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airspace of defined dimensions within which Flight
6 i% X) `1 h4 h/ J" G8 J3 HInformation Service and Alerting Service are provided.
. ?2 U$ L) l& V6 O) ^4 uF
) h* V9 d9 M0 \9 f3 M$ Dd0 {; @5 h6 n+ W( k
F r& M$ q( x1 J/ W
in! d8 G$ L1 m+ t% F& H
a
. x0 b8 ^, G" y6 eF% t8 ]! R: r! \9 K& ~
s b2 a( _& f) Y! l
s. V" X( D1 H1 p% z! X0 l
飞行指引仪自动显示(FDS),
" B4 C2 e' m/ ], c. P/ c- z* ^( z当飞行指引仪的开关处于关断的位置时,自动显示的飞2 e( }% @( d z/ e
行指令。
/ i X9 m0 C" S- G, h飞航情报区(FIR,UIR),
* c6 [$ _$ ?; I3 ]一个有飞行资料服务和警告服务的范围6 C; N- Z. [* j3 }( w7 {
度层。
4 F9 @, I8 Z! }$ ?" B' h9 o) f8 ^50表示
/ `" r0 S/ B) n显示自动飞
! Y Q# g6 y5 K* J英汉对照民用航空词典B OEING
6 h- G0 u" b2 Q, f YTECHNICAL DICTIONARY 64% p, Z9 t" |/ j; [
FLIGHT SPOILER, See Spoiler.
. C/ H& ]2 |# p- q4 @: F- aLOAT SWITCH, An electrical switch which opens or( r- }2 ]2 I }* X" m4 i( d8 E
loses an electrical circuit depending on fluid quantity in5 T$ z2 K9 o9 }: Y$ h3 [
e reservoir.
4 B: D* v! [* W+ k6 fLIGHT TRAINING DEVICE: Any device having a full* f0 E- F- F7 L: L3 V! A8 B
cale replace of instruments, flight deck area or an) x' f8 E3 H0 x
nclosed airplane cockpit includes the equipment and+ G* r( k7 @! c1 A
rograms necessary to represent the airplane in ground' c) U) w! V$ Y) x
nd flight conditions.
5 t+ Y! V% M* S5 z* C7 R; j" dLOAT VALVE, A valve in a fluid reservoir which opens
3 U( V& ^+ ]/ ]# [4 x4 D1 m' and closes an inlet or outlet depending on fluid level.
7 @' o, a+ _- s" Z% c' ?LOWMETER, An electrical transmitter for measuring
, E3 C( `4 Y4 e. U4 vthe engine.9 ~0 K; ?1 w: x; x9 W# I3 n
LUORESCENT LIGHT, A light emitted by a gas filled/ r" j( V( n+ D4 y9 P# H i" r- E
飞行扰流板,
) L0 n' r: L. d9 q/ [见Spoiler.
* k5 H2 ~# Y, k浮子电门," M& U% f5 j* ^3 V* J' e' _ ^
根据贮液箱内液体的量来接通或断开电路的一种电器
' b, H Y e, k% ^% }; M开关。 m3 L0 x) f; P4 }7 z$ p$ T
飞行培训设备,7 d* o/ Q- [. ~3 s+ z i
仿仪表、驾驶舱区、或封闭驾驶舱的任何设施仿真装置。
+ A: D E* Y8 s$ I4 C1 k" X9 R# u包括可体现飞机地面和空中状态的设备和程序。
8 F7 @ h4 p' ^ O3 ~' T1 }& O浮子活门,! X! k3 R$ n: A4 }; v4 ]1 Y6 a
装在贮液箱内,根据液面的高低来开启和关闭进口或出3 J* X5 } m2 d1 @% C& L) m
口的活门。
6 X$ F4 R% E2 T9 u流量表,
1 T) T2 r6 f/ a' ]5 e用来量度流向发动机的燃油流率的电传感器。8 G) \ M" y, X3 a
萤光,
?* o1 h F: x8 m) g% [由一种特制的充气管所发出的光。7 _2 P0 |; `1 f% ^
F+ Q2 W T( G, l0 h
c
- f+ j1 N' z/ H7 v( }6 O pth- t7 O2 c0 K4 }% i B
F
+ y& E |. T5 ?8 P. O- `s; V9 i8 E) T: p2 g8 e- F2 H
e
1 t/ e" D. O6 A" [9 @8 Qp1 f+ |' R A, s' |) T
a7 K7 c$ a* F+ n* k
F+ i# D; p# q$ Y3 i+ I
a
' w6 C! i4 |2 } z0 ]' I5 v8 EF
$ n" N |9 T0 l* x; w( I1 Hthe fuel flow to
" v4 L4 b; L3 \. `F; @0 B" B6 l, d
tube.5 P6 U- h6 U) W6 b4 q) [
英汉对照民用航空词典B OEING
1 Y0 `( ~9 [" G& B1 j" HTECHNICAL DICTIONARY 65
" ~9 Q8 Y: b7 zFMC, SEE - FLIGHT MANAGEMENT COMPUTER
( y9 d0 P* z/ e# T9 OFOD, SEE - FOREIGN OBJECT DAMAGE
6 U; @# W$ g B6 vORCE BALANCE VALVE, A valve controlled by the8 o% o; h9 V/ J+ }& f& n
OREIGN, Offside; opposite side.
+ h, u0 |) }. _8 _: B b' HOREIGN OBJECT DAMAGE, Internal engine damage& r4 ~3 h1 d+ G/ @: B
ue to objects entering the engine air inlet.6 G. P; I6 {/ K5 P) C
RM, SEE - FAULT REPORTING MANUAL
% O) m- c3 |7 g1 j9 {UEL CONSERVATION, The activity of planning flight! c" a0 N; k" E2 U
ltitudes and cruise speeds so as to minimize fuel. Q) k" Q( R8 m3 P2 q( ^
onsumption.
' Q$ V7 S, L n' `/ F2 x9 y; m4 I" M" FUEL CONTROL UNIT (FCU), A component on the
2 }* M Z, Y9 W9 Z2 Y' d& qngine for controlling fuel flow for starting and engine
; r6 Y0 M% Z$ z7 r$ ]& CF, l+ y. B, N* x. O
feel computer in the elevator system for hydraulic
" u, c \3 ^; b! n1 C2 r& opressure supply to the elevator actuator.3 w# h8 K% i' f8 q- U( c
F
5 K8 F( @$ q" _9 D2 oF, o* ^5 g& h" o x @7 f
d
2 ?# q9 m7 q. h" k" A' z7 t1 UF
0 ~ k5 N! p7 s4 V3 d6 F3 G& z% n% qF
& x3 G: o# i4 p* z2 ta
3 I, _8 e0 c, e& V. w- d- o9 Jc( f- L7 |- m& t% Y# j+ @
F
! g7 Y& J# R" s/ p1 G8 s5 xe
, J4 k& {% s3 Eoperation.2 Y& f) P* d2 p1 y( P
飞行管理计算机,
1 g% f' y. M- Q: G2 u见Flight Management Computer.
3 h! O3 {. i1 ?* R外来物损坏,5 u" F! \. a0 g
eign Object Damage/ Z: {, q% Q5 Q6 U( H# u* P5 ~
见For .
. d- \3 W, @: i1 l6 h( ]平衡活门,
" \3 d" {( C3 M6 D. [, U内的感觉计算机控制的活门,用来向升降 G% L. N) _/ e) l
外面的,
2 F1 i2 n3 ^2 ~0 p% p8 W8 b" U另一边的,对面的。
" v g. Z& L( Z/ A2 e2 r; j d" G3 p, i外来物损坏,* T7 s4 S. y" v0 D4 l h$ \( T( x
由进人发动机进气口的物体所引起的发动机内部。# x+ q2 V4 K+ N2 \
故障报告手册,
: e+ r" j$ q+ F# O, _5 W7 }见Fault Reporting Manual+ W. L# h8 K" h7 T
力
5 A; ~# Y4 F W5 [8 j9 m/ t由升降舵系统" Q2 X% ~$ |2 n# P5 ~) I' ]
舵舵机提供液压力。0 A* y! z( O! G1 {5 Y. ^
损坏
) P. ]$ l: }& ]/ E5 @, ^.
1 K0 ?6 S2 J4 h! i* q, u7 w- _约燃油,$ q( [- [* r4 `; [. f) w$ `
为使燃油消耗最少而对飞行高度和巡航速度的计划。8 j. o" `1 _7 ^. I1 B% }4 _
油控制装置(FCU)," i2 ^) W0 q* X# A3 ~3 g8 f9 M4 e
发动机上的一个部件。在发动机起动和运转时控制燃油) L2 D0 H( S' X( M$ Q$ l0 a
节
/ b7 J- T- n/ H' G3 @/ C: c燃1 X4 ~$ @! O1 Z4 R, U
流量。4 k7 T7 t4 e: _
英汉对照民用航空词典B OEING' m0 Z( v# ^0 R: v4 K
TECHNICAL DICTIONARY 66! b: R+ S& w! \+ @7 X& j4 }# W
FUEL FLOW, The rate at which an engine consumes. G" K$ R) ^) ^- Y4 C0 Q8 q( k
UEL HEATER, A component on the engine for heating
: {' O+ N( \! o% w3 iUEL JETTISON SYSTEM, A method for reducing
4 X. A6 |6 D& Be
0 G% \! F+ C+ a1 c2 L, ]4 jULL FLIGHT SIMULATION (FFS): A flight training
, Q- t2 I: p1 |1 o% sevice that incorporates full visual and motion systems8 k, P' w6 e+ K" f+ i2 l
nd specific model airplane.
0 u9 D" h' y1 L6 I* {) {ULL-WAVE RECTIFIER, An electronic circuit which
1 M3 U7 W* Y- @6 ?hanges an alternating current signal into a pulsating
0 {* g) q% M! f2 O8 S6 Hirect current signal.2 s n6 x* {' b) m
or& E- J( ~1 L( l
AGE PRESSURE, Pressure measured in pounds per. p3 m0 K) ?8 f
GALVANIC CORROSION, A form of corrosion caused
. k p% S# L2 g8 }9 k7 b! |7 y7 y8 `by the contact of dissimilar metals.5 y3 E' e, ]. ~8 M4 @: {( ^
油加温器,8 S9 N1 I1 t, f( L6 O8 G+ O
热燃油以防止发动机燃油' W% n6 ~5 w! ]( Y
急放燃油系统,' o8 ]- `- C5 R
中的燃油向外排放以减轻飞机重量的8 Y- K' q _- s# g: g* O
动飞行模拟机(FFS),
! P5 y- P; @. m* h0 S2 ?1 {一种飞行训练器。它综合了完整的视景和运动系统,以6 M, u; B. [( X$ X U* j1 ]" f
具体的机型。
( \$ l ^" }( \/ r3 I# ?波整流器,
9 h. P# U6 |1 d1 ~用来将交流电信号变成脉冲直流电信号的电路。# j5 a; R+ F4 n/ R$ ^3 h6 S
压,
, Y% K- ~4 d/ S8 j: @8 G/ J平方英寸若干磅(psig)磅/平方英寸的计6 _* H z7 p* _2 [/ k- U
电解腐蚀,0 h' o5 ?; E/ F" s8 `! ]0 D
一种由于不同种金属的接触所产生的腐蚀。
& ]. e! h1 ?2 ofuel measured in units of weight per hour.% a3 L9 I( u- `( U' G3 m2 I
F
8 e6 Q) v2 R$ j2 I- W# ]fuel to prevent icing conditions in the engine fuel
/ d4 W+ H. a! T! [- xsystem.
4 g G! Y; V# y7 mF9 `9 c6 d6 ^* O( x9 g( s# y
airplane weight by discharging fuel from the tanks to th
! }1 D( i% n8 m% r) q3 }' ?outside.
' z) R `& J" }6 d' KF
" }3 y) w7 R0 f7 W2 n' ed
0 k! m/ G9 C5 U' E" na
, Y8 N2 @7 [/ S. h5 m# }/ FF% ?# Y7 X6 j4 m f; B2 ]
c
$ c3 r% o" n8 ^7 |d0 ~: p9 Q7 f) G9 y
G
l D4 `) G: |% ?0 [0 g: aGAGE, A component for showing quantity, pressure,, w% s2 B$ i6 `. X
temperature by a pointer or numeric display.: A) f! j$ K, N8 Q
G3 I' P. C! z/ k
square inch gauge (psig). L6 `9 N9 o; ?3 F/ e2 D* `/ k
燃油流量,
) M! x. T S9 A5 t5 {1 h, q/ D发动机消耗燃油的速率。以每小时单位重量衡量。. \7 a, [8 Z: {
燃! F6 u1 j3 p# i2 ]$ }6 h: s
发动机上的一个部件,用于加# t# a0 k, Z; c/ L5 P
系统结冰。 G. S" d0 i# `) t% D3 P" j/ _
应9 y! t* |, O5 A9 ? U$ B! H1 u
一种通过将油箱* ~; v$ R; u. n$ _ c
方法。6 Y3 E9 Y! R& }; K
全
5 O" X5 G/ N* Z及1 H: C3 P' }. q: q- P4 e6 F3 K
全
" y3 f! q5 S* Y- C1 f) U4 _* z% g计量仪,
+ z" Y" v# m+ s2 ^, j, Q0 J由指针或数字显示出数量,压力或温度的部件。+ ~4 @' V. C0 q+ Q- m% I6 L5 C
表
j: p$ B! i. n b; i# I单位是(每& G( d: c" {7 `. E2 a
示压力。2 N/ l* O. y `6 S
英汉对照民用航空词典B OEING
4 B& w9 T+ H; {( \1 }6 X; E% D; YTECHNICAL DICTIONARY 67$ P/ n) d. R' C. r( d/ i* t
GASKET, A seal between two flat surfaces.
( Q9 E( i- `, v7 ~! Lbe individually controlled for the amount, y! N- P3 V9 J0 A+ `$ d/ P
nd direction of supply.6 T5 Y( b. O w1 ~, } W8 d
ATE (NO. 1), Airport location used for# z. x" e3 X( r0 r# q
ading/unloading passengers.
9 y+ L* G3 n4 w: lATE (NO. 2), SEE - LOGIC GATE
& d1 v+ z& _& l; {2 TATE VALVE, An actuator operated, sliding device in a; R8 e9 n' m* O$ B
uct for closing and opening the duct passage.
: Q t/ y" V% q间的密封物。
! ?& f& f8 w! j* [调节供气口可控制空气的量和方向。
" O6 C2 [1 H& a! M, p: g登机门,
" a: {- {# | o2 Z3 n- ]' `机场内用于乘客上下飞机的通道。
2 R; Y0 T9 T$ N% l逻辑门,
7 {; f' }1 z; k* j# [/ I见Logic Gate
: N9 `2 }6 N) a3 P5 \7 X5 yGASPER AIR, An individual air supply for each4 ]& n9 |; _5 c$ q- A9 X8 C+ q
passenger. The air outlets are in the Passenger Service0 Q! }" ]% Z2 F# [% u: g4 e
Units and can
2 |7 D4 P6 A3 a/ G# X L+ X: xa: L( g1 C0 ]9 s; r
G! ?2 _8 f/ P& }# X/ \
lo
) p+ H" l d+ y Z, m" tG K( \" o R; Q
G
( k; d4 {' W& Y" ^- v4 c% u# L( hd
- Y! c* I& W5 @; l6 r7 P+ [! V0 v密封垫,5 G! ~- h! B7 ?& H0 H7 Y7 j
两个平面之& g% v# c: a; G# c5 A* }
乘客用空气, h) H c( u1 J: {% U
给每位乘客的单个空气供给。供气口装在乘客服务设备
* `: T* y) H( i! a; ^' s内,个别) E7 j4 x2 [* o6 i4 M% h% `4 K7 m
.$ C2 |9 ~* U' N6 I8 ]% n
闸板活门,5 J% E2 v3 G7 i i$ M" Y
管道中由作动筒操纵的滑动装置。用来关闭和打开管道3 m9 a$ X( k+ J. h( U6 c
通路。) d6 S$ H! V$ P& Y4 Z4 R
英汉对照民用航空词典B OEING
) j! Q; k8 h% g% e$ tTECHNICAL DICTIONARY 685 o8 H0 B/ `) C/ `! L4 F
GATEWAY, A functional unit which connects networks/ L; F2 U+ ] M, T9 l* q) c
r systems of different data formats.
% i) B5 }) y; x0 C9 Y0 TRS.
$ Z) A6 d* I2 O- B oENERATOR, A mechanically driven device for4 ~9 `2 Z2 ^% H* p
ENERATOR BREAKER(S) (GB), A device which will
8 s. s/ W8 p$ V) \5 S; J- R3 dtor from the
: I, N" [9 Q% o7 T8 Y) c' olectrical bus(es) it powers.
5 K$ ?! V! L( qent with& E) v6 L4 P% x. y# \1 T
o rings pivoted on axes at right angles to each other
* R) p' o$ y# k8 N" Nllowing movement in two directions used in the flap
& i/ r2 @, J+ R# a/ M: z- J( X- L2 Vxtension and retraction system.
: ^9 F( ?/ t- Z1 h D接在一起的功能
) e" [ w/ F7 D, @件。. R* R) `8 h( t ]( n. |
o5 C! }( m" v5 u
GEAR DOORS, SEE LANDING GEAR DOO
+ X4 r5 D! ^7 S5 f, a4 M" ?) r" d0 \4 yG$ i2 ^3 d" T. k/ k- A1 ^& O
producing alternating current for airplane electrical
1 M! t) w! O1 w4 X, bsystem.
$ n. w% P1 F4 r& u7 u% r, z' CG9 v1 Y5 S1 [* K# P- O1 Z* Y/ C
separate an electrical power genera
/ r. ]# Y# ~' n7 o( C; K( m; j* qe
& _9 @! L% ]# @, B7 b! B5 wGIMBAL ASSEMBLY, A mechanical compon
F- A/ I4 ~5 I+ |/ f1 M7 M( Mtw
7 e4 B1 t$ `. e, B1 S' g' a- Ha. c8 N$ I! @4 Y5 j- B* E
e" Z) x1 Q; H1 j Y
闸门,
3 o0 N" y! H7 c3 Q3 _ D# v" p一种将数据格式不同的网络或系统联& W/ n/ s) b" @. c% b8 s5 _
元 x- G7 m/ f3 F0 P( y
起落架舱门,# g7 u( t, R9 a l. z+ `3 ` J1 B7 ?5 B
见Landing Gear Doors.
7 l! f/ V% j M' w# E; U4 e8 ?* [+ p! f发电机,9 g' \6 p4 v" w0 @' a7 h2 t
为飞机电器系统产生交流电的装置。6 E. `* u; q' J+ u1 G
电机跳开关(GB),! Z" V) L. u9 n; |5 k
机与由它供电的汇流条断开的装置。! G! k. i5 K& [% O, r- r, c& M, E. X
襟翼的伸出和收上系统内的具有两个圆环的机械部件。- u5 x! O) c T
个圆环的旋转轴相互垂直,以使部件在两个方向都能转
+ N$ {' n( J4 X( T。
' \5 d4 `$ J# l* K0 U0 m* C由机械驱动,
. k' m, s/ U1 B2 ^* s$ F$ Y% w! [发
% V; Q3 G$ o2 b2 V$ m, @能将发电
- L+ K, j( f0 H- k( c9 U万向架组件,% |& `. `! F2 R* y% |* v
两
5 `" |: z) k8 E) Z, T动
g- l( d4 b* z英汉对照民用航空词典B OEING
( n$ k* L, m- b; y( V+ U8 PTECHNICAL DICTIONARY 69
9 u+ |% C$ j" |GIRT BAR, A rod attached to the escape slide which4 i5 I: @5 n# h* I5 R3 l( l6 k
engages brackets on the floor for automatic slide9 O1 z) u3 _. {: V! d0 P
peration when the doors are opened.' _1 {4 Z* U8 X; S! V
LOPE (GS), A vertical path defined by a/ T/ z7 M/ i- n( w8 W
ased electronic signal used by an airplane or+ ~" s, q6 p' @: \3 N' M, l& V: L
LIDE SLOPE/GLIDE PATH INTERCEPT ALTITUDE,
# d. f9 J, ^% @1 G8 U: }% F- xhe intersection of the
# f: t* E7 |( `ublished intercept altitude with Terminal charts by the
5 {! U. m) [/ Utart of the glide slope/path symbol, is the precision FAF;3 H6 e! p# I! G; W# e6 ]; Q6 T
owever, when ATC directs a lower altitude, the R+ O, w# g+ Y0 S
地
! ^( V ~( f/ \9 Q3 N上之锁钩相齿合,以便滑梯自动工作。$ i6 N0 N- q& w4 K% A
滑道(GS),
3 ~1 I' @0 i; r" Q2 C8 j由进近或着陆期间,飞机或飞行员使用的地面电子信号
5 `# S$ ?& I7 W1 `+ r* j# M) y垂直下滑航道。
3 k& t+ `7 x( D/ x, N- G6 l滑道/下滑航径切人高度,
% M0 P) v( }; R+ d进近时切人下滑道/下滑航径的最低高度。在: x8 t' L- f3 c/ C8 m2 \
最后进近定位点。但当空中交通管制指挥一个. P9 ?/ V& y, |
低的高度时,由此产生的较低切人位是最后进近定位" _( |; j% E/ M$ U
。' r6 j1 o( b; I8 V9 {
o; Y7 p n/ O- ?6 R9 p" I
GLIDE S6 {# i5 \2 J# A% x+ _) `
ground b% a: v, q5 V* u7 s$ ~; Z
pilot during approach or landing.4 M; i- C6 k% u
G" @5 W4 @4 _' G
The minimum altitude to intercept the glide slope/path% Y6 R( a) P5 y8 n9 W5 C. P& B
on a precision approach. T* w& S& [+ J; A$ L3 s; N, D4 Q
p7 j2 Y8 d" o) w: X" v3 C0 C1 e8 r" q
s
4 ?( `& i6 h) a9 y: L* q* F' H( Th/ b7 h Z$ k/ i; T2 H
resultant lower intercept position is then the FAR.- F8 d, K) ?# m
束缚杆,, d3 f3 D/ k: L6 M
连在逃离滑梯上端的杆子。在机舱门打开时,与机舱5 H1 S. j. I& ?9 B& X
板2 Q2 \- o/ ?" b4 T2 C* a F
下7 x# _: L( W5 A( I6 p5 \
确立的一条) I9 f7 n4 ?: w5 n. I+ W* q
下
& Z/ `% L7 X+ q5 z* T5 f在精密
) O2 C: ?! i7 T% }* c2 D6 zJeppesen机场图上公布的切人高度与下滑道头的交接
4 T+ ^) ?# |( h点。是精密
, c7 Q3 l1 r* o0 O# K6 k3 p- \较
1 T. q4 g X5 A6 W- L* H点
* l2 d0 b, b" h9 r: z* e* \英汉对照民用航空词典B OEING
0 n8 ~; g; a/ H7 G( [' CTECHNICAL DICTIONARY 70
5 H* e5 @. n, @0 i3 D$ _9 c8 UGLOBAL POSITIONING SYSTEM (GPS) (No. 1), A% M- Z8 P: s2 c& j9 ]1 O6 O. m
pace-based radio positioning, navigation, and
! s# I4 a" h. D: ^7 m- o) hmetransfer system being developed by U.S.A.2 N1 n n# w- p# V/ @) r+ c/ v
epartment of Defense. The system provides highly# k9 z% d' E4 U# l
recise" L Q8 k* s; B% p
nd provides a worldwide
( q: v9 {9 w$ common grid reference system. The GPS concept is
( W, J1 v, n/ u: gredicated upon accurate and continuous knowledge of5 i9 Y- y# T' k+ L) u! k$ u+ ~
e spatial position of each satellite in the system with3 j4 v! `& P2 U
spect to time and distance from a transmitting satellite
& \7 o$ |5 `6 N% b1 p. ], Z: _! Qthe user. The GPS receiver automatically selects
6 w2 ~, ~, e7 M5 e; T3 `, Wppropriate signals from the satellite in view and# Y% U" Y( ^& C* u
anslates these into a three-dimensional position,
8 u* M/ x( A* R8 R/ t, s. L$ jelocity, and time.
; \/ a5 d0 G2 hLOBAL POSITIONING SYSTEM (GPS) (No. 2), A
$ {7 i: |, w# l1 Z6 ingrange navigation system that takes navigation input' t+ a5 r4 j- c1 O- v8 c7 w
om transmissions generated by a series of satellites in0 K; @# F! U$ A, l- [4 d
LOBAL NAVIGATION SATELLITE SYSTEMS (GNSS),3 n) D$ D9 s6 @# P3 A* K/ A
ternational Civil
: p! O4 v. N9 v. Jviation Organization (ICAO) to encompass any
2 `0 c' S: K, k% k" [1 W( Z! ydependent satellite navigation system used by a pilot
) z: R, H. ~2 b% v9 d" Eperform onboard position determinations from the
. M+ ?% g r0 a$ |- c( C# A7 |O-AROUND (GA), Airplane maneuver where the pilot is+ G8 P; E0 z9 R: i
in the final approach phase of flight and decides not to
z; d8 c' u0 V# {9 E g% ~land. Thrust is applied and the landing gear retracted so0 B# @; ~, A7 P7 d( w5 ^# w$ b3 {
as to climb the airplane to a safe altitude.! w; c& |& r/ l8 h4 Y
GO-AROUND THRUST, Maximum engine thrust to be
# _' f- N) ]+ F4 Z0 ]$ T+ Z2 Cused during the Go-Around Maneuver.: f- z5 h' p% I3 n" W
统(GPS)(NO.1)," g. y: ?8 _# i
电定位,导航,和时间转移6 _% j- q7 ]7 Q) M* Z- z
统。该系统在全球连接的基础上,给无数备有适当设备
+ V1 X2 v6 L9 r: P1 U" x) n户提供高度准确的位置、速度、和精密时间信息。该系
; A/ h- `: v @ y6 }响,并提供世界通用性座标系统。全球定
) f+ { g& J7 ~% c2 b( c4 M信息之原/ w! W+ q) b! G
为基础。全球定位系统自动从所见卫星选择合适信号,
" A) E, w. C- `4 i- [" B. }( z& W' r并将这些信号转译成三维空间位置、速率、和时间。
3 x8 v. p! I$ Y9 V0 X' |" ]全球定位系统(GPS)(NO.),& a4 I- X) h0 q' L( Q
一种使用一系列同步卫星所发射的信号作为导航输人6 F ~* }. T! ^! R2 p" D
长距离导航系统。
: q- c% l- ?: `' g2 e球导航卫星系统(GNSS),
, A( f( A; H/ g航组织采用的“伞形”术语。它包括飞行员
7 g/ F" e) ^- Z% E料做位置判断而使用的任何独立卫
4 p% c/ i$ u& x) f导航系统。
* \* f! G# z' b: w# d% y复飞(GA),
5 z D: K. Z7 ^# C& }6 b1 ]飞行员在最后进近阶段,决定不落地而做的机动动作。
# a6 X5 z* V$ I- ]! q复飞时需加油门,收起落架,以使飞机爬升至安全高度。; ]7 _* j; |$ K
复飞推力,
0 L- \$ |0 I4 U9 O$ _7 A9 x飞机复飞期间使用的最大发动机推力。; J0 O9 ^0 N8 ^( |4 l5 ^
s
& E4 c; Q2 Z" `) M8 N3 m, _9 M# g, ^1 Mti% l; d: d- }2 n z) l
D
8 r1 W) U" V. x4 |0 _- m3 ]5 h; l7 maccurate position and velocity information, and p/ F( Q& O7 v3 ` _
time, on a continuous global basis, to an unlimited
0 d, |( F, c. K* G" Z K& C' gnumber of properly equipped users. The system is
9 }% w! z3 m) z) {) S( tunaffected by weather, a
% B( p5 c f p `6 t) m, d) Fc: [4 B5 F& V' P6 f" J. j- Q
p# U7 v, o# A5 h H7 o' @( y
th
! o: E9 J& O8 i8 c/ Mre
8 Y6 {8 {5 `: W) Yto
* ^: Z& R3 ]" e/ Z& z, g2 Z/ X; }a& f) y) F" g. Q2 g
tr6 v3 }2 y" Z, j# ?
v
5 s+ v. E, G0 P# y' M$ OG
; q$ f$ e4 ^! clo+ W1 u. F# g: d0 E9 U2 F
fr) L( B! E; L: p
synchronous orbit.
0 {* Z, B9 v9 DG
9 w! y4 x _- L( P1 J# ZAn "umbrella" term adopted by the In
, _7 _2 w' a5 `A
7 i9 l" C$ }0 U+ F6 N4 [in
( o! b/ ?9 [. uto+ k4 [7 I$ t% ^; H
satellite data.
0 N3 |2 r9 E- O9 s1 V) ^全球定位系
/ g" N# e1 p' h6 p! G由美国国防部研制的空间无线8 ^* {2 `2 G- S
系5 i# v) ~; D: p( k ?
用* S- b+ `& U7 }) [: P0 A
统不受天气的影
3 C/ Q/ R) g+ q* U+ P5 N* |) y位系统概念以系统中每个卫星具备相对于发射卫星与用6 C8 C9 k2 P1 X4 \
户之间的时间和距离的准确且连续的空间位置
! _1 T( z5 W- n( F$ p( x则5 v' L4 O! a' ?' x4 l" H5 d4 {0 Y
2! r2 @2 d/ V. s) e0 P
的 ^: m3 Y6 S. U# i
全
* l. v' q k. d" r4 _0 f1 Q是国际民
4 w! P2 `% V1 Y/ i& ^ u) B A在飞行中根据卫星资
' S) l7 ]% f/ f4 o( [3 x3 G星* @! T* |+ M0 j0 a- y2 B, u
英汉对照民用航空词典B OEING, E$ l# V- ^' U
TECHNICAL DICTIONARY 71 A( p: h* ~3 h' j; R9 J
GRADIENT, The ratio of height gained or lost in a given
0 E2 T& t- s5 l% `- I+ Vdistance to the distance travelled.& E# Y4 ]- j' o) E+ ~. I {2 ^
rbon! T8 } S' ]6 V3 A; @
r access panels, landing gear doors and flight, ^, _* i# }5 [- l b
ontrols.3 P, F* `5 R$ R* e; d
IRCLE ROUTE, Is the shortest distance3 A7 i( D; L( b* u o
etween two points on the earth's surface. It is the line1 U {8 [' t& H7 a7 o
rmed by the surface of the earth on a plane that4 r$ F# n% ?% X/ M8 L; p& b
asses thru the center of the earth, the departure point,
7 C( B1 y8 N5 C. m: Et line
+ Z3 ]6 Z6 ~ d, T! ^, Q, jal Conic Projection
- P+ @/ g: a' P4 @3 A+ W) t. cpproximates a great circle route.5 a- c+ R7 L" _! H% g2 q% w3 x# Q. Y
GROSS WEIGHT (GW), Total weight of the entire
\* a4 O V" R. Hairplane, fuel, oil, cargo, passenger, etc.
$ m4 E5 w- P' o' t& f/ H) l& y/ ]5 vGROUND, A part of an electrical circuit or system that
$ i/ r) k2 u1 V8 u s- x0 whas zero voltage.( ?' \! ]: X8 d9 @% o
GROUND FAULT (NO. 1), System fault that has
' m; T. k0 x( B0 u" z& @occurred since airplane landing.
1 y1 i8 ^ J1 S5 k1 }- D轻的材料。用以制造舱口- |& b3 q9 y/ v& z, i
,起落架舱门和飞行操纵面。
3 h* _9 M/ s2 p3 S6 i5 {圆弧航线,
3 r2 n. g* x" G, |7 l1 w8 Y地球表面两点之间的最短距离是以地球中心为圆心,在
- L* J/ C$ {4 y7 g9 ~1 e飞点和着陆点间所形成的弧线。由大圆弧航线形成的真
: L% f, Z/ S! s* g3 d迹不断改变。在兰伯特等角曲线投影上画的直线接近大
. ]1 a0 y+ I3 J* u; ?. E全重(GW),1 q4 `/ K: ?& b8 S- ]: @
整架飞机的重量。包括飞机,燃油,滑油,货物,和乘- x7 p \1 s4 _/ F% |
客等等在内。
$ V! [, }! l: a# U地线,
7 z+ Q7 c& d* a2 l1 b$ X4 ]4 R; Q6 z在电路或电气系统中,具有零电压的部份。( j' N+ ~, ?4 _% M) y" R
地面故障(NO.1),
S; G* l# Y8 g自飞机着陆后所发生的系统故障。2 L, s" L( B" {
GRAPHITE, A strong, light material made from ca! a3 J1 w& F6 \! ]# {2 K% a
fo: Z; s: }$ M! p+ G- g; f$ {9 l$ E+ y# o9 L
c. y( W$ }; c" L$ q0 A ?
GREAT C
8 X) K0 {5 G" C0 G5 c' `b
- B: d4 O; Z. M/ [fo6 ?9 ^; B# D# x. ~
p2 I" W. m% ?. o: X+ X \
and the destination location. The true course formed by4 Y* [+ R/ A* I/ K2 m; Q+ T
a great circle route constantly changes. A straigh
: H( z) L) F* n2 Tdrawn on a Lambert Conform" f: k0 {' ~& f, `+ P- G
a
5 A+ ^, e. G/ p0 }3 D; zGROSS PERFORMANCE, Actual or measured- `, G( U4 ^& m+ a: ?
performance of the airplane.% f6 N# J$ P8 M! W8 W6 k
梯度,
: L; y( `6 z# ?4 f: y3 O在给定的距离内,获得或失去的高度与所经过的距离之' B# J- ]8 |$ D- R, ~6 A, A
比。, Z4 Y6 q7 ^/ E& h5 o9 p
石墨,
, B! M' ~( s. D一种由碳纤维所制成的强而
! Z/ M& P3 L |9 p, y盖
; y# p0 Y; C+ o) J3 K( f大
' @, L9 E* }( C7 [9 X) V起
8 m# g2 C N) o9 ?航
% B4 S8 O2 p. S$ Z( y9 b圆弧航线。
1 }- [" p% N! }( R* y1 Q/ Q总性能,; H1 E. L3 G: h! _" ]+ N! S- a3 W
飞机实际的或量得的性能。
( w6 A+ J5 }8 [# F5 _3 G. ]英汉对照民用航空词典B OEING2 D$ }+ X6 ]1 ~% |7 o3 e0 l |
TECHNICAL DICTIONARY 722 X9 R+ }- c8 P; Q& E
GROUND FAULT ( NO. 2), Loss of a ground connection
: I, q) M( ]2 g; Eor a short-circuit to ground.
# F8 i# S/ q, m. t# AGROUND SPEED (GS), The speed of an aircraft' r0 V% ^- [. x" L# Q" E
lative to the surface of the earth.. g/ C) g) A, b# h U6 J
ROUND SPOILER, SEE SPOILER2 f2 k; l" W" O/ F
ROUND SUPPORT EQUIPMENT (GSE), Equipment0 P' X9 j4 W- F5 {3 m* g4 t+ U
sed to service, test, move, power, or repair an airplane
5 Y% U# |+ n6 B, R, C" ~( W1 Ohile it is on the ground. n1 @2 P( v d1 I- f
ROUNDING POINT (TERMINAL), An electrical+ Z' F- P3 V" I9 L
onnection on the landing gear doors for electrically
8 K5 @6 O2 N: X6 T+ D% Rrounding the airplane. An electrical connection near
. X; m! \( J0 r- y' D9 Q* Te fueling station for electrically grounding the fueling3 W. g' C- v. P. u0 T" k, y. R
ase.
* U0 V5 q1 k" N* tS, SEE - GROUND SPEED
0 j4 w! i1 [0 K. a. m3 _, x5 VSE, SEE - GROUND SUPPORT EQUIPMENT
# \/ n. ]4 n. U- w! B% \1 KNO.2),6 P7 s4 Y$ P+ D) ^, B) l% _
地速(GS),
. {0 c. d8 x* h6 g/ K8 K飞机相对于地球表面的速度。9 y4 q& e/ S' N I9 m
地面扰流板,; l+ G7 e4 U- e
见Spoiler
- M5 t% z6 T) l& Pre0 O- z7 l5 U2 z! J6 Z
G
( z* R7 x4 N) G9 A ?) d" {G
+ z# I& h. ?* w# c9 vu0 {5 r( @( P+ E; ?
w( [! \ r, K7 F6 n
G
. W) V4 V- |! D+ Rc
; r z6 h0 _4 w ~g' @4 C' j" E9 l r# x
th
- s0 Q i! @! v; ~b9 Z. m6 H9 v$ R/ p' E- ~
G
' j q' G& |( p# mG
, }7 p+ D9 R0 a1 k% _6 |! o: xGUARDED SWITCH, A switch that is protected against" ^/ o6 e5 V* w E# N
accidental movement by having a cover installed
, N6 Q, A( _% [& r4 tdirectly over it.: \6 v, Y! ^: n
地线故障(7 @' [$ w, r' Y/ ~' e7 ?. f$ x
地线脱断或某线路因短路接地。
& n# y; Q; N% Y$ _; p/ u. }0 r5 B9 W- p r
地面保障设备(GSE),6 j; G* U$ W5 l) X% N# r
当飞机在地面时,用于勤务,测试,搬移,动力,
) C3 a% s7 _6 |8 _或维修用的设备。6 \0 W( l* T" r+ g& ]$ c0 j) D
接地点(接头),4 _( {0 D. s1 ?7 h( n
是在起落架舱门上的一个使飞机电接地的电接头是在
3 l% E/ e" W; w) R: x+ ^' l加油口附近,使加油车或地下油库电接地的电接头。& g [9 a" O) l z3 u& X6 B& B
速(GS),( B Z; n7 L, X- R+ K9 A
eed" ~# F3 y5 i7 V1 F( t
供应% ]9 X% y. x, k- ~' ~
。
! ~4 e0 a0 j7 S地
# _. p% A# m6 r& w见Ground Sp .- @* `$ \( k# w: o
面保障设备(GSE),* X# u, d7 t9 s) M- i# l6 d8 L4 I
见Ground Support Equipment S" D5 O& g. U7 ]! O$ J# f
地9 ]0 N: _% b# X; f; x9 A4 K
.& J y: x' j; Y$ Q
带保护罩的开关,8 s6 ~. H9 V3 k; F0 N& o
为防止意外拨动而直接装有罩盖的开关。8 f4 L/ F' B6 l. W: c5 s
英汉对照民用航空词典B OEING
2 E& ^- i+ [1 g+ FTECHNICAL DICTIONARY 73+ F% Z# S8 ]$ Z- V+ e9 o+ I( C
GW, SEE - GROSS WEIGHT
! O" k! ~$ J# m& K1 p+ X- }4 Y( QH: i9 A9 T, W" P
HAIRLINE CRACK, A serious defect in structure; a: S7 w7 R6 j, V1 `4 O& S
crack that shows as a very thin line.
- |. e! l1 z1 q+ THARD-OVER, A maximum pitch or roll maneuver.
c+ e, ]/ z: |( }$ ? q8 b* KHDG HOLD, SEE - HEADING HOLD
7 W" d8 g9 S! p l4 T% \ w1 s! o2 mEAD END, In a hydraulic actuator, reference to the
' k7 U2 b$ A* b- H) B' `5 w5 uart on the piston side of the actuator.
% [8 P. f: j( G1 lHDG SEL, SEE - HEADING SELECT0 V, U7 i0 K" D7 ]( _
H
7 M" Q, }2 Z0 n1 Yp
5 P! V! d" i. |2 {& vHEADING, The direction an airplane is pointed
, C8 o* R) e [referenced to true north or magnetic north.8 H; a0 e4 \( D k. v6 H7 F
全重(GW),# b8 t4 W% v, t( [* b
见Gross Weight.! b" S( Z* z, y% Q8 x
细缝裂纹,
1 B$ T( k- q, f' b& J+ i5 X h7 y结构内的严重缺陷;裂纹的外观是一条很细的线。
% [$ R4 ]! k4 B6 v b4 q急偏,' d' }- @4 [% Q4 O E* a9 P* T
最大俯仰或横侧操纵。
2 b% x* ~8 ]6 y, S+ D: |向保持,; {8 k' B0 F/ q/ ]. H2 r+ X
见Heading Hold
6 I) T9 v4 L" y) q; Z航$ B4 A8 `7 C. q
.
! L2 Q2 y$ H! \6 H" r5 P& Z航向选择;. N! i; }, F: g# _
见Heading Select.5 I2 Z& t$ x$ D: F; L
顶端,% a; {( x$ w4 C, d0 U
液压作动筒中与活塞相邻的。
- n) J) r" o& s相对于真北或磁北的飞机指向。) F6 D7 N! f+ [1 f
航向,2 L: s% Z' ?" n8 S3 \0 O: f
英汉对照民用航空词典B OEING
. s/ L6 _4 q, E6 v5 U! vTECHNICAL DICTIONARY 74
U `; Q7 D' _6 nHEADING HOLD (HDG HOLD), A mode of the autopilot* @" \9 J0 Q; L# s
irplane heading.
; N0 @6 D* n+ V2 ]4 Zt% S4 R, z+ N S, ?0 V" V+ {) k
e
# M. H$ C' _) k: v) |8 z2 ]om- K1 F8 S- s; o
g or' H- y6 u9 y3 ?
(HDG HOLD),
9 }/ [) s' T' p; D(HDG SEL),, [0 ]: R- X1 r
交换器,
6 C$ @" k. c4 U4 A有很多通道的金属组件,气体在通道里流过时,一股气
0 @% I0 [, q/ d& J2 q& Z: |可被另一股气流冷却或加热。
; o# w8 G7 `1 p+ u. _% G$ }5 Qsystem that maintains the existing a, i- n, D3 o3 h* e$ @! Y) ]' c
HEADING SELECT (HDG SEL), A mode of the autopilo: Z: ^5 j. G3 y e' ~: f7 a
system where the pilot selects the desired airplan4 i# W2 W3 Y0 z: {9 t/ s& r
heading.
; F/ ?4 L( y7 t( ^) DHEADWIND, Wind or component of wind coming fr+ ~0 b8 c7 L) E* d: b, b/ w
the direction of airplane travel.; ~! |( B8 w+ C, h. y
HEAT EXCHANGER, A metal component with many7 L! I4 g. k3 i
passages through which a fluid can flow for coolin
7 F, J. r- ?- F+ |# dheating one by another.8 h7 V. Z. ] g6 E
航向保持
* o# j, y9 b Y/ M* i) J* b自动驾驶系统保持现在航向的方式。& Z, V. M& J% }8 a
航向选择
" m( t. P3 [1 u& K* ~5 g; Z自动驾驶系统由飞行员选择航向的方式。
4 u1 i2 _" }& {/ ~" W5 D, P顶风,
0 W' P) w* X# g5 u' B' L: o/ J `来自飞机前方的风或风的分量。
& H0 ]" K. K: K. A# S, I9 \3 O- `热
' j% j; N" q8 v4 A流0 q$ k3 \; O6 m. H
英汉对照民用航空词典B OEING
% `) j4 V( {# T8 ^" ]7 o" ?2 Y/ x. [7 ~" KTECHNICAL DICTIONARY 75. N) N' K! |+ \. T
HEIGHT ABOVE AIRPORT (HAA), Is the parenthetical0 d! e: }8 t: D+ R8 o* G# a. X
figure following MDA which, when added to the airport
& t' i, |) l" k) \1 `; ?7 g2 T3 |levation, will give the MDA in feet above mean sea
5 G' O6 R- X$ h0 I1 j, ~4 V8 Fvel. A HAA will follow a DA or DH only when there is6 p! |) t: O( e, K$ a7 P/ J' o
o touchdown zone, runway end, or threshold elevation
, D4 y0 ~: ?' D+ n3 B4 N), IS the. |4 r* K; x7 M; U$ B4 D( X
arenthetical figure following DH, DA or MDA which,1 u8 T$ ?7 B4 @6 x( B) ~1 \9 n
hen added to the touchdown zone, runway end, or
6 A# d2 X) z" J& w* Greshold elevation, will give the DH, DA or MDA in feet
" Q: L2 s: w8 j: Q* `& G) ?cy of one million cycles per second.
$ O$ S" _% I: s' HEXADECIMAL NUMBERING SYSTEM, A numbering3 ]4 E! Y& q. g6 ^0 |' e2 B3 P
ystem with sixteen as the base. The system includes$ q9 ~' J- d% x- m. u+ n
igits zero through nine, and letters A through F
* r9 ?" x- H$ _: ]) k5 \9 Y) rpresenting the numbers ten through fifteen., i7 u3 g" f7 T
IGH FREQUENCY (HF), The frequency band between
G) N, O* s2 Y6 q, `场标高相加后即是: \- F' A7 Z& c7 F0 W. j
DA高于平均海平面的英尺数。只有当接地区跑道顶端或5 a. q; v0 X" I* C, Y
道头标高不可得时,机场上空高度才跟着决断高度(DA1 H( N; n6 g3 x) ^ I# @
DH).% @5 O6 {8 R: z: v% t) e( H! R' K
HAT),0 ^4 j' S( g$ V: R6 }1 R
最低下降高度后括号中的数值。它与接地" _: T* H q) M* n# d" x+ o7 d o
、跑道顶端、或跑道头标高相加后即是决断高度(DA,, J1 @" x' U" q' d
H)或最低下降高度(MDA)高于平均海平面英尺数。
/ W8 Q. a, v' M6 y9 h) T/ X的最低天气条件同时公布的。- T1 h G! I* u- q4 o
率。
- @: C$ T1 ^# i4 Y" q% t: R" q一种以16为底数的编号系统。该系统包括由数字0至* j( y2 z7 B: {3 r8 G4 L# I0 z
,字母A至F代表10至15. V6 U5 g8 S4 k* r, S! m( r
频(HF),
9 }1 Y# Q: q f* b( D赫之间。' Y% X. L, g- L. [, o$ j
e: w4 O- J: G) y/ G! K4 K
le
% x( u/ x/ N* V7 F Un1 E4 j7 \$ G5 p9 w' j! p
available.. o4 T1 s' ?- l5 P( \! \5 W F
HEIGHT ABOVE TOUCHDOWN (HAT/ k3 d4 w8 _, T* Z' B
p- S# r, g( j0 [! N5 c* T
w
\$ ^4 D( [& m, n: M6 qth
5 U8 a' e3 c' ^above mean sea level. HAT is published in conjunction
/ b% n0 l0 M5 {3 C( iwith straight-in minimums.
! r C1 l! \, }# vHERTZ (Hz), The standard radio equivalent of
]' z8 i1 r! m$ B: mfrequency in cycles per second of an electromagnetic
2 [, J+ Z3 M+ g. C$ S, e+ swave. One Kilohertz (kHz) is a frequency of one
# ~5 H1 ]! H4 C0 m4 t: J ethousand cycles per second. One Megahertz (MHz) is a
, v# o( T3 }( F% C1 Ofrequen
" O6 H# K1 p9 ?! nH. j! m) U. J, N' _8 W
s9 {" ~8 a, j3 t- G/ M5 E( k
d: [; c2 v: e! r( h6 A6 M6 S, n
re
3 o- O, a: m, X2 [* K: TH
( j/ N A7 ^4 b p6 a% I/ v- P( O3 and 30 MHz.: n% w, R& Z8 h( F: d l: n8 G
机场上空高度(HAA),+ w7 y& a o' u
是MDA后括号内的数值,它与机* G; X, |: _/ V: Q3 A
M
2 I9 L# @% |: v9 D) K跑& o- U& a9 r! M$ \6 \- j: S4 G
或
! E" u9 H8 Y2 C) P: i) i3 q% g离接地点高度() o# @7 [! D' X
决断高度或
1 V# T X: l; b区
9 D* K. u# B t" M2 MD
5 }6 n, E: s: Q5 S0 Y接地高度是与直接进场着陆
. ] a4 G6 r2 P# O赫兹(HZ),9 d* V$ B! t8 d8 B5 k" ^0 U
单位是周期/秒的电磁波频率的标准射电当量。一千赫
+ z9 F0 U. c. W7 ]/ o% p( W0 T6 e兹是每秒一千周期的频率。一兆赫是每秒一百万周期的
+ a' b, q. C/ p* ~! Y0 W% v频# s. S$ D H/ L
十六进制编号系统,
3 R( W7 t9 C0 }0 v99 ?$ h6 L+ _( c0 o5 E2 Q
高
$ L5 @* m% V* I5 b- `频率带在3至30兆
3 ^+ t/ l$ H% b$ q: \, v英汉对照民用航空词典B OEING& O7 b Y5 d7 ^2 F: P
TECHNICAL DICTIONARY 76: r2 A% Z- R) w0 Y: [
HIGH SPEED TAXIWAY/EXIT/TURNOFF (HST), A long
. j8 R. W! e8 l/ Q; x( z3 | K K4 sdius taxiway designed and provided with lighting or
( W; `# d- a6 N" [% F karking to define the path of aircraft, traveling at high6 i N" A6 i+ _% g% A6 W7 K6 Z' J
p to 60 knots), from the runway center to a, k5 e3 Z& B% {' |5 E( [
the center of a taxiway. Also referred to as long) |# \# ]3 _, f2 S! ^4 A& z+ J$ u" y
it or turnoff taxiway. The high speed taxiway is
6 f0 u; x8 \4 ^# k4 M( e% r5 gfter
! E Q- Q5 k. a [+ c% _ancy time.
0 S6 S) ~+ J5 q8 }6 ~$ n- i5 x3 ^r a+ K9 X2 ]( X; V H
eavy component during removal and installation on the% [ n( E: v) b4 m$ y& ^) z; A/ V
irplane.% d8 ~- X* i0 ?
OLDING, Airplane maneuver to keep the airplane from6 z i& [0 j/ w8 D
rogressing along the intended route of flight.
/ P; c: x2 o0 ] _/ `OLDING PATTERN, The predetermined maneuver I1 N5 h o# Z% F
c control.+ e( [7 Y, Z9 l9 w# d# F2 W
OLD/HOLDING PROCEDURE, A predetermined
8 L) Y" _3 D/ g/ V" I$ M3 M0 _: Maneuver which keeps aircraft within a specified$ ?, R: M' z1 A/ ^) x- @
irspace while awaiting further clearance from air traffic" F! g2 a; s- u0 s6 C6 e
ontrol. Also used during ground operations to keep
) b) D: u, y$ ]" fircraft within a specified area or at a specified point
' ?7 P& v7 K% Nhile awaiting further clearance from air traffic control./ c0 [; v4 Q0 U6 C5 ^8 {, K
he standard holding time is one minute at or below
- p0 y8 w1 \* r0 f; K: E) @$ U4,000 feet or FL 140 and 1 1/2 minutes above. The
; i* R3 A' `! G# f- w+ r; t5 x! Q$ Oeparation between 1 and 1 1/2 minutes is FL 200 in
2 e- q8 t3 z: Y, l+ i, e(HST),
: a' d- u4 G" S6 U" T道。该滑行道有灯光和标志表明飞
`7 c3 B; f- v. {8 B( ~( {% T, e# t从跑道中心到滑行道中心一点高速(可大到60海里)通
: T) W7 U1 F7 |: N I* }* D的路径。也被称为大半径出口或脱离道。高速滑行道的
& M+ a. E' x' u' c- D2 N% {计意图是加速飞机着陆后脱离跑道,从而减少跑道占用
7 H' m% D8 ?/ n$ x3 U时间。 h4 A9 l3 w# G4 \
安装过程中,用于放下或抬起$ N% f# [: E8 W7 F3 T
动机或重部件的装置。* J3 h4 j9 |- o! [
待,! Z$ X0 Y; Q/ d9 H* ^4 b! E7 S
使飞机不按预定航线继续飞行的机动动作。
- q- _' H$ i3 x8 h1 _3 G待航线,. q1 l3 _0 d/ o5 s
处于指定空域内等待空中交通管制下一步调度
& |; E* V: B2 ?9 x8 C等待程序,
$ W: f. q- O! o7 h4 {保持飞机在指定空域等待空中交通指挥的下一步许可
7 `% \* X& e* W" T! C的预定机动动作。也用在地面操纵来保持飞机在指定的地, Z1 k" l5 M( V1 N J- x
区内,或在指定点等待空中交通指挥的下一步许可。标准
5 C4 v5 i. q" \# L的等待时间是在14,000英尺或高度层40以下时1分钟,
) @# W0 D0 y" m8 u5 ^- _" l以上为1分半钟。有些国家以飞行高度层200作1分钟和
* ]# O, R5 p! C1分半钟的划分。
; l2 n6 f. b" O0 C8 @$ }; g$ xra
' C" i/ C2 c7 c8 c( w3 L. im$ W, Y8 `" G3 Y! w) ^
speed (u
* x j. _! |5 m9 m. F% ?5 qpoint on& ]! \) a' h, s6 J
radius ex( |3 i6 u3 t, ]( s0 s: ]) _# |
designed to expedite aircraft turning off the runway a
! T! h, [2 w' {8 [3 w' Z) vlanding, thus reducing runway occup
5 b9 e4 S0 U( m% nHOIST, A device for lowering and lifting an engine o8 h) h7 d8 P" D* S
h
3 a g+ B* n" S$ d; a! U0 G, v* ga
1 U: |/ }9 b u) W9 o: t# O) GH9 ?% M% D- E3 N8 R" R$ a8 Q( K
p+ ]2 X/ L5 ?5 h+ e' U N
H) S. C- g0 E8 w: ~" L5 ?* p7 L
which keeps aircraft within a specified air space while: u" R _. b+ O% ]# y$ R2 M' o
awaiting further clearance from air traffi
) `, T. x7 E7 cH
* }! `* E: s- x" Om: H+ [3 t7 c: N: S: I
a
/ @7 K G4 \" u; y, tc1 `) A& `. R, | s
a/ g: A# j2 @4 {5 s- a* a
w
: k" f' N) l/ ?! {/ t2 b7 |T6 z- w4 u% F) ?) A$ Q2 O
1
5 u v! G+ x! g/ Ps" Q. o9 q) e' o: \5 k" E' T
some countries.* k9 b7 _3 C) }) Y( q2 V" [, s" k
高速滑行道/出口9 z7 @% a9 K+ L1 t+ @
是一条半径大的滑行8 _& I9 l6 {6 ~& e, N9 s# L
机/ k) ?) x- [' n, |4 M
过$ b) k. R3 w9 Y* S. a
设
+ m7 @' f2 ~) [( t的
9 B- z5 }: x+ O; A5 S' b3 {吊车,( e; ~7 o: V( U6 O
在发动机或重部件拆卸和, V u r$ ]) j1 V0 v( r" O
发
8 x7 Y8 V; f h9 @1 T+ }等
! J7 ^7 `" {( z/ N$ [# p等
( Q1 l$ Q" h6 S U- f使飞机) x% E, w! v! s+ m F. v
的预定机动动作。- I) w" ~/ p* p+ g
1
3 W7 ~ f; G* i英汉对照民用航空词典B OEING `7 T [+ b% H6 a4 D
TECHNICAL DICTIONARY 77: Y) r* K" `5 W" T
HOLDING FIX, A specified fix identifiable to a pilot by3 \; s! e) g7 k- Q6 T
NAVAIDs or visual reference to the ground used as a
8 ]( L2 V; {- ?: W3 @) oference point in establishing and maintaining the
$ {( E, O& K4 U( B- rosition of an aircraft while holding.( D' u0 @- p% q: w! @8 ~
OMB, A hexagonal material made of metal or4 [7 q o0 ^3 W3 N
omex for sandwich construction of panels.
, w( t! F( M6 @) uHORIZONTAL STABILIZER, The moveable horizontal
1 ?- N. A4 i% [7 Y, W' S) q5 Dsurface of the empennage used for pitch trim.5 r$ E( n3 v$ k" D$ A
HOT BATTERY BUS, A battery bus which is not7 B- R" i0 y+ U' P- y
switched and is always energized from the airplane- R7 w+ j* `# Q: B$ R9 I7 j
battery.& S( ~, l# Y! E7 q
使用的一个指定. P/ t: z- m* g0 }- O$ K8 O( X2 i9 \
位点。飞行员可根据导航台或地面目机参考识别该定位! |2 h/ C5 O2 W7 ~1 c# d7 y! w
。
! {4 S, G9 @% y5 |3 o窝,2 s0 [+ R7 g1 F" k9 i. V9 Q
一种用金属或Nomex制成的六角形材料,用以制造夹芯
* H1 r& ~1 o. _. Y! A6 F% T8 Q$ I板。
# y/ i4 e4 R) w# C6 o) L水平安定面,
0 [& O% d: r* {, v* Z. M' P8 B飞机尾翼的可动水平面,用来控制俯仰配平。
& L y% D' m3 Z, T" ?& r热电瓶汇流条,
+ X6 g+ X2 u1 X$ T6 O无电门控制的电瓶汇流条,始终由飞机电瓶供电。
' n7 G/ w ]0 A( p/ ?+ H4 Rre5 w ]4 t6 U, Z1 e, a4 ?
p
' F9 _- z7 C2 fHONEYC+ D" Q+ {% r$ l: x
N; ~6 z v* e$ s2 _+ i9 A
等待定位点,- {$ U8 G6 l! }* l7 Z8 L, W
等待过程中在建立并保持飞机位置时# b) D. h: }7 [9 P. ?' a
定: @: F' y$ B' ?% K! o' k$ ?+ g
点
$ h, I: C3 o6 C% p& g蜂
; D% X7 X. I, q0 p8 |2 q+ p7 m面
8 {8 X; E- a, q) Y, Q英汉对照民用航空词典B OEING H+ ~! ^" j$ |7 q s
TECHNICAL DICTIONARY 78
7 o+ I# d. h, F$ l& m& ?6 C/ qHUB CAP, An external covering to the axle of the main8 y( M4 @8 Y" y/ _3 j, @0 i
landing gear wheels./ a# ~) \' i. B% y# U7 P
HYDRAULIC FUSE, A device in the hydraulic system: o4 P, B5 D! D* G4 m
r stopping fluid flow when a leakage occurs in a line% K& S' C2 g; Q
ownstream of the fuse.$ G% x1 H' _! M$ u4 L; O
S, SEE - INDICATED AIRSPEED- b( [4 f& k/ Q1 I9 l8 y
ER PLUG), An electrical device for# [; @6 M' q3 g2 e+ X# M/ f
producing a spark in the combustion chamber.6 K& [" o4 }! L3 U: Q% Z9 z
压保险,. ]/ G" I! C! ^. N
液压系统内的一种装置。用于在保险的下游管线上发生8 s, }* ?! _' G5 ~+ C
漏时,阻止液压油流动。) i. r& x7 |. O
示空速,% L3 v, d. d* n4 Y5 \& y
见Indicated Airspeed
/ h! U9 c: J kfo
x% Q9 S, c) o* a) w3 D1 b# jd
' s! @: {* K# \! \5 x. w MI IA, E8 L; ?2 }; p/ p
IGNITER (IGNIT* Q' g& f# @( u0 N/ o9 `% q8 q- y
轮榖帽,* Z# g o1 @% H1 e
主起落架轮轴的外罩。7 b5 H* a! a0 t7 b5 }- n7 i, \+ Q
液
& S L, e+ U. z6 F6 l4 ?; a泄( v" ~: V7 W# l! b; E
指$ o0 y) {5 \9 J! @6 ?/ \
.
2 S1 A) g0 K0 D+ J' {, P在燃烧室内产生火花的电器。
' d" E# O6 S" x5 w点火器(火花塞),
& X, e# v+ u" a) T& h1 T4 b英汉对照民用航空词典B OEING
7 U9 c0 h5 t: |) c/ k6 YTECHNICAL DICTIONARY 79" n9 y( ?& L, G- T0 w E0 ^
IGNITION EXCITER, An electrical component for* z+ r; }( k$ [4 L; Y( }
supplying high voltage to the igniters for producing a
# `+ X& P$ V5 d3 B% B5 @spark.+ x! k9 @3 _2 r/ m2 y5 `# a- I
IGNITION SYSTEM, A system for starting or continuing
% q4 }5 {, M f. m1 R& R& Y8 Wcombustion of the fuel-air mixture in the engine% y9 S- D9 x5 \% s2 K& M e
combustion chamber.. J D! V* L8 \& t" K% L+ I
S, SEE - INSTRUMENT LANDING SYSTEM
# N4 C5 z' O7 u+ r/ z, P, Q3 G" `PROVED CLIMB PERFORMANCE, The rotation and
, x; P8 k6 Z. G. ~" n6 |+ wlimbout speed increased above normal to increase Z! d0 }& @. m: D) ^/ O
DICATED AIRSPEED (IAS), The airspeed read
$ M$ y( t1 ~9 ?8 Q& |3 v5 s' ~8 Z火系统,
7 H9 v( c" h/ r一个使油气混合物在发动机燃烧室内开始或继续燃烧
" q/ ]3 l! x9 S0 [' R" M! ?系统。$ y2 x! c: t' r5 [8 {# r( l
表着陆系统,
: e& ~: w( V/ r2 \) Z, N1 t- Itrument Landing System: V, d) s. \. y c( [' T# D- v, c- O
ILLUMINATE, To turn on or to provide light.
6 e! c3 S" Y/ C$ Z- tIL/ N, r" k$ E D) Y4 n) o* E9 P
IM6 W: M$ K% Z6 [
c
" t* R+ n/ \9 H+ g" Q. Uairplane climb performance, especially if an engine
. l# I; x$ q, f( h6 G0 l9 bquits.9 e( l; u+ m7 z
IN
. G- `, [- R7 u! c0 t9 S" h( ?directly from the airspeed indicator without any
& t% n; S, u* g$ f% Z3 tcompensation./ h' A7 I9 y7 j: ]
INDICATOR, A component for showing quantity,# A9 y- B {9 a% G9 o
pressure, temperature or position by a pointer or
* J9 l* [5 S# ^0 bnumerical display. (Similar to gage (gauge)).7 g( V; {% ]5 y' { g; l
点火激励器,+ \; o3 g5 n, V. k4 N4 F$ Y9 u
向点火器提供高电压使之产生火花的电子部件。7 w5 Z, C# H7 ?9 f! L& {
点
& C9 Z- x* s9 }% D3 E, i3 }; L的0 |4 {4 q1 u: W4 ]& F6 D
照明,
/ b+ n8 C3 f) ?打开或提供灯光。# p/ a: i+ y9 ] A. k/ X% D
仪. v$ C0 Z' u6 O2 J: J2 T
见Ins .
) A8 v7 r3 B+ O# P7 q8 T, ~* I, @进爬升性能,
4 p3 S, D" c+ N" f/ O R/ i用大于正常的抬轮和爬升速度,来改善飞机的爬升性& y* E. A. r" [" A2 s
一台发动机不工作时。
o# \" F0 Y" l; @* ~+ J示空速(IAS),
" W- S; }$ R0 O( y6 A9 J3 M" ]" ]正直接从空速表上读出的空速。
$ b. [* p, i, v, b- O K指示数量,压力,温度或位置的部件(与) b% _, w6 z' I- ^4 S/ [
计量仪类似)。
& m8 c% L3 D0 A- m% \9 L4 I改
/ K! ^/ F$ @; Q: d/ b+ C9 M能,尤其是在
) R( h. R, f- ~3 @+ a- i* { Y指- |$ M3 Z8 K8 ^- F, A
未经任何校+ j6 t e9 }+ q. c
指示器,
/ V) i, g H& w0 l% G) B2 F2 A用指针或数字来* C: B9 V ?& X, j1 }
英汉对照民用航空词典B OEING8 D) k! U' i! W+ U8 j, m& G& Z
TECHNICAL DICTIONARY 80
9 G- g- A7 P5 c8 hINERTIAL REFERENCE SYSTEM, A self-contained,5 U; e0 d$ @7 r, I" H' y; _+ t
navigational system based on the measurement of
6 j' j0 Z# W7 Dacceleration and attitude.
+ f0 N$ J7 F l# R7 pINFLIGHT PERFORMANCE, The performance of the
g- u Q3 R W! ~* T# ]& C- Q9 @ IITIAL APPROACH FIX (IAF), The fix which identifies8 ]7 s) o2 w& R2 l2 c$ Q
e beginning of the approach to an airport.( F5 l$ T a, f2 n0 f
LET GUIDE VANES, A fixed set of blades in front of
. n: Y& j' t: b# _n engine compressor for directing airflow to the9 w$ B6 j6 v1 E! j
ompressor.
3 U0 B# R1 x' k# `! F$ tNER LOOP CONTROL, For autopilot operation this is# b* `! r4 j( D& w+ ]+ c
e basis control of airplane pitch and roll attitude
& l+ w( O% n9 |, N" n, H$ c- X中性能,
( x2 ?; C1 W/ L) K飞机的性能。5 S5 {( a8 m3 _; {
起始进近定位点(IAF),
* e6 S4 a' Z+ Z% Y. J标志向着陆机场进近开始的定位点。
) L% a0 {: r* K @# [进口导向叶片," C( _/ B* s& v8 W
发动机压气机前的一组固定叶片,用以引导气流进人压
3 V! t- p( G- ]1 }3 q5 M气机。+ u5 l% l+ h2 s' C8 ^
环路控制,/ \. [) n# S: N9 ?; `# R: A
对于自动驾驶仪操作,这是无关飞行航道的飞机俯仰姿
0 E" P, @: I9 M制。3 b1 _ d7 N% ?' j/ R( O z9 X
aircraft while enroute.
, U* I: }7 j }2 e) jIN
. b+ K. f0 [, P8 {9 Tth* f8 {/ S1 ]) d4 s1 Y. f: k
IN. U- v! h& F' m' ? E$ x
a
2 o( ^, a6 h3 {7 J2 P9 K9 ^2 Jc( y8 [1 F. ]0 Y% I# A! m! Y# v
IN' \2 s0 J6 ]% A- J, n: n- ?
th/ D; l8 R2 q' S
without regard to flight path.2 H- Z& o- k% k' d% ^7 O. w6 g: a
惯性基准系统,3 P5 o6 }" t/ U% G* W" g
以测量飞机的加速和姿态为基础的独立导航系统。" K+ m. {4 f$ {5 Q, ?9 ^2 a, Q
空
2 M2 F1 f/ z. u2 P# N. y飞行中- f5 l: v8 n1 }) g" g
内
1 W% r9 c2 y* @/ x1 s- Q态和坡度的基本控
B7 {, c8 \6 `6 O0 F英汉对照民用航空词典B OEING
% e: M9 z. [; `" g* H: J Z* n9 Y4 UTECHNICAL DICTIONARY 81
1 i" S* R1 w" ?3 }1 uINNER MARKER, A marker beacon located between
. [/ m1 r! k% @6 q9 a8 Tthe middle marker and the end of the ILS runway.( V) o6 P( @$ [ K# f1 B9 `! O! T
OP, SEE - INOPERATIVE
, o0 `4 [2 |9 J7 S7 n# VOPERATIVE, Not working or operating.+ U0 C4 H1 b6 U* Q; F# a$ ?
STRUMENT FLIGHT RULES (IFR), Rules governing4 Y2 Q7 F8 W: g6 t
e procedures for conducting instrument flight. Also a8 P) g& Z6 r4 Y H
rm used by pilots and controllers to indicate type of
. r' d6 m7 P6 D! xight plan.
, F+ t$ z* a/ H8 R6 D+ A! CSTRUMENT LANDING SYSTEM, A precision
8 {$ g$ p+ D( n) z# _; r- O4 I: W; fstrument approach system which normally consists of7 a% U- a2 g; V
e following airplane components: localizer receiver,
" t5 |9 Z0 Y7 C) \/ vlide slope receiver, and marker beacon receiver.3 c( I0 F1 t0 k$ r) l N
OLOGICAL CONDITIONS
6 y# ~+ g }) r+ wMC), Meteorological conditions expressed in terms of
: e3 k- f4 z2 _9 Eisibility, distance from cloud, and ceiling less than the, b, ^6 n Y( }
inimums specified for visual meteorological1 F1 j: S7 J0 L
itions.5 M! p# x: L0 P1 q Q9 T
STRUMENT RUNWAY, A runway equipped with% R2 x* |5 L( N: _2 x$ b! U4 f
lectronic and visual navigation aids for which a
8 }* X+ k: ] f, X. t$ y5 {) grecision or nonprecision approach procedure having1 n0 [2 L, I2 j. X$ }2 ^
间的信标台。 q! k3 I, m' U0 G2 d
不工作的,
; E1 z: J+ {: I' L- j# b; ~# O见Inoperative, {0 i `8 B: {0 F+ i6 b% t
IN. k0 @& \/ b+ S" I/ k: ]
IN) t* {1 j0 i5 u' n
IN
1 r! n' D! j( N1 {" L- g* v& |th
0 |# S$ t( ?' Q" b9 jte, k5 @" x0 B: [. q' V/ h6 W( [+ X9 ~
fl
- }/ Q* r3 Y6 o% G/ ?IN
% e( \0 P- ~) l- X1 F# J z+ oin
+ J+ Q( q8 L0 C: [th5 X: o+ A' R( Q) V
g
* \) t4 c& F$ @' DINSTRUMENT METEOR- Y A2 A* B' E3 j2 @% j
(I$ |' m; |6 \% h& _
v
+ T. |' [4 _6 rm# {( g2 S" _, [& P2 o
cond& m: z) E3 h8 N+ _7 X6 H
IN1 v8 b+ t0 g; |9 Q$ W) Z' |6 T% G
e
5 t; ]) o2 _: T1 ^4 p \p
) v/ \" c$ X% W i s2 }: Dstraight-in landing minimums have been established.) b. J7 e6 J* F& N7 K1 u
近指点标,# [: [; H; y$ d8 N
位于盲降跑道头和中台之: G' t9 g% n5 S8 ^! S7 v- Y6 {
.
# B3 O+ l# Y. p7 c8 g8 N" W不工作,
3 o' q3 ?3 y9 m. [/ K& g不工作或无法进行操纵。9 U: i$ h5 b2 |
仪表飞行规则(IFR),* G1 k0 M/ C$ ?7 M. ~# B. \! J. s
仪表飞行程序所需遵守的规则。& X5 y# O# S- g( f! D! a
仪表着陆系统,
$ n% Y0 E* o* @8 O- N' l6 ?一种精密仪表进近系统。一般由航向道信号接收机,下
* Y% u! {$ d- ~滑道信号接收机,和指点信标接收机所组成。
7 z& N# r" F# }- x* W以能见度,与云的距离,和云幕高低于最小规定的目视! D" k# U! q# q. t/ z6 q& Z) I2 b
象条件的一种气象状态的表达。& U8 {( t4 e: G, r4 i* W
用于以精密或非精密进近程序作订明最低天气标准直
% t8 v- T/ p: x& r着陆的装备有电子和目视助航设备的跑道。6 O6 ~; e9 n) d. Y
仪表飞行气象条件(IMC),, [1 a% ?! I0 {; [ _
气
8 J" m6 T4 L. s' z8 G+ _仪表跑道,
& ]/ f7 [$ E1 c( Y% D线* j5 E: K3 g6 D. ? e2 S
英汉对照民用航空词典B OEING# [8 b3 i9 P" B6 k9 O1 y; w: b' X- [. w
TECHNICAL DICTIONARY 82( T3 K2 _" ^' g
INTEGRAL TANK, A metal container formed by the
% s# s. v9 _0 S" D4 @ qlane.
+ _" X, D3 m3 n0 ycted
) D: E R) ], E: r" p: kcircuits.
" h) O0 ^! g1 M: fManual
. }( l5 F' E9 V( ^6 \# l9 ~0 Q1 Derformance data providing range as a function of a9 w3 T5 J1 n0 t7 A; l0 w7 l
hange in airplane gross weight.
$ q8 Z9 N/ B( T4 X" F! nTERNATIONAL RESERVES, Reserves required by
3 |( i! `7 p k$ {( T3 {, ke applicable governing agency when flying
. v6 q3 r4 S) R; O4 t$ q& dTERNATIONAL STANDARD ATMOSPHERE (ISA),, c+ E3 E( o i0 K8 t+ {
he hypothetical vertical distribution of atmospheric4 c& q3 G; X8 j, D4 Z8 u
mperature, pressure, and density as defined by the& c& U. A t" J |' l& P1 R! K' h' f
).' [3 ~8 z, }+ h' R/ N
TEGRATOR, An operational amplifier whose output
o: T7 h4 E( ~' a7 D; u. foltage is determined by the input voltage, the input* {0 i8 V4 j1 U
上
P% [) x: g! y3 o8 X存燃油的金属容器。
; U0 Q# `9 P' B. o3 w% f4 N6 G,
- O: O' T+ x! n+ k- Z飞机总重量的函数提供的性能数; R5 h* L0 g: L5 q2 ?* Z
。
0 o0 c8 h2 S, P% |) N! M际航线备用油量,
) P) |" y/ n9 d% j在国际航线飞行时,有关的政府单位所要求的备用燃油0 Y! x% g! K" Q7 T- S
际标准大气(ISA),
3 L$ g! |* y0 J1 g A国际民航组织(ICAO)规定的,一种只在理论上存在5 y% T! t; W! r) K) Q) @2 J+ y
大气其温度,压力,和密度的垂直分布。* C) x# H Z" R
分器,. r: I3 ?- U& I( U
由输人电压,输人电阻,反馈电容和时间微分而决定其
: F2 J3 |) |8 U. ~4 I; H4 G6 ?, n运算放大器。
- a% @8 j$ j" u/ i6 E' I" y1 bwing structure (spars, ribs, skin) for storage of fuel on8 K( |& d5 y/ y- P6 t
the airp" Y- p$ ~0 h# ]7 R' Q. a& V! P# t
INTEGRATED CIRCUIT, A small piece of1 q2 k6 j+ A/ Q
semiconductive material that contains interconne8 {5 A1 f+ p* p/ L: }' b
miniaturized electronic5 U2 S$ \$ t3 w- U- D) o
INTEGRATED RANGE, Tabular Operations1 R5 n& l3 H. _, N( C
p! Y$ F0 c, E4 ~3 r. o7 y# Q# ^5 U
c. R/ q$ q% q0 z j( Y( c ^( h
IN
0 w$ H6 }( r' j6 W {. E. zth5 I3 `& R; S, {: B6 Y
international air route.4 M8 p4 h! d- {7 Y, s
IN% G9 y; ~2 @8 t( l$ \
T
) s/ f. w4 t2 p+ Hte
$ C* p) c- P+ W" nInternational Civil Aeronautical Organization (ICAO
; a |" P8 j+ _& E+ g- d7 mIN
9 M+ f" q# T' Bv( u! `4 q$ `4 M
resistance, the feedback capacitance, and time
; K+ L3 W! A: @ ]differential.: b4 _! k: m0 N- p' s8 ?
整体油箱,2 B8 v4 ^+ h8 n8 S2 `. h4 T& Z
由机翼结构件(梁、肋、蒙皮)组成,用来在飞机
1 W$ G4 h4 c4 D0 b6 {! n$ m+ h储; q* m% ^3 ]0 C6 b- P
集成电路,
( x# @2 n% t- {6 r% I+ k一小片内含相互连接的微缩电路的半导体材料。( @( Q1 O3 H2 X$ M+ E- N* [% s
综合航程
2 s/ F* S9 x4 i- O6 c8 ?* w0 [2 r' a1 s使用手册将航程作为* F5 ?: I2 L( `7 ^
据
: H0 `. v! F: Q. J9 V6 B国) c6 [! U) ?7 l6 o0 ?5 N2 q* g
量。! o' w k4 c |8 N+ i& ~
国
1 ~0 ^! g$ P! P- C* U的
2 }$ P2 o8 E4 k D, I积
! E/ C8 T9 f* L' E' v/ Y输出电压的+ m9 w) k5 z. n: f
英汉对照民用航空词典B OEING
8 Q% B/ ]: a) `9 X6 j: M" Z2 r& XTECHNICAL DICTIONARY 839 Y% |' `0 a& V+ I$ p ?% o
INTERLOCK, A wire connected in series with an5 _% D, X7 q4 W" k+ T+ ? D
equipment or device, or a condition that allows1 T- |% A* w* O, c% Y5 T
operation if all requirements are met.
3 q. ~' ^# X7 \: r, if the United Nations whose$ S( X% j% V" G8 d0 E I
bjective is to develop the principles and techniques of/ y4 E" e0 _, W
ternational air navigation and to foster planning and; v. @) ^6 A; @9 m. T Q+ c
evelopment of international civil air transport.4 y' h2 n: p" Z' ?+ d, K
TERROGATOR, The ground-based surveillance# {* B( L8 m& y% C
dar beacon transmitter-receiver, which normally scans
" F1 S" v# B v A2 n0 A( Oll
' i4 k. N6 i1 q# L8 l9 O% N7 Don the mode being used to reply. The* Y6 r& O1 M. k$ k) F; J" W" v X
plies received are mixed with the primary radar, R l9 j. ?- A' [+ }
turns and displayed on the same plan position radar7 n8 `1 i/ A; _+ D
cope.0 g8 M; ]7 s, d
TERSECTION,
# P5 `0 w3 ?% J% k, Q6 G1. A point defined by any combination of courses,2 d% k0 {# M: w8 _, @2 I7 i
radials or bearings of two or more navigational9 ]" p9 O* z! s$ x% H* C: w
aids.
9 O" N# N2 \6 U1 Z, P2. Used to describe the point where two runways5 ] {* x9 s' G8 m# U: L
cross, a taxiway and a runway cross, or two0 \( ]0 c) d% x$ X, [; F
taxiways cross.: ?8 W8 P u. F. b
cy)/ V3 F2 u3 e% l6 r2 ~
tem.
3 Z- P% A4 f9 L3 Z0 P0 |/ U6 ~者5 N3 w4 h( ? ?
当所有条件都满足时才能工作的状态。
0 k5 J" P' h; I4 P( x组织,
" U0 K$ D& b" L7 g0 }: t航的原则和技术,促进国际民航- t- n( {( I4 ]5 W# }
输的计划与发展为目标的联合国专业代理组织6 U3 {( O, G) D+ s
问器,0 Q9 h: c3 g( r/ S' ?
一种地面监视雷达信标收发机。通常在工作时与主雷达
. [% g9 j4 h: Y( j3 z' T连续的无线电信号,不断地重复要求与* ]0 i' d- H" u/ \
接收到的信号相混合,显示在同一平面位置的雷
) N4 G7 U) n- |/ Y, T: ~达屏幕上。- r) O* i! A9 V9 A
交叉点,
. u" F, G/ z* v* d1. 由航线,径向方位线,或两个以上的助航设备! K( a: _/ a7 L) o5 I1 T
的方位交会而确定的一点。
% L& b* L/ ^3 F2 Y2. 指两条跑道的,滑行道与跑道,或两条滑行道5 j2 i# b; D" Q: K
的交叉点。) t- r6 W" t* h* h& u5 L8 x$ A' b
INTERNATIONAL CIVIL AVIATION ORGANIZATION,* [9 X; ~& d2 s5 [! Y% s0 R- y6 i6 v! @
A specialized agency o& t/ P/ A8 c- I+ v/ S1 ]7 C
o
; ?# P5 d4 C) S1 E3 H, f" Rin! ?! {) W; i8 s5 f8 W' J4 g0 t
d
3 E% j) l$ H( Y+ gIN
- _4 W6 {( ]9 \/ H5 lra$ `& _) x* y+ ~; ~
in synchronism with a primary radar, transmitting' U7 L* j6 Z3 v4 m# C) c& C0 v
discrete radio signals which repetitiously request a
# h* [* Y- x- x4 k2 ~transponders
+ u" G( y0 ? s3 m, Vre# D2 {6 i5 n' e
re
$ K! H2 [+ u4 z8 }$ T4 t, v' Gs& d7 C3 A2 c5 I O
IN
: V7 ^3 L1 z. @; X7 f/ UINVERTER, An electrical device for changing direct) k/ A% i. O6 ` u r
current to alternating current for standby (emergen
3 d& q* k; Q1 g& \9 x5 ^) `power supply to electrical sys2 V/ L& W; z. N; e6 w! B' }
联锁,
# P% H# S1 I+ g一个以串联方式将仪器,设备联接在一起的电路。或
3 }! [! e# Q' g+ J是
$ h& D _$ e5 `: \! `, E8 F1 k国际民用航空
; ?+ \ D! |+ X, B9 i一个以增进国际航空导9 l: s/ q5 W, y8 T, T. q
运
! n/ q6 Y3 W: d8 f8 f+ |询
9 ^/ u1 ]9 `1 ?' ]) y同步扫描,发射不
' F% ?4 A e6 g8 o, q其工作方式一致的应答机进行回答。所接收到的回答信号
: @5 P1 u# f+ B' b: n与主雷达
6 R8 h9 G: `; P! s+ S变流器,
0 Q- I. i# i5 @0 x) S用来将直流电变成交流电;以供电气系统备用(紧急)
3 w8 ~$ t7 A( {: L( n电源的电气装置。
( N* w0 R6 h0 N- p. U r英汉对照民用航空词典B OEING' p4 w- b" r! @! p4 ?* G6 S3 p+ C
TECHNICAL DICTIONARY 84
/ o2 i% S- l I, r3 U# z2 g/ y- I+ t# [IRS, SEE - INERTIAL REFERENCE SYSTEM8 B$ i X$ D( {$ ]6 S
ISA DEVIATION, The amount of temperature or
; t0 Q; M0 }( I- z, V: A5 Ysee International. J8 }- U# x& z* ~+ I) `* G
tandard Atmosphere).
- p$ q ?# K$ SLAND RESERVES, Reserves required by the
8 U1 N) @4 d- a p" g8 {) X) A% gpplicable governing agency when flying routes# e; C) b/ E1 R, _
etween islands with no alternate airports.% Q" P2 w! I) ~$ w9 y
CONDITION, Cabin pressure (altitude)9 H8 i! r! W" ?( s, K
maining constant with changing airplane altitude.1 f* j2 ~# f+ b8 c
ising the9 A) d6 G0 _; e1 N$ J3 h$ A$ U
a: p/ C7 m4 ~$ y- G, k8 ^* H
,
$ ]' g6 x& u" ?pressure difference from ISA (
+ I; A0 W S4 B) y0 v4 m3 D! CS
: L+ [, q- @ qIS
7 F9 j/ ^- a) z1 Ma
( W) a9 ?. x. j& ~# i7 B- {b) B$ Y5 `) A( g+ X' ^ ~
ISOBARIC
1 z5 M2 V! Y$ D1 c- Z' V9 [/ W! ore. h& J: ^8 {9 \; v0 l; G3 S
ISOLATION VALVE, A valve in the system for0 ^6 I# T4 K2 y+ y
separation of the system into sections.
" f+ y$ |! `! A5 U f+ lJ
% H$ D* I3 B7 lJACK, A mechanical or hydraulic device for ra
" f7 J) {; S3 a8 j" }airplane.: d, r% X* {) @) G+ l8 G
JACKING POINT, Location on the airplane for using* _: Y4 j& W5 @2 s! o
jack.5 _" v/ q4 i Z: Y& h+ i/ }% g
惯性基准系统
" o4 p+ j7 C2 o2 f- h见Inertial Reference System.
# @7 y5 w) n" r8 f* n与国际标准大气之偏差,1 h5 P2 C& [( {+ s9 @$ X* t
压力与国际标准大气的差值(参见国际标准# G8 j3 A# d6 j. _) r' o' G
有关政府单位要求在没有备降场的岛屿间飞行的飞机
4 A% w" c5 }) [! b" j8 C6 z带的备用燃油量。1 Z2 p A4 U# `( n
压状况,) o O" ]) M8 U$ \/ { k3 P! X( y
在飞机改变高度时,座舱压力(即座舱高度)保持不变
% u( x+ X7 ]" |/ ]5 ~状况。
& I* a: h4 U7 ] L% s斤顶,
' `4 [. l: J( _, a# u3 a7 J+ Z3 |用以将飞机抬起的机械式或液压式的装置。
0 d- U& ^% E" J" a; ^$ h! s温度或
+ u/ h( l$ e8 Y" H8 X) P/ P大气)。
/ `" u4 L" N' {7 e2 U. ^5 X" Y岛屿备用油量,1 T* E: \3 T! ^- E0 I! v
携3 F9 K# i4 s2 o) ]& j6 B. x
等
4 Z" r9 k% O8 p0 ?的( C; \5 r6 w7 l& E6 S5 p
隔离活门,& {' P3 Q$ q3 k
用以将系统分隔成几个部份的活门。; v" ?6 v& F/ q' \% Y5 z/ a! _" P
千
3 T- T& S7 @, I( x& A千斤顶支点,
1 C; u( J: K1 B: G飞机上可以让千斤顶吃力的位置。- v3 P' r% m3 E
英汉对照民用航空词典B OEING5 v. x' `: q! b. T
TECHNICAL DICTIONARY 85# q5 d) D5 w8 |' j- S4 z: L7 G
JACKSCREW, A rotating threaded rod used to drive
+ c) V2 r6 w% Omoveable component such as a flap or stabilizer.; S$ |9 Q( D* K B. N
a 致动螺杆,
, u3 u6 P' p9 [用来使可动部件如襟翼或水平安定面运动的能够旋转
6 q! t0 O8 N9 w" i% H: T的螺杆。
5 E, _. r- o/ [& T' R2 v英汉对照民用航空词典B OEING
x, K l5 o0 R7 [* E0 r) o2 PTECHNICAL DICTIONARY 86( }* W! `* B h+ K
JET PIPE, A control component in some valves and7 e+ R+ f) @; g a7 g: _
ET PUMP, A component in the fuel system, operated
+ s$ C* x; q. y- Or removing water and fuel from a fuel
% O9 i( Z3 l; I4 E7 ` _nk.
+ R4 f4 L9 e! [! U) G q. v射泵,
6 o% {1 V) c& h8 ~2 B! a$ x内,由燃油压力来操作,用于从燃油箱中排除2 x; e# G. t* q" L" U3 x% _) P
和燃油的部件。" Q2 R" c2 _9 P; f- `, k; J1 P) s
actuators for controlling the flow of hydraulics or) }% H2 ^* `) ]% L4 |5 Q2 L
pneumatics.8 a/ _8 y4 P; D
J. j8 L7 e" s4 a! g0 w3 R+ p$ a
by fuel pressure, fo
1 i7 `+ ~) C- T0 L7 @" G& ` Kta
# W: s2 R7 K' t喷射管,* ]& V* Q3 k0 C
在有些活门和作动筒中的控制元件。用于控制液压和
0 @ L, ~' m, p- J# O1 ]气动的流量。
- v, h+ x5 z; d K0 J6 M引
/ T) e( l& d; ^5 A8 x% ]$ r9 M* U燃油系统
! Z; m+ o, d/ b1 m: W水
% f# M. P, A, A3 R& I" ^英汉对照民用航空词典B OEING
+ H8 r! `. L; N+ xTECHNICAL DICTIONARY 87
- r. K9 p6 z- ]; B8 i) EJOGGLE, An offset in sheet metal construction2 ]& s% j4 s% ?3 ^1 y+ T
designed to allow one piece to overlap, either higher or$ i I5 {6 x( F
wer, the other piece.1 o3 m8 B! u2 B5 V$ |
OULE, A unit of electrical energy of 1 ampere of
8 W) L2 Q9 j( b) h+ @urrent passing through a resistance of 1 ohm for 1
) p, X' [% r: Q4 V! y$ Uecond. Ignition system energy is measured in joules.0 H+ O2 q, J' t, b
UMPER WIRE, An electrical connector for temporarily& r% } S3 j2 I3 R$ n
ypassing part of an electrical current.
: e& }' y0 v6 U, g- wUNCTION BOX, A container which serves as a joining' e# g& t$ Z! U3 j
lace for electrical connections. May also contain
! ~/ U; C" m1 \6 N8 hlectrical components.
/ E8 s& g$ P0 mEEL BEAM, A structural beam in the fuselage center
& h: n5 a4 W1 A9 P* K3 W& Y& vection (wheel well and under wing center section) to
0 L' @; _+ y! N9 ~$ RKEVLAR, A light, strong synthetic material for5 p' S( Q. j. O- R) G
secondary airplane structure.4 O R x% B: z& C
,使一件金属与另一* s* u: d1 D1 Y& K
相互叠合。
2 [0 g* @' z7 R, @. v耳,
$ T( J$ |6 A3 ^% a/ J' J电能单位。一安培电流通过一欧姆电阻一秒钟所需的电
% C8 I5 y E; ?5 `3 m) E7 @为一焦耳。点火系统的能量用焦耳度量。
: b1 A) `/ u4 p `1 M2 G接线,7 q. e( I$ J8 C" [) I( d" l% r
用来暂时旁通部份电流的电器连接件。 G$ I) }0 N, p! h
线盒,
( b$ t! ~" D) Q9 S ?做为许多电接头的汇集处的容器。也可能内含电器。
' s# L: z; z+ ]% p梁,5 n/ l- W0 z8 {' \
机身中段轮舱和翼下中段,用以防止机身弯曲的结构。
! g3 U& A) S2 q. P/ \* G3 f" yKEVLAR,/ I" X( G2 L$ i* h5 L& Y/ c
一种即轻又强的人工合成材料,可供制造飞机的次要构
# C+ [$ \; |0 Z. \件。
6 W; @, t d. j* qlo& Y5 ?# D( X. t( }- [8 K
J7 \4 z( W+ Z- f
c
& }- x* V+ |$ O, z0 B/ Is
3 Z$ f I) [* a0 ~6 Z& c: G8 FJ
3 ]- R% t8 W( ]2 ~5 Jb
5 r4 W$ o! u) x( bJ: L3 B2 K! n" k- k( F! ?9 E9 e4 l
p7 F# X( h1 W+ a" p( D* ~% _
e& d. M: g4 l: \* U8 G6 s
K) F, }, h8 M/ w& X, L- |
K `3 e0 e0 I" F$ S4 a! w
s* _- E T* ~, |9 [* y5 w2 L5 d8 `4 Q
prevent the fuselage from bending.
9 ]! L* F* x. _折接,% f0 c! L; q8 I, }
一种平面金属结构设计的弥补法
% ?6 r1 i- e U( }件
2 _, j; C% S, g" L' b% x. f焦& Z; \* ?7 z& Z* Q
能
+ o6 `' `' T2 [; n- k9 q跨: [" p+ T8 e0 H. _# a5 S
接/ g3 e K3 y( ]; t" j V$ {
腹
' F% G- }) R$ X% X英汉对照民用航空词典B OEING
0 ]: P, z M, q x, zTECHNICAL DICTIONARY 88
4 ^5 U1 w3 e& DKILOWATT, An electrical energy unit, equal to one* u8 y- I: t# ]/ e2 X! W
thousand watts, for specifying generator power output.
3 c1 z: _1 ?; T0 v5 l1 MKINK, A sharp bend, twist or dent in a section of tubing,
. g/ H. a5 G- r' W/ gwire bundle or angle stock.% e( h: Z f- E3 J$ P
KNIFE EDGE, A very sharp edge on drilled or machined
9 S* u. N7 Q% H* Ametal which is usually the source point for corrosive
" B1 h" s& ~& _4 w. Battack.) J; l8 L m3 w
KNOT, One nautical mile per hour.
( q5 m A+ L8 P/ H+ B( aKREUGER FLAP, A type of leading edge flap that is1 B2 S S* K m
fixed on the lower side of the wing and rotates forward
! P" V) c/ D8 d3 Z. l3 N! X# ^into the airstream.3 p1 N' G$ Y$ s5 j1 L% x
KW, SEE - KILOWATT
& v( g5 N) M$ V3 V* }% E! YL
! ~0 m4 ~- d) p# M8 \LABYRINTH SEALS, Rotating and stationary
, U" P( @ i3 F' Z, I" a1 Z# d& z: t, Zoverlapping structures which utilize differential air
% H& h9 f5 m+ d9 x! E' }pressure to form an external seal. Most commonly used# i9 `- D, E' U8 G+ L5 m! B
in turbine engines. o" a, s2 h/ ^9 @( [, B
扭结,
$ ?& y6 z8 E" r/ v2 y/ \在管路,电线扎,或角材中的尖角,扭转,和凹坑的部
$ C) P' {3 y! [4 d份。; s" Z8 r* e) \6 u+ [; x% m$ C( z q
刀刃,
+ P; N- h4 J) k钻制或机制金属的锋利边缘,通常是腐蚀的开始处。
! S; C* O- ~/ t9 I节(K,KT,KTS),- L: X }6 q7 b0 w# L
每小时一海里的速度。6 d% C0 P' Z, o9 y* h) _
克鲁格襟翼,+ M" |' X2 }( d& T6 ]9 l2 T3 ]" K
一种前缘襟翼,位于机翼翼根附近,旋转前伸。/ O0 M. N8 |& A+ K% e
千瓦,
4 b1 U; Y# N! v( {见千瓦(Kilowatt! M7 n' M+ g O8 d; ? L+ V
千瓦,
* [" N6 B) J+ c2 f$ J2 C+ Q1 D1 H电能单位。等于一千瓦。用以确定发电机的输出功率。# J$ G- d/ p6 N& z6 b+ a# e$ x
)。! t0 {- O6 i$ U3 f4 i) J
蓖齿型密封装置,* N3 z, N0 x7 B$ G, l: z
旋转并且固定的重选结构。用气压差动而造成外部的密* P. m1 w( A! i
封。在涡轮发动机上最常用。
$ [% m1 Z" W3 s$ T) G英汉对照民用航空词典B OEING
( m' i# l' F) O, y" d+ j7 c9 CTECHNICAL DICTIONARY 894 V& f) W" r3 g2 F2 B7 p
LAMINATED STRUCTURE, Composed of layers of a7 I7 x [6 i* X# Y9 |. C n2 C
ake a
7 G( Q; ^, V* L( Rht structure.
$ A- r% l- I/ i7 v* |/ c- l2 s4 w.E.D., SEE-LIGHT EMITTING DIODE.
1 K: h6 f$ m6 L$ {3 F6 LANDING GEAR, The nose and main wheels with the
5 V9 Q! z0 Q$ g O$ X' gttachments for supporting the airplane on the ground.
# R6 n# D2 d# @( ^LANDING GEAR DOORS, Panels operated by the
# u2 I) r s3 F5 t3 f! u4 s4 Ulanding gear for closing wheel wells when the landing
3 C* o f4 T, ~& N7 ?gear is retracted.) M0 V) f3 k: j" y' \2 v+ Y
LANDING WEIGHT, Gross weight of the airplane at the U$ |5 Z% |5 z1 {# J+ ^0 @
destination or alternate airport.
0 c% |, R a! ^/ s6 ]5 G4 e7 x发光二极管,
; o! O7 M2 u) t8 G) F; [见Light Emitting Diode
' Q: Q4 x. w' c j9 h8 U6 qcomposite material bonded or cured together to m
4 b2 ?7 w- O; j" c# c) b/ Z+ H( }strong and lig& n( E/ A) F: L" A. ]8 ]: b6 Q
L6 n y7 @& R3 _! K5 E6 n5 a2 D/ ^( ?/ Z
L
( f; X% [. |2 c3 w6 Y# Aa
. G3 y: C7 _9 I: g分层结构,
, q# c4 L) Y- D$ I& g) P# P/ d一种牢固而轻的结构。由多层的复合材料胶合或固化而 w+ d0 u2 d$ u
成。
5 t; `6 j6 l0 O1 ].
8 y# }" [. D7 f0 a$ @: q$ o起落架,
% P% t! D2 _, `; h2 h( p9 t s用以在地面支撑飞机的前轮,主轮及其附件。
* b, d. ~. A; v u3 l4 s2 \! I起落架舱门,# q* P3 B# ?1 ~
由起落架操作,用以在收上起落架后关闭轮舱的面板。: K! |& j. s* l& \: g* k. C) |
着陆重量,
7 s6 h( o' E0 b: o: d0 ]5 k飞机到目标机场或备降机场时的全重。8 p2 L5 [$ Q* A3 f5 e/ ^* Z
英汉对照民用航空词典B OEING# e0 W! U1 w ]/ U
TECHNICAL DICTIONARY 90
% O4 \% l5 I( R7 jLANYARD, A cable for supporting or holding pan
/ ]' Y! ]0 J2 G' f& Eopen position.
2 X5 X6 h# @* L0 x0 |" ]els in' T. }6 [7 J8 J, c) s
AP JOINT, An overlapping sheet of metal, joined to the3 f" e* p" [& i
dge of another sheet in aircraft structure.
! V) U6 z" _0 E' m: dASER GYRO, A gyro which uses two laser light beams/ i; Y T: }3 F1 ~/ n
measure angular rotation.
( G+ W* b/ I3 G& z.. X% D9 Q0 k0 ]# v& w& n, E
ATITUDE, Measurement north or south of the equator
5 L6 o1 D3 ]; @5 H ?s, minutes, and seconds. For INS equipped+ V) N! `0 q% T" f" i
degrees, minutes and tenth of minutes.
! L/ o. M7 P9 l) a8 y0 q U- }l device for. R' m% A# Q: e3 ?4 l) d" |, z
hanging stored chemical energy into direct current.9 j1 u" J% E+ j5 Z4 m
ses lead, lead oxide and sulphuric acid.8 y5 v/ A4 R W! v; i7 x! C
搭接,
' y: y7 @) o) z飞机结构中与相邻金属薄板连接的重选金属薄板。+ b3 Q7 T d; P" A# y* Z7 Q0 j2 {
激光陀螺仪,
2 k, F I7 h/ m; c$ d. p" b一种由两条激光光束来测量旋转角速度的陀螺仪。. y7 ^. ^5 J* m2 W9 H
用以紧固或锁定的装置。- f. H. \/ n: N& ^
的轴。
; U. }6 }0 o0 j2 x8 c方式。% y, C: {# o9 x7 \
度,
3 F$ A ?/ L" r1 X2 W H% i4 ~地球上与赤道平行之弧线。由赤道以北或以南度、分、& {) c/ p4 W' W/ g) }
度量。对于有惯性导航系统的飞机则以度,分,和十等
- | ]. F; C& K, _% k" ]' h9 c- x度量。
9 F$ y2 B3 `' ]/ S酸电瓶,4 a" w. ^7 L% g8 H8 A+ W0 G1 L
将贮存的化学能转变为直流电的电气设备。它使用铅,
7 h. z4 k% [5 O& h8 v* M化铅,和硫酸。
: V4 F/ u5 Z9 h( [9 \: e. ^! s( o$ b3 SL+ F0 z9 G2 v* E' J5 ^
e A) f) _% {# d
L
& l$ X7 M8 q6 c+ j( k' xto4 t1 h! t& I, }2 [" P
LATCH, A device for fastening or locking.+ ]( V" T( l8 B. \; A1 o- i
LATERAL AXIS, An axis passing through the airplane's, p& l G- O* N* _8 Z3 r# ~
center of gravity, from wingtip to wingtip6 i( H* o/ L/ v# J
LATERAL NAVIGATION, An autoflight mode in which0 T; t2 Z# _( ~& i; g) v
the FMCS is used to control the airplane roll.
- a3 w+ f3 o" a2 L3 H4 X+ i1 E3 Z' lL
5 l4 d4 w) t3 v! [) qin degree) R0 M+ k- n' q% L
aircraft in
; ?" y; m6 Y7 w% c8 K! N' D* aLEAD ACID BATTERY, An electrica d1 w: ]" o2 E. T0 ~
c/ _# }( a, Y, m* v& e2 I
U6 L5 T" m# j: M! K3 l, q
牵索,8 @) `/ D$ `$ `7 @) J& G# |/ x' i5 C
用以使面板保持在打开位置的钢索。0 u: j4 d1 U- y9 S. E; W
闩,
' X# Y" y5 Y: p横轴,
; Y3 ]% v! b1 Q通过飞机重心从一侧翼尖通向另一侧翼尖
d. \; c# V2 j+ p" _8 ?3 q# J水平导航,
" g* v, \( `6 v' _( Z( X' r! j! J% h8 E使用飞行管理计算机系统控制飞机横侧的一种自动飞/ R! ]/ a( ]' g# M
行
. [& x4 n4 ]' v/ { c0 @) w纬$ M* Y7 H* J" y8 Q- w1 W2 T/ z: m L* t6 M' S
秒6 j( u% _! I/ b; ^) ]- `
分8 @. {* N, }/ D, `. L% P/ D( x3 |
铅4 g- S5 {, n9 Z% ^
氧
Z- Y% \2 l( r+ l英汉对照民用航空词典B OEING
8 H7 H8 H L: L* _+ m HTECHNICAL DICTIONARY 91
1 A; X a0 T* t+ s1 Y( tLEADING EDGE, The front edge of a wing, stabilizer or
A& N/ k" G* b7 y0 {* m. OED, SEE - LIGHT EMITTING DIODE& y p! G% y+ R' Z+ ?: M
EMAC, Acronym for Leading Edge of the Mean
1 W5 ]: F) ?. ^0 p0 o" ]0 d6 I5 Berodynamic Chord.
/ Y4 q. v# k# _ n7 f7 gIFT, The vertical force produced by the airflow past the
A' B l. m/ |" m3 N. Y& Ds of the wing.
1 I5 x( y: k V6 v7 eIGHT EMITTING DIODE, An electronic device which
6 b" A$ P: x& V4 y: w( j+ Utes with red, amber or green light when supplied8 c; C% o; @2 x# ]
ctric current.
I9 w+ y% F8 Z# V) @,
) K) Q: ~, V8 {: K! ^control surface.% S& O) [ U9 ~! ^; {2 _+ g- l
LEADING EDGE FLAP, SEE - FLAP: `( h7 N; m N
L: f" e! r; V* o& @; k5 R
L
9 t& D- f# p* a% MA
# k6 D: k; E& ?( m( pLEVEL-OFF ALTITUDE, Altitude of which the airflow
0 G! p- ]1 n# @past the upper and lower surfaces of the wing.2 \% P2 z" _" s+ h
L$ T# n ^5 H h; E/ n
upper and lower surface& E; B9 Z- |% v$ ?
L l0 Y3 g4 ^, \8 B
illumina
( w3 g+ k& [+ w! F8 {6 mwith ele
9 l1 s& S3 }9 x8 U前缘,
9 J( \ e1 W3 u: Z6 ? K机翼,安定面或操纵面的前部边缘。8 M1 _# |8 z/ H- d! k/ {
前缘襟翼
+ i6 @4 i1 X" Q: L# X q2 c见Flap.7 x5 v) `! m! I6 s: C0 W/ t
发光二极管,
: c5 ]& n3 I9 B* \: d$ W: [+ }ht Emitting Diode! ^, Q8 F+ K0 g$ q7 _$ p1 _
见Lig .
( y# F4 b) }$ o% V! z( p; ^; s均气动弦前缘,
5 e6 z u, ?1 v+ F平均气动弦前缘的缩写。见Leading Edge of the Mean
( z* c! w' R5 H- A/ ?% l8 R平5 y9 e; @6 ~" {) E" `* E8 ?
Aerodynamic Chord.
* t/ I( A: i* u3 Y' y力,
5 E A. U4 |) p# m R' \' x过机翼上下表面所产生的垂直力。: x9 j3 y8 v9 n: }7 J+ F9 O7 U
光二极管,
. v) g9 g0 b( v通电后能发出红色,琥珀色,或绿色光的电子元件。
, V9 S$ ^' f) ~1 g i4 T; l: e, q* j% i改平高度,. k6 o# y! Y6 e/ H% ]
飞机因巡航时发动机发生故障而下降至的高度。
- d- v" L( O+ h/ i" b. o升
: N1 i0 ^. f/ g& g3 D) b2 W气流流$ U* k: e, q8 d- O& g* E5 ]
发
" r# D: v) V4 |! K C( O英汉对照民用航空词典B OEING
! ~6 [1 d. H* ^7 m' CTECHNICAL DICTIONARY 92
Z6 z& `3 Q% L3 _1 O1 ZLIGHT PLATE, A component part of an instrument
# P- [: w2 c2 o9 z! w, B" ^panel for illumination of words on the panel.# v! u; s: U+ b& a1 b& p* ]" b
LIGHT SWITCH, A switch which contains a light. The9 }: q, V9 M7 i" I( B m
opened or
9 X; v/ Y9 u3 M) {7 q Plosed.' A! J4 |. x* ~$ B8 g
n electric actuator which turns off electrical power to
& k8 w( U; G- i% U: n& o& ~e actuator when the actuator reaches its open or
" l9 M# ?0 b' Z1 R slosed position.
& Z4 I- C8 c$ z# AIMITATIONS, Performance and operational limits7 k9 p+ o5 L, b. c. L
sted in the Airplane Flight Manual (AFM), such as+ U" d! u& c; f- k
aximum airspeed, maximum altitude and center of
# r: g3 g% c3 C. [6 zravity constraints.; ~. t$ a% K c, [& p- ~
y9 Q) a5 Z- x4 a D5 {$ K# N
craft during line maintenance$ x/ v5 L7 v8 ~6 R0 g
perations.4 p! r" f" m9 h1 ^& n
ontrol+ U" ~3 _1 D: H% }
display unit allowing control of information to and from
( t- M1 M `3 uthe scratch pad and designated areas of the display." H7 o6 P8 o" p* @4 g
光电门,- _: Q, w" t8 \$ k
电门开关而决定灯的明灭。
4 F3 T4 R1 f5 I1 \' H1 L在电作动筒内,用以在作动简到达打开或关闭位置
4 T' o0 }& G8 Q" ~4 ]5 a, A: q时,切断电源的机械式操作的部件。
1 a% x8 H$ Y) ^各种极限,3 c/ q( o* Y4 r3 n0 h8 l2 |4 q. I
飞机飞行手册(AFM)中列出的性能限度和操作极限,1 p6 z: C3 n) t6 |
如最大空速,最大高度,和重心的限制等。
' W# s" N* w. b' l; B2 Y在航线维修中,可以在飞机上即时拆换的部件。
) T4 C; N1 q! W' q飞机管理控制系统的控制显示器上的电门,可控制草稿
$ ^$ I; ^3 I8 c- C# U% h @栏和指定显示处信息的输人和输出。
& P' {7 d& n$ Y$ q2 N9 Nlight either turns on or off as the switch is8 P, w- @) R, Y# _' Y
c
; ]3 O# ]* E' R- W% }. [. TLIMIT SWITCH, A mechanically operated component in
" e* V3 ^$ f" ~' l8 V- za
& T9 N; d: U6 d1 j0 y. W, [th
8 n, U: `% r% L" G% J" jc0 t# M0 b$ Q3 j1 c% w% j) a
L. m" [) ^% ]2 C* {( o3 q
li- ^; s( B% U6 \6 Q4 T
m$ q# G% T! u$ z0 e" c$ s& g
g
' A/ s( I- {/ Z3 {. kLINE REPLACEABLE UNIT, A unit which can be readil3 d3 |; g+ K2 k4 e
changed on an air
$ W5 P' I$ w( Z6 `2 M% po# s) C% |5 _$ l# H8 ?& e) ^
LINE SELECT KEYS, Switches on the FMCS c+ Q' E0 D! A! Z8 l a8 |# c( E
照明板,
, Y/ o# O4 e4 _( l仪表板的一个部件,用以照亮仪表板上的文字。+ c F/ ?& z/ Z. g; [0 s
灯
$ H, J9 o' f( N Q" {" r6 r带灯的电门。$ u" [3 X5 w. c) f- D
极限电门,& g# X* O: H& C& q# ?5 o- P
航线可换件,
5 J. q( [/ G) g# m" P行选键,
; W+ C# }6 N( z( r0 A英汉对照民用航空词典B OEING# l+ y) J5 J, d* `' [/ A% r7 \
TECHNICAL DICTIONARY 93
5 x# Q) a- B5 W2 T% Q5 o J8 [LINEAR VARIABLE DIFFERENTIAL TRANSFORMER,
0 D# I" c# q$ B) E9 D9 nnsformer with a linear response.
3 L$ o- ~. `$ s [' jNAV, SEE - LATERAL NAVIGATION' \$ `# n! }0 y) p- X
OAD AND TRIM SHEET, A form containing tables and
" F4 s5 d$ J& u* Qharts to account for the weight and balance effect of all
& {/ c) ~. t( ~3 P) jpe of an
. {+ P0 U( V$ V( t$ RS approach, normally located at or near the point of
( ^/ q: s- V$ H9 Aecision height.. Q* R) H' ^' R& X1 N: w7 a5 r
er
t( A9 `: u+ a0 \( S/ Meacon at or near the point of glide slope intercept of an
1 n& C6 ]- n- kS approach.
3 B7 t. _1 U. i) X4 i% fich provides
9 [: ~8 t$ k1 z) _& `" p/ ?lateral course guidance to the runway.' t$ `: z, b. F- b. [! [
差动变压器,: ]3 u h' Y4 m: s o) n: O$ Y
平导航,% P( Q, t9 t" l/ F. a
vigation) h; D0 i! N5 U/ L
A differential tra# P3 w# {3 S, \$ g/ c
LINK, A short connecting rod for transmitting motion.2 a' T& d" S$ p4 j+ ?! G/ d
L
, g; @; X" o0 P( EL$ M v1 Q/ X ~+ D6 G( L
c! I: j( M" q- O- s
items and fuel loaded before each flight.
8 c% T7 Z8 o3 x2 QLOAD FACTOR, The ratio of the lift being produced by
9 a7 b* O4 w( e, H& vthe wings to the weight of the aircraft.* V% X( _/ X' ]
LOCATOR MIDDLE MARKER (LMM, MM), A marker
$ A c1 x3 D% L I. `beacon that defines a point along the glide slo
/ k" J. B5 S/ I( o1 z1 uIL0 k7 l- m7 @8 x8 ]$ a @: L" U; @( N
d
4 |. k+ S! }4 I2 O- \9 T1 \5 D/ `3 mLOCATOR OUTER MARKER (LOM, OM), A mark
/ U4 p m) E; D! P& E; K4 Zb
& k; p( w( f4 k8 q) _IL
" N. H o/ V; [# a' F; F( T7 mLOCALIZER, The component of an ILS wh
/ _" P6 q# \ [& R6 ]; @$ j线性可变) [' |# {/ F+ \, A L* |" |5 S* ~
具有线性反应的差动变压器。
! ^& V6 I7 N+ ?% I连杆,9 ^# C ?5 }& u; Z6 R% Q- E
连接在两个部件之间,用以传递运动的短棒。
4 Y6 U/ X( P" a p+ ~# m水
5 }1 ]: E! O4 x5 \见Lateral Na .
; W" A8 v# W5 E5 s; J7 z3 v( p重和平衡表,7 W( j/ {, E a0 z
有着显示每个航班前飞机的各项业载和所加燃油对重
5 r; z8 x9 q s1 a1 r( O( O8 ?衡影响的图表的一种表格。
0 }: b* f% n4 K,9 t. t& b( q! t7 f- }2 @
附近的一点的指点标。4 ^, q1 i u0 i) Z4 K
近仪表着陆系统的下滑道截获点附近的指点
0 \0 ?8 j8 \3 \6 `- E) d. h。
0 N: u4 k5 z' f* D0 k+ O! a仪表着陆系统中的一个部件。它能提供到跑道的水平航) u: ?8 \4 [, V- N0 _
道引导。
7 a1 r2 {2 n. n7 b% l0 a载, W: G( j- Y' {& ~9 P
量和平
# S' W" Q4 q" B6 l装载系数
* c" e/ |$ r5 y4 g( k; ?机翼产生的升力和飞机重量的比值。
3 n, E5 p+ t0 T8 j' k, N中指点标,
2 H6 l9 u: Y" J8 @( s Q用以指示仪表着陆系统进近的下滑道上通常相当于决
+ Q4 N, L+ X$ u$ M断高度或其0 ^1 G: r8 C$ Z) I9 R4 K2 [* J
远指点标,
! M; x- ]0 X4 a+ Z' j; |位于或靠
9 Z* s4 Z% o* e6 ?8 D6 _3 |标
: `, o% B8 `4 Q. V& p航向道,. X( q' O3 @) E, F
英汉对照民用航空词典B OEING/ W1 B3 R) y+ ~" k; V
TECHNICAL DICTIONARY 94
4 p6 x- ^5 w r5 T9 C" }: G" T6 D BLOCKBOLT, A steel fastener which prevents unwanted1 x6 K( N3 {8 v0 h% Y7 d
rotation by using a collar instead of a nut.
$ |5 J9 k: C0 K: J( r, f8 ~6 V# ]OGIC, A representation of complicated electrical and
. a1 \1 f5 b0 plectronic circuits by simple symbols called logic; k0 O2 O) X9 J H! h
ymbols.
( k5 O. p1 n7 F% X( AOGIC DIAGRAM, A diagram that uses logic gates to( H0 \# t* v. Z) `- j; b; ]
present the function of a control circuit.2 v8 ^; q5 m1 F5 c: F% V1 s
OGIC GATE, A device or circuit which has no output- d5 P; @: Q! e1 V
ntil it is triggered into operation by an input signal. A4 R% d2 K l# W) @, ^; L1 V# d$ c
gic gate is an AND, OR, NOT, NAND, NOR, or
$ D4 G6 n U3 a: h1 m$ bLOGO LIGHT, A spot or flood type light mounted on' m5 z7 T2 ?5 o3 g, n1 g4 I5 O! Z K
aircraft structure and directed toward an airline LOGO or
0 D% R# t$ E+ m7 G, D) Zother message on the fuselage or tail surface; for5 T/ D0 i" F. A. C i/ N
visibility during hours of darkness.
) s5 v1 ?' D5 V7 @0 z% X3 M. },
. s/ V6 A( L3 s钢紧固件。: q' `. a2 I. Y9 _+ b" m% A% b
逻辑线路,
; e( u& a- B- j( C* ?7 g用简单的逻辑符号来代表复杂的电气电路和电子电路。
, b" H5 U, K8 _- L) p逻辑电路示意图,8 ~& k/ e# q$ W3 o3 H- V
一个用逻辑门来示意控制线路功能的图。
, M R; ]$ d, y' p+ c# [; o. D逻辑门,
4 i# a8 n- _& i/ c只有当输人端有输人信号触发时,才有输出的一种元件
' Q, v, ?0 T+ e0 w. }+ l或电路。逻辑门分为:与门、或门、非门、与非门、或非' F8 s5 ?1 q C! M7 l" T
门、和异或门。. c% K" y1 N1 R
标志灯,
" [- d7 b1 K. b/ Z* P1 x4 W在飞机结构上装置的聚光灯或泛光灯。用于直接照在机
- T2 j+ v2 r' f9 b+ f R$ D0 e身或机尾上的航空公司徽标或其他标志上,在夜航时照亮7 } Z3 H9 U" j8 n5 u
这些标志。
' U' w$ j5 k- v2 L: y7 z1 FL
/ C& i6 R( ~: R# F% le
% a/ q0 |( G% r; rs7 y+ ^3 H1 ^3 f2 W" b
L1 A5 b9 b, `: L z+ X
re
( r8 d6 m% {- l/ CL
* f. N4 V& A7 A1 |" pu6 p }+ m3 U9 U5 T f% p6 M6 h
lo
/ [7 A: l0 U9 Sexclusive OR.
2 |) w+ r8 q4 S/ c" q% Z保险螺栓
6 @6 n$ t6 {7 g; s0 B/ f6 r用环圈代替螺帽以防止不必要的转动的
4 q# m5 ]. \3 j, A7 W英汉对照民用航空词典B OEING
! i5 ^2 r# g6 f0 PTECHNICAL DICTIONARY 95
3 F- \* b$ X; Q7 t- zLONGERON, A structural component in the horizon
j# H1 z% B) j/ ydirection of the fuselage or nacelle.
* A( T" q3 g; ^6 ltal
^4 c! A+ R) R7 Q4 H; t( T) @RUISE (LRC), Cruise speed that is
. u( K8 a6 V8 H+ H2 v! yssociated with fuel conservation, producing fuel; r' q1 r+ g: C" _+ K7 {
ileage one percent less than the maximum fuel
: \ l8 Y; n4 i9 Tileage available.
( h( v8 G3 v5 U2 P2 DONGITUDINAL AXIS, An axis passing through the) d" C; K3 N2 u& l
irplane's center of gravity, from front to rear.
. {8 _5 C* g# d1 ]not; W% v# T( {- T: E7 s/ y
OUVER, An opening with slots allowing the passage of# g/ Q3 a) J) i: `6 U2 h {! W! a
远程巡航速度, }7 a$ N& Z! i8 Y- i
一个与节省燃油有关的巡速度。在此巡航速度下,每4 b* U; J. h7 H p
一单位燃油所能飞的哩程,最大的燃油量航程小百分之
3 l6 g% j5 l X8 u; [+ N v; V一。
; J: t8 s* p3 Z! v5 n8 Q! u9 \! y纵轴,
e5 z$ r1 \$ t4 E4 S9 p' j6 v3 S由机头至机尾贯穿机身重心的轴。
7 n/ M$ r5 d: \9 {) [6 {' M4 `0 o叶窗,
9 q" r( q0 m9 {7 |有多条缝的开口。! B$ c. W- L" Y/ W& i
LONG RANGE C
& s$ C. w! R, n& _9 T3 N8 X* V5 F6 Ta5 u% t5 C4 S: J) V
m6 d8 X9 _; l& M, f
m
; s, S# Q* P+ T4 ^L4 j% w: e6 s3 R" ], I) p2 I, E. ]
a, E3 D1 D0 I9 Y) w' u
LOST MOTION DEVICE, A mechanism which does
5 y2 {$ ~9 L% |0 A0 A) X# l$ L+ Koperate a component following initial movement of. s5 S5 W" H9 w" L1 Z; u
control input.
( \1 r5 k! J+ R; k# cL8 ]6 e1 P6 Y% A( j
air.# _: a7 K2 y: _5 b7 {
大梁,! b/ { z; t' G2 T7 h5 b$ }! C
机身或短舱上水平方向的结构部件。9 `. d) G( m+ u; F
航2 Q4 y* g. Q- k% _$ z- a0 E
比
x% z" Z d/ ]+ a* o# ~空回装置,
# c; p, m2 X# ?+ y, \在控制输人初始动作后,即不再操作部件的机制。用于+ B% b) X. H3 }& ^% h' t
飞行操纵系统内,以防飞机指令互相牵制。
1 N6 A' f1 x2 A% ?" u百
6 A! b# F/ k; c% B" g让空气流通的8 R: G0 f0 F; s+ B
英汉对照民用航空词典B OEING# g% @' r. f0 n
TECHNICAL DICTIONARY 967 I$ O+ N$ W9 R P% r
LOW RANGE RADIO ALTIMETER, A system that+ c, P( b; t: H: {# ^ i
measures the vertical distance from the airplane to the
9 J) J$ I/ E, G/ I. t- W* l- Trrain.
# l( B: l0 G) M8 N" e4 l) k- `/ vRC, Stands for Long Range Cruise speed. Represents
( g1 H5 h7 \! j- b, Pe typical cruise speed for a given jet airplane; usually
. | @/ e5 u: s! k( ?( @& Jxpressed as a Mach number.
+ m& ~( {5 X- c) B. iRRA, SEE - LOW RANGE RADIO ALTIMETER0 p2 ~* c1 ^. F) q3 Z" o% j/ l
RU, SEE - LINE REPLACEABLE UNIT$ d- O x+ J$ `9 u. l$ C
uce friction& t- u) K- q0 ^$ B# ~
etween moving parts. It can be a natural or an artificial$ c9 j4 x$ d0 e; M$ o4 z
aterial.
: y: b) U% L7 p6 FAC, SEE - MEAN AERODYNAMIC CHORD, B- z. k4 O" y8 f
ft's true+ Y0 ]+ B6 E# ^$ X
airspeed to the speed of sound at that point.$ ^9 E7 u9 F8 e7 p; j0 L. p+ i
的系统。9 o: R( s% u" y$ @
远程巡航速度的缩写。代表喷气式飞机常见的巡航速. j5 @9 X6 J2 X' c# L
,通常以马赫数方式表示。/ d( i7 ^9 t% K( A
空无线电高度表,2 I" U9 p% J) j
Radio Altimeter
5 _7 \' W5 O; tte& e9 m, c& q. q& g- F
L- N' d/ y+ o t1 q& }2 t
th1 e- v/ W: l) ?" m
e/ E" l: [. F2 [( u; f1 ?
L
" N5 L9 u9 A1 ~( WL
9 J3 Z) {5 y/ Z4 lLUBRICANT, A substance used to red' h- f8 S5 \- d: d/ ^& N4 O/ M& Z! x; H
b
) G( `) z4 V0 R5 \m
4 A& z( m$ y. D9 U$ ELVDT, SEE - LINEAR VARIABLE DIFFERENTIAL4 N. Q+ D }4 o" H+ E* M1 y. w
TRANSFORMER; I! r2 D1 [& X& j. X) b
M
6 I) ]7 F+ R3 z$ @8 ~M
3 ]4 p" _' q* t- GMACH NUMBER, The ratio of the aircra) s5 |; e. z" @& G! s/ r
低空无线电高度表,
; \ s9 U' H' B/ O9 E' ^一种测量飞机至地形的垂直距离
9 n9 B- S) c$ J' d8 V远程巡航速度,- s1 h, {& O! a/ v, ^/ r
度% Z1 o" b' `' k+ ]- q4 X
低* U) Y+ g2 A# p1 v
见Low Range .8 M: Z5 j; c3 I8 M, T* O! g& s3 W
线可换件,+ z% c# O6 V: s$ X/ O
见Line Replaceable Unit
( z% H$ _* o, b, c航
. A) V0 C4 a, f7 s.6 U2 |; f% G7 ]
用于减轻运动物体之间产生的磨擦的物质。它可以是天" ?+ c8 u5 o$ J% N2 `
的或人工制造的原料。
& e1 @* l0 Y* W0 R见Linear Variable Differential Transformer! @' ?! T. N- t9 O/ o/ a0 u
润滑剂,) K2 ~+ @5 j* l1 M2 Y# E% a8 K, L
然; b* W, y& h @4 ?
线性可变差动变压器,9 @ i+ s* L/ \2 {$ q
.
9 y; M M& R0 e7 T* y" \$ Y均气动弦,
# F; q1 [6 M/ W; Y% X4 `+ t见Mean Aerodynamic Chord$ w. a* c/ ]! |2 o# }
平
9 n+ X! W, a5 [+ A# p% g( ~2 Y" g" |6 v.
: P, c9 U4 r, j) ]; b空速与该处音速之比。
. y n( b* ?; p5 ~# U' ^ b马赫数,
$ N; v9 f: l7 M) a飞机真& a6 f. `3 A! Z$ B# p
英汉对照民用航空词典B OEING
% |0 p! \) m; @4 [; R6 a& ZTECHNICAL DICTIONARY 97* _( n& y* S* M* c& V( f
MACH TRIM, Correction to airplane attitude (nose up)( s; m, k3 y8 f+ G2 h
during flight at high speed by using the horizontal/ T$ h! ~5 C7 m: P" t
tabilizer.
+ G5 ~* s, T/ YAGNETIC HEADING, The heading of the airplane4 O; n' f9 `% T( X1 Q* q
lative to magnetic north.4 z, K# r2 O2 ~
AGNETIC VARIATION (1), The difference between3 y; U5 v7 Q0 a* g) x8 Q
agnetic and true north.; @6 d! G% I, x0 m- D+ n' c3 {
north.. e; _/ f3 S. H% J! V
here is a continuous small change of direction
3 B9 K5 F3 Q1 a wf lines of magnetic force over the surface of the earth ,9 H1 s, t- ` C6 m/ ~- K' o
agnetic variation at most locations is not constant over
1 ~1 J0 \7 ~4 |+ D7 hng periods of time. Lines of equal magnetic variation
+ h0 E. _4 j6 G; O6 u+ xe. (see1 H o" W H1 A& N1 H' N2 k1 P( S9 l
tation Declination! ?/ y0 K! i" o5 T B
s& D/ h3 w" M0 P" N
M
4 {& N; I2 J; c+ O$ N4 E0 z9 Vre
$ k2 M: `, q3 pM6 Z8 j7 F' @) Z! r( k
m
5 ?8 `# w! i% s- c) P% TMAGNETIC VARIATION (2), The orientation of a
1 S6 d9 t M0 U$ G9 l2 Ihorizontal magnetic compass with respect to true
6 T9 U5 Q2 k$ H/ m7 dBecause t
& g, Q/ T# B! H, }0 f Po8 _" ^3 q# H" s% o, _. ^
m, a0 S, l: E$ x2 R" p, y2 B
lo- f3 \' i+ h! j0 x0 n2 x$ |
(isogonics lines) are updated on Jeppesen charts every3 @7 \. Y6 T1 o! v/ B$ Y
five years in accord with worldwide practic G+ y2 \! F \$ _
S ).
- q. \# x9 i D) r i4 \8 FMAIN ENGINE CONTROL, A component on the engine
9 {1 v2 @% t7 x* f m/ yration.
# o1 D! H; Y' A' v3 n; lMAIN GEAR, The main wheels with the attachments for8 ]% H% e: d& N% Z* B
supporting the airplane on the ground.. }( y+ X" X" f& w9 ^ U9 a0 p
MAINTENANCE, Work accomplished in support of the
8 I5 N, D8 Z/ {- i1 g3 d! Istructure and systems of an aircraft. It includes,! v. W0 a$ P3 {9 Z1 U5 a$ y5 y t
inspection, overhaul, repair, preservation and the% L/ o% F) s# x' k3 k- B
replacement of parts.* q( U0 A- {: o
马赫配平,
/ c9 d9 _: ]) Q用水平安定面对高速飞行中的飞机的俯仰姿态所做的! }1 f N6 f1 Q! D
调整(机头朝上)。
% m$ Z f2 W' k4 ^0 X磁航向,. H; v$ z# o. H: n
相对于磁北的飞机航向。+ C- j" A7 |0 k& x" G! i+ G g
磁差(1),
+ S' v2 }! U4 x e) r真北与磁北的差别。/ G$ r0 M v6 f* x
断的微量改变,磁偏角在长时间内多数是不一致的。每2 Y$ [4 b6 s; Z V' f
五年Jeppesen手册会按照国际惯例校正等磁偏角线(等3 I; Z5 F' U$ m' \8 C/ D/ g
差线)。(见基点偏差)
- k& A! M- C4 X0 w. l9 s, H主起落架,3 G1 T* @) N' A0 C H0 |- M+ d# X
用以在地面支撑飞机的主轮及其附件。
9 F0 d6 q) h4 A, C% R$ n" o4 n维修,% ]1 S3 o) [$ Z' K l3 r
在保障飞机系统和结构时所做的工作。包括检查,大修,9 u0 T( v8 h3 c5 K
修理,保养和部件更换。6 x, K+ y8 |( x2 X5 {
for controlling fuel flow for starting and engine ope
* u$ j& y, w+ X4 i9 Y% [磁差(2),# N. B$ n0 p9 c" A
相对于真北的水平磁罗盘定位。因为地面的磁力线在作
_8 l* d# S- B, B" b不
5 z7 {' K. m5 P* F1 x: L磁( W% f( F! Z! }
主发动机控制器,
" G( q N/ ~# U0 [1 N; \发动机上为发动机起动和运转控制燃油流量的部件。
/ a& q/ M- Q9 |; A2 E2 Y英汉对照民用航空词典B OEING
+ S& Z# t6 f! e; d+ `2 Y& xTECHNICAL DICTIONARY 982 U# `& p7 C8 Q9 G: ~& X
MANEUVER CAPABILITY, The ability of the aircraft to
0 E# M' v, j9 kertain load factor.
9 K( m. C% J+ R8 w$ uMANEUVER MARGIN, The amount of residual
9 _. i# x6 v( H _& A2 y9 V6 Laneuver capability present before the onset of buffet.( Y) C' H, ~9 L$ M
MANIFOLD, A duct or chamber with several inlets and. O* f3 h+ }. a4 u; Y1 L
outlets for air or fluid distribution., @' n& H' `+ ?0 O$ y* [$ U
the
3 c1 P( N% a9 z$ o5 Q/ \low of
3 ^1 a! y! ?! q7 q/ ]e flight compartment. On specific
& A) y$ S- m; U, Q& t( Dccasions it will provide conditioned air.. k) D. g |" e& N1 j4 S* Q3 R
omponent by hand.+ N, ~+ S& P% _% d$ W! _
MANUALS, Books with instructions for proper
W0 l( J1 m- z) k1 Amaintenance and operation of the airplane systems.
# H [2 y0 W' e, z0 O( J) V7 I: b$ TMANUFACTURED RIVET HEAD, The head of a rivet
9 n" P) b* x) @3 U* \3 gthat was preformed during its manufacture (see upset
3 [: o8 r! _2 o6 j" b( uperform certain maneuvers up to a c
* f# ^. x& X6 l5 P4 |- I3 Ym8 Y7 p% N) e% x8 \/ R4 r
MANIFOLD INTERCONNECT VALVE, A valve in
- j @% X& W) n: }, w( Aequipment cooling system for providing a normal f
. P$ p7 p2 K0 p5 I) z/ `8 ]- V) k& Srecirculated air to th
% n8 S3 R4 ~8 H% D; k- d4 do5 W; h4 b7 i9 [# a2 @* ?
MANUAL OPERATION, Method of operating a
7 W' r. y- b! |1 W% b" Mc. O; n0 q$ h+ O$ s6 Q$ b
head).
. \' z0 V: A( \) W% w" A. Q' qMASS, The quantity of matter in a body. It gives the
! l' p. `9 V4 Pbody weight when it is exposed to gravity.
% I& d' f/ C+ |9 y机动能力,6 u( g5 e8 y# v
飞机完成装载系数达到一特定值的机动动作的能力。
" j' V% Q) ~% Q* f" N8 d机动性余度,
4 c$ \: |' e- J飞机在遭遇抖振之前,所剩的操纵能力的大小。
! |5 @# p0 S3 y* K _总管,
- ^. S/ P2 d2 B ]6 o, Y用以空气或液体分布的多进口和多出口的管道或容器。, w" j/ F0 l) A3 n, m; c3 E
总管联接活门,
2 a/ p* s2 w2 U; k设备冷却系统内的活门。用于向机舱提供正常再循环空
2 F. o% C6 ?1 v, M8 o3 O3 s/ {气。在特殊情况下会供给空调空气。) y; Y/ x/ d, y. x7 B& `' s; q/ u, w
人工操作,5 }4 a2 p! m, _
手工操纵部件的方法。
$ f9 r1 K9 b8 O4 V: |明书。
& P5 _. I- {$ ~1 S3 |& Y6 L铆钉头,! y# m. [+ s) s; B: g! q( o* e
在铆钉制造时已定形的铆钉头。(见膨径头)。
9 [; u/ f8 e) m9 D; U: s, w/ ?质量,
4 l$ r3 j5 F2 G6 g4 _( Z& H一件物体的物质数量。当该物体受到地球引力时质量产
7 _; w5 t9 c& _3 P& D生重量。
: @3 X) P5 k* Y5 Q手册,
' h7 N U ~: f1 D4 s为能正确地维护和操作飞机系统而编写的说
4 _, B7 j+ n) l; F3 Y2 I- q% x机械制造的
) G; x0 [/ L1 M2 Y1 A- f英汉对照民用航空词典B OEING
9 h+ S* b: h& ~; D3 H2 q0 K jTECHNICAL DICTIONARY 99
7 U$ W9 m& Z p4 ^, bMASS MEMORY, A memory that can store large1 i" A7 p3 S1 G- v6 S
amounts of information and hold that information: W8 T2 ?/ N# Q6 F: Y) g1 \' h
permanently.- j1 T0 Z1 a% b$ e& M% B- @
AX CLIMB THRUST (MCT), Maximum engine thrust
3 M5 n* j- n; m- V; U; Lximum engine
: m6 K, f. Q8 u c F3 rrust to be used continuously when one engine is/ l! }$ C* S- X1 S) O6 T
operative.
+ E4 C4 Q% s& ~ ]% bEOFF THRUST, Maximum engine thrust to be# @" e: X/ J" o3 w' F2 m
used during takeoff.6 z% G8 p+ d% ?
FF WEIGHT, The maximum take off9 ?$ r& P; y6 y% u. R# s5 X
weight as permitted structural limits or performance
. p2 {/ `" ? v: plimits, whichever is lower.
! ?5 R7 [0 s+ m, [RANGE CRUISE (MRC), Cruise speed
5 I, z( t8 `1 q+ Pance3 Z. |7 h$ |1 x/ d
to locate8 ~) M$ V3 f1 {( n9 P4 E6 T; k$ \
the Center of Gravity.
& F) I, T+ N( q) Z" z. z3 r$ L主控台,
6 I, p$ b4 e- T; ~' }* W控制系统操作方式的装置或系统。
! |# x* Z5 `; c9 J9 `大爬升推力(MCT),
' c5 w/ p$ l( B: X6 _) V6 t飞机爬升期间所能用的最大发动机推力。
# E* o' l$ R& M# RMCT),
# N9 v! v9 ~4 m, a! H/ z) e当一台发动机不工作时,可以连续不断地使用的最大发 B2 q J5 U' U: Z% b
动机推力。
; A5 ]' \/ _- ]1 p起飞期间所能用的最大发动机推力。3 ?2 U5 z) |" l- R& \
结构极限与性能极限两者中的小者许可的最大起飞重
# b; P! y3 ]0 u- S. z1 m。
* z3 o3 b- e/ Z# j* M大航程巡航速度,8 X1 P$ Z9 X! q5 i3 \
最大的巡航速度。0 u4 H) l# _( J1 { e
平均气动弦,- A5 h9 k8 [ A9 H0 V
确定重心位置的基准. c$ r3 H% j2 V; l- o
距离。
/ y* u$ h( f* Y. uMASTER, The device or system which controls the! `- G W+ S2 t3 C% e
system mode of operation.6 T2 \- [# D2 V! a$ |) s f' x) [
M
B* C' B& D$ d0 P/ f. h Vto be used during climb.: b9 F# p3 K9 ]$ e3 m
MAX CONTINUOUS THRUST (MCT), Ma2 Q3 f/ r' |* ?/ T: ]0 ~
th
- N5 g, L5 \1 Y3 q* lin& R3 h/ M( X( W" e g0 m7 R
MAX TAK
5 Y) ~3 [" U; e- j& hMAXIMUM TAKE-O o2 z$ @% M% E( O# _8 g! ^
MAXIMUM
9 O' B7 d6 D7 C" H; kproducing the greatest amount of range.
) A: P! @7 u! o2 n# `- c% rMEAN AERODYNAMIC CHORD, Reference dist+ f- \ t6 a9 Q
located at a fixed position on the aircraft used
5 \- U% U* P' J1 T. D7 B大容量存储器, M$ R4 e* P, E" {4 M# Y! [
可以储存并能永久保留大量信息的存储器。
* F5 z1 l) P- I% G1 T8 g' |3 O最
+ A% N ~, U, S* a最大连续推力( {7 m5 |6 ^" \$ G7 |/ ~$ F
最大起飞推力,
& f, B$ C Y( m3 ~ A2 g最大起飞重量,
: Z' W J1 k6 m' h4 Z& k# q量
! Z( X" f9 g3 |% M最
! z( Y5 I2 e& W( r+ v, L' [+ S能使飞机航程
/ S4 p2 V1 D: Q# K8 l位于飞机上一个固定位置,可用来
; h" m1 k) x$ g I! d" O3 Z英汉对照民用航空词典B OEING: ~% s* X5 q; f( c K
TECHNICAL DICTIONARY 100
8 s' K \3 u, {% r3 M dMEC (NO. 1), SEE - MAIN ENGINE CONTROL Q6 i, o' n8 s/ Z& |* l9 P$ ^% y. M
MEC (NO. 2), SEE - MAIN EQUIPMENT CENTER# u7 r) p4 Q/ U
EL, SEE - MINIMUM EQUIPMENT LIST
/ c( p4 j+ ]+ d" H- L/ \tem the memory is where
8 C# L; J. |+ z1 h; xformation is stored.
5 z! l" K" Z/ y, q. L' }: SMETER, Any mechanical or electrical device that is% a" u- Y: d. Z3 R# `8 u
air or
5 j/ u: m" x4 N& u# S! N) ypoint along the glide slope of an ILS approach. It is
# M- C' l' P& y; gnormally located at or near the point of decision height.% C j3 s5 S# S. S- @" [* p% ?% j
,
1 o0 O$ G b) t. x2 L# ?3 k0 N见Main Engine Control
' _/ t7 g' Z0 e2 i+ J/ e! ZM
& n, Q2 F+ ^; A& |: p; c5 GMEMORY, In a digital sys
. Y" m& \, @2 B6 yin6 }; Y: Y0 J( [% L% L9 g% s u
used to record, indicate, measure or sense a specific/ p( A P9 w5 i' ~
portion of an operation.
! Q( ]: j. G, i$ ?METERING VALVE, A valve for controlling flow of3 g2 i8 y( Q ^2 r) R
fluid.
0 M6 ?5 s; x( A6 k P9 QMICRON, A measurement of filter effectiveness, one% ?. K1 L5 g# G; r1 q
micron equals one millionth (.000001) of a meter.
1 q) k) U+ ^7 I7 L5 W: N# OMIDDLE MARKER, A marker beacon that defines a7 h! E# v" ?# x7 _$ }( J
发动机主控制
7 n/ B( X, `, {: T; ]- p.3 p6 T. z5 `: a% A. C& E; o" Q
设备中心
, m. n* Y+ P$ x E+ C9 N# h见Main Equipment Center
8 Z0 O, z6 y+ h1 ~% ^总
0 @4 l9 m; j4 y% e- x! D, B/ X$ E.$ v0 E- h6 d3 X* a
低设备清单,- p1 L5 o' t, Y( W$ k7 F
见Minimum Equipment List
2 L- |6 {$ K3 I- B" j3 l6 j最
, d, }6 n' V& `% ^3 _- Y) ~.* a8 P6 m) Y1 U1 C6 }' d% E
在数字系统中储存信息的地方。
* O# @" Q4 \& k4 I& O: }9 X; [7 ~* A计量表,
' @" x/ J9 a" L9 ^$ ^0 W) j用于记录,指示,测量,或感受一操作过程的一个特殊0 A4 s ?$ @! s9 k/ u* @$ H& Q7 o4 _
部份的任何一种机械或电子装置。
+ q' d ^9 v0 M& a7 G量活门,
/ Z# A! V+ I8 Z6 Q3 p# Y6 ?' |用来控制空气或液体流量的活门。
" @9 W7 k! Q6 a& q微米,$ _3 d0 i @$ E3 Y
过滤器效率的计算单位。一微米等于百万分之一米。
: A- F; s/ c' J8 b在用仪表着陆系统着陆时,用来确定下滑道上一点的指- j/ r; M6 }2 z
点信标。它一般位于或靠近决断高度。
/ K7 Q( d8 s; S存储器;
/ F$ O" v& @/ V9 I% c2 w计* r) T7 g6 d) r* N6 w
中指点标,! q; {* b5 L! N' y% [0 m
英汉对照民用航空词典B OEING o0 C: l. ~( _% J) W7 g1 N
TECHNICAL DICTIONARY 101( W+ h; W; _" |
MICRO SWITCH, A miniature mechanical device that
# g" W+ s; L" V* j9 s8 Zcompletes or breaks the current path.
( [, t2 E. T6 A.1 R" W. l: m2 s* a5 g. l2 X4 M
MIL, One thousandth (.001) of an inch.
" ~, P& r, k/ I2 bILLIBARS, A unit of barometric pressure equal to8 @1 J/ [6 ~1 w- p# d
approximately 0.75 millimeters of mercury.
! f1 L# m6 c1 J8 v# K/ M8 xThe lowest; R5 t+ A" i3 R( n
ltitude to which a descent is authorized for a& L. P$ |2 P( A1 ?3 Z. c3 E; \
onprecision approach.
4 T0 O8 `1 b9 N6 u( h# q. GINIMUM ENROUTE ALTITUDE (MEA), The lowest
. g5 ]( q! ]% S( r/ d5 Z' rublished altitude between radio fixes that meets
) x( B% F6 V4 J/ Q. _7 nbstacle clearance requirements between those fixes
. N0 y# N0 d, pand in many countries assures acceptable navigational
* f1 E0 t+ e# {; z7 F rsignal coverage.
# D4 y- P1 e2 e9 u9 Eoperation of the airplane with certain systems or
! o2 v0 B5 S9 ]) t1 {subsystems inoperative.8 W: z3 @0 {- g7 T. W9 [8 g
approach R+ _2 |5 o9 E% J% N
cannot be completed to a landing and results in a Go-
9 _0 v: [( x: r1 R( dAround.5 z j' Z1 H K- A1 g3 B
一个能形成或切断电流通路的特小型机械设备。
" F7 r4 x+ ]2 i7 Y! w话筒,
+ B/ y; X% ?+ j" n) \* B话筒一字的缩写。
: c9 K& h" i6 D% a. J6 D8 {8 Y0 A耳,
) f* I, Q ~, D$ H一英寸。& m9 N* ~ \) I7 F. B& g" ~
毫巴,
% s$ @+ ?. w) ^* B一个度量气压的单位,一毫巴约相当于0.75毫米汞柱。
0 V0 C$ V: Q5 W5 |低下降高度(MDA),# m7 f# O3 j$ s& l* U' h! c
飞机作非精密进近时所准许下降的最低高度。
' c. U8 G1 g3 ?- ]1 r Q1 b低航路高度(MEA),, Q% w; {4 ~+ [: j0 ^* @9 D4 n% ?
在导航用无线电定位点之间,符合越障要求的已公布
( B F' d$ A: {+ w7 Y" k: N的最低高度。在许多国家,最低航路高度保障了合格导航. X6 s* g* q! @5 D
信号的接收范围。$ ^5 f5 i" d* q# z
最低设备清单,( ?& g/ C! u6 q% _
何# \4 g2 o$ J2 g, f! { _
作飞机的文件。5 P7 o; F: E( |) `% w2 p3 a
复飞(MA or GA),
9 Y, e1 Z6 r- T4 E# N8 \飞行员因未能完成仪表进近而导致复飞所采取的一个
' K- q. x' Q, }机动动作。
- j2 D0 Q$ ], q% U L; ^MIKE OR MIC, A shortened form of microphone
/ Q, P8 F; q* P! O/ Z/ cM
$ a0 ]1 a7 ~ B7 ?' _7 @. gMINIMUM DESCENT ALTITUDE (MDA),
9 X3 X/ K/ g, P U' z) T; Oa
. X) B! @' q5 t6 ln0 f# T4 a9 w' X$ k. P9 \1 F* G9 ^
M/ Y6 n+ z, X) a( M) z
p
3 \% l4 S- ~- U0 Do
7 E" a* v3 S+ n+ p4 M# BMINIMUM EQUIPMENT LIST, Document prescribing
\- i* f8 i- {: v* F" t! W! N2 p z% qMISSED APPROACH (MA or GA), A maneuver
U" R5 B4 e1 e& ?conducted by the pilot when an instrument
( L% ?# [. u4 v% `$ ]' W微动电门,# W. ? u& ` }" z
密0 D. i# _' |5 v4 o7 m
千分之
: O; D9 |6 M1 F& _4 K最
6 v! w$ `! U# Q: M- e, H最3 W4 U! D) |: ]$ P" E ]3 @
指定飞机在某些系统或子系统不工作的情况下,如; F6 a' f* D( A
操 N' I; s, U" \/ v
英汉对照民用航空词典B OEING. \% H0 g2 |( R9 y4 g- @8 P
TECHNICAL DICTIONARY 1027 m/ _4 m y, h& m1 t* h4 ]/ C B) j
MIX VALVE, A valve assembly with two or more$ |! O$ D/ A& Q# o: l- }0 U
individual valves used for airflow distribution in air0 \4 w/ E, x- Q5 r' F! k, W
stem.5 E/ J9 O: [! S7 ^; X
MMO, The maximum Mach number at which the aircraft+ a0 K: f/ Y7 V( S. q
MODE, A specific operating state or condition; i.e.,- m. E; U: s0 Z, T2 P+ Q9 u$ c3 U
Autopilot mode, MAP mode, etc.
' T5 H6 H' b" _- o& ve
. h2 A" L; u$ [1 ^- B) t C* H; BMODULE, A housing that contains related system% [7 \' ~* D& c: r T/ I$ R3 A( U! [
MONOCOQUE, A type of construction in which the1 k: ^( b" A- i$ ^/ I/ r
ONOPOLE, A speed sensor that senses magnetic
$ D( d1 B) D6 {4 S! }pulses from a magnetic nut or gear teeth on a shaft.9 @/ [9 q' W, e: o' S4 b' [
he controller.8 ~. K7 R4 X( g3 R/ p8 V- G
MOTOR OPERATED VALVE, A valve using an electric
; {* P/ r- S* ^% i3 rmotor for opening, closing and modulation.1 `! m% w5 W( E- ?" F% D5 s
个以上单
# C6 ^+ f. c; s活门的活门组件。; x' a) b$ z1 `+ l
飞机可使用的最大马赫数。
7 o J+ m% R- P5 b1 J O" L' x式,MAP7 W: a; V" Y5 ?5 O
方式等等。
# y. l+ \" `" n/ \/ }3 U调制,# j$ J7 `) T4 g' k# p
组合两个或两个以上的电子信号,使一个信号随其他信/ n' r' E e1 @+ m, ^
号的变化而变化。
# Z( J* d1 S' t+ u& E: @. t7 @组件,2 l) w5 |9 n2 Q* \( _' Q3 a
极,
' w: I: s+ h- ]$ U& t帽或齿轮轴上的磁脉冲数的速度# \, g% I: F0 Z3 s5 ~: L) W/ ?! c
/分钟。
, D* v# C! ]/ N! r1 Q% \用电马达来开、关和调制的活门。2 R9 @# Y8 m+ G5 v' w
conditioning sy
( B, Z) F; v2 U" b. B3 {3 P# J& ?may be operated.
1 Z, _! @0 G/ }' p5 tMODULATION, Combining two or more electrical8 \/ ]4 P! R% ]5 p0 G! o
signals with the result that one signal is varied by th
) _9 m5 A7 u; Q8 _( A0 S+ o0 Sothers.7 N1 @3 M8 s- E u3 S
components.
" \; P4 e- u# u5 q- ^fuselage skin carries all the loads.
1 U F" E& |, oM
: e+ l7 k" z# fThese pulses are interpreted as RPM by t* Q+ O$ `; R" U9 S: P9 V- _
混合活门,9 I0 P: M8 M# H, ]4 W2 e+ y- D" g$ _
在空调系统内.用以气流分布的具有两个或两+ S3 V1 t' t" s: w
体6 o3 {! ?% x* w5 m0 D/ P8 q# b
MMO,
- z% @, [2 X! L方式,
- S! h2 O) @/ W/ _- s: z& |一个特定的工作状态或情况,如自动驾驶方
; ^1 A4 E" ~+ N1 F内装相关的系统部件的机体。
% H4 n+ R5 A5 ^2 k6 g硬壳式,
# f& P: H$ \: r( P7 B机身蒙皮承担所有载荷的结构形式。
% H) E# G" h9 Y4 I0 W, _. b单
& O: {3 M0 d x8 w- Y% X一个能感应到磁螺' d9 Y7 L- y& O1 `
感应器。这些脉冲可由控制器译成转
! M2 b9 O' i8 n3 U3 ]1 u9 ~马达操作活门,
5 m! V- E5 T+ f1 y8 w* D- v4 C6 I英汉对照民用航空词典B OEING) _" C1 k9 J# U* H s T
TECHNICAL DICTIONARY 103. Q1 N1 c1 L9 ?! ^
MSL ALTITUDE, Altitude expressed in feet measured
@+ B1 ]' `& _' T; b2 qom mean sea level.' }* y6 O# {- r% N, T
reducing the noise of the airflow through the pneumatic3 [6 E" S5 D1 r# Q" h9 t1 D
duct.
; @6 f3 q3 p; E7 y! ?MULTIPLEXER, A device that allows two or more
5 {) p8 H2 \3 S$ D+ n& r, nsignals to be transmitted simultaneously on a single) S. I) b, [# f' p5 [
carrier wave, communications channel, or data bus.+ w( M' i; Z0 a. s d% g
essure compressor rotor.
3 f- K' z9 W3 I' p: ~: bN1 BLOOM, A change in engine N1 and thrust indicated" `+ ^" L1 O5 V0 C9 \2 y; t4 g: T7 F
N1 gages and detected by the autothrottle BITE
; _7 F3 |+ i& F' B( Gduring throttle hold operation.
5 H( g' v8 p n1 l% X! u, PN2 , High pressure compressor rotor speed.
) F: Y q. Z* X' KACELLE, A streamlined enclosure on the wing or
# |9 ]1 \" ~5 l% E/ G面量起的高度。6 }9 ?" J/ {! a
经气源管道所生的噪音
; U/ q; \ G: ?( k$ I的装置。 f* r( h7 T/ s; O( ?, I- O# h
多路传输器,
( {1 B9 \3 C4 l0 b. c9 j- {一个能让两个或两个以上的信号同时在一道传送波,一) W, y: Y7 z/ s3 s
条通讯线路,或一条资料数据总线上传递的设备。. i F' l% P# k# r+ I3 \, q
N1转子转速,& D* r7 K+ @" ~# j) N
发动机低压压气机转子的转速。
, m. P6 ~; s6 x6 s0 r6 ]N1激增,
+ Q% f1 h7 l( C8 R" B; g油门保持过程中,在N1表上出现的由自动油门自检探) k2 ~/ Y( o# D5 Z' A" ~8 @. {' y Z
测到的发动机N1和推力的变化。
$ L# L/ q& i* v l2 S( i+ A0 NN2转子转速,8 g4 k& |8 A3 T" q: _7 s4 F% R' k1 I+ X
发动机高压压气机转子的转速。# C0 W$ E, H8 a
短舱,
9 Q I8 m7 {( C) P, u# p# q. h机翼或机身上为安装发动机而用的流线形壳体。; T$ s( ]7 |! c% Z& O" }0 J
fr2 P3 s: W3 a+ P! h1 P0 _
MUFFLER, A device in the pneumatic system for
* y8 m8 L( ]) _/ F8 DN
2 m q* ?# v5 \& ]7 p: R, xN1 , Speed of the low pr2 j J8 j% R, G# C* h
on the
7 @ H( f0 q$ c2 \' M2 j4 lN/ N- v! S4 k7 Z$ I0 Z4 K
fuselage for the engine.
1 a0 S" C) r" o1 e平均海拔高度,; E' G3 u! G8 T1 B; C
以英尺为单位,由平均海平
9 Q. ]( u+ H9 w3 j消音器,- d* Q, S- ^; o: r$ a% G% H
在气源系统内,用以减低空气流0 L5 ?8 c1 D2 C+ b [2 m* |
英汉对照民用航空词典B OEING; h, B0 N8 A# r6 d$ f
TECHNICAL DICTIONARY 104
% m0 K$ i% j9 f: }( D+ VNAND GATE, An AND gate followed by an inverter to
, D3 A: D' {: `9 A, ]: aform a binary circuit in which the output is logic 0 if all, A# Y' r7 a0 s; r% G2 O
puts are logic 1.
6 m4 y7 I# p8 T; W; @9 _+ xAUTICAL AIR MILES (NAM), The actual air distance
* y) o8 k( D. x/ e* S% ~respect to a
' X6 I; q" k8 I9 d* A9 jtationary object.! S4 I" A2 N A, O) c
istance: k% \& }8 C6 p' T* s# b8 B" S. S! [7 j
travelled in relation to the ground expressed in nautical
) t/ T2 G2 l1 E+ ]& W3 _miles.
1 M" k+ V( X; S3 b& t5 [( hnce equivalent to 6076.1 feet; D6 g) G7 C5 `* |- h
r 1852 meters.: n5 o# h! K" v( O
hical
3 r* s: y, d1 ?% `- Q# G; h M6 IEGATIVE LOGIC, A form of logic in which the more
" X- T2 x% X( {" z& |% Gnegative level represents a logic 1. {. n4 H0 t, [. F# n G6 N
EGATIVE RELIEF VALVE, A valve in the1 X) E4 g5 Q' D7 W; c
e to be' [6 A8 m1 [9 |" ~
above airplane altitude (or cabin pressure to be below
& s6 I) V% w5 D! O. U5 cambient pressure).
# @6 V: |& A6 M0 |% E% e$ K有
' z4 E0 p1 N: J0 q: n人为逻辑1时,输出为逻辑0。
" f8 T/ `4 @4 Q8 R) P. r海里(NAM),
% q1 I# I) F9 h' O4 K来表示的飞机在空中所飞过的实际空中飞行距3 G- ^( U- D7 \) l4 ^
地面物体。7 v a. b3 z# ]# ?$ Y
以海里来表示的飞机相对于地面所飞过的距离。
3 [+ ]" u+ N$ Y: } F: Q里,
! C/ f; R6 G) V4 X9 L4 q& H相当于6076英尺或1852米的距离单位。
& e5 S3 }2 a: w0 Q1 m8 ^+ R+ W导航,6 V* |# f5 [3 ?7 B4 U2 ?
反逻辑,
* I2 F! |) [) U; Z [4 I6 S正电压水平越是代表逻辑0,负电压水平则越是代表逻; O! @$ }9 v% a1 `' q- I
释压活门,# L% w; @7 _# \- l% g' _' {8 D
增压系统内,用来防止机舱高度超过飞机高度(或机舱: i9 j6 u4 t' I n
压力低于外界大气压力)的活门。
1 p6 J7 P/ V- s" e vin/ y& X/ X6 Q' I9 }
N( \5 b" l/ }; \7 D, w* R+ j
flow expressed in nautical miles without
* s0 ^' X( V! hs4 s) O# Q/ \, E6 v+ |
NAUTICAL GROUND MILES (NGM), The d5 W# g9 ~* n" \0 d( j
NAUTICAL MILE, A dista; @2 v+ s: T# P; K* n" A, Q
o
3 t% @2 j3 k n' h5 wNAVIGATION, The art of determining the geograp: l4 Y( E- V5 @3 J; o
position and maintaining desired direction of an aircraft
4 g9 x9 ? @' J. D9 A' h" m+ Yrelative to the earth's surface.
' F- _4 ~1 U: E- p: K3 j/ }N7 ~" h& Z( y) D A7 q d5 M9 i# _
positive voltage level represents logic 0 and the more6 I5 w# H. _" O% v7 }4 c
N1 C. A& y: L: n' [3 E8 l$ y$ D& x& H
pressurization system for preventing cabin altitud
7 J t) U0 W- T1 d) \4 ]2 B7 W非与门,
7 I/ S6 q9 C W# T: t% h在与门后面紧跟着一个反向器的二进制电路,当所
a& }) h$ |* q输
5 x/ X# b o- a+ F4 d& N空
; B L4 {( s! M7 ^0 n/ [ Q以海里
# ~3 Y* u6 _4 e; x离。空海里无需参考
- q, Q4 A: d* X, `( Y3 `0 y地海里(NGM),
9 E; }5 Y; j0 o% D5 ]海
* T9 }2 j2 `& x# _决定飞机的地理位置和保持飞机相对于地球表面所希
( D# L2 }8 e! |1 ?望的方向的技术。
3 q& c- I. E# W9 ]6 l辑1的一种逻辑形式。
! G* e- |' R; w# D负5 L) |, }: L0 J a* ^: r1 t
英汉对照民用航空词典B OEING# m- ~2 E$ g9 I9 {) }6 Z: S, l6 X
TECHNICAL DICTIONARY 105
4 W! p. w% ~5 X1 z" y( M& mNEOPRENE, An oil and grease-resistant synthetic# [; h) g8 |8 }) `9 H7 y' X6 I
rubber. Used mostly for seals and self lock nuts, etc.0 y( e* o* E4 z( I
EUTRAL SHIFT SENSOR, A sensor used for
$ l9 j" M$ {1 H9 ]NET PERFORMANCE, Aircraft gross performance
2 B8 r0 ?# J- V1 ocalculation6 T, a- ?9 P: c7 O6 ^
purposes.
- _ x# v# }5 {+ S. N% Q! vNICKEL-CADMIUM BATTERY, An electrical device for9 @6 S& }" q5 Y1 p: F. P
changing stored chemical energy into direct current.
* N$ y" D: P, n# t3 V" }6 E! `ses nickel hydroxide, cadmium hydroxide and
8 D3 ~9 M/ n2 \. `7 T6 lotassium hydroxide.
# |5 L% c7 w' G* {NOBLE, A term used to explain the properties of some7 j+ u) B. |) Z# f
lements that are chemically inert or inactive.
3 B# X, J. C6 y* s6 KNOISE ABATEMENT PROCEDURE, A flight path and
' Q: [' @9 e) z1 j% B1 f7 o6 Llimb profile designed to limit noise in the airport area.- `4 v4 \4 q. z& u p+ ^, r: @. \7 O
construction. (Nomex is a trade name.)0 y: ?" |0 e; `; V- B8 R
in only
7 Y9 b( @: C( S3 C7 E; Hone direction.
. _$ L: P" l* ~* S) a氯丁橡胶,6 C, B4 o4 i' k" g
一种耐油和油脂的合成橡胶。多用作密封装置或自锁螺
% C2 @( c/ L6 F. H$ l7 H$ w帽,等。
4 ^3 q, u7 g/ c立变换探测器,' P4 A8 F7 m; p7 M |4 f
用于探测升降舵和安定面配平状况的传感器。
1 q. a, b3 ?% ^/ M/ L8 ^: _性能,' M3 j& P8 `* I) {. d) X
机总性能减去由当地有关单位为了使性能计算* ~) }. s6 A) e3 M8 E7 t& H
较为保守所定的一个量后所得的性能。4 E& Y( d! w+ B: J7 [
为直流电的电器元件。它使用氢氧化
8 f3 }7 ?) F) y) a' b) y6 k0 C, h、氢氧化镉和氢氧化钾。
( T6 ~$ W7 d8 g性,
" J$ n+ j" I, T4 c用于解释有些元素不易起化学作用的特性的名词。
) A- Y6 P$ T% b4 R/ ~低噪声程序,
3 u- C+ l' Q! U一种为降低机场地区噪声而设计的飞行航迹和爬升剖
! A- w# N1 \5 o5 s。
$ H1 w$ G, `; R: l+ j是一种类似纸的材料,用以制作蜂窝结构。(NOMEX5 S Z; y: q2 C- y, a
商品名)。
1 X* @+ N' {! `7 R只允许向一个方向流动的活门。7 A, r0 U e# X# w
N5 J7 p. a% T) A. E0 V4 r$ R
detecting the elevator and stabilizer trim condition.
) A1 _: T5 y( Xdegraded by an amount determined by the local& f5 q" O/ a! ?! L/ s
governing agency for conservative& O4 L' b0 S2 H5 V. _8 F2 ?) c
U$ B3 `/ U/ B+ d
p
# O. K9 L+ P3 [; Ie
: r- s1 _6 D/ W6 B8 {; a: [# X9 sc
! ]* r9 |8 x8 F, O O9 W- nNOMEX, Material similar to paper for honeycomb
1 J e2 j: {& Z5 g) s1 kNON-RETURN VALVE, A valve allowing flow3 o7 W* l* h2 c: G% |9 I' @
中3 w8 Y5 z8 Y' Y# c4 h- `& x/ g1 q3 {
净
9 }8 m5 C; D7 q( E# { Q9 V5 W; x% s以飞
. U4 W2 c7 @& W" a镍镉电瓶,
& H+ a E1 p5 `& t将储存的化学能变3 I0 T& j: R" e1 L
镍
9 F0 V. V2 k1 W, B: \4 M惰* @* X" W6 ^5 s- ?6 p
降( W$ o9 h7 K! B$ J+ E% ~
面 G# h$ o- L6 z; Q; F# b
NOMEX,
* Y, T" t! U; Z是" |* ~& `8 @ D! M( c, a, ^
单向活门,
. v# P) R. X# i9 {$ o英汉对照民用航空词典B OEING0 T" `; y1 U" X$ }( g: M
TECHNICAL DICTIONARY 106
9 i6 S i2 \) ?1 G2 qNONDIRECTIONAL BEACON (NDB), A radio beacon
0 T. b$ ?9 o7 S! |9 C. Q7 x0 Kwhich transmits nondirectional signals whereby the pilot
4 E2 Z$ B- L& x6 S1 Lcan use the ADF to determine his bearing to or from the0 I! v5 I: ]7 T7 Y) }
station.
6 W. v" h4 b- M6 x4 sONVOLATILE MEMORY, A type of memory which7 g" R9 t% Z# w$ }
does not lose its contents when power is removed.3 E/ l% j0 c% X, v) P! v9 S
rm7 O V+ W1 C/ N6 J1 c% V
binary circuit in which the output is logic 0 if any of the
4 \2 r# e0 f' [3 j. o0 g8 H qinputs is logic 1.+ t% _8 {6 e; D8 z! [( T
NOSE CONE, A device on the front of the engine that* B' P, }8 V, J4 v3 S
guides airflow to the primary airflow path of the engine.& s/ B8 u; T1 i& h, ^$ k+ O
the nacelle for air inlet to! v9 n5 P9 u, V* Z
e engine.
$ Y- T* ^- E uOSE DOME, Front section of the engine for
' j$ a! N& {. D- Y! Wtreamlining and directing airflow to the compressor.; p( k$ M/ {: W/ q& Y* D/ l1 V
),
2 q, U/ r" w1 i# f3 I" f6 ~ t2 a能够用自
. M: Y, E4 x# B2 Y1 m6 R6 U* y' A定向仪(ADF)确定他的背台或向台方位。
~4 m: ~$ ~0 k, ]. G( K久性存储器,
. B* N' U- D+ s在失去动力或电力时不会失去记忆内容的存储器。
& }! h, }! {$ b0 A在或门后面紧跟着一个反向器的二进制电路。当任何一
( ?7 R# J# k9 H/ Y! p; w4 x6 w输人为逻辑1时,输出为逻辑0。
, P- e7 A# f7 r0 ?' m一个位于在发动机前端,用于引导气流通过发动机的主$ P4 T- E0 e E4 |! Q
气流通道的装置。
# h# |4 _6 J2 e& \引导空气进人发动机的短舱前段。
9 K2 M X" F& ~# R0 Q部整流罩,0 ]/ G# ^" B; e& E/ d
用以整流并引导气流进人压气机的发动机前段。& c' z9 f5 F+ V# O3 y( i( M# X9 ]: G6 w
N, C* \' \, d3 e; V
NOR GATE, An OR gate followed by an inverter to fo
F; n q" [/ p) G: S1 l0 G' pa
2 | y9 C3 h: W+ X# n* kNOSE COWL, Front section of
; H/ e" t# x+ u- ]0 V7 zth9 }6 Q1 Z5 u' D7 d
N' t3 J) E1 r" b6 D) S' t
s$ ?( B4 m: e. J, |* `
无方向信标(NDB. ?$ l4 X/ ?0 d; h
发射无方向信号的无线电信标台。据此飞行员
' A: c" b* ?! }8 M; | y动3 ^& D% M, O$ Y( J$ l
永
8 R( P8 _' ~7 ~0 [: ~或非门,
4 P# c% a0 p* o( ~5 B/ {# ~个2 V- q+ S0 X- A- }- |
进气整流锥,4 x9 ?( r! L- y4 | o: {) t4 b. E
前整流罩,6 g1 L' t0 m' U6 x$ T- X
头
7 x8 _8 i) B' d( z% O9 n英汉对照民用航空词典B OEING
/ w+ q+ \0 Y. W. ~TECHNICAL DICTIONARY 107
# f5 D& Y0 D8 R, L& X5 ]0 }NOSE GEAR, The front wheels with the attachments for. S3 v/ t+ ^4 G, V" i
NOT, A binary circuit with a single output that is always) K, ~! h0 ^# U) L
opposite of the single input. Also called an inverter.
5 A$ A3 z. \) Ztion that has the shape of a "V".$ ?- }0 K' Z" |! K' _1 `% e
t.
, d) N5 X8 m' E F, T% FO-RING, A circular shaped rubber or synthetic material
% Z% i" \* W3 b' H2 D* ~2 {7 S& L/ asealing device for pneumatic and hydraulic systems.; q6 h! G* t1 M$ m* l6 b
PERATURE
- Q0 L. K1 i; j* J2 Ee, ~, F+ |5 X" P: z/ @
in the path of flight.
8 }4 B, u; [ r1 u, oOBSTACLE CLEARANCE, The process of flying the& ~2 n+ n: B c# ]
aircraft over all obstructions under the flight path.* h/ I5 h! i- D' X& ^' E( o
Which obstructions are considered and the amount of
2 ^- b& J" d; T+ G4 Jvertical altitude required above the obstructions are/ u* `. v/ c2 k9 M, _ r. I
determined by local regulatory agency.! q+ e4 p `$ i. m
非门,
" V( M% _, p; N I带有始终与单一输人相反的单一输出。也称作反向器。
. j; G- @. N$ L7 I( S C# u一个“V”字形的缺口。
# g* [) A+ L8 A+ j! O, q# c喷嘴,
3 b$ O, C. P9 y; m* S形圈,/ B; P7 H: E: S# v* ]% x5 a8 y" P* o
用于气源和液压系统,圆形的橡胶或合成材料制成的密
0 k% d0 A- \) z: Y% S封装置。9 T5 ~- x( j: z- A8 j( ?7 D- ?
外界大气温度,
- T( q% {1 L! h/ G1 B" f见Outside Air Temperature2 G1 ^8 @3 p: i! B
supporting the airplane on the ground.
" {: k1 h1 ~2 C* \6 k+ G5 rNOTCH, An inden0 t2 k( G5 K# s3 u& L
NOZZLE, A shaped device for directing flow in a duc
* F3 a& o( @/ @$ g! gO
+ i3 }8 {" f! g$ S/ fOAT, SEE - OUTSIDE AIR TEM# U! A6 E1 R! c; ?. d7 g
OBSTACLE, An obstruction protruding into the airspac9 k8 j H3 K( L' o, Y1 J, q! e
前起落架,: R1 k4 {% c1 r* |3 [) {
用以在地面支撑飞机的前轮及其附件。; Z# D1 {+ L" A0 Y! _7 H6 p& i3 z
凹槽,. F! A, i& z7 W7 P% z' L2 \* f
引导管道内流动方向的具有特别形状的装置。; O' `& W! u# w) o" e& e3 x/ {
O1 r0 P! q& S% c+ V& |/ P" h2 s# C4 F
.
& B: j) |! @9 q越障,. E2 N7 I0 V9 G6 E
道上所有障碍物的飞行过程。障碍物的选+ r6 E* B) i. I9 w
择和飞机距离障碍物的高度要求由当地有关管理机构决( J- q! \) ~4 b. T1 t# z
定。
. B! r0 o+ g: ]. ^( z障碍物,
% r, V& _7 J& @" v进人飞行航径上空域里的障碍物。
9 s1 k" J/ I6 H( P/ [9 a" d, R& M飞机飞越其航. D8 n- \ d+ {7 n: W
英汉对照民用航空词典B OEING
+ Z" m% `! |/ U+ m/ q1 JTECHNICAL DICTIONARY 108
7 X) O( a5 |8 P3 I) o; K3 ZOEW, SEE - OPERATING EMPTY WEIGHT
- |! v6 g0 n+ U4 T9 I5 }FFSIDE, Opposite side.9 j2 Y0 @4 w- \0 x
IL COOLER, A heat exchanger for cooling engine oil5 T8 u0 K2 P( E* h6 h; s" J4 |' l
by fuel flow or airflow.
5 A2 V; E7 [. bATOR, A device used to separate unwanted
- i2 }2 ] [( J8 k- eir from engine oil returning to a sump or oil tank. H1 K0 q( D8 O$ @* M" T
OIL STRAINER, Type of oil filter.) b0 p0 l, H. \* E1 K& T5 _" Z
LEO STRUT, SEE - SHOCK STRUT
1 d9 Y% q, `& r9 gNSIDE, Same side.' ]: T5 n5 T" `, y9 G
ll weather navigation system.
9 k& H; W5 _4 \0 G% uch is not
# q% q$ a0 b, D# V: }& `continuous from power supply to ground due to a break% k" N7 d! r% c" C, p0 D
in the wiring or failure of a component.
( s. }7 ?- @7 R2 x见Operating Empty Weight
: ^* f8 g: ]; ]3 Z+ f* y3 iO$ t0 S' N9 F$ X7 |
O
, z- y+ t8 a! W: I7 v, `# f: POIL SEPAR
% T* G+ K: n/ h, n. ^1 ]8 Na
7 c! x3 D4 |+ U3 W2 t' F! rO2 D# o3 `" n4 |* z+ C
O
7 s. v: p, d4 b1 JOMEGA NAVIGATION SYSTEM (ONS), A worldwide,8 e6 _0 w# C/ ~
a
5 m5 U$ U% Z* I7 b8 K' x( D0 qOPEN CIRCUIT, An electrical circuit whi1 k6 M+ A) n2 [$ `" \
使用空重,
; K+ c* l: A; ~/ ?- k, o.' g( l$ d E; N t, q6 z4 C
面,; {( D6 q9 _4 H7 C
油冷却器,
; a- E7 Y6 |/ H) r+ n3 p. w利用燃油或空气的流动来冷却发动机滑油的热交换器。. e+ l ?: y$ c: q
油分离器,- p9 Z* V) S3 F9 ?# B
一个能从回油槽或油箱发动机滑油中分离出不需要的) h3 r( Q0 x9 k
气的装置。
8 Q) s( p* P5 u8 j% Q滑油筛,2 V: ]" b5 R, `: x$ `
滑油油滤的一种。1 V0 a( q; P* j7 M
液减震支柱,: [$ o" Q' x# d! M: Z
见Shock Strut
7 ]$ I( [+ D6 {$ {' X反+ ?& P+ R# X9 }) K9 p' v; d
相反的一面。
3 \$ ]7 A2 t1 h% m$ g. x+ y. I* d滑
( u9 j" h: I: t8 |, l, s滑
( o8 e) L' r; L' @空
; z0 V/ ^! r3 v7 x6 ~4 \油
: i- p9 ~9 _* k6 I6 ?9 S.
. D4 m( R1 |% T' k! l面,
9 F5 S3 V% |$ b5 Z- q相同的一面。
/ E5 V! J0 B; a+ K4 b5 W* o8 s7 `个全球范围内全天候的导航系统。3 n5 E' Y8 a! X2 p9 X
或组件损坏而导致从电源到接地点之间7 U1 q3 c7 b G* ` `
不通的电路。
" v# X) \( B% k5 Z/ Y5 ?同
) C0 N$ _1 K3 u7 H奥米加导航系统(ONS),$ ? p3 Y& H4 v
一/ {+ L& S( B4 ]2 F
开路,) H$ `0 D2 L/ |9 h% F @8 c
由于线路中断/ Q/ r5 M |) M, _6 x1 K- h6 I, L6 @
英汉对照民用航空词典B OEING
9 s8 a, |/ z. Z9 q9 MTECHNICAL DICTIONARY 109# Q1 N5 C8 D- x8 ^6 j" K9 O
OPERATING EMPTY WEIGHT (OEW), The weight of
1 o9 e1 s2 ?4 jan airplane fully serviced, including the crew but without8 w( f, y! }) F; W8 ?; }! ?" {+ S1 R
fuel and payload.
' ?4 [7 d5 c1 [; e9 f0 l9 |PERATING ENVELOPE, Defines the environmental# c9 U" u3 Q2 [% M
OPTIMUM ALTITUDE, The cruise altitude which results, D) a, t+ x# i
in the best fuel mileage.2 W! @4 [; S8 `3 J( p* E* V
OR GATE, A device or circuit with two or more inputs of; D. r7 c$ {5 O+ T# U3 ~
binary information and one output. The output is 1 when
% _/ {6 D. Y' fany one or more of the inputs is 1. The output is 0 when
2 G7 D0 e) n/ n' d9 |+ F5 l2 ]# qall of the inputs are 0.
% X+ N5 ?; w9 q+ A @3 Q. yORIFICE, A specified size hole in component for control
2 L6 E6 l, z# Zof fluid flow from or to the component.$ }, l, R7 Z% i; l3 K' w
ORONASAL MASK, An oxygen mask covering only the
; E! I+ d# i) R, d1 D, T4 Pmouth and nose." G4 V& ?! t; M! ]& {4 d' ^( A
OSCILLATE, To swing back and forth with a constant, ^/ ~5 R: b$ n+ W* f, \0 G
rhythm.' K! i7 N$ b- {/ c% K- z& G
使用空重(OEW),
: s; ~! ~. z& l2 T) s6 w0 W$ ^使用包线,
" q- `) z P" ^; b& `( d- B确定飞机准予飞行的压力高度、温度和速度的环境极
8 ` d U, l: \) G* B/ o6 ^或门,
% l$ w! W, {4 r$ {8 H' x具有两个或两个以上二进制信息输人,和一个输出的装; C4 |- Q" g# S6 u' Q
置或电路。当输人端有一个或多个为逻辑1时,输出为逻3 S% Q0 G, E3 `% |+ c) u
辑1;当输人端都为逻辑0时,输出为逻辑0。6 x, d7 \0 R' V7 S/ c
量孔,
1 F! z' p2 D& F7 \ q. F- ~& h0 v部件上用来控制流往或流出该部件的液流的尺寸已确
( s' q+ r% k9 i% `5 h定的孔。9 |7 \6 ^0 G2 |' v( i
口鼻罩,
* S$ d" L4 |3 w2 i: U仅罩住嘴和鼻子的氧气罩。
Q/ {1 k( ?4 ]; v% z振荡,# N7 H# [5 n c
以恒定节律作前后的摇摆。! A% Y# }2 b+ g; o: p7 o
O9 _- p; a' @, s2 e1 _- ^
limits of pressure altitude, temperatures and speed3 a6 g, |* i& l; Y
within which the airplane is certified to operate.
: A Z8 c6 ]9 c$ w8 j一架勤务完毕的飞机,包括空勤人员,但不含燃油和业$ z0 U0 J5 N3 `5 y# t0 r
载的重量。
" k! a+ ?: f" e3 _限。
4 Y& g$ i1 y+ u& L4 Z$ Q最佳高度,
1 Q8 M2 s, H& B5 H( Z7 G# \可获得最佳燃油哩程的巡航高度。
/ z/ S% s/ S, U+ p# \; @英汉对照民用航空词典B OEING
9 b' b; |# |9 y: UTECHNICAL DICTIONARY 110
" z- p" N' C t3 J+ dOUT OF DETENT, A condition away from neutral or a+ `4 r8 b2 M0 } B1 R( r5 V0 N: J+ P9 i
OUTER LOOP CONTROL, For autopilot operation this
) \: V8 W: w9 \( E$ w& Wis control of the airplane's flight path to a target.
+ n9 m: z! `5 v7 A* B9 CExamples are control of heading, altitude, and vertical
3 e% o# ?5 |: z# C+ b- ]# dspeed.7 T' q3 |! |. _8 c% D+ f
UTER MARKER, A marker beacon located at or near
! ?' A, V) o" u# me glide slope intercept of an ILS approach. The OM is
1 c( r3 i% t; U& j5 T+ L8 tnormally located four to seven miles from the runway
6 X" ?6 S) k& L3 breshold on the extended centerline of the runway.
W9 I+ t- k( }/ zW VALVE, A valve in the fuselage for1 J% Y) G5 ^+ J
g the airflow from the fuselage to ambient for$ u$ ^; J. R) a9 O. H
ation control.
* N% \: C: _" m& B5 ~* ^UTPUT, An information signal going out of a system or+ f* R+ q* ?7 z2 i/ [, B
part of a system.0 h+ c& W2 K: Z
UTSIDE AIR TEMPERATURE (OAT), Ambient, or free5 [6 r3 O% K$ j- t3 I; k5 U
OVERHAUL, To return an aircraft or one of its; }" {* I+ @- I
OVERRIDE, Operation of a component by a method& j( N% x2 ^# k j' i6 X
different from normal operation.
% d4 M; l' n' M/ U" C( w操纵杆离开中立或槽口位置的一种状态。
1 Y" H% q; M+ m/ B/ I; J制,
* k5 ~* _4 i' c4 Y- A3 @+ S航向,高度,和垂直速度的控制。
; k1 |! d% p1 @. z* E& ]指点标,, f/ J; U* i8 |3 ?$ z2 [
位于或靠近仪表着陆系统下滑道截获点的一个指点信
; g6 X2 a: I+ B% a# V标台。它通常位于跑道中心线延长线上距离跑道头4至71 F2 C2 s6 G6 Q- Y2 j7 A; k# g
海里。
( ^1 I& ], G6 l8 ^) V/ r+ e流活门,% Y' q7 P; ~! F: f" ^+ l5 c7 f
机身内用以控制从机身流向外界大气的气流以进行增
}$ l+ B- D6 f1 ~+ R! J控制的活门。
+ `5 p0 }" i2 m n9 D输出,
$ W* o4 C- W7 r! W; Z' }从一个系统或系统的一部分出来的信息信号。
) O5 l" `" f. ]0 o# y' c界大气温度(OAT),! a( I; W! ~0 R2 ^- r
外界环境温度或静止大气温度。8 y4 @# q5 V+ h" ~ L
修,
8 O/ r, D) s, k7 c; k将飞机或飞机部件修整到近似全新或制造完成时的状
8 @4 y3 j; ~: M W& ~! {, I超控,
, S" F8 n; {, H用不同于正常操作的方法来操作部件。
6 ]8 @) O" A6 o2 e8 Knotched position.
# U/ B: U, V5 R0 uO. N/ }2 o9 t9 g: ?; z: V
th9 B2 ^2 v' C" ]- `5 Z6 `, z( Y9 i& g
th: Y+ T# J$ u+ G, n) @
OUTFLO
* \5 O7 [- P9 ^; Bcontrollin
6 f5 D l* p- e+ r vpressuriz$ L" C0 [: A+ z' q1 \
O: K o: p0 D% ]
a
h3 i4 Z0 N+ T. i# eO$ ]0 m. o+ u" b4 L8 t/ J
air static temperature.5 C4 ~7 ]! Z! s
components to a like-new or just manufactured5 F4 }, Q# e% }+ u+ y4 ~
condition.
; G! h( O% f, \ I. ^+ O脱离卡挡,
9 [2 \) U* g; B2 j' B外回路控4 p4 K6 v! \3 U, d
用于自动驾驶操作的对飞机飞往目标地的航径控制。例 V% C2 b' T8 @7 n; g6 X+ V4 y
如
" F: Y+ z9 ^8 Y0 s" n3 D% s远1 k* A! W( Q# _# p% A$ i" \
外: w8 f" v1 F' g# E) b) [1 q4 G- y
压" O ]- d# { O/ |+ X) k
外2 ^" A* H' s6 y' F( _, Y$ i
翻
3 ^( U' p4 Y8 K5 Y; s* f& O态。
, p6 T. h8 j, G( U, v英汉对照民用航空词典B OEING! G% `) d+ V0 }$ R# S( D
TECHNICAL DICTIONARY 111: S1 U6 H3 W( G
P M3 Y. D% C& ?' k: c
ACK VALVE, A valve for supplying air and controlling
4 P j1 n* K0 F$ @* imanifold to the air
: w8 O( M# L z" l% J5 y; t' W6 wonditioning system.
1 Q) k3 f2 ~! }( All piece of any substance or
& L# o) |& z+ X8 _# ]2 Cphysical matter.8 T+ C( ?( Q8 I
h9 l+ u* `1 l; k# B
rovides flight crew and attendant announcements,
7 z( f0 h+ y3 O6 R6 m- }oarding music, and chime signals to the passenger
* S, C' k7 Y; _, e# L8 J/ M# Rcabin.
4 f; G8 M+ N. n, P6 g% J; NASSENGER ENTERTAINMENT SYSTEM, A system2 m% V! V/ }: n5 c1 c& o
tertainment to+ S, o6 w9 D: F: l+ V+ h1 z
e passengers.6 l' p0 s6 C5 r' f3 [/ s
PAYLOAD, That which is carried to the destination,
+ y' T2 U5 E5 xuch as passengers, cargo, or mail.. ?0 X8 j8 H# |, \; B& Y
CA, SEE - POWER CONTROL ACTUATOR
5 _; `* D3 C- {0 m& }& T2 lPDCS, SEE - PERFORMANCE DATA COMPUTER
: s- j5 D- y9 |) Y9 Y9 FSYSTEM
7 G- [! M8 p+ o" h8 [- g调组件活门,; G! Z# J* e$ {, ~( W4 L: ?
由气源支管向空调系统供气并控制该气流的活门。9 \2 D8 a5 ?/ y( `! F" ^
任何物质或实体非常细小的一部份。
/ a3 Q) p$ W( M/ Y2 t旅客广播系统,
1 I- I3 I8 r# F' h! J能使机组人员向客舱进行广播、播放音乐和发出谐音信, {1 ?( N& s2 [2 b2 o4 }1 C
的系统。/ ]4 _# b' ?" _# N7 B
客娱乐系统,
1 t$ Q4 M7 U5 |( ^ ^# O+ M频和/或视频娱乐服务的系统。5 `, g5 b% G& R7 h
由飞机送往目的地的载重,如乘客、货物或邮件。
2 R8 I) I: q: ~* }* K+ e- W4 t( U力控制作动筒,
& g3 j# e" V+ o" T+ }见Power Control Actuator A( ?2 C5 m( _# N. O
P7 P, F7 @) D: C" V) C- o
air flow from the pneumatic! f8 P: ^' x2 T* S5 x
c, }# i j8 t8 b: t
PARTICLE, A very sma
\+ ~ {6 E& s9 ZPASSENGER ADDRESS SYSTEM, A system whic8 H- ^% j1 s* U6 Y) V. Y( {
p% h9 w3 `0 T: |+ k) |' E9 `
b
5 R4 q- R N# E' I) }% _7 _3 NP( N: M- m2 k( K7 W) }- `& t8 T9 _
which can provide audio and/or video en
x# Z2 a: A/ e9 t1 ^6 h" i% pth( P6 |4 P: X0 i( J1 E% z0 m7 M
s; P0 j: P( P) Z' n, W9 [( [" h+ s
P
/ z/ g; M5 }3 kPCU, SEE - POWER CONTROL UNIT# P7 I. {9 w% t6 o) X& K% D
空
; r/ i H w% G/ [# P微粒, _$ R; o0 i9 c
号( T# E4 m( ?* h: d, t' ^% L
旅
; t# P! v7 d2 c, O6 Q' B向旅客提供音
& f( C- N+ c) q6 a+ f9 x业载,2 T+ ~8 w% }3 C0 h
动$ l% x/ A4 J' y) o9 R
.( d: M0 O; m1 b
Control Unit
* ^% R- j) A/ u& P6 |4 y5 N- F动力控制组件,
8 S1 D# R% I8 T见Power .
$ g% Q8 H7 V& w# l3 ^" w4 N性能数据计算机系统,
4 Y! F/ [" R4 P见Performance Data Computer System.- A6 t1 m% v0 f) z" {3 S5 p! [
英汉对照民用航空词典B OEING
" P( Y* ]7 J7 ^" ]9 ^' oTECHNICAL DICTIONARY 112
7 {1 M& d/ I9 ?' q5 u' X: u8 X% ~PEEN, To cause a more corrosion resistant surface by; j' K0 I$ ]! G) t9 m8 b
multiple impacting it with a hard material such as steel. x- Y5 A$ d4 n0 L( O) s
pellets. Term for this is Shot Peening.% e% D6 A* M# N, {) _3 u. X" Z
Defines a position on the aircraft relative to the mean
+ k5 ^3 Y0 U* P& K' e/ Xaerodynamic chord of the wing.
# |# }7 Y& j/ t) ar as a percentage of a fixed
; y1 }$ T w% A- n& kmount rather than revolutions per unit time.
& w3 Y8 c! \$ P1 l3 Y& Hamount.8 f' J, |2 U6 S$ _
ERFORMANCE DATA COMPUTER SYSTEM (PDC,
1 ]9 d2 Z% s/ D( f# uPDCS), A device which provides data to achieve the
/ c/ @( f: N% C* t3 Umost efficient and economical operation of the airplane.6 s ^* Z! ?$ ?9 R6 Z4 Y3 U1 W
PHASE OF FLIGHT, A portion of flight specifically
% ]* _8 L. G0 @devoted to accomplishing such things as takeoff, climb,. i# y& ]& ]0 s5 B8 q
cruise, descent or landing.
& S0 L; S; i# k! x这个过程名为喷丸硬化处理。
* X3 v( m" Z r$ @# T平均气动弦百分比,* [& ?8 @5 z7 J. z' {9 c! D
间转数来表示低
: d) S% [! X+ p2 ]6 m( F# ~5 z& f ]* _压压气机转子的转速。) M( s6 [" Z8 _- M" E; c0 I
性能数据计算机系统(PDC,PDCS),
& a* P. @# k& X. B+ Z T8 e/ [一个能提供数据,使飞机达到最有效和最经济的操作的
! l, J' F2 \7 F* R3 ~ j5 l2 F置。
7 U. _- |- T+ C1 k- F6 v/ ^行阶段, g! m3 i o( W& T
飞行中负有一定任务(如起飞、爬升、巡航、下降或$ i0 {" L, W. i. y$ [; P( O
份。
9 b8 v. F3 T! |* Z- T$ V; d0 EPERCENT MEAN AERODYNAMIC CHORD (% MAC),+ z6 t. f b4 T2 N& W
PERCENT N 1 , Expresses the speed of the low6 b4 u8 a* h+ X4 q
pressure compressor roto0 a" V3 m M+ W0 `4 B
a5 Q% S& k% S; }# o$ |, \2 |3 r9 G
PERCENT N2 , Expresses the speed of the high
, G8 e6 A$ P( {6 C4 Rpressure compressor rotor as a percentage of a fixed
! t6 D7 E- M. Z8 PP# J4 e! A% w: R- @
喷九,) n$ V. c/ U( `
为形成防腐能力更强的表面,多次用诸如钢丸的坚硬材7 u4 h9 `. G; s+ Y+ v3 N
料冲击表面。1 T- c9 W) K+ A* `# @" }
用来确定飞机上一点相对于机翼平均气动弦的位置。
; D. J, q! S1 DN1百分数,* ?; u& Z4 r( m7 `* b. }
以一定量的百分比而不以每一单位时
/ q5 F) c7 U" n1 K& U5 y ~& ZN2百分数,
( a; \+ T3 a. `- @以一定量的百分比来表示高压压气机转子的转速。
( G% H; P% Y$ m3 r! _装
f; Z2 ]( I @" m. _6 G飞
6 s+ K& j) y6 L着陆)的部
, F% Q; k& C3 B" P英汉对照民用航空词典B OEING2 E% M* u+ T+ y) Q, R1 k8 Z' S* I
TECHNICAL DICTIONARY 113
! p% W0 R* `( D# s4 u! U# ?# fPHILLIPS HEAD SCREW, A cross point screw with two3 v4 u/ ~! T2 s0 q, f
en with a flat tipped Phillips head
, m$ e0 f: ^8 ecrewdriver (see Reed and Prince).! M$ O( L2 W! ]; ?5 z* T6 l
ITCH, The rotation of an airplane around its lateral& X% g; F- L- |+ j5 H- F5 m/ H8 h
xis.4 G) I+ c. E _- I+ A+ e
ne
% S+ b2 J$ a0 rose up and down movement controlled by the' H/ y& [. M; m: \+ M
levators (and stabilizer for trim).
$ ~: J$ q7 O, J- `( H2 o* HITCH RATE, The rate at which the airplane moves in3 S; b0 x. V6 }7 X# }* v: {+ Q
e pitch axis (nose up, nose down).
3 X/ t' K" b) b& u5 R) Y( e. tTIC TUBE, A tube facing the airstream
. U3 b/ n# h$ n$ H8 g" h" Ahich measures ram and static pressure. Used by
/ y \8 |1 ^" W, u4 Birplane instruments.
: q8 U7 p& h& j丝钉。由平
- J7 Z P i1 G7 E十字头螺丝钻驱动。" j! B3 b+ _8 S' R" q" { h
仰,4 c+ C" D5 Z6 s5 {" A6 q% a) [! h
飞机绕横轴运动而造成机头的上下运动。
1 s* q+ h! o* ~* c% r) j9 ]一侧通向另一侧的水平轴或横轴。升降舵控制3 n0 t# E* R3 }& B$ g8 w
头绕此轴作上下的运动。(水平安定面则用以配平。)
( Z4 e: l* l3 i' {. }4 v$ ^! m$ B' G俯仰率,
4 C& e: S T% `9 k) y5 C飞机绕俯仰轴运动(机头向上或向下)的速率。
% P5 K# a# G$ R$ f$ M) @管,) b- ^# w& R) T* b
开口面对气流以量取空气的总压和静压,供飞机仪表使) j/ q1 O0 B9 o# s
的管道。
/ t4 {2 b; s6 P- }( a! h0 kdistinct tapers. Driv" H# ^* x; {" ?" E8 [
s
$ ^ K$ {6 d/ p: Q% r5 @P3 f2 F: U. q; E3 v+ K1 c! }3 D: d
a
! I2 K9 }" x5 W# a9 l% [/ yPITCH AXIS, A horizontal or lateral axis passing- R0 `4 }6 _4 K% E! z3 `6 T
through the airplane from one side to the other. Airpla
& n0 A2 m! k/ d* K8 ]9 |n
4 R+ i7 t1 Y2 H( y+ P" ee
2 [* j8 R. q- {- a/ J4 W4 A& lP
) }7 d2 O, M4 w2 Oth& p! U+ u$ Q+ E' S
PITOT STA
- p/ s1 d( n$ {2 Iw$ o! \* _0 y/ R. u% T' P9 f# b4 z" E
a
& x- S# p+ w Z! U9 k2 u$ |% r十字螺丝钉,' w1 \# y! o- G
螺丝的顶面有两个明显的锥形十字四槽的螺
$ N/ i. W+ D4 l* s6 a3 l顶
. H4 u8 k9 ?/ `6 w2 E0 s- x$ `俯# A3 w1 E) Q: g( d$ C' J* O# A. r/ X
俯仰轴,
3 e7 c- m/ \2 U4 ]2 w8 e从飞机" R4 E; M" S% {8 P" E9 F
机 S4 r% h$ _9 v
总静压
& u5 J& I& ^4 w: P$ y7 u用1 I3 M' n- [) y, N9 ]
英汉对照民用航空词典B OEING
# G9 G* l; h* M/ `- f+ `6 ZTECHNICAL DICTIONARY 114
2 ]1 {6 b5 \' W5 r7 n8 MPITOT T
$ D* f9 L& r2 w# J6 j+ N1 tmeasure
0 \+ G8 ^4 v) S/ EUBE, A tube facing the airstream which- X& C U+ ]6 r
s ram pressure.
4 K- @- D K. y' y( n1 uPLA, SEE - POWER LEVER ANGLE
2 B, ?7 o; [. }0 @r! z6 A' ~! B/ f1 C6 \9 r1 T
e
, W/ M" V* p8 C. JLEXIGLAS, A registered trade name. A transparent& X# Y* g. o a3 m
r any purpose.
0 U: ?" x& Z$ W% PNEUDRAULIC, A system or process which is a
! L) l, H: O% \9 _( f3 tres.
' w3 I. V- ^% W7 J9 E/ f) F% mPNEUMATIC (NO. 1), Cold air, controlled and/or8 o# [/ n6 f9 ~1 o$ e# a" n
pressurized.0 O" {; Q A; Z5 y7 s
托管,
|: r5 c2 x7 z5 a; A面对气流以量取动压(冲压)的管子。
) e4 d# {. t J' o# d门杆角度,0 J, z, ]5 T( ]' a: o( X
见Power Lever Angle+ `3 y, n+ I: R3 f" Q4 ~, X g
PLACARD, An attached sign providing information o, C4 H1 ]4 v0 G: b' @
instruction.
& E* i1 H! r, @* ^, b8 s9 ~PLENUM, An enlargement in a duct which changes th8 }/ l& E9 X( d3 N- `8 v' W$ w4 `
flow characteristics of moving air. Used to remove
2 x- M6 P# [7 C9 K8 d5 `' H+ vpulsations caused by variable airflow.7 [! h9 }: U7 P3 V) v; p: z! ~
P
+ U8 m1 O3 N) `% p& a4 k8 Jacrylic plastic material used for aircraft windshields and
, ?$ p" [' z$ Z: P- }/ M3 lside windows. JARGON TERM - sheet plastic of several% V) G( M6 c7 Q0 ]' x& Y- k
types and used fo% D9 x1 J% s/ J
PMC, SEE - POWER MANAGEMENT CONTROL
1 q9 S+ O2 O! M7 Q6 h' y) PP- a& D. T3 i/ E; E' `& x
combination of hydraulic and pneumatic pressu" ?' D( v! |; f7 P1 p0 G0 z$ o
皮' D9 u, P; d6 A* F7 ?' p4 _
油
8 ]- K# e+ v5 Z5 n" p' ^.2 S) d% B5 G: m# V' x# m5 U1 \
脉动。) j- g# l2 s4 [$ }+ T1 b
机玻璃,! z: w. C% N, [6 n
名。是飞机风档与侧风档所用的透明丙
5 ~6 ^' ?( s8 X+ ?4 Y6 {控制,; K1 r% m. W$ p2 P* v- _
标牌,
( T. q- {& ^5 D, J+ V提供信息或说明的附贴标志。. _1 i8 o' X3 n; S& t' V
整流腔,
& \2 O a9 n7 Q0 l' B. {9 \管道中用以改变运动气流特性的扩大部份。用于消除可7 t# ~5 v2 h/ L/ v: O \
变气流引起的
7 `3 {/ v% b! A% D- U7 A* T有
5 o1 F. {# `3 {1 R是一个注册商品
3 ~$ `/ _0 p7 K9 F7 ?/ j3 L烯酸塑胶制品。行家称之为多用途化学合成胶片。
7 h3 Q5 y7 n3 e# ?2 ^动力管理5 { f) `8 a# d) e: x5 x5 ^, L
见Power Management Control.
% y+ Z5 N$ @2 g% K3 F动液压,9 |2 P7 L6 z8 i$ N V; C* K3 y
推动的系统或过程。
7 `9 N% v" h/ q- U( ]" _1),
7 @6 M; t$ g: }. D8 |。! a4 D; d: E/ p
气
. @( O6 R m ^! L( X M由液压和气压混合
1 ~4 r& T% }2 P( }压缩空气(NO.. ?8 m w! W9 e' v3 `+ F
经控制和/或增压后的冷空气% ?' g2 K+ l! ^2 J( _; @% C% `! v& {
英汉对照民用航空词典B OEING
. D( p* K4 z/ m- n) lTECHNICAL DICTIONARY 115( y4 K* q0 B5 v- d3 S
PNEUMATIC (NO. 2), Air, controlled and/or
" G1 s) T {+ X* p; Rpressurized.2 ^% p$ j. O& K& m0 u1 L, T! g/ ~
OP OUT INDICATOR, A device on a filter which
4 `* {+ c; R; _7 g& E7 c9 Oroughout a material.3 _) W1 C) j& k; `1 O
ition.+ q& U9 ]0 g" P
POSITIVE, Definite and intentional.
c Z9 w$ W. ^+ Z5 U(No.2),
, q$ h. D! M4 ]( ^9 u出指示器,: G* v2 }/ t/ W; O9 X' K$ f. U
到达一定的压差时,它会从壳体内
( S# Q! N, d0 ]( t& T指充满整个物体的细微小孔或空隙。
" P4 J* |/ n( X7 C置基准的飞行管理计算机的一种操作。
$ r# w$ l5 N1 A. |: @! |肯定的,
" w6 f! Z8 G- e一定而且有意的。3 w9 B. n. t, h4 e3 E" h- i
P
; h# E% G9 X& j6 \4 j' Fprotrudes from its housing when a specific differential
1 h# u" }1 J" Y( d c! Vpressure is reached.
/ y5 }& v g* Q& i6 B# }5 I3 p( |POROSITY, The term for pores or small cavities' @9 J' H: T4 _5 v+ s+ u8 t
th( U# _9 o0 ]3 S' M
POSITION SHIFT, An FMC operation used to change
+ ]( U( B( _+ P+ |0 sthe reference of present pos
4 l/ M0 h6 F; U' P! Y压缩空气
, t0 `+ \8 K7 ?6 g' N& j经控制和/或增压后的空气。
8 b3 o/ U& ^% r8 u' P3 Y# B弹2 z3 y7 Q' P E/ F, p. C
过滤器的一个装置。. t1 O) b3 {; [' N
伸出来。" l l1 w7 H" J# \! ?' t
气孔,
# n; E5 D/ X' J9 n8 t移位,2 v# z- P( g+ N' O% p* q% ^ L
用于改变现在位6 J- H4 c: h, X2 U3 i
英汉对照民用航空词典B OEING
/ C: c% u& J" l7 e4 m' XTECHNICAL DICTIONARY 116! I+ \4 E) q6 L( j( y/ v
POTENTIOMETER, An electrical device for changing$ |& A: W o) `+ i8 v. m+ o
the voltage supply to an electrical circuit component.
+ e! N# d! R) z1 f& }4 {r+ I3 F- m0 n5 q* [
bly for operation of flight controls.
9 t. n1 ]( _& X/ y8 ~+ [OWER LEVER ANGLE, The angular scale on the6 B; h3 v& J! T& i, R! H
main engine control for showing movement of the power( z }7 e: \* k! c; b
hrottle) lever.% f t8 K, m8 d
OWER MANAGEMENT CONTROL, An electronic
" A' t3 P( b; qngine control.0 `5 G+ t0 F& w1 l( u
OWER TRANSFER UNIT, A hydraulic motor/pump for
$ X0 g3 w% u8 v5 ]upplying hydraulic power to components when normal
$ S7 C. V( g. l8 J8 Y8 F/ t9 r3 ]" s0 BRECOOLER, A heat exchanger in the pneumatic9 F2 [; b3 K) j/ v9 s
lied
2 M) B& b5 Z9 j5 h4 s作动筒,
k' s4 P1 O4 }4 W6 G# m件,
; l( p! j- I1 G( h/ T1 K油门杆角度,+ N7 ?8 [8 \& y- t1 p
主发动机控制上用以指示油门杆运动的角刻度。
8 L( P1 B* V5 |0 y动力管理控制,
! y c2 i- G, ]0 M控制发动机的电子装置。
?2 v5 P# M. G. l. k) k0 t3 ]力转换装置,; d% m2 `$ d, W- ^
当无正常的液压来源可供使用时,用来向部件提供液压. `2 g" z4 G4 L! H
马达/泵。1 h: R. J4 g1 d3 c9 B/ |6 T
冷器,# K, v" q/ S x
中的一个热交换器。它将发动机引气冷却后
4 y1 Z+ t4 q/ s# @, n1 _供给气源总管。
# n" Q4 p, |. PPOWER CONTROL ACTUATOR, A hydraulic actuato! u: y" \- h/ ^4 g" p3 L9 X
assem$ R* O( J( W/ X& v) g
POWER CONTROL UNIT, A hydraulic actuator6 Q2 `2 r8 {. s8 ?3 X2 c, ^5 E# p
assembly for operation of flight controls.3 d: J* @8 w8 P. ?
P
2 V8 j2 y) a- i w(t7 c; y$ w+ Z' |4 U* G# W1 g
P2 D4 G( W6 v: t; x8 I& U; w& u
e4 M- X/ b5 R9 V- {9 }
P. V; \6 X. ^# g1 U
s
) T/ m7 J: o/ Q3 hsupply is not available.
! i, x- Z$ ]* l. uP
1 t- z5 X# b" |1 `% U Ksystem for cooling engine bleed air before it is supp
8 S7 b8 P) C5 b6 C% T4 E7 b4 zto the pneumatic manifold.7 Y5 K$ a4 y; e, ]3 C' }: a$ W2 n
分压器,
" {8 y0 Q0 K2 K+ `) G- Z0 W h2 T* r用来改变向电路部件所提供之电压的电气装置。7 s' g+ n% U7 f* [; C- O
动力控制
: k; K6 d9 r) S# p6 N1 D4 b2 }. s0 w用以飞行操纵工作的液压作动筒组件。# V2 g# B5 X- |3 O( A
动力控制组; `! c+ Z+ E, o1 _: e4 U4 O
用以飞行操纵工作的液压作动筒组件。
u8 F1 e% q7 b U2 z1 S; s动
* K0 K, n/ ~( e/ c4 O$ Y动力的液压
4 J/ q6 n# D! Y预4 T4 C- [4 ]7 X" {4 c
在气源系统) j1 y6 E( N6 K. D4 U! B
英汉对照民用航空词典B OEING
" i/ N- }" i: p: LTECHNICAL DICTIONARY 117
( E8 i5 `1 p" P6 `7 r+ \3 qPRECISION APPROACH PROCEDURE, A standard
3 R& F, S+ r4 n, D& e; p' i% Z/ _6 xedure in which an electronic5 Y; D" q+ |4 F( H
lide slope/glide path is provided; e.g., ILS/MLS and
2 b/ _. [7 f) s" S/ MPAR.
6 b0 G2 b. u0 Y. Y: @) hRESSURE, Force per unit area usually measured in
& j$ M, g( G5 E! g- S: mounds per square inch (psi).3 ~! {- }8 {0 z( X, f; T0 D) [' T
RESSURE ALTITUDE, The altitude displayed when
& n& d. J# ^$ {0 W2 D$ qe barometric pressure on the altimeter is set to 29.92
7 S( S, a5 l' i9 gRESSURE REGULATING AND SHUTOFF VALVE, A
: q+ s' U [" u6 E8 A: ^$ ralve in the pneumatic system for regulating bleed air
. S) n& S a! `( Y0 c J: zpressure from the engine to the pneumatic manifold." x: h. M; ~- ?. u; G
RINTED CIRCUIT CARD, A plastic or fiberglass card
2 V, J3 {8 L9 E1 r8 r; y9 R* qith electronic components and copper strips forming a
8 S' e" w3 H$ k$ I- q* ~, Circuit.- L; v5 ?7 T" N: w; ^/ `
RIORITY VALVE, A valve in the hydraulic system for) J2 B7 z. Y: J' w
ROCEDURE TURN, A maneuver where it is J1 n! w6 V& e) g
lane
# ^, z: _4 X4 Tproach course.
+ ^3 G, K! ]+ O. d& \' S9 b精密进近程序,
+ y0 m6 ]- x$ l- {8 v' r9 [己提供有电子下滑道/下滑航径的标准仪表进近程序。
" v2 O1 O# p, p1 q6 ]- P如:仪表着陆系统/微波着陆系统,以及精密进近雷达。: z; b: t) n8 i; Q B2 ]: F' {
压力,
1 p7 W- B# k2 C$ n0 n$ c单位面积上的力。通常用磅/平方英寸(psi)来度量。
9 G6 w& f9 F* x: i, ?5 B9 u$ ~5 q压力高度,
{: H0 V0 K. x1 x8 _; q+ j% x4 U当高度表上的气压调至29.92英寸汞柱时显示的高度。
8 x* A5 A8 I* M! _8 V2 C3 C7 }力调节和关断活门,6 \4 v. h9 Z/ g
气源系统中用以调节从发动机到气源总管的引气压力
! z7 I! S- ?: g( y的活门。
/ V8 C+ b+ C0 c5 m8 M刷电路板,
4 J' V. Q v, f1 X% O- K3 `由电子部件和铜丝所组成电路的塑胶或纤维玻璃制* e- s7 Z# j; H( U3 [ [6 o+ Y
薄板。
$ \8 i' j: D' z" {8 e先活门,! G/ y, u- e; o7 S
,用来使各部件照合适顺序操作的活门。* z1 j. H$ R) b
序转弯,
! e, M6 {0 W" d" K" i Z7 Z5 O后进近航道时所做的机动动作。
* N1 {) F% ?7 p winstrument approach proc
* w' L/ e5 f- [( E4 [. k1 ]g
1 W/ T6 ] Y7 n: F' JP
) y1 y1 \4 V: E$ _" x! l+ {p5 U3 f9 H, C9 W" J, z( F+ ^( Y$ W% T& s
P% I4 W2 T% m8 }
th- C9 |" B& |! v; ^% x
inches of mercury.% r; G. G; t! N9 a) |
P% q, s& w( H3 T9 v3 g2 n* I/ l# A
v
4 n2 R1 ?2 z( @P$ I2 \! r; C! Y/ r% E& i1 l& b0 P2 x; j
w; |3 E3 E- K* x9 @1 m7 N2 X- X* A
c& z( b( n5 G/ H! b2 k
P. ~5 s& |: L) `2 u1 x6 L7 H* K/ _
operation of components in proper sequence.' H @6 Y9 u4 d# x) W
P. a( x# T6 @1 h( D% w; n
necessary to reverse direction to establish the airp
6 ^3 y6 v# g Jon the final ap
: m' P$ m% n; X. M8 s压, Q. V& B6 q) H2 D4 t6 D/ w/ C: r% R( a
印: x+ {! ^& B. I' C2 C0 L1 B/ m
优
# k' w$ r7 r c液压系统中6 h6 K) ?+ G- ]- h1 r Z! I
程
' u* _8 p2 s6 ?4 {在飞机必须反向建立最
9 Z2 f" F* @! c- h, l' O英汉对照民用航空词典B OEING
5 ]8 d9 K3 C* W2 x" T+ [+ LTECHNICAL DICTIONARY 118& K. }1 e/ T j+ C
PROXIMITY SENSOR, An electromagnetic d
' ?+ G& x2 ?! T) _+ M, | Zsenses the po4 d- `3 C& Z# }3 c Q
evice that
3 S" G# S, J& c4 wsition of a moving actuator. The sensor
) B+ @5 }! }$ X. h) S: Ias two or three wires." J2 z: f, P, Q* Q1 j6 }
ROXIMITY SENSOR ACTUATOR, A steel plate
. v) Q2 N3 e7 X* Z8 D) Rcated on a moving component for operation of/ k# U9 z4 R8 B0 u/ N' s8 l# D
roximity sensor.
5 g1 c9 ^5 A. W1 @5 V% t5 N9 {" RROXIMITY SWITCH, A printed circuit card for
p3 h9 G6 Q' d) N1 i7 ytransmitting sensor signals to indicating lights and
/ c1 Z i, I; f8 |6 z% @, d邻近传感器,
- p6 ~ r1 O9 T7 _+ y能够感知运动中的作动筒位置的电磁装置。该传感器, Z# \1 L0 f2 U
有两或三根电线。: F; J1 v% q- i+ v( S
邻近传感器作动器,
9 r1 b* V3 @; G位于一个运动部件上,用以操作邻近传感器的钢板。8 M" N% j# A" c- ]+ w# Q' s
近电门,, Q: S0 a. @$ [, s, G
传感器信号传输给指示灯和电路的印刷电路板。8 x8 D) m' ^# S/ U: C' d! ^# n5 K
h1 U8 [5 ?, z" c* A1 v; H" |
P
% ]" b8 r; [ [' O: J8 blo
: `1 t) G6 g" v p+ Op+ Z$ S# T, ~, V( m( B6 W6 N
P. I) t( \' g6 Q4 i1 t
circuits.
( W3 N1 w F' _1 T! `- e邻
2 {$ y; w* G7 s0 |0 R用以将
# I& G4 S4 X. @- W! d; L2 ]6 l7 ]英汉对照民用航空词典B OEING
; ?& j1 ]. Z* R/ K) q$ [- GTECHNICAL DICTIONARY 119, c6 p+ A+ p! m6 a
PRSOV, SEE - PRESSURE REGULATING AND! n6 `5 O" m4 \8 `* ^( s, a
SHUTOFF VALVE( ?8 G+ T2 M- H0 a, v* w: A6 x3 J
TU, SEE - POWER TRANSFER UNIT$ [% _4 ~. n3 d# n! W1 w7 G8 z! K. r& v
removal of dirt from the air cleaner.; d: u/ C$ M6 A! _/ o8 h7 `
n
8 v5 I# [- D# z5 \QAD, SEE - QUICK-ATTACH-DETACH! P' m5 [/ W! H- n& K
ICK ENGINE CHANGE
( z5 t& J& ^) P1 f; f( F" a5 Lheight above airport elevation.% P; z- q: D t6 l' T/ O
NE, Altimeter setting 29.92 inches of mercury, 1013.23 ~) \) J& ~3 o/ G N6 X
QNH, Altimeter setting which causes altimeter to read: p! ~( ?9 d# x6 X8 |& Q( i% p
height above mean sea level.2 r- D( ^( c$ O( ?& f& T
活门,9 m9 p$ X8 Y$ a2 h u1 N
P
# M1 |- o8 ]1 A- ?PURGE VALVE, A valve in the pneumatic system for
/ b& T$ n8 b E9 u) A8 F( @PYLON, A structural component for supporting a/ f* p* V' X. D, r# w+ b+ p! J2 A
engine from the wing.
7 G1 \1 l! Y$ R- rQ9 ~. P( [4 T2 p1 m/ K/ ~; @9 K
QEC, SEE - QU
) W: H: [) {7 }7 D. V$ |. cQFE, Altimeter setting which causes altimeter to read
& a3 b" ~& w7 T$ x1 aQ% J/ @& {* \- P) U; T) n
Hectopascals or 1013.2 millibars.- [' P1 L e: b5 N; ^3 K0 w
调压和关断
8 y0 O" I/ c1 P8 z见Pressure Regulating and Shutoff Valve.
+ |; B4 X, I* ]* y G5 o4 h. |5 v动力转换装置,
# v, t7 d8 e7 m见Power Transfer Unit.1 X' _( g$ y# {5 l. s1 _* B2 I
气源系统中用以清除空气清洁器中之灰尘的活门。7 ]5 k& K1 }; N5 I) A' M( o1 O" t
速装卸,
# w/ k! O2 {! C$ ~3 `见Quick-Attach-Detach
+ R0 \% }5 P1 A) k/ r Z+ ?除尘活门,
' u- b- D U3 S$ N- e吊架,
* J% {6 `# @4 K" i用以从机翼支撑发动机的结构件。
& |) K: _# v/ R9 k7 S( D' t快
. ^' u, d# t. d+ \" x./ s0 t0 ^: m, k6 a4 r) n9 I
见Quick Engine Change6 \; }, l8 g) S0 \7 S$ d
快速更换发动机,' {& ?" x( {( C
.
$ w' y, Y/ f: j5 N3 W. s场面气压,4 i8 R, Q: f$ E# j3 h
准高度表设定,
7 ]6 r1 [+ V3 p# ?: w; `# a2英寸汞柱,1013.2百帕斯卡,或1013.2毫4 R2 f- Q5 q3 Y! q, B$ H
修正海平面气压,
% O9 c# c6 v. _! ?; p! |& y" u使高度表指示飞机距平均海平面之高度的高度表设定。
# X9 Y3 t( a/ S6 A使高度表指示飞机距机场标高之高度的高度表设定。! A" q& |& O$ o) |! A
标 D5 \& m& p) D) ]1 T( F
29.92 A/ o* u: r( |9 {$ v
巴的高度表设定。
' F% u8 k- W4 }7 c) t/ E英汉对照民用航空词典B OEING
' t5 J$ l: d! B( K+ yTECHNICAL DICTIONARY 120
0 j2 M, `) Q4 G5 YQUADRANT, A mechanical component shaped like a7 n# M5 R: Y$ O, P
quarter of circle for transmitting cable motion in airplane
* N+ @ O9 y' QQUENCH, A heat treating process to make the surface+ c4 ]+ \7 _2 _. X( @$ B* ?* }
of a metal hard. The metal is taken from the furnace and- {8 R- `: g: k' U0 [ Y
QUICK ENGINE CHANGE KIT, A collection of% X7 V/ _; p0 ~) u2 `
e engine positions of a particular model+ W# p- Z D4 X7 R: G! e
irplane.2 R9 Z/ P) o) b* o
ng/ ] \8 w' P2 n. |. j8 c6 d! r, u2 \
accessories (hydraulic pump, fuel pump, starter) to the
# }6 s8 V. D% _: \; Q: ^- dengine accessory gearbox.( s% X/ M1 t# \
S, Established the
! c. N9 ?8 Z6 n+ bminimum amount of time to cool the wheel brakes9 k# G, F# \# D; C# R
before the next take off is permitted.
8 }# |$ V- A% t: @" Q0 Z* L进油或水等液体中。
- M( N% `" U, L/ A! g& q% m快速更换发动机成套设备,
9 W: t# s: ]2 O. S* H0 b& m置的所有部件的集合。
4 }2 r" L% K" x9 \" d8 M用以将附件(如液压泵,燃油泵,起动器等)接到发动, n! A P: b) H& @- V
附件齿轮箱上的夹具。
: A9 w+ ^% Z: I, r4 o快速周转极限,( t1 l( R2 D+ X, b1 D+ E1 g
在下一个起飞许可之前,已确定的飞机轮刹车的最少冷+ e# J6 j1 \ L p) t0 D+ A' d( F
却时间。
) T, j8 y3 i/ E- `control systems.5 M. S# k0 @) b! M0 a1 P
dipped in a liquid such as oil or water.3 h) r1 Z: f8 x4 M3 a+ T: k
components allowing installation of a basic engine on to) x) u& P6 H6 o: n: O; V
any of th% y/ u, b% e9 _3 V9 }
a
* {% K s- s" J4 {( Y* uQUICK-ATTACH-DETACH, A clamp for attachi* f; t+ N2 E$ E" G$ e% g
QUICK TURNAROUND LIMIT
' T) v' C+ L+ ]! c扇形盘,
. n/ A i1 ^ k3 p& J飞机操纵系统内,用以传递操纵钢索运动的扇形(四 i/ J3 P- F' @
分之一圆)机械部件。7 |# T9 O2 J/ O8 v8 k2 v
淬火,
k2 j# ~' j& _) @/ M: o一种使金属表面硬化的热处理过程。钢铁从熔炉里被取
3 U& l% l! @. u! a4 i& ?) f1 ^出后再被泡
/ s, k( E1 B4 B2 B( U( s$ M; c% ]用以快速地将一台基本发动机安装在一种机型的任何! U; \6 H$ A0 }$ O% ^
发动机位3 ~) X& Q# Q8 J
快速装卸,
* T; n% H0 W/ L( s机
8 M8 c3 a" M) Y5 c英汉对照民用航空词典B OEING8 U8 Y& T, X% o0 _! g8 @
TECHNICAL DICTIONARY 121
% e) I( Q: S$ S( v3 W" eQUIESCENT, Condition of an electrical circuit when no
8 h0 Y4 q) A# m, g' ~0 I) ERACK, A place for storage of modules in the
) G" Y/ L! d2 S5 c+ {$ m$ n: Clectrical/electronic equipment compartment.1 }2 L0 C! }4 s( U2 w
ADAR, A device which measures the time between the
+ {7 E- ?/ [8 z9 ktransmission and reception of radio pulses and provides
% C( o' ~ G/ }( Yinformation on range, azimuth, and/or elevation of
8 F3 j, R# i; P* V* zbjects in the path of the transmitted pulses.* L; h5 @. {% j2 W
om a, `& C4 V' s. ]0 A
ar.8 S, ~6 b6 f- L
RADIO ALTITUDE (HEIGHT) (RA), The distance of an
& J3 d. C% p% g$ i7 L0 Waircraft above the ground, as determined by a radio- n- g: ]% J7 b5 E& K& s
altimeter system.
8 P; k, x. P5 C+ N7 G8 ` URAM, SEE - RANDOM ACCESS MEMORY
6 X& i1 F7 ]% X. _4 Z* `# qRAM AIR, Outside air that flows through heat
2 I" Q- D N0 a6 B- Y, r( @" [exchangers in the air conditioning packs.
% P2 r: R1 T. b支架,. h# v8 z: v4 F$ W
电气/电子设备舱内,用以存放组件的地方。1 t. m4 K: l p0 ~9 x
雷达,
, Q0 S, t% d% }测量无线电脉冲从传输到接收所需的时间,并提供范$ K. m% z" C. X( Z; H7 ?
围,方位,和/或脉冲信号传输途径上物体标高的装置。$ d; `. v5 d" Z* z- {; s t+ w5 s
由使用雷达的空中交通管制员给予飞行员的航向。
6 d0 C9 K7 }& N# _! j) F b施发射出来的磁方位线。% a& U/ h: _+ J/ B+ }5 Z- K
无线电高度(RA),6 {0 c) \. j: w9 [( {- L$ O7 S
由无线电高度表系统测定的飞机与地面的距离。
& R; r3 p% W. L0 d$ k随机存取存储器,
: A; M3 D; U- E4 s* Q见Random Access Memory
/ V! ^1 d; @* M `1 {0 }9 tinput signal is applied to it.
$ a. C( [: j: F6 fR5 E" o! V" x5 z7 R, X+ d
e/ ^* E5 e$ v' _% s! n/ J& h0 @
R+ Z; H" h. z4 F0 p& l1 p
o. F3 ] U* R2 _. |) H& t
RADAR VECTORS, Headings given to the pilot fr
/ C: j0 [, I$ j; ?9 E/ y& xcontroller using rad* O5 D3 C9 C: ~) o7 C
RADIAL, A magnetic bearing extending from a
/ E9 f8 f' _5 Z8 ?VORNORTACITACAN navigation facility.
7 B1 @! q1 t+ F( H寂静状态,8 S( a; M& z% a5 e# K5 ?, ^+ v
电路上没有输人信号的状态。 y- F3 {8 U& X# Y
雷达引导,0 o' q6 K0 W! Q; }
径向线,
$ s1 Y/ @* U0 m9 ~) o4 u' r/ A由甚高频全向信标/塔康联合定位/塔康系统导航设8 p: D2 G& @; ?
冲压空气,+ h0 ]0 W/ S, L4 \9 f
流过空调组件热交换器的外界空气。! I O9 a+ H" J3 d2 }/ l- Q9 K
英汉对照民用航空词典B OEING
# y5 y# H1 s% b- l" ^TECHNICAL DICTIONARY 122" R+ V8 R6 w; @0 h) u( m2 x/ i: V! j+ z
RAM AIR TURBINE, A device which extends from the
, A- M$ w m: w! d6 `, driven by outside airflow for4 s0 _8 u l2 ?5 S; q; q
mergency supply of hydraulic or electric power.
8 p D8 I! C* C6 {& U. t) sANDOM ACCESS MEMORY, A type of memory in
5 w5 Z. ~6 U4 a5 L- fdata can be written into and read out of.( \* ^3 `' U. `. L% J3 }
used for short term memory.
0 t4 V; w8 o& F5 \5 dAT, SEE - RAM AIR TURBINE
2 m8 K% l1 D. {# ]ATIO, A specific relationship between one number& n4 s- m; ?7 ]
alue and another.! N I S+ O5 l! L, [$ u$ T
ATIO CHANGER, A mechanical device for changing
2 E+ g' D" ^- c" s& W& N. G" }* \utput speed or movement relative to input speed or% J1 [+ f1 w9 p9 Z x3 s( }
AW DATA, Data from sensors not modified by the user. K, g6 n: S$ E; f* B
况下提, A# M, u, n! F
液压或电源的装置。
$ d v! O+ d. K0 c机存取存储器,
) e/ |/ D$ r( h! M# h一种可以将数据记载和读出的存储器。一般用作短期存$ r1 P c2 M, m5 n
。" [+ t3 s( m- I8 ?
压空气涡轮,3 l6 U( B1 T7 @! x- D. J# `1 h
见Ram Air Turbine
8 E/ t% _# L% }3 g" K/ Dside of the fuselage
* Q4 }. W& I) p' D9 l' ne1 d$ |& l6 I% h& g
R J8 w0 X* B: {- H! q( N8 J
which the# W2 q* f' o* c
Normally
/ ~% H! I2 ?* w. m- S/ G3 Y( F3 JR- \1 Q% ]+ U+ h" X5 o* s a& @. _
R
' A+ B. q' ~" L# T" u6 e$ Mv4 Q6 ^7 ^9 N5 P7 ?
R
3 f% p0 x2 G+ G: c& d! To( Y7 n6 j3 q1 _: p6 A
movement.
& L- K2 p: |* Y: ~4 H8 i* ?R
( ^) i. c& ^& P/ _0 \! D+ g! l' Qsystem.
8 ?1 A- N* _5 p$ {! f冲压空气涡轮,
: D2 O% G: U) A6 S* `从机身一侧伸出,由外界气流驱动,以在紧急情) D% M2 y5 I& D- r
供
/ f. N0 u$ w2 o" g+ O随! G- F+ }5 D E8 W3 n% H: B
储
- L8 I+ h, m. e' t' E D/ s冲; D$ W8 Z, t8 w' o" K- n# X7 k0 i
.; v. B3 _$ d8 v+ x
比率,
% N+ x- X) f: K. e; K* @4 l一个数值与另一个数值之间的一种特殊关系。! K( W1 n9 p( Q9 v0 ]# \, h) M
率转换器,& a( w- O# k% I% u% ^% U5 l
用以改变输出速度或运动与输人速度或运动之间比率
" ^9 t s/ V0 l8 j6 B始数据,
( F+ ~$ R2 r+ u! b5 V' P任何修正的,由传感器得来的数据。0 |3 [1 S5 \0 w2 C
比% G/ s& Z2 s/ a1 L3 b
的机械装置。
* a' E% z: T: O4 F原$ i; j( s1 g f# c" U
没有经使用系统作
' P { }5 V6 m- `3 s英汉对照民用航空词典B OEING6 j3 m3 s x# b! A0 Z; J! Y' q8 B% d
TECHNICAL DICTIONARY 123
$ }4 K$ f2 L5 r# r x* MREAD-ONLY MEMORY, A memory unit in which
k' W- m4 O4 z( Uthe computer. Under normal conditions the stored
( g3 I, @3 w. N. Hinformation cannot be changed.
% Y& i/ H; ^% M3 I; f! ?ECEPTACLE, One half of a two-piece connector. It is
- T! h. W2 q5 k% A# k2 v! qusually mounted on a support, such as a panel.( `1 m* j/ x1 s8 j
RECIRCULATED AIR, Conditioned air mixed with air( j3 K: L: g8 H0 P# b
from the passenger compartment.8 L% |8 D3 N ^' h5 K( \* I
EDUCED THRUST, A thrust level less than maximum- F$ l- e8 A( P: y3 L% m
rated thrust.
3 Y8 R1 ~( w1 t: QEED AND PRINCE SCREW, A cross point screw with
! H$ E' I. Q D7 ia single straight line taper driven with a pointed tipped
: R$ i' e# M) t6 JED SWITCH, A switch with two magnetic plates acting
1 _4 u8 T# J/ u, ^0 G. l$ qs contacts and operated by a magnet.
; ]# F/ u9 J- H' ^; [) b6 u只读存储器,
q- ]4 `( a- k/ _含有由计算机永久存储着的指令或数据的存储器。在一; O! {8 \! h) Q6 x% ~1 u8 @& W
作任何的修改。
0 `& i% n C$ N3 d插座,* T8 A& L; f! D( J* N/ ~. z
由两件组成的连接器的一半。常被安装在支架上。* K% Y" D+ ~: f) D8 [5 \
如:仪表板。
% \% t6 P2 g4 `& V, T4 g- ~9 P) p+ o再循环空气,
1 k1 W: S% U( E& y( D8 E: A8 `调制后的空气与客舱来的空气之混合。
7 B" p' [! b& y% G! o+ D) T1 y减推力,4 i& m! }* D- g* n N* E
额定推力小的一个推力级。4 L& |9 J, y( e$ M" k/ x
十字螺丝钉,
" g- a$ z- z$ ^9 E* m+ O( u的,带有一条直线锥的十字
/ [0 C2 Z4 I4 F: W2 e. o舌簧电门,
6 F/ Z$ O4 a4 M F由一个磁体控制使两片磁片接触的电门。# d9 y( @8 H* {6 ?7 D
instructions or data are permanently stored for use by
, E. c: J* W: k" F5 AR; E2 ? U' c* U1 }5 `( F* k4 q
R+ L; e' I6 Q' m4 a7 Y. d6 J; ^
R
, d- g0 t' {' t$ f- e0 Q/ bReed and Prince screwdriver. (See Phillips Head.)6 Y3 P( `! U: V
R
+ |/ b0 }- U5 X9 O- za
6 E, S* m' ?! A1 ]- {般情况下不能对存储信息
0 r$ P! Q5 T, M7 K( J( ^- @比最大/ o6 H# e8 g# S1 E# Y
与尖头十字螺旋钻配套使用! x2 c' q* ?, k* f
头螺丝钉。6 p: Z; \: i& D: u* N; _9 U% _* X
英汉对照民用航空词典B OEING8 }6 @1 i( W# E5 S5 z* x( c' C
TECHNICAL DICTIONARY 124; j) u1 @8 a1 F8 m* o$ P, g; X' g
REFERENCE LINE, A line used in a chart as the& l8 M0 ~8 A4 ]! O: c# P! u( a: V# t
starting point for applying corrections to chart input
9 C" d. a! `: q3 S! }$ L0 xalues. One or more reference lines may be used in
0 E+ R9 P" Q% ^% U- i) uuccession.; A; H9 Q$ g3 w& B
D TAKEOFF, A takeoff which has been
0 l! c( X& T8 j9 S.# Y* ?! ], w7 e3 [! U# e
EGULATING VALVE, A valve for controlling pressure
, s% c/ Q0 g L$ s9 GELAXED, The state of an electrical component or
* V7 e0 t S, W. }" w) Vwitch that is deenergized.
# V" |9 q. h. X1 |+ [RELAY, A switching device in which the contacts are! q4 ?5 c# a/ z1 ]% p
opened or closed in response to separate current or. U, d/ [ z2 F; c' k2 V
oltage.
' u) m: O1 n URELIEF VALVE, A valve which prevents high pressure; n2 S9 p( {. G
a system by venting the system to ambient.- }/ Z W8 _7 m7 A( j- {
起点的线。使用时可用$ x1 N. x O+ s; R, _+ Z; z
条或连续使用多条。8 a! n" Y5 W ^6 b6 C# p3 i
断起飞, [ P* {8 P& C1 L( {# d
离地前被停止的起飞。
& q" v" F4 q, S0 {# a/ D, ?节活门,
7 j8 C; K* ^/ r- G& _+ U8 J$ d制压力或流量的活门。) S, R' Z' Z$ O5 x
放状态,! `( n3 {5 _& K3 M
电器部件或电门处于关闭或没有通电的状态。/ k# t: M) k9 V5 Q
继电器,+ k# s& q" Q: J; y* b
一种电门装置,其接触点随着单独的电流或电压开路或
+ B' u4 J# n( {+ k合。
' X$ }; f4 M) P释压活门,
- |+ a& G' h, P通过将系统与外界相通,以防系统内压力过高的活门。. z/ f3 ?' o4 t& z
v' ~! y% l! C( a
s
6 H, |9 n' G1 cREFUSE/ ^7 U7 g6 n/ [# O
stopped before the airplane lifts off the ground) e: m& S+ `& i! g8 F$ L; z
R
$ e' w5 D8 I" t4 O2 Oor flow.
M) p% V( ^& m# J& lR
& Y, Z8 p+ Z) i8 O" P L5 Ks
2 `5 K0 W3 w( O) Z# B2 W6 N+ G8 iv
5 A8 ~9 a% d2 U% K' l I( `in
1 ?0 C4 ?7 Z- F2 K2 W6 h8 d9 z2 m基准线,
X) n* n( t' q) ^: ~8 v在图表中用作修正图表输人值的
& P$ A9 G- b. q- \( m! p( p一$ d0 g1 f4 O, Z+ ]& U. ~5 P
中
4 b) _9 ~9 S0 o$ R3 \在飞机
4 l3 ?$ r/ h) L调5 s7 s; X3 E- S. Y7 q
用以控8 m( a) N5 A" |
释
2 h' C7 {8 I# V& `- u: r! Q闭
7 w: P/ v' h1 P% Q英汉对照民用航空词典B OEING
+ H% l3 F* P+ v0 i% K+ i$ |TECHNICAL DICTIONARY 125
( C- u$ T5 X5 K: G! ^( @( DRESERVES, The required fuel remaining on-board after1 M8 B: l5 R3 o2 P! n/ V( D
ESERVOIR, A container for storage of fluid.
9 s! S% G4 z0 g7 C; Z& _ESTRICTOR, An orifice for reducing the flow and5 `9 L- i9 r7 m
ressure of a fluid.
4 b/ ]% E# s: U; U! S' }ESTRICTOR CHECK VALVE, Same as restrictor but
! e4 t+ e% a* K+ }; H% R$ X# ? H7 bllowing flow in one direction only.
+ U, ~/ F5 D9 D2 sdecrease the3 |0 I l% ~( t' n) ]6 x; ~* U, @
ngine thrust to idle.
* I8 D3 w4 |* Q! S1 R: oREVERSION, To change to a pre-determined mode.
' C! M! A1 j5 ]* w+ Zctrical device for changing the
6 b* w/ A0 T( hsistance in an electrical circuit.
0 l k Q5 k- \- z备用燃油,
* x; S3 S* ?8 |, N照规定,飞机在到达目标机场后,机上需要的剩余的燃1 C0 z' R6 I4 l! b5 ~& j8 ]
油。
- T' L0 [8 K& l- T2 P( ?储液箱,
) Q. |# g8 R- O; u2 D3 A用以储存液体的容器。
8 m) @ |. X7 {: }( s限流器,
/ M0 \) u, M9 e8 b用以减低液体流量和压力的量孔。
) u8 Q1 P* u3 s8 |流单向活门,
* q: W; f) M0 s; ~5 `一个与限流器类似,但仅允许流体向单一方向流动的活
) F+ A9 ?% D" k. {$ E3 A1 n b门。
7 `% @7 _: K4 w3 s* Q8 ^2 T/ E) D门,0 x9 p8 A/ W" z0 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 N1 |& v, K5 Y9 W% q
。1 p1 R: x+ J" k9 h; B, b; h
改回到预定的方式。
. ~5 S, |2 C4 I" _用以改变电路内电阻的电气装置。
. H: ^' S( w5 q6 `. f1 }+ Narriving at the destination airport as determined by1 @7 B4 T' }5 ?* K% q
regulations., O8 M& C$ D1 _
R
! A+ e9 h( z) l- XR6 ?& h# e! |3 E5 j \4 a2 a' ?+ z
p+ w, B# _5 T& P$ p
R2 v0 o% I1 m- T; [- b2 |
a: T$ f0 O% `$ N3 Y
RETARD, An autothrottle mode used to" P! N+ J2 {& {" h+ K
e. `$ H' \ U ^5 d: U
RHEOSTAT, An ele2 B/ s) p$ s# F+ m$ \+ w8 ]
re; ~" B, d r! t3 O6 `
限
0 {+ b; F$ Y* Y; F2 J拉回油
' |- O2 \2 r" r" q态3 x9 i5 D0 l# k. S, Q
复原,' s+ r0 K+ J0 ~! r y; C
变阻器,
+ }( v C: L3 g: f, n1 Q. h5 S# F英汉对照民用航空词典B OEING
4 O+ Q* Q- k' ~! t5 k# lTECHNICAL DICTIONARY 126' s1 ?' O- A* E( o+ x% r
RIB, A structural member of airfoil shape in wing,
% l" G: ~0 `5 E/ Kstabilizer or control surface.
) r/ `0 p# d# {; lIG PIN, A metal pin for inserting into a moveable
( i. V( m8 [: \# B3 U8 {6 Romponent before adjusting the control cables and
) _3 @; B: ~+ t& Unkage.+ x- ~& y/ ^+ S; h
IGGING, An adjustment of airplane controls and doors
: [3 a7 E' D/ }5 `2 ]3 g; Fr proper operation.
& f" [; G0 q% x# ponditioned air supply to the passenger cabin.$ @7 e5 T) d3 {& I; N. s- K
装销,2 ^: @( e- H, Z; |8 a
在调整操纵钢索和链系之前,插在可动部件内的金属! M9 k! T6 k: E
。
( e( S' K7 z) r( O( U Q: q校装,0 n- e& g) D. s; k, ~) {# {2 @8 \
使飞机操纵系统和舱门能正常工作而做的装配调整。
# D Y/ W2 _$ G6 |6 O空调系统中,将调节好的空气送到客舱的管道。' S0 S1 A8 }+ I1 p9 L# k; u
R
" {4 L# }" F$ lc
! [. `, }& W" w. a$ e2 `li
$ ^# D, d( O: q9 T' MR3 n4 _2 V- I" ?* _9 Y. }" h/ i
fo6 t; e/ f4 b% i6 | ~* c6 }9 E
RISER, A duct in the air conditioning system for
& |8 L0 Z% W1 nc
3 F5 u) O: r0 v翼肋,2 |0 m' e2 @/ F- Y( y. X/ z
机翼、安定面或操纵面内具有翼剖面形状的结构元件。. {4 i5 I( x# I9 w& V6 l; @
校1 C4 z9 k( ^$ T( t
销7 e2 b+ j+ h2 g1 K
立管,
, @1 o7 S! E9 V$ f英汉对照民用航空词典B OEING
1 @$ K/ r; {# c5 I1 YTECHNICAL DICTIONARY 127* O# W$ U& n- t. L' o# S/ v8 |
ROD END (NO. 1), In a hydraulic actuator, referen) _+ e2 W4 A! x$ Z
the part opposite to the piston side of the actuator.4 c. ?7 |$ _- O2 h
ce to/ `. \2 y7 }/ L; L
D (NO. 2), A mechanical device usually a( {! A; b5 j" T K! L8 N
bearing, clevis or similar component attached to the end; F( i# X2 w( w
of a link or push-pull type rod.
# L- w9 q' d2 b( C6 O% D8 X9 ^OLL, The rotation of an airplane around its longitudinal
+ W2 b6 D+ l; Y. Gaxis.# q, d, l$ u$ i Y- Q4 G% G- ]
OLL AXIS, SEE - LONGITUDINAL AXIS3 t w" Q) ~7 p
连杆端,2 U3 a) h& d' y" V' q' v
杠杆端,2 \/ [7 U! k- | s/ n, _
一个连在活节连杆一端或推拉杆一端的通常是轴承,& w8 m7 ?9 b2 \/ g5 O9 s
吊环,或类似元件的机械装置。
# O1 r7 P5 E6 U7 A+ n" l滚,2 H( r0 `9 I$ i9 t X" ?1 E
飞机用纵轴作为旋转轴时的运动。& N! \; y" ~6 D" g$ {! @
横滚轴, R( e" k* A+ v# Q I
见Longitudinal Axis' {* M8 ~, r, m2 G- R V+ g, l% v' P
ROD EN# b4 n: v; |# B/ X/ C
R
/ z- s9 E2 C" A! t/ U, SR
' |6 i! v0 Y2 } L' ^( N' v9 y液压作动筒活塞连杆伸出的一端。! D8 i) V* s& y6 C, \* g
横) K- f2 D$ e" N( {
.
5 M3 w) y& Y0 i# ]) Z英汉对照民用航空词典B OEING5 w, O1 C! r" I% [
TECHNICAL DICTIONARY 128
. O2 P( V4 _3 K8 S) J( SROLL RATE, The rate at which the airplane moves
+ R. ^, T" Z& R; y* ^' |on the roll axis (wing up, wing down).
. J3 B3 J5 {4 m0 p! cOLLOUT, The final phase of landing where the$ }0 I7 q h# s# T! p
OTARY VARIABLE DIFFERENTIAL TRANSDUCER,
/ K; b* b: p& v" G; Z. ?ROTATE, A maneuver conducted during the takeoff& k2 Z; U: B+ o) @
n5 d$ ^. J2 x5 T% U5 W* ^
raise the nose of the airplane into
' d+ a% h- F. r* `e air. B' b" x T* D
OTOR, A rotating section of an engine (turbine,0 s4 [) Q- O, s5 ]" Z/ U9 p- L
ompressor) or a generator.
- o, }$ Y8 p- p# ~ROUTE DISCONTINUITY, An FMC operational# F3 s" [ E" e3 O- G0 b
condition, in which parts of a route are not joined or
, |; _0 X8 q0 P5 ^1 ~) Wconnected.
0 i& T! n& \( i2 yROUTE LEGS, The portion of a route which connects
, `) @, e9 Q2 s9 ktwo way-points together.
& Z* b# C" l, ?陆滑跑,
4 w) i4 E" z* T4 [1 U9 ^ w5 S' ]的最后阶段。此时飞机在跑道上减速。
2 v6 q$ m3 ?5 X/ w4 |. N( E,3 w0 y: r, i0 D7 W- O; y V, i
R
6 }/ D3 V( b; A% V Mairplane is slowing down on the runway., n# D7 J: Z) b% |
ROM, SEE - READ ONLY MEMORY
- J4 m7 d5 t/ c$ D( k5 i4 dR8 s$ {8 Z1 I7 k2 S
A device with a rotary input and a linear response.
9 T2 D& Y8 u0 L7 D* o* s# Z0 |ground roll. At the rotation speed, the pilot pulls back o: Q) q5 V: Q) L- z
the control column to
Z2 B4 s, J2 _# ]) Q+ Pth
4 r# a% n3 r, G. k8 aR" a: a; C. ]) D( y6 ^$ K+ _
c
, l# c9 @ G1 ~0 a' }9 V横滚率,
( x. \5 `, U" p( ^9 l x2 g飞机绕横滚轴运动(机翼向上或向下)的速率。$ E5 _8 I, O8 p- s( I
着% I. E T; H$ ~+ M
飞机着陆
& r* H+ c% H' \8 \, X只读存储器
" Y M8 O. c: Y: @见Read Only Memory* Z7 Q% C6 f( |$ }% ?9 B- V
旋转可变差动传感器,
1 T- J2 M9 O8 z人和线性感应的装置。0 e0 S- @7 l/ w8 X+ u6 ~! g' W
抬前轮,/ c$ c" ~( D! t
飞机在起飞滑跑期间所做的机动动作。在飞机达到抬前( f0 i2 O% k( b! K, w/ E
发动机(涡轮、压气机)或发电机的转动部份。1 A9 [+ T& [ b( c4 N
航路不连续,% w) Y5 v. Y" R2 t! p; w" j3 A
一种飞行管理计算机的操作状况,航路有些部份不相连- e" H1 b: z q8 c" b+ ~
或不相通。
7 V' i% O5 P Q; @! F航路段,0 ~! }( x. M/ v; u. R- q
将两个航路点连接起来的航路的一段。
$ a+ n) z: b% W' g9 K6 g+ b2 b# i' Q一个具有旋转输
, N- v" Y$ z5 b4 V- V0 q. l* {轮速度时,飞行员向后带操纵杆,机头上仰,前轮离地。; L) `& [; j5 q
转子,
. w- h' [. H1 [, m0 X9 m英汉对照民用航空词典B OEING
1 ]; T5 ?8 j* ZTECHNICAL DICTIONARY 129: F5 l7 r: ^- u. E- A& y
RUDDER, A hinged moveable part on the trailing edge
0 b5 P4 g1 l3 L: Z) e5 B% mplane yaw (left and right)" s! P) Q9 {) t# E7 c5 k( A& g2 I
ontrol.
0 `$ g8 d) G2 `. NRUNWAY VISUAL RANGE (RVR), The horizontal1 P( O# k4 D) l z1 S* A
a pilot can see down the runway when flying an* i1 U- ?, K! E
pproach.% W+ L2 _7 Q5 h# t* v* `( ]
of iron and iron containing metals." T2 N- s+ i* P! ?: S% B4 p
is usually a reddish brown color.
9 p; ~7 u' y. B% kIAL
9 u; y7 K% S, Z1 S+ f' x/ l3 ITRANSDUCER
, G; u, J* T/ h0 A1 ?S f/ C" l* [. k# `! S
SAFETY RELIEF VALVE, A valve in the pressurization2 }% f, s. a6 Q4 H9 X+ r7 I
system for reducing cabin pressure to a safe operating, P" [+ d/ a! d( z2 r0 s# u
pressure.
# T/ Y1 w7 I! X3 z0 h- h; ESAT, SEE - STATIC AIR TEMPERATURE
9 U; e Y6 h7 \3 X" Z' B或向右)的可动部件。
' n/ g! }3 ~! H, _' f进场时,飞行员向跑道方向望去所能看到的水平距
# I+ D/ x& s+ s! B& n( l6 T9 T。& f. J# }- W$ R2 S
铁和铁类物质的氧化物。常为褐红色。
- u9 `0 I ~; h2 D! u2 l# e4 M见Rotary Variable Differential Transducer2 D- O! x6 t2 L- R& [, J$ z
of the vertical stabilizer for air
0 \ o/ Z3 P' M3 s: g2 @4 cc2 t* a4 `/ w6 V
distance6 B; w) d; P5 w$ B
a
8 \* b: a! Q& k* X; c v" V, z6 ORUST, The oxidation# S" u; r- w6 F
It* U& T9 c" P* N, L& k5 a7 X
RVDT, SEE - ROTARY VARIABLE DIFFERENT
S. l. R0 G5 d1 [* [( m方向舵;
( K4 v6 |/ `: D. B铰连在垂直安定面后缘上,用以操纵飞机偏航(机头向
( b- ]5 N8 x1 Q6 k( P3 e左
( Y( \" L1 K: |8 Z+ W跑道视程(RVR),
9 |5 N4 R- ]2 N% i4 K1 e飞机+ s) m! d0 P3 Z
离% J+ L- U3 F6 r' e$ M$ M3 a
铁锈,. ?/ k5 J f1 A- D1 T- C
旋转可变差动传感器,' K3 _9 `! E \
.' ]# Q7 o$ a+ ]5 \- o
安全释压活门," X* ~2 `5 l5 B! Q
在增压系统中,使座舱压力减低至一个安全的工作压力
: N0 k( }0 M; r的活门。
# T: M/ P* Z1 S# M& S0 w0 y静温,' ^1 |/ z& D* f9 Y; J+ p& G, ~1 ^
见Static Air Temperature.
+ D2 u: p( f: s& U6 I6 r" `2 q) t英汉对照民用航空词典B OEING5 L( p% E6 ~9 s# ~# a
TECHNICAL DICTIONARY 130. Q: y( x- K! {$ ~
SCAVENGE, To remove oil from the engine bearings or
' _0 J! Q/ @: i& D3 h7 m2 M4 ato remove water/fuel by a pump from a tank.
9 l' J# w- ?3 wCHEDULE GENERATOR, An electronic component in
/ {5 n; A, P7 e9 m# J C. }e pressurization system for controlling the operation of& h, p/ c. r) S" f- L- f8 l
e outflow valve. k* [+ n$ { q
CHRAEDER VALVE, A valve for inflation of tires,
6 u5 B V" y* g+ ~truts and accumulators and for pressurizing the water* Q+ X- n7 P/ ?' r6 g% n; ]
CR, SEE - SILICON CONTROLLED RECTIFIER
a! H* \0 Z8 W1 W$ a0 BCRATCH PAD, An area on the FMCS control display
4 T7 c) b9 n0 s `( sunit used for showing characters activated by the
/ _6 w m7 k/ Tlphanumeric keys.
5 x9 W! \ P! w) @, ]5 O- XSCSI, SEE - SMALL COMPUTER SYSTEM
, K: z# ^3 w# Z n2 _INTERFACE9 r0 y0 a W0 w- {5 L( \
SCUPPER, A shallow receptacle around a filler neck of, D( r4 G% t% w. ^4 @' A$ X
a liquid tank to catch any overflow or spillage from the
( z7 E; i8 h7 t. P5 Gservicing operation. The scupper is normally fitted with a: i" `0 _7 a. E& K& R8 n
drain overboard.) y3 g* |7 k2 o) J3 D5 P
SEA LEVEL, The standard datum plane from which4 g# h+ F, I/ e3 i
altitude is measured.
# @& ?( B [+ k& f% z7 A- f去油箱内的水和燃( z i; }$ ^8 N' \) a5 {
。 \. H1 O* `. B7 B( w4 L1 M
程序产生器,
6 v5 B. n6 B7 k* C% G$ G在增压系统中,用来控制外流活门工作的电子部件。$ V1 g& O6 }4 {& q# x. D: S8 D
chraeder活门,' I3 z8 `2 ~% W7 `
Schraeder公司出品的一种活门,用以为轮胎、减震支
4 N0 s) b6 Z M充气,也用于从外面为水箱增压。
: m, Y. m+ Y& k3 |4 F. h% Y( e可控整流器,
8 Y" R% P: s5 f; H1 g见Silicon Controlled Rectifier6 @$ F) g4 W3 G J! I$ Q
S- q' } t0 p; U4 }: V
th9 g' I- f8 }- N
th
2 F7 d( {3 M4 W& k9 m1 GS! y9 u2 ?! d2 B% A! O& h ]
s
: a% x/ o6 x: c/ E/ utank from outside.( H% g: a6 I2 t( j& D5 e# g6 d$ B
S
% N: Q9 ~) W' E, o2 US
9 d- Q' I% y+ Q1 x2 w9 Q' na6 ~2 t0 g% l. e, [7 E+ Q Q
回油,
4 z& i" j* P9 G' h6 x& Z. `除去发动机轴承的滑油,或用泵来除+ m7 e! D6 V3 y4 }; I( I( P" i
油
y8 `0 s! K- ?: r, ZS* {6 J z, p0 C; s
柱和蓄压器* N4 r% ]/ V+ W1 p6 @
硅# f6 }% c0 Z# G' u
.
( i4 O( f( l" v5 T- |+ N9 D稿栏,
( b9 D5 f* D9 oFMCS显示器上的一个区域,用于显示由宇母—数字键
# E3 P. J6 [$ D! A3 m# ]/ ^2 `激发的字符。7 G( G. U; |; ~- s/ H' \5 z1 J
小型计算机系统接口,8 M: F Q+ o9 v( X, k+ g" H
见Small Computer System Interface/ J: l& P# Z' `& L; h
草
& U. e7 ~$ V/ d5 P/ I$ B5 a盘
" x- x! t$ D% m1 i2 t7 c" j$ E! u; n.
9 g/ I- ?4 {$ ]" i" V. L1 ]; m放泄孔,; [' R. M% d8 y2 n/ k6 |/ L
液体箱的加注咀边所装置的小型容器,用于接取勤务过
; @' e' u5 a, r: z" s; l程中任何溢流的液体。一般都装有通向机舱外的排泄管9 ^& C3 e6 l8 Y
道。) G0 c$ W7 t: t
海平面,
. |% X; {( {1 U( N/ z用作高度测量基准的标准平面。
" @7 F( J! _# Q5 U英汉对照民用航空词典B OEING, b/ i5 M" T# {
TECHNICAL DICTIONARY 131* E# [% T$ Q2 k8 M* t" j- {
SEA LEVEL STATIC THRUST, Maximum rated power
( E# R! d9 M/ q. n' `. t9 V+ xproduced by a stationary jet engine during ambient- H8 {- |1 a, A X
onditions at sea level.7 n' f0 b$ w; v3 ]5 W# m- P
s for
0 p r7 X6 s! v3 ureventing air or fluid leakage.) {9 l) G: e$ y* \
SECTOR, A given distance between two checkpoints in: u' p/ Y1 D& y
e flight plan.% e% v; o1 S3 o( p% ?5 ^$ @
ELCAL, SEE - SELECTIVE CALLING
# v, F j7 e; M6 qSELECTIVE CALLING, A system that automatically
7 X) N7 N: h# Z# GSELECTOR VALVE, A valve in the hydraulic system for% a% g+ W9 ? Y: U, v* e6 Y' Q
o one side of the actuator
: T; d4 a2 V$ v" T5 und the other side to the return line.0 u" }. R3 ~5 P* ]. Z- O
力,2 I/ ~* _' m: H, M
在海平面环境状态(大气温度、压力)下,一台固定住
% r* ]$ _% k& C# ? T: S, X的喷气发动机所产生的最大推力。2 v+ x( S' _- ~' S
在两表面间防止空气或液体泄漏的元件。
4 |$ N3 _6 R! c) u航段,
: @( H; j) N: P7 a: q: }& L& ~飞行计划中,两个检查点之间的已知距离。! C, o1 m& s" B! E: J1 [9 e3 w1 D
择呼叫,* i, p# R+ U) B+ s! q$ f4 ?
见Selective Calling$ c' k3 L' b# g5 ]2 B
c
* V- y' d) Z& [' c4 cSEAL, A component between two surface8 ^0 {# W3 G7 Z2 H* P3 a; O
p; p' ]& J0 C0 O$ o! F7 E
th0 q) \' _6 j' G8 @% i {2 p, `
S, s" p3 Y; g3 V* V
alerts the flight crew to a call from the airline ground% g" Y* u; j; x- G; m
station.! G P# T: l% a( Y' \8 p" H
connecting hydraulic supply t3 p1 Z/ N- T" P) U# `' y* }
a6 C9 ?7 H4 F1 K3 `# _' G8 C
海平面静推
& q X, T# S G' g3 b) |封严,7 I& J' J. {/ B% y3 w
选! X n' q- [& i( K4 v% F% U
.
- m) {" U* q$ M/ D) {, Y选择活门,0 m/ r, d: K+ u# t! K1 T# o
端连* D, s' [ {9 Y. M- ]% I$ U
回油端的活门。9 h6 J6 E3 T9 L
选择呼叫,; }3 o) ]1 v, O U7 L
一个能自动将航空公司地面站呼叫报知机组的系统。
3 B- S6 d, R" a' n; h1 K6 o. n5 O液压系统中,用于将液压源一端连接作动简,另一& p! ~. _8 N+ I! O9 j# b( y ^6 {
接
8 ^5 @2 S4 g, \3 Y2 k; J+ v英汉对照民用航空词典B' p2 k9 X v8 S: _
SELF SEALING COUPLING, A connection between two
% D0 h( n- u2 P+ x' V8 tfluid filled hoses for preventing fluid loss when the hoses
1 J4 a5 [, U1 s& _5 Lrated.
% f) F9 U/ J9 T9 g7 D7 u& KSEMI-MONOCOQUE, Type of construction in which the f. B" E4 a; D) T7 @' {* D& w
SENSOR, An electrical device for detecting variable- j) j* Q, |) ]
ENSOR ACTUATOR, A device for operating the, \+ c9 }- h& b0 \
SERVO, An automatic control system which checks its6 w" R0 ?7 g* ?6 h- x3 t0 H
gainst its input so as to achieve a desired6 C) |' f' f) z( U& W7 M5 M; F
MED, Hydraulic pressure for the servo is. T4 r) |0 h& z3 a
resent to allow the servo to internally synchronize to* f; k) j4 w: W( ~( h+ K' x J
e proper position, but the mechanical output of the
0 V# V5 f8 d1 k3 B5 G/ `. hervo is not connected.5 Z" q3 s% L7 V5 h0 ~
自封接头,) m- C5 e) s3 u, F R; h
活门堵住通道,自动封闭而不) @* w% ? ]8 |# Y- G a1 `9 j2 @
让液体流出。7 @: V7 p3 S4 b' D! T2 R% m
半硬壳式结构,2 R1 t# k7 {- C
使蒙皮,长桁和隔框共同承受所有载荷的构造形式。/ ], F5 L3 u f
感器;5 F1 s# q! M5 c2 B6 U& X
量状况并将结果以信号送至指示器和指示灯的
; v- J# B1 d% D' P$ B% }! d电气装置。/ ?' X6 G2 _5 m) T9 v
传感器致动器,: r2 P2 o; E. \1 i& l% a5 w
。; Y/ h) {/ [- m$ Z2 _% Z
伺服系统,) i7 P( w M5 x- C( O
能检查输出和输人数据,以便合适调控的自动控制系
5 ~) T' H# `7 g) W统。
) o A* ?1 @1 F4 T J; K伺服预位,9 N5 \, p- O6 Y
液压使伺服系统内部同步至适当的位置,但伺服系统的
0 W5 E) f9 D$ Z6 `+ A+ G- Y6 X机械输出还没有接通。
- j/ t6 D% I5 U, v2 Dare sepa7 S& r0 k& J6 \" G# z _5 X
skin, stringers and frames carry all the loads.
# O P% n6 S4 w9 W7 Fconditions and sending a signal to indicators and lights.3 {; o5 V1 H: V& W# {# e" Z. I
S
# D) Y1 A" Y5 U) {sensor.
' g p5 I9 l5 Z# `output a& w- a2 x, N; G) v
control.) T) f4 F0 o4 h2 L2 z, @
OEING: ~0 e1 J0 |# E, O5 H
TECHNICAL DICTIONARY 1321 g7 V% i3 m, x/ l$ b. i
SERVO AR
. I+ }7 _9 E/ N, I* c( Tp
) N y: u n# I3 @3 B( Cth
$ I' p) m1 a2 [8 J; B" ns* V# b( x: O5 W$ \" ]1 s
用以连接两个充满液体的软管的特制接头。在两个管子
+ p" O7 Y1 h* Q2 f分开时,接头内的弹簧即使6 Z9 K f* l }; c6 a* s8 j$ j
传 w. W, S! H: x# W2 j
检测变4 p% Q" `1 v8 t3 u
用以操作传感器的装置
. A. T7 |/ C* S& R英汉对照民用航空词典B OEING, l4 u" e+ o3 i. q
TECHNICAL DICTIONARY 133
E$ W' q# b( `7 D. K* `+ `' uSERVO ENGAGED, The mechanical output of the" J* i' u' [& k9 x; p
servo is connected and the servo can move a surface or
+ L: b9 \8 Y: @) ?& kontrol2 E d' _3 I5 v$ ]9 G
SET SCREW, A small screw (usually headless) used to
. I$ O; n" H$ L) ?9 jeel, or knob onto a shaft and prevent* X* G& c3 i v8 a
tation.6 C/ X. \& f2 e* I5 F
SHEAR, The stress exerted on a material or, assembly
9 i* o5 ~7 z3 H- H, R" ?! uwhich tends to slide the mating surfaces parallel to each
0 Y: B+ w% d( ]: u7 F% N/ \ther.. |6 X* R; Z) l( z5 ~" X7 ~
SHIMMY, Rapid oscillations (left-right) of the landing0 s% j1 T7 T) Y, q- Q) n
ear wheels.
) L- E- ~4 Q1 y, L' x2 |) Z+ J预位,# Y. c- B$ Q( A7 q0 Z4 }
伺服系统的机械输出与伺服系统已接通,伺服系统可移( p( L( Q+ S$ z3 z( V
动一个平面或操纵。
6 P6 A( x! X8 @+ |小螺丝钉(一般是没有钉头的)用于将滑轮,车轮,或& z' w/ l& }7 E: W+ w# l
钮紧固在轴轮上被免转动。
, p7 I( @' I k7 s; Q) |7 o3 O7 Yc* Y! g h; g0 [7 q# ]$ s
fasten a pulley, wh
0 z7 s' J) d2 U6 Fro
9 r5 K* P7 q5 ~% U7 c# ]: aSG, SEE - SYMBOL GENERATOR; [( B9 u1 ^0 t
o
% W% [6 I Q7 p) Kg# Q$ d; A- X; C* S6 Q& K4 V! |
伺服系统+ x/ q% c3 j( }" f5 c
定位螺丝钉,9 P$ {7 X" v: N
旋) g. w# ?" z8 I# K4 [: o7 b* r; A
符号发生器,9 N& m& x* D Y" H$ O
见Symbol Generator.0 u9 t/ m: T. i/ `, d; S4 y
剪切力,7 c+ T, N5 w {4 k
加在材料或组件上的应力。该力往往导致互相平行的成' K9 S1 }" Y1 w2 T5 c$ ~9 X0 O! u
对表面滑动。 m) W# p- L3 b% U( Y p1 t
摆振,
F5 o8 u+ S" n7 B起落架轮子的快速的左右摆动。6 X: ?1 v8 a. c7 x( s8 Y
英汉对照民用航空词典B OEING* o# J- x4 ]: m/ Y* W- l1 p. {
TECHNICAL DICTIONARY 134
: X; n( Z2 E" s7 L# ~SHIMMY DAMPER, A hydraulic device for damping
/ j& B" H' H' p/ s2 p) Tshimmy in the landing gear wheels.
, V) t4 N5 R. p; x) }5 p/ Z2 par for
/ s n; V; K4 L9 M0 V8 p( gsferring oil from one; Y" N$ b: X9 x% B; n
chamber to another through a metering valve.$ f" V( @/ q1 i+ h# w
,$ n) G* b0 \7 T& r2 S5 S5 p/ E5 ^
一室以减9 A+ ^' x. c+ T. Y
着陆时产生的冲击震动的部件。
2 ^4 j% @* o- ]: r0 M# CSHOCK STRUT, A component in the landing ge2 V6 x, @/ P [# J5 Z8 R
absorbing landing shock by tran/ e6 u0 W& R6 x$ r- h/ ?) ]5 I9 v* I
减摆器,; @; y0 n! z5 K
用以缓冲起落架轮子摆振的液压装置。% J* n- G6 }- k" n
减震支柱
: ~3 F+ V7 a* _7 w- e e/ K. ?. p起落架上通过计量活门将油液从一室转到另
: h/ W0 V9 Y. Q7 U' c少 `8 \: I4 u& z( S, }
英汉对照民用航空词典B OEING& G3 {: t- ?& S2 A1 U. p' h8 @
TECHNICAL DICTIONARY 1350 C( u1 _3 B8 y$ ]
SHORT CIRCUIT, A fault in an electrical circuit
2 ^1 ]9 d+ @# V, o( hoccurring when the power supply goes directly to: @) D9 E( l8 b8 W% m' S/ J; h
ground instead of to an electrical component.
; }2 V. M, C7 u; ASHORT RANGE ALTITUDE, A cruise altitude chosen to
* g5 ~5 s" K+ q! @inimize fuel burn during short trips.
- T- e# ^8 Q* u4 JHROUD, A metal covering for enclosing the APU on2 }" h# B+ R! s
e airplane. An external tube for enclosing a fuel hose.
! e2 w Y7 ^( H# fHUTTLE VALVE, A valve in the hydraulic system with2 E3 M0 r( n2 g' U5 B
- STANDARD INSTRUMENT DEPARTURE& k# W( P* \. G( V
f the
+ L8 g1 _* X/ Z7 p3 lr access to the components on the engine.; H! ^. F0 H% }- ~% r5 E9 s! S0 M
短路,. d3 |+ h0 }: d; q
短程高度,
3 D) D) n/ Q0 k3 F' D为在短途飞行中使用最少燃油而选的巡航高度。, ^$ f0 Q+ M, m) Z4 T
护罩,
- |$ ~( _! i- I" N0 |5 E' w P飞机上包围着辅助动力装置的金属罩。包围着燃油软管
8 ]8 k" N) S$ V6 E用活门,6 E) ~2 B/ ] O: R2 Y
液压系统中,具有两个不同液压输人管和一个输出管
7 u1 x& R: ?+ Y8 j( z的活门。6 J$ K: a6 ~3 F7 k
标准仪表离场,
$ k( q. x: l0 u# t/ Y见Standard Instrument Departure1 r0 i! Q- P$ _' _7 A" _% W: Z; d
m
/ H! M: S6 y! G" x4 K; W0 `S
0 K3 @" f* V* z0 b* R" K& v8 i4 \3 oth0 [! B4 k4 l" ?9 e6 {6 g; V! e
S9 I8 V& V0 [5 L
two different hydraulic supplies and one output to a
6 K+ _ a8 i+ N9 G* ucomponent.& S" v0 {5 ]& b7 e, F' o+ l
SID, SEE! I; s& K# t: W; u( U1 _- S
SIDE COWL, A removable cover around the sides o
7 @; c7 k) T8 q- [7 P) jengine fo4 ]) ]. S7 Q# C9 e; Y# K& v, P
电路中电源未经电气部件就直接到地线时的电路故障。- e, u/ x* t9 \
防
0 X$ o$ r3 U7 t+ O1 X; P6 W的外管。* _) b/ N6 ~! Z4 k$ I: I
两
0 m4 w9 o6 H7 S* F0 O./ l! d3 O0 @- f
机两侧,被移开后可以够到发动机部件的可卸罩
7 W6 ]) K# G$ M5 W8 n7 M( n。 e$ V( \2 _4 X" d
侧整流罩,
" v! w; w7 m: G* p/ K* K9 O Z- \发动
6 q: ?) _. v- m# A子
+ \ t7 P8 v5 F英汉对照民用航空词典B OEING
- {6 p" R- F7 F L4 Q) lTECHNICAL DICTIONARY 136
4 f0 E* @9 j4 W$ z+ pSIGHT GLASS, A glass window for observing fluid
8 X2 Y# Z1 N) S& b1 m" Gquantity in the reservoir of a machine.
o7 }( A- z+ r, that can be used to transport information for- o7 t: w0 `9 B
communication, control, or calculation.
0 v1 x4 c% v' A4 NILICON CONTROLLED RECTIFIER, An electronic1 j4 L' |; O7 l8 j4 }( m
device allowing current flow in one direction after the7 w. G- v' b2 p# [2 \) Q
device has been pulsed at the gate.
) n+ @- q, F# `6 L( Y, ? C9 ZSINGLE SHOT MULTIVIBRATOR, An electrical circuit, D ^2 P% U" `" G- U _
-stable multivibrator.
# E1 @$ }" L( T) m' Z5 _0 R0 h: d! }如电流或电压能用于传送、通讯、控制或
: z+ ?2 N' M& w" R. U. }算需要的信息。
& k# e# H) K' t3 P9 |硅控整流器,
; n& U$ P1 t, s; j当其控制极受到脉冲后,允许电流向单一方向流动的电
' [ y$ |" b. J* Y, _子装置。" ~3 R9 q& p y: i8 J1 k$ }
息多谐振荡器,
x* W8 |0 ?, c( B输人信号触发电路时产生的脉冲的电路。又称单
- Z' c+ B0 @( _) n: O pSIGNAL, An electrical quantity, such as a current or
/ } @, B- W, q7 Tvoltage
9 z" c+ K' E' t6 gS9 y7 J1 g2 b9 \
which produces a pulse when triggered by an input7 k) W! B- r6 ~8 c2 O- d8 r& M
signal; a mono
" i+ M. G* v) V' X, q检查窗,
# ~+ o) Q+ S [# f0 U% F用以观察机器的储液箱内液量的玻璃窗。- s' f& w+ u" ]
信号,
1 W) q) O: {& S, |6 u- u/ {电量的一种。
. T9 D1 g' a4 y. T5 }0 P计
9 W6 |/ L' A# }: B冲
+ I J4 s1 o8 c& O8 G5 m当一个0 Q3 k; _: j( ~6 o y% _: A% E
稳态多谐振荡器。
" k! b+ b4 t% R英汉对照民用航空词典B OEING" V! E, w5 X4 r$ }
TECHNICAL DICTIONARY 137- |" W$ k( L- M5 a8 |; \/ y4 R6 T! `7 c
SIMPLIFIED FLIGHT PLANNING, Rapid determination$ \! c# l- W) Y7 [: K! S# F
of trip time and fuel using a chart providing these data( \! z6 G0 ?$ b; a, x. s
for the entire flight profile from brake release to landing.
5 |1 r7 G) O$ J+ h R& gSLANT RANGE, The line-of-sight distance between two
a1 i5 U }$ w+ Zpoints not at the same elevation.+ Z! l N' l) T- Z3 _3 a
SLAT, A moveable part on the leading edge of the wing6 {/ t$ V& Z1 o) B$ E3 T
for increasing lift at low airplane speeds.% D6 ^5 c. c* g+ }6 i
划,
8 {: h9 [% q% j5 j0 o8 j迅速定出从松* b; f" s/ b( @( @8 n
车到着陆的整个飞行所需的时间和燃油的过程。
) f/ x5 a( c5 S8 x斜距,
S( }' J- M( Z7 i* N4 Z不在同一高度的两点之间的直线距离。
: M4 |" D4 {: M+ q3 M% o% j; _缝翼,, K* L3 D" ^0 ?6 D6 `- B; _
用以在低速飞行时增加飞机升力的机翼前缘可动部件。
2 r5 r- W2 N4 z' u4 g; e简化飞行计
3 C- t! |' Y0 O: _' @0 W由提供旅途时间和燃油等资料的图表,来. S# t: n$ U$ K1 o# b' u: j
刹1 I- \# a f7 A, X
英汉对照民用航空词典B OEING
: N/ |- ]3 J2 o+ U; ]! ?TECHNICAL DICTIONARY 138; p6 s( b* i% ]3 `* ?+ F
SLOPE, The amount of incline a runway surface has
+ z8 m- i" k: n% G& |; o( xrelative to absolute level., r1 t5 i; b a, C9 P5 o
SLUSH, Runway contamination made up of a mixture of
[- B# x* `/ q' G [8 I; }' Bater, snow and ice.
% i3 s7 v+ b- q3 o# q5 k9 uSMALL COMPUTER SYSTEM INTERFACE, An input
1 N, a: M p. H3 j; J$ C+ [1 Qand output bus that provides a standard interface
1 k: U" o+ Q+ Q6 ~) t, Ebetween a computer and peripheral devices.
. S3 H" F+ W1 Q3 Z6 X/ {; pSMOKE DETECTOR, A device whereby the flight crew
# Q7 I( N5 I' F4 C1 Fan be made aware of smoke or fire in specific areas of$ x/ |# i7 e$ Y) T' J6 A
the aircraft.
& B7 M/ F2 V6 ]6 a, K3 WSNUBBER, A part of a hydraulic actuator that slows. k" f" {( x; y* }7 G" j4 Y$ b9 v
piston speed by restricting flow.
; V/ L. b( O" @OFTWARE, The stored instructions that control the a5 [2 `: V; _, n' D
perations of a computer.
9 B8 P3 _: H" ^& k: @, H- P7 s+ ?) Bng2 z7 ~0 \: X! e
other devices.
5 J0 ~3 w- Q' h4 {7 MSOLENOID CONTROLLED VALVE, A valve controlled
' D$ \4 R* l) a5 C6 l" M$ Y' uto open or close by the solenoid.
) g% _- z+ O0 B雪泥,
/ K, }$ D. U2 Z$ a) C$ }积在跑道上含有冰、雪、和水的混合污染物。
- ?$ x; F% v' k+ U小型计算机系统接口,- t' B% X; E$ s0 S: d( `" J
一个能在计算机与周围装置设施之间供给统一接口的5 m" S) c, h( |
人和输出总线。
8 m# t5 v0 k$ T( J7 A烟雾探测器,
- n. x' j2 B7 g8 U在机舱或任何指定区域内能测到烟雾或火并报知机组7 o$ o* O6 x, O% f+ U) ?
员的装置。
3 V" P. ?4 C( l- y, m冲器,
. M" S7 w: i( x$ {) F; P u液压作动筒中具有节流孔的部份。这些小孔能通过限制
! |3 l0 h, H0 ^4 e液油,以减低活塞速度。9 X) c& A% e8 p9 E- T" y
储存在计算机的指令程序。用来控制计算机系统的工; E: g7 E% B$ w s+ f; ~7 m
作。1 e) F8 x( `- x4 M$ C; `. p' Z
操纵其他设施的机电装置。3 Y, K; Y! W# h1 b, L+ ]5 j
电磁活门,
$ r9 N& B+ T0 o( S用电磁线圈来控制开关的活门
( B' D! @5 c9 O8 nw. R: ^* y; j. v6 B) B
c" c% Z$ @, T0 S* Q
S
) U& Y- {; K* I' io
1 N: k S. n( B; YSOLENOID, An electro-mechanical device for operati
% `# a, H* a" u- |. v8 R斜度,
" |$ Y ~ E, y* `) O跑道表面相对于平面的倾斜量。
$ @$ I! n' L; D6 W! U输" x- M& r4 `! V! ?7 ?
人) F- @- {& G! m
缓( L: R7 [4 W5 J
软件,
$ I ~9 o# V- `: f# g电磁线圈,
; Q; C( P% d! ^- d- i用以
( V7 ^2 }. f9 f/ V( w英汉对照民用航空词典B OEING
" \; p' O8 n8 U: ?1 P5 e9 xTECHNICAL DICTIONARY 1396 ~1 G* V8 x8 I0 L7 J J
SOLID STATE SWITCH, An electronic circuit that: W/ F2 X: e( J2 |) x3 p4 F
provides switching in a current path.
7 ~5 f+ R/ B# K3 }) \% J0 L' x- jSOUND SUPPRESSION LINER, A component in the9 @% _& |6 v1 e2 ~4 e G
nose cowl and around the engine for absorbing engine
' s- y7 f" k% |3 fnoise.
" S9 H0 D+ ^" E1 J- s6 A9 ySPAR, A principal spanwise beam in the structure of a
9 b5 n# p# ~: p4 Q( M0 \SPEED INTERVENTION, Pilot control of the speed
8 o1 J3 N1 q* }0 ^4 h y& f1 ?SPEED SCHEDULE, The planned speeds for a specific
7 \' ?8 `0 [4 l9 B, O9 o* Lphase of flight.
+ B7 E; H" r* t9 Y4 s/ a. s' O晶体电门),5 |" x% J m& d% V& w
消音衬,
3 [3 P* q" c4 c在发动机的周围及前整流罩内,用来吸收发动机噪音的0 L% H) H2 w) {* ^' h( T
部件。. ?/ ~# b8 o2 K0 \& I3 F# \4 n; L: E
梁,
1 N0 `- o9 [4 X/ C& U6 J机翼、安定面或操纵面结构中的沿翼展方向的主梁。: @8 N! A. q5 F8 j. v
速度干预,/ Y2 j& D* \% \, v [
计划速度,
( K4 G; ?& \, H, L+ j为一特定飞行阶段所定的各个速度。
( S+ l2 i: `! R! `+ @! f! Hwing, stabilizer or control surface.
4 t+ c! G- Q8 m4 k R4 nduring VNAV operation." j0 R: D9 t) p' V( p
固态电门(
* j1 C' V" m% Q( k在电流流经途中提供开关的电路。2 J' w# j% ]- m4 Y( e
在VNAV(垂直导航)操作期间,飞行员控制速度。
8 }2 Y& q; g/ t, s3 D" u英汉对照民用航空词典B OEING' s$ f. B% y. t9 o! F5 x
TECHNICAL DICTIONARY 140
4 j: y9 u" V x+ n- I# _- wSPIN BRAKE, A device in the nosewheel well for
, \4 i/ [9 r# [. y" H/ _; _stopping the wheel rotation after retraction.8 y, X& k, a# n6 D' O2 I7 M4 q6 w
SPINNER, An aerodynamic fairing attached to the fan of- j/ R5 Y% \) C' ]/ Y* i! v
a turbofan engine.
* w7 T: G3 X7 \2 KSPLICE (NO. 1), A connection of two airplane skin
$ H+ i3 g( |' [& u2 csections.
/ \( g5 F; A' ^# R/ ]/ _SPLICE (NO. 2), An electrical connection between two) @: U9 {7 D3 c0 i# O# F
wires.! l+ q) i, @9 A3 g8 i; B% `* C
前轮舱内用在起落架收起后不让前轮再转动的装置。7 w" E" M/ i0 u
旋转罩,
1 D( t6 u" E8 I固定在涡轮风扇发动机的风扇上的气动整流罩。( A/ Z3 k+ Y6 a+ l1 _' c( B
拼接,
" W- J4 o/ I! ]% b, r3 g8 a飞机蒙皮与蒙皮之间的连接。, O5 }' F2 R2 a
铰接,
6 g6 Z! ^/ f: y9 o4 s. O: H两根电线之间的电接头。# f4 B' w" K2 j/ C8 v) L
停转制动器,+ Z' Y+ n! e/ b3 d- C S
英汉对照民用航空词典B OEING
& n% J; S. E( `1 D e0 [% T$ y- f1 u5 NTECHNICAL DICTIONARY 141
2 ^. K D' J) z+ tSPOILER, A hinged moveable panel on top of the wing.
" s1 I7 E3 P7 E2 {Flight spoiler- assists ailerons for airplane roll
& G: `9 x2 [) O8 b(wing up and wing down) control0 w; g4 i4 F- G$ X. j5 H/ d. H
and for aerodynamic braking in L% I; f% q" z+ ^
Ground spoiler-for aerodynamic braking on the
* U7 c$ v; ~8 P7 dground only.
4 o& R4 S0 O, Z5 A9 \0 SPRING LOADED, A condition in which one part of a. B( J4 ]" z" Q0 _6 X C
evice is held in a particular relationship with another
+ A, a) i* U1 S' ^1 v% Ft,( i% k% z% |9 X0 H3 E& F: @5 B. m
r original position.
& e6 n1 m) i( U( G) wSQUAT, Airplane on ground condition.
4 d0 V7 f1 W4 H P- c) d B6 HQUAT SENSOR, SEE - AIR/GROUND SENSOR
& K; Y, ~$ C# ? E1 H/ bSQUAT SWITCH, SEE - AIR/GROUND SENSOR
: V( X$ k$ j' B- Y, D: G扰流板,
' V+ |, Q' @$ h5 t {4 Q% p1 y铰连在机翼表面上的可动翼板。
* Q, p- z K b飞行扰流板一功用有二。一、协助副翼来操纵飞机
* q+ u5 O9 q- {7 v的滚转。二、用以在飞行中或地面滑" ~. m2 u! k& T% ]2 M
跑时作为减速器。7 a1 |5 I9 z s& r
地面扰流板一仅在地面时作为减速器。* M8 X5 W! \0 J5 k
簧加载的, l7 `# E2 q3 S1 _
由弹簧使一个装置的两个部份保持特殊关系的一种状
, ~9 ]* o. W& W/ A- |态。该状态允许一定运动,但继而回复原位。
2 ~, z0 r6 G( P, B) X' b# f2 x+ a着陆传感器, V+ o5 B p( z" n
und Sensor# F+ E/ h% P8 d4 p2 ^. w. ?' y- b! O
flight or on the ground.. I6 X* Y h. K3 F7 I/ r
S
3 F0 y# _' r* K. Ld- z9 A# O" t" Q* X- K1 O: [, f
part by means of a spring. This allows some movemen
$ C2 S7 e1 ~$ S: Rbut returns the parts to thei3 P; k# r/ d5 ~- b# P
S9 r! a; D! C0 R1 W) b; _
弹
n2 h8 S/ g0 u+ I; Q! f! n: S着陆,1 k# s% v$ y$ N0 F5 n5 ~
飞机在地面的状态。
( O4 H n; _8 ]/ f) p b见Air/Gro
8 S/ N5 R8 f% |0 ]/ E着陆电门,' z$ j! `0 H$ T1 |* I6 J
见Air/Ground Sensor .
& i- R* n, u8 b0 J英汉对照民用航空词典B OEING
( ?: E1 h" f) V7 R5 f9 c! ?/ }TECHNICAL DICTIONARY 142. L# d8 I( L" n8 G' f
SQUAWK (MODE,CODE, FUNCTION), Activate- n" x7 S. n! l8 W
specific modes/codes/functions on the aircraft
8 q, i3 m& a6 }; }0 `7 [ansponder, e.g.,” Squawk Three/Alpha, Two one zero
x; q9 V1 _" a8 [five, Low".( s* q6 |: r0 j" y0 o0 `* i8 |
SQUIB, An electrically operated pyrotechnic device for
, Z2 l6 S; [% T! {% l' Ubreaking a disc in the fire extinguisher bottle to release
, _/ ]' [# t" u' _% g3 ]9 ~8 M/ [. athe extinguishing fluid. Also used for escape slide1 N& T+ [# b2 c. U
TABILIZER, SEE - HORIZONTAL AND VERTICAL
3 E, J1 q- u# G/ y2 P$ z2 j# zSTABILIZER
+ `, W2 {- b8 j8 S7 C' ZTABILIZER TRIM, Movement of the horizontal tail to8 }0 O" `4 }! h6 w) L
hange the attitude of the airplane about the pitch axis./ x! Z. |3 E9 O+ v8 E0 K
TAGE, A numbering system for the compressor and* r& M% ^" T* k: o& N; l
turbine of a jet engine.9 h, N3 P! @4 ^
TALL, A flight condition during which lift is destroyed
0 O4 _% D; P' Yue to slow airplane speed or attitude.( I. {3 m3 a6 J, }! U
to enter from the top and flow
2 j& U- G2 l. d# i& u. qout to the system. It prevents picking up debris off the
, ^+ |4 J" E5 S. }5 b, tbottom of the reservoir. It can also control fluid height in
% b! d; [. T) `the reservoir.+ f4 |: z, Y, ?: o3 J U, }+ ^
能),* G7 n2 Q1 v1 j
使用飞机应答机时的一种常用的指定方式/代码/功
# E* a) } P. ~: ^4 z能。' c: ^: }, j X' Y+ d
管,
3 B( U: |6 a5 O% Y8 o* B- B用以爆破灭火瓶上的圆片,以释放灭火剂的电控烟火装/ t; F* j# z7 O s
置。也用于应急滑梯放出。
, Y- L6 K( u* d& ?0 T- T定面,
( ?+ { [, V+ M见Horizontal and Vertical Stabilizer* \9 G; U4 [ e/ U
tr
0 Q9 Y3 e# ~* S# V8 ~4 l- u+ zdeployment.
7 j$ \: T0 y8 u6 c, `+ y% G2 VS
: O: V, I# c7 ]3 B- YS! H& @8 t! o- f; p2 m F
c
6 b% W. \* r" ~6 [, q8 H, kS% H8 f4 A, c( W H0 H$ U8 M' w) U2 n
S1 ~& {3 J( ~* o- q3 y
d; i* Z: T9 p, m. ?" [9 b
STAND PIPE, A pipe raised up from the bottom of a
# \! b5 B2 e. X4 j0 [reservoir that allows fluid
- ^! x# m" H+ E8 V& ^) H2 c* x发送信号(方式,代码,功
# t% G& b( W. P) V3 A5 |( k! j爆& e: j- ~/ U4 ^6 e1 I
安
9 n; @) D( X$ y2 O; W.3 y) T) S/ N# s+ W3 `" [# [, {
定面配平,4 z+ x2 ~$ y7 R$ C3 |% s5 q0 a
为改变飞机绕俯仰轴的姿态而做的水平安定面的调整。) @5 A* x' T( Q1 }. D! p) Y
级,% M/ I# O2 m5 h4 { A
用于识别喷气发动机的压气机和涡轮的各个段位的一6 j. C# I4 [' l5 b7 a0 f
种编号系统。
( M- Q* d0 Z, y5 [; H4 a y失速,2 P- f# i( V. S- D: q1 B) B* F s
飞行速度过低或姿态而引起升力失去的飞行状态。
! _* q+ U6 ]4 T; b' ?/ x回到系统中,并防止带起容器底部的碎屑。也可控制容+ D) m$ ~5 j: {. A5 u+ a
器内液面的高度。" t2 ? Y9 D7 G4 j6 H
安 {. S6 S2 U% i+ C) @. w
立式管,0 r' p* C/ R* |: h. I/ R
从容器底部立起的管道。能使液体从上流流人,然后外6 ?; O8 }0 H7 y' K9 P
流- \* m6 D1 Y2 w" s2 s
英汉对照民用航空词典B OEING" y; F" H% u; c4 a- [" l6 s
TECHNICAL DICTIONARY 1438 q( K6 h# d, f$ a
STANDARD INSTRUMENT DEPARTURE (SID), A
$ a* P2 ^$ g9 y# M: ^IFR.6 s! K3 @/ Q. s0 ^
TANDARD TERMINAL ARRIVAL ROUTE (STAR), A
( t# z; t# ^/ c2 H/ u7 I0 _3 S6 V! rublished procedure for approaching an airport IFR.
! B3 H: ]6 g; Q5 uTAR, SEE - STANDARD TERMINAL ARRIVAL2 C. \7 f3 p) `3 ~1 L$ j
OUTE" A6 s* F2 v! b# Y; |9 @% P
TART VALVE, A valve in the engine start system for
8 ~ |3 F- ~( ?: o# ^upplying air from the pneumatic manifold to the engine
1 \" A* O" G* B! O5 A1 @tarter.
! o) H% g5 R- \; o7 a9 }: ~: ^5 n6 rTATIC AIR TEMPERATURE (SAT or OAT), Ambient4 K9 C6 `" Z# E* o+ M* @2 w9 T
or outside air temperature." u5 j: s8 y( a I* r
STATIC PORT, A small hole in the fuselage for sensing6 u2 d4 [3 g; g, Z2 O- X" d
static pressure for airplane instruments.& O3 X! t7 [: A P% ?* L
STATIC PRESSURE, Pressure in the air or fluid at rest2 j, m$ L- E4 V0 B6 n
measured in pounds per square inch.9 `$ K; d8 X7 W, }8 B( Z: d
ID),0 v/ c6 P0 S! T% @
用于使用仪表飞行规则离场公布的程序。
. R* d& R- G, x4 E% ?; @4 g B标准到场航线(STAR),! ~2 ]1 F1 w8 }
用于使用仪表飞行规则到场的公布程序。
$ h0 o2 @1 k( b/ G4 R: Q标准到场航线,. J; A/ i2 K: t3 e6 I1 h
见Standard Terminal Arrival Route- @/ C) M2 ?1 H4 D' Q
published procedure for departing an airport
- m( T& V9 V& Y7 g' y/ [6 wS
. `# @- C' O A. G# A2 j! c- ^3 Sp- k& T! A6 I. p' |( c
S
4 B8 r( @# p6 G+ }) C( I, FR
: {. v4 J V; m, b" ^' w- _1 u$ iS# y$ s$ _& b" b0 m
s
5 L# N& I% |2 H( as
4 F! _% j6 ~# r# hS
5 `( F2 w! V! W3 m! n标准仪表离场(S
/ ^1 ^+ [2 B5 s+ \& G.2 p" z M# K; E: f
起动活门,
! N9 p( r F$ b3 {7 i发动机起动系统中,用以从气源总管向发动机起动器供
" `: ~( v) Q% R" o' W# t w3 x的活门。$ P5 O$ U5 H4 F! H) g% `! f) c. x
温(SAT or OAT),
1 z# p+ N: G9 `; t a, ` V1 X环境空气或外界空气的温度。
9 A% x/ O7 F7 q3 D9 C0 v压口,
/ L4 a$ W9 S$ X5 z9 }位于机身外表,用来为飞机仪表感应静压的小孔。
2 L, e5 _# l8 \: C# r7 T1 Z静压,& E) m" _( a- U- p
静止状态的空气或液体的压力。用磅/平方英寸来度量。6 |. U$ A- _! I$ b
气9 f" _# X0 V$ S& R# k( T
静" V4 e8 f. V+ a U. o
静
p! s/ g' W3 W; i/ X, d. ]英汉对照民用航空词典B OEING
3 v* C* G; _/ WTECHNICAL DICTIONARY 144 m/ z4 k; P# _/ c% H2 @
STATION, A vertical reference plane along the fuselage
1 `0 V* `4 r5 f, L4 A" bfor measurements along the fuselage.$ D: F; ^# L, V9 n" B& o; S4 C
TATOR, The stationary section of the compressor
' A* k3 U' Y& C: A1 ^etween the compressor stages in the jet engine.
% {5 B: m* ]' K3 PTEERING ACTUATOR, A hydraulic actuator on the
" y' j# O0 U& j; ]% n' r$ h8 blanding gear shock strut for steering (moving) the
9 h0 J- K: k. N" C, o! x' mnosewheel left or right.* X' X& C" _; y0 ?0 k$ b$ w5 W
TEERING TILLER, A hand-operated lever in the9 _$ m! H" `" j# M3 _8 k
osewheel left or/ R8 `. i# r& K @
ght.
9 m4 O* H+ u- |, n3 JTICK NUDGER, A device to push the control column. E0 Z B+ p& g7 N
rward just before a stall occurs.( A3 ~) U. } |$ r8 ?7 N
站位,
- x3 w: `+ M: {$ e! O4 I用以沿机身方向度量的垂直基准平面。4 n8 g- {6 _$ w) Q3 V4 Z0 G
定子,
^( l6 S8 j2 N+ Q) u+ U喷气发动机压气机各级之间的不转动的部份。
% f# p1 r0 e" P弯作动筒,
9 C: c+ q' e" {" ~) K. D减震支柱上,用以使前轮左右转弯的液压7 r0 Q% |1 c8 ^: h' N( @$ h! [' @, {& w
作动简。% e; B% C; G0 t! X
轮转弯手柄,
3 X& x; R0 G3 k# O6 R% S7 a' @内用来使前轮左右转弯的手柄。; u: \7 p7 A0 ? R
动推杆器,
, M( m; D% f0 _; w. c" Y1 Z- }2 o7 ~在失速前能将驾驶杆向前推的装置。
9 t; U" S% r/ |4 }- fS
' `9 ]2 K6 G7 f, ^5 j7 Y: ab
3 x! f. l8 w1 _. xS3 ?3 `- f: f9 o3 o1 p
S2 `% p: d+ X. M8 v0 p& ?
control cabin for steering (moving) the n
) U* N U, [2 z, P+ `0 P; rri3 U3 `. f& B4 |, s4 |
S* B2 G6 q. Y) N8 f) W* ^
fo
1 @6 e( L8 q# h x& _$ t0 Y转( |* x, J1 v0 ?' h9 P/ i
一个在起落架+ L/ r( u' R; d& N' C. c" h
前
- S& i, ?0 {7 n: p; |: `0 b8 _) T3 s驾驶舱$ q" K/ B: d. z9 e; D* b# B! e
自
) V# B4 h- ?4 n3 T* T$ q+ e英汉对照民用航空词典B OEING
1 D) K# m1 p) E* _! Z$ D" FTECHNICAL DICTIONARY 145& x$ I/ x( [& |8 }( o
STICK SHAKER, An electric motor operated devic9 Y$ \ V) Z# D* Q
the control column which shakes the column be# K) K' q( F9 Z! B; j
stall occurs./ q3 K% N+ Q. s
e on0 i* J3 R9 ?9 w) P. h+ u
fore the
9 v2 }' w/ ~1 ?) Z- Y4 s) zTOPWAY, An extension beyond the end of the runway
* ^. E7 ~4 B$ o" V$ p' k; Which may be used to decelerate the airplane in case of
# d+ W9 \5 I6 O% `: ?n aborted takeoff. It cannot be less than runway width7 K* R! o" M, `$ h- X" x' O
and must be strong enough to support the airplane- B) t& @: T7 v# Y" w2 n
置。
; V2 j E& u. U* V% a# f速安全道,% c3 l" \8 z1 z: j" Q9 D
跑道两端,可用作在中断起飞时飞机减速的延伸地带。3 q" G4 ~1 f* [: \# a! B; @
它的宽度不能窄于跑道,硬度也必须能够支持飞机以免结: r5 n! z7 f! U- ^" Z
S* U2 G- R! R1 H% o0 Q. T: }% u
w
+ y" `5 b8 [0 h/ x- w1 xa- I( ~- \% Z0 M2 j+ V/ g
without structural damage.+ C7 k" D: v6 H/ }
STRAIN, Structural material deformed slightly due to the
4 `; X1 S4 a0 H$ G5 K: X$ paction and forces of stress.+ y4 H2 h w& @2 J& v# K
振杆器,
* ]3 o, r& m8 `! z驾驶杆上,在飞机失速前使驾驶杆振动的由电马达操) R/ R* { D5 [# n) U3 D1 g! r9 z5 S2 k
作的装
# I0 [" Y$ S6 _& p; d4 a ^减
1 H7 {* w) H- p+ G构损坏。
7 P" q# v, f/ A8 h# C# P8 W% h应变,) W* p) r0 R8 b# X( I6 Z! M
因应力作用和受力而轻微变形的结构材料。# e5 _, d5 u( A! }/ ~& ^5 g# K
英汉对照民用航空词典B OEING& W; E* k1 K; ?* L2 c+ \, f9 q
TECHNICAL DICTIONARY 1464 t/ I, \4 N$ F2 E4 @& ?
STRINGER, Structural components in the fuselage or& q. Y6 i; e: y7 I5 ^
wing for transmitting skin loads to frames or wing ribs.* l2 d& S1 D( K7 g# h
STROBE LIGHT, A high intensity flashing light on the+ P7 }2 I X6 H
wing tips and empennage.
) l6 i; f. B8 P' L6 VSTRUCTURAL MEMBER, The part of an aircraft
: a P* D7 v) K* s4 R0 S+ V" Wstructure that has been designed and constructed to' G; a2 } J0 m$ v; V
carry and accept loads and stress.* a+ P6 t' g* ~7 s$ Z# r
STRUT, Mechanical components of the landing gear for$ V/ x q) x$ e/ W! j
keeping the gear in the extended position.$ y2 S$ T" w9 W W7 D
机身或机翼中,用以将蒙皮载荷传至到隔框或翼肋的结; q) G2 E4 V' q2 N) s
构件。7 m/ A- q y/ I8 [3 T; T; A( {7 Z
频闪灯光,
1 [- V- V, p- B0 w# j位于翼梢和机尾的高强度的闪光灯。2 e% O! Z2 i" u, }3 T# M+ k7 z5 i; @. x
件,
8 u# e2 W' d, ~- s( Z飞机结构的一部份。为运送和承受负载及应力而设计建
# K3 T& P2 v5 t! d9 p成。; m9 d5 C2 k8 E* w6 z6 X
支柱,
# v$ m y5 K. H& H+ W起落架上用以使起落架保持在伸出位置的机械式部件。( f D1 |$ @* w! o: u8 ]# a3 E( B
长桁,4 E6 n/ ?0 V: f8 L
构
7 X! J, O! w8 {! ^" Y& a9 ^8 Q; B0 N造. o, {+ i- M. A. I6 R7 ?
英汉对照民用航空词典B OEING
3 [: ?+ |7 h+ `$ B/ }3 y1 _TECHNICAL DICTIONARY 147# |- e* P* M) [/ o n
SUMMATION UNIT, An electronic component for o/ X4 f1 I1 d! a- c
adding fuel quantities in all tanks sending a signal to the( _( F. _' ^* W8 ~# ~: h. g
tal fuel quantity display.* ]" [/ O* q! L( T
UMP, A lowest point in the engine oil system or fuel
5 i6 D# f8 B3 {9 dnk.0 A7 X$ [& p, E
UPPLEMENTAL DATA, Additional data stored in the8 B+ Q& j7 S1 a9 e1 G' D
MC memory, supplementing the loaded navigation
, _, l0 A+ [: Y; D- D/ S, {9 I+ Wata base.$ Z% d0 o* o0 N
n' Y N6 o1 b8 q" ~5 H
eviating from normal modes.
% U9 o$ B! ~0 f2 r' l: t6 }SURGE, A sudden change in the airflow through the
8 B9 V+ r5 J8 G4 X( E! y% Othe compressor not being able$ b% e8 F% G1 x: Q" o- ]+ u
compress the airflow.( M1 g" t& X9 E8 m
SWAGE, To squeeze together two or more items to6 g% L$ g, P* G! h
form a permanent unit. Example: a lead or steel piece/ r1 x8 ~' y( A
on a cable which forms a stop or camlike unit. Also to. i2 k0 G( E* ]( O$ T, k
reduce the diameter of tubing.2 x3 n$ N% E1 M6 d, R6 l9 A
SWITCH, A device which changes the condition of an8 C" k0 Q L! m" ]8 p$ M& E6 {4 B
electrical system from on/off or open/close./ V `- a( o ?( k; i2 }/ ~1 P
燃油总和器,
" @; U f5 e* ?. g将所有燃油箱内的燃油量相加,并将总油量用信号传至
# Y; R% |% H/ ~& Z8 O" {/ z量显示器的电子部件。! ?' T. v" `& w
集油槽,
0 {, h! E7 z0 i6 L1 H. R7 g a+ }发动机滑油系统内,或燃油箱内的最低点。
' W: {0 u3 A j4 g5 s, T增补数据,( y8 X% x+ a q9 e/ |8 G; ^
飞行管理计算机存储器中的附加数据。用于补充导航数
& [5 z+ n; f$ s据库。
( i9 r2 Q5 D( O: l% R,
1 ?5 ]( {9 y3 I$ E2 Q w$ @5 X附加的数字飞行控制系统方式,当偏离正常方式时使4 ?! P9 w. Y: d5 D9 C) n, A
。
8 [% q- c3 x8 t( Q过发动机的压气机的气流的突然改变,而导致& l. R- {5 [- [5 [
气机不能压缩空气的现象。
7 r& R7 ~( L- [0 K陷型模,$ p( H. T( ^' C, @- y6 k; H
挤压两件或两件以上的物体来制造一件永久性的元件。
1 l6 d3 t6 U0 W如:一块铅或钢在钢索上形成一个止动器或凸轮之类的
- w2 G# \3 z4 @* H8 U件。也可作减小管道的直径之用。/ [; H- U$ A1 q. A* A# ?9 M
开关;
3 g3 @; ?3 ^% q) I改变电气系统通/断或开/关的装置。
1 G& C# ` F5 {. b1 @! P2 ~to
4 O$ V [$ O' a+ J2 K4 T8 q& Y3 ?. Y c7 OS' l" E! I! z+ D' m. ]6 B
ta7 [( y# n& d6 q& G) J
S
2 L' a8 U* }" A0 ~: e. ^F) q) T% m9 P# b. s4 @" Q
d
4 U6 o9 [+ s/ v. ]% ZSUPPLEMENTARY MODES, Additional digital flight
2 `2 L: p5 T$ E w# N; P: Pcontrol system modes that are available, used whe
6 k. M( u5 v3 Nd
* T5 C$ ?* z$ |% y1 U4 f3 jcompressor resulting in# }: j% x' I0 D
to
5 o9 o6 C, J. k' K2 l$ P: d) V油
7 h; `- U* v% T$ m# U辅助方式
( H5 J& l, Z$ E# s2 r用8 o: `: n& b! [; x
喘振, j* D# E5 Z0 h a" }$ Q9 Q: {
由于通
, F0 m/ d2 e* q, b4 @# X压
+ k% s) r0 a) B ~ f8 Y% L例
8 u5 F5 {/ i3 x元, s4 |; D; ~ C3 N6 \( F- z: X3 k
英汉对照民用航空词典B OEING
9 W! v0 p, S; w8 oTECHNICAL DICTIONARY 148
1 C# T9 _+ r' c9 ISWIVEL, A device for rotation of components.. A2 j9 j2 o4 J; m, g" a3 J
SWIVEL COUPLING, A junction in hydraulic7 q' `# O" S4 k1 M
bes for allowing component movement.1 W" k: ?; H5 M, |- c
YMBOL, A graphic view of an aircraft component in a
2 K) v! r' p, G2 |# V1 p# u! aery simplified format. Used on drawings to represent
* @% r' \, ^* z6 k9 g$ w de entire component.
5 [( S3 V/ }3 N! fSYMBOL GENERATOR, Generates the video signals
8 ~. W$ f, q' E. `) R" Y7 Mthat are displayed on the EADI and the EHSI.
* c2 ~* e( T8 g, ?3 C% \( NSYNCHRONIZER, A device or circuit to make the units
/ x, r( V) F- l0 xperate in unison.
& o! n' a e5 Q( TSYNCHRONOUS, Refers to two or more things which$ X) {6 |: D( G7 H& K' |
happen in a system at the same time.. ]' E# X T! o" a3 a- p/ @
用以使部件旋转的装置。1 v! O/ R! V8 j( F ?7 p Q, f
转动接头,* L) g4 v! }, ~! D
液压管线上,使相邻的液压管能够动的接头。* j0 M3 o7 g# u- h
符号,0 d5 [; E6 l( J6 f
飞机部件的简单示意图。用于绘图以代表部件的整个结% P, a: s8 |6 _) `, `( X
构。
) z2 `3 y: d3 w+ a& N3 f符号发生器,; l' o M, R; _6 r" k* x
为姿态指引仪和航道罗盘产生图象信号的装置。
+ `) {' S- g4 s. P1 \% d& D同步器,$ G, |" h6 A% o( X3 p
使元件操作协调一致的装置或电路。" A. Z6 u, t) z, t8 r
两个以上的东西同时在一个系统中发生。
3 a! N! a2 W6 U$ j5 ^tu6 z. |2 q/ d7 W9 k3 C! R
S# u9 n3 m' {& F/ L0 `
v# q4 F# q# l0 B1 |- i" O+ V: G% Z
th3 D, T; M+ r+ `4 f
o
9 A+ D0 o) U& ?* k转座,
% j$ t. a0 t {2 [同步,
( a& W( I* z* e0 u. O7 d指两个或! T3 G1 T0 G% T7 J1 a% z. N
英汉对照民用航空词典B OEING
1 e5 L: I4 E+ l$ d+ h6 ?& D8 w: rTECHNICAL DICTIONARY 149
8 d5 u! {; E- M6 O0 zT/ M A: p9 Y' b; g' R3 _
AB, A small, hinged, moveable part on the trailing
$ j* F$ @2 _/ bdge of a control surface (aileron, elevator, rudder).
% W1 g+ a' q1 T7 `9 j5 s2 QBalance or control tab - moves in an opposite5 s. V7 s8 ?" S/ o3 v6 @. S
direction to the control surface for assisting
* `# R4 F9 U" L4 min movement of the control surface.& ^8 |' D1 N2 {6 Z" m7 U
Trim tab - provides controlled deflection of ailerons2 t9 g [# k! u, N& y
or rudder to compensate for imbalance in+ g \" j- q& l! L1 j
thrust or fuel quantity.
3 o( I" c- m3 J/ J0 AStabilizer trim - controlled deflection of the horizontal% O( R* N$ v3 v" M5 h/ ~
cy
* h4 t% ]* T+ Pproportional to the speed of rotation.
$ B- C% x% K, D9 O& }TAI, SEE -THERMAL ANTI-ICING
2 u4 y Q0 c/ [' cTAIL PIPE, Duct at the back of the engine exhaust.
, F) e6 J* K0 g" H+ m# LTAIL WIND, The wind component relative to the
% U0 V- x% ~3 @/ V2 d0 ?" y8 sairplane direction and coming from behind the airplane.
9 g c6 p: I9 o3 F/ v! J# ^$ b5 D: N调整片,
% U3 f8 C$ ~' g$ t8 L铰接在操纵面(副翼、升降舵、方向舵)后缘的可动小
$ T+ \/ ]7 d4 t( g# ^/ [: I5 {' |; X部件。9 M+ m+ t" z9 T9 M1 w' j( I L
平衡或操纵调整片—与操纵面运动方向相反,用以帮+ S. @7 ?9 ~3 t. ], V
助操纵面运动。
2 b, q6 n# q2 z" U配平调整片—使副翼或方向舵作控制之下的偏转,以0 L/ @. Q- q: C5 f# T: x+ s
补偿推力,或燃油量的不平衡。
( _+ q/ h( C; o5 d! O8 F安定面配平—使水平安定面作控制之下的偏转,以减
% P' C# |& T8 t. g少操纵力。/ m y* {- }) v! C, [3 \
机,6 T; O1 w6 Y+ L8 }" ~# ]
提供频率与转速成比例的电流的小发电机。
# T6 H7 q7 w1 O% l热防冰,$ C( u# B8 D1 L& o. V" J3 D1 U. e
见Thermal Anti-Icing
& I8 \% V& \8 B( v! j% [T
8 C5 @: E& t6 J" s4 De
: T( ^9 Y5 J* O! pstabilizer to reduce control force.1 ?9 I6 ~' Q; M9 @0 q4 \. F
TACHOMETER GENERATOR, A small electric( H: J! A0 u) f4 \
generator for supplying current at a frequen* a0 F) `& D2 l, B# b( J* W- M5 H
测速发电6 r: C) F5 \5 i" z. X
.
( @' C% X+ b1 u4 T尾管,0 f" X2 d$ c W
发动机排气管后部,用以排出发动机的废气的管道。
. U: W7 M( d( A e% P& a/ R顺风,
+ s) ]1 I0 ?7 g; `0 Q飞机后方的来风在飞行方向上的分量。3 w1 @; L) z# m( p; R. l8 z( M
英汉对照民用航空词典B OEING7 w) b. \6 F; A7 \/ n% b3 \( O1 ^
TECHNICAL DICTIONARY 150" g! o8 d/ f, g: d J, L
TAKEOFF ANALYSIS, Analysis that evaluates the
- j8 M! `& c" @6 d$ i8 l" pairplane takeoff performance capability for a variety of
- u, `$ |1 v/ Z* zenvironmental factors at a given runway and airport.
8 N' |* R( u/ K& M' j' cET PARAMETER, A specific goal such as( q+ h8 j# N( F' S8 t# D
irspeed, thrust, engine speed, altitude, temperature, or
3 ]* e5 _& ]- } t: w: C4 _te of climb which is to be achieved./ t$ y6 u9 ?6 P0 H7 X$ s
ASK TICKET, A computer label used for tracking the# o$ f2 f" G4 ?, A/ I
ompletion of a task.# ?1 [0 [7 _7 [" b1 A8 L
RATURE6 M4 X& t- [( |) p/ \3 [5 |. s
AXI FUEL, Fuel burned from the time the engines are
$ I- o( Q% I, K& E( r) {r.
# [' B4 s' o4 `" p. YCAS, SEE -TRAFFIC ALERT AND COLLISION
0 s- x5 V: h$ {8 O- T; R6 x) wVOIDANCE SYSTEM
) N5 D7 }) H, C% G欲达到的特定目标,如空速、推力、发动机转速、高度、; @: V' G- h/ {8 ?! h; ]
度或爬升率等。2 _( @- W. H7 B0 J( p s
工作记录单,$ p! Y. G5 Q" n; A8 x
用于追踪工作完成情况的电脑记录单。
% k* J1 F P* H' [! h7 A3 D1 ?6 c' A- m全温,. {. b7 _6 W5 _1 G# o. A
见Total Air Temperature
- k" y0 ]8 D* gTARG
: [ n2 r! e, N8 Da7 W9 I; K( h3 K. d4 E
ra
2 |) ]- k/ R1 ^5 O+ x& V1 y& X, IT, x# X0 X. b* P
c1 Z+ g8 W7 r4 {, S. V/ O3 P
TAT, SEE - TOTAL AIR TEMPE7 M) i! D- ^% a% ?( t" ~
TAXI, Movement of airplane on the ground using/ b9 o) t2 J% ~' d& A% ]3 m
airplane engine power.( n6 S3 l E9 e9 ^! j
T4 A& ~& Q# l4 {
started until the airplane begins the takeoff maneuve1 Y" Z& s) H H! L
T
) j" J8 ^+ e) Z" `/ e- BA
+ d* B7 v& C5 l2 S" ~; r7 W起飞分析,7 E1 u6 _' k8 M9 Z3 D
对飞机在一个给定的机场和跑道,在各种环境状况下的' Y% N$ |! Z2 D3 t
起飞性能能力的评估。
/ Q! ^; g! p, y R. j( Y目标参数,
1 Q; h# g4 d3 e- Y温
, \6 \1 {" ?: |1 D5 O. ]+ x·) t9 E! c% h: b1 ~7 ~5 L
滑行,
6 E/ K* m+ {1 ?! G行燃油,
* [9 q. f) p. U5 B |! M6 Z0 Y8 N; x起动,到飞机开始作起飞动作之间,所消耗的; Z! F; f# x) H A" o
中交通警告与防撞系统,* b/ p. T* C3 `; C* k- }) _
见Traffic Alert and Collision Avoidance System4 s8 L5 ~5 b9 [4 m7 Y
飞机凭借发动机推力在地面的运动。
6 U' K7 Q4 ]7 {* u2 N滑2 _6 a- d; Q. Y( C" s
从发动机
4 X8 k% d* g) E1 i% G) r0 c燃油。
- ?7 p! ~- V: g; @0 M7 ^, A* D0 f# J空! ~; j9 s& p% N; u& p3 S
.
+ J" q7 o3 f9 |, \英汉对照民用航空词典B OEING* `3 D( B) v# ]3 L! |
TECHNICAL DICTIONARY 1519 J! n& R% }8 @% V7 B4 g
TCC, SEE - TURBINE CASE COOLING# u# } X% T* ~7 q% T
EE, A pipe or tube connector manufactured in the, _- o+ O2 E! Q4 P2 H& v1 Y& y
EFLON, A synthetic material for hydraulic and
8 V9 n2 W# w* u# B$ d8 ^neumatic seals.
- j0 R8 k* ]/ A( C. M3 MEMPERATURE INDICATION STRIP, Temperature
9 I4 V" K' y+ U$ l5 R- Aensitive tape which changes color at high temperature4 y2 P" B1 ?( [( X: t* p6 |
r indicating component exposure to high
7 }% }! E7 p3 f( ~0 N; w+ }4 U. qTEMPERATURE INVERSION, An atmospheric% G3 {2 l4 Y8 m
condition which causes the outside temperature to+ C9 c0 j0 z- x! ?: f9 N* R$ I% ~5 R
increase as the airplane altitude increases." F9 y$ L- u; ~0 H/ G* a, x
TENSIOMETER, An instrument used to measure the
9 O) e! M t4 U' j# `( p% vtension applied to aircraft control cables.
% E/ q" E' F9 z冷却,
+ O* @9 Z2 i& W( xT
0 u4 d8 z( O: V( {8 ?shape of a T9 o) R$ C/ L$ v( `5 ^+ l+ v
T
9 m9 @! A; f3 m( u% Rp
( ]# J+ O* G) t% t& Y# L2 r$ gT
8 I5 E. M; Z& D9 R' Ys
- A5 U f( Y/ _fo" W. c: V D/ V3 s# _! n
temperatures.
, {& y; z7 Q, x4 d+ m7 [8 a7 s涡轮机匣
; U6 A% C! \9 x" \见Turbine Case Cooling.
$ E# ?- }" z- F字接头,/ c; r; z; @/ m- @
的管道连接器。% ]. z! x$ e' l0 U
氟隆,
9 \8 n) r1 t: A/ \) p用于制造液压和气源封严的一种人工合成材料。) X* F3 y8 L0 s0 m
度指示带,
% p5 b N3 U) i遇高温变色,以指示部件周围高温的热敏带。
3 O/ H) Z8 C7 e逆温,
" V5 ]6 L( I. r, j一种大气状态,引起外界温度随飞机高度增加而增加。
- M0 P& p c* I' \% b( \9 @4 B) E张力计;; T. N; G3 _8 l$ a
用于测量飞机操纵钢索上受到的张力的一种仪表。& c/ M, A, f1 F+ w
T7 ~" a7 B& a3 K# t, d
制成T字形2 d7 O s6 N% R: `/ X" U2 I
泰8 U: ]6 V" l; ~
温
4 O+ x2 f+ b$ D3 t1 ~8 Q3 ]8 z8 F英汉对照民用航空词典B OEING, P$ i/ g& T( t' E
TECHNICAL DICTIONARY 152
8 W3 t3 s/ v$ z4 {THERM9 M& B: l2 a! ~5 f
formatio2 d# x# ], S8 V
using ho+ B& M6 S5 _: [, r& K
AL ANTI-ICING, A method of preventing ice
- W( a( {- H3 s0 K6 ]n on the nose cowl and wing leading edges by, T9 J1 }) g! m9 ~6 G
t air.
# S# D2 i6 l A4 D8 k2 sTHERMAL t
1 o3 ?* i# I( N* X* R% bin a tube fo en tube& j, h% W! G, y$ J
is pressurized with oxygen.6 u' X( F" D4 w; Z0 \. W
HERMAL RELIEF VALVE, A valve which opens to
- V- c: D9 ?8 I% I# o/ lture.
' \ S- d$ C* sHERMAL SWITCH, SEE -THERMOSTATIC SWITCH/ o0 @4 a0 h: K( A/ b& t. U G
e
5 I0 k7 z- ?. M% w8 a& N( X) isistance changes with a change in temperature.) o8 h+ u+ T' C( B% S
防冰,$ Z' o% ^! j8 S$ H! g1 T1 i
用热空气防止发动机前整流罩和机翼前缘结冰的方法。
U* y) ]3 ?& V在管子里,使管子受氧气充压时温度不致于上升的一% t, e. ?% ]5 s
个刷子形导线元件。
7 R. l" b4 v9 B+ T" S控释压活门,
8 W0 L% j8 }$ H$ s3 C过高而打开,以减低流体压力的活门。
8 m+ S+ l% w2 S" U4 y电门," D" h7 c: e( B: |9 o
见Thermostatic Switch, [# C! L" P) y! x6 U2 [4 a
COMPENSATOR, A brush-like wire elemen
3 ?* A5 [% k4 O& \r preventing temperature increase wh% w0 s. n2 b3 A8 ?; _
T
6 U6 u, j3 f( J) |decrease fluid pressure due to high fluid tempera
' ]' K! `8 v& {, R/ y- ZT
* f8 d) O, t8 [# y0 ^ i/ A, h& LTHERMISTOR, A temperature sensitive resistor whos/ O; J" `- `% G5 z' L, F, v: p
re8 S7 f! r' v- q
热
' ^- g0 G6 ^1 w$ H热补偿器,
. c% j9 l! H j3 z- \% ~9 Q |- [, ~4 t装
* K' D+ q# g- q热7 X# e p) q: ^8 F
因为流体温度 @- u- C' H; Y3 |3 E" l5 D
热
! y; J5 L7 o/ [. M- m7 k, W# U.: j9 Q- x5 ^9 p/ ~6 {/ l' t
,热敏电阻+ N2 Q. a ]% ?$ @7 m
一种电阻值随温度的变化而变化的对温度敏感的电阻。. y5 y2 n" f" {" @3 _! K
英汉对照民用航空词典B OEING
. `( s4 Q- ~9 C+ ?) F" d+ {' wTECHNICAL DICTIONARY 153
, }: K* R5 l" n& t: X" Q4 qTHERMOCOUPLE, Two different metal wires joined at9 p0 t) m# K9 I2 }, v4 Q
urrent is produced proportional to the temperature
9 N! n% n* b o+ ~9 j8 Adifference.. |7 i5 @' D5 f
THERMOSTAT, A component set to operate at a. N8 T9 ?& S& L: w' H
efinite temperature for controlling electric circuits and$ v7 V/ l8 a8 K K: @
alves.
7 Z; @, p$ ?7 Y) E6 Rmperature sensitive switch which opens at a preset- D+ Z/ w9 T ~* O1 y# N0 z" z0 r
mperature.
8 ]% T1 _3 u nTHR HOLD, SEE -THROTTLE HOLD7 l1 z5 r8 g3 y
即产生与温差成比例的电流。
) R7 J4 r% H7 j' ^用来在一定温度下操作,以控制电路和活门的部件。) u5 W( G6 m Y' R b3 V9 [" F/ ^3 L
恒温电门,! P0 l. z' j1 A3 }7 _& j
一个热控的、在预定温度断开的热敏电门。
2 q- i# a1 F/ j1 d见Throttle Hold) K# f. U. w! Y3 f1 h
both ends for temperature measurement. When both- ~7 \% P5 n% E
junctions are at different temperatures, an electric* r' N) K* ^6 @! N, ^
c
5 V; y# f$ e" N+ {# P- t% jd* }' h0 `- N5 S2 K3 Y" ?; ^. _( D
v- k. ~( \4 q6 |, r- g, G* x$ B2 E
THERMOSTATIC SWITCH, A heat controlled,
4 F# d- M5 `7 `te+ T* |+ r' X* q+ B, O
te; A: _" E' P" ^ d* S
热电偶,
) U% d, f+ C/ S1 q用来量取温度,两端相连的两根不同金属导线。当两端
4 F; @: m) N- W; T T6 d# g. V& i之间有温差时,金属丝内
- @$ C' ^% G! W3 x( K2 B恒温器,
! ~, y- J% p: E0 y8 B油门保持,
, m j3 k( O c! }* i2 |: C7 _5 W# z1 \.0 B. G3 u0 J7 _; Z2 F1 o
英汉对照民用航空词典B OEING
( G: Q' i/ v* e0 ~1 WTECHNICAL DICTIONARY 1542 t7 x; V& g! R( k" ]4 } G' R; s
THRESHOLD (NO. 1), The bottom part of an opening in$ h# Z4 J" ^2 i( a9 m
a fuselage doorway.
# G$ P3 \. Y" R" \1 _/ ~2 r. 2), The approach end of the runway.
" U( }- V" j- z: @ t( [THROTTLE LEVER ANGLE, Angle of throttle lever
# w' Q V+ z( Y' }; ~6 s( pdisplacement./ l i! B- |( [: N' M; s
HROTTLE SPLIT, An engine control condition in which
" x C) z( w5 A( Jthe throttle lever angle is different between throttle( W! @, v$ V& P5 W& R$ r
levers but the engine thrusts are the same.
& Q z+ L; P, _HROTTLE VALVE, A valve in the fuel control unit for
% Q7 ?& R+ g# k9 c: M& Hcheduling fuel flow to the engine., _) A$ m0 q4 D8 l! n5 C
机场跑道到场的一端。
* D/ p! ^8 X) g; n9 o2 p0 X. P油门杆角度,
K O: _0 m& Y. V Q! c油门杆手柄位移的角度。
7 i( a( E4 M! I r+ T( r$ {油门分叉,
8 { W, L9 Q1 s! p: t1 G1 A一种发动机控制状态。在这种状态下,油门杆之间的油6 \1 e7 \/ W" F7 L
门杆角度不同,但发动机推力相同。8 t. R4 {# L, F% v& b
流活门,
, A5 ~9 N9 O0 f( J0 b4 s# e& D燃油控制组件中,用以排定燃油流量的活门。( T2 M( o9 q$ v; y
THRESHOLD (NO) e. o$ Q3 ]# w" w
THROTTLE HOLD, A mode of the autothrottle where* i9 d2 c% B1 t; E' i
the thrust levers remain where placed.
2 Y9 z6 ^. p z/ d- h( u% dT2 L, V- l: g0 l& v# J* ^
T
/ R% z7 Y) T$ G6 Rs$ s% W) u! k, l8 O0 l' @' ]
门槛,8 l4 m; p# j0 b( W
机身舱门开口的底部。" @, x# o( Z* o# s1 n% F
跑道头,
% V9 t7 r7 \& Z7 `) Q油门保持,# w& x; k0 Y& r! |0 k+ K
自动油门的推力手柄不改变位置的方式。4 }$ d* ?1 \, p- r3 [5 Y
节
$ ~1 q! M% P" j. r- }# I+ R$ H, M7 _英汉对照民用航空词典B OEING
: ~* T/ z( [: p( f* G: e4 q* b: d7 vTECHNICAL DICTIONARY 155
2 w+ v1 z5 D1 ~2 v a* GTHRUST, The driving force produced by a jet engine.
' D3 V) H! x7 j) S" Z4 S1 tHRUST LIMIT, Maximum allowable thrust for a specific' l4 Y& t! z1 N0 b
et of conditions.2 d9 w/ z! [/ n6 y8 z( I. Y" I) D
HRUST MODE ANNUNCIATOR, A display unit or part
9 R, |1 i+ _ E- {0 ] k% X5 P( Af a display that shows the engine thrust mode." I. A8 e6 g! F5 ~7 M& C
HRUST REVERSER, A mechanical device located in: Q: f2 P' n: z; O4 [. L z5 t; a: G9 Q
e fan or exhaust section of the engine for eliminating
9 l9 g* x# E" ?: @$ Lrward thrust by deflecting fan air or exhaust gasses in3 ]9 n# P( H+ ]& l
e forward direction can be used for stopping during
1 i9 t, ?! ]. L v( V2 planding and during an RTO.. J: V4 f6 |1 }+ M- _( a; x- R( }
推力,
- G g3 p6 l) @1 G力极限,3 b k; Z. s* X m) I' b/ d
在一组特定的状况下,发动机的最大允许推力。; n* z1 ~; M$ z3 Y% M# d! Y
推力方式信号牌,! G+ H9 x5 E7 J$ C
显示发动机推力方式的显示器或显示器的一部份。
2 R! w% ^$ ~7 m3 \反推装置,8 w* t3 Z$ n2 h9 j" v# N3 P
位于发动机的风扇段或排气段的机械装置。该装置通过
( c" {: ?( P. U* a0 J1 W5 t使风扇空气或排出之废气冲向前方,以消除发动机向前的" K& p, d+ w& A3 s' l D" D- `
推力,并减短飞机在着陆或中断起飞时的制动距离。' ^" D! [, n% I/ n
T4 J5 W/ V3 V. l* Y5 P$ C
s
- F7 }( ?- }: {: r% ST
/ r# a. S) m C1 Ho. I% i* y0 _9 @$ t W) h* n
T: p3 ~' o! \9 z
th6 y5 w3 `* s* M/ }
fo. R2 b* Y, g! [. h0 y# u7 L
th
7 W/ D; u% F; C1 _' i( a喷气发动机的驱动力。
. Y f4 n2 ?7 W- m$ H推) G. V2 _( h' w6 f
英汉对照民用航空词典B OEING* @1 i, R7 b" ~* `8 X7 [. ?
TECHNICAL DICTIONARY 1564 i K7 F1 @ [, }0 S
THRUST REVERSER COWL, A cover around the thrust
X# _# X: r3 sIME DELAY, An electrical circuit for starting/stopping1 T0 o* i5 j$ ~9 ^; d8 ^0 ]! b' Y
e flow of electric current to an operating component K1 _8 x. Z7 d" G
r a period of time/after a period of time.# ?; x: C* A7 ^3 C6 L) c. f# F0 h5 L- a) d
IRE SPEED LIMIT WEIGHT, The maximum weight; ]6 n4 L/ ]/ x. g
permitted at takeoff that results in a liftoff speed equal to' E8 Q @ d' C5 V& e8 J7 E3 F# b0 y
e rated tire speed.9 q W1 k9 p4 s( d1 p" {
OLERANCE, The part of a specific measurement that
, k( f: i4 s6 v( ?" kallowed to vary in dimension. Usually given in a plus/ O- h) b5 A3 ~* a- z; X2 I) |
) or minus (-) format.
$ S& l& z6 g+ r0 g# k6 O* _CLIMB, The point at which the airplane( F0 D" t) q8 {% @0 ?- V5 l
reaches the cruise altitude.9 d6 M# [; X# z: H6 m9 C# t
ts the cruise altitude and begins to* K. C4 f j- q
descend.' U" `+ Q& f O2 c+ j7 d2 c
for transmitting
' U- S: w! {9 _9 T/ w3 e' _' @twisting motion to the control surfaces.
' M; ^4 {+ x' U1 A) _! S0 },: ~ H7 f4 M4 F; f( B' J) _/ T
的6 c- g! p v2 V/ X9 Q0 k- s3 S
部件以进行维护。8 V7 H; ^* f+ v( ]1 W
延时电路,* ?1 e" k1 K+ T9 \6 I
用以起动/阻止电流在某一段时间内后进人工作部件
+ v) r4 [( R4 F* l, H; P4 K2 ~/ |2 y的电路。
( m. a( q' Z& R i2 N6 O( F- \轮胎速度限重,
' s9 @# O( G; u" {; g飞机起飞时,使离地速度和额定的轮胎速度相同的允许( E8 V8 {1 O' U' `0 Q$ m! b& {5 b
最大重量。
9 k" q. i. o7 y; E* ?) h, N0 A公差,, y( ]0 ~# h+ M) m- G& p
特定量度容许有偏差的部份。通常以(+)或(-)
l, V+ u* @' Y7 n( D/ n的形式表示。" J( ?5 S9 ^' ?/ o
爬升顶点,0 e6 D. [! D8 g: u. @
飞机达到巡航高度开始平飞的那一点。% y }+ O- R4 z3 u( l: g
下降起始点(TOP),% B' E& a" C9 @8 r0 V+ t& h: M
飞机飞离巡航高度而开始下降的那一点。
8 q5 @ B: @0 o+ D& x* k4 i操纵面的管状部件。
+ f1 }. K" H, N+ M3 Sreverser of the engine that can be opened to access
( P2 t9 w+ e, R7 Ccomponents for maintenance.
- Q- R7 u/ P4 w6 E; \7 X# H" \5 s* XT9 h |9 M- j9 z5 x
th
' ]/ l' N9 B) d" L: ]fo
# ^/ O+ N2 Z, j9 j/ ~- |, I9 TT
4 x( Z( m% Q) {7 ?th, a+ H5 N2 ]# E) L9 C% E
T7 b, C) G0 [ Y7 x4 X) |
is
7 y# e e$ H- Q% j(++ X. `+ ~" y& N9 p( y G
TOP OF
, ~/ N) E! l# e; }3 y8 E; cTOP OF DESCENT (TOP), The point at which the) \0 B5 `& G7 p% J9 O* P( d
airplane depar
* d; \) t$ }( f. t1 F6 ATORQUE TUBE, A tubular component
- c& F* c1 b3 H5 T反推整流罩% D) ]* l" I3 Z" L1 E' t7 }
在发动机反推装置外围的罩子。取下后可以够到内部
- B7 M. w3 }4 j0 z扭力管,
9 |* q% s% u0 q+ T$ D8 i6 ~用以将扭转运动传给 O& {) @4 b8 n3 W' U3 M6 I
英汉对照民用航空词典B OEING; n) Z8 U o, y
TECHNICAL DICTIONARY 157/ l" X$ }: Z" \$ b0 Y
TORSION, Twisting of a material or part caused by& ]% E* w4 p6 }+ l& ~, O% @/ M# m
external stress.- k' g6 y7 f8 Z( Z
ORSION LINK, A hinged linkage connecting the inner
5 B: n$ H! Z4 t+ g2 q; knd outer cylinders of a shock strut.
8 f& p+ |$ ^4 B6 ]due to the ram+ K8 W/ I/ t5 s O
ffect of high speed flight.
6 ^' ]- i4 l7 H9 u' JURE, Pressure higher than ambient
1 C0 s# u* J+ u) _9 t' Hressure due to air flow, measured in pounds per! L( h3 b& `* \" T# O% M3 m$ m4 |
quare inch (psi).
' S( n: u! L$ Ber than: s* {: ]( d1 U, b% W! H7 H+ t: ^
mbient temperature due to the compression of air flow,, L8 i; p' H( J! H- l
easured in degrees Celsius (C), or degrees. N9 [ }( K3 s2 w6 L
ahrenheit (F).+ J) d7 a- i8 R
TOUCHDOWN, The point at which an aircraft first; w: H; B% ^3 S
makes contact with the runway.
) B0 [/ J6 {% ?( D生的扭转。 X; o& C: g! Y& j( U
扭力臂,
" r* f; Z7 f, ~1 _减震支柱的内筒与外筒之间,用以防止活塞旋转的铰链
* A$ [9 Z# l P0 i连杆。. V( C/ }2 u. G% x7 j+ P8 t
的冲击效应
4 t6 P; A/ H" U. ?( B7 b* J4 t引起的温度的升高的总和。* H) @. P8 a" v0 E- J
总压,, O- ^7 x/ {! q3 z# o3 a
由于空气流动而高于环境压力的压力。常用磅/平方英
" R9 e) `9 n- u; J8 p# [, d(psi)来度量。
" S0 m) X7 L% G1 [0 Q全温,
0 A/ }# p; m; P, f3 t由于气流的压缩而高于环境温度的空气温度。用摄氏
' }3 d7 n4 x+ m! q! x* Z% ?(°C)或华氏(°F)来量度。5 P# V/ Y3 D) U) R7 I6 j9 [. b- O% H8 w
接地," Y+ o5 u1 R4 k! y. }5 y
飞机降落时,飞机最先接触跑道的一刻。
w5 d! E2 e9 |* l: i& Y$ zT
$ d, k# R9 s- F* z( La$ R0 f/ e# y3 T
TOTAL AIR TEMPERATURE, Ambient or static air5 x" y! s v& [0 R4 u4 S% G, V( S
temperature plus the rise of temperature
/ w# B2 ]+ V+ E' N; \/ Q, y+ G: X5 Te
" d1 I5 i1 ~! ^- i% j& I( @TOTAL PRESS0 I. U, p1 R3 c9 F* R% s: N2 S& r7 @
p
" b8 n* J, I+ f4 l! A: Q) Us
- c, y& W# w$ sTOTAL TEMPERATURE, Temperature high
5 }5 G* V3 ~9 S3 Wa+ q$ Z1 S# G. ~9 c9 @
m2 u/ z- T* X7 I3 p3 G
F
8 U# K& K9 V1 S* n- Y扭曲,$ A; l+ Y, w2 T+ \* T' f
物体受外应力的作用所产) z8 \7 K3 u0 ]" o
空气全温,' A! P: X! v. s
环境温度或静空气的温度,和由于高速飞行# j0 `& `3 u, p" a$ i3 @
而
! G8 E7 r; C/ [, i2 n寸+ K0 P8 ~9 r4 b+ D, H
英汉对照民用航空词典B OEING
# p9 ~& u2 @' DTECHNICAL DICTIONARY 158
/ n: l/ z& o5 s. D! Z$ ]TOUCHDOWN ZONE ELEVATION (TDZE), The B& y+ h4 _+ s: t: _
highest elevation in the first 3,000 feet of the landing
* r8 Q" v% o( S6 ~/ Lurface.
9 a. `6 o6 P8 r2 w. W6 Xrt of nose or main landing gear for
7 z6 s- F W) n3 o$ {ttaching a tow bar to move the airplane on the ground.
0 [2 b7 f* H" p; q y" H9 G7 ralong.4 E+ u' z6 V3 Z j6 @4 h" f
RACK (NO. 2), A navigation term that describes the& b& |. h8 }4 Y6 m- T
TRAFFIC ALERT AND COLLISION AVOIDANCE$ \+ [! y, V% Q) _/ `
SYSTEM, A system designed to alert the flight crew to2 N, _0 G8 U1 @% f
potential conflicts with other transponder equipped
2 x" n, p$ j- c+ U @8 Gairplanes flying in the same area.& O1 c7 g* g) k7 j! H; u1 X
TRAILING EDGE, The rear edge of a wing, stabilizer or
2 o* R. _; B+ ?' Ucontrol surface.3 S: ?4 L/ ]3 ?
TRANSDUCER, An electrical device that either takes
! L, Z9 S5 w. L/ velectrical energy and changes it into mechanical
5 b" t: F8 Q3 T" cmovement, or mechanical movement and changes it& F0 \% v$ J% W" [5 S
into electrical energy.7 f T7 ` A3 o4 r
TRANSFER GEARBOX, SEE - ANGLE GEARBOX
% A) m+ n6 p7 p1 h# ]+ e3 S$ U高(TDZE),: K# ?9 O' i0 Z6 W$ t$ i
高标高。
# p, j0 |8 Q+ N% E4 {0 f前起落架或主起落架上,用以接上牵引杆以便在地面上
9 S5 K* l. `! |6 S1 z) q' A动飞机的部份。
# }" N/ i K0 E# \, [* y+ N轨条, n+ { z+ p ?& j) X" @
迹,
0 D1 a1 ]# t7 @4 |# `形容飞机航迹在地面的投影。- [+ p/ n6 ]: J3 s; Z% \
空中交通警告与防撞系统,; f- g2 M- G7 A5 p
用来警告机组人员可能与其他装有应答机且在同一区
7 H+ b, g. ]4 A( k6 _7 ]域飞行的飞机有冲突的警报系统。
2 b5 P; A7 H. t- p2 m后缘," B, b( T9 Z0 l5 H
机翼、安定面、或操纵面的后边缘。, U5 y, A+ l7 w+ N
换能器,
' g, z' s. A( f, q0 Q, W能将电能转换为机械运动,或将机械运动转换为电能的5 I! {2 t+ Z$ C: ^
电气部件。
3 Z' Z3 V* R! m; l转换齿轮箱,
- ^" C; _' @8 i见Angle Gearbox
. [8 T0 u' Q" `+ W# \6 Zs l8 d0 ?7 H. c$ Y7 I1 I7 L2 `
TOWING LUG, Pa0 z- J# P L# i* L, q
a% ~7 S/ K! F9 C1 ~/ g
TRACK (NO. 1), A structural member for attaching fixed
u" Y5 a* H5 d" G% e2 y9 lcomponents to, or guiding movable components! U8 V- A, X1 Y. Z; F" F$ E
T' S7 }/ z4 r( a1 c+ A: M b
projection on the earth's surface of the path of an
& Y) O7 G9 {8 }7 e" Pairplane.
! J7 [# t9 o; q7 M/ O接地区标+ C+ U0 F. T1 k6 i2 }' b
跑道头端3,000英尺的最
% f5 N& v) p* ?5 l7 Z% Y; ?牵引环,
3 ]! v5 P& T7 H# L1 W移* [! h5 [7 q; q8 Y' e. g' S
用以接连固定部件,或引导可动部件的构件。
' @5 }, e9 m5 m/ O) Q( F航' y/ o' e0 D" g: X
导航术语。
9 [$ A7 b. c+ U5 p.3 _9 P! ~4 v7 j. b
英汉对照民用航空词典B OEING ~2 J6 U' s. s% t
TECHNICAL DICTIONARY 159* z0 U8 z0 R" ^/ W! s- ~
RANSFORMER, An electrical device which uses
( t. f2 X) y- W! aRANSFORMER RECTIFIER UNIT, An electronic
; m0 _" {. T, ~evice for changing alternating current to direct current( K: X- w. X2 n
supply airplane electrical systems. d. [& f& w4 m# ?5 q) u$ g
lse signals or triggering pulses/ O) ^ G0 `' E, |
nd cause component breakdowns or failures.; ^* T s, n; o) b) w
It consists of a base, collector
' |6 b: n2 e: k; u. p# V- fnd emitter. Two types of transistors are PNP and NPN.
; u a, w' b' J* N。
* i2 s$ b( Z% ~* i9 G( R变压器,
& M2 A3 I9 k# O. c1 v; v磁感应,将电能从一个电路转换到另一个电7 }, S2 C" [1 M' f9 g
变压整流器,
& l6 a% n# q0 H6 j1 ^ F用来将交流电变为直流电供给飞机电气系统的电子装1 ~9 d( _5 r7 _1 s; T$ v, A, z
置。
1 Z i- \" E9 F% [ A7 w瞬变,/ }/ P% p4 N4 l* W9 t u
信号或输电线上的瞬间电涌。这种电涌常会产生一些错$ q# w3 m) I: X; ~8 H
误信号或触发脉冲,造成部件故障或损坏。+ G7 X& J$ ] q4 o
晶体管,
+ r: S3 P6 }: ]固态电子部件。通常具有三极:基极、集
p1 ?- j0 [( c2 V. e/ A! d极、和发射极。有以下两种:- q# Y m* N g3 `8 }, [
PNP(正负正)基极电位低于发射极。
% P* X) D+ |, xNPN(负正负)基极电位高于集电极。
" O$ I$ O9 O/ h: vTRANSFER MECHANISM, A component for
$ b9 H) ~' K+ j: m" Stransferring motion from one place to another.
# l: {& H! L( h! M( g! K8 ST2 u5 K9 x6 A. T. Y- O. i1 l C8 \' J
electromagnetic induction to transfer electrical energy9 b$ w* Q$ `8 e% S! c
from one circuit to another circuit." |8 |& E# @/ J6 J7 }8 l5 K; W
T/ Y0 ], s+ }5 ?. `" C8 l5 U
d
) t% a6 Q% C3 @& A t6 L; |to: t" d* |1 u5 }) F/ |& ]( h
TRANSIENT, A momentary surge on a signal or power
$ G" l# _- B* u6 Dline. It may produce fa
7 x2 S2 m6 f) h' v& |- c+ |5 Ua
& b! S% ^& k. p( r# w% X! `TRANSISTOR, A solid state electronic component for0 u" y: x& X5 A, r4 [; T
use in electrical circuits.: h: Q. P2 w# \ E/ I
a% x5 a% U7 b* i! I7 v6 l, j: U$ Z* s
转换机构,8 x: L" I+ J/ q! |) g
将运动由一处转至另一处的部件7 Y1 G. I. h4 h9 I
一种利用电
( B+ M( Z7 w; ~2 R( h路的电器装置。
( p. P5 Y p8 s& G5 W' V0 c电路内使用的2 \4 \7 Q8 _, z/ G+ e
电
8 o ^" n4 C) D+ E1 B, v英汉对照民用航空词典B OEING
h2 p: J7 t6 ]" I5 oTECHNICAL DICTIONARY 160
! s8 @. i/ J& {6 ?' ^5 [TRANSITION, To change from one phase of flight to4 s3 ]+ m# `" y. z! Q; P
TRANSITION ALTITUDE, The altitude at which the4 b7 s* J) X5 F6 W( f& p
ltimeter setting is changed.# n6 H7 ~$ ~( m: m* @
RANSLATING COWL, The movable outer portion of% n. R7 D$ s6 S! w. `4 `
e thrust reverser cowl which is operated during3 O2 I) z: W0 o' |( c
verse thrust.
5 l3 s- n+ s4 s3 ]. h5 U: @RANSMITTER, An electrical component for sending- m) y6 D) O2 B4 S E
formation from one location to another.
: h0 E( v/ P8 u& c1 iTRANSPONDER, A radio transmitter-receiver which& k9 }) l: i. W, L6 l
ansmits identifiable signals automatically when the
+ k3 L0 E: ?8 p( b `& P, ZTRIM, The adjustment of engine and airplane controls1 i$ [, L# k0 c1 P$ p
从一个飞行阶段转成另一个飞行阶段。
! m1 l) ~6 l/ ]$ V5 h5 H5 |过渡高度,
; G+ O9 n7 h! | p改变高度表设定时的飞机高度。 e8 S5 v2 n1 Q* Y V9 S
平移整流罩,, X$ X2 [, r+ `$ S. l* u
反推过程中使用的反推整流罩外面的可动部份。
( ^) L$ S# [$ R3 k* a4 e8 ^发射机,) T# ?' n( z! x' P4 V, Z
将信息从一处发至另一处的电气部件。# r# G5 ]( Z) U2 D# r
应答机,, a% z$ n$ s; v; k- D- W( P( Y8 X
在收到合适询问后,能自动发射可识别信号的无线电收; z' S& p+ c7 v7 o8 t8 ~9 F% O
发机。. J) B& J2 H3 B
平,0 X4 t3 K+ o" \# B3 H( i" Y u7 ~
动机和飞机在平衡的状况下工作而做的发动机
; e. ^6 |3 K6 E6 Z5 |another.7 ?9 i: d$ a9 R) u( ?$ J0 e7 [3 ]
a/ t: I' z) S3 Z0 ^% p- x* }
T
3 P! E4 O5 c3 ]& X7 fth% {5 a2 t ?# T7 \
re/ H' ^( i/ l1 b. i, k
T1 R+ V/ T" s* o8 b5 M6 c4 J- {7 ?
in
! b, F( t$ Y+ g* T# ^& M6 Ptr
9 }$ b' m! S1 d3 d2 [* tproper interrogation is received.3 G# H/ t2 X6 w1 f1 G% h0 K- [2 H# l! \
for a balanced condition of operation.- N( u. w7 `7 V! O1 `) y B; ~# Y
过渡,
$ _+ H, q$ a" i" n) ]配/ G( q2 W( s9 ]
为使发
7 _2 C( F- `& V) n# G2 I- a$ i和飞机操纵系统的调整。
( S3 H6 N7 d" q6 h0 g2 e1 e英汉对照民用航空词典B OEING$ }0 y4 v* [% }$ | `* _
TECHNICAL DICTIONARY 161
6 q' g! r$ N- Y7 d3 oTRIM TAB, A small hinged movable part on the trailing, [; u, u' A5 k. f/ C
edge of a control surface (aileron, rudder) (see TAB).
% S& q# L# h' kL, The total fuel consumed from brake release
7 E9 I6 s( {9 bthrough climb, cruise, and descent, to landing at
$ N9 S/ @4 M% p& k$ ?7 X: p& J$ `7 Cdestination.2 F: N1 R! e5 ]
RUE AIRSPEED(TAS), The actual speed of the
' Z( U( a* Z; O: [aircraft in relation to the moving air. The true airspeed is
; `" |3 o' i6 H& a) T S6 Yated airspeed corrected for position; u) k$ {6 r3 S3 Q5 y
rror, compressibility, and temperature effects.
0 o! B! |! n2 g/ J6 U# V2 Z4 Gribes
7 Y6 ]% |4 B) K' |& V: R wthe output value for each input. V5 ~8 X7 c# f) \0 G$ O
ombination.
" h" T8 A1 X O% z$ e铰连在副翼和方向舵等操纵面后缘的可动部份。6 t x& G) j# C: ~
航班燃油,
( l/ X+ D4 g% Q1 @: o. m7 v- V8 `+ c一个航班由松刹车开始,经过爬升、巡航和下降,到) r1 Z* t p9 a7 E- {
目的地着陆为止,所耗的全部燃油。
( u: |7 T' `9 Q" _3 t* a变压整流装置,3 v; Z& \" E; m1 {/ }% q
见Transformer Rectifier Unit$ i, |1 i3 {; w: Z" z7 ^$ U s! j! @
TRIP FUE
9 e) M, { R1 D( m- ]TRU, SEE -TRANSFORMER RECTIFIER UNIT
' Z9 Y+ G- ]- f1 Q' t: {* M+ c& ~$ fT
# C3 Q! W& h$ g+ r8 c. Lequal to the indic e: W% k1 V, e0 o$ C9 G
e/ E" k/ E' E8 V d
TRUTH TABLE, in digital logic, a table which desc
f4 r' z- O) d( la logic function by listing all possible combinations of
J: p1 ]1 c3 X& W8 Y/ U! jinput values and shows
) U5 T5 O& l) N! u( V5 u7 `c/ ]* |/ }- V6 V/ C
配平调整片,
7 h8 P/ z) A: a& V: O* S+ d在( n% i4 E O8 F' `* w- P( G3 F
.1 K0 C+ }2 V6 Z b1 W
真空速(TAS);
( G1 @1 j/ g. B! L; O0 ]. e对于流动中的大气的实际速度。由指示空速经过
4 M8 W; V% k; f# z真值表,( V( V- y0 B8 v
数学逻辑中用来表达逻辑函数的表。该表列出了所有可) A. x8 r ~7 F
能的输人组合,和每个输人组合所产生的输出值。
- E5 |! N4 q7 @4 H- {飞机相
* b& S" d: I4 i位置、压力和温度校正而得。! \% o; O9 r1 g; }9 N( L" d
英汉对照民用航空词典B OEING
- e/ ~/ b2 G9 | WTECHNICAL DICTIONARY 162
7 [- X. z9 B z. H% p" z, ETURBINE, A rotating part of an engine which/ G% X- G% U: i1 E( `/ } N
kinetic energy from the combustion chamber ga: I$ o: P! L: w; d+ i. w
extracts
9 S* o ^/ ~# p- sses.
" y- \% T N0 {: U/ ihis energy is converted to turbine rotation which
' ^2 ? d6 i" htates the compressors and fan through a coaxial
4 ]6 N) c9 z3 P9 W% G8 z) ?. Vhaft.
3 j% I& p9 u4 X0 K$ ~6 h8 J; R9 y, QTURBINE CASE COOLING, A method of cooling the
& H2 y% ~+ h) y6 mngine by using fan air. This cooling process is used to z3 G g' A b. N6 m4 B
TURBOFAN,
' v* j# W* W Q' N ]9 Z" C(1). A jet engine in which the first set of blades is a+ e) y& [4 V& h6 U2 K# F1 w4 h2 a( _
large fan., j. S5 s8 n" q$ ~3 N
(2). An air driven fan/compressor used in air
j6 N: G4 m& j: ]$ Vconditioning system.
% ]0 u/ z7 n3 V' jTURBULENCE, The movement or shaking of an
8 v0 c2 P0 W! S. \2 E3 |& fairplane caused by unstable air masses." I7 D, D V" U4 I4 Y. w9 s
涡轮,
9 G! N6 W0 b7 K* o2 y: F4 j/ i发动机内,从燃烧过的高温高压气体中撷取动能的转动
: p- ?/ s8 ]" m; X份。该动能使涡轮转动,涡轮则经由同心轴带动压气机
, R3 Q8 n. z) p8 z w7 V k风扇。/ m' {1 C: @8 V5 `
涡轮机匣冷却,
3 x, N9 T- o) X0 `% s用风扇空气冷却发动机的一种方法。该冷却过程被用于% P3 H l3 S- [" {+ F' B
效率。
. v" f$ W! Z" r; K* G: f0 s(1).第一组叶片构成一个大风扇的喷气发动机。
7 S8 }6 O- T1 s(2).空调系统内的由空气驱动的涡轮和压气机组合。
' i6 @: R% u# v: c6 \' F8 {颠簸,! k- k6 _5 l0 c+ T! Q% j
由不稳定的空气团造成的飞机运动或抖动。1 y0 I8 ~, p" h0 i
T$ i8 K, l2 ~* \3 g+ A+ ]
ro
- v% v3 X$ Z% y8 |s
. f4 ~6 {/ [' y- t& g8 He
& m- ^! X/ K( \3 O* fincrease engine efficiency.
" j% t: u5 H, z7 o8 C/ W; L部: X! K$ a+ u- U- W. a" D0 I( J
和
( O6 n$ Y7 ~+ e9 U. {# p提高发动机( h. e6 Y4 f- b! t
涡轮风扇,% g! O( y' J6 b# |
英汉对照民用航空词典B OEING
8 z; \8 z5 g! X: Q( ETECHNICAL DICTIONARY 163( p# C/ W0 e" P9 `
TURBULENT AIR PENETRATION SPEED, A speed' e. p2 `- |2 X/ C; D' `0 Q
that provides adequate maneuver margins when flying0 \) L/ V8 d5 @, P: V( c; }
to unstable air masses.
6 V I. p+ K) w1 t: f# N, [: b4 C! jht
7 u: Y: w2 s- c+ l- u' r' h5 xstment in the control8 L& ~3 q+ v" w$ s) q# z
ables./ \( w5 V/ Y: r' u, w
UHF, SEE - ULTRA HIGH FREQUENCY
# t, o* J7 J& r0 L4 FNDERCARRIAGE, SEE - LANDING GEAR \( n0 E( C2 E( ^ f
UNIT, One of the type, a single component.
4 L) X$ z( i: [: E/ D* \UPLOCK, A mechanism on the landing gear for keeping
' P$ p8 K" D' V' H. }+ l. Zthe landing gear in the retracted position in the wheel
1 `+ C: }* d8 A8 a. F8 Bwell.: m V0 O6 q- V7 w* H
速度,
+ x6 S* j: x* P4 V: L, ?纵裕度的速6 _( }) m: y: [7 `. H
。7 w# f% T2 d+ @, ^5 a
调整操纵钢索张力的% c2 \2 y( b# c6 ~9 t) h3 H2 o
械装置。
5 Q3 ^, w0 T r# Q% C$ x) ]高频,1 h' e5 \1 D2 p5 [
见Ultra High Frequency
1 g" [- x8 y& G/ U0 [" Iin
+ |; y: i# }% t( N& \% F$ fTURNBUCKLE, A mechanical device with left and rig
$ |6 F- m a, C7 G6 qhand threads for tension adju
+ R3 z9 O# F; |* G1 L! @c, ^1 p- q, y5 S
U, h6 x' w# W ]- n# u, r R$ n$ v
ULTRA HIGH FREQUENCY, The frequency band
! O; g) l0 X$ p2 R/ y9 U* \between 300 and 3000 MHz.# f' [: V% r/ w6 s7 ], X
U
% J B; x- s# F) I* r颠簸穿过; c, Z. F7 p' \% s, G
飞机飞进不稳定的空气团时,提供适当操) J2 ~# ~" K" a8 s; W
度: n7 w! n6 U8 u0 J0 m
松紧螺套,
+ _, C) C t9 Q2 D& X k7 Y8 T具有左旋螺纹和右旋螺纹,用以
7 X! [/ b9 M9 i( t3 V) w$ c机
7 ]& h- ?1 G. ?/ i( ?3 L" `3 W超) V* h* g# V1 m* F
超高频,% l6 }% Z3 b/ W4 s
频率带在300 MHZ至3000 MHZ之间。6 i& z$ B: Y0 q: m* J; V2 K8 ~
起落架,* e* B( }7 H, c' k/ V) T
见Landing Gear: P6 ?8 `- `' f5 C
单元,/ Z5 x6 o$ E/ T# T
某一类型或某一部件。
7 R+ v1 D: m+ s G% c) p上位锁,5 L2 z# x% V; L4 Q) O6 J/ }
起落架上,用以将起落架保持在轮舱内收上位置的机
, P2 r1 n/ Q5 {5 C构。( A2 F( v, a% |4 I
英汉对照民用航空词典B OEING4 g9 w* j( q, {" _5 B, w8 H( ?+ O
TECHNICAL DICTIONARY 164
/ d8 f4 c% r: gUPSET HEAD, The head produced on the tail of a rivet
( r0 L6 ~- y2 g: vduring the installation driving process. (See& t `3 ^, G0 I
Manufactured Head.)- N9 N; Y1 B' Q: L l) ^
1 (TAKEOFF DECISION SPEED), Is the maximum
0 j; J# O9 t/ `: ypeed at which the rejected takeoff maneuver can be |/ d) W! T7 C' I% U
itiated and the airplane stopped within the remaining
3 q* x* s' _+ {eld length under the conditions and procedures defined
2 @4 p& V8 _/ l( r& l# P% Tthe FAR's. It is the latest point in the takeoff roll where
; S% |4 i7 S; T Q5 Q1 Rstop can be initiated.
0 m! S# g7 G( H" ^ yssure+ v i' \8 F/ E7 r) B
dient capability and maneuver margin.
0 M- N7 A+ E% U. gVACUUM, A negative pressure or pressure below
0 F7 f+ v" p" G3 [! n2 eatmospheric, measured in inches or millimeters of
' }% p% _! s0 s1 [0 H) Z' i* J; q6 n/ w7 Bercury.% z$ V9 _ W' d) F$ w+ D8 t
is' d# H. y7 T, M3 Q9 p
VENT, A small hole orifice or restrictor in a component$ O* {- T3 C, F/ b# y2 m
for allowing pressure in the component to be the same
9 Z( G: G8 H% m6 C- C: V/ x( zas ambient pressure. w% z) u% ?6 p) h5 g+ o6 } D
在铆钉铆接过程中,铆钉尾部一端形成的凸头(见
, Y( z, A+ L% P- ZManufactured Head3 S Z5 [- Z2 }9 o$ d u2 j2 K
V
( _/ F7 O6 C8 j3 W& G* hV
, H( D, K; P5 r# G' q1 ^s3 ?. o4 ~& ^+ a: @
in2 U7 o P3 I$ V+ }5 `, n
fi# b1 h# Z! L1 Q' J
in- o+ z( [8 o+ B; v
a
& z% _9 T; g& Z% T8 r7 g! wV2 (TAKEOFF SAFETY SPEED), The speed flown after& K5 J% R9 l( G$ w
takeoff during engine-out climbout maneuvers to a! ?. @) L- ]/ r8 w8 Y+ G4 x
adequate gra
& O- {; T; `$ Z2 E9 z" Nm
( D9 M* j: j( ]6 _3 r' f- vVAPORIZE, The mechanical process in which a liquid& i4 b, D/ L2 R4 {, [8 Y! E
changed into a vapor.
' Q2 z; K) y& z" t! RVECTOR, A heading issued to an aircraft to provide- w- O. d* {1 \4 F9 ~' N
navigational guidance by radar.
* x4 A% O5 q) w" c9 E- u铆钉镦头,/ }8 S! Y3 l3 f, P8 [' @
)。1 F$ p9 R% m1 e
1(起飞决断速度),
9 C H+ {6 t& {. @2 C3 n: S, [) P根据联邦适航条例的规则和程序,飞机能进行中断起飞! d7 r H' v; y- P0 o
在剩余场长内停止的最大速度。它是在起飞滑跑时仍可" b7 |4 q/ e& X, v
住飞机的最后决策点。
( s1 `; A' D9 ]+ I/ g速度),
2 @2 p% c! t" p! E在一发不工作起飞后的爬升中为保证足够的梯度能力. `7 y) J1 E" a7 ?7 C. f8 N
和操纵裕度所飞的速度。 t1 [5 x) Q* H! l/ Q& r
若干寸(或若干毫米)5 E9 Z, |- X$ z+ p) I
汞柱。
6 I. D6 q" \) j6 F* }8 N: O. z) \) [蒸发,2 O. S. O; O4 x( v9 A6 F: v
液体汽化的物理变化过程。1 r, c) M2 }% ?6 R5 C
引导,2 z- X1 c9 m2 k) T% `
由雷达提供的航向,以给予飞机导航引导。7 [7 {5 l- T% W% Y: D+ P
通气装置,% E& o/ ?+ |+ {: z
部件内,用以使部件内的压力与周围环境压力相同的小
3 n; [ C! B4 P' _0 A% @" D孔、或限流器。
+ B: p* ]# M5 h+ e3 XV. |/ {$ Z% V7 G0 C Y
且; u0 N7 P7 ^* I7 |
停- E w: c. a K( S' ~. w& v1 H' S
V2(起飞安全. W" K1 ]1 H# `$ |& O) B8 M! F2 `
真空,5 `9 h: l" k2 p# {$ e
负压或比大气压力低的压力。常用
1 a! H T. v& E5 M% C英汉对照民用航空词典B OEING; @8 M& U N2 ]' }0 o4 c
TECHNICAL DICTIONARY 165
+ C5 y# \& F' C* V) _3 uVENT SCOOP, An air inlet/outlet on the bottom skin of
) i- H; |; w! c* a4 p( {ir
1 u# O* w& \8 n3 Z$ @VENTURI, A part of pneumatic duct with reduced flow
! d7 o f+ C7 i$ f9 ^2 ^# `$ \rea for airflow measurement. (Principle: As air velocity
' L, m! K# W' ?9 X. h0 U0 [creases, pressure decreases).$ M& N# A# P! O! g& N. h
ERTICAL AXIS, A vertical axis passing through the8 G( {8 x$ X1 B+ r
airplane from top to bottom. Airplane left and right7 D v5 o4 \% s! V! s" Z' r2 o' _
trolled by the rudder.
5 L6 s3 u8 i+ `+ m, F" bVERTICAL NAVIGATION, Functions which provide
u; l9 K% H) |0 Wguidance signals to control the aircraft during climb or& |9 ]7 B8 b( L4 B, A% w$ Z9 _
descent.
: F i% u3 F4 i.
% N0 O# U$ f$ p0 K/ D! ?通气进气口,7 P; T d) D: M
位于机翼下表面蒙皮上,用以燃油箱通气和提供燃油箱
- J" I' d" f p- ]: X0 ~内正气压的空气进出口。
T* H( j2 f" v( J; P, ^文氏管,
: t( `% b0 t$ k& a! O5 d5 }气源导管上,导管截面变小以量取空气流量的那一部
2 @+ a1 t4 b2 u份。(原理,导管截面变小时,流速增高,压力降低。)* v; _* N9 o- n- z! m& X! b
垂直轴,
" {3 y( ~1 F# i# D, d由飞机上部至底部的垂直轴。用以操纵方向舵,使飞" `, r" M; C& e7 F3 d* z
右运动。8 [# J1 b( r* l3 h2 O# F
直导航,- v3 e8 I4 S6 I8 [/ H3 f: P3 T+ E
,5 Q ]7 U* U1 C4 R- m) n
the wing for fuel tank venting and supplying positive a
* y4 ~) g. H* }0 l+ y0 w fpressure inside the fuel tank.# @8 d2 D C4 l) X5 p. N
a+ f; O- l# n8 _8 g) P
in9 r4 r$ J7 m+ q& Y$ O
V$ ^8 p7 R( N$ ~6 p
movement con
4 u w6 v+ h2 J2 L/ _" q+ sVERTICAL SPEED, The rate of change of altitude; a+ E- k# W% O2 U. p
机沿此轴作左
6 u+ k4 ^3 G0 L垂7 \' S5 X# `5 p& N) O" y2 |9 _
在爬升或下降期间提供引导信号以控制飞机的功能。
* h7 l8 ^# F% X0 R垂直速度& z$ g% }8 H' Q9 t
飞行高度改变的速率。
/ k% B! V" h, q& x* r, o英汉对照民用航空词典B
# s. S0 S; r1 ?8 `" C9 k! \- u* FVERY H" o2 p* G% k3 X
OEING
: a5 a9 H( N( t7 m6 E: sTECHNICAL DICTIONARY 166
# q5 | H @" s" @VERTICAL STABILIZER, A vertical surface of the+ _: u/ n; }+ N/ ^3 M7 j* o- p" ?
empennage for stability/control about the vertical axis.
9 [8 M, r7 D6 N! zVERTICAL TRACK, A climb or descent profile.1 @9 I# w' G) Y% E8 p/ x: A3 ^. L9 N
IGH FREQUENCY, The frequency band6 _6 Q5 }4 D5 p% k, B( v; c) R
VHF OMNI-DIRECTIONAL RANGE, A navigational b% c3 I/ T: @& q+ z X8 v
system which tells the airplane's bearing from a VOR
! W! T7 W) X, }2 l/ V7 B2 dround station and its deviation from a selected course$ l# W, [4 {0 s, S5 c; D) _
/from the station." [9 A, W9 c* Q1 z$ J
ISCOSITY, In a liquid - it is the resistance to flow.2 L' Z% }& G ~: x; k9 j
VMO, The maximum design airspeed at which the
[0 | v1 R- l# E3 Hairplane may be operated. T) h. ~; H3 c7 p3 ^. {4 ]3 X3 N
在飞机尾部,用以保持飞机绕垂直轴的稳定性和控制! E( I1 c5 O: S* M6 g4 E# @8 w
的垂直面。; n* G4 X7 D: } Y) Y f
垂直航迹(VTK),1 B+ |9 k6 {+ V/ i- }
爬升或下降剖面。$ m3 T, u5 Z- v; P2 O" {/ z
甚高频,
1 S$ ^; D/ ^& \# T30 MHZ至300 MHZ之间。between 30 and 300 MHz./ z: ], Y1 { @* W
VHF, SEE - VERY HIGH FREQUENCY% e: c! ?1 [! ~1 B
g5 q% ^) [! n* Z2 J* ]9 \; i" _
to
; O2 x! l x7 P5 i. ~$ pV- Y& q. h2 f/ `; M; D
垂直安定面,
! W% F/ B) \3 p* v M' a* D频率带在+ J& v9 {' i* I0 E1 z8 X
甚高频,
/ ?4 K% p5 a/ n M; `% f见Very High Frequency. _4 }& ~1 }7 u
甚高频全向信标,! r ~8 }+ Q' [3 U- v8 _( ~3 x& W
系统。该系统可提供飞机到VOR地面台的方
* Z. P# V( Z/ C; D$ |位以及飞机的向/背台飞行的航道偏离。
/ o8 ?) n* U. ^6 Z3 i/ R2 o& u粘性,1 Q& z- f! a( i) K+ u7 [
液体中阻碍液体流动的阻力。% ^# j, O$ `$ B
最大使用空速,
3 S+ M; `' b, I: B1 I飞机可使用的最大设计速度。5 _+ i- }( o4 U0 @
一种导航6 T) p5 z7 r0 B
英汉对照民用航空词典B OEING" w+ i7 i; _, E# o4 k2 y% u4 O
TECHNICAL DICTIONARY 167( b; b# c( A& D- ]5 v2 p
VNAV, SEE - VERTICAL NAVIGATION' s0 _" O2 @) T
VOLATILE, The ability to vaporize readily.3 K8 o( P& J9 f/ L) h
LE MEMORY, In computers, a memory whose
, t6 c' X# K- @' Y7 ~* `9 MOR, SEE - VHF OMNI-DIRECTIONAL RANGE
. i1 f) F6 X6 [1 `( sVORTAC, A combined VOR and TACAN station.2 b5 f- e: W3 T$ r% b
ORTEX CONTROL DEVICE, A small airfoil on the, c& G0 s( U6 L; L5 y, ^
acelle for improving airflow between nacelle and wing
. f) T2 P) {5 e1 p" `" P$ A0 aleading edge.
, \4 A( E: l( ]6 UVOLATI: c5 m: I7 v) Z8 V0 I* A( s2 L
contents are lost when power is removed.* o/ f& L R+ @! N( Z9 z
VOLT, The unit of measurement of electromotive force.. r- U$ y* y A! t5 x% R
V
( Y* {. [9 s; f/ C5 U+ w+ ]V4 {6 A9 P% [. t/ o+ x
n
; Z5 R q- P6 x$ `/ u垂直导航,
! f+ S$ W. r9 z+ b1 t3 c- e2 y. C- w见Vertical Navigation. k, r o, U8 J! B" L2 P
易挥发的,, `- _ M( b) h0 }) }! E1 {
随时可以蒸发的能力。
, z3 S3 B: ^4 c/ Y" {! S. w易失存储器,
( y6 D% j' i& c' I在计算机中,失去电源时存储内容便丢失的存储装置。. l2 F$ \7 ^. b
伏特,) Z5 Q8 p: J5 [/ c9 L* Q( Q
电压的一种计量单位。
, l) H' o2 N" G! l+ [ \4 ^甚高频全向信标,
# ?: B7 S' e- q8 xtional Range5 J% v# K5 v" J6 ~7 C( P' N
见VHF Omni-Direc .
' Q g2 h, a. GVORTAC,
4 q e* [ g- w8 k9 r" |6 q) s兼具VOR(甚高频全向信标)和TACAN(战术空中导- X5 @3 I7 y; ?! x- S
航系统,或称“培康”)两种导航设备的导航台。
4 \5 R7 ^6 I! s涡流控制器,
0 x! [2 v, Y u J! E9 P发动机短舱上,用以改善短舱和机翼前缘之间的气流的
. y% N/ H4 a. [小翼片。
/ j/ r0 Q- z7 ]英汉对照民用航空词典B OEING
- A5 Y P0 C7 ?5 n3 a- CTECHNICAL DICTIONARY 168
2 t3 A# ]6 D; x2 X% y7 z# L: DVORTEX GENERATOR, Small metal airfoils, located on& ?6 d( f" M& U M+ h$ Z5 U
wings and fuselage for delaying separation of the air/ ]. y4 I1 E$ o+ ^; g9 @
ating local turbulence# U* G* x" m. f
ortex).4 m4 D- |, W2 l- N
357 U5 q6 X- I$ C# m( h0 U2 r+ m
stall speed in the landing configuration.
5 ]1 u2 v9 \- D5 t$ y装在机翼和机身表面,以在气流中产生局部紊流(涡
/ _; x' q8 [3 B. U ~( ^流),来推迟气流自表面分离的小金属片。
1 L' A3 {2 `( \4 f8 t度),# ^ C" Q; @) { Z+ o2 c' C
在着陆形态时的失速速度的1.3倍。- s, H5 Z' n* E, t7 f# ?
见Vertical Track
: f S: F0 ?5 D: A- q2 v: G$ vflowing over the surface by cre. I: _! V5 z- R8 G' y% q/ W
(v( E# v$ S1 ~7 w6 G7 h! k5 o- ~
VR (ROTATION SPEED), The speed at which aircraft
) K) z6 L3 W5 A6 Z: ?rotation begins in order to achieve a speed of V2 at
6 |. D# q/ f2 l4 T e" q& B3 @: \3 Ifeet above the runway.
: p# z3 x2 d4 R" {1 CVREF The reference speed at the 50 foot height in a- G" q5 B' J/ K, I+ ?
normal landing. This speed is generally equal to 1.3
7 v% e; J" |0 _) _5 ntimes the
/ @/ i! G/ y% _0 @: A; P, jVTK, SEE - VERTICAL TRACK- f5 L0 j2 Z7 b$ m* J' k
涡流产生器,
" }% i" A" J% J& D' i7 ZVR(抬轮速
. \: b6 I2 e* u- a7 X2 a7 d" ?+ A在该速度下飞机抬轮开始以便在跑道上空35英尺时达
- X8 Y- I1 x" K; }$ Z到V2速度。
0 B2 r+ N$ }* t5 l' XVREF,
, A+ w. m4 Q1 O飞机正常着陆时,高度50英尺时的基准速度。通常是飞
G( H0 s& @# T; ]+ G机# c+ d# v3 P9 j9 I6 H5 g* s5 X9 c& [+ @
垂直航迹,
- ]* R" | D- L.: Q: ?* I; ]: g% R7 a+ U
英汉对照民用航空词典B OEING
8 Y2 @7 B: t) D% j- qTECHNICAL DICTIONARY 169
g- D; c& E0 |8 x/ f5 tW- P' b! v6 D& C: X8 [) B. x$ v
WALKING BEAM, A mechanical component attached to
, D6 C' Z: T8 t1 _: w3 E% jthe main landing gear and a hinged support which helps
4 p5 ^/ X/ m" F) D' Sthe actuator during retraction of the main gear.7 `. @3 U! s2 ?
ATER LINE, A horizontal reference plane along the3 |9 @7 R* i1 @1 D
fuselage for vertical measurements of the airplane.
0 O/ o }6 A+ K2 G* I& yWATER SEPARATOR, A component in the air
! q1 n' K0 C9 Aonditioning system for removing water from the air: M, ?$ N( o4 n$ F9 q/ V2 B7 R7 U
动梁,
- H6 S0 b& x0 R4 Z8 b主起落架上,一端连在减震支柱上,另一端连在铰接支
( z4 U. q; U7 V% O撑上,用以协助作动筒收主起落架的机械部件。
4 m! t0 D+ c4 q+ f: R) B1 t线,
6 a* M3 d2 t8 Z1 p9 z; Z沿着机身展向,用以量取垂直方向的距离(或长度)的! B M! a1 \$ @1 c# f; G6 f2 f
水平基准面。
! J2 |, ^3 n4 V2 D6 c* x f0 W; G水器,: O" h- t/ [2 L- z- g
空调系统内,用以在空气循环机的空气下游除去空气中! I `8 m) ]3 X, H) N
W9 [; @$ {/ v$ F0 H: r2 j$ T( M
c
& l) s( ]2 [$ |! A' P' ~) C, Pdownstream of the air cycle machine., m* T0 o, j& N# i6 e
水0 t% I; l; U! b" a* e% d, i0 _- _
除
0 D: H! S* G, p! w1 \! H* m8 U, p的水份的部件。- h1 A; z1 J/ e$ D
英汉对照民用航空词典B OEING" \" |9 o6 B# M
TECHNICAL DICTIONARY 170
% }$ @9 Z3 U; Y3 q* }4 D2 wWATT, The basic unit of electrical power.
) j" [$ w5 q. f V9 {( b' `7 xWAYPOINT, A predetermined geographical position
7 H! v5 u N0 z% r) ^( Nused to define a route. The waypoint is usually defined! e9 ?2 p% b) q& f4 n! y
in terms of latitude and longitude.
7 w4 @7 {" k7 ~4 ]+ WWEB, The portion of a beam or channel that has been' H) G0 u7 a) s% t& M W- D! B
installed between the top and bottom flanges. Its prime: k1 m- x# f& D7 l
purpose is to furnish strength.
$ D" @. ~% V8 J! P8 A* R. ZWHEEL SPIN UP, Rotational acceleration of the landing' y% t% ^& s& u7 v
f the9 i; P) J: |2 `
nding gear (undercarriage) after retraction.
- b4 I ]: R6 y电功率的一个基本单位。$ }! U$ R7 m% L- W: \( D& F
位置。通常用经、纬度来表示。0 H' Y3 U' ^& i. l" }
腹板,
2 U2 ^8 q: ~$ \" W* M* R梁的横截面。常见于上横梁与下横梁连接成工字形。主$ b5 u/ h4 `, b" b0 x) M4 C
要作用是受力。
- d0 U' g% v2 D5 N+ B轮加速,
3 q+ N7 m" p% O' g7 q飞机着陆接地时,起落架轮子的旋转加速度。
. x9 z# [: d" C! D轮舱,
& n2 _# D. K* i6 a k$ G飞机的一部份,用以在起落架收起之后,收藏起落架的
! C0 B2 W7 X ^& Y/ H/ u% d' [$ h* g那一部份。
& `9 L Y. B% L: K) Ugear wheels at landing touchdown.! m' M6 ^: \" v6 @7 X# s) x
WHEEL WELL, A part of the airplane for storage o
- ^# F4 u9 B1 N. g* o0 X0 ]la( u i0 U9 U o2 @; l- z6 E8 g
瓦特(瓦),
- [$ U! _) x4 ?, E3 K& k8 l! p航路点,+ F1 G; _& ]' Y; e6 [
用于决定航线的预定地理
* N1 i* E2 L0 } \; j& |: u机
. y. T5 B3 F; O8 K英汉对照民用航空词典B OEING
3 r y; f. R- `- `TECHNICAL DICTIONARY 171: k+ R- I# @( f: u/ F/ x6 I
WIND COMPONENT, The effective wind relative to the
/ x% J1 i/ I6 C. M$ Shorizontal axes of the airplane.! i+ u, Q" R- O$ L
WINDSHEAR, A change in wind speed and/or direction7 v5 q! ^ C( ~5 Q9 R! b
a short distance resulting in a tearing or shearing( s& ]1 @2 L6 B2 Z8 {. ?1 ^3 E
effect. It can exist in a horizontal or vertical direction and4 E% n- E2 `3 r1 R0 J: w5 g
occasionally in both.7 V3 Q' U- d" g. b5 s$ a" L
WING CHORD PLANE, A reference plane from the tip) D# [, y& V+ `* j. y, L* J% b
of the leading edge to the tip of the trailing edge of the& }. _7 p$ S' |/ v8 d( H
ing.' S0 X3 C: k+ q( W" N
ING GEAR, The landing gear attached to the wing
3 K! ^ P z% Ytructure.0 {% S. W$ `) ?. G: k
ING ROOT, Part of the wing which is attached to the
I3 m1 r$ C. N. i% l- T1 Sselage.
9 r1 S9 @2 n% a. @" OWORD, In a digital computer, a word is a group of bits
) o- E* W2 X$ {( bwith a specified length. The typical digital word is eight
5 z* t. g; Y6 {( k5 R0 }! \$ [9 Ibits long.
% z/ k- Z. p. S8 e风向量,6 N+ Z: S( D3 ?7 ~* U7 } N
相对于飞机水平轴的有效风。4 T# r4 c N, a
风切变,( `7 n" g5 ?7 F! H7 [
短距离内风力或风向的改变而形成的撕拉力和剪切力。
! t$ z ^. n+ k2 v. `可发生在水平方向或垂直方向,有时会在两个方向上同时3 N+ A! @3 Z/ d0 C; q3 z- z
出现。8 r* c$ p; d2 Y/ E6 H$ z$ n0 ?
翼弦平面,
5 D& ?: e5 C2 _通过机翼前缘顶端和后缘顶端的参考平面。* M n# Q, B3 H
翼下起落架,
* v5 _( M3 O8 X2 L* i5 A4 T0 k7 B接连到机翼结构上的起落架。$ z y7 o5 h# E7 t5 m" l3 z
翼根,
: b* f U1 Q, m机翼上,与机身相接的部份。
/ W2 x( B( w5 \4 d字,. |9 u% W* s3 }) C7 K5 r
在数字计算机中,一个字是由一定长度的一组字节所组7 Y% ~/ K6 e" _* \) X
成。一个典型的数字字,有8个字节。
1 O+ |. f3 V, o6 }6 v( G2 ^7 a) Ain( o2 Y5 ?4 e6 L, |+ C. I, c$ Y
w
$ T; _3 B* f2 GW0 v6 s! _0 K& z
s
1 t0 j) d% j r. z6 j+ ~W
2 M7 N) U/ J1 M2 i1 tfu, w& W) z" |4 ], k
英汉对照民用航空词典B OEING, F' B% p! J! b' H0 G
TECHNICAL DICTIONARY 172; {) A- g* ?+ b! q1 b
WRAP AR9 X f7 \% s4 m& f& e( L
computer's
. a6 J6 c1 Y- g* q& U5 KOUND, A BITE test comparing the
3 A a! o: A. Y3 ?* p- i- ]2 xoutput signal with an internally stored value." o; i; G- P" Q5 J
XTK, SEE - CROSS TRACK
, P W3 |, x% e' r, R3 C7 ?AW AXIS, A vertical axis passing through the airplane
8 v3 {2 c% z5 y) ^: z0 ffrom top to bottom. Airplane left and right movement
8 f: y, a9 k9 Qcontrolled by the rudder. (See Vertical Axis).: D' ]2 q" R9 p
AW DAMPER, A system that is used to move the
! D* q$ Z, w& K' }: v! ~( R' c* l; tdder a small amount to oppose airplane yaw.; A+ y0 [+ z' X, N
es. V. J% ~1 F: B+ q
回测,
; `# {9 b+ u% a自检系统对计算机的输出信号和内部的存储值进行比
7 S% b( ~" m% P1 b6 o. Y较测试。) {0 F( |4 A" q/ N+ Q" L
交叉航迹,9 s5 V9 {" f1 L+ @' q' d, f
见Cross Track7 V8 R+ T4 c( _4 ^2 H4 s- x
X
; O( S j, i. L6 q& w.
# x6 U% ^) ~$ p& U/ j# L {( P偏航轴,- N% |8 l- w, z4 W
又称垂直轴。由飞机上部通向底部的垂直轴。飞机绕此6 ^( c" P5 L9 ]" ]6 f( b& |0 g) g
轴运动即造成机头的左右运动,这种运动是由方向舵来操
8 Y7 r7 Y& F4 S纵的。
; q+ F9 y$ i# E: M% ~& y& R* e: E偏航阻尼器,
6 F$ ?# J1 B" _ s; ^; E' ]9 f用来少量移动方向舵,以抵消飞机偏航的系统。
7 I$ [! j. g2 K+ B飞机绕偏航轴运动的速率。
; X; v5 y, r1 ?5 E# b# @Y" }3 u1 ~' ?6 \" g* }
Y
8 o5 s) w H2 s' N1 xY/ L1 c! k, C- y. [9 `
ru! P x( N3 |' e& _* {: ~
YAW RATE, The rate at which the airplane mov# L5 g3 x4 v8 `, [2 k# B
around the vertical axis (left, right).* L& z- ^9 d/ G5 B
偏航率,9 o! u6 {7 q# k V, `; y1 k
英汉对照民用航空词典B OEING N( ~: e5 P' O: X2 l8 F, @9 t G
TECHNICAL DICTIONARY 173
F4 l$ U1 R! [/ t, y! zZ1 Y8 _, u7 s+ V3 r- q: o" p. `* f
ENER DIODE, A special type of diode which, when, _ u* f3 _$ e4 @* Q( E# s0 C8 o2 \
ZERK FITTING, A device through which oil or grease is8 b; K9 f' |. s4 K
upplied for lubrication of moving parts.: [5 Q1 B1 j3 e& `6 @
ZFW, SEE - ZERO FUEL WEIGHT& ~' Y M1 @+ y* V7 ^
ZERO FUEL WEIGHT, The maximum allowable weight
( V: L1 J+ a# ]% O: z5 ~: G, ?excluding usable fuel.
# b1 H4 l" e* y8 C2 q纳二极管,* h. [! H* S5 _
又称稳压二极管,是一种电子装置。正常电流可通行无6 _; c$ k7 E8 d( L" n
阻,但反向电流则必须在电压达到预定值之后才能通过。6 m' e6 ?: Z: w( m
在飞机电器系统内做为调压器之用。反向偏压时,它有一3 r6 a% {9 Y: p% a! L7 d0 {$ @
个恒定的电压下降。
; p- H6 y7 r- Q7 e3 X1 h& w; hZERK接头,
! G$ y: G( B2 d; I$ T$ b8 }7 _ZERK公司出品,用以接收滑油或润滑脂,以润滑活
/ F/ B4 e# w$ k, |5 n, P动部件的装置。; _' d; @( t( }6 y% T5 z
燃油重量,$ S# w2 |; n; }0 U% Q" D$ _& t: e4 m
见Zero Fuel Weight) c7 n( A9 w4 O5 n. h+ }2 ~9 u
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reverse biased, has a constant voltage drop. This; \! d3 q/ @2 Y! N3 o& j
property makes zener diodes useful as voltage
+ e7 c* J! s4 @1 tregulators.4 |/ ~/ W) t7 U7 P# K
s
3 F- h$ s6 i) U5 a* g! f齐2 h, y% Y p/ k# |
无1 W4 D& P6 x" l
.
]4 d* F5 I3 @无燃油重量,
4 o$ S( s8 n; Q8 C3 P) {扣除可用燃油重量之后的最大允许重量。 |
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