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英汉对照民用航空词典 [复制链接]

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21#
发表于 2008-12-24 21:46:35 |只看该作者
FLARE, A maneuver to transition the airplane fro/ |. y$ T/ F$ Z( C: |8 j a 4 {/ ~+ Q: d8 N5 t0 q6 g; @% rFLIGHT CONTROLS, Hinged moveable surfaces o9 Z$ Q, V& Z" M! S4 e wings, horizontal stabilizer and vertical sta4 \- Y% r% O9 T( U* C, E2 s OEING( i% J5 c8 U- @0 d' l TECHNICAL DICTIONARY 62 7 T: ?* g0 D2 b F& La ) m$ p7 S6 r4 P3 E4 O- w: ?8 Z7 po ' G8 \/ n& ~- A; S襟翼速度计划, `! Y# C. R! c9 X3 \6 `: [ 提供各个襟翼位置的推荐机动飞行速度,此计划以VREF . ]& N$ l3 j& R' X' w加增量为基准。9 D0 L5 d7 a7 r/ Z, {7 I 拉平,/ S" b9 }) |0 l& { 一种将飞机从进近过渡到在 7 K. M: q0 h; H' R) U4 [3 X飞行操纵 6 t1 K& ]' ~; e) u( E2 H铰连在机翼,水平尾翼和垂直尾翼上的可动 ' L1 r- `) O- ]( o, e+ @8 W! G9 Z% X英汉对照民用航空词典B OEING

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发表于 2008-12-24 21:46:54 |只看该作者
TECHNICAL DICTIONARY 63 # a, a2 I4 L, Z: a5 ?/ {' j( c$ DFLIGHT DIRECTOR POP-UP (FDS), The automatic R4 B5 B3 y# v* K display of flight director commands with flight direc$ q0 j' Y( |! n# _7 @6 ] switches in off position.9 X% l7 \$ j5 @4 i/ J% S tor 0 s# y" g! \: A2 {" ^/ J% DLIGHT INFORMATION REGION (FIR,UIR), An$ a2 a$ X% c& T! Z FLIGHT LEVEL (FL), A level of constant atmospheric5 c! c+ x0 E( i: @% c' K; g pressure related to a reference datum of 29.92 inches of$ f$ W' `. q* [& d" s0 q e- h mercury. Each is stated in three digits that represents % E% m7 J! ^* W" C0 b8 W! |, Yhundreds of feet. For example, flight level 250 ! C. z" B( k8 k( Frepresents a pressure altitude of 25,000 feet.% W& g9 z& N4 \8 K) _ FLIGHT MANAGEMENT COMPUTER (FMC), An $ M, |2 h$ F! B9 m7 ~0 C- jairplane computer used for navigational, guidance, and& L1 Y; E) f9 x1 @) K' s3 q" ~+ V performance computations. - Z! A! {. t. o2 S* NLIGHT MODE ANNUNCIATOR, A display or part of a( Z: R3 j. Z, d0 h& t8 T isplay that shows the autoflight mode of operation. p+ g) c- f5 X' t/ z+ ?LIGHT PLAN, Specified information relating to the / ?9 H7 T; o. Ytended flight of an aircraft, field orally or in writing with / d3 a O" Z- x7 R( ln ATC facility. 5 g7 I+ s/ x( Q( z! Y" m, DLIGHT PROFILE, A description of the flight which * B. M* p8 k, f5 I' E2 i: wpecifies the climb, cruise and descent altitudes and) ?, w8 R2 r4 M! R$ ]# X4 F6 \ peeds to be flown./ P) r, j% n& a$ a 限定的空域。6 V" h4 @( F1 y! X( E, Z9 p" v 高度层(FL),. K4 {. Y/ F6 s- C2 j! E) I 相对于29.92英寸汞柱参考数据的气压恒定的高) |2 f3 \+ P$ W/ x* l+ E! j 每层均以三位数表示,一百英尺为单位。如FL 2 ! t% O3 c. q7 G/ ?3 Y) t% F( k压力高度为25000英尺。; p* [5 w% D. [# n( |) f; t: c 飞行管理计算机(FMC),* D0 {& d" h1 d \# O# l' b; [ 用于导航,指引,和性能计算的飞机计算机。$ \6 W4 Q! b' x5 W1 ~4 n 飞行方式信号牌, * z* Q3 h; f! \+ h$ Z+ U" m行方式的显示或部份显示。) F( C ~( t$ s. c" m 飞行计划, : W: w; H8 B( S# S6 ?向空中交通管制作的口头或书面报告。内含与航班有关; q: `+ v8 {: ^$ y R 的详细资料。1 z m0 l" V# P 飞行剖面, 3 `4 b# m7 I8 |9 U# _4 X对一个航班的描述。详细指明爬升,巡航和下降所飞的 , I" ~) u2 h9 k2 E高度和速度。7 q% @* h) a% D3 L, G' d6 @! t' U F

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发表于 2008-12-24 21:47:03 |只看该作者
airspace of defined dimensions within which Flight . V i* E" d: J6 H2 ] x0 ?( n6 KInformation Service and Alerting Service are provided. , P% D1 I6 y) |2 c8 j' f, }8 O0 F3 rF; E! ?: l. [6 J; |# l d 6 \3 c2 v% E* J2 ~ F+ v7 @0 xF/ n( p) ~( j0 w6 C7 n/ B8 O, j. Z in) b$ w, M) T/ K) A& {2 g/ l a + u* d9 i1 s- h7 v2 @+ M, CF 7 r% V8 g4 B; N) e0 L3 Vs* b" G& g4 ~0 O" B+ k. J+ e' p" @ s( \( j4 k( p! S, f 飞行指引仪自动显示(FDS),. y6 R/ O3 s6 c4 f 当飞行指引仪的开关处于关断的位置时,自动显示的飞 4 d ?; e( w, s% u行指令。5 }% ^1 ^/ a a, d6 B 飞航情报区(FIR,UIR),& V3 V2 p' ^0 F7 E 一个有飞行资料服务和警告服务的范围 ( S/ `2 L5 f- {) h8 k7 J$ t1 n度层。' k7 L# x" F' W7 U; ? 50表示) z( A, [8 h3 u9 ]- @ 显示自动飞 * N- O( K% w; R1 M; B! d$ I英汉对照民用航空词典B OEING k- Q% {* H" ]$ N- cTECHNICAL DICTIONARY 64 & G$ a9 o. ^$ k G) r9 a7 P+ C- LFLIGHT SPOILER, See Spoiler.4 f4 ]; Z: N8 }$ t% h LOAT SWITCH, An electrical switch which opens or ( T7 w2 X+ z; Y- P9 Hloses an electrical circuit depending on fluid quantity in2 N7 R2 a1 Y' N' `2 l e reservoir.* Z2 O9 k' G6 Y, s9 y' `6 j$ Y: \) l* T LIGHT TRAINING DEVICE: Any device having a full. s! ~. `( j# o& ~ cale replace of instruments, flight deck area or an; x: E7 Z. _/ N* k* j3 Z* D9 h+ s3 h nclosed airplane cockpit includes the equipment and; n2 r0 y% ^ z' Z! D+ ~5 ~" C" ` rograms necessary to represent the airplane in ground/ ~ ~( E8 _& c- a0 L# W nd flight conditions.- H& v$ y. V/ U" C# @; }" g LOAT VALVE, A valve in a fluid reservoir which opens$ c( |) Q4 B- Z0 B# ]6 U& x nd closes an inlet or outlet depending on fluid level. . i5 e1 Z$ f5 I+ [* R/ R7 uLOWMETER, An electrical transmitter for measuring8 `* n" V* ]+ X9 \+ I6 B the engine. ! A# [8 b5 P( t# I3 c% KLUORESCENT LIGHT, A light emitted by a gas filled$ b3 W& e9 n5 _8 I' S- O 飞行扰流板,- [; P& h, c& m" b0 @4 z0 } 见Spoiler. ; P3 y# ]' Y9 f. H3 ]浮子电门,) ^4 `# q) T& k 根据贮液箱内液体的量来接通或断开电路的一种电器 " K o- [$ }) n2 h1 C) @. j. L开关。 8 [# }. ?$ j" M& b5 u3 j" K& p飞行培训设备,1 V6 G6 S; V6 Q( p/ K8 |1 F 仿仪表、驾驶舱区、或封闭驾驶舱的任何设施仿真装置。1 c, b# f+ L0 k0 [" B+ x 包括可体现飞机地面和空中状态的设备和程序。 a' }6 e; p) x# y% O0 w 浮子活门, + i/ {& B1 L6 M+ b装在贮液箱内,根据液面的高低来开启和关闭进口或出 4 ] G- r, S$ w6 d- c口的活门。 " E* O; A |5 a4 t* z! w/ r" K1 K流量表,# U/ x! P' [3 b$ W/ z4 n 用来量度流向发动机的燃油流率的电传感器。4 Y+ S* T. `# N0 n9 Z- j 萤光,0 N/ Z1 R, `1 E* v 由一种特制的充气管所发出的光。1 |/ K0 q; }% F, f0 z! ]0 I& B F 4 H5 ~) ]- q7 m) Cc# L" s/ g/ k8 A8 G# i- b1 C: O th 6 H+ t' p1 e- K# M" S8 u; ]F ( ]2 w K; Z/ v; M' `6 }) s/ y: Ls / C, G3 A/ ~# o8 i Z7 V5 Xe" F$ [* {+ L. R+ \' Q p + w/ _% l8 t% C! _+ l2 @6 ?5 `a 9 d' N* ?" q; S/ A% b2 i+ RF# O4 N3 E- c; A9 C& S, A3 ^ a / K, t" {% K) {2 e( dF) u- S u/ f y, W3 V4 o: e! Y$ r* d the fuel flow to$ l$ E7 [: }& c4 Y) f0 ? F7 j# g( F, |8 |- u tube., m5 z2 y! V( |) m1 f 英汉对照民用航空词典B OEING 3 Q7 X0 B* P6 g: V: R7 _- yTECHNICAL DICTIONARY 65 ( |9 ]; c7 D0 c O9 ^FMC, SEE - FLIGHT MANAGEMENT COMPUTER$ z) v+ w" ]& J: J* j) v! O FOD, SEE - FOREIGN OBJECT DAMAGE # N9 U9 W' r9 ?ORCE BALANCE VALVE, A valve controlled by the, o+ P! O4 p; M5 i OREIGN, Offside; opposite side. . R3 y% O- p/ fOREIGN OBJECT DAMAGE, Internal engine damage1 \+ m( p% A- {% w ue to objects entering the engine air inlet.. f! P5 ]: G9 E: W# X# ?* }3 l RM, SEE - FAULT REPORTING MANUAL, _+ n% L' |$ H6 @ UEL CONSERVATION, The activity of planning flight- d5 e, k0 h- c; m+ R7 S ltitudes and cruise speeds so as to minimize fuel 4 h! W- v$ ~& w/ {% o- r, l( monsumption.9 B: L+ X9 @" V. i. W; I* T9 W: a UEL CONTROL UNIT (FCU), A component on the& e* G; k) b! A2 [# y1 k ngine for controlling fuel flow for starting and engine/ C8 B. Q4 P \5 H F ( I% z4 W1 U: ^+ a6 s/ ufeel computer in the elevator system for hydraulic ( Z/ i6 }$ S: ]2 @+ l& C0 Ypressure supply to the elevator actuator.& `- G/ x- W# I- H. ] t F9 c) Z( L5 `$ D: \; [6 h$ k F( s( Q$ d3 {8 S0 I6 } d + u$ L# p7 f( NF! S: i# Q3 f$ F* J E* @. l F ! B+ _. T$ u) i( ba 9 E" n3 K% [$ d; F7 _c " R3 e( f! Y8 m5 m) NF5 H9 y; O8 n" F [. G3 g e1 G! D% J" f, k$ ^! P6 \1 G operation. " r7 v8 D# ]5 ]# X D- U飞行管理计算机,4 p: n# G; x" G" Y+ V1 U6 H 见Flight Management Computer. ' | q9 U3 a0 M9 {/ T外来物损坏, n( \# F; w5 p* O: } eign Object Damage" A; |, i* O$ i2 f H/ \$ @: Q1 ` 见For . ; u/ z/ ?' `- b6 I5 Z# E2 _平衡活门,* j) G1 p6 L( p8 \' I' @# S 内的感觉计算机控制的活门,用来向升降 d% Z3 h! v( }: S 外面的, 4 i; M0 u& M7 Z) b另一边的,对面的。3 X; a2 S4 [/ Q, ?( Z+ e9 H: f 外来物损坏,1 O3 F3 _: C# F 由进人发动机进气口的物体所引起的发动机内部。. e/ o+ H0 z0 m9 d0 O2 B 故障报告手册,2 r; ^ w$ Y B9 L P# [0 w 见Fault Reporting Manual$ p* [3 A% @5 v' ~/ H1 h( j8 p2 n( m. |; k @由升降舵系统 4 X% X0 t) i6 t+ h舵舵机提供液压力。 7 u7 N5 J2 V, M! Q" j损坏6 Q7 B* h* V. U2 g$ g1 v/ N' G# O; {) t2 _$ _/ ] 约燃油, 2 s- H4 ?- K% S/ ~" C7 U! C. H+ ]# ~为使燃油消耗最少而对飞行高度和巡航速度的计划。 ( a9 Z: s6 L& ^, q1 A油控制装置(FCU), 1 N: \# y% i0 u1 R: C1 o1 A发动机上的一个部件。在发动机起动和运转时控制燃油 * l! p" P8 x0 y0 x2 X; D% v) o& }+ v! ^$ t# }( _2 R: p; q" Y3 Y' _: }9 F 流量。 + R! |! U S2 a4 S( d" U英汉对照民用航空词典B OEING 8 }* v8 n6 _8 \+ gTECHNICAL DICTIONARY 660 G/ L8 ?9 @* y8 N' m S FUEL FLOW, The rate at which an engine consumes5 c+ I+ I) I- l9 I F' ? UEL HEATER, A component on the engine for heating 8 L( ~$ p# V0 z- TUEL JETTISON SYSTEM, A method for reducing 0 H+ ~! C7 D' v7 A$ Y3 [& G% ?9 Ce 7 r' t1 ^0 m5 E9 l) b v; U* YULL FLIGHT SIMULATION (FFS): A flight training, x- z) y( f1 X) d$ Q evice that incorporates full visual and motion systems " r0 R% B4 v: H$ _/ Gnd specific model airplane. 5 ?2 V+ o- ^2 G) ~% g( c$ z* ^ULL-WAVE RECTIFIER, An electronic circuit which $ O' ^; F- W5 L) {8 ]) n1 O& ^+ rhanges an alternating current signal into a pulsating1 m+ {. r! x2 ]! c- s2 H, A irect current signal. , W! [& c4 |0 ~4 D3 e) B- R* cor/ E! \7 v: O9 b AGE PRESSURE, Pressure measured in pounds per & ^- R7 T/ q3 NGALVANIC CORROSION, A form of corrosion caused / n2 K& V1 w: h9 p' yby the contact of dissimilar metals. ( d. F+ R5 K& e+ K油加温器,/ O1 H: U) |, s+ m7 w! \: c- z8 Z 热燃油以防止发动机燃油 7 j/ [# Z0 l1 Y, Q0 h. `急放燃油系统, & a3 m' v9 S, r2 c% o0 f% }" }" m中的燃油向外排放以减轻飞机重量的6 a! `6 k' D7 R% V$ K- Q/ ~8 ^0 x 动飞行模拟机(FFS)," ~# e/ m l, q$ P 一种飞行训练器。它综合了完整的视景和运动系统,以 $ W4 G# C8 j1 s* ]1 a具体的机型。, {% }, Y0 Z' C0 i 波整流器,# Y8 B6 j5 ~; V) M 用来将交流电信号变成脉冲直流电信号的电路。 # E- s! M; T& p. T压,7 w* A* m8 S4 z9 G! ]& u0 Q 平方英寸若干磅(psig)磅/平方英寸的计& t) o f; r' N5 O5 Z+ d9 K 电解腐蚀, + n' r, X& O- T' V一种由于不同种金属的接触所产生的腐蚀。 J( b3 p7 a* Y! x- Z" `. A fuel measured in units of weight per hour. ( R2 N0 W" m9 _9 }3 h0 P9 RF( p9 V! _7 k3 Y. T. | fuel to prevent icing conditions in the engine fuel3 {) a* O A* ]6 J system. & D# A5 K4 b( R- h0 A6 g6 a8 AF 9 w1 {2 Y+ Z* i) E7 eairplane weight by discharging fuel from the tanks to th / q+ Z. S) t! o1 Aoutside. 8 {' B% \" K7 J+ N c2 j- T8 PF# p+ s: F; v3 u: d" a. T- j* U g d9 ~+ [$ z* i5 L- Y! [, _2 f& C( y a % _' x+ d4 ~! m8 q, JF ) A( Z/ [5 B2 g2 M4 wc. c3 z& m8 {* T- y& l d. r2 u3 B" G2 n# x8 ^8 e G8 j$ O8 |9 v4 E. H GAGE, A component for showing quantity, pressure, $ \2 Y4 |9 M g6 Y9 rtemperature by a pointer or numeric display. & u; c( r* S1 e5 F5 HG9 F3 a! x0 b8 a4 \; P9 d square inch gauge (psig). " X& z0 f& S; p* k( l燃油流量,5 |) i& A" e: C0 D& Y- u 发动机消耗燃油的速率。以每小时单位重量衡量。+ e2 J$ T' j2 u* O3 y q) P" s7 L0 I' l! f 发动机上的一个部件,用于加. a: I, J; H; h% D7 t1 j0 |$ a 系统结冰。 : L9 |" N# ?# Z" L# Y; y+ E p, g' p3 [ 一种通过将油箱 . n, |0 p f3 r, {方法。5 G9 S6 Q; P8 I- S( f' j8 h* D' Q4 i9 D! j1 C" v& `6 ^ {/ `9 `0 L7 N. S2 X) ? A1 R$ y: N) I: S 计量仪, ( V# N: B( I" W p$ X由指针或数字显示出数量,压力或温度的部件。/ H7 ]/ ` |" U- U2 O1 X b) r- B8 w5 ~8 Z2 a6 p单位是(每 1 Y0 L. J! _2 u9 B' ?" F示压力。 / e! N, }* v" j) F英汉对照民用航空词典B OEING4 j! E9 q! C4 [4 j8 v TECHNICAL DICTIONARY 67( `2 j3 `- k, `9 f GASKET, A seal between two flat surfaces.# y5 l1 p/ i- m% i* {+ P be individually controlled for the amount( w: q3 s6 p" j! h; x% W% R& v nd direction of supply. $ D' ^ J1 P& o0 O$ f6 {ATE (NO. 1), Airport location used for# t1 l; h/ r8 L; S: | ading/unloading passengers. $ C3 [! a' i: q" m# P0 O5 N3 ^ATE (NO. 2), SEE - LOGIC GATE; T0 K i% Y& y, w2 K9 @. d ATE VALVE, An actuator operated, sliding device in a2 }# \2 S7 ?. l/ m# X5 z uct for closing and opening the duct passage. $ E9 m/ O$ \% k间的密封物。 * s5 s% d8 K' z( }: b/ t4 y1 e调节供气口可控制空气的量和方向。 9 G9 F$ |9 @ T" D登机门,5 e J) f1 U. `/ ?" O8 r1 D 机场内用于乘客上下飞机的通道。 " u8 _, Z# o8 H# T逻辑门,% W" k2 Z# E, k" z4 ^ 见Logic Gate& h& f. ^) G: h- R6 F GASPER AIR, An individual air supply for each 0 A) I& J' C6 qpassenger. The air outlets are in the Passenger Service) h% v7 U1 }2 Y3 d9 G, o Units and can ) \. P% z1 @1 M7 [- J5 ua ! E+ a" |+ b" z9 N' ?- \G |. c6 ]. R1 |' N" O lo 5 ]* e: l5 x& i& q/ z1 xG 0 l5 x2 V* h" f( |) Y% |G ' h( ]2 P; ?3 d. L4 Xd 8 n% @% q! h3 x7 Z; K+ x密封垫,$ D, f* ^" r' s4 L4 [ 两个平面之9 s! A( q; a! Z# } 乘客用空气, 9 F" I9 I8 p6 f# c给每位乘客的单个空气供给。供气口装在乘客服务设备' k" M$ m; \/ e' F# l5 G0 d 内,个别2 F! H6 F. X# W" B9 r. e" G& e* w6 H' [9 W& x闸板活门, % ~! t$ q, L n0 i管道中由作动筒操纵的滑动装置。用来关闭和打开管道( e4 M; ?" T, E+ o$ X A5 C) F% z 通路。 : z* ~/ h" H e英汉对照民用航空词典B OEING 5 Z& O# E& H( q' d3 ETECHNICAL DICTIONARY 687 D: V) Z9 c I4 y8 v4 t$ w GATEWAY, A functional unit which connects networks/ m4 y& o( A% s# q r systems of different data formats. % }& I5 W2 l8 @7 {% u; ^4 C* YRS.- p0 f8 H; \" u2 S$ D) m) r ENERATOR, A mechanically driven device for * L3 w; m, {/ c# W oENERATOR BREAKER(S) (GB), A device which will w! a, g( q+ t1 g1 s' [tor from the9 ~7 I1 h& a8 h; H lectrical bus(es) it powers.! }% G. v, g+ z6 i8 c ent with # ^! ?6 d7 E) T/ I1 co rings pivoted on axes at right angles to each other # g `: A- \& B0 ]llowing movement in two directions used in the flap0 v, [' w+ U' P; e xtension and retraction system. # n5 R2 `) P4 { E! r" I" V接在一起的功能 7 |. B% t# h# U件。4 @& O/ h' S4 V8 b: t& y% @; x o 6 @8 v3 D: X; U7 \: K3 SGEAR DOORS, SEE LANDING GEAR DOO5 ]9 l; R* ], I) N G' u% u1 t* n0 F3 J producing alternating current for airplane electrical5 R/ ]& F# H' f E. C. e9 ? system.- C+ V' \$ y" }) {; h G: t3 {5 ~ ~* N9 i separate an electrical power genera+ c L( m7 e7 w# i$ A$ f; b e4 f" L9 Q* z. Y7 q GIMBAL ASSEMBLY, A mechanical compon2 R# F' l6 B% N# Z5 Z4 F tw2 j2 H0 W2 l' C1 a6 O4 R a' {( i+ X P3 }' C. T4 { e7 x w8 g, m& S1 n. F# O 闸门, 6 r; _$ c, L- b/ x* v( ^ |( m一种将数据格式不同的网络或系统联' p0 ~/ e' l- q2 v# ^% ?* _1 g {5 j `8 ^; @0 | 起落架舱门, , B! S5 W. {( M3 X8 T8 }* P- _见Landing Gear Doors. |+ w- G/ j3 k4 V8 @$ e: E发电机, / ~: E: f, O% `2 T" d- `为飞机电器系统产生交流电的装置。7 Y: o( @4 q* D% A1 u$ d 电机跳开关(GB), ) X5 Z( x. a/ a机与由它供电的汇流条断开的装置。 ( b! M/ ^& u* e/ X+ Q4 Z+ H襟翼的伸出和收上系统内的具有两个圆环的机械部件。 3 E; d* A$ j7 R) \个圆环的旋转轴相互垂直,以使部件在两个方向都能转) F4 D. w! L( J+ {4 c9 L3 v7 r4 D' j6 k4 z- |) A由机械驱动,; n$ }5 }3 p2 x# F9 x; I( \: _3 |' m$ [. B# w 能将发电 1 w; |; { }! r# r万向架组件,+ G" Q3 n* p* ^- ]) O: x, U& o1 v# q# I! u: [7 p) ?/ h1 o$ n+ J& K( \5 H! ?0 v. B 英汉对照民用航空词典B OEING 4 I; o, N4 x1 E" P5 K% V1 b" D* \TECHNICAL DICTIONARY 69! I* A+ U* D8 T4 t, g GIRT BAR, A rod attached to the escape slide which $ B0 I# w' ?$ r7 S9 P: yengages brackets on the floor for automatic slide 2 S- g8 @/ r; B5 V8 {- e( I0 C: iperation when the doors are opened. 7 B5 X" D+ L6 a, W* DLOPE (GS), A vertical path defined by a: r: D. V, m( g3 i3 U6 j/ r8 k ased electronic signal used by an airplane or) j* p- F: o: A: d7 P Y8 ~0 G LIDE SLOPE/GLIDE PATH INTERCEPT ALTITUDE, 8 Z2 x# S. u# s0 u, jhe intersection of the : \" Z X" t8 R: q5 G2 e. Sublished intercept altitude with Terminal charts by the , a# ]& T* }4 B- d4 Ltart of the glide slope/path symbol, is the precision FAF;1 p; S, C: H1 M7 } m owever, when ATC directs a lower altitude, the 3 M% [7 {* @" N0 ]% `4 ~5 n* {) b1 _ u5 d- ~( ]4 _$ ^上之锁钩相齿合,以便滑梯自动工作。4 u. c) t' O% }! q0 I 滑道(GS),4 X; [$ S" Y7 o; t" f% } b" T 由进近或着陆期间,飞机或飞行员使用的地面电子信号 3 M5 D6 N+ v1 F5 [: t) U. h1 U垂直下滑航道。 ; D) r, ~' F5 \5 v6 _% @滑道/下滑航径切人高度,0 |* w6 s8 Y! q8 { o1 d+ k 进近时切人下滑道/下滑航径的最低高度。在, t- L0 T# _& O& ~9 U 最后进近定位点。但当空中交通管制指挥一个 / q7 ], J' c# W7 r! O- E; F# i低的高度时,由此产生的较低切人位是最后进近定位1 c9 d3 T$ v5 j% J9 ~1 p7 H6 Q4 j5 W) D. D3 io, z1 Z2 O$ N" y, O: i$ S GLIDE S% p* s% R$ M( D; { ground b 8 K( [- w8 v+ v. Jpilot during approach or landing.: }7 e |( |7 } `+ h/ M, w# o1 Q) b G 8 @% o4 R; h/ m( ^The minimum altitude to intercept the glide slope/path4 C3 c+ t1 x2 u% J u on a precision approach. T6 {/ T( J) \( [; ~ Z; J p- @9 V8 G) Y! g; `2 p s 2 f) } i+ a+ ]3 n$ _h 7 Y# g' h/ d- I V7 J* v. |- ^resultant lower intercept position is then the FAR.- S2 e; h. o9 K5 g 束缚杆, Y# e/ {% m( n$ ?; X% }' X, x/ L连在逃离滑梯上端的杆子。在机舱门打开时,与机舱, H3 [: g$ [ E% n' @- f% ?0 s( d0 O8 {; y; Y! o" s& X( N$ Z% U 确立的一条0 o W9 y& r* N" D( k) K% S9 h7 n1 X/ s5 p* t b" |5 o& g在精密$ z+ G7 v. _+ @4 J b# b% z Jeppesen机场图上公布的切人高度与下滑道头的交接- n7 u, F y* J8 { 点。是精密 7 m: u0 W) w, w1 N# ^$ _) H+ M! ?+ G3 u G! G0 z# S8 O5 W; \7 F: k7 W/ x英汉对照民用航空词典B OEING( ?4 @0 j" T# t! o& } TECHNICAL DICTIONARY 707 P9 |/ i7 q7 r Q- p( v GLOBAL POSITIONING SYSTEM (GPS) (No. 1), A* `/ w8 {5 i. E" d" O pace-based radio positioning, navigation, and8 a' M+ {" d6 x+ N" ~+ z: `; i7 h metransfer system being developed by U.S.A.& T& x6 @ R1 ? epartment of Defense. The system provides highly1 `3 z( r, _; P recise ! |) O u6 E# [. K! H5 t8 nnd provides a worldwide - N$ |+ @, S' gommon grid reference system. The GPS concept is / J" Y$ }! p5 W) iredicated upon accurate and continuous knowledge of+ z2 o0 l) P( c' Q7 a0 c: ? e spatial position of each satellite in the system with 5 z/ _* q C' sspect to time and distance from a transmitting satellite 4 N/ r8 ^" b, T' T# lthe user. The GPS receiver automatically selects . g& L2 L* ? G9 U5 a+ rppropriate signals from the satellite in view and , Q- x1 t, g& i/ B$ J# J+ Hanslates these into a three-dimensional position,; v0 x& O' A7 q2 F0 I* Z$ O2 P6 p elocity, and time.6 @* N- U5 N0 x LOBAL POSITIONING SYSTEM (GPS) (No. 2), A: V) E$ N* V% O! A* u J. i ngrange navigation system that takes navigation input. l% _& l" D8 R7 c n" W om transmissions generated by a series of satellites in X( D1 L) J1 W* { LOBAL NAVIGATION SATELLITE SYSTEMS (GNSS), s$ K; }5 ^! W9 D6 | ternational Civil , s8 g! }( ^; n: N3 q5 Aviation Organization (ICAO) to encompass any 5 ~! Q& l$ j7 L( c8 Y3 gdependent satellite navigation system used by a pilot7 U& G( x( R4 O# N( A perform onboard position determinations from the ' \9 i$ \' N. {3 x M% V6 `4 E, lO-AROUND (GA), Airplane maneuver where the pilot is ) C# U* D4 b# L! e x, qin the final approach phase of flight and decides not to8 T) m# w) K _6 Z: ^6 |6 s land. Thrust is applied and the landing gear retracted so- k) G0 f G b6 s' f( C0 @ as to climb the airplane to a safe altitude. , l- x& l% _, M+ @GO-AROUND THRUST, Maximum engine thrust to be/ q5 u( q9 y- R used during the Go-Around Maneuver. 7 q9 d4 b. x& @; ^4 J4 j统(GPS)(NO.1), - P0 [. T! I$ ?" d0 s2 u电定位,导航,和时间转移 P' y9 a& B% U1 } 统。该系统在全球连接的基础上,给无数备有适当设备 0 S2 K( z; ^! h$ w; v1 Q& {9 J3 x户提供高度准确的位置、速度、和精密时间信息。该系 : J( N! z. J% B3 j' O# ]响,并提供世界通用性座标系统。全球定4 j0 k0 M k' B2 v 信息之原% G. V2 N; A- O) C N* v% N 为基础。全球定位系统自动从所见卫星选择合适信号, - G6 n! w% K3 H并将这些信号转译成三维空间位置、速率、和时间。0 l/ o% ], ?: @3 k4 A' v9 S5 i 全球定位系统(GPS)(NO.),8 g, N Y" U5 U' l* [ 一种使用一系列同步卫星所发射的信号作为导航输人' S5 L1 Y4 ~1 e# ? y 长距离导航系统。 + l# K! ~! R* m& E) F6 _球导航卫星系统(GNSS),9 }. O- S3 v5 p" O$ i- B 航组织采用的“伞形”术语。它包括飞行员" Q0 B# W1 O& t( o& J5 | 料做位置判断而使用的任何独立卫2 Y& z) j X1 A% F) W/ A& ] 导航系统。! b+ J; W/ { ?' k# k 复飞(GA),( k- T( N* ^% T7 v7 M 飞行员在最后进近阶段,决定不落地而做的机动动作。- H: p8 C6 H3 H6 w0 R6 J' T& @# @ 复飞时需加油门,收起落架,以使飞机爬升至安全高度。 ! p3 \. @, v# Q. h, m4 p2 v* d复飞推力, * S4 w1 c9 q5 d" _飞机复飞期间使用的最大发动机推力。 3 m: t& N; |- I. `; u+ D% p, W" |s " E+ I! H: |" z( a" @) y" {ti* K6 n; k5 x2 m D . q9 n7 T& ?8 A8 Taccurate position and velocity information, and p # [, x) P& @, E4 ]) Qtime, on a continuous global basis, to an unlimited 6 q% |- C8 ^1 S7 j/ Enumber of properly equipped users. The system is * s8 f& R7 T) ]5 L# o/ B! a0 I9 Wunaffected by weather, a 7 ?8 `( M' {0 r8 t8 Sc% m6 ^. L4 C. m6 @# q p0 c) g' O- t# b# N+ s1 _ th0 X- B0 L" d$ v; \ re1 J; P, A: w' W3 |7 e( u to) U" N4 @ e4 c& o4 T a! ^ s) v1 ^& D$ K/ K' O tr * b" o: O `1 ?1 ~9 {5 [v# {( W2 N1 P) x+ K G/ x) a0 W+ H% | m- e. F2 {) a lo0 d9 T% I* G2 w+ Y3 x8 n fr3 X6 N6 b1 c$ n synchronous orbit.! G1 ~: ^0 f) p G 2 b' R" {4 N& Y+ gAn "umbrella" term adopted by the In/ R' h0 s$ Z& P( C* c A* {, U' S! Z/ Z% r1 A; d in " |; o; V" C& e8 Lto/ h4 s% ~0 A& h2 {- p% v+ N satellite data. . r. W- Y) D2 K2 V3 u7 S全球定位系1 ^8 V2 y4 K/ l, u6 b+ Y 由美国国防部研制的空间无线9 ~( B' n8 B, e, v t6 g9 X$ H/ j# H G9 a& e$ o: [8 U. K0 t, B0 [" q! Z; _# e) e: {- c 统不受天气的影 : {: G: B) o4 m& N: D位系统概念以系统中每个卫星具备相对于发射卫星与用! s/ \, e* X2 { 户之间的时间和距离的准确且连续的空间位置% K2 u. ?6 L# ~+ p. j6 h, ?1 D2 V6 t9 W4 n. L3 z) q$ i1 b! ^" T 2 & D6 d! a* z, o. w1 b7 K# u5 n) L" o# B9 x8 S5 _5 l. B2 f& Q" o0 u. }' Y5 P# }: C4 {2 a" }' s 是国际民: ]( H) J" |% f/ X7 r0 Q3 I 在飞行中根据卫星资% A7 h8 l5 h+ L# |$ Q( W8 O5 T0 m$ t. B+ u英汉对照民用航空词典B OEING 0 X& ^; p, K& l- YTECHNICAL DICTIONARY 71 ' z$ T6 n! e4 HGRADIENT, The ratio of height gained or lost in a given $ f' z3 k$ t1 @8 O5 ldistance to the distance travelled. * c# }1 [; G1 n% E) r) j* Mrbon / @2 ~9 B4 ]- D! D) K; y7 K) e" |6 jr access panels, landing gear doors and flight% ^5 s; y( [, |! j ontrols. A6 _. _4 p, O" U, Z IRCLE ROUTE, Is the shortest distance , w: k2 E. V7 g* {8 jetween two points on the earth's surface. It is the line ) x8 s" E, r" ~# O3 Q3 t3 M4 ermed by the surface of the earth on a plane that& ~# v2 p! j& ], C0 ]+ j$ T asses thru the center of the earth, the departure point,. N+ |, ~3 d6 I, M7 Q" d7 e t line# B- w, v. [3 @ al Conic Projection 2 {* n: F# B: A- Spproximates a great circle route.5 I8 M1 a& O! \ \, c% { GROSS WEIGHT (GW), Total weight of the entire: E1 G: M0 E4 d5 `7 Y/ A( ?, v airplane, fuel, oil, cargo, passenger, etc. + Y5 o; p8 H) @8 K1 MGROUND, A part of an electrical circuit or system that" w+ j: A3 c6 O! G% [" v has zero voltage./ D6 Z7 F8 I9 \4 r- G* J+ ]7 j7 G GROUND FAULT (NO. 1), System fault that has6 ^. t, T* @3 {( ]9 O% W j, S3 Y. Q# V occurred since airplane landing." P0 e! v8 O5 z$ Z' H 轻的材料。用以制造舱口 ) U5 z# {! H4 S6 M( { W( e,起落架舱门和飞行操纵面。 6 d' F$ P! d" Q3 a1 i- A3 m7 F% f$ ?圆弧航线,8 M+ ~% ~! j, d; X: T 地球表面两点之间的最短距离是以地球中心为圆心,在: U# _) @& H0 K0 I J 飞点和着陆点间所形成的弧线。由大圆弧航线形成的真- F" z: N/ N5 b8 y7 c/ X% ? 迹不断改变。在兰伯特等角曲线投影上画的直线接近大 ; q% O r2 T6 p2 E! u( w) d5 X全重(GW), ~7 v* s9 v4 b 整架飞机的重量。包括飞机,燃油,滑油,货物,和乘 4 t. p- n- j9 v n" ]' d% h* V. s, u客等等在内。 " p3 b, Q& F0 D2 d" B) h. [' }地线, ) q+ ?- H. V) v a3 W+ v |; Q在电路或电气系统中,具有零电压的部份。- {9 i1 T. }( \& ] 地面故障(NO.1),0 M' L+ n3 z' f3 d. r, W" \ 自飞机着陆后所发生的系统故障。! ~: v+ w8 h8 K) b" Y GRAPHITE, A strong, light material made from ca 7 W/ {8 y" |- R1 Z* ^$ ^fo ' ?0 m: X+ U- u. I. K2 V5 }7 Kc9 N; _! g; N# t" n GREAT C- V9 g$ c+ \3 K b. F6 t) y- R( a' v fo & m; V$ B3 i' D7 l$ ^p1 _0 G! l4 e+ ]8 A7 t% T, S and the destination location. The true course formed by: o2 W, J+ q% P& A1 j. ? a great circle route constantly changes. A straigh- b P1 u+ c( n" K drawn on a Lambert Conform 6 z: _8 ^/ n$ r- ]. s- P6 fa ~5 h) c& R: e! q GROSS PERFORMANCE, Actual or measured : K! L, j7 {$ ]* O( yperformance of the airplane.# e# W! s, s& k9 s" ?. V/ e 梯度,7 L5 V1 _5 U0 `: B7 y" \+ @ 在给定的距离内,获得或失去的高度与所经过的距离之 2 J2 z& R4 w9 q( \7 \) P比。 8 Z7 L8 f" r/ ^, {& `, S# W石墨, ; B$ h# |1 k' T8 y6 ~一种由碳纤维所制成的强而) O, F4 G) }' \+ l/ [3 Z$ c0 r: q8 C9 Z* Z% B1 j8 `8 |3 P0 t: |& V7 ^- m/ L! }3 Y5 g' b7 L. y2 J2 w/ T4 G& f2 ]& z( v 圆弧航线。 7 k2 h0 Q5 c5 @4 u) r总性能, 3 E% O! T" R. ~! Q) X+ P. }+ \飞机实际的或量得的性能。+ ~0 h0 X1 t- [ 英汉对照民用航空词典B OEING& U! |$ Q& a) w# @ TECHNICAL DICTIONARY 720 a1 E! h) v6 j C2 M+ V0 T GROUND FAULT ( NO. 2), Loss of a ground connection, k* C" ~0 i+ [, `" u- S" s or a short-circuit to ground.& t: H5 d8 ^9 D0 X. A GROUND SPEED (GS), The speed of an aircraft % P" q/ L* E# T; g, b( C1 g5 H1 Qlative to the surface of the earth. ; l L7 _! }% S9 U6 N$ J# HROUND SPOILER, SEE SPOILER, }% i2 M" q( B i) K2 N ROUND SUPPORT EQUIPMENT (GSE), Equipment' J* k2 P4 ~4 [) p: P sed to service, test, move, power, or repair an airplane - G9 y' D+ a, O3 |: Thile it is on the ground. g7 @( J) b+ V. O/ pROUNDING POINT (TERMINAL), An electrical , p, P m/ F o2 y! T7 Ionnection on the landing gear doors for electrically" O* C7 B( I! A. J% m rounding the airplane. An electrical connection near " Z: ] L# L4 b ae fueling station for electrically grounding the fueling9 e6 w: d# _, I+ q ase. I* p2 b! s, M7 e3 m) m0 x, e8 W/ ] S, SEE - GROUND SPEED4 g; E$ Q, L. ~, _6 t T1 P SE, SEE - GROUND SUPPORT EQUIPMENT " ^8 z0 ?+ G5 G( p2 n2 }/ v2 rNO.2), @0 o! U! j; R; d5 E地速(GS),. r' G2 A$ Z+ y" U( A* \7 y 飞机相对于地球表面的速度。 c- A9 e9 ^2 R 地面扰流板, , \% s& u1 f# q+ z6 k* R6 V见Spoiler H0 K) Y6 V! h4 {9 m% u, Ire0 j" z# l6 Z2 X( ^2 ~: o' [ G 7 N5 k4 g( k+ p) f) Y( K: R3 O& vG9 q) r% [' @$ p. M u6 B4 ]: A0 p9 i$ {8 e7 b& S w8 E( y! v6 v0 _* {2 h5 j3 u G2 O9 v6 e* A& u8 B( `1 |( I c 0 _* M, T2 P5 g' m" _1 s" n2 } Jg ) d: \2 [4 k+ n: j: s+ t. j% Kth8 }" S4 ~. A3 B b + V. k r. W r6 d, e3 sG: K1 c9 d3 D) Z% O8 \0 J; b+ t0 l G 9 K( O# i' T4 q) S+ @GUARDED SWITCH, A switch that is protected against * C0 Y& g6 x. p& r( Faccidental movement by having a cover installed & e( ~8 s2 a/ R' l# K$ Ndirectly over it. 2 r- M1 f% A( J0 R3 t- C; ~地线故障(3 t0 n; p7 Y( L H* F 地线脱断或某线路因短路接地。+ f" w, h a1 ?& L% s H . * ~4 Q; x! w4 e8 q地面保障设备(GSE), " Q- h1 G8 L" w7 r; q! d/ s, s! S当飞机在地面时,用于勤务,测试,搬移,动力, / g9 ?5 B# ?2 T6 M2 ~或维修用的设备。; W# V* f" ?7 q* g! i- `& s 接地点(接头),! I) d% Y- j5 f, R" I9 ^ 是在起落架舱门上的一个使飞机电接地的电接头是在 : x3 Z8 ], r6 ]& Z' Y加油口附近,使加油车或地下油库电接地的电接头。 . [+ R8 z- |1 P7 k! O2 ?速(GS),# k. N/ S! f) y+ C eed 2 A3 a" o) c7 a供应& O1 Q5 t, P6 W7 ~; D$ T8 T/ S6 K* Q. Y" k& M5 p; G! Q' _2 i! `4 U" j" Q) E# [+ T7 c7 B见Ground Sp .+ Y4 {7 l2 b" k/ N2 d* V+ { 面保障设备(GSE), 5 t/ C+ [& Y4 J& \) Y见Ground Support Equipment8 {- M6 U" d; p( W$ z' Q/ H8 s$ w# L+ Q5 p U" |. R. z% I7 I+ \! ^9 j带保护罩的开关,1 c3 x0 z( R/ I% S# |/ U7 a 为防止意外拨动而直接装有罩盖的开关。 + t) U" O% d' {9 ~9 v英汉对照民用航空词典B OEING( [$ |; h6 h8 A TECHNICAL DICTIONARY 73+ W) D! a0 c. r) i% T9 a: `) V GW, SEE - GROSS WEIGHT) U- |! Q; G& \( J H4 o0 q3 [7 {* M, A/ k! T I HAIRLINE CRACK, A serious defect in structure; a$ f" r0 L( n, r% k0 l% t crack that shows as a very thin line.2 j$ J* f: l1 H" F6 N* i: {2 o) c HARD-OVER, A maximum pitch or roll maneuver.$ e. M2 ~ j( R/ S8 w5 e HDG HOLD, SEE - HEADING HOLD ( `6 R& J; p% o2 f) q7 K9 NEAD END, In a hydraulic actuator, reference to the 6 I+ Q' @- @) M: g8 {, Jart on the piston side of the actuator.1 x& D! B$ ~% c6 D7 ]7 g; q/ M( c HDG SEL, SEE - HEADING SELECT [" r8 L; L) M0 MH ) l# C. h, K# ^- lp% o) n4 C* t$ l2 s# T: U HEADING, The direction an airplane is pointed- H' d% ~& }7 u. U referenced to true north or magnetic north. * g: a! D3 q, S9 c; E, w3 l全重(GW),$ I6 E* W' x" m 见Gross Weight.: G! B8 `8 J% V8 z% H! \ 细缝裂纹, ! Y' w1 O. E) s/ Z1 B! `$ [$ u0 I0 N结构内的严重缺陷;裂纹的外观是一条很细的线。 % g# m4 _- }, O) V% K i0 S9 @急偏,- X& t4 M4 O( [2 m 最大俯仰或横侧操纵。 9 q! j* {& f: ?" y. d; F向保持,/ {4 H) @: _8 W- r; v( O 见Heading Hold0 f" v1 R% ^: P$ B( Y1 D) m/ I B2 y: k. S2 b4 k) n3 y* j8 z, f+ s4 \航向选择;9 w5 B% \& U9 A4 i& V 见Heading Select. 0 \- w* [% T% j+ {顶端, / P7 C: e' J* N液压作动筒中与活塞相邻的。& C: ?# O6 s% {: Q6 m: Z 相对于真北或磁北的飞机指向。 . Y- a. i# ~5 z6 x Q1 \; @航向,% I9 S8 F q2 U4 e- H: i3 C 英汉对照民用航空词典B OEING- I/ k: S! M, y% C2 y TECHNICAL DICTIONARY 74 & I4 O6 p! `! Q& g6 d5 W" w* fHEADING HOLD (HDG HOLD), A mode of the autopilot' [6 K3 ~$ P& T4 i irplane heading.! C6 V1 O( `* p# u, A! k) X/ h t- ]/ Z% _3 h+ j" f e ) _6 q$ \' W2 d" m% Q- w7 ]om0 }' V9 h1 I; }7 ] g or( W: U9 z" }9 K9 @# S1 N7 O. T. t (HDG HOLD), % C7 Y, v: p+ A) W(HDG SEL),; M9 o' Q1 }9 ^# R7 T% Z# V 交换器,+ U+ ^9 [) H* \! Y* E& v 有很多通道的金属组件,气体在通道里流过时,一股气1 T( p! X3 {/ x/ { 可被另一股气流冷却或加热。 5 V% P( l6 J( R4 b$ isystem that maintains the existing a ; `7 M& ?7 o& r2 M" _* t& P2 wHEADING SELECT (HDG SEL), A mode of the autopilo1 i3 d8 I0 d- ~" k9 ^ system where the pilot selects the desired airplan + n2 o' B( S- A. Kheading. * t& R/ E; A9 i9 W6 C# h% zHEADWIND, Wind or component of wind coming fr1 w6 v& q# \6 U5 l/ A( ~% } the direction of airplane travel. 7 H4 x9 g7 d7 XHEAT EXCHANGER, A metal component with many & v8 V- `' p1 |( \passages through which a fluid can flow for coolin! ?/ N* `; ` a' {& t. _ heating one by another. 4 y# u/ x0 b/ p- W航向保持 ) T* w/ i; W, Z1 q& h* o; m/ U自动驾驶系统保持现在航向的方式。1 g- O9 s+ g$ j7 l* L 航向选择% H4 t& C4 z& P) i6 y" A4 k 自动驾驶系统由飞行员选择航向的方式。' ]% p F' ] s' B% ]+ Q, L2 K 顶风,7 m# C0 u. Z* z, o* B; l 来自飞机前方的风或风的分量。7 I( v5 R$ s) S) A1 P2 T; ]3 C! ?/ t" ]7 ^: s7 P7 ^8 K) R& k0 s; I) a0 h英汉对照民用航空词典B OEING5 ^& s) q" J, ~% m TECHNICAL DICTIONARY 75 " q7 q6 p: i; {, `" u1 k8 e: hHEIGHT ABOVE AIRPORT (HAA), Is the parenthetical; D8 m0 O S5 J" _7 K: C |6 [ figure following MDA which, when added to the airport6 P/ @! T# x9 f1 m! J3 O levation, will give the MDA in feet above mean sea 5 _8 y9 b w: Y% w, lvel. A HAA will follow a DA or DH only when there is* U& e2 A6 s+ Z, d- _# J o touchdown zone, runway end, or threshold elevation1 j% M& Z* h) @& \ ), IS the * U* W/ j7 k8 V# k) I$ M; marenthetical figure following DH, DA or MDA which,) W+ l7 v% j. p hen added to the touchdown zone, runway end, or8 K" _( ?: }4 @7 o* b reshold elevation, will give the DH, DA or MDA in feet; K+ O5 R j% k1 u ], \ cy of one million cycles per second. r& @+ \3 V' o EXADECIMAL NUMBERING SYSTEM, A numbering V& h; Z) z( |( j0 eystem with sixteen as the base. The system includes 0 [( M. g( R, ^- ^& x, T+ k3 kigits zero through nine, and letters A through F $ x$ X8 O% l. A! Z1 Q7 N' Dpresenting the numbers ten through fifteen.1 U0 ~5 b7 B$ _$ {$ ^. `7 ? IGH FREQUENCY (HF), The frequency band between ! G: ^ n/ x* d, q" N. M! s场标高相加后即是 ) F4 [: g0 I1 Y$ z$ C- l7 }DA高于平均海平面的英尺数。只有当接地区跑道顶端或 1 A) P1 }$ Z" I. n4 t道头标高不可得时,机场上空高度才跟着决断高度(DA % E8 [+ ^. I/ x8 r' w" D+ t2 \DH).! ]: t- |- r4 {$ {; `: u1 k0 D HAT),& Q% q$ z7 Z" U2 D 最低下降高度后括号中的数值。它与接地- a, m: F/ C! Y 、跑道顶端、或跑道头标高相加后即是决断高度(DA, - ]" s% b4 j% m ?8 KH)或最低下降高度(MDA)高于平均海平面英尺数。 / u9 w9 w: S; _7 t的最低天气条件同时公布的。 4 w1 u6 ?0 T# g7 ~率。 # D# K$ k2 L$ A. B2 ]' v一种以16为底数的编号系统。该系统包括由数字0至0 B3 ]- C' N- y# ^. V+ H0 t ,字母A至F代表10至15.2 G" e9 ]+ j& G' X- t2 T 频(HF), ; X( y$ H+ Y7 a0 g+ v& D赫之间。& F- [4 V8 g, o9 n' Q e ' \- P- `+ |/ V `4 X @( ^le [: w- _+ s6 X3 w3 o0 H1 pn 7 `0 i4 v3 J4 W2 Q: Aavailable. 2 l3 d, m" h3 t8 _7 DHEIGHT ABOVE TOUCHDOWN (HAT6 L) }4 M& ^5 J4 n. ` p2 m7 U0 v% Z( o, v+ g w 9 c N! M. H( R8 g4 Eth ( `( q' W8 y. d! Xabove mean sea level. HAT is published in conjunction. o$ Z: c$ g, G! j with straight-in minimums.9 @) a' \0 @: {) C- T HERTZ (Hz), The standard radio equivalent of % {. H0 b: G# W0 @& a5 N; H# ~5 yfrequency in cycles per second of an electromagnetic + J0 A/ A, ^) I( L1 w m# swave. One Kilohertz (kHz) is a frequency of one1 S' k9 d3 @! a J1 q$ O thousand cycles per second. One Megahertz (MHz) is a - s' H8 `# W; L) b, v. v% zfrequen) M, U# ~# [+ s H 3 D1 d7 h: ]$ \s" @0 b4 r; V7 J0 B. Z d) a: {8 K4 w5 z) J re: F0 n# u# E& T3 v H- @& }* |2 g8 b6 e 3 and 30 MHz.# g" `: ?1 F0 S; m% U 机场上空高度(HAA), 8 W5 Y5 B* G$ S/ d* s是MDA后括号内的数值,它与机 5 C) s3 ~9 [0 [M & g: p0 h4 f1 j/ E" J" `+ Z4 C r2 G& V8 y6 c. {( O1 g* L# C; b. h- r2 L离接地点高度(& \, q2 F7 @2 o6 p1 y 决断高度或 " P% a: ~) s4 I/ P, Y9 T; U% z( U3 @- z% k. T. R5 }! SD: N% E. s& P, j% X7 d/ T; @2 u 接地高度是与直接进场着陆5 Y8 _" N) f$ \ }! h. \1 W 赫兹(HZ),& W( z0 ~# p9 { ?: S9 d2 s1 v 单位是周期/秒的电磁波频率的标准射电当量。一千赫 % V9 U8 u# N* U$ ~2 R兹是每秒一千周期的频率。一兆赫是每秒一百万周期的6 M% ~- `- K- a" z0 }$ ]/ J- i6 r+ j8 T2 }( A) e. E4 h 十六进制编号系统, 6 M9 A6 r- K& V4 E. D- d( U( E9 7 \9 c) y3 {8 w7 H! w1 o3 u x' I2 k0 _' V d( J. O; l. a! [频率带在3至30兆 . R8 r0 h/ {2 x( Y' o3 h英汉对照民用航空词典B OEING - R' A& }: b) [4 b" B) }$ F# ITECHNICAL DICTIONARY 765 X$ C2 }& H9 O HIGH SPEED TAXIWAY/EXIT/TURNOFF (HST), A long8 y% @8 e2 n1 A; d ] dius taxiway designed and provided with lighting or 7 n1 s. D2 Q v6 carking to define the path of aircraft, traveling at high ! r0 {1 j* V5 |9 B6 X: gp to 60 knots), from the runway center to a : E! h4 B1 B1 G( Athe center of a taxiway. Also referred to as long ) W7 c9 u' E7 l2 M& cit or turnoff taxiway. The high speed taxiway is$ k6 {6 H5 Q" @' D) b1 A fter: \$ w( M Y2 U ancy time.0 s8 q7 K4 e3 c* I& c r a0 a9 u* z+ D6 G' g6 _4 F eavy component during removal and installation on the. E/ u) O* S5 q O% O/ j irplane. 9 a; t- F& q% @# r- ^/ HOLDING, Airplane maneuver to keep the airplane from/ k/ [& V1 X( X3 z/ B1 i rogressing along the intended route of flight.& Y7 U7 u! Q- p# T. W OLDING PATTERN, The predetermined maneuver0 L7 T- ]9 l5 l c control. 5 ]: M; a! l$ N5 [! KOLD/HOLDING PROCEDURE, A predetermined 2 O5 i1 W+ P4 K2 |aneuver which keeps aircraft within a specified S9 D) F& _6 u0 C) m* \! Lirspace while awaiting further clearance from air traffic. G4 n9 K; y( `( v- o/ l& l8 ^* R2 T ontrol. Also used during ground operations to keep . E1 [/ s, {1 x0 N' sircraft within a specified area or at a specified point 4 k! i" J; M8 j! v" Phile awaiting further clearance from air traffic control.$ o# P, g, T5 m# m he standard holding time is one minute at or below' x* X' Q! W& _. N; D3 w/ E) j- e 4,000 feet or FL 140 and 1 1/2 minutes above. The3 h b5 z' b. \$ a: F6 h eparation between 1 and 1 1/2 minutes is FL 200 in% b# m+ n: [! }( t* W. |. W0 V0 i+ K (HST),' X7 f0 \- R# J5 E9 L 道。该滑行道有灯光和标志表明飞 * T' |( ?5 z) o r7 F8 j从跑道中心到滑行道中心一点高速(可大到60海里)通 , ]0 D5 s& x/ L/ L% e* z的路径。也被称为大半径出口或脱离道。高速滑行道的 - h1 d' ~$ x- w* X& p计意图是加速飞机着陆后脱离跑道,从而减少跑道占用 8 l& V$ B% j$ m时间。- c8 O7 M# l/ b+ S7 ~, K 安装过程中,用于放下或抬起' M% J6 M; ^- V* Z2 ` 动机或重部件的装置。: z1 ?! E7 L7 i }( q6 x- V 待, [2 ?- c6 \- m 使飞机不按预定航线继续飞行的机动动作。 ! v, q0 I7 |3 m: } }" b* q6 S1 i待航线,) l8 a& ?; V, U9 Z 处于指定空域内等待空中交通管制下一步调度8 J1 V# ~: ~7 L1 g2 M 等待程序, ' W" I- D. j& V( y2 J3 ~保持飞机在指定空域等待空中交通指挥的下一步许可- ^% b' I5 S! L. U V7 N 的预定机动动作。也用在地面操纵来保持飞机在指定的地 + o; `: n) w6 q1 |区内,或在指定点等待空中交通指挥的下一步许可。标准( X% |! k9 R C2 Z# U( s% w 的等待时间是在14,000英尺或高度层40以下时1分钟,& \9 Q* l4 t( I/ |. `6 h& k3 P 以上为1分半钟。有些国家以飞行高度层200作1分钟和6 Q% {- c# W: d/ T/ v' x& v 1分半钟的划分。8 t: U9 `: a0 x2 X | ra 2 w; G% v" O4 E" n3 ?3 V$ Q1 ~( Ym- i; G, X G+ @9 w speed (u+ {# x# l' y& o! d3 u point on 5 ~7 T1 |& [1 F( P. w$ X; Oradius ex + b' ~* x3 _/ p9 adesigned to expedite aircraft turning off the runway a + J/ k C9 ]6 x7 Y+ g. I% olanding, thus reducing runway occup z; }* Y) L7 ~- R# AHOIST, A device for lowering and lifting an engine o9 I1 ^: l8 t) p* Q' Z' c h ) Z7 J4 V: c, f3 D% c/ ua0 ]/ Y6 I0 U: y- n H- [) o- _; s% r; h2 M9 |* E/ Q p & C7 W% Q6 g- x) D2 M& r1 U8 O1 jH8 l+ }3 |8 m6 E& b1 ~. `1 @ which keeps aircraft within a specified air space while! L; D n( n! j& a* Q, K; G awaiting further clearance from air traffi . @! A4 e1 E' a4 _+ Q C; HH$ y, c- s0 e0 d1 q1 e& D! Q: x m * S1 G i6 o5 `3 ]( ca ) m7 n! d# J0 ^( x/ [c n9 x- G. \' q5 X) v9 N' La B+ `/ F4 C: o3 p w * w2 B5 V; a, C' r: PT; j& L7 ~& X7 e5 y+ k5 T. H 1 + G! q+ T: |6 S2 l+ [s! `, Z" b$ h6 ]5 w* h0 d2 S; h! T some countries. 5 ~5 P# l/ W4 h9 ^" R( J高速滑行道/出口/ d) m) X3 R9 Y1 ] 是一条半径大的滑行# D/ ]# l: d& r# g! p4 d& U) T) S+ n* E8 `+ U7 A! [* u9 ^# Y2 S# [9 S# D/ B2 `/ u7 V- ]) L6 C/ T, `, }- P% b* l+ Z0 e: i9 d! f6 s% h 吊车,- R; l5 X: W' ^( n9 l. {; r 在发动机或重部件拆卸和 4 d4 x# _5 K/ ]. ?) g$ Q) y+ M4 ]# N5 Z" ~0 |% {0 F9 i+ K! _6 _% q3 j; |: v& C 使飞机 - Q$ p; q* v, V的预定机动动作。 / C: o( h0 ?$ j' [) t( I1 ; E! t3 s3 U, [8 T( f- I英汉对照民用航空词典B OEING% J6 f3 M p) N( h$ S TECHNICAL DICTIONARY 77' Y L$ b5 v$ Q4 [ HOLDING FIX, A specified fix identifiable to a pilot by7 u! d; F* L; c" v, W; ] NAVAIDs or visual reference to the ground used as a' n u/ [1 P: x2 O, N ference point in establishing and maintaining the+ }! n6 S6 B$ Q, m; Q osition of an aircraft while holding.1 A1 G8 k+ Q4 B$ E) C OMB, A hexagonal material made of metal or0 j/ \1 f. `5 n9 B! P8 H/ i omex for sandwich construction of panels.! O A1 V7 J7 _! P/ ? HORIZONTAL STABILIZER, The moveable horizontal ~2 T. z7 a( c+ u& ^surface of the empennage used for pitch trim.. C( d/ E$ Z, H, z HOT BATTERY BUS, A battery bus which is not5 a o0 Z( B7 g1 G8 a$ a switched and is always energized from the airplane 3 a6 r3 t+ I* r6 Kbattery. # A1 V- _1 `, P# ~6 N' h使用的一个指定 ' }9 D: Y" X! L; R8 @位点。飞行员可根据导航台或地面目机参考识别该定位 / j# N0 r' X& V6 e' f! W/ b7 X& X; M* n' B8 O, z窝,+ n; ]$ Z+ Z, ^, V) |, Z 一种用金属或Nomex制成的六角形材料,用以制造夹芯 * j- h T8 u: P. V板。+ ], `: o( L+ i# _' r1 I# x6 s* s 水平安定面,4 I- T, v: v6 F6 @" q1 I 飞机尾翼的可动水平面,用来控制俯仰配平。. ?) s; r% \& Y+ c# R6 S 热电瓶汇流条,% e" K2 t* k8 U7 A0 y- g" o" ^4 C 无电门控制的电瓶汇流条,始终由飞机电瓶供电。5 X# [6 {& Q- D w4 s8 e7 g, f re& j" l! I+ P& J- O8 a* W- \7 P* l q, U, U p ) S- T7 [: _/ \/ |( D# YHONEYC 5 P0 {4 D$ ]; _) ` BN & g2 @& F) A$ x l, E# v等待定位点, 4 T: r% v9 w' y& h$ Z等待过程中在建立并保持飞机位置时 + t7 O- A3 v4 F% n" g5 S7 `' h8 D3 X; y; o- k# P n2 T1 K3 X8 ^3 X& n0 I2 ~1 ]& R! R$ q* @% d7 m. {( j+ p+ s英汉对照民用航空词典B OEING2 B( k3 D7 L4 J- I TECHNICAL DICTIONARY 78 & h1 w+ K4 ~4 Y8 [. }! @. k, }6 `HUB CAP, An external covering to the axle of the main/ W: F3 p( y% `0 f/ D" Q9 v landing gear wheels.6 l; H5 N6 n+ s/ \- N, n# J1 ~ HYDRAULIC FUSE, A device in the hydraulic system 5 {1 J. J% [4 P$ w- br stopping fluid flow when a leakage occurs in a line ' P5 O: h; G8 J: Y$ M. F8 `4 cownstream of the fuse.# `8 j& q! ~. _) v: N S, SEE - INDICATED AIRSPEED; w" |5 g. |& V3 D, G( x" w ER PLUG), An electrical device for& n6 F5 W- z2 y7 W- q3 L producing a spark in the combustion chamber./ H& g4 N) {0 w3 Q; @, @0 g% t4 }: v' N. Q 压保险, * E2 {4 G ]/ v/ l W$ U液压系统内的一种装置。用于在保险的下游管线上发生& v1 ^; p7 m: I 漏时,阻止液压油流动。& C) ]2 ^: V. z; g 示空速, U5 D6 r8 M0 w$ T 见Indicated Airspeed + N. C7 R( s2 ^ }5 \& [ hfo+ {% v! O6 s1 a; \4 ` d) q5 m& J$ @3 r, T0 x I IA9 @/ ~3 ]4 `" S( H, [6 ^. o. w IGNITER (IGNIT& U+ b1 {9 T+ r& h; h. H% Y 轮榖帽,0 e( D* V# m1 b9 H6 X& G 主起落架轮轴的外罩。 ; q W" ?0 l: ]. ?6 u& a& n5 y! ~, `# v) M, c+ [* i' a6 m! x1 g* _) d6 Q' R$ C5 W, s0 O9 r3 w3 j$ r& @+ c3 ~* t) q; g1 X 在燃烧室内产生火花的电器。 % B9 g& v: p5 ?+ h/ l: k点火器(火花塞), ^ S0 J; J& e/ V& t7 ~1 m 英汉对照民用航空词典B OEING # R9 s; r8 a+ i( Z$ ~8 FTECHNICAL DICTIONARY 79 8 T* H5 B% |$ h8 U' R- yIGNITION EXCITER, An electrical component for * y& H# n" k. g$ ?) R2 P) Asupplying high voltage to the igniters for producing a 7 `' D2 m6 \# ]# B: Ospark.4 S# E2 P. A) j$ Y IGNITION SYSTEM, A system for starting or continuing 8 s- z. g7 [4 R0 B5 }combustion of the fuel-air mixture in the engine% z7 o" W |1 b' K( C7 O- c- T. |8 Y$ { combustion chamber. - A* ^. C3 `1 E* V8 R' ~8 M1 v. m( ]; j+ nS, SEE - INSTRUMENT LANDING SYSTEM 5 H5 ^! i$ D$ m8 {+ W6 {* Y) jPROVED CLIMB PERFORMANCE, The rotation and 0 b+ T7 R* ~7 qlimbout speed increased above normal to increase ' U6 O8 D R: A7 C) k* R" MDICATED AIRSPEED (IAS), The airspeed read * I8 E& S* O" H7 S0 ?7 e. ]火系统, S& w' s1 v# b3 |& A# s* e# M0 ~3 O1 _一个使油气混合物在发动机燃烧室内开始或继续燃烧 3 U# c% a. w# J. Y* K7 x系统。 $ e0 L# x3 O, c1 C) r3 C ?% R Z表着陆系统,/ X% T# m; Z1 ]/ ~6 w' Q2 u trument Landing System ) Q5 P! [; Q+ ?% lILLUMINATE, To turn on or to provide light.. c/ V( N* X W IL / o5 S; P' ]$ @" r5 N& AIM 1 ~3 a; W9 e7 [" xc , S" s# F8 |" L* ]9 K! J9 j+ ?- ]airplane climb performance, especially if an engine 9 D3 k2 W0 r2 b; f7 Uquits. . H+ F* W7 x# }. I6 R7 a' ?IN ! B! W6 s$ W5 P2 B/ Wdirectly from the airspeed indicator without any " g- }7 a, X A' {/ D$ Acompensation.7 c/ V! i) {/ B9 J5 a6 Z INDICATOR, A component for showing quantity, ! s% b/ D1 |- ?9 l6 Y2 S4 F- Rpressure, temperature or position by a pointer or. J6 @1 Q: }7 s/ y+ ]* s numerical display. (Similar to gage (gauge)).9 X; {9 Q! d& Z& Q. @" Q! |' y 点火激励器,% |1 Y# k4 a' N% H) h+ o6 H# H6 T7 N 向点火器提供高电压使之产生火花的电子部件。" \1 N$ ^3 ^# e( N3 a( H5 c6 |& ] Y( ~! X2 o: c; w5 F, B& v' \: I 照明, . X2 j1 J) X" l7 J9 R( S打开或提供灯光。 ) ?, I( e c0 p- s! T+ W2 r9 e6 d见Ins . 5 P: m3 M n5 v& O0 A进爬升性能,4 n8 D) ^4 u- X 用大于正常的抬轮和爬升速度,来改善飞机的爬升性 + Q# Q* l( A2 S5 q一台发动机不工作时。 ( U' R- C$ }: R, b示空速(IAS),0 F* D2 ^ @ |! j; w4 }& M( w 正直接从空速表上读出的空速。1 l9 j0 \) G8 v' R, Y 指示数量,压力,温度或位置的部件(与 ( R" E& h2 x! ^* p6 W计量仪类似)。; t+ v% s* V6 ~$ I2 ~1 A' e1 ^9 D( I& Z: V能,尤其是在$ i% P+ X. u6 F$ Y7 `4 d0 E7 V6 F3 @# X8 M. ~& K 未经任何校 F, T1 [1 B6 i) S8 f$ O) d; }" L: c指示器, & |9 W9 C7 w* V2 n用指针或数字来- b- @$ P) p1 C% O 英汉对照民用航空词典B OEING , U, g7 g, E. ]' l, O1 uTECHNICAL DICTIONARY 80: X. ]5 ^0 ~( Q, K3 a INERTIAL REFERENCE SYSTEM, A self-contained, ; V7 `! D. d7 E2 Q. Hnavigational system based on the measurement of7 v+ O I' x5 Y$ [ acceleration and attitude. V4 t7 [3 ?0 b( w: U INFLIGHT PERFORMANCE, The performance of the 5 s& M* `3 d6 x( n( a# m5 cITIAL APPROACH FIX (IAF), The fix which identifies' p$ j1 x# i9 l6 u9 {* Z/ q e beginning of the approach to an airport. 8 j8 n5 U7 a7 E9 a4 n/ G" z7 vLET GUIDE VANES, A fixed set of blades in front of0 K1 n0 c6 d# l% B& f) U- P8 ] n engine compressor for directing airflow to the 1 d2 w! x1 d# }ompressor. 1 }8 n6 _1 `& K" ?5 A6 s! jNER LOOP CONTROL, For autopilot operation this is* g; v2 Q$ {7 Z& r e basis control of airplane pitch and roll attitude 8 y; r5 ^& a' v4 s# X7 }中性能, 0 ^" ?0 n) R7 p' W" u+ I: {2 h# Q飞机的性能。+ _8 [7 ?0 n' j$ X: o4 H: H" [1 c 起始进近定位点(IAF)," s8 w: s& R8 a3 B 标志向着陆机场进近开始的定位点。; Q/ B) X; k: j 进口导向叶片, w3 k% y- k! _: N2 @发动机压气机前的一组固定叶片,用以引导气流进人压 4 m6 W% @8 q2 V1 l, R气机。 $ _1 C2 s/ f- p! a环路控制,4 U, @$ h8 b. j/ U; ?/ k 对于自动驾驶仪操作,这是无关飞行航道的飞机俯仰姿, [( z7 |' ?# N6 R O 制。2 i7 P; L, [8 F) i0 O( Q3 c aircraft while enroute.; m- q: ?$ b, n$ n, {; S( H IN ) Y4 ]/ j% u [- K. G( Gth6 @. j# K" L8 o) P8 i a IN 8 s& m( |; C5 s. a' X/ {- ^- Ya ' x0 P; j# o( Zc4 W' j* b% f1 ?- H0 D IN 5 c0 u$ i! C& ~' f+ a+ y# Y2 |th( P0 P! A. o" L. v9 ^8 J8 l4 L without regard to flight path.4 O& T2 v% p* |: ~3 X 惯性基准系统,2 P7 f% V3 r6 \" c3 ^. u 以测量飞机的加速和姿态为基础的独立导航系统。 : G% u9 D$ x" ?' J& E( T k5 ]7 |1 I8 |' o$ t# n6 Q- O 飞行中" {, u \( A/ E# ~2 t9 t6 b3 d9 C9 A" m, Q1 l0 D9 p! g& t 态和坡度的基本控) a( M3 r* \+ E$ o" z s6 @ 英汉对照民用航空词典B OEING1 k& L3 r* C# @$ ] TECHNICAL DICTIONARY 81: L7 ?, f, \% S INNER MARKER, A marker beacon located between9 t0 T# [# `* b the middle marker and the end of the ILS runway. * ]: \& C1 a, ~OP, SEE - INOPERATIVE) ~! q4 p4 A5 A. ^3 p. |4 ^ OPERATIVE, Not working or operating. 2 A! B7 n- o3 ?2 H/ H& ZSTRUMENT FLIGHT RULES (IFR), Rules governing+ z! q% o! G K8 e: | e procedures for conducting instrument flight. Also a+ ]2 u7 B M8 ]* F4 o [! G4 H# z rm used by pilots and controllers to indicate type of2 N3 J, z3 f T* v ight plan.* Y6 e6 S9 W8 X. k9 A6 B STRUMENT LANDING SYSTEM, A precision8 P0 i- B" i# g# A m- a- ` strument approach system which normally consists of ( H5 x& f( r: y+ o" Oe following airplane components: localizer receiver, " L* ]) d9 ]* I* E$ k1 c" G2 flide slope receiver, and marker beacon receiver. 9 v" @5 j# K2 ]OLOGICAL CONDITIONS $ q" @1 f3 X, D4 r J6 W; eMC), Meteorological conditions expressed in terms of 4 m" u4 L# z9 N$ Gisibility, distance from cloud, and ceiling less than the 7 N0 t% I1 K+ T% z: {inimums specified for visual meteorological* f) V5 {5 L' a+ I6 e. H, N! S itions. $ f% Z: E, g3 U: o) |STRUMENT RUNWAY, A runway equipped with : E+ M1 {+ M" c+ q- _0 n E3 P# Wlectronic and visual navigation aids for which a# \) @5 }1 p; D4 U$ W1 k2 i recision or nonprecision approach procedure having 4 C' Q( Z6 i9 \, f- Z) f- m间的信标台。+ E. v$ D9 Z* ^; c9 p+ z 不工作的,3 r- ]0 M L- D3 c( l 见Inoperative $ x; M0 s2 k1 h) VIN9 F" N+ n' \8 g IN8 ]7 C- l+ k* Z) V y2 {+ S4 ~ IN 6 u$ a8 n7 K: z( {0 H+ i( l: cth9 ~( J$ m# g% I7 L te 8 U1 Z, x6 A/ O& j9 q4 z# \fl 5 _( p7 a% A4 s2 K2 J$ i, f" T/ FIN; c( d' p, Y/ S( i: ^' ?" g in# p# {/ e. g$ r+ ?/ Q th 3 n- ]' l; E! ]4 q$ W( d' A( G4 Q/ lg 8 d/ G4 X- F5 R& O# s' uINSTRUMENT METEOR 3 U0 N! ^; Y1 `+ u3 x(I ; c* ?0 g! w' L# |v7 G- e- p( B; k! J6 K: ?0 j7 j% @% Z m# E7 q/ M4 ]" G cond) k- B ~; V+ @! m! W# I IN 2 U* Z; i+ F- n# b5 f2 r3 W/ I3 ?e y; x3 q* v/ I; |* Y8 Ep4 O& L( m* _ q2 F3 O& e straight-in landing minimums have been established. ! x: R$ G! F; G' K( r( x& G近指点标, 3 D2 E4 y) @: G) E; a0 L& F2 {位于盲降跑道头和中台之! f1 _3 y, ~0 Q7 t# P% [, ]) Z. [9 P% I. c$ }- k2 u* A1 y; u 不工作,5 M$ M6 l3 l4 l) }( o! ?6 W8 k: z& h 不工作或无法进行操纵。 ) ]6 f! l% b7 \仪表飞行规则(IFR), $ z! v# S( x& x仪表飞行程序所需遵守的规则。 & n9 I, Z5 d& l# a7 D3 C% Y4 g仪表着陆系统,/ ^& z$ [; l9 c' Z) Q4 n% ~ 一种精密仪表进近系统。一般由航向道信号接收机,下' d( y; U1 T" B3 H 滑道信号接收机,和指点信标接收机所组成。4 z7 @1 G2 F% `- W8 o 以能见度,与云的距离,和云幕高低于最小规定的目视 M! G7 t$ g0 C( R) C象条件的一种气象状态的表达。 8 i9 H9 ?* I. @7 X用于以精密或非精密进近程序作订明最低天气标准直 [3 p2 H- L- k/ J$ L着陆的装备有电子和目视助航设备的跑道。 , z* }+ b8 I: }. @0 A仪表飞行气象条件(IMC), 6 @! m+ d9 f) X/ d' U" r2 E5 S8 c8 t+ W, a仪表跑道, , Z' ]# f# q% Z* f* h/ y% {6 s) r3 a线; I/ Q; X- D, v) d, L1 p 英汉对照民用航空词典B OEING 0 A6 U; A3 K, X8 H8 H2 {& lTECHNICAL DICTIONARY 82 8 V& o% F: p i1 AINTEGRAL TANK, A metal container formed by the , Z8 q0 ?* E0 b7 ?0 {lane. 7 v Q* k p& E4 i4 i, `: I0 ?cted, t" x! m+ _! a) x( m5 m circuits.' u3 n3 G3 F% _ Manual * ?0 G ^* R j, Q9 \1 Lerformance data providing range as a function of a * `' |6 g: U7 Y6 s' yhange in airplane gross weight.9 Y# {$ ^/ a) G% M TERNATIONAL RESERVES, Reserves required by 8 h2 J# c1 R1 U$ X5 m. N7 Y& a, oe applicable governing agency when flying Q6 I3 t U2 Q- v/ i* L TERNATIONAL STANDARD ATMOSPHERE (ISA),( j9 x+ t: W$ z" w* H5 L4 H/ | he hypothetical vertical distribution of atmospheric $ x# u: P" a% H# k) X7 |9 I2 s9 Gmperature, pressure, and density as defined by the . l& L2 N8 K# y)." @' D, H" c2 t7 V TEGRATOR, An operational amplifier whose output2 u7 v7 ~1 H# H" r c oltage is determined by the input voltage, the input 5 [4 g+ H' t0 K% d& `3 J, L) K& u- i+ q) O. @" O 存燃油的金属容器。 + i% p& G) ]* G( d- T" q" n# [- v; _8 y0 h8 ] 飞机总重量的函数提供的性能数( b$ p$ w8 [/ ]( g0 N i- v$ M1 w1 ^9 s际航线备用油量,! Z; G/ o' X0 d5 m) |' } 在国际航线飞行时,有关的政府单位所要求的备用燃油 " ~ f/ ]0 _. f5 \际标准大气(ISA),0 `( U/ O8 \* u+ @ p( j 国际民航组织(ICAO)规定的,一种只在理论上存在7 o3 q6 F% ^! Y E 大气其温度,压力,和密度的垂直分布。 ; Y# k" b4 g" X/ D p, ~分器, 6 f0 k6 g5 t) O+ H% _由输人电压,输人电阻,反馈电容和时间微分而决定其" t9 ?7 R# T& S, | 运算放大器。 6 j7 K+ m( R! ^6 Q* _7 ^wing structure (spars, ribs, skin) for storage of fuel on " A/ E. t- u8 ^) K. z5 E5 X" ]the airp4 S& G. n2 c5 _ INTEGRATED CIRCUIT, A small piece of L6 I, e; T+ p1 p- ~. _ semiconductive material that contains interconne% \- p5 n" t* V/ l& Q- O miniaturized electronic- j8 D8 }5 Q0 D9 n& h) j% H# | INTEGRATED RANGE, Tabular Operations8 B# g6 k) j) \: `3 k5 t p* P$ n5 n- N1 ~' ?. M1 J& B c: A1 F/ a' ~. o IN) {# G+ d; x F8 q/ R- d- O0 g: T. M th 7 Q* U" B' q* r$ c ]0 G4 y, S% binternational air route. ! t: s0 A4 `: u8 \; {* m6 OIN $ X. Z% B& N0 I/ f0 ^T . c) q. T Q- h# m. q/ v% r/ Kte4 W4 T& _! N) q z/ S International Civil Aeronautical Organization (ICAO # h/ q! D) Y3 D1 r! _: Z8 pIN5 u1 @; y; `7 | {! U v* o$ {* V" [" t( Y3 B resistance, the feedback capacitance, and time 4 Z% _5 V* Q- B/ r, t% o" \differential. x& L5 z* N. P( P* R/ Q6 z0 s6 D整体油箱, 2 Z1 M8 O( ]% R$ N9 u8 F$ W1 l0 O由机翼结构件(梁、肋、蒙皮)组成,用来在飞机 L6 ?- A' h3 G" K3 l: l4 T: [2 V; t+ c" L4 ~7 f/ e集成电路, ' X" A. P# g, t一小片内含相互连接的微缩电路的半导体材料。 V6 N5 z5 d3 b0 } 综合航程 6 T( M4 n8 g: Q1 i: y* s( Y2 \7 g5 I使用手册将航程作为7 l/ v, `' I- t/ \" k0 i! T. x8 M: U2 ~) r4 q8 F: D- @0 N2 @, M( a' x 量。- L( B, n+ _: e, h7 c8 `# X, s+ L- s: N8 ]/ x5 ?6 } k/ O% |# ^$ E. o% T. ?/ T& G/ g z- a \& C1 ~/ C" { 输出电压的' W2 P3 U# r( A) S, `6 k2 I 英汉对照民用航空词典B OEING , P6 m4 B. M, j7 ], Z' O8 {" WTECHNICAL DICTIONARY 83! Q# N* V- O; c4 [- W INTERLOCK, A wire connected in series with an, }" O k$ a+ o- l. O/ K equipment or device, or a condition that allows4 D$ O4 S, M! G9 ]' Y+ b* P operation if all requirements are met. ( X0 Q8 ?" X8 t0 r) @f the United Nations whose4 J& D6 c& {. W# m6 m: t bjective is to develop the principles and techniques of ' _' x, a$ e# a2 E1 Wternational air navigation and to foster planning and / N/ i3 X# T: p( y. G" A; Tevelopment of international civil air transport. : y. J. ~) X+ R+ [9 I$ _4 {TERROGATOR, The ground-based surveillance0 a, g0 i6 l' f% V dar beacon transmitter-receiver, which normally scans2 @+ S$ ?( I1 M8 K ll# Y/ m. o! q7 D( Y! p on the mode being used to reply. The 8 b# q9 S+ E3 B# \8 t& o9 y( _plies received are mixed with the primary radar . [! h6 v4 B3 _- f0 }turns and displayed on the same plan position radar ( E# Z5 t! i! j$ R0 lcope. / f; L8 b3 a( T; z) E A* j* `, KTERSECTION,& n* |; u' n* l# P! c' l 1. A point defined by any combination of courses,: k2 y% Y3 u! V$ X$ R radials or bearings of two or more navigational4 @5 ?1 C% g/ D4 w aids. % A' r G. u# t6 i: ?# O* d- r2. Used to describe the point where two runways) \4 B" u- f. m) z2 l# K) M7 w cross, a taxiway and a runway cross, or two 0 T$ {* x5 _6 y9 `: X1 gtaxiways cross. 8 [) V+ f, ]; x3 fcy)3 X) r: i* [. n7 n* V/ {5 B tem.3 o$ u& G/ H# B7 ^8 P+ N0 p0 i4 Q( C) f7 b- m4 k5 ~9 m 当所有条件都满足时才能工作的状态。, |0 p/ p% |9 X* v9 j 组织, ! E8 ?/ r9 l2 m+ T) }航的原则和技术,促进国际民航9 o* E7 E8 U; ^% U7 z$ z2 | 输的计划与发展为目标的联合国专业代理组织 " X- m3 L( b6 \1 `5 l4 Y问器,5 p: M$ m, `& [" d A 一种地面监视雷达信标收发机。通常在工作时与主雷达! t+ i* O3 J, P& `1 Y0 B: I3 ` 连续的无线电信号,不断地重复要求与6 u: Q3 d& u! k5 x, y4 f 接收到的信号相混合,显示在同一平面位置的雷 1 H2 f2 ?! [: @* e2 y9 @: Q达屏幕上。' }5 \- b8 U' b( }0 Y L$ [ 交叉点, 7 N- L4 |4 m, G1. 由航线,径向方位线,或两个以上的助航设备 $ w' F2 M5 L p4 ]* Z: k/ N* s9 k- g的方位交会而确定的一点。0 L8 p/ T" S% M9 R 2. 指两条跑道的,滑行道与跑道,或两条滑行道1 i( o& J* Y* o% ?% r 的交叉点。 1 @* A8 N% ~ p) ?+ PINTERNATIONAL CIVIL AVIATION ORGANIZATION,8 b: b. x8 F5 P5 u9 D6 |, p A specialized agency o 0 J; o$ J5 p; L0 mo : I" I; p: p3 x8 n5 h) K+ yin4 L1 \( n3 H0 t% r$ Q d Z: L# {& x6 Q, I$ |1 V& b" {# c: h1 ] IN6 w9 f6 p7 c3 S+ H* K2 V ra 2 \. h- o. v! Q0 q/ ~1 uin synchronism with a primary radar, transmitting * h0 S5 l' m1 F$ A# Ndiscrete radio signals which repetitiously request a( S& A X* Q$ f8 R+ ^9 ~7 H E transponders/ Q8 t- j4 b% x/ ]# S3 y6 } re3 I' p) s- q" [ re & e7 J. f3 B9 @7 js ( a% U; G9 B* ?1 l" B& R1 [IN 2 d9 Z) \- b) b1 YINVERTER, An electrical device for changing direct, x" P, F$ ]; q- d( T( K current to alternating current for standby (emergen8 c. c: x9 a6 e% W x2 |3 q power supply to electrical sys# ~2 Z; F8 r0 ^+ s* ] 联锁, N1 Q: W+ X* d" h# R 一个以串联方式将仪器,设备联接在一起的电路。或6 ~. B% P: `) P% K* y- e b0 j- q% e国际民用航空4 @- M, w! w, {; ~ 一个以增进国际航空导9 K/ p4 j0 [7 e4 E6 n" e: T+ q g6 G, U' V( \5 b* O1 [0 A3 X* l同步扫描,发射不 7 k& n+ k. y& Y; k其工作方式一致的应答机进行回答。所接收到的回答信号 3 m( G: W% }5 P! |9 }) k9 f) @5 a与主雷达 x/ B3 T# Z+ m) o8 h' x6 f$ [变流器, ! t, O$ O3 \3 }& j0 E用来将直流电变成交流电;以供电气系统备用(紧急) c3 z; S O" H2 v" R6 ?/ W 电源的电气装置。 # x5 [' r- ~3 f. Z英汉对照民用航空词典B OEING : }. t, A; d, pTECHNICAL DICTIONARY 845 u9 [$ a$ p1 u9 f& q IRS, SEE - INERTIAL REFERENCE SYSTEM 2 n' Y. }) J. d3 `ISA DEVIATION, The amount of temperature or# h6 j8 l" H' h8 [7 m( @ see International9 [8 r" l2 S/ U( u g6 P tandard Atmosphere). 0 i: ^* C! e. D/ k5 w) b* LLAND RESERVES, Reserves required by the . L* h; M! `; {& r { F2 Kpplicable governing agency when flying routes 1 T* h/ g: D2 E" ^( U% Y* \0 ~2 Detween islands with no alternate airports. ; @- \3 O5 F) |% f$ O4 ?& BCONDITION, Cabin pressure (altitude) |$ o/ p$ [/ r maining constant with changing airplane altitude.% s c& r! g8 y: S0 O# w ising the1 L7 |) H: ~% a C/ i a # f! O9 u, [3 S3 n( u& b! z: s3 z, i R, o5 S/ |/ K pressure difference from ISA (4 D( }* u$ { {0 z9 s3 X S / S1 L/ }5 B) dIS + ^) l- }5 I7 M- `$ Ta % Z, P2 M6 R; ]8 `b ) F, P5 w4 H/ h* iISOBARIC( F+ R1 U$ }0 u re + M. P6 M+ ]7 U" I# U5 v) eISOLATION VALVE, A valve in the system for; H7 B- U/ |# [ d, m, m3 F separation of the system into sections. ( W/ T: |& H4 @1 E' wJ 0 m' n: s: M6 f5 ~& P3 \0 a; lJACK, A mechanical or hydraulic device for ra8 P7 X+ v& I7 J: [9 s _ airplane.6 M4 v( h2 d. Z6 f( H JACKING POINT, Location on the airplane for using2 v4 |/ E) g6 _ jack. / Z, t0 h7 e' e8 Z+ f1 T7 x惯性基准系统. v3 T, A$ M0 H* o# f9 A* N5 C 见Inertial Reference System. 3 c' {9 |. ^- a$ T% D与国际标准大气之偏差, & w' q4 o( { G0 i% @7 o6 r0 U: }压力与国际标准大气的差值(参见国际标准 ; o7 z9 z5 X# V. @有关政府单位要求在没有备降场的岛屿间飞行的飞机 . p' B1 o5 \& H带的备用燃油量。% [+ n: m( u( k, N6 G5 w1 o 压状况, 2 i+ P# I5 j3 B在飞机改变高度时,座舱压力(即座舱高度)保持不变0 D$ ?/ ? V0 d# j* e 状况。6 d, ?3 Q& n' L. t( y5 K 斤顶, # N1 x. V7 t0 q$ v用以将飞机抬起的机械式或液压式的装置。 2 h4 q" }- N- v* i, Y" @" f温度或 3 r2 t& h& f0 g2 Y; Y6 P# {2 n大气)。 2 |* g& K/ ?+ `+ J" ]! D- c/ a9 F岛屿备用油量,) @" A' z+ G! U r% b% t! ^& K; T( ], C \- C- z. c& ]1 V6 z% H9 q o4 v5 }0 O! ? 隔离活门, , `7 w' {% }7 @2 D2 D% P用以将系统分隔成几个部份的活门。 5 h( ^3 [! S1 a2 h" M$ W3 W, C9 u# ?! z1 c千斤顶支点,4 ^' d, G: S2 X 飞机上可以让千斤顶吃力的位置。$ I+ O0 n% a. T. V 英汉对照民用航空词典B OEING 2 ]/ C5 k7 K- b3 UTECHNICAL DICTIONARY 85 , O4 }* r* O! D" q* W! k# @JACKSCREW, A rotating threaded rod used to drive5 Y1 Q. i) i( V1 l2 j moveable component such as a flap or stabilizer. # W6 O4 H9 y7 k% I* _a 致动螺杆,+ ~: s( n: J F k5 r& Q 用来使可动部件如襟翼或水平安定面运动的能够旋转# G0 R, [/ t5 D3 W! l2 B 的螺杆。 % M2 S2 L5 `' o英汉对照民用航空词典B OEING; u4 f+ `2 R4 d; {' I TECHNICAL DICTIONARY 86$ P+ q! ~5 y% _! M; H5 F/ | JET PIPE, A control component in some valves and 0 d' u# N4 }2 O; Z: VET PUMP, A component in the fuel system, operated - A5 }% \+ }. mr removing water and fuel from a fuel! A, q0 h0 f5 ^% N8 ^' @ nk.7 F7 I' |+ q: ?# K! l 射泵, 3 ~- F: T( g+ I6 k+ M( J M内,由燃油压力来操作,用于从燃油箱中排除 - E* O/ S5 v/ N B9 c2 P, I和燃油的部件。' |9 c! ^- U2 d/ W" `! K3 l4 g: R( B actuators for controlling the flow of hydraulics or& [+ Z- v/ W% j. t5 | pneumatics. 0 R. r( l+ U, ~9 G) Z4 `- pJ! I0 Q6 v$ ]. _+ n. x by fuel pressure, fo 0 b C' t& G! u6 v2 B% O, Y( ^# K0 J* Wta. `# Z& @3 A/ @3 Q9 d6 }: y 喷射管,3 E, O2 w0 b/ \- r& `$ ~$ R5 g* i 在有些活门和作动筒中的控制元件。用于控制液压和1 ~* L& E: v) ?5 }- y 气动的流量。 9 I* @# `7 C, q: [6 V. |( s: ^$ H8 G$ Q$ R 燃油系统3 L/ b: ~- {3 M) y2 |) j" x6 ?3 _4 t" _! G: @" Z# k( B$ S7 k+ s3 D/ T 英汉对照民用航空词典B OEING * w! B& z( c# s! j8 _TECHNICAL DICTIONARY 87 % x2 F/ |* K* E2 N1 Z/ w: @JOGGLE, An offset in sheet metal construction 2 ^9 o$ z4 ?5 O% C% E: ~designed to allow one piece to overlap, either higher or0 Y7 T8 t. h( H9 `$ N7 U U1 E6 g wer, the other piece.' ~( v% U6 [, j" B2 z7 J( e OULE, A unit of electrical energy of 1 ampere of ; H3 {1 b+ S- {* Surrent passing through a resistance of 1 ohm for 1 3 {) k& q9 t) q+ w9 \* \econd. Ignition system energy is measured in joules. ) Y. B" H, r$ `% T2 J0 R4 G" EUMPER WIRE, An electrical connector for temporarily 8 C& v8 k4 i( H% \ypassing part of an electrical current. 3 m, G+ j6 R0 MUNCTION BOX, A container which serves as a joining ; f7 f" y( y& N. h/ ilace for electrical connections. May also contain ; B2 P h* a: A/ d: flectrical components.( e H$ O7 D: ~* c% _6 f. E0 \ EEL BEAM, A structural beam in the fuselage center1 @% o8 I3 P+ O ection (wheel well and under wing center section) to. C) P1 K" U5 L7 f6 c KEVLAR, A light, strong synthetic material for 4 a0 |8 Z6 r7 }) J7 G wsecondary airplane structure. 6 W+ i0 H7 ^& R,使一件金属与另一 v# {7 p% @$ [7 {% z1 A. F 相互叠合。/ G: q3 O0 X8 W9 l 耳, e8 {2 U3 r+ |; X( b7 |1 { 电能单位。一安培电流通过一欧姆电阻一秒钟所需的电9 Y0 F+ {/ x" }# m1 G 为一焦耳。点火系统的能量用焦耳度量。" z9 D) G. ]+ o1 h' M0 d 接线,# P5 `2 [8 }$ s: J0 J7 @* w7 W1 f1 l 用来暂时旁通部份电流的电器连接件。 ( k- m" B1 R3 ?1 b2 J+ n- g4 a线盒,7 x5 W+ K& i3 \9 H 做为许多电接头的汇集处的容器。也可能内含电器。0 C% }) o. L! B! M9 k4 x0 b: y; k: N 梁,5 a( [; y' f b( O! B7 |1 }6 F7 @0 R 机身中段轮舱和翼下中段,用以防止机身弯曲的结构。% ?, a8 g% t- \2 J) W2 R KEVLAR,0 D1 R" ]$ N0 @7 }& @* c( r: b6 c# A 一种即轻又强的人工合成材料,可供制造飞机的次要构 ( L; F0 j9 u# S/ g件。/ Z0 _% }. l# I' y" H4 S& ~1 B lo & F( r% Q% i4 B+ K) |% X4 iJ( ~6 Q% H) \! J$ H2 ^ c% C, p- z2 P T8 d( A% J- Q s7 N0 y' B. ~+ ]; |, ^5 s& n) W# W0 C J * |& I) p" V6 z) P) j) B3 d/ rb k0 u" r, X" u, F: y% cJ6 I- o9 k% n2 \# J& T2 g5 u" d( n p1 Y# H& j" ]: K e 2 o7 s/ ^0 g# K( p1 s9 _K # T0 r: z$ A( U! SK! A# M. F% j8 W _6 ^$ r3 _ s$ b X ~5 y2 t0 E6 t prevent the fuselage from bending.3 F) F& g3 m3 l 折接, j: L- k' a1 Y8 C- a 一种平面金属结构设计的弥补法 0 K% e$ e- R8 n/ O) e, E% O; M; K0 o* [. k* ]2 \! ~/ P/ I$ n' o% n7 a$ T5 n6 _$ c* ?6 {" C6 `* ?! s8 [# F: H% Q: w* p5 T/ B. Q7 \" k( W$ S& j+ M' k; c" a# v8 k1 ]( o) p4 c' f; ?英汉对照民用航空词典B OEING3 G: C+ o! f& H3 g `! l/ I* K TECHNICAL DICTIONARY 886 p3 t* G7 L( m, Z5 K3 j KILOWATT, An electrical energy unit, equal to one ' z1 r8 n: X* Ithousand watts, for specifying generator power output.3 y! j3 d" x: n# n) B) s KINK, A sharp bend, twist or dent in a section of tubing,. |3 _0 Y O: E8 C wire bundle or angle stock. * p# H+ C! u( p7 bKNIFE EDGE, A very sharp edge on drilled or machined 7 D: b# N5 w5 W7 fmetal which is usually the source point for corrosive' q7 m; o- U$ ~" T attack. - a9 _; M. K& z: [- ~1 U0 bKNOT, One nautical mile per hour. - k0 l( }3 D# ~, CKREUGER FLAP, A type of leading edge flap that is' N2 I, r+ \' _- l* Z' v% i fixed on the lower side of the wing and rotates forward- @& M) i& \# ]4 d into the airstream.' M; a5 n Q& e5 S1 W* i6 { KW, SEE - KILOWATT ; g% T7 f+ Y1 Q/ Q/ o8 |L6 X+ O) M1 G2 Y- C, c9 b LABYRINTH SEALS, Rotating and stationary 3 T% v; H1 ]* N) q4 \. T% {overlapping structures which utilize differential air / B, g- u; [) J$ b8 A# R& apressure to form an external seal. Most commonly used : n6 C5 j( {* O- B3 o6 x4 din turbine engines.: c; b {( n& u 扭结, 0 j3 C! t% W8 v* [/ c* k在管路,电线扎,或角材中的尖角,扭转,和凹坑的部 t& t$ ]5 U; F! v: s; ` 份。6 Q/ E4 U a6 { 刀刃, " ~9 j$ s1 }$ h3 [钻制或机制金属的锋利边缘,通常是腐蚀的开始处。* m- Q) B; Y3 b$ n9 ?3 W O 节(K,KT,KTS), / R" ~* e: {) B1 o: ]7 O9 V每小时一海里的速度。 5 V5 P: @' `5 D7 h克鲁格襟翼,( e) ^! W0 r. N* Y2 b 一种前缘襟翼,位于机翼翼根附近,旋转前伸。 ) M3 X6 @: C. Y4 t/ D- T8 w' l千瓦, , ]$ R$ [# {* D7 @见千瓦(Kilowatt 8 I3 E! R( x1 T千瓦,, |6 L0 ]6 s! R 电能单位。等于一千瓦。用以确定发电机的输出功率。 9 K0 c1 g; G- f" p3 X)。 : F j1 h/ Q2 q蓖齿型密封装置,. ~3 o6 h0 p3 t0 e& h, D 旋转并且固定的重选结构。用气压差动而造成外部的密4 g& l9 v& b4 ] 封。在涡轮发动机上最常用。' u9 p8 M1 \ T- Z+ U" z 英汉对照民用航空词典B OEING% I3 }$ R! P( r1 w) D TECHNICAL DICTIONARY 896 k9 E8 O1 n+ X! p- Y4 x( M LAMINATED STRUCTURE, Composed of layers of a7 e; b- M7 {/ Y8 D6 s6 J ake a : v* Z* A! P- M: M j3 l0 aht structure.8 Y! i8 u( B# b2 Q; ~ .E.D., SEE-LIGHT EMITTING DIODE. 4 Z+ X% A, D* Z0 EANDING GEAR, The nose and main wheels with the & K; s l) Q' G2 \) p L, X# Q4 dttachments for supporting the airplane on the ground. : J1 ~1 r& L' Q ZLANDING GEAR DOORS, Panels operated by the+ h; l1 B6 z9 _/ e) L1 h landing gear for closing wheel wells when the landing4 T$ R- g0 z8 a* P. a gear is retracted.- @. }, P6 A" m# _8 f, c LANDING WEIGHT, Gross weight of the airplane at the 5 U, I( t R" odestination or alternate airport.$ D( t2 I3 ^3 j! W 发光二极管,1 p; [/ ^% L3 q% t 见Light Emitting Diode0 f. L4 [2 V5 u j# Q composite material bonded or cured together to m! W0 l+ G- A) Q4 u @ strong and lig% e3 v l3 g1 ~ v L 3 L% J; V" j0 oL4 N- k) R8 m1 r* ?- Q a& w# F' K7 f0 G: i7 Y; i 分层结构, 3 F+ c* y, o5 b; ~9 j* l/ [; x一种牢固而轻的结构。由多层的复合材料胶合或固化而2 o6 {7 W2 B3 H, o' C. N0 z 成。! F: k3 h% V% b4 y* [# y1 A5 J- c0 _% E. ^& P6 k起落架, - r# s) s( ^- o1 l* F1 t! l2 _( C, {用以在地面支撑飞机的前轮,主轮及其附件。 1 Z" J2 y( f9 q/ p. {- h9 L起落架舱门,# ?8 u0 Y; a' D) b2 ? 由起落架操作,用以在收上起落架后关闭轮舱的面板。 7 {: \% {6 p! [; G着陆重量,% A, h0 a5 i3 a5 x 飞机到目标机场或备降机场时的全重。 # e& B" Q% g7 N英汉对照民用航空词典B OEING ! B, J8 r, M$ \) gTECHNICAL DICTIONARY 90' D! N6 A1 K5 ~ LANYARD, A cable for supporting or holding pan) W* x+ ^: ]+ u$ z' _5 G open position./ Z6 I: F `: [9 ] n# u els in 4 [/ I2 s. K+ a2 o: Z, T- SAP JOINT, An overlapping sheet of metal, joined to the ) L, X$ }% v8 c/ Xdge of another sheet in aircraft structure. 4 X; @" z( Q6 wASER GYRO, A gyro which uses two laser light beams8 w/ p9 J! d+ J- A" e measure angular rotation. " Y+ d$ Y9 e5 g: _+ g. 4 C2 {3 Z: @6 OATITUDE, Measurement north or south of the equator% E% M, E8 w3 w/ z# M- g s, minutes, and seconds. For INS equipped , N* C& o2 I7 y1 |* ^5 ]degrees, minutes and tenth of minutes. 3 L9 Q0 r' V! V4 \" hl device for8 \7 w0 a: t: c& G5 s( W# l v hanging stored chemical energy into direct current. , f8 i* [+ d# ]/ wses lead, lead oxide and sulphuric acid." S- k' d/ _# h; G7 F, c 搭接, # R+ P! Y t2 E" r& S/ L飞机结构中与相邻金属薄板连接的重选金属薄板。 5 c2 F- `/ X$ q& Y" N激光陀螺仪, l, J( E6 i G9 U: Y 一种由两条激光光束来测量旋转角速度的陀螺仪。/ q$ |! ~% ~2 b2 Y3 D1 \5 K 用以紧固或锁定的装置。% {0 Q* r5 m( i7 E+ k 的轴。 8 W& b- F8 B9 @; B" ?" I e( x方式。" }5 M% B" I0 ?" t$ W 度,7 d( R* H2 b3 G+ ]+ \! [1 c 地球上与赤道平行之弧线。由赤道以北或以南度、分、 g1 j5 f, }6 u8 @1 Z度量。对于有惯性导航系统的飞机则以度,分,和十等 + s& M( f! b) v( Z, X, t( `' w/ r度量。3 w! A" x4 f+ K, P& Z1 h 酸电瓶, ^6 Z4 W8 `. P/ `将贮存的化学能转变为直流电的电气设备。它使用铅, ; _6 I. T" d8 I; C化铅,和硫酸。 2 R3 i' M' M# J$ D) D: OL) V) A! t1 t+ S4 {9 i1 A e: T6 R; g6 `2 Z2 H6 n& K L 4 n A6 n( k' C( q. \. d6 Z! bto* B1 W+ p) w" S LATCH, A device for fastening or locking. & t4 b# A7 P% R/ j2 Q6 p! F' s1 JLATERAL AXIS, An axis passing through the airplane's" r! v5 ]: |3 m center of gravity, from wingtip to wingtip ' g6 ^1 K1 \+ u7 Z! BLATERAL NAVIGATION, An autoflight mode in which 4 V1 H) C& S7 ?# kthe FMCS is used to control the airplane roll. r! E2 b x8 e L+ p* {9 c+ e: C0 r( W in degree/ J& c1 P. @! |8 x aircraft in' Y$ g# A2 |- U( b LEAD ACID BATTERY, An electrica: g1 W/ _% `2 Y0 @ c$ i, V1 {, _" g3 x7 e1 b U y) O0 c9 S* N1 }+ R L" U 牵索,! G3 V- A7 X2 |! V) y$ ~ 用以使面板保持在打开位置的钢索。1 U1 Z$ U* F- C4 o$ }4 B 闩,% e/ S9 D1 M2 B. i4 b; z 横轴, E( U9 S% b; [6 S6 h/ l9 U& g通过飞机重心从一侧翼尖通向另一侧翼尖 $ Q% z+ f& c$ e3 e水平导航, , S1 n1 J f5 F, b5 d5 Y使用飞行管理计算机系统控制飞机横侧的一种自动飞 4 ?4 F: u$ e- v# a- X) `5 A. S8 _0 k4 d' H1 ^' P! t5 j8 @- w/ u! c: s! i6 ]9 q+ k: z7 l' _7 B% Z! o: P. T& ?% J* w4 K" K, u( V) J8 z' ~* G: X/ A2 a3 X7 }# G" x1 V/ A5 D4 Z英汉对照民用航空词典B OEING 6 z! W. l& |! t4 JTECHNICAL DICTIONARY 91 1 u' R" e( [ p6 e$ R& sLEADING EDGE, The front edge of a wing, stabilizer or! q6 v$ h, ^% I) ~( w$ @2 w ED, SEE - LIGHT EMITTING DIODE, ~5 x' F# y& a EMAC, Acronym for Leading Edge of the Mean - z. [% C8 a# N& g$ I# z$ Terodynamic Chord.5 d r$ }9 D' j) [9 O2 Q6 a- y2 H IFT, The vertical force produced by the airflow past the 0 C5 O: A* K7 D, j5 Z" L2 ds of the wing.! M2 v3 W" V8 b. T IGHT EMITTING DIODE, An electronic device which q3 ~% [5 A/ K/ d2 [ tes with red, amber or green light when supplied( i* O/ L, J6 x+ ~ ctric current.% E3 p, t- v ? y" U: E. r7 v# z7 P- w( }" N7 Rcontrol surface.( w; R0 n& V, U" `! S. E2 w" K LEADING EDGE FLAP, SEE - FLAP9 r$ K+ M( Q Q7 T7 k: `& e2 c% F L" g& x0 N8 Y9 o L - a# g6 b1 `( a1 aA* @' b& S0 k( m( t+ L H: U. r LEVEL-OFF ALTITUDE, Altitude of which the airflow 6 h' Y0 w1 [+ x: Y% P& S' P7 upast the upper and lower surfaces of the wing. % D" R6 g1 T. ^- oL3 Q4 f8 H. L4 d# }+ c+ V2 i( J upper and lower surface 8 T" T* J' ]. c) [L 8 r+ Z4 Z# h6 X& T' v ]# villumina" v! y1 A/ V) B8 o( L with ele! E6 N2 W) X% K. t2 R 前缘,7 t7 N6 E8 }; b5 h 机翼,安定面或操纵面的前部边缘。 ) j6 A: N0 U* P% z2 S前缘襟翼 2 |. W& _3 L* e W见Flap.3 ^, y2 o+ N, [% v' k5 D# g 发光二极管, ! H% Y1 L0 l* v5 C3 M7 Iht Emitting Diode. v: o% e- f: M* k0 C' z% t/ g 见Lig . 5 ` i S5 i- M' R) z均气动弦前缘,: A' _, e2 y% F 平均气动弦前缘的缩写。见Leading Edge of the Mean . n1 ]; D* G6 V3 p) F! U& m1 M0 H9 O5 Q; Y- E- _ Aerodynamic Chord., [/ _' a F5 V9 l& a; ] 力, 1 x# l: R2 B1 ]7 `过机翼上下表面所产生的垂直力。 % Y- W; D+ h9 g/ V" C" H光二极管, + `% V5 B4 ^1 c8 K通电后能发出红色,琥珀色,或绿色光的电子元件。, w% s7 U- | H. H( t; J8 j 改平高度,4 y1 d$ O2 P5 J" t" a W7 C 飞机因巡航时发动机发生故障而下降至的高度。 + n2 l9 R5 I5 V' l- s% d% R' `7 }8 o3 r" Q$ J& b+ E, |+ v' t: D气流流 ! Z* Q7 l4 T" d1 {" ~- C9 R4 a0 y3 T1 I% d) [+ H: ~英汉对照民用航空词典B OEING% Z7 s( z; o; z _. ~ TECHNICAL DICTIONARY 92; O- i6 f6 e) X+ B, L LIGHT PLATE, A component part of an instrument; m& ^7 Y+ s9 C. S3 |- q) D, h f7 ~ panel for illumination of words on the panel. 2 q0 {1 n' ~9 _8 Y) \5 MLIGHT SWITCH, A switch which contains a light. The / s( {7 t" L) n; `' ~5 R5 sopened or/ m/ B' q; M7 Q5 X4 b" h# c1 v6 S losed. . P- C6 o: X# H7 un electric actuator which turns off electrical power to/ F1 ?6 w+ r5 X) c1 _ e actuator when the actuator reaches its open or9 z4 d& t/ z# w3 N6 d1 ^- w losed position.: I+ z, A2 {0 s1 d. t IMITATIONS, Performance and operational limits5 ~: K0 g2 ?% e) h sted in the Airplane Flight Manual (AFM), such as* ?" B( e C2 o0 E6 L( F4 y aximum airspeed, maximum altitude and center of7 _. y4 M$ A9 w6 [ ravity constraints. ! K) x) r* n* I0 _/ y( H, ky! t9 `; m0 J3 O/ {, t craft during line maintenance3 R9 g, u5 K# S V6 ?$ t perations.7 h& y s8 v% ~ I ontrol K3 _0 p5 ]7 U" u display unit allowing control of information to and from, Z5 b' {+ q5 M the scratch pad and designated areas of the display. + ~& ]6 F0 J/ x9 r( S5 X* ^- M- ~光电门, - \* J- m5 h! a1 T4 v/ y电门开关而决定灯的明灭。 B7 M& h. j5 ]6 w 在电作动筒内,用以在作动简到达打开或关闭位置# G" `9 D$ g; `( H 时,切断电源的机械式操作的部件。 3 n; M) }6 [+ A4 \: u; q8 L2 z各种极限,! {; s z9 p* E ]8 s' } 飞机飞行手册(AFM)中列出的性能限度和操作极限,9 N% _! `+ o, d) s 如最大空速,最大高度,和重心的限制等。0 q( g3 s4 T5 O R. Q9 m 在航线维修中,可以在飞机上即时拆换的部件。+ h* u- l8 I8 @2 i0 @7 z 飞机管理控制系统的控制显示器上的电门,可控制草稿0 x1 G) R' ]( b 栏和指定显示处信息的输人和输出。9 b0 c: r3 Q* K1 o& O9 ? light either turns on or off as the switch is % P( v& |% X, r! g& _c B i; y' c8 `) A1 ULIMIT SWITCH, A mechanically operated component in" I- W x. L- U; t+ A% O a& M0 Q% `3 G8 B# s/ M; U th, ~5 u. a6 c$ i, C( t c + ]% y0 G% l6 C% [2 z: Q$ z. \0 yL $ e' C7 a( {) Dli) w+ q0 f# i# ? m" L0 F/ C9 I- r g & r) |. q+ |+ g9 |5 g% i3 G" p" z$ dLINE REPLACEABLE UNIT, A unit which can be readil ) G. A+ y( ?1 O* m+ M2 T3 ~5 K! achanged on an air : i& O3 K- k' A" s$ Y) {" \5 Vo % Z' Z8 c1 i4 u4 ]( LLINE SELECT KEYS, Switches on the FMCS c! F3 n* [" H. H+ ]$ \5 H 照明板, 1 H" v4 C# }! W4 {( ]9 ^" j仪表板的一个部件,用以照亮仪表板上的文字。' i# ]; ~: j8 N1 y. L2 N1 X5 D) q8 G; d# h7 Y 带灯的电门。* b7 j" T! `$ b. I, s" k. S" G 极限电门, ) z; h6 P' {+ _9 U. Z9 x航线可换件,! n- y4 p& O, @- q 行选键, 5 o9 S7 Q; A# K$ L4 j; K4 `英汉对照民用航空词典B OEING + z7 j3 ?9 L/ v- O, gTECHNICAL DICTIONARY 93* N" k* D% ]4 s" s+ A% l LINEAR VARIABLE DIFFERENTIAL TRANSFORMER, * {. a/ Y% \& p( N2 s* o8 y0 @nsformer with a linear response. # D. P, y1 X( F$ N6 ^* A! ~6 HNAV, SEE - LATERAL NAVIGATION) p2 M, e: E5 h& c( T OAD AND TRIM SHEET, A form containing tables and 6 O% E8 x* N$ H$ S' wharts to account for the weight and balance effect of all 4 H( Q+ v. N! j5 ^3 K' j9 ?pe of an+ L8 C( w# e% G* q; Z7 D: C! ^3 t S approach, normally located at or near the point of " f- O. [" {6 o) C, N0 {+ }/ @ecision height. 1 i1 Z$ b- B4 S1 _$ H7 i. E, Ter . X# m; b/ @) g& }& Ceacon at or near the point of glide slope intercept of an1 d( q" g- G3 I8 Q S approach. " h/ Q+ _7 k7 \; l0 {ich provides. d, z+ d( P8 L! N. A lateral course guidance to the runway.3 a6 |5 ?/ A: F( k 差动变压器,* o5 g! _7 r0 s) k 平导航,# z `' l* o" B4 p! T/ i vigation 8 r6 E/ m$ m3 m0 q3 hA differential tra; ~( d. G. T: \% D7 R LINK, A short connecting rod for transmitting motion.. s0 Z& w+ Y4 H Y7 y |. r L 9 U f! a, L. S: v6 ~L# D8 n0 t& A( ^4 q4 U! P& | c/ @. ^& v# _" S6 e! i7 n1 r5 E! D items and fuel loaded before each flight. 4 Y+ [7 s4 x0 ]# w" v* Q4 g# ]LOAD FACTOR, The ratio of the lift being produced by4 b5 I: I% X/ d# X$ D+ ` [/ \% \ the wings to the weight of the aircraft.( W2 Y2 h+ y) q* j4 m+ H; P" T$ v LOCATOR MIDDLE MARKER (LMM, MM), A marker 3 W/ S. n8 O+ k, Y5 i5 Kbeacon that defines a point along the glide slo 9 b3 Y& V8 P7 ^IL 9 m/ [7 a* |7 f( J; F0 N2 G) hd 3 O3 j: S0 t8 K2 R5 SLOCATOR OUTER MARKER (LOM, OM), A mark ) _ p4 @3 K% W+ k+ bb0 d4 u% {- {5 n9 t3 T! p/ V IL 2 l- q9 _0 G% }LOCALIZER, The component of an ILS wh / `% w p& l2 d" h- o; y+ r线性可变 % ]$ P9 ]( l! N: }& i' l5 `! V0 F具有线性反应的差动变压器。 8 r: |0 s# v2 a连杆, % P" c& [/ J- O! [, ~& O连接在两个部件之间,用以传递运动的短棒。+ u. p# e7 [4 K. n5 s+ f6 l9 A5 q1 Y$ N见Lateral Na .- e- p2 W- f# N* N 重和平衡表, ( o7 N- n8 c5 a( v有着显示每个航班前飞机的各项业载和所加燃油对重& Z5 d' y: g; @6 ~; O/ O 衡影响的图表的一种表格。 9 I8 c' k. |& [$ D9 L: I) N" _/ X" G5 G* b r( K( n6 K1 a2 `附近的一点的指点标。 % I. e) [$ x+ v8 }3 T N近仪表着陆系统的下滑道截获点附近的指点4 A1 o3 M. m' [$ _- D% C0 T9 L* o) P仪表着陆系统中的一个部件。它能提供到跑道的水平航 + ^/ \( g9 ^. n) T道引导。, y; X8 I3 Y( s, @; T1 s0 A, \- n8 T* m! u 量和平- ?1 i9 X0 {( k3 Q4 h' \ 装载系数# d" E( t9 x: W2 ]* I1 [' } 机翼产生的升力和飞机重量的比值。# ]4 M7 i& N, R8 R" P1 A8 R 中指点标,- b" m0 T* K5 r( W4 p7 N& Z# f* B; @ 用以指示仪表着陆系统进近的下滑道上通常相当于决 - U9 c% H; x( z+ J断高度或其 e3 y1 A/ M4 X 远指点标, . ?4 o1 I' u7 f5 G/ |% h, y. p位于或靠6 h8 j$ m) h; |0 l2 x* v: v3 D# D) @5 r7 R/ P" @9 V8 L 航向道,8 o7 C& v% Q* b6 B5 R$ e 英汉对照民用航空词典B OEING & m. k' G+ w3 K$ m4 s8 T- L$ STECHNICAL DICTIONARY 94! b% _1 A3 Y) _( I9 y% }; v7 B LOCKBOLT, A steel fastener which prevents unwanted $ {* Y/ a* {3 C0 Erotation by using a collar instead of a nut.( q0 C. H/ a \) k OGIC, A representation of complicated electrical and) i% ^/ b3 x0 d/ f& z lectronic circuits by simple symbols called logic1 ?: F1 z1 Y: `3 }+ f2 z8 S$ y ymbols.4 S2 @7 L/ E( z8 U" x! ` OGIC DIAGRAM, A diagram that uses logic gates to) Y) }" E$ l: t. ?( W# i present the function of a control circuit.! t7 K$ P- v" V% r OGIC GATE, A device or circuit which has no output; w7 l' b9 T. | ntil it is triggered into operation by an input signal. A 5 q8 c, m( q) B2 ogic gate is an AND, OR, NOT, NAND, NOR, or4 U" n) h8 N2 `8 _9 i8 ~3 _# ] LOGO LIGHT, A spot or flood type light mounted on % B; N7 s$ ]+ R( }; o9 U1 x; q6 vaircraft structure and directed toward an airline LOGO or) h: B; N2 N8 `. a0 x/ ] other message on the fuselage or tail surface; for $ w% A& u- Z2 M3 gvisibility during hours of darkness. 4 W! x: C9 D! e, D2 {; T' x! J) n8 f3 K' R, Q9 y钢紧固件。+ N+ C& V" A$ |' h F% ? 逻辑线路, 7 m6 W! N @8 b; U/ H用简单的逻辑符号来代表复杂的电气电路和电子电路。2 A' ^2 v8 i- _% J1 j" ~) m0 C 逻辑电路示意图,1 N4 X9 D% X9 j 一个用逻辑门来示意控制线路功能的图。+ H2 T* A' s+ P- D% H" b 逻辑门, ^5 u! S6 a3 q只有当输人端有输人信号触发时,才有输出的一种元件 ' e! l# W' d- `# D* b, g7 H或电路。逻辑门分为:与门、或门、非门、与非门、或非: F/ q: _0 z- H, U* b3 e 门、和异或门。 3 V% x# m( @2 h$ `/ X+ N标志灯,. _4 o% s* l; `- @8 ~. O; z 在飞机结构上装置的聚光灯或泛光灯。用于直接照在机 ) c. j' ^! m' |. q+ D9 D身或机尾上的航空公司徽标或其他标志上,在夜航时照亮/ p8 X; `( a$ M% p' X8 v- U; w9 i 这些标志。 9 w# ~8 x; k5 L$ c1 i' s6 EL; b* }9 L5 u! P e3 X# V$ c) R `. ^ s k* a; e) b$ c0 L) A ^7 C' O% \L9 l0 F8 v& j/ s$ }+ S re : p0 f& o. Y$ F9 B9 H+ n+ XL1 J( M' T' N/ n( K( Z u 0 \7 c* q4 U. l4 q3 j5 E' blo; Z! x2 i _2 Y3 }! ~0 Z& L6 }( b exclusive OR.9 u1 p% A2 p0 K) G# i: S5 e& C 保险螺栓 0 c7 O3 `) m o* s用环圈代替螺帽以防止不必要的转动的 2 i, O8 m) S, `8 U) d英汉对照民用航空词典B OEING & q( w S$ K$ p, V0 n. m* `. PTECHNICAL DICTIONARY 95( C& |( _1 u$ g' J LONGERON, A structural component in the horizon & q( R, U3 d. q; |2 [8 tdirection of the fuselage or nacelle.0 v1 L" w9 K4 y" u& g tal 8 R3 v( r$ n/ q2 ~; J) X4 \RUISE (LRC), Cruise speed that is4 t( ?5 r; I$ J* F ssociated with fuel conservation, producing fuel; R$ K7 ]# D |8 @# f$ U ileage one percent less than the maximum fuel ' ?* \1 u+ S" `6 j) e0 nileage available.0 A; q# n% L% `4 z9 ]6 q9 b ONGITUDINAL AXIS, An axis passing through the & m% y* {: P4 pirplane's center of gravity, from front to rear. ( U3 V7 m f% R1 z- g- m# m) ?* Lnot7 ]2 ?1 E0 G9 n3 v" y OUVER, An opening with slots allowing the passage of9 d2 e& ?. \* I; E. r7 [- W 远程巡航速度, 6 q# A1 V/ M' _: a" [& G: z0 z一个与节省燃油有关的巡速度。在此巡航速度下,每 i0 W. O+ c1 e5 \# d0 E- I 一单位燃油所能飞的哩程,最大的燃油量航程小百分之9 l; E" u6 s) g5 l 一。0 G# I" U& x' N# n$ m- k, g3 U 纵轴, # t" t8 f, G8 x" _5 n" M0 a由机头至机尾贯穿机身重心的轴。 . }6 r7 o0 ]- u) C" `7 p叶窗,$ U4 ~1 }$ t4 U m+ @ 有多条缝的开口。 / |0 y3 b# |/ M% n1 VLONG RANGE C 7 H$ Y- g8 [6 e, B( q1 K. N+ ]! Ga 2 F+ Y$ a8 z- i [) y) mm , P7 R! w& r( fm6 C0 I3 K* a( C% W1 x L ( q& \( ~* N% X {" G$ sa" h9 U9 z4 W/ P& H LOST MOTION DEVICE, A mechanism which does 4 q5 G; @1 _$ D& g. ]0 ?operate a component following initial movement of3 R$ B2 ^5 g4 N4 _3 C" ^1 n control input.3 C8 w, M; h# D( N: l3 }" | L 0 }; X$ l5 h3 {& _4 s" ~" iair. # b7 u, A' i6 I: X' Q大梁, 3 [5 F+ w+ I) h4 c机身或短舱上水平方向的结构部件。& m( K8 f6 W! p. R8 P; ?* @ Y8 V% J2 k- g" A5 B [* Q X) `/ ]& Y空回装置,; ~- u" b6 Z: O* U3 m0 V 在控制输人初始动作后,即不再操作部件的机制。用于 R' ^7 X; y! ` 飞行操纵系统内,以防飞机指令互相牵制。8 _5 o. v" L: n/ K, a$ z. I4 U# P. C; S6 d l1 c, @3 J2 H$ ] 让空气流通的 0 K, a/ }1 m. b: l7 c$ q英汉对照民用航空词典B OEING3 S) x$ n0 b- F/ w" C" ^ TECHNICAL DICTIONARY 96 3 y2 ]( g/ i. h B2 y/ V3 Z! eLOW RANGE RADIO ALTIMETER, A system that 0 V- L+ l0 e7 M4 ameasures the vertical distance from the airplane to the ' ~* v5 I! f' g. Nrrain.! P: m- w6 g1 L# S6 ]' d4 B RC, Stands for Long Range Cruise speed. Represents . o- l8 p9 i. N& Ie typical cruise speed for a given jet airplane; usually. u2 C9 p+ I2 l- P6 w( ?) o- { xpressed as a Mach number. 4 a0 M t# W2 g- l# ERRA, SEE - LOW RANGE RADIO ALTIMETER 3 q1 h6 V$ v3 G8 J# ?RU, SEE - LINE REPLACEABLE UNIT ) _( _, I$ V- f. l9 Kuce friction 9 ^0 w4 f' a8 C1 \" a! Y4 ^/ ketween moving parts. It can be a natural or an artificial ( J' B$ l6 A/ _$ A, Baterial. E* B0 M z% {% y E4 P8 m2 FAC, SEE - MEAN AERODYNAMIC CHORD ( T: G9 a0 r6 S m$ q8 M' xft's true, a ^/ u @8 @# g3 l7 i; @ airspeed to the speed of sound at that point. 9 |% o+ O; y. e9 t1 I7 d5 s的系统。+ |/ N% k& J; `# {. V 远程巡航速度的缩写。代表喷气式飞机常见的巡航速 ) X/ _1 O ]) m- },通常以马赫数方式表示。6 G0 s9 a. L d- t' z 空无线电高度表, 8 S$ k3 h+ x( v6 y$ k# Y! ERadio Altimeter " ?, a. V1 V2 M8 r* ^ Ete! K. |: K; }# B3 Q" `) Z L* B- P$ F0 ^ l2 D3 Y, a6 x2 j th 5 e! ?; h0 }( ?* g( Se' [$ z" k; k) B3 E& ~ L0 X8 F: \# T8 J2 L4 ~: S. {. \! e L% U: `" N9 M, z# M! a" m) y0 e$ v LUBRICANT, A substance used to red; k5 f* l! u* P b5 n/ O, n5 M7 Z( d1 A, J$ {( I m! R* u! v/ b# T4 K- f( G LVDT, SEE - LINEAR VARIABLE DIFFERENTIAL7 P# G5 g& Q8 w) B# _5 o. B TRANSFORMER " X! h4 k! u% Y2 k( \: P. F/ g* QM 3 _" Z$ o% @+ [1 yM4 t: }- n) C d2 d6 X$ g MACH NUMBER, The ratio of the aircra/ L c0 [6 L$ \ 低空无线电高度表, . L0 y+ Y( d1 l/ G: W一种测量飞机至地形的垂直距离. H" m% Z0 P6 F 远程巡航速度,- Z* X# G* i: p3 U/ A, L: j9 g5 v% A" ~8 a8 q+ e+ k" N$ y$ H见Low Range . 6 j9 \; w: u0 B: |3 x, {3 T线可换件, + K/ e2 [6 H3 q- ]$ A& [9 l见Line Replaceable Unit3 S( {) F5 m. J- r' Q# b. f) p6 ] N/ b) J. V! b! o& O0 k! O" O( E: B; W6 A! m 用于减轻运动物体之间产生的磨擦的物质。它可以是天 , i9 I: h* l) ~7 [; a的或人工制造的原料。9 e; w9 o( O ~6 |# g 见Linear Variable Differential Transformer' [2 `7 A0 S% w2 @( l; {9 j( P 润滑剂,/ T2 F' S" D4 X! R( _) y1 a) [, t R6 g* ^# ^+ U! _# I 线性可变差动变压器, 4 g( P0 `4 A! Z2 w: Q- O; ]0 w* X2 M* U8 Q H* l8 @2 O- @ 均气动弦,8 j+ {6 k8 t% f- a 见Mean Aerodynamic Chord ! o( P( G3 `; y4 L- m7 l$ B' Z* U3 h: f: u; J6 x& L8 B2 q6 K, \& d" b) W# n6 W1 z1 G空速与该处音速之比。 # e- W% U- I' p$ M6 y马赫数,6 `; }3 D4 P/ V" F1 J 飞机真 9 B- ]- f3 b# n& c) b/ ^9 X英汉对照民用航空词典B OEING + Z/ J1 R5 _1 e' _# p- s0 bTECHNICAL DICTIONARY 972 F+ q- [. @; @* { MACH TRIM, Correction to airplane attitude (nose up) : p+ U* {, Y3 u3 e; \$ r zduring flight at high speed by using the horizontal 7 N }9 R Z6 e8 U; e' Btabilizer.0 o+ F/ R2 O; S) V AGNETIC HEADING, The heading of the airplane" ]4 ~$ f' U1 c; _ lative to magnetic north. 5 u% ~4 ?6 W9 m$ YAGNETIC VARIATION (1), The difference between % O' E0 L; X7 e" H& ?7 r6 fagnetic and true north. ^1 A" q1 e; r4 `& Z1 Y% tnorth. 1 K& I) L. I) R/ w* {5 \! }here is a continuous small change of direction, ^- [3 v" W' G" D+ [" u' N f lines of magnetic force over the surface of the earth ,& p @& p. y! ^& A* M8 Q, T$ E agnetic variation at most locations is not constant over) u# u& [2 }) R; d1 h% d) K ng periods of time. Lines of equal magnetic variation . e8 U2 Y/ T( te. (see4 L# f2 W+ b" U: P7 [1 y tation Declination% A- B: X! y9 z7 H s1 D9 m/ t- ~& b& V0 {+ t' Y# \2 Q: n) @ M% Y- K, b8 z- Y# y* _2 a re % d0 t7 C) ?- OM , Y+ |" D2 M b4 {1 Vm , P; V0 E7 l; w rMAGNETIC VARIATION (2), The orientation of a# V% V" P2 x; n horizontal magnetic compass with respect to true ( t% @' f9 h* q6 M4 }Because t8 x5 C. s. [8 _5 Q! Q& q0 W) { o . z: ]8 n2 u& Y; p3 c gm4 K3 L. `: P5 G0 r/ `& ~& h lo . n+ y7 d: ~: o3 g# n" u3 W; @(isogonics lines) are updated on Jeppesen charts every 6 i, m' c7 J; u% O( e" jfive years in accord with worldwide practic ( E% Q- @( s# j9 r3 m c( jS ). - b' w. U2 i, K" x2 m5 S) QMAIN ENGINE CONTROL, A component on the engine( l0 I1 S' G: q8 S& @ ration." J! }) a; o8 s; d3 C MAIN GEAR, The main wheels with the attachments for( j$ c. K* p E9 M; f/ O% `7 x supporting the airplane on the ground. % y! ?) l! } O( U& B, ZMAINTENANCE, Work accomplished in support of the & `$ S2 e! T Ostructure and systems of an aircraft. It includes,3 q( N! Y) c3 X9 p# v" C inspection, overhaul, repair, preservation and the& U+ u' W, O7 q' z* P replacement of parts.! ~$ E) ^3 F; g- w3 j' R 马赫配平,# q0 g3 E0 L( s3 m+ T: J 用水平安定面对高速飞行中的飞机的俯仰姿态所做的5 Y1 i' n0 r- I0 x9 c H- P; Z- Y 调整(机头朝上)。4 u/ i$ d4 z7 O8 v4 j1 f 磁航向, . y( f; c. B6 i( c# ^+ g相对于磁北的飞机航向。 ) v+ C9 A1 S$ I磁差(1),+ i2 I: [2 _: e$ |% L 真北与磁北的差别。6 z) B5 S5 a1 I0 A& s, C3 y 断的微量改变,磁偏角在长时间内多数是不一致的。每& r* b! t# x3 @) Q0 I2 R( \ 五年Jeppesen手册会按照国际惯例校正等磁偏角线(等; E5 D" o% b/ J- G6 s0 s 差线)。(见基点偏差) # s. n$ B1 D+ T7 ^4 s9 j5 m主起落架,& W4 r* J6 O* O! X* A/ l 用以在地面支撑飞机的主轮及其附件。" @# W2 c, V) W: c) Z) A1 @7 d 维修,- z' H+ v9 S; I( {# y0 D' F& F$ N6 M 在保障飞机系统和结构时所做的工作。包括检查,大修, 5 h' u+ B& s& R2 I& r修理,保养和部件更换。 ) _2 t7 v3 K9 `8 l7 Y1 k& l: v/ ^" Cfor controlling fuel flow for starting and engine ope L2 |/ t- ^' l6 b' { 磁差(2),0 [/ i* o% I) c$ j w# L 相对于真北的水平磁罗盘定位。因为地面的磁力线在作& {5 `% t* W+ W; L. y. g8 }; R" z5 c+ ]- s+ c2 Y. H+ s' k1 _2 D# b' H- n 主发动机控制器,6 X3 {1 e6 X7 y, ^3 x 发动机上为发动机起动和运转控制燃油流量的部件。. H/ z+ Z& S$ b 英汉对照民用航空词典B OEING ! H% W& T+ Z3 k+ \TECHNICAL DICTIONARY 98" B' O' s( H' p: I9 d; [' m MANEUVER CAPABILITY, The ability of the aircraft to 7 K& u/ u1 ^8 S& S6 x/ o) sertain load factor.+ r B. [- S8 U- n0 F/ o( t MANEUVER MARGIN, The amount of residual" F9 N9 P3 k4 `& Y4 w& I aneuver capability present before the onset of buffet. 5 c4 l9 h: O" O% x- @0 B; p6 QMANIFOLD, A duct or chamber with several inlets and' X; I- J8 l5 }) K& y$ j3 r outlets for air or fluid distribution.3 \$ d+ M. {: o- C the 0 z# p6 e' g! ]/ Rlow of+ S8 }& w+ d, Y7 ]& O! K' X e flight compartment. On specific$ x" _( c3 q# c" n ccasions it will provide conditioned air. ( H- T1 r9 p$ I F! gomponent by hand.( Q8 r. }! ?. V" f, K MANUALS, Books with instructions for proper# ^% R* ]5 X5 w, ?8 l8 W maintenance and operation of the airplane systems. O$ `5 _$ u( W/ QMANUFACTURED RIVET HEAD, The head of a rivet8 K3 \% X- f4 e1 `% z that was preformed during its manufacture (see upset . N8 W1 g/ |( |; A wperform certain maneuvers up to a c ! x$ b. H6 m% W5 j. p- Mm& b3 f4 \2 O* s* x3 P6 o9 v MANIFOLD INTERCONNECT VALVE, A valve in , `$ e! L7 W: q( ^* A( Xequipment cooling system for providing a normal f ( X+ Q0 q# F! n W% A! xrecirculated air to th; Q9 u" O& o* E1 q! c o, e, N7 j/ c) j% Q7 j: _ MANUAL OPERATION, Method of operating a A( Z, k7 O9 U, L H6 X7 Ec 2 Z. E* z' B- R* ?- |0 Ehead).! { H0 V+ K+ r' D$ Q" a MASS, The quantity of matter in a body. It gives the' j) k3 g, w! e* ~* r body weight when it is exposed to gravity. 9 R$ M1 T; Y! y9 T+ u机动能力, 6 Y$ g) @, l" P! H, _2 f2 s飞机完成装载系数达到一特定值的机动动作的能力。& H4 _+ `' X1 h+ y# J1 c% \* L7 \4 l 机动性余度,. n8 F+ p) E; _- {3 \ 飞机在遭遇抖振之前,所剩的操纵能力的大小。 * |& l+ R! |- S. _& v3 x2 x总管,7 a! ?# M( w' R4 b$ K 用以空气或液体分布的多进口和多出口的管道或容器。 ^4 t) l! _* u, H2 b/ D总管联接活门,9 j6 U, {: @4 b1 y. B" P, [ 设备冷却系统内的活门。用于向机舱提供正常再循环空 ( j0 Z r/ N' T* T气。在特殊情况下会供给空调空气。 ! P# v; h# J, l" A& S) ^7 G1 P5 g人工操作, ) B7 Q( O# c5 d" I% }8 [手工操纵部件的方法。; k4 A0 z; N$ V4 j 明书。6 o! G6 y( V6 a) B2 y( ?& S 铆钉头,* Z) a! i9 B) H( M- k$ n1 n 在铆钉制造时已定形的铆钉头。(见膨径头)。/ H& a9 F7 K. D5 ?: \ 质量,) d7 S! V) l( e2 r; R) {5 b 一件物体的物质数量。当该物体受到地球引力时质量产 & U/ z% E6 g8 ?# k1 [$ i生重量。 ! K' Q* M4 j- E; a0 g手册, 7 F5 h, g" |7 Q" J% F) p$ m1 y为能正确地维护和操作飞机系统而编写的说 9 F3 ^& s& x8 h机械制造的 , e9 g0 k+ _- _, C0 C5 i英汉对照民用航空词典B OEING 2 D, q" _* {* W8 VTECHNICAL DICTIONARY 99 # `* X$ S6 O" d7 {1 m2 S5 uMASS MEMORY, A memory that can store large- e: o1 H( b6 n1 W1 Z( F% s amounts of information and hold that information) X! W. R- F% q" o: u6 y1 I permanently. " h1 i; j% d: [0 Y$ rAX CLIMB THRUST (MCT), Maximum engine thrust 0 F6 O6 z! t, Y, ~" H3 ]ximum engine! w' \/ ~( l+ R1 r1 L8 } rust to be used continuously when one engine is `( C w7 N% U2 N, s& v D0 X% O operative.* R2 _; c1 ]- h EOFF THRUST, Maximum engine thrust to be , w" g S( Q3 Hused during takeoff. % z5 T2 I9 \( Y; \+ IFF WEIGHT, The maximum take off& u8 _( G7 [! q0 ~ weight as permitted structural limits or performance5 C% [; Z4 L3 B9 g$ o limits, whichever is lower. / c. o* l8 [4 P9 uRANGE CRUISE (MRC), Cruise speed & c' f7 a' E8 q9 Q: Jance + P% F2 i3 D$ c: U ^' ?to locate5 x2 o% m; ~: u+ d the Center of Gravity. & P# ]0 ]3 [% Q/ }) u5 h: y主控台, ! U) R3 d/ a7 n! e+ J: v控制系统操作方式的装置或系统。1 P6 s% o8 ?5 d6 G 大爬升推力(MCT),5 l; L- h' s9 T 飞机爬升期间所能用的最大发动机推力。 - R5 \$ A# h# G# Q! }$ Z* p& HMCT),* ]* T; j9 a7 t; J( v) H 当一台发动机不工作时,可以连续不断地使用的最大发 , r7 J5 U/ N* b: t7 R% a- q. }动机推力。: P1 b, }3 ^' f* k& ` 起飞期间所能用的最大发动机推力。8 E6 ?6 j" b' ^! C* w! X L# Y1 j0 B 结构极限与性能极限两者中的小者许可的最大起飞重! v% t* w% v h$ M+ L! U! [: y# R( l8 g! ~2 A 大航程巡航速度,' n; `; J! O/ s, Y 最大的巡航速度。 + V' {: n8 d3 m% P$ g5 U% @# h平均气动弦, % r9 {6 Y0 _. Q. s9 ~' l* D. T确定重心位置的基准) y, J+ p4 L j( S& q- n 距离。 + [! _0 |! i- JMASTER, The device or system which controls the% X+ J' O2 q7 n9 x2 W system mode of operation. + h3 @$ e! T, W) k4 s8 bM! C [+ {! B3 u; E to be used during climb. 2 _+ u2 g z5 s7 w. g7 c$ h/ A" PMAX CONTINUOUS THRUST (MCT), Ma! g# V8 S( Q) x: W' C8 } th' n: z% d5 Q( M6 H, ?' b g! A in . o2 N& }& x0 O6 R' C: ^6 E a, `) OMAX TAK, v# ?. |7 v4 H/ a2 q, Q8 _+ C MAXIMUM TAKE-O q z/ s$ e$ `5 r) b' x MAXIMUM) x7 m: e }$ D8 q producing the greatest amount of range.6 b, `% d( ^( C( [4 P% u MEAN AERODYNAMIC CHORD, Reference dist- z4 ?2 l& R* t9 t located at a fixed position on the aircraft used% |( s' `' ? E7 T0 j: ~ 大容量存储器, . Y- b2 _6 D2 w) L可以储存并能永久保留大量信息的存储器。7 q. P3 r O" N d" J! n" Z3 Q4 G- q# M7 y' m8 Y" L1 B5 {1 b最大连续推力(5 T' X! A+ z+ j- s: j D9 o 最大起飞推力,' H* w, Z6 I: H% C7 d5 m- m& T0 G/ b 最大起飞重量, # K s% H+ h" y& |4 C% d. Q- m! z+ `" J* F. C0 `' W! c* h. u5 ~4 ?0 g7 H- s) q0 \ 能使飞机航程 / ]- y* K" s7 n位于飞机上一个固定位置,可用来. _ R5 v5 h2 w6 F 英汉对照民用航空词典B OEING + J' z2 o+ ]3 |9 b; WTECHNICAL DICTIONARY 100% L, s& G* Z5 t+ p MEC (NO. 1), SEE - MAIN ENGINE CONTROL. N5 K$ |+ ~* H( E* C MEC (NO. 2), SEE - MAIN EQUIPMENT CENTER # ^4 `$ {! b9 \1 l4 D, b$ d, `EL, SEE - MINIMUM EQUIPMENT LIST% L* Q4 r) K$ B7 v0 |# |+ \+ j7 { tem the memory is where q7 a. k R1 m# }3 X" Eformation is stored. ; ^, O2 ]8 @0 v5 b8 G: U! Q9 {METER, Any mechanical or electrical device that is 3 X1 T: O$ L1 P2 e0 jair or* G2 R0 F0 w1 a2 X! ]; e4 R point along the glide slope of an ILS approach. It is) d( m" W0 O x3 x' u4 x normally located at or near the point of decision height. 2 U5 s+ a, G, H$ ?$ p2 O9 @7 \* N4 s1 U* B' j见Main Engine Control. V# o7 V+ y3 g+ J M- ^' u" Z9 v& l) W1 C! T MEMORY, In a digital sys : L' s2 [2 p4 Vin: n; D+ J/ r0 v3 a used to record, indicate, measure or sense a specific+ G, e! A, S+ n, o portion of an operation. ) W+ ` r" r6 X6 mMETERING VALVE, A valve for controlling flow of ) j8 a9 l5 X1 d& Afluid. - A# r7 H- S) t' N2 BMICRON, A measurement of filter effectiveness, one0 i8 |: ~: b4 g5 L. Y micron equals one millionth (.000001) of a meter. # X0 r ?" U9 U& X IMIDDLE MARKER, A marker beacon that defines a7 c; S2 i# a; ? 发动机主控制 : ^5 f. x4 W S; @# X* j# R1 o( F3 m$ i( h4 q- p设备中心 4 H* ~: k0 B3 s3 P3 A( y( R见Main Equipment Center " k9 k5 ^$ u- g7 }: v2 w# @$ j8 G# z# B9 L0 Z+ `, {* L5 t* P5 e& M7 P& E) Z 低设备清单,- @0 O/ p: `2 Q) `* E6 l 见Minimum Equipment List, S0 b |$ I2 P, ~( _, ?* ~7 E1 v+ F$ k! Q$ V N/ p6 F/ {' n* J9 O1 e+ k) k% B( q& f% r g 在数字系统中储存信息的地方。 ' J; |' x2 P8 M4 ? _" `) J+ E, F. L计量表, * g1 C, U# O+ z5 ~9 g/ \0 [用于记录,指示,测量,或感受一操作过程的一个特殊4 ~0 ?. k$ c1 K [- \4 N5 H Q 部份的任何一种机械或电子装置。9 h) S3 }3 y" t 量活门,; t. h, Q) Y) n" g* N% u- d 用来控制空气或液体流量的活门。- Q& S2 @2 N! T4 ~9 o( H# @ 微米, C0 B# O: H0 k- Y 过滤器效率的计算单位。一微米等于百万分之一米。 ( Y. M0 I7 t7 h6 ]0 p6 s! d: b' G' H3 K在用仪表着陆系统着陆时,用来确定下滑道上一点的指% |; ~1 ?8 I2 q$ x' P+ v0 K' M 点信标。它一般位于或靠近决断高度。% }+ q A- I' Y$ f 存储器;* U& G2 p! ~2 S5 L; e) B9 [. j% v* { z; y, w7 e4 A! m 中指点标, ; P) N) d& X: w7 S z; f7 U英汉对照民用航空词典B OEING " e. {: Q% w" h) R& _0 G$ e2 OTECHNICAL DICTIONARY 101 . E, Q7 L! e) _; m* JMICRO SWITCH, A miniature mechanical device that . B3 s3 h/ ?0 l% Ecompletes or breaks the current path. O5 o* e3 y1 r: i0 m .1 W* c/ c: T7 q* u% V7 O MIL, One thousandth (.001) of an inch.. T$ u- j& F8 k8 b% h ILLIBARS, A unit of barometric pressure equal to 8 W8 [' w2 H) ^, ^2 p0 w8 X, lapproximately 0.75 millimeters of mercury. # z9 _4 f* k. f) F8 L2 dThe lowest ! I/ {* w# f) q/ A% r! E' w' eltitude to which a descent is authorized for a: O! `% t1 B4 Q0 j+ V- v onprecision approach. 5 D& }: V* I7 n2 Q2 RINIMUM ENROUTE ALTITUDE (MEA), The lowest8 N6 F9 Z* L" c$ v! Z9 I ublished altitude between radio fixes that meets; L( m% d: j8 B: X; \ bstacle clearance requirements between those fixes0 T1 s. Y9 x5 A6 R and in many countries assures acceptable navigational # t: N* r: U3 K5 Z! Xsignal coverage.( L! D a, F$ g! `* s operation of the airplane with certain systems or # o( y3 \. ~, n, csubsystems inoperative. 3 B# S/ Z& o$ Qapproach; `' H; j0 t% x cannot be completed to a landing and results in a Go-7 _5 p, \* V7 b- @$ k7 q Around.3 F! p3 m6 P* z4 K/ D) E2 y 一个能形成或切断电流通路的特小型机械设备。 ) i, a; \$ G' l! B+ c: A5 l话筒,+ U2 w" S3 {+ g1 ?5 E7 W+ R 话筒一字的缩写。 " `- x0 t! D+ _6 }耳,9 @8 ~1 j( W! \+ O' ~ 一英寸。 0 p" Z! s2 {( Z8 X0 D6 }: K, {毫巴,& f/ a9 `; _+ S3 q: m( t 一个度量气压的单位,一毫巴约相当于0.75毫米汞柱。" a8 s* v* E) e, O; W9 T; P 低下降高度(MDA), 3 i6 c- r r1 N3 o飞机作非精密进近时所准许下降的最低高度。. O9 s: c$ R( W8 b' b6 } 低航路高度(MEA), 6 P* n+ C9 b9 w& n/ h: j' @8 @- K在导航用无线电定位点之间,符合越障要求的已公布 7 o& Y# g/ S4 e7 U2 O- ]的最低高度。在许多国家,最低航路高度保障了合格导航5 G( H$ m A" }$ I0 K 信号的接收范围。 ' N2 m+ v) `- @最低设备清单,# ]8 g5 |: u! b/ H/ ?, [7 p' t. o作飞机的文件。/ ]% `' n9 D; Q8 H4 k 复飞(MA or GA),. N9 P" m+ w% S& {' M 飞行员因未能完成仪表进近而导致复飞所采取的一个 , X, h1 v) M! d0 x机动动作。 8 ^% m+ R! |- ^+ j0 kMIKE OR MIC, A shortened form of microphone 5 S5 n, J; e: z7 w/ S/ E6 gM ! X4 ?) k$ r j/ U, N9 {+ @$ {MINIMUM DESCENT ALTITUDE (MDA),, j+ P& t* z! Z' q9 S: ~$ | a # k. w1 j7 U6 D% Mn: i5 F& [3 T$ x# Y9 X; O3 X5 P M6 i& [# p- v) X! b p 7 t; v" z* _8 J6 h2 y- @o * @! S# I* p. k; w8 @2 s1 vMINIMUM EQUIPMENT LIST, Document prescribing + S7 _' ~$ d( T( t% XMISSED APPROACH (MA or GA), A maneuver 4 g! a1 V: t4 t/ Jconducted by the pilot when an instrument8 L( e2 E( d3 P1 r) M' D 微动电门,! ^2 Q2 U8 b& ]5 o! k2 K/ G* n( b7 Q8 S 千分之 9 {8 j4 F- U# k( C) p6 ]+ a$ `* ~0 G# B9 b6 Q/ E- M' E& ?$ W( x$ {! j 指定飞机在某些系统或子系统不工作的情况下,如 + @/ M0 G. Q( o4 \, k. }; j2 O; ^& }3 T0 {3 u* ^7 t1 l 英汉对照民用航空词典B OEING * d. n$ x; A# c$ pTECHNICAL DICTIONARY 102% b' k; g- M9 g. x( v$ |$ Q MIX VALVE, A valve assembly with two or more " U1 q, O ^0 C' t/ tindividual valves used for airflow distribution in air " ~" ? t# h/ d8 n3 Fstem.' N6 W: Y( R) @ b# v( t MMO, The maximum Mach number at which the aircraft : B/ k a2 h5 J9 B: ]! kMODE, A specific operating state or condition; i.e.,9 N+ I/ | ?2 I+ t9 f% a5 G Autopilot mode, MAP mode, etc.# x" P" q! l, s- |0 @4 _, K: M e 9 |0 R- _0 U" J6 z3 l, N/ BMODULE, A housing that contains related system / z" F6 W& I* L' d, I( ]MONOCOQUE, A type of construction in which the J6 c2 c; ^* L9 \6 v ONOPOLE, A speed sensor that senses magnetic ; V, F' L1 Z1 i3 vpulses from a magnetic nut or gear teeth on a shaft.! @. W! O9 U/ l" r. u6 v he controller.: e. O: J+ W/ N8 u9 V9 {4 g8 ] MOTOR OPERATED VALVE, A valve using an electric ( Y) T$ Y3 Z2 r; _$ B+ h4 i lmotor for opening, closing and modulation." E3 l4 V. E$ }9 Q* ]9 ^1 c 个以上单 ! \4 V- \) _! m- [活门的活门组件。 [' l3 v2 g) }+ U) ?9 _5 I 飞机可使用的最大马赫数。1 N7 J8 v6 R) I+ w- i8 w 式,MAP; w0 w( X$ W7 n6 j$ S% k' R! ] 方式等等。9 C" u$ P7 f5 d& e; S 调制,- Q* |+ x" C( \' Q7 s4 @8 U 组合两个或两个以上的电子信号,使一个信号随其他信 ; w, N9 G2 J4 |& l$ x号的变化而变化。+ Z9 e, G0 f2 E+ Y' g1 a 组件, 9 E% w D$ }: Q0 F极,- h% E5 `5 |7 n2 Q' F( E 帽或齿轮轴上的磁脉冲数的速度3 V0 ]) G# C" X/ l$ @, K$ l& X7 x /分钟。4 r9 Y' s. O% R- W4 s- G 用电马达来开、关和调制的活门。* ^# G2 G; s% L* |# V conditioning sy - ?2 k% _% l9 O$ m4 p+ Pmay be operated. , r, Y; V7 w: e% V: UMODULATION, Combining two or more electrical- b( U! X) A2 H1 h3 x' K signals with the result that one signal is varied by th6 P8 P; a2 C+ G( p9 r0 P others.( T, _8 Z" ]7 u- h+ Q4 L components. , u& U: m% t2 c2 W$ b9 l( O1 wfuselage skin carries all the loads. 0 |+ ? h/ E" y& T FM1 i; u1 I+ S& Q" C" q5 h; W; Z These pulses are interpreted as RPM by t $ a( D9 A+ u( \3 |混合活门,2 r I( a: u! L& Z' d" L# o4 ~ 在空调系统内.用以气流分布的具有两个或两 ) u+ t. |: S) C* {; N1 P1 y6 s7 }6 z* G7 t: p6 m1 K* dMMO, % i$ s f3 N) T* s6 W" k4 ^方式,( |) r5 w8 Q; U5 q& `' n: ] 一个特定的工作状态或情况,如自动驾驶方 # |6 F' b7 c3 c* y. b内装相关的系统部件的机体。* P7 {+ l4 a# ?9 [' M+ k 硬壳式,/ X- c: e* B3 S5 \ 机身蒙皮承担所有载荷的结构形式。 0 h0 h" B( `) z6 J) l# o g1 O- Y/ n$ o7 f一个能感应到磁螺. R7 j. W, @3 b1 m% D 感应器。这些脉冲可由控制器译成转0 O0 |: r/ d# L+ Z 马达操作活门, + ^5 d4 I; r; C英汉对照民用航空词典B OEING ) @3 M% {# M; P* xTECHNICAL DICTIONARY 103 8 @/ x$ @, @) ?0 NMSL ALTITUDE, Altitude expressed in feet measured( J* S E/ A3 r9 A' d0 m om mean sea level. 8 E* `4 P) d# z/ c2 Areducing the noise of the airflow through the pneumatic h& G: }# U. Z duct.! ^$ b4 k+ v) b& K MULTIPLEXER, A device that allows two or more# b+ \2 m; c: ? signals to be transmitted simultaneously on a single " n' n; T5 r V0 j# fcarrier wave, communications channel, or data bus. 5 Q* b) j# s" `' Messure compressor rotor. % E, D* e* \, Q9 {N1 BLOOM, A change in engine N1 and thrust indicated9 `3 W/ Y. ]3 u9 [ V- C0 A/ Q, S7 n+ y N1 gages and detected by the autothrottle BITE 5 w3 U3 _3 r; |7 K, Sduring throttle hold operation. # s& z* W3 s8 J8 s; v. z( MN2 , High pressure compressor rotor speed. " D9 B8 |; j- C! n1 AACELLE, A streamlined enclosure on the wing or $ v4 J, B S0 ^( J2 V4 H4 {面量起的高度。6 [) c4 i6 X4 p8 r 经气源管道所生的噪音9 _3 r. l. V( B: r" R# { 的装置。/ b3 g+ J, K& R. ] 多路传输器,# I w5 A, z2 L/ h 一个能让两个或两个以上的信号同时在一道传送波,一 0 f( Z# n3 K' j9 r条通讯线路,或一条资料数据总线上传递的设备。. _, t4 Z( }+ E* i) i+ t1 j8 U. h" K N1转子转速,: _( q% D( E8 G5 j& T 发动机低压压气机转子的转速。 # {8 B4 v D* LN1激增,, y5 A$ ^; U& V! H. s 油门保持过程中,在N1表上出现的由自动油门自检探 9 S) w, F) I. N; s4 v: Y/ d测到的发动机N1和推力的变化。* @0 ^3 F L" ? N2转子转速,4 `4 |/ N+ ~" G" E 发动机高压压气机转子的转速。 ) U) `, e+ l9 \8 f短舱, " {. a. m$ S8 l5 h1 Y% s8 s机翼或机身上为安装发动机而用的流线形壳体。% H6 t5 p8 G( y fr ( ?5 ^# A- i# p- ^MUFFLER, A device in the pneumatic system for , W" u2 S ~. r) JN) w3 o* f* Q6 @6 m& a N1 , Speed of the low pr - k9 N; u' ?. z/ S! Non the* r G; W8 s+ k3 m9 K# ^" d) \7 l# y N' V( h/ v7 ]& S# E fuselage for the engine.9 ~( b' W. M$ H7 n( c3 S 平均海拔高度,! t& b% D- a6 e) N$ p 以英尺为单位,由平均海平 0 H. U3 H, {+ ]6 w/ j* k消音器,: g6 q8 X2 R; y( m8 O 在气源系统内,用以减低空气流4 p# s( m8 S* q 英汉对照民用航空词典B OEING$ H& q# Q, ?! W U$ v% } TECHNICAL DICTIONARY 104 0 s. ]/ e3 ?+ i$ f: ANAND GATE, An AND gate followed by an inverter to+ S7 n6 `& r: @9 D6 ]2 |* c- D form a binary circuit in which the output is logic 0 if all2 ~. q) Y( o7 z5 l2 a puts are logic 1.9 J8 {0 h( x# r/ t+ c& p8 P' s AUTICAL AIR MILES (NAM), The actual air distance " P, m a( A4 }respect to a- d# T# _8 B4 O# D. i/ I. D tationary object.% B5 A: {" y. v. H$ g* v, N istance I! S" l) R$ U: j; ` travelled in relation to the ground expressed in nautical 8 }! ? [: [, T! Rmiles.; F: [5 t3 T' I nce equivalent to 6076.1 feet$ O6 @6 X a, z6 |0 b0 l4 P3 `' m }' [" o r 1852 meters.' w! @6 ^+ }% y, e9 I) E hical+ @* y: S5 Y1 Z. F EGATIVE LOGIC, A form of logic in which the more) l s/ F1 ~( u3 l" j negative level represents a logic 1. / O' S1 B- j8 [$ `& U1 f2 \EGATIVE RELIEF VALVE, A valve in the - @8 H2 x% Q- j# i7 ]$ ]# G+ i; We to be |: r" v0 `5 fabove airplane altitude (or cabin pressure to be below " r( |: g$ j2 pambient pressure). , u9 w( f% s+ q" E0 W1 q4 ^; Q# |9 S) J7 Q 人为逻辑1时,输出为逻辑0。 + d' D8 Y* u: e/ i b1 f海里(NAM),; f$ [ ~ c; F5 l2 S* ~ F* ^ 来表示的飞机在空中所飞过的实际空中飞行距; U% i' u- b( ^7 b5 i; h 地面物体。 ) I* b3 G+ G7 D以海里来表示的飞机相对于地面所飞过的距离。 ) H; }4 r: f& A' B里, 3 V5 {' p( [- _) [8 D2 D# d相当于6076英尺或1852米的距离单位。. [) u1 P9 P# D7 x' k7 a) T 导航,$ }+ f" Y1 {2 W8 E1 v 反逻辑, 2 U) k. N2 N2 Y* w' f! q正电压水平越是代表逻辑0,负电压水平则越是代表逻 ' V7 j) I" h$ A: ^. o) a# U释压活门, - O [7 ?2 p7 M$ H. C增压系统内,用来防止机舱高度超过飞机高度(或机舱 / o0 n; y3 b7 i% P- d+ ]压力低于外界大气压力)的活门。9 \1 m+ f5 T0 q( p0 G6 l in- d2 L* |$ s, _ N- `3 g0 c) ^. U$ L6 k flow expressed in nautical miles without# _1 o+ B1 T. K7 {$ a s ! p3 T; \, F6 p6 gNAUTICAL GROUND MILES (NGM), The d " c: _/ {& ?+ r; k- S% KNAUTICAL MILE, A dista8 {6 ~3 \8 r( L7 g o/ l% P- f7 b; t8 i- r NAVIGATION, The art of determining the geograp) T3 }/ {! `' h/ f Y. X5 o position and maintaining desired direction of an aircraft & G4 g( e* L/ R( T7 ]7 ?% ~relative to the earth's surface. & t) B* x' c8 c" mN. C) R* F$ c6 f- T% J0 X positive voltage level represents logic 0 and the more " |, c% i$ U( _9 R' G/ H" y- _N( @* F8 y. Q( p( c& J3 [ pressurization system for preventing cabin altitud( ^* p1 [. A7 `2 G& E7 P- q 非与门, 0 K. k- T6 O9 c# K. j, E% _在与门后面紧跟着一个反向器的二进制电路,当所 ' `1 a* R; s1 o M2 }* X2 `5 g+ B; h& b! [ _& ^% A4 h% w! E7 \, h: M% e( T/ }以海里 ) A* r" B( P1 m; i" Q. g3 D2 c离。空海里无需参考 + V! v" B! _0 r% c0 j1 g地海里(NGM),: X. V4 o2 g) t/ c: c( Y) G9 c4 d9 }* g2 c- t+ w5 y# J决定飞机的地理位置和保持飞机相对于地球表面所希' b# e/ J" u$ ]0 S 望的方向的技术。 M5 M. w* S* g2 Q) h7 k$ h 辑1的一种逻辑形式。 * b3 _) h* T) l; g+ c7 x, H' Q6 z( p+ S, }* p. m英汉对照民用航空词典B OEING" M, u6 V: y5 m1 y TECHNICAL DICTIONARY 105) }0 I; w( h# ]- j6 g0 Z NEOPRENE, An oil and grease-resistant synthetic ) m% w' j. T" K. Nrubber. Used mostly for seals and self lock nuts, etc.$ e/ M8 _* @8 |4 z+ \, }. ? EUTRAL SHIFT SENSOR, A sensor used for( q( K* e) W2 Y( k NET PERFORMANCE, Aircraft gross performance, `' B, G: ^" q( ~2 o8 Z0 d calculation , X& r# @$ f0 y& ?purposes.- ~" f( j$ s- g6 Y3 _ NICKEL-CADMIUM BATTERY, An electrical device for6 A% m1 f* E* H2 x" j) | changing stored chemical energy into direct current.' F$ C* g# Z+ J* N ses nickel hydroxide, cadmium hydroxide and0 b% j2 X1 V3 [8 K9 G8 y4 E! f) R otassium hydroxide. P2 k; W% x6 Q% z" E5 p NOBLE, A term used to explain the properties of some 0 \3 I5 `" X$ y4 W# Zlements that are chemically inert or inactive. . [% Z0 z" X1 |3 RNOISE ABATEMENT PROCEDURE, A flight path and8 g$ U" { f2 [ limb profile designed to limit noise in the airport area. ; r& b9 W+ H' Q5 x8 ]# m. Gconstruction. (Nomex is a trade name.) ! @7 k- k: [6 ^7 E, Fin only. Q9 ?) F: M" T) ?3 L: g8 { one direction.* n# d6 c% D( r& x1 M' F S 氯丁橡胶,1 u9 O9 O4 S9 s* q. x 一种耐油和油脂的合成橡胶。多用作密封装置或自锁螺 7 C8 X2 V. e: t1 B: S帽,等。: z6 F2 ~6 z- R5 Y 立变换探测器,9 j7 D8 b% x- [4 ^' `1 W; H 用于探测升降舵和安定面配平状况的传感器。5 {/ d3 F' ?: c) [# ~" l 性能, , _ j, o( Z6 e. Y机总性能减去由当地有关单位为了使性能计算 / Z7 j) e- Q% r+ L- I% A$ `+ r较为保守所定的一个量后所得的性能。 6 }9 F' ~% b& a( a8 x为直流电的电器元件。它使用氢氧化2 k! p5 p9 F( b8 Y Q+ z 、氢氧化镉和氢氧化钾。: a; `5 k8 `- j8 A6 G8 P" M$ Q1 \ 性, ( P5 I1 x* F4 }: ?) g7 [用于解释有些元素不易起化学作用的特性的名词。# K% r' @4 E; G+ |) Y 低噪声程序,# l* k. B; @. w) i% h0 h* ] 一种为降低机场地区噪声而设计的飞行航迹和爬升剖 * E2 |, r# Q( C) P/ X2 c+ t- C# d9 B& a是一种类似纸的材料,用以制作蜂窝结构。(NOMEX6 H0 A: F# I- _3 S0 A9 p 商品名)。 ' e+ W/ S" k) h6 H2 v8 {只允许向一个方向流动的活门。 7 a9 G( i0 l6 E- x4 oN # O2 x' ^# f9 }3 P' e7 xdetecting the elevator and stabilizer trim condition. & ^7 \8 D1 @$ o2 Y. x) o3 o; G) @% [degraded by an amount determined by the local8 ~; K( Q$ ~5 L" v! t" ^ governing agency for conservative8 [) z5 D& `9 U a+ i9 u U# [9 d! L! c R( ^# E0 Y% { p7 y1 D! [7 U$ {$ d9 B) p e6 e) d8 `' \. b/ ^* r; l+ j1 G c / q' R2 B D$ eNOMEX, Material similar to paper for honeycomb, V. l; f ~* p NON-RETURN VALVE, A valve allowing flow + \2 s, b' S9 K5 T5 O6 I0 v M4 C4 `4 I, o+ g5 W& K/ U1 v1 \& ?4 a8 y以飞+ n, O* T1 h# H6 x: ~ 镍镉电瓶,6 \$ i$ T9 ^& N. |6 Z 将储存的化学能变 4 j/ L( D R# R, g' q. ~" f6 i1 X' S! p' J1 z0 ]$ ?# {7 j( ~/ v2 h' z4 c, h; n' c) u" W5 t. f! k9 K8 G( Z1 e& A& D4 G5 g1 {7 rNOMEX, + y9 W' {) k$ p; k. E4 B% o1 Z& f. c* B5 ]0 V 单向活门,& x# M" @. d3 J# m' ?* w 英汉对照民用航空词典B OEING" Y) u9 Q: ]: W9 L# w TECHNICAL DICTIONARY 106 9 ^6 i/ S6 u& c4 C y% hNONDIRECTIONAL BEACON (NDB), A radio beacon 8 ]; M+ `" I& p" mwhich transmits nondirectional signals whereby the pilot& W- X! h$ k# A can use the ADF to determine his bearing to or from the$ `/ b: s+ O! Z2 Y' A( q station. 4 E$ R8 h5 L8 u" \ONVOLATILE MEMORY, A type of memory which2 C! T' f5 Z' K6 M; g3 j. j6 O) O" X does not lose its contents when power is removed.1 s% q- r3 R8 T$ q rm : i4 _1 l" I( X W9 Y Abinary circuit in which the output is logic 0 if any of the , i5 C6 h- H. U3 ^inputs is logic 1. ! M: p* L8 r9 N$ E& B' M$ z, a0 bNOSE CONE, A device on the front of the engine that% r1 s/ x/ m+ }: `+ W) [; N guides airflow to the primary airflow path of the engine. 6 x% F/ H( g& J9 W" M& W0 n. Sthe nacelle for air inlet to1 u/ F, |& R: G3 N" z e engine. , w, |: Z7 p1 m u6 \OSE DOME, Front section of the engine for) q8 g, y% C% Y3 Y+ @! X treamlining and directing airflow to the compressor. . G3 K0 P& ]- q/ R),: ]- C' @. {9 C2 ?; K2 p7 k' ? 能够用自3 z# K. B! _ h! ` 定向仪(ADF)确定他的背台或向台方位。0 l7 w) _$ F1 E8 N, k& f 久性存储器,, b" ^0 c S' S) o 在失去动力或电力时不会失去记忆内容的存储器。 : @5 U8 \. V. j% K6 L在或门后面紧跟着一个反向器的二进制电路。当任何一 ; o |6 Q* D1 _8 b* {5 j+ m% C3 H: e* U输人为逻辑1时,输出为逻辑0。% X1 K' C/ h0 S# I: E9 W 一个位于在发动机前端,用于引导气流通过发动机的主 8 h, S5 f! k9 M, U* z; A% N' c/ m气流通道的装置。 - ?2 U2 [# h3 j( ^3 n引导空气进人发动机的短舱前段。- {: d1 ]/ ~, ]8 I( c9 j4 { p# B 部整流罩,$ Q% ?+ b! s, Z7 o' O 用以整流并引导气流进人压气机的发动机前段。5 M' E; I9 B9 r# T: v! U6 S N 2 P; [4 Q; m2 G5 l1 VNOR GATE, An OR gate followed by an inverter to fo. w5 Q: {% p q5 t+ { a. {4 c( q- `- P8 [ NOSE COWL, Front section of- x" N5 S5 V K0 H1 }; H N th 7 ~1 q3 x# ^! x: Q) l- |N: ~6 ?! O3 V8 ~& F. p s - N0 X: C; }& ~( z; B: i% D7 G5 w无方向信标(NDB ( V9 J" x, P, K$ u5 o发射无方向信号的无线电信标台。据此飞行员7 |. k; n4 a9 Y& b5 a( S" P$ y8 S* L- r5 R9 t& J" p- U- x/ Z* _6 D. M 或非门, f, M: ~. N! P6 E# k& Y1 q; M. {进气整流锥,5 _ ~8 B* b7 c4 M5 C3 S 前整流罩,( ?8 F" Z: k4 {5 h& Y( o' D$ v2 i3 k j' d9 [; Q# o' k3 n英汉对照民用航空词典B OEING% `$ R2 H2 [4 G& y TECHNICAL DICTIONARY 107 3 D( N3 e( ^" p- d. I# B* XNOSE GEAR, The front wheels with the attachments for0 ` t" w0 G3 F9 @. X/ }% V NOT, A binary circuit with a single output that is always$ ~/ W1 n, x. ]; j opposite of the single input. Also called an inverter. 8 a% s0 R4 i1 K4 C; Qtion that has the shape of a "V"., G6 u4 Z( J+ ?, I% C t.# J* _/ J/ v0 U4 k- [ i O-RING, A circular shaped rubber or synthetic material$ [; g7 \$ Q+ K+ O sealing device for pneumatic and hydraulic systems.0 c* m6 R( U4 e! P" `) |+ q2 O PERATURE ' @+ l, I4 }! q+ [e - |& Q- T- z9 u8 ]in the path of flight. # C2 r4 T9 _7 j TOBSTACLE CLEARANCE, The process of flying the6 P2 [6 ~0 i q% O( e aircraft over all obstructions under the flight path. ! V5 x: z+ I6 J' e3 @7 |0 ?8 Y2 TWhich obstructions are considered and the amount of - `( M- p3 d8 J- o3 Pvertical altitude required above the obstructions are ( O, I9 K+ l" G9 |6 adetermined by local regulatory agency.$ o6 ^' I+ S6 b; ?3 u) l& m2 ~ 非门,; p: a: x( q5 T 带有始终与单一输人相反的单一输出。也称作反向器。 * m8 w% n- n) a1 @! q, X一个“V”字形的缺口。 * W( B9 Q2 T' X( {喷嘴,4 Q# B+ w6 k; t9 D8 U 形圈,) K9 b2 X) c, {" U* B 用于气源和液压系统,圆形的橡胶或合成材料制成的密& b8 q( B5 @2 N. n" w3 o* U, O! A9 p 封装置。 1 z, u; \+ |8 w外界大气温度,; M, W {* v/ i2 n 见Outside Air Temperature ( _* s9 E, x: m7 Asupporting the airplane on the ground. 9 u- S$ H& A$ q2 hNOTCH, An inden6 c% ? p& [ g7 ]# m. u- {( I NOZZLE, A shaped device for directing flow in a duc! H8 d. s* f1 @2 n3 h O 4 a: L9 ^ i1 Q( H3 HOAT, SEE - OUTSIDE AIR TEM : F( b6 U( U0 O( ^# x- DOBSTACLE, An obstruction protruding into the airspac : k+ h& F8 c& ]前起落架, : E+ A$ }) I+ A1 l7 W用以在地面支撑飞机的前轮及其附件。 . r e: T! Y6 I, s. b凹槽,5 h6 A$ X0 @ W" e/ S6 x 引导管道内流动方向的具有特别形状的装置。# e r8 t( \, T# P% |- T( l" a O" ]) A3 P: P+ x! V/ n H A9 e2 A0 k+ Y6 a" E; }9 T6 W3 \# r8 Y2 m! o. K5 o 越障,1 R7 A9 J! X. q, |; e3 W 道上所有障碍物的飞行过程。障碍物的选) `0 D. Y" B: b! S9 L2 a& z' F# ? 择和飞机距离障碍物的高度要求由当地有关管理机构决( I6 B$ \& ]( n# O 定。/ W6 i7 v! O9 o& Q0 G5 e 障碍物,( p, c# { ]% ]9 x) _ 进人飞行航径上空域里的障碍物。 & B# |* Q, Q9 }6 C9 A) K U6 ~飞机飞越其航( i- _# P, D. `% @6 t 英汉对照民用航空词典B OEING3 Y- a* `$ M2 |0 b& e TECHNICAL DICTIONARY 1089 @) L) Z4 d3 O; C; b2 ~ OEW, SEE - OPERATING EMPTY WEIGHT : W6 d5 z- i; l3 k: Z& }FFSIDE, Opposite side.1 Q6 t# U+ |' G6 E- [* P3 u IL COOLER, A heat exchanger for cooling engine oil % q7 B- Q) A1 P$ B+ K7 zby fuel flow or airflow. G3 j: q7 u# Z, p ATOR, A device used to separate unwanted7 c ]2 F4 \) n) Y L0 M ir from engine oil returning to a sump or oil tank. ! F" E" `* M" e8 sOIL STRAINER, Type of oil filter." w" B1 q; L* E* C8 i LEO STRUT, SEE - SHOCK STRUT ( ^: e$ I# T W8 ~NSIDE, Same side.- a$ f8 h0 w) F% z# S ll weather navigation system. $ Y5 `- f, ~$ och is not$ |: d5 O- k9 y4 c* w; j continuous from power supply to ground due to a break# a1 Y# W6 X) ?" [ in the wiring or failure of a component. $ b6 W( k9 o" O" f: W2 \ C' l( w; `见Operating Empty Weight + v: a7 h8 Y T2 j% x% X. ~9 }O4 k+ ~# b! U( O2 z) k f: D O8 a( T9 v' B/ d" ` o OIL SEPAR/ Z' z% X$ H1 H u8 _ a ; Q4 C5 ~% G: o9 Y+ H4 C" ^$ G+ WO8 l+ C4 T' ^1 f; W! U7 ] O" F4 w* [ _; g) ?0 J OMEGA NAVIGATION SYSTEM (ONS), A worldwide,0 Y4 U; ^8 z- _/ P; M7 i a & W+ N0 i0 R' W4 ^6 a# NOPEN CIRCUIT, An electrical circuit whi 4 r3 O; Z5 V2 M! Q7 n0 P9 ^使用空重,' C6 T5 c6 S. o- g2 m( b W. P c( O' j Z# E" ? 面, ; _9 u O' x" v" h油冷却器,+ d9 `/ b* w4 S6 A- K 利用燃油或空气的流动来冷却发动机滑油的热交换器。 & A$ H9 }) `% x- H3 `油分离器, $ W- {! K0 A( I6 d1 M: `一个能从回油槽或油箱发动机滑油中分离出不需要的 9 Z" s% z! J0 s/ L, w9 R1 t气的装置。 - E* v5 T& I9 A( B0 F) j滑油筛, ! b& s# r4 J _8 |5 k滑油油滤的一种。 % q2 l- s; N- h: g1 o/ H液减震支柱, ) |# U$ \9 x1 w: h见Shock Strut$ L* U8 \7 H# |# J9 a$ x; e9 c+ K/ E8 I T5 s; T4 Z 相反的一面。: O l5 p5 p$ H; r+ T2 [9 I2 J* c4 a: D4 c! ]+ W( T9 O# ]& C6 @) t1 X$ W7 X/ n, B, R3 {3 B, @# B3 o! r; N8 N4 A A- e* o1 A0 L( n* l( s 面,3 |5 u. B8 @8 O; N1 L9 J 相同的一面。 , ?4 p- @& i3 @6 `% e% `个全球范围内全天候的导航系统。 9 Z" r6 T' Q* J2 E: ~* D7 ?或组件损坏而导致从电源到接地点之间/ d8 L5 n4 a0 O$ h U 不通的电路。 0 q3 R" p1 J3 V/ s" t% r* E/ [0 {. f1 i* |: ~' D% b 奥米加导航系统(ONS), 8 G" V& B. r0 e" W4 T( A; U' l" }! A' @8 R 开路, + f0 C0 J/ U7 E+ i由于线路中断 ( g- m0 B/ U0 T; t$ o7 }4 {英汉对照民用航空词典B OEING0 O1 b1 b" o, O" k TECHNICAL DICTIONARY 109& M1 d( R$ h; Z7 {( g0 L& i OPERATING EMPTY WEIGHT (OEW), The weight of' N7 w. ~- O. y5 x/ l an airplane fully serviced, including the crew but without- d8 ?2 _4 w- B fuel and payload. , A9 b: ]- C( F+ H& Q2 GPERATING ENVELOPE, Defines the environmental - G4 y4 o) Q1 Y y- {, \OPTIMUM ALTITUDE, The cruise altitude which results , F# j+ p) X' g- l+ A& J' m# Bin the best fuel mileage. % u- f3 ?9 r' i6 uOR GATE, A device or circuit with two or more inputs of" q5 q5 ]) c" v0 w D% d binary information and one output. The output is 1 when! u( M2 q C6 t$ Z any one or more of the inputs is 1. The output is 0 when7 ?9 \5 C3 u! t4 S1 G, t all of the inputs are 0.2 K6 F- n a2 w ORIFICE, A specified size hole in component for control# A: c, q H2 J/ ~, v% f; D+ a of fluid flow from or to the component. 2 E F9 H) X$ X3 S, d6 w$ L7 vORONASAL MASK, An oxygen mask covering only the 9 G, N, E* ~3 Z# g# g9 qmouth and nose.: L% ~# o/ I% q% V: ^6 p OSCILLATE, To swing back and forth with a constant* q+ H1 O4 A c7 V# c7 b7 q+ | rhythm.2 J; n5 V! q/ [, C, N 使用空重(OEW),( N$ `7 m8 V' F, n! g( K1 `2 b 使用包线, % z: P7 [, e: c9 d+ p确定飞机准予飞行的压力高度、温度和速度的环境极 P4 e, \ x' I" O' { 或门, . t6 Z4 s- K9 M. f具有两个或两个以上二进制信息输人,和一个输出的装* c# x# f3 K! l, j+ Q) v6 r- q 置或电路。当输人端有一个或多个为逻辑1时,输出为逻 - Y/ ~+ e) |" s" y0 e9 ^- _$ c. V辑1;当输人端都为逻辑0时,输出为逻辑0。+ h; P1 c; _/ }% }$ f) o6 L$ t 量孔, 2 p( S4 j" r# ^部件上用来控制流往或流出该部件的液流的尺寸已确' d/ u1 D, H4 \& f 定的孔。 0 P) M* r* E. e A# ^# |( y* g口鼻罩,6 }, `% L0 K ]: [, B7 @3 K 仅罩住嘴和鼻子的氧气罩。 8 v! f% @ D3 T! B- Z5 E6 h振荡, 2 v4 L! P1 ^2 e# w以恒定节律作前后的摇摆。 2 z+ r: ^, p7 ^; D- YO3 _8 ^ j" z0 d9 y limits of pressure altitude, temperatures and speed+ F) q, K1 x$ I9 [0 D" M3 D within which the airplane is certified to operate. 4 B V' c+ }' f" m1 Z一架勤务完毕的飞机,包括空勤人员,但不含燃油和业 ; z) G& b; x2 K3 h/ L e- D载的重量。& ~. u2 @# E4 B# { 限。 7 Z) i7 Z- F% Z最佳高度,( g( `7 }, L( }/ g 可获得最佳燃油哩程的巡航高度。+ G7 `) f# B9 z* o1 F 英汉对照民用航空词典B OEING ; s' ?! E2 G% k- w- gTECHNICAL DICTIONARY 1105 q7 m% T) Y1 i3 }/ H* ~/ ^8 A* X OUT OF DETENT, A condition away from neutral or a/ i/ u* L- E0 O. | OUTER LOOP CONTROL, For autopilot operation this C6 X6 n1 Q$ Q- x5 @7 q0 ~ S is control of the airplane's flight path to a target. 0 Z7 o1 S# G2 o$ j! d: oExamples are control of heading, altitude, and vertical$ P% r3 S5 h# h+ Z0 N speed.8 s; P) i: { }6 O: @; K) s UTER MARKER, A marker beacon located at or near + c; V& s; }" ~' t- j Qe glide slope intercept of an ILS approach. The OM is 0 k1 o% l; j9 \5 s& C' j4 m I* Knormally located four to seven miles from the runway 3 C+ O+ w$ _! s4 P/ E) F& ~3 {" lreshold on the extended centerline of the runway. ; u& ?- Q) Z3 m+ z; T! xW VALVE, A valve in the fuselage for 5 [, ~' E5 V6 {5 d( Fg the airflow from the fuselage to ambient for 4 D9 P& W3 F3 E. ~" Uation control.$ _6 G2 m& t% i& h. ` UTPUT, An information signal going out of a system or T/ E1 z8 r# `/ X: Y% Fpart of a system.. I4 _3 c4 R3 @ UTSIDE AIR TEMPERATURE (OAT), Ambient, or free # y# v: b3 ~; SOVERHAUL, To return an aircraft or one of its; H/ z* J s0 m$ b7 z% h/ K# F OVERRIDE, Operation of a component by a method# E) ~* {; D8 D" ?3 \ b different from normal operation.2 k" V$ t$ ^* S# O/ X3 w! w 操纵杆离开中立或槽口位置的一种状态。 / [! A$ }4 R* B' P3 s( c制, : d5 Q% o; K: k' t1 U航向,高度,和垂直速度的控制。" C6 _$ Y6 J7 V: _ 指点标,, A/ E S3 S/ K J! B* s 位于或靠近仪表着陆系统下滑道截获点的一个指点信 ; r# Y3 @! Q/ [' F6 y标台。它通常位于跑道中心线延长线上距离跑道头4至7 & a$ R, T5 v" |& X4 `海里。 , p! s+ O) j! u) j流活门,) u: ?4 b: w7 ? 机身内用以控制从机身流向外界大气的气流以进行增5 I4 J9 i( ^4 m. A6 e; B+ T 控制的活门。 2 w& D# E" o# O# D) h) p2 s0 _: b输出,0 ?3 l1 x7 `( m9 l 从一个系统或系统的一部分出来的信息信号。 $ ?& I [2 V4 U+ ~& v: P界大气温度(OAT), r" V$ X6 a1 l( Q) E# P 外界环境温度或静止大气温度。 0 A. O1 w5 D# h% g n5 E修,7 ~4 R' e& c$ u& R# K% R+ p 将飞机或飞机部件修整到近似全新或制造完成时的状 " M& \, U! L- ?" `; H超控,4 }, R8 }* J, A/ C ~$ r9 g 用不同于正常操作的方法来操作部件。1 z9 {3 \% ]: F2 x. Z3 W notched position.8 o+ F8 v; Y, G7 x# M" h" D! E% x O8 n5 m+ n5 Z! D2 f% D1 u2 n! C th * U2 R3 \6 d7 [th 4 l3 c7 _; h* B$ Y. v O" N, zOUTFLO ; r [3 K/ k o, icontrollin + F7 a8 g& a8 y& `, B1 o% Opressuriz: j. c" S7 s4 P( ]# H O 9 O: w) @7 O( {% P6 F( s' Ya& H4 Z ^7 Z( Q; Q/ q: \8 g: u O, h7 b2 ~1 X# p$ h" y* l air static temperature. * K! R4 `- v% c8 kcomponents to a like-new or just manufactured 2 |( e+ E! T6 z& ]condition. : E! _8 U4 t- z/ A+ b脱离卡挡, # @! a) ?8 \' F6 S- f外回路控' T }1 E. b; A: m5 Z9 B4 l1 ~) S( o 用于自动驾驶操作的对飞机飞往目标地的航径控制。例. p" l* w1 _' f+ ]3 X1 ^; |4 p, S b) D/ a5 v# x9 _! M1 i- ~# ^; G" b$ k4 P+ [) v9 E$ a* i O% v# o3 w) ]3 i: H; p1 y+ h2 N! P( q E* G% L: @4 ]; s* c, A" e 态。4 f0 ]+ I1 k c q6 T 英汉对照民用航空词典B OEING 6 S# o$ H2 I H5 _1 WTECHNICAL DICTIONARY 111 % C# p% ?( w8 g1 I* D$ b2 yP " l6 W, s! S# s, c+ i7 {; NACK VALVE, A valve for supplying air and controlling$ R" b* h* ]: o7 L! r manifold to the air4 j0 E) H0 h/ [5 ~3 n onditioning system.& { i8 [0 d% e! L* D ll piece of any substance or + |9 Q8 \+ x, O4 qphysical matter. # [( ^1 d2 n# m' Z1 ^3 Gh . y& J2 I4 M' ]- O% X3 ^rovides flight crew and attendant announcements, & Q5 l$ y8 k* M& @oarding music, and chime signals to the passenger+ V- j" Z; y( o5 y1 m6 [) c cabin. + @$ R8 j4 ^' {1 W# h* c, dASSENGER ENTERTAINMENT SYSTEM, A system% q& }6 U, U" I; i* B _ tertainment to$ r3 u O% J, I! N6 J6 y e passengers.2 N( H; s: W) ^. O, v PAYLOAD, That which is carried to the destination, ( p2 N1 W S4 m- `( M" Auch as passengers, cargo, or mail.6 ^9 v4 n$ ~/ N' N6 G CA, SEE - POWER CONTROL ACTUATOR; H% F; c0 h6 H" J9 j. i5 |; u PDCS, SEE - PERFORMANCE DATA COMPUTER ) k3 P2 v( ?: K5 p% rSYSTEM* q- E5 t" l6 d3 o3 C 调组件活门, ' {6 ]# k9 M$ W3 z H( h- E* `7 G由气源支管向空调系统供气并控制该气流的活门。- |2 Z/ n4 t" x4 s, y 任何物质或实体非常细小的一部份。 3 ^& w. i! J. i. q* t8 L% t旅客广播系统,4 t. o9 c1 N5 d5 f3 F" r 能使机组人员向客舱进行广播、播放音乐和发出谐音信( B: x+ a. N* Y% p1 ?! z 的系统。' Q3 r' m( T, {% g 客娱乐系统,7 k6 U* P `, ?6 a 频和/或视频娱乐服务的系统。 s8 @1 }* u: i 由飞机送往目的地的载重,如乘客、货物或邮件。 % W/ e8 L9 J7 \( k0 F$ r力控制作动筒,$ m3 e+ j. K6 `" f: ] 见Power Control Actuator9 k; Z8 s; l L0 D P R* I5 W' R4 e- z: b# m/ A air flow from the pneumatic* k( U" Y# Y7 K# h' ?$ l4 o) V7 k' u c & _6 v/ L! i/ N7 @6 yPARTICLE, A very sma 6 J8 o! V; _- u" D: ?PASSENGER ADDRESS SYSTEM, A system whic" B7 L4 Z, D& c& ]8 `1 F p : y* L- \6 P0 S% [# f2 Z/ Z+ \b $ G$ d) q! P' V3 q% r3 W; \P 8 s" @2 f) o! Y' jwhich can provide audio and/or video en9 S9 }9 O' Y# a th , y6 t% y/ W1 gs 3 C- e7 Q* T9 d; BP ( y' E3 P I; S' o+ _PCU, SEE - POWER CONTROL UNIT1 N) e" E4 m! V. J. t* w$ }% T3 B; {: b. J" [3 M微粒, . i0 c7 f' N& b% I' L- \: U& S0 O. q$ A- D' a% K3 F% n$ M1 e P9 u向旅客提供音( a; h, I5 |; _- @ 业载,! [; D$ n* D# o- R$ p' Z# e5 U( U- g" z4 g2 I ." n7 d, I. w9 W$ j$ ^: P Control Unit % J' a+ `7 H9 N. I* A. ~$ D动力控制组件, ~' {5 t- [ h+ F# v7 r6 v 见Power .: a+ J6 W& R. R3 \3 Z( | 性能数据计算机系统, 2 @9 X/ \7 T5 s5 F6 x2 d- G% y见Performance Data Computer System. 7 Y% E4 `8 v4 x& F英汉对照民用航空词典B OEING+ I# p, V8 P, ^3 [0 ] TECHNICAL DICTIONARY 1127 N: g* L- e! e7 U0 e PEEN, To cause a more corrosion resistant surface by2 J- m4 c& V2 F. T% S7 G, Q; B5 m multiple impacting it with a hard material such as steel1 p* }) `$ w2 ], N pellets. Term for this is Shot Peening. ; W# t& }$ a$ tDefines a position on the aircraft relative to the mean( Q: V* x9 `$ z# K aerodynamic chord of the wing. 0 x. P/ X$ ~5 p" i$ p8 E+ gr as a percentage of a fixed ! d, h6 j0 u& h) N/ Xmount rather than revolutions per unit time.9 l4 I3 ?( } l* T9 U1 c amount.3 ^7 k3 R; U; d, y K1 o ERFORMANCE DATA COMPUTER SYSTEM (PDC, 2 y! L( {" f7 {$ bPDCS), A device which provides data to achieve the: C& C9 O1 v+ b4 M) x8 B most efficient and economical operation of the airplane.4 `1 ^8 e* O2 T. d' ]7 [ PHASE OF FLIGHT, A portion of flight specifically5 _* R" b4 \. a; x" Y- W+ s devoted to accomplishing such things as takeoff, climb,- ]3 a' o& ?! O6 M cruise, descent or landing.: J6 U0 [9 u2 M 这个过程名为喷丸硬化处理。- @& ~ _! P' \6 M& @; [2 \ 平均气动弦百分比,& X' X Z, t/ h. @# R 间转数来表示低 + S8 d# ~8 f0 m, S9 p压压气机转子的转速。 9 @ i8 {) r& x4 J! ~( x$ F性能数据计算机系统(PDC,PDCS), & y& w; O, F# Q( l5 l一个能提供数据,使飞机达到最有效和最经济的操作的 : g; [3 w5 x6 P: r置。 " u7 n4 V# ?$ U/ b! Q行阶段,0 P3 h/ G5 O! f; K" ^ 飞行中负有一定任务(如起飞、爬升、巡航、下降或 7 F: v/ G7 T& r- O9 \份。 0 N- x! H. `2 b5 U3 r# P0 R1 LPERCENT MEAN AERODYNAMIC CHORD (% MAC),6 T d3 v" M! _$ q0 R0 ~ PERCENT N 1 , Expresses the speed of the low4 e& q% v4 z) @2 I pressure compressor roto' |: w4 X$ a+ _; R# l a 1 I$ W# T6 }, _. PPERCENT N2 , Expresses the speed of the high- x- ~9 V: a/ E# x pressure compressor rotor as a percentage of a fixed : [' L& I+ V) d8 Z. |# pP+ T' u1 b0 @( Y* ?# P+ B' o 喷九, ! O5 m$ K3 V% ~- P为形成防腐能力更强的表面,多次用诸如钢丸的坚硬材/ X/ T; O. |3 N 料冲击表面。 ! y; o1 h8 a- i6 {用来确定飞机上一点相对于机翼平均气动弦的位置。 a* _& H. {+ z; \1 R" c+ bN1百分数,& J J- d4 i9 U2 W N8 N* C, K 以一定量的百分比而不以每一单位时 + h* t5 T2 j% dN2百分数,( u3 |5 ?. s% r 以一定量的百分比来表示高压压气机转子的转速。- k4 {, {0 N, ]* t: p% W0 P& A/ h! V; @* N, v( G% A+ T5 m/ Q$ O& G% W* G" `- W3 m 着陆)的部& t- \6 f" ?8 L 英汉对照民用航空词典B OEING 2 p' ?0 ~# f. I$ A dTECHNICAL DICTIONARY 113' U" V) l" x/ S& j! P! A+ I; Q/ c PHILLIPS HEAD SCREW, A cross point screw with two6 t/ K- y! a, k$ J! w% \! b1 F en with a flat tipped Phillips head* w9 G8 a' j- H$ K0 z crewdriver (see Reed and Prince).$ p. J6 T; N: W- O4 Q' o ITCH, The rotation of an airplane around its lateral5 @: Y: ^9 N2 A( j: N) b xis. # Z* E/ V8 x( g6 [! \% j: fne 3 X& C) A; W l# qose up and down movement controlled by the $ o: k2 s# T: [levators (and stabilizer for trim). ; \" Z+ W* B* I5 K# P$ OITCH RATE, The rate at which the airplane moves in 9 s( t& Q- o5 o, p) e( Y9 he pitch axis (nose up, nose down). 0 R- w9 U' H- N( |+ }5 U% l4 KTIC TUBE, A tube facing the airstream @2 ]$ o# c/ u3 u' m8 Z$ c( c hich measures ram and static pressure. Used by 4 z) Y: v5 I5 O' b# h8 z9 oirplane instruments.$ y, {5 U: }+ f1 K: I+ H7 R 丝钉。由平, _# d& S! _$ R" b; b4 E, s 十字头螺丝钻驱动。( Z1 P1 w# [* D, ^0 ~; ^ 仰, 1 a' o" t4 |8 Z2 Z5 B. S飞机绕横轴运动而造成机头的上下运动。) x8 m% ~% r, r) o# p 一侧通向另一侧的水平轴或横轴。升降舵控制, j+ X% _& [. ?" v( J2 A* J 头绕此轴作上下的运动。(水平安定面则用以配平。)! S' i, f. H+ {3 m7 U 俯仰率, 0 i) m1 h; \3 ]; N" b0 |' W飞机绕俯仰轴运动(机头向上或向下)的速率。 - A" a6 b' n# Q$ V# C管, 2 b# ^# K# S6 w9 b: `开口面对气流以量取空气的总压和静压,供飞机仪表使0 ~- c M$ B: ~! ^" |8 `4 ^ 的管道。 3 y/ |8 a1 j& W4 S6 f0 k8 J, Zdistinct tapers. Driv : B, W0 B% n6 r2 w* vs$ |- |; m8 C: O1 u! Z2 A m! \ P ! d/ m; g$ A+ `% `( r& C1 da* q1 R3 @9 \/ J! x j w' n PITCH AXIS, A horizontal or lateral axis passing 4 C/ e" `0 u* t' gthrough the airplane from one side to the other. Airpla$ I& s, L) k2 n3 U# K n 3 P" J/ c! n: G5 j; We7 Y& I: r* }* s% e P / Y* Y! A' R. A3 q( Rth 4 u* T+ s+ \, Z% pPITOT STA5 e# W7 E6 W* v" B* F/ R w 5 k9 S9 q% o$ C: y; n5 a8 Y% W! `a 6 d8 p+ M L+ G十字螺丝钉,/ q, H! n' x' x: z% A( N 螺丝的顶面有两个明显的锥形十字四槽的螺 ; I4 O: z% G1 D( K" D- H3 F8 W) `" h0 }! D4 b: Q4 \, Q" c: O" \! a. k: {俯仰轴,; u1 S+ n9 w* ^; C0 s( E: H/ t% H 从飞机2 y% y ]0 }6 T/ C$ q v: _' r# Z3 T2 Q8 p) C 总静压; W: X8 t4 {! A S+ \& H. Q6 U# O) a( |, t% I英汉对照民用航空词典B OEING. F* S/ _3 F/ I% V" u) } TECHNICAL DICTIONARY 114; y1 \# }2 }- f- B PITOT T 5 m% S7 `# x( v! a5 l4 wmeasure( l) z$ L* H2 ?4 ]$ N6 V* u* I( B UBE, A tube facing the airstream which1 h8 T/ c4 u' @$ a) T s ram pressure., l2 i7 l2 Q/ L8 Z PLA, SEE - POWER LEVER ANGLE% n* J# a( e+ Y7 d r " p& R5 p Y+ J( i5 Fe & U$ S6 _$ i" c' u; U; d$ ?+ XLEXIGLAS, A registered trade name. A transparent9 W" z! L* E! m& Y5 r2 X r any purpose. 6 r6 g2 Q Y; v& CNEUDRAULIC, A system or process which is a' i8 G: J2 u( {+ w i o res.# L0 o/ _) D. b6 S% w PNEUMATIC (NO. 1), Cold air, controlled and/or! g* M. {9 d& c' `1 N9 a6 y pressurized. 0 c3 h1 p5 s+ z( i托管, 2 r" r7 t. l8 b1 e2 _7 m面对气流以量取动压(冲压)的管子。' i# h3 k3 z ?" f6 q! E/ }2 R 门杆角度, 4 s- e9 h$ Y8 N( P% y" g见Power Lever Angle7 Q: z" e# v0 [; h9 [! p/ I PLACARD, An attached sign providing information o * C1 Z7 J2 B# z3 N/ R$ Finstruction. 5 i6 O4 z/ H# P0 L& bPLENUM, An enlargement in a duct which changes th6 \: I- C/ ^3 K. A$ q1 K5 ?& E- X8 j flow characteristics of moving air. Used to remove3 k {0 p7 T0 C' E) S$ @" O pulsations caused by variable airflow./ C5 N( F" E- k H1 v; z P+ Y8 R: }' K4 m acrylic plastic material used for aircraft windshields and9 u; r7 q3 L9 ] side windows. JARGON TERM - sheet plastic of several ' [$ r* m# W+ d& Ptypes and used fo ! ], |# n+ y" c1 b& d+ fPMC, SEE - POWER MANAGEMENT CONTROL, w& q% I7 c5 J/ R! v P + J$ t; X/ N! Q2 q7 Pcombination of hydraulic and pneumatic pressu ) m. V" J$ M5 [- c2 Z+ t# V+ b1 [; I. n8 \9 V6 d" I( b) |/ h9 T7 B7 g6 V9 v4 J8 g8 n. J& F8 p1 K7 e脉动。 , N" Q% C+ E" \/ q, v' r; ]机玻璃,! o7 ~; {8 X+ y+ l: U6 _4 k2 m2 c 名。是飞机风档与侧风档所用的透明丙% f3 f& t' F0 }5 y( @ 控制,* C% m5 O5 h5 N7 @6 ]9 M 标牌,+ ]; R4 f# b" w6 s 提供信息或说明的附贴标志。 2 _3 O9 v: _4 ^4 t整流腔,+ e. C& _, N* a0 O 管道中用以改变运动气流特性的扩大部份。用于消除可+ V I; B( J2 Z0 k 变气流引起的# F z7 R% M7 `+ F. h( ?3 B X) y: `* w& |, ` 是一个注册商品; g1 A% T; Z& l! N& b# w 烯酸塑胶制品。行家称之为多用途化学合成胶片。 1 h A' `3 j3 w( }动力管理 : I, u/ P# N. `* D见Power Management Control.( S; S# j- F3 W7 w$ M5 P 动液压,4 c# C2 F+ n, |8 g 推动的系统或过程。- P& J9 R v( {; l+ n0 F2 _& r 1), , o- T; e0 y* V0 a: w8 ~' o1 j! a6 O. P* ~7 r A4 k1 Y/ e) ^由液压和气压混合 " E0 ~- l/ z* t7 u- A, l压缩空气(NO.7 \4 A/ e1 m, k) q" r 经控制和/或增压后的冷空气( b; y- Z( S9 [6 D' a 英汉对照民用航空词典B OEING + V% |, Q$ M$ O# }* z. ZTECHNICAL DICTIONARY 115* l& G$ `% u* i# ? PNEUMATIC (NO. 2), Air, controlled and/or- R& \( p& Z5 o6 V' \2 P% r2 Y pressurized. 8 C* g; p6 B3 m9 I) \8 Q0 BOP OUT INDICATOR, A device on a filter which : b7 R; w1 Z+ e7 M& kroughout a material.1 [& I8 s. Q; I- N2 `' z' K ition.0 I! Z# ~0 i1 H Y9 M POSITIVE, Definite and intentional. + d& z6 _; s: q. |(No.2), 1 t. }9 I6 Q& H6 v/ G4 y出指示器, 1 T6 q; P" }8 u0 c: E% }到达一定的压差时,它会从壳体内 . W$ }# n' ?0 c; N指充满整个物体的细微小孔或空隙。 4 g6 L7 U9 B' Q y( o* m4 w- h置基准的飞行管理计算机的一种操作。4 ]$ _7 B5 y5 ?! q' m 肯定的, # X( \* @7 ?% \1 a! Y1 x一定而且有意的。 3 i* G3 }; B$ o6 W+ `/ lP ' B) C& Y9 A4 r/ mprotrudes from its housing when a specific differential, n. j+ C! [ E' ?& _% g3 j# e pressure is reached.2 s; a2 \& }7 l Q; k POROSITY, The term for pores or small cavities% ]' d8 H) a3 i th1 o9 U0 M. i2 b/ y POSITION SHIFT, An FMC operation used to change5 n5 B( a( Y; c0 [ A$ [6 E the reference of present pos' v4 e! ]5 f! A! `# s5 a 压缩空气1 `1 I: N! R1 ~+ @ 经控制和/或增压后的空气。 ; h6 }0 M: q6 p* J; U1 N( U8 e) q& e3 D- g8 X$ s 过滤器的一个装置。 / C1 p- v1 m" z. ^$ r8 }伸出来。 # G! Y1 A7 M$ L- l气孔, 1 b$ O5 l; z& Q# v( A: s9 x移位, 6 a% m& I N" I0 w' G8 Y! J; a) D用于改变现在位! o9 m& g) | v- B 英汉对照民用航空词典B OEING ^, y- Y4 x( Q5 I& @/ pTECHNICAL DICTIONARY 116 # o2 b9 `: H- }2 iPOTENTIOMETER, An electrical device for changing " y/ |" v* h5 ^0 uthe voltage supply to an electrical circuit component. / t* Z; m1 S% E( }. Qr+ U- C1 q$ A, T2 v2 n6 Q' k/ }) u+ @ bly for operation of flight controls. & ~! g$ W5 [0 VOWER LEVER ANGLE, The angular scale on the : r. d- |* ?) O0 ?) K; gmain engine control for showing movement of the power3 W0 i9 {6 r! C( O2 z hrottle) lever.! D6 ]9 G. [% B* N OWER MANAGEMENT CONTROL, An electronic# R, p; ~& f+ n# x* }+ [ ngine control.; x x" L+ c$ z OWER TRANSFER UNIT, A hydraulic motor/pump for/ V* i7 h! s4 j* U' P. q. S6 ] upplying hydraulic power to components when normal & \: E' y7 b* m% }# fRECOOLER, A heat exchanger in the pneumatic/ F* E2 \3 B% @$ X! z+ A& I lied # _6 o* [. c% r5 ~+ U作动筒, . o+ L% L, V- r- Q' c6 L8 R+ s件,* r6 X6 u% t1 l 油门杆角度, ! u7 E) J. B. s: i. Y1 P1 o主发动机控制上用以指示油门杆运动的角刻度。 # e, G# `9 k4 Y, y( V! y* I动力管理控制, " J i1 \# ^, |4 k控制发动机的电子装置。 4 S7 s6 C* L' l. k; W- R) H# U. H力转换装置,# Z: D. t6 t+ x 当无正常的液压来源可供使用时,用来向部件提供液压3 t4 ?2 t% v1 j7 g# C/ r+ p 马达/泵。: k2 y' m; \/ m. ~; F4 k5 M 冷器,7 [. r5 R% B, k 中的一个热交换器。它将发动机引气冷却后 ) U: S7 o$ o$ m6 F% Z供给气源总管。 # r3 S3 G3 _, D7 s9 k% g tPOWER CONTROL ACTUATOR, A hydraulic actuato ( t0 r7 v1 C$ {- hassem 1 I. w* r3 C& MPOWER CONTROL UNIT, A hydraulic actuator* O. V7 \- J! i9 \4 \ assembly for operation of flight controls. ' w2 H4 P6 q6 G6 }' wP - x% X; v/ d' s; ](t6 h1 t5 Q2 E! J, C; ^) h Q P 1 d X, |3 z' ?' l9 G- [2 A. M Ne . G y0 O& G' Q' F; ]! {/ [P , u7 t- d& }5 z: vs & J* A3 q) h5 w d: y% f+ gsupply is not available.+ G# f, S" Y$ L, O P - q8 j1 o% X4 q6 `- t2 w! S: Jsystem for cooling engine bleed air before it is supp& b# @9 y. e. J: U to the pneumatic manifold.- x3 f+ k1 M/ ^ F* {9 U 分压器,5 U9 L1 C* x4 x+ `( J* V# _ 用来改变向电路部件所提供之电压的电气装置。7 X8 R- a2 Z1 X 动力控制- F/ f1 q) c( B" g" D+ I 用以飞行操纵工作的液压作动筒组件。 ) \+ e" ^ v# O8 u动力控制组* ~- y0 g- i: W+ R& L; z 用以飞行操纵工作的液压作动筒组件。* u( {! {3 v. S5 K) y2 M0 l' i$ p5 T/ H, b% L4 {8 {9 [1 i 动力的液压0 C7 p2 R8 a2 N1 @* i* z- T: |. U, k/ U6 f. B3 r8 y8 u& N) u2 w在气源系统& q4 t) J' G- M" a! w/ k9 f 英汉对照民用航空词典B OEING 7 n" s) D/ i' D+ \$ M7 T: Y! QTECHNICAL DICTIONARY 1179 m; g% T- }' F& L9 n2 R: w PRECISION APPROACH PROCEDURE, A standard! _' a1 x/ H) y& L* ? edure in which an electronic 5 Z9 r+ l! r" W$ @+ }6 P d! B% ilide slope/glide path is provided; e.g., ILS/MLS and+ z% Z+ p6 Z# x" ^! Z: M0 i- _ PAR.- \5 y: K$ E8 U6 d RESSURE, Force per unit area usually measured in. ?9 Z- m8 Y) @ V6 Y ounds per square inch (psi). 4 C0 Q% F6 K ], Q5 V" l* yRESSURE ALTITUDE, The altitude displayed when0 ^- m0 I4 N5 @5 M' I3 x e barometric pressure on the altimeter is set to 29.92 : j+ l6 l6 C/ O4 @) IRESSURE REGULATING AND SHUTOFF VALVE, A 2 |* i3 U7 A" O" @alve in the pneumatic system for regulating bleed air % n8 o8 |, a& f5 X! vpressure from the engine to the pneumatic manifold.- ]2 O* R0 ?' }- A% U4 d RINTED CIRCUIT CARD, A plastic or fiberglass card . i+ h; h/ E4 R" a8 l: I# S% lith electronic components and copper strips forming a( h i$ R* p7 j8 g( M" U ircuit. : c: y! V B+ Q% i. tRIORITY VALVE, A valve in the hydraulic system for 2 o' ^- r# u4 q4 i" pROCEDURE TURN, A maneuver where it is8 b& u/ V- _* ~3 p8 @4 Z6 o lane. r7 ^; k5 h" t: `; p2 L proach course. 5 N' J/ P6 c! j2 C: ]6 o# }: h精密进近程序, % Q3 N6 T5 H J1 V. y& [己提供有电子下滑道/下滑航径的标准仪表进近程序。' v4 Q9 m8 `: k/ l D 如:仪表着陆系统/微波着陆系统,以及精密进近雷达。 0 O9 V* `; q' H1 M; S, w% D压力,0 \$ z! a$ H8 G! o' Q0 f3 X 单位面积上的力。通常用磅/平方英寸(psi)来度量。 f8 J* z5 [& O. B2 N- J, R# F压力高度,5 V. T$ d$ s( {4 m8 N) B" u 当高度表上的气压调至29.92英寸汞柱时显示的高度。, n2 [% k7 E% j; t( _, s 力调节和关断活门," E3 A: P w5 t" J- V$ p- F 气源系统中用以调节从发动机到气源总管的引气压力3 l' T8 O% N4 q+ i9 V9 f& { 的活门。( s# w+ n$ N. M4 S9 K2 s# c- y# S 刷电路板, 6 J( c i% l8 _$ v" P由电子部件和铜丝所组成电路的塑胶或纤维玻璃制( f" T# x! D1 f' N I8 O' C% Q0 b 薄板。) D- G! D! s/ r- S6 C) f# F& t 先活门,6 F5 q6 o' {9 \6 V/ g- S( O3 g ,用来使各部件照合适顺序操作的活门。2 t4 \0 L# Z& g) x0 p7 d 序转弯,' ]# N* Y7 X. j) o' T6 d/ G, r 后进近航道时所做的机动动作。: U6 X1 e% b2 ^# W instrument approach proc 0 ^8 \. N- W$ _7 ~g 0 w. `) {; t( LP! t) O2 {3 D7 H p & K- k# {$ B$ I: DP: g$ b6 t& d; r" c1 e th2 b4 o; K6 r+ F) m! E1 w! t" r inches of mercury.( a7 u5 v6 x2 S; K P $ S. j' q+ \3 q3 c& N5 X+ b& Fv ' x) A9 z. Q" b0 s6 E2 wP8 L$ O- S6 E& F7 p w- b. @# F* E) w0 N+ q" _% i# j c ! g3 s0 _- u! _) b' P8 p3 e7 vP/ x( k$ Q1 j9 l M1 C) [ operation of components in proper sequence. ; u- B3 Z; R6 g4 iP" q5 {9 C$ m$ i* Q, U necessary to reverse direction to establish the airp! g" h+ d5 s9 O+ M) D; |6 n' g4 D' V on the final ap ! M8 e( x% V1 H: n& P1 [, b- ` p* z% F" m3 m- }* X% M- m$ K1 D6 k1 P8 v! o" X# ^7 B1 u 液压系统中3 O( [. G, ^% I4 \- L. b* m6 g9 c! T# l在飞机必须反向建立最, O9 F7 t& N* \. J8 p- T- Q. m- d" W 英汉对照民用航空词典B OEING # l8 ^, e( U$ I- j5 H9 `TECHNICAL DICTIONARY 1180 T' E8 p. q1 M7 b% _7 ^2 P PROXIMITY SENSOR, An electromagnetic d5 [: e V4 d8 c. Z senses the po; j J7 c+ D8 `9 f$ \0 v7 Q evice that& w2 G, a# Q; r0 M sition of a moving actuator. The sensor 7 R4 A/ u8 H2 y8 a0 b$ ~. mas two or three wires.1 `; g. n* I1 U8 j ROXIMITY SENSOR ACTUATOR, A steel plate # s/ b& L0 H" z+ ?cated on a moving component for operation of8 R$ ~3 S. N" z1 O* K2 p roximity sensor. 0 r7 T( f) M. J6 ^( ]- fROXIMITY SWITCH, A printed circuit card for ( S5 e) a3 J8 W9 s; g$ \6 C& ktransmitting sensor signals to indicating lights and % o6 C3 O1 f& y/ H. b邻近传感器,! Z% m1 z6 `. A! E* W1 Q( y, B 能够感知运动中的作动筒位置的电磁装置。该传感器 4 `" w- T' Y5 z7 Z有两或三根电线。% R+ Z/ M% M% j- A7 u 邻近传感器作动器,9 U" ^9 ~2 i& O0 Y; x 位于一个运动部件上,用以操作邻近传感器的钢板。# S2 y4 j; d7 c5 i L; B, \2 I. ~% ] 近电门,9 _7 X9 ~: a- `) s3 c, r 传感器信号传输给指示灯和电路的印刷电路板。+ M/ k) ?% y+ f0 b" ]* H h) M5 f0 M- W% H. x P) m! w2 B; m1 R5 q4 C& ]) m/ p lo) F$ e# {8 `6 f# q6 I6 X+ G1 Z p ' ~4 R# x- @' H e6 t7 v0 _P; ?: W2 T& N4 h0 t0 Z0 j0 ~+ V circuits. & j$ \# S) k# h" N- _0 x! d. p4 [, j- y4 A6 N用以将/ M) h$ T/ {( U3 N: ?( r6 n 英汉对照民用航空词典B OEING" G' i; _( D3 m TECHNICAL DICTIONARY 119; g q6 E' G/ M* v; D2 ` PRSOV, SEE - PRESSURE REGULATING AND / T2 ]) k9 x( t% MSHUTOFF VALVE / H3 n) l+ I' C' z- Z/ ZTU, SEE - POWER TRANSFER UNIT $ u# M/ C- s2 C; n5 r( Eremoval of dirt from the air cleaner.( N* h% \* \) t& o1 m @1 U) P2 i% f n 6 V- K: [* I3 K* ~QAD, SEE - QUICK-ATTACH-DETACH2 O- l" b& J0 x5 X( ?8 D7 z8 V ICK ENGINE CHANGE & e2 ~$ S5 W" m, Pheight above airport elevation. 3 Y0 F( Z: {! X( I/ Y. D1 P' eNE, Altimeter setting 29.92 inches of mercury, 1013.25 ]$ R. a1 J! a. M QNH, Altimeter setting which causes altimeter to read5 Z$ b& I" t$ {! y9 v/ f/ K height above mean sea level./ o6 f/ b/ k! Q 活门,: E( s5 o5 W B# k, O) ~) z P ; P& ^; b8 q& I9 T' ]PURGE VALVE, A valve in the pneumatic system for4 @* D# @. O# C# t; ^9 u" k) l PYLON, A structural component for supporting a % ]9 w0 }7 @0 [) Dengine from the wing.9 S* B( |' b {& s3 B3 j, }6 N Q4 z# _4 |1 v/ V3 w QEC, SEE - QU 6 h9 [6 _8 I; w2 |# JQFE, Altimeter setting which causes altimeter to read ' d' Y+ A% { I P2 `8 K2 Z8 \! MQ # r* r5 Q$ H h$ r3 VHectopascals or 1013.2 millibars. 5 U( O! v$ q" \调压和关断0 f2 Z+ z, U# d: N! y- s9 n 见Pressure Regulating and Shutoff Valve. ' G% g# h5 e( ]动力转换装置,7 l n5 _1 q1 T- n5 T \# B 见Power Transfer Unit. ) r `; ^ X; O @气源系统中用以清除空气清洁器中之灰尘的活门。 9 V+ y* |4 X8 F4 X3 V速装卸," Q3 _6 G9 S- k; Q' x 见Quick-Attach-Detach9 i1 D: F/ O% ? 除尘活门," T" B" u/ R' m4 j 吊架,1 x( [0 l2 W- d. B0 |+ [7 I& Q% @ 用以从机翼支撑发动机的结构件。 4 P8 C/ n5 H$ ~. C5 {' x3 Q& S0 n( P# S' d0 R, Y/ x7 F3 ` @' v) ^见Quick Engine Change% b1 a! C; {$ Y; g1 v7 z" ` `- W 快速更换发动机,1 B" Z( y* B* E! ?. Z, X* g7 e, Z6 f) l z* b场面气压, 4 H( @- y& J- b( s准高度表设定, ! H4 Q7 J( c" J2英寸汞柱,1013.2百帕斯卡,或1013.2毫 - C9 Y) R2 {+ O0 X( y修正海平面气压, ( {& h& Y2 q, m4 @/ x使高度表指示飞机距平均海平面之高度的高度表设定。" U$ p0 \0 g5 e( `. s 使高度表指示飞机距机场标高之高度的高度表设定。8 b4 d8 |% }+ D. p4 U/ T% G ?9 x0 d" U! g. A 29.9 . Q& u$ M6 C8 ~* c巴的高度表设定。 9 ^9 a8 n4 m- c4 g2 ^ Q( ?7 {( t英汉对照民用航空词典B OEING5 o5 ~% w* k0 N) [$ S TECHNICAL DICTIONARY 120 E% O$ y0 U" X3 r( PQUADRANT, A mechanical component shaped like a; u- c0 s2 p0 Q quarter of circle for transmitting cable motion in airplane+ v5 _' m2 }, k QUENCH, A heat treating process to make the surface # C$ j, G/ o# k: ~. d, s- p' L8 tof a metal hard. The metal is taken from the furnace and+ ^; p! v# ^, l$ r- ~4 Q QUICK ENGINE CHANGE KIT, A collection of3 R: u4 `" o8 @0 J! @; f" a* a; Y e engine positions of a particular model) [* Z/ |+ Y; v, L( H3 Q: l irplane. 0 J/ L& d" L- Bng ) z3 G3 ~/ r: a; T' Z, E" |accessories (hydraulic pump, fuel pump, starter) to the2 {% y$ l$ S+ F2 ?; G" W% } engine accessory gearbox.3 c n; f+ ?+ k' t- N6 f. N S, Established the# }! \$ R) q- j- j& m7 ?/ r0 h9 {' P minimum amount of time to cool the wheel brakes; G$ I& O7 ?" y% P before the next take off is permitted. ) h5 i0 d, z5 T& }进油或水等液体中。6 p9 b/ [& B& ?4 ^ 快速更换发动机成套设备,; C6 I# s4 R3 J1 F 置的所有部件的集合。, h# ` h7 l! @: W 用以将附件(如液压泵,燃油泵,起动器等)接到发动; u9 J! `6 Z, n! C$ w' K% z: r 附件齿轮箱上的夹具。$ o, a' F7 }, U' r }: A: @. l+ n 快速周转极限, $ R1 K" e# {! M在下一个起飞许可之前,已确定的飞机轮刹车的最少冷, f0 s- Y! Y ? 却时间。 5 g6 U; @" D) Y0 S8 ^7 Pcontrol systems. + f3 |' R( ^- o( }2 ~dipped in a liquid such as oil or water.% C& I" ]# y6 I: J1 F/ y8 L components allowing installation of a basic engine on to $ W% E: b1 r4 rany of th! B3 ~6 o5 \# D" ]) s8 x3 c t2 l a 2 b! A$ s. @, N) RQUICK-ATTACH-DETACH, A clamp for attachi2 M a. u, Y+ i QUICK TURNAROUND LIMIT$ i2 b$ u/ i5 F 扇形盘,' F& m3 Y+ Q$ p# h$ C 飞机操纵系统内,用以传递操纵钢索运动的扇形(四: `- T& n9 v' b3 N* L& ^4 a( X 分之一圆)机械部件。 7 u0 x; z! C' A" G. h1 O9 g6 a' Z8 ^淬火, 0 f5 H6 ~6 o9 j4 Z; N( M5 ]一种使金属表面硬化的热处理过程。钢铁从熔炉里被取& z, L8 C- L2 S6 H0 x* s 出后再被泡 5 ]) j, N& I6 k0 w5 t7 u* g用以快速地将一台基本发动机安装在一种机型的任何 : t) b; O' Y: p, ?% X发动机位 7 ? C6 M" A, A9 o快速装卸,9 D6 J* Z2 `% a9 O% K+ S5 v t9 K& {* t0 m$ H/ O' r$ ]2 j' h5 x英汉对照民用航空词典B OEING ) v9 F; P: t/ z" N1 u6 e; iTECHNICAL DICTIONARY 121 # H' h9 Q* Q) P4 E1 M6 `QUIESCENT, Condition of an electrical circuit when no , y5 F6 ?5 k- F0 y) ?; `RACK, A place for storage of modules in the & w% N3 l( f3 ulectrical/electronic equipment compartment.$ j4 W! c0 u$ j3 ~9 S# K1 [5 F ADAR, A device which measures the time between the / _- z- c+ F, \, I, d+ h+ Ztransmission and reception of radio pulses and provides; U, v, J9 A, o1 w- ^9 k2 w information on range, azimuth, and/or elevation of. N& b8 Q! @; ~- m% v: f' Y# t- H- @ bjects in the path of the transmitted pulses. / R! ]0 m; `# q- y# g$ Y/ \om a & X! m; b8 ?: ?. G; Qar. ( l1 g& G: I& mRADIO ALTITUDE (HEIGHT) (RA), The distance of an + |2 Y7 d4 Z! j1 s# e8 l# j! Faircraft above the ground, as determined by a radio" Y8 a/ o3 T1 Y( E. b altimeter system.$ m4 J3 i! e7 Y2 J/ f4 ] RAM, SEE - RANDOM ACCESS MEMORY - [8 ~* A! N# s; c: \7 T$ d% HRAM AIR, Outside air that flows through heat$ C) u8 B; O* ^, N# Y exchangers in the air conditioning packs., k0 u* `( x/ ?& k 支架, . N& |% ?# m2 \7 T电气/电子设备舱内,用以存放组件的地方。7 o' t5 J% u j9 x( Y9 U; s 雷达, 1 B( i+ q$ P% h) z6 f测量无线电脉冲从传输到接收所需的时间,并提供范8 G( Q0 s$ x8 t+ x 围,方位,和/或脉冲信号传输途径上物体标高的装置。+ I) q/ ~9 A& M6 v% c h6 q 由使用雷达的空中交通管制员给予飞行员的航向。 ' ]7 M' N- a* m5 H& r7 s施发射出来的磁方位线。( k6 S. z) |) N b5 U 无线电高度(RA),( c4 F( J S3 |1 o3 d 由无线电高度表系统测定的飞机与地面的距离。. {3 j3 K; V! ~) ^ 随机存取存储器,+ ~1 G7 G A/ h4 x v 见Random Access Memory" t- U+ W5 |, |* ?9 E input signal is applied to it.* H/ N: J9 B5 o! K5 @4 Z; h R. G {% M9 |) H8 } e ' U- E4 W S5 `/ J$ K, P6 `; sR9 K5 d, V# O7 h o6 Q* [5 E9 Y- @. P7 ?) b RADAR VECTORS, Headings given to the pilot fr5 G! b" i6 c4 I$ y' y; v controller using rad & ]- p# Z. X* l$ |4 QRADIAL, A magnetic bearing extending from a9 a+ p( ^+ H# ? k VORNORTACITACAN navigation facility.' {8 `5 C$ t" @3 m' H; t3 Y 寂静状态, 4 \) f( U8 I: ^' h6 \ Q* ]. a电路上没有输人信号的状态。 + N: t1 U" b; ^ s0 N雷达引导,; A8 O- d" T |2 a& c" ~ 径向线, 1 `5 ?* l7 N5 w4 r" D2 D' u由甚高频全向信标/塔康联合定位/塔康系统导航设 " }: k g7 _/ D冲压空气,$ @: X/ g( e0 W5 J 流过空调组件热交换器的外界空气。2 @ `$ e8 Y. w0 f 英汉对照民用航空词典B OEING $ w: l! m( n" V3 m2 GTECHNICAL DICTIONARY 122 9 F! d1 v% D/ R- I( m: B' lRAM AIR TURBINE, A device which extends from the% g) r. S( R' O. @5 i1 a , driven by outside airflow for, E. o7 ^0 h) C mergency supply of hydraulic or electric power.# j6 k" t& `! {- s' s2 F2 v ANDOM ACCESS MEMORY, A type of memory in$ N+ Y) j$ d. K, H6 ~/ f& Q data can be written into and read out of. + f2 t' @3 A7 J" J0 j; `6 Nused for short term memory. - s3 S6 W V% R- o/ @# MAT, SEE - RAM AIR TURBINE ( J9 I0 x3 T, X: |& r9 R) o2 m6 FATIO, A specific relationship between one number & ]1 m2 w; R, \2 xalue and another." `/ \$ D6 q. o7 J I9 P: |8 | ATIO CHANGER, A mechanical device for changing3 e }3 ^; d) l5 O8 {6 E utput speed or movement relative to input speed or) q, G' @) z m* Q4 u- M AW DATA, Data from sensors not modified by the user! y1 w( o! H, S; d 况下提 5 O$ S) [% V" Q0 C液压或电源的装置。3 m/ E! T& K9 P 机存取存储器,* y- \) V2 U) Y+ r: x( N+ Q* @ 一种可以将数据记载和读出的存储器。一般用作短期存% u/ Q; g$ y0 O. H: D, [" B7 ^; C8 d. S 压空气涡轮," x3 K5 [6 u2 }) @% ^/ @! z0 z! v 见Ram Air Turbine; ~% r$ t2 H2 ?( Y2 Q5 t, ` side of the fuselage % \" S' Y5 i3 G- He , c& V+ {* U! @9 Z lR ) E; R, q! ^5 Q, u7 U4 j) S$ |2 e) hwhich the6 @: k5 B A0 v- V; } P Normally * t, `" F0 A8 R" }3 wR7 f" H+ Y4 |" n8 f8 |1 f3 U# v( i6 H R 3 u3 U# g- n! zv, a% L. H; Z5 p" u9 ? R4 b: S7 ~4 u4 A0 q& f/ I o 0 x5 ?( q% s) g8 o' u( }$ _$ Dmovement.! d% w m6 Q* I7 L- _. _4 p! G R2 ?: a# r) F3 E3 _+ K! H& Q system. 6 m' K9 A+ S$ ~- S冲压空气涡轮,, T. O' S" s5 C! Y& K1 G1 l 从机身一侧伸出,由外界气流驱动,以在紧急情. X4 k* R% X) ~& h+ P; f" ?7 ^0 ]: q! g- x# u/ {* x! w2 T, B% V. U" g3 |8 O2 J+ A6 l# L. y! E' c/ _! {, s% j2 c1 W. b& F7 [' ?比率,' T' s. Y" _) W- a- K% p+ _ 一个数值与另一个数值之间的一种特殊关系。 6 [; w- O7 t( p/ s, E- _: k率转换器,# f% u# O& Q+ p; E3 P$ V- i 用以改变输出速度或运动与输人速度或运动之间比率% L0 |4 S! F4 w; D! w8 w' { 始数据,+ X3 V+ t" k( l# ~. G4 o2 f- z# a' ~ 任何修正的,由传感器得来的数据。 / F" \5 ]- v* e6 O, c0 E) O4 T" w8 r5 d8 s" M: S的机械装置。 `! B0 \9 V$ j- ^' Q4 a9 ~; D, I- J; c. x$ x4 @2 q没有经使用系统作 . _, T" E; w1 }2 g5 q英汉对照民用航空词典B OEING# T; y* }, ]6 R, ~3 k! I6 d1 ^- h4 L TECHNICAL DICTIONARY 123 . K! K4 ^/ `! _+ u9 @3 ]READ-ONLY MEMORY, A memory unit in which 2 S8 Q$ R5 T2 Z5 m: i5 `2 @" Zthe computer. Under normal conditions the stored 6 ?) P V( [; k, r' Y) `information cannot be changed. , n7 @2 f& u) V: `* fECEPTACLE, One half of a two-piece connector. It is 0 X W7 y5 G; Z' musually mounted on a support, such as a panel. L& B( J; R0 z6 T7 j4 `2 H+ }RECIRCULATED AIR, Conditioned air mixed with air0 Q1 G8 A- z4 p6 l. ~ from the passenger compartment.2 d0 e9 g1 I8 b" M% S EDUCED THRUST, A thrust level less than maximum 3 |% z5 l8 z, X% rrated thrust.' b8 A7 n' [; s6 j& X EED AND PRINCE SCREW, A cross point screw with 3 F* B. |$ u) X9 d2 c% o7 _# Wa single straight line taper driven with a pointed tipped 7 H- b0 z* a7 E) F' g0 p5 lED SWITCH, A switch with two magnetic plates acting 9 R+ z& i! [* ]0 k9 ~9 Ks contacts and operated by a magnet.6 ^8 e4 G0 }0 ~% a 只读存储器,( A1 _* {: l) }9 F7 s- ~; } 含有由计算机永久存储着的指令或数据的存储器。在一 * @5 N0 |2 i! |- ~作任何的修改。; o+ W0 b7 M( A$ M- z 插座, ) F8 S4 } |* T, `, V6 i1 u. b由两件组成的连接器的一半。常被安装在支架上。, P' D& E' X( N/ b+ y' I8 H$ Y' a/ q 如:仪表板。 2 |- }3 L8 m( `再循环空气, # F( Q& h8 _$ J! c2 z调制后的空气与客舱来的空气之混合。 : d$ s6 r$ ^: C/ L) c减推力,& Y& `; t+ X9 F {1 s0 V( P# S# f 额定推力小的一个推力级。7 _ Z& l; W9 X' H) l" o* J; q0 k* ]% K 十字螺丝钉,2 g u! z9 ~$ `2 d; x5 E 的,带有一条直线锥的十字) G3 K: N5 ]- t, q5 v6 Q 舌簧电门, % ~) _% s) f$ P5 U: A" E由一个磁体控制使两片磁片接触的电门。 ! x2 k2 Q8 Y' K* `, p$ Tinstructions or data are permanently stored for use by9 ]5 R: x" p: A: K: h R ' O- F+ U& V, a6 V' e1 Y& ^R 8 Z) w/ c' U- ^6 I2 |* KR1 E. H p+ J$ V. K! U9 o- ^+ ~ Reed and Prince screwdriver. (See Phillips Head.)8 P& P* H% _7 U+ A R * V0 x0 e' V0 h7 D4 W# Oa k1 C+ @- i9 [/ j6 G般情况下不能对存储信息 T F" X/ d7 p# `3 z 比最大+ \* a2 M( F6 Y+ z 与尖头十字螺旋钻配套使用, c P& E" B6 \6 v* C2 I J6 i8 r 头螺丝钉。' o5 |5 [& Z% {' @ 英汉对照民用航空词典B OEING 0 z8 n9 q1 V: ^% JTECHNICAL DICTIONARY 124+ ^. ?: c$ i0 r4 U/ H' i- K% q3 l REFERENCE LINE, A line used in a chart as the7 F9 P' C! Z( \8 q+ C starting point for applying corrections to chart input 3 z& Z* t* M/ Ualues. One or more reference lines may be used in$ e; g% x* r- n, h) E8 N( S uccession. + ~1 ] E3 I" E, X$ a; F3 LD TAKEOFF, A takeoff which has been5 U d5 x; b# z& |! N . ! L" g7 Q. i, s. G7 |, @EGULATING VALVE, A valve for controlling pressure : e8 e" H3 O6 m1 S0 v' ]9 lELAXED, The state of an electrical component or3 U& r3 o6 G1 Z! f4 G1 \' e witch that is deenergized. 6 [, u& P4 ~. m2 ?4 B6 U4 `RELAY, A switching device in which the contacts are ! b9 h5 b z; c9 {4 ~. e( fopened or closed in response to separate current or" d4 ?; c) m6 Z u oltage.! m, V7 u9 \$ u RELIEF VALVE, A valve which prevents high pressure # n; C& W0 b+ r+ k+ D4 y. Ga system by venting the system to ambient. 8 D3 t# ^" V4 @起点的线。使用时可用2 [3 z: r$ ]0 z" y9 w 条或连续使用多条。1 f& j4 @6 R, J8 ?" l8 \5 | 断起飞, 2 ?. e/ j0 _# y& @( |离地前被停止的起飞。 }/ d, Q' Z. c5 U3 J9 E节活门,6 u" X0 R- l" n6 \2 W8 K7 Z 制压力或流量的活门。 0 l* V# f& f$ J8 Y. |3 G& h放状态, , y$ l7 Z, o! E" A2 \* O% Q: ?电器部件或电门处于关闭或没有通电的状态。: G8 p4 }$ V4 R4 m H 继电器,8 @; }; j, L E2 t- \2 k* m/ ]3 ? 一种电门装置,其接触点随着单独的电流或电压开路或/ e) |) l- {; B* i 合。 $ x- m+ K# x* J! t& D6 B释压活门,- @8 K: d7 x( e4 |! ]. ^ 通过将系统与外界相通,以防系统内压力过高的活门。1 Y; E& B& }4 ~# n ~+ @ v# B& B& G' f+ w1 j s. q' A3 {8 M% T' n$ K REFUSE - O3 e& n; m0 m0 y2 K+ h0 W9 b6 qstopped before the airplane lifts off the ground% O; n4 ]5 v( c/ a9 V R a* P3 B# w( e+ V' l( ` or flow. 6 M- ^) h3 ?+ x* q6 ~R ( X! Y. `! L' c4 i js' V& h3 D ~$ y; O* e v , N) p' ~/ l$ m2 B5 J* Sin ( d' q) |% n: \ B/ L, o基准线, 0 p7 `' ?( @2 a6 b5 K. E- _在图表中用作修正图表输人值的2 x2 [! a8 a7 r* x. U$ Y. P8 y. k+ }1 N7 t8 u6 K$ b1 q在飞机 + [' F7 g% y: ?! s: M0 g( y6 l6 e1 X$ D! M8 O0 l) c& ^7 }% X 用以控$ F$ V5 R# _% O* F& A5 ~- n1 e9 y% j5 A( [8 \* O& |- r% L0 c# M2 q9 q% r7 Z8 T$ ~5 ?( \英汉对照民用航空词典B OEING ( S2 `, m, z8 u! ?0 ~( MTECHNICAL DICTIONARY 1259 }" r. [$ J/ s& n' i5 l* ? RESERVES, The required fuel remaining on-board after8 r8 S: \: ?, X, X, `) S ESERVOIR, A container for storage of fluid.$ ?$ l2 u9 w' ]! } ESTRICTOR, An orifice for reducing the flow and ' B. m, G7 G3 G( V3 b1 qressure of a fluid. / p$ v2 k: u Z. WESTRICTOR CHECK VALVE, Same as restrictor but1 r2 Z& Y: M0 B2 V llowing flow in one direction only.1 `( J2 x2 ~- p" I7 X- G decrease the % l5 A* M. e: r3 {3 n5 X/ a" S: Gngine thrust to idle. T8 _. Y$ @# L( [4 T1 hREVERSION, To change to a pre-determined mode.7 \! \. R! v& x: J, k ctrical device for changing the' a9 l! z6 p: q# v% I sistance in an electrical circuit. - `- ]( _3 J# h& w, ]备用燃油,6 d+ m, j2 Z+ H p" ~ 照规定,飞机在到达目标机场后,机上需要的剩余的燃 3 o0 H7 v7 S: W% c- z油。9 n& [. s3 E7 M f9 Q 储液箱, 1 ^5 T1 Q- S! G# ?! B8 c用以储存液体的容器。; \# B6 f9 p% Y4 M# v! J 限流器," ]# r" u6 `$ {' z. S; A 用以减低液体流量和压力的量孔。 ( J1 T5 V% Q, b. `7 i# R流单向活门, ' F1 s1 p% I: v8 b# O% }一个与限流器类似,但仅允许流体向单一方向流动的活( V9 J( m# v5 n0 i 门。 ( W; g7 j; M5 r门,& f; e0 y. `! u" t/ H' G 自动油门的一种方式、用于将发动机推力减小至慢车状 0 M' S5 `) L2 {' V7 K( n: \6 G3 t3 z L) M$ U4 E; j1 s, B0 Z( I改回到预定的方式。2 p R% c, s& W" r 用以改变电路内电阻的电气装置。 l) ~/ B# J J- j3 _# Z4 X" h& Narriving at the destination airport as determined by # J' q& l/ h* u- I9 w& Iregulations. ! I8 D" @; [. d' H/ D% oR2 J. g9 i7 \# F- [) \! E4 M R # x% J! ?% v5 Q f5 Pp8 Y! ^+ x8 p! \# i* x" V8 [" i% x R( C" B7 x6 Z. l2 |) J6 n a4 L5 J+ [6 P/ [7 O- _ RETARD, An autothrottle mode used to- r6 A" g/ F8 O! t e 3 [, M( }5 Z: D2 R. CRHEOSTAT, An ele * i- A y }) u7 ]re7 N0 f2 }/ m7 r8 R% ~% G" H) i) w" o) A! k; Z/ m3 y# E* g拉回油 & U* u! @7 @: o9 N7 E; l$ F/ A$ d5 e% R; k 复原, * V5 o% z L, Z! @* v变阻器, 3 X. ^% N1 f Z! i1 ?3 v英汉对照民用航空词典B OEING. F5 @/ c0 L/ b! @2 T TECHNICAL DICTIONARY 126) B1 J4 ^% n; g, o! ~ RIB, A structural member of airfoil shape in wing,- A2 h1 t+ a, W* v$ X5 c stabilizer or control surface. - u. r7 K# {# L3 p5 yIG PIN, A metal pin for inserting into a moveable0 P$ i w, Z) D0 N' W* I% }) o omponent before adjusting the control cables and8 i! h; d& k4 _5 y6 Y$ O4 {0 \ nkage. 3 ^' Z1 [& ~" w. q5 B( o0 G( gIGGING, An adjustment of airplane controls and doors6 U! _6 J8 H' X9 J8 S2 m1 {. U r proper operation.2 E J, g& Y$ B3 [ onditioned air supply to the passenger cabin.; H8 ]0 s% h% q! j 装销,2 l5 k- C. I* O2 K4 B y' @2 T 在调整操纵钢索和链系之前,插在可动部件内的金属 + y. C2 i( k9 d2 s1 w) V+ \9 O0 h- _" I' K- {* x校装, ( w; G7 Q; n3 S# Z E4 z5 G使飞机操纵系统和舱门能正常工作而做的装配调整。 % e0 h+ V: J Q9 C; i4 L空调系统中,将调节好的空气送到客舱的管道。6 _+ g9 T( U3 v R3 z( K' o: E8 d7 E# y& i; w c ) v' B. T5 i: I% h Pli . _% y9 ^9 p- K: b9 x# E* I9 dR 9 @2 O: v) a* Qfo + _8 m/ Q; F$ n" F4 D9 ]9 k% s1 s6 v, ]: HRISER, A duct in the air conditioning system for # g# {, s x/ O; ?7 A# g3 F+ mc , Y" f* u+ z4 B. w( S翼肋, ' R* e1 M1 V: C& R2 f" n机翼、安定面或操纵面内具有翼剖面形状的结构元件。 * x8 [ L- ~8 N$ z9 n" Z) I( ~. `* K8 `: D5 _4 e, {' l0 z- n- k, g- U4 V+ E' B立管, + D2 k0 d7 j6 t$ |# {英汉对照民用航空词典B OEING. V t# f2 y( h TECHNICAL DICTIONARY 127; t3 e' J& J3 M& p2 a/ t ROD END (NO. 1), In a hydraulic actuator, referen! g, U$ C0 {; I. m$ ] the part opposite to the piston side of the actuator.6 m2 O) c7 K {8 Z! ?" z! B; N ce to - q' s2 n1 u! S# L; @. j) d7 ~D (NO. 2), A mechanical device usually a' m( h! p8 o/ Y+ d# c/ O! c4 ] bearing, clevis or similar component attached to the end & m3 x2 i; i* W& ?$ {7 y/ pof a link or push-pull type rod. 2 l6 J( ?# J& y" g" iOLL, The rotation of an airplane around its longitudinal 3 c- F7 E+ F- G$ R1 d6 e# f9 \axis. 4 h2 {$ F/ [5 O, JOLL AXIS, SEE - LONGITUDINAL AXIS 6 q. E' N5 p9 R1 p0 k- O连杆端,5 T, i$ o3 b V; N. b. z8 h 杠杆端,+ f/ @1 n) v4 o% I/ F4 s r 一个连在活节连杆一端或推拉杆一端的通常是轴承,# K, L, C2 p* t: Z, \ 吊环,或类似元件的机械装置。0 @2 J: R" c' |9 C# m 滚,7 \( {% l( |7 r. e: Y: s$ F" M; ^. E 飞机用纵轴作为旋转轴时的运动。% }0 ~8 Y2 @$ }' H- h, U- { 横滚轴, ) Y# Q O& X0 G1 z! F见Longitudinal Axis x+ E7 B0 Q! n ROD EN6 r/ u6 @7 G- B/ z) C R / c# L* Y0 ~6 ]0 p! F5 J6 |' TR 8 w$ ?1 G/ T' ~8 E/ F5 K液压作动筒活塞连杆伸出的一端。 ; k( j5 g1 \7 [& i: C0 \& p6 l& N. R: u. W+ r b( i, [; r8 j F( n$ ?9 l3 k+ P, `7 G 英汉对照民用航空词典B OEING . m: G# H7 \, i' M/ Z H1 p4 PTECHNICAL DICTIONARY 1286 j/ Q0 T3 }/ K2 Q ROLL RATE, The rate at which the airplane moves# Q( E: Y6 a+ H) o1 J( r on the roll axis (wing up, wing down).; `0 Z- c8 U# \6 ~5 Q% v, { OLLOUT, The final phase of landing where the " [5 b5 M$ b9 |! U' |, b) U$ _OTARY VARIABLE DIFFERENTIAL TRANSDUCER,+ P+ d$ K. x! ?- _3 P5 m ROTATE, A maneuver conducted during the takeoff ) q+ t& i+ ^% m1 A% Kn7 H; h& {- b4 b" l f raise the nose of the airplane into- L) _3 R# X7 J( e6 ~- ?- _! @- z5 a0 _ e air. - Z: @/ L y( @0 R- J/ V, QOTOR, A rotating section of an engine (turbine, $ e' T! _- F: ^ompressor) or a generator.7 F3 W# f7 D- [+ U+ M ROUTE DISCONTINUITY, An FMC operational 3 w) D. s, v/ g: q8 }condition, in which parts of a route are not joined or* \4 y3 \' f0 ~, q5 D6 } connected.8 \( m- ] z" m! G) m @ ROUTE LEGS, The portion of a route which connects & R O* S, X6 r8 W; u% I# ytwo way-points together. . j2 j; G2 {6 Q0 e: S陆滑跑, $ m/ |* L. d6 a7 k e的最后阶段。此时飞机在跑道上减速。. b/ u' H/ ], ]/ q9 u8 ?3 ^9 s- e M' d" x; \9 E R! T- b; [7 v. B" s7 m9 h& w airplane is slowing down on the runway.8 J( g! T# L6 \4 | D ROM, SEE - READ ONLY MEMORY . X/ q# r& J& [% P9 wR 8 ~$ c: h" \5 E, q: dA device with a rotary input and a linear response.6 T4 H$ m* N4 F, }! w0 ~5 w3 c ground roll. At the rotation speed, the pilot pulls back o 5 ^# i2 b0 F8 ^% y' |* Y6 x# `the control column to " \8 ?' m1 x( m5 p8 Yth! m+ U: L: i( r, u R % J# R( ` C' T- v; a2 O5 Xc 3 U2 Q- Y+ [/ B横滚率, - D; l$ C3 E) `' l& x; S飞机绕横滚轴运动(机翼向上或向下)的速率。9 u7 R% z5 E3 j, R# Q9 @( c" M, F1 {. H- }; m 飞机着陆1 `1 s( Y* i& Y" ` u B 只读存储器 3 j; g7 @& I/ d! Y2 C见Read Only Memory * o1 Q# u) W; O; O1 `旋转可变差动传感器, 9 {7 {1 |( Z; u, X8 B) Z% T人和线性感应的装置。$ k: B; Y3 j( |% I% ~) f6 Y. [3 g 抬前轮,7 p; }' T# C: |& s) w9 w1 ?' U, g 飞机在起飞滑跑期间所做的机动动作。在飞机达到抬前 2 ~: ~' e3 j+ K/ Q% t发动机(涡轮、压气机)或发电机的转动部份。 ! z" g {( t# o7 ]3 E' Z航路不连续, 1 M% b' M: L5 s! m- Y4 N2 F一种飞行管理计算机的操作状况,航路有些部份不相连 % |; g6 `1 u9 b" m; Y( I/ [3 n或不相通。 : h$ H" f# A F# Y7 t: E9 D航路段, % \: j: A$ J! w3 K- I p6 T1 L$ _- Z将两个航路点连接起来的航路的一段。: N- s1 ~" c$ {3 P 一个具有旋转输 ( H4 r# h6 q% B& b2 h% T7 f( w) a轮速度时,飞行员向后带操纵杆,机头上仰,前轮离地。 }# u) t# m( @( Q- R3 {转子, 1 g$ X+ H+ C9 G英汉对照民用航空词典B OEING % Z7 @% @" k3 i% J- h* @0 cTECHNICAL DICTIONARY 129 - q- ^% u9 ~; ORUDDER, A hinged moveable part on the trailing edge / X" T8 h' o/ z% Y- j# Qplane yaw (left and right) 6 R1 U* {9 z4 N$ wontrol.# X- D9 _$ M S3 F RUNWAY VISUAL RANGE (RVR), The horizontal2 n' b' W8 J( h5 d c a pilot can see down the runway when flying an$ T! o7 c/ J, D# ?% E: y pproach." }! J$ \* d1 X( H of iron and iron containing metals. 8 D+ A1 k# j `5 {* cis usually a reddish brown color.7 [6 c4 _' `9 F8 b% I8 ~8 Y IAL ' J5 Q8 s' R" @( P% X+ W# b8 pTRANSDUCER) K; b& ^8 u+ D& ]% m7 z S , b* s$ ]. b5 ]( p; Q( k# ?SAFETY RELIEF VALVE, A valve in the pressurization 4 g# |$ Y" |4 C4 i, m8 dsystem for reducing cabin pressure to a safe operating & y9 W" L% g9 Mpressure.: Q+ E e3 ^$ t% X* V4 i SAT, SEE - STATIC AIR TEMPERATURE 4 `$ Y d# U2 F) P% R或向右)的可动部件。 . m' g2 M# k0 k N: ?# G3 K进场时,飞行员向跑道方向望去所能看到的水平距 7 r3 H- U. u8 |! n6 @6 {- ]8 o( b6 _, A9 b E6 a 铁和铁类物质的氧化物。常为褐红色。# w G2 j6 D6 z1 r 见Rotary Variable Differential Transducer C+ x# i5 J: Q7 f) X5 q* Q) Q of the vertical stabilizer for air) M; \5 s0 }/ @1 r c , n% T& F) ?+ f$ jdistance4 y O! |$ T2 }3 x! u a ! g9 U* T- R# M9 Y- p" f% g1 R, |3 LRUST, The oxidation- ]- y8 m, i0 ~5 M It; }/ l- m9 P- p RVDT, SEE - ROTARY VARIABLE DIFFERENT + E! S; F$ W+ ]) O+ A$ C. Q方向舵;$ h: y# L: R' M& J( L 铰连在垂直安定面后缘上,用以操纵飞机偏航(机头向 ( ~- {( n6 F& W- H- K! g6 P! N- V跑道视程(RVR),# B& N, }. ]$ _5 J/ q" i& F 飞机+ r; O, g/ Q: d9 Y, x# `$ t+ f; U1 I- P8 ]4 ^ q" `铁锈, % |, J: I; {% j' w6 {7 K" |5 A1 y. w旋转可变差动传感器, : @) @2 c3 F c4 v* D1 \0 P/ _- K.- J C2 l7 l& d2 c1 a: z 安全释压活门,7 X) g6 w: Q0 A5 O$ ?8 D$ g: [5 M( T 在增压系统中,使座舱压力减低至一个安全的工作压力 M: _2 Z, B" k) T5 ^ 的活门。4 a( R" C3 K) c; s 静温,! w- i* z) n; B 见Static Air Temperature.( v$ m0 d" g4 U 英汉对照民用航空词典B OEING+ W; @! j' G7 c% x TECHNICAL DICTIONARY 130 % J3 Q. \( H% h% P% gSCAVENGE, To remove oil from the engine bearings or 6 A. _ S. Q& ?/ cto remove water/fuel by a pump from a tank. / e: R9 [! Y. V$ p$ T% zCHEDULE GENERATOR, An electronic component in 4 ?: y# ^- |: U. K" z& h1 se pressurization system for controlling the operation of 9 w' E! [+ [1 T% _e outflow valve.. Z% \/ C/ c. P, ?# F" Y% {1 @* l+ B CHRAEDER VALVE, A valve for inflation of tires, A& T% w) ~: M" o6 a1 Q! U truts and accumulators and for pressurizing the water! u1 ~, E- ]. @" v3 A ~ CR, SEE - SILICON CONTROLLED RECTIFIER 8 m3 ` f4 X6 p6 V% T( x6 tCRATCH PAD, An area on the FMCS control display! X0 A. i! }* M4 @& v, _& A" q+ P unit used for showing characters activated by the , d" i% b+ t, Y! g: L, F, }lphanumeric keys. 3 Z4 _. d; F0 f. z5 NSCSI, SEE - SMALL COMPUTER SYSTEM. X% p( N* y$ b1 e: g INTERFACE7 u8 J8 W* T) H7 r0 L) [- D0 U SCUPPER, A shallow receptacle around a filler neck of; h) T5 ~) z; J$ F% A5 t) B a liquid tank to catch any overflow or spillage from the $ }8 {# j+ U$ D9 a3 N% tservicing operation. The scupper is normally fitted with a: b) H$ p- C6 ]: c) l/ ^ drain overboard. / G/ a! C" {; I9 SSEA LEVEL, The standard datum plane from which , {5 i+ n5 C+ Z3 C }altitude is measured. / W7 K% Z8 i b( |去油箱内的水和燃 6 j" }1 G9 w. d( p4 x+ {' K$ E* R8 X g/ t: K" C程序产生器, ! X, s5 r+ Q: M' N3 X在增压系统中,用来控制外流活门工作的电子部件。 7 A4 K D6 i! M- l* f8 Zchraeder活门, * W* z9 m1 I( E/ Q! ]Schraeder公司出品的一种活门,用以为轮胎、减震支 ' g( e' y% ^. ^$ j* _2 L充气,也用于从外面为水箱增压。 8 _$ G: x9 r/ U4 y9 r可控整流器,7 Y3 E+ y: ^0 \1 ] 见Silicon Controlled Rectifier# X# N0 a' c9 Y. x9 z" b S" s) P% a) [5 f& _0 j/ J th" k% G6 _8 L) r) A2 } th" M% ^3 t4 X, z# @; u S% r9 C5 ~5 [8 r5 h4 [ s s# U [3 w7 y( K) J' n7 E8 ? tank from outside.4 V8 b% K0 S* I3 f+ M S* }8 j, ~% S# S2 k S # v, C; F* w" N% a- ra , u8 l" R: M" }& ]. N回油,. D8 @& g, ?. d8 Y9 M 除去发动机轴承的滑油,或用泵来除* Q( x6 R6 `; z8 |. m4 h7 L+ n4 N& K S , Y) V1 U% V3 W' J, a柱和蓄压器 k$ n8 u! [% u+ m# a) }) J8 G, W# T1 }( H* s) r+ x 稿栏,- k' t9 O3 G2 ~( X/ o3 l FMCS显示器上的一个区域,用于显示由宇母—数字键 " z) m* l& h8 v c激发的字符。 U$ ~. z5 Z- O0 F5 f小型计算机系统接口, 9 N, t1 g. h; c; i5 x7 A见Small Computer System Interface- _: {, O2 [ Y+ g% Q! c: V* e1 A, E- k) |3 y$ F2 ]: I8 U% o2 Q) C e1 L1 y8 f8 B6 b0 K d. M( ~ 放泄孔, 9 Q+ q0 i" k8 [, N/ t! P液体箱的加注咀边所装置的小型容器,用于接取勤务过6 U+ M- o; L1 z* {. [: F) P; _4 B 程中任何溢流的液体。一般都装有通向机舱外的排泄管6 X. V1 ?: n5 Q b/ t z8 _ 道。6 \- E- ?: ]' Z' X 海平面,8 s; M4 }/ @& r. R& }" a 用作高度测量基准的标准平面。6 u0 o3 U. x8 u2 [8 e* S) ? 英汉对照民用航空词典B OEING ) y R7 Q7 ~7 o0 I2 V& VTECHNICAL DICTIONARY 131; R! C. [. ?6 o; @8 _ SEA LEVEL STATIC THRUST, Maximum rated power 2 Q" w+ l1 r3 Qproduced by a stationary jet engine during ambient' |9 }7 q+ f1 a" y* [ onditions at sea level.3 ] B- O0 n' H s for * o! Q4 i$ d1 M2 h' Q/ X; Creventing air or fluid leakage. 7 H: n2 r2 h% A+ K$ ^$ RSECTOR, A given distance between two checkpoints in / h! V# @" f# S, g5 he flight plan.6 Y9 `2 ~" V* k' H; C y3 o. ^ ELCAL, SEE - SELECTIVE CALLING+ J" F5 P/ p9 Z/ b0 H/ P SELECTIVE CALLING, A system that automatically 1 _- O4 w: s, V; m7 b% x3 [SELECTOR VALVE, A valve in the hydraulic system for Y' W( a6 |9 O6 G: o; Po one side of the actuator2 _; n6 K* X' s: r( e5 g, h6 w nd the other side to the return line. 9 d7 b9 {+ k4 \力, 9 E( }9 A6 O2 b2 [在海平面环境状态(大气温度、压力)下,一台固定住! ^" E3 S' H, F7 _* y0 Q. ^$ x 的喷气发动机所产生的最大推力。 * z. M( l. T0 u% F: E在两表面间防止空气或液体泄漏的元件。 6 f) d6 J: r ~5 R9 k航段, . I }3 e! n# B+ C+ h% b# y飞行计划中,两个检查点之间的已知距离。" w5 _; v) P/ d& i1 n$ M, R 择呼叫,+ L) V! Q) g1 X6 T( [3 V 见Selective Calling \9 }( t1 ^) f- Qc! p. M4 G3 o! p SEAL, A component between two surface* \# `/ X+ l, k; }/ D p ) G5 p$ U% B9 |' U! n3 Qth: }8 `2 C: g4 B+ ]1 ~ W S R. Z5 w& A; K$ m. R, K8 ] alerts the flight crew to a call from the airline ground f4 [$ g9 S' v4 b2 y station.# D+ Z( }4 R# w- [' {7 F$ w connecting hydraulic supply t, P/ j+ A- u% {, e a: w' g( r* C0 l3 M( O4 M" ` 海平面静推3 ^9 A3 Z0 A# w- M 封严," i# L3 W- j7 c( r9 C, {/ g7 z G$ N; [: p .* `, C1 G/ S, Z8 x0 R$ o- z) r( w 选择活门,$ ]# R" t: v5 z8 Y+ c- c2 R* p 端连 7 b( c7 `) D1 C- ~回油端的活门。3 Y Z/ q; @# T1 a; G 选择呼叫," O$ M; H; o& b( y 一个能自动将航空公司地面站呼叫报知机组的系统。 & d$ o8 n2 u# z4 O9 w液压系统中,用于将液压源一端连接作动简,另一 2 k* r7 r) [9 O) h: Y _5 N+ [$ i1 l& A英汉对照民用航空词典B% ~ ~& s$ @0 @9 e" l2 q, |# A* u8 R SELF SEALING COUPLING, A connection between two 8 K8 I0 t+ f ^- V# mfluid filled hoses for preventing fluid loss when the hoses! Z9 ]& }0 H- p z& e3 g/ l$ r rated. 4 W @$ p+ C/ M1 S ESEMI-MONOCOQUE, Type of construction in which the% ?) k0 ?5 A) o$ [- U1 s SENSOR, An electrical device for detecting variable 2 [9 n; `. m \* |" ?% i2 fENSOR ACTUATOR, A device for operating the ' E8 \2 W0 k2 c! ~$ R1 rSERVO, An automatic control system which checks its& N6 @: H1 N# d. d5 M' @8 F3 a gainst its input so as to achieve a desired 5 S. m, m0 I. X5 L) iMED, Hydraulic pressure for the servo is9 i l) U5 T- W" ^3 q; B resent to allow the servo to internally synchronize to : A3 A" r9 k- Q, P# H: x1 ne proper position, but the mechanical output of the 9 k+ W$ K K$ G8 iervo is not connected.5 J0 j% @+ \& M# }4 V6 h) q( P1 D 自封接头,5 w) {8 z2 ]$ }/ I8 T2 v* T 活门堵住通道,自动封闭而不 ! W- O {" N. R! u让液体流出。) l+ B9 G I' B, S% ^ 半硬壳式结构,8 V9 n; R% g$ b 使蒙皮,长桁和隔框共同承受所有载荷的构造形式。. g& l% D, \ |9 ?% p 感器; 0 W+ n* P4 y9 t g量状况并将结果以信号送至指示器和指示灯的8 c7 L% P1 u" P6 P; ^3 g 电气装置。 % Q& r1 T s. j7 W" w, T传感器致动器, : V! F" C( |7 O8 ~* P9 M8 E+ b( p; C- Y# ~1 t伺服系统,( ]2 e; @& H6 K4 R! r8 ~3 c 能检查输出和输人数据,以便合适调控的自动控制系 0 P8 l" I+ e- `' l1 v统。' ~0 d, d9 X* k# [& x4 z/ N 伺服预位,- \/ v; I# I$ M! N, t 液压使伺服系统内部同步至适当的位置,但伺服系统的 # P ]6 I: S1 D5 M: b机械输出还没有接通。; Z4 i2 v/ L) U6 A j9 Y3 X$ K are sepa1 O( E5 s, P- O6 y skin, stringers and frames carry all the loads.) b) W: F$ u! W, \2 [: i conditions and sending a signal to indicators and lights. + W' b! q4 A5 SS3 J5 F0 t& p" T4 W sensor. ) \9 h) U/ s' uoutput a # [2 }+ z; ^/ ycontrol.* E R3 [$ h- B OEING# k3 c, ?, W8 T/ j9 C- N! { TECHNICAL DICTIONARY 132 , a) {0 x) s0 Y- MSERVO AR \# Z# m8 b/ @0 u: ~/ t5 E p7 ~* `/ y5 n S' b6 ^; L1 g2 q6 ` th ) Q" ^0 [/ [: D/ j+ js! T4 F8 H* H" U* K9 z% W 用以连接两个充满液体的软管的特制接头。在两个管子 " }3 [+ J a! w1 ~8 B4 a* g分开时,接头内的弹簧即使 - E- ?- a" R3 U0 x j) Q8 _, x& q3 d, P# {5 {检测变8 {* f8 C9 i/ L I+ _0 f 用以操作传感器的装置 5 J7 |3 c% q' _' V英汉对照民用航空词典B OEING 3 q" i! \9 K* UTECHNICAL DICTIONARY 133- [9 O% M. M( @" I2 b( y SERVO ENGAGED, The mechanical output of the ( {+ X$ @4 h1 D2 W+ T# Aservo is connected and the servo can move a surface or + u# d7 `$ c, _ U3 zontrol , E4 q1 v; g* E/ \SET SCREW, A small screw (usually headless) used to , y, B. r# X- E* p" _eel, or knob onto a shaft and prevent ; z! {* x9 w5 I1 @+ }tation. 1 r+ W' P1 j3 r/ c3 ]8 k! ` l pSHEAR, The stress exerted on a material or, assembly ) [: r" _ Q8 _7 h$ p5 y! _2 qwhich tends to slide the mating surfaces parallel to each 8 q6 k0 U; E+ W- B2 kther.: j5 J8 a; r) e6 ]. d% w SHIMMY, Rapid oscillations (left-right) of the landing ( [3 S2 V! q" [5 ~! mear wheels./ u. Y( T) C- q4 W1 c$ { 预位, 3 Y, }! M/ X0 w' X8 K2 ` b伺服系统的机械输出与伺服系统已接通,伺服系统可移 5 R8 C* X1 X1 g3 b动一个平面或操纵。/ }/ e' Y, o w1 p 小螺丝钉(一般是没有钉头的)用于将滑轮,车轮,或0 a0 O" J# B5 x0 T' ~! h% E 钮紧固在轴轮上被免转动。 7 B& h- K* F F: L+ p4 oc 8 L; \& m' E; \0 ^fasten a pulley, wh$ S2 B; I4 l9 S/ M/ X- w ro5 z* w/ |) O' R. C/ w SG, SEE - SYMBOL GENERATOR 8 l" C$ s2 C, A% J4 `5 T! I2 f* C% _o9 Q6 {% d" G0 d5 p: c) F g7 B/ {" j q' x& p' V* v 伺服系统/ l7 ~! K3 X8 Z- I$ y 定位螺丝钉, 8 |5 F+ D! P ]- W. U2 b( ]- W, V: ` | 符号发生器,& l( i( @8 v$ L% V' D 见Symbol Generator.4 K6 l8 ]7 q2 ?6 s# _2 p( f 剪切力, : m( {+ B+ Q+ R- g# X& t5 D3 y" s加在材料或组件上的应力。该力往往导致互相平行的成3 ]7 [3 U `; P" k( } 对表面滑动。' S/ m5 p% z0 y& B0 A: {( ^7 k" B 摆振,3 \; M/ L0 |" J9 _ 起落架轮子的快速的左右摆动。% D3 A# i/ H$ s/ d8 U1 }. A1 _" \ 英汉对照民用航空词典B OEING) H8 j6 u4 S% r+ A* C: n. I, v$ C TECHNICAL DICTIONARY 134) j# v9 b% t% v SHIMMY DAMPER, A hydraulic device for damping9 z1 S9 r" @. a8 Y; \ D shimmy in the landing gear wheels.' P% O9 j. `4 M; J( }( S1 N ar for. Y1 ^7 F n- U* k5 L" R: U% [8 g sferring oil from one% H+ ^5 g' t5 Q6 W chamber to another through a metering valve. 8 H" P0 t. O4 ?2 w& a1 Z% E8 w+ a7 O- q一室以减 8 d3 a/ D% p& q着陆时产生的冲击震动的部件。9 O$ S- r% H$ U) [/ ?) L( ~ SHOCK STRUT, A component in the landing ge/ Y# e* |1 k) o' w0 p3 | absorbing landing shock by tran 5 c/ ?6 u, }+ O& z, B减摆器, ! }0 x9 G% k3 i( U用以缓冲起落架轮子摆振的液压装置。8 P. t. h6 ^; c# W! n 减震支柱* a4 c7 K: e0 }) |/ ~1 Y" r- G# Z 起落架上通过计量活门将油液从一室转到另 0 Q' ~- }: j" ]1 q4 A+ ?; K- E1 E3 \( L7 H! j 英汉对照民用航空词典B OEING 1 h t* B1 Q2 a4 f) b9 I V3 y l. bTECHNICAL DICTIONARY 1353 u( f9 r& t) y0 p2 m* z$ l7 J: C( P SHORT CIRCUIT, A fault in an electrical circuit 3 M& w5 ]1 {: H coccurring when the power supply goes directly to ! R6 d# M. L/ |$ uground instead of to an electrical component. 3 O" N5 ~9 l' B( x" I! K: v" o" zSHORT RANGE ALTITUDE, A cruise altitude chosen to' }/ t8 u) d7 \ P/ u inimize fuel burn during short trips.- w( l( |/ R- O* A& v6 v$ |! \8 m HROUD, A metal covering for enclosing the APU on 5 f# A% X" |* Fe airplane. An external tube for enclosing a fuel hose. & p- R- e: V- R. f0 jHUTTLE VALVE, A valve in the hydraulic system with Z, q' K% i, w) o - STANDARD INSTRUMENT DEPARTURE! t0 M t. ~! `' V: Z f the ) h. M: p4 h, a% yr access to the components on the engine. 2 ]& ]8 K# B2 W5 d2 I& e# C短路, `/ A1 J+ e, ?( B- y0 o3 U+ a3 | 短程高度,) `/ K, o! A. U% S 为在短途飞行中使用最少燃油而选的巡航高度。 ' U9 T" o. I5 S9 \护罩, # S8 |( _; ^& d/ a. P飞机上包围着辅助动力装置的金属罩。包围着燃油软管 7 Q2 _1 Z, r2 i j a: D3 L" \用活门,. a) M5 X1 {7 ?# k 液压系统中,具有两个不同液压输人管和一个输出管 6 O; v$ Y9 N7 n4 S2 m4 w的活门。 - ^; h' m7 z3 l# e2 K7 }& T标准仪表离场,1 y+ c/ F3 u0 N+ t1 s9 b) p; n. M, a 见Standard Instrument Departure: N+ v J% q5 `6 f7 H2 z, s: ` m $ o! N) Y* ^3 f+ ~S % m f; {! d: G" B7 y6 qth ! _* {2 B- ?% \# m% b4 K) kS* r& Q; }; D& B& r; m two different hydraulic supplies and one output to a 6 y( {. v1 l1 F7 Z) E) n, Wcomponent. : E+ N$ q3 q4 n2 i: C0 ySID, SEE - k0 Z# x+ }% T8 P/ [SIDE COWL, A removable cover around the sides o 8 Z, z9 `: _& gengine fo6 M+ e3 O9 C$ \ 电路中电源未经电气部件就直接到地线时的电路故障。9 N) Y3 }; ?# R, h. U2 t6 m. }" S1 d1 K的外管。" M1 `6 x w! L" i# }' q# T0 c5 q7 w; B3 M) ^! P7 ?& @* @5 x. M- x$ S+ U. B$ X5 [5 M) m! ^ 机两侧,被移开后可以够到发动机部件的可卸罩 ! `+ m& @) [) ]3 F3 ~4 Y- ~" z; N4 \9 u. h侧整流罩, " h" i/ Q6 {, t; b/ m% [发动 8 d, B' K7 Q @5 W( |* X! N+ A$ Z- F0 S' y" w 英汉对照民用航空词典B OEING+ ?& S6 F$ _+ B" f9 v TECHNICAL DICTIONARY 136 % Y+ c2 {/ r8 m2 qSIGHT GLASS, A glass window for observing fluid . W, g. d4 Z" {3 n* g& yquantity in the reservoir of a machine. * P6 L& L/ ]/ i3 q( o, that can be used to transport information for5 V; S' ]5 r: Z& k( h% ^+ M6 } communication, control, or calculation. . z5 E& X6 |: E) [ILICON CONTROLLED RECTIFIER, An electronic ) x$ m- g, E) _- T5 vdevice allowing current flow in one direction after the ) m* m- @' Z) G! Y2 R! udevice has been pulsed at the gate. * Y z( S+ H5 o& n5 |/ |9 c$ jSINGLE SHOT MULTIVIBRATOR, An electrical circuit* a! `% x! H. | -stable multivibrator. ) k& y9 H, s' R如电流或电压能用于传送、通讯、控制或 . F* Q( B1 P2 p6 m2 L- W算需要的信息。 , H( `% A4 ~/ H6 M$ d硅控整流器, ' _- Z6 a/ O1 a3 U# M当其控制极受到脉冲后,允许电流向单一方向流动的电- c; Q7 w" x4 ] 子装置。/ o1 n9 G! n! s 息多谐振荡器, 1 j& ^' |2 ]3 d- e, e6 ^( F" P输人信号触发电路时产生的脉冲的电路。又称单2 q1 c5 e" o0 U SIGNAL, An electrical quantity, such as a current or9 E- J; P: S M- J2 [, z voltage 9 T% i& b% R+ T* O9 H* c1 s# a$ tS# N- \2 c7 _, b: B. D which produces a pulse when triggered by an input5 k( n5 s- b$ j+ W5 C0 B signal; a mono 3 L: e; b7 S7 k- w$ ~* u: f, G检查窗, # N& P# W9 A3 K3 U用以观察机器的储液箱内液量的玻璃窗。7 J# W( q" M2 t; G4 o1 t2 a 信号,, R7 `, ?: O' Q 电量的一种。 3 `; ?0 c2 _" b8 O" G7 R7 z8 L# Y! k# Z& H! w" ]. R0 K9 m! U0 X 当一个 % I, o8 W' s0 X3 c$ R G3 P" c; n" `稳态多谐振荡器。 7 K- W) O1 ^$ k9 ^" S- [, Q) h英汉对照民用航空词典B OEING6 t: \. R& E! {6 w TECHNICAL DICTIONARY 137, U% D C7 A) z+ e( j SIMPLIFIED FLIGHT PLANNING, Rapid determination ' N8 s) f }0 g4 u9 m! v2 b) Sof trip time and fuel using a chart providing these data ; o! i5 q4 Z& \# V9 ]6 b0 Sfor the entire flight profile from brake release to landing./ q% U. v9 U% h5 e SLANT RANGE, The line-of-sight distance between two 1 K+ F: M! V* tpoints not at the same elevation. 9 f* U- @6 V/ c/ A6 X& l# Z" rSLAT, A moveable part on the leading edge of the wing# q& V0 Y& H( H& z4 w B0 ] for increasing lift at low airplane speeds. 3 z2 x+ O7 b6 d8 o+ m划,. m1 r3 ]( a" ~" f! c+ F$ e 迅速定出从松3 h1 `* X8 L" `9 Y: c2 N B1 i 车到着陆的整个飞行所需的时间和燃油的过程。- W! a5 `" P" Y 斜距, & y6 N& D3 i! `! I0 i% a# Y不在同一高度的两点之间的直线距离。 ' L j4 `1 }; |7 ~ X$ F! S ?缝翼, ! r8 h6 K. q% }. t用以在低速飞行时增加飞机升力的机翼前缘可动部件。! u! \ J' f) n1 W7 O K. ~' V 简化飞行计$ O+ X3 v# j7 k6 \ 由提供旅途时间和燃油等资料的图表,来3 f0 B' K G9 k# g' v" g, H' ?: U' {8 b+ m5 i! L英汉对照民用航空词典B OEING 3 o# a. W! C. r8 rTECHNICAL DICTIONARY 1388 `( ^( w6 G. ~9 e3 w SLOPE, The amount of incline a runway surface has 5 N4 N `' }2 @relative to absolute level.) G4 M) B V+ q, m; l SLUSH, Runway contamination made up of a mixture of8 C0 g% o% i7 V1 P, A ater, snow and ice. ! C% {7 ]; ^- Z0 TSMALL COMPUTER SYSTEM INTERFACE, An input 8 J- z/ O% @3 B3 J# ^( g1 d( `and output bus that provides a standard interface( I/ d# e- z) R8 n& T3 b between a computer and peripheral devices. 5 F7 @! b- ^, g% o5 `* xSMOKE DETECTOR, A device whereby the flight crew8 B# b' s2 L9 F' S an be made aware of smoke or fire in specific areas of$ c- k5 }6 f+ G, L7 P% Z0 _$ y the aircraft. 7 y$ M/ m5 Y5 N$ }5 kSNUBBER, A part of a hydraulic actuator that slows& m/ s8 c5 p9 O8 c. K7 g' B- { piston speed by restricting flow. 0 }0 w6 ^, @3 z8 q3 GOFTWARE, The stored instructions that control the9 B( P E7 ]6 ]3 }( K perations of a computer.0 K9 \4 E2 E j# R2 a3 z" G0 l ng7 H0 X$ ^" ^8 c4 `/ G/ Y9 p% N' C other devices. 4 G! Q3 E( N6 p W- n$ l; p8 wSOLENOID CONTROLLED VALVE, A valve controlled # Z) [! G) S: r5 f' Xto open or close by the solenoid. % j7 K# A1 _ c0 T' P雪泥," W! l: ]% c0 f 积在跑道上含有冰、雪、和水的混合污染物。 * g5 \2 F5 u- U小型计算机系统接口,7 k' g4 L3 [, o. V1 q/ c* I 一个能在计算机与周围装置设施之间供给统一接口的. y$ E }! D3 H7 J) l4 y4 l- x 人和输出总线。. Z/ s; i" V/ O 烟雾探测器, 6 v" U/ O- s+ B1 j4 a. s3 v在机舱或任何指定区域内能测到烟雾或火并报知机组6 A! G( H; z C# M- }4 s/ f/ A 员的装置。 # X0 s4 y6 @/ e9 D冲器,% M: i; C! r; ]6 m# O* x" s 液压作动筒中具有节流孔的部份。这些小孔能通过限制 0 Z, q: {/ Y+ n4 k0 R' c液油,以减低活塞速度。5 c/ _+ g8 J' H! X; {4 F 储存在计算机的指令程序。用来控制计算机系统的工 3 ?8 Y2 |3 n o作。 3 M# _/ C4 M4 b操纵其他设施的机电装置。 5 b/ q# d8 J4 P. E( d( h5 J电磁活门,2 ?& B/ E! B' m( M o 用电磁线圈来控制开关的活门 % D, k4 a& v' ?4 }( \* @w 6 c4 o0 _/ M; N% ?- k5 a( oc" \" j; z" }' Q8 f Q S3 _: X" K R2 j. D: [$ ^5 Z o2 a7 x1 c' {1 g$ x3 p6 m SOLENOID, An electro-mechanical device for operati 8 o$ }/ S2 l7 e& k* {$ B3 f% S斜度, r7 `% L- @0 ]9 e1 \' K跑道表面相对于平面的倾斜量。 2 M" @, |3 a: G8 G3 |. b, R5 B1 K1 G3 _' @$ o' D0 h4 ]* k# g( ~ F# Q+ T0 E6 W- t* l$ ^3 R$ c. C( R 软件,) U9 O& |! _* ~4 y: J" R+ x 电磁线圈, 9 v, k* K5 C7 [: f2 m8 N用以 7 f( t9 z% y j! y, S& O英汉对照民用航空词典B OEING q$ j9 \; Y+ |6 @. D" N) O" A TECHNICAL DICTIONARY 139+ h% G. T6 F- O" r/ m SOLID STATE SWITCH, An electronic circuit that + `- r6 l( B$ p, D5 ^1 T0 iprovides switching in a current path.# l, F7 W& M# z3 g0 U SOUND SUPPRESSION LINER, A component in the' C" R& d! I9 X/ G" j nose cowl and around the engine for absorbing engine5 }+ D* C* }' |; `0 U/ B5 w' u noise. 9 s9 y1 @( u( j) PSPAR, A principal spanwise beam in the structure of a* p- x) c! p6 O% a5 D SPEED INTERVENTION, Pilot control of the speed! w& }6 i l- }$ D$ h SPEED SCHEDULE, The planned speeds for a specific" H' l5 l7 Q8 v _2 ] phase of flight.$ M/ B1 h& g" Q# [ 晶体电门), : {6 f; {) m( y, T, o: O8 V消音衬,4 e& U, X, X9 }7 b" F 在发动机的周围及前整流罩内,用来吸收发动机噪音的 - P9 Y% y( `; v* g( m部件。 c: J3 ]& e6 `9 e' E7 w 梁, ) N: r( S* h d机翼、安定面或操纵面结构中的沿翼展方向的主梁。. M" z Z- W& v: W r$ o 速度干预, % X& h9 ^9 h; Y- V计划速度, 2 G& U5 h6 g- ^" A% M1 Q/ q( W为一特定飞行阶段所定的各个速度。 0 ]& U# r! H! z+ ^: ~( K! `wing, stabilizer or control surface.$ J+ p) E6 }. B. G% x during VNAV operation. / F9 |% X- ]% g; `固态电门( v5 P V( |9 [) e) t在电流流经途中提供开关的电路。& N. I8 w: E/ x/ g7 f! x" D r 在VNAV(垂直导航)操作期间,飞行员控制速度。 3 V+ R+ _# l; a: l英汉对照民用航空词典B OEING n+ E" L5 U0 n5 mTECHNICAL DICTIONARY 140& ?9 ?3 s# L2 c5 A& [ SPIN BRAKE, A device in the nosewheel well for . {: _/ d& M& T# q+ K% h+ _* Mstopping the wheel rotation after retraction. ' I J* z/ {' @0 Q! ^# P! fSPINNER, An aerodynamic fairing attached to the fan of, |- @7 D) Z$ B! A/ V: a |2 u a turbofan engine. + w2 ^8 P0 I# q" t. bSPLICE (NO. 1), A connection of two airplane skin v" J. K# O9 `$ E- |% P% O8 w sections. % R. c2 i# S4 g; P6 O6 F P& aSPLICE (NO. 2), An electrical connection between two0 ~' \# t+ y0 u wires.* F# ]' S# c. S+ z+ W- E 前轮舱内用在起落架收起后不让前轮再转动的装置。 * W! ]: T7 B! ]; f1 B旋转罩, + X6 Q# f& w& o, K固定在涡轮风扇发动机的风扇上的气动整流罩。 * S7 m- u3 Y& C) w% x" m6 J拼接, . r0 _* F& v( B) K! T; b飞机蒙皮与蒙皮之间的连接。; s# p- J/ B- q+ Y 铰接, ! ^$ d3 \/ @( r% D; E3 S两根电线之间的电接头。9 R9 ~5 j' a; Q/ l& G# R 停转制动器,1 X. ]3 y& w' M' U/ p8 g7 `- Q3 W 英汉对照民用航空词典B OEING# w; `( h# f/ q& ^3 ^3 H. b6 l TECHNICAL DICTIONARY 141 # X2 [6 ]8 k9 x9 g7 A. LSPOILER, A hinged moveable panel on top of the wing. 0 \) J( B, X) }1 _$ D; } l6 `Flight spoiler- assists ailerons for airplane roll$ a0 t6 A: h/ V (wing up and wing down) control ; s! }4 A% q8 F- r& j* A/ F1 Q) Cand for aerodynamic braking in # C. h6 s; b" o: r" ]5 hGround spoiler-for aerodynamic braking on the & N; n4 |' B1 Z7 i' [" c& _ground only.- n! Z5 e- L: W7 v* V PRING LOADED, A condition in which one part of a 8 y m- ^- P1 Y8 W$ ~- Uevice is held in a particular relationship with another5 z) {. S& j/ G8 b/ u' A t,, W3 M; l8 u+ |, a/ m0 d r original position. 8 L# C% Z2 V- l' |% {SQUAT, Airplane on ground condition. 0 Y( \6 H6 D; v, R$ L: N5 [QUAT SENSOR, SEE - AIR/GROUND SENSOR 3 z8 ?9 O( p5 K& Z: [0 b V1 [SQUAT SWITCH, SEE - AIR/GROUND SENSOR4 _4 z& X6 ]" Y 扰流板, 6 D+ _( w# N+ B' a% I8 H& ^铰连在机翼表面上的可动翼板。3 z% W5 ^) Z; k4 k3 G) T. c; M 飞行扰流板一功用有二。一、协助副翼来操纵飞机 - k; |# G2 s( N的滚转。二、用以在飞行中或地面滑3 B# y, J! I# k" s( B 跑时作为减速器。 7 l3 P$ Q: Z. n+ _ M地面扰流板一仅在地面时作为减速器。, a! I. h( Z; p& v/ ` 簧加载的,- }' o4 K% ^9 a& Q) ? 由弹簧使一个装置的两个部份保持特殊关系的一种状 ) l' e% G* Z+ d! V' f8 v态。该状态允许一定运动,但继而回复原位。 ( A+ o1 n' T* j2 Y1 r, a8 d3 C着陆传感器,# t# h' L/ A {4 v2 n und Sensor $ T7 S) T% Y' i5 Z9 T/ aflight or on the ground.2 d5 l+ C5 s: g" I; {- y4 X: S S7 f4 r5 J( K D2 ^0 ^, B* P9 y1 d d & I+ A0 ~, e. [" T% E' l- Spart by means of a spring. This allows some movemen; h! Y7 }: y' u5 v; Y: z but returns the parts to thei - a8 a- D( }+ a- s6 e% [S7 k; |6 C" s) d- V% ^& t5 Z! S. g2 [" Q/ s& ], F. E着陆, 3 q0 Y4 \% V3 B C9 C. P9 o' _飞机在地面的状态。 , E: w& |3 X6 `% ~& l! k! V见Air/Gro" i1 p# G1 v5 W+ Z" q3 Q8 M! S7 [ 着陆电门, , \6 f+ B6 B4 ?& x0 W$ ]& j* s& \见Air/Ground Sensor . 7 S: Y. q. ^$ H0 @' n" z8 S& D英汉对照民用航空词典B OEING& h# Y# A$ I5 Z) P6 Y9 ]4 Q TECHNICAL DICTIONARY 1423 v7 p8 m% v" V SQUAWK (MODE,CODE, FUNCTION), Activate" l- Y7 m7 m% X9 W$ m! C9 O% q/ v( Z specific modes/codes/functions on the aircraft 7 ~ Y& N- I2 ]6 w6 ~ansponder, e.g.,” Squawk Three/Alpha, Two one zero ( a# Y) @# w8 l3 d# N- mfive, Low".* S7 [' g1 Y4 Y% z: p SQUIB, An electrically operated pyrotechnic device for4 w- W7 I2 @1 [# l! Y, ? breaking a disc in the fire extinguisher bottle to release6 `3 t+ a$ v( J( O the extinguishing fluid. Also used for escape slide & H8 H6 p# l& |3 ?0 L1 ` JTABILIZER, SEE - HORIZONTAL AND VERTICAL& p3 a! l/ s6 D$ W STABILIZER / r- |4 u( s% g9 }0 Q& `TABILIZER TRIM, Movement of the horizontal tail to* X+ P% ]% O, P1 T hange the attitude of the airplane about the pitch axis.3 c3 Z1 q; t2 `$ Q# B3 L' g6 t TAGE, A numbering system for the compressor and ' V( Y. F# J3 g" e v6 ?2 p1 [* qturbine of a jet engine. ! p. o( E, q: [TALL, A flight condition during which lift is destroyed 8 G; e3 T, B$ i. Q0 u9 q& q& que to slow airplane speed or attitude.& w. d# V+ X) @9 u/ B to enter from the top and flow $ V/ J" I+ P4 `7 ~out to the system. It prevents picking up debris off the - G J y1 |- _! l% Sbottom of the reservoir. It can also control fluid height in* @. ^7 z% S! H5 v the reservoir. d# W% o. o5 O" } 能),/ `2 L+ V4 N5 e 使用飞机应答机时的一种常用的指定方式/代码/功 & z, ]$ @/ j0 ` w; n/ |9 H能。" U* j: R% T* ]! x2 h9 O/ s 管, + U0 \! e& Z$ [- V0 u用以爆破灭火瓶上的圆片,以释放灭火剂的电控烟火装 3 f3 `3 p( R( C# U4 b置。也用于应急滑梯放出。 ' c3 U7 j/ J0 v' v$ V$ s0 k/ I& ~6 [" P. x定面,2 m) I! Y% E5 O9 ^6 s) J$ [6 \ 见Horizontal and Vertical Stabilizer) M+ x6 i9 K+ B6 S2 l. a Z# c% W tr $ o- A% S9 a8 C* N6 Sdeployment.0 R/ a# R ?- f S ' t( |) P8 ]) c, i5 ~% iS * n: a& K2 A% G( W$ U8 Mc& P& X8 m b; R X3 C S 8 e: {' K9 U$ }) ES4 x S# L# A- m! ~ d ) y" c7 q9 Y( ]STAND PIPE, A pipe raised up from the bottom of a2 J: w0 w+ a J+ N reservoir that allows fluid 3 u3 g4 X: t$ u% ` \发送信号(方式,代码,功" S1 S3 D. {' U; p$ R; o8 d6 d$ u+ U1 U1 Q& ]2 S, G) o0 N6 f. `" k: S% S; K% Z) J$ L$ I3 O/ Z% O3 m7 b 定面配平,' @, X- `$ w' F2 G6 W9 | 为改变飞机绕俯仰轴的姿态而做的水平安定面的调整。 5 s) C" f) _) a- B) P% Z& }" K级,- N/ o) }* S# r; K2 u+ i4 F. H! {5 ~ 用于识别喷气发动机的压气机和涡轮的各个段位的一* a6 D3 ]4 Q! h% G# o; }8 f! E 种编号系统。$ G( t3 D9 Y/ { d 失速,8 a" x7 c7 {/ f( X$ z+ }: l 飞行速度过低或姿态而引起升力失去的飞行状态。; [; Y$ `- X. @& E8 n c3 | 回到系统中,并防止带起容器底部的碎屑。也可控制容- W) v9 t& l: P0 T1 A0 _' C 器内液面的高度。 * [" [+ g5 ^5 q: k* w) k" H$ m& [) Y1 m+ n 立式管, # t, n8 H/ U+ [ l6 g. J# l从容器底部立起的管道。能使液体从上流流人,然后外: W6 ^( q7 s4 G% I2 C3 W# S: n# n0 b I I' u; _9 V 英汉对照民用航空词典B OEING: D+ d# V" |0 E: {2 a: r) C TECHNICAL DICTIONARY 143* {7 t9 p2 [( m# j' ?$ w STANDARD INSTRUMENT DEPARTURE (SID), A9 W( l0 n w* M2 Z6 W. t IFR. % V# z; I+ ^' ?, jTANDARD TERMINAL ARRIVAL ROUTE (STAR), A5 q4 s( N, F' ]3 e6 ~! I) x ublished procedure for approaching an airport IFR. ( B ^( F; @3 G7 ]TAR, SEE - STANDARD TERMINAL ARRIVAL! i+ _5 W1 {7 `* P+ H OUTE 6 c! `0 y. R, D8 y0 \$ g4 K* @TART VALVE, A valve in the engine start system for 4 M. K8 r- \7 b( I' O- @upplying air from the pneumatic manifold to the engine4 U1 S: e6 Q0 a0 r e! \. f; k tarter.% j) A0 E# v3 \0 B TATIC AIR TEMPERATURE (SAT or OAT), Ambient 7 e( B1 F& R3 F$ z* e5 Eor outside air temperature. ) Q8 K& B& K% o$ r& h" F# Q) MSTATIC PORT, A small hole in the fuselage for sensing. @' i- @. E s+ r3 F" S% Q static pressure for airplane instruments. ; j: M$ \, L* k0 mSTATIC PRESSURE, Pressure in the air or fluid at rest: L, J% u( o, j5 A, d& T/ P7 o! U measured in pounds per square inch.5 }5 S" C6 q* v8 Z# v8 s$ X, X3 A! K ID),, C# q- K! S, k" v! w: D 用于使用仪表飞行规则离场公布的程序。4 d& G. M8 p7 s- a 标准到场航线(STAR),; D: I% z8 a" R" K3 U 用于使用仪表飞行规则到场的公布程序。7 q$ |+ d1 O9 U1 c p0 \ 标准到场航线, . U) t( N* a0 q见Standard Terminal Arrival Route ) \1 o6 G( Z+ p: F4 L# E& ?published procedure for departing an airport' A; i* {/ e- F S 9 K0 Q5 x* T" Q# @6 m& sp ) J' K0 z( [0 ~S& [, w5 ^/ E, r* U R $ g1 x* x) d% K& GS - b6 r. f6 ^9 k% s8 W: @$ \s* S( H1 M% e: l8 i/ ^( K s- c- F) m" _9 l6 i7 z- Y S: @9 h6 B0 E8 J% P& r) j 标准仪表离场(S 7 K4 ~$ ]7 x+ o/ W1 I# q: Y7 n0 M2 e8 u# ` 起动活门, $ ~+ W* s" F: x) r6 u |发动机起动系统中,用以从气源总管向发动机起动器供4 O I+ c% u* F+ e 的活门。 ) y9 h9 }# X* f% W" l温(SAT or OAT),% B9 N/ h( ~2 _ 环境空气或外界空气的温度。5 c' {( }7 ?# R* T9 W 压口, , M- _$ x( q' {2 d位于机身外表,用来为飞机仪表感应静压的小孔。 , w0 l& J8 J; u% F" O J静压, 0 L9 r8 e% J9 B- v3 |+ X' n) p静止状态的空气或液体的压力。用磅/平方英寸来度量。 4 B z1 b' x1 ~, l. j. p# F3 y7 v# e& q1 W! h9 `) u4 ^* O% a8 e# W8 h0 H/ @5 I" ?7 p' V: u0 F# l9 ^' c" d$ O1 l% F英汉对照民用航空词典B OEING 0 c+ U) @, ~5 gTECHNICAL DICTIONARY 144 $ K1 _( W; ]. t6 uSTATION, A vertical reference plane along the fuselage % q/ L0 I/ K$ q- \0 p% kfor measurements along the fuselage.# s+ ]0 H% J' z5 }) i9 r/ _8 F TATOR, The stationary section of the compressor. S/ x/ E( f: y* e2 z+ \ etween the compressor stages in the jet engine. 5 h/ E5 {, d3 t- y& ~9 {TEERING ACTUATOR, A hydraulic actuator on the ! ]4 {# [" W0 q+ f% Hlanding gear shock strut for steering (moving) the 4 k- G. k0 {' M9 W: Hnosewheel left or right. . _- Q) N5 F [7 DTEERING TILLER, A hand-operated lever in the$ m4 G( j3 y* H osewheel left or 0 z( u% y5 Q; w& y" l9 N' W) O$ Oght. 2 Q Y3 Z$ L! f) u) A V0 eTICK NUDGER, A device to push the control column# p4 L$ H0 p* n4 v8 x, G. g1 i rward just before a stall occurs. & e% Q# S. ~/ S站位, ^% j0 E/ N, o" c6 S7 |' P 用以沿机身方向度量的垂直基准平面。4 K" k1 _3 b$ Z 定子,5 }# e8 S2 {( @. N) S 喷气发动机压气机各级之间的不转动的部份。) C3 @, |. U/ D+ x9 S9 b5 u$ }0 u" I 弯作动筒,2 i$ P% t/ A( A6 y9 C1 ~" _6 x 减震支柱上,用以使前轮左右转弯的液压% v8 @ ?$ A p) g 作动简。, @# `0 }* t4 b( I8 z7 [, j 轮转弯手柄,1 v# `4 W9 q- \/ X 内用来使前轮左右转弯的手柄。7 g' s" b5 z/ g/ U$ M 动推杆器,/ A! {5 Y6 `% u- Z$ _ 在失速前能将驾驶杆向前推的装置。 * }3 w# [" y6 NS 7 ^2 ]* b l) Q% @4 w8 Db |, o0 Q3 v9 I S" r8 b! E9 X0 c8 a7 M. `4 J2 A S ) m# X- U/ @( P/ mcontrol cabin for steering (moving) the n - u( H1 U, L+ w0 O& _6 Sri' e' l, i. b# W. p- O/ q) G$ ^2 A S & _9 p1 d/ f' Hfo R& G: ?7 e! X# N$ B* w0 L9 L+ G3 S9 q, c一个在起落架5 w1 H+ M) N1 ]. W# N; F+ N* R' h7 d& J1 j2 H, k2 I; I驾驶舱, T$ k( v/ c: s. c4 g" [& x3 B; i! h: h( A% Q; J6 V! B: k英汉对照民用航空词典B OEING ; c- N( V' Y5 a% v- h6 m, pTECHNICAL DICTIONARY 145 * c* o0 Z% Q7 q- xSTICK SHAKER, An electric motor operated devic ! @1 j$ q/ U7 b1 F) A2 Ethe control column which shakes the column be4 O6 w& N" X( |0 {3 y stall occurs.) p3 W2 N/ I! A6 u0 C0 s: A e on( p6 C0 U2 g' L3 m4 a5 I, x& w fore the& X2 r$ T* m4 c7 e4 [# M TOPWAY, An extension beyond the end of the runway # K @, S% z: F& F" Z- k, W5 k' lhich may be used to decelerate the airplane in case of , _. c7 O7 t! N1 a, gn aborted takeoff. It cannot be less than runway width2 ?9 `4 I9 W, q) E; e2 y% i and must be strong enough to support the airplane4 P2 M. U" |' `+ t0 G) x 置。 . @, ?+ P5 R! O9 b3 q1 ^5 Q$ \速安全道, ' [3 q$ u% K& j9 J2 p跑道两端,可用作在中断起飞时飞机减速的延伸地带。 ; X% Y8 G8 `7 m4 }" \* F' A它的宽度不能窄于跑道,硬度也必须能够支持飞机以免结 ( a. E: x9 E( f: |2 Z9 H cS 3 i& `7 k5 }$ _) b! \0 F4 @w! G' t( R* j# C/ O0 L% a4 s a2 h2 q$ D3 m! S: m8 j without structural damage. 2 `3 }! }7 i$ E( k h3 e7 @* ySTRAIN, Structural material deformed slightly due to the ! {- D) i$ s) b, U$ u: f' `! kaction and forces of stress.4 z- _% U* B" w; t) e# L( ? f7 x! q 振杆器, 8 Q. @: N; [0 F7 d! c驾驶杆上,在飞机失速前使驾驶杆振动的由电马达操 : R1 h# `/ P5 d5 r& b作的装 4 O0 R' ]+ I( [1 c: x/ z4 h" v- D) u) J3 A; q5 y 构损坏。( x6 F" R1 a% @* a 应变, " y& u, p. R+ A因应力作用和受力而轻微变形的结构材料。' N5 I3 T" M3 w g1 q, d( p- N6 q 英汉对照民用航空词典B OEING 8 }+ X/ y( A! TTECHNICAL DICTIONARY 146" K1 @! s3 n9 I3 t STRINGER, Structural components in the fuselage or7 y! q8 ?8 d. T P, ?) x4 K wing for transmitting skin loads to frames or wing ribs.1 X2 ~8 h4 K- B4 @! ~. A9 o/ C# F STROBE LIGHT, A high intensity flashing light on the % U! r* s, \- B9 p- C6 B! ?wing tips and empennage. : ]9 k' A# `8 J N( OSTRUCTURAL MEMBER, The part of an aircraft " O8 Y6 j: M f2 o" v9 a ^7 }structure that has been designed and constructed to . C5 {, S; Y0 ?3 H+ p! |6 Xcarry and accept loads and stress. X6 X# v! i; \+ Y. Z" _" c STRUT, Mechanical components of the landing gear for) q) O. c0 Q8 f* @8 f+ ~' q keeping the gear in the extended position. ( ^ C, L/ k/ W3 A% v6 e0 r机身或机翼中,用以将蒙皮载荷传至到隔框或翼肋的结 ( r0 g" d) y+ G7 C# V+ r/ Y1 ?构件。+ u5 M" p0 |% B 频闪灯光, ! _ b( z: c7 ?; ^) j" d- z位于翼梢和机尾的高强度的闪光灯。5 M7 [/ {. h: ^3 u: g$ M) [- h5 A0 E/ | 件,& B9 \% T; z5 ~1 N$ k5 }' W, C p% ^ 飞机结构的一部份。为运送和承受负载及应力而设计建 0 M2 z+ t8 t4 [9 \1 c3 c成。) w! m; @( R. e3 T 支柱,' A$ n4 x+ Y. | 起落架上用以使起落架保持在伸出位置的机械式部件。 5 H9 x: x% D+ }0 ^3 {$ @4 l8 R长桁,7 }3 l c. g D/ m; O! `. N. U {' u$ q+ K7 ]% @: k( o' d( G9 `3 q) w1 p( F英汉对照民用航空词典B OEING " `' l! J$ q+ oTECHNICAL DICTIONARY 147* `$ a& v- d% ]/ I1 J+ a SUMMATION UNIT, An electronic component for3 v9 x! b: h" k8 o6 _ adding fuel quantities in all tanks sending a signal to the R: E+ W. ?4 r0 ^, `) qtal fuel quantity display. 6 l4 A- s4 J, [8 c0 ^7 B$ SUMP, A lowest point in the engine oil system or fuel 1 V" s" o# C# `8 y4 ]" r' P' cnk.3 q0 ]* ^3 q2 s) A& y1 y UPPLEMENTAL DATA, Additional data stored in the7 O# P+ L* g. a8 c0 g: g ^ MC memory, supplementing the loaded navigation " g9 W) i1 x' Jata base.7 a3 I% v( Q( e: y n 4 P$ ~% v5 e) ?eviating from normal modes. ( C. o0 b2 n& q* MSURGE, A sudden change in the airflow through the p J4 b3 l& T4 G4 } the compressor not being able / P Q: r G1 N7 c Zcompress the airflow. # A) M4 l0 H( ISWAGE, To squeeze together two or more items to 6 z) ]0 _( m" [* m# x, x+ N& Iform a permanent unit. Example: a lead or steel piece , s% ~ ] x/ \ v5 R! H7 w% k0 Ron a cable which forms a stop or camlike unit. Also to 1 Z/ J& |0 i$ d2 creduce the diameter of tubing. 8 j$ N$ ?4 d) o. q; w, w! oSWITCH, A device which changes the condition of an: T g1 c* z6 R3 o/ M* } electrical system from on/off or open/close.- t9 q, a8 c4 i4 K0 E: } 燃油总和器,$ N( y2 v5 ^" \1 H0 {$ v4 W 将所有燃油箱内的燃油量相加,并将总油量用信号传至" @, r; X# j( p) R' X 量显示器的电子部件。 $ y3 A: P6 g2 S% ?/ n3 |+ f( X* Q集油槽, 8 \! P$ A N1 l- T$ J; @发动机滑油系统内,或燃油箱内的最低点。 ' w% a- u2 Y4 ~9 Y; j+ |增补数据, 5 l$ w5 ^# A/ ~. {飞行管理计算机存储器中的附加数据。用于补充导航数 $ ^, U. K8 [" T, \/ a! [; g8 n据库。+ W s: z+ y, P* `: _% y* H6 n8 B4 L$ Y 附加的数字飞行控制系统方式,当偏离正常方式时使$ y' I8 {* `+ `5 r+ R5 _, Y0 N* ]+ T& ?" j1 E& h1 f+ x4 Q, _7 p 过发动机的压气机的气流的突然改变,而导致 # G3 F1 I9 N& N2 G气机不能压缩空气的现象。 " l5 t2 H- \7 g5 q9 m5 k2 l4 L5 t陷型模, * T7 \& G7 }/ p挤压两件或两件以上的物体来制造一件永久性的元件。6 u/ S+ |9 H7 d 如:一块铅或钢在钢索上形成一个止动器或凸轮之类的 % E5 j% B4 o+ i% W8 ]件。也可作减小管道的直径之用。( f Y; j) }! K1 f( ?# D6 C 开关; % y4 A4 t/ L; u5 C. A) Q改变电气系统通/断或开/关的装置。# |# i; d. E9 \( D ?. } to 4 l& V% O/ y1 i! \. p" s+ W; e$ W+ @S % Q& Q6 ]' T8 f" b9 V$ W/ P; Bta, u) s3 ]/ V% M8 c) r- ^( P S0 e7 R( D5 l9 e) I# B F & j# A. ]% p8 r6 Zd + k* G6 C* E" E4 K. ?SUPPLEMENTARY MODES, Additional digital flight8 M" z! a4 d# w9 A+ N( A+ b# ^ control system modes that are available, used whe- F! I9 P) ^4 J d / D( d' O9 g" x( l6 g+ \compressor resulting in ~' u( y. Z) Z, U% B to 2 X7 y7 y1 r# G, `" ^6 D; {0 G- N$ x! {) L 辅助方式7 i8 ^8 B8 I& v! F. R- F0 w6 x& j$ Y% }% e$ l9 f 喘振, ! v! g) V/ t8 K1 I2 y) B8 A' V由于通% D5 b3 b3 @" d& }+ [" j1 L4 s: z& h l# l: R% x/ z) b8 e. J4 H, @0 x+ r8 L1 {8 b; F+ R: o% H. C3 G- @英汉对照民用航空词典B OEING; F3 p6 I7 \; {" v/ u5 L TECHNICAL DICTIONARY 148. u! N: q; m# z9 }2 t: z SWIVEL, A device for rotation of components. A: ?( \9 K- Q: Y a SWIVEL COUPLING, A junction in hydraulic9 f4 D' G- H3 Y) L) I bes for allowing component movement. 5 }7 y+ H9 e/ i3 y0 @1 zYMBOL, A graphic view of an aircraft component in a: ~! X1 M: N) q1 X/ H5 _: D ery simplified format. Used on drawings to represent Q T( f6 `/ {. P3 L F e entire component. 1 l# ^+ l4 y- \# S* j, P- t6 VSYMBOL GENERATOR, Generates the video signals ' x5 F9 b! ^: j6 Z+ k2 Bthat are displayed on the EADI and the EHSI. 3 E2 q W' t7 L2 Z5 {SYNCHRONIZER, A device or circuit to make the units ) i/ P+ i/ R9 Rperate in unison.0 @. J7 }7 N9 F9 w4 A. t SYNCHRONOUS, Refers to two or more things which 9 i |9 s& B6 I) h# Thappen in a system at the same time. 3 m9 A) \. A" X) b! Y, a- `用以使部件旋转的装置。- j* y* y8 L+ ? 转动接头, / t8 J+ s$ U, g2 o+ P1 c液压管线上,使相邻的液压管能够动的接头。8 N* A5 J$ A4 H8 n& w 符号, 4 |6 ]2 i' V$ k# C# U8 Y( ]飞机部件的简单示意图。用于绘图以代表部件的整个结; ]" K) Q9 S# O, ^* f$ g! l# ^1 g 构。( b7 I( m* w9 z! p, w8 @5 T. D: G 符号发生器,5 @3 o; Q; U. z+ J3 H" O 为姿态指引仪和航道罗盘产生图象信号的装置。* C/ Q) ]" ^3 O; x9 o4 d- I) c 同步器,$ s' j _" T) o9 p: A1 r$ E1 |: V, q 使元件操作协调一致的装置或电路。 . p! }( H/ M2 ^* b* w7 |8 b两个以上的东西同时在一个系统中发生。 ) f2 J2 n3 P3 r# c; |# ntu4 O) F& c+ ^. v" e0 y: h! h S) R% m" N$ F% {# H; c, \- P. f v* b- Q# F' ~& _' c1 [ th / c# C6 ~2 w7 J. q. }5 D2 c2 L* `o* {6 R* O5 c6 x) \ { 转座,6 d* O- {4 V% | 同步,4 b/ {, v$ I1 p 指两个或 5 L9 \6 q, V1 c1 N" h" [: R B英汉对照民用航空词典B OEING 2 u! T8 K2 U) A, BTECHNICAL DICTIONARY 149 3 U3 \5 v& w0 w" UT : `& o+ W7 U3 i; \0 V4 F: XAB, A small, hinged, moveable part on the trailing ' |* r. B2 |- W8 R: odge of a control surface (aileron, elevator, rudder). 8 x% o$ z7 K3 e% iBalance or control tab - moves in an opposite & J0 b1 p% e5 L& H/ H, h; S5 sdirection to the control surface for assisting9 o N9 n% q( I: _ in movement of the control surface. ' A% _( }/ R/ Z. W% UTrim tab - provides controlled deflection of ailerons# p+ S* d" V F) n ~! o# f: Q) t8 ~ or rudder to compensate for imbalance in 1 [4 {# [9 V: f, X( h/ tthrust or fuel quantity.7 K( q0 C9 C# w. X2 l* F Stabilizer trim - controlled deflection of the horizontal2 {9 R( ?6 ?* {3 N! Z9 W cy * U8 r5 K' Z) {proportional to the speed of rotation.5 h2 W/ P1 ^9 K$ {7 o1 [6 C# ? TAI, SEE -THERMAL ANTI-ICING - ^0 ~; v- `# x; c" A) J- b- \( {TAIL PIPE, Duct at the back of the engine exhaust.. ^7 j: Z2 @2 x3 X4 [ TAIL WIND, The wind component relative to the: p& a8 g# e. [! N8 h& C8 H7 b2 y airplane direction and coming from behind the airplane. ) J3 G$ g) b! W) ]# |调整片, + D* r6 _4 u0 w7 S6 ^+ E( m: P铰接在操纵面(副翼、升降舵、方向舵)后缘的可动小 8 N. [2 |, L5 ?5 t2 f% |部件。 2 K/ M$ v! E8 E" D平衡或操纵调整片—与操纵面运动方向相反,用以帮% p5 `$ Q& D C% u% E5 C 助操纵面运动。$ d1 u4 i* ~3 y 配平调整片—使副翼或方向舵作控制之下的偏转,以 2 g6 Y9 X( o7 b7 b+ a# O补偿推力,或燃油量的不平衡。 6 ]2 m! k) y0 t6 |3 y/ V' N安定面配平—使水平安定面作控制之下的偏转,以减9 s, S! j* i/ A! Y: v+ D 少操纵力。2 F) }7 h; r# R 机,: Q4 l: X% p& q$ A 提供频率与转速成比例的电流的小发电机。1 ]! K& N1 q& p& ]" O5 A7 a3 m 热防冰,; F# H' R* Q" k* j 见Thermal Anti-Icing# S, ~! D& u, S T- i6 J; Z! g% F& ^- [+ O4 a$ z# M5 V3 T e $ d- [% S3 _2 t: U8 qstabilizer to reduce control force. % b; X7 P$ I! J% ]9 sTACHOMETER GENERATOR, A small electric! u# @$ ?& J# J1 o) u% \$ { generator for supplying current at a frequen e1 b1 P7 X# o( |" E 测速发电; Z7 f/ E+ @ c+ P& {0 f# J! g2 }尾管, & [6 k* P$ R' s/ C1 T发动机排气管后部,用以排出发动机的废气的管道。# c1 J* L$ G; p+ N7 A) S# G* F 顺风,' i. p1 U3 X! f' h 飞机后方的来风在飞行方向上的分量。 5 ?; z7 ~* v# F! o0 g. W英汉对照民用航空词典B OEING 9 g) x3 Y# _; ~TECHNICAL DICTIONARY 150! t. u! O& _( X7 N* l K- @ TAKEOFF ANALYSIS, Analysis that evaluates the * l: P' ~- s3 R7 H kairplane takeoff performance capability for a variety of) Z, g. I0 ]* B- I environmental factors at a given runway and airport.7 Q$ J9 f( S8 S+ Y ET PARAMETER, A specific goal such as+ @/ Q1 v3 a6 I5 c1 N3 w irspeed, thrust, engine speed, altitude, temperature, or " y7 I6 t% H7 d: y1 n5 Qte of climb which is to be achieved. * t6 E9 w% A/ w5 V; T( B+ TASK TICKET, A computer label used for tracking the ; A" v' }9 R7 w" n: y, z' aompletion of a task. e- e* X2 B7 F0 aRATURE . ]1 E: s- p, J q7 nAXI FUEL, Fuel burned from the time the engines are1 a; T. M+ G, A+ w6 q r: t6 n r.! ?" E9 I w) t! C CAS, SEE -TRAFFIC ALERT AND COLLISION ) {" D1 {1 {. _' `+ P% X# m- AVOIDANCE SYSTEM * K9 e6 w% N% e6 M欲达到的特定目标,如空速、推力、发动机转速、高度、+ s7 q" O) \# @0 w4 i3 |- e; d4 k6 N 度或爬升率等。 ) t" y6 A5 M6 h; ]9 Z! y工作记录单,8 Q4 v, |' b6 R! Z N 用于追踪工作完成情况的电脑记录单。9 o+ F8 p9 s. x8 T4 x- _2 z 全温,5 a K: g! r P& r 见Total Air Temperature * n4 g+ m! A! z! N N9 xTARG8 S6 ~! E0 I+ x* T! [ a 5 j* R+ ^$ Q0 n5 _' Tra W2 v- d' i7 D% d# B T . D6 ]) s1 b; y' w. Ac! R& t+ F2 G8 l* \! F) g# B' F TAT, SEE - TOTAL AIR TEMPE4 }& `& d8 W0 N TAXI, Movement of airplane on the ground using! h8 c+ \' N1 Y6 A1 H. ] airplane engine power. 2 i- o0 o* Y+ ~T. A0 c, e( j6 V! f+ P7 ~0 m started until the airplane begins the takeoff maneuve/ k. R% k7 {: U9 C& G2 u+ ` T3 a4 G3 x! f% x' h" L A- S, O$ A& d/ t' E$ P: ?: ~ 起飞分析, / Q: L1 r2 v) Y; t9 U" u# ]# [对飞机在一个给定的机场和跑道,在各种环境状况下的4 b' O6 M6 {1 j& Z% R 起飞性能能力的评估。6 b! Q) U6 C6 E% O9 W3 l 目标参数,% C6 i: h, B# e6 K9 D. A7 H5 v6 p: F6 u Y( A( `+ M- t( W$ `! w· & m& v# r6 B2 b4 I$ q8 X" f) \滑行, & r* [2 \$ Z0 t9 t7 b行燃油,* y% n; L! Z# E5 G8 T- B1 B' Z 起动,到飞机开始作起飞动作之间,所消耗的 " I3 k8 ]4 U' E$ i8 r中交通警告与防撞系统,. l1 d: r* t; y2 z 见Traffic Alert and Collision Avoidance System . h9 p3 o( D/ U9 V飞机凭借发动机推力在地面的运动。 9 k) X$ I1 a1 o) W$ {- G" b: G# B# y, |+ i; i 从发动机# {4 O3 k8 K0 ~2 D& h7 u 燃油。8 H% T& i9 l, b1 ?* A& @7 [/ F% E" v! h/ X4 | J* Z5 X5 w( j! Z! d7 e# U' Q# B 英汉对照民用航空词典B OEING ; x- Y0 h& D' G! P+ M* STECHNICAL DICTIONARY 151 ( q5 M" {. v$ T: RTCC, SEE - TURBINE CASE COOLING 5 C9 }% V% `3 P5 @8 BEE, A pipe or tube connector manufactured in the 6 b. v# m, A0 k) jEFLON, A synthetic material for hydraulic and% M0 B( J! [9 D+ b( |$ O neumatic seals. ; V; h0 R! x$ ^' NEMPERATURE INDICATION STRIP, Temperature ! o: `. C I& B" i/ Y- uensitive tape which changes color at high temperature 3 U4 @% B4 o3 ]6 [r indicating component exposure to high * [9 P- \3 g, T+ n8 oTEMPERATURE INVERSION, An atmospheric / n5 p& l" w, _* Fcondition which causes the outside temperature to$ j% z. M+ i5 s5 J1 ?. m5 u* i increase as the airplane altitude increases.9 ]4 `* \; {# G TENSIOMETER, An instrument used to measure the4 w5 l( B8 Z3 l+ Y+ c, D- V4 R tension applied to aircraft control cables.& k" z2 c$ C- K5 A+ U) v1 d" E7 p 冷却, 3 f3 C2 l0 W8 N1 o, N! FT 6 T0 n1 L& }; \( ]! Pshape of a T. S0 ?4 D( B4 l7 u4 N V T6 u6 W# B* Z: w; D* O( t p! V4 w" ?) A6 n* a$ } T* w& L6 t }( c" \; L s8 y' i# D- m1 t" P* ^$ b' } fo * T, z, c2 [( G& W5 ~' z: Qtemperatures. 3 e, M" k" i5 {" P7 O涡轮机匣 3 h# ?4 H* I) K! {见Turbine Case Cooling.( ?. z. l9 U) H: S* l5 c8 y 字接头, : n. ]+ d, |! i8 t/ {: P的管道连接器。' h1 v# r$ {' Z3 K- h* j 氟隆, 2 \" H# \, `$ C) g: H用于制造液压和气源封严的一种人工合成材料。 7 a# G* P+ m. H- }- S度指示带, 0 r9 D, t7 T. F) x b遇高温变色,以指示部件周围高温的热敏带。/ k4 o4 ?: ]( a3 Y 逆温,- E7 ?# U2 g! E& b- i& s 一种大气状态,引起外界温度随飞机高度增加而增加。 : o( ]2 B6 z5 t' ]% u张力计;- ^9 Q+ G3 S7 [ 用于测量飞机操纵钢索上受到的张力的一种仪表。 ( m& }; H' V* G3 l0 H+ }T i9 \! Y0 B2 G- e* B/ R制成T字形 0 y9 T- w1 C" i" t3 s5 d% j2 ]0 H/ P! o3 C: W& P7 ? 英汉对照民用航空词典B OEING- A2 V9 }* f& }2 {* y, P: n$ Y TECHNICAL DICTIONARY 152 1 P; ^( F4 c3 B2 w/ g: Q0 X* xTHERM1 ` J' t o# @- G6 V formatio ( w& I6 \' P& O4 pusing ho + h/ i- d+ e2 f9 U' S5 C) @AL ANTI-ICING, A method of preventing ice ) _; X2 v+ y2 b+ ~" |" [7 ]' cn on the nose cowl and wing leading edges by ) A7 ^ F4 T4 J; K4 Ut air.% `) ^' Y# _5 N: n- }! o/ Q THERMAL t 1 i6 W4 V3 _. B* {$ Sin a tube fo en tube ) b# |: g0 b# Gis pressurized with oxygen.( A' T' z/ ~! v* }1 t+ }/ } HERMAL RELIEF VALVE, A valve which opens to / [$ s# x2 S$ ]$ a/ L/ Z7 g. zture. 0 z( U) Y/ o$ EHERMAL SWITCH, SEE -THERMOSTATIC SWITCH ' N4 f: w! O% Z0 R; {) i/ Oe o- o7 c, D3 N& t( @sistance changes with a change in temperature. , \1 J# R. R# \' |, t. m防冰,! j+ f5 A1 a$ O2 o; f# E9 R# T1 n! \/ c 用热空气防止发动机前整流罩和机翼前缘结冰的方法。6 d: ]& e+ z8 B' K& n) j 在管子里,使管子受氧气充压时温度不致于上升的一 8 A, s" P8 f4 |) Y( Y! D个刷子形导线元件。0 d7 w' S. b n9 G7 W6 H8 r6 w 控释压活门,: x! i8 I- k4 `0 H 过高而打开,以减低流体压力的活门。 ' \# T* L% }9 P+ ~电门,9 f( m1 N( J4 I, m$ Y 见Thermostatic Switch % ^& p$ S5 S+ J9 `8 u$ }" YCOMPENSATOR, A brush-like wire elemen4 W* u% x8 e4 V7 e( N; \ r preventing temperature increase wh: b3 A7 t5 s& x c. {6 ] T 5 o( B3 m$ N& Mdecrease fluid pressure due to high fluid tempera + y5 ]4 d5 X- r" jT0 Z& a; @: ]5 A: S4 z" X THERMISTOR, A temperature sensitive resistor whos# A, S7 d; K1 S* H1 I re ) r5 s, O8 ^9 ~8 ?" d4 W1 U4 x- C G7 ]( P/ H6 |5 h热补偿器, 6 C' U6 C$ G6 _. l" |+ N+ A2 T5 r8 S+ M- e& Q, {* K/ T! f2 D) P' o! n因为流体温度5 J- d9 y9 R- h6 {+ v1 E i9 z1 l8 b$ m! s0 P& Y) H2 W+ d4 ^$ B ,热敏电阻5 |* X$ G4 }. }; q7 p, b 一种电阻值随温度的变化而变化的对温度敏感的电阻。 : B( _' \. Y; l: u1 `+ |英汉对照民用航空词典B OEING# M; d% d$ {' e& I/ Y# z7 a' X TECHNICAL DICTIONARY 153 ) M) p( Z6 T3 |3 @0 @6 |* ETHERMOCOUPLE, Two different metal wires joined at- K: G) b6 K, b6 T4 I+ ^# R. B urrent is produced proportional to the temperature # m4 t3 T& A/ s" C+ z2 l1 P; Mdifference. 1 m; R7 G+ k+ k- oTHERMOSTAT, A component set to operate at a $ D' L2 n% u" K: f) P: |efinite temperature for controlling electric circuits and; o; u' Y X c6 f( Y( D0 }% o alves. ' M; }5 `8 o3 _) }# R0 Rmperature sensitive switch which opens at a preset N j6 K* s! Y/ C. Mmperature.- Y+ e& W+ g! e/ x THR HOLD, SEE -THROTTLE HOLD 5 O5 D. t% {* {# s1 Y即产生与温差成比例的电流。 ( u4 X1 L0 a5 p+ M用来在一定温度下操作,以控制电路和活门的部件。: }# O) ?9 ]* v& H9 A5 f9 U7 i4 W+ Z 恒温电门,3 K- @! A# N$ @ 一个热控的、在预定温度断开的热敏电门。% o* P% p5 V0 R- ?- {3 r* S3 C 见Throttle Hold( u- v) d& _: g* V# Y% V both ends for temperature measurement. When both 0 J1 }4 |# g+ djunctions are at different temperatures, an electric5 \1 B0 H) n' O1 u c " F& [# l% i0 a' ed" h0 }6 z9 K" h+ x$ R _ v) C! R; l/ } J0 A1 ^2 F0 B THERMOSTATIC SWITCH, A heat controlled,$ Z: n9 g3 l X m te K. D2 t( j' ?5 n3 W/ kte & o1 ~: Z% d* l- \6 b8 {( w$ a热电偶, / \, d8 O" c9 \) N5 _用来量取温度,两端相连的两根不同金属导线。当两端1 J" L4 W4 j" ?% N# Q9 G 之间有温差时,金属丝内 4 p: r8 F* L1 O3 H; s; l2 U恒温器,0 e2 Q, ?! F& {/ M& i 油门保持, 3 E+ c( h, w; B" F9 w o; O W: M- a* t英汉对照民用航空词典B OEING . m0 ?, o) [+ h8 yTECHNICAL DICTIONARY 154 $ i# B4 Y( M8 ^; BTHRESHOLD (NO. 1), The bottom part of an opening in5 Z5 q8 d1 h. j4 g) K# f, g9 \& T a fuselage doorway.0 s: p6 X' b1 @0 V- D1 u- k . 2), The approach end of the runway.2 a6 [/ \0 d) G% q& s THROTTLE LEVER ANGLE, Angle of throttle lever / V. A4 }1 j4 n+ H, v' J! Xdisplacement. J4 p3 S( C9 N$ U HROTTLE SPLIT, An engine control condition in which k) d$ Q* U% i4 ~: S the throttle lever angle is different between throttle , c6 j! z' \ mlevers but the engine thrusts are the same.- Y# B& P* A" _3 `- n/ p HROTTLE VALVE, A valve in the fuel control unit for) D+ n, r* j5 k7 G6 x8 K! n cheduling fuel flow to the engine. 8 r" I, z+ |1 q h- V9 g( ?机场跑道到场的一端。 $ {5 v4 B8 U# T D# n. \/ L" m5 M' w油门杆角度, & U0 g, `9 h2 _/ G3 o- Q% B9 b油门杆手柄位移的角度。) G+ k+ S( t4 i: h- H a 油门分叉, 8 v5 M: Q1 X4 F: A一种发动机控制状态。在这种状态下,油门杆之间的油# ~" T# A# V0 H n+ L+ U: ? 门杆角度不同,但发动机推力相同。 1 r- }" M1 `* o5 o, \3 A; @流活门," _5 _- \- m- T 燃油控制组件中,用以排定燃油流量的活门。 ; C9 E& K0 \4 }5 fTHRESHOLD (NO B4 k% h: }2 {5 DTHROTTLE HOLD, A mode of the autothrottle where" x& \9 X$ N" c/ h3 F" n the thrust levers remain where placed. 9 a7 J* f% @; G) yT " M4 Z4 i3 J2 u; zT - E6 `& T, `( h. x+ h& U+ Z- ts : F- ` o2 ?) i3 P. l2 c门槛,7 U4 l ~3 D2 M. `4 F' F 机身舱门开口的底部。# t* [5 \9 ^6 s3 p4 d9 l 跑道头,* ?* b+ F( H+ j1 T# k 油门保持,8 j* V. D% A% K6 i, g) @) f 自动油门的推力手柄不改变位置的方式。 ; h. C. D+ Q/ @5 y+ I* U2 A" m6 `+ q0 @, M英汉对照民用航空词典B OEING ?# i9 P" g4 _- ]1 @6 ETECHNICAL DICTIONARY 155 - N- n2 ~6 U! s5 \$ B" t* M5 E7 DTHRUST, The driving force produced by a jet engine.! a* A4 B9 J8 R% G# L HRUST LIMIT, Maximum allowable thrust for a specific ( D# N9 q+ ~2 U, Tet of conditions.& v, F. L: T; U' d' | HRUST MODE ANNUNCIATOR, A display unit or part+ R! D) }& [) S& S' v f a display that shows the engine thrust mode. ( }( Z5 K J( e: G( l! s/ ~6 ?HRUST REVERSER, A mechanical device located in( s0 K. I7 j* U. n0 |+ U+ Y7 _' m e fan or exhaust section of the engine for eliminating3 ^! m6 s( [9 a" J& w rward thrust by deflecting fan air or exhaust gasses in 3 ]# D4 p2 H, B5 W( \e forward direction can be used for stopping during + f; R- ?* P$ ` H9 qlanding and during an RTO.0 y* v' C$ ]% T- u 推力,; B- r l, K" r$ Z! X% x7 ]; X1 o 力极限, , e# u! R7 [ T5 f; X9 N8 v在一组特定的状况下,发动机的最大允许推力。 % V+ L- s3 q$ h/ L+ |* P% |3 d推力方式信号牌, - \, K; i- b( G1 r( D, u- k显示发动机推力方式的显示器或显示器的一部份。; N8 A! D/ B7 z4 w" }+ n! i$ p% p 反推装置,0 \, u. [ K) W: w 位于发动机的风扇段或排气段的机械装置。该装置通过1 d B3 g& c6 c; V; W p F& T, L 使风扇空气或排出之废气冲向前方,以消除发动机向前的! P) E; r- g7 n% r* J0 v! T5 l; } 推力,并减短飞机在着陆或中断起飞时的制动距离。0 R8 _( X2 H5 h) E T* X2 z% ?) t. b; _: P s( {4 {# s+ E6 _9 m4 |6 M# r b T 4 m6 b$ o% f/ Uo , o; v( Q6 }8 Z5 y2 o. iT 9 _' j+ S; ?' F% q. T" J9 A1 H9 Yth/ m0 W9 [* E8 {( S fo * r0 b! D& ?& tth' ?0 ` _# z0 J% g/ G 喷气发动机的驱动力。& k: x, D6 ?/ T% i5 h) |' |8 a$ r# w) ~+ _; |, w$ Y英汉对照民用航空词典B OEING. D& y9 I. ]9 E) F TECHNICAL DICTIONARY 1569 a3 m: {9 f7 v) H' x& y THRUST REVERSER COWL, A cover around the thrust% j) k- H \2 I4 q2 S+ C* E IME DELAY, An electrical circuit for starting/stopping ) p/ z2 ^9 ~9 U' {/ N Z) @e flow of electric current to an operating component0 s1 q) y! x/ H) T& d r a period of time/after a period of time.$ h$ R% G4 ^' |! y0 M+ \5 x IRE SPEED LIMIT WEIGHT, The maximum weight% G, y; M3 d7 |" `; e. g* r) v( W permitted at takeoff that results in a liftoff speed equal to 0 f1 W- y# ] A7 P4 Q; d* ]& \% We rated tire speed.1 @; V f3 M# ~/ S M, h4 `# q* y OLERANCE, The part of a specific measurement that & }5 S6 L5 J) Q) K- ?allowed to vary in dimension. Usually given in a plus 2 m6 D% v' m) J- k) or minus (-) format. ; c" f/ \/ a2 u! ECLIMB, The point at which the airplane " }; j6 |$ C, ^* k% i: Creaches the cruise altitude.7 g. n; ]2 E! b5 |4 P1 U ts the cruise altitude and begins to 7 n+ R% t4 I8 k8 j& d& i: ?descend.! D( T1 l" N; C) { for transmitting+ L' ]; y+ N7 [- R- } twisting motion to the control surfaces. 1 ^& m% u P/ h; {7 k$ l$ k; F; ~. y- l1 P$ ^7 i2 u' P6 K2 _. D/ M5 ^! _ {% F 部件以进行维护。 6 G/ b( S. d" ]4 d& U" `# |- D延时电路,. `1 U% J7 N. V# b+ | 用以起动/阻止电流在某一段时间内后进人工作部件# `6 w+ c4 |* H* S, u/ i, ~ 的电路。9 E/ n$ b3 L. ]6 u) i% t% ] 轮胎速度限重, 9 W; S! I: f E" [0 b飞机起飞时,使离地速度和额定的轮胎速度相同的允许+ u: t& f$ n6 d, B, O 最大重量。, D. b* f; Z. L; O" m. H1 c# r7 T" F 公差, & Q2 p1 P5 h$ c0 i特定量度容许有偏差的部份。通常以(+)或(-) # Q4 ^" C! D- X5 a N5 H- \的形式表示。 : _7 j1 g8 J' [) p" ^爬升顶点,) ]- w9 b$ V- _/ h& h& m! w1 {' v 飞机达到巡航高度开始平飞的那一点。 & o, V1 g- ]+ P: p/ B" _" a下降起始点(TOP), * o; Q' H2 ^) M5 z! j飞机飞离巡航高度而开始下降的那一点。2 j' D1 P9 ?: P# v- X6 | 操纵面的管状部件。 9 {* |, o+ F% U- breverser of the engine that can be opened to access: j8 g7 K7 j4 ~2 D \( p) a& ` components for maintenance.: V( }/ c/ B6 ~/ \8 O T + c/ _0 z4 ]/ j; l( Z' b3 lth9 |9 g7 O% W& W2 @9 p @! Q fo( \; j& z" d3 R T ) C2 h0 G( o( ?; [1 L0 O4 wth 0 s1 ?* ~! W; p4 ?# M8 M5 }: ^T: G7 r, V) S) R is$ f. U. \4 E0 K (+8 {: y- V7 }4 `* W; N TOP OF 2 `- O7 @+ G s' jTOP OF DESCENT (TOP), The point at which the% L8 w; s3 V% k3 ]( o) E airplane depar+ ~* J8 w3 H. N4 b0 k TORQUE TUBE, A tubular component ! d: @0 K4 u: L4 C/ U/ ^反推整流罩 ) G; |; P4 V7 ^, n在发动机反推装置外围的罩子。取下后可以够到内部 1 M- ` m j8 O' H1 O' K: }% N扭力管, 3 D0 V1 f5 |- f9 k- c用以将扭转运动传给 M' m b `) j) v9 }% C英汉对照民用航空词典B OEING 0 ]9 m1 c/ w) M( w7 |) WTECHNICAL DICTIONARY 1572 s e0 H3 Y- v+ J4 l TORSION, Twisting of a material or part caused by5 t' }3 z; Z( ^: r& k/ ?$ d; A external stress. . x2 w6 F$ |6 ^( l1 Q5 c( RORSION LINK, A hinged linkage connecting the inner 8 {/ }+ h# G1 }9 f9 Tnd outer cylinders of a shock strut. + F. d; H5 p8 X2 Ndue to the ram # X. \1 i; w g6 ^* m2 Rffect of high speed flight.& ?+ w' m' ?, V" I. R, _- H! b URE, Pressure higher than ambient$ Q/ W) `' ?! a/ ~6 W3 L3 _ ressure due to air flow, measured in pounds per" p! P% E1 k! Y# K9 r' Y( g# G; ` quare inch (psi).4 z% L0 z( ^6 j7 P% F' y/ O er than0 m& Y% j$ B& ?* m9 a! V mbient temperature due to the compression of air flow, 9 w6 q' R: y; K- {, N6 weasured in degrees Celsius (C), or degrees - D- ]6 E- R. I- l8 e; M- Uahrenheit (F). " [+ [& |5 r8 XTOUCHDOWN, The point at which an aircraft first 2 q7 t2 f& N& W) d+ x0 w% }+ Kmakes contact with the runway.1 v0 `. |2 O7 l9 O( c& }5 l+ a 生的扭转。 - e% |' s/ o" m6 h扭力臂, , I# I- r5 T# m# k减震支柱的内筒与外筒之间,用以防止活塞旋转的铰链 ! d4 t& z: B- [% x' M连杆。" s A" r6 t0 W$ r! E0 ^& V 的冲击效应 W z* ?. ^! i' b3 a引起的温度的升高的总和。 2 h; }' q9 b3 o总压,( h8 O7 F) y4 U1 g5 G 由于空气流动而高于环境压力的压力。常用磅/平方英8 M3 T& X5 A+ S (psi)来度量。* e0 A' c, I0 I* q& p B( \ 全温,# ^9 t. S q6 J; s% J% }1 b 由于气流的压缩而高于环境温度的空气温度。用摄氏 ! K9 L! I3 O8 A(°C)或华氏(°F)来量度。 ^ a0 f) X( e; h# E接地,; C1 g! L. E+ E' @( y0 H 飞机降落时,飞机最先接触跑道的一刻。 8 f' D' k5 L; p& h+ XT" ]+ b& N: s7 S2 d' r( e3 T a : e- @$ E" Q; h% i3 O6 x/ I0 y- r: q* RTOTAL AIR TEMPERATURE, Ambient or static air6 C, S6 Y E2 }3 V- x. ? temperature plus the rise of temperature4 n8 v6 x/ V p* ^; o e ' W8 M' v0 O. t$ _8 H3 ]8 ETOTAL PRESS 4 O6 L) N0 Y+ F# I: s( kp ( X1 N3 g; ~) e \s, ^9 ^9 K* }! w6 J! F$ [ TOTAL TEMPERATURE, Temperature high/ m& n7 Q7 \2 b& x" g6 _ a# G. L4 X4 S- V m; R& n2 M/ C# `. |" p4 d6 r F; W+ p: w$ I; o9 H- j L 扭曲,- O# l' f" T$ X. n7 X: O2 Z! \1 S- ~ 物体受外应力的作用所产. d1 R$ R7 C& e t. g1 L4 X 空气全温,8 K8 B$ j2 ~2 F- z7 z 环境温度或静空气的温度,和由于高速飞行 2 g' @; C e$ l2 _5 S! _: h4 v( [, @- \: N6 c: c5 S: [; c6 M0 `% e3 r* H+ o. r s" O: A 英汉对照民用航空词典B OEING 1 g$ u1 ^; m9 E; L0 p p# `TECHNICAL DICTIONARY 158$ T. h- r4 D5 j% u- ] TOUCHDOWN ZONE ELEVATION (TDZE), The- e4 R6 Y' b; }2 O9 N2 W highest elevation in the first 3,000 feet of the landing 4 \$ K# k% k1 N7 e. c6 \# `* iurface.: g% h# ^+ |' A- Y, s1 i rt of nose or main landing gear for2 A0 U6 ]. k& d1 s ttaching a tow bar to move the airplane on the ground. . d. Q4 ^0 s8 U `7 B9 x: v, valong. % B: j! ^6 h) y) i) ~RACK (NO. 2), A navigation term that describes the 5 F' A, M6 K. A e4 FTRAFFIC ALERT AND COLLISION AVOIDANCE) q" l' {$ I7 X: j SYSTEM, A system designed to alert the flight crew to % s8 a) P9 d) U d+ j9 k, Q/ upotential conflicts with other transponder equipped ) z( \/ B0 a9 }* V/ {airplanes flying in the same area.% i, L" t0 P) {5 ]$ h; m TRAILING EDGE, The rear edge of a wing, stabilizer or # y+ d+ M! r& U5 Y5 ~. K1 x6 J" D8 `" Ucontrol surface. , y) @8 g, B: x" C5 P$ r: uTRANSDUCER, An electrical device that either takes 8 h, Q. D L& U- q1 [electrical energy and changes it into mechanical 9 K* K3 s J1 hmovement, or mechanical movement and changes it ) l- o7 b) ~* B4 J7 _/ c% jinto electrical energy.: A/ E2 z/ U! Y$ }) n TRANSFER GEARBOX, SEE - ANGLE GEARBOX 2 b2 V9 {: Y: l" s- f: l5 j1 a) e% x高(TDZE), - d# `( Z9 S& |2 o; \: K& @, ]高标高。& D. J7 y/ K; o$ r4 C; s 前起落架或主起落架上,用以接上牵引杆以便在地面上% }5 V) o* f6 h 动飞机的部份。6 g+ O6 _ @* j1 l/ [9 ^8 B 轨条,, D! @* M: l# W( g9 a$ }4 x 迹, . @1 ~, n4 q' l形容飞机航迹在地面的投影。 # S6 L& e. l1 w2 J' O4 \! g, P空中交通警告与防撞系统, # D4 L4 m7 }, V6 I用来警告机组人员可能与其他装有应答机且在同一区 " C6 D8 F/ D8 L! S域飞行的飞机有冲突的警报系统。 - N6 ?, C) G$ v; L2 z& b后缘, % w! ]- r! Q, O, o机翼、安定面、或操纵面的后边缘。 0 ` W6 f8 w' p8 F# n" g7 J* X换能器, 9 y+ q$ x7 W. \- F能将电能转换为机械运动,或将机械运动转换为电能的 v; S# h6 j- l% `0 a 电气部件。 , w( J! Y' Y1 U: b- B: k$ |6 b转换齿轮箱,2 c. a( G, e E' ~' A; `; z' ~ 见Angle Gearbox7 e+ R! g# `6 P7 k! ? S3 `. v% ? s & ?, L: T, W5 l8 y4 e* t) R; oTOWING LUG, Pa; W# K* i0 H( |& n* [8 {, J6 r4 ] a ) ^5 W( w6 ?) t( ~( N5 |; a+ s; bTRACK (NO. 1), A structural member for attaching fixed ! Z9 D9 W4 l* j( p- u1 Mcomponents to, or guiding movable components 5 g9 Y+ s! \4 OT 3 S# k& ]' N$ |% A" b2 @projection on the earth's surface of the path of an8 d6 ^1 _- m% S; p airplane.7 z5 z$ K* Z8 I- c Z/ u5 k8 @, f2 d7 v 接地区标) O7 n% L' o. t6 u. v 跑道头端3,000英尺的最$ A7 v( p( b9 Z/ h1 V3 o 牵引环,7 d0 r" G. B; y& a- ^5 K b+ w- ]% K% [: l 用以接连固定部件,或引导可动部件的构件。8 | U% T9 Z8 D6 u- P8 }1 R3 J2 U: b# T9 y: [ 导航术语。 0 q$ g* w+ `* `5 ^! p# e3 O+ j' k) _# S9 `7 ~: S英汉对照民用航空词典B OEING/ |2 o/ u; B$ j: c+ R: X! ^: } TECHNICAL DICTIONARY 159 1 b6 v( j1 b: m oRANSFORMER, An electrical device which uses2 z3 v; k$ y; p* X8 R) B- d$ ^ RANSFORMER RECTIFIER UNIT, An electronic # F; H+ \5 a" ~8 C- Cevice for changing alternating current to direct current7 `5 g5 A: j& h* M1 N, x/ E6 F! H/ V supply airplane electrical systems. ( D6 D6 c. v7 Klse signals or triggering pulses) \6 q7 m0 U6 x" I5 f/ v* U7 ^ nd cause component breakdowns or failures. * f- f4 n3 _( y3 }3 WIt consists of a base, collector; J) u2 S& E& L; |" f4 Q" ^( g t2 h nd emitter. Two types of transistors are PNP and NPN. . T) {: i3 Q8 w9 i O. T1 ]) {7 ~3 H变压器,5 D2 V E: ]# Y9 Y 磁感应,将电能从一个电路转换到另一个电 ( j$ z* q' Z" E, ], Q) h5 S变压整流器, 7 C: k: A, o+ I6 W* M: C: p用来将交流电变为直流电供给飞机电气系统的电子装 1 Q: [5 Q$ ?5 f( |置。 3 f# ? f0 k6 N& X ^瞬变,5 G+ A2 p6 i* ^8 J! X9 y6 Z 信号或输电线上的瞬间电涌。这种电涌常会产生一些错- N/ | ^' r$ T, Z- a; z2 K 误信号或触发脉冲,造成部件故障或损坏。 " i& ]: q1 d" X2 d晶体管,3 J/ ?" w( U$ M) W/ H 固态电子部件。通常具有三极:基极、集( s% j' U# N# v& K2 e* T 极、和发射极。有以下两种:" ?% h) Y& _/ X+ ^( {# R% d PNP(正负正)基极电位低于发射极。 A" k, B' b7 _# J4 @( @8 l NPN(负正负)基极电位高于集电极。# x( X% r% k5 M6 ]% _ TRANSFER MECHANISM, A component for1 l1 c% Q7 g9 P6 s: h" ?' K1 X6 H transferring motion from one place to another. * g" k7 w' A) Q8 L% lT! i0 N) d3 A- W. U4 m electromagnetic induction to transfer electrical energy! _# b+ c. _; y9 o A& L( N from one circuit to another circuit.- v; t& P5 w" d# c T' x. N5 c! l6 b; A4 T% Z* H d % ?2 S4 F. @6 p& r' q9 `) B6 eto0 V$ M$ _9 {$ |" t, |9 r2 x TRANSIENT, A momentary surge on a signal or power 9 E' @ J7 K* j, x2 c4 L4 `line. It may produce fa' b+ j- Y @* Z* s a % C/ L2 T* T8 }# D/ jTRANSISTOR, A solid state electronic component for& p9 }) W. p: S use in electrical circuits. & P8 A/ m& K5 z0 {* Ea& Y3 A- q$ Q$ f: I1 Q 转换机构,6 i$ Y) Y* i0 Q2 s( N 将运动由一处转至另一处的部件( [0 T" W1 S) H: s" |% x 一种利用电! }: L$ p( P! i) j8 s 路的电器装置。+ W$ ]* _3 g" X$ N# _ 电路内使用的4 R1 m. w! C5 S4 [" ^. ?9 W/ y$ x% r3 Q, k" | 英汉对照民用航空词典B OEING/ N U1 Q8 L( V. C4 @ TECHNICAL DICTIONARY 160 & G* R! `# s; {TRANSITION, To change from one phase of flight to # n' b0 J- u% S/ N" K" JTRANSITION ALTITUDE, The altitude at which the ' K4 ]- E9 J' b6 W$ yltimeter setting is changed. ; `+ i- V8 W( CRANSLATING COWL, The movable outer portion of . y" {: c1 W; a; [& k3 m: |e thrust reverser cowl which is operated during# j7 q9 h8 V2 V6 \# |: \4 U- m verse thrust. $ N, y7 G4 {$ ~RANSMITTER, An electrical component for sending 5 B, a6 b6 D$ j" B/ T7 w6 b% b: E* Jformation from one location to another.8 D9 D+ m Y) g y TRANSPONDER, A radio transmitter-receiver which: }& t1 s) }; ]3 X- Y6 d2 i$ V ansmits identifiable signals automatically when the, l- T2 ]+ }1 n TRIM, The adjustment of engine and airplane controls5 |7 S: C6 V$ A$ T7 S7 T 从一个飞行阶段转成另一个飞行阶段。9 Z+ j, H( |' O$ K6 C2 n 过渡高度,9 |; ?! P4 H) t) w5 J6 e% B 改变高度表设定时的飞机高度。 $ M# ~( W1 `; w& f! d0 ~, d) E平移整流罩,( A& [' n( o/ ^/ {8 G5 g 反推过程中使用的反推整流罩外面的可动部份。! g% F, C& E; U p8 { 发射机,1 [6 b/ H7 _5 M& l1 {8 O 将信息从一处发至另一处的电气部件。! w+ R u+ |3 q 应答机, , O" k; _7 |8 E7 m u在收到合适询问后,能自动发射可识别信号的无线电收 2 L. @6 v2 Y2 j, T发机。 4 ]$ V- @; L6 i. C0 K9 C: J平,- j' a0 G! I& ]# L 动机和飞机在平衡的状况下工作而做的发动机 0 R9 S# p; N Y8 f. Qanother. 8 I3 b* Q1 N$ v2 L, \a8 @" t/ l% q, F) _1 R% D5 k T+ I$ i, Y4 J$ h% Y$ k$ P th * ?' N5 E- B- mre G5 |) _8 g5 d1 L, t: m T - S/ w! g1 }% V0 G! Uin2 h5 }% v+ }- [, a) s tr, g, k; P' o" H proper interrogation is received. 6 C2 Q9 F0 W7 {8 i( G% i) Cfor a balanced condition of operation. , M" w+ q6 m8 z" ~& n9 r过渡,$ j; M, o6 V7 s: p9 D' ` V# e2 C: |' c9 j2 ]3 ~$ R 为使发 + w: n3 q9 W# p$ O9 x和飞机操纵系统的调整。 . c% V- R' v' v$ f; I; x( s; H! @英汉对照民用航空词典B OEING/ [" C& ~3 U l6 X TECHNICAL DICTIONARY 1612 a( G+ {) N4 @ TRIM TAB, A small hinged movable part on the trailing 0 a! [" g q" @: h, y9 P5 V8 A5 ledge of a control surface (aileron, rudder) (see TAB). 3 G2 E! u7 V; j1 n9 iL, The total fuel consumed from brake release. h) d1 Y+ o/ F0 @ through climb, cruise, and descent, to landing at5 @2 J3 U6 F+ u1 e5 K/ I7 g destination. " n0 {) E' q2 `+ ^ cRUE AIRSPEED(TAS), The actual speed of the$ u C3 d% u. p" [( X aircraft in relation to the moving air. The true airspeed is # Q0 G+ t# b* I. k* Eated airspeed corrected for position% f w2 ^1 ?+ Z4 P& K5 ^ rror, compressibility, and temperature effects." U* r% m, ]( e: ?5 Q" a( x# O t ribes 5 ]: K$ V+ m' Z; Y+ K$ Pthe output value for each input Y4 E K" F# X( m/ ?2 oombination. 0 S1 x# b! b% Y+ j铰连在副翼和方向舵等操纵面后缘的可动部份。$ T7 @+ E9 ^3 q 航班燃油, V$ z; @; P5 O) \一个航班由松刹车开始,经过爬升、巡航和下降,到 ) L6 D6 [% { S目的地着陆为止,所耗的全部燃油。4 |! \% Q ~9 d- U# Y2 }! m 变压整流装置,. G- V& F" j: f 见Transformer Rectifier Unit 0 H* ^& K& W1 H, yTRIP FUE3 X. l1 q- l. D2 ^5 c$ C) a! u TRU, SEE -TRANSFORMER RECTIFIER UNIT 9 R G; l9 W) X1 O5 |. TT % _+ e& ~# F3 j1 |6 Fequal to the indic$ N9 ]$ U# Q: R9 n9 M! k e * Z+ Q/ L9 `. FTRUTH TABLE, in digital logic, a table which desc 5 u5 A6 H, d7 u$ M; K6 Ba logic function by listing all possible combinations of " ?0 |' V' U' qinput values and shows$ h! @& H( r1 q6 q f c 2 e) s2 t9 y6 d5 |% G- A配平调整片,1 j9 f& {* v$ o, T: T% V) Z" I0 C V" \* y4 S. I8 M% l& l0 b: Y0 e) v, w5 e真空速(TAS);% s( c+ Y" H: ?5 y" Y* u 对于流动中的大气的实际速度。由指示空速经过$ R- g0 c; j5 y3 S3 u 真值表,* n; h6 b/ S- w 数学逻辑中用来表达逻辑函数的表。该表列出了所有可% B; }& c( t$ {+ s, F, X 能的输人组合,和每个输人组合所产生的输出值。 " k5 z' u. x' k飞机相* c6 C7 z; r# Y4 s) _ 位置、压力和温度校正而得。 ; _( v9 _2 j8 l' A. g! T英汉对照民用航空词典B OEING$ V" t+ }" o8 K1 h TECHNICAL DICTIONARY 162# o) Z+ z' K1 O TURBINE, A rotating part of an engine which " T# Z* [/ t& a: s! |2 C* rkinetic energy from the combustion chamber ga+ E3 _2 ^- [, b' Y$ f9 r extracts) r* [2 S' g% y6 z0 a ses./ w' E( p- Z& t his energy is converted to turbine rotation which $ M3 s+ Y+ D3 D9 R4 d! atates the compressors and fan through a coaxial ' n% z: t9 y* p2 p. L: Ghaft.) r9 e: ?* G+ F& `' H/ m TURBINE CASE COOLING, A method of cooling the( o) I' d$ c# I q- K0 E' i ngine by using fan air. This cooling process is used to) U- @# y+ V6 J- C5 e' v TURBOFAN,7 A) ?. R6 G2 ]9 D5 R) N( h (1). A jet engine in which the first set of blades is a 7 _$ S7 L. f7 Y0 E' g+ L% T$ b+ Alarge fan." Q+ x5 r% \4 G: Q4 e+ R (2). An air driven fan/compressor used in air% u9 O* C4 T" x) Q1 p conditioning system.0 C8 v( R1 B0 \ TURBULENCE, The movement or shaking of an ' K2 U5 K! J; W; u) Nairplane caused by unstable air masses. 7 U) S6 {# ^# j/ Y: C涡轮, % W" z! x! p, U- C! N! H% P% A, ~( \ G发动机内,从燃烧过的高温高压气体中撷取动能的转动 k$ m4 c; _' X- G( n) B f; @ 份。该动能使涡轮转动,涡轮则经由同心轴带动压气机7 B! p$ i9 O* S; W5 ^0 } 风扇。 ^3 m; f8 G! P& X 涡轮机匣冷却,/ T. W! A, V" K* n1 L* w 用风扇空气冷却发动机的一种方法。该冷却过程被用于# p# r; {3 J7 A7 I5 y% j/ ~ 效率。. k0 M/ T, r# m# I' o I0 S. x (1).第一组叶片构成一个大风扇的喷气发动机。 * q0 Q1 s! e. s5 ^* q% J(2).空调系统内的由空气驱动的涡轮和压气机组合。5 t9 y! ^" e) O- o2 c2 D& j 颠簸, % G, P. R! e2 |; `$ ^# {由不稳定的空气团造成的飞机运动或抖动。, Z3 G6 Z5 l! N T3 k# r0 d8 d( Y- l6 e3 Y8 V$ J. C4 \ ro5 k6 [0 P0 S' h; j5 D7 ^# q s 2 J( U6 V' t# `: we" F9 [. ]+ {& |8 V8 [ \! K7 h) i increase engine efficiency.5 l8 B! i8 a% e9 Q8 i: a6 c/ N4 h3 ]# V4 \1 f |# X+ f* t0 N* W5 _: P/ Y$ c3 @提高发动机* g$ g+ W; C" r7 J) h9 ^ 涡轮风扇,' |: T+ I& ^8 @# D4 S/ g 英汉对照民用航空词典B OEING9 J+ o/ j1 o8 J, u" e( l. @ TECHNICAL DICTIONARY 1637 |* q0 m: V4 Y TURBULENT AIR PENETRATION SPEED, A speed ! R; `5 U+ i/ B0 A. fthat provides adequate maneuver margins when flying : F' J7 ^% R( _to unstable air masses. 8 k' D1 `) K% p; a0 \" P. }4 Jht" U$ p# q6 p6 Y! ^" K$ j9 e( ? stment in the control' v' ? H/ s4 C, F" y* S ables. 1 H8 b% c7 P- ]% P7 L! V. ~+ MUHF, SEE - ULTRA HIGH FREQUENCY- G8 D, N: B2 } NDERCARRIAGE, SEE - LANDING GEAR# p5 y [; M/ z( E$ @ UNIT, One of the type, a single component. ( y4 p- `& Q+ u6 V: |- XUPLOCK, A mechanism on the landing gear for keeping " Q) b' B8 u$ v; \/ j* A- A Fthe landing gear in the retracted position in the wheel 8 w( I1 a& Y1 ~3 c! N6 x% dwell. 3 A4 [( D8 c" h速度, " H6 V/ c$ ]( U; ?纵裕度的速 1 O$ T0 g/ j$ `/ n' U$ s$ r0 Q! ~' d! A5 P6 O5 [- {+ f2 _ 调整操纵钢索张力的 3 |' Q& f# f$ z7 B; S" V4 b械装置。 + O% [# S! o6 @ W7 A高频, 1 _7 ~* x% z' ]6 M见Ultra High Frequency9 M0 F: w6 m- W8 l6 E in2 h G2 E5 g' p TURNBUCKLE, A mechanical device with left and rig $ |( {! }+ K: H; w, L* b8 Mhand threads for tension adju9 X: G2 h* i" v5 [9 u$ S c: X$ V1 i: \; c( o0 _ U 7 [8 M$ u j( t3 e8 T- o8 O$ xULTRA HIGH FREQUENCY, The frequency band! a& W: X" d9 N- Z% v. R( }: x between 300 and 3000 MHz. ) I2 H/ H3 Q8 }) j7 c8 M% mU1 u) y# V( g( D3 {0 }/ h 颠簸穿过7 o8 @ [( H, ^5 K 飞机飞进不稳定的空气团时,提供适当操 1 y5 v Y* \: L- F5 T* M' g$ X! A0 `- _1 Y( w松紧螺套,' H8 M1 t( |, i! i 具有左旋螺纹和右旋螺纹,用以" |- M' ]1 h7 U/ Y6 x4 E, @3 s3 {6 n9 E& _7 K5 I3 E' @! z, G9 ]* W+ {超高频, ) c* T* Z+ `( e8 q频率带在300 MHZ至3000 MHZ之间。8 f2 s! I5 W/ K$ @7 F: o0 Q 起落架,8 O* A# y& \# U* G2 J 见Landing Gear 9 n8 d, _# q6 @. k- D2 Z单元, 3 O; x8 G) X+ T某一类型或某一部件。 0 y5 Y1 F, Z3 m k: y上位锁,8 [/ i; M+ [4 ?: O 起落架上,用以将起落架保持在轮舱内收上位置的机3 k% U0 {7 B/ M! {* g% h$ I 构。 2 s+ P( e& v. [8 z4 r英汉对照民用航空词典B OEING * O5 q8 x) L d, S/ [TECHNICAL DICTIONARY 1640 j. \ g4 S" ?, l; J9 D5 o' G UPSET HEAD, The head produced on the tail of a rivet % _7 J' ~$ f4 k. {1 W: i. x* Y2 jduring the installation driving process. (See 4 Y7 g- a- Y) B+ G5 J- cManufactured Head.)5 _$ P+ k$ H7 }& P 1 (TAKEOFF DECISION SPEED), Is the maximum 8 d$ e9 a# v+ z/ [5 {+ Q5 Q Opeed at which the rejected takeoff maneuver can be 3 ~' w- W$ r; l3 l# @% h6 Q( C' v; {itiated and the airplane stopped within the remaining5 {9 X; q5 j0 x/ F eld length under the conditions and procedures defined 4 H6 [3 H9 E) S$ Kthe FAR's. It is the latest point in the takeoff roll where " l3 ?1 g% }6 |- Y. {: lstop can be initiated.8 d% x! D9 q: T- a ssure : h, Q# p! C( G! g8 }7 B! T' |+ pdient capability and maneuver margin. P$ u! Z/ L% ?" J3 pVACUUM, A negative pressure or pressure below2 Y% R1 E: g! V& r* j: U atmospheric, measured in inches or millimeters of8 V- C9 c- [3 a5 j7 r+ u2 U( S- d% o ercury. 1 f" W- K. `0 _4 B3 P! b$ eis & X/ i" `, g0 Y/ MVENT, A small hole orifice or restrictor in a component * b0 i X6 v# `! o7 y7 `" V5 Mfor allowing pressure in the component to be the same' O- ]0 ]# i$ j) A# e as ambient pressure.* i2 }0 V- Q8 @7 { 在铆钉铆接过程中,铆钉尾部一端形成的凸头(见3 ?6 |9 Y; K7 s Manufactured Head# l- v- V- J! K) U" m6 K& S" ? V 6 |9 ~# S ?- a% sV, R6 d0 `* `( I s : L q- l* I6 u- y+ D7 @1 tin+ l) T7 s. ]& Q0 z4 _ fi 7 f& I# s; J" ein. F% Q* E. a+ q# c9 d1 } a0 R: \8 a. t3 J) f' \ V2 (TAKEOFF SAFETY SPEED), The speed flown after: A0 u$ A0 F8 h takeoff during engine-out climbout maneuvers to a( O! M6 I3 Z2 P/ w: w& f! L8 Z adequate gra / F5 E4 M4 g' ?0 om( k' P$ i) w! e; u- ^# n x6 N VAPORIZE, The mechanical process in which a liquid ' J8 w- c1 B# nchanged into a vapor. - Y: b, b+ D. E% F. zVECTOR, A heading issued to an aircraft to provide : [' d: c: w2 ^# L% z3 D; i1 snavigational guidance by radar.( C, o( K7 y( b$ G6 Z 铆钉镦头," V+ ]! N* E# w+ B4 {3 p )。 - D' z: z7 K" o. {1(起飞决断速度),: E; E& p3 y7 _# I9 | 根据联邦适航条例的规则和程序,飞机能进行中断起飞' _5 s9 X8 j4 d/ ?9 B2 c5 I 在剩余场长内停止的最大速度。它是在起飞滑跑时仍可 0 n! q; Z ~. K8 V, j1 x住飞机的最后决策点。 . k- [; ~: y$ b# T6 d/ C# W) p2 ~速度),& m# U" _, X; o8 D6 C u 在一发不工作起飞后的爬升中为保证足够的梯度能力 * H; c( ]% O; @% ~, h和操纵裕度所飞的速度。 / x0 z$ D8 V( \+ j若干寸(或若干毫米): i0 M, A* J8 r5 w 汞柱。4 l% s" `' }; E; V* W4 _8 B" j 蒸发, . t2 r2 E* K4 c% u- F+ [% W液体汽化的物理变化过程。" n7 w2 ^6 s1 h5 z Q5 h9 g. |3 }" T) L 引导, ; m! _ B7 Q. X6 ^9 r- Z; g/ X由雷达提供的航向,以给予飞机导航引导。 2 |: r9 [; y3 f: }+ s+ o A) s% }: j通气装置, " z7 u$ ?* C6 ?. G1 ]部件内,用以使部件内的压力与周围环境压力相同的小 5 N' K3 `8 Q. X; g J1 _孔、或限流器。; k' L7 {" h7 v' i8 h+ ` V & x! B3 z$ @* j8 G P" ], M* Y( K2 \( O. m, ]- G7 z" ` V+ f, ?0 i4 N! {V2(起飞安全 3 O/ g5 g [- e& G, C真空,1 F" G% G; F, E$ | 负压或比大气压力低的压力。常用 ) b5 N1 J @* w3 p4 V, k英汉对照民用航空词典B OEING! M+ ?- |& x9 E4 } TECHNICAL DICTIONARY 165 5 Q; R. e' [- w8 ^- \1 C& q: JVENT SCOOP, An air inlet/outlet on the bottom skin of. K {2 B. z( a/ Z% Z4 g ir ! n3 M {" B4 c) F" J8 i9 VVENTURI, A part of pneumatic duct with reduced flow # I9 e7 c" _2 A9 z% M) Zrea for airflow measurement. (Principle: As air velocity 6 y* F: B: |8 F2 r# ^5 x6 vcreases, pressure decreases).$ V! [9 Q! u6 r! D, \ z ERTICAL AXIS, A vertical axis passing through the- h* p! X' ~3 l% h* K# ` V airplane from top to bottom. Airplane left and right - P* y6 G% ~4 y2 u- c6 E# Qtrolled by the rudder. 2 z6 W* T) N* }VERTICAL NAVIGATION, Functions which provide : {) _7 E; v9 y' P! c/ v1 X0 Rguidance signals to control the aircraft during climb or% r) t2 ~. U% G2 k descent.6 C& D& Q1 j& j$ g7 i . * M% M) U$ Y. p% M通气进气口, 0 r$ _- w3 v% S' S6 p位于机翼下表面蒙皮上,用以燃油箱通气和提供燃油箱 $ |% l8 Y9 C6 o x内正气压的空气进出口。/ D% e- g" E" t3 L 文氏管,3 @3 ]: ^- {& s9 C3 W( @9 |5 w 气源导管上,导管截面变小以量取空气流量的那一部 # j- |9 M. O( M7 q; D% i, e i* w份。(原理,导管截面变小时,流速增高,压力降低。)' x, f% `/ {, r& d9 s 垂直轴, ; ]$ L8 |# ^+ R4 R. [8 z1 Y8 j9 @8 G由飞机上部至底部的垂直轴。用以操纵方向舵,使飞 4 h) J6 _# V: _9 l6 ~& E右运动。 6 f" Z& y4 ^$ H: ~- ~& f直导航, 8 Y& B0 w+ V+ e7 A- y% r0 D' {& R/ S5 o& Q* w the wing for fuel tank venting and supplying positive a $ _8 D! z- A- A( t. d1 jpressure inside the fuel tank.( _ {4 V3 C6 x" M6 |/ F# [; I( e a ; W0 B1 v7 e Q. e# ^0 vin / a7 ^9 j% v+ v2 U1 wV 2 j ?. B! \6 c! h7 D9 x: emovement con9 w+ \$ X# Z9 ^2 ^% x VERTICAL SPEED, The rate of change of altitude & y: Y5 E5 I5 c# J D9 D7 u* j机沿此轴作左 8 l: g0 I! D$ x$ d( w0 P- _& p# N( J# A% P 在爬升或下降期间提供引导信号以控制飞机的功能。 7 ]" O- `, h3 u" A& J; {+ Y垂直速度 # b8 O2 B0 x% R1 J4 \3 ?/ v飞行高度改变的速率。 " S5 n6 G9 e6 G/ G4 f- u9 Y英汉对照民用航空词典B : D* Z) Y* B+ iVERY H 7 r, S7 K* b8 u- @OEING* y$ R+ u8 L8 F0 ^ TECHNICAL DICTIONARY 166 # Y3 O5 ]2 K2 d KVERTICAL STABILIZER, A vertical surface of the 8 d E7 H& k6 j2 E- @empennage for stability/control about the vertical axis. 7 [- A0 B c. M( dVERTICAL TRACK, A climb or descent profile. . c" q0 H N+ |# [: M8 {( w& ]IGH FREQUENCY, The frequency band9 k6 F2 A; S7 R" Y- C$ I) q/ t0 ` VHF OMNI-DIRECTIONAL RANGE, A navigational. q3 R: d4 E* v$ ~5 T6 U system which tells the airplane's bearing from a VOR 6 C# D! O% x- {/ p6 ~0 D. kround station and its deviation from a selected course 9 e$ z, F( c# B% p* A7 w/from the station. / V% a. x9 w. F2 R! V, u) d+ TISCOSITY, In a liquid - it is the resistance to flow.) U+ t6 \% q& V% J VMO, The maximum design airspeed at which the 9 Z- D6 G' z' k! P& ^airplane may be operated.# {! |9 a3 l/ g6 U; G 在飞机尾部,用以保持飞机绕垂直轴的稳定性和控制6 z. z: V5 K4 N t) @! M! N 的垂直面。' T% J; K: \ _ O; T4 e 垂直航迹(VTK), ; b# a" @- A, c$ U7 u# e/ a爬升或下降剖面。 , H$ J& q% J e甚高频, * M, O9 y0 k% L7 j+ j30 MHZ至300 MHZ之间。between 30 and 300 MHz.) C2 n, a. J8 i0 W# C8 B VHF, SEE - VERY HIGH FREQUENCY : c6 n! P/ k3 Dg ' S' d1 J! t+ I- c+ v. sto ' q6 {/ J2 O! a9 w4 XV# K- j& t: O% u 垂直安定面, 8 @- q& Z3 r, b0 [3 w# ^, h3 e频率带在 4 S$ r1 r9 s, j7 b- h3 T2 y甚高频,6 u! f: {9 G9 e 见Very High Frequency 0 k- w9 m' e. v* B, Q甚高频全向信标, " D' `7 ~7 l4 E系统。该系统可提供飞机到VOR地面台的方; P C+ w! ^& |" D 位以及飞机的向/背台飞行的航道偏离。, M" q0 x/ j; N; d1 z 粘性, 4 e9 \7 ?: F2 b0 q/ B# V液体中阻碍液体流动的阻力。 + v0 r. m5 F/ X最大使用空速,; @6 Q% V' M- \1 W, X 飞机可使用的最大设计速度。 9 @# ?: z/ N z" F+ |6 j* T3 C一种导航 9 w2 R4 S2 P( D- F1 @& n( Y3 z y英汉对照民用航空词典B OEING' I+ `) _. ~1 {" r& e3 q4 w# T TECHNICAL DICTIONARY 167, ^7 S7 f/ a3 r8 D: e$ d VNAV, SEE - VERTICAL NAVIGATION & P6 P# d2 d; a# }! {! G& ^5 D/ hVOLATILE, The ability to vaporize readily. 9 S' I4 X! J# ^LE MEMORY, In computers, a memory whose( J3 j/ m9 L# Y9 [' k7 H9 T# K1 k OR, SEE - VHF OMNI-DIRECTIONAL RANGE * ?! A2 X, c8 _1 l. i4 V- v( LVORTAC, A combined VOR and TACAN station.3 L. O1 [" ?( J) v/ o ORTEX CONTROL DEVICE, A small airfoil on the. E' r! g6 z+ q. } acelle for improving airflow between nacelle and wing! @* E4 H2 ?: T+ r6 k6 g O leading edge.' V) m: {1 Y# J( _2 } VOLATI# B$ r5 c+ `4 {/ q contents are lost when power is removed.. h- u& x7 X& V' e! u9 f$ g; B VOLT, The unit of measurement of electromotive force. 0 ^! v, Q1 Q8 p+ J4 jV 1 d' M% }; B9 }/ L+ P: K& L) kV 5 z' Y) L7 z8 C6 w2 ^& in ' h/ Y% X1 I* Q% N: d- b垂直导航, 2 F, |. t( T, ~; W1 f见Vertical Navigation.' K# p2 ~3 E. \- u' ~3 U 易挥发的, & w# s- j3 t+ R3 |随时可以蒸发的能力。0 z/ m) K( A( L. [. `( ~ 易失存储器,1 Z) I. w0 f+ J/ T0 m- u. ~% J( p9 q: u 在计算机中,失去电源时存储内容便丢失的存储装置。1 x* `6 m+ e' R; _ 伏特,% d" ?' g& Q& s" | 电压的一种计量单位。6 H9 j g9 @: J3 d( E 甚高频全向信标,; p4 `* D; [$ a5 b; I% [ tional Range 1 v3 f+ r/ y M* o: N见VHF Omni-Direc .1 B0 q; s% x# Z' P! o* ~' e& t9 t+ x VORTAC, 9 z# x, U) a# X2 L7 ?$ K3 Y. ~兼具VOR(甚高频全向信标)和TACAN(战术空中导 ; v3 v+ q/ r! D& Z* a& ~航系统,或称“培康”)两种导航设备的导航台。1 P) E- s# [$ ]1 ? 涡流控制器, 1 Z9 A6 J) p4 D2 g发动机短舱上,用以改善短舱和机翼前缘之间的气流的. l2 ], Q1 T6 ^0 i7 R" t; l 小翼片。 X4 C7 g0 e5 ?1 z6 k6 Q! D 英汉对照民用航空词典B OEING8 J8 M2 z# {0 D7 F* v! t% d TECHNICAL DICTIONARY 168 3 V8 {* a" }6 d7 F n) \VORTEX GENERATOR, Small metal airfoils, located on " V( k. T, [- S( U. {9 @8 p1 E! s4 fwings and fuselage for delaying separation of the air' w1 I( t! I2 b. @/ f ating local turbulence % L) @! W0 a8 ]4 F1 o+ H- Qortex). w8 D! X* t; y$ m/ y! J5 p35 . d- c2 C( O6 p' a" w# j9 \* [stall speed in the landing configuration. 1 e- Z' T8 E$ u* N( A: {装在机翼和机身表面,以在气流中产生局部紊流(涡 % ?7 I( a3 o6 Q" P6 A$ @" l流),来推迟气流自表面分离的小金属片。 4 F) y" |0 P& W8 I* l: @3 N度), 5 |7 h2 _. ~( ~, R, r$ }* f" U在着陆形态时的失速速度的1.3倍。 ; e, l5 r4 U8 t7 h见Vertical Track& b! B+ x4 O8 t. `' C' K% h! A flowing over the surface by cre+ `3 A0 t' W5 }, { (v9 L( Z/ }5 s6 d, W$ ^' a% j8 D9 L) E VR (ROTATION SPEED), The speed at which aircraft 7 v( h7 g7 X% p5 y2 orotation begins in order to achieve a speed of V2 at , \, _+ _# Z( ?2 v: A* [feet above the runway.; a/ c3 u% o/ M% o VREF The reference speed at the 50 foot height in a ; R, R ]6 l5 t: W2 f: g" j! Lnormal landing. This speed is generally equal to 1.3; q( M$ C+ G0 T- m4 u times the }' {4 a- X8 T' ], y- {8 e" r1 gVTK, SEE - VERTICAL TRACK0 u3 T" n9 [: [9 O; k0 Y+ G2 t" E9 u# { 涡流产生器,# {, N& e, r) k VR(抬轮速 ; z% Z) H& S6 r4 s在该速度下飞机抬轮开始以便在跑道上空35英尺时达# b w. b, u7 E" Q 到V2速度。 6 _8 n# {6 @" ~% f, D* G* kVREF, ) R4 R" G8 E0 b+ {飞机正常着陆时,高度50英尺时的基准速度。通常是飞8 _, p0 n' e2 }. V$ |1 n1 U6 x; U" c( q垂直航迹,- Z; B: f! R. V2 ^8 ]7 p2 T. ~7 N5 x, j: {5 _* K1 a, ^ 英汉对照民用航空词典B OEING+ c+ [6 d: v! K' ~) x TECHNICAL DICTIONARY 169 * l4 c1 c1 b1 sW$ E: [+ g- l* ^7 u {% V" x WALKING BEAM, A mechanical component attached to * D3 A* \5 ~" y- A; w9 S: W# G3 Gthe main landing gear and a hinged support which helps+ [. f5 K# d3 H( m9 K2 r0 g the actuator during retraction of the main gear. ) D$ ?0 j4 u% H- i9 t: rATER LINE, A horizontal reference plane along the / n, L6 z6 r0 m8 ?6 efuselage for vertical measurements of the airplane.5 Z; H" }+ e( C' j( U WATER SEPARATOR, A component in the air5 _0 S3 _( O2 E3 j) v, c onditioning system for removing water from the air! f* w+ o) A( q2 _) T. u4 Q- O& B, X 动梁, 3 N! R+ B0 i5 _: \0 Y2 j主起落架上,一端连在减震支柱上,另一端连在铰接支 - o3 A: w, s$ N; ~$ V0 G( m1 Q: S, |6 J撑上,用以协助作动筒收主起落架的机械部件。. |5 J9 Q, P; C 线,( ] \5 a$ y6 M6 J* t 沿着机身展向,用以量取垂直方向的距离(或长度)的( N- t* H* m! ]5 D4 l7 X, | 水平基准面。/ v( l; |6 G' [6 I2 h 水器,9 S0 g1 |, W D0 Q5 q 空调系统内,用以在空气循环机的空气下游除去空气中& H7 S+ [) F8 N& A: Z2 r W 5 v. h+ R9 W4 A6 Bc ! v' v6 x( S. d9 qdownstream of the air cycle machine. % V5 ?' x! F# Q3 Q) {; ~2 v0 q) z2 ]7 s; }1 ^+ ?& A- Y& \4 {) O的水份的部件。+ f# \" ?+ g; b! ^ 英汉对照民用航空词典B OEING / d2 I) ^; g y! ?! `& \TECHNICAL DICTIONARY 1706 }' l- ?. j+ _9 E' u$ h* y WATT, The basic unit of electrical power. , f, s8 k. E! W4 q7 H+ WWAYPOINT, A predetermined geographical position $ b5 V7 t3 j/ M; tused to define a route. The waypoint is usually defined+ r' m7 h) h) l: ^* L( [ in terms of latitude and longitude. ( C3 b' ^+ |, ~; A lWEB, The portion of a beam or channel that has been $ N8 G1 f0 _( w4 ]; f" y! V2 q+ }; Iinstalled between the top and bottom flanges. Its prime, F) ?+ a8 r$ S, x7 } purpose is to furnish strength. # l+ L$ {1 l l% WWHEEL SPIN UP, Rotational acceleration of the landing( k- [ j; Y6 N* W6 u3 w2 n7 u f the 0 ^6 E$ v8 L) |# K7 x$ W8 a4 Xnding gear (undercarriage) after retraction.: h8 P) f& u/ x( y2 s! \5 h 电功率的一个基本单位。 3 B, I0 N5 n$ @- o' b0 U- m位置。通常用经、纬度来表示。! o0 M# c& w7 n3 C3 _; M4 O9 l) H 腹板, * p2 f9 L% [( X梁的横截面。常见于上横梁与下横梁连接成工字形。主 . y6 {0 y, n6 R" e# E( [要作用是受力。 , _; v1 `. Y0 M( Z. j1 T/ ]* a4 q轮加速,$ C- G3 P0 Q, R, X$ I0 w 飞机着陆接地时,起落架轮子的旋转加速度。 ' ~1 [. w4 ?; H- r: t轮舱,5 } P' c1 v9 h# v 飞机的一部份,用以在起落架收起之后,收藏起落架的 ! Z& E& H- ^4 b* z# {7 s那一部份。' u, R5 J- A9 t gear wheels at landing touchdown.# S7 K' }" |$ u WHEEL WELL, A part of the airplane for storage o 0 {0 a( ]/ V) ^$ s |' G/ z; ila ; ]4 H- U! N4 j$ V( |瓦特(瓦),* h4 q! L! _) l* ^( @# q" k 航路点,6 y Y; a, P2 Q4 S; t( a% n7 n' N. P7 U 用于决定航线的预定地理 & k) l' M1 k$ y& ~( i; A7 I; s, ^/ V# K! | 英汉对照民用航空词典B OEING ! p! r j' G" t$ ^, OTECHNICAL DICTIONARY 171 & w$ l- k% h0 w! l5 {# MWIND COMPONENT, The effective wind relative to the* F2 Q% T1 u0 N6 R- ]' i2 K9 x9 t horizontal axes of the airplane.9 X" E) `. H" ~. d WINDSHEAR, A change in wind speed and/or direction 1 L: ^' n4 N' D' j- Pa short distance resulting in a tearing or shearing9 q7 z1 V I( G$ b7 E effect. It can exist in a horizontal or vertical direction and ) D2 p7 l; c6 doccasionally in both.2 e: b: q [; g& x/ n2 d1 y WING CHORD PLANE, A reference plane from the tip 1 K7 y& n! f$ p8 Q! q7 pof the leading edge to the tip of the trailing edge of the - x' m; E: a; \! i9 v7 Cing.! B* m( j* @7 I# U ING GEAR, The landing gear attached to the wing9 ^, _8 @; l Z8 x( k tructure. - u, H* l* V2 _7 z( V+ @& L ]" y/ xING ROOT, Part of the wing which is attached to the 6 C8 t) u8 p+ [* k* v/ w% @1 i @selage.) I* r- z7 |( H1 D WORD, In a digital computer, a word is a group of bits4 |2 k# b2 {' ^; C8 S- r with a specified length. The typical digital word is eight1 y( l; L1 u r3 S7 a; j bits long. 4 H+ D$ C- @4 D# i9 g ?风向量, & Y% H/ [' W" v& e3 t. m( z4 o相对于飞机水平轴的有效风。 ) o" Y4 c- m9 y; [; h q风切变, I; w8 r" D$ Y6 ` 短距离内风力或风向的改变而形成的撕拉力和剪切力。 : r# u% y z1 H( w! M0 T0 ^$ D可发生在水平方向或垂直方向,有时会在两个方向上同时( o! a9 V! t8 ^* R: G 出现。$ z6 a4 L+ L; D 翼弦平面, $ K, }. e2 K- z& g# G8 Q通过机翼前缘顶端和后缘顶端的参考平面。 3 u3 e( Z f. N) V% k翼下起落架, 2 }1 a9 D' H, b+ c' w4 o) [1 r接连到机翼结构上的起落架。5 D& e8 s+ v6 K5 `5 b! o2 P* b 翼根,9 q: o4 S0 i; r a! T 机翼上,与机身相接的部份。 8 A, d- U/ s$ `$ b1 z+ B4 W) X) _字, % S" }. s! D* \* r" o. G在数字计算机中,一个字是由一定长度的一组字节所组 + i8 d# ?+ w1 C成。一个典型的数字字,有8个字节。8 V9 |+ I+ n5 |' t: A9 D8 V in - }. I' U9 w1 \( D* a; L2 C8 U+ e# Tw' ]+ j1 c& u0 [9 F9 P W5 B6 E* X: V, K4 [, w! `1 H s# }( Z8 D& l H) d4 [& ^; w7 S W# [. W2 T/ ]- |8 D fu! g, q8 _: M2 P4 o6 v 英汉对照民用航空词典B OEING' J4 M6 w% p: v5 ~9 B7 K* ? TECHNICAL DICTIONARY 1727 J: ]/ x2 \) h" O WRAP AR1 c! V! n. X2 c5 S computer's/ L2 {8 z6 O0 @* b OUND, A BITE test comparing the$ U$ |5 ~- \3 t- Z output signal with an internally stored value.+ U1 z; T7 a2 A: \; F XTK, SEE - CROSS TRACK( E$ b. f* Q- j8 Z. D4 z8 s AW AXIS, A vertical axis passing through the airplane. s. o" p2 h! i0 U$ q from top to bottom. Airplane left and right movement$ M* P+ d, R% g8 o- W2 c" O/ t controlled by the rudder. (See Vertical Axis)., w5 o# ^9 P3 Q. q, h AW DAMPER, A system that is used to move the 0 w1 L+ V/ U! e" l9 I& ?! I( `. x; L2 _dder a small amount to oppose airplane yaw. % y0 C$ I7 T4 U+ C8 X' L8 ues 6 \1 k7 t d" p& i回测, ; L' I1 b) r; i5 E8 c自检系统对计算机的输出信号和内部的存储值进行比 . A( I9 G* V6 @/ k: y较测试。$ a, F- g8 X1 T 交叉航迹, . \! W) _: P* X7 h4 y% G; H5 |) [见Cross Track , G( E4 M9 W0 l& n! E" `X. l, J' F6 Y5 u5 Q1 G$ T2 d$ L. m3 k( w! ?+ G1 G 偏航轴,3 A' \" V2 E$ H( K e8 x 又称垂直轴。由飞机上部通向底部的垂直轴。飞机绕此9 s P/ j9 N/ |- K$ b 轴运动即造成机头的左右运动,这种运动是由方向舵来操4 {* R% p' E" I$ c; c4 V5 g 纵的。 " Z {5 O9 H8 [' N7 t偏航阻尼器, . _! | D6 S2 Q3 r$ M; c! o用来少量移动方向舵,以抵消飞机偏航的系统。 ; D1 a/ u& {% z! I- A" n5 W/ e( P飞机绕偏航轴运动的速率。5 Q2 D( i2 q$ v Y4 P7 l/ p9 F9 i5 a Y 3 M+ q0 S! z' D% I5 ?( [Y 9 A, P8 K1 W+ @8 yru 4 ?% f2 C0 A5 g6 b4 p! FYAW RATE, The rate at which the airplane mov : H7 h8 Z! Z8 O1 t6 iaround the vertical axis (left, right). - P! |. B" D4 H0 e偏航率,! F, ^# _$ p* i/ Z' ?4 t 英汉对照民用航空词典B OEING / E; Z \" c! W: y& kTECHNICAL DICTIONARY 173( W" t9 v0 g% n; z) D Z$ L9 P; {3 v0 e& J% y ENER DIODE, A special type of diode which, when4 h" O! j4 v1 z' k4 N: F ZERK FITTING, A device through which oil or grease is/ a& w& Y. e; N% m: J, K upplied for lubrication of moving parts. 0 r1 `/ t4 Z# g$ q/ Q; a4 EZFW, SEE - ZERO FUEL WEIGHT 4 N! D U/ a6 o" v dZERO FUEL WEIGHT, The maximum allowable weight) R/ C" Q# }' @0 n excluding usable fuel.3 y2 u5 M2 s1 _3 s" ~ ~5 w. I( T 纳二极管,2 s4 e; V& [9 K. t& d1 C5 T 又称稳压二极管,是一种电子装置。正常电流可通行无 . _. S5 |2 Q3 D" `! O阻,但反向电流则必须在电压达到预定值之后才能通过。 " t/ S# u, u! j. H/ O2 ?- p0 Z在飞机电器系统内做为调压器之用。反向偏压时,它有一* Q4 T" ^' B8 u( b: ` 个恒定的电压下降。 3 \: a' U- A0 D* A) e" iZERK接头, ( M! i7 ~# v: v2 ^ZERK公司出品,用以接收滑油或润滑脂,以润滑活 ! S1 C1 S/ j! V. H1 q S4 f2 K3 b动部件的装置。, A( C% ]4 o: A6 [- h/ C 燃油重量,- C1 r1 T/ h2 Q6 o 见Zero Fuel Weight9 O/ @% v2 d$ k! T, ]$ I( r Z 5 p0 i5 M2 b- Y4 q6 [6 Y/ Greverse biased, has a constant voltage drop. This 7 q% ~9 Y% a+ c& ^1 W0 ]property makes zener diodes useful as voltage4 }2 \( d7 U+ `, q. @. C regulators. 7 R8 P; Y ?' {& Ls, C% ?6 x+ F9 M3 p. K! F+ D$ E/ ]4 H; u1 ~$ E. A* Y* [+ `7 g# u Y/ o& F% |1 B8 f- r6 ^ 无燃油重量, , f' n7 Y: |- Y3 L扣除可用燃油重量之后的最大允许重量。

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