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英汉对照民用航空词典 [复制链接]

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发表于 2008-12-24 21:35:01 |只看该作者 |倒序浏览
英汉对照/ v8 `0 v& j2 w C* D 民用航空词典) t5 l1 K6 l( d# o 波音商用飞机集团 - o% A* E3 H; _3 J+ X |BOEING COMMERCIAL AIRPLANE GROUP$ i+ h3 C6 g( p" P4 o 英汉对照民用航空词典B OEING 3 H/ I% e8 L1 i+ `( MTECHNICAL DICTIONARY 1 0 A3 @, d4 C+ ^A S, I2 p, u T' x0 X; s ABEAM (ABM), Beside: An aircraft is abeam a station / t9 d8 q% N# V$ q( K) fwhen that station is 90° to the right or left of the track of6 C- @9 D: H# S the aircraft. ) y/ ~. q3 m/ f$ ]ABSOLUTE ALTITUDE, The actual distance the aircraft4 D2 D4 ]) S2 t# T- W8 V is above the ground. 3 J" o4 v6 c4 u. a) w0 K/ R* `ABSOLUTE PRESSURE, Pressure of a liquid or gas" w. N! K; h7 M6 @ w' j measured relative to a vacuum. 4 ^4 j: y( b S2 s$ X4 z" O1 ~ QACARS, SEE - AIRCRAFT (OR ARINC) REPORTING4 b Y7 Z: N2 I ADDRESSING AND COMMUNICATION SYSTEM ( Q3 ^0 O @, a2 X8 KACCELERATION, The rate of change in velocity with: t* J8 u; [2 ~! X6 [1 W# `9 ] respect to time. + b$ [6 l+ m% n% |) LACCESSORY GEARBOX, A part of the engine, # v: b; H `7 T( J& Hmechanically driven by a compressor or an angle 7 n/ t; t2 ~. B- N2 F& ggearbox, for driving components necessary for engine 4 a8 g. s& f6 }' i! j1 |' M正切, ! X& I9 |2 m7 @0 w, ]9 u! {and airplane operations. * z$ ^; }; c: y2 R1 n当电台在飞机左侧或右侧方与航迹成90 度时,飞机正 . q! t7 s" b! O( p切电台。 4 S. q* }) Q# f# ]绝对高度, 4 i8 S+ o n6 x飞机离地面的实际距离。9 j/ q) k$ V1 L1 T; z9 P& v 绝对压力,. g6 F3 H6 t$ ~- |! J' q/ {: Y 相对于真空(无压力)测得的液体或气体的压力。 6 j( ]! C M7 z- A1 j2 M飞机通信寻址和报告系统,3 q4 a) A* G) M2 f5 `& \ 见Aircraft(or ARINC)Reporting Addressing and* h' r7 N8 @: l& g6 n4 I Communication System. ; |6 T! s" U! Y9 c. c S9 _8 B9 ]" o加速度,: z% W- o1 I: @ F 随时间变化的速度改变率。/ Y' \8 `$ U1 u1 _2 M' X 附件齿轮箱, ! l) E& \$ U/ {6 i4 ~) X" b发动机的一部份,由压气机或伞齿轮箱带动,用来驱动6 V7 C3 w2 k9 E3 ~ 一些使发动机和飞机工作的部件 - }! d* a h) r2 m3 [- _& L9 T英汉对照民用航空词典B OEING7 I- p- f# R( e1 v2 {3 o TECHNICAL DICTIONARY 27 C2 V- W; Y& H M4 I$ D9 | ACCUMULATOR (NO. 1), A container with hydraulic1 L% r! r% z- a0 t o ts when normal hydraulic supply is not6 L; k1 k0 |8 v8 K8 t( F vailable.5 T% J" u, M: x) L2 z f CCUMULATOR (NO. 2), In a computer, a special 1 N% s' ]/ l2 \& M1 H/ a4 [torage register associated with the arithmetic logic unit,6 v# j0 q X+ ~ olding the results of a computation or data" O: P' o6 {3 q: q! K$ Z$ m& V/ _ ACTUATOR, A mechanical device operated electrically,6 o0 J/ o- ?) K+ b- q% S0 M! E hydraulically, pneumatically or mechanically for# Y9 J O( ?, l2 ? transmitting motion between components. " o3 Y* D" T* }. ~6 i/ KADC, SEE - AIR DATA COMPUTER; Q" N: L( k/ {" O( M9 q8 f- k: n4 k ADF, SEE - AUTOMATIC DIRECTION FINDER& M; B- B. Z/ Z$ m4 |( w ADI, Attitude Direction Indicator, An electronic display of0 q6 G- C: B4 h4 X! }- y airplane attitude information in pitch and roll. " S! p0 e4 F$ }3 O) H7 E# E2 }蓄压器(NO.1), \; y7 q. N; s. x6 Q含有靠干燥空气或氮气增压的液压油的容器。当没有正 ( `/ C$ u" p# U; K, \常的液压源可用时,该容器可用以驱动部件。 2 ^. ?; \6 w: R$ r3 `存储器(NO.2),/ R3 w- ^* n2 d7 ? 计算机中,一种与算术逻辑组件有关系的特别存储寄存2 D" t: u# }. d1 A r/ l 器,用来存放运算结果或数据传输。 + Q6 v+ J. I0 ?( A0 t飞机状态监控系统, 3 C4 c+ O+ r3 n0 W见Aircraft Condition Monitoring System 1 o' p9 S' Z) Y9 d( v% |" k/ T. Yfluid pressurized by dry air or nitrogen for operation of4 g3 g5 L0 h, l, [ j% ]3 o+ Z componen / M9 Z, g* Q6 y# j/ @/ f% @a( j5 B3 J. H2 H7 A" O! c* _" b, v5 V A 2 B! K( \* R2 |$ m: d& Ps1 T5 m' k& s* W7 a9 x used for h 4 J! t# \3 O( m* `transfer.' P. A4 I4 k1 l; r& M$ F. h) g ACMS, SEE - AIRCRAFT CONDITION MONITORING: Y) U( P( Q* ^3 Z9 {0 z8 L SYSTEM . ( J2 } I7 f. M, ]9 Z作动筒,1 k' V* G5 X8 F. t 由电,液压,气源或机械驱动的机械装置,用于传送部7 u0 w: c! o7 e4 Q4 a 件之间的运动。 , P! f' A$ B% {大气数据计算机,9 T8 ^4 Q R! Z5 y 见Air Data Computer. & ~6 } f" q7 W; @# ]; J* k自动定向仪, ( l- B( Y- `6 [/ G) O' u* s见Automatic Direction Finder.8 N, E! F7 z5 t% \1 {; @9 R 姿态指引仪,2 Y0 e4 J8 f1 ^1 Z- @ 用来显示飞机的俯仰姿态和坡度的电子显示。 ( O" d& H1 E- a( ]英汉对照民用航空词典B OEING& u1 E" C0 ^7 X! e: X3 ]# z TECHNICAL DICTIONARY 3! C% D# E" U h L5 [ AERONAUTICAL RADIO INCORPORATED, ARINC is- |% l d" l: \7 x2 s6 I9 X! y , . _$ y$ t4 M/ Knufacturers, and foreign flag airlines. ARINC0 w9 `8 ?+ ~$ X9 V( | evelops and publishes standards for electronic 3 f o! Q& \) T" X" V2 yquipment and systems.0 `. |! u" B s+ p8 B; T0 y7 \ GILITY TUNING, The capability of the DME to7 a# U' f$ F0 j0 W' J0 u0 u lternately tune between two different DME stations in 5 g/ R2 J2 s: u6 ] _8 Urder to get two distance readings from one1 ^4 D" {: E1 ^& K- C terrogator. ; t' H( ^( L, E4 M" zge9 a9 ?0 P- R1 o) q/ L2 X/ k ILERON FORCE LIMITER, An electro-mechanical( f3 [, ]1 W, C% q3 Z IR CLEANER, A component in the pneumatic system4 O: z: H4 Q% u4 L$ b( B) P upply to the air! h4 R& W# [8 |7 N+ b onditioning system.- j1 l: p: d2 S2 D/ D2 M 订并出版# }4 j: Y" S. _% j7 ]; T 子设备和系统的规范。# s# s, t! w( O* L" j; F$ k2 ` 快速调谐, ! m, ]; R1 G3 M6 V+ v4 N' q机载DME通过交替调谐两部地面DME电台以测得来自8 p) F( R! i7 J0 C$ K 同一台询问机的两个距离数据的能力。0 C/ q$ ^$ C# `- J. l+ }9 ` 翼操纵力限制器,; {+ y) K8 Y+ p5 c' R5 ^5 @. p6 N 装置。在自动驾驶工作期间,用来限制驾驶盘- p) C* }2 W& K2 @3 V' U. y 气清洁器, * @6 h5 \/ ^! b$ L部件。用于去除供空调系统使用的发 : j- m- y" I( `2 la corporation whose principal stockholders are United& I' j* r) |/ \ States scheduled airlines, air transport companies- e6 j4 x2 g" n aircraft ma $ a. Y3 r7 Z* _+ Q: bd" E, ^% I6 N' \1 D/ c$ `+ U e 0 o( d: n: H, r6 M$ B& jA6 m/ T8 T G# R0 T0 I a l' z/ Q/ v L o 7 W* I" ]9 K# [in + ?7 q- U6 H4 ?6 B9 C5 ]7 ]; F' x6 XAILERON, A hinged moveable part on the trailing ed 8 u, S; h& U w9 I- pof each wing for airplane roll (wing up and wing down)" X' u* S1 M. M4 M+ y& c q control. 1 j% x+ Q5 I3 z# eA) G) m$ k# E4 d \2 c3 O device for limiting the control wheel movement by the " F0 ~4 ^6 G2 L0 E/ a6 hautopilot during autopilot operation. / E; g ?7 @% a/ Z% Q( q( @) ]% l; gA - T/ k. M) I( E7 @7 ?1 D4 W: ]- Qfor removing dirt from the engine air s 7 R5 j+ `7 V# W- h' vc `0 {6 M/ J& S 航空无线电公司,; W* I' ?) i4 _% W( V1 T& M+ ` 主要股东为美国定期的航空公司、航空运输公司、飞机 - t' K* J$ `$ m# D制造厂和外国领队航空公司的组织。其目的是制2 i# L" W- O6 b& j/ m. U3 [- Y$ l+ I6 O& W, p: F7 E! k副翼, 5 ^5 N! h R( o# u \铰连在每个机翼后缘的可动部件,用于控制飞机的滚转 1 U1 ~! w+ ^: Q9 e* D2 V: i8 ~(机翼向上和向下)。4 b) V; e1 C4 U9 y, \2 e, s: ]$ [1 N 一种机电, S2 B& C7 _5 v 的动作量。 ! w' G. p/ x3 G* j2 ]- }- d$ H6 w" c: j8 l+ O; J+ `: W 气源系统里的一个0 R; r( R3 `# [; r/ a/ N3 { 动机引气中的灰尘。 - r9 s' L' J# V9 G3 k1 o英汉对照民用航空词典B OEING3 n7 X ^# O4 U; k3 S* ~ TECHNICAL DICTIONARY 4; N. P5 M0 o$ V n" `8 | AIRPORT ELEVATION/FIELD ELEVATION, The1 l' v9 [$ c! O+ C6 \6 `- }5 C highest point of an airport's usable runways measured f1 Z, [% n7 e5 X6 {5 V8 b6 t in feet from mean sea level. In a few countries, the 6 ?' u0 [* T, gairport elevation is determined at the airport reference ) z, c' Y# g6 R) P0 Npoint. * Q7 k" ]. ]. A9 }, e T* M5 WAIR ROUTE TRAFFIC CONTROL CENTER (ARTCC), ( O& n. @* W8 q6 U' N( ]7 @ervice1 K! n' u( z9 r( Q* C# N4 Z ase of. t' j" Z; h% |0 s: ^# e& ~% I us flow of air traffic.2 q2 Q- I/ F: @ IR CYCLE MACHINE, A compressor and turbine on a: x" _6 P) q. e3 Z( ^/ F ommon shaft for cooling the air in an air conditioning , t2 D% k- S" C( G0 y3 W/ j( W# Pystem. The air is cooled by expansion from high to low) j. R( k" z W4 y' Q8 a+ P2 ~: W' h ressure across the turbine. The compressor is driven B- Z# t1 H( W6 I& K y the turbine. ) R: [( d. x! r7 e中航路交通管制中心(ARTCC),) v$ h% p- |, @ 域范围内使用仪表飞行规则飞行的飞机提 ! v' R1 P9 c! ~) `. }7 j! z管制(ATC), $ ^' ~' B( \7 O2 p涡轮冷却器, 9 C$ }7 V$ s0 \6 |2 A% j% Q8 ]是装在同一的压气机和涡轮,用于冷却空调系 ( W7 z# p$ y3 q% A统中的空气。气经压气机压缩后,由热交换器移去热量,1 }7 [# X2 z' A `% V 然后经过涡轮令涡轮带动压气机。通过涡轮之空气,温4 s0 j8 E9 U; G: \% E 度下降。6 I5 i/ o3 W, p6 W A facility established to provide air traffic control s4 s% X$ M G& M1 M/ ? to aircraft operating on IFR flight plans within controlled ; N0 D6 I, p# A( N% S: hairspace and principally during the enroute ph : J7 c! I9 \7 C. z# H& P( Gflight. # h* g* F0 G2 W1 {$ I3 A8 E ?AIR TRAFFIC CONTROL (ATC), A service operated by; l8 ], n( M' K9 R7 ~ appropriate authority to promote the safe, orderly and I9 B/ \* i, w1 e) t: Fexpeditio 9 R: S; b+ Y$ ~# ]0 w2 y; VA 3 `- [7 m! M4 C. mc7 G" V$ E# s' @: U: ?% C/ i; e s * P# V g$ J- e5 B2 Up5 `7 A: G) _" i z b4 I' P$ o$ E Y/ j 机场标高, " I+ i/ y, A0 N指海平面与机场可用跑道最高点之间的距离,单位是英# I# G4 h( p9 |& V% N 尺。有几个国家的机场标高是由机场基准点而决定的。 # E; K8 B0 I2 w: u* s; L: I1 r# y/ ?给在控制空 & r/ t4 ^4 X/ I3 Z* `& R! j( E( e供空中交通管制服务的站台。( ^6 z' r3 q. [1 l3 a 空中交通# ?+ F0 D$ [0 o7 m$ Y& X3 @ 由有关当局管理,旨在促进安全,秩序,和效率的空中 , k" u. w0 K. p- ~' w' I交通服务。 Q# j# y" v( g" g 根转轴上 ! D; _5 a R6 I5 R! ^5 }. W+ ]5 Q2 O; e$ B: q: m7 `6 S5 T2 U3 V% V0 y1 n6 v 英汉对照民用航空词典B OEING1 q, ?. {2 |; W7 M1 J7 F 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; l4 N$ ` U. P6 _ data information, such as altitude and airspeed, based 2 B5 n9 H% u+ R: ^: Y. don pressure and temperature measurements.; _4 \! R7 ^8 R' Y5 \ t, \' @& h3 n: m es air 7 d: C( J% _6 w7 T+ _IR TRAFFIC CONTROL, A system comprised of 6 \! z; [7 T( L- f3 T) |round and airborne components used to identify, track6 g1 ~" A4 v, e- I; l0 b5 @ OUND SENSOR, An electrical device operated" `8 A& ~& S" S y the landing gear, which transmits on ground/in air ) [& [/ q6 S* G3 q5 E9 l" d# yformation for system operation in flight or on the; `7 Q! V' r( _ y& X% D round. 8 p7 h- K3 ^+ s* x* FIRBORNE VIBRATION MONITOR, The AVM takes. |5 s& T; p& |7 Z# N2 U8 a3 q9 N e signal from the engine mounted accelerometer and1 T7 f; h' R( d4 A alculates the vibration on that engine. - Y$ r: I2 s+ j& u0 z0 ?3 a `/ Lcorridor equipped with radio navigation, n5 E- b9 `; P8 @+ b aids. $ y1 e$ N! R' m0 C- a/ @$ ?0 ZAIRCRAFT (or ARINC) COMMUNICATIONS 9 c4 u0 {+ }/ u6 }- S. C5 f! LADDRESSING AND REPORTING SYSTEM, An; B# u/ K4 G! l- {* M6 W addressable digital data link system which permits the + Y5 f& s) i/ y& h, Cexchange of data and messages between an aircraft0 _* {+ m- |! K* V% N) L, [ and a ground-based operations center over a radio : c- n' i/ @8 G( o' ?network. ) U0 q6 B% K- f3 x1 t. BAIRCRAFT CONDITION MONITORING SYSTEM, A$ @1 z! \: c ~- G ~! P& ]3 |4 x5 h system of sensors and recorders to monitor various : y5 y* m5 w6 t7 K' J5 x: Wairplane systems' performance and status.2 w7 G$ A. q- p6 o5 D* _ 机, . k5 X% C5 ]2 @; s( b' I中交通管制,0 I+ Q: ^# R0 l4 p# e$ a- w 一个由地面设备和机载设备组成的系统。用来对飞机进' A# M8 e. C% J" H9 ] 地传感器,; _. S! s6 v, d" U$ F4 s 一个由起落架操作的电气装置。用于给空中或地面的飞3 K7 V9 ]- a' k7 p: a 系统运作传输地面/空中信息。(有些系统只能在地面3 n$ }1 }9 Z6 ^ 用) 5 x' {9 u0 X( K4 n( \载振动监测器(AVM),- j2 u$ H9 Q3 s AVM从装在发动机上的加速器取得信号后计算出该发" E7 \8 Z- [8 y9 i4 D 机上的振动。' I$ d- A6 `) l7 o 式建立的控制区域,内有无线电导航设备。. G/ ~1 g# B) x 飞机通讯寻址和报告系统,+ W" b7 n; N, f7 x8 w 有种可寻址的数据通讯系统。利用该系统可使飞机与地 7 q* G5 Z- K# z3 p4 y2 ?面操作中心通过无线电网络进行数据和信息的交换。 & @* B9 l) d- u; A飞机状态监控系统, - k( u% T4 f5 I+ H: Y2 O: b! ~& s, X一个利用传感器和记录仪对各种飞机系统的性能以及( l+ [9 \: {/ u& r7 o 状态进行监控的系统。) e" m7 j) D3 o) L& _ A 2 U% s4 y& [. L, E. g3 rg/ D) M2 ] I2 s9 E( w @; ^ and locate aircraft. 3 b% u, D0 q; z' r6 ~AIR/GR+ l$ c _5 e7 q/ k1 v. k2 r4 Y b % m$ K1 }" `; S- T3 A; i- @. o" lin 3 R& q; s' W9 ^8 Y$ Tg' p& q# X! f; W& W* ] A+ k( m8 S3 k1 r; {% V th + O T' P! f" h8 {/ H/ Wc $ n8 ?0 V! V8 c' v; _, iAIR WAY, A control area or portion thereof established 1 @! Y- y. E+ _( ? Lin the form of a ( M9 M" R1 ^" [6 j d大气数据计算 $ j U$ D. A& \% l) U. S' M+ D根据量取压力和温度而产生大气数据资料(高度、空速 ) W7 ~$ q6 v/ n/ K X等)的计算机。; _8 x' e) Z" e d2 T2 }2 E& v+ j: a! {, z, H" c" _3 E 行识别,跟踪和定位。! `- \0 j% [. z6 f( u, H) N6 J# m4 Y7 J0 | ^1 \7 l) r( }/ ^/ M. H7 Z$ g; a% r% P. a. i 使' P2 f4 I9 ~0 `/ u4 |/ I( c+ E3 w' N4 e2 z/ O/ t; u7 ~5 j z; e# x- k* w& b# E# _2 M 航线," ^# N$ ]4 d0 @' w% ` v7 ~8 Y9 A 以走廊形& O& b" B! }3 c1 X1 e" T9 x( Y* | 英汉对照民用航空词典B OEING8 m @' {# _4 ?0 ^" h TECHNICAL DICTIONARY 6 ! Z, z" j O1 A5 W+ U6 |* RAIRFOIL, A surface designed to obtain a useful reaction,& i a% ?" z. o) z such as lift, from the air through which it moves. Wings,$ x7 f6 c. a) G# k/ B1 {/ w; w0 ` stabilizers and control surfaces are airfoils. + h' i; c8 v, GAIRSPEED (IDS, TDS), The speed of the airplane4 E- Z5 c. D8 L3 d8 s. E3 k5 L rough the air. - ]1 }3 S R. K2 c( ]: s3 sD INDEX, An adjustable pointer on the + R: t2 X' T* pirspeed indicator. : T6 @0 v2 L- A: v6 z% M) W9 band legal ability - @0 \" V, h. l: h8 _fly.9 M& T9 E% ?' }- d6 S4 y2 R/ ~ m, for example, the procedure for finding the ' ]) o7 T( ^6 k$ }1 n9 s4 Uquare root of a number.# e: {3 h+ D" T0 r% s+ ~ y. U. d+ j6 g0 k# v+ a re, wind, ' p/ f- x. R: d' O% E% v0 {+ Y, qand aircraft flap setting. ( P& L+ M( M& x8 ^& R, V是翼面。8 l4 t+ l% V, y6 _% D- ] 速,( x) }: l, x7 T2 t* m% i 飞机在空气中运动的速度。 8 @- ~, N" D1 H; S! |8 F/ w5 o3 F9 k% l2 r 在空速表上可以调整的指针。3 C$ o. l# A, t$ L, N7 J, L' {6 X 机械飞行能力、和合法性的飞机状态。9 n$ \. H% ~7 b+ n/ J3 } 一步一步的解题方法。例如,计算一个数的平方根的步 & l4 N" ]8 u; e; Z) ^7 C* |# T6 C; D4 J" L) q. A( v: ~资料的法定文件。 0 L( A; D8 i+ K( K$ x翼位置成函数关系。 + e1 h/ V5 `) {3 s, ith 5 v, E- U' w! `( t( i5 t4 j: i7 yAIRSPEE1 d7 b9 I+ u4 j2 K4 L+ g4 ~ a 8 [/ P! ^7 q; }; }AIRWORTHINESS, The condition of the aircraft with) p& E) J: _4 X- ] w1 c; o" g respect to its aerodynamic, mechanical, ( [+ `7 n) Z7 F, j, q& X4 Oto! Y$ |( c @- o+ D6 s ALGORITHM, A step-by-step procedure for solving a6 K) @. R- I+ S9 |$ s3 [ proble 6 T3 u) J# q8 M$ s Ws7 A m, V$ L# U# t AIRPLANE FLIGHT MANUAL (AFM), The legal {0 c/ @6 g1 y8 s5 Y/ @document containing performance and operating limits, j" R/ a( y. ]. U. K9 z' }7 k operating procedures, and takeoff and landing7 {" R! g( ~+ k; M/ B- E performance. 9 ~. w- f" b# P3 b4 f* s: \! Y( iAIRPORT ANALYSIS, A comprehensive set of takeoff . l, ]1 @9 f2 G5 D" c; k/ x% tweight limitations for a given airport runway, generall: m, V! D3 F: k8 U presented as a function of airport temperatu ; v2 h- A/ b+ n% L翼面,2 W$ C: o' q# B 用以从气流中获得反作用力(如升力)的表面。机翼,7 c. N% v0 F) C' g1 ~5 f/ ^% S7 v 安定面和操纵面都# y% Z" d, ~3 {7 f# z. \: j/ {6 Y( Y3 t$ l u空速指标( b2 W" N1 ?' P 适航性,4 j w( p v0 w, I 有关气动能力、 ' j$ [/ H& z: ?+ D( Z2 u* b0 L演算法,* u ?$ e1 h* ]7 n; T1 d1 @; }- a# x1 K4 I8 ~3 q A8 U 飞机飞行手册(AFM),9 i b: H3 u9 s( L 包合性能极限,操作极限,操作程序,起飞和着陆性8 c% ?0 g7 ^! ^ U% o7 q% ]' G7 K7 _ 机场分析, 1 L& I( B! s' G ]( h一套针对给定的机场跑道的详细重量限制资料。通常与 6 [/ v1 O9 h' J7 y) S机场温度、风、和飞机襟- K- G# O' g% A# ]5 U7 R 英汉对照民用航空词典B OEING8 E" T2 x# _) z, q; \ TECHNICAL DICTIONARY 7$ L& H) h2 Y. a AIRSPEED BUGS, Adjustable pointers on the airspeed' @4 h: v5 N0 V indicator. 0 ~% ~+ U3 l+ Y, @ALLOY, A mixture of a basic metal and small amounts# I) \/ ?7 p3 T* N1 t5 l N f other metals to change the properties of the basic 0 y; q6 R% @ g2 l- }etal.. D' Q) r9 P" S* [# t4 }: | Minimum airplane speed.6 }: Z: H/ B) j6 c% W e of. r n3 G: Z2 Y8 B+ a itting airplane angle relative to ' ?# X; W, E; w7 Yirstream for the stall warning system. . o' l% y) J& b! b3 _another. , [ N5 l7 U4 K4 U; mLTERNATE , An additional airport selected during3 |8 L& z9 t; u; p+ {$ E" {1 m. ~' }$ Z a5 Q 合金, 4 P& p' ^2 [; X' A, R在金属中加人少量其他金属,而改变其性质的一种金属 + }( a* Z. a- e1 B; |9 O |合物。 ) ^: ^# k& i* d4 X$ [飞机的最小速度。 ) H: G8 u3 N" p4 v速警告系统传输飞机对; T. X, A& C9 c' g; o/ O# f, C 流的相对角度。% b& r- M; w8 t+ o1 J 由一个状况改换到另一个。7 z$ y' m0 C# H# m& j: a0 p 降场,3 M* M5 [- G/ \0 f' q) v 划时,除了目标机场之外,所选的另一个机: ?- d2 p0 g5 P w/ W o; ^) J" t, {+ ] m ( Z$ Q2 i7 L, M6 L( G' XALPHA SPEED,: h1 B% M; L3 ~4 h ALPHA VANE, A small moveable airfoil on the sid % J- m/ i/ S4 z6 S# I" N6 nthe fuselage transm2 T) g4 T* c& W a ' N/ j; Q+ H4 o+ U7 Q5 Y6 A9 U3 |ALTERNATE, To change from one condition to" ^2 p+ u1 o0 ]) E* m0 V! f: d$ s A - `% w: @# s3 {flight planning, usually near the destination airport, to be : r- i8 P6 M5 P" b* ?! |1 sused when it is desirable to divert from the original, f* Q4 h; \* l$ e3 j6 X destination airport. * k: j1 l1 S' `, E2 ^/ K空速游标 7 M0 U8 @, l7 a* Y空速表上的可调指标。 , |% j p, ^* t% d1 l% k; O, f' a; p( A E迎角速度, 6 C! @& E8 q. U/ R2 W迎角叶片, ! P" L6 A/ }5 L- O+ h* s: c位于机身侧的可动小翼面。为失+ |+ B# e9 p; H1 s4 O0 @. k1 Z4 q0 h3 k8 v5 ^8 ~- c! M5 r8 p 交替, + r$ V8 j# k- B* j# P: B. K n( d0 i$ W% G: j 制订飞行计' g9 m' b6 O: A6 t 场。通常在目标机场附近,以备不去目标机场时,改降之6 D$ X k" j. X2 y" K" l! q) Q 用。 9 n* n% ]+ x/ e( i5 h0 ~英汉对照民用航空词典B OEING 5 R9 p! A/ u1 ^& \ F4 [6 ATECHNICAL DICTIONARY 8( X/ g3 J& _0 K" ^ ALTERNATE AERODROME, An aerodrome to which9 I! A V, S! ~. j' B- {5 j1 Z an aircraft may proceed when it becomes either2 e2 c' d: H3 q2 X$ U6 T2 F3 s u possible or inadvisable to proceed to or land at the ' s# j* t7 w+ J. merodrome of intended landing. # G8 J! i2 B/ x; yTER SETTING, The adjustment of the altimeter - ?7 A. p/ }1 f) i% g3 s' t& ^account for local variations in atmospheric pressure. : y8 _& [; D5 ]4 \5 k JLTITUDE ACQUIRE, A digital flight control system - v6 r5 p( J2 x" o7 Pode to transition from climb (or descend) to level flight. # p# V- b* E; n; fLTITUDE ALERT, A flight deck alert occuring when the0 `0 z) o, n; C: r% y8 f: B4 z irplane approaches or departs a selected altitude.$ G) u) g$ @4 ^% {1 A8 E LTITUDE CAPABILITY, The maximum altitude at! h" C8 U6 s: x- x hich the airplane can be flown at for a given thrust, 2 k# Z# |7 @7 D3 Cpeed and atmosphere condition. , P) u5 r( Q4 I$ T. }4 PLTITUDE HOLD (ALT HOLD), A mode of the autopilot" G1 }+ J' X( i; y( e r flight director to maintain a selected altitude.' S! E1 l) Z4 P3 L* l6 \4 D9 D irplane's altitude during VNAV operation. ; h1 C4 k7 S0 q: z4 G机场着陆时,可作着陆使用的7 b: G) V$ R/ B4 L. G 场。 - j9 i$ D8 R9 _, s& k+ { m+ o: F3 f2 r根据当地大气压力变化而对高度表所做的调整。 8 [9 i1 c( B. l" U9 C0 b一种数字式飞行操纵系统,从爬升(或下降)改平的模0 [# n. s% {! _. W8 \& h5 F2 P5 G y9 `, q度警告, % n3 K! w: n4 y4 B9 ]当飞机接近或偏离选定高度时,所出现的驾驶舱警告。. D% m% H7 o" @3 o! Y' Q+ W 高度能力,. z2 ~& h$ a; `: U. x9 ?' c 在给定的推力,速度和大气状况下,飞机能飞达的最大) a% V" r/ ^; I' K ]7 K 高度。 / C; e: N# g8 }5 t! g高度保持(ALT HOLD), 4 o0 q9 E. o" ^自动驾驶仪或飞行指引仪保持在选定高度的一种方式。1 E0 t* ]' [: C0 a( U v* ^0 a) `, M; d/ {1 {! t员对飞行高度的控制。# D! M+ A$ F- c4 G) U im ) q/ @! o; N; ~5 m% ka% S) g* O- w% |. o+ e) v! [ ALTIME . r3 g6 S: V S2 }9 Z& f4 n+ x; l vto - m, f# C- B/ p5 U$ c: M( tA. O9 u" y) Q4 c) A7 y* L m0 O! q$ R" O! @9 U# e) s# p5 [ A5 G, }, X" ?5 i( E a* R5 X+ _+ P( K. R A4 ?- s# _( }/ t: D w 5 V5 Q$ F5 V- N* w& Ks" m* _ Z3 r" D! A. r A1 a+ b" s3 j2 Z+ W9 W; i& M o- Y0 S+ T( _" r( o ALTITUDE INTERVENTION, Pilot control of the6 |3 d/ x9 f l& P# l a ) Y- E4 M& l/ qAMBIENT, The surrounding atmosphere. 2 Q7 C. B) e/ ]$ x* \1 Z0 x备用机场, ) g- k( o2 `) S8 M, @& l4 c当不可能或不适宜在预选 0 o( G( D4 A' _4 y Q b9 J+ k G2 N0 N% |" @7 S' d 高度表设定 2 Y3 O( ` s6 u" M6 P' q. q+ x/ ?6 Q高度截获, 7 w8 F- f, F! ]- g+ J3 `/ t& Q+ `! g& n7 c( N* v% C2 c7 h6 e5 A7 q% z! Z; m3 L5 q& P, I高度干预+ e7 \/ U3 r5 }3 ] 在垂直导航工作过程中,飞行 & D7 |" G5 `( q7 A8 X* q' i3 V周围环境(地面气层),4 C3 k. j8 w3 h7 @5 a0 |$ Z 物体周围的环境(特别指大气)。 4 N4 i$ \* l" Z; H) n英汉对照民用航空词典B OEING 5 r# p% b; G/ v! o$ q, dTECHNICAL DICTIONARY 9 % |: j, ]+ t8 [% ~AMBIENT PRESSURE, Pressure of air surrounding an " N% k4 z9 \" r" n) G( x. M" R, Qobject, measured in pounds per square inch (psi) . 7 w* h$ D. b+ m7 {* CMBIENT TEMPERATURE, Temperature of air8 Y3 A3 @ x2 P mpere. 1 l1 h) I* s( v# _! Kurrent waveform.. ~- p% f u4 k g an" Y) t0 ?& j( G) p" |3 \8 E nalog signal to a digital signal. , e- f, b o2 v, s: V" \ore inputs 6 s1 O( l) G4 `" uf binary digital information and one output. The output 2 a1 q2 e# m: Q) O% b1 only when all of the inputs are 1. The output is 0 % C5 {) d9 a+ V' F; g1 Nhen any one or more inputs are 0. 1 d$ E+ f# A: v+ ?4 e/ Z# q面气压), 3 z) ^# B* b& r" C( L* E; d- G境温度, ! p* F2 Z. F' ^! M, ?8 n1 c气温度,用摄氏度(°C)或华氏(°F)来 3 r- v! O7 [) M4 F {& F( j$ v3 {+ P1 _2 F2 }7 x( R电压或电流波形的幅度。5 F$ Y! j) t. J: Q% Z3 ] 性变化的信号来工作,或产生连续性变化的信号 " [7 l. r* ?; ~& w3 N0 v; f统。9 t# r. ~. ^3 R9 i& ?( }9 F 将模拟式信号,转换成数值式。6 c+ {4 T- R8 y0 \0 w8 w 一种有两个或两个以上的二进位数字信息输人,一个输% I/ R, r) z$ x% s. G 的装置或电路。当所有输人为1,输出为1。当任何一个* m) z8 }+ F( h3 v8 l/ f 一个以上的输人为0时,输出为0。7 \6 `9 C* i1 i: y, c/ I A3 T d; |7 g6 k- F surrounding an object, measured in degrees Celsius 2 o8 B, W4 f+ x+ S" C; V(°C)or degrees Fahrenheit (°F). 6 m+ } \) J E; t& ?6 PAMPERE, A unit of electrical current. One volt across* r! e1 t" S; o7 J6 w one ohm of resistance causes current flow of one 9 E' r- s; Y# I/ v% U5 {" ma 8 ^( P6 F1 i. i9 s" Q6 D8 `AMPLITUDE, The size or magnitude of a voltage or- D6 D' Y t5 S4 @0 _7 D M c, Y# v$ x, s% H# W: B# C ANALOG, Quantities or representations that are - J. J$ O H6 `% t/ Kvariable over a continuous range. # p! |% \; Q% t7 YANALOG-TO-DIGITAL, The process of convertin " k/ t2 Q$ L" R! e/ `a* n, |7 [ ]1 A0 M2 O AND GATE, A device or circuit with two or m/ g# R+ z+ y( x: S: n' i7 {; W o ( \. d) [: Y, l: ? K! cis ' |6 `8 `4 a }w 1 B0 o& l* q7 \! g- `2 l1 i环境压力(地 5 F3 F# L4 U* G( z物体周围的空气压力,用每平方英寸多少磅(psi)来) d2 X" y- k/ o7 V5 i 度量。 2 g U% E# @8 b+ l+ V& E) Q4 x# A9 `; V# a4 [" @8 n* }物体周围的空: x- H( C l2 L n) h" x 度量。& W1 } ^) H! X7 V o 安培, , S. s7 v1 x, \9 C( d' V) }' |电流的单位。% k: r3 l/ X& p5 ?* M. ^- [6 [ 1伏电压在1欧姆的电阻上所产生的电流为' v7 j2 U8 O- Q# K1 [. f$ _ 1安培 . O! w; d' K) A- e+ F% @9 W振幅,% i, a( G4 z* B" F, h. Y& n 模拟式," t3 F" _6 M/ h V 用连续 $ n( K9 w' I/ W; ?" h* r2 k" E8 M+ i+ g8 s* H& S从模拟式到数字式, ( K& I8 [# A. p% [与门,: @+ p, `6 J+ P6 q! P8 U3 D# f& d' l, |) O( i0 l0 ]1 T* {/ S1 ~* C& j) s' B# c0 h 英汉对照民用航空词典B OEING) N* p6 b9 X8 o5 {. q1 q TECHNICAL DICTIONARY 10% R" M# [! {' Q9 G$ E ANEROID, A sealed flexible device containing air at low) L" ?+ ~7 n2 R; |" u( T. i* A: V$ p pressure, which expands or contracts during change of / N+ q3 z& ^- d% cressure outside the device. - d( u3 J- V, v7 V9 a' aically r" U! u4 d' s m7 W- _7 N1 Ur changing the direction! X B, Q1 R1 {9 J W9 c f drive.: F. h- S: g4 d5 p5 i7 r of the wing chord in( f# X7 D! k* a lation to the free stream airflow as it moves forward & [% s0 f- R+ S9 d3 q6 ?rough the air.3 }, D6 U! M; H i3 {! U al axis of the 5 N& k0 F5 V1 Z6 o4 @aircraft.5 @$ X! q5 Q* x 胀或收缩。4 m$ D. ^; n [! W: e9 M5 l 箱。是改变驱动方向的机械装置。7 C4 g; d: O, F& ^ 机翼翼弦在空气中向前运动时与自由气流之间的夹角。 " G9 K' X: x6 s# g$ f7 ?4 S+ @ x3 A# }, T8 d p 5 t6 p5 q" h' p) {' G$ ~ANGLE GEARBOX, A part of an engine, mechan; y4 f8 |7 V) v, V9 r driven by the compressor, which drives the accessory5 X" B% f) F" e' i' [+ S% j# m gearbox. A mechanical device fo $ I4 w8 y8 _0 d4 F' K8 qo" f% W( m) k3 \0 X/ h ANGLE OF ATTACK, The angle5 d6 P% e1 L0 E0 r( k re + g4 z- W( n3 l e+ _( Fth / I6 w3 w- d4 LANGLE OF INCIDENCE, The acute angle which the m" N% _9 _, }5 T% ` wing chord makes with the longitudin7 R n: G3 k" N- T7 d' L7 R- } 膜盒,4 c b$ W! Q0 u- w+ X; R" S 内含低压空气的密封弹性装置。当它周围的压力变化! |& n. A- T) ?' F' ^# U 时,会膨9 v6 D/ _ @5 a, T 伞齿轮箱,/ W! o; C- d Y* [ 发动机的一部分。被压气机以机械方式驱动,然后驱动 ) n' p X( m5 o( e4 h2 i附件齿轮5 L4 i+ G( I1 k% K 迎角, ; p. u2 k5 E) `( @) k安装角, $ K" y9 \( j$ T0 _4 u飞机的纵轴与机翼弦线所形成的锐角 ; O, p9 A$ e3 `0 M英汉对照民用航空词典B OEING/ t0 k4 C) w+ a# r2 M' Y$ B) J TECHNICAL DICTIONARY 11: E2 D# C( `3 P. v% f- J$ Y3 J% ` ANNUNCIATIONS, Audio or visual indications used to2 y2 {$ c3 P- |. s call attention to an event that has taken place. 2 q: t) y; Q1 u0 oANNUNCIATOR, A visual device consisting of a number$ M( M1 Z: E l9 A3 f ly. ) ^/ ^! t# d- [ Y. j6 y7 U3 ZANODE, The element toward which the principal stream - ]/ x) ]6 ^9 I$ F+ W5 Kof electrons flows. , d' r9 i. l5 u; D% mANOMALY, Not normal. 8 t; s0 L9 ?9 YANTENNA, A device which, used in conjunction with a : U9 t- z: |; Z, c4 ], c- Stransmitter or receiver, is used for radiating or receiving$ O' k: Z0 a' U: W* T( O! h* D radio waves. ( b; Q0 N. A9 @; i, ]NTI-ICING, A method of preventing ice formation on( f* m$ B1 E# p$ L4 g& R" y e wing leading edges and engine nacelles. , y0 \4 C5 U5 L# E3 ~9 l/ r7 ONTI-SKID, A system for providing maximum braking9 h: R+ f" [( o5 N) n ithout skidding for any runway condition. Anti-skid ; k: ~ z) a+ z/ y' ?omponents are part of the brake system.) j: K8 t1 C$ x4 J- d 告,/ J8 e6 E# i* [ 当发生事件时,以声音或目视指示形成的提示信号。% d6 [- K0 |& H) C4 M! c2 F 与之有关的电路的现有情况或已存在的3 t) M7 I/ i4 f. Q, [, c) n7 `9 c8 C5 A$ m6 N9 C, h 正极, % r6 J: F# z* E主电子流向的极位。 6 P+ ^2 P0 t0 y1 A" {8 q异常,; Y2 o8 @* E7 h ^. g( e 不正常。1 b& u5 Y9 c8 g+ M4 x; w9 A4 M 天线, % t3 v! K: F1 _一种与发射机或接收机共同工作来发射或接收无线电+ T& v9 Y% X. I6 f, i 波的装置。- @4 Y5 m' a/ c, e) B0 w% ^8 O 冰,3 `9 B! ?' e b; |' c a5 k3 y 防滑系统,* Q/ f& ^) D0 {9 j+ k8 j 一种在任何跑道状况下,都能提供最大的刹车能力而不9 K, d) f0 N2 y5 x9 I4 { 使轮胎打滑的系统。防滑部件是刹车系统的一部分。 N# b* T$ o6 e% g" W$ O h; ^. p- H8 G of lights. Each light indicates the condition which exists4 W" _' T2 G. v o; a or has existed in an associated circuit and is labeled3 ~9 p4 b; h% c6 h; Z$ ` according % ~5 W, U0 u) HA1 b% X: z$ o" Z, B* i th _/ P, L9 @# K2 [$ C% b! q# jA0 y& z1 B0 w: }! J* Q1 m w % j, W1 }( `% g8 y) }: j# Ic/ n" W2 k1 P2 L) _" `. o' o- w" \5 Y% l+ E2 w; C \' y' j3 t C( D; D信号牌,6 N; r1 v" v/ p" v ^, z, m 由一系列指示灯组成的目视装置。每个指示灯都有相应 ! {# D3 v2 l! |( X% z& w' H! j的标记,用来显示7 Q3 S: H4 X: G6 A0 U& H6 G6 s4 a! C' w* v# ^- y: s" J2 c6 i" w 防止机翼前沿和发动机短舱结冰的一种方法。 4 ~ g3 O7 w$ b+ T: s- `英汉对照民用航空词典B OEING- [/ i- _( R0 o2 [% h3 d" I TECHNICAL DICTIONARY 12( u H/ Z" S3 r) F1 I: p3 f APPENDIX, A supplement to the Airplane Flight Manual 4 z7 Y, g2 @1 @- v' `tained in the basic manual. A 5 B8 X% o I/ |4 mollection of supplementary material at the end of a5 F0 f4 _, v5 Y2 C: a ook.0 c2 v, j! U: z; o- C/ v D of the " b# a; w" c4 y8 E4 B5 ~0 T9 ]* t' Qrsion link on the landing gear.. D0 L( c( v I2 W! g APPROACH MODE, An autopilot/flight director mode& j: V& u, I# Q. {, z3 q which is a combination of localizer for roll control and ! g+ n% N& w/ N8 @( [glide slope for pitch control. This mode is used when full( g5 T9 g. @8 U+ u+ ? instrument landing system is available., f, @ O$ ~0 l2 D% f8 L5 R APU, SEE - AUXILIARY POWER UNIT/ ]% b' j8 t, V% ]- h W2 l/ D6 N ARINC, SEE - AERONAUTICAL RADIO / @+ x3 i9 Y x1 P f$ g, F; m. NINCORPORATED % f* Q* p: V# O1 V% \ARM, To make ready for operation.4 n% p8 c+ R' i# e 附录,# {. }+ b9 e- T8 H! W( V s/ i 飞机飞行手册的附件,包含基本手册中未提到的飞机形 * n& z, n* n+ A8 n4 P/ e态的其他性能。是附在手册末的补充材料。 / h- B6 W$ W& c$ |2 X/ T; D7 P顶销,! M. @- m7 U2 k3 M2 D k 用于连接起落架扭力臂两部份的销子。& J! K. A/ H* u8 h 进近方式, - o" h' {2 |2 X/ n G' e; V, K一种综合了控制横侧的航道信号和控制俯仰下滑信号 6 u/ L! |" ]! n' k! F8 J6 x6 z9 p的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系 ; n- n3 L$ d: j6 t; m统正常时才使用。 ' F4 G& P" G7 V4 L- }- k, L辅助动力装置,8 n5 N5 u& k. j% G* [8 I8 I! e- m \ 见Auxiliary Power Unit 9 a2 S- b/ b; c( h" ~9 k: d5 Rcontaining additional performance for aircraft4 X3 B" j: K7 t3 x" C2 v configurations not con 4 G J1 q7 Y& B& j4 U+ Ec9 [1 G3 {4 q& ~% O5 I2 e" z8 D b& Q! I" M7 Q% g9 J3 _8 s/ f APEX PIN, A pin for joining the two sections9 E& \8 V" A2 _) f3 ?1 B to, B# {5 b$ Y2 W, a. S# [7 L+ O+ O7 u; ~- n3 Q9 F4 n" _ 航空无线电公司, 9 A4 z1 r) S6 n. ]; s见Aeronautical Radio Incorporated.7 R5 _' _9 E/ ^ 预位, 1 B n; @( I8 m1 |' I3 W部件可以开始工作的状态。 ' `+ F, x# o, R4 T. i英汉对照民用航空词典B OEING : g3 Q( y; j; S, {3 d( ^* uTECHNICAL DICTIONARY 13 ! U2 k; _) }* \, Y. ?4 o; qARC, The curved track over the ground of an aircraft 5 o. w6 c& Y8 Q/ o: H- b wflying at a constant distance from a measuring- D* m; W& a4 U+ e equipment (DME). ' m; H8 w: `" Cin the limits of self-contained system0 g0 @# [$ X7 V$ P3 s+ r+ W4 J2 f apability.% _: o5 f7 [- t1 G0 v tem for opposing or restricting . o3 i0 L! q6 ^ovement. 9 [0 D% g/ ^, T! A& ~SPIRATED TAT PROBE, A sensor that measures total0 w: S6 x+ U2 p, i! J ir temperature when the airplane is in the air and that' Z8 U; a# ?. c. q8 E( c. h* F easures outside air temperature when the airplane is ! D; W' b# G9 g8 J. f$ |9 c4 ^* Yn the ground. The outside air temperature is measured ( d# n6 |1 u( v4 {0 ^SSEMBLY, The fitting together of a complete structure+ k! y' f/ L& C8 ?. H, C SSUMED TEMPERATURE REDUCED THRUST, The 5 l/ n; W. c' |: J1 `8 }+ u3 v& iATC, SEE - AIR TRAFFIC CONTROL / g$ C+ A; E! p% Z4 ^4 f: D* `1 F- j! a0 |* @2 P系统中所产生的一种用以抗拒 & g9 R& r; x6 q3 H作或限制动作的力。 $ g7 }' R b8 i) G" {0 q6 E头,9 D X# u$ s0 y 用来测量飞机在空中时的总大气温度和在地面时的外! L5 \3 G9 Z$ ~- Y) A# `! x. S& y1 | 温度。地面外界温度的测量是利用引气将外界空气吸入8 W" `: R6 Z5 n* M 头,以达到测量的目的。8 \" a Q8 z$ j1 I+ D7 m8 @ 配,% [4 o0 b0 V4 Y/ k$ m6 {, \ 一个完整的结构或组件的过程。 ! B V0 m; T. Y( j6 h j2 k假设温度而得的减推力,: U" u" j3 l6 `, w' u9 A b 推力设定值时,假定一个比实际外界空气温 + X! J1 @; |0 r9 B5 o9 v# Q空中交通管制,. b5 u2 C2 L- }+ {6 y 见Air Traffic Control8 q* z! U8 h# k# _. ?! S; v AREA NAVIGATION/RNAV, A method of navigation 9 g7 o' [/ Z4 }2 cthat permits aircraft operations on any desired course ! L/ h& W3 p. W4 _0 C+ kwithin the coverage of station-referenced navigation: U3 `7 S* ]( I, r/ k/ ~# `& \/ s signals or with 2 @7 e9 j* Z1 N A5 e5 ~* M' [( cc 3 f, m' U! s; W& a/ r/ zARTIFICIAL FEEL, A force developed in the flight / R8 j, }8 S/ v& o8 u* qcontrol or brake sys9 X: o4 [ B' j& u- I m) r# ]* L4 ?# d: M) K- w A; q8 l6 X5 c6 K0 N a 9 ^3 _0 e1 Y8 i% Bm. P5 F% U) @) t3 E6 m5 [. m o: N; R, h" B$ C/ O# V by using bleed air to draw ambient air through the 1 U2 s# x1 }" J7 K# U$ e8 Y# Qsensor when the airplane is not moving.* L) B w" M/ E* G, v+ J A1 D. {; }" s% R or unit. ! P8 g: I& g j% ^A ! K3 I. {/ q Z# Q. k" M# E# Klower thrust obtained by setting a higher than actual 4 G. c% P( Q6 k& y# @Outside Air Temperature (OAT).+ ]& i: [6 ]8 G5 c& t% n9 G+ e1 T 弧线, " h) o" V/ b( t+ k飞机在围绕DME台等距飞行时的弧形航迹。: I' v ^ \2 `% b1 f 区域导航,4 S1 y3 n1 T2 @" m9 k7 p) C" ?) N 容许飞机飞行在有电台参考的导航信号或自备系统能 5 y/ d6 U( c) x( f- o/ e力极限范围内,飞行任何预定航线的一种导航方法。8 l3 a- ^5 i0 _, d; c 模拟感觉8 t/ m# T3 v/ ]0 ^; ]- h1 I 在飞行操纵系统或刹车 g) L: \2 @; l( `7 p# x2 g! q0 j0 k" u& U5 J吸气式总温探 4 k* p4 F4 _7 Q6 T4 Z1 J" Z% K @* A& V6 T" j& S3 }* A U; @# K) [' ` ]. H H4 l: d' i2 ~; K- _, O: K* X组合成; |4 r; x4 i6 K7 w; h( L7 F- B3 A* f$ e( A- x# y0 y& r, y' l) R9 ?# O, ~在选择起飞; L0 U6 Z( w7 X; C. E: { 度高的温度而得到的推力。用这种方法可以减少发动机的 6 g' Y5 t$ v+ b' o5 _磨损和维护费用。 + L( x' y- I1 N; r& U, r, W4 k' q) `) D7 j) g# V: W英汉对照民用航空词典B OEING ) ?# J3 L8 [: g9 j3 ^TECHNICAL DICTIONARY 140 {: G+ i9 ^% t5 C ATE, SEE - AUTOMATIC TEST EQUIPMENT# `, }! x% A) w0 m+ N2 }1 B ATMOSPHERIC PRESSURE, Pressure of air due to the 9 O q$ w( t' O5 g1 ]* L4 D7 @. |arth's atmosphere, expressed in pounds per square & R- q" E: e9 }+ p; gch (psi) or inches of mercury (in Hg) or millibars (mB). 6 l/ {) _. O2 h, n' YTTITUDE, The relative orientation of the airplane with( u! a4 Y3 S+ a- I spect to pitch, roll, and yaw.( s/ a: _; J5 h& B- F/ o2 N( i UDIO CONTROUSELECTOR PANEL, The panel in 6 H" u) b5 q: M9 }, ?4 N* Xe airplane which controls and selects the routing of " ~6 `' `) H! M+ T- E' audio. 8 Y3 D' f6 K& B `UTOLAND, Automatic landing using the Digital Flight6 z3 n+ ?) }% S' B. s$ o- D, a ontrol System. 2 g( d6 V9 G f/ o" K' Gn. 8 S+ \! K; q2 e0 x: v( DM, A system 6 F# `/ |0 u9 `( {. z5 `9 l. Yomposed of all necessary subsystems needed to guide* G7 s' {; {% d5 e8 H8 i e flight of an airplane., p& Z. q9 f; X# } EQUIPMENT, System test 3 |- v* ?4 c( ~# vquipment that operates under computer control. 0 i) T5 s3 L. o+ _装置,

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e5 y* C4 y: v3 v6 o3 p% \ in " U0 V' j" C( J1 w/ n$ CA 1 c, s$ W' D) K; m4 a" j) gre; w! G- D' y1 k; H5 G, t A 4 j6 v+ L! `/ B. M2 R# fth 3 }; P! v$ j% r8 J2 \2 Ia2 j8 K+ ~& U2 Y( _$ E; r A 3 y" c! I$ g* W& _. {- }/ LC 4 |; Q1 {" P) V- C- [AUTOMATIC DIRECTION FINDER, A system which # ]8 b! F$ Q |determines the direction of a radio statio0 w; c Z) u- H: T: ^7 x5 l AUTOMATIC FLIGHT CONTROL SYSTE* g0 S; x$ |9 W0 B B1 G c% u( h R6 K# P9 o+ Y9 L* J O, q th . V' i) T. n! x( t) JAUTOMATIC TEST ' u6 w: z( x" I/ j6 |. pe ' f+ J6 T6 [2 {, S8 F, m& F+ \自动测试: A) X9 U% e. m& l4 m0 F) l/ L 见Automatic Test Equipment.( r2 y4 G: D2 G) d 大气压力, 0 O6 n# A4 A4 x4 ^由于地球周围的大气而产生的空气压力,以每平方寸多 3 w5 h$ M& q& \+ ?5 D3 B# x% W# B磅(psi)或多少寸高水银柱(in Hg)或毫巴(mB)来- R x' O. [& `6 v" R 示。 - [6 d0 E! @0 ^! C7 S9 q' F飞机姿态, % k6 G" c, }, s9 m飞机与俯仰,坡度,和偏航有关的相对方向。 $ p3 [8 @( r& E+ |! A( J音频选择面板, . j# n M& r$ Y. u0 z飞机内用来控制和选择音频通路的面板。0 y2 |. W4 s1 e2 |7 }. G- [1 q u6 R 自动着陆, 6 N; n- ^8 m8 Q3 Z! |使用数字式飞行操作系统来进行自动着陆。7 f6 V. g1 ^- Q4 ]( W+ D 的系统。$ v0 r) ? L- }, K! s _+ \2 }0 j" l# R2 ?$ Y6 N 系统所组成的一个系统。 7 {1 [" n) V V7 h) U: @在计算机控制下运作的系统测试装置。 " U/ @" |0 H9 f# m* }: Q# e5 S) X% h8 i1 R/ A! K: u7 J 自动定向仪(ADF), 3 D& K5 N0 q, X9 l3 J# ^' F% i确定无线电台方向 / N+ ]- T% B: l2 e+ K+ p自动飞行控制系统& s4 ]/ D4 W3 F 由所有能引导飞机飞行的子! e' V9 N" F+ F8 Z7 C9 m 自动测试装置, ! _$ f$ S0 Y+ y6 z+ F英汉对照民用航空词典B OEING 3 V; ]! Q( Q- B" l/ dTECHNICAL DICTIONARY 15( t, E) L4 ?3 k/ a. x! h+ r AUTOPILOT, A system which automatically controls $ V/ w( A' ]0 G6 a5 E7 j& Cand guides the flight of an airplane. ; r3 b) u" c0 I3 V# ` LAUTOPILOT FLIGHT DIRECTOR SYSTEM, An. c$ z# S. l3 a( v2 N tor+ d& r0 V9 b8 [- ^8 ~9 U; F UTOTHROTTLE, A system which automatically. W# e+ x$ ^. J; w0 ` ontrols the throttles of an airplane. ; L4 K* x6 x8 W( j, FPOWER UNIT, A small turbine engine in 7 ?4 ~2 y% Z" d5 ee airplane for supplying electrical and pneumatic; ?; h" L5 a$ `& Y ower for systems operation on the ground or in flight.6 y# v) N9 R V& [/ _1 M0 d VM, SEE - AIRBORNE VIBRATION MONITOR V% w4 K/ i* @XIAL FLOW COMPRESSOR, A type of compressor8 u1 P, S2 U+ S; a) r2 P. P sed in a gas turbine engine in which air passes through " V$ f/ z8 ?( V3 c9 }# @" sXIS, An imaginary straight line or an actual physical # x/ n$ z8 A: @2 aomponent (such as an axle) around which a body can/ w, e% Q3 W/ k& s0 |: k/ W tate. 3 D+ [7 T' f' T0 I1 u仪, o5 j8 `% f# M2 \0 Z& V5 J( p1 \; x2 v4 m, `1 c: D8 z 自动驾驶飞行指引系统, # O) E; F$ ^ r7 l动驾驶和飞行指引功能的系统。 9 w. i- ]9 F1 Q2 z动油门, 5 W6 U) C: U, v! D7 _8 `自动控制飞机油门的系统。 ! y9 R2 {" {0 W% y是飞机内的小涡轮发动机,在地面或空中给各系统提供& c* O& y' @: u. @6 T0 y 源和气源。 & R! [2 X3 _$ T称。, N. s# \8 B1 {, u5 U$ w 载振动监视器,7 q1 v2 n1 T4 A! J+ ~' H+ V; _ U 见Airborne Vibration Monitor # g% P( p% u+ d3 Z- b! Nintegrated system containing autopilot and flight direc " C p7 ~7 W K. C4 Ufunctions. + Y- G* r3 q8 `& `, ]A - v- C' y b( d; e& Oc * k! J2 _) j3 K1 r- J3 |6 D6 J$ KAUXILIARY+ `5 ~! _3 Z0 S e th ' H& I* B: |6 cp% R# S K' n: m+ t3 Z AVIONICS, An acronym designating the field of aviation 7 j [0 [ W6 n m+ ]6 Zelectronics. # z# |; H2 P7 n! d) KA ( s4 z3 v1 D. K8 b2 bA9 O2 n5 U" w6 L$ A) R$ Y+ j7 n$ D u 3 b3 o; s; H; V. @the compressor in a straight flow, front to rear./ R7 q- f: q9 L+ b# X' n v6 W A) W& ?# v- c3 G* b4 k c0 r7 `% a# J* `& w ro. j' |) T. T* r: d 自动驾驶 8 a/ W* U& M4 W/ |7 x0 S动操纵和引导飞机飞行的系统。 : Y* F3 \& S3 n一个综合自 $ U* B: P0 K2 e/ k+ G" d7 q2 @9 n& G3 ~) H辅助动力装置, 9 ?3 V. R/ ]4 [; f2 g+ x8 b! b7 x% a% [2 F; A% l( n 航空电子学, 0 n2 I/ j6 c& N) H' u6 q是航空电子领域的一特有名 5 T" m% Z9 v# v0 }# G& @% v' L `6 j5 K. h5 m7 O- F8 Y$ J) s/ S7 s 流压缩机,, A2 ]" ^8 J# f& W& H. s- `) u3 ~0 z 一种用于燃气涡轮发动机内的压气机。空气由发动机的 6 V1 p# w! B- h7 @9 p8 B部流出。9 R: w; Q1 i& Y6 G. e* E, m: V 线, / F- J, t# ]& g( E; C1 _" s可让物体围绕着作旋转运动的一个想像的直线或实际 2 s4 e) G0 F0 ?( g3 y在的部件(如轴)。 7 x8 C5 f* Q; B+ X* {/ n+ n2 Q1 C; L0 Z4 D 前部轴向流人,压缩后,由后/ f+ ~9 E! A6 w3 Z. m$ v; y% g1 }9 d, d3 |# ?# h; \! J( ]5 V 英汉对照民用航空词典B OEING ' o: d5 R) m/ [8 M& Q& ]TECHNICAL DICTIONARY 168 A" C! e4 [; r6 F' i. T6 S B 2 w" ?. o+ L! Q1 zACKCOURSE APPROACH, An approach to a runway9 g( L$ B* R* l0 m0 w6 V versed. 2 ^. Y$ h" L: a6 down on the EFIS that ! F" ]3 l) {) loes not readily change, for example, navigational aids.5 k: F* g/ G" l p' p1 s) \7 {8 w vement in the tank or reservoir. ; Z7 G1 d2 b# KALANCE TAB, A small hinged moveable part on the * G) |! F, T% _' f3 P3 {$ n6 wailing edge of a control surface (aileron, elevator, # o) X$ `6 a C; X# g3 P1 l航道进近, ' l3 ]- T+ \+ D* z" Z! I: y相反的进近方向。当反航道进近时,无下滑; s8 Y1 X* p' m: o3 g1 o1 U 显示在电子飞行仪表系统上不经常改变的数据。例如:* u) ^% w" M! T% ?1 e 航设备。 8 U m4 E5 U2 p! u. W4 c8 m在燃油箱或滑油箱内阻止液体流动的隔板。) @& R2 x* D$ r) S! x8 Q3 e9 @ 动补偿片,) ]' k6 B$ K0 ^9 n 铰接在操纵面后缘(副翼,方向舵,升降舵)的可动部。( p: P" p) U5 [& w% W L 与操纵面相反,以帮助操纵面运. Z+ X) |1 Q4 w B # p2 `: P D! z* N8 Lwhich is opposite the normal approach. For a3 a' v' _1 c7 l7 V$ y% \ backcourse approach, glide slope signals are not 8 X. O) ^) [7 B+ i( F, Yavailable and the sense of localizer signals must be " p/ X2 n1 `) ure & y; j# ^0 r+ L/ V6 j; y O: gBACKGROUND DATA, Data sh* C- T# {4 i: P# K7 {7 [% h. i& m d* E4 }% \6 E' J2 E BAFFLE, A partition in a tank or reservoir to prevent0 Z5 N/ K ]1 h/ P fluid mo' D- R, z$ n% ]; @4 b/ e) M8 R B% w1 K1 X1 l3 Q tr% g6 g# Z1 W Z% { rudder).The tab moves in an opposite direction to the 3 n; d1 a0 J4 v. I3 Dcontrol surface for assisting movement of the control 0 t7 q2 N% l: F# K: fsurface. 6 }1 T3 k4 E! ]8 _: E1 R! G8 O. R n8 u; ~" k9 y% B) X与正常进近: s4 ~* ^' S' n 道信号并且航道信号也必须逆反。3 Q8 t+ _# d! ^) `, I6 t0 G% N5 ^- n 背景数据,5 p1 G5 x6 D& `6 Q6 z( i, T; u0 l1 \0 W$ p9 r+ `+ Q9 \ 缓冲隔板,$ n3 B$ Q; i$ F) D+ h! d3 \+ m- e8 S% [: E5 U 随动补偿片的动作方向 $ k* l0 Y/ n( k$ L动,减小操纵力。. X; b% J2 a! H+ B' ?) p0 f E 英汉对照民用航空词典B OEING% O$ x: d" n* d- f( W8 z) g% l% | TECHNICAL DICTIONARY 17 0 D" R/ L/ D9 V8 ^1 k7 O# YBALANCED FIELD LENGTH, The field length8 o3 ~$ J" \6 P$ x* {1 U associated with optimum aircraft performance when1 i7 w' J0 M F7 Y5 V$ Z5 j& R0 ? bstacles are not a constraint. In this case, after engine7 l! K- b& N$ e' s% N) T" | ilure at V1, the distance required to accelerate, takeoff# l7 l5 E2 C) ]- C; ]8 c, L+ K3 | nd reach a height of 35 feet is equal to the distance6 R7 A: e1 r3 X) O, L- n) } ALLAST, A weight installed in an aircraft to maintain8 {: ]' U9 g( m# Y ALL NUT, A fixed spherical nut driven by the & v' ]! ?# |- jAR OUT OF VIEW, A signal used to remove the flight4 t& N' }4 y- K% b9 {% ]# r AROMETRIC PRESSURE, The pressure of air above, u, B7 f$ r' ?# L( n' B g) or 2 l( J9 l7 r1 N% I5 N I* Y) @millibars (MB)./ Y% @# Y" I& N* B, I/ _' F) v4 c+ D ATTERY, An electrical device for changing stored + p% y: d/ F! N# Y性能的场长。在此 7 K6 J% f* F& {# f0 a. @6 o$ }$ S况下,V1时发动机故障,要完成加速、起飞、离地359 u7 i$ z4 J% Z& C; P6 O" Q 尺所需距离等于相同速度下完成全停所需的距离。9 l* z5 s% I _% {2 E 舱物, d% y$ R$ r3 K" @! y! W重心在许可范围内面装载的配重物。$ {4 O! x L0 h$ w0 n 形螺母, 4 l7 X R% q$ \的固定的球形螺母,用以使襟翼和水平+ j% J% N! o7 \" K$ e 引杆消失,/ u0 O/ G' U. b; ]3 X: T& J) a 指引杆的信号。 : h9 E9 L# o3 E5 b压, 2 G! o o5 K# m9 W( b1 K( r" s压力。通常以多少寸高水银柱(in 1 k( w# f$ y" n B T9 i. i q$ q% s瓶,- ^. D! r; c6 |& F) M) R 的化学能转变为直流电的电气装置。 * M4 G$ S& X. s* G2 Z; m8 @o " c* F" v% k# Pfa ! k4 `+ i; X2 q% {1 wa" g, F$ Y, n( T6 a) s required to stop from the same speed. 1 |3 r) Z: q: Q$ L$ EB. T0 K! a0 Y/ W) J" a R9 p# ^ the center of gravity within allowable limits. 6 r: K! P" U7 _/ ~8 \4 P) s) PB( z& i6 N/ l% j5 l2 t! d( S/ g jackscrew for flap and stabilizer movement.$ O3 _3 y3 H& q4 y; K B- `5 o) f6 ~6 E director command bar(s). : q2 m5 Z9 R: ^B 4 @& x1 v6 Y. i4 R8 P+ l; Kzero pressure measured in inches of mercury (in H : P4 V$ `/ o, _2 y" S/ kin 5 |6 L* q4 G" H- |3 q; CBASE METAL, The underlining metal to which alloying p- X; Z! V" R! J D7 w% f agents or metals are added.( s; Q) W1 t$ i# L% i1 R1 C+ q B , f" C7 j4 o; K1 ^chemical energy into direct electric current. " }: C$ ?# a q0 A: ?; B \平衡场长,5 U6 R2 b, b g1 z3 x 当障碍物非限制因素使飞机达到最佳 8 v' H7 Y% o/ \- K1 r, Y Z2 V9 {5 g: r7 j( y! \) m( U9 H1 A0 |( \; t8 j, U% C, b8 f. I( N; s; b为保持飞机0 k# |, Q/ P) s/ n) z$ ^6 S, l8 g1 _* U$ V* J7 d( F 由粗重螺杆驱动 - G+ Y# J4 E8 i W% i7 d安定面运动。 2 _& ]4 j8 C2 `5 D: @7 n9 O6 m% c; o( Y$ J# s/ q用于除去飞行% H0 I0 d& B( s C& ~$ i5 O0 C# n( p: \1 E0 L0 f( B, c' _ 零压力以上的空气: a3 x, E8 p* e M+ y Hg)或毫巴(MB)来表示。1 E; m% H0 q' R9 _: E5 Q1 a+ U 基底金属,& w+ {6 g2 C/ [ 指合金中的主要金属成份。4 n6 |' c( D. `5 I/ h+ h' ^( q$ z3 \4 F3 L将储蓄( e" \8 i7 e8 I7 h! v7 r7 w 英汉对照民用航空词典B OEING ) W" x" b: M& X- `TECHNICAL DICTIONARY 18 3 l; y% n% @ }$ I* {( _- QBATTER2 n% t8 G- h5 \% |! ~ direct cu: f2 ~& O. X; m5 R9 H2 W power su* [) s' A4 r) k( z' Y4 p+ H Y BUS, An electrical conductor supplied with : c6 s) |& s+ d6 D2 Hrrent from the battery or transformer-rectifier for0 l" ~3 z, h. j6 g. X pply to operating components. M* A8 }7 i/ o1 Z; s% \% ^0 @ CHARGER, An electrical device supplied5 `. S5 y5 B# p1 J# \! u ith alternating current, which produces a direct current+ D% w4 o T6 |1 W( Q7 z: \/ ] utput for charging the battery on the airplane. . j4 `) x' N8 n# h9 tAY, A compartment in the airplane structure.6 r4 {9 `) S% {+ T" N CD, SEE - BINARY CODED DECIMAL / v6 d4 v2 b0 K. gEACON, A device which emits a signal for use as a$ E9 I7 u+ B8 r2 Q uidance or warning aid. 1 b3 j! ^7 i! c. eBEARING (NO. 2), The direction from an airplane to a / J( B# @0 y0 i- m" e& m/ lground station.1 o# E4 P8 ]0 R* e 瓶汇流条,2 {; Y' i% a {0 g; q 将从电瓶或变压整流器来的直流电供给工作部件的导 : R% z- D2 b* P5 l6 U1 D体。) B. \, m; f: G* L) i( N# A 瓶充电器,5 `/ b4 z. w' a8 r4 o 用交流电向飞机内电瓶充电的电气装置。带有交流电的4 i6 \# A5 N1 q4 Z- L 气装置,该装置产生直流电向飞机上的电瓶充电。 5 |% w9 @, N- m舱,. _' @! R$ N4 d& l7 [7 r 飞机结构中分隔的空间。2 q0 P4 p0 B9 `' W& x" f9 X! @ 二进制编码, 5 |! o0 x* |8 N6 s. `见Binary Coded Decimal " }+ r# p6 a7 s" `& m- S' ZBATTERY1 b$ H! a9 s" p0 u( B2 {, { w- j7 u* Q% r9 t. Z/ c( W! m1 A% |% l o 2 t4 P2 [" b& h1 _# M r6 sB # X# Z% r8 d& i$ F9 xB, d) _, k9 h5 ` B " d8 H6 t! m; D1 Sg+ `, H2 b0 Z% ]! G BEARING (NO. 1), A surface that supports a moving % F4 E* }( K+ c8 W" `# \! o5 D4 u& \, Opart and reduces friction between the two. . s/ m2 q0 ?0 ^0 {8 M% m! W( l. T6 v- i( C6 v. ^* d- ^) K+ V( W9 V( ^1 l Q0 p% l7 O: `8 y7 H' H( F* k* i& S, e# B. P7 Q# D p" ?& U1 a! ~/ T3 i! X# H# C- M. W) _6 h' \# z& [+ S n9 M 信标,0 `6 Y" ]! L( f0 v 发射引导或警告用信号的装置。 N$ X% N8 c& F7 p 方位(NO.2),8 a) P+ w' m- L 从一架飞机到地面台的方向。+ w. t! |8 d0 p: v9 B0 A, }7 t 轴承(NO.1), 2 Z+ a6 u& y6 o' ]用于减轻机械转动磨擦的机械装置。+ s& Q. i0 e- Y3 i1 W) s- q 英汉对照民用航空词典B OEING " @- g C; _2 jTECHNICAL DICTIONARY 19 8 o) v: K; E5 {7 }" s9 ` [BELLCRANK, A double lever in the control syst! h6 e4 ?% h2 b changing direction of motion. `' |& F8 ?( @em for - P, G: G9 g. h- Dct in the7 S6 r3 } Q& ~! i9 T3 {; k2 }8 ` neumatic system for absorbing expansion of duct due4 B, \" `, q' E$ Q2 p6 E3 @ heat. 0 I: e) ]& w+ }2 t) a5 yELLOWS (NO. 2), Corrugated folded or pleated0 Z5 ^) j( |, H' G: r2 I* p ontainer or compartment used to measure pressure.& p9 v7 o* k" l4 l" D EZEL, The part of an instrument case for locking the 5 V3 D/ W1 M5 n( V7 U" olass.3 }9 @& ?% x; o- L! z. A IAS, The potential difference applied between two p$ H1 x( ~3 [/ {! ~ oints for controlling a circuit. , p2 m3 x; X2 E* c. \1 s: XBILGE, The lowest part of an aircraft fuselage. A place 5 Y% O: u1 X- ?) ^! U2 W3 b# zwhere water, dirt and other contaminants collect. u) r0 |. u/ ?9 {. O1 D气源系统内提供管道热胀冷缩所需要的余地的波状 / i5 C7 r' E% k1 w) q轫管。 ! P1 Q. W& D! p% r/ F空膜盒,7 t# d% A/ B& M/ b9 y- @* r 一种具有波状表面的容器。用于量测气压。/ M7 ^* C, l7 O e0 S- K 嵌沟缘, 3 k4 f! F1 u L# D: X将表面玻璃固定在仪表上的圈状零件。3 v% T, v5 Z7 b o 压, ) z6 p6 X1 _& z( n; y在控制电路的两点之间的电位差。8 }/ a3 @; {: c. ?( z( Q 机身腹部, , `8 r3 m7 u$ j+ u# v机身的最底部,通常水,脏物,和其他外来物集存于此。 ! {8 F/ H9 t+ ?8 yBELLOWS (NO. 1), A corrugated flexible du & M$ \5 v! J' z1 j8 q7 z# {p9 k% H$ s* ~8 o( C to - K- g) |6 _$ K; d5 X+ ~B' W: b3 o2 s! z& c c ( z1 _1 y- A- eB + w0 r4 w# N, B" M4 ?. B( ]g P, S7 l! B- q FB " R6 w0 U+ o' Q8 j5 h& X6 Ep 6 Z6 Q1 s% s% k直角摇臂,; }$ l9 T6 ^& k- D& a 在操纵系统中改变运动方向用的双臂摇臂。 : j' L' M9 [6 S. ~; c$ q7 f7 Y+ m' O波纹管,5 e' c. ?/ O( l9 [8 t3 s+ \. [3 \5 G2 V; s6 [8 K" P/ f( v: c4 u2 N) ]8 }) ` c7 t1 X: w$ A: c1 q' v5 e/ o+ C U w英汉对照民用航空词典B OEING & G7 A- E Y) x7 I" O4 {TECHNICAL DICTIONARY 20 ' E. _; Q: _9 G( J) R {BINARY CODED DECIMAL, A system of coding each * r/ P* y; P- T0 u vdigit in a decimal number using the binary equivalent., |* k3 s' l9 ?. W# W( \' f" ?* a BINARY NUMBER SYSTEM, A number system using! v& x% @. T6 a0 \; A3 E# f+ x/ Q s & Q& G& C8 f/ `+ F% y+ t v4 JIT, In the binary number system, the smallest unit of! P/ G* f: _' Z" b6 k- P formation, consisting of a 0 or a 1. 1 o' g; L) d# ?3 E2 MITE, SEE - BUILT-IN TEST EQUIPMENT5 _$ N+ i: J: s# S# V5 G: u LANK DISPLAY, A display that does not have any + M8 f5 R, {0 v' f, K; b4 gdications, normally due to failure. 5 K) R6 I, k" L- m, f# ILACK BOX, A container for electronic circuits to record ( y0 {2 s& j6 {* U; qight data.* Y3 L+ { D' {! l LEED AIR, Air taken from the engine to power various. y: P( I5 I3 v8 S+ c ircraft accessories.: D' e O6 B4 X% A1 [( ], @ A valve in the pneumatic system for air ) S* N9 A5 N6 i2 o6 d$ [supply from the engine or auxiliary power unit to the9 ~9 t, k+ F$ a/ F% p2 Y pneumatic manifold. A valve on the engine for reducing9 c. X& e( Q2 n; j pressure in the compressor section.' S4 ~+ ]! w4 N 进制, , I7 c0 P) M. @! q9 R4 }进制, 0 T" h8 K ~. U) F" ~一般用0和1)和2为底的数字系统。1 \+ l6 r" T" f& @$ ] 特(二进位数), & D" Y; o' U! k! |; r- b N二进制中的最小信息单位,包括0或1。 0 @! Q' i, B) x c内自测系统,( O6 `, Z5 f: Z' z+ J- w6 V3 a 见Built-in Test Equipment 5 V: u3 ?: Q3 n' m0 o/ ]9 _" z) |two symbols (usually denoted 0 and 1) and having 2 a; z: k6 e) Z2 c* v its base. ' N* ~; `" H# g9 Z, [B6 e7 P% {# b. \- ~3 E in 5 V9 @& q6 \) s/ WB- s1 A( O( h, t* l% k B- f: C& [1 |1 L& @* \ in1 P ~5 D7 C5 c S B( ?" w8 A f+ t( `0 D# b fl # i j2 {9 g3 z# zB( i' Y: j/ }" m2 l" F+ } a" d7 i5 K( [7 T6 K BLEED VALVE,. ?1 b v- ?7 f5 ?' W 二进制编码的十8 a8 }. \8 j* K Y 一种编码系统。用等效二进制位数编译十进位数的每一# m# u% b* r* `) v0 F5 b' N 位。; b* x% X! C5 i' j" ~* p. T+ ?. @% X, b* z, S. m! l以两个符号(; a: h8 N5 G+ U# c( A4 D( h6 h& Z) g$ i, b J' {* M- T5 b& i1 R$ {+ ~" z8 n .' p7 a, D5 r) E) B 白显示,9 T6 ^3 P# G/ o. a; y! F 通常因故障而造成的显示器上没有任何指示。 2 C/ y/ S% g1 J& F0 K+ [匣子, + A9 t8 ^. W; E装有用于记录飞行数据的电路系统的容器。 . r- K' w$ {% f: ?' Q6 a气, . e1 b* h, T. p取自发动机而用以驱动飞机上之各种附件的空气。 $ c; T6 v) g6 C1 v气源系统内,使来自发动机或辅助动力装置的空气进人 5 G( A5 w; u$ M气源支管的活门。发动机上,用来降低压气机压力的活门。 7 _( t- R$ Q3 J+ Y6 @8 W) G" v/ m. E1 K, s6 M, n U0 ^7 z# y6 Q3 k7 b3 x% [2 |8 N$ J$ f引气活门,* O5 _! g' B: @6 D. \ 英汉对照民用航空词典B OEING0 [- L! h9 T, P2 ~6 f TECHNICAL DICTIONARY 21 ?- E4 N8 e. c# V3 ~ BLOCKER DOOR, A device on the engine for blocking 5 G' k5 u2 k% x3 u/ {3 N0 Ithe normal airflow during thrust reverser operation. ; H% s8 |, R; D5 c0 @+ r7 ELOWER, An electrically operated fan for circulating air. . c( `5 G4 ^( o5 i' iLOWOUT PANEL, A panel in the structure between0 t0 ~' z7 a; ?- F9 l o compartments that opens to equalize pressure in 7 p* U% t( z7 ae compartments. 9 Z. N0 T0 U. c8 c8 wODY GEAR, The landing gear attached to the 5 b" a) V0 u9 U, L7 B6 Q9 g# [grounding. ! s- k9 J( M! x' j; h; y正常的5 ~' }0 r8 N8 R* A1 y 气流。. Z7 }2 N* U6 H4 J, ], s1 c 鼓风机, * q7 y$ y' H2 I; O用来使空气循环的电动风扇。' @8 i- v" [, J3 ~4 a" g+ t9 R 压口盖,; `7 a8 G& W' U- `( x! b 两个隔舱之间的口盖,打开后可使两舱压力相等。 : i$ c# ?9 \+ W; w5 n, |& l; P身起落架, ^9 b1 i: ?- X' t1 J* C 身构架上的起落架。 ) a' z o" X- X, H4 ZB3 f) I$ }" A* T, X1 z# N8 e- Y B+ v, Z* l' a1 L; }0 F1 K' |$ \ tw 1 W3 Q. g8 S( r+ v$ } Z( Kth $ y- X% T9 ?- \) ?5 A _/ r" aB % W: T* o, q& A, d4 v9 Qfuselage structure. 1 p) |9 h' K* v, a' EBONDING JUMPER, An electrical connection between , F6 f& v5 R0 y0 ]9 J# `# ^a component and airplane structure for electrical ! q) w5 h& a2 K8 l0 U8 I阻流门, ) Z7 C& P* f* V8 {( M发动机上的一个装置。在反推工作时用于阻挡 9 m" N4 }1 F C; r" V2 {( q5 y+ \0 N+ u; ?: q2 k3 N- Q/ j2 K, d C. L! x装在机2 Z/ @4 C8 a0 a5 X- } \* R 搭接片,2 h1 O) ?2 `9 S( i9 l2 J 连接某个部件与飞机结构以形成接地的电接头。" d: f) y8 G+ e. o/ O: l8 c& } 英汉对照民用航空词典B OEING7 y# F2 h$ o9 I' M TECHNICAL DICTIONARY 222 ^# ^6 ?6 L4 K BOOLEAN ALGEBRA, A mathematical system for / M: e1 @: M3 j$ o4 O7 y/ dwriting combinations of logical statements.7 P' V6 c$ e3 e BOOST PUMP, An electrically operated fuel pump for 2 C( P% _& ]4 v9 [fuel supply from the airplane fuel tank to the fuel , T) Y8 _7 K4 {/ P4 `manifold., Q/ k( O. O" w, L8 n, z BORESCOPE, An electro-optical device for looking at ; D) {* x6 h6 ]# C. \+ Wternal parts of an engine through holes in the engine. 4 y* U+ X2 D6 P1 G0 |8 V, s2 ?orescope ports)+ A6 N" r: W$ D3 `6 N, U2 ^8 s5 z OURDON TUBE, A curved flat tube in a pressure gage . G$ U" w! A% f7 i7 @8 y% c! x3 |2 mr moving the pointer when pressure changes inside1 `( H1 h r8 H/ \) P: M on the ability of the brakes to. _: z. q# c' u" D4 v3 M bsorb a predetermined amount of energy during a ! q& s8 S1 S5 f2 Y; v1 @# p% @jected takeoff. 1 {) u* t5 I: F. O/ q# U用于通过发动机内的孔(孔探口)观察发动机内部件的2 Z2 O) e( L" C R7 H" e* x 光设备。 : I. ?& O5 [0 d端管, 4 b1 T( S/ e" O- ?1 D测压计内的弯曲扁管,管内压力的变化时它使指针移 ' a6 Z2 c1 o5 U& ]力。" k- H7 {! |8 y! L. Z 极限重量, . N; G0 {7 l) |" I! h0 o! y, t9 u; G8 v7 r6 {( o$ G. [1 g6 g起飞重量。. u# y5 e1 j* J [. n/ L 发动机滑油系统与大气相通的通气口。/ p3 w! A2 M8 \! j; n in( ~0 P* G% \ |. E0 c6 r( F' M (b / A! P5 t6 S6 K3 U! S% wB3 N+ c9 r0 d" y fo1 B7 H; \+ ~" U; f6 M# z. J the tube. + n9 r* \- C1 |; u0 N EBRACKET, To enclose or surround.' g2 n$ ^; |) t2 Y# e4 L BRAKE ENERGY LIMIT WEIGHT, The maximum& ^/ _; H6 z% _) A6 F4 g$ I& D takeoff weight based( b6 O S! o' t1 j6 B, v! ? a. b* j! T+ l& Y& Q re) o% [- Q l# R1 k+ _ BREATHER, A vent to ambient of the engine oil system. $ {" k7 A, n B) V3 s4 p布尔代数,* ^4 t6 T, N$ n7 m, I 一种用于编写复合逻辑命题的数学系统。 5 i' S# `1 p2 i* y9 h增压泵, 4 j! j- J) r5 _+ p' o3 W4 H5 s( V( p从飞机油箱向总油管提供燃油的电动泵。( L. ?" A; f" h* K& I 孔探仪,* m9 ^$ s4 t. L" b- q. H. ~. b: h% M( Y; h/ P7 A; X+ K0 K4 O" ?. N1 u动,以指示压 z1 U! g4 \8 |- V" c托架,& p+ H9 a2 s8 G( V3 `) C; z: i 用于作支撑、装托、或围绕之用。9 X+ h& A- |# X. s6 x* c, @7 `* F! x 刹车能量 , ?/ b- \0 t3 U1 Q1 O5 w中断起飞过程中,取决于刹车吸收预定能量之能力的6 x) O$ j/ T2 X0 E* h+ [( f# x+ m) e6 S5 T; c( b$ U' B& t通气装置,/ t1 }6 t( v2 z% y1 T0 D; v 英汉对照民用航空词典B OEING+ m; F0 B- C5 y; Q( \7 y TECHNICAL DICTIONARY 23 " w; X) x7 f- v7 ~* R3 zBUFFET, Vibration of the wings and airframe resulting; L7 w$ _* y1 \1 ]( E from unsteady airflow over the wing; caused when \1 W+ J- W* a airspeed is too slow, the bank angle is too steep, or2 @4 c6 x% Y/ U3 F# n8 n/ a irspeed is too fast. $ y% Q5 A7 x v5 uUILT-IN TEST EQUIPMENT, Equipment installed on / c8 _4 D% t; ^& G6 X) B' Ue airplane and in airplane systems to test the systems$ w7 G0 F# [3 m' O; e3 `/ m ithout external test equipment. 8 U' [8 ^6 ~; v5 p& ^& q9 dUFFET MARGIN, The amount of residual maneuver* }5 y4 j, V+ b' F apability present before the onset of buffet. 0 V# F) a" S: d$ H5 y& MUG SPEED, A preselecteed speed to be observed 2 Y# x s+ `, M4 Z" c9 m8 Q8 _nding sequence.5 N; `! b: P! ~, f7 B k! \8 `* Q4 a0 {7 |8 m* G ng landing gear operation. ]8 O, J! |3 O/ G( p6 A4 W速度太慢或太快,坡度太大,均会引起抖振。 $ A* V& K% e6 f2 I% @自检设备, 6 ~8 \' g- w2 N安装在飞机和飞机系统中,在无外接检测设备情况下, + G! q2 s8 Z8 C2 ] b用于检测系统的设备。 0 ?: C: \! B' X- @2 Z抖振裕度, / n! L! |2 l' `( m% j0 g `飞机在遭遇抖振之前,剩余机动能力的大小。 3 r" m6 I5 y: g' N. z. Q1 W标速度, ) D, R4 e8 A2 |( w在某些机动飞行过程中,特别是在进近和着陆时,飞机 + n; o8 }/ S6 _7 m7 q预定速度。% r g0 v& v- R 力装置, 3 @6 P6 ]$ y; ? G5 f# C: y架工作的一种机械设备(弹簧或减震器)。. m, {8 F1 V) h% }* q( y 流条,6 |3 m6 O" ]- B 在部件或组件之间传输电、数据、或定时的单一电线或 * O5 z1 o2 l2 F; `, Oa 2 V$ B, v/ v: k! `. eB, e# n5 k8 e& |; e th 8 T0 D7 p- S: B7 @7 F+ i4 `7 @w8 I3 `) ~: ^- ~1 B- H B X3 ]% m# ]( Vc / R$ ?* m# g4 m, ZB % l* j; M: P7 j7 R4 ?during certain maneuvers, particularly the approach and. U' V: K, I: ~5 X" | la , j0 R8 @$ E7 e3 Z' ]BULKHEAD, A structural partition in the fuselage or % C$ c8 p8 V- }2 N0 B/ Z* Nwing.6 V& ^+ k" N% x; \( A BUNGEE, A mechanical device (spring or a shoc 9 T/ Z+ d2 b7 U/ y- Dabsorber) for assisti / M7 F% s9 z# C+ gBUS, A single wire or group of wires which transfers% d) z- j. e4 h: E power, data, or timing between several units or 2 B' g$ E. `3 n7 E* l0 bmodules." ^- @7 c% P0 ` 抖振,* Q% N5 W& `* R4 f: U! t- h# W 由于机翼上表面的不稳定气流引起的机翼和机体的振 ' g9 i; ?, n0 q动。飞行8 c1 f5 \; {& I5 S: x2 w$ R0 L# k- ~1 j5 @& V9 X/ S( T" | 所应保持的. ^- A5 H! M2 C" n$ I9 e$ M 壁板式隔框, + _# f) N/ b9 } ~3 w机身或机翼内一种结构隔板。 , Y/ G4 s2 D; @; Z) m' O- n4 \5 Q9 l* U! P' n 用于协助起落! T. i0 J% E# `8 l9 j7 ?3 g7 b1 X2 ?- B" I 电线组。 % i% a5 s0 O1 W7 _: s* }8 J) Y英汉对照民用航空词典B OEING * s2 P, Z, a3 f% ZTECHNICAL DICTIONARY 24

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BUS DRUM, A mechanical connection with pulleys% P! G j. Q8 E% f* d cables in the control system.9 P9 ?) C2 j# c# S: l# [) J# V3 i and3 S0 q' r- X: W! S y l$ r l circuits for control and protection of! C; I& n& Q) C4 b lectrical alternating current supply to the airplane.2 i) S4 ]( n' I: J* y- V8 R duct for closing and opening the duct# ]- ~1 K" t% u* ?+ M, B" t$ P assage. , b% \& x# M- cUTTOCK LINE, A vertical reference plane along the: A, W, s. K+ v" z, G* B selage for horizontal measurements of the airplane.+ l( q& `9 Q* i. U 接。) D: k! |- Z+ z `, O% {# K 组件,内含控制和保护飞机交流电源的电 # U5 l: k" `" m1 S2 `/ |2 s& K* a) K! W$ z" a作动简控制的转动装置。用来关闭和3 y- q: H/ `9 `, j, O 启管道。 3 \1 S8 u# e( T4 S8 D' w% Y$ l- T) M沿机身走向的垂直参考面,用于飞机的水平测量。 ; J3 o& `' z% ^; ~! GBUS PROTECTION PANEL, A module (black box); D$ F; E( e6 k0 | containing electrica % D( c* e2 k7 g( [+ ` ne0 i' M; a2 d3 w( m* P* s BUTTERFLY VALVE, An actuator-operated, rotating + R; ?* X7 o. P( k+ @9 rdevice in a2 _- t: i3 N" g9 e4 u# e1 u p & c& P) U) L; \* @3 ^B / O) T* ?5 _9 N8 S6 Tfu 4 I1 G3 v3 n1 n. d H$ i转动鼓轮,3 j' Z2 |( @% i- R8 |4 s 在操纵系统中,具有滑轮和钢索的机械式连- @, U5 w, c& h: B6 N: z3 y 汇流条防护板, 6 `. ^2 b1 y7 ]) X+ h黑匣子式的 2 P' R3 x. f2 g' J/ J+ B' E- \+ E$ S u2 j$ e: X, X5 b, g 蝶形活门, 9 v# m; l8 x4 a" y/ s& n是一个在管道中由 - {. F- F, O) G. L( W8 Z8 V3 V4 U8 a1 j' A# ?( a" P s+ V8 B 纵剖线, ! S4 m M4 `: o- z英汉对照民用航空词典B OEING ) F/ d9 g. {# [% f1 |' jTECHNICAL DICTIONARY 254 w! L" w1 T+ n4 x1 m BYPASS VALVE, A valve through which air or fluid will9 I/ K- M8 i) [. }5 z7 T flow if the normal flow path is blocked.5 m Y% u9 ?5 O# g `; u$ q5 i BYTE, A group or string of binary digits. A byte is * }! u) t( Y+ n- K ~sually eight bits long. 3 k/ \! P/ c( ^ABIN ALTITUDE, Atmospheric pressure maintained ! b2 ^5 U' c4 d. e4 Q; v" Z$ |ithin the cabin, indicated in terms of feet above sea + y1 X: o8 q3 U3 @ALIBRATE, To repair, adjust, fix or correct the " p9 f" O( x q) e. Qeasuring capabilities of a measuring device.( h4 y$ D. S: c- j$ i: D ALIBRATED AIRSPEED (CAS), Indicated airspeed' R6 O: ]/ m& d8 K AS) corrected for position error.3 a) s' F0 R* P' F6 K1 f4 [ nical ! w3 ~$ l! H2 s/ ?6 Fomponents." X1 y# m. Q: y n, T/ }$ H# z; r9 c- W- K 节, / l5 d9 j- k, q: M8 g9 ]一组或一列二进制数。通常一个字节长8位。, b: l( G2 y' W( ` 舱高度,4 R9 U1 k# E6 F1 m0 q7 A& i( {0 R 座舱内保持的空气压力,以海拔多少英尺表示。# g2 c9 S6 S4 O( M2 K 准, p' i+ M4 l! I# z, |8 M修理,调整,定位或改正测量装置的测量功能。 # ~% Q3 H( L: p1 e+ Y- Z. P正空速(CAS), / t- k9 R& g6 r5 d% H8 s" v在修正了位置误差之后的指示空速(IAS)。 / `6 Y2 r- T2 o用来移动机件的一种转动装置。6 h1 ~4 r% ]6 f& S+ q' X2 ? u' i4 G0 p2 K2 T& N8 F C * C7 K% A" S7 b1 y% R+ ^; DC0 s6 o/ R9 v& b w* ]7 J0 W( T D level.8 {! U5 A1 ^4 p, T C5 m, z: P4 V0 B# a( f m * x4 q+ s' E9 {$ _% F8 UC' j! [; Y. ~8 }2 @7 Y (I6 F+ I r: ]- C8 s CAM, A rotating device for movement of mecha + w7 L; F# Z3 |; yC1 ^! @! z* j' a0 ~' i# Y. m4 | 旁通活门' ^4 A9 c/ M' ` 气流或液流在正常通道阻塞时所经过的活门。6 o8 i, e, G8 J& Q7 p, [: d1 d# d! W+ w. q* m( ~8 X: M2 C! B2 }9 g- r4 w& o' h) g. t" K1 } a% D% s3 s2 u3 S, y 凸轮, ) h: o3 M* Z" y% a0 R# m& f5 E英汉对照民用航空词典B6 m2 I: O. R$ L7 o7 B( O8 W) N! z; @ CAM-OUT, An autopilot condition in which the actuator ; A% C ?1 d4 z0 ^8 i2 C bdetent piston is overridden, either manually or by the $ Q) K% l3 S- W* D# ~) bther autopilot actuator. 5 e, V) Y o! SAP, SEE - CAPTURE e9 T& I9 d; e3 \' R9 p/ A" r APACITANCE, The measurement of electrical energy 4 |' a+ H7 L2 H( x8 h; P! Ftored in a capacitor (condenser). }& V' m2 S# d9 uAPACITOR, An electrical component of two metal- W) U8 e# c8 I5 m. x lates separated by a dielectric material, for storing + T( n: D, e8 {% D: Ilectrical energy.- U% U3 P5 @0 L3 h$ R- M CAPTURE, An autopilot or flight director function to " f- M% B: h2 f0 u) oacquire a selected mode. 1 q% X% V; Z0 ~& D7 L+ DCARD FILE, A container on the airplane for printed2 }) g9 I' S1 { circuit cards.8 W5 m0 _, Y( Q9 Q/ t" z4 R9 q O 一自 & x8 G% J Z; x0 |, V/ c% A动驾驶舵机所超控。 2 i- ^# ^, y' W: Z- ]2 e截获,8 k; U2 p+ I5 T! ?1 i8 `$ ] 见Capture9 Q( p* M- k5 G( M3 }; Y2 c" R o - W: n7 Y4 M- P9 A) [C ; B& o) I% i* G0 NC% N; Z+ u0 }- L" _% ^6 ` s. i l: `; u+ k& A' ]6 A- F# M C( [7 d7 S+ _5 Y! K p8 w# X& F9 s! } R& I5 N e2 J! i M+ v5 \- R0 e+ U. V4 R, b: i 凸轮不工作, # X- _; D/ E1 \5 Q! g一种自动驾驶状态。此时舵机锁定活塞被人工或另 # ~) J6 o- H/ `) J) U$ {' `* W+ b' d% T! I( g# q 电容量, ( Z' C. J' l* c; o1 x& T* v( y电容器内所储存的电能的量度。+ L; r1 D j7 x/ b1 b 容器,% n* H# A2 U) E+ F3 {/ d 两片金属中间用绝缘材料隔开的电器。用以储存电能。3 B: e& a0 Y; v" L 截获(CAP), $ L* i$ B7 e' B6 D. W自动驾驶仪或飞行指引仪的获取选定方式的功能。* r, c6 |, _4 M: r 线路板盒,6 L* o& y [& F9 o( X9 V 飞机上安装印刷线路板的容器。 % s' ~, H" s; O# O9 a+ H2 @' |) S$ c6 Z+ t: P OEING% _9 Y) B5 |# l3 Q9 \ TECHNICAL DICTIONARY 26 & w/ M2 V' ^! o英汉对照民用航空词典B OEING 0 p; q) b8 A( r/ \+ M hTECHNICAL DICTIONARY 276 o+ v6 g$ x" ]7 J0 X& V# @, k8 g CASCADE, Two or more similar circuits or amplifying- W6 X! E4 k! I! P+ u$ S6 G stages in which the output of one circuit provides the 1 T; n: v7 N0 L7 Hput of the next. ' p6 g; Y# z8 aASCADE VANE, A vane for turning the engine airflow; ^0 ]; G- ^$ P6 w uring operation of thrust reverser. 6 ^$ a1 g1 o" `# W4 e. vASE DRAIN, A drain carrying lubricating and cooling ! i& U5 N s/ H+ N2 z7 u; duid from a hydraulic pump.: q! ^$ Y) _4 ?' t: J) X5 m ATHODE, The element from which the principal / L+ m7 }. N" |4 C/ Z- Q2 R' ftream of electrons flows. $ d, t- y8 }' m; V/ s, lATHODE RAY TUBE, An evacuated glass tube with a + S, L) o8 ^! [" W0 }7 K6 b, {CEILING, The height above the ground or water of the3 x( q: J8 X2 e8 x$ E- t base of the lowest layer of cloud below 6000 meters; }6 C& t7 x! S% m (20,000 feet) covering more than half the sky.5 p* h j S' E P; ]* l8 r 程。该- i5 g* \, M4 L) s 程中,一个电路的输出为下一个电路的输人。 : T! j7 |, L3 e) y' S叶栅叶片,* C# h1 c9 f4 j# I" v 在反推工作时,使发动机气流向相反方向流动的叶片。 % R+ p( U+ ~# _. R9 i匣余油管, 3 k, G# H: P6 [" H! P液压泵多余的润滑液及冷却液的排放口。2 J) `# q9 q; p" R 极, ' ~7 i: [/ c1 R& C, n电子流流出的极位。 $ \% _9 C& C$ r; Y) o/ K% E极射线管,% Z9 n7 y1 `3 ^9 g 有显象屏幕的真空玻璃管。用于显示信息。 $ L! ?# E* N7 b% y1 t* b5 I云高(云底高),' K7 X# q8 ]+ V' J$ h 6000米(20,000英尺)以下已覆盖一半以上天空的最 + z# |2 p8 V0 b* B, n低云层底距离地面或水面的高度。5 Z6 j; Z8 c6 A+ ^: x6 { in ' V% r/ D7 E4 `% ]8 X7 KC5 D, P* p, P0 `5 C/ f; }; I d) `5 k( @5 y2 c e$ k1 \ C E- [9 S% Y1 _, A* v, d fl) l7 U0 g% p \- G7 a C' B, F9 J. p1 I s 0 _: a& J' s, _& N$ n% yC / A! T/ c' X, Tviewing screen, used for displaying information. 4 Q W( V1 k" G; ?$ n3 r8 w级联," \ N" Y0 ?; G* ?# w7 M4 c* e 两个或两个以上的类似电路的逐级连接或放大过+ \6 v% M4 Y" X7 n9 K& T. l) E6 m* y, {9 y5 \6 f% }- r2 G- W2 U6 r" ]5 g8 x# y, O0 W9 M% N3 Q; Z# b9 X% x; U# h. p* H 一个具! n! L' l( ~' C- U6 w/ E; ~ 英汉对照民用航空词典B OEING ; }3 s+ w3 F' W a; ?% V/ ~TECHNICAL DICTIONARY 28. r7 t# K# ?: @ CELSIUS, A temperature scale in which zero is the. Y% B# L4 U: [1 H4 c freezing point of water and 100 is the boiling point of3 \. Q6 W1 p) _) Z P3 z Y2 A water.# | {* [0 I7 L6 f6 L CENTER OF GRAVITY, The balance point of an object+ Y* |7 o) q& C r rigid structure expressed in terms of percent Mean# ]. t& ~ Q. Z; G" w2 V/ P erodynamic Chord or in inches from a reference point. ( s- l0 S+ Z5 }ENTERING CAM, A cam for moving a mechanism to a* u m+ ~7 Z0 b# @5 z eutral position.7 Q2 y' _8 }1 R4 W IGURATION, A configuration of the O7 A. f3 ?: `# P! o) C- ?9 q ircraft approved for operation by the local governing ; i2 A E' G9 I$ m2 Dgency. ) H; |4 S. f: P6 F# R/ Q+ P# yENTRAL PROCESSING UNIT, In a computer or " M" T7 l6 R. Migital circuit, the section containing the arithmetic and + a# L# F& `6 n+ Jgic,control, and internal memory circuits. 2 ^7 ~0 v8 s" TENTRIFUGAL FLOW COMPRESSOR, A type of* C1 C7 n$ A+ x# t( O* C ompressor in which air is taken into the center of the {, b* ]2 Z2 A; c; H+ Lpeller and is slung outward centrifugally into a diffuser ) w1 y5 E# ? T1 p' \1 }, Dhere it is slowed and pressure is increased.$ t# D8 i, W8 s0 H; u5 \8 F7 { CG, SEE - CENTER OF GRAVITY / s1 y4 V( C, I; n构的平衡点,以平均气动力弦的百分比或 7 Z2 _- ]% x* {8 ]& q; ~某一参考点若干英寸来表示。5 H+ u5 c) y4 M 中凸轮, & n) Z5 K. D/ s3 n+ y将机构移向中立位置的凸轮。 $ O+ A2 a' T" @, u# t格的装机状态,. `, ` }5 g$ M' \% Q" s& h 由当地主管单位批准使用的飞机装机状态。 . |5 i) Z" |% d! q4 X中央处理器,3 S& R/ ^& [- g! z3 p4 e$ n/ F 计算机或数字电路中含有运算,逻辑,控制和内部存; g4 N1 p+ p! P* ~+ g) B$ @ 储电路的部分。& u2 Z/ I. k7 K* y: e 心式压气机, w% U: d. w- O8 a" d' h1 {" W) S T压气机的一种。当进气到达叶轮中心时,被叶轮离心抛3 Z j' G2 D, m 进人扩散器。在扩散器中气体流速减慢,压力增加。3 F3 ~+ C9 [% `( T1 m! q% @( _$ l 重心, 7 g+ ~. Z [& `见Center of Gravity ; W. d2 c! t5 Ho z* @0 G: \% Z A/ d- E& a/ M5 z! r1 A* u- O C# n" Y4 F' z4 ?/ _2 I; u n1 t2 ~' b2 p& j. V/ Y/ ~ F$ K4 t CERTIFIED CONF 3 X: |9 j: P2 Q. C: c" Q$ Y" S( Ta 4 U) s& K8 M# ka+ n. S5 l4 _9 H' |) q4 P C1 g+ B; h% h5 t; { d 0 E7 c; V4 r& H( U8 blo% r% a, X! b# }# `' x C # s; w) e# B+ a* _) X* G8 jc9 ?1 F) M7 ]2 J, Z, M8 W7 F im + G1 e0 K I3 w, t7 jw$ G9 l1 V) T( W1 e" C' h 摄氏度(°C), w' O, [) j4 Q( ?$ \ 温度的度量单位。在此单位中,0°C表示水的冰点, $ G7 ]/ [! J4 {, V8 j100°C表示沸点。6 B+ W) e8 }; |" L1 n" W 重心5 F# l* \+ l3 {/ V4 ~$ t' ^2 W 物体或刚性结* i- o0 p2 g8 j! Q5 f* R+ `% M) O( D9 L4 z" A3 M* }( T4 I0 l% ~- w/ W, p. ?& V* L/ O# A: j8 R! k3 T+ X( [/ z7 F. x0 K( o: P% s" F( ^0 |: l) N英汉对照民用航空词典B OEING# _4 D; p1 G' b6 ` TECHNICAL DICTIONARY 29. w- }; j4 {2 l+ s CHANGEOVER, Conversion from one mode to another. / E1 Z% U( }. p( |; QHARGING VALVE, A valve for supplying air or fluid to4 h* {2 O8 }( y% x0 k: j4 ~ HECK VALVE, A valve allowing flow in only one' ^; K3 h3 R' h. H irection. See Non-Return Valve.$ O8 \5 D; ?% n& t HECKSUM, In a computer, a summation of digits or ; P, ]% {9 \0 G4 z3 N" q: Oits which are primarily used for error detection. # ~8 B* D% F! x, G0 ~* Y+ Z$ c) U. qHIP DETECTOR, A magnetic plug in sumps of ! V l+ y3 r5 B9 bbricated components for detection of internal failure of & O2 U# [" Z2 S3 X9 k7 _- ?e component. * p& a+ E0 T0 W' I1 ^6 GHORD, A structural component of spars or frames. $ v0 k( v* h# s6 w( h' G, E5 y添活门, : u6 t( X: l/ t$ R8 G' Q! ~/ S& @% ]器充气或加液的活门。 8 G5 Q1 K( h! V Q+ ^单向活门," B1 F) Y) e8 w! ~ 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) z( b3 I3 f- X. k6 u# X a reservoir. 8 h& A8 u# T4 l! A( I) GC5 o, P4 o, l. t% J/ Y* j' m d& l3 i) s# t/ J) A C $ l8 b1 F& k; d4 u5 eb 8 d4 ^) T w4 ^8 eC ' b2 g: n3 k' }# v- G( O6 clu : ~7 C: R% a3 Q) jth8 ?, h- W2 z1 q. b. A% I# k _; \7 q% R C4 R# T; s$ h% _; K q4 b 转换, % s* M) w, b; H+ _& x2 T由一个方式转换到另一个方式。. ~; _; H7 B/ x; }/ L8 X% ~3 b) D& `+ \$ o2 B5 k& M2 G$ i# ^$ x用来向储存/ u* x# \3 k) @7 t& O3 G7 O- @- q5 f4 U% S 总和校验,. `& w3 ^* @4 ^9 n3 E _& I6 V! I1 h 计算机中,把那些用来探错误的数宇或位数的总和进' W& ^* V& ], ?" a 求和计算。 5 @% m" d( a" m% L4 I: Q4 t属碎屑探测器, 2 |1 A+ E3 T+ U% K8 C* z装在被润滑的部件滑油回油管路上的磁性塞子。用来探; G4 n' s3 b, S8 {1 ]0 _7 p1 U 部件内部有无损坏。8 k, y8 P, M3 M. D: L2 c( X1 e 弦,5 w, ?3 y1 _; N+ V. D1 v 梁或框架的结构部件。5 b' R) t( J' y0 \1 ^" ]# Z. y: Z1 `% r& ?; O( A) M& K, ?( T. j' f% Q- p) X: k" w- U$ @$ v4 T- S4 |: y: j Q. J3 r. b3 r1 ^; b& B( Y, p b! l英汉对照民用航空词典B OEING* d! y; }% u/ \, l! i1 f TECHNICAL DICTIONARY 30 : u7 l; E/ W6 d2 UCIRCUIT, A closed path through which current flows5 {4 |0 I- r* L% @, L ource.% k! Y- s7 D% D$ m8 I( a% |+ R) A& U IRCUIT BREAKER, A device that automatically' H$ l H, J: e, A eactivate the system.7 q$ H5 n! A# ?4 R- t+ l lear of all non-frangible objects which& t; }% S" e( U" V6 l* j" X ay be used as takeoff distance available when$ y- ^. X. W1 S z* U alculating a takeoff weight. ) { w* ^2 T3 b6 Ur water under the control of the appropriate. W; h! V/ Y4 t5 j/ g. Q uthority,selected or prepared as a suitable area over ; k1 `* A* _. s) ^* Uhich an aeroplane may make a portion of its initial5 I: K9 K+ [8 D8 H limb to a specified height. $ N: H8 n, D. S! ^( w1 N+ Zincreasing.6 H Y$ k. D1 a. B F sed5 a' n4 c' H& O$ s9 d1 [ V% \ LOCK SIGNAL, A continuous string of pulses used for1 S, L0 m x$ `* d 开关, : J7 U( c4 E1 g" [; @# _$ @! k+ z故障情况下自动中断电流以保护线路不受过电损2 J; k' J( W. M+ y 体障碍物的区域。在计 4 y5 T: g$ ]9 C! `6 f; j起飞重量时该区域可作为可用起飞距离。- p* z1 I. z- M+ K2 ? 是在有关当局管辖的地面或水域内一个界限明确的长% N) J M7 U4 ?0 u; N& ^ 形区域。在这个选定的合适区域内,飞机可完成初始爬2 A5 i5 d4 v! d$ y. a4 x 的一部分,上升到一个指定高度。 7 J8 d* h& { g$ h飞机高度不断增加的飞行阶段。- p8 G7 l" r' {5 k# a' M 钟脉冲, 4 m1 i+ P( q! E: u% J( U) o5 ^/ ~步的连续脉冲信号串。 C8 ?3 q, O5 `+ c. j from a source, through various components, and back # S5 J) i5 Y/ v* v. o/ eto the s6 B& p S/ `) S' D6 H C 0 K0 ?$ G% W6 P( d7 kinterrupts the flow of electricity (current) during fault ! e* r0 V* q! \: N Qcondition to protect wiring from excess current. Circuit7 B# Q- B2 ^) y: H: | breakers are also used as a means to manually; F( E3 J5 t3 y5 y8 y5 Y; u d2 m' R; `7 j' A$ v- I1 b1 v CLEARWAY 1, An area beyond the takeoff end of the . c# w% X8 K7 b+ Urunway which is c - \% M( M7 N0 r$ J' t- Im % T9 Q% ]" S3 o% \- cc+ u1 ^6 {6 `) v9 Q# @ CLEARWAY 2, A defined rectangular area on the 3 d% [, P6 }$ f( A% l8 @7 s3 `ground o. ^$ {; {: m$ m2 v0 M* l9 \ a 7 A6 |( o& s5 c$ t0 b# Ow# C% {! y5 N. k7 N/ p: O- Y0 G0 \ c 6 @: o+ O$ d: m. U3 JCLIMB, Phase of flight where the altitude is% l# Z+ s6 v( z9 t4 P* O) f CLIMB LIMIT WEIGHT, Maximum takeoff weight ba 3 S0 p& }8 T# con a minimum climb gradient with one engine 7 q( q, ^/ x7 I- Rinoperative. ) K+ \" d& ]- | KC : Q! E6 F( ~5 b' m. T% j; s8 jsynchronization.* z V2 a/ h" C. k$ t; ] 电路, # h! Z2 h$ ?6 ?. t$ O一个闭合的回路。电流由源头流出,经过各个元件流回 - a. z: g" g( T源头。 5 l# x4 o: _" C; ?+ A; E, g7 f% r0 G: |) T能在. S6 e8 \" y7 ^ 坏的装置。跳开关也可用于人工使系统无效。, B" w4 [' d8 A# { k$ u" ? 一号净空道,$ e* P1 i* z% ? 是跑道起飞端以外,不含任何刚2 n% r6 L0 D R: |4 `1 N' ^& {+ P3 _0 {3 `6 e# k# U# g# q8 P 二号净空道,' e! C6 t% O G- T5 l: }+ T. G1 A8 ^5 E1 I+ ?" P; A x; [0 E) q2 f 爬升,% Y. S2 z3 u: k1 x: [4 B 爬升限重,) `7 Q3 B2 @/ ? 取决于由一台发动机工作时的最低爬升梯度的最大起 & V2 Q* ~. |8 R飞重量。 a- c( H" C6 N' y% ^* e' e# n$ A g/ O1 ~/ O4 \用于同 * a# H% W9 `+ u( E1 V! w( A J5 K英汉对照民用航空词典B OEING 9 D7 J! ~: Y3 @2 L( MTECHNICAL DICTIONARY 31 / i2 J, q) u/ c4 ^1 [6 dCOALESCER, A device in the water separator for 4 B" }! O, O$ N9 C9 ~5 E. Mollecting moisture from the cold air. ( X3 k8 ]- k1 @- Z: N/ en antenna with a receiver or transmitter.7 y8 r& \- D6 x he cable has an inner conductor and an outer- g4 A: t ?3 p( @" i rounded shield. 1 B! m7 w& E ?$ ^ting one inside the % I0 A/ b9 r9 H, ~) @' ]' Z/ F% s5 Ather for rotating the low and high pressure ; \/ c! s9 Q4 o. S' e0 l: uompressors by the low and high pressure engine3 ^/ u- z+ ^/ W rbines.- C: D: h5 ~1 \& T, x' O OMBUSTION CHAMBER, A part of an engine for/ @/ B6 x( A+ Q urning fuel in the air supplied by the compressor." K$ B6 t/ j, F0 i8 v D) C2 p 置。9 v2 \3 B2 l0 _1 y. j: f! q! z T 射机的电缆。电缆3 Q/ r& ?& A) U% x4 c 中心导体和外层的屏蔽所组成。 5 j3 M6 m% R, a9 d两个套在一起旋转的轴。用于使发动机低压和高压涡轮 o9 s% c/ z9 j; z7 v/ t别带动低压和高压压气机。 7 l/ s6 w! n2 D* T( V. \+ a烧室,! N7 M- q# t% m5 X+ q2 C 发动机的一部分。用来使燃油和压气机所提供的空气相 " g) X: ~0 g+ J- _0 E合而燃烧。

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发表于 2008-12-24 21:38:35 |只看该作者
c 0 G* a; U- A2 v) b+ R: XCOAXIAL CABLE, An electrical cable usually7 v t4 E' _3 X o) W4 X6 }9 x connecting a. f/ C1 Z* H# q$ {1 z# L5 I T 6 ^. S' _. J7 v! S/ {, |% c' l' |. r& ~g' Z3 y- V4 R5 n: N6 p- f5 l' ?2 y COAXIAL SHAFT, Two shafts rota , |6 x% w2 ^$ ]! Ro9 v& v" o0 k. [" o- u c " t- L4 G* e* \6 P+ x8 Ftu# q- l; \! j5 v C ( ~9 M" g: `; K9 b: Pb/ t9 w' w# L) X7 f3 m$ D. u 凝聚器,9 j, Z) ?, h# d- n% X 水分离器内收集冷空气中水份的装0 h1 G% C. Q. ^5 e' ` 同轴电缆,1 M0 b7 g9 l9 B; g% b. |* {7 ~ 一种通常用来联接天线与接收机或发5 K' p; I4 w- ?) j* L$ W) U1 F- c" q& D. T8 V( _ 同心轴, 7 Y$ c |3 }/ X9 E7 |/ Q1 C! g2 G( _- Y+ N% _- X: T. D o9 k. c2 J' O# {1 d" I; [, c Z. ~3 E 英汉对照民用航空词典B OEING ) p4 e C7 C0 P0 S# Z8 ~( QTECHNICAL DICTIONARY 32 - f! c3 o" n! V/ }9 t/ F2 OCOMMAND BAR, A flight director pitch or roll comman ?7 ^; b$ S( B$ `& \4 mindication.& R+ G* G( t0 N8 t H d e. f, P* C+ J* C OMPANY ROUTE, A route flown by the airplane 6 W' r5 z2 c1 g% I7 K% s4 n) eOMPASS LOCATOR, A low power, low or medium5 p7 r2 v. K3 F8 q equency (L/MF) radio beacon usually installed in 7 z& x# U" C/ U& i6 Yonjunction with the outer or middle marker of an ; D& T) q* a6 {2 ?" E z; ttor (LOM), A compass9 Z4 i* n% |$ i0 K) [0 t locator installed in conjunction with the outer. f. g$ _+ \( s2 E, ^/ G marker of an instrument landing system.$ Y( a- E4 [: W/ P ss9 \ n% L5 U) N `; U, T le( i0 ?1 _: K; G! b, d. X OMPENSATION, To offset, balance, or counteract.. r: L! p: Z6 l4 ?* m3 ] OMPENSATOR, A dual capacitor for changing the fuel& j! c5 r1 w* L6 f0 X- T aging circuit capacitance due to changes in fuel4 h, N: N9 @8 h5 P' \8 S ensity. 4 R& T, k+ H A& L* Q( ?: SOMPOSITE MATERIALS, Non-metallic materials used* z0 [) X( O E9 O) v r airplane construction. Fiberglass, Nomex, Kevlar, 6 r; H; v! V# R8 Z5 I. Eraphite Epoxy are composite materials.7 W; z. z2 L6 n' T& e$ h 司航路,/ A8 p5 N3 }' {, y* n& D J7 h 在飞行管理计算机数据库内由航空公司飞行# b7 {. z8 \/ v8 {1 b 盘定位台, j* A. \2 q, j2 Y; w' A& I: P 与仪表着陆进近系统的远距或中距指点标配套安装的 3 E# v$ f8 Q) N+ W4 w8 p' {功率、低频、或中频无线电信标装置(低功率NDB台)。 5 x% J4 k3 \- _' I# ^程序中用来导航。 [; e2 C. g* n% b ~1.远台,$ i3 v4 z, E8 S% D 与仪表着陆进近系统的远指点标配套安装的罗 - u' s6 u$ E3 F& g盘信标台(NDB)。/ X" l' B/ w1 {# o% q! s 偿,# O6 x8 r+ c% e% h7 u4 V 抵消、平衡、或中和。! m" e) [& M8 `5 b, o 偿器,; ], Y2 Q. Y, m2 r/ D8 D% A 在燃油计量电路中,用来改变电路上的电容,以与燃7 G$ b+ [3 o. n9 ?9 W 密度改变所引起的电容改变相抗衡的双电容器。 # [% N8 C/ {4 P- j$ g1 w% z8 J合材料,8 r9 _2 Y! z& r {; U# J 用于飞机制造的非金属材料。如纤维玻璃,Nomex, ! |% r% U. c# E: U' `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- d; {; }3 S5 {6 l- \) z R% a, ^, H operator that is normally stored in the flight 3 K0 I( \# _5 Nmanagement computer's data base. , i+ O0 @- c6 n& |9 t0 wC+ W' ]& I8 d# H8 B" w/ { fr ! y8 B: @! t9 Y+ D! L$ ec- g' R, m, c: \. V) y* l. X2 E6 G) ~ instrument landing system (ILS). It can be used for ) B/ z# p% g: \2 z- Mnavigation as authorized in the approach procedure.5 s$ I( q4 ^. [) ^ 1. Outer Compass Loca ! }2 t7 C) p% H: F3 V2. Middle Compass Locator (LMM), A compa % O4 r2 U* n7 h) ulocator installed in conjunction with the midd9 g i1 E, [! t4 P1 B% y6 W marker of an instrument landing system.. X6 g3 ]# _4 Y2 U( T C 3 V. ]1 X, o L- @) }C ' f1 w( R; y8 Mg" [& P( k6 D! [$ } d 4 R6 X1 J* j O9 T8 s! {% Y; h! PC 7 C, q1 y: ?- B1 a+ c( y+ X. cfo ; A( H9 L8 x9 ag4 _+ ]" x4 m3 c6 ? 指令杆, 2 \5 A( ]" Q E8 U2 [6 I% P4 M# R6 T飞行指引仪俯仰或坡度的指令显示。 $ O3 n/ A! q5 J. J5 u7 J3 Q: Z& s7 S8 A 通常储存 $ l9 h9 j1 t% M: n3 p: G+ ?* f的航路。 - ` ~1 W$ v: I% c3 b6 B! m' W$ S: [+ O* W {( z' n: I. f$ M' H+ ^0 O5 E7 x经认可后在进近 9 q( Y" B& W; b4 W4 `/ T$ f @2.中台,! Y5 E/ u+ H' L- m5 J6 p 与仪表着陆进近系统的中指点标配套安装的罗4 n# q: C) W; @0 l1 R 盘定位台(NDB)。4 L( ]1 v# | ~: v! Y8 I! l4 E0 z* {) p7 k' O4 \) G2 _( }( v/ o3 |* s( Q+ @9 T3 j K- c- W, @" j% S# Q5 X b i& \ K) V! m1 }# F! L, T. g, l 英汉对照民用航空词典B OEING# k# G* G T9 `, z TECHNICAL DICTIONARY 335 E% p1 h% o5 B" @ e by ; F1 z1 m( I: ~+ X4 } ? Kor increasing air7 [6 w/ x7 y ~ z' G4 U ressure and temperature before the air enters the , G2 b% v6 P; Y* R3 J6 Nombustion chamber, Low pressure compressor - front ( D/ q7 m n0 D2 h* lection of compressor, High pressure compressor- rear ! m i0 s, d$ ROMPRESSOR STALL, An event that occurs when * O' z5 L$ }, Z4 w9 \5 x2 ^ere is a complete stoppage of air or reversal of air flow- Y$ I: H6 L7 q COMPRESSOR SURGE, SEE - COMPRESSOR 3 t: j* \# p o# P- C: E; @7 X+ JSTALL COMPUTED AIRSPEED, Indicated airspeed$ B; n0 Z4 j7 P, K+ W8 p0 K3 ^ corrected for the static source error.: Z: [" P2 ~2 L6 O6 N0 m: E 的机械轴来驱! v. u% J9 G" G# E% { ,用来增加吸进空气之压力和温度,以供燃烧室使用。 2 t0 p; e, @" R) r1 D$ x6 Q8 g压压气机—压气机的前段,高压压气机—压气机的后 + v$ s6 C) n; o; q* S! P4 K) }" i) A+ E, a气机失速, 8 x1 K2 C# o9 v; j9 P4 F当气流完全停止或通过压气机时气流方向逆反的一种 f( ~( |$ P- f 压气机喘振, % K" h6 N Q4 V8 T! c X% P见Compressor Stall: N/ q, ^/ M* n) e# d COMPRESSOR, A rotating part of an engine driven2 M0 K3 S* A" m' N" {/ ]9 G- L: h% ? a mechanical shaft from the turbines f \- v1 P7 D7 K p : C' N" D/ e8 T' f& k! T nc2 t% b) |! y. o% E s ( Z% R- u: H$ u4 ^+ w) p: tsection of compressor.& q [& ^" }0 T: e' B+ `/ {% g$ K C7 N0 C6 ]" A) X8 V1 l" ^ th7 i2 A- D0 B9 w. A9 y( A0 P through the compressor. 2 c$ A+ U, _+ W' I压气机, ) m+ z9 d6 K: E* d1 m发动机内的一个旋转部件。由与涡轮相连 - P& z2 f; t% }) ~4 f! b0 u; N" `, K) `& v1 y. @4 {1 k# S, X6 K" o' [$ X/ _& i# ~6 g. [. t+ r0 W" T1 R' ^4 A3 j2 v# d# G: Y8 M 现象。+ D4 w" N1 s4 v' R9 I6 h9 z2 Q) }4 g) P" h) O8 J计算空速, . e0 m; h6 h6 b5 K' M修正了静态源误差后的指示空速。- L1 J. M. h, f; V: \* A9 { 英汉对照民用航空词典B OEING$ B( n9 c8 P; G. z TECHNICAL DICTIONARY 34

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发表于 2008-12-24 21:39:27 |只看该作者
COMPUTER, A device that performs arithmetic 0 {2 H8 k: G9 a V% Soperations, manipulates data, and makes decisions.$ p3 h4 V+ y9 n+ U ditioning # Q: n2 C0 p6 c: y2 Cthe air and the9 ?$ t9 m- t; B frigerant or moisture vapor is changed into a liquid.$ _4 w' j) t6 I8 U5 o2 O ine4 S2 a3 O. s7 x* m! @# [ ONFIGURATION, The position of flight controls, , d% Q4 c( c2 Wmissing which2 @+ J* z+ ]6 c/ B may affect the aerodynamic performance of the 6 m& d# x4 m' ]5 R; }airplane. / e) K- T# s) i( G置。 ' c* C, N* L) ^" I. s中能使热能散发到空气中,以及使冷冻剂或湿. S9 o4 G) V9 B' w) w 转变为液体的部件。0 R+ K8 c2 {; D7 h$ F 连接到飞机结构上。+ S5 _% |+ O; x( j- a7 m 态, & C; R7 Y* ^1 r5 t定飞行阶段中,飞行操纵面,起落架等的位置。; u1 J# e# X8 G8 x% e, q- U5 ]8 g ),- N6 H2 a' P8 [* L8 { 受到影响。" A) Z8 k& }% V& } CONDENSER, The component in an air con; H9 {, ~ K& G! J6 H+ M6 u system where heat energy is given to( P1 U" Q8 `( t- ]: l. d re: q H3 i" J) R8 i" s/ ~7 D; P7 n! { CONE BOLT, A bolt in the shape of a cone for eng 5 \' s+ K4 x9 O- nattachment to the airplane structure. s3 W" `% H% ~) p! l& P. a C* E' \, j1 [) G landing gear, etc., for a particular phase of flight, e.g., 6 U5 X8 T# V7 N, T" U: UTakeoff Configuration, Landing Configuration, etc. ; A9 D% y) G# p$ z. { d" f; z5 [CONFIGURATION DEVIATION LIST (CDL), Appendix 3 P# |0 q) H, Q2 |1 E; I! o1 m4 ~in the Airplane Flight Manual (AFM) allowing operation! d' G' W) H0 d+ A$ P of the airplane with certain airframe parts' D) ]: U4 X5 u3 k 计算机,5 u$ T- U8 O4 x 能作算数运算,数据操纵,和决策的装' y) s! V0 ]2 {+ }! T9 ~ 冷凝器,& k5 N8 f# T( I; p! b 空调系统2 ~6 k7 c. R, n5 a# X+ m1 E3 V; L% F$ E* i3 M: J* J 锥形螺栓,3 z; B: {+ }* e$ q9 r% X 外形是锥形的螺栓,用以将发动机4 }; M5 w: p; ^$ w5 K, L3 J2 j4 v r/ }" W' d2 m' b在某一特7 G) B# u, t) P3 O% l 如起飞形态,着陆形态等。! D ]$ P& |$ Y0 ~- N. z% d 缺件单(CDL 8 w6 ?* J7 \0 q. ?: W飞机飞行手册的附录所开列的飞机上某些零件的清单。2 o( L2 L1 A4 [) e. c* z 在缺少这类零件时,可以飞行但气动性能可能 / Y0 U$ \7 _. Q1 j英汉对照民用航空词典B OEING4 y4 d" E( g% Q% Z 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) N; M7 k, `6 w component for changing variable engine gearbox speed 9 [, y1 {& \0 y. NONTROL AXES, The three axes of the airplane which6 I+ Y. X4 e1 e+ W) @# D re perpendicular to each other and pass through the; E5 a7 O8 r/ o1 [' q/ K enter of gravity of the airplane. / k" a# y9 @3 m' `7 Z9 o' Q' qPitch axis - Horizontal or lateral axis, passes through- c( K+ Q# B3 J3 Q1 x8 |1 t the airplane from one side to the other -. f5 q7 n: w+ v nose up and nose down control is by 0 \* q3 O6 q- H, e7 ]" [* ~elevators (and stabilizer for trim). * ]& s* G1 W BRoll axis - Longitudinal axis, passes through the) s* \/ j# N% p9 n0 @ m# L/ \( r airplane from front to rear - wing up and4 i- W5 [1 g: e wing down control is by ailerons and. z h5 \& H, W/ u7 Q2 p flight spoilers.9 S) A# k2 o4 l8 L: H Yaw axis - Vertical axis, passes through the/ `7 z* j; n/ {7 _ airplane from top to bottom - left and* z7 f! d1 E6 M1 _ right control is by rudder. * F1 J) @. v$ g" }/ G* d; X置, & s& q/ s9 v2 |. b制轴, ! g! Z) I' `! l- H通过飞机重心互相垂直的三个轴。( t$ [; R+ t2 s" \* }" x: N8 f 俯仰轴—又称水平轴或横轴。由飞机的一侧通向另 & F y n9 D5 |: \! g/ t侧。飞机绕此轴转动即造成机首的俯与仰/ s0 v! Z/ w: e8 a7 ~) b" P 俯仰控制是由升降舵来达成的,水平安定 ' D8 v: K0 P& ~9 J4 c5 a, r则为配平之用。9 b( }7 U+ L/ E3 |) g+ {& L 横滚轴—又称纵轴。由飞机的前部通向后部。机翼 * O7 w0 k. g& ?4 {下运动由副翼和飞行扰流板控制。& D, J# \; }# C# h 偏航轴—又称垂直轴。由机身上方通向下方。飞机 : O8 a9 \$ e; Q0 G1 P此轴转动即造成机首之左右运动,此一运 " M$ o/ N; ^9 Z由方向舵控制。 0 I, T1 O1 h$ p) m4 J! f: Mto constant speed to drive the electrical power.2 U- M7 o2 d; Q* W5 h C1 \4 P' F! ]8 s9 \+ g& D a" R/ ?4 e. e; k4 i1 \$ m& ^! q c . \5 J, M4 a# f: f) Q恒速驱动装( z/ l9 }- n1 f+ n$ y8 J3 z$ n 将发动机齿轮箱的可变转速转变为恒速以驱动电源的# Y; x' ^* z% c7 M) J: O' e3 _ 液压机械式部件。 # w) F5 [( w6 l% O6 ^( g% R ?# [5 Z1 X# j# l7 w* s {# C+ f( m+ O" d+ L2 `) Z4 t. o$ k, S4 T {! n, I- a0 a! P" {9 O {7 n. g6 L* ^0 d% D7 h/ o5 C9 l, A, i: x0 u8 n3 a( T9 o6 o, H; a; E+ u英汉对照民用航空词典B OEING& A+ Z' m* L# n* A2 [0 I" g TECHNICAL DICTIONARY 36* `) P0 c# l! D& s+ M. J9 C CONTROL COLUMN, A mechanical component used5 b* j) n& S3 c1 ?; U rs) d, N) ?; U0 l nd elevators. $ ^6 Y: n& O7 t4 w$ d2 hONTROL SURFACE, Moveable panels on wings and 5 q" Z/ @8 k. X5 N6 p' c* Z* vil for movement of airplane on pitch, roll and yaw axes. 0 u3 I% m( B8 a* z/ HONTROL TAB, SEE - BALANCE TAB( ?# d% u( Z$ [9 _ ONTROL AREA, A controlled airspace extending , O o! |5 e4 e* Gpwards from a specified limit above the earth.: D3 {" z1 z% f( }: l [ ONTROL ZONE, A controlled airspace extending X0 Q" `& C" }- ?. _0 d0 w: M pwards from the surface of the earth to a specified, e9 {2 e% ]" o! i3 q" i pper limit.% X6 U# ?! i- H. K8 Q! A: @ is , `9 Z' ?% W, Y9 }, m( t" q) |o IFR flights and to VFR flights in accordance' B) @) ?" U6 C, A g7 u- V1 { with the airspace classification.$ @: _+ i ~ r" O) F 机械部1 Q0 j* o. L0 O5 p4 J; d7 {2 X" u) l- e6 ~/ R3 z1 ]9 \! y操纵面, , f, }+ n9 f3 n, Y机翼和机尾上的可动面板,用以操纵飞机俯仰,坡度,8 `7 V5 Q" P6 A6 ^ 和偏航运动。 * @; ^$ b) ] k( x! G3 H2 o7 K1 L操纵片,4 ^$ u& f! L1 y0 B9 Z' o8 n 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 spoile1 X' \- h1 p" _2 h a. f1 p. a4 ~1 j/ T- w8 X* m3 q C5 d' A; s8 g, b: N$ r+ k; D5 v ta / H9 g, n' w; ^) p' gC ( }5 K; i9 c% SC- z# C" N& }1 A u - a' k9 u) A$ j; zC: k5 f# C! Y, i( Q u 6 b2 n0 R) {) ~0 `/ M5 lu v' B" h9 o+ d* J" RCONTROLLED AIRSPACE, An airspace of defined " p R# ?# l$ Q) X \) `$ x Fdimensions within which air traffic control service ) ~7 W! P, n; s; hprovided t2 \0 R$ B+ u. ]0 l- |2 `* j8 y M5 U7 q 驾驶杆,' {) o+ t+ s& y# R$ G4 z 飞行员用来操纵副翼、飞行扰流板和升降舵的3 I/ [% I9 s* B6 V x5 O# H1 x* Q7 R$ d7 _7 a, c( i/ n+ ^% u; t+ q3 j5 |. I 管制区域, 9 S3 ^/ r' n+ M高于地面的指定极限以上的受管制的空域。 3 u# u' J( u% J. O制范围,7 ^! l K9 Z0 k8 g- S' a) s 由地面到指定的高度以内的受管制的空域。& B- j+ V7 H- B5 W. D" n4 J 一个范围明确的空域。在该空域内,仪表飞行规则飞行) w& @+ v( M3 D+ S- W8 G; K 和目视飞行规则飞行有空中交通管制服务。. w7 ] r5 F a( X7 S/ z2 U/ a: Z( y/ E3 h2 F 受管制空域,( _' r9 y# @# R7 ~* G! Z# D 英汉对照民用航空词典B OEING! q5 W$ f: K( ]0 a TECHNICAL DICTIONARY 37 8 _. }4 F' g2 sCONVERSION, To change into another form. 9 T/ \6 v* ~$ i2 z0 H" iCOORDINATES, The intersection of lines of reference,0 o7 h- ^' o7 v. ~8 v: v+ f sually expressed in degrees/minutes/tenths of minutes ; \8 T" V( _5 l' J& S+ nf latitude and longitude, used to determine position or # H$ U9 t9 T& {7 bCO O9 P* h+ i: q' Y3 X4 X; A8 { destruction of th ) `! J6 I6 n" J, e$ I2 k% k2 Vchemical conta % ~! c: p! l: i7 z3 U+ C0 {$ }COWL, A remo 3 t! T# M0 g p5 J. }, t8 ^for access to th) B" m% C5 Z& p& R. ?7 q7 E Fa % }# L; O7 k. `" `& T' @7 B4 bNose Cowl - Front section of the nacelle for air inlet - y8 _& {3 n3 H' B1 d! rto the engine.3 V7 ^/ J: h1 F9 n5 F; { Side Cowl - Cover around the sides of the engine.( [5 L! b/ j9 p5 u; ] Thrust Reverser Cowl - Cover around the core 9 [9 g8 k! [* S1 l/ |section. 2 r2 o3 _3 `9 d. s% bTranslating Cowl -The moveable outer portion of the t, n' K- B0 [0 W% s+ c* Wthrust reverser cowl which is 7 g4 p2 o, p6 [/ N! Aoperated during reverse thrust.4 Q* H5 E# A3 l; ^7 y 标, ! s1 @! O: j9 L! y6 e5 E基准线的相交点。一般以经纬度的度/分/十分之一分 8 A' u4 ~* j [) C) ]( d0 q读数来确定位置和方位。 * f: R" \& }0 \5 n: M腐蚀 % }' O) y0 T! ^8 c. @! i动机外部可拆除的罩子。发动机上的构件必须要取下 - V( b5 ?0 i( [% j流罩后,才能够到。 4 M2 F6 i2 r% r- `3 j8 A! Z d) O, A+ h4 ]* Z 机的短舱的前段。% A3 r- k1 k3 K9 j: x* a4 M 侧整流罩一发动机两侧的罩子。 - p( b/ d& l3 B8 G$ E3 t2 ~2 P反推整流罩一发动机主体外的罩子。 2 ]9 x7 I9 s8 U+ b$ Z/ E1 i移动整流罩一反推整流罩外可移动的部份,在反推工 ! f8 E) s" S! a1 r/ m作时使用。" @$ w& X; k6 s2 ^. A u & ?, h6 C5 X s+ co - ?$ t5 h7 ~& a) e* ~location.5 X% s5 R1 A2 O( Q2 [ RROSION, A chemical action which causes gradual- j$ I* A$ f+ `, p4 E e surface of a metal by oxidation or 7 k8 P) S' @0 wmination." }2 I# ?8 o4 [& d& E1 Q. W vable cover around the engine sections ! f/ B. G3 Y# qe components on the engine. & X) i* Q* w( W. F1 i, un Cowl - Cover around the fan section.2 ?" s) S% a8 ~& K 转换, 7 U' M& g* N6 x1 I5 M) K" t. D$ P改换到另一个方式。& o& f1 H+ I6 W, B, K; W. {$ u5 ?: W, \: q7 B+ i0 E: C$ r' S7 W8 R2 P/ b9 O5 C: ~6 C) q/ G- C/ j6 n* S氧化或化学污染造成金属表面逐渐破坏的化学反应。 3 X8 V) j% D* ?0 ?1 z- e& t( w- W发动机整流罩, ! k; E. v ~/ k. F; S9 T2 o4 b2 }0 [/ p. S) H3 u+ [# m: _' H 扇整流罩一风扇外围的罩子。1 G( z; {- k+ M7 P/ r 前整流罩一引导空气进人发动 , z$ `+ K$ Y3 B, ]英汉对照民用航空词典B OEING$ p. @1 u8 N9 Z/ a' a/ d3 g5 H4 r TECHNICAL DICTIONARY 38 5 T; u1 S* K8 ~6 i/ e# F& cCPU, SEE - CENTRAL PROCESSING UNIT 5 E* |/ f; Q) l |- g' f% MCROSS TRACK, At 90 degrees from the desired track! g a7 d' L5 S9 y! H f the airplane. For example, cross track distance is the* N9 s! e( a* q; R! y istance from the desired track measured 90 degrees ; r% F: M8 b- w! Som the desired track." J# F5 N Y7 G ROSS-CHANNEL, Electrical wire(s) connected from7 B: G7 R2 b( z2 k5 L, r0 ] ne system to another like system, for example, FCC$ A. h; `4 \* P) Q3 c& R5 Q " to FCC "B". 5 U( D- O! { `% b: T. An adjacent engine or one on the other side.- u- |' u" a8 M l crossfeed & U3 A/ e- A9 {" l9 sanifold for fuel flow from one side of the airplane to the5 c. A! V% w m \1 v% `9 g7 P ther side. 1 r) D o. x3 B7 C* [- yre 6 L, j+ o) D" O# B n4 J% vRUISE ALTITUDE, An altitude or flight level! L6 C& w# N' X* B8 g) ~1 D9 j8 v b/ g& U! s/ O o 3 D* k6 ~, M2 b7 u% y, {! Hd ' Z% z* K% E4 P T+ O" m: E8 _8 Ufr8 R9 q* X" u( M0 s C p( y/ n% w; U" w( p5 v: G+ x% ~9 ~o/ V8 z5 c9 G/ L8 y) b "A. x/ y7 C. Q) E7 u3 m$ \0 b, ] CROSSFEED, An interconnection between fuel + V0 q. z5 x9 u* ?% wmanifolds for fuel flow from one side of the airplane to: H4 u/ a8 u j* C a- N5 ^0 G- l! K2 w CROSSFEED VALVE, A valve in the fue % _) [& J6 o5 R" t' vm $ L4 R" B: R. D2 Q3 G0 No $ {0 D7 v( N) X" T* FCRT, SEE - CATHODE RAY TUBE 3 B; z0 P3 I/ Y+ k0 hCRUISE, Phase of flight where altitude and speed a . E! m0 }) G$ ?basically constant.4 \' ?. q& |9 n; U$ c C9 h6 _) B; Z1 s: ~! k) n maintained during enroute level flight. J+ |/ w) g' S% P中央处理器 9 u3 J9 {: `* E9 g& v见Central Processing Unit.% a1 | v+ v& A) D7 u 交叉航迹(XTK), 7 S/ d1 X' X+ b' y9 r与飞机预计航迹成90°角的航迹。例如,交叉航迹距离 y* L& C. q; B2 ~) c* H" H* Q+ ]是用与预计航迹成90°角量取的到预计航迹的距离。0 u, T5 x4 T$ E$ i' ?7 E 通道跨接,+ _- Y. G, \ W. U5 ~# @9 a+ ~ 电线由一个系统接到另一个类似系统。例如:由FCC ! ]9 v, U9 U0 f7 B" B“A” 9 w9 x: d3 ]9 B+ K* ^% d接到FCC“B”.6 O7 Y" H3 A7 O6 s 机身另一侧的发动机。" v3 w. X8 H. o 于使燃油从飞机的一侧7 S5 i: a$ I/ s3 z- z 向另一侧。! X8 s' A0 n5 Q 见Cathode Ray Tube 8 V+ v- M* X$ h交输,. {% r) l. ?8 [/ ?# X! Y 燃油支管之间的交连设备。可使燃油从飞机一侧流向邻 - F6 [$ I0 ]. X% f近的发动机或在) T# U0 g- k9 t6 I; T/ r; I6 x 交输活门, # q9 W3 d5 {8 {. F, X燃油交输支管内的一个活门。用 ; ?; s* r' d& G* L0 J$ D4 m$ I! D; O" v0 s/ X4 ?7 A6 Y) G 阴极射线管,7 E2 s/ c1 c# s8 L% [1 d1 r . 4 ]2 w! X0 j4 C& ]# i7 j阶段。0 \3 C6 b. n, i7 z* J0 C7 p 航高度,/ R) h) k: ?. ~# o6 Q# S% d 飞行期间,飞机所保持的高度或飞行高; y' V: ^3 a0 V+ } 巡航, ' r: K/ a4 A: Y" x6 k飞机的高度和速度基本上没有什么变化的飞行, |# ^7 K; ?3 H3 s9 s1 u' z7 c1 |1 ]5 O; g+ h在航线上水平3 a# T$ ]* V* _6 y 度层。 ( c; }# I) s7 s& L" T) G英汉对照民用航空词典B OEING 7 T0 E6 c# r) o% r% G1 N2 l+ ^! PTECHNICAL DICTIONARY 39. d& c( E! v( W. l' l CSD, SEE - CONSTANT SPEED DRIVE# b" r2 V' ~/ T5 R1 h- p$ A4 m2 B CURE, A chemical change which takes place in a resin 6 b* f& X, b% H( o9 _and fiber based component causing it to solidify. : ~( c+ R9 U* ]: O. Y- |CYCLE, A complete series of events that take place 7 P7 t: l9 K' g+ {3 ^$ F, U8 Zgularly normally in a continual sequence.3 N8 w- L( [1 ?& V' \ AMPER, A device for slowing down or limiting6 a a7 v( N2 b& r/ U! B DASHPOT A mechanical damper for slowing down ; s) m7 n. _' Y( t3 `2 Bovement by restricting fluid flow.% |- w6 }/ k- q2 R }$ X$ c D 7 V9 R% j- ?& j, bATA BASE, Stored information which is used as the b% g* f, H2 u9 k3 F5 m0 @ba" t" ~ A( E5 L V" U2 \! L( r: m DATA BUS, A conductor over which digital data is . ; r$ s {1 }$ C. ^1 P9 Jtransmitted. ; ^4 e! |. M& C9 f9 [8 B8 _DECELERATION, To decrease in velocity.- f2 w; Y2 |0 d 装置," ~- j* V2 Q5 C rive 1 g6 u' e: K: M2 T* N, {re, k9 S5 J6 j( g: P D 5 \& x. N) J: s' R7 z, S. \D 5 ?: l" i! N' l- {" t6 P( A; w2 \movement.. M# b/ e9 z$ m" }! |, l3 m m: C' ?3 z! ^. \8 d7 ^5 E \ ATA, Another name for information. " f7 p) C& e, R- O. ND 7 M2 t9 \( I1 k5 m5 gsis for computation. ( M* G n( P/ J: } d% Y恒速驱动 6 F; W v4 [8 x( w7 J. Z见Constant Speed D .% n0 y& m( n' P+ I 期, % {1 T7 W& }# v7 r" _不断重复发生的事件的一个完整系列。; w# W3 v6 H `+ L9 M 尼器,2 _# ^0 y# J/ a2 T 慢的一种机构。1 m$ a- o5 i! b- F, p8 @/ v) z. @; H8 m" Y' H7 ~+ b8 v 用限制液体流动的方法以减慢物体运动的机械式阻 + _* r! D# F/ h( c" c L" x7 l: D- u$ Q/ A' Z. e# F) D/ m3 w; r- d* ]5 V7 B) s, b料的另一名称。5 e8 o+ [: t3 @6 s! Q- X 据库,6 X' X; U/ y3 o2 M9 I0 ~ p 数据总线, $ B8 H7 q5 U8 H) `: {, b" v2 ?一条或一对导线,用来传输数字信息的通道。 ; a9 A5 T# Z" |% W1 U. w减速,2 I6 B/ _9 t c' z 速度随时间的递减量。4 T, ]; Q6 M$ n+ v3 N) W+ l 固化, 5 K9 Z5 j6 e" k, G+ v+ y ]4 s树脂和纤维部件内化学反应使之成为固体的变化过程。 8 R$ L2 ]: t: x2 @! h/ `7 d3 c, ]+ {3 i1 x* s7 L1 b, Y& D8 c0 [( d3 h- y3 ? 用来使运动减 9 j0 Z: y# L! h6 W, \冲器, + o9 [# D' Y. n5 a( t4 m器。) y! D. Y" D# c0 M7 l4 ~ 据, " J+ r; `3 T7 ~+ w! L' b/ w. y% t l6 ^ L" k+ j9 j8 h: O4 \4 `6 I$ j2 d2 ]储存起来以便在计算时使用的资料。 + s. X8 c9 B2 Z6 y, @* m英汉对照民用航空词典B OEING9 Q4 X. L+ a( O; b" @0 | TECHNICAL DICTIONARY 40 / E; ]+ e* ~& o! r3 yDECIBEL (db), A unit of gain derived by computing the * D# Y% s; v+ I6 ptio of input power to output power. 5 D( s4 b# E; U" G( ?4 wECISION ALTITUDE/HEIGHT (DA/H), A specified/ @* Z6 E. Y" Y* H$ W ltitude or height (A/H) in the precision approach at ; e& J2 |& c) z! n! k% p* mhich a missed approach must be initiated if the ' L/ s$ m2 k' QECISION HEIGHT (DH) 1, With respect to the7 M& ~4 u' B; z- B$ \" l% ^ proach or # l$ X8 d' \. [execute a missed approach. : E0 s0 G0 Y: h5 y: lproach to trigger the decision of either7 O/ V7 N v8 Q, k nding or go-around. $ P& q! g- S4 H1 xECOMPRESSION, The loss of internal aircraft air% ^" q$ Q: \9 o3 n/ j" u; b# a ressure. 7 r* o6 V; }+ o0 m; uE-ENERGIZE, To turn off or cause to not operate.! t. w3 S3 k: R q4 A rom the tanks 1 t& r3 f% U5 t! T& F2 [# ?: Ousing airplane fuel pumps or external suction.& T0 L" w: s. V 算的一个增量单位。分贝2 N6 N0 I+ E6 \! L" y 常表示两个声音信号或电力信号在功率或强度方面的# c2 `$ t; c+ L; | 对差别的单位,相当于两个水平的比率的常用对数的十5 l* p. b, X6 G 断高度/高(DA/H), / E: p; ^$ w* h' A在继续进近必需的目视参考没有建立的情况下开始复 9 ]; @) U5 W" u. E的精密进近中的一个指定高度或高(A/H)。( [: V% ^6 d1 p3 n6 y0 \1 r. K 断高(DH)1,! s" X' T/ b' T+ ~; W' k1 q$ Z 操纵而论,指在使用仪表着陆系统或精密着陆雷 % L1 E" M" z4 C8 v( m生继续着陆还是复飞决定的高。 + h8 v4 Z+ v& y2 ~: u$ w飞机失去内部空气压力。 ( s( E7 e5 h2 y4 u! A4 I开, . U5 Y3 C/ l& h* [8 }9 a: j关断或使不工作。 $ r/ r2 \: ^8 f' _% W0 I机的油泵或外部的吸油装置将燃油从燃油箱排9 a6 z# Z1 s& ? 出的方法。! \$ R* x$ p9 G8 f ra2 h7 p& }. b" V a; x# N/ V D * A6 Y4 {. y/ C/ da! w9 L$ O& c) F; P w* j" M, X6 ^, v- Z# S0 K required visual reference to continue the approach has8 o- ~9 k( L% s5 C& [ not been established.6 g2 K" U6 p5 e8 F" l D / ^2 p* [* i" v; V* D- ]- moperation of aircraft, means the height at which a " F" _. K3 W5 d$ Ldecision must be made, during an ILS or PAR + ~: _+ J( A/ k% Hinstrument approach, to either continue the ap . h- r6 R. P# e' ]to0 a1 Z$ M( p3 |- E5 B DECISION HEIGHT (DH) 2, An altitude used during a ) R7 k" y, [9 A* E( wprecision ap ' \5 Q+ C: q3 V2 G. O3 dla0 |! k& I: e/ V D % s, ?- {0 _& Y, T+ Jp$ Z6 q) r3 i1 A- W D 2 g2 B1 Q$ F6 p* h2 b2 _DEFUEL, A method for removing fuel f 4 C0 z H0 h0 l) F分贝,! H' Q9 ]# k; X1 y1 u% |$ g 以输人与输出功率的比率来推2 u$ x) K$ A& A5 i7 J3 w R" z: f; L0 d3 G( H( N' x n1 O! j/ X* j: U; t2 ~8 J* s6 \, Y, K1 c8 O7 a6 X: T# a0 g+ [8 S1 Z" S4 a. y1 p4 q h* `2 X4 o6 ]8 K9 q0 t8 I6 C( y就飞机 % N7 d" l7 Q/ u1 J$ v9 i( E达引导进近时,必须要作出的是继续进近,还是中断进场2 l; @4 G7 X! | 复飞决定时的高。9 n5 v$ y# Q% c8 y6 ^ 决断高(DH)2, # n6 G; G1 a* ^3 p$ {精密进近时产 ; B* l# c4 e* Q& x$ A7 a. A# B* d失压, X# ]3 R" h! N5 |% f8 g* x: p, Z6 a* ]) k; W排油,3 t% ]- k1 m2 s8 ~& m9 j' S x 用飞 3 u; ^0 @0 `' q u' L/ t英汉对照民用航空词典B OEING * {# \9 e7 G# b& _3 yTECHNICAL DICTIONARY 41, t. H, w$ v$ {6 O ~! R) Q7 T0 ?- ^ I DEFUELING VALVE, A valve in the fuel system for 1 o- u* j/ E! A" Q9 F3 ^8 }efueling the tanks and for transferring fuel between the' h, G! R. a- [- F& L# B E-ICING, Removing ice after it has formed on aircraft. $ o% o0 J m6 y' T/ lChange or difference.; I# {' x, R; o+ C EPARTURE CONTROL, A function of an approach( r* l& j$ d2 o: Z: v ontrol facility providing air traffic control service for & V8 q! a* [" ]( a+ z0 A: ieparting IFR and, under certain conditions, VFR $ Z4 o% @0 q I) D; P: F @EMODULATION, The process of retrieving information. s1 j9 `8 b3 ]5 R1 t carrier voltage. + T) X* W3 Y+ e# F0 S" X8 pation.3 @) E( L I9 A& O lic 4 J* t" h+ s) y z& H5 H6 _creasing hydraulic reservoir air pressure to% u" |6 O: [7 G4 B3 C7 j* C mbient pressure.* ?4 g$ W7 i# s8 L( z) Y; l' T 箱排油和在燃油箱之间 1 d( c3 H9 I) @& i% h: B2 e8 k送燃油。 0 r4 \( ^% N( l0 Y冰,5 l- e, \1 }% g0 \- y* l 除去已凝结在飞机上的冰。 ?: }$ m* K3 @ 删去或取消。* e" Y& m c; S9 _# e' u7 u S$ K 量, * ^& \& B- Y# H& n9 q变化或差异。 4 i* P! l, }8 \) D( g( x1 |9 I场控制,; I- C3 d, O; W! F, Y( L1 M 给用仪表飞行规则离场,和在某种情况下用目视飞行 ; @+ G# M. I+ L; d则离场的飞机提供空中交通管制服务的进近管制设施3 L, B& J, @4 @. h" S, k! Z; L# j" o- c. Q$ s 调,$ ~; @ h% N- I, |# U 电压中获得调制电压的处理过程。 + l+ V) u: u, G, o) W# G环境" K8 f4 y$ z( ^! Z/ t+ @$ R 力相同的活门。 ' \3 d8 D2 s; Y7 md - |+ q( n( q( ^/ F4 T- mtanks. / t `( e3 Z; @$ [4 G; e% V; wD " e- M* n4 _. y& _* zDELETE, To remove or cancel.) T( B% u; y. [* q DELTA, - V' [ t7 }" F1 ]D$ X# {$ n* i( u7 B/ { l c) z8 F! R% t6 {. {$ B5 w. n d 5 d: z* m: c1 J! Q/ L. i& A/ gaircraft. & n3 Y* \4 m5 @2 lD5 T7 i8 x; b/ c1 l7 j2 J( \ (modulation) voltage from a modulated/ x1 I. t" k; I G DEMODULATOR, A device or circuit which performs & {- [+ d. l) |; J2 N% |; ]1 fthe process of demodul - @# ]4 G& v1 Y' X+ oDEPRESSURIZATION VALVE, A valve in the hydrau( [% D- x* @5 I4 F% [5 f system for de: }: e/ I' k: h$ F! Z. M8 C a # A# s7 ]: k2 {! L- l排油活门," p; L4 B: F7 ]3 k2 V 燃油系统中的活门。用以为燃油+ H3 ^. V( C+ l, F& r$ o' l1 p- C! b+ y( T; c, H( c# r9 J" \0 P8 a1 P; g( ~% J1 n删除, ' b3 J K; G5 L3 Q- E1 ^6 K; h% n# Z9 H, ~" i( l' G2 a0 J4 M: l7 Z$ q! }5 k- I/ k( [) f的一种功能& K, Q9 e( ?( n2 ]: L1 g8 M0 ]3 \2 V+ N6 t+ v3 h4 C从载波. }* a m! b9 R% ?1 [ 解调器,& l( g% _9 F# o 完成解调过程的装置或电路。) m% P7 |" d- J2 ~ | 减压阀,% {0 T6 E/ d( `$ L 在液压系统中,将液压油箱空气压力减至与周围0 Z- P( a+ v- c9 R' j; g$ s) M( e( D2 |英汉对照民用航空词典B OEING $ a; o+ T2 C+ {2 V* t& v! I6 z. ]TECHNICAL DICTIONARY 42 + s/ w% s6 L+ b7 m" q2 o5 gDESCENT, Phase of flight where altitude is decreasing.0 L' k1 n5 y" r ETAILED FLIGHT PLANNING, The calculation of fuel " S, N2 f0 \% R: I1 tnd required for a trip by considering each phase of- s$ G2 o4 G; v2 y- b ight (climb, cruise, descent, reserves).0 \0 X$ B! a- a& Y% d' w) B3 _ al or9 H) ~9 K5 {3 o6 K ETENT SOLENOID, An electrical solenoid used for 3 G( h7 B% G2 ]) |& [; At. 4 X9 a* d! p+ _1 `$ z# v# \specified course or ( A2 a% b3 a1 ^# T6 e& e4 [6 }rocedure.1 @$ Y9 c$ Q1 r% I. X& q e. 5 w2 P6 |/ G2 @9 m, y7 Z' S; x% G飞行计划, 5 D. Q) g) N1 I y |9 ?将航班中的每个阶段(如爬升,巡航,下降,备降)都 ! O; [4 L: F3 T6 K* b人考虑,来计算该航班所需要的燃油量。 R9 n& v. C) q* q9 s. d. X! o用来感应情况之正常与否的电气装置。 / a$ h6 ?/ m* o) b4 I# P; c定电磁线圈,& P+ q# H9 }2 o" h$ s4 G 出接通的电磁线圈。 4 w% L3 {+ G! @% R差, % s9 S; ^6 t( T( C9 d; M8 p; L与指定的航道或程序之差。 ( ]/ S$ E& X- a% P) H1 c+ f用气压或液压操作的活门机构中的柔性部件。 ( r" }; ~6 A3 |/ [& \! c0 ]) AD- t; O+ |+ S% ~) u Y8 \3 Z# b a8 V$ x1 W y( n fl! ~" R" Q* j2 W, } DETECTOR, An electrical device for sensing norm& R2 J7 M3 |4 c abnormal conditions.$ \2 h9 N+ e/ z7 a. e( I D3 Z4 s) ^4 G: ~4 p p, o controlling the engagement of the actuator outpu8 M2 D- R/ P% R: ]1 b2 ]9 e DEVIATION, To change from a8 F! y2 w, g# R3 `) q E! B/ P* |7 I p ) f% A) b+ V) Y9 z7 T5 O# cDIAPHRAGM, A flexible part for operating a valve 1 U/ V) j9 s N8 J6 pmechanism by pressur( _( |7 ^ b5 a; | 下降,4 _+ V1 {% v/ `9 C7 ~ 飞机高度不断降低的飞行阶段。 1 {9 e+ `7 H% b4 `$ ]详细; q: S1 l# W4 ]& r! ]0 O. @! O3 E5 U% B3 w- O+ ? N% ]! u$ k探测器,: ^: \# W. K# W* k" ]0 X4 ~5 F" n: W( J用于控制作动器输' u2 |6 O! L# P# R! L3 _, ?9 ?* E4 V3 { 隔膜,1 w, Z# p; K6 J3 a 英汉对照民用航空词典B OEING ; C3 p! ], |0 QTECHNICAL DICTIONARY 43 ! ?+ o( e( w7 G8 W- j. X9 _* V ADIELECTRIC, A material which does not conduct/ J' `% u0 Q" d* \! z! h) d electricity and used between the plates of a capacitor) g3 z+ G3 X. t$ y% B- g2 k (condenser). ( l0 D3 O4 s O8 Lnother pressure in the same system, measured in4 t- d. N& @, S- F ounds per square inch differential (psid).9 O" ^5 {0 Y; d- A IFFUSER, A part of an engine between the% F4 g5 L" B3 Q' F- s) m' x6 c ompressor and combustion chamber for reducing the8 s a& ~( j1 j+ o( ] air pressure. 5 d# O" A, j+ R K0 e {igh , o) E% X. ~, ~! }pulses.& g& j( c$ B5 E& Z! T9 J) U, T. J ignal that is a close approximation of the original 7 ?6 W& n# |8 A+ P6 [1 Aignal.8 V0 H! e5 v) |2 V IHEDRAL, The angle between the wing reference / T# T% j/ J- I3 Y+ rlane and water line. 8 }# Z8 m1 f2 `5 w/ @* H5 D的压力,以每平方英寸 X; W: {5 K* D6 f 少磅压差计算(psid)。 d* e4 J* P& J" O" K2 P 散器, 0 L! m4 S8 L* w( Q8 ]8 a发动机内压气机和燃烧室间的一个部件,用来降低空 / V$ y% @5 l5 z5 x增高空气压力。 0 q1 f8 H; ?" o4 E1 O; @% `( c/ P6 W换,7 m; N/ |$ T' q! |4 A 的连续可 4 }1 q; t. z/ Y7 q0 ](模拟)信号的处理过程。: w; B& w& p6 o; I 反角, + G6 ]4 ~$ [. l( l+ l机翼基准面与水线之间的夹角。 S% V: Z: D( T& a3 b; ~0 f# }* VDIFFERENTIAL PRESSURE, Pressure relative to0 h- V3 m+ v7 T5 [7 t. u7 @ a $ U* j: q" ^ P1 ~p: x% u% ?* T! X2 z1 \: I D / U2 _9 B* N" x" x8 [( m, Gc. h! ~) `; r3 E* T1 G3 ^ airflow speed and increasing the 4 R: B' X+ s& N! [" SDIGITAL, Digital refers to a signal whose amplitude2 W8 ~0 k$ j) H- ~. \ Z remains constant for a finite period of time. Digital$ q) z. z$ N0 V* \9 R- y signals are commonly represented as a series of h 7 Y# P# p! i* t3 z& zand low % E8 ^2 T5 ^% eDIGITAL-TO-ANALOG, The process of converting a ! w8 A8 c- {- p5 Mdigital signal (binary) to a continuously variable (analog) 6 A( O2 V7 |! z! T: U& c. |s) d0 |# _! J7 M s" w) X: e4 B0 g1 O D9 F* w" E' g* t& A! W p $ K% k( J$ j8 T, A电介质, 8 S( q( M! n3 f一种用于电容器板之间的不导电的材料。. {5 P9 T6 X6 E4 ?. d& e% z 压差, - c0 j# U. x! Z& W1 L相对于同一系统内另一个压力 2 ^, V e8 S! B6 Q r. L U# `; Y) G3 ?/ H* s; v4 X. a" N$ W8 f) [; c+ q: i+ T 气流速并2 V0 o- L- Z$ J$ l" y; x 数字式,) l: g# H$ C6 H6 s- X; g 指一种信号。该信号在一定的时间内,振幅保持不变。) g# L7 @1 s" L" T5 P, S) P3 ~ 通常由一系列的高低脉冲表示。 / f6 A& u0 Z8 [1 a6 x数一模转 / v; y7 X1 N( M3 W9 q- G将数字信号(二进制)转换成与原信号相似 % _9 [3 I2 o9 G3 x: ^/ j4 _6 O( o) p# t4 X0 r2 v8 a C" o7 X; Z7 B6 @. U' A英汉对照民用航空词典B OEING% R1 i4 m0 ^. r( p TECHNICAL DICTIONARY 44' H. W3 D+ w0 w DILUTER DEMAND REGULATOR, A component in the' @( Q7 X' y5 W* |: k crew oxygen system which mixes air and oxygen and . z2 n; C% Y9 O4 m) u! c2 ^3 @upplies constant oxygen pressure even if there are ; ^2 @) }# g9 G% ]hanges in ambient cockpit pressure. 0 B& t* y7 P [% X$ ZIM, A word value of light. For light control devices - dim ) }0 T% }/ d. n6 W5 m1 Vthe opposite of bright. & k3 e- p2 z: @: Q# w. pIODE, A device which allows electronic current to flow( m3 m# c% g, Y& Y9 R6 U only one direction 1 x7 z$ S! v7 R5 x/ \uid in a reservoir. 1 D# N/ s1 w9 ? y4 x. `DIRECT, Straight line flight between two navigational ( ?$ d/ L& \0 l" C7 x9 yaids, fixes, points or any combination thereof. When * j1 v N G" j" U! ~used by pilots in describing off-airway routes, points , S5 E4 O: O) i" F! N4 Ddefining direct route segments become compulsory 5 w+ `8 o; Q* }1 w0 v1 Y. M0 Areporting points unless the aircraft is under radar & g3 X0 p8 O% |* E `3 P) y- e# vcontrol. - @) ^4 u; c; ?( W3 I* v: y节器,: U6 ?3 T/ e h 将空气和氧气混合, 5 [0 C6 {8 K; b* w! {9 d使驾驶舱环境压力改变,它也能提供恒定的氧气压力。 , H5 O) `9 O8 r5 b3 s$ Q" E q6 W4 L; Y" A( H- X3 z一个形容光线亮度的词。对于灯光控制装置,暗的反1 N' B8 U& f! h 词是亮。. E" m: @- g! L2 o 极管,# S9 p0 p: R3 x' Y' O 只允许电流向一个方向流动的电子装置。 . j( t4 z9 b0 }6 o器内液体的量。4 |& E1 H9 }0 b* V# C 直飞, 1 g# J" r) q& X1 X两个导航台,定位点,导航点,或任何的组合之间的直. O" q1 \& a# d2 R- I% g5 q0 \ 线飞行。在被飞行员用于描述偏置航路时,除了在雷达控1 Z% e# K& a( e3 J* [ 制的情况下,确定直线航段的导航点成为必报点。( ]8 @0 j3 d4 J8 h# X s2 e9 C/ \6 z& s6 Y: g c + [1 a$ w$ H) f! i' W. vD * h7 r2 I: z" y: w0 Wis 3 X7 P# Y1 h6 ^; l# |5 FD" H9 [6 N- R: c! i in% \* A; ]/ I* f/ o! f" j: h" z DIPSTICK, A calibrated rod or stick for measuring a2 R* T" D6 o2 P* d4 Q g quantity of fl, ^! P9 f* ?. a- G, x 稀释氧调 1 P" a5 @, J1 p; |驾驶舱氧气系统中的一个部件,它 ; Q! p( B, H: u- u* V; w* c3 ]0 b( \1 O% J4 }# E! U+ g' o5 k- Y* M: l" ^. y" D [ b! ?0 ] o- {7 V' E! a, P3 v' C8 Q Q B; D, t: z$ _* C5 H量尺,; t, i* e$ n$ j; m$ p4 L- M 校准过的棒或尺,用于测定蓄液9 q5 b3 }# C. M3 }( a6 ` 英汉对照民用航空词典B OEING 9 A5 M4 E3 N# V2 i9 @/ C: F0 r5 T$ vTECHNICAL DICTIONARY 45

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