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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' ~/ H
力
1 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$ g
.1 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节
% v) o& }+ v! ^$ t# }( _2 R: p; q燃" 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* O
燃3 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应; 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
全
- S( f' j8 h* D' Q4 i及
9 D! j1 C" v& `6 ^ {/ `9 `0 L7 N全. 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
表
) 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" B
.
9 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# ^% ?
元* _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 r
。
4 D' j6 k4 z- |) A由机械驱动,; n$ }5 }3 p2 x# F9 x; I( \
发: _3 |' m$ [. B# w
能将发电
1 w; |; { }! r# r万向架组件,+ G" Q3 n* p* ^- ]) O: x
两, U& o1 v# q# I! u: [7 p
动) ?/ 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 ]% `地
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% J
。
9 ~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
板
% ?0 s( d0 O8 {; y; Y! o下" s& X( N$ Z% U
确立的一条0 o W9 y& r* N" D( k) K% S9 h7 n1 X
下
/ 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# ^$ _较) H+ M! ?+ G3 u G! G
点
0 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
系
/ j# H G9 a& e$ o: [8 U. K0 t用, 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 V
则6 t9 W4 n. L3 z) q$ i1 b! ^" T
2
& D6 d! a* z, o. w1 b7 K# u5 n的
) L" o# B9 x8 S5 _5 l. B2 f& Q" o0 u全. }' 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 O
星
5 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/ [
盖
3 Z$ c0 r: q8 C9 Z* Z% B大1 j8 `8 |3 P0 t: |& V
起7 ^- m/ L! }3 Y5 g' b7 L. y
航2 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
地
' _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
地
/ 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( Y
航1 D) m/ I B2 y: k. S2 b
.
4 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; ]
热3 C! ?/ t" ]7 ^: s7 P7 ^8 K
流
) 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跑/ E" J" `+ Z4 C r2 G& V8 y
或
6 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区
% 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 }$ ]
频/ 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 o高
3 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
机& U) T) S+ n* E8 `+ U7 A
过! [* u9 ^# Y2 S# [9 S# D
设/ B2 `/ u7 V- ]) L6 C/ T
的, `, }- 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/ ]发. ?) g$ Q) y+ M4 ]
等# N5 Z" ~0 |% {
等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 `定
' h8 D3 X; y; o- k# P点
n2 T1 K3 X8 ^3 X& n蜂0 I2 ~1 ]& R! R
面
$ 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& n液
5 y! ~, `# v) M, c+ [* i' a泄6 m! x1 g* _) d6 Q' R$ C5 W
指, s0 O9 r3 w3 j$ r& @+ c
.3 ~* 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 |
点
& ] Y( ~! X2 o: c; w的5 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仪
! 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
改
' e1 ^9 D( I& Z: V能,尤其是在$ i% P+ X. u6 F$ Y7 `
指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 |空1 I8 |' o$ t# n6 Q- O
飞行中" {, u \( A/ E# ~2 t9 t6 b3 d9 C
内9 A" m, Q1 l0 D9 p! g& t
态和坡度的基本控) a( M3 r* \+ E$ o" z s6 @
英汉对照民用航空词典B OEING1 k& L3 r* C# @$ ]
TECHNICAL DICTIONARY 81: L7 ?, f, \% S
INNER MARKER, A marker beacon located between9 t0 T# [# `* b
the middle marker and the end of the ILS runway.
* ]: \& C1 a, ~OP, SEE - INOPERATIVE) ~! q4 p4 A5 A. ^3 p. |4 ^
OPERATIVE, Not working or operating.
2 A! B7 n- o3 ?2 H/ H& ZSTRUMENT FLIGHT RULES (IFR), Rules governing+ z! q% o! G K8 e: |
e procedures for conducting instrument flight. Also a+ ]2 u7 B M8 ]* F4 o [! G4 H# z
rm used by pilots and controllers to indicate type of2 N3 J, z3 f T* v
ight plan.* Y6 e6 S9 W8 X. k9 A6 B
STRUMENT LANDING SYSTEM, A precision8 P0 i- B" i# g# A m- a- `
strument approach system which normally consists of
( H5 x& f( r: y+ o" Oe following airplane components: localizer receiver,
" L* ]) d9 ]* I* E$ k1 c" G2 flide slope receiver, and marker beacon receiver.
9 v" @5 j# K2 ]OLOGICAL CONDITIONS
$ q" @1 f3 X, D4 r J6 W; eMC), Meteorological conditions expressed in terms of
4 m" u4 L# z9 N$ Gisibility, distance from cloud, and ceiling less than the
7 N0 t% I1 K+ T% z: {inimums specified for visual meteorological* f) V5 {5 L' a+ I6 e. H, N! S
itions.
$ f% Z: E, g3 U: o) |STRUMENT RUNWAY, A runway equipped with
: E+ M1 {+ M" c+ q- _0 n E3 P# Wlectronic and visual navigation aids for which a# \) @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" r气
2 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& `上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
储
: [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/ \" k
据
0 i! T. x8 M: U2 ~) r4 q8 F国: D- @0 N2 @, M( a' x
量。- L( B, n+ _: e, h7 c8 `
国
# X, s+ L- s: N8 ]/ x5 ?6 } k/ O% |# ^的
$ E. o% T. ?/ T& G/ g z- a积 \& 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 p
者0 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
是
- 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 e
运4 E6 n" e: T+ q g6 G, U' V( \5 b
询
* 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: s,3 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
携
! ^& K; T( ], C \等
- C- z. c& ]1 V6 z% H9 q的 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 a千
2 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: [引6 V. |( s: ^$ H8 G$ Q$ R
燃油系统3 L/ b: ~- {3 M) y2 |) j" x6 ?3 _
水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件; M; K0 o* [. k* ]2 \! ~/ P
焦/ I$ n' o% n7 a$ T
能5 n6 _$ c* ?6 {" C6 `* ?! s8 [# F
跨: H% Q: w* p5 T/ B. Q7 \
接
" k( W$ S& j+ M' k; c" a# v腹
8 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 A
.
5 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行- X) `5 A. S8 _0 k4 d' H1 ^' P
纬
! t5 j8 @- w/ u! c: s秒! i6 ]9 q+ k: z7 l' _7 B% Z
分! o: P. T& ?% J* w4 K" K
铅, u( V) J8 z' ~* G: X
氧
/ 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& m平1 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 }升
8 o3 r" Q$ J& b+ E, |+ v' t: D气流流
! Z* Q7 l4 T" d1 {" ~- C9 R4 a发
0 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. L
灯2 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. n
水
5 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
+ ^/ \( g9 ^. n) T道引导。, y; X8 I3 Y( s, @; T
载1 s0 A, \- n8 T* m! u
量和平- ?1 i9 X0 {( k3 Q4 h' \
装载系数# d" E( t9 x: W2 ]* I1 [' }
机翼产生的升力和飞机重量的比值。# ]4 M7 i& N, R8 R" P1 A8 R
中指点标,- b" m0 T* K5 r( W4 p7 N& Z# f* B; @
用以指示仪表着陆系统进近的下滑道上通常相当于决
- U9 c% H; x( z+ J断高度或其 e3 y1 A/ M4 X
远指点标,
. ?4 o1 I' u7 f5 G/ |% h, y. p位于或靠6 h8 j$ m) h; |0 l2 x* v: v3 D# D
标) @5 r7 R/ P" @9 V8 L
航向道,8 o7 C& v% Q* b6 B5 R$ e
英汉对照民用航空词典B OEING
& m. k' G+ w3 K$ m4 s8 T- L$ STECHNICAL DICTIONARY 94! b% _1 A3 Y) _( I9 y% }; v7 B
LOCKBOLT, A steel fastener which prevents unwanted
$ {* Y/ a* {3 C0 Erotation by using a collar instead of a nut.( q0 C. H/ a \) 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; ?
航
* @ Y8 V% J2 k- g比
" 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
百; 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
度
/ A, L: j9 g5 v% A" ~8 a低
8 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) p
航6 ] 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
然 R6 g* ^# ^+ U! _# I
线性可变差动变压器,
4 g( P0 `4 A! Z2 w: Q- O; ]0 w* X.2 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平
: 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
不. y. g8 }; R" z5 c+ ]
磁- 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
最
- 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量
. Q- m! z+ `" J* F. C0 `' W! c* h. u最5 ~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 O,
9 @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 }: v总
2 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
最
! Q$ V N/ p6 F/ {' n* J.9 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
计% 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
何
/ ?, [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& ]
密5 o! k2 K/ G* n( b7 Q8 S
千分之
9 {8 j4 F- U# k( C) p6 ]+ a最
$ `* ~0 G# B9 b6 Q最/ 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. }操; 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 P体
1 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单
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 W有1 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输+ B; h& b! [ _& ^% A4 h
空
% 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 }
海
* 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负
( 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/ X。
2 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中 M4 C4 `4 I, o+ g5 W& K
净
/ 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镍
. ~" f6 i1 X' S! p' J1 z惰
0 ]$ ?# {7 j( ~/ v2 h' z4 c, h; n降' c) u" W5 t. f! k
面
9 K8 G( Z1 e& A& D4 G5 g1 {7 rNOMEX,
+ y9 W' {) k$ p; k. E4 B% o是1 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
动
" P$ y8 S* L- r5 R9 t& J永" p- U- x/ Z* _6 D. M
或非门,
f, M: ~. N! P个
6 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
头
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+ Y
.6 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# |# J
反9 a$ x; e9 c+ K/ E8 I T5 s; T4 Z
相反的一面。: O l5 p5 p$ H; r+ T
滑2 [9 I2 J* c4 a: D4 c
滑! ]+ W( T9 O# ]
空& C6 @) t1 X$ W7 X/ n, B, R3 {
油
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同% r* E/ [0 {. f1 i* |: ~' D% b
奥米加导航系统(ONS),
8 G" V& B. r0 e" W一4 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 ^
如
; |4 p, S b) D/ a5 v# x远9 _! M1 i- ~# ^; G" b
外$ k4 P+ [) v9 E$ a* i O% v
压
# o3 w) ]3 i: H; p外
1 y+ h2 N! P( q翻 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
空
* w$ }% T3 B; {: b. J" [3 M微粒,
. i0 c7 f' N& b% I' L号- \: U& S0 O. q$ A- D
旅
' a% K3 F% n$ M1 e P9 u向旅客提供音( a; h, I5 |; _- @
业载,! [; D$ n* D# o
动- 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
装& A/ h! V; @* N, v
飞( 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- H顶
3 F8 W) `" h0 }! D4 b俯
: 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
机$ q v: _' r# Z3 T2 Q8 p) C
总静压; W: X8 t4 {! A S+ \
用
& 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+ b皮
1 [; I. n8 \9 V油6 d" I( b) |/ h9 T7 B7 g6 V9 v
.
4 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
有( ?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: w。8 ~' o1 j! a6 O. P* ~7 r
气
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( U弹8 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) y
动2 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
预
, 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压: n& P1 [, b- ` p* z% F
印
" m3 m- }* X% M- m优$ K1 D6 k1 P8 v! o" X# ^7 B1 u
液压系统中3 O( [. G, ^% I4 \- L
程
. 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- _邻
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 {' x快
3 Q& S0 n( P# S' d.
0 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* g
.
7 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
标 ?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
机
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
供
+ P; f" ?7 ^0 ]: q! g- x# u随
/ {* x! w2 T, B% V. U" g3 |储8 O2 J+ A6 l# L. y
冲
! E' c/ _! {, s% j2 c.
1 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) O比
4 T" w8 r5 d8 s" M: S的机械装置。
`! B0 \9 V$ j- ^原
' 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
一
. U$ Y. P8 y. k中
+ }1 N7 t8 u6 K$ b1 q在飞机
+ [' F7 g% y: ?! s: M0 g( y6 l6 e调1 X$ D! M8 O0 l) c& ^7 }% X
用以控$ F$ V5 R# _% O* F& A5 ~- n1 e9 y% j
释
5 A( [8 \* O& |- r% L闭
0 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 t。
3 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
限
) i) w" o) A! k; Z/ m3 y# E* g拉回油
& U* u! @7 @: o9 N7 E态; 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 d。
2 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( ~. `* K校8 `: D5 _4 e, {' l0 z
销
- 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 \& p横
6 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
着# 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左
- 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# `
离
$ 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 `; z
油8 |. m4 h7 L+ n4 N& K
S
, Y) V1 U% V3 W' J, a柱和蓄压器
k$ n8 u! [% u硅+ m# a) }) J8 G, W# T
.1 }( 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
草
! c: V* e1 A, E盘
- 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( r
选9 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接
: 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 ~* P。
9 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 _传
, 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旋( ]- 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& a,
1 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+ ?少; 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 t
防
6 m. }" S1 d1 K的外管。" M1 `6 x w! L" i# }' q
两# 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( |子* 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" G计7 R7 z8 L# Y! k# Z
冲& 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
刹
" 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, R输
5 B1 K1 G3 _' @人$ o' D0 h4 ]* k# g( ~ F# Q+ T
缓0 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
弹
! 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
爆$ u+ U1 U1 Q& ]
安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安) 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% I
流2 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 y气7 v# e& q1 W! h9 `) u4 ^* O% a
静8 e# W8 h0 H/ @5 I" ?7 p' V: u
静
0 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* w
转
0 L9 L+ G3 S9 q, c一个在起落架5 w1 H+ M) N1 ]. W# N; F
前
+ N* R' h7 d& J1 j2 H, k2 I; I驾驶舱, T$ k( v/ c: s. c4 g" [
自
& 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/ z减4 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
构! `. N. U {' u$ q+ K7 ]
造
% @: 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油, `" ^6 D; {0 G- N$ x! {) L
辅助方式7 i8 ^8 B8 I& v! F. R
用- 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
压
& h l# l: R% x/ z) b例8 e. J4 H, @0 x+ r8 L1 {8 b
元
; 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: F
温
6 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$ {滑- 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& @
空
7 [/ F% E" v! h/ X4 | J* Z5 X.5 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" t泰3 s5 d% j2 ]0 H/ P
温! 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 U热
4 x- C G7 ]( P/ H6 |5 h热补偿器,
6 C' U6 C$ G6 _. l" |+ N装
+ A2 T5 r8 S+ M- e& Q热
, {* K/ T! f2 D) P' o! n因为流体温度5 J- d9 y9 R- h6 {+ v
热
1 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节
" 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) |
推
' |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
的' 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! _而
: h4 v( [, @- \: N6 c: c5 S: [寸; 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
移 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- P
航8 }1 R3 J2 U: b# T9 y: [
导航术语。
0 q$ g* w+ `* `5 ^! p# e.
3 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 [" ^
电. ?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: p
配9 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
在
" 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: a
部
6 c/ N4 h3 ]# V4 \1 f |# X+ f和
* 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$ r。0 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度
* 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, @
机
3 s3 {6 n9 E& _7 K超
5 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且 P" ], M* Y( K2 \( O
停
. 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( w垂0 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 }
机
. V$ |1 n1 U6 x; U" c( q垂直航迹,- Z; B: f! R. V2 ^8 ]7 p
.2 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) {; ~水2 v0 q) z2 ]7 s; }
除
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机; 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
齐+ D$ E/ ]4 H; u1 ~$ E. A* Y
无
* [+ `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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