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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 3 H0 g# s8 } C2 x! G" b) y [" `民用航空词典 - z' k+ j$ J7 t2 U波音商用飞机集团& Y7 r3 g* O* Z6 q BOEING COMMERCIAL AIRPLANE GROUP - ]& W: v' F( K/ {英汉对照民用航空词典B OEING * O$ ]) V$ \4 ?% mTECHNICAL DICTIONARY 1 J+ T Y7 b" ?' {; D E+ H A 9 c7 c% d0 v. `# MABEAM (ABM), Beside: An aircraft is abeam a station : x' A1 N& k' Cwhen that station is 90° to the right or left of the track of3 L' k7 Y1 I) e3 L: \ ` the aircraft./ `- \7 ]; t$ A; { ABSOLUTE ALTITUDE, The actual distance the aircraft( r, {. u1 W. }3 a' Z is above the ground. 6 i% D3 S. g; \* H! Y5 qABSOLUTE PRESSURE, Pressure of a liquid or gas5 U {& c1 m4 ^3 n. H: y measured relative to a vacuum.; `4 v4 h: v! G- _ ACARS, SEE - AIRCRAFT (OR ARINC) REPORTING' _! v2 w. {/ y0 x5 u. m9 A ADDRESSING AND COMMUNICATION SYSTEM! U7 W$ n' s1 g2 o ACCELERATION, The rate of change in velocity with + m; h* `6 B' g% rrespect to time. % s+ u4 `; l- y8 SACCESSORY GEARBOX, A part of the engine,$ V- w x* H! ?2 N mechanically driven by a compressor or an angle- ?; l' i( O. K) E0 Q# G gearbox, for driving components necessary for engine! w6 E3 l( i( _ 正切,6 d5 e J, j' R: u and airplane operations. # G3 x5 f" E" E8 e- O9 c. |0 W* ?当电台在飞机左侧或右侧方与航迹成90 度时,飞机正2 R% s$ ]1 J8 @/ w+ E. F3 M$ J 切电台。4 i2 |- P# X: u7 l! m, L3 s 绝对高度,1 T& W. \7 l: O" i 飞机离地面的实际距离。# y( M% D5 P' W% e2 V, S1 I* \ 绝对压力, $ S3 L8 \: r5 J: _相对于真空(无压力)测得的液体或气体的压力。 , S1 ?) L0 ^, A% K1 G飞机通信寻址和报告系统, # \& u. \+ a% ~; c7 }0 S8 p见Aircraft(or ARINC)Reporting Addressing and% c5 I5 Y8 M+ C Communication System.6 w9 w" f- ^4 q( @: ^ 加速度, : u8 P# S" m: R8 ~随时间变化的速度改变率。 7 \0 E" r1 Q5 j/ T$ d& R附件齿轮箱, - k! n: _: [' w- _/ p$ P* z( }发动机的一部份,由压气机或伞齿轮箱带动,用来驱动 $ d2 n3 p) I* H& K一些使发动机和飞机工作的部件4 j; N4 W& t" ^; m4 h7 v4 f9 A 英汉对照民用航空词典B OEING & `5 P1 t$ p4 b9 VTECHNICAL DICTIONARY 2% a D/ X5 I- A0 R; G ACCUMULATOR (NO. 1), A container with hydraulic ) z, A8 i) C) i* |0 rts when normal hydraulic supply is not) f9 v! f' V! s vailable. + B: E$ \# Q' Q/ _0 bCCUMULATOR (NO. 2), In a computer, a special $ J5 o8 k0 ^0 Y) R) Y# Atorage register associated with the arithmetic logic unit, ' f3 L. w; l: Z$ u+ ]4 v% O& u0 ?olding the results of a computation or data 9 {) [9 ]+ v) K0 E4 c: l& G+ k$ tACTUATOR, A mechanical device operated electrically,- p' h/ [# A* j' r! @ hydraulically, pneumatically or mechanically for 6 t S) b6 L6 o2 _$ s" Etransmitting motion between components. : j& k4 i" g7 nADC, SEE - AIR DATA COMPUTER! `: k1 U5 O6 h/ U- `; i ADF, SEE - AUTOMATIC DIRECTION FINDER8 g7 r) q3 ?) U% t! m. o$ ~ ADI, Attitude Direction Indicator, An electronic display of. n* A0 w2 i0 L2 }" H( d airplane attitude information in pitch and roll.9 i( U- |( D: z0 E; `$ T 蓄压器(NO.1),1 b+ G* T; Q; D- ^$ k* Y 含有靠干燥空气或氮气增压的液压油的容器。当没有正 4 D6 l5 k* ]7 d常的液压源可用时,该容器可用以驱动部件。 + W& y% E, ?3 I# |! k# h存储器(NO.2),/ E8 U6 w$ |% M* K9 O 计算机中,一种与算术逻辑组件有关系的特别存储寄存* P# i# P/ N7 }. u 器,用来存放运算结果或数据传输。: r9 Z* k) Y. t' {9 d, A 飞机状态监控系统,7 H; ^, t% t$ V: a; j% ^ 见Aircraft Condition Monitoring System # ?, G6 M/ ~5 Dfluid pressurized by dry air or nitrogen for operation of4 t1 L( a/ m1 e0 f componen3 c7 d. d) Y0 O. `% e6 X a7 I7 n) y" o6 M' h- ` A6 g/ T/ T6 f) ~& b4 e% `) f, s s. ]3 l: W' p, {; Z6 u, d used for h : V l7 [& v- ^0 ztransfer.2 r: {7 M% }9 G T' m ACMS, SEE - AIRCRAFT CONDITION MONITORING : @% V6 H1 Z" QSYSTEM .$ t6 f9 a' w% M- z) m 作动筒, ; e3 w2 L5 [* D& I6 {由电,液压,气源或机械驱动的机械装置,用于传送部 ! O6 F% z! _' P* H/ V! v件之间的运动。' W& ?8 C# L- G& @5 Z. [) r! ^ 大气数据计算机, 2 E, e9 m) S4 I$ E. D3 R# ~. L见Air Data Computer. : @5 E% l$ S$ l: F4 e4 o( h自动定向仪, # M, |! ~8 b; M! Y- w& c8 a% {3 q7 S见Automatic Direction Finder. U4 H4 U( X7 v0 l; d9 w姿态指引仪, 3 K( y! z- H6 Y# ^, P用来显示飞机的俯仰姿态和坡度的电子显示。. Q+ F2 s, u0 ]7 M5 ~ n 英汉对照民用航空词典B OEING. N: ]+ A4 m6 E" t! N1 O% d9 } TECHNICAL DICTIONARY 3: G7 n; D; A1 i* Q/ N2 P AERONAUTICAL RADIO INCORPORATED, ARINC is * }" o. J3 Q. b R( O, 5 r# q; Z' Q& `' U+ w' S, ?4 ]nufacturers, and foreign flag airlines. ARINC / a K) {0 p" U- G* Revelops and publishes standards for electronic # n/ o% \7 O2 w4 F. N) `quipment and systems.6 u( h) J( z9 U2 t GILITY TUNING, The capability of the DME to+ \! M _. U# M! h" s9 N% D9 T lternately tune between two different DME stations in' `) j# o. u0 q' c* ]0 t% ] rder to get two distance readings from one% P' E& E2 R% p% L, i3 S: U terrogator. ! {9 K5 f0 I d4 Y4 {, G3 L& H. Sge- O/ _+ L9 @- T) @% ~+ e ILERON FORCE LIMITER, An electro-mechanical : ^; M' M6 l' b4 nIR CLEANER, A component in the pneumatic system( D `$ L. b" ^7 O7 U, P$ _% x upply to the air& U) {: {9 ]& }: R/ j4 z6 v7 j. M onditioning system.+ n( L; I' V; ~0 r 订并出版 ' K6 V: g& B8 i' {( c9 N) o子设备和系统的规范。# D: h9 k6 F& `& j1 Z 快速调谐, 6 B& G: i& R+ M" W' F6 ?机载DME通过交替调谐两部地面DME电台以测得来自( N* y7 m9 }9 t" p 同一台询问机的两个距离数据的能力。* F" y$ W# P/ b! N2 Y 翼操纵力限制器, 5 [0 M4 J4 g- j+ _装置。在自动驾驶工作期间,用来限制驾驶盘1 l& I q$ b% k" {0 {( M; m0 ? 气清洁器, $ z5 Z. F- E/ d部件。用于去除供空调系统使用的发 " L% V a( v5 _0 o& A* J2 @a corporation whose principal stockholders are United" W0 w$ {2 g$ M, f; Z. P/ j; N States scheduled airlines, air transport companies" K9 _2 \9 A5 B' H) p" ?2 C aircraft ma5 q' {, \6 C. J/ d d * G1 ^' y- D2 {: we . a+ ~3 }: K d; M, R) FA $ ~& x6 P* d! T, }: Ha 8 O6 A& R/ g) g- c0 C4 L" io7 x3 q; @9 a; Q& L/ K in- w6 g$ h5 M0 L' l9 V. M: E AILERON, A hinged moveable part on the trailing ed" O# ^! J; C) m, O1 E% P8 l, W0 e9 G of each wing for airplane roll (wing up and wing down) : P' n7 w4 b# |) i2 \5 P5 Wcontrol. # W+ F6 S) R5 @0 u; ` ~1 HA - d2 K( q l" R5 }1 |4 E* Odevice for limiting the control wheel movement by the( Z7 [" K, m6 q$ `) ? autopilot during autopilot operation.6 f9 F8 c, |/ `7 Z, `& z4 [ A ; R# e1 E# m$ ~6 s rfor removing dirt from the engine air s; x. E8 z* {, I" C c 0 d1 K8 x( u2 ]航空无线电公司,* U, E4 q+ ~0 y' u$ C 主要股东为美国定期的航空公司、航空运输公司、飞机$ W+ r) x+ n5 l 制造厂和外国领队航空公司的组织。其目的是制" v4 i% G; j) v R9 u' m* f8 T5 E副翼, - m5 K7 ~5 o( M" P) I. i铰连在每个机翼后缘的可动部件,用于控制飞机的滚转8 P8 {- }6 o0 F (机翼向上和向下)。( Y; ^, [* X$ l' r1 f! E, W" k M4 S; p; r; d 一种机电 }3 g: x7 G, w" A! G的动作量。 - [/ F9 _% \% I7 h; F0 E6 L8 T n Y2 u3 ]& q 气源系统里的一个 # Q% o* e6 D8 J/ {动机引气中的灰尘。 0 Y F, F4 [% S& o$ Q英汉对照民用航空词典B OEING- ]+ k; `0 _: Y TECHNICAL DICTIONARY 4 . \' [$ p+ M0 i/ W. ^% wAIRPORT ELEVATION/FIELD ELEVATION, The 0 J. c& ?! K5 A9 @. whighest point of an airport's usable runways measured 1 g1 |, ?! q* k% p2 `0 iin feet from mean sea level. In a few countries, the 4 ~6 D/ V* w8 f! |! K0 {airport elevation is determined at the airport reference I; @4 w( d3 Z5 U3 A8 o9 A7 k+ j point. 8 `8 P$ I9 |: R$ @AIR ROUTE TRAFFIC CONTROL CENTER (ARTCC),7 k1 u7 `/ _. \$ L& k, v( V5 r1 M3 |1 y0 v ervice . r# B4 z7 x( R! b2 P6 x, Xase of 8 k' W3 x X' o; @us flow of air traffic.! x: l8 ~/ m: ^ IR CYCLE MACHINE, A compressor and turbine on a ! x q% E5 q* \ Q* g. }ommon shaft for cooling the air in an air conditioning! k# K. k! l7 l- E4 G7 q2 E$ ^) H ystem. The air is cooled by expansion from high to low7 r2 f) O9 x5 C4 D! b, @3 S1 i& x5 O ressure across the turbine. The compressor is driven 6 W Z" a9 _1 fy the turbine. - t' P1 X. x, u+ L4 D2 W中航路交通管制中心(ARTCC), ! E2 c+ X: l( Z/ y- N4 E9 e# l域范围内使用仪表飞行规则飞行的飞机提' }& c$ Y! q$ |1 l7 _' X' G 管制(ATC), 0 ?* Z( B' B' P" X) @" L- y涡轮冷却器, & a6 K/ W/ q) E; \/ L# a是装在同一的压气机和涡轮,用于冷却空调系 * a& \$ z- W5 S; R I$ w4 K8 R统中的空气。气经压气机压缩后,由热交换器移去热量,- ?8 I% N7 j4 k2 p 然后经过涡轮令涡轮带动压气机。通过涡轮之空气,温 3 |% b2 h2 q1 \7 P( l0 A9 d度下降。 " @8 [! A D1 S% D% }+ g9 FA facility established to provide air traffic control s) [. R/ s3 D' T9 H7 Z- k to aircraft operating on IFR flight plans within controlled 8 W; j8 \& ]) @+ p6 M" h5 s, sairspace and principally during the enroute ph* E7 [9 J$ q W6 Y* L/ l2 A: p flight. 7 P* i' E+ H. _0 LAIR TRAFFIC CONTROL (ATC), A service operated by! V8 o P- U8 y p5 O( A appropriate authority to promote the safe, orderly and G* A' k& U; _5 Jexpeditio: }9 m( r3 ^. m# v5 B4 H1 L A 4 f0 m+ J* z! p- f( m' f- Yc 8 N8 e) p- A' x! U5 Ws 4 L& F7 E# X2 i3 N% h1 Bp 1 z& Z! W9 v6 cb E9 `* F( x$ L9 L机场标高,) Y4 L5 z. m! h9 m0 u P 指海平面与机场可用跑道最高点之间的距离,单位是英 0 |; U! j5 h" z d6 ?5 [+ t3 I尺。有几个国家的机场标高是由机场基准点而决定的。 3 D4 e6 b: W6 I/ l$ H q, p$ m9 B f& ?3 W: H! u 给在控制空$ o. S0 v9 o# n: j 供空中交通管制服务的站台。6 B2 Y- _0 _- a, u- c( O4 \ 空中交通 - O; B% l" I& I% A9 j' f由有关当局管理,旨在促进安全,秩序,和效率的空中 j9 P: V: `! f+ t 交通服务。 5 }+ V* y- Q+ v& ]! e根转轴上 : D2 _7 C, _* F' {( p9 c6 ~. P+ {! a! i' f& d. B8 S4 h3 e5 e# a 英汉对照民用航空词典B OEING 1 Q0 ^% ? f1 `$ M# i0 ?3 _TECHNICAL DICTIONARY 5

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发表于 2008-12-24 21:36:52 |只看该作者
AIR DATA COMPUTER, A computer which produc: O; ?$ T# } p0 K2 V data information, such as altitude and airspeed, based' J* J1 N7 y+ j9 K2 ^* Z on pressure and temperature measurements. 6 j( O5 ]+ B8 I" ?' g6 {es air " M0 [. Z* ]- C+ [. E& j( S/ J) ^IR TRAFFIC CONTROL, A system comprised of + v' u: Y. B0 rround and airborne components used to identify, track 7 ?3 I/ r9 h: Q: ^, E6 cOUND SENSOR, An electrical device operated7 }4 n& w7 \" U: \% F* k y the landing gear, which transmits on ground/in air! b) i# \1 c- y6 _+ H formation for system operation in flight or on the. p: o+ i7 ^( i, |4 s8 Q& } round.# Z, o) g$ ~# d' [0 ?/ h4 W IRBORNE VIBRATION MONITOR, The AVM takes 4 n# f. G3 o! f, v7 ^" P, n: Ce signal from the engine mounted accelerometer and ! y( k% f; u& f6 B6 H6 v) k( `alculates the vibration on that engine.4 _9 u. m7 S7 _1 W5 K8 L7 | corridor equipped with radio navigation; o6 G& a v: p% @: A aids. . q C) ?# h, xAIRCRAFT (or ARINC) COMMUNICATIONS$ \1 I( p0 J' Z1 [2 C/ A3 E ADDRESSING AND REPORTING SYSTEM, An ; k5 s9 H3 G1 X# Q1 A N; Paddressable digital data link system which permits the( f. l8 l4 j& E2 j- l exchange of data and messages between an aircraft 2 _* c2 E$ z! m$ o& [5 q0 wand a ground-based operations center over a radio' V) y$ y3 ~/ {' s3 U network.* ]: B6 n: |3 v AIRCRAFT CONDITION MONITORING SYSTEM, A% H l$ h& w6 ?" [ system of sensors and recorders to monitor various( O2 e. T% {1 u- s$ _, f airplane systems' performance and status.: u4 e2 X# i) a" h# U9 r) }7 Z 机, r% _4 U8 p0 k 中交通管制, " _9 ^( r J/ y. ]3 n1 |" r2 n一个由地面设备和机载设备组成的系统。用来对飞机进 ) H) ]0 d( L- t4 `地传感器,6 l6 b; f+ k8 A" f, ]: ^5 E- _, K 一个由起落架操作的电气装置。用于给空中或地面的飞( a. l- `9 t5 B7 ~/ v) ~" |7 h: U1 O9 y% g 系统运作传输地面/空中信息。(有些系统只能在地面 k q5 K# R8 s# j7 l; a7 l O用)+ s, S/ A, U0 s8 h' J1 s 载振动监测器(AVM), " m$ E. u8 r$ ~AVM从装在发动机上的加速器取得信号后计算出该发# O6 p% v1 ]% {# o 机上的振动。) K8 H9 f! \/ A 式建立的控制区域,内有无线电导航设备。/ A( S2 }1 y/ o7 c9 r: l4 X 飞机通讯寻址和报告系统,, _3 b9 U' v7 u V6 y 有种可寻址的数据通讯系统。利用该系统可使飞机与地 ( S2 F9 l: U, i. B2 L面操作中心通过无线电网络进行数据和信息的交换。! I8 ]8 l. Q0 L0 F0 I2 k 飞机状态监控系统,0 K2 q/ b( Q! ]- k 一个利用传感器和记录仪对各种飞机系统的性能以及! f2 [" }9 O/ B# y 状态进行监控的系统。' E, _! l' _5 i& E' {5 n( T! o! h/ E& ~ A# c9 @9 ?) E8 Y6 x g % X( Y) A0 J, n, r, m- K0 oand locate aircraft.6 o& p: S8 P% f, b( h' }, J AIR/GR4 R3 g+ v1 J* e# F6 t; H b' k1 M& i# ^% E! `) L; p in9 P& i' _! r( w g # y0 j0 n" A t* B# C: ?+ S5 PA 2 U$ }0 o% h T0 J: `" pth 7 `$ M( c: ] P* ~/ b- T+ Hc& m' T, L6 q* ]7 A1 Q4 C8 p AIR WAY, A control area or portion thereof established / x1 ~0 x4 W# h T, ^) \9 Rin the form of a1 F+ k) ` A4 @$ a3 ?* ~# p 大气数据计算 ; ~; x0 Z; P( m1 n8 F根据量取压力和温度而产生大气数据资料(高度、空速" \; r: T7 l6 D2 W 等)的计算机。 9 e# J3 K8 T: }6 m# f" a5 d5 q+ K G j行识别,跟踪和定位。 / l( L+ C8 i; I! D2 D5 @* n/ X, v$ d5 Y7 ?; w" t" x( h* X& @3 n+ o' Z使& S, X' D6 W1 i; ]/ T6 @/ I6 M) Z( z0 L& m; e! K: L3 m% O8 i; S e: }' `+ m 航线,0 v8 O2 c- m* U% H8 r. ? 以走廊形 6 [1 q H5 a) i英汉对照民用航空词典B OEING" n% ~9 H9 j* L2 a* ^+ O. Z TECHNICAL DICTIONARY 6 5 E- q! c3 e9 r2 x9 z/ x& aAIRFOIL, A surface designed to obtain a useful reaction," |! F+ }5 d% d6 A' Z such as lift, from the air through which it moves. Wings,( m+ [# y3 I: m0 e& g) ? stabilizers and control surfaces are airfoils. 1 d* f0 ~$ T8 |AIRSPEED (IDS, TDS), The speed of the airplane: r) o4 Z( j2 i [- p" P$ N. K rough the air.9 X1 V6 q9 | q. O' A$ O; ? D INDEX, An adjustable pointer on the : E, U+ B8 b( `& @& uirspeed indicator. 7 S3 I& z2 ~& x: k1 vand legal ability2 [% s4 S" j H. \% x3 t% ?" P fly.1 [* }% _" u! N; i m, for example, the procedure for finding the # q& J& q7 k6 W1 p& fquare root of a number.; e, N# X# M( Y4 s: u) _6 A y - S; `! w/ p# \4 y! ]0 Hre, wind, 3 v6 n" T( A- [9 ^+ @8 J& a+ dand aircraft flap setting. 8 a% R# S$ o7 v; a& k7 h9 |是翼面。+ e! i3 f7 ?! d) v+ r0 }' L 速,3 W! m h8 g7 g& ` 飞机在空气中运动的速度。 . U. N4 T& h2 R( v, `/ f3 c2 Y+ z/ C' F k- t$ B4 t 在空速表上可以调整的指针。1 M$ M% m4 @ e B) m1 Y4 G4 N; y! W 机械飞行能力、和合法性的飞机状态。' a" y7 x u8 D 一步一步的解题方法。例如,计算一个数的平方根的步 ' r+ K2 f8 M, ?& u0 X1 i# O+ H- G& r; Q8 I) U7 Z! k& q9 v资料的法定文件。$ g+ w8 c0 z2 {3 } U% s. M! | 翼位置成函数关系。 + y3 k/ Z1 p( `# Vth 5 T4 L3 Y \3 _0 QAIRSPEE4 F: {' i( v6 S. w: ~! e* X2 U a 3 ?5 ?. E2 m% ?5 N) t# g8 I' tAIRWORTHINESS, The condition of the aircraft with# t: o/ Z& R& S( N! z' X respect to its aerodynamic, mechanical, & k% R3 V& H# K/ vto8 k$ [# @, t0 b; ^6 y ALGORITHM, A step-by-step procedure for solving a , h' s8 d8 \3 jproble * D) A, Q+ A: i% d3 y) I1 ms \3 C" L8 q# j8 o2 _ AIRPLANE FLIGHT MANUAL (AFM), The legal 7 c# M7 k; G. fdocument containing performance and operating limits,( U# \" b% |( x" Z2 s( b" ] operating procedures, and takeoff and landing3 z+ X4 d# F1 j4 C performance.+ G. L! x0 v( S AIRPORT ANALYSIS, A comprehensive set of takeoff 2 [$ |5 z; r' F8 _: M0 u; S1 f, `% eweight limitations for a given airport runway, generall 0 T, \: Z) L: G$ M! a/ R; P: Ipresented as a function of airport temperatu ( \' F$ t3 @! ]% l0 t翼面,; J3 K+ D. Y( N; T$ r" j 用以从气流中获得反作用力(如升力)的表面。机翼, % J4 K2 H8 a; |8 L1 ^# B+ }# ?$ M安定面和操纵面都) S$ o5 z& p6 h# p3 ~/ V2 w: E% M+ s( ?6 o& H 空速指标5 J- K8 w6 R: v; A& } l 适航性, 9 W; l3 q/ G; c& u: P: ^5 }, J" C有关气动能力、0 T+ I5 ^2 c( v; T* v 演算法,, i) @6 Y6 ~( E+ a" \( I, M' `$ O" `, B& B& t 飞机飞行手册(AFM),: k+ C; W8 l/ A$ O, s2 @$ H 包合性能极限,操作极限,操作程序,起飞和着陆性 : s) W8 e, W9 Z) s$ t- @: y- k/ | p' w! N 机场分析," P1 T7 p, x; @3 [; M& r 一套针对给定的机场跑道的详细重量限制资料。通常与 ; |. L# v! E* C# K' ^( Y, ~& {4 Z机场温度、风、和飞机襟 ; {9 R" a- H6 w! x8 A4 D# y5 Y英汉对照民用航空词典B OEING/ a$ K |/ _" Y+ h* O TECHNICAL DICTIONARY 7 6 W. ^7 i9 V7 \$ ~% g6 `+ ?AIRSPEED BUGS, Adjustable pointers on the airspeed9 I; |! N' x/ S9 l indicator.$ N4 Z0 e3 d" |2 [ ALLOY, A mixture of a basic metal and small amounts: w7 V. M4 ?- k f other metals to change the properties of the basic9 R* j2 Z; ~) c etal. A2 M8 a3 D1 H3 s, h' g1 m Minimum airplane speed. 9 `; m: r3 C! r0 H: {e of 5 T& }# }' R! ^8 b& r) witting airplane angle relative to ' a+ u4 I! {. U# Z: Iirstream for the stall warning system.! Z4 t, d2 `) { another. # c& T! x W) ]4 R' _, B) uLTERNATE , An additional airport selected during 5 \8 G# {" F9 | i9 [$ S0 N8 g9 f F( x. L. a! Q6 P 合金,% x* h8 F" X/ p. ^3 C 在金属中加人少量其他金属,而改变其性质的一种金属 ' n/ i: u+ b' g合物。 5 E) i% K- E0 ^) g飞机的最小速度。) w9 s [ \: s% G5 @ 速警告系统传输飞机对 ( b. |0 d( P' ?7 f; v# B! {1 r流的相对角度。 0 a" ?. e# s. Q8 |$ c6 z由一个状况改换到另一个。 # M3 f* G" u) \( r降场, 7 f. N& I9 K3 N" G$ E+ |划时,除了目标机场之外,所选的另一个机; z4 K8 Z z' [7 p& h8 R4 S: q o ) ^8 ]) _4 \! g, F* }# R& O3 Jm: l" n& d( x5 n ALPHA SPEED,) N: E3 n8 Y1 ^4 J- u ALPHA VANE, A small moveable airfoil on the sid 6 Z) V3 N2 b( v1 b: g) @0 Cthe fuselage transm ' b$ J4 H" r/ i; u" xa- @' i' i' G1 d& G ALTERNATE, To change from one condition to 4 _( L( {% w) }/ @. s Q% OA ' T. D7 H1 Q; {+ T/ bflight planning, usually near the destination airport, to be0 p, O" w6 \9 l used when it is desirable to divert from the original 7 V9 u9 H! _8 V. \9 |destination airport. + K( i- [- _, @; ?空速游标2 ~+ u' R$ s* ~* g4 ^ [3 e! M1 ` 空速表上的可调指标。) l) o+ c6 B6 l# }; U! D" F8 \/ x' A: u迎角速度,. F$ a3 W1 {% n- X: `! Q/ P 迎角叶片, / j$ E. P& z" q1 m9 ^3 j6 d! M位于机身侧的可动小翼面。为失! _* G. [2 s% @8 ?& m ^) g/ `6 b. [( z3 Q$ q' U7 k交替,9 g' e; B$ A* y7 Y. H9 G' n7 V- \4 \/ L, j 制订飞行计 ) B5 z( a9 ]5 e' S, j$ x. P场。通常在目标机场附近,以备不去目标机场时,改降之, G3 O5 @2 c/ ~4 y+ F) ]# z( e 用。 * U6 J9 c7 x! w3 I! w6 E英汉对照民用航空词典B OEING- S1 d; C4 ~! K% r. O, W TECHNICAL DICTIONARY 81 p O: C# m$ f2 R, L ALTERNATE AERODROME, An aerodrome to which5 m* J/ I ^0 {+ U an aircraft may proceed when it becomes either ' C3 s) g! A( N5 ^possible or inadvisable to proceed to or land at the/ c0 |; ?5 y* M n% [ erodrome of intended landing. ! x) o8 W _: T! \TER SETTING, The adjustment of the altimeter 1 X) Z4 Q; B9 V) Q& U' @5 A6 Caccount for local variations in atmospheric pressure. 7 G6 n. [5 `3 k" j' X" ^* }3 hLTITUDE ACQUIRE, A digital flight control system " x8 e- I6 m2 ]" xode to transition from climb (or descend) to level flight.9 Q3 u2 o' `- g2 W, c% r LTITUDE ALERT, A flight deck alert occuring when the, v* O+ O! H9 \. j+ A irplane approaches or departs a selected altitude. ) ~" ~3 Z# e* X. j8 Z1 RLTITUDE CAPABILITY, The maximum altitude at d# j8 C: |$ n$ q$ r8 i hich the airplane can be flown at for a given thrust,# C! A3 a7 s7 b peed and atmosphere condition.+ ^* h9 k F+ _) x7 l LTITUDE HOLD (ALT HOLD), A mode of the autopilot- |- i% T9 u0 h, T% ~ r flight director to maintain a selected altitude. 7 B) i* Z1 Y" eirplane's altitude during VNAV operation.) r4 T- w) o; V' u8 P5 g 机场着陆时,可作着陆使用的 % @& u a) w g! o, j场。8 o0 F+ a9 w- X( L; b ]) E2 n1 x& s0 `& d7 W$ X根据当地大气压力变化而对高度表所做的调整。 0 l0 L4 F8 R0 N1 K D5 L一种数字式飞行操纵系统,从爬升(或下降)改平的模3 |7 E& \6 P3 J7 @( ?9 H" b: A) ^$ g! U& P4 V' E 度警告,6 A g0 p, A: i! ~* N) h k 当飞机接近或偏离选定高度时,所出现的驾驶舱警告。 ' d. D+ h0 {0 U' C高度能力,1 o( D- x0 m1 T8 i; }0 E8 { 在给定的推力,速度和大气状况下,飞机能飞达的最大 ( {& p+ A* G: i% a高度。 5 M6 Y0 R1 J. C: H( Y& y! H9 s) |高度保持(ALT HOLD),) Y; S# q. z; y% J# e- V) z 自动驾驶仪或飞行指引仪保持在选定高度的一种方式。& e1 _7 `# w$ j% \8 d+ z6 e A$ ^$ ?7 O! H+ T8 D0 m/ X+ h4 ? 员对飞行高度的控制。 7 s( H& S! @/ c- n5 h, i/ ~. _( kim0 f1 ~$ j8 C/ V( O) w* j! v a2 c. g0 ^1 Z9 p6 o ALTIME & d" Z, T5 d5 v! u4 Gto! L5 v- P- [# P* c b6 _ A; M! N2 X7 g0 O; d" q m& j, I3 U6 K" F6 g% m, a A9 K9 ?) ^% Q9 O2 J a6 h! n& V' E# Q2 k" g6 g5 q A% m- q+ O2 c8 i7 W, A, |3 e w / q8 g9 c% n7 S' u0 V* Ts $ z7 e8 Q }4 m- ~A. _6 g# Y5 \1 Y4 y0 d0 [0 h( P o - L$ r. t% r# D( \ALTITUDE INTERVENTION, Pilot control of the 9 A) J6 b. n0 z' ^% E& u: S- ^* da + E9 K$ A$ q eAMBIENT, The surrounding atmosphere. + O& j, Z# T5 X7 z$ e备用机场, . E; e1 ^1 L# \. q" O当不可能或不适宜在预选) v0 a& |. n4 }6 a# z# F$ c2 g$ k4 A1 i高度表设定 ' {) p; q# t5 P高度截获, 0 d/ U* D5 o3 q2 l/ ~# p5 z2 R7 c# H! C- f8 g5 Z2 M3 J0 I: h/ a! d& D 高度干预 ' {3 ?8 I8 ^ G) Q在垂直导航工作过程中,飞行 ' g8 j/ G4 u8 n7 d周围环境(地面气层), 8 f" _: i' l, p- D" ^物体周围的环境(特别指大气)。+ Q. ^2 M. d& H9 S& l 英汉对照民用航空词典B OEING 8 W0 M3 {6 e' {( u' C( z' XTECHNICAL DICTIONARY 98 ?, K) [; s. q* i) I3 [ AMBIENT PRESSURE, Pressure of air surrounding an ) P5 ?, p& a& E8 tobject, measured in pounds per square inch (psi) . $ [! b) R3 a; e* R9 a0 OMBIENT TEMPERATURE, Temperature of air 6 V# c" L- f- t, z: lmpere. 3 N w1 p' A; t. Yurrent waveform.3 c4 r4 _# h9 E, K9 h( s0 Q2 \4 K: [ g an/ i0 ?" \, d, A nalog signal to a digital signal. 9 Q5 J/ g8 S) tore inputs3 g6 u; H: d/ Q! _- u- R# Y( n8 g) l% j+ o f binary digital information and one output. The output 4 K& q* O8 |1 i0 n* n1 only when all of the inputs are 1. The output is 03 `* x' c" P5 k, V+ q+ \, `! n hen any one or more inputs are 0. P9 Z3 _$ ?7 R/ Y0 n7 p; L! M面气压),; a$ u# `. b5 W& i. s' A5 [& | 境温度,% H7 n! @: R+ |" y \ 气温度,用摄氏度(°C)或华氏(°F)来2 Y9 N/ D8 @; b K' A5 }4 F3 `- m' J8 [电压或电流波形的幅度。/ t& g( D% {7 @: d/ \ 性变化的信号来工作,或产生连续性变化的信号) y0 e2 h9 F: e+ D* a- R& |7 D5 f# r 统。# M) b0 @/ R3 T) z+ W1 f! } 将模拟式信号,转换成数值式。 " C) n: E4 @' h" J9 |& C) d一种有两个或两个以上的二进位数字信息输人,一个输 5 `4 i6 |4 Y" f" q' A, g的装置或电路。当所有输人为1,输出为1。当任何一个& {! L/ K2 q) y( ]. e 一个以上的输人为0时,输出为0。1 E* ]& M5 Q1 U( M1 L A- f& i8 K8 [: ^7 v _9 a+ G surrounding an object, measured in degrees Celsius7 f' W1 _8 x Q (°C)or degrees Fahrenheit (°F).' K' ]: C- E& T AMPERE, A unit of electrical current. One volt across ! I( Y) X0 Y' d+ E% Z) m" Fone ohm of resistance causes current flow of one + y; V& ~* U8 Z0 M; `! @4 q( Qa! [ J4 r6 [ O# I% n AMPLITUDE, The size or magnitude of a voltage or1 f: L4 |$ e0 _# r c 8 D6 w5 d/ V) ], A# ]& l" |1 QANALOG, Quantities or representations that are! c, b" v- M+ d: C% h/ M variable over a continuous range." d7 j4 w( N7 ~4 X) B* N- @/ J/ D6 | ANALOG-TO-DIGITAL, The process of convertin ! P( R8 Q8 b) Pa / e7 A A7 u2 \( {$ N' ?AND GATE, A device or circuit with two or m% h& M Q' i$ z: u o 7 _8 k- T2 p' |. q9 P0 a7 q% pis ! `3 C, g3 j. X- r4 P- g: S; Qw# A6 P2 N B$ a* a9 R- Z9 a 环境压力(地 6 f3 R- L) \% W1 G1 J5 Y' Z2 g* E物体周围的空气压力,用每平方英寸多少磅(psi)来 0 B6 e& t6 @5 m! P; f* D度量。: j% T. R# o) V5 K: z4 _: ] R1 c( \) W* @0 P物体周围的空- ~4 X7 ~# ^' R* E* j2 Y 度量。 # d, m* {9 b4 b! b安培, 3 S# D; u3 Z7 d电流的单位。6 l6 k3 t" @% K. T* `) _4 a 1伏电压在1欧姆的电阻上所产生的电流为 * |* D; M2 R8 B. t" b$ Y% B, G4 E! w1安培 + a r1 e% A' B振幅,3 B% f: W, v2 R! ?1 }' Q 模拟式, 9 F+ ~' M8 |- [7 u用连续 2 R, x& S# b! R8 G4 m; j; v0 ~: r' q; J# D从模拟式到数字式,* f$ k e- j3 Z' T+ B4 j- m' s* } 与门, ! ~, R2 S0 P1 T# b: [0 G2 }+ A5 ^6 M/ R! E; x% ^! K4 z6 w9 A5 |1 L/ \0 _2 S. z: _ 英汉对照民用航空词典B OEING, j& f1 `' H z* l TECHNICAL DICTIONARY 10 ' ?- L& ^; c' _, \0 R% tANEROID, A sealed flexible device containing air at low. I2 r4 S7 }, I, v( O N0 U pressure, which expands or contracts during change of( t2 o; m9 C% y$ l2 O ressure outside the device. 0 u4 Z5 M# |( {* c" ]ically: b$ e5 B; P1 N0 G* R b r changing the direction/ a1 N+ K/ X5 n/ H f drive.7 O0 }& r7 j: Q$ r. ? of the wing chord in; C- a5 \. M$ M% i0 p9 G lation to the free stream airflow as it moves forward0 }& @, d* W+ C$ a rough the air.# I$ h/ z0 d! w3 b3 | al axis of the # Y. l/ n1 g% C* x' zaircraft.0 N. F# _2 T9 o( i, F 胀或收缩。 7 a1 u" o& h( S& x( m4 b. P5 k箱。是改变驱动方向的机械装置。* ^8 e# V d, w 机翼翼弦在空气中向前运动时与自由气流之间的夹角。% u1 ?5 o2 @ A; t8 [! I3 L5 M7 v6 Z% g$ N# k# T- r5 H' {p5 `: Y) x1 V% j3 O ANGLE GEARBOX, A part of an engine, mechan + f# P6 b, H8 Z8 t+ `5 jdriven by the compressor, which drives the accessory: G# z# Q! D |% k- r% r4 X gearbox. A mechanical device fo8 o0 ?5 ^1 `6 w+ X- R8 W o2 ?$ n* S9 z4 k" t b0 v6 Q ANGLE OF ATTACK, The angle7 R# W( h1 n+ g" t re * |' O. h: d2 ^: {/ Lth7 b6 m2 t' j5 V5 e- `/ e, z | ANGLE OF INCIDENCE, The acute angle which the ^* R x" }) u7 T7 v% B wing chord makes with the longitudin2 f5 Z4 w0 L/ Q4 {) \. R: U 膜盒, 4 [- {: ^) p9 F内含低压空气的密封弹性装置。当它周围的压力变化: R! L6 R6 w. \8 n- s. D, D 时,会膨 : L( {+ E0 m2 P. k, d( b伞齿轮箱, ; f0 |, K# P0 T发动机的一部分。被压气机以机械方式驱动,然后驱动 2 j; d+ |- \+ m附件齿轮 ( l, W! x3 x0 @ a迎角," t1 M: Y1 X5 d0 x K 安装角, ( A' j2 z7 x* y1 ?飞机的纵轴与机翼弦线所形成的锐角2 q, n- d$ s2 j: C T8 ]! }0 ~% I 英汉对照民用航空词典B OEING : u5 a4 x& ?! L0 lTECHNICAL DICTIONARY 119 E* x. O4 d# x6 Q6 K# Z! P M ANNUNCIATIONS, Audio or visual indications used to# f- [' b1 H5 S) \% L, G# S6 r call attention to an event that has taken place.) p# _' |3 G- P1 U8 ?3 j ANNUNCIATOR, A visual device consisting of a number 5 r) u: ^' l% r. Hly.5 n' |4 x3 e+ G8 ~8 f& X& y ANODE, The element toward which the principal stream & I n& y- q5 M% Qof electrons flows. / _$ g5 Y. b( u7 f6 N7 g6 |2 WANOMALY, Not normal.4 c U8 f5 H2 a* Z# P ANTENNA, A device which, used in conjunction with a1 K* e# y6 i/ |) m4 `2 A transmitter or receiver, is used for radiating or receiving9 b0 l8 `3 ?: t! Z radio waves. ) D1 m( m! k4 X$ z# a/ {NTI-ICING, A method of preventing ice formation on 0 t1 ?/ q( k+ {) l9 r! be wing leading edges and engine nacelles.0 z2 r$ C! @/ B5 ~# R& m9 d NTI-SKID, A system for providing maximum braking3 u. ]$ _9 f4 E; P! C' {- _ ithout skidding for any runway condition. Anti-skid. l0 B7 T, }1 @. a3 R! a3 C6 l" @ omponents are part of the brake system.7 \' a3 Z+ {0 F- x 告,. Y* d+ G- F8 U7 e 当发生事件时,以声音或目视指示形成的提示信号。0 o; T, x$ P4 |, Z# ? 与之有关的电路的现有情况或已存在的 7 c" y2 v" D r5 w2 s3 b2 ]( y1 r6 @, e* o" |0 u) W9 ~ 正极, ' m$ O8 d t: Q+ {2 R' N2 ^5 S主电子流向的极位。4 A% B0 U2 }* y+ i* _9 A 异常,1 s; R8 \, P8 P9 Z# K 不正常。 / k( {6 I A$ {$ e天线, . M4 b8 f. P' c# n: f9 P( |$ x0 J5 V一种与发射机或接收机共同工作来发射或接收无线电 / R8 s2 s3 M3 `6 F1 z( Y5 ]2 v2 u波的装置。 ; V7 m6 s. B2 |* g4 I n7 w; i k冰,: t. ]5 J* N$ F. H7 Y 防滑系统,! `7 J8 |: a% M& Y$ c* U7 O 一种在任何跑道状况下,都能提供最大的刹车能力而不( o! `2 y2 G- O% z, c 使轮胎打滑的系统。防滑部件是刹车系统的一部分。' p$ v3 e; F- J of lights. Each light indicates the condition which exists 1 c! f' Y# z4 m$ I7 uor has existed in an associated circuit and is labeled5 i( a' }- V7 I5 s according + S) |% @- Z* E. A7 BA . ]3 G* e# O6 z+ i- S; _th2 R- e9 w! O& n/ \- K" ~ A 7 |. a" Z$ U& gw * i/ m9 E7 u0 Q0 \1 v; _1 Hc' Q8 |9 a% c0 { P% o! A" g9 f& [' N4 ~ 信号牌,1 F3 A1 ^0 y# U' \! p# T 由一系列指示灯组成的目视装置。每个指示灯都有相应 4 a4 M# @2 ~! ]+ J' N* u, O7 f2 A; L% j9 J的标记,用来显示. i- O* f! u. s2 \5 l! h" U$ M: z7 e* F9 s' O0 X, Q+ E4 [4 L9 a+ h; R 防止机翼前沿和发动机短舱结冰的一种方法。6 n3 U: }4 A" x7 J: O 英汉对照民用航空词典B OEING- i" m) [ G" s TECHNICAL DICTIONARY 12$ f7 O" t3 Z" X$ s8 Q+ O APPENDIX, A supplement to the Airplane Flight Manual ! m' c; P6 g# P5 _tained in the basic manual. A2 R: [) X3 j3 ?; M, E1 W, @ ollection of supplementary material at the end of a " t; n F* \6 f; r% J. h5 Y7 Nook., C7 ? P8 K/ ?# m of the * N/ q0 Z5 l& x1 A% f) ersion link on the landing gear. 4 J; P( Z! O: J" |3 mAPPROACH MODE, An autopilot/flight director mode # }1 f, [; K7 S4 y/ @, ^which is a combination of localizer for roll control and % A. z5 q/ x, x. B3 L6 hglide slope for pitch control. This mode is used when full' W f2 @- I. Q& S instrument landing system is available.2 @5 ~* P$ I- T" G9 l( a7 t0 c: [ APU, SEE - AUXILIARY POWER UNIT: j- M9 b( t1 T7 E ARINC, SEE - AERONAUTICAL RADIO 6 P- N- T) K& b- w" XINCORPORATED; C! `4 { u# _! A ARM, To make ready for operation.! G/ u$ J/ W0 }: { 附录,% k6 F5 O! g. j( C* u4 ?* h# h 飞机飞行手册的附件,包含基本手册中未提到的飞机形 * [& k4 n" c, ^" h. o7 l; Q; Q- a态的其他性能。是附在手册末的补充材料。3 J9 N9 d, H0 [; I 顶销, 5 r; O5 I# @7 x' N/ y/ ~6 y; Z, j用于连接起落架扭力臂两部份的销子。' X( D1 E# N& B% S; K 进近方式,0 U" T- `! D3 S% n2 B 一种综合了控制横侧的航道信号和控制俯仰下滑信号 9 ^! M; Z/ K4 s的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系 4 Q9 `3 u# {0 D/ r统正常时才使用。' a) x( o5 z0 i+ ~ M 辅助动力装置, 4 |5 n) M4 Q$ H8 P+ s8 M见Auxiliary Power Unit 3 T$ h/ f& U, @" c6 @6 n% d9 [containing additional performance for aircraft% t. @# z7 C* j6 Q configurations not con 2 W: Q: H' ?0 U9 H f% ac( z, G# p) k2 J3 q4 n b6 t! i+ N, Z" y4 ~' q: d APEX PIN, A pin for joining the two sections * F* j! T5 K* o. d/ xto, F6 |& t! x. O6 u8 F( i( S0 c' g, j9 Z$ h, w" Y9 R! H( n* ^航空无线电公司,8 S& j+ D: I8 r( ?5 j 见Aeronautical Radio Incorporated.: I* z' j" A" H 预位,3 T% s$ c. C/ j; [' a 部件可以开始工作的状态。; {! L; M* c; p1 o 英汉对照民用航空词典B OEING# u8 w3 [4 i9 P% x& Q- c' S' Q# y TECHNICAL DICTIONARY 13 1 A, Q# @& ?, lARC, The curved track over the ground of an aircraft 4 A8 y7 Q5 J0 s' Cflying at a constant distance from a measuring - Z& ]" c$ @$ p9 P$ j. t4 m" \equipment (DME). 0 m. [. k5 ^, A1 a+ K6 x' z6 ~in the limits of self-contained system Q% q% S* j* O# f$ _apability. & B* Y. K% G9 W9 j: Gtem for opposing or restricting' d, a) k U6 e2 d/ w ovement.. {* Y) f' B* P4 Y SPIRATED TAT PROBE, A sensor that measures total1 t! q1 ^* l# A3 j4 S' V# ^ ir temperature when the airplane is in the air and that 8 j; u) s5 Y2 b1 ~easures outside air temperature when the airplane is 4 D% M& T3 u* C) K! M0 Qn the ground. The outside air temperature is measured* v5 I# {. d% a \: T SSEMBLY, The fitting together of a complete structure , R4 }6 Q/ x0 F0 X- D+ ?1 \, c$ {SSUMED TEMPERATURE REDUCED THRUST, The& Z& H$ L! X; Y1 t6 E; p0 s9 I ATC, SEE - AIR TRAFFIC CONTROL! ~# ^* i9 R% f, D( }6 `0 |' M5 i; ]系统中所产生的一种用以抗拒- P2 U1 s8 M" U4 B3 @; b9 \ 作或限制动作的力。 0 b& S+ l5 C. a$ C- K头, $ K: M$ I1 a: D" r% ?" `: ^用来测量飞机在空中时的总大气温度和在地面时的外 0 ^" z$ V0 _: z3 u! u" K温度。地面外界温度的测量是利用引气将外界空气吸入 " p R5 w& B: X& v头,以达到测量的目的。 0 ^' m# ?$ v8 F7 C/ L配, 5 V: T- o+ p( a* T6 O( G一个完整的结构或组件的过程。2 a# s/ J" i) E$ @8 X% o 假设温度而得的减推力, 1 D0 G6 P; r9 j7 S' A推力设定值时,假定一个比实际外界空气温( {6 Z' {( g' B" m# a- ~ 空中交通管制, : `. T/ n. p4 o见Air Traffic Control& E: ?2 G# c3 K% W, C1 V0 ^# x AREA NAVIGATION/RNAV, A method of navigation9 L' a S6 m) R that permits aircraft operations on any desired course% W, g" _1 v1 T% L! [( m+ J$ G within the coverage of station-referenced navigation r$ v1 c4 F5 M: s( x* ~# xsignals or with! ~, [, a0 r2 s! s/ f c $ e; p5 I( t; m9 X" ~/ oARTIFICIAL FEEL, A force developed in the flight . N/ H: T5 q9 Q) {3 `7 Rcontrol or brake sys - h8 N% t8 B+ Om . w* R6 z# \1 O% DA$ }/ M1 M2 p% Z7 {" p% ^2 [! g& e" J a 6 J6 H. f, R1 e- d+ }) j& dm) T S! Z" f" c' S. ~# N a# o o j5 O) z) t/ e" n; a0 I( ?: L by using bleed air to draw ambient air through the" c4 A+ i3 {3 y( D sensor when the airplane is not moving.1 C! @+ V) B1 k5 Z/ T A( n$ F# P+ a. P5 e& e or unit. $ d' W" M' l' P9 E; h1 S' q1 g, ]A 5 Y9 ^4 N2 {5 H" r" }lower thrust obtained by setting a higher than actual3 R* W {1 r! x |0 u! d Outside Air Temperature (OAT)./ v* }$ l* H; X; O# C 弧线, 7 l" P5 _' L% G- m- x1 G飞机在围绕DME台等距飞行时的弧形航迹。; o( L( R; l1 z$ W1 i 区域导航, 1 G2 N: n% D" y容许飞机飞行在有电台参考的导航信号或自备系统能: M3 U4 L+ [6 ~. B) _ q 力极限范围内,飞行任何预定航线的一种导航方法。6 l. r8 _. x: ]) o3 V- @ 模拟感觉! X) k! j: y4 Z; q7 C+ {. l 在飞行操纵系统或刹车 : V s f* Z. } K9 x& O8 h% r R: F) l7 y 吸气式总温探4 E# d# G% x8 v' o9 X+ c& ~2 C' A, i4 E' n( i) O, }$ c4 E' E3 y# F d% H: y T2 M1 Z; l组合成2 `* [0 O* F( y: I/ O$ C2 ~3 G" F+ K1 e1 g, ?' L4 h- v) f在选择起飞3 d: Y8 \8 `# Y q9 E, Q5 N5 K' K" @ 度高的温度而得到的推力。用这种方法可以减少发动机的1 h8 G1 v: K( G4 o j# j8 H 磨损和维护费用。1 y2 Y+ O) h, v$ n1 Q1 E( x1 `- G5 d1 }6 J英汉对照民用航空词典B OEING6 y v( [( Y! t, t3 j6 J- l TECHNICAL DICTIONARY 147 g! {2 I3 R; I+ N; h ATE, SEE - AUTOMATIC TEST EQUIPMENT* O* C3 V$ k2 K& l* ]$ M5 F0 R ATMOSPHERIC PRESSURE, Pressure of air due to the 1 a) E7 \. U1 C* a7 Xarth's atmosphere, expressed in pounds per square8 C J0 q% B% `$ N: B c ch (psi) or inches of mercury (in Hg) or millibars (mB).3 }2 x6 h+ ]8 S5 P% J, B TTITUDE, The relative orientation of the airplane with " S& o# v+ T& s7 |% z* l8 l Rspect to pitch, roll, and yaw.2 ~) Y- t- m; }; j UDIO CONTROUSELECTOR PANEL, The panel in 4 o. @3 u2 i, u5 B9 A! ne airplane which controls and selects the routing of 6 R) P* u, ?2 m5 T5 uudio. $ w# C! ?8 @; D8 r1 |" N- ~3 mUTOLAND, Automatic landing using the Digital Flight S4 e4 j& L9 Y. v X" H ontrol System., h6 X G" E8 E% v! `0 F n.& W8 q+ V0 w3 r1 {4 a M, A system 3 i( `( [- N1 O. qomposed of all necessary subsystems needed to guide 0 ?2 g5 }6 h$ T# B+ @2 P1 s1 t! w4 He flight of an airplane., i3 x1 d+ ^) g EQUIPMENT, System test+ P6 H+ p! l% B& j. @ quipment that operates under computer control.+ u# ^3 e+ P, M6 T7 k1 O( T 装置,

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e9 Z+ g5 X% m% z5 F. C in7 Z. W, i3 H( @2 u% ] A ( Y0 _7 G ?* @ K% E/ T5 S3 ~re 9 I# T9 a, ]6 ?. [A + O i4 w* j! q% Zth" m; T# L) T4 H a F) b- k# d2 x$ H" q# {( { A3 t; r, Z. l% v7 }2 B C ( o a) h+ I$ ]0 ]9 Q- q- TAUTOMATIC DIRECTION FINDER, A system which 9 c% q* w& W9 ]) V, f( u/ |determines the direction of a radio statio8 I+ M. M: g+ S) I0 E8 T( `. I9 V AUTOMATIC FLIGHT CONTROL SYSTE ? e1 [6 F% [. Q% K c 3 T# x/ @2 U* pth D2 M( C9 f2 s* Y% T+ qAUTOMATIC TEST ; Y4 N3 p, U( s3 ~0 V* X# F. He! |4 ]( w4 ?+ B* L 自动测试 3 \% P$ a" P5 Q/ N3 @7 u$ M. }见Automatic Test Equipment.! _- @8 J3 W! [- p" p2 r 大气压力, 4 Q, F1 }" X5 b2 w; M由于地球周围的大气而产生的空气压力,以每平方寸多( a" `1 f: u/ `9 d/ `0 d, ^% E 磅(psi)或多少寸高水银柱(in Hg)或毫巴(mB)来/ n& i* Z: c U1 _) r6 ^0 z, r 示。 $ l; z W3 k4 e0 o6 S飞机姿态, 6 \, M$ s" h9 f" q6 @8 B飞机与俯仰,坡度,和偏航有关的相对方向。9 t# l% w, o2 G# M( L' v) e8 g 音频选择面板,7 K; T* _& U1 J7 I' T 飞机内用来控制和选择音频通路的面板。 % m, ?: a3 o' Y' R) q自动着陆,( v! |* g, S- Q* v. l* Z4 U 使用数字式飞行操作系统来进行自动着陆。 % z7 L. H$ ^9 L$ _! i的系统。% O; e o# I, ~& s; J# V {5 _6 `$ ~5 N! ]7 w系统所组成的一个系统。 $ t9 f9 j7 f4 G7 G& F- ?在计算机控制下运作的系统测试装置。 3 ~$ Y2 [8 G8 [2 W" _# [# e! P1 |/ T9 c9 h, b; | v# @+ c. i9 ]" e 自动定向仪(ADF), ) `) H$ e$ r* }( K/ \+ m确定无线电台方向 # r) F1 s9 o2 F6 o5 S自动飞行控制系统 $ b. u R$ O2 r7 l, I: L由所有能引导飞机飞行的子( X4 Y, F2 J- k" R& j 自动测试装置, : Z9 _+ _7 r$ g5 T+ q) ]英汉对照民用航空词典B OEING% {- g9 g, t, L TECHNICAL DICTIONARY 159 q7 F/ @/ g6 J7 G AUTOPILOT, A system which automatically controls - |; w; a9 J0 `% U. Wand guides the flight of an airplane. F, Y9 ?/ ~* L+ ]2 V& y6 mAUTOPILOT FLIGHT DIRECTOR SYSTEM, An ( b+ J# a/ q# G ^5 ]; W" i6 ator. @& B+ Z4 z% k) l1 l# u8 H5 y UTOTHROTTLE, A system which automatically( k& Z5 T( O" m9 _3 `' Y ontrols the throttles of an airplane. / _3 `" A1 E# ^2 f* Y$ ePOWER UNIT, A small turbine engine in R3 U" [: X8 d3 m e airplane for supplying electrical and pneumatic 4 N j" A% W) Power for systems operation on the ground or in flight. & }2 q& ^, J! z6 U9 V/ R* V8 C( Z* \VM, SEE - AIRBORNE VIBRATION MONITOR, K: k8 e* Y! |1 Q$ u8 ] XIAL FLOW COMPRESSOR, A type of compressor6 }( {. q# ~7 ^5 P" X- s sed in a gas turbine engine in which air passes through * M$ l. E- J1 a0 d" O6 mXIS, An imaginary straight line or an actual physical' g( d5 a9 H) m6 m omponent (such as an axle) around which a body can 2 Y* ~% ~3 x" B7 Ltate.! G' U6 }, I) ]+ T0 D3 E, N3 [% d 仪,5 L! Q t8 C3 h, |9 d" B3 V2 H& N& ]8 K" g 自动驾驶飞行指引系统,* t) E; w, K, M) L% k 动驾驶和飞行指引功能的系统。 0 \# W) k( L0 t s/ t. y动油门,1 P( Q! \8 e7 k; o* h 自动控制飞机油门的系统。 ( ^, }0 b* m4 f是飞机内的小涡轮发动机,在地面或空中给各系统提供 + }6 ~' G6 i7 z- J& z源和气源。$ n3 J' ~; s1 z! b5 d( d- r5 s& i: F 称。, R% t: e& f4 `3 q 载振动监视器, * H/ f* g! X7 }* _见Airborne Vibration Monitor \7 D& j; k D! dintegrated system containing autopilot and flight direc 3 o. J& H" J: g- z8 a! jfunctions. F: f G7 y P6 E A / D; ]* B! }5 B. [# \! mc 8 f$ T8 i* m6 C7 F* c% G* rAUXILIARY( T, S9 j, M. `# G: g9 P4 K* M+ Z th' j1 q, Z7 K" S: @ p ' A% x& ]" G7 v( ~" E& {4 |AVIONICS, An acronym designating the field of aviation / N* u% V8 |- X) felectronics.5 s- n& j5 U: M A + _. {# h# N- J/ s9 A4 jA) g; \5 u6 x; [" D1 j u " t5 `6 d; J; u3 T9 {the compressor in a straight flow, front to rear. + N" [* e1 j7 y3 i9 b: NA , c$ C# Y/ O% |5 kc5 {, M' F- f3 f( E5 g ro& }) A! c( I) s, E/ ~/ w& G0 a 自动驾驶 0 D9 a* }: Y+ d9 ^" X- d( K) f8 d动操纵和引导飞机飞行的系统。 2 u) X$ n/ h6 @* |( F% E. `一个综合自 + I4 z, b% D9 W" R0 V. l$ a+ h; E) _ 辅助动力装置, ' ~3 o! E! H4 H% _8 B" ?0 _0 B; \% N+ \ @) p* S3 T2 I航空电子学,% d8 {/ `: e% {" X9 X' A9 _ 是航空电子领域的一特有名9 {6 |: T5 ]. O1 F/ {" D: v1 J6 R( W, K( c2 W7 f1 m G/ q; T/ Y- q1 x2 i 流压缩机, ( i% M4 N4 ?! F, [) O" j一种用于燃气涡轮发动机内的压气机。空气由发动机的% O4 k: a- n5 m5 c' J 部流出。) k7 P P: S3 L. q& O8 d+ ~( r 线, $ ~0 ?$ F, }5 M/ N可让物体围绕着作旋转运动的一个想像的直线或实际 7 x: \8 F% h" h8 ^9 L1 N6 z' U+ B在的部件(如轴)。 6 b, f% X" t* F" P; {2 {- s9 o* D/ `/ U7 k前部轴向流人,压缩后,由后 w$ }6 R, o7 u" t9 i N8 O! x6 v1 R2 {9 f- i* X5 j' f* F t: k' d' V 英汉对照民用航空词典B OEING ) G0 ?% f! v2 m* ]7 V6 ITECHNICAL DICTIONARY 16 0 _" \0 q2 L; F. CB6 m% w, x/ p8 y5 W. z O* _9 |0 I ACKCOURSE APPROACH, An approach to a runway* o8 z+ B0 k3 j: H" m. Q K- u& \6 F versed." {/ q$ \6 U' { own on the EFIS that ! v6 h8 v6 d; R0 Ioes not readily change, for example, navigational aids. + m8 e3 @+ S; F0 S yvement in the tank or reservoir. / {5 U. I K$ X$ l! DALANCE TAB, A small hinged moveable part on the0 n3 `" @( c, Z0 B. w, F6 s ailing edge of a control surface (aileron, elevator,: @! w8 @# _# ^$ y, x8 A! n 航道进近, % o* W5 Z) f, K1 |) s相反的进近方向。当反航道进近时,无下滑 % u0 \% z- w" n显示在电子飞行仪表系统上不经常改变的数据。例如:5 g. s0 i3 j! B; a N/ Z 航设备。" Y7 l) M0 Q& S+ e2 w2 q7 _" Y% b% g 在燃油箱或滑油箱内阻止液体流动的隔板。 & Y: b, `+ |" e6 J7 I" s( R- {动补偿片,; B1 \) P3 \, m2 b+ U$ l+ V 铰接在操纵面后缘(副翼,方向舵,升降舵)的可动部。, o7 c8 g/ z) w0 f8 X4 C U) ?" h9 X 与操纵面相反,以帮助操纵面运" H2 P% b O. X h B5 s1 d: M' y+ j. A, s which is opposite the normal approach. For a& b# a/ m: A- X, O; {( G backcourse approach, glide slope signals are not. V: f4 F- o3 u8 _: v2 j available and the sense of localizer signals must be& q; k0 j8 v5 M7 h7 F% |# ~ re) w; M# |; e# `. T BACKGROUND DATA, Data sh $ c# M8 g8 b) J' m5 vd+ B& b! ~7 {; \5 U- L9 ] BAFFLE, A partition in a tank or reservoir to prevent 5 c. y! ]( ~; F# `& O+ bfluid mo0 { _0 q; s+ N% b8 r B2 M) e) ~. ~$ A h7 C- [3 K& Z$ @ tr + ^' G7 l( ?5 _! h# _- p! Zrudder).The tab moves in an opposite direction to the : O: W% q3 i/ V% d8 a! _; z) t8 dcontrol surface for assisting movement of the control! T/ v; R5 D7 Q( Q( Q/ ~ surface.1 q6 }# R1 ]) D* a/ q0 p2 J2 r" w4 L5 c/ |2 P0 w" T1 Z' d与正常进近 . C" ], \0 c8 p+ W! J道信号并且航道信号也必须逆反。9 d& O$ X+ W0 X' @/ H 背景数据,/ d! S3 ?0 I0 o8 \ Q, m6 d: H9 E+ w- i2 |# D1 K6 D7 h缓冲隔板,& ?5 ^2 B9 x8 f6 A& p& O% U3 [+ u' G: l8 B: t% @随动补偿片的动作方向 3 o, ]8 U H0 l2 c6 S. D* M0 c; [动,减小操纵力。. j+ I9 A) M4 M+ w* q, N 英汉对照民用航空词典B OEING 2 ?# K5 c) [/ g1 \( F. yTECHNICAL DICTIONARY 17, L5 R0 u: Q. Q# o/ S" B BALANCED FIELD LENGTH, The field length 9 P' H1 A- d" D" ~" |) s0 D' Qassociated with optimum aircraft performance when9 g! C. f. Y" B: [$ E: R3 u bstacles are not a constraint. In this case, after engine+ s ~1 D% U' o. _8 G ilure at V1, the distance required to accelerate, takeoff 5 ^- K/ \; ^ B$ Pnd reach a height of 35 feet is equal to the distance ! z7 p; T g& `" N% ?& X: v. n: XALLAST, A weight installed in an aircraft to maintain 3 Y$ g# p; O* V. O7 P5 |0 aALL NUT, A fixed spherical nut driven by the ( o. w! a5 V6 w4 r, f; k' UAR OUT OF VIEW, A signal used to remove the flight3 M, k6 `; |8 n( D- l% o1 w4 A% N AROMETRIC PRESSURE, The pressure of air above. T8 m. \2 I. p3 p% [: t6 C g) or* U6 K' b+ u: [3 t* l |- N millibars (MB). & [; e8 y) r- Y% c9 o# m- Q GATTERY, An electrical device for changing stored' @* @: d0 n( T- r, R& A0 T 性能的场长。在此, k! o8 b3 F8 u% `# S2 \. O% ^7 @9 E$ a 况下,V1时发动机故障,要完成加速、起飞、离地35) c7 F5 ^, r& [ 尺所需距离等于相同速度下完成全停所需的距离。 + d) |6 G) I6 J$ n( ? K舱物, . r. u1 x# o9 d/ S9 D% r6 m重心在许可范围内面装载的配重物。 , u. {5 V$ y1 V1 n形螺母, / D# z( u9 K, u0 P的固定的球形螺母,用以使襟翼和水平 A6 j, [% }+ n- i: V9 Z引杆消失,( t0 C; T& v- o 指引杆的信号。% W( b+ [( g3 s% [! T 压, 5 H4 i/ n) s- v" Q6 G# Z6 v0 o压力。通常以多少寸高水银柱(in0 ]4 x' E i+ a, m# P- Z: N. A 瓶,# C9 z5 M5 q5 K 的化学能转变为直流电的电气装置。 2 c6 ^/ h) d1 fo8 ~" w8 ~; b, z$ `; f$ {; P fa , ^5 ?) ]3 s3 H5 ja' i$ e: \, z2 B& p0 a/ J7 [' \$ o required to stop from the same speed.' ` f# R4 ^+ j B ' ?# @/ V( u6 S; T+ fthe center of gravity within allowable limits. ( P+ B* A9 T3 JB " ?# Y% ]9 q- v1 g7 pjackscrew for flap and stabilizer movement. # w1 ^& O5 `% M/ @) GB# d0 u8 l3 s& s6 J" p1 w/ d director command bar(s). ' u. V2 `' \. R$ E/ B# [B0 ^5 a+ v4 z- f zero pressure measured in inches of mercury (in H1 |# f/ K2 t. N( `- _5 \4 O4 v7 D in+ M9 K% P4 {, _# ?" k2 q BASE METAL, The underlining metal to which alloying . g% x' h, _8 a1 [ q/ bagents or metals are added.! y5 ~7 X3 c5 ~: c8 P2 m B # Q* s. Z; X9 H, w- D$ L5 mchemical energy into direct electric current." ?8 Q1 o0 O1 g/ P; G; ~ 平衡场长, 8 g# p* k) s5 @( T+ C当障碍物非限制因素使飞机达到最佳 % [/ M7 [" X3 h! V2 f) T1 T/ ]; v9 c: Y+ V8 |$ I5 g, R4 }# {7 g) p5 Q; v3 c+ e8 V6 y% }1 Z; r为保持飞机 7 I" ^7 u# |( W h! a1 R/ Q% k5 a/ j% H, a3 i5 o& M& r6 ]# y( V& ^! O 由粗重螺杆驱动 . f/ M8 ]& A0 Y" }. j安定面运动。 # d- n2 J1 m& Q# t& H: a B; A- g: }, P; \. U6 [3 q 用于除去飞行! Y- Z: @" l! v, E, X6 v1 G+ B. F1 o; U8 b+ y零压力以上的空气 * s' ?( s6 J& D p' QHg)或毫巴(MB)来表示。0 z! t2 S8 `, N, X3 T3 @7 M+ \' | 基底金属,) f f. ~- Z! D/ ?9 a 指合金中的主要金属成份。 2 W; J8 `/ C! G% V9 o* ^; k; R5 c u: ~2 y+ g- |9 U" ]5 z将储蓄 , F s O7 t) C! V英汉对照民用航空词典B OEING5 Q, p2 I" c* H/ Y; ~9 M TECHNICAL DICTIONARY 183 ^) r; J. U0 ~: Z& F! o$ R$ q BATTER8 n9 T# I, A5 s) @/ E$ J+ Y direct cu, n* N$ P. Y) h" I! p/ i' u power su ) I* }( `! k( h& `4 GY BUS, An electrical conductor supplied with : D/ n8 g9 ~8 E3 p2 M( W1 X+ urrent from the battery or transformer-rectifier for) S# ^; a6 x# Z) u pply to operating components. & j& a7 h6 O# R* q6 o7 |8 _CHARGER, An electrical device supplied 8 j- U" c$ O, O4 cith alternating current, which produces a direct current, H8 l6 J5 Q; M. v utput for charging the battery on the airplane.$ l7 s# b8 e; l2 E- B AY, A compartment in the airplane structure. # i O# |" b) a# B! h: ]CD, SEE - BINARY CODED DECIMAL 9 w6 w2 T5 f. xEACON, A device which emits a signal for use as a # `6 m: l$ p7 S7 k& Z0 T# duidance or warning aid. - H4 C; E" W k j' I# ]BEARING (NO. 2), The direction from an airplane to a5 z+ N0 v% l5 p2 ] ground station.7 h6 a( b. W- O 瓶汇流条, 9 O' h0 f0 ^+ C/ M将从电瓶或变压整流器来的直流电供给工作部件的导7 S+ D. |2 \7 Q1 Q' G0 ? 体。 ) J- l$ Y+ Q& X4 R P瓶充电器, " i6 P- ~% k/ a5 E% M; K/ Y用交流电向飞机内电瓶充电的电气装置。带有交流电的 2 N7 H' u. b t* ~1 y气装置,该装置产生直流电向飞机上的电瓶充电。 ' P) u I1 v5 R' n舱,3 n/ h& k9 _5 x. c/ g6 p 飞机结构中分隔的空间。$ |' m6 A M1 P, V: f! g8 M- g# N% D 二进制编码,7 N( W' Z- |6 ^3 w2 e 见Binary Coded Decimal8 R8 Y1 G9 i9 U& c8 u" T BATTERY% `6 w0 a, @% e9 @( [$ w8 X0 u ^ w w" `9 u7 y2 i7 P V3 r: oo2 \/ i' o- p5 S# Z) I/ S( w% M9 Z B Q. t- [# [5 T2 ?9 k B : o w( x& m* T# t8 I' JB 0 w0 A& i7 q( b! R" C* v% Jg 2 g v/ W# g! H4 xBEARING (NO. 1), A surface that supports a moving 7 n4 Z1 z- x( J `- Epart and reduces friction between the two. * ]! y# s5 X, N& g, E5 _( ]1 k T* ]- T4 f T, g: U+ n8 G- v9 n [9 R" P- o4 N, H0 [% u$ J+ M& L- q/ P- D3 m8 T% W4 e1 R' o/ C7 H# i& Y- T( |! ^. j X! q7 @ 信标,+ L! j. p! l$ C7 B 发射引导或警告用信号的装置。 ; C7 G0 l) N5 Q: q$ D }$ M方位(NO.2), ! q( V+ C4 |. z3 ]7 V从一架飞机到地面台的方向。1 U! D+ F8 e5 o1 |2 m+ ^ 轴承(NO.1), , F( u9 [3 `& }/ U4 m& {用于减轻机械转动磨擦的机械装置。 6 \3 _/ B r E e* z英汉对照民用航空词典B OEING 1 A, P6 }! s$ BTECHNICAL DICTIONARY 19+ t, C1 J2 u8 R5 Y! } BELLCRANK, A double lever in the control syst [; b" J* S, F# B! n( tchanging direction of motion.+ ]. c5 ^) s5 R+ k em for9 c, m# }# f6 r6 X& T. F' i ct in the8 z/ }0 \6 h5 W0 D! }% ` neumatic system for absorbing expansion of duct due4 j& g; N2 l7 `( k: C% C heat.7 z7 D8 P% Z" L; W2 g$ j& Z' x ELLOWS (NO. 2), Corrugated folded or pleated" k7 x1 v, \' a7 v- `6 x ontainer or compartment used to measure pressure.8 P0 ^6 N- D3 r, b8 }/ h+ @ EZEL, The part of an instrument case for locking the 9 b! ^# h% z1 L: W7 F- `lass.; W! V- h8 O6 |8 G' {/ r IAS, The potential difference applied between two 9 s, I! K. O. ?0 ~( Y/ ]" R h9 Ioints for controlling a circuit. 9 K2 e7 _% b+ v1 wBILGE, The lowest part of an aircraft fuselage. A place+ q7 Q& W' \! i where water, dirt and other contaminants collect.) l! L6 y! k% y; F6 E! Q c 气源系统内提供管道热胀冷缩所需要的余地的波状/ j9 t6 F. @3 y/ X7 [5 e2 G$ l1 G 轫管。 ' }5 D! q1 H3 G# K+ @! ~# s空膜盒,4 _& u3 f F" s. U8 N2 d 一种具有波状表面的容器。用于量测气压。 ' [+ r# F% i7 ` l9 a" U1 ^嵌沟缘, / j4 L& g: `5 r' }( g将表面玻璃固定在仪表上的圈状零件。 % W, m7 ^6 c9 N! n压, 4 [9 ^) e3 h2 b$ j2 v在控制电路的两点之间的电位差。; @: Q( u0 P0 G* t/ u5 j0 f5 d" m 机身腹部,$ V+ k: [8 c) J+ T/ ?3 t$ a; z( p 机身的最底部,通常水,脏物,和其他外来物集存于此。% s$ G2 h7 O8 Y2 \0 z7 a) B BELLOWS (NO. 1), A corrugated flexible du, |2 w; S5 Q5 c p 6 U! @" ~& e& }# F* N0 x4 }to2 Q; g; w& n: O B, m) b" O0 X$ l4 g9 F c # ~1 o6 ~" V+ {, qB ( f* L1 X, L/ X5 tg c! P$ e- v+ O" w% H0 z' I; `6 h B: n) ?7 C. y% | p: b: a1 F! r5 q8 X; q 直角摇臂,+ Q! m; j% s4 d- t 在操纵系统中改变运动方向用的双臂摇臂。 & X" d% J% }5 D7 D" C波纹管,4 O! C. Q8 o: {/ u# \" A6 |1 T' j3 h" {2 j6 a) i2 `* c- }6 i$ t4 E. n* m# c9 ~. B0 ` Y: y7 v/ E! |. [: N% W Y: E/ R1 I; W英汉对照民用航空词典B OEING 4 l$ E! w j; C1 m& ~TECHNICAL DICTIONARY 20* m. N/ E6 n% S6 d# n' p BINARY CODED DECIMAL, A system of coding each2 j6 U! |! K8 `; t/ r( B digit in a decimal number using the binary equivalent.& j- N2 P- k7 K/ w BINARY NUMBER SYSTEM, A number system using $ H( N8 \# {: l! [: l% As9 b4 k! T5 _) U9 i1 O5 | IT, In the binary number system, the smallest unit of : ~% t, ~/ h G+ ]" lformation, consisting of a 0 or a 1. 4 v- ]: l% z B% i: h1 yITE, SEE - BUILT-IN TEST EQUIPMENT ! L+ i/ K1 d @% G, U9 OLANK DISPLAY, A display that does not have any ; z6 H" P. E5 C9 ^2 Gdications, normally due to failure./ {4 `& J( R8 m* _% z; O LACK BOX, A container for electronic circuits to record) s2 m0 { X/ G m/ w, G ight data. # X( P) r. E t$ V: E* d4 Y, zLEED AIR, Air taken from the engine to power various0 W. w8 N& W( \) g ircraft accessories. 5 g* E2 Z% W5 C. \A valve in the pneumatic system for air, ]4 E2 K4 o# l. P) H supply from the engine or auxiliary power unit to the. Q, E" u8 [7 E) t pneumatic manifold. A valve on the engine for reducing 0 y' ]7 L. ] }. hpressure in the compressor section. ! y! t1 X( n4 q I进制, - z! P; s6 x1 E2 |- u1 O0 q% W7 `" W. _进制, 2 t/ f7 z/ `, o一般用0和1)和2为底的数字系统。6 G% @0 e6 L/ N8 H$ j 特(二进位数), 4 j: O) K9 p# ] V _9 I! _1 t二进制中的最小信息单位,包括0或1。 : q }& B' i |; @6 j内自测系统,( ]9 w) A& M7 i# }& n 见Built-in Test Equipment . y9 z" `- d/ w# P' c2 a$ Mtwo symbols (usually denoted 0 and 1) and having 2 a& H7 L- Z3 I2 N3 g/ @ its base." f& x) v9 k" w4 h B5 i. p G" i* H( q( |+ o. r8 A in ' l. J7 P% V5 Q0 i5 FB5 T4 g* {- Z# O: N$ [8 y/ o5 h B & f% Z! D9 W% A; m& r5 r! Kin ; O m0 o) @" w$ E; Y- DB4 p- q2 U7 `0 J/ N8 [/ L6 v fl3 n! n0 h( n, o- C B " M" {. @& U* s8 o6 X2 I* z; t! |a+ h; O4 |$ E# i BLEED VALVE, e% T8 [* ~! b2 {8 Z' ]- S二进制编码的十. p& p- t0 a1 d0 I3 Z 一种编码系统。用等效二进制位数编译十进位数的每一: |+ a& q6 ]5 S8 n: r/ g 位。/ R( v" ^0 ~4 A) g+ d* U: t% A1 Y" E# V% C& Q9 n" b 以两个符号( 5 {2 }1 {% h; M# C8 W6 [7 j" j. m7 {2 D4 V3 f F. S . 4 a+ j# i; m5 ]1 J% L) X白显示, 0 z, K p ?8 J通常因故障而造成的显示器上没有任何指示。 ' ]: V( m" K- i/ ?9 t% i' V匣子, 9 {8 W& h6 w9 Q3 o5 K" f T. K% Z装有用于记录飞行数据的电路系统的容器。 ' I j7 k* j+ N+ N气,- S6 ~- }. O& g. l% C& @ 取自发动机而用以驱动飞机上之各种附件的空气。1 o7 |# A* Z9 H2 Z8 M f 气源系统内,使来自发动机或辅助动力装置的空气进人9 S6 B; x& s _$ j) K( ^9 J, { 气源支管的活门。发动机上,用来降低压气机压力的活门。 ! v; A Y E: N+ j% Q' o6 M; h, L! O! U! J4 ]! S" |! C+ z4 F4 j) M! v3 s% c& i2 m8 L. x$ o引气活门, - _* X$ Y3 x0 d) A1 x1 g9 [& v2 \9 u" f英汉对照民用航空词典B OEING $ }6 b( O$ u( E) g& |8 @( S" _TECHNICAL DICTIONARY 21 9 ~% Z3 ~1 w' J2 J* z4 c5 ~BLOCKER DOOR, A device on the engine for blocking- q F# k$ Z) O' j the normal airflow during thrust reverser operation.# X% I6 }# d% O6 K$ D" d& Y: g; u) @ LOWER, An electrically operated fan for circulating air. * j# n+ A1 N0 t( G2 O' nLOWOUT PANEL, A panel in the structure between 3 f% {; \7 o9 d0 W$ ?o compartments that opens to equalize pressure in ! l; [/ C* b' Z7 ?e compartments.6 C0 o- W6 G5 _, d/ J" j* |# O ODY GEAR, The landing gear attached to the& y) ` V3 q; h# t$ M& M9 X, }2 M grounding. + B( k/ }% S) `$ C' [正常的: h7 b! w5 s2 h! p+ c 气流。; S" U0 `0 d% Y7 u6 i6 ]; v 鼓风机, $ ~/ z4 w' @: F* G- d1 x用来使空气循环的电动风扇。 / [3 {0 `5 F; y- i压口盖, / ^# Z8 J, }9 J( ~两个隔舱之间的口盖,打开后可使两舱压力相等。1 |9 @, E* q) x- M! w, a: ^$ x 身起落架," M* \; r4 ~6 P0 H/ d" r; ^ 身构架上的起落架。 C6 K' }" |' L, p- ?: ~ B * o% b% B% p1 nB 1 I1 `( h, I) Qtw " P) E! E7 ~% vth. V7 h# x. f& \ B/ w$ O" A6 E5 t fuselage structure.8 x) o, f& C3 A6 `% h BONDING JUMPER, An electrical connection between3 \/ v) p- b; N a component and airplane structure for electrical( y- l* ]$ E5 J0 i/ P 阻流门, 2 i* \6 y( \# h/ N [发动机上的一个装置。在反推工作时用于阻挡 0 I" E% F) k2 L3 B! f; i6 z& } g+ z7 Z5 K8 a; r5 V. ? T9 c. Z 装在机 * R" h x5 ^7 X搭接片, 5 @, O" d8 Z2 k: Y连接某个部件与飞机结构以形成接地的电接头。 1 m0 Y1 s& Y( n5 t英汉对照民用航空词典B OEING : ^7 b& t1 h7 w) D8 f: ^# b: a4 STECHNICAL DICTIONARY 22. S* |0 F( ~* K- }( V; a, j& p( _ BOOLEAN ALGEBRA, A mathematical system for 7 A a3 L7 L- f- Fwriting combinations of logical statements./ m4 K2 ]! ^# X# h' Z BOOST PUMP, An electrically operated fuel pump for ) _% D$ k& y4 M* Ufuel supply from the airplane fuel tank to the fuel( j3 ^. g3 H1 C& r manifold. ' i: h4 @8 {$ E9 n0 [BORESCOPE, An electro-optical device for looking at/ W6 a1 P+ u- U! w& Y+ D ternal parts of an engine through holes in the engine. 1 `$ }3 Z4 A6 q$ qorescope ports)6 c1 H8 x1 i7 o& x; Y6 e OURDON TUBE, A curved flat tube in a pressure gage $ k- }7 r" p" W1 B9 G5 a; Jr moving the pointer when pressure changes inside ) W B. h4 i+ G5 ?0 ron the ability of the brakes to ! c2 D! Y4 b0 e* G: y+ ^' `bsorb a predetermined amount of energy during a/ c7 Z7 m8 L! V jected takeoff.7 H% _$ ~+ S( z+ T" A 用于通过发动机内的孔(孔探口)观察发动机内部件的3 Y. }" M2 k" s+ F/ ~ h 光设备。 4 Z8 D* Y1 k; H$ B1 M0 I" H端管, & c0 O( W5 g9 a' I5 v8 o5 L8 S测压计内的弯曲扁管,管内压力的变化时它使指针移/ y( ` ?- F. Y7 \" m4 { 力。* @7 _" x' m/ h; Y; U/ f* d 极限重量, 2 I3 ]: O' ]( C; L, i- c M: c& W H& I3 y+ w6 W起飞重量。2 _3 p6 i8 X$ w$ ?# W6 {, u 发动机滑油系统与大气相通的通气口。 % N& n" t s# [! Nin 9 f1 a& ^0 D4 f$ z+ _(b+ b$ I. P$ u% b B3 @ B: C- G/ f) y4 S% X7 o& J fo & N( @2 k" o+ I. q/ i* h: s) v; M" nthe tube.4 n3 g# d+ S& C) G1 W) l5 O1 g BRACKET, To enclose or surround.) N' J, s4 ~; S+ o0 i1 d) O BRAKE ENERGY LIMIT WEIGHT, The maximum: W. d4 F5 \2 ?0 Q$ E0 p% t W5 ] takeoff weight based ! v* N$ r4 j. i+ i" E ja3 q7 d, g# ?: ]4 F F7 k' M3 J0 {# U re7 I6 ]$ S) e. Q/ L2 s0 E( V BREATHER, A vent to ambient of the engine oil system.( Z4 M7 ?6 w2 F1 Z, b 布尔代数, 3 U* _" s$ N! P' G一种用于编写复合逻辑命题的数学系统。8 Z. Z8 ^" Y9 H* c: g q/ ?2 | 增压泵, 7 o" p0 }) I; O ]! U9 R/ w3 V从飞机油箱向总油管提供燃油的电动泵。- y) T2 @* v/ E 孔探仪, 3 e2 X7 M" l: v8 G; L/ p& H; L8 q" s2 v2 p1 t8 c3 M B- T* t6 w2 n- G3 q* ]# g. l6 @" L 动,以指示压 0 I# J+ L% s% e3 t托架, 1 T8 K; Z+ Y. R; F% D用于作支撑、装托、或围绕之用。 ( t$ R8 d( E- V& V4 V$ }刹车能量 ( C$ v1 Q" V6 R% J: P% }中断起飞过程中,取决于刹车吸收预定能量之能力的 0 u( y' i8 }0 I; r1 T9 }' J _' Z+ P; j: R通气装置,- ^4 `8 y' h6 P* Z 英汉对照民用航空词典B OEING ' r5 q) D& K, F# y$ K8 x \7 @+ MTECHNICAL DICTIONARY 23, U0 U2 w$ W" O# M BUFFET, Vibration of the wings and airframe resulting * F8 V" j) L# k) q8 G8 \, L+ d- ^) m& ^# kfrom unsteady airflow over the wing; caused when; E* ]9 z/ {& n airspeed is too slow, the bank angle is too steep, or4 f+ G3 h4 m! U7 C( J* Q irspeed is too fast.- {! `$ @- X' y* F6 z5 G UILT-IN TEST EQUIPMENT, Equipment installed on 8 ~' _; w/ o# c1 S+ M8 i3 xe airplane and in airplane systems to test the systems7 {$ W: {7 p- `. ~& _ ithout external test equipment. 8 U" s) I. X. tUFFET MARGIN, The amount of residual maneuver & }' S m' ?5 qapability present before the onset of buffet. ; R, A! q* Z* ?' ?5 F0 rUG SPEED, A preselecteed speed to be observed# y0 f0 M% U$ k# ^6 L- Y( a nding sequence.; `% v, x% O0 T4 `/ } k1 L( o! Z- | a ng landing gear operation.9 ?5 K6 o7 x. x/ x4 O% E- o, \) | 速度太慢或太快,坡度太大,均会引起抖振。, ~; s4 j9 M6 ~* `* c 自检设备, 6 F+ W. A2 J! M! N# {: J+ F安装在飞机和飞机系统中,在无外接检测设备情况下,. O1 h0 b2 I+ H9 F7 z( y! h 用于检测系统的设备。 * g" ?5 o; B- R, D抖振裕度, ; Q6 {. b1 o& y8 Y飞机在遭遇抖振之前,剩余机动能力的大小。 ' R/ H2 M1 a& {标速度,/ F7 ]' v. b% \/ X* h, p 在某些机动飞行过程中,特别是在进近和着陆时,飞机 e5 o6 ^' q2 W* n4 b预定速度。 ) Q+ W/ t7 Z/ \; q' V力装置, " N6 D+ {7 r2 L架工作的一种机械设备(弹簧或减震器)。 1 G% N4 d$ X7 ~# _) M流条, : B ^ I+ U. F4 E/ y在部件或组件之间传输电、数据、或定时的单一电线或 4 r7 P2 o% j ] U' d3 \ Ga ' P9 S7 a% `, P/ P9 w) M, PB5 ^; v- `. Y+ ^ th% O; L/ ?: |2 w* @+ n% ~" @8 u( t w . v9 q0 Y. Z9 l8 R8 x) n/ | w* jB ) |( t# ?; N2 C- Q9 ] xc- J1 |( @4 Z/ T. q B! r) o+ [. ^/ y5 V# S4 j3 M4 o/ l( o+ Q during certain maneuvers, particularly the approach and % c. W1 W7 J. V* c3 q* K7 Q- M) ]la9 ^+ G: T2 i2 B$ f; w+ R+ n5 I( q BULKHEAD, A structural partition in the fuselage or . s# X& `9 |. H6 S5 O* S& Hwing.0 K7 j; r: y; S1 G# [& _3 U BUNGEE, A mechanical device (spring or a shoc " \* R; i4 n5 a/ z# N q0 D* l, q* sabsorber) for assisti: \7 C- A7 E" J- K0 U BUS, A single wire or group of wires which transfers . V9 ?; {6 |% {" h- U' ipower, data, or timing between several units or " t9 R x |* r& _' T: rmodules. 1 h) u1 M6 }, A) R6 R# E' `抖振, . N9 H$ u3 Q/ V/ s由于机翼上表面的不稳定气流引起的机翼和机体的振8 I# J5 K7 A' l, I) v6 |% l( ]- L 动。飞行- M. e* A& V% q; V6 I6 s) @ {% w; x" W0 Z! |7 Q1 t( c所应保持的9 n& m& d# D: u$ K4 I- D0 @ 壁板式隔框, 1 T8 K1 ~9 W0 L8 O3 ~! R$ K1 j% F机身或机翼内一种结构隔板。 1 S# }2 z, b% M# R9 y8 z5 e- K' d( j( c( i% [5 y用于协助起落; ?/ _' x* C. h( R0 Q" g# M3 p& u 电线组。 . D( H3 |( }% m2 p. D1 O) E8 o* ^英汉对照民用航空词典B OEING1 \+ T) D9 M# g! `6 [* V TECHNICAL DICTIONARY 24

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发表于 2008-12-24 21:37:30 |只看该作者
BUS DRUM, A mechanical connection with pulleys $ N$ _. w/ K/ Vcables in the control system.7 }9 m7 w+ J) z0 a7 p# b and % n; N* J4 O' @9 z }1 D4 Hl circuits for control and protection of . ^' O. h* J1 Olectrical alternating current supply to the airplane. % w% O5 ^, R2 l' l' Q8 _- ^+ gduct for closing and opening the duct 0 ~4 E& O; o) o' Lassage. / |$ P7 _8 w2 WUTTOCK LINE, A vertical reference plane along the 2 A8 c, O3 ^" Cselage for horizontal measurements of the airplane. & v" o6 Y0 S1 \4 O$ u接。 `& D: c0 _7 d6 F+ S组件,内含控制和保护飞机交流电源的电 * g) |( K* r5 v" G {% ?' S" ^# p6 G7 T2 h6 i2 \" k3 R作动简控制的转动装置。用来关闭和9 w) k' v8 N" P) p$ J7 Q/ p 启管道。1 C3 e7 K) @6 u8 H+ u5 h 沿机身走向的垂直参考面,用于飞机的水平测量。2 ^: t. i; Z. M) J' o BUS PROTECTION PANEL, A module (black box)1 g) \' g4 V3 [8 I containing electrica( o$ j! O; R9 J2 d e 5 H8 M. H" [8 Q) d7 }; |5 U" @BUTTERFLY VALVE, An actuator-operated, rotating5 [, v1 g2 t$ T; c9 \9 ~, | device in a ' r5 R# L6 r2 m5 k0 |5 N& G0 h, ]p/ d O; L+ Z4 {6 K# f B 9 W7 i! `/ D7 Q% M9 w3 Wfu / H; A/ @7 g* z8 }" }4 I0 t转动鼓轮, 6 V) X; |8 \4 p在操纵系统中,具有滑轮和钢索的机械式连 5 T- K9 b& c& O汇流条防护板,4 \2 X0 [% A. y- a/ w) o9 @5 D 黑匣子式的1 _( w/ z: Z Y6 ?0 i4 b! Q7 |8 ? Z2 w2 B& | X蝶形活门, ) s5 |* }' v1 J" d4 c% M( S是一个在管道中由 A! j8 d& }. O3 i# V- X4 ]- r: ^( Z; E3 P. I纵剖线, $ d& u7 }$ h6 d6 d. O" s英汉对照民用航空词典B OEING8 C/ A9 G7 r# l, [' I4 A' I; h. } TECHNICAL DICTIONARY 250 U( I ] d, M q0 |2 C2 H5 ] BYPASS VALVE, A valve through which air or fluid will j8 ?. U! H8 `* Q# q# @3 n9 bflow if the normal flow path is blocked. 0 h; q! N" ?3 O# a0 l/ TBYTE, A group or string of binary digits. A byte is" ^9 i( n [7 f. I- s+ i! N6 p z# x sually eight bits long./ P: ?% N! c. O T k ABIN ALTITUDE, Atmospheric pressure maintained 1 x9 o8 B8 s3 K1 `- a* @ithin the cabin, indicated in terms of feet above sea ; m9 T$ A$ u+ Y( k& k4 c3 lALIBRATE, To repair, adjust, fix or correct the# M! b, G1 X3 E8 ? easuring capabilities of a measuring device.+ i- D+ x$ O0 } ALIBRATED AIRSPEED (CAS), Indicated airspeed * M5 X% D: e- b( oAS) corrected for position error.) |4 F7 b2 j; P1 q/ j: ?+ k nical( [6 k' r( R( e) p, l" @3 F. U omponents. 1 M9 p1 G9 }" U# `4 H2 n: I1 Q9 e& N8 o) g2 S! X' Q 节, 3 K* M6 s; Y" d& O: i一组或一列二进制数。通常一个字节长8位。 * {6 K" Z M( y4 P/ C舱高度, Q; R: j' y. S9 E3 A 座舱内保持的空气压力,以海拔多少英尺表示。 A/ K9 Z2 z- G1 ?) i5 t1 p; @ 准, / X H! \2 E3 D& I! n* g0 F$ Q% E修理,调整,定位或改正测量装置的测量功能。, _% b+ b& f& T% j. q 正空速(CAS),7 U1 H3 \8 q( Q. Z/ I9 L 在修正了位置误差之后的指示空速(IAS)。 $ o/ {- h% l- I6 G4 I3 W8 m; R( R1 I1 M用来移动机件的一种转动装置。; S a0 n( Q2 y% `8 w4 f/ [ u ' s @' n) k" V9 B+ @C ) |5 J7 {+ k" Q7 ]" e% D# e0 pC & a% q9 Z/ I* C& Qw: t8 O q% [6 p0 x) g# { level.2 C( J# W" E' S! `8 ?; E C # t# C5 n& C- A& I- Rm ; |2 D* l3 @& G* X, w2 U+ m* AC ( ], ?1 M" p5 `! d(I7 e& S7 G8 T0 C+ l2 O) G CAM, A rotating device for movement of mecha2 d0 ~4 i! h; G s0 b9 `; v6 k C % T# o- c0 S8 ~5 l- T3 a" ^: S. w旁通活门 h0 u t1 }5 { 气流或液流在正常通道阻塞时所经过的活门。 # J& R6 @# f, \% `2 [( [8 x" @, A5 e+ Y8 F1 |5 m( v# z1 [2 h, J. s5 D$ w+ |$ l4 ?) x2 }9 w2 ?6 U" c5 o( T/ \ 凸轮, * f* \4 a1 O. z, G) }; k1 a英汉对照民用航空词典B! H, w( v9 x8 ~% r' T) C/ v! ^, _ CAM-OUT, An autopilot condition in which the actuator' b3 N6 A. V- a# O, ]# S7 E detent piston is overridden, either manually or by the! V0 A/ [ I& j& x ther autopilot actuator. # z% c! i9 E' L3 @AP, SEE - CAPTURE - q) o% g; u9 L2 q% u& j9 GAPACITANCE, The measurement of electrical energy% ] i+ U5 R$ ~ tored in a capacitor (condenser).0 u8 u: y% T4 ^) l- | APACITOR, An electrical component of two metal , A1 ?/ g% W( E9 t2 glates separated by a dielectric material, for storing" p( L; b9 D3 v: [+ v G lectrical energy. ( E6 | d! B6 k# N) ~: q" PCAPTURE, An autopilot or flight director function to$ E/ z U8 c8 s( o+ O9 i- T acquire a selected mode.0 W' X: p4 C* j CARD FILE, A container on the airplane for printed 3 Q; j4 d8 P- Q: ?7 Z' acircuit cards. v6 A4 U. ?* n 一自4 A$ t, e( N0 W5 s 动驾驶舵机所超控。 ) F0 H+ p9 Z7 l% a9 a8 h截获, * u8 _, q1 S+ S' S: D( m7 U见Capture : {! k0 B. u2 E" s) u9 ^, H7 Ho! N3 ~- A/ a4 H C0 A& H, g% U5 R4 A" \0 f C , w' j. y: a& Us ( q, }7 `7 m# y3 c* G- w; ~C 3 h' L$ }. _! {8 P& Zp j0 }8 d# s$ Q" M' E e & H5 {" b, Z6 J Q/ x& v凸轮不工作,- Z$ Y X/ u5 H 一种自动驾驶状态。此时舵机锁定活塞被人工或另$ e2 t- r1 }# M4 E% ^9 p5 ~: a' Z$ z( Y/ R: S! F 电容量,2 t, L3 S7 x+ {8 L" q" P& m 电容器内所储存的电能的量度。. F9 _! [' U* s. B$ b: h d 容器,4 H0 C* I$ q$ k1 t0 O: ? 两片金属中间用绝缘材料隔开的电器。用以储存电能。 ; u! [ V( w( V0 E截获(CAP), 8 Y% u8 s7 Z, G' s& `9 a自动驾驶仪或飞行指引仪的获取选定方式的功能。 m: R7 j3 s% _: F* Q线路板盒, # Y8 ]7 W2 L! ^, _/ s/ ]飞机上安装印刷线路板的容器。 [9 t8 {" S U5 ]4 m# Z U4 `/ W( r1 K0 d OEING, e# q* r8 H# x9 n4 T4 J TECHNICAL DICTIONARY 26, |" r$ H9 f1 y$ m0 {' ?0 y 英汉对照民用航空词典B OEING1 \: ]$ w) X# j. Z TECHNICAL DICTIONARY 275 ~) v: Z2 `, k' ^ CASCADE, Two or more similar circuits or amplifying * p' G! s& J0 _8 h. t3 M" O5 Lstages in which the output of one circuit provides the ) \* `3 M1 Y3 H% `, U1 dput of the next.3 P' m9 i% C/ j0 m+ n: i ASCADE VANE, A vane for turning the engine airflow( C) Y/ l3 ^- A9 ~' N uring operation of thrust reverser. . G+ v/ |2 L0 T* c0 s. PASE DRAIN, A drain carrying lubricating and cooling c3 d0 V6 P: w2 _" i0 q uid from a hydraulic pump.$ N" W# C& o+ A8 \5 ^ ATHODE, The element from which the principal* N/ H! n3 P! b/ `! u tream of electrons flows. $ r1 K7 @& u2 ~) ]7 kATHODE RAY TUBE, An evacuated glass tube with a : G9 _3 d2 ]5 X$ V" SCEILING, The height above the ground or water of the7 u, S% z( c+ R; @ base of the lowest layer of cloud below 6000 meters* }$ i# `9 J; e% x (20,000 feet) covering more than half the sky. 1 k6 {5 a& t; W$ N) V" L. Z程。该 1 P/ ~! x$ k8 t程中,一个电路的输出为下一个电路的输人。* Y h6 E# P, N1 c, e 叶栅叶片, a( Y' ^ K3 z: @* n2 T 在反推工作时,使发动机气流向相反方向流动的叶片。 5 F2 @; d x0 P匣余油管, 1 l! ^! n" f7 Y+ b液压泵多余的润滑液及冷却液的排放口。 . l7 d$ J+ y( A1 ~1 {- F/ K. Q* o极,/ ^2 }4 ?% J, U4 m8 _5 g 电子流流出的极位。/ y4 V6 `; y% _# A+ d 极射线管,+ `2 w7 F H+ S$ Y- ^ 有显象屏幕的真空玻璃管。用于显示信息。 - Y# T6 Q& D# ]' l( \0 j: _# r云高(云底高)," Z; @% c( y$ i, R) x 6000米(20,000英尺)以下已覆盖一半以上天空的最 4 G. u5 A6 x: s9 ?* c$ G低云层底距离地面或水面的高度。9 i7 V& y7 a/ K: J& o E. y4 D& u; Q in 4 o% l2 E, ~3 P$ T, o$ Q3 wC3 A/ u+ f0 S H+ i% Z8 B4 n$ E2 n2 E d ; I5 V/ H+ Y$ D1 bC : \. R; q% j. ?9 {: ?fl & b; O0 u" V' ^C ; a2 ]: }, V% O; x- {s 2 c; x' S* U0 q* l: D2 [; ZC 3 r' f: Q+ V9 {- m+ v0 }1 N- l" |viewing screen, used for displaying information. " X$ R f' `; m5 P3 `级联, ' ]) }7 x; q2 Q' s2 R# N$ j两个或两个以上的类似电路的逐级连接或放大过" L5 j0 k, F0 g' F5 \9 m- r6 |9 W+ o: r9 Z9 e0 |; X% |- k" V8 S$ J# h% ^0 f# S- ~2 T; ~$ R. R6 w# r7 N, j2 R J+ @一个具: K% a5 |3 e% L/ r- a1 | 英汉对照民用航空词典B OEING ' L9 y, w- \9 y1 q+ \0 E9 y# ]TECHNICAL DICTIONARY 28 3 h: c- ^0 m. TCELSIUS, A temperature scale in which zero is the% t$ f( z; b& Z8 | freezing point of water and 100 is the boiling point of6 @. Z- z( V/ N! _- } water.# F3 k% m* l% O0 X; R& X CENTER OF GRAVITY, The balance point of an object 5 l+ q4 R8 G8 m2 M ?% b! Fr rigid structure expressed in terms of percent Mean2 x) d4 A" P" V# p3 z/ I erodynamic Chord or in inches from a reference point. . Y O/ o) c7 h& X/ J% S" u8 A }ENTERING CAM, A cam for moving a mechanism to a + A4 q2 \* ^8 t/ b9 ?5 b$ yeutral position. / {) [+ L& W2 h5 Y) M# v) l+ L* {IGURATION, A configuration of the5 X: m4 B6 m, G8 r4 _ ircraft approved for operation by the local governing K. w' p, O/ Xgency.+ c0 |# |& z) e6 G) w- b ENTRAL PROCESSING UNIT, In a computer or5 D5 T v }$ O0 }; B1 d% v igital circuit, the section containing the arithmetic and7 K Y7 V; L5 ?+ x gic,control, and internal memory circuits.- T5 m& o- i( X ENTRIFUGAL FLOW COMPRESSOR, A type of. b1 r5 F7 M6 P) A# q2 j ompressor in which air is taken into the center of the- t) m2 x3 G3 V peller and is slung outward centrifugally into a diffuser0 Q9 ?( L4 @" g8 p1 D' @ here it is slowed and pressure is increased. 0 {: u! G+ Q" @ i8 nCG, SEE - CENTER OF GRAVITY" ] D; Q% g+ k) }* b: T 构的平衡点,以平均气动力弦的百分比或2 ?! T1 @% @* |1 D2 E& d 某一参考点若干英寸来表示。 2 s* T0 F9 N, N& \中凸轮,: ^- s1 U4 n; M! p% V8 H' o 将机构移向中立位置的凸轮。/ h+ q/ L& k( n0 Y8 D/ [& R 格的装机状态,, r/ W; K& {/ N 由当地主管单位批准使用的飞机装机状态。 # E% F9 f% T7 w3 X4 d& S$ e2 p- i: w中央处理器,, O; X9 f) s v/ L# Z1 S 计算机或数字电路中含有运算,逻辑,控制和内部存- q4 f6 \' z3 d 储电路的部分。 ! ^! w% s% r: s心式压气机, : R P! l& b# W压气机的一种。当进气到达叶轮中心时,被叶轮离心抛9 _% a: t. r: `+ t1 w3 T+ H9 v 进人扩散器。在扩散器中气体流速减慢,压力增加。" \& Z+ R1 \% e2 s; Z! d9 d# L 重心,6 G3 Q* \4 z" C" L& S+ K9 r 见Center of Gravity. W9 m7 o: [; k o; Q0 _. O. J. E A , ]9 [) ^& W( ]: y YC N! V# t2 g3 r+ N6 u& ^8 {; | n 1 o, }/ g. R( h) j6 p6 xCERTIFIED CONF9 R% v& s" ?7 b8 ^) Q# u a% y7 |, g2 l% F) i: U: x a) b4 o. i6 c* X C ; k6 f/ i# ~: w/ Q0 G3 ?d: n: K) n |) \/ W0 t/ b7 g lo % Y. O% Z$ i A( RC : [* {+ e" o# v0 k; ]c : h- R1 g9 g" X r N6 e" Tim + C; Z$ v+ V/ n- z1 Zw ' b, V" B3 W) N% n$ [摄氏度(°C),# O+ I$ \0 E+ @1 _ c 温度的度量单位。在此单位中,0°C表示水的冰点,1 u: d; u3 t- N7 j; K" r; s; l 100°C表示沸点。3 S6 L' H* m( F- m% u 重心 " J6 t6 ` Q5 x" ^物体或刚性结9 w% ^! [. H4 r8 P3 J$ D/ [" E0 M+ G! q/ `2 h1 J3 s7 p8 y( b- J. s w4 P3 f* @/ f; W% V( C- a+ J% a$ e$ W' S' G0 s. }3 P& ]" j; G4 F, u: K% h# u 英汉对照民用航空词典B OEING : @0 @! }& j4 m' ITECHNICAL DICTIONARY 297 h/ ~) Z0 \! U& H' x. G CHANGEOVER, Conversion from one mode to another.6 }1 y! E% ?. C- ?7 A& S HARGING VALVE, A valve for supplying air or fluid to( R; I2 x: R/ G% A' n2 h, P HECK VALVE, A valve allowing flow in only one. E1 |$ a9 F6 X! Z! L/ t irection. See Non-Return Valve. 6 h7 k1 V; T! b* U2 |$ J$ ZHECKSUM, In a computer, a summation of digits or3 h0 J7 z- j' j: Y1 x its which are primarily used for error detection.7 `& |) ]4 H$ { HIP DETECTOR, A magnetic plug in sumps of, j7 O9 V; H4 g7 D: @ bricated components for detection of internal failure of # c, [/ ?" w3 g4 S7 `; e. j9 K' ee component. 0 Y3 H$ I$ Q: ?; yHORD, A structural component of spars or frames.& ^: S' w6 P" ~+ T# d: A5 x) \ 添活门, $ ]4 k) I( ]7 d, c: z器充气或加液的活门。 5 n) B1 p4 S+ B5 a: [' @* I1 U单向活门,, T$ r c' z8 d3 I9 k 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 8 }* K; b" _& N# va reservoir.7 _' i2 \# h8 C1 [! u o C/ ^( M8 d9 A! n# z1 ? d ' l4 F- o7 q; N4 UC ; d' Q0 Y5 r- y7 {- F) m6 n* _b / ]* N% i: b- B3 M) ?C- P" g8 ]: }5 J lu! e* ^6 o7 g& G N th ( F6 @3 m% P) |" J# X4 _: f1 gC9 ?, X, R3 i, d4 Q O" V 转换, $ ~ X0 p0 f( s1 ]1 l; G由一个方式转换到另一个方式。% S, l6 {9 T( o0 ~6 l+ j, P7 g4 T0 O/ w( f4 Y0 l 用来向储存9 Z ?7 n. q% ]+ D% B# d& o1 I# X4 A- |- n* W- [ 总和校验,: l$ E9 w& V+ E( Q 计算机中,把那些用来探错误的数宇或位数的总和进4 S* R# P* {3 ?4 x( B0 [3 x4 u8 M 求和计算。 ; e$ I6 \, Y1 B* o属碎屑探测器, - r6 {; j) Q. J- i4 J5 [/ X$ ~装在被润滑的部件滑油回油管路上的磁性塞子。用来探 # ^; ?( G) X7 ?* t/ L' D部件内部有无损坏。 & y. e) z; M- B/ a弦,3 \6 q8 @# ?& V& t 梁或框架的结构部件。 F; `+ b2 E$ j9 I$ L3 a G' \, D( Z; L! a# S0 O/ V1 r* l8 H' F* u1 {7 y8 P n: x- O. M0 E9 J# j6 w( M# _/ v2 M, u; p c( h! F3 O" O! G8 I/ v" z2 s3 O3 n英汉对照民用航空词典B OEING" y& q2 P2 p/ t0 F7 b TECHNICAL DICTIONARY 30 , B( p# r; e4 p/ nCIRCUIT, A closed path through which current flows, \( `4 |8 O1 g/ L; k ource. 8 e' T0 _2 G/ Z2 \0 TIRCUIT BREAKER, A device that automatically * _, P" t1 t4 w/ p, Ueactivate the system.0 x# X+ }+ d2 p4 j lear of all non-frangible objects which , d& ^8 K. A' ]! nay be used as takeoff distance available when + Q( n2 I, y( K8 x* W/ y& talculating a takeoff weight.- J Q, J4 q3 W% B5 J4 [- H r water under the control of the appropriate 4 \0 S, Q) U7 M quthority,selected or prepared as a suitable area over 6 d4 h$ o* x& i. M6 Which an aeroplane may make a portion of its initial3 m6 H' t9 p" _ limb to a specified height." }* s# W9 N7 L! n/ p increasing. 6 x- k0 F! a. ~sed + y+ X5 u& q& \LOCK SIGNAL, A continuous string of pulses used for + X& A) c% ] u3 ^ `开关,! Y6 P; {. L" J* x m% @ 故障情况下自动中断电流以保护线路不受过电损 : E7 x+ X) P' H$ X- ?0 C+ L体障碍物的区域。在计, k9 |0 s0 y6 C) e, Y 起飞重量时该区域可作为可用起飞距离。 ) [/ C' d$ Z! [0 `& p4 Z1 M' z( c是在有关当局管辖的地面或水域内一个界限明确的长 4 y9 M9 t* X2 q* @6 U1 i形区域。在这个选定的合适区域内,飞机可完成初始爬 % H* C9 S4 ]. F7 m' X H b的一部分,上升到一个指定高度。 ; q$ @) c% \( R0 I, g8 Q% D飞机高度不断增加的飞行阶段。6 p; e3 _1 d# h5 S- A1 V% o* z 钟脉冲, % [8 m# f; }( |6 Y$ z步的连续脉冲信号串。 0 ?# ^! i' l q! l& @2 Vfrom a source, through various components, and back, E* h) }7 K6 c# @ to the s( i0 ~ ~, f8 _+ H3 \1 h& x C2 h" |" Z! S+ v$ E) J" d interrupts the flow of electricity (current) during fault 3 q: s" ?8 [) u+ ], k4 F+ x, zcondition to protect wiring from excess current. Circuit 2 L0 `+ r% n) |6 N7 V- ibreakers are also used as a means to manually$ Y& O3 ^4 b) m: f7 M d3 p v+ p; x( }* P CLEARWAY 1, An area beyond the takeoff end of the 6 p' C/ G: K4 d( Nrunway which is c 2 m& `$ S7 s3 L- }. X8 P3 b; z9 \, Nm5 H/ k: O; e7 Y8 v+ ]& s& X' t9 F c : j4 Q- Y w9 b9 e* O9 S$ P5 gCLEARWAY 2, A defined rectangular area on the 8 Y* ]2 Y& M0 U, |; L$ A5 _6 @, h4 Nground o8 h5 ]: o& M5 e7 s a # ]- g, i$ o Y: t/ \1 Bw. U( c- x. P, V c & B8 a4 \. u' [, Y' v8 X9 Q4 [( f; zCLIMB, Phase of flight where the altitude is, I" M; V% o4 m) y CLIMB LIMIT WEIGHT, Maximum takeoff weight ba& X3 ^; j! p# K9 `& B on a minimum climb gradient with one engine 9 ~1 i9 s& i$ _: Y8 ^inoperative. ; N. l. c( ~: `& @8 w( jC7 j6 M) h) G6 M- h9 Q synchronization. # L5 H- e+ `* n$ b1 V# }7 C电路, 1 u; D1 D+ d- J7 `7 m一个闭合的回路。电流由源头流出,经过各个元件流回) u0 Z; G2 s& A 源头。7 [, [* d: F8 u }: X3 ^) i8 |3 N% P* Q% Y 能在 5 u4 p5 g2 Z* k- L5 s坏的装置。跳开关也可用于人工使系统无效。 . Y) b* @) B& u: ^一号净空道, # K8 F3 W4 w; A4 R6 C6 i2 a是跑道起飞端以外,不含任何刚5 b& B) o/ g# l" O# O0 O5 I) k: Q+ ?二号净空道,( z5 A' P- x# P) U6 I/ G/ h& k& t! ~% A% B4 J" S! x K1 x5 c0 {* @爬升, # Y" [. f; g1 k+ H% I爬升限重, + Z) Y- p: ]1 n+ P' `' `: m( y取决于由一台发动机工作时的最低爬升梯度的最大起 ) v% w) ?& n% G$ u( \5 f飞重量。 7 t4 u7 v9 i" F' v* l7 S% L. m6 i 用于同3 @" W9 [4 ^- \3 [ 英汉对照民用航空词典B OEING 5 T# s# C7 G8 c1 v P! e- ~TECHNICAL DICTIONARY 31 , N) v* Y: s, N, [COALESCER, A device in the water separator for / {8 g) v6 l, m# T) B+ `4 ~. ^ollecting moisture from the cold air. & Y0 O' G5 n* I4 n3 Z, `# Cn antenna with a receiver or transmitter. $ l+ g: G+ C/ q& _0 y* vhe cable has an inner conductor and an outer& V* q* R1 Q5 h/ `; G rounded shield.9 X; [, P8 W# Y% m! Z; M ting one inside the 2 ^' d) A2 e* C1 }4 kther for rotating the low and high pressure5 Q0 @+ I+ I! v ompressors by the low and high pressure engine2 y) J9 z4 T7 U; ?7 f rbines. 3 V" @- A# G7 D2 ^0 b" LOMBUSTION CHAMBER, A part of an engine for2 m) f' p. f( e& k- o urning fuel in the air supplied by the compressor.* q/ Z% @# N5 d0 c& k 置。 ' w& `0 W7 u/ `1 w9 ]射机的电缆。电缆 ) k d; D4 R& }, l- C中心导体和外层的屏蔽所组成。2 P @$ k' \) |. R 两个套在一起旋转的轴。用于使发动机低压和高压涡轮1 }5 n8 K; ~) U& E& @* F4 { 别带动低压和高压压气机。9 [3 h7 h7 J4 _ 烧室,! v) u: A4 ~1 A! d 发动机的一部分。用来使燃油和压气机所提供的空气相+ E1 R8 q; x7 @/ m6 p* Q 合而燃烧。

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发表于 2008-12-24 21:38:35 |只看该作者
c- g/ u; j% {1 k$ l COAXIAL CABLE, An electrical cable usually ( u' Y6 D/ M0 C+ _connecting a# F$ |8 l7 L7 S V T $ ?+ R0 P) {8 n4 x' C( {4 Qg - C2 M6 t0 r# x1 S: F& a, |COAXIAL SHAFT, Two shafts rota - m) u7 C3 U% do- W+ P3 p$ N% C, ] c1 T; `( M x* h" m tu+ Z1 d- a, L7 Q8 u% y. m( A C1 t# M! R% y- s/ G6 {( Z. s2 S( d b% U z2 K6 d" F; j- } 凝聚器, 3 k$ C- U1 m: f3 b水分离器内收集冷空气中水份的装: c/ V6 H/ P* V 同轴电缆,% N7 V6 P1 `6 z; ] 一种通常用来联接天线与接收机或发* c; p2 Z# w9 d4 m W) l/ _& v6 C* U: N6 m) }( q( k- Z! f 同心轴,4 ?4 D4 }" D' u6 G: _+ ~) m& j, `" k: h4 M5 O! R# e4 \" b' z% P( p; |* ?! g1 v) V, l5 N6 Y9 Z& F1 J$ m. f$ S 英汉对照民用航空词典B OEING 3 v% J7 f; A3 b% p$ O' FTECHNICAL DICTIONARY 32! v% F1 R5 u! f2 q Q8 J% j1 ? COMMAND BAR, A flight director pitch or roll comman ! e4 X( G, b, Y; Y0 P% E5 Cindication.! k+ I; a3 C% F% Y& q d! U) f) G0 \" h. N6 G$ T OMPANY ROUTE, A route flown by the airplane ( s7 e/ U! Q x4 Q- `OMPASS LOCATOR, A low power, low or medium1 e8 a" I& S8 y equency (L/MF) radio beacon usually installed in' b. q4 R" Y4 s5 W3 |% J onjunction with the outer or middle marker of an/ r* G2 Z' Z7 z7 n- e tor (LOM), A compass $ t) x1 z8 d, X& Z- A$ {locator installed in conjunction with the outer 6 Y, j3 a6 [. {4 l% d( `2 Ymarker of an instrument landing system. 3 T4 v$ J, q9 g' jss# K8 }+ ^4 W6 l/ @6 R1 M le 6 T: _& k* O9 x" A- E; J8 k' KOMPENSATION, To offset, balance, or counteract.9 {* L) I H+ B M OMPENSATOR, A dual capacitor for changing the fuel3 i$ G/ }8 e8 J1 w @ J aging circuit capacitance due to changes in fuel ' T* Q1 k7 O7 y- Q J! w- m- D1 zensity. 1 E( T% p8 W' H* h/ B+ pOMPOSITE MATERIALS, Non-metallic materials used $ v/ R5 r1 G+ yr airplane construction. Fiberglass, Nomex, Kevlar, p% x8 N8 f( R& _ raphite Epoxy are composite materials.1 b- q* b5 L7 W: \' x: A! l2 I 司航路, ( _1 t/ v9 o! l在飞行管理计算机数据库内由航空公司飞行4 c8 ^* J+ y% S. ~/ M" e* C. x0 W 盘定位台,( p7 W# M' _. h 与仪表着陆进近系统的远距或中距指点标配套安装的 - q9 M# i6 k, @! f" M& d7 H功率、低频、或中频无线电信标装置(低功率NDB台)。 $ |' x( `# j/ X6 g! d# c. U8 Y程序中用来导航。6 o5 O2 ?6 V2 r- B( c 1.远台,. n. R% q3 Z3 s 与仪表着陆进近系统的远指点标配套安装的罗, h( I* H( d5 M! E! G. U 盘信标台(NDB)。* D2 u. c; A( ] 偿,# ^5 [7 ~! E. P6 H5 @ 抵消、平衡、或中和。 9 \0 }1 V, ~ ^" z' v$ O7 |偿器,4 R- l+ u( `( B. `$ x 在燃油计量电路中,用来改变电路上的电容,以与燃 . y. l: w, ], j; J密度改变所引起的电容改变相抗衡的双电容器。 ) V( J2 y9 t" g+ S( ^, k合材料,* | K" k+ q) O7 q 用于飞机制造的非金属材料。如纤维玻璃,Nomex, " L+ o, F3 T' o1 {, Q+ l; }0 D* nevlar及石墨环氧树脂等,都是复合材料。

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发表于 2008-12-24 21:39:01 |只看该作者
C 6 Q7 E7 W% }( i6 ]# [operator that is normally stored in the flight $ A% b" Y& D. D6 V- y' Smanagement computer's data base.+ x9 `9 W4 b! p! O7 s8 I/ H3 F C ! n' D3 \. F- _/ B$ z9 @" C9 E5 [% pfr + Q# N9 x; m& n# e" r1 v. X$ ]1 Tc 4 R5 a1 M* S5 v0 Z. u& V5 d7 k; Finstrument landing system (ILS). It can be used for3 Q( g& W9 P: e* i: n# V" C' q- @ navigation as authorized in the approach procedure. 9 Y2 I. M) J" e1 x5 P0 S) K7 q1. Outer Compass Loca5 ]( Q, N9 J4 g) R: B 2. Middle Compass Locator (LMM), A compa7 @* O) W) @+ T; c locator installed in conjunction with the midd: h% @7 d2 W( N/ G" }( ~% @* U marker of an instrument landing system.* f0 Y. h* `# q3 f, d t8 h C # W! \+ ?1 k& U! p y& ~( Z4 NC& O5 Q+ x" i5 m9 m$ o7 ? g 1 f. f( n% l8 s, T; F" Ld 4 d, v5 e+ a3 S7 y+ K8 c& NC# v* g f: f q0 }! L* ] fo5 y2 Z) E* n9 h5 z$ A4 A g , m n! c& X$ h指令杆," Y X+ K9 [1 e+ U 飞行指引仪俯仰或坡度的指令显示。 ( W' K9 [: @: S) c# ?/ G& `% [% b2 \通常储存 5 N3 y* n4 ?' y- n9 ]的航路。 * {* I. j2 G3 X* D1 L7 j* [8 K4 z$ e o3 ]% [* g/ ~6 e- Q" F 经认可后在进近 0 a9 V: u+ N' m& Q: M: V% z2.中台, 8 j" z' y- w* e! H: P+ e' m与仪表着陆进近系统的中指点标配套安装的罗 5 w1 j, @4 I6 k. U3 h$ n2 U u盘定位台(NDB)。 6 S+ v5 c) X% I7 }# j3 L* x( o5 M+ |* e2 g, c. c0 z/ q$ k8 v9 u! h% l0 u6 e& e' \5 o) g* P# v) }0 z, J0 u) z0 ^' p( _5 f3 q( W K; Y2 z2 d$ D# k- k. L% `* p- o8 C% P 英汉对照民用航空词典B OEING) M1 h4 C/ c: L8 D2 I m6 K: v TECHNICAL DICTIONARY 330 M: L- `% z. t5 e* B by" Z' x& n) d& W* W% l or increasing air. `- [ W1 E+ K1 a ressure and temperature before the air enters the 0 \; r# o5 s2 g1 @. [' ?) h6 B, ^ombustion chamber, Low pressure compressor - front/ ]" {% B4 J7 g ection of compressor, High pressure compressor- rear* S }+ o2 t4 o OMPRESSOR STALL, An event that occurs when2 X, |1 L F/ X. N ere is a complete stoppage of air or reversal of air flow4 m6 r8 }0 V- C8 w, F7 X- H! a COMPRESSOR SURGE, SEE - COMPRESSOR3 D9 l+ m+ `& v STALL COMPUTED AIRSPEED, Indicated airspeed' X2 M8 V( \( N, s6 G corrected for the static source error.$ R- m# R) e4 G! b \ 的机械轴来驱: P7 ~% R+ |- B4 H( |" G o2 \ ,用来增加吸进空气之压力和温度,以供燃烧室使用。 4 U( F% e; n; |4 T* x压压气机—压气机的前段,高压压气机—压气机的后( j5 P/ V* N1 e, a) }4 ^' S% c( n/ P0 M9 A% \; S$ @9 `1 f5 q气机失速, ' N2 F8 s9 [9 @当气流完全停止或通过压气机时气流方向逆反的一种# E% i+ p1 r1 L x7 b 压气机喘振, * R0 ?4 d- C* {1 x1 O7 p见Compressor Stall4 n! }5 H& Z( \* l" ^! | COMPRESSOR, A rotating part of an engine driven3 z5 p* y! F& G( z% [ a mechanical shaft from the turbines f4 x2 P# C" z; N% f' o: ~: } p& J! o) q: m- Q# ~( A: ^ c7 c: m' S7 H$ x s 9 Z) c" f1 b( r) p7 _section of compressor.1 H) Q9 y1 b! n4 h% q1 C0 ? C 6 A; n8 {' N: \4 yth+ S8 e5 ?" I, V$ b) X' h through the compressor. ! E7 P& }' q! I- r压气机, ; C! G+ g0 C" E7 {/ q0 |/ v* x发动机内的一个旋转部件。由与涡轮相连 0 Z6 E; j( t7 G/ {: ~2 x+ C$ b+ n3 T3 O" n1 I; Q: V; ? O: x" Q' o& n x9 n! y/ m! N% x/ U+ S' N1 _' ~5 A0 c* W1 _" c9 C5 R1 Q# D* u d" L现象。 3 }/ l. O w, z9 \6 L9 r- G( l0 P1 }8 A% U, {3 Z计算空速, ( I1 T" |- K; R9 ]$ w7 f2 l; N, L修正了静态源误差后的指示空速。1 I% T9 t3 K- M! H z- q; ?" E* [$ j 英汉对照民用航空词典B OEING j" e; O7 w; q5 G( UTECHNICAL 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 arithmetic5 f$ a0 Y$ l- m: Q% v operations, manipulates data, and makes decisions.- u' l" n0 @! P$ E ditioning" H7 Z! p- k9 T7 B: p the air and the * ^3 m/ ?$ {4 W- N% p# Y# ofrigerant or moisture vapor is changed into a liquid. % \4 B1 r, u+ U8 m1 ?ine) \& O: ~( n5 D6 o$ k! b ONFIGURATION, The position of flight controls,3 `# B; b V. l& n( U9 J% d$ G missing which" j+ B3 t3 O0 l+ A1 B- t may affect the aerodynamic performance of the7 _* A- |6 U f5 N2 ?& b/ [* N s airplane. 0 S% k3 a( v% A: r% K% `* {置。: M# {4 |, r+ T0 Y 中能使热能散发到空气中,以及使冷冻剂或湿 % l! T; o9 y: }, t0 M转变为液体的部件。 2 e) w/ A5 a- {! O8 H连接到飞机结构上。 , Z8 j& z& L1 Z: R态, ; d1 P2 G2 z# E& v/ j定飞行阶段中,飞行操纵面,起落架等的位置。: U, M; s# b8 z$ S% p) \: Q ), 5 l5 z: ~& e/ N- J U1 y) G8 Y受到影响。, h r0 D1 z2 n: ~8 |9 R& f CONDENSER, The component in an air con9 B) A: S1 f4 _/ } system where heat energy is given to3 b& g6 l) p2 _+ ? re1 j, A" r, I. r; P7 [1 | W CONE BOLT, A bolt in the shape of a cone for eng u- @8 ]* b, O. n1 h$ a% A attachment to the airplane structure. ' Y, A1 m7 x7 h6 a- L( r9 e3 WC ; ?' O+ K. v9 N5 F; f& Flanding gear, etc., for a particular phase of flight, e.g., " q# @& q: k. J: Q( HTakeoff Configuration, Landing Configuration, etc. $ P5 u/ J5 n) yCONFIGURATION DEVIATION LIST (CDL), Appendix7 Q; S( o+ Z5 H$ q in the Airplane Flight Manual (AFM) allowing operation `- V+ m; w* V8 ~, U of the airplane with certain airframe parts. a8 o& d# B* d( V3 W1 m$ ^2 c5 i 计算机,+ G9 t( p4 Q( `6 d 能作算数运算,数据操纵,和决策的装 , L% i8 J. H$ r# s: ]$ `- e+ ?2 D: J) @冷凝器, $ r5 c! i2 q+ P空调系统 # L# C4 g. b3 }+ |8 G& O: b' ]; l# Q8 o锥形螺栓, $ z* v* w4 U5 H, I2 h外形是锥形的螺栓,用以将发动机 " z. o! E( e9 Y7 O6 V1 C o; @" c" C* P; ], q$ P在某一特" G7 f. B" @. f 如起飞形态,着陆形态等。2 i: O3 x. ]$ V( P9 U3 b 缺件单(CDL6 i3 G& z- Y* R9 a2 v9 ^ 飞机飞行手册的附录所开列的飞机上某些零件的清单。 1 c% h+ _- P1 L' w$ K$ ~$ f! z在缺少这类零件时,可以飞行但气动性能可能1 q y Z b/ F g9 P% K. n2 F7 _ 英汉对照民用航空词典B OEING ) s n* Z$ B6 Y9 Z' LTECHNICAL 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-mechanical2 W# ?& r7 S N component for changing variable engine gearbox speed: p/ |+ `5 R$ `0 F( V ONTROL AXES, The three axes of the airplane which- [& }) r* t$ p' g/ o+ Z re perpendicular to each other and pass through the , v& [1 X W! C' O7 eenter of gravity of the airplane.2 T% i* ?9 d- A. X. \ Pitch axis - Horizontal or lateral axis, passes through # S! E: S3 q/ rthe airplane from one side to the other - 3 V; c" R: G. r; q- m6 Snose up and nose down control is by , k$ U* i3 H1 G) A3 S" kelevators (and stabilizer for trim)." h9 _, ~/ k" [* |& F* h Roll axis - Longitudinal axis, passes through the6 {! G g2 o; K0 I( { airplane from front to rear - wing up and . J% d6 A: P4 I' d7 s7 ~1 Z7 Y3 d" Ewing down control is by ailerons and/ G1 Z+ ] d1 B. }" k- R flight spoilers.) e4 Q+ S3 ~ l( R) W' L% v Yaw axis - Vertical axis, passes through the0 T$ ^7 w6 `, K: a+ C* z airplane from top to bottom - left and4 Q) N. l s9 c right control is by rudder.+ y z* x! K7 a. b) N3 Z8 ]1 \& l 置, ' a6 y+ v8 @% j; R1 B+ V* V制轴,9 F+ \4 y+ M6 @9 ^. [1 ? 通过飞机重心互相垂直的三个轴。 3 d( C5 s; H9 p% U0 o俯仰轴—又称水平轴或横轴。由飞机的一侧通向另 g$ R2 _: K3 ~' z6 ^+ b$ o侧。飞机绕此轴转动即造成机首的俯与仰 1 } }, Y: o7 J8 i. t俯仰控制是由升降舵来达成的,水平安定 U7 }, K! J3 L. x$ y则为配平之用。) _: D" h; W+ l5 B6 | 横滚轴—又称纵轴。由飞机的前部通向后部。机翼1 A, A8 b4 y% @" a3 i- U" v* a 下运动由副翼和飞行扰流板控制。) f1 i" h5 @1 p$ y& w) _ 偏航轴—又称垂直轴。由机身上方通向下方。飞机 % j; u* E" L6 b" f此轴转动即造成机首之左右运动,此一运8 r* I& ~' D/ x( I- O 由方向舵控制。 / y- b! P* p' i. S: z/ C$ }to constant speed to drive the electrical power. 6 F7 I: x% \+ S" @7 Q. W, E! A! E' rC ! H2 h8 C" ]9 [a ' R% f8 i x' C! B9 E( M4 N- `5 Vc* U! B5 R/ a: R 恒速驱动装. z7 h4 g ^( N& e: r2 j* b$ I 将发动机齿轮箱的可变转速转变为恒速以驱动电源的) [7 c D& N5 c B+ F' H0 Q 液压机械式部件。 * I. T9 P% }4 E s& L5 q7 ]3 j, I, B. b4 ?$ E/ g& ?& h( c7 Q) {2 T. Z# w D1 X6 s% {* w" G, i& ^0 G: L* Y$ i; U# U4 _! k" E: u3 u8 r; w$ g$ A: y2 x+ K/ \" o# A: d# F( D! B6 H% i7 q% D' A1 Z. f5 L2 B! @% ]英汉对照民用航空词典B OEING& K- m, [- k* {. q% T8 O TECHNICAL DICTIONARY 36 2 B. g# w, b) ~CONTROL COLUMN, A mechanical component used ) ~. p/ V$ F. i- M& b5 j0 Yrs " Q6 {4 K( Q: Z; f: ?9 C* S& ond elevators.8 ~- Z) K$ Y4 h8 u; R' M" K9 e ONTROL SURFACE, Moveable panels on wings and ' `; ~$ s. t! o7 Ril for movement of airplane on pitch, roll and yaw axes. * y" ?+ G3 W, H1 W+ ~$ Q; fONTROL TAB, SEE - BALANCE TAB - D! j5 L/ Z. h- C, b, eONTROL AREA, A controlled airspace extending0 U+ H# z. S ]4 y pwards from a specified limit above the earth. - t% t9 q' m+ o, JONTROL ZONE, A controlled airspace extending 9 H& Y" p. ~" _& A& \4 \! _pwards from the surface of the earth to a specified' k% l% }6 ~4 F1 C0 ~$ T pper limit. ! E6 w+ w5 t# O7 his 6 ]5 H2 }7 M" l7 uo IFR flights and to VFR flights in accordance% a: A9 O) } O with the airspace classification./ X: K5 M7 c( T* h2 ?) i- j 机械部1 s* h; ~; s+ {& R; R' v0 x q. n; E B4 O9 H 操纵面, : m& R8 p& V$ [- Y+ ]2 P机翼和机尾上的可动面板,用以操纵飞机俯仰,坡度,/ @# }$ i- {' M$ n3 g& V' M 和偏航运动。 & g& u+ T9 f" C1 U, k6 K操纵片,8 ^1 W/ v; i4 f" C 见“平衡片”Balance Tab

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10#
发表于 2008-12-24 21:40:09 |只看该作者
by the flight crew for operation of ailerons, flight spoile/ S, S, V- V7 D& K8 w a" t: `) }5 |0 L9 D# \# r( e9 B C1 Z) q( U; Q* f/ f1 p0 r3 ^5 e1 V ta ( m1 Y6 z- f" h1 T) U4 MC1 h2 O7 W$ J& Z# i3 d+ Y4 q C& h f) N3 I/ W9 o6 _$ f4 k V% } u! L7 s8 G! ]3 M X/ e C4 `7 _ l9 ?5 M: | A5 D u , d( L* K- [2 Zu1 d0 J0 X3 g2 N9 y! Y/ v CONTROLLED AIRSPACE, An airspace of defined U6 n1 Z! ^' m6 U4 n& b dimensions within which air traffic control service& { h1 y+ b% E8 s: ]) C& Q provided t( q' V5 r) E2 b 驾驶杆,2 J6 T3 O4 M+ {, ] 飞行员用来操纵副翼、飞行扰流板和升降舵的 & [( L, M$ [0 B! v! ]% T# F8 u( k* m1 z' m/ D+ {8 @6 K/ Z4 s* w0 P3 I/ W管制区域,5 R; x8 ?5 r0 n0 g" B 高于地面的指定极限以上的受管制的空域。 $ `. D$ U' e3 V/ A6 C2 r制范围, & j2 I1 [3 c- ?- M由地面到指定的高度以内的受管制的空域。 * `" T! e& G. N+ J: C# u一个范围明确的空域。在该空域内,仪表飞行规则飞行 " \, A- I6 ]) o5 b- z和目视飞行规则飞行有空中交通管制服务。 9 P& a! V! p7 Z: q& q4 h" B" u0 m, A$ _+ T* W% ?2 j受管制空域, 3 c) X! {8 z6 \英汉对照民用航空词典B OEING- X; C' X7 W1 A2 c TECHNICAL DICTIONARY 37 ' Z/ E% O4 l) @$ o4 MCONVERSION, To change into another form. * D8 v$ O" ~( y. X0 X$ A6 Y* qCOORDINATES, The intersection of lines of reference,. |# O: K$ I5 e$ ^. Y W sually expressed in degrees/minutes/tenths of minutes R! l5 J( q* [* D' n9 g7 K0 U. v2 J f latitude and longitude, used to determine position or' N! {$ L9 R8 l: w, F8 n- |% e) u( F% f CO 7 |. y4 ~% T: Q3 c( ~" a6 |% o3 Mdestruction of th & `& X1 K [- L5 o5 o* t0 Mchemical conta6 W% I. k( |8 V; `9 |& d COWL, A remo # o2 a9 ~! Y g7 q/ ]for access to th- o3 M3 l& a4 A% i$ s1 A Fa # h, }! @5 v- j8 W: [$ I# |4 oNose Cowl - Front section of the nacelle for air inlet+ I4 r% y" Q( d# S! z, O" m to the engine. 4 n o: k% w1 C q3 K; X) }9 WSide Cowl - Cover around the sides of the engine.5 {* Y4 i* I$ }6 ^2 y3 `0 k Thrust Reverser Cowl - Cover around the core . z( i0 f/ }* X7 x4 msection. ! _- |! [$ p: Y: ATranslating Cowl -The moveable outer portion of the 3 M+ X* J6 ~, i3 P/ z+ Y5 mthrust reverser cowl which is 2 y+ B+ d6 u/ e. voperated during reverse thrust. ( j4 ^# b. M- X1 ^3 q: P W( ?标, " Y2 Y/ d; r& o" Z: U+ `/ w# D基准线的相交点。一般以经纬度的度/分/十分之一分! ?: ~* l5 ~7 e! Z+ l; z* V 读数来确定位置和方位。( H. z O, W+ _1 c! ~" } 腐蚀 . h7 b& {' u# P! }5 z5 R, E1 _9 l2 _动机外部可拆除的罩子。发动机上的构件必须要取下2 {4 Y9 R- r/ [8 M# ] 流罩后,才能够到。" `8 c4 h$ F6 N3 ]# F: I( }: X, { J' j3 U( u机的短舱的前段。 % S; j2 J/ B/ e3 y. f侧整流罩一发动机两侧的罩子。 ( X. m1 n0 ?3 z反推整流罩一发动机主体外的罩子。 . |$ J' d" e, c( B8 B移动整流罩一反推整流罩外可移动的部份,在反推工/ z# m; l: m, |4 \$ X 作时使用。 N$ B. _. o$ R+ t6 i+ nu' Y" E6 _, w1 l+ |4 U* G2 o! P o8 B( p4 y2 c, ^" G; ?7 y5 @- \ location. ( [9 u: x9 i! U* [4 j4 BRROSION, A chemical action which causes gradual7 ]% b w3 n: w: X* \. u2 s e surface of a metal by oxidation or ; Y5 E( C- @1 V* U- T* B2 m% qmination. , D1 Q& H4 R9 A6 Z F- Lvable cover around the engine sections * |5 \6 w1 x6 s) d C: @e components on the engine. ; Y% p$ t& P& [7 Un Cowl - Cover around the fan section. * h q, `3 o9 c0 Q转换,, ]$ U4 a& Z& V$ o 改换到另一个方式。9 Q4 [) E! j6 W8 g: |1 Y o5 M& B. d) I* R/ h& Q4 o# E/ G A* ^, a o4 p1 R1 M# \0 x" U4 P 氧化或化学污染造成金属表面逐渐破坏的化学反应。 * u( n& L. Z* |' _7 Y发动机整流罩,. Y8 i4 v7 t$ {+ j5 _9 s4 D2 W0 \+ }- ?2 g' }% O! u/ E( c7 L6 f1 n 扇整流罩一风扇外围的罩子。5 H- e9 W5 e: [2 I* G) G) Y6 w 前整流罩一引导空气进人发动( l3 } Z& b0 W) D" V* R0 f# l4 p 英汉对照民用航空词典B OEING! }2 e/ `( X% X TECHNICAL DICTIONARY 38+ U0 B0 d# B) q+ s2 q CPU, SEE - CENTRAL PROCESSING UNIT" ~/ h2 k) |8 L) U2 r& y/ |# A CROSS TRACK, At 90 degrees from the desired track+ c' `- L! E1 K) |: J3 ^) e2 ` f the airplane. For example, cross track distance is the 0 i) X& ?4 S9 l1 cistance from the desired track measured 90 degrees# f& e( R& [- m8 N+ M4 L om the desired track. " G7 P5 l% s6 v4 }- [9 u6 rROSS-CHANNEL, Electrical wire(s) connected from ( f9 d3 A* t# a4 C+ Nne system to another like system, for example, FCC7 z6 ]& r) P, l " to FCC "B". 5 T, s) l$ x, O1 P# X$ q6 Cn adjacent engine or one on the other side.) c- o; M1 F2 P3 Q" i" j l crossfeed ' |3 u$ ?: U4 Eanifold for fuel flow from one side of the airplane to the 7 j: {& {6 I1 @, G: }ther side. - e- p0 D+ C6 T7 J* t6 j% F6 g, [& Cre/ Z0 V$ @" T- o/ m/ g RUISE ALTITUDE, An altitude or flight level $ v& P1 z+ J( ?8 g( d# O% s" D# f) ] o! ^" z/ H0 ~( V# Q( i6 j d ) s; ^7 b4 f- _fr ( i9 r9 c) w2 M' M; q) e. VC + U6 l3 T3 }0 Y4 H" Ro T; v0 t: X3 X "A* t( u! Q- j7 o& r6 g CROSSFEED, An interconnection between fuel 2 X9 T2 k" M: kmanifolds for fuel flow from one side of the airplane to6 X) M3 u# _, _8 T6 U/ g, ~ a 9 m9 x' V s% u9 cCROSSFEED VALVE, A valve in the fue % j6 X# g; e- i- W) \m 2 p6 a* l& s$ L5 e- Co7 s' h8 r6 M" H1 q CRT, SEE - CATHODE RAY TUBE : N+ e( T9 B* Y# I r& d, |CRUISE, Phase of flight where altitude and speed a / v$ P8 f; ^* s: F* H/ h4 Q; gbasically constant. 2 u. C5 e3 w) E9 _# WC3 {1 x [0 f) @8 u! O maintained during enroute level flight. 2 A7 o$ ]4 S9 [$ c% Q中央处理器 7 \9 b4 ]5 w5 i+ u; `$ e见Central Processing Unit. 2 s1 O8 @1 _$ T3 o' v0 V. N交叉航迹(XTK), 1 `1 Z o. i3 u$ H1 m9 l与飞机预计航迹成90°角的航迹。例如,交叉航迹距离1 Z9 M: g, p9 ?0 f9 n 是用与预计航迹成90°角量取的到预计航迹的距离。8 j' f& E; N& x" p3 A 通道跨接, 4 @3 {; ^ j- c4 _" G( b5 w电线由一个系统接到另一个类似系统。例如:由FCC $ w/ H8 V9 b0 E) k4 s, g5 ? @“A”2 R9 M* t8 t( V+ ?6 Y 接到FCC“B”.: l3 p. w$ }) W( b' c 机身另一侧的发动机。 & h/ C1 Y4 b* F _于使燃油从飞机的一侧 5 E# I) @8 z# G! Y0 p向另一侧。 , R3 ]0 e8 G- ]: D见Cathode Ray Tube! R0 N7 K1 P% B0 d9 v3 S 交输,7 b2 I9 I, O" x 燃油支管之间的交连设备。可使燃油从飞机一侧流向邻 % y n5 u, I# h0 o" R" J1 R近的发动机或在6 P& m# H# [' l" ~/ C0 ? 交输活门, . N: S0 y6 j( ?+ a. x/ h6 w% k燃油交输支管内的一个活门。用1 m% }9 ] F3 B) J& J, r( N r& U `: H" o阴极射线管, & C; s" U' P) f. " ]! Q2 e' ~; \9 q# k阶段。 3 Y+ P7 b: B+ k1 L/ R航高度,- {1 K+ V$ z6 k2 x. K 飞行期间,飞机所保持的高度或飞行高+ {) a: w: y' T4 Q/ R4 s0 `' G 巡航,& M8 ?- Z7 b9 s! X/ R X 飞机的高度和速度基本上没有什么变化的飞行 3 A+ d$ k' A3 L/ Z. `# z, u6 b' K' Q' `( _! J8 O在航线上水平 ) ]" U; B. j1 L9 S度层。 6 ^8 k1 W8 X& y: T6 l2 U7 [* ?9 |2 k英汉对照民用航空词典B OEING! Q+ e; A( Y7 p: m: f& e TECHNICAL DICTIONARY 39 # G+ r6 F* `( t% p2 u2 m* z' m1 {4 zCSD, SEE - CONSTANT SPEED DRIVE / P7 ]0 e! `) r3 y1 {7 V4 J0 hCURE, A chemical change which takes place in a resin, ^4 Y% ^5 U% I and fiber based component causing it to solidify.3 r, s) ?! p8 ~# W i3 s8 y9 H CYCLE, A complete series of events that take place6 k# H7 A; f L0 C7 y- K$ ? gularly normally in a continual sequence.# m& c& ^( P: c6 }2 m AMPER, A device for slowing down or limiting- _. w& d i: Z/ B3 d DASHPOT A mechanical damper for slowing down5 V) R; h/ Z9 n* N* l ovement by restricting fluid flow., n3 `+ L& x& D( Z D ' h" I! y/ I z" b1 [# Y, ^; _- yATA BASE, Stored information which is used as the( k/ R3 ^9 z ]$ u# d ba, w) l9 V( E; v- A DATA BUS, A conductor over which digital data is .0 Y7 `: o u# }; } }7 M9 W transmitted." H7 j% @* ^+ v1 {, z DECELERATION, To decrease in velocity. : k& r/ Y* E/ L- z4 K: c装置, # Z7 F% `7 g8 S- u; `rive ; J5 D# O, Y0 y7 Q9 r2 T0 Y. H* }re6 x" J1 m) @0 O& o D" a. V- ?6 D. r6 b/ a% C D ; b) ^. Y5 L& z1 |! k+ W4 B# Amovement. # u* ?1 N [6 f! Zm 4 W) W' ]* P3 d- H9 qATA, Another name for information. , c$ ^) ~* R: q8 ED 4 s. }+ w! K( p/ _! O& R4 v+ zsis for computation.4 u% n# F( a b- g 恒速驱动 % @2 N" o( c- H7 @见Constant Speed D . 9 M& ^% c! v6 S0 o U# X& @" y) G期,% o& p& c. _* T. U; v' K% [9 y. O6 K 不断重复发生的事件的一个完整系列。: z0 H0 B$ i- r. q' o" b# s% g. b* v 尼器, 8 R) v) B" \. ~慢的一种机构。4 ] y2 y8 L2 V+ B* N0 G# X" r$ F- e& z9 L0 R- p: Z用限制液体流动的方法以减慢物体运动的机械式阻6 h/ ~( G# |1 d# |7 @ H5 p, Q$ u) t; S1 u0 L1 x% b% L, _+ b d5 _ z9 N 料的另一名称。0 W% V# ]- T# |# i8 { 据库, ' Q% H& Y% V. A4 {数据总线,+ f& V1 y. ~- h 一条或一对导线,用来传输数字信息的通道。" X7 F: I% j" v" u% m5 o8 d 减速, ( W$ w3 m+ ~- q+ I% m' j速度随时间的递减量。 / o; B8 L) [* f, w6 o固化,% Z' {* k5 m, j, |) s5 A" i 树脂和纤维部件内化学反应使之成为固体的变化过程。7 ^& Z) P; ?# y- {% Z0 F m( _* G3 f+ k# y" V/ e$ e- E" U- ~( |6 i9 G; A, K1 o' q7 [ 用来使运动减& b Q$ q, [# ] 冲器,* `" z c4 x# H7 N) w( O% t 器。& g1 `6 T z, q2 J 据, 2 D% A/ U: n7 V& g4 f' {5 ?# L7 A4 h$ U( T4 O$ s% f+ }! ]$ W/ o" I8 M 储存起来以便在计算时使用的资料。 8 ], n( t4 O# s$ {) H: W% d英汉对照民用航空词典B OEING : d0 h. p) @! k/ b0 {1 i9 u( gTECHNICAL DICTIONARY 407 n& l0 |$ u6 B k* r DECIBEL (db), A unit of gain derived by computing the 6 N- ]' \" d7 }! }) a. Ttio of input power to output power. ( G7 `1 S+ H( I# X* A3 JECISION ALTITUDE/HEIGHT (DA/H), A specified " i# }; C: M8 E- g3 k2 @& ] Ultitude or height (A/H) in the precision approach at3 p" ]& B# v2 C& I hich a missed approach must be initiated if the) ~! @$ z6 Z! h' d+ X+ R8 u ECISION HEIGHT (DH) 1, With respect to the 3 q: H4 m0 v% u$ Z/ k1 bproach or( y: V6 ^4 ]! H% u$ J" L8 H execute a missed approach.( @- m. J% O- w/ R proach to trigger the decision of either2 U$ L- x3 f; a) I! C2 u nding or go-around.+ B* D; N: P: \1 C" H ECOMPRESSION, The loss of internal aircraft air * B2 o# f4 ]3 p3 l) o' mressure. ; B& Y# ] i/ JE-ENERGIZE, To turn off or cause to not operate. ' H. t. i3 ^1 f' srom the tanks $ R* }* |5 j7 H' @5 N: ~2 J2 `) wusing airplane fuel pumps or external suction.1 S0 |3 E, O2 H" ` 算的一个增量单位。分贝 / V5 M& P9 A8 S) ]- D6 L2 d# ~* @* T常表示两个声音信号或电力信号在功率或强度方面的 & o1 t# y, v2 F8 T/ N& t6 c对差别的单位,相当于两个水平的比率的常用对数的十 ' y$ f* k, V5 R3 \7 G: A断高度/高(DA/H),+ E; ?$ L) l- m6 t 在继续进近必需的目视参考没有建立的情况下开始复 . ~0 ~7 s+ ?$ K4 m& z; ?: s- W0 R的精密进近中的一个指定高度或高(A/H)。, ~7 C- X7 c1 G8 i 断高(DH)1, , C, E3 L% _9 c( z C0 ^操纵而论,指在使用仪表着陆系统或精密着陆雷 * W0 z4 o, @5 b生继续着陆还是复飞决定的高。/ k4 r) U/ i& h/ I$ c1 t1 t 飞机失去内部空气压力。% R: b; o! s' s/ ^" I4 O 开,9 k6 `- _5 C% _* q$ R" K8 l8 p7 H 关断或使不工作。- Y* F6 k. o; C8 _$ I) X! x 机的油泵或外部的吸油装置将燃油从燃油箱排 7 x7 Z. `) n* p6 T7 g Q" T出的方法。 7 @- w/ ]( F# Ira & {7 |( f: P' L# Y2 h, c" BD 7 K; |0 C9 ?( }0 L8 U2 Ha, g1 P; B9 y7 k, S4 `7 {# V w , |8 {+ q- M1 @8 Brequired visual reference to continue the approach has ! }+ K4 S8 |2 y$ Z) D* x( jnot been established.. M; Y: o4 F& g D 8 W1 B; O z8 t' E/ w j2 G, [* foperation of aircraft, means the height at which a- U3 R* ]) K( o2 ?8 W decision must be made, during an ILS or PAR 2 d# v* K2 a! j2 v3 Pinstrument approach, to either continue the ap! X$ \" Y% g3 H8 U7 n" _ to $ u# G4 R+ {+ c$ y8 ?DECISION HEIGHT (DH) 2, An altitude used during a5 g+ }: S) p* @4 B' R precision ap) z2 a+ v* D6 Y8 _' N la5 U3 p0 B, X) ? D: u L6 z" p7 U+ ` p * X" V: a7 Q) t& g. eD . [: W, Y# b, c/ \DEFUEL, A method for removing fuel f( I" H- I3 e5 E* `4 E1 [ 分贝,- r" L& n+ H2 P/ N( ~+ d9 u' ^ 以输人与输出功率的比率来推 9 j; I1 L5 O% V) }5 i$ ]+ x2 s4 `/ M) z% ]' {3 E o/ P# r0 F7 L; r6 y2 e( v. i; W3 I$ s) b4 R b2 w7 v+ P; t* ^# A% G2 \4 \- x9 A3 x7 ?7 ~3 S0 x1 O/ F0 ^ o/ y# H x 就飞机" j& B3 {" r0 Q G3 ?( M 达引导进近时,必须要作出的是继续进近,还是中断进场+ ?2 S' B/ o+ X) ?) d 复飞决定时的高。# Y9 P3 e5 T+ {2 x* X' _. Y* z 决断高(DH)2, 9 y" N% f- j5 W. i! |5 ]0 x精密进近时产% a* ^: Y. s4 } 失压,' e1 {* J+ J, `. P# o0 }! d( z2 ~& t排油, 1 U7 p9 p( F) h8 ?( S用飞 N0 h2 @- v3 M4 ^9 H) p 英汉对照民用航空词典B OEING3 r# H" B5 h8 H' j) ]; l TECHNICAL DICTIONARY 417 Q# M9 f! y. P" M DEFUELING VALVE, A valve in the fuel system for 7 O) G& L$ @3 g0 R7 I. `efueling the tanks and for transferring fuel between the' H4 r& V& l8 T9 b% j7 Y! z1 w' q, F E-ICING, Removing ice after it has formed on aircraft.: k5 g. y4 N2 I Change or difference. }& b5 Y" l% I- d6 g1 w8 EEPARTURE CONTROL, A function of an approach0 |, ~4 I' o. @: M ontrol facility providing air traffic control service for 1 _+ y" v; a+ y3 H, Weparting IFR and, under certain conditions, VFR 2 r0 _0 k+ `2 yEMODULATION, The process of retrieving information . G5 Q) E4 X: W9 y1 m& e2 wcarrier voltage. , V# @- P4 a. ~, |" `ation.# B- U7 L; {0 C8 e lic ' t. ~" G: b# s: O# j% ]3 Jcreasing hydraulic reservoir air pressure to 4 O3 Y# g6 E2 N- |" d4 A- s ]6 Tmbient pressure.. a8 L, G7 {3 i 箱排油和在燃油箱之间 " [" n; E+ u# q# Z+ S! I; K& z" ^+ D) g送燃油。3 ]) ^3 H' W7 y; I y 冰, 2 u. {5 x) ^5 W" x( B除去已凝结在飞机上的冰。6 n$ Z# t- K, D 删去或取消。 % D# f& C V3 {量,' M1 Z' P4 l; ]. }* A: W9 { 变化或差异。3 |) d1 R2 v& N& Q 场控制, ; i+ S3 H* \9 B6 h2 c( F% m给用仪表飞行规则离场,和在某种情况下用目视飞行 0 P: ~- {, e8 O" j! D则离场的飞机提供空中交通管制服务的进近管制设施# O; R2 g' `9 h% k* l' d( N z& E6 z调,; i0 B% @4 B0 f2 V/ Y3 ^% E 电压中获得调制电压的处理过程。, [/ J8 H& n0 h$ P P/ S+ J L 环境 2 v/ l+ {" n6 ?' ^% N% ]5 x力相同的活门。) e4 r( S, E3 z- P6 O) a' P* B d. A5 x7 Q* `8 a. Q, { tanks. 2 c" R! O% U" K4 x' `; C1 iD2 j3 Q# ?+ o5 ]5 r: Q% B DELETE, To remove or cancel. ~( f) }9 V: N0 NDELTA, , d4 e% g/ e, x1 m7 ED7 P) [* Y3 D3 p c - D$ W& m; `/ Z2 B. @! dd * F( e1 _0 A6 {* |aircraft.1 P+ I) `8 ^& H8 r( b D 2 s! i3 o( b0 @- h& V, D& O(modulation) voltage from a modulated; v! h+ n5 Q# a5 X& B' E7 l DEMODULATOR, A device or circuit which performs9 C9 y/ H8 G) l0 a5 v8 _9 e the process of demodul & s8 M, `* d; \( D3 T h9 ODEPRESSURIZATION VALVE, A valve in the hydrau0 s2 S9 }, l. {9 I1 h/ P- P) \ system for de - T, D. I$ c9 Q. Q9 D/ Wa( E+ V0 B% A5 W' Q* s 排油活门, & F" [0 O. \, c2 \- z1 p8 e燃油系统中的活门。用以为燃油 + F l9 r" r! u. Y* s+ ^9 [0 g) M) `+ S F0 k+ p* J) X$ s; s n% p/ d8 c& f- r: v8 D& A' V; H 删除,& X, f, d- N: X" y8 f v4 g- h( S1 I J$ ?3 U* F) l7 Z# \. D8 X9 G3 v5 h% A: s1 D4 c' n' v. a$ ]* ^& B: [ 的一种功能 ( V7 m8 X0 q* u1 Y' {% x. g: A, |2 z7 U, h从载波: _5 ]. O- y2 r. C 解调器, 8 }; k V q1 q. e8 T& l$ V9 I完成解调过程的装置或电路。 / q- o e& m: m+ G% Z& h0 H$ u3 W减压阀, " S- _# _9 c4 R" S8 S# O在液压系统中,将液压油箱空气压力减至与周围1 l, B' ^# _6 t. W7 k/ @- ^, V7 q! [ X 英汉对照民用航空词典B OEING8 X- }2 N) K/ s1 B: U/ G TECHNICAL DICTIONARY 428 f. F; r2 ?6 p' h4 [( c( c- W DESCENT, Phase of flight where altitude is decreasing.! B" w/ {/ n& \( _. J8 h ETAILED FLIGHT PLANNING, The calculation of fuel 5 V7 N/ D8 ]9 `nd required for a trip by considering each phase of 3 d9 u* z; i7 Vight (climb, cruise, descent, reserves).( }3 K1 u; X$ v& D. Q al or & E+ n" a; f/ S, S6 e0 XETENT SOLENOID, An electrical solenoid used for0 d/ j" l# x, b% a) A, T t. ( }' U! r: Y( L0 h& j3 \specified course or # R) i- s+ _6 wrocedure. p Z5 z8 J9 O7 Y7 R e. 7 N+ G7 y6 C; Z+ V+ J# H飞行计划, & z: N1 a, S$ q6 Y7 r将航班中的每个阶段(如爬升,巡航,下降,备降)都" ]! \( o! G& e 人考虑,来计算该航班所需要的燃油量。 & T- S: d" ]8 Z4 {4 ?" s9 L2 ]用来感应情况之正常与否的电气装置。* C/ O/ @' ~7 D* S# l 定电磁线圈, - X+ ?! b- M8 o3 L1 [( ~4 ?5 `% d出接通的电磁线圈。 : ?5 _* ~: Z' X# f差,1 n/ Q1 [2 h& j" {2 \( U8 @0 T 与指定的航道或程序之差。. s9 {* v+ c" d9 u& t( D& ` 用气压或液压操作的活门机构中的柔性部件。 : u7 a4 ?5 v. ]8 f0 @D 1 X5 w& t' X. I; n1 `$ _a ' F& O7 O1 I! m) u- @( Tfl ) L9 x h* j; T" O6 w! l+ FDETECTOR, An electrical device for sensing norm+ P' E- c% l% F' P1 K9 r abnormal conditions. . U. J& E8 A! W2 s4 d3 ^ e$ kD # Y3 P4 r( P2 j4 Ccontrolling the engagement of the actuator outpu 6 ]: X" D5 s1 _8 ^4 ADEVIATION, To change from a7 o5 o- S& ^' ~) \ p3 ~, i% k" ~7 \7 e DIAPHRAGM, A flexible part for operating a valve" F+ E1 V& x0 k mechanism by pressur) T0 [, u [% M" u 下降,! N3 C# z4 C" E v 飞机高度不断降低的飞行阶段。( V8 Z) _2 D, X1 u8 K6 z0 D% \ 详细: } k. d' Y" }. ~- [3 K$ u# J0 e) } 探测器, 9 {' ?% C5 q: L% W; e7 t; H7 }% L( B7 N2 ^ M9 k2 T用于控制作动器输 W7 v/ x) ~" D/ g, }* u" A% o4 w6 }- v; b% [( h8 ]/ b" X隔膜,, }% Y* T3 x: R, | 英汉对照民用航空词典B OEING ! G8 h+ Z V, Y; |+ _" B1 pTECHNICAL DICTIONARY 43 : l, m Y, d. `9 p1 nDIELECTRIC, A material which does not conduct ( u- a9 a1 }+ C3 `7 r& _/ w$ |7 qelectricity and used between the plates of a capacitor . |1 X$ r0 @5 j& O# N: `(condenser). H5 E+ w2 C& qnother pressure in the same system, measured in 9 `! p" u) @3 H Dounds per square inch differential (psid). $ |; p: w5 w7 E: I$ cIFFUSER, A part of an engine between the4 E9 t/ y, d, [* n ompressor and combustion chamber for reducing the & J0 n" B; \, [+ rair pressure.& N4 i2 @9 @: p* T igh0 P" s9 N0 ?8 N8 x. Q: b pulses.- V7 x% S% E' ~4 t2 u$ C3 e) X ignal that is a close approximation of the original3 G: T+ U* J% q% u ignal.$ D: h3 x1 x: k. T1 b IHEDRAL, The angle between the wing reference( c! C+ X0 [6 ` lane and water line. : a0 n- ^6 d G y: `, s, |的压力,以每平方英寸 7 q: \5 C( ^" U少磅压差计算(psid)。 2 p. E# P. J! Z ?- X% t$ ]散器,, W; t$ a7 n6 v g$ { 发动机内压气机和燃烧室间的一个部件,用来降低空 / a$ U0 M8 L' S$ k/ n增高空气压力。 ! q4 k, l" J6 Z换, / l2 U0 E) ^* ^/ u: R" L& @的连续可, w1 t" C0 ?1 [0 ?& [/ ~& a( } (模拟)信号的处理过程。 ! ^- [+ C5 t: Y; o, A反角, 8 a9 P, P# ?: F' z机翼基准面与水线之间的夹角。 7 i' F3 g5 ]4 v2 \. u {, oDIFFERENTIAL PRESSURE, Pressure relative to+ D K6 w% |, ?+ T' ^5 f7 v: X+ K$ v: s a& z; H2 B3 p/ g& g( ~% ~1 {4 D% d p2 b; m9 u1 G1 H- K4 d3 J4 F$ v9 j D1 o& R t0 [: \3 ?7 P3 U c2 w* h; q* G( s airflow speed and increasing the, u$ R) q& Y4 P5 G! M: K# L DIGITAL, Digital refers to a signal whose amplitude 7 w4 _) y; M1 a& d; Yremains constant for a finite period of time. Digital$ u' R1 I+ O$ E6 F; u signals are commonly represented as a series of h 2 @& a2 u' e3 d' i: @! f! ]and low 7 R5 C+ w# ?. d4 H$ N: P. kDIGITAL-TO-ANALOG, The process of converting a 7 q, P5 O8 v# r8 _0 Rdigital signal (binary) to a continuously variable (analog) 4 S& W+ c3 S i: is 7 [. p7 Z1 @3 M/ Z, i- a3 L) }s, B9 [& p! q( }# j D/ l+ g. C- {6 v# b$ x! h p* m" J5 c4 H8 d! X 电介质, - U+ Q$ m( r, Z一种用于电容器板之间的不导电的材料。. J9 e1 \9 c" _+ ] 压差, / a+ D( A2 J& l相对于同一系统内另一个压力( I8 w+ a+ N+ l$ F0 o2 U) A/ I& i3 W* z% ]: P: [- R" @, {* [) E4 _& i/ ^+ a( {7 @气流速并 2 N* I- j; n T0 w/ n$ {! x数字式, 0 I1 ~& V9 p8 n2 V- T指一种信号。该信号在一定的时间内,振幅保持不变。$ k/ b9 {$ |2 \ N! W5 P 通常由一系列的高低脉冲表示。 * d+ `7 D A1 i! Q5 N& z1 n! h数一模转4 a1 u$ I! B, U 将数字信号(二进制)转换成与原信号相似$ I0 B( ^% v8 H% z. @# d1 ^4 e( k; z/ w0 T$ q: z) J# C7 v3 m) |0 z 英汉对照民用航空词典B OEING 0 [; z& o6 Y4 ]$ B/ [ [; BTECHNICAL DICTIONARY 44 , G& c: j3 ^( _: e( X& m5 c9 uDILUTER DEMAND REGULATOR, A component in the + X) @9 J2 w0 V& d/ F1 ccrew oxygen system which mixes air and oxygen and : L! P+ `7 Q6 T! B" S9 Z# Iupplies constant oxygen pressure even if there are- i; Y" {4 m+ x* w# r hanges in ambient cockpit pressure. 9 K& Y0 X O; H2 a1 S- OIM, A word value of light. For light control devices - dim 8 B4 o6 Y1 x, ]3 A* E% Uthe opposite of bright. $ I7 ]! V* P9 }- K) M2 Q4 r! jIODE, A device which allows electronic current to flow- }$ G3 S$ H& V8 D* O5 H$ V0 n! L only one direction ) J1 f# z7 [4 b& f7 Tuid in a reservoir.7 e0 ~5 f6 k; s DIRECT, Straight line flight between two navigational a i: D# ~( z4 Q( G/ F aids, fixes, points or any combination thereof. When q0 ^2 i, A2 Q/ o0 |5 R* G( ]& G used by pilots in describing off-airway routes, points ! E# R P1 w) a' Z; z7 Udefining direct route segments become compulsory" c$ X# L0 T2 Z6 ?, l. L/ s reporting points unless the aircraft is under radar' J- \* s4 ]: u7 ?& L0 V control. 7 l, C G. r) v' P0 O5 G8 W( z7 e1 ]节器, - [$ T7 G+ k' h: j将空气和氧气混合, : C% S! R* q9 w1 j使驾驶舱环境压力改变,它也能提供恒定的氧气压力。0 v- {& s+ z: ]2 ?- D; D1 s- p- e, T; b5 H! B5 B! m7 w. x7 H) [ 一个形容光线亮度的词。对于灯光控制装置,暗的反4 R) F Q- O1 M 词是亮。 ' C4 P' t0 c+ H# n+ Y$ l/ J0 m极管, & F! l% P, L3 I( y8 I( |/ w& V只允许电流向一个方向流动的电子装置。0 ~& ^% z4 c7 C 器内液体的量。' e, `. W( C9 O, R" b0 \ 直飞, 7 t. n: c! Y9 l' N$ A" _+ T两个导航台,定位点,导航点,或任何的组合之间的直 % c7 A, n9 ^" e% s线飞行。在被飞行员用于描述偏置航路时,除了在雷达控$ e$ X$ j1 N" d9 c: V# d 制的情况下,确定直线航段的导航点成为必报点。 . V, l8 i0 S4 a) P+ os- N! ^! K% y) z1 r c8 x$ `- D% b8 K: J& I D8 l4 S* f! A+ y; r is8 Q5 r$ u8 u) I) P1 _1 f D* x9 j. t- i& R$ V; G7 L in 6 ~& c* o7 L. VDIPSTICK, A calibrated rod or stick for measuring a 5 x. E; K+ t0 ^' G+ {quantity of fl 0 L6 j- Y; Y; t3 w8 T稀释氧调6 ?' `: L( P; C8 t 驾驶舱氧气系统中的一个部件,它 , X% o. S0 r2 E# Q) O6 u2 W8 }& p3 ~" s, \, R! `0 T- C4 i& B W3 c0 ?' j& N3 d1 \4 J' R# y* R6 L2 H3 F; ]2 r6 _) k# E) A$ C 量尺,1 s9 _1 w d* P! n# g 校准过的棒或尺,用于测定蓄液" M6 f) K* F# [: ?0 J3 A7 L; x2 ?/ s 英汉对照民用航空词典B OEING 3 H' U# h: J4 B. ITECHNICAL DICTIONARY 45

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