E) Z2 u7 B; X$ x! v9 |s $ \. {! u) n/ ^+ q9 L$ B4 D+ ?C1 W/ e' v3 r7 y% Z" r, ~$ u viewing screen, used for displaying information.$ W+ M, K+ M, P& s0 t: l. S6 A$ Y, t 级联,3 M% Z8 L) f! g/ l 两个或两个以上的类似电路的逐级连接或放大过6 ^! p/ G6 `, U' Y% t) W! J5 q# D" A; h/ V2 y5 j7 F# B! o* g9 l0 R6 b: V# B- z. |& h8 h4 u$ r! Q& ~( S. L8 ~ 一个具, ]! g1 m, c- s8 d% q: R% S 英汉对照民用航空词典B OEING 6 v4 C! E3 Q& D9 L p7 r$ bTECHNICAL DICTIONARY 28. b$ p# H8 C# A CELSIUS, A temperature scale in which zero is the5 a, T; v2 q) G freezing point of water and 100 is the boiling point of , h2 E% M7 d' F3 @+ xwater. 2 z. O3 w$ F7 Q7 L2 e5 M4 mCENTER OF GRAVITY, The balance point of an object! v1 S( L+ h. Y5 P/ j. P- G' _ r rigid structure expressed in terms of percent Mean . a/ X; Y* h5 berodynamic Chord or in inches from a reference point. ( p' j. Q6 { t+ q7 M& o& m/ J9 J. dENTERING CAM, A cam for moving a mechanism to a0 d8 J( l3 F! _7 m F' n eutral position. * N0 p6 Q- p& |2 j; T) SIGURATION, A configuration of the ; f5 f: E$ h) c4 J# D* s4 Xircraft approved for operation by the local governing $ r, y, K8 S, i2 Sgency. y% `+ k+ E8 a6 ~7 @ENTRAL PROCESSING UNIT, In a computer or, N: I1 K/ t8 c igital circuit, the section containing the arithmetic and 9 z; {: i- i6 [$ {# \" o: C9 tgic,control, and internal memory circuits.: F( T; T+ d; k$ c8 D8 _ ENTRIFUGAL FLOW COMPRESSOR, A type of : |9 \ M! T6 B+ Y4 {ompressor in which air is taken into the center of the5 ]" Z8 C* h. P& g1 a peller and is slung outward centrifugally into a diffuser ! q( \1 t" V; M- p! H( where it is slowed and pressure is increased.0 O4 c# t o& I4 `7 S CG, SEE - CENTER OF GRAVITY ' Y8 t$ \) N8 d) Z+ s构的平衡点,以平均气动力弦的百分比或3 w( f4 x, q" B: T8 ]# E: t" W; ?- z 某一参考点若干英寸来表示。; G2 G$ B* t' ]3 N V# Q 中凸轮, # t% C3 c/ v& }! S- H/ n; ?将机构移向中立位置的凸轮。 H) Z5 N( h X 格的装机状态, 0 o3 B) e ?4 m2 N由当地主管单位批准使用的飞机装机状态。 ' p. `& S1 q' u, m% a( C% W% a9 k. F2 Y中央处理器, # n) R' ~3 [. b" g8 E( ^计算机或数字电路中含有运算,逻辑,控制和内部存 1 l9 k u5 E z+ n( J6 }储电路的部分。- N$ D R0 }# J, N1 w, A2 ` 心式压气机,$ X# @4 c: P: R h 压气机的一种。当进气到达叶轮中心时,被叶轮离心抛 1 a5 I5 E! E4 q' m! h& l# x进人扩散器。在扩散器中气体流速减慢,压力增加。 / }% Y& g# w4 H) l& k重心, 9 ]" j% ]$ s p见Center of Gravity 1 `, T0 x% H0 f; D4 N) fo! V7 F* p8 V) V4 b5 o4 ]; O A @5 Q1 ~4 A1 n: V$ Y8 e7 G4 F5 CC + v, }) s3 C0 y9 a9 rn0 @9 |' c" l8 `0 G5 g CERTIFIED CONF 9 l1 M# }2 Z( n4 n# Z% e' `$ L+ aa , W; \. |8 v$ ga9 I/ Z/ Z/ m% ^ x) N) T$ N C . a6 O; _- \7 |- [7 zd * d' }) P, G* u8 ~) {( F; Alo. V6 F- j( K" c7 m- [7 |2 g3 q; L C. Q$ Y& m' ]7 Q4 d j5 X5 K% t/ J c ( i" R7 R5 r! O, Gim" }! l$ _& g B" l8 }4 }/ W. P0 D w $ K, m% |* p. @4 m3 S1 r& C摄氏度(°C),, J3 `; y0 @8 @; o- E 温度的度量单位。在此单位中,0°C表示水的冰点, ' Y3 E5 O& Z1 O$ e100°C表示沸点。* T, k6 S+ }% w) x- ]% R* m 重心; d, q- X+ }( m1 N5 B# ^" P3 @6 F 物体或刚性结) ?' o0 l, k) g ]: F# Z' P6 W+ B/ `# I( D3 r3 O& S. V: V) j% r9 y$ L) p* B8 W/ ~9 t6 y( W8 W2 `7 a P- e1 o5 @# C0 k1 Q. H' Y6 t5 U7 t. H英汉对照民用航空词典B OEING6 o' m* @ Q5 u. L% d TECHNICAL DICTIONARY 293 M3 f- _, D$ s CHANGEOVER, Conversion from one mode to another. ) h/ v5 P) @! H* ]* |: ^7 hHARGING VALVE, A valve for supplying air or fluid to+ O- @' h# Y( A9 b HECK VALVE, A valve allowing flow in only one 3 j( {9 F$ G+ q3 @irection. See Non-Return Valve.1 O* c1 D' U1 a5 w HECKSUM, In a computer, a summation of digits or . j! l" s' P/ R8 K& E, ]5 Iits which are primarily used for error detection.# O8 f) w; o I7 O' j( Q( u$ z HIP DETECTOR, A magnetic plug in sumps of 8 n) @" u7 a% j1 E0 gbricated components for detection of internal failure of $ {+ D& q4 F0 B) Ee component. 8 H- n6 a+ r9 s7 jHORD, A structural component of spars or frames. + }( E' n) g4 ]- r0 Q$ H* _$ y添活门,1 r' p1 S5 F i/ e3 @& X5 A 器充气或加液的活门。1 e6 ^* n1 ]$ _% M9 X( A8 c; g 单向活门, 9 y6 S ]3 p% G/ |, q! h6 [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 $ f) ^/ O: s% k0 S4 H w% ka reservoir." }+ I1 |1 Y: D* q4 ^9 } C7 e& { }* n. a0 U& l d+ u, o* `2 c0 y9 W, T( H4 H7 a/ F C: }" ?4 j# t$ n b) S$ W% K. W$ ~& C C) i$ G# i& F1 v; F: T lu # X) H& b% F$ Q! P+ O4 @- Y3 }, t+ Pth 6 q( s/ b* C3 M: |0 C. a- `& mC" L- \" N! Q' m8 C C7 { 转换, : [- N% ^5 T9 F2 P) K+ O- w由一个方式转换到另一个方式。) M% I! u: Q/ m3 j3 u4 A3 ?7 h7 N. E2 J) _' E3 c. t3 [用来向储存 # f. C/ p! D6 q- I) S( w' i( i. c2 ^总和校验, . ]" ^$ m7 z" v2 d9 d9 `5 Y计算机中,把那些用来探错误的数宇或位数的总和进( Q/ W3 V2 X3 S1 x; n# g 求和计算。9 C3 q0 W( |2 p2 B% I; t# | 属碎屑探测器,+ F& \2 }* c( ?9 @; U* W 装在被润滑的部件滑油回油管路上的磁性塞子。用来探0 E9 d8 v8 `( ?5 ?7 m U" ` 部件内部有无损坏。 8 X& B4 r; w- k) j. i- i, v弦,7 D: s! B8 x$ P$ j( n( }5 d 梁或框架的结构部件。, p" y. G5 F8 b* B7 G+ B2 U4 k$ }. F: S( R1 H E* b3 A8 K0 R2 k: h- V# Y* C4 b( m% i- O3 o1 w6 I8 c7 t1 Z( j2 X) b" a }% V) m2 K# h8 n8 B英汉对照民用航空词典B OEING 2 D$ }- @8 e0 S$ q& C- hTECHNICAL DICTIONARY 30 & v6 h/ ~. F! k- K7 \1 V; vCIRCUIT, A closed path through which current flows. L& R1 ]9 ~ w ource.: E% {! O& j; c IRCUIT BREAKER, A device that automatically0 t( V, E7 A* x @ eactivate the system." Z4 g6 j( K2 g5 d& H# @% W' ^ lear of all non-frangible objects which : O7 c3 ]! T \* Vay be used as takeoff distance available when * d1 G( P. k o* j$ x4 walculating a takeoff weight. / m. I8 ^& D/ N5 ?, mr water under the control of the appropriate- H3 q3 Z" i* O) u" ~ uthority,selected or prepared as a suitable area over # H. T9 G8 p: l+ F& A/ Qhich an aeroplane may make a portion of its initial 1 `6 ]! l1 p" g6 flimb to a specified height.8 L7 \5 w2 N7 T7 X increasing.& {' Y4 _) a0 ?4 W* H sed+ |% N. h N! ]- ^. x LOCK SIGNAL, A continuous string of pulses used for, r( f9 |* E6 o+ @ \- q) Q& ?: ~ 开关,+ I/ c% ]) G' X+ i 故障情况下自动中断电流以保护线路不受过电损' b0 j0 O' m5 C5 m, [+ O 体障碍物的区域。在计3 }8 q# \- S, H9 i8 Y4 { 起飞重量时该区域可作为可用起飞距离。! ?. N& Y% ~0 J 是在有关当局管辖的地面或水域内一个界限明确的长2 Z+ B3 _* W, a2 w1 A$ `# ` 形区域。在这个选定的合适区域内,飞机可完成初始爬 $ \1 q9 [8 [2 r% m的一部分,上升到一个指定高度。& N8 H, K4 A9 r0 b; q( e& y 飞机高度不断增加的飞行阶段。: w3 ^: A7 C- Y 钟脉冲,3 d% K; Y! e9 r 步的连续脉冲信号串。 r* b) S) ?- E" A& F from a source, through various components, and back- T& }& M A. d" B# H- d% l9 | to the s7 |, W, i5 i8 X# E7 p* M6 ^ C 0 A# _$ P6 u3 ointerrupts the flow of electricity (current) during fault 8 h1 x/ O- L0 O! Ocondition to protect wiring from excess current. Circuit l( g6 D* G! w$ n" U vbreakers are also used as a means to manually 5 X6 t* l/ M3 G. Z1 _( Hd7 O0 j# \, G; O; _" f3 d' y CLEARWAY 1, An area beyond the takeoff end of the + ?) Q7 D3 J: r3 `+ i' J0 Grunway which is c8 G2 U' @2 }# S4 ^ i6 |* j m" i' C( T" `( A' X" Q c 7 j- F! C( x% {$ [CLEARWAY 2, A defined rectangular area on the+ p: P# O4 z/ ~ ground o3 M! v; c# ?* s- m a : E* H3 D4 i# t2 g3 B& I8 K" ^' m4 gw 4 s! p' A9 C' B. R6 j, Lc Q9 C6 `/ ~9 ]" @; Z CLIMB, Phase of flight where the altitude is , O! }$ \2 e6 Y4 r; O( d8 ?$ xCLIMB LIMIT WEIGHT, Maximum takeoff weight ba; C- V w! E8 U3 o1 F$ `+ j2 s, g on a minimum climb gradient with one engine; M$ b" G6 t. b) v' ]9 e" x* y7 C inoperative.6 E5 x1 U, u' g- P2 W4 L) ` C- K* \, ?! E+ D' z synchronization. 9 G9 }. S T' I3 m7 p3 i6 \$ E电路, : W9 F+ s/ o$ a6 S# ^2 Z& O- E6 t一个闭合的回路。电流由源头流出,经过各个元件流回 8 o: Y5 A+ H# S' u* x源头。& { A! O( y3 t' j- N# F# I$ p9 `9 p& g( e/ |8 }: N' c% v4 K 能在' \ J( t& O8 l+ k8 k: W 坏的装置。跳开关也可用于人工使系统无效。5 N, h! {! q1 U1 J+ f* g3 g 一号净空道, % Q: `, u8 q- c6 |5 i5 }6 \是跑道起飞端以外,不含任何刚0 E: a) F& {0 w+ m: U6 [" a6 Q. w2 J- ]& y( C, O0 o0 Z二号净空道,+ ~7 W7 O5 i" k* {" t! M5 c; e8 g O4 n" [5 j8 R. x/ k7 S# | j( w2 T9 H# c爬升,+ }' H5 W6 {: f: _% }+ R1 F/ D. A 爬升限重, ( x2 O9 B4 \9 U, J) i取决于由一台发动机工作时的最低爬升梯度的最大起& e* ^0 \) Y2 b" I 飞重量。 . Q( ^, ~6 [7 B4 J1 J2 L" Z: M' n/ b6 w q% V 用于同 1 z4 \+ N/ a* H J英汉对照民用航空词典B OEING9 { g' q3 \) [+ F. G! W& Z TECHNICAL DICTIONARY 31, Q, }: q# X' f) M! M COALESCER, A device in the water separator for4 p+ l5 f, y( }; ` F9 T; J ollecting moisture from the cold air. 0 U" s* Y" n6 K/ on antenna with a receiver or transmitter. 3 ^- `7 C8 w6 f5 ghe cable has an inner conductor and an outer( C5 \, z2 v5 R1 S( y' f rounded shield.( l) _5 q2 Z6 `6 \0 Y8 L6 @ ting one inside the / b, s5 O( h) N9 L3 `8 P: u+ x0 Bther for rotating the low and high pressure! W7 F0 p9 f$ Y% M ompressors by the low and high pressure engine5 F, k+ C2 b! U rbines.6 h9 J: R2 e- i" Y1 i: _ OMBUSTION CHAMBER, A part of an engine for ( j1 V) o' F" `- W! hurning fuel in the air supplied by the compressor. / {6 D7 J6 }9 \ p$ l( X置。 ; X3 g# [' h% P& _' u( t/ K射机的电缆。电缆+ z! v- Y$ q$ Y& Z0 T) v 中心导体和外层的屏蔽所组成。 8 A [1 M1 v9 B2 V两个套在一起旋转的轴。用于使发动机低压和高压涡轮. t3 `* h) Q" A7 I) U 别带动低压和高压压气机。 $ s4 c8 y, I% Q; m" Y烧室,# C* _% q4 c1 C5 D g& X7 Q 发动机的一部分。用来使燃油和压气机所提供的空气相 8 h; ^ }+ T6 @- k% g+ N$ K合而燃烧。

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发表于 2008-12-24 21:38:35 |只看该作者
c 5 a3 t3 {, _3 k: d9 rCOAXIAL CABLE, An electrical cable usually" w/ [1 Y4 o5 `" F g$ R connecting a 7 A3 l R# }9 `T- K2 t5 \0 n) z h/ h& [ g% C( D, c; p7 ], I# ? COAXIAL SHAFT, Two shafts rota & t# i7 y9 j9 F+ o6 C9 Go % E8 z% ]5 N% f: V4 p) w7 Qc- r1 I+ |/ R+ M tu0 U3 U3 {3 V3 H9 B- w C9 M9 Y6 h( w& ^/ i Q b , S' c9 l6 d& {& X- ]' ^凝聚器,0 j A% \+ `/ K, U$ v9 i 水分离器内收集冷空气中水份的装. F" i) q* ?5 h+ P$ S 同轴电缆, - G3 v6 W, y' x" ?" Y# b b- B/ F# O) s一种通常用来联接天线与接收机或发 1 W2 e2 ?& h2 | |6 u4 _# D" R% s+ ~2 u4 o9 n; j. I& m同心轴,6 l- t+ f3 ]( J# T1 @* t8 y( A- v. H5 l# F' e6 P3 M6 }1 c- D/ }7 [0 H- z8 B8 c2 G, r( g( J- ] 英汉对照民用航空词典B OEING; s' W) Q; w, j5 Z/ K' J TECHNICAL DICTIONARY 32 ; w* s/ d0 {1 Q; C+ b3 [# m3 Y4 SCOMMAND BAR, A flight director pitch or roll comman 8 o* a' G' j* r' B5 W! x7 p( T7 Windication. % F( W+ V! w! x7 s' X/ `# C5 Vd: f3 f- U5 z6 e! m$ Q* H1 }5 B! R OMPANY ROUTE, A route flown by the airplane6 Q' p$ M- T8 E k OMPASS LOCATOR, A low power, low or medium9 A5 t5 C$ U4 {. _ equency (L/MF) radio beacon usually installed in' a/ v; e# q/ ^2 ] onjunction with the outer or middle marker of an {% `7 O- G0 ftor (LOM), A compass . {" e5 V5 m3 }$ O' h" Llocator installed in conjunction with the outer2 |1 A+ w6 p7 E4 \" v9 T0 d marker of an instrument landing system. 5 J+ Z% Q, t q, A) b3 @2 [: G+ K% @ss; A+ `4 K. O" A; J. h# g le 5 G, s- f4 O; G fOMPENSATION, To offset, balance, or counteract. 3 \7 i- g- ~: g2 k. T) KOMPENSATOR, A dual capacitor for changing the fuel1 L; C' L7 b& r! `( [ aging circuit capacitance due to changes in fuel - f( g2 {+ h: O! |ensity. + m' {+ R( N/ ]+ {& A9 q# S" d LOMPOSITE MATERIALS, Non-metallic materials used/ Z8 f; V4 Z# z0 Y9 Z; G0 ] r airplane construction. Fiberglass, Nomex, Kevlar, , y3 e& X* A) T+ M7 Kraphite Epoxy are composite materials. / W5 P. H( B7 x3 v司航路,: p& l2 g2 p+ i' p7 b 在飞行管理计算机数据库内由航空公司飞行 C1 {0 K$ l" e7 x& }; y盘定位台, # b( w6 z( T6 v与仪表着陆进近系统的远距或中距指点标配套安装的3 w# Q3 U7 C/ E. S 功率、低频、或中频无线电信标装置(低功率NDB台)。/ l8 Z" o: F5 q6 ~6 U7 o7 Z1 _ 程序中用来导航。* q v! A% j( o! Q7 R2 @0 m 1.远台, : N; f! e5 @1 U0 I与仪表着陆进近系统的远指点标配套安装的罗6 ~3 Z/ }1 B7 V" W 盘信标台(NDB)。 ' x% T) e0 O( i偿, 9 Z# v+ t6 `0 C; J$ H0 M$ ^抵消、平衡、或中和。 2 S8 _. v; n- a1 e" J偿器, 5 u4 i3 g3 d1 M. V. a' k/ J在燃油计量电路中,用来改变电路上的电容,以与燃/ A7 a7 B8 b n% ^; C. j* d5 m% @ 密度改变所引起的电容改变相抗衡的双电容器。+ ], |- a+ r u3 d2 |* B7 c: R- ^ 合材料,9 \2 u! y5 Y- I8 V: Y* o 用于飞机制造的非金属材料。如纤维玻璃,Nomex,: M2 q$ ~, |& o 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 3 C h) Q3 t5 k, Z* e; yoperator that is normally stored in the flight - q$ I( B1 ]) Cmanagement computer's data base. ]4 X! x1 ^- Z9 M# J& b5 D) w( _C. }" q0 u' r7 h, L$ v2 F2 _& F6 R fr * J' q: n4 v) _/ M$ W4 jc ( c( g, k$ i0 s' D0 }5 N! i% Vinstrument landing system (ILS). It can be used for* F0 \/ z9 u9 b& `2 V- b navigation as authorized in the approach procedure. 4 k5 A. ~8 j8 h8 Y# D9 D- {1. Outer Compass Loca , ]* I, z7 J5 c0 Y2. Middle Compass Locator (LMM), A compa 6 b0 N1 d" L6 Z# ?6 J2 tlocator installed in conjunction with the midd. @* M! S0 q1 H- t marker of an instrument landing system. 7 q8 M# {. N. a5 T7 R2 i; jC % _+ K- L% ?+ r. F* eC # v4 O0 e3 `- d9 v& N8 Lg ' F+ k! J, w6 b. E9 c1 F- P! q: Fd 0 _6 w7 z. B* F Z+ Y' LC % l! n' l, r) J3 rfo O7 P( d$ j8 p# R: C3 T g- j) u/ `0 x e: p" k 指令杆,' g( P! I+ E* G$ }+ [ 飞行指引仪俯仰或坡度的指令显示。 5 \) U7 Q" w9 s8 L% T9 F0 `4 @ ~! i8 S: f8 y. z* N9 }通常储存 4 h& _) l3 g: R8 I' m2 z的航路。7 } C) R; p, T; w' w% ?; ?3 h. f& o' \. v" `$ G7 {: s2 n0 M% f- d2 {: k 经认可后在进近2 D7 x/ Q. V# D& H 2.中台,* Y, ?+ j( x/ f% Q5 S& T+ c 与仪表着陆进近系统的中指点标配套安装的罗2 d7 X& z: J$ B# L* X2 f! m 盘定位台(NDB)。 # \# m" D. q. Q P9 j. P$ g. `4 R3 @# O) b+ q: l/ }, w( T5 x7 a4 q; q, {% k: h5 M1 T2 J8 T: ^) y7 Q: Q: L- e! ]$ W3 K; u- h, v$ }K . Q6 \( `5 _1 w+ P, S4 I: w英汉对照民用航空词典B OEING ]8 n4 K# M, e, E TECHNICAL DICTIONARY 33 m8 ~6 Q5 i% R8 C, D+ Dby 0 Z* V0 W/ y8 Q' nor increasing air - P- u0 r& i8 X' p4 S Lressure and temperature before the air enters the' h8 r, J9 L4 q) k7 K ombustion chamber, Low pressure compressor - front 8 U L ~7 J$ b+ H. n! f6 \ection of compressor, High pressure compressor- rear. K. t% j5 i7 B3 T, k* v OMPRESSOR STALL, An event that occurs when8 }8 a1 I% t5 `# Z ere is a complete stoppage of air or reversal of air flow* E- C: H) p! X I% ^ COMPRESSOR SURGE, SEE - COMPRESSOR1 @- z: }* c* w- @ ^4 ^ STALL COMPUTED AIRSPEED, Indicated airspeed1 L2 X7 g I+ c5 S3 e corrected for the static source error.) s, _* R9 U4 N; I) Q 的机械轴来驱 - n! X; b6 j7 M6 d; g+ K,用来增加吸进空气之压力和温度,以供燃烧室使用。 ( i0 H% q8 j$ D; f+ {9 ~: K压压气机—压气机的前段,高压压气机—压气机的后 6 z6 F7 V" T6 z4 f* o: Z. c; D$ `- @" L气机失速, 8 P$ s8 P) e" G% }% k' ~当气流完全停止或通过压气机时气流方向逆反的一种 3 V8 l' g; o2 N( m, t压气机喘振, * D, v7 x" J0 W$ P9 K见Compressor Stall ! J4 `/ C0 ~: B, U$ V: H6 m" ]COMPRESSOR, A rotating part of an engine driven# X: n/ h r5 o6 h& f a mechanical shaft from the turbines f 8 u) v. V! R* U* X0 |9 o- K+ J# Up . j/ ~- i3 h/ d- s6 v k# g1 F5 r0 s9 Ac2 U1 p" y2 L" a s ' p6 d2 w3 a; W( F( `section of compressor.1 {3 }- T( e$ ^4 o8 H* j- u1 j C % \7 M3 Y6 h: @+ \1 c0 `th % ]- R5 {' a$ F7 S. o+ J0 uthrough the compressor. 3 g/ k4 E8 H- t) [( @) q# B# P压气机, 3 g, P: p- Y( b& A! _发动机内的一个旋转部件。由与涡轮相连) r3 ]( [5 ~$ C1 C ?) h U2 s, L3 V. p# y4 k8 z7 S6 T! p* ? t' n4 X: \* t0 L+ P; y( d2 } 现象。 : ^* p" d* t/ J* q3 @: x6 j3 I: @$ c; r0 L1 \* L 计算空速,. m3 ]. P6 }4 c" z6 @) v0 z! P/ u2 G 修正了静态源误差后的指示空速。 3 W# N7 `% s; w) H- ~英汉对照民用航空词典B OEING , @* y6 R z/ g5 t" nTECHNICAL 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 # P9 g7 \- D( z9 R# U. z4 k5 [! c+ Poperations, manipulates data, and makes decisions.) q$ r" g" Z( d( q' U ditioning4 U0 q" X' [3 p5 O the air and the5 y; o: s0 {5 J frigerant or moisture vapor is changed into a liquid.2 Q) k0 \3 |6 a) g% A9 \' ~ ine - C( o R& `4 gONFIGURATION, The position of flight controls,: \% X+ T3 P$ e/ J8 ]# _4 E C- S missing which" j( g7 f5 A. A% N$ s may affect the aerodynamic performance of the6 O0 L3 f% Q. o; z+ o6 c4 Y7 N airplane.' a* Y! q* [' v d0 I+ G 置。7 s7 j' B4 W1 @+ {* t6 H 中能使热能散发到空气中,以及使冷冻剂或湿 / a9 S4 @8 r$ B3 ~0 `# M转变为液体的部件。" V" o9 ^2 o- y7 w 连接到飞机结构上。 1 F6 |( F& i2 _- @) G/ g8 {态,! }- O/ [- j& ?9 t4 H* Y 定飞行阶段中,飞行操纵面,起落架等的位置。1 L& f( ~6 Z8 ~3 T' G$ R ), 2 I/ M6 D- r8 Z5 _* g8 O受到影响。3 g. l$ _# y+ o CONDENSER, The component in an air con6 S) G, i1 m$ ]8 f6 l system where heat energy is given to 1 Y; o- D+ H6 t! \( @( s: y, _$ l% Z9 ere3 Z0 a- H3 u. ~. j8 X Z. y CONE BOLT, A bolt in the shape of a cone for eng ; W$ Y& d8 z) d2 N6 z; Z) j5 Nattachment to the airplane structure.3 C3 g' R0 F, E3 `6 r/ h C. j' m7 Y2 n# s7 H n) S landing gear, etc., for a particular phase of flight, e.g., 0 |' ?" u- ^+ l0 ]1 Q9 jTakeoff Configuration, Landing Configuration, etc.4 t8 [# k2 K% p1 j6 V CONFIGURATION DEVIATION LIST (CDL), Appendix) m! S/ _( l% N, a) q& s in the Airplane Flight Manual (AFM) allowing operation) n; E7 y+ q* i" | of the airplane with certain airframe parts 6 u" L( M! V- U1 b9 v+ ]! O4 ^计算机,( k% W' L: D# N0 A8 K) u 能作算数运算,数据操纵,和决策的装7 E4 _. X: U- [/ b8 z# p: i# w/ ~ 冷凝器, ) r: Z: r9 C6 K空调系统 . m8 Q/ Q2 I1 A$ J& D9 G" L9 l- c锥形螺栓, 2 Y: p7 v/ N, ]( g+ o外形是锥形的螺栓,用以将发动机/ q# N5 o4 [& I6 g% b: Z1 T2 j: w# ]* ^, F3 Q6 I' y/ |$ c4 r! q 在某一特 ! e+ y# T# v' `% q' _, _如起飞形态,着陆形态等。 0 _/ `( ^! Q, C7 ]缺件单(CDL ' D& L! f* d3 j5 l飞机飞行手册的附录所开列的飞机上某些零件的清单。 # ]: U3 `4 o: N. r& ]在缺少这类零件时,可以飞行但气动性能可能$ p2 K; R; Y5 i 英汉对照民用航空词典B OEING! f( ~7 J$ Y) K TECHNICAL DICTIONARY 35

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发表于 2008-12-24 21:39:49 |只看该作者
CONSTANT SPEED DRIVE, A hydro-mechanical ! b- f3 z& z3 }0 V$ `6 ?component for changing variable engine gearbox speed 0 ?% o5 `, S! wONTROL AXES, The three axes of the airplane which0 [" k* G1 R8 e5 p8 k: E$ j+ n re perpendicular to each other and pass through the& _8 \8 Q$ k7 w+ m( c4 B, y3 M; V+ C enter of gravity of the airplane. 2 ?; P6 P2 s# i! x, z; H$ YPitch axis - Horizontal or lateral axis, passes through9 _ z( `5 W X* a9 f% \ o: Z the airplane from one side to the other - 4 S+ n+ u+ y" P: c7 E# Z& ?; Unose up and nose down control is by! W5 ]3 g! X' X. j8 I t0 M+ q elevators (and stabilizer for trim). / a! P5 X+ n0 l$ {* QRoll axis - Longitudinal axis, passes through the 5 w. t0 J, Q2 mairplane from front to rear - wing up and: z" S2 R8 ^7 j$ ?) H8 |4 v/ i wing down control is by ailerons and( k) T0 X$ l& S/ t1 @ G flight spoilers. ) o |! ^9 D: U2 hYaw axis - Vertical axis, passes through the $ r2 ^0 y$ e5 c* vairplane from top to bottom - left and . u# N4 G0 L0 s1 Tright control is by rudder.& f5 j* F* J! Q. ~- N) G 置, . ^) X# v3 x5 H' ?制轴,& g: V/ e4 H1 j2 e4 o( I1 Z 通过飞机重心互相垂直的三个轴。 5 n/ R2 w1 c. H) x俯仰轴—又称水平轴或横轴。由飞机的一侧通向另 ( u: U0 F4 W- s$ P0 ^侧。飞机绕此轴转动即造成机首的俯与仰' p) ?; F# M: R3 w4 R9 r) ] 俯仰控制是由升降舵来达成的,水平安定* j Z! a( t, { T7 M$ W; H' O W3 I: W+ H 则为配平之用。 5 Q; T9 {( f5 x# B& {" u# y横滚轴—又称纵轴。由飞机的前部通向后部。机翼 ( f0 w1 _. J* ?/ i" Y) P下运动由副翼和飞行扰流板控制。 , c) _$ b6 v0 q1 a. X偏航轴—又称垂直轴。由机身上方通向下方。飞机" q1 `+ B* Y7 r$ i* U) t 此轴转动即造成机首之左右运动,此一运 " h" }( N+ L3 c, e7 f5 Q" m1 w7 Q由方向舵控制。, {) R- T' j+ U: o2 o* o to constant speed to drive the electrical power.7 Z+ I" ]/ g- d9 U, K C5 q7 J( W$ Q& Q3 v/ N' Z0 ?) B* x a$ H4 P7 g2 |0 C c 8 ^7 R3 s, H% g1 g, F恒速驱动装" z( k% h& X9 d) s1 y- S( R 将发动机齿轮箱的可变转速转变为恒速以驱动电源的 0 ^. W) E8 e9 x2 c& [$ H液压机械式部件。1 o" `* u0 `1 W$ @. { z7 `, {7 _! G) A0 Z3 D& L5 i& E$ B4 ~& S, c2 Y0 W* {8 Y+ V( _7 @* D/ ~. U+ D6 W* n Y/ e% ^$ v6 J7 z( Y. B7 N7 ^$ l2 v; A: x2 ^3 Z" c6 m8 x 英汉对照民用航空词典B OEING* c, i4 G' U2 q9 r2 G+ X w TECHNICAL DICTIONARY 36 ' ]8 {, m. Z3 ?1 h) FCONTROL COLUMN, A mechanical component used$ T* c# C( ?$ H3 h6 \6 G rs - t! A; n. c, V) B8 rnd elevators. . T ^, Q6 i1 C: C0 H0 [ONTROL SURFACE, Moveable panels on wings and& X P3 g( y, G. R( {6 U0 E il for movement of airplane on pitch, roll and yaw axes. ' j7 j/ H/ J+ dONTROL TAB, SEE - BALANCE TAB, c' x' ?2 ^. s; R ONTROL AREA, A controlled airspace extending0 r, @# ]+ c' j8 c" w5 @: p* f pwards from a specified limit above the earth.' V+ N9 N+ L; f3 ]: g* k1 X- l E ONTROL ZONE, A controlled airspace extending8 C3 [/ @$ F4 Z' G* I& S pwards from the surface of the earth to a specified6 B# ]; e7 j9 |* _2 j" w, T pper limit. 8 s; |4 t7 O0 ?5 ais ; h5 p/ z1 `& G h) ^$ q: _/ qo IFR flights and to VFR flights in accordance% D: C0 b# e5 p$ E6 {. l3 q with the airspace classification. ! ?: z' h6 H: O8 r# [# L" p, U. T机械部 8 {: O0 w9 ~( @; f% T2 h/ _& \; x7 u 操纵面,: M$ e N" T; q2 B7 V 机翼和机尾上的可动面板,用以操纵飞机俯仰,坡度, Z3 [ u0 m6 d, P* L: d和偏航运动。 / f1 G; k8 F9 T0 w, U操纵片, 2 `# c& D3 E" A, J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 spoile4 ~3 w6 J5 L5 \! p: m a" U# V9 d9 p/ Q( P3 Q C( b W+ e/ Q5 U; p$ @1 q+ }" h! v ta3 q! O' |8 w$ }% q8 m# p C 2 A+ ^! _1 m3 K cC ) ^8 d; n! c- I! O6 K) Zu( A+ ?3 H0 y6 \# [0 D3 e. M" @, ? C4 b+ k3 n- M5 ?+ F8 c u& `7 ]/ q; X1 g u : i& F! G( S" T! qCONTROLLED AIRSPACE, An airspace of defined- e/ Q) X. E" x" {- c dimensions within which air traffic control service/ |7 b$ q* D( L6 t& {) e provided t # G- e* Z# H" Z$ V4 }驾驶杆, 8 r" ~& y4 i `% @飞行员用来操纵副翼、飞行扰流板和升降舵的 8 c: X! n1 |6 z4 K! e# A& U' b+ j# d1 q3 x( k" i1 d* k) p管制区域, ! F0 K! R) p: `高于地面的指定极限以上的受管制的空域。 5 x8 s& I5 K8 G4 p" F. J制范围, + Q* _+ T3 P! @1 Y) T/ Z+ \6 J由地面到指定的高度以内的受管制的空域。 + T q3 K4 l, K. v$ G3 y( i1 P0 V: X一个范围明确的空域。在该空域内,仪表飞行规则飞行# X$ v7 N* c* t8 E# |- c 和目视飞行规则飞行有空中交通管制服务。6 G+ Z& ]5 [ H3 R: A* b5 O# ]+ v. O( L( a( b9 L8 \受管制空域, 9 v2 V. e0 M# [) d英汉对照民用航空词典B OEING" F: K h" [3 O( s7 ^ TECHNICAL DICTIONARY 37 3 m, ^- _( S6 M' T1 O5 M" {CONVERSION, To change into another form.4 E. h+ W5 D" E3 O/ R, y COORDINATES, The intersection of lines of reference,5 E# C9 W3 U+ w: G3 i H0 L$ C3 ~ sually expressed in degrees/minutes/tenths of minutes* Q$ l! ~/ `+ k. v5 ~ N f latitude and longitude, used to determine position or9 U- U+ [9 _( \3 z% a) C: a2 ^7 J% r CO , Y2 K6 C% Z: |; udestruction of th 8 j: }& n% P _: b0 W& H) Dchemical conta & E. g7 @, ^ H- `' w: g' `COWL, A remo * m3 [. S( `3 C' W. wfor access to th1 W( ?. e8 `7 j5 R1 D Fa. J) A; x/ ~. b8 w( D Nose Cowl - Front section of the nacelle for air inlet - W8 A! J6 g/ Y& K% jto the engine.6 Z9 b- w4 q0 k1 b1 K h Side Cowl - Cover around the sides of the engine. 1 m: N0 J5 R' R+ {" F7 d; bThrust Reverser Cowl - Cover around the core- I/ \( _4 Y0 Q2 p6 d section. 7 ]3 z- |0 i% ~+ W3 \' b1 YTranslating Cowl -The moveable outer portion of the1 R: W' b' y1 s- X* ~1 @5 t' V+ ] thrust reverser cowl which is - @8 X5 j% w0 i7 _! b& ?( ]* ?operated during reverse thrust. ( G* e2 Y9 i$ t7 s标,: P0 }. X/ _2 s; R# u 基准线的相交点。一般以经纬度的度/分/十分之一分 4 D' J4 `4 P, L8 W) ^6 [$ E! o读数来确定位置和方位。 ; T- F$ B0 w3 s. n5 G# Y& Y C- ^腐蚀 - L$ Z, j( X8 G s2 f, }9 ~动机外部可拆除的罩子。发动机上的构件必须要取下1 m# K' _ x+ f7 J( Q$ K$ e. l 流罩后,才能够到。' d2 |( e! `+ ?4 I# t- C% C g6 F' m8 K3 k. A* h机的短舱的前段。 * J Q/ w5 J+ l侧整流罩一发动机两侧的罩子。 8 n2 o# s, h* |! `反推整流罩一发动机主体外的罩子。; w7 R# s& m$ M, K ^* L 移动整流罩一反推整流罩外可移动的部份,在反推工 + z/ y- d# y3 L" R作时使用。 ' i$ }7 t+ Q- Y, G, ?% gu 9 m' T- R$ g! oo, q" o# Y1 Y* F* N location.$ t& B( v* K4 ~2 ?# _ RROSION, A chemical action which causes gradual" A# v! w+ ]0 ~ e surface of a metal by oxidation or - q4 z4 q) c$ i2 H) D1 X0 amination.+ l% C6 i9 X3 v+ z vable cover around the engine sections $ ]8 P) o1 ]4 c* Ye components on the engine. 8 z6 d3 }9 s% ?* z0 N* E' `n Cowl - Cover around the fan section.0 y5 H3 [4 r6 D7 g" O" y) a 转换, & v. V% s' _) b4 H改换到另一个方式。 3 {( U( ~3 n; \% a* k- c$ V1 B4 \% z2 g8 e$ j4 I' X. B7 ?0 G, z8 \; v; W$ I" b; ^% e& x$ @( |# ~$ D 氧化或化学污染造成金属表面逐渐破坏的化学反应。 # P1 q P5 b1 g, b5 A1 e/ z5 k发动机整流罩,5 ?3 d; R: f* l1 t) N# s7 R9 E' H9 @( u/ [0 D7 l7 |- |- ]4 p, H+ K; s* @/ Z扇整流罩一风扇外围的罩子。: j, y9 T: h$ \, y+ ~ 前整流罩一引导空气进人发动 7 q4 J1 g+ \* [" W8 U" u2 H英汉对照民用航空词典B OEING+ L+ k# p4 q" x0 P+ Y- `* G TECHNICAL DICTIONARY 38 + N7 h. i4 J( }+ LCPU, SEE - CENTRAL PROCESSING UNIT 2 Q/ |1 z: _; R# J' JCROSS TRACK, At 90 degrees from the desired track . s$ x8 H7 [) e2 Zf the airplane. For example, cross track distance is the ) k# V& ]& d' u8 |( i, h h0 Xistance from the desired track measured 90 degrees8 R* q8 @/ Y$ M1 g om the desired track." [7 N0 @; N% r f, @* R ROSS-CHANNEL, Electrical wire(s) connected from3 [) ?( X$ F3 U2 U. ? ne system to another like system, for example, FCC & q8 x$ M7 {# Z% G" to FCC "B"./ S5 p; n* O4 x6 T7 l9 z n adjacent engine or one on the other side./ @ C& k1 t4 u! y( V: P( y) Y8 A( v l crossfeed " n* I8 c) i6 q9 m' H* p4 yanifold for fuel flow from one side of the airplane to the ; o9 ^. x7 r' w, Wther side. ' S) m7 W7 ]' X, N. \6 S7 ore- B7 M7 X3 ?: f; H3 P RUISE ALTITUDE, An altitude or flight level 3 T7 s# i" f, S0 p) n. L3 T7 K! Q, ~9 U o g* ~# \, [( X9 k7 O* F d 5 v8 s2 f% f7 t$ T8 ufr # b, p, C' C3 O: _C % o4 _/ \$ `7 R2 uo m$ _9 d% o' @, r7 N1 v! q* W "A# Q& R. x: ?0 T, E' m CROSSFEED, An interconnection between fuel; t" e, x: H5 W. R manifolds for fuel flow from one side of the airplane to4 n) Y$ C% x* [; \5 P a% q8 J& Z+ t( p, m9 W$ X/ e( E CROSSFEED VALVE, A valve in the fue $ } ?: E0 {& [" F0 Q+ H& y! y Bm9 L9 u( ?. P$ U, ~& M% ?2 | o 8 t" |6 r0 M9 B2 ICRT, SEE - CATHODE RAY TUBE( u+ h, \- u# M9 o- O) \5 } CRUISE, Phase of flight where altitude and speed a- I" v* Y7 F6 t1 h% Z R4 m basically constant. " P' {6 ~+ }2 w6 L' g& f' HC! e4 ]! c4 l5 y2 I1 C/ o. i maintained during enroute level flight.& `+ X {/ R! n4 J/ F+ E( y$ }! p, ^ 中央处理器 8 G& s9 V9 a6 O" T! y见Central Processing Unit. 2 r* Q1 x: o" O& b交叉航迹(XTK),& Q7 b/ M3 e. W, e2 g( J' ]" { | 与飞机预计航迹成90°角的航迹。例如,交叉航迹距离 : p) J \, ?% |. \4 |# \8 E# E9 f是用与预计航迹成90°角量取的到预计航迹的距离。 9 B8 O w5 `# l通道跨接, Q% }7 f# K9 s0 G, p" V 电线由一个系统接到另一个类似系统。例如:由FCC3 H% X9 c' d( ]) z9 g1 ? “A”7 F. m, m: ?; }7 R5 _% w 接到FCC“B”. # T Q; k2 ^0 I' i机身另一侧的发动机。 & H2 E5 @; w1 g; q于使燃油从飞机的一侧) k) P Q+ }5 ]' c+ k4 ]6 B 向另一侧。) Y" }1 U' J( z) u' R" m 见Cathode Ray Tube- `, m* {- \! q 交输,% `7 D1 P7 {. z+ s( e 燃油支管之间的交连设备。可使燃油从飞机一侧流向邻 $ {+ c7 _( n) }& D. g近的发动机或在; h" f# Z, S2 ]) @$ s( m 交输活门,5 Y- F) t4 w: V- ~! p# k" J7 \ 燃油交输支管内的一个活门。用6 n1 [% ] o. C! m: A* ]' }' {3 ?; G3 e, O阴极射线管, 7 U1 ~% y N& D- e% p& ].6 n p, I. N W" b 阶段。1 d& e, Q N6 W1 t 航高度, " b7 S1 w8 I6 m飞行期间,飞机所保持的高度或飞行高 ( k, I: H, A: K3 w. E3 ?' y" A巡航,% g1 I) R/ u' Y2 X6 L5 C( _ 飞机的高度和速度基本上没有什么变化的飞行3 w! c5 z) H. i) F5 X5 c' W4 s1 }# J4 Z4 ~在航线上水平 1 Z2 U# x4 V: Y* R9 Y9 F/ B( z度层。' X% ?) \/ w$ M 英汉对照民用航空词典B OEING $ }7 u4 `. X) H8 P+ j nTECHNICAL DICTIONARY 39 & C# A' ?1 ]$ K; i" B6 ^CSD, SEE - CONSTANT SPEED DRIVE 1 N( o+ `& F2 Q2 ACURE, A chemical change which takes place in a resin, f- c: \% [5 W3 O r# `/ H$ v and fiber based component causing it to solidify. . M1 [1 P6 ?4 ^7 l! h2 d$ _5 L( ^CYCLE, A complete series of events that take place + a9 `4 M' l, t5 x& j; Y* Bgularly normally in a continual sequence.2 `+ E$ u6 L" ]0 B5 f b AMPER, A device for slowing down or limiting 9 R( s/ Y+ U9 e0 KDASHPOT A mechanical damper for slowing down & G. B2 T, X! o3 ~! s( i/ X. Govement by restricting fluid flow.1 I3 U/ p6 b4 x0 c7 a: K+ Q D % T0 q9 {3 T3 rATA BASE, Stored information which is used as the 1 c4 D o6 b2 y$ `2 [8 mba6 Q9 q% m: M0 W9 R6 U8 n DATA BUS, A conductor over which digital data is .. ?' B d. v8 A6 Q2 |& e1 S transmitted.+ Z% J4 ^8 ?( t8 N/ Z DECELERATION, To decrease in velocity.1 |$ `( T" P) L% @) D 装置,: H3 A* d7 j0 O6 M) U' m. R rive ) w: d1 h- K6 D6 B$ [6 Fre , h+ ?, y& F" s. R' bD: V0 Z: z {, \& j# ^9 R D, W1 S3 ^7 e( K- L! \+ ]4 ^, u& s movement. _: ? e# j5 l i* [1 v$ `m q$ w3 w8 @% l; B; e2 R C ATA, Another name for information.) k* c2 d$ I! ]" Y9 b9 o( V D . }! r2 {) y; rsis for computation.6 e! i0 ^1 j3 @: T1 }9 T 恒速驱动' N6 s6 |9 _/ H* B S/ D 见Constant Speed D . . x# G% a$ k' A; I" o$ j期," f5 Y( _; p1 ^( E+ b; S 不断重复发生的事件的一个完整系列。 3 H0 c- A% ~' X$ ?8 W4 h7 F尼器,) A5 d: S- K: h* @1 v 慢的一种机构。/ ^" F( Y, M3 z4 B( R' i" Z3 q0 m3 w* x1 K4 U用限制液体流动的方法以减慢物体运动的机械式阻! A; ]9 y) d( Y& B5 b9 ^0 I4 [4 X) r5 p5 C; L7 {" o; o8 c$ }3 }. M" o3 E/ m 料的另一名称。4 C# ~! L4 y* x- D0 Q4 T 据库, : b1 j' _8 h$ Z F" `! W数据总线, 4 o& K4 i) k- ~1 q一条或一对导线,用来传输数字信息的通道。 % j* ^! O, x6 b' O- h, j& M4 U+ `' L减速, 1 |, N/ `# P* b0 Y5 u8 O! d速度随时间的递减量。) @/ I" t/ @; P! z 固化, 9 B) X/ S0 `; A2 B树脂和纤维部件内化学反应使之成为固体的变化过程。' Q2 b" t8 O" I/ _+ L2 |& N+ ^6 g f. u. W; B2 Y0 N7 C9 ?# `% ? A9 ~0 j8 B 用来使运动减9 [' y5 D" g2 ? 冲器, ( l0 i; H6 F: P器。- T4 c q! w. d1 C) v) e9 P 据,( \' e- u. k. c6 ]* G7 h& R9 [% S9 K0 o/ i, {" l z6 P# R1 b 储存起来以便在计算时使用的资料。 ; ]9 `& q) n* y5 x7 M5 e英汉对照民用航空词典B OEING ' i3 U6 e! w4 x' E# d q: UTECHNICAL DICTIONARY 40 % d- J; _6 e. ~% _+ U/ |1 E+ gDECIBEL (db), A unit of gain derived by computing the6 ?/ B: V" t! {0 a8 P3 Y4 G3 z tio of input power to output power.8 k" o, J8 B$ n3 @& Z. S ECISION ALTITUDE/HEIGHT (DA/H), A specified 3 w8 O# l" b" H% h3 Sltitude or height (A/H) in the precision approach at 4 b6 L' ~' ~! t" {8 D0 W& d7 ]5 xhich a missed approach must be initiated if the " I8 _7 k. _/ P$ j4 _1 S' x2 D+ iECISION HEIGHT (DH) 1, With respect to the9 f) H4 ?/ V4 n+ `# k proach or ) E" Q8 U% c, h2 Vexecute a missed approach.7 T2 \) V( P3 G- b4 @: X( K9 l0 c proach to trigger the decision of either : ~+ ?/ m$ P# Z I$ C# Hnding or go-around. 4 H" x# |/ j* \9 [- eECOMPRESSION, The loss of internal aircraft air- m% L1 f; s/ j5 V ressure.5 r3 |4 U, J# w% l$ ~7 y! L E-ENERGIZE, To turn off or cause to not operate.# S8 _5 ]4 m3 S. H rom the tanks ( y5 [1 n( T1 A+ ?7 qusing airplane fuel pumps or external suction. $ k4 Q! ^: E1 l& Y8 z% b+ g k3 M算的一个增量单位。分贝 : e% @& m& A) L常表示两个声音信号或电力信号在功率或强度方面的 8 c) F. A) Z: q2 m5 i7 F- W3 v对差别的单位,相当于两个水平的比率的常用对数的十 3 `! C4 _1 M5 r3 r断高度/高(DA/H), ! T' x9 S1 d$ z4 a+ G" D在继续进近必需的目视参考没有建立的情况下开始复 6 e/ A' C* v8 a1 ^+ W的精密进近中的一个指定高度或高(A/H)。 6 U+ V$ R: H! c, C! A% T断高(DH)1, ; d/ T8 e( _+ |7 E) N4 q操纵而论,指在使用仪表着陆系统或精密着陆雷& J7 f3 j5 d1 u3 r: x+ W. Y 生继续着陆还是复飞决定的高。 2 ?$ C) T9 A( o2 R L- \( [飞机失去内部空气压力。 ]# R9 F; Z, y/ T; w开, " J# N$ X* n! s7 s1 q. I5 t$ ^关断或使不工作。 1 F l" e! E8 Q5 h( z机的油泵或外部的吸油装置将燃油从燃油箱排$ R5 m( K F. o 出的方法。. [1 O9 U/ U, u' O! q4 H1 ^2 Z) L ra : }9 V( m6 b! J$ K( o* t' SD7 g( G8 Q3 E4 u) ` a ) }' M. J0 U5 mw, ^# y& r: v% A$ H+ K# V required visual reference to continue the approach has 8 I/ D7 o+ Z2 j5 {) Enot been established. % D$ p! C' ~! E. f' z, YD : ]+ x* H2 y* f2 O& t# }operation of aircraft, means the height at which a) c* E2 v: |+ _2 s5 W3 r% V decision must be made, during an ILS or PAR & {4 a+ d5 s& A0 einstrument approach, to either continue the ap0 \* G8 c2 C; j" L2 h1 P; \& T) k6 u to9 x3 ]) S( _! Q: H% t0 L DECISION HEIGHT (DH) 2, An altitude used during a0 A4 x2 s! I- C' @7 y3 m O2 n precision ap 5 a8 ]3 Q5 A2 y( ola ! k) y# S& \6 M) e: I5 ED 1 E6 h) Y" F( `; x9 A. z, V- rp 1 V# ?7 N/ Q) [# J8 `D9 H3 L% N7 y3 F* M3 ?* M J) V- R DEFUEL, A method for removing fuel f 7 O B6 V/ {8 ?3 O! ]) D分贝, " s" z; ~; P) D% ~, C e* H# Q以输人与输出功率的比率来推 # W: J4 _' f, Z% b/ p$ N$ R: m+ @ L. a6 b& G3 U+ U& n7 S8 a3 Y: E! K9 J1 P5 a: L) R% r# J2 M# m+ |7 v$ ~# ]- E: B: }0 `0 k* X. h* Y7 _9 A' ]) U+ V+ b! c# j( j7 U' @+ Z$ C2 s' t就飞机" y$ ^. o6 X. I 达引导进近时,必须要作出的是继续进近,还是中断进场. k. m/ X: M; y) L0 x. [ 复飞决定时的高。 ) N- _- c3 J7 v6 K决断高(DH)2, 8 b- E' i* u" V; @+ O精密进近时产 , \# I* Q' m+ A) R- r8 g$ q N4 {% L$ A$ ]失压,2 ^8 K2 E5 T! \ v, H. K( G- H6 S: f4 M排油,/ s$ {+ y; ?5 s0 a4 c: c 用飞 P% z8 } c+ E4 e# Z9 F英汉对照民用航空词典B OEING$ P* Q0 {3 o4 @" u4 A+ e9 F% B TECHNICAL DICTIONARY 41 3 Z4 h8 A% r) ~- e: c# m* hDEFUELING VALVE, A valve in the fuel system for , X5 w, S# Y7 |$ |& Aefueling the tanks and for transferring fuel between the+ j# w8 p7 S x, V: @ E-ICING, Removing ice after it has formed on aircraft." O# I! r8 z- Y/ @7 G" i Change or difference.* `2 U0 w& l5 `4 N' J EPARTURE CONTROL, A function of an approach 2 _7 B G5 h% _8 x; u$ y8 vontrol facility providing air traffic control service for3 ?- ^5 j5 H! Y eparting IFR and, under certain conditions, VFR. Q U3 v7 Z, E- {. b& v" T EMODULATION, The process of retrieving information ( Y8 B; _1 e8 j3 c5 y# ?carrier voltage. ! T; a7 m* u( @( {# y9 P; j/ [: u5 oation. 4 Z; t3 |+ A/ H, n) i! Glic 0 q$ K* t- T C1 N, X* c3 |0 ucreasing hydraulic reservoir air pressure to " {4 z+ \8 \* Y0 ]9 S# gmbient pressure. . L# l2 U5 x, r1 l' W8 T! J4 B箱排油和在燃油箱之间5 |! b0 B* I! I) v 送燃油。 ; u$ V |# P) K冰, + |/ s9 M, Y0 y$ S- {: i5 i- c除去已凝结在飞机上的冰。 5 v" _+ R1 v$ k/ R. F4 L删去或取消。 ) S: ^% o. @; g! a% e5 t) m量, 1 P! q! p: d' R+ F' X/ V( a变化或差异。" K3 L" c9 g" E* @; h7 x; n+ r ] 场控制, ) B3 I/ a, U! u% ^+ |& s给用仪表飞行规则离场,和在某种情况下用目视飞行4 `0 v4 l0 J2 }& h( u 则离场的飞机提供空中交通管制服务的进近管制设施/ L* C6 G; x! S. Q2 t; K1 l( ~8 W4 j: \9 I- d调,7 l9 B! ~0 G9 D# B+ ?: i2 T% n$ | 电压中获得调制电压的处理过程。 ) g& u4 q: _2 d. r! Z1 A环境( h! Z) I; h& W 力相同的活门。 # Z8 n6 g1 Q% a" rd 5 f+ _7 M k) j$ h3 n$ u9 ~, w' gtanks.0 q* m; H' Q9 v D7 J P/ z+ h9 G* V, z2 J! }0 p% R DELETE, To remove or cancel. 3 o+ S3 x6 y: v. \5 V. [DELTA,* p* P+ r' s% B! j& B1 y! W% j D / F& P: I0 ?% B3 C1 V/ g( \c - c) u, I" k3 ]: W# p7 g1 od & E, A4 ?3 b/ {/ Raircraft.. |7 K7 _ G! S' c% j D$ \) A9 I s+ _" m (modulation) voltage from a modulated / I# M' x" l" x* SDEMODULATOR, A device or circuit which performs: s/ V- Y% u8 `$ \9 [ the process of demodul 7 A" ~8 `) V+ p& h/ c5 b5 v, jDEPRESSURIZATION VALVE, A valve in the hydrau / }* [1 _+ D. b; ysystem for de' a: ^& Q, c' |) x. o( W' C( w% K a ( @2 r; V/ d+ f5 y7 }排油活门,0 I) V. Y% x! `1 ^* X 燃油系统中的活门。用以为燃油 " O. L q1 K ^- ]9 V Z6 j* A# r: ^$ U+ e' T% S/ S" i. i h# E 删除, L4 a& A8 ]4 K7 ?+ K$ I- B# d, p/ J" {( t1 h- I: b1 S3 w# q' Y/ w! L2 y' u6 b7 ^* e的一种功能7 R8 H C. h/ s' v, M- v8 N' R5 @% Y% W$ q# E- w0 ~, S从载波 8 s5 F" w g4 P4 M$ t解调器, 3 W, c6 J$ x# z9 }) U完成解调过程的装置或电路。 + b7 T" A& J7 @4 u减压阀,- S) @/ y8 F% d; ]$ ], U2 O' w( {" J 在液压系统中,将液压油箱空气压力减至与周围 ! M9 v5 A3 r3 p- H, v8 _$ i! Z! g# O: ~ S( l4 }& e8 v8 k英汉对照民用航空词典B OEING - L6 P; M2 R, `+ P! E, h& HTECHNICAL DICTIONARY 424 B$ ?2 |4 K% ^6 Y DESCENT, Phase of flight where altitude is decreasing. + ?" _" V; {7 ~0 N" mETAILED FLIGHT PLANNING, The calculation of fuel 9 n& L# D4 n4 o+ End required for a trip by considering each phase of " e" D2 {, G; a/ |; h5 @: y( {ight (climb, cruise, descent, reserves).* z, H9 G! j" O al or* V5 K7 O; T* s" P# @ ETENT SOLENOID, An electrical solenoid used for; H7 B8 {; @) R t.; y' R) {; \) m+ m specified course or ; c; g8 z6 W& o. y( orocedure. 8 J' q* O% {, b. D( {& X2 he.9 J: O9 m6 k1 _( Z! i 飞行计划, * [- a+ b# N1 _" T2 Q将航班中的每个阶段(如爬升,巡航,下降,备降)都 & D/ k0 `0 U6 ]( a' v! s, y1 B7 Y6 g人考虑,来计算该航班所需要的燃油量。! l% }- }( @- ?) d; W 用来感应情况之正常与否的电气装置。 ' h4 g' `* a1 X: R& Z$ X6 `定电磁线圈,2 Q" ?+ ?- Z. K$ G) } p+ A* N 出接通的电磁线圈。9 K1 i3 ?! Q4 ^8 v( e: e& W 差,! j2 Z' |9 N S 与指定的航道或程序之差。4 P/ Z' p" z+ D; e* p' O) C 用气压或液压操作的活门机构中的柔性部件。 3 _6 u$ s; b' ~" E V: E7 L/ t0 uD 8 _( a0 @2 ]/ Na p1 V# P6 F% E! d) J8 Y, h+ F) X fl3 `: h1 n7 _! f5 r DETECTOR, An electrical device for sensing norm2 e% ~3 ^4 G# M6 g( W- @ _ abnormal conditions. # `# P v. j6 K% p* @& {D ! d: p- V% y, V# qcontrolling the engagement of the actuator outpu2 S- d6 c, @8 J% i6 @. G" ? DEVIATION, To change from a3 o, f2 m% B% M( N$ A) C# ]) y p / K& a' G" H3 C" }) e: }8 ~DIAPHRAGM, A flexible part for operating a valve & Y# i& V* [! v6 vmechanism by pressur , Y- c2 N+ B0 J* n5 [0 e9 d下降, 9 n' q9 ~5 C" O" g9 _1 U飞机高度不断降低的飞行阶段。 ' p) Y$ Q' w: r! N( ~详细 ' g$ i, o& z0 g# _0 ~% @. m l0 s3 ?/ z探测器, r0 b. `2 [$ V4 ] }4 P g# o' R; R5 s 用于控制作动器输3 O, C1 J( d4 W, s" N9 E" f2 O( Q5 K5 e$ Z; w8 p4 X' ]! c6 P; R, |& [/ n 隔膜,9 P' u% j" w [9 N0 T; T; [/ p+ \ 英汉对照民用航空词典B OEING , Z; B1 {8 `, B2 PTECHNICAL DICTIONARY 43% J, L- C5 w" d/ S* A. k1 w DIELECTRIC, A material which does not conduct7 T9 e5 j# S2 H, u% o3 P, o electricity and used between the plates of a capacitor: ?0 L# \4 i- M2 d, A' u1 G; B (condenser).: `+ }2 z- g$ B- j! t nother pressure in the same system, measured in* U6 S; ]! _& ]" d8 E* r8 T ounds per square inch differential (psid). + v3 P2 x3 A0 fIFFUSER, A part of an engine between the 9 d9 H7 m. d+ A m- L* P% p7 pompressor and combustion chamber for reducing the L9 V) O$ s- k air pressure. 9 U. V* H8 J# J) righ 4 r0 @) u% Z) [ Y4 [& wpulses.& [4 i! k' [1 h2 b1 K3 O, [8 q ignal that is a close approximation of the original! G$ b7 |+ `" a% [4 p8 H' n ignal. 1 o9 M# D. p9 d# v& vIHEDRAL, The angle between the wing reference1 A0 K1 X; @- b. q lane and water line. , z6 y q/ o! ?( p% P的压力,以每平方英寸6 f) q3 c/ Y& E& Z 少磅压差计算(psid)。 & i7 F9 ]! Z+ Q L散器,5 \ A$ _( s9 Z& A 发动机内压气机和燃烧室间的一个部件,用来降低空9 y, q( J+ B( k* z 增高空气压力。3 j% N7 G4 T# x% L7 ?9 a0 X 换, , v1 t' M' Z L$ d1 k* n4 {! S的连续可 7 h- F: x, s9 J6 f/ m* s- z(模拟)信号的处理过程。' C. }! }5 f; Y! U 反角,. \1 z a: _+ S' e' D0 t! F; F 机翼基准面与水线之间的夹角。* Z# ~: d/ k6 Y. g4 F DIFFERENTIAL PRESSURE, Pressure relative to 8 W, u0 L. M# X Y# |a ) U" e- H/ r% f% h5 S* t5 P9 C) ~p( u# `' F( r- i3 M9 C D : c3 j1 N* D- }! H/ c0 rc3 F, @4 K( n. }! Y3 G8 E' H airflow speed and increasing the1 P8 A7 k" F, ?4 D7 \6 M3 ?* Q DIGITAL, Digital refers to a signal whose amplitude 0 ], L+ k/ Y* B3 Sremains constant for a finite period of time. Digital/ ^6 D: @1 a% ] ^' G1 `. p8 j9 { signals are commonly represented as a series of h - |) z* S3 q i' eand low 2 X5 y% D+ \2 D7 ]1 kDIGITAL-TO-ANALOG, The process of converting a 8 K$ H; }: S% D+ [- K$ Ldigital signal (binary) to a continuously variable (analog) 6 F$ A8 }$ f5 w! l* Ss! E( o: f. C2 \! x0 W4 C s 4 r; q o. k. K5 N! }# b1 ]. j3 W+ bD3 V, x7 w( M+ e/ ~& n* R0 @ p 6 X$ n5 W& U4 j; H8 L9 r2 C电介质,+ Y+ A& d8 f5 S 一种用于电容器板之间的不导电的材料。 / _) X8 \7 Y4 z4 D5 n压差, . X0 U( Q. f' h- E$ a0 H3 A相对于同一系统内另一个压力 ; a0 R) m( G/ z( y% V! y5 W! R2 S7 ]2 d* `7 S# O9 x* `5 Z7 X1 N$ n1 U7 B! Y! T气流速并5 }! \9 R8 ?% J+ q& v, q) t 数字式,& q8 f2 W8 n: o6 { t g 指一种信号。该信号在一定的时间内,振幅保持不变。 9 d; x% W1 X$ D% |通常由一系列的高低脉冲表示。 ; P9 K! V# s% m# S1 F s" V e数一模转 " l- j1 q# p$ d: C将数字信号(二进制)转换成与原信号相似 6 D5 N! P. d% B! M8 ~6 d3 Y( @' Q, o( K y/ D1 S4 E7 e4 j2 _7 Z英汉对照民用航空词典B OEING" {8 q. `' N( p$ I* F: L TECHNICAL DICTIONARY 44 ; S. W9 }0 |$ |" ~DILUTER DEMAND REGULATOR, A component in the X; W# S9 S5 g crew oxygen system which mixes air and oxygen and9 V6 R1 J! e+ U* a! F. h9 g9 e) p upplies constant oxygen pressure even if there are ( B! |3 q; o; L- Y9 l khanges in ambient cockpit pressure. / L2 c; N9 t. ]/ K5 Q a. H) P( Z* zIM, A word value of light. For light control devices - dim + ]8 M. s8 A& k: n" Cthe opposite of bright.9 p0 X U% |- J4 m7 C& O IODE, A device which allows electronic current to flow+ @4 D- I) ]7 ?, I only one direction ! y/ b( |# A2 N. |9 auid in a reservoir.( f5 s9 _2 j! y: F& o DIRECT, Straight line flight between two navigational : l% U3 I6 O- f5 C, O9 X+ zaids, fixes, points or any combination thereof. When ! J- A1 |! p6 p' H; Nused by pilots in describing off-airway routes, points 0 ?0 W) _( W: y( M& ydefining direct route segments become compulsory 9 g$ W5 a* `, m: J- F$ l9 Ereporting points unless the aircraft is under radar $ _. e; z( x0 b6 y5 _# Ocontrol." Z+ j+ L+ A- b ^% ~ 节器,9 s5 y5 F0 h: Q' D6 b 将空气和氧气混合, 8 i& X/ e; ?) R$ a+ a使驾驶舱环境压力改变,它也能提供恒定的氧气压力。/ o. z5 b2 K1 A) S8 Q2 r5 k( {, R8 I$ H9 x# V 一个形容光线亮度的词。对于灯光控制装置,暗的反# G4 X9 t9 Y0 R) A1 ~ 词是亮。) ?4 S( P6 S- C/ d3 d9 R/ S* d# t 极管,9 F/ |7 {$ V9 ]( @- Y 只允许电流向一个方向流动的电子装置。% m I' p) P4 F2 \$ m3 @& i% f- u+ ~ 器内液体的量。7 I! |* {% U% @% n+ Q; h 直飞, . o, C8 {5 ?0 z/ T两个导航台,定位点,导航点,或任何的组合之间的直 # l+ z ]) u c& j5 v- v$ N/ r线飞行。在被飞行员用于描述偏置航路时,除了在雷达控/ n5 z, w3 L N2 w% ^. M+ q 制的情况下,确定直线航段的导航点成为必报点。5 |$ M% p6 A3 \4 J$ ~3 C s5 P5 E2 A5 n+ P3 p: o c4 R$ C5 J4 ?. n1 l D % }* z3 n! U8 k5 w1 i2 xis & T2 x3 s. e; ^- ? H$ L' h$ ^D9 M; ^3 d1 |0 T: A/ x' n* _5 I( I in' M. n3 Q" P5 A% J" ]1 B/ q DIPSTICK, A calibrated rod or stick for measuring a: a- U7 u0 S% R quantity of fl3 D8 A$ t- q2 z7 r) L2 y6 w) Q: Z 稀释氧调2 c' V' k* c. n) { 驾驶舱氧气系统中的一个部件,它 8 v3 m' a/ A6 Z' n% g' }! b5 d; X5 m4 `+ X2 o; W4 S; K% R. C& f# J3 q- S# L5 B9 ]9 _) D1 d) s) d# H0 A& D) ~5 P量尺, . U+ h9 A$ m' N z- d2 n5 i9 ?校准过的棒或尺,用于测定蓄液 * y; a7 H; A7 z- X+ O: ? v英汉对照民用航空词典B OEING* D" L! A d/ x/ f7 \6 Q5 Q( ^7 k TECHNICAL DICTIONARY 45

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