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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" `2 {! z, l7 C 民用航空词典 & i2 L/ J7 C- E波音商用飞机集团# q) P/ R& p- _+ F' j X4 h BOEING COMMERCIAL AIRPLANE GROUP 4 l6 d3 v; P0 j7 [& @英汉对照民用航空词典B OEING7 i# e& c: L, [. e; j TECHNICAL DICTIONARY 1' {2 O: _; N/ D/ E& |* V3 e3 m4 c A " t, @1 L# q0 K4 SABEAM (ABM), Beside: An aircraft is abeam a station & D0 f, K' ~$ [when that station is 90° to the right or left of the track of; ]# B$ @ p) A* X5 C9 K the aircraft. & r7 O- k/ Z" r; S7 CABSOLUTE ALTITUDE, The actual distance the aircraft % ]$ F' T* @8 E9 G/ t% ]( Qis above the ground. % z) R& A3 j( J# i6 s M5 E& jABSOLUTE PRESSURE, Pressure of a liquid or gas U, J x" O* `* r0 h/ w$ {; ?measured relative to a vacuum., d6 \5 l# @- r" m5 L ACARS, SEE - AIRCRAFT (OR ARINC) REPORTING B! o; D$ k' [8 l" |ADDRESSING AND COMMUNICATION SYSTEM0 a* h V( w9 f1 f: w; j/ u7 ` ACCELERATION, The rate of change in velocity with ( C% T6 M9 C9 L+ K( P6 n/ Xrespect to time.' I# F5 l$ ?2 d8 e9 V4 z5 c2 v ACCESSORY GEARBOX, A part of the engine,6 H5 M5 U9 y5 Z+ T; q$ g mechanically driven by a compressor or an angle 1 o0 a; L1 ?7 z$ i+ Cgearbox, for driving components necessary for engine 0 y. r% W' \, y6 d正切, " u/ z* G3 y: x" i! Z7 Nand airplane operations. $ b7 X: ^) M# ~# C; s当电台在飞机左侧或右侧方与航迹成90 度时,飞机正 4 b ^ x$ I- n$ h* o4 t2 J切电台。 + e& c) l+ o. ^绝对高度, Z8 z% C3 k) n, ]0 a* p3 v1 z; G" n, W0 P 飞机离地面的实际距离。. c3 c4 a. J# _ 绝对压力,' K! d0 I9 H. j1 M0 r3 c% a- w. A1 k 相对于真空(无压力)测得的液体或气体的压力。 2 J0 m. J8 y4 p; A: _飞机通信寻址和报告系统, : T$ v4 _4 W l' E1 v见Aircraft(or ARINC)Reporting Addressing and0 }/ c. s. V$ R- e Communication System. * J9 I: W- F$ v* W" h加速度,3 {' ?- g& K* _; Q 随时间变化的速度改变率。 " {( `/ o& L1 ^+ h5 d* ]4 R5 G附件齿轮箱, 9 K% G) S7 s( T$ |6 _: v发动机的一部份,由压气机或伞齿轮箱带动,用来驱动" x5 i* M$ P4 \; ~ 一些使发动机和飞机工作的部件 # F0 U* C) z7 w! R0 a, V" v% b英汉对照民用航空词典B OEING9 l6 f* Z4 V; i4 l5 P, u8 e TECHNICAL DICTIONARY 2. l: D- x+ s' h# Y ACCUMULATOR (NO. 1), A container with hydraulic ) A+ b- D: i1 }' O: Hts when normal hydraulic supply is not % y$ m; `. z( E2 l0 qvailable.; K0 A) i5 z- U) t* o W CCUMULATOR (NO. 2), In a computer, a special 3 A) w5 @! e, R, p' q4 o/ storage register associated with the arithmetic logic unit, " F* r0 u* S! w8 T& ^' \olding the results of a computation or data' b/ K4 z+ u) C# Z; Z% s3 c! h ACTUATOR, A mechanical device operated electrically,/ E3 T4 \% }/ k+ ~/ W- L' h! x hydraulically, pneumatically or mechanically for `, J5 a0 ~8 q) |1 i9 Z3 Ptransmitting motion between components.) ~( m' f3 o8 N ADC, SEE - AIR DATA COMPUTER* a% V6 V( t" M9 s ADF, SEE - AUTOMATIC DIRECTION FINDER 5 p0 f/ @# V& B9 }! H+ P& ^ADI, Attitude Direction Indicator, An electronic display of) \+ S: }5 E: _3 j% U- m airplane attitude information in pitch and roll. 5 L2 c% k8 V l, [蓄压器(NO.1), 1 U* }& V) m* q) @* q" Y4 F2 m! w含有靠干燥空气或氮气增压的液压油的容器。当没有正& ]" ?. L. n5 o7 [6 I/ D6 G 常的液压源可用时,该容器可用以驱动部件。( M% K1 |# X$ p+ b$ t9 J/ z5 ^7 x 存储器(NO.2),+ y9 l% b0 f& O8 q' m 计算机中,一种与算术逻辑组件有关系的特别存储寄存 8 H7 g$ o- |3 |9 Y' T器,用来存放运算结果或数据传输。 - E4 b; e8 u2 z. c, j飞机状态监控系统, & c3 y+ |% f# h1 ?" ]4 M+ s见Aircraft Condition Monitoring System- f" P/ u7 C) `" f fluid pressurized by dry air or nitrogen for operation of! W- F9 m/ `# t* V9 U' Y$ ~: q7 C componen 2 V6 Y8 C) s1 b! i2 |7 ua 0 s& f3 ^6 C# d. u- G7 ZA8 I& x% S8 t( ]8 ]: V s & h$ f1 Y1 N0 ]2 ~5 g5 fused for h0 F+ j/ n% _+ v$ T. [; d transfer.+ h e; f1 ?0 ] B7 o. p ACMS, SEE - AIRCRAFT CONDITION MONITORING; y' Q% v2 N7 s- p9 k SYSTEM . 1 H! P! V6 ?* q8 Q& G! ~3 R作动筒, & R9 N' i; v0 t由电,液压,气源或机械驱动的机械装置,用于传送部 7 ^5 Q2 H+ D# u3 h: ?; i; r2 I件之间的运动。8 }8 A* N; N( p5 v- T3 } 大气数据计算机, ) u: d# a ]# }) b+ N见Air Data Computer. , X% C7 [# Y3 P$ t& X5 l自动定向仪, # y% _$ B: S5 ]$ Y$ o; t见Automatic Direction Finder. 2 O1 z6 F# D4 _5 b% ~姿态指引仪,0 g. n" i& _" m1 i 用来显示飞机的俯仰姿态和坡度的电子显示。 / f9 P: N# ~5 q. I: E" A' e: W英汉对照民用航空词典B OEING ) M, a: @1 g3 z- [0 \' M3 oTECHNICAL DICTIONARY 3 + N6 i$ N: f- |8 gAERONAUTICAL RADIO INCORPORATED, ARINC is 6 F. x/ R: T+ r" \8 p! I% C# j,/ r/ K2 G% ]; G0 u F! P2 n0 I) [ nufacturers, and foreign flag airlines. ARINC/ a" x7 V5 T1 @* O" T/ R, W2 d evelops and publishes standards for electronic- J$ \ q* A- T0 D, ~( l, @ quipment and systems.1 D/ `# B' T" K5 I GILITY TUNING, The capability of the DME to8 e3 Z. M, w( S; g: J q5 q lternately tune between two different DME stations in$ J6 [4 n; @5 x q rder to get two distance readings from one T1 z1 M0 O4 q" s* c terrogator. % i- F; H6 y: f6 R- y) }ge2 u+ k/ S! s1 r ILERON FORCE LIMITER, An electro-mechanical# L/ g) ^1 E- R5 F6 |0 ^$ u( J IR CLEANER, A component in the pneumatic system9 ^2 g) G' @$ C0 e, S upply to the air E( w9 g! I2 s/ v/ F" c) b onditioning system. 5 g: z/ x) E: q. }订并出版' V& }& V. F% w g% } 子设备和系统的规范。3 a2 E+ e2 j# ]0 q+ y7 R 快速调谐, . y' n4 x1 ^4 A2 x1 G机载DME通过交替调谐两部地面DME电台以测得来自. n. z; C5 e4 H4 b 同一台询问机的两个距离数据的能力。6 _* J9 _( i) w: H0 g0 O 翼操纵力限制器,' D2 D$ x- G* _1 j8 u6 T9 O 装置。在自动驾驶工作期间,用来限制驾驶盘. ?/ \2 A/ C9 d: L. A 气清洁器, ) m: }! p) Y9 ?: H& I部件。用于去除供空调系统使用的发1 ?/ e& W7 P4 h0 l% N+ n: y a corporation whose principal stockholders are United, n' P, S5 ^1 Q9 t$ N States scheduled airlines, air transport companies 9 ~5 J9 B4 c' `. c8 h+ caircraft ma: M5 p, C* u0 ~. A: Y0 U. o S d / y% H# ^2 }5 F0 Ye + h. ~0 M0 k+ C: ~5 iA+ x5 Y8 j. K% Q, S/ B3 {& F% N% k a / M g+ T1 e5 G( uo" n: x5 n7 a' U3 _# n3 ^ in ' E5 I- G2 E; W1 f2 |& vAILERON, A hinged moveable part on the trailing ed/ X1 r9 l% k# N) w2 B0 D' p; \ of each wing for airplane roll (wing up and wing down) $ C1 T$ ^; V( T$ z8 @) wcontrol.0 N5 F+ P, L8 Y- E9 l* D A v# e- Q2 S% g! n3 ~1 s2 [ device for limiting the control wheel movement by the* c+ q% k3 Y6 Z: [8 b5 e/ g9 n5 R autopilot during autopilot operation./ x3 d6 j: u: P# y- U! u- b A + t1 p! R8 `7 n/ {+ ]$ r0 Q, B6 F( Ofor removing dirt from the engine air s ) i/ v; _% B, \$ h" Pc 7 q) ~# j1 M# t' d航空无线电公司, 3 L+ m, M4 U8 o) E: o- `2 f主要股东为美国定期的航空公司、航空运输公司、飞机 2 A% ~4 G% r6 o2 j) D7 l, x制造厂和外国领队航空公司的组织。其目的是制 % y |, O- i" D p; S" k! f3 k9 h 副翼, # d$ O4 ^' q, V1 m, G( T铰连在每个机翼后缘的可动部件,用于控制飞机的滚转1 W9 v+ R7 Z' G! w6 D3 x (机翼向上和向下)。 5 x4 C; B4 I/ a: j) `6 N+ t1 d4 K) D( q- n) j$ _4 I 一种机电" Q3 N& J4 \" l" i/ u* s 的动作量。 . T( P4 k2 y# w/ B Y7 k6 J# C0 S' o0 G5 d# }, s. c 气源系统里的一个 3 F& c/ R4 @% _动机引气中的灰尘。 * y# U3 y: ^- o" d5 Q- N4 a+ i% s英汉对照民用航空词典B OEING ( A" \: L8 }; C8 LTECHNICAL DICTIONARY 4 R8 k" \+ v9 y: {7 v! \5 g; f AIRPORT ELEVATION/FIELD ELEVATION, The; {3 N8 r6 |% {2 _ highest point of an airport's usable runways measured 1 f0 R6 e4 ?# i& b2 }. E5 e, W1 tin feet from mean sea level. In a few countries, the 0 I) }; d; q3 @" B/ Lairport elevation is determined at the airport reference " y; g& @. C5 D* _! L# J2 K' x0 ppoint. , d+ E( S+ [1 |+ ]* i' [+ F/ V4 S* o. cAIR ROUTE TRAFFIC CONTROL CENTER (ARTCC), : z' \; E( G/ a/ _ervice+ s2 p+ w- G9 W& i2 r% t ase of ! G# ^( l' d1 N0 b1 _2 }9 nus flow of air traffic. " H# ~3 j2 `$ G# y, WIR CYCLE MACHINE, A compressor and turbine on a % Y4 _3 e8 @9 ~ Iommon shaft for cooling the air in an air conditioning* I2 f$ |+ e! w4 t2 M$ C ystem. The air is cooled by expansion from high to low9 T" ]! A1 H0 W* a4 }/ h ressure across the turbine. The compressor is driven 1 ~# R8 ~* o: Py the turbine. : Z1 Y5 i/ M% L6 ]中航路交通管制中心(ARTCC),: }- m9 D3 N( f4 s8 c) X 域范围内使用仪表飞行规则飞行的飞机提 * F' Y8 ]8 ]6 T% q5 o管制(ATC), 7 v/ a9 i4 w, C1 e3 b涡轮冷却器, 3 ], a, ]' \ b: m! a是装在同一的压气机和涡轮,用于冷却空调系 ) k \ b; W I$ J: b/ H统中的空气。气经压气机压缩后,由热交换器移去热量,, E$ D& [5 |8 S4 S. T 然后经过涡轮令涡轮带动压气机。通过涡轮之空气,温 ) J4 Q' Z( H3 k& u1 q度下降。7 x$ z% j, H3 {* J A facility established to provide air traffic control s9 S+ b0 E! U" j6 h. [ to aircraft operating on IFR flight plans within controlled4 b4 d3 e% q' V& Q4 m% V airspace and principally during the enroute ph & W5 T4 h7 D9 F6 ]5 h: H$ cflight.2 U' R% T5 y$ N; B7 h6 O6 T3 } AIR TRAFFIC CONTROL (ATC), A service operated by' c9 Q( B( _2 C: {0 U0 ]& G' {5 A6 Z appropriate authority to promote the safe, orderly and 4 U6 s l8 t* }- Y- @# h1 X, Eexpeditio" a2 ]. u6 w5 D7 F/ M2 E' c A , ^+ `& ~2 d. N+ Dc* f. ]* t7 q8 a) _9 a% _ s ; L/ }/ Z4 B' i" U4 v; zp9 o" w1 c8 X3 z6 g* T b6 u' T6 b- y* f8 u1 V6 ]/ o3 j 机场标高, 1 ~7 a y+ G8 g1 y: ?5 E% X7 z指海平面与机场可用跑道最高点之间的距离,单位是英 / B7 k9 \9 [8 t3 H. Y尺。有几个国家的机场标高是由机场基准点而决定的。 9 r( @0 ^1 m# [4 m, I; n& D3 \2 U8 u! t& m; V" p; T% L* w给在控制空 6 k' u7 Z' o" O: d3 w( A' Z供空中交通管制服务的站台。! s' N. H; t( w8 k4 ] 空中交通 0 d6 c+ v2 m; t9 a5 g由有关当局管理,旨在促进安全,秩序,和效率的空中! @7 P8 d) N% J 交通服务。 ( f& e4 c9 u3 E" Q0 ?2 w根转轴上. Q& j# _8 H9 l7 {. o$ R& L( q y1 x+ ]) j4 ^! s. d2 I; r$ g- s1 w2 K( I% R& k4 H英汉对照民用航空词典B OEING3 p1 h8 K9 W3 y! _: v6 P6 J5 k( I0 } 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 produc9 _+ Z% y# d9 n data information, such as altitude and airspeed, based/ ~7 c+ k. ] x' q on pressure and temperature measurements. 8 v8 H# L; A- wes air6 Y, @/ q4 |# b4 ?5 H IR TRAFFIC CONTROL, A system comprised of. l' Y! k" W- P& E9 b% C, i round and airborne components used to identify, track) q4 V# [& f: W" i F OUND SENSOR, An electrical device operated + n3 f7 j; r6 v+ d1 ~( Ty the landing gear, which transmits on ground/in air: |0 F( j9 c8 r$ v+ Y6 C+ S6 b formation for system operation in flight or on the* m, b7 S( t6 G9 y0 b; q8 V8 D0 A round. ) p( {3 N+ e% X& zIRBORNE VIBRATION MONITOR, The AVM takes& u9 A3 F( w# \, v6 ^% s: b/ H& @ e signal from the engine mounted accelerometer and u9 H! l; y4 `- P2 ?9 b/ Ualculates the vibration on that engine. 9 }- [) ~. S0 g( O3 `8 c. tcorridor equipped with radio navigation e4 D7 C9 P" }. Z9 M aids.$ S9 E. R" X- @$ { AIRCRAFT (or ARINC) COMMUNICATIONS & _; l4 x0 f6 m! [; N8 PADDRESSING AND REPORTING SYSTEM, An2 I( l% X2 X+ a! ?9 H5 f addressable digital data link system which permits the; O# V+ W7 z/ y* V& a7 x' k exchange of data and messages between an aircraft . c% _$ Z- K" l' x. _and a ground-based operations center over a radio 8 t# @6 L" D& o$ P' V! m. @ }" cnetwork. + ?9 ]: R0 d. ^' ~3 |& x. b8 dAIRCRAFT CONDITION MONITORING SYSTEM, A2 X0 s' P9 `: S- Y3 a system of sensors and recorders to monitor various8 O+ h" t6 i5 ]) C4 A5 I airplane systems' performance and status. 6 A+ i) K# A& V$ W* i/ G机,8 c/ X4 z9 H# ~. g+ a9 U; A5 q 中交通管制,7 E0 r9 h- X" j; V1 v. F s3 v 一个由地面设备和机载设备组成的系统。用来对飞机进1 H6 N& c! P' L* T. X: p; Y+ K 地传感器, % q0 X8 P; D3 X" X; F一个由起落架操作的电气装置。用于给空中或地面的飞 : P5 z: E; B# d# G系统运作传输地面/空中信息。(有些系统只能在地面 3 m0 y1 M6 I( G4 |: R5 {' o用) 9 W8 B& b) F0 X4 G7 v载振动监测器(AVM),; C+ N1 h3 R8 F1 h5 A AVM从装在发动机上的加速器取得信号后计算出该发; D- E0 e8 ^7 y4 H4 p) b 机上的振动。 ?3 H3 C8 w9 ~ s3 J5 \9 K 式建立的控制区域,内有无线电导航设备。* Q3 b" j% }. o+ [5 x 飞机通讯寻址和报告系统,+ P" J, C6 g1 `- V+ t2 |0 O 有种可寻址的数据通讯系统。利用该系统可使飞机与地 * L$ J+ h, K! D7 |0 E0 a) k面操作中心通过无线电网络进行数据和信息的交换。6 f+ [( P0 Z8 G5 M 飞机状态监控系统, ) i; L% a! e7 p% X# _2 q: a一个利用传感器和记录仪对各种飞机系统的性能以及1 Y0 y* X4 b4 B 状态进行监控的系统。% b" U7 r/ Q- R5 W# D7 S A 4 `& P; F& d2 y) Kg - D8 q3 V3 R' |- B) Hand locate aircraft. : s* |! }4 i' Y3 A0 `+ K pAIR/GR; E7 o) i" n F/ \2 ` b" v/ R+ A) y' q# p5 Z1 \( s in , I# G# d1 x6 W/ \( r& a% R) u8 `g ( \ D _: E2 |5 @5 g* dA# ^, g7 w: `/ H- u th , ]5 n8 [, Q; G8 @% u* |c0 X( c- i) b* e+ x9 d AIR WAY, A control area or portion thereof established( V2 q9 N/ b$ L; r: r9 H in the form of a 7 j0 H) @2 \, e& V: C" F大气数据计算 ! @" q5 a9 z" I根据量取压力和温度而产生大气数据资料(高度、空速; T) u7 [( H K8 { 等)的计算机。 3 ?* Q% K& ], S- U6 @/ L* d8 A% W, y: p: G& x7 k行识别,跟踪和定位。) |3 C, S6 P2 e, V; t4 t f& c8 H& m5 j% H, }8 Y) e, {; b* M$ K; T n% @% {! K- B使* E. {* _3 `, e' v' k2 C {" n* w' `0 \. W: l6 n+ n( o$ s+ i& n! n 航线, / D- e5 y* @$ Y4 L以走廊形 % d' H+ i0 O) W3 Y) O# L4 a英汉对照民用航空词典B OEING ' k6 _/ s% y' o1 a4 B v/ g# u- T6 PTECHNICAL DICTIONARY 6 1 u0 ? m: i6 c1 ^AIRFOIL, A surface designed to obtain a useful reaction,% r' e8 a. B5 |" H' x such as lift, from the air through which it moves. Wings, 2 u" z6 r: n+ q+ E! G: Bstabilizers and control surfaces are airfoils.& ~1 V6 Q$ `! q! q6 {$ h3 \9 a, R AIRSPEED (IDS, TDS), The speed of the airplane1 `5 M- b& Q$ Q: @3 y# Q) W rough the air.7 @6 J9 ~# o) ~/ q: i0 Z7 M, t1 c$ n D INDEX, An adjustable pointer on the + o6 m+ k& g- H8 `6 sirspeed indicator. # z: h$ V3 X l! t0 o( Qand legal ability" u2 A! }8 b3 t3 q- u4 }0 D; C fly.# B7 i( u6 s0 `0 S4 }& M- F m, for example, the procedure for finding the/ E' k' l Z* X# m$ S) c quare root of a number.4 p# i7 I# ^( I y 2 q! ?7 @6 E2 E* |1 A0 \5 {re, wind,4 _, g4 ?3 A! P2 O1 l1 J# g7 w and aircraft flap setting. # R* O4 U2 @/ B是翼面。 & V) y" o6 x0 H3 V/ d6 ?. M+ K w速, ; P A( U% c7 f' }7 U飞机在空气中运动的速度。 1 k9 {+ u- s& U: B9 C4 }/ u0 E" u9 l' \: g/ J 在空速表上可以调整的指针。% L3 ^. j# @7 N2 }/ R 机械飞行能力、和合法性的飞机状态。2 K4 i- A, B1 p3 S0 V 一步一步的解题方法。例如,计算一个数的平方根的步+ Q, x i* D- m) F2 t/ b; n1 M# z* M, W/ N3 P4 E8 F6 c. J. m' D* f, [) R 资料的法定文件。 ! y$ }- Y2 y6 K4 q) Y翼位置成函数关系。9 X I' Q- b4 {6 j7 P th( o' m. K1 M% i9 W# H4 |6 _" ~' { AIRSPEE4 f* `. H3 S B) Q8 D8 ?" a a - O/ ~7 y1 J' H- I: V2 c8 U* s5 jAIRWORTHINESS, The condition of the aircraft with & h0 Y# {4 M" W# a9 s# g7 Frespect to its aerodynamic, mechanical, ' a% Z; H$ X/ x8 Q$ vto 5 A, R( H6 N- O, p% U' UALGORITHM, A step-by-step procedure for solving a * e0 G* f- m1 I! I0 V( \5 gproble- M. t7 U K) A0 m s0 A) X. _, W- b AIRPLANE FLIGHT MANUAL (AFM), The legal& G: H; O, y1 Y- I9 D document containing performance and operating limits, 5 k& s! A% ]/ _& z0 d7 ooperating procedures, and takeoff and landing . U% {% S' U2 M' O6 operformance.% Z* F5 q. l: {; V" h AIRPORT ANALYSIS, A comprehensive set of takeoff0 d1 f8 J3 {7 j* o5 T9 ]' ? d weight limitations for a given airport runway, generall * H2 ^2 h. V" C6 F; z( J; c# G; X8 Xpresented as a function of airport temperatu R# F$ Z5 s( Q- ^( ^ 翼面, : q# B) d, Q1 j+ X" ~! D* Z用以从气流中获得反作用力(如升力)的表面。机翼, + X" \" X* }8 u6 L安定面和操纵面都# @: r: {( O! r3 ?9 _8 L* L# s) {8 H3 ^+ Z: g- L+ a% B L* c! O空速指标" C5 B7 r) a1 p% m% `% `3 Z+ z9 |+ d; E 适航性,& g4 p9 H! y" N" A 有关气动能力、! @. D/ C2 [; B* x 演算法,/ Q2 f& d$ N. Y5 T% _) j; A3 Q% V! H. P, |7 w( K8 N4 ~) { 飞机飞行手册(AFM), 4 Y! ?9 [2 i: Y包合性能极限,操作极限,操作程序,起飞和着陆性 $ W6 c! O( S. x2 C4 p' L# K: f) ^" x t 机场分析, - J R( H: _) n J; s一套针对给定的机场跑道的详细重量限制资料。通常与 0 T0 U6 T, z* L- k: L; @& }& i% w3 y机场温度、风、和飞机襟3 j. m4 r' D& a 英汉对照民用航空词典B OEING1 _' p3 }: ]) l, f- C TECHNICAL DICTIONARY 7 7 I% P% y1 J. i: Z- nAIRSPEED BUGS, Adjustable pointers on the airspeed+ ]( K# J% V. F- t* f9 q! w indicator. & B/ t5 Q! N2 X n# W4 P" lALLOY, A mixture of a basic metal and small amounts & C# Z+ x- Z" d8 w6 wf other metals to change the properties of the basic , ~7 D7 h" M9 |etal.( @# n# f0 x) c b5 q Minimum airplane speed.$ B% x( ~" j: z2 ] e of ! Y% u( h/ }# X" v% Y9 k7 N% a$ gitting airplane angle relative to 5 D; j$ w4 L8 y$ y! A) H9 rirstream for the stall warning system. 7 o$ }! q2 q- \ G1 `another. 1 H7 h' c' b: v1 u8 ~LTERNATE , An additional airport selected during 5 C7 f: q' J1 L+ X, c) ~5 O$ z9 k6 `; @& R3 M/ y Z$ o合金,9 g0 e4 o' b9 k9 | 在金属中加人少量其他金属,而改变其性质的一种金属 1 H+ q; u+ N3 |! p! w3 [1 x合物。 . e- p$ n h7 o X9 {8 z飞机的最小速度。1 ]6 P( x3 Y+ ~, m 速警告系统传输飞机对 ) l1 f/ Z( i5 T. T3 f流的相对角度。 + ]( h0 V; r. l9 A+ y5 s( U由一个状况改换到另一个。, Q+ t4 A5 O. m8 V 降场,) t' ~9 j/ p* D+ ?" P' w; j; z" E3 e, ^ 划时,除了目标机场之外,所选的另一个机 * ^% B' ^) ~' Q' `% `o1 f) w% Y5 o$ s4 O m7 j$ H. k3 {# P, D+ |# I# q ALPHA SPEED,8 C: |' w* R- V7 a ALPHA VANE, A small moveable airfoil on the sid , ^0 N8 o3 x! c/ xthe fuselage transm) ^" ?$ q8 x# Y2 f a 5 m, ^+ Y6 \: V+ TALTERNATE, To change from one condition to2 c! `4 F, b1 w3 H5 e( O: t A/ E# ~% Y, s3 x7 \ flight planning, usually near the destination airport, to be ]( e( k. B" Y7 t used when it is desirable to divert from the original % C; {* i* F/ x- `destination airport. ; |5 T( M, I4 U; F" @& F7 m! P2 K空速游标: P) p1 x) G7 {6 e 空速表上的可调指标。 & t1 g, Y$ _" K/ K# H! s0 T* c; [4 u3 d4 }3 ] 迎角速度,; c, O" n# I" u/ e1 L2 x7 x; w 迎角叶片, * ?8 l; A! b$ m# V+ p& E3 a位于机身侧的可动小翼面。为失 2 P& ], ?+ G7 n$ l1 _6 _( q7 u' L- q$ I 交替, % _, ~. e7 j+ ^: d9 g" j. d6 o8 W- V9 ]% @) w, K5 I制订飞行计 4 F7 S( D+ @# g8 h4 m& C- ?# O/ g7 N场。通常在目标机场附近,以备不去目标机场时,改降之 7 x) P Z8 D5 O/ Y+ e4 p- S用。; q8 X/ V# l4 n& a) f; h 英汉对照民用航空词典B OEING' P* k5 f2 t3 G4 x7 s TECHNICAL DICTIONARY 8/ q/ C6 e5 C3 ~* @ ALTERNATE AERODROME, An aerodrome to which$ G4 a& Z9 |! \6 R3 C an aircraft may proceed when it becomes either " z! T; ]; @& e7 apossible or inadvisable to proceed to or land at the9 r Q& w; r0 H: _ I0 \; s1 q erodrome of intended landing. ~; x$ o* U# b1 C) u' k. j8 G TER SETTING, The adjustment of the altimeter! l/ R& x; w( B/ [ account for local variations in atmospheric pressure. 9 j* }6 p! L1 h7 }) D" DLTITUDE ACQUIRE, A digital flight control system% ]; y7 s. B3 U1 J, t ode to transition from climb (or descend) to level flight.8 ] ?3 X k0 ^9 ?# } LTITUDE ALERT, A flight deck alert occuring when the $ z. O( _8 C. r* a) n" t8 Eirplane approaches or departs a selected altitude. n. K0 x# R' k* `+ U8 l4 _! b v' } LTITUDE CAPABILITY, The maximum altitude at ' i; s1 z0 X" E$ K2 R* E* ^4 Lhich the airplane can be flown at for a given thrust,# v- O* K7 x$ V ^$ @$ \ peed and atmosphere condition. 0 a, x: c2 J, x5 cLTITUDE HOLD (ALT HOLD), A mode of the autopilot 4 E* j5 U/ V* D! ~r flight director to maintain a selected altitude. 8 W! e% z) ^% \! kirplane's altitude during VNAV operation.0 {% r6 W5 g1 U2 \. u 机场着陆时,可作着陆使用的 h/ m7 m y) X 场。 5 Q1 A" e; F! f$ x6 o4 F2 N1 {9 \/ R 根据当地大气压力变化而对高度表所做的调整。. l! b+ ?' o9 B( g! ? 一种数字式飞行操纵系统,从爬升(或下降)改平的模/ l: _' p" [ p( G) D- V% a4 Z& u# r% P e4 Q9 m' [- {' T0 u, H6 {* u$ ?+ n度警告, & e* ?$ F/ }8 d2 c* ^( D当飞机接近或偏离选定高度时,所出现的驾驶舱警告。 / ^8 i- X* a6 s! H4 m& g& J高度能力, F5 ?3 p1 y" v# a4 D在给定的推力,速度和大气状况下,飞机能飞达的最大! e0 d8 p2 K( J4 T7 k! d. T1 H 高度。, G" [5 A. V; h) j$ D N 高度保持(ALT HOLD),0 K! n: w' Q- H2 T+ s. v% w 自动驾驶仪或飞行指引仪保持在选定高度的一种方式。 7 q& l) W k8 [& N$ p2 M1 @' [! ]7 C) e: v0 t" m员对飞行高度的控制。/ ?$ w6 k' |8 x2 {, c6 A7 Q4 H im * V, g7 D1 W# B+ Wa1 T7 L' W# y( v1 s% q ALTIME , c8 n+ X4 t. d* A& V- z1 Sto4 m5 C+ l( T0 n A , i9 }' z) ~% t' ~, O$ C- q1 ~) J- I2 r! um7 u3 Y C' k4 m- Q( w/ l/ Q A' L4 f7 Z# U& M. K a: Q/ v) [# i7 r' ?; e ^. o A& `: g5 v R. c8 w& L+ l w5 } _9 H- N# n. E" o( B+ ~ s& E( `0 e a3 R+ l* Z A6 D% w8 E/ m& J+ m! l o/ P6 w8 v; p8 P% a ALTITUDE INTERVENTION, Pilot control of the & j l2 {2 r7 Ua 1 E; N- G' u3 ^# EAMBIENT, The surrounding atmosphere.9 r4 _8 ]' k3 h* v0 e2 A: Z0 H 备用机场,) G+ u; N! f0 u# d8 c6 |2 v 当不可能或不适宜在预选9 V3 U5 l$ z4 m: v0 C' `3 E6 P. l! s. g高度表设定 1 n8 P. X, M+ K4 m$ A$ j9 n2 N高度截获, 8 W2 P3 |0 F \* u$ Q, ~5 h& p- t p% B7 Z) ]6 M. z- W7 M5 l3 j2 L7 L高度干预 : }6 O6 j6 A0 J- q0 k在垂直导航工作过程中,飞行 , E! A* K( ]$ M. k9 d. S周围环境(地面气层),! L% h: o0 ^9 }' R2 k7 M6 @ 物体周围的环境(特别指大气)。- j2 u4 r7 _+ ~% A9 Q 英汉对照民用航空词典B OEING / `* h# t; ~4 }9 s. L' I* STECHNICAL DICTIONARY 9 9 Z. J- d' v* p. U* HAMBIENT PRESSURE, Pressure of air surrounding an & i! e& B' M' V+ i0 ~object, measured in pounds per square inch (psi) .( x9 v# D) c, `3 H' m; l9 C$ } MBIENT TEMPERATURE, Temperature of air : c0 y. c) N2 Y' |mpere. # z2 S: E! O2 _8 e9 Iurrent waveform. 9 N0 @7 z0 u2 ~5 z( h) X1 ]g an* O$ B5 x' {: u, o: p! d nalog signal to a digital signal., Q1 Q$ V! ]( E! J+ L8 A6 ^ ore inputs7 ^+ k* f3 ^4 ~* M0 r/ ?3 [ f binary digital information and one output. The output & m. Z+ E% J3 E) h. W; o1 only when all of the inputs are 1. The output is 0 2 C, e! \: [ a, t+ B( j6 ohen any one or more inputs are 0.0 p! @, t$ B' E2 a, B1 a" S6 i6 f3 ` 面气压), # ] O! F7 t# @- v/ @9 G# o境温度,$ M7 U$ o, D' u) w: { 气温度,用摄氏度(°C)或华氏(°F)来; L5 p/ T% b; U) Z# z Y" n1 {5 h$ O) V8 T2 m9 ^电压或电流波形的幅度。5 Z$ G( b X$ S0 l' A 性变化的信号来工作,或产生连续性变化的信号6 q' ~1 i& ?- @: j6 k 统。6 u2 H% e! C+ T* J: ~ 将模拟式信号,转换成数值式。' U2 d# O( r. K! A, C* J! v 一种有两个或两个以上的二进位数字信息输人,一个输% S. G8 [. C/ X 的装置或电路。当所有输人为1,输出为1。当任何一个4 ~0 w7 `& ^) K* [/ L e3 M# m. t- B 一个以上的输人为0时,输出为0。% R+ a, H! }5 r$ c, N0 | A . ]2 @! a& V2 |+ C8 P- }) E# ~. Dsurrounding an object, measured in degrees Celsius ) N& B8 c2 N* Q1 ~(°C)or degrees Fahrenheit (°F).0 x- {! t3 y9 l2 z AMPERE, A unit of electrical current. One volt across ( g2 S9 |3 Y% V# Zone ohm of resistance causes current flow of one# s5 c$ q+ Y7 s# S a 4 K9 \/ S3 _' n: [( x/ BAMPLITUDE, The size or magnitude of a voltage or0 M9 e1 J# \2 L4 i; @ c7 N* U3 d- P7 S& B/ h9 @7 j1 i ANALOG, Quantities or representations that are 8 c8 U% D$ n- |" ]& bvariable over a continuous range.2 Q6 @9 G6 r- U* g8 N* M ANALOG-TO-DIGITAL, The process of convertin, A$ {" ?$ s9 R a, w( b8 Q& s" d+ U C4 N9 p AND GATE, A device or circuit with two or m1 @. m! f; T: A- P4 `( A( b o& Y5 |" B5 |; r* N1 K is3 X# }$ V. o6 B w * x8 W9 l1 [$ l4 }! {, o/ c; p环境压力(地5 C9 D' H% z9 [& u& U: Q 物体周围的空气压力,用每平方英寸多少磅(psi)来' u. s* z$ ~1 ~% D8 _6 _ 度量。4 Z: F7 j4 {1 \+ A' x4 R! N* c6 a- a 物体周围的空# @( {" @" t7 d( N 度量。 4 H# Y, i2 S0 d+ q% {) l! d安培,/ k1 {+ q5 e1 |/ i2 J" N 电流的单位。3 a" M% N: N3 N4 ] Y 1伏电压在1欧姆的电阻上所产生的电流为" q( C8 H6 H6 z Z8 ^8 K 1安培2 l( T* d* c! \( W2 Z 振幅,( C8 {0 d! T; _& b$ W 模拟式,' c' _( T$ z3 p; z* q5 z. o 用连续 9 P' y( D6 P% V6 ^+ G" M# a8 `% |- j! v) J4 J 从模拟式到数字式, % ^# z0 y; ~ }$ I与门,2 W( T0 G% y" _* p1 W1 K5 H6 u9 G" v# t/ u7 L: z" v8 D7 A" L7 ?, r( k# Q英汉对照民用航空词典B OEING0 {9 A, i/ G# Y9 y TECHNICAL DICTIONARY 10 : p) I$ c0 w8 OANEROID, A sealed flexible device containing air at low ; e }$ J- [! G) e2 K6 B" Ypressure, which expands or contracts during change of , |& o( `/ P8 b$ mressure outside the device.2 H& {3 M2 l6 c% f* `# B ically ! ^& j% B* M4 K+ _3 K, c5 Nr changing the direction ( @4 i# y" z4 Qf drive. u% s! t* o4 s0 j of the wing chord in* `: j4 s& x. _$ _ lation to the free stream airflow as it moves forward % a* K$ n0 Y7 d, Q& @9 F4 yrough the air. q* i' a0 ~+ k' Y al axis of the & H. e0 ~, I4 R& H' g/ y6 |5 Laircraft.* U2 I, |# u" m. {+ _ Z 胀或收缩。 ; s- C6 h- P3 F! e0 ]箱。是改变驱动方向的机械装置。 {/ n! p1 i4 i+ c( B机翼翼弦在空气中向前运动时与自由气流之间的夹角。! N1 d" B, \8 G/ t3 q0 X, Z- ?! q0 v Q, ~6 F! E; u0 jp 3 ?7 E) ~3 _* K6 d# ~ANGLE GEARBOX, A part of an engine, mechan : i3 G' L* j4 A$ w/ s4 Z( ydriven by the compressor, which drives the accessory , K$ O- P5 O# T3 Q) E- Ngearbox. A mechanical device fo; b% c* p1 B- @9 Q3 \; q. b1 ^- w& i o 5 Y g" r( u' T/ I0 \6 j( UANGLE OF ATTACK, The angle $ s. z: Q4 V2 w. tre; ^ f- ~- a4 B3 n T th $ m- q7 I% ~3 e2 G: ]( l5 }% u" H- CANGLE OF INCIDENCE, The acute angle which the3 l( C! q- h+ W0 T wing chord makes with the longitudin 2 I5 \7 {1 o7 p8 K膜盒, p3 K8 X6 o& \- r7 V# U$ O内含低压空气的密封弹性装置。当它周围的压力变化, m: M2 Y' [4 v: @9 \% T 时,会膨, p1 J! x" a" k0 c8 b 伞齿轮箱,8 W1 f, O4 ~! ~ 发动机的一部分。被压气机以机械方式驱动,然后驱动 . j# q! Q+ R. b& }* I, [附件齿轮 % C! a& K3 M$ \4 n迎角, ( A- p/ Q. Z" z5 X4 O安装角, . u1 D2 | y. ?+ X飞机的纵轴与机翼弦线所形成的锐角 " f: _* Q$ E+ n0 a$ r, m- i# b英汉对照民用航空词典B OEING / u* A+ U8 o0 L) m4 Q+ z" QTECHNICAL DICTIONARY 11. i, R* Z* R4 y2 I3 v \ ANNUNCIATIONS, Audio or visual indications used to 2 P# I+ ]/ ~9 O1 Ccall attention to an event that has taken place. " B# X9 Q7 Q. M. d% c. DANNUNCIATOR, A visual device consisting of a number & U% _/ t5 s2 h7 A- [& O* Oly. 7 q6 t! H: K# {$ a; l. y* oANODE, The element toward which the principal stream 1 g. L" n# B. o5 }( J+ B2 Wof electrons flows.+ r% D2 p: p5 F) Q4 O ANOMALY, Not normal. * a- n% }7 v' H( {3 t8 r+ xANTENNA, A device which, used in conjunction with a8 b, y6 G0 a2 H+ ^ transmitter or receiver, is used for radiating or receiving , W( i3 c5 m' c' ]3 b1 ^0 Cradio waves.$ ~: x8 A6 O2 @" R$ ` NTI-ICING, A method of preventing ice formation on * G F) g0 {9 ~5 Ye wing leading edges and engine nacelles.- H$ s5 B- I! E o( v* e4 C NTI-SKID, A system for providing maximum braking& X4 ^% L1 o. c! E: s. K ithout skidding for any runway condition. Anti-skid+ Z: t! F" V6 ?' j6 ?( ?& H( x4 w6 f# ] omponents are part of the brake system. / [/ j: ]) r4 s告,) j9 ?: ? D8 c* B7 I. @) @( S 当发生事件时,以声音或目视指示形成的提示信号。0 q( j' p( b; _" d# K 与之有关的电路的现有情况或已存在的 , p' q$ D; u; L8 W0 {) t1 Y$ ]7 F% O9 A ]8 d正极,5 a, t6 s# W, [$ ^8 ^6 E& Q. c3 A 主电子流向的极位。8 W# { }! h. \& X 异常,# l/ J% p8 `2 b, u% f) O( N 不正常。( Z' }$ Z) |4 R 天线,1 f" U# X$ _0 Q! P d 一种与发射机或接收机共同工作来发射或接收无线电9 h4 A/ F: ]1 x9 v! W" L8 ] M 波的装置。 ; X: z( z+ z& P冰, 7 S, o+ V( s' P, W" R1 c7 `$ S防滑系统,, l# S! _( j! G' h; s5 R3 @ 一种在任何跑道状况下,都能提供最大的刹车能力而不2 L$ v) L2 l9 T' w1 T9 O 使轮胎打滑的系统。防滑部件是刹车系统的一部分。1 z+ E2 R# ]5 x. U* N2 Q6 C+ S0 d of lights. Each light indicates the condition which exists 2 k7 I) q5 _" y% A- n/ yor has existed in an associated circuit and is labeled9 c" o9 b$ C6 H7 j$ ~ according . z* w- G# u' \. x$ \8 w) E9 _5 @A$ P5 v! N- `: X0 d th ' Y9 ?4 r) ~% `9 kA N& _4 M. m# |2 m" l! n, K% A. P5 M w " V0 n. \( R: a& X4 c% ?c! q$ ~5 V7 q6 c; z4 J+ _' U' p) V- @: P j 信号牌, 8 j2 t: v+ P7 D由一系列指示灯组成的目视装置。每个指示灯都有相应( H, K+ {# p% [8 w9 J5 P 的标记,用来显示. g; l3 ]; c, H9 i; n9 I. R' X) `+ n9 V( V) u! U( h3 K- r2 U/ ~防止机翼前沿和发动机短舱结冰的一种方法。3 e; x* ~7 {6 @9 P1 y$ U 英汉对照民用航空词典B OEING / O% y" J5 @6 I0 K; t' ~1 |0 J ]TECHNICAL DICTIONARY 12) A) Y. l5 d7 G0 g- @ APPENDIX, A supplement to the Airplane Flight Manual " R' E* o5 c* |tained in the basic manual. A - p: i8 T& p1 s, V3 L* A& oollection of supplementary material at the end of a + A F4 `9 b% pook.7 L7 d Z) W7 d- N) K/ ^# | of the , `# u" ]" Z' U3 }rsion link on the landing gear.; [* N( E6 u- x; y APPROACH MODE, An autopilot/flight director mode , T5 F; A& `2 u9 _6 {which is a combination of localizer for roll control and6 a. {$ v# M6 U- f8 T glide slope for pitch control. This mode is used when full . Z0 _! W$ R% f8 w7 z! Minstrument landing system is available. 4 {* }$ [1 k5 L" X) C( WAPU, SEE - AUXILIARY POWER UNIT ) t) p6 s9 X8 _/ a N+ S: CARINC, SEE - AERONAUTICAL RADIO9 [& r+ S. Z9 g1 X INCORPORATED 9 v" O8 M" b$ G$ U# O. I6 O/ ZARM, To make ready for operation.0 j P8 [- [0 o) u |0 j 附录, ' U- t1 C6 x4 H0 M) p飞机飞行手册的附件,包含基本手册中未提到的飞机形+ h! e, t% Y3 i D1 K% n l. x 态的其他性能。是附在手册末的补充材料。0 {7 E$ R3 [. s 顶销, 5 { J8 X- r; I( g# M用于连接起落架扭力臂两部份的销子。 9 Z. q! M( \2 ?8 l8 X5 L9 J进近方式, # m3 b4 f2 f" D$ |一种综合了控制横侧的航道信号和控制俯仰下滑信号 6 G Y! w6 t, v- b' b% I# S1 j的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系 % g8 l2 ^6 U0 c( s3 i- e1 S. D( i统正常时才使用。! H8 X @) j. F; W- A, m% p5 B 辅助动力装置,. G" J3 i+ T& k2 s 见Auxiliary Power Unit6 F) n/ {% Z# j) O6 m containing additional performance for aircraft @/ A+ g$ ? `3 b3 tconfigurations not con7 l2 |* j- ?5 _" Q c) |- u4 p. N. E& Z" q4 c+ Q b3 i/ s+ L0 i8 r APEX PIN, A pin for joining the two sections! g5 V: J- n! n- Q4 _8 V to7 x+ U; z5 a# d% L8 r8 s5 i% t" p7 N7 r5 }7 v航空无线电公司," A+ ^1 p$ Z+ P1 i 见Aeronautical Radio Incorporated. & x. I) }" Q; i- m- H$ I$ T3 Z0 `1 J预位,% L$ e1 m5 v" e; B ^: t- `( J 部件可以开始工作的状态。7 _9 i! h2 }9 B; h. I. m" | 英汉对照民用航空词典B OEING6 o" u/ f9 w" F! B w TECHNICAL DICTIONARY 131 D$ g. Q4 z7 i# I3 h2 d0 ^ ARC, The curved track over the ground of an aircraft, l" F3 a! P3 I* u+ ` flying at a constant distance from a measuring+ M% T! P) b" m) `! c equipment (DME). 2 ]5 E/ s& E3 |- _/ C0 B1 O7 }in the limits of self-contained system 1 D% x2 h3 l3 sapability.! u' P7 V4 D; c4 `( l# I tem for opposing or restricting3 L8 R! p# a9 L m ovement. 8 v. M8 {( j# h" }* Z) ]SPIRATED TAT PROBE, A sensor that measures total* d5 f( ~, ~. P/ t ir temperature when the airplane is in the air and that9 A1 I! q$ R6 `% Y2 q7 \3 K! { easures outside air temperature when the airplane is 3 v R# M5 s9 |2 r3 S, c% G0 fn the ground. The outside air temperature is measured 4 i/ I+ \$ a. t. S9 Z& p( LSSEMBLY, The fitting together of a complete structure 6 m' z3 W2 g3 P- ~* h' MSSUMED TEMPERATURE REDUCED THRUST, The # A1 i4 ?" @- H! NATC, SEE - AIR TRAFFIC CONTROL 1 Y7 g. [" g4 P0 v& J/ V) G( q- r/ l, [# E8 G 系统中所产生的一种用以抗拒, J- c$ K# a5 } 作或限制动作的力。 " b7 X9 L6 H9 N% v) |( f, @3 M头, 8 n9 @% i# S7 o用来测量飞机在空中时的总大气温度和在地面时的外 + `# I0 b1 e" ~7 K- e6 J% t温度。地面外界温度的测量是利用引气将外界空气吸入 6 y" l6 G D" R y' M头,以达到测量的目的。3 v& `8 y- h: }. k, f! Z 配, " [. ^7 M$ I _5 A2 H7 I5 P& D一个完整的结构或组件的过程。 , L9 z' B" x; d假设温度而得的减推力, . s. \+ z. W8 t p+ d1 [. w9 ^0 {推力设定值时,假定一个比实际外界空气温 " E' e- i u1 q' |5 L空中交通管制,9 y9 Q# K- x& y, Y/ {/ ]7 Q 见Air Traffic Control 2 T9 S9 s( F2 A, yAREA NAVIGATION/RNAV, A method of navigation1 ^/ J h2 r% {# ?& Q that permits aircraft operations on any desired course - s+ ~% k% I- ?9 j+ F1 S% `within the coverage of station-referenced navigation S7 r& s& @: Y/ q9 Psignals or with ; `+ v3 | R% rc ) W2 G% U1 {& b" tARTIFICIAL FEEL, A force developed in the flight 9 U9 C, _4 y. K, gcontrol or brake sys9 \" s! i- [% ? m 0 B# x: E7 v5 c% ~4 ^A1 Y2 x) Q }- Y6 ^ a1 c" [8 d4 g& K) u m+ A O* O+ F/ _, W r/ T. y2 g, R/ O o) K& Q. M1 S/ q, K by using bleed air to draw ambient air through the4 T+ n1 X3 d' F" w5 V; m: h sensor when the airplane is not moving. 4 }& G& z' ^' L3 F9 O- ?1 v0 S+ `A) G$ D9 x' g B, D* f or unit.- L5 R6 o/ n- f4 n$ b A$ P- l' o/ P: r! q lower thrust obtained by setting a higher than actual 0 c$ z& h! i* Z+ P6 ?% ^2 V& mOutside Air Temperature (OAT). ) y4 M/ ]& U T# p# L* q弧线, % b" i! A" i! _3 r4 `7 b飞机在围绕DME台等距飞行时的弧形航迹。% ~3 C: V/ F% s$ L) M 区域导航, . O2 \3 I) N$ v: }容许飞机飞行在有电台参考的导航信号或自备系统能 % [9 R0 C0 L% b# |力极限范围内,飞行任何预定航线的一种导航方法。# t& U1 J" j4 }' L; I. E 模拟感觉; O3 p+ l: M- f& x; j/ b 在飞行操纵系统或刹车4 M* Z" r8 b8 u" J; z& |( ]. ~, C5 w! h) R- S吸气式总温探 3 I% @+ {/ c0 f% U, ~5 X' U( O: [1 X7 p- M6 [" _; @8 M$ T: u# r: g1 S% Y+ J R" K8 w- D组合成) | [1 |$ `8 v7 ]$ j6 n* f" w9 F6 ~在选择起飞 : f8 D l2 x4 x1 f, F! q度高的温度而得到的推力。用这种方法可以减少发动机的 ; n3 f4 X$ m. u2 H8 m0 X4 [磨损和维护费用。 0 D7 h6 ^ f/ |& i% a6 B M; a! [4 e9 N: U英汉对照民用航空词典B OEING$ x* Z" J+ p6 U) t9 U1 {$ ] TECHNICAL DICTIONARY 14 4 X8 A+ K0 o; M. i. r* Q/ P0 y+ tATE, SEE - AUTOMATIC TEST EQUIPMENT Z0 Z) s6 Z0 _, v, Z ATMOSPHERIC PRESSURE, Pressure of air due to the7 p; W' \, j( n+ ^1 D arth's atmosphere, expressed in pounds per square ' L0 u6 Y- @5 |" jch (psi) or inches of mercury (in Hg) or millibars (mB). , i4 X. S# U( ]- \% [, f9 @TTITUDE, The relative orientation of the airplane with! z7 s- z' B4 _% l) }# h spect to pitch, roll, and yaw.# E- Z) r$ b* Y UDIO CONTROUSELECTOR PANEL, The panel in 5 t% U/ E4 u3 n1 q/ {" f# G+ ye airplane which controls and selects the routing of ) g5 n& R2 m& m5 K( R0 g- v, h6 _, |udio. , ^' l* c) {. q u6 ? @UTOLAND, Automatic landing using the Digital Flight 7 i* N6 [* X2 N% Z" Control System./ ~6 ]- h$ g& T+ z" n n. 3 e" ?8 G8 M7 c, [: L# U3 n$ ?M, A system7 d4 P+ x2 Z1 ^% Z- [+ V4 V7 X omposed of all necessary subsystems needed to guide& _: E' x- ^. n# o0 ~8 o: v e flight of an airplane.& R) a$ @* l, v" v) I EQUIPMENT, System test - }& G8 ?# h4 k! j5 Q2 iquipment that operates under computer control. & t/ ~+ v/ F+ M! ?' g装置,

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e 9 Z( Q: Z: R3 Win 6 |0 L6 l/ S0 jA0 Y5 c, E2 E( x7 `6 k' D re- }* ?; o% l: O: v A! V- e0 z! \' r- W% o th0 |1 r+ @* Q4 Z2 O$ u a! d8 Q7 D. p* n6 D' w A / T6 K8 }7 K- g+ {; z2 @C - G) e5 g; w2 }+ F5 vAUTOMATIC DIRECTION FINDER, A system which 8 f1 [2 y# Q* g- @& v0 ]& V3 Vdetermines the direction of a radio statio+ U7 ]- T* _: Q- D9 |1 H AUTOMATIC FLIGHT CONTROL SYSTE a$ \) _4 i4 J c * o; I ]' T2 x$ }* Xth A k7 `1 u, ?7 t+ X4 b7 P+ R0 WAUTOMATIC TEST+ K+ W. L' n8 b; N9 D7 ?% { e 4 s. w% {3 P0 }, U' E自动测试 8 N& {4 L2 |% _ I8 ~) ~见Automatic Test Equipment. # A3 _* S |3 M9 _) i大气压力, - M* o* O- l1 m, j1 a! o1 C由于地球周围的大气而产生的空气压力,以每平方寸多 l. a w; ~- b4 f( |磅(psi)或多少寸高水银柱(in Hg)或毫巴(mB)来 7 m/ |" b) Y' Y% U1 r% H; X7 Z示。- Y% w( n# f) W; f3 [1 R( W( E: u 飞机姿态, 2 Z# ]- m* s u4 g% D" _飞机与俯仰,坡度,和偏航有关的相对方向。 0 n" l6 G+ J; x' R9 N) q音频选择面板, ( u7 V9 s% B' B5 l0 i# q# i飞机内用来控制和选择音频通路的面板。 6 ~# n- s1 f; J2 O7 B7 W- ^2 _0 J自动着陆,* _4 I/ T% ^8 Z C- B, T 使用数字式飞行操作系统来进行自动着陆。. ~7 J4 Y4 g2 M( c& R 的系统。 : k! Q4 w; G! m' d- F$ M$ Y, b3 D! ^% Q系统所组成的一个系统。 - m9 t) u* u+ m a在计算机控制下运作的系统测试装置。 & n5 ?1 o/ ^" |; I" f' [) a' n* g3 h4 C9 ^" T) g5 h( |- [* ~$ s7 E2 ?, y. b# f自动定向仪(ADF), $ O& Q1 ^( f% f: c确定无线电台方向) r) } P1 [$ K 自动飞行控制系统 & e7 J, ]0 k: H$ [3 h* E# i由所有能引导飞机飞行的子8 J$ Y' J$ g' \2 @- @ 自动测试装置, 5 L; N6 E, U# M9 m' T英汉对照民用航空词典B OEING- ~# z; U5 ?4 H, e3 i8 z TECHNICAL DICTIONARY 15& d: C. O! C$ i X! H" ?" Q' M8 I! M AUTOPILOT, A system which automatically controls . e: z6 l- a- e1 n7 fand guides the flight of an airplane. ) p- h! E/ W% g$ s, K+ U! aAUTOPILOT FLIGHT DIRECTOR SYSTEM, An- v; R( d9 q' A tor7 H, u9 _/ |: P& u& u UTOTHROTTLE, A system which automatically4 {$ z( X6 L! u# j' v' N ontrols the throttles of an airplane. 4 G& I7 [$ U! P7 _& LPOWER UNIT, A small turbine engine in5 ^# o) E$ N3 }4 l" v e airplane for supplying electrical and pneumatic# n5 {" Y0 A$ e- s& Q& B ower for systems operation on the ground or in flight.% h5 Z+ A* B0 R" {6 Y' O# B# J VM, SEE - AIRBORNE VIBRATION MONITOR 6 T3 |; Z/ b" CXIAL FLOW COMPRESSOR, A type of compressor 4 e$ A; @" A* \: a' ^sed in a gas turbine engine in which air passes through 1 a9 m% x. w$ @' v7 gXIS, An imaginary straight line or an actual physical. k% `# }% [' H( N- c* S omponent (such as an axle) around which a body can % k: l; J$ K- c6 ztate. 2 w- S. e7 O6 X, R7 i6 e仪, 4 K) b, D6 h* f i( f1 J! h* O- B" o+ f 自动驾驶飞行指引系统, 2 }+ M/ W5 M5 @9 t; l& A8 n7 R B2 H动驾驶和飞行指引功能的系统。 1 D' T. j% q3 D& T动油门, F7 u P9 L7 c" V ]5 Q自动控制飞机油门的系统。 1 ^- S! @0 |7 u0 O: e2 [6 c9 l是飞机内的小涡轮发动机,在地面或空中给各系统提供' W8 t3 @4 x; r9 A7 j( c! I. g9 Q 源和气源。3 l: \* x' E0 c% { v' q; [$ S2 m 称。5 {- W/ F- ?6 _1 a' i8 P 载振动监视器, % e. J& ~- S. `2 F& b见Airborne Vibration Monitor/ Y4 g5 ?# A7 a: ]5 B integrated system containing autopilot and flight direc; W! V8 a( X4 e functions. : T# l- |3 s/ I) E* g4 n* ^ ]4 T8 RA 8 [) J3 B1 x3 U* j% [& x2 kc & n5 g, d% o7 x1 zAUXILIARY 2 E& i5 y) w, Qth 5 a+ [ i5 L J6 [5 Mp ! D3 z5 R2 Q2 {' T' K% lAVIONICS, An acronym designating the field of aviation 9 Z8 q$ L$ V' M! u4 ]0 Telectronics.4 `% _2 t4 Y x, F) O; ~ A & V5 E( R1 ^: n# }A! B: G$ K5 t. |: H& [ u 8 P [# w$ n F6 [! Y( \! `1 mthe compressor in a straight flow, front to rear. * X7 n D; O+ `+ C0 i& c! X" WA% K( ^4 K T) t. f3 l c* F* F) t2 c+ |/ I- ]7 @4 b ro$ Z4 l# g7 C; j% l+ K! g5 l. p5 x 自动驾驶/ H- o/ N( l* U. X' g 动操纵和引导飞机飞行的系统。! b9 E8 F/ V: j' r5 T 一个综合自 2 \( ]+ E2 y% A ~9 A" l/ p8 \* m/ x; _, Y 辅助动力装置,* l- X2 \' }6 O9 w: e! ~8 k2 C3 @ ]( B) ^# N4 ~ j$ `航空电子学, 6 G% L& ?* a( d2 c* B+ O. ^是航空电子领域的一特有名. M3 I9 ~, l" A" ~/ x) P+ h: V# y4 I m& m! X' w X8 w+ K7 q' s 流压缩机,' ?; [# n& D7 o; C! ^ 一种用于燃气涡轮发动机内的压气机。空气由发动机的 & W) a8 Q( n2 t部流出。4 L/ U' g2 x; [0 W2 \ 线, & B2 Q; T1 k- k可让物体围绕着作旋转运动的一个想像的直线或实际 9 Z, U+ a3 y. Q4 `0 a3 R在的部件(如轴)。 3 v- k3 L# p; f5 ?' r' F* `. R l8 M 前部轴向流人,压缩后,由后 * q) W% B5 ?0 o& z# @8 u+ Y. c% x: y; d3 Z# h" S ~ b/ U$ a! Z. Z; Q& } 英汉对照民用航空词典B OEING# \/ _# _, V0 [4 h TECHNICAL DICTIONARY 16; j1 [: J# ^" Q( { B/ s5 y4 A2 ?2 u ACKCOURSE APPROACH, An approach to a runway `4 `" M: L. `! q: L* |versed.0 R! v! c8 T+ m/ U, v own on the EFIS that ( Y v0 J/ I4 D9 Z0 _) foes not readily change, for example, navigational aids. ' F8 V. d- o+ u3 h! f! \) N f/ ~vement in the tank or reservoir.9 j9 A1 [1 ]7 X! \ ALANCE TAB, A small hinged moveable part on the0 |; V6 w, C" r5 G$ Q ailing edge of a control surface (aileron, elevator, 6 ?4 ]) m, O& f$ y' W航道进近, [3 o. m1 K- _0 }) t! T9 j 相反的进近方向。当反航道进近时,无下滑7 {6 H0 H" [; Y6 `$ h 显示在电子飞行仪表系统上不经常改变的数据。例如: / D [9 O9 }2 c7 D5 A. O# R* c: S8 c7 X航设备。 & Q9 p4 a! g, j0 T0 \在燃油箱或滑油箱内阻止液体流动的隔板。 % P; |$ X3 w8 l; R: A# @动补偿片, + u# }5 G7 i" `' \% l5 T6 A铰接在操纵面后缘(副翼,方向舵,升降舵)的可动部。 a* q; ]$ p$ g$ }! J* z 与操纵面相反,以帮助操纵面运 8 p* }- v6 i0 w8 E" S0 F# Y0 Z3 HB * D* `* R6 }7 G9 j/ bwhich is opposite the normal approach. For a& S: r) N2 e$ W2 \$ {( E9 ~0 \0 T2 d backcourse approach, glide slope signals are not- P& u# L/ U8 N2 H/ G+ f2 ` available and the sense of localizer signals must be" @: s. K" ^7 d/ T! [- W" @' [ re 9 W- @% l- y! wBACKGROUND DATA, Data sh+ V; a' {) P Z* J: y d ( s" E( V3 ]! j+ C+ QBAFFLE, A partition in a tank or reservoir to prevent. h" f" k& m. ]+ t5 x fluid mo+ T. V/ s8 {4 ^4 ?( ?% ] B $ ~* N/ c% P7 a9 l w1 b' S! Str 6 A5 C- z) c, Y" k# K0 orudder).The tab moves in an opposite direction to the: d2 d+ N4 N3 b9 z! z control surface for assisting movement of the control+ _9 X u- ?2 ~! s surface.3 [0 A& n1 ?* m4 q/ t/ _* {# |! h$ @与正常进近: t& P( \% M0 F1 ~2 a 道信号并且航道信号也必须逆反。! E& y9 H( ?# _; ~) d" o 背景数据, ( W6 G: u( x: n. S) K, f% M& n. h) f6 g 缓冲隔板,0 h8 Z4 p- {$ N! `4 W# f* ^5 `- u/ e0 {# U' L' i+ `6 p: V& N随动补偿片的动作方向 * }% n: m! a( y+ x$ c动,减小操纵力。- v- \# n3 W# u- l5 F& l 英汉对照民用航空词典B OEING# E- Z: ^ E8 g' @ N8 W1 `( @ TECHNICAL DICTIONARY 17 $ M4 S' P7 O8 N- GBALANCED FIELD LENGTH, The field length; m0 d2 m) ]. D/ } associated with optimum aircraft performance when 6 z3 F' V" o: P! V4 Hbstacles are not a constraint. In this case, after engine , L) z( A" S: {4 Q( ^, I) n6 j9 t! f" Rilure at V1, the distance required to accelerate, takeoff % I8 Z- R6 x+ C. q1 Dnd reach a height of 35 feet is equal to the distance0 Z ^' N* \; Q; I& g ALLAST, A weight installed in an aircraft to maintain" ]) t9 o) o/ u6 Z- ~4 C ALL NUT, A fixed spherical nut driven by the : p. q& C, Y; |5 o4 M- tAR OUT OF VIEW, A signal used to remove the flight0 D( e3 O- z U4 v7 J/ r) F AROMETRIC PRESSURE, The pressure of air above 6 G0 D$ o4 _* c' M4 Tg) or $ S5 o+ T4 `8 E7 a5 amillibars (MB).2 U, H6 b$ z* c, p! \& E% A- L ATTERY, An electrical device for changing stored ; D0 P0 j# C8 H- ?* f性能的场长。在此 # C; X7 f9 `8 Z4 @8 L况下,V1时发动机故障,要完成加速、起飞、离地35 ; w# {% F- N+ C y9 u( s尺所需距离等于相同速度下完成全停所需的距离。 $ i/ f4 w: R7 k Y6 x8 E舱物, $ L- o; v( D# Z3 ^+ g: D重心在许可范围内面装载的配重物。 3 n# z! N+ J4 I& q形螺母, * e4 ^, h% `( G3 C4 \- G+ l- C的固定的球形螺母,用以使襟翼和水平 # B) u+ l$ N( C2 D. e引杆消失, 7 o( Z% {' ]8 G+ o% z指引杆的信号。 * S( c8 S$ X6 V6 f! c9 f b压, % ]5 i3 e* q# y% v: d% ^压力。通常以多少寸高水银柱(in : \5 i. T5 J+ l3 z; t; u/ g瓶,% Y; U) ?7 E* F; s 的化学能转变为直流电的电气装置。 ( j8 e6 n5 H4 z9 F s" T H* X( uo1 [! l1 \. h5 g/ B6 ^4 J X fa : B4 Z8 `* J: q r' ?! T& L( Va 9 f( p9 t) G$ ^: j+ y3 S( d9 crequired to stop from the same speed.. L6 Q& z6 i" `2 D) w B" P) ^! j; V/ u the center of gravity within allowable limits. - y0 i. U; g+ i0 P$ h' T2 e; PB) G" a3 s% {, E: m8 h6 w jackscrew for flap and stabilizer movement. 6 v: p" H$ X; v/ O; c; r( h* G6 pB0 V/ n5 n5 q6 Q; E- w \* w X director command bar(s). " D+ U, Q, ~1 v d2 P C( q1 }B2 F; A- e" O1 z' a% W5 b4 c zero pressure measured in inches of mercury (in H * B) e4 Z! g6 C: E( Q4 [in ) E; X4 V1 O0 W- L7 l9 L1 X7 {$ jBASE METAL, The underlining metal to which alloying0 R. h- p. X) J% S3 q. Y; s agents or metals are added. , K8 a+ g' e$ q) Y, D1 K6 JB 3 r3 ^) W; j9 ~8 J7 ?; V/ u0 cchemical energy into direct electric current.+ @& y! G& T# g* L D 平衡场长,7 y$ N. x8 ^% k0 b9 D/ ^ 当障碍物非限制因素使飞机达到最佳 " c5 z% G7 l6 K* C6 u0 |+ a# J( L8 _$ ]% {7 N/ D" s. O' U5 h" z+ o! k5 N( W' { 为保持飞机 1 _9 E u4 D3 t- \! c8 L t% p. B) E* N1 A$ e% t1 B7 ^0 n 由粗重螺杆驱动: Y: w! l" b" @' _1 B& W 安定面运动。 " F! q8 x! O1 v u3 {7 J* D0 T: X$ t. s/ X7 m用于除去飞行 3 }9 p' n7 K3 t& g! a( ?* P6 o4 Z8 E0 B% M( o零压力以上的空气 ) l5 y* |' c6 I6 S* e# ^Hg)或毫巴(MB)来表示。 / u1 f$ g" p$ X# G R1 f$ U基底金属,; z3 l: J0 F9 S) q) I0 Z" ^5 ~ 指合金中的主要金属成份。0 B i3 c( ^5 |' g0 J2 e( o; R5 c# C: \4 U% H' l) n9 l将储蓄 : J) Q% g7 C( z英汉对照民用航空词典B OEING& `7 y$ \ W }- d2 f7 H1 g, U TECHNICAL DICTIONARY 18 o2 b3 m2 E, n5 B) B* ?# K( B4 BBATTER $ c4 Y% F' ^7 Udirect cu 4 T- ]$ V/ g" e$ S0 q$ Zpower su % X. q/ w3 z: sY BUS, An electrical conductor supplied with ! B, \& V) ]/ b' \+ |rrent from the battery or transformer-rectifier for " P: `2 ?2 Y) P1 s, Y# {9 [# wpply to operating components.7 w' D& @7 P. s! F. W8 j CHARGER, An electrical device supplied8 r# Q# K2 p: A" A ith alternating current, which produces a direct current7 [) b, [5 g0 C* z8 ?# y* ] utput for charging the battery on the airplane. / ]. U0 g. w" PAY, A compartment in the airplane structure. H ` g# G3 c0 L Y9 WCD, SEE - BINARY CODED DECIMAL 2 v; h: l: F) ~7 w$ x* DEACON, A device which emits a signal for use as a: e9 D$ R/ D& j, R, `1 y uidance or warning aid.- r2 b3 \) n1 J' _3 ^$ ~ BEARING (NO. 2), The direction from an airplane to a 5 T& H: |8 I. |1 Q+ s7 s7 E( Z) |ground station. " p; Z/ p$ X7 R- n瓶汇流条, 3 [+ s0 y' L# E) f ^将从电瓶或变压整流器来的直流电供给工作部件的导 1 |) b( x( U5 `4 i+ Z3 H' I体。 0 }! a' V- Q4 z- M5 q9 Q8 R$ h瓶充电器, " o) M; U+ }& T$ v- I. O: u用交流电向飞机内电瓶充电的电气装置。带有交流电的8 i% v$ Q5 S0 j5 |" ` 气装置,该装置产生直流电向飞机上的电瓶充电。8 @& P; O/ m6 v ?4 Y- R' a 舱, ! |( [& \6 m9 ^' K飞机结构中分隔的空间。 1 O" G: h9 U7 b7 \3 S) t/ J二进制编码, ) F% H% d$ G, _+ _( A见Binary Coded Decimal * d7 Q' Q) D* L: t* |4 w$ D3 D- FBATTERY 1 g l4 v* e& c& E' b) E3 Vw8 e: F: K/ h) _" f4 }( t o ) ^0 e5 p9 \9 F5 LB9 w3 m9 a2 F/ z9 U! h B3 ?( _# G" Z1 c7 a b' }) W" ^ B * S" B7 H3 A3 n; l9 v, Y9 u/ Hg $ A: ^% [9 x9 M( t" s' i @, zBEARING (NO. 1), A surface that supports a moving5 U' ^; ~4 A1 \+ a$ E7 ~ part and reduces friction between the two.( J' @% N/ h, V# ^" |/ u- E0 l+ N- }" G0 k) k3 H6 G# s9 [% I9 y( j p' w( P: E3 W3 W4 C* j: [0 h: r1 c- I1 I, h! C+ p8 g' p5 v$ m7 T9 s- Y; A$ i5 G* y, N, X 信标, % B4 I8 z \+ M# T% v: `发射引导或警告用信号的装置。0 N/ p4 c/ }3 ]! d0 ]" Q g2 g 方位(NO.2),6 U: H- I; b. ^& p1 p0 b* x$ m 从一架飞机到地面台的方向。 3 z. F- c5 w5 W0 J& U' C. G轴承(NO.1),1 Q3 s& e( h# A. ^# s9 y; X6 K' @3 i 用于减轻机械转动磨擦的机械装置。 ! D6 C% |6 b4 H2 y英汉对照民用航空词典B OEING# H% C9 C: V. W8 G' C8 M" n TECHNICAL DICTIONARY 19 - q) {7 j' o7 q$ FBELLCRANK, A double lever in the control syst" V- f5 p1 C+ N# g/ u changing direction of motion.3 }: d! o1 \" Q7 y5 X4 Q em for $ l9 a" }' \5 yct in the / ?6 c' c( B' |! _6 Y, B" Hneumatic system for absorbing expansion of duct due/ G2 Q7 x$ ^5 t, \5 R heat. 4 P; o4 c7 M+ MELLOWS (NO. 2), Corrugated folded or pleated! b/ o4 k" L1 v7 e: d2 h7 Z: m) z2 `0 n ontainer or compartment used to measure pressure. , X, C9 o2 [, ~- M6 @; WEZEL, The part of an instrument case for locking the 6 S9 Z1 e+ w7 B. s7 flass.! |, p- y L! e; Q0 j) C4 M IAS, The potential difference applied between two" i" I, m) l0 P V oints for controlling a circuit. ; A% y- x. {) T: l5 Q% @BILGE, The lowest part of an aircraft fuselage. A place H2 ^- c) h! S. N* C: c5 xwhere water, dirt and other contaminants collect.8 L; g' j% {1 A S 气源系统内提供管道热胀冷缩所需要的余地的波状 ! H0 ^. j+ w1 \. @轫管。 / @' D; v6 H! r: D! ?' V J空膜盒,5 I1 a$ n- B5 k5 ~3 _ 一种具有波状表面的容器。用于量测气压。 ! Q- \( ?: B2 Y) `+ |嵌沟缘, R- z+ _( Q6 @$ _ 将表面玻璃固定在仪表上的圈状零件。 : T8 K, P0 E! h9 @3 a: Q& g( J3 a压,: n g/ g( f- j6 x; D" { 在控制电路的两点之间的电位差。- l! g' W; k6 h: N7 p7 ` 机身腹部, + U5 }7 y* X7 `! b; Q机身的最底部,通常水,脏物,和其他外来物集存于此。 * J( X% h8 s' S- k5 P$ xBELLOWS (NO. 1), A corrugated flexible du 5 g4 T. y* O$ L0 P4 i' R6 R, ap5 t2 z R6 G- Q/ g. q to7 Q' t& q1 i+ q8 k+ i B 4 Y1 a* i: e+ Dc7 @7 I) g; A* d9 f7 W* Q4 X B " B7 Q8 K& o) Z% f5 sg " T1 h) d% L+ M: b, n* G$ o8 |B 8 h2 S) W- V, u Q9 G1 N" D3 sp+ m/ p( B3 G& p, p% P 直角摇臂, , A# @! _( ]' R! ?在操纵系统中改变运动方向用的双臂摇臂。7 u$ b9 t& b0 v$ }6 v% m T 波纹管,8 t, g [+ s) G3 t% K) V X6 g! Y% M' E ?' W8 J& W; j+ e6 Y9 U; ?. F7 E" H2 }( s+ Y6 m% Z5 I2 ~) s: f1 z* D$ f9 O- F l: p+ b- ]8 l英汉对照民用航空词典B OEING. J7 q% T) B) C5 k0 F, E7 ] Y( `. e TECHNICAL DICTIONARY 20 . C% `5 z# w2 d! PBINARY CODED DECIMAL, A system of coding each% h6 ^$ S5 @- l* m8 e5 F* \5 \6 s- F" @ digit in a decimal number using the binary equivalent. ; J5 h! L6 e+ a& G8 G' R& GBINARY NUMBER SYSTEM, A number system using' u# s: h3 _$ d/ F, f0 E s 8 T3 }% z' J8 [/ h7 }$ W j- mIT, In the binary number system, the smallest unit of 5 G; y+ N J+ |) F8 xformation, consisting of a 0 or a 1. " O% ^+ c# {5 ?: f: lITE, SEE - BUILT-IN TEST EQUIPMENT " O# d5 x n. B" ALANK DISPLAY, A display that does not have any: @5 E+ |+ j9 {2 W. h dications, normally due to failure.3 i# J0 {& j( H; b LACK BOX, A container for electronic circuits to record9 `( T0 Z6 ?* P# `2 j5 ~ ight data.8 e0 }* N5 g4 g LEED AIR, Air taken from the engine to power various4 A3 X6 j9 G+ q; e0 n7 H, K ircraft accessories. ' P& u' A8 s0 g2 }: i/ [5 W0 Q/ RA valve in the pneumatic system for air9 V J8 I! x! B. B. N; ? supply from the engine or auxiliary power unit to the 4 r- v4 c8 o t8 Z8 \, p0 Apneumatic manifold. A valve on the engine for reducing$ v. t' n9 J6 g/ v6 f pressure in the compressor section. 3 j: M) x" `# T进制, * a6 R( t1 w+ { S l8 e进制, , R: [) z4 s: V9 `4 U; \ [5 b一般用0和1)和2为底的数字系统。9 h- M! c3 D' _8 s( z, l5 M 特(二进位数),1 z t9 k" \1 m& g6 ` 二进制中的最小信息单位,包括0或1。 & y' h2 |# x7 U1 |* K7 Q( O/ b内自测系统, 0 \8 c C- J* k f见Built-in Test Equipment % q' c; F& ?5 k8 w" E1 n. H+ O9 Otwo symbols (usually denoted 0 and 1) and having 2 a6 ~& G+ E$ N/ F0 t, m o3 c its base.; I) J: f8 U) G, P) j/ G# I, x6 W3 j B+ k2 j( U+ X) ^$ r8 Z9 w0 [ in , j* U' ^2 W7 `" bB * x* {7 k7 N, D* B2 oB Z3 X1 D; V* n& G9 d) Pin 0 R& U4 c3 e" A+ t2 C3 ^9 e% L# tB6 }$ s1 T: ]" t- @, P' v0 | fl' ^' o9 B# `! F' n2 K B7 h* k! W% @6 o; ]. y: J7 }% [ a, C$ |5 T7 n! g BLEED VALVE,& t; B; ^/ q' |/ `5 ^ 二进制编码的十4 m+ ]% @, P) `# e0 {% Q 一种编码系统。用等效二进制位数编译十进位数的每一 ' y, e' {3 U6 C, u& u/ |- Z位。 0 b* l9 n" P# f @4 O% V6 a/ }& G- Q1 z. v- O' q. J以两个符号( 9 b2 r" A8 _& ^, b t: p# h5 z5 Y7 Y; R5 w& s7 e L5 H4 [2 d$ [$ D+ u! C% [9 p0 V .. P. O/ L$ Y0 ]4 y+ X 白显示, " b. G. l0 E+ B通常因故障而造成的显示器上没有任何指示。) r! `" s, i& w+ F/ N& O- r 匣子,1 J! u" _, X3 _ v 装有用于记录飞行数据的电路系统的容器。 ! W1 I- T6 h o9 K# G1 }% ^+ ^6 d气, , r; W. s9 u$ C5 g取自发动机而用以驱动飞机上之各种附件的空气。 # v( F+ ^. c, l: C. J3 m' U1 [/ |气源系统内,使来自发动机或辅助动力装置的空气进人8 F( s6 T2 H, r- C 气源支管的活门。发动机上,用来降低压气机压力的活门。1 P' D5 \" q3 {+ [3 E9 u1 g* @& ^! p; S/ |' |- R7 g: Z6 I8 y: e, E9 b6 R1 S引气活门, 9 T# s5 ^- u9 z' T. X" K英汉对照民用航空词典B OEING : |3 E3 \+ i7 L. I# N7 aTECHNICAL DICTIONARY 21 s7 k B+ y/ ~* ?1 I9 H: k( H7 W( N BLOCKER DOOR, A device on the engine for blocking 7 U, {4 o6 t0 D0 Pthe normal airflow during thrust reverser operation. + ], l. {3 G1 w/ M8 S8 c, b8 MLOWER, An electrically operated fan for circulating air. * ]4 K! [4 t+ e' ?7 l& r+ n: Q' ELOWOUT PANEL, A panel in the structure between9 T( u( @/ j; V5 w' t9 r o compartments that opens to equalize pressure in 3 ]2 @9 x& S$ n5 b( v& ^" f0 `9 ee compartments.2 d0 }! M5 A1 ?4 A# d ODY GEAR, The landing gear attached to the # Z1 J" A! E& \grounding. 4 G/ Q2 f9 M! S1 `' \2 q: ]正常的 ) ]6 o. P; Z/ R: Z% R气流。4 g1 x1 h. S% {" E 鼓风机, # L* G0 }# ?. _* @7 d用来使空气循环的电动风扇。 , e- |8 R& V( N, M7 o压口盖, - {1 H' P3 q9 `8 m/ h" k: Z两个隔舱之间的口盖,打开后可使两舱压力相等。 - \ w4 X( y4 L. h2 ~. t' W身起落架,. y. T8 }0 o8 ^# U 身构架上的起落架。 9 x0 @1 A3 f! Q3 eB! y: y& B6 B' J" G B 8 l7 }7 q" J( v* ^4 \' {0 g* Gtw9 C0 R! J+ C7 {- x. v: ?+ j th L2 H$ k* j' Y# H. fB 7 u0 X. R4 D9 a% z2 N0 afuselage structure. 3 V6 s! {4 Z6 Z* ]) gBONDING JUMPER, An electrical connection between % w( Q2 ^% n9 R( ]- s. Ua component and airplane structure for electrical/ J# h' C% J" |- E 阻流门,, q) c. Y) C0 @ [ 发动机上的一个装置。在反推工作时用于阻挡# ?+ H' M& C, S+ O, g5 S$ d+ k; \/ r+ S. U I) t: v* X8 E: O9 i9 S8 C: t 装在机3 Y, m! X+ c+ \' U6 h* @$ @. l$ K& @ 搭接片," U A6 y6 Q: S* V5 X3 C1 |) E6 A3 c 连接某个部件与飞机结构以形成接地的电接头。0 x" ^ r, _0 N8 `) {: i, O% B: Z 英汉对照民用航空词典B OEING # H7 F0 e5 ^3 k8 xTECHNICAL DICTIONARY 22& F) k( [2 ~+ ]. {5 a BOOLEAN ALGEBRA, A mathematical system for % @% `, r1 ]/ e' d. iwriting combinations of logical statements.! `- r, S" S ]$ j BOOST PUMP, An electrically operated fuel pump for ( r W0 e5 _6 ffuel supply from the airplane fuel tank to the fuel + }* b( i, z& v1 R6 s1 Amanifold.+ e6 |0 L0 E3 J6 W; z# Y4 p8 ]" |8 D BORESCOPE, An electro-optical device for looking at( i1 R, n! [3 y4 L' q2 X4 F3 |( V ternal parts of an engine through holes in the engine.7 H$ x6 h9 ]; d2 S5 C( \6 N7 y orescope ports) ) y/ E+ a( b4 k2 P. h( {OURDON TUBE, A curved flat tube in a pressure gage7 X( \, k, T) O r moving the pointer when pressure changes inside : \* ]5 ?5 b+ [' o1 R2 d: Y1 hon the ability of the brakes to % U& E' i h7 x) R. Hbsorb a predetermined amount of energy during a1 i$ c$ ~! }5 t" `+ a' H9 _ jected takeoff. ( o7 V4 k! ~/ `7 A' ]" a/ T用于通过发动机内的孔(孔探口)观察发动机内部件的% i, k$ `7 O3 i+ \0 R 光设备。 6 {% Q, y! \9 F6 a# ]# a端管,2 j6 ^2 m' i, u4 X" l# i 测压计内的弯曲扁管,管内压力的变化时它使指针移0 Y6 f7 n. U) D, L8 I 力。 ' O* ?7 ^6 m: D6 j0 d8 O- M6 e极限重量, 9 m9 c: u$ [3 p) F& e- B; t2 q/ [4 b9 p1 X- p起飞重量。 / W3 H1 P0 }) T& q8 \( G% ~发动机滑油系统与大气相通的通气口。 - G1 `& l8 y9 ~/ X) u; A3 V! Win% H! |* j% p$ ]& H$ N" y/ U1 L1 t (b 0 [. V; G8 e' ^7 hB 0 }2 H) e+ T5 K: j3 H$ |9 r( Vfo ' J2 g3 d1 W. S# S7 e4 U4 F, Cthe tube.. @0 a+ m! i1 d BRACKET, To enclose or surround.' O) n( l; i* C% f N4 { BRAKE ENERGY LIMIT WEIGHT, The maximum1 y& A, O9 h( G- X* A4 D takeoff weight based ) W$ L$ W* N* X: Z( [a. ]6 ]- i' d _% a) ^. t re 3 @$ R* A3 H) c9 UBREATHER, A vent to ambient of the engine oil system. & I5 y4 f2 `' F: A布尔代数,3 ^8 H: f. x4 z3 f% S 一种用于编写复合逻辑命题的数学系统。 , t+ e1 [3 }. }增压泵, 7 V, B* W+ C# c从飞机油箱向总油管提供燃油的电动泵。 - W, i* b/ m& l/ Z! B0 s孔探仪, . K$ v, ]5 B1 S: V. T) O' Q9 I1 [7 p5 g# ]' v7 C: y3 P! G# ]! X# t; b0 v( i( Q 动,以指示压( M q, P w* a- O0 d/ F 托架,8 o# Z D5 J% f) f 用于作支撑、装托、或围绕之用。 1 z" t# s1 D* F3 q$ ]刹车能量 P# I/ |8 D2 \2 A" x中断起飞过程中,取决于刹车吸收预定能量之能力的! M, n2 v6 ] B! [) |/ F& V, {- ^5 k- T% @ a 通气装置, 3 j' r0 Q4 d3 ]! {6 S英汉对照民用航空词典B OEING- f& b4 |) ~* m0 X6 y3 w9 v TECHNICAL DICTIONARY 23 . \9 x: o+ J: Q% O1 k* S1 W/ CBUFFET, Vibration of the wings and airframe resulting+ j" d; D* `7 K, P4 C from unsteady airflow over the wing; caused when. z% G/ U3 u) |) ? airspeed is too slow, the bank angle is too steep, or ! B: C$ [: W/ t; b. d" W5 Mirspeed is too fast.9 I6 ~& ]7 {$ A! W0 h* J. G0 b UILT-IN TEST EQUIPMENT, Equipment installed on 3 c' v9 p2 E. n# k. @e airplane and in airplane systems to test the systems. T- U8 V" X: E5 N$ a9 y ithout external test equipment.+ O1 X! R p x UFFET MARGIN, The amount of residual maneuver ( w1 h% X+ e$ \% O7 Tapability present before the onset of buffet.6 U( _% ?: P1 }. _+ g p UG SPEED, A preselecteed speed to be observed; N7 }9 x4 f9 M ]! Q8 x nding sequence. 3 u9 q: P0 m9 V8 H2 Z9 O, nk3 ?/ u* y( O6 G0 v0 Z0 _ ng landing gear operation.+ j& `( I7 w0 }, z 速度太慢或太快,坡度太大,均会引起抖振。 ! R+ y |: E- Y9 y7 B+ [# ^+ `2 j/ g7 C% [自检设备,1 H+ T% F! ?8 ^7 B 安装在飞机和飞机系统中,在无外接检测设备情况下, + v" w5 B2 l* Y [: p% U用于检测系统的设备。 . ?* e4 U( d- n/ `抖振裕度,& g$ l2 o* b" F c 飞机在遭遇抖振之前,剩余机动能力的大小。 ( p7 `# s5 {2 l# \9 q$ z标速度, & J& \8 z6 o" {. T在某些机动飞行过程中,特别是在进近和着陆时,飞机 / W. \+ P* U! R3 d预定速度。' t, [& e3 I2 a5 q _4 m 力装置, s5 d/ x* q4 ?& R, C架工作的一种机械设备(弹簧或减震器)。 7 D- q% U" a. B! ]' W$ ^流条,9 x: l% B5 ? U4 j& d8 s4 U: z7 s 在部件或组件之间传输电、数据、或定时的单一电线或 / w& U! l8 \/ w" ja 8 {/ d" N! w v8 O( J# XB% R0 L, u. y9 v9 x0 U! m6 I5 ~ th. v2 l: G7 {9 h; B7 k w; Y' V& r3 {! i; j" u& r4 ~- i6 u B. Q6 i. A* D J c8 A5 K( o1 \ f7 k( K9 n" `7 r. T+ h B9 P" J7 P) D. T. n- c" I during certain maneuvers, particularly the approach and) z! \- ^- M X8 I# j la $ w ^0 Z8 c( C) B b" L mBULKHEAD, A structural partition in the fuselage or # n; ?! m; `. A# i" Gwing., @3 m1 N; g! S% `5 C' T BUNGEE, A mechanical device (spring or a shoc $ V2 R$ y8 v1 Z" gabsorber) for assisti, \) u! U& T8 q6 H BUS, A single wire or group of wires which transfers$ R1 E* q& l( C9 O: \4 b power, data, or timing between several units or9 D$ c7 Z x3 X3 D( p `0 Q) w modules. ( }* v t7 R0 _; b抖振,+ C$ M# B+ M7 h& w, A: Y 由于机翼上表面的不稳定气流引起的机翼和机体的振 - x/ R! `: z9 H) u) }# O动。飞行 ( d( W6 u. I% \, ^: v, ?, s2 v! J8 a. U3 u3 _/ D 所应保持的: p& q$ ?/ `1 { 壁板式隔框, 9 c, l% g. j$ |3 ]9 E6 T2 ^机身或机翼内一种结构隔板。# ]. O8 _0 q0 @: f# K; \7 \$ |$ {( c1 n$ Z! x2 y% _用于协助起落 6 G( R* [5 @8 U( A. u/ b! x) i2 a. X3 }8 D. y) { ~( o电线组。 - A/ N) p# s5 N, W: l$ i+ H英汉对照民用航空词典B OEING & Z$ } E* y% N1 W5 t ATECHNICAL DICTIONARY 24

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BUS DRUM, A mechanical connection with pulleys z) x7 _& `, ~: t5 i, e* m cables in the control system.! m N/ I8 P4 O+ H and 4 B& T8 S6 N" d% ? il circuits for control and protection of ! J9 v! K5 c5 Y4 m9 w$ S( ~ glectrical alternating current supply to the airplane. 2 k* n7 w' P4 ~% G& Tduct for closing and opening the duct ; a# U( {0 w0 qassage.: k3 z4 F, T1 ~' M% _9 A4 ]( ` UTTOCK LINE, A vertical reference plane along the % U8 D* E2 t, r* D1 j% l8 O hselage for horizontal measurements of the airplane. 2 K& R) s' j8 |7 C- e+ N, u* |9 n接。 & r/ o# ?+ F2 b- R组件,内含控制和保护飞机交流电源的电- c; B5 w- |' N4 P& J, m; |9 x& t" l% N* I, ~作动简控制的转动装置。用来关闭和 7 H$ l) L5 @4 v, ?4 Z% b启管道。' D$ F0 k8 y7 ~ 沿机身走向的垂直参考面,用于飞机的水平测量。$ b( X% j) w' A& J9 v- P4 L BUS PROTECTION PANEL, A module (black box) - n7 n2 q8 W9 ucontaining electrica5 w4 | K/ ?% ~5 x$ x4 j e . Y) B; t4 X# u/ N' W! L+ H6 RBUTTERFLY VALVE, An actuator-operated, rotating ! h* I) x4 w8 U& {" r- z* s/ Ndevice in a % l' q, X/ o0 p m2 W0 T! op - K3 U1 a9 K+ {' i1 F" QB 8 o: |, S0 t* ?fu; f; _, U0 Z1 @3 D 转动鼓轮,2 A. r2 x' |3 A. L# V( j* } 在操纵系统中,具有滑轮和钢索的机械式连 ( _+ }) W4 Y* Y8 E" \汇流条防护板, - n6 e# t# y% I1 l6 G+ @黑匣子式的 L3 B8 d$ o z8 L6 `7 r/ i3 w6 N2 Y9 O# F) V% @. \' B9 G蝶形活门,0 G4 A: ?$ c# \+ \8 R: L 是一个在管道中由5 ^3 H1 P: d1 ]0 y/ P& B4 e5 A# V8 v0 s纵剖线, / s0 }% T5 `, k1 H+ D5 d9 [ N英汉对照民用航空词典B OEING6 H! U: d" I. \7 N6 U3 G& m- ] TECHNICAL DICTIONARY 25$ l; P2 P0 L/ N. q BYPASS VALVE, A valve through which air or fluid will5 w: ?0 S# T8 ~7 j; R- i/ B1 U w flow if the normal flow path is blocked. 5 c; ]1 {0 u+ C3 c) P- X. d' kBYTE, A group or string of binary digits. A byte is ( }* J% G$ v# b. F# _+ nsually eight bits long. 0 [4 j* h% O# t& ?6 L7 M# v; XABIN ALTITUDE, Atmospheric pressure maintained L! g% p$ n% [ithin the cabin, indicated in terms of feet above sea 2 n4 \: z" s! v9 R4 s+ A- XALIBRATE, To repair, adjust, fix or correct the! H7 G2 e* o8 K( ]; ], g' a4 n easuring capabilities of a measuring device. ! Q, R! M! x ~1 fALIBRATED AIRSPEED (CAS), Indicated airspeed & u& s: L* a8 YAS) corrected for position error. ; K* v0 i4 o: G) U* U o. onical. k# [5 F0 o$ R- S! h5 d2 i# p omponents. 0 i+ P" r$ i& b& y ~/ \0 W4 ^1 d4 K% ? 节, - U/ \2 O* Y: [+ L5 m一组或一列二进制数。通常一个字节长8位。0 n7 A+ u3 a7 b! G a2 a1 h+ ` 舱高度, ! h. o2 t5 _& X% @9 ]6 j$ ?( k/ ?* ~座舱内保持的空气压力,以海拔多少英尺表示。. d+ J" O% K* x" O 准,. Y+ Z% E ] G% [8 d 修理,调整,定位或改正测量装置的测量功能。 / [' ]3 v% [4 \* {; j4 B正空速(CAS), . |4 s4 ~1 m! i4 }在修正了位置误差之后的指示空速(IAS)。& r3 b4 L- b [/ a" N" f W 用来移动机件的一种转动装置。 $ V; t8 }$ h3 Z3 Tu2 O& S! ]% [* q C: x, J$ R& G( e$ D g# Y9 V C# R. y& L8 O* r& v w & w* ~& @% y& V2 qlevel. " O5 N# r6 n9 s3 dC ; W7 F. T, O* m& Z3 wm5 j% x7 c4 v0 g5 G C; t5 F9 C* c. p) q1 l0 H (I 9 a3 e1 m8 i! D; I' G0 n% P/ g/ ?CAM, A rotating device for movement of mecha 1 Q3 p! {5 T$ s: w6 j: o$ r* J3 vC( f7 Q' h. Q0 s0 }: |% R I/ [3 l 旁通活门 4 I3 k1 M! Q2 L/ ?气流或液流在正常通道阻塞时所经过的活门。 M7 K! Y+ a1 F+ d3 C8 x! J& o, ~ p. X+ p% A9 n- s2 H+ s% R, ~5 Y! L6 B2 I! j, J6 I3 c% l) j! k: H9 D2 O( E 凸轮, 8 f) b, o0 y* Q$ U2 d1 h英汉对照民用航空词典B + d4 g1 [6 B" LCAM-OUT, An autopilot condition in which the actuator 9 Z" e: h; A, \detent piston is overridden, either manually or by the2 |% C, Y7 P" @ ther autopilot actuator. . L2 A/ A5 { U" W" {/ KAP, SEE - CAPTURE7 E2 `% |1 G& t5 s APACITANCE, The measurement of electrical energy 7 e+ E9 ~: v; a+ J4 Btored in a capacitor (condenser). - G% u V' `7 vAPACITOR, An electrical component of two metal # k' T4 h4 ^: J5 L- xlates separated by a dielectric material, for storing# J7 {* O: n! i8 ]7 @! B lectrical energy.* ~7 D" s2 j! `8 w+ X3 t7 a( G& M% X' r CAPTURE, An autopilot or flight director function to 5 H8 v! A- b" M% Z3 R. vacquire a selected mode.+ E. |9 r! s; j- m' b ~ CARD FILE, A container on the airplane for printed % @; R7 U1 A+ k; p: U9 ]! k) V5 i0 Vcircuit cards.) o1 N' B$ b' t, }$ N# l2 M 一自- X2 ? b w# t1 x! u L 动驾驶舵机所超控。 v; V: k. c' g7 b+ `. K 截获,* P) O6 g9 s; u2 O7 F( d1 E4 n! X 见Capture / w, W2 @% a: S. N/ do $ Q2 [: I( Q- F/ y3 U5 f+ vC 6 h# B$ Z* Z& r7 ^* U, _) W) ]/ BC $ r) |9 M6 N4 o' P7 B1 ^, q% rs ; w0 I. k- Z# Y2 OC" Q' j) g# z& X p 2 G' N# k8 M, R! `e+ C$ J( P; X; ^+ R+ o1 o$ o 凸轮不工作, - \( k$ \1 o. w2 y& E一种自动驾驶状态。此时舵机锁定活塞被人工或另 @# p% f5 j3 A, {% X' `+ Q# c2 G7 L8 w, B/ X3 h电容量, * J' k: T+ j& C- `5 m) f; M电容器内所储存的电能的量度。2 l0 b5 e; S0 F ?9 G5 p" b3 Y9 p9 X 容器,7 t! E7 D% _" u p3 t 两片金属中间用绝缘材料隔开的电器。用以储存电能。5 r. ^( j3 A* |% |" {- [& A" M 截获(CAP),* C+ W: z$ l9 A5 F 自动驾驶仪或飞行指引仪的获取选定方式的功能。 1 d. n7 T; O _% ~* B9 c: n线路板盒,5 w# L* x, `% _5 V 飞机上安装印刷线路板的容器。 7 G( }5 B1 r+ |+ E, |9 s, m6 u# s- d5 }* ~- _, J5 ZOEING3 b: o* _/ L0 v* P) r7 o0 j* g TECHNICAL DICTIONARY 26- L. Y7 i. m7 {- j3 ^ 英汉对照民用航空词典B OEING; G! w J1 }3 k T# `6 w TECHNICAL DICTIONARY 27 T5 W- a' q, m0 _* hCASCADE, Two or more similar circuits or amplifying 2 T5 r& `3 f4 b9 P- U/ h% F* r6 }stages in which the output of one circuit provides the 2 p3 p) m" Q2 J. M. V$ L; a% E; J; oput of the next.0 M2 V2 _# H+ _4 O6 r ASCADE VANE, A vane for turning the engine airflow 2 l- |7 L" j/ \uring operation of thrust reverser./ z: b$ I# J% ? ASE DRAIN, A drain carrying lubricating and cooling8 @; v6 Q' r/ j- Z uid from a hydraulic pump. : P. K. r9 c3 r4 s+ T( G `: qATHODE, The element from which the principal( \4 _3 k7 ^/ J tream of electrons flows. # k: R- x1 |) U/ b7 c: \ATHODE RAY TUBE, An evacuated glass tube with a & Z1 {. s$ v: w! K* YCEILING, The height above the ground or water of the ; x7 q# V) C3 v2 ]5 }4 Ibase of the lowest layer of cloud below 6000 meters 1 N2 S% T Q* y8 f! S+ [, y(20,000 feet) covering more than half the sky.: S- o0 e5 @; Z) l9 ~# b* k9 J. ? 程。该9 V& F) H8 C2 G$ ] 程中,一个电路的输出为下一个电路的输人。 + S5 i8 L+ x" m% h叶栅叶片, R7 f/ N) [: y 在反推工作时,使发动机气流向相反方向流动的叶片。 " P" S3 e* ?! Q* `! h8 ~匣余油管, " o- @6 d+ `# Z" M4 U) o8 W1 ?液压泵多余的润滑液及冷却液的排放口。2 G4 }7 p* E# R7 R 极, ! a. N' ~' @( t电子流流出的极位。 % h' s( H+ m) f% m; v. j; }3 M1 s极射线管, b' c8 w3 d9 W- ~5 s9 u3 _9 L有显象屏幕的真空玻璃管。用于显示信息。& ^& q& S( [9 [' i" W: a 云高(云底高), * q( o7 d o: Y9 D' l4 G6000米(20,000英尺)以下已覆盖一半以上天空的最 # G3 @' f$ a! y c2 c低云层底距离地面或水面的高度。 , l! h7 T+ M: D' q" Ain 9 U/ T& S O6 G0 U5 Y4 UC) d; @) P* v8 }: d3 z5 c% P d + L& H% ^+ {" }' G; bC6 r% E$ ]. F& c) U( i/ m% o fl 3 u5 d& R" }& PC/ O6 f9 w: a) \: P7 g. j/ h s; A" g! Z; k) [' O C ) a1 E$ k; ] j. M7 u1 iviewing screen, used for displaying information. 4 l" P2 ]$ q) V+ p8 {% @级联,/ W+ x6 ]! x6 G6 @* C. N* t 两个或两个以上的类似电路的逐级连接或放大过 |! _' g) t# m! R- {8 ~, r/ Y8 A6 `6 Z7 T3 X- P0 ~* j; a* ?: ^2 X& d3 u6 W3 k( l' e- t4 ]4 D0 J5 g7 a' \$ c5 Z4 D0 x' E% Y% F一个具 7 ?) k* I9 R5 |' J英汉对照民用航空词典B OEING / G; Q, [+ R& ?3 E7 P% nTECHNICAL DICTIONARY 28 4 d/ J& }, @# x, s# J, uCELSIUS, A temperature scale in which zero is the 0 L' o, F, L( d4 e' Pfreezing point of water and 100 is the boiling point of. y% I, G' @6 y) S water. g4 Z+ b7 B. Q% n( ~CENTER OF GRAVITY, The balance point of an object 9 [( J i7 U- g/ J8 x1 L/ G: n' ^+ Or rigid structure expressed in terms of percent Mean 4 B, s& _; X9 u# G+ {0 _+ P& Verodynamic Chord or in inches from a reference point.1 X, z* a" I4 f s5 q ENTERING CAM, A cam for moving a mechanism to a3 E) W8 p% j9 m4 ~ eutral position.( U! J% p6 J2 m* r# A2 s6 _1 P" e2 c IGURATION, A configuration of the . ?; x; {( i: i3 Jircraft approved for operation by the local governing) y8 N; n) C3 i$ V! T gency.) B/ y) y- T: C* @4 V3 K ENTRAL PROCESSING UNIT, In a computer or 6 O$ D8 s& M3 eigital circuit, the section containing the arithmetic and5 W, x e4 F- T& `; _& ^ gic,control, and internal memory circuits.* w3 g; a6 ?8 a5 r# N, f' n ENTRIFUGAL FLOW COMPRESSOR, A type of7 ]: `0 D, f- k: E0 Z" S ompressor in which air is taken into the center of the ) y `3 _- u& c/ x. z9 X8 b( Mpeller and is slung outward centrifugally into a diffuser * x8 T" q" ~6 M7 \7 @1 [7 Fhere it is slowed and pressure is increased. % L( y" d& W' PCG, SEE - CENTER OF GRAVITY 2 n, e$ y& @# o9 M' A构的平衡点,以平均气动力弦的百分比或 ( K" q% w8 S" q: r某一参考点若干英寸来表示。! u# w5 O+ A/ U 中凸轮, 3 ]$ \3 s2 M3 Q将机构移向中立位置的凸轮。 Z0 S4 ^" F' v9 A- d. u 格的装机状态,' g! _8 \5 Q; v9 p 由当地主管单位批准使用的飞机装机状态。 2 p0 j- F i% u中央处理器, , D, H% l# [1 i" ] i计算机或数字电路中含有运算,逻辑,控制和内部存 8 F" ?+ P3 i8 T0 v' S储电路的部分。, H# C: O% X8 E5 T7 J) A: r* x 心式压气机, # H, s; I, |: t" K9 M- O$ m4 Z压气机的一种。当进气到达叶轮中心时,被叶轮离心抛 ) u. G& i g$ |6 B6 c. T进人扩散器。在扩散器中气体流速减慢,压力增加。9 {( M6 H2 T9 v 重心,6 T8 Y, N% R& F6 z. v8 |; F 见Center of Gravity " z7 G7 ^) m0 a. R( So3 {2 T' _9 Z) F# E A6 x) d7 m! p5 J! z' p C 1 y$ z, j; O4 |3 l$ l. \n1 M1 f5 Z1 G" d* e CERTIFIED CONF ) C/ o. w) f5 G5 Ua. J+ f% V3 j& D* e, U a ) n7 Z2 d# N; l* @) aC & j# W1 z% t* z, Z' |/ H/ l' md 0 b( ]& J4 w4 @& q" _2 X& Wlo ) K- r5 f& u" mC9 A2 x6 D4 A, M l S/ G c/ S, i8 v. M& V7 h, J/ D! [, m im ) o; U0 `0 F2 H, zw . r/ L: Q4 o# R g9 C( O! w1 @0 l摄氏度(°C),: [7 q7 Z+ d. {1 C% j3 J W 温度的度量单位。在此单位中,0°C表示水的冰点,2 i* Z6 N0 j5 J$ y. T; b3 Z 100°C表示沸点。9 W/ N4 f ~% O. a" @" t 重心 & T9 W$ ~( N" Q物体或刚性结/ v4 u8 Z4 ?9 G. b+ l) ~* m* @5 d. c9 C6 f) h- k- T; a' j, ^6 g: ]$ k/ }# P+ _8 o. G3 E- _: x$ n9 X! o) x9 U4 P/ W+ Q- a1 ^# y- Z9 R- I英汉对照民用航空词典B OEING/ Z, L. b" z) B" N' ^ TECHNICAL DICTIONARY 29& w2 W- n) |9 I9 K- E: a& i1 i CHANGEOVER, Conversion from one mode to another. 5 }/ R- S7 W" T$ T+ MHARGING VALVE, A valve for supplying air or fluid to , A9 J0 T6 b6 F3 L4 Y' }$ W& A& HHECK VALVE, A valve allowing flow in only one & H8 K1 j+ Z# s& M& X eirection. See Non-Return Valve. 8 w) G6 t( F8 s( m `HECKSUM, In a computer, a summation of digits or $ a, }# C# b' U$ T4 Sits which are primarily used for error detection.% S# Y( n0 \* X8 F J! Y HIP DETECTOR, A magnetic plug in sumps of 7 h$ Q: R* a( E; H! \! obricated components for detection of internal failure of8 B4 w7 [4 A! y. S5 S# k* n e component.2 E& [7 `! q- g* S3 v$ U# r HORD, A structural component of spars or frames. - {4 w; a2 m" W; P/ C) ~添活门, s1 K% F& J, K$ e4 e器充气或加液的活门。 ' s" q+ P* H! C" {; L单向活门, & h! r( y% j9 V2 X" p+ R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# e3 r5 r" v4 W a reservoir. 9 P% a5 _( @; g: s! HC ! {5 p8 A) J$ F+ W8 B# vd % H2 C1 {$ d$ M) F1 xC 2 y4 U% M! k# l) s, V8 R! Tb2 ~2 J* X1 S( o2 S' M9 m6 T/ F C $ H0 m* z! _, ~ ^8 a" |lu 0 H; m' o" S& u7 }th% o. X) m% G9 ?7 _: i+ Y% Z& V C& D3 c8 H4 \. W- V/ S 转换, 3 o7 o; W0 i5 S8 I8 T5 c7 k由一个方式转换到另一个方式。 9 a9 c- [# ^& ^$ r: O% n: z9 J+ B' R# w0 h 用来向储存" p4 W$ \& [/ a' I( S- e5 D3 v" X" [总和校验,8 P0 L$ i) s/ P9 A 计算机中,把那些用来探错误的数宇或位数的总和进/ k* r( q) t! k) L5 `3 a- _) ? 求和计算。 ) e2 a! }" P: o+ s属碎屑探测器, ) g! o9 r+ h" C7 ?! y装在被润滑的部件滑油回油管路上的磁性塞子。用来探3 |4 M& u( v$ k 部件内部有无损坏。; u/ G# Y/ d/ _: w0 z 弦, . u B+ w; ]4 `* I+ S- n- m梁或框架的结构部件。 + O5 a9 g$ h; `" @+ p# F' @# o" ?' a/ E q- \9 V( @/ r5 c8 @) z+ m# n! [# ?& M$ ]4 T! W# Q& y! s/ ] G8 h$ c3 X6 j; A0 }, I3 f2 r2 J5 P S$ w. t9 x* d+ Q英汉对照民用航空词典B OEING 5 B( ?( x T' U/ p0 ~$ S uTECHNICAL DICTIONARY 30/ z6 N" \4 ]. o CIRCUIT, A closed path through which current flows 4 b9 z7 k) g7 x! eource. 3 |/ n1 K3 p& k" [1 p! V+ y0 iIRCUIT BREAKER, A device that automatically : x7 F# W* N5 J, R I# ^, K8 meactivate the system.# ^& q8 T, u7 B7 ]5 f lear of all non-frangible objects which 9 c3 }5 ^9 {" d; ]' @2 @ay be used as takeoff distance available when 4 l2 J, E* ~7 I- y/ Lalculating a takeoff weight. ( p& d7 L1 ^+ V$ e* e; E* }3 Tr water under the control of the appropriate/ V* ]5 Q6 h, e, U4 l uthority,selected or prepared as a suitable area over 5 \8 C. U& U4 O6 [, a) Phich an aeroplane may make a portion of its initial - d9 Y9 B1 u* J$ i* Jlimb to a specified height." n% f( l1 I2 x increasing. + U0 A0 V1 ^; v0 v- Y* Ysed3 G; |" [* u6 W0 u. {+ l LOCK SIGNAL, A continuous string of pulses used for 1 M) b. ? L0 P' s( R! b+ y, F+ h( o开关,5 n; ^. h. }. q 故障情况下自动中断电流以保护线路不受过电损8 N7 L7 ~9 q% K 体障碍物的区域。在计+ h. f$ `; ^' F 起飞重量时该区域可作为可用起飞距离。 ' l+ s" m" v1 U- u是在有关当局管辖的地面或水域内一个界限明确的长0 f+ f% A* E/ D* L. z" r0 c 形区域。在这个选定的合适区域内,飞机可完成初始爬 ; P4 I$ I) ^6 q% J3 F' A的一部分,上升到一个指定高度。 : ^% E7 ~& D( R+ \+ I0 X飞机高度不断增加的飞行阶段。6 s2 O1 g3 M4 x# g! G 钟脉冲, - g) `3 ]: e) a) `4 v步的连续脉冲信号串。1 A; P& l' {. ]! I& S. t8 d- ~) |$ v; P' E& x from a source, through various components, and back0 Y0 d" m2 n+ X2 }# J; l) \ to the s ) ~4 f2 u; g! ~1 X# l( VC 8 W g. S" G. b) zinterrupts the flow of electricity (current) during fault" N8 ?+ G, N2 s, X1 [# w$ \ condition to protect wiring from excess current. Circuit , {- P9 N4 \ S3 E* v% Y5 Mbreakers are also used as a means to manually 1 p" F6 K7 A- O. |" j7 P. }d! o! B# G$ M# s6 O. O CLEARWAY 1, An area beyond the takeoff end of the 3 \ w0 X2 l1 X) A* `, W' prunway which is c; U$ O) {0 u6 a m 0 _5 ^+ k( e( T! d' F: fc 2 Z$ U8 f, v6 v5 r7 ECLEARWAY 2, A defined rectangular area on the2 M% N4 C- ?* @ ground o / N2 u. b8 n4 _2 J3 ]: O" ma# X0 V& h$ s0 O$ } w; [/ Y" T0 R9 E' p8 ~, O: f c ) `9 d5 a+ ]. N; Q( Y1 i# b3 PCLIMB, Phase of flight where the altitude is ! ^1 ?6 |/ x6 `1 sCLIMB LIMIT WEIGHT, Maximum takeoff weight ba 4 `+ b7 [9 I+ }on a minimum climb gradient with one engine 3 C4 F/ V( S# N4 [8 w+ g! Hinoperative. * I: D! @# Z3 y1 }0 aC- A6 V) s3 ~. w J3 p! k synchronization.( ^! s& C, u" C! z/ u# a& U, y 电路,, [+ N! A/ E6 s5 X- ~% j 一个闭合的回路。电流由源头流出,经过各个元件流回 / ? S: A0 K# f; D7 i2 f源头。 ' |+ h: x7 W7 m& l; H8 }: O7 b* T; w& f+ v4 ^ J 能在 $ x! r s8 Y( U6 j# S& d) ~坏的装置。跳开关也可用于人工使系统无效。 X: _9 a/ K5 C k一号净空道,# o! Z! e7 Q3 N! f 是跑道起飞端以外,不含任何刚, a# q# w/ }5 T+ [" d, H( m' G6 v1 m. P: a& d9 D6 ] 二号净空道, ! d1 B. \8 y. T! @0 n) k3 [) z. O/ s. _/ j0 l" F, w+ v, j" d9 n3 a1 N5 m! q( j% ?7 i爬升,5 E0 F9 G" ^8 t# S 爬升限重,' \- V( D' { ? m& x1 x b 取决于由一台发动机工作时的最低爬升梯度的最大起 1 ^* z6 I7 p5 l7 v! b" Y- W. z2 q u飞重量。 h2 h, i! C# Z: M& k) k" l& u3 e$ r: w% x. d 用于同. n8 W" H5 l* x! V* [: F& p7 q9 X 英汉对照民用航空词典B OEING0 v6 t) d$ H6 ~ TECHNICAL DICTIONARY 31 o/ D9 F8 e9 ], \! H! GCOALESCER, A device in the water separator for" L5 D3 J* m' b/ b: M ollecting moisture from the cold air. # j+ a2 a7 E3 `2 q, ^+ O' I& Ln antenna with a receiver or transmitter.' A, Q J0 ~8 l1 A# X! z he cable has an inner conductor and an outer: P, p( S; e6 Z: X; e, v rounded shield. 7 D# o; x5 x" s' m0 z5 y) eting one inside the 3 |) d$ I( m3 L5 @9 Y$ w0 pther for rotating the low and high pressure' {. S( ?& w3 Q, } D- `: _ ompressors by the low and high pressure engine3 @, K5 f% {- D( a rbines. . C4 c- ?: r& i$ D# j% ^OMBUSTION CHAMBER, A part of an engine for) K! _" D: |8 C0 i' B0 r urning fuel in the air supplied by the compressor." w1 p, Q- A/ @9 E' W V1 n 置。 " }* h+ S' f& s Y" Z" d) B3 S射机的电缆。电缆$ O+ `0 c+ P( D6 H9 m 中心导体和外层的屏蔽所组成。/ c; q2 I* W* m. a8 z- y 两个套在一起旋转的轴。用于使发动机低压和高压涡轮 ) J& t9 `+ c6 |+ g6 u) J+ a别带动低压和高压压气机。# I# v l+ w {# _: A" _2 s" j 烧室, ! j/ i7 Q+ ?8 k0 m! d! m3 ?$ I发动机的一部分。用来使燃油和压气机所提供的空气相' _1 `, y7 Y1 J1 `( s 合而燃烧。

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发表于 2008-12-24 21:38:35 |只看该作者
c . s% a- h3 }1 O7 O6 T% ]/ qCOAXIAL CABLE, An electrical cable usually" R4 ]* P6 K. ^& H# ^8 o* N connecting a % V& L7 {7 b: n- W$ T/ B* PT! A( L; {% e5 }! x7 Y- e1 f3 _# B4 \ g 2 R0 o3 C! D! }, s" e* ]COAXIAL SHAFT, Two shafts rota ( h2 ~& }$ a# \" J8 T: M% ]o 7 s5 z- m& z. U: l$ {+ \0 kc 9 O6 i& C5 O: o4 m* E' ytu C: f7 `+ [$ b7 W) j2 J( B/ S% HC % _7 C% C7 a* e! n" @; r* J( ]% sb! @( [4 u# p3 ] e 凝聚器, . [7 g* u: c t. w- Z水分离器内收集冷空气中水份的装1 T7 v3 H, E+ t/ P. G4 i% c4 g/ h 同轴电缆,! j/ J2 u. M% q6 @# C: A0 _& i 一种通常用来联接天线与接收机或发 % a) A8 L! `1 W. @6 |3 |! D% N0 ? 同心轴, ( ~, V* |4 T/ p b' V4 I7 X8 k- J5 u+ ?- ~( O& {# f3 Y0 R+ ^6 e( ~( W& m( h 英汉对照民用航空词典B OEING- H. Y7 t; o" H' ?3 X; S TECHNICAL DICTIONARY 32 % F9 ^7 m8 J- X1 k( t3 p- I0 o6 oCOMMAND BAR, A flight director pitch or roll comman: ` X% Z7 @: t indication. : O6 v! d% O! Nd" F) a+ V) ^+ ]6 _# D OMPANY ROUTE, A route flown by the airplane# z3 X( B, Q2 x( a0 E V OMPASS LOCATOR, A low power, low or medium5 S+ Y# s7 w$ }* n% ~ equency (L/MF) radio beacon usually installed in * W; r) l' T2 ^3 k U& c5 lonjunction with the outer or middle marker of an0 s* ^3 {: k! }4 ~% a9 P) v tor (LOM), A compass & N' F; w) d3 u. e. l7 s; p3 clocator installed in conjunction with the outer& d; k2 c) Q5 M8 `. ~$ a7 k marker of an instrument landing system. ! V# w& Y5 I) O5 _9 rss8 G8 D @: X, M( J le . |9 b7 E- {, b) r' \OMPENSATION, To offset, balance, or counteract.* v# p* e/ C; ?1 G6 B$ U OMPENSATOR, A dual capacitor for changing the fuel 3 w& u7 \) i1 {# zaging circuit capacitance due to changes in fuel6 @, e. [) w. g! r/ W9 w, c ~" G ensity. T7 m$ |! F8 a9 s2 w$ R: N/ n- hOMPOSITE MATERIALS, Non-metallic materials used : y0 g z Y2 t2 I) O& Rr airplane construction. Fiberglass, Nomex, Kevlar, $ a- q/ @: W+ o: j4 r6 s" k$ nraphite Epoxy are composite materials. - `6 I& P6 S, L! C" H- F; N) s司航路,: h8 U7 {; J" [7 m 在飞行管理计算机数据库内由航空公司飞行 % T/ ~2 ^# ?/ Q( z盘定位台, 1 O8 r2 _& D7 ^( s与仪表着陆进近系统的远距或中距指点标配套安装的 + _8 I1 \4 Q% {6 S) `* e; T功率、低频、或中频无线电信标装置(低功率NDB台)。3 _$ ?6 j1 O, R 程序中用来导航。+ i! K2 D( r% P* l3 q& }% M; A' k2 v 1.远台,5 X. C/ d a+ D4 X 与仪表着陆进近系统的远指点标配套安装的罗 % p1 f$ b) S7 L$ r7 ]$ S9 \1 y盘信标台(NDB)。- `# u# O% {* o/ A' J. Z( l% i$ z2 |/ y 偿, + Q5 [/ [6 | m9 y抵消、平衡、或中和。 3 f! {& J% l2 _) |5 X. }( U# ]# U5 I偿器," @( {% \! Y, |: o( Y9 j- k 在燃油计量电路中,用来改变电路上的电容,以与燃 ! r3 Z8 c- U3 x& k/ A2 V密度改变所引起的电容改变相抗衡的双电容器。' W5 T z8 v- U& s3 K 合材料, 0 ` |$ n; q- l1 N4 d; o用于飞机制造的非金属材料。如纤维玻璃,Nomex,: o6 j2 m& H8 b9 u2 f. y/ g) b 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
C9 m5 {/ }9 S! E1 R operator that is normally stored in the flight$ [5 |( P3 l1 z3 p8 q* q4 u7 Y management computer's data base.& P* c; Z" W% r* R: z7 ^8 k! h C ( g+ n, x$ D/ ^9 g, n; [; rfr 9 M% x: K& {. V% r$ T3 m8 @c 2 \: ?' q4 G7 ]4 J; z$ H6 Rinstrument landing system (ILS). It can be used for 4 |6 t/ O3 v' Z* }- W2 N5 q4 Vnavigation as authorized in the approach procedure. $ [ T, `/ ~9 J$ M+ Q2 T1. Outer Compass Loca 0 y' n+ l* i& \6 f. ^2. Middle Compass Locator (LMM), A compa ; |* X1 E% a3 S2 S' i- P6 r! _5 Wlocator installed in conjunction with the midd 5 R6 Q& K- R* [: P, j( N6 Gmarker of an instrument landing system. * Z% B) j/ b' z1 i/ f: ?2 vC2 V( w: R; k' G9 ^! D) X C3 h0 B9 U, v7 u9 `6 S9 m( A: i: } g $ ?" G+ `) U) ]d- U$ z, ~: F: ?. @6 M C) @9 L. c" H0 C; a fo ! C' Z6 B9 L# |g' V Z( z2 Z6 x& Q. A2 T _ 指令杆, ) E% b( `( C/ Q, `- U飞行指引仪俯仰或坡度的指令显示。; ]# b& o- V4 i( c8 U% T+ z( z4 c9 T, Q8 t/ a: M( ? 通常储存 + N8 r5 A# b, X7 j% z7 ^5 C的航路。: N) w( X; c' ]2 k& Y5 m( r3 _ M, O& {. J8 A! Z( N/ l6 l# b8 F$ C" `+ {4 K. s 经认可后在进近- X7 y2 M! W) S7 }6 H 2.中台,& o- ^. S9 u7 Y! a. z' E. P/ @ 与仪表着陆进近系统的中指点标配套安装的罗 7 |, b; E+ T) m- T/ S$ C: ?盘定位台(NDB)。1 G3 _' k5 i0 J9 [1 D8 l# @- Q. [5 P: d6 |3 I& m5 ^# P& A9 t3 k! }3 w( i( x$ w2 C% v) ], s- P* C+ W. A, u6 d$ k v& b, ]) F1 n5 R7 s K. p4 {, i# G& u 英汉对照民用航空词典B OEING 1 |- N0 O& u% ]! M/ T ZTECHNICAL DICTIONARY 33 o! C( [! W) x$ S6 C by. c0 u- R ^3 o# K or increasing air/ R* @; J: z" R8 K1 ]$ o ressure and temperature before the air enters the ! @0 o I; z$ d8 M+ mombustion chamber, Low pressure compressor - front- S4 X% n; q+ H* \3 |. ]3 u% G ection of compressor, High pressure compressor- rear 7 N2 u$ m9 ^7 r$ m- M- w qOMPRESSOR STALL, An event that occurs when' p/ X/ z3 n& t. i* }" S* Z) `: u" } ere is a complete stoppage of air or reversal of air flow5 U3 h4 N( n4 Q* A! R3 W COMPRESSOR SURGE, SEE - COMPRESSOR( c( _6 s1 s v% X/ \: b0 ? STALL COMPUTED AIRSPEED, Indicated airspeed v- G# ?# Z# c) @corrected for the static source error. & m9 |5 T a* i% N7 F的机械轴来驱. f! ?0 u: M/ Q ,用来增加吸进空气之压力和温度,以供燃烧室使用。3 a7 \: ]5 K7 y; N( x% a 压压气机—压气机的前段,高压压气机—压气机的后 ! m6 w( p: |+ e0 }7 z+ ]7 |1 P* i9 v! p0 L气机失速, 7 W# Z2 B: k6 \3 L当气流完全停止或通过压气机时气流方向逆反的一种 * |/ w/ p& s* m% i压气机喘振,% N, X8 u+ G1 p4 l 见Compressor Stall9 O# T( Y9 ] x COMPRESSOR, A rotating part of an engine driven ; Y' y, _0 |9 L% C+ O( A+ b6 `! Pa mechanical shaft from the turbines f) r3 D- e- D3 e( V$ b% I p ) Z2 P0 `1 Z( l5 S2 _+ wc& Z" H$ T- a5 ]+ t$ W O s & D8 g' A# L2 T. j$ ~+ b' f8 fsection of compressor.: z/ P2 v K& e8 o- c2 I8 f C ' B2 E: v _0 q! w% }! l+ B5 h$ c+ Nth 5 g6 |+ w0 x* l( X9 m$ A& sthrough the compressor.: Q) {8 k9 a4 _7 ^ 压气机,, g3 \: y6 P8 L# j8 L* X 发动机内的一个旋转部件。由与涡轮相连 6 V5 ^, n- B& h6 u3 l/ E5 {0 D- ?3 G1 M" {7 ^- ~& q. L' ] t6 w# C G# f# x8 |! v& ]0 _* G0 W" h3 C2 U* [; |1 z g, O现象。' ^ J8 E. j, \+ w3 v, r; x9 _; |9 v+ U1 m* L. B ]0 H 计算空速, : c( {1 S5 p9 m2 w修正了静态源误差后的指示空速。3 O, {+ s) B7 s5 R 英汉对照民用航空词典B OEING ; l7 S9 J ~" C+ S3 TTECHNICAL 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- K( K( [6 P+ d% N7 w( G operations, manipulates data, and makes decisions.& e$ j9 S* V# g ditioning 1 @% n2 n- v1 pthe air and the0 @$ w+ J. V, e1 Z8 j& d7 h frigerant or moisture vapor is changed into a liquid. " J5 z% S4 Z3 V, cine8 ^- o; y$ O- S ONFIGURATION, The position of flight controls,1 J& {* Y9 b$ ~3 B$ i missing which9 e3 C0 g6 v# ]' w1 G5 s& y may affect the aerodynamic performance of the 9 v- }9 e& b' h# U: M9 B" |+ nairplane. , g1 f5 e' ?. d置。 $ v5 j3 x6 m2 S* [1 C& T5 o中能使热能散发到空气中,以及使冷冻剂或湿 + o" u1 p. T& t' R7 `7 g: q& t转变为液体的部件。 8 @, {! k: {4 ~; |连接到飞机结构上。 % [$ ^3 \. g- |1 J' Z6 s态, ! K( Z- K8 W3 c% y5 z4 c8 l定飞行阶段中,飞行操纵面,起落架等的位置。 ) G0 C( v' W; o r, ]2 C% L% X+ {), 4 [( u3 k* b( o$ J/ Q5 x受到影响。& h6 C1 x. m5 _ CONDENSER, The component in an air con 3 q$ l0 T6 f; |, F. J' Q2 P- |; zsystem where heat energy is given to 0 L' U/ q8 q$ Xre $ B* k9 a9 @. @& LCONE BOLT, A bolt in the shape of a cone for eng4 }( _% u+ \& {1 u& b3 c attachment to the airplane structure. 1 R; p: D) i, i7 ^; C6 C% B6 I" N& RC : Y2 l- ]9 F4 r4 T( olanding gear, etc., for a particular phase of flight, e.g.,4 Z* e* D: b7 E3 c8 }* q8 R Takeoff Configuration, Landing Configuration, etc. ( B$ N3 A$ n* J# ]* _CONFIGURATION DEVIATION LIST (CDL), Appendix , a3 P, A7 a3 @0 `6 ?+ Qin the Airplane Flight Manual (AFM) allowing operation; T- W( d Y4 S of the airplane with certain airframe parts 4 [; V6 h0 ^: v( i( T7 z# C计算机,3 G! `* ]* O) u* |6 J4 ^ 能作算数运算,数据操纵,和决策的装 8 o3 D$ k7 O D1 z! _( O冷凝器,$ J" f% q5 y. I( y, f$ R 空调系统 * R* o8 [- h" ^; j6 ` s% q6 [ U% ~1 N8 H3 f1 g锥形螺栓, . _, F+ R! h! k! Z外形是锥形的螺栓,用以将发动机) e6 o+ y/ g# m8 d% a) t; G4 o) J+ a# x' A4 q) q) f 在某一特 ! ~6 s3 H8 C' v1 B) a& h6 t) L如起飞形态,着陆形态等。 9 o- ~& Y5 r) `8 o0 `8 d7 \缺件单(CDL 8 w x3 _6 u" i1 A: \飞机飞行手册的附录所开列的飞机上某些零件的清单。2 `) D" n! i$ [9 ^! v 在缺少这类零件时,可以飞行但气动性能可能 * o1 d2 w0 X2 p英汉对照民用航空词典B OEING # Z+ ^& X( s9 z% c0 `3 B" \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 0 j, B: x* r! l% K& y! O( z+ l8 Lcomponent for changing variable engine gearbox speed2 g- O: U$ F2 M: M$ c$ A ONTROL AXES, The three axes of the airplane which Q3 x$ Q4 W7 L re perpendicular to each other and pass through the 0 G1 Y: s: q- f* L- M( R6 Jenter of gravity of the airplane. $ a8 A* C$ ]; _. wPitch axis - Horizontal or lateral axis, passes through, j0 ^) r# Z3 n7 ~: z- ? the airplane from one side to the other - & |- C5 `& O# e% a5 Jnose up and nose down control is by: M$ `: D9 z* F elevators (and stabilizer for trim).2 l8 X: y6 s1 C Roll axis - Longitudinal axis, passes through the$ i8 v j/ b: O* m' ?! f- k8 d5 X airplane from front to rear - wing up and ' t p1 i$ P0 o3 e4 u$ [wing down control is by ailerons and ( l7 E6 S1 a0 a$ U- h4 `6 N7 uflight spoilers. ( Q+ _ }: h6 J- C. P2 FYaw axis - Vertical axis, passes through the" e( {3 T+ c9 [- T' F airplane from top to bottom - left and , p' h1 e$ i7 V. y/ Y6 O' U* I/ mright control is by rudder. 4 c2 C/ w1 L" y5 i1 ^+ ~# }置,$ ]; G/ X' `& W' n" q7 H0 Q# x 制轴,! d. o+ D& W: J+ R z) \ 通过飞机重心互相垂直的三个轴。 / \1 q3 s( F& y) x% t: U3 @! |, @俯仰轴—又称水平轴或横轴。由飞机的一侧通向另 z/ G4 g/ N# B3 i% i O# t) r: ? 侧。飞机绕此轴转动即造成机首的俯与仰 1 W/ N1 d, u7 A% p6 {" ^6 L俯仰控制是由升降舵来达成的,水平安定, ^! H, b; ^4 k( }' d% [1 n' G 则为配平之用。 * T* h7 T; L7 ^, D1 n4 H横滚轴—又称纵轴。由飞机的前部通向后部。机翼 * g% O4 r; D! \1 V+ ]下运动由副翼和飞行扰流板控制。4 b; D* i/ X. ^ Z, J2 ~+ b3 z 偏航轴—又称垂直轴。由机身上方通向下方。飞机4 [4 d7 d1 C. R" K 此轴转动即造成机首之左右运动,此一运. o4 U+ P+ {8 y9 B0 }. j1 t8 R 由方向舵控制。 ^: Z# t5 M6 D- J6 r9 O0 {to constant speed to drive the electrical power. ' P# H) E6 X- L |0 fC1 e; y7 S, `. }; j, M- T a 7 B$ F$ I0 U6 D9 L/ N( b* sc 2 [6 \* ?9 B. g" P3 y0 v恒速驱动装. ?" j3 e/ n9 K6 Z6 O6 u/ U 将发动机齿轮箱的可变转速转变为恒速以驱动电源的 : U0 A7 j/ K' z. O' Q @液压机械式部件。 2 e, Z6 [# D! L5 L( {% V; x/ m" B% W. z/ \, [% G* N8 ]& R2 w1 n" `& K2 B+ }. [/ ?' Z9 v' z/ g$ M8 n4 I: s& N) \9 T& I% W* H9 k; e& Z6 z& f, u* p$ o' r! N8 B! V. x# f& Y英汉对照民用航空词典B OEING ; S7 b# T& Z4 _TECHNICAL DICTIONARY 36 + Z: k+ n* d" K" b- ?CONTROL COLUMN, A mechanical component used8 e+ n% k8 `$ V& ?/ W rs / _4 B- J% Z2 i0 N; j, _6 P- Ynd elevators.( ^- k* y. v% j7 y ONTROL SURFACE, Moveable panels on wings and- c/ G+ t0 R' `' L& { il for movement of airplane on pitch, roll and yaw axes. 1 D* v8 V) I) Y% ?7 G! hONTROL TAB, SEE - BALANCE TAB% t) P$ a" v: D# F5 U ONTROL AREA, A controlled airspace extending& w# |9 f' H" s* |. b pwards from a specified limit above the earth. # G- j+ u2 m& b$ T# wONTROL ZONE, A controlled airspace extending 1 [( q, s* }! D3 t" R$ @pwards from the surface of the earth to a specified ' @7 k6 G: P4 E. @7 Q5 zpper limit., P. M' @/ z J4 z' N7 S& T is* V" Q; J, l6 u" n o IFR flights and to VFR flights in accordance ! b2 V' I( U8 |' D8 E& h; o$ Awith the airspace classification. 8 p1 R( _* h0 c e# c4 p* M机械部# m& G1 Z2 s) V) X2 J7 G# s, l3 K2 I' @& r 操纵面, : P) A5 u6 y' d机翼和机尾上的可动面板,用以操纵飞机俯仰,坡度,, E2 a6 [; c! {. V9 e6 k 和偏航运动。7 v$ L6 }. _; q$ }+ n1 I 操纵片," u2 Z0 U& \$ {+ E* L 见“平衡片”Balance Tab

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10#
发表于 2008-12-24 21:40:09 |只看该作者
by the flight crew for operation of ailerons, flight spoile 7 c. _# f7 H7 b) Z' I2 La # f' \: Q4 c* a) iC ! t( e+ _, L/ {. C: sta# f! h# N; N8 d+ ^! X0 D+ _9 n C % T/ n1 I( ^3 Q/ q9 _5 M3 A: SC , v$ X+ `8 ?" k h- v, qu" A, T" ^& n( c C # I" z6 g t* J F {4 O- su 9 n! p% h' |9 O0 Su/ X, Q7 y; A8 `4 P CONTROLLED AIRSPACE, An airspace of defined f/ b: b# H+ |# t+ c; l d( \ dimensions within which air traffic control service % c2 v1 H0 F$ F3 m7 Vprovided t ; ` G) c8 z: c& U) [3 s, U8 z t驾驶杆, 1 q, K- z. G( `9 ?2 U" b! q飞行员用来操纵副翼、飞行扰流板和升降舵的( n5 B+ ]( \, M* _" t% T% o, q% [& b9 c7 x- ]# V5 f q5 F* I: ^6 @4 ?" q8 x% f" |9 c+ R管制区域, W+ t6 A2 s- R5 S3 T& r5 \高于地面的指定极限以上的受管制的空域。$ b G' r7 p# c- o X 制范围, Q( U( z5 t' G6 H$ c由地面到指定的高度以内的受管制的空域。8 u% D1 b$ K& J: E 一个范围明确的空域。在该空域内,仪表飞行规则飞行) Q. S" O+ u2 b2 T- C 和目视飞行规则飞行有空中交通管制服务。; s' B) H, `6 G4 N$ D# }% E, S0 f& O0 Z7 \& P 受管制空域,; }/ H9 W! M( h+ u0 X0 M q/ n; ` 英汉对照民用航空词典B OEING . G- `6 K% t) a qTECHNICAL DICTIONARY 37 ( _- B. L8 K% l( R2 x. ?4 o5 s$ jCONVERSION, To change into another form. 9 e% c4 _* e- E9 aCOORDINATES, The intersection of lines of reference, , L7 u( M/ c$ P3 ksually expressed in degrees/minutes/tenths of minutes ) y( }7 d0 l2 o: x7 y Gf latitude and longitude, used to determine position or % D* X/ K9 N4 qCO6 ` y1 }; e& q6 J2 p destruction of th ( l; p2 k! c0 S6 Ichemical conta 9 b, M4 |# ]( u) R/ X3 g9 CCOWL, A remo 3 J6 N; M' g9 T& z( z8 ?9 F3 _for access to th ' v) x3 a. v. W( U ~5 S+ oFa 7 T. A9 ~0 e x( PNose Cowl - Front section of the nacelle for air inlet [7 j+ n8 J" X) s0 t: xto the engine. 4 B! b( t2 l, X' p# X; YSide Cowl - Cover around the sides of the engine.' ]# o7 _& |; I' c* C Thrust Reverser Cowl - Cover around the core % r: t2 y1 d$ Z: x: usection.+ f6 ]5 d Z, p' v' _2 S6 r. F: ? Translating Cowl -The moveable outer portion of the 3 @% M8 }7 J) U6 ^# |thrust reverser cowl which is- Q- F9 ^6 X6 P2 I1 u operated during reverse thrust. ) H/ V. X0 o* H! Q, O7 {标, ! w7 V, t/ @0 g7 @/ c6 W3 O" g& [基准线的相交点。一般以经纬度的度/分/十分之一分7 ` p! M7 W V 读数来确定位置和方位。. j# e* H1 X- l 腐蚀 / r3 \0 r) R0 Q9 q动机外部可拆除的罩子。发动机上的构件必须要取下: [! Z n* R: @! j' P: q4 G 流罩后,才能够到。 " k$ [$ ?: \9 q+ C1 a2 {" u' j" H% Y机的短舱的前段。 - u, ]* K4 e3 ~# B1 k% ^侧整流罩一发动机两侧的罩子。& l" j( I( n! a5 f/ K: P 反推整流罩一发动机主体外的罩子。 & {1 h3 G7 c( I( A移动整流罩一反推整流罩外可移动的部份,在反推工% x( l L7 E8 Y6 j 作时使用。 - O! a4 P$ ^) e; W# Du6 O" S* S2 \1 F. s& H( `, r0 Z o 6 k; c0 m; b: blocation.) d. `- n- |5 j3 m2 @( A RROSION, A chemical action which causes gradual + V) n" P4 q r4 [' f" m- `e surface of a metal by oxidation or& _/ L; o3 k- n mination.: Z* p+ k; ~; d v0 P) B vable cover around the engine sections " P) c+ c9 t5 W" m9 n+ Te components on the engine. 1 H) H; z# d4 O9 R( Dn Cowl - Cover around the fan section.8 } @' P p0 h9 y. z& p 转换,% b- {( a/ \( {4 ^ 改换到另一个方式。! f! Y9 x' R8 N2 m# \: ?& q( e9 o, C. a S$ @" p$ P) W3 }( g% L9 u# t# W. d8 ~$ R& F; {& v7 D {0 L& A 氧化或化学污染造成金属表面逐渐破坏的化学反应。3 S: m( T* n$ O9 w9 \ 发动机整流罩,2 s6 k( _8 b W; @" X& \) }" r' [ \' s& X, j0 B. n0 \; G% p+ ^; a L- | 扇整流罩一风扇外围的罩子。 9 y, P5 M* u: w7 a- x前整流罩一引导空气进人发动9 R6 @! o& |9 V 英汉对照民用航空词典B OEING% `3 N, O% \8 A$ L" Z# o# @ TECHNICAL DICTIONARY 381 n( F8 O3 j$ K9 m, @! F- S. p6 D! b CPU, SEE - CENTRAL PROCESSING UNIT& u3 |$ v4 F; G. B$ n7 K CROSS TRACK, At 90 degrees from the desired track & s- \1 I) t* N, }f the airplane. For example, cross track distance is the/ {. Z& L! f( S& _( ]: D- x istance from the desired track measured 90 degrees ; y8 Y# Y- q0 L* {3 |) q; ^om the desired track. 3 o$ f, e* ^6 `5 }% GROSS-CHANNEL, Electrical wire(s) connected from }; j% @6 e5 i, H+ J7 q7 R; y4 O3 ` ne system to another like system, for example, FCC" |+ L# ]! V* S$ C7 u2 @. x Q " to FCC "B". A& d/ R" N& u% c' h8 S n adjacent engine or one on the other side. ( W- x. U4 t) U" _" O/ E; Ll crossfeed/ E& c$ ^+ ?# Z anifold for fuel flow from one side of the airplane to the6 {8 k! g, D3 N+ Z ther side.5 g |9 e8 o, [, c re ' d# {/ L) q4 Y7 Q' W* \# zRUISE ALTITUDE, An altitude or flight level T' g! @! ~+ y0 r" A$ K' A8 h3 A+ w3 k* Q" v- e. fo" t0 V! e2 ~; G d % i6 ]' U( t" A1 b- R$ P& [" @fr 0 i7 f5 |& n. `$ w$ RC ! m! q4 G( `6 K( }- j" |. Eo3 l" ]4 u! \9 E6 \' l4 p$ |- [: k "A $ o1 s4 y% v3 y/ MCROSSFEED, An interconnection between fuel . ?' C' ]& l( p+ f7 F9 [manifolds for fuel flow from one side of the airplane to6 g; R! h0 ?/ W8 X* x0 N7 L- B a7 ?5 {* l0 W& [1 l; H# g! B* b CROSSFEED VALVE, A valve in the fue1 ?, i4 V t& r2 p/ W7 U m : ?9 r/ K0 p' }! W( lo6 M4 B1 N' Q/ h3 s, p3 { CRT, SEE - CATHODE RAY TUBE5 Q5 J/ E2 w4 t' h" j9 C CRUISE, Phase of flight where altitude and speed a ' d0 N7 n5 L( Z4 Cbasically constant.0 @/ ]4 s/ ^% g C7 v% f: V4 b4 I4 a0 P maintained during enroute level flight. 6 U) H" S1 n. v% y中央处理器 / s& P+ S* a7 O9 N. W2 e4 i见Central Processing Unit.5 I5 z5 r! H, A) ]+ q# t+ K 交叉航迹(XTK), - @" e% h2 C9 J! _% v与飞机预计航迹成90°角的航迹。例如,交叉航迹距离- p _* Q+ N6 k 是用与预计航迹成90°角量取的到预计航迹的距离。 " \3 S8 }; a$ Z$ p通道跨接, 0 N7 P) |+ B+ P# v" N# ~电线由一个系统接到另一个类似系统。例如:由FCC t2 w/ q6 A/ V$ F2 x3 b+ e9 d6 u “A” 3 T1 ?. e7 H! G6 D0 W( \接到FCC“B”.- V, I, B% C B4 ^% b( \7 [/ i 机身另一侧的发动机。; v' z$ m1 ?$ o% X9 z" l+ y 于使燃油从飞机的一侧 9 K) E: J) ?4 N6 {! |6 R向另一侧。 + V- M6 q2 N5 h& {) `) { j见Cathode Ray Tube4 h) I* }# H9 O5 s6 v: M7 ]* R. Q* ? 交输, * t& q0 |3 G' J) E% {3 l8 L$ W( ]% }6 z燃油支管之间的交连设备。可使燃油从飞机一侧流向邻 - q, e9 i; {1 `$ M# H近的发动机或在 - F q- D* m2 v# z5 u交输活门, : q- k# W$ B$ O' z* u; l燃油交输支管内的一个活门。用6 I6 W0 m/ G3 F0 L$ c& d$ J ~4 ^$ u$ y" Q7 Q4 s5 q) X 阴极射线管, 5 v, x/ U- v5 G& k C/ }+ a. - \ f9 C9 w3 w2 }- J6 _阶段。 ) A: T4 J: R l& b航高度, 0 H. [6 _5 m4 X2 R& L飞行期间,飞机所保持的高度或飞行高( H; k6 U4 B8 R2 U) U1 B& n2 G9 E 巡航, + b5 B% _6 H, p) ?. l飞机的高度和速度基本上没有什么变化的飞行% z3 E' L* n' k v$ z% [# }7 \/ R5 G' {: V2 m) O5 z在航线上水平0 x0 u, K; R+ R: I. c0 ~ 度层。 9 F# Y6 [3 R, \7 A7 N1 w英汉对照民用航空词典B OEING' U+ E8 G, b+ ]; X! X TECHNICAL DICTIONARY 39 , ?% o/ v" t, d/ [4 u& t: yCSD, SEE - CONSTANT SPEED DRIVE / K; M* O" {% Z4 B! y8 M9 O& f3 O8 SCURE, A chemical change which takes place in a resin: _0 k7 N, ]/ ^ and fiber based component causing it to solidify.6 I$ F" z4 F3 w+ y CYCLE, A complete series of events that take place# e6 Q) ~) o2 a1 S gularly normally in a continual sequence. z. w3 L; j( @AMPER, A device for slowing down or limiting & v/ ~* t3 T" F+ |, rDASHPOT A mechanical damper for slowing down) C+ H w" `" S ovement by restricting fluid flow. 1 F; Y) `/ ~8 _% v6 `D1 v/ p! _5 S# M ATA BASE, Stored information which is used as the , G' `0 p) h$ K- z& C1 Y0 mba . B# D# I5 \7 `DATA BUS, A conductor over which digital data is . ; U" Q3 h$ |2 M& c9 h! E _transmitted. 0 I% f- E: }0 eDECELERATION, To decrease in velocity.1 \: S9 {% }5 A" N 装置,1 A' D/ z8 l% u0 L rive3 s$ E3 S' _# S$ g" ~% F2 y$ B8 u* d re2 S5 i) ]- O+ L' t; e0 g9 J U# ?4 U D 8 D" n7 O3 g4 Y; c6 W! }: `3 D1 [D, M6 {6 N7 x) j. a: b5 b K# | movement. 5 G3 S& ?+ f* I- e+ Wm% F2 y; g l7 T; _: o ATA, Another name for information.9 Z3 Q( G5 s& @! ~4 J4 j D( r/ q. k7 D) c6 @" f5 T sis for computation. * Q1 R1 J6 K- g5 }( v恒速驱动* h5 h- b* l0 F$ V, U7 K; x( X4 \ 见Constant Speed D . 5 D9 C3 V% }* i期," P0 k; q, l: p- W: M 不断重复发生的事件的一个完整系列。4 w% S; S4 l& O' d% E' \& T2 W 尼器, ! _' _: ?6 A* s, ?; `! W& Q/ ?4 {慢的一种机构。/ U0 M& w5 r. G p* u& L) S/ c7 [2 ^3 {( u* w用限制液体流动的方法以减慢物体运动的机械式阻0 N1 j: f7 k$ x U& z% d; k F- a, r$ E9 k. t8 c) X( T! R! d& T: j料的另一名称。5 a+ J+ r3 e6 a/ M/ H; H+ }8 x6 j 据库, 3 V1 z; q# p: b$ Q0 U% a数据总线, & V, L7 N' R6 B5 `一条或一对导线,用来传输数字信息的通道。 * o2 m4 _8 z& e; K, x/ _, l/ w; e减速,' e# ?' ?; i% k* T' J ]. k 速度随时间的递减量。 / j* T- X$ t4 `7 L固化,7 B) J) P5 F& y. s 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) ]5 R4 j+ V6 H' z6 g9 a" J& y$ W* Z' O; A$ |$ A* M9 a- H 用来使运动减( q4 j$ T9 X8 [: T0 e6 D- ~ 冲器," }# y" P) G- U( O6 W& I* t( D 器。 ( q( V3 x1 r' D1 ?据,0 P2 f: t' @! m, c$ ?7 n; H3 {/ i$ X1 v/ q1 J) ?. e- F; x l: ]储存起来以便在计算时使用的资料。 - m" ` D k# c' h7 S9 f英汉对照民用航空词典B OEING2 p' w) u. r: n" L: U9 x8 g TECHNICAL DICTIONARY 40 . c& ?0 j& Z4 k+ g; k" x* S- v" |0 @DECIBEL (db), A unit of gain derived by computing the ) ~& j& l6 l# G1 q- Ntio of input power to output power. 1 O# Q8 ]: u" NECISION ALTITUDE/HEIGHT (DA/H), A specified: ~/ q- D% @% p; p7 N ltitude or height (A/H) in the precision approach at , j; v1 n" Y- y# m7 Xhich a missed approach must be initiated if the: |: l* Z' C e: I, x# Z ECISION HEIGHT (DH) 1, With respect to the 0 D0 ?& |1 A6 Kproach or 0 d/ k/ x( K: Rexecute a missed approach. ) r& Q' {( G$ t9 {' [0 yproach to trigger the decision of either* A9 ]. D4 d: l6 T2 P nding or go-around.5 j7 `4 U* u" G1 A1 \2 h ECOMPRESSION, The loss of internal aircraft air / n+ J0 @, n% R) I/ \2 hressure.& H" m5 j1 U+ o7 q. ? E-ENERGIZE, To turn off or cause to not operate.* b$ P, X6 k9 G5 j: A- A1 w$ g rom the tanks 9 C4 W1 \: i- N9 `- cusing airplane fuel pumps or external suction. . X1 O3 o/ U# R; B* H算的一个增量单位。分贝 ( W1 e! t* T( F$ |3 s. c常表示两个声音信号或电力信号在功率或强度方面的 . Q# |/ T6 i- z4 |9 D; L对差别的单位,相当于两个水平的比率的常用对数的十! m, q: ^: e% H7 N: @7 d( B 断高度/高(DA/H), 1 d+ z7 |# l( I5 P/ P* X8 n8 s在继续进近必需的目视参考没有建立的情况下开始复8 }4 h% q3 u: G5 l' A2 P 的精密进近中的一个指定高度或高(A/H)。 ) Z- `" h8 [5 y: }% Q$ x断高(DH)1, / L1 F# {" U; X3 F n+ a5 a操纵而论,指在使用仪表着陆系统或精密着陆雷 2 N% u, _6 W+ p: d- Z+ B生继续着陆还是复飞决定的高。 ; \% c% }/ |5 o! @飞机失去内部空气压力。; G/ j' S8 s+ |7 Z4 y' } 开, * c X: @/ [5 k% H+ U. s关断或使不工作。* i0 z: O8 x4 Y' ] 机的油泵或外部的吸油装置将燃油从燃油箱排0 d8 e* i. D \' H6 e. [: k 出的方法。 + S7 b% R. i9 f* k) @ra 6 y8 j+ j' N# k0 SD8 j+ T4 K9 W- x ?5 o a, _+ t" n3 q3 b6 P2 b% H w . U8 k3 N( c5 p3 B$ K( Y9 prequired visual reference to continue the approach has# a: T- j G' L+ H0 u9 f not been established. 4 H5 D7 c+ s0 r8 V- K- FD9 J% N3 I5 w" K% e# k2 \# A8 w operation of aircraft, means the height at which a , B( t0 P- Z; h! Y Mdecision must be made, during an ILS or PAR( S' U' T2 `* ]& O instrument approach, to either continue the ap' y, S+ `2 I1 s# S3 A to $ m& V2 D$ p4 h1 k$ UDECISION HEIGHT (DH) 2, An altitude used during a+ @( L( T4 k9 ^- w precision ap $ s1 v" S' E9 ?la ; i+ j% o7 s: QD! s* P: p2 d1 C8 [ p ( P$ r$ @5 \" p$ X4 lD( s/ u* B# s' k DEFUEL, A method for removing fuel f* {7 b; Q1 v; [# \1 P \. W 分贝, ! W: q1 R4 @& F以输人与输出功率的比率来推" ^9 J$ T5 Z6 `2 ~* t/ Y( F6 H9 _5 h8 z0 x& E/ T# I6 P1 P6 e9 W N0 o7 u! M1 K) L) `1 v- {/ E& [. k7 a, e; b5 L4 y% P' U3 A, _( r4 p6 M6 ?$ j8 \6 @ 就飞机 1 A* l" |/ Y1 u- r$ v$ {3 E3 k达引导进近时,必须要作出的是继续进近,还是中断进场* d7 d7 o. O- [ 复飞决定时的高。, k3 t1 V3 F$ O( f! v# K 决断高(DH)2, ' G* X. Z" D! i精密进近时产# N3 ?& z9 N3 x 失压, " j& d" d( `' ~5 T, I$ U; F: N3 d- g/ {9 h; M 排油,8 I8 x. y+ w* G 用飞 $ m( w: {6 o& A, V英汉对照民用航空词典B OEING/ r) |( I( o/ {1 a% s TECHNICAL DICTIONARY 41! d- G1 r' R. b DEFUELING VALVE, A valve in the fuel system for9 ?( l7 N$ h" N4 Q+ u5 ~' a' `* o" @ efueling the tanks and for transferring fuel between the" [) ^) V- N! c& a+ o3 X9 A* I6 p0 T E-ICING, Removing ice after it has formed on aircraft.8 w; U8 D2 u, o Change or difference.& @; F0 |7 Y' O/ v EPARTURE CONTROL, A function of an approach" p5 _& Z$ R3 N; e' h4 M N ontrol facility providing air traffic control service for( J5 B/ d4 y2 i. L eparting IFR and, under certain conditions, VFR: |( ^0 Y5 s! m* m6 V EMODULATION, The process of retrieving information, @6 I q$ |% c$ `. G& E" ] carrier voltage.; K1 d& d. B) D' _) i. j ation. : N1 R5 o" r- Zlic 9 R6 y) J1 w+ H8 Zcreasing hydraulic reservoir air pressure to |% @0 T H2 n7 G, X, N% z, b$ L mbient pressure. 7 F4 M" {9 N* ~箱排油和在燃油箱之间 5 c# B7 X! u. |& d送燃油。: r3 S7 \# N( } 冰, ! C1 W4 j) r$ Z除去已凝结在飞机上的冰。9 `- F! C |1 O' ?" l5 p& {1 w: Q3 U& R 删去或取消。9 B1 Q4 |) E& Q4 W$ i4 ^6 x4 |: r 量, h$ _! U" g1 N& j* M 变化或差异。. q. R$ b5 {5 p, }# V7 \7 o 场控制,; [- t* P; P U E2 A r5 p1 n 给用仪表飞行规则离场,和在某种情况下用目视飞行7 j- j" K* ?# _9 m( p 则离场的飞机提供空中交通管制服务的进近管制设施8 m& j, U- J0 B' p9 g Z" O! }: R1 ]# i# A 调, . m& F- f# X. g电压中获得调制电压的处理过程。 - g1 T3 F0 O) U Y0 L, x& y% z环境 3 e- J3 [. D: W0 V3 Y力相同的活门。2 e) x8 B/ F1 Q2 q d1 e5 K: O( c! G+ D% K tanks. 4 }2 a7 |3 n+ v) ~D- _1 ^1 Q3 u6 v9 C: T: ?9 V3 e5 K. r- A DELETE, To remove or cancel.4 A; z- q" F# {4 | DELTA, 5 R9 `2 t& t" g) M* w }D% b/ [: G2 P) `* X% g c) s; C/ C8 Y1 g: t3 ^) r. S, ] d! }% \0 H5 U4 t: e aircraft.4 D: h, K# {7 T5 v, r D# K2 j1 z1 X% h* m (modulation) voltage from a modulated& V' m: x q! A4 y; q( p DEMODULATOR, A device or circuit which performs # |' t2 L C5 _* ?0 ~. b0 O! Nthe process of demodul* q% S! l, ]8 ^2 b1 z* [$ C, O DEPRESSURIZATION VALVE, A valve in the hydrau9 e. {3 V: L5 G- t w% ^) `* R system for de2 Z' \, @4 l; J" l a 3 q& I' U/ s6 q, f排油活门, / ?" {# K+ o2 c1 V6 ?- Z燃油系统中的活门。用以为燃油, P% O4 g' q# R3 Z5 G9 |" t5 M0 Q V/ g+ b8 P* G6 p; w1 g X" \" Q$ ~删除,$ }* V* n3 x7 R6 l; \# |) d A% q p( D, _ P' C0 I3 O7 [+ L8 @* K! i) y; N0 ^1 l的一种功能 ) n2 t( R* T+ ^/ u, c* W- v1 n" s4 ?3 }1 z 从载波 " G& A) [ r- m9 I; T0 [# p解调器, + A9 V' P j+ p% t! h7 K完成解调过程的装置或电路。 5 l# C: `9 f! R* Z; e: G减压阀, 4 q6 G# ?* K4 k) h# ^ D7 d: ?7 z在液压系统中,将液压油箱空气压力减至与周围% v i A4 D. m2 {* V2 T! ~; k7 h. ~6 V# z' o- o) W 英汉对照民用航空词典B OEING: U( f' i; \9 k; ^3 l+ a+ s TECHNICAL DICTIONARY 42. s1 c' C* v! g) k DESCENT, Phase of flight where altitude is decreasing. 7 Y' B# ]. ^) b, _ETAILED FLIGHT PLANNING, The calculation of fuel2 x$ v7 ?5 W* b nd required for a trip by considering each phase of 0 ]6 `3 y0 E$ \3 Uight (climb, cruise, descent, reserves).8 ^: E3 |/ B" Z& \& [ L al or5 I! i, d+ y$ e ETENT SOLENOID, An electrical solenoid used for ' ?# o; e4 c- p# L, x% F2 H4 mt.8 Y8 h' B. [1 \( V' s; W specified course or ) g9 W; ^9 p0 {$ J& ^; \# x4 brocedure. 5 Q Z: [2 t* Ke. $ g x5 s4 d6 V飞行计划,% g2 F4 }+ r* N 将航班中的每个阶段(如爬升,巡航,下降,备降)都 T3 S( U$ p+ h/ y- @ 人考虑,来计算该航班所需要的燃油量。 3 q+ K7 \: ~: f2 K" d" X用来感应情况之正常与否的电气装置。2 N6 e: f1 u* j 定电磁线圈, & K% b1 M3 ^5 f$ Q* n出接通的电磁线圈。! Z) v- H0 h d! D 差,4 E |6 T0 ^! } 与指定的航道或程序之差。& g7 L2 V) F" f# `$ B! c 用气压或液压操作的活门机构中的柔性部件。$ v8 L* }6 Q) d$ w! ?% _ D" ~* ?; _4 k4 s! T4 j! K! I; C a 0 S# D5 L5 V$ W, G$ c' g8 a3 Rfl: v4 P; m/ O8 n+ ^) j4 H% y DETECTOR, An electrical device for sensing norm + w1 q; G' n3 U F' b6 [9 C4 rabnormal conditions.2 O; h. O, {3 V8 ]$ g! C D8 y- h5 V; G% p, F' L; M controlling the engagement of the actuator outpu3 K7 V7 h/ e6 s/ ~( S* D DEVIATION, To change from a + {! Q. Y |6 S& b. P' z& @/ Y6 A2 jp & W. e/ d8 Y# ?5 ?; g# HDIAPHRAGM, A flexible part for operating a valve , B0 g+ n# S. Q* O# Nmechanism by pressur* \* V; _' o! j2 p 下降,5 w7 D* R( [# y9 A6 F* A 飞机高度不断降低的飞行阶段。% ?: W" A7 G" a( f7 Z- Y 详细/ h8 n& _5 N/ h0 A# s. Y4 p- Q* X% x# n探测器,0 O2 j4 A2 o7 z4 s3 Q: Y. j6 C8 ]. m用于控制作动器输$ {# b; w8 m5 X! ]) f7 u3 C" Y" G9 F- C" V/ \隔膜,7 R" w+ Q: @; q6 n4 f/ C0 N 英汉对照民用航空词典B OEING2 z" k' i* ~7 c2 L4 J TECHNICAL DICTIONARY 43. U) I7 A& f/ T! S7 P" } DIELECTRIC, A material which does not conduct5 I$ O5 B5 z* C2 e, a, p& X electricity and used between the plates of a capacitor - c) K0 M0 \/ [' S(condenser). ; }& F3 `2 W+ p o! Inother pressure in the same system, measured in - @! ^5 l) r' C5 _ounds per square inch differential (psid).) |- r& C) h: r IFFUSER, A part of an engine between the T2 c% c* \6 o# D" Y0 [- nompressor and combustion chamber for reducing the ' w: a/ b. f6 e2 Q) h) z& }" u4 a; rair pressure.- n2 m% C' e6 g* o igh $ t ~0 F7 _' o6 ?pulses.: k$ {2 G0 S! I: f+ g. H ignal that is a close approximation of the original+ q d" [3 h/ _2 M) n2 u ignal.5 i# ^; V) b, y" P IHEDRAL, The angle between the wing reference - n: N: y, {- z2 B- g) P* I ?lane and water line.8 N7 i$ I8 {6 j3 Y/ w. l4 J* f 的压力,以每平方英寸 ' M- `7 r% O; T0 q: V% Z9 G: y5 d少磅压差计算(psid)。6 ^$ @9 x; F/ p, Y 散器, & ^ Q1 O" D6 u2 ]; @) r$ R0 ]发动机内压气机和燃烧室间的一个部件,用来降低空" I: y8 B. X, R) X* n! X; Y 增高空气压力。 P8 j- R$ q1 n' {换, 0 f8 P; g* N g1 l8 \. ]' r1 F2 q的连续可 , @0 k0 x6 B& X# Y. |(模拟)信号的处理过程。$ u8 M8 i4 U! E1 T0 z8 q$ A! [ ] 反角, 9 p8 u- J$ [ L! J) N- `机翼基准面与水线之间的夹角。# j( n Q* a: ?( g' `, B DIFFERENTIAL PRESSURE, Pressure relative to & S+ _9 d! s% [5 |. u) r( Z# Ja0 {5 b: h( T2 a: \ p & K# ~& p; D a/ K0 s$ Y5 qD9 p( Z3 S# e* P. L2 U* g: f c 6 m( M: [0 ^2 X4 r5 S) [( \/ a& pairflow speed and increasing the - Q5 E9 D+ T4 i+ JDIGITAL, Digital refers to a signal whose amplitude 8 m) o$ K, L$ Y7 Y1 | m eremains constant for a finite period of time. Digital- O& x6 _' f# o. \3 I& [: ]/ N signals are commonly represented as a series of h $ A4 ]; ]' H: ~# eand low * d. `+ V+ f( A! eDIGITAL-TO-ANALOG, The process of converting a & N$ q4 `. V/ g+ pdigital signal (binary) to a continuously variable (analog) 7 O8 h, e. }; R* S: Ds ! y5 `( |3 T- ~1 Z8 n% y$ r& fs * M& Q) @8 D4 G! Y0 Q) zD ( C9 Q- W5 R: K' B+ Up1 A, s4 u! K5 X7 s4 H- n% I. Z 电介质, : |! w7 r! F2 x! f$ u5 n2 ~ o一种用于电容器板之间的不导电的材料。 - x6 V: E2 C; z' W8 _* ]/ k压差, $ O' ~$ q! b$ x' V, p; l0 y# e相对于同一系统内另一个压力# R+ f, Z7 S2 W) s7 x# K2 P: A* n+ b G2 ]9 R- u6 L2 k) C5 }+ o+ F+ N4 J1 f) R5 Z& G$ h( [3 R 气流速并: O" V: j3 f! m3 d- Q& r$ j. c0 s 数字式,4 P) ]0 b8 f# G2 { ?# E 指一种信号。该信号在一定的时间内,振幅保持不变。 s, a! ?$ n/ y0 g" z, {( U 通常由一系列的高低脉冲表示。 1 g4 ~4 {/ k3 v$ t数一模转 ' V" i# t! e6 ?. [% f将数字信号(二进制)转换成与原信号相似 9 o" N3 V' K: Z% W+ o) B+ }# U2 b/ Z. g% [, x0 H' S+ \: C. z4 {! B/ p1 Q" ~ 英汉对照民用航空词典B OEING # z" {6 r/ T/ BTECHNICAL DICTIONARY 449 o1 Z, z. r6 l DILUTER DEMAND REGULATOR, A component in the$ F: O) c, h6 P7 o \# q! N3 x crew oxygen system which mixes air and oxygen and8 T2 O Y3 V6 k# r) ?9 ~- Q' q upplies constant oxygen pressure even if there are0 c, _/ |6 K# g8 o: y hanges in ambient cockpit pressure. 5 x; G5 q$ H7 CIM, A word value of light. For light control devices - dim % |, `( J" ?" z" _* X0 E+ cthe opposite of bright. & Q; o- n) }0 P6 ` t# Q8 pIODE, A device which allows electronic current to flow! U5 w* f& a; l8 V$ g# D5 b% L% K only one direction - e4 s7 u% t: l8 g, ]8 z- Zuid in a reservoir.( R( Z' e7 d+ [ o DIRECT, Straight line flight between two navigational 2 N' C( M, p! [+ _: S: A7 raids, fixes, points or any combination thereof. When + l. C$ l7 }! l& K& d8 Kused by pilots in describing off-airway routes, points ; V7 Z4 |* g9 A& wdefining direct route segments become compulsory4 b, d# l% p6 o4 S( F z4 G reporting points unless the aircraft is under radar) @7 ?! S4 b* O control. 7 M* K& h4 d2 d; f( ?节器, 2 A/ Q8 l/ o: T0 V将空气和氧气混合, " ?( K9 r1 t3 K! Z9 n4 J* i' b使驾驶舱环境压力改变,它也能提供恒定的氧气压力。8 @& _+ O' o3 x$ Z* k: _$ f G+ P, j- s- X 一个形容光线亮度的词。对于灯光控制装置,暗的反9 X# a. D% v; D- e2 x 词是亮。 W0 d" G- p% L# U, R' L; C, @ 极管,& j+ `# K" J. x" _: r 只允许电流向一个方向流动的电子装置。 / E$ }& A1 c0 F3 ]4 M8 M器内液体的量。 : I3 i5 c5 ~# ^$ N3 L直飞, ! c1 v* c4 P& u2 s' J2 r. P两个导航台,定位点,导航点,或任何的组合之间的直 ' a6 g( b$ `! h线飞行。在被飞行员用于描述偏置航路时,除了在雷达控 1 j4 t/ ^; v2 z! ?制的情况下,确定直线航段的导航点成为必报点。$ o3 k" ]% }9 s! E$ Q s4 r3 D, G4 X: ]( {" Q) e8 I- `7 Q0 Y c + K% q( x) ~2 z8 C9 UD / x E+ W+ C# _! ?: J( D( }0 Dis w$ @2 g3 `/ A% K+ f% T D 1 n" g+ x, i- j6 x7 k5 Xin7 L- e; U& y( D DIPSTICK, A calibrated rod or stick for measuring a0 B6 b9 x! @0 R, z4 E9 _( k quantity of fl$ z7 t2 ~( g. y6 c! h 稀释氧调% y* |: I/ m; S0 y% c5 b7 F 驾驶舱氧气系统中的一个部件,它 # M+ i/ u; e9 ^# \/ B8 r& d- C% S9 `5 J9 m8 J5 A, h4 X5 U: t5 T* z3 j8 E3 c; s2 Q: j- M1 s) ]$ O. R0 o& B+ V. j! D3 L. } 量尺,8 J% a a& q4 t) _/ i 校准过的棒或尺,用于测定蓄液 # n: @; B' A9 |/ p英汉对照民用航空词典B OEING 8 }! x, ?3 g3 _7 zTECHNICAL DICTIONARY 45

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