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airspace of defined dimensions within which Flight
+ c, h7 W2 P, L" y8 jInformation Service and Alerting Service are provided.% u) G; T& `0 F/ S" `' S" F
F
3 U: s8 Y* O9 c1 I) P- }2 bd8 v; f/ ]6 L4 F% j( N
F( \0 T9 z# {* w5 o, `. \: C
in. S- }# S4 x# \1 V4 t5 W( W/ {
a
( G. q, B7 c& s4 I" x7 Y3 r" @F
U# y6 T: D1 k0 E" Ws
/ v2 x6 }+ Q# U7 u4 Y; b0 H9 Os
* o) E7 y' Q( p$ U9 Q飞行指引仪自动显示(FDS),
X$ M- B2 D: C! K6 A当飞行指引仪的开关处于关断的位置时,自动显示的飞
9 S: g- L% M0 G9 Q# J9 [2 f行指令。
~, f' O6 K9 l, o. q. A' ~+ q+ g飞航情报区(FIR,UIR),
, A- A$ Q' R. h8 l: a+ V6 H一个有飞行资料服务和警告服务的范围: M% ~) E1 a: ^" |2 F$ w# I" U; Y% B; q
度层。' Y; \% Y8 Y8 q
50表示5 u1 P$ u: U9 P) y2 N
显示自动飞
5 P6 R- `' [7 W# g. ^5 j0 O英汉对照民用航空词典B OEING
% |" L( @" B& wTECHNICAL DICTIONARY 644 ~2 r% V5 i% u7 K6 C& s. y
FLIGHT SPOILER, See Spoiler.. W" H$ d0 T4 I: C( B0 c( L, P
LOAT SWITCH, An electrical switch which opens or
- ]6 X' _0 s. ]" O2 m0 kloses an electrical circuit depending on fluid quantity in% x- Y( y0 }/ [: t/ x. B
e reservoir.9 F' ^) V# E* ^. g7 n
LIGHT TRAINING DEVICE: Any device having a full" x4 `( r. A8 f& ]) l
cale replace of instruments, flight deck area or an& @2 [2 G! d, ?, m: F
nclosed airplane cockpit includes the equipment and
- B9 W, N, S$ g% |3 M4 Urograms necessary to represent the airplane in ground
/ l j0 G2 E7 t' Ond flight conditions.5 v# ?8 y' M& I$ F2 W
LOAT VALVE, A valve in a fluid reservoir which opens
a8 V- h O8 Y5 l3 q' W3 i/ ^( and closes an inlet or outlet depending on fluid level.
" {9 p1 q$ I" ~, h5 WLOWMETER, An electrical transmitter for measuring+ q) K1 |2 G- k1 u" i' s- @; U V0 g
the engine.% A8 d6 c9 G' E
LUORESCENT LIGHT, A light emitted by a gas filled
8 M6 y8 A( O. ]* Z# C飞行扰流板,
f) X' o) B. S) ?( s7 N# y9 ]见Spoiler.
/ B s9 v5 n1 ~" u# ^6 K" d浮子电门,
+ d8 @# O$ Z1 i$ M7 O根据贮液箱内液体的量来接通或断开电路的一种电器
; X0 I) I9 o( h6 ^8 p. q1 u, Z开关。) t/ m' `6 s9 l, f u
飞行培训设备,
5 D* h9 r! Z1 m/ O仿仪表、驾驶舱区、或封闭驾驶舱的任何设施仿真装置。
- g e4 n/ m0 D# C包括可体现飞机地面和空中状态的设备和程序。
: O8 K$ w3 B! D- g* i浮子活门,
3 w& m0 Y- n8 _- M! Z5 x4 |& \装在贮液箱内,根据液面的高低来开启和关闭进口或出
/ T# E8 D* C+ y- r6 f5 @口的活门。
6 T( Z0 F2 O/ g) D1 x流量表,
# T, J/ j" F+ k用来量度流向发动机的燃油流率的电传感器。2 b) S0 E2 z) W i, Y
萤光,
) Q- k: B" _& c8 j0 ^/ @) y& j由一种特制的充气管所发出的光。
1 z1 _- K- F p h! MF
5 A" c F7 s. [) m5 ec$ Y6 g+ d( A/ g8 I+ I/ q' c
th3 F6 j+ o3 q% U7 P
F
4 j: O( l8 A: `- [9 u. Ns
6 z9 l. h( _( M" s3 k oe/ z8 n+ a, z1 D) e& E
p
! v9 J1 P' ^: Ma2 |6 e) d" ^: W! C6 H C( ~
F
: A; i4 ?, _8 x1 B- Ua
& E# b! q1 y$ j( z( F& S+ uF6 o4 d2 u' Y$ V. t( Q
the fuel flow to+ w* B% r5 h7 A& j/ t
F
}" {1 A, I+ \+ atube.# {2 ^7 T2 W7 Q7 _$ w1 K) B- A) }
英汉对照民用航空词典B OEING
+ P! U, N H! M5 @7 q' k+ I1 O0 ^TECHNICAL DICTIONARY 65
5 J7 F c2 e7 m! }9 T- RFMC, SEE - FLIGHT MANAGEMENT COMPUTER
) J& g' q% p8 O0 w/ hFOD, SEE - FOREIGN OBJECT DAMAGE Q- o$ g% g6 M& @4 y: |4 \+ f; x6 ~
ORCE BALANCE VALVE, A valve controlled by the# s8 y/ B. u: V4 @. U
OREIGN, Offside; opposite side.; Y, N3 v4 G, N! S- {
OREIGN OBJECT DAMAGE, Internal engine damage
- H9 u! J3 Z0 c/ j6 tue to objects entering the engine air inlet.
7 n! s5 x/ Z# w3 WRM, SEE - FAULT REPORTING MANUAL
) w2 q0 H0 D) K$ ~+ B% rUEL CONSERVATION, The activity of planning flight
5 F6 h) b) p. l3 s, v/ ]4 B0 }ltitudes and cruise speeds so as to minimize fuel
8 ^- ~ S4 n+ D ?1 d, Xonsumption.
- ?0 A3 i; t2 [) u9 b# _UEL CONTROL UNIT (FCU), A component on the
" x& u! f) q( ]" t& {5 d: J, Pngine for controlling fuel flow for starting and engine G# E9 E: K6 p! ^$ C1 Q! {
F
) W7 @* P f+ t6 e% Afeel computer in the elevator system for hydraulic) A# d$ M- Q, u5 ?
pressure supply to the elevator actuator.
2 s R) d* h$ K% }3 z# mF
) Q9 u/ U" }% S: h1 DF
% F6 G( F( Q( p2 T+ \$ E' ]/ Qd
: F4 u* G/ N3 O. r( C. i$ x( a% z- D4 {F" k4 [- Q" | {; ^( ]8 _
F
+ j3 S1 \3 @8 ]! Sa+ ~- g. w# O$ `
c
: E$ Y9 e5 S" A6 n* HF6 Z6 k- s& R. U3 l, S! p G# Y
e9 s8 J" p8 z6 u! ?0 z: q
operation.& E) @% U% n$ ]
飞行管理计算机,+ x0 z3 Q2 U7 D
见Flight Management Computer.
& ?9 v2 B/ H v( i) N H! J外来物损坏,
+ `5 S4 J# {* F% b8 yeign Object Damage
# U6 h$ U$ U J% x* m- q见For .! y6 u. \6 _+ Y1 Z9 I
平衡活门,
: h% v8 y- ^; Z/ @- Y内的感觉计算机控制的活门,用来向升降
" R% E& i- ^; T% g; Z8 x外面的,
5 d) S3 G! b3 ?8 Z: \9 I另一边的,对面的。- t- |3 a1 r6 h4 |6 M
外来物损坏,
# ] _0 Q, a/ G' i; [6 a$ _. B% S由进人发动机进气口的物体所引起的发动机内部。
& [! ]; N% d# N. p! [) I故障报告手册,
. \4 c1 r% B. S8 U: h% L9 n见Fault Reporting Manual( S" H) Q* `; B* u* o+ \. E" }
力$ z4 W) _7 L5 @9 B1 |
由升降舵系统' ^/ ]" m0 U% o
舵舵机提供液压力。# ~ F4 H7 S0 B! P
损坏5 e+ P) O0 C9 n4 |7 x
.
; x& e# ?3 Y; C" Y) h+ o8 ~约燃油,6 S$ O% { g7 |+ w* T, U+ X
为使燃油消耗最少而对飞行高度和巡航速度的计划。, i" {. N) R" O& C
油控制装置(FCU),
( V' F9 K. G( Z4 P发动机上的一个部件。在发动机起动和运转时控制燃油
5 {9 \& H, w2 k% z' a) R. [, i节. U. d0 b) i1 ?2 ]. }5 b8 t
燃4 Z/ a2 [" M7 P( o( C1 C I
流量。1 |1 b. U% ]% f# [, K' v( I
英汉对照民用航空词典B OEING
' [% s: f: j. s. l# G* _& T! \! B9 NTECHNICAL DICTIONARY 66
" h6 z/ K/ Q! }+ [; v* b w- ?3 \FUEL FLOW, The rate at which an engine consumes
1 A0 o5 c4 R4 t: w& aUEL HEATER, A component on the engine for heating$ F5 R, b( h( m0 T1 l
UEL JETTISON SYSTEM, A method for reducing$ j1 X/ S. G4 Q. Z
e
7 G- }3 q7 p7 ~: XULL FLIGHT SIMULATION (FFS): A flight training
! U ~" Q2 M9 z% Y: T. `+ ^evice that incorporates full visual and motion systems: j2 O e/ w" J2 U9 l- G
nd specific model airplane.
: I7 G6 {5 N0 l6 T' GULL-WAVE RECTIFIER, An electronic circuit which
4 N6 k0 }# T5 u9 l& H9 nhanges an alternating current signal into a pulsating
1 l6 T4 {9 d. U I# d2 iirect current signal.! g* k3 B O1 G. w! p3 }; i6 J Q
or
2 q7 T/ M# I1 U, H. [AGE PRESSURE, Pressure measured in pounds per
; _) i# ?* Y* AGALVANIC CORROSION, A form of corrosion caused% `8 B/ \5 V& V; P' N( w$ S' K
by the contact of dissimilar metals.2 G- G5 K6 U# l7 U
油加温器,' R x( ~, U! e& D
热燃油以防止发动机燃油
9 r: S5 ~4 y* s4 |' [" W. W6 d% v急放燃油系统,/ i6 k* O0 V: i# k) ?- i
中的燃油向外排放以减轻飞机重量的$ I7 T! a3 _4 T1 B! N8 a* U) Y
动飞行模拟机(FFS),; h" a) z9 @; L# \, U$ l
一种飞行训练器。它综合了完整的视景和运动系统,以
- ?2 ?1 b C# a具体的机型。
# O: u' j7 x+ M+ ^$ C5 R8 k波整流器,
) C% k* I; _6 B9 z2 B用来将交流电信号变成脉冲直流电信号的电路。
! u1 c/ g3 i) ^$ }压,
) _8 h$ u6 F5 g1 |平方英寸若干磅(psig)磅/平方英寸的计3 f: s% F6 n1 [; U* b- `
电解腐蚀,4 e. Z+ \4 R/ K% k" Y' J( v5 k1 D
一种由于不同种金属的接触所产生的腐蚀。8 S$ v7 ] M& {" J
fuel measured in units of weight per hour.) n- M' [' `+ X j
F
, Z, m4 J% M5 \) b" {fuel to prevent icing conditions in the engine fuel5 e8 I3 t* P" A* i
system.- C) W; D3 F3 O4 x* n3 H7 f" v7 `8 `
F1 o# n7 T. Y A! m5 X
airplane weight by discharging fuel from the tanks to th7 ?& w3 D9 u! [( ~9 p
outside.+ I6 X/ e* `# Y( @4 h3 J
F
6 B3 N; u, J: v8 W8 z4 y6 T F, g' vd
2 U5 ~' E- |" I1 xa/ [9 S( s) U3 L0 `3 `* h& a
F
" D/ z$ ]+ m% j X# ]+ C& t$ U$ rc& k: s/ ]" R- c% f
d
. N! c& ?& |* W K. vG. V3 W: v, s4 a+ N( B- x5 C
GAGE, A component for showing quantity, pressure,
, E4 _9 {8 m D5 Etemperature by a pointer or numeric display.2 p& m g# \6 }$ M- d- u% j
G
& R, c6 K# C+ H3 C) y4 s: M0 fsquare inch gauge (psig).8 n: ^$ w2 B, T3 D; G0 e3 w
燃油流量,
6 O: p6 W5 g' }发动机消耗燃油的速率。以每小时单位重量衡量。; W5 z; }- @) {' g4 S, ^
燃* [9 M @4 J- Z9 I
发动机上的一个部件,用于加2 L1 A. P# A7 C4 `
系统结冰。0 L& k: k2 @$ [3 _/ Z8 D, V4 a
应" V# q* q, {/ A( ~
一种通过将油箱
5 a0 t! n$ e+ \) F2 _方法。) g( \! G7 I/ s( o' H
全, h8 Y; z, j" B- j% u& ~
及
, Y9 N+ X! w' M w全7 F% Q( h, f' {2 G7 `
计量仪,
$ d7 p& K7 g* F由指针或数字显示出数量,压力或温度的部件。
( |. Y1 z6 x: Y" }& w! E表
' Z0 T* Z5 ]9 g. R3 {单位是(每: s$ b$ s- s+ u. v
示压力。# A+ P& V6 s7 e5 z5 M/ J$ I$ u3 _$ |; u
英汉对照民用航空词典B OEING
+ W) S1 _& T. b1 S$ O, DTECHNICAL DICTIONARY 67
2 t# o" p9 l& SGASKET, A seal between two flat surfaces.
, v, K. S' b! _* @$ R4 lbe individually controlled for the amount. F# r& f7 o) X: ^
nd direction of supply.
6 }* [9 j2 _* j! `* v; hATE (NO. 1), Airport location used for
$ j; b# P. u# d; T, r# z; i+ U& i+ Cading/unloading passengers.
% @ ]9 ^0 y7 L& e5 f* G2 L& CATE (NO. 2), SEE - LOGIC GATE, U7 J( T" p7 n7 m2 [
ATE VALVE, An actuator operated, sliding device in a1 C3 U% b4 E0 P P5 X0 `
uct for closing and opening the duct passage.+ r3 D |' Y2 |, g( O- ]
间的密封物。7 f& |4 Z" k1 Q# m+ b1 o; _
调节供气口可控制空气的量和方向。1 H: i- Q) g6 v
登机门,
- A& K, F: [5 [9 L. p; p, N: D0 p机场内用于乘客上下飞机的通道。* W; t/ F: W! |. K# j
逻辑门,2 F% o( c- u& I6 ~( k- i
见Logic Gate9 N6 i& \/ S* Y5 w W2 a
GASPER AIR, An individual air supply for each& M# O$ O1 x. v% [4 R9 D& R
passenger. The air outlets are in the Passenger Service
2 o% f$ }8 j, g$ X; v$ b% p4 CUnits and can
# Z$ h1 o5 N( D' r6 s0 _' [' @a
1 b S. u( M: M5 V: [3 ?G2 k( S% n& d( X: ?( E
lo
# q8 c4 F) y0 i- P8 BG
- H% b) t* H& i KG
* M+ q, z3 Q- e' w% i! C( D2 z$ \* Xd
; u& @6 @( z8 o# o' {密封垫,
2 ]2 Z/ |' D7 e( J6 C$ E两个平面之& C- }9 R. ?4 E
乘客用空气,
* o, Q* X1 O* c给每位乘客的单个空气供给。供气口装在乘客服务设备/ M$ O5 J; ~9 Q7 ^
内,个别
; E: C# C" J/ x) p# I, Y.
$ ]( X9 y% X' E4 g& U0 ]" k, p; y闸板活门,
/ \( F5 L6 m6 Z管道中由作动筒操纵的滑动装置。用来关闭和打开管道: e* I' u; d7 R- M. g* ~. C- A
通路。
3 g8 u' p- E- {# n' e7 |' A英汉对照民用航空词典B OEING
4 ^' L7 u# G, u k6 P A9 L" mTECHNICAL DICTIONARY 68
X) z# X( v/ G% R+ N$ \% nGATEWAY, A functional unit which connects networks
, `1 d0 P2 b5 x# i* rr systems of different data formats.
. P) f5 _0 ^6 R: f F! pRS.4 \& k- x9 U# X8 J* U
ENERATOR, A mechanically driven device for
- I) K- ^+ b" ^0 r7 |' @2 V5 X) jENERATOR BREAKER(S) (GB), A device which will
" m) \0 x0 w7 w/ ztor from the
, I1 }. w0 \! Q* Tlectrical bus(es) it powers.' o& @+ @: h' |) E
ent with3 s7 }5 j* R, ~' d, i0 H
o rings pivoted on axes at right angles to each other1 X r- r! C# H7 n/ Q
llowing movement in two directions used in the flap
. x# _4 v' H9 k5 Rxtension and retraction system.
4 I- L! Y2 W! Y9 k" F* Q& Y接在一起的功能
/ x8 D0 S) c0 t4 Q件。
4 ]6 `: l6 ~' }5 C# `9 ?/ Bo
' q. P8 I, l0 P0 U* a: TGEAR DOORS, SEE LANDING GEAR DOO
. U: j. t9 \ i; h7 }! X- qG8 a% ~; U" g. `9 I* u0 z8 r
producing alternating current for airplane electrical
) A2 s1 T8 g2 v" J% ^+ |system.* O ~( K V# Y* |4 G
G
! j8 e9 u+ y1 L) B- Q/ B* u: A5 q- P6 A& }separate an electrical power genera
9 a1 M( m; H" S: h, We
( Y) s$ k: ~( I ^. x# Z# U6 NGIMBAL ASSEMBLY, A mechanical compon. ], G' ?: p9 c) F! m# ~
tw8 N- G. j0 P0 G0 `
a! g0 K- n: E# P% r( P+ E) c; \
e0 }) j8 M4 r# y- g
闸门,$ t, X+ ^! A3 l1 ]) M% b1 V
一种将数据格式不同的网络或系统联
- {% Z7 y; x5 `" K. f1 p元* z: N2 [0 E; y) c& h
起落架舱门,
?* i& O2 b, Q见Landing Gear Doors." S2 T8 X4 Q% ]0 ]& `" ? ~! U
发电机,6 Y- X# B6 |3 n/ E4 b" t9 a
为飞机电器系统产生交流电的装置。. C @- R; `3 ~" o% [# U9 h0 A, _! s; S
电机跳开关(GB),
# H9 L# {9 `5 e$ ^& s7 `机与由它供电的汇流条断开的装置。
7 q6 p; w8 x" {( W; Y! w襟翼的伸出和收上系统内的具有两个圆环的机械部件。7 }% u7 [/ q& s' h* b2 g, Y9 Z
个圆环的旋转轴相互垂直,以使部件在两个方向都能转( U1 k( ?1 ~: Q$ ]- k! k
。4 e/ d) s5 G0 i# e
由机械驱动,
8 V' m; e; H9 k. P& [发3 e5 C9 m% u1 e* t& t! X; `* ?1 X( l
能将发电
+ V. t; p, M9 _, u万向架组件,: R5 X5 ~4 k) L6 K c1 g' D
两
: Y* q, Z* l$ z1 l" L9 a动
; n8 P# O; @& L) M/ o8 h英汉对照民用航空词典B OEING" _5 P& o4 d& l' d- _. m) b6 ^
TECHNICAL DICTIONARY 694 D3 [0 `% k3 }. X; H
GIRT BAR, A rod attached to the escape slide which* ?, J+ o) A. @% Q {* s" w
engages brackets on the floor for automatic slide* `0 q9 J4 d, H4 \
peration when the doors are opened.* |/ v" K" Z! }. P2 x3 b
LOPE (GS), A vertical path defined by a- T7 | M4 Z1 o9 N( [* Q
ased electronic signal used by an airplane or
3 \9 z" I3 b8 y' |( B7 D+ ELIDE SLOPE/GLIDE PATH INTERCEPT ALTITUDE,
2 P7 h' ~) u* [( m8 Hhe intersection of the3 a# j, t2 J6 q' {
ublished intercept altitude with Terminal charts by the
; W6 F; C. K {% H( x6 e( n) Wtart of the glide slope/path symbol, is the precision FAF;
8 Q: X8 ?" g8 A; D3 Towever, when ATC directs a lower altitude, the' H# |$ d7 [; Q/ s1 B# p' }
地
# [2 E H+ w1 I% x D上之锁钩相齿合,以便滑梯自动工作。
3 k7 @* U6 u* i/ V滑道(GS),
1 Y3 Q, `2 p& Z# e* B- \. R由进近或着陆期间,飞机或飞行员使用的地面电子信号& f- a1 l7 ?- L& g- v# h: {
垂直下滑航道。
' s! B2 ]0 h6 |+ f滑道/下滑航径切人高度," s& P. V2 s3 v4 f. U `
进近时切人下滑道/下滑航径的最低高度。在
; r3 g6 H! I1 r( Z m8 {最后进近定位点。但当空中交通管制指挥一个
& s& D: }. s. Z; D8 X' p低的高度时,由此产生的较低切人位是最后进近定位
$ X( a4 Z: I8 L。
& t( Z& u( R$ m/ V/ G) R1 ho( |! ?/ ?) @2 Z( L6 i9 r
GLIDE S( x& K: f6 d) d# R
ground b
7 O6 s3 S9 o! T8 Z J7 _7 }8 Zpilot during approach or landing.8 E3 G B* {5 D9 g& l" C; K
G
5 n/ ~# V- p7 e0 AThe minimum altitude to intercept the glide slope/path
- h! L0 e# e$ K/ U7 M6 w# \( [on a precision approach. T9 k; k$ D7 a& P( v
p6 l: f5 H z9 V9 `2 R, B0 S
s1 u0 g( w2 {5 h/ N3 C
h
) u( K6 a8 \! u. n- p0 |& H8 A/ Iresultant lower intercept position is then the FAR.
; a! t+ m1 q, T Q5 m/ h. h0 c束缚杆,( h2 l' h. y& m$ u
连在逃离滑梯上端的杆子。在机舱门打开时,与机舱9 ~2 @7 r0 p) t3 ~! q# R7 H7 Q
板3 ~9 v6 F' J$ e8 r0 s
下7 [4 G+ v, X, f1 I, W
确立的一条. s) Q1 T' Q6 w( @3 S. B5 N
下# r& {' ^1 b$ ~% `. G# n1 d Y
在精密5 Z5 T G% K/ |
Jeppesen机场图上公布的切人高度与下滑道头的交接
* A" ?9 u3 N3 i) e( C点。是精密
[% i+ w, Y7 o* z( `! C. a较- T( P/ i' g- a* N
点0 Q1 ~1 S% k$ K4 I8 {% o' w8 v
英汉对照民用航空词典B OEING- R c0 \, z8 Z8 d" r) b$ ^
TECHNICAL DICTIONARY 70
: V- v' N# z( U3 JGLOBAL POSITIONING SYSTEM (GPS) (No. 1), A
h0 ] j5 E" w# \4 o+ upace-based radio positioning, navigation, and d9 ?& T; E: ^) Y+ C+ _+ S: y
metransfer system being developed by U.S.A.: j) v& n) r& e' U; G
epartment of Defense. The system provides highly( X, h; y% Z9 G4 a, l8 p8 l
recise
( F( @3 X& d6 `2 H" jnd provides a worldwide
" V6 J- m8 F ]$ \% b6 W, n7 gommon grid reference system. The GPS concept is
' k! k, q" A; P! U* r& _redicated upon accurate and continuous knowledge of
9 T+ ?3 u" J8 [: t4 I5 ve spatial position of each satellite in the system with
7 c& D: o5 ?! k) Pspect to time and distance from a transmitting satellite
+ v/ Z2 c1 F- D( [+ Dthe user. The GPS receiver automatically selects
# X: ~5 }0 W, Y2 J* j- f% a+ ^+ tppropriate signals from the satellite in view and
( Q/ W' P; ]. X( ~anslates these into a three-dimensional position,( m" |; {7 {. w6 @& \7 y
elocity, and time.
" D& s7 q, J1 g6 p; a* l; o9 ULOBAL POSITIONING SYSTEM (GPS) (No. 2), A
0 Q$ K$ ^5 K9 K# V; V+ y* Tngrange navigation system that takes navigation input
3 m$ w" T% o- S8 J6 m. G; nom transmissions generated by a series of satellites in- l2 I+ w5 |9 ~# s3 O; Q8 h' u" v
LOBAL NAVIGATION SATELLITE SYSTEMS (GNSS),' S* Q1 P4 Z6 r3 K
ternational Civil
# @4 r9 S, F4 n! z5 D7 xviation Organization (ICAO) to encompass any* ~" U ~- z+ x: T; S6 `: D
dependent satellite navigation system used by a pilot
) y7 }, R( l, e4 d |# W- J* e" fperform onboard position determinations from the! R$ R# w8 T. ]
O-AROUND (GA), Airplane maneuver where the pilot is1 D5 ~6 m* X* ?/ T
in the final approach phase of flight and decides not to
: M/ k, ]+ k4 F" A; \$ E. vland. Thrust is applied and the landing gear retracted so2 P8 D4 c. F8 M. e
as to climb the airplane to a safe altitude.0 `! I! s3 q+ \% f) t
GO-AROUND THRUST, Maximum engine thrust to be" v9 ~- \. \2 _
used during the Go-Around Maneuver.9 \ W- C0 a) x% I, f! d
统(GPS)(NO.1),$ k5 I8 ?( ^# k: _7 k0 o) l! N
电定位,导航,和时间转移- c0 G& S Z- S' Y7 U; H8 i e
统。该系统在全球连接的基础上,给无数备有适当设备/ X) o, i! o8 q3 N
户提供高度准确的位置、速度、和精密时间信息。该系
" A2 n' \" |* z3 W5 u响,并提供世界通用性座标系统。全球定
/ {8 v, ]9 H! f+ y信息之原" {: m7 G2 {/ r* |. D' Z& \; p6 Z
为基础。全球定位系统自动从所见卫星选择合适信号,* l; w" M# w& z% }( z- `+ e n
并将这些信号转译成三维空间位置、速率、和时间。
; r1 k* ]% w; w全球定位系统(GPS)(NO.),
5 \6 ?* Y- B8 k8 _: P, G一种使用一系列同步卫星所发射的信号作为导航输人: p" p% M3 R& D$ l% g
长距离导航系统。; C& I6 i: T& H
球导航卫星系统(GNSS),
+ r6 I! t, K6 ]' D" v7 Q+ M航组织采用的“伞形”术语。它包括飞行员2 c6 G1 q7 M/ |2 e; _
料做位置判断而使用的任何独立卫. ]; y% n7 i5 m" o9 y! P j* k
导航系统。
$ }0 A x8 v! B% q复飞(GA),
# v. }7 G* I+ i, l6 J* i7 u: E飞行员在最后进近阶段,决定不落地而做的机动动作。5 ]% e- m9 \4 B0 z0 v
复飞时需加油门,收起落架,以使飞机爬升至安全高度。+ t- V. }2 Q$ D
复飞推力,
" k% C5 X5 V4 b" b7 P8 Q# a* f飞机复飞期间使用的最大发动机推力。2 N7 x1 h6 g- E: E
s
/ v0 t& i7 G" c- W( mti% M1 l5 B2 C b
D8 d$ v5 Y# ^& C9 B/ A; n) i
accurate position and velocity information, and p
) Q0 m6 n# B- j% k) w! `time, on a continuous global basis, to an unlimited
6 t7 b8 ]) @0 k# o1 X/ T, onumber of properly equipped users. The system is
! ]4 V# t; I: a/ `7 k: ~$ wunaffected by weather, a
& i& l" _" m9 i9 w- U1 ?8 rc
: F7 U+ l8 W" n/ ip4 V n" m" P' r9 u
th
2 i# K1 ?/ J' [7 ~: g: A* Nre
$ V9 n& K& b: w/ Y7 c, B% Pto
# g0 g9 `( h H3 ea
9 H F" d9 k' q" n' u" D# `) E5 Z; Htr
, v( ?& w/ d( I1 x% ^/ b6 a4 Mv5 C- p4 F1 m8 S0 M7 ~* t( r
G
; k' D. N p X2 G( {* u0 Q' m9 X* q9 Rlo- s* d4 k3 j7 Q5 B6 f! O
fr7 L2 |0 O' q# n/ c3 o
synchronous orbit./ {0 D- Q$ a. v
G
% K% z" `, m4 P6 fAn "umbrella" term adopted by the In
/ d5 D1 @- W( f; ?9 o* @ q: F% i, OA
$ Y& a5 w, @# w- Win$ M8 Z/ f# r! L1 _& T- A
to, P7 ?' c- U0 Y L! j* g
satellite data.. A. w- ]" |3 Q) `
全球定位系
8 o7 D5 z# @ T7 p. a, q4 I5 a由美国国防部研制的空间无线" i6 D+ L& W4 c, J. D
系
" z$ u5 c3 h" y用) n; Q. F* a2 K' @+ H
统不受天气的影( h, d* h8 A; N( x! Y5 a# W* A
位系统概念以系统中每个卫星具备相对于发射卫星与用
0 c- _/ @$ I& k2 C$ i4 |, i' G户之间的时间和距离的准确且连续的空间位置
8 `, t( C d" y. @6 y6 Z( W( }则
! |. G _% _& _) t9 v20 n: F! h2 i: g6 e# @
的
5 i6 C% U8 U2 e- G全
s9 O& ~! C7 W2 V$ |8 H1 ?% c是国际民7 m4 W( _: Z% P6 e h
在飞行中根据卫星资/ {- x* a+ l( S
星
" P0 P' O6 Z1 q/ N) n英汉对照民用航空词典B OEING
( `7 i, L4 G( }7 U, uTECHNICAL DICTIONARY 710 R2 \, ^. f; d) O9 V' X8 }
GRADIENT, The ratio of height gained or lost in a given
& x+ u E, ]4 F+ xdistance to the distance travelled.. Q5 V/ n' |* C3 W$ u R! l1 a
rbon
. Q: c( E/ c. u6 d3 Ar access panels, landing gear doors and flight/ F. c8 V- t5 h
ontrols.
# V9 a3 x3 Y4 N& _/ v. sIRCLE ROUTE, Is the shortest distance# f( e& G: L. { S7 L. n: u) o
etween two points on the earth's surface. It is the line! k. s$ r$ N0 j6 {' i0 Q
rmed by the surface of the earth on a plane that
' e: U8 H. t2 G) @2 gasses thru the center of the earth, the departure point,; {, k- i' S, b* e# u9 P; i/ _
t line
7 }2 @- G* ]7 d1 V3 e' i2 Fal Conic Projection
$ z) l- v& u, V: X* V4 Ypproximates a great circle route.- @4 [5 A6 R# d- @4 j* i
GROSS WEIGHT (GW), Total weight of the entire0 W- p- {& H% e1 _
airplane, fuel, oil, cargo, passenger, etc.
! t d: o$ T$ H/ Z( JGROUND, A part of an electrical circuit or system that
" n, }, i# Z# jhas zero voltage.
" I5 J6 K3 Z2 X5 {% HGROUND FAULT (NO. 1), System fault that has! B; H9 L' ~8 E; c8 Z7 `
occurred since airplane landing.
) V" J7 \) R6 n& D轻的材料。用以制造舱口
1 m+ }) B( U6 {# O,起落架舱门和飞行操纵面。
_4 V& G, w: @2 n* b5 i圆弧航线, ]2 g5 P! y* W; o; O& e
地球表面两点之间的最短距离是以地球中心为圆心,在! V% I. U( q# H+ B3 z, m
飞点和着陆点间所形成的弧线。由大圆弧航线形成的真' [$ A p7 q4 j; \
迹不断改变。在兰伯特等角曲线投影上画的直线接近大; k: [) _ f$ u' @# O
全重(GW),
7 P" L( f+ s5 m$ M, ]: @; v% a整架飞机的重量。包括飞机,燃油,滑油,货物,和乘
- I' L/ O0 S( M ]客等等在内。6 l- G2 p0 n% g& f5 g- }1 g
地线,- w$ q7 v- ~: n+ V( n
在电路或电气系统中,具有零电压的部份。( A: ]& X) Q) t9 C4 {
地面故障(NO.1),
! K4 s+ a( k, ]/ y E自飞机着陆后所发生的系统故障。
. [; J, I2 n k- z* E q$ {GRAPHITE, A strong, light material made from ca$ w, n) U5 o$ q
fo
" n. ?% R0 K4 sc, |2 _ j# i4 H( n7 k. O" k
GREAT C
7 x4 C$ R8 Q1 P4 }b' T) d2 h* E, o' N g8 F
fo1 F2 I* _9 Z d% ~4 `, I
p, a7 @. E3 |" b
and the destination location. The true course formed by' l! ?9 _/ z! ?/ B U
a great circle route constantly changes. A straigh
) X8 @4 H, J+ G! i* ydrawn on a Lambert Conform2 D' z) ^; ]! Q- J6 d- h4 K0 `( P- y
a
9 M- S1 s& [: S- T9 P+ E7 L3 xGROSS PERFORMANCE, Actual or measured& R# E4 W% |' R# {5 o; D
performance of the airplane.
' Y; }- f+ q" d$ [6 t" B梯度,& f. W5 a3 i' C8 B4 L) K
在给定的距离内,获得或失去的高度与所经过的距离之0 k- `* B8 c$ y$ O
比。$ ? L4 B3 @6 i( T7 {) F* N I# J
石墨,
# Z$ ^8 M( H% t" A一种由碳纤维所制成的强而. l) W0 F! {6 v
盖) [: O& K" ?0 j7 o
大
) C$ _" x$ X7 o8 f起
?) l5 a- Z; n+ o3 {航
) b* H1 {$ I" A, G; b2 N! J圆弧航线。
6 v! g) ?# o, [总性能,
9 \) @* \5 v) t4 H飞机实际的或量得的性能。 e' `- b$ k* K3 |: p5 H4 r- |
英汉对照民用航空词典B OEING
6 b( S! s" D O3 Y' jTECHNICAL DICTIONARY 72/ Y' c3 J- X# F; C
GROUND FAULT ( NO. 2), Loss of a ground connection
) O7 v0 {4 ]( eor a short-circuit to ground.( H p0 k0 |3 X, s: V5 l) Y
GROUND SPEED (GS), The speed of an aircraft
$ S5 h: r9 w4 `8 Y* jlative to the surface of the earth.0 Q N1 y1 W* }+ r# j- d; d7 J8 W
ROUND SPOILER, SEE SPOILER% S6 h( p3 I. a5 |
ROUND SUPPORT EQUIPMENT (GSE), Equipment
* \) B0 D) j6 F F2 D6 ^2 W0 R0 esed to service, test, move, power, or repair an airplane$ W" ^9 a7 X' W& S: N3 K% e
hile it is on the ground. |' C* j' [5 L; u
ROUNDING POINT (TERMINAL), An electrical) W; ? f. {/ q( O
onnection on the landing gear doors for electrically4 v0 X4 z G8 w
rounding the airplane. An electrical connection near
) |; d8 }6 T8 H+ we fueling station for electrically grounding the fueling
\ K& ~2 W4 E+ r" Z- f; k: Gase.! m6 x/ ^! P6 G7 l
S, SEE - GROUND SPEED1 @- | B3 b/ x5 h1 ], ~
SE, SEE - GROUND SUPPORT EQUIPMENT
9 U% d/ x$ R/ f! k ?; ^! zNO.2),
. j5 |% V* E+ W, |. R% w地速(GS),& S8 I. |: u. I$ N m* [
飞机相对于地球表面的速度。
8 n+ r8 j4 ~% m" r' p# n8 A( {地面扰流板,
4 t* n* c; K+ I2 m' E见Spoiler4 A2 w% y6 I: u8 B* o6 p
re
8 i% n* Y/ h0 Q& N2 JG9 i, ^ }! t. t
G3 W! E# ^! ~: q/ P/ m- Y
u% p% Q$ q; h5 q5 U
w0 e1 p4 s3 L& e7 \* V8 g" r
G
6 G+ {* s9 x r7 F/ i1 ic/ [2 D- |0 S7 d) ^
g
& x- h, T( t. K+ c o( R' |th2 W! ]' B1 n; I# e% s' e% ^/ W
b" K# q. c, ?; }3 d) X) p/ G7 B
G+ F6 q. V4 K) i
G
: y4 V. A1 j4 HGUARDED SWITCH, A switch that is protected against* }6 B; q2 {4 G. z) h4 d; ?/ z
accidental movement by having a cover installed/ N0 z9 M& c/ s0 M, y, t: Q
directly over it.
" v4 I" }* _+ q7 n8 A地线故障(
* P, {$ M8 y( U& E( b地线脱断或某线路因短路接地。( e' S) q+ o2 U! D: m
.$ m8 {6 l/ ~8 e
地面保障设备(GSE),; `, i5 b8 Z# z$ e) s; p; w
当飞机在地面时,用于勤务,测试,搬移,动力,& ^7 W2 S% X J- o+ T- b, _
或维修用的设备。
: j6 E! }: f! o! o2 y0 O接地点(接头),* J [: T6 o, V9 _- T- N7 w
是在起落架舱门上的一个使飞机电接地的电接头是在
* f4 h/ @* V% s: l加油口附近,使加油车或地下油库电接地的电接头。7 @6 O1 d5 p2 r0 d- o4 k- K* X4 G
速(GS),
8 }2 D* e$ Y& x, keed
6 p+ t D( \6 U7 o' Q; w5 r供应0 o2 {2 b! l0 i4 D( n- }, {8 x
。# F y$ n" n# i& H4 U1 c. K9 n8 P5 f
地
% ~0 V" J! t, G, ?, \/ ~见Ground Sp .
k5 b% j$ ]8 T, j3 i' r4 A" o面保障设备(GSE),
6 M+ o6 H) y: C' }" y$ \见Ground Support Equipment$ k# H L, I4 _
地
6 B4 b+ o4 C. H./ ?+ F$ `) l* e& S0 O) j
带保护罩的开关,+ R/ {+ c. y- p) i; O2 v
为防止意外拨动而直接装有罩盖的开关。$ Q# |2 H' X; {6 n: K7 A4 \ H
英汉对照民用航空词典B OEING8 g2 A2 L0 w; U/ X. H) ^8 {
TECHNICAL DICTIONARY 73; g# N( d k1 Q! g3 h
GW, SEE - GROSS WEIGHT
. {. J1 z8 c% s D. b) Q( p9 PH8 f& ?- @( H: j; N9 \! @0 J* l7 T4 Z
HAIRLINE CRACK, A serious defect in structure; a! |+ W( ^: A+ T( t# y& r
crack that shows as a very thin line.5 k! p) F- C! z$ @4 i
HARD-OVER, A maximum pitch or roll maneuver.9 E" z2 R6 k& }+ [/ i& \
HDG HOLD, SEE - HEADING HOLD6 m. ^) X- D$ h- V# L
EAD END, In a hydraulic actuator, reference to the8 E9 k3 o% m0 b
art on the piston side of the actuator.; V: i$ B+ Z& {$ o6 E& D
HDG SEL, SEE - HEADING SELECT
) e$ j5 k) Z/ [) c* o7 A* PH
8 K+ q* V" [. q1 n) C/ |* [! gp
2 G" `$ y) U' |1 AHEADING, The direction an airplane is pointed
1 K7 M# |: J' D3 V1 I/ Qreferenced to true north or magnetic north., @: |" |$ T& m7 w+ a4 W
全重(GW),6 o8 K4 d' o# B3 g$ V8 k9 e8 A( y
见Gross Weight.
& E7 b- o3 p, K) G0 T* m" U) j细缝裂纹,9 f9 X4 ~9 |+ E& Q1 p/ O
结构内的严重缺陷;裂纹的外观是一条很细的线。
1 \- ]0 i) d+ F) ]# \; |- @6 j急偏,
) g$ P- n! J! x1 n$ X/ ]; D最大俯仰或横侧操纵。
) s5 O# _, u: e5 z向保持,0 N5 d# W0 z& _7 Y. C" H) L
见Heading Hold1 U1 R3 |* a1 ], r' ^1 Z
航 Q# N6 p7 j ] y3 E
.( w) F9 P \% y/ K ]- v m- y/ U
航向选择;) R/ N$ O/ ]( P
见Heading Select.
5 ^5 k( p% i- T, T顶端,
! F% p* [. a9 Q S& J4 p) X& B1 u) b6 A液压作动筒中与活塞相邻的。5 _" v/ P% s& @5 a# `$ K/ |% C
相对于真北或磁北的飞机指向。
, Q w' y0 ~4 T; O* V; m& w0 c航向,
: M+ X% @3 n3 l4 e3 D& n英汉对照民用航空词典B OEING( U: B# T6 `8 c$ T
TECHNICAL DICTIONARY 74
; J8 Y( Q& |& VHEADING HOLD (HDG HOLD), A mode of the autopilot
( F, o* ^! _8 D7 B K8 O! Nirplane heading./ N X* _& P: t8 S: y) C
t
w# V: A! [% Ke
2 g! |6 d! [8 D( l& T' c) R3 n2 mom: e6 `* x! V: Y& h$ f1 J6 t
g or1 b* @( v/ \2 G) n
(HDG HOLD),
, ?3 d8 Q( a, o* ](HDG SEL),
$ S/ `) {9 M/ B, D交换器,
% y2 L* r6 t4 Z% m- L6 ^% b3 b; z有很多通道的金属组件,气体在通道里流过时,一股气
+ b" E5 i# s6 j$ e& M# z2 u可被另一股气流冷却或加热。
% X& j( a P5 ?) f/ Nsystem that maintains the existing a
$ \9 n8 h. G' d! b [HEADING SELECT (HDG SEL), A mode of the autopilo
! o" K# X: w9 J. x/ O# vsystem where the pilot selects the desired airplan
0 s( {3 H7 ]! |( r; N& z( nheading.
, {. u; m0 c$ N2 g( vHEADWIND, Wind or component of wind coming fr
9 H& V: K" o# w8 |( B/ p- T+ zthe direction of airplane travel.3 j* v G: P, @' o6 M
HEAT EXCHANGER, A metal component with many
( |6 i6 F7 j, m" Z* M% Bpassages through which a fluid can flow for coolin6 I n+ k* ~- M8 o5 U
heating one by another.0 r3 M J9 B& y- A9 l) p+ X
航向保持
7 p) n* f, U# ^自动驾驶系统保持现在航向的方式。6 s' t# ^, H9 w: ?9 ~
航向选择
: Z2 v# O! q! M3 s O8 G* _自动驾驶系统由飞行员选择航向的方式。1 F% S: U2 e! W6 H% a# c
顶风,( t8 j, E( e- T- H& [
来自飞机前方的风或风的分量。
& x! C1 k- W0 K) B8 _" \ I" w热( F; A" M, m0 a) b3 F& _/ e5 h: ^% Y
流5 \6 ]0 t c; ~6 h! N3 ^
英汉对照民用航空词典B OEING8 Q6 l7 m3 G G* {6 T1 |5 C
TECHNICAL DICTIONARY 75
- G; I% n# P: I! LHEIGHT ABOVE AIRPORT (HAA), Is the parenthetical
i" n A' J' Q5 O* }. p; K) vfigure following MDA which, when added to the airport
, O' F, c& f3 T: k8 Alevation, will give the MDA in feet above mean sea- I1 l& `6 x! E0 R s* C0 ~" w
vel. A HAA will follow a DA or DH only when there is
* z; z8 ]1 m+ }: ]* Y5 k5 ro touchdown zone, runway end, or threshold elevation; h# A4 x' d( n8 w) j' B
), IS the9 F6 @; o7 D, ~9 u% N+ a
arenthetical figure following DH, DA or MDA which,7 ^7 Q E# `) t$ [& c2 ?! V% i. b! d# n
hen added to the touchdown zone, runway end, or6 k" s& S- p* I; u; ~4 Z
reshold elevation, will give the DH, DA or MDA in feet
1 g e& k) d- z) W4 `: p3 s4 bcy of one million cycles per second.5 a2 S5 ?& ]% q9 ~; Z
EXADECIMAL NUMBERING SYSTEM, A numbering- ]# H, q6 m+ e5 }! k0 _
ystem with sixteen as the base. The system includes/ M$ g* R; q5 Y8 |* K
igits zero through nine, and letters A through F
/ @3 L- ~0 p( y) b, g" s4 ~- m! Vpresenting the numbers ten through fifteen.0 y% t7 J- A, ^2 Z# Y% V
IGH FREQUENCY (HF), The frequency band between
8 {$ w8 I! X! m+ e; c* z3 w# `场标高相加后即是
! P7 {7 i) ^% p, h' f yDA高于平均海平面的英尺数。只有当接地区跑道顶端或
4 G/ z( @7 e# W. d! w) y道头标高不可得时,机场上空高度才跟着决断高度(DA6 N5 U, Z$ N& V3 [' b5 X' F
DH).
- s% k% ~9 _& y( j1 JHAT),% s0 D& X$ s {
最低下降高度后括号中的数值。它与接地" h8 Y, [' Z9 l6 x9 R
、跑道顶端、或跑道头标高相加后即是决断高度(DA,
3 k$ n6 h6 k; W$ NH)或最低下降高度(MDA)高于平均海平面英尺数。
; Q& e/ K6 l2 V L) F的最低天气条件同时公布的。
4 x: p' K6 A2 O/ b: M率。& L1 @+ E# |4 G* [/ |8 _5 I
一种以16为底数的编号系统。该系统包括由数字0至
& o" H- b" ^2 m% n,字母A至F代表10至15.
S0 c& w- Q4 z) h频(HF),% }. G [2 |; @
赫之间。7 A- v- p, w5 b. C6 f! |
e
: X, n5 {! d0 g" Kle- T- M- { i+ P' B2 r
n
- V+ j+ l5 O0 i. l' _* favailable.( C6 W( ^: i6 B* e+ G! g9 N- N6 d
HEIGHT ABOVE TOUCHDOWN (HAT
8 Y6 o2 U* r" A6 l% m0 M) ap/ S! o' d7 V+ s9 I
w% P+ a5 \/ l- K# E
th" ~% D0 ?$ ]8 k
above mean sea level. HAT is published in conjunction
) D9 _% I) A3 z* Z5 nwith straight-in minimums.7 p' H% ]0 T& o. m! s
HERTZ (Hz), The standard radio equivalent of* L9 ^6 Y' h6 {
frequency in cycles per second of an electromagnetic4 Y8 D p6 {1 U8 ~, T
wave. One Kilohertz (kHz) is a frequency of one2 ^1 t% y' d5 n, s. y0 I
thousand cycles per second. One Megahertz (MHz) is a9 x* k0 B/ M) s
frequen( d- c& I! g% a- O( C
H
# v( X& J: t7 ks/ C2 N3 m6 s9 y( r4 X/ y) m6 f& K
d3 w! n2 S2 c. M* W$ s" E: f+ d
re/ p( r! g6 g& J: o9 R
H6 c- k D5 A4 j0 ^
3 and 30 MHz.
" D& i( Q- ]- n机场上空高度(HAA),
+ Y- z {2 k; S9 k9 J9 y6 I是MDA后括号内的数值,它与机6 s6 ~8 Q$ n7 O# }( |) r
M
% g# n- \( X. [% t$ v跑
) c+ _- F. C6 U2 n f- P或
6 F$ v' h+ S# F: }, u离接地点高度(% `, y$ Z& S4 {6 d- ~2 i
决断高度或3 i2 `/ ^# Y" Z( z5 |# h- }7 u5 k
区7 ^" I W, {% w2 C
D1 _: R# z" \# _' Q2 Q
接地高度是与直接进场着陆3 S) I6 H+ q, l3 s9 S& @: ^
赫兹(HZ),
9 o! `$ ]4 n3 `+ ?: t0 r单位是周期/秒的电磁波频率的标准射电当量。一千赫
3 N$ U/ Z5 N' N1 b兹是每秒一千周期的频率。一兆赫是每秒一百万周期的
2 d/ i5 \' ~1 z6 E/ q/ p2 S# M频3 B. q4 C1 m$ k
十六进制编号系统,
6 I, k9 F& V2 b6 P3 K3 {+ O9! @4 R' w& E6 e# V/ U N
高
4 I3 m; {9 o5 z2 V频率带在3至30兆
, P: M. ], `4 F3 o英汉对照民用航空词典B OEING
# B4 x( `0 N1 o- k& \# {7 GTECHNICAL DICTIONARY 76
" H9 @7 Z: X! @$ z' y0 LHIGH SPEED TAXIWAY/EXIT/TURNOFF (HST), A long* A$ u# O) G" V- O5 A$ R6 D
dius taxiway designed and provided with lighting or' e. K0 O, {8 _5 I7 h
arking to define the path of aircraft, traveling at high* I8 B# X& _/ {( `3 K
p to 60 knots), from the runway center to a- q+ Y* _9 T6 W- Y8 {, a) N
the center of a taxiway. Also referred to as long
0 T6 z$ X# K$ c5 W7 F$ [% [6 G" Eit or turnoff taxiway. The high speed taxiway is
* r& z3 Z+ U' ^! W5 T5 A: rfter
# ]0 ~( ^! G" N* S9 {- s/ xancy time.
, f+ ?. N6 a5 m( y4 gr a4 F5 L7 N2 i7 I! J( _4 e& p; e
eavy component during removal and installation on the
0 {6 F& a1 T# B* p5 X4 Sirplane.
& z5 y5 l, R2 {# uOLDING, Airplane maneuver to keep the airplane from
( J, L9 J8 J0 T4 g4 I" P; trogressing along the intended route of flight.
' _3 h7 Y5 _7 o. L3 ~# lOLDING PATTERN, The predetermined maneuver
% [( r: j- R' D* ?" Ic control.3 X M$ c( v- f i# g. e$ Y
OLD/HOLDING PROCEDURE, A predetermined* U9 Z; T1 x4 }, i7 a* \
aneuver which keeps aircraft within a specified; j) c# Y" Z5 o" d' w% ^/ `' Y
irspace while awaiting further clearance from air traffic3 |; g5 p' D) l0 y1 O7 q/ G0 g5 t
ontrol. Also used during ground operations to keep
Z; A! o9 I5 `; L5 j5 fircraft within a specified area or at a specified point
5 M4 _, W. } F: ]hile awaiting further clearance from air traffic control., v( `0 k( r' ~7 y: B& t) z n
he standard holding time is one minute at or below3 w |2 @/ d) y' G) |9 v* V
4,000 feet or FL 140 and 1 1/2 minutes above. The
! j% n" ^9 ~( }; F. N1 I' beparation between 1 and 1 1/2 minutes is FL 200 in& m% o2 N( g8 P
(HST),+ Y7 L' M% a7 V" q, I6 v' y. K- P
道。该滑行道有灯光和标志表明飞. z a. T$ ? J/ T4 K3 s* L
从跑道中心到滑行道中心一点高速(可大到60海里)通% I s* ?4 `0 h6 s* V7 [* ]
的路径。也被称为大半径出口或脱离道。高速滑行道的2 Z8 J7 i- p4 r3 W. g
计意图是加速飞机着陆后脱离跑道,从而减少跑道占用
' x. ]) o7 q; F( s1 h4 y U3 [时间。
2 Z F' K! m, M6 m4 j( P5 ^2 `9 Q# O安装过程中,用于放下或抬起! S( J7 c; [) V+ y, ^+ O- b7 T; z; O
动机或重部件的装置。( A: e+ D( [6 V, S D0 k
待,
: D) k3 G3 U, ]" t使飞机不按预定航线继续飞行的机动动作。
" G: Z' ^% A( n4 N; _/ B待航线,
" r+ |; i: K/ U" b6 k9 E, W2 ^- b! t处于指定空域内等待空中交通管制下一步调度
: [; C* q7 O8 H! |等待程序,% z' W+ N( ^' [( l2 E8 Z. V* S- ?
保持飞机在指定空域等待空中交通指挥的下一步许可' k" ~2 o" w, K' |/ w
的预定机动动作。也用在地面操纵来保持飞机在指定的地8 z3 R2 f$ s1 |' t" w) l" l
区内,或在指定点等待空中交通指挥的下一步许可。标准1 z3 i( S6 O! i/ y& n" E6 `
的等待时间是在14,000英尺或高度层40以下时1分钟,
: G9 }* T' J s$ Z1 m以上为1分半钟。有些国家以飞行高度层200作1分钟和, r) X K) t+ u9 ^
1分半钟的划分。0 @ T) \# R7 a7 |: V* i. d* J
ra- L& L" h+ |+ ?& n
m
) q" }0 ?" h) ~* [& Wspeed (u8 I4 C0 M; O5 q) ~; ^9 o" p
point on
7 A5 F' ?; `5 G! kradius ex- q5 ^9 j( f8 {+ E5 ~
designed to expedite aircraft turning off the runway a
, S6 Y- j) y5 q/ B) S% zlanding, thus reducing runway occup+ L3 ?$ i& E% |6 N- Y( {% ?
HOIST, A device for lowering and lifting an engine o: e, z/ o: }# u; ]1 w; c
h
( x! b- ]' ~6 a sa' a! S0 F2 d- c z$ O
H
5 _/ a* W: e( F. p+ J j1 fp
& q p. y T, y @) ^! K0 G, QH. s' J* q& F" r
which keeps aircraft within a specified air space while
( g" A) A" N: p5 Jawaiting further clearance from air traffi0 B. V& J* \; s \0 y
H2 x/ e; P, ^/ K
m
2 ~0 T* _7 a# N) Ka
9 f8 D5 {& H! }c9 K0 Q# q9 R4 c6 [1 ?+ ?9 t; J
a3 e# u3 J7 n+ l a! C
w
( f9 J+ m) a( c0 s7 ]; WT
8 ~! Y0 w* l( E7 [11 j8 t; G' D. W
s
0 R6 `- m1 s+ c1 e' M" O& }2 Ssome countries.+ `. M' I7 S! j8 N7 N! X4 V* j
高速滑行道/出口) v+ W. T: l. \' |9 g/ a0 g2 A
是一条半径大的滑行
( J2 ]7 _9 ^9 j机: O4 i U% y: R3 R6 J0 M2 U `
过/ H1 ?2 }6 T: Q- N6 r* P
设
" x: ] {$ I5 w" n( H/ r& D的* G$ L6 c" N( C" U0 n& X2 R
吊车,. [$ o; B1 `9 `
在发动机或重部件拆卸和6 H7 y: W# n+ t8 a3 r( w) @
发3 _1 ~. X9 x7 p
等
7 r0 Z. I. P7 @ K0 S' Z ]1 |等
4 E& o9 s+ Y( G0 r, y使飞机! }) G H5 [+ H7 H+ O' j) }
的预定机动动作。% I+ S2 X# c; S1 M8 q
1/ p% L2 y( I( F# _% u+ k
英汉对照民用航空词典B OEING
7 N: g6 U' {! v$ xTECHNICAL DICTIONARY 77; ?. D% |+ y0 Y2 ^$ H* Q: \
HOLDING FIX, A specified fix identifiable to a pilot by7 q2 k( G" `- `! t3 D
NAVAIDs or visual reference to the ground used as a7 p: O7 n4 `5 F: \1 l
ference point in establishing and maintaining the* A/ u! n9 Z1 V3 e
osition of an aircraft while holding.
, p4 [; p1 H7 P% w, a2 y( oOMB, A hexagonal material made of metal or$ J& y/ ]3 M X3 y, k+ n
omex for sandwich construction of panels. A0 K0 O) m" N9 R/ t% R0 [
HORIZONTAL STABILIZER, The moveable horizontal& C8 X0 B9 r. Z
surface of the empennage used for pitch trim.+ T% P6 ~1 e' ?, Z! T
HOT BATTERY BUS, A battery bus which is not
% Y* l. Z! I, i0 t( aswitched and is always energized from the airplane
5 |5 R% ]; _: n- ?; g Fbattery.3 P7 V- m# j: t0 [' U) W$ O
使用的一个指定
5 A8 ]+ j6 l, w4 V位点。飞行员可根据导航台或地面目机参考识别该定位. h9 C4 S0 c5 e5 s: W c
。/ v* \6 ?3 o6 @7 d% N$ N6 B
窝,
9 s" r b7 {7 t: j, H" D一种用金属或Nomex制成的六角形材料,用以制造夹芯
% V S# Z W7 l) Q& g板。/ x! ?$ b2 n2 u: D3 ]
水平安定面,
- x7 H/ V5 k* c/ a _5 j% K飞机尾翼的可动水平面,用来控制俯仰配平。0 ]0 v* e8 M$ Q6 z
热电瓶汇流条,6 A) z( s% m6 _- `+ a& c! Y
无电门控制的电瓶汇流条,始终由飞机电瓶供电。! ]% l$ a/ D* a: _1 _: w0 i) ?, p R
re5 e7 ~6 w, C: C" G# V4 d; e" |
p" p/ {& R% }! Y+ e* U- A m
HONEYC
: A8 M* X8 w; I. [N( z* u ]) v% B* @7 N
等待定位点,
+ a8 @. i) h4 n) }等待过程中在建立并保持飞机位置时* E) t0 a. S$ p3 R9 A) q3 A
定5 Q* ]: g% P8 @0 G; p8 h; B- w
点
+ i8 a4 J+ I2 J蜂
0 N2 _ |/ u* j; s面6 L7 _ y2 g1 m* [! |2 h8 f2 K
英汉对照民用航空词典B OEING
% O9 b, x. J) O9 uTECHNICAL DICTIONARY 78
$ t8 @0 Z( a, _- ?8 O3 zHUB CAP, An external covering to the axle of the main5 Z/ x$ l; D. h; }4 a
landing gear wheels.
' H$ A8 `6 ~ o( I! x9 {. Q5 oHYDRAULIC FUSE, A device in the hydraulic system
1 ^6 q v* u5 A& ]r stopping fluid flow when a leakage occurs in a line
( h6 X! k% a5 k, wownstream of the fuse.( b& W3 E5 P2 M% R6 R7 z5 S2 C k
S, SEE - INDICATED AIRSPEED" y/ ^! S) {! P( I$ s) W
ER PLUG), An electrical device for" A& c; i- m8 K0 _
producing a spark in the combustion chamber.; T% m m: y& Y' b; c
压保险,) T" L! a/ E$ _5 k+ ?
液压系统内的一种装置。用于在保险的下游管线上发生' G9 D1 M5 L8 R+ l6 Y& h
漏时,阻止液压油流动。% f. S5 n) J/ V @. ^& x
示空速,% p+ h: C1 E# G0 u8 J% K! w& N, L
见Indicated Airspeed% Y' U4 C2 F; R7 @; m9 U2 |- }" e2 m
fo- C0 Z# q( d6 |( Z8 L' w4 R
d
3 g. x9 `* Y6 S3 m" BI IA
: |+ }, U/ A% S h1 O8 g' `! PIGNITER (IGNIT. Z) m& H6 u4 x r
轮榖帽,
n S* e( ]+ p0 d主起落架轮轴的外罩。
$ N4 t, `" h- }$ n1 I' h* w" t0 W液
, @; i7 h& w# B s# v2 f/ p8 F$ X" y泄9 a1 F+ {# M' a3 `7 j7 ^
指9 _- c# s5 S! V A
.
: i4 e; p, m) |+ x, I5 U5 F3 q在燃烧室内产生火花的电器。0 ^" b# t. H' u* t( J/ i/ r
点火器(火花塞),
* J( C8 v! T0 G# w6 ^7 b9 C英汉对照民用航空词典B OEING* r6 Z* {( x/ T
TECHNICAL DICTIONARY 79
& s0 E/ z$ p3 I2 b. j* dIGNITION EXCITER, An electrical component for
- n ?1 b; L) m8 X( b* Lsupplying high voltage to the igniters for producing a
; ]$ f5 L9 g5 e' g- T6 _spark.6 x) `% k4 D7 I/ e" {7 ~+ ?1 ^
IGNITION SYSTEM, A system for starting or continuing0 U: O* a6 F _# l! E$ Z% v% O
combustion of the fuel-air mixture in the engine
6 y$ L! u. C4 t* R% h( }- lcombustion chamber., T2 ]8 }! a3 o ~) e' l# W
S, SEE - INSTRUMENT LANDING SYSTEM
q" Y5 Y+ h/ K3 XPROVED CLIMB PERFORMANCE, The rotation and
* W7 x! ]4 j& j0 U+ K' M9 Hlimbout speed increased above normal to increase
# ?( X0 n6 q( tDICATED AIRSPEED (IAS), The airspeed read
* p5 w! i8 m# R# ?; K: Y* m' g% D火系统,) j1 e8 k' O5 y; X, m6 Q) p9 R& M
一个使油气混合物在发动机燃烧室内开始或继续燃烧
0 _. I- U/ L/ O% y- F% Z系统。 V) o1 u( D' ]; n: p
表着陆系统,* |2 R( w( u1 y3 s" J& y* z
trument Landing System0 q& A/ m' w$ c2 H2 r% J( p' l% h
ILLUMINATE, To turn on or to provide light.
; v3 G3 l) `6 z3 L# |& G9 T8 qIL/ G/ _2 G2 f6 T# ^$ C
IM
( [/ H% G* t3 g: f3 I% Vc' ]: b9 G% _6 @7 S( h8 I3 e) j) g
airplane climb performance, especially if an engine
& m* b0 x; t* ^( d$ M/ {; vquits.
X& D* P; T0 s* X/ cIN9 M* g1 s5 k8 z* Z( X
directly from the airspeed indicator without any
. X6 A( e9 Z% U& A, {compensation.
5 J1 }7 P: K6 oINDICATOR, A component for showing quantity,
( ?# n! h$ l M# f! T7 xpressure, temperature or position by a pointer or
1 ~- C! P B; `( G- P& ~/ Znumerical display. (Similar to gage (gauge)).
0 @ a a8 E$ Z点火激励器,+ d1 B+ s) e" M3 k& V/ \6 L
向点火器提供高电压使之产生火花的电子部件。
3 I# M: [4 N# A: L6 t" X. C7 l4 u点4 U9 v, S' y2 d! A, v3 r
的& T1 R7 e3 b8 Z; R
照明,1 O" j/ Y& s4 k" z
打开或提供灯光。% O2 ?8 f) X3 G) L% z
仪" @+ \; a( {, m$ c
见Ins .
. O7 K) Q; L6 _& a* F进爬升性能,: X. V! \. g, L8 W: ]: D2 L
用大于正常的抬轮和爬升速度,来改善飞机的爬升性
0 z) r+ I( D* g* z0 }- G: D# \一台发动机不工作时。+ U0 Q' J& t" _* ? r
示空速(IAS),
+ K+ P, S. d0 ]+ ]正直接从空速表上读出的空速。
) {% ]* y5 V- J* N) H2 m指示数量,压力,温度或位置的部件(与
" B: {4 Q9 z) y8 W. R计量仪类似)。1 S# b- K6 V2 [' g2 b
改
: j g. K" d1 b能,尤其是在# V' w ^( P6 X4 L
指; Z6 h9 t! B. A: v6 i
未经任何校
/ O. v; x2 g/ f# ]4 c: f) ~- p指示器,
# i0 ?$ @4 h m B9 s用指针或数字来
2 C" q4 U2 P- o9 M* t3 S英汉对照民用航空词典B OEING
' w+ [5 c6 X. i/ ^TECHNICAL DICTIONARY 80' u1 r/ I/ H! C+ X& a8 c& S# b
INERTIAL REFERENCE SYSTEM, A self-contained,% l- t' a ~+ F# k) \! \, G# M; J
navigational system based on the measurement of
( c! M- t% j4 H H# Y: Jacceleration and attitude.% e8 a" l. Z9 g% c4 s9 ~
INFLIGHT PERFORMANCE, The performance of the% ]. | `# ~/ W" A- Q" A
ITIAL APPROACH FIX (IAF), The fix which identifies
2 w8 N! X% \# @: Ie beginning of the approach to an airport.4 _0 N; o. X" z/ p
LET GUIDE VANES, A fixed set of blades in front of
. i# ?7 }6 O: O7 N9 L; @n engine compressor for directing airflow to the
& T4 B. u' w bompressor.2 E( P7 e8 Z; F
NER LOOP CONTROL, For autopilot operation this is
/ Y* }8 l/ ~. Y5 C# Ze basis control of airplane pitch and roll attitude6 B) _* a' Z4 A, ~9 Q) r6 a
中性能,
G4 K& Q* P% Z, {飞机的性能。' F* c4 p) w2 _& \: Q
起始进近定位点(IAF),
& q4 ~9 C' J) ~6 l标志向着陆机场进近开始的定位点。
) t8 P/ h% G! e: g$ H* D4 ^9 b进口导向叶片,
* a: n K- Y1 _# p) g* K发动机压气机前的一组固定叶片,用以引导气流进人压& l; a( u' s& ^ i; t# r$ `
气机。
8 t3 V5 n2 Z% ^% `环路控制,
" ?# T' q, R5 S0 }; v, x s/ e对于自动驾驶仪操作,这是无关飞行航道的飞机俯仰姿0 H' a9 I5 _2 | `9 {# `( {
制。
0 S. Y2 S+ |8 J! R: \, a5 caircraft while enroute.
! x( w' R6 W; s6 V5 Y3 s: _IN" @% U" O# f% j7 B! i7 k! y
th
5 F8 K @- g2 Q4 nIN" x; m( |) Z5 l
a
z8 a9 s* z- |: ^) P$ ~" rc! f2 x* P8 D$ J+ s& v; J! H3 \
IN* V4 O; R! ~7 H' S" s6 X0 Z
th# U6 w) c5 [0 ?' O
without regard to flight path.' ^" h& l" ]$ k% U2 J0 f; W
惯性基准系统,
/ Q2 W j: x9 C9 a' V以测量飞机的加速和姿态为基础的独立导航系统。
# s, l$ G5 C" x: m+ q. w空5 N$ F4 x; u w: U6 z* ?& c/ `
飞行中
" \2 u, k: b. p内
7 ]% k2 Q' [2 p' b7 h9 M% Z! n态和坡度的基本控$ v# a$ X" @/ n4 A0 N7 S* @
英汉对照民用航空词典B OEING: K0 e) j! C4 i, S# f
TECHNICAL DICTIONARY 818 L) ^7 q+ A8 J- N
INNER MARKER, A marker beacon located between/ ^$ F- V/ W1 b( [9 v
the middle marker and the end of the ILS runway.; K* j8 E, l3 ^) U. w6 e
OP, SEE - INOPERATIVE
9 v2 q% _8 V! S/ p: s0 }' MOPERATIVE, Not working or operating.! s7 t0 Y0 ~; j
STRUMENT FLIGHT RULES (IFR), Rules governing$ ^& N: `+ u7 I. I6 g
e procedures for conducting instrument flight. Also a
' Q S: A( Z7 C2 Hrm used by pilots and controllers to indicate type of
; i, T5 R* y( @6 H' ]ight plan.
2 I2 C t; [/ B; [+ L- X2 b3 wSTRUMENT LANDING SYSTEM, A precision0 Z' n0 c$ l' _3 C9 l" B- c G! _- u
strument approach system which normally consists of
; W: @& Q- u; s- x! ^e following airplane components: localizer receiver,7 ]1 r) n p1 A& B8 _/ j
lide slope receiver, and marker beacon receiver.4 s/ L2 u4 M% P. k# w" [
OLOGICAL CONDITIONS- R; F; T$ b1 S3 R. b3 F
MC), Meteorological conditions expressed in terms of
9 G* ]/ p, O( K6 Q7 G' ^3 A; Xisibility, distance from cloud, and ceiling less than the) X+ s% y$ d0 W4 |# R( d' B
inimums specified for visual meteorological
7 n' ~! X& ^# }/ @itions.
9 K g! x1 M+ r! p9 rSTRUMENT RUNWAY, A runway equipped with" D: V9 t& X/ w
lectronic and visual navigation aids for which a
3 a' w& q( S# ^* x5 q' Arecision or nonprecision approach procedure having
) c$ L- o' p" V$ C( Q+ a: T间的信标台。+ K+ l/ Z3 o9 E5 N' M/ o8 q* z
不工作的,
+ A( ?1 N$ T, G! u+ }见Inoperative4 X5 J' `- f! i6 D' x- x" L
IN2 f( i/ p" ]) I* g- Y, \
IN: G1 k6 v1 S) @; ]" L/ B
IN. t2 D% Y' `( l Q
th
& O$ h5 h/ V9 w' Z8 y: Vte
, u7 Z1 P" \1 g/ kfl
6 g% A0 v$ A7 UIN/ d, x A( [- g7 k0 |2 W
in
! B4 B3 `2 f" s6 E3 T! j" J* Sth
. C4 n D7 s5 Y, wg& o2 A. |2 A `; A, _& Y
INSTRUMENT METEOR
@, q y. V2 ?' z6 E5 j(I0 [; `% |( U; F9 p! Z
v
9 g; b9 x1 W2 X- |1 w; Sm- f- N2 K& Q) ?/ A' d8 F0 W0 N. V
cond
5 U, E) i" F5 i2 I: p. SIN: V( x! l' m# j4 j: F+ ~' ~
e
0 W$ }" E3 G, w0 o0 ]+ ?% Yp0 @/ W3 ^6 {# U% a- P" t" n% B
straight-in landing minimums have been established.* s5 Q5 Y: X' Y: e
近指点标,, B* G, d8 @$ Y' u! Y: I
位于盲降跑道头和中台之: A' G* s! H' v5 j
.
: u& I# _% m7 T q8 M; u不工作,
+ g- J O/ l6 Y F/ F- T1 u不工作或无法进行操纵。
2 X3 d% q3 k' _7 S: ^: v4 [$ ]( V7 V& ]仪表飞行规则(IFR),0 O; e9 h8 q9 A
仪表飞行程序所需遵守的规则。4 ?; `( s+ S/ N. ^ J& O
仪表着陆系统,: @& Q: B5 F+ u9 j/ s
一种精密仪表进近系统。一般由航向道信号接收机,下' h" e6 D' B w* o) f" R* l
滑道信号接收机,和指点信标接收机所组成。, q: D. b' C8 |. j# |8 Z
以能见度,与云的距离,和云幕高低于最小规定的目视0 H" E; ~- b | d
象条件的一种气象状态的表达。
4 u% [; R$ B: ~3 I9 _* `) h6 f用于以精密或非精密进近程序作订明最低天气标准直
8 _/ S/ @( _) g* Q着陆的装备有电子和目视助航设备的跑道。& l: n! [7 l5 J2 C m, Y
仪表飞行气象条件(IMC),
5 @# x" U6 k4 n: E5 J& U7 c$ e气
* a- k# k. A+ b) s) G仪表跑道,
. S7 i) x# k- G, C线$ V/ m+ ~ A4 C0 j. ~
英汉对照民用航空词典B OEING
! C; Z$ Z$ L8 D( q% A: [" Z1 ~TECHNICAL DICTIONARY 82- n0 ?' ^/ o1 z- j
INTEGRAL TANK, A metal container formed by the
: Q" H% l% N1 [, b: @ U7 d' Ilane.
% \; l) G1 A) D% v. r$ V0 Q- `cted. P8 U5 T+ a+ ?5 A6 d
circuits.
" W0 N- E, J7 N$ L9 W/ o4 @' R/ Q' T' ^& nManual
# S* d6 A* R$ @4 E: `erformance data providing range as a function of a
E Z% |* Y' I$ Q3 S; {hange in airplane gross weight.; ]! O& h# v: [ i
TERNATIONAL RESERVES, Reserves required by
! m' F) u9 f( `3 `: ?2 Le applicable governing agency when flying- J9 V3 Q, `% ~+ W% Q
TERNATIONAL STANDARD ATMOSPHERE (ISA),( n) }2 Q. P( i+ f
he hypothetical vertical distribution of atmospheric
" m! n1 L6 k2 {; g0 p# Y* V2 ^mperature, pressure, and density as defined by the' R- }! ^/ C& y9 }; ^# j
).
0 W% i1 \* i7 q+ ]# ?" `5 UTEGRATOR, An operational amplifier whose output, @% {7 ^5 x5 `* T4 \& ]
oltage is determined by the input voltage, the input2 E' V4 o* y) N F7 p9 E, t. [, [
上( p) g' R' `8 o( |1 ]6 _& `1 R4 N
存燃油的金属容器。3 \2 ?3 k/ x" E, d% \
,
4 |2 c3 S# {2 L" F' q5 F飞机总重量的函数提供的性能数
9 ^& k& j" o# y# l! j# [7 c2 o。
, M& c& R7 e% e' n# J. z' m) `际航线备用油量,; R. j _' A. n5 z3 E0 e4 U
在国际航线飞行时,有关的政府单位所要求的备用燃油; B R7 E9 e, Q# R
际标准大气(ISA),
9 l" P8 c& E6 {7 M, O9 s2 y, G5 @国际民航组织(ICAO)规定的,一种只在理论上存在6 U/ }6 h, V- ~$ d& K5 T1 _
大气其温度,压力,和密度的垂直分布。
. G7 L7 p. X' E8 y分器,- w5 X |) Z& Z: g8 \1 ]
由输人电压,输人电阻,反馈电容和时间微分而决定其, F) Q% F P0 k! u/ I) ~# q
运算放大器。
1 m0 c. X9 f1 D8 N+ A7 Y' Bwing structure (spars, ribs, skin) for storage of fuel on& D5 ^, R) C/ z* E* B, h
the airp
% V# P* J) ]) @7 @, |9 u1 j6 SINTEGRATED CIRCUIT, A small piece of4 b8 l/ F% ~' q! |+ H2 q9 Y
semiconductive material that contains interconne
0 p3 A3 d: B& q& P0 _miniaturized electronic, @/ q6 u, O- n t. h6 j& I. d5 s
INTEGRATED RANGE, Tabular Operations; P6 p% i7 n' {
p
; P z; @1 ~; w0 D* ]8 y# {c K ` a# x5 }* P8 F
IN
# E* J7 a& t8 D9 Q( [th. B! _( a! {3 E$ Q1 M% ^2 E$ m
international air route.
" L! R3 J+ L$ EIN
: ?! i* K. }9 L$ ^! s. `4 kT
2 A& D, e0 p4 D. ?te' d- y. S6 ?. ^# U+ C
International Civil Aeronautical Organization (ICAO
; g' U" }: S# H8 zIN
4 s1 U: B3 e! D) Nv/ a/ U4 ~5 h; n7 }' O
resistance, the feedback capacitance, and time: D4 _: `2 O. @: `) d S/ f
differential.: J( B$ H$ a+ @
整体油箱,
( `0 O" \3 n% u0 l+ c0 _ B由机翼结构件(梁、肋、蒙皮)组成,用来在飞机' o' F( z' n. t8 U
储
* J: e, E1 ^" I% r( k8 M集成电路,. Q" O: e8 [+ b) i8 v" Z9 `
一小片内含相互连接的微缩电路的半导体材料。% m) ?8 _, `2 B3 ?6 V
综合航程" D- C3 Q& @) Z: O1 P) B$ a& }, ^
使用手册将航程作为
6 N2 ]# L5 J: q) N, n5 _- L据
+ U) E' Z( K3 I9 S! Q国
7 {3 e7 j* g0 O5 @, L量。" u" j; ~6 T5 ~0 o0 {2 b- L( j
国
/ V, b7 ~+ N7 h7 t2 S的
, z9 H( n$ K* G! ?积
% D3 P+ W8 D2 a5 ^5 X* Q& p s输出电压的
" C7 w( o# s" Q$ k英汉对照民用航空词典B OEING
- r; T, `* ^9 c7 j( ` r" MTECHNICAL DICTIONARY 83/ C: d* g3 u0 H9 z: h. c/ Z
INTERLOCK, A wire connected in series with an! y; a: |! u8 s2 U* s; Z2 P
equipment or device, or a condition that allows" ], l/ L: N9 @
operation if all requirements are met.
6 D& n' \6 H2 V @! pf the United Nations whose
% F6 Y4 `2 }; d0 b6 Q; t* e# {9 [bjective is to develop the principles and techniques of
1 u V: r4 d- | J7 r1 ~ternational air navigation and to foster planning and) Z" Q( y. @. P0 u
evelopment of international civil air transport.
7 w- M, ~) W, T5 K7 B L3 ~7 i) kTERROGATOR, The ground-based surveillance( m/ W2 E. B( ~9 f" S
dar beacon transmitter-receiver, which normally scans% j) z6 P/ }; u3 q. T5 c
ll$ w Q i1 }8 b
on the mode being used to reply. The
, P K9 o$ Y# C+ z. ^/ \" F2 Wplies received are mixed with the primary radar) d$ S c! O- }. p
turns and displayed on the same plan position radar1 x R. k5 A6 j5 ^; K" e3 q
cope.+ Z2 v0 x# {8 b) D
TERSECTION,
3 o6 R5 h) Y) u1. A point defined by any combination of courses,9 }2 E* v9 W# u! J
radials or bearings of two or more navigational4 f3 B3 e& o) U
aids.* t. i% N" j6 L
2. Used to describe the point where two runways
: @7 A0 l; F/ }& ecross, a taxiway and a runway cross, or two$ a1 k$ K- {3 V% Q
taxiways cross.
0 X. d$ ?- U& l8 v; g9 m' C8 Mcy)2 }7 K7 b5 z: ~* Y, R$ K5 _( R+ C
tem.$ _, \, F8 u1 \' U9 G( O) Z2 j
者# k/ o6 j( O0 L- f2 G' c( ?
当所有条件都满足时才能工作的状态。+ K) q) {+ A0 y3 A' U
组织,. g r. _, l0 Q: M. H" A# c8 f& p" G
航的原则和技术,促进国际民航
3 f; \5 W( X8 Y$ d3 y输的计划与发展为目标的联合国专业代理组织: M2 ?& C" _8 D
问器,
6 v4 a5 i2 J, B1 O1 H8 W w1 u' t2 [一种地面监视雷达信标收发机。通常在工作时与主雷达
3 m! [! q( [6 P' O连续的无线电信号,不断地重复要求与
' d2 U, Z# ]6 r8 s- R接收到的信号相混合,显示在同一平面位置的雷
0 ^( F4 J" {* N( N1 U6 B, P1 y达屏幕上。: f J6 l( z7 F$ h* J# E
交叉点,( g; Q4 d# i( f% F6 d1 C |8 V
1. 由航线,径向方位线,或两个以上的助航设备* X9 P: U: {( Z/ ]% C! @1 E2 l6 @
的方位交会而确定的一点。, ]) i( X+ P3 i
2. 指两条跑道的,滑行道与跑道,或两条滑行道+ C! {" x) A% N. e* b
的交叉点。
- h3 y1 p# S- G: U+ [INTERNATIONAL CIVIL AVIATION ORGANIZATION,
@2 m( t7 ~0 Y# ~A specialized agency o5 a5 ~4 L- S$ c/ N9 F3 t1 x
o& z# r* a* s4 C! G. ]' c( x8 z+ s
in
* W" u C% v2 q6 w: xd
: T& H1 M# C% n, |$ h; `IN
' O, I" W& Q: n8 e- o% Yra" \' T' d6 G1 h3 a& f- e3 f- C
in synchronism with a primary radar, transmitting
, o# ?; N; w; x; Adiscrete radio signals which repetitiously request a
) M3 }4 G* q$ }3 F- Xtransponders2 F/ R7 q* n* i- x; g: A
re* W8 M3 M- ?% m- w# S
re7 p4 X" g; c( |$ R3 d9 C
s
! u6 C9 J: \: |- j7 W' y; LIN
0 q2 V3 Y3 v) ?$ D3 O, }INVERTER, An electrical device for changing direct
3 a7 T$ E; |9 y* ecurrent to alternating current for standby (emergen1 I: y( X2 Z; e; ^( l/ k# d# `9 M3 d' L
power supply to electrical sys
. N0 S% a% n s; E$ M& G+ T" k联锁,
{2 X( @6 D ?- H8 H一个以串联方式将仪器,设备联接在一起的电路。或
+ R' t; I5 j- ]是
' k5 f; k3 ]1 b8 i( ?国际民用航空3 w2 [" a* {7 ^0 x& P& s/ ~
一个以增进国际航空导) _, v+ ~8 C% `' K& e- |/ Y6 S
运9 `( G5 C: Z; e% r, G
询
7 i" |7 Z( J! k" I: k! n: o; s' l/ A同步扫描,发射不3 @ U% t. L z/ ?5 p7 |
其工作方式一致的应答机进行回答。所接收到的回答信号% a1 S) i( F2 k3 h
与主雷达
7 j+ K1 R& v) R' E% o0 ?; E变流器,1 f4 |/ O: \, |- n* W) d4 M
用来将直流电变成交流电;以供电气系统备用(紧急)
2 ]4 m( L5 k7 @* c电源的电气装置。
- a3 N# }# |7 C& F英汉对照民用航空词典B OEING
* X+ x& l# p; ~4 P5 x1 i" U% [TECHNICAL DICTIONARY 84
/ ` c1 y7 _# g" Y0 TIRS, SEE - INERTIAL REFERENCE SYSTEM/ r c) s7 G2 X) ?. U2 y& r
ISA DEVIATION, The amount of temperature or
: O5 h7 u1 T. X$ Z: psee International+ B: A/ M- ^6 j9 v& ?8 @9 W K
tandard Atmosphere)./ m( d$ c0 I* v- }/ U& S' C9 z' `
LAND RESERVES, Reserves required by the
: T, u, L0 t" @pplicable governing agency when flying routes
% Q. N; \' }2 E( h, v6 }4 C4 Wetween islands with no alternate airports.
& n- ^1 w. u9 o1 UCONDITION, Cabin pressure (altitude)1 ^% }. a, a) q& @: ~
maining constant with changing airplane altitude.
: y5 B( `' T0 F; ^$ a( w1 _ising the# l0 a* O5 j2 R
a
4 X T Z8 R1 v2 G Q' V- a1 v* f- S,. _" s# m2 p+ y! s8 @
pressure difference from ISA (
2 c. i9 X# K C7 I0 X7 o6 V" A% ~S
2 H5 N6 N1 J9 c5 j; P% dIS- N+ j3 X c( a- `
a
7 f, J1 O9 }- |. K2 Xb
6 y( c& q& g# X. C6 t2 TISOBARIC3 w) P; r, s+ |
re
6 |4 o, f/ @+ t c' f! O: ?. g9 W1 ~0 ]6 nISOLATION VALVE, A valve in the system for
. a% l( ~/ G9 Q& [3 @* o" `separation of the system into sections.
- s* b3 D6 |! ZJ5 L) ]8 M/ L: Q+ W
JACK, A mechanical or hydraulic device for ra% y5 d5 }. B/ D( k/ s! d
airplane.
* D# p* K; j, m/ t( YJACKING POINT, Location on the airplane for using2 Q0 j+ B9 }6 N' \6 ?
jack.
* c& K. g3 x6 N$ M3 W; w% y惯性基准系统3 M6 s+ x- H" g/ h0 t5 i% k
见Inertial Reference System.6 `5 P C ^2 c& }3 I; R7 G' `
与国际标准大气之偏差,5 ^" r, `2 N+ b( O
压力与国际标准大气的差值(参见国际标准# a& s1 m& d$ w% a0 k
有关政府单位要求在没有备降场的岛屿间飞行的飞机
# t3 d4 x$ w/ t; \6 ?! v带的备用燃油量。( o! x' f9 h6 }% _/ V
压状况,* G3 J1 C+ y1 ~. m; U
在飞机改变高度时,座舱压力(即座舱高度)保持不变) c& X) ^& D; N" q: W3 v7 Y0 @/ w
状况。( s/ d. |6 _2 x, f* G( x% E. h1 j
斤顶,
7 W- h- ~9 w6 A用以将飞机抬起的机械式或液压式的装置。3 y3 n9 S, N7 m, J; ^$ z1 ~2 N* u
温度或$ l5 d0 X6 n+ n O9 p+ l9 z
大气)。
7 e( Q3 h& I5 G8 L, Z岛屿备用油量,
9 y7 |/ c6 p+ \. s! r- s/ s& D d携* I# w* S6 |9 G5 L& S
等1 P4 Z" F$ J8 i5 l# P/ |
的* \; `3 b2 k) G5 V
隔离活门,
5 g% F. ^ F* [. F用以将系统分隔成几个部份的活门。
6 t4 }+ o# n& s( r0 U千
9 x) x7 d5 _ |: D+ i; S0 x# c千斤顶支点,
$ P$ L! n6 |! M5 R1 k! t飞机上可以让千斤顶吃力的位置。
! w5 z# p$ _1 H7 B* J Y英汉对照民用航空词典B OEING" B+ l; g2 p+ x2 M& B8 U
TECHNICAL DICTIONARY 85
+ r: Z) z3 {5 [- WJACKSCREW, A rotating threaded rod used to drive( I$ L3 o& }2 P
moveable component such as a flap or stabilizer.
) x, L) e( U5 {a 致动螺杆,
/ R; @, O( s* { `& y; y2 A4 A3 j用来使可动部件如襟翼或水平安定面运动的能够旋转
# m. ^( u" x% q& h4 c! y4 j的螺杆。
- A. m4 V/ `# t( g/ J- |2 n$ g英汉对照民用航空词典B OEING
: X6 m8 J; z6 f2 p1 H" r( g0 TTECHNICAL DICTIONARY 868 \" a$ X6 s4 A; s0 j7 x
JET PIPE, A control component in some valves and
E/ ~6 u' V; wET PUMP, A component in the fuel system, operated
: A. }# q1 l7 L7 @4 j( h# Y7 H8 R8 Kr removing water and fuel from a fuel* s9 C0 U0 ]# v" [; R
nk.
7 B: o+ ~/ Q2 D. {射泵,% P: T, q u3 b- u6 b' b. H
内,由燃油压力来操作,用于从燃油箱中排除
" N3 D+ S$ Y; S9 n3 `6 p8 Q和燃油的部件。, i: ~. d" e0 Y8 @: A+ m
actuators for controlling the flow of hydraulics or
# J( G5 |. Y. |7 w+ {' ^* E) Tpneumatics.; F4 |. P B+ V& ]. Q
J' @2 T8 S C+ l$ Q) h
by fuel pressure, fo
( `& X0 `6 o% W& Qta9 V5 K; Z/ R- h5 s+ W# U
喷射管,
$ a8 E9 c. I0 O3 t8 b在有些活门和作动筒中的控制元件。用于控制液压和
3 {& I A, K# Y) P气动的流量。
: J8 {9 W/ ?8 _5 p% a' W引* [! Z' i$ _" ~- V S
燃油系统4 ^# [, K* E4 Y+ A
水
+ @/ @ s7 h' f- w. C英汉对照民用航空词典B OEING
B( i/ Z, l( dTECHNICAL DICTIONARY 87
, Y) G+ L$ L U7 L( H0 N# BJOGGLE, An offset in sheet metal construction
; N. \5 H% Z# @8 Y5 A) xdesigned to allow one piece to overlap, either higher or! Q. U& {5 h+ I: n7 {& j& t% e8 @
wer, the other piece.& T" s$ z- t6 T: J- T$ E/ L
OULE, A unit of electrical energy of 1 ampere of! B* _8 [6 l* s H0 ?
urrent passing through a resistance of 1 ohm for 1 \ i: e6 y8 q* q
econd. Ignition system energy is measured in joules., Z/ Q8 V, D& K9 d& E& r- t6 T
UMPER WIRE, An electrical connector for temporarily
* F& e! D& H+ ^8 `( Jypassing part of an electrical current.
; ?. J: D) N( U6 B; |! M: DUNCTION BOX, A container which serves as a joining/ `% |, C3 ^ B, N4 o& {: X
lace for electrical connections. May also contain; ^5 v0 L& l3 ]& o: t
lectrical components.+ x2 @1 N+ G+ H, j {5 M
EEL BEAM, A structural beam in the fuselage center
% w. J b4 ^/ s4 Vection (wheel well and under wing center section) to
2 r3 b- p+ q. C! H# I) x+ iKEVLAR, A light, strong synthetic material for8 L4 ^) c/ T6 e
secondary airplane structure.! T9 q W9 `6 ~; p8 @' O; Y
,使一件金属与另一
& l6 e( J5 @" x1 o+ J8 c相互叠合。) f& t& t. e( u' |# T! @
耳,9 w9 ^9 e( M' f) a
电能单位。一安培电流通过一欧姆电阻一秒钟所需的电2 {! O1 x C0 T* W7 s0 N
为一焦耳。点火系统的能量用焦耳度量。
4 p# G+ }" o9 j2 I/ k, M5 X接线,% I- J' G: Y% Z5 z. H" C' O- ~
用来暂时旁通部份电流的电器连接件。6 r/ m8 o4 \; p3 Q9 d1 f- t
线盒,
, \4 q( ` \/ l做为许多电接头的汇集处的容器。也可能内含电器。+ G3 q6 P9 d8 P) K9 g
梁,
U2 |5 g) s: f$ w- \- u B机身中段轮舱和翼下中段,用以防止机身弯曲的结构。' k8 b% ]2 ?( H7 i$ a# s$ N
KEVLAR,' o2 O4 v2 d* w: ?4 L0 ^9 O
一种即轻又强的人工合成材料,可供制造飞机的次要构; }/ M `7 o2 T1 B4 @
件。
7 M/ T) f, | Y! k" e' z6 flo
4 g. i6 _6 M% s# s! tJ' W$ J" w' F, }, y: M
c
1 q8 G) f7 h) f$ I) e2 bs/ t/ D. B0 |# I* x z% `8 n: c$ W. J
J X; l! G# Q5 t6 n" \4 z
b- W; b" \5 J, s/ ]) j6 w
J/ V" `' {. |+ |, ]
p
* p- C) y! O5 u, _8 t7 Ee
% ]8 I9 M9 H% F$ L2 b4 YK3 A6 P2 A& Y1 @( O b
K
; h4 {& x- J+ f6 Gs/ r( _8 i+ b% k$ Z8 A0 m
prevent the fuselage from bending.0 k5 V$ G6 \- Q3 W- z" R1 D8 ^ Z/ o
折接,
, D& ~- A* H% s) Y, _& K t: `+ y一种平面金属结构设计的弥补法
7 E6 j4 o$ B0 ~& t) M件9 {# F+ W0 v# c$ U. y
焦' S; l0 P: l% @
能3 b" p, z# {4 G+ W6 Z
跨
- {- I0 E- \. H i. T接0 s6 O j r) t% `
腹; D# _1 L {& [6 R
英汉对照民用航空词典B OEING
/ `" A7 t' A1 n2 @TECHNICAL DICTIONARY 88
2 q" t f% O( P( NKILOWATT, An electrical energy unit, equal to one& Z ` {# V+ o! e
thousand watts, for specifying generator power output.
* }1 x, E4 b8 C V! A7 eKINK, A sharp bend, twist or dent in a section of tubing, ~" t0 j+ P, d) t: Q
wire bundle or angle stock.
( X0 w: j- G' r0 \7 FKNIFE EDGE, A very sharp edge on drilled or machined
2 p2 n2 b$ n! Q5 i8 T! u9 o* `metal which is usually the source point for corrosive+ u3 P# v2 S; k
attack.* s l2 \7 Z' D* R+ L9 n
KNOT, One nautical mile per hour.
0 z) c, x( _3 B% |4 q5 EKREUGER FLAP, A type of leading edge flap that is
# m) \8 S( l: `. G2 X% Gfixed on the lower side of the wing and rotates forward* y! N% S4 V* E
into the airstream.
7 u0 c' S3 `, G2 ^KW, SEE - KILOWATT4 c5 m% P1 G/ ]
L$ P! g* h5 W2 A& o( j
LABYRINTH SEALS, Rotating and stationary2 ^5 H7 o' W0 z6 i, v2 m% J" J* A7 X! X
overlapping structures which utilize differential air
3 Z" T! x! d5 y4 [1 `" hpressure to form an external seal. Most commonly used
7 N7 v: G3 x: m- L+ hin turbine engines.( B) K3 h; u0 [) ]" U3 {$ E
扭结,' p9 y) r! y& N' J/ H3 c3 m$ n
在管路,电线扎,或角材中的尖角,扭转,和凹坑的部* {9 F! U6 B8 w% B' ?# a
份。4 G* O! H: G O" ]+ p
刀刃," x8 c9 p- v) S! O0 N
钻制或机制金属的锋利边缘,通常是腐蚀的开始处。
& K$ l6 C. y6 J5 \7 |5 ?节(K,KT,KTS),
* O1 Q: l. K3 Y' b& `# x每小时一海里的速度。
0 Q; K( r" f# c6 N- V! R6 t4 J克鲁格襟翼,
: O# s% l# j) ^( O- A* A一种前缘襟翼,位于机翼翼根附近,旋转前伸。
9 `5 s) {6 B, C7 A7 H% n0 H千瓦,
7 `! w4 n" P% T" W见千瓦(Kilowatt- `" }" z) ?8 S9 w# }$ i; t# e
千瓦,0 C- ~# ^$ b# D' e) U
电能单位。等于一千瓦。用以确定发电机的输出功率。7 P, m* _& t: l% h, s& c. t
)。6 ^8 ?' V! \4 h9 j Z
蓖齿型密封装置,) y( ~; \* D% B& V" b
旋转并且固定的重选结构。用气压差动而造成外部的密
( }( G+ c2 R* j$ J封。在涡轮发动机上最常用。- A! Z6 s9 r' ?
英汉对照民用航空词典B OEING- [9 o& W8 O9 E" l( D+ Y; k
TECHNICAL DICTIONARY 89
# e- V; q0 w, t. N- ]8 QLAMINATED STRUCTURE, Composed of layers of a
- M0 \ |+ k3 N make a
; U5 o/ m4 {4 zht structure.
4 \: N' E# S$ i- Q.E.D., SEE-LIGHT EMITTING DIODE.! n0 P# e2 z) F ]/ s$ l
ANDING GEAR, The nose and main wheels with the
0 ]2 A: G4 k7 ^% b$ j, fttachments for supporting the airplane on the ground.2 q1 w& [6 E5 `7 [# D# I$ X
LANDING GEAR DOORS, Panels operated by the
; i! M. n% X2 i8 ~* K2 S( [: zlanding gear for closing wheel wells when the landing+ D' Q; @0 L- M" P) Z: t3 m
gear is retracted.& Q6 Z& u0 t/ T4 N. w6 B! e
LANDING WEIGHT, Gross weight of the airplane at the8 @: V0 |' S! Q4 c3 {& |
destination or alternate airport.
, Y: R" U: T/ }6 ]& f m发光二极管,
2 a& \. w9 T# @: H3 |4 f, [2 i3 E见Light Emitting Diode
% I' P* E% C Ycomposite material bonded or cured together to m
& I) e3 [# J. }1 Qstrong and lig
; _: e) {9 W, s. p& ^L
. L5 l% C. `3 yL n, p' \" I2 e" P8 c7 ^" h/ [" X! l
a
, J0 C I/ f& E% D2 J分层结构,
( `1 U5 J) A0 l0 M7 d4 ~- {一种牢固而轻的结构。由多层的复合材料胶合或固化而
1 l9 ^$ m1 w1 o8 Z8 k* S, O- }$ a成。
6 [- d8 c, \" x: Y/ p/ o" Z.
! E/ e d3 H1 _* i! e, K. V( u起落架,
/ H5 D7 G( P, ~2 R用以在地面支撑飞机的前轮,主轮及其附件。2 Z! l. ^8 S6 C8 {1 X* ?5 V
起落架舱门, {5 s5 p- X Y0 s
由起落架操作,用以在收上起落架后关闭轮舱的面板。' s3 e7 r% J$ c; Q" L+ R5 H0 `
着陆重量,
{; k: x9 A2 F飞机到目标机场或备降机场时的全重。
' l' O1 d6 R) i' c, ]英汉对照民用航空词典B OEING# X; u7 y: _* v; N3 H
TECHNICAL DICTIONARY 904 p$ l" `8 {5 U7 ^6 F9 h
LANYARD, A cable for supporting or holding pan
& N* l ~& J8 Y* `open position.& Y7 \7 m; k$ R" n
els in
5 b R ^/ g2 J9 {' Q8 ~" Q0 GAP JOINT, An overlapping sheet of metal, joined to the$ l2 P4 L: O4 X7 s( v
dge of another sheet in aircraft structure./ g1 f Q q; B a1 s8 x6 n
ASER GYRO, A gyro which uses two laser light beams( ~( c/ D5 _, Z' e, y( B
measure angular rotation.1 i3 t( y# {+ r
.
( {/ d/ S' }* a6 v5 S5 wATITUDE, Measurement north or south of the equator
% K5 p& u. [5 G/ h: Ks, minutes, and seconds. For INS equipped
, `) t) `2 \/ pdegrees, minutes and tenth of minutes.
2 q6 g9 i! ^5 p7 a! ~l device for
& O8 K+ V8 n! [hanging stored chemical energy into direct current./ H `) r- @5 X% R. B P3 g
ses lead, lead oxide and sulphuric acid.6 A" c% o5 `1 S* X, j3 E( B
搭接,
, I" y/ K( J( G/ _% k h飞机结构中与相邻金属薄板连接的重选金属薄板。6 ~( t8 t: `* y( o# l
激光陀螺仪,) f- f" v- Z J
一种由两条激光光束来测量旋转角速度的陀螺仪。. Y/ Y a& x' |( A7 M1 C" `
用以紧固或锁定的装置。
) b5 u! R4 X+ N的轴。
; ^4 V, |) H8 ]2 o9 n* M方式。2 p2 U* z5 B* Z% c) j1 j
度, w( L% ?9 G# r9 `( h- Q( z
地球上与赤道平行之弧线。由赤道以北或以南度、分、
; A7 J# f) s. C; q. h: S5 ^. y& H度量。对于有惯性导航系统的飞机则以度,分,和十等
/ k9 K' h' {2 n' Y- t7 ?7 m度量。4 R; |- F" f+ T/ y5 P! l
酸电瓶,
& y7 g/ ^) r" v0 Y* f) f i将贮存的化学能转变为直流电的电气设备。它使用铅,: l9 D, q$ M# _& H, c1 M8 i
化铅,和硫酸。4 r8 } _# [1 B5 x
L
6 k" O4 o& ~; x' `2 q) I8 `; } \; @2 k! we& F- z d# A0 l9 I5 x1 G
L
' e x, p$ g) U- K8 T E/ Kto
" L0 U8 X9 _! y5 Z9 G P4 |! qLATCH, A device for fastening or locking.3 k4 [! [3 z& u4 V$ `
LATERAL AXIS, An axis passing through the airplane's9 d; o. M. D3 }% V' @0 K! T
center of gravity, from wingtip to wingtip
- S1 ]: ]7 @& h' D/ p5 `LATERAL NAVIGATION, An autoflight mode in which
+ t. a' ]: ?# r; N1 uthe FMCS is used to control the airplane roll.
6 c" m$ s) {9 a- \- Q9 w. }7 P0 IL
8 a' }* e8 y( j; N0 \in degree
# j/ t" L: k* B! p) g' p# x8 G- J% ?aircraft in
: I4 n, `* f3 q4 uLEAD ACID BATTERY, An electrica& O2 Z e3 g Z3 t
c0 C$ s0 E) j. t
U
5 m& _# U6 o5 E1 c牵索,* y P4 r# g- M! J- ?
用以使面板保持在打开位置的钢索。
6 g4 H2 o5 }$ i( _- I) k闩,. y/ j' Z; _0 ^9 W/ b3 V
横轴,1 D! s8 h. u: d' W: n2 W
通过飞机重心从一侧翼尖通向另一侧翼尖
& Q6 h/ Z8 Q. D1 h* e9 C9 c s水平导航,
( J$ P( _; x4 y- ]7 p& n2 H& S+ |使用飞行管理计算机系统控制飞机横侧的一种自动飞# j( v% X: N3 ?3 X
行
7 x+ g: y4 M5 L0 R% q, u& F纬8 m( _& f% ^) {+ j% M& F* {
秒. ~6 A/ u/ c# j
分
$ S: y& b3 Z- M0 ]6 K. j( u8 \; I铅/ w! a* v1 N$ o- ~- @, h% a
氧4 k( n" u5 W& @5 g
英汉对照民用航空词典B OEING9 w) j& k3 K$ D
TECHNICAL DICTIONARY 91! ^ D5 Y2 T& B2 n3 @& i
LEADING EDGE, The front edge of a wing, stabilizer or6 D* l; y: U- E$ n4 j
ED, SEE - LIGHT EMITTING DIODE Z& X* J q7 Y" F/ t
EMAC, Acronym for Leading Edge of the Mean
+ R% E" k2 `( P5 w' Cerodynamic Chord.
1 s) Q$ S* v% k" LIFT, The vertical force produced by the airflow past the9 I8 O2 Q! @9 R* R1 `, V. c- u
s of the wing.
4 }: S- ]# P. R/ W. EIGHT EMITTING DIODE, An electronic device which) @$ T( p. w+ `5 W7 h+ ?' L$ Q
tes with red, amber or green light when supplied
) @: ~- b$ H A/ a3 nctric current.4 |$ F7 v& @; T/ `5 p- {
,
5 ?$ |" j8 X& ?1 \1 r: I+ Ycontrol surface.7 ~; } h% v0 r# y: @: A" |$ _! g
LEADING EDGE FLAP, SEE - FLAP- W) k! Z5 i4 Q
L' L) J+ X; z% p
L
3 O) ?3 G, ^: U( tA7 G) A6 Q1 @: o- W
LEVEL-OFF ALTITUDE, Altitude of which the airflow$ b- h8 ^, L0 ~
past the upper and lower surfaces of the wing./ {; H- f, X' k1 s3 W+ x) Q N
L
: V3 ?" u1 |' }% Fupper and lower surface: p `9 L! h' Y$ T
L6 _0 S5 c. V* |( o2 x5 H. N
illumina
. p0 a- o- M/ q4 awith ele$ V' {: [' j: j2 U2 {0 _
前缘,
" T s, [' y' h1 Y机翼,安定面或操纵面的前部边缘。
& ^" g8 y$ V+ H9 K前缘襟翼* K* M! g# A, P5 s$ |
见Flap.
" { u$ J* R4 a1 C发光二极管, g2 j8 T) Y' c. ]. i* L) y. t$ q
ht Emitting Diode4 d. I( l+ y0 C9 K, N% Z
见Lig .
% \3 n/ v: n) R7 m# u均气动弦前缘,
/ D4 t" g9 {/ }0 \ {/ s8 K7 C平均气动弦前缘的缩写。见Leading Edge of the Mean5 o1 @ T0 J7 M/ q3 G8 r0 r
平, G! w" H) ^0 \1 p
Aerodynamic Chord.- q; a) ` @/ U
力,
3 W. K. @/ t4 }过机翼上下表面所产生的垂直力。
/ T( G5 q1 C k- f3 g' h3 s光二极管,
. d" Q% A3 n; o0 s通电后能发出红色,琥珀色,或绿色光的电子元件。
7 i2 |" n9 |, P* w6 |改平高度,( f& l% ^ S5 m
飞机因巡航时发动机发生故障而下降至的高度。; O7 L6 u" x6 f/ Z( |
升) ^/ h' J K5 e0 q& Y" b
气流流
' b! Q3 Y0 b6 e* i发
+ ~9 ~) q" d2 ]+ g; B英汉对照民用航空词典B OEING
1 f5 s% P( m& r- s2 e. w9 ]- cTECHNICAL DICTIONARY 929 o- i# E8 b# `6 M, B5 g
LIGHT PLATE, A component part of an instrument
# S# D! E$ y! j- c4 T$ {' Dpanel for illumination of words on the panel.
7 g; ]9 i* g" u! C, TLIGHT SWITCH, A switch which contains a light. The, x; ^" Q1 F3 \* Z. A1 {6 t" H
opened or) f* l" M! a u0 ^* r- n5 Q: `+ ]
losed.( P/ W9 n; s4 f) @0 v1 y8 ~8 X
n electric actuator which turns off electrical power to
9 E$ E' t' {/ q' t0 f, me actuator when the actuator reaches its open or
w: G# F* f* E2 P, w- C% Ilosed position.) X) ^; n4 m6 a# G3 N* L/ G9 k! ?
IMITATIONS, Performance and operational limits5 s# u, W" t8 t( s2 Q( _7 v
sted in the Airplane Flight Manual (AFM), such as
/ R! D! _. @3 A3 caximum airspeed, maximum altitude and center of) N. o0 o( X0 w1 ~9 _, B
ravity constraints.
8 A! |7 r# F! F% y3 G( Ty
$ U9 a3 h/ x) z, r7 Q% c) b; a4 |craft during line maintenance7 ]6 n$ }: ~/ s4 B7 l2 c
perations.
D3 `, i# Q- V: Z, T% s: |( {ontrol
4 a* m4 M8 \6 e; ydisplay unit allowing control of information to and from( [+ Y \& a1 C! i ^
the scratch pad and designated areas of the display.7 }! j" f6 C0 ^( a
光电门,5 d W6 h. j# X W. n* M2 C& p# V
电门开关而决定灯的明灭。
) J- }" W, ^ _在电作动筒内,用以在作动简到达打开或关闭位置, A" M l9 z- z
时,切断电源的机械式操作的部件。6 w$ H: i' t3 O5 ^: L
各种极限,0 c5 }* B- Z$ d- I# r% `
飞机飞行手册(AFM)中列出的性能限度和操作极限,. _2 t" v3 w/ P) q; E
如最大空速,最大高度,和重心的限制等。& g1 e/ N% p B- G' e1 ?
在航线维修中,可以在飞机上即时拆换的部件。' q- c5 h, b" _/ A/ ^* c9 e7 L
飞机管理控制系统的控制显示器上的电门,可控制草稿
2 S& G% b7 [8 M- @5 D栏和指定显示处信息的输人和输出。4 A, A/ K8 |$ L, c/ _+ C
light either turns on or off as the switch is
/ |$ k* e$ q ~$ `( B4 Z- O( n& @c( i' E2 V R4 S; i( ^4 X
LIMIT SWITCH, A mechanically operated component in
! V# Q' h6 `+ n M4 w# r% ?a
0 Z- d# `; L6 \! f# ith: j1 H! i7 f7 U6 D7 Y3 t8 F- i
c
( L+ j$ t' L. kL
$ k) P2 [8 V& O& p. Pli
2 P4 ]$ u$ Y% H) Dm1 |* v$ S/ e7 G+ I+ e' E4 _
g
6 b6 r7 `( [" M0 q) OLINE REPLACEABLE UNIT, A unit which can be readil
6 X! F/ |3 Y# X4 u4 u" Vchanged on an air v- B7 L! C; ^' J6 Y
o, ]( g# P( M$ v2 z/ P3 N
LINE SELECT KEYS, Switches on the FMCS c
6 O% E1 m1 e( @3 h5 f照明板,% r9 e- p* }. l( A! ]
仪表板的一个部件,用以照亮仪表板上的文字。
$ j- F& g; `9 }灯
) b9 g9 g" r4 C5 o带灯的电门。( h! M1 D) q: u# {& s5 N
极限电门,
$ v- i; y b& n1 ?* d3 `6 W航线可换件,
5 ^1 [! y4 g2 f& }( r5 w: \ H. x" B2 b行选键,
/ C! M& D& _, |: U0 U% ^英汉对照民用航空词典B OEING# J- s# q9 e- } _, v3 o
TECHNICAL DICTIONARY 93" W( t! q& x* K7 ]! n% m4 B
LINEAR VARIABLE DIFFERENTIAL TRANSFORMER, B6 F2 z9 s- L4 y) Z+ ~
nsformer with a linear response.5 B1 e: {' x2 {$ z, ?! C
NAV, SEE - LATERAL NAVIGATION
1 c2 y: }- Q( _, AOAD AND TRIM SHEET, A form containing tables and2 }# u/ p: Z$ P6 r7 ]- @
harts to account for the weight and balance effect of all
# q7 [/ q) v6 M. Wpe of an0 q: s8 w" c& u4 n- w" I# U
S approach, normally located at or near the point of7 p' k7 h- t M' D
ecision height. V$ o! `! o- ]6 n
er
; H Q, y( c, Q1 |9 Y3 U- ^eacon at or near the point of glide slope intercept of an
7 Q, t$ ^8 O, V. wS approach. t0 ?' B, u- T7 }) S
ich provides
- n0 }2 W0 e" p) xlateral course guidance to the runway.
9 s* O* n. B1 z3 f' z3 ]3 q差动变压器,2 x l8 Q+ S, v) x9 m W6 e' G
平导航,' P+ w) H" \7 r* }7 j
vigation1 P c( r! ` R' W. e9 C
A differential tra
/ E- z2 x% S2 BLINK, A short connecting rod for transmitting motion.
4 x. p6 v; A: K1 G# }. s9 cL1 q4 A. O$ q. Y6 @# |9 A
L v% L1 Y& _! u# B3 u) _" U8 Z
c
! q3 @+ a: ~* s* F8 n- G5 _4 h: [# ]items and fuel loaded before each flight.5 U9 p8 X: X1 d+ a& j: G
LOAD FACTOR, The ratio of the lift being produced by* ^' F& X1 r& W* C, R
the wings to the weight of the aircraft., M% |0 z: F" A3 B( n
LOCATOR MIDDLE MARKER (LMM, MM), A marker3 W' Q( Z7 _' \4 _
beacon that defines a point along the glide slo
2 Q5 u! R, p, U' {( WIL
' l7 Y' a5 Y, z9 q( L8 P; _d% S: T6 X1 E% U+ z! E- i8 d
LOCATOR OUTER MARKER (LOM, OM), A mark3 i# C3 E' m: a3 L8 V0 ^( K
b
7 c* j- ]0 s: G4 G, ^$ N/ X0 _IL2 T1 ]/ @+ K5 }
LOCALIZER, The component of an ILS wh( x" ~) ` ~) `; E! y" i; i
线性可变
$ o3 {7 d1 S4 k具有线性反应的差动变压器。* C6 m. e2 h# t8 q/ H% u
连杆,
3 E2 M7 F. T" t连接在两个部件之间,用以传递运动的短棒。
2 z& ^, m% q0 R水4 P" t4 G- J+ u V, a# J$ l6 d! o
见Lateral Na .3 U |) ^' Z. b* J8 R
重和平衡表, c G4 t- f: g; p* v3 i# A
有着显示每个航班前飞机的各项业载和所加燃油对重4 \. j; S; O9 }/ v9 y1 G
衡影响的图表的一种表格。
9 Y. g" a: r: ]5 w, d2 A. Q# y2 X,0 \. z( L/ G2 D
附近的一点的指点标。" B% S' @# w L* i) u9 U$ g
近仪表着陆系统的下滑道截获点附近的指点
8 U9 M0 _$ y" Q; e1 u) R1 j。
& R" ~# T* j o6 z: w9 B M仪表着陆系统中的一个部件。它能提供到跑道的水平航
5 \3 G# F+ D4 A道引导。
! t2 ]! Y6 i- N) m- C载9 U" l: Z6 m( s6 H2 K
量和平
7 v% y( O6 _1 g装载系数. x5 E: M0 I) f# [' E9 w
机翼产生的升力和飞机重量的比值。5 t$ H, {$ {5 P) |6 W) w; _
中指点标,
$ O- Z7 T5 s* E6 G; L9 P+ D用以指示仪表着陆系统进近的下滑道上通常相当于决# z% w/ D; c3 v6 e8 `2 Y, K% }
断高度或其
! E5 Q( Y2 N- D7 }! \远指点标,* P* l0 T/ h5 t: D( V
位于或靠5 N8 I& _/ L3 l- G
标, I. T1 a/ e& v" F! I
航向道,
. L) J9 E) A+ b英汉对照民用航空词典B OEING# t9 \: E. G3 e5 _% g4 ~6 G
TECHNICAL DICTIONARY 949 K5 ]$ ]" Z8 |% q
LOCKBOLT, A steel fastener which prevents unwanted
/ h* {! L- `, m. ~& a% r+ C( Y9 A6 Mrotation by using a collar instead of a nut.7 x6 J: Y, m2 t) y
OGIC, A representation of complicated electrical and. _+ e: i; k9 `0 Z( p( I
lectronic circuits by simple symbols called logic6 l* G6 H9 j" U4 X* d' Q& z- n& w
ymbols.6 X5 D# l9 @" e6 W" J
OGIC DIAGRAM, A diagram that uses logic gates to
# @0 @( Y& p" e2 F* Bpresent the function of a control circuit.1 [) l' ?. ~# o- N# Y
OGIC GATE, A device or circuit which has no output
% ?9 G- a( `: A2 z4 d+ bntil it is triggered into operation by an input signal. A% R2 H; P8 N% ~8 K; [+ I- `0 [
gic gate is an AND, OR, NOT, NAND, NOR, or
* h3 c% {2 G6 d% NLOGO LIGHT, A spot or flood type light mounted on4 J: m- m) E3 e- D3 _& [" J3 ^6 r
aircraft structure and directed toward an airline LOGO or2 ]0 A' f/ Y- n. `9 L) X
other message on the fuselage or tail surface; for2 w9 b7 M" b5 f
visibility during hours of darkness.
) @( ]+ ]) r! V,
4 R# r: _5 w4 D2 ^8 b; O' I钢紧固件。& S4 p/ T5 Q, f* h7 q; Y" {
逻辑线路,* X0 D: o n1 `6 n3 |) B
用简单的逻辑符号来代表复杂的电气电路和电子电路。
) L* N; F! l! I逻辑电路示意图,5 J% {+ K. x/ l
一个用逻辑门来示意控制线路功能的图。! o+ v/ T% @$ C* [3 x4 e/ ~0 t- @
逻辑门,
. R( M% r4 M; V/ P5 |, O只有当输人端有输人信号触发时,才有输出的一种元件4 p# m0 `/ j* l9 ^2 K; Z8 K
或电路。逻辑门分为:与门、或门、非门、与非门、或非1 A# m% k" r' J: y7 E* O
门、和异或门。
7 `) g, C6 t3 ^2 A1 Z4 V8 _标志灯,
; Y9 Y4 U6 b& [* `+ T% ]5 |在飞机结构上装置的聚光灯或泛光灯。用于直接照在机
( M% ]" p* S8 u g8 O% u身或机尾上的航空公司徽标或其他标志上,在夜航时照亮. g1 O5 a8 I, x# q
这些标志。
* g# e' [0 B6 M E3 \6 FL
, Z' T0 u. W4 ^, c6 L- [e
1 r) Q1 x; X/ T- e5 I+ os
) L) h1 j1 Z; S: L, hL
7 Y7 `2 Z- s1 g% _; t& u ]re+ i. l& r6 J; t+ U; U1 v$ A
L" a" s3 G% E4 Q2 u* G
u
& o; t7 w( D1 l. i, q5 v; l. l" @lo
z2 Z4 u; K8 K" b7 m% Bexclusive OR.0 o- M3 b# e/ E9 F( \
保险螺栓
8 p0 ]: E( ?" F U# p. T用环圈代替螺帽以防止不必要的转动的5 o% e; c# I6 a8 ?* w8 J# E
英汉对照民用航空词典B OEING
. D! m! @4 m$ B5 x. m, rTECHNICAL DICTIONARY 95
7 c# M8 A8 R0 n4 G" v- LLONGERON, A structural component in the horizon/ @. H# a7 E* X5 \
direction of the fuselage or nacelle.$ w) {6 x2 u; [5 `. N! [
tal* a" h5 k9 B+ t5 R$ j! y
RUISE (LRC), Cruise speed that is
% n# R \: U6 J0 J; {, `ssociated with fuel conservation, producing fuel" c1 d, G+ t4 F4 e% M0 K
ileage one percent less than the maximum fuel- D6 L0 l2 M. U
ileage available.
; @8 m3 X( K+ c4 S8 RONGITUDINAL AXIS, An axis passing through the) l- O6 s& l. r; \3 H2 B% r
irplane's center of gravity, from front to rear.
i4 r6 e h b" l" y" ]not
7 X+ ^" c! [# w& Z, a, oOUVER, An opening with slots allowing the passage of
, G- ^: I5 v) N6 @远程巡航速度,
, v/ ~& _0 T9 `2 R# |! B一个与节省燃油有关的巡速度。在此巡航速度下,每0 f& A1 f* s8 ^' [
一单位燃油所能飞的哩程,最大的燃油量航程小百分之
6 M. N. r* K2 U5 K1 e一。
l$ o* |6 @+ A: L纵轴,
# I& }* o4 v) ^/ v6 ^由机头至机尾贯穿机身重心的轴。
1 l& N5 U" R7 q' J) r叶窗,
, x2 P4 n" x8 j+ l. H有多条缝的开口。! ~; H1 L, x9 A& i# p
LONG RANGE C
* |) e7 E5 w- ?* s/ wa
3 M( ]" n: ?1 u! ~, R5 w# Bm
" \ O$ B, O% V3 N0 L) Q8 C! Xm! H3 Y. b7 q% P( ]
L) R5 U# r: L4 G9 S8 Q# s
a: e' d7 E$ `" \+ z3 P
LOST MOTION DEVICE, A mechanism which does
4 J2 M( h3 R1 R: O' @& |operate a component following initial movement of# v$ p, m& H1 P0 r8 c8 X- ]
control input.
/ P, T4 a2 {$ b! [/ i, w+ ?0 y9 QL
+ S1 o+ N- v- Q6 U8 }% U& Mair.
' i K* n2 N, `9 L# C! r大梁,
! Y* @. A9 B0 }- Z机身或短舱上水平方向的结构部件。
4 A( d' D0 e/ w6 O航2 x# z8 u" @( q- v8 T
比
) E4 I( [' T, R6 ?/ V; g) x空回装置,& m! T6 I2 G& [7 I3 e: m
在控制输人初始动作后,即不再操作部件的机制。用于2 H: J) E5 I9 b& t5 ^
飞行操纵系统内,以防飞机指令互相牵制。
$ o! ~7 ]" b, x" g% b百
/ ? M8 ]4 _5 ~) o7 o让空气流通的
, v8 P8 \# F; i5 J7 l$ C) y8 r英汉对照民用航空词典B OEING
( H4 ~/ j' H, U! eTECHNICAL DICTIONARY 96
% \ D$ o/ c% r3 i8 HLOW RANGE RADIO ALTIMETER, A system that
( }% Q$ v3 u( F9 F5 umeasures the vertical distance from the airplane to the) O3 s& l& Q( |1 Q ]) t. I
rrain.; [. o. \3 \% } |% s( U
RC, Stands for Long Range Cruise speed. Represents
- n( H4 W; u" ]8 ie typical cruise speed for a given jet airplane; usually9 S5 M( Z7 j N: t" a) M
xpressed as a Mach number.% q D# K/ [2 q0 a/ \' C4 w6 v( d
RRA, SEE - LOW RANGE RADIO ALTIMETER, x" x t" `5 L5 l
RU, SEE - LINE REPLACEABLE UNIT: s! O" @: M4 w; u2 v
uce friction# T4 }; U6 g, |9 v$ _( v
etween moving parts. It can be a natural or an artificial
; _6 W8 O- f) |) B3 U9 Saterial.. \$ G2 r1 Y. w \0 m
AC, SEE - MEAN AERODYNAMIC CHORD7 j$ v" |# p5 Y
ft's true
1 R Z& s7 F2 q# q( P1 G) i( r9 \* G8 Aairspeed to the speed of sound at that point.
1 s8 v8 ~- }& q' S的系统。
4 x9 [, Y) T8 U( Y, M+ Y远程巡航速度的缩写。代表喷气式飞机常见的巡航速. |( J1 n, s. K, l
,通常以马赫数方式表示。4 [9 x5 W$ Y3 d! y9 S" d1 w( U. A
空无线电高度表,
. @) x% `4 Z9 s' m" F5 kRadio Altimeter( [( H: U' {" m7 U% I6 C6 K8 a; g, Y
te. c7 z$ x# y3 m$ i) ]7 }
L2 E3 |& A% Y7 L4 w
th9 l4 ~- O7 J9 B) u+ ?- Q
e P G; Y9 W2 o( E* T) ?4 a
L
3 @5 c( N& L5 s# [4 B+ W- |5 yL$ M4 e/ |2 y m% s. i# i" v7 T) s
LUBRICANT, A substance used to red% `1 F6 R9 T/ O7 b
b
8 J$ Y! R4 B9 l" U) _m3 {7 X& z6 b$ e/ V6 C* ~4 N8 j* v
LVDT, SEE - LINEAR VARIABLE DIFFERENTIAL
7 i# n* o; c$ b* PTRANSFORMER7 r7 M& g1 \3 C; U6 e+ W: T
M7 h* R3 s: \9 r1 W# S% Q
M
. v0 S$ ^& t: T; ?' B3 J- eMACH NUMBER, The ratio of the aircra- v/ ^" F, ]+ d% c" [1 w% P7 X) G$ R- n
低空无线电高度表,
: d5 N6 R+ S4 W; P! t3 ]一种测量飞机至地形的垂直距离" j3 {; g$ A+ {6 }4 X% }
远程巡航速度,/ m( [: t8 h) }, q$ e) K# t
度6 T9 Q6 O: Y( Z9 u- @9 F
低( P& X/ _' _9 T j
见Low Range . ^. s# G6 e* ]9 F. O
线可换件,, `% T5 G! I. {0 B1 F4 u
见Line Replaceable Unit K d D% W( Q& D% ]1 C0 { }3 F
航/ @+ x% Z+ A6 V' H3 `
.3 Z6 b/ D+ C$ Z9 f/ x* S
用于减轻运动物体之间产生的磨擦的物质。它可以是天: r& n; K0 @- {2 w% `
的或人工制造的原料。0 c4 o2 C& \8 l3 m1 l
见Linear Variable Differential Transformer9 B! C' H4 B+ V7 P
润滑剂," w" n! E/ |- g6 \) p8 z& w& z% d2 [& U
然4 j0 x y$ T( A
线性可变差动变压器,
; j5 V% P+ G; _( J& e6 M" n- y.1 Y n: k. U. \; E& T1 x
均气动弦,' s# M: t# l) |1 G5 N. R
见Mean Aerodynamic Chord
+ G( ?- }' C2 h- p平
5 t0 e, Q* F# n7 l8 A4 J/ Q.
! Z9 G: D, P$ s; u7 }! P# K$ f空速与该处音速之比。! t$ n; Z6 b+ ?4 O
马赫数,- [' t; l+ c( K
飞机真
! u2 A& m0 l" m3 M5 N! P1 i& A5 {3 h英汉对照民用航空词典B OEING% t' ^3 h7 @% C: s, P( o B* N- k
TECHNICAL DICTIONARY 97
: }( J G: `$ \MACH TRIM, Correction to airplane attitude (nose up)- O8 |" d8 y" v- X+ i
during flight at high speed by using the horizontal: K. {; M. \' v0 H+ E5 ~$ e% L' r4 G
tabilizer.1 p! `$ `- q2 v5 ?& p% g s. N
AGNETIC HEADING, The heading of the airplane3 [0 g: f7 k# f" B
lative to magnetic north.
* F. o& H1 X/ H$ r% v1 R! oAGNETIC VARIATION (1), The difference between
; x6 q {& u: t/ Sagnetic and true north.
( Z9 ]9 s3 n) J u O# _8 ^* i% D; Knorth.
* a2 w* q. D5 A7 L! mhere is a continuous small change of direction2 ~- U6 t5 m8 u
f lines of magnetic force over the surface of the earth ,
% u8 Z8 F3 v3 |0 Q2 R8 }agnetic variation at most locations is not constant over
- r$ _5 X& r* @" o7 Fng periods of time. Lines of equal magnetic variation, P6 \+ R& t" @
e. (see/ j* F+ O) ?4 Z4 m! t
tation Declination
0 y% y0 T3 v/ v9 os' `& N" t, }& `, K9 S: R' ~
M/ M- q5 k4 p: F' g/ G$ ^9 S0 S
re
/ x i( E* E4 m( z G' tM& {1 g' h3 s; f. @/ N. X
m
! L2 v/ y. [! t8 T! ?MAGNETIC VARIATION (2), The orientation of a
' U" K, t( O! B# S0 W/ C9 E! ahorizontal magnetic compass with respect to true
! ?3 e0 j! Q/ u% g$ |8 t; ABecause t! O' G) C6 E0 `: F& Q# y0 x
o. E: t2 ~3 Q* W; O
m
R4 U3 K b$ g" y9 Olo
$ K% R2 l2 A* z; S(isogonics lines) are updated on Jeppesen charts every
+ d4 b7 I5 g" A, r4 xfive years in accord with worldwide practic/ L/ s2 [. t' l5 ~* y1 k& A' a
S ).
: l+ Z! N/ d1 @7 q- SMAIN ENGINE CONTROL, A component on the engine
, V6 |& U) Y8 Q3 s9 B6 G& aration.
4 V* n* e A5 N$ T+ RMAIN GEAR, The main wheels with the attachments for; S2 F* Y5 U, U5 r& u
supporting the airplane on the ground.
+ r# A" S0 e0 u/ ^& N9 ^MAINTENANCE, Work accomplished in support of the9 F0 y7 c9 q# d
structure and systems of an aircraft. It includes,
" G4 s, d$ I% Binspection, overhaul, repair, preservation and the
2 q* {- R; a+ t+ |replacement of parts.
, N; `1 V0 Q# P0 W6 m( A. F$ _马赫配平,
+ D( @4 F& _4 S6 W% h( e用水平安定面对高速飞行中的飞机的俯仰姿态所做的! Q* q6 C8 j; f9 @
调整(机头朝上)。: H3 z5 V, {% H. d
磁航向,
" j1 f S$ X: ]8 ]" S3 r8 X7 I相对于磁北的飞机航向。8 j( j N$ }2 @
磁差(1),
3 ^$ t& W( K ?' R% \真北与磁北的差别。
$ O; d; N" o" B+ u: P, {断的微量改变,磁偏角在长时间内多数是不一致的。每5 H$ b5 {' [- w
五年Jeppesen手册会按照国际惯例校正等磁偏角线(等
! H. z a- g: T5 k" u. H B差线)。(见基点偏差)# J5 ^( i/ g% _( F: r' F+ o
主起落架,, x7 c I! l- P. a) |
用以在地面支撑飞机的主轮及其附件。
: A0 {- j) E3 V% K/ |5 G" M" w维修,8 i4 @( a5 S8 H# G/ F# ?3 X$ V2 L R0 g
在保障飞机系统和结构时所做的工作。包括检查,大修,
; M) L, ?, `# z6 r修理,保养和部件更换。$ B F G b* ?# T% k; S$ q
for controlling fuel flow for starting and engine ope
4 \! |$ g+ a* p- j磁差(2),
2 z0 l) p2 j& [' E8 G相对于真北的水平磁罗盘定位。因为地面的磁力线在作% h" D, s" T* u0 j; k$ c' I1 _! \
不
) D+ V+ s9 S: M0 Q磁+ W; l" o' Z: L, b
主发动机控制器,
: P4 a8 }* i2 e9 M, E发动机上为发动机起动和运转控制燃油流量的部件。
& O2 z' @ C) a' V2 `. m英汉对照民用航空词典B OEING. U( J( G8 Z* L* |. A
TECHNICAL DICTIONARY 98; d) i# L1 Y& g
MANEUVER CAPABILITY, The ability of the aircraft to
) {0 f* h6 w1 `. N! Xertain load factor.
# [% \7 ? E' t4 l4 F9 AMANEUVER MARGIN, The amount of residual0 w( h2 M) K$ }2 Z" f5 u9 m+ y. ?
aneuver capability present before the onset of buffet.# E4 e/ O6 j+ Z9 d' w+ k# N; ?0 y
MANIFOLD, A duct or chamber with several inlets and
9 J7 E* `6 j. f! W ]) h+ ooutlets for air or fluid distribution.% C; _. h1 p, Q
the) ~3 y% n' H3 M @! {
low of3 e m' z9 b( g( X
e flight compartment. On specific
6 _ T& X! D! v' b5 F+ iccasions it will provide conditioned air.
+ C7 r; E5 Y6 B+ komponent by hand.
) P) p( E `- v) J; M( Y0 |7 ?' PMANUALS, Books with instructions for proper. n5 B5 H# z+ q% P% x+ s, Y: O
maintenance and operation of the airplane systems.4 |/ c0 w! i2 T
MANUFACTURED RIVET HEAD, The head of a rivet' G- X& |/ I1 s$ ]# M9 {0 l/ {- ?7 U
that was preformed during its manufacture (see upset: ?' {! `2 n v) Q7 p. {# o Z
perform certain maneuvers up to a c5 C ^6 W5 e+ z1 N$ d
m1 k2 X0 q# u& G; K) P' T* R
MANIFOLD INTERCONNECT VALVE, A valve in5 P9 v4 L2 C1 |; l& }/ E
equipment cooling system for providing a normal f
) b$ e2 Q# M2 Q; ~0 J; Arecirculated air to th
1 k1 R( F) w" eo
1 Z d; r: l' t$ H) {% v; Q5 i( V/ `MANUAL OPERATION, Method of operating a
6 Z( Q9 T. Q" r. fc
) M5 r4 m+ o4 t3 \head). D5 p6 F8 h2 g2 F% C
MASS, The quantity of matter in a body. It gives the
' _( l$ k) ]" Ybody weight when it is exposed to gravity.
7 g5 z8 Y! _0 G, t6 R- E机动能力,2 w, q/ B; E3 G- S
飞机完成装载系数达到一特定值的机动动作的能力。; ?4 o! q* b' b2 l! X7 U) C- m+ D( G
机动性余度,
2 a5 k& S2 X$ F8 y( l飞机在遭遇抖振之前,所剩的操纵能力的大小。: o8 `, @" T6 M; l
总管,
9 C. h( k4 c6 \& Q用以空气或液体分布的多进口和多出口的管道或容器。
2 t( n7 P/ ?8 t3 ~/ Z总管联接活门,
5 m4 }# }$ c) [8 t0 x6 O设备冷却系统内的活门。用于向机舱提供正常再循环空
$ _" K" A4 ?7 }( g/ D/ R气。在特殊情况下会供给空调空气。
8 ?( q0 C! n( S' l; y人工操作,+ n' U7 |+ M3 {9 S* U( l) ^
手工操纵部件的方法。
0 f) I. f) y! | I+ w明书。8 ~. ^0 I" z: u8 l. |. u- n
铆钉头,# X9 y' \/ z ?( z
在铆钉制造时已定形的铆钉头。(见膨径头)。3 Q) C: A0 S$ C% Z
质量,4 Y! R( w, K) Z1 {
一件物体的物质数量。当该物体受到地球引力时质量产$ V/ z- j; G9 ~) s/ H$ |
生重量。
0 C) i$ c2 l, W: _& ]手册,
0 T3 }2 n0 j$ I% j为能正确地维护和操作飞机系统而编写的说& q) X: g ^+ u# R( n7 k3 t: o
机械制造的
0 i' W+ D9 q# ^( E0 j+ F英汉对照民用航空词典B OEING% F* w* @+ N6 Y, W8 C2 H" P
TECHNICAL DICTIONARY 99
9 V* q* I) F4 z/ J& S8 e% `3 GMASS MEMORY, A memory that can store large
- _. I& g# c# C5 |amounts of information and hold that information, F2 V3 b5 K0 K) J5 ^3 J
permanently.- h- {0 W8 e6 Y. R' j* h
AX CLIMB THRUST (MCT), Maximum engine thrust
. S' N! g# L. ~- t* `# Uximum engine
$ m( n5 h" S. g5 L- _9 Y+ G! }; @rust to be used continuously when one engine is
* O3 [/ H- h. e. B6 O! Toperative., j) j! }6 N0 [$ ]& b
EOFF THRUST, Maximum engine thrust to be* C* B; M% _ Q' ?8 f( X5 N5 H; U A* V
used during takeoff.' N6 a. c+ D) E( o" J$ c( n
FF WEIGHT, The maximum take off. ] \9 c7 k/ U) r( a
weight as permitted structural limits or performance/ ?3 u9 T! V- \* b4 j
limits, whichever is lower. S F4 @" I2 ?" F; T
RANGE CRUISE (MRC), Cruise speed
1 p6 ^9 ?6 l" E1 B* eance; y3 a5 C! R) B* n/ X3 J
to locate" V/ ~* ~3 V3 n8 U6 Y; V# [
the Center of Gravity.
- z5 [6 C$ S- f3 c# S主控台,: i. c& g' d, X
控制系统操作方式的装置或系统。: y/ ^* k- U: [
大爬升推力(MCT),
1 K9 U' R) A" d* e飞机爬升期间所能用的最大发动机推力。# [1 v9 W- R* p. Q
MCT),$ k5 H' H2 @5 L% c, ]9 x
当一台发动机不工作时,可以连续不断地使用的最大发
7 P4 { _3 o u& h动机推力。
# |+ f. ~( k4 H# Q7 j# _- a; r6 e起飞期间所能用的最大发动机推力。
) ?* d8 \$ g$ G结构极限与性能极限两者中的小者许可的最大起飞重
1 h& P c$ r! v7 z% `。) k" h. L% w% i2 n
大航程巡航速度,
% {# r" q1 g* h2 p$ ~最大的巡航速度。
( ]& K2 n* N' i. b a8 m [* K( r平均气动弦,
5 Z2 K. n7 z2 b$ E% q, G6 M确定重心位置的基准
( c% M; x# i( o3 T距离。1 z: X" S1 E9 z' d. H3 ]0 ?
MASTER, The device or system which controls the
1 @2 [9 D { E3 c, Tsystem mode of operation.
) T1 \9 g6 B% h; eM
! ?! O" C! I, B+ Fto be used during climb.: J8 s$ c* a! O: ?
MAX CONTINUOUS THRUST (MCT), Ma
' v# P2 j- Y9 F4 _& V$ Z- }% cth* [0 O2 n* N& }9 p- d
in
+ Y* [; V. O! v: e( e$ M5 c/ nMAX TAK
; j3 M. f p- T0 r0 p; |, i9 fMAXIMUM TAKE-O
8 }3 @5 T* \4 a1 n7 l% z( q+ u8 NMAXIMUM. c3 p' K( C1 h
producing the greatest amount of range.
% ~' W e! g+ WMEAN AERODYNAMIC CHORD, Reference dist+ z2 u/ n; q9 T5 C$ r. n
located at a fixed position on the aircraft used
; H: {2 w$ O0 t" K, Y2 U大容量存储器,0 k) q! }5 q" n5 c
可以储存并能永久保留大量信息的存储器。
! {* E l' ?7 M/ o+ Z2 l+ b+ J最4 N& c$ k5 H4 k% k; b6 S- E
最大连续推力(
3 t6 D6 ~' ^- f/ o. t( Y最大起飞推力,
: i% N" D( [& R, g# Q1 c最大起飞重量,6 {3 Q7 n8 g K9 W. q6 h6 ~
量: u7 G& r7 R" D
最
+ R2 U8 g6 {. h/ Q, X# H能使飞机航程
9 D- x9 G5 B7 C( q. b# P' t* K位于飞机上一个固定位置,可用来3 I6 L3 v9 i' x0 `/ v. L3 B8 M
英汉对照民用航空词典B OEING
7 F$ y1 f/ `9 F# W4 W1 STECHNICAL DICTIONARY 100( ~* I/ s' @+ c# C, k% ~
MEC (NO. 1), SEE - MAIN ENGINE CONTROL+ O6 C0 L) G3 ]* p3 Q# Q
MEC (NO. 2), SEE - MAIN EQUIPMENT CENTER
# ?- a( J1 O, Z' t- A2 [EL, SEE - MINIMUM EQUIPMENT LIST0 U2 | y3 Q+ p- e) V' e j" h
tem the memory is where
, i w; E9 h- H9 L; ]formation is stored.( ]( f2 \% j. R; m
METER, Any mechanical or electrical device that is
7 d1 v0 k3 D' L$ ?: vair or
7 _+ \' D, e8 Xpoint along the glide slope of an ILS approach. It is
* P$ U4 X! s3 z* q5 ]+ H, K7 V2 ^0 lnormally located at or near the point of decision height." u4 @+ a; y" d1 w$ _
,
, Q+ q* [; x" O8 l1 A见Main Engine Control0 G$ q- n. I- l4 I8 M/ ?
M
0 x" D1 Q- l& L3 EMEMORY, In a digital sys$ y/ Z6 k1 V$ _3 o! Q8 l( O/ b
in- ^ D; O2 `' `1 {' N/ l
used to record, indicate, measure or sense a specific
- H* |0 F7 M, q) E5 t6 o r, fportion of an operation.+ F2 N$ O6 N, e7 l9 ]1 X
METERING VALVE, A valve for controlling flow of
& l3 w: R( g. R$ T; s2 efluid.
) m- t7 |8 F( X+ F/ sMICRON, A measurement of filter effectiveness, one
0 ^2 Y* D$ D$ w% Q6 r6 hmicron equals one millionth (.000001) of a meter.; F6 Z, u9 w, `0 u7 i; l
MIDDLE MARKER, A marker beacon that defines a3 U+ s* _2 J2 \* V, t
发动机主控制
+ e8 I k3 y$ e- w7 G$ ?' ~9 X.
9 h/ w' r: k! t# p g设备中心
6 H/ v: t. m' d) v见Main Equipment Center7 z7 ]9 [* N. \9 ~. j
总% S8 I1 A1 `0 y' P Z f, ~' e
.
% Q l. Z% R; H8 D! |低设备清单,
! ]! O- N- H' O8 v1 ?+ V见Minimum Equipment List5 W+ z% D" d5 w
最3 M4 O8 [2 K0 ~# p* G
.
" E2 i9 b8 M! {在数字系统中储存信息的地方。5 e; ~. @2 {& p: m/ I! Q
计量表,& T) G6 l6 f ~! \" N
用于记录,指示,测量,或感受一操作过程的一个特殊7 D; z) H8 S7 {2 Z5 i
部份的任何一种机械或电子装置。4 o3 q/ w1 W7 Q
量活门,
7 A) N9 @0 a! u+ w% Q& h( b用来控制空气或液体流量的活门。! l+ Q! r" Y ]% m# m
微米,
7 S! B$ m# q4 j7 c& n- Y过滤器效率的计算单位。一微米等于百万分之一米。
0 t8 \/ Y i' B- t" `( n6 y! Y在用仪表着陆系统着陆时,用来确定下滑道上一点的指# e; w- I# K3 K f
点信标。它一般位于或靠近决断高度。. H. R0 O; X n$ q4 ^ U
存储器;9 `. k8 P* j8 V8 U; c$ @
计
1 y V+ `3 a" ]" `' g" w中指点标,
' G- c6 n( V3 U4 Q% W英汉对照民用航空词典B OEING
2 f0 r* a% k3 d k" X0 jTECHNICAL DICTIONARY 101! e6 {! M: J' N- R" {4 B
MICRO SWITCH, A miniature mechanical device that- l g& v( v& Z4 D& g
completes or breaks the current path.5 b2 g9 `9 p6 b6 H/ W1 C
.
2 [$ X" Z7 f: d* k C* gMIL, One thousandth (.001) of an inch./ L) M2 k# J4 M4 M/ r( v# c
ILLIBARS, A unit of barometric pressure equal to
( O! U$ B+ T/ P$ b& h) M8 Napproximately 0.75 millimeters of mercury.
5 ]9 T1 `; x: x3 H; w, c9 CThe lowest
! t6 m* b% d5 R; hltitude to which a descent is authorized for a" @2 D# k, `2 v5 a5 G1 J/ V% f% z/ \
onprecision approach.
& P* E( p3 ?8 x/ eINIMUM ENROUTE ALTITUDE (MEA), The lowest
" f2 H! s+ [5 ]# n kublished altitude between radio fixes that meets- F) [4 i x( K) O' E/ r" E
bstacle clearance requirements between those fixes
, g# h# A! s9 Wand in many countries assures acceptable navigational* V2 t6 ~) K1 c) y' P9 n0 D" P" z% V
signal coverage.& G+ |; e( x5 H! K
operation of the airplane with certain systems or7 N; b! P( }( [) q" E' g* d
subsystems inoperative.9 I, M7 l+ \" H) j, O, C
approach/ j! n/ c& o2 S' B# n
cannot be completed to a landing and results in a Go-
. W1 U3 N& S1 |: EAround.
' N& _. _7 _# P' ]一个能形成或切断电流通路的特小型机械设备。* q% b0 i- R x( L
话筒,
) | T1 Y/ H* o9 r" L, N |* O话筒一字的缩写。
6 J# o9 m: [# f' F3 r9 U耳,
. M, C; a" T# W$ Z2 Z) M一英寸。1 \0 ]: {, ^( {7 e
毫巴,
: S; O+ M: `. v/ g+ D9 Q一个度量气压的单位,一毫巴约相当于0.75毫米汞柱。
0 z; P6 d( f+ s* f. U3 S" _低下降高度(MDA),
- \$ ?: G9 X! @飞机作非精密进近时所准许下降的最低高度。0 n, x& ~2 H; y( v& a9 J& {% I! q/ ]
低航路高度(MEA),
' v( y0 `% z0 K8 M在导航用无线电定位点之间,符合越障要求的已公布7 f8 h6 D. U) ?: ^' O; E
的最低高度。在许多国家,最低航路高度保障了合格导航" {9 M0 y, Z" R0 C2 F
信号的接收范围。: i/ a! P y0 p0 b6 t/ B
最低设备清单,
" }, g- n/ U; N' I! ?何6 m7 M! S+ {9 R% f/ a6 |. _3 _, z
作飞机的文件。4 e! Q+ q$ g% x* @1 c% `
复飞(MA or GA),% ]8 P) o0 e, a7 s
飞行员因未能完成仪表进近而导致复飞所采取的一个
- o* S5 N. i D机动动作。" G: q2 d# l, |$ T5 W9 f
MIKE OR MIC, A shortened form of microphone1 `6 {/ }9 u: Q/ n6 [( n
M' m, ?: e, O0 W, h' q2 C
MINIMUM DESCENT ALTITUDE (MDA),
7 }! C! o) B% N5 V! R' L( fa
5 ^# w4 K* E2 n; `" r7 In+ U! ~# V' N) M
M
! s" h9 M" F" g: \$ m! Ep+ D/ A+ B. h B- H2 `! e
o
7 Y8 m- ]& L9 e* w" s3 n/ h& qMINIMUM EQUIPMENT LIST, Document prescribing$ V* l( P) U; `. f( X
MISSED APPROACH (MA or GA), A maneuver6 a% |) d1 W3 l0 k, m5 R3 @5 e
conducted by the pilot when an instrument: W* w* A3 v- Q8 Y) V6 F. H
微动电门,
7 ]& \) n: j" ~3 V% U% `密
) a/ i' A* t% V6 f/ E千分之
) {9 Y+ z! h: l. p5 w) |& P最8 S3 t$ ^6 ?" s( o/ Q4 Y" `
最# T, Z O: V3 T1 ^' S1 l1 T4 @
指定飞机在某些系统或子系统不工作的情况下,如5 x% {3 X/ u" p& B
操
1 y9 s& \6 V. E/ Q: A3 I. i英汉对照民用航空词典B OEING5 S4 Q, W" a( ~+ U U
TECHNICAL DICTIONARY 102
! K# ?# F6 L! L. w6 w& ], L' dMIX VALVE, A valve assembly with two or more
+ ~# \$ I' R- W' v% Z0 J: M; |individual valves used for airflow distribution in air
1 r2 ^2 b8 o7 B* c$ Astem.7 }4 E4 Z6 \# }) [ v2 ^2 p+ r
MMO, The maximum Mach number at which the aircraft
) Q0 ~4 z) R) |% q# fMODE, A specific operating state or condition; i.e.,
. s' X# P P# PAutopilot mode, MAP mode, etc.( d. ^, _8 W& m. \, f+ d. P" X
e" {3 {) G" j# P# z# p" R# j
MODULE, A housing that contains related system
" z: I9 N$ x! J. _4 K/ SMONOCOQUE, A type of construction in which the6 r3 Z7 i; ]% I, e( Y
ONOPOLE, A speed sensor that senses magnetic
+ u+ x( w( j- L. epulses from a magnetic nut or gear teeth on a shaft.
% O1 ^4 X: {# z- y5 G. Fhe controller.# x7 [3 U# M5 s% x7 G
MOTOR OPERATED VALVE, A valve using an electric
0 b6 P0 [3 |: B4 G' _* ~motor for opening, closing and modulation.
% C; f$ K3 y, Z/ g个以上单
, ~% V4 Z; O; q' ?' V8 C活门的活门组件。
+ s0 C5 b* e4 M- ?飞机可使用的最大马赫数。
7 i7 x6 B d' T6 }+ Q式,MAP
3 {$ a K! }; x3 x0 @. M方式等等。
# X' X {" \: W, ^ B调制,
& u5 l6 W% t4 M; N) O组合两个或两个以上的电子信号,使一个信号随其他信9 X4 l" g }4 s7 w- L
号的变化而变化。4 g3 ~0 y; l$ y3 ?% ^/ Z
组件,
' ?# r. K* N0 X! {/ R( r极,
/ N# s$ r% T+ H& k) f帽或齿轮轴上的磁脉冲数的速度8 A) ^0 c$ S2 o1 [$ C4 M5 }" ~
/分钟。9 d$ V) c2 ~8 s1 ~" E7 p! M
用电马达来开、关和调制的活门。* {! i8 E7 }& P p* }5 A
conditioning sy
1 S: n/ L3 o0 r8 l' umay be operated.+ C) d' N, y; L
MODULATION, Combining two or more electrical
2 l( Z* b9 |! j; ksignals with the result that one signal is varied by th
5 a3 F* s# g* a& a3 a3 } L$ U% w, yothers.4 W1 M3 w9 K9 c3 d9 S7 ^& g2 B
components. U o3 P0 p$ L3 Z( {
fuselage skin carries all the loads.% E7 V) k$ k9 v- r8 a8 w7 Q) E
M
! O/ n4 Y8 y$ J0 kThese pulses are interpreted as RPM by t+ g) k2 c, x9 u) d! E
混合活门,3 [7 b9 S. i* L, P7 ]+ s- \$ U
在空调系统内.用以气流分布的具有两个或两
# b7 X7 ?# A) P5 r/ N" q体
- p# q# [# V% ~7 r& |7 fMMO,
; U8 q- R) ~. L* J. i6 z方式,
' o% `& |8 [% K9 O; [* r一个特定的工作状态或情况,如自动驾驶方
7 ]' U6 A& J6 @' x: o3 I* P内装相关的系统部件的机体。
0 a3 \) n, u% H8 [& S+ J0 @7 Z4 \6 x硬壳式,2 m2 B# w& d# s, ]$ b: |+ q
机身蒙皮承担所有载荷的结构形式。, l4 E& ~+ L6 X
单$ h; ?( I+ l* ]: r" k. _
一个能感应到磁螺
* U! n* }+ I8 X感应器。这些脉冲可由控制器译成转6 q" \2 [* U. N6 x: d9 n
马达操作活门,$ u+ Q4 w) z& P! Q$ X
英汉对照民用航空词典B OEING
6 W/ n8 m" E7 Z6 I) \" \/ ]! nTECHNICAL DICTIONARY 103
. N: c+ V/ g$ mMSL ALTITUDE, Altitude expressed in feet measured
3 d* b7 D2 a6 uom mean sea level.
0 N p1 j7 x- yreducing the noise of the airflow through the pneumatic! Y" y( [+ f3 o) Y2 l: s, i
duct.
+ m+ _- O. }/ {, h0 Q; gMULTIPLEXER, A device that allows two or more
! [& e# P5 z6 ~signals to be transmitted simultaneously on a single
5 O+ }* z5 c6 C) R- V1 {; s: ~2 `carrier wave, communications channel, or data bus.
' l. K" e; C$ @, `essure compressor rotor.9 B% m0 y6 a) i5 w
N1 BLOOM, A change in engine N1 and thrust indicated" o/ t5 C! ^8 y: e% A+ g" \4 }
N1 gages and detected by the autothrottle BITE/ J5 J' n* l/ ?2 I5 E* c
during throttle hold operation.. O; o/ @3 b6 H+ H7 `* h8 w z
N2 , High pressure compressor rotor speed.
5 \2 V# N! h" m( ^ACELLE, A streamlined enclosure on the wing or
1 n7 @% g$ Y/ ?. J5 y面量起的高度。1 [& |! k. Z( `% n" `. N0 ~
经气源管道所生的噪音
; g9 ~# e8 l" T* [7 h A5 @的装置。" |; W5 U9 \ |! \3 ]
多路传输器, T, v; D. ~4 s# z
一个能让两个或两个以上的信号同时在一道传送波,一" c* S) [9 ]/ a) \9 v/ N# q: W* @
条通讯线路,或一条资料数据总线上传递的设备。
. C* ]2 S% T# s/ ]0 j9 k! m. oN1转子转速,( A2 d7 t# v$ L1 w! @- T3 R7 Y
发动机低压压气机转子的转速。
* _4 ^+ D+ a6 ^+ \+ R! e+ _& X- u4 tN1激增,/ M( |( @* m! c
油门保持过程中,在N1表上出现的由自动油门自检探
) Z7 G- T4 V. C2 E7 _测到的发动机N1和推力的变化。
4 U \( g, J* uN2转子转速,! g8 m: I+ g3 h7 v1 l
发动机高压压气机转子的转速。
2 J0 z7 U# K: b; n2 ~# G短舱,4 Z% J7 P, a2 w$ o
机翼或机身上为安装发动机而用的流线形壳体。3 ^6 T4 o& K3 o- T/ F. R5 m* s
fr
6 e1 ]7 W/ r. D: R. l1 p- AMUFFLER, A device in the pneumatic system for
! R) o! q% ?5 X6 o+ V1 E NN {1 p3 z+ Y$ r* n) ~" r
N1 , Speed of the low pr
( D+ R A3 S' Z# v( Oon the
$ T% f& F) l: ~N3 D+ D# d9 K2 e3 O5 i( Q
fuselage for the engine.. |8 x7 z Z; {, U. [$ G. k: K
平均海拔高度,* a6 M: J- P* ~8 ^6 R. A
以英尺为单位,由平均海平* x% `- o* @# }- E' s
消音器,) s2 `/ A4 q7 E) _' q: h
在气源系统内,用以减低空气流, z' r9 p" ]2 }4 p. u% c
英汉对照民用航空词典B OEING1 G# U$ Y+ i: R: r% b1 e$ ?
TECHNICAL DICTIONARY 104
. h- [( n+ c% z2 ? {4 PNAND GATE, An AND gate followed by an inverter to
* E, C7 ?+ g9 K0 }9 Zform a binary circuit in which the output is logic 0 if all5 {# {. A9 Q) x
puts are logic 1.
. O& S$ a: x/ c/ f7 p$ wAUTICAL AIR MILES (NAM), The actual air distance# H- B, `: v* W6 q# D$ X
respect to a
# X4 t& y: H P9 s- ptationary object.! e) i+ ^) H: s* M' E5 e |8 U$ ?% p
istance
: n2 N# L# s$ Z. H" |1 ftravelled in relation to the ground expressed in nautical& V# n/ x" F$ }8 X; x5 p
miles.
% Y6 h3 t; A( Z2 @* T9 c0 i; o7 wnce equivalent to 6076.1 feet, \* I; C6 g: x7 K: w# G
r 1852 meters.4 x+ T+ Q! o1 o' Q2 K
hical1 i* s/ l; x7 c% F; `& b* q
EGATIVE LOGIC, A form of logic in which the more
3 [7 J$ M. n& nnegative level represents a logic 1.0 \( Z. Q5 j4 V
EGATIVE RELIEF VALVE, A valve in the
+ j. P0 Y1 G) }5 I0 j5 u, a* Ue to be
5 u% i. s% F3 B+ Jabove airplane altitude (or cabin pressure to be below' P5 e1 i* {+ a- J" Q3 t
ambient pressure).
2 C9 j3 o9 B5 r' U6 C, P% d b5 C有
% o& x9 {. t7 A# |* @人为逻辑1时,输出为逻辑0。* A( O; m4 w: j ^* J# Y% [
海里(NAM),& {+ w7 Z5 X$ \7 g. E' ]& ^
来表示的飞机在空中所飞过的实际空中飞行距 E9 b3 H5 I% t. x6 w. c
地面物体。/ M4 V! s6 G0 j( L% e- ~; f# F
以海里来表示的飞机相对于地面所飞过的距离。
/ b8 ~9 _! B. T/ G2 n里,/ K2 P, r: x0 v+ T
相当于6076英尺或1852米的距离单位。
2 H9 s% l$ N M! }导航,/ x4 G- U; P. H
反逻辑,5 Z. \; B8 r8 f4 Z; l- S
正电压水平越是代表逻辑0,负电压水平则越是代表逻
, S3 Q0 y' I' l0 m/ f; E ?释压活门,
; L2 Y7 M, ~- `8 [" M- P0 u增压系统内,用来防止机舱高度超过飞机高度(或机舱& ?" l2 d2 g6 T8 s* `2 c
压力低于外界大气压力)的活门。$ w4 {7 _+ _# [& l d5 O* k
in
% }" `/ s- `( P$ h' z/ C5 jN( W/ P O1 a& ?
flow expressed in nautical miles without
1 n! q0 d9 H, l. |$ t# Fs! z1 i+ N- e7 |2 w. b
NAUTICAL GROUND MILES (NGM), The d( c3 t1 z* |" N
NAUTICAL MILE, A dista+ t; ]2 E* W) h) v# i
o9 I+ e# q8 E& c
NAVIGATION, The art of determining the geograp
D# W3 l Y- D: A: I* Cposition and maintaining desired direction of an aircraft
I8 o: {7 n* V' O4 [+ o) ^relative to the earth's surface.& J9 T- |( m( S0 }
N4 V8 m2 \# P9 N; y1 w
positive voltage level represents logic 0 and the more0 G5 C9 U! | \8 [8 Y- S- ~
N
. J, u. n' N# e) Y& rpressurization system for preventing cabin altitud
: W, I4 G1 y2 z6 x% R6 y: R3 J7 o非与门,
+ P. P; l$ a1 w- `在与门后面紧跟着一个反向器的二进制电路,当所
. J) A0 }9 y5 y! W2 P输
8 F, `2 _- Y ?2 U% q空
, d# c" d' o% k6 B# ^以海里% B6 k, K7 ~) o- @7 G. B8 p& ]. y
离。空海里无需参考
1 D& Y U- J6 t! _5 N' A地海里(NGM),$ v" V' R* P- }+ Q
海 B$ |5 Y& m6 }
决定飞机的地理位置和保持飞机相对于地球表面所希
" E( x$ W; X- p- e! X望的方向的技术。
" G( U& v6 i1 f# u辑1的一种逻辑形式。% Q% W4 P0 h. i/ F, X# g' H9 ~- i
负
) j d$ ~. F* g英汉对照民用航空词典B OEING
y+ q6 a0 e/ h: c5 b1 C2 M8 iTECHNICAL DICTIONARY 105
J# x' K9 q7 {NEOPRENE, An oil and grease-resistant synthetic
O2 r" }5 I8 ^4 P) u5 ^rubber. Used mostly for seals and self lock nuts, etc.' q4 u# G: A/ y% B* r3 M) r
EUTRAL SHIFT SENSOR, A sensor used for
0 W$ G8 E+ E# T5 i1 o. U1 T2 [NET PERFORMANCE, Aircraft gross performance
. i1 @% C, B" \) ?! v3 b6 q1 Icalculation/ {! ~8 |2 m5 y% Z/ l5 S. C& H1 C$ R
purposes.1 e9 G4 k3 C6 E$ j* H7 P
NICKEL-CADMIUM BATTERY, An electrical device for
. P% d7 V. E8 Z! A9 mchanging stored chemical energy into direct current.# N6 C1 j) x: s* O6 F% t; V3 e
ses nickel hydroxide, cadmium hydroxide and) Z1 o0 g7 l1 V
otassium hydroxide.% i) o$ H& g8 z3 A6 M- {* k
NOBLE, A term used to explain the properties of some, F6 M$ C) E) ]% F
lements that are chemically inert or inactive.: a4 D! s3 s5 T. H& Z
NOISE ABATEMENT PROCEDURE, A flight path and
$ o/ m' U' F) w- ?$ }limb profile designed to limit noise in the airport area.7 X* R2 m5 r0 r9 _7 s _# I
construction. (Nomex is a trade name.)/ R7 k- H A) P; M/ k
in only ^% ]+ K! U1 `5 n; O1 L3 E0 M+ i4 r
one direction.' v' W0 ?8 a3 Q! G
氯丁橡胶,6 T6 m L6 {# g" Q
一种耐油和油脂的合成橡胶。多用作密封装置或自锁螺
) ~% D: G9 U: y7 q帽,等。3 R, P6 L0 k1 z |9 l, M* u# O
立变换探测器,
7 ~, z; D+ `3 R2 A4 X `- N( N用于探测升降舵和安定面配平状况的传感器。% O* r v' h5 ^0 {% ?+ Y6 a
性能,
; y. K4 R% n$ }: w1 [( F机总性能减去由当地有关单位为了使性能计算0 {5 ]: }' O: N
较为保守所定的一个量后所得的性能。! p* J/ } Y: P% A2 m% E
为直流电的电器元件。它使用氢氧化
' R' c1 y* _8 f! J3 I( g% |、氢氧化镉和氢氧化钾。
* c- b& g: ~+ a. B; c性,8 U+ A2 h4 b/ M3 i3 V
用于解释有些元素不易起化学作用的特性的名词。6 l; F4 {! J, ^5 S
低噪声程序,
" y W5 K' v/ L2 N' l一种为降低机场地区噪声而设计的飞行航迹和爬升剖
P, {4 l, X# C2 W0 }。6 s8 X0 [$ P* M5 s) B. ~1 [
是一种类似纸的材料,用以制作蜂窝结构。(NOMEX
' Y# k9 U9 E/ F _4 z商品名)。
f5 z8 T. W- B5 l5 L8 C4 V只允许向一个方向流动的活门。
: b: O/ p! w6 e; o, qN
, ?+ E- Z. |! x7 o* S5 K& u" Zdetecting the elevator and stabilizer trim condition.4 t! R7 J0 M+ d/ n
degraded by an amount determined by the local
9 z, m8 R" u5 F# j& l1 v! Rgoverning agency for conservative- Z# h, |1 s4 N% d! K
U
" i% a1 t8 h/ ep
! g7 b- `8 c' v P$ Fe
F' l6 ~$ @5 Fc6 T7 n2 W& R7 K: h6 ~( v
NOMEX, Material similar to paper for honeycomb
3 ?5 x( c* z# d. @NON-RETURN VALVE, A valve allowing flow. I3 Q& B4 v" [- O& }1 T
中4 `# P/ Q1 i7 X# G- V! I: i- Y
净
' b% i8 G4 n( F; f以飞
( }) I4 Y/ Z& J8 v镍镉电瓶,- b! U5 Z! b g6 n @
将储存的化学能变3 p) o' d, [+ Z* [1 X3 K
镍
% ?; |( x0 g S1 B# J惰1 m/ C/ p8 z( m+ }$ a+ y
降; P: ^# @$ M$ v+ [- P
面: S# y6 @( }$ u
NOMEX,
. t6 |( s2 W3 e* A- g是4 K7 Y# M& e ?* r% J, s
单向活门,
% q2 p9 M8 J. @+ U9 A; g英汉对照民用航空词典B OEING
5 e$ C0 F) E& y, Q2 ZTECHNICAL DICTIONARY 106# p. x) d8 q1 X! o% F: G
NONDIRECTIONAL BEACON (NDB), A radio beacon9 W# J/ i, ?+ T* z
which transmits nondirectional signals whereby the pilot5 w& }) [$ J H; C% r$ r! E
can use the ADF to determine his bearing to or from the
8 Q" O, u. W' v' kstation., U, d9 S4 X! {/ z% e
ONVOLATILE MEMORY, A type of memory which
6 I! C3 Z& I4 C7 i- rdoes not lose its contents when power is removed. c) n9 G: v9 I6 W3 v# O" h
rm
1 z; s l& T( r2 y" l; W& Pbinary circuit in which the output is logic 0 if any of the1 ^6 W9 S. O4 g
inputs is logic 1.
$ j& w0 q; q. c! s) [% XNOSE CONE, A device on the front of the engine that
9 K0 `' {7 M* Q, C( Kguides airflow to the primary airflow path of the engine.: A8 D7 B r; V8 M4 q/ K
the nacelle for air inlet to
8 K- T K2 {# S, b$ ?e engine.
0 |+ o* b/ x, P8 K0 Q5 C$ k) [OSE DOME, Front section of the engine for
6 N4 H+ i6 \$ Etreamlining and directing airflow to the compressor.
; U* o1 C7 O- O$ { F, d6 u% l z),
4 n) H0 M! b. K* _4 W能够用自
7 R8 y) w; v$ s6 P$ }& i定向仪(ADF)确定他的背台或向台方位。
3 k) h& G- p5 h5 }% T8 T) r8 ?. q久性存储器,1 a7 a1 `) f B A$ g% \3 u; L
在失去动力或电力时不会失去记忆内容的存储器。
- W( R0 v) d, l: T, z* X在或门后面紧跟着一个反向器的二进制电路。当任何一
; X+ R5 _0 j7 E输人为逻辑1时,输出为逻辑0。8 Q8 b3 ~# P) X! x6 S$ q
一个位于在发动机前端,用于引导气流通过发动机的主, _0 @* l5 l2 @& n
气流通道的装置。
, H b- J+ \4 H X- V引导空气进人发动机的短舱前段。
, z% x$ b2 b+ q% R/ ~部整流罩,
8 X6 l0 f9 o5 h% F用以整流并引导气流进人压气机的发动机前段。; u! u$ ^- T C1 P0 @
N3 \: X1 B8 A9 t8 z% U8 e
NOR GATE, An OR gate followed by an inverter to fo
+ j( r6 E- H m; q7 ?) e- T6 {7 ja
o# v7 J8 k. { mNOSE COWL, Front section of% d% u8 Q( W1 b C# B" `
th* U6 S# u* N* J3 R+ [3 p# |
N! U8 j( z! E1 f% m5 i/ r
s
/ a. R* ~( M# \7 h& M- n) M: [无方向信标(NDB5 g8 ?3 f" C+ G |, k
发射无方向信号的无线电信标台。据此飞行员+ i6 U7 R' Q& N/ z0 \0 D, L1 d, Q
动# ~7 ]! }1 v" |# N& s/ e
永. k% H& l8 K) O# D* Q) X E
或非门,0 @0 [$ b8 e; Z6 d$ D
个% W$ j# x; h# a. b8 l8 M
进气整流锥,
; a' [. `. C9 m% u L9 G前整流罩,
+ t% s4 b7 x) d* R y9 B+ O头
/ `2 Q0 l3 x5 s! T5 b+ \# `8 |) w英汉对照民用航空词典B OEING) L3 u/ @$ s& y6 n. P1 W
TECHNICAL DICTIONARY 107 f* i( Z9 s& _1 c/ N
NOSE GEAR, The front wheels with the attachments for$ {1 `! J7 v$ t
NOT, A binary circuit with a single output that is always5 b q9 d4 i% L# i, z x
opposite of the single input. Also called an inverter.7 l% a6 v. ?$ u) I2 K& ^5 P$ n; @
tion that has the shape of a "V".
; a& S5 ~8 |4 P9 vt.3 L% z w) c9 d4 `& j& R% \3 |
O-RING, A circular shaped rubber or synthetic material1 C/ P4 k g- ~! s
sealing device for pneumatic and hydraulic systems.. k# ~8 g8 O$ y0 Z. H" `( ~
PERATURE
% V3 F/ `* R( ~! P& x8 We
" Y2 }: j, D7 R. Q3 {& f5 Gin the path of flight.
4 o% j1 T* t* f5 [0 e$ g4 g" Q& HOBSTACLE CLEARANCE, The process of flying the% l; H: s) y9 `+ s" V n
aircraft over all obstructions under the flight path.
5 b5 |- s; G4 D, i8 f* e2 Q% `; ZWhich obstructions are considered and the amount of1 `5 }8 T/ {( a8 ~& j, U$ [& v, @
vertical altitude required above the obstructions are6 Q, L( ~2 M7 H" L$ i
determined by local regulatory agency.
( @" d6 d& D9 r% N非门,7 k3 |6 q: @2 t9 B) A' E2 c/ @
带有始终与单一输人相反的单一输出。也称作反向器。
, x; l _; z1 \7 A0 \( i一个“V”字形的缺口。6 o4 k& |% H. R5 x, r
喷嘴,) r+ g/ [0 [- e
形圈,: n+ u9 u# {) X7 {* h4 T/ j
用于气源和液压系统,圆形的橡胶或合成材料制成的密
& Q' V2 v& u; E _; \# \封装置。
# m' |6 T% i' [- s1 Q外界大气温度,
4 B( C- y, m% U! Q9 }见Outside Air Temperature
) b* P% i$ {6 o) w. R3 ^supporting the airplane on the ground.
' ?9 k F( e" O& }: R4 c& B5 \5 CNOTCH, An inden
# e$ E! M; ]1 K5 h" I& }NOZZLE, A shaped device for directing flow in a duc
6 d+ M" V4 }: f2 V2 j' UO
/ n& X, n( ^$ ~! X+ ` iOAT, SEE - OUTSIDE AIR TEM
" i5 ?2 l3 L9 M4 K6 w! uOBSTACLE, An obstruction protruding into the airspac
6 u3 N% z, W% U" W' x f& D% I3 p) K3 @前起落架,6 T; U& l+ U8 _( W; K3 d
用以在地面支撑飞机的前轮及其附件。2 E9 q8 P$ y, m3 l+ j, U, H
凹槽,& P# I$ ]. v p' Z1 [( m
引导管道内流动方向的具有特别形状的装置。# v. b/ ?4 R0 j* i1 ]$ y
O
& @9 I2 a$ t. a" V4 P.$ _/ M; {" T. s% {. H+ T
越障,
0 L! |- U* U7 U9 H/ h' Z道上所有障碍物的飞行过程。障碍物的选
- ~( @( S* u D2 V4 D0 r U择和飞机距离障碍物的高度要求由当地有关管理机构决/ ~, \& M# L% {7 `) J
定。
8 K% r" J. u( Q' E N7 H- w1 s障碍物,% w8 Q: Q' Z v# d9 [% e
进人飞行航径上空域里的障碍物。
- g6 {% W! `( O3 V飞机飞越其航/ I' ^: n. f4 u/ z
英汉对照民用航空词典B OEING5 @3 }2 M. ?8 _* } f: @- ^+ e
TECHNICAL DICTIONARY 108
3 U' z4 _; @6 q; L! XOEW, SEE - OPERATING EMPTY WEIGHT1 j2 x% \5 }+ {0 |+ @
FFSIDE, Opposite side.: E; D; [8 f9 x1 t9 N2 h# x0 F
IL COOLER, A heat exchanger for cooling engine oil
" \& l, |' ~* iby fuel flow or airflow." o, p- ~% Q z4 y- S2 r
ATOR, A device used to separate unwanted0 p" @: a/ ]1 L0 u$ T! ?: y3 Z
ir from engine oil returning to a sump or oil tank.
) N; Q _% A) U; Q' ]" o* W+ mOIL STRAINER, Type of oil filter.
" e0 y- ?, I# t/ m0 v0 aLEO STRUT, SEE - SHOCK STRUT
. u. P2 T0 e1 F# n C5 {, MNSIDE, Same side.( n# y7 G( M6 D8 s- K
ll weather navigation system.
7 |6 P6 n0 g8 j# ych is not
# M0 y- |; s5 Fcontinuous from power supply to ground due to a break A$ S4 h2 R' _6 Z, N% a
in the wiring or failure of a component." I! {% [! c% v& Y2 ]
见Operating Empty Weight
; [3 M7 ]' e v R8 d$ B' ~! jO# d! y+ d/ V/ | d7 R2 `
O
p/ |4 ?- h* m2 K$ aOIL SEPAR# y! Q) \: g! [* S# Z
a
$ J5 T c' i6 Y, s. _1 @O
" {# f$ \) m4 v; M, @O
2 Z6 d: N# \, \4 nOMEGA NAVIGATION SYSTEM (ONS), A worldwide,% ]" ~5 A, d% |9 w B& a. r
a
! g; ?& m5 ~5 w4 QOPEN CIRCUIT, An electrical circuit whi( j k/ H! ?2 Z8 M
使用空重,- p# L' @% l& L5 X
.
5 _ j1 ]+ S: z/ n/ A# h面,
% y* w2 [2 m! q! P7 r# z% S8 _油冷却器,3 I3 Q/ k5 W: S( H' m7 O
利用燃油或空气的流动来冷却发动机滑油的热交换器。1 O' \! k- g) @6 {9 N
油分离器, H6 x% q7 D$ h& U; Q) g
一个能从回油槽或油箱发动机滑油中分离出不需要的1 F% ^" u6 L. _
气的装置。
6 r; p6 a+ F Q; g$ i滑油筛,/ |/ a1 A& w7 {1 R6 i9 A. B
滑油油滤的一种。
+ e6 B( `* u% M' ?液减震支柱,6 Q+ A2 A. f" {( o
见Shock Strut6 ~1 X# t; g2 {- v9 i% n
反% O& `& {$ t# [1 Q- K" g
相反的一面。9 c- B# k) k0 W' l a, }1 v q- E A
滑
v2 X/ W8 X9 q, Z5 g滑# r* R2 ^7 T3 a9 a" d4 r0 {. G
空$ a5 n$ Y1 \' \9 W
油 g N/ F' ^7 q. ^, f) u
.
! W V$ X0 i9 D( K5 H7 _8 M. T面,. Q0 b+ j3 e! d( I, h! d2 W0 [) I
相同的一面。
" p& b5 H; Z" A* r# u4 R+ o7 @7 c个全球范围内全天候的导航系统。
' W' b5 r4 P7 w6 M: c或组件损坏而导致从电源到接地点之间$ ^9 F t3 s1 i3 g% i6 z
不通的电路。
! A# Z; l- X4 S) e同& f9 I5 O) V |1 R# h% }
奥米加导航系统(ONS),
3 L! P$ O2 L+ [; {- }. L6 \一
% j' [; t h* C$ D( U/ s+ E& g开路,
6 S- `& B. w, r; u' l+ n3 N由于线路中断
4 y. E+ F q% \3 R" d4 N y6 a! K英汉对照民用航空词典B OEING$ K1 y+ t' O6 z7 m
TECHNICAL DICTIONARY 109
8 w% @+ b( q5 n& z' L5 fOPERATING EMPTY WEIGHT (OEW), The weight of
' k U( `2 p3 t) ?, Ian airplane fully serviced, including the crew but without& v; F' M; W- N5 J. T6 [( O
fuel and payload.) ?4 L' k ?, [- `5 w: A3 ^
PERATING ENVELOPE, Defines the environmental5 D( A) W) ^3 O4 {7 I) I
OPTIMUM ALTITUDE, The cruise altitude which results+ @) L2 D$ X8 U+ B7 \/ m
in the best fuel mileage.
' i0 g% B9 W2 D5 X, IOR GATE, A device or circuit with two or more inputs of
5 w6 r4 f% B' v& z# o1 Pbinary information and one output. The output is 1 when( {6 f/ C( s/ ?, P o$ e# s
any one or more of the inputs is 1. The output is 0 when- C9 K6 \' r0 V8 O! k1 Q# }2 r
all of the inputs are 0.0 j1 Y% X+ f" A
ORIFICE, A specified size hole in component for control: ~+ C2 Z5 Z7 f: q& C5 j9 S" x
of fluid flow from or to the component.
, z2 I0 V1 \2 s' w7 ?$ vORONASAL MASK, An oxygen mask covering only the
" S! y; F, g- i3 q- Z. K; S, d i# hmouth and nose.
2 w0 j8 W' s8 x" f* B" Q: cOSCILLATE, To swing back and forth with a constant
; `1 s! r' p7 M7 f. F& L( Xrhythm." m/ ^6 S$ }+ T) {" o0 ^, W7 s1 s
使用空重(OEW),
/ n. j& A6 J+ D% |4 R3 o使用包线,
; `3 j: j5 ~! e: W确定飞机准予飞行的压力高度、温度和速度的环境极
' E9 `( r8 t: \! o- x* z或门,
- e6 _' j" t% K* P. F具有两个或两个以上二进制信息输人,和一个输出的装
+ c) U1 h8 V- a% `" q; M# i/ {置或电路。当输人端有一个或多个为逻辑1时,输出为逻 }2 k% D8 w3 k6 z3 ~/ A4 V
辑1;当输人端都为逻辑0时,输出为逻辑0。
- g0 e# g z. d5 U, n量孔,& ^5 _0 C4 j6 C4 z8 h9 ]
部件上用来控制流往或流出该部件的液流的尺寸已确) @. X3 B# s" m$ a# i
定的孔。
! [6 `$ X6 n6 }, n9 a" b4 b口鼻罩,- _0 h$ {, ~2 ?+ m6 v. k2 K
仅罩住嘴和鼻子的氧气罩。# h& l8 [5 A7 p7 f
振荡,& D/ C- Q7 r$ k1 @
以恒定节律作前后的摇摆。% ]! g1 l( T: u# y9 q
O
% |: g" k: G4 Olimits of pressure altitude, temperatures and speed
" k6 k$ T/ d fwithin which the airplane is certified to operate.
4 p7 o3 `+ r8 W ^# G8 p4 k7 a一架勤务完毕的飞机,包括空勤人员,但不含燃油和业: |; v- K+ A5 Y1 l: D; I
载的重量。3 z+ A3 @& g+ O; f) q; q* p
限。/ O1 x' k. W) n6 c2 ]
最佳高度,
% s; Z' E! R9 h$ M可获得最佳燃油哩程的巡航高度。
! K5 G+ L7 u5 y3 ?( J8 D+ [英汉对照民用航空词典B OEING4 X. Z ~' j4 j3 ~, ~% q
TECHNICAL DICTIONARY 1104 k- w0 v" J) y- E: P
OUT OF DETENT, A condition away from neutral or a' K# G7 D) D& v- x# T; d
OUTER LOOP CONTROL, For autopilot operation this) r& B4 g! v* u# c! n
is control of the airplane's flight path to a target./ R6 |! y; r: r/ l3 }
Examples are control of heading, altitude, and vertical; M# `4 l% h$ W7 p% C) `
speed.1 v6 K2 _# g8 R# s( {
UTER MARKER, A marker beacon located at or near
4 A' g. B7 j4 ]* T0 me glide slope intercept of an ILS approach. The OM is3 t! v8 I- m W4 L8 I+ A) T9 e
normally located four to seven miles from the runway8 `+ L' R$ w. H' P0 @
reshold on the extended centerline of the runway.
5 O: L5 o1 K$ D: y& eW VALVE, A valve in the fuselage for; O1 _, q( _, K
g the airflow from the fuselage to ambient for
7 b q& b2 j( d- ~; V, O, v# z/ z1 Wation control.# t6 l5 u) d, `& a
UTPUT, An information signal going out of a system or. t3 e( V& Y1 q$ X T' m
part of a system.
& Y: x. n% j4 t+ R( IUTSIDE AIR TEMPERATURE (OAT), Ambient, or free$ _. o/ e ^. p3 I
OVERHAUL, To return an aircraft or one of its! M) B. a0 k& i( `0 S9 K
OVERRIDE, Operation of a component by a method
0 \6 Z7 [- C7 S. Edifferent from normal operation.
/ e7 U1 r. L- q1 ^0 C1 {- v4 T操纵杆离开中立或槽口位置的一种状态。: d" G7 d% |0 I1 u" {
制,1 d/ S/ ~8 P! f* E
航向,高度,和垂直速度的控制。
% N) k9 l& o9 F- K7 c指点标,0 r3 h2 |, }0 ~% h5 w: J$ `' {
位于或靠近仪表着陆系统下滑道截获点的一个指点信
$ f! `) R: ?+ t- ]/ S标台。它通常位于跑道中心线延长线上距离跑道头4至7
- x3 A% H& q( P# M海里。4 l+ t8 a7 a( x8 A2 w5 s
流活门,! L* R; I3 i7 ?7 W( k! G
机身内用以控制从机身流向外界大气的气流以进行增, o+ @& X1 v" V5 s4 Z
控制的活门。) J, l: x c7 H" d' ]& ?2 t
输出,: ?9 r. T ?- i* y/ Q) @; m
从一个系统或系统的一部分出来的信息信号。
# ]# [! w# O5 W; n5 D" Y界大气温度(OAT),
( f/ N7 I5 R2 h! c# H5 x外界环境温度或静止大气温度。# T) n$ Z# ^! m
修,
" M/ g0 P/ L& s/ L将飞机或飞机部件修整到近似全新或制造完成时的状
% W3 M" E I; ^ b/ k+ L- M! |超控,
, N6 B8 O# ?0 `3 B' o用不同于正常操作的方法来操作部件。
4 o: [1 m5 D7 r s, G5 e$ m5 unotched position.
/ ? ` d9 o3 {9 BO
6 x$ L8 B! C7 G/ D: gth6 R; H) c+ w) @+ b- u$ v
th8 P; ?; ^, }& l! C& O9 U
OUTFLO
8 t0 D6 F6 K! |! e7 D' `controllin5 j: y1 \- j' ~3 b) @" ~: z
pressuriz
! v0 g/ y N4 G* ^O
0 W+ d- A& x& X4 `a
* {: @, _; A( e: P# XO- Z# s5 M4 h4 l' v3 i' R- ?' P
air static temperature.+ {4 k# Y3 z: Z* m; V% a8 A
components to a like-new or just manufactured6 D5 c8 @" X E4 m( Q7 K
condition.2 I" P* M$ f: K, k8 U
脱离卡挡,& i7 N9 y' U- q
外回路控# V5 X' T8 @) |$ C6 _9 |
用于自动驾驶操作的对飞机飞往目标地的航径控制。例
: \8 Z4 @" v0 Y S如3 R) I& v2 ]) A# C4 ~
远" T4 W4 c- a* |# W' ?: z4 q5 o
外" ^" p6 g0 e+ Q! k- G! l9 Q
压; [& m4 H4 s; H2 T; y5 I( y
外! L* a- r1 {. N% r
翻; o. v& E) m" }* f8 b
态。
9 q& E) k' f7 \( l7 n0 t英汉对照民用航空词典B OEING
4 {0 f Q- }7 r4 M0 @7 ETECHNICAL DICTIONARY 111
f" \, }4 }5 P; ^P
) m) {$ M4 h8 z4 QACK VALVE, A valve for supplying air and controlling
+ k2 e# K8 G9 z3 T& K! Gmanifold to the air2 ~2 J! w; a7 B& j/ W, l
onditioning system.
/ D( n; T2 m1 i! K! \/ cll piece of any substance or
8 M0 V/ Z e: E: R! [physical matter.
# F* D7 ` _1 E4 r6 z* o `2 Rh
! Z+ d8 Z# i7 f3 G+ E* Qrovides flight crew and attendant announcements,
5 T; P! Q6 n6 z" R. L9 ~oarding music, and chime signals to the passenger
+ E; ?$ ~" k$ g. i- Ycabin.% f% o, b; e) y9 {0 `
ASSENGER ENTERTAINMENT SYSTEM, A system2 e4 O6 s/ ~" ?5 B$ z
tertainment to
& Q" I9 X6 z& c, E8 z6 q# ?e passengers.! s3 z) d4 n) X
PAYLOAD, That which is carried to the destination,3 K* `3 m ?" a1 Y0 ~
uch as passengers, cargo, or mail.6 o' x+ u! H8 K( c+ K
CA, SEE - POWER CONTROL ACTUATOR! D# U# T$ S3 h. n
PDCS, SEE - PERFORMANCE DATA COMPUTER
0 c5 l( I3 w, WSYSTEM
: { {' L+ D7 B2 X* X调组件活门,' i/ Y! O1 ~' S7 q4 L' m
由气源支管向空调系统供气并控制该气流的活门。7 L$ R2 _# w& C' Z3 Z2 `1 V
任何物质或实体非常细小的一部份。
~5 h6 _, b. _! c) B旅客广播系统,
) S3 A1 V8 k2 p7 ]+ z能使机组人员向客舱进行广播、播放音乐和发出谐音信
2 J+ x! {$ `, X1 A& A- D的系统。5 q2 o2 Z, s3 T* K) r3 |: ~0 ^5 ~/ F
客娱乐系统,% P1 t/ f" O( S' f
频和/或视频娱乐服务的系统。
) w4 ?8 Y4 L7 e由飞机送往目的地的载重,如乘客、货物或邮件。
b, O/ M. t" S( E力控制作动筒,
3 [. S& @3 O! b/ Z W见Power Control Actuator
& p5 H+ x! d+ p# T6 y1 S; M$ L! iP
1 B! H8 `) k# v* s& V- b( uair flow from the pneumatic# ~1 l4 b: v+ y, ~5 t9 G
c
9 s& X$ e. ?1 o3 t7 TPARTICLE, A very sma
! A9 r$ Z( Q# \6 e5 P: Q4 e, B- MPASSENGER ADDRESS SYSTEM, A system whic# }" ]& B; x9 Y2 f. P
p
* }0 x% d M9 Q2 Eb
' @& M% @) T) EP* V z3 @0 ?; M- d A x# W
which can provide audio and/or video en
$ K) _- Z) U2 [th
6 i5 Q' A" v/ n) V% x. s* Vs( ]0 A H; p& e3 ~0 E, N
P
+ @; u5 N6 \! }PCU, SEE - POWER CONTROL UNIT
$ P) R7 x$ R9 \3 u! |( L8 p空% i5 c* p$ g* H4 Z4 t: v
微粒,
( N- T0 W; L6 u; V. `/ V0 G( J号) a+ _' s& y" @8 E3 |4 w0 p
旅1 G! E+ J6 v2 u! J
向旅客提供音2 e7 C; F" |/ d6 P
业载,
6 l/ G/ k3 i' P1 M& S% T- O动
2 Q9 |. ? o# _( p( u5 ].
0 b& H" Z4 y9 @( \Control Unit
) o8 t! O/ R; ^& w; @; w! E动力控制组件," A% c% f' ]* v' s1 c, o) H
见Power .
3 r& c$ L' |0 k3 b+ V性能数据计算机系统,
& Z* r8 l$ M- @, t4 |. c$ U见Performance Data Computer System.
! ^: P9 e7 Y z0 t9 |英汉对照民用航空词典B OEING
5 I$ S9 @' E4 ?; w8 j8 K; g! iTECHNICAL DICTIONARY 112$ `2 Z* y# I5 O, b" @7 q+ U' h
PEEN, To cause a more corrosion resistant surface by0 @9 y7 S6 d+ r2 w: @
multiple impacting it with a hard material such as steel
- Y9 }" u( h* V1 e; M9 y2 Gpellets. Term for this is Shot Peening.; C: T3 I- {. R
Defines a position on the aircraft relative to the mean: Q) \6 f2 l [( }4 P( {5 k9 b, O
aerodynamic chord of the wing.9 L( V/ h, j( k3 A! T( q( O
r as a percentage of a fixed
% m k, X# ~/ gmount rather than revolutions per unit time.
! t$ L, p. C; L+ c ^+ Mamount.0 g; ]6 u4 |' s p7 p% C- v$ M
ERFORMANCE DATA COMPUTER SYSTEM (PDC,: F& Y, s9 X( W x$ D8 a
PDCS), A device which provides data to achieve the
) C* N1 u" g( E, P9 Z. `most efficient and economical operation of the airplane. A" b* j; v1 R! }" [7 `, `1 T
PHASE OF FLIGHT, A portion of flight specifically
& A* [" C6 }8 \4 ^devoted to accomplishing such things as takeoff, climb,2 `- _% u+ R1 D/ A, }) P
cruise, descent or landing.4 _4 f9 O/ j! w9 O
这个过程名为喷丸硬化处理。
# f+ Z3 x3 Y* a: I2 I平均气动弦百分比,
* i* V3 X0 ]& I* `0 K& v间转数来表示低
6 b5 f7 X# a V8 C; r6 D+ T, \1 k压压气机转子的转速。' \' Q5 o% o% }* W: {. M
性能数据计算机系统(PDC,PDCS),& L/ k1 I( R) t8 d: e1 h9 K+ U: s
一个能提供数据,使飞机达到最有效和最经济的操作的$ x6 y/ w+ N" c" w" q% g% Z) T
置。
u' z/ k) i: J/ L; w$ Q行阶段,
* H: | u# t P% o+ q) ]& {. H% ~; c3 l飞行中负有一定任务(如起飞、爬升、巡航、下降或- P9 a& h6 f1 y( z: @% \
份。 k, N- f. Q+ k; v& ^. y6 E
PERCENT MEAN AERODYNAMIC CHORD (% MAC),' X1 p$ B, C2 e0 c! X0 z' c
PERCENT N 1 , Expresses the speed of the low6 @3 y% S7 ~+ z- X# V
pressure compressor roto
* Q/ J9 l# L/ |7 }' ma
" q5 r: n: X( y# {PERCENT N2 , Expresses the speed of the high. E. c* O' a; c# Y9 I8 u- k; u n
pressure compressor rotor as a percentage of a fixed
) G4 m y, o3 gP. l: {, |+ ]% \% i& G
喷九,$ `4 H) o' Q. t* }. e |
为形成防腐能力更强的表面,多次用诸如钢丸的坚硬材. h- X1 [) \. K
料冲击表面。
% N5 q1 ^- W( A用来确定飞机上一点相对于机翼平均气动弦的位置。
4 \3 ~2 j2 ~) k7 tN1百分数,
6 B0 N8 [4 W* x以一定量的百分比而不以每一单位时
# e. W, }5 s: ?( |- v3 D6 oN2百分数,- n7 j" ]2 ?- V6 v9 k+ n
以一定量的百分比来表示高压压气机转子的转速。
! B- i+ ~$ b2 S( J: Q2 Z/ e装2 k. a' M, C& w: |
飞
3 O* z4 ^9 _( @; q2 R着陆)的部* Z S& v8 o7 @8 H$ e
英汉对照民用航空词典B OEING7 t( [- B2 W: t+ |. p/ _$ j% U& F4 [# v
TECHNICAL DICTIONARY 113* E2 G* q2 U4 K6 ~$ I5 g
PHILLIPS HEAD SCREW, A cross point screw with two5 p; t, O2 \0 U2 S4 f0 L8 h
en with a flat tipped Phillips head W% ^' m# d! k
crewdriver (see Reed and Prince)." }; A; d! P7 e7 G, c/ @* b4 `
ITCH, The rotation of an airplane around its lateral' R* D9 X+ ? x Z
xis.
# m9 w# a& q! m$ z a& Hne$ u- H& r1 v& f1 @
ose up and down movement controlled by the
" w3 A* X; P, O* h" mlevators (and stabilizer for trim).
) h4 A( m" o M( o5 k! C0 x8 XITCH RATE, The rate at which the airplane moves in
) M2 n: W7 I& n+ r! A) we pitch axis (nose up, nose down).# c# [$ h4 J. N0 h# t8 O' m
TIC TUBE, A tube facing the airstream
. R2 D- e. w5 A( {) q- Z. yhich measures ram and static pressure. Used by0 ?/ S) o2 @4 s. C
irplane instruments.
4 D- W3 Y( A' `丝钉。由平
, b) S! f* ^; {7 V十字头螺丝钻驱动。
2 K9 [( B. ?' t* f/ a: i5 b* [仰,
& ~5 |% F( |( I4 |5 n飞机绕横轴运动而造成机头的上下运动。
5 u' g1 q7 k1 `一侧通向另一侧的水平轴或横轴。升降舵控制1 f1 }* x5 C9 V5 O% ^4 | T# _2 e
头绕此轴作上下的运动。(水平安定面则用以配平。)
$ [9 c0 b+ _2 f7 w俯仰率,
( w0 l0 {1 M$ W+ E! r- f. T飞机绕俯仰轴运动(机头向上或向下)的速率。- y* O0 p. b! ~% N0 h3 N
管,3 W+ b5 a/ a1 V3 g# \: y4 f/ x- S
开口面对气流以量取空气的总压和静压,供飞机仪表使
* n p1 I- x# H+ J, b6 P的管道。
6 j6 V0 s2 V# ]! j3 _+ O- j; f' Hdistinct tapers. Driv
. y P1 u9 D4 x2 ps: Z, ~# O* f8 M# K" q [
P: J8 b% |. P% j' b! G* Z% D: @$ B
a i) d2 F1 x4 }6 e
PITCH AXIS, A horizontal or lateral axis passing- _* [$ `3 O* P& x. L6 a# u
through the airplane from one side to the other. Airpla8 p) |/ X+ e* y7 Q. \& N; y! a
n d) D* o6 l, f
e2 ]3 p/ p& j" ?) }* F: c h
P
0 v4 z! z5 a, tth
3 ?5 X: G8 i4 s; @' [PITOT STA7 u" h6 x8 `2 V+ Q9 O' v
w
. [! _& d. ~/ ra% H6 Q D1 Z) |6 m/ U) m. q/ Y
十字螺丝钉,
9 G3 I6 |) }! u" v. Q k! A螺丝的顶面有两个明显的锥形十字四槽的螺: R) ?7 y, d! ]4 d: d
顶
5 O1 r! ]3 T4 {$ z2 h8 v9 }+ F; C俯
0 q7 O/ j$ z8 e* }" A( _俯仰轴,4 n" a3 ^" ]+ ^
从飞机3 z$ ?1 r% B' K8 L- V3 |9 a
机
3 j8 s# ?0 E/ `( o5 y; O3 a# E总静压 [7 ?0 ^/ w7 c& n$ m+ s
用" W4 X5 o9 C8 e" g* z" M5 w. P
英汉对照民用航空词典B OEING3 s/ y- s6 z2 o- W, d
TECHNICAL DICTIONARY 114
( v% ]+ E \7 LPITOT T
1 r; g/ e1 |9 @measure
# I J! K3 d& B! g2 |" BUBE, A tube facing the airstream which
" Q$ Z2 j6 W) S8 W* bs ram pressure.
6 n0 @! t" d/ X- H Z, J$ @PLA, SEE - POWER LEVER ANGLE N, H, s7 u8 e
r
' _" @3 X5 J: x% }9 l$ [! ^ Ne
, G- T$ Y3 C) T4 g$ p& C5 n. F8 ILEXIGLAS, A registered trade name. A transparent
2 b6 [) l+ s$ J5 mr any purpose.
, [1 W& X8 [' X' y+ ?2 eNEUDRAULIC, A system or process which is a
2 J1 Z) L* E ]6 {2 ~0 Dres., [! T# h9 {$ }/ h6 X4 z* w
PNEUMATIC (NO. 1), Cold air, controlled and/or
9 E: s% R& H& ] ~' g3 Apressurized.
+ K2 T' j' y1 x: s6 W# R( m托管,9 `3 T+ _2 K4 G* w
面对气流以量取动压(冲压)的管子。
6 I/ r' M" ~9 f/ O+ W/ u门杆角度,
/ Y" l" C- v* G' R: T5 b8 G见Power Lever Angle7 V, t: S( k$ w- n
PLACARD, An attached sign providing information o
$ ~. r6 v# o q( W0 R& ?- h/ finstruction.
) k( H% G$ Q4 j$ e- S- ]5 e, KPLENUM, An enlargement in a duct which changes th
9 S) z/ S4 {7 K# V% d: B9 Iflow characteristics of moving air. Used to remove
) A% J/ r) _, S5 B* Rpulsations caused by variable airflow.3 W9 g. m& m4 P, ?7 S" H. r" k4 R3 m
P
, y$ J; q. M( b' _' macrylic plastic material used for aircraft windshields and" Q G0 }" _* z" I2 f
side windows. JARGON TERM - sheet plastic of several$ d( Y/ g* p4 i$ w2 c
types and used fo7 W6 G+ D! O& |# P1 ]
PMC, SEE - POWER MANAGEMENT CONTROL$ w- u9 x( [8 K9 i' H+ B
P
% b, W+ }+ I2 e3 @combination of hydraulic and pneumatic pressu1 K6 B% S y$ i' t! K% O
皮 @. H8 U% N3 @2 @
油
4 T. d/ i+ y: l* ]" k1 x.8 L# `* S3 h8 C1 M2 @# k
脉动。
( f3 H# }$ Q4 ~( ?: P4 G& P机玻璃,) `6 j5 |4 ~2 V0 V' g
名。是飞机风档与侧风档所用的透明丙
/ n o2 H, p6 _4 K# q, x j控制,
& g* v6 X; E; s标牌,. j; w4 [( R4 t. v
提供信息或说明的附贴标志。& a4 S, m6 h; ~# F3 B' h- U w: h
整流腔,
6 t: E% |4 q' }/ J管道中用以改变运动气流特性的扩大部份。用于消除可1 _- N' W. c+ O X
变气流引起的
& a5 q: P) Y! ]1 r e$ y有
3 [8 R$ {# o& N' e是一个注册商品' v. |, B. [1 q: L# R
烯酸塑胶制品。行家称之为多用途化学合成胶片。
2 j8 A# x% b' V9 Y动力管理/ h- l9 Q5 G1 w7 Z
见Power Management Control.
& ]; J0 C/ n& }# @: b动液压,# h, g5 `( v$ D! m* k
推动的系统或过程。8 i* k3 {) M2 ?3 \& D u. o/ _6 [
1),
]1 \& ], V/ E6 j。6 i! c9 y p8 ?: {( b
气1 E& x2 l; z1 P7 R. A. Z6 _: {
由液压和气压混合/ ?7 c% n+ p/ L6 I( S, J6 ]7 Q1 Z
压缩空气(NO.
: R2 |1 R: X! {经控制和/或增压后的冷空气
' b. O/ T9 N4 L* b' f" y- A/ m英汉对照民用航空词典B OEING
* p4 H' ^' @7 I+ k/ E9 @TECHNICAL DICTIONARY 115
9 F, ?0 v8 C7 @* s: gPNEUMATIC (NO. 2), Air, controlled and/or
+ r* X% |5 y. x% {& Tpressurized.
0 M. |$ \$ ~& C; n% _8 y, dOP OUT INDICATOR, A device on a filter which# M5 L1 K4 k5 o% @
roughout a material.
0 C1 {. p; d" F5 n9 eition./ u# |- s* C" }6 l$ t
POSITIVE, Definite and intentional.5 \" d. U9 J* ~; K" ?5 k& u! A
(No.2),
" T" f8 ^$ z" |/ {; T4 a出指示器,6 s, l9 n+ u7 l6 i. X; s
到达一定的压差时,它会从壳体内0 X1 E8 C/ @" I2 U7 S Z2 c; `1 S. Q$ M) Q
指充满整个物体的细微小孔或空隙。
, @9 g5 m8 w o9 S置基准的飞行管理计算机的一种操作。, ~ j. G | L3 i
肯定的,1 U% f7 [2 T" s' H C
一定而且有意的。" R& A8 q1 u: Y9 L+ \
P
& [' O. z G( i" l) i* bprotrudes from its housing when a specific differential
& w Y$ F/ q; k6 d) O# ypressure is reached.9 K9 y6 X2 o w- _
POROSITY, The term for pores or small cavities
! P5 x6 E. z, h0 bth" ~4 ~ g6 y! s- |7 \ K
POSITION SHIFT, An FMC operation used to change) i7 h. @. E. C
the reference of present pos3 h. T/ Q1 q9 `. x
压缩空气; Z0 U6 l& r6 Z! q
经控制和/或增压后的空气。# {3 w% |! E/ Q5 `$ e& i' U
弹
0 |; f2 b- z0 B/ j过滤器的一个装置。
- O7 r, M0 w) H2 s* Y$ O5 L伸出来。
. f& Y; Z$ s9 }; @4 r+ Z( l5 k气孔,
' N' f! f$ w! n- U3 z+ R8 _, W, J5 F k移位,- r; r# H& Y2 X* \
用于改变现在位
5 u) o0 C2 f, s6 q英汉对照民用航空词典B OEING! ?! L( V. n* z1 x: `& u5 m
TECHNICAL DICTIONARY 116/ E) _1 w3 p# N4 s, H( n' f) a' n
POTENTIOMETER, An electrical device for changing
5 S1 e" Q: N O) P. ~# mthe voltage supply to an electrical circuit component.7 F0 m9 O$ u2 i" ~" V1 h
r
! M7 H2 H7 i. [bly for operation of flight controls.
& }: c; j( B2 O; [" s, V% HOWER LEVER ANGLE, The angular scale on the/ {" F& q; t# N( Y+ H
main engine control for showing movement of the power
; i _0 ]+ g0 I' e' B8 jhrottle) lever.% _$ R- V( G1 w1 p
OWER MANAGEMENT CONTROL, An electronic: w! L" F7 S r3 `
ngine control.( M1 ]" V/ {7 h; \
OWER TRANSFER UNIT, A hydraulic motor/pump for
5 F" {( q0 M4 {+ fupplying hydraulic power to components when normal
& U9 {" M. }, ~RECOOLER, A heat exchanger in the pneumatic6 U6 H: L6 B; \! i8 p! e( _4 n! ]5 s
lied2 X: `* c" m( l- C
作动筒,$ u; J# ^; r; g' H5 `
件,; A- ]% I2 C3 W+ t* S) n# T
油门杆角度,
6 Z" _. V$ I+ F: T9 H主发动机控制上用以指示油门杆运动的角刻度。8 C( Y2 S1 c# A m4 {" a
动力管理控制,
% I' ~) {: p5 Q8 q) f控制发动机的电子装置。- ]. S! f6 `" w8 b
力转换装置,% `. q- ]) i' U/ \' ~$ ]
当无正常的液压来源可供使用时,用来向部件提供液压( S4 p1 x$ _; j
马达/泵。
7 n! X( l( ~2 f; H2 |冷器,
" u& S5 @" [! X( a+ O0 _中的一个热交换器。它将发动机引气冷却后) G$ v5 u7 @# |5 m# \
供给气源总管。9 G' Q0 Y# W H0 r
POWER CONTROL ACTUATOR, A hydraulic actuato7 [+ o# ^7 S: ^ u. T
assem& F' F# f0 A9 [
POWER CONTROL UNIT, A hydraulic actuator& j5 h7 X" ]% ~6 O8 ?# u
assembly for operation of flight controls.
7 }4 R* o5 e. c' O' a2 NP
9 n- a: [5 Q- G(t6 ?, l: m3 |7 v2 P2 C0 W1 t" p
P( d: I- p+ c% R! i- b
e
5 a$ F- F8 Z+ `/ GP: u7 b" v- n; l) `$ C
s
/ g3 }8 T& }; G! O( Y: Ssupply is not available.) X0 ]# {( v* r8 h p
P
- A3 j' J0 A+ Vsystem for cooling engine bleed air before it is supp0 P; m) {, D/ {/ C* i7 r1 x4 N- o
to the pneumatic manifold.
8 A4 F8 W& n& {& `/ k# X; q c$ j1 O分压器,) g$ @5 y" [$ u; V5 L$ u
用来改变向电路部件所提供之电压的电气装置。
. K6 O3 N; d" V* f9 b8 g9 r7 D1 W动力控制
$ m5 r- {9 Y0 ^5 s0 I4 k用以飞行操纵工作的液压作动筒组件。
( q4 V- O- H. R7 _动力控制组
) p/ V+ R" T5 ~用以飞行操纵工作的液压作动筒组件。# I. }+ m7 k" C# A7 r/ w
动
/ L" U# a5 E4 v8 X1 u) K动力的液压
; v" D$ M; _' F ^8 @6 V预3 a7 w% I( A) H0 l
在气源系统+ ~3 V! a/ k0 O0 D# l
英汉对照民用航空词典B OEING
1 l' J8 L+ k& d6 V; k" LTECHNICAL DICTIONARY 117! y# C/ N/ ~2 R& d1 D# j2 U; q
PRECISION APPROACH PROCEDURE, A standard
$ I: N3 H7 I4 Redure in which an electronic& x" D" n* Q4 B1 t+ R
lide slope/glide path is provided; e.g., ILS/MLS and
5 S8 R& ~6 S C2 D5 }PAR.( N0 P; }& \2 c4 X% {# ^* L6 f1 |
RESSURE, Force per unit area usually measured in
# V" E, B0 X# X Eounds per square inch (psi).+ I9 X% R6 s- z" s) z
RESSURE ALTITUDE, The altitude displayed when
! n* y. l! t: ^) ue barometric pressure on the altimeter is set to 29.92
1 R0 [) d- p1 ^5 ^2 Z1 Y' f7 \RESSURE REGULATING AND SHUTOFF VALVE, A0 {) v/ Q; x+ D8 s5 P( A' h& ]
alve in the pneumatic system for regulating bleed air( g- M9 r4 |7 p4 |
pressure from the engine to the pneumatic manifold.: u" ]% U4 f7 E" o/ m
RINTED CIRCUIT CARD, A plastic or fiberglass card
# z2 S0 M5 t7 E' M! e6 @1 cith electronic components and copper strips forming a
& j9 M. s! A7 S1 p% a' y6 |* L& Kircuit.
) s% e( \4 I) x$ {! u3 I* x& ?RIORITY VALVE, A valve in the hydraulic system for( B. y2 F* `9 j/ ~6 T0 i0 u
ROCEDURE TURN, A maneuver where it is
, ]8 M: n u$ k; t7 Qlane
6 J( s; R$ |4 \! y9 ~proach course.
$ Q- G+ l/ S) g: @' X) r精密进近程序,
2 b. P4 v- t% Z. S* V己提供有电子下滑道/下滑航径的标准仪表进近程序。
8 h ^3 x) `) y: V9 E3 O% E6 A如:仪表着陆系统/微波着陆系统,以及精密进近雷达。
5 d8 U; A5 ~1 G9 C. a9 W压力,
3 z, V7 c7 U! [4 ^" N& m单位面积上的力。通常用磅/平方英寸(psi)来度量。
9 D) n2 u' w7 N* L# A2 o0 }' t- }压力高度,
) ]5 V6 J2 X7 a, f% ?3 M当高度表上的气压调至29.92英寸汞柱时显示的高度。8 ?7 y4 t1 x/ X {0 Z: v ]( Q
力调节和关断活门,
1 u2 c6 g6 m9 W气源系统中用以调节从发动机到气源总管的引气压力) G8 s) ^% _6 y( A, C
的活门。
; h4 l" t3 ^% h1 R刷电路板,1 w' z0 y6 i! _5 ^/ v. j- n( ]; K
由电子部件和铜丝所组成电路的塑胶或纤维玻璃制 K# B, C, w5 G
薄板。4 f7 ] c# z2 U4 F
先活门,
6 m+ Z# C0 h2 W,用来使各部件照合适顺序操作的活门。: s2 P( V+ Q; U& v, T- T
序转弯,
; R$ i1 x$ I6 _$ W3 i/ `后进近航道时所做的机动动作。
8 B3 W5 o& r: `* K5 ginstrument approach proc
2 n: ]( Q: w6 a; R. p! K2 Eg
+ x; o. ? o. d K; KP
" I7 k/ ?8 P; t6 p0 \5 v% L* Rp
0 @9 T% C5 \' ~/ d/ kP ^& T% n6 m# @7 O
th
4 @. D% t/ q( ]1 t0 d- w1 Qinches of mercury.7 F$ `) t1 m! {2 i2 ^
P
1 A9 ~ G, K3 qv5 ?* \& X6 j# _- Q
P+ @6 p( F( `* u9 r8 O- }- l
w9 u# w: g5 l4 S) u
c
$ ~7 F+ Y( e% }P
. T. h/ ]/ n! |/ _operation of components in proper sequence.
( p& u# Q+ b1 F" ?P: d7 T, X& B9 [9 A% I$ J
necessary to reverse direction to establish the airp% p O% o. `% ?5 Q3 @$ o. F5 b
on the final ap8 A; z% Q% y& c1 r
压
! A) j" A3 S7 I印8 N4 G5 D ]- ^6 v, s6 d O
优
# I( B& J2 X% k) e9 ? s3 w! R液压系统中' i, s K! \% b! c
程0 n! P+ j* e& R5 O" w7 s
在飞机必须反向建立最8 b* ?5 O: C4 Z& V& S6 ?
英汉对照民用航空词典B OEING
/ }5 G( m. i9 E' O, Q! vTECHNICAL DICTIONARY 118
% D e. W3 Z$ x; [' n- \PROXIMITY SENSOR, An electromagnetic d2 g8 g0 T/ t- d3 u5 v8 u3 G
senses the po4 |' w; P4 \) ~, O) J: O2 E* }( J3 P- g
evice that
0 M% F/ `5 S* Z* csition of a moving actuator. The sensor* g. O `; L$ M& S& t. @% C
as two or three wires.
0 x' G( ?8 b4 K5 I- UROXIMITY SENSOR ACTUATOR, A steel plate
! ^9 V7 F n4 l% X3 R" i* acated on a moving component for operation of
/ b. ~ M8 T; T* t I' Groximity sensor.& `4 ^) m4 f& x. y- B8 V
ROXIMITY SWITCH, A printed circuit card for: F2 x4 K. P% T6 G: L) `2 T* L4 W
transmitting sensor signals to indicating lights and* y+ `! x2 ^# i% F* `! O
邻近传感器," }& a8 Y( P+ [. g u
能够感知运动中的作动筒位置的电磁装置。该传感器$ V/ ?6 n! {0 ?
有两或三根电线。; S2 M4 Z5 s( W& q; n& z1 k: N$ ?
邻近传感器作动器,
$ v1 V) Q8 a' y$ Q% q3 }位于一个运动部件上,用以操作邻近传感器的钢板。
7 c( j& x* j' Y4 F% _3 W近电门,5 w& m! I/ j( B
传感器信号传输给指示灯和电路的印刷电路板。: d. `* x& K1 i
h
/ i3 X( v7 H0 T6 T9 \P% B7 e! _1 ?) g3 B5 A5 a @5 Z
lo. l& t3 ], O6 u
p
2 q! o+ Z2 _* c( EP
- Y% X- `; [2 C# Z& {0 G! kcircuits.
( n9 o8 ]& X- V/ l" f邻7 ]; ?# h, \& X' `% C/ X
用以将
) K3 }- Q" F1 N3 c/ J; W m1 E/ j英汉对照民用航空词典B OEING5 o8 [$ T+ N0 }8 `$ U
TECHNICAL DICTIONARY 1191 N' S1 a& H0 J. [5 z. K! K7 G
PRSOV, SEE - PRESSURE REGULATING AND
% \: ~0 U7 ]# D& R% nSHUTOFF VALVE
8 x6 X3 d' B5 m. Q* t4 f wTU, SEE - POWER TRANSFER UNIT, c8 B9 g( ], v5 J* g
removal of dirt from the air cleaner. ], F* K# Q6 E7 b% u1 G
n
. h2 D1 ]. W8 @9 O [QAD, SEE - QUICK-ATTACH-DETACH' f! R) [$ R, {& b* D; M. O
ICK ENGINE CHANGE" c+ Y0 |8 Y% x# |& y( R( m- B# u/ e
height above airport elevation.
' ^' k2 w/ Q+ Z% j; L' Q' k; FNE, Altimeter setting 29.92 inches of mercury, 1013.2
4 o- a' X+ _& fQNH, Altimeter setting which causes altimeter to read& E; Z8 e& h/ F% F
height above mean sea level.. L/ B2 C- i$ L: S6 F. ~5 [+ u) M
活门,
0 I9 b: K" {5 a. I# {* r0 K2 G4 n8 hP
0 [5 P2 ~6 K" A1 s. q5 qPURGE VALVE, A valve in the pneumatic system for
5 M% Q5 c: O, n4 _! @3 H) q iPYLON, A structural component for supporting a6 {; l4 b G3 P/ A8 k6 M7 L
engine from the wing.$ ]5 S- `; I. x, S! N, J
Q+ f/ g& X$ s) I% N( |
QEC, SEE - QU" `' Y( @; y4 t! Q
QFE, Altimeter setting which causes altimeter to read7 E! ]5 C4 |& y9 X6 J% J. v' n
Q
4 {4 M1 u6 |" c cHectopascals or 1013.2 millibars. G0 G( T3 _1 Z1 x M; m
调压和关断
/ U$ a1 I t Y1 B* U% R0 b' ~2 x见Pressure Regulating and Shutoff Valve., Z) O: i- w% i4 O" G' R6 [8 B
动力转换装置,
3 ~- C% t# P4 J. e0 R# f4 S/ Q见Power Transfer Unit.
) {- b9 @+ p. Z8 l; M" n' U气源系统中用以清除空气清洁器中之灰尘的活门。+ e$ F8 X9 T3 j5 e! h- D$ w8 F& z
速装卸,! q" s% w0 j: t% n1 R+ Z( Z7 M$ K
见Quick-Attach-Detach
; t' {: M. \3 U$ }5 J6 c+ R" Y0 |) g7 B除尘活门,1 H5 a/ l4 ^1 H
吊架,# k2 _$ q8 \3 b6 Y0 R( u( Q! v
用以从机翼支撑发动机的结构件。* u' R+ m5 [. B, y
快
' b4 c7 H/ c/ P5 f$ l.- g4 ~5 I% u( s6 a
见Quick Engine Change: I W# x+ _% b* |. {+ n
快速更换发动机, _. l' t0 B: x8 w' J' y' E$ L0 E
.
! w! n3 f! Y2 }1 k! f) B5 z- V场面气压,
% I- g3 \0 q1 J5 v准高度表设定,4 d- W7 f ^& B6 W+ k7 g- {
2英寸汞柱,1013.2百帕斯卡,或1013.2毫
& r1 ]. C1 i' A% w- g" ?修正海平面气压,
9 R6 t5 f/ c: w; I7 |8 {使高度表指示飞机距平均海平面之高度的高度表设定。
' g, o0 E' d: `& C6 {1 |; W* b使高度表指示飞机距机场标高之高度的高度表设定。
) N3 I9 Y& P, I) B m) L& D标4 T% y" J7 _ h+ ~, \
29.98 c" r6 E0 U; l4 j _& P
巴的高度表设定。
' z7 H5 y) R4 f( ?2 q$ U" z英汉对照民用航空词典B OEING5 ?7 a0 j# x- v5 `, D1 e# l
TECHNICAL DICTIONARY 1205 p9 Y# b/ X+ x m' L7 w$ b
QUADRANT, A mechanical component shaped like a
6 v$ H6 p& y2 ^; m7 `quarter of circle for transmitting cable motion in airplane
$ Q: T1 S: w6 d M3 BQUENCH, A heat treating process to make the surface: J+ }- N. y) E+ ^' {
of a metal hard. The metal is taken from the furnace and
1 p8 y7 U- K7 X" U, AQUICK ENGINE CHANGE KIT, A collection of
) J- A$ K" J" ^7 } G# t7 Be engine positions of a particular model+ X6 O- e7 B) b }
irplane.
& B- h# d) `# t/ @: Jng
* m( L: L1 |5 q, oaccessories (hydraulic pump, fuel pump, starter) to the
: n4 i0 k( T7 ]engine accessory gearbox.& \% y, I6 N) y: M q
S, Established the
* {% @6 ]1 i' e2 S4 ^: `minimum amount of time to cool the wheel brakes
G2 u2 e- t0 p' `" c# l! @ @/ d! Qbefore the next take off is permitted.
# a- w0 K8 C/ X7 \4 ]- u2 B进油或水等液体中。
# w5 u4 J( N' s% G快速更换发动机成套设备,
/ X) j5 v' g A+ g2 r! ?置的所有部件的集合。7 ~7 X+ @1 y6 V* R* ^1 t/ ]
用以将附件(如液压泵,燃油泵,起动器等)接到发动
& s. }" {) @3 |, R# Z# q+ q附件齿轮箱上的夹具。4 Y$ R( G, G/ C9 z2 ?. N+ O
快速周转极限,
! _% E: t! F% r, }. ~$ h# q2 Z. r在下一个起飞许可之前,已确定的飞机轮刹车的最少冷
{" Q) _5 e: i6 i2 I却时间。
5 f. k, f; G7 d+ S* m3 Y) x3 hcontrol systems.
$ n; s9 M! I% d' g/ Gdipped in a liquid such as oil or water.
V4 u) C4 ^% d2 i( I6 w9 hcomponents allowing installation of a basic engine on to
: M* ^% d3 Q' {# Sany of th0 y( h2 E! z+ O; e h7 T
a
' e8 B# t9 Q: D0 s- ]+ xQUICK-ATTACH-DETACH, A clamp for attachi
% `7 B2 m0 ~0 R+ Q, F) _QUICK TURNAROUND LIMIT/ X) M5 |! L1 a' j) b1 H7 Z
扇形盘,
- D7 H! K3 d- s: x飞机操纵系统内,用以传递操纵钢索运动的扇形(四* b# x% g. h0 ?1 X
分之一圆)机械部件。7 Q% h! s2 q/ Z4 K
淬火,$ X0 T: L. C& J+ F% t2 U
一种使金属表面硬化的热处理过程。钢铁从熔炉里被取8 O5 U4 _7 g0 B( r! g4 G7 T& k
出后再被泡! H- |8 z! b) s y8 o$ v# \) n
用以快速地将一台基本发动机安装在一种机型的任何
) f0 x2 S7 |" _' j4 }) n发动机位
# i6 n5 r$ ^ ^, Y快速装卸,& N2 b0 F6 a2 k! o' b
机! U' \- |; X; C& l) _) Y3 x
英汉对照民用航空词典B OEING
, J8 A6 d: R7 G! f0 ^' Y) T' g9 T% YTECHNICAL DICTIONARY 121
, H, ~7 O/ D q5 {9 KQUIESCENT, Condition of an electrical circuit when no
& E8 \/ M6 e: z0 o) Y/ F3 |% r1 u7 IRACK, A place for storage of modules in the8 a8 q Z3 B1 p' L9 _
lectrical/electronic equipment compartment.
+ a# ?/ t( F7 B0 `+ |, E' yADAR, A device which measures the time between the
J, I6 u. v; s* z1 \* `* f% Ltransmission and reception of radio pulses and provides
: i5 k+ M; a7 |6 t R- i/ H0 d. Dinformation on range, azimuth, and/or elevation of2 Y P& {3 J& E: C/ u
bjects in the path of the transmitted pulses.7 S7 o' z9 I- C7 L8 _# ^
om a
2 ~5 v; A" E/ X! k6 ]9 A7 d) M3 Qar.
- U: `. ]' C, i! l2 Q4 kRADIO ALTITUDE (HEIGHT) (RA), The distance of an7 H+ a0 h! ^) d; Z1 d
aircraft above the ground, as determined by a radio! i0 H7 a+ |& g, o& c
altimeter system.
, o7 B# r% j3 F; { _3 X3 b/ mRAM, SEE - RANDOM ACCESS MEMORY
3 W, o2 b" [# u; }RAM AIR, Outside air that flows through heat
( H: s5 z1 n7 D8 n- Z! b, Wexchangers in the air conditioning packs.) N, T6 \9 K/ ~7 O# I7 M6 Z
支架,
/ I0 q) c) m5 H5 u. U* Y电气/电子设备舱内,用以存放组件的地方。
6 [" H$ P# T0 Z2 v( q+ ^3 ?5 U雷达,9 Z ~& s N- V
测量无线电脉冲从传输到接收所需的时间,并提供范
9 a$ H( }* [+ N+ g# d9 M& I- ]1 O% o" N围,方位,和/或脉冲信号传输途径上物体标高的装置。
" @$ q& c9 d8 T- v8 ?由使用雷达的空中交通管制员给予飞行员的航向。
+ a8 }0 j5 e2 f" q! m施发射出来的磁方位线。
* C, D/ \2 ^3 \% n% ], e2 r* _无线电高度(RA),: _# x% n9 M# U$ _2 H( @
由无线电高度表系统测定的飞机与地面的距离。: ~& ?9 G0 z/ g
随机存取存储器,
" |$ I. Z+ C, f见Random Access Memory& C. |/ D- g7 g* G& K+ P# b6 p8 e
input signal is applied to it.2 b' E3 ]) M4 u3 X% {4 E3 v7 K; h) v
R
( r8 |5 z7 k$ P$ ^6 je9 P+ w7 x) Y. X L, G E
R1 b# E0 ?0 L, I. A6 g1 v
o
1 a5 o" w! }& {% aRADAR VECTORS, Headings given to the pilot fr
& F) W8 H }* jcontroller using rad7 |/ \6 Z: x, Y4 u% n. x' G
RADIAL, A magnetic bearing extending from a2 T4 D/ u) i( e+ c
VORNORTACITACAN navigation facility.
$ J4 |* Z; g ^: O3 Q寂静状态,
1 v6 v# ?0 w7 K9 S' k3 T4 |电路上没有输人信号的状态。
" t9 R5 |7 P. p2 l. G6 a雷达引导,! O# ~) t9 t M0 h) u& e# ?( s! B
径向线,
- ~# q, J$ O3 J( X* r由甚高频全向信标/塔康联合定位/塔康系统导航设
$ Y9 j( \( N) v, w5 f冲压空气,* f2 C3 ?8 J% A, P" i
流过空调组件热交换器的外界空气。3 u1 T$ Y8 G) E+ y
英汉对照民用航空词典B OEING
5 ~, G! E ]& t$ YTECHNICAL DICTIONARY 122- q, v. f0 O( X: q
RAM AIR TURBINE, A device which extends from the/ ~5 k. u1 M: t. b! C
, driven by outside airflow for
3 l* i* p, c2 ~: Emergency supply of hydraulic or electric power.
9 p: m. v# s: x, I$ O4 e# G7 _: MANDOM ACCESS MEMORY, A type of memory in
! Q p" }& \: G% g# mdata can be written into and read out of.+ @. C9 M3 O1 P, S) @( X
used for short term memory.
5 V' s0 ^5 B4 @AT, SEE - RAM AIR TURBINE& M# F' [# c' O$ v1 W9 f V7 r! ?
ATIO, A specific relationship between one number% G, v, h! r3 m4 ], y+ A
alue and another.
& K+ l- d9 L# z6 i# C7 A& lATIO CHANGER, A mechanical device for changing
0 A4 X$ b9 a- h0 |2 S4 N0 zutput speed or movement relative to input speed or
7 O/ ^$ Y: \6 F& f( i6 KAW DATA, Data from sensors not modified by the user
1 q% I" q2 `5 n6 u" T况下提
+ l. f' p/ b b$ F液压或电源的装置。6 T$ G+ @( t& o/ Z* ^
机存取存储器, `, }* r9 b& j5 b" d/ G
一种可以将数据记载和读出的存储器。一般用作短期存
) {5 ]* D9 C: N1 L! w。: [* c' |- ^3 m, I8 i
压空气涡轮,( a. T v7 \2 s) g& H" D- T4 h4 y
见Ram Air Turbine. f) E9 e; `) K% U
side of the fuselage, {0 {/ ^0 K5 k/ Q0 d0 q
e
; k. n0 D2 e# l- v) n! jR
4 u7 P4 b% x* r4 w6 s+ S4 V7 Hwhich the/ \) G) o' A8 a% \ z' I) f" Y
Normally- k$ J+ U8 n/ x$ P5 @
R
3 q; ?- W5 i) w$ JR
# Y* C1 Q" s6 jv9 V% s: J9 V" d7 n9 |
R
3 g# Y+ ^. N3 X2 g7 p. yo
8 u8 Y7 l% N O) ]/ ~" A2 W: Mmovement.+ C+ @: s. H* A- E
R2 _6 i% m9 [4 b! \9 @- G3 P
system.
$ Z. {* N- `& u; `' v- e6 u1 w冲压空气涡轮,3 j+ [: T6 f3 L. B7 E: R
从机身一侧伸出,由外界气流驱动,以在紧急情* o, V7 O, b7 P* a+ b
供) ]* ]' Y5 Q. B
随/ G, j6 n# H9 C& F: v% m
储1 a5 f4 W1 p6 Q9 z/ W
冲9 ]4 S# X4 x0 m( p- ~( b
.
0 `3 F M% o- v8 L* A- T比率,
5 U" k, `3 C6 ?, \6 W$ w一个数值与另一个数值之间的一种特殊关系。5 U7 {2 `5 L* C& K4 E" `) b- ?1 u
率转换器,9 t/ ]! K' g1 Q' t1 d2 h
用以改变输出速度或运动与输人速度或运动之间比率0 r4 I% q" J; Y. x+ E$ o7 T
始数据,
$ F1 @; @" E& t; l8 G/ B$ [任何修正的,由传感器得来的数据。
5 ~ D7 s4 j4 q/ e1 L0 z比
' `+ W8 ~2 B$ i; e5 D的机械装置。
; {/ ^* V8 b( f/ T C& g. |原
; x* Q1 I6 k. ?6 V没有经使用系统作4 b4 @% J! Z* T" w3 h5 }
英汉对照民用航空词典B OEING
2 [' y! Z' r; WTECHNICAL DICTIONARY 123( |& ~; d9 l- W0 M! l! t6 `) m
READ-ONLY MEMORY, A memory unit in which
. R N3 [0 x0 M; \( p# K3 Rthe computer. Under normal conditions the stored
1 f! A( O: f! |8 Q einformation cannot be changed.
) X+ i( Z4 e# t! L7 g$ A" w' pECEPTACLE, One half of a two-piece connector. It is
8 t1 z9 R- G1 [4 D3 Wusually mounted on a support, such as a panel.! q4 r& n( k0 V9 W& ]- k
RECIRCULATED AIR, Conditioned air mixed with air
2 F# K& X% w$ g3 |from the passenger compartment.
7 I0 v" D$ H5 ~" l1 G# p8 r/ \7 ~$ dEDUCED THRUST, A thrust level less than maximum
* x+ _! B- G2 G; q/ l3 C) u' y- }- Z! arated thrust.9 _. \! r" y' S# L6 Q/ }$ M
EED AND PRINCE SCREW, A cross point screw with; {& Y$ `) z4 `- H( Y
a single straight line taper driven with a pointed tipped
$ K: v5 T0 q4 F& K3 T( fED SWITCH, A switch with two magnetic plates acting# G2 Z* P, ]9 } |' M& E: I
s contacts and operated by a magnet.
4 y# B4 z9 M- ?# ^只读存储器,
. T' q& ^+ @0 Z. I2 n; b4 y& P1 y含有由计算机永久存储着的指令或数据的存储器。在一7 l! S; B6 r( O- q) [
作任何的修改。, s, X) B0 p* n! p# l7 T: t* r6 _
插座,
( U% \" r: u- X- Y/ i0 j" m4 h' E由两件组成的连接器的一半。常被安装在支架上。
" ^( Y4 h6 u/ B$ q/ x: `& g7 G% E如:仪表板。
8 Y5 R0 \. c+ \再循环空气,. }' z- t$ B$ t& Y
调制后的空气与客舱来的空气之混合。- R1 M. S+ B8 X3 m1 r7 g4 n! A
减推力,
/ o& g ]9 J) ] N. j! D* y额定推力小的一个推力级。
( |, z8 w! u9 Q( W9 |十字螺丝钉,, I4 y- o% k( n6 f! J9 F+ Y
的,带有一条直线锥的十字
: P ~$ B# [$ b5 z0 E1 @, l舌簧电门,4 T2 Q. B) w8 Q# r
由一个磁体控制使两片磁片接触的电门。
9 I0 F1 | i5 N9 o* D1 @instructions or data are permanently stored for use by9 X$ a" [6 N+ j! V6 z
R8 _( s, j3 u% c. Y& H3 P
R
" x2 j9 D8 F: j+ PR% b( d! o5 R7 R3 i y
Reed and Prince screwdriver. (See Phillips Head.)$ H4 M1 g/ w0 G
R) O! n/ e. g8 o4 b2 r3 D; j+ o
a. t* m- o/ N) z7 C6 u: J* P9 h
般情况下不能对存储信息9 V1 O6 z2 C z' h' \
比最大4 f7 n0 g7 r# |! s4 h/ i+ _
与尖头十字螺旋钻配套使用% J5 q2 }3 ~3 B9 O- P. H4 a! n6 A
头螺丝钉。
; W* ~( N8 [$ [英汉对照民用航空词典B OEING1 X2 `3 e/ G }9 ]1 n2 z- F
TECHNICAL DICTIONARY 124
7 o& B9 f8 X- lREFERENCE LINE, A line used in a chart as the8 ]) v7 `/ h- t
starting point for applying corrections to chart input: r4 L. ]* \$ ^0 @7 b1 W& y
alues. One or more reference lines may be used in
* W. ^5 {! f/ G; zuccession.
1 ]; G* G/ q9 b1 p/ r* } [- CD TAKEOFF, A takeoff which has been6 M0 N, i n( {* C+ x5 V/ {
.' C6 d" P* j3 d/ P$ h( W
EGULATING VALVE, A valve for controlling pressure
7 C- I* `( x0 V' X Q( WELAXED, The state of an electrical component or" q4 a- L) }8 h* b
witch that is deenergized.
+ j: ^+ C# }- w$ cRELAY, A switching device in which the contacts are- f, D; [4 U9 c6 {# M# d
opened or closed in response to separate current or
" V6 L- J# U) q3 ?oltage.5 ^- k( m9 E' _. P! x5 E
RELIEF VALVE, A valve which prevents high pressure
' S5 _' e1 c! K6 e5 S7 ` aa system by venting the system to ambient.7 p H3 E0 J- L0 H
起点的线。使用时可用
9 y y( S) l/ ~; g$ r; e- B条或连续使用多条。
8 p1 q, ~/ ~$ z" i8 q9 G断起飞,1 W% Y Q S- C g2 D, @8 H- ~. ?
离地前被停止的起飞。
) ], h/ W9 `0 \; g3 Z8 h* q: X5 w节活门,
0 W8 I8 |) w- e* F3 }# R6 k5 q制压力或流量的活门。- m' ]+ g, T: N+ a# w
放状态,
, \ R/ g: x5 J( P: d电器部件或电门处于关闭或没有通电的状态。
# q% W2 d; M9 O3 l U0 r6 {$ R继电器,1 j0 k' E6 q1 [* l
一种电门装置,其接触点随着单独的电流或电压开路或5 J7 [1 ?. c! _) ?* e4 f
合。7 N9 P/ R8 S7 U; ~+ \& l
释压活门,$ E7 J- d1 v+ F" x
通过将系统与外界相通,以防系统内压力过高的活门。 }% @3 p" f% P" Q" N$ \/ F
v
7 e' n1 G6 l8 g9 ~' xs
* j9 ~& c1 N- E5 L3 cREFUSE
" f" L: t' B, k wstopped before the airplane lifts off the ground
3 K* a$ X8 o1 ]% ~% ?+ l3 PR! Z. L) S3 D+ q |8 g
or flow.
6 ?0 ]3 v3 v2 \$ m1 @5 YR
# N! C2 U' e' n# [s
* M. o1 B' t. yv
. L3 s; T9 ]$ N& x& ein
8 M$ Y2 z- |+ i7 ]基准线,6 T7 ^2 G( H1 P: p: p8 D
在图表中用作修正图表输人值的' |" M& m+ x- O! m# Z3 V
一# g: Y9 O3 c$ u* }* L
中. o( v8 `, n9 r/ @1 Z- U/ |" Z
在飞机9 e& a7 X* y( |" y' V9 s
调
* i: {9 B; X* s用以控7 C6 C$ o' q5 f0 p6 @9 W
释+ ]$ r u6 J) m0 m3 {3 H0 F: F$ \
闭
: A9 @" s* @! Q' H英汉对照民用航空词典B OEING
) n6 A, n/ f% F5 n; @; N# E2 [TECHNICAL DICTIONARY 1258 `8 L* J! p. l/ Y+ k! k
RESERVES, The required fuel remaining on-board after% X0 N1 f a+ O& P( Z
ESERVOIR, A container for storage of fluid.3 o& Q" O, }0 F i
ESTRICTOR, An orifice for reducing the flow and
1 U+ Y6 ?8 ^$ `ressure of a fluid.7 f" ?0 W1 ~* m: W1 Q/ K
ESTRICTOR CHECK VALVE, Same as restrictor but" P- M9 Y0 Q( R2 ]' V; V. J# {
llowing flow in one direction only.: m+ C. T; b2 b. b3 k
decrease the$ n8 F6 V8 R0 W
ngine thrust to idle.
9 ?: _ ~" ]+ E& ^4 GREVERSION, To change to a pre-determined mode.
8 m, R& @1 Y9 ?2 W. Q i; Octrical device for changing the* n7 v' o( v. o8 ~0 D( E
sistance in an electrical circuit.2 E& D2 I; _. C. j$ e
备用燃油,
' Y7 h, I0 N; H照规定,飞机在到达目标机场后,机上需要的剩余的燃
, x) s9 L0 w/ p6 s: W8 p6 ] Z2 p油。
8 B7 c1 P1 ]2 U5 I8 U$ X0 {& S储液箱,( @; v0 |3 t4 W. Q6 h4 L
用以储存液体的容器。
7 U% q: i& u; m; i+ |限流器,9 y+ P2 i4 O+ a0 u6 [5 [" P: @- x
用以减低液体流量和压力的量孔。/ _$ Z' i2 K. s' f; K% [
流单向活门,5 l; O) ~( H1 k. p2 R+ R8 K0 t
一个与限流器类似,但仅允许流体向单一方向流动的活
# M" P0 u* r4 Q4 E$ V! B/ Q3 ?0 h门。
* ~+ g, X; V% o7 v- P0 V* | J% s门,5 b6 |9 F+ M9 O w ]) W7 U7 @
自动油门的一种方式、用于将发动机推力减小至慢车状
+ C) G) ^# V3 M。
2 k* v8 k) J* e" L& \改回到预定的方式。9 L% S3 E) t# }' l5 T) E& M
用以改变电路内电阻的电气装置。; J% ] q7 R' W$ f: w7 V% w
arriving at the destination airport as determined by
! y- b" Q6 F9 j; u( T! L# ~1 f Qregulations.% i/ I: Q1 E; ?$ F* y3 u
R
8 J g/ M) r" O YR6 s- g) ?8 {% _/ V6 q' ?
p
/ u. V! L9 W, b! l4 L& i& zR+ N$ M2 ?7 c5 h* V' N+ G f' w
a- b; ~! z8 t! M
RETARD, An autothrottle mode used to
) y* R6 o/ Z" [5 E5 p0 ue
1 k1 C t4 e0 o% r' D( e3 u/ }, GRHEOSTAT, An ele
6 Q1 s- s: Y8 Z' z4 @re: w. U+ _" D! W- r
限5 _: \4 ?, s Y
拉回油
' J# I" m" Z9 Q% F9 K1 ]% l态
% X. Q7 t' N) }5 B: I% p" A复原,
- O' V. _7 r; m0 ^' l, k) z变阻器,/ o+ m; y9 o; d# Z# P6 k
英汉对照民用航空词典B OEING
. J5 a' q5 P: h }8 ITECHNICAL DICTIONARY 126
' d& Q& N1 C9 D, G9 b0 J$ F1 I, iRIB, A structural member of airfoil shape in wing,$ @% h( f- \- z5 c! G) k6 p; u
stabilizer or control surface.0 [1 [- a/ b" t$ t& B
IG PIN, A metal pin for inserting into a moveable
A9 p/ o) o5 i' t8 Momponent before adjusting the control cables and; W5 e$ O' r9 {/ X
nkage.8 H8 f$ i4 F( c r( y( ~$ f
IGGING, An adjustment of airplane controls and doors
1 E! h; P2 Q6 h5 b& [$ vr proper operation.
( M& M0 Z* y8 B% W# honditioned air supply to the passenger cabin.0 M3 m+ G" G* S$ G: P4 U
装销, s4 ?& k4 f( n( L
在调整操纵钢索和链系之前,插在可动部件内的金属' v/ c* c' G& _% ]" U5 m" ?; v) ]
。, [4 r# S/ A- ^8 a4 D
校装,
0 t+ N$ `! \8 i1 d* m2 u) {使飞机操纵系统和舱门能正常工作而做的装配调整。
' s8 Y8 |: m& ~4 R. @空调系统中,将调节好的空气送到客舱的管道。
7 d% D; g7 j6 LR
/ e. X! N; o3 O9 ~c
^/ r6 \4 r7 ]. Z& \' \$ Q- Y& S% u, Ali
& T" Q' x8 K" b; l+ ], y6 x. a& [% u, _8 XR4 M- X) M1 q7 C
fo( ~/ M# z# I) J' ^* M8 @
RISER, A duct in the air conditioning system for' E: H5 a3 O% O8 ]/ h" `* r% Z
c
& S- x/ R9 b# F+ @翼肋,) I7 B3 l. C. o1 S U
机翼、安定面或操纵面内具有翼剖面形状的结构元件。 {/ i- v. O9 N8 U$ q
校5 N8 I4 U3 C2 i" f
销
8 G( R; @0 f) G8 Q. K) P立管,
2 b% }+ ^3 u! B3 ^英汉对照民用航空词典B OEING$ C! o, i3 |4 `
TECHNICAL DICTIONARY 127
, t- j! P" U( C/ oROD END (NO. 1), In a hydraulic actuator, referen9 z5 l8 Z; q& m( O1 E, P- E# V" o6 M( H
the part opposite to the piston side of the actuator.0 [4 S' U7 w9 w1 Y, T, `3 m1 M
ce to5 q5 x, j, X& ~) p: O
D (NO. 2), A mechanical device usually a
- j [) }, S. Pbearing, clevis or similar component attached to the end9 c2 d$ \7 p% F5 @
of a link or push-pull type rod.( |2 ]8 N5 ]4 M$ `* S
OLL, The rotation of an airplane around its longitudinal
- }. @) g+ `: \ f6 F9 |axis.
8 s; f* ^# C) f' _- HOLL AXIS, SEE - LONGITUDINAL AXIS
- Y" \4 p- X5 u, J" q连杆端,2 M1 a, E2 W; C5 t
杠杆端,
4 E) K. Z2 p7 D& H+ i/ s D5 M% h一个连在活节连杆一端或推拉杆一端的通常是轴承,1 ~ @7 q' B( a
吊环,或类似元件的机械装置。
! O* e9 r0 `% \1 k2 }' P: M滚,
7 `' ?' H6 Z+ f3 p" X飞机用纵轴作为旋转轴时的运动。% N( L+ h; r4 z" N
横滚轴,
5 k! k. |/ N: c6 i+ O& Z' @& U见Longitudinal Axis6 q9 W! {4 K6 c+ g
ROD EN
2 A9 c8 E3 s5 x! QR$ n2 r4 }' P! c8 _
R# r' R7 Z/ D( A! Q9 |3 W7 f
液压作动筒活塞连杆伸出的一端。
& F1 D9 \* l9 o% u V横
" B8 ]2 H# A1 [) D% H0 t., g$ e" m, @) t* R" ?6 c- H3 B
英汉对照民用航空词典B OEING
" P6 T; e# [6 g2 b- G# u, Q0 }/ vTECHNICAL DICTIONARY 128
, M! w9 Y; f5 I5 _0 o- d! GROLL RATE, The rate at which the airplane moves0 V' m/ C( n$ K- S- \
on the roll axis (wing up, wing down).3 c3 Y: X& M+ r
OLLOUT, The final phase of landing where the1 A5 K9 ]5 ] m: G
OTARY VARIABLE DIFFERENTIAL TRANSDUCER,: \* h' s; H; A, I/ @6 a1 U9 a2 c& C
ROTATE, A maneuver conducted during the takeoff# H; Z4 p9 ]" Q$ q* H
n
3 \! n: I- t1 G. P; Q) b4 R5 Z$ graise the nose of the airplane into4 j$ u% L' U P5 D7 M% Q6 W j
e air.% ]% e: j6 L; a8 I+ q
OTOR, A rotating section of an engine (turbine,: J; [7 n. d9 {& ~% C- |
ompressor) or a generator.
7 l9 s' E% v; r/ }# J2 t* A, TROUTE DISCONTINUITY, An FMC operational
5 D; x" e9 c$ e8 L$ v2 b* Gcondition, in which parts of a route are not joined or
) U" ?9 w+ j" [" Pconnected.8 Z1 s' x( V& N; m) A8 `
ROUTE LEGS, The portion of a route which connects
7 B" O, ]; v: L$ a- N7 J! Otwo way-points together.- b6 f' r9 O! f3 X
陆滑跑,2 e. `. B! I% f; c; y( u2 _2 ]
的最后阶段。此时飞机在跑道上减速。
; r3 W6 A2 t) z* D0 m" |,
$ D$ [' X/ X# x3 tR, r/ ]5 w' w6 t0 _! v
airplane is slowing down on the runway.( a3 F6 y* Y$ U5 w9 D' `& k
ROM, SEE - READ ONLY MEMORY
9 P( j: V3 x+ R# [" m+ M# uR @; n5 R' x2 Q/ G9 l
A device with a rotary input and a linear response.
: |% I( F. O, W: q9 S, H& jground roll. At the rotation speed, the pilot pulls back o9 F( S- ?" ~+ Y$ W8 n
the control column to- B6 |" M' ?% z- W, V/ G! T. G8 c
th
- }- U# [. s8 M& e. i+ f7 wR
/ w- F$ S7 r) z2 a/ ^% n2 L4 Xc
4 r, y3 i1 y; z/ e% n% r横滚率,! @1 s* d" X3 f. ]3 H" m
飞机绕横滚轴运动(机翼向上或向下)的速率。
* D7 J- K0 U# b* r3 A1 K着
( ^. F' S* o* @% l, s9 T6 p2 U9 \+ |飞机着陆
+ Y$ \7 c6 y; q3 L* S+ ]! Q4 Y% c只读存储器
" X% x+ z1 N0 |1 R+ o- Y见Read Only Memory
3 i) F- a- o. c$ W4 x; C旋转可变差动传感器,
$ b; F! Z+ Z5 d( \# n, s3 w2 Y人和线性感应的装置。
) K7 ^ d7 ?. l: \3 O抬前轮,
: n+ K3 V) U8 D1 F) @3 {6 t i: d飞机在起飞滑跑期间所做的机动动作。在飞机达到抬前& T0 e8 m$ C% ~4 B, L9 M. q
发动机(涡轮、压气机)或发电机的转动部份。2 _/ [8 Q" }) h% t0 |; U+ q* T8 D
航路不连续,2 p2 l2 @, p; n0 q) F; f2 d
一种飞行管理计算机的操作状况,航路有些部份不相连! a' G& e' U+ ^ E, Z+ @
或不相通。+ z: V1 b: D7 ?2 d9 V
航路段,! G V" s. P$ ?. F
将两个航路点连接起来的航路的一段。* k6 r, [0 x4 J9 D. D, `
一个具有旋转输3 Z4 O J7 p: q4 R
轮速度时,飞行员向后带操纵杆,机头上仰,前轮离地。
" ?. l1 \* \# h5 r7 g0 N+ R- O9 F转子," O0 r6 {4 x2 W/ ~! N! B
英汉对照民用航空词典B OEING
& U; H/ \4 A7 P: ]$ e% G- H6 T; ZTECHNICAL DICTIONARY 129
( Z, @ u) f" O I6 O8 QRUDDER, A hinged moveable part on the trailing edge0 r9 t& i( K# R8 S& {% d c/ H
plane yaw (left and right). V# D( x' B8 P, y: U7 [
ontrol. K/ ]& O+ B' p% u! F
RUNWAY VISUAL RANGE (RVR), The horizontal$ B, G7 H `2 {, ^! B8 A' M
a pilot can see down the runway when flying an8 n7 Q& Q0 b9 H
pproach.
8 `: c, p1 q8 _' V# g3 K* N Bof iron and iron containing metals.
2 z: e; q/ O. E- q% r, S5 E xis usually a reddish brown color.
7 N0 P% q; m* S9 F# q1 [5 I7 @0 T% {% XIAL3 O; e2 y( \. O/ M, P; A
TRANSDUCER
" Y( t8 L) }- @3 c! ES" g X/ f& n- R: ~! H g
SAFETY RELIEF VALVE, A valve in the pressurization
8 A0 e4 \: ?) U, ~* T6 J* T/ V0 i, Csystem for reducing cabin pressure to a safe operating
- f& R1 J1 G/ `6 Dpressure.4 T% C; Z5 z* w L U3 r
SAT, SEE - STATIC AIR TEMPERATURE
3 \1 Z7 f( b9 T% ?或向右)的可动部件。
$ d! H# B2 Y( `) P( L. {. \进场时,飞行员向跑道方向望去所能看到的水平距
& N p. Q5 E. L4 o4 L& ~+ {, J. `: E5 [。
- F+ Y- z7 ?$ Z( q$ v( N2 @# `9 X铁和铁类物质的氧化物。常为褐红色。
2 u) N3 q' T& f见Rotary Variable Differential Transducer
" E; ]$ h2 c* B; _9 v! [of the vertical stabilizer for air
t1 F; p% C$ i1 {9 i& G/ Ac& n& c9 u5 Z2 U2 I
distance
0 Q8 [$ M2 `) t; F, v; W; ua1 H3 T6 k& O+ k/ f
RUST, The oxidation4 s, w1 m4 A4 i9 F5 G
It/ `+ @1 I. u+ d1 }
RVDT, SEE - ROTARY VARIABLE DIFFERENT5 L- J/ K" g: n6 b- [8 N& A$ v
方向舵;
5 e! Z) U" T9 s# _1 [8 [3 ]4 B铰连在垂直安定面后缘上,用以操纵飞机偏航(机头向2 R3 W% _! A. p
左
5 P$ i3 R2 N% a5 L+ D跑道视程(RVR),
* B$ N Y5 O' ~% y飞机" G( f* T2 Q, k
离& Z* O' Q+ ?0 U, l6 [1 s) l
铁锈,5 O" R7 m( K% f$ U
旋转可变差动传感器,
5 _# n! v" I3 F4 k.
1 B& U1 p% H5 d- [安全释压活门,6 ]' {) u/ ]7 I3 z& ?& E) r7 v/ k
在增压系统中,使座舱压力减低至一个安全的工作压力) B% F7 t- w2 s6 D- n8 d: [
的活门。' v* o1 t6 J# P [# ]$ ]: D
静温,
$ i; d; u7 Y. b: i见Static Air Temperature.
9 |0 T; k: m* j, ^英汉对照民用航空词典B OEING
( d' i, t( \* D8 ^/ V/ GTECHNICAL DICTIONARY 130
! ^% z0 u6 }0 A1 Z$ |2 {SCAVENGE, To remove oil from the engine bearings or# F7 Z7 k: `5 N+ V8 I8 t, H( W4 K* }
to remove water/fuel by a pump from a tank.
1 j- L" }9 k; x6 A8 BCHEDULE GENERATOR, An electronic component in3 M3 p R g3 o
e pressurization system for controlling the operation of! I" ^2 c _# e
e outflow valve.$ p- F; Q6 [; C9 p2 v8 B
CHRAEDER VALVE, A valve for inflation of tires,6 D! b, T2 @' e! P7 T
truts and accumulators and for pressurizing the water7 D3 K. r- P! v5 a4 u4 B$ }
CR, SEE - SILICON CONTROLLED RECTIFIER
, M" x. F2 B8 k4 p% \# HCRATCH PAD, An area on the FMCS control display
: h5 `7 L, M6 I# E, f0 D( ~7 h" @unit used for showing characters activated by the
. w8 L; f+ E# O5 l* flphanumeric keys.
4 i9 H0 P% F" V$ a0 l4 ]SCSI, SEE - SMALL COMPUTER SYSTEM
9 f. f+ M! F a1 Y0 MINTERFACE- _$ M6 s% C; }" [. \/ P& W8 j
SCUPPER, A shallow receptacle around a filler neck of
5 L+ D- J1 X3 c0 g1 u w: ~a liquid tank to catch any overflow or spillage from the2 r. N: r& P4 N$ ~- J" }. b( Z
servicing operation. The scupper is normally fitted with a
5 B1 c# v; M9 Wdrain overboard.& c" ~7 c$ v$ m7 M. t2 L4 A+ |" [
SEA LEVEL, The standard datum plane from which
a4 Q& O; |/ ?: O+ b6 D- waltitude is measured.$ f* e! ]& E6 ]8 T
去油箱内的水和燃
( p1 y/ \2 I ~7 a。) }- a* ]* d( O7 u5 S
程序产生器,
' j# s3 j" v! K6 _* i3 m在增压系统中,用来控制外流活门工作的电子部件。* H- x2 ~* S: @7 v
chraeder活门,
$ c. p1 a. O) E& NSchraeder公司出品的一种活门,用以为轮胎、减震支3 o' Q; n* J! q: |- t. e2 m
充气,也用于从外面为水箱增压。
- e5 z# }# g4 V3 E可控整流器,4 h/ ?7 I7 a, K+ O
见Silicon Controlled Rectifier
. {* v$ [5 x' C, R+ o- z& I Z$ tS
; P0 Z- C2 \% M" \! y4 d* h" Hth
' ^4 ]8 j9 P; Y1 c$ j' D5 r$ z. pth1 k* `( X( I$ s, o/ t* ~: M
S
$ a$ o) x- _1 t" J' Ts
" f- Q: L# H% D7 n- H9 ]4 etank from outside.! N3 i, B* m" T7 @: V- ?1 W
S
6 k. Y- K- w1 p' GS
% e: H* U5 f" I3 t6 @* T7 _7 sa
" e1 ]$ z0 I8 j3 s( E5 `8 z回油,
2 H$ G: l" f: }3 w$ e除去发动机轴承的滑油,或用泵来除3 ?2 J1 n4 f5 r3 X1 U, k/ x
油: Q c; u/ [7 a& x4 Z/ ]
S
( d G/ l3 b, [8 x/ `1 s柱和蓄压器* Y6 G+ i8 ` Y: }* `& s
硅
2 J% l8 S* I6 U4 `5 G# n.) `5 Q8 q' z& b$ P1 |! ]% W1 X7 M; X$ P
稿栏,
2 J8 _5 w! e% |, P! L, {0 S0 zFMCS显示器上的一个区域,用于显示由宇母—数字键
' E3 S6 J/ i& u) }# r; ?6 v g6 n激发的字符。" E1 e" x. \3 `- l( i z; W
小型计算机系统接口,
$ K4 P- ~4 k4 ? s. r; j见Small Computer System Interface
4 s: O# |- t+ K7 Y; u3 }3 ]# \- f草
) p$ g0 |2 ^ W1 d } ^盘: M3 V. d# E; d3 b! ~* ^
.' a, L ~" p2 W# R. j
放泄孔,
* U- I. R7 y; E$ T液体箱的加注咀边所装置的小型容器,用于接取勤务过' x! y) }! x% `. P0 e6 P" p
程中任何溢流的液体。一般都装有通向机舱外的排泄管
) C# B) P2 z! ~. Y8 z# E) G道。
3 T3 x- P, ]; M; f) J海平面,
; e7 b- x" |( o1 @9 X% A用作高度测量基准的标准平面。6 A- w& D! [& |3 U* |
英汉对照民用航空词典B OEING
: s& B7 ^' p7 mTECHNICAL DICTIONARY 131
, S$ m4 j& R' N ~1 R6 I' rSEA LEVEL STATIC THRUST, Maximum rated power- `, g2 T9 b. I5 Y$ ], y
produced by a stationary jet engine during ambient; X( b z: G- a
onditions at sea level.9 v: |9 t+ E' p3 f" o& s, p
s for
( ]4 G* r5 S7 y% n3 I L% F* p& Nreventing air or fluid leakage.
% Y* d& z% q3 b5 C; ISECTOR, A given distance between two checkpoints in
0 R9 l/ @. Q- r5 ]% b1 _ w0 Ke flight plan.
c: `# M0 A7 A2 `ELCAL, SEE - SELECTIVE CALLING K! s' g, n& Q0 e; [. R3 \$ {( r
SELECTIVE CALLING, A system that automatically
4 ~/ m1 Z0 H" b7 q) iSELECTOR VALVE, A valve in the hydraulic system for
} y. s1 }" Wo one side of the actuator2 e" L2 r: [' F, _ f. c
nd the other side to the return line.
6 _# _# B/ a1 Z' E% S, R* D力,
/ O' F$ ]+ V9 f7 l% c; m. b% o在海平面环境状态(大气温度、压力)下,一台固定住
* [' W8 S9 X. H. d* U' l6 j的喷气发动机所产生的最大推力。! `: K; h, M, e! l3 H; S% d3 k
在两表面间防止空气或液体泄漏的元件。
4 w; a) @9 [+ H$ z; a+ ?$ C* `航段,
2 G* C* z- ]/ W8 h# z飞行计划中,两个检查点之间的已知距离。0 j; h% o9 f8 [
择呼叫,7 A/ i9 L4 N, H, [7 r5 f: @1 V
见Selective Calling8 J6 D4 o& C3 c* N# ^9 U! s9 r
c9 K7 y6 e/ C9 r7 D: i0 \
SEAL, A component between two surface
0 k; U5 s5 ~4 _- W4 g3 N, Yp. g7 H) v7 P/ Z. g* m9 F" Q
th
2 @# o, @6 H) `. I4 N3 }, K7 US
3 z7 Z% x% N; ]. Q% _alerts the flight crew to a call from the airline ground7 u# ^4 k* o5 o' i# o
station.; Y) z/ K4 l! e. s# K
connecting hydraulic supply t
" T0 d0 L& ~8 ?& ua
3 K: u3 G' g# b1 P/ ?' p海平面静推
1 A2 B; p9 S6 E: ?( j" _封严,
0 W H5 I" w+ L$ \# k选$ A( U e% z6 Z' ?6 e+ C/ V j
.
4 ?: ` t* ^. w s' l- x选择活门,
, C3 r+ X) j1 p端连% t+ Q% l' F; {9 ^7 ?. n9 C
回油端的活门。
7 j2 ]. p9 N! v. q选择呼叫,# M0 r, K t, x/ ?0 D4 h
一个能自动将航空公司地面站呼叫报知机组的系统。
( K$ z( J; ?$ i g液压系统中,用于将液压源一端连接作动简,另一
7 ^; Z: e: k& Y' [接
1 g( S' s! n3 ]4 L: |; N英汉对照民用航空词典B
$ d l( K2 Y9 _$ \$ G* y9 fSELF SEALING COUPLING, A connection between two1 f1 ^/ w- e4 C3 g
fluid filled hoses for preventing fluid loss when the hoses
! I# Y# `2 W5 ^" N; F1 J+ M( t! vrated. N$ ^: N( q! B/ C4 ~+ Y" w9 f
SEMI-MONOCOQUE, Type of construction in which the
& E# U' q( g; ^SENSOR, An electrical device for detecting variable. Z* U7 m$ B9 _7 Z
ENSOR ACTUATOR, A device for operating the# \ p' D+ \: R
SERVO, An automatic control system which checks its" d1 h, ^1 y) [: Y1 z0 h
gainst its input so as to achieve a desired
% V/ p/ d' T: M- Y) y9 AMED, Hydraulic pressure for the servo is3 T3 J! [& F* ]8 l) {* {$ t# Z
resent to allow the servo to internally synchronize to$ |7 P5 j$ p' f5 p
e proper position, but the mechanical output of the) l: E% U( i$ B, d" w# @$ @
ervo is not connected.
; P. f: R' Z% [" @! l自封接头,
1 b" ?9 w! h" I9 }- p& e活门堵住通道,自动封闭而不+ V- r8 b- j# u# l4 r$ s" A2 ?" P, k
让液体流出。
- F1 {6 k9 C6 e1 g' \' L$ p' ?半硬壳式结构,
% T/ {3 e; A2 U S& z1 ~" j使蒙皮,长桁和隔框共同承受所有载荷的构造形式。" o2 c4 ]4 u2 G0 W, {5 ~
感器;+ s* y( o# s& Y/ R" [& C/ G2 y
量状况并将结果以信号送至指示器和指示灯的( d6 O( Q4 [" f* r+ Z
电气装置。
% z( w0 d `1 c/ y( m3 v; h传感器致动器,# O, n( O, t5 s9 ]- X5 M
。3 y# J9 t) t/ r' r, |! a
伺服系统,
% g2 \* n! a% F7 w3 h( k* p* s/ S能检查输出和输人数据,以便合适调控的自动控制系: A% m! j# W% }6 C* v
统。; q; g/ h& n/ X" ^5 n5 K
伺服预位,: E% P* x" j; O2 M F: K
液压使伺服系统内部同步至适当的位置,但伺服系统的 B; k1 [: m: J# g! Q* X
机械输出还没有接通。
" F! l3 o; n. h' J/ y" L7 _are sepa* e, F* G) L% D* h. C6 J, ^) d5 B
skin, stringers and frames carry all the loads., u9 r. x, o% h$ G$ I5 K' |# d9 \' N
conditions and sending a signal to indicators and lights.
( P; @6 a8 T" hS
* R- s$ ~" J+ ?2 asensor.! h5 h: ^* M y/ }. ~
output a
/ M( R" X" ]3 H' J. m! |1 }control.' [1 T; C# J' Z2 x& a( p
OEING0 _* M5 a$ A- y$ Q. G( _& z; Y
TECHNICAL DICTIONARY 132
2 e n& g% |3 e; m( |- Z/ nSERVO AR; f1 u" x V1 u6 D' Y0 [5 L
p
" \/ Y( \" `% J1 oth' p& H) U9 T% V
s& H& ]$ y, D8 F9 h6 {$ r3 Q
用以连接两个充满液体的软管的特制接头。在两个管子
! r6 m/ s) }+ m2 p$ j分开时,接头内的弹簧即使
8 u7 Y4 I9 G5 l g$ N0 o传+ L' Z& G( ^6 I0 N
检测变" f+ l% C$ ~, z* ^4 A# ]" x. @% C
用以操作传感器的装置
# g8 x' \# d) z1 S0 ^" R; e2 w英汉对照民用航空词典B OEING
" D2 k" m( R" f4 A$ jTECHNICAL DICTIONARY 133 |! a, l/ j5 H. w2 g* p2 j
SERVO ENGAGED, The mechanical output of the
" D, {1 R6 K& B& Uservo is connected and the servo can move a surface or- k) j; }! Q' e, X( Y
ontrol
" g0 C7 f J3 ESET SCREW, A small screw (usually headless) used to8 Q: T; G7 d* Q! m
eel, or knob onto a shaft and prevent! b' S- [3 ~* U% `/ y& _
tation.) j! u |$ W0 x
SHEAR, The stress exerted on a material or, assembly
' t6 h! o+ |9 [0 P9 B- Lwhich tends to slide the mating surfaces parallel to each
8 ]2 B9 x( D8 {. p! E0 bther.
( D9 S- [/ y3 O# JSHIMMY, Rapid oscillations (left-right) of the landing
9 a+ X3 x: f* Y4 S" q9 p$ cear wheels.
; D0 ?9 `; F. c7 P预位,/ h8 s1 L1 j# p& V+ B( r
伺服系统的机械输出与伺服系统已接通,伺服系统可移/ Z& S! W$ N5 v/ T8 P3 `
动一个平面或操纵。
@( }) l/ C) y; Q小螺丝钉(一般是没有钉头的)用于将滑轮,车轮,或
* Q, C! r6 }- j) C1 r% g钮紧固在轴轮上被免转动。
! G! C8 W/ b! O+ ^/ {c
9 B! S, c8 F: |* m! x c, Q, efasten a pulley, wh
. Q" q4 E2 N, G; L: M+ Kro [, {/ Z t* N/ C4 e
SG, SEE - SYMBOL GENERATOR
0 u U( L( G. v1 j& B Y- Yo4 v$ C5 ~% c+ Q6 Y8 J* t Z
g, R8 }5 E: E' ~3 R- z
伺服系统' ~! e8 j' L9 w1 P6 w- m
定位螺丝钉,
5 h& a2 a+ F$ ?8 H! |$ A旋
8 ~( d4 z5 s7 H0 |& q符号发生器,
f3 `$ M0 a0 D* k: J见Symbol Generator./ O$ U. s0 x' R. x1 L2 K
剪切力,
7 u2 ?9 D( A9 I. u& a加在材料或组件上的应力。该力往往导致互相平行的成
& `9 ~& p0 k1 F! B1 E对表面滑动。
, q D* L. Z3 M& L摆振,( Y; O6 H p4 @ O
起落架轮子的快速的左右摆动。
% z6 R4 a& K! |2 E英汉对照民用航空词典B OEING4 K$ o# Y' U2 u
TECHNICAL DICTIONARY 134
8 j$ p! L, i: [2 b% ^SHIMMY DAMPER, A hydraulic device for damping
3 ^/ I* s2 P! S, _shimmy in the landing gear wheels.- l* p3 W" ~" l1 l* Z) c. W' a
ar for7 c y. r& s4 v( m( Y5 H% h; a
sferring oil from one( C. ^9 u+ M+ P- l3 r
chamber to another through a metering valve.1 p/ Q3 d' |6 }8 I0 v5 [ ?
,' b1 t6 S! j4 c; l
一室以减
* B7 _" u% l1 g3 y& F着陆时产生的冲击震动的部件。" f2 W/ c& t3 w7 O
SHOCK STRUT, A component in the landing ge: ?& U" U3 Z/ U+ a) E& r2 u' H' R
absorbing landing shock by tran* s& f2 W3 ]) F$ |' Q: C7 a; e
减摆器,# t( ]: I4 P1 n& {# K) S8 C* ]
用以缓冲起落架轮子摆振的液压装置。
0 z: k w5 W( P( ]9 G. U减震支柱4 ?1 X; i! F7 t- G3 d$ a
起落架上通过计量活门将油液从一室转到另5 Y! V3 ~2 ~8 F$ i. [# {( Y1 i! N' ]
少
! S! A, ^: x3 ]( x6 E) b6 C英汉对照民用航空词典B OEING
6 i2 q# ^. ^- b4 a3 v' kTECHNICAL DICTIONARY 135
* M }* n0 b' |. P. s( \( dSHORT CIRCUIT, A fault in an electrical circuit
% [" a* y* R; b" D2 [7 X; d. koccurring when the power supply goes directly to
$ _3 E' e3 e9 P2 F2 ~ground instead of to an electrical component.
, Z4 v, a9 d* |! B( |' iSHORT RANGE ALTITUDE, A cruise altitude chosen to
$ J0 s" i) Y# W7 y: y3 M! }- binimize fuel burn during short trips.
! s, E* v; g+ N/ @- eHROUD, A metal covering for enclosing the APU on% H2 \3 d& d9 `, o
e airplane. An external tube for enclosing a fuel hose./ w) O X3 d) R+ z, P" |
HUTTLE VALVE, A valve in the hydraulic system with
4 l; O9 n- ~8 g& k% ]6 _8 A- STANDARD INSTRUMENT DEPARTURE
6 q) `! k! K# ?4 D. ff the6 i* {' ^$ f: l4 ^
r access to the components on the engine.
6 q9 `0 W# j7 S1 ~短路," }+ o( H& ^& H9 I7 X
短程高度,$ I% f6 c5 T7 O% Y( }. ?1 f
为在短途飞行中使用最少燃油而选的巡航高度。
" k( _; L. H, t. m! c4 G6 \护罩,' H& Z$ `# ~0 Y. i8 N
飞机上包围着辅助动力装置的金属罩。包围着燃油软管0 U# e H, s& Q. F; e4 P* u
用活门,
) m" _9 S/ y/ l液压系统中,具有两个不同液压输人管和一个输出管
5 N. d& Y! T5 u% R的活门。# i9 w5 K6 B& Q& P0 A% A
标准仪表离场,
# b7 G2 i5 V, S( n见Standard Instrument Departure
4 X; Y# J) z! Tm) ]4 ^- @4 {) F# E" u. J: x8 p
S
, z, z; P8 \8 Uth3 p6 ?' z" F5 K+ v4 G
S
3 J+ _. v/ H; W [" N+ a5 v0 stwo different hydraulic supplies and one output to a
3 D3 F' T, h# x% |" F" Ccomponent.- u8 Q" A; U( I+ W& J
SID, SEE
. h! N4 D9 i: u+ Z. b& j. kSIDE COWL, A removable cover around the sides o" a! m. N2 g" _* P
engine fo! H& h4 ~) O& P; t- x% y P4 H5 ~
电路中电源未经电气部件就直接到地线时的电路故障。 i2 z: P. z+ P
防
0 W& ]) u% P' k3 L3 ]的外管。
: p( R) h' X3 \" ]两
0 F9 Q" x! h# |1 J5 b.6 ? x" E* r& l: m p
机两侧,被移开后可以够到发动机部件的可卸罩4 e/ l: l$ v7 h/ n
。# }/ c& P! p9 j/ Q# w: N
侧整流罩,$ a9 O* ?6 b1 K5 @3 U0 S- S8 C
发动
( ?, U9 v* C& ]4 H子
1 Z& B( A9 n S! U. {/ \4 n+ }; U英汉对照民用航空词典B OEING6 w) Q8 _, i+ h3 U1 ?
TECHNICAL DICTIONARY 1360 ?/ o& g: O/ A" V# O- |
SIGHT GLASS, A glass window for observing fluid
% ?1 ~$ U4 p' Q J5 b2 C4 Cquantity in the reservoir of a machine.
+ `& p' P/ e! q6 z" f" [, that can be used to transport information for0 r7 G. s4 `# v% {# a. D
communication, control, or calculation.
& _; h8 L6 b9 l& s) ]ILICON CONTROLLED RECTIFIER, An electronic3 u- g G' v: E
device allowing current flow in one direction after the
8 p# {$ H$ T4 }! J x6 ddevice has been pulsed at the gate.2 h# h, |+ y$ h7 K
SINGLE SHOT MULTIVIBRATOR, An electrical circuit7 a+ H/ O4 u- `+ t0 ]% w6 d
-stable multivibrator.8 l. C7 V: L. Q: J1 w# A1 x
如电流或电压能用于传送、通讯、控制或
; d7 \# D8 e1 [算需要的信息。& t9 |# _1 W# p4 N7 j
硅控整流器,
. \- ~# o& {1 H$ s$ T& |/ q当其控制极受到脉冲后,允许电流向单一方向流动的电
" G* {" B! `0 T0 t2 f子装置。
! t- f! w0 \' z2 R. F5 K息多谐振荡器,* |$ n; a- j) j0 ~/ j
输人信号触发电路时产生的脉冲的电路。又称单2 D& d% ~- q6 m; G- y1 \% W- M$ _
SIGNAL, An electrical quantity, such as a current or" ~3 z, Q2 K% R6 v$ ?; }7 J
voltage* u$ J" ?/ g0 Y: n1 ?
S' y3 P& ?+ m0 V' e/ {- {
which produces a pulse when triggered by an input
9 ^& ~/ I3 ]# ^7 T/ }signal; a mono* S* F" d9 v8 D) e
检查窗,$ \$ h9 {' x2 G: P' i
用以观察机器的储液箱内液量的玻璃窗。
* P- R" u3 u8 N信号,$ }) i( g* g6 G6 L
电量的一种。! h1 s; m" }6 e: `
计
" _* u( Q0 D: `: O# J$ e冲% r( U, }, ~% d: B) W, E; R
当一个& D, `! r. u. B% ^1 Z9 L* w$ B
稳态多谐振荡器。5 A2 }+ O5 A8 j/ u ^
英汉对照民用航空词典B OEING& ?) g. ]% I- r4 s
TECHNICAL DICTIONARY 137 [' o3 H, p' a$ ]" i
SIMPLIFIED FLIGHT PLANNING, Rapid determination
* h3 f& K; `" rof trip time and fuel using a chart providing these data
& \. W+ s3 ^# s2 c( k/ Ufor the entire flight profile from brake release to landing.
6 A7 c$ Q% [. A+ Y+ lSLANT RANGE, The line-of-sight distance between two
$ s, { T5 ]0 [3 l3 ?8 o: S! Ppoints not at the same elevation." Y* |7 ^2 R: q4 k" a) C; f" x
SLAT, A moveable part on the leading edge of the wing
. h x8 g( w- D$ W2 C" c& ufor increasing lift at low airplane speeds.
6 B0 j6 {3 `, t$ k2 n* M* ^划,
1 P/ f9 p) k. S4 Y; J迅速定出从松
, l$ A% R+ i# i& D: d车到着陆的整个飞行所需的时间和燃油的过程。
. h/ Q/ P$ {4 l0 s斜距,
4 w9 o' \" \3 [. F# n不在同一高度的两点之间的直线距离。2 I" f/ k( Z( _3 ~/ K
缝翼,
$ z2 {# B/ z$ J) e5 i' K用以在低速飞行时增加飞机升力的机翼前缘可动部件。* X) g( E+ M! k. v
简化飞行计
3 ~! a% a1 x/ F由提供旅途时间和燃油等资料的图表,来
% [4 }/ m4 |& E8 N4 b刹
" K! y6 h" l, z) u英汉对照民用航空词典B OEING1 s! w4 O0 p: D W
TECHNICAL DICTIONARY 138
% ~ Q- H! \! c8 {1 q7 wSLOPE, The amount of incline a runway surface has* s* A0 q3 k% a0 n. s! M4 \* e+ Y; S
relative to absolute level.
" X+ E, m& |5 NSLUSH, Runway contamination made up of a mixture of e5 @, P0 Q' l+ Z" |. `& A/ Y$ F
ater, snow and ice.+ t" H- V- y1 O6 Y) ~
SMALL COMPUTER SYSTEM INTERFACE, An input
# x, U9 D' Y% H; I/ H% @and output bus that provides a standard interface* Z; B2 G' x: I: |3 j
between a computer and peripheral devices.
8 q# F5 C. d t0 ]) F% f* ?SMOKE DETECTOR, A device whereby the flight crew
* O. X7 i" r7 H8 J0 Z! w1 Jan be made aware of smoke or fire in specific areas of( t& L6 u2 h6 W$ u: O. L$ l* x9 F
the aircraft.
6 K- @; a( I. T' U6 R [* jSNUBBER, A part of a hydraulic actuator that slows
# t5 ^' R. V" b' N6 ypiston speed by restricting flow.' |- |, M8 t* b: K$ |6 v
OFTWARE, The stored instructions that control the1 u' s! ?2 L% K* k6 M
perations of a computer.# ?; B# N+ ?8 U
ng
1 p0 `7 C$ c) E* w1 Z5 lother devices.
+ W4 f% C! u0 H# bSOLENOID CONTROLLED VALVE, A valve controlled
5 ~* E) S1 c! M* w7 E( ito open or close by the solenoid.
; p2 N/ p4 J% D8 K( @/ i/ g雪泥,
5 O$ [5 s1 L7 k2 P P9 _积在跑道上含有冰、雪、和水的混合污染物。3 G L- Z9 N4 k* W! F% Z
小型计算机系统接口,
8 a5 g W& u) u* R5 O一个能在计算机与周围装置设施之间供给统一接口的! n7 q! b6 H- U6 k
人和输出总线。
8 n' o- F- l% N+ q% R: H2 h烟雾探测器,0 D4 O8 Y3 z! k! L. o- J
在机舱或任何指定区域内能测到烟雾或火并报知机组7 f3 [1 q$ ~& R+ Z. p7 j
员的装置。/ c( L7 z/ {" t, {8 ?2 j! ]
冲器,
: j% T {% w6 Z4 B; y9 \液压作动筒中具有节流孔的部份。这些小孔能通过限制
) p- |2 D% I6 ~. R. n0 f液油,以减低活塞速度。
1 `+ o0 c$ L/ D储存在计算机的指令程序。用来控制计算机系统的工
( Y J; |8 [ k; c, S0 S7 v作。
. F# L# n, c! D5 p, x! ]; \. v操纵其他设施的机电装置。
( [% j: Z, v! f' r电磁活门, R) _: e4 Y- j6 `' l" {& ?- G" Z
用电磁线圈来控制开关的活门
. W4 ^( o8 N, O2 ^( a$ ]w0 X, o* c8 i3 S+ B2 f1 f
c4 g8 h( z' v6 H0 ^* v' L
S% _0 U/ s9 W- {1 E; f
o5 T& I0 T9 E& f
SOLENOID, An electro-mechanical device for operati, W0 u* w9 U+ T& N. ]9 H% E
斜度,
+ c7 L( r% E6 ?- u! c9 z. E" s跑道表面相对于平面的倾斜量。
! l" B' _" c& S输: J/ ?* ~4 ?" m% @! M3 a- ?7 h
人0 t8 ?0 p5 f% y1 U9 _
缓
) [9 F7 ~4 B2 [3 q/ m' I1 B+ Z软件,) N; S7 R$ V }1 b8 r1 b' l) K6 K
电磁线圈,1 X. s$ w6 E+ r, i. @2 X, J
用以 g0 S- P- B$ i0 B; J; K+ F
英汉对照民用航空词典B OEING7 z! y3 _. _" h
TECHNICAL DICTIONARY 139* u! F1 R% s% @3 T0 X
SOLID STATE SWITCH, An electronic circuit that
; t3 C: d! E( e5 Z; R) u* `provides switching in a current path.
& `' Q$ D" o# LSOUND SUPPRESSION LINER, A component in the# ~* G& u3 s9 {2 C: [
nose cowl and around the engine for absorbing engine
; U2 H3 r$ S+ `1 enoise.2 Z0 f) [6 T4 u( D8 M* k
SPAR, A principal spanwise beam in the structure of a
$ p D( s: C2 E0 @4 FSPEED INTERVENTION, Pilot control of the speed: ^. g" F) Z0 C
SPEED SCHEDULE, The planned speeds for a specific5 i9 i4 H: \7 X& C1 x
phase of flight.$ A4 y O3 `( ]% ?# ]
晶体电门),. F r1 p& q0 z. Z1 E8 f
消音衬,2 Q* T9 j, \$ H9 W- b
在发动机的周围及前整流罩内,用来吸收发动机噪音的! U0 ^" x* s3 m
部件。/ W! E/ S7 D' \. P1 r. x, Z/ F! ^
梁,
1 ]" K" n. d: A! r9 ?* D5 a( [机翼、安定面或操纵面结构中的沿翼展方向的主梁。
* W: A" D, v/ Y& u9 v V& R! q D速度干预,$ o# M! a& Z- H8 ]5 [$ m& L& `3 d) W
计划速度,6 l% W5 f/ Q! Z2 A
为一特定飞行阶段所定的各个速度。
" s. V- m' V2 {2 nwing, stabilizer or control surface.7 `. t" `8 c3 g5 C' R6 V% ~
during VNAV operation.( o P7 O: Q5 O0 w x
固态电门(' b. n) M, N$ P& v, d6 l
在电流流经途中提供开关的电路。
) G. C7 s) @: m- d6 U2 ?$ ?在VNAV(垂直导航)操作期间,飞行员控制速度。
# c; {" m) x1 @# @: n+ J6 F7 H- S英汉对照民用航空词典B OEING- y4 }5 W* D( r
TECHNICAL DICTIONARY 140& Q. k* P* @8 y# f. f9 u
SPIN BRAKE, A device in the nosewheel well for
% j9 A5 X4 w, Pstopping the wheel rotation after retraction.) n. D3 P1 m% m$ S
SPINNER, An aerodynamic fairing attached to the fan of, L; X: D! z3 O, y9 W& A5 R
a turbofan engine.3 x% \1 o9 ^9 \
SPLICE (NO. 1), A connection of two airplane skin
' v' s# W7 |+ V+ m7 o2 [+ Ssections.
" u3 J7 N# I9 CSPLICE (NO. 2), An electrical connection between two* }/ H; J9 d7 s
wires., W( P4 O/ y; }
前轮舱内用在起落架收起后不让前轮再转动的装置。
, E( A/ L* m* k& {' M! L: y旋转罩,8 s8 r' ~. o u
固定在涡轮风扇发动机的风扇上的气动整流罩。
, C) Y0 R; L u8 I# z! J# Y4 z拼接,0 y3 ]6 O0 N/ k' m& o$ |; k
飞机蒙皮与蒙皮之间的连接。
0 F# m1 @5 J4 N; v0 t/ J铰接,
. E6 o2 a7 t ~* X9 G# q两根电线之间的电接头。
1 x3 Q1 i! q8 ], `* s停转制动器,
_/ _ _: W9 D2 a" k. q: r, b英汉对照民用航空词典B OEING; d' x2 j( @7 g0 s; u" d# \
TECHNICAL DICTIONARY 141& q' Z' }5 f* _
SPOILER, A hinged moveable panel on top of the wing.
( O& W0 M; I: ?1 t( nFlight spoiler- assists ailerons for airplane roll
1 N5 l' Y* F Z U(wing up and wing down) control& b2 S7 j' a# A2 ?6 |- B4 `6 V v# \
and for aerodynamic braking in& Z" Y4 x! }+ p& w; u
Ground spoiler-for aerodynamic braking on the3 Q+ C- M/ t2 O/ ]/ k. E3 x
ground only.
% U# |2 ^& p- A; x# i, QPRING LOADED, A condition in which one part of a# o# W. E o. i# t+ n8 ]5 B
evice is held in a particular relationship with another2 |. J* \4 A7 G: _7 b5 B/ t
t,. i1 s- C; C1 G& Z% x( N5 P c
r original position.# Z( n" m% @9 r
SQUAT, Airplane on ground condition.; M9 {5 m X2 }1 s9 ~6 j: X+ Q
QUAT SENSOR, SEE - AIR/GROUND SENSOR
: W G; u) k+ C6 y% I0 B. a$ TSQUAT SWITCH, SEE - AIR/GROUND SENSOR
1 n. V8 y3 g/ T5 f8 e% U9 s$ o扰流板,
% F } {) g3 K0 y0 y) ?铰连在机翼表面上的可动翼板。9 y4 [4 F& C- ^, S& q6 }
飞行扰流板一功用有二。一、协助副翼来操纵飞机) d4 ]8 G, b8 ^ v
的滚转。二、用以在飞行中或地面滑
" Y b' k T5 q跑时作为减速器。
3 O! g( ^3 T) ~$ M地面扰流板一仅在地面时作为减速器。
2 x# ~/ w7 W/ R6 D- i簧加载的,
: ?( B/ h/ ]6 v0 F由弹簧使一个装置的两个部份保持特殊关系的一种状
# @$ D# ?' }$ m$ ?2 g态。该状态允许一定运动,但继而回复原位。+ r5 M; R4 Y( y: W: {1 p7 b
着陆传感器,* A, c4 L C' ] C2 q
und Sensor
/ X" u$ Y9 N; o: X: ?& Cflight or on the ground.
5 F% B3 q6 v _3 s* oS
0 f- |: F0 y7 o5 L! yd
2 \4 K2 i) x& [1 g; x- Ipart by means of a spring. This allows some movemen
8 l7 u, [ @5 X0 c0 j1 X1 h# Tbut returns the parts to thei+ _/ ?" @% i& |6 K% q
S
5 a$ A' R" k+ l. _4 ?/ c弹
3 m3 `3 i2 s7 {8 A着陆,6 D3 @, E, e. n; i7 w
飞机在地面的状态。# W' B4 T6 y U( e/ J+ `, t
见Air/Gro7 K- R# T- [/ [ K5 ~0 `/ V
着陆电门,
2 N) q9 y# o; u, T8 h) {见Air/Ground Sensor .- J! z5 f1 o- G; W4 q& c! b
英汉对照民用航空词典B OEING7 @4 R& `0 X2 h
TECHNICAL DICTIONARY 142
' ^, Y5 q, j+ S4 N, R. X, I6 x) n* BSQUAWK (MODE,CODE, FUNCTION), Activate
7 e4 P" p( D8 N" Mspecific modes/codes/functions on the aircraft m8 Z9 ~# k1 D* ?( h$ Y7 c
ansponder, e.g.,” Squawk Three/Alpha, Two one zero+ {( z2 S5 ]. C+ C U- Q# H
five, Low".
9 ?$ K9 c: p( z! d& u3 u; n% qSQUIB, An electrically operated pyrotechnic device for
# U. Q1 ~4 ]% C9 T, }breaking a disc in the fire extinguisher bottle to release1 Y# z( ?+ s2 V2 x
the extinguishing fluid. Also used for escape slide! q; p5 l3 F4 H& ?, _
TABILIZER, SEE - HORIZONTAL AND VERTICAL4 ~$ M v: S& a, `( E. A
STABILIZER, y, k6 M3 X) W2 c2 ^3 o
TABILIZER TRIM, Movement of the horizontal tail to; i" H+ H5 ^% l+ J6 p5 D' j! n8 k. ^
hange the attitude of the airplane about the pitch axis.
! J# z1 K$ w1 p8 q0 |' J( G- Y) ^TAGE, A numbering system for the compressor and
% f- |4 N: R6 \* f! J: J% {9 C5 wturbine of a jet engine.! G& p6 k* z; o3 B! v" [/ p
TALL, A flight condition during which lift is destroyed
# l* ~. Y& O6 C2 l4 J0 a5 Tue to slow airplane speed or attitude.( M; ~% ~6 p$ Q( o i
to enter from the top and flow
1 i, p7 U z% A( ~4 mout to the system. It prevents picking up debris off the
8 f# M# j, I# s$ Vbottom of the reservoir. It can also control fluid height in
: Z% G) i2 e( p9 S4 Ythe reservoir.9 [) T6 [4 G: ~0 n
能),
4 D9 l, {, d7 B5 Z8 f/ @使用飞机应答机时的一种常用的指定方式/代码/功
( d8 c) r" L0 z7 u* K) z3 `能。
' ~+ A' {0 c$ T/ z. t2 I# i管,
1 j) o. Z- r( U6 s3 y用以爆破灭火瓶上的圆片,以释放灭火剂的电控烟火装2 x# ] ^, @6 r0 B0 X. r: O
置。也用于应急滑梯放出。4 n: W0 J, X3 k8 B6 ]6 I( @
定面,
+ T" @( }: F" Y4 ~见Horizontal and Vertical Stabilizer
7 {7 a) }- z% ~" n' ?8 Q/ ntr
; H5 b, r0 R6 \7 Xdeployment.( A4 l7 J7 M4 z( v" V$ ?
S5 ?# J* D3 n) z- w3 \8 i
S
8 v% Z. Q+ {- C6 Cc/ Y3 G3 P2 W; V+ A- n
S
, i( E, U1 Y3 ~8 M" r# D2 s- C; CS/ R# D8 _2 e2 m# m9 v; s" w! ^
d7 `1 A$ m2 i# M
STAND PIPE, A pipe raised up from the bottom of a$ }. J% F' k( [0 T/ X% D5 N& r4 C, i9 m
reservoir that allows fluid; s0 \% Y6 h1 `* U7 Y
发送信号(方式,代码,功
; J5 `5 J" n& d7 w% |& `爆
3 ^% m. s7 G; s, |# K1 W' ^/ O/ W: `. L安
4 n9 w3 [7 Z: J; z9 O3 [. J8 @.! {4 a( Y, X e1 J0 {
定面配平,
2 ~( z; p: _" D2 }3 H% `/ q- W为改变飞机绕俯仰轴的姿态而做的水平安定面的调整。7 V, d5 f% J7 [) g- U# A
级,8 a L: y) D4 a( |8 A, U. N* ~
用于识别喷气发动机的压气机和涡轮的各个段位的一7 |- {; Z$ B0 g( Y
种编号系统。
" {; N. x( l: u! T, u+ v7 W+ x- |) Y失速,1 i1 B# J7 O4 M7 p
飞行速度过低或姿态而引起升力失去的飞行状态。
9 O0 U/ t4 N1 W3 i回到系统中,并防止带起容器底部的碎屑。也可控制容2 v& M6 F& \' {$ ^1 ^) T8 K8 o+ z
器内液面的高度。
' Q1 j5 H2 \* G j安
: C7 Z+ q# J1 a- ?5 A立式管,- e4 x) i' @0 d+ P1 `* q$ q
从容器底部立起的管道。能使液体从上流流人,然后外( S, ~ c4 u/ X& r1 G
流( m# ~1 D1 i6 s$ Q9 X
英汉对照民用航空词典B OEING/ S+ |! N) [! m" p% n
TECHNICAL DICTIONARY 143
# T% |3 ?% X% n( e/ b" ZSTANDARD INSTRUMENT DEPARTURE (SID), A
% o! a' G) y: e* W* f1 m3 X# tIFR.3 Y3 _0 ]! k1 [' h% X
TANDARD TERMINAL ARRIVAL ROUTE (STAR), A' A/ p. O) u$ C
ublished procedure for approaching an airport IFR.
( g! a" n& V1 K+ d4 U* ^TAR, SEE - STANDARD TERMINAL ARRIVAL, Z+ F% K* @* X+ f
OUTE
; C3 Y7 U0 c Z0 QTART VALVE, A valve in the engine start system for4 P2 H5 |$ H0 y* |2 L$ u
upplying air from the pneumatic manifold to the engine
% T1 {# V- r4 d" S8 Gtarter.
2 h5 k4 ?8 T& n5 G3 @# W& d( E3 h kTATIC AIR TEMPERATURE (SAT or OAT), Ambient
$ L6 k6 k+ R _% j F' Aor outside air temperature.: y# e z/ V! ?. B: c
STATIC PORT, A small hole in the fuselage for sensing( A; B% t" ^8 R C
static pressure for airplane instruments.
8 ]' k. I6 r# [7 QSTATIC PRESSURE, Pressure in the air or fluid at rest! ~6 d: ]8 p+ w7 n
measured in pounds per square inch.7 t9 t4 z5 e& B. [
ID),
# s7 U6 A% @' I' A; q* [4 Z) N* C用于使用仪表飞行规则离场公布的程序。) Z8 `9 p, P7 Q/ l( D
标准到场航线(STAR),1 v/ ^: B9 Y( w) \
用于使用仪表飞行规则到场的公布程序。, E! k& J/ i# D9 H6 p
标准到场航线,
6 V8 A, f G( d9 h见Standard Terminal Arrival Route% S1 i2 l& T2 N# Q
published procedure for departing an airport
2 K; U/ v& d: @* u) LS
; G( L" z7 l# d c3 O7 }0 p- rp" Y9 v* L9 [& S
S' o$ s! C3 R0 t* u6 e
R- r! O) B5 Y% Y
S
" S2 { x2 [8 Z/ V" gs
0 K' }2 ?, K, |2 ms' V: b. L* C. Q& V+ r
S
' F) ^" E2 }* X7 ]- W标准仪表离场(S7 B- l# s8 ]6 M6 z
.$ b! z) d: a, X G( z9 P( {
起动活门, f! K& s \5 j" t# K$ @8 |
发动机起动系统中,用以从气源总管向发动机起动器供
5 Y$ M5 @ d; k4 S5 ?的活门。
/ k3 U0 T1 A0 i3 @温(SAT or OAT),
7 p: a2 i( f( D7 j4 R8 K0 U环境空气或外界空气的温度。6 p- D! F9 T* I- N
压口,
4 v6 o( C4 W. B& b位于机身外表,用来为飞机仪表感应静压的小孔。
$ B' x1 e1 Q$ l9 l5 g: a5 L9 }静压,
* y: r2 H: S% n静止状态的空气或液体的压力。用磅/平方英寸来度量。
9 C+ D. m( S% ^, }8 q气
% b+ R& D% \' g- E1 |/ v静4 ?1 q" D0 \; v4 ]+ C
静
/ T: Q2 h6 N5 j4 j1 @% W+ O+ E8 ]3 Y英汉对照民用航空词典B OEING+ j, U- _- W) ?8 _# H" w
TECHNICAL DICTIONARY 144$ ~* e7 Z# t q3 q
STATION, A vertical reference plane along the fuselage
$ A5 _: [4 |, Nfor measurements along the fuselage./ r# V4 a4 v; P4 p1 ~3 B" w
TATOR, The stationary section of the compressor4 Q1 q) c. F% O0 G) V2 N8 {8 @/ ~- I2 g
etween the compressor stages in the jet engine.
/ w& [6 B0 j3 X7 T M% FTEERING ACTUATOR, A hydraulic actuator on the( G, P/ V0 \6 ~
landing gear shock strut for steering (moving) the5 E& ~5 y! { Q+ j9 X; b4 B' b; y, o
nosewheel left or right.7 S2 z% f* e9 R! `6 S# D
TEERING TILLER, A hand-operated lever in the
/ H1 i* Q5 q5 e/ |) uosewheel left or
8 C2 s' ~& M v# K8 L9 Mght.) j, @ U( x% i9 {/ x2 v* V
TICK NUDGER, A device to push the control column
9 r4 z. ~& C9 I E/ Frward just before a stall occurs., n. c0 j) Q/ D
站位,
1 j: y6 z& A4 y/ ?$ z用以沿机身方向度量的垂直基准平面。
" e, l# t& Q) \) Q定子,
7 s. i/ V: A* r* ]喷气发动机压气机各级之间的不转动的部份。7 i: H, g$ h k9 r- F8 B5 x; ]8 h
弯作动筒,- A9 a/ ?# r4 W
减震支柱上,用以使前轮左右转弯的液压
" K- y) Y- {( @/ [作动简。% f/ S/ Z' P- Q9 N; A5 x# s4 C
轮转弯手柄,
J8 F: N) D, [/ W# y, i内用来使前轮左右转弯的手柄。% U$ Y7 c7 g8 R7 O0 a
动推杆器,
) P1 P2 D" _" f" N: D在失速前能将驾驶杆向前推的装置。9 o& g; ~- X! P% d3 i& A
S
) e8 [$ j- h, J& j/ bb( y2 \9 g$ ?( m" A- w/ J0 X K$ O
S+ @$ t3 }! j' Q8 X# t
S
, L: Z5 y, \7 i* Bcontrol cabin for steering (moving) the n6 j! d! c& t( M5 c
ri& r+ N: [% f5 Z4 u0 V
S6 z" L& G+ {5 b' E! x
fo' c8 L6 d0 b6 R# a7 r/ `
转
8 j' t+ G! ], m1 {3 s$ L9 y一个在起落架0 ?$ G3 ]6 ?9 G% i
前
4 m; O$ q/ i9 c驾驶舱
; j( j# y0 ~/ K' o. u* g9 |; W# O% u自! H ^6 W6 h5 @
英汉对照民用航空词典B OEING) V! d/ T. N) t/ [
TECHNICAL DICTIONARY 145
; r7 l: o9 m3 B- c1 n9 V4 `STICK SHAKER, An electric motor operated devic$ @3 _ s1 Q6 c3 d6 Q
the control column which shakes the column be; y9 f/ m6 i: G" a
stall occurs.
4 G$ x; s$ d l! Ke on
; P6 p- W6 i5 cfore the! E8 j. R# Q; t7 j7 T
TOPWAY, An extension beyond the end of the runway e4 B" s. ]8 N v: {! A2 S3 G
hich may be used to decelerate the airplane in case of
* u& O5 z9 P4 S8 F# Z' wn aborted takeoff. It cannot be less than runway width/ d. U3 r& U' x$ A; [5 ~+ _! h
and must be strong enough to support the airplane% I, i6 {" \# M& T8 D
置。
) ~; I+ u- N4 n+ y速安全道,& W- {' i, t4 I7 V" W* a4 X
跑道两端,可用作在中断起飞时飞机减速的延伸地带。
" U* {' ?' \6 {- y& r2 q它的宽度不能窄于跑道,硬度也必须能够支持飞机以免结1 E, T- \- w7 j
S
1 T4 t U; v1 @# ~4 O+ Y8 V f; B0 iw
V0 ^/ C: k* Ra
% S9 n: V+ L# }* z5 S+ D( V Bwithout structural damage.3 u6 Z/ X: h1 ]1 q4 ?4 ~' ^8 {
STRAIN, Structural material deformed slightly due to the7 g5 ^! p @" x, O- y
action and forces of stress.- w7 a' H' g; X+ }: a6 V2 w8 o9 _3 E1 g
振杆器,# w" l% u u$ k0 q- H$ e
驾驶杆上,在飞机失速前使驾驶杆振动的由电马达操4 I' o. y8 D. o% ]4 J: R# V" C
作的装
8 `: @( b9 G& y) V减, ?: Y. Z! m, h" c
构损坏。 w, m2 [, n2 `( ]
应变,
/ A4 [, n# j9 d& g" d/ x1 e因应力作用和受力而轻微变形的结构材料。
, |+ a) C- ^* ]9 j1 z& k英汉对照民用航空词典B OEING
* }+ s& k5 @; xTECHNICAL DICTIONARY 146- M% U* ~5 d+ I% p' H6 {
STRINGER, Structural components in the fuselage or
, S2 P, ]% V a+ lwing for transmitting skin loads to frames or wing ribs.
5 N$ E; M8 P8 g% d z& J# K( M4 gSTROBE LIGHT, A high intensity flashing light on the
) U3 g. ^# b- L2 ^/ Twing tips and empennage.* k e$ o3 [; ?9 i4 M+ e7 k* ]
STRUCTURAL MEMBER, The part of an aircraft3 \" l3 _6 v* F+ E/ c4 I
structure that has been designed and constructed to2 W* u- \6 x' l0 o& k+ O, J$ ]
carry and accept loads and stress., M, |/ V* D% y
STRUT, Mechanical components of the landing gear for
" m/ W/ H2 ~, ?! R' ]keeping the gear in the extended position.$ w7 n% K) s# [! z8 ]
机身或机翼中,用以将蒙皮载荷传至到隔框或翼肋的结
, r4 h* c" o! C; Z构件。9 t8 ]; z% I/ v
频闪灯光,8 l( \# o T7 w7 `' f: T- k
位于翼梢和机尾的高强度的闪光灯。, a [4 ~. W0 w$ h
件,
0 c2 ]& f3 S0 k" j- C5 a飞机结构的一部份。为运送和承受负载及应力而设计建
( f2 C5 [, {# o: y成。
: {$ b5 h* }/ `6 h支柱,
4 \# c; C$ I2 g" \) g N起落架上用以使起落架保持在伸出位置的机械式部件。, ~3 X/ S4 E) Q4 m ?7 z
长桁,
' `. I) `1 o- j5 X9 X% J构
8 }. Q. d ~+ R G6 r! {- b造
9 c! K$ Z) z9 V7 b1 Y英汉对照民用航空词典B OEING
0 C# `/ ^0 w; g7 a: b, {% ZTECHNICAL DICTIONARY 1475 h8 Z u& C9 Q; I
SUMMATION UNIT, An electronic component for! i4 u: ?) H! A% H
adding fuel quantities in all tanks sending a signal to the( r' [* S. P' v$ o, C% I
tal fuel quantity display.5 I. c- s* j+ U# L n- @1 i6 G
UMP, A lowest point in the engine oil system or fuel
) ^# B1 W- H: ^" C$ T3 K& j$ @! Onk.1 i1 d# s* h4 v
UPPLEMENTAL DATA, Additional data stored in the0 J% w! {: Z! f' F
MC memory, supplementing the loaded navigation4 i* M5 {$ c# N. w5 v4 F$ d
ata base.- H% G2 ~+ b5 F, N- {4 N
n
- Y' k8 s! t- N3 L% Ueviating from normal modes.
( Y2 `$ N; x u' R1 cSURGE, A sudden change in the airflow through the
/ \1 _, p$ _) \; bthe compressor not being able4 N0 k7 ^9 c; G9 q! Z9 J1 u
compress the airflow.8 L2 {5 i9 B' [
SWAGE, To squeeze together two or more items to
$ |& X2 g3 |" Y Y: l+ }* h+ b% Jform a permanent unit. Example: a lead or steel piece
9 Y1 Y, {% G% d( e9 y& fon a cable which forms a stop or camlike unit. Also to! y7 C1 N5 U( h# e! @5 ^
reduce the diameter of tubing.& y4 J( l5 G1 b- Q
SWITCH, A device which changes the condition of an
. C/ u9 C1 y0 i4 Belectrical system from on/off or open/close.
% n6 J, o) n0 l! ?8 s7 N+ b3 n7 V燃油总和器,
5 I- l. A9 s7 w- j6 ?, h2 W将所有燃油箱内的燃油量相加,并将总油量用信号传至
- d9 G. I: h, T5 g* r量显示器的电子部件。
7 r3 t' A; V+ M" A) n! F2 }1 J }集油槽,
# y2 ~3 _' C+ X7 A J发动机滑油系统内,或燃油箱内的最低点。
9 W3 g5 S% M7 z+ B增补数据,! `, P2 u4 _2 {. y$ B
飞行管理计算机存储器中的附加数据。用于补充导航数6 k9 c) j$ L) ^4 }- x8 z1 `/ K$ ~
据库。& n8 ^; m; L! E- n; S4 M- X1 W
,9 h- i) l3 d7 R7 f2 E
附加的数字飞行控制系统方式,当偏离正常方式时使
+ Z2 r) o* E4 U。
2 I$ V* p( T( Y/ X! `4 r6 f8 C过发动机的压气机的气流的突然改变,而导致* @9 P1 y$ T$ A6 e. f
气机不能压缩空气的现象。
, D$ q. D' a3 X6 w陷型模,
% p/ D1 \; O! F6 E挤压两件或两件以上的物体来制造一件永久性的元件。8 U# z* G6 w u A$ \% u
如:一块铅或钢在钢索上形成一个止动器或凸轮之类的. f# {+ ^+ a3 n2 v3 b! H
件。也可作减小管道的直径之用。
5 c: c2 L( _, k0 w开关;8 e9 G& W$ f8 z5 C- {& l2 ^( u2 a
改变电气系统通/断或开/关的装置。5 e5 N- n6 Q; x0 X6 v1 x
to- U0 e2 k9 e3 F# s. w. ^2 v; j
S
" i+ B7 i2 b6 ~7 s+ X2 D/ \ta
9 a: A4 y& ]- S5 S* [S9 `+ h5 |" \3 m2 y7 h* J
F
0 A0 ?: `9 Z( ], O+ c7 H7 hd8 o# h$ f4 g9 A
SUPPLEMENTARY MODES, Additional digital flight% p1 I8 B0 K0 }/ U7 c/ R- L
control system modes that are available, used whe2 g. n5 h+ t$ [: K% G7 F
d1 `& D( Q! A' V; T
compressor resulting in
( w' h& {8 K% i7 h) _3 B. Jto& F; B* \ H6 B3 o+ z* n
油
0 G, ^9 A& I) r0 ~辅助方式
0 @+ o6 g+ \1 w7 c" ]' F; \用
$ L" |, r, o8 q) L喘振,! e7 u# i% t ]" v0 t
由于通
! w# V# b e; J) n压
5 F5 G. J; I1 u4 q! t9 g1 B8 N |例$ E" Y. y- e+ U- ]8 C
元
3 X. q, f+ ?- I& M, F' u英汉对照民用航空词典B OEING1 `/ ~' Q3 J, p+ ]2 W4 b
TECHNICAL DICTIONARY 1486 \ U$ F* u% |0 p$ \3 b# b
SWIVEL, A device for rotation of components.
& u& v7 L) g/ QSWIVEL COUPLING, A junction in hydraulic
! q$ {& w. C6 _& }( @' obes for allowing component movement.: C5 X& J& k. F/ m$ o& j
YMBOL, A graphic view of an aircraft component in a! @5 S/ u. f- i- P/ z" C# s
ery simplified format. Used on drawings to represent% Q9 ~5 J6 V$ \% R6 b+ B y2 o) K
e entire component.
3 w9 J) N1 k+ K# C3 |+ ZSYMBOL GENERATOR, Generates the video signals8 Y s! f p H1 O+ V
that are displayed on the EADI and the EHSI.$ \6 H+ L- k' X3 R
SYNCHRONIZER, A device or circuit to make the units
" T- Q" Z& c9 |8 nperate in unison.& C1 n! c; ]( e: Q4 B: G% A
SYNCHRONOUS, Refers to two or more things which6 O8 E: j' j! O9 P( g# m2 g
happen in a system at the same time.
6 i8 F: C: K% P用以使部件旋转的装置。" Q1 Q3 k" x% z# v6 a* V
转动接头,8 }$ |8 e( ~* N9 c6 t
液压管线上,使相邻的液压管能够动的接头。
* [# N# g2 _$ p2 f/ A2 I符号,
7 R! t' R, H/ m* W; k) q- t5 f飞机部件的简单示意图。用于绘图以代表部件的整个结
1 A; {* o4 Z3 t b7 e构。
2 {' Q3 R3 S$ }/ g符号发生器,
+ @' b; k4 n& E5 l, e9 k8 s8 F: V为姿态指引仪和航道罗盘产生图象信号的装置。9 j/ a5 Q: B, r* i& Q6 F8 H. N
同步器,
0 |8 j+ q: [5 @2 M2 h# B使元件操作协调一致的装置或电路。, j; K2 j" z5 ?! d" Z% L. a
两个以上的东西同时在一个系统中发生。7 {: A+ O- Y9 R6 z0 e/ J& m% U
tu
0 R5 \0 U( y, X* z8 O8 T0 n) kS8 ~- a: ^, v3 T
v
) m4 |/ T# b ~- b$ E3 Zth& q/ @7 G! C7 d( H. i0 Q2 ^
o
2 ~3 i$ ?7 K. a转座,0 j/ e; L/ Z: B$ h
同步,
# p5 {( h& a. G l$ b: Y指两个或, ]' T1 `8 }7 g0 G/ x0 Z3 E
英汉对照民用航空词典B OEING
2 b" k, ~7 Z2 t& vTECHNICAL DICTIONARY 149& r- P1 J' Z! G i3 T* r7 P& D
T! ^: r, b$ v% ]) K6 z6 W7 y
AB, A small, hinged, moveable part on the trailing
- M% T+ q2 I, ]) y) E/ @dge of a control surface (aileron, elevator, rudder).( p" X9 |/ N) P/ Q% F: d4 i$ }
Balance or control tab - moves in an opposite8 O3 ~7 J0 b4 @
direction to the control surface for assisting
: N+ h' a, `" n$ n: ~& x! g5 rin movement of the control surface.
2 j7 {1 y" [! |) s$ O$ aTrim tab - provides controlled deflection of ailerons0 G+ [1 A1 e# W* {
or rudder to compensate for imbalance in$ `+ o9 U' E p; |8 T& I3 g
thrust or fuel quantity.
1 N5 P" B: N/ k3 T7 |Stabilizer trim - controlled deflection of the horizontal8 _0 {/ T5 s$ z" H- `5 E1 `8 C
cy3 H% Q q4 Q+ R3 M
proportional to the speed of rotation.6 b) w, I T; Y$ _" X- o
TAI, SEE -THERMAL ANTI-ICING
; |8 o ~' M+ J4 S! LTAIL PIPE, Duct at the back of the engine exhaust.9 @& p9 W1 Y9 b. ?# H
TAIL WIND, The wind component relative to the' a$ V. z. K+ ^0 Z5 w! h& o
airplane direction and coming from behind the airplane.
/ G4 l, [8 P9 x调整片,
2 n. j4 D/ }6 A) E$ K" V' j. J: L7 o铰接在操纵面(副翼、升降舵、方向舵)后缘的可动小
, S+ S' Q {2 C& s: W部件。1 e# R$ v) z- H+ A
平衡或操纵调整片—与操纵面运动方向相反,用以帮/ ^. H* O* |& H" l# g
助操纵面运动。6 B \0 i# E; h1 R `1 ~
配平调整片—使副翼或方向舵作控制之下的偏转,以, c" R" e! T' [ `3 b2 U" O
补偿推力,或燃油量的不平衡。( d! g' s7 q! R: H; l; z7 f
安定面配平—使水平安定面作控制之下的偏转,以减
# P; Y- F. z0 V& R6 O+ Y少操纵力。
( M, H. k' b' Y2 K- I9 I; Q' x) z4 A机," C1 K6 `$ J2 Y. M
提供频率与转速成比例的电流的小发电机。
' X: ^$ i# C Z热防冰,
5 c8 ?3 I2 g" B0 H% e& U) {见Thermal Anti-Icing
$ Y( s6 l! [/ w6 J' kT
% h/ z5 h2 ? E" ]e7 t0 }5 M) d" r- ~
stabilizer to reduce control force., y/ K: C8 z/ A% o7 R8 @
TACHOMETER GENERATOR, A small electric& j. }; l1 f8 A! B1 _# v9 m
generator for supplying current at a frequen5 o1 y/ P( c5 ^( J6 L% a& G
测速发电" t4 [* A. X* l7 Y1 H0 `
.
+ z+ H! O- M( a5 @尾管,# B0 s0 q/ ~' m3 V
发动机排气管后部,用以排出发动机的废气的管道。
( H, J" m6 @! E) I% U: p+ N, ~+ i顺风,
+ L. |4 v7 Z& Z& z3 h* J飞机后方的来风在飞行方向上的分量。* m9 A6 H0 ]) d( w; P4 ], l: ~; ]
英汉对照民用航空词典B OEING
5 q H3 B' X: V4 T) }. k$ m3 hTECHNICAL DICTIONARY 150; T d) ^( l6 e2 _7 l8 y
TAKEOFF ANALYSIS, Analysis that evaluates the/ g2 O }, A- r2 f5 Y% F, Z2 U
airplane takeoff performance capability for a variety of Q. m+ X# ?( S9 t3 f. @ v
environmental factors at a given runway and airport.
" K N' k5 q* k6 t6 O& rET PARAMETER, A specific goal such as
6 R: |, S/ J+ B( Z1 z) P; N# [irspeed, thrust, engine speed, altitude, temperature, or
$ P7 z+ W6 S% P% j/ _+ vte of climb which is to be achieved.
; c2 j4 J3 y$ WASK TICKET, A computer label used for tracking the
p# k# L Q. z0 |( c+ r4 j, `7 M( Mompletion of a task.( V, P+ v1 _- i- d0 Q
RATURE8 \+ p* Z7 K: D7 I0 f$ q: O- M' n0 Y
AXI FUEL, Fuel burned from the time the engines are% ]$ v5 ~3 B3 E: e: h
r.
. \4 V, f! w, ]CAS, SEE -TRAFFIC ALERT AND COLLISION8 o+ t& D, E. s9 c3 h( d. E
VOIDANCE SYSTEM
) i; m+ }, o0 F3 h$ J1 d欲达到的特定目标,如空速、推力、发动机转速、高度、, C1 e {% C; j& ?- v
度或爬升率等。2 o6 G0 ^; @. K9 {
工作记录单,
T8 u9 n% ~) d: j2 a用于追踪工作完成情况的电脑记录单。
0 O' b% K+ z$ V6 G全温,
% g Q- U6 g. A5 a5 h8 R见Total Air Temperature
: Y; W+ q+ I6 A0 d$ p* v2 G0 TTARG
7 |* @, r/ B, P$ x7 w4 y: z) o- Ea' i0 j; C+ @! C/ d% y' W8 _
ra, ~* v+ Z/ I3 q. ~( F& m0 _
T
% a1 j; E. y" r6 gc5 }" d. B( Y- R5 X5 v' ]( s
TAT, SEE - TOTAL AIR TEMPE/ S) a, ~$ ?& W6 S" {4 B8 x5 d9 P
TAXI, Movement of airplane on the ground using z# a L: K: j; ^. |( U
airplane engine power.4 @- \( y% _- D6 g
T
0 }! ]( e- j% lstarted until the airplane begins the takeoff maneuve n( \$ @3 u: l5 M( h6 }
T8 z5 D! e5 e0 b! }" ]. n
A
/ O1 V) {/ I- Q2 L+ }/ o起飞分析,
0 c6 U2 C! N4 ]4 c0 V' L0 g9 P2 }对飞机在一个给定的机场和跑道,在各种环境状况下的
9 l- V& a' X! T0 p! ` `' }0 a5 L+ ^起飞性能能力的评估。: M, H2 `$ s/ T6 o2 m! a
目标参数,5 O" e( R4 _/ d: p" h. C+ S
温
9 Y0 E# @' I2 J: V9 a·
( l d- e2 O9 X滑行,
8 Y G" u* h" b! ^: G行燃油,% j5 ], l, k" W" D' ^# o0 l
起动,到飞机开始作起飞动作之间,所消耗的
% n- l9 n$ ^8 R# W; g中交通警告与防撞系统,5 C! i$ i# `+ r o
见Traffic Alert and Collision Avoidance System1 i$ E& x+ q9 ^& }7 Y
飞机凭借发动机推力在地面的运动。
\( P4 o4 r2 |4 a滑9 n: n" U9 \" @9 R M5 G
从发动机# D+ U* p$ l6 Y& o- C6 O+ ?
燃油。
/ s! A! `1 z/ D/ Z空
, P) L6 D+ B# |9 n4 R.
# V, i; d; r$ H! w3 \+ B& I r英汉对照民用航空词典B OEING
3 l6 E6 i& [+ Q, n9 |/ n) YTECHNICAL DICTIONARY 151
% C: T7 I- j5 }0 mTCC, SEE - TURBINE CASE COOLING
# d c! A* r, E) E+ i0 nEE, A pipe or tube connector manufactured in the1 l' R7 z6 A7 @6 C5 U# u
EFLON, A synthetic material for hydraulic and- x( j u) W$ r% D% |: N
neumatic seals.& D8 r! s7 U( ?7 {) l
EMPERATURE INDICATION STRIP, Temperature3 I( C, _, l' Y5 S4 n% J
ensitive tape which changes color at high temperature
& d* w0 `4 c2 z7 l# I- V8 ir indicating component exposure to high" x, n: N7 Y4 e/ \$ A
TEMPERATURE INVERSION, An atmospheric
1 @/ i0 i* f7 T- q! J* pcondition which causes the outside temperature to+ u r& q2 c; o7 Q8 N) B8 S& y. j
increase as the airplane altitude increases.
# g8 c8 ^8 l- o! wTENSIOMETER, An instrument used to measure the
- H% k/ U( U- d) x& Ttension applied to aircraft control cables.8 h1 u9 k! I, h N9 H J
冷却,
7 L/ C6 B% R5 E2 sT8 J+ f5 h9 l7 g5 U: I" _1 N
shape of a T
u* z W8 h; t' L8 z, @T
' d3 Y3 }# i( g+ @" w% P9 g; }& A$ Mp# A8 r# o! B/ j% |& |
T
- i7 `! J# P6 u( w7 G9 ^' zs
1 {' V& J$ i9 R% Vfo2 m0 ~7 } y5 h% T) v' D
temperatures.
& r+ w8 x, i9 |2 W% O9 ^ t9 R' o涡轮机匣
$ ]# D1 m1 T; F. `# | b/ L见Turbine Case Cooling.8 F# N% B1 i' O! ?) x$ D1 X D- m
字接头,
" S% ?5 F1 T$ B. Y的管道连接器。
' ~1 ^9 L4 j5 J& O) R6 b氟隆,
2 N/ f8 B. O/ E& Q用于制造液压和气源封严的一种人工合成材料。# x6 J5 g; l4 S6 l6 Z( e" N
度指示带,
- \+ X5 @1 G+ X# Q& m3 ~. q遇高温变色,以指示部件周围高温的热敏带。% g# j) w+ R: f4 f) g* o! b
逆温,7 c; R1 n2 z3 m- G( ]( V& |
一种大气状态,引起外界温度随飞机高度增加而增加。
z' S6 `$ D4 B3 S! A( K. P张力计;+ l5 d$ b' I. M
用于测量飞机操纵钢索上受到的张力的一种仪表。) e6 v7 v; g/ g& f% ?: J7 E
T
1 k) Z) O+ V' [! e制成T字形
% M [# ^/ {" O1 w3 a: B/ j" X泰
: _6 J7 W2 k& S2 l8 F# O9 q温7 S* U n; q& ?, F4 q
英汉对照民用航空词典B OEING
) u5 o* c5 e3 \ G6 z& uTECHNICAL DICTIONARY 1528 g) x8 |) J1 z+ ]* }- j
THERM& ?8 u/ D' y; S" n7 F
formatio$ a' q1 E% H. Q/ E! C
using ho' P9 I5 P- O7 _' h
AL ANTI-ICING, A method of preventing ice
5 C# d1 ?/ y" qn on the nose cowl and wing leading edges by, a( C& f f, l+ ?; T$ {
t air.
- v1 M9 N- h+ @* z6 lTHERMAL t
$ N% R/ j* T- p2 h9 Q; C6 Ein a tube fo en tube
3 S) L& b" x! W- e! P2 x' {is pressurized with oxygen.
1 ~9 o2 n8 p' h; K% n3 {) B& THERMAL RELIEF VALVE, A valve which opens to
! _9 Z: q! J* l# W2 gture.$ D1 n3 m) F3 T% I8 [5 Q- q+ V
HERMAL SWITCH, SEE -THERMOSTATIC SWITCH/ v* y6 M2 @# S2 p
e
/ a. F2 P4 F4 }5 M' ~7 rsistance changes with a change in temperature.
) V0 _" H9 Z& C5 ?+ ^! ]6 d防冰,
/ D. h2 M8 d- T3 }; B用热空气防止发动机前整流罩和机翼前缘结冰的方法。& A/ x8 d% e3 k
在管子里,使管子受氧气充压时温度不致于上升的一& f; p: f- Z- a
个刷子形导线元件。9 ~# t3 y/ t: H; y! Z6 |4 l3 o
控释压活门,
/ k# ^$ m7 t, j2 ?* \过高而打开,以减低流体压力的活门。
5 J; o5 u! k# o& q电门,1 A/ E, _' P( P/ |3 e& W
见Thermostatic Switch
) m& i$ I2 z. OCOMPENSATOR, A brush-like wire elemen( e9 k# |5 W' ?
r preventing temperature increase wh0 T W# G' B3 F' ~5 E
T. N% k6 V1 c u4 y L$ C
decrease fluid pressure due to high fluid tempera, M: i7 z8 k5 p. z5 W+ [; D
T4 {: T* o9 _1 l4 F) F
THERMISTOR, A temperature sensitive resistor whos5 K8 h' D s9 w" n4 G A1 J7 t
re
) Z9 g+ L O5 T/ D' n7 _2 w7 P热. M3 W8 v# y# q4 h: z* h
热补偿器,/ i0 I* b$ I0 \; [
装
4 c8 @, \/ s+ Q" c7 ^热
9 h8 N# h, d. D9 a; @' H! Y因为流体温度
2 d7 q7 W, p& `. M" e( V热' `* ]: h& L, F: s
.
9 C! c. C' Q; m5 D+ `,热敏电阻
: t$ z* t& x, m" ^4 N+ p一种电阻值随温度的变化而变化的对温度敏感的电阻。
3 ^" X0 w# p; o" W0 H6 O3 u英汉对照民用航空词典B OEING
0 h* x4 S, g% e5 {* O+ fTECHNICAL DICTIONARY 153
) d. R' w: J) n3 w- x% ~0 e$ nTHERMOCOUPLE, Two different metal wires joined at! V% ? p" j, R1 H, M
urrent is produced proportional to the temperature
6 {5 f9 m4 y6 l; u2 F F7 @difference.$ Q, ?6 L4 T/ L5 Q$ ~( E3 K- T
THERMOSTAT, A component set to operate at a
/ [3 E% j" d" v: ~- r. Gefinite temperature for controlling electric circuits and
0 n9 K# G" Y# E+ ~alves.
2 S$ T, Q, g+ K/ ~8 Xmperature sensitive switch which opens at a preset
. C; ? V1 }1 H' p8 d( I* ~' xmperature.6 ]/ ?" h& L! M0 Z
THR HOLD, SEE -THROTTLE HOLD
0 t. }4 l: g8 i0 K* ]2 P) p( Y- ~即产生与温差成比例的电流。( ~, L2 H! H/ q: m
用来在一定温度下操作,以控制电路和活门的部件。
2 u R; C) p# }$ W% w恒温电门,: c( t o7 T0 w3 Q- y- O2 {
一个热控的、在预定温度断开的热敏电门。 e1 Q+ s/ u2 S; D& @. `4 H' s
见Throttle Hold- K$ `9 @, y& ^8 G2 d3 J* g
both ends for temperature measurement. When both
$ e u1 K5 a' c) M6 l2 U Cjunctions are at different temperatures, an electric# m0 W' M* G+ o# \' |
c
* e7 B$ r: l2 y) J& p( j' ]d8 l* Y0 @" w4 X# b2 {* i
v) G: w& [4 @& a% N* v- \/ H: Q
THERMOSTATIC SWITCH, A heat controlled,
% V0 Y1 q( o8 Ate
8 \8 x7 ?% V% \( a; `; z* yte6 X7 F# W6 j- s1 [- F* X e% R
热电偶,
) _8 _* e6 n0 m3 T/ Y6 K* O用来量取温度,两端相连的两根不同金属导线。当两端; B! c H% t8 w& Q% s" {
之间有温差时,金属丝内- y" L( f" m( l# `' D
恒温器,
d a" s f. j2 z I0 G7 `( M) v& s油门保持,
% V, \! D! m1 j+ e1 U t; e$ O.
x! v- ]1 q* R7 [7 v& k" ?英汉对照民用航空词典B OEING
2 f+ @4 H! z# m& `TECHNICAL DICTIONARY 1547 ]+ k x3 V6 O+ ^& G, v8 V, [9 u
THRESHOLD (NO. 1), The bottom part of an opening in
' }( z2 B3 ^1 Z* ^6 m: |" fa fuselage doorway.' C$ A( v- k; h
. 2), The approach end of the runway.8 `' Z3 t9 {# M5 z
THROTTLE LEVER ANGLE, Angle of throttle lever
/ n$ o$ k8 L( k+ ydisplacement.! N6 x& Q* }" Z, i
HROTTLE SPLIT, An engine control condition in which
* V$ d- q8 u3 ^* N! c/ h# Vthe throttle lever angle is different between throttle/ Q0 j# f5 {7 p4 m3 ~
levers but the engine thrusts are the same.6 T( q9 g, ~# x
HROTTLE VALVE, A valve in the fuel control unit for
3 r) h, k" [$ p& H1 c2 jcheduling fuel flow to the engine.2 F" ~ {% |1 G. e! g
机场跑道到场的一端。
5 ~8 o' K* S: o( c; Y油门杆角度,8 w( g; d& p6 L
油门杆手柄位移的角度。
; ^6 b1 i( [' V油门分叉,
/ |7 b5 B5 M# S' o一种发动机控制状态。在这种状态下,油门杆之间的油
2 z9 {; ?3 _. r# y0 h' z门杆角度不同,但发动机推力相同。
# m8 g1 }# y: S6 T3 e$ N0 P7 P4 T- m流活门,
& i, l% {3 C3 A, A/ z, o燃油控制组件中,用以排定燃油流量的活门。
, m# @/ [ `( E' TTHRESHOLD (NO4 X" G7 z0 ~& _. U
THROTTLE HOLD, A mode of the autothrottle where* M9 Y+ f X' C- L8 F$ a0 }. \7 e
the thrust levers remain where placed.- I; X% q4 V/ \) q0 W
T
4 Y+ @8 h* C- X/ KT
% Z2 H% a4 F% W- A7 P* R% Hs
N5 ?7 b' J9 t" ?门槛,2 K. T: |+ E$ k: V
机身舱门开口的底部。
2 l. Z3 b( \( A# m) c跑道头,( V0 Y' u5 X) k1 W. ?5 U9 y8 a
油门保持,
: [' h; K! W( D自动油门的推力手柄不改变位置的方式。+ l( b- D! c3 m, \
节& e0 z+ C$ u# V; d
英汉对照民用航空词典B OEING- O3 w1 c7 w3 ^! K! I
TECHNICAL DICTIONARY 155
2 V1 g2 Y* q! D" B8 ITHRUST, The driving force produced by a jet engine.8 l( t1 \; j/ ~$ h5 D& [" P3 ~6 i
HRUST LIMIT, Maximum allowable thrust for a specific
# x" \4 V C* E. xet of conditions., m% ]/ S- [& a
HRUST MODE ANNUNCIATOR, A display unit or part' C* d6 a8 a. N5 p& ]1 e
f a display that shows the engine thrust mode.; ]: c+ `; V; D x6 p0 M
HRUST REVERSER, A mechanical device located in
, a; t# @" i4 g# De fan or exhaust section of the engine for eliminating6 W0 E4 K! M) z: d! M* B3 J
rward thrust by deflecting fan air or exhaust gasses in
1 D1 v, N! b: c' Le forward direction can be used for stopping during
+ L! K) C6 Z* | G( v8 c9 \- b; slanding and during an RTO.( A0 c; Y8 [' K
推力,5 G3 i" k* C s
力极限,
, |# j; C; y# o* _6 f& r0 T& v& K在一组特定的状况下,发动机的最大允许推力。! F3 l4 @( I7 h6 Z- w
推力方式信号牌,& I6 \& h& r& w E. u% e
显示发动机推力方式的显示器或显示器的一部份。
8 |' w1 b$ {5 E# E5 l! J+ }$ ^反推装置,
! y8 b% Y* U" B& b P% x! ]位于发动机的风扇段或排气段的机械装置。该装置通过" f3 r$ H6 Y3 T/ r
使风扇空气或排出之废气冲向前方,以消除发动机向前的
( m* T A& i( g2 Y3 d推力,并减短飞机在着陆或中断起飞时的制动距离。
; @7 t! `" R5 w7 L- {0 e: jT. |" x5 N( L3 d( i. O/ \/ p/ d
s
% c9 P/ k6 f0 k2 j4 e& o& r* wT- d& f% n+ x0 a/ v) E
o
: I6 i7 ]% ]" d4 \! Z4 ^6 ^T
% ~/ t$ Z! S- p# xth9 ]! a+ L* F0 u6 U
fo
8 M6 S1 v3 N" I! cth" _& u9 U6 a, J" C
喷气发动机的驱动力。
7 K4 J [8 U0 [( a0 ~) ]) Z推
2 ?' m3 O( h/ I, n% o+ q英汉对照民用航空词典B OEING6 }( {( ~0 z( g# F7 i, D- q. J
TECHNICAL DICTIONARY 1568 I O5 @9 `& @( ?4 Y
THRUST REVERSER COWL, A cover around the thrust
4 v* h# o7 T8 V' w1 k7 Z6 F) ]IME DELAY, An electrical circuit for starting/stopping
( n. E0 ], u, c# J7 E. K4 ^e flow of electric current to an operating component
8 B. ]6 r3 L3 a& Q9 u0 rr a period of time/after a period of time.
* k8 G: ~8 E- lIRE SPEED LIMIT WEIGHT, The maximum weight0 C4 a! J8 I7 X% [& t* C( r
permitted at takeoff that results in a liftoff speed equal to1 t% Y/ z+ r) f4 M' h
e rated tire speed.
& g8 c% D' T6 c" Z7 oOLERANCE, The part of a specific measurement that
$ a) T1 Y4 c0 V, {! @allowed to vary in dimension. Usually given in a plus7 {) y3 Z4 [6 I8 h- O+ [
) or minus (-) format.3 t# c# N* E0 f# ?6 P
CLIMB, The point at which the airplane* O; x* P5 |- ]) W
reaches the cruise altitude. p; g4 @# p: W! h) N
ts the cruise altitude and begins to$ m U4 @$ N$ p# B
descend.! a/ y! ?4 x; c) J/ @ @
for transmitting8 q4 g+ ~2 Q: t9 D
twisting motion to the control surfaces.
% i A0 p7 S2 e9 C' P3 x) R9 q) k,
. h i! k6 d5 c0 Q% [的
+ G: d& U/ ~* s部件以进行维护。/ ? I3 j) C: R. A
延时电路,& ~" q! B6 p1 ]% Y4 n& |
用以起动/阻止电流在某一段时间内后进人工作部件 @8 ` |' a! Y M6 _5 ^, W$ n
的电路。2 y( x- H8 E) i2 H0 n/ g
轮胎速度限重,
7 _. B6 ~/ y! S飞机起飞时,使离地速度和额定的轮胎速度相同的允许% t, s \# _; n/ i! R8 @( `9 o
最大重量。+ i4 e) z7 a# ^/ a+ x
公差,
% g" n! s8 I+ \% D4 |; a# H0 H% z$ B0 v特定量度容许有偏差的部份。通常以(+)或(-)
+ h0 M7 u8 }$ O. v3 q的形式表示。+ Z% I9 m. Y- b- y$ j% S
爬升顶点,3 C, _ V6 w+ J" @: _7 Q
飞机达到巡航高度开始平飞的那一点。; g/ L5 p7 P5 Q I" f- }% M3 j* `* Z; s
下降起始点(TOP),; |8 C8 j8 i) N* s+ B/ |4 Y+ i
飞机飞离巡航高度而开始下降的那一点。
b( \( x5 s+ B# H" Z操纵面的管状部件。
3 r) L) x7 g; W" m, greverser of the engine that can be opened to access
C2 c& a/ a/ T/ R" e$ ?components for maintenance.
2 E4 l0 Z$ s: k8 c, jT9 S; G( X7 |2 f5 z- I
th
$ H) w0 a1 t4 R2 Bfo3 x6 T7 H/ g u7 [! O4 b$ M
T
& U) ?3 V& I" \9 ~5 s Eth
. g* b* U; C, S1 A- s ZT0 t. t* x: C% w% \
is/ f. [2 s. \- Y
(+
4 R2 N% d I7 V8 [0 D+ G# GTOP OF
6 B1 h; a" l( N7 q$ lTOP OF DESCENT (TOP), The point at which the9 _- L7 }0 e z& i! `: P
airplane depar0 `) f$ ^" q% r! J, W
TORQUE TUBE, A tubular component
8 x) k1 A B; _+ {3 ]反推整流罩
" G* @5 m0 \4 @1 E+ m6 z& v在发动机反推装置外围的罩子。取下后可以够到内部
, A9 v, B& b# d6 {* l3 p8 O$ U扭力管," h' s, o9 f2 n) R3 j# j {# P
用以将扭转运动传给( Y! Y5 @0 n4 x3 I% h
英汉对照民用航空词典B OEING4 s6 @1 T2 w/ n, V2 Y! D- k
TECHNICAL DICTIONARY 1579 M( j2 H8 z7 k6 O V3 @
TORSION, Twisting of a material or part caused by# H- y1 A9 h# s
external stress.& ^2 s" ]1 S$ `# F( _
ORSION LINK, A hinged linkage connecting the inner4 R5 W7 Z$ z3 T% f7 h
nd outer cylinders of a shock strut.8 ^5 I6 Z* E/ c" c
due to the ram7 d- I+ a9 P, _- e& @: _
ffect of high speed flight.
6 O4 [6 H/ P- O+ {4 d3 T: R0 v% QURE, Pressure higher than ambient, w! j+ L" V9 | Y+ a/ l
ressure due to air flow, measured in pounds per/ u: T& u% F0 Y
quare inch (psi).
Y# l0 V- P& Qer than' u. C+ B6 W; M% m6 Q' K" q4 \
mbient temperature due to the compression of air flow,7 K E; X8 z/ J6 f( x+ I6 {& b
easured in degrees Celsius (C), or degrees" I. @+ t/ J" i5 B. B4 @
ahrenheit (F).
$ {+ T7 s6 D% T* f' j9 h( KTOUCHDOWN, The point at which an aircraft first2 S- J: I) i3 I! t
makes contact with the runway.
6 H9 U4 f, e; k9 ^生的扭转。4 r# ^6 N- B& k2 f6 ?2 `
扭力臂,
0 q1 P- d5 g& c: g( Y! f8 c5 v减震支柱的内筒与外筒之间,用以防止活塞旋转的铰链: u& v5 c8 I. \
连杆。( ]" \2 i$ U$ I$ G/ c2 E
的冲击效应: z# j. z# F9 S! Y# ] H
引起的温度的升高的总和。
6 a8 [% X# M9 o- H总压,
! E/ _, G% s* B; n; N+ X由于空气流动而高于环境压力的压力。常用磅/平方英7 @# ~( L* G9 r0 x% w- w3 v( G/ L7 h9 n
(psi)来度量。$ `2 S, e, g Q' o5 S9 A- Y
全温,9 A# k6 ~; f/ Y0 }. d5 G
由于气流的压缩而高于环境温度的空气温度。用摄氏+ E/ ~/ c# V/ q, H. g% c1 u) U+ l' c
(°C)或华氏(°F)来量度。
5 `% e( O8 p: w- w0 m, o: p" W7 o接地,
, [. l: n( e. I8 M# w飞机降落时,飞机最先接触跑道的一刻。- k% r# a) ^* Y8 c1 [
T
; m1 Y: t6 R2 q, O2 T1 C$ i* G5 Ca9 l- S3 r7 j$ l
TOTAL AIR TEMPERATURE, Ambient or static air' C: `" _* Y- o# c; G* o+ a
temperature plus the rise of temperature
W$ W" i6 s' C% r/ d7 I- R+ W7 ve
; l. u7 o9 N) P! {+ XTOTAL PRESS7 b4 C/ A+ y4 g) _' Q6 z$ `& a
p9 j, ^+ ~3 w. D9 c0 ~- c% ]
s
$ |' `. R- O7 m! V. uTOTAL TEMPERATURE, Temperature high
c" g* p# f9 i6 Q9 ta+ N- j4 D/ o3 O& i8 z: ~
m
p- V; ~4 U+ Z" T1 Q. rF
" Q7 \. r# j) x3 k+ W, N; X扭曲,- y! a" n- v6 B2 j; I
物体受外应力的作用所产3 Z% C! F5 E* \4 F: ]1 n' Q9 ?$ U6 B
空气全温,
; i" d/ N* P. N. t3 L环境温度或静空气的温度,和由于高速飞行8 K+ E$ q# w# ^
而9 m$ H; x3 Y% Z0 n1 F/ {8 r
寸
) j& I" H4 }$ A4 ~! R英汉对照民用航空词典B OEING
$ L& g- @* \0 P' a" ]% q$ T2 N' Y$ LTECHNICAL DICTIONARY 158' W5 ]8 y. \- _4 F [
TOUCHDOWN ZONE ELEVATION (TDZE), The
* f7 k2 N7 m" |; n$ S2 m2 ^; O+ Chighest elevation in the first 3,000 feet of the landing3 I& K$ Q8 }8 L7 ^7 t/ V, C
urface.
" j0 [) {3 @( u& F1 vrt of nose or main landing gear for
3 e4 E! T; f4 L' A( _4 x9 ittaching a tow bar to move the airplane on the ground.2 h' U1 G' O4 U
along.' H2 l" f/ s4 F. I. n
RACK (NO. 2), A navigation term that describes the. Y3 o/ ^9 o6 k
TRAFFIC ALERT AND COLLISION AVOIDANCE
- P8 C8 |' n: b/ Z' w5 G/ r8 YSYSTEM, A system designed to alert the flight crew to A$ C. M5 W0 F+ z# Q
potential conflicts with other transponder equipped
) z" c* e- Q) I: xairplanes flying in the same area." k* W( X, s2 ?6 m) @* i+ D$ b' n
TRAILING EDGE, The rear edge of a wing, stabilizer or
3 j1 t6 a( t+ m( |control surface.
6 U8 D, b- ~9 l. s' \ MTRANSDUCER, An electrical device that either takes( Q( o. z& F2 z: q) @+ {! f
electrical energy and changes it into mechanical
9 G2 |2 j8 P$ p( E9 {8 T3 c8 R5 D. Nmovement, or mechanical movement and changes it7 N3 [5 Y4 {* A+ c, k) j
into electrical energy.
: D0 I B6 u1 x5 X @* @TRANSFER GEARBOX, SEE - ANGLE GEARBOX* _1 ?, t0 C, B) U0 [# T9 ~: h+ M5 P8 V
高(TDZE),
1 @ {4 a8 I' ]0 [高标高。. H& n7 R0 R8 v1 ^0 V2 j4 M
前起落架或主起落架上,用以接上牵引杆以便在地面上0 O! k w1 W( M Q& @
动飞机的部份。
4 n5 X3 ~ O) B7 f轨条,
$ f" o [$ p' e$ \3 T( s$ w; L迹,/ W& S6 c5 K5 I8 M
形容飞机航迹在地面的投影。
5 b+ R [1 z2 _# K空中交通警告与防撞系统,! x- i( x( s6 B; ?1 y/ h5 O0 m% \
用来警告机组人员可能与其他装有应答机且在同一区9 C$ d1 r5 m& U s' J; N
域飞行的飞机有冲突的警报系统。
4 N$ R& ^$ P' v后缘,
/ L9 J: S, }+ Y: R5 `* A机翼、安定面、或操纵面的后边缘。' ~8 g9 ^, l& `0 p! a
换能器,& m& y9 ^7 W) E% e n; j+ w: k
能将电能转换为机械运动,或将机械运动转换为电能的
# T! \8 x) K9 _$ {/ `电气部件。
+ ]7 S1 @* \8 ?8 T3 h* r" _转换齿轮箱,
6 b) p( O% T2 P$ U# `见Angle Gearbox& x# H6 t. L0 M6 v( `; B# o
s$ ?/ T: G. N$ t: I. K) f2 s
TOWING LUG, Pa
( U5 \8 a$ |9 G4 G+ d4 sa* l: n! h8 ^9 [6 T, [7 @$ V. B! B) x
TRACK (NO. 1), A structural member for attaching fixed
- f& n2 d# J7 B6 y5 z- E1 s8 t! p) vcomponents to, or guiding movable components
$ N5 R# m' N3 V. |+ K1 ? U! h ST
5 X+ t4 L% F+ mprojection on the earth's surface of the path of an. W. n" I# }1 y* S2 k3 R& V
airplane.: B" U3 Y# h5 k. ]2 v7 J8 s
接地区标: t! I G" e% F2 Q( L
跑道头端3,000英尺的最
$ ]; y8 q/ n5 j& e牵引环,8 F$ y2 O0 s* O! H! C
移2 W6 I* y- z; g1 P* q# J. m# n4 \
用以接连固定部件,或引导可动部件的构件。3 s+ K! K/ }! m' F% C
航: c) G- P+ \4 E7 C
导航术语。* U, e8 d' P& m' o
.
- n9 i _' b8 a英汉对照民用航空词典B OEING
8 a. W( ~7 }* \7 sTECHNICAL DICTIONARY 159
/ T% a. c% R, s2 {$ w+ QRANSFORMER, An electrical device which uses( J$ \' E9 @, @: A4 M& @
RANSFORMER RECTIFIER UNIT, An electronic, [5 C5 O3 | |$ a0 e4 X5 U2 L3 k
evice for changing alternating current to direct current K7 _1 R/ u X
supply airplane electrical systems.
" I, M/ ?4 l8 ] S/ f! A& J, b) @lse signals or triggering pulses
- ]: \ e- M% _9 s, C hnd cause component breakdowns or failures.
9 z5 z3 | @5 P) a0 i9 KIt consists of a base, collector
" l% y% U& D! K1 Gnd emitter. Two types of transistors are PNP and NPN.
. A) ? e: w% E+ J+ G' W。
- n: M- D2 e" N" O6 u) _+ ~变压器,
& P6 L* J5 r$ Q" ~磁感应,将电能从一个电路转换到另一个电
7 ]8 e2 l7 q2 s/ H变压整流器,! T, P, J _- |+ D/ G
用来将交流电变为直流电供给飞机电气系统的电子装
" M+ x3 C4 ~& x置。
+ _) ]3 @) p: q瞬变,3 d8 r ~, V( I
信号或输电线上的瞬间电涌。这种电涌常会产生一些错( N$ C5 l" _7 N r, j0 L. z; A0 @% I" ^
误信号或触发脉冲,造成部件故障或损坏。
( u9 q2 P. Z# e3 x! H晶体管,
1 Q0 G1 s% \9 }6 ~* A固态电子部件。通常具有三极:基极、集
/ ^! C' r. v, N+ Q0 _( ?极、和发射极。有以下两种:
! r5 P. v' V8 S% y0 O' N; \PNP(正负正)基极电位低于发射极。! k4 o j' o# u4 H
NPN(负正负)基极电位高于集电极。
/ z/ J1 H, J/ _TRANSFER MECHANISM, A component for6 {' V2 ~$ A, e( }0 {0 N
transferring motion from one place to another.3 W" m2 q% g0 E0 y6 G8 A) L
T: p1 m! G3 I" D' s
electromagnetic induction to transfer electrical energy6 L! A* ]. M/ i9 E
from one circuit to another circuit.& z3 I- S( O D0 k$ h+ t3 W
T
& ~* M+ H7 t6 Vd: A Y) V( S& H8 B5 _7 G0 Y
to0 U8 r9 k: L: U! v/ z1 d1 o7 a! T6 Z
TRANSIENT, A momentary surge on a signal or power
/ u v2 M" z: J- j- Eline. It may produce fa) x$ c0 @5 A1 m Y6 R/ t" q( Y; X t- z
a- \0 l0 I- r7 @4 a% m
TRANSISTOR, A solid state electronic component for3 B1 D- e& U! ]8 s
use in electrical circuits.# g8 u6 L6 X6 k9 U* y
a
# {* C. w) j. M4 `3 t5 n- T转换机构,
. T/ m& `. j. o# a2 i: U5 `将运动由一处转至另一处的部件
: H3 O: w7 s( z# z一种利用电9 W0 \) W- Q9 a* l
路的电器装置。
$ \8 @/ ^' i, g) f6 y7 k9 N3 C+ K电路内使用的7 l% o7 L: W' }" I/ g' g+ o
电6 x" f- v/ V. Z7 G: p: @4 E
英汉对照民用航空词典B OEING# B: ]( o) z1 f* S6 O3 ? x
TECHNICAL DICTIONARY 160
) z! w8 u: [; }+ S+ N. PTRANSITION, To change from one phase of flight to
% w/ @* h, ], gTRANSITION ALTITUDE, The altitude at which the
- [: C6 u) Q- D1 i; o4 Mltimeter setting is changed.
. K- p; H+ b- A/ Q9 rRANSLATING COWL, The movable outer portion of
4 C" L$ q! I4 Me thrust reverser cowl which is operated during4 b% f2 i% v& n/ B. y9 ^. b! m/ ?
verse thrust.
) c. ^; J! y0 ~7 H; Y5 eRANSMITTER, An electrical component for sending" g5 @9 C. W# ~+ F- G
formation from one location to another.4 v2 j! v5 y- J; B; d
TRANSPONDER, A radio transmitter-receiver which
4 S' w: G/ ?* H6 ?9 Vansmits identifiable signals automatically when the" j4 m/ N3 }7 k2 q4 q1 g5 m2 q
TRIM, The adjustment of engine and airplane controls
1 A% f O' O2 x0 [+ ~4 n0 C/ x从一个飞行阶段转成另一个飞行阶段。& R' \; L8 r" A5 }# C$ y
过渡高度,% }' i: f) w5 }$ M# [. l8 w" [/ J
改变高度表设定时的飞机高度。& U! P3 I7 i* p" a5 j
平移整流罩,
5 z6 o" w& I* ^" K* v2 G' Z7 o反推过程中使用的反推整流罩外面的可动部份。9 ~( J* W6 t1 s
发射机,' I+ R3 ^) q% S3 U" _' [
将信息从一处发至另一处的电气部件。
- A& N; Z' O. m* b& l应答机,
; u* @* [6 q- S! q在收到合适询问后,能自动发射可识别信号的无线电收
6 q/ l4 e- a- o2 I/ ?( N3 k发机。
: J' \7 b3 q: h- d" N平,
) g: f ]- b0 r1 i动机和飞机在平衡的状况下工作而做的发动机
$ i5 X. ]% }6 W, l) Qanother.# ^( w1 R' I4 G- {5 T
a
6 ? ]' H0 g2 c% Z5 HT2 v+ ^" d% I& s" k
th. s+ m8 b! M+ i
re( L' P! c6 v8 ], f- c2 |: P
T: `: y8 o. n! _) c) k
in
2 j0 i3 S) N/ h# d, @" Ptr
& z4 |2 r/ [2 a: O% O& t" @* b8 Vproper interrogation is received.
( f1 n. H) c2 Z1 @- [' ~/ U! }+ ffor a balanced condition of operation.$ }5 n0 r; Y0 _6 x( c
过渡,1 Y% G/ N# T: N$ Y/ }
配
9 d+ u$ X$ ?$ Y# w l7 x, w为使发
0 R# _7 n p+ b. r1 G) z( C2 I和飞机操纵系统的调整。6 i3 D+ Z" ^. w! x2 ?
英汉对照民用航空词典B OEING
9 d& ^* v6 B7 ?" T$ NTECHNICAL DICTIONARY 161
; M3 c$ C H$ [) @" N" V2 V/ aTRIM TAB, A small hinged movable part on the trailing
/ p+ N6 B4 @% M: Dedge of a control surface (aileron, rudder) (see TAB).
_9 j; h6 ^' T& f4 h9 _L, The total fuel consumed from brake release
/ C2 f" f T8 o. z e2 ~through climb, cruise, and descent, to landing at
# O2 K$ b5 M9 r% C! D8 _; sdestination.+ i. z& y2 E I7 ]$ [3 u
RUE AIRSPEED(TAS), The actual speed of the. ~1 a7 F. p/ w' u: q% U+ U
aircraft in relation to the moving air. The true airspeed is. {6 S0 X4 u$ F! e
ated airspeed corrected for position
2 ^3 H' Y9 ]4 }+ \2 d3 |) qrror, compressibility, and temperature effects.
& t2 @" Y) n1 k( L( ~2 X+ ]ribes
( _- @; F1 Q4 J0 u9 nthe output value for each input& f# u, v, Y1 y% W' M: l+ G
ombination.. x# k4 |8 f8 j" Y* y# r( ^, ?) r
铰连在副翼和方向舵等操纵面后缘的可动部份。' ?; x, x/ X4 }( M2 `( [
航班燃油,9 u( k6 f/ T5 K0 b: H8 e* }
一个航班由松刹车开始,经过爬升、巡航和下降,到2 j( s) i% i2 v, l/ t
目的地着陆为止,所耗的全部燃油。
9 X' a8 K; D( U- T) a& e4 C& \1 v变压整流装置,3 k9 x9 R) V% T9 |
见Transformer Rectifier Unit
% ?5 K p+ a9 @! ~& ?TRIP FUE: ?3 P$ i7 Q+ h8 e, K
TRU, SEE -TRANSFORMER RECTIFIER UNIT
8 Y" c2 _9 a) A' Z% ~* L& HT
, _" C" O1 t a9 n/ ]equal to the indic6 d$ }; \) b4 \9 [
e$ G2 \* e: z* o W! H6 r
TRUTH TABLE, in digital logic, a table which desc
& x6 i9 ?* m+ j, k8 i9 X7 k1 \a logic function by listing all possible combinations of) l, y3 A8 [, L4 h
input values and shows
# x4 ~. a+ I, L: c/ Fc J! l$ F1 X) I
配平调整片,
0 b" T6 m; S3 w& b4 R* @ J, S在
H7 U" ^9 h2 Z8 j.
8 X( Z" s: q- B. W# w/ p真空速(TAS);
1 S9 k# }8 p6 z0 d+ n对于流动中的大气的实际速度。由指示空速经过7 _' Y) M: B: V' ^/ @6 C, [- H
真值表," w( G( h C# f, c$ H8 r
数学逻辑中用来表达逻辑函数的表。该表列出了所有可8 H0 i) q# E+ Q
能的输人组合,和每个输人组合所产生的输出值。
8 v) W0 G9 B% ^0 H4 ]- X飞机相% U; [7 c8 R! h. U. L
位置、压力和温度校正而得。
) k, \0 B, n7 Q) x0 p英汉对照民用航空词典B OEING
" b8 g" }$ V1 n4 J' DTECHNICAL DICTIONARY 162
3 u; ?" c9 n2 Z0 Q+ H& U' kTURBINE, A rotating part of an engine which
! a$ e6 h4 K5 ?& T7 h# U% W/ X- Z7 X) lkinetic energy from the combustion chamber ga& Q4 W, l v+ ^& j+ R
extracts
# j6 ^4 q) x. J& K6 ?% e3 }5 H! Hses.
8 p( T7 i8 H/ ihis energy is converted to turbine rotation which3 l! X4 f& c9 H" s# Y5 ?3 r
tates the compressors and fan through a coaxial3 d% M T2 Y* N) r
haft.
$ O3 N# f7 H4 A4 c) d7 MTURBINE CASE COOLING, A method of cooling the1 }" V5 L8 M( ?* k2 a) _6 _2 k
ngine by using fan air. This cooling process is used to2 w ?' ~6 x7 b+ g
TURBOFAN,
. A/ Z: W. `) R0 G ~(1). A jet engine in which the first set of blades is a5 E: I7 J# X. }" X
large fan.
2 S8 Y" Z o' ?; r) @$ P, O3 K(2). An air driven fan/compressor used in air
2 a9 P; W, q6 Econditioning system.
8 F' x% W! @. u2 n- ^/ VTURBULENCE, The movement or shaking of an
% R2 U3 q! M. n( A7 I7 d5 Vairplane caused by unstable air masses.9 V0 A! q" I# x$ v5 J1 ]1 }) L
涡轮,
: F! c h! |/ |% e3 j( D发动机内,从燃烧过的高温高压气体中撷取动能的转动8 q8 U* z1 l; a/ }: C
份。该动能使涡轮转动,涡轮则经由同心轴带动压气机% F% v9 Q: p6 u; e# ~
风扇。8 _& |1 U( M. X# I% b+ v! F
涡轮机匣冷却,2 r/ K9 q0 T& q* _% u! H
用风扇空气冷却发动机的一种方法。该冷却过程被用于
4 S: [. i1 q3 Q效率。
7 }8 a6 W; G( k$ h8 c% i(1).第一组叶片构成一个大风扇的喷气发动机。
, r* _6 T+ L( C. Q3 N. e(2).空调系统内的由空气驱动的涡轮和压气机组合。
/ h+ l# z# l% Z" U. ]颠簸,
( R( [, |* \- l9 c- B6 y: U! w由不稳定的空气团造成的飞机运动或抖动。
, I, a3 ?3 h+ R( nT' x' E* y8 z' O! v8 a0 J# N
ro
) g* E* B' C1 K6 vs" j' |% l6 T" E8 R6 E
e
% |+ ~5 G1 I" s" ?' B. V2 o4 Iincrease engine efficiency.
$ C7 `& k9 q9 t部
: }& \) [+ C4 B4 ?6 P和3 J0 L2 J9 P$ j! n8 V+ f2 g
提高发动机
4 u3 ?; S$ P) z2 w" Q8 T! O W涡轮风扇,
" O) ~, c( {4 e8 `) b7 a0 n英汉对照民用航空词典B OEING
5 d* a! w/ T. h3 b) @4 ?3 `: q/ ATECHNICAL DICTIONARY 163! T3 T0 w9 D' w5 }: h
TURBULENT AIR PENETRATION SPEED, A speed
% S* i& S2 V1 t( Tthat provides adequate maneuver margins when flying
/ O* v& R/ [/ i8 L* O5 Mto unstable air masses.
; E: `" x& C! d! @) K- @, G+ Wht0 g/ E! B: l# O7 w8 k
stment in the control9 w. H3 n& C: S5 l1 u
ables.
) Z! ]5 O! x$ l4 jUHF, SEE - ULTRA HIGH FREQUENCY+ s* d+ D p% N& l6 ?/ W
NDERCARRIAGE, SEE - LANDING GEAR" ^5 z, g' v6 Y/ X3 f5 J
UNIT, One of the type, a single component.
! k. V* Y- d4 Q h9 wUPLOCK, A mechanism on the landing gear for keeping% Y1 M, A6 g, c X3 @. K! [
the landing gear in the retracted position in the wheel
" E, K l! h ^+ h/ C* W2 \well.0 ~1 K3 r6 O$ w
速度,
4 ]" [+ |( k! Q纵裕度的速/ |9 ]8 c, f. ~
。3 Z' S/ a/ ?4 O& ]6 i
调整操纵钢索张力的, v$ i, s' Q: ~3 K, v0 l% ^
械装置。
; w8 F: W6 q- [' l0 T* f* ?7 z高频,; A! W2 b* j7 `; z
见Ultra High Frequency9 z) f: j0 b" b' D
in$ l) H+ R8 M' {% l B
TURNBUCKLE, A mechanical device with left and rig# H* n. I3 T6 C1 u V5 F3 l0 F0 a* a
hand threads for tension adju
6 \$ i7 O8 X/ G7 b1 @% @c" i+ h. X9 B& k1 c
U
6 d7 [- w$ P0 a" ]6 y, OULTRA HIGH FREQUENCY, The frequency band
9 D5 k4 a1 j# \' C, f. ebetween 300 and 3000 MHz.; t; \* t/ ?* B0 h0 R
U5 P" s3 n+ l& x
颠簸穿过
# W; A2 m/ z+ _. |飞机飞进不稳定的空气团时,提供适当操" D: ]$ B, a& ]9 [9 S
度1 g: W7 I2 ~% X
松紧螺套,% v* p2 I5 J# f- v
具有左旋螺纹和右旋螺纹,用以+ T0 x8 {( n* [) t7 `8 t
机
- a: G# X1 F# o/ {超- l( S6 j7 d( o* c: S
超高频,6 |' ^3 l! g0 V& G* A
频率带在300 MHZ至3000 MHZ之间。; b% Z, [& P) {+ x0 u( J
起落架,
( X4 g7 H- s& z( i5 g2 [" O见Landing Gear7 R5 S& {& I+ @" ]7 S' w1 T
单元,4 X9 m2 k3 W$ I: O8 D. ?
某一类型或某一部件。
+ h2 M. n! Q$ k5 a6 N上位锁,
9 v/ i# D/ W8 H+ o2 e/ ?' P2 h起落架上,用以将起落架保持在轮舱内收上位置的机. i( w1 [1 j8 Q/ E7 U
构。$ D; |3 n# l1 I7 X: m$ f! M
英汉对照民用航空词典B OEING
* z1 T, z& D9 w$ ?' lTECHNICAL DICTIONARY 1647 E" I( L$ [, }6 D4 Y F
UPSET HEAD, The head produced on the tail of a rivet/ S" J& g, R! w8 v# `) H3 g! D
during the installation driving process. (See
% u, o- Z4 Y$ E+ S5 L& e% MManufactured Head.)
3 o4 [! u) r% g4 ~* a1 (TAKEOFF DECISION SPEED), Is the maximum
/ V9 W' E& F0 C4 ~ v3 [7 Npeed at which the rejected takeoff maneuver can be
0 [$ v8 ^% C! e* ritiated and the airplane stopped within the remaining: b& j. S% o; }) D" P; C
eld length under the conditions and procedures defined
z. j) L) O3 F8 \6 \ Jthe FAR's. It is the latest point in the takeoff roll where
* Z7 X: e2 c7 ~, h# i/ J4 @7 |stop can be initiated.
6 I7 C. K! h Y: |: \+ Kssure
+ a" J4 K" ~- ?7 [dient capability and maneuver margin.( N" q1 p: U* K( v( M
VACUUM, A negative pressure or pressure below
6 G6 Z9 |2 t) o/ F5 B* R2 F) Zatmospheric, measured in inches or millimeters of$ q/ G3 w9 a& Y
ercury.
; Y8 f/ E9 d% O+ d) w. Z4 i: ^is# l/ [5 D8 o _
VENT, A small hole orifice or restrictor in a component$ z# b* Z* j1 {8 @3 E7 q4 |
for allowing pressure in the component to be the same
* e5 p$ \( }, t1 X% J! {: ?as ambient pressure.
" Q* }. [5 ~( `" ?! Q1 }, \在铆钉铆接过程中,铆钉尾部一端形成的凸头(见
) F. |/ D- K% U9 U' o* t* ?8 |Manufactured Head
: X9 C7 _. g, x% E3 W6 {( IV: f7 B! F) z$ n7 g0 Q* t
V
* P0 @5 L3 I; N6 ms6 B4 [8 i$ _+ c6 l
in2 j& B8 b) l9 R/ X3 I1 }: B5 \2 X
fi4 P$ j1 h5 {$ P# n0 p
in
( F+ k" {) M9 r+ U7 Ea# V/ j, }" \7 |4 \
V2 (TAKEOFF SAFETY SPEED), The speed flown after) n9 v3 y# x1 r1 r0 h3 @
takeoff during engine-out climbout maneuvers to a L4 M7 w* f7 ^) f. H1 l
adequate gra! |0 ?& z8 l6 ~" u
m& a+ N d0 r0 u1 M( s
VAPORIZE, The mechanical process in which a liquid8 T5 b, M$ i0 L* d3 X0 \
changed into a vapor.0 x7 ?8 F/ c4 e5 W* f
VECTOR, A heading issued to an aircraft to provide
4 e) ?4 _$ Z3 l& N) ^navigational guidance by radar.5 z" W& O1 F' Q- e; g
铆钉镦头," Z" a" P; v3 z: J% q7 J, x) i- m3 K0 ~
)。
' _& Y6 t6 `' u: B- k+ H8 G1(起飞决断速度),
& u6 c% K U6 ?5 b' w根据联邦适航条例的规则和程序,飞机能进行中断起飞
2 Y7 l- y/ v8 X在剩余场长内停止的最大速度。它是在起飞滑跑时仍可9 K- b6 S1 q. u
住飞机的最后决策点。3 x& }" ~& q5 p) H
速度),1 L# ]! R+ T5 r, n* @
在一发不工作起飞后的爬升中为保证足够的梯度能力
: ~9 _. K( A" ?% H" J/ t! v和操纵裕度所飞的速度。
7 ]; n0 T- l! E6 n3 J若干寸(或若干毫米)3 L; m5 ]% x( D' F; a
汞柱。- D# Y0 Q7 [, @. k [# k* O
蒸发,
[9 ~" d2 |5 O+ h: C1 o液体汽化的物理变化过程。
0 @2 h) j: M# F# L4 |引导,9 U5 A) x% i% c8 H
由雷达提供的航向,以给予飞机导航引导。0 ~8 s: i) c/ k1 {
通气装置,
9 c x& V9 |. o5 d! z" E' f部件内,用以使部件内的压力与周围环境压力相同的小
; f: g0 `& s) G; x% T孔、或限流器。9 R5 G: F0 A7 R# }, q, C
V! ^ a4 g( o b L0 p" ]" {
且
0 ~' i% P: @7 m. }4 ]0 W停8 o) ~5 s, ^% X
V2(起飞安全5 Z/ v) B& o. W, w4 \& ~$ U. H- B
真空,: Y( g8 }& O0 H3 ?3 H! G6 c6 R
负压或比大气压力低的压力。常用
7 C+ d3 M8 `. C! [2 J英汉对照民用航空词典B OEING1 @% K p. \0 h, g/ z% d
TECHNICAL DICTIONARY 165
6 P4 u7 {' r! c$ A7 R! UVENT SCOOP, An air inlet/outlet on the bottom skin of7 F) f7 j4 o% N
ir- K/ h! z* m3 ]
VENTURI, A part of pneumatic duct with reduced flow
7 g w% P/ R4 e6 g nrea for airflow measurement. (Principle: As air velocity; Z6 d7 ?( n) j. c, f, M9 W
creases, pressure decreases).- _$ ?8 O, H% X0 i" J; h' L
ERTICAL AXIS, A vertical axis passing through the
( x% f c' W% x& @+ H7 D6 \3 k) vairplane from top to bottom. Airplane left and right& y/ H5 }: R' b7 _ b# q i7 |
trolled by the rudder.6 w( Z' [1 g& c3 c: z7 Y4 t/ W
VERTICAL NAVIGATION, Functions which provide
* [$ }& f9 k/ ~3 q) s- |guidance signals to control the aircraft during climb or" P0 C) u. ~$ D" Z
descent.( X% w5 |. P# V
.
' ~" J+ D* f/ w; z, y' J% ^通气进气口,
6 f8 K3 W, v8 Z% I位于机翼下表面蒙皮上,用以燃油箱通气和提供燃油箱
8 X H3 g( r! D: f内正气压的空气进出口。0 s7 d b- {0 Z( i% |" y
文氏管,
7 `! V4 \* v z! H* r+ Z w气源导管上,导管截面变小以量取空气流量的那一部! F# P) Q' r# H; D
份。(原理,导管截面变小时,流速增高,压力降低。)! Z: A6 L7 T' G8 h) C6 j; h1 t
垂直轴,
& g, T% G' S8 W5 F8 u4 Q由飞机上部至底部的垂直轴。用以操纵方向舵,使飞
% V1 Y2 N+ k S/ F3 `1 W5 `右运动。
& h* r. [" W: ~& M+ H* E1 U直导航,
, u) h2 q; v7 X4 \" J. c# g9 F,
9 k& {' c+ F& H2 Y. ~: t Mthe wing for fuel tank venting and supplying positive a
) Z- U: y' o, I) v ]pressure inside the fuel tank.
7 j1 B% D/ q* k6 a4 [* J0 d& G& Za1 h; A/ S4 X8 P8 `" h4 `: v$ a! L. b' ]
in
1 G0 f/ G( J- H* gV D5 H6 ` x5 ~# r- T
movement con
! Y% _8 m! r: t4 iVERTICAL SPEED, The rate of change of altitude
- e& B; M. d0 i* S7 L机沿此轴作左
/ s. G# U" y/ K& A1 T! [垂
. k3 _$ R6 q6 i5 d% v+ r; h( h在爬升或下降期间提供引导信号以控制飞机的功能。
, P6 I( ]- y3 G3 H/ y垂直速度
; C. V1 L3 p5 k6 v- N9 w2 w飞行高度改变的速率。" @+ b7 `( n9 C1 `$ u7 _3 V7 i0 f. t5 d
英汉对照民用航空词典B) F* d9 a( I$ _* o+ C
VERY H- i5 z( o7 e# m& ]7 o5 [
OEING; O6 Q4 _: I! l* P' @5 {
TECHNICAL DICTIONARY 166: d( M ^/ N. J' Y) f3 X0 k, s
VERTICAL STABILIZER, A vertical surface of the
: G& u0 L6 x' I9 Z* ?8 kempennage for stability/control about the vertical axis.
+ ?; y. T8 _* k0 ]2 r+ w) j( xVERTICAL TRACK, A climb or descent profile.' g" r2 t. C7 G+ M4 p
IGH FREQUENCY, The frequency band
% L0 P! Q5 @0 H6 N1 nVHF OMNI-DIRECTIONAL RANGE, A navigational
) w+ w0 A* ]1 r- F2 g; isystem which tells the airplane's bearing from a VOR, W- A# R; L9 {/ B# u/ L' P8 \9 P$ @
round station and its deviation from a selected course
+ [& ~9 l& l3 ?6 u/from the station.
, `+ l3 q* M; p$ x, E' yISCOSITY, In a liquid - it is the resistance to flow.
- \8 } H6 L4 ?1 ]" O' |- c; t; EVMO, The maximum design airspeed at which the/ ~- \7 x& x( V( m3 ]
airplane may be operated.7 \9 w( @1 Y) n7 q! C% f, l0 }
在飞机尾部,用以保持飞机绕垂直轴的稳定性和控制
8 a8 |, Q1 h" d Y1 [6 k L的垂直面。/ W6 x, H1 I4 k5 f V, |0 ]
垂直航迹(VTK),; V6 `! o4 {; q
爬升或下降剖面。0 j& p9 n$ K; ?. \
甚高频,9 E6 M* \$ c: g7 D% F
30 MHZ至300 MHZ之间。between 30 and 300 MHz.
% |$ H/ w; B% k5 ^: bVHF, SEE - VERY HIGH FREQUENCY- V) H! V p' D: v. j9 K% z/ [
g
) ]9 n+ y9 V6 x/ H J) H7 U/ b |% |to
9 O' Q# R3 c& ?- B0 Y/ Q' Q: xV
4 N+ G/ t* k3 |% ]垂直安定面,: }2 s! T$ i; {, O7 C
频率带在
! [4 _7 W" j& O7 L, E: V0 Y( B/ Z甚高频," \* M9 G% x, [* B+ s
见Very High Frequency
: X$ p- [5 j5 f/ n甚高频全向信标,& T# c) u4 T" K( \
系统。该系统可提供飞机到VOR地面台的方
5 S! }4 D, Y8 L0 i6 S4 @位以及飞机的向/背台飞行的航道偏离。2 V# n: |9 W" K/ ?& [* Y, n. [4 z
粘性,! |' H2 u# i3 l$ \' F
液体中阻碍液体流动的阻力。
! m: W2 u r6 c7 v最大使用空速,
9 I$ f$ P) j) ~7 ]- m0 e飞机可使用的最大设计速度。! S4 H* C* Y* O
一种导航1 E! N8 y0 Z, v# [& o2 X
英汉对照民用航空词典B OEING, p5 |0 s$ w' H- q
TECHNICAL DICTIONARY 167
' M& c% r6 j* q/ P! X* LVNAV, SEE - VERTICAL NAVIGATION# k* F6 R* D1 `& R- z( Z3 ~
VOLATILE, The ability to vaporize readily.6 }$ e5 k% G! G" n" B4 ]4 x' V
LE MEMORY, In computers, a memory whose1 e& W/ @1 Z9 ]1 U7 Y) q% j
OR, SEE - VHF OMNI-DIRECTIONAL RANGE
6 I& v% p8 d' u$ ^3 N( ~5 p3 k+ kVORTAC, A combined VOR and TACAN station.
* h' `# I; p+ a/ eORTEX CONTROL DEVICE, A small airfoil on the# ~' r( u! z, h% k
acelle for improving airflow between nacelle and wing! ]0 V3 T- k5 ~/ k6 c
leading edge.8 L. s1 y$ |- W# t9 P) K5 t+ b o
VOLATI9 S! ~9 ^3 Q6 S
contents are lost when power is removed.1 }4 e8 e# L5 X8 U9 L
VOLT, The unit of measurement of electromotive force.
; ?; o$ U F& j pV& H% x' C/ a+ Q) i. R, y# j
V/ U# q6 N- e/ D* E9 Q
n: H- b7 E- r8 _) Z1 e% }
垂直导航,, {' y: |' R" `) N: \
见Vertical Navigation.; p- x9 o7 D- V& A7 g6 a R
易挥发的,
) u m; a: A* a随时可以蒸发的能力。, J5 U0 v3 i! H" [
易失存储器,% X$ R0 a, O& Y' q% Y
在计算机中,失去电源时存储内容便丢失的存储装置。 M+ c" `- |2 V9 n" {4 C4 l
伏特,
$ e! v9 N7 X- J3 M电压的一种计量单位。! E1 X1 F8 w4 K( \ o: d
甚高频全向信标,
. x4 ]- `) v! X8 Xtional Range
2 y0 N+ E9 E. W8 N- Y d5 g见VHF Omni-Direc ." v7 A9 D' [" z( W' `0 Q
VORTAC,
: v4 \( ~7 f# H4 Q4 w- d5 a兼具VOR(甚高频全向信标)和TACAN(战术空中导! Q5 \" F0 w) z, V, t/ E
航系统,或称“培康”)两种导航设备的导航台。) ~ p4 O: t/ d& L6 i1 h' j
涡流控制器,
2 Q" T+ k6 r, t. u发动机短舱上,用以改善短舱和机翼前缘之间的气流的
# _4 z f6 b! |3 Z3 V1 [小翼片。
: }4 j! }, w$ r- m0 }英汉对照民用航空词典B OEING# b# G0 r0 Y, u0 d6 U
TECHNICAL DICTIONARY 1681 m+ q! V! H1 f3 [! T2 f1 U
VORTEX GENERATOR, Small metal airfoils, located on
u0 {; F& J( C6 q+ _3 Zwings and fuselage for delaying separation of the air
' X# p' v) v' Pating local turbulence* J9 M5 G+ {; {& z! C
ortex).. s. x; G2 o5 D8 K: t/ r5 g
35/ E u: b. \, _" T
stall speed in the landing configuration.
0 H& Y9 M/ _7 o6 \: B; V# S7 k装在机翼和机身表面,以在气流中产生局部紊流(涡
5 y* N3 {0 f+ \+ X: M1 ^流),来推迟气流自表面分离的小金属片。; @$ P5 i$ V: t' J5 S
度),( {; e$ _0 I' r1 W0 q
在着陆形态时的失速速度的1.3倍。4 K r6 R5 p! ?4 X7 C; w: |
见Vertical Track
. }% J* J/ I+ J0 h# n; R( x- U4 @" uflowing over the surface by cre: Y) L" D+ t; F% x6 t& ` ^
(v% l. m, N. m+ L6 G3 b2 D
VR (ROTATION SPEED), The speed at which aircraft
0 Z& L1 j6 U+ F3 [! Xrotation begins in order to achieve a speed of V2 at
7 J( {% |! c0 m- p# J1 Pfeet above the runway.7 Z. S4 @7 B; ]% o2 ]& a
VREF The reference speed at the 50 foot height in a) k. d1 l! M( B) H2 {, \; d
normal landing. This speed is generally equal to 1.3
* C: \! X( L h% F5 B; C0 v, j4 {: [times the
% [+ z, Z8 D2 P- f1 pVTK, SEE - VERTICAL TRACK
6 T1 O( {$ c0 d6 a" ^/ r2 J涡流产生器,3 a. g) z {2 z" ]; }
VR(抬轮速
2 j( n$ H n( b# o* l6 c3 c在该速度下飞机抬轮开始以便在跑道上空35英尺时达" A3 L' W0 ~7 D5 a( i2 A- h g8 x
到V2速度。
; [- `! Z. K* z# z; k" aVREF,) F7 i+ L1 ]" Y6 Y; @# C
飞机正常着陆时,高度50英尺时的基准速度。通常是飞
0 Z7 n$ T9 I6 _7 ^" y5 Q$ m& w$ g5 b机 H- j; p" j/ ?+ d* e+ ?
垂直航迹,
. W; i6 v L$ _7 X8 i.2 B+ p: }3 g0 v! ~% k6 u! q. f& W2 r
英汉对照民用航空词典B OEING
0 L$ K! T8 f1 b0 d, L# K( ?$ _8 JTECHNICAL DICTIONARY 169
1 g4 d1 X+ D9 n4 ]! h0 [W6 w8 Y: p' S( r* J
WALKING BEAM, A mechanical component attached to6 c+ J0 d. x2 a3 u
the main landing gear and a hinged support which helps
- E, Z8 i8 c, [5 {% kthe actuator during retraction of the main gear.
) Q8 K! n( M) n: t2 f( uATER LINE, A horizontal reference plane along the5 e4 l% X) o) R
fuselage for vertical measurements of the airplane.; @% i9 k# Q- g" R0 L
WATER SEPARATOR, A component in the air! q5 }$ q* m: e
onditioning system for removing water from the air+ B+ S; p3 B8 o" Q; P+ y
动梁,
, w* E" J1 c. U2 X/ s; `1 l' e, O) \主起落架上,一端连在减震支柱上,另一端连在铰接支
2 A5 z k% c9 e4 T6 Y撑上,用以协助作动筒收主起落架的机械部件。2 T+ i& }1 ?" Q7 |% ~8 @
线,
% w. q/ S$ T4 w3 ?# r沿着机身展向,用以量取垂直方向的距离(或长度)的
1 T; {$ r4 I6 {! g5 c* V0 B4 j水平基准面。
/ U7 ` V; `& M! b$ V" n+ f水器,
2 L& T* s$ Z1 W* N0 k2 e空调系统内,用以在空气循环机的空气下游除去空气中
: O7 B% Q4 {+ p0 C+ hW+ a- j* G7 H; m- Q/ b$ z. N
c+ p8 l8 b8 o. _! i2 h$ [
downstream of the air cycle machine.
$ |6 |$ @. e- ^( \" Y& u! \水
: q; B* Q& @$ u除
2 [# d" |% ] z9 e z" |- [的水份的部件。
" v% ^, e( N+ G( J1 S9 q+ w英汉对照民用航空词典B OEING
% n0 x7 W& _2 V8 R8 a/ yTECHNICAL DICTIONARY 170
/ z- r/ s( ]9 |' TWATT, The basic unit of electrical power." x _6 O* {9 @/ v+ b1 m
WAYPOINT, A predetermined geographical position
; ]7 \* X* }0 _& }5 `* Wused to define a route. The waypoint is usually defined `# n' _" ?& z2 E3 Q6 f. _ T
in terms of latitude and longitude.
( @5 I; A9 j; B& ?/ T9 p* g- _WEB, The portion of a beam or channel that has been
1 c# _8 i7 t2 C! }) Vinstalled between the top and bottom flanges. Its prime
" {6 D) p8 v, x6 g; Q) z4 Z8 Mpurpose is to furnish strength.
0 }) {( \0 |, L* e8 JWHEEL SPIN UP, Rotational acceleration of the landing
1 E" m8 ?$ I) t; m# D' Hf the
6 }- M7 [) c' r; O0 {* Bnding gear (undercarriage) after retraction.
# ~ V r# `, G: P# ^; y) H% N: \6 b电功率的一个基本单位。0 N- X( W; u4 E4 \" m8 E6 n! H
位置。通常用经、纬度来表示。
g5 J2 @4 d0 ]$ L' V腹板,
5 `/ A5 v. H- y) ]梁的横截面。常见于上横梁与下横梁连接成工字形。主
4 ~* j) k) B' ]% V/ T4 J% X9 Y( h要作用是受力。! \; g) P9 l' c Y- Y) j' S
轮加速,1 u# H% n# M# i) s, T
飞机着陆接地时,起落架轮子的旋转加速度。
6 Z7 P, _8 `5 J$ A2 L2 ?) E2 C' \轮舱,8 c$ c" p+ Q3 P- i) j' x7 P
飞机的一部份,用以在起落架收起之后,收藏起落架的* p! B- y: W, N+ w
那一部份。6 Z( l1 U9 o9 z: P# C
gear wheels at landing touchdown.: e1 |/ i+ L5 y; ?, A- h$ i+ e
WHEEL WELL, A part of the airplane for storage o9 |6 b( |# l" _$ R8 B7 j
la
8 ~* Z k5 R. Y. M瓦特(瓦),
- R7 ~7 {8 L l8 z) |航路点,
, B( [% \& W% C1 v0 C5 e5 r0 k用于决定航线的预定地理
' j7 p/ b( a( A, S( D& ?3 ]2 a3 {机+ i* x( @( f: i4 h0 ]9 e
英汉对照民用航空词典B OEING
0 g% T" |1 R. x$ `8 O% [+ u( s" UTECHNICAL DICTIONARY 171
9 k6 p8 u6 K3 _WIND COMPONENT, The effective wind relative to the8 B0 k+ c& k4 }, } ^( r
horizontal axes of the airplane.
7 M& R- B5 m) |9 lWINDSHEAR, A change in wind speed and/or direction
4 p( a4 s0 P1 j' F4 `6 B/ o! v" ka short distance resulting in a tearing or shearing# L$ |+ a" n; } s, Q' U \1 e5 x- D
effect. It can exist in a horizontal or vertical direction and
1 z2 i. N% z6 H' \3 Koccasionally in both.# m! V5 f/ _' U7 A q. y" ~
WING CHORD PLANE, A reference plane from the tip2 |; h" r# y. [- I2 D
of the leading edge to the tip of the trailing edge of the0 E4 |: }. T" Y9 F& \. {
ing.
! p5 u) c: ^) G4 r" XING GEAR, The landing gear attached to the wing C' q2 w8 ?2 w2 a- M# H: N
tructure.
* L0 i `' N1 JING ROOT, Part of the wing which is attached to the
) f4 o1 x# w6 gselage.4 M3 G3 k! h! @4 d) G4 S
WORD, In a digital computer, a word is a group of bits
2 r+ ^9 E# o) u8 _with a specified length. The typical digital word is eight) \5 u3 E7 _: \9 y/ J' H) p
bits long./ {2 c) A4 }8 b* S- Y6 C
风向量,, X7 v8 s/ @' c' e. |
相对于飞机水平轴的有效风。, E$ q8 e( R+ y8 _; F: h
风切变,8 J6 L- {9 _3 _& k$ T! R* G
短距离内风力或风向的改变而形成的撕拉力和剪切力。$ A. W% c; [* V7 t$ H# U
可发生在水平方向或垂直方向,有时会在两个方向上同时
u4 z# K( U& K# g6 z W6 x出现。
; m) u6 o# X$ V- u翼弦平面,
6 O/ B( y! s4 X' ~通过机翼前缘顶端和后缘顶端的参考平面。) g" P5 W- r' v# X3 P% k, n
翼下起落架,
8 t; x- `& K/ X. w/ A接连到机翼结构上的起落架。
' k+ Q7 u+ v# L0 X; ^翼根,
, X& x" n {# S机翼上,与机身相接的部份。
" a! T" E9 `; o4 R7 p5 _. F* u字,
7 \6 ?2 y/ Q) m [在数字计算机中,一个字是由一定长度的一组字节所组
% M ^# O3 V6 a$ _成。一个典型的数字字,有8个字节。
" R' f" X* {, \3 gin
. U* X5 ]; X6 n1 G( g( Uw: `2 o0 t1 v# K, D2 i+ \8 v
W* \2 K; [9 v9 n% V* n
s$ W, b& @9 g# `1 f: B
W( h# G3 ?9 u' P6 j& F' U/ i4 ^6 {; x
fu& ?7 z! N$ F9 b! w \
英汉对照民用航空词典B OEING
. w1 t0 X+ F2 P9 f4 [$ kTECHNICAL DICTIONARY 1729 H! Z5 ]; d6 v! B a# H
WRAP AR
7 C7 K+ N1 k8 z" B" g* ^9 Q; e, vcomputer's
- C: d0 P& O6 U/ N3 J. k, fOUND, A BITE test comparing the! G0 j) [1 x1 k& ~+ ~
output signal with an internally stored value.6 e% }) n9 D5 ^6 \5 c/ A( ]
XTK, SEE - CROSS TRACK
/ O% r, Z6 a# JAW AXIS, A vertical axis passing through the airplane
+ h/ d4 N: `# |0 [4 X" V; ^) p; Zfrom top to bottom. Airplane left and right movement3 }7 H2 ^( W+ q# ^6 z4 v* D) I
controlled by the rudder. (See Vertical Axis).! p/ u( w4 x3 J. Y3 V
AW DAMPER, A system that is used to move the5 y2 D3 Y; ?1 L6 ~1 P7 J$ L$ G. H
dder a small amount to oppose airplane yaw. d9 p! Q6 Z- K! W1 e/ l
es \0 d9 e) \2 Y9 X3 V; u
回测,' t0 S: a4 E1 q8 e
自检系统对计算机的输出信号和内部的存储值进行比
+ i% m: K* R8 L! b6 G/ q$ [较测试。# o: N$ D' D! s% C& B0 J
交叉航迹,; q- C9 B9 I7 b; v% s/ s
见Cross Track8 F5 z2 Q3 A0 k
X4 j5 I- R& G' h8 U
.
4 y- l; @. @6 w6 r; g偏航轴,
' Z8 t! X- Y$ ?( Y, z: U; w( P' P6 U又称垂直轴。由飞机上部通向底部的垂直轴。飞机绕此
7 G; y0 c D, c+ V6 e! z轴运动即造成机头的左右运动,这种运动是由方向舵来操
! s0 W7 X! K4 ]纵的。0 `+ N. w$ x/ a
偏航阻尼器,
) u0 A; }: f* `6 `) e用来少量移动方向舵,以抵消飞机偏航的系统。7 P' _' F7 O+ E# t5 Z
飞机绕偏航轴运动的速率。
$ C: U4 V" F' g4 @1 K- [5 wY4 ~0 }" _3 Q3 ~8 |* g
Y; S. l! Z$ e* S' o
Y! _; t- b* \* u' p0 \! z! f
ru( u# e* R+ m1 R, k, M) v9 v2 t
YAW RATE, The rate at which the airplane mov; i) t: B' H1 D. L
around the vertical axis (left, right).4 W# i8 c8 g3 [5 d( o
偏航率,
* x( c4 e4 r; E$ M3 x英汉对照民用航空词典B OEING
5 b5 i+ x5 V2 S z0 e( _+ E$ hTECHNICAL DICTIONARY 173
" y: q' T& V1 s, l. r1 [Z5 C. v& |. n0 {
ENER DIODE, A special type of diode which, when
2 X7 c" q3 {% J" a1 [, qZERK FITTING, A device through which oil or grease is$ a, Q$ o3 ]; ?" {) l0 ?
upplied for lubrication of moving parts.
1 Q8 w1 r7 R& N# [+ LZFW, SEE - ZERO FUEL WEIGHT- N' O" c3 c: Z4 {) v( j+ j1 Y
ZERO FUEL WEIGHT, The maximum allowable weight4 S ]! \$ K. ?0 C3 j$ G
excluding usable fuel.
# Q+ @% v3 M! ?) }" ?7 r纳二极管,
. ?* C7 Q, C1 G) f* F又称稳压二极管,是一种电子装置。正常电流可通行无
- l5 d1 S- F: H阻,但反向电流则必须在电压达到预定值之后才能通过。
: e4 O( ^6 n+ T+ f9 w在飞机电器系统内做为调压器之用。反向偏压时,它有一$ B& c8 ?2 _/ z
个恒定的电压下降。0 G% |# O Z; g* H& F
ZERK接头,) G* V; O0 b- ^
ZERK公司出品,用以接收滑油或润滑脂,以润滑活
; ]( s, X* I' F2 r0 O7 y4 C0 L- w* ]* [动部件的装置。
! L7 @1 t. p+ n \5 C3 w7 x燃油重量,- x7 M: S* P" P
见Zero Fuel Weight
9 v) r/ W& a, mZ
# P4 K5 Q6 ^: W: P* Q8 r3 d# Rreverse biased, has a constant voltage drop. This
t; X1 q: l$ ]# a* ]- f: x# {& x9 }property makes zener diodes useful as voltage
% z5 E. I: R. [2 b" _) T: Y& Jregulators.4 s. t9 q, f% C5 X% z6 ]8 Y
s
4 c, Y0 B( N, o& ]齐, C5 I+ v: g" k8 b" P" n6 K( y
无3 {6 z$ u' @4 e
.
0 a+ y: n* [) W$ T* B无燃油重量,4 [+ w( h. B0 n4 E6 X, Z
扣除可用燃油重量之后的最大允许重量。 |
|