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airspace of defined dimensions within which Flight# H+ M r- K, O% F _! n$ V
Information Service and Alerting Service are provided. I! [6 \% S) h2 I# _$ T
F
7 W: U6 ]9 p2 qd
6 V3 X1 F. W3 T6 h: w. `F3 C" ~: U, R. Y5 Z
in
. m- P0 B3 m, W+ V2 e. L' Va
7 `3 J% M7 d/ x5 ^ ]F
k' @/ x0 O" Q, @2 _s4 e H% K: u2 ^6 p' b" p
s
2 J9 g+ G9 Z/ w4 `% I6 h2 F飞行指引仪自动显示(FDS),
4 B( m- |5 C( i- Y5 L* X当飞行指引仪的开关处于关断的位置时,自动显示的飞) }* n, q4 ` ^ S! d2 ]* j# K
行指令。
. Y/ s0 p9 |; b* A( H) r飞航情报区(FIR,UIR),6 w8 E$ k: S4 p5 ~0 S; z
一个有飞行资料服务和警告服务的范围
* A$ ^$ m! D/ s; N3 o9 b% U. i度层。
v5 E+ h( r7 h, W" _50表示
- z7 s9 i+ Q) M- M' F显示自动飞
/ t, r' A" r: O6 A/ K英汉对照民用航空词典B OEING& S$ P5 d) g& e! e
TECHNICAL DICTIONARY 642 | M) L2 @8 l
FLIGHT SPOILER, See Spoiler.
2 V, b- L" F6 }0 oLOAT SWITCH, An electrical switch which opens or& d, y7 z) U y% G0 |9 Y
loses an electrical circuit depending on fluid quantity in
2 f1 }- r+ W) ?* l2 e0 We reservoir.
# I' i9 M% z3 F6 N" {% HLIGHT TRAINING DEVICE: Any device having a full' ]9 @; B2 W9 h' y8 @- C7 h4 d
cale replace of instruments, flight deck area or an: p% b: C1 e# v
nclosed airplane cockpit includes the equipment and. ]- m J4 i" L# m' H% {* a
rograms necessary to represent the airplane in ground X3 c( p: L6 Y* L! @
nd flight conditions.
: e# ^$ l; p' b6 S& O, g6 yLOAT VALVE, A valve in a fluid reservoir which opens0 h& J$ H/ F( ^3 [& H
nd closes an inlet or outlet depending on fluid level.& _5 [1 q {4 S0 v2 x; R
LOWMETER, An electrical transmitter for measuring
' W, M$ e$ K5 q1 _( z8 hthe engine.
* _/ _3 R+ G! ~( l7 M, ULUORESCENT LIGHT, A light emitted by a gas filled
; \8 S# D" a3 O* ^" K; m飞行扰流板,
2 G) O0 V) S- w0 z见Spoiler.: t& U" ]( G& A
浮子电门,0 @1 `% W* P5 m; {( a
根据贮液箱内液体的量来接通或断开电路的一种电器6 S% L9 p5 ]3 _, U& O6 g
开关。
; K( W' v! q! s) J( [飞行培训设备,
& Z7 ? ?9 e- [ _, W B仿仪表、驾驶舱区、或封闭驾驶舱的任何设施仿真装置。
# P4 C T7 |! V6 T3 s8 J6 ^; b+ Z包括可体现飞机地面和空中状态的设备和程序。
" D G) _5 F4 f, b* D6 o2 I# w浮子活门,. A1 k/ v6 i7 j& `; @0 X
装在贮液箱内,根据液面的高低来开启和关闭进口或出8 _( K6 i$ K& D
口的活门。8 L. f9 h1 P/ |0 n2 E; \( o$ ~5 _
流量表,, v' E/ Z% E$ V- q8 y' F* ?; q& w
用来量度流向发动机的燃油流率的电传感器。
+ r# X Q, C; l萤光,5 E, {: ^3 A, }2 X3 k* o4 Z
由一种特制的充气管所发出的光。7 R- j; p, A2 r$ w& D6 O: P
F
6 M, z4 o/ w) r5 qc9 w1 L, l# x0 y: T( K+ r' l4 Q
th
: }: e+ m, ^7 g/ Q% F! wF
+ o; |7 C. `' \) g# ss
% P7 P7 h0 r% J* @" u, Pe0 Y" G7 j' u7 f
p
& j3 r, t% V1 ta% S$ b' S3 n3 b
F; J5 Z4 M. i+ { s
a4 F6 n# D. ~$ A0 w; l6 B
F
/ h6 P7 Q; R2 Cthe fuel flow to
1 H% g" I7 u5 P$ v1 _F
$ Q" V4 s- T d ctube.' g4 ~ @ @- W" D0 g" K T
英汉对照民用航空词典B OEING C, I$ J# \2 a( f) E$ c
TECHNICAL DICTIONARY 65
0 p' |* z, R: h# `FMC, SEE - FLIGHT MANAGEMENT COMPUTER6 ?$ ?, s$ J& [! \0 F7 H
FOD, SEE - FOREIGN OBJECT DAMAGE
$ o4 O! L% X: `9 gORCE BALANCE VALVE, A valve controlled by the
/ `9 q& C1 t+ C' H' `OREIGN, Offside; opposite side.7 P6 o$ G w) p A ?" T T" k" M
OREIGN OBJECT DAMAGE, Internal engine damage; C3 ]" J- d" X% p0 J+ y
ue to objects entering the engine air inlet.
# k' E, W n1 W$ M/ @RM, SEE - FAULT REPORTING MANUAL' N) s3 o% j1 D3 M: m! `6 q
UEL CONSERVATION, The activity of planning flight# L" ] Y7 S" a0 r2 ^/ a
ltitudes and cruise speeds so as to minimize fuel
* [$ R! w' N; O6 \# F% \. Consumption.! f6 M& v1 O6 n
UEL CONTROL UNIT (FCU), A component on the: z5 J3 |2 K6 W! Y6 |/ [
ngine for controlling fuel flow for starting and engine
& [7 Y$ j2 R: \F9 B9 L$ L- L. Y5 ?7 D- }, g
feel computer in the elevator system for hydraulic: s" x1 [+ \% a
pressure supply to the elevator actuator.
# p2 \9 d/ s4 u. F1 IF
6 B- Z- s% Q) P' C/ NF
; k/ o3 S4 L0 [- f D, V, rd! g6 ?" U$ I1 A9 F+ V/ v7 ~
F
" `1 B! R4 y) KF
, l" Q: y! ]6 x" ~; l7 g+ da8 P3 j1 g, E# W& T8 X
c
- ~5 F9 Y5 A2 b( F0 q3 ?F
/ M1 _9 r+ w( N, be: k+ g2 O% ]. M/ a/ k
operation.
' `+ T$ G4 p( C: H8 h飞行管理计算机,( ^9 k/ z+ F3 [+ t
见Flight Management Computer.# ]5 I i6 k+ O" J" e# T( _
外来物损坏,
) w& o' L( x; U6 z( M" t" Deign Object Damage3 x/ v. y2 N1 m, x
见For .1 q1 p5 b7 T0 r7 o7 E6 ?
平衡活门,
- [4 q" S3 Y+ j内的感觉计算机控制的活门,用来向升降
/ p& I7 w) L3 ~( g# `" g2 I* H外面的,
0 }$ Q; b4 u4 a0 D另一边的,对面的。- b# M1 [8 n! d, }6 G: ]6 _7 u
外来物损坏,7 J6 O% F1 ^/ ?2 u
由进人发动机进气口的物体所引起的发动机内部。
4 r1 B# P' v8 ~故障报告手册," R- {2 ~$ A9 V6 s& J
见Fault Reporting Manual
, F2 Y' Q8 v; o+ B" N力
) }: d2 ~. ]( M) P由升降舵系统
/ ^5 Y2 z/ X I. m) o* d8 @舵舵机提供液压力。 B. }6 I1 `7 Y D
损坏' _# j) i2 k d4 J
.8 s7 `, z% J/ x0 T
约燃油,
" i* w$ ` p; c- ~, |# d! H为使燃油消耗最少而对飞行高度和巡航速度的计划。' e, w0 t7 ~! u5 O
油控制装置(FCU),( s* z# s' N1 m) a3 @0 W
发动机上的一个部件。在发动机起动和运转时控制燃油
$ M2 g+ c& R- a! t% q) Z7 y节' t( W7 W% a {4 h: m
燃) B+ K" W- h0 h/ V2 I
流量。
4 X$ X1 w5 p, m: C( C英汉对照民用航空词典B OEING
4 x* g8 y1 h/ sTECHNICAL DICTIONARY 66
c4 g+ Q0 J4 P7 w- V. N" g) nFUEL FLOW, The rate at which an engine consumes0 M! _. l8 n" ?1 o5 l6 N
UEL HEATER, A component on the engine for heating9 R0 X; d7 R- A! r
UEL JETTISON SYSTEM, A method for reducing
& J3 V6 H' S2 G( {5 O+ `e8 t! ~/ q: ~+ J- ~6 H0 m" d; s
ULL FLIGHT SIMULATION (FFS): A flight training' [ h7 W1 o* `$ q2 V& w2 V' W
evice that incorporates full visual and motion systems
- N6 J k: `+ E5 W4 d1 s) P& qnd specific model airplane.
! ~2 `8 @+ A6 l4 F$ L* M5 xULL-WAVE RECTIFIER, An electronic circuit which2 \7 K5 ? r8 j8 y- f
hanges an alternating current signal into a pulsating
+ ?# z1 ] k3 {1 J0 Oirect current signal. S2 G: w1 _: w9 {: ]- p# i
or/ B; g8 O: M. t" D* r
AGE PRESSURE, Pressure measured in pounds per
F% s- B4 |: zGALVANIC CORROSION, A form of corrosion caused8 u0 D8 H. M Q5 s% O
by the contact of dissimilar metals.
* p9 s& e: n+ y$ [* f: d油加温器,
# Z& C, f+ F4 g" n/ O2 H热燃油以防止发动机燃油$ ]7 z. {6 P9 z. {# r; _
急放燃油系统,
4 [: ]! j8 m$ `; v中的燃油向外排放以减轻飞机重量的: G$ p y1 N% N& Z" P
动飞行模拟机(FFS),
- b: K( }3 d' ~一种飞行训练器。它综合了完整的视景和运动系统,以
! @, Z" x6 q+ R, q) }具体的机型。/ N# b( U6 y) b3 t2 E
波整流器,. f$ g l$ V& e @- n9 o. r
用来将交流电信号变成脉冲直流电信号的电路。
" K _! n$ l6 d4 E7 I( h9 Q压,9 K& x% D$ P' |: P+ X
平方英寸若干磅(psig)磅/平方英寸的计. q/ H. y% ^; v; E/ G5 ?4 C
电解腐蚀,; G$ N$ ^- m8 e; f/ @, @
一种由于不同种金属的接触所产生的腐蚀。
! T$ W! K2 U& K) \fuel measured in units of weight per hour.# A; K, v, d6 f# k6 V8 V' C4 z
F% ]$ @! X% A. C+ o$ g
fuel to prevent icing conditions in the engine fuel
% K! T4 q9 Z1 _$ {7 s, ysystem." [" J3 n6 m) r0 _
F
/ L& X; z# z- ?7 g9 Y: aairplane weight by discharging fuel from the tanks to th
8 E# N% U0 {& Y, z* toutside.! C( Z) P9 |6 b. x Z0 l
F
0 G$ }: ~ s; Z# e# S, _. Sd, l9 q# X& g4 P" z; H5 T0 C1 x' S
a
. L3 N( t2 O# `, L+ e6 b& ^3 KF
2 ~: ` g8 y% p, z# D- H5 {* M+ kc
. a0 Z4 ^+ f; ]d1 y H5 y$ y1 T* a9 i
G
2 h. V$ E& h! z# _GAGE, A component for showing quantity, pressure," N0 `! u* Q" _: V4 L
temperature by a pointer or numeric display. ^4 x9 X! u2 _7 V4 g' t% A
G6 Q0 ]4 j5 w9 P1 G
square inch gauge (psig).6 _( v: X2 h" }% R
燃油流量,
% J1 r) k4 M7 b! _! r发动机消耗燃油的速率。以每小时单位重量衡量。1 v" b9 T- {$ e$ Y& F6 h' E2 `! \
燃
' O! x. k% [& N9 J2 N: @发动机上的一个部件,用于加! n s, l# s b# ^5 O4 P; ?: Z
系统结冰。$ Z+ |2 J+ ?- A& K: e4 s b. m0 d# r
应4 f) |0 ^0 w9 R8 K, `9 ~# v1 W
一种通过将油箱
1 Y$ H/ G+ v5 H9 w- X5 \- k方法。
9 O6 ?4 `7 C q& ?! g0 T1 ?# b全0 r8 l3 G% h7 i: c* H
及' y- l/ H, f. a7 r- f: D
全! {/ N5 q! g+ `( s
计量仪,
6 j* _$ x I& ?, [3 k4 H% n& _由指针或数字显示出数量,压力或温度的部件。
& E& |3 T+ {+ i& @5 m' X, S表
* T" e! l8 P& r& h6 M+ d单位是(每
1 |: [: t& B! |4 l; @4 f示压力。
. T0 C$ Y: V2 c+ o4 z3 }+ S# p英汉对照民用航空词典B OEING
: |1 [8 ?/ S, v$ x5 p. X* T/ ^8 {TECHNICAL DICTIONARY 67( p5 C. Z# t, S1 E- r( _8 G5 W8 Z+ B
GASKET, A seal between two flat surfaces.. J% ]' \4 j( _# w9 r* l
be individually controlled for the amount4 q/ }! [7 j% _+ @$ W4 E) l
nd direction of supply.0 o/ l; h$ R) J! l& } f1 a
ATE (NO. 1), Airport location used for
9 y+ y! x' R: T% Bading/unloading passengers.
: T- w {3 x& M. J. GATE (NO. 2), SEE - LOGIC GATE
5 |5 v" H8 n1 k. |$ p$ fATE VALVE, An actuator operated, sliding device in a: T, r. e8 B+ d) e
uct for closing and opening the duct passage.9 [2 y9 |- L! B" q
间的密封物。. U6 ^6 }5 H# {) s n# C
调节供气口可控制空气的量和方向。7 a8 t0 N- K' N. D
登机门," F9 ^8 y$ ^" [- L# m1 `; Q
机场内用于乘客上下飞机的通道。
4 R2 \( `5 U6 v& D4 E+ j& ]' h. S逻辑门,& V. E# Y& m6 p3 P; \ }
见Logic Gate
1 D, k$ x3 |9 g9 e* k+ }' C$ [$ x sGASPER AIR, An individual air supply for each
: q# I6 X0 |1 [* Vpassenger. The air outlets are in the Passenger Service. m1 A. X/ P* s: d
Units and can" K6 {7 }4 G( p
a8 U5 Z) r4 J# |( ^0 n
G
0 k3 i: x: ?5 L, `+ W$ \lo
9 L' r, r+ b! A; F$ J/ j0 a; s6 eG/ L }" W' [% p5 o+ P. X
G
6 y! J u4 K( S7 E+ M7 Hd" O8 u0 n, h/ U8 h, j w& v. X& F
密封垫,; M+ _9 o2 k# e: M7 w
两个平面之. F; B5 }- c- O. n) I
乘客用空气,
" M! }+ b! k; a# q给每位乘客的单个空气供给。供气口装在乘客服务设备% R w- W) t8 u* L
内,个别$ B! }- _$ ]) H4 K$ M6 T0 i
.
5 _. `0 r1 R) S6 L) R) J闸板活门,8 S! B5 f+ E J3 Y0 B+ R2 V
管道中由作动筒操纵的滑动装置。用来关闭和打开管道; O5 h! r' ~& e/ F5 {9 _$ ~
通路。
% o' r4 O* I2 r! V: A英汉对照民用航空词典B OEING
, w% h- Z/ Q% V1 l8 [( XTECHNICAL DICTIONARY 68. ]' F. I0 l" |" M9 k
GATEWAY, A functional unit which connects networks
" |% ]5 \7 _3 @7 q8 Wr systems of different data formats., i8 ]# Y" f) ^
RS., A8 ~: q' s. V S7 v
ENERATOR, A mechanically driven device for+ B4 \) C( |/ F8 J
ENERATOR BREAKER(S) (GB), A device which will- T' j+ o( ]) h& |$ V. } a2 Y
tor from the
9 O" y/ h) z% Wlectrical bus(es) it powers.8 ]0 n n9 d7 g
ent with8 O4 L3 @# ?/ s
o rings pivoted on axes at right angles to each other
) W& @& Z5 a* |$ B- fllowing movement in two directions used in the flap f0 g2 y2 k+ w, t
xtension and retraction system.
" F% {/ W6 S. V% ?! w- W' H& Y接在一起的功能
* y$ j4 W) L$ U2 ]件。' H' y( t8 i5 C1 N# p
o
( u7 V& f- Q& sGEAR DOORS, SEE LANDING GEAR DOO( Z0 _2 X7 Y3 q4 S7 u. Q
G: c& ^" T" f0 R
producing alternating current for airplane electrical
/ I% m3 l: c/ _( esystem.
6 h2 ^9 n& p& u' ?G
9 r; E* a3 \ O3 Pseparate an electrical power genera
/ N/ n; Z. {: ie2 b( G( p" w1 D' W U. n
GIMBAL ASSEMBLY, A mechanical compon
, X* d" ~. q$ U- Utw
6 b9 P. w: a/ _$ h; x- h, Ma
u1 i" m% H3 Q* l# D+ Ce9 z. o! ]' V% m) x/ \; @
闸门,
+ {1 `6 G7 a2 I: r1 P& L/ y一种将数据格式不同的网络或系统联& h5 x9 h, h6 l* m
元) r T8 w0 E' A$ ]# `' a
起落架舱门,
" I& q* | v& s见Landing Gear Doors.
9 u ?, M$ E8 ?& I发电机,, j3 V1 K0 v" p/ i
为飞机电器系统产生交流电的装置。
& E _* b) N+ t" S* T电机跳开关(GB),
, P) e# ^* i. r4 t: C! r- z机与由它供电的汇流条断开的装置。
3 i5 Y0 {8 G8 w7 g襟翼的伸出和收上系统内的具有两个圆环的机械部件。
# I1 b* k5 g0 M! R个圆环的旋转轴相互垂直,以使部件在两个方向都能转) y4 }6 d* ?6 L/ r" w' r
。' C6 k* M, F6 [5 |1 L- M
由机械驱动,
/ q! i- P' W! n发$ X0 G. P8 _+ y/ y: B
能将发电
?* A, B4 A8 B" ?9 ~万向架组件,
8 w% J* t, R; c: v* Z z: |5 L" b两
% ?% S( x" u! _7 b# @动8 o! U; o) f n
英汉对照民用航空词典B OEING% v& G4 Z6 v5 l
TECHNICAL DICTIONARY 69
1 n, C1 s5 V3 { X/ p( G- X4 eGIRT BAR, A rod attached to the escape slide which: i$ t2 V( p# {4 ?* v
engages brackets on the floor for automatic slide, J: }$ n1 ?/ _" t% L
peration when the doors are opened.
1 j5 z7 b. L& `& J1 \" rLOPE (GS), A vertical path defined by a
! p7 _7 r" ^2 D9 f. }ased electronic signal used by an airplane or
% p3 m+ ]1 N( X2 z, ?% z% o7 O0 t$ yLIDE SLOPE/GLIDE PATH INTERCEPT ALTITUDE,
8 ?4 M8 R- x! v5 [- j; P: w) H8 Hhe intersection of the
* {' v$ Q2 B1 _* o, Oublished intercept altitude with Terminal charts by the
) `0 P- P5 G, x9 k4 ltart of the glide slope/path symbol, is the precision FAF;6 d: R4 u; t) R& h- d
owever, when ATC directs a lower altitude, the9 \ ^0 H2 t* g3 J" o d
地- D* H( Y$ P5 A+ C7 j6 \
上之锁钩相齿合,以便滑梯自动工作。
6 ~( q" A) a5 n% [( x滑道(GS),! ~- i% \* ^4 H( R
由进近或着陆期间,飞机或飞行员使用的地面电子信号0 j6 J8 z' C( w8 h* {+ `
垂直下滑航道。
! @ ~; c( J6 Y1 j7 c滑道/下滑航径切人高度,
5 ]/ o9 _2 c* ]0 B7 p! S: j进近时切人下滑道/下滑航径的最低高度。在
, ]. {. T6 _+ Z7 F最后进近定位点。但当空中交通管制指挥一个
6 ~5 J) s$ H9 _0 K低的高度时,由此产生的较低切人位是最后进近定位3 u _+ n! G& ]$ H$ e- B: A
。( H; `8 Y7 |# G: v6 ?& Z4 z
o9 ^. s' B. A; m7 N& U4 H
GLIDE S- ]& z) N, L# {4 c) @" d
ground b
/ }0 J; c1 Q8 V" H$ Rpilot during approach or landing.+ a/ s. b J+ Z$ m
G, {! i1 g$ q6 Z
The minimum altitude to intercept the glide slope/path& B/ Q4 G' q* a- B+ H; ?
on a precision approach. T3 f# y6 T1 Y6 F2 ^9 b
p- T; r) ]! K- y7 n5 M( ]9 ~. j
s
/ m* x0 q+ h- n" \! G! dh% D2 z; b/ ~, m, Z
resultant lower intercept position is then the FAR.6 t- K) B. A9 b
束缚杆,/ K( m' O% ~) M% G
连在逃离滑梯上端的杆子。在机舱门打开时,与机舱
9 c( ~& ~8 T" C$ q9 C! m板4 R2 l6 X, j. a" c0 S( }
下, `, y+ _6 ~) R+ X
确立的一条
6 o9 p1 I7 U: {0 H' {! C3 P6 A下4 l5 }& f" D& ?
在精密
. \. i$ y2 V2 a% }2 S) E& }Jeppesen机场图上公布的切人高度与下滑道头的交接
1 j# `: B% v' Y. Y点。是精密3 |# P- r2 [: i8 w4 l
较
5 G! U, e8 f/ k, I0 \. R; \点) w, F& {' F) A* p% I4 u' Y2 U
英汉对照民用航空词典B OEING* s# q+ f9 ?* h6 J2 z& g
TECHNICAL DICTIONARY 70& l1 F5 C k$ M7 \
GLOBAL POSITIONING SYSTEM (GPS) (No. 1), A; p) I+ P' F, |! u# M
pace-based radio positioning, navigation, and; C8 u( b8 g8 C
metransfer system being developed by U.S.A.
4 M5 b* _- N$ W2 T& ?5 z% bepartment of Defense. The system provides highly
6 w; \* b" t' O" }: Q! C* Q8 [recise
; T$ c- l2 T. f1 t% K% P% r2 Ond provides a worldwide
! K4 [8 i; ~8 P! f0 V8 `& x& [ommon grid reference system. The GPS concept is
+ ?& H1 I: ]7 a+ y% {; F# R; lredicated upon accurate and continuous knowledge of" s% }! i& y8 v1 g( y
e spatial position of each satellite in the system with, g& t9 _$ }. G: W' ~
spect to time and distance from a transmitting satellite
: R& B. f4 j) j e# A: m, Athe user. The GPS receiver automatically selects! r; X" U6 t w' P( i
ppropriate signals from the satellite in view and0 R) e* }6 ^5 ]/ F! C h
anslates these into a three-dimensional position,
) t8 j% Q5 l) V- F: ]elocity, and time.
! N3 e; j( k- W- ~3 |LOBAL POSITIONING SYSTEM (GPS) (No. 2), A/ i% D% {0 s( S* M& }
ngrange navigation system that takes navigation input+ ]" C: E+ P* @4 p$ w
om transmissions generated by a series of satellites in: q- S. K. W: }3 U( z; A
LOBAL NAVIGATION SATELLITE SYSTEMS (GNSS),
- f& U' S+ U9 C3 |7 m- _ k9 `2 rternational Civil; O5 f- G& G+ `' U
viation Organization (ICAO) to encompass any4 `' \8 L. r' x- p* _4 R
dependent satellite navigation system used by a pilot
8 X( C4 W/ q4 G' b6 j0 ?perform onboard position determinations from the' c9 Y9 B# `4 v2 l
O-AROUND (GA), Airplane maneuver where the pilot is" ^0 @* [# [& m5 b4 e5 Q) V
in the final approach phase of flight and decides not to0 U c) X0 I B: U# Q0 ^+ Y7 M
land. Thrust is applied and the landing gear retracted so2 [! Y9 k/ E/ Q8 [7 F
as to climb the airplane to a safe altitude.
5 e; e; J- A. O: f# h+ UGO-AROUND THRUST, Maximum engine thrust to be. Y8 o5 T& w( d1 l- z
used during the Go-Around Maneuver.8 C: E3 e8 v7 \
统(GPS)(NO.1),, x+ T. g8 O: P) F# j* N! E2 ]: k. z
电定位,导航,和时间转移
/ t0 ]* s3 @0 t+ X统。该系统在全球连接的基础上,给无数备有适当设备
- r- t% N Y& ]' ~2 a# `户提供高度准确的位置、速度、和精密时间信息。该系' z/ X2 u) t3 n1 Z
响,并提供世界通用性座标系统。全球定& [5 j0 P4 f, J6 [3 w% u
信息之原. f# |% B% L& P4 H2 }, Z7 L$ n0 y
为基础。全球定位系统自动从所见卫星选择合适信号,3 ?7 X9 A$ r' U4 c
并将这些信号转译成三维空间位置、速率、和时间。
7 p* ?( o4 g, \* H全球定位系统(GPS)(NO.),
, b4 ^8 D/ D' L8 q. f4 Z一种使用一系列同步卫星所发射的信号作为导航输人
- B7 m' _; w/ i/ N长距离导航系统。
# D1 k, g2 l' X6 B, a- X6 I球导航卫星系统(GNSS),, G/ m! f0 b. n7 _0 O* I$ @9 ~0 W
航组织采用的“伞形”术语。它包括飞行员
6 m0 B8 W& I3 S: i, C料做位置判断而使用的任何独立卫$ {- q* h' C" G4 F4 f5 K% f/ w
导航系统。+ u1 J: Q9 _: Q7 e& Q, {1 U4 F
复飞(GA),
. z7 q7 m" E7 `& H! A飞行员在最后进近阶段,决定不落地而做的机动动作。! u, G6 D% Z b: _4 @# p6 o6 b
复飞时需加油门,收起落架,以使飞机爬升至安全高度。
@1 R- Y4 }! O4 Y. q$ G! v! y, Z0 F复飞推力,5 K- D% F: x" Z5 s% T
飞机复飞期间使用的最大发动机推力。 D8 _# b% x' ? j. |
s2 b! o8 ?# j: `% C% u1 O) M; S
ti% \" v+ `9 C% z
D
1 g. _. f3 \, |0 n ]9 W" p% Vaccurate position and velocity information, and p
% K% N' ~1 C. z$ utime, on a continuous global basis, to an unlimited
& W- A+ M" ^; K9 s% y7 i# Pnumber of properly equipped users. The system is
* z- R' G: ^; }9 C& Iunaffected by weather, a8 T5 u$ P( }5 V, d) }5 B3 o1 L ?
c
% F% ^& ^ M( y+ ip7 w5 P' ?: Z& ?. _, _% f) p
th
2 w* r. ^ R& {7 u. h/ Mre
: [: b* b8 `) i: M# Cto
) r" \- X) Q5 u0 C8 V3 X0 z8 aa
% s8 T0 k' d) P# D# l; Ntr1 S" V/ A- f( u3 Q
v
5 y( P7 G }1 h. p) VG
6 S& |0 c& |/ c! `" Y( V' wlo( q2 `! E0 e' Q/ {6 e, R7 X/ w
fr
& j, v% p+ v! Lsynchronous orbit.
w; f- u+ z2 s/ B6 m, d" w" @G2 C2 B7 r- _/ `: r& M% @# ?
An "umbrella" term adopted by the In
4 k( c( Z8 x8 ]# H# SA6 r- r. X2 z1 k& n0 ?% }: h
in
* l$ A, I0 P4 {to
5 C4 r2 O$ L$ }6 @ Lsatellite data.4 K+ d; Y4 ]( w H+ t
全球定位系
' d! \4 @, ^& W4 M1 A由美国国防部研制的空间无线- i- f% n3 i+ A# F4 T
系, v0 F( e& N# a' [; ~
用
5 D+ z, c) i/ G7 w: E; O- K统不受天气的影
- c2 ` K* V0 [! w+ @位系统概念以系统中每个卫星具备相对于发射卫星与用
4 T! z* o; Q# @' [3 T户之间的时间和距离的准确且连续的空间位置6 f6 Z! q1 \7 e) u, P& o& o# W& p
则
! F w- T8 z- L7 O: l2
8 `" d; p6 V6 {1 ?, B的
3 M- Y, y9 F6 a- ^& ~2 N* }全6 |' C5 R* P3 }+ l3 M# z
是国际民
0 g+ j1 a `% `在飞行中根据卫星资3 ?1 \3 V1 K5 B$ W
星) x% p8 n& ]6 L. {5 z
英汉对照民用航空词典B OEING) B5 u$ r: V5 x; q% D: T+ ~" [1 {
TECHNICAL DICTIONARY 71
( [1 m" K, {8 a- IGRADIENT, The ratio of height gained or lost in a given s6 O& J8 A9 F, \" `/ L
distance to the distance travelled.
( Q1 d9 y2 a3 I; p0 }& J9 {4 ~9 vrbon6 W! \# j* a$ ~$ m4 M. ^
r access panels, landing gear doors and flight
; x& U ^: ?8 |) w# @& B# yontrols.' P/ A- B5 g, K" X' R
IRCLE ROUTE, Is the shortest distance
! v; p5 O9 ?4 a/ U/ K2 zetween two points on the earth's surface. It is the line
3 R, n* s& a( Jrmed by the surface of the earth on a plane that
# N6 Z* m6 K) @: j& @! e, e' _asses thru the center of the earth, the departure point,9 b( F2 ^7 d$ G
t line
9 n6 v4 m& W/ q2 D2 ]! Oal Conic Projection
; U% e; M6 r ?3 G& x3 F b, gpproximates a great circle route.
0 Y# \' @- L; ^8 h/ T7 ^GROSS WEIGHT (GW), Total weight of the entire5 Z$ D/ A6 t6 o9 b( P
airplane, fuel, oil, cargo, passenger, etc.
' }* y# O3 Y- x- zGROUND, A part of an electrical circuit or system that
; w# {, `9 z4 S- F7 [has zero voltage.
* h" Y- ]" j5 |0 a' }GROUND FAULT (NO. 1), System fault that has7 f, F$ o" O' A* M Z2 p3 j4 h# \: f
occurred since airplane landing.
! A0 N# [0 n* h9 v R5 V7 b轻的材料。用以制造舱口) e8 Z4 }/ j$ ]0 k
,起落架舱门和飞行操纵面。
: R+ }6 c! _6 W! u& Z圆弧航线,
- x0 Y, Z% C+ }0 ]1 u D% S$ o地球表面两点之间的最短距离是以地球中心为圆心,在1 I& e% G9 }: x8 O0 P. Q8 N
飞点和着陆点间所形成的弧线。由大圆弧航线形成的真5 j8 s b$ ?# {/ e8 S" }
迹不断改变。在兰伯特等角曲线投影上画的直线接近大 ?9 g3 I7 Q! e2 e" B
全重(GW),9 |; b/ X! \9 a7 N- V: T; h2 ~
整架飞机的重量。包括飞机,燃油,滑油,货物,和乘+ L' j: D5 I4 V
客等等在内。1 Q6 k- ^$ T r8 V" F9 ~
地线,
; _4 a& l" ?3 x5 y9 k在电路或电气系统中,具有零电压的部份。$ q) I8 C" X' L# E; G& J( y* X! M' L7 a( l
地面故障(NO.1),
' ?. t3 |- @3 J+ H' _3 s& n" \自飞机着陆后所发生的系统故障。
/ i' c; o( }" q6 OGRAPHITE, A strong, light material made from ca
/ ? ~- \6 ^: l3 w0 Q5 f5 X, Tfo
. M9 Z! g) l% P+ V' H: @% @c
. ]$ Z& c: n9 y$ J; E* Z: v, YGREAT C
5 M1 z: k! S3 v8 ^* t( {% `0 t8 J. d9 gb( f4 ^; C- A' d( U# n" k
fo
' l& Z8 P; O: v P: z1 [) dp/ W! n) L# W- X" o1 U4 p F
and the destination location. The true course formed by
5 V. p* V7 W }$ Z' J" da great circle route constantly changes. A straigh! k9 d$ }8 ]- l% W4 y
drawn on a Lambert Conform
# p; E7 S, `: T3 l( Da
% X5 c4 P1 X; ?GROSS PERFORMANCE, Actual or measured
G9 W# x) y: J: u7 ]3 Qperformance of the airplane.5 D. [; e7 s$ J+ P$ v" F
梯度,; p! { |7 y+ o4 L0 ^
在给定的距离内,获得或失去的高度与所经过的距离之
# v0 |, w' v$ \比。
5 `/ i! E t8 g/ D, K) }8 J E/ P' }石墨,) ~! O6 K' _+ Z/ W+ D* }& `
一种由碳纤维所制成的强而
1 t! H) J8 A' y盖
( H K3 @' W, b; G$ n0 [大1 z3 F4 V3 m7 \! z
起1 w& J( V4 N7 q2 `1 \! w
航2 T4 V. B+ ^4 F* k
圆弧航线。% b8 `* B4 ~4 S& D
总性能," s; J" b) k7 c. _, m8 O" b( p
飞机实际的或量得的性能。
" _6 \" `7 b! s* g; v9 D. B英汉对照民用航空词典B OEING
* `% j) n" m! n5 M8 _" yTECHNICAL DICTIONARY 725 f& d7 ]! y5 a$ l: s) ]
GROUND FAULT ( NO. 2), Loss of a ground connection. I* w! W5 Y& M" E6 G" g! @
or a short-circuit to ground., Z/ k6 f! C+ _
GROUND SPEED (GS), The speed of an aircraft
% D$ e i: o& P6 F! o& Wlative to the surface of the earth.
; o; F: z: |2 |ROUND SPOILER, SEE SPOILER
2 [% h9 G$ S5 m* GROUND SUPPORT EQUIPMENT (GSE), Equipment
, n" A4 l- `0 _; m0 ^sed to service, test, move, power, or repair an airplane
% `1 G+ u4 p0 N; C) O2 @2 Khile it is on the ground. B/ d/ P9 C9 \* j( b
ROUNDING POINT (TERMINAL), An electrical4 h7 J5 x# P# c
onnection on the landing gear doors for electrically$ Q6 x0 S1 d/ f0 _
rounding the airplane. An electrical connection near6 F; a- E" ?; w$ g9 H6 p
e fueling station for electrically grounding the fueling6 R0 ~) E: s$ V6 r# y, M
ase.' O$ v( r: e6 k9 u, h
S, SEE - GROUND SPEED
. B: A" I% X5 h2 g3 I4 DSE, SEE - GROUND SUPPORT EQUIPMENT
* [% s7 f$ Y6 H! x! }2 w" @NO.2)," {, H8 y% B2 E! y
地速(GS),
9 n. W- t. \% D# b; h飞机相对于地球表面的速度。
, l$ r8 I; q. [2 r9 b- D地面扰流板,
$ D9 U7 `8 w( }7 l2 \8 e2 ]5 A见Spoiler& L+ k5 Y' A) c
re
, I8 {' u0 [" C$ r! h. Y$ }% nG$ J% G# u7 M" U; i2 \) A! W0 {* k
G7 `# [1 `( B" [) v* b; D3 W! m
u! Q- g! _* h: I# P1 }
w
7 v- ^0 Q! U( i- [- P& h; vG
9 Q/ g" ^! K+ y3 T. {$ a/ ~c$ S J( i/ i1 Z8 u' |, w2 o
g, R9 I+ T+ P: P! _' j8 G1 f$ \+ ^. @
th
' Q, e8 I3 N9 n, o2 A: d7 D, \+ J1 {b
0 u0 l5 O1 B. \: g8 XG" W7 c7 v1 O9 W5 z' e. W! Z: Q
G
, X8 ^' M6 P+ q" J: Z! V$ qGUARDED SWITCH, A switch that is protected against& I) p0 P: C$ `
accidental movement by having a cover installed
1 d O# h p4 v8 f% bdirectly over it.' J" ]% d7 M( d7 w h
地线故障(
, G+ w- q# }3 O3 z# g地线脱断或某线路因短路接地。
3 Q3 Y7 _' n% U.
# l2 h! I4 I, b地面保障设备(GSE),
F) T& t, ?$ y# v. I/ \4 \7 B" \当飞机在地面时,用于勤务,测试,搬移,动力,3 U; M2 W, C/ h2 ~
或维修用的设备。/ }, @ D+ O( r' N
接地点(接头),
5 b4 C1 x9 V% m# z是在起落架舱门上的一个使飞机电接地的电接头是在
& W: P+ I% L4 ]$ K& }: ^& q C加油口附近,使加油车或地下油库电接地的电接头。
8 K5 o8 U4 F- C! u+ }& H速(GS),
3 G. {) d" Z1 _1 [# n! Y) _eed$ B( r0 G) N; r/ Q
供应
" g D. L; s" H( c。
4 {" B" _6 ^3 K7 V" C地1 g# A' g* J, ~5 F: Y6 S! W: Z1 z
见Ground Sp .
* X0 m! x& ]3 ]4 J: |; ]面保障设备(GSE),
; v( C" A. }8 N; @8 Z' N见Ground Support Equipment
! E T2 p- _ u/ E1 r. o8 J地) a) @' j; u9 G! [& @; Y) `7 p
.
' P. A1 B# }) Z4 Y2 A0 O5 s带保护罩的开关,
: j S/ q5 Z$ T% i$ d3 u为防止意外拨动而直接装有罩盖的开关。
" K/ {! r. y( L- ~2 _& }1 F9 K英汉对照民用航空词典B OEING4 {# ?+ j: P+ y) G9 m4 d8 F
TECHNICAL DICTIONARY 73
$ V1 ^, B% w o3 }+ r JGW, SEE - GROSS WEIGHT; y2 }, k7 S6 a' e8 ]
H
5 _1 D) F3 q* J% @3 jHAIRLINE CRACK, A serious defect in structure; a
( c2 C. |3 _8 U) W# B4 ^) vcrack that shows as a very thin line.
6 Z8 R& [0 P n1 l% N4 QHARD-OVER, A maximum pitch or roll maneuver.
2 H% r: e* i2 i2 \HDG HOLD, SEE - HEADING HOLD
# k$ `- A U, A- _; ZEAD END, In a hydraulic actuator, reference to the
% D1 L7 w9 E5 p) sart on the piston side of the actuator.
; ]! E# x7 Q) U( j& g7 R9 gHDG SEL, SEE - HEADING SELECT
0 D. s: Y" ^- E* U8 UH* p# w: U: U5 y# K$ z
p3 A L! M7 {8 t* B' x# I
HEADING, The direction an airplane is pointed
2 n( i- c% X& o$ l. N6 oreferenced to true north or magnetic north.
8 C! B8 O( z1 |7 ~ z8 { G全重(GW),
& g9 S% V9 T' ]9 u& s. G见Gross Weight.
/ B4 W) I! T' Y! u$ m细缝裂纹,
4 R: R" D6 V6 _4 v1 N# N5 k6 l结构内的严重缺陷;裂纹的外观是一条很细的线。: {: [+ {8 h% Y. ^
急偏,
4 W1 x8 ^* D: y' ?最大俯仰或横侧操纵。3 H, X: r$ V5 c* x, f, A; z9 v
向保持,
3 f8 a) I: M0 Q+ g$ L7 p, V见Heading Hold; U: W( x0 r7 U3 y
航! G o! I5 c! V$ ?$ @0 s$ O
.2 _7 w( c, \/ v" s. \7 @
航向选择;0 W! n& x2 O& r
见Heading Select.6 a0 T, g5 A( E) d! i
顶端,
) K) w1 Z g. W! i6 B }液压作动筒中与活塞相邻的。
5 T$ e1 U; H0 V) h, C相对于真北或磁北的飞机指向。
+ |2 L! M& ^9 B- }# c+ _航向, h) ^. p2 M1 q: O" q3 p# \3 Y9 h
英汉对照民用航空词典B OEING
& ^& h/ Y, Q0 G; ?- M4 b. J$ \! @TECHNICAL DICTIONARY 74
' y9 O( ^' f6 l0 I& C) }9 i% `HEADING HOLD (HDG HOLD), A mode of the autopilot
6 r1 i- q% z t6 f( h' nirplane heading.
2 X1 L- h/ j# E2 J: ^! ct1 c/ ^7 ]: ]* X! o- n
e
8 e% c/ }, B' F: _om
3 ]* `2 ?( A% X- Qg or8 @( i* _, n% r* [9 M3 `2 M) ~7 r, [# L
(HDG HOLD),
6 H# R7 }$ C k8 |0 K$ R(HDG SEL),* @/ f2 K( F; ~
交换器,
) Z' w' m6 N6 K0 U( L有很多通道的金属组件,气体在通道里流过时,一股气+ ~9 v+ M0 `" a* x' }7 T
可被另一股气流冷却或加热。0 D% N$ F$ I: |" u2 T
system that maintains the existing a
. q O; t0 L8 M9 cHEADING SELECT (HDG SEL), A mode of the autopilo; a. @5 [! D( `# K M# `( }
system where the pilot selects the desired airplan
& Y* t* r( P% [, M5 ?+ W" _. sheading.& _, g) N K, Z" L& q
HEADWIND, Wind or component of wind coming fr
& W8 l2 _& {/ h& E6 k% r( gthe direction of airplane travel.* z; V& ^7 v$ R. V
HEAT EXCHANGER, A metal component with many7 {( N5 e9 f6 p9 F
passages through which a fluid can flow for coolin
1 G8 G( v1 `0 n# r2 @+ V% c+ a* _heating one by another.
* D* c, d, C( _8 r航向保持3 {5 M$ h& x7 E" c; {' P8 K
自动驾驶系统保持现在航向的方式。( Z* Q# X- ~. _4 l+ _& d
航向选择
) \) i$ E2 a2 O# w' G' W自动驾驶系统由飞行员选择航向的方式。
% p2 ^, m+ E9 A) {8 J9 l8 p2 o( Z顶风,: ~3 b( U( r# I0 l3 ], l' X
来自飞机前方的风或风的分量。% ^ d/ ~* K( R& [$ M' v
热
& P* J" c; h! ?) V- N流
; \6 [& X% s5 T c; M英汉对照民用航空词典B OEING
1 K3 ?! }2 @" g; J+ M. v) RTECHNICAL DICTIONARY 75: d6 e. V$ |! B8 Y- W* V9 S$ u
HEIGHT ABOVE AIRPORT (HAA), Is the parenthetical
% E7 h. P- o. V5 I9 o, Hfigure following MDA which, when added to the airport6 X( k! v! \/ R1 z* X
levation, will give the MDA in feet above mean sea
$ e7 j( O) q6 \9 s2 Evel. A HAA will follow a DA or DH only when there is
; x- R7 [5 i. S7 K K3 \o touchdown zone, runway end, or threshold elevation7 w- W6 q, i4 b, C
), IS the( X! Z `; V! T8 V
arenthetical figure following DH, DA or MDA which,4 }2 X$ Q6 }1 P: u
hen added to the touchdown zone, runway end, or* U9 H! ?0 }/ W: H
reshold elevation, will give the DH, DA or MDA in feet4 R$ a7 M/ D- z0 d$ k( w' B
cy of one million cycles per second.. O P" R1 [* c/ V
EXADECIMAL NUMBERING SYSTEM, A numbering
5 z3 e& ]6 c* ?8 \6 X- Dystem with sixteen as the base. The system includes# z8 n$ v) E; Q& P
igits zero through nine, and letters A through F
! G5 K+ h4 F& hpresenting the numbers ten through fifteen.
8 X- a1 {) |" oIGH FREQUENCY (HF), The frequency band between' n2 J2 [' O' y$ K1 ]' w$ ]6 C
场标高相加后即是( r @6 Y( }0 e/ s }
DA高于平均海平面的英尺数。只有当接地区跑道顶端或
8 F. M) C' P8 t) k, K道头标高不可得时,机场上空高度才跟着决断高度(DA1 y) R( H# l2 s$ r
DH).
/ B% t' J1 }. EHAT),: k. E7 p+ r- j
最低下降高度后括号中的数值。它与接地
/ d, Q7 z0 }2 U& r) E, {) b、跑道顶端、或跑道头标高相加后即是决断高度(DA,
6 y5 v! D9 ?) e9 `0 }0 qH)或最低下降高度(MDA)高于平均海平面英尺数。% M' w% k) B/ b& Z- b- a# A
的最低天气条件同时公布的。
/ m' W! h$ S2 I7 M- y d率。+ N2 @' u6 u; H% `( N
一种以16为底数的编号系统。该系统包括由数字0至
+ I* {" L! z! l,字母A至F代表10至15.0 t" X/ X1 X8 F' a5 x& q3 v! j
频(HF),2 C3 `" b D+ B" [0 l% ^% O
赫之间。* N7 W n" q7 ^% s: R( {& D3 A
e
5 _4 S0 k( U; i( sle% \/ ?2 \4 k; c& C/ V, ]) _% Q
n
/ E1 y' K: m' ^) Wavailable.
7 q2 f% w8 x8 d- JHEIGHT ABOVE TOUCHDOWN (HAT M5 \ E* h/ U* [/ H/ V& B
p; g0 ^& n- g8 x" P
w
4 h1 I$ e( h) `( uth
1 ?3 w( u! i; ?% a4 Q! w, Vabove mean sea level. HAT is published in conjunction! |4 O- K+ b- u% M% n5 |+ O- G' e* J
with straight-in minimums.
. A6 W# Z9 t! {7 IHERTZ (Hz), The standard radio equivalent of
, k d' Q4 u3 R3 c3 z, Tfrequency in cycles per second of an electromagnetic
7 Y R2 O H7 j- rwave. One Kilohertz (kHz) is a frequency of one; H/ ]5 ]7 }: n" S
thousand cycles per second. One Megahertz (MHz) is a
, H. G5 g1 h4 K$ W" Wfrequen" ?5 T* ]8 `% K2 |) Y" U3 t$ M
H
" |, u2 x& n$ j3 ~8 ds
6 K0 z" i& {" ]5 B: yd
3 i' r0 n* Y" R8 x( dre
% N W3 B; |/ ~7 p$ q. U; x8 lH2 G5 r2 W5 h0 i0 s! C
3 and 30 MHz.
/ X- o' C* K$ d9 l1 u( K, M机场上空高度(HAA),
0 a# k- \9 X/ Q# q. g. e是MDA后括号内的数值,它与机
) i8 E- @' V9 B( iM
+ L+ Z2 u( {) a跑$ {+ N4 r" Z% q) P& [5 t
或
% G8 c" E! b( J3 h6 a离接地点高度(* |$ v+ a* c& u: W6 m( r8 j+ Y6 K
决断高度或
. w+ R8 u6 R, c) @' ?& {4 D区% e, @& f% q- {8 F9 f8 \8 u t8 m
D
8 \ v& w) v3 P接地高度是与直接进场着陆' c* {, \ k5 D r7 s
赫兹(HZ),
& x. z; |1 i4 y; x. W# q( l9 \单位是周期/秒的电磁波频率的标准射电当量。一千赫
" r4 z0 E3 p& q k7 ~& E/ ^3 r兹是每秒一千周期的频率。一兆赫是每秒一百万周期的2 E! ~7 J$ J. s* G
频
. r1 y/ J8 Z4 p/ `. w7 {十六进制编号系统,2 S% `; f( H+ `* D( Z+ \! f
9
" U+ F/ [" @) x" V/ m% g高
9 q$ J$ b; y5 A% ~$ T: {频率带在3至30兆
0 i: ?9 C! @: u英汉对照民用航空词典B OEING
3 B+ D/ x" i5 C) d! iTECHNICAL DICTIONARY 761 k. n. M: Z0 h! k( p8 {7 i8 {
HIGH SPEED TAXIWAY/EXIT/TURNOFF (HST), A long9 Y: t4 v' M. S& `
dius taxiway designed and provided with lighting or
: I$ H) L, F: l4 aarking to define the path of aircraft, traveling at high) Y) T ^0 C0 o$ |, E# q! a( s6 @- P
p to 60 knots), from the runway center to a. {: e- Y: b% B
the center of a taxiway. Also referred to as long
* W" O1 w0 e: G |9 Tit or turnoff taxiway. The high speed taxiway is
+ C4 j2 T, W! G# Y R& h0 mfter
) S" M. o: @" @: B7 d3 b, qancy time.
& u6 o0 I1 b3 F% g" u0 pr a
/ i3 v7 [ _5 Zeavy component during removal and installation on the0 l. m C+ e1 g2 c
irplane.
9 I- B4 h* T+ q% i/ p1 `OLDING, Airplane maneuver to keep the airplane from1 k' a) |' ?! G8 M0 e7 k
rogressing along the intended route of flight.
# I9 f2 R$ B0 V. M" E7 ?& ZOLDING PATTERN, The predetermined maneuver. B% u. A# f( }5 @ g N4 }
c control.
0 Y4 r, }" C+ R" ROLD/HOLDING PROCEDURE, A predetermined
8 q( ?! _9 J- F) j4 F; vaneuver which keeps aircraft within a specified
% }& i- h5 w! G0 @irspace while awaiting further clearance from air traffic
2 Q; y W) H5 f& Fontrol. Also used during ground operations to keep+ V* ?4 }0 N- n; H1 p
ircraft within a specified area or at a specified point
- ^. }3 M3 U T$ F+ Z3 Ghile awaiting further clearance from air traffic control.8 b2 N* E( L0 d& P
he standard holding time is one minute at or below% R0 R& h g' M* _( @, t/ E$ U
4,000 feet or FL 140 and 1 1/2 minutes above. The
9 i3 V. N9 r v: z1 V( Yeparation between 1 and 1 1/2 minutes is FL 200 in+ y7 ]7 Z; q9 B1 T$ S
(HST),
% F; i; t* f/ G: _9 ~2 M& a道。该滑行道有灯光和标志表明飞
/ W* v1 Q; p4 d从跑道中心到滑行道中心一点高速(可大到60海里)通
, k1 U7 L# ]6 ]) C$ B) Q9 {6 Y' M( l的路径。也被称为大半径出口或脱离道。高速滑行道的- O L4 d9 ?& C3 o1 P
计意图是加速飞机着陆后脱离跑道,从而减少跑道占用
& F% S2 \8 K$ Q: h时间。
* E5 z t2 q5 R& L! \; a安装过程中,用于放下或抬起
# J: i) p- v" ^ `动机或重部件的装置。+ t: d, ]0 P( J! J& r
待,& y% b0 V* N, Q# [. S- n
使飞机不按预定航线继续飞行的机动动作。
$ u# b, B3 S8 D) l y. i( k待航线,' I8 l% x% V! H% ? C/ f: {& C$ P! d
处于指定空域内等待空中交通管制下一步调度; }$ R0 n) G# a7 O u4 Q# A
等待程序,
2 y" [2 a0 u! x保持飞机在指定空域等待空中交通指挥的下一步许可
# B8 M6 J V( _9 L5 z的预定机动动作。也用在地面操纵来保持飞机在指定的地
0 t) V: i- U O( \* p区内,或在指定点等待空中交通指挥的下一步许可。标准4 S! k5 E/ X8 a5 a0 ^
的等待时间是在14,000英尺或高度层40以下时1分钟,
/ t- d' |4 G- ^9 a* e以上为1分半钟。有些国家以飞行高度层200作1分钟和
8 m" ^4 W& z; F/ x0 _* G1分半钟的划分。
# G$ P9 L; ?' h: Y/ c7 [" t% g8 wra0 z& R8 T ~7 r$ Z a9 l% |
m
) i* b1 e3 T g2 fspeed (u3 B7 W: z# c3 L M; C6 T5 r1 t/ K
point on
: d$ J" s4 K, H3 J/ a& a sradius ex
z1 r f1 L S; {% k7 edesigned to expedite aircraft turning off the runway a
2 H0 ?4 I& C. ?" C) j) O+ planding, thus reducing runway occup6 u- N$ @7 B+ G# l' |
HOIST, A device for lowering and lifting an engine o" U2 a$ d( g/ I$ o& ~
h
6 U$ z8 j7 o1 i1 p5 q- M: da
7 d- F. h9 Q& v0 iH
z( }, H" z' B; Zp: M. N3 p4 Q0 Q( u- j: x& _/ N
H
& H, c# G- \) _( swhich keeps aircraft within a specified air space while
- ]& y2 u3 s, [" P3 bawaiting further clearance from air traffi
' [1 V2 s, V2 E8 j+ d/ PH0 |0 y7 }- j$ w, F5 ^
m. ]* h5 v# o. q. b/ I
a; P r# b7 S$ x- ?
c* r+ C& m) p, v2 u9 m
a$ F$ ]& V. W2 p1 V7 f
w' f x- [- n( q D7 U
T
! O2 F5 }/ d |, T2 c: H19 F% U6 L2 ^3 w. n/ t: I1 x8 a
s% v X' p8 B) o5 ^, s; p' l
some countries.
+ E* t# g- B- G5 F高速滑行道/出口2 K% o* h" c4 q: Q+ ?
是一条半径大的滑行
+ R0 W$ x" J4 }! D N机& w' D$ _: t" M) @! L' ]. k% G
过: n0 r+ }- {+ L2 j; [
设( o# ]% O- w* F# {
的
. o0 c+ O7 A5 n! u7 d, s吊车,' h4 i: v/ ]. P$ H$ R7 c
在发动机或重部件拆卸和
& _) w7 |- R$ J发
0 ?3 L, e" d' q( N, |: ?, I* ~等
0 Z2 L7 V+ r/ s8 _ }等
, p4 p1 N$ D- Y$ ?4 m9 |, V使飞机0 _: k, X m0 G0 j1 A- C
的预定机动动作。
4 w Z) Y2 W4 y5 s# K4 I1
5 r- v2 `' {1 s' t" w* F英汉对照民用航空词典B OEING
}; c: @$ E$ B# A+ ]# @' n2 yTECHNICAL DICTIONARY 77
4 ^" Q! M# w, z1 T/ O' ]% C# ^9 iHOLDING FIX, A specified fix identifiable to a pilot by8 d; P1 m3 K# }* K( t' Y& [
NAVAIDs or visual reference to the ground used as a
; x9 _2 Y9 G% c( m" I) V9 z5 [ lference point in establishing and maintaining the w( L$ ^" F0 n. }; L# [% c
osition of an aircraft while holding.7 B8 k+ S4 W! K4 I: S T
OMB, A hexagonal material made of metal or
# j& @" ]; p( M4 H. h& G1 c- momex for sandwich construction of panels.8 B7 a3 l, M: B9 c+ t8 P" W6 Z
HORIZONTAL STABILIZER, The moveable horizontal: p4 ?) v# l8 Q/ s' P
surface of the empennage used for pitch trim.
: t4 n' X z9 M' {! g' n2 lHOT BATTERY BUS, A battery bus which is not
9 o4 J- a3 s) c2 e6 j( iswitched and is always energized from the airplane
0 _2 Z- |4 P! u3 ~7 k! G' Z* Ebattery.* d( L) | V- C( F9 Q9 G
使用的一个指定" f o$ z, d" o: n: } I v
位点。飞行员可根据导航台或地面目机参考识别该定位
k; N8 K3 V1 P! c$ R$ `) ]。
" k$ [" c% w& m5 s5 Y窝,
; }. e ]& @3 _; ]+ v一种用金属或Nomex制成的六角形材料,用以制造夹芯% j; M" v* A+ l
板。
; f8 i* J: ~4 \3 C3 c# p. y, O水平安定面,; X, }9 J- B2 \3 H3 G5 `/ T1 T, I
飞机尾翼的可动水平面,用来控制俯仰配平。2 L, q" T' j4 t, x5 X6 k# f: e
热电瓶汇流条,2 c2 _5 L& s! L' {* Z* n: d
无电门控制的电瓶汇流条,始终由飞机电瓶供电。
p0 r$ A" @3 I/ A7 g# n0 z, d5 bre
+ v7 L) H7 c2 I) e/ U) t5 ap$ ?0 i0 p1 W! N* ]& ]& P+ ` `' x
HONEYC7 C; s' w6 P3 }2 F2 d
N
K P$ k, a1 B等待定位点,
, l6 S' ~+ g! i/ v8 D0 y! d等待过程中在建立并保持飞机位置时9 M) N% z) c2 L& C1 z
定
2 K2 [# i' v% ~3 h s点
: a$ C- D9 {* Z% }/ W5 E* Z& |蜂6 o3 k7 M, c9 H) e
面
R! V$ r# h" ?' T! P2 }8 g! }英汉对照民用航空词典B OEING
5 H/ z/ M+ s, x% N1 tTECHNICAL DICTIONARY 780 |" u. I4 { r T% {8 t. I0 s- I
HUB CAP, An external covering to the axle of the main
0 ~+ `3 D. `' U6 H1 V" y; g% Glanding gear wheels.1 t/ O$ c, Z# M+ J+ G
HYDRAULIC FUSE, A device in the hydraulic system
* Z! Q$ [1 K- A3 P. z0 V/ ir stopping fluid flow when a leakage occurs in a line/ A) ~: H/ \- [
ownstream of the fuse.
: P' b: b) t _3 z- s2 A( yS, SEE - INDICATED AIRSPEED
/ Z" k) F& _! S5 J+ YER PLUG), An electrical device for
* s0 p' Z8 G# j! cproducing a spark in the combustion chamber.
4 X# h6 V: t( z( y压保险,
( m A" L% \0 }: a; n* T液压系统内的一种装置。用于在保险的下游管线上发生+ T8 H4 }) B) a( n7 R5 j3 L
漏时,阻止液压油流动。& ` [' s6 w/ E; h) {! E# p) p4 F
示空速," j! f( k3 B( D3 `, M6 G
见Indicated Airspeed% k; |+ I" [. P* j, x L& G
fo
, _8 p( |9 f( d. K% y( }d
1 Z& ?0 o* q. ~( eI IA
0 Y6 H' e9 Q; L9 W/ i4 L8 _IGNITER (IGNIT
. B( C& x. p9 W4 c* l1 b* L轮榖帽,
4 X: @! z' Z- m4 R) J- j主起落架轮轴的外罩。
- B# [/ i; c/ l# R! n8 o液( T* J$ J& J; s8 G7 i5 B
泄
B- k6 H8 X/ |( f Z指3 L( Y" n0 O% l, r, Y
.
. ^1 ~1 ~. y& j9 I2 Q$ ]' k3 g在燃烧室内产生火花的电器。, J% c& o2 E# w( e8 d9 a
点火器(火花塞),5 X( M* t0 \$ F5 n; E
英汉对照民用航空词典B OEING8 `$ T( k/ i. X/ k4 h1 e$ n
TECHNICAL DICTIONARY 79
. j, u1 g+ ?) H' j1 q6 `IGNITION EXCITER, An electrical component for
/ M) `; Z u9 b) ^supplying high voltage to the igniters for producing a7 j/ U3 u- \% t/ z; A9 a0 Z
spark.- \- W* l+ M/ f8 b3 X d4 Q
IGNITION SYSTEM, A system for starting or continuing
4 ?6 N) C9 ~6 ^3 E, p( `combustion of the fuel-air mixture in the engine
; S% d& Q0 e* q" u) hcombustion chamber.: O$ X3 N- ^$ \$ g0 y( J2 D( x
S, SEE - INSTRUMENT LANDING SYSTEM
5 u3 h+ E2 J9 {* nPROVED CLIMB PERFORMANCE, The rotation and$ C* e6 t! |: |: z9 R7 ~4 W, |
limbout speed increased above normal to increase: d. _3 f8 Q) U) O! r
DICATED AIRSPEED (IAS), The airspeed read) W k" a0 W; k4 B; [9 z
火系统,, m2 C9 M4 t% G! H6 `
一个使油气混合物在发动机燃烧室内开始或继续燃烧
& b2 S& c+ `- l1 g" X系统。3 q8 G+ m5 i4 ]. t
表着陆系统,( E/ o% a* |" Q1 u6 E* N2 P8 T. K4 B
trument Landing System C: i! d/ g p8 X9 u& s' A! U- R* r
ILLUMINATE, To turn on or to provide light.
0 @# d9 `4 ~! R3 ~3 a. |8 RIL
0 d. O- `1 C: u" r+ h, y RIM
9 Z% b) h; M! G& c" ~" Dc2 A* f$ d' Z# g a k- i% y- j
airplane climb performance, especially if an engine# B; D. u0 Z/ n. v8 c* B
quits.
+ N! x3 h! j. m( ]; N$ o/ z" q% `/ EIN8 s; r$ h* ^! u& ^
directly from the airspeed indicator without any' M* y& o' X% H0 F
compensation.
, d4 R- c: u% W' V4 i0 GINDICATOR, A component for showing quantity,& h1 `5 V- n/ x2 m2 t2 t3 z
pressure, temperature or position by a pointer or ]! i8 ^5 Q; A" ?" d( R0 {
numerical display. (Similar to gage (gauge)).4 ~, U: r; C% @3 w2 p; e% x! m7 s
点火激励器,
$ q( ^% L9 @ i2 y" _. c# p7 d向点火器提供高电压使之产生火花的电子部件。
( H3 E. W+ H! j4 \8 ]+ L' a+ c# |点! u {$ E: ~- G8 G. {+ ^
的& R8 t( U9 f8 Z
照明,
1 {7 w8 Z2 @7 @* b7 c% y! N6 }打开或提供灯光。: ^$ a$ [, Q c! g2 h
仪
( u+ o" i- O& m7 v8 }见Ins ." q. [3 \9 K3 Z7 o" X( F4 x# ]
进爬升性能,
, V! l. L+ ~- Y用大于正常的抬轮和爬升速度,来改善飞机的爬升性' b3 I( d. i) {& a& }% M
一台发动机不工作时。
) P1 f f$ D; g% [3 r' t) l5 y示空速(IAS),( Z& l. ` E7 j! {. _1 p, `$ D
正直接从空速表上读出的空速。
8 N% p( V9 Y; j2 l0 X5 Z指示数量,压力,温度或位置的部件(与
9 ? `, P4 t5 l' m# r计量仪类似)。% i0 R9 F: d G8 N B+ ]$ ~
改
" E' v+ c* _/ Q; g. ^" e7 c能,尤其是在
! m% A% Q( l/ ^1 L9 }, v8 d7 k指+ C/ ~8 F5 p8 f, m8 v. L
未经任何校. I( P* ]' }' I+ o" ] K
指示器,8 x& X7 r4 D0 x6 d; e# N% U
用指针或数字来! g( W- A$ O1 `& R( L3 z2 A, G* }
英汉对照民用航空词典B OEING
7 B2 K+ T: D7 R2 Y4 d( PTECHNICAL DICTIONARY 80
/ m1 Y* o# S" |# RINERTIAL REFERENCE SYSTEM, A self-contained,
3 O. H1 @& |. y" l2 u: E, Q7 h4 ?4 C( mnavigational system based on the measurement of6 r _: f9 ?( B, C u
acceleration and attitude.; l( V* \3 e f" @/ V
INFLIGHT PERFORMANCE, The performance of the1 ~0 {% I. `6 a1 w; L5 V' _
ITIAL APPROACH FIX (IAF), The fix which identifies: m* O$ I# }1 F
e beginning of the approach to an airport.
$ P+ i4 o: @. f0 k$ J) g7 k! LLET GUIDE VANES, A fixed set of blades in front of5 D# h, G6 S- c4 k! {
n engine compressor for directing airflow to the" l7 Z" d' s. K& \3 W
ompressor.8 B) c( t4 n) ]: d! ^. Y9 e
NER LOOP CONTROL, For autopilot operation this is
" a0 j/ H$ M% Y }e basis control of airplane pitch and roll attitude
8 p$ R1 ^+ L( V3 l. b中性能,) F, z, A% s* w
飞机的性能。
' G2 {" n8 C6 L- q7 h5 r起始进近定位点(IAF),
5 U4 [6 v+ n* v0 P' u0 p, B标志向着陆机场进近开始的定位点。3 T. h5 q( H; c* U. V/ P
进口导向叶片,% g) ~# m# P9 a3 R2 Q
发动机压气机前的一组固定叶片,用以引导气流进人压
: n8 f: D/ D' Z0 j- Z. G气机。
Z9 W( R, b; j, p环路控制,. \6 j! G; R( R, w1 h6 y
对于自动驾驶仪操作,这是无关飞行航道的飞机俯仰姿& O. L% P- ^5 \ ? E+ L- Q/ X' Q0 C9 q
制。9 P' I9 ]$ s3 [) s+ w, }
aircraft while enroute.3 F+ `9 v$ g- _: s" ?- A
IN
4 r7 q( ?5 @5 e+ vth+ S, \. k8 Z$ e9 I4 u$ `
IN5 t1 H' r/ W! u: [) t# Q' ^
a& C0 P9 ?/ i* u: \
c R' K6 e0 e1 I& H& J4 e
IN4 }1 L9 W/ m% z- |5 o: ?* [
th
2 N% Q) `7 a- I% {3 k7 ywithout regard to flight path.
4 ]' ]. f U6 E+ ~- z/ b惯性基准系统,
/ `7 _* \# U3 E, J1 d" Y以测量飞机的加速和姿态为基础的独立导航系统。
9 v: v8 S" r7 w- R7 a空* c, B- k) z& C [/ x, c3 t3 X
飞行中/ M& u/ [* s& z( @* z$ ?
内$ ~8 T! S) S) M0 ~: \
态和坡度的基本控0 H$ Y; Z) p- O" T: ]1 j7 X: m
英汉对照民用航空词典B OEING3 f0 ^; {7 }, h
TECHNICAL DICTIONARY 817 M% t! y+ _6 t/ |) v- W
INNER MARKER, A marker beacon located between3 y% W+ {' t/ c5 g& a& I* E c
the middle marker and the end of the ILS runway.
. y: B( m ?( q5 z) F3 i) e- R5 T h* iOP, SEE - INOPERATIVE
) d3 L# r7 j% v0 c& m7 H1 oOPERATIVE, Not working or operating.
5 B& |2 \7 r' w, Q# M VSTRUMENT FLIGHT RULES (IFR), Rules governing
* Q9 k& l; I6 v: ve procedures for conducting instrument flight. Also a
$ R: U/ k" e- s. v2 V: @rm used by pilots and controllers to indicate type of
2 V9 t- ]+ N$ V6 Iight plan.
8 D& p( S- N* J3 i# R9 p) SSTRUMENT LANDING SYSTEM, A precision
. F: V! x, c. ~% I+ xstrument approach system which normally consists of
0 f1 Z% h5 }4 Se following airplane components: localizer receiver,! x; S% p# d( E
lide slope receiver, and marker beacon receiver.9 L& C3 H+ b7 z/ Y- r0 [3 s [! X
OLOGICAL CONDITIONS \+ H& V- V% U* u
MC), Meteorological conditions expressed in terms of; T$ H* _" O# q! Z4 d$ p$ n( |
isibility, distance from cloud, and ceiling less than the
7 @2 A# d) T5 P3 Jinimums specified for visual meteorological
5 U( Z: ~" }& K- S1 P5 e6 {itions.. q+ r: \+ Y3 r2 g3 ~/ i' s; e
STRUMENT RUNWAY, A runway equipped with
3 z. h& l1 {# c+ Mlectronic and visual navigation aids for which a
% ^7 R" Y2 E( v+ S3 a+ G5 Drecision or nonprecision approach procedure having
3 T6 T% X& M' j; `; H5 Y& u间的信标台。) D3 _4 m `7 w) Q5 z
不工作的,4 x) h& U. ^4 l8 d. z$ ^ u1 P
见Inoperative/ v2 V& i/ U4 U1 c
IN9 s0 ~6 S* \# W- T$ ~0 R
IN: `! Z( x' x, Q3 e" e
IN9 u. ^& ?' X0 I2 g) S6 W; z2 s2 w
th
9 V5 ?2 N+ n e+ _' D4 ete2 g" O1 y2 k7 Q) d- p6 C
fl
P1 |" f5 ?( e2 aIN+ S3 D0 w6 p3 H5 p
in3 m+ X- v: I* w' ]4 T3 P5 G
th- e( w/ E0 c) S% T
g
. D: M# N, Q/ Y0 aINSTRUMENT METEOR
9 O8 `; q1 T6 M8 u5 t: y(I) j' g2 s$ k, z* @) I# F
v1 L. i/ N2 f" ~: C& k! y$ P
m' E8 d$ i3 g& N5 R( C* F
cond
2 U9 d. S. o: |3 [; F1 I5 b# gIN L4 D3 A1 [( `4 \1 M( p H, f8 t
e
4 G2 P$ p) K$ mp
& T% S- |+ H9 A" ]$ J, Wstraight-in landing minimums have been established.
" q2 w1 o- {" i! ?- L近指点标," N- Y1 d0 s/ I; n% \
位于盲降跑道头和中台之
0 G' c" B4 k7 q w' ^9 G. |: Y. L& a7 e* _
不工作,
3 w! h9 y0 Q1 d' ]9 ?- J1 @1 m- N不工作或无法进行操纵。" z+ ~# ^% ` `6 a/ z* d A) U) m5 P
仪表飞行规则(IFR),
& F* a' U: x2 |0 n! t8 c仪表飞行程序所需遵守的规则。1 S1 r% U7 G& ], L7 R |" \" H
仪表着陆系统," A* a( F+ Q) V* z
一种精密仪表进近系统。一般由航向道信号接收机,下
- I3 w1 G2 {0 H" f5 L1 k滑道信号接收机,和指点信标接收机所组成。) A( Z0 ]$ h1 u6 W! l1 s- A( c
以能见度,与云的距离,和云幕高低于最小规定的目视! A8 D+ O( {7 _! M. x
象条件的一种气象状态的表达。
2 c5 S- o& A7 t" P+ _! h7 t/ u; f用于以精密或非精密进近程序作订明最低天气标准直
; B( a$ v$ G6 P着陆的装备有电子和目视助航设备的跑道。# d1 C5 V$ @( q8 w, |
仪表飞行气象条件(IMC), n/ F/ C h8 g( E- N" w! q! [
气: p7 q6 [- e6 @4 c0 s6 R
仪表跑道,
) ^$ z. N7 }; N! `8 d5 s o线
! _. G( M+ |0 a英汉对照民用航空词典B OEING
( n+ o4 Q. h; T' J) kTECHNICAL DICTIONARY 82/ P+ ?9 P, N! k1 }2 k. }
INTEGRAL TANK, A metal container formed by the& m7 s$ {& R8 @) c) X: ^$ ^
lane.' f7 p5 y' N, i5 K; j" Q1 h
cted; ]/ u& n- J. R! V# ~
circuits.2 s# S H% X' s, W' ]4 i
Manual
: ~: }' A' @0 O1 y6 |0 Performance data providing range as a function of a1 `$ t$ J9 v' o
hange in airplane gross weight.
& O( c D( W6 Z, hTERNATIONAL RESERVES, Reserves required by- R) P. P9 |9 }* V& a: m' v
e applicable governing agency when flying5 b# }; B% e7 f4 v9 F* q6 S
TERNATIONAL STANDARD ATMOSPHERE (ISA),) J" Q1 R5 D. O2 s
he hypothetical vertical distribution of atmospheric
+ G$ g( V, m. s! j; R9 Ymperature, pressure, and density as defined by the3 n) | f/ W* x, |# B8 j( l
).6 \# z" Z3 J) L0 M6 t8 P& y8 W
TEGRATOR, An operational amplifier whose output
4 ?- |( U% I3 V9 @oltage is determined by the input voltage, the input5 s: v8 o3 t) ]7 I6 u
上) w0 n1 d% {3 ^& ]
存燃油的金属容器。
. U. k- r, T$ M* @( b6 {,
% @1 ~' a. j% @3 J飞机总重量的函数提供的性能数
5 z( z, D# ]6 K) e。
! {! x7 m* ?- C1 z际航线备用油量,
5 c# L; F Z( Z' u在国际航线飞行时,有关的政府单位所要求的备用燃油, m. b% n% U1 k, F- P
际标准大气(ISA),
, G9 W/ R! k0 |: c国际民航组织(ICAO)规定的,一种只在理论上存在" I( c+ s+ Y5 c4 s* n' J) ]
大气其温度,压力,和密度的垂直分布。
" C/ k! I' g K/ N- \3 W0 ?% g C* [分器,8 @- ~) \4 g! Z3 |7 H. l
由输人电压,输人电阻,反馈电容和时间微分而决定其
; k- ~0 Y, X0 d4 v! E1 _- \运算放大器。
; }0 e P1 V z; Q3 T, Bwing structure (spars, ribs, skin) for storage of fuel on C7 G/ c8 M5 Q3 R
the airp4 ?; I9 d8 ~' S" v% f% P: Y5 s
INTEGRATED CIRCUIT, A small piece of
, o6 i) o( l! V* g0 k4 V* osemiconductive material that contains interconne
: e. R4 o- |! E0 w- o2 ~miniaturized electronic
& E# X. Y& N3 \ W+ b+ H! uINTEGRATED RANGE, Tabular Operations; V! `: e0 J% s: D2 L& J
p
2 H5 ]& f& r# u6 \c8 }& p* m4 ^0 @! Q) J' M
IN( ^. T7 @2 T' ?5 h7 N/ B
th0 e: D0 T" X8 D0 x
international air route.1 N0 Z: g9 L+ |& R( q% R5 ^
IN
( X' {% C7 l: c; mT
5 f1 d9 |+ L0 M/ h" Q" ?0 ote
L: r0 x' M# u- S/ B- _International Civil Aeronautical Organization (ICAO
2 E z$ \1 i; d8 a& e* [/ WIN
2 L' @; L, U7 f9 ?v9 U& [& s, ]9 _) H
resistance, the feedback capacitance, and time8 v& h& m5 N u9 S- L/ B
differential.; W: H7 T" t6 i
整体油箱,4 Z4 D; O7 }" b4 a; z+ h
由机翼结构件(梁、肋、蒙皮)组成,用来在飞机
" K: y( X9 ^) m9 {) n, t储% a. p) n) c% y8 H% c% v. l6 c
集成电路,& R; `+ _, \: k
一小片内含相互连接的微缩电路的半导体材料。
5 V$ C. J- C3 m6 w% y1 @, U3 Y( `; C综合航程# A# u0 |, n- R. [
使用手册将航程作为
' C3 G* w, K3 `4 y0 U据
! z S' E* o. ^1 Q4 R0 e国
5 a( l9 u5 z& w2 x: [量。$ R [4 E6 q8 z$ k& q+ C9 m( ~/ s- J
国
1 G4 i& y) u/ V' ~/ k5 t) U+ {的4 X. f9 Z6 }7 j4 U* k
积
1 [. l# N7 ^5 N$ W% l输出电压的
& f% |) {5 `4 E英汉对照民用航空词典B OEING5 ?) Q9 Y8 w: ~5 G* b
TECHNICAL DICTIONARY 83
C$ K2 L/ J. p/ w; CINTERLOCK, A wire connected in series with an3 W1 A' d, b1 {) O1 n. f1 _5 O8 m
equipment or device, or a condition that allows {( C- c9 Z# v
operation if all requirements are met.
; j6 b) d* y5 y! zf the United Nations whose' r1 R8 ~( T- v2 F) l
bjective is to develop the principles and techniques of% `7 @/ _6 [* {, m- w w
ternational air navigation and to foster planning and
- Z. ^5 W# z# A- Levelopment of international civil air transport.1 d2 h0 w' |! U
TERROGATOR, The ground-based surveillance1 g6 P# L+ A' ~
dar beacon transmitter-receiver, which normally scans
6 u7 j8 e/ b) V* Y2 vll; t" o3 b# \3 H' E; V( a: t
on the mode being used to reply. The
8 S, R$ ~7 H& V+ C: R& Gplies received are mixed with the primary radar9 i) K8 Y5 j- N& {" M8 @ p# _. U
turns and displayed on the same plan position radar
) A r9 H. n8 _cope.$ j' `: T1 x0 P, g: @) P" S
TERSECTION,- f. Y. }9 D1 |+ `, n8 b
1. A point defined by any combination of courses,
/ o5 u, O% M. e6 I) Gradials or bearings of two or more navigational9 e% A1 k" h) K: P
aids.- T( m+ Y3 C5 G- V
2. Used to describe the point where two runways6 z" z" i: R* A+ O) ^
cross, a taxiway and a runway cross, or two
* g: c9 S6 N* A* @taxiways cross.0 P2 @& W& b8 S5 s) Z, t0 S
cy)& J) o( e$ Q! A7 w O1 T( a" g
tem.
, Q u2 t( ?0 K. a% ]9 r1 Z者. M7 I* v) P S* M
当所有条件都满足时才能工作的状态。
8 C r4 T) ]/ U2 e. N组织,
! Z0 V* h L9 n: `航的原则和技术,促进国际民航
# i8 y5 F7 t/ K) [7 _( H输的计划与发展为目标的联合国专业代理组织8 w+ t" i2 x/ q8 [9 g0 N1 k3 G
问器,4 v8 d- v; F0 U6 T
一种地面监视雷达信标收发机。通常在工作时与主雷达
@# q. T% o$ |连续的无线电信号,不断地重复要求与
$ P( {0 Z) l( K j5 |& z, h接收到的信号相混合,显示在同一平面位置的雷& V! ^; D3 m# J# z; Q* w, a
达屏幕上。+ \6 p0 s/ N; Y ~" h# W) j
交叉点,/ ~" V. t I" Z4 q" Z
1. 由航线,径向方位线,或两个以上的助航设备
7 c2 K3 ~4 z6 L, J+ B的方位交会而确定的一点。
$ R. I4 l( _4 F$ Q) u9 i8 K2. 指两条跑道的,滑行道与跑道,或两条滑行道, A; D! u* d. e1 @
的交叉点。
8 v7 E! }6 V2 a, \9 TINTERNATIONAL CIVIL AVIATION ORGANIZATION,$ t- p( W1 C! B. x0 E$ X+ |
A specialized agency o/ b- o7 W0 a! B
o
+ r; U$ C7 ?2 K" j5 \8 Pin- E: J% K' B. {/ B; ]. U
d6 D) L8 o" z$ {) W
IN% p, r! ]+ a0 Y3 i/ D3 ]
ra
* j( I! y- U! ~5 R1 H* Tin synchronism with a primary radar, transmitting
- O1 _1 }* Z' cdiscrete radio signals which repetitiously request a
2 z# R) N2 l/ E& gtransponders
?. d7 k& x' ]& F6 H! M- V# X/ _4 Nre
8 q+ O' W* q8 c$ j, [re" s( M) e9 H$ ?- C' k
s
/ e, A0 ^8 l7 `* k/ ]IN) |6 g/ l J, p# G3 Y1 `
INVERTER, An electrical device for changing direct
: A% V7 \; B& b; ]% i- n/ F5 {( Pcurrent to alternating current for standby (emergen7 s9 \/ F, n" j8 e8 W
power supply to electrical sys2 T/ _* e% v2 O. O6 U+ a2 `
联锁,6 k! L$ U# m( g7 l7 ?/ d
一个以串联方式将仪器,设备联接在一起的电路。或- N0 v* A! ~; g. g5 B- @! I
是 j" s' h( S( M
国际民用航空. R$ g6 i+ Q! x
一个以增进国际航空导( @2 s4 v1 t: O5 H; L
运 W/ y, r3 I- f5 g
询. R. g# L: k+ b
同步扫描,发射不& i5 P% u3 N$ t& N
其工作方式一致的应答机进行回答。所接收到的回答信号$ {0 ~# Y5 t9 P
与主雷达
# v! n$ n* f9 G# r. k: o9 B变流器,/ U# n- p9 ^: o" z8 J
用来将直流电变成交流电;以供电气系统备用(紧急)3 a0 t C+ w* K" ? k, k
电源的电气装置。
, |6 w9 @8 p) L7 K( m: {1 Q0 i英汉对照民用航空词典B OEING- C# \+ g) w C0 W- }, \3 h
TECHNICAL DICTIONARY 84
5 y( Y& o% F1 A4 S. dIRS, SEE - INERTIAL REFERENCE SYSTEM
( M6 l* J) L7 ^- ?# D# k1 S/ C' xISA DEVIATION, The amount of temperature or
) G9 w5 Y% N7 r" isee International" B; g5 j y* ~# I' H
tandard Atmosphere)./ @3 }9 e# F- C( z* f. |
LAND RESERVES, Reserves required by the) j9 w) H# x2 H4 h" @. s4 J3 W( k
pplicable governing agency when flying routes. @% j( F% [' ?
etween islands with no alternate airports.
, U/ Y3 H. _7 x& y7 F* y+ O7 KCONDITION, Cabin pressure (altitude)
0 h, O( K+ i, r; Y4 Mmaining constant with changing airplane altitude.
; X& O, A& y3 Y/ y0 J. m* Pising the
1 ]+ ~' [ H, L: Fa( I$ s3 Z! ^ C- E
,
+ K M$ Y: U7 z, T5 ?pressure difference from ISA (! ^! H$ D% H$ l/ j4 w
S
; ]" y1 e9 p3 j2 G9 T* qIS% t0 f4 N9 C. W) O
a
+ R9 o1 z, m! O3 i% }) e; B. \5 ab, h( V C$ ?( c# G9 n. t8 F
ISOBARIC
6 [0 a# N7 k. S. S' u6 c: Sre
' u# k1 K. ~" z2 p6 M+ C# P3 L8 PISOLATION VALVE, A valve in the system for! c1 a1 ]: W+ x% M
separation of the system into sections.! i: ?. N2 W0 a4 b! ~# S
J
# {5 ^ ~7 v; ]0 _. F% z% k* k- @JACK, A mechanical or hydraulic device for ra7 ?0 j$ T; U1 D3 s3 C
airplane.* X1 j% R: a4 ]2 f
JACKING POINT, Location on the airplane for using
1 l- A& n7 w$ M& m& _jack.
) M. m0 h" w* l1 `" Y9 r惯性基准系统( ?# T0 v: _- S4 D" l' ]" z
见Inertial Reference System.
+ x% ?% A/ z T' Q" Y- k' e与国际标准大气之偏差,
( }$ T- l z6 v: v9 Q+ ^; J压力与国际标准大气的差值(参见国际标准
8 |' C/ [. X) v有关政府单位要求在没有备降场的岛屿间飞行的飞机
" A. q2 x8 ?5 \! \/ r带的备用燃油量。9 j7 y7 u1 E+ t, p/ S9 Z' m
压状况,2 f* I: u2 _) x c4 Y8 _: r
在飞机改变高度时,座舱压力(即座舱高度)保持不变2 v0 j% V* K) E9 I- _2 l q8 F
状况。% ~9 _6 j7 ~- e! `8 D
斤顶,
! `, m, h0 Z" G: r/ A用以将飞机抬起的机械式或液压式的装置。
4 _2 n i8 Z! P温度或/ d8 [& k; Q" K4 R- k3 ]
大气)。* f6 `& _, e7 f/ q
岛屿备用油量,
$ l i4 e A4 W( h7 m携
$ k4 S( c; c3 j2 w6 P等
. W/ U# o+ b0 G# u( Y9 m; S7 R的) |' G8 P( r) P$ T* [
隔离活门,. _2 N y3 _. I' D# W3 v- a* s/ q
用以将系统分隔成几个部份的活门。8 Y9 U4 _0 x, W9 _% U
千, i, a9 ]/ J4 D5 U2 q7 Q' S
千斤顶支点,+ F: [& @, N4 m" r% b
飞机上可以让千斤顶吃力的位置。
8 S$ X9 T4 v* \! [( V$ x5 ^( U英汉对照民用航空词典B OEING! ]8 J9 O/ H" ^8 ~
TECHNICAL DICTIONARY 85
/ I& |6 |5 a" Y4 A( @+ cJACKSCREW, A rotating threaded rod used to drive
0 T2 w- F: T- umoveable component such as a flap or stabilizer.( c& t+ o6 u! W2 |$ x5 A' A# k
a 致动螺杆,
. H8 X$ v: ]' n3 I% P9 f用来使可动部件如襟翼或水平安定面运动的能够旋转
9 _5 x v: R' ]- T的螺杆。
- \" q$ _; z6 G8 B; j英汉对照民用航空词典B OEING$ Z! A' u1 R$ O9 ]8 k# ?( L' l
TECHNICAL DICTIONARY 86( j u1 e4 m& R3 `/ m
JET PIPE, A control component in some valves and
) R/ s% x; K) S9 m: h2 v, P4 |ET PUMP, A component in the fuel system, operated8 k: Z7 K9 R4 @/ _9 b
r removing water and fuel from a fuel
4 o6 \! |- X7 G& u; }' Tnk.) [; N, W, C# ^- Y
射泵,8 }4 A" R- A/ h( l5 _
内,由燃油压力来操作,用于从燃油箱中排除
$ A7 C$ e9 l1 @6 z' x和燃油的部件。
8 @1 b# ^0 K6 E% yactuators for controlling the flow of hydraulics or
: V/ l* z* C! w! B' q, Gpneumatics.
% l1 ^+ ~0 S# dJ
3 F0 H' S/ g3 |" L. Pby fuel pressure, fo
- s: y7 y( b! Z2 s0 d: ]ta/ {% [' W+ D+ z0 p: ^
喷射管,
3 x7 K9 U7 a" `3 b, R- r u在有些活门和作动筒中的控制元件。用于控制液压和
0 A) O+ _) u. D( j) o5 K气动的流量。7 l' ^1 U; o7 n# u! F: \
引
. L* @" x2 U/ C4 W* s8 y7 B. g燃油系统
4 p0 o m9 o+ `* \) O* \水$ z z: t0 `0 k( o: X* s
英汉对照民用航空词典B OEING! ?' r( m& ]8 M
TECHNICAL DICTIONARY 87
* A- m6 X7 J+ w! h" T, T( }8 ^JOGGLE, An offset in sheet metal construction
8 T( A! }. ?3 h5 r; u/ l# ldesigned to allow one piece to overlap, either higher or5 V" t* F5 @4 ?, _
wer, the other piece.8 q9 K/ J4 i" w2 }3 G
OULE, A unit of electrical energy of 1 ampere of
- V2 z) B6 J1 Q1 `- h6 |urrent passing through a resistance of 1 ohm for 1+ y' b$ y; B7 R0 S' ^" h& l
econd. Ignition system energy is measured in joules.6 M" Q! O+ x' O: A# q
UMPER WIRE, An electrical connector for temporarily
3 _8 l3 a' V2 b+ \) E2 _ypassing part of an electrical current.
5 w5 e7 G1 j6 |3 Z) Y) x/ gUNCTION BOX, A container which serves as a joining
' S- r: z" O+ t0 elace for electrical connections. May also contain2 A3 F) z* e! [. o( W' A; p1 z
lectrical components.
$ e: W! K1 V+ C7 ZEEL BEAM, A structural beam in the fuselage center
5 Q7 w" N8 X" f1 m( aection (wheel well and under wing center section) to% f8 S" c9 d4 V7 T0 i' D- F" t. q$ f: j
KEVLAR, A light, strong synthetic material for y7 N- A5 U; k$ |- ?. A* c: F
secondary airplane structure.4 T' {' x% R& W2 |& |# r
,使一件金属与另一5 z& { h4 Z2 e0 N7 J# K9 A1 m
相互叠合。
0 M0 e4 ]9 E1 [耳,( f% I. [/ N5 ^2 m; \7 I
电能单位。一安培电流通过一欧姆电阻一秒钟所需的电
) p1 G' X8 m( l0 ]为一焦耳。点火系统的能量用焦耳度量。
8 h3 g9 P+ _7 A- ~接线,
9 Y: `: [) Z' e用来暂时旁通部份电流的电器连接件。
V! D6 w5 F$ d线盒,/ G8 p8 V$ @6 [
做为许多电接头的汇集处的容器。也可能内含电器。
! H5 S% b# [' Y! }" u梁,) w+ W. P% e, Q4 [. y) H& ~; l! u( ~
机身中段轮舱和翼下中段,用以防止机身弯曲的结构。
2 Q6 C* Q6 U; z1 p: t6 q$ t+ aKEVLAR,
3 w7 \3 h; u$ `7 a, D一种即轻又强的人工合成材料,可供制造飞机的次要构& d5 z. v5 _3 Q; F
件。8 _0 V' [( v! d2 n; O( `* v
lo/ F' u9 y3 D# \9 v
J% Q# {2 l# R" }
c
% T+ Z+ Y: x2 ls+ @8 B* g6 r4 G; f
J
; ^% e1 Z# J0 C& Hb8 H" A ]2 V2 |4 a3 _7 Z
J
8 }; _- n; Z7 |p
- |9 Z, ^) g) \. ^: \' Y! I& re0 a' F8 f) L/ y. Y* p
K% M3 F; ~& M5 u3 f3 ?; p
K. b* K& E6 u5 T( N& O# J# x
s
, h, T o, ~% k4 zprevent the fuselage from bending.
; Z1 T9 u/ G, ~- ^折接,) B7 a; y& i" ~& Y5 d! ^9 H, O
一种平面金属结构设计的弥补法% X" `% ?7 o' S
件! k; x6 E" z* x" ^
焦
1 F3 K$ r2 l5 ?6 U; Z5 J `) F能
/ t0 M8 d1 i4 s; M* ^' g5 B7 q跨
& V, c4 {" A$ T9 p% G, v% L接
r! I7 l6 \9 b& @( q' Z腹
5 ?/ r6 F) z+ g$ ]英汉对照民用航空词典B OEING. @8 \* E. G- \; _) `. `
TECHNICAL DICTIONARY 88 |+ \' i/ d# f/ L
KILOWATT, An electrical energy unit, equal to one
2 q% @/ P _! @* m6 Athousand watts, for specifying generator power output.
! r2 S3 `3 W B9 u5 ~, mKINK, A sharp bend, twist or dent in a section of tubing,( { C* H8 h$ F4 ^0 ?$ f2 B
wire bundle or angle stock.* k- I) C8 m# O% z) u8 O& K
KNIFE EDGE, A very sharp edge on drilled or machined
& @3 {, p# V9 s0 t7 Z" E3 }metal which is usually the source point for corrosive5 {) `7 ], d* z7 X! i5 \
attack.
# x4 O5 w. I% p3 NKNOT, One nautical mile per hour.6 t) F: H) J: _8 N0 q
KREUGER FLAP, A type of leading edge flap that is5 y# x6 o4 U" Q7 L$ E
fixed on the lower side of the wing and rotates forward
9 ~; y0 y" N- h1 i1 o: Yinto the airstream.7 d; H6 j! n; q
KW, SEE - KILOWATT! N$ k3 T8 @! k7 ]% m: A
L% A1 j: g' y0 a$ C
LABYRINTH SEALS, Rotating and stationary
1 X2 Z- N3 y( }& J5 z# V b$ koverlapping structures which utilize differential air
I) ~; R8 N8 s9 \/ x: jpressure to form an external seal. Most commonly used$ Q9 {; _( r( t; Z# b
in turbine engines.2 @' Q2 \9 X) L& V7 D
扭结,
# ]; \8 V8 B6 O% l2 j5 X$ Z+ J5 |在管路,电线扎,或角材中的尖角,扭转,和凹坑的部
% C( A) }0 ?( S# ~& N3 |" N3 {/ }份。
3 X& Z4 E- ^6 `& y5 O# A刀刃,
0 F. Q$ I6 B I& b$ ?' ]钻制或机制金属的锋利边缘,通常是腐蚀的开始处。
7 [) t! v6 s- \8 q. ]节(K,KT,KTS),
" T- b9 \- {; X每小时一海里的速度。
9 f9 ]8 _+ R3 x8 U$ X克鲁格襟翼,) V- f R& Y1 n% i
一种前缘襟翼,位于机翼翼根附近,旋转前伸。3 J6 o. K) e4 r6 d
千瓦,% S& _( r% p' R. L' P2 B& h
见千瓦(Kilowatt
( ?* N, @/ F( X+ d' G4 P# {千瓦,% U! f/ @) b1 r4 ]
电能单位。等于一千瓦。用以确定发电机的输出功率。
7 o' }. Y2 L$ M# Y- K)。
+ n% T. i6 y' E1 k# h; j5 ?( M( l蓖齿型密封装置,9 ^. Z) a& Y6 L; t5 F S
旋转并且固定的重选结构。用气压差动而造成外部的密3 N/ i' r- ?; W
封。在涡轮发动机上最常用。7 T4 c7 k7 K ]# D% U' S9 n4 b
英汉对照民用航空词典B OEING, p' C. v; r: j( W* i" z; o2 m I
TECHNICAL DICTIONARY 89
8 W- s0 J! d. G' L1 U0 k8 wLAMINATED STRUCTURE, Composed of layers of a# e( D- J8 b5 m! `2 F/ z
ake a
z4 p* O1 } J: bht structure.! f; h6 K, Y+ U/ R2 b. o3 x# O* F9 A
.E.D., SEE-LIGHT EMITTING DIODE.
! q) X. P' k6 x! Q6 ?* KANDING GEAR, The nose and main wheels with the9 l- Q# z5 e4 I- D+ L
ttachments for supporting the airplane on the ground.
+ C' L/ ^$ G3 r1 iLANDING GEAR DOORS, Panels operated by the5 l& R G) x4 b# `7 C! G$ @$ s
landing gear for closing wheel wells when the landing
9 Q8 B. S; R( C8 ]7 z5 Jgear is retracted.: G9 \& Y1 @! f; S9 b7 o
LANDING WEIGHT, Gross weight of the airplane at the" O, V1 V0 n% D
destination or alternate airport.
# U5 X; T" s" _: I4 n发光二极管,3 Z* G3 t; h5 A7 \# I
见Light Emitting Diode, \: [4 G; x( h
composite material bonded or cured together to m
: Z0 P$ P5 ^0 b- N7 a' Rstrong and lig
0 J9 P: ]5 R8 u W) ^L1 R& `- N: u1 Y+ |* x% ]
L( z v+ u; U9 r0 ^/ ?
a+ ?! _; H8 [! m/ @
分层结构,
% A* s: V4 \+ [: _一种牢固而轻的结构。由多层的复合材料胶合或固化而$ E7 g! c* ]9 l
成。- j8 L$ {0 J+ X! b- C$ S
.
# C+ O# [- t; z" _* F: L# L. a- u起落架,
$ U$ p. g. c; [, t5 O0 P+ p8 [用以在地面支撑飞机的前轮,主轮及其附件。! R6 K) |8 N* v ?# G! v
起落架舱门,+ z' c# r2 e6 c- ~
由起落架操作,用以在收上起落架后关闭轮舱的面板。
% m$ I% ~9 t9 Z1 L) |着陆重量,+ h6 R9 k5 Z( B
飞机到目标机场或备降机场时的全重。8 s; f6 E7 M2 i: c8 k3 C& {' F
英汉对照民用航空词典B OEING$ E7 z7 b) @. [7 m
TECHNICAL DICTIONARY 90
3 y: U5 f6 n0 Q2 ^* _- i! | uLANYARD, A cable for supporting or holding pan
2 Z/ }, o* W N* eopen position.
, `+ D( ]# A9 Vels in7 M8 @; |( U3 N5 i! Z- l6 ~4 Q
AP JOINT, An overlapping sheet of metal, joined to the
/ m. R& j, Y, m0 b4 rdge of another sheet in aircraft structure.
! G. W9 _+ a9 A1 Q5 z: KASER GYRO, A gyro which uses two laser light beams4 }5 j! }5 a; [. D' f8 n5 a( \, }
measure angular rotation.
) p& f+ @2 f- `) ^9 f v$ _' N.4 l+ [, }7 e5 Q% v
ATITUDE, Measurement north or south of the equator
) }# n/ ~2 T4 w) |4 Ms, minutes, and seconds. For INS equipped
- y$ x; u% C+ P9 \* _! v" E$ Vdegrees, minutes and tenth of minutes.
$ d3 w* P5 T6 Fl device for/ I: f/ X" Z9 d3 e8 A) n; H
hanging stored chemical energy into direct current.
4 [: q3 K: m6 g1 oses lead, lead oxide and sulphuric acid.6 g* ~; B/ k5 u- ~
搭接,
& {# H) Y2 w7 j' f飞机结构中与相邻金属薄板连接的重选金属薄板。
" s* S$ o# F. q' D激光陀螺仪,8 {. O/ e; {6 e0 D# S* B1 z: `
一种由两条激光光束来测量旋转角速度的陀螺仪。
: q4 e5 T/ G0 U# m% n- s用以紧固或锁定的装置。
: \& Y) e$ C' D0 g的轴。2 L0 ]4 X( x8 w
方式。0 z8 f h3 J* w0 S, d* b
度,
" C9 a3 u. p' ~. ?6 V4 e4 W地球上与赤道平行之弧线。由赤道以北或以南度、分、! V, r, c- l) r5 h
度量。对于有惯性导航系统的飞机则以度,分,和十等0 x' X0 S) D. X, ` i1 x I
度量。
4 u) y3 P1 u/ V) _+ t8 H6 u- _酸电瓶,
7 J: u+ Q" q- o; r. M将贮存的化学能转变为直流电的电气设备。它使用铅,* k1 @. m/ I- D
化铅,和硫酸。
H3 K: g0 P0 m! m2 V3 s7 d5 qL
% J4 c9 p# F+ Fe
j' h! R7 C ?; R; vL* c; R7 w9 J0 e" [
to
8 b, s2 G3 ?; Y' \7 kLATCH, A device for fastening or locking.
0 i3 U J! S5 W! rLATERAL AXIS, An axis passing through the airplane's
1 P3 t1 c8 O: `3 W. G ~- [* zcenter of gravity, from wingtip to wingtip. B4 Y1 k0 j* L- @
LATERAL NAVIGATION, An autoflight mode in which
6 s# B- Z- B# O4 g# ?the FMCS is used to control the airplane roll.
$ X; P9 ^8 G) U) X+ lL5 u- K4 b( Z2 x$ I6 z1 x
in degree
. y: o0 ]: ` g/ H% ~- gaircraft in
3 K! w9 j' I; kLEAD ACID BATTERY, An electrica
) M, E" Q; z U& m/ u7 w# Z) Pc
+ @8 O' t- p6 h9 k/ N* W) qU
6 q# J" r2 @4 e3 H+ ]( J; \1 E& X牵索,
/ |) u7 s2 k1 l; P用以使面板保持在打开位置的钢索。
9 t0 s: h/ ~# f, n3 Q5 h0 l2 U闩,, r+ {+ j9 e1 ]0 j
横轴,- e6 p6 e/ y6 ~0 b4 y' i
通过飞机重心从一侧翼尖通向另一侧翼尖
; } q0 ]/ ?' ~6 q! p3 j+ M水平导航,5 V# c# E% |0 L' x R/ k: Z
使用飞行管理计算机系统控制飞机横侧的一种自动飞
# g+ O$ V: P) ?& e' S行
0 j- h! @' b8 `4 T纬% p2 P* l9 K, j7 f) k" T
秒
& O4 E5 Z* b2 y2 [' _分
& h0 y, g! M+ \2 M6 g: _; @铅) I7 ^, G. |- s* }7 k
氧7 D$ Z8 ]! R8 ^5 r' \+ H' C, l
英汉对照民用航空词典B OEING
0 N4 }8 u/ K/ E5 i: E9 ZTECHNICAL DICTIONARY 910 H- d [5 m8 Z' ?1 }' S$ B
LEADING EDGE, The front edge of a wing, stabilizer or) U/ Z( k- Y q" h
ED, SEE - LIGHT EMITTING DIODE
6 N7 |8 [7 s! F9 @* h) i! E- |EMAC, Acronym for Leading Edge of the Mean' `& T% j. [) z4 m
erodynamic Chord.6 }7 E/ G7 y N( _
IFT, The vertical force produced by the airflow past the
! V0 S+ v; c. ~* p. `. \s of the wing., Z3 {* E- W0 ~
IGHT EMITTING DIODE, An electronic device which
g1 @. }8 o; R4 |1 i) jtes with red, amber or green light when supplied. q0 |5 C+ H! N2 Y
ctric current.6 p! Y/ X7 a& ]2 z
,
6 U9 d+ \! m! _8 Q3 m+ dcontrol surface.: L/ J0 s0 e& X3 J
LEADING EDGE FLAP, SEE - FLAP4 J! b7 U( ^; `
L9 ~, `% }9 _0 z* c* {% X% @5 U$ x, b/ ?
L
# \, `! p+ Q$ f4 q% E3 IA
e. H ^2 z# B4 Y$ A4 GLEVEL-OFF ALTITUDE, Altitude of which the airflow
4 M& v1 Q! G1 H' b) p6 H5 ?2 `past the upper and lower surfaces of the wing.
f6 M" b) a* l1 G4 \& mL- N& w: u0 s9 g- q- x
upper and lower surface$ Y! u* h- Q# ^: S% k7 O" P4 e
L5 s! v& g0 q5 v/ [
illumina8 ^) l# s5 T2 e/ Y& W
with ele
: i! q7 ?/ ^+ C& c/ \6 K前缘,5 Y- b0 A! V) a* L
机翼,安定面或操纵面的前部边缘。 r, B& s; ~- B
前缘襟翼
8 O" n. j$ K1 M9 C& N见Flap.0 G6 m. e1 } U Q1 m0 f7 S
发光二极管,& s4 [ S4 ], i; B7 N6 d, F9 Z5 \! G! N
ht Emitting Diode
; G& m' l! d3 H5 h; H见Lig ." |& [; B: y$ v, K# j$ Q
均气动弦前缘,3 P- X- X# t# T5 e/ F+ S( ? v5 w' @, g
平均气动弦前缘的缩写。见Leading Edge of the Mean
6 B* P# X5 O( l8 E) Z% O平
! G. v! K6 y3 g8 e' MAerodynamic Chord.
- l- u9 A; E6 v+ @7 q+ C5 P" h3 G8 S力,) E) U! o6 F: x8 t& F
过机翼上下表面所产生的垂直力。4 ?' y8 T4 S- G+ O% y; N
光二极管,
, d0 {" j1 j) M, r$ H1 D通电后能发出红色,琥珀色,或绿色光的电子元件。
, T+ m# [( N3 W. m7 X9 `# t改平高度,
2 Y4 ~) w( m0 T) ]$ B6 Y1 }4 y, J飞机因巡航时发动机发生故障而下降至的高度。
+ D5 t$ A- |' N1 {升4 s4 ^* H+ v& A( i o
气流流& O" F3 }% m/ V0 a7 O- o
发* v( [- D% s; i- K6 S) S8 B
英汉对照民用航空词典B OEING) E3 s0 l z3 W- U# w, W
TECHNICAL DICTIONARY 92: T' f# R% Q1 J3 \1 F( Q, s5 r
LIGHT PLATE, A component part of an instrument% z' X9 _- t/ ]8 U- C4 ^
panel for illumination of words on the panel.9 i* x/ ]* W: r' |3 X
LIGHT SWITCH, A switch which contains a light. The
2 z1 S: s$ j1 n' p# Jopened or
! A8 p" ?$ ?7 V( t; Ilosed.. w, a0 {7 g' u/ E& L
n electric actuator which turns off electrical power to9 ~& t. C: L9 b' B6 Q* m
e actuator when the actuator reaches its open or$ T$ C w0 b7 R( d0 J( T$ P
losed position. _6 w! I( s L7 n# E
IMITATIONS, Performance and operational limits
& ?% G' q1 p' `: H$ F& ]& Y. \* V5 lsted in the Airplane Flight Manual (AFM), such as. N$ U! i& M& u. V
aximum airspeed, maximum altitude and center of2 p# t7 n0 T [
ravity constraints.
: x2 ?+ l2 D% H. B( Y1 c4 Cy
, q/ I: O0 ?' b+ J" ^2 a* m5 ycraft during line maintenance2 m* F) Z- r4 U
perations.
& S% ?$ q5 h% Hontrol
- k. i7 \' D3 o/ N ]2 wdisplay unit allowing control of information to and from: {! b1 D+ u$ X, g& X. {* i
the scratch pad and designated areas of the display.& j$ I3 A/ S0 U! i8 Y/ N# s
光电门,
& w8 j A8 L7 x8 `4 n5 T; Q% H% c电门开关而决定灯的明灭。 t2 N, g* K$ c8 F) J
在电作动筒内,用以在作动简到达打开或关闭位置
' {: ?- h5 p; A+ H时,切断电源的机械式操作的部件。% K% T( [- W; V, e
各种极限,
8 J1 X% y9 I3 J3 [飞机飞行手册(AFM)中列出的性能限度和操作极限,; p$ \, A) m' y" S7 s& y
如最大空速,最大高度,和重心的限制等。: Z: S& k7 s4 O, ^
在航线维修中,可以在飞机上即时拆换的部件。* y3 K$ |. N4 p/ }/ Y
飞机管理控制系统的控制显示器上的电门,可控制草稿
2 e0 U4 C `6 j( J O9 k栏和指定显示处信息的输人和输出。
w& Y& [+ M( y' dlight either turns on or off as the switch is- z+ ]6 }( c0 H. Z3 `( W3 K! Y+ v
c" H/ E0 W) R* [1 g" W* T+ ^
LIMIT SWITCH, A mechanically operated component in: _4 l% H7 {) ~9 |# V
a5 r2 v0 k6 u1 [" I5 I. b3 Q
th* m; b( B* T0 r' V& x! N+ ~3 Y% K+ t
c- ?% }" L& {2 f9 I% d3 Y: D; ^
L
4 F/ x- h, o! u: G, dli& V4 i8 H; X% s3 `6 g# Z! B" ]2 ~
m
/ f* ~4 E/ P @* Y) a0 E% E2 W) Ng/ ^. q+ Q, _3 `( y% j' Y
LINE REPLACEABLE UNIT, A unit which can be readil
; ?* h. Z3 j5 \; g" schanged on an air. {# `4 j, m w- T3 o5 [4 x* y
o8 L) p6 f+ n( r
LINE SELECT KEYS, Switches on the FMCS c
2 ~7 S. r4 _ g; V& J照明板,
5 M$ c/ G) }; _5 I7 i$ I仪表板的一个部件,用以照亮仪表板上的文字。
0 Z8 Q# |. f. v) p4 d灯3 B `2 s3 q; L) y5 ^
带灯的电门。
, B ?. u7 h! J: k极限电门,% d2 W3 h0 v- ~( k6 s/ T
航线可换件,
3 Z! n! I1 d/ }行选键,3 C1 t+ Q+ d9 o n2 w
英汉对照民用航空词典B OEING
3 N9 h: F1 {: Y2 `. U( YTECHNICAL DICTIONARY 93& @2 Z# A5 P, n# C+ f2 o8 u- T6 G
LINEAR VARIABLE DIFFERENTIAL TRANSFORMER,
5 p0 G* U, i, dnsformer with a linear response.. m9 ~4 p: S `: b" _% V
NAV, SEE - LATERAL NAVIGATION
+ `+ [& n {" pOAD AND TRIM SHEET, A form containing tables and
! G4 v5 g* b ?7 O; Vharts to account for the weight and balance effect of all
3 l+ ]+ d A' J) i" qpe of an
9 I i5 d/ k1 Q5 [8 w0 z. o5 q# L' |! TS approach, normally located at or near the point of* ?6 M8 |/ }6 i4 U% ?
ecision height.
+ x2 m4 s/ J$ |5 _7 \; ]er1 c: u* R# N7 L& {. q
eacon at or near the point of glide slope intercept of an, {% T4 C+ R% S8 D0 {* _9 F2 _% R
S approach.
1 `4 J8 Y2 {0 |' J4 s7 T! _) @ich provides
- r6 c- k: ]3 \* D+ I; U+ Ylateral course guidance to the runway.
( b; }- C6 H% Q J/ {% p" E8 h差动变压器,
: _) l4 @6 A# h: P$ V& h平导航,
. e: ^6 a( D) Tvigation
" n6 m" n( G9 t4 Q' `A differential tra0 p( q, J+ B7 K3 |
LINK, A short connecting rod for transmitting motion.0 a1 v2 \& g& u1 D1 F+ N
L
. u4 k+ U# I6 I( B0 @* q0 _2 YL
, j: |5 e0 \+ oc, [! H, e+ y0 D7 U
items and fuel loaded before each flight.+ S: G# G1 f1 a' a; u! R; Q
LOAD FACTOR, The ratio of the lift being produced by
3 Q$ B' C& M1 ~% Q8 R6 athe wings to the weight of the aircraft.$ v9 C, ?) V8 v9 n4 a
LOCATOR MIDDLE MARKER (LMM, MM), A marker
7 z* q3 W5 Z9 G$ F; Jbeacon that defines a point along the glide slo
' C& `. o+ O/ A3 VIL
: H( }, ]9 a, R. ]0 C) W9 [2 r) kd9 j. N. j& j+ c% q$ [1 |
LOCATOR OUTER MARKER (LOM, OM), A mark
. ]/ D ?& X8 ~- Y$ Pb
5 `2 D) i( m4 y# y, BIL
0 [2 ^' D$ C% fLOCALIZER, The component of an ILS wh" m/ t3 }) S* [3 h. N7 S
线性可变$ m! W/ b3 a, |+ Z; \, F- E. O5 W& @
具有线性反应的差动变压器。
3 F- s# S( j0 c8 e% D* p4 u连杆,
9 f, _- M/ {3 b2 }, p连接在两个部件之间,用以传递运动的短棒。" T+ J( ?& F$ U& F5 h+ ~8 r4 w0 T
水3 R# T- h6 G+ R' H4 }3 b& N$ n: z% n
见Lateral Na .% j. `' o) v/ x8 x
重和平衡表,
( H1 H9 X# F) `2 s! ?6 T有着显示每个航班前飞机的各项业载和所加燃油对重3 M9 W) B, L6 `/ l/ Y
衡影响的图表的一种表格。3 h& G3 W" H- d- w$ ~
,/ u4 T+ c- K8 ^
附近的一点的指点标。
& m# M" [5 z( M! B9 c. q* C近仪表着陆系统的下滑道截获点附近的指点& r( L6 T6 V" H
。+ v8 D# G& t5 }$ x0 L
仪表着陆系统中的一个部件。它能提供到跑道的水平航
! x, X% E( F5 y3 m道引导。* j( d0 ?6 i8 y% N# q$ U
载0 T$ P& c$ g" D/ ]. L
量和平; X- _+ C+ `0 ^5 g/ C. V3 _9 E
装载系数1 W; q d8 r/ \* l. J9 x
机翼产生的升力和飞机重量的比值。
; z, J# a1 z$ W中指点标,
" F4 ]# p: N e- }用以指示仪表着陆系统进近的下滑道上通常相当于决1 U/ Y, r) l/ S& ^! R: x
断高度或其8 a" L# U& y% W; X7 u- W# D
远指点标,
4 |- N9 M8 T0 V* P. q位于或靠
% g& [7 O; \- B# g/ {% X标" R, p5 x9 H! I4 f% w
航向道,
2 n- B2 P2 U5 L$ m! Z英汉对照民用航空词典B OEING" U" [ ^9 l/ |& F+ @
TECHNICAL DICTIONARY 94( v1 A4 d. n- X+ U/ z3 \. p3 z
LOCKBOLT, A steel fastener which prevents unwanted
6 X& T' \6 o8 C8 @; `rotation by using a collar instead of a nut.
7 c! N* ?$ E5 Z: dOGIC, A representation of complicated electrical and
) @0 h- Y( ]' n8 nlectronic circuits by simple symbols called logic
2 f+ d) B. f" i) Wymbols.
8 u& {* |1 J' j: Q, H; AOGIC DIAGRAM, A diagram that uses logic gates to! A4 M! Q2 t! K% F9 l- D8 W% D
present the function of a control circuit.* k. [$ R" y8 H7 b5 @, r- G" ]
OGIC GATE, A device or circuit which has no output' M6 y# Z7 R+ N# e4 D. ~
ntil it is triggered into operation by an input signal. A
% b8 \8 X+ ^: _gic gate is an AND, OR, NOT, NAND, NOR, or
$ V' j% o8 X( T/ WLOGO LIGHT, A spot or flood type light mounted on
/ N& T4 U# a, q& G5 j, g! a8 O+ yaircraft structure and directed toward an airline LOGO or( Y. b S' m0 g
other message on the fuselage or tail surface; for
. _( ~ h. }6 L* h6 s3 fvisibility during hours of darkness.
/ ~ Q" ?$ R; e; N6 u* ?6 `,6 p ]! h4 ~1 N% e5 ]: O3 T1 ^5 s
钢紧固件。4 E1 U# Y, h) Q3 u2 E8 _/ S, D! j
逻辑线路,
. T) L9 G& P+ q, M8 p" I2 q2 ~用简单的逻辑符号来代表复杂的电气电路和电子电路。
+ E2 P4 {8 d( l4 H* `" f( l逻辑电路示意图,
\! Q8 g/ U4 ~# L y一个用逻辑门来示意控制线路功能的图。
6 U* B- o0 y7 d4 W0 N! a! A& P逻辑门,
9 a6 R3 q Y8 b% _只有当输人端有输人信号触发时,才有输出的一种元件" C) w2 ]* y* _2 W/ e! x( o
或电路。逻辑门分为:与门、或门、非门、与非门、或非
' Q9 m0 L; T; I& o" x门、和异或门。
' l% @; p( d. f标志灯,3 s" c3 w, ~, w4 X' g
在飞机结构上装置的聚光灯或泛光灯。用于直接照在机
# x% l0 A+ }$ G5 E6 Q2 w" s身或机尾上的航空公司徽标或其他标志上,在夜航时照亮* n" p; z, W7 c3 \( n
这些标志。
/ v+ }5 j. z1 T3 YL; Z0 D( V9 l4 Z' [
e
; B9 W0 \" G( X5 Z4 y0 U. z& Zs1 Y; J. _3 P6 h+ y; @: I2 } f. h- s1 J
L ?' w, b2 G2 r" p
re
: {; A0 g% a/ U) l: Y' k* m _L
- Z3 f' ^6 c _( H9 a7 ]2 Gu
2 ~5 b- y0 h$ v/ L0 V2 p7 vlo
; e2 c1 {6 Y! A' O; |5 Q1 Hexclusive OR.
- [* M! ~( g! p9 i! x保险螺栓
' B. h* P* L: E$ }6 h& _1 p; Q1 W用环圈代替螺帽以防止不必要的转动的
$ y7 r g; y# l5 [8 A( J* A. ~# }- t英汉对照民用航空词典B OEING
& \; z. G, ?1 gTECHNICAL DICTIONARY 958 o' [8 E3 _3 C- F
LONGERON, A structural component in the horizon5 K' E: w# F& l4 T+ `$ g1 ?( @
direction of the fuselage or nacelle.
8 b: U- f! C; t& Xtal0 [1 d" x7 A1 T7 z5 j
RUISE (LRC), Cruise speed that is2 R% Z1 p" w; Z0 ^7 _3 `' D
ssociated with fuel conservation, producing fuel
6 E/ E3 @5 U, X& V5 Vileage one percent less than the maximum fuel
4 e+ U, D3 x0 d! g% _ileage available./ k5 X6 C* R$ K& h( ?' p5 U
ONGITUDINAL AXIS, An axis passing through the6 L3 Z/ d+ z: S. C
irplane's center of gravity, from front to rear.
% ]3 G& M* ^' a# n5 rnot
" M) u& _& Q* ~- `/ LOUVER, An opening with slots allowing the passage of
1 n" Z* @3 U4 m+ }6 x- a* ]0 |2 w远程巡航速度,
" L! O' F& s, Z! k6 j. L一个与节省燃油有关的巡速度。在此巡航速度下,每( T% A8 H i% G; s
一单位燃油所能飞的哩程,最大的燃油量航程小百分之* o$ ~, }! B$ I$ F
一。
1 Y) W; Z9 C t; X纵轴,
" {# O8 |+ i) [# P2 b由机头至机尾贯穿机身重心的轴。
2 j7 o2 C# z, D9 V. [. G w叶窗,- @% X$ F) f2 D% G1 A& C/ u
有多条缝的开口。8 m2 ?* r+ L. R
LONG RANGE C: n I; A* C7 b' t$ `
a( ?# K6 \; o/ ?( n+ {) p. j
m0 I1 A) x. \' b& A) N
m, W9 @$ [$ J y1 t9 @$ W
L
2 s" b# v/ o9 }0 I. ?. va
6 S2 H. ]) P7 Z' V1 @& QLOST MOTION DEVICE, A mechanism which does8 `6 X; ]* q: U) `6 h
operate a component following initial movement of
! F8 X9 G$ _# a# h7 {& Q) v- Wcontrol input.+ Q8 \" f) a, D- m0 j4 a ?& r
L T) b4 F9 U1 Y( h
air.$ Z. z% l+ S% Y1 Q ~1 D# O
大梁,7 q) ]& D3 v, Q% p( ~! r
机身或短舱上水平方向的结构部件。$ S2 {5 _8 a+ O$ X4 W
航
* _2 v- ]6 B3 Y7 ]) ~" V比
/ t7 C+ t( `% e: K, J空回装置,: s- h* S V1 N) K, G# _
在控制输人初始动作后,即不再操作部件的机制。用于
7 t- d( m2 R. J飞行操纵系统内,以防飞机指令互相牵制。) T7 K ?: T$ w! l& ] f* h& h
百
( P. z' D& U2 ^0 {0 c; k让空气流通的
$ e0 S5 G6 a- i( d) e& y* u英汉对照民用航空词典B OEING2 C- g$ |# e4 z
TECHNICAL DICTIONARY 96
' p& y- k4 i% ` {! GLOW RANGE RADIO ALTIMETER, A system that
$ _# I- b, @7 K0 I( Hmeasures the vertical distance from the airplane to the. R) q: j3 t5 P7 Z4 R3 }3 N
rrain.
# j" Q$ h2 I) u: J3 D$ x, wRC, Stands for Long Range Cruise speed. Represents/ F# v3 c, i+ Q+ a
e typical cruise speed for a given jet airplane; usually1 ]- k7 z8 v" W7 C5 w
xpressed as a Mach number.# P0 r) H6 \2 B) T( X4 a
RRA, SEE - LOW RANGE RADIO ALTIMETER, B2 I8 x1 d0 J: E% I6 W m
RU, SEE - LINE REPLACEABLE UNIT
* Q& t! f& Z+ I3 i, }uce friction
& \( v4 i: N K9 ^" Q# z( ~etween moving parts. It can be a natural or an artificial
; W$ l. `3 k1 ^* l. ]; O0 Xaterial.
# M+ W4 J# o) e* I; cAC, SEE - MEAN AERODYNAMIC CHORD
( ?8 G, X2 V4 a4 s4 jft's true5 R) u( N: y0 P" c2 o0 D6 ]2 ^
airspeed to the speed of sound at that point.
0 ~. y a l' S, F( M5 U! o* n的系统。1 o: i2 y& q+ A: y" g9 R) H
远程巡航速度的缩写。代表喷气式飞机常见的巡航速
& ?/ n d3 a" b- R- ]' P8 Y,通常以马赫数方式表示。" b7 F8 K* Q9 V, @- U
空无线电高度表,
. m0 i& v4 I6 |4 fRadio Altimeter
5 j4 o- H) c7 j6 j) {te
+ f: {1 t- c& {' }+ D; r8 Z% N4 SL) o1 q" I( @6 K' h) }
th9 m6 \* X+ d. j' B# `( S6 _; w. p
e8 V: \& P! |; _
L- G2 M3 v3 [' y: j& f+ h: q2 o
L. c# D% M. A7 t7 S$ B
LUBRICANT, A substance used to red
+ h! E1 a# @# X& n' u3 Y7 x3 U4 yb n! a( v: ^1 H# a! ?! A, \
m
: o+ M6 c: R- d0 h" s* Y) jLVDT, SEE - LINEAR VARIABLE DIFFERENTIAL! q+ [4 m: V/ z( l
TRANSFORMER
7 j/ C$ \8 C, g# M; C* c! VM# M, ^6 G1 Y3 p1 q& @ R
M
( c" K! o! w( M/ R: cMACH NUMBER, The ratio of the aircra1 U1 N7 Z ~/ ?9 v8 E. q9 M$ P2 I
低空无线电高度表,& n. x6 R& v/ Q6 q
一种测量飞机至地形的垂直距离2 S Y) a, {2 m; ^1 ]8 L R3 m
远程巡航速度,
5 v$ \9 T8 R5 o* f" F度6 L, h& X1 V: P- x
低 b' Q) R7 q( t5 o4 J( R8 i
见Low Range .
0 H. ?' a: Q- B1 O5 C线可换件,5 I8 {9 K. r! I3 T5 S
见Line Replaceable Unit
2 E, r9 O/ _+ B+ y航2 D$ L4 v$ z, S x- J
.
+ Q! q1 F* Y0 c. k) ^' r用于减轻运动物体之间产生的磨擦的物质。它可以是天0 w- d5 T' l% Q' D
的或人工制造的原料。! k' w9 n4 H1 v: a( E5 f9 ? F/ `
见Linear Variable Differential Transformer
+ E. X4 C/ n3 D( w$ M润滑剂,
6 p& Q0 W, v! | m7 r4 U' X# w6 F然
2 b: K( @/ y5 s4 }线性可变差动变压器, j G1 t$ L2 I5 o+ C2 b+ u* y" l
.* \- Y2 h; B) o
均气动弦," J! a/ l1 Z6 R8 B( N
见Mean Aerodynamic Chord
# i' M. W, }! ?; k. n$ N, K; p9 K平
4 e$ |& k) G$ ^* z.
5 m0 Y# L6 X+ I* [9 E空速与该处音速之比。, l+ ^4 \9 Z0 w* v
马赫数,! `( R: `& f& @( ^# I6 V
飞机真# P! M. c7 G: |
英汉对照民用航空词典B OEING, f3 _( c4 J! r3 }- p
TECHNICAL DICTIONARY 97
# e/ l6 p# z* w y) y1 aMACH TRIM, Correction to airplane attitude (nose up)) G9 u9 @2 M8 E; v4 d' a; `
during flight at high speed by using the horizontal
- H# Y3 U: }. ?0 G; v# Vtabilizer.
; Z% S3 u( |7 M0 J% {( \AGNETIC HEADING, The heading of the airplane% D/ J F5 l( g3 Y5 ^, v" @
lative to magnetic north.5 L0 U( E9 j) ?2 `5 w0 m
AGNETIC VARIATION (1), The difference between
7 D; n+ E7 f6 K3 Gagnetic and true north.
5 H' z& ]$ o( `8 M4 W. }north.2 a6 ?( a; l. a7 c+ e T7 q. b
here is a continuous small change of direction5 ]2 K1 |" E* E3 ?
f lines of magnetic force over the surface of the earth ,
1 \' m, q9 |% D4 g) S% P& Uagnetic variation at most locations is not constant over2 g1 |; b$ W3 }% I6 I+ Q
ng periods of time. Lines of equal magnetic variation
4 Y' ^# C* W0 S1 A. E! de. (see
- a, a0 H1 y! _" dtation Declination: h. @$ ?. j! w6 i' R4 d" r m
s
1 \) h, Y) c6 S! T& {M
: P1 _; c! ~' q, j7 are: L# P" {) J. w
M: U1 M1 w5 J D7 j% T \3 v
m3 X* H7 Y; e+ T8 E. d% G3 q( {
MAGNETIC VARIATION (2), The orientation of a
9 d: `; Z5 x, Y( K. ^: p: @+ b" qhorizontal magnetic compass with respect to true
" N; f2 T+ {3 U2 ~! LBecause t) A8 d- D2 {! p9 k
o0 M( `' {$ L9 I3 s
m
9 m* }8 v5 Q+ U6 o' G& [lo
4 @/ c# A, z/ t7 q(isogonics lines) are updated on Jeppesen charts every
: N, I' p9 ?7 ?" X* L- P; c* mfive years in accord with worldwide practic. q3 \ v- Q; Q$ ~
S ).1 |6 w4 [3 N5 d4 J& s
MAIN ENGINE CONTROL, A component on the engine2 \2 Q1 C; \4 _( Q6 t8 l" r
ration.
9 |" ]+ t# A8 a. M2 TMAIN GEAR, The main wheels with the attachments for
( G* h$ c, R1 x; osupporting the airplane on the ground.
' V( S) j: J% _0 Q+ f- ZMAINTENANCE, Work accomplished in support of the' y; R9 b2 Y3 Q
structure and systems of an aircraft. It includes,' |) e1 D- x; }6 L H- h. X' I& W9 |
inspection, overhaul, repair, preservation and the
( n5 e) k* _) ]( Kreplacement of parts.% @1 g! A6 I8 U9 \' I j2 T: v5 g k
马赫配平,
# i* h; A. V$ @8 i用水平安定面对高速飞行中的飞机的俯仰姿态所做的
, F2 V/ d) {0 [% M( e调整(机头朝上)。
. c: m# w+ {5 j* b磁航向,1 Y( L+ V& p/ Z6 q2 H
相对于磁北的飞机航向。8 @% x( a8 ~8 L5 f; G5 `3 k3 t8 q
磁差(1),( N. Z& w: m2 ?
真北与磁北的差别。
' m1 ]. W# W/ _+ a) C/ T& m断的微量改变,磁偏角在长时间内多数是不一致的。每, }, `, ?2 G2 H9 _
五年Jeppesen手册会按照国际惯例校正等磁偏角线(等
* n$ V& {4 W: Q {差线)。(见基点偏差), Y& t8 \* W, u! q
主起落架,/ P* _$ `5 H+ U) k
用以在地面支撑飞机的主轮及其附件。5 S/ ^: z* g& U, R
维修,9 a& n" g5 w, f, j+ |/ p3 Z
在保障飞机系统和结构时所做的工作。包括检查,大修,
7 S5 D) w u$ ^; \) L f修理,保养和部件更换。
2 {* `& I3 U: u" @7 rfor controlling fuel flow for starting and engine ope- n" c2 u/ p# Y, b- m5 N1 b6 h: k
磁差(2),
3 m. }/ |( V' v( A& g相对于真北的水平磁罗盘定位。因为地面的磁力线在作+ k; Z, i$ T& B0 S3 l9 y5 Y
不7 t; P: z! P, Y7 g& Z5 U/ K& l( ~- M
磁
+ r: v4 W: i# j& d主发动机控制器,& x( W2 p/ m7 H3 \6 ^' Y7 v# B7 }" M3 A0 T
发动机上为发动机起动和运转控制燃油流量的部件。
: S) }7 a$ g, m& B; u# | U英汉对照民用航空词典B OEING
- |* p I4 d" d# ^+ [: VTECHNICAL DICTIONARY 981 V; Y6 m7 X; F+ H# x
MANEUVER CAPABILITY, The ability of the aircraft to) q5 m" m- O1 a1 E/ ]
ertain load factor.7 U% D. P D" n, F3 \
MANEUVER MARGIN, The amount of residual: Z/ ]. h8 L8 W* O+ Q6 g/ n. U
aneuver capability present before the onset of buffet.' u2 h5 A' B) D O
MANIFOLD, A duct or chamber with several inlets and
3 V$ I3 {2 B) X. | ~4 n) houtlets for air or fluid distribution.
/ i9 c9 U6 Y+ W, w- o5 qthe
% l% u0 i9 ~& A, g. h4 `0 Ylow of
. S- B9 c! ^$ W7 L/ Re flight compartment. On specific
# s8 _7 @" s- Q9 m" hccasions it will provide conditioned air.( l) ^! q2 ~0 u
omponent by hand.2 P& x0 _ w2 ?3 g# m5 D
MANUALS, Books with instructions for proper8 t& {/ T3 |7 ]: K# f5 t5 c
maintenance and operation of the airplane systems.# I8 n4 e: i1 i; }* L F9 ^
MANUFACTURED RIVET HEAD, The head of a rivet' H2 i* [( T5 Z! k* e2 i8 `
that was preformed during its manufacture (see upset
/ ^% m' _; E; s+ [" s7 B2 tperform certain maneuvers up to a c0 X# q$ Q' t9 w. ^
m
& ^' d5 H0 |" o3 NMANIFOLD INTERCONNECT VALVE, A valve in8 A" R: B- Z) j4 }
equipment cooling system for providing a normal f2 f2 C z: T1 q) ]! e6 M! f' u
recirculated air to th
# @0 ?( j* k3 ao
) J: j2 K- Z& |2 G4 x% s0 }* QMANUAL OPERATION, Method of operating a! |# X& t% y! k' a) M& o" M
c3 e; [. ]8 I& k. P7 @3 E R c: ]. C
head).
2 Y3 d4 f8 e- z2 S+ @9 _ LMASS, The quantity of matter in a body. It gives the
% o, k" o; g7 @, Mbody weight when it is exposed to gravity.8 z9 A" e" H. p& T
机动能力,
3 v) b" Y8 |3 I+ T! X' ^飞机完成装载系数达到一特定值的机动动作的能力。7 Q P9 U9 d, ^. K! f
机动性余度,1 I1 ?& B' b5 A0 U& q' Q
飞机在遭遇抖振之前,所剩的操纵能力的大小。
( z! q7 B* D# |5 \0 D5 e总管,# h2 F9 Q& L; i4 e: I
用以空气或液体分布的多进口和多出口的管道或容器。: f) N! M6 U: O* K+ k
总管联接活门,
8 u6 m# G. q6 E9 ]& s7 A; e4 E设备冷却系统内的活门。用于向机舱提供正常再循环空
. M) E$ ?3 F; g7 x: x% \- ?1 {气。在特殊情况下会供给空调空气。
2 c, X. W9 S! }' _5 V7 _3 v人工操作,4 z. Z% K& b7 |' O4 @* ^' L
手工操纵部件的方法。
6 \( P" F9 ~/ x" t明书。
1 [! w$ [* B3 C3 c铆钉头, x9 ~) ~% d0 W; g
在铆钉制造时已定形的铆钉头。(见膨径头)。5 [: g7 I! x) i0 M g6 D! f
质量,5 i4 F2 q$ `! ^( L
一件物体的物质数量。当该物体受到地球引力时质量产: P- E- Q$ A) `. J- T# A4 n
生重量。2 M3 _* y# P" h& U
手册,
+ T0 W0 y4 N! k0 X' w为能正确地维护和操作飞机系统而编写的说! j! W0 h( h- \
机械制造的+ }% q; E# a* f9 h3 e- J0 E" ?9 [
英汉对照民用航空词典B OEING; }- d2 B3 b- i* b, T
TECHNICAL DICTIONARY 99- h- M4 ~$ T# B
MASS MEMORY, A memory that can store large
2 a6 L$ R4 a: P. Lamounts of information and hold that information. v1 ?8 B0 h5 o; o
permanently.2 g" \# ^1 @ ?! s# n4 E3 y8 E
AX CLIMB THRUST (MCT), Maximum engine thrust r: L! ^9 L( p2 C3 J6 K
ximum engine! ~+ I% c- z4 e& Y4 W/ J9 L2 X
rust to be used continuously when one engine is8 `* \& A* l) i) f: }# D- q
operative.
+ l% u7 k) {) zEOFF THRUST, Maximum engine thrust to be
( F* e: W8 u5 qused during takeoff.
! c0 \( D( E" D# g* D3 SFF WEIGHT, The maximum take off3 O X0 I0 Y; z0 H0 E# l
weight as permitted structural limits or performance! o Y4 t5 ?6 \- e0 O9 g1 I* k: q
limits, whichever is lower.
9 G+ ]: O% M! J7 ?" dRANGE CRUISE (MRC), Cruise speed
! \- X o6 `( u) R# H* g! K. Aance
, `. l+ T3 f# L5 l2 ito locate) m7 [5 t+ @- K" R3 X
the Center of Gravity.
. o) Q- j- I" s8 y& C' j/ G, a% I主控台,
* F; O, _; W' |1 f控制系统操作方式的装置或系统。
. e E2 e! ~1 J" t" E大爬升推力(MCT),% E, J H5 N, O
飞机爬升期间所能用的最大发动机推力。
' m: w7 J2 L( M- UMCT),9 g. l8 m5 M6 ~1 k- L* }
当一台发动机不工作时,可以连续不断地使用的最大发
- u$ M: t2 w. _动机推力。
. i) I" y L* j) w, @: @2 a4 |" S起飞期间所能用的最大发动机推力。0 z0 z. _: r/ g1 n
结构极限与性能极限两者中的小者许可的最大起飞重6 o3 a6 X- A Z
。
2 n0 m9 ~. Q6 u( J0 J+ L" M2 V大航程巡航速度, b# a9 e- ]. L& F: K( X
最大的巡航速度。4 v2 x+ g& ]+ y8 w: a, N5 K' ]# m
平均气动弦,
& Z: L$ i! s: }! M% Q9 Z确定重心位置的基准
4 d5 w+ C- g0 V. l7 p距离。2 k% h9 a/ v9 k/ o c( }
MASTER, The device or system which controls the
9 [; t% S: _2 M* ksystem mode of operation.
/ A' O7 U Q! N0 jM( @7 W+ a% g: T8 Z7 I7 l
to be used during climb.
5 D* _) W3 `9 Y/ m d/ y" LMAX CONTINUOUS THRUST (MCT), Ma/ m4 T9 M1 {& d- g" x
th
4 ]; t# J- v8 R( A6 E( Iin
+ H8 h/ F; ?' N0 b$ p4 VMAX TAK0 j* z, f; k$ ^& G, F9 G9 t
MAXIMUM TAKE-O3 B' t# b. a! y- [% W; j+ E! C
MAXIMUM+ u5 f9 d R7 J" j) C
producing the greatest amount of range.
# b) G5 M7 D9 N4 l1 ZMEAN AERODYNAMIC CHORD, Reference dist
8 u) W. ]) ]( J. ~located at a fixed position on the aircraft used
- I- u* I( K0 L( v" }4 v9 K大容量存储器,. e+ u# {4 V* P ~/ i- T
可以储存并能永久保留大量信息的存储器。
- r! M8 k* Y) a/ |最/ G* {8 e! |: Y$ P, {; j
最大连续推力(
5 L) m# H5 ~; V" b& V最大起飞推力,
) l+ S7 {# |7 j3 I1 b8 F" r- H最大起飞重量,. @. H! N( M' e1 { |3 p- @
量5 F, B/ ~: x( t. F
最
1 c0 {! \! b2 `" H( s2 D% N能使飞机航程+ Y" _+ W, w' F; h$ I% s; U
位于飞机上一个固定位置,可用来
1 S! A. C6 M/ j/ u5 `英汉对照民用航空词典B OEING; F. e+ P" d7 j2 _) C- ~
TECHNICAL DICTIONARY 100) O! ~, c1 p/ A/ F ~2 U- q& o
MEC (NO. 1), SEE - MAIN ENGINE CONTROL( c! z* x. C" M/ O- i' T" E
MEC (NO. 2), SEE - MAIN EQUIPMENT CENTER
( S0 X' M9 F) J& V9 cEL, SEE - MINIMUM EQUIPMENT LIST
* T+ x& J6 p, H1 t0 H1 Utem the memory is where5 G, t+ t! F- d) N {
formation is stored.
, @! S. v, S; W3 wMETER, Any mechanical or electrical device that is7 ?6 z! V. G- g" F! z% {4 Z4 M
air or
" w0 G8 N. W0 ^% |4 ypoint along the glide slope of an ILS approach. It is
- T# F' n) ^- hnormally located at or near the point of decision height.% k" l& ]/ f1 e) e' {- y
,
x8 Z: b( ?4 S2 f见Main Engine Control
; Q/ x' Y7 o* n* P' p1 o4 j4 mM B9 R4 r8 k: W! Y
MEMORY, In a digital sys: m% Q3 z. r( R) f
in
1 v* d" ?5 {. ^# J4 n. }, ~used to record, indicate, measure or sense a specific
]9 V! h, i; a0 V9 xportion of an operation.
4 Y k1 t6 A8 m, t/ jMETERING VALVE, A valve for controlling flow of
1 g* \( Q h: X: ~1 T6 |5 k0 ?fluid.0 F" A0 x5 n4 v& \1 B) M k6 ^- y
MICRON, A measurement of filter effectiveness, one
5 e+ ~2 D3 i# \0 x2 y' ]micron equals one millionth (.000001) of a meter." Q# Q( z2 @7 o+ t
MIDDLE MARKER, A marker beacon that defines a
{4 n( d3 }. L" [- m发动机主控制
# J6 e' |- U% i9 D8 z3 W; ~2 @.( k1 \5 L6 w! C# A9 b3 m
设备中心
5 N& {1 T5 d4 b3 S+ ~3 a7 G见Main Equipment Center; {, C! O0 d( g5 E8 w
总5 G+ Y/ q* \7 K A
.
5 n/ S; E8 E, c- M! ^( X a7 q低设备清单,
2 w) j+ c' d# h$ D见Minimum Equipment List: o4 H0 D/ f# p6 f$ f$ f0 C! Z
最
$ G- J G" G7 L: F+ N.0 \7 }' F" t% T% J( u/ N* F& M
在数字系统中储存信息的地方。
4 |9 {& ^+ j- Q, |: U0 O计量表,. w2 V: V& @) E7 j( N8 w
用于记录,指示,测量,或感受一操作过程的一个特殊
# R0 z# u5 u0 `# ~- k( U, ]部份的任何一种机械或电子装置。
& Q p/ \8 g' C量活门,
! ~. i/ I* D6 x! D用来控制空气或液体流量的活门。
3 @8 \! c3 L* G) C# f; M微米,( B2 a% R& h' i- Q' Q" V
过滤器效率的计算单位。一微米等于百万分之一米。
# ?/ |' h2 W# X. f在用仪表着陆系统着陆时,用来确定下滑道上一点的指
, m- e/ Y+ i* c0 |* e! t ?2 C点信标。它一般位于或靠近决断高度。
$ A" H. g; A6 u: c j+ M# i( _存储器;& W1 W: g! V1 v
计3 | v9 V6 o. @" W0 x
中指点标,
% k/ ^- b7 f# P, _$ [, {! |英汉对照民用航空词典B OEING9 ?# _8 @3 @* _3 [$ D
TECHNICAL DICTIONARY 101
5 u7 _7 }7 ]3 h4 |7 t1 t6 IMICRO SWITCH, A miniature mechanical device that
+ t& P- @0 |$ _7 f9 tcompletes or breaks the current path.& l3 ^2 ?9 [) U* Q( @
.7 H5 b; C& d2 f, Z T
MIL, One thousandth (.001) of an inch.
: @# h6 }, a- o/ i N9 K2 pILLIBARS, A unit of barometric pressure equal to4 B0 @- v$ c. `
approximately 0.75 millimeters of mercury." y( P/ n/ A6 b. O
The lowest# @' D9 _' H' S( z" }' z
ltitude to which a descent is authorized for a
! e; ~# L- s+ O* \7 h* @! o( |onprecision approach.0 b7 Z& R4 B" K4 ]+ Q6 n1 b
INIMUM ENROUTE ALTITUDE (MEA), The lowest
" I7 E4 V) P6 |9 b, \ublished altitude between radio fixes that meets
# T# q& c' q+ U9 V: W' jbstacle clearance requirements between those fixes& b5 S4 ~ O7 D% S- V" e/ |
and in many countries assures acceptable navigational* w$ j( Q8 Q3 K2 r( M4 f
signal coverage.+ g0 v- J9 q9 r$ z$ r& b
operation of the airplane with certain systems or
0 r1 V7 m% }5 nsubsystems inoperative.
' \$ n/ ^# z& ^+ J9 o& aapproach
1 P3 U. O }; W: w# D8 R' @2 E* kcannot be completed to a landing and results in a Go-2 Z; ]7 C3 i: O( u6 Z9 q- a2 L; y
Around.
, f& c& W% Z6 E' P- q6 m6 Z" a一个能形成或切断电流通路的特小型机械设备。
2 s% U3 H: |) r( Y2 W# M$ k5 \话筒,
: z( B& ^% k7 S ]( |6 r话筒一字的缩写。, x b6 @" ~; T3 N/ X; c
耳,
2 w% s/ k* x& G, i* ^! ^! `9 {一英寸。
8 }2 p! X6 S7 S+ K毫巴,
. |# Z8 p, [; k* y) u一个度量气压的单位,一毫巴约相当于0.75毫米汞柱。. B4 f' H1 E4 q# u! r6 p X
低下降高度(MDA),
% K' T- o* W: |* K飞机作非精密进近时所准许下降的最低高度。* R( ?* T9 ~2 e: ?
低航路高度(MEA),! a- B! m+ ?+ U# X5 X5 m" o7 r8 Q
在导航用无线电定位点之间,符合越障要求的已公布! j) t/ v, T8 i6 I( g. T
的最低高度。在许多国家,最低航路高度保障了合格导航
& R0 L/ F5 e# e" w9 ^信号的接收范围。
6 O* B& w0 d# J" P. g+ Z最低设备清单,
$ f/ [. E3 m5 P0 ]何
2 m4 U& S1 c( C2 n2 Y作飞机的文件。$ B1 ^9 E% T5 c: p& _
复飞(MA or GA),) |: v* `9 q( n/ i6 ^
飞行员因未能完成仪表进近而导致复飞所采取的一个
8 k$ @7 A) v; V+ g, J机动动作。
% V3 k0 x2 o7 g) {/ e7 oMIKE OR MIC, A shortened form of microphone
9 n9 [. q' p- |+ H1 cM; k% m0 n* j. H) }( O! }$ ^
MINIMUM DESCENT ALTITUDE (MDA), z3 j: X4 [- ~8 r5 ]6 Y
a
9 ^( V" h3 M# ?n
4 y( [9 I. f& S& Q5 Z! u& D5 gM
/ ~* P9 } |2 Y' P! Yp0 q; C) `+ ~/ e% J: o* @
o
" S. t# n. A4 P7 G! r8 I4 }MINIMUM EQUIPMENT LIST, Document prescribing
4 l9 S7 }* X: Q8 B. GMISSED APPROACH (MA or GA), A maneuver
: n' U# D9 B$ ?( m% D4 ~conducted by the pilot when an instrument
3 q# @( |3 z z; O微动电门,
Z0 b9 D1 ]/ u C. k, N: i6 s i密
- z$ L. q) c, Y* X7 o6 f# E千分之& K# R4 i4 O( X
最
& V {- O4 z( O4 s最
* B; ^8 @& v! e指定飞机在某些系统或子系统不工作的情况下,如* U. d! K; Z) R; J9 R
操
, _# Z9 x" }; [' t1 W$ R2 d# a英汉对照民用航空词典B OEING
% R$ v1 C1 x- [+ v/ e! @# [) ~TECHNICAL DICTIONARY 102
. E0 b- p) z( y+ | FMIX VALVE, A valve assembly with two or more
* l: s- h0 d3 b5 K6 y' [/ Xindividual valves used for airflow distribution in air5 k% _+ [* d( I* z+ l5 e( Z
stem.) t. s) H! R8 T" w
MMO, The maximum Mach number at which the aircraft
) M5 x5 C3 v5 K9 B" |+ a% @MODE, A specific operating state or condition; i.e.,
, s! k- Q% G" |9 i! X7 oAutopilot mode, MAP mode, etc.! T* L, Z8 {2 }. Q
e" w# N9 ?3 C: n5 j, C& j8 @
MODULE, A housing that contains related system: [9 u* U/ l' q2 A: z
MONOCOQUE, A type of construction in which the6 l, p5 ^4 Z$ g) [, H7 E w
ONOPOLE, A speed sensor that senses magnetic
& E2 T* P4 D8 C! X6 }pulses from a magnetic nut or gear teeth on a shaft.1 u3 F) x3 V. O8 Y& p8 j
he controller.
; [, P/ v) o; C$ W$ PMOTOR OPERATED VALVE, A valve using an electric4 X$ E& m: C6 |: f) J9 m6 A
motor for opening, closing and modulation.1 f# u, N/ w* d. e
个以上单
! w3 ~& R l3 l6 Q8 E活门的活门组件。
( W9 s0 c, T5 w5 ?( E6 E n飞机可使用的最大马赫数。: x5 @4 v0 j$ S
式,MAP
: t3 I9 t9 J3 I: j g( f# y方式等等。
% @# d d, S) ?2 T- W调制,
V" w c. a1 P5 d3 V组合两个或两个以上的电子信号,使一个信号随其他信1 V! H' t: R! J. ?7 L4 A
号的变化而变化。
' ]7 g0 G! h/ I7 i1 e* T组件,
- d2 _- R% \; e极,
6 H- R1 h1 I: j7 b1 a x# \帽或齿轮轴上的磁脉冲数的速度
$ `, _9 K4 `( C( ]. x/分钟。6 N" r# |$ V+ l" [# g3 m' F
用电马达来开、关和调制的活门。
! D V8 e$ L! d! `conditioning sy
( y- j5 u, U" ^( Imay be operated.3 Z6 z, ^, j) u5 K) N% S
MODULATION, Combining two or more electrical
b9 i' G* W" h6 K2 C! @signals with the result that one signal is varied by th4 t; K: Y/ f/ x% e) X
others.
8 H: `: J3 `( O/ J# P+ V; o* L: qcomponents.
% r `/ C5 y* D/ j2 ]3 g" pfuselage skin carries all the loads.
+ h- X4 v6 {7 W) b% H/ NM. _# C& y2 Y4 V7 m
These pulses are interpreted as RPM by t
" m. w+ G3 x: a0 ^, Y混合活门,
/ k' L {2 s4 Z" K1 B! k/ Y5 D在空调系统内.用以气流分布的具有两个或两& R( P6 U* x' O, Z
体
d& H4 {! r+ q' ^MMO,
# Z; E. q+ u9 V. P, A2 @9 p- r方式,
* K4 c; l9 b+ `# t3 l' g B/ \1 N U一个特定的工作状态或情况,如自动驾驶方
$ y; {5 B+ d) d1 Y" i内装相关的系统部件的机体。
; W# U9 R; b u( y3 A+ J7 D硬壳式,
4 j6 J. V9 H( y; r机身蒙皮承担所有载荷的结构形式。
8 ~+ F9 D2 A. _3 z" u- b# w单
7 J% A8 U9 F, P. f+ H- q一个能感应到磁螺8 F# g. E: J) O# z3 |( P
感应器。这些脉冲可由控制器译成转% ^4 U6 h+ H7 z+ i
马达操作活门,! c. H4 t3 J& W# m( F l
英汉对照民用航空词典B OEING
, r2 M" X) o7 j" w& `TECHNICAL DICTIONARY 103
5 W" B( k% O8 {: w- cMSL ALTITUDE, Altitude expressed in feet measured2 B! U4 p+ I5 m, I6 N- e
om mean sea level.
" {' i7 D8 E X* p7 x+ C6 N# ` U& Freducing the noise of the airflow through the pneumatic
! M5 h, s% }$ w" @! q7 a6 wduct.# e, H* k# G0 S M
MULTIPLEXER, A device that allows two or more
; Z( S3 D" D. {- W" Y# H/ o1 Csignals to be transmitted simultaneously on a single
0 A+ V( M% \- T9 z3 `6 j- u9 ]7 Wcarrier wave, communications channel, or data bus.
f( S t% n5 o1 O8 j7 Pessure compressor rotor. c7 y5 j0 t( `$ s0 P3 V' a
N1 BLOOM, A change in engine N1 and thrust indicated
% U7 H' o5 A. z1 F& @5 e: L3 t3 pN1 gages and detected by the autothrottle BITE n; k+ F0 q; H+ c, y; X% z
during throttle hold operation.
; r- b" J. f* ON2 , High pressure compressor rotor speed.
5 V9 F' ]+ e+ G5 kACELLE, A streamlined enclosure on the wing or) t' [/ P/ T( {( s% @2 V4 K
面量起的高度。
( _( O4 f5 X+ U, T& }) _经气源管道所生的噪音% R% J. `/ `4 M0 w7 V" W
的装置。 ~' H5 s0 |/ X# S- _
多路传输器,
# q% E/ Y! y4 i2 t6 q7 i1 P一个能让两个或两个以上的信号同时在一道传送波,一
; G0 M$ l. q0 _3 d5 ~条通讯线路,或一条资料数据总线上传递的设备。- G9 K" Z0 g& r% ?( a+ K
N1转子转速,
) h" j3 f3 Q5 k" P+ e发动机低压压气机转子的转速。
- x9 V& p1 s* v* W2 I! H9 X0 h% Z) ON1激增,6 Q9 n$ j* K8 o2 e8 t0 B4 T7 v- T
油门保持过程中,在N1表上出现的由自动油门自检探
S8 g) t4 m- l" w& k测到的发动机N1和推力的变化。
1 ]. s! X& S# ~7 P0 XN2转子转速,
; @; s7 [! U' l9 p/ G发动机高压压气机转子的转速。: D% z! w( F7 N% u( D l
短舱,
: s/ x0 E+ S9 W- G: `( s6 x机翼或机身上为安装发动机而用的流线形壳体。8 K/ m' j; f. d& ?0 r! u
fr( l9 x6 z! T3 f
MUFFLER, A device in the pneumatic system for& }2 z. |6 [, U* N% z# l( d
N
. Z; t$ Q& F, Z. fN1 , Speed of the low pr' k8 ~" f* [+ H$ }% a
on the
) C% M7 @: r2 N6 eN, h9 b9 P4 g6 n, `% `, j2 B
fuselage for the engine.
$ h' I) L1 S, n2 O平均海拔高度,! `0 F& ?# G1 H+ w
以英尺为单位,由平均海平7 ]1 X' v" F( |1 T( m
消音器,
) I; e4 j) m5 v+ w在气源系统内,用以减低空气流
: k% l8 s+ p' |- I英汉对照民用航空词典B OEING( t6 U1 T/ Q/ H9 } f; G
TECHNICAL DICTIONARY 104) x! G( a6 j j9 c9 H3 |- i
NAND GATE, An AND gate followed by an inverter to! ~ w$ W2 j* e6 b; [
form a binary circuit in which the output is logic 0 if all
0 ]7 x, q1 B' |puts are logic 1.5 G9 K& X3 A! }5 n1 @2 `
AUTICAL AIR MILES (NAM), The actual air distance
/ k5 x: R' q/ wrespect to a
2 Y% R4 i1 F- o0 ~& c- l+ \tationary object., n8 U) z1 K1 R
istance
; p2 @( r* _; f% y6 Htravelled in relation to the ground expressed in nautical! y1 r! V" @% m! ^% ~& G; s
miles.
! x p7 H9 E! m' `8 E: p* ance equivalent to 6076.1 feet R1 J4 ~( {! |. i
r 1852 meters.8 h; G- n. N6 q% M R
hical) ~0 r9 b: g, C! U: P, ~7 i$ ]
EGATIVE LOGIC, A form of logic in which the more! C6 s! r2 k8 Y' V9 Q9 a
negative level represents a logic 1.0 Q! o; n+ S* r' Z
EGATIVE RELIEF VALVE, A valve in the1 o9 J: {3 e8 x( o$ V
e to be
+ _1 F5 c6 o( |6 {0 @# f) a; Nabove airplane altitude (or cabin pressure to be below* g6 x, W: x7 B$ s: m
ambient pressure).+ A- d8 k' i5 g+ r
有
$ _8 y) X/ t9 K* [人为逻辑1时,输出为逻辑0。
Z. V2 n, c) f6 |* A% D9 j v海里(NAM),& P ? X1 T4 j% k" U6 n- @! H* d
来表示的飞机在空中所飞过的实际空中飞行距
% e6 `- s# ^3 v6 \! ^' O8 O地面物体。
/ c+ V% ^4 A$ G) t% A以海里来表示的飞机相对于地面所飞过的距离。
$ H! m5 Y3 p2 j8 f7 f$ U里,
* P' n6 P; M" Q3 |; O; Q) @相当于6076英尺或1852米的距离单位。. i7 a1 B7 \ H1 |7 O2 }
导航,
# N1 R. v% J9 Q! r反逻辑,
* ~5 r% I) M) ^. m8 ?正电压水平越是代表逻辑0,负电压水平则越是代表逻
; [0 D+ U6 n% J释压活门,
3 h m/ Z' j) Z ]- b& @( P3 ?增压系统内,用来防止机舱高度超过飞机高度(或机舱
& o# ~4 F5 ]2 ^$ E4 j/ q. |+ A压力低于外界大气压力)的活门。
: m2 [# X H" s$ n- O. |in
9 }, p t9 ~. z' n& V+ X: d6 G$ H! rN3 Q- t0 S% Z+ P; g4 ?
flow expressed in nautical miles without
9 n4 L6 M' S) R* Y+ k$ Zs
* y' v L5 _" ~NAUTICAL GROUND MILES (NGM), The d. T% h3 S' d9 @, o
NAUTICAL MILE, A dista: f- |, y e; a0 k6 n: R5 c
o& M- ?/ ^! G+ U, P
NAVIGATION, The art of determining the geograp. h/ d }, V! h$ X: z" t2 W) {
position and maintaining desired direction of an aircraft6 b0 ^8 S, q- t ~* h9 X1 O
relative to the earth's surface.
& F- B4 M( Q7 }( MN! j4 Y! C9 W, _' g: C1 k
positive voltage level represents logic 0 and the more
. s; M. Z* `# v( QN
3 }3 |9 O+ O. k; S& wpressurization system for preventing cabin altitud: S1 N; w3 M: @6 g! U" U, g
非与门,
3 y% P R( e, p9 i2 F7 n在与门后面紧跟着一个反向器的二进制电路,当所
4 n$ s4 [3 z# S j输" e" V) P6 o+ L* B5 @
空
8 b u( L1 d$ P1 W4 [( p4 c( r( h7 f以海里. t2 h7 z$ t0 {: @9 ~3 b; U
离。空海里无需参考
5 t- A: M" _, Q D地海里(NGM),+ I9 p) w( l& F) G0 U
海
5 Z9 B& M" G$ a/ ^9 \: E决定飞机的地理位置和保持飞机相对于地球表面所希
6 c& L; R7 w" G& k; P望的方向的技术。 B6 f0 p E5 E* V( L0 t) ^+ `5 ~
辑1的一种逻辑形式。
, y1 r$ x" y3 d3 q' `负
, E3 H/ ]' q* R$ x. N% s8 d英汉对照民用航空词典B OEING- s7 S) V$ r+ I; ^0 U6 J, C
TECHNICAL DICTIONARY 105
1 I% l4 l% k. v- [; M% S4 u: `NEOPRENE, An oil and grease-resistant synthetic6 V) i" k% I7 o7 C0 J
rubber. Used mostly for seals and self lock nuts, etc.
7 N1 w0 z) ?' `+ k9 |! gEUTRAL SHIFT SENSOR, A sensor used for5 {: j3 _! m3 Y" r a0 }
NET PERFORMANCE, Aircraft gross performance
9 L4 D; d# \4 N! Z% rcalculation
* G% h+ v4 f. A& K1 ^/ O3 Q$ E L( gpurposes.
, m. I+ N/ o. `8 nNICKEL-CADMIUM BATTERY, An electrical device for
" y. Q% A9 P* qchanging stored chemical energy into direct current. J9 ^: b1 a! H8 ?9 K$ X! c
ses nickel hydroxide, cadmium hydroxide and
$ k; [1 \6 _& k" \, H: Dotassium hydroxide.. ~/ N- F7 T* J+ G+ E
NOBLE, A term used to explain the properties of some! i7 t9 h# B( @. ^" W
lements that are chemically inert or inactive.( y% d0 Z# j% C; v2 A
NOISE ABATEMENT PROCEDURE, A flight path and
# R `' c! |6 E: Elimb profile designed to limit noise in the airport area.6 l5 z' A- D4 |3 |* m$ `
construction. (Nomex is a trade name.). @+ ?$ L* z! n3 v7 p; k$ B$ A
in only
% Q# P0 H6 s: Y0 t. d- Qone direction.
7 V2 i$ W# D& W3 e' P氯丁橡胶,/ |5 @7 i: G5 A- y* j7 g
一种耐油和油脂的合成橡胶。多用作密封装置或自锁螺9 U: |/ r5 F8 Y2 r/ G6 d
帽,等。; j! f! p j* C- R
立变换探测器," {$ t% Y2 D" z+ s
用于探测升降舵和安定面配平状况的传感器。
! D, Y/ J, G4 _2 Y! Z性能,
/ e! p9 V1 ]& @" S' ^机总性能减去由当地有关单位为了使性能计算
0 |2 |3 R: j! b$ [) C( F6 X8 [) G较为保守所定的一个量后所得的性能。
/ z3 M8 P3 p( Y8 U9 d3 X1 g为直流电的电器元件。它使用氢氧化
w+ b7 a1 |/ a5 F1 e、氢氧化镉和氢氧化钾。$ y8 F5 J7 A: o
性,) x' k5 m* c* D; J
用于解释有些元素不易起化学作用的特性的名词。
. O) J K* ?$ I+ \0 m& s低噪声程序,
8 ]* i. B% f" P7 n2 t( Q一种为降低机场地区噪声而设计的飞行航迹和爬升剖( l/ v5 H' }6 ]3 ]! Z% Z
。' r N6 e) M$ y' |* G" E
是一种类似纸的材料,用以制作蜂窝结构。(NOMEX
/ v( N3 b6 E6 B3 C商品名)。5 U! z' T; e: z8 h
只允许向一个方向流动的活门。
, O& `$ [0 |5 R0 aN7 p4 G' y3 r% X, c% D
detecting the elevator and stabilizer trim condition.
6 c% t( `- k$ \/ b4 T7 ddegraded by an amount determined by the local
3 a! @ q7 J2 b/ h* _1 W6 ggoverning agency for conservative
1 \" o( K0 v6 w9 x3 c3 V) [1 }U
8 C9 N7 u$ W1 K/ np3 X; z+ K3 D$ n/ n
e1 Q! j. I( i; [( S5 i9 ~' P
c) f6 q4 u8 ]8 C3 r" I/ X
NOMEX, Material similar to paper for honeycomb
. h/ S4 j+ G" l7 Q/ v* ?6 DNON-RETURN VALVE, A valve allowing flow: Q! h* E; N( F9 j# C: B+ M
中
/ K8 f, h2 m* ?( {* Y$ e净9 J3 U* z/ U! O8 g) t# y+ D
以飞2 P6 d: W9 B# r/ N1 t
镍镉电瓶,
: p% ] V0 c: U将储存的化学能变
2 ?; b9 w9 [$ U1 I5 u9 W镍. R! h# ]# H: D. Q* \ E
惰7 P0 ~: I" L. @% v' K) i7 L o; N
降- J" [+ e$ ?1 R* `4 O8 _
面
2 n0 \! ? |+ k2 Y5 l# C! g0 pNOMEX,
( ^9 s/ i) P8 T0 M是0 `2 s0 J, @* y! u* p
单向活门,
3 s) I+ S6 P8 ~/ [! W2 X0 B( n+ @ Y英汉对照民用航空词典B OEING
2 K7 |+ ?+ I6 Z$ q' Q3 WTECHNICAL DICTIONARY 106 Z' q- z# Q* n
NONDIRECTIONAL BEACON (NDB), A radio beacon5 }. D! b3 z3 l- Z8 S# y
which transmits nondirectional signals whereby the pilot
3 U. W7 J C- g- t2 N( f4 `, ]3 mcan use the ADF to determine his bearing to or from the4 q. ^: P8 {; ?' w9 T) t
station.0 W9 C$ |2 G, Q6 P2 c
ONVOLATILE MEMORY, A type of memory which- ?. G' ]! }3 P" }/ |! t4 R
does not lose its contents when power is removed.( e+ P, i+ _) U Y4 ?, [
rm
1 F2 ^$ R$ M1 Sbinary circuit in which the output is logic 0 if any of the
; L* E, h" k2 X/ kinputs is logic 1.
. I& _4 e! f5 l) R5 X, zNOSE CONE, A device on the front of the engine that+ l8 @0 L* o: r {
guides airflow to the primary airflow path of the engine.
7 a0 {1 L% ~3 K9 M3 Lthe nacelle for air inlet to
$ N% o! p; n6 U3 G me engine.! y& h7 G( Y/ M/ R
OSE DOME, Front section of the engine for
7 G! V }4 Y1 s5 N I, ktreamlining and directing airflow to the compressor.( y) s ^( O, Y5 g; ]) X
),- [6 e& H3 B. n+ d; L! i
能够用自
; o- }; r+ j/ Y6 ?6 P定向仪(ADF)确定他的背台或向台方位。
) |4 `' E' E+ l8 E( ?8 v9 |5 r久性存储器,/ s5 [& `2 u: ?; R- Y7 r: F
在失去动力或电力时不会失去记忆内容的存储器。
* X5 K& n1 E, x0 }% a% r- e# k/ l( L在或门后面紧跟着一个反向器的二进制电路。当任何一5 K' ]1 J) q2 i; Q- O
输人为逻辑1时,输出为逻辑0。
! z- j5 y- C8 c8 t% K9 w一个位于在发动机前端,用于引导气流通过发动机的主" A# b+ h8 K/ |" O! G: _
气流通道的装置。
0 P4 o4 h$ T8 `引导空气进人发动机的短舱前段。% ?" B* u; y3 R
部整流罩,; X& \) i0 \; z6 E- b
用以整流并引导气流进人压气机的发动机前段。
4 i) N0 l& D' @2 u9 M7 v2 vN
' o0 n+ p L2 C. e; x; |+ k; WNOR GATE, An OR gate followed by an inverter to fo7 b- p0 `9 ^' Q
a/ k3 L4 h5 }( B m9 k
NOSE COWL, Front section of# C& u( O0 f& g, ?0 R
th8 [ l1 K3 z! @5 I
N8 e. h; h0 S, |8 ]# s: I2 w
s
3 r1 \& s* L0 y4 ]4 f9 u无方向信标(NDB8 ^( ^- @% m2 C' `( Y
发射无方向信号的无线电信标台。据此飞行员/ O! [ m' d' P# s1 I! P" s
动" h/ k) l' O& l H6 n
永
3 p# S" X) q! ?% L7 a或非门,6 j/ |* O! }& R, W/ c
个
8 `* H; v" U/ _3 k进气整流锥,
& }' K$ X5 T$ R5 q前整流罩,0 L( x* f$ E8 j) q8 z: I
头" U( j' n5 Z4 F0 G
英汉对照民用航空词典B OEING
( _& Y0 |" j) [3 c) Y+ QTECHNICAL DICTIONARY 107
! ~* Q. m* h; {, a, _1 f qNOSE GEAR, The front wheels with the attachments for
& F5 G6 G3 {. ]3 o9 k; }NOT, A binary circuit with a single output that is always
/ O: G" ~' `6 a+ Y- Lopposite of the single input. Also called an inverter.
: @7 Q* O0 T7 `! Ction that has the shape of a "V".! z6 `4 m) e {; z: `! g# ~
t.& r G( f0 Z' B+ Y6 l( z
O-RING, A circular shaped rubber or synthetic material
V. y" X4 x6 @3 tsealing device for pneumatic and hydraulic systems., ]9 k1 g8 V/ x4 o
PERATURE
6 O, S. Q, H E* H6 [e1 {. i3 _ t7 p# }6 U, K- m% n1 ?
in the path of flight.) T0 D7 T4 S7 L
OBSTACLE CLEARANCE, The process of flying the
4 ~8 }+ ~2 a6 m% ]6 baircraft over all obstructions under the flight path.
' k8 _0 Q( d: X: |! \0 @Which obstructions are considered and the amount of& C% J5 h: g, X) F% T) x) j
vertical altitude required above the obstructions are
2 Y7 G, H5 K! o. P) Jdetermined by local regulatory agency." i8 A2 X3 S' Y! E, y8 b6 j
非门," d. y( U4 b4 h6 k( n5 q6 Y' h/ `* X8 z0 ~
带有始终与单一输人相反的单一输出。也称作反向器。$ T% R$ x- N0 e5 m% J7 ~7 I. u
一个“V”字形的缺口。9 N) c0 C1 p$ i3 s( A% R9 Q: x b
喷嘴,
) z. s: I" y; p# v( U3 _' V1 }形圈,2 C6 ]1 J, B2 C3 f1 L
用于气源和液压系统,圆形的橡胶或合成材料制成的密
: Q+ w! ?! h! j+ s封装置。
' S# X4 s! h7 S' u" |& \外界大气温度,% s3 Q) H9 R6 j. a$ S% |
见Outside Air Temperature. p$ b) k0 ~$ |/ q
supporting the airplane on the ground.
/ U2 |+ M8 b$ V4 F# t- @NOTCH, An inden
% C+ c& ~4 D; Z, BNOZZLE, A shaped device for directing flow in a duc
$ r+ g: Q% D) ~' e3 ]O
. e" A3 l$ S4 }; pOAT, SEE - OUTSIDE AIR TEM( g; [; L+ p' r
OBSTACLE, An obstruction protruding into the airspac# [4 t5 U6 c+ q4 |& d3 e
前起落架,0 e# ], x! M4 U7 s
用以在地面支撑飞机的前轮及其附件。
% B- x7 g4 [$ A1 F3 ` b凹槽,- @6 w1 Q8 E" \& X: u
引导管道内流动方向的具有特别形状的装置。; R+ N: l' ?. a- A1 E2 m' A4 C& S
O; _1 Z2 }! X: i5 ]! T8 a1 w
.7 }- c. q5 o- n6 E2 E8 c# o ~
越障,9 _0 E% b% \. I0 f( ]1 s! i' {
道上所有障碍物的飞行过程。障碍物的选
- j/ n1 A+ M2 T* o* A+ r: `1 `. w* n9 s择和飞机距离障碍物的高度要求由当地有关管理机构决
; n9 K6 @5 ?5 b# @+ Y定。
( C- p% s- O Y! e障碍物,# b1 h7 Y6 _$ U7 ~) \. l# l
进人飞行航径上空域里的障碍物。' V6 Z7 B5 `. z2 E; }6 P
飞机飞越其航
% I/ e) l7 v6 G/ ?! \2 N英汉对照民用航空词典B OEING, Q) u+ L9 Q5 q! D9 H2 K8 @4 J" n
TECHNICAL DICTIONARY 108
7 G7 Z6 f5 d T! FOEW, SEE - OPERATING EMPTY WEIGHT! O+ [- ?% U( ^/ @, V0 L
FFSIDE, Opposite side.
0 R4 ^8 t- f! @$ @IL COOLER, A heat exchanger for cooling engine oil2 k" ?, x% _% n/ v% v, [! \
by fuel flow or airflow./ ^0 l0 d0 Z7 Q) ?9 Q8 H
ATOR, A device used to separate unwanted" t/ B4 F; z3 o& W9 b5 V" u
ir from engine oil returning to a sump or oil tank.
0 {* U, Y# `2 c' T2 cOIL STRAINER, Type of oil filter.0 j' ?' T3 a+ X( S
LEO STRUT, SEE - SHOCK STRUT
/ N! [" y7 H* j' U+ V/ v4 _1 [NSIDE, Same side.6 y1 E3 I* b& g& ^( h
ll weather navigation system.
2 g% d7 {- n/ p; }3 b5 Vch is not
, g+ S8 R; y$ |continuous from power supply to ground due to a break7 a0 X. t$ c3 h8 o* P
in the wiring or failure of a component.( r. |; d: I k
见Operating Empty Weight+ p: t0 n) `) G/ y7 H
O
4 R2 N- ]7 w; I6 Y6 X; a- _: dO
; [0 m* g( ? m. c. K! u% v( h' Y3 @OIL SEPAR; u0 P) G7 b1 f( [( \* ~) c
a
9 C$ X7 }4 G( b( O* MO; L: w m# l) Y( E' c" T8 y, j
O0 V9 x( V# f. _( [' P
OMEGA NAVIGATION SYSTEM (ONS), A worldwide,
. m7 P7 k7 G, @+ t- B9 va% i; E# g4 D, F. Z, y8 x
OPEN CIRCUIT, An electrical circuit whi
) R0 K* Y6 x: v7 g使用空重,# q. ?6 r& ~& D$ V
.
; [! @1 u) _) N+ h8 p: t* E: T# H面,
; M Z5 J3 l" d- d油冷却器,
9 `+ j, S' [' ]. g# m U4 D, c利用燃油或空气的流动来冷却发动机滑油的热交换器。, ~1 d; v' I% i
油分离器,- W0 }. D9 g* Q0 n% _ y
一个能从回油槽或油箱发动机滑油中分离出不需要的
& ^, t6 D% H8 m! U气的装置。
4 L s; h7 n- s" N滑油筛,$ Z, A. b! s7 u( }! G
滑油油滤的一种。
; W' F3 F( X, E9 \) o液减震支柱,
1 ], N) o0 Z/ D4 Z3 G4 J g0 s见Shock Strut
( `# J5 \2 C, a! K. F3 G反
" I3 l/ B' c. g: h5 m' G3 @相反的一面。. Y3 ~" d3 ]( J- ]
滑
4 x$ y! H0 h# `' W6 V滑1 }6 X! a" r" r
空: q/ t0 N3 Q% w( o' z) s& M
油
( x/ v" `/ K- `/ N" H) P' u d.
! i3 A) x2 A. N' u4 b面,
3 y9 }4 i2 f; G; G/ X2 {相同的一面。: A. f' J; }% t$ v8 o6 N( _
个全球范围内全天候的导航系统。0 @! I, |6 D+ p9 b$ ^
或组件损坏而导致从电源到接地点之间
! e2 X2 v; f2 y$ t8 X8 k+ a不通的电路。8 a$ x- q G. k& X. s9 ]
同- e+ `; b; r5 X7 m
奥米加导航系统(ONS),0 q- K$ k7 y( L! W' h; J
一* k1 ~6 [/ L% O, Y* {4 v* H
开路,
4 @0 o" ?) Y, `2 u由于线路中断, u" w& w$ a& B9 p
英汉对照民用航空词典B OEING
, q' n9 } ]& R# j; @+ b/ h4 E8 Z1 @TECHNICAL DICTIONARY 109
7 L" j; m! h; m( f4 O1 E, sOPERATING EMPTY WEIGHT (OEW), The weight of
, S( {% R. z5 f8 qan airplane fully serviced, including the crew but without
. F) c; x+ o" Dfuel and payload. ?5 y) C& ]& J; V0 ?0 y: f
PERATING ENVELOPE, Defines the environmental
, v6 a. r* P3 K# |! t% c: MOPTIMUM ALTITUDE, The cruise altitude which results' H/ x3 ?" h1 Q6 x
in the best fuel mileage.* N* Z- I4 ]! r
OR GATE, A device or circuit with two or more inputs of$ w/ U+ @2 ?) c. A
binary information and one output. The output is 1 when; q* @: L' R" h. {- j, h3 |6 Q
any one or more of the inputs is 1. The output is 0 when
1 z. n" e |2 a0 h9 b$ yall of the inputs are 0.% S0 a: P& `) p: H* c
ORIFICE, A specified size hole in component for control+ ]" X3 z: U9 G F
of fluid flow from or to the component.
1 Y0 Y/ H/ ^1 u+ [ORONASAL MASK, An oxygen mask covering only the
: D9 F% x) \8 q2 u% Emouth and nose.
4 s k$ N/ x* I7 ]1 Y$ ~- U4 E" JOSCILLATE, To swing back and forth with a constant& H9 L: I& v% I2 I Y0 t' J
rhythm.5 B. e& I& B3 C/ _- r( I6 a8 e) J1 J
使用空重(OEW),
* b/ m2 u5 R7 X2 |使用包线,1 Y& ~8 d' _% C# q- H/ w) V# g
确定飞机准予飞行的压力高度、温度和速度的环境极
+ f6 D3 O0 C/ Y! b2 ]( g或门,: M4 J+ H. y; f- J% 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
/ W: q2 C1 \" Y: J2 g置或电路。当输人端有一个或多个为逻辑1时,输出为逻
! ?# v5 m6 O X+ P# w5 f: q2 w辑1;当输人端都为逻辑0时,输出为逻辑0。 O, k1 A& \/ c4 h( A
量孔,
9 M1 Y8 `" s3 K) k& | s部件上用来控制流往或流出该部件的液流的尺寸已确
! N* i; |- }$ L: G7 D: T( q定的孔。
+ y2 g3 g! @7 N4 f g7 S6 F口鼻罩,
5 {" R/ G& a6 k仅罩住嘴和鼻子的氧气罩。
# Q1 D3 B4 B+ u( S7 H9 T% v振荡,
6 g1 w8 t6 b' ~$ x$ K' p) h: b" j以恒定节律作前后的摇摆。0 F; e2 O& ~ C( U0 a
O8 d; \. F( E; i5 Q0 t: d5 i! l3 P6 e5 @
limits of pressure altitude, temperatures and speed
* L4 C( g C9 H1 |9 p3 wwithin which the airplane is certified to operate.. A, }4 L& l$ D: v
一架勤务完毕的飞机,包括空勤人员,但不含燃油和业- ^# g6 c, H; e
载的重量。
0 L' T9 t2 q$ y( f限。3 F% r0 H! i! Q
最佳高度,+ k- o+ y# C' e; N9 ^( N/ T9 O6 m
可获得最佳燃油哩程的巡航高度。" E+ |- `* V3 ~7 B$ S' u9 W% S- I
英汉对照民用航空词典B OEING) a" }3 \9 P M. d6 `8 @
TECHNICAL DICTIONARY 1104 r$ K" f1 |) h+ t1 k6 f/ R
OUT OF DETENT, A condition away from neutral or a
0 h; z$ v4 A4 x1 N, w2 QOUTER LOOP CONTROL, For autopilot operation this
6 z( X: l7 c/ [1 \" G" a) Ais control of the airplane's flight path to a target." X2 q& _0 H- [
Examples are control of heading, altitude, and vertical
. W2 @6 _/ | Z% B$ Uspeed.' U0 _- q# d7 ?6 K0 j6 }. m7 P7 U
UTER MARKER, A marker beacon located at or near0 s; d3 R/ X% }! o* v
e glide slope intercept of an ILS approach. The OM is
8 g3 ]( j' H0 [3 T' ]5 ~6 Jnormally located four to seven miles from the runway
# j |5 J( c- Z; Treshold on the extended centerline of the runway.+ V" f* W: e/ p; Y6 D D* W
W VALVE, A valve in the fuselage for
, S) W0 R+ S+ [, Z4 W, c3 g# U6 Dg the airflow from the fuselage to ambient for
/ t/ D7 V$ [6 r2 uation control.2 h+ k# g9 R2 L+ P) j* Q1 Z
UTPUT, An information signal going out of a system or6 E/ i- k0 ]+ z2 S4 ?5 v
part of a system.0 C1 ]7 D* H0 g+ A
UTSIDE AIR TEMPERATURE (OAT), Ambient, or free
$ r- G5 ^. H+ J* q" q5 F# o( m& _OVERHAUL, To return an aircraft or one of its
6 ^$ s. M- f2 w. s% {8 ?OVERRIDE, Operation of a component by a method
- J/ W, q, D7 xdifferent from normal operation.
% i4 Y4 b% W) }/ I; O- I& D操纵杆离开中立或槽口位置的一种状态。4 u. W( u+ G+ s! W# c
制,9 U1 g& {& a( j6 Y7 |; K
航向,高度,和垂直速度的控制。
$ R5 V H4 y; l& E4 B指点标,
4 Y) _( T k4 F" U- `) c9 q1 z) ]: O9 f位于或靠近仪表着陆系统下滑道截获点的一个指点信1 B: i }) E+ s0 S' P; Q2 f a
标台。它通常位于跑道中心线延长线上距离跑道头4至79 |; [% @; L, M; n4 E5 p
海里。% g1 {5 v+ Q' J) l0 P6 d! D# X
流活门," ?- Z) }1 Z4 R$ @. S# k: }6 f
机身内用以控制从机身流向外界大气的气流以进行增
7 }& T1 H# H/ f: f控制的活门。
5 j$ ]" {7 a Y: U. W. Z输出,
3 u' q g! F& P1 U' x从一个系统或系统的一部分出来的信息信号。) g% \* V7 _: K. V6 y4 z
界大气温度(OAT),
l4 u: s4 p' ~: a外界环境温度或静止大气温度。
2 `7 W5 n9 t: e" D修,# p6 ?6 p' O9 `( m( s
将飞机或飞机部件修整到近似全新或制造完成时的状
4 ]& e- P5 L1 j' i" Q& S+ {超控,% B; C7 A. I2 Y
用不同于正常操作的方法来操作部件。+ d4 {/ j3 B* G9 x4 Q
notched position.
1 H; @* v. {. s8 k/ [O
5 u& ?) m" v% L5 o( B6 ?8 Oth! W; l1 R% v! t' [
th; f" n l [9 n* `1 i9 j
OUTFLO
3 _/ D* N1 N7 @controllin
: Q9 k; M9 h a9 |3 Xpressuriz
% u% A- Q4 _& b% XO
+ V0 e6 O2 ~& q, b; W4 \a/ K. a$ m) e% d5 ~( h
O# u4 H# F( Z+ c/ s
air static temperature.2 K K+ _( m0 V9 E+ I; o, w2 i
components to a like-new or just manufactured
# @" ^' d8 Z$ ]9 y, y& }: rcondition.2 k8 z9 [$ ]* Q5 J' {' k) a
脱离卡挡,
1 i0 N! \: l! \& K! x外回路控& p' }9 M# t% O2 Y: m8 C, h
用于自动驾驶操作的对飞机飞往目标地的航径控制。例
& y$ @5 K0 ~7 q2 H如# ~& P7 n7 @# q' F: Z" Y9 e
远
# Q d5 @ X$ N3 L! u外
8 J& g2 f+ Q2 _# _8 n S压
0 T. E! P, F& \2 g/ \5 t外
0 X# L( C7 ~* x& U翻
) k8 _2 }/ t# Q$ d" ?态。
7 j( t$ _" P1 d B' u$ ]6 o/ U英汉对照民用航空词典B OEING
6 l7 R! r& ^2 u5 `/ eTECHNICAL DICTIONARY 111
" J' y2 B4 ^2 y0 QP- T; e2 T) A: n
ACK VALVE, A valve for supplying air and controlling
8 G; x" Q( j; Tmanifold to the air
" _2 q% v' X$ o% m% @* j% O; A, v) v/ Yonditioning system.
7 }5 L+ n2 x, s O7 f3 y9 H3 [4 A+ Cll piece of any substance or
7 @6 x/ b) O8 ~physical matter.: Q$ ?- B S. E# ^: M# Y, U
h
# A4 a: [, L6 J$ P6 d+ R* F$ q3 yrovides flight crew and attendant announcements,
9 L+ y* h' f+ _: Xoarding music, and chime signals to the passenger" l6 x& N3 J! Z- @, _5 B
cabin.
+ N* e7 B$ I1 @2 I- h0 O0 FASSENGER ENTERTAINMENT SYSTEM, A system
% n4 i% D9 ~" R1 y- W7 stertainment to
0 E% a9 x7 j, d# Ue passengers.% T+ i, W3 y' z6 X) Q
PAYLOAD, That which is carried to the destination,
, d2 ?( f' W2 O9 T4 V4 G' b9 u5 Ouch as passengers, cargo, or mail.
0 P8 e3 s; o' h# t7 YCA, SEE - POWER CONTROL ACTUATOR/ J0 `1 K+ w1 N+ c8 o1 F( q
PDCS, SEE - PERFORMANCE DATA COMPUTER9 w; d' q% j! o3 @1 B7 R y+ D+ q
SYSTEM- h+ d4 a( i7 I3 A# O
调组件活门, n' V0 k' ^& H. A z; l1 [
由气源支管向空调系统供气并控制该气流的活门。
+ H. A5 ~7 |. d) X& z4 z. h任何物质或实体非常细小的一部份。) F4 t7 x' ~5 J6 Q( ~
旅客广播系统,# W4 T# _; _; Y8 Y% ?
能使机组人员向客舱进行广播、播放音乐和发出谐音信; x+ E7 n, `8 T5 Q2 W) N
的系统。
- } e& K# V e3 |3 h2 ~; L3 L客娱乐系统,7 J( V& D) f$ [ m* E! ^
频和/或视频娱乐服务的系统。
$ G2 Y4 U* c( A' Z7 V: i) [4 t由飞机送往目的地的载重,如乘客、货物或邮件。
0 |( W! O, |4 j! m% Z力控制作动筒, P4 ~- U* y( O6 A3 ^
见Power Control Actuator7 J1 b7 X) u8 n; ~( J
P9 F; u: a2 b$ R ^5 f
air flow from the pneumatic4 x( e& h: u% l% e
c9 m3 } i" V- e3 X" P/ z
PARTICLE, A very sma& x+ O; }1 A) I a7 G% }
PASSENGER ADDRESS SYSTEM, A system whic
0 U8 }; y3 v# i7 m {* dp& _5 ] i# `- N
b
" L/ ^. y9 I/ H& s/ ZP* I3 E1 B9 \! M8 j' w
which can provide audio and/or video en
2 w; j8 a) W+ i" a6 ?' a: dth" D/ d% ~, g. K& g
s6 P& |: `' z4 U
P
( j& Z) c) X) S5 m" s0 u3 z, z4 qPCU, SEE - POWER CONTROL UNIT, ~6 x% N7 T- r- l" o- H' X
空. S$ p' Z o" y1 b# b% @ T: d' ^
微粒,
: c7 ]5 S6 i }$ Z' n号
6 D4 Q; L0 T' U6 L8 b9 U6 |旅
: G) h1 q; m$ z2 ]& g9 c9 r" l7 x向旅客提供音$ k# \ t6 o9 {: X
业载,; j3 K6 Y w3 q- W
动
+ R# {$ l" z" Y.
% L. Z1 a4 ]2 _7 A4 G$ T O2 kControl Unit
5 u( r5 }- T- [3 t; C- H动力控制组件,% \! F i( b- m. t, W' m. b
见Power .4 ?6 L& i' [/ v$ p% T" n3 K/ N
性能数据计算机系统,( o8 M4 C6 `. N# f
见Performance Data Computer System.( X& u: E! Y) c/ A% s
英汉对照民用航空词典B OEING
* X3 Y: ~+ h0 b2 }TECHNICAL DICTIONARY 112( B7 j4 L/ K8 e
PEEN, To cause a more corrosion resistant surface by
b: o( N% X5 Q" i/ k) H5 R4 umultiple impacting it with a hard material such as steel
+ B1 }3 ~1 S: b. Dpellets. Term for this is Shot Peening.$ W; r+ u' L0 z; Q9 X
Defines a position on the aircraft relative to the mean: e% A: q9 ^/ J6 X; n7 J
aerodynamic chord of the wing.+ ]% ^: |% w7 k; \! l
r as a percentage of a fixed
/ y3 |% I. c+ |1 b7 J6 tmount rather than revolutions per unit time.& P/ G- u9 i' f8 R% Z3 D& A7 |- V
amount.
9 M5 _- W" e% |: g/ H6 b2 pERFORMANCE DATA COMPUTER SYSTEM (PDC,- l. ?+ J0 ~7 f" b
PDCS), A device which provides data to achieve the
$ ~' r! _' S4 K! @0 S) E$ U7 K$ O i# Qmost efficient and economical operation of the airplane.. B/ u: _& D# Y, @$ I0 M/ |# d
PHASE OF FLIGHT, A portion of flight specifically+ r! O" I4 m, q/ }- s6 c, J
devoted to accomplishing such things as takeoff, climb,7 u9 k6 X" t1 ?( ~4 ~+ |
cruise, descent or landing.' l/ M- T) m* E' d8 O/ l
这个过程名为喷丸硬化处理。, I3 w5 W4 \* X' q2 ]
平均气动弦百分比,
) d" I6 K- Y8 K" X$ c间转数来表示低/ }0 b0 a5 G# ?, k; x
压压气机转子的转速。& `( |: m9 g/ X, E' Z3 w$ y8 i+ e, V
性能数据计算机系统(PDC,PDCS),
; @9 A/ v+ v9 J; Y1 q- L一个能提供数据,使飞机达到最有效和最经济的操作的
7 \8 M. C# t2 }* u置。
0 T% t+ S' i9 n4 G" S! X行阶段,. g4 j* @7 Y: f( r) {
飞行中负有一定任务(如起飞、爬升、巡航、下降或 a/ `2 x6 m5 A; p0 w5 z
份。7 a4 t" b/ }9 m, b
PERCENT MEAN AERODYNAMIC CHORD (% MAC),
; v% @+ a9 J( p& Y: p$ n( HPERCENT N 1 , Expresses the speed of the low: _; g0 e! v, u M
pressure compressor roto
4 }0 C6 u- M( Y, |+ t$ Wa7 j9 R# F" t( T4 q7 J2 R% s6 b4 ^3 i
PERCENT N2 , Expresses the speed of the high+ G4 [% ~- t) Y( g: z, ]
pressure compressor rotor as a percentage of a fixed8 }/ ?7 M& R) l$ `" m/ S" b6 a2 D
P6 E$ M& e" t5 {, E2 V
喷九,
2 c% `; v( ^8 \( U2 x. L% L0 F为形成防腐能力更强的表面,多次用诸如钢丸的坚硬材" Y' D% o+ {. a
料冲击表面。( ?& }8 ^# b3 q. {
用来确定飞机上一点相对于机翼平均气动弦的位置。; G3 ~) j5 a, ` T( {. n2 i8 \
N1百分数,0 S( u+ |( d) t5 s/ N9 n; n2 o
以一定量的百分比而不以每一单位时; U9 S( ^2 J8 X9 S9 C9 V
N2百分数,# [/ t+ ]! f7 b6 g
以一定量的百分比来表示高压压气机转子的转速。
) e* d6 q9 o" M" x; ?' n装
4 B2 _+ `% Z+ h( o飞
. w. Q. J9 x V% j7 k着陆)的部
8 q% D# x" E3 C0 c( Q& b) l: q英汉对照民用航空词典B OEING7 B. h* T) |2 O/ A5 ]6 n
TECHNICAL DICTIONARY 113
j3 a5 ]3 z8 |8 N$ S7 [PHILLIPS HEAD SCREW, A cross point screw with two3 s# t4 E+ T6 [0 i' ^$ v
en with a flat tipped Phillips head3 H. m3 z6 A7 x7 F) u; T
crewdriver (see Reed and Prince).
5 F/ u# j7 G& {0 ? C aITCH, The rotation of an airplane around its lateral
4 {: w) y* m: Xxis.
9 f" m& U r% Y, Dne
9 k! g; Z1 [( O% v( ~7 hose up and down movement controlled by the
+ Z* b9 m: e: _! Z5 w' llevators (and stabilizer for trim).! A: g9 o! X! ?9 p
ITCH RATE, The rate at which the airplane moves in
9 O+ O: Y: [ Y6 x5 n! Ze pitch axis (nose up, nose down).3 D. e2 w- q: s+ {
TIC TUBE, A tube facing the airstream, M: s$ W8 d$ k& s; T
hich measures ram and static pressure. Used by
$ V/ h+ B3 n& m5 D- t5 ]irplane instruments.( k q" `# h* I: W5 P( R
丝钉。由平0 t/ D0 {" u4 K9 v' l8 G
十字头螺丝钻驱动。 K5 q' v$ V: Y1 z6 m; x
仰,9 L( S! n' }% C/ R- j
飞机绕横轴运动而造成机头的上下运动。; Z5 U7 M" W4 U. c/ Y2 G
一侧通向另一侧的水平轴或横轴。升降舵控制$ p _( R! T0 V7 f1 f' P) X
头绕此轴作上下的运动。(水平安定面则用以配平。)# |% l7 v0 U" |$ O+ J; f# j
俯仰率,7 x; c8 @+ E" ^$ j5 E0 T8 J7 v
飞机绕俯仰轴运动(机头向上或向下)的速率。6 V8 f$ F# O! Z N& v( b5 }2 a
管,
2 J9 U8 B, M8 q开口面对气流以量取空气的总压和静压,供飞机仪表使
9 Y! O# S# U6 r" V的管道。% x# N9 R( e5 c4 N& O9 N4 j
distinct tapers. Driv+ f" C, Z5 |" y
s! z4 X3 T+ R7 B; G
P+ h1 a5 ]9 b4 Q% n
a
& n, C2 A: }( {! f" M: k0 V6 _+ MPITCH AXIS, A horizontal or lateral axis passing
8 o x+ K4 T/ Othrough the airplane from one side to the other. Airpla
9 `# B' ?; V$ B/ ^' }* f# I An: r3 ]- p; l& x$ J z6 `; O
e
' k1 m) d3 a3 HP
$ }- |9 |) X; g+ y2 J9 \. M- ], ath- j2 K! s" w7 L9 J5 |, @0 w% z
PITOT STA6 C/ a3 S) d/ G* N$ W9 I: n( r x
w
' f$ X' K3 c) l+ g3 f* xa9 Z. _5 X# J2 j' V1 ]6 S- j
十字螺丝钉,
$ `, L+ B/ e2 k! } k6 G9 }螺丝的顶面有两个明显的锥形十字四槽的螺2 S; o+ O5 U+ A9 D% M/ n3 o o
顶
5 L& R3 k. S$ n( e* h# Y _" a) |$ p俯2 O- k( j& o4 u; V2 c
俯仰轴,
- U% P; e" _. s* T! N* c- h从飞机# x+ B! C1 ?0 _* t( u! g3 E
机* i7 K5 @% U. E m) M! s6 w3 f
总静压
7 f' C7 x) L) M用, @: A0 K$ W1 E4 }
英汉对照民用航空词典B OEING2 v) Q& s/ v- ?* W5 P+ q1 Z+ S5 L
TECHNICAL DICTIONARY 114
6 ?( p+ I, v# z- W6 R+ q4 iPITOT T
& I3 `, x1 B5 S! M$ R& Nmeasure; f8 v" v: u D9 K/ j- I) v! _2 u
UBE, A tube facing the airstream which
# Q" M, Y x3 B* J, k3 Ls ram pressure.
! z/ |% j H( O; \PLA, SEE - POWER LEVER ANGLE
" O% Q: B3 H; k% k4 u# N. {r
$ f5 X' K- s4 Q, W0 D# q: ~e3 P& d. p" B% r+ x1 u
LEXIGLAS, A registered trade name. A transparent. F" x9 S) E. d" U4 S1 t+ D; V
r any purpose.
- S- i, |) A6 J8 A& oNEUDRAULIC, A system or process which is a: w; p* `" T: D# d, r; ~0 a
res.$ G# i8 `& v# T5 ~; S
PNEUMATIC (NO. 1), Cold air, controlled and/or
, [" P. @2 B7 h! d8 upressurized.
h5 T. G# f. n5 p* U) L托管,2 f0 J! X/ V" {4 ^! e7 g' _8 U
面对气流以量取动压(冲压)的管子。
2 @" ]6 z( J6 V; B门杆角度,8 v8 G9 D. u2 ^$ q( {0 m( F! f
见Power Lever Angle
; O, s& ]: L* A' UPLACARD, An attached sign providing information o6 n; M1 T8 |! I# `
instruction.( i1 A6 D: I! Q5 P& ^# ~
PLENUM, An enlargement in a duct which changes th
4 n v# }9 Z {& p$ Nflow characteristics of moving air. Used to remove+ f" W& Y9 b( P3 n7 z, F
pulsations caused by variable airflow.
2 i* | r) [0 r) F6 r$ A: A1 oP
* R q; V" c- I% y6 e* Y9 ^/ ^acrylic plastic material used for aircraft windshields and/ ]. N$ T f3 H4 M" |
side windows. JARGON TERM - sheet plastic of several" P* W( d3 j% M8 w- Q
types and used fo0 e* N' d' `: |# S, H( {( y
PMC, SEE - POWER MANAGEMENT CONTROL
* z( Q5 j, L7 R; p, n/ d8 I0 DP3 n2 `1 r. N9 H! \0 W
combination of hydraulic and pneumatic pressu) Y; `3 ?+ h1 p, ]3 Z. f
皮+ ?5 _- k5 a4 V$ s, ?4 _
油5 _8 e1 R5 G% I! Q/ D, N4 x
.$ X O5 M( J* e1 i
脉动。7 \& l @' h" L+ h0 }0 ^
机玻璃,8 j1 a+ @: @7 |! d1 j
名。是飞机风档与侧风档所用的透明丙2 J T2 H! v! W8 J* |2 G8 i
控制,
' e& l$ f8 J" D p1 X4 L. }标牌,
! I- @5 \! [* P7 E0 b+ e提供信息或说明的附贴标志。) o4 r- {4 x# m% k6 r
整流腔,
6 {2 P. K, u4 S u5 p. w, m管道中用以改变运动气流特性的扩大部份。用于消除可, d& q. Z( s& q5 R
变气流引起的
$ f% g! k1 w/ @% b' t! e有# @1 ^$ R3 v' t3 M& A0 h5 [. E
是一个注册商品
" C# \& f- [7 a2 F烯酸塑胶制品。行家称之为多用途化学合成胶片。. S6 g7 `4 F/ o: b8 r
动力管理. `, `7 D0 E) [2 W, f! c
见Power Management Control.9 Q. c! U; |4 \) {8 z( W
动液压,9 j8 [6 F- w9 f- j5 c7 z7 N- d8 n+ h
推动的系统或过程。 Q* y1 o$ C7 ?
1),* B9 `# d; F9 d, ^4 n. y
。
|& f( N B7 L气
% U5 k9 L8 x, r# D$ N% d% Y! n由液压和气压混合4 [( W7 v8 |* n& K% ^1 B, Z
压缩空气(NO.' G1 K. e, L/ T! V/ A0 N1 e9 j
经控制和/或增压后的冷空气% V6 K9 h+ X: W, D2 T
英汉对照民用航空词典B OEING: f9 k6 l8 v( p
TECHNICAL DICTIONARY 115, I$ S6 |. }1 M: f- b* U! O: K8 k! P
PNEUMATIC (NO. 2), Air, controlled and/or
5 c! L; `1 N0 b# \, Fpressurized.
2 S" M: x0 \! ?OP OUT INDICATOR, A device on a filter which
( b3 _7 c" t/ f: R8 Aroughout a material.
( J, B' d4 H' H: |8 U s* [ition.+ i3 ]; _5 i! g$ f, T9 }& {
POSITIVE, Definite and intentional.
" L# i6 z: K5 g Y% k% X7 e$ c(No.2),9 _, J# y) S. W, A' l
出指示器,8 g) Q: g: G. ^
到达一定的压差时,它会从壳体内& }% m5 ^1 X$ _% x7 n
指充满整个物体的细微小孔或空隙。* \# h5 ?* ]$ U& v! n
置基准的飞行管理计算机的一种操作。
& G" @& q; M6 @7 G: X肯定的,6 j7 [+ m6 _/ [& a: O: Q& [
一定而且有意的。
& X W" [! u, N0 NP
1 ?; w, }6 Z: }( c& r% ?protrudes from its housing when a specific differential \' H# f8 j3 r
pressure is reached.
, A1 s1 A$ ^* t! [4 O- Q7 ePOROSITY, The term for pores or small cavities# Q* A. _( s) n; {' G
th
% n7 R7 s% x. P2 g( j9 APOSITION SHIFT, An FMC operation used to change, X% [: q& a1 X3 J
the reference of present pos2 c" w, [) I# b/ H% A/ S5 b
压缩空气( K' y/ J+ b) K& B- m3 Z
经控制和/或增压后的空气。
: s8 x4 t* \; B$ j& b弹
6 g1 I+ e4 l3 l% A过滤器的一个装置。
7 K4 n$ @5 T5 p5 N2 w0 b伸出来。
9 g: M3 K1 ^8 _( s" E气孔,! b- n- r6 |6 f% G. B0 f. w3 U) H0 P1 @
移位,
' a+ k. M8 T4 S' A用于改变现在位
) E8 n& p3 p+ {% P: M英汉对照民用航空词典B OEING& {9 q; j5 d: }0 _6 ~; k
TECHNICAL DICTIONARY 116" g. I! C" n7 M% b
POTENTIOMETER, An electrical device for changing) q) `. I, _; W6 f- f- ^9 L5 N3 S
the voltage supply to an electrical circuit component.2 b2 h$ Q% p! T
r! O* Y1 A8 v3 B, @
bly for operation of flight controls.
# q% a- V! Q, A" }( m+ FOWER LEVER ANGLE, The angular scale on the
0 W8 t& S0 L5 W& Smain engine control for showing movement of the power
J0 }+ u, k* H2 |hrottle) lever.8 Q) b: s: f/ h |/ w- w, e
OWER MANAGEMENT CONTROL, An electronic
0 O5 Q1 n# y8 Ingine control.5 B0 @. N/ E9 B5 m; t+ s! t
OWER TRANSFER UNIT, A hydraulic motor/pump for- u) S) |/ y3 A6 _$ z/ j- @
upplying hydraulic power to components when normal' Y) c+ k. B3 S0 U( `4 S; E
RECOOLER, A heat exchanger in the pneumatic
* B( X' P* l7 L1 Ulied- u5 R2 ~" ~) b7 ?; |2 k
作动筒,
2 X5 K: F% w3 Z' W. w. d件,* D8 p! H. {- `" M( ?+ p7 j
油门杆角度,. d. H: m2 ?' R2 ~7 ]
主发动机控制上用以指示油门杆运动的角刻度。; i; L% H) `, A
动力管理控制,2 w0 j& x+ o4 X2 ^9 w4 T$ o5 C
控制发动机的电子装置。' l0 r/ g- x& \6 ?
力转换装置,: b4 Y! I5 U) I6 g) t. `) |1 |
当无正常的液压来源可供使用时,用来向部件提供液压
1 \: c" H* S4 G( V马达/泵。! v/ B- W5 S3 O* e& |; r1 v# B1 D
冷器,! C5 ]! F4 l4 W
中的一个热交换器。它将发动机引气冷却后( V3 Z+ E8 e& `. G
供给气源总管。
# G/ \" s3 C+ DPOWER CONTROL ACTUATOR, A hydraulic actuato8 Z& Q z8 e% h, q7 x! g
assem( g* X3 t5 I9 K/ A
POWER CONTROL UNIT, A hydraulic actuator& F" _4 i; C+ r" g1 {- p
assembly for operation of flight controls.
t# d! b W. Z! P1 n1 E9 a) Q/ ?' VP
. N5 a$ `- A* B0 G Y0 N" u$ k(t5 z, u* C2 d7 ]
P" m4 L. |4 F. `, {5 w7 k8 d3 {; o
e7 d9 p! q. M4 K: Z1 S1 f
P% R; c7 E& b5 \2 N+ I
s5 Z3 {2 Z# k+ M* F
supply is not available.0 G. f, i$ S5 G" y) T
P
7 y$ x$ Z8 F" vsystem for cooling engine bleed air before it is supp
9 {0 k9 [+ E+ Kto the pneumatic manifold.- M+ p( t0 R8 F, G
分压器,
8 j+ Q3 X0 U: W- U9 y用来改变向电路部件所提供之电压的电气装置。
& i8 g5 l: s+ d( K动力控制: E( N& r8 A, y/ `+ ]8 ^) t
用以飞行操纵工作的液压作动筒组件。
5 `) A7 U4 y* ~9 t9 X' q动力控制组
7 K, U: ?* r: z1 r! j用以飞行操纵工作的液压作动筒组件。$ V7 ^7 [# i3 F! ?6 g/ t! |
动1 }! \% y* X: P+ a4 G
动力的液压
& Q! |) Y! S0 R4 ~) L预. c( f" K( X/ L: s) s4 P |1 t: ~
在气源系统% a' a. z, J( `7 S8 R1 l, b8 R+ R
英汉对照民用航空词典B OEING
8 ^* x0 y1 ?2 FTECHNICAL DICTIONARY 117+ S* I0 j5 y: p% }: |
PRECISION APPROACH PROCEDURE, A standard' P. N \$ q& j
edure in which an electronic
4 | u+ t1 I- S- p* Zlide slope/glide path is provided; e.g., ILS/MLS and
$ ?; D5 ?1 Z$ B( R X+ jPAR.
, J8 Y5 }2 s0 D. PRESSURE, Force per unit area usually measured in- a) m* X; j, i5 u4 V
ounds per square inch (psi).8 {' Q$ Z; R/ n7 L
RESSURE ALTITUDE, The altitude displayed when
; h- |: a. M$ e( U* r7 t- y ^e barometric pressure on the altimeter is set to 29.92
- ]: Y( i& C6 R; VRESSURE REGULATING AND SHUTOFF VALVE, A# a" f) j! Y5 o
alve in the pneumatic system for regulating bleed air X5 D8 |% S, Q, G" ?; u H1 b3 ]
pressure from the engine to the pneumatic manifold.* S$ m5 \/ B7 |! s- l0 \' f
RINTED CIRCUIT CARD, A plastic or fiberglass card7 z: i8 N" K( M5 O2 Y, o
ith electronic components and copper strips forming a' x9 x0 D8 x. _% h: x& K1 i
ircuit.
4 e# M+ E. ~6 s" Y4 j3 w9 {; hRIORITY VALVE, A valve in the hydraulic system for0 {* c: V' F3 ?7 u, d
ROCEDURE TURN, A maneuver where it is
% H! `: `' F7 c; B% f, X8 olane( I1 F( o& T- l5 C
proach course.! L: D# k5 x; {' @$ E. T ]0 y
精密进近程序,
w H/ } X* u' |/ I$ N4 m' j己提供有电子下滑道/下滑航径的标准仪表进近程序。
6 ~, D B5 P8 @: O7 L* ~如:仪表着陆系统/微波着陆系统,以及精密进近雷达。9 F% j* U8 ]+ _1 ]! j+ M
压力,
: |& A7 {& V6 S' o+ m单位面积上的力。通常用磅/平方英寸(psi)来度量。
: F: V, J! m* n" r压力高度,
2 ?, G- T, }/ r! C. a当高度表上的气压调至29.92英寸汞柱时显示的高度。
$ \- x& P# t) v% p" e力调节和关断活门,9 J8 J+ q* s# |; }8 Z
气源系统中用以调节从发动机到气源总管的引气压力 D1 c4 |6 Y, j/ C
的活门。6 ~0 r' T/ F9 { ~$ A* l
刷电路板,5 K* p1 b) O; `1 P
由电子部件和铜丝所组成电路的塑胶或纤维玻璃制
: ]: N8 a1 y. P8 Y+ d. T' S" R薄板。( K, D, C/ X+ p- N& R
先活门,
+ [& F, U: m7 W; n: H,用来使各部件照合适顺序操作的活门。
$ M8 N t" ^& M3 M- r; Y; @4 [# b序转弯,
0 Y" q1 F! C" i$ ~3 r) D后进近航道时所做的机动动作。1 ?& T% m, r9 d T* g4 h6 J" m
instrument approach proc( \* W! m4 K9 n4 \
g- Y; r( f' [+ x/ k- J
P, H" D) x; {) l1 t, B& ~' r" S
p8 e0 @2 J! g. M+ w
P9 F; U3 Z7 X3 X* ~4 B& H# J0 M
th6 j1 g3 h( [! T; C% L. Y2 Z5 d2 q! {
inches of mercury.
- C2 \( H: z% N* wP
! I; C2 v1 ?! z8 z+ M& _v
# _1 L- y6 K8 U. E0 H$ {9 \' C9 vP
9 V9 y$ F5 Q3 @$ P0 j0 v: zw
4 i1 ~5 |/ F! ~/ H+ ec% V9 e& y* {+ j6 p
P
( i) H# N# ]2 p4 W/ w% H9 ioperation of components in proper sequence.9 m5 r7 t& P, \% P i4 i
P( G0 t( S0 ]/ t2 v, v7 [) F: d
necessary to reverse direction to establish the airp
8 a8 o6 n8 O. x3 n- mon the final ap
) T0 V/ O% s' ^8 N( e压& t7 e3 w- q) z( o
印
3 c, a* e! j4 }. b2 ^& }# U优$ g5 H' J' I1 k
液压系统中, Y0 ?- ?4 a! B" Q
程
5 S- G* l+ u! z, N+ w H在飞机必须反向建立最/ Z+ U8 o) s( Q1 n/ z. q
英汉对照民用航空词典B OEING
K2 |, I/ g5 t! YTECHNICAL DICTIONARY 1189 N# n- O+ b) s' q q
PROXIMITY SENSOR, An electromagnetic d+ w' f1 }" v. Q9 Q4 V8 j
senses the po5 O' t% D! H3 q1 h8 |) J
evice that: I" S4 ]9 d1 u
sition of a moving actuator. The sensor
' k( \/ d, z# {3 A, \' V+ \$ W' bas two or three wires.+ v& H# K" \/ V( Z; v
ROXIMITY SENSOR ACTUATOR, A steel plate# h z* t) @' P8 b) D1 M( i1 e# ~6 C
cated on a moving component for operation of3 @* e$ A3 j) T5 m3 h, U
roximity sensor.# e1 ^$ A$ i7 a
ROXIMITY SWITCH, A printed circuit card for
; `- v3 f" y8 _$ S8 k8 [transmitting sensor signals to indicating lights and+ ` J' N& k- Q6 m% l) J) F( f
邻近传感器,
2 v Q9 V: f" U能够感知运动中的作动筒位置的电磁装置。该传感器
r, i: ]) W2 [有两或三根电线。
2 J0 r3 z% L1 }7 w+ h邻近传感器作动器,! F' D8 D" D; E6 ]
位于一个运动部件上,用以操作邻近传感器的钢板。- N J+ `# b3 q9 H8 C2 o
近电门," [% q0 `9 H8 n% y' h# B/ ~
传感器信号传输给指示灯和电路的印刷电路板。
0 W/ y1 k1 @$ R/ R: s, V; Xh
; D: [, C8 q) S% H. bP
- D' X% c1 G. o- klo
+ R+ o4 j. V6 |8 A5 Xp+ \& r d: E( b5 g) a7 B5 |5 m
P
# ^9 n2 t' P _# }circuits.
4 F* { p3 }! L' a* J邻 \6 I" A8 {& g& U& T l
用以将
. ~! r7 Q; g+ W/ Y' o; B, K6 d英汉对照民用航空词典B OEING
& q2 n$ G8 F3 G" n! CTECHNICAL DICTIONARY 1197 ]$ F5 Y& \8 G
PRSOV, SEE - PRESSURE REGULATING AND
4 k+ k$ l5 w2 ISHUTOFF VALVE6 U4 Z+ O4 u& f2 [2 D* E. ]
TU, SEE - POWER TRANSFER UNIT% |2 ?# q. I$ P9 K
removal of dirt from the air cleaner.
" x4 A# I! L8 Z1 s. W# r En
1 `6 k- ] U0 VQAD, SEE - QUICK-ATTACH-DETACH
" B# G% H6 I$ M1 H. DICK ENGINE CHANGE6 ~- b, z& _; ?
height above airport elevation.0 {( I6 d K a. M8 e8 }
NE, Altimeter setting 29.92 inches of mercury, 1013.2
2 }9 ]& E7 p. AQNH, Altimeter setting which causes altimeter to read9 S& k2 G2 n% r) n* y- x
height above mean sea level.
, f9 U, z, L# i& E/ w N活门,
) d) Z1 O5 \4 bP
! R v' l! H* s$ r% g0 n& ~ QPURGE VALVE, A valve in the pneumatic system for4 e- L' e; s n
PYLON, A structural component for supporting a
! j, b+ T3 Z$ ?0 W4 rengine from the wing.
8 C4 ]: f+ Q9 \7 Q O5 ]+ s% aQ
# z5 `5 Q. B" u& j fQEC, SEE - QU
1 j; J N t1 l$ E1 p# G" fQFE, Altimeter setting which causes altimeter to read4 [/ ] B9 T6 l& B
Q. j. U$ s: {; w% Z5 o$ o
Hectopascals or 1013.2 millibars.+ N8 S1 e: ]9 F4 b# e
调压和关断
2 n4 P& Y, K& C. A见Pressure Regulating and Shutoff Valve.6 P/ n8 q7 ]. ^
动力转换装置,: g1 K. J7 K6 C- Q4 n& J# ~. Y
见Power Transfer Unit.
, _" {+ g0 u: M$ T% a# E气源系统中用以清除空气清洁器中之灰尘的活门。. o: A( J! \( _2 _! n
速装卸,
7 Y9 l9 m6 }( X' U7 m% r, U见Quick-Attach-Detach4 t" o* C& T) z$ f2 { o
除尘活门,
4 n, n8 b1 U/ W# e吊架,
# ]( X5 W( ]7 t+ h8 T. ?7 e- F用以从机翼支撑发动机的结构件。
2 ~1 t/ O/ w1 h% P- x1 y7 Z快 ^% Q6 ]1 C9 g7 H6 v! e" T
.% q1 s& v, i: c; a, @
见Quick Engine Change, j- ~- J9 A3 u0 x! `( h; W/ q
快速更换发动机,1 j/ d# S4 D6 x
./ q9 T6 C: G5 K
场面气压,
`4 K _! I+ y准高度表设定,
. V9 @& ~5 T$ w: b9 ?, b2英寸汞柱,1013.2百帕斯卡,或1013.2毫8 J$ x& B% d3 i8 v6 t' {1 D
修正海平面气压,; \8 _6 ^ t9 V7 U+ Q: ^
使高度表指示飞机距平均海平面之高度的高度表设定。
. z3 G; i) {3 _) [$ L+ n6 r$ y使高度表指示飞机距机场标高之高度的高度表设定。
; Z& b7 `8 V4 n# ?3 p$ X8 B标/ {& j- d" X$ L3 N# v7 W3 X" N
29.9- n4 ~0 e3 m2 l8 H& k1 b% b8 L
巴的高度表设定。
- ]5 U7 g- \, _+ b* g( m6 R( [1 B英汉对照民用航空词典B OEING
1 c) O5 ^$ m) F# `5 E6 U$ z2 g9 e8 TTECHNICAL DICTIONARY 120
1 i! D+ J: r0 O2 n$ ]9 vQUADRANT, A mechanical component shaped like a# U7 X. q5 G$ `
quarter of circle for transmitting cable motion in airplane
. e8 j0 f5 \# ~QUENCH, A heat treating process to make the surface: k5 d6 f r3 r! V; F1 q
of a metal hard. The metal is taken from the furnace and$ M4 m" E- t5 p5 b1 \
QUICK ENGINE CHANGE KIT, A collection of0 J1 @& @7 i9 f1 Z2 ?( H* ?. O
e engine positions of a particular model
7 A& h0 q0 c. M0 n; Birplane.
! W |" c% `6 w" `' ang
1 g+ J# j& R5 haccessories (hydraulic pump, fuel pump, starter) to the
! U! x2 W6 L0 i7 y! P( X# Bengine accessory gearbox.
g( L) I6 p" |; Y, P. FS, Established the
: Q; ]+ n8 I1 e8 ^, K* t% Z5 Kminimum amount of time to cool the wheel brakes3 j- z" h q& g
before the next take off is permitted.
/ v1 W- v c% I/ z进油或水等液体中。* D* ?. z* F" b4 T& b' R
快速更换发动机成套设备,& N; L' v7 }: ]' `( c4 ~" E- z P# o
置的所有部件的集合。
( _, V- l5 a2 e8 F用以将附件(如液压泵,燃油泵,起动器等)接到发动3 ^- z; o# l) j7 s, a0 Z
附件齿轮箱上的夹具。
) r8 w; P; h4 E8 u6 Q" z6 N快速周转极限,
2 C0 {$ [6 \3 @5 S' h+ J在下一个起飞许可之前,已确定的飞机轮刹车的最少冷
7 ?/ M: x6 D4 D) L, B* t/ C$ J* T却时间。+ |% Z1 P0 X/ C3 \1 Z k8 h$ S
control systems.
: ^8 w, ^6 j4 @1 kdipped in a liquid such as oil or water.
6 j# ?; K* w a. N% F- q/ d: k" Tcomponents allowing installation of a basic engine on to% T, N) C% L. E, c$ o
any of th/ a2 ~6 `8 k, J
a0 R* i5 W: A! {1 F
QUICK-ATTACH-DETACH, A clamp for attachi
$ J4 x) V: J! W2 lQUICK TURNAROUND LIMIT
; l+ V" J1 x: p, }: U扇形盘,
! B) ?) |' g1 z1 K( E8 s+ o$ H8 s飞机操纵系统内,用以传递操纵钢索运动的扇形(四
+ N$ w0 X/ M' `; h" O分之一圆)机械部件。5 ^ W/ n% Z4 g7 U' H$ W C
淬火,
( Q; Q1 O: ^* c7 j; D( y一种使金属表面硬化的热处理过程。钢铁从熔炉里被取% e% D/ A" r! o+ n+ {
出后再被泡) i0 o! O: z* p5 i: M
用以快速地将一台基本发动机安装在一种机型的任何
- w& V* b( p# g( t4 l9 t发动机位
8 ^0 L: N) x7 I' J& h8 K- g快速装卸,
; }1 t3 Q3 N G- g1 ]4 N机- ]$ e K& @' Z5 }3 o
英汉对照民用航空词典B OEING/ W( _: c: F0 R3 V2 [+ c2 G
TECHNICAL DICTIONARY 121
$ I; ]4 M% X0 kQUIESCENT, Condition of an electrical circuit when no
* P/ e/ z3 W! Z1 l* B0 cRACK, A place for storage of modules in the
; f4 a# M8 N6 E6 k# G" rlectrical/electronic equipment compartment.
" M5 Y4 ?. j/ X& \$ eADAR, A device which measures the time between the
x; b0 J) F5 q- {5 H# ltransmission and reception of radio pulses and provides
) t7 D& k6 ~% B: e6 l( c' v% _information on range, azimuth, and/or elevation of: S& @1 G1 H7 l o
bjects in the path of the transmitted pulses.0 f% b" W3 I, h4 Z8 @# x/ Q
om a- e2 |: y6 [$ S0 g& \( o
ar.
: h, O; I5 [1 o2 R. rRADIO ALTITUDE (HEIGHT) (RA), The distance of an/ X6 g, s4 D% g4 U4 y
aircraft above the ground, as determined by a radio6 t! s v d: |+ r5 W; ^' t' O
altimeter system.: X+ a+ H" o2 C. [0 p7 d/ Q$ Z3 u
RAM, SEE - RANDOM ACCESS MEMORY( D7 B! N) V) C! S+ S
RAM AIR, Outside air that flows through heat
( Q6 u6 H9 J8 ]7 M9 aexchangers in the air conditioning packs.
- ~: F2 K, x. f5 Q1 S3 S- _1 v支架,
( j& I9 w6 P. ?6 V8 o. n; |电气/电子设备舱内,用以存放组件的地方。
7 N8 p g# W/ a& \- B% I/ Q9 S雷达,
& b& j; ~4 o; u: {2 K测量无线电脉冲从传输到接收所需的时间,并提供范3 h; [. _9 f6 B' t6 S' H
围,方位,和/或脉冲信号传输途径上物体标高的装置。
$ {) f( `6 ]; c由使用雷达的空中交通管制员给予飞行员的航向。: _+ [3 z! G6 E# H, `# u8 [
施发射出来的磁方位线。
9 O# {/ P% ^% o! K无线电高度(RA),
3 O' I* i! \6 s! g/ U1 k9 X2 I. X" t由无线电高度表系统测定的飞机与地面的距离。
6 b1 B0 J) ~2 k8 r# D [1 S, J$ O随机存取存储器,
9 T# W: s1 k3 P" x( U$ s见Random Access Memory/ Q @; @7 c4 n9 ?3 I$ w& U- [
input signal is applied to it.
4 a4 Z# h* L, g5 h; JR# a) W8 b% d3 {* t' b5 @
e
% P. h0 w4 V4 l6 p) qR$ Z X4 P1 p4 |% k
o
. X6 n) H4 Q' p8 |) l) k% z+ |RADAR VECTORS, Headings given to the pilot fr
1 `& p/ w. j( Z I8 H. Hcontroller using rad
. t# {+ r( E3 ]5 g) d7 k& I+ {! {RADIAL, A magnetic bearing extending from a
6 c3 {2 ~; q% i( w$ TVORNORTACITACAN navigation facility.
" O( S' ^) z8 P+ w) O. a寂静状态,
$ g* [" z: B1 g( v( l电路上没有输人信号的状态。
" Z }; N& p2 ?: a( j雷达引导,
$ s7 S! n4 U% l6 d/ V) C径向线,; N$ e) h! b' Y% u9 _
由甚高频全向信标/塔康联合定位/塔康系统导航设- s: O, L- f0 h. \
冲压空气,) b; V4 i, ^% }; q8 b+ p1 v1 `
流过空调组件热交换器的外界空气。0 _+ \' T" _( S/ K2 G& i |) c# h
英汉对照民用航空词典B OEING
8 O% e H$ q: Z9 x" ^; i6 ITECHNICAL DICTIONARY 1221 c$ F! D& j3 r
RAM AIR TURBINE, A device which extends from the# b9 n1 d: h m' l, U9 Z
, driven by outside airflow for, l: z: I9 d0 e& ? w
mergency supply of hydraulic or electric power.
* {$ A, _ O) m5 SANDOM ACCESS MEMORY, A type of memory in
; }: w! {& B! `+ Zdata can be written into and read out of.* @" A1 S6 m3 s% {" A
used for short term memory.
; g5 {( k; J2 N4 o. Y+ ~AT, SEE - RAM AIR TURBINE
5 u6 y# l9 Q9 Q; ~# hATIO, A specific relationship between one number
( E7 }7 L5 q& s& L" v8 P% V/ z, Xalue and another.% O, M3 r l/ o% U1 G
ATIO CHANGER, A mechanical device for changing/ o9 R2 Z+ K, W9 F8 n& i& ]9 ~
utput speed or movement relative to input speed or: e# i' { _5 Z
AW DATA, Data from sensors not modified by the user
9 t% `% W( S. t况下提. H u( F3 H J( |
液压或电源的装置。) f q5 b% d: o- {, o) S
机存取存储器,
7 b7 s, F5 n% _6 U一种可以将数据记载和读出的存储器。一般用作短期存$ f( j. @$ O$ K; W
。2 A6 K+ N" ^% Z- c0 k
压空气涡轮,
( t6 J" R" A! C3 x) @! t$ |0 p. _) K$ [见Ram Air Turbine
4 J _+ \5 g1 zside of the fuselage9 x* z2 g/ u+ Q5 V
e8 i: o% a- V2 o+ E7 ` B
R J1 F7 u! n9 u! o
which the
3 J0 g2 T: M, R. n6 y; oNormally
1 Y1 ]5 K( M1 V i, U4 }4 UR
E% E7 n G. R F) H' H* {R
; v3 S" D. ?7 R; l: y; c9 W* Vv5 ], N- v) ~4 ^4 a4 b
R Q8 G+ n" J% S, t, ^2 W$ p
o) O- U) H2 N3 c" ^4 }
movement.' u% A* |" E: w
R
m6 q3 _' I' L4 ^2 {- w$ r7 }system.' p% Q" T, g) \# j5 f! _
冲压空气涡轮,
: W7 \" r- x* |. j* h从机身一侧伸出,由外界气流驱动,以在紧急情( P( H, }* K* {7 k1 b
供. V) \2 A: W9 W. Q' q
随
1 N/ b6 l( b) |6 ^2 z2 O% L& K储) t9 s) i8 Z: H& S. z! N
冲
( e0 Y) O. `. P.
$ ^' r. l! d, W. t; w" Q0 M比率,/ V' C. Z; G) {) p& Z
一个数值与另一个数值之间的一种特殊关系。
3 A0 ~4 w# s S- X! y8 \' n率转换器,
4 h0 u; H" r% ~8 ^: J" e) S, B用以改变输出速度或运动与输人速度或运动之间比率+ k" x& P. e5 Q- b% q+ J/ E
始数据,
; _. X+ P9 L8 w9 ~9 x9 k, S! D. z任何修正的,由传感器得来的数据。# E/ v7 l1 N( N. q+ d3 L4 e* w
比# d$ E4 V5 U' D* V
的机械装置。5 i2 ~( r" t, J1 G6 I# y
原* E) y) M4 }. Z
没有经使用系统作: n: o6 Y; D" Q) b( m
英汉对照民用航空词典B OEING
; l" G) B, \- K9 e) ITECHNICAL DICTIONARY 1231 r1 Z3 W7 n* t9 Y( o( F* ~) g i
READ-ONLY MEMORY, A memory unit in which* S2 t& R+ f1 k7 m3 e' l
the computer. Under normal conditions the stored/ U3 m' N& M* H2 ?! T& f
information cannot be changed.( D! N8 B9 k7 e
ECEPTACLE, One half of a two-piece connector. It is$ N5 d( c9 z3 ^
usually mounted on a support, such as a panel.
; A1 n$ r, u5 W6 Q0 ?( j+ GRECIRCULATED AIR, Conditioned air mixed with air5 C6 z! `/ i6 a& Z3 G4 S G
from the passenger compartment.
) x4 ]6 g( \7 T" @* m, P9 qEDUCED THRUST, A thrust level less than maximum5 x+ E3 s/ G. [6 h$ w% x$ T; g% c6 H3 N
rated thrust.9 r- v& r' R, }5 O2 H; i/ x
EED AND PRINCE SCREW, A cross point screw with2 @' E" u% h* g% N6 U4 M3 G
a single straight line taper driven with a pointed tipped! w( T8 {' y" f
ED SWITCH, A switch with two magnetic plates acting0 d+ m: h- B5 }3 T* T+ ?, _7 R
s contacts and operated by a magnet.4 o+ k5 R7 b) J6 j3 t* l
只读存储器,: h5 b x5 g& E" [
含有由计算机永久存储着的指令或数据的存储器。在一3 _7 ~* j- Y4 Q% n/ L- C
作任何的修改。+ e7 s: n* V5 I, `* y+ D
插座,
% U; t2 v! v/ s; z# |2 }! d由两件组成的连接器的一半。常被安装在支架上。' |- b% ]3 u& Z! ]6 [* H* O: G
如:仪表板。
$ j9 y" D% f0 t$ u再循环空气," ^+ d2 ]8 c2 ^
调制后的空气与客舱来的空气之混合。! c( J l1 {. ?( H! W y
减推力,
+ c; @0 c3 T" u+ b6 h7 H) m! _额定推力小的一个推力级。
) N1 \# p, c) u& O; O十字螺丝钉,
+ b! N7 }+ O; l! D! m; W的,带有一条直线锥的十字) ^- ~ q9 L& U5 r \3 M
舌簧电门,
: F1 B* k2 b& p* e由一个磁体控制使两片磁片接触的电门。; O+ ^' P/ |3 j% y5 e4 i+ r5 K- s
instructions or data are permanently stored for use by
( [0 U# ~1 D" S" t1 dR7 O, h9 |) \' k6 I1 D; W' ?0 t
R: o* N: ?, a5 ^) ^
R; W+ k% t) c* i
Reed and Prince screwdriver. (See Phillips Head.), U0 [5 p* }2 @9 P* S
R
$ `1 i$ j) P0 {1 a" i) M4 Y# ja
7 O! s, |' p- c# H }& E般情况下不能对存储信息
|# s/ c s* y2 L" O6 u比最大
$ A$ G- I7 {) |8 g0 f# N2 M与尖头十字螺旋钻配套使用9 T: ]: k, |, Y$ c0 I) J- O! k' Q
头螺丝钉。
( \3 B6 ^) h# i英汉对照民用航空词典B OEING
7 k. v- n4 _0 H/ O/ {8 N6 dTECHNICAL DICTIONARY 124' y8 M7 w9 p, Q8 T0 x
REFERENCE LINE, A line used in a chart as the
% d6 |; G. Z$ g/ ?starting point for applying corrections to chart input
/ P" O- S# ?8 W; R- \( Ualues. One or more reference lines may be used in" w5 i, d# c9 ?
uccession.
: v' W& A7 Q d) r5 rD TAKEOFF, A takeoff which has been+ V1 U# A7 l! R% h) l1 M
.' |4 I3 N& @5 D$ M4 b
EGULATING VALVE, A valve for controlling pressure
" G2 X! c" e: w2 t6 QELAXED, The state of an electrical component or' y- P+ w+ ^$ [8 d) F; z
witch that is deenergized.
. L1 H- z$ P3 H) z: bRELAY, A switching device in which the contacts are3 U; Q9 \: t% k" F
opened or closed in response to separate current or$ u5 z% |! n) Q& H Y( S4 W
oltage.) \3 C0 K( I& i+ r- w
RELIEF VALVE, A valve which prevents high pressure* L9 _+ i* s+ x/ C
a system by venting the system to ambient.
9 S0 g3 e3 d. {* Y, F" C4 a. ]" G起点的线。使用时可用: I' C5 a0 J9 S. h: b, _$ }
条或连续使用多条。# s$ O; Y; `9 r* H3 {# Y. u1 ^
断起飞,
) W6 T L l& H. ~2 d' _$ a I离地前被停止的起飞。1 L6 P1 m ~1 V9 w" {1 |; C
节活门,
9 J7 c" Q [* m) c) ~3 S9 ]制压力或流量的活门。* p. v7 z! Q# d0 g l6 a" [
放状态,3 A# k( |0 F7 ?' r5 t$ k
电器部件或电门处于关闭或没有通电的状态。
3 j* L# m' P. W8 ^3 n. H* U继电器,0 L R7 `2 I" ]0 ^, T
一种电门装置,其接触点随着单独的电流或电压开路或
1 _# b( `. a0 \. s合。
* |& W0 w7 R" l9 _$ A- c释压活门,, @7 I& x( t8 S- I' ^) P
通过将系统与外界相通,以防系统内压力过高的活门。
$ Z6 o; y! r l3 q1 av
( U% J+ e7 R% s: a6 L6 M1 u: us( m9 g* F$ ?) ]
REFUSE2 a$ L" h/ r, }" h# ]$ ]. V
stopped before the airplane lifts off the ground
2 i3 ~7 k/ [; d! KR
" D' x% M' }8 l1 |0 Y2 s6 xor flow.
/ ]. H' S! x) [$ E# e8 E' c4 b! vR. L8 i1 P; [ M5 |+ z1 g
s
& u: H$ _( U3 O5 v) av7 [1 D0 a: X/ ~8 ^# Z0 A( Q/ l8 a
in
7 _$ m6 {$ N' X) [基准线,
8 x- N4 c% u8 ~- f8 x在图表中用作修正图表输人值的5 g" T+ }0 o6 o1 P j
一& M: w c! {- y2 W; _
中
4 |3 y8 p2 ^4 Q/ I( C* m在飞机
" Z5 Z8 [3 U: l调% e8 y; w8 r* v) M' T; j( \) D# V
用以控
; A5 h& m7 Y6 G5 n0 I释6 c. Q P' M5 y/ _& g
闭2 [! g4 Q3 x" H+ M
英汉对照民用航空词典B OEING
S1 z& }+ R X7 [TECHNICAL DICTIONARY 125( {" W# g* ^7 l% |
RESERVES, The required fuel remaining on-board after& A7 ?4 Z3 ?/ U8 ~3 { k% |' D) f
ESERVOIR, A container for storage of fluid.) A& Y9 y! p. o! `
ESTRICTOR, An orifice for reducing the flow and
! m$ t& U( z' _ressure of a fluid.
1 a) S! r2 z4 T' |+ l- BESTRICTOR CHECK VALVE, Same as restrictor but. z) L1 J5 o7 Q) Q& G' f( l
llowing flow in one direction only.8 D- k8 [5 z! V9 |& y/ A( R4 Z- {
decrease the
$ j5 A: u! H8 m5 q4 Sngine thrust to idle.
0 B0 a/ F) ^& M' {" j* TREVERSION, To change to a pre-determined mode.
- F8 B) B. g1 ^! @ctrical device for changing the0 ^% V- a6 }* k0 x
sistance in an electrical circuit.
; _; r3 t) g+ |( ]4 C, i备用燃油,2 Y( g1 b4 ?5 j# ~
照规定,飞机在到达目标机场后,机上需要的剩余的燃
0 k! H; }% ^$ b& I. n) a油。
+ A* P2 `, W, |$ N储液箱,& W% ?0 A$ a2 {
用以储存液体的容器。. w7 a9 ~5 I* K1 r* P. j
限流器,1 c, @7 w2 P( D' n, _
用以减低液体流量和压力的量孔。
1 D9 _& `* ~ ^5 Q流单向活门,
6 T4 e% m, H2 X, i3 E5 m O: q一个与限流器类似,但仅允许流体向单一方向流动的活
! f: m. X: O1 F, ?( c( |% K门。
+ q( R$ @0 Z* v& l9 L0 \门,/ M- \8 V2 Z0 u8 ?: ] \
自动油门的一种方式、用于将发动机推力减小至慢车状
- _) ?6 B8 k: M: U" W) i。
* S( W' d$ o) i改回到预定的方式。1 A% d' {8 @. @* A; m8 p& T! l
用以改变电路内电阻的电气装置。
( ?# q A- S' Rarriving at the destination airport as determined by
4 t, S& Z6 e2 [/ L' [# Vregulations.
% z" y- F$ u! \3 y& OR3 ]% j2 D1 C5 E* h' V( F$ w: @- p
R
/ g4 q! d5 x1 C4 h1 ^4 q' lp+ \) W1 P: W7 F" |# N' x! M
R2 {8 i2 e }' Z9 F
a
7 \1 E4 ]4 Y t! ?. q8 w9 eRETARD, An autothrottle mode used to
9 [+ N d# D+ A0 [6 A9 x* Z1 K' Ge
& ]$ _- s8 j5 B: U& PRHEOSTAT, An ele
1 @% Z, j/ h( [# [( G- x$ w) W1 n! Hre
5 K- v7 X( U& U$ z6 f! w限
% h `) c% G$ k2 u2 W+ Y拉回油: R7 P1 c8 o; x- N2 s4 V0 ]3 g
态5 h( Y4 V0 K* s" j5 ?: k, m
复原,
) Q- y3 h6 f7 F5 r7 o: D+ _变阻器,6 ?/ p& h. J6 h/ _3 _
英汉对照民用航空词典B OEING; c' W/ L* N3 t8 J3 h3 U
TECHNICAL DICTIONARY 126
: u. W7 i& l" r( {RIB, A structural member of airfoil shape in wing,1 w) H4 L3 ~7 I G9 R
stabilizer or control surface.2 W( {$ ]. ^3 p
IG PIN, A metal pin for inserting into a moveable
: ]# b7 V1 L+ u xomponent before adjusting the control cables and
4 Z- S# x( w( h' {6 q& C2 J0 B7 Z# hnkage.
2 q4 W' f, _! W2 I; ^IGGING, An adjustment of airplane controls and doors
* Q# S- @" M0 n/ ]+ rr proper operation.' \9 j. K8 s$ U& e3 k' {
onditioned air supply to the passenger cabin.
/ d( ?4 C6 a, Z& r/ Y, D装销,
$ G7 I5 H+ s) u/ _- [在调整操纵钢索和链系之前,插在可动部件内的金属
# I0 Q+ O) S8 a' }# D。1 O4 y5 @' |( J0 x) G3 X
校装,
; w# @2 e# M, `$ h$ t; o& V使飞机操纵系统和舱门能正常工作而做的装配调整。
% e* ~/ M# h# |6 j8 n4 r+ D1 [空调系统中,将调节好的空气送到客舱的管道。
$ J# S J9 N8 a2 B2 q5 [R Q9 d4 d" F1 @ m) Z) z% [3 U
c
7 ]; i4 o3 U, a9 n6 O" L, hli! _! f5 r" O( u% i+ U
R0 x( t5 B% R+ p
fo
" }" B/ g: [( p# I, RRISER, A duct in the air conditioning system for
) p; \* N6 i, K2 z/ Zc7 j+ K) J" c: X, R/ s
翼肋,+ \; }) n5 s2 {5 U! D- n9 H9 ]
机翼、安定面或操纵面内具有翼剖面形状的结构元件。+ H$ O3 Z3 W* O8 d
校
! k/ n! g) u8 `! @1 @) E* h销
1 u( z: i$ s' c) u% U3 ]立管,0 Y8 u1 m! w" A! X, ^
英汉对照民用航空词典B OEING
6 K( ^# j9 m" vTECHNICAL DICTIONARY 127
* _) v4 C; y, z rROD END (NO. 1), In a hydraulic actuator, referen
+ R& J0 R! ?( t9 Ithe part opposite to the piston side of the actuator.
1 P2 n+ v. M- }; O4 gce to. f4 U# b( \, j: f7 S/ c
D (NO. 2), A mechanical device usually a, M9 t& d4 G" ^8 h' r
bearing, clevis or similar component attached to the end
, w$ q/ K. B6 q& M X1 Q# ], Yof a link or push-pull type rod.' ]+ `! k: B4 U! \6 f. v4 P
OLL, The rotation of an airplane around its longitudinal2 Q1 U7 f! S3 Q3 I' W
axis.8 [! ^, B. ~' u- l5 s3 [
OLL AXIS, SEE - LONGITUDINAL AXIS! D4 z$ P- b4 C. [3 ~; a* [
连杆端,1 H1 X6 }6 E6 J) {) N
杠杆端,7 Z( U& z8 H0 J! E- M ]& Y
一个连在活节连杆一端或推拉杆一端的通常是轴承,
: t9 ]7 o" ^, d2 ~/ L7 j" L吊环,或类似元件的机械装置。- X( Q3 _! f! r
滚,
4 w; w9 h6 Z# z. b% P9 J飞机用纵轴作为旋转轴时的运动。) o( K% z. v0 F$ j. g4 I9 Y* y
横滚轴,7 K6 K" B9 K: h9 S
见Longitudinal Axis
# d$ l v! ^& f+ V5 LROD EN) A7 G8 v1 @: }% D/ E6 t
R$ n. R, S# ]8 O0 V
R# X# v& |9 r, O
液压作动筒活塞连杆伸出的一端。
; V7 r' b) V* q S+ G: y横% U8 C' l( x$ O1 G
.% p; z2 s( Y1 t% x* Z/ i% G) ~' o
英汉对照民用航空词典B OEING
3 \5 o/ M/ u% nTECHNICAL DICTIONARY 128
1 S: ^/ R- j; m) `7 jROLL RATE, The rate at which the airplane moves
6 g3 c; [, K2 X3 K( e2 Aon the roll axis (wing up, wing down).
|4 V2 @1 L/ c0 J. R" ?OLLOUT, The final phase of landing where the
* b+ k& \: |5 _+ @, t3 m% AOTARY VARIABLE DIFFERENTIAL TRANSDUCER,
3 `/ n/ [5 m! t0 e5 F/ }1 N" mROTATE, A maneuver conducted during the takeoff
" c8 ^2 Q% h7 n* L2 Hn. t6 f, h, m1 c* w( ]
raise the nose of the airplane into
6 l% Q3 N# E: d" t1 O0 Ke air.
7 y. j0 [* _( T N$ qOTOR, A rotating section of an engine (turbine,4 @$ }1 B3 f+ j$ t
ompressor) or a generator.
& B* E6 Q* |1 RROUTE DISCONTINUITY, An FMC operational E- ?2 o1 C h; A
condition, in which parts of a route are not joined or
, g8 t; H1 D2 M4 w8 v9 g$ bconnected.8 I& F+ R* n3 A1 e1 y3 n Q
ROUTE LEGS, The portion of a route which connects6 u9 d! h( I. G7 Y/ Q3 G
two way-points together.% S5 q! u" ^% ]' c) ?1 o" Z$ c
陆滑跑,
2 ` M8 t+ X6 T, f: \6 {的最后阶段。此时飞机在跑道上减速。
6 c$ s% |: i& a; u9 Y,
! z' E2 r) B* w8 h$ RR2 ?, \5 ^4 I9 J8 t; H+ T
airplane is slowing down on the runway.! b! Y9 j/ _8 c2 q, P
ROM, SEE - READ ONLY MEMORY. ~5 k5 G' {7 C+ W3 Q
R
- {$ I! |2 k8 n4 FA device with a rotary input and a linear response.
9 m _7 a# \$ \" g+ g4 A f" L; Jground roll. At the rotation speed, the pilot pulls back o( {' z; B; @3 Q) o r
the control column to, w2 m. B$ m, L: h" w0 F! D; Q) D4 g6 u
th
& o. R" m+ t/ u) t* h* l( u% lR3 z, m) C$ F: H& G2 |9 ^4 j" Y: K! g
c
: B8 Y; y- M' h" q3 v3 K横滚率,+ I( ^" h% X) o# ~
飞机绕横滚轴运动(机翼向上或向下)的速率。0 t0 P2 Q. L6 T) T+ S+ P$ B) i3 i9 T
着8 V d& `+ z$ ~" C2 k ?/ _: m$ F
飞机着陆
O9 g8 ^$ i/ Z( d9 w只读存储器
9 B' R* ]% G' v/ S见Read Only Memory
* j5 y4 u0 c+ \旋转可变差动传感器,! B; Q2 \: Y* V6 g
人和线性感应的装置。 ?( F8 g" b) U) g, P5 W
抬前轮,& L$ Q. j/ S( @9 @0 g
飞机在起飞滑跑期间所做的机动动作。在飞机达到抬前
- n% s, l' r5 H& W4 z; B发动机(涡轮、压气机)或发电机的转动部份。0 o# G) b$ M; U
航路不连续,& s9 {: u( R2 k+ F8 s0 R
一种飞行管理计算机的操作状况,航路有些部份不相连& R+ m/ |; ~' N4 y. Q
或不相通。5 U& M/ x$ c/ u* `; c
航路段,7 U0 d) Y# N8 D: g& n
将两个航路点连接起来的航路的一段。& O3 ~2 z3 m; _; | I' f* U- M
一个具有旋转输
3 c2 h2 x% ]% N- Q' `& y; n6 z8 m轮速度时,飞行员向后带操纵杆,机头上仰,前轮离地。. Y5 S: p: Z) ? V# P( I
转子,0 q% f, u2 f+ y
英汉对照民用航空词典B OEING2 [/ ?9 ~6 ?: q* v/ y
TECHNICAL DICTIONARY 1292 v! }6 b- K' T$ Z
RUDDER, A hinged moveable part on the trailing edge* @' }$ I4 u6 v N3 u, ~
plane yaw (left and right)
+ l& h, u8 T9 [) @$ O2 i* _+ f3 h+ pontrol.
$ ?# H+ o) Q# M9 h* g' ~2 }RUNWAY VISUAL RANGE (RVR), The horizontal0 T" A( M% Q3 P' j+ A; k+ G
a pilot can see down the runway when flying an8 E; o, p5 [1 U3 \
pproach.
1 n6 R% ^4 U1 J ~+ p8 z1 Uof iron and iron containing metals.7 ?1 I; `. N: }/ r7 w
is usually a reddish brown color.3 V1 j; Z* R0 r" }' r1 a& W: q
IAL6 E1 G; |5 `0 q
TRANSDUCER
' g$ T6 k4 x+ H) q. L# q4 CS$ `0 P/ l/ B! E2 d! k
SAFETY RELIEF VALVE, A valve in the pressurization; P/ Q: L2 }& t2 c0 x
system for reducing cabin pressure to a safe operating6 J" S1 G# H( f6 w. B# t! |
pressure.( G- M8 N& E+ J6 T) W% D7 f+ }
SAT, SEE - STATIC AIR TEMPERATURE
3 J2 w( Z& M2 x5 E3 W0 a8 H或向右)的可动部件。* p$ V% c) u7 z ` z! _2 e+ T
进场时,飞行员向跑道方向望去所能看到的水平距
4 B" s! S4 Q1 ^( A" R: p% W* R。
" }1 P( Z( O" ~: b" O铁和铁类物质的氧化物。常为褐红色。
! T$ [8 b* e3 w4 M' R8 b% b见Rotary Variable Differential Transducer
( _* x% T" o% S" s/ A9 i* vof the vertical stabilizer for air
& N; `, P% y: j" H; V! z; Jc
/ X1 B( T9 ~" y, _ M1 T! wdistance
" l( f6 F: n3 T6 {a
' ^- V2 v; p2 G1 ?8 R% K+ H! \RUST, The oxidation" Z V7 O/ ]& R$ T
It0 w; C; y k/ `. J( }
RVDT, SEE - ROTARY VARIABLE DIFFERENT
. m4 _- U; z# c$ ?- ~ P- [. i: E: c方向舵;
7 T. S; L/ y+ `. k铰连在垂直安定面后缘上,用以操纵飞机偏航(机头向8 `& H l! \+ b- T- O
左
& m. |: G( G0 l, c跑道视程(RVR),+ j, n8 W: s1 U9 B9 y
飞机
, G- `1 F: i$ E) g* b# V d$ H离* _ k! w7 t1 I6 v3 x. P. X
铁锈,0 Q* |: E0 e' Z4 L' s
旋转可变差动传感器,6 [% ^8 E. \4 e% R7 E- v1 @* r0 v
.
; o# c v( p( r: c a安全释压活门,, d- r2 K1 t S! n
在增压系统中,使座舱压力减低至一个安全的工作压力& Z* }# `$ a0 s0 R; {
的活门。; ]- H% F+ t" m; S% d
静温, {0 L8 O8 D- ]) m+ f E, Y
见Static Air Temperature.
& f3 R7 o" I& Z I+ i6 K9 R英汉对照民用航空词典B OEING7 d1 N3 G6 e- X
TECHNICAL DICTIONARY 130
4 U. k6 ?& G4 m! {$ {SCAVENGE, To remove oil from the engine bearings or3 V: [9 y9 @2 r9 N0 Q
to remove water/fuel by a pump from a tank.& C A- [1 t3 q: n9 y
CHEDULE GENERATOR, An electronic component in
5 m5 Z6 H4 H' g! S9 x$ te pressurization system for controlling the operation of- `. l8 M, r; G" w; o( s; u3 d
e outflow valve.2 t8 p; u' r% t" m, E. q
CHRAEDER VALVE, A valve for inflation of tires,$ n: g7 d. T0 O4 z6 ^6 i4 v
truts and accumulators and for pressurizing the water+ \9 M1 {- ^& J7 B0 ~) @' D7 c5 ~# h
CR, SEE - SILICON CONTROLLED RECTIFIER
- g l: C* E+ Q# RCRATCH PAD, An area on the FMCS control display: n/ J+ f- a: T; {- j1 g
unit used for showing characters activated by the
5 p! A" d1 a) G2 g2 Zlphanumeric keys.
' m- t$ \7 |, _- {) OSCSI, SEE - SMALL COMPUTER SYSTEM
' K6 V/ Z r) t! OINTERFACE; B( z* q4 ?+ f, Y
SCUPPER, A shallow receptacle around a filler neck of% ^7 W, t. x8 G, z3 M
a liquid tank to catch any overflow or spillage from the
1 b2 b) G& f H$ m9 c; c. Gservicing operation. The scupper is normally fitted with a- \' p3 V9 l1 o+ F! }
drain overboard.( \- `( n$ N5 i' o1 |, ?
SEA LEVEL, The standard datum plane from which
4 p; v" C# i. E2 E1 ?altitude is measured.1 }7 B" E+ d: f6 c; Y4 `+ P
去油箱内的水和燃* N, ?' h/ Z, Z
。' z. x6 N* S+ ?: d
程序产生器,
- _2 l0 g3 w" u: F在增压系统中,用来控制外流活门工作的电子部件。5 w, \* k/ z( q# _! R% s
chraeder活门,
' a. j7 W! G& R# W% x2 k; d. QSchraeder公司出品的一种活门,用以为轮胎、减震支* k3 g' N( K6 k* H
充气,也用于从外面为水箱增压。
( E9 P% u: `# v1 O* J可控整流器,2 y6 X: R; H0 S v5 D+ E. Y5 V: ^
见Silicon Controlled Rectifier# }2 A. H2 D3 ~ u1 e
S5 ]3 q% V7 o/ Z" h# X" o
th
+ f4 O/ E/ M- v; l3 E; b3 ^th
H7 b0 J$ k4 `! A BS
% b) w6 }9 ?; `' M0 i9 Ds
, N- c) {$ e3 b0 Y/ Y( Y- {tank from outside.
4 C" a! v2 B% \ k! eS
- H; c; F1 c5 T. PS
. A5 @. W6 h- y' g- Ka
# z5 A+ z; D" h+ |0 T. q% h回油,
: M) s6 D& y& p. m除去发动机轴承的滑油,或用泵来除" q1 L u8 y1 g# T* Z8 P! C& G
油- C" j' E' k+ ^. j5 |. O
S# K$ Y9 S5 z" X- c9 {6 u! w
柱和蓄压器
/ g9 a2 {, Q* G. H- t硅
- c* m& n* n1 j* U# D.
3 o) O" B' ^( U9 Z( F" y: H稿栏,
; e! A$ r( l0 NFMCS显示器上的一个区域,用于显示由宇母—数字键! c: y+ W, l' Z" g
激发的字符。+ R% X/ Y4 q2 Q9 l! }
小型计算机系统接口,- u. Q2 q! h/ `6 N5 \
见Small Computer System Interface
1 h; N5 B8 P. _6 R6 N草
* o8 H1 s, J4 M N+ ~盘! K' g0 j% L$ j
.6 F+ J# S0 K; l- e) ?
放泄孔,
+ F9 a' W$ o7 Z. p6 [* S液体箱的加注咀边所装置的小型容器,用于接取勤务过6 q1 C8 A9 Z, L/ F# z
程中任何溢流的液体。一般都装有通向机舱外的排泄管8 n3 F2 R. F7 S7 e7 l; A) D
道。
. U2 z4 c3 E# x3 P$ `* e: Z海平面,
8 y+ H/ L$ c e* S4 g% W5 F用作高度测量基准的标准平面。
4 J- _7 o7 A3 n: o( o0 V t英汉对照民用航空词典B OEING, Z; h2 G! d5 g$ \
TECHNICAL DICTIONARY 131
4 ^! C4 ?& a8 z: Y, GSEA LEVEL STATIC THRUST, Maximum rated power
+ }2 n5 e2 z; E) l" z wproduced by a stationary jet engine during ambient
) }" {1 d9 G- z3 g" f3 Eonditions at sea level.
, n" ]- b& J: n; Is for. o0 I: y# R. c1 [& Y; @$ |5 z; p% v2 y+ [
reventing air or fluid leakage.
- T8 n+ E% ~) e2 \- {, c. o$ x9 ySECTOR, A given distance between two checkpoints in# o3 t5 Q, n4 N; p7 t1 r v
e flight plan.4 K/ Q, r, k2 g8 p/ U
ELCAL, SEE - SELECTIVE CALLING Y9 m K$ ~. W8 e: X- a2 \' [
SELECTIVE CALLING, A system that automatically
2 F; [ W# n( j1 O9 K }- m+ g; {SELECTOR VALVE, A valve in the hydraulic system for
% F" ]# v' }6 T3 u5 f) Uo one side of the actuator
4 A* @* ~0 d* `# j! Gnd the other side to the return line.
4 z& n% d0 u- U/ I5 E* X力,/ [+ b' K$ ^ Z1 f$ i* ]$ d- k
在海平面环境状态(大气温度、压力)下,一台固定住
9 B, S2 d1 Z% ]的喷气发动机所产生的最大推力。
# C, r& |% F9 X( ^$ L% `2 f" ^在两表面间防止空气或液体泄漏的元件。4 q% j6 Y* W9 D% ^: l, H
航段,8 A0 i8 K! ^: P# N7 ~% d& o- a3 H# Y
飞行计划中,两个检查点之间的已知距离。9 `# X+ s3 ]3 ]8 X8 D" g
择呼叫,& [+ _9 _, W5 N7 S
见Selective Calling
4 d& T! F: p! |7 D( d A( x8 O; Rc/ g5 ^! k5 l3 V4 K
SEAL, A component between two surface; } m, w- d& G! Y9 K( U
p
- z1 @, u3 ~# H/ @8 Rth
- Z: B8 ^& N$ u- |2 ES" H0 n6 P2 e. Q% ]6 }
alerts the flight crew to a call from the airline ground
0 y) s( Y. }# C6 G0 s3 jstation.
% L* W: U: k5 T- c6 vconnecting hydraulic supply t& x2 D( u) F- |: u! [; }: W3 N
a, R9 h; W8 t% O/ r, O* h- ]( N
海平面静推+ L& y& W* k1 L1 s0 I0 g
封严,5 f" @2 }) q& R8 ]
选5 c& i6 Q3 J* y$ s1 c# [) n
./ a, ]1 Q* n E! D$ h
选择活门,
4 E& I, u- `9 D2 Q2 C' k9 L端连
' s6 ~8 u. j( }% s8 T" D3 T. n; q3 ]回油端的活门。
1 d* Y* u! T4 F8 x选择呼叫,
- v; A$ H6 d2 j一个能自动将航空公司地面站呼叫报知机组的系统。
# h$ u" M+ l2 y5 R7 m. m液压系统中,用于将液压源一端连接作动简,另一
8 s) `4 ^/ e: |$ h7 |接
X+ Z3 P" j: z: ~; N' F英汉对照民用航空词典B
, h+ t0 ?5 Q6 a$ {3 [ g2 TSELF SEALING COUPLING, A connection between two
2 H h: q5 n3 T' N* T4 Z) Hfluid filled hoses for preventing fluid loss when the hoses- S6 q4 B9 B: d3 B) q, g9 m
rated./ Z3 p- e# `5 M/ [1 F
SEMI-MONOCOQUE, Type of construction in which the
, ^2 b- E5 T; w5 {& Q3 MSENSOR, An electrical device for detecting variable# e$ e) u& z, c! ]! c3 g. }6 q
ENSOR ACTUATOR, A device for operating the; f* H; ~9 @. d
SERVO, An automatic control system which checks its
1 ?5 G$ g8 X$ V- q# ogainst its input so as to achieve a desired
* ]# @3 _7 n0 FMED, Hydraulic pressure for the servo is2 H- h b/ U3 S w4 W: I- M
resent to allow the servo to internally synchronize to
4 Q4 i) ^4 R+ D" D( {* `e proper position, but the mechanical output of the
1 k4 H- X' i+ j% S) rervo is not connected.. U8 I/ N) i: p9 N& x7 N
自封接头,9 z5 V( e W1 r3 O8 N. z
活门堵住通道,自动封闭而不+ Y& j/ x4 u9 h
让液体流出。
% y) X( p$ [" L- ~* e# H半硬壳式结构,
, a" W/ y! j" e* j使蒙皮,长桁和隔框共同承受所有载荷的构造形式。( {; s) E9 S8 K3 q }
感器;. j3 R4 _+ H' \) O5 X
量状况并将结果以信号送至指示器和指示灯的
# H( ?( s1 C2 g0 ~电气装置。
, z3 V: o6 Z0 ?! v传感器致动器,
) ?% E( i, k3 K( N。; K7 ~8 Y3 u: ~
伺服系统,
- Z' {# g- w9 P# _7 J. `能检查输出和输人数据,以便合适调控的自动控制系
7 I: b i' {+ Y4 L+ l0 q统。
. W2 B- W7 y: q6 U, F& C伺服预位,
9 A5 D0 x b$ r% s液压使伺服系统内部同步至适当的位置,但伺服系统的2 i0 [( \: Q5 ?
机械输出还没有接通。( j& i" h# G3 c3 R: P! }7 T8 ^
are sepa) D6 H' H5 S3 K6 x$ j8 N2 z2 R: f2 P
skin, stringers and frames carry all the loads.3 G' i- p/ ], @. Z: W+ F B# U5 y' [
conditions and sending a signal to indicators and lights.
$ G x/ X+ ]+ o7 _4 z0 V7 r- `% z: qS' p! x ]. W S3 o
sensor.0 k H4 b) t5 e% c F4 d
output a- X8 I1 m j. A8 Q
control., x; g0 @9 X2 X5 C. L* k
OEING
/ H( P* ^; ^3 E+ qTECHNICAL DICTIONARY 132
0 Y+ m: ~# i4 m( X, D2 N0 \$ FSERVO AR9 b6 l* O, {/ y8 j0 h' \- z- F
p# f* K- i2 l$ A7 ^
th$ R" H$ H6 M# a5 o4 ?' N! x2 Q. i
s' U( V- ^& S& Z% ]& O+ V
用以连接两个充满液体的软管的特制接头。在两个管子
; L- f& c, [% ]% Z! d$ f6 S# n分开时,接头内的弹簧即使: ]9 |; ^# J8 Y& b
传
4 E; H4 T4 a% @$ k; Z6 o$ ~检测变
7 M" l8 c6 p7 G. ^" q9 |用以操作传感器的装置5 T$ _$ {( [, s
英汉对照民用航空词典B OEING
% ~9 m/ H& Z4 `# i6 fTECHNICAL DICTIONARY 133
, D7 W- U+ x. j) Y4 j1 ?SERVO ENGAGED, The mechanical output of the
, [2 v5 u/ l. ]% U; e3 H1 H) {0 a8 ^5 Eservo is connected and the servo can move a surface or
: W. x, p- i9 a2 Y7 S1 B0 b- Dontrol
9 a4 a4 ?. s& Y! JSET SCREW, A small screw (usually headless) used to0 U7 B% T0 Q5 ]# P+ f1 D
eel, or knob onto a shaft and prevent G4 w) y& M4 ^9 G% _# R
tation.$ K/ L; m+ g$ l# g& P3 F
SHEAR, The stress exerted on a material or, assembly
* R, w) J! ?, ?4 |9 Z2 [% F, Vwhich tends to slide the mating surfaces parallel to each
2 \0 E! e) B' y1 jther.5 @+ v. k: P6 p( t' E' [% T8 O
SHIMMY, Rapid oscillations (left-right) of the landing: K- \. O. ?) w. q3 m2 N
ear wheels.
( A2 Y6 i3 C/ X) `" h. ?预位,( G$ R9 z* Z6 U; J" @ ~
伺服系统的机械输出与伺服系统已接通,伺服系统可移
/ A9 Z( K1 c7 i5 H, a- [" Y动一个平面或操纵。
& D( h# S2 R; F小螺丝钉(一般是没有钉头的)用于将滑轮,车轮,或5 C( g7 \3 h2 |2 f! t0 P
钮紧固在轴轮上被免转动。1 C. L6 ?2 J' Y7 K
c
, ]! V% {# ]9 {, K4 ]% Yfasten a pulley, wh
1 T- c a5 x( m1 O4 Gro
) ] m, |: ?! q+ p7 W& OSG, SEE - SYMBOL GENERATOR5 m! o0 i4 R, K
o8 e2 L: t* }2 k
g
" f$ ?( |6 D5 Y伺服系统9 j' B( N& Q. B! e
定位螺丝钉,
+ H, |/ }5 A/ t# ^4 c. _6 u# K9 o旋9 c6 j! p* ] M6 l2 P% Z1 F4 H* g
符号发生器,7 m: F) B3 F8 @2 ]: Y" |
见Symbol Generator.
8 W, [8 A, A' B; H0 o7 k5 O7 y剪切力,: |- w5 m: Y- Y! r
加在材料或组件上的应力。该力往往导致互相平行的成
% f8 q, e" B% H% u% x- H: a& v4 b对表面滑动。: P( s- u8 h' B& p& m) }
摆振,% D5 _, u& m( t6 a
起落架轮子的快速的左右摆动。
9 `* V% \7 Q: C* z" k$ z英汉对照民用航空词典B OEING
& B: i$ k/ s% c7 t) K& pTECHNICAL DICTIONARY 134
- M* ]6 u6 L( l5 m0 jSHIMMY DAMPER, A hydraulic device for damping9 }& b* m% b3 s! p- E$ p( p
shimmy in the landing gear wheels.$ |2 G0 a7 q- U& n. Q, l
ar for
% @7 h5 m: f9 I" Ssferring oil from one
; ]% b; P' u* A, ~* Achamber to another through a metering valve.8 q h( ]* R K" D" X! N* _* \
,2 \7 ^, Q: k2 k( V
一室以减# n( D q. z% B9 j/ Z1 Q
着陆时产生的冲击震动的部件。
) q6 b* {: o5 oSHOCK STRUT, A component in the landing ge) S: {( O! A8 g8 q3 V
absorbing landing shock by tran$ }5 ^7 Z1 z: W! ?# `
减摆器,
9 N' I. S/ o+ i# }" o- x4 `& D用以缓冲起落架轮子摆振的液压装置。
. C5 ^% o# R: J9 ?& m# x减震支柱# @5 {/ S3 M" D6 z* m) n
起落架上通过计量活门将油液从一室转到另
4 K% B, c0 X! g) w. T7 T$ A1 x+ D8 t少! l0 ] z2 B0 i7 s+ s, \
英汉对照民用航空词典B OEING+ @( H0 D2 U! a; I& f$ O \! P& a
TECHNICAL DICTIONARY 135" m, J0 \: l; S
SHORT CIRCUIT, A fault in an electrical circuit
5 W! M! Q+ y" P' G" Qoccurring when the power supply goes directly to6 R6 @3 _" Q' g+ z7 V# n# Z( K
ground instead of to an electrical component.& b% [5 | T: y8 p( q& [9 ^
SHORT RANGE ALTITUDE, A cruise altitude chosen to
# x2 }2 H$ }5 Q" O1 G0 }9 Qinimize fuel burn during short trips.+ X) a7 P0 Q, d+ @8 X
HROUD, A metal covering for enclosing the APU on6 I2 s) n: o* m& K/ W& X. W
e airplane. An external tube for enclosing a fuel hose.
1 E; n; {0 k6 \- b4 p- mHUTTLE VALVE, A valve in the hydraulic system with) V" W- s e0 @7 ` i7 j8 |9 W
- STANDARD INSTRUMENT DEPARTURE U3 M/ O* n. U2 A- L4 N) ^5 Q
f the
1 c& y" q; Y% P. P9 z+ Qr access to the components on the engine.! g1 o; j. g& x: o9 y
短路,
- p" n \, ]- A8 u3 Q% C2 H短程高度,
! |- \9 S( a( z- g9 F2 U- z为在短途飞行中使用最少燃油而选的巡航高度。+ q/ c0 z2 q* E, [2 X, k
护罩,* A! K$ S# Z; V2 B# _0 I7 f
飞机上包围着辅助动力装置的金属罩。包围着燃油软管
5 M" Z6 M+ ~/ l% F# J: T) v' J用活门,
- v0 [# P7 R8 `0 a" [' ^液压系统中,具有两个不同液压输人管和一个输出管
+ ]+ Y! x2 d$ H7 _# o的活门。9 Q1 u7 V/ _3 Y! Y+ b' K+ w: `
标准仪表离场,! \( k8 s, M8 p, l
见Standard Instrument Departure5 Y% ?/ b; y: m; Z! j8 ~% s1 t
m, V- q& S. k; C- T
S+ ^, i; T0 g* k" B
th3 V+ E9 o8 E+ e5 u! r3 C' K! r
S5 a H3 K0 T) l$ z, j
two different hydraulic supplies and one output to a
5 x2 Q9 H# ]$ {7 y: Fcomponent.
( R+ t5 L. C7 v7 i# Q3 [1 Y& fSID, SEE
) C$ L9 B. \9 w& @; M1 @! s) qSIDE COWL, A removable cover around the sides o+ v% Z# n" I7 Z. y, H$ K+ f
engine fo
+ y' }4 n0 Z6 n5 ]/ T* {电路中电源未经电气部件就直接到地线时的电路故障。
; ^( j( p. D) t" x: V' N防
4 w T$ i7 ?; J4 }8 |0 a的外管。
! ]9 k8 r: y; ?两
) [0 ?" `# Z4 n- a.. a. e, Y7 ^* g6 u7 n ^
机两侧,被移开后可以够到发动机部件的可卸罩+ d5 V3 V; q" b1 e6 q
。! p2 ]3 R! [; [+ I* ?
侧整流罩,, B$ G( Z; H* V; p. H; \
发动
( K4 r; p7 `& O( C子; t K+ E: O* t0 ?0 v
英汉对照民用航空词典B OEING. b9 g8 ]- n1 i1 b& J! p+ O* U
TECHNICAL DICTIONARY 136" C( g2 Q! J) K0 M% d! A
SIGHT GLASS, A glass window for observing fluid
: @5 i) f; b2 s+ J: c0 y/ U" j- M0 M1 Rquantity in the reservoir of a machine.- t: R" x" C6 \- U# |, W. s9 O
, that can be used to transport information for9 }; V; W7 h, L) _1 R. [ f
communication, control, or calculation.
7 a+ D) V) ~4 e; L# g0 Z/ XILICON CONTROLLED RECTIFIER, An electronic8 @; H" @9 Y+ j+ E9 n4 A
device allowing current flow in one direction after the7 k' ]% D5 K3 f: u$ \0 g
device has been pulsed at the gate.. L( E1 X! `' y
SINGLE SHOT MULTIVIBRATOR, An electrical circuit! a# d: F% u, g0 A. G+ @" B8 v4 ~$ c
-stable multivibrator.
2 _- {0 A9 `7 r' @如电流或电压能用于传送、通讯、控制或
5 O* Z: L9 @) ]. P5 C算需要的信息。
! j5 G% x5 z9 I* A; l9 A& M4 @硅控整流器,
1 I7 C4 J4 N$ k$ }当其控制极受到脉冲后,允许电流向单一方向流动的电! x, z4 K; Z$ ]/ X( D( o
子装置。% @- G! j, D4 `* [; L @- O
息多谐振荡器,
- R! ^# B5 a8 n! z& Z) }, L输人信号触发电路时产生的脉冲的电路。又称单
4 v/ \6 x- ^ a; L, N% u" XSIGNAL, An electrical quantity, such as a current or8 ]! p4 Y4 O! G: H" P7 P. X* [1 `
voltage' X/ c" G8 ]0 J; Z- B4 P
S
2 D& g( f! f6 n) I, o: Jwhich produces a pulse when triggered by an input
6 ?. D' P; W! Z' r6 @signal; a mono* C. @8 x7 s6 O& e" @& J* x
检查窗,
3 G2 w- p! k2 e, u9 {" S, S1 @用以观察机器的储液箱内液量的玻璃窗。( z$ D, n& g; h" \0 O' u
信号,
0 z. b1 \1 _2 i" |7 Q, W- G: X电量的一种。
z4 L4 Y- t( u) }# j+ v- X计
2 @1 e, f9 K" T8 ]冲
+ f+ [& d3 S+ I7 n6 Y+ f% U当一个
3 l& d, I- |* A% T+ {& V% l稳态多谐振荡器。
. F$ f7 ~- x4 R- z/ ~英汉对照民用航空词典B OEING
9 @: @2 D1 f% k2 F3 aTECHNICAL DICTIONARY 137
* M' q; C- p4 a9 H! G4 nSIMPLIFIED FLIGHT PLANNING, Rapid determination% N' h) _) g! }3 c
of trip time and fuel using a chart providing these data6 |% P! U5 ^' Y# g- p
for the entire flight profile from brake release to landing.
" N, i, Q) Z9 x# hSLANT RANGE, The line-of-sight distance between two9 X% J, n3 g8 ]' s8 t
points not at the same elevation. A3 q5 ~* O( \3 L
SLAT, A moveable part on the leading edge of the wing
) \& { O; d. B) _' K& K! p% i+ Zfor increasing lift at low airplane speeds.
: V# s0 o, Q0 J n1 S划,
# T* x& ^3 z' g, _; {! V% {迅速定出从松
9 a7 v( [9 a7 f/ G) A# f7 U7 d车到着陆的整个飞行所需的时间和燃油的过程。# ~0 T r3 D% ~5 q; d( b# K
斜距,# M) ~8 t, ], c' S
不在同一高度的两点之间的直线距离。
+ M3 j8 t. g8 m3 `& e' b( j, D缝翼,% q4 r) }1 o- b0 f6 S
用以在低速飞行时增加飞机升力的机翼前缘可动部件。: x; Z: g6 m8 L- M! k! n* E& H5 i
简化飞行计
2 L$ t$ M- r1 ^7 r5 r8 d由提供旅途时间和燃油等资料的图表,来& X7 H& k* O# q4 V' S) ^
刹
. H4 s) @+ m7 R英汉对照民用航空词典B OEING
$ ]( a; _7 S C0 j# g/ f# @% tTECHNICAL DICTIONARY 138/ L( w- D8 J4 h
SLOPE, The amount of incline a runway surface has
: q2 e, h) ^8 [- Z: n7 \6 Irelative to absolute level.' r6 p. X+ _( w' Y1 v/ k8 B7 |
SLUSH, Runway contamination made up of a mixture of
" D. r! X0 C4 ^ater, snow and ice.
# i( B2 l2 v% WSMALL COMPUTER SYSTEM INTERFACE, An input
0 U3 u0 i l$ F- J' P: X% x6 Eand output bus that provides a standard interface
' p! S% d+ v. k9 R( K9 jbetween a computer and peripheral devices.
# L, W _1 s5 _7 QSMOKE DETECTOR, A device whereby the flight crew
0 v( v2 G7 H" q/ @an be made aware of smoke or fire in specific areas of
5 Y m) p% |% P9 ~+ k/ v- zthe aircraft.
, G1 w$ d: y- RSNUBBER, A part of a hydraulic actuator that slows/ O4 A: |& }; V+ ]" v( Z7 j1 {4 f
piston speed by restricting flow.. c2 J `7 M b) `. a
OFTWARE, The stored instructions that control the
/ H' J" j5 w0 ~( ~perations of a computer.
. F, `$ k. x6 _7 o$ Z L" Sng* g6 j8 v! g2 c9 X
other devices.
/ y. {) K X3 H$ O d! z4 {SOLENOID CONTROLLED VALVE, A valve controlled$ G$ \6 a- c3 v- X% e- ~8 J
to open or close by the solenoid.
) u2 U4 Z2 e5 b" @+ o雪泥,* y2 _9 ?" d5 h0 ?
积在跑道上含有冰、雪、和水的混合污染物。- m" ]/ A. N0 a- K' D+ |; x
小型计算机系统接口,8 T# K5 q3 a; \7 z5 S
一个能在计算机与周围装置设施之间供给统一接口的5 R, K$ K3 _* U& l& K/ }- P
人和输出总线。 B' r( E+ ^* j9 i
烟雾探测器,( T( f+ Q& g ~
在机舱或任何指定区域内能测到烟雾或火并报知机组+ z0 Z2 Z* _; x1 B
员的装置。% Y. [& Z; v6 X3 C; @
冲器,$ S" T/ V0 ?1 r
液压作动筒中具有节流孔的部份。这些小孔能通过限制
0 _* h3 F; k5 \液油,以减低活塞速度。
& `" o4 N7 X" r9 t2 d; P储存在计算机的指令程序。用来控制计算机系统的工7 h1 F9 r! s. W! [# d
作。) g% R7 Q$ H6 N1 a
操纵其他设施的机电装置。6 p) q+ j7 U9 l; g& r
电磁活门,
+ C* i, j3 W5 E# ?. [1 z" k$ u8 T! P用电磁线圈来控制开关的活门
0 U6 R- x' \! `& q$ } j" w: Mw. Z9 y" A1 U% [5 J4 h
c
& C0 B, u( Z, y5 y7 Y( @S7 |: l* U% L7 F: R2 p& C
o' K% j* {5 F$ p: A1 ~
SOLENOID, An electro-mechanical device for operati
/ @' _1 K, ~8 b# g斜度, e4 k9 i7 S$ s- o. p. K+ y
跑道表面相对于平面的倾斜量。
4 ?$ p8 o. q. Y. u输( O- A7 j3 T7 j
人
) @* e d7 k( P- p; w缓1 w# T' ^+ ]% q2 L5 R l: ~
软件,
8 z9 j4 B8 g* D7 h- `电磁线圈,/ ?; p4 N# s, `% r7 q
用以
5 t+ S* x- c1 _! w4 j英汉对照民用航空词典B OEING) F: p3 |7 S" k8 \
TECHNICAL DICTIONARY 1392 N/ ?7 U, O3 N$ _) {+ q
SOLID STATE SWITCH, An electronic circuit that
6 }0 r- T) f& [# i* G4 S* Tprovides switching in a current path.9 Y" i- ?" I2 t8 [) [* v
SOUND SUPPRESSION LINER, A component in the
$ B3 W, \3 R! Rnose cowl and around the engine for absorbing engine+ N; {! L' i1 C' s( Z4 N- F# N
noise.
% V) |/ j+ v* m- u7 MSPAR, A principal spanwise beam in the structure of a
* B1 x! _0 F) W/ G; L0 I! PSPEED INTERVENTION, Pilot control of the speed& u+ U5 r0 L2 k& N
SPEED SCHEDULE, The planned speeds for a specific& O+ ~6 f" S! j- c9 M9 G- r
phase of flight.
S" \- ]0 [/ r" C. {6 x晶体电门),2 y) Y A8 [) l- T
消音衬,$ H6 f/ Z+ \" |3 m5 d
在发动机的周围及前整流罩内,用来吸收发动机噪音的
, a G6 q" Z, x( o M部件。8 i* Q% B) P! Q! i& c: B
梁,
3 e+ y# f% \7 H机翼、安定面或操纵面结构中的沿翼展方向的主梁。* S+ p6 ]! t' T3 g
速度干预,
8 ?3 }0 G: D. A# B9 U8 v. b计划速度,- c5 Q1 O! X; J/ w9 ^5 d
为一特定飞行阶段所定的各个速度。
. n; a; ?, ]+ Y% k" B. Qwing, stabilizer or control surface.
( S. A, p4 r1 t- j: B7 I. }$ Gduring VNAV operation.
% p- b& p# g* C4 g3 w. V固态电门(0 J2 N0 D; W+ ^
在电流流经途中提供开关的电路。; F, P- L" c; V6 I: Z# B/ v1 l
在VNAV(垂直导航)操作期间,飞行员控制速度。2 ]0 {9 I) ]" p0 }7 F
英汉对照民用航空词典B OEING
7 H( I' T4 B# }TECHNICAL DICTIONARY 140, [; C# b3 x4 d
SPIN BRAKE, A device in the nosewheel well for
Y' @6 D/ t( O Z% Kstopping the wheel rotation after retraction.
; x h4 b- Q5 v# q: B6 BSPINNER, An aerodynamic fairing attached to the fan of/ _. g: \7 z) q7 Z; @4 v. t& L6 Z
a turbofan engine.
% a' {- w3 p# ]7 ISPLICE (NO. 1), A connection of two airplane skin
) y0 N7 M- s6 A% p# lsections.4 ^# H6 v0 O4 m1 I
SPLICE (NO. 2), An electrical connection between two P, J9 g) x: |+ S# F
wires.
Y) X5 ]; [; f3 b9 R# A4 [前轮舱内用在起落架收起后不让前轮再转动的装置。4 Y$ F1 @) E$ p( Q3 W( \
旋转罩,
+ H, J' f3 |; @8 R' B, u* Z固定在涡轮风扇发动机的风扇上的气动整流罩。+ D: z8 Z* c/ ^
拼接,
% u9 o1 i4 Z4 L7 J飞机蒙皮与蒙皮之间的连接。- R- P! W' ~6 G5 _3 f& S' R
铰接,1 x) y2 A7 w* }) J
两根电线之间的电接头。
% p" Q, l4 @# D5 Q P停转制动器,+ f" c& ^, }. G; p5 \: `! A. [
英汉对照民用航空词典B OEING
: Q* [) A' m- W$ a8 H: Q; R: m% STECHNICAL DICTIONARY 141* ^+ T3 I% A# m/ W1 G5 a- Y2 n4 R9 @2 J
SPOILER, A hinged moveable panel on top of the wing.3 f9 ?. ^. A3 M( T
Flight spoiler- assists ailerons for airplane roll2 I7 w5 v! h0 ], \7 t
(wing up and wing down) control
) I6 Y( I6 W8 h: Y2 }3 Pand for aerodynamic braking in
, N/ i( q: e* U/ bGround spoiler-for aerodynamic braking on the
3 y8 S# B$ q. d* _ground only.! [, l2 t I" k, H$ I) J* ?, y0 L
PRING LOADED, A condition in which one part of a
8 w% b- o0 ]3 G3 u3 Q$ y. j+ `) ?evice is held in a particular relationship with another4 [+ I. m$ P: C
t,
' E1 D; h" Q, h7 l! K5 ^* W$ dr original position.
* @. L$ W0 n5 q+ n" U) R, \SQUAT, Airplane on ground condition.* T- {5 T& L6 G
QUAT SENSOR, SEE - AIR/GROUND SENSOR( M9 a7 V ^+ d& K# f6 l
SQUAT SWITCH, SEE - AIR/GROUND SENSOR$ }- N# W2 y# w* ^- U# _5 [. n
扰流板,2 Y) d) C' G5 i# L9 b9 {& F% ~
铰连在机翼表面上的可动翼板。% T* H7 x; [3 Q: f$ {
飞行扰流板一功用有二。一、协助副翼来操纵飞机
! U4 }! J @; u0 f8 ~% r的滚转。二、用以在飞行中或地面滑
' _( Q8 F9 H2 ~+ T4 W% }6 g, P跑时作为减速器。: P/ F( v# I8 P* t1 G, q/ J
地面扰流板一仅在地面时作为减速器。
+ |, ^2 H+ X6 }% Q簧加载的,8 f# o$ K; ^ g. L5 E8 I' A
由弹簧使一个装置的两个部份保持特殊关系的一种状
7 Z/ p5 \* K( d态。该状态允许一定运动,但继而回复原位。* C6 D* d5 Z- l) p' `; N
着陆传感器,* {7 V# z1 D5 V: l3 R+ x
und Sensor4 _$ q1 z. O. r! U8 K0 G
flight or on the ground.
: C3 E; a9 U# Z; }+ _8 uS
$ R7 p( o8 B: N/ o$ [d2 w# r1 \& f7 o
part by means of a spring. This allows some movemen
$ B9 E. @. ?) u9 d+ h" {; d; Y" Gbut returns the parts to thei
% Z- ]3 R7 Y5 p$ Y" VS
' g7 D$ b2 T1 f1 D/ d弹
+ @. o& q! @! u. b着陆,
$ B1 V4 C; I6 p1 J+ G飞机在地面的状态。! O8 ^0 y! A Z, Q4 C, n
见Air/Gro( ]; r) W7 ~6 [- u8 n
着陆电门,
* V d" L( S& ^8 y7 O6 b/ d见Air/Ground Sensor .
5 Q. t7 w) K+ g- u, Z英汉对照民用航空词典B OEING
7 o/ p6 l3 s2 I fTECHNICAL DICTIONARY 142; \& D+ Y+ ~9 ~$ a
SQUAWK (MODE,CODE, FUNCTION), Activate+ N5 N4 q% {* F. G; z
specific modes/codes/functions on the aircraft
* O2 D9 S' y- }ansponder, e.g.,” Squawk Three/Alpha, Two one zero
6 B4 O3 t# B! O. Zfive, Low".* Q# Y+ W: ]1 e" e" c9 o
SQUIB, An electrically operated pyrotechnic device for1 V5 Q+ Z& v# U6 s S
breaking a disc in the fire extinguisher bottle to release
6 V$ n: h/ I9 }5 v- ~- hthe extinguishing fluid. Also used for escape slide
6 P4 _' H3 H1 [" R: V) J. v) l0 wTABILIZER, SEE - HORIZONTAL AND VERTICAL
8 j' L ^' `9 r, rSTABILIZER+ w; k5 F% Q6 }; W/ q, V$ W
TABILIZER TRIM, Movement of the horizontal tail to
$ O8 K" r1 S/ F7 R& khange the attitude of the airplane about the pitch axis.: M& I2 n; F' `9 T, q
TAGE, A numbering system for the compressor and# _5 H K- }3 `9 F3 D' t$ P
turbine of a jet engine., S: f. j- m+ ^" Z" n/ ^
TALL, A flight condition during which lift is destroyed2 u4 }4 y- @/ _% M
ue to slow airplane speed or attitude.9 @& u8 @ f. \" u0 F" l
to enter from the top and flow7 T/ g: p+ l6 ]' i
out to the system. It prevents picking up debris off the* N+ v$ s; E9 {$ _6 z
bottom of the reservoir. It can also control fluid height in
$ m* ~3 j$ E/ l: k; o& X. Hthe reservoir.
; P8 D E P- o ?! k# G! ~能),
0 h8 f6 l' l; t3 m" Q使用飞机应答机时的一种常用的指定方式/代码/功
6 a, H. O9 N" D, j能。
7 Y2 t3 X# n0 Y/ W3 Y. l6 _; y管,' n/ V9 r: `: e' Q, A9 `: Y
用以爆破灭火瓶上的圆片,以释放灭火剂的电控烟火装
, p" `4 u9 E( t, N- R# A6 T置。也用于应急滑梯放出。9 d' `4 x+ N4 y) ]' P2 X6 J" s! i n
定面,4 Y$ B2 P9 E" I* J' t% z- l
见Horizontal and Vertical Stabilizer
- k9 p6 d1 \5 I u3 v' Ntr
9 U$ Q7 W7 _! _0 u; m7 ?deployment.
: y( Z7 `# m% g4 R, Z4 E7 u& zS
0 x6 W! b' j, h' E$ zS0 m) k7 m" h' V, I7 I+ Q
c
! `1 `( U$ ]- Y' l m) ~4 D0 SS( J' |7 Z9 V! X% a% ^( j+ k" Q- }
S/ e% w4 s' ]* e0 E# T8 Y7 M
d/ S: M" [; k; ]
STAND PIPE, A pipe raised up from the bottom of a
& G! R) w0 g8 F/ F) X, R! w `# \* ]reservoir that allows fluid
1 n; N- \2 y! A" @( e9 j发送信号(方式,代码,功; ~: j# n" z$ D7 Y7 M
爆
7 z9 o, x+ }" o4 C安# M1 c G& k. m3 a9 i! r |
.
% n' \% w' A5 K' x+ D0 {: Q- l定面配平,4 O: W* m0 a- m5 w8 C x" }6 I3 U# M
为改变飞机绕俯仰轴的姿态而做的水平安定面的调整。
; T; u8 W$ Z/ S1 ^, ]3 ~ z级,
& u3 ]# ^7 J) |. 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 M' ?; Q1 y; ^+ S种编号系统。
: @+ O& ^0 D `8 I- |5 U' x. K( q失速,7 Z. d' z) C' u5 h1 g/ Z9 ^3 c$ F
飞行速度过低或姿态而引起升力失去的飞行状态。0 x( m: z [1 Q8 |5 q% M) L
回到系统中,并防止带起容器底部的碎屑。也可控制容
- t/ a$ Z5 e, [7 x A; P; Z1 p器内液面的高度。+ ] `( H. }# c6 s* W, X
安
- Z! q/ m1 Q% ~9 d) B9 ~立式管,0 Z8 H/ T2 c' X$ |
从容器底部立起的管道。能使液体从上流流人,然后外: b# b2 j2 |/ q2 t2 {6 H/ H
流4 B6 Y3 e) \. J! y& I' C* n
英汉对照民用航空词典B OEING3 _, C+ ^* h8 d
TECHNICAL DICTIONARY 143
, l. P z) T* T0 s1 K' RSTANDARD INSTRUMENT DEPARTURE (SID), A
5 X% b( u$ k' i7 AIFR.& h* J, H- m+ L3 I. W: P- j* E
TANDARD TERMINAL ARRIVAL ROUTE (STAR), A
) V! F$ |9 {: L1 B- e6 @. z Iublished procedure for approaching an airport IFR.9 \+ d8 M. v, K$ T# l J
TAR, SEE - STANDARD TERMINAL ARRIVAL2 N ]& p' P: b, e
OUTE& C& L6 [) i9 W' x
TART VALVE, A valve in the engine start system for2 V s8 ]- q$ v- d' B1 H$ ~
upplying air from the pneumatic manifold to the engine
6 G/ c2 ]! w- }tarter.
4 P0 _1 Q0 G2 z3 t+ H CTATIC AIR TEMPERATURE (SAT or OAT), Ambient: k7 B! U$ F$ b( L7 |/ m
or outside air temperature.
) t \- v/ \, ]STATIC PORT, A small hole in the fuselage for sensing, Y" C, r6 i3 A
static pressure for airplane instruments.
/ L2 n9 k7 G, \) ?) v& zSTATIC PRESSURE, Pressure in the air or fluid at rest
& _ n8 _% c# m) u. p* ^! }4 b* jmeasured in pounds per square inch.
0 v" R& ~( k: W- [% B3 U' mID),+ f+ m; {* H# Y
用于使用仪表飞行规则离场公布的程序。9 S+ z9 V7 |. y w2 m, S" E
标准到场航线(STAR),
+ ^) H" a% S8 [3 W' N: ~用于使用仪表飞行规则到场的公布程序。
& u" i; f# K5 ?% W: K/ r+ A+ I5 {标准到场航线,9 k& I5 u9 x% X& N: P
见Standard Terminal Arrival Route
N$ u) b6 m/ _9 H' z kpublished procedure for departing an airport! ^. D" H& y z( e9 G* o0 n- p/ }
S
4 R9 \! K9 a; d- d9 \# o2 |" x- P$ @* yp9 U( o1 x& q" W6 D f6 |: g
S4 P0 z. H* _ V! v3 O2 ^$ T
R
; k. j2 G1 U! u7 ~( h4 CS
! `& v; b ]8 Ss6 x9 l# @' G+ b* W: u1 j
s* X l( ]7 w( B) a% V1 _, j! v# \
S
: N5 a6 L. E! q+ U I标准仪表离场(S3 K& g- w7 p; V2 P0 D1 a
.! Y, Q5 x/ Q# D; N0 a% X) {
起动活门,7 [* Z, `& X8 J
发动机起动系统中,用以从气源总管向发动机起动器供
. A. E) z; j8 l& _" N& q, l, V的活门。
. k, |0 o6 W: o- x+ n. O5 z温(SAT or OAT),% Z8 B4 |: o8 G+ a3 t
环境空气或外界空气的温度。
" h( [. O4 P- ~% a; r! d) [ U% V8 \压口,
. V- f9 R; a5 z: m* o* t位于机身外表,用来为飞机仪表感应静压的小孔。- b U5 I" B! a; w
静压, q) q9 [( B/ p8 p: t6 p
静止状态的空气或液体的压力。用磅/平方英寸来度量。
" D5 G; S+ j/ |/ n9 [9 a气2 _" K( b( Y8 C9 h) J: l8 Y" C
静
) s3 t" s/ B5 e5 A6 Y I' A& Q静3 Y" Y u6 x6 r1 \/ w
英汉对照民用航空词典B OEING
) E7 f# }7 S. n* V" kTECHNICAL DICTIONARY 144+ {" w# u" _8 I0 ~
STATION, A vertical reference plane along the fuselage
2 y; M0 E1 l3 o# k+ Lfor measurements along the fuselage.
* l4 N& C: a2 F: Z+ nTATOR, The stationary section of the compressor9 B b9 S7 y0 C5 g) P
etween the compressor stages in the jet engine.
. r8 H5 ]2 E; Z3 \* `TEERING ACTUATOR, A hydraulic actuator on the3 d5 l; Q) X1 Z6 Q
landing gear shock strut for steering (moving) the4 J4 D- A0 s5 U" a; [5 D& T4 r
nosewheel left or right.
& t" x) D4 c s$ b; b' P6 fTEERING TILLER, A hand-operated lever in the! z3 m' K* U2 R* ^8 \
osewheel left or
( m- C3 t1 p& j* F4 a5 I. Eght. P9 x& g) Q( t
TICK NUDGER, A device to push the control column
- F- P& t. o) j9 grward just before a stall occurs.* u. f0 H$ u+ U, o! y/ N" z
站位,
9 f) U9 _- W8 S6 Y% l* ?: B用以沿机身方向度量的垂直基准平面。
/ P& r8 b9 s+ e定子,8 U9 W. _$ x3 r( X) i5 ~
喷气发动机压气机各级之间的不转动的部份。
2 I* ]2 ~0 O' w5 B弯作动筒,
3 Z. \% }$ F5 D6 u9 X1 s减震支柱上,用以使前轮左右转弯的液压) e# l" e: @6 e* C8 v( f
作动简。
+ i5 S7 V$ U3 H7 T* o- i; X; K d轮转弯手柄,
" r$ w2 r/ r. ] a! R; j内用来使前轮左右转弯的手柄。
Q. d4 s( N3 P# I动推杆器,( \ }! }4 l! I( F3 _
在失速前能将驾驶杆向前推的装置。+ ]5 b' H1 g+ O
S1 ] t5 `5 N. e A' k
b& }+ d! b$ t/ T% W3 T- [, Q
S
6 l% j5 r+ D* f9 b2 Y GS
7 u. u0 }; [4 Acontrol cabin for steering (moving) the n
$ N T/ s5 e- D( H3 rri
7 W, G5 e* a. Z# @. OS
$ D: v: W: p3 {3 {' f# l5 h+ K7 yfo
. H$ ]6 {1 s" K' k转; Z( Q' i, x7 @' z$ n
一个在起落架: [; g/ ^' f* W# l
前& o! k. Q" Y ]1 k/ a
驾驶舱( B; u/ o5 J, O9 b/ u9 ?& A) I
自6 l! |, P0 {. [* {
英汉对照民用航空词典B OEING
4 B7 m( c0 Q1 @( hTECHNICAL DICTIONARY 145+ n! i2 ~. C; n& e
STICK SHAKER, An electric motor operated devic- B" T) D. A9 _8 l) K
the control column which shakes the column be8 ?8 O/ @/ L, p! N1 k. O
stall occurs.8 c1 A: t( V0 k7 q* n! N/ b
e on
4 n, {1 r% l( `8 }" z$ i+ ~fore the
* w8 G, o6 @! h# h3 `# J/ uTOPWAY, An extension beyond the end of the runway
4 [, k9 d# o0 Khich may be used to decelerate the airplane in case of- h6 z# T- F# V" Z% N% w
n aborted takeoff. It cannot be less than runway width
g% w `: j4 F5 @( land must be strong enough to support the airplane
9 S) z' d% F1 R( t# i置。% G( w* }+ e" ]( V1 z4 D/ s) Z
速安全道,
2 t# e4 M1 H! {7 s5 d跑道两端,可用作在中断起飞时飞机减速的延伸地带。) Z: m3 C! L6 [" j
它的宽度不能窄于跑道,硬度也必须能够支持飞机以免结
& n0 |" r6 {2 T \0 Q' QS
( y) f! r6 m# r# V0 {* ~3 m: h" [w! n5 `& W J+ e( ?
a
}2 Q+ a2 v/ h5 j, j" T( Xwithout structural damage.
! u- q8 v8 C+ @5 K& eSTRAIN, Structural material deformed slightly due to the
% i5 [3 U- ]/ _6 M( @9 Baction and forces of stress.4 d; {3 O0 M/ y( X% E6 U
振杆器,1 |6 \. ~9 T' l; p) `* Q6 W' `
驾驶杆上,在飞机失速前使驾驶杆振动的由电马达操. F3 C7 n( G |
作的装" I! R# x. q0 p# {* z
减3 E. m' D" [) }$ W
构损坏。
9 O, D, s; b5 M! l% f% A/ M/ ]7 L5 d应变,
7 D) d% e+ @2 D0 \ L因应力作用和受力而轻微变形的结构材料。
' M0 P, @9 l# c- R, ?& T" Z9 P s6 Q英汉对照民用航空词典B OEING) J: m& o" y* z9 |7 B) I# j
TECHNICAL DICTIONARY 146, G4 Y Z( P$ G* w3 L+ @7 s1 v
STRINGER, Structural components in the fuselage or
% m/ m% Z& r/ c! e# C. {wing for transmitting skin loads to frames or wing ribs.% q' N! S6 t. R! d# h( \( M
STROBE LIGHT, A high intensity flashing light on the4 `( Z% T, A. O9 R9 l/ y, L
wing tips and empennage.
" P3 }+ M9 K1 d' S# gSTRUCTURAL MEMBER, The part of an aircraft
4 K: B. \) D$ A7 j. Ustructure that has been designed and constructed to
; j3 G# R! C" n: wcarry and accept loads and stress.
1 J; a8 U" A! j# WSTRUT, Mechanical components of the landing gear for
- y! A. p; h2 p& d+ I0 Ykeeping the gear in the extended position.
! b- K( @! P) v1 H机身或机翼中,用以将蒙皮载荷传至到隔框或翼肋的结
, n; Q1 Q" T+ e6 o6 O6 l9 q% O构件。
3 } W+ _6 L L频闪灯光,. k) Q4 ]! ^# T2 \& Z
位于翼梢和机尾的高强度的闪光灯。
/ W7 y& |4 i* B0 e* I, W9 h件,7 Z$ {7 [" R k/ I7 |
飞机结构的一部份。为运送和承受负载及应力而设计建
. ]+ {8 f4 c" D成。
# x# s+ Q$ U5 Y5 K, ~支柱,
0 |. w: c5 r. v6 h) G起落架上用以使起落架保持在伸出位置的机械式部件。! z- y! D# F8 M- o! G" @1 M
长桁,
5 S- d! }6 l3 K; l/ R- A构
4 g5 `& F( {6 C6 I( M/ `造6 g- Q d3 I( V# ?. H5 m* L% b
英汉对照民用航空词典B OEING
: ]# T+ ^5 t' L4 q& t+ U0 X+ a9 cTECHNICAL DICTIONARY 147
3 u3 U$ F: {# A4 z6 WSUMMATION UNIT, An electronic component for
2 o8 G8 V/ W* v* W- j' Cadding fuel quantities in all tanks sending a signal to the
/ j3 H* o9 k9 \7 i1 v0 @, K Ytal fuel quantity display.. b b' M. A- e. A T
UMP, A lowest point in the engine oil system or fuel0 \1 `: |6 I2 ?8 {4 w
nk.- O7 W9 M$ W* y; v' j; t/ M
UPPLEMENTAL DATA, Additional data stored in the
4 z1 W" t5 w7 ?' r, i# ~* ]MC memory, supplementing the loaded navigation+ e2 k# F# j$ ^* A$ |
ata base.
9 o: I# {3 [2 P# ]1 ln
1 L& d* Q- A9 Z# I7 }4 veviating from normal modes.
/ `$ P# b) g5 Z+ X' F- FSURGE, A sudden change in the airflow through the$ U( q& C- E2 ?# x
the compressor not being able) r4 Q: M8 c) b( n
compress the airflow.* D6 @3 w7 S( W2 @+ `
SWAGE, To squeeze together two or more items to
/ r; {; K* c: s2 Fform a permanent unit. Example: a lead or steel piece) f$ h; m8 K4 t$ Z
on a cable which forms a stop or camlike unit. Also to- n6 U) M9 C( s6 ?% G; ]0 |
reduce the diameter of tubing., i8 z5 s# ?4 b7 b4 {
SWITCH, A device which changes the condition of an
: Q& J8 i D+ L( h0 d4 D" welectrical system from on/off or open/close.& T7 n6 Y( Y `0 N+ u q# B
燃油总和器,
) X$ V+ e3 A& T" `' z$ \+ Q1 L& x将所有燃油箱内的燃油量相加,并将总油量用信号传至
I% `) _' l3 t" W' i量显示器的电子部件。3 h4 `2 t K- }4 R$ _" x, L
集油槽,
) L$ i5 [2 U$ J发动机滑油系统内,或燃油箱内的最低点。
+ v4 z. M# M' m6 P1 {+ M. P增补数据,
8 H# q5 k# k @飞行管理计算机存储器中的附加数据。用于补充导航数' r, H' b/ a p8 H+ o
据库。6 ?* R% o: T* D( c2 Q: C2 ]1 o5 k
,. ~9 e7 p5 _9 S6 Q2 z7 |
附加的数字飞行控制系统方式,当偏离正常方式时使$ [6 m4 W" F( q" K }+ u+ n+ z$ h
。
2 u% ~+ P- k* t! E, F# L8 B8 m过发动机的压气机的气流的突然改变,而导致6 H# x/ f1 U7 P3 x- L# `" l! |
气机不能压缩空气的现象。
- x, `8 \0 g) e% D4 v陷型模,$ l+ P: D" I5 @9 C9 g
挤压两件或两件以上的物体来制造一件永久性的元件。; d2 |) S/ r7 b P
如:一块铅或钢在钢索上形成一个止动器或凸轮之类的4 Q% ~, n ^+ v. r* N
件。也可作减小管道的直径之用。1 a+ I5 W: m+ [" x5 w2 V
开关;$ s1 K% c5 N+ b4 ]1 Z. ]$ ?! ^' q7 P
改变电气系统通/断或开/关的装置。
% s' L4 a5 k) k9 b7 ito3 j0 r3 M v4 O# K! |
S
" m3 @* E' H3 n' q# [ta
3 w9 E0 F; O: Y8 {6 Z; dS
# s5 \. M& @$ r0 f4 r. jF% h5 z- s& K- r6 v: G6 {& g6 @( f- ^
d
3 x& o) s4 a1 f- [, B5 vSUPPLEMENTARY MODES, Additional digital flight1 S! y4 q' j9 L, m+ v% d( I
control system modes that are available, used whe
, K0 u7 B2 ?: T4 ]0 m% Dd4 p3 o: w- T! y6 {
compressor resulting in
6 x1 i3 l) v9 t/ L) J4 H5 J; Cto1 ^9 H; |& H( o; C' B$ p
油
( s% z) P! u. o: P( Y" Z辅助方式/ s) q) l1 N% f6 y" ~' y1 x( f) n
用' S, a& y& J u) n: G; z, @, }
喘振,: h: g0 Y$ H; ~! g* s$ T4 o4 O5 U# g
由于通, S* D/ m. Y1 j3 T/ Q j
压
! d# ]8 f4 ^7 k; ^; F" z例
, F; I7 [' f$ [* L( N元2 w# r' F1 v6 D6 _" c
英汉对照民用航空词典B OEING* r1 N) L: K9 y4 x h' }- Q
TECHNICAL DICTIONARY 148 o6 I, M& I' F( b; t7 p
SWIVEL, A device for rotation of components.& n# S+ H; k) [6 j
SWIVEL COUPLING, A junction in hydraulic/ o" c T0 I' D/ M) |6 o- N o1 H
bes for allowing component movement.
7 S9 K$ [- |( W( _$ h) CYMBOL, A graphic view of an aircraft component in a
- B4 O/ Y2 [$ H- _ery simplified format. Used on drawings to represent
7 r$ s" g* } c4 ne entire component.
. r4 Z1 D- v' x7 v3 g vSYMBOL GENERATOR, Generates the video signals5 F: I( f; }$ Y! `# k
that are displayed on the EADI and the EHSI.
6 V3 @2 i8 N4 X1 r. h+ x% ZSYNCHRONIZER, A device or circuit to make the units
% N% _) F1 C9 n5 f, S6 Q1 \" Fperate in unison.
) \& ~. k" g& W" \SYNCHRONOUS, Refers to two or more things which
' a7 g% A0 c$ L! ~* z4 a( N1 f7 khappen in a system at the same time.
3 R9 g& a' t. Z% V0 p6 E' ?用以使部件旋转的装置。6 H& g. Q' k3 F
转动接头,2 x% V5 a6 e2 Z0 N W B
液压管线上,使相邻的液压管能够动的接头。
6 [6 }1 h T: U9 l q符号,& Y! u+ F2 R* k7 n! O
飞机部件的简单示意图。用于绘图以代表部件的整个结
$ U0 u7 y3 C( I1 s) w \构。) J# G* K3 M6 |* k1 X6 X
符号发生器,2 S4 O5 D) p' l4 q5 n
为姿态指引仪和航道罗盘产生图象信号的装置。
1 n! B1 D( k4 I7 f" M K同步器,; ?* Q u6 _4 y9 }; I& U# E1 |
使元件操作协调一致的装置或电路。
' {& \9 `# a0 Z( _. H4 y) F两个以上的东西同时在一个系统中发生。
, f& J9 [0 p2 Ktu% V# \0 F& c e6 V
S' F @0 C2 S7 r
v
7 S* b) c& t7 Q* Z6 y$ K: Nth) F( B, ~( i, P6 b
o
( t9 ~: p" L+ t) V转座,
* v: ^6 F- H' C# a" @同步,9 o: Q/ m1 @ k' @& Z. Y
指两个或
! d, ]' ~, B3 m英汉对照民用航空词典B OEING
- i3 P* a4 a2 h" h2 OTECHNICAL DICTIONARY 149
0 t" i) \; N" J: k- b4 OT% v2 s, w" w. `% H$ `. R
AB, A small, hinged, moveable part on the trailing' W! @2 Y* ]! S
dge of a control surface (aileron, elevator, rudder).* K2 E* x8 ^! n+ j- z7 l/ V
Balance or control tab - moves in an opposite5 f# a7 P9 b! ]- y" O1 o
direction to the control surface for assisting) e: }. q- @5 \
in movement of the control surface.
& u5 m( U$ X6 } @0 wTrim tab - provides controlled deflection of ailerons3 T) u; k0 C" f3 k* R5 v
or rudder to compensate for imbalance in
6 m+ S: X* g9 N( r4 f8 b5 Zthrust or fuel quantity.
6 \; m/ U1 N6 l( J* S! DStabilizer trim - controlled deflection of the horizontal. T5 z: G3 e6 B# a+ |/ g7 ~: K* u, p
cy1 v: s% {- G. v9 m; e3 u
proportional to the speed of rotation.2 q0 p1 a) [% P) C
TAI, SEE -THERMAL ANTI-ICING
# {1 @( d8 O9 m( nTAIL PIPE, Duct at the back of the engine exhaust.
, C6 Y% Q' y. D3 e; m3 XTAIL WIND, The wind component relative to the
8 z9 l' M ^# l; L9 t/ lairplane direction and coming from behind the airplane.( C% r7 V3 `8 o H' P
调整片,
7 Z. R2 X' s- R% f- \铰接在操纵面(副翼、升降舵、方向舵)后缘的可动小
$ E6 l' K$ Z- z, w2 Z# s部件。7 C& z$ x, G) ?% l6 _' l
平衡或操纵调整片—与操纵面运动方向相反,用以帮7 q$ J0 s8 Q' I$ J' w7 P: Z
助操纵面运动。
8 p- ], O) o" R9 A+ {. C: K配平调整片—使副翼或方向舵作控制之下的偏转,以- r# a6 J% x2 X
补偿推力,或燃油量的不平衡。
" w) s$ S+ }$ L" t* B9 I; s* q2 _安定面配平—使水平安定面作控制之下的偏转,以减
3 ~$ Q1 n/ r% M& ^5 @少操纵力。
' G( o F( u0 ?) `机,$ X% [6 H6 P7 z4 F# |
提供频率与转速成比例的电流的小发电机。
1 T- A) e0 N" U- y2 S0 W" T热防冰,
, D3 Q" ~9 D* k+ W, K4 S见Thermal Anti-Icing \5 ?( w6 h. P# D' k4 _* V1 F# D
T b1 w% B$ a- x: L
e
! z$ v7 }% x4 ]4 _, _# h% q' Bstabilizer to reduce control force.
& F! n$ L9 f& @! Y3 qTACHOMETER GENERATOR, A small electric
9 w% x7 ^) C' Igenerator for supplying current at a frequen! K# G+ p9 r; h! h+ b4 B9 Q
测速发电3 w& i5 p* `7 [
.9 P3 R, o/ v! P- V2 R- }
尾管," j* r# v3 _6 {$ ^( A
发动机排气管后部,用以排出发动机的废气的管道。0 S' j$ d/ f1 D" g0 l4 Z
顺风,* ~! s0 I. s/ p( \5 R
飞机后方的来风在飞行方向上的分量。! d9 e$ ]$ C: T
英汉对照民用航空词典B OEING: S, b6 i* Z9 }* e6 D; x
TECHNICAL DICTIONARY 1504 M' F! ?' [5 p
TAKEOFF ANALYSIS, Analysis that evaluates the' T; k( i& f# C: m) C0 }, S
airplane takeoff performance capability for a variety of% b: O1 o# s/ e0 i0 U/ |& G- g8 H
environmental factors at a given runway and airport.
5 P# X% X! ~# F% r0 a2 s; xET PARAMETER, A specific goal such as
L$ j2 J) [- N: D- j% firspeed, thrust, engine speed, altitude, temperature, or
" q0 n: X1 F3 N k, O. E6 Kte of climb which is to be achieved.
9 o% f& L, B3 |" Q4 sASK TICKET, A computer label used for tracking the' h( h% l' Q/ N- C' _1 o
ompletion of a task.
% i- }" ]. |" t9 b2 K2 ~RATURE0 l" A, X3 ~9 y( P+ J1 }+ T0 s- `
AXI FUEL, Fuel burned from the time the engines are
+ w8 ]# r. r' u$ Kr.5 q, q+ j5 E' h3 |) G- j1 I
CAS, SEE -TRAFFIC ALERT AND COLLISION, J; _' W1 a5 J( v; h& P
VOIDANCE SYSTEM4 E2 H l4 M* }6 Y
欲达到的特定目标,如空速、推力、发动机转速、高度、0 W! m% V- B% a
度或爬升率等。: \% B9 O8 C" ~
工作记录单,
0 j% R* d% Y1 p" R用于追踪工作完成情况的电脑记录单。
1 W0 {9 `* Q" b* A1 P) `全温,
0 N# L6 z! K, B Y2 F见Total Air Temperature
% N( ^+ P m5 @+ cTARG4 e, q6 O0 ?5 h7 f$ Z
a
/ P; t, b1 ~* ~+ qra4 a" n6 W! s8 ?- B) p$ I2 s9 J
T
( c4 h7 D- M$ w9 h; Z' a, Hc
" F! R" [8 h6 P1 W5 |TAT, SEE - TOTAL AIR TEMPE
. q5 p' {- B' Y- @TAXI, Movement of airplane on the ground using
9 F9 I, E& A* _, F* o( Rairplane engine power.
3 `* A# G' K5 m* n2 ?1 g0 zT, P+ n) D+ P8 J, L# Y* H
started until the airplane begins the takeoff maneuve
9 b9 H) P7 E8 s# j0 C% sT
# w( g" ?, o1 d6 z; \- [- z+ hA" g2 Z8 |8 i/ o$ r0 C r% q
起飞分析,5 i+ a$ `. P; U: A& W+ j
对飞机在一个给定的机场和跑道,在各种环境状况下的
, m$ ]7 L1 l4 N3 [7 b+ h起飞性能能力的评估。5 J: M1 `/ v( U& o" J6 o
目标参数,* T/ E4 }' S* i' i
温2 b( B& t' X* I+ h$ G- Q+ h
·7 x. @, x) v- c' ~+ C
滑行,8 H- I: L% H9 I0 }
行燃油,
+ N+ y6 ^. a \+ O$ M0 g起动,到飞机开始作起飞动作之间,所消耗的
" }, `( m8 P8 u3 O中交通警告与防撞系统,
! A3 E' t: ]9 a; P) T* a3 ^0 F" C见Traffic Alert and Collision Avoidance System
0 S; `/ i; h4 P( [飞机凭借发动机推力在地面的运动。3 @# e- |$ l+ k9 `; O
滑' w* h* G5 n7 \, Z; G2 [
从发动机
7 m8 q: D- a% V2 V# C2 s# i8 q" y( R8 }1 r燃油。
! e/ V. w2 P: e空5 A0 {9 ` a9 E/ e2 S+ z* q
.) u/ W8 R: ?5 Y/ M% }: k
英汉对照民用航空词典B OEING/ U9 V( `; U, {0 O$ ?( s
TECHNICAL DICTIONARY 1516 g& [3 p, U% _; D
TCC, SEE - TURBINE CASE COOLING/ s1 K, w$ |& [0 L; j' L. y
EE, A pipe or tube connector manufactured in the
' m) d4 Q; B% f6 z( a8 I5 {EFLON, A synthetic material for hydraulic and0 V0 d& w( |! }# f) k
neumatic seals.
! D+ b/ ?# Q! a4 \1 v3 yEMPERATURE INDICATION STRIP, Temperature1 S h% ~" V6 _8 C# ^% a
ensitive tape which changes color at high temperature1 E6 I' w6 _* o6 ?9 S
r indicating component exposure to high% J3 W. B3 v5 w* d9 ]- W6 i
TEMPERATURE INVERSION, An atmospheric
' {% X/ L4 D( S. `: dcondition which causes the outside temperature to
6 |7 [4 t' m% H9 h; r: T6 ?" bincrease as the airplane altitude increases.- k; `. ^- q9 p. Z& r! X9 k) O# U
TENSIOMETER, An instrument used to measure the) X1 X+ p) K* |3 f
tension applied to aircraft control cables.
+ j3 \1 k' k" [- z- C" ^冷却,
) U/ e5 b$ }' R$ U8 I; Q; P6 oT
/ w) L: J+ p" ]) i% h1 z; a. A1 `shape of a T
6 o* C4 Q* t1 }6 CT8 ?0 L! S6 [: i" A$ ]2 b, b/ T" b
p
& p5 t2 | O1 ET
8 x2 e1 L. O5 I- Ts4 J( s0 J" V+ i4 L
fo
8 i4 h, x. P4 h& P: H. k) Vtemperatures.
& o) `: w `$ D7 y涡轮机匣
; {+ A! \: G5 j6 W/ j& f见Turbine Case Cooling.
& i/ i) l/ x. c& Z) F字接头,
& g3 j9 x& Y a' \的管道连接器。
' n/ e& a1 G9 P氟隆,
0 f7 D# Q3 N* B: U7 I; l# h% B用于制造液压和气源封严的一种人工合成材料。
' {2 w: [; t3 N4 e0 y# m度指示带, B, i, i, a1 s* b+ ~/ l/ I; R
遇高温变色,以指示部件周围高温的热敏带。
3 ^- r. w" E. K* L" X逆温,
: R4 T/ S8 ]* F8 _( {# s, F* o* ^ ^一种大气状态,引起外界温度随飞机高度增加而增加。
/ ~* I6 p) K# v5 N ?) L7 u张力计;
9 P2 k4 S7 a) f用于测量飞机操纵钢索上受到的张力的一种仪表。$ R" j; x5 O( _) _6 i+ v' k
T) a; O9 ?0 F) S0 U
制成T字形
5 L5 [$ h6 ]& q' v泰
; W' D9 }2 I, _ K! z$ N温
& f% M; `5 H2 ^' L! p6 {) o英汉对照民用航空词典B OEING2 j2 r' r; V; @" G
TECHNICAL DICTIONARY 152
: t. J3 L, c0 Y" a- q. f1 JTHERM/ x3 C" X0 `( V* J4 \& f
formatio& b/ }+ o5 E" x* A# V
using ho1 v8 k( x9 E8 D- g# {
AL ANTI-ICING, A method of preventing ice
, }: z4 q/ [: O- H+ d( yn on the nose cowl and wing leading edges by
9 {& N* d" U4 l& S& ^; wt air.- b" G' l$ l/ Z* x7 N; `
THERMAL t
* r" W$ }3 z% tin a tube fo en tube
) j5 H; O8 w2 T7 @is pressurized with oxygen.2 d3 B8 F, T0 Y9 M
HERMAL RELIEF VALVE, A valve which opens to
. T9 R/ m4 [8 rture.
, W3 F) l# `% T! nHERMAL SWITCH, SEE -THERMOSTATIC SWITCH
+ v) ?1 _9 s' O2 Ze% _4 s4 ]' M- H: l9 a, D8 U+ P3 s' v
sistance changes with a change in temperature.
( C4 H/ R; G1 g; J* \防冰,
: A% ^* s8 W; U+ [9 N) W: Z用热空气防止发动机前整流罩和机翼前缘结冰的方法。
5 ^3 q9 ]% Y9 p1 w! T. c3 j在管子里,使管子受氧气充压时温度不致于上升的一3 ~' P6 {. K6 s; T
个刷子形导线元件。
9 N- d9 F4 q% t: h控释压活门,0 o2 G- I: x C, P
过高而打开,以减低流体压力的活门。
9 P- {, K5 D x! a! q {) t1 B电门,+ d% l: _& d: f0 P6 H8 H% F
见Thermostatic Switch
) C# L) _9 U+ t) `9 c8 ACOMPENSATOR, A brush-like wire elemen
7 _- @$ }4 R- `5 s% Sr preventing temperature increase wh
) v0 H$ M% y' g4 fT* ]* B/ H- {: @. ^0 S
decrease fluid pressure due to high fluid tempera
0 l& F+ i4 w5 C. uT
& |9 Q/ e# d6 M3 _+ K/ ?8 y$ qTHERMISTOR, A temperature sensitive resistor whos4 e4 Y( c1 R6 k( r1 E; T, `# i
re
8 m9 w1 M; j& \. R) N热+ B$ Y$ `# x- E5 {8 x/ A4 U; G) M
热补偿器,0 ^3 o2 w; N: O* k: N/ f$ g2 r
装
1 Z- Q, s, q! x6 a/ n热
" ]0 C8 {& o9 h0 [& ?* ^因为流体温度
" e9 R8 V* X5 Z/ l. C热
6 L& s' @3 u' C, [, U.
k% l' k2 J8 {% p,热敏电阻
7 ^0 i6 s# @9 p% m* C! G一种电阻值随温度的变化而变化的对温度敏感的电阻。
1 E8 n2 m9 E% v: v英汉对照民用航空词典B OEING
% I( P8 A& T7 `' N, VTECHNICAL DICTIONARY 153/ M* W7 T4 ]8 c- l& H4 p6 v: T
THERMOCOUPLE, Two different metal wires joined at
, i8 e, [3 p: v- J' O* _urrent is produced proportional to the temperature$ ]1 e( G" K f4 }
difference.
. C. A( l+ Q. O: QTHERMOSTAT, A component set to operate at a
: R- K! T) A9 Xefinite temperature for controlling electric circuits and6 u; @1 r' E5 ^0 X7 g0 b+ R6 x# |
alves.- o; z2 `1 h" {7 g. o; [/ m8 X
mperature sensitive switch which opens at a preset
- L) F3 }% U( Y0 T. x, n. i& J2 X3 u% ~mperature.
7 m, F- S4 [3 A$ \/ i9 G" F; k/ aTHR HOLD, SEE -THROTTLE HOLD
! e, {: @3 g+ A3 m+ E! `. A即产生与温差成比例的电流。
$ i9 k/ e% l, Y用来在一定温度下操作,以控制电路和活门的部件。' j: o& J# O! S# z- M5 v! J
恒温电门,' \8 h! I) N0 a3 u9 R) b/ Z/ G
一个热控的、在预定温度断开的热敏电门。
2 g R: j" p1 B' R! X% U; W见Throttle Hold0 X3 Z! S# i* M9 B1 `" S
both ends for temperature measurement. When both7 M8 Z5 x2 ]8 ?' Q9 Q& O
junctions are at different temperatures, an electric* `8 S! }; Y" ]% g! G
c
( B* U E2 ? c. pd! S+ x$ Q0 E8 M/ n
v; X1 X. Q. g! C2 e
THERMOSTATIC SWITCH, A heat controlled,
8 I% X5 I4 z, @* w' u4 L* Zte3 @$ T7 Y; l5 n' }. V6 t: X
te
8 L Y0 a, } M热电偶,
- p3 Q2 Y5 P; X$ ]1 ^: O用来量取温度,两端相连的两根不同金属导线。当两端
& G5 o6 z3 }% b之间有温差时,金属丝内
. [- v& N) N/ }恒温器,
) v) r; J6 P; F1 ^油门保持,
7 p5 q% _, I+ C& h6 ^.% y9 U" f% g; _4 ]& o
英汉对照民用航空词典B OEING4 f0 Q) R- \$ x! c% h2 K9 h* r
TECHNICAL DICTIONARY 154
- u4 f) P) S- v9 d& \ k: _4 hTHRESHOLD (NO. 1), The bottom part of an opening in; r/ O5 S, j9 D. Z( S
a fuselage doorway.9 C# M, @. {* R6 v+ ?
. 2), The approach end of the runway.$ o5 y! V; ~! D& T6 Q' s3 F
THROTTLE LEVER ANGLE, Angle of throttle lever
0 K7 n% A0 R( p7 S1 ]displacement.3 _% k q9 Y; a0 V4 Q
HROTTLE SPLIT, An engine control condition in which( {, C3 d6 i; B/ c4 R
the throttle lever angle is different between throttle
) r: ?: w5 ?; q& a4 J1 K$ Ulevers but the engine thrusts are the same.
; t6 [' N! S' c, W4 _HROTTLE VALVE, A valve in the fuel control unit for. n/ b; [+ L. @6 b) P6 H
cheduling fuel flow to the engine.' i! `" ]0 y0 F! B: W9 U+ J
机场跑道到场的一端。
& Q' u5 a" g& j# k" B( n, N/ T油门杆角度,! C3 ^$ R% \9 E# g) u
油门杆手柄位移的角度。
: U1 @; }; _" c$ e! [& l油门分叉,6 @, V1 e& u1 e0 y; A; }6 p; |
一种发动机控制状态。在这种状态下,油门杆之间的油
% i! ^/ R$ L% Q1 w# r4 |! H门杆角度不同,但发动机推力相同。; V$ ~2 Y% l# u; k2 k- C' m$ Q; ]
流活门," _. p8 s% `6 X, b3 r
燃油控制组件中,用以排定燃油流量的活门。2 p6 o" k% P# Y4 F; F2 L* T. ^8 _" \
THRESHOLD (NO3 I9 Q6 I8 _' D
THROTTLE HOLD, A mode of the autothrottle where$ ?) V% ~0 y# k" z
the thrust levers remain where placed.
, b. P" k, \0 e; j9 U+ Z* K0 YT. ]5 B8 R; t* w7 b
T% Q' {0 o$ V+ @, i
s
/ b3 m# ~1 g$ C( e门槛,+ k1 ~- {; J2 p3 R, R
机身舱门开口的底部。% O- v9 H: g ~ z
跑道头,
2 g9 p5 E: F7 c) m油门保持,/ T/ Z: l; f3 m
自动油门的推力手柄不改变位置的方式。5 [3 {* V# ` I2 C1 |
节( W7 P1 N2 I! g- J: B! i* y
英汉对照民用航空词典B OEING
0 e. X: P- t" ETECHNICAL DICTIONARY 155
% k! N0 }$ n3 N. y0 J& cTHRUST, The driving force produced by a jet engine.& @' y; w) Z' C+ ]# Q. J2 p
HRUST LIMIT, Maximum allowable thrust for a specific( n. J! y. @. v
et of conditions.% @$ [" ?) ]; D( z0 e. y) L
HRUST MODE ANNUNCIATOR, A display unit or part
9 w. I S8 i6 pf a display that shows the engine thrust mode." l# Y D$ S+ d% ^' K( k
HRUST REVERSER, A mechanical device located in
! o: r8 i7 D4 f1 c' l9 J! v2 J' c5 oe fan or exhaust section of the engine for eliminating$ R: I, _. S0 G+ X; m0 [
rward thrust by deflecting fan air or exhaust gasses in/ j# H+ G% m; }; [
e forward direction can be used for stopping during
) s& e+ I1 o! U, ilanding and during an RTO.
P _: n9 [% c推力,' Q1 m& w; ^1 k( I) x: c4 Y2 m
力极限,4 }, S v0 s2 d* [+ `
在一组特定的状况下,发动机的最大允许推力。 ? b" i, ^; J: A
推力方式信号牌,& R3 d9 o/ H [0 D$ m; K
显示发动机推力方式的显示器或显示器的一部份。
# g8 ~% q( N" u" h: w% K反推装置,
7 W8 O6 c ~. A6 `# `位于发动机的风扇段或排气段的机械装置。该装置通过
1 [6 Q# [% Y! n \( c使风扇空气或排出之废气冲向前方,以消除发动机向前的
Y+ k. w, c3 i) {1 [推力,并减短飞机在着陆或中断起飞时的制动距离。
& U! B$ b: k- GT
% E0 s) C- N0 L# R6 u0 C. I) ]s4 \2 K' h- n) ^ R9 h. [
T* D( A9 [$ w( v! [. R8 Z
o
1 A4 Z9 Y" J% a, fT
! Q: s+ ~$ ^ m! W" v4 e. x/ R& Cth
( F8 a/ ~; g4 Y: L: Cfo
) m. D) d" s* Dth2 v% w8 O% M8 @0 |8 I! m
喷气发动机的驱动力。
. A# E9 p7 { q l1 u. N# c) H推
! e" ]9 N8 B) L8 w6 z* a" p( L. s英汉对照民用航空词典B OEING& d# ?- e' ]/ \; W: j4 N# y2 L0 k
TECHNICAL DICTIONARY 156* n" ?0 \6 O- }$ t
THRUST REVERSER COWL, A cover around the thrust; @9 f2 N$ c5 `* e5 S h* K8 A
IME DELAY, An electrical circuit for starting/stopping
, `- {. U- j+ m8 M# @9 `; j* h" `e flow of electric current to an operating component
7 O: m8 g. a9 X3 C' O# H# r& B) V9 N' nr a period of time/after a period of time.) _* |3 x& s9 }
IRE SPEED LIMIT WEIGHT, The maximum weight" Z# z( b& t, S; }! R
permitted at takeoff that results in a liftoff speed equal to4 L+ y( J! O( ]
e rated tire speed.# P$ d$ |8 b( N. F/ l
OLERANCE, The part of a specific measurement that
" v2 i1 D* N, U3 Dallowed to vary in dimension. Usually given in a plus! ?" G! \/ L6 ]7 D: w
) or minus (-) format.
( i: j; F! k# \8 j- iCLIMB, The point at which the airplane5 F5 Z8 @: I9 @6 H4 D
reaches the cruise altitude.
8 K) e$ A8 u. @+ r* G+ ots the cruise altitude and begins to
( U, F+ F- X8 U/ w5 edescend.) q* \( d" S3 O' {* O3 ~
for transmitting9 p" d! C6 ^( P# _
twisting motion to the control surfaces.9 s3 D) e) {# \! x' c8 o3 X
,
' v# H2 D3 {( s M) O9 b& d' u的4 ?0 k' x# `! `, A: n- z4 F
部件以进行维护。
: r1 c0 V" G, ]. a' Q: b延时电路,
9 U2 i1 L& o" A4 p. t用以起动/阻止电流在某一段时间内后进人工作部件/ l) {/ _; M& \' ^, C* \, q9 n
的电路。3 ?2 A* P q3 O# Z% c: U6 q
轮胎速度限重,. c8 O4 ]9 `* O3 c" a- p
飞机起飞时,使离地速度和额定的轮胎速度相同的允许2 ]+ K5 F; ~6 b ~; g: v
最大重量。( o0 l. V3 _/ U" R9 }6 y! W; [# Y
公差,
5 ]. _4 k0 Q$ ~' A( I, I特定量度容许有偏差的部份。通常以(+)或(-)
: {1 L5 W, w' w的形式表示。
; q2 P+ o0 c+ [" O爬升顶点, h7 S# X: |' D
飞机达到巡航高度开始平飞的那一点。& r4 U3 E+ C ^7 e# a
下降起始点(TOP),: T& }+ X/ O9 h3 Y% R2 @- w
飞机飞离巡航高度而开始下降的那一点。# u+ A& b4 i& x( j/ e5 p
操纵面的管状部件。9 _0 u' A$ w* |- h( {' ^# n8 A
reverser of the engine that can be opened to access
$ F, \: J5 m# H U1 |components for maintenance.
& x- N* ~ k: W, u7 QT$ E- L; B- |6 a( b3 {/ L
th; U* C( y* [, L" j; H
fo$ w; c% \& N( q' k4 Q
T
/ E8 _9 C. z4 k8 Uth
& o9 X3 y) {: M/ v: V1 @T
/ n) ^) f, F$ T! A- A3 ^4 u' ]is7 U/ M9 `5 I9 E& H6 p
(+
& _# r% m; {6 Y5 u4 vTOP OF( q! g/ g' t2 G7 I2 m* _6 E
TOP OF DESCENT (TOP), The point at which the
/ O" P5 T, s# I% \. U+ W0 E, ^7 ^airplane depar
. c1 B8 `. _: D8 f. M/ kTORQUE TUBE, A tubular component- O3 U. D# u; |' w q
反推整流罩9 k! ?% U% x% y% M
在发动机反推装置外围的罩子。取下后可以够到内部" A- d: J5 G) H& k
扭力管,- x, S( V4 L8 x& y% i i7 o W: R
用以将扭转运动传给4 f# f* [3 k% J3 n9 D0 B
英汉对照民用航空词典B OEING
1 O' C9 u% p+ HTECHNICAL DICTIONARY 157! J( `1 B( f" a* Z( E S
TORSION, Twisting of a material or part caused by
0 \/ L% @$ y( s3 Iexternal stress.; H, r, J0 u; ?: z: [% k/ [9 R
ORSION LINK, A hinged linkage connecting the inner$ K6 E0 m+ N2 }" ?* B
nd outer cylinders of a shock strut.2 U+ B! n2 @: Y! r" O9 c
due to the ram
: H3 [* Y6 @0 \8 e. p& {0 Wffect of high speed flight.
* @9 c Q1 F+ R% |, ?URE, Pressure higher than ambient6 J; l: h- `1 e
ressure due to air flow, measured in pounds per
% X. N7 G& g" e2 g3 o: Rquare inch (psi).8 p" a+ X. S7 q3 I! I! {" ]7 p% y
er than5 m3 t" g! Y. z
mbient temperature due to the compression of air flow,$ Z! J1 l, V1 @0 ?$ W7 o7 P
easured in degrees Celsius (C), or degrees8 k2 x# c% J( R4 }& w: T
ahrenheit (F).
% S& k; y H8 \7 pTOUCHDOWN, The point at which an aircraft first k' r; m3 }! M* ]! C% z2 W" w
makes contact with the runway.) G% P, N9 c+ z6 Q. K7 m3 r8 K- }
生的扭转。4 Z3 Z, ~1 L8 x
扭力臂,+ `9 Q* y) N2 U7 c J' f( O3 a
减震支柱的内筒与外筒之间,用以防止活塞旋转的铰链
1 y" k( \* e$ J, Y, ]* \, }连杆。
L3 O0 G5 |/ A9 U# F的冲击效应2 Y3 q2 S- _5 b7 O1 V3 S2 P( _
引起的温度的升高的总和。5 w% s8 E1 X E% Z9 O
总压,- }( D) W, y+ O& Q d
由于空气流动而高于环境压力的压力。常用磅/平方英
/ f, r+ E& O& { T* A(psi)来度量。2 o0 a0 q$ t5 [4 x- W
全温,
/ p: E3 X6 P0 p- a. x7 F' X; D由于气流的压缩而高于环境温度的空气温度。用摄氏8 n" w& R. E5 c) w5 x% H
(°C)或华氏(°F)来量度。
. [) b: j0 H0 r+ W# h0 z& o接地,
( d1 D# z) z- [4 c0 n# a5 a飞机降落时,飞机最先接触跑道的一刻。, G8 ]3 T7 n% g0 P
T4 C$ m5 R. {3 J) d6 u
a! b% A+ J- h7 N6 V( O! K- y4 G7 m
TOTAL AIR TEMPERATURE, Ambient or static air
+ u# A. }+ \* |; [2 V( ~/ z+ Dtemperature plus the rise of temperature
+ w4 |8 O% V4 W p) z" a+ ?* A: l ye3 D: X6 X/ O! \1 ?& M
TOTAL PRESS( h# t; ]. d7 ~$ m& m6 [
p9 J. V/ T J& L8 I" T. M/ @
s
. ~7 r1 X3 h( y. r# M \TOTAL TEMPERATURE, Temperature high+ m$ r0 [- Y- M b, V" c
a0 e2 c9 Z& B" r( d( v
m2 g% v% d; e7 e4 l" L( K
F
% A' D; Q/ F9 `% }扭曲,4 V. e" t* H* I. b q% t
物体受外应力的作用所产
. {+ G: ~' l) L/ ]+ K; h空气全温,
, W# X& L. z* V* t6 S- U M0 T' }环境温度或静空气的温度,和由于高速飞行! r8 ~" ]) o2 q1 `( h
而6 g3 c. M5 s0 O" N5 r
寸
0 o3 R$ Q6 B* B: c2 S0 T英汉对照民用航空词典B OEING
6 Q7 G6 ^3 q& Y( x! x9 gTECHNICAL DICTIONARY 158
* l9 k& V4 s0 f2 M* N5 D+ jTOUCHDOWN ZONE ELEVATION (TDZE), The
2 A. L( q$ \+ L# K1 l4 Zhighest elevation in the first 3,000 feet of the landing
- N6 ~7 I3 w b' N: m4 F4 aurface.2 ?8 ~% Q- \# `0 T4 U# ]
rt of nose or main landing gear for
- X* M/ Y) J( }# ^ttaching a tow bar to move the airplane on the ground.+ _& }& N3 {, g
along.
- H7 S/ I$ _* H% ?7 s& X& ]- \RACK (NO. 2), A navigation term that describes the! J7 z0 n5 A% G2 \
TRAFFIC ALERT AND COLLISION AVOIDANCE0 @! O: \( L9 }# e/ }2 \
SYSTEM, A system designed to alert the flight crew to, j% E: y7 }* V" ?+ Q* y
potential conflicts with other transponder equipped$ `8 p/ _) d. I! a" U( m% k$ m
airplanes flying in the same area.2 X3 y0 C" ^& a/ M3 ?1 w
TRAILING EDGE, The rear edge of a wing, stabilizer or1 f/ A" K+ P4 i1 k; k6 p2 [/ n
control surface., g. o: o# B7 I- \7 Y f
TRANSDUCER, An electrical device that either takes
8 Z% O# B# @ w7 Oelectrical energy and changes it into mechanical
' T, d* J+ \; _, F. Lmovement, or mechanical movement and changes it) u8 @3 w; s& T! G+ E' M, S
into electrical energy.2 t) u4 F% B+ C. C7 Y' T, S% f5 s
TRANSFER GEARBOX, SEE - ANGLE GEARBOX
* Y5 ^1 x4 F- R+ V/ c高(TDZE),5 R3 e n" R: g$ j
高标高。
) f9 g1 c- `5 p1 C/ x9 S前起落架或主起落架上,用以接上牵引杆以便在地面上$ `$ G% D3 K; p2 u* e* k3 B; {
动飞机的部份。/ [; s+ p* `* t; }
轨条,
/ C" N- A- w. U( c2 G! Q4 O6 `迹, `* Q' u& r8 E
形容飞机航迹在地面的投影。
; }3 S7 |7 _3 O& b空中交通警告与防撞系统,9 j7 v1 D2 H& a
用来警告机组人员可能与其他装有应答机且在同一区$ c" C3 E) F' ?# ]2 _
域飞行的飞机有冲突的警报系统。 _2 ^, P% @5 j. ?5 {9 o
后缘,
" \: Y+ {9 M8 N机翼、安定面、或操纵面的后边缘。
0 z+ V% I3 B# {' {6 p% c换能器,, j- N* e( ?' p7 O9 B1 X
能将电能转换为机械运动,或将机械运动转换为电能的
) x1 A; ~+ f' u0 T; M( _ h电气部件。
1 h8 I+ ^" b, r9 y" l9 \转换齿轮箱,
3 ?% i% a2 U N/ \7 U见Angle Gearbox' [& i) K! h: S
s) L6 L) D" r. k
TOWING LUG, Pa3 v. ~6 F6 F2 p1 V
a- ^# j# C) A* D s6 g
TRACK (NO. 1), A structural member for attaching fixed
2 ~+ I* J. y. a# l( ]: Q1 _components to, or guiding movable components* R' }; u* d! y0 s- J
T; {; M9 S9 j+ J3 t2 ~7 \
projection on the earth's surface of the path of an
8 k$ e. |9 P" [- Rairplane.$ y% u, t# `9 g9 T" ^
接地区标" X1 d! @, T" A, q( n5 o2 K
跑道头端3,000英尺的最' X- y6 v) G5 ^
牵引环,
- ?6 w. p4 @( u, b( T* \, @: m移
4 q6 G9 G2 b$ }0 {5 i1 p5 E% E用以接连固定部件,或引导可动部件的构件。
+ B; @( s# B" a7 d航
8 X2 x4 m9 ^* ^9 }" }* O+ w导航术语。2 b- ?7 L7 K* Z, | l3 d6 ^+ g
./ y0 I% R. d4 m# }% w9 k5 D
英汉对照民用航空词典B OEING
& V: n' V0 a: d7 Z+ J$ n! b7 h' C- FTECHNICAL DICTIONARY 159
) I2 [# r+ G. I/ c2 Y% CRANSFORMER, An electrical device which uses% [+ O7 {+ r6 y
RANSFORMER RECTIFIER UNIT, An electronic
( _% M2 M+ `& fevice for changing alternating current to direct current' _, Q* q7 c3 x" \. e
supply airplane electrical systems.
+ M7 L1 Q6 X. V K" u" J, O K6 ?lse signals or triggering pulses$ `& j4 Y m" Y l8 ^" j" Z- r
nd cause component breakdowns or failures.
5 _" V- A& y4 e6 T+ FIt consists of a base, collector2 N6 K4 b0 V; X' s
nd emitter. Two types of transistors are PNP and NPN.
, p4 o2 y7 _( c5 ~' p。3 j K' u. I4 Z9 Q5 O6 I% j) L0 Z
变压器,
8 ]0 p. t( t# q- S4 m4 Z" A3 Z0 ^磁感应,将电能从一个电路转换到另一个电1 g/ X% n" Q: D% w
变压整流器,
$ g1 `: b0 q K6 n6 v用来将交流电变为直流电供给飞机电气系统的电子装
6 |9 d# y0 C) G& h置。
: i7 I0 Y; A3 a# c瞬变,1 s" D! L; q, D/ {! u
信号或输电线上的瞬间电涌。这种电涌常会产生一些错* u4 r5 L5 |4 g3 r
误信号或触发脉冲,造成部件故障或损坏。
; A; S; @* o- e+ u) B晶体管,
4 j7 o |* Q- Y3 W2 B7 w3 t2 e$ z) ~固态电子部件。通常具有三极:基极、集
& a& C3 h9 i x$ V+ L极、和发射极。有以下两种:" n$ a/ f% n; R. X0 m& c# j# F- I
PNP(正负正)基极电位低于发射极。$ G! d0 m- e1 t6 c
NPN(负正负)基极电位高于集电极。
& k9 B$ K; D7 J8 L. q' ~( }TRANSFER MECHANISM, A component for8 g5 x# w, f4 N
transferring motion from one place to another.
& k- |6 f, X; \T y J* |1 y4 ^
electromagnetic induction to transfer electrical energy* v9 f5 y7 A4 a, s! ~% p7 h+ L3 M# X8 p
from one circuit to another circuit.
1 E5 |7 Z# ^ F lT/ K# C# Q P" @1 w
d
9 T9 K; X& o( ]8 v7 d/ }to
* O8 [# N+ o+ R2 E* uTRANSIENT, A momentary surge on a signal or power% V7 R$ Y) q3 D# `
line. It may produce fa) y) B: E$ \5 N9 X
a
8 |3 T& w! ~5 G% fTRANSISTOR, A solid state electronic component for! s. f; S# d7 y W2 Y! K
use in electrical circuits./ C9 P: t& L' S3 R& k
a
% B( N6 X# x/ ?( D9 W- ?转换机构,3 z8 D. Q0 E6 Q$ ^3 u L5 g. f
将运动由一处转至另一处的部件
( K9 d: \3 C) b; @) ?( y9 v一种利用电
$ ?& y/ i( |4 A8 T4 s1 d路的电器装置。( C. f( r6 k9 X7 ?" y0 p! e+ g/ x
电路内使用的6 h! u4 I; ]0 d1 L+ O# h
电
. w& ]& W) D9 a* p8 z- |2 v英汉对照民用航空词典B OEING( \) V- r3 h% ]0 S/ Y; |, A
TECHNICAL DICTIONARY 160
3 s! O- {8 U" d+ N/ P- U4 s( }TRANSITION, To change from one phase of flight to" k' ?0 N4 j5 M! B
TRANSITION ALTITUDE, The altitude at which the. G, m- f% }. w
ltimeter setting is changed.3 r6 Z0 e3 A% @; H# u6 ~
RANSLATING COWL, The movable outer portion of
9 [9 ^, `, T- {# `) N# P+ q- b; z1 ye thrust reverser cowl which is operated during {& z7 W* q" m3 S" N: \( |0 U) \" E
verse thrust.5 W0 g3 P6 g' U) E- I
RANSMITTER, An electrical component for sending
$ j; x: a6 \- f1 U% r6 z+ vformation from one location to another.2 q e2 |4 x0 W w% n
TRANSPONDER, A radio transmitter-receiver which: a6 \) b1 S' v
ansmits identifiable signals automatically when the
3 U& G2 f' C( A% i- M. FTRIM, The adjustment of engine and airplane controls
* W: j G+ Y1 Q从一个飞行阶段转成另一个飞行阶段。
) @7 F+ \) `( _5 D& u3 n: f) `) ^过渡高度,; m/ j; p4 O$ b' M
改变高度表设定时的飞机高度。/ ]7 i: v9 _' u* c4 C
平移整流罩,
/ r* w' v m1 W# {1 P* n p. r- {反推过程中使用的反推整流罩外面的可动部份。) E- u m: h u+ Q4 L
发射机,
2 I. ]( O" U# Q3 M: g6 F. u将信息从一处发至另一处的电气部件。
$ g5 U6 w$ ~9 O# L: o应答机,& ?6 p; B4 }# w: Q( f! \
在收到合适询问后,能自动发射可识别信号的无线电收6 w) d4 ?2 D8 z E
发机。
/ S# Z& a. x5 c' b平,
5 E- J, Q, u! [. ^5 h t动机和飞机在平衡的状况下工作而做的发动机
, V) Y# C3 M1 E& U! Oanother.
7 G* i4 \3 R* j' E/ _2 H% `a
; B4 d7 i2 w! _# e# `, YT5 K3 @! _" s+ }* R# |3 Y- K
th8 L2 k. v- x8 ^" a |8 i
re
3 @- s7 N: J/ o! s0 G& ST
% ^" W, `8 y$ b3 e) w! }) vin
# f# q' u4 I/ {3 z0 {tr6 I% z' C; d6 B& g, X- |
proper interrogation is received.
) n/ N7 R+ d- ?$ ~; r# U" afor a balanced condition of operation. k7 P) o' A5 o8 _
过渡,. }: P8 j1 z3 I4 q- f
配+ \# _. i ^& a9 Y& z4 [1 j+ X' R! k
为使发0 i1 d% ]* `( L+ ?" S% J6 s
和飞机操纵系统的调整。
. K: {( J* v& W4 T! s: B+ k英汉对照民用航空词典B OEING
( o* g4 E6 E0 c5 p! B- gTECHNICAL DICTIONARY 1612 z7 ~* a# |# P6 e8 ~
TRIM TAB, A small hinged movable part on the trailing
' x, W( U# v$ _+ T$ }* hedge of a control surface (aileron, rudder) (see TAB).5 q' j9 c9 M- F
L, The total fuel consumed from brake release
* y8 A* X: W) xthrough climb, cruise, and descent, to landing at/ C# P9 {2 _: ^8 P
destination.
% @) X% ?: f4 x q- T& s# h# ~RUE AIRSPEED(TAS), The actual speed of the, S; N3 D( H$ Y
aircraft in relation to the moving air. The true airspeed is
/ r. z) U9 W" c* l q; uated airspeed corrected for position
4 C- J- h- d* O, y* v9 [rror, compressibility, and temperature effects.
" K% q; {. D/ o8 H; \2 s# [# Hribes" G7 K* X3 f. u) R- G
the output value for each input
; ~$ j6 w! K2 V! V* w4 U- Z! i9 L5 S. wombination.
* k/ U6 e# ^* u5 r$ {铰连在副翼和方向舵等操纵面后缘的可动部份。/ U1 u T- O( t' C
航班燃油,
3 z, N. a) {& J/ Q8 P) t2 _5 v0 l一个航班由松刹车开始,经过爬升、巡航和下降,到
/ S q* D+ i4 b0 u: o' ^目的地着陆为止,所耗的全部燃油。
& n& g' Z' c! q8 x& q1 v u变压整流装置,
/ x$ x5 L- i3 B+ y7 Y. o5 W3 ^见Transformer Rectifier Unit% ?8 `3 H6 B6 C9 [ ]
TRIP FUE2 G6 j& I/ N4 t0 y* ^* d- W
TRU, SEE -TRANSFORMER RECTIFIER UNIT% ^6 S* U$ M' O+ Q( H, c
T: P& B" n" j. y( V3 Y
equal to the indic
4 F9 p& X- U) Z. oe
! F. e) |! d z) A- t/ H# k" g4 A2 {7 yTRUTH TABLE, in digital logic, a table which desc4 X& i6 U: t( M" z+ v
a logic function by listing all possible combinations of% G7 u# S2 L- s0 O4 ^8 B! T
input values and shows) E5 q5 N/ }# n0 S
c( G6 N% u' F# x# z4 B2 P5 }
配平调整片,
& V/ ]+ V0 O0 W9 k# l5 o8 n在( ]( J r* i8 B* s
.
- y" @* O0 ^3 I& Z, p真空速(TAS);
! Q. Y( Q7 P% k( v: P& K" l$ ^对于流动中的大气的实际速度。由指示空速经过
( S: g; a- x6 J' G: r1 `真值表,
& {/ i/ I8 k0 x数学逻辑中用来表达逻辑函数的表。该表列出了所有可
- \2 ~2 p( T4 u2 A能的输人组合,和每个输人组合所产生的输出值。
" t4 b( O- P& m& [" N飞机相
8 D1 k) f9 V6 i位置、压力和温度校正而得。
7 O/ x$ W4 z" D$ D: _8 X# h0 e英汉对照民用航空词典B OEING- ?: E& R( X8 f: o" R- l" ~# K
TECHNICAL DICTIONARY 162
: R- G; l* K+ N% j8 t1 \) uTURBINE, A rotating part of an engine which9 K5 x% p/ j# K+ h; Z9 |8 [
kinetic energy from the combustion chamber ga( T0 U' z [! D) u" D
extracts
1 E- y& D6 H: Y. rses.! O8 B7 o& L( l% W% o1 l7 g" @1 T
his energy is converted to turbine rotation which9 f3 j! X7 C& z5 Z
tates the compressors and fan through a coaxial
N: ~$ }- e7 P* ~; X: Y- ?haft.$ v! l9 q( A( O7 V6 y6 ~
TURBINE CASE COOLING, A method of cooling the
: {' P7 u0 Z) `3 mngine by using fan air. This cooling process is used to9 Y7 {* m9 G& q, h
TURBOFAN,
; r' h6 w) q- p(1). A jet engine in which the first set of blades is a
9 g9 f- U. Z& f$ @+ c J4 G- wlarge fan.3 m/ E t- S, n) V: G0 R
(2). An air driven fan/compressor used in air
: }1 w9 f) \+ F8 O7 g& A9 Bconditioning system.6 w; ~- ~& n. d5 r5 V+ ]. w- Y
TURBULENCE, The movement or shaking of an; e3 w$ H+ n# t9 H" S, h+ _
airplane caused by unstable air masses.9 m3 @7 j8 a; M# }% e
涡轮,
' O: t+ R6 T8 Q, b5 i$ s( ]/ M* ]' p7 k发动机内,从燃烧过的高温高压气体中撷取动能的转动
% d& Y9 Q# [. h. ?0 M8 z8 _份。该动能使涡轮转动,涡轮则经由同心轴带动压气机
% y& Q0 N0 B( i+ Y6 C V风扇。
b. Q, u& ?$ X: i% P+ \" B涡轮机匣冷却,
( u3 G5 v/ a' g7 c用风扇空气冷却发动机的一种方法。该冷却过程被用于9 l; o. e7 W* p3 J8 l, K5 u h4 P
效率。
0 K! S6 b, C7 c+ L# n2 [(1).第一组叶片构成一个大风扇的喷气发动机。
L2 a; S7 v! z' a% Q7 e(2).空调系统内的由空气驱动的涡轮和压气机组合。
- y: \) e W7 @颠簸,4 M% b* N5 G4 m6 p9 p/ Q
由不稳定的空气团造成的飞机运动或抖动。! I# Y! F. O5 h# v3 U5 u9 u/ Q
T
2 c7 c/ W1 k2 F) }7 ]5 U0 G @ro' N- }% V$ j! s5 e0 k( c4 ]
s4 X, v0 H; ~1 e" F8 P
e
, s9 U. w* ]( D$ }7 X# Jincrease engine efficiency.
9 Y7 f `, a( h1 X5 v5 h( M% i部; z9 m% g! Z9 V5 [6 V
和
+ g; N! j+ X. b3 n/ z提高发动机
# O- N) ~+ I- |5 |2 H; d涡轮风扇,9 Y- [/ |4 i6 r* s% t
英汉对照民用航空词典B OEING
' D+ i# n9 T+ t. PTECHNICAL DICTIONARY 163
( i* { |% l e& b: n5 vTURBULENT AIR PENETRATION SPEED, A speed
4 V; i2 o4 Y, A' q; kthat provides adequate maneuver margins when flying5 ^7 Q- q; n) ?* {9 w
to unstable air masses.+ P, d2 G2 p, {: O/ @8 d6 P* r
ht
: P+ |# v7 F1 d4 T. c+ Estment in the control0 Q5 t; r0 R4 B5 F8 Y7 W2 {, Q
ables.
! R% U$ f# l0 L* GUHF, SEE - ULTRA HIGH FREQUENCY+ g8 N# i6 [+ v2 L- R
NDERCARRIAGE, SEE - LANDING GEAR3 [* F! G, d: t W! }
UNIT, One of the type, a single component.
/ P" t$ \( H' ?7 b/ }8 H) v2 dUPLOCK, A mechanism on the landing gear for keeping
; I/ M0 r u) N7 Tthe landing gear in the retracted position in the wheel1 s2 |) R9 Z% Y m/ I
well.
/ S4 W0 d5 y2 m" y) O速度,
3 P2 Z& \8 w. N6 O纵裕度的速! p2 I+ v7 Q$ C, t7 d
。" S8 @1 A: W: A1 n# s6 l( Y7 N' O
调整操纵钢索张力的
! J' D4 }+ u$ V R; k械装置。
3 U' Q u3 { J) j) `8 U高频,; ^; e9 D; v0 E4 W; M7 [
见Ultra High Frequency
& m$ Q* k+ n5 Q9 Uin
- t* B1 ^) t; i7 t8 P' Y# p- W5 y! q, }TURNBUCKLE, A mechanical device with left and rig( H( O* l, e' u
hand threads for tension adju" V( z0 y9 X3 a. D
c
2 r, v' P) M, t; E. o z" ~U
& m x8 H" q$ d/ [5 C$ r* VULTRA HIGH FREQUENCY, The frequency band
9 H) \7 y7 O' sbetween 300 and 3000 MHz./ s \3 U5 z! t% i
U
4 k2 Z% Y% L. f }& a7 m' j3 Z2 \颠簸穿过3 v: F4 T( i- h, B L0 @7 P& y
飞机飞进不稳定的空气团时,提供适当操" W0 G! a) D. Y4 f- ^/ n0 r
度
& f0 h$ b% w/ i6 [3 r9 B松紧螺套,
2 s5 M/ m7 |7 t: B具有左旋螺纹和右旋螺纹,用以
2 \7 T8 [- |% D4 \! g; \4 I' o% C机; G, P) Q# L% F. O8 S2 z/ s$ h
超& P! k/ F' G" f" i5 |# z
超高频,0 }: z0 T# F6 @1 q( C4 l" X' U; t
频率带在300 MHZ至3000 MHZ之间。; u9 ^- m" o5 h' d" D
起落架,
[* S0 Z; _- z见Landing Gear: z7 [" E2 g5 U+ P. F1 U4 \
单元,6 F- i" z8 i7 p! c+ n* c
某一类型或某一部件。6 L2 y& ^0 C5 z& d
上位锁,
. E% S0 R H9 I: e+ c起落架上,用以将起落架保持在轮舱内收上位置的机$ p$ P1 N3 x4 g; h$ Z, c
构。 O* j5 Z) M- I2 @0 V* H8 s y
英汉对照民用航空词典B OEING* V; q2 {: k& M. _2 m+ S3 P
TECHNICAL DICTIONARY 164& g! V$ J) k( H
UPSET HEAD, The head produced on the tail of a rivet
* s$ p5 [% _' b5 N. Q# G' |/ cduring the installation driving process. (See/ x( m# \' [0 E# Z% N
Manufactured Head.). O( c1 }2 Z i' Z
1 (TAKEOFF DECISION SPEED), Is the maximum* w; c! d& x) Q4 ^5 `
peed at which the rejected takeoff maneuver can be
- D2 v0 w1 y0 Aitiated and the airplane stopped within the remaining
7 t8 v' o5 n4 w- i# Zeld length under the conditions and procedures defined
/ w9 I' H' t1 `. C# F; B' dthe FAR's. It is the latest point in the takeoff roll where
2 n" ~1 v0 `' W% zstop can be initiated.
7 L# ?- w/ d: W4 kssure
/ ^6 g( F# i( M4 ~+ S" ldient capability and maneuver margin.
+ l1 m% E- i+ O2 \1 w9 @, X" ^VACUUM, A negative pressure or pressure below+ G) F' i" ~; ~2 N
atmospheric, measured in inches or millimeters of: a- i( }! I5 V4 F9 y5 e2 Z
ercury.0 n! j" v6 \, I0 o' \
is
: Y( k' o; y) x; _7 N5 P3 BVENT, A small hole orifice or restrictor in a component
( ~# A% ?* s# ifor allowing pressure in the component to be the same
$ y n6 n2 i+ `0 _( s: Zas ambient pressure.9 X; \$ v! a; |- Q& R
在铆钉铆接过程中,铆钉尾部一端形成的凸头(见
- ]3 ^" j" w* E: kManufactured Head
z( o% U" Z& ?V) P& }% ]# ]* i: |2 d1 |
V& t" K( F; S }9 ]" w
s, _( ]5 p) _2 T5 ?0 d* w
in. x, {8 K* n/ l3 b9 B
fi
" v" F. r) v9 I" tin3 I. h. M( v$ @% K1 s+ b" G
a+ X" ^& e1 {& B9 M" _! s7 @1 |
V2 (TAKEOFF SAFETY SPEED), The speed flown after8 M' x& _2 F# X3 b4 X4 U/ p# ?! F
takeoff during engine-out climbout maneuvers to a
2 {: y, s7 c( c: Z" K* Q" sadequate gra
7 l/ `! {: e+ u" o& ?m
0 z" V" h! f; oVAPORIZE, The mechanical process in which a liquid0 T6 {* W% ^3 y7 A, b
changed into a vapor.
' C n3 T9 C w, m6 q; tVECTOR, A heading issued to an aircraft to provide3 N/ A4 |. R( c
navigational guidance by radar.5 B, F% t4 t9 T# N* S
铆钉镦头,& D( ]" t9 u$ g1 n, C
)。
" M+ k, A$ [6 e+ S( Q( d1(起飞决断速度),
& }7 o9 ~. z) k: K# y% n根据联邦适航条例的规则和程序,飞机能进行中断起飞' f0 z# `1 x2 G' Z, |, o0 A' E; n
在剩余场长内停止的最大速度。它是在起飞滑跑时仍可
( ?, g% G# C' V- P& K住飞机的最后决策点。; _9 e9 c6 \6 z2 ~
速度),
) e0 N2 f9 t# J/ t1 S; I在一发不工作起飞后的爬升中为保证足够的梯度能力8 t# b @( D/ s
和操纵裕度所飞的速度。! Z1 ~5 Y3 ^- i ~3 D
若干寸(或若干毫米)
( l' ^7 x" P9 p% s/ q( m3 o汞柱。1 i) _1 p; [ S: r) v5 h* G
蒸发, ?0 J2 n$ K |0 X# R, \
液体汽化的物理变化过程。
$ E, R6 J I e! M! K3 Z引导,
4 `5 Q K6 H( t) @6 e. H# X由雷达提供的航向,以给予飞机导航引导。
3 f. }' R, H3 n# |, j通气装置,* C( ~0 @ K' J0 x2 D
部件内,用以使部件内的压力与周围环境压力相同的小
) c+ @- G8 L2 C5 ]孔、或限流器。: W* R/ n% V, N6 U9 j- C
V1 j, Y; N/ U% k) t/ }0 A
且0 h; n% H, O1 G
停* L2 A3 s7 P* P: a" P& `) s4 `
V2(起飞安全
9 N9 {& l6 R% \/ U真空,# b7 s1 \' k* \5 [ O1 W9 p2 Q
负压或比大气压力低的压力。常用
. w7 i5 {3 T u: d. [& ?; M英汉对照民用航空词典B OEING
. g: a* g9 I6 G7 |5 a: v0 H! N* rTECHNICAL DICTIONARY 165
5 K" p: V* n7 Q6 i9 L3 q0 QVENT SCOOP, An air inlet/outlet on the bottom skin of0 u# P% R- i1 O4 Y, V1 h# t1 s# w
ir j8 n5 p' S! C; s5 {( S0 d
VENTURI, A part of pneumatic duct with reduced flow* @% D3 V, T; L/ j6 o
rea for airflow measurement. (Principle: As air velocity
, j+ [% z1 H0 X- y, U7 acreases, pressure decreases).$ c- W- y6 X3 j4 Z& f
ERTICAL AXIS, A vertical axis passing through the
: F3 \9 ~! C- q6 l( Y1 ]# ?/ R- ~airplane from top to bottom. Airplane left and right
3 A a+ ^1 A: j# N7 O0 C* {trolled by the rudder.& D) f, B E3 l/ G. {# N2 U
VERTICAL NAVIGATION, Functions which provide7 Q4 a: _: t" @2 }0 P
guidance signals to control the aircraft during climb or
' C2 K% O5 V5 g edescent.
) v8 }" |5 \$ i) Z/ f6 r" \.9 w3 M2 B8 w6 o; x
通气进气口,8 _$ g7 \9 Q3 l' Q4 O% C) u
位于机翼下表面蒙皮上,用以燃油箱通气和提供燃油箱* F0 i) D7 W& P4 q
内正气压的空气进出口。
3 C2 H% Y* U8 a: T/ I) G) {- Y文氏管,& f! ^# i$ o# m! @' T0 A
气源导管上,导管截面变小以量取空气流量的那一部
1 w. H. c6 C& E份。(原理,导管截面变小时,流速增高,压力降低。)
\2 N% c- d7 B( U+ [垂直轴,: e" K/ [, X: O7 l
由飞机上部至底部的垂直轴。用以操纵方向舵,使飞
0 {4 T% e, i: q) w) B3 P. D右运动。
% S p) N" t# @* \6 r$ q( v9 s直导航,# o# V7 ?) ~% y2 Q3 w7 w
,
% K- t; W; ^5 l# B' g' Q# tthe wing for fuel tank venting and supplying positive a1 Y+ Q/ I/ g; H5 q4 f: s
pressure inside the fuel tank.
$ v i+ Z% u I6 ?8 L8 X8 X1 H4 E. ba
0 T) l$ ]+ c: M7 K* Bin
& ?, x( z0 K3 D+ i2 E7 ^V: y4 }$ Q# x/ G3 g# M
movement con$ z9 u9 L, ^6 v6 d; N8 o
VERTICAL SPEED, The rate of change of altitude
5 \* t" J1 y0 v1 I5 G机沿此轴作左
0 _& L- L* k% f6 x3 `垂
" A* v! w. E( R7 \. I在爬升或下降期间提供引导信号以控制飞机的功能。
' N; `. t: b- ]6 [, [# f( }+ `- M垂直速度! k& g2 M4 y8 u5 S2 {
飞行高度改变的速率。
1 k% i& Q0 `$ O/ G! J1 O# q英汉对照民用航空词典B
* Y: n# c' n* Z" ]2 vVERY H2 C9 C; a4 A1 G) \6 R; l
OEING
5 o. M+ B/ k* q+ \; vTECHNICAL DICTIONARY 166
" r( z+ z$ l) \VERTICAL STABILIZER, A vertical surface of the0 |- L0 I7 i' o2 {- j9 x6 k
empennage for stability/control about the vertical axis.
4 L" c2 }% x/ l1 R# _VERTICAL TRACK, A climb or descent profile.0 D1 z+ ~; _; {9 d1 u
IGH FREQUENCY, The frequency band
7 ]& ] t' y' X3 B0 ^# y; E0 PVHF OMNI-DIRECTIONAL RANGE, A navigational! b9 r% H7 Q& j+ d( U( z* i8 h8 E
system which tells the airplane's bearing from a VOR& s f) T& A8 g4 p
round station and its deviation from a selected course L) ^1 j: C" s, f* G! [& e
/from the station.
3 b6 X2 ~# n/ W/ G& z) ^ISCOSITY, In a liquid - it is the resistance to flow. k& p1 h; N0 W/ q8 } Q) B, ^' l
VMO, The maximum design airspeed at which the* Z# e) ?7 k( J6 i% G! X
airplane may be operated.: s; m( v1 ?$ Q; @8 l
在飞机尾部,用以保持飞机绕垂直轴的稳定性和控制
. Z3 d( e8 z( u f( D2 Y的垂直面。7 l1 r2 h. Q8 p. z6 q, k
垂直航迹(VTK)," N1 |+ E9 |- Y% h( U X
爬升或下降剖面。
% }" f; X( B$ Y* d甚高频,4 U/ B0 _3 r+ l: Q& s
30 MHZ至300 MHZ之间。between 30 and 300 MHz.
1 G% B) ]; m9 p" ZVHF, SEE - VERY HIGH FREQUENCY
; o3 w8 w4 p+ b$ y" d& Cg: y \0 C% }, }, ]
to) \) |# N3 L% n9 ^0 S7 A* C
V
/ T5 t3 ?/ I" ]7 r, a, F垂直安定面,% t3 q. }9 T1 n: C2 |! g l
频率带在
; ~) ^# S" q; E甚高频,
9 |2 X( y. u& e+ q见Very High Frequency8 X7 D# C& l& h3 f
甚高频全向信标, m, g5 B! q8 X6 Q9 ?
系统。该系统可提供飞机到VOR地面台的方6 S/ p; w0 {+ A; i
位以及飞机的向/背台飞行的航道偏离。3 R7 a& B) c; m! e' S
粘性,4 T7 o& u g* `2 o5 Q: `
液体中阻碍液体流动的阻力。& w" |9 }- F6 U) W: V4 e8 t
最大使用空速,8 i5 Q/ N. m2 e+ M! ^- O
飞机可使用的最大设计速度。1 ]( P' x) B5 Q# Z6 {
一种导航, d$ D& x+ o" r' a' i
英汉对照民用航空词典B OEING4 ?4 b2 @, e j. D. H2 z4 A
TECHNICAL DICTIONARY 167
' {8 k& W' o. [" d8 u. E) iVNAV, SEE - VERTICAL NAVIGATION2 m3 h% h0 r0 {8 k5 u% \
VOLATILE, The ability to vaporize readily.# i5 t) Y. m# k: T
LE MEMORY, In computers, a memory whose1 H- f9 j5 A. x7 B0 ~, u4 r% w
OR, SEE - VHF OMNI-DIRECTIONAL RANGE/ A$ k. C( o4 B4 ?# v
VORTAC, A combined VOR and TACAN station.3 [, A2 {0 M% R2 P. f }1 |
ORTEX CONTROL DEVICE, A small airfoil on the
+ Z/ j) s7 I, q; F: W/ I- `- f- i4 pacelle for improving airflow between nacelle and wing5 i0 {' x6 o3 \
leading edge.) u8 U# f/ n6 A0 f
VOLATI
; `5 f5 L& S) rcontents are lost when power is removed.; p& i. |- _5 J; ?
VOLT, The unit of measurement of electromotive force.
4 @5 g G+ V" J6 W! ]) zV2 ]- j6 _3 i/ s$ n: K
V3 S8 r1 u6 [4 A
n/ E# G& x( @7 |* L9 Y) d9 A9 |) }
垂直导航,
- m) R( U, p6 K. [, \+ E见Vertical Navigation.
* K! D6 Y/ w! m: I易挥发的,
, M7 x" S8 n0 r- m! s; _2 M随时可以蒸发的能力。
/ H1 P, @3 l) r; A# y- y易失存储器,& o" H, }5 |' ~( u$ B& e: R
在计算机中,失去电源时存储内容便丢失的存储装置。% r, P" H! a8 q4 ?0 ~2 w( [
伏特,; j# C6 I5 @1 j+ q ^" D- O
电压的一种计量单位。# ~4 Y* K0 J0 z5 L0 `0 f% A
甚高频全向信标,/ J6 b$ q6 ` S* M
tional Range
) I+ t: q; V1 C4 B, t见VHF Omni-Direc .4 `6 F5 M% i0 l
VORTAC,5 N, d) N2 O1 l; [
兼具VOR(甚高频全向信标)和TACAN(战术空中导7 K0 Y2 p B7 `1 H, l) a
航系统,或称“培康”)两种导航设备的导航台。" R. n, i4 i3 l9 V
涡流控制器,2 x/ f% V! [6 z4 A9 r0 H% D( F# ]
发动机短舱上,用以改善短舱和机翼前缘之间的气流的" D7 O; ^5 n5 i6 d, X' m4 }! X3 x! T7 w
小翼片。- c' w/ C* ]) H h6 m9 U" J
英汉对照民用航空词典B OEING, B% l8 U" ?5 p% J( h' Y* a7 Y2 O
TECHNICAL DICTIONARY 168! v2 ~5 A, P9 o
VORTEX GENERATOR, Small metal airfoils, located on
4 \% @* `/ U4 Twings and fuselage for delaying separation of the air
$ r: L! I* [7 ?ating local turbulence. G0 F/ u4 a# [8 n/ H
ortex).3 R) L, V5 Y0 X
35
4 ?9 [4 ^8 l V ustall speed in the landing configuration." N* g) A( _( O, l: {( I
装在机翼和机身表面,以在气流中产生局部紊流(涡" [2 F) k6 S7 N+ ^( T' k- X( K
流),来推迟气流自表面分离的小金属片。: o" ~5 m+ p& m7 P
度),1 N, z4 |: d1 q1 H$ O
在着陆形态时的失速速度的1.3倍。
& F7 a8 j3 t8 A) B见Vertical Track5 c, g6 k4 F1 |: K- N
flowing over the surface by cre
0 }2 t/ I, E; r* c(v
( {5 `' V/ P0 S M8 U4 O* t# mVR (ROTATION SPEED), The speed at which aircraft
+ j$ A$ ?! g( r: X2 j6 V/ y0 zrotation begins in order to achieve a speed of V2 at5 G' i0 G- {8 U# [& ?% E+ M
feet above the runway.
; a) b" s" j' H9 XVREF The reference speed at the 50 foot height in a% U$ L' h) ?/ l; o
normal landing. This speed is generally equal to 1.38 v% l7 L& l7 j' O( {
times the
' x, R& `# q2 {( h! ZVTK, SEE - VERTICAL TRACK
8 J4 x. u" D4 w: Z; P5 V8 o涡流产生器,% J* p) N1 z7 n1 E4 V
VR(抬轮速
6 G2 c. m4 x9 z在该速度下飞机抬轮开始以便在跑道上空35英尺时达
: ~; _$ ]. A4 U, e7 j T, s3 `到V2速度。
2 u- `8 P( B) `VREF,2 P1 J2 Q, g1 J$ D) }! h9 _4 W7 a6 [& s
飞机正常着陆时,高度50英尺时的基准速度。通常是飞
6 h+ w5 H: K5 b" A7 D$ o& M机
- L: ~! L5 i$ i4 l8 V; f垂直航迹,
- p) q' b6 f" d( _$ v. X+ Z! C7 l.. i! u( l. \6 V( D5 O
英汉对照民用航空词典B OEING+ `* M% j& f5 c+ k4 N d
TECHNICAL DICTIONARY 169- O Z, v+ J+ u8 g; s) j) o
W
$ U9 T! j d' W; K: WWALKING BEAM, A mechanical component attached to: t4 ?/ t: `5 a' c: P
the main landing gear and a hinged support which helps
8 _& y) V- }* t3 }the actuator during retraction of the main gear.2 s$ w" Q$ u& n
ATER LINE, A horizontal reference plane along the
- e0 @1 A5 Y$ r( Ufuselage for vertical measurements of the airplane.
# P, ^) M' V0 Y& K! p; }8 \WATER SEPARATOR, A component in the air) D5 w8 n) G. w- l: O
onditioning system for removing water from the air
1 ~$ u1 X( e& C" w0 P) d1 h动梁,
$ Q9 z& k' t3 l8 c$ l主起落架上,一端连在减震支柱上,另一端连在铰接支5 N T/ I4 m; E% r; {4 ^
撑上,用以协助作动筒收主起落架的机械部件。4 U/ V6 k( c0 {! T
线,
; @$ P6 ~5 u# _5 s9 n' u沿着机身展向,用以量取垂直方向的距离(或长度)的
7 t+ L7 Z4 J9 y' w, G水平基准面。
# t- H' J- x2 g, Q8 H, X: O水器,8 c5 j; t! N8 ~& I
空调系统内,用以在空气循环机的空气下游除去空气中+ L9 [) R# c: V2 E
W
# B" `5 w9 C6 f' j" Zc
9 t: `2 p+ g, f4 O; I: bdownstream of the air cycle machine.1 |: i6 n4 q i( {3 V
水
- [8 H: p' V& U! N3 `9 t除, A1 u0 D8 l( M) x1 h8 v
的水份的部件。' ~. j1 r- ~0 N9 B4 U& U
英汉对照民用航空词典B OEING
- u1 r6 P0 T+ f" `TECHNICAL DICTIONARY 1708 l* p C" {2 w# E9 f) p4 H
WATT, The basic unit of electrical power.
- k" Q8 W7 F) W! N9 j UWAYPOINT, A predetermined geographical position6 Q2 x' ]2 H. y
used to define a route. The waypoint is usually defined, y( U) |3 X1 _6 w) i
in terms of latitude and longitude.
. C' T. L1 S% p, S3 b: VWEB, The portion of a beam or channel that has been5 d7 a* g" _/ E+ Q! y
installed between the top and bottom flanges. Its prime3 G: ?# d( [. }6 Y$ u# U5 H- ^
purpose is to furnish strength.* J0 i3 G5 B' Z! ?8 h. Z6 j
WHEEL SPIN UP, Rotational acceleration of the landing
- D8 Q0 d% `2 if the% Z7 P! q3 X* b* H
nding gear (undercarriage) after retraction.& Y5 w$ ~. _+ Q2 [& E
电功率的一个基本单位。
( O% {2 r1 f6 ~9 v' Q. r* O位置。通常用经、纬度来表示。" f g) v1 K+ O+ M
腹板,7 m& v2 ~/ {; q* D
梁的横截面。常见于上横梁与下横梁连接成工字形。主1 J/ ?# {7 I7 [& |4 Q+ m
要作用是受力。
+ j2 v/ A# C3 x4 B! i( p0 s% D9 ^" w+ D轮加速,
3 U r$ ?+ D: c" K& G* u飞机着陆接地时,起落架轮子的旋转加速度。8 A( [- u- x5 i% A2 D
轮舱,
- ~/ Q; ]0 C* }# ]. d' H7 k9 o& `飞机的一部份,用以在起落架收起之后,收藏起落架的 Q# E8 z/ O' e& G! }
那一部份。2 Z% U! Z( \0 c1 Z( L6 `- y
gear wheels at landing touchdown.
! K" s8 ~( ^6 V+ }5 w$ `* XWHEEL WELL, A part of the airplane for storage o7 q0 F. ^3 `% v$ I9 p
la
0 J0 K4 }9 N5 G2 w8 X) z) d瓦特(瓦),8 y3 X4 [) @' [& e+ G
航路点,
' E( \1 {- l- ]7 Z* `; w用于决定航线的预定地理/ N! I4 _+ f% a. E) f. F) d
机; _+ d& z3 z5 W7 i+ T$ F4 q: T+ N% D
英汉对照民用航空词典B OEING
8 m9 ]! j8 d9 V/ z0 y. t, HTECHNICAL DICTIONARY 171
6 f: _$ P9 Y$ Y. DWIND COMPONENT, The effective wind relative to the0 Z* |, y* x: V0 |
horizontal axes of the airplane.
3 c0 V! f6 k$ B4 m) AWINDSHEAR, A change in wind speed and/or direction/ r" f' g( c v
a short distance resulting in a tearing or shearing3 s2 F5 e5 C4 J: R
effect. It can exist in a horizontal or vertical direction and
( D0 p' `% Q+ K% z- O- g' Soccasionally in both.8 T1 {. N: P. L0 Z
WING CHORD PLANE, A reference plane from the tip
# ~0 ~; }) }% L8 dof the leading edge to the tip of the trailing edge of the. _! h0 E3 |( m
ing.1 F& G& l8 W! d }# P3 O
ING GEAR, The landing gear attached to the wing
2 A6 s7 |$ [- j/ A) E" vtructure., C" w- ~( c/ K" g7 g! |, R8 I9 t( T$ l
ING ROOT, Part of the wing which is attached to the
2 y7 V" }& n/ q eselage.
7 j% w4 Q; v- _- w6 S/ mWORD, In a digital computer, a word is a group of bits2 | V# ~3 J7 n- B8 v# u' E2 u3 u
with a specified length. The typical digital word is eight' d5 P5 a- V9 P# @, \5 L
bits long.
% Y$ ~9 Q$ O+ k# m风向量,. \; q( o! V% d1 T. C3 r+ H: y( ], L
相对于飞机水平轴的有效风。
* Q& e7 J" b$ r& ~, d0 v- a2 p风切变,4 O1 g1 F& ~, }2 @) \
短距离内风力或风向的改变而形成的撕拉力和剪切力。
1 F0 M, U! R" Q可发生在水平方向或垂直方向,有时会在两个方向上同时& E9 c0 r" _, s# o' b
出现。
# Q2 T$ l5 C6 x# V9 n+ s# r% y翼弦平面,# g" G9 y7 q. z/ n \% r, D* M
通过机翼前缘顶端和后缘顶端的参考平面。: V$ N q! A7 t0 l$ X9 p" n6 C
翼下起落架,# j& z2 m" {9 u8 |3 J+ W% e, h
接连到机翼结构上的起落架。5 w4 [ \* }$ T
翼根,4 P, O7 s! Z u! o
机翼上,与机身相接的部份。
- [6 I6 T- q' `字,) h/ k1 P( Y/ I, `3 m6 ]
在数字计算机中,一个字是由一定长度的一组字节所组
: Y* }0 ? o* j) Y* P成。一个典型的数字字,有8个字节。
; ` ]/ M$ R* `( \5 jin
8 f+ a: n; L2 B' Y" }w
/ i3 }; o2 y8 ?$ X7 zW
( U* r: \" u7 l5 P3 B/ js+ ?* X$ }1 l) A4 B7 x6 g
W# @ I) u4 N4 u( A8 C2 [
fu
m# G2 } Y( d `' \& I英汉对照民用航空词典B OEING
( I) f+ P/ w: E7 M; q' J% _TECHNICAL DICTIONARY 172- f' F% Q% A1 ]' M
WRAP AR
5 E, h4 e1 s, @. }% xcomputer's" C5 a; |4 s9 g9 ` k N
OUND, A BITE test comparing the
; w5 [4 h+ `$ ~6 s$ ?; ~9 F' Qoutput signal with an internally stored value.) a8 w( [. E i+ q6 d4 _, D" m
XTK, SEE - CROSS TRACK1 }6 ^7 A1 Q8 B6 ~+ O; G, q
AW AXIS, A vertical axis passing through the airplane
; ]: U! J5 ` o. H4 A3 \, D3 Ofrom top to bottom. Airplane left and right movement
+ Y/ y. a3 U9 ?controlled by the rudder. (See Vertical Axis).* k: p% C. R0 Y9 D, j& y+ L
AW DAMPER, A system that is used to move the
5 [* v6 X/ v, W; W: ]$ N! Zdder a small amount to oppose airplane yaw.
( O( A& T1 m; y; ]/ Wes- \5 h0 T% C* g
回测,2 R, u6 i: D! `0 G9 n
自检系统对计算机的输出信号和内部的存储值进行比
0 ~. l o9 w9 l) ]! {" E较测试。
% H' p/ a0 m1 i* R, e% W1 _交叉航迹,+ [' v- W" |$ ]2 O# y7 f
见Cross Track
d; m* r' V* fX
5 B. Q: Z1 B! q.
2 [; D7 a% E+ G1 h( x& j! Y/ C# N偏航轴,
; R; ~* ? ~. z* k' }5 o* ^; A E又称垂直轴。由飞机上部通向底部的垂直轴。飞机绕此
9 w" @% b8 W5 p8 V' x; Z) Q0 p轴运动即造成机头的左右运动,这种运动是由方向舵来操
. V) k5 A. l ?2 b) p纵的。% N% L$ \& S5 J; N
偏航阻尼器," `, M* @& K# \: g
用来少量移动方向舵,以抵消飞机偏航的系统。1 W7 [. [# B. t
飞机绕偏航轴运动的速率。
3 ?( M7 s( u7 i: tY
8 F) {8 j! U% G8 s: n4 y) n4 uY
+ g G- W# u; L* dY
. c2 `9 O. C" _) F3 Y! O: dru- i9 [2 w" V# z/ z8 T- Z$ z- ? y) h9 m0 Y
YAW RATE, The rate at which the airplane mov
* s/ K" C$ k0 Earound the vertical axis (left, right).& q5 p" Z/ t$ \3 H
偏航率,
# L# f% Q t7 c6 S* m% H' T# n1 M; V英汉对照民用航空词典B OEING3 E" R1 c, j* `3 h
TECHNICAL DICTIONARY 173
- T9 v) G5 Y9 y7 v/ }) c; K1 D( @Z+ P' a) g% ~1 _* |- J5 R4 I9 W
ENER DIODE, A special type of diode which, when4 E# N8 D; D$ ^5 X) D3 A
ZERK FITTING, A device through which oil or grease is
; c! T2 o, P6 {upplied for lubrication of moving parts.
3 @3 G# {- D- z# u; J# ]4 F7 N/ WZFW, SEE - ZERO FUEL WEIGHT
' U h9 y. i7 eZERO FUEL WEIGHT, The maximum allowable weight
5 X) r u# Z8 B0 g" Pexcluding usable fuel., T+ r$ a) w( I7 x$ g8 x2 _# N: t- f
纳二极管,
! q+ l' Q5 W- ?( D" s' t/ e又称稳压二极管,是一种电子装置。正常电流可通行无+ s8 W- P \3 e3 a+ T- ^
阻,但反向电流则必须在电压达到预定值之后才能通过。( O6 ]1 }, N6 O6 \& T5 v" K H) Q
在飞机电器系统内做为调压器之用。反向偏压时,它有一) x5 W. A; p. q1 t T
个恒定的电压下降。- ^" b& D6 m# N
ZERK接头,$ e Z) M# K* T, k/ a1 z$ [" s
ZERK公司出品,用以接收滑油或润滑脂,以润滑活
; M' q5 x; L" G# W/ t7 ]动部件的装置。0 m9 R0 p2 r6 K% n8 l i6 D
燃油重量,5 N* z& o4 g; J+ W' _; u# k
见Zero Fuel Weight' L) {8 h9 `0 n8 M! M/ g; J H
Z: A& n6 Y+ J' i8 H: ]* ]. }; Z
reverse biased, has a constant voltage drop. This& X/ u7 R* D5 P0 V
property makes zener diodes useful as voltage& _! r. N3 C" G6 S1 r
regulators. i; o E* L4 K
s$ c+ f* q+ t7 C. p7 D& H: U7 D
齐
+ B. f, s' z% ^无
) t: B# i9 G, U% i$ p4 w.8 B9 S5 K& V+ ^
无燃油重量,3 F4 R! X/ D8 ^! h
扣除可用燃油重量之后的最大允许重量。 |
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