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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 5 V/ o L+ n! o4 v6 S* q. A! L民用航空词典3 J$ ~. `6 @% T5 ? 波音商用飞机集团 9 x4 q) J" e( ^, b; qBOEING COMMERCIAL AIRPLANE GROUP " b" U9 @5 P4 `/ G英汉对照民用航空词典B OEING M" n5 Y" g2 L, ]2 P3 ~+ b9 a TECHNICAL DICTIONARY 1 3 N! I5 L, u( |8 p) K( q, MA , y) P# u9 t1 |. u! MABEAM (ABM), Beside: An aircraft is abeam a station 7 E7 I- R. Y2 U$ c2 V! }when that station is 90° to the right or left of the track of , f( f* t& ^" H9 cthe aircraft.5 P$ D% k0 m9 a* \& U4 V6 b2 o8 ?% o ABSOLUTE ALTITUDE, The actual distance the aircraft( R& Y3 V: a0 `* {- u* M is above the ground.# r8 t9 O/ i% I7 S ABSOLUTE PRESSURE, Pressure of a liquid or gas3 `8 K5 o' ~ R( B/ i measured relative to a vacuum.; Q% O/ i. W4 i" ]$ V* z% L ACARS, SEE - AIRCRAFT (OR ARINC) REPORTING / P& ~6 z: i6 k0 T% _ADDRESSING AND COMMUNICATION SYSTEM . S+ N' I. H6 S. hACCELERATION, The rate of change in velocity with7 S: @! q9 L& {& E4 p# E3 Y7 j respect to time.$ h' T! Y4 y- m) O ACCESSORY GEARBOX, A part of the engine,' g- t0 {) x. r. _3 P/ o mechanically driven by a compressor or an angle ^! U7 J4 m+ M1 c6 |( T. |( egearbox, for driving components necessary for engine3 x& H4 J4 L: w- |) j' i, v 正切,; b& O. ]$ B! l k and airplane operations. 1 m! G4 P+ G/ j, O2 t9 S% {8 F当电台在飞机左侧或右侧方与航迹成90 度时,飞机正+ ]. d i, b2 r7 O; e2 A 切电台。8 s3 x n4 w) ~) ?) `$ A. z6 `: c 绝对高度,3 Q* f8 D/ o4 y, s: { 飞机离地面的实际距离。 9 v, I9 W' {3 U; k# {7 D绝对压力,2 C( N4 b, i, I( B2 u 相对于真空(无压力)测得的液体或气体的压力。 0 o' E/ E! r5 o! M6 L6 Y5 Z飞机通信寻址和报告系统,( v/ ?3 H0 G: F4 @8 }/ D# e) s: K6 m 见Aircraft(or ARINC)Reporting Addressing and4 J6 I6 e3 E' x- K j2 L0 u Communication System.$ b; Q( P" ?' q5 A. s, `9 v% x 加速度, 0 |! l1 t9 G0 a. x随时间变化的速度改变率。 ) `( c( C3 K2 y) R1 A; s附件齿轮箱,* R) r2 C) v: h3 i0 ~+ B7 C* D( q 发动机的一部份,由压气机或伞齿轮箱带动,用来驱动5 S" _; P* p. K$ W+ u0 k 一些使发动机和飞机工作的部件 9 z$ h. H6 d+ ]% ^+ F) ~5 u' }英汉对照民用航空词典B OEING 1 `0 r Z7 I, _* W+ a' `7 E0 E0 S7 eTECHNICAL DICTIONARY 2 ! ]9 t# V% D8 L0 R2 }3 _ACCUMULATOR (NO. 1), A container with hydraulic- ]8 z# t4 l3 T* M* D7 Y ts when normal hydraulic supply is not) H& s8 Z# t8 Z vailable.2 t( ]) e9 |1 y0 d* V CCUMULATOR (NO. 2), In a computer, a special 7 Q( o4 M: V+ Y3 @" t+ C- gtorage register associated with the arithmetic logic unit, , |% O" Y+ c3 c$ X$ H* d' A5 J2 tolding the results of a computation or data1 i' U: R' x% I0 v/ n* [ ACTUATOR, A mechanical device operated electrically, 9 P3 A/ ~; `" x* chydraulically, pneumatically or mechanically for 9 [$ Q( i2 r% q# n3 Htransmitting motion between components. 8 k8 U, F' v# `$ kADC, SEE - AIR DATA COMPUTER + Y; W1 z" c2 r: ^& DADF, SEE - AUTOMATIC DIRECTION FINDER$ N% _. i5 X9 {! F ADI, Attitude Direction Indicator, An electronic display of & A( z& J5 _* H& H/ q" i. Sairplane attitude information in pitch and roll." ]. m4 H S) s' [2 O 蓄压器(NO.1),6 l% p* K: E5 {0 f- E: \: _ 含有靠干燥空气或氮气增压的液压油的容器。当没有正- i+ y: `* O8 i) i3 W+ a' U6 e 常的液压源可用时,该容器可用以驱动部件。" v: a0 c1 F% X- l [$ T" z. z 存储器(NO.2), : g# X$ Q' r8 y9 C7 ` |3 |计算机中,一种与算术逻辑组件有关系的特别存储寄存 8 k: |$ c* ^ K+ n器,用来存放运算结果或数据传输。 * ]. \& M# Z" v' ?3 {& E% M飞机状态监控系统,. R S( G5 b- X. R3 o5 F, } 见Aircraft Condition Monitoring System7 \; G! l' L% r ~$ k fluid pressurized by dry air or nitrogen for operation of r( z! G9 l/ k% w0 }9 E componen$ O9 G" p2 n( l8 u a3 Q$ {) c6 {! u, b2 o- W4 q( |7 d A* X& `& V# c( B1 i, O9 k s& d. f3 |0 n& b used for h . z% G7 k$ m. [/ h" A3 ptransfer. ) |! U5 f/ G1 ~ACMS, SEE - AIRCRAFT CONDITION MONITORING8 ?; c1 e w& D/ Z9 O/ t SYSTEM . 4 Q$ g: ^( ], X6 D作动筒, ) p M+ j0 }- B由电,液压,气源或机械驱动的机械装置,用于传送部" ]+ c) |+ J. X5 ]: ~, a3 O 件之间的运动。" _. [+ ?+ C' t2 X( ^3 F 大气数据计算机, ) C% d+ L/ S% Q; b: e% G见Air Data Computer. 6 o- u* t1 B6 k& t自动定向仪, 2 e; S$ U# Q; ~/ A* \) S见Automatic Direction Finder. $ Q) ? I0 n. b! d) S姿态指引仪,/ m# d# e. c- E- j4 v3 p& { 用来显示飞机的俯仰姿态和坡度的电子显示。( [# p' q1 l l1 ?, w9 }5 g 英汉对照民用航空词典B OEING6 p3 K2 K, y4 b# V; F0 | TECHNICAL DICTIONARY 3 ) s% ?. V+ }) lAERONAUTICAL RADIO INCORPORATED, ARINC is " _) h4 Z1 r2 T8 _& D; K9 J, * l4 G/ A# {, \& O. ^+ u3 P' Vnufacturers, and foreign flag airlines. ARINC+ s7 q6 z* I& w( Z8 e evelops and publishes standards for electronic0 ?) }* p1 @, t4 y, E quipment and systems. 6 }+ D# d& b. [( s9 ]GILITY TUNING, The capability of the DME to1 ?: E# F9 E, q4 s0 z- Q8 T lternately tune between two different DME stations in - [! b% m' `$ z& a6 Xrder to get two distance readings from one % m( E. ]( h H- L( fterrogator.6 q/ q8 T" Y5 M) D ge$ _0 T. d- u2 z* L' S% U ILERON FORCE LIMITER, An electro-mechanical ( [3 n9 B4 L. Z# ]3 |0 m# y1 wIR CLEANER, A component in the pneumatic system; p/ G/ R+ M1 ^ s4 A3 `4 U# W- h upply to the air' w; m) R4 ^1 R! b onditioning system.& @0 F3 O m2 Z4 g; j5 M# t; ^! O" } 订并出版 & [; `' }8 z# q v3 {2 J子设备和系统的规范。/ N C/ _* [6 Z 快速调谐, : W# y# _) q8 r) d0 m机载DME通过交替调谐两部地面DME电台以测得来自 * E f% O' ~7 I8 K$ d2 \同一台询问机的两个距离数据的能力。2 q# R/ g* \/ `2 C 翼操纵力限制器, / C1 `0 H7 K0 g; _装置。在自动驾驶工作期间,用来限制驾驶盘 : }- z5 s; I( ?. f气清洁器, + @0 O7 B2 D9 @部件。用于去除供空调系统使用的发 ! c& g# G. G' j1 r' {a corporation whose principal stockholders are United% q3 [5 R& G4 d; D* W States scheduled airlines, air transport companies: p4 }6 n4 e6 b# x6 T aircraft ma F2 M, k; A- i4 \9 R8 j! d! E3 G1 k d 5 w; T& W; r$ me$ Y9 U4 n& u U: p& t j8 V* G A8 o+ v1 Y8 z& F( {1 }$ Z4 J a 5 }$ ~% s0 J1 {" ?4 M$ G, b" Io & t' @1 E# X# D5 @. V* J; Hin/ Q y% S! M5 j/ ] AILERON, A hinged moveable part on the trailing ed, o2 U# K5 Z& [. g3 U* V4 Q) o; z) l of each wing for airplane roll (wing up and wing down)1 x% W& T, D S2 S( J; ~4 n8 u control.8 T; w; z. f8 u A' `+ i0 X& x3 ~% m, a* I, s device for limiting the control wheel movement by the 5 o; [2 r# f% p! Q/ Jautopilot during autopilot operation.4 D) Y' A4 \- b. ~ A 6 o. _1 N: |: W) a0 N/ ]' y- S; \9 rfor removing dirt from the engine air s + S4 b2 \$ V. o+ K* D& }c; I6 }2 T7 v' U1 s8 A& [" L 航空无线电公司,$ C; F3 T2 j, Z/ d 主要股东为美国定期的航空公司、航空运输公司、飞机 1 x0 C3 \2 ?$ s& Q3 t/ `/ R+ Q制造厂和外国领队航空公司的组织。其目的是制 - k; Z6 B6 q% U2 E) t* i" @' f7 m: B副翼,3 W Q+ N1 h, d( j: r0 C9 B, ` 铰连在每个机翼后缘的可动部件,用于控制飞机的滚转9 A/ t: |- a, J8 L# q3 K8 x: F( O (机翼向上和向下)。 + F& B! W7 W- s2 U/ B6 v3 }# C2 }# e" v- i- g; `8 c% u 一种机电 - T# S$ ^; G; `4 X1 p0 g的动作量。 0 {; ~. f+ @ w4 H# B% s5 A& V3 i 气源系统里的一个 6 {1 D1 Z/ N6 d2 `/ P动机引气中的灰尘。" R! O( Q: O+ h/ h. f$ G$ p5 c. t 英汉对照民用航空词典B OEING- I0 x; O8 f! S8 g3 o) Z& r TECHNICAL DICTIONARY 4; a" D' r( J) A7 [$ U1 P AIRPORT ELEVATION/FIELD ELEVATION, The 2 g! u. k2 m2 nhighest point of an airport's usable runways measured 2 n0 @8 T4 V& r, { Jin feet from mean sea level. In a few countries, the + \/ C4 K% I) f/ \airport elevation is determined at the airport reference3 X! }; m7 ]" t$ G$ I point. * `; x4 E* q2 E# L: g2 ~ YAIR ROUTE TRAFFIC CONTROL CENTER (ARTCC),$ a, O; |/ `/ G/ x7 k6 Y ervice' A, E7 F+ Y8 T9 |/ y% o% o ase of , R, q E: }. J) |8 i# Aus flow of air traffic.3 \1 B' O9 \' X; L. X6 k$ f4 s IR CYCLE MACHINE, A compressor and turbine on a 8 p8 @' c# Z. R' n! t$ X g. Nommon shaft for cooling the air in an air conditioning; q) p/ \: x) g* p3 g* n ystem. The air is cooled by expansion from high to low : F7 J- _" R" v* S; ^- _$ yressure across the turbine. The compressor is driven ; F! u1 `, E% \: S5 My the turbine.' j8 r7 u' f, D/ p$ Q q 中航路交通管制中心(ARTCC),1 p& `" P- ]* c1 e" g 域范围内使用仪表飞行规则飞行的飞机提 L( M' b7 g! J+ L- m 管制(ATC),# \% i; K4 }& i' s* r) S* P+ C4 r 涡轮冷却器,5 g" g, A: b$ x6 {8 J# ? 是装在同一的压气机和涡轮,用于冷却空调系 ) X$ j8 q! S' ~& f$ G4 P0 f统中的空气。气经压气机压缩后,由热交换器移去热量,! ~0 }' E+ V/ E( H 然后经过涡轮令涡轮带动压气机。通过涡轮之空气,温 . x6 U" B' S$ y2 V' D3 _) Y, [度下降。 , G/ B2 l/ \9 M3 CA facility established to provide air traffic control s# Y4 |4 E$ B2 t$ ~6 q8 t. Q$ l& s# H to aircraft operating on IFR flight plans within controlled1 P; w& b0 S) e" ?6 B airspace and principally during the enroute ph ' [! T' ` S/ A& E1 G+ A% wflight. + D. d1 Z1 {* U$ M- [' Z4 KAIR TRAFFIC CONTROL (ATC), A service operated by 2 X- Q& Q$ e8 Yappropriate authority to promote the safe, orderly and0 Z% Z: ]1 L4 f8 r" s expeditio , c% `, h9 D2 H. u$ nA0 [9 F9 K. N; c, N4 x \0 R c" e1 q2 m6 h, B6 T. B& x5 { s - S. D5 `* Z$ T2 E+ f, [. ]% Lp p- g I/ O' \* yb - B. b6 g6 v7 Y6 C. q5 G! l7 G机场标高,2 z( t. M. r" K1 F5 l$ Z( Q8 ~8 V* A 指海平面与机场可用跑道最高点之间的距离,单位是英 1 w# E$ R9 m2 E J5 g尺。有几个国家的机场标高是由机场基准点而决定的。 ; Q3 C$ s3 Q( w) X e. r. O( J8 {% w4 A. D 给在控制空 . C# b3 S1 ?% K0 `供空中交通管制服务的站台。, M6 H9 I* F& x% \ ~; `) } 空中交通 ' `. h* X" j. q) y" z; I! ]" Z由有关当局管理,旨在促进安全,秩序,和效率的空中2 ^7 Z9 y3 W+ g. A$ Y 交通服务。 , @; B& r y; e% i根转轴上1 \( ]2 H; R! R( ~2 \5 U2 {+ v/ X- Z1 B5 `/ O2 s% m' i9 G( C- }/ j' A英汉对照民用航空词典B OEING! V5 \8 p3 @5 ~ TECHNICAL DICTIONARY 5

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发表于 2008-12-24 21:36:52 |只看该作者
AIR DATA COMPUTER, A computer which produc2 N( k1 T) x5 M6 g3 |2 T data information, such as altitude and airspeed, based* |* Q0 Y5 O4 A; W/ f5 _2 Q on pressure and temperature measurements. ; `, _* k& g( P) E3 @/ C9 Wes air% Q, F: l; L7 `; `3 l IR TRAFFIC CONTROL, A system comprised of 5 ?: u( |( Q1 B7 v8 i a$ y0 m7 Nround and airborne components used to identify, track 2 |6 \5 c3 Y7 G( W" s9 L( tOUND SENSOR, An electrical device operated / F$ A! @5 y9 Yy the landing gear, which transmits on ground/in air6 r9 k6 |% z. u& u! E a formation for system operation in flight or on the% z# w5 \: w5 g4 Z round.5 b: G+ L7 L' }# @5 s0 ]( [/ K IRBORNE VIBRATION MONITOR, The AVM takes! }3 O' T4 Z3 g8 R2 M6 Q! x e signal from the engine mounted accelerometer and% i6 g. R: W- g8 v5 [+ D alculates the vibration on that engine.) C6 }$ }4 c8 j( o corridor equipped with radio navigation / q% c2 m2 `2 ` J4 X. g$ F* vaids. : n6 n9 V# g8 l1 L4 O/ O4 V1 j: bAIRCRAFT (or ARINC) COMMUNICATIONS + Y$ p3 x6 X1 o( H4 P: b( y6 R* E" |ADDRESSING AND REPORTING SYSTEM, An ! Y, R: I/ ^( {2 j, Caddressable digital data link system which permits the 1 w0 W0 _2 s# h8 {3 E) H+ aexchange of data and messages between an aircraft- O8 f k* |% T* G2 n' P and a ground-based operations center over a radio" J" U1 B% f4 G3 }; i$ ~ network.* ` d8 x2 K1 a/ m/ ` AIRCRAFT CONDITION MONITORING SYSTEM, A 5 _' e* k& e7 L2 ]/ b5 tsystem of sensors and recorders to monitor various) k2 t% m6 z! Z/ x& U) u4 \6 m airplane systems' performance and status.5 u' Y) b! i( J 机, & @0 W$ G4 `' N- ^% N中交通管制,7 ^* E* {) U+ T% J" B 一个由地面设备和机载设备组成的系统。用来对飞机进 0 e4 K) n$ b' k; r4 G& |地传感器, 5 T- F) b# i5 m- K+ K一个由起落架操作的电气装置。用于给空中或地面的飞 " R$ F# l+ |" i# b系统运作传输地面/空中信息。(有些系统只能在地面* X4 s5 _: m7 [9 a0 w' X3 f 用) $ z' r v0 ^1 R" P' D+ g4 \: E载振动监测器(AVM), 5 H" p- p* H) \8 \% z; uAVM从装在发动机上的加速器取得信号后计算出该发 m/ }6 h1 i! \% L q# d机上的振动。 & g, ] m6 D9 P% K式建立的控制区域,内有无线电导航设备。6 ]( G# p$ C X. m. P1 C 飞机通讯寻址和报告系统,5 v* r% j: P, `2 X: D& L/ I 有种可寻址的数据通讯系统。利用该系统可使飞机与地 1 k% k# C6 D- z" d9 z k D面操作中心通过无线电网络进行数据和信息的交换。 8 O6 L% ~; |+ g飞机状态监控系统,: J& i5 n% O% P* A y$ f5 e9 F 一个利用传感器和记录仪对各种飞机系统的性能以及 * U( k& L6 _+ f1 [8 g8 g, d状态进行监控的系统。. \: e! B+ c( @& _2 T A5 Y" K1 a# J# I3 a9 W' G4 V. |7 q g ! z1 a8 A3 D( o" x) q0 j& L+ u1 j; @and locate aircraft.7 ]0 H8 x, ?8 {2 {& H: h; j. M AIR/GR X2 k8 J$ B& z% A. yb# ^, A* s$ j5 y in j8 E$ e( ]. a% L" v$ f' W& H3 @: V g ) ~) ^! T4 t7 [, {, J+ IA 1 {7 O2 `+ Y, wth3 E3 @* M6 t8 J# x, y c " A- j& }7 e0 g( H) Y* {, [* MAIR WAY, A control area or portion thereof established . c* E7 `2 J( w( lin the form of a A- Y0 c* o" Z0 W$ g! S大气数据计算& f0 q, Y( F Z# C# i2 { 根据量取压力和温度而产生大气数据资料(高度、空速 6 ?2 t7 B2 q1 o! w+ T等)的计算机。 $ S' g/ c8 Q& Z7 Z) e# i1 k, M9 j: i5 Z7 k4 t# s% \行识别,跟踪和定位。 2 G# a8 N% ^0 D( v8 I% @7 e+ R' u2 R. S% M1 r& Z8 ^# s9 k9 R6 O- Q9 ^ 使 2 {) w6 G, h* i) I- b" `4 C( g! j2 p' F) t9 q' M# W. m1 u" v; L& n6 E4 [/ D航线,/ {2 Z4 ~" d. j( i4 ?% B 以走廊形* g! m$ C% e) `) Z+ _/ ]% p1 Z" } 英汉对照民用航空词典B OEING Z) r6 x D0 l9 ~! [( k; q5 `8 cTECHNICAL DICTIONARY 6 `% j ]+ H# m! _AIRFOIL, A surface designed to obtain a useful reaction, 5 m2 ^0 c2 E0 ?& G- k# l; L }such as lift, from the air through which it moves. Wings,4 G# x% ~2 ~( C. `+ h5 E& k stabilizers and control surfaces are airfoils. 0 v0 i- n7 q. m) SAIRSPEED (IDS, TDS), The speed of the airplane # D o0 a* _& L0 K& Frough the air. & v* O) K9 e* FD INDEX, An adjustable pointer on the - @3 J3 T( q) c q3 ]7 d1 Mirspeed indicator.. C* H3 B; H, Q5 ]- d and legal ability 4 u5 p5 f1 F3 @- x/ Mfly. " O: L' T" j6 D5 q' y! _m, for example, the procedure for finding the5 \" \% O* y1 E8 D* W* g& ] f/ r- ~ quare root of a number.3 o* |3 H9 ~3 D+ u: l y# ?) x# W, H/ U# I$ d- M re, wind,* K' ]% y. G6 G8 _1 v and aircraft flap setting.8 i% ~# t$ P: ~) Z* T% A# T( u, L 是翼面。 ! |) p, r3 E: m' G @* R ?) E& b速, , ^+ Q- D1 P$ |8 n6 J飞机在空气中运动的速度。 # G7 Q/ }$ [8 \- W7 {4 `8 @) ]2 [, u7 K% I T+ N2 K8 z% Z& X* l( d 在空速表上可以调整的指针。, d& v& y, {' U$ q0 I! B 机械飞行能力、和合法性的飞机状态。1 G% n0 }+ }$ n: G I# y. ^/ Y 一步一步的解题方法。例如,计算一个数的平方根的步: }* {; F& B( `6 Q. \' Y' J8 p2 n$ @0 a7 i7 C1 o+ k$ q6 w6 y+ i6 i9 k 资料的法定文件。7 \' ~6 K: O' [ 翼位置成函数关系。 ( K9 |! Y L: Y1 Fth 1 H0 Y9 \5 q2 D' B6 ?AIRSPEE # l" W4 U6 [* Q0 R7 V; C0 ^a 4 U0 G4 o' X0 L) U- m8 J V6 H# _AIRWORTHINESS, The condition of the aircraft with! q" M) L* A3 D. ]" O# z8 O' | respect to its aerodynamic, mechanical, / S! R4 A6 A dto. e: v' }9 E, d ALGORITHM, A step-by-step procedure for solving a ) K% y' b, `( Iproble 2 {3 [, \, D, o$ C& v% I3 V" us# l j. o( ?) N) d AIRPLANE FLIGHT MANUAL (AFM), The legal % y- |/ l; G v3 F- Ydocument containing performance and operating limits, 6 _/ V' Z8 R+ v% q$ y/ E) b' e! zoperating procedures, and takeoff and landing2 y E- b3 e$ M3 \8 w, J performance. 5 M% x0 k& M8 n" k3 ]AIRPORT ANALYSIS, A comprehensive set of takeoff; u7 q1 P) z, M& c6 v weight limitations for a given airport runway, generall $ v: B' _: c' ?5 v/ d& c: k% xpresented as a function of airport temperatu 6 J! V6 r$ D' B' Z! H4 V; ]8 T7 X翼面, * \- m6 {. ~2 a$ Z- ^" I! V用以从气流中获得反作用力(如升力)的表面。机翼, 5 q6 L, g2 r& M* d' D安定面和操纵面都- [" V( V) j+ o7 \( v3 _9 U! h% J% u0 a; _+ U2 N! |* F空速指标 & z; P% W, _( y; c适航性, 0 k6 f2 j- j: f4 Y; u+ `有关气动能力、 1 ?, z2 A: B# [" s7 i5 \' Q演算法,' s& R0 `4 ~# |1 R, y% y4 Y1 a2 a9 X( P5 p& \2 z! b* O飞机飞行手册(AFM), 7 ^3 V1 C; `, U& ~包合性能极限,操作极限,操作程序,起飞和着陆性! r9 R2 D! |% c* ]6 c' o0 k* g7 `* j$ l( ~机场分析, " |( c3 |" ?7 S. _8 l一套针对给定的机场跑道的详细重量限制资料。通常与. i5 F$ {. C& z+ p. S 机场温度、风、和飞机襟 , y0 q' s4 e u6 S英汉对照民用航空词典B OEING 8 N/ H, J$ \. Q" e; a- Z, PTECHNICAL DICTIONARY 7 7 v9 E8 o: t7 C' d7 ?& X$ XAIRSPEED BUGS, Adjustable pointers on the airspeed ; T3 W, ~6 _, {5 D0 ^indicator.& y! ~7 [" N# |* F- t' d+ h ALLOY, A mixture of a basic metal and small amounts * P' k, D3 k1 U, e8 hf other metals to change the properties of the basic: U c% R1 V7 l7 K$ Y$ |* o9 D* r2 G etal.& o, p0 J1 E' A* k+ s1 W Minimum airplane speed./ L6 \, @# K# {% \3 s+ m8 ^: O e of . z) M$ x r# u1 g9 _itting airplane angle relative to 5 a4 p/ c& k2 R3 e A! y; sirstream for the stall warning system.+ u6 `) m5 j) I& t' v3 B another. ; e& C8 R# a" v3 `7 K0 `LTERNATE , An additional airport selected during8 F" ?/ x- ? u W) y! K) U2 o- Q( n; j2 }* S$ p! H 合金, F3 e, P* S7 A* g; z在金属中加人少量其他金属,而改变其性质的一种金属/ C1 i& a' q8 ]+ a- n- Y 合物。, ^: v; w- a: C 飞机的最小速度。 7 T+ g( L( K7 |$ \) E* f# g0 P速警告系统传输飞机对 / S2 Y M: a; d0 {$ l( T流的相对角度。) j. M+ I( l: _. _& x 由一个状况改换到另一个。 8 A' N2 S h& ~: y降场,. M- Z, Z o) }' w2 W0 b7 M6 L 划时,除了目标机场之外,所选的另一个机 - V6 j+ P$ t" q( n4 `( ~o 9 ^$ h/ e7 K. O! qm+ _' f+ ]# T+ Z" P, B ALPHA SPEED, U) w+ d5 Q/ rALPHA VANE, A small moveable airfoil on the sid 7 z' Y; [2 l+ M6 j* Lthe fuselage transm2 d0 G- T5 s/ ~! z3 r B a; j; @- W m# u( p ALTERNATE, To change from one condition to ; z6 a+ g7 t7 S; g6 I DA ( P( B# y+ p- e3 Z' `* Lflight planning, usually near the destination airport, to be( w& [9 O: L$ J used when it is desirable to divert from the original& G1 J$ ^3 q: {: X destination airport. 8 {9 y% k0 I/ Y* e空速游标 1 g, p b' U5 h# A1 |- F, i空速表上的可调指标。" w2 e. Q8 o" y0 J1 |. w; Z' R6 M# S$ G8 A 迎角速度,! q2 f) `2 {, {7 R 迎角叶片, : v1 p0 X0 ^6 i6 M位于机身侧的可动小翼面。为失$ k# T: c) d# Y( g4 o2 Y9 e1 y: S7 ^. ^2 [3 j: X交替, 1 a( `2 ~0 m# Y* D, b' V! Y( [' s( d3 g) G 制订飞行计 " X6 u* J- b$ J6 Y5 e场。通常在目标机场附近,以备不去目标机场时,改降之* F. O! l) y7 @& m# y 用。+ R; p1 P, E3 ~3 P 英汉对照民用航空词典B OEING: a3 [- v. V2 g6 v( k TECHNICAL DICTIONARY 8 ) W: S5 J% W% M, c8 HALTERNATE AERODROME, An aerodrome to which' K8 F5 M6 i2 S: k* O- P [3 y an aircraft may proceed when it becomes either 2 {8 r! X% a6 e; E( x: fpossible or inadvisable to proceed to or land at the0 L2 t4 }9 {9 p8 [! P erodrome of intended landing. 0 s+ v: x: l8 B' }TER SETTING, The adjustment of the altimeter 3 }+ Z( ]1 K2 Y: @1 J( G: e' L+ Vaccount for local variations in atmospheric pressure.1 a5 k1 S3 P$ M) J LTITUDE ACQUIRE, A digital flight control system5 |' D1 ~' o4 l" ^ ode to transition from climb (or descend) to level flight. % {. R1 P: z4 hLTITUDE ALERT, A flight deck alert occuring when the ; l- b' J; D5 o( E U0 A0 w$ o1 @/ Mirplane approaches or departs a selected altitude.' C/ x( ?6 ]! u* N' o' T8 i0 W LTITUDE CAPABILITY, The maximum altitude at: d' H, f4 f! U7 z; k4 c5 D0 U hich the airplane can be flown at for a given thrust, , d' B. K$ o6 K1 n: t+ x7 x5 Q% T! Dpeed and atmosphere condition. ! x7 U E9 D( KLTITUDE HOLD (ALT HOLD), A mode of the autopilot ' q" W; B- H6 M/ d( }r flight director to maintain a selected altitude.$ n/ N1 y4 e8 m8 M1 k& @ irplane's altitude during VNAV operation.1 K# W3 x: }: A" @: a 机场着陆时,可作着陆使用的8 b' h. j, l, v# b 场。 2 d- T- F, s& C1 U- g8 I; R3 h/ x: b5 H4 e2 ]7 d6 y( _根据当地大气压力变化而对高度表所做的调整。( R1 l0 M0 ?- r! w' z1 d6 [$ y# @ 一种数字式飞行操纵系统,从爬升(或下降)改平的模! C5 q1 P4 c7 U2 M9 \2 T: a. ]. ]- [' g% Q8 D* T! W 度警告,: F! E+ N ?# b0 B: q 当飞机接近或偏离选定高度时,所出现的驾驶舱警告。 " Y. D9 J# O+ j' d& I( |. j高度能力,- |' [; k2 b7 q# E# c 在给定的推力,速度和大气状况下,飞机能飞达的最大 6 ?6 H/ l" M3 X& y高度。 ' e2 z/ u# l' x8 g高度保持(ALT HOLD), . v: X/ K9 O: B- M* I, r l1 y% d自动驾驶仪或飞行指引仪保持在选定高度的一种方式。# v/ {& a4 u+ `. m, Q% Z# m- F( ~4 } 员对飞行高度的控制。 ) a! [, ~! m |4 X6 \6 [# Gim5 C% h$ j( i4 u0 \' K8 ] a ) ~6 k, p4 F4 k& HALTIME # r( P5 P8 J4 Q. p/ vto . B$ M# O1 L( E* ?% S+ V$ OA4 ^) [' r, V- P% z. B5 L( k m! t1 H3 G8 L) ^' D+ z A 8 w2 z3 H7 i, F: y* _0 Ja 3 J/ t5 E3 i1 R [+ w/ qA6 G2 }' r/ |6 I/ g w " t$ I& H+ D) K( B& s* Ms / g# I$ f+ U, h+ ?+ sA / i u% J1 H, B# P) p- ^4 to ' N6 `/ Z& T; fALTITUDE INTERVENTION, Pilot control of the ' Q& Z" a7 L1 l d% Ma3 a4 Z& ]; R( O% I- v AMBIENT, The surrounding atmosphere. 2 }5 u# h! Y. ^& Z; n9 G5 s4 p, b备用机场,- A- b( Y. b+ P6 M- g3 [0 L( ` 当不可能或不适宜在预选 * {9 c. R2 H) F" g5 G! P: [) M4 z$ Y2 ?% \& A0 q# e高度表设定0 c+ Q+ ^5 s5 u( q7 P1 i, f" w2 j 高度截获,* M" L- i4 @9 U5 C- x3 R, ]5 V1 k/ z) ]& f! d: I0 w+ ]' z; @. X) r; A" ]' _! i1 e 高度干预% p# L, X3 S4 w4 J 在垂直导航工作过程中,飞行7 [5 ^) `8 }; H g6 J, b- s) \1 ^ 周围环境(地面气层), . E# O4 D1 V; D) u+ @物体周围的环境(特别指大气)。: g+ P4 q) i1 G* l2 C) w 英汉对照民用航空词典B OEING- y0 E! O1 U* u5 w; [% K TECHNICAL DICTIONARY 9# W/ N- s/ ^$ X/ r- ]- K AMBIENT PRESSURE, Pressure of air surrounding an: n* F$ f* n- p( Z9 _: I# k object, measured in pounds per square inch (psi) . + n. ]3 E/ |$ z9 WMBIENT TEMPERATURE, Temperature of air 2 ^/ ~: \ h' a2 wmpere.- I8 ?# T2 D, _* t( B urrent waveform. 9 u3 f/ t4 q. F2 b8 \g an , E1 A) ]1 v& s( f, j& Nnalog signal to a digital signal. V$ t0 \4 h" o" Vore inputs 4 k1 R2 e. F/ J6 j0 ]" zf binary digital information and one output. The output / R2 K- C% r! B& y1 only when all of the inputs are 1. The output is 0 $ ]# b, p% o- E2 Qhen any one or more inputs are 0.; _7 D j2 ]- |4 x W8 T 面气压), ) ~, m1 P* j4 H; F) G境温度,# G5 x1 v9 e3 ^; z 气温度,用摄氏度(°C)或华氏(°F)来 & ]- D( i. p! x. u; @5 s6 \( v: f, \! d: ~+ R2 U; i9 Q) Y7 P6 x 电压或电流波形的幅度。( j3 v; e" A: E 性变化的信号来工作,或产生连续性变化的信号: G: F* o' f7 Q! v7 W3 n 统。6 v: }# ~5 a1 M& H+ z: I* l 将模拟式信号,转换成数值式。 ! @* o( i9 W- H: |一种有两个或两个以上的二进位数字信息输人,一个输+ Q' Z6 n! ^) h 的装置或电路。当所有输人为1,输出为1。当任何一个 ) B9 F' N; L1 G: d) ?" [一个以上的输人为0时,输出为0。( f$ _" N E n! u6 t5 @" b, T A ( s! Q0 R! h/ `' D9 V8 R3 Y2 ?8 psurrounding an object, measured in degrees Celsius ) g7 f2 p" c8 L1 _5 c( P(°C)or degrees Fahrenheit (°F). 3 G, f8 D7 }# h; w6 v% `AMPERE, A unit of electrical current. One volt across4 d! M: _( s9 s) k7 u. O: r; s one ohm of resistance causes current flow of one 2 p7 B. k# m# oa4 ?( W; Q' i$ C3 b& l- E$ C `! n AMPLITUDE, The size or magnitude of a voltage or # c* N& m1 I6 d& m( H# Yc$ `! l# I) K- Y6 z# O0 A ANALOG, Quantities or representations that are & a( n/ U) u* C; e6 l+ {variable over a continuous range. ; {* O- [. Y l* r8 lANALOG-TO-DIGITAL, The process of convertin7 I( I, x9 O) h* y8 R4 B6 E4 s# q a3 w" e: V% m. J; { AND GATE, A device or circuit with two or m ; D; ]3 E9 S) h: n7 co. [" W, O- [* U1 }& I is* d7 x6 c" x6 Y1 { w* x v0 P5 a6 i! f 环境压力(地 5 s/ i6 s; |+ ~: P物体周围的空气压力,用每平方英寸多少磅(psi)来# _( R% ^9 M6 H* \! W 度量。 ; @! R, @" J ?! @1 T7 X6 f/ r& d# a7 G& l: X( H9 v7 r物体周围的空 , F. p% z3 R' r- G, y! a# P度量。 - E/ T. \4 v; F+ X" {* f/ Y安培, ' M1 [3 K* h4 B/ R; K9 x Z: \1 I$ t电流的单位。 % g+ k8 T, L- y7 K+ T1伏电压在1欧姆的电阻上所产生的电流为 " d# o. k0 s. I; X3 W; A1安培5 |$ e9 N# p/ S" ~4 }( c 振幅,9 X7 k4 q- a2 T+ q 模拟式, 4 C9 f% P0 c: a) I+ W用连续 8 h4 k" G3 o" d7 h! B0 H1 a. A- \7 q1 T 从模拟式到数字式,4 q) _6 o5 R$ F" d+ L9 E$ o& I 与门, R5 S2 m7 `! H% r3 _: o8 e2 |: ?, b) P) z& e% F& D& ?英汉对照民用航空词典B OEING ; x2 p7 ^# b+ DTECHNICAL DICTIONARY 10+ r( X3 D' W' K" H ANEROID, A sealed flexible device containing air at low3 a8 H4 L7 p: {1 Z pressure, which expands or contracts during change of- l1 s1 n2 C% w ressure outside the device.4 V) M; y3 B' b7 r) ~ ically0 Z; r& S0 ]7 K' {* }. K2 J r changing the direction$ R7 n# C: {; h( U( Z0 o f drive. 5 F3 P. W8 |3 L/ E/ \4 n; X s# Eof the wing chord in* T+ E- A7 u+ i- `8 c lation to the free stream airflow as it moves forward , p+ H9 g% h; ?) K0 }rough the air. . d1 B: B5 q) N: H3 Sal axis of the / L, h& V/ o/ N0 y+ T0 N1 A. yaircraft.2 l% t# A/ K+ l! ]1 K6 j' j2 ` 胀或收缩。" i6 T8 s y0 P4 g; e$ v 箱。是改变驱动方向的机械装置。8 t. \5 y" c& X0 T Q' S 机翼翼弦在空气中向前运动时与自由气流之间的夹角。* O5 r5 L. U( |1 E$ O) k, P; _3 c' dp& H; I0 ?9 s! x ANGLE GEARBOX, A part of an engine, mechan ' g7 \" |! E# {# d$ w) udriven by the compressor, which drives the accessory ; o7 s* Q4 k; Q* P. n. Qgearbox. A mechanical device fo ; H3 j0 G* f% H, _/ [- eo# G! S" c7 h5 n: D ANGLE OF ATTACK, The angle9 J% B+ z9 i( R! S- @ re% }9 u9 i6 H' }7 i4 o8 o4 h, N th ' i5 P$ m7 K, z% lANGLE OF INCIDENCE, The acute angle which the6 t7 ?7 w. v4 F( u6 V2 C wing chord makes with the longitudin% l- r, a* h# a: F7 d& _3 I 膜盒, + r6 q9 f5 D. M5 j# a内含低压空气的密封弹性装置。当它周围的压力变化 5 j2 p6 U8 Z& H: [, G7 y时,会膨 $ f4 d. ^2 z6 j5 O4 t- C伞齿轮箱,' U+ e9 f7 s. X. N2 ?9 e 发动机的一部分。被压气机以机械方式驱动,然后驱动$ }; G. G# S4 V/ s5 a: v4 P! E0 p 附件齿轮8 H( G; a- ?0 N& b# h( i 迎角,; u7 Z0 @" b0 \% j: A$ s# I 安装角,' y8 G( _4 u. v/ {1 ?) J+ a 飞机的纵轴与机翼弦线所形成的锐角; q# t; p' r' R" X4 P 英汉对照民用航空词典B OEING% |- L/ Z& @; [* ?! @' q TECHNICAL DICTIONARY 113 ]: W7 q% r7 q5 n, Q& j ANNUNCIATIONS, Audio or visual indications used to 3 R, M9 J& D2 _+ J% m6 [9 mcall attention to an event that has taken place.6 V! z0 k9 A' `7 z ANNUNCIATOR, A visual device consisting of a number9 w; T2 ^# ?! Y ly. / |0 H3 O! F. b3 `# zANODE, The element toward which the principal stream * { B1 D9 `2 K7 Q' o3 Tof electrons flows.2 @+ m1 |- z! |+ O* H( } ANOMALY, Not normal.# n: Z- V' d# T- a9 z0 d7 @ ANTENNA, A device which, used in conjunction with a 2 s) U: H3 ?9 F* _) Y/ U% j- s* `transmitter or receiver, is used for radiating or receiving 9 v9 Y; I$ r3 F$ u7 [: |radio waves. 8 F) q: ~! B3 P9 t3 FNTI-ICING, A method of preventing ice formation on + x* p* C" D2 V% ]9 z( ~e wing leading edges and engine nacelles. 3 F7 n; s$ n4 k2 R: q! m" iNTI-SKID, A system for providing maximum braking % [* c* W9 r, k& f1 j; Uithout skidding for any runway condition. Anti-skid1 O7 Z, T3 r3 a* `9 U A! z omponents are part of the brake system.' V0 B) A1 L" L 告, ( w# s! A: L9 e当发生事件时,以声音或目视指示形成的提示信号。/ g$ w9 L: X- }$ T, H3 N2 A" K 与之有关的电路的现有情况或已存在的 7 F: z* H* i8 L9 O- A: r, I5 ]" s, i$ s4 r# ]8 a p/ B- ?6 i( x/ p8 i1 E4 e正极,% k, @' u' r: W: X; ] p# C& Q 主电子流向的极位。9 [5 Q6 J+ c0 S- B 异常,! ]3 h0 _( U) I7 C9 ]+ r- W 不正常。 1 O2 k+ p! @9 t1 P8 v天线,; v; C3 }# z% h: A 一种与发射机或接收机共同工作来发射或接收无线电! i, \4 f' F8 s/ V8 V' o 波的装置。 $ V0 }. x$ b- n8 W+ q) o" [ h& h' d冰,9 k6 h1 _ d* Q) f" a J& _6 ~ 防滑系统, & }- ~: h" ~2 m: l* Y. W一种在任何跑道状况下,都能提供最大的刹车能力而不 1 C/ V; x) @, @9 d6 E$ c使轮胎打滑的系统。防滑部件是刹车系统的一部分。 8 f2 u( w+ `, n! o* G: |of lights. Each light indicates the condition which exists# [" b+ K) m9 X5 W5 p or has existed in an associated circuit and is labeled A! Q( ^- X* h" I. a according 8 I. {* n" T# BA2 k) N$ u' A4 }/ ~ th- ?) \" a/ z* v+ R- h* S* x4 ~$ M# k A( N1 U. J/ j3 e* _8 L. b w+ a% b1 c6 X! A. ?3 c% C& n c. i0 r1 P+ a+ H( K2 }2 O, z/ x. r' g, T# w* Q0 L9 a# L 信号牌, 8 g. ^6 N9 U/ ^# Z# E- y" P: |由一系列指示灯组成的目视装置。每个指示灯都有相应 7 y+ F1 J: h4 d( }5 G5 @的标记,用来显示 ' L: ^" Y5 h* W' @! C2 {1 G" d! o6 d7 \$ d- F1 [1 u8 T$ g3 }) S6 }9 L防止机翼前沿和发动机短舱结冰的一种方法。0 b- m* e% ?7 u: J- w; y# R 英汉对照民用航空词典B OEING& X9 z5 u6 ~, r& W9 i) J$ z" y TECHNICAL DICTIONARY 12 0 N: l6 ]4 j0 L" ~/ jAPPENDIX, A supplement to the Airplane Flight Manual + f# S/ \9 {9 f" stained in the basic manual. A/ ?6 { ]7 R) D: P2 _! D, z0 _3 Y. `- b ollection of supplementary material at the end of a2 k5 z$ T5 c g ook. $ R0 d( H( ^6 a; Vof the# v; l7 a" s* J( h rsion link on the landing gear. . v7 _$ B4 G7 a4 z" HAPPROACH MODE, An autopilot/flight director mode 4 @6 y& r0 o" t! w& ]7 lwhich is a combination of localizer for roll control and 3 A: N! |& _; o$ \7 Q$ y7 Iglide slope for pitch control. This mode is used when full ' S( ]( V" Y9 g) k% F" u; D- winstrument landing system is available. 0 c" Y! R! c7 |8 `% kAPU, SEE - AUXILIARY POWER UNIT 9 s3 @( e# m$ J7 o. A8 gARINC, SEE - AERONAUTICAL RADIO U7 L. O n! S+ D; W; A, t INCORPORATED + [* A8 Q2 Z$ j: e) K* L) WARM, To make ready for operation. 3 z8 s# J, q' B附录,# |' }) l2 I- I/ D, R, Y6 e 飞机飞行手册的附件,包含基本手册中未提到的飞机形 # y1 o* ]% U/ B1 \; O6 v. q' J: k态的其他性能。是附在手册末的补充材料。 9 D/ B1 O! D3 G/ l8 N4 {' v9 @顶销,, ^5 c% r$ P+ q1 `7 F 用于连接起落架扭力臂两部份的销子。 * t7 ]9 n) a9 m8 j进近方式,3 y$ `3 W+ i" t, o1 d 一种综合了控制横侧的航道信号和控制俯仰下滑信号3 V G3 e. L% V# X. Z, }. D* v 的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系$ T% G) i7 }! [4 o) ^ 统正常时才使用。& m/ o+ F& h$ X. Q6 z3 `0 H8 { 辅助动力装置,3 |% _1 r" r0 ?' z: R( B7 |% v 见Auxiliary Power Unit 7 C- H9 @* a3 R! I3 G6 J. bcontaining additional performance for aircraft$ U1 |& k2 V1 ^- [; a configurations not con1 {5 J2 o0 g6 S1 @7 b" C* h c 1 X$ H* P/ D w% ~2 sb- G* C# k9 U0 g# w( d4 I1 @8 ~$ r APEX PIN, A pin for joining the two sections / e. G' {$ O7 P; k* w, z# zto * P$ W* J$ K" u$ z" U$ Y' U8 Z. _5 B$ s8 ^ 航空无线电公司, d6 _( Z9 U/ @5 { V9 N见Aeronautical Radio Incorporated. $ }% B$ E2 v/ c5 e( g预位, ! e# d' A. i; W$ ?7 o1 M$ ]部件可以开始工作的状态。# g; D. m) M% I P s 英汉对照民用航空词典B OEING- i, | e" e3 Y% R! ` TECHNICAL DICTIONARY 13 1 l. Y4 Z, P" C; l) T! MARC, The curved track over the ground of an aircraft5 D+ `( @1 N/ t% S% b2 y: }, g flying at a constant distance from a measuring ) ], F5 |4 Z. f4 |0 l0 Y2 _3 Wequipment (DME). 9 P! B" G2 J- s( Q( d Xin the limits of self-contained system: p$ S3 K% J- j4 P apability. ; v( x( m; |( S7 K& x' Ktem for opposing or restricting$ @% N3 c% E3 @9 V- J ovement. , m* @6 [9 B6 I; b( QSPIRATED TAT PROBE, A sensor that measures total ) D+ C/ H" h$ p& \* `$ j1 V% D% Cir temperature when the airplane is in the air and that " _4 \4 g7 C/ m& L6 Feasures outside air temperature when the airplane is ' ]. S. ?2 z& _n the ground. The outside air temperature is measured : v2 [! `' n( k& A4 ?+ ~; E& }8 DSSEMBLY, The fitting together of a complete structure 8 t% N- I: g- p) n1 v$ `SSUMED TEMPERATURE REDUCED THRUST, The : P5 |3 L, K( G0 D5 Q% W! ?' H0 A. aATC, SEE - AIR TRAFFIC CONTROL2 a; f8 r. S# H: J7 m5 V; n4 x6 U! e9 `4 Y v. T/ } 系统中所产生的一种用以抗拒% U, k f+ R! C 作或限制动作的力。. t, e; R) o( y# A 头, ' n, `1 d# E+ F& g$ D$ H. T5 {用来测量飞机在空中时的总大气温度和在地面时的外* r3 ^" c0 {: | 温度。地面外界温度的测量是利用引气将外界空气吸入 8 Z0 y+ K2 \3 h) `头,以达到测量的目的。 ) C9 C# S7 Y! n7 Y* I配, / K& {9 W; j6 x. r2 \一个完整的结构或组件的过程。$ r) f4 ?5 d: Z, d 假设温度而得的减推力,3 K$ _% }, U( M+ N: w c0 [: [& V3 x 推力设定值时,假定一个比实际外界空气温: z$ U( ~3 `( Y" G6 X0 } 空中交通管制,! @9 d' S* J% ?9 N1 K/ v 见Air Traffic Control+ ]; H1 {/ z/ w' o$ O AREA NAVIGATION/RNAV, A method of navigation " ?5 ^. o; g Y9 v3 z: ?: p* j/ kthat permits aircraft operations on any desired course $ `( ~. x1 E8 } D( ^- P3 Iwithin the coverage of station-referenced navigation* p. J. b: i6 I" w" T signals or with $ e0 g) P a5 M7 S% ]8 gc: q: T' M2 l3 z) l; _3 ] ARTIFICIAL FEEL, A force developed in the flight ' r7 q& c. J+ s/ i; P0 econtrol or brake sys* @3 X9 e" D; Z" [5 S: D' V5 g m4 R: ?/ D1 h" Y0 Q1 A A ! a: J' Y: s9 `" u+ C# N0 d. d+ ra2 {+ r, _+ v3 Q1 n2 g- R% Q9 { m 9 ^5 `+ U3 c# X- e' {o/ }8 H5 x# ?: @ by using bleed air to draw ambient air through the $ V) n+ k1 ]4 e% h( e1 _sensor when the airplane is not moving.4 X- M5 f& f0 u+ Y: I L* f A1 w& ^ {2 X6 ?6 m7 R or unit.' z0 [& M: m1 o( q8 V! { A) {9 v: ?4 K9 Y. T) ?( j% c lower thrust obtained by setting a higher than actual . P( m$ M0 @$ B4 COutside Air Temperature (OAT).9 Y( q0 E6 `6 c 弧线,* t$ U2 O! ~5 S/ F 飞机在围绕DME台等距飞行时的弧形航迹。6 u6 y8 \" }% J% T$ o2 x 区域导航,9 N# h0 J- a, j: u. [ 容许飞机飞行在有电台参考的导航信号或自备系统能+ M" N$ z1 n1 P7 Z. Q 力极限范围内,飞行任何预定航线的一种导航方法。1 `0 V3 l* K8 q% z, `3 N/ a& T 模拟感觉5 B7 l2 O# r' m# G 在飞行操纵系统或刹车2 i) |) K# v: B9 j# c6 J# A, N9 s' M# X" p- D- p) `0 G3 _吸气式总温探: _/ I8 m; Q& u3 U; s0 Z1 C; W. w( F9 h# e1 P! A ]+ M% e3 z" ^5 \4 `: h8 ^ M H a% n# `& { 组合成 8 l: M3 n3 D7 B2 w2 Y# E$ `: l; v/ J5 _1 ^! B+ y- ]* `# Q在选择起飞 b7 X5 Z9 R) V. G! h( p, J9 z- k度高的温度而得到的推力。用这种方法可以减少发动机的! `% H F7 e7 l/ \( W 磨损和维护费用。 3 l( \! Z+ @% o7 |# @2 p$ l! o& n 英汉对照民用航空词典B OEING, O4 a7 [ y* @6 j TECHNICAL DICTIONARY 14 % p1 g) t. }' P( E4 f7 h3 D2 IATE, SEE - AUTOMATIC TEST EQUIPMENT! t& l* @9 G/ p- \ ATMOSPHERIC PRESSURE, Pressure of air due to the % f( y2 I6 Q6 U! sarth's atmosphere, expressed in pounds per square 1 B# ~3 O! e) k4 dch (psi) or inches of mercury (in Hg) or millibars (mB). 5 v# z3 ]/ B3 n! ~4 UTTITUDE, The relative orientation of the airplane with1 A; m1 b. N6 b9 r0 m( M7 o& Z# S spect to pitch, roll, and yaw.1 [# n1 Y. g. o UDIO CONTROUSELECTOR PANEL, The panel in0 I- x: I0 ~. `% m e airplane which controls and selects the routing of # L: M$ ]2 X4 Q( u* D) C$ judio. , L- A' [$ I* O" L0 ~+ @1 h8 ?. TUTOLAND, Automatic landing using the Digital Flight 5 [) I) F3 t; }; J- tontrol System.( h/ X) w$ ?. E2 Q' G4 J6 g n. 8 V" P2 c0 @; I, Y4 u+ k: nM, A system 0 B, o# x2 x- i, q7 P$ |omposed of all necessary subsystems needed to guide * c! G3 m2 c+ ~' W# ?e flight of an airplane.1 K0 v Y) L( G0 F EQUIPMENT, System test# x$ p- F/ ^/ s% k: [7 T quipment that operates under computer control.5 V9 W& K: t% Q- q" N0 }- Y 装置,

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e+ x; n6 {. `) n' n! o# v in % Q# C/ Q6 \$ w% T3 P- T9 a TA" K3 p6 U- F$ L/ k4 w: R) m" u re5 s4 W- f$ E* z0 B7 a. t' H A % h; D3 [, _% Y2 [7 ?# x. Y' Mth& U+ T4 j, k# [# K# @ a ^, F4 [ W. S* T A 9 x E& y+ T/ ]; q* j4 r, P JC: h6 K6 t; X6 M7 [9 h* q AUTOMATIC DIRECTION FINDER, A system which " A+ a; S3 K5 E& E) zdetermines the direction of a radio statio 9 f/ N4 I2 G- `AUTOMATIC FLIGHT CONTROL SYSTE " s' O* N {0 d" v- d1 dc6 ~( V, h/ b5 e& V8 H+ k th; [& u$ T g5 g& x, s( l' w4 M AUTOMATIC TEST+ f8 s7 J9 p9 u7 S e ( `4 O4 v- {- x' Y! a1 z5 ]自动测试 ) Z5 f7 d, a# I T" U2 n: U. D( L见Automatic Test Equipment.) h* s5 H! k. b& B4 P7 o0 e2 F 大气压力, 9 d/ X/ ]3 n" V! L由于地球周围的大气而产生的空气压力,以每平方寸多 3 p& u1 F2 @$ }/ L磅(psi)或多少寸高水银柱(in Hg)或毫巴(mB)来 & c; V5 i1 L/ @9 h示。7 b: Z1 @9 y$ t9 w' m H 飞机姿态,2 r- O% t/ F8 l/ m 飞机与俯仰,坡度,和偏航有关的相对方向。 ' c' H% H$ c+ l0 P0 x$ r音频选择面板,2 [; S1 w( L# u8 g 飞机内用来控制和选择音频通路的面板。 6 O7 Z* L+ s8 K+ A6 Y3 ~2 l" x自动着陆, / w l Y! g- i: _' l使用数字式飞行操作系统来进行自动着陆。% K$ B8 s% F# e/ x- N+ y 的系统。 6 X+ g" f6 e4 \' q/ k. h! x0 I/ e m0 `- g! [系统所组成的一个系统。1 h; V2 T0 e: e D9 C8 u 在计算机控制下运作的系统测试装置。 ! _! j* o# I- u) d) S/ {( v$ D' j/ h$ R' b% Z" z# G' X: d$ c1 _3 \/ X" ~ l5 D自动定向仪(ADF), 2 G X7 \ ~: m6 ?3 @7 p确定无线电台方向& o6 p w* j0 M2 s& u6 ^) q 自动飞行控制系统 / |" B+ e* C0 T8 l由所有能引导飞机飞行的子' z8 S) _; L' o0 i: O p- q3 R 自动测试装置,9 J+ p/ ?! U& e& _' W 英汉对照民用航空词典B OEING+ [: X; ?/ N9 [0 h' |4 G: F TECHNICAL DICTIONARY 152 f. h& }# @+ J7 Y. e3 E AUTOPILOT, A system which automatically controls # E( t: V* ?3 @and guides the flight of an airplane. & Q3 ]6 y1 [/ X7 e9 v# CAUTOPILOT FLIGHT DIRECTOR SYSTEM, An- F3 c2 V- e. D) g0 F9 _& c; W tor" N3 g& e p2 H/ F! b+ j UTOTHROTTLE, A system which automatically 2 H+ d3 e( k2 K: d; E0 |7 U, Gontrols the throttles of an airplane. $ O: c. K2 |3 L# D1 v3 QPOWER UNIT, A small turbine engine in9 G. L$ ]/ c( Z. P0 k" T e airplane for supplying electrical and pneumatic 4 |6 s) q7 D7 E: Jower for systems operation on the ground or in flight.1 H3 u: N6 c5 f! {1 r VM, SEE - AIRBORNE VIBRATION MONITOR % |8 w0 x$ R2 O7 P% W LXIAL FLOW COMPRESSOR, A type of compressor + N% W" U, K$ m) J- |sed in a gas turbine engine in which air passes through 8 k* A0 X ^, Q, p# gXIS, An imaginary straight line or an actual physical : B5 M+ R/ u: P) iomponent (such as an axle) around which a body can ( o4 j+ t9 K G- x4 A) Jtate.6 ]. [; Y5 z2 |% A7 h 仪, 0 R; v3 X$ C; N! n+ o. R# } @: c. |. e5 Z% ] 自动驾驶飞行指引系统,: `5 G, }% R! b2 a8 I 动驾驶和飞行指引功能的系统。 & `6 |6 Q$ Z- c* I3 I动油门,* M) J1 `) N/ a+ G) _ 自动控制飞机油门的系统。( {: v0 F. M7 x5 j 是飞机内的小涡轮发动机,在地面或空中给各系统提供+ Z m" v6 B# \& ] 源和气源。/ c% X8 |4 d/ G. _ | 称。 : O1 \! ^+ H" t2 o+ q载振动监视器, 2 { t) M/ `: z' K0 z5 ^2 J见Airborne Vibration Monitor + M4 j1 n- C, L2 X6 W6 F/ Yintegrated system containing autopilot and flight direc4 J+ b- ^, t8 K0 q( S functions. . K! ?- w% G! h/ |( q# s( n8 X( ~A : D1 c4 K0 }2 g! q& i+ vc2 P6 ]% D% r$ \7 {" y- ~ AUXILIARY # B8 j o" d. Q. R* Jth / p/ t! c4 I0 N2 f4 R9 Kp . U/ Q& q8 e- z" z, rAVIONICS, An acronym designating the field of aviation 5 x, d/ Y0 w5 t6 `7 t' j7 felectronics.) T7 [; h$ n( g; h! i( s8 e A ! _$ `6 ?" h7 C1 G! ? {( ~A& B% J3 d7 z2 A" J' \ u' O& _* A) d/ n0 i0 ~: h the compressor in a straight flow, front to rear.. M, M+ }, Y0 x$ R% ? A / G6 m* p2 B1 s3 x9 y9 ic ) M$ Z; C4 t* X/ D0 e+ [ro . T+ W3 i- X" b( Z1 T自动驾驶9 k+ C* v; Q4 k7 Q4 j n0 | 动操纵和引导飞机飞行的系统。 : U8 K: K4 o0 C' W' J% N: y一个综合自' `3 x" j* }3 k4 ^) J! k: P0 h5 j0 S, {6 I: N( K1 {3 @辅助动力装置,4 b* K; n3 K7 V* [: A* r$ Z% q6 X- n! C |# q a* ^3 X航空电子学,) a$ T0 O6 y, ]3 W 是航空电子领域的一特有名5 N2 `$ a. a! ^- W8 [* Y5 u1 j! F0 ]. w+ L$ h1 ^, A# {: s p; F 流压缩机, 6 J1 Y9 O3 m8 p: Y" V一种用于燃气涡轮发动机内的压气机。空气由发动机的/ a- k, ~6 g* P' w' B: t+ ? 部流出。 b/ b4 d5 {& r' N线, 2 N6 u& U. L0 S- B4 ` D可让物体围绕着作旋转运动的一个想像的直线或实际 4 C# b, w0 F! M, y, g4 K7 X在的部件(如轴)。 1 A! o1 W2 }3 K- b4 T2 K5 A' D: R! X( o- j8 t H! O, i9 ] 前部轴向流人,压缩后,由后% P7 Y4 K: u: R0 U$ p- c# F7 Y- S' @! o' Z+ M6 e; r) h9 V- H, J4 Z, n; d英汉对照民用航空词典B OEING 9 h. r6 |" A/ ?# C7 K7 z6 gTECHNICAL DICTIONARY 16 I6 c7 M3 K5 Z4 hB - c$ I8 a/ ~! }2 m' i: bACKCOURSE APPROACH, An approach to a runway$ b4 ~" T4 h# x" y- q6 |& a7 o versed.# g) d y+ p: ~; ~ own on the EFIS that1 d1 r/ s# a' _ oes not readily change, for example, navigational aids.9 a) Y* |. D& d9 Z2 ? vement in the tank or reservoir.$ C" f% M$ s5 w8 C; V: x ALANCE TAB, A small hinged moveable part on the( }/ r5 K8 M5 S% O1 g# p* o/ J" s ailing edge of a control surface (aileron, elevator, ; h: _$ ^4 p+ I航道进近,4 Z d( m0 s. S, c" n, D# q 相反的进近方向。当反航道进近时,无下滑( r& B1 h O( n: |# b3 J 显示在电子飞行仪表系统上不经常改变的数据。例如: + ^" ~0 \1 x% p/ |航设备。4 V- r+ T+ b0 ~1 M+ U. |1 E5 ] _ 在燃油箱或滑油箱内阻止液体流动的隔板。- `. P& P( T, B5 g8 s 动补偿片,+ j C" P8 p& J: p: R' N$ r 铰接在操纵面后缘(副翼,方向舵,升降舵)的可动部。4 U- q5 t0 y. q n4 c" l. X 与操纵面相反,以帮助操纵面运+ [& z' W T" x B/ K$ }4 p! X. S/ [ which is opposite the normal approach. For a# _2 z0 j0 ~9 S! N8 @- r/ N backcourse approach, glide slope signals are not & ~! ?+ |4 E5 O3 L* p9 P0 Xavailable and the sense of localizer signals must be ' n. ^! J( j& N7 H% Sre* g1 R1 S4 ^ l& H' p0 n BACKGROUND DATA, Data sh ! x' z2 q+ C1 m% Ld8 x P( k- r$ P9 L3 E8 _; t% _ BAFFLE, A partition in a tank or reservoir to prevent - ?3 M# T0 Y' P& d7 o( C9 i# lfluid mo % l; [0 l, }1 i7 J A6 ~! MB9 G$ A& M( ~* @. l5 o: ^/ \6 o K tr0 ~7 Z+ ], p- @5 Z; V rudder).The tab moves in an opposite direction to the0 @- _: H- u& {2 U% ? control surface for assisting movement of the control$ |' h. |6 y, L0 i- ]* H surface.' ^5 J- e! W; U+ T7 ~# r" |0 U& `1 q3 o* w- I$ X与正常进近 0 L7 u! m/ \. m道信号并且航道信号也必须逆反。. q) f5 r, h' ?5 u( `, r7 r7 {! _5 [ 背景数据, ( Y/ v) } N" |. y/ h" d4 @+ s5 @. Z3 E1 r3 r7 o+ E5 i8 r1 }/ ^ 缓冲隔板, * @: ?* d- ^. P- V2 e* T" I0 a3 K. `! u. {+ V随动补偿片的动作方向 0 ^ q! X5 S" z# W3 ^* a3 [0 T动,减小操纵力。 $ u0 [' Q0 }7 V3 ^: w0 z) `英汉对照民用航空词典B OEING $ `; C$ \' C! {# D+ G6 }) ?TECHNICAL DICTIONARY 17 " U" ~5 o$ o+ QBALANCED FIELD LENGTH, The field length , Y' C1 E5 P5 e1 F5 u7 e% A" Massociated with optimum aircraft performance when% l+ x @2 G6 Z1 M! ^ bstacles are not a constraint. In this case, after engine 9 G& E4 w+ e3 J2 k% }" G r% Iilure at V1, the distance required to accelerate, takeoff 4 k" e2 J5 y& g- B% @4 jnd reach a height of 35 feet is equal to the distance 7 S2 i3 v% E$ y* ~. f& N4 PALLAST, A weight installed in an aircraft to maintain 3 s- M* h6 `4 |4 C% T$ kALL NUT, A fixed spherical nut driven by the1 U4 y; v* e3 j. P( D m, ` AR OUT OF VIEW, A signal used to remove the flight4 U- D. l! I1 u( u$ g0 f t1 g AROMETRIC PRESSURE, The pressure of air above % q: J C2 i4 b! I# lg) or3 \+ ?3 u5 ?- p C8 \ millibars (MB). , u+ }5 j) C1 D$ eATTERY, An electrical device for changing stored " {( U( p; c7 v, V+ X. |* O ^性能的场长。在此3 D3 q3 j$ x. L9 x0 a# L6 ]; z% g6 B- ]: i 况下,V1时发动机故障,要完成加速、起飞、离地35 5 V9 L# e8 Q* ~; K尺所需距离等于相同速度下完成全停所需的距离。 / K3 ? k% }- Q舱物, 9 f# W! y; R8 ?& [* o! z重心在许可范围内面装载的配重物。 1 L; f2 k9 U$ O形螺母,* ^# ^% h+ @9 l+ n: Z 的固定的球形螺母,用以使襟翼和水平) ^; A' a" h: p t X, u 引杆消失,% P2 w- z0 S8 I1 T" ]4 ?- ^ 指引杆的信号。# [7 o1 g8 g2 {# ?& P 压,/ R5 E: `* X. x6 G* F 压力。通常以多少寸高水银柱(in5 X* e$ V: R( l { 瓶, + `+ t! T! h9 x* G的化学能转变为直流电的电气装置。 ; b$ B, Z) G! Go, j# W" i. s: B" G4 F9 K8 k% B fa- F% I% \- A+ B/ ?6 `8 o( n+ n a& F3 T* o" c4 h required to stop from the same speed.* u1 o3 X% L8 S. z+ K i: T B' j8 j/ Q$ D4 n* u7 c the center of gravity within allowable limits. 9 {! F+ V: R$ k/ nB _! n. F! _' X& ]# T9 p+ d jackscrew for flap and stabilizer movement.$ C3 f# o1 A* R3 |; g0 R B# B* Z4 K7 Z# W: \ director command bar(s).9 U5 V5 t3 s8 p) [- A: ^8 F B* k# a `6 t! C* ^3 @ zero pressure measured in inches of mercury (in H- Q/ q6 `6 q; m* l" l8 B ? in9 D, y3 V8 u& X( d BASE METAL, The underlining metal to which alloying + N+ f% x9 p1 C3 |agents or metals are added. & i ~, H+ k4 P$ B% \- f) rB) K6 \2 Y, s1 w0 D' _ chemical energy into direct electric current. ' M$ s* Y3 q4 n& `* D$ P平衡场长, ! H8 Z8 d, l$ ~当障碍物非限制因素使飞机达到最佳: J. m' H! v8 j$ Z+ i0 v, j* _. s6 @$ y& n' Z# n; ~" @" M4 d; Z2 |# }. I; N* z& b# W2 @# s) K8 D S 为保持飞机, l6 d/ z7 M" w: \9 f/ k1 w* w" e, y9 P' Y* T$ b由粗重螺杆驱动 7 c# v6 K' ]2 h& w, j @0 h+ d' G$ K安定面运动。2 J) s' b. a; u' E& k9 m7 M/ R) ~- d O3 e! i: e" N" C/ i" }7 }( m8 z 用于除去飞行 $ t. ?" [5 L6 | @+ a: V# p) k/ C3 B( w零压力以上的空气0 \3 R+ ~. ^( z/ {( a Hg)或毫巴(MB)来表示。2 X9 u5 g* Q( P5 u% U& A7 @; M 基底金属, 7 F- @8 H/ ~5 V# s指合金中的主要金属成份。 0 T/ I# a5 b& y! M. n) ]7 L$ w- H. g$ [+ I将储蓄 . f( z- _" L; ?7 g英汉对照民用航空词典B OEING. y% k! |$ |: }2 x' e0 m7 H TECHNICAL DICTIONARY 18 ' o1 l/ z9 \6 w( B u0 DBATTER- Z5 E( ]2 D0 Z8 r2 u$ V4 c" @, G! x( w direct cu6 g i$ x( w- V0 L0 e power su0 o! V1 e/ s% A4 e Y BUS, An electrical conductor supplied with9 x) ~$ ^/ i% `! d9 e rrent from the battery or transformer-rectifier for $ S: ~5 x9 V4 Apply to operating components.+ Y: q+ o: q; I. t. s; @ CHARGER, An electrical device supplied3 K0 m g' d/ j- r ith alternating current, which produces a direct current 7 h- a( S$ V" H2 u' vutput for charging the battery on the airplane.. ]% m3 Y" Q. b" T. L) ] AY, A compartment in the airplane structure. 5 Z5 b: c0 p# p$ sCD, SEE - BINARY CODED DECIMAL/ E7 h: Z: B; x- [# \# g0 S EACON, A device which emits a signal for use as a. r% R5 ^; Q! c0 K4 {; I uidance or warning aid. / l6 Y! l5 \ L' i! C" SBEARING (NO. 2), The direction from an airplane to a : L- B! h: H" X$ u/ ?ground station. 2 \: _* A$ F7 N# z# j; n瓶汇流条, , T# [( u9 H' i% N2 _将从电瓶或变压整流器来的直流电供给工作部件的导 3 R2 G" f0 q! X1 l" q6 @# O' m I" H9 _体。5 @8 Z/ X9 j: q, t' x1 @1 u 瓶充电器, ! ]. v* c, h; k用交流电向飞机内电瓶充电的电气装置。带有交流电的8 i3 Z9 n- y. a( b4 k4 f 气装置,该装置产生直流电向飞机上的电瓶充电。 9 r: @8 L- {2 I: v舱,' T% @- F; s% [' b0 g7 F1 \ 飞机结构中分隔的空间。' }1 @; [7 j V$ _' [- Y1 p 二进制编码, 4 D( _( Y \3 u, R+ B8 [$ I* F见Binary Coded Decimal * N" w( c4 l( i& n! r' {' EBATTERY& u1 f* @$ [; l+ P& C, W h) d7 j/ ] w6 r. B( W- s# A3 C5 I# N3 J' r o 6 N7 B( q' c3 \5 g Z/ I! O3 Y+ ZB0 `3 u1 g7 p: I2 J( C B& n9 l! j$ Q6 k5 o5 U( u. v: a B4 l# `# y0 c% ?% p0 K! l8 _% [ g 6 k3 F' O4 s2 {: K! k* BBEARING (NO. 1), A surface that supports a moving ' T$ E4 x1 x; X+ _part and reduces friction between the two. 4 s: O+ t9 K7 I0 J( I: v$ g$ j5 o; Q# h8 v; i* r5 P& [; F7 M) G8 D. M k) w, e. J6 C- O7 j" w# o$ w7 R/ V9 k: \" s9 A( Y. Q( M; `8 c! G2 c3 d. c/ z- b/ ]' F; s% m6 N5 `信标, , T) ~0 F" |! p% R发射引导或警告用信号的装置。1 v1 E/ i+ M$ ` 方位(NO.2),3 T4 s# `$ b# J& h2 Y- S# e 从一架飞机到地面台的方向。 * F: w) L: A" Z+ Z: T轴承(NO.1), . h/ L+ c1 @$ h; w: ]% ?用于减轻机械转动磨擦的机械装置。 1 D6 _* M; t5 F" v/ S9 E! g! d英汉对照民用航空词典B OEING 5 ?$ Q& y) X- j1 Q( vTECHNICAL DICTIONARY 19$ l5 E& ~3 L6 R BELLCRANK, A double lever in the control syst 0 s$ X% S! ?2 t8 }- a3 \) e# Gchanging direction of motion." m( l& v/ X8 D# w2 J em for& Q& ~% U5 {* N0 M; B# k ct in the* X' o4 W+ Q, |, @3 B neumatic system for absorbing expansion of duct due + N& ]# U& v9 t5 c5 \1 @heat. : @# m; n4 {) g% I6 \$ v! m* GELLOWS (NO. 2), Corrugated folded or pleated % `" A6 O& l" yontainer or compartment used to measure pressure. 1 N, y- P) p( o9 uEZEL, The part of an instrument case for locking the * H; y$ \6 ~! g2 _/ d; q9 |- z# f, ^lass. " U6 y. x/ }0 nIAS, The potential difference applied between two P# o+ q7 i9 W. d' y oints for controlling a circuit. 0 L& }* |: n, z$ Y* @( J+ hBILGE, The lowest part of an aircraft fuselage. A place2 Q7 p9 R) Z" k. w0 ?$ V2 r9 S where water, dirt and other contaminants collect.0 E1 v; b8 |- H# M1 T \. u1 i 气源系统内提供管道热胀冷缩所需要的余地的波状 - i5 M; \7 ^& n. Y1 r2 U+ b轫管。" @6 @6 X$ E0 j! r 空膜盒, ( h8 U" ]" T4 J; a! Z- h一种具有波状表面的容器。用于量测气压。 ) U+ B6 T2 N$ l5 e" n# J# L9 a嵌沟缘, / H% b4 F" `- b5 R将表面玻璃固定在仪表上的圈状零件。 ! ^; @# q5 \% |% {+ ~" Z- B" _压, 3 S u/ x E% c9 ?$ Y在控制电路的两点之间的电位差。 8 y2 U X% u" j, W3 H机身腹部, 3 O& _1 S$ R. [2 T8 r+ n+ R机身的最底部,通常水,脏物,和其他外来物集存于此。. L+ v+ G6 n& c# e BELLOWS (NO. 1), A corrugated flexible du / a2 {8 S Y8 e+ B3 q# Op% L9 \$ o* c. n! ~1 u# Q8 a to D; Z% z& ]2 b& u5 `6 d B% E2 J5 c1 T% j c+ q" _2 l$ \. c6 C0 A$ n B 8 L2 S9 x& {; u0 n; ^g + l: v& b1 C8 aB1 a$ u) s0 P4 [5 t9 y p5 |1 `, \/ Q7 }. O 直角摇臂,3 y. D3 U/ Q; t: U+ M 在操纵系统中改变运动方向用的双臂摇臂。3 _1 f- ?, W# \" g2 \& f 波纹管,1 b7 W- R: u8 f5 P3 Q2 m" O* j( r! v: Q0 b$ A, Q9 u8 I" | ?/ A) {: j- i- x7 g5 Q/ W# K0 F% [ G9 U$ w7 s2 C+ `6 f. n! }" F6 ~英汉对照民用航空词典B OEING 1 b3 z1 l/ o8 Y0 s' oTECHNICAL DICTIONARY 20 # ^5 t; x4 i7 |: s: zBINARY CODED DECIMAL, A system of coding each ( `+ m2 x, \ y+ B# D0 o& e* y- Ddigit in a decimal number using the binary equivalent.1 d3 P7 o" \. N9 k' L+ e& J BINARY NUMBER SYSTEM, A number system using: v( r, ?! C5 T, s$ b, R6 M" M& O s 4 B# o- N9 t- V! |& xIT, In the binary number system, the smallest unit of 2 U7 x5 C6 V! Q9 V& x C4 N8 y5 _formation, consisting of a 0 or a 1. ) V3 Z/ C. E7 L/ M9 ZITE, SEE - BUILT-IN TEST EQUIPMENT M6 d: W' R4 H! aLANK DISPLAY, A display that does not have any0 n# m, o% q3 x7 N. V" d" u, n dications, normally due to failure. , S1 Y7 \; i. nLACK BOX, A container for electronic circuits to record: o& u z+ ~3 R9 n7 _& j9 K+ s ight data./ y; [' C1 H' f1 w' e3 l, a LEED AIR, Air taken from the engine to power various ! |' ]) `' R- s2 dircraft accessories.2 A6 U4 J M' h A valve in the pneumatic system for air 3 l/ t. z$ W( C" asupply from the engine or auxiliary power unit to the: I0 g8 {' R: {8 T- S) m pneumatic manifold. A valve on the engine for reducing3 l/ Q$ W" U: M/ j+ N9 h pressure in the compressor section. " r- Y0 q+ K5 z, V$ t& k( I8 e进制, 9 c3 P, S7 V* q4 }/ F! L1 C进制, # M1 g* Y& m1 }) ^& ]3 |, U一般用0和1)和2为底的数字系统。 * M+ x7 g6 v; n8 _4 V7 I特(二进位数), ( N: u/ J+ ?; \7 k" g% B6 t二进制中的最小信息单位,包括0或1。" y1 ] _% t- x$ {9 W; ` u3 z. D8 h 内自测系统,# R2 i* {8 E3 H0 W 见Built-in Test Equipment + B, R+ N) ~6 B. P7 M( dtwo symbols (usually denoted 0 and 1) and having 2 a" a9 R: q2 R0 ^/ W# k* G3 f its base.- S# B! R5 ]4 b% }- V. @ B Q1 I/ C, f9 ?% ?7 {, F in 5 S9 t" z1 A+ ]B 9 J2 @, t9 |( p5 @+ h- \6 AB& B @; S5 s8 i in ( Q! u, Y, K* G6 F( @& }" ]B; M) s: E, }4 b7 e- C fl ! f; Q P4 U* `& Z* qB 7 d' D6 i7 Z1 r& t5 }+ w: D( Za & X, K9 s3 o8 a5 n5 G0 FBLEED VALVE, 8 l# ?/ L* ^0 i9 S8 x/ ?% y二进制编码的十7 H' ?8 p% y2 Y) o 一种编码系统。用等效二进制位数编译十进位数的每一 h; O' T- S: V5 @- @7 B! |0 L 位。 5 @6 [# L; w) O O9 J# l/ A( `% A! F% Y$ t5 L% l: v% ^以两个符号() a6 Y7 {! {1 j4 B7 @& A& @3 ?6 g# P, R, T4 V) B. e1 v. - F5 X7 }7 j A) q+ u) a( G; p白显示,( g) ~2 Z# r1 P/ r: } 通常因故障而造成的显示器上没有任何指示。 - w6 E% X. U6 B匣子, 7 E# P7 f5 c/ t# @1 i0 N装有用于记录飞行数据的电路系统的容器。 2 o' J" J. r: V- h8 O" q# z' ?气, : n0 i& T/ Y* E3 p! P8 L取自发动机而用以驱动飞机上之各种附件的空气。 2 A9 {6 i% T0 n2 M气源系统内,使来自发动机或辅助动力装置的空气进人9 \* C! f2 s- k+ D7 \: b 气源支管的活门。发动机上,用来降低压气机压力的活门。 ; u, Z5 P( e4 Y) s9 B/ @. m5 x. A- M7 g; u% k7 g; Z3 T9 \5 Y! w1 z$ r1 h) o6 t' @; E4 v! `7 o5 U9 w+ Z: }. s: | 引气活门, - c5 M) J4 C3 h英汉对照民用航空词典B OEING * O& o& j2 i6 E' M% e! w1 }TECHNICAL DICTIONARY 21 " C3 v- Y2 ^. {BLOCKER DOOR, A device on the engine for blocking, Q4 W) g# y9 h& \; m the normal airflow during thrust reverser operation." A+ T3 C4 V7 A2 | LOWER, An electrically operated fan for circulating air.; s: _7 X2 J1 \. O, j! g; z2 q% J LOWOUT PANEL, A panel in the structure between' I$ t+ l. T& u1 L6 d! E, A( Z o compartments that opens to equalize pressure in. E/ S: g: c+ h) G2 _5 T7 q e compartments.: l. {5 f K* f" ]/ `0 P8 M ODY GEAR, The landing gear attached to the/ T5 x3 E' @' O0 j; o: n, M6 u) \0 r grounding." S9 m9 ]3 {- j+ ?% ` 正常的 $ F1 t: B6 j* ]8 H- o气流。 $ p' |& Y) p X3 E0 O0 O鼓风机,* @, u$ U! u8 P: V* }3 t6 x& w7 G. K 用来使空气循环的电动风扇。 " N3 X4 M1 \* F) Q7 |" D压口盖,- U+ `/ v, X7 W- i8 b( m1 f: g 两个隔舱之间的口盖,打开后可使两舱压力相等。: E V; p; ]2 N, w! z 身起落架, 1 r: `2 b* a4 [身构架上的起落架。 9 [9 D8 o+ ?8 Q) wB & T+ @. Z4 a4 q! B2 dB + W+ ~* q/ Y6 g: [3 ]tw : [) f7 ~" j( ?th. v6 [8 a& h( c: }1 m5 H2 m( k B% H5 n# }% ]4 g# P fuselage structure.) M F' } w1 D. y; X' r2 {3 k BONDING JUMPER, An electrical connection between ' G. S3 p& q7 y9 N- _* [$ D& Wa component and airplane structure for electrical , d# c# H. W2 C+ `$ e阻流门,# L% o3 r3 P0 k; {! ] 发动机上的一个装置。在反推工作时用于阻挡" B* Z ?! w- K; c1 T2 p' b( r6 |/ R4 I0 `2 [3 J$ p7 e8 t 装在机) n9 y% c0 R# s2 [- ` 搭接片,) M, g5 ]* w3 u- ] 连接某个部件与飞机结构以形成接地的电接头。 * g. A$ f+ n6 Q英汉对照民用航空词典B OEING / @2 Y: r& D% F3 d1 F6 Z JTECHNICAL DICTIONARY 22' h' {9 C: e* \( ^/ Q1 D+ `* w BOOLEAN ALGEBRA, A mathematical system for9 M( N6 t1 k$ n4 N3 f writing combinations of logical statements." s+ ^* s# R" P, W) i+ y+ D BOOST PUMP, An electrically operated fuel pump for+ P8 o! s7 `% h) t; {1 g) C fuel supply from the airplane fuel tank to the fuel: g! n) j+ V3 w manifold. d8 N' L0 O4 cBORESCOPE, An electro-optical device for looking at 3 t$ B; h# g. b E5 |6 u& v5 @ternal parts of an engine through holes in the engine.% J+ g/ Q2 U: g/ C orescope ports) ( `9 f) j3 O+ v3 h: C% ?7 N6 UOURDON TUBE, A curved flat tube in a pressure gage! ^ P% s" P- g7 J y! C; K) F0 J" r5 J r moving the pointer when pressure changes inside " }/ N5 E7 p E8 `% b5 d* N6 O/ von the ability of the brakes to$ e+ H. s6 z Y2 E* G/ y bsorb a predetermined amount of energy during a ; `6 x' S+ D6 k; x7 _! Kjected takeoff. : r7 u3 t& `- \4 N3 U0 A用于通过发动机内的孔(孔探口)观察发动机内部件的, S$ @% K5 O+ p) `3 s) w 光设备。! k1 L0 P0 v4 b; _4 h3 F 端管,2 @' r2 g7 A3 E5 ^ 测压计内的弯曲扁管,管内压力的变化时它使指针移 , n8 r# k+ |9 P9 ?, m) h5 S" U D力。) s7 B. j0 C+ s N/ }8 l 极限重量, + ^1 x4 w' C6 q- k9 I# J) F6 e' r/ i% V. }: e 起飞重量。6 f- N9 Q4 m6 _. Y2 z2 D7 w" {3 x 发动机滑油系统与大气相通的通气口。 3 a* R9 U! U4 u5 ]" t; `in X8 [. t! T$ y1 R(b 1 h* F. v; A7 A* M/ J, A' DB . k+ u. J- { W$ S7 o* b* Afo - H9 B) y1 \4 e. lthe tube. 9 r! u# l. P3 O; _* L% D( w6 X/ pBRACKET, To enclose or surround. - c/ m: f! G; C. d+ ZBRAKE ENERGY LIMIT WEIGHT, The maximum4 }, V# {- I9 x5 e, a8 B1 B8 A takeoff weight based" j5 N( O L9 p, l6 Z a! s, a# X- w7 |* K- s re4 m w- c J% o5 k: O BREATHER, A vent to ambient of the engine oil system.* w1 d( o3 c; `5 U. U: M% S 布尔代数,8 }3 s+ G5 ~3 f! F6 Y& L4 t 一种用于编写复合逻辑命题的数学系统。; d) M& [) G- n* k0 D 增压泵,& [3 {1 M& b, ~2 W4 o" o9 h 从飞机油箱向总油管提供燃油的电动泵。 ; K+ a2 {, f) P: q孔探仪,: k/ f& U! S& R# G, J4 l) _2 G/ S' D: n- S5 d9 t5 u1 x; T- d- {6 v3 d( x: J# m7 |: ? 动,以指示压 & D6 g- L1 ?2 A& e; G托架, L; } s9 T6 c. i! e" V% P+ v用于作支撑、装托、或围绕之用。 " M( N+ f$ t" w刹车能量 + M3 e2 D4 V. _' l j中断起飞过程中,取决于刹车吸收预定能量之能力的 3 N! j) B: z; m7 l- }8 t7 T/ w$ }9 `: [- C通气装置, , ^% p9 y' E) l英汉对照民用航空词典B OEING* s5 E* I) t3 e' { TECHNICAL DICTIONARY 23 4 |! X) z7 S9 bBUFFET, Vibration of the wings and airframe resulting $ d) h0 Y( Q. rfrom unsteady airflow over the wing; caused when 8 _3 ?4 @) l3 l, s; Kairspeed is too slow, the bank angle is too steep, or f) M9 ]( p% \irspeed is too fast.. a, x' M0 \$ X! g G UILT-IN TEST EQUIPMENT, Equipment installed on 5 I0 ?5 h) `4 N6 K$ ^) je airplane and in airplane systems to test the systems8 Y, a: J* w+ S ithout external test equipment. " p3 ~ W8 ?( P' {2 ^$ f! GUFFET MARGIN, The amount of residual maneuver3 R+ @" T# U1 n4 m2 a apability present before the onset of buffet.9 F* W J' @7 ~% C1 @* M/ U UG SPEED, A preselecteed speed to be observed8 I- ^: a4 L# w O nding sequence.7 D5 f3 Z# e9 y* F k $ ^0 @( H6 m" t9 B: ?) yng landing gear operation. ; p. S6 D& J# y, N+ o L# C" C速度太慢或太快,坡度太大,均会引起抖振。 - D a# y0 q; h$ Z2 s% ~自检设备,; m1 n( I, A; W" T4 l* A C# M9 w4 r# F6 V 安装在飞机和飞机系统中,在无外接检测设备情况下, ; q0 u+ J4 a4 H9 v) L4 E用于检测系统的设备。, b, A- [+ W' B6 ] }. f 抖振裕度,- B! o, Y4 |! V& ~: d7 N 飞机在遭遇抖振之前,剩余机动能力的大小。. U& V* \/ W; O+ J% d 标速度, ) ^8 U3 P+ h" F9 M1 @7 d/ F7 M在某些机动飞行过程中,特别是在进近和着陆时,飞机( a( F# |2 ?4 O. Q( k9 I 预定速度。 0 n% ^2 U2 \7 n# T# {力装置,3 ?. }6 b; x1 ^/ H 架工作的一种机械设备(弹簧或减震器)。. I8 ~' I) I% V! V) W/ c# E( r 流条, ( k0 z- c. c2 P) l1 ]' n在部件或组件之间传输电、数据、或定时的单一电线或 . i% z: {- b3 v% _+ z6 c, ?a2 R' T" p+ O& I6 q. E' T* O B B3 W7 k# y' Z th + Y* j, D. ?* Lw ' H. a2 D. v; _% G. h- l$ i' Q9 TB, |0 ]* {2 ?$ G c 1 l: ?/ C. N2 ~! M1 t( aB6 o7 ^! F0 b7 [7 ]1 P during certain maneuvers, particularly the approach and5 k- B6 U" m8 a9 ]( [5 v- q0 @ la - z8 q" s& C6 `$ q' B' f" o# kBULKHEAD, A structural partition in the fuselage or + ?1 V) I$ O/ p7 |wing.4 o4 n9 r6 b' P8 [ BUNGEE, A mechanical device (spring or a shoc 6 e! @" K( n% D4 iabsorber) for assisti . d. ?6 r R2 J( ~9 DBUS, A single wire or group of wires which transfers 5 C& n6 K0 w0 r* M0 u# Ypower, data, or timing between several units or 6 R1 t0 L: n: T# k3 hmodules.4 {- x4 X v) T1 D 抖振, 3 y T; k& v( w0 F$ y5 O+ w由于机翼上表面的不稳定气流引起的机翼和机体的振 # E( Y& M- [8 y动。飞行7 P0 b' h( h; ~/ z. D5 M0 M: v4 p6 ^8 c* \- X; k7 G所应保持的3 e: `5 U4 [) g% w! _, i& v 壁板式隔框,, @+ O Q4 G. u# m$ p1 G 机身或机翼内一种结构隔板。( S0 H& N( B3 j/ `0 B. ^( M- O6 C9 K7 S/ e# T6 o 用于协助起落5 j9 l. M" C* I+ A1 F8 X' z; w7 e! f- X" g6 A4 c D 电线组。 I: [+ x0 A# I' N3 f9 `英汉对照民用航空词典B OEING ; ^5 L) \. e1 Q B) b8 o8 OTECHNICAL DICTIONARY 24

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BUS DRUM, A mechanical connection with pulleys& R' e* W/ h, y! w% ? cables in the control system.: `2 O) `+ ]# Z y3 E3 a$ a$ R3 L( h and & s, M" o$ N9 ?( z% _l circuits for control and protection of : d5 p( h' H- a/ C B. U6 W% \( hlectrical alternating current supply to the airplane.$ W& ~6 x& }: L" P& F- S1 E/ e) u/ R duct for closing and opening the duct: [" k6 \$ i. X! Z5 Z6 E# g( _4 I assage.+ S. i' L! e* N6 O UTTOCK LINE, A vertical reference plane along the* W8 A- U" V: {6 Y" J% i* g2 A selage for horizontal measurements of the airplane.* c" x( P3 H! G& D 接。) W: L ]' d' \$ e6 _ 组件,内含控制和保护飞机交流电源的电6 Y# ^8 q( D- g [4 N5 B1 ]% \作动简控制的转动装置。用来关闭和 & q5 y9 U7 v# h$ X启管道。 6 p; V- i$ l7 T: |沿机身走向的垂直参考面,用于飞机的水平测量。 $ z/ z6 k* t: `# H, xBUS PROTECTION PANEL, A module (black box)/ z e% N) ^) J0 m( `+ A containing electrica ; W5 j* A' ` U' J! b/ Je 7 h' W3 O/ _+ x7 [3 E& }BUTTERFLY VALVE, An actuator-operated, rotating# A* c0 R# h" b device in a3 U5 Q+ P- w% _! K6 r: u; K* ` p 7 V. R, m! ]/ x" r" QB 8 Y- F( @" d2 {: |# `fu% F) M! N3 m5 R A2 n. X: Y" h 转动鼓轮, 8 D' v! E0 Q L( _* B$ v在操纵系统中,具有滑轮和钢索的机械式连 * o4 M+ p% z/ Q3 ^; a3 P. F汇流条防护板,0 b! a9 M7 t8 z% [. W5 _! b 黑匣子式的 - b0 Q8 c# x4 g' d8 g- o* Q+ }# z: I/ T H) c蝶形活门,! _/ H5 |: d4 W/ F8 _ 是一个在管道中由 * `9 k2 I0 Q1 ]. e7 J* {. z% e2 g: I9 ~5 e( u5 x- N纵剖线,% {0 Y5 r. \; r; ?7 E 英汉对照民用航空词典B OEING 6 Y! y3 D2 s# r) ?4 rTECHNICAL DICTIONARY 255 z& ^+ m {; M O+ J: |( w1 | BYPASS VALVE, A valve through which air or fluid will/ }$ A/ O5 Q% [ flow if the normal flow path is blocked. % j# X/ A5 h4 [9 k! UBYTE, A group or string of binary digits. A byte is, O; ~2 q! C' n7 w9 M/ x9 ^0 c sually eight bits long. % C7 A/ b& [5 gABIN ALTITUDE, Atmospheric pressure maintained4 m( }! L+ R+ q" U5 n' c _) a ithin the cabin, indicated in terms of feet above sea6 s5 }* \ ^/ F4 d ALIBRATE, To repair, adjust, fix or correct the5 d8 I: N* u* a# B& U3 C easuring capabilities of a measuring device.& w( s o; `+ T0 h% Y+ s ALIBRATED AIRSPEED (CAS), Indicated airspeed+ p# P* K( B J3 D AS) corrected for position error.+ ^6 ~. {4 m: n3 M; [9 t nical4 p/ ^9 {+ v+ [ omponents. 5 S8 {+ Y5 d, M* T, W7 C# T* }% Y$ y% i! I+ q9 C( w7 C节, # B2 r% T1 `( A8 M/ s! k一组或一列二进制数。通常一个字节长8位。 + J# p2 D0 ~- w6 }6 ?4 u) q舱高度,, Q) x4 [% E& }/ } 座舱内保持的空气压力,以海拔多少英尺表示。1 s5 Q# K+ M9 H% U( i6 n, J0 x {8 s% E 准, - Q, N% _, x9 M5 u7 a修理,调整,定位或改正测量装置的测量功能。 + S! h; L+ C& ~1 }, Z9 d正空速(CAS), 5 Q$ M& Z; O( o3 o' {8 R在修正了位置误差之后的指示空速(IAS)。 * f, \4 E" E8 @- e) n用来移动机件的一种转动装置。! _2 z: T/ T8 G2 x# g) B8 g u 0 u8 x- G5 G" h) y, Z: @6 F8 R& kC 9 I) U; Y- r) U$ o6 z9 ^5 Y0 pC 0 O; |4 I# v, W! o3 nw* O% P; I, e, n8 V level.9 v: e" ^- a5 m* e- e4 u C " q; i: D/ K. I6 T1 Dm $ F! P; X2 J; J9 m) nC ) v9 u4 w/ x! E! U(I7 t1 X' ]' m G. J* f' G7 l CAM, A rotating device for movement of mecha! Q$ w" I s% U. R, }/ {, W# H C : o, \' m' d o0 T0 H& D) R6 q! n) n旁通活门4 S v4 n1 P: t 气流或液流在正常通道阻塞时所经过的活门。 ' {4 u$ }% ^: ?" t* k, t6 A1 V/ K; c+ }/ |1 R* A0 n5 a& I! W5 ~% f9 z0 P$ L' O; v. {7 H9 P' [0 u1 F. t6 q" O" w9 p( i凸轮, ! R1 T9 t& Q# f6 U3 ~5 J英汉对照民用航空词典B9 `! z+ x' G- J9 X CAM-OUT, An autopilot condition in which the actuator$ s6 `& [- h, j* {- Q9 V8 ?$ z detent piston is overridden, either manually or by the 7 h: c& K% n3 ~/ j* Ether autopilot actuator.: V$ n+ z" f5 h' O, y/ i8 U+ Y AP, SEE - CAPTURE 8 L( {! {6 J; O* S& A8 NAPACITANCE, The measurement of electrical energy $ H1 U6 ~2 E3 V% @' qtored in a capacitor (condenser). , i( _1 n) F! ~% i) QAPACITOR, An electrical component of two metal 2 B; b1 f/ p$ `, A7 Hlates separated by a dielectric material, for storing * ~+ \1 b g+ l( ^$ U/ Olectrical energy. j, Z* O4 t0 E( N1 SCAPTURE, An autopilot or flight director function to % f0 o. x3 A& a8 m" Bacquire a selected mode. 0 u' K* k3 [ }5 l% i( u( vCARD FILE, A container on the airplane for printed 3 p6 N& }% q0 t; Ccircuit cards. * x( H: s; d( f% V* c+ v9 {& X一自- U+ q }2 F! ^$ T 动驾驶舵机所超控。& y, z' @! I J 截获,! r& l0 b2 V7 T4 q5 F8 o8 d 见Capture0 j6 x8 s: T" W0 } o 6 Z; I+ h' @$ R2 j0 Y2 ^C7 N% Z/ q. l1 x C 4 {+ h1 m- T9 N" T( P/ t/ Rs ; @ H% |4 U/ w3 Y0 jC 9 V# Q% j( U9 n: {p- Y, g$ J) |8 ^/ ]# | e2 ?3 F. J' J" {2 R& P) J 凸轮不工作, , A" @+ [" G! g* W! L一种自动驾驶状态。此时舵机锁定活塞被人工或另 . A2 @* K0 @; r. o; l& G$ q( Z0 A! ]* M# k, M' X% d+ S% Z 电容量,0 K* V$ f" c) S 电容器内所储存的电能的量度。 ' u6 Z/ y4 b5 @7 E' W8 j容器, * O2 E6 O! A; e" a两片金属中间用绝缘材料隔开的电器。用以储存电能。) i7 e2 R. l3 ], c9 j% } 截获(CAP), ( D% g% l! u" B6 N7 Y自动驾驶仪或飞行指引仪的获取选定方式的功能。 % ?/ C. z; W4 y$ ~& q线路板盒,4 n. y7 C' G# R( I6 G7 Q 飞机上安装印刷线路板的容器。 - }, o) r) W: m$ Y- N7 Q) ~0 A L i+ X8 I* z! O% J( N7 Z OEING1 o) u E7 e7 w% y8 n* v TECHNICAL DICTIONARY 26 / q+ O) d: s' z* f+ T7 x3 N" o英汉对照民用航空词典B OEING1 }, k( e5 ]2 K& A TECHNICAL DICTIONARY 27: @8 K2 g! B N; `7 u% Y, ]; d CASCADE, Two or more similar circuits or amplifying 1 o/ E0 R+ b- e7 o9 u' nstages in which the output of one circuit provides the0 q' P; m; R5 r S put of the next. 8 l) t7 H- F b" S Q- UASCADE VANE, A vane for turning the engine airflow/ Q: w- c$ |; @7 {5 ]0 s uring operation of thrust reverser. : [0 v# J, C" D- a6 G) ]0 [2 eASE DRAIN, A drain carrying lubricating and cooling, r% T) ]+ x# M. y8 Z uid from a hydraulic pump. & C( G- Y# W5 ^* l, ?ATHODE, The element from which the principal $ ~% h8 |/ U6 s1 |tream of electrons flows. . ]: `, T2 ]* T4 G0 ?( tATHODE RAY TUBE, An evacuated glass tube with a 8 d" B3 U7 `4 H9 ?CEILING, The height above the ground or water of the; | \3 k2 @2 n. q0 K base of the lowest layer of cloud below 6000 meters2 B+ J; H8 I! O# ]2 M (20,000 feet) covering more than half the sky. 7 v4 n9 B2 A3 k2 C4 t4 P程。该 8 C }7 Y9 j8 P程中,一个电路的输出为下一个电路的输人。2 H. w& q0 @& F" ?+ }$ U6 B 叶栅叶片, # `& v0 U7 m& q: T- B在反推工作时,使发动机气流向相反方向流动的叶片。0 H: q3 T0 V R* r6 [# G# }. I! u 匣余油管, 6 P" K# S$ s2 ]液压泵多余的润滑液及冷却液的排放口。 $ ?$ k% L) l7 h: c8 [极, 9 a4 s4 R% Z; A% Y电子流流出的极位。% `& _2 E& x' k, F* L 极射线管, % M- k+ C* t. n$ x9 ?: z. N- G有显象屏幕的真空玻璃管。用于显示信息。 0 L( y9 I) M5 T, p: E% p云高(云底高), j2 r5 R/ l+ U" _ ^6000米(20,000英尺)以下已覆盖一半以上天空的最1 V: b' F9 d6 b. f! p! \* b, a3 U/ } 低云层底距离地面或水面的高度。" e1 N! L, E" p- W* S/ z; \ in$ [! B4 {- w$ T v# ^$ d" ?/ B& L6 b C u: M4 {( J! q6 f# vd& U9 n s2 O2 k C 3 ~# C6 ^5 X) V. ~fl6 }9 {5 T/ \0 Q# Z C 4 [. v; y3 [/ _0 T/ v2 rs / N- \9 w) e/ B' D& ?8 aC/ e" ?; p" r4 Q5 v" v viewing screen, used for displaying information.7 P) }1 j2 t* G9 j( a: M/ N3 W 级联, ( `- N) _: [0 Q# J两个或两个以上的类似电路的逐级连接或放大过 ; e1 l* w2 F; o4 A1 e6 M9 M- ?1 u0 S, E/ A1 t4 U4 p% I) @! }( R; R# K0 m9 d" l) h7 p, S5 T2 U# ^- ]' s0 W9 _9 D( I2 _: y9 G 一个具 ) K" T0 B, E0 N7 } K! q; P英汉对照民用航空词典B OEING : c. M; ]# E9 m6 i& o2 [0 s6 P1 \5 `TECHNICAL DICTIONARY 28- }0 V8 H5 b4 a) s CELSIUS, A temperature scale in which zero is the% c d$ [: w9 K" o freezing point of water and 100 is the boiling point of; K1 `& Q/ y3 s, U. x- W; r water. 4 y* m0 W+ ]0 g0 `' o7 V/ ~4 bCENTER OF GRAVITY, The balance point of an object ( F' B, y2 E5 V4 S4 \; j6 _r rigid structure expressed in terms of percent Mean' E) R# I0 U8 J9 [2 P: A erodynamic Chord or in inches from a reference point. : {( t3 I4 H* X2 F3 _/ p1 kENTERING CAM, A cam for moving a mechanism to a" m" h5 ~2 y' L5 }4 U eutral position. g3 y8 i% B# k, N IGURATION, A configuration of the 4 X! U+ Z# l+ L5 F tircraft approved for operation by the local governing! A0 l5 U0 E/ h4 Y# z- G/ x- q, Q gency. 9 y5 c, r7 g& ` c* F! wENTRAL PROCESSING UNIT, In a computer or " o5 E, n' c' }$ Gigital circuit, the section containing the arithmetic and0 v6 _' b* U6 I- u) V gic,control, and internal memory circuits.- I9 A, T4 |' ~& C) y0 ?+ K0 y ~. | ENTRIFUGAL FLOW COMPRESSOR, A type of ) y5 {0 s$ Q+ }+ b2 s. W) x1 Vompressor in which air is taken into the center of the ( Z* g7 D% `# H1 y5 epeller and is slung outward centrifugally into a diffuser/ u1 Q! {' S; h9 s4 H% z) L1 o1 L here it is slowed and pressure is increased./ d& p" j9 w7 Q, s/ X W CG, SEE - CENTER OF GRAVITY + _+ {+ q/ [; ?7 {& ?) Z构的平衡点,以平均气动力弦的百分比或 * i( Z1 m7 ]) K! E6 T某一参考点若干英寸来表示。 + f) r2 r% _. P% g G/ V& D中凸轮, + z5 r: J" X& ?7 X7 E将机构移向中立位置的凸轮。' o( _" ?: O- |% O" u2 l! B 格的装机状态, 3 O" z! T3 Z& L( G由当地主管单位批准使用的飞机装机状态。$ \: K. A; s- z, Z 中央处理器,9 c$ Q+ V4 b) w" R 计算机或数字电路中含有运算,逻辑,控制和内部存' }- Y' R3 g3 V' t; B9 [ 储电路的部分。# l4 g; Z6 ^( H! M 心式压气机, 1 k. @" G2 |8 W U& C. _* z压气机的一种。当进气到达叶轮中心时,被叶轮离心抛 Y+ ]; ]+ g: t进人扩散器。在扩散器中气体流速减慢,压力增加。4 D5 g$ F& g4 t' c$ a 重心, & ]' d/ M) Y3 j见Center of Gravity _5 j, S" n. H H7 x# ?5 v& n: go0 i4 y- E$ s4 k8 S; b0 H% J8 H A4 J6 h D8 o7 g4 N0 \1 R K( m C # ]" u+ p: k9 k* r( In; q4 `9 P; O& {; G5 ^, e# q CERTIFIED CONF( w* t8 a: n) U) a2 m a6 W: n5 _# R* J T4 [. V a . t- X/ K s2 O' cC # `3 I/ I* l& s% T8 ed 1 r# u: |+ m( |7 y* \lo % s0 d& B) W8 V$ J# v/ E$ q/ GC/ r6 X) m! {& b c) G+ N0 G$ f# G5 `$ ] im 5 I, m% s6 l$ h v( c2 k4 cw y: ?. o E4 W4 k8 ~摄氏度(°C), 2 |3 k' H: W! D) }3 G$ l7 S6 Z温度的度量单位。在此单位中,0°C表示水的冰点, * o( O6 J2 F6 q: B4 g( Q$ ]: x$ E100°C表示沸点。 - ?, X$ V E6 R/ s9 g* x重心 , { b, E4 x- I9 _- k9 ^+ b, O物体或刚性结 + u8 G5 Y/ [7 D% c, k8 x1 @+ V9 G. G' J* s3 j1 V0 E1 m/ X: X* k4 }8 O3 [; Q# {" M2 @( h! U4 [9 @7 R* ^3 T' C* E: g A3 F4 ]( w, X; c7 I, l+ g! L6 W. p0 L4 e) n' r; ~/ C( t% q3 d/ s 英汉对照民用航空词典B OEING * g3 F' A+ L0 uTECHNICAL DICTIONARY 29 " |: [! ~; O; Z! w! v+ ?CHANGEOVER, Conversion from one mode to another. ! M c6 K, f t" q& ]$ n, ?HARGING VALVE, A valve for supplying air or fluid to6 v+ m2 R( j, k HECK VALVE, A valve allowing flow in only one; l3 e% {- b8 {+ T1 \ irection. See Non-Return Valve.' t8 A; F1 Z9 \7 O HECKSUM, In a computer, a summation of digits or! W3 i1 [* Y7 g+ k! Y# X& c* s its which are primarily used for error detection.& P$ Q! k! }, [ HIP DETECTOR, A magnetic plug in sumps of1 j. s4 K) f& t( x/ e* Y# M: R! ] bricated components for detection of internal failure of 7 w1 n% i* S& b+ N# ~e component. 9 e# O7 A0 }3 d3 F; oHORD, A structural component of spars or frames.: F' p% c. y( e5 Z$ } 添活门,: N6 g1 v' Z! _: p( y. a 器充气或加液的活门。 . ]9 g/ Z0 ^% f4 k单向活门,1 G( I. o+ p5 c5 C 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! G) X9 ]5 k! W) F$ ^8 {) j a reservoir. * p( v' E8 s) |7 EC ' g& x+ S V3 M3 _1 dd T9 y/ [1 @+ e1 a C 4 q6 a9 B6 v i; ~4 }( S& g" q, f1 mb2 z6 Z2 B2 x2 u; d1 `" v2 p C 7 p! k I. r U& r5 Ulu & O5 T9 ?6 {' Hth 0 j$ a, d/ S4 N( NC , S6 G6 o+ d) E r. ~9 I转换,8 t$ F; ~0 k% p0 o( V p 由一个方式转换到另一个方式。5 H4 o) F) u$ j( s( C! D0 I9 l2 X* F: l 用来向储存/ `7 O9 l b8 V3 ^; }% y9 Y [8 q9 G; V. t" U2 w) @ 总和校验, 4 b4 |+ _' d2 f8 d! l7 B, I9 y计算机中,把那些用来探错误的数宇或位数的总和进! f# j4 B4 a& P4 ?3 f2 r" Z5 ~ 求和计算。 + b7 j$ z' O3 z7 h' U属碎屑探测器,/ u; D, Y8 R3 y- W6 W$ a 装在被润滑的部件滑油回油管路上的磁性塞子。用来探' k7 m3 @' O; F4 d# y9 D; q 部件内部有无损坏。: {4 A8 @2 a: \" B 弦, % U/ i, I9 M6 R7 Y梁或框架的结构部件。 # F; V: S" @9 A0 s+ y" C' F4 M4 r. Y( f( o0 p4 R& D' A/ z* S1 }3 V& J# Q- K+ j" W, C; @7 K# N9 L9 d7 U9 U( s6 [) j, q6 X+ J1 B7 b1 @ 英汉对照民用航空词典B OEING R8 R( `3 o7 QTECHNICAL DICTIONARY 30 # j, R7 H6 U" W3 v6 W* `CIRCUIT, A closed path through which current flows! k$ Q% x. ^/ r: f ource.7 q3 S; W2 F; m/ P0 J IRCUIT BREAKER, A device that automatically : @ n; }5 e8 [* m- Reactivate the system.7 ]' f- _* Z2 B! q lear of all non-frangible objects which ; ?: E, C# P$ Y. ]* Lay be used as takeoff distance available when8 d5 U5 ]% q( Q- J6 {- Y9 W alculating a takeoff weight. + b! |: C* E$ l% Qr water under the control of the appropriate$ W) @3 [7 G* w" f1 u) y uthority,selected or prepared as a suitable area over4 H3 \* L+ [5 E- i hich an aeroplane may make a portion of its initial. x+ R8 R5 i5 D9 b5 M) { limb to a specified height. % Z j3 i7 d! Z ?1 R8 j! iincreasing.% |+ {8 }$ x- ?! F7 J sed 3 Y; e* T y3 ]( a9 ?, @LOCK SIGNAL, A continuous string of pulses used for 2 M! S; v& f6 J U1 U. h开关,6 z% h$ p/ Y0 d. ^' G2 \* x6 N 故障情况下自动中断电流以保护线路不受过电损 $ W( ~. E- e6 ]5 t体障碍物的区域。在计+ b# K* J* P7 |2 J 起飞重量时该区域可作为可用起飞距离。2 i$ h4 ]3 {( a8 }6 U% T 是在有关当局管辖的地面或水域内一个界限明确的长) V, R' ?; \' }7 C D 形区域。在这个选定的合适区域内,飞机可完成初始爬 ) J5 j8 T5 c- O& a: Z的一部分,上升到一个指定高度。 ; j5 {3 T+ F. Q% f9 V8 Z飞机高度不断增加的飞行阶段。) ^% t& z* Z. S7 E; v 钟脉冲, " E' H) W+ P/ L. }2 b步的连续脉冲信号串。 % R1 m% b T I& i3 Yfrom a source, through various components, and back * p' E- q& S- H% O2 f* N Xto the s 5 g6 Q/ {" l2 m& z( N* m, EC & y; }' r! X x0 K. Ninterrupts the flow of electricity (current) during fault) @2 b" ?, Y7 [+ ]. m( k condition to protect wiring from excess current. Circuit/ Q/ |. K7 z" o @' ` breakers are also used as a means to manually 2 y( @1 {9 J' E) wd ) Q: |/ r$ u" E, H; N9 ^CLEARWAY 1, An area beyond the takeoff end of the8 S } l3 k) Y" S runway which is c' O1 V o( w1 _# {: X/ S m6 H; [; k3 R8 L7 ~' v5 o c5 ~- q. c- x/ k, ~& } H" P+ }( X# N CLEARWAY 2, A defined rectangular area on the. w7 p! H$ |- Z$ B7 E ground o " h" o* X7 L! {# J/ S" Ka * W1 @+ K% e$ g! y: `- mw - j( p& [: p" n( Rc! w# v6 Q4 S2 J5 i9 F B9 J CLIMB, Phase of flight where the altitude is1 K, Y' K- e9 a. a' k CLIMB LIMIT WEIGHT, Maximum takeoff weight ba$ z" `8 p9 q; i: }+ n5 L on a minimum climb gradient with one engine/ ^/ u* t9 C @6 g inoperative.9 Y( q- ^2 B3 E# N) | C' a7 `2 d4 `" n2 f3 r2 l0 W% C, _ synchronization. / [- Q% w: V3 c0 s1 y( J电路, 6 w- K, v4 y+ f一个闭合的回路。电流由源头流出,经过各个元件流回 ' U7 b- x/ \; N7 `$ m源头。 9 F+ T. C) ?; x; x2 \2 ]- d+ j E3 A- H 能在 9 }7 q9 K( ?. ]. d- c, B坏的装置。跳开关也可用于人工使系统无效。 " |+ K' ?, R o+ B一号净空道," G1 h" d& x$ b* t 是跑道起飞端以外,不含任何刚 + j8 K% d$ g; `1 H. Z2 a# Y+ _) ]* j: d, g9 U 二号净空道, # w8 t7 B/ e S$ j( k+ }. c9 B1 f# R0 ]& z& `, j2 _! s# @* S" \. ` F5 j! A爬升, 2 Z. y7 l+ h+ c0 g7 A5 g6 ~& X- e爬升限重,& g/ m0 T" x, Q# Z8 |; N- K 取决于由一台发动机工作时的最低爬升梯度的最大起+ N2 b8 z7 |4 Y/ ] 飞重量。 3 z. }2 j3 p$ _: {& B f5 ]/ G2 k9 R3 @" K, O- O0 Q8 \ 用于同7 E& W6 B$ _+ ?3 C" R9 z 英汉对照民用航空词典B OEING ' W* r$ w$ }8 U4 RTECHNICAL DICTIONARY 31 - n' ?/ h7 O/ I" R4 V3 ]COALESCER, A device in the water separator for 0 I g! u3 D: b, k, Wollecting moisture from the cold air. . G+ W( o* h) u! {! m r! Wn antenna with a receiver or transmitter. 7 n3 C" J$ ?% b7 O9 b7 R. O' C( Che cable has an inner conductor and an outer ( H" W1 s# Y8 p, X' Frounded shield. $ Z9 e: Q* D; H$ w" j) t/ ating one inside the 7 v! \/ Z5 _* cther for rotating the low and high pressure 9 D' M6 H, T9 ?ompressors by the low and high pressure engine & x! T7 a: `5 P5 Arbines.4 g# F8 D J: z OMBUSTION CHAMBER, A part of an engine for( G; e, |" A3 ~) F urning fuel in the air supplied by the compressor. & x1 @/ i5 \' ^* z! i* z置。 ; {1 q Q) V* v' i射机的电缆。电缆 / `1 ]; \) {, L4 y7 E/ ?! p中心导体和外层的屏蔽所组成。 * o8 E; W, I; h. |; |两个套在一起旋转的轴。用于使发动机低压和高压涡轮 : N0 O$ O4 F# X4 L4 ?+ Y) n别带动低压和高压压气机。% h$ E$ c, Y) ]9 U( o3 @ 烧室, * P/ c: c; ]* }* [4 j6 N7 x1 Y发动机的一部分。用来使燃油和压气机所提供的空气相 $ ~4 \* b7 U: Q# H$ i, s" g& U& o合而燃烧。

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发表于 2008-12-24 21:38:35 |只看该作者
c 1 U1 j' U7 ^5 B3 I! hCOAXIAL CABLE, An electrical cable usually ; v7 N L, A% d. ?: J3 ?/ `connecting a Q7 B, R1 c: \T( S2 r( b" |/ `/ l& ]& U# p g# ^& q3 j6 `2 N/ E1 g9 _$ k COAXIAL SHAFT, Two shafts rota: i1 b0 }0 m8 N8 C o3 v( e7 E: b; _$ C9 [- J' [ c 8 o. Z! m _! I/ H. ^0 U4 utu5 v4 u1 s$ q- X' g9 @$ P: {. { C0 m5 o% h) ^9 k1 ^) ~/ K- F# x b/ r% {7 s4 [' o. b) q9 x 凝聚器," ?: j" o$ H c5 w1 d 水分离器内收集冷空气中水份的装 . o* ?9 S: G* n; q1 }/ ~同轴电缆,* X# F! U {# W1 ]! O6 s 一种通常用来联接天线与接收机或发6 k/ G% z8 }* ~' D7 q/ }4 O, r! p: C/ C! G4 {6 s 同心轴,$ h5 r5 o% m- V( u9 ?7 s @: A) ]" [) ^) A3 Y) C7 @1 j. n. p6 T$ N. Q2 T3 T) u) z7 C0 F3 P英汉对照民用航空词典B OEING4 F0 a* M4 i1 r. p8 `# n8 n, D TECHNICAL DICTIONARY 324 F: E" C2 F/ _; Y7 M$ y COMMAND BAR, A flight director pitch or roll comman; D/ T5 z0 a6 a& }. o% c; U indication.+ y7 V9 G& T$ M. n/ W d 7 W$ X9 T7 V5 K5 F1 x3 ` E; h* \6 IOMPANY ROUTE, A route flown by the airplane, i2 w- `5 L* Y- R0 {1 Y* F# M OMPASS LOCATOR, A low power, low or medium ' L. Q& O+ U. h+ `: [equency (L/MF) radio beacon usually installed in* H" G7 i( n5 d, L' ~3 T8 } onjunction with the outer or middle marker of an! y5 r) J% Y% i, f+ r tor (LOM), A compass; c2 w( Z* G3 J+ Z& y/ y4 `1 o locator installed in conjunction with the outer , r$ H/ p" O% o, U% \# |marker of an instrument landing system./ L5 ^, \, c+ E3 d( a3 R ss0 J: f' U6 |) h) b2 D7 k le 0 t9 p9 K9 `; e* B) Y% z6 VOMPENSATION, To offset, balance, or counteract. ; J* m1 S, W! ZOMPENSATOR, A dual capacitor for changing the fuel 6 ]/ w( h: E0 G3 K& t$ paging circuit capacitance due to changes in fuel 4 \0 A8 e/ I0 P8 {$ O! F7 O" Qensity.7 j0 D6 o y: C# E4 l( o$ } OMPOSITE MATERIALS, Non-metallic materials used ' T0 c0 [& g* O5 Gr airplane construction. Fiberglass, Nomex, Kevlar, ) S) l* p2 }8 g }$ {7 V! ^+ mraphite Epoxy are composite materials.+ C4 z, v5 O) U+ L5 y7 e 司航路,2 g1 c" _# n3 t9 g 在飞行管理计算机数据库内由航空公司飞行 * D0 J) c6 ~! R: U盘定位台, " j" Y c% }9 f: E' G; [与仪表着陆进近系统的远距或中距指点标配套安装的$ J; G2 A' Y: U7 Q& J 功率、低频、或中频无线电信标装置(低功率NDB台)。 ( o; c7 E/ E1 P/ j& H2 T3 m程序中用来导航。. C+ p% L' s& Z! D) |2 z8 } 1.远台, 7 @5 s0 x) y5 n与仪表着陆进近系统的远指点标配套安装的罗7 {' ~0 u: u2 W5 C7 N+ I; n 盘信标台(NDB)。 5 C' A$ m5 v7 M. B! g偿, / T$ m3 {! B' R( l$ T4 A1 u抵消、平衡、或中和。/ L2 Z' `+ R5 L; ] 偿器,0 T' L' F) B0 F. z 在燃油计量电路中,用来改变电路上的电容,以与燃* _: y# N& ~" d; Q7 w( P# d 密度改变所引起的电容改变相抗衡的双电容器。0 w2 m" G9 V% F4 R 合材料,) _' w9 J0 L9 u* d' [ 用于飞机制造的非金属材料。如纤维玻璃,Nomex,) p2 q f% C. T evlar及石墨环氧树脂等,都是复合材料。

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发表于 2008-12-24 21:39:01 |只看该作者
C/ ]$ ^6 X. l- M y4 A( e+ [ operator that is normally stored in the flight G, M1 C; J1 X9 omanagement computer's data base.. z/ V& F, [) @! j$ g* F8 q C d" x+ s& \. P3 Q' c! @fr - X( ?- W& `5 R: [4 b2 hc . f) U7 w+ j9 u% }' Y4 B5 xinstrument landing system (ILS). It can be used for. F7 U( C, {4 _1 b4 J navigation as authorized in the approach procedure.7 ?- X) }- K `/ @ 1. Outer Compass Loca $ Y/ N: e! _" d8 g$ j' K2. Middle Compass Locator (LMM), A compa $ u1 @; P! x# x/ g t6 dlocator installed in conjunction with the midd " e- a/ w+ S" A9 Zmarker of an instrument landing system. ?% w# K% k$ S5 v0 v C 2 p1 `. h" P/ ?% r3 qC2 y& h& H2 S: y$ j( f g" O, Z/ s* r# P, B6 D d ' t3 S' F$ L1 ?: @1 Y& f" aC e! r" ]4 k. T, s fo4 h' y0 q) J; X- t! H% [1 ]5 U& { g " z. }( M: V' s7 |, M# h指令杆, 0 D7 m, H- ]+ D c7 x* S; P飞行指引仪俯仰或坡度的指令显示。 6 z) L5 }, k/ @% @2 J* E E* h0 L6 ~3 a7 K2 V' p. u+ s通常储存- d7 w! Q0 m( M4 c: a 的航路。0 f& c( A, T- j3 [7 i( V7 L. F- b. S! }1 M# b4 |2 l8 r: a3 v, o, N, D; Q0 m2 U) l4 L+ H 经认可后在进近 " n5 L/ I+ E$ G' F4 ]2.中台, + s @; u/ M6 [1 d& _5 |与仪表着陆进近系统的中指点标配套安装的罗& q0 @5 p$ k- {+ U* d 盘定位台(NDB)。& ^& R+ C7 |. p2 R# ?. P$ |9 d. }3 e$ a! R, [. }7 P W% q- `6 i0 N! K6 y; H# n" l& @. a* @! Z! p7 s. v1 w1 n: F% S2 hK1 H- @* {6 h# d* n3 J9 t0 ^ 英汉对照民用航空词典B OEING % x0 {) `8 G+ _' W& {& rTECHNICAL DICTIONARY 335 `9 Y# G% U5 p8 B by& x/ O; p$ o5 F5 k2 | or increasing air* j. ]* N2 O2 z. F ressure and temperature before the air enters the : G! `/ r0 W( H! j2 d, Jombustion chamber, Low pressure compressor - front 6 l/ I6 h) Z% r5 @. V6 j& ?ection of compressor, High pressure compressor- rear8 f4 [4 G D5 d) X4 E/ E+ K( O OMPRESSOR STALL, An event that occurs when; t9 J" \3 c6 F2 E6 q ere is a complete stoppage of air or reversal of air flow. d9 i3 X5 t" A9 _/ M) B COMPRESSOR SURGE, SEE - COMPRESSOR" N1 @, g: F9 g% M% z3 z5 N1 { STALL COMPUTED AIRSPEED, Indicated airspeed% }9 p" f" m; X7 b3 _8 {2 y corrected for the static source error.$ S: [# n( n' C2 I 的机械轴来驱6 `' s, x+ B& _: J- B2 V ,用来增加吸进空气之压力和温度,以供燃烧室使用。$ u/ T% r8 j/ ?; }8 l) m 压压气机—压气机的前段,高压压气机—压气机的后 5 O, R& `) k! k# ` @* b" B9 e7 A' O2 A: A0 J) J气机失速, $ y# Z+ o5 ?: `2 Z7 T+ I当气流完全停止或通过压气机时气流方向逆反的一种5 W+ W8 l, ~2 s5 A( { c. Z 压气机喘振,, ?$ ?- q! I% z/ C- |& K 见Compressor Stall" U! c/ r8 x- Z+ ^ COMPRESSOR, A rotating part of an engine driven * S$ a- U S% Na mechanical shaft from the turbines f5 t/ v* |0 p; w1 O. ]+ j. c, q1 i4 ^ p% t2 m0 K4 D( s2 X6 \; l# B c4 `5 V- j2 m) h% A s3 k# A0 y8 S6 F, W section of compressor. " Y' q# S+ }& }) z" Z9 G( xC ! M# u& @5 }6 x/ {" Uth # `5 @3 @5 l9 ~6 ~0 dthrough the compressor./ A, ?7 G& a% f! `) }/ o 压气机,- T' G6 c4 U: H# R. F9 ?0 M8 M% N1 G 发动机内的一个旋转部件。由与涡轮相连 4 k- I; F. S$ A1 @, F# J8 \ I* s& g- E4 ~% u5 F$ q5 c' S; r4 j+ C# o( {# X5 { L2 E9 v* K6 E$ L F9 u+ P( T' b% b, [现象。+ C: V' v+ k9 `3 U- a, y% m/ B0 j/ U 计算空速, " p( g9 t n; H# J2 r7 r7 G修正了静态源误差后的指示空速。 / V3 b) O P( T# q9 [: b( Q英汉对照民用航空词典B OEING8 O- v5 ?& [- n' \" Q! {, Y 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 ) ~. M( ]* K. Z; d. _ Voperations, manipulates data, and makes decisions." o4 L0 W" \, o, X ditioning 4 b% ~3 D6 I1 H1 Nthe air and the ' H! l# C- _ rfrigerant or moisture vapor is changed into a liquid. / i4 {. \1 N* W8 p( Hine5 X0 k$ O) ^1 U3 q& Q" q$ q* j ONFIGURATION, The position of flight controls,2 _* R- F9 c2 C3 ? missing which " I4 _4 ~( V4 smay affect the aerodynamic performance of the / D2 D0 e) I: b7 G! O+ [9 Wairplane.! l) b$ t/ {( ^3 u8 \" u; Y 置。 2 n7 \; s) _# f- A: z Z+ V中能使热能散发到空气中,以及使冷冻剂或湿! l4 |% ^& f; `& I$ o& G 转变为液体的部件。+ P3 ^+ ]% Y) D1 s6 n 连接到飞机结构上。4 k6 {% Z$ t" ^9 F3 @, T8 h 态,8 ~$ c+ @1 ?( ?' @ 定飞行阶段中,飞行操纵面,起落架等的位置。* Y8 d1 a+ v0 q( @+ G ),# Q2 |5 q$ {4 m3 Q" o, S6 H- k% ^ 受到影响。 ) ^1 _* o# z& z L% q1 i1 X* I$ H' ~CONDENSER, The component in an air con, V, u. a% Y1 Y4 w6 @2 j H system where heat energy is given to4 u/ Z" f# C- ~0 H1 | re. H1 h- }; O( N* Q `5 B CONE BOLT, A bolt in the shape of a cone for eng 4 \7 G; h( | qattachment to the airplane structure.( F9 w3 N& ?+ b1 a% h! z C * r- t! ^. i/ d4 D( g' jlanding gear, etc., for a particular phase of flight, e.g.,3 l5 W4 }4 L: T' K6 a/ y Takeoff Configuration, Landing Configuration, etc. : ]3 u' h1 A1 ICONFIGURATION DEVIATION LIST (CDL), Appendix. f6 r( K5 r8 l! {( M; t9 r in the Airplane Flight Manual (AFM) allowing operation, M& j+ e& ]8 O) ~1 D of the airplane with certain airframe parts 6 s* N& Z4 r9 i8 y4 T计算机, # |2 _7 |4 G4 x. ^/ I) e2 H能作算数运算,数据操纵,和决策的装 K# K n8 i+ R/ B* Z; B/ l G冷凝器,5 Y7 y4 T: t7 M1 \8 w3 L2 O 空调系统 $ P9 o) k7 f! l5 ]) F' k0 a! Z9 {3 R1 K/ L4 ^ 锥形螺栓, . p. x; y; f9 t! w. n5 s外形是锥形的螺栓,用以将发动机 , y% M4 R) ?$ p* i+ T; H8 ~) J& g( b0 T5 a" B4 ~* {9 ^& i2 R 在某一特3 x0 w9 o, ~; o% o; Z 如起飞形态,着陆形态等。 * ], u4 l- J* \% h缺件单(CDL5 O& b4 u4 U* }" c( N/ `! s 飞机飞行手册的附录所开列的飞机上某些零件的清单。 6 H% r: u3 B& Y* {! ?在缺少这类零件时,可以飞行但气动性能可能% L/ I& P" |- D" F 英汉对照民用航空词典B OEING" P0 D0 r; t* k2 `: W1 c TECHNICAL DICTIONARY 35

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发表于 2008-12-24 21:39:49 |只看该作者
CONSTANT SPEED DRIVE, A hydro-mechanical! h1 B+ }+ r# ^. {- V component for changing variable engine gearbox speed3 g. s8 @3 F$ {/ b6 D: V( z; ~( s8 W ONTROL AXES, The three axes of the airplane which 2 I ~* a9 N3 ?; Kre perpendicular to each other and pass through the # Y+ R! F( p/ \) ~( F+ fenter of gravity of the airplane.; ?9 b; P& e$ z$ k, N r# S0 }( Q Pitch axis - Horizontal or lateral axis, passes through: Y* c$ {0 D7 g$ w the airplane from one side to the other -! e# }1 t# [9 ^7 E, t& j% _6 Z) ? nose up and nose down control is by 4 J; f! f+ c9 G# qelevators (and stabilizer for trim).. ~- k0 w% B6 J+ b) w+ F0 ?8 d2 u Roll axis - Longitudinal axis, passes through the ' x/ o: S" h6 [+ X v2 {airplane from front to rear - wing up and7 q. W: W0 o0 K/ D \ wing down control is by ailerons and ) x {- @, [6 B9 t% \) F' d# fflight spoilers., V. |. b# R/ T2 G) A Yaw axis - Vertical axis, passes through the9 h1 a; I$ b8 H3 V; I0 @ airplane from top to bottom - left and/ x6 U" U7 r0 O! Y8 I5 v* K right control is by rudder.$ V' F) f% p+ z* q$ @' G( t 置,/ k3 }/ m" h4 `) a0 L- m 制轴,6 F- j Z/ s. g' v( ^" u5 ] 通过飞机重心互相垂直的三个轴。5 h* F; a, N0 D, z- J: C% e 俯仰轴—又称水平轴或横轴。由飞机的一侧通向另 , u. h( l3 h8 Y" p* M. G侧。飞机绕此轴转动即造成机首的俯与仰- Y9 n0 ?) x$ o 俯仰控制是由升降舵来达成的,水平安定" d1 A# ^: Z x; w& E! Y6 q" L1 ^: | 则为配平之用。 % D7 @5 t7 z9 i' I# n横滚轴—又称纵轴。由飞机的前部通向后部。机翼 + e& J4 B( g- V3 V+ q下运动由副翼和飞行扰流板控制。1 p( Y! [- x! s( Q0 z; a 偏航轴—又称垂直轴。由机身上方通向下方。飞机 - g t3 u& {& u5 j# c4 y此轴转动即造成机首之左右运动,此一运 / M5 t$ w; O, \3 t! {3 Q- f由方向舵控制。 * U' z4 J9 }6 l+ \; _3 L zto constant speed to drive the electrical power. 3 j4 ?' N: ?) }6 |7 aC! M: G* ^4 j. C X3 E& y. |9 Y a ) I# C* m% ?% i! i2 mc) M8 K/ e& ^0 A. r1 q' v8 y 恒速驱动装6 I* F0 E. a* [+ J- S 将发动机齿轮箱的可变转速转变为恒速以驱动电源的 $ w& R+ l) K! N8 `6 x! c9 w6 A液压机械式部件。 : x# i, X3 y5 ?7 \$ \2 J0 f! l" G; k" n1 G+ {- K: I; n2 d' y9 t" K" ?, ]( P+ i! F. R1 ]+ y9 K: K) I6 j8 ]( y0 F8 X6 m# q* N6 H, e1 a/ d: ]( x9 }- [# ~9 a, \ r5 |: q# i- \5 t( S英汉对照民用航空词典B OEING' C0 |/ \' R# w0 k4 R9 }6 C TECHNICAL DICTIONARY 36 5 ]7 {6 A! ~3 ^7 ECONTROL COLUMN, A mechanical component used 2 k; L/ C' V0 v1 M! _rs4 I* u, r. g; t. u. m nd elevators. 7 i* ]9 @* ^8 g! MONTROL SURFACE, Moveable panels on wings and4 Z8 M- b& K$ q! l4 x' d il for movement of airplane on pitch, roll and yaw axes. & N2 o& Z# k3 c: Y( rONTROL TAB, SEE - BALANCE TAB3 K9 Z3 E4 Y4 ^1 f9 W) R) G ONTROL AREA, A controlled airspace extending 2 v- g5 o6 q0 X5 B/ {' w4 n: S ^pwards from a specified limit above the earth. + Y* U7 x* v( [7 z- c- H: \; \; k1 ZONTROL ZONE, A controlled airspace extending7 d: Q% u/ c) Y* Z* I8 Q pwards from the surface of the earth to a specified * D$ ^# y# l% D/ ]0 Q1 k. xpper limit.6 z8 v& [! L* J* N is 6 v' z4 f# X& \' _! R+ _* p: S+ A" [# qo IFR flights and to VFR flights in accordance * n7 n7 c' @( x0 G% R6 zwith the airspace classification.( F: B3 z% L3 l- @ P2 { 机械部1 r2 D9 H. }( {" X v+ x( a- v6 a* x+ _+ E$ W操纵面, + h& l9 M7 x: _! a% H) x机翼和机尾上的可动面板,用以操纵飞机俯仰,坡度,$ h( N3 u. p; |& e% R 和偏航运动。; }; |% i* o: }1 n 操纵片, 3 k, `2 y) a7 p' x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 spoile8 r; E1 N$ d! b7 M' t, y a$ q- C5 _9 w9 a7 I. d8 _9 O/ _1 j! w; @ C" r0 X& }% x! e% @9 b$ Z9 g ta/ V U- L$ H6 O( Z9 w3 A% R9 y C; r6 l7 a0 w3 ]- V: n C% }2 h: s' ^# S/ C, Y% A2 H u 0 ]7 p( x1 h8 f7 u3 cC 4 n8 @1 ^+ g( @; w; r& Xu n- J1 @& d+ d [: b6 a$ _% V! s5 Tu - y# Z$ c/ k c" C+ MCONTROLLED AIRSPACE, An airspace of defined ; }/ E- c* S1 L o( g& X- J1 F7 edimensions within which air traffic control service 9 n- T9 a' d' R: @3 T4 s3 Uprovided t6 v7 H: m0 {8 `9 S9 \" h" X5 h" b& x& e 驾驶杆, 9 m M4 ^, U' d8 p* a6 V2 D8 h飞行员用来操纵副翼、飞行扰流板和升降舵的 / M! b7 y7 i' N$ g+ b. q7 v7 N3 s/ N$ S$ T" h$ F' D1 B8 Y2 e/ N" n( L+ @ 管制区域, p" N( y6 r) W `3 C0 f高于地面的指定极限以上的受管制的空域。 ; K- ~4 r# e* n7 _6 l& W) M制范围, . f' M" J0 f4 V1 @由地面到指定的高度以内的受管制的空域。1 j# q: L/ A) l# B, ]) A( ]8 ] 一个范围明确的空域。在该空域内,仪表飞行规则飞行 ) `; n6 S! _* J" q$ |和目视飞行规则飞行有空中交通管制服务。 0 e* O1 k1 ^1 B* p$ L# i! G0 c( U! ^% m) ~8 @" X4 a受管制空域,7 P8 U; h# ?* w' @( Y2 F4 A( i7 x 英汉对照民用航空词典B OEING $ h7 i+ Q" I0 y1 }* T5 lTECHNICAL DICTIONARY 37 + P+ ^+ g! U) QCONVERSION, To change into another form. $ X- T, b2 g0 s% o, ?' L/ Z# CCOORDINATES, The intersection of lines of reference,: g1 o* |& B, F/ i& }# V4 m sually expressed in degrees/minutes/tenths of minutes 8 A7 I6 C K+ ?2 G& i* ~f latitude and longitude, used to determine position or 8 v/ |+ p1 Y# r% oCO2 y4 ~9 O- ? R* } destruction of th d) b4 z3 v) X! `4 ~* L5 bchemical conta ' c8 Y* {& `3 o6 XCOWL, A remo b: J4 S: o; W' Q' Y for access to th 8 v" ]! F5 @, B1 z) nFa / e4 N, p% J3 _- N5 aNose Cowl - Front section of the nacelle for air inlet: z: w% E& r C to the engine., ~) D/ N& C5 k$ Y: o Side Cowl - Cover around the sides of the engine.6 J8 }8 [( Y7 h' W Thrust Reverser Cowl - Cover around the core; {% l8 o$ {( Z: L section.: q7 R( O6 ~& \& r/ P* V p Translating Cowl -The moveable outer portion of the3 B& t) D9 {% f thrust reverser cowl which is 4 F9 O; Z- l! g3 s- woperated during reverse thrust.% H/ ^4 y7 C' W- d) C5 s 标, 6 r7 t; ?" T; {( `& _基准线的相交点。一般以经纬度的度/分/十分之一分 " Y3 s5 Z8 i. o8 X/ y读数来确定位置和方位。 4 Y$ y, i# r1 P" V/ G3 `腐蚀( S7 y% Q% s T7 P& ~ 动机外部可拆除的罩子。发动机上的构件必须要取下2 |) E) B: M' }1 I/ t 流罩后,才能够到。 ; Z/ Z. z$ _' J* p, M& i/ `" M+ _( b% G6 ~9 n I$ u6 h) } 机的短舱的前段。 3 e& Q" A% N' C, R侧整流罩一发动机两侧的罩子。( R5 f. g7 h4 |! v7 R& P! t' p 反推整流罩一发动机主体外的罩子。 ! R9 l. \& _2 E+ n7 w1 N% N- s移动整流罩一反推整流罩外可移动的部份,在反推工 ' E8 l9 @% `2 s8 g作时使用。0 f2 {& c q- l: l u 2 u! N' p: n8 w/ c3 s- W. so # u' h* `4 V8 g- p# B* @location. : ~8 ^( `/ M. N' q' E: `RROSION, A chemical action which causes gradual* o$ @$ M0 E; \9 S e surface of a metal by oxidation or / k* p6 r) O5 F8 W" i8 e5 fmination. $ s3 a: ?5 P0 q( V2 G! S5 d5 e, Lvable cover around the engine sections * {* l3 F5 d7 D# ^e components on the engine. * h5 I3 @' J3 @/ _- R: Mn Cowl - Cover around the fan section. & f- E9 }# w+ |/ c. f; K2 z转换,- S, j& T- x4 h 改换到另一个方式。 + B( u& O$ n$ w4 |& D/ U- c7 H5 @# N" K+ S6 x2 U! S9 L# I2 t( l* Q& q- L0 j& [6 ^" Z6 q$ U氧化或化学污染造成金属表面逐渐破坏的化学反应。 & {% M+ k6 b9 i: q发动机整流罩," L' p% C+ R6 d% A) s+ k6 b, p) t& p( e) t9 y$ y9 \5 Y' U7 [$ g- V8 q: F0 Y% V扇整流罩一风扇外围的罩子。 ) ]' ~$ V! _5 A" }) X1 a( {7 S前整流罩一引导空气进人发动 7 D, R( L! ~2 Z* d5 F5 V英汉对照民用航空词典B OEING j @+ B7 h) e- ?1 O6 K TECHNICAL DICTIONARY 38 ! l# l8 ]& J3 QCPU, SEE - CENTRAL PROCESSING UNIT! x3 y3 ?2 P2 }5 R CROSS TRACK, At 90 degrees from the desired track ) D, q S, ?( B% v$ }0 d! _f the airplane. For example, cross track distance is the2 H, L) E" h4 i. |% Y I istance from the desired track measured 90 degrees( Q2 d$ z0 I$ R, J( l om the desired track.. B' @& W1 I [8 [) j! ^* p ROSS-CHANNEL, Electrical wire(s) connected from 3 B, q# o6 A( Mne system to another like system, for example, FCC H/ O$ O" J6 b, _; S" to FCC "B".+ Y" [! N; k9 P" [8 |3 d n adjacent engine or one on the other side.8 n/ L$ U$ p |0 n9 o% j l crossfeed ( S& J1 p7 E4 D, L' p" a6 ganifold for fuel flow from one side of the airplane to the 3 L6 }: }# r( Rther side. r. e, M! [& M3 \* [) Wre 3 U7 r( o( M: J3 g0 G! b' y& KRUISE ALTITUDE, An altitude or flight level3 H" V4 a9 S" N0 _8 U. w$ d) x4 Z6 L& F) Y o 8 J' F1 E4 v( n# l2 W) t2 v' y8 jd: V, ]+ i# g) m# }1 ~/ t% ?5 C% g fr ! }) n7 F- d- n1 u1 | E; s" iC , ?" ^: x. e4 }0 n7 p: fo3 L+ F. h5 r+ J! Y- V "A 5 T) b& P7 {, B- ?" F2 s' JCROSSFEED, An interconnection between fuel $ [# z& @4 b. Xmanifolds for fuel flow from one side of the airplane to8 T: q" j1 P1 s a ' W- W/ K* F; k4 V; ICROSSFEED VALVE, A valve in the fue; ?9 T0 A" K0 u9 ` m( ]1 _2 k" D3 I3 a w6 h) T o 9 M7 Y3 G4 N. a6 UCRT, SEE - CATHODE RAY TUBE: v( s3 k/ e0 ` CRUISE, Phase of flight where altitude and speed a/ Y8 F9 v1 ~, r basically constant. 6 ?% G5 X, R+ \0 v' @8 LC ' x7 e+ U) o, k/ \* }2 @maintained during enroute level flight. , d) b$ V C) m/ O* `中央处理器 - [0 Y k$ ~0 S& ~+ ~1 @见Central Processing Unit.. j y4 S% b8 q' Z 交叉航迹(XTK), - [/ L/ K% T6 t% |与飞机预计航迹成90°角的航迹。例如,交叉航迹距离 $ f1 B' [6 ?$ v9 |* j5 [是用与预计航迹成90°角量取的到预计航迹的距离。4 u# ?- [5 f2 I! J y7 ~. i2 C 通道跨接,5 q9 q4 J* [, J7 I% u @7 w, L 电线由一个系统接到另一个类似系统。例如:由FCC ) c1 C& \6 l: T( \# p+ u& y“A”; F3 m% u% v" o! x- h1 t 接到FCC“B”. # L2 O; P' k+ t& a0 X0 o机身另一侧的发动机。 & E" _% U1 {' R/ x于使燃油从飞机的一侧* I" j7 X/ X* R4 I5 b 向另一侧。7 p2 k2 V2 I! z 见Cathode Ray Tube# L9 _3 q, M" h/ M 交输, : {5 p1 \5 i0 H. e5 w燃油支管之间的交连设备。可使燃油从飞机一侧流向邻3 w4 S; g* \0 ~8 R- X6 | 近的发动机或在. [- }9 s( c, D# S) n 交输活门, r! n; u0 D( B 燃油交输支管内的一个活门。用8 q2 @( S/ W; A, x5 D! ^3 _6 K6 Y; ?9 ~) W" ` 阴极射线管, # P5 q/ ^" B( y; M7 l) @. # ?; Y) s+ w! }( n( y+ u+ `3 p阶段。$ L# x' }% ~; f4 {+ U: T0 V 航高度,' m# Z/ k4 [; D; q" k J 飞行期间,飞机所保持的高度或飞行高 ) E+ w$ {* R$ o7 \1 Q. U0 f巡航, , [% a* T C; i0 P0 \飞机的高度和速度基本上没有什么变化的飞行3 w; k. u$ o! {0 V- r7 x; \; n* e* V+ |/ C8 K, n 在航线上水平/ b1 U) T( _ L/ Z/ Q% o& N& {& R 度层。 2 `! h$ G' C1 l! ? n% H. k4 e英汉对照民用航空词典B OEING' W; o) `7 F" l; d* @6 ]/ [& x TECHNICAL DICTIONARY 39" |* |& a- C& \$ b! c4 |! d6 Q3 V CSD, SEE - CONSTANT SPEED DRIVE , Q! g% J- i, N6 J5 yCURE, A chemical change which takes place in a resin4 c I% @; @4 ~ `( g and fiber based component causing it to solidify.$ k& L2 ^! N8 f) [ CYCLE, A complete series of events that take place/ p: } v) G, ~. P# S" r' } gularly normally in a continual sequence.2 X% ^: A4 |$ t7 o AMPER, A device for slowing down or limiting* f G% a3 T1 B5 k# }8 e DASHPOT A mechanical damper for slowing down/ I* N5 Z/ ~ a. @ \' @ ovement by restricting fluid flow. . [& {1 w: O H7 u* |2 ^3 w' sD , { i8 s) `$ Q6 `& {ATA BASE, Stored information which is used as the , ] O4 t( _0 J, g/ a: Dba ; w5 n, r/ W! a B4 R- tDATA BUS, A conductor over which digital data is . * `; ^ Q5 J ?& p$ N) Z; wtransmitted. O: p9 y+ h1 W. b0 T. X DECELERATION, To decrease in velocity.5 ~& |6 b# l8 s% ^) h# ? 装置, 2 w' b# \; z+ w0 t% j+ urive 6 f3 V* Y9 _$ y: H. pre # j2 \: L0 i6 l! s0 I* ?D' r1 }* l, v4 y D ! {2 r! S* o# g) }. D4 Kmovement. # r2 \' }7 Q4 w5 m: I1 Mm ( Y: Z. n! {% P3 G; u$ @ATA, Another name for information. ' a- n1 F; _3 ]: U5 b2 O' zD% {* r2 U1 ^" T sis for computation. + |9 e% i! }& _- p6 r. X# y恒速驱动 ; t x' _' B# g7 N+ X2 X7 x见Constant Speed D .0 ^% K8 n" Z, U* o9 g5 r 期,$ n8 M( M* h6 R3 Q8 K 不断重复发生的事件的一个完整系列。 $ S# t! U# ]" U尼器,$ ?/ ]8 _- {$ G* M* K 慢的一种机构。- i) [% x( `2 q H1 l1 R: \: X) s 用限制液体流动的方法以减慢物体运动的机械式阻 % s4 ^, d" O' E0 }* k, R8 I2 P5 ?3 Y' p2 W0 X: Q- Q. L5 e; X0 z, H1 J3 V4 V+ S/ D1 K 料的另一名称。 + F4 v9 l2 |2 ~* D$ r% z6 \" M据库,! D2 g4 g* r( W 数据总线, % [: L3 {5 S# E一条或一对导线,用来传输数字信息的通道。 9 Y6 k4 t0 f1 w& v, f减速,2 [, y( v+ h* C% z, H 速度随时间的递减量。 ! t" B* E9 V9 t' l固化, c' @, a1 Y! T2 o! Z& F树脂和纤维部件内化学反应使之成为固体的变化过程。1 w& B( i/ m9 u. b3 m- h7 v7 I6 g, Y( p$ z6 j p' \3 f' U$ w) l7 D0 L 用来使运动减 / s( V( I; l' @ Z* U2 X冲器,: H3 n. h! `7 m" Q5 A 器。. J4 |3 k) B1 b" C 据,/ x4 M s5 n# W& I0 t* s' c( ], _& Q! ?# s: D2 V9 u/ i) K- V储存起来以便在计算时使用的资料。 % u' ?3 O7 |& Z2 z: e: \英汉对照民用航空词典B OEING2 [. q' I( Q9 L( g2 X- c TECHNICAL DICTIONARY 40 ; c0 @- w+ U/ NDECIBEL (db), A unit of gain derived by computing the ! [; ~1 ~' E5 V1 F- _! Ctio of input power to output power. / u. L- a8 @; Z1 RECISION ALTITUDE/HEIGHT (DA/H), A specified4 h% V3 m3 V5 [% _+ D* x# b, c ltitude or height (A/H) in the precision approach at' G! K( s9 O0 w7 q# u' U. ^ hich a missed approach must be initiated if the! Z7 O5 Q$ _3 [3 O; \8 J T ECISION HEIGHT (DH) 1, With respect to the5 Z8 R. ^+ | F& [% n; m! r proach or0 f" T* b0 T1 q execute a missed approach. 5 o3 Z' g! e. I0 Kproach to trigger the decision of either 2 d6 n/ s. s8 b, |, M6 Y9 T4 Ynding or go-around. $ w# w$ ]: B& x) \1 i: RECOMPRESSION, The loss of internal aircraft air ' G* }0 U) g, N6 h7 {, F) Q3 j6 gressure.* W J% `2 u1 a% J8 d* n5 `& |2 l E-ENERGIZE, To turn off or cause to not operate.7 s1 i" F7 b' C/ } h rom the tanks" I0 d1 s( c% z) N- s! ^% I: b using airplane fuel pumps or external suction. : X. K' N) I. {; W' c算的一个增量单位。分贝; H$ W8 O3 k$ j# V1 n2 B 常表示两个声音信号或电力信号在功率或强度方面的4 w0 `( A8 G4 d. }% D 对差别的单位,相当于两个水平的比率的常用对数的十 ; O1 {2 ?& S `* N3 }0 d7 l断高度/高(DA/H),8 k- M& x" b4 Y+ c7 J+ `' ^ 在继续进近必需的目视参考没有建立的情况下开始复 - D# ]9 T8 A& p8 w的精密进近中的一个指定高度或高(A/H)。 % r _, N+ _' g: i* {, Q- G3 U断高(DH)1, . S+ R \2 Y1 o {- t: k0 B/ A操纵而论,指在使用仪表着陆系统或精密着陆雷# {9 H9 m' C+ E 生继续着陆还是复飞决定的高。 2 h {. A' M; l2 x3 y" x飞机失去内部空气压力。 " Z. L+ o$ o1 G0 \2 f# L* @( [开, / A) ?$ P% I; O0 C3 N关断或使不工作。 6 S8 i( Z# M2 d$ @0 u: d5 n; W机的油泵或外部的吸油装置将燃油从燃油箱排: q3 G- \7 G& M' e8 W 出的方法。 8 [. c" `% p% U/ r* ora $ }, m9 ^; B1 X3 p0 e/ \( KD ) O7 U4 L$ d8 y- I6 W$ I" oa 6 b& B) j# r) \* K; W! K; d3 f) Dw 4 w- y" ?5 q0 }3 Nrequired visual reference to continue the approach has3 j7 {9 P/ K5 v& u4 p not been established. ; _% x2 s6 \8 x+ g% F( nD ) C! l5 a+ K% p0 g0 Doperation of aircraft, means the height at which a0 C/ d$ m$ i* K/ Y" d j) P decision must be made, during an ILS or PAR& |2 J4 |/ M" z/ {! C8 Y9 F; c instrument approach, to either continue the ap, O9 d4 u: E2 j W% e to1 M) G# |& P# _! h: I DECISION HEIGHT (DH) 2, An altitude used during a . _. i: w M$ w8 k' |precision ap 2 s1 c+ P& e9 C& w8 |la9 ?& ]& u/ j' X7 `( ?# J0 E# [ D: R* w5 m! R$ A* L: h p; K* N* Q# x; \7 S8 F, E2 Y D4 e( C% K7 s$ r' o) M DEFUEL, A method for removing fuel f' `- s" l% k0 \% B, A 分贝, 0 Y; ?* t6 r6 p4 w, @4 P2 e `' D以输人与输出功率的比率来推 W3 @0 I& o, q I% o, I% Z- _* |" n# }+ W) u7 w! y( U% T! b( i& C: v* _9 d4 h3 l4 o; m' v7 W2 T" w) j$ Q5 o! E; y8 r4 z: w! i# {6 D- C9 `0 C: B* G 就飞机6 m+ g O( }7 q5 W# Z 达引导进近时,必须要作出的是继续进近,还是中断进场 4 H1 @+ N* D( b复飞决定时的高。 # g; ^/ E% g* t( R/ n+ m% [决断高(DH)2, # x, k% ?0 {7 s( U, u精密进近时产 ~7 d$ g ?) I 失压,0 E! Z$ _) G8 j6 n# J/ ?! ^9 p/ ^7 ~6 \) \8 `6 R2 f7 G e0 O 排油,/ _2 m6 Y6 S: w$ p8 K 用飞 2 h+ q4 J1 Y) I& d# H英汉对照民用航空词典B OEING# } M2 {4 {6 b8 | TECHNICAL DICTIONARY 41# H( ]8 E" b" T- I( P DEFUELING VALVE, A valve in the fuel system for 3 P7 U7 p# z& W4 }: M& Defueling the tanks and for transferring fuel between the( ^$ R& Q5 U: c' U8 i E-ICING, Removing ice after it has formed on aircraft. 8 \7 {' Y2 u8 kChange or difference. " e8 i" @% q% x2 BEPARTURE CONTROL, A function of an approach0 B, ^7 W/ S; Q: h3 j7 I ontrol facility providing air traffic control service for $ T8 B' G9 H; c U: Veparting IFR and, under certain conditions, VFR / b$ m$ v0 N' `8 p; \+ _/ gEMODULATION, The process of retrieving information. I, V# n. H# a" e! ? carrier voltage.# c F+ m: ]# Z ation. 0 W8 G: }& z! P4 y1 T1 L: l0 }5 blic : q$ S" B) F1 `7 }" {( g- l/ mcreasing hydraulic reservoir air pressure to 1 d1 g+ T1 {6 o! R. `1 hmbient pressure. q m$ r9 L& z; r! } 箱排油和在燃油箱之间 3 {8 G# r% T$ J5 b: B/ F送燃油。 & z' J z. i0 }4 K" ]: j" _冰,( s4 [) v4 O$ [# C; g 除去已凝结在飞机上的冰。 ) D. n; S! F1 n4 A2 T删去或取消。 2 B. V$ K, w/ E& F: b4 J量,9 W) M+ c7 x3 _$ z) Y' ~2 @ 变化或差异。 ! V/ |8 s+ X2 r! X% N: V9 {! Q7 o场控制,1 {- Y5 r% |- A" c/ u 给用仪表飞行规则离场,和在某种情况下用目视飞行 5 G9 ^% E6 u8 P则离场的飞机提供空中交通管制服务的进近管制设施 & x" t5 R$ H3 H% h7 y# |) p3 d3 f8 I, c7 ~调, / D3 b8 Z4 D+ q' S电压中获得调制电压的处理过程。; G; |# U: g* ?4 e+ w8 c 环境 $ p* M" p$ \- U( w: E+ F3 G力相同的活门。, }4 s% ^' |9 B" W d9 d5 b' \- R. J" }$ x tanks.8 I' K' h) m! ^$ t D % l0 u5 U! \+ R% N/ B& Z9 k- zDELETE, To remove or cancel.6 [' p/ C) {# W; ?8 n' L DELTA, 8 g9 N. z- V9 T" g4 S7 c$ M' O8 JD4 ]. W U% n6 l: k5 M! d c4 t) N4 M8 L5 | B3 b, G d; W( b$ X/ Z3 y# M/ r aircraft. $ @4 V7 x5 k+ c; I( F7 TD! s F2 I% t( H (modulation) voltage from a modulated $ V) Z& ]) `' `+ hDEMODULATOR, A device or circuit which performs6 a5 t- o+ ?/ z' a8 f- ]! p the process of demodul% {/ T# P1 n1 r* W( R2 k" Q5 _ DEPRESSURIZATION VALVE, A valve in the hydrau / x( a+ C* y2 F# qsystem for de, f4 z( ^: i& y% x a 4 r [# `9 D! e5 Y; c. z排油活门," X3 p7 z- D! R! a 燃油系统中的活门。用以为燃油 3 `1 T; S+ `. u# U# l$ y: _7 o7 C5 h* w0 W1 c1 C# r& R6 s2 @$ U5 |5 h: ~. z 删除, . Z: v. @9 t) _9 P+ ?% r# q( E, w! `8 D8 l( W* w, ]! n" W- p w: S6 X" s5 |3 o Q8 }# q# D 的一种功能 S0 C, N9 V% z0 x; ?0 D: V3 p/ [6 O/ }6 t! x从载波 ! t4 k' m2 U3 G# k! p& x8 O3 h解调器, ! |7 x, \' w& r5 v# Q4 w& w+ n完成解调过程的装置或电路。 . e( u2 }5 h6 F1 P5 h; E减压阀,) @4 P- {: Y5 V/ p& J( y# a 在液压系统中,将液压油箱空气压力减至与周围 f1 Z" r. x/ k4 T4 d! O2 s L. q* V! E 英汉对照民用航空词典B OEING v( W, D: @2 Q/ dTECHNICAL DICTIONARY 42 - t5 T% u* O& E4 [8 @: ?* hDESCENT, Phase of flight where altitude is decreasing. . J$ y, e) _! ^; qETAILED FLIGHT PLANNING, The calculation of fuel% d( y3 ]- r! Z- g3 c; Z nd required for a trip by considering each phase of% d! a/ x7 K* ?/ ^. t0 a& W+ c1 v+ ?: z: ? ight (climb, cruise, descent, reserves). 2 V* r8 Z6 ]- K1 Dal or4 C: R; x' A( s/ \1 Z8 K. X; e ETENT SOLENOID, An electrical solenoid used for 6 ?3 s2 p2 J, K! X' P3 Q0 x* At." z; E9 w; E+ n }* o8 V8 r specified course or ; q3 m* `+ O; V& s0 u3 ]rocedure. 5 @ p" @0 X3 j1 {# v8 Se. 7 z# y x1 Q+ _" P5 q! A/ d飞行计划, # v; _9 T- U6 |1 ?5 a将航班中的每个阶段(如爬升,巡航,下降,备降)都 o V, [5 w. E4 j 人考虑,来计算该航班所需要的燃油量。+ S+ P2 E& A! n# j. K 用来感应情况之正常与否的电气装置。* ^! b8 X g& a+ ]3 s8 Q" ^ 定电磁线圈, ! Y3 O1 y7 ^4 ~. X) K! |出接通的电磁线圈。 + m% f6 O. o* A" T& A3 a) J$ z差, % b* W/ u( k: t$ o与指定的航道或程序之差。. |! x/ X8 h' d8 D. T/ i m+ _2 l5 x$ X 用气压或液压操作的活门机构中的柔性部件。 7 C- `7 ]3 q) S/ kD' E$ Y- ~5 F# ^ z9 r' } O( \) F a" O; y; q: q7 m0 U. A0 F fl ( r8 B5 \9 W0 F4 hDETECTOR, An electrical device for sensing norm, c g$ f5 m5 i4 Y3 Q3 f abnormal conditions. 6 z: H$ X6 P! qD# E# f0 b. f( o) V0 L1 m controlling the engagement of the actuator outpu! B9 C5 l7 z6 h/ Z DEVIATION, To change from a6 F0 T9 o4 i. n5 S$ z! i p! Y& [$ D. x" h2 \0 p* [ q) W DIAPHRAGM, A flexible part for operating a valve- N: J' [1 M( u# T/ j( y& J y mechanism by pressur H7 \) {) \: N5 c5 P+ x/ a下降, + O& C: [, b; }' @) T" F飞机高度不断降低的飞行阶段。 4 n# x# }2 p/ t详细; D3 {( y( ~8 q! h. q1 c/ x$ F: T' I6 I; ^5 }$ z6 }. t 探测器, " {0 U$ I; S6 x" E! M# n* b; \& h& K/ R8 ]用于控制作动器输 l2 Q$ c/ |3 W6 F6 g. |4 h3 N) w! I: U3 y6 {8 L隔膜,3 z" I; V% S7 O, s( y, `2 x ? 英汉对照民用航空词典B OEING ; E0 w$ x( s. O" C S" UTECHNICAL DICTIONARY 43 : G" f7 R; P7 w) l1 e3 }DIELECTRIC, A material which does not conduct- y: n; _) n) {* T/ Q! V& h electricity and used between the plates of a capacitor . J3 K% Q* @- r. {" m1 m2 Y% g(condenser). ) D I8 K0 I3 N) |nother pressure in the same system, measured in 8 V3 x7 F4 V4 Uounds per square inch differential (psid). % U9 L5 R- V; R- Q- `4 SIFFUSER, A part of an engine between the. E9 S4 i9 w4 C5 h+ P: d ompressor and combustion chamber for reducing the! G' i4 b, U- }! a air pressure." t) d! d( a+ l1 r igh p8 F6 K' y/ X4 K pulses. , H4 D5 j, l; z7 tignal that is a close approximation of the original $ E% y( x! r- I$ K6 Jignal. - V+ E" c$ f8 kIHEDRAL, The angle between the wing reference# y' E4 p9 O" p% S7 K; ?5 b lane and water line. 7 t L ]3 [+ ~' E( Z6 q; B的压力,以每平方英寸 ) V3 u( w, K6 H2 Q& r5 r, F少磅压差计算(psid)。 Q6 |3 d/ Q0 ~& A散器, ' a I# c- K; T. W) g发动机内压气机和燃烧室间的一个部件,用来降低空6 q' i* m! Y( x! F 增高空气压力。 / g0 s: m4 H4 A5 T换,8 B9 Y+ z+ h! c& k+ f3 t# X, ] 的连续可# i! u/ \! z2 f0 `. l0 J& A$ x (模拟)信号的处理过程。 $ e. o: R O+ u& ` } [, F反角, : w- R0 B" x. p5 ?7 T$ D' \2 h机翼基准面与水线之间的夹角。! K# A! @6 K+ P9 t DIFFERENTIAL PRESSURE, Pressure relative to . |, t$ U% `2 G8 Y0 ^: S: }a " J) _! _, B' w1 v4 q2 Pp& ^4 V9 i1 }. R8 s* Z" ~ D8 N$ ?0 X9 c1 j c3 e, x, ~+ t6 R4 G2 i" s1 {" ^0 ?% r airflow speed and increasing the3 c; a" i6 J+ K' `" k* ]$ C DIGITAL, Digital refers to a signal whose amplitude 5 _5 C! X- x8 }) |+ iremains constant for a finite period of time. Digital9 y- Q9 q7 z" d signals are commonly represented as a series of h) t. B* R* q6 ^ and low 9 F3 a7 k8 T5 {5 ZDIGITAL-TO-ANALOG, The process of converting a& U# X9 A' V& v- s$ w0 z digital signal (binary) to a continuously variable (analog) 7 s5 w$ F0 M& @, y; X8 hs 3 {5 ?8 Y' _$ F9 m* U/ u2 {7 [s9 C! L7 H$ ~" T# N' P) Q9 V5 y D ) u* a5 A. H' r' t$ q5 \/ n P/ rp$ r9 V! V( Z" l9 ^" P% o 电介质, : l; _& V: n; s. ]一种用于电容器板之间的不导电的材料。. b1 H5 `* R) O, I/ F% z 压差,+ ^; i: c5 D6 { n 相对于同一系统内另一个压力 ( u9 l' l& f! I, H" F; [, l7 u5 n+ c% D) B& O" q3 O6 w& V) A7 | 气流速并8 j! ^ T; X5 X" ] 数字式," A- `: n, B$ m* T* L$ T: H9 V 指一种信号。该信号在一定的时间内,振幅保持不变。6 n, Z& _, x) j$ |% L8 k 通常由一系列的高低脉冲表示。" p% D7 f: L. Q' X 数一模转$ B" d" V: W: C* O# g! L ` 将数字信号(二进制)转换成与原信号相似6 p9 E) J$ h+ `" E& w2 s4 H1 x: X4 q ?# E3 h: o/ o, q" V3 h9 X* z2 d英汉对照民用航空词典B OEING' J; U% I* J) I0 C7 `* y TECHNICAL DICTIONARY 44# ?5 s9 i: P) u! g2 F DILUTER DEMAND REGULATOR, A component in the/ I( r- {+ i" L' \ crew oxygen system which mixes air and oxygen and 8 P/ w1 r; n9 {8 ]+ T+ {/ Supplies constant oxygen pressure even if there are; t3 r- }3 p6 H' r# o4 w hanges in ambient cockpit pressure. 2 j/ ?$ _$ B! G) t, t, U4 WIM, A word value of light. For light control devices - dim1 N9 H) A0 @) q' [8 a; p the opposite of bright.3 j- z* H5 v# M1 e+ a; m IODE, A device which allows electronic current to flow - C h) v/ l5 Q; Y5 L, F! bonly one direction ( {% Y, O; d1 T o: Huid in a reservoir. 9 I1 R4 O6 J- PDIRECT, Straight line flight between two navigational 7 _ W% i+ L' w& a/ n. j0 Paids, fixes, points or any combination thereof. When 0 B- M R( p: N; a4 g6 Q0 wused by pilots in describing off-airway routes, points5 i2 i: ^! H; g defining direct route segments become compulsory8 \0 y) v) e1 U, c% B2 n( B reporting points unless the aircraft is under radar , ^) E, B4 ^6 v( ^- P! u1 }control.4 `- m( O0 z0 O# C* k 节器, . H9 e) l; \ J将空气和氧气混合,7 m: b" _ O! n 使驾驶舱环境压力改变,它也能提供恒定的氧气压力。+ d9 R2 Y+ D0 I9 q8 }; V) v7 u$ g+ j8 @& _) ^ v% P 一个形容光线亮度的词。对于灯光控制装置,暗的反2 P( V; r, I7 V. J% V) P 词是亮。% e7 a7 l& M7 M" I3 H 极管,, S; S0 r7 t, l( t 只允许电流向一个方向流动的电子装置。6 g( C6 ]4 F) y9 A! `* e: w 器内液体的量。 " s# S5 H8 ?1 ^$ A直飞, % M2 z" I: T7 h' ~6 h( S0 e两个导航台,定位点,导航点,或任何的组合之间的直: {% F& u- {) |( k6 U: t5 w$ _ 线飞行。在被飞行员用于描述偏置航路时,除了在雷达控 * R) C" m6 e' u5 [# T& G; n制的情况下,确定直线航段的导航点成为必报点。5 I' H$ Q O& n8 z2 d s5 [, t! _- |2 u% S M c9 ^: |# w5 [- [: s- w ~( U D 5 }0 U4 n8 y* M# M. |is7 A+ w6 z6 Y6 E D; o" b) f$ a% d9 P; b: A+ l in 0 F5 _' K. s2 B8 |DIPSTICK, A calibrated rod or stick for measuring a$ q$ N+ O7 H% ~9 _2 o3 n( {& D, ?" O quantity of fl ) V. M9 k/ Q! i: p稀释氧调# @4 t4 Q: J. f9 J% O 驾驶舱氧气系统中的一个部件,它* a) G$ Q! X$ x: a8 ~2 Z" {7 T# s2 u/ u E& [$ {) u5 T' R: N4 z1 G1 L! u! c) d$ `/ I2 H! P6 ~1 U: J0 ?+ [+ D4 z, r# e# P2 I0 b量尺, : t( ]2 i+ \! @校准过的棒或尺,用于测定蓄液 : |/ O! j7 e- n8 I' j/ s7 v英汉对照民用航空词典B OEING " D+ e( S w/ G/ q% W" w GTECHNICAL DICTIONARY 45

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