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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 ) o( Z% l. z8 w) u1 O民用航空词典 3 d6 v |$ n2 K; B/ t2 Z) S波音商用飞机集团 ) |4 `6 X9 p7 v& CBOEING COMMERCIAL AIRPLANE GROUP9 e+ G+ m2 o" P. c( s4 g 英汉对照民用航空词典B OEING ! j* w7 s( v# kTECHNICAL DICTIONARY 1 , S4 E1 Y' ^5 ]A2 ?% l2 l; K2 ]8 A2 ?+ j6 }4 Q ABEAM (ABM), Beside: An aircraft is abeam a station 6 Y5 e' o" M5 l& G# J6 Awhen that station is 90° to the right or left of the track of5 O7 @# A" I# y( d the aircraft. % b) O* s1 o d, E! WABSOLUTE ALTITUDE, The actual distance the aircraft# `& s3 V( e( a( d7 u1 \$ Q" w is above the ground.) J! y$ Y X5 d- X4 G ABSOLUTE PRESSURE, Pressure of a liquid or gas 7 ~" b0 a {! E) Z5 s. ?6 Emeasured relative to a vacuum.0 S1 L6 n. M- Y ACARS, SEE - AIRCRAFT (OR ARINC) REPORTING! ^0 U ^/ r2 G, T- r ADDRESSING AND COMMUNICATION SYSTEM9 V6 K a1 ^# Z8 w2 k2 f ACCELERATION, The rate of change in velocity with7 T1 @ k$ n5 N* i6 y/ H% t respect to time. . }0 y% @/ a ?8 C" }ACCESSORY GEARBOX, A part of the engine, : j& n1 E- b& _7 E) t- a' Qmechanically driven by a compressor or an angle, i! L$ j8 ^1 l2 n gearbox, for driving components necessary for engine " \9 L$ ~/ V# l" s* s) S正切,- M3 T9 G, h) \" E8 d" K and airplane operations.6 T7 y% a$ `6 u2 F' w; x: k7 T, B, P 当电台在飞机左侧或右侧方与航迹成90 度时,飞机正6 I. y$ r4 O# e; k0 ] 切电台。 , h3 \) } ?7 n" U( Q绝对高度,& x+ u0 x$ e8 k' o! v- } 飞机离地面的实际距离。+ @' |1 r, |0 c0 t4 ] 绝对压力, , }% f7 J% K2 ]$ n相对于真空(无压力)测得的液体或气体的压力。 8 m3 e! M( x7 g( x' t+ m8 l飞机通信寻址和报告系统,! y3 r: q) f2 w) ` 见Aircraft(or ARINC)Reporting Addressing and ' `2 F, j' O6 p' M3 X7 ^# X/ YCommunication System. , e/ q' n6 Z/ w+ _加速度,4 g( J! P \- F% \' B 随时间变化的速度改变率。 . v; J6 f# ]7 r* {) T6 X6 A附件齿轮箱,; J9 i5 U+ f# U O4 N+ n D- j1 q0 Z 发动机的一部份,由压气机或伞齿轮箱带动,用来驱动 6 Q5 z$ n- d0 }" t, e一些使发动机和飞机工作的部件 % p* n1 z& x0 n英汉对照民用航空词典B OEING" @" X) i' y) [) z5 q7 L TECHNICAL DICTIONARY 2 . V0 l! b! \" l* [2 ]% ]ACCUMULATOR (NO. 1), A container with hydraulic) }# l' M2 G5 g q4 t7 _/ p ts when normal hydraulic supply is not4 h4 I- ~! M: |2 O: G, a vailable.+ ^. C+ ^" K# _' `7 f1 e CCUMULATOR (NO. 2), In a computer, a special: ~# G9 F" M* v; I7 D1 V torage register associated with the arithmetic logic unit, 5 `) l8 b$ q# s/ eolding the results of a computation or data3 g1 y" z$ L/ a# ?$ s& N8 u ACTUATOR, A mechanical device operated electrically,* D# T3 r3 L4 {" V4 G6 h7 K4 K7 k hydraulically, pneumatically or mechanically for 7 s/ w. |+ U9 a' q, A; ltransmitting motion between components.! ]0 A+ l; g/ N r9 Y ADC, SEE - AIR DATA COMPUTER A( ^. F' R& K( O+ j" BADF, SEE - AUTOMATIC DIRECTION FINDER , \" ~% F8 R: Q; ZADI, Attitude Direction Indicator, An electronic display of5 |0 p3 N3 U" H' ^0 [ airplane attitude information in pitch and roll.8 F) d2 Q. v. R9 [: V$ ~: H 蓄压器(NO.1), " z) h- ], P: h: @; k含有靠干燥空气或氮气增压的液压油的容器。当没有正 + ~: y( ]- P7 ?5 n& }; R常的液压源可用时,该容器可用以驱动部件。5 B3 y+ V2 z0 r 存储器(NO.2), 8 {) h4 a4 j. C' W8 x# T计算机中,一种与算术逻辑组件有关系的特别存储寄存. t+ H* t' T! A! k! ? 器,用来存放运算结果或数据传输。 - W/ D" o# E4 a- c% a; K飞机状态监控系统, ; S1 v% l0 x1 F见Aircraft Condition Monitoring System 9 _' U _& y5 t' Ifluid pressurized by dry air or nitrogen for operation of & k3 k% E b1 J% q6 tcomponen. u3 y. g- K ]+ p+ u" x: @" c a " r0 P. D( G, [ OA : s# C. U9 ^& Q% \& U. Ls o _% Y, O( t1 h4 y4 aused for h 9 h( ?% y/ o6 i7 z s+ Dtransfer. , T/ S. x @, q7 d: @+ uACMS, SEE - AIRCRAFT CONDITION MONITORING ! l" [8 N7 v7 g2 D9 }2 ~SYSTEM .6 \5 i8 I" Z; q! Q 作动筒,6 O, z; P @$ y) x2 h 由电,液压,气源或机械驱动的机械装置,用于传送部 , Z% k% Q& N7 _, o; k( P件之间的运动。1 s) g; [+ \) { 大气数据计算机,. D% B- W* G$ k+ x- _) R+ @ 见Air Data Computer. $ ~$ j2 ~! i8 R- ?自动定向仪, & _! F$ H/ d1 r见Automatic Direction Finder. $ d# o t M& B* f3 K% r姿态指引仪,7 |9 L2 X9 d0 z" ]% _ 用来显示飞机的俯仰姿态和坡度的电子显示。 1 F0 C+ ^2 i2 ]. h8 z8 T+ ~英汉对照民用航空词典B OEING & W) G$ Z% \$ ?TECHNICAL DICTIONARY 3 : c5 o, l3 B" X8 g) Y* n# OAERONAUTICAL RADIO INCORPORATED, ARINC is7 w: \" G2 | Q1 c' v( Z , 1 y0 d* w- O% [4 I! n; Znufacturers, and foreign flag airlines. ARINC 0 T0 K( F, [+ revelops and publishes standards for electronic + A0 ~; L) w7 v0 ^/ {# m+ Qquipment and systems. * P' j3 ]/ A# ^4 I4 D. f: nGILITY TUNING, The capability of the DME to d, }! ?0 ^) _% `0 |9 l6 K* F9 K lternately tune between two different DME stations in 0 K( q' @3 G- u7 Prder to get two distance readings from one ' w( h$ U I: V& s& i, O( |terrogator.0 T8 b( _: u8 S ge3 M7 W% M, @9 z% X$ h, F ILERON FORCE LIMITER, An electro-mechanical $ s c9 _. A3 W8 ?IR CLEANER, A component in the pneumatic system4 R7 X* W8 S9 H) ]4 @ y upply to the air : ^) y/ J8 I0 ^ X0 j, a9 Xonditioning system. + k. x' Q, c6 F6 X订并出版 ( q2 ^1 |; e- ]1 `: _子设备和系统的规范。 6 H& s8 |3 c) j; O! [) H. S4 w, Z快速调谐,1 _; @: C; l9 r: n% s7 I0 d 机载DME通过交替调谐两部地面DME电台以测得来自 4 [( ^6 Y# s. f# K& x; G4 m同一台询问机的两个距离数据的能力。 9 N I, \7 }1 f: w4 B9 R翼操纵力限制器,: w- a5 O4 M( l3 s, P8 r" h5 c 装置。在自动驾驶工作期间,用来限制驾驶盘* j0 m% P% `) Y 气清洁器,0 g- t" \$ ?7 y' x' C3 d 部件。用于去除供空调系统使用的发 ) @8 N$ P4 c# e, W% {a corporation whose principal stockholders are United & G% w! _* Z& x9 o, H5 V+ PStates scheduled airlines, air transport companies + ^* x& Q3 ?- v* P: \( \aircraft ma. Z# J. A# R4 Z& a! r/ T d, Y2 f% t8 e/ R. d9 W. d# ^. d+ T e * k, H8 H! U" G9 `# W/ u( jA 7 t5 D2 X3 K' p' H; p, l" `, ja: j I' n3 j4 n. O! Q o' }4 g- I, ?- {+ K in 9 b1 ^ [. `, a0 p2 a# d" S0 y5 h$ g1 vAILERON, A hinged moveable part on the trailing ed , N3 z3 G' x1 C6 Q! ]of each wing for airplane roll (wing up and wing down) # E7 r: R" V. ? H. scontrol. ' G( g! e6 U+ F$ a% W, A/ |; JA , z7 y- o/ L9 K, A- P, p2 Pdevice for limiting the control wheel movement by the, v) h7 G: y* w2 D& n. J2 d; G/ \7 z autopilot during autopilot operation.0 n7 p( ^/ R, r5 B8 `% o, B A , f6 G3 Z! }* w- R0 ifor removing dirt from the engine air s " M' a- b# s e3 A7 Q, Xc8 L+ W" W# F2 [* i% Z( g4 W 航空无线电公司,7 v# h+ `+ k$ @9 X) F2 p' k* p 主要股东为美国定期的航空公司、航空运输公司、飞机 / [& O+ F. b! n制造厂和外国领队航空公司的组织。其目的是制 ' b3 t: Q1 f- [% r: k* C' m8 X( O1 d) }4 e% ?1 D) x副翼, ! W p0 j2 w" P9 H4 h. D铰连在每个机翼后缘的可动部件,用于控制飞机的滚转 , O; I9 n* l- X% E(机翼向上和向下)。 6 b1 Q) R5 I& M+ {, G6 K$ D/ Z& E: P7 D 一种机电 5 g2 c& K$ v& Z2 q的动作量。' b1 p' w! r' ?; W- ^: {- R: o! m$ [1 o" G0 ~, F: N% e气源系统里的一个0 L# V( i! A( [. r2 I) c) I; A J$ s 动机引气中的灰尘。 & }& _0 @9 j7 I! B" K英汉对照民用航空词典B OEING E9 y5 v8 ^9 U/ W TECHNICAL DICTIONARY 4 # C- z8 f$ p) e# L5 Z/ aAIRPORT ELEVATION/FIELD ELEVATION, The, u1 c$ x; J/ V8 |2 J highest point of an airport's usable runways measured; a4 C, n G, P4 l in feet from mean sea level. In a few countries, the0 K$ U; |! }0 \% M& V- @, N airport elevation is determined at the airport reference 6 n8 }) G$ s( @" ~5 @! t: {' Opoint.' ]( W- M7 Y2 W' e AIR ROUTE TRAFFIC CONTROL CENTER (ARTCC), 4 l: A2 D2 L1 c! u8 mervice # z* O" E2 z4 E# `( Nase of5 g7 z. h S% a T us flow of air traffic.9 y3 j8 K# S3 W6 p0 ?" @7 y IR CYCLE MACHINE, A compressor and turbine on a & h: V& d( r- n& n, S. s' kommon shaft for cooling the air in an air conditioning5 U- R; I1 F7 M. P% J ystem. The air is cooled by expansion from high to low9 ~& _9 V1 d* J, s! n6 I ressure across the turbine. The compressor is driven( A7 Y; @$ q/ j$ r; F y the turbine. : d: c' j& c! Z6 m `7 h! n中航路交通管制中心(ARTCC), " r. o, G4 |% A- i# D域范围内使用仪表飞行规则飞行的飞机提 $ }$ m# }, J) ?# l! f9 O1 D$ k管制(ATC),5 [! w% ^1 J9 o3 e O 涡轮冷却器,* _4 \1 `- X* e( g 是装在同一的压气机和涡轮,用于冷却空调系" G. k( f$ \& k2 j U6 a 统中的空气。气经压气机压缩后,由热交换器移去热量,& J, |0 ~4 T( @6 v% |$ g( @, ]- \ 然后经过涡轮令涡轮带动压气机。通过涡轮之空气,温 ; j/ R; J# y; W5 k! T' u; w度下降。 " Y& p" M, h% F' w4 w$ vA facility established to provide air traffic control s2 g' P5 V0 }7 U" W' w6 ^- ` to aircraft operating on IFR flight plans within controlled) I0 K/ c n. ~: U5 S- f airspace and principally during the enroute ph + {5 o% L, i8 l+ Uflight.2 ^ C$ j+ @0 H/ [# n3 G. ~1 ?0 i AIR TRAFFIC CONTROL (ATC), A service operated by ( \5 P8 D! B' q3 _* l1 lappropriate authority to promote the safe, orderly and3 G) l9 A$ s+ d& a% V expeditio: H# _* J8 f& s6 g; E. U6 O- }' V) ] A 3 S' g3 i- U' a4 W9 }# gc0 g* X& f8 Z! T6 K- B s + I& v8 z- j3 B# ~p; A5 I/ p. r- h, }2 d# E b 6 |1 O: T; _* v, @0 c2 N+ O* v机场标高, 4 e4 M% y/ C1 _; J( u$ i) A) I指海平面与机场可用跑道最高点之间的距离,单位是英/ Q% h! i5 b3 z# H 尺。有几个国家的机场标高是由机场基准点而决定的。, B2 P* K$ u% h' H* i. b. W0 p1 W2 s给在控制空$ [5 s2 L! X! |5 | 供空中交通管制服务的站台。- S. J5 m& t8 ~! g1 @: J 空中交通, Z) n3 ^* c. |: i. x 由有关当局管理,旨在促进安全,秩序,和效率的空中' }7 H7 k- }9 k3 _. B7 b 交通服务。 * T$ _9 n+ t: ?根转轴上 4 E/ S% I! o2 c7 |3 |! [" a& }, W+ {: E# y6 ?. A6 u6 v6 T7 [" S8 c3 ~ 英汉对照民用航空词典B OEING ( `0 I- M3 h+ O5 m; U9 ]8 jTECHNICAL 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 1 T7 P- }4 G/ e% X6 o& ~% w: Q& Fdata information, such as altitude and airspeed, based) [* }4 ?2 E8 w4 L! w. }( }5 j on pressure and temperature measurements.' I8 S: E/ W4 Z m5 t% o' k es air ( S! F v2 }+ L8 x8 ?: QIR TRAFFIC CONTROL, A system comprised of / C# U3 Q$ M* b3 H; \& R8 O! g0 Rround and airborne components used to identify, track2 D4 v( t/ ^$ T ^! `: d: Q% F OUND SENSOR, An electrical device operated , t/ W+ S* u6 A3 i' m3 Y. [y the landing gear, which transmits on ground/in air. W5 D+ G* v$ X6 {- n4 q6 F% b formation for system operation in flight or on the . Q1 p. K0 r% {" {& A8 Q" c3 nround.6 H4 R4 r& {! X$ A IRBORNE VIBRATION MONITOR, The AVM takes( H, Q6 m& C& ~% H. v7 a- G8 e/ |1 } e signal from the engine mounted accelerometer and - Z2 V* L T; X- W6 D& P" G: X, }2 balculates the vibration on that engine.; h6 t# P' n% @ corridor equipped with radio navigation. O- I1 l3 z9 G: g/ n) u$ O aids. 5 O) s% l- @ o$ I* C. C% oAIRCRAFT (or ARINC) COMMUNICATIONS / o! i& Y( R. o% \5 nADDRESSING AND REPORTING SYSTEM, An 0 R# y1 S5 e! g; `addressable digital data link system which permits the7 i5 y( l% O, O0 j exchange of data and messages between an aircraft 9 | S) J" P& kand a ground-based operations center over a radio ) N! A* S/ ^8 w Fnetwork. " [( A, w! t6 eAIRCRAFT CONDITION MONITORING SYSTEM, A: K9 m8 ]0 O! _- }. b system of sensors and recorders to monitor various* X4 X1 c6 J3 e' n, D) G( `. ?/ J airplane systems' performance and status.+ n9 S+ X/ m* B' X& J/ a 机, ) q* l i1 |' j! K/ F, F) `( B中交通管制, 1 H% W8 f2 b: [& ^3 w* u一个由地面设备和机载设备组成的系统。用来对飞机进1 S! R8 Z6 q8 ^9 B# L 地传感器, * z0 B0 j. u' M0 C$ {" G& `一个由起落架操作的电气装置。用于给空中或地面的飞1 E' {$ V' i" U4 B5 _# t 系统运作传输地面/空中信息。(有些系统只能在地面 ! C) ]5 N7 P3 z) A, n% s! n1 `& r用)4 d+ ] i: M$ Q, W9 M 载振动监测器(AVM), 4 J9 [4 Y" |' S# t+ W$ L. [: `AVM从装在发动机上的加速器取得信号后计算出该发 ( f& D! n/ L9 q& ?机上的振动。# P8 a' z$ `9 i. _; l 式建立的控制区域,内有无线电导航设备。 : c4 C# H f5 J9 [飞机通讯寻址和报告系统,7 B9 q, B. m- b- }, A7 J' G 有种可寻址的数据通讯系统。利用该系统可使飞机与地 H6 m& [: v) T' G+ h# w 面操作中心通过无线电网络进行数据和信息的交换。 9 T4 K* g6 d5 n W2 v( ~飞机状态监控系统, 1 y* l0 Z0 H9 \# L一个利用传感器和记录仪对各种飞机系统的性能以及 / f. a d, v7 L状态进行监控的系统。 5 ?4 t. H; a- N' x( Q0 b2 FA ( U! J0 X7 G9 w* Q7 \' B4 lg, o# G. x1 k8 i: A6 F and locate aircraft. . [. q* `/ \9 [" h: U* d. w* N1 ^: XAIR/GR * K; m' W5 T1 q2 F. z4 r) T7 i. jb8 Y' M7 t) Z, s in + p# T: _% y- [* B$ Fg 7 ]6 G, Q% @2 YA 0 k. D% P1 E# J& Xth8 V8 s9 E4 ^4 O; U. Y2 y: G c; W! K, q$ \$ S2 q, F' \ AIR WAY, A control area or portion thereof established r, ?4 e& m& lin the form of a 1 m% u( \; l* @# Q5 g# @大气数据计算 9 F7 U1 V v' ]根据量取压力和温度而产生大气数据资料(高度、空速- i- X7 J0 [/ G0 T! X: ?4 Q 等)的计算机。! ?. Q( k: {$ G: x* b7 y7 f: w% \* h9 t, A3 m 行识别,跟踪和定位。 / `5 @' D' M3 h& E& l( r& d2 r) Y) S% |, w9 O0 D# C$ U' a7 \使 + N. A7 R0 v9 }1 z0 z, p4 v$ M7 h+ C2 j. g" R, @7 p$ X$ A Z* m x航线, ' D9 N7 k0 A3 P5 c以走廊形 ) |0 u( Y( ~3 M; p2 W5 G( |英汉对照民用航空词典B OEING / j: S6 ]. k. r. G3 N2 X& jTECHNICAL DICTIONARY 6 8 i) M* S( s: I, s7 T% ?. u4 _AIRFOIL, A surface designed to obtain a useful reaction, . A" t$ I k) t0 c7 \& Nsuch as lift, from the air through which it moves. Wings,9 q% ]& ^0 S0 M8 H5 n$ Z stabilizers and control surfaces are airfoils." H/ |' m R9 R0 c5 I AIRSPEED (IDS, TDS), The speed of the airplane + H+ E+ M8 K& Z# Z7 Zrough the air. 2 x! \6 n# E1 e2 |D INDEX, An adjustable pointer on the j/ S% I: G0 Kirspeed indicator.$ C& t9 {7 p( X: P% v" i% K and legal ability4 P8 p Z& n# i fly.$ K2 G% K& k4 s' P/ j$ F. u) L4 _ m, for example, the procedure for finding the 6 K: N( K) s( l" [4 [quare root of a number. # u# n w! `2 I8 _4 F. |y$ z" ?, W; o8 a1 r( X( {" ~$ u re, wind,6 j- ?5 {3 a' O( u( X K8 _ and aircraft flap setting.( d6 U: @ H# Z4 `! E 是翼面。 * N7 R+ s$ L6 s9 t' K% w速,# u$ m4 [8 }( H4 v8 ?% W9 T) U 飞机在空气中运动的速度。 2 p( V# ^) |( h1 _2 y3 X1 G$ C/ h+ F. Y 在空速表上可以调整的指针。5 D3 _) Q9 b1 @, O' x 机械飞行能力、和合法性的飞机状态。 % p! m; S6 A; A% L+ U$ ^" ]- Q一步一步的解题方法。例如,计算一个数的平方根的步 ; T: g$ q9 U! n7 r2 U6 A2 O; j' ~& I) E# @# H" o5 Q. A2 _0 F/ c: N& s8 T& ^/ v( ]* h1 Y 资料的法定文件。 & h7 }8 _0 o+ y, z$ I0 r翼位置成函数关系。 9 ]8 d. R' l& kth% o* e8 W' g5 }0 F* T AIRSPEE" _" V, T5 a* t1 B a. y" L- P- X; B; w* U1 _ AIRWORTHINESS, The condition of the aircraft with' P' D/ n+ O' E- [: Y& k respect to its aerodynamic, mechanical,$ G$ n5 z. d- V; c; s to2 c/ @& A, z3 B, v ALGORITHM, A step-by-step procedure for solving a ' q* A: Z* l" G9 L" k1 Iproble ^; z7 I0 f+ E; b) m# `s / p1 W& w6 \7 _AIRPLANE FLIGHT MANUAL (AFM), The legal ( T; A% K/ @8 y0 ?% M0 {2 q2 b" Cdocument containing performance and operating limits,3 q: p4 n" `7 e( o' w% w' N operating procedures, and takeoff and landing* t c, o/ f$ ?. E performance.: f/ k% \3 x& w AIRPORT ANALYSIS, A comprehensive set of takeoff8 D( Y7 F; |$ @( d. Z8 J weight limitations for a given airport runway, generall 9 p" k! u, b0 z. f$ dpresented as a function of airport temperatu# v/ A& o* ^" o& o1 s' o: z: J 翼面, # o& i6 J) e& |8 u0 K6 j0 e用以从气流中获得反作用力(如升力)的表面。机翼,0 X; l4 }4 f* s; c+ A2 u2 A1 E 安定面和操纵面都 ) L) i: g. G9 n: Q$ l! E+ r3 s1 K空速指标 3 Z7 r: M5 T2 {, ^+ h1 q- S适航性, , Y* n1 l7 m7 ]3 \有关气动能力、 f) X, J/ `' h; Q7 Z) K2 Z演算法,4 }, R; D; k9 S2 V( ]* t$ _8 @. K" H/ p, G+ w飞机飞行手册(AFM), . L1 m$ M" z* O, {, i; B, H包合性能极限,操作极限,操作程序,起飞和着陆性 + o {. D4 r+ o+ a$ H0 X2 v# v8 {4 B机场分析, " X' l' S4 T0 L: n! e* d一套针对给定的机场跑道的详细重量限制资料。通常与 4 o. s% |- d( M$ \ r8 _机场温度、风、和飞机襟 $ {; A* j S- g) V$ {: m( n英汉对照民用航空词典B OEING 2 c9 r; B' C7 w1 `) g2 N0 t6 }TECHNICAL DICTIONARY 7 ) j, N9 Y/ W+ |* U! U/ o+ lAIRSPEED BUGS, Adjustable pointers on the airspeed! o* b! e5 r3 [2 x, f indicator. 2 E3 z( s/ n$ B# K) c" fALLOY, A mixture of a basic metal and small amounts/ [) f. V: j; R h f other metals to change the properties of the basic7 p0 |2 c- T4 \2 P( G- m etal.' T+ x+ z4 f7 ^9 h; q" S' G Minimum airplane speed.9 X+ v% G0 n2 R e1 M2 u4 l7 w e of4 m' B0 f _- T: d S( a" |6 u+ w itting airplane angle relative to$ J! l2 M) L- T( X; f8 S' e irstream for the stall warning system.$ @. D' i% e1 d% S" S" ^' f4 a another.( ?8 H4 n$ Z# ]9 \2 g1 M LTERNATE , An additional airport selected during3 P1 Z9 |2 t3 \8 O$ g: Z2 C. D" e+ \9 \# m; u8 p 合金," w% ~ D7 _: B: ? 在金属中加人少量其他金属,而改变其性质的一种金属 / h: w4 h2 G. j4 q# D9 k* N/ U合物。$ X! H1 j+ T* V* H$ N 飞机的最小速度。 . G+ v# l' @) Z% @速警告系统传输飞机对 |2 R( y: x8 v) V( Q0 R) j& ?流的相对角度。 $ @+ J% S0 k4 b+ {: K+ Q# F由一个状况改换到另一个。9 v( e; ^5 V2 Q0 W6 }! C' N 降场,! T3 S/ N- r% X- ?( c 划时,除了目标机场之外,所选的另一个机 ! \0 B8 o8 O. \# ?; X$ w( Fo 9 |& L, V% U5 e) y2 f8 K7 a! hm6 N( Q, J: j1 @! o2 ? ALPHA SPEED,: q N2 @2 ?8 z ALPHA VANE, A small moveable airfoil on the sid - }/ W; w' x N. `4 ~; u) othe fuselage transm ) v1 S: l- O; s7 [2 w; va8 j, m0 C7 h1 H. M% Q ALTERNATE, To change from one condition to % H( b, Y# I' eA; s2 s% L& r# u; e# M flight planning, usually near the destination airport, to be% \9 `* i* t5 ?% `3 q+ Z1 c used when it is desirable to divert from the original . T3 \$ J, z: r) ?$ cdestination airport. . j9 n8 D/ H" F空速游标+ S1 X w% E! ` 空速表上的可调指标。 ' n5 ?+ a5 Z" k6 z: l* j, u7 N% D0 p3 ], w 迎角速度, ! w* u9 k" { {6 E迎角叶片, 4 f3 d0 O$ _( G) g% l2 {位于机身侧的可动小翼面。为失/ R2 _3 \: Z4 i" Q+ Q% ~+ J1 s5 z$ ~' ~ 交替,5 ~$ Y: X0 i! W) {; S* L" G6 r2 I7 \+ u+ F 制订飞行计 $ v, z, j+ e$ n1 y8 g场。通常在目标机场附近,以备不去目标机场时,改降之! W5 L: X1 j$ H; f* z2 Q" j 用。; ~& {1 ` F6 N! C2 Z4 I5 m 英汉对照民用航空词典B OEING O. p7 M- a' V4 e; ETECHNICAL DICTIONARY 8" _2 n( Q' M Q* Q# S2 d ALTERNATE AERODROME, An aerodrome to which% w* q5 P" q+ I an aircraft may proceed when it becomes either * u+ ^! d7 _# A! qpossible or inadvisable to proceed to or land at the$ h, m% p7 B2 l: ?7 E' g1 c$ ] erodrome of intended landing./ k e" _6 [# |& R TER SETTING, The adjustment of the altimeter6 p7 E7 H5 ^" h account for local variations in atmospheric pressure. ! ?/ v* X6 [* F- ILTITUDE ACQUIRE, A digital flight control system2 A$ [( N" [- V1 \8 I7 [% L ode to transition from climb (or descend) to level flight.! F/ p& h, \3 I2 _( V. _ LTITUDE ALERT, A flight deck alert occuring when the$ D+ a) u* [2 S& J2 M% E. o* {7 W2 Q irplane approaches or departs a selected altitude.4 ]8 z$ n, \6 u+ m. c3 }3 ~ LTITUDE CAPABILITY, The maximum altitude at3 U: Y; Y( I* d8 l hich the airplane can be flown at for a given thrust,3 T6 l' D' O2 e8 j+ l9 o peed and atmosphere condition. : D- X$ G8 m Z2 O( `2 YLTITUDE HOLD (ALT HOLD), A mode of the autopilot5 c% V, \( w2 J( a! Y) E2 w% A" l r flight director to maintain a selected altitude.' N7 O% u6 v- F0 I! [ irplane's altitude during VNAV operation. " R# X& t0 F: U机场着陆时,可作着陆使用的 ^) O/ ~! W j场。 ) K" ]! m1 E M4 G! j- ]- X, K6 Q5 o- K5 N, T 根据当地大气压力变化而对高度表所做的调整。 ' z" d7 X9 E2 A t" _( n1 v. e一种数字式飞行操纵系统,从爬升(或下降)改平的模( F+ D" Y: s* ]2 y& U( s$ U5 D' b% c" s; K ~. V7 r: {1 T# b$ U度警告, 8 p( K# f8 D: B8 a4 B' Z: \) q当飞机接近或偏离选定高度时,所出现的驾驶舱警告。; f9 l9 A. E3 p; \5 l1 K 高度能力, / V: h5 U; H4 |( F/ q) x在给定的推力,速度和大气状况下,飞机能飞达的最大* d$ T# F! V, K3 k+ U: R3 d 高度。 3 l% a! r/ E8 d0 {( L0 p5 x高度保持(ALT HOLD),: T8 H8 x& [6 ?6 G; u 自动驾驶仪或飞行指引仪保持在选定高度的一种方式。4 G p4 T3 S4 D6 G8 `; [1 R- ^6 r& ~7 h b6 j2 n4 d- } s8 ]9 ` 员对飞行高度的控制。 & x) Z5 ]3 V5 }( jim / O/ ~* A- F" ?/ v' G Ea ' G& G/ u% J2 A: y3 Q) o) w0 Q& JALTIME( H. J& f+ g" G$ M to2 G; v- J, |9 E# R. m5 C A - P# f7 Y& i' H$ Z( ~m" z9 H( W$ T& B B' T A 6 s. i9 F0 d& j* ~8 F% ^+ Ja2 V( y/ E% I% A7 G3 K* X6 I A# H: n; W5 p$ c8 t w5 c* u% F( b) M, y0 h s2 f8 Y1 ~, I$ R0 z5 g( w5 Y A 3 w G6 C1 s! [! W7 zo6 v; J) l2 F4 u8 Q( C. M ALTITUDE INTERVENTION, Pilot control of the/ \) q( S0 ?6 Z! C) U }+ w a; {3 W. z- d) d+ S1 P* C8 d2 g AMBIENT, The surrounding atmosphere.* z) |5 o7 b# u 备用机场, 0 H5 |2 f# h, ^8 ]4 V" S当不可能或不适宜在预选; i4 N, [9 K* \# ^4 p% G! z7 H0 l5 \& Y+ B, ^0 ?0 M6 o! d+ n8 K高度表设定 ( t; A. l3 b+ S7 L8 e5 j高度截获," ~/ V9 S/ o0 s& Z0 S- N) w+ |" w! y8 D% }: `% g& o! t/ u) u; u7 K" t高度干预 - y+ @/ Y8 y; ~7 m7 q在垂直导航工作过程中,飞行 - r8 a4 q! \) T- j周围环境(地面气层), 9 f8 z) M2 O# `: M9 M& C物体周围的环境(特别指大气)。9 p+ L5 d0 H: h" ^3 W 英汉对照民用航空词典B OEING, ~ d1 x$ {- K6 ^ TECHNICAL DICTIONARY 94 W# o0 h! X. Q, S3 u AMBIENT PRESSURE, Pressure of air surrounding an + y2 u9 ^9 @8 h( u0 Eobject, measured in pounds per square inch (psi) .. V" f9 b" l+ ]; {) l3 p1 m MBIENT TEMPERATURE, Temperature of air 8 `/ ?9 E* r$ N7 [mpere. 4 V3 i& u1 h! e% j( a0 `urrent waveform. ! D8 M+ \/ p+ m, B! y+ Cg an" w- v% Z1 E* P7 O5 ^# u- u6 N nalog signal to a digital signal.! c) m3 H% [1 d ore inputs6 r! }5 {' }" Q: k z f binary digital information and one output. The output + z% {- B3 i. l0 N1 only when all of the inputs are 1. The output is 0 : _8 L& H( C! _4 ^9 P) @0 z+ [hen any one or more inputs are 0. ; h# Z& H0 l. f6 g面气压), & O! n) S8 t. K( T% j+ V境温度,$ F& \, a4 I5 k, _ 气温度,用摄氏度(°C)或华氏(°F)来 # ?6 ~+ `/ j( w. T- x+ D: X( i/ f9 f @) m 电压或电流波形的幅度。 3 u% v! g& x8 L性变化的信号来工作,或产生连续性变化的信号 ! t, n1 w' ~. B/ J统。4 a' F. D6 }& n0 ^- K7 g) { ^ 将模拟式信号,转换成数值式。 1 J" E5 K2 h$ ~. I* A! L一种有两个或两个以上的二进位数字信息输人,一个输 1 _9 z2 i# T7 M$ f8 {8 l- k的装置或电路。当所有输人为1,输出为1。当任何一个& H l# T' g% k$ j% L! ~ 一个以上的输人为0时,输出为0。 / u- S! l& P, P$ J0 y! ~4 ^A ( {8 x9 S# [" L' r6 t- jsurrounding an object, measured in degrees Celsius $ C5 D3 Y4 V U(°C)or degrees Fahrenheit (°F). 3 S8 U; F3 |5 V; K7 w3 vAMPERE, A unit of electrical current. One volt across7 w' g9 @% i9 c/ G2 ]4 F) d9 y one ohm of resistance causes current flow of one % d4 I* X$ Z: [% L, |# d4 a& v& xa$ S% ~0 q7 p! _. `+ u8 e1 K- N AMPLITUDE, The size or magnitude of a voltage or $ w) P8 C. N |1 \; [c ! |& X, h% f9 f t$ [; xANALOG, Quantities or representations that are, K; S& ^- g! r2 o variable over a continuous range. - l' a3 |2 i" U& FANALOG-TO-DIGITAL, The process of convertin, T' W, Y9 W; P, X) X a ( H7 }0 j- D6 mAND GATE, A device or circuit with two or m: Z* r1 e& y7 K1 h! Y$ {* ]: Z o. s) ^" M; B, F- S0 j is/ h0 C/ b9 a. D+ o$ {' M2 G; g# l w0 s! Y; H* G% S# r) I9 ~4 ~0 A 环境压力(地 ; z5 k" ]3 k# B3 l! U# ?& R物体周围的空气压力,用每平方英寸多少磅(psi)来3 [5 n* W' c& v9 g 度量。+ ?4 F( M4 a# ^6 e$ T1 A. U# w9 u0 v' j8 Q& G- b 物体周围的空 7 Z1 _, _+ |* p& g. ~( ~/ k, f, A度量。 + P5 E4 I' L9 J安培,. Z& h2 m) q1 s' ?, y: y& e; d+ t4 R 电流的单位。$ Y& X% `, U+ M3 P% Z, ?( p5 O 1伏电压在1欧姆的电阻上所产生的电流为 4 M5 G" J$ y# K: }+ {! T8 `/ |' a1安培( q, k$ I; O/ ?1 l4 {0 F) W 振幅, , C! r& \8 ^) J" F模拟式, . N7 o- D/ ~: P5 S: ^8 E2 G' n# c用连续 ; r# d u! m, b1 O- L8 z' v# k' | L8 i 从模拟式到数字式,) r V! p3 w# z B: D( A# A. C 与门,( p2 K$ u1 g( x& g2 h2 s' D$ k" G) X* N3 s t, W$ F 英汉对照民用航空词典B OEING4 \. i0 p X3 w8 I TECHNICAL DICTIONARY 105 ], l; ?6 T- b% |* f3 K" j5 X8 I ANEROID, A sealed flexible device containing air at low 1 }* ^+ T+ ^: C7 Q; t+ b( `8 N" }3 hpressure, which expands or contracts during change of! |$ ~4 t A8 R, v, _" A S2 s ressure outside the device.* E* U; z z2 ]) }6 _ ically ' ?3 [! }8 _2 ], ?0 d! Q. q1 ]! ar changing the direction& j$ c- `: l! T" ~( n f drive.% L! _0 [( g+ x9 m7 f- G- K of the wing chord in7 B! H Z( r$ t$ o) G. w7 e1 h% l lation to the free stream airflow as it moves forward , d/ u* P! b0 q4 B0 l3 prough the air. . c4 u2 v, A l4 f) xal axis of the . ]) z; a0 b! p( b) P2 o) vaircraft. ' h6 o" s* u( i% k! n! M胀或收缩。- q- p# v! N: m9 ?' M- ? 箱。是改变驱动方向的机械装置。 # ^- _6 y4 Y2 e$ g" R机翼翼弦在空气中向前运动时与自由气流之间的夹角。( e. b) A: [) `+ `% G0 e: a& l9 V ]3 H- W& X' p' H: _p 6 q. Y4 Y7 E( t) Z4 EANGLE GEARBOX, A part of an engine, mechan : s. l l% m* i$ C" ddriven by the compressor, which drives the accessory5 Y( r4 c; V. g7 u& T" d# [; [ gearbox. A mechanical device fo& f, O% O7 }6 n3 L Z' P! s o& l" b3 h, r! T ANGLE OF ATTACK, The angle, {& F0 |. _* g re # H& L. ]( Q2 }/ f. J0 b- x7 H6 Hth ) a4 D/ T( P0 r* p9 A! n$ _ANGLE OF INCIDENCE, The acute angle which the4 r% Q5 q; d' @9 ~/ L0 y wing chord makes with the longitudin 3 j! |5 I/ ?0 R膜盒, , x. I0 G, T$ T- w4 r$ L内含低压空气的密封弹性装置。当它周围的压力变化7 ~6 O3 {4 i! F 时,会膨; R1 U/ W& n7 F+ V1 }. U 伞齿轮箱,) n- v X0 |* g x* |4 X 发动机的一部分。被压气机以机械方式驱动,然后驱动 7 z% h; E4 ?' b" B5 w. K附件齿轮& P8 q- Y, x; E 迎角,' p. l: R5 S1 n; ~! z( n9 Q 安装角,# v% ^* y' O: [# F 飞机的纵轴与机翼弦线所形成的锐角 6 J$ E0 e6 C$ Y$ N3 D7 X' Z英汉对照民用航空词典B OEING O% p, G) _0 w# a! v TECHNICAL DICTIONARY 11 . I/ e% O3 K7 Z* ]3 J1 \ANNUNCIATIONS, Audio or visual indications used to : `, V3 Y: @9 Bcall attention to an event that has taken place.; p, E! h# Z: ~8 j ANNUNCIATOR, A visual device consisting of a number Z7 |8 D, i; _; B: a4 dly.% k9 O6 w6 P- @6 `9 p* L( W: ?1 g; J ANODE, The element toward which the principal stream - T- I' {3 W' w @0 D% oof electrons flows. " [) K4 {0 q4 _5 ~8 ?ANOMALY, Not normal. ! ~$ o- v& \8 }0 `, \6 |ANTENNA, A device which, used in conjunction with a+ b5 o" }& K9 Y$ h! Z transmitter or receiver, is used for radiating or receiving }& H @$ z/ y$ g8 C) N# E; z radio waves.# I9 n" l R* @8 T: y NTI-ICING, A method of preventing ice formation on+ S1 R& ` Y% g% q7 T" }! s: \ e wing leading edges and engine nacelles." N. b4 F' f: ^$ e4 n2 x4 @0 d. K NTI-SKID, A system for providing maximum braking + r: q6 q+ d8 n X/ Eithout skidding for any runway condition. Anti-skid( Q9 e3 G4 v# P! I5 G omponents are part of the brake system. $ r9 [! @; m# v) A$ j告, 6 u+ j. }( r1 S! n0 \& h当发生事件时,以声音或目视指示形成的提示信号。 " x+ b; R' E0 d8 G7 a) Q与之有关的电路的现有情况或已存在的4 j! e9 f. R1 a7 ^# z5 g9 V# H* _6 h& ^/ F2 s1 W, N. `% b) N' Z# T正极,1 H* ?$ h0 s" |; ` 主电子流向的极位。 z6 W: O7 I. T异常, & u% N$ n4 a& J, L不正常。 " b- |! x b. x3 D4 C @天线, x& G$ Z& H- a' E, ^! B5 K一种与发射机或接收机共同工作来发射或接收无线电: f1 F4 F8 c' _; \2 L, f% ~ 波的装置。 ( ^) m; E X4 j- N0 l+ V冰, ( ?! s8 s8 e' o9 q/ x防滑系统, & f f" _9 T, w! M一种在任何跑道状况下,都能提供最大的刹车能力而不 / r3 x$ }; g/ n! O4 u4 n& F: n使轮胎打滑的系统。防滑部件是刹车系统的一部分。5 [- U1 b5 D% J2 r of lights. Each light indicates the condition which exists! h/ `" c) k8 N2 c4 { or has existed in an associated circuit and is labeled ) q, e# N* p: m- eaccording2 J* w# Q- [. _% Q. b2 R- G A - q2 y" P* G) M: {th * M+ q4 i# [# [$ Y* {/ tA- H% n' P1 ^2 O1 O! e w 8 M' N9 b+ N0 n# R: Hc* t; G! `. s" t7 l* M. x; s% B. i! |& L& Y8 h8 ?$ L9 {信号牌,1 K) H9 q$ O3 m n; {/ q& u5 f 由一系列指示灯组成的目视装置。每个指示灯都有相应5 s3 P; D/ r" m- \. I 的标记,用来显示 % v( d) P2 w9 K r) m' t) x i( k* Q& \: e$ y: k! s( _ 防止机翼前沿和发动机短舱结冰的一种方法。 0 p4 I, g% o+ A英汉对照民用航空词典B OEING % s4 c2 o0 w8 \7 Z1 j2 STECHNICAL DICTIONARY 12' {$ Q# b9 X2 F8 M6 t' c8 ` APPENDIX, A supplement to the Airplane Flight Manual2 q) ~( d& e* I. u" j+ Z) m$ v tained in the basic manual. A+ g: S3 q6 k) R$ T ]5 B, G M ollection of supplementary material at the end of a : k. u$ `- b, f* S# Kook.6 i" x$ b. G- B; X( a of the 0 x. K: h# h! C- e) Srsion link on the landing gear. * I8 j3 r5 i; M& ^0 ?6 D+ oAPPROACH MODE, An autopilot/flight director mode ( P7 r7 L/ u* e8 D& twhich is a combination of localizer for roll control and 0 X! ^9 M$ Y; ~glide slope for pitch control. This mode is used when full / t$ I1 L' N( A. k& minstrument landing system is available." _: }* x- H) f APU, SEE - AUXILIARY POWER UNIT/ |$ q$ q9 j" v/ c6 {1 d ARINC, SEE - AERONAUTICAL RADIO . D5 O) g9 t" q! \- p: HINCORPORATED / x0 y/ I/ e- Y3 i' v; v2 KARM, To make ready for operation. 8 z0 F4 p; e/ d3 C0 w/ v附录,% v1 Y* }+ {0 _1 g 飞机飞行手册的附件,包含基本手册中未提到的飞机形 {8 ?( r4 n$ Z" y/ b; A. | 态的其他性能。是附在手册末的补充材料。 . B' a3 q% e: L; o顶销,5 H7 G7 a4 a8 C9 j7 Z1 C+ e 用于连接起落架扭力臂两部份的销子。 1 i# o% {& h" R; O, g进近方式, ) I0 e. U& P! g: T一种综合了控制横侧的航道信号和控制俯仰下滑信号1 V; z! ~, j9 x& w2 N 的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系7 a* r$ Q$ O! O7 g/ R 统正常时才使用。 ; u7 n( J. A1 F& I% H' |辅助动力装置,, y3 M/ f% @- J0 `9 a& r; ^ 见Auxiliary Power Unit * f$ p0 _9 {: Acontaining additional performance for aircraft - R, J7 M% f6 |8 j: B! Z3 Wconfigurations not con/ Z9 o7 b/ Q" ` c . W9 L! G2 @2 Wb + B& U; g: S# g! o3 d9 vAPEX PIN, A pin for joining the two sections 8 m4 V; y1 M8 g5 P6 wto 7 x2 j6 V/ K0 v/ Z: F. x# ` u2 `" |( C# H$ t. k( [3 d2 l/ C9 j 航空无线电公司, - l$ e6 ?) h- k! o% ?* E, N3 G见Aeronautical Radio Incorporated. 3 R. M$ t* ~0 C8 o' n预位, $ y4 G1 J7 R8 Z9 `$ x1 u* y+ F部件可以开始工作的状态。/ ^0 m, p6 s& h' z% c1 E/ S 英汉对照民用航空词典B OEING9 `7 b% z7 W" u; h8 V) W/ a TECHNICAL DICTIONARY 13 ! ?$ }$ S& V+ W" D2 Q9 ]+ o' P) uARC, The curved track over the ground of an aircraft' k: u( n% o! K8 G1 {6 b flying at a constant distance from a measuring 9 I. C1 v/ Z X, z) H! Bequipment (DME).5 G. ?. Q" n3 o5 [: s3 `4 p6 ]* ? in the limits of self-contained system & _3 v4 l, j% r4 [* G* z) k; qapability. * n& S" O) @1 ?; C! R6 ttem for opposing or restricting6 v" a+ z% `- q ovement. % i) {) z$ a) R9 YSPIRATED TAT PROBE, A sensor that measures total! ?! | d' I: T: N* A6 S ir temperature when the airplane is in the air and that - R. c, N+ r" N6 ^/ R8 U( Weasures outside air temperature when the airplane is/ ^/ t$ I+ m) l! P; J6 x* S n the ground. The outside air temperature is measured% t6 C: w6 K( K: c: i+ L SSEMBLY, The fitting together of a complete structure 3 q8 q' F, b1 b+ `5 ?, }# K6 n9 ESSUMED TEMPERATURE REDUCED THRUST, The 4 @0 y. I9 i" k* W$ eATC, SEE - AIR TRAFFIC CONTROL 2 ]5 e; r) o0 y3 ]7 @3 _$ \) x8 f. l3 D) v: s# O系统中所产生的一种用以抗拒4 O/ M$ H) i% [4 M9 k1 ~6 u7 r2 Q 作或限制动作的力。0 k5 u5 n" K' T 头, " Q+ P5 o3 Y; o4 T' {/ S用来测量飞机在空中时的总大气温度和在地面时的外+ b: R/ a! Q, p 温度。地面外界温度的测量是利用引气将外界空气吸入 7 e5 D: n& m6 }; q' g+ S! Y头,以达到测量的目的。 1 G( _+ j- T& Y% }4 O配,) R% ?& ?4 i0 X* r1 x' h) d 一个完整的结构或组件的过程。 1 L$ A* k" B, i5 e假设温度而得的减推力, 3 }, S# u3 \1 o& t; r" R2 e推力设定值时,假定一个比实际外界空气温 3 K9 \) j' T, G" p7 g3 n c空中交通管制,8 s( f% q5 s0 m 见Air Traffic Control w5 F3 r& u- Z# e2 w7 c: z. wAREA NAVIGATION/RNAV, A method of navigation2 _. i5 P$ S* w0 I# x that permits aircraft operations on any desired course0 e% h+ C- M! U% U& W within the coverage of station-referenced navigation ! y, K% ]! X0 {/ Msignals or with- d9 q$ v8 ]4 A& ~- h! t2 z c ) L' }0 a+ @8 w! }ARTIFICIAL FEEL, A force developed in the flight $ E/ D1 q4 u3 y& P* Vcontrol or brake sys 5 g5 X$ s' R: j& p n) Ym5 g9 P& J7 n' {; m A- ?$ N4 G. n5 P a & E- R7 S7 c: J2 g1 @m 7 Y" d" W( N8 y+ p( o0 yo 2 e6 q1 H" ^4 ]0 Z$ I- ?7 Wby using bleed air to draw ambient air through the5 }9 y/ m- T5 w# x a sensor when the airplane is not moving., X V7 K1 T7 r- L A8 ^0 s! u! `# p4 \ or unit.' w1 Z8 l- X8 K( R A & x: }4 _; H& R9 F" \, dlower thrust obtained by setting a higher than actual & f. `+ B$ m( ^( ZOutside Air Temperature (OAT).* j' R9 K9 K) z0 m 弧线,: n# [( V: t3 ~5 N9 t( G 飞机在围绕DME台等距飞行时的弧形航迹。5 r6 |! y3 k- S. B. U 区域导航,3 R4 T; B1 H- g E 容许飞机飞行在有电台参考的导航信号或自备系统能/ ]. q9 Y6 |' J. B 力极限范围内,飞行任何预定航线的一种导航方法。 : N2 c1 p% d. o5 a& S$ e* I1 M模拟感觉 * C. A: s {4 G$ R0 g在飞行操纵系统或刹车. I% H) K) w% h7 z8 n- g8 f( T, T! j吸气式总温探( ~$ u( U2 w7 w; Y& F m D1 m! ]+ y" t; b) B( G0 ^6 h3 \2 {* A- r B3 Y2 e; G8 p& O, M1 b4 | 组合成# u% ]9 \4 W% B7 l* z, S( a% G/ O3 \, T* g4 ^+ v9 }$ o- O 在选择起飞( s7 j+ b# j" S, w+ l 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 S. @6 f. R t) G* Y& t( l. b+ Z8 W磨损和维护费用。/ B: t' U' z- G7 h. E4 e; y) W) w) P7 ?7 M6 `' P英汉对照民用航空词典B OEING2 W3 D* Z- V, \+ T# {& ]4 [ TECHNICAL DICTIONARY 14 9 l; t8 q+ S* H! ^2 Y/ MATE, SEE - AUTOMATIC TEST EQUIPMENT 4 r* }2 h, a! ?. e/ RATMOSPHERIC PRESSURE, Pressure of air due to the6 Y7 _" a* [( O& I- B. D arth's atmosphere, expressed in pounds per square ( d' H3 i& v# U; ~; K2 L" W1 gch (psi) or inches of mercury (in Hg) or millibars (mB).7 e' m8 D( O/ w$ U; a# b* h" V TTITUDE, The relative orientation of the airplane with 0 S4 q$ \$ D4 l- n4 ^, Vspect to pitch, roll, and yaw. 8 t( `/ d* A6 V8 f# d7 f9 x0 ~UDIO CONTROUSELECTOR PANEL, The panel in) u6 c; u4 g; |+ Z7 ^) U7 Y, E e airplane which controls and selects the routing of& [+ [+ ?' Y" h% P l udio. , v8 v# V( a+ G4 {8 ]% gUTOLAND, Automatic landing using the Digital Flight % `, o) c8 m( tontrol System.* G, g; Q/ [$ ~0 g" j y2 m n.8 q3 G6 Q# ^8 I+ A M, A system( s$ o# J9 m+ R" Y: ^9 c omposed of all necessary subsystems needed to guide9 O* U& h. c" Z1 h, E+ w, f e flight of an airplane.; ^, D6 v! n& n* d$ p% ^ EQUIPMENT, System test : D. r& p6 {( _% v; Fquipment that operates under computer control.: W1 [) N" f; ~; _- }6 W 装置,

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e6 V0 n, t& e& M, T6 K1 w" O in 9 b8 U0 y; R# i2 C3 l$ KA $ P- I/ _' K, P; M/ m2 R3 Fre# R. w6 S1 W) A. J5 U3 ~( `0 y9 U A ! {+ ?& O' X) j( D3 ~th6 B3 S4 S3 {0 b1 B$ O; N a # Q ?9 @, X" n [# p1 l9 h7 R1 SA 6 Z* j& A/ f2 t# e c0 b7 VC 4 D) @) t2 L0 s8 o7 {2 i$ h j* kAUTOMATIC DIRECTION FINDER, A system which" G- X% w: y6 l determines the direction of a radio statio 1 X5 M+ c" X p/ UAUTOMATIC FLIGHT CONTROL SYSTE! o. x0 `+ J2 g c" _4 t' J0 v h7 \! \2 A th ! X. V6 Z4 r6 f* C4 n4 PAUTOMATIC TEST 1 h& B8 c' Y$ e2 z! t; O0 ?e) B& s o1 m* F3 J; Q+ {' k b1 T 自动测试 , k/ D" v6 g) [0 S. T1 x/ T, k见Automatic Test Equipment. 4 R" `8 M7 i: H1 j& }8 u' s" U- d6 S% J大气压力,0 m" w p6 _5 i( g! K2 { 由于地球周围的大气而产生的空气压力,以每平方寸多3 [& g; a& Q' Q$ C6 D. t, f 磅(psi)或多少寸高水银柱(in Hg)或毫巴(mB)来% f4 q3 t4 r, W e" _ 示。! Q, O0 U( k+ I' w& h# e- v. j 飞机姿态, $ q g8 B/ p, W/ Z* b: a飞机与俯仰,坡度,和偏航有关的相对方向。) B3 N/ V/ W: y0 @ M7 ^ 音频选择面板, * Z3 m9 z' \" d2 O, u1 K飞机内用来控制和选择音频通路的面板。 8 |- a2 q u5 X6 q3 z自动着陆,1 V h( [( K" J5 Q; Y 使用数字式飞行操作系统来进行自动着陆。+ r0 e+ r5 N# [5 K4 J0 J' T' s. U 的系统。, Y: \5 V: Z6 d9 U' T0 v, u8 V {4 v2 @: {' \8 A- H 系统所组成的一个系统。4 W; z; Q8 H) ^9 }% ] 在计算机控制下运作的系统测试装置。 % q+ G; R2 z+ [ x( @- U8 c' v8 X: _) O9 M: L( x! W w% P: e) J 自动定向仪(ADF), * H# z: U5 ]1 x0 q2 G确定无线电台方向 0 A" E0 L6 s0 R) O; _- [& r+ H. t自动飞行控制系统9 ?+ s6 `/ L( ]% p+ v& v4 o 由所有能引导飞机飞行的子. o' V( j7 Z* V) C$ F' H$ V* P 自动测试装置, 6 ^( P; {; ^; W- u英汉对照民用航空词典B OEING 6 M" l) v( I7 |6 `0 w1 u8 Y( }% _TECHNICAL DICTIONARY 15% u! W+ Z8 ?8 d. ?) t AUTOPILOT, A system which automatically controls $ w2 c/ J5 |5 D! T8 s$ M# L* m" Gand guides the flight of an airplane.! k+ j" [' |8 F' x& P AUTOPILOT FLIGHT DIRECTOR SYSTEM, An 7 m. U1 P2 ~! a; N4 Ktor7 ? M$ I/ b% E% k UTOTHROTTLE, A system which automatically5 s, X! W4 O5 v- x ontrols the throttles of an airplane.8 r0 t! D0 }* u: W POWER UNIT, A small turbine engine in6 h# D0 X3 R4 Y8 ]; Z5 f e airplane for supplying electrical and pneumatic ) w6 |1 g' q7 Fower for systems operation on the ground or in flight., g4 e4 p4 J$ }0 O VM, SEE - AIRBORNE VIBRATION MONITOR / }8 k% e3 m6 J# T3 |+ UXIAL FLOW COMPRESSOR, A type of compressor , p8 q9 g0 E3 z% U8 ksed in a gas turbine engine in which air passes through ' K% a* l' r9 MXIS, An imaginary straight line or an actual physical 7 U6 q. {) o2 a8 [omponent (such as an axle) around which a body can Z3 u8 [: \# K3 H, I tate. / H( ^* R/ k2 [) K仪, 6 ?1 f7 Z" J2 j% [! d# M: I6 _: T& `1 r: ?1 ^8 W 自动驾驶飞行指引系统, % z% Q1 A8 K( p5 \' B# F动驾驶和飞行指引功能的系统。 0 ]% `* a9 ^: b# x8 M动油门,* {$ d! N. }/ e" |( m, C7 h3 ^ 自动控制飞机油门的系统。 ( _) O: r# \ |8 H; E是飞机内的小涡轮发动机,在地面或空中给各系统提供9 o/ D& p$ F$ D: H 源和气源。 * T5 D( ^6 G& O0 Y0 k7 _$ l1 K4 r称。 / z; [5 {+ k5 F载振动监视器, 3 t# [8 ?! ?' B2 m! y见Airborne Vibration Monitor2 M3 _/ S' a- Z- P+ h3 |" A integrated system containing autopilot and flight direc 1 V+ M4 r. {3 ?6 \+ T! hfunctions. 1 w$ V) W" R5 R K3 ?" QA0 ?" J1 ]* B" l* S9 c" S c; f; M/ x7 V1 Y0 e AUXILIARY/ M1 A2 n5 Z) R th, H& v* G( M. W: ~/ R p9 L5 r9 x+ o$ R" B) Z AVIONICS, An acronym designating the field of aviation0 }: p3 w5 f% N4 w# ]3 J electronics. - X2 Y J: e4 }# L( sA & l7 w4 j3 u* J2 t) BA $ c& H6 E& G' Q9 `) Y [2 w: gu* R2 r1 T. D( Z+ O the compressor in a straight flow, front to rear.' l* K, X% B2 ?+ U A + P: w: ]+ j1 j* U& ]c ) B1 f7 e N- |; pro & U' T( D/ T6 A" i# O! s6 Z, ~* g自动驾驶0 b# U! q& D( A! x K, f* u3 d 动操纵和引导飞机飞行的系统。3 h( v: e! B# L0 p 一个综合自 ) _6 X. A" f, K/ r% \: M4 V+ [+ u! \1 U1 [ 辅助动力装置,9 t3 e( D4 h' s/ v* t* I- ~5 f! G/ h' A# `航空电子学, 5 ?- |1 D, J' o1 c; ^& n- C! _是航空电子领域的一特有名4 d) N) f/ {8 s% u6 Q9 c1 v, f' u( i5 @* |1 N* i+ P6 R/ {" V8 y* z8 y2 T' g4 @流压缩机, ( Q; ], s0 {# v! `2 L2 A' N一种用于燃气涡轮发动机内的压气机。空气由发动机的* h# Q1 a0 ~7 z4 S$ \1 \ 部流出。7 r7 }+ j. `* h" {$ u+ c- p5 e' z2 r 线,1 R' K( `6 L3 |. M# R( T% ?6 F# L6 Q. r 可让物体围绕着作旋转运动的一个想像的直线或实际. I9 y0 O/ F8 r. o4 G2 b+ G 在的部件(如轴)。 9 l! Z" m, ]1 T# d, K+ x& c& |6 a6 N0 E& d 前部轴向流人,压缩后,由后 1 e7 l7 c$ |1 R0 O8 S4 M4 T1 b# W, H% ` y4 m u0 S5 n' D4 U" F: K- g* Y, }) P 英汉对照民用航空词典B OEING 2 Z Y" g! G9 `5 v8 Y3 STECHNICAL DICTIONARY 16 2 @, k/ ` C- ~: M! kB # ^& h! o( Z7 r/ H, V* w. n2 @7 NACKCOURSE APPROACH, An approach to a runway 2 |. g) c' Q! c5 e* Uversed. ; A: i X( M- T! J% Fown on the EFIS that + T1 W( j* j0 E8 ?7 aoes not readily change, for example, navigational aids.! t; e. W c. P2 f" c% z vement in the tank or reservoir. 6 r: H5 i4 c9 p3 }! x# nALANCE TAB, A small hinged moveable part on the y. e; X8 |; r' Nailing edge of a control surface (aileron, elevator, - |5 Z6 q4 _0 ^9 a5 e9 V% D航道进近, $ k# k; |& i* a% R5 B- I相反的进近方向。当反航道进近时,无下滑 ( U6 F) E% S- ?% W5 S显示在电子飞行仪表系统上不经常改变的数据。例如: % x i9 [$ |$ k- y5 f2 _航设备。4 I" V3 @" J/ n4 s8 j 在燃油箱或滑油箱内阻止液体流动的隔板。 ; {. y4 K& C5 I5 p* X+ m, J- B- H动补偿片, " g5 t/ h1 ?- t铰接在操纵面后缘(副翼,方向舵,升降舵)的可动部。 0 l( [5 q4 X2 _3 u与操纵面相反,以帮助操纵面运 , n3 i, M' q3 H8 q2 ]; j/ N, O$ p8 jB n; Z, B: ]+ L5 Y+ _+ c' w6 w' Pwhich is opposite the normal approach. For a / i9 T$ I* r' f* dbackcourse approach, glide slope signals are not3 Y. i8 a2 p( z9 N/ ^' y available and the sense of localizer signals must be" q) F N0 Q" j% z re U' Q. _, T7 G7 y% yBACKGROUND DATA, Data sh 5 \9 J$ d: e4 C2 J h5 W9 `0 ?d : q, U9 k r" V" s& Y; BBAFFLE, A partition in a tank or reservoir to prevent9 D1 n8 q% A M7 Q) X M! \ v" a fluid mo7 F v1 [- g& \. Q B 8 \! F9 k2 ~3 D& j( i3 c8 q; f( gtr % {2 O' r6 P8 `; J; Lrudder).The tab moves in an opposite direction to the . q7 A5 ^7 y6 X3 I' x# ^; F9 H: [- Q) Tcontrol surface for assisting movement of the control ' D! f+ A1 R/ W! z" {surface. 5 v2 G5 _( q+ `) g4 Z2 N" `& |& ?; ?) w 与正常进近; W4 |" C( X) H) G$ f 道信号并且航道信号也必须逆反。 5 P+ y ~1 w/ U背景数据,9 X. ^. p. f4 M# o/ E+ C* {; w' Q* k. J; y, _缓冲隔板,9 w d" Y! H# j: B( W2 K$ N- W! g# k- h随动补偿片的动作方向. j4 K9 I. M+ u' h& {9 i) H 动,减小操纵力。 4 o" t1 q( R! u, t: G9 A英汉对照民用航空词典B OEING4 @ B% Q* @: W% _9 W TECHNICAL DICTIONARY 17# w, B ~# f" L+ {# K3 e2 b BALANCED FIELD LENGTH, The field length + Q/ C2 k5 Q# I' m8 n& w. passociated with optimum aircraft performance when # c2 E* j8 b; n8 c, k% G; }" Bbstacles are not a constraint. In this case, after engine 9 y9 T$ ^# v& F$ O# x4 i9 Bilure at V1, the distance required to accelerate, takeoff 9 h1 D4 H' H0 G. U9 D6 snd reach a height of 35 feet is equal to the distance9 A2 b3 o2 h" V, F; t5 O1 n0 | ALLAST, A weight installed in an aircraft to maintain 0 n/ f3 v& Q Q# }ALL NUT, A fixed spherical nut driven by the & Q: X, I+ `/ {$ U/ `- |AR OUT OF VIEW, A signal used to remove the flight 3 s9 u" `) u8 J9 |$ HAROMETRIC PRESSURE, The pressure of air above! a2 R+ Q, q; ~6 P! v g) or # Y! S8 _5 {& P9 G0 omillibars (MB).* l! ^1 s9 i" ]3 e6 i ATTERY, An electrical device for changing stored E, E0 k# q/ Q/ v$ o 性能的场长。在此 / L* w2 U7 c; `: w况下,V1时发动机故障,要完成加速、起飞、离地35 ! N: a0 z( R) C* c7 j, n3 r& n尺所需距离等于相同速度下完成全停所需的距离。 8 N3 t+ G; r4 Z. ]; \舱物,2 Z ], U9 Z" ?" C 重心在许可范围内面装载的配重物。 O0 ?) @; F; z" K: C6 A, I 形螺母, & k1 y- a& k8 q, T: p, H6 b的固定的球形螺母,用以使襟翼和水平" I7 H) R/ b2 ~, U4 P# B" D: d 引杆消失,, L6 i* }! D9 f 指引杆的信号。2 K4 V* c4 Q9 u- }0 X: s$ B 压, ( J7 |6 x6 N# l# H压力。通常以多少寸高水银柱(in ' E' E u' `% n% b9 d瓶, 7 c. c* t1 \; w/ n的化学能转变为直流电的电气装置。 ' f9 o. ~1 X2 J4 d0 Q' Y7 W2 jo9 A* F- K4 S* C9 P fa ) w; f: q) o+ g4 [# _ qa # F* l s4 X0 D, W% D& T7 S; Krequired to stop from the same speed. 4 `8 [% e% y+ m6 f6 i- lB / q* Y! B) c4 Z0 P9 _* c" \' Vthe center of gravity within allowable limits. 2 b/ t0 E% n1 R& _7 |$ s6 j- mB 9 a' v0 Z4 A4 e/ g7 Ejackscrew for flap and stabilizer movement. 4 p* ~+ n9 k4 ^6 \B2 K& `* {+ Z6 b1 P* n director command bar(s).; e* w, H' ]9 I, Q5 @3 N; m B 4 z3 M/ Z. N# ^7 S2 r) ?zero pressure measured in inches of mercury (in H% H9 d- N7 Q2 q9 C in ! `/ E/ C+ J& O( _3 r* oBASE METAL, The underlining metal to which alloying 2 n. i! _$ Q$ |; Qagents or metals are added. 6 N1 S; b2 v' q& A6 C' RB; x9 b0 o- \8 | chemical energy into direct electric current. 5 G# A* N! h$ Y5 o. D4 S, q) b9 F; ~平衡场长, - M. O! L* L+ J; W% h9 C当障碍物非限制因素使飞机达到最佳) G; _% ~6 w4 E- R$ Q1 |( q a/ |% ^' u ?# h) A: m/ d5 m+ G3 P6 u+ F% ]4 k7 {7 L' k为保持飞机 0 g/ q# l) d5 q. c+ a' P5 t- E2 U7 _7 | Z2 K' F: ?* Z5 m7 f' D 由粗重螺杆驱动 ( {# A/ x& i* N }& @" \( u安定面运动。 " `: n, s9 b# M# H. O& a/ e! e6 }: |& x# Z2 v+ c: s! `% } 用于除去飞行8 h& F' f1 W& X% s. F d& F$ ?; z 零压力以上的空气 9 C3 n0 ?% ~ u; o% m2 M3 N+ [Hg)或毫巴(MB)来表示。 2 b+ h9 I: F- j7 T8 ^, F基底金属," A: U2 F2 L0 g) W. R8 ^" b- u# Y 指合金中的主要金属成份。 6 R8 h$ L6 S) v3 J, t! `- i5 D& j) F将储蓄 r0 G8 k8 e) A- L, e英汉对照民用航空词典B OEING % y2 t- K4 i: P) M$ u. \: qTECHNICAL DICTIONARY 184 w& c8 A; U1 ? c( K3 G( { BATTER 3 ^. J# y8 [, r. fdirect cu 4 Y( L3 T! A$ G+ ?8 V% Xpower su: ]; {: G/ {9 g5 L; p Y BUS, An electrical conductor supplied with & s; F0 n' \/ P9 Drrent from the battery or transformer-rectifier for 3 ?1 c+ V$ {6 j$ Jpply to operating components.' z1 h P2 a# |; E+ f CHARGER, An electrical device supplied # K' ~( M. k o0 \+ A7 i4 Jith alternating current, which produces a direct current% f: q4 G/ I5 g q utput for charging the battery on the airplane. % v8 W, U( i! p# `AY, A compartment in the airplane structure. . S9 R# C0 Q7 }( ]. G' _: ?$ mCD, SEE - BINARY CODED DECIMAL+ }% U7 a' W( y) U1 J, t EACON, A device which emits a signal for use as a8 v) B f ?% [" A- k8 N$ W uidance or warning aid.: {: u$ S4 F" R" Y% V: U2 z: X BEARING (NO. 2), The direction from an airplane to a & X, _# }7 o- K3 Qground station.' s. H( G# P, p2 a: |" O 瓶汇流条,( t# a" l2 U4 z: X1 Z, J 将从电瓶或变压整流器来的直流电供给工作部件的导 9 l% t8 t/ t2 t3 P ?% |体。 7 b& O; V8 s, f# j- W: G6 `5 j瓶充电器, : u" y9 o/ g9 j$ g6 _用交流电向飞机内电瓶充电的电气装置。带有交流电的 ! k& \& E. C# m5 V) p. ^气装置,该装置产生直流电向飞机上的电瓶充电。 ! ?, @: ?' `' y. c+ q舱,2 q/ {( o0 h0 T. x/ i 飞机结构中分隔的空间。 * d1 O& I2 g3 h E- t二进制编码,4 |& s% i4 r" V' D 见Binary Coded Decimal/ \1 I1 O2 W$ W0 u BATTERY * m. {& B! {: ?; p L' ~6 ww" F% p8 J, f2 u- ~ o ! e7 x) w1 r- B2 L' o* J0 B. lB f# E; B1 ?& }% O3 C& h& VB 4 P; O) J0 b% }/ W$ P6 a' xB8 Y: k) f: _' r% G: F& V$ h3 O g $ J8 i8 A4 c2 Z$ I9 R QBEARING (NO. 1), A surface that supports a moving+ w8 p9 o; {( r) J" \ part and reduces friction between the two. 6 `5 A0 q4 O! F' e( Y5 J% N& _' e, w J' L& }3 ~1 {3 S" \+ y z2 `) c* `, G# }* M: g9 B! ?+ W3 Z6 A. ^* c+ d! P: ~/ I% S8 I! {: \7 R2 q) n6 u2 E5 n' A& V- H1 m3 F/ x+ Y' }/ U0 |/ Z# c信标, ) u: L$ ~2 r9 F发射引导或警告用信号的装置。* e6 h. m8 y' w9 Q4 B# S5 I% K 方位(NO.2), 6 V: G" {" K5 b9 C U从一架飞机到地面台的方向。 F3 y8 ]; f( F9 m轴承(NO.1), % W2 V* ~' }) y用于减轻机械转动磨擦的机械装置。 " @3 _. K; o% g: q( b/ v$ x英汉对照民用航空词典B OEING 7 i, r0 ?4 a) K" p$ E& S. oTECHNICAL DICTIONARY 19- R, L% ~8 H3 E O BELLCRANK, A double lever in the control syst 5 M, _+ M+ j5 ~! a% Rchanging direction of motion.0 |) i' G C' a& B, \1 t em for( l5 F1 c" B% X8 Y1 T g$ e7 l0 I ct in the" N8 M/ Y) U- i1 ^) x/ A4 W Q9 d neumatic system for absorbing expansion of duct due ; W! l; J$ z- n/ U1 Oheat. 6 c6 j, u- \% q$ J; |+ p( {9 z! ZELLOWS (NO. 2), Corrugated folded or pleated ' c3 o! V1 `' yontainer or compartment used to measure pressure. ; b2 m" p5 b' F' R& E8 V# mEZEL, The part of an instrument case for locking the1 E+ J/ V' j5 m7 H- |/ o lass. % R$ K! W$ D9 n# {% f- v6 {IAS, The potential difference applied between two4 B0 M2 o8 r9 |) I" { oints for controlling a circuit. $ d8 R- N! k: X" gBILGE, The lowest part of an aircraft fuselage. A place ; W( p# I5 w4 c, n2 V3 h# Dwhere water, dirt and other contaminants collect. + ]/ e( U; _8 Y4 x5 e: E9 K气源系统内提供管道热胀冷缩所需要的余地的波状, f+ K5 ~- t4 E( r 轫管。0 b* Q' V; j9 M- D8 Z, D+ t0 \ 空膜盒, . J% R5 Y8 x/ F, ]# c2 H一种具有波状表面的容器。用于量测气压。 : D' B' n" N( f' K' }$ [/ Z嵌沟缘,3 _" h: m+ S3 O8 M. c8 ]+ A 将表面玻璃固定在仪表上的圈状零件。! h M7 o8 Q; l' U7 \- z 压,' @( I/ f( s% @! h& `% T: j" u 在控制电路的两点之间的电位差。! i. G4 p) e8 o/ D8 K' k 机身腹部,0 [! w, R0 ~! K' ] 机身的最底部,通常水,脏物,和其他外来物集存于此。6 s; J& ~4 o: N% @ `3 Q BELLOWS (NO. 1), A corrugated flexible du : ?& p H& q. T( d. o5 R5 Bp ! X# _' f9 N8 zto # d' b/ e# E% a1 J- G3 @3 AB + {, l7 [! @- G; @" m# ?c ( P( t5 F& X9 U! o4 y% VB $ ^3 L$ n5 N7 s1 Yg* Z: U* C) C# }6 t5 q. D9 C8 e B ( F' H% I3 q% e1 s! ?p + [& [6 o1 A. |( D直角摇臂, " p) c6 k. s4 }/ Y# z在操纵系统中改变运动方向用的双臂摇臂。 4 u, S2 u% Y# i) Z波纹管,+ F* ^- _' ?+ M2 h) d! w! {, X: z. u: e* {- P+ `/ b) J8 n* ~; H2 g" s3 A0 a6 W) t' c8 Q2 V. a' o! @1 u/ l8 a" M- d8 g. x8 v, l英汉对照民用航空词典B OEING- G4 v) I7 s) w1 Q l: ~1 f, z TECHNICAL DICTIONARY 20 F5 L( X, R* v: ~BINARY CODED DECIMAL, A system of coding each7 h# h, D4 ]5 H9 X* E$ v digit in a decimal number using the binary equivalent.% J: L, G& \' g& h/ P+ G BINARY NUMBER SYSTEM, A number system using ! ?0 i7 t1 c+ v! Ys8 C& b$ a% ]: d$ C. p& _ IT, In the binary number system, the smallest unit of. n8 z1 }, H* t2 \7 l* ?! O: W; v8 O formation, consisting of a 0 or a 1.5 x6 K3 r p7 Z0 Z4 _ ITE, SEE - BUILT-IN TEST EQUIPMENT $ b- V; `( A0 @+ wLANK DISPLAY, A display that does not have any - I) x1 }( ]' \8 Jdications, normally due to failure. / ^. F2 h; k+ {- q' z5 M0 SLACK BOX, A container for electronic circuits to record5 w9 B1 m4 {6 q/ L& O7 `/ J- z$ s% ] ight data.: Y h/ Y, t+ Y- B( r9 X LEED AIR, Air taken from the engine to power various* E3 |! ]6 i' T ircraft accessories. 8 l3 x: z! z! s& M4 L. z4 ZA valve in the pneumatic system for air$ P4 W& R& Y6 n* w- ~ supply from the engine or auxiliary power unit to the $ m! ~* D0 c' Spneumatic manifold. A valve on the engine for reducing 7 \' _% O7 v0 t: rpressure in the compressor section. 3 m& s! \7 i" o& T/ W进制,7 W1 a; \! O/ x8 u b+ i3 y 进制, 3 r8 j. i9 B3 }一般用0和1)和2为底的数字系统。. U T; c6 p: s* q' k Y e 特(二进位数),0 F1 ^8 v2 o5 b6 E g D3 q) J. G! o 二进制中的最小信息单位,包括0或1。 / `% Q7 W n& s% a6 d内自测系统, / x- y1 u7 L. z见Built-in Test Equipment 1 k( U; Z0 u- stwo symbols (usually denoted 0 and 1) and having 2 a$ Y9 ^/ r6 s$ I its base. + f5 l0 ?) D0 c6 C5 E: q2 ^1 CB 6 s. c, ?' b$ w2 q: C8 W8 T: ~in! T/ C& B% Z8 p' y! q1 D3 D B5 g. y7 U5 ?( I: k B : Q& z& J3 @1 V; A, c7 c/ F% ?' oin: U; d+ b, e/ x: w B : S4 } n: E7 _! h2 @fl $ P' T9 E( G) w Q3 p: ~B, G2 D- S1 J; k3 l F a ' r& \4 R! I8 ^+ {2 P, j9 GBLEED VALVE,5 G; K! ^* ` K7 J4 L 二进制编码的十 ' m; w# i3 \+ V @9 G |, z" [一种编码系统。用等效二进制位数编译十进位数的每一; r4 z+ w/ b" s5 \& W( y3 R$ C 位。 3 H* X0 ?5 O" @" |# _1 m$ Y) g* d1 P' r8 @! i& Y 以两个符号(/ Q9 V$ `) W# P. N1 t& ]9 t7 c5 b3 D/ |- s+ D$ l F8 c. c8 a& @6 l0 @# x/ M. 8 ?# L- U N9 K! b+ v" Y9 P$ z4 Q% l白显示,! \: `) B. ^' x5 \; F. i 通常因故障而造成的显示器上没有任何指示。+ c2 g! n0 @- d) B7 l6 W 匣子, ; K0 ]* M8 g5 O1 Z' o装有用于记录飞行数据的电路系统的容器。& J1 z1 q- Q/ t 气,, v% j; i% @- x& Z( w B y9 i 取自发动机而用以驱动飞机上之各种附件的空气。 9 N) v4 w: T/ l" t3 S气源系统内,使来自发动机或辅助动力装置的空气进人0 }( E5 n! W& B! U2 I. s- U 气源支管的活门。发动机上,用来降低压气机压力的活门。 , Q+ \( B" T7 u1 g* A$ L% g. x; _. F& k' C5 l5 U7 Z9 z. Z% |2 D7 K1 N' s, Z- u9 w3 f9 E: Q 引气活门,5 d4 a8 s# J$ R$ a$ S# z3 v 英汉对照民用航空词典B OEING+ G3 }' }2 F- K5 L+ {5 t TECHNICAL DICTIONARY 21 ; m! B+ V$ o9 F5 A6 d" I; vBLOCKER DOOR, A device on the engine for blocking / D* x9 ], J1 E; |+ T Ithe normal airflow during thrust reverser operation.% E0 Y3 W4 v( h% B6 p- j' ? LOWER, An electrically operated fan for circulating air.) C9 ]/ h" J* I x LOWOUT PANEL, A panel in the structure between: f( `8 W1 E8 o. R L" J o compartments that opens to equalize pressure in4 ~( H- s _! K$ r; R3 q e compartments. , r- I0 O- a9 U; \5 C! v( v6 FODY GEAR, The landing gear attached to the } o# I# U9 C F) }grounding.; Z% \# n* k3 ` v( _ 正常的7 T: i" r6 `3 t, j2 m 气流。, Y" k8 Q- L1 u S2 R% v& y- g 鼓风机, ; K, T* A9 U' f$ c9 Q用来使空气循环的电动风扇。 " h+ F, U! a& q6 M) u压口盖, 9 Q$ z/ b i( g( c两个隔舱之间的口盖,打开后可使两舱压力相等。9 K3 c, K5 x1 \3 R 身起落架,8 G; e/ P- ~+ _. x' d" { 身构架上的起落架。( n7 o! o4 g1 Y/ B B1 Y5 m: |$ Z! U+ L. }* \7 I2 ` B1 l/ P; Y- m5 e) s* X; U6 C tw & |8 K. {7 n" e# Tth/ [$ v- C+ U1 v" T B) v1 y, J- R: p2 n$ F. x9 c: y fuselage structure./ B: i- w; k7 w( Y: u) p BONDING JUMPER, An electrical connection between 2 ^' d) {3 m' K2 La component and airplane structure for electrical1 Z8 B2 ]7 S# n1 Q 阻流门,. U/ \( J8 a' y' S- B2 q) i0 v M 发动机上的一个装置。在反推工作时用于阻挡8 S$ a" a% a, u4 S, q+ G# _/ T5 W$ K" E% w- Q6 s. O8 x+ t9 g+ |2 h0 b, Y: o! N) Y装在机# [3 d5 V) G) r2 {: B- u 搭接片,, H2 [0 X) C _( L! l 连接某个部件与飞机结构以形成接地的电接头。 , J2 B5 i& ]; Z5 h英汉对照民用航空词典B OEING - p7 Q8 j1 ]+ CTECHNICAL DICTIONARY 22. [( G$ Y' a0 [; l BOOLEAN ALGEBRA, A mathematical system for) I9 ?/ E+ X" Y6 u" H' y writing combinations of logical statements., o l$ Z# ^& |, g% u! V BOOST PUMP, An electrically operated fuel pump for. l- |& Q6 f5 K4 B6 N8 V) x G; F fuel supply from the airplane fuel tank to the fuel ! W- Q6 t+ e1 t. ` i6 Q- |6 y7 ?manifold. + \8 T- N7 |, d# p6 k0 N2 FBORESCOPE, An electro-optical device for looking at2 E, B/ L2 ]& R, m0 {% B0 G ternal parts of an engine through holes in the engine.1 [5 F0 b5 t& o2 J2 e7 R0 | orescope ports) 0 q" F I6 ^6 y- k0 y- J( COURDON TUBE, A curved flat tube in a pressure gage. Z8 f2 M0 \) r6 t/ N% [- o r moving the pointer when pressure changes inside* Q9 T! R4 o4 c on the ability of the brakes to 1 `' Z) z0 X- r0 y& Ybsorb a predetermined amount of energy during a6 \9 _$ h; h3 v* G- k jected takeoff.3 ^/ V" |, i! @ 用于通过发动机内的孔(孔探口)观察发动机内部件的 - t' K- ^: E, j1 }/ f光设备。 $ N$ d: H6 m8 k7 S& Q7 d端管,3 s& g4 @1 A0 q- o9 Q: r3 x 测压计内的弯曲扁管,管内压力的变化时它使指针移 " g- U) L1 F* x5 J力。# ^/ t8 f" O9 R- m2 d$ ?- C 极限重量, # x2 Y8 }. Y8 N1 W+ m0 @" ^' f; S; L. Q, R 起飞重量。 + l! K4 [7 W3 E+ V5 V9 e, y发动机滑油系统与大气相通的通气口。: Z5 z3 b1 b2 t8 e: G" } in - X7 R$ A8 r% {) \% U(b. U, B* }) l" f+ G3 j$ v/ E B 3 D( T U% y ifo # l& S& y5 o! |# Mthe tube. , t7 b. q; O7 Z* `9 n. u% i* ~1 ZBRACKET, To enclose or surround.- [; Z: r/ Y! v1 E BRAKE ENERGY LIMIT WEIGHT, The maximum 8 U# E- z! w% x$ X5 {1 Btakeoff weight based ( z, g/ |: `% w( w: Ca 6 }9 t$ z* ^1 R( c1 `! ire* V: |+ a6 y) t5 Y% @ BREATHER, A vent to ambient of the engine oil system.) {* m$ W }& G* r, n0 f+ H 布尔代数, 6 ~# X6 b( |3 t一种用于编写复合逻辑命题的数学系统。 * p; {$ s: n6 A7 l+ o6 \增压泵,: _! N4 Y7 W0 m9 y. L 从飞机油箱向总油管提供燃油的电动泵。5 s* b3 ^/ t5 v# z3 H 孔探仪,5 P: r, i% G; l! Z) m$ Z% P% }8 X. V- m3 y+ {' e2 F& N' ]1 ^7 d" W0 e+ P* L. }动,以指示压 x1 x# c: R5 Y托架,0 J; V/ I8 G2 ]0 A/ | I 用于作支撑、装托、或围绕之用。 ( y- e' e. {3 }- e% o+ K, y刹车能量, K- \, [5 B% `5 k. f5 v 中断起飞过程中,取决于刹车吸收预定能量之能力的. f6 |4 e" l) I$ e5 I1 Z$ B: Q$ c% j& S通气装置,- o0 y) Z' J! `& w; [ 英汉对照民用航空词典B OEING$ K8 u) j" S2 w: A% b TECHNICAL DICTIONARY 239 C) X6 \( J4 P. Q' K# N) f* n. _ BUFFET, Vibration of the wings and airframe resulting9 k% I7 |$ S2 h from unsteady airflow over the wing; caused when3 X4 _" u' b5 I2 ^9 E5 p airspeed is too slow, the bank angle is too steep, or ' K) g$ O' v* c N3 h! Hirspeed is too fast.6 d: T& m" \- ]0 U+ M' w J4 N UILT-IN TEST EQUIPMENT, Equipment installed on 3 Y. B( H" l" u/ h3 l4 n {0 xe airplane and in airplane systems to test the systems # ], P$ n+ b7 _% n% S- Z7 fithout external test equipment. . i% l! p( ]( h/ X4 |6 {UFFET MARGIN, The amount of residual maneuver5 E+ C% q4 y# ] V8 r" o: o apability present before the onset of buffet.5 u+ H/ k" n) T6 ^ UG SPEED, A preselecteed speed to be observed ( w. l5 x9 g, h; u2 P5 v% X! A/ Nnding sequence. / |% p7 r& u$ |7 Gk. Z1 t: o( I8 i1 F/ o; ~* {$ A ng landing gear operation. : ^2 M* m/ U) t: l速度太慢或太快,坡度太大,均会引起抖振。* E/ t7 J- F4 c" f2 f 自检设备, 6 q, G% p8 ^- G0 J4 M/ q; T) j安装在飞机和飞机系统中,在无外接检测设备情况下,; \$ Q) p) H. z( F3 N* |5 s. i! r 用于检测系统的设备。 8 @& w% G2 v" Z( _抖振裕度, 2 u3 q+ `/ C1 L0 I9 y8 G1 c飞机在遭遇抖振之前,剩余机动能力的大小。 + ^/ D2 R8 [( h% o- y" s标速度, ) b/ o8 _( }+ N6 K# Z) ?在某些机动飞行过程中,特别是在进近和着陆时,飞机/ [+ t( T% K$ x+ h 预定速度。 2 k! n) A% q% N1 `( c7 O m* j% v力装置, 5 Y+ `+ Z+ E7 X5 |* O# X7 `1 J0 L架工作的一种机械设备(弹簧或减震器)。2 w$ y- o! d/ |( l9 [" a 流条,) t; [: k2 T1 T- t& M9 M0 [. u: J' @ 在部件或组件之间传输电、数据、或定时的单一电线或) B. ^; ^) p! ^- Q a' Z0 X: S6 A- X: e+ @9 h/ ] B0 u+ a8 Q# C' u; ~: X th x7 a0 Z0 W$ V' k( _. [# Rw) `4 T! p% T" N8 U0 S% X7 h/ k: J B$ a$ B! S$ }% b2 F c , ^5 l4 X# f( ?9 [B " U, }9 c# K; E6 O, [( @* @during certain maneuvers, particularly the approach and- K$ r( B8 e3 @) R la % b! U7 J; y4 a& N, c, s5 ?BULKHEAD, A structural partition in the fuselage or0 G! S8 Y0 z/ E6 W wing. 4 r+ |2 q+ Q2 j' ?+ C6 QBUNGEE, A mechanical device (spring or a shoc $ {# N9 m7 a2 V- D' {; j& tabsorber) for assisti 3 f1 H6 m) w3 b' oBUS, A single wire or group of wires which transfers3 t4 y+ @) ]# T: z$ M# K# H power, data, or timing between several units or 0 g5 G3 S/ U; r7 smodules. ' u. [( h7 U+ k ~! }7 @抖振,1 m+ q$ |' ^; I- v% |8 S5 P6 ?6 K 由于机翼上表面的不稳定气流引起的机翼和机体的振 ; h- |6 g' T0 a1 f动。飞行" F7 n0 Q" ^2 K: a9 N9 m' a j* D+ j4 D/ ~ [所应保持的 3 C6 S0 X. M! I7 U壁板式隔框, ! y: H% p5 R5 B, T9 k3 X: R( K机身或机翼内一种结构隔板。4 f' R5 |, z# A$ ~5 q' x) X4 ~$ X, m. }+ Y! E9 h: J 用于协助起落 , u$ F6 L" B) @5 e) V; ?2 q7 a( I$ r1 n- g# |) U9 q 电线组。 ; `0 X. q; K; \* j4 c英汉对照民用航空词典B OEING 7 `7 ^3 T, K+ q: d6 OTECHNICAL DICTIONARY 24

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BUS DRUM, A mechanical connection with pulleys , {4 U( y6 m1 v5 h+ @cables in the control system.5 m5 m+ z9 F2 e4 t- A( b8 E and . K7 S2 M% k% _4 L8 z0 _% zl circuits for control and protection of8 o: E* _& a1 P6 [ lectrical alternating current supply to the airplane. 1 o4 {+ i, v3 u2 z" C0 r" iduct for closing and opening the duct. F0 z Z( l. c1 e# X/ n( V5 T assage. 9 ?# \" {5 M9 i0 v# cUTTOCK LINE, A vertical reference plane along the1 d0 u( q- d% j" {( i selage for horizontal measurements of the airplane. 3 c4 t/ b4 T5 u. j1 f) i接。' N4 v' ]2 o$ X. [5 ~- X8 t: Q 组件,内含控制和保护飞机交流电源的电 ( Z. q9 V. \, c8 N: q# E. B' Z/ m- k {, j 作动简控制的转动装置。用来关闭和 * F/ C- q0 g% u启管道。% {; p: j. Y0 {5 L* b 沿机身走向的垂直参考面,用于飞机的水平测量。 + N3 s; k" F6 Z c( xBUS PROTECTION PANEL, A module (black box)7 t7 b0 `5 h( r, F& U2 S containing electrica! C/ p/ M4 O+ W, q! J e- G5 Z8 |% D* g& q0 W, v BUTTERFLY VALVE, An actuator-operated, rotating: v) e; d: D; m3 { device in a% ]. j# }0 _& @- h7 c9 Q p 8 {7 J" P" X) F* WB9 i4 _: f: W$ l5 P' R fu7 q% p* M3 z! y4 V/ a) J 转动鼓轮, ( C9 y7 c: K( G( J1 b1 z在操纵系统中,具有滑轮和钢索的机械式连 # ~; i4 O! a* p$ l汇流条防护板, ( O! p) R$ U& {& q4 d4 k/ j黑匣子式的1 L" U' X: H: c* r/ A# @7 p" f" ~' I+ ^; u0 t& U 蝶形活门,4 k8 p0 ~' N4 `' ?; w 是一个在管道中由 ( b4 y" k- \/ h( J* |) K, ]6 `" O* b J纵剖线, ( h3 A! |( R% P2 T% d' ?; e英汉对照民用航空词典B OEING 1 k$ t, W2 w2 J1 JTECHNICAL DICTIONARY 25 ( B* s% W0 E5 R6 k C, }5 Y3 n) TBYPASS VALVE, A valve through which air or fluid will4 t% I( V6 v; z7 Q. n: i flow if the normal flow path is blocked. 6 T& K! j! ?: |+ l: @1 bBYTE, A group or string of binary digits. A byte is( J- [8 |' ?) {0 e! Q sually eight bits long. 4 ~* R6 u" e7 m( R) XABIN ALTITUDE, Atmospheric pressure maintained" _- l/ d* E8 ~! k( w+ O0 _) N ithin the cabin, indicated in terms of feet above sea % r# R# [1 w! H; O' l2 D9 p- wALIBRATE, To repair, adjust, fix or correct the ) K- J# s1 w: N! H& Teasuring capabilities of a measuring device. 2 x, B; T0 W5 ]- b2 ^ALIBRATED AIRSPEED (CAS), Indicated airspeed & J2 i9 I/ l* s- N) [; P+ S1 @AS) corrected for position error. - T' ^2 {+ o& h' [$ ^nical9 l* A' ~7 R; t O8 m omponents.( f7 [3 k3 }* q9 i; Q4 ~* \: a: V' N; u- I/ z 节, 0 t! | f0 X1 Z8 ~, i0 Y* n, U: u一组或一列二进制数。通常一个字节长8位。; w% t+ u% h- s3 V 舱高度, / n" l7 }( S+ B- q; E# U# e座舱内保持的空气压力,以海拔多少英尺表示。 # I) B& L1 ~, u* n a2 Y1 c: _准,( ], q" j3 q, z4 [, C 修理,调整,定位或改正测量装置的测量功能。: H" ] O, V% v0 K, l+ _; @ 正空速(CAS), - X9 h6 F2 A! ]6 ]: @* F在修正了位置误差之后的指示空速(IAS)。 0 l3 d+ D4 V" i0 {) V5 n用来移动机件的一种转动装置。 ' L! r( Y) l Z0 M7 wu) p$ J' `! E) Z% g& w1 M C & N, W0 _2 M) n; KC# { k/ r! R$ E7 c- y+ ^# { w ) L: }7 i% c3 J" R$ Z: J. rlevel. * b8 p0 W- n- X* X( w9 r) ^C 8 Y+ v# T Y" ^m . I$ e* d! ~: L6 H# U' O% `. XC& \7 e& B- T8 P* L" I (I4 ]$ x% Q( N6 p" S& ] CAM, A rotating device for movement of mecha ) F1 z& ^3 P. I7 e8 xC 0 v" h5 O g( \* f( O$ s" N旁通活门 - r4 N. f, o) U$ ]$ L气流或液流在正常通道阻塞时所经过的活门。 N2 j4 p, Y: C+ C# d9 a+ u a3 A+ ]+ I0 C0 G; O) r% T, x9 b" M \$ Z% O2 D" C& @) }, `. I8 D% L9 [# B: n3 s& `& E7 ?( H) Y 凸轮,' d( d6 T) ~, f0 d/ a 英汉对照民用航空词典B / {: I$ I( u. H( _' l, XCAM-OUT, An autopilot condition in which the actuator! r4 V) \" M- ~: V* M/ u detent piston is overridden, either manually or by the q0 }, Y. h2 t" k7 D. V' ^. ether autopilot actuator.& z" V% G& E8 U: D4 g2 ? AP, SEE - CAPTURE * e) x1 J% _+ j+ r- ^# |$ bAPACITANCE, The measurement of electrical energy: c# E3 h: t: y/ x' r# c& O8 v tored in a capacitor (condenser). 7 }% r4 c- e: M/ ~APACITOR, An electrical component of two metal * ^/ h2 F( u1 C% k7 y5 i2 y0 N4 wlates separated by a dielectric material, for storing$ @0 r5 q& u5 O: j' k lectrical energy. 1 N4 l/ M6 n$ f, _9 X9 R+ z0 ] OCAPTURE, An autopilot or flight director function to . U4 A. j/ q0 G+ }acquire a selected mode.0 N7 g9 `8 I5 B1 W; C1 w' u5 O4 a CARD FILE, A container on the airplane for printed , k! Y# R: W. {circuit cards.- j* G; ]- V1 y) ?1 C; Z; D 一自 ) l8 Z! s* E/ a L" I动驾驶舵机所超控。6 C5 F& z% `" E/ q3 m 截获,8 g/ j, Z% K2 ]7 A- k- g" Q 见Capture% P( H) C9 @9 w7 M$ A5 U o : o; m. D6 y" F! j, c( aC C, A8 h E: i1 _0 r- F5 a5 |C 3 Z6 n6 o: [- p7 z5 c7 @8 [; i! v' ys2 S& t* m$ u! C) j4 f3 y& J C . s3 D3 s9 c$ |" }0 Ap ], f9 j* _- ~& x5 X' r( Oe' k( h5 H1 b* W- l 凸轮不工作,7 B. A$ F6 v& s# b$ u% b0 X ~6 a1 W 一种自动驾驶状态。此时舵机锁定活塞被人工或另4 N1 H* f' d9 ?+ ? ^7 a( ]+ K) K: b% L0 j K. O5 r 电容量, 1 s; {" w4 x- ^电容器内所储存的电能的量度。 1 w1 Y- Z0 C; Q$ Y' h容器, " b$ `- a7 L, f4 Y7 d3 n% z两片金属中间用绝缘材料隔开的电器。用以储存电能。4 }/ C) a) _# A0 J7 J" E h 截获(CAP),$ v1 ~8 y" _) [4 G2 f3 c1 F 自动驾驶仪或飞行指引仪的获取选定方式的功能。 E9 E2 F1 j" b. }% ~3 y 线路板盒,# @2 k+ H0 s- ?+ i2 h4 l6 ^ 飞机上安装印刷线路板的容器。 $ E0 E9 W, ~" L" B. m9 a5 b" C5 [) x OEING" \/ S, D A6 u; n$ W" ~% s8 E* B% X TECHNICAL DICTIONARY 26' t8 J" ]/ f: m( m- V 英汉对照民用航空词典B OEING . l6 R) o- u% ^7 \TECHNICAL DICTIONARY 27 + v. U. K6 x" m* vCASCADE, Two or more similar circuits or amplifying / ^8 G) e6 T8 E; |' x- `stages in which the output of one circuit provides the: M. M& s3 w' h3 F! G: @) ~, y: R put of the next.- K. j1 L+ M5 d# e6 _2 h2 @ } ASCADE VANE, A vane for turning the engine airflow( t8 A2 S9 i; Q uring operation of thrust reverser. $ d9 p' h4 Z' a$ _- eASE DRAIN, A drain carrying lubricating and cooling 1 B4 l: |" ^& i/ f! S4 I8 a! euid from a hydraulic pump.1 l! s2 P6 v T1 K) M [, Y. b: a ATHODE, The element from which the principal6 C3 B3 w. `. D& G7 ^ tream of electrons flows.! N# b" h; a6 o! |( X1 m( M- a ATHODE RAY TUBE, An evacuated glass tube with a 8 Y! b0 [; o4 XCEILING, The height above the ground or water of the 0 A; _1 B( X n2 m7 wbase of the lowest layer of cloud below 6000 meters0 Z- k8 Y8 u' Q/ } (20,000 feet) covering more than half the sky.: j) R ~. S2 I: f6 a 程。该9 k; A2 A- a* Q5 W$ l; S 程中,一个电路的输出为下一个电路的输人。# \ U9 ?- f1 G( Z6 a" n 叶栅叶片,- n. c( e R( e( @5 {' u( @: E 在反推工作时,使发动机气流向相反方向流动的叶片。' |0 w T! c% t1 P2 j! `- f1 ?5 Y 匣余油管, ' d, T* k8 j, t8 `) z9 ^4 a液压泵多余的润滑液及冷却液的排放口。- @' i0 ?1 W% c( M! I/ z2 ?7 M 极, 2 ?" k* x0 w5 U/ _) U电子流流出的极位。+ A, Z) b' U4 a" ~1 c 极射线管,& r8 W% N" ]5 o* z7 J) Y% n b 有显象屏幕的真空玻璃管。用于显示信息。4 H& N- e7 T# q7 j8 W/ w8 u 云高(云底高),8 q" h3 b# ^& C& h. T( h9 s5 L% D, E 6000米(20,000英尺)以下已覆盖一半以上天空的最 - B5 S) u/ p# r) L5 H' U' W, P低云层底距离地面或水面的高度。9 d1 r& P/ {3 z. p, C# A3 b9 o in6 Z( o5 E2 X( U- J( v. ]8 [ C3 t& ^. @& n; V2 [7 n d! r) _0 C/ g6 z0 | C# [8 W$ @8 N3 I7 h1 |: E2 J7 ? fl / n2 Q& X: b6 R6 T% M& nC% ]) f' |. B! V1 |1 Q. x s ' X% r5 O# ]* J; i* G0 j' t! t9 \. uC % B" v' v' w5 w" `, Y( t% S2 Fviewing screen, used for displaying information. 9 p' p. r- T2 n/ D级联,8 K% E) Q; E! D: c, h( F, m! K. G 两个或两个以上的类似电路的逐级连接或放大过 : G5 [- m5 \& D& G6 h7 ~5 Z$ J# b# _" |. Q$ m1 @7 H6 J% S+ A7 w! _$ Z+ c1 D& E2 V8 }; u, l% E7 o" ~; y# n0 L 一个具. z8 V( ^; ]' a2 C, c0 M1 U" k 英汉对照民用航空词典B OEING # ], O- n5 E S5 v9 l( STECHNICAL DICTIONARY 28( y# }: Q, V! u2 h CELSIUS, A temperature scale in which zero is the # @# {1 l$ K4 ~freezing point of water and 100 is the boiling point of% Z1 y/ F) c8 U6 \5 U. i, e water.& ~" B$ i( N ^2 }5 [( t CENTER OF GRAVITY, The balance point of an object; i; _- T- k/ q9 u* T1 C6 F r rigid structure expressed in terms of percent Mean ! d+ ~$ m( k5 g- K5 h3 Q* K2 werodynamic Chord or in inches from a reference point. 8 \1 y9 c; L9 n; l5 s( G5 q- uENTERING CAM, A cam for moving a mechanism to a. R; E( u0 p1 L) G eutral position. 0 j% Y* i- B! a% d2 g3 H/ r8 [IGURATION, A configuration of the/ [' S3 Y8 F- _% \- Z ircraft approved for operation by the local governing ! V3 F: U- P' d5 o6 ]+ A, pgency. / J5 C+ r# g$ V$ _* y6 T# `2 h7 lENTRAL PROCESSING UNIT, In a computer or2 ^5 b7 x o: K& | r" N# @7 V igital circuit, the section containing the arithmetic and 5 M" L* U9 \3 `( Qgic,control, and internal memory circuits. 1 A, U5 }/ a; n8 T. l3 MENTRIFUGAL FLOW COMPRESSOR, A type of ) O! {: k1 t& c# B( L1 L8 F5 m$ @3 ^ompressor in which air is taken into the center of the 7 B8 {' J: j; V/ s! \: cpeller and is slung outward centrifugally into a diffuser ; c. S1 `1 k6 U# i7 @here it is slowed and pressure is increased.' _ B% d5 f! O; i CG, SEE - CENTER OF GRAVITY9 ~+ ^8 t/ y" D: Q0 H6 _- T! K 构的平衡点,以平均气动力弦的百分比或 1 x' z" T" F; P6 K8 S3 z某一参考点若干英寸来表示。& [* H$ x& W+ }/ \1 G/ ^: T 中凸轮,% R. i2 _& a- ]" I+ r 将机构移向中立位置的凸轮。 6 x$ A8 Z& I Y9 Y7 i格的装机状态, 2 m: o2 B! j. s* }7 B/ k$ a由当地主管单位批准使用的飞机装机状态。 ' v4 e) \4 A1 H4 |中央处理器, 0 B# E9 V j2 _* x( Y" a: c计算机或数字电路中含有运算,逻辑,控制和内部存: f2 @3 i- T: ]7 O. q7 G! c* p 储电路的部分。- t3 ~9 W+ {/ w* r3 _ 心式压气机, , S- _& v0 U1 D& {. J压气机的一种。当进气到达叶轮中心时,被叶轮离心抛 , \; j7 L5 A0 d进人扩散器。在扩散器中气体流速减慢,压力增加。 A% n! L& W9 N5 T, N5 Z, N重心,5 ]# m+ g8 Q8 `% {8 b3 l4 B 见Center of Gravity" x7 P3 }2 p1 U" ~3 X" I8 | o7 n/ \: T$ u s! h- L+ W! F' q) ~ A 1 F2 C) n' s" s4 E5 }9 Y* LC , E. T7 I/ {5 i6 A: v9 Dn- T1 R6 |/ \* s2 v8 d CERTIFIED CONF! \' o! i3 D7 N9 I3 Q. x6 W5 Z a- P( _; K& h. G2 n( O0 z* y3 C9 F2 D a " Q+ f- X$ F" X6 V) VC - |; X( z( V# @3 o3 `' G: o$ Xd $ ]7 i; u7 m* Z, C% Flo 5 E) _3 c; L% XC * A2 ^' S' v7 S/ J: i ?5 a& fc ' x# ?4 h: V; w2 G: j9 ?+ lim- ]- P! g. B9 w; H2 @* q w2 t" O& q5 ^: @+ s 摄氏度(°C), ) ^! O9 H/ k" f E+ V0 u4 D温度的度量单位。在此单位中,0°C表示水的冰点, % Z/ r/ ]" s" [0 B2 t* T3 X100°C表示沸点。7 T- u7 L( F' t: g 重心( N1 P9 C( Q) U( H- K: t1 q/ e9 R 物体或刚性结 " }3 R- w; Y1 v3 y# [1 ]: ]& I |) A7 ]/ P! n0 R* }5 K Q- Y% G! f% f: T8 C: V' J% s6 ^" [' I, {7 r5 I/ v; t4 a9 ]" ~/ ?4 t0 p! ~1 D& { D* d$ X( |5 ]英汉对照民用航空词典B OEING. W* x" m" {3 |0 _ TECHNICAL DICTIONARY 29: |2 }0 u' m: k6 A CHANGEOVER, Conversion from one mode to another.6 u# Y" u. X( [4 I5 J3 i7 n" s HARGING VALVE, A valve for supplying air or fluid to + f! V( l/ n3 l; w6 |5 j* h* tHECK VALVE, A valve allowing flow in only one$ g4 B7 u; ~+ [; M, B irection. See Non-Return Valve. 4 o, Z9 }, F% R% PHECKSUM, In a computer, a summation of digits or 6 k, y. Q i) T1 aits which are primarily used for error detection. 5 Q: \" X! Q2 y* C! r& S$ zHIP DETECTOR, A magnetic plug in sumps of) h+ Y9 m' `* ?" `" z bricated components for detection of internal failure of 0 k. o, w8 \1 ~+ ?4 Ze component. ) p) z" X( w! T, |$ b* `8 r5 Y+ Y8 KHORD, A structural component of spars or frames. - v' I1 ]( ^* A( F: p3 ~6 B$ j添活门, ( @5 {/ l0 W! K0 ^器充气或加液的活门。% t+ T6 e. G. s: r, k9 K8 n# Z1 e& G 单向活门,/ n6 z- b. ` s* _; v 仅容许单向流动的活门。见Non-Return Valve

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发表于 2008-12-24 21:38:05 |只看该作者
C! {1 u7 G' ?. R, H8 J4 f0 K k a reservoir. 1 r8 E' V3 Y9 w$ ]( p. MC- e* f6 b/ p0 y1 f2 s0 n d ! J9 X; P* {' l6 q( mC 8 {1 P7 a- W! ? Q8 _) _b8 ~1 L x, a3 R8 W F9 O C ) o& g1 t( ~0 {lu " Q5 H4 q. I8 b) ^th" f f/ H' o6 l& F* I C 2 o/ m6 x; S2 T3 ?/ f转换, 8 \5 G/ B" ~5 P2 J' m由一个方式转换到另一个方式。8 T$ L3 K9 a$ S+ y& K5 ?6 [7 ]* R U5 P* s$ \3 I 用来向储存) g; U3 E H9 B+ I: p2 [/ I% K! @5 N! d* L+ @总和校验,) D" A/ E* i! D 计算机中,把那些用来探错误的数宇或位数的总和进2 l" x7 f" N0 v% v# h 求和计算。7 ^8 z" k) b5 f! e! D& Y 属碎屑探测器,. F6 d1 g$ A# `$ r1 f# v5 u/ D4 J 装在被润滑的部件滑油回油管路上的磁性塞子。用来探' O1 J; f q" k1 |! F 部件内部有无损坏。$ ^' ^2 {9 [2 J- i, O2 B) n 弦,$ `: B5 k, D. A 梁或框架的结构部件。 * F; l" v7 s5 l% t/ N3 \; b# M- Q/ j6 b! H6 W" t3 Z' l) \8 O% r. e) ?5 T2 k# k: P+ I, {# R0 w- P; x) R/ W- x' v5 o) A% L$ p2 K- P# _2 t0 P 英汉对照民用航空词典B OEING' n/ n6 Y* s1 Y( a; l TECHNICAL DICTIONARY 304 _3 E3 O7 d6 C, l! s CIRCUIT, A closed path through which current flows# T8 _, z# j* h% q; P- _5 X ource. 9 g/ ]$ g; z, s9 `IRCUIT BREAKER, A device that automatically9 q# C c' L* h! w2 P& Y% c7 b) h! ] eactivate the system. 2 J: E& S0 c6 c& N9 hlear of all non-frangible objects which ( \3 n( s0 ^% k6 @' xay be used as takeoff distance available when . [7 `8 `" k, zalculating a takeoff weight.: L0 `* X- h6 C r water under the control of the appropriate ! H/ P2 C) R1 F8 K" p( tuthority,selected or prepared as a suitable area over & ?7 ]/ u$ L0 Ohich an aeroplane may make a portion of its initial 4 i& e- s% u0 C& {( C& Q9 Wlimb to a specified height.3 J2 R8 D8 B; u. y X, G7 V increasing. 1 X2 s) @, t" `1 o6 zsed . B* m# [5 F, y e9 `* f/ N+ N6 MLOCK SIGNAL, A continuous string of pulses used for8 u% k4 _6 u- {% p4 |% N 开关,- R* s4 ?& G- E 故障情况下自动中断电流以保护线路不受过电损% r( g; h' `: l. _2 M! c 体障碍物的区域。在计/ r2 ?, W/ K# K G5 W 起飞重量时该区域可作为可用起飞距离。 ! E7 v6 w: Z; D1 |7 S6 s是在有关当局管辖的地面或水域内一个界限明确的长/ X( k( `/ `4 |* H+ m% ^. n& ` 形区域。在这个选定的合适区域内,飞机可完成初始爬9 B6 k7 s ~! @6 J' z 的一部分,上升到一个指定高度。3 F( o: z, }1 f3 t 飞机高度不断增加的飞行阶段。( D* x9 {- ~* v9 M 钟脉冲,- C; t! h/ M( R# Z5 h! O 步的连续脉冲信号串。 : L) j2 T' g; p1 w/ Qfrom a source, through various components, and back& |( Z! |) |3 T0 F6 x2 \; A to the s ' f+ e8 b" `* [C( I) |2 Y0 n: ?5 a interrupts the flow of electricity (current) during fault ' r/ N n2 X2 T1 i$ E" ccondition to protect wiring from excess current. Circuit' [) B+ H/ N& r, r9 s T% n0 K breakers are also used as a means to manually7 X7 R& _* T& x7 } d9 K1 ? y8 @5 R8 A. E2 T0 Y CLEARWAY 1, An area beyond the takeoff end of the # r: n5 G! j" M: Q7 ~7 S y: Trunway which is c, Y g0 h! I } m 2 z6 k% |3 s' E7 b- [' ^1 z8 Y0 Rc $ ~ J0 y. s0 ?. dCLEARWAY 2, A defined rectangular area on the # \8 o6 l/ r/ v* u2 H Q! {0 o- I( Iground o7 D4 O3 v) \. n2 I$ m7 s a& p: a# j i3 Z& y w 8 c& l- x; P" mc7 h' P+ t* P) G) U( B8 E7 C CLIMB, Phase of flight where the altitude is: |4 _ m! c* r4 ]2 `% [% e8 w$ o CLIMB LIMIT WEIGHT, Maximum takeoff weight ba # v. W5 h* p& L% O6 don a minimum climb gradient with one engine$ z5 p5 @: I& s8 K inoperative. 7 q' C% w! ?3 T. V, G" IC + d3 L' o8 Z" w% x- } n# |* U' Ksynchronization. ! z. _6 ^5 w7 s; k' b9 j电路,+ s B0 n' G0 i7 N 一个闭合的回路。电流由源头流出,经过各个元件流回" Z S; H8 g- \' z+ k# } 源头。% c; p1 X3 z$ F6 c1 \8 g5 ~" Y能在 0 N& X& ?! \% q, \' C坏的装置。跳开关也可用于人工使系统无效。 W0 T5 g5 y; v9 [$ B9 s一号净空道,& {3 T, E4 R0 Q; Q9 V; x 是跑道起飞端以外,不含任何刚 - Q, ~% ~+ g: |# Q, c0 }7 K5 q' `5 {$ H1 k, h( |3 c/ F 二号净空道, ! B6 T$ `2 Q/ ]9 g/ _( V* d4 l/ a0 _* T, N0 @ c4 R/ M( T3 H- _5 _ 爬升, # |9 F! p" _" E# @爬升限重,; K# x; L/ ?( \& ` 取决于由一台发动机工作时的最低爬升梯度的最大起" v. V- r/ i. `5 I; d 飞重量。 " g+ n& I7 m! B0 ^0 d- m. e$ d- z9 C; ~ 用于同 / _5 E m" `& r5 U* z6 @英汉对照民用航空词典B OEING ' _* F6 T) E$ rTECHNICAL DICTIONARY 31 0 t3 Z' a1 {( a3 S5 h0 z* vCOALESCER, A device in the water separator for 5 L, L/ F) Y( K1 M( oollecting moisture from the cold air.4 M% z, E1 j7 S! } n antenna with a receiver or transmitter. " L% K9 U% x9 ?- o- Q0 s+ ?he cable has an inner conductor and an outer 1 P# I3 @7 m8 N1 h/ Y2 Lrounded shield.1 [, |, g$ M! t A; `* Z! a# P ting one inside the * |' p% C9 o* _. c+ Uther for rotating the low and high pressure- o# C3 ?; @8 n$ F ompressors by the low and high pressure engine 3 y, u& ?9 U0 S, K6 c, r$ ?rbines. & T, K, j/ |# J8 K# K8 t c8 m1 SOMBUSTION CHAMBER, A part of an engine for " p) \7 \/ M/ lurning fuel in the air supplied by the compressor. ; l; X9 l; i, O置。$ \, S- u( e, a2 d) }' a 射机的电缆。电缆( t6 B- I: \$ C, ` 中心导体和外层的屏蔽所组成。 + q1 ]- d; x! O- ?& E两个套在一起旋转的轴。用于使发动机低压和高压涡轮 8 T: }7 J0 h" p; q; n: F别带动低压和高压压气机。 5 B+ C/ p& \ A烧室, 7 z" P. S3 n9 e( @2 }/ q发动机的一部分。用来使燃油和压气机所提供的空气相 1 [8 R" M/ E* c) x合而燃烧。

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发表于 2008-12-24 21:38:35 |只看该作者
c4 G6 ?1 V0 B0 U' Q8 z6 K6 X. c# f- X COAXIAL CABLE, An electrical cable usually $ b% j. S# p+ e+ n7 Dconnecting a * n# ]( p6 n2 s% zT8 z$ E6 z, }; J0 M# \2 t g8 Q+ v. i2 T: ^! j' A; |, q COAXIAL SHAFT, Two shafts rota 6 b+ j! D% E0 x) go7 o4 \; Q# M. v5 x z c * J; W# J% d# Vtu * O% L5 Y' y! [7 I+ f7 U6 A5 PC" V1 I! v |) w0 h. { b / v0 O4 O$ N1 ]" g9 f2 |3 F, q- \凝聚器, ; `* e( p; n$ g& i$ ]水分离器内收集冷空气中水份的装; W) R X0 o! y! P( ?3 Z 同轴电缆,, o8 p+ c, ~2 j9 E9 m 一种通常用来联接天线与接收机或发 - b5 K3 m4 k1 V0 Q" o1 E# F9 ~+ c6 d6 m同心轴, 6 Z& ]7 h# [5 W0 B' Y1 Z3 w& L1 f3 a4 x" n3 X# }! {/ Q! J. w$ D9 m# v$ a8 y5 w, Y9 {+ w 英汉对照民用航空词典B OEING2 A: t$ j, G% s/ S3 S2 S TECHNICAL DICTIONARY 32* K6 x% r5 ~/ C5 W! x( ~- n COMMAND BAR, A flight director pitch or roll comman * P u) j8 ^, U- T2 M1 [indication. : h- @5 ?: P- P* k3 V, fd 0 m, K6 Q* S9 ~3 W _OMPANY ROUTE, A route flown by the airplane . z2 _. e7 B' d% p6 ~* XOMPASS LOCATOR, A low power, low or medium: ?- x% W" A w8 V6 {2 z equency (L/MF) radio beacon usually installed in; P! I; y6 ~; l/ X onjunction with the outer or middle marker of an" f/ `% }5 Y: e1 u1 f# W( ]- S- W+ e( X tor (LOM), A compass& x5 ^4 s$ Y6 u) c* L1 D3 E locator installed in conjunction with the outer* S, W. Q+ N4 a O! g/ B1 N! O9 ` s marker of an instrument landing system.! b+ v! N% w- r$ ?6 i* s/ s ss & n# f& ?/ c% S8 _le& _! {! Y) L3 t( X" g) F OMPENSATION, To offset, balance, or counteract. - f: Y% \$ T/ G/ Y$ V! fOMPENSATOR, A dual capacitor for changing the fuel9 @ n/ W0 I1 r% P7 n* E; c7 X& ? aging circuit capacitance due to changes in fuel ! L! N& C x* d- [4 C: ~$ g; `ensity. 1 a( _8 s& J: J, wOMPOSITE MATERIALS, Non-metallic materials used 9 [( T4 r) B5 n$ L, I+ P, Sr airplane construction. Fiberglass, Nomex, Kevlar, 1 f& I' f) U$ T# f1 X6 f5 K p3 ?raphite Epoxy are composite materials. ( F9 Y' c" h9 d- n% C; m. S司航路,5 w& D) p$ d9 [+ O* v% { 在飞行管理计算机数据库内由航空公司飞行 & r' b1 ^. C/ O! p' s盘定位台, 2 Y7 I/ o% q3 Y/ O4 G" q; G0 U与仪表着陆进近系统的远距或中距指点标配套安装的 # |! B* y0 x: f& }- h# M. ^, b功率、低频、或中频无线电信标装置(低功率NDB台)。6 I8 s% [$ [' v4 A: A1 Y 程序中用来导航。 8 \6 J" p3 Y; g/ }1.远台, 3 e0 h' ^0 O2 [与仪表着陆进近系统的远指点标配套安装的罗 , [% U5 }4 a% I; L0 }( o盘信标台(NDB)。 ) M R7 l. X9 L4 p偿,, C' l! U/ o; ~+ ?$ M 抵消、平衡、或中和。6 n% k9 ]+ u* b) o3 H 偿器, 5 s' ]) O5 ~7 g! n8 E/ X2 _* ]8 p在燃油计量电路中,用来改变电路上的电容,以与燃 - |3 B+ u+ j2 j5 ^. E* i0 x密度改变所引起的电容改变相抗衡的双电容器。 3 p4 T9 _+ y5 s- E# n合材料,$ `( G- o" l- Z 用于飞机制造的非金属材料。如纤维玻璃,Nomex, . G* k$ h+ K! u6 y1 f* i/ i$ S: mevlar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 + W6 e( ?4 ?" x# ]operator that is normally stored in the flight' H1 ?0 `5 [" t% o& V management computer's data base.* X9 t: P6 v& ?3 z8 [* ~ C% [6 C3 F: n. c5 U( [$ P fr : g/ @/ Z N1 v8 o( Hc9 A5 D, [" |8 y+ g8 S instrument landing system (ILS). It can be used for 2 ~- Q8 D7 ]$ [ E* n+ Dnavigation as authorized in the approach procedure. 6 d! ~' F7 K5 e1. Outer Compass Loca 2 W' `( \( E( ~1 L5 s2. Middle Compass Locator (LMM), A compa ' w7 \, e3 R. e3 q& U6 I+ U ylocator installed in conjunction with the midd/ f9 p1 I& U/ l$ D* q! \9 x marker of an instrument landing system.5 P g) F3 Z- | C ! y6 ^* y& Y4 K5 J1 ]$ D* eC 9 Z; G/ y# Z( N/ r8 g; wg0 F' \6 z% ^: c- U% ^ d. q3 R, w' W. M! Y# ]/ s C 1 H/ d+ p7 |' a* }0 Xfo. F3 Z* ?) A* o7 m g8 H# w0 Z6 ^% U! U 指令杆,+ M, [* S7 {/ F' ]9 T 飞行指引仪俯仰或坡度的指令显示。 7 A3 B- R& `& _, C8 R5 k3 x* P. q6 i- E+ u: ]/ X 通常储存" s' e" C, k: a/ @& W8 i 的航路。+ l: |( Y3 b0 D( B0 H ] p. V. E+ _' L# Q& Z- b5 F5 h [. }: X3 P4 `* j" p 经认可后在进近 9 P. S2 @ o. A1 T+ P4 U5 {2.中台," z/ Q; G# O$ e- ~; j+ k$ C) i3 S 与仪表着陆进近系统的中指点标配套安装的罗 9 `% b8 T/ l% A" m盘定位台(NDB)。 4 z4 g- K' E% F! |' r8 y b6 ~. f; t# p6 [- t7 M2 ?1 C! K) ?$ _; Q$ C, e, F% Y# k# H2 U* f) N' K9 Z/ O- R8 c. y3 z& E8 I: i5 M3 [K $ u' E8 g& V) W" d+ X+ ?4 J8 q) k英汉对照民用航空词典B OEING 4 ^0 T! ]8 ~! _9 s, WTECHNICAL DICTIONARY 33 5 Y/ V) _% d b' s) M5 p! o/ Q+ bby 7 v* v, I/ r! V- X: H- R$ Tor increasing air / F. d/ y! {6 g9 `- j8 d9 H. h3 Yressure and temperature before the air enters the $ W% z+ a, y% W' c# _ombustion chamber, Low pressure compressor - front+ _8 r7 b! j; h ection of compressor, High pressure compressor- rear 8 p4 V) t& q' s M. |. A: B. iOMPRESSOR STALL, An event that occurs when: t; X" ?1 }) g# E ere is a complete stoppage of air or reversal of air flow U3 m& t0 r; A7 r, L/ W& { COMPRESSOR SURGE, SEE - COMPRESSOR - R8 ]5 Q( n" ]4 uSTALL COMPUTED AIRSPEED, Indicated airspeed& ~; |1 U' n6 C! |+ `" L9 ` corrected for the static source error. : N8 d' z$ d( c6 p+ I) F的机械轴来驱 u% i% v8 |1 K- X: K,用来增加吸进空气之压力和温度,以供燃烧室使用。6 {7 L9 h$ b! x7 n3 Q 压压气机—压气机的前段,高压压气机—压气机的后( q" @ s. g/ k/ o8 D# ^" H/ J: n) I2 k r$ D' Z" F 气机失速,8 M/ w c, `! V. c5 L5 | 当气流完全停止或通过压气机时气流方向逆反的一种5 v+ G$ i9 @# @, X* M 压气机喘振, ) z$ p4 o" D" v$ u0 J见Compressor Stall6 q g9 _( V* _/ S7 U COMPRESSOR, A rotating part of an engine driven 9 _7 A+ D0 y: y. g2 x/ ~# ~/ aa mechanical shaft from the turbines f ) g+ N) L! P( R) q9 _& v2 np) ~! Z% L2 }' V, }8 o6 C! @ c 3 r% m. E. v/ h! n5 D5 ?s V. L' I' J1 E5 v) ^$ Y* A7 U section of compressor., q8 Q6 `# ^9 x7 s C # A0 _9 L3 J* _& \7 ?" Q1 y5 D6 E3 @3 D) n8 Sth ; o8 W7 y9 z( V; J/ _through the compressor.! \, x( y- P$ U8 x2 Y 压气机, $ R( N. |. O/ [' W( K0 d发动机内的一个旋转部件。由与涡轮相连& C- C5 b' N: i, V" }5 J) C- x9 C: C4 A( H0 E' j( Y2 @9 d4 e3 C/ a2 L* ~* M u) ?0 F/ Z5 \ O4 Y/ x) Z! t0 P- w- p现象。2 e/ v0 A6 t% |2 e' R' |, n& D' Z% h ~# [计算空速, & |6 K; N `/ r; m修正了静态源误差后的指示空速。6 p4 t+ c0 C6 x+ _" f 英汉对照民用航空词典B OEING : t/ U* K8 g4 N) m, Q c2 `TECHNICAL DICTIONARY 34

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发表于 2008-12-24 21:39:27 |只看该作者
COMPUTER, A device that performs arithmetic # }: v6 ?- \ ~2 Goperations, manipulates data, and makes decisions.7 m! I, f' S6 X7 y5 D! t ditioning 3 ?: U) ^' K2 w: dthe air and the! G c+ N& [# X) h0 k6 A frigerant or moisture vapor is changed into a liquid.! F% N8 ^; K4 R, v; Y( i ine . n2 J& ]9 y. C, n6 d' PONFIGURATION, The position of flight controls,/ \ s" |( s" Z! c3 s9 ?! b' K0 Y missing which 5 h# }: g5 i+ s" kmay affect the aerodynamic performance of the) B: n+ C# M8 S/ K% t airplane. / t* V$ W+ U8 w- ~置。 : a5 N" `2 c& s1 X: G! Q中能使热能散发到空气中,以及使冷冻剂或湿 / n& o+ }! w# n ?. q# \8 O2 E转变为液体的部件。4 X) Y2 z% R, p5 E3 I+ A 连接到飞机结构上。- R2 f5 {1 V s9 N% x5 c' o 态,/ D4 b7 ?, S- ` 定飞行阶段中,飞行操纵面,起落架等的位置。 / _# ?& ^3 n' g4 M6 W' K+ W), ) U8 `3 U* n6 `8 V4 d5 g受到影响。8 N: }6 u* S, s) {5 w" j( ~ CONDENSER, The component in an air con : Y" `6 d9 q: x1 nsystem where heat energy is given to" j* o. K$ }! e3 H7 i) [0 _4 z re 1 [) N- w( A) G' U, H% t `CONE BOLT, A bolt in the shape of a cone for eng 8 A6 G+ V0 k- @6 ^ ~attachment to the airplane structure. 8 O9 v [$ t( H$ ]7 Q2 M/ m7 AC + M7 y5 {: @' q0 C6 o+ _, flanding gear, etc., for a particular phase of flight, e.g., # O( _1 {& j1 o# ]# [Takeoff Configuration, Landing Configuration, etc.: K' Z) d/ r, [$ w" e CONFIGURATION DEVIATION LIST (CDL), Appendix5 @( L* ^& Z3 _9 b8 C in the Airplane Flight Manual (AFM) allowing operation 3 z+ l( D' j+ \; e4 n( ~7 g7 oof the airplane with certain airframe parts ! L- o" g S4 P' X, p" ]0 M计算机, * I7 \& y3 J) n: B6 K能作算数运算,数据操纵,和决策的装 0 I9 J" C, o1 W2 Y9 k3 @" z. a冷凝器,/ _1 `( u# j, E 空调系统& G' s% o* q+ p) j3 o/ {& L5 L- [7 P( Z6 c 锥形螺栓,. {3 _0 I8 Z: r X- U0 _! v 外形是锥形的螺栓,用以将发动机3 o8 k4 k3 w" i& z5 T) X+ ?% u" Q8 I( f2 A# _% b在某一特 / x$ R. G* X) b0 h3 n0 D0 S g如起飞形态,着陆形态等。/ l' \' O% c6 _# h& q% F 缺件单(CDL 4 ]* d9 z- C( H2 e, O, l( h" a飞机飞行手册的附录所开列的飞机上某些零件的清单。! E0 A0 ?- H. J/ ^. ^9 I- y9 m 在缺少这类零件时,可以飞行但气动性能可能 8 H2 S6 d/ G$ {2 W# L1 @: \; h英汉对照民用航空词典B OEING 2 D, ^4 {' }6 u( g: w `/ j' Q; Y9 pTECHNICAL DICTIONARY 35

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发表于 2008-12-24 21:39:49 |只看该作者
CONSTANT SPEED DRIVE, A hydro-mechanical - m0 o3 F4 m4 J: Q, e$ A) x' ycomponent for changing variable engine gearbox speed. g) K( j0 F9 q$ o6 I9 o ONTROL AXES, The three axes of the airplane which& ?, w7 O3 \& h& e3 t; ?. z re perpendicular to each other and pass through the . M A% ?4 `0 W/ [2 ^9 ?) F/ ~9 N9 l4 O: Benter of gravity of the airplane. / \0 `$ S0 Q- T+ fPitch axis - Horizontal or lateral axis, passes through: ]9 e% g' _) o L the airplane from one side to the other - / z) j$ E/ O! a$ Y5 Y5 ^nose up and nose down control is by 4 _1 h- p; q: Z% t; r) X. U6 R& Yelevators (and stabilizer for trim).% `2 \! b* Z6 a0 v8 B# Z' S( P Roll axis - Longitudinal axis, passes through the . L1 L5 e0 g0 F5 d T- c5 ^airplane from front to rear - wing up and " l5 t/ T& a' f: o& y( _3 ^wing down control is by ailerons and6 N0 O h d' t flight spoilers., M$ r4 a8 K Z# Z! e Yaw axis - Vertical axis, passes through the7 y( }3 Z& I* Q3 T+ |+ ~ airplane from top to bottom - left and 4 z \& Q4 b' @$ w5 x8 Wright control is by rudder. " q- q3 k; \/ @置,& k% d- m! O0 t0 ^- e* f( h 制轴, 6 f5 I5 e% N8 B4 I& O9 Y& f通过飞机重心互相垂直的三个轴。 y! x2 M% _: I* D& r& f俯仰轴—又称水平轴或横轴。由飞机的一侧通向另 8 Z: [" W, M+ t侧。飞机绕此轴转动即造成机首的俯与仰7 k0 `, R* z l5 [' o 俯仰控制是由升降舵来达成的,水平安定& Z9 \: @3 ~0 g- d# H1 H 则为配平之用。7 v$ r# t8 v5 k& e4 z% I 横滚轴—又称纵轴。由飞机的前部通向后部。机翼, p1 l0 Z' N+ ~) o# j- M5 |) f 下运动由副翼和飞行扰流板控制。( [; \$ h. [" s1 p# c' ]( j 偏航轴—又称垂直轴。由机身上方通向下方。飞机6 \- y3 v5 D& M' B1 u& D 此轴转动即造成机首之左右运动,此一运" t. M2 ]3 K- x7 s4 |: K3 D 由方向舵控制。 # b$ B2 C1 W- ~" R; _4 O- Dto constant speed to drive the electrical power. , ?4 `5 \# f' ~$ uC ; B9 O' t, h6 c( r: G! T( Sa % M7 d/ ?: Z$ \2 `5 s8 Kc. L% a( C; Z' c. L 恒速驱动装& \5 s2 M/ P# P4 C) h* v 将发动机齿轮箱的可变转速转变为恒速以驱动电源的 J9 B# F P# `4 f 液压机械式部件。5 S0 r9 t* S; \5 _+ H; ?4 K2 G, b( j% b, P/ O& F7 a: i+ J* b* j+ H0 p' l' t6 u1 `& ^+ d! z2 @2 q* \, D5 L; B; H4 I* P" N+ R6 a$ A1 _, D3 l6 R% u% _3 t* H- o8 Q2 q) a0 [, Y. `. }) a/ M' W# z4 N 英汉对照民用航空词典B OEING 3 W) |( ?1 L$ E6 g. Y& y1 y6 rTECHNICAL DICTIONARY 361 v2 K" k4 Y; @' U; @ g) ` CONTROL COLUMN, A mechanical component used$ W0 x/ D7 N* l2 j: r- C" ?: [ rs! c4 |' f) t# e2 I" c) P, z4 M nd elevators.' d0 k; y6 o: t3 P5 R ONTROL SURFACE, Moveable panels on wings and $ E/ |' ?! {7 {' uil for movement of airplane on pitch, roll and yaw axes. : s7 Q! k1 T+ X; l; {ONTROL TAB, SEE - BALANCE TAB ' l, H0 g X' d8 F" w: e1 Z0 i' hONTROL AREA, A controlled airspace extending6 v" r8 Q- _+ ^; h pwards from a specified limit above the earth./ i P1 O$ ^$ ]) U& e7 C ONTROL ZONE, A controlled airspace extending 4 V1 h$ d, c- v1 }* O; Jpwards from the surface of the earth to a specified' J+ m. h" \+ K! F pper limit." x) n$ u) u0 y% @9 ?8 v8 [7 | is1 M8 r8 `1 C$ b0 X6 f2 T o IFR flights and to VFR flights in accordance ! k, W% R) G! L, M( Twith the airspace classification.7 @/ C2 u( u3 O7 O 机械部 " Z/ l! U" Y3 L% T4 n! J6 A0 I* _- d0 C! r9 _操纵面, 9 T7 p) v2 x5 X- ]4 W/ _- E5 r2 W机翼和机尾上的可动面板,用以操纵飞机俯仰,坡度,7 U G; ^* }3 [8 {# s. J" o 和偏航运动。 & v, y" r7 y3 j" W) w操纵片,9 g+ N# h! T& g/ h 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 spoile0 F$ y$ u6 P; q% O* Y a; C1 G' H1 k5 M7 G5 E9 w C/ J# e @. I1 _$ ^! c7 O4 l ta 5 h) W* Y ]1 RC% t, O# @8 n& w2 t; Y) {& y; \2 M C / Y }$ g& y6 B/ ju2 _5 S# P% z# b- e7 B C : n% l3 @5 d* g1 o8 v( X% X) Wu $ f. y5 R* ~* M* Ou; l& [* E4 a5 P8 ?) W CONTROLLED AIRSPACE, An airspace of defined % J3 e+ S2 G' w Q) ^* V R" kdimensions within which air traffic control service ~8 _" B% t" f5 l5 E. b3 jprovided t9 m" j+ {# ^+ q& T. q 驾驶杆,' ?4 _; @, W0 T8 l: u! Y9 S 飞行员用来操纵副翼、飞行扰流板和升降舵的, C5 J& Q! g* f) J( K" M9 D7 {0 D; @! I2 o8 e" A. @1 A管制区域, 1 A) A+ c2 n4 w高于地面的指定极限以上的受管制的空域。 - s7 E7 u3 t E P# c J: i制范围,/ n. @0 A; ^/ B" D) E" u$ D, a' Z 由地面到指定的高度以内的受管制的空域。 , R1 ~6 L& S. F0 M2 M* E [一个范围明确的空域。在该空域内,仪表飞行规则飞行 6 [# |; j; G: D* K1 m! o. i1 X和目视飞行规则飞行有空中交通管制服务。9 f; M3 h+ C$ I H' v2 s! }1 P) B" z! }受管制空域, + O8 ~+ S, B2 O. Z; R英汉对照民用航空词典B OEING # P0 u4 s( y8 xTECHNICAL DICTIONARY 37 4 |+ |7 O7 M1 i( @3 d* _/ B7 R+ xCONVERSION, To change into another form. `2 \ G) c/ D9 i: ~7 \, aCOORDINATES, The intersection of lines of reference, 6 l: ?! R/ t2 k3 n1 f4 ]sually expressed in degrees/minutes/tenths of minutes ) X3 S$ M+ ^9 {f latitude and longitude, used to determine position or 9 t+ Y: h; v! b, d3 r: d) sCO # |' j' e" X9 L1 ndestruction of th% A! m# l, c( d& ?3 q8 x/ ~ chemical conta; W; m1 [2 Q$ V. L- ^! g/ p) J9 ~ COWL, A remo W& i7 A$ v( D for access to th( T9 L1 F: \1 f5 [4 o Fa) Y- F3 m# M+ S Nose Cowl - Front section of the nacelle for air inlet 9 M4 E1 V4 `/ ?. ?; dto the engine.) }5 ]' ?- D8 h4 w6 [& |! R7 m Side Cowl - Cover around the sides of the engine.' c& J9 N$ M0 [0 r% v9 z6 x Thrust Reverser Cowl - Cover around the core* A: Y7 A$ K0 x, P4 d- V$ C section.8 }8 N* A3 S+ U; F& j- l7 ~ Translating Cowl -The moveable outer portion of the9 Y) T- W$ q' s3 M& ^ thrust reverser cowl which is ; `' X, D4 y: H, @# p$ uoperated during reverse thrust. 5 B6 ~2 j4 {; J" }5 ~1 z标," S. ]* A* w5 @ 基准线的相交点。一般以经纬度的度/分/十分之一分5 e6 y" e" ]; k! D& O 读数来确定位置和方位。" o+ Q! F7 M# P/ Y( y, r5 P. j 腐蚀 - m n3 Q, d8 n4 `, Q" q9 J动机外部可拆除的罩子。发动机上的构件必须要取下 6 C8 Q! P' S4 Z- \流罩后,才能够到。5 Y. S) @$ u2 w: [2 P/ E& G: u" \; r ^/ } x8 }5 v 机的短舱的前段。 & l: ?0 V9 c4 v! b( j- M8 q0 b侧整流罩一发动机两侧的罩子。' T9 }$ w" Q+ F' r% ^ 反推整流罩一发动机主体外的罩子。 , o _1 k- R- n6 x( E) x移动整流罩一反推整流罩外可移动的部份,在反推工 : T% e' Q/ D* i- }, f! a& I作时使用。 F9 l) H- ~% au# i, P: G' S5 g+ b) P$ Y o . I3 W+ ?% h' g- u8 Z! Olocation." A% E" m+ A% N8 E# V( m. R; C RROSION, A chemical action which causes gradual; I, [- x3 c1 Y% b: B3 E e surface of a metal by oxidation or! l& ~/ g3 ^& \7 z mination.8 B& O" D: o* v* t) j vable cover around the engine sections " f% Z) H4 v' y6 xe components on the engine. ) x r! L* v- r8 j/ hn Cowl - Cover around the fan section. - |- g' {* a( z' I转换,( m. i% }( X, p5 I* ] 改换到另一个方式。1 O' ?$ A' z0 M2 z- ]2 O6 ], U+ Z; X W+ }; ` y8 _) ?; X! {; {% R& ]$ b) U. `4 ~6 \: q2 ^氧化或化学污染造成金属表面逐渐破坏的化学反应。 # q) |' J. P, [- c. T! k: y发动机整流罩, 3 {8 d- Q# P7 p- C Z. R# M4 B; J$ [* S8 O- U1 a T1 u% w$ I5 ~2 Y D% t$ A1 U% X扇整流罩一风扇外围的罩子。0 M R) q: z- K; y2 k+ O; _& g 前整流罩一引导空气进人发动 # ^/ `5 C w, K英汉对照民用航空词典B OEING & C9 @8 T' V: H; p- I j6 HTECHNICAL DICTIONARY 382 z6 X& w/ E+ k. u CPU, SEE - CENTRAL PROCESSING UNIT 3 T, \; W! D5 I, MCROSS TRACK, At 90 degrees from the desired track + V; z! Z5 h6 z: l9 g0 if the airplane. For example, cross track distance is the 1 Y4 ?# d5 ]- I" V8 S4 g; j' H" }istance from the desired track measured 90 degrees 1 S9 ^6 i3 U7 }9 j4 I8 hom the desired track. ( }6 k6 N0 a$ G5 ?1 w6 wROSS-CHANNEL, Electrical wire(s) connected from1 z1 P0 _. j" M4 l9 I# p ne system to another like system, for example, FCC - ^' d G0 O- {6 Y" to FCC "B". 9 Y" q* ~2 \! R$ }* d8 H. Hn adjacent engine or one on the other side.& w* t8 n& I' P- p$ Z7 \: J o l crossfeed, T7 |( W& l) [+ s anifold for fuel flow from one side of the airplane to the+ H* M: ^0 o# l& D; D* T ther side. $ [1 O$ I/ Z+ K$ j9 Vre+ g" \ D4 l4 ?/ K RUISE ALTITUDE, An altitude or flight level6 }2 j: O) f$ q) a5 Y' j( q( {! _) eo! R- N1 V! c2 Z4 p9 J0 k d ' A* {1 [( ~7 X l4 W' b$ x. Sfr " i g; Y' W* h; N' n4 C% PC 5 M. l- i! N6 }1 D1 ~5 {/ yo8 ]4 {) t# R# o "A b( C' S3 A$ b6 z. y8 K0 E* tCROSSFEED, An interconnection between fuel * U8 ^: C: E ~, U) E* w, Zmanifolds for fuel flow from one side of the airplane to: a1 t2 T- Z) \ a8 H. ^8 O4 T: i! h" ^ |8 B6 W) z CROSSFEED VALVE, A valve in the fue% | W) z* b3 I$ u& @% ?, [ m' X: k2 L6 Z; M1 B) E8 p o& A% F j) y# i+ h$ \ CRT, SEE - CATHODE RAY TUBE7 w% F( J9 x! D, q9 u CRUISE, Phase of flight where altitude and speed a) | @; v. L( h1 Q9 a/ _; L basically constant.3 l* I6 L8 d# h G) T C ' y/ C% U/ N7 e8 Z. tmaintained during enroute level flight. : X5 B+ A3 p, N中央处理器 $ v2 ^! [7 \) N3 ^5 m见Central Processing Unit. 5 D# A7 X9 D# c* p9 v交叉航迹(XTK), . X9 U. T# `4 J1 O# H* |' X9 s( j与飞机预计航迹成90°角的航迹。例如,交叉航迹距离 + ?$ Q5 ~/ f3 b& K* |" g是用与预计航迹成90°角量取的到预计航迹的距离。5 i! A( V6 C) n( W 通道跨接, ! _; h3 P5 M" x' Z0 b9 T电线由一个系统接到另一个类似系统。例如:由FCC 9 Y8 ^0 |. k& O; t“A”. C* n; F! d" j% N& g3 k8 C4 |) D: u 接到FCC“B”.6 l7 k3 g& b8 T5 Q3 X 机身另一侧的发动机。 ; b: q+ {9 V: ?于使燃油从飞机的一侧 5 g" ?, q3 V7 B向另一侧。4 @$ J; B# J2 H" F$ O& m! b; f+ M 见Cathode Ray Tube 7 n( `6 V' p; ^& t% C- f交输,- Q1 `7 K5 r* R9 y+ J- Q( _ 燃油支管之间的交连设备。可使燃油从飞机一侧流向邻0 `7 B) v# d7 {- f. F% r( b 近的发动机或在9 y& O8 ~) p) x+ q+ r 交输活门,8 K* [7 D) i. K' B 燃油交输支管内的一个活门。用' l& e! v8 P+ B( P1 M8 M# \9 ~2 ?% _6 W$ B阴极射线管, e9 Z9 v( n- }0 E- R6 R . z2 c* F/ W. k 阶段。 e3 d7 p: k/ v9 j2 r+ Q; Q航高度,5 L) L& H5 a7 a. q2 C. q 飞行期间,飞机所保持的高度或飞行高6 R- K; y0 c3 l6 l2 X5 o+ P 巡航, 6 D0 ^* A L9 ^* f# {飞机的高度和速度基本上没有什么变化的飞行 3 j- m7 P( D9 c( l) g" C# ^4 E) c2 m( }在航线上水平 7 Q# f* A7 n+ e度层。 ; Q8 R5 o: x1 I/ k8 l2 p% q英汉对照民用航空词典B OEING . v, Y% u. ]8 a7 m: eTECHNICAL DICTIONARY 39 7 {' P' Y5 [) t& \6 P8 ^CSD, SEE - CONSTANT SPEED DRIVE% o+ q5 p7 l' v& \* z/ q. U CURE, A chemical change which takes place in a resin5 m' T& `/ M( a8 @$ u and fiber based component causing it to solidify. ) D, o; x7 @* r5 Q9 S3 pCYCLE, A complete series of events that take place5 p/ S3 J6 y8 [+ W/ O9 c gularly normally in a continual sequence./ Y# M- k9 @0 ^9 ~1 R4 C# O AMPER, A device for slowing down or limiting % A$ U4 R4 m( E9 l, D2 I( HDASHPOT A mechanical damper for slowing down% G% J0 N) e# H4 M- `; |3 ` ovement by restricting fluid flow. * r0 g F+ K$ r* ]5 J9 h3 k+ qD 4 X$ t) e, h8 hATA BASE, Stored information which is used as the * P( `- w7 K" h! A& \$ M( h/ {. Jba 0 Y: C2 @* Z5 ?& a4 c+ v! LDATA BUS, A conductor over which digital data is .- Z2 E5 T7 t! K! o- W O transmitted. / C7 l2 `3 w8 i& J; j, BDECELERATION, To decrease in velocity. 3 _, f u& x. @; v% Y3 o装置,$ K6 C& A* X, z" I5 V+ ^$ | rive% v8 [2 V1 |9 G, X re / Q2 p4 I$ |) s' R5 oD% Q7 L# g6 `8 W$ m, I& v D . ~: R. }" B, v+ c& Nmovement. 4 a5 a3 b: E7 a I, J: [( xm 4 K$ w u' B2 G* x, s( WATA, Another name for information.3 a1 F4 T) O% t! |6 D D9 c& j6 k! _# P' V sis for computation. ) W- r( ^# Y: X5 N恒速驱动, ?+ c* b5 u5 J2 i0 D9 R 见Constant Speed D . ; n, J0 c7 q$ y期,. C" x- D! R! L 不断重复发生的事件的一个完整系列。 7 w6 u) p% |. i3 O尼器,, k E/ n3 Y6 q: B 慢的一种机构。 , `4 n2 f; P5 Q0 |2 A1 B9 i) @9 D$ g5 V' k0 m1 p+ F 用限制液体流动的方法以减慢物体运动的机械式阻) g8 }: k* g& l1 V5 a' q2 z6 ?3 d2 I- N$ q0 D! w8 m* ?0 W7 A& b5 l料的另一名称。- o# H+ c( j9 _! X 据库,% e; K5 Q9 l1 h E e7 x 数据总线, , t/ J, N& ~: E一条或一对导线,用来传输数字信息的通道。 2 x; H) D( J& \9 _减速, 0 d- ?/ O0 i6 @/ x速度随时间的递减量。 / X2 n |0 j1 f9 N6 }9 V, O固化, " w* b$ F9 V7 f! N: a) G树脂和纤维部件内化学反应使之成为固体的变化过程。 " V4 y. B2 p( [9 _0 E& B# Y1 O8 y# w9 @) g/ Q9 m+ h$ G9 N 用来使运动减 * _5 ?8 l) P) @+ }7 E; O冲器, 0 M) G6 d# m4 k3 n1 b! i1 c器。" E7 C1 {" l% ~; e2 C) W2 e 据,; R0 W& o/ i+ v8 X3 A' A8 P5 @) @( V* y: k( w0 x6 M/ Z" M6 l0 Y. x储存起来以便在计算时使用的资料。 / E# X6 h- c& ~" G" g* V英汉对照民用航空词典B OEING ; B( n" J# R0 \' f( E, fTECHNICAL DICTIONARY 40- t3 h/ U2 b B9 J z! u DECIBEL (db), A unit of gain derived by computing the* `$ i6 A( h8 C+ H tio of input power to output power. + t& {5 o; i8 } m5 D' }$ h4 ~ECISION ALTITUDE/HEIGHT (DA/H), A specified # V* j- K' n) T$ x& ], E8 Sltitude or height (A/H) in the precision approach at % z8 c% d. Y/ X+ o$ d4 ?2 R4 z% bhich a missed approach must be initiated if the+ }5 v, x' z5 m& i! f ECISION HEIGHT (DH) 1, With respect to the0 ~8 U$ L' g3 A7 K proach or 2 I$ P' t5 B7 D% }+ j' vexecute a missed approach.: r; x( q$ T) z8 l proach to trigger the decision of either . ~% V0 I) y* o0 t. N, lnding or go-around.4 }& S- R3 x1 m ECOMPRESSION, The loss of internal aircraft air* d1 d/ K! {, X( d, K ressure.- \( f! C3 b2 E: T9 I, o E-ENERGIZE, To turn off or cause to not operate. - ?' G& F( T* R5 ]6 x: _% ^6 vrom the tanks+ b5 U1 J, \9 P! \ using airplane fuel pumps or external suction. ! f% O. q+ e( Q: O+ [) d算的一个增量单位。分贝 ( H3 e) n( w/ W. N7 V' i; N# W9 n5 C常表示两个声音信号或电力信号在功率或强度方面的6 V- g! Y2 M J0 H1 B5 z' r 对差别的单位,相当于两个水平的比率的常用对数的十 8 N% Z, u) Q& X; a6 z断高度/高(DA/H), ! _! i! q" ^7 [在继续进近必需的目视参考没有建立的情况下开始复 . d$ r$ O0 Q2 S% I的精密进近中的一个指定高度或高(A/H)。- b4 h0 \% e# [' S1 Z3 [ 断高(DH)1, : ?4 e$ N6 \7 W0 Q. x2 ^2 |. d操纵而论,指在使用仪表着陆系统或精密着陆雷- J% s) t; d. P" k! b, x 生继续着陆还是复飞决定的高。" N7 O4 B/ i, O. h9 G0 A 飞机失去内部空气压力。 6 W$ g9 G% Y; M+ d3 N8 y+ g开, ! _% d* t( b9 O9 W+ _关断或使不工作。 * D- D- t" \7 d4 A机的油泵或外部的吸油装置将燃油从燃油箱排 ; ^# {) U8 x' R" [: r1 c出的方法。3 f& h1 k7 s* n9 s ra/ K# r' p2 g/ h! V) j" q D ) V+ m1 e, u2 ta 0 b0 b: F" z4 P/ N! E8 ^4 rw6 l9 o- y) K6 i1 p5 M required visual reference to continue the approach has' s6 D1 _2 m& E not been established.2 x4 O& |, g6 Z( X! z% R D- G& e2 e- m9 s. A5 A/ b operation of aircraft, means the height at which a! a2 d$ C" a8 ]! U% o decision must be made, during an ILS or PAR3 r, R2 q2 b |! q' p instrument approach, to either continue the ap! p& j" x9 k; o0 { to% Y2 K( s& |' @. C8 g5 B: W, k DECISION HEIGHT (DH) 2, An altitude used during a " l( X& y2 ^3 J( U& Z+ Kprecision ap : y# s7 ^" a1 B3 B, X0 m; S" Y+ dla: Q- J# H1 U/ r9 J D4 T, Y/ N4 J7 g8 B p / U* |' f0 m" `, QD L! g' N- `! N6 L5 H5 W0 K3 x DEFUEL, A method for removing fuel f) X- M: a1 }( Q2 d 分贝, ; e1 L \7 p) N3 K3 c* G以输人与输出功率的比率来推7 |+ ]& _) P- Z& l0 W& y" {$ T; _ l% }4 G6 w+ Z1 z8 ?7 J- i6 _% Z; z6 I7 O( l& C" j- }5 W0 Q7 B) N6 Y) x( V. o& Q0 P( W4 F$ h6 [$ U6 m+ ]' k( B1 r( `, C' U6 _* I% T q就飞机3 {0 B6 n* D3 D* r' ? 达引导进近时,必须要作出的是继续进近,还是中断进场 2 o* C2 U5 A2 }. v; @. R. ~4 P/ \复飞决定时的高。, B# [4 a3 e' \* T# D 决断高(DH)2,4 O7 n% R; n7 s* I0 _8 v 精密进近时产 ; {$ S5 H) d* p# O; `& `$ L失压,2 e4 p+ C8 V7 B& K8 y7 H% S! v+ W- \7 C0 }) _4 i0 B4 n 排油,8 ~: Z$ t. s8 B. t8 K0 D 用飞 ( X+ O$ l. Q# C7 {英汉对照民用航空词典B OEING ! R5 W2 B& N6 Y1 H. z" CTECHNICAL DICTIONARY 41& ^2 ~% y+ K: f" B5 w DEFUELING VALVE, A valve in the fuel system for( v5 M! H8 ?; T# I' W efueling the tanks and for transferring fuel between the % i, @) |/ x9 W& K3 W7 @) xE-ICING, Removing ice after it has formed on aircraft. : `6 M' g0 M h# WChange or difference. . y4 ^3 A" n- g1 `5 ^4 QEPARTURE CONTROL, A function of an approach ) b4 k! i0 Z/ e. K. iontrol facility providing air traffic control service for 4 o2 n# ]7 I- }" U9 i& Meparting IFR and, under certain conditions, VFR $ n* p/ v( O: N( U3 ]6 F7 U, j: g3 bEMODULATION, The process of retrieving information! v- k! j. o% V! { {& a8 V2 { carrier voltage.3 A4 r: {7 X2 f0 b( Q2 S ation. , U1 D$ a, W3 q) glic" R' v3 A6 C3 F7 L' h creasing hydraulic reservoir air pressure to - P6 ]* P- M7 Lmbient pressure.5 [9 x9 S6 l4 n [5 H9 t) b 箱排油和在燃油箱之间' n" S* t: O& O7 E 送燃油。 F! G, {. |1 ] 冰, + ]1 e$ ? S6 p1 v9 Z) c除去已凝结在飞机上的冰。 - X# x6 Z) H& f; @& M删去或取消。5 ]7 o. W. }% U' }& h n 量, - Y L, ^% t( ^' p' e# R变化或差异。 + A/ A: E9 P. g; Q* F; V! j/ O场控制,( Q7 l- m$ a5 E: t D* y% C: } 给用仪表飞行规则离场,和在某种情况下用目视飞行& B" n8 B: F1 @ 则离场的飞机提供空中交通管制服务的进近管制设施 # V9 L4 e2 w3 Q0 Z" L) x0 _+ r9 |5 i) x- n" ?5 i/ w9 W+ H2 ^ 调, * J+ k9 K& w. h. U- a2 O电压中获得调制电压的处理过程。 + ?% g1 E2 D8 X, x% L/ q环境. G: c- i& h, C3 ?6 t) o 力相同的活门。, k2 B& C3 M8 e+ X5 X8 F# P6 y3 h d . i6 K- d7 {9 H z7 |tanks. & j. \" W% f" H4 RD% A1 Q; p0 R4 p0 g DELETE, To remove or cancel. ( y t Z. o; k# l/ l; s/ R6 v6 WDELTA,$ t/ S+ y! p W5 { D- {9 ]+ H! S( w& l/ {% P c3 A, Z% J/ n3 C# y5 L/ b d $ B4 |& c- _8 E! saircraft." u8 d' z0 h, A; q, k D " H7 F2 f. W: `/ }: Z(modulation) voltage from a modulated$ J* @/ S, M' F* ~! r/ L DEMODULATOR, A device or circuit which performs8 s4 e0 s; e; W' L) G+ {: M the process of demodul 4 o! s( Y( ^1 r+ f- ?1 E: F) e& YDEPRESSURIZATION VALVE, A valve in the hydrau: n V' y: m8 _( ?: w: ~0 n/ m2 O system for de& K3 R& s# ~; Z |) j6 E% z* g a! Y, ~& j3 w# D% G4 W" i5 w7 Y 排油活门,! K# r$ }" O9 w! A/ _0 F, l 燃油系统中的活门。用以为燃油) O3 K/ E/ v* N+ T( y7 d& I( c$ F6 i. n" s3 U6 X2 S6 x, V5 n7 q% q! `4 j4 W4 @+ E 删除,3 v+ u% r+ u9 }9 Z: W4 } i+ \( t0 ~3 z: j! r; H* M. N$ u% G) e/ S& S& g+ S6 u: {( V 的一种功能 7 V, d6 i" ~3 [$ Q# @6 m G' O$ \5 P. ?7 _, B' t 从载波 1 Z- S. D" @" M- s解调器, 4 t0 [+ j: p1 @) Y# E完成解调过程的装置或电路。! |& Q2 s/ X5 t 减压阀, 1 z B/ t! O7 C! S' U' r8 T在液压系统中,将液压油箱空气压力减至与周围: D. p% e+ U9 O' n' V' K3 F m: @, C# z8 g. g/ R- ^) x# |英汉对照民用航空词典B OEING # w7 z$ C8 z/ E# d; mTECHNICAL DICTIONARY 42 ' E" c8 u, Q) y t/ B) t* ADESCENT, Phase of flight where altitude is decreasing./ @+ q5 l* ?: b' K ETAILED FLIGHT PLANNING, The calculation of fuel3 G! L) b; a6 O3 m1 s2 ~ nd required for a trip by considering each phase of! D5 G# A% W5 d$ g ight (climb, cruise, descent, reserves).0 x8 F# R) K+ f6 m% T al or 7 h# Q9 i/ j0 y4 t/ L# cETENT SOLENOID, An electrical solenoid used for 9 C0 u9 a |% g2 o2 ut., I: y2 |1 z0 N1 E! I1 M8 _ specified course or / d) Z3 F9 t3 I; V0 D$ Erocedure. # g0 @% P0 b$ V6 }/ G3 P( [+ ce.* ?& y9 c: Y) T+ u% m- y4 A/ I* d 飞行计划,. \- U* l; _$ t9 I( c 将航班中的每个阶段(如爬升,巡航,下降,备降)都 0 b) P+ F! a) _* F$ ?( S! z" ^. F* P, m2 V人考虑,来计算该航班所需要的燃油量。 * b/ N# C+ |4 P& f) O用来感应情况之正常与否的电气装置。7 e9 G; K6 B2 `$ p 定电磁线圈, n2 Z# m( Z. [: X 出接通的电磁线圈。 3 C% t: L( k1 g$ d" v) q差, : E- I9 u' s9 i. C与指定的航道或程序之差。 0 P4 X0 M; u- W用气压或液压操作的活门机构中的柔性部件。& m2 _6 ]# q4 w( F6 V D; U, a, V; p% [ K& p3 w a 5 }" T7 j+ s2 v. T( V* Qfl3 v: D+ H, e$ |$ m1 _ DETECTOR, An electrical device for sensing norm- x5 k! `: t& j% p1 A( W abnormal conditions. & Z* A3 j; S8 F+ S3 JD, h4 v9 I4 K6 `# |- R controlling the engagement of the actuator outpu 6 I9 a$ Z3 [' W3 dDEVIATION, To change from a$ c6 W$ j% a; }, [( D" D p9 d% H8 F- F$ h, E9 v1 h8 a DIAPHRAGM, A flexible part for operating a valve1 D" R$ [4 _/ @+ R, c mechanism by pressur E% O) A# [0 ^/ I' l7 l% h0 E- d下降,& o. B$ W) ~8 }7 Z 飞机高度不断降低的飞行阶段。 4 |2 \: @" T: _详细0 S y. C; r# t! {; I8 N4 v! ^; p0 ]* e7 ]- S+ K7 }2 \# D( b 探测器, 4 S! N4 X5 `+ n9 F1 c |7 n; g4 X+ _3 y, i6 C 用于控制作动器输 # P' t7 W; e. L4 F9 ~8 s. k+ B7 R4 y* @7 B' ` 隔膜, 2 v( ^4 u2 W+ A/ p& P+ t* Q英汉对照民用航空词典B OEING& ]8 n0 R% l, R5 l( U TECHNICAL DICTIONARY 43 5 w6 b" ~ O+ R- _DIELECTRIC, A material which does not conduct; k2 a, l3 K6 }. e electricity and used between the plates of a capacitor9 _0 H8 Z+ ~; o. L% T, T) B4 R( S (condenser). 1 Q# z1 f$ H+ S/ h) Hnother pressure in the same system, measured in 8 c( B' w' n! Uounds per square inch differential (psid). 3 f) F8 _9 K+ q, J8 DIFFUSER, A part of an engine between the( _ }' `5 p: M% ]2 |& h1 m ompressor and combustion chamber for reducing the: X2 h ^2 L( L- [3 U) m/ g; S/ X air pressure.9 r9 T+ j* W% B) f5 T \ igh2 c& R$ s. f% ]& J& S- I( C2 t pulses. 8 d! B, j9 m$ o/ k3 cignal that is a close approximation of the original 8 c2 [1 ]. q! s4 k; ^$ Q' X) ?$ L& j3 iignal. ; m+ j& ]3 c- |5 WIHEDRAL, The angle between the wing reference4 S: o$ d, a* v lane and water line./ f3 n+ T, E) j% g 的压力,以每平方英寸 ! R5 B" ^6 w4 a6 S' \, Z, L少磅压差计算(psid)。. G+ g( w) _* D; f 散器, " f3 B/ w; G2 w5 f发动机内压气机和燃烧室间的一个部件,用来降低空 5 ]' N, ]8 t* f; L6 p/ N增高空气压力。 9 Z6 b" v7 o! Q# b1 O换,9 }! \! ?4 {+ Y$ Q0 U$ N 的连续可 9 q% p4 c8 V2 s: d2 l(模拟)信号的处理过程。 4 J6 A# n, n9 i5 z# n' j2 Y$ m* [反角,/ O: v1 x+ \0 h, ^4 P Z$ G 机翼基准面与水线之间的夹角。 + X1 ~0 E( A6 v0 U6 p6 TDIFFERENTIAL PRESSURE, Pressure relative to, ~- h b- F8 C a # k8 j8 L8 R- |1 Z$ L/ ]p 9 ?7 O# i% Q7 M j; BD8 \- B, S. Q. N8 v7 z1 \ c ' I# b1 z6 e! jairflow speed and increasing the0 y3 |' ?+ P$ f8 g2 }+ i DIGITAL, Digital refers to a signal whose amplitude ' G* y; t% P0 iremains constant for a finite period of time. Digital 2 D, w6 L4 g' j0 V- msignals are commonly represented as a series of h6 u; u+ U1 _1 {+ X3 m! F and low, z. X4 }4 I' a8 ?) i& M DIGITAL-TO-ANALOG, The process of converting a, m, a) i, p9 n" b5 T& g% r digital signal (binary) to a continuously variable (analog) 1 L4 T/ H3 ^5 k) T5 {s; p# c) ]% N2 j# C2 v: }. {% V s; r1 m5 |! i. i9 ^; E8 w2 i D5 E1 B2 g; ~% D1 K" X# @ p/ f* B8 h$ w4 m& H- F' r0 b 电介质,5 v- f) R6 g0 h8 T" q1 M: Y 一种用于电容器板之间的不导电的材料。1 G2 Y# m3 l+ e% X 压差,4 e2 Q# h+ l ] 相对于同一系统内另一个压力 ; O4 |+ t* L7 Y7 x6 k: A. e @' B: T; @) \& K# J- `8 f3 ?) I" d$ n, U8 }, C1 X* [6 T 气流速并 w) n8 m9 y" L4 E& I 数字式, 7 r0 Q3 ]0 ?* ~0 n% w# {8 n9 `指一种信号。该信号在一定的时间内,振幅保持不变。2 |, n; L9 S) W) i 通常由一系列的高低脉冲表示。' m3 @5 } \: Z2 o3 d 数一模转, e! N; c o3 Q' N 将数字信号(二进制)转换成与原信号相似 5 _! ]1 V, u& e5 G3 Y! ~& j7 U/ b5 e1 R0 b: {4 H: \% g) ` 英汉对照民用航空词典B OEING $ V1 r d% h- }4 J# F+ D* h0 FTECHNICAL DICTIONARY 44 . ?+ K# S" Q% W. {DILUTER DEMAND REGULATOR, A component in the9 ^# W5 P9 Z3 `0 G- ^ crew oxygen system which mixes air and oxygen and$ ] p/ F6 M1 o( I upplies constant oxygen pressure even if there are ' n* z% ~4 c4 \- W' vhanges in ambient cockpit pressure. s w c# r* G6 S% b: b IM, A word value of light. For light control devices - dim ' q5 ] y0 Z5 N& b8 c$ Qthe opposite of bright. / I3 ]7 p0 U3 U' i+ q* n- oIODE, A device which allows electronic current to flow1 M6 d/ m" O: Y$ [/ U0 b) Q only one direction 0 l" t u1 g' Z: [* xuid in a reservoir. d" G( T9 y* P+ w DIRECT, Straight line flight between two navigational; {& E/ ], J! [6 @$ a* J2 S aids, fixes, points or any combination thereof. When 1 ]8 R6 K5 }. ^used by pilots in describing off-airway routes, points5 @0 N" U" O' o* q3 p, Y$ ] defining direct route segments become compulsory ) v5 I9 O! l1 F Xreporting points unless the aircraft is under radar2 E5 P7 W; y9 \ _' m control. 3 ?) G% F# u% V7 C& I节器, 1 [6 f; [: U' S将空气和氧气混合, % V9 ^! e0 o0 ]8 F- f使驾驶舱环境压力改变,它也能提供恒定的氧气压力。/ r& R7 e8 _: c% I7 O, W. w5 ?7 m8 {3 p2 | 一个形容光线亮度的词。对于灯光控制装置,暗的反 2 \& M/ |3 t. Z2 G& t% a9 s6 Y词是亮。 5 n) l" j8 r& N# m {极管, % |9 n$ `5 J% i4 V2 W) E& J只允许电流向一个方向流动的电子装置。5 m% H* Y& x% r/ H, a( [: t 器内液体的量。, d' b4 s% W/ { 直飞,' }; j* x, M9 N8 w# L+ O* j3 v/ r8 j9 ] 两个导航台,定位点,导航点,或任何的组合之间的直, y7 B8 ]3 D m/ ~' Z2 f: v 线飞行。在被飞行员用于描述偏置航路时,除了在雷达控( R' d! p% ~2 |! v 制的情况下,确定直线航段的导航点成为必报点。' m# F+ H3 A" [" b( s4 N s - ^8 B3 m& k+ M: Yc : E; a2 E2 d6 x% {4 lD 5 u+ f0 u8 g! N& { W3 nis 3 }4 t+ o* J# I6 uD# V3 j* E9 i. q4 n% b in ) D) P6 c3 ~: CDIPSTICK, A calibrated rod or stick for measuring a& ~% A! _, S- S% U) s! ~ quantity of fl" z$ _' N0 o0 i; g 稀释氧调, Y9 ~9 R# G: p/ l+ d$ |4 b: u" M 驾驶舱氧气系统中的一个部件,它- l2 d( z4 B2 ?1 F5 K+ c2 E+ h7 a2 E* D% W- r7 P3 q' |2 a$ F4 t- X) [' W4 O1 o2 y" Q2 A3 ^) n+ ~5 s! A" l( W. l( p( r0 P7 d; F量尺, + L+ {) K& N) j( f" A校准过的棒或尺,用于测定蓄液/ s7 W* e6 S8 Z5 z2 I 英汉对照民用航空词典B OEING 8 d( k( O+ `( [0 j# kTECHNICAL DICTIONARY 45

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