- 注册时间
- 2008-9-13
- 最后登录
- 1970-1-1
- 在线时间
- 0 小时
- 阅读权限
- 200
- 积分
- 0
- 帖子
- 24482
- 精华
- 4
- UID
- 9
  
|
airspace of defined dimensions within which Flight
4 t& f! S2 Q$ a; B1 K+ ~Information Service and Alerting Service are provided.
% ^/ e: n8 }- d2 QF
7 u: Q5 q" E* v, M" Hd
0 L. @: v* Q3 J HF
2 Z" T2 m1 E2 C2 |, Din9 L# `2 K, A4 V9 ]
a
) o; L# K; l% M# g4 {F z, {# [$ W* e: T ]
s
3 E! m" ^1 M, N8 }s
( A6 H4 T) {. ^& {飞行指引仪自动显示(FDS),
' Q$ x( }( g9 f* O5 {+ U! e当飞行指引仪的开关处于关断的位置时,自动显示的飞
?' a3 m6 Q& Q" L$ A行指令。
2 N) v! S) A/ h8 y1 c5 \飞航情报区(FIR,UIR),
7 O" h' V/ [" W* V6 C一个有飞行资料服务和警告服务的范围
; W# ]4 _7 D0 ~9 F9 ~% s* G度层。0 ^4 F& t- v( s# B: y
50表示
, B ~4 ~6 I3 x显示自动飞" o5 K L" w( o
英汉对照民用航空词典B OEING# f* J% P6 ~3 x; {8 m
TECHNICAL DICTIONARY 64
c' `6 B3 ~0 r7 uFLIGHT SPOILER, See Spoiler.5 E' w) k6 q% Q
LOAT SWITCH, An electrical switch which opens or
8 m. F+ a3 s5 r5 Oloses an electrical circuit depending on fluid quantity in5 W5 Y* \5 w1 w* C
e reservoir.3 M( Z7 D% V4 Z1 \
LIGHT TRAINING DEVICE: Any device having a full
# B; r1 L7 C6 [3 C' Jcale replace of instruments, flight deck area or an
Y4 y$ o" _2 D# `( E. Tnclosed airplane cockpit includes the equipment and
# C' ^$ U, G' f0 Z/ @# programs necessary to represent the airplane in ground
! E3 h' c1 |+ k9 ]) \& z! Snd flight conditions.6 O- k9 d# O' n8 w6 g
LOAT VALVE, A valve in a fluid reservoir which opens
' h+ X0 E* d, t) X& {9 ]5 H/ a3 `nd closes an inlet or outlet depending on fluid level.
& Z. a% u: b6 D2 g8 ~LOWMETER, An electrical transmitter for measuring$ K9 P5 ]) w: @1 R
the engine.# f! |1 n" |* Y! n- ^
LUORESCENT LIGHT, A light emitted by a gas filled1 ]0 k% K0 |1 C3 ]: p
飞行扰流板,
# U. X- r. }. |+ q% E见Spoiler.
4 O" s9 Q& j; s/ S浮子电门,
8 u% T% C# m4 T- ~+ I6 u6 D根据贮液箱内液体的量来接通或断开电路的一种电器) z/ S5 K2 j, m/ M0 X% \7 z
开关。
0 N( _ V4 j. P0 q9 g) V2 b飞行培训设备,9 g: {9 E9 D4 Y! \
仿仪表、驾驶舱区、或封闭驾驶舱的任何设施仿真装置。
q1 q; i7 F5 r( d( w0 s9 T" r包括可体现飞机地面和空中状态的设备和程序。( ]' ?3 N- W m2 i
浮子活门,3 u9 J6 ~9 F/ m9 W" |
装在贮液箱内,根据液面的高低来开启和关闭进口或出
% d* | g: @* e3 D6 J9 {口的活门。' `5 e8 z& h' D5 v2 p7 }/ y- H
流量表,
3 G3 b% A: Z/ ~3 I4 t* m6 k; s2 ~用来量度流向发动机的燃油流率的电传感器。
7 o: S$ P' b: q: J萤光,; X* r- o2 G; R# k8 p2 ^* c
由一种特制的充气管所发出的光。% f* r. ~* ~) Q# Q0 p
F
) p2 Y/ _, s+ ]; n! w5 j3 ^- qc3 R$ z5 i* q5 {" {* s/ B
th
1 H( X2 G, s, I V3 T9 N/ IF& b. l" G; Y* U$ @* G; B8 A" W4 E
s
8 | s# j( ?, u# M2 `" ae
5 L; l' l" B3 W; ~! ^p
5 w( V/ T1 I% }$ |( Ea0 w# n1 B5 \2 I. }: m! W p. h. H- C
F
! }+ \3 T* i; p' m' i+ qa
9 _2 W2 Y+ S" A, @7 i |$ hF- E! N! h4 l# d/ y/ ] v
the fuel flow to) f1 d# {8 }! w: x
F! u6 c7 i! c/ i
tube.
% @) l" s9 i: {' X0 u* a' y: j6 H6 t$ N英汉对照民用航空词典B OEING k. W( D; d( o# L1 ^9 u2 H8 |
TECHNICAL DICTIONARY 656 ~8 {$ s, Q- ]
FMC, SEE - FLIGHT MANAGEMENT COMPUTER
, z# C. {+ I$ X% i; k" UFOD, SEE - FOREIGN OBJECT DAMAGE( |( |& H2 |& j7 z: d
ORCE BALANCE VALVE, A valve controlled by the
7 g- b3 _, L. C( x- l- X5 rOREIGN, Offside; opposite side.
7 e, [3 X, h4 k# q' t B5 g# g# YOREIGN OBJECT DAMAGE, Internal engine damage
# t! L+ @% h* Q5 R1 E' B& Eue to objects entering the engine air inlet.$ D/ k0 |! s7 _% K
RM, SEE - FAULT REPORTING MANUAL, w _& e8 J* p" }4 Z
UEL CONSERVATION, The activity of planning flight+ Q) l" d- M0 }# S; P! Z$ i( p/ T
ltitudes and cruise speeds so as to minimize fuel
8 d) f. Q( T# r& _onsumption.. g8 B3 g. y" Y& H
UEL CONTROL UNIT (FCU), A component on the7 ]$ T S1 ?6 A n. @' c6 e
ngine for controlling fuel flow for starting and engine
) X/ O' f) a3 P9 W- J+ v, ] h! Y, p% iF b e/ {( P0 |4 @
feel computer in the elevator system for hydraulic
3 O9 ~" R5 A, Y' y3 o/ @pressure supply to the elevator actuator.2 m. [$ [% y8 {5 \: A5 y) w
F
0 E m) T# s' l/ x3 DF
. }' n, x; A4 F$ I9 K6 ~8 w. }' ud
0 m4 F% \ e# ]F; C0 o: ]9 S' v \' _5 e% [+ [) R
F- f6 U* ?( C- i5 @1 V$ M; Q% o! _
a
+ b" S5 Y% p# H {% kc
* H* w) M* }. j+ VF' k3 q+ ]( e; M
e7 S# B$ O3 | d8 w4 C! i/ l4 A) ~
operation.9 o# B/ q1 J8 ~: V9 t/ }
飞行管理计算机,
4 ?' Z- h5 Y2 G见Flight Management Computer.
, X: _" f- z8 b. O7 l+ _$ J, g0 o外来物损坏,
+ J$ z4 b# o- U4 Xeign Object Damage2 E) V; H. R' k: p( s/ T
见For .
4 e6 o6 W8 ]' C! v9 Q平衡活门,# ~1 h& A* Z' t7 f. l. m
内的感觉计算机控制的活门,用来向升降4 h/ w9 p0 o' w
外面的,, @% j* j1 j) I3 c) g; \7 @1 \
另一边的,对面的。
# l; `/ l# _! X9 c0 u外来物损坏,
$ F5 B6 q! N. U3 c! Z由进人发动机进气口的物体所引起的发动机内部。
+ `3 W9 @+ s: E& `( X: S故障报告手册,
/ i ~! Q$ R7 Y( A1 D/ W0 o+ C( D' J0 r见Fault Reporting Manual4 o, |$ w. v7 @- y
力- a: V: c3 \- ~& ?3 R$ Q _9 O
由升降舵系统
; Y7 D P8 |: C舵舵机提供液压力。5 T. K: V% P" z1 |6 W' o% s
损坏! p- x7 r3 Y* Z
.) z" z2 F$ |5 _
约燃油,
& n, V1 n( T& Y V# ?& V为使燃油消耗最少而对飞行高度和巡航速度的计划。; U0 G4 }7 R8 F2 j' r
油控制装置(FCU),
: P$ y/ x7 V2 ^) {% D/ u发动机上的一个部件。在发动机起动和运转时控制燃油
6 q( R& C+ B, V: m节
9 l7 x' _' c: w2 ? ?9 E& |& t( S燃
6 O# ^- D! Y8 Q8 y- Z, ?# j; |& a流量。
' @4 D% x$ d7 X# u/ U5 U英汉对照民用航空词典B OEING
+ d( p! \7 X3 \TECHNICAL DICTIONARY 66
+ T5 H4 G: \, X! e KFUEL FLOW, The rate at which an engine consumes
8 ]4 V( y+ ^% N, nUEL HEATER, A component on the engine for heating0 e- E- p. o- w* N" ?
UEL JETTISON SYSTEM, A method for reducing
. a( A7 O2 C, s' I- {e
4 Z$ ]! j- I7 GULL FLIGHT SIMULATION (FFS): A flight training
6 T$ y5 Q2 v8 e+ W. q; }evice that incorporates full visual and motion systems# y; y* J+ Z5 O- C7 w" E
nd specific model airplane.: S4 B9 |* @$ t, V+ J
ULL-WAVE RECTIFIER, An electronic circuit which4 F/ H6 l, z) S7 z2 d
hanges an alternating current signal into a pulsating
* z2 q( ]- W+ U' w7 Nirect current signal.
0 t; J& J& z! }/ r3 f1 Jor5 Q* @. T9 u% V# I/ z
AGE PRESSURE, Pressure measured in pounds per
0 _. N4 K8 I, N/ V8 N8 _GALVANIC CORROSION, A form of corrosion caused
8 w5 s0 r8 y* d* I$ w* E( @by the contact of dissimilar metals.$ p1 W1 z) I3 Z
油加温器,; H" k O9 a( {' v2 s2 C$ `2 t
热燃油以防止发动机燃油
7 N/ H0 `# S2 s% E7 ^, p( X& f* b急放燃油系统,6 j( n- x: q+ i9 w8 Y
中的燃油向外排放以减轻飞机重量的2 z: S- H. Y& r9 n$ B) I
动飞行模拟机(FFS),( z+ L" M3 b4 ` _3 B1 i( \
一种飞行训练器。它综合了完整的视景和运动系统,以
' _' h0 @* g7 k6 J, O( S# K具体的机型。
3 n) w, T v. d' n( v2 p3 |波整流器,- _, g1 u6 \& d
用来将交流电信号变成脉冲直流电信号的电路。
; `- c' {! n2 m4 j- \, {! Y, j' d压,5 E( Y( h, a; U1 s1 j5 g, D$ P
平方英寸若干磅(psig)磅/平方英寸的计 ~* h% I9 I9 O
电解腐蚀,
" u, X* p. X# c D S一种由于不同种金属的接触所产生的腐蚀。
3 [ K6 }7 ?$ I# D5 H/ U5 V7 Ufuel measured in units of weight per hour.
0 Z7 P% T: m$ ]) `/ a. r1 ]F+ n$ n6 ~0 D+ r
fuel to prevent icing conditions in the engine fuel) @* P5 a2 z( ?2 Z G! R$ N: ?
system.) \2 f4 Y1 p* D/ M
F
7 F$ i! b, U! Q, l/ T2 [" t' {9 aairplane weight by discharging fuel from the tanks to th
+ i# a6 w0 l6 M( U0 ~% j; m: X0 m0 @outside.4 ?6 g) [/ @4 O6 g+ Z; E# {% i
F
* Q# U) d' \2 i5 f6 B! Yd) v& m; u I. y1 P& k( o- w5 k
a! Q1 R( F7 }9 G( O
F
0 t+ u/ A+ H% P! C2 e* D4 F9 Ic$ a2 {; p1 T5 A* L! U
d
4 h: Q( N6 F) {' [) [5 TG) k% O3 @8 c- @
GAGE, A component for showing quantity, pressure,2 K* `) ^/ F+ W3 B5 e+ h
temperature by a pointer or numeric display.
3 Q* g: }& u( [8 jG
; ^6 p' [# k. N' w" b, asquare inch gauge (psig).- c2 h2 d! y0 c/ b
燃油流量,( _, M Q: L+ N+ s! k h9 V1 M
发动机消耗燃油的速率。以每小时单位重量衡量。
$ F8 g6 Q5 P' ^- B+ n' E; q- T3 {燃
+ J) R: o! U; D发动机上的一个部件,用于加
: u* w ?7 _2 [$ ]系统结冰。/ {$ M) x. x% h) ^# V9 f x
应
4 t0 L) \* b9 D$ Z( A& c一种通过将油箱
$ X) r# |& d& M* Z# w) h方法。- R( ^ e" q5 ^
全. U# x2 B0 Y- f! P- i7 a: I
及, l% |' f0 f1 J0 w" ]& m9 }
全; c- E: C& C* a# H
计量仪,
0 v/ X3 G6 ~( `由指针或数字显示出数量,压力或温度的部件。
8 U: X" F* I" D4 w$ L) D表9 J: ?# F9 C% c. V* [+ u
单位是(每( f1 w- R- R# D% }4 a
示压力。1 a2 h( ~3 E0 ?. N8 ]8 i0 |/ l2 {
英汉对照民用航空词典B OEING
# [7 k/ D; ]9 w x9 iTECHNICAL DICTIONARY 67$ m5 Q( b. d+ ^! ]
GASKET, A seal between two flat surfaces. m% d" e! Z& R4 l
be individually controlled for the amount
1 W- H9 K% E3 z! @3 ?7 e) Xnd direction of supply.% `+ Y; i, ?; e4 c) \; n
ATE (NO. 1), Airport location used for
& @& o3 Z( W0 h) i! D4 w, H, J4 Fading/unloading passengers.
( u6 @' z& m' h' G0 ?* `7 ^6 aATE (NO. 2), SEE - LOGIC GATE
- v" \5 h; m. O2 j0 X& ~ATE VALVE, An actuator operated, sliding device in a
1 O) E2 x+ r: T; Tuct for closing and opening the duct passage.
6 r3 D' W1 S+ n, @6 ]0 B' T' b9 G/ z间的密封物。
/ I1 S) t1 ~9 n( Z6 }调节供气口可控制空气的量和方向。
4 @- \4 Z" ~! U/ G' _; C+ R% U M登机门,% `6 e9 e6 Q: h& ]1 e
机场内用于乘客上下飞机的通道。
6 d: ~0 v% I9 A, P4 A' I, p6 K逻辑门,: J1 w( ]7 m/ M7 q3 n, x
见Logic Gate
6 i: v; Q6 d/ A7 Q' {- u; u `GASPER AIR, An individual air supply for each/ E; l- P" [5 C2 _* a0 K
passenger. The air outlets are in the Passenger Service8 o4 f& f/ q8 w/ C# h5 F2 z4 Q! {
Units and can7 t' B+ y! r8 Q) a% o% y
a: D4 {0 j8 { K( v3 u, j; P
G$ y! y! U7 T0 ]" E1 m
lo, V$ Q/ l+ O; K& P6 |1 V& r
G
9 u v9 r# z) o% l" uG
# ] ~- F1 X& x+ f! W* ad
+ [( Q( l! {2 B8 i$ B+ \! T密封垫,
* I0 L9 {0 O9 f f) G4 \两个平面之) Z) Q( @& @! e* e$ H4 P) @* ^
乘客用空气,
" p" W8 B8 K' T6 t2 d% p. C: w给每位乘客的单个空气供给。供气口装在乘客服务设备
" @7 K" U% m w& v& U7 L内,个别' {& i) x) U- M
.! A* k0 ]0 X# Q( Z" z5 P% y7 F
闸板活门,
+ g9 ~; K/ O D1 }) ], O管道中由作动筒操纵的滑动装置。用来关闭和打开管道
2 V( c/ @' h/ ]+ @9 ]% ]+ u6 Z通路。$ n1 ^- B2 y* n* m
英汉对照民用航空词典B OEING0 S) |7 [5 i: g
TECHNICAL DICTIONARY 68+ }# ]+ _9 D, W! t& C7 F; w9 {. c
GATEWAY, A functional unit which connects networks# _5 _0 j8 N+ \4 B8 V
r systems of different data formats.; ?0 {8 C* n) I
RS.
* B/ v- y' S- m- T7 GENERATOR, A mechanically driven device for1 \8 L9 w% s, |' M( s2 m. B
ENERATOR BREAKER(S) (GB), A device which will
8 W2 D& j a3 C, r& c: ^3 Stor from the
' M3 U! m9 K( m+ P: [& Electrical bus(es) it powers.
, R$ }3 y: k+ S6 t) Q( ~: h5 P6 ~ent with8 E6 W& z- c) F6 F
o rings pivoted on axes at right angles to each other
, V4 I* X( r3 q* I& G* V, @llowing movement in two directions used in the flap
4 ~5 U7 E: I5 i8 e/ j! Z" B( p5 k1 Extension and retraction system.) `& O, g( M0 e! k. @: U* Q
接在一起的功能
. o2 J' D) n E( T- I+ _, _4 t! ~% C件。
& q6 v, _: m4 ^o& m1 X% p* b( ^8 S, Z7 C1 V
GEAR DOORS, SEE LANDING GEAR DOO
8 R1 x E: n7 t2 MG% ^# [5 t6 W/ c+ W- a$ T
producing alternating current for airplane electrical
3 g+ ^* W" g2 A. H0 X9 nsystem., A! j% Y e' v/ S' ~
G8 y: Z! d/ r. \4 L0 I M9 G/ e
separate an electrical power genera8 c' a c8 S9 ]* o, o
e/ P z4 B" k: T v6 y0 j' f% b4 O
GIMBAL ASSEMBLY, A mechanical compon$ E" v: n% b/ l0 d
tw
; [( H6 N; t* [$ k6 c# e6 Ia, y; F8 _) I5 a: H$ E: l4 k2 d+ l
e2 c( w8 d! r6 \0 M
闸门,7 \" z+ N! I5 c3 [: ^5 h' y
一种将数据格式不同的网络或系统联2 S. Y- |" v, `7 ?+ H3 A( l% Y
元' `( `: P# W# K# k
起落架舱门,- }1 Q4 ^# x3 d9 G p8 r
见Landing Gear Doors.* ^& m' w5 ~; S q0 Z, p i
发电机,
; k7 w; l b# W& B0 f+ Y: `为飞机电器系统产生交流电的装置。5 e1 h# o4 o3 u+ _, p
电机跳开关(GB),9 p( E4 _- [6 t# i' P- C; J6 T
机与由它供电的汇流条断开的装置。7 G' ]" u( T9 E+ J
襟翼的伸出和收上系统内的具有两个圆环的机械部件。
. x# H& G$ g1 n* v; s" S/ B个圆环的旋转轴相互垂直,以使部件在两个方向都能转/ _7 v3 K5 A; Z" s+ D* H/ {, u9 _
。6 c s' x9 S; D5 C7 [" x o: F
由机械驱动,, E1 U4 k( I- H* L1 k! Y
发! F+ I$ P# L/ P( [, {
能将发电' |4 R$ I" F2 |/ s
万向架组件,
3 T6 G& B% ?: o \$ c两
8 P, s) K# c+ f动
! j8 f2 T: r& J英汉对照民用航空词典B OEING5 H& u% {/ Z- [
TECHNICAL DICTIONARY 69) p9 N3 y" g1 A1 q
GIRT BAR, A rod attached to the escape slide which
7 p& r4 X% N/ aengages brackets on the floor for automatic slide
c0 z7 f; M# k: j% n; tperation when the doors are opened.
3 ?- @2 ?8 M, C2 J/ @ K1 A8 P3 w8 HLOPE (GS), A vertical path defined by a
, t3 J4 e% G5 c9 Yased electronic signal used by an airplane or* x1 h& N+ F. a9 B, h
LIDE SLOPE/GLIDE PATH INTERCEPT ALTITUDE,
; B5 n6 k9 ~" g' o4 p, Ahe intersection of the: `7 g& Q6 p9 G% U, U: F& F
ublished intercept altitude with Terminal charts by the
* ]5 o/ x. H0 e3 i! |6 Ntart of the glide slope/path symbol, is the precision FAF;! }. L6 O' U# W: @2 X+ s
owever, when ATC directs a lower altitude, the+ k# D3 a. W" Z) s6 H8 l. _; O6 L
地
* D# t& R6 d8 I' |- n6 _- @: ~$ V上之锁钩相齿合,以便滑梯自动工作。
4 {& G: R2 u& f" K- N4 \# s# m滑道(GS),
6 G7 e& u5 i% p q由进近或着陆期间,飞机或飞行员使用的地面电子信号
/ E- d: K5 x5 J1 R垂直下滑航道。! o- c( ~( J N
滑道/下滑航径切人高度,2 }% k3 k! ]1 I3 \
进近时切人下滑道/下滑航径的最低高度。在8 K* E; H* e- Y5 F) O8 P+ d
最后进近定位点。但当空中交通管制指挥一个
0 k8 i; J3 T+ X2 y# h低的高度时,由此产生的较低切人位是最后进近定位
C# ~) f( P0 K3 K) K% H。
* L2 Y# D% w( R, s6 m; M }. }o: V) d* t* g3 o$ @2 G! C1 R
GLIDE S
% t% C" w) c" T1 H% E0 k2 Cground b6 ^$ l! }- w9 M q1 V5 g1 v, `
pilot during approach or landing.2 j5 A" e- V+ N' D+ K8 g I
G
2 _6 V+ A) N# v: X2 A" S+ QThe minimum altitude to intercept the glide slope/path6 i! {% U3 g$ q( U- z' s
on a precision approach. T/ {4 p& n' T; W8 O
p
* T* u& v! k0 g( Q! f8 hs
' V0 ]* |# ] x8 ah
( h: L. o m/ G, b+ bresultant lower intercept position is then the FAR.. A2 _5 D2 D2 x5 ^8 o
束缚杆,
0 ~3 e) x# J) `: x& o3 g' Z {5 a连在逃离滑梯上端的杆子。在机舱门打开时,与机舱* a( k, m. R3 q$ \; T! M1 Z% o
板- i* l1 K/ G1 K( O7 ?/ U
下
$ K6 V9 O) h. j) r* O确立的一条
% h. m# G3 b8 a" n4 n下+ M1 q9 S9 ^& w
在精密0 O- v8 k1 D% P! r, N7 k" i
Jeppesen机场图上公布的切人高度与下滑道头的交接3 g3 k0 Q! t4 X! H$ U# T
点。是精密/ f, Y4 Z! ]( U+ L
较/ g: D# a% E, o3 u/ S3 S1 K0 J" N* f
点
3 X# X) z- z+ |. K4 O- y英汉对照民用航空词典B OEING4 B3 L4 |( F& U. y
TECHNICAL DICTIONARY 70
) G3 R+ D G) B9 k1 O* F7 I0 c- K/ KGLOBAL POSITIONING SYSTEM (GPS) (No. 1), A
- `3 Z- c% }, c. X1 W! |pace-based radio positioning, navigation, and- ?2 Q) y7 ?( K% a/ U
metransfer system being developed by U.S.A.8 ]/ m+ m" u# P$ \
epartment of Defense. The system provides highly0 d: \: m2 n' C6 D: p# s( A
recise8 X5 F+ G( k* U5 w: y# Q5 u: @+ V
nd provides a worldwide/ F) ~; _9 Y7 v/ C/ K( w
ommon grid reference system. The GPS concept is
3 F/ K7 [1 h1 Dredicated upon accurate and continuous knowledge of
/ J1 `9 g- U; h' X* o6 B7 U2 ue spatial position of each satellite in the system with
+ ~9 L% _2 |) {: w6 c( fspect to time and distance from a transmitting satellite
3 F0 _; C, I' D: o4 ^the user. The GPS receiver automatically selects$ Q* V3 ?1 S6 O0 W2 b
ppropriate signals from the satellite in view and
8 y) Q4 n: @( ?9 a4 D9 ~anslates these into a three-dimensional position,) c0 K( l% `- Q8 ^0 o0 N
elocity, and time.+ Y& z- p; _* S, c; c. k9 h
LOBAL POSITIONING SYSTEM (GPS) (No. 2), A* [; |5 L G& w9 R; M) k
ngrange navigation system that takes navigation input/ B- l; T, P8 U+ [" F
om transmissions generated by a series of satellites in! f5 v) N4 H7 F9 _9 q' t
LOBAL NAVIGATION SATELLITE SYSTEMS (GNSS),
1 n4 B' c1 O8 H+ t: _ternational Civil
1 f* m2 o* D: z8 rviation Organization (ICAO) to encompass any
/ p, T% ?9 Z' ^# Z+ w* A4 Vdependent satellite navigation system used by a pilot
% i% e( x& O4 q% \; @perform onboard position determinations from the
+ j1 ] }9 H1 P- jO-AROUND (GA), Airplane maneuver where the pilot is
% X$ l" ^5 u5 }5 `: ]& Pin the final approach phase of flight and decides not to' z( M# C% e3 q3 ~
land. Thrust is applied and the landing gear retracted so3 }2 U$ r! m8 w J I
as to climb the airplane to a safe altitude.
$ x7 i* }1 j; h6 `GO-AROUND THRUST, Maximum engine thrust to be
8 y8 R/ ^! t) k- Q9 xused during the Go-Around Maneuver.% w/ g, V$ n7 e% k7 f
统(GPS)(NO.1),9 ?/ l2 L8 O5 T$ {
电定位,导航,和时间转移
5 O: g! d3 h$ j* i统。该系统在全球连接的基础上,给无数备有适当设备' {! I' Y3 N# e* s
户提供高度准确的位置、速度、和精密时间信息。该系7 Y( b" g% n. A# {9 a
响,并提供世界通用性座标系统。全球定
! l+ X: f$ V* ]信息之原4 G! ~+ m l9 M) T! m
为基础。全球定位系统自动从所见卫星选择合适信号,
" m/ k- O$ S& x6 A$ d并将这些信号转译成三维空间位置、速率、和时间。
( Z8 _3 y8 O9 x% S3 ^: k全球定位系统(GPS)(NO.),7 F1 s( K; x( _ S- e; x& N
一种使用一系列同步卫星所发射的信号作为导航输人% T0 f7 O ^* s( d, C. k7 |
长距离导航系统。
6 Y2 X! O! \8 u( ~球导航卫星系统(GNSS),8 x' D, P- w; t6 U
航组织采用的“伞形”术语。它包括飞行员+ h; C. j) g j# }
料做位置判断而使用的任何独立卫0 J8 n F) Z. [) ]- f* j
导航系统。. A. h7 ` S" x. i6 g
复飞(GA),0 r. g$ Z1 z1 y% I
飞行员在最后进近阶段,决定不落地而做的机动动作。
. z" a W' H) }9 \复飞时需加油门,收起落架,以使飞机爬升至安全高度。
3 j+ U, {8 M# x: i- V! q复飞推力,) c& }% N4 f: k# {. _
飞机复飞期间使用的最大发动机推力。
1 j, A4 g; t9 P* }! hs
- n/ R3 V( a5 Bti
* x2 a5 p. i, Q% E1 t( ^0 ID. j+ `! M/ d- k
accurate position and velocity information, and p
# @' T' n2 ?2 Y/ Ktime, on a continuous global basis, to an unlimited0 S5 t$ v5 k* Y/ `& b, `
number of properly equipped users. The system is' c4 k& l6 Q" i: Z. B- v& _
unaffected by weather, a! a* Y0 d( l7 n; r; M" y
c
' T5 o( t$ k" J" @p: k: d$ O2 A- W: Q+ v8 @2 L
th
( c& v8 ^9 f7 m" h# Hre0 l4 B. {7 A' X( ?; n( B
to
" T! E4 c5 d5 {* K; ia
0 G4 D% J' V4 }" u P% j6 d( D2 Qtr
; e) V6 I& l6 L" m: s- {v
8 c8 W* {) j. _G
$ o5 }5 Z7 p+ dlo
; |- o0 N( j" e8 t7 S& Y1 l. v2 lfr& k+ P: j0 J* W3 |
synchronous orbit.( x; ~5 v( D+ ~0 F x |7 \$ I
G
; E% N+ b* {0 {4 x* OAn "umbrella" term adopted by the In
0 ]6 D% a3 p2 e4 Q; Q; D0 AA& C6 \" s1 p* N$ G* r
in: o. [2 P( l7 \) M
to
+ C8 I- J+ s9 gsatellite data.7 u/ j# ?! Z( ? r; g% S
全球定位系. n) f' o- Z3 Q
由美国国防部研制的空间无线8 |4 u* E. L* p" ~8 ]" `4 h" X) {
系: Z- |5 l1 t0 N2 T( x
用
2 j; n+ a* {1 q统不受天气的影% h4 m: ^8 Z* [0 I: O
位系统概念以系统中每个卫星具备相对于发射卫星与用
5 y/ _+ m2 `* n* m; w* I' M7 h户之间的时间和距离的准确且连续的空间位置
: L+ h* G& a1 x( |6 C" w则
H [* r7 Z3 G6 e8 C, c, F2
3 \/ z* k. j3 d2 j4 \: c的
) l% a4 l5 a o全
6 |7 k4 T' u W是国际民' g' C+ S1 f9 S/ z( c U' _
在飞行中根据卫星资$ w: X. T. y$ i6 i: M
星$ N8 J, i1 R7 x# \' p+ y
英汉对照民用航空词典B OEING: _1 }) [2 F+ B) t
TECHNICAL DICTIONARY 71+ G& x' q8 d: b7 G2 y) {! V! n
GRADIENT, The ratio of height gained or lost in a given
, b: L D4 L2 b( }8 P* zdistance to the distance travelled.6 s0 N6 V! {! ` S/ g
rbon/ Y9 r% E2 Q( i2 K P4 \* `
r access panels, landing gear doors and flight( M+ V0 d0 T- ^6 ~' F# S
ontrols.
1 @# b; k2 T( K$ d1 F% D( ~IRCLE ROUTE, Is the shortest distance4 D" R0 A6 z# `1 `6 n
etween two points on the earth's surface. It is the line
; w2 e, ]: x1 s+ @rmed by the surface of the earth on a plane that5 S7 i+ e- H p+ c4 Z9 p
asses thru the center of the earth, the departure point,( `( x, A( @7 t' f* [1 |2 [
t line
. O' G7 @5 L U8 lal Conic Projection
/ m2 o: U ?* H- @ z0 t, Wpproximates a great circle route./ w$ U( u" Z$ ] p
GROSS WEIGHT (GW), Total weight of the entire
2 M1 J7 ]; C( j; W7 Z ^airplane, fuel, oil, cargo, passenger, etc.
8 @3 n* t {% G% Q; b [. nGROUND, A part of an electrical circuit or system that
4 J y, g1 D' uhas zero voltage.: g; }# R+ C" T: {2 Z
GROUND FAULT (NO. 1), System fault that has. X" \& ?, ^, _8 G! s) O4 _: p
occurred since airplane landing.( h9 |1 k$ b& q4 w+ m" Y
轻的材料。用以制造舱口
/ `0 @7 p Y6 x4 p$ ^,起落架舱门和飞行操纵面。
- _$ W$ C9 s5 s+ p. U0 a8 T圆弧航线,1 h- B7 F% m( ]+ J" E Y2 @
地球表面两点之间的最短距离是以地球中心为圆心,在
/ B6 B @* V" |" I' E飞点和着陆点间所形成的弧线。由大圆弧航线形成的真
/ Z6 Y$ t# e; Q. y; M' d+ F" X迹不断改变。在兰伯特等角曲线投影上画的直线接近大
Q4 U6 C( o$ j% c全重(GW),0 l; i6 Y3 @( z# y0 X5 n. I
整架飞机的重量。包括飞机,燃油,滑油,货物,和乘3 R% g7 j0 c5 [) D8 g
客等等在内。
. O' K$ }; n0 U }% C4 d地线,
* \6 i; D, S) h, l在电路或电气系统中,具有零电压的部份。' O1 y H: t3 @5 k% r+ W- D
地面故障(NO.1),
4 Z! c& C' G, S8 C* |# e% e自飞机着陆后所发生的系统故障。
: C5 k! Q3 n; R8 WGRAPHITE, A strong, light material made from ca) c2 M+ n/ ?, Z: p2 w
fo
0 D% Q2 A- w6 mc# x3 Z- |- a& n6 f9 z; `
GREAT C q; C, ~3 y$ A- d/ H0 t
b
3 K5 V) C- E" q6 V4 ufo
C9 K. c6 F, v/ I% A( Zp* }9 a# E; Z D7 o
and the destination location. The true course formed by
|' l: t; m$ Y1 e. _! m1 l; Ea great circle route constantly changes. A straigh' o7 } W9 R4 X/ M( F
drawn on a Lambert Conform
) l$ q' N( B2 E" i6 xa$ W* B8 V! e* {3 m- ~* Q0 B
GROSS PERFORMANCE, Actual or measured
0 A( `! p% g5 S& g; h1 f+ Operformance of the airplane.
3 |9 P) |( c1 E" k7 }4 T梯度,2 `; [) v/ z! m# }0 J' s2 i9 j
在给定的距离内,获得或失去的高度与所经过的距离之
8 F3 |) K) s* y+ s' K+ o比。6 b( M2 _( C8 j2 u: h
石墨,
; t+ ^. R1 B9 A6 R# _- `! o一种由碳纤维所制成的强而
$ W3 T- q4 b: M4 O; R: p: h: H9 U ~盖) D3 \- s$ @ T9 q* h( N* X" }0 k
大, a& c4 i6 \, F; m3 u& Z/ p
起 v/ J* g/ j' s7 s
航( e! n8 ?1 D% _3 u# o: h/ E
圆弧航线。
( {; U f5 V5 {/ S6 e4 h4 ]总性能,* J; X G! j, D1 u8 m
飞机实际的或量得的性能。' E: l: B; F; l8 F6 c8 {
英汉对照民用航空词典B OEING
4 Y" g6 i0 Y W, P6 h' oTECHNICAL DICTIONARY 72
" E, @- p4 n- {! p+ Y0 rGROUND FAULT ( NO. 2), Loss of a ground connection
t; K2 b; i, `) gor a short-circuit to ground.
+ P; e+ w' a/ H/ i7 v0 Y# a' U! HGROUND SPEED (GS), The speed of an aircraft2 o' f" K, r5 W9 ?' c" `: g
lative to the surface of the earth.4 M7 M) X( ^8 }6 q2 L
ROUND SPOILER, SEE SPOILER
8 [. m$ a! c) V. O0 AROUND SUPPORT EQUIPMENT (GSE), Equipment
, t4 M# v! H! [6 used to service, test, move, power, or repair an airplane
, o; p: J. j2 `; c# p) D" W1 thile it is on the ground.
+ v0 j: y( E2 W5 ?ROUNDING POINT (TERMINAL), An electrical! j$ Y' C5 T" g) P
onnection on the landing gear doors for electrically* @1 ?6 i, y2 E$ J) E1 I
rounding the airplane. An electrical connection near% i. E; q# ~$ j6 s
e fueling station for electrically grounding the fueling
! w; A) G" r. R( X# R ?8 base.
& A0 `/ T- m! V+ s( v S; _S, SEE - GROUND SPEED
0 @* x" N0 d- v; k' \SE, SEE - GROUND SUPPORT EQUIPMENT
% g7 j z) \! u7 |% G( j4 b& [NO.2),! E7 W% I& K. h& Z7 ^, w
地速(GS),/ j$ s r/ w' ^) J; O8 B% e
飞机相对于地球表面的速度。
, C6 Q b) x9 r4 y% R4 ]# W地面扰流板,# K+ _8 E8 N; t
见Spoiler
" c0 A* \4 T( [re4 O9 n: `. T' q# G! A$ A9 q
G) t* u+ d9 b) e
G
- z; L0 l }" D6 A3 J% Su+ G% P6 r) `" A1 V
w! ]! X% U- m1 `5 X6 e& R: q
G
- @2 G0 {! L3 i0 J6 [c! r; L+ H% T/ G
g8 o9 @3 H/ T' f* A
th& u. Z& k1 O: B1 V: `, R: p. G5 H' i
b
! y' ~# J6 d0 Q1 y& x1 ]G4 C$ p8 u0 J5 ]7 {$ W! E' e3 a
G
, z( B# c0 f* R9 H9 BGUARDED SWITCH, A switch that is protected against
2 C3 G- c) H+ Y* Q8 g2 w2 | Xaccidental movement by having a cover installed
( _5 e) h* l" odirectly over it.' J V; V$ {9 a/ s
地线故障(
$ D- N- b0 M4 i8 Q; ]地线脱断或某线路因短路接地。
$ F; b: |) r3 u: O0 e n0 Q.
/ `, a2 A, Z% H( f5 _3 V地面保障设备(GSE),
# T6 ^/ c: K5 |* D当飞机在地面时,用于勤务,测试,搬移,动力,
) I1 }4 s2 u: ^# e, p/ g j或维修用的设备。
8 `1 G* d; q/ B6 {. P$ @接地点(接头),% M7 F1 v. B( z- l0 p
是在起落架舱门上的一个使飞机电接地的电接头是在: v/ u: w3 R' H+ Y& C% _' P% Z
加油口附近,使加油车或地下油库电接地的电接头。- Z+ p4 r( s% ]' D- Y
速(GS),
$ M- Y7 w3 V5 B. q+ X- Teed4 H6 n8 e. ^( I8 u# T6 @+ r
供应* {/ g& C1 Q) {( J4 U
。$ e O9 X0 v1 B
地/ T* L( r9 d K! G5 l2 N3 y+ v
见Ground Sp .7 O# a+ d0 n3 e
面保障设备(GSE),5 ~+ b: C# d- I& x
见Ground Support Equipment* m% {$ q6 i0 N* X' Y
地2 T* Q: H4 E1 L8 j* n0 J7 C
.
% l( W) [ Z0 [带保护罩的开关,
# {% Q. ? a0 Q ~- r8 z, c为防止意外拨动而直接装有罩盖的开关。0 o$ V* P. q+ V$ m% [; _/ b7 H
英汉对照民用航空词典B OEING
- f; v# A- B! fTECHNICAL DICTIONARY 73
2 \/ M- o8 Y; k* V+ ?% @GW, SEE - GROSS WEIGHT
$ m$ ^9 p1 w! A2 w/ d& Y- V6 C4 eH* D2 X% O$ T" \
HAIRLINE CRACK, A serious defect in structure; a6 Z+ C: [" ~: l, \
crack that shows as a very thin line.( B- j8 b3 ~" W! {" O
HARD-OVER, A maximum pitch or roll maneuver.
9 v4 i$ A& y$ T4 k0 l! IHDG HOLD, SEE - HEADING HOLD
0 v& f: v' @; B* ~EAD END, In a hydraulic actuator, reference to the
6 a2 f, E& w2 T: A1 r. \art on the piston side of the actuator.
- |9 L1 y3 g: a! {" i( OHDG SEL, SEE - HEADING SELECT- u- j7 r6 e, J' J4 k
H
1 t- ?7 A- C- Q& _p# P0 m0 m9 n4 b7 M. d7 o V( p) ]
HEADING, The direction an airplane is pointed
% @0 v" V# H0 r( e9 Mreferenced to true north or magnetic north.$ {. ^* N1 X% ~/ [5 S P
全重(GW),
# ^0 s1 Q: q& V6 x见Gross Weight.& W6 T# P: s* j5 H* F$ W* W
细缝裂纹,
) L/ o7 z* F5 L* F8 y* b) u结构内的严重缺陷;裂纹的外观是一条很细的线。" I0 U8 S) o2 t4 B8 n# j4 i' J8 O
急偏,* x. T* B( g7 K" e
最大俯仰或横侧操纵。! N9 D) Z+ i( i& u" ?9 V; C
向保持,3 Y+ \& A W4 l$ k% j- h/ r0 C# w
见Heading Hold
7 D, e* m& c# O8 ~ W% k8 H航
: Q( O- c4 N( H* N. A.
; L) W4 ^, H4 t" z* d& J) H2 e( P6 _航向选择;2 b3 s/ k9 B" D( g3 l
见Heading Select.3 f) I) B3 s$ S% V1 V- V7 u
顶端,
/ T$ A9 [- r; u2 r液压作动筒中与活塞相邻的。
9 f' d9 U0 [8 \; D6 g相对于真北或磁北的飞机指向。
2 y8 R7 T* J% p. c) e1 G2 X# }航向,5 J, Z3 `* q/ o' M% D i6 e
英汉对照民用航空词典B OEING
+ T0 k' k1 y* E6 v# X; Z( kTECHNICAL DICTIONARY 74
" j$ D7 D) y5 \1 P1 h0 P" ]8 hHEADING HOLD (HDG HOLD), A mode of the autopilot, m" Y: w- r% S5 g: y
irplane heading.( Q3 O. B. O: P! Y
t# M2 v* P$ C( w' g+ W1 G" _# |
e$ k1 N' u4 |, x7 [' e/ o$ e
om
8 t# F5 m2 @2 X9 Qg or
6 ?7 n1 w( D1 o3 G+ v J(HDG HOLD),/ q" @' J9 h* [8 ~
(HDG SEL),
4 z0 q1 O6 P' G# l3 L# W k1 t s8 }交换器,2 m# u/ I# l: }( Q- k, B# [! a
有很多通道的金属组件,气体在通道里流过时,一股气" M" `& X R/ L1 [7 a7 I- t
可被另一股气流冷却或加热。
1 o- w+ [& d5 k a4 bsystem that maintains the existing a, U7 T- `5 i1 o% {. x0 Y
HEADING SELECT (HDG SEL), A mode of the autopilo6 y' i* D2 T5 X% s
system where the pilot selects the desired airplan
5 \1 W# e4 i1 Uheading.
6 F# u1 y) {1 k7 C7 J& THEADWIND, Wind or component of wind coming fr
# D9 D5 u8 @4 F4 Lthe direction of airplane travel. P2 o/ m7 {% G* G
HEAT EXCHANGER, A metal component with many/ j6 ]* y# x) u2 u, S, ~
passages through which a fluid can flow for coolin
! o; l. |7 @! O' |2 [, cheating one by another.$ [9 D! U% Z3 R
航向保持7 \( C! \6 ?' l* l$ M( T% ?
自动驾驶系统保持现在航向的方式。
% c, m! X: G9 K航向选择# A5 k& K& a. [6 r) z5 \1 a
自动驾驶系统由飞行员选择航向的方式。
/ a' P! ?( v6 }0 |: O; ?" G, j顶风,
0 h* o& I$ m$ F3 X( r来自飞机前方的风或风的分量。0 Q' q: O9 \7 {/ j1 {' i# a1 C
热 a7 y$ Z' G+ ^2 F- L
流; B3 }9 H- |! j
英汉对照民用航空词典B OEING
" _& ~! _' ^- L' xTECHNICAL DICTIONARY 752 G4 S0 F$ N' q, l$ N, a: J) [: k
HEIGHT ABOVE AIRPORT (HAA), Is the parenthetical6 @; T+ o4 e* J# x3 D+ g+ N
figure following MDA which, when added to the airport
, ]$ l' f+ P7 \levation, will give the MDA in feet above mean sea; z1 _! ~7 j! {
vel. A HAA will follow a DA or DH only when there is
# i4 m; n2 i! W% P3 r/ zo touchdown zone, runway end, or threshold elevation' |8 ^% O7 O7 O# n% D3 b2 E* Z
), IS the7 P( J+ }# F3 ]7 J0 J, K
arenthetical figure following DH, DA or MDA which,
8 @$ s% o X' q4 B- u, k! Lhen added to the touchdown zone, runway end, or6 A9 |; J0 I9 R0 x6 ~
reshold elevation, will give the DH, DA or MDA in feet& x! o3 T3 N7 V/ {( _
cy of one million cycles per second.! g' K g! |: e# e! f
EXADECIMAL NUMBERING SYSTEM, A numbering
F6 _) b! a7 wystem with sixteen as the base. The system includes& h/ Q) E* x! X) F% p* M1 y* Y4 I
igits zero through nine, and letters A through F8 g2 H, p% _/ r
presenting the numbers ten through fifteen.
0 B( a: {! i% G: k1 z- n' qIGH FREQUENCY (HF), The frequency band between
* s, t+ Z3 R% D" p9 }! ?场标高相加后即是" q1 r7 X" v) c+ s$ V6 N. o& _
DA高于平均海平面的英尺数。只有当接地区跑道顶端或. t# T/ Q" J0 s3 ~% U
道头标高不可得时,机场上空高度才跟着决断高度(DA$ C l" V$ L, J' C# \' ^: M
DH).# ?2 @/ b3 g' G4 m; }
HAT),
' H. j5 R' F2 g% _最低下降高度后括号中的数值。它与接地
; k( x6 x4 D$ d、跑道顶端、或跑道头标高相加后即是决断高度(DA,
6 s' q3 ~ p9 o; g6 h: P8 c! X7 wH)或最低下降高度(MDA)高于平均海平面英尺数。 X# Z) r e V
的最低天气条件同时公布的。
* a, m4 @2 Q% a8 k: U* N率。. E) Y/ k. y' W6 d' |
一种以16为底数的编号系统。该系统包括由数字0至4 C$ h) t+ P$ l; N4 S; U$ @
,字母A至F代表10至15.
: L- J( q( c* [3 a. N; Q频(HF),0 |. f4 i! H, g- @# p8 A
赫之间。, l0 Y% Q- @ Q$ d5 V
e2 k& z9 [9 g2 k
le, P \- r: G) D3 a: K
n
" }/ B- Y- W* P6 k2 B+ qavailable.
, m9 T5 |. R3 U0 g( g6 tHEIGHT ABOVE TOUCHDOWN (HAT
) V, r. P# a4 C/ H8 C4 np
4 w9 {8 v% Z4 Z+ fw& `6 m5 I. H1 l2 d
th) y; Y4 R6 d. Q5 c
above mean sea level. HAT is published in conjunction
, P0 J$ A% O7 [. E6 i2 Uwith straight-in minimums.
3 J6 i3 { Y) @3 t- q9 `( _8 y2 c8 \; e y4 MHERTZ (Hz), The standard radio equivalent of5 m5 h6 d* K9 H6 v+ H" i1 Y2 s
frequency in cycles per second of an electromagnetic
~6 S! z2 M1 ~" g# R4 ^0 l2 d6 ]2 kwave. One Kilohertz (kHz) is a frequency of one
( m( ?3 J# L$ Q) |thousand cycles per second. One Megahertz (MHz) is a
. D5 B( h1 v2 ]) y% z. a6 ]! c5 sfrequen
1 ~7 k/ c6 h/ BH
g: z8 f' O- j) o, E1 k, vs
/ @8 h# B+ o2 b: p+ W( K6 }/ H! Md. U# l9 {: S3 d! S" w. ~
re% y2 H! H7 e% G8 ~) M0 A/ s
H
, |, B* E4 N: l3 and 30 MHz.7 O4 S: t: m! |
机场上空高度(HAA),3 j! Z9 I- ^1 H# m7 l5 K0 m4 J
是MDA后括号内的数值,它与机
2 A! Z$ s) T0 CM. _% o2 x1 V# x' U& `
跑. S2 ]5 @! d3 r* {4 U; P$ h) W
或
a: R- Q" x# X7 O2 B+ x4 T: K: A: w离接地点高度(
7 y6 c: f9 L0 l决断高度或1 e6 t2 j: @. x/ q, U' R
区4 A. N/ p8 Y% ]. g
D$ _7 U5 Z, f- U0 F8 F, ~3 @
接地高度是与直接进场着陆
' x7 E$ E4 z7 e- q赫兹(HZ),: }* c* f2 L" N/ c+ x
单位是周期/秒的电磁波频率的标准射电当量。一千赫" ~% t' B: }/ ^) g2 q: i) O
兹是每秒一千周期的频率。一兆赫是每秒一百万周期的: O, C* j$ |/ H: z0 T+ d3 Z9 z* A
频
) t, {% c. e, V# N( O3 t/ H十六进制编号系统,
6 `( C% z! C* ?5 g% W' B$ M9; K# V, [3 V0 {" L" f) h, t2 h( s3 _. I
高! `; D3 F) ^: \7 E) d- S
频率带在3至30兆
$ i' \3 ~2 i8 I3 L! j$ ?: y英汉对照民用航空词典B OEING, X- N/ n: W$ t. E; Q5 A
TECHNICAL DICTIONARY 767 \) F$ q8 w8 n! u: V' |; u
HIGH SPEED TAXIWAY/EXIT/TURNOFF (HST), A long
2 Y$ {0 s) g% W% N/ Ydius taxiway designed and provided with lighting or
1 [- |2 j/ t5 Z" g) marking to define the path of aircraft, traveling at high( e( Z& i! [0 y( Z' ?) ~6 {
p to 60 knots), from the runway center to a
( |) }) f, Z, t \$ k6 v5 z* tthe center of a taxiway. Also referred to as long
1 c- U4 ^) q+ \- ^. uit or turnoff taxiway. The high speed taxiway is
: Z, k+ ~4 b' X6 Jfter% Y# c3 ^- \, m( p1 O7 `8 O' m+ T
ancy time., r) v7 T+ i% g" [) j! b" `
r a" ]/ b* q( N; e/ K1 c% K2 t1 c
eavy component during removal and installation on the
j( q3 ]+ Y6 G2 \irplane.) o/ n5 c8 ^1 P5 s
OLDING, Airplane maneuver to keep the airplane from3 K- N8 V4 S4 f' S. `: @
rogressing along the intended route of flight.
' ^/ t8 }9 h& i% J ?0 |! ^OLDING PATTERN, The predetermined maneuver
8 w5 B* U- }" E0 R( F" e: T+ R }c control.7 W4 K& W1 H/ N4 Z8 o
OLD/HOLDING PROCEDURE, A predetermined
; {$ E- N3 J5 `4 |aneuver which keeps aircraft within a specified0 k+ z1 @8 l" `& x
irspace while awaiting further clearance from air traffic
. [$ d. B3 x1 f' U- Tontrol. Also used during ground operations to keep6 U9 a5 K& V7 d4 X$ O! P
ircraft within a specified area or at a specified point9 M& d( z* J- a. o- o1 G+ f6 b- p
hile awaiting further clearance from air traffic control. M% b6 i' a8 \7 V1 _
he standard holding time is one minute at or below5 B+ B1 B- L' N0 L3 A
4,000 feet or FL 140 and 1 1/2 minutes above. The' v9 z/ S P' i0 g6 b
eparation between 1 and 1 1/2 minutes is FL 200 in* R% W) f5 r' x7 z+ a
(HST),& a6 q1 a8 S3 s5 i% c
道。该滑行道有灯光和标志表明飞
, V1 x1 v, M7 w1 ~; [4 M从跑道中心到滑行道中心一点高速(可大到60海里)通
4 E/ V: E5 V/ S的路径。也被称为大半径出口或脱离道。高速滑行道的
) j# r( k! a- Q; F0 @: }+ C5 _计意图是加速飞机着陆后脱离跑道,从而减少跑道占用
! @! Z# A6 R6 k7 t& f6 |9 k3 }时间。, [5 F3 n8 {5 C1 ~0 d) _' ?5 n
安装过程中,用于放下或抬起
, ^4 h! ]* g0 q7 `4 ^6 ^动机或重部件的装置。0 T- }6 ^0 ]. p
待,4 B$ a1 ^) z `2 K( [6 G
使飞机不按预定航线继续飞行的机动动作。- M0 y3 y/ E3 a/ H2 M
待航线,; N6 u! L0 G3 K& ]5 q
处于指定空域内等待空中交通管制下一步调度8 p( b+ ~) E! @; w, d) [
等待程序,
! ~6 F) a6 ?' k! E/ P保持飞机在指定空域等待空中交通指挥的下一步许可
- X2 D4 q4 |. Y3 |2 ~3 v的预定机动动作。也用在地面操纵来保持飞机在指定的地, h/ ~. n: m9 g% ^
区内,或在指定点等待空中交通指挥的下一步许可。标准
1 f/ X+ }" w+ N; y/ _; R+ J/ E的等待时间是在14,000英尺或高度层40以下时1分钟,$ X5 ?1 \( c. x- _! H# Z3 J
以上为1分半钟。有些国家以飞行高度层200作1分钟和4 m: |! V3 i! }1 m1 ]
1分半钟的划分。
# U8 D# n7 Y8 nra* m3 M2 B, d# Q) j& @5 x8 q
m, z1 f% G7 [$ r# g
speed (u
/ b5 ~) v& v. `2 hpoint on
7 e' U: R, `& }+ \4 O( A; w& mradius ex, T( S, |7 `4 Z$ `# F; {( J
designed to expedite aircraft turning off the runway a
2 B' a* y$ }9 W1 elanding, thus reducing runway occup
1 W6 ], v& `* B- @HOIST, A device for lowering and lifting an engine o
5 Q9 z/ }5 r; Qh& m$ L' q% m& i: e
a% a- s# ^3 ^1 M& J8 d/ }2 G% S
H; U! ` ?; ]2 a5 |, B, W2 `* S) p5 Y
p& L& ?9 `& z$ Z5 v! }4 Q
H
' T2 P& x( r( T& i S, jwhich keeps aircraft within a specified air space while. g- T- s; _6 x1 c, e
awaiting further clearance from air traffi
, |% M9 u. g* W( X6 ^6 p# _H
1 g8 G0 t8 K2 q( um) u0 ^3 E7 u. H4 p
a, S" `* s& c$ T/ {
c- m: G0 A' ~8 [2 c$ o$ M
a* e3 u' @# M5 B8 t( I1 O
w
4 s1 |$ J* J: [5 ^6 k" H( nT
' w. X- `1 o, J" {0 {4 M3 V9 w; d1$ C/ D3 h- i" t W& J! v' T1 ]
s% |/ e# |& W/ L4 q5 [
some countries.
0 _- {5 M* s& ~8 M% n高速滑行道/出口1 U; V& l) S# ^4 E
是一条半径大的滑行8 C8 s$ L3 S6 J5 ?" [2 H* H8 T9 M
机1 b, G4 L0 a( \3 a! W. k1 j
过" V; J7 t2 W2 v, K1 ?: `
设$ i$ o7 X5 r& d5 G
的
* M1 {" p( q: {& S( V$ l9 r% ~吊车,
" E4 Q$ ~9 ~" e, u; k在发动机或重部件拆卸和+ C; o, Z: b4 j1 Q, h
发' a5 m6 C1 n4 }% t0 c- Z
等" h" j0 \2 k/ b8 Z6 t# Z5 w
等. |- m0 a8 i5 j: I& G+ d
使飞机% V$ [" k9 N: S
的预定机动动作。
" c- D' r, i+ ?4 f; i5 x3 S1" O# u- p2 j- t: M' K
英汉对照民用航空词典B OEING
5 S! N7 R3 S( u8 q& |, {6 WTECHNICAL DICTIONARY 77
# } B8 A8 u8 ^: Z& U# g7 V6 n/ JHOLDING FIX, A specified fix identifiable to a pilot by
2 C0 U/ T8 y5 [1 L5 U0 UNAVAIDs or visual reference to the ground used as a4 s, f( f3 D9 Y3 ^6 j$ X/ M
ference point in establishing and maintaining the8 @* E Z4 C+ d2 D' c& S' e
osition of an aircraft while holding.
; e8 `* O. @. o3 R j: j( ^! kOMB, A hexagonal material made of metal or
, ]& Y; W; {) n! M, W$ Comex for sandwich construction of panels.
. N1 f2 i7 c$ u. sHORIZONTAL STABILIZER, The moveable horizontal
z T2 u4 E6 @7 y3 y: B/ q& `surface of the empennage used for pitch trim.5 [; L% q: [" U) H1 X
HOT BATTERY BUS, A battery bus which is not7 Y: T' [. v* s8 i$ U
switched and is always energized from the airplane
' r: u1 l) t: p6 p( b% F/ Obattery.' r- ~" D( k7 q. a' y' p
使用的一个指定' q7 [ Z4 F+ [, A: ]
位点。飞行员可根据导航台或地面目机参考识别该定位
$ o0 @* h6 j, E3 W。4 q, p& f5 S8 \; U
窝,
; d( F! x# N9 U3 H% ]2 d" U一种用金属或Nomex制成的六角形材料,用以制造夹芯
" G1 Z4 ^7 S3 Q' I, J板。8 r8 c& ~2 d% C2 ^; G) h" l+ ]
水平安定面,- p" @; L9 P( h' F
飞机尾翼的可动水平面,用来控制俯仰配平。
; G/ }* Z9 A+ } ]4 j1 S2 ~热电瓶汇流条,, ]/ k1 j! @6 `0 B! e( `
无电门控制的电瓶汇流条,始终由飞机电瓶供电。
& g3 Y. J0 u l7 fre
* q2 R# y z4 ^p2 B2 k+ A! ]" j5 N8 ]6 e
HONEYC
' o0 q/ B5 j) u" X' i9 UN5 t8 @8 S5 U$ h5 S% o
等待定位点,2 z. w/ G, _$ K- y
等待过程中在建立并保持飞机位置时
5 ]) Z4 s% y7 U# V8 b& F! j定
7 b* T! J. O0 T# L) X; r8 `1 ?点% W4 x. H3 s7 A, u- o4 S+ Z
蜂% z3 o* Y3 N% y; C( S) K$ w! Q
面# f) g' t6 g: H1 ]! P. }
英汉对照民用航空词典B OEING4 N: T* m) \' h- |4 T& F3 e
TECHNICAL DICTIONARY 789 w. P- H* C- t2 L. ?9 g2 K/ C0 F
HUB CAP, An external covering to the axle of the main2 T2 o) c; S' k$ B/ }" r
landing gear wheels.+ c: O( a% R m7 U/ F# w
HYDRAULIC FUSE, A device in the hydraulic system
9 \# _1 @* C2 I/ Z1 Fr stopping fluid flow when a leakage occurs in a line8 w! v" x- ]" @8 T' V3 p
ownstream of the fuse.
9 y# O( T! s8 dS, SEE - INDICATED AIRSPEED
; N) |, g0 l! Q$ q8 ?1 \. V: LER PLUG), An electrical device for! Q% N0 b: P8 b) K
producing a spark in the combustion chamber.
; A; `( x( Y) B, ~6 I压保险,% ~( n6 e: B+ }) \ n( p7 K
液压系统内的一种装置。用于在保险的下游管线上发生
& M9 X/ o% y* b. W" J, M: U3 ?漏时,阻止液压油流动。& z7 a, H1 y+ f- L5 I) }1 w5 l) Q
示空速,
6 W7 b: W* N2 F0 V3 J1 h2 i4 p见Indicated Airspeed
. l5 ~/ R, t: \+ z8 }' afo; U) \3 P# K/ M
d
" p7 ^( {$ k2 y+ @I IA
' m0 J# L# ?! sIGNITER (IGNIT8 T& @6 t& k9 a( J% G [
轮榖帽,
. R& }7 |! z2 v5 o5 ?主起落架轮轴的外罩。
( W* k, ~$ T3 ~1 @ p g液7 s* F7 i. h8 k
泄
/ R" T' q& i0 K1 H6 T指
# ]! R! c/ {% Q% V, D/ x/ O) l( v% v" d.
8 @7 q; s g4 E3 t# Q" t在燃烧室内产生火花的电器。( Q% H9 \' Z; v" l. G# k+ X- C! ~
点火器(火花塞),1 f: l4 T" B" i2 R: g* ?1 s
英汉对照民用航空词典B OEING
; g) e' m* L3 s V! X# ~/ \+ tTECHNICAL DICTIONARY 79
! ]1 J( g" K9 ^0 wIGNITION EXCITER, An electrical component for9 k" ~: f) u$ f( N
supplying high voltage to the igniters for producing a
5 G! V; E: d1 ?- k4 d5 v. Z* gspark.
R9 N0 H% V0 e4 DIGNITION SYSTEM, A system for starting or continuing
+ }6 N! o& }5 m' Z- Tcombustion of the fuel-air mixture in the engine$ ]5 u9 D1 s7 g- Z, _$ \. I
combustion chamber.$ S E# @0 A/ }% [7 u
S, SEE - INSTRUMENT LANDING SYSTEM
( u# J$ ^% ?- ]PROVED CLIMB PERFORMANCE, The rotation and
! T- P3 I$ X0 @! Qlimbout speed increased above normal to increase
" Q+ u: y. n! x4 XDICATED AIRSPEED (IAS), The airspeed read
, ^0 D' k, h6 |3 x8 z火系统,
' \# `5 i+ k" e+ E) Q一个使油气混合物在发动机燃烧室内开始或继续燃烧
7 T' p' o4 j7 O4 W* R4 {6 w系统。7 g" ]. @; R# z8 t
表着陆系统,
: O* k- @4 c Z, }' K2 _trument Landing System
7 a. R% S; P2 _ W, PILLUMINATE, To turn on or to provide light.
0 t9 h# U, ~# bIL7 J1 s2 f* {) q. S: H) m
IM
( v' W$ O2 p+ z3 N7 ^c
9 q; O* {& b: C) w% `3 C* |" P h+ fairplane climb performance, especially if an engine, x r p4 N# E
quits.8 }6 x. C% I) R6 ^/ q& \2 n, @$ s; ^
IN* h! W# ]) J1 `
directly from the airspeed indicator without any
- Y1 b. Z' v! L' p2 z1 k; jcompensation.
; e" d+ ^. d' G' DINDICATOR, A component for showing quantity,% N$ Z7 z1 u9 U
pressure, temperature or position by a pointer or K: A- x. G7 R. J) X6 i: \
numerical display. (Similar to gage (gauge)).
. H+ Z" @9 S& |$ x点火激励器,
! R9 ~' P; ~( H( u5 H6 S4 M& k) V向点火器提供高电压使之产生火花的电子部件。, |* i" V' E G( E, ?* P
点
0 k6 P8 Q& f5 ]% I. J5 g4 m% E' @' P的( F8 b; \2 n3 P
照明,
- h9 k/ N2 h0 J打开或提供灯光。. V3 P" _' |% {! H
仪0 j$ y/ A3 k: d7 _ N; B
见Ins .
2 _' O2 O& y- e1 ?进爬升性能,
! u& q! K4 Z2 n5 z6 `用大于正常的抬轮和爬升速度,来改善飞机的爬升性8 n, Y1 R2 t# K+ r) r2 g
一台发动机不工作时。
6 C; _+ ^6 S$ h) G9 s示空速(IAS),
6 v% F v) ~1 Z* k正直接从空速表上读出的空速。
& l% S' G- @* B/ a. W+ d& Q$ n% D6 C指示数量,压力,温度或位置的部件(与: l7 S5 A) ?0 D6 r" l. X- Q3 s
计量仪类似)。+ w% E( l. G4 G( Z
改
; y n% i% A9 c* ?. P( x- b能,尤其是在
: P) D8 x% r2 |指# ?/ f! }4 l- s! V1 n. ]$ x
未经任何校+ W2 ~) k% }" W+ m8 T& z! y; A, |
指示器,
# E; I V9 ]8 [, v7 v用指针或数字来
5 @' ~& `7 o F+ i9 a3 n N, L, ~英汉对照民用航空词典B OEING: s9 H% t2 R; z( ]+ m7 R. Y
TECHNICAL DICTIONARY 803 d8 ~& B& A x ~0 h
INERTIAL REFERENCE SYSTEM, A self-contained,6 Y1 E5 r$ W' e; u( G* ?
navigational system based on the measurement of/ k ^& N! T# M0 v- t
acceleration and attitude.7 a: t! p" F" z! p; G% @& U
INFLIGHT PERFORMANCE, The performance of the e2 q! j8 S$ i
ITIAL APPROACH FIX (IAF), The fix which identifies' K7 |* T9 l+ _! A
e beginning of the approach to an airport.
( {2 V& x# `$ H& nLET GUIDE VANES, A fixed set of blades in front of/ a. G7 f, p1 ]6 Q% Y/ _4 N
n engine compressor for directing airflow to the' A* r9 S9 l! j8 l! }* a
ompressor.3 |2 i( M8 [7 C3 e3 ]
NER LOOP CONTROL, For autopilot operation this is* w' _1 A- v1 Q; Q! f
e basis control of airplane pitch and roll attitude
6 @. h6 {. u: a中性能,
: i& r5 @1 }$ l5 h: ~/ M. u飞机的性能。. v" e* W |9 W! m. _3 V
起始进近定位点(IAF),
n4 w& g; q4 S标志向着陆机场进近开始的定位点。
& ^& a) K6 P0 O" L, R8 Y$ a进口导向叶片,' N% G, k5 {9 C7 p
发动机压气机前的一组固定叶片,用以引导气流进人压
& Q& T$ s' \) v( W气机。) O5 x$ p6 U) I1 D8 |/ c
环路控制,0 ], F+ C( c2 v
对于自动驾驶仪操作,这是无关飞行航道的飞机俯仰姿+ y2 Q- Z. q- i2 X0 }+ o* h
制。
6 i, ^2 }1 ]( b& [" T$ h8 x) zaircraft while enroute.* z% t4 J6 x2 g& z2 W' P
IN
( u/ N+ d9 i# K* _) [+ |$ f; F0 }th
: D3 j0 {* J: Y: g' D* AIN
. H( R, d% a; w, ^: sa, j- m5 ^/ J/ j7 l" w* `4 Z- m
c
2 H3 |2 U2 z+ X0 IIN
2 Z9 n7 A: z J! wth
) E7 S4 M2 p. r, i ewithout regard to flight path.
~8 {5 {& h1 r惯性基准系统,* U8 f% S3 w: a B% |
以测量飞机的加速和姿态为基础的独立导航系统。
% b3 ]' s4 o2 I) K' N空( K1 ^. n$ \' l8 ^- P" u
飞行中& A4 [' r0 _' g7 M c, {# l! B+ _
内+ C* x& l! @" D2 M1 {
态和坡度的基本控6 u. Q) k4 K+ J# ]
英汉对照民用航空词典B OEING
" h. N# G5 E; H0 pTECHNICAL DICTIONARY 812 h; J3 [5 u8 _; Z% T$ `7 P
INNER MARKER, A marker beacon located between3 Q, `2 ^6 e/ R3 `$ l: M# ?* A$ G
the middle marker and the end of the ILS runway.1 }; A N4 z" H
OP, SEE - INOPERATIVE* m. P2 _' @8 M0 N |0 ^4 d8 _
OPERATIVE, Not working or operating.5 r" |& {$ u& I2 H) {
STRUMENT FLIGHT RULES (IFR), Rules governing' u) g: h5 k/ O* p$ p- `
e procedures for conducting instrument flight. Also a& x2 W6 Y: D. h% Z& ~1 B5 }5 G* R
rm used by pilots and controllers to indicate type of5 {7 r4 ~8 E1 I3 H8 K1 \2 j* |3 a) S
ight plan.
]& K; `% \3 l( p- QSTRUMENT LANDING SYSTEM, A precision
. H! g9 _8 P% e5 u1 c0 \7 ]- G# ^0 kstrument approach system which normally consists of
; {: O4 i3 B' t9 O/ \e following airplane components: localizer receiver,# b6 j- z, x# Q {, t
lide slope receiver, and marker beacon receiver.
) H5 S8 \. J4 j/ d* ` O) O+ E" {9 ], l) mOLOGICAL CONDITIONS
7 R5 E2 G6 m6 D: B; CMC), Meteorological conditions expressed in terms of8 J* t* M% }1 I x" i" ]# F: v
isibility, distance from cloud, and ceiling less than the% P N% {, l: F5 l
inimums specified for visual meteorological6 H6 P2 A8 Q2 s! s# V
itions.
, S* R3 w. `0 f3 D. sSTRUMENT RUNWAY, A runway equipped with
1 q- N. E: t0 [# u% g. n4 U- Glectronic and visual navigation aids for which a. E, D( v2 `* T) G+ J, d0 b5 H0 @1 A
recision or nonprecision approach procedure having1 K+ }% }4 l5 l
间的信标台。/ R: |" _! K; J# D% o( x6 a1 _9 W
不工作的,
$ e( G/ Q4 f9 D6 G9 y% R% ?见Inoperative
0 m5 n* |& Y5 f [IN
, ]2 u! H, X6 x r4 a# F/ c8 \; xIN
" w4 }* s2 ?1 e4 T5 A) GIN! i7 R: F- g4 c7 x- u7 Z
th; O9 J" ^. x+ k/ `2 ^
te' @( ?* U7 H/ ^ q
fl
1 s! {7 w& h# { U, G8 H2 J/ A/ [" s1 |1 xIN( A, o6 p! A0 ]& X& v, Q" q* ^8 I ~
in
' u' e1 C& f8 }th1 @6 a c6 L, S
g8 G6 E# L9 P9 B5 f- H. [6 D
INSTRUMENT METEOR: x. { m5 p0 v) ^+ ~$ T5 f9 A
(I8 g5 N* k# Q2 d, l
v4 O1 K% A$ J+ ]+ g a
m
* T: E; x( d) b$ |/ m$ n/ { [cond1 }% Z7 j, N6 ` J- A5 ~% q% j
IN' @$ G. [7 Q( i/ |+ E5 q
e# \; D" x9 g8 I
p% ^' ]5 g) z: P3 ^, G
straight-in landing minimums have been established.& M5 ]8 @" k! o3 @3 E4 s, U5 K" D
近指点标," B4 a& r/ o7 K. j
位于盲降跑道头和中台之
5 B; v. d' S! C$ ?.% z* N+ }' V) A9 i, S* z6 F
不工作,% h# `. E# t& Y" @5 H
不工作或无法进行操纵。- b( G- u- G) [3 t2 s
仪表飞行规则(IFR),
+ Y) i( |9 Q( [; E2 P; n仪表飞行程序所需遵守的规则。
6 _ z5 I5 |) J. o( |9 `; B! B仪表着陆系统,
: V& ~4 _: [! V7 H3 b, P1 X Y一种精密仪表进近系统。一般由航向道信号接收机,下
& N% u; G+ B1 ^* g$ J- D滑道信号接收机,和指点信标接收机所组成。
, n- Q) B. l. {. P2 z/ J以能见度,与云的距离,和云幕高低于最小规定的目视
: x0 P0 k/ n$ X& [0 f, p象条件的一种气象状态的表达。
9 \& K% ?$ i* X# F用于以精密或非精密进近程序作订明最低天气标准直
; s G$ f( ?2 J& s2 s4 g( @( Y着陆的装备有电子和目视助航设备的跑道。8 R5 X, w9 v W, r
仪表飞行气象条件(IMC),
4 k0 ^0 U2 e" @% q# S气
4 d4 Z' Z3 I7 R, {6 R; `- z仪表跑道,
) f% A$ L/ ? p: @/ J线) I& w9 A8 [/ }7 L5 {2 u/ l$ c
英汉对照民用航空词典B OEING: z6 g$ p8 T' `, H- y4 l4 M$ |
TECHNICAL DICTIONARY 826 f! Q0 A6 p1 \# M$ j
INTEGRAL TANK, A metal container formed by the
) J2 T$ F1 S- q% T% X6 Slane.
* Z* ?: \- ~- ^* n+ Acted8 M: y1 f* V# y2 X8 d: J2 s: E
circuits.
1 P" i& \- \* F5 Q/ v% _5 x4 ]! @Manual) L) {+ d$ Q1 H/ B
erformance data providing range as a function of a! H N& a. X. h, _
hange in airplane gross weight.
2 E& z; Y5 t1 f+ CTERNATIONAL RESERVES, Reserves required by* n1 [5 x4 F! A# x
e applicable governing agency when flying
8 e" @( F& b1 }, t- v0 }2 I) _TERNATIONAL STANDARD ATMOSPHERE (ISA),
' d+ P' e# ~& mhe hypothetical vertical distribution of atmospheric
N; L& e$ a Y9 i9 zmperature, pressure, and density as defined by the
* m' j& h# r( e).
* O) ?' Q& F3 X& YTEGRATOR, An operational amplifier whose output
8 B5 @8 d t; l* a1 c3 Roltage is determined by the input voltage, the input
' q5 n' |8 P6 b! @2 t7 o- j上
( w# c H( s5 @: s4 f9 D存燃油的金属容器。% M) Y- Q3 a. Z( g( V; Y
,
1 {7 f* |8 U& W- ^, q: W! W: g飞机总重量的函数提供的性能数2 D8 B' {1 h3 c& a& U, _, H+ U
。
1 W3 {( y& b! H9 G际航线备用油量,
, v* @' `$ }6 a5 u. a在国际航线飞行时,有关的政府单位所要求的备用燃油+ P7 y5 Q, t4 N s7 u( ]* D U
际标准大气(ISA),
$ r; M5 v4 |0 p) i' O国际民航组织(ICAO)规定的,一种只在理论上存在2 {' N4 B m; Y. O/ }
大气其温度,压力,和密度的垂直分布。: o1 a% G/ ^) k8 y
分器,# K7 c* D. G, g) m% d2 G
由输人电压,输人电阻,反馈电容和时间微分而决定其+ N; B+ T# A7 K
运算放大器。, Z) Y2 p, i3 b% a) J, y f- Z5 J
wing structure (spars, ribs, skin) for storage of fuel on6 z: u' S$ x+ w$ p
the airp
! L) } _% _! @INTEGRATED CIRCUIT, A small piece of
; e7 `* w; M5 A7 t% csemiconductive material that contains interconne
5 E+ e0 m- D; n+ yminiaturized electronic
/ J7 q, D, m6 i, pINTEGRATED RANGE, Tabular Operations4 |! K% J: C$ s" _& z% {% V
p
! w7 s. Q' H5 ?8 x; l; Yc
. Q0 R' @" m/ C: e4 OIN J% O: ?, k# ^' W
th
C# K* B- h+ @international air route.6 i$ t6 s" a, Y2 ]! d9 J
IN( _( M7 L8 x3 f: L: Q9 E
T
- r4 b2 W- Q, X9 }te
g! E! t# X; F* o# @2 MInternational Civil Aeronautical Organization (ICAO: h: {2 t: c$ y7 u
IN
% d; Q8 r- t. A" W: M* q9 Av% U* w3 x! n5 {8 E7 e8 P
resistance, the feedback capacitance, and time' u, x& Z: i. v5 P2 t. S
differential.
, O+ Z; U* C8 {整体油箱,2 b6 G- j4 T( e0 K+ s, \0 A
由机翼结构件(梁、肋、蒙皮)组成,用来在飞机8 m4 }* J) H% c$ n5 }6 o1 G' b
储% K5 p% F w; V5 ]+ ]
集成电路,, ]7 q* b' |9 V+ _+ @
一小片内含相互连接的微缩电路的半导体材料。
/ j+ q2 [& g" Q综合航程" g( L, a2 |1 U( z4 j% w; {
使用手册将航程作为3 S* ]( Z2 @5 Y8 d+ U
据! F G0 B v. Q3 w
国
$ m2 {' @0 P: m2 S* p: b) ~量。9 b2 ?$ U7 m2 S% j' S
国! `3 j4 e* I2 v% o
的' I4 V* [6 X: I, U4 Z; l
积
& \, S1 w- d) B' [输出电压的/ P* s: }# R" F5 ]
英汉对照民用航空词典B OEING1 Q6 [ j/ l) a2 \5 }/ |3 s
TECHNICAL DICTIONARY 83' @* c5 |# E% g# _
INTERLOCK, A wire connected in series with an
5 l# z) |$ o3 A( h/ N aequipment or device, or a condition that allows
# a% y/ b0 p) {* J* roperation if all requirements are met.
, [/ P( b- u- F& `4 pf the United Nations whose9 u. |% j; F" o
bjective is to develop the principles and techniques of, s& |2 G. l# F6 ~# V
ternational air navigation and to foster planning and) C: R; R' s# H5 j$ x3 l# w5 u! n6 d5 T" E
evelopment of international civil air transport.
/ U# @ D5 G, P) `TERROGATOR, The ground-based surveillance
& ]+ `& A9 s# M& v6 a1 Bdar beacon transmitter-receiver, which normally scans
* m7 x; [* W! ?( O4 s& gll
! B" z" V- g9 [, I8 Jon the mode being used to reply. The; S; F; G5 h8 J; W- B# b. a) l
plies received are mixed with the primary radar- R8 I$ R; \# ?8 D' |% ~
turns and displayed on the same plan position radar
/ b' G7 a' i- \) [+ Icope.& S! P0 g# F4 c- w5 D/ H$ v
TERSECTION,/ n$ C" i. j B- {
1. A point defined by any combination of courses,0 M: H8 L; H0 C+ X. p% ?# c& N8 t
radials or bearings of two or more navigational
! ~7 g) g- H6 F- p _9 maids.
* m8 h' K4 q: A; \2. Used to describe the point where two runways
8 H9 f7 m( r, J* c# ?cross, a taxiway and a runway cross, or two
* ~; n: f5 \! utaxiways cross.
+ a0 ^4 d. m, G% \cy)
- G1 f5 Y7 w7 Q2 i7 ktem.
7 q) W! z5 j0 C者, Q0 S/ C! `! b" {2 Z4 w
当所有条件都满足时才能工作的状态。
8 I7 |* z) {8 Z0 `组织,
" Z7 s) x4 B" Q. N# L航的原则和技术,促进国际民航
6 Q' s$ V3 j" p. z: H( e输的计划与发展为目标的联合国专业代理组织
+ q1 d* r* O! B) X& ?/ |问器,3 n3 r6 s# [! t; v3 y% h
一种地面监视雷达信标收发机。通常在工作时与主雷达
( I. Z8 B/ J1 L! v2 p% b2 r连续的无线电信号,不断地重复要求与" d) U U: c6 Z+ a
接收到的信号相混合,显示在同一平面位置的雷
9 L' M/ D2 q. y9 C( I达屏幕上。
3 _7 r! v% R8 s: w8 k' |交叉点,. K! h `# ^* f6 ~7 I6 I% e: l
1. 由航线,径向方位线,或两个以上的助航设备
2 W. l2 |: O" `5 h7 l" C5 M0 U( ^的方位交会而确定的一点。
/ h" N) q7 n: a9 L) n) l( M8 ]2. 指两条跑道的,滑行道与跑道,或两条滑行道
. g3 c7 v* g3 x& |. _ Z的交叉点。
' W$ h) Z, X% d, F( I5 b, F% _4 f9 PINTERNATIONAL CIVIL AVIATION ORGANIZATION,
1 R' R3 w; v) e3 C9 DA specialized agency o
9 B5 U& b, _& u; O; I& a: go
^& ], [1 v8 P4 win
& C8 n- E; ?7 N. |9 h3 p& k) qd5 J2 b$ p* E, k# l% c/ |: Y; l
IN, u% F/ X1 J6 z) f
ra
4 I0 I5 P" l" V2 Win synchronism with a primary radar, transmitting* Q! w8 U& r# F4 F
discrete radio signals which repetitiously request a1 q+ S; w( Y4 p/ X# b' ]* \
transponders
' J& n) z1 L5 {% ~- cre
7 N: ^3 S3 }% T2 _" T0 O4 Ere
$ V$ ~7 N( x7 l* I; f ts5 h9 N# b; A2 g" U1 F
IN& k8 R* T) `% j+ c* |) [+ T
INVERTER, An electrical device for changing direct
0 d# Y' w) a; [ O0 ~, Q7 kcurrent to alternating current for standby (emergen# e q7 n G3 O& r( B
power supply to electrical sys
6 g! }6 k+ W( S9 r, ~% o" p3 Y联锁,
7 A- `9 \) D* ^) z' y( _一个以串联方式将仪器,设备联接在一起的电路。或
% A$ _+ k" o, M; D# Q- c) o是
* d; X3 t! o x6 H$ [ w国际民用航空
7 R' `) Z+ @3 }2 a# j一个以增进国际航空导
7 ? |+ O; U2 X! {运
! |2 e! B! ^1 j6 C" s询
% r# C! J/ w. @3 H同步扫描,发射不
' i7 q! q4 k$ F* S0 w+ i% _其工作方式一致的应答机进行回答。所接收到的回答信号) o; a3 t! g( {8 Y7 v" X0 a
与主雷达
y) b# H4 S8 u% f" @4 s2 | T变流器,2 T0 ]4 q6 S% a" R `
用来将直流电变成交流电;以供电气系统备用(紧急)
1 B4 ]) I% m( \/ w! y4 S. D \; r8 G电源的电气装置。# |9 R* r! K: S7 r% f9 H/ F: w# y6 u
英汉对照民用航空词典B OEING
. N1 {+ O6 b5 d7 V8 e2 P8 ?" ~0 @, LTECHNICAL DICTIONARY 84! i& n& i$ P8 L
IRS, SEE - INERTIAL REFERENCE SYSTEM6 ~, Y; R d( j+ ^8 L
ISA DEVIATION, The amount of temperature or
) D$ _2 Q6 [) q1 i# e1 l2 ssee International% R% v/ W$ [/ T+ Z+ |; x. T9 ]
tandard Atmosphere).) n5 p" }- k# \& T* b+ j+ }
LAND RESERVES, Reserves required by the
2 p' s0 x: Y9 P) P# Upplicable governing agency when flying routes! t: g S8 r% j8 l8 v( p8 n' c8 k9 o" X
etween islands with no alternate airports.; F$ L& k' k, K% G/ e2 N
CONDITION, Cabin pressure (altitude)# K/ \. j7 q" k; I' y$ _
maining constant with changing airplane altitude.
7 T# D9 o# M: H6 c8 ~" oising the2 E; K6 H5 @& ^" w* [/ z! \
a
8 ~" J. j, T5 c( I. Q0 \; H2 @,$ O8 j0 r, S3 S; Y- w
pressure difference from ISA (
% C d, J& _' e( j9 HS( G$ k, }5 j9 L8 f* s7 N. k5 j+ Q$ _: L
IS
. }6 _( |/ e5 v3 @0 b ua
: `3 ^' \+ N0 Gb
: S' @4 X, h/ J5 m1 cISOBARIC
( k6 O. J, a) s! Dre. \& v2 V K% B8 e2 U4 [
ISOLATION VALVE, A valve in the system for2 @. v9 D# M+ b! e: D% v
separation of the system into sections.
0 i* k% g6 y" T* i9 C- PJ/ z+ l" ~$ x d4 I# i
JACK, A mechanical or hydraulic device for ra
6 ]& _( m. i6 j/ Wairplane./ U7 s. H! n$ e2 L
JACKING POINT, Location on the airplane for using
8 w4 d. T: i+ T0 }jack.
3 d% W# h* u# H5 z5 f惯性基准系统 I. P7 l: F. S. A
见Inertial Reference System.
+ B u- s( I0 e1 u) {5 R; ]. b( o与国际标准大气之偏差,
! k: l5 C( [ Y( @压力与国际标准大气的差值(参见国际标准
K1 D4 e* g$ V( B( i2 l* q有关政府单位要求在没有备降场的岛屿间飞行的飞机
* @5 b9 `- G7 t' E带的备用燃油量。/ e* ?6 c* U6 x! z- B7 ?* S, V& q
压状况,' @( R3 N- n4 s" W; Z3 W' z, X7 L% Y8 |
在飞机改变高度时,座舱压力(即座舱高度)保持不变
: T$ `' A: s; u P {状况。5 v0 ~6 q9 ^% T* _4 @$ t2 v" R
斤顶,8 n9 P ?- t( U! N' l6 @$ v
用以将飞机抬起的机械式或液压式的装置。0 \+ p2 Z" Z1 \* t; x4 w! v# K0 |
温度或3 T; o( b1 ], ?$ A% c
大气)。" a7 `8 ?7 i- d9 k1 V" k
岛屿备用油量," ] Z% \" ^, U+ o: p+ k
携, P' Z6 Y: z @, u: _" ]
等
8 w' q; x! Q0 X3 _$ o4 v7 k9 T的
" ^: T! g: N8 b X. `! A隔离活门,
, B$ w1 s9 _! ?6 h4 w( `0 w用以将系统分隔成几个部份的活门。5 @' w' c9 O+ U K& ?
千$ F& L/ x: p% V6 G
千斤顶支点,+ |1 `1 |' p2 h3 ~
飞机上可以让千斤顶吃力的位置。
' |5 p; f& N2 _. z7 s英汉对照民用航空词典B OEING5 k# a+ T) V9 K
TECHNICAL DICTIONARY 85
1 v( h6 @; G% n& u2 y/ cJACKSCREW, A rotating threaded rod used to drive% m% c# i( h6 D+ _: P
moveable component such as a flap or stabilizer.3 d! O2 X% L! g Y- W/ g
a 致动螺杆,6 c/ Z. [- o' F1 z0 ~# L
用来使可动部件如襟翼或水平安定面运动的能够旋转
% x3 J. w* ~5 h& H* K# P的螺杆。) ]$ g5 q# a! w" T5 J: r
英汉对照民用航空词典B OEING
5 J6 d/ V6 p; K/ d- M) W3 \TECHNICAL DICTIONARY 86+ |- i T8 W9 I7 ~5 V
JET PIPE, A control component in some valves and1 P4 M0 t0 E; o# B" R4 V, J
ET PUMP, A component in the fuel system, operated6 Q& f( @8 I" Z% |5 _
r removing water and fuel from a fuel
: ]5 l9 l0 X- ynk. i+ k h+ ]' [4 D; E% B
射泵,
/ Y# E' ?, G$ ~/ G内,由燃油压力来操作,用于从燃油箱中排除) [6 S. S* ^, R0 O2 z9 ^ g+ D
和燃油的部件。, b; [7 |7 h% s: e& k I
actuators for controlling the flow of hydraulics or, L0 _! O }7 T5 Z5 M& [% f4 ]: @4 P
pneumatics.
: r. `0 ^6 I' ^- H+ oJ3 ?7 R+ C! i; d* q0 a% o i
by fuel pressure, fo
$ I7 D7 M+ L% Q1 r7 P% Bta
2 K7 |0 D1 A9 @# z喷射管,
+ D( k/ c% }1 C4 ?; G8 z) y在有些活门和作动筒中的控制元件。用于控制液压和+ U: G7 V) S! z3 ]- _& R
气动的流量。6 ~1 O$ r7 @" H# d
引& B3 ^* o5 V9 k" K4 G7 o
燃油系统9 _4 U7 s. R( S
水5 h- C2 z- j1 ~& ^1 w8 ^9 D2 L" q
英汉对照民用航空词典B OEING
! a, w6 ?7 j! y" s4 n+ r& hTECHNICAL DICTIONARY 87, p: s( e' e+ \3 X9 s
JOGGLE, An offset in sheet metal construction
6 x, Q& y! h8 x. g2 L9 cdesigned to allow one piece to overlap, either higher or
0 w; W, Z6 v1 O0 H5 T' pwer, the other piece.0 R! y5 U. F K& q: d' t
OULE, A unit of electrical energy of 1 ampere of/ j- b8 z: a/ }% t1 l* n* g
urrent passing through a resistance of 1 ohm for 1
# Q, u. Q/ m9 _* \% [ Zecond. Ignition system energy is measured in joules.2 }2 c; B" ~" J5 W" O6 C
UMPER WIRE, An electrical connector for temporarily
4 C2 Y: t& V! D |ypassing part of an electrical current.- z5 o" n9 H/ d! K3 j6 L
UNCTION BOX, A container which serves as a joining
. ^* {1 S. T$ ^8 q3 xlace for electrical connections. May also contain
7 L; n% X$ w/ y( s1 K7 ulectrical components.
7 F! L( [: R" c/ ?EEL BEAM, A structural beam in the fuselage center
2 [5 T2 l% g9 @$ H* |ection (wheel well and under wing center section) to
* m8 x- H) g0 M& a3 g' U. ?' FKEVLAR, A light, strong synthetic material for
/ A( T9 H" |3 @3 v8 C3 w) A# X6 }secondary airplane structure.
3 o7 p4 i# h+ W,使一件金属与另一
+ n, t1 P, W6 f: A$ Q3 B相互叠合。* ~7 V1 |7 x9 ~4 S" s+ r
耳,
1 N2 j L0 m- I- N) W电能单位。一安培电流通过一欧姆电阻一秒钟所需的电
) S* K0 h2 z$ w ?. a为一焦耳。点火系统的能量用焦耳度量。3 O, J( d) P0 d4 }0 a$ b
接线,
J1 l2 m7 F ~1 x H用来暂时旁通部份电流的电器连接件。! }) d; X6 p; D* A% t, u& d) g
线盒,0 D( \# h$ t8 H( I0 T7 |
做为许多电接头的汇集处的容器。也可能内含电器。! h5 L0 A4 \% ^9 Q/ W
梁,2 Q# r/ C d/ A- j5 e
机身中段轮舱和翼下中段,用以防止机身弯曲的结构。
1 o+ ]% [6 ~1 `; ]4 C' ]) LKEVLAR,: |$ C B2 f+ Q9 ]3 x
一种即轻又强的人工合成材料,可供制造飞机的次要构/ v6 T1 F* \9 H% ~9 A
件。9 R7 \; M3 H0 |" I9 W! k6 ?1 u
lo ~6 E ?& j* ]1 V1 n
J- }' H) k( a; e# f) x0 _
c, h' o4 y g: s$ [( Y
s, x/ A( Z; }6 O: S
J% ]. Y' e+ b) [0 \
b
, w6 L6 R0 P' lJ
5 S6 Q z9 h9 Pp
* [9 h9 h$ [! P9 T4 C8 p& Pe% a+ x" q* h1 { Q
K# r n; O5 b, `. b$ @) }
K
. A$ d' F0 J" p# Gs6 H0 O5 l- K3 c. u1 y: ~: h5 A
prevent the fuselage from bending.1 a* e) X% a, X3 |- D" y# T
折接," p+ n1 F9 f$ l
一种平面金属结构设计的弥补法
& Q5 m& k& X& C& O件! A6 D6 c% f8 x# |& ?
焦. q! d$ u+ g1 i8 U( A* m* p. p/ R
能. ~& F# J& t' e; P$ Z7 t+ v
跨
% w/ k8 `$ y3 I接7 M, r& u" ?/ V7 Y
腹
) u+ I+ n0 j' D* ?% S! K英汉对照民用航空词典B OEING
{" j8 ^( I& M3 F& D; O) N, H2 ?2 NTECHNICAL DICTIONARY 88' K9 N* Q' ~. ?! W
KILOWATT, An electrical energy unit, equal to one* H3 ?9 G" f* [
thousand watts, for specifying generator power output.
( b+ t; C! H: ]! I( P1 T# e+ e! jKINK, A sharp bend, twist or dent in a section of tubing,
# ^, N4 f+ c8 i( C$ b: [+ l6 n7 pwire bundle or angle stock.
/ z. x% }/ `# [: C B6 cKNIFE EDGE, A very sharp edge on drilled or machined
0 y! l1 ^! k9 u rmetal which is usually the source point for corrosive
) L8 h ?; i/ q) U8 I, D# v0 Jattack.
6 \+ Z9 Y- y. e# j) ]% N" J* uKNOT, One nautical mile per hour.
4 k. ~+ u8 @: s! C8 ]; I6 l) pKREUGER FLAP, A type of leading edge flap that is1 D" @, B& b1 _* j* }: W
fixed on the lower side of the wing and rotates forward
3 p) _5 ? D( G' X1 ^% ?into the airstream.1 n9 T0 q6 M( p: b* H' [! s5 R
KW, SEE - KILOWATT
; d% R1 S% Z( x9 }: e- |1 YL2 ? I- K9 S& g- Y4 B
LABYRINTH SEALS, Rotating and stationary, d! p) P! w( n& Z9 r
overlapping structures which utilize differential air4 x$ ^. c' Q6 z }9 u0 Z
pressure to form an external seal. Most commonly used
* e( f: h# `. \2 T4 ~, |in turbine engines.
. _5 f3 b- T2 ^扭结,
% b1 B) ?3 t0 a, ]* N/ n& P, @在管路,电线扎,或角材中的尖角,扭转,和凹坑的部( V8 D0 @" U5 n! ]% j: @0 |8 u' C K
份。+ Y) o: s% }2 O# D
刀刃,
% b5 O# r# }2 P( i钻制或机制金属的锋利边缘,通常是腐蚀的开始处。
6 u5 u+ V& }/ Y. G节(K,KT,KTS),; Z- s/ J9 |* g q. S, u) J
每小时一海里的速度。 Z( }9 A) G6 e9 h1 A' L9 Q; a
克鲁格襟翼,
! q/ i& a3 E# ~% r# Z% j一种前缘襟翼,位于机翼翼根附近,旋转前伸。
& }" D1 n5 W. d6 Y/ i8 W3 b千瓦,
4 i# f7 K; W" b; U见千瓦(Kilowatt
8 D/ O- W5 g" b千瓦,
. n2 o/ ~8 p- |# N7 c6 t" D' ?电能单位。等于一千瓦。用以确定发电机的输出功率。+ |) W# G9 r/ Q% x4 _
)。1 z/ x }; w+ h$ \& `
蓖齿型密封装置,
% `0 V, e! D3 P7 y" F1 c. N/ N旋转并且固定的重选结构。用气压差动而造成外部的密
\- x @$ c0 x+ Y/ h! p l! R封。在涡轮发动机上最常用。
n- L2 s8 Z6 ^' ?2 F* ]英汉对照民用航空词典B OEING& l4 ^: B3 H+ K5 i7 \
TECHNICAL DICTIONARY 89
/ F- G+ n. V9 l- ~ @LAMINATED STRUCTURE, Composed of layers of a! Q" g4 ]0 c) D, Q
ake a( O1 I2 d6 p" z/ R' `! `
ht structure.
. _. M: C, K+ |1 U, m( R# h.E.D., SEE-LIGHT EMITTING DIODE.
/ w2 C. ^% I. n! ]3 o6 p* `ANDING GEAR, The nose and main wheels with the
" ]0 ~& O9 f/ M! S8 P ]( }0 Xttachments for supporting the airplane on the ground.) T; m7 }$ s) j" Y2 U
LANDING GEAR DOORS, Panels operated by the; ]; g1 ]9 V( t$ \; j4 d" {; Z6 V E
landing gear for closing wheel wells when the landing4 C8 i, \/ @7 ?& K( k
gear is retracted.
5 e1 g" X3 q$ z s! kLANDING WEIGHT, Gross weight of the airplane at the8 }, e1 K, g+ h) u! O4 D
destination or alternate airport.2 ^2 ]4 d# d9 D3 A5 \% ~5 j
发光二极管,9 E! Y2 G' e) ~& f! V5 l( p
见Light Emitting Diode& O0 N9 K+ c+ ~; h
composite material bonded or cured together to m
. m- ^" v/ d- \9 ~0 o% ostrong and lig3 J8 P, F! W7 f( v; r+ H
L
" a+ P+ x( J4 ?, D- C; Y R- |L) G1 }& z5 ?, c. G6 S0 Q$ k+ Z" j
a
& H, _. P4 Q) Y9 v, @分层结构,
/ l0 ?; Q- T# Q' L) b5 o) a0 O* J# ]一种牢固而轻的结构。由多层的复合材料胶合或固化而
. O! p" b5 l8 i成。3 F5 Y: [7 N0 D. h/ k; w( S. h
.. U9 Z( _: i- ?+ _8 o
起落架,/ K E& E& X$ A# G/ L T
用以在地面支撑飞机的前轮,主轮及其附件。 n8 ^! P6 a* Z9 Q% s4 {
起落架舱门,
5 U3 D7 H$ Z0 T2 o) Z由起落架操作,用以在收上起落架后关闭轮舱的面板。
$ h" r/ V: z2 j& l着陆重量,
% {& y- }- v0 f& O; S+ g7 ]飞机到目标机场或备降机场时的全重。
+ L$ a8 {5 Z( N3 r* Z+ t; s英汉对照民用航空词典B OEING' m5 ~6 \* P' J- O' T/ p
TECHNICAL DICTIONARY 907 L8 v! P& {7 l2 A# A. H/ d
LANYARD, A cable for supporting or holding pan3 Z( j9 o4 h9 _& H
open position.; h6 Z- J; p1 F$ j9 |8 N3 D
els in9 Y: ? g: {5 @1 P. Q( c
AP JOINT, An overlapping sheet of metal, joined to the
' p2 x$ [* x2 Ddge of another sheet in aircraft structure.6 q/ ?6 f }- Q* ^, ?, N @' c
ASER GYRO, A gyro which uses two laser light beams u% a" P+ s$ L
measure angular rotation.
$ R4 n$ K: @0 D5 M5 e5 J- n7 w.
& b3 Z k- E0 k( [, ]ATITUDE, Measurement north or south of the equator$ |* k, E2 E" T4 y
s, minutes, and seconds. For INS equipped5 |9 E- j" c$ d4 N0 _% J
degrees, minutes and tenth of minutes.8 b0 Z9 h& E- `9 R" ~) b; j5 X
l device for! o6 H! y3 W: w5 f! Y6 \
hanging stored chemical energy into direct current.* b: k& z R) H/ |' O
ses lead, lead oxide and sulphuric acid.
3 s/ e; J7 A) K% L! Z搭接,3 d( {' q" B% i9 R j
飞机结构中与相邻金属薄板连接的重选金属薄板。
; ^* k! l& e& L" M激光陀螺仪,
& u8 F3 L: p$ `1 U一种由两条激光光束来测量旋转角速度的陀螺仪。
4 A: R; n# A5 U8 ~用以紧固或锁定的装置。6 ?" Y. ~# _& k+ p
的轴。% w( m7 R- X; ]0 d: B
方式。' j @1 j$ K( z, J5 d* p: Y
度,
) }$ }$ e- G4 [. V) g地球上与赤道平行之弧线。由赤道以北或以南度、分、
" W# \/ b1 U* M度量。对于有惯性导航系统的飞机则以度,分,和十等
* } ^$ q2 @* U. ^7 b. b5 z度量。
! I3 d! s1 X3 m3 F1 c6 w酸电瓶,
( J8 n$ m" ^9 `将贮存的化学能转变为直流电的电气设备。它使用铅,- [6 O) r8 V% G$ J% N% U
化铅,和硫酸。
. d5 q7 u6 O0 S0 K& QL! b1 {/ a: M5 U. h. u
e, B' E3 X( N7 Z5 D8 _) t9 O
L
- {# ~5 f: f! H8 v4 Ato/ i5 c+ v8 K; K: d8 ^% |) m% m" C
LATCH, A device for fastening or locking.
; ?& X6 c' d# T' t+ u. t! [* I5 fLATERAL AXIS, An axis passing through the airplane's" p/ ?, V. R; k5 Y. \
center of gravity, from wingtip to wingtip$ J* Z) {% M3 W5 Z6 _
LATERAL NAVIGATION, An autoflight mode in which1 Z. L5 S: l0 X' a' O
the FMCS is used to control the airplane roll.* c9 i" J5 ]+ v/ O
L8 l. g+ B& u* t# V4 Q+ @0 H$ I, t
in degree
9 C( `- _+ g' u* ~/ l6 Jaircraft in
7 s! n" L8 ~. E% R. @5 ^0 V vLEAD ACID BATTERY, An electrica# |6 h; j# `8 ~, u% ~7 z$ ]
c& i: B/ K) ]8 ~ N/ ?) m
U
5 Z% u4 ^3 }8 L1 c) V9 j牵索,
f s2 L/ U w" _( @% B7 B# U1 _- T) ~用以使面板保持在打开位置的钢索。; g. r' w) |3 L% L2 ~4 D8 X# }
闩,
( Y7 ~% a8 i' x- z- o* |横轴,
- m) T" I& ~0 H% k% Y4 V通过飞机重心从一侧翼尖通向另一侧翼尖
, W' s8 [" J6 z* e水平导航,
& `3 A a4 T0 p( Y使用飞行管理计算机系统控制飞机横侧的一种自动飞
0 J R+ B& a" l/ U0 Z. U' h0 y* |行
/ _& }: b5 }2 n纬" w0 |* S0 u8 n' W, o
秒; T& d$ ^, L7 `& @
分6 ^5 e/ a. b& T/ }- N; G/ E! `, w
铅
& `9 F" ?9 Z5 Z4 i |+ L, \# J: O) g氧
# L3 D0 Q5 I5 G5 h英汉对照民用航空词典B OEING" L3 z1 x1 l* c& a7 Z$ M9 v4 ]
TECHNICAL DICTIONARY 91- X0 C6 y' t1 N8 Q, x0 ?
LEADING EDGE, The front edge of a wing, stabilizer or: O' U/ a4 x% z/ Q7 G, R' e4 h
ED, SEE - LIGHT EMITTING DIODE3 k- }0 E! A' n& A% D
EMAC, Acronym for Leading Edge of the Mean8 _- `6 e' S& t' |+ { D# \
erodynamic Chord.' y6 e9 }3 O q
IFT, The vertical force produced by the airflow past the2 f& r) y( L( `
s of the wing. L- v" n) v4 Q* {# \
IGHT EMITTING DIODE, An electronic device which
4 A3 G5 w: ^! s9 d8 w" Z# C& Z' ktes with red, amber or green light when supplied
( G. k3 U0 b% N: e, D: J4 ~( ?+ Kctric current.
6 T0 Z+ s" f# Y) E7 _9 L6 t! t& Q, d,
# ~, S( ^2 S) f8 M8 bcontrol surface.- E1 M! ?/ N6 q
LEADING EDGE FLAP, SEE - FLAP
/ c$ d# K) z5 r/ KL9 V8 X% k) Y, y# L4 d
L. Z& D; {& T8 n
A/ F2 q6 e& V% b% \. X
LEVEL-OFF ALTITUDE, Altitude of which the airflow
# b5 p' }* s9 G3 qpast the upper and lower surfaces of the wing.
- v' ^1 B, b3 gL
5 u S6 G: e5 `( S# N+ ]) Pupper and lower surface; L8 e+ M* {8 d: e0 p9 E9 n
L0 R6 F/ p6 {! D0 y
illumina$ h/ n% Q4 U* j, e. V4 ]# E
with ele; {: P, d- H) }, k! j3 Z& f. a
前缘,
- p( P6 m7 H$ ^9 W/ ?机翼,安定面或操纵面的前部边缘。
2 V3 G+ d. L4 a% W p" X前缘襟翼
* |, b& {5 {2 ^' H& i见Flap.
C6 M% I7 t3 s& R发光二极管,
% m/ i* ]9 S* f9 c% z7 ]" uht Emitting Diode
5 w" F1 w/ |3 x8 }+ }' O0 R见Lig .: `' i& p6 ?7 `* n* u9 a( h
均气动弦前缘,7 I9 A0 F- a. i# }5 \
平均气动弦前缘的缩写。见Leading Edge of the Mean" U* Q, s9 V4 r7 U0 {- [ M% R
平# M. d2 }. `1 J9 s* d- d) r
Aerodynamic Chord.
; E5 e4 H) \' } e7 Z _力,
, [( e X$ {; t. O" v过机翼上下表面所产生的垂直力。+ f1 e4 _2 P; G, ~1 g
光二极管,
4 O$ i8 Q5 d! ]% ~: R8 K6 {: e通电后能发出红色,琥珀色,或绿色光的电子元件。0 I0 C1 T3 D5 e2 e' o- q% a* u
改平高度,5 y3 s) Q# @, o: G
飞机因巡航时发动机发生故障而下降至的高度。- J; e" L2 j- d
升! M/ p8 n, f( e7 Y- t) _1 k
气流流
1 }: X4 p( j& V1 r- f发# U" A7 y3 [. T" q8 h
英汉对照民用航空词典B OEING0 B; p2 y9 `. C5 \ Z O1 x
TECHNICAL DICTIONARY 92
; _; P0 q% n5 B( c1 S4 xLIGHT PLATE, A component part of an instrument
" r( G4 \) ^6 l. }* Jpanel for illumination of words on the panel.
1 |) B( ` g! r9 TLIGHT SWITCH, A switch which contains a light. The/ p C& L* ^: q+ ]
opened or& u j7 j+ p6 v5 Q- a) u# f( R
losed.
: r$ t/ J; w( F8 Q( Y/ c& Un electric actuator which turns off electrical power to
( F. T7 ~2 f1 K! J+ _e actuator when the actuator reaches its open or
4 K# z; l9 [: J/ ^losed position.
! A7 v9 ^4 R/ p5 c/ o9 q2 O& `IMITATIONS, Performance and operational limits
- P4 g/ F$ I, X$ X0 a4 x8 X4 Lsted in the Airplane Flight Manual (AFM), such as
* t' @ [1 {6 U" e3 k+ Aaximum airspeed, maximum altitude and center of. A- \" j1 c6 L7 c/ v
ravity constraints.
% s& ]: S% ?& B; Ky2 S b% B! J. C5 {8 b- u
craft during line maintenance( B, h" U& T! Z( q
perations.( l: c. \. h @2 N: c
ontrol4 W+ q- G6 }- ?; L2 G! |( E g* G
display unit allowing control of information to and from* H3 h0 B G5 R/ A' v0 X. {
the scratch pad and designated areas of the display.
) ^; {0 c6 A' o" F3 b8 N! g& e& _; H光电门,
9 V7 o9 u8 E4 ^4 u( E电门开关而决定灯的明灭。- A. ~1 k, v) M
在电作动筒内,用以在作动简到达打开或关闭位置
4 ?4 _3 M/ _& L! O6 X. S% R9 u' r时,切断电源的机械式操作的部件。1 g% x6 ] K/ b f" V* l( V! S+ T1 G
各种极限,) H; U+ N# ^1 C" L' q0 n, [
飞机飞行手册(AFM)中列出的性能限度和操作极限,
$ s" g! t" N9 W, w. z如最大空速,最大高度,和重心的限制等。! `& d$ |& I# q9 T; q- g) @
在航线维修中,可以在飞机上即时拆换的部件。" F" u2 R1 Q% |' g1 [; Y" r
飞机管理控制系统的控制显示器上的电门,可控制草稿' V) R# z% S, `. f2 B" F W, x2 B
栏和指定显示处信息的输人和输出。/ N/ X# j0 {' y E5 n; \5 Q. W
light either turns on or off as the switch is
; {% C+ }/ e; z& Tc* W" r% g. u7 l4 Y. R1 n# y7 R
LIMIT SWITCH, A mechanically operated component in
8 |% I- U- h- Ua0 q9 S* J. }8 X- I' a
th
- L1 J4 G; ^$ }& N2 t# i, Qc
) b5 L6 p' f- @3 k" |/ z: A' D0 }& QL
% e* q' U. H9 Y. _li
+ O6 N% a* N- L( e8 Jm
, m/ C) r' j4 o0 }+ C- kg
$ A% |, L) f9 b6 Z O! L7 g! I. jLINE REPLACEABLE UNIT, A unit which can be readil8 F* K9 ~: O( e$ S$ L5 X& D, ?
changed on an air
, \" \" N7 ~+ K& Zo
; ~" s+ K) T& {8 y! }2 X LLINE SELECT KEYS, Switches on the FMCS c2 E7 h% W3 z% W- W
照明板,
* d# h* x9 X% S" v6 K( Z仪表板的一个部件,用以照亮仪表板上的文字。* W5 ~! }& A& m5 d0 B$ C2 `
灯
5 H# v1 ?/ ^0 i+ i7 l/ p: E带灯的电门。: \- ]! a4 a2 L9 m9 X: G, l d
极限电门,
! }1 {* {# A* \& p, T$ t航线可换件," Y+ S7 y- e: R5 K0 u: L! N) {
行选键,
, F C/ a, O$ c7 w! q3 [3 u英汉对照民用航空词典B OEING
/ Y% M, Q" S, G UTECHNICAL DICTIONARY 93# j' ^8 c+ B% V
LINEAR VARIABLE DIFFERENTIAL TRANSFORMER,
0 l3 l9 E2 ?, Unsformer with a linear response.$ e5 v' a5 n: W2 G: C
NAV, SEE - LATERAL NAVIGATION
; K3 u" u" A, IOAD AND TRIM SHEET, A form containing tables and0 m$ U: i: m+ U; |- ]2 l+ Z/ J
harts to account for the weight and balance effect of all
/ \( q3 \8 q( B( U4 c" {5 Bpe of an
3 @0 F( h( a1 w I6 [4 p0 ^S approach, normally located at or near the point of8 ~/ h P B3 y* f7 T
ecision height.
( b2 X( L$ u1 z5 y9 A2 v9 ~er/ P; ?9 B2 S5 i5 B
eacon at or near the point of glide slope intercept of an
3 L% i4 z6 O T! F- m4 g# wS approach.
, U7 @! a; f8 N9 o, r+ b: p: {ich provides: W3 T4 s p. [1 A0 i
lateral course guidance to the runway.
" C$ u l/ @( T) h$ o- q* f$ g差动变压器,
* R4 }! {1 B# K平导航,% W7 m$ C. V: b# k
vigation
. j4 j3 N1 `( D/ x4 @9 f$ CA differential tra
( K+ a5 }3 E, Y3 c7 w% eLINK, A short connecting rod for transmitting motion.
1 g! b! i3 A( d5 eL" F: P- w# `/ x, O# N
L
! \" c( |: _, }% e! k! qc
( T% ^& J6 P: v5 V( \items and fuel loaded before each flight.
( ~9 `+ j: |# GLOAD FACTOR, The ratio of the lift being produced by+ s V. G' K& f# `) v& b
the wings to the weight of the aircraft.- E' V- q/ O/ q
LOCATOR MIDDLE MARKER (LMM, MM), A marker
- t7 o3 {, q; K, f+ F& d. u0 Cbeacon that defines a point along the glide slo
" a3 m( k' P* l# _/ e6 \$ p( iIL" R; s: K9 E2 f- f2 {" Y
d
9 {3 P, c7 A- J; Q+ xLOCATOR OUTER MARKER (LOM, OM), A mark- V8 e5 N3 j$ i/ r6 r' n
b) i5 B( V8 b4 ?8 W% J6 ]% K) k
IL
6 J4 q! O& l( ]; D/ D, rLOCALIZER, The component of an ILS wh
7 V% Z1 H+ r7 [' t线性可变6 E3 C: ?+ a2 ^7 [* P+ n% u
具有线性反应的差动变压器。" ~3 t* X# R q" R8 a$ W' u" G
连杆,7 }$ V6 M( m4 l: R5 E4 a
连接在两个部件之间,用以传递运动的短棒。
p3 t- C5 w4 R- a" E$ u2 x水& W; u& g7 L i& p8 U9 K
见Lateral Na .# m1 z) _8 X* N
重和平衡表,* w$ }1 X& M' z0 O4 u" _5 e' \
有着显示每个航班前飞机的各项业载和所加燃油对重4 G U2 Y# ?$ R- M
衡影响的图表的一种表格。
' S/ P4 _4 A) J6 E: E,
4 s; e" G8 w- _! N+ l; w/ H2 K( l附近的一点的指点标。7 N; e2 V7 v# V8 H
近仪表着陆系统的下滑道截获点附近的指点6 V p8 F7 W; S- b
。0 b, B4 p/ K" o) |# L, T* D) u7 z! c
仪表着陆系统中的一个部件。它能提供到跑道的水平航9 o* a8 V2 b" w+ x/ {, S, c- j
道引导。1 `# `# R$ V9 `1 E, z
载3 L! i7 Z* p; Z5 V1 Z+ r" v+ g
量和平
8 ?. h! {9 X- Y7 `& M* ^装载系数
0 n/ C8 I; m/ g机翼产生的升力和飞机重量的比值。' b0 g' D% D/ z; y
中指点标," W4 _* C/ |' v# }; _/ d
用以指示仪表着陆系统进近的下滑道上通常相当于决; U' R( g. i4 h- p% E
断高度或其
7 ~7 P7 l8 i: p远指点标,
) F1 k! d4 p% S) l& c位于或靠: _$ E7 Y4 f( l6 m9 N0 c& C6 H
标4 V2 m4 t4 m. d" X
航向道,
7 H1 u* J) ~2 g$ n英汉对照民用航空词典B OEING* p- \% F$ i: g2 V6 K1 l
TECHNICAL DICTIONARY 94# i O* C* h. P
LOCKBOLT, A steel fastener which prevents unwanted P: T0 a% B/ i0 a/ ^! E
rotation by using a collar instead of a nut.
6 h. L3 v6 W) g& iOGIC, A representation of complicated electrical and
! G* [! S1 I! }) O7 `5 Hlectronic circuits by simple symbols called logic
, @" S2 _3 _! R9 u, Y- o% V& `) Uymbols.& v( r3 j j* U" Z* s4 n( P5 x8 a
OGIC DIAGRAM, A diagram that uses logic gates to9 _$ _8 L0 q9 \8 O& `
present the function of a control circuit.8 g/ t2 W$ I, G1 E( ~7 V, t
OGIC GATE, A device or circuit which has no output! g9 Y8 f( o' A% \ F+ r3 K
ntil it is triggered into operation by an input signal. A
& S( j- P) ^4 t! b% Q) @; a/ Mgic gate is an AND, OR, NOT, NAND, NOR, or ~. G/ ~2 N9 }7 D8 x4 J g
LOGO LIGHT, A spot or flood type light mounted on
0 g. u/ s' a( @. `aircraft structure and directed toward an airline LOGO or4 ?+ i5 g) g; A
other message on the fuselage or tail surface; for
) s. _/ K* A1 v2 mvisibility during hours of darkness.
! F# H9 w' d. |3 r2 O! o1 o& Q,
4 \' R; M) B& z0 f4 @4 C$ P钢紧固件。6 Y/ w7 V8 U+ h2 H) L+ i
逻辑线路,
* Q/ f/ _: |( }: t用简单的逻辑符号来代表复杂的电气电路和电子电路。
' Y5 s( x. Z2 N% h逻辑电路示意图,
- l# S9 n! u( o9 V7 c) x一个用逻辑门来示意控制线路功能的图。
. Q7 R9 X2 I3 k. O: t: x逻辑门,
6 B2 E! {( O" d, S) N/ Y只有当输人端有输人信号触发时,才有输出的一种元件" _, f( G8 G. [: F
或电路。逻辑门分为:与门、或门、非门、与非门、或非" n" ^ L: i" c! {8 _6 C
门、和异或门。- V6 X* |# n9 [
标志灯,' W! w3 v+ H" P; l! h
在飞机结构上装置的聚光灯或泛光灯。用于直接照在机
4 ?9 p" B6 f2 R. y( C身或机尾上的航空公司徽标或其他标志上,在夜航时照亮
- N9 l- N! D# [- q' I; I1 g. n; W这些标志。
! ^$ ^8 j& H+ hL `/ t R$ ]: `
e
* K0 s9 U% M3 U8 f$ r: T us2 ?* G8 W; |" l2 A/ C; ~. D
L( X X1 z; c. {, D* D4 T* m
re
" ]; \3 M0 `" E8 @% m# s" }1 bL' ^5 D# y! z# M& u- k1 S z
u+ T) Z1 N0 o0 [( t( B
lo5 Y6 R0 h, t# r
exclusive OR.& E. D, Y% G2 q( ^
保险螺栓
' p7 A9 B) }. K; F j用环圈代替螺帽以防止不必要的转动的
' z0 u9 X! q7 V3 K英汉对照民用航空词典B OEING
, v! o9 s; U! H; j1 o; J' nTECHNICAL DICTIONARY 95
# X# s. z1 g* ]3 y) pLONGERON, A structural component in the horizon7 G+ W; n1 y* e+ m) U3 \
direction of the fuselage or nacelle.( C0 i! W* L9 c! }) }8 o1 a' l
tal/ Y" j1 n. b- U, B }" J- `" Q
RUISE (LRC), Cruise speed that is
/ h* [ j+ X* A/ _" ~ssociated with fuel conservation, producing fuel# r @7 l: _8 r6 i# P; o
ileage one percent less than the maximum fuel
0 O( J! C9 V! s, w2 Uileage available.1 z1 u/ M+ A) R0 W
ONGITUDINAL AXIS, An axis passing through the+ M. A1 S/ n0 d$ n+ t3 C
irplane's center of gravity, from front to rear.; h: J+ K V/ D" F8 p6 _2 [- U: _
not
8 ~; A* O& R% ~OUVER, An opening with slots allowing the passage of
5 L- [6 l9 q* V+ r) [" ]* P1 J远程巡航速度,/ N: ~7 D3 Y3 h r/ [
一个与节省燃油有关的巡速度。在此巡航速度下,每
p7 O2 c% H0 t! j9 f一单位燃油所能飞的哩程,最大的燃油量航程小百分之( `3 f: ?) J# F
一。0 ^* s% f' {' R9 {3 w8 ]3 t
纵轴,' b0 A& a3 L9 Q( H) h; l
由机头至机尾贯穿机身重心的轴。
+ P9 I/ o2 n w' r, p J叶窗,3 w7 \6 b. k; v& o. [: |: ?
有多条缝的开口。& U+ g, u3 a/ ~4 @
LONG RANGE C' h& \8 s9 g3 x- [8 _' G+ _# i
a5 J1 n2 ^( R6 J2 j* |
m0 y1 q( y( u/ p7 ^- U
m7 Z( ?# t3 _" D3 W
L
* F+ R1 G' E2 P4 m* da
- [0 F u" U) `" h3 yLOST MOTION DEVICE, A mechanism which does
9 f7 x {! i) k9 soperate a component following initial movement of+ ]$ W$ j' H/ N
control input.
4 m( p% t7 ]' F7 y8 r0 cL* S$ v0 G" z9 {, _. ~
air.
$ K+ D9 ~* c, y' r; c8 R大梁,
1 }- R1 S4 V8 q6 |& ~6 w机身或短舱上水平方向的结构部件。
0 o$ E2 O7 ]+ s/ g; x6 l' ^) ]- K4 H航
' ^4 h+ ~- J, M% n比
4 z! v( p9 _5 W# y空回装置,
4 I0 }$ `8 k; k在控制输人初始动作后,即不再操作部件的机制。用于1 `8 l0 X* e4 [; e7 D" \7 A8 _, \
飞行操纵系统内,以防飞机指令互相牵制。
# Z) [7 [; n7 B百
7 Z! w9 c# x$ P* t) ~* Z. g让空气流通的
! ]. n7 o0 [ y' T6 E英汉对照民用航空词典B OEING
! i: f% Q4 r1 ~- kTECHNICAL DICTIONARY 969 d3 @) q' [& \. M8 j
LOW RANGE RADIO ALTIMETER, A system that
% ^/ m, j, i: p5 }6 {measures the vertical distance from the airplane to the
# S4 a# x4 Y7 z brrain.
4 o- r3 H& L8 J. j& h4 z+ a! O% ZRC, Stands for Long Range Cruise speed. Represents
9 i8 X' M! Z# N3 ^. f/ q2 ye typical cruise speed for a given jet airplane; usually+ H2 O3 @* s; x! v" Q2 Z
xpressed as a Mach number.' T7 |2 P& |! Z. Z$ }3 ^ [
RRA, SEE - LOW RANGE RADIO ALTIMETER
* Q( \( X. Q7 y7 sRU, SEE - LINE REPLACEABLE UNIT
+ Y! O* _9 ^5 ]0 r6 r1 @- v Nuce friction
7 j9 C( F# ~4 Z2 C- b4 Netween moving parts. It can be a natural or an artificial
, k E, v& n' } Qaterial.
, ?/ Y4 E' T: p" |3 {( E. sAC, SEE - MEAN AERODYNAMIC CHORD
* e+ z( W' T5 [# R+ N- j/ Eft's true* Y: y0 o: H$ {' N$ P
airspeed to the speed of sound at that point.2 d! _9 e; X* Q( B" w$ K1 N' h$ v
的系统。
$ W! V9 A- L& F M3 a2 O1 o- ]远程巡航速度的缩写。代表喷气式飞机常见的巡航速
# P7 ^+ N+ e5 |,通常以马赫数方式表示。9 @$ n9 V) ~( T& P& `- G
空无线电高度表,
: q; T+ s) U/ [1 N/ r! j7 kRadio Altimeter
5 P# T9 p, }5 R* [" ] S; ^# Nte
" S- O* H0 Q0 C+ FL- }# w/ B: v( f U: _3 \
th
, C1 |) k2 q: G$ i0 g8 we
3 X. }, k4 C2 p# {# Z* o! O- rL
1 b! v6 d9 p/ RL( ~, H8 N7 k: ~3 P- a% o
LUBRICANT, A substance used to red2 Y6 N" D; o5 C" f5 g) o" R
b
% T3 G: r9 m j d, ]( Tm
7 Z6 V; Z% f, |LVDT, SEE - LINEAR VARIABLE DIFFERENTIAL
8 W1 e3 v$ U, @8 k9 M# f' f7 pTRANSFORMER( q) H2 K% [* e8 d
M
, Q! X/ r) N) }% b' `M! X! L( Y2 p- b) f; Q
MACH NUMBER, The ratio of the aircra& k& J) n# `* ~
低空无线电高度表,
7 P. G% B: X8 i, p- T9 |1 K0 L一种测量飞机至地形的垂直距离
- Y. `) j+ S3 Q$ n/ C. Q$ m/ X# n远程巡航速度,8 X: f/ f Q _7 b; [
度8 _9 l* V6 ~' q% _6 G
低
+ Y# ]1 r+ o1 Y. R$ \3 t' q见Low Range .
$ B& P, x/ t: V# F: L- W线可换件,* B3 c/ I, n6 c) i
见Line Replaceable Unit
6 @5 P- k* o& O2 V1 L1 u/ X航
$ |+ e2 u5 K) p$ y- Q' o.
, O3 p/ Z9 y9 ?5 a" Z用于减轻运动物体之间产生的磨擦的物质。它可以是天1 I0 B& K- M8 l4 ?! a) t
的或人工制造的原料。. h, `- J9 W5 H
见Linear Variable Differential Transformer7 D+ Q9 i) u* w; ~* ~9 ~- D% \' a2 e' d
润滑剂,- E3 B6 u! O% V7 D$ p
然- c' \. R; B9 D+ P
线性可变差动变压器,
/ t$ U* O/ ?7 c" M.
1 r `- K5 [* {# G/ |均气动弦,6 c+ L) G4 w0 ~$ Z, {2 J& I" ^" R
见Mean Aerodynamic Chord
" S' s9 Q- a8 e$ o平
$ c. p e2 G5 L9 S4 n4 _6 A./ {0 P6 q4 |" `+ d* O1 b5 L
空速与该处音速之比。
; a0 ~& R& z) ?% O- N: V/ e马赫数,
$ b! L, n2 }7 D" ], ?飞机真- W$ F, q( H/ {- d' w- M
英汉对照民用航空词典B OEING& U: `4 H0 k0 K
TECHNICAL DICTIONARY 97
$ l8 c) i0 j4 c# t; LMACH TRIM, Correction to airplane attitude (nose up)
! e1 y4 ?/ k; z4 lduring flight at high speed by using the horizontal
2 \* l+ j0 }) B+ Btabilizer.4 F9 S, W( \5 M" W. ?8 T5 k
AGNETIC HEADING, The heading of the airplane/ y) t1 u# y* i# A: t, A
lative to magnetic north.
- n/ h) c* j6 sAGNETIC VARIATION (1), The difference between
9 f" A" ?$ T+ W; { Wagnetic and true north.7 R( x7 F7 o8 u7 X/ u$ x
north.+ C& s/ B; O K; l C1 R# G3 u2 x" z
here is a continuous small change of direction
; l, g e- r+ t p" j. tf lines of magnetic force over the surface of the earth ,
h1 K" c2 |, A3 }/ m. Pagnetic variation at most locations is not constant over
3 d5 ^$ W8 E- w4 e5 V9 t: Ong periods of time. Lines of equal magnetic variation
& v. l0 U7 H! D) ?8 oe. (see
3 X0 j0 `# C1 l$ Ptation Declination0 r2 Q4 U5 _5 t0 Q1 D- Z! b
s' I# e/ v# I% e5 Q% e
M
# ]2 D& k' e" q3 m+ Y# Ire
8 j' y) M- A: @3 Y7 RM
4 ^3 E5 b$ E% w* ]& R* z2 i" c; u7 hm+ I* l2 d8 V0 m {2 y% U2 w
MAGNETIC VARIATION (2), The orientation of a3 y) ]1 d* }, r+ l. Y9 @" z( r
horizontal magnetic compass with respect to true
; d `& q4 }5 x s( X2 h- W# ~- i+ ]- zBecause t
; M7 N8 |6 j7 z0 Yo/ c: G5 t$ A5 j5 ~ S3 |, w: ?1 ?
m4 M4 K3 P* v* a. S/ ~
lo/ H% W& z9 b6 R& \3 A+ F# w
(isogonics lines) are updated on Jeppesen charts every
3 N" i. ~* t% E& ]3 r0 Afive years in accord with worldwide practic
. H- G5 A' D- {$ H [S ).
7 @/ O5 j0 o" DMAIN ENGINE CONTROL, A component on the engine
+ A. h4 N1 u) Wration.; ?) g* ]! h! m: r+ `$ j- l) w
MAIN GEAR, The main wheels with the attachments for, @, ~8 j1 H8 l
supporting the airplane on the ground.% l* {) J3 j5 D# Q
MAINTENANCE, Work accomplished in support of the* O% s4 @ E! ]4 i; R6 J
structure and systems of an aircraft. It includes,
& C$ E0 R3 A) ^* m3 winspection, overhaul, repair, preservation and the
& l g% @7 K; T& Jreplacement of parts.
; ?6 K! ~2 Q. L$ b) E0 i" o马赫配平,
+ [! z# e4 x i& A8 h! q* G用水平安定面对高速飞行中的飞机的俯仰姿态所做的
/ a/ ?' B& k3 X j" B; Z2 R调整(机头朝上)。+ ^9 k; J Q/ ^! b
磁航向,2 J8 v2 \2 a+ P- @0 B
相对于磁北的飞机航向。9 H) L' ]5 X$ ]+ ^) [. V# F' q
磁差(1),9 t" }5 k5 D+ B; c/ H7 I- Z9 G) e2 ?
真北与磁北的差别。
8 [ z2 o, n& f1 i9 }# Y% @断的微量改变,磁偏角在长时间内多数是不一致的。每
$ b- P8 S- E; t' P, x五年Jeppesen手册会按照国际惯例校正等磁偏角线(等
/ f7 b) D; i" p5 A差线)。(见基点偏差)
6 b0 F& f* o8 `0 o+ G主起落架,0 J+ ?3 U4 H4 @1 J" B
用以在地面支撑飞机的主轮及其附件。5 \) Q6 a6 k4 c0 I5 ]* `" F
维修,
- p! r% j8 g* t! [# j在保障飞机系统和结构时所做的工作。包括检查,大修,
* E2 G0 Q& J A- A; J# f0 C. R修理,保养和部件更换。 H. @% d+ z9 Z' Z2 S
for controlling fuel flow for starting and engine ope; D8 W5 ]# i p/ A* P1 D7 q! z8 l
磁差(2),
, K! c; H% V& c1 N3 ?8 r8 I相对于真北的水平磁罗盘定位。因为地面的磁力线在作 V) g( J, u2 i, g L2 x- E- F5 s
不0 T$ M7 ^# U3 X
磁% B5 @; A0 R! O! `; P3 R% X
主发动机控制器,6 V5 \9 ^& S. r! _
发动机上为发动机起动和运转控制燃油流量的部件。
- h1 N ^0 E; Y! B英汉对照民用航空词典B OEING" P' I( S8 m4 F
TECHNICAL DICTIONARY 981 U* M \1 v; q
MANEUVER CAPABILITY, The ability of the aircraft to% p* i$ @ x# H- M, f- y
ertain load factor.
) l, a' N. e- O. u2 r) [MANEUVER MARGIN, The amount of residual
) L4 H/ s: i0 E& E i1 _/ J/ \aneuver capability present before the onset of buffet.
% v" U$ d4 J$ B$ Z0 ZMANIFOLD, A duct or chamber with several inlets and
) Z& q" z$ O1 S$ V1 m( M# E- Qoutlets for air or fluid distribution.0 u/ v- ^9 Y4 R6 z
the
6 r- m) K5 Z4 J7 H: F+ ] rlow of
7 ?$ b; |1 y; ne flight compartment. On specific
: B% T8 ^4 e$ F6 L# Pccasions it will provide conditioned air.5 c" v. x, n) E' w1 v, z
omponent by hand.
M0 b; A- g/ R& v* Y: p, ?6 N0 eMANUALS, Books with instructions for proper
! w# |! o/ Q2 Emaintenance and operation of the airplane systems.
* p& j$ e* r, |1 kMANUFACTURED RIVET HEAD, The head of a rivet: S# l' V& H9 ]' s# H1 ?
that was preformed during its manufacture (see upset9 q6 C6 b# R+ ?% v. w4 E. k
perform certain maneuvers up to a c! ]& U( ~! \% V# b0 d
m
# y I/ u S% M) m3 A- UMANIFOLD INTERCONNECT VALVE, A valve in0 E9 G4 R( z/ x( ~5 K7 k
equipment cooling system for providing a normal f
! r' e8 h) g( b: z1 Frecirculated air to th0 a. U4 W/ R7 S; H: I# l
o6 _, w! Q0 |3 J$ E$ T
MANUAL OPERATION, Method of operating a. B0 `6 q4 k6 s/ s* l$ x- K6 k
c4 C7 r) n8 \" _( e% P0 s
head).
m4 v+ b1 A/ {) `! PMASS, The quantity of matter in a body. It gives the
6 G& h# _, J8 ]9 xbody weight when it is exposed to gravity.# Y6 e* ^" A3 Z% F+ A2 u
机动能力," U% t9 B) q! H# E7 K
飞机完成装载系数达到一特定值的机动动作的能力。
& }' }1 o7 }1 w: |机动性余度,
" q1 A1 v# i5 q) G' z飞机在遭遇抖振之前,所剩的操纵能力的大小。3 v6 _$ |/ _ c
总管,& M+ }- c) H1 g3 ~- i
用以空气或液体分布的多进口和多出口的管道或容器。6 n" w3 {9 p# y7 T% z7 H
总管联接活门,, \1 t! |: M* E: M
设备冷却系统内的活门。用于向机舱提供正常再循环空
6 [% Q& P h$ b y" Y9 n气。在特殊情况下会供给空调空气。% t) j4 f1 E# W$ e% o. ?
人工操作,' P9 O0 N% t9 u
手工操纵部件的方法。 C2 t* q0 ]$ c' F* q z, o
明书。
, Z% U* @0 t h7 v铆钉头,
; x1 k3 B; ~6 R+ B5 g在铆钉制造时已定形的铆钉头。(见膨径头)。
" o9 [& S. R( p% r/ x质量,
& N C/ `( j$ z) b# A一件物体的物质数量。当该物体受到地球引力时质量产
9 K. @ R3 V! I/ `生重量。
% w. S& H5 w6 L* i. g, D% v. w* s手册,, J' b5 j7 S# @& I0 x
为能正确地维护和操作飞机系统而编写的说8 o4 D5 _9 T& S9 E, K; t
机械制造的
# S/ C2 E# y$ ^/ [英汉对照民用航空词典B OEING, K7 g6 J6 l# N& a& I2 s6 E
TECHNICAL DICTIONARY 99
4 C! j& h g+ h! a8 [1 x$ A& RMASS MEMORY, A memory that can store large
% X1 X, @8 i0 J. i7 j) Qamounts of information and hold that information C7 W& l" ?9 K7 y6 y" Y s. ~
permanently./ b6 M$ y2 w' k" b+ ]
AX CLIMB THRUST (MCT), Maximum engine thrust
: ?; Q7 s& ]/ xximum engine _% ]9 k& G" H2 F
rust to be used continuously when one engine is
# i* \! h: a) t# ^: h; X' Joperative.
6 }8 S) d7 I# d; sEOFF THRUST, Maximum engine thrust to be( h) u: p6 Y9 Y( `7 l: `$ b
used during takeoff.
0 S' y9 q+ Q5 y$ E8 u. ?FF WEIGHT, The maximum take off
/ E' Y# j( }* B! {) k1 Yweight as permitted structural limits or performance5 e; B* O2 Z- `' ^4 K
limits, whichever is lower.
3 G' e$ b, L" U' M7 MRANGE CRUISE (MRC), Cruise speed% m4 w% B: J* D" h" b
ance
2 i5 i; r+ q( I. \4 d2 vto locate
. w* ~- u$ i5 w x3 Jthe Center of Gravity.
: S+ I$ O; A( S: c1 \9 H4 M: e1 h主控台,6 @ r5 Z( d# m m) @
控制系统操作方式的装置或系统。
4 y% ? |- `; F. S大爬升推力(MCT),
, M. F9 F; E# `9 T飞机爬升期间所能用的最大发动机推力。# G+ F' i0 H8 r. ~
MCT),$ s+ I0 g1 F5 f& i+ N0 R
当一台发动机不工作时,可以连续不断地使用的最大发3 @% F! X& p3 H1 F
动机推力。7 U5 [( ?: y; s1 L+ b
起飞期间所能用的最大发动机推力。
7 U4 g. d1 i! ^$ v* H结构极限与性能极限两者中的小者许可的最大起飞重
1 ?. B' S; e% r$ ?* p。
. Y8 Q0 v# }( m3 m大航程巡航速度,
3 x- i+ k0 W5 e/ ?$ D* w最大的巡航速度。
& d: }2 f2 O, j' G* L- \平均气动弦,
3 q7 T& a6 F- I! }. c- X确定重心位置的基准
" F" y4 [% l* @9 }+ Q" t# a距离。5 `% b- C: C! j Y) L8 U+ v% V
MASTER, The device or system which controls the1 \/ k1 x* k7 p3 Y4 b0 B
system mode of operation.
4 \* i2 W* J( T# W3 OM1 \' R# S p! B
to be used during climb.
/ B& J; F1 F5 y' iMAX CONTINUOUS THRUST (MCT), Ma
; T' n4 |( q+ @( jth! K$ p9 A2 ?5 B1 Z2 g1 ~
in
* k3 [7 z! |0 T, k1 y& {0 v5 y! jMAX TAK
* Z+ F' P& V4 H- q0 P2 M+ GMAXIMUM TAKE-O
5 B0 w+ u% d. L1 wMAXIMUM' _' r9 O. M: D) R5 U
producing the greatest amount of range.: x& o$ A, R5 u7 r! n3 b
MEAN AERODYNAMIC CHORD, Reference dist- c5 c. S) \6 d) d1 c' a, ~
located at a fixed position on the aircraft used
. ]4 h8 a% i1 `大容量存储器,
1 Q6 S D X7 E5 v. F4 g可以储存并能永久保留大量信息的存储器。
! c2 y( W3 y. n6 e最
0 N, E# i3 l, ]0 c [. P. W最大连续推力(0 r1 O. [$ u# q @3 T4 D2 R; b
最大起飞推力,7 ^) f# b! Z$ W& g6 p9 h. X
最大起飞重量,
" l h4 @& N+ j' _" e: P量
+ Q) W1 _1 @4 }2 o) ~: n& H最
* `9 j; s( K+ z" ^! ?0 U' J能使飞机航程
/ m& X. p7 r4 T) U. s- D7 [位于飞机上一个固定位置,可用来9 N( k2 {1 D. A1 e
英汉对照民用航空词典B OEING
" p4 v+ F" W2 M& ATECHNICAL DICTIONARY 100# Z* ]6 Q9 {# C8 @: e
MEC (NO. 1), SEE - MAIN ENGINE CONTROL
6 l2 b- r* i. j' P- }% U; e6 }MEC (NO. 2), SEE - MAIN EQUIPMENT CENTER8 @; y0 H1 Z2 `# o8 `: b3 o2 {
EL, SEE - MINIMUM EQUIPMENT LIST
0 ?5 r e6 _5 c! d% utem the memory is where+ M9 u2 D9 h4 m( x' Y% c
formation is stored.
" _! O# O# E: |9 j, zMETER, Any mechanical or electrical device that is
7 |9 X; `) p& z7 f; x1 jair or. D1 P/ ^' }& F. }% {( _" U
point along the glide slope of an ILS approach. It is' H6 V3 c: {7 D7 v( L: _9 y/ B
normally located at or near the point of decision height.
& \# A5 V0 e$ Y& Y- h0 S: ^+ w,) D& [! e( g" z! r8 {4 Z4 \- C; z( s/ D
见Main Engine Control* J/ h B7 W- z. n- E3 N- E+ Z
M
9 s7 T+ ~, g2 X. c/ GMEMORY, In a digital sys- g. |, [6 T3 c' I
in
) J# E: P7 G; f2 L$ r; U% D+ Hused to record, indicate, measure or sense a specific( v- e) V7 j( r' }! A
portion of an operation.
; D; ]7 S( D' b" ~' }METERING VALVE, A valve for controlling flow of
& }3 y K" `) J4 Z. Zfluid.8 h# _( H% {3 [4 r! K
MICRON, A measurement of filter effectiveness, one
( G0 H7 s$ t E9 Z3 e5 {* @ @% Smicron equals one millionth (.000001) of a meter.
% R+ X1 C! s. ~MIDDLE MARKER, A marker beacon that defines a
6 j1 q' I' K8 S2 f& s5 u发动机主控制
. U6 Y& O6 X$ ^8 ?! A: u: X9 V.; s- p% W* w% f+ `8 C
设备中心: ]% R* E) R0 d0 t; P6 u
见Main Equipment Center, D) Q. W- j! H% s1 `5 q& _8 l
总$ h$ M/ U3 g: h# H
.3 v% W2 l* `. ?2 G7 p1 l
低设备清单,0 k4 g1 g0 N# Q4 f1 _% y
见Minimum Equipment List
( E8 F) [2 b. ?7 k0 Y K最
4 m) ^" b2 G$ d/ S# g. W9 \2 G7 }.
! G' i; M9 f. Q1 ~* V+ x在数字系统中储存信息的地方。
]: s" s$ A D) k- ^( k计量表," N; v' u- L( x" k
用于记录,指示,测量,或感受一操作过程的一个特殊
6 X8 w, S& z9 D9 P- e部份的任何一种机械或电子装置。
) j9 ], \! u# V5 r量活门,
& R, X4 @& ^! o( o8 P, P2 b i" [用来控制空气或液体流量的活门。
* h1 E) R' }7 H9 z$ S' g微米,
9 T2 c5 v# ]8 |# Y过滤器效率的计算单位。一微米等于百万分之一米。' s' R' Y2 H* z$ P, _" B3 x% j
在用仪表着陆系统着陆时,用来确定下滑道上一点的指& H; V3 j3 N0 d
点信标。它一般位于或靠近决断高度。
~4 @4 O/ u, ~) u& d1 C* k5 `存储器;
1 w9 V6 q& w" z/ N5 B3 _7 f计
2 `9 V$ ^5 _$ H$ b中指点标,
' J7 I+ f; z6 x: ]1 q英汉对照民用航空词典B OEING
w1 T- i; p& Q! p2 E6 u( a) cTECHNICAL DICTIONARY 101. g* [9 m1 I7 ^8 |% e# r
MICRO SWITCH, A miniature mechanical device that
9 j8 I$ e& @" w4 Jcompletes or breaks the current path.) b; c! i; p8 ~) b, W4 ~7 m
.' I' b$ Y. c" }$ _, s. u0 g6 @
MIL, One thousandth (.001) of an inch.6 Z2 P' W$ ]) r9 a% W9 @/ r/ P
ILLIBARS, A unit of barometric pressure equal to
% Z% c+ y- U2 f, x `/ p$ capproximately 0.75 millimeters of mercury.& H! ? `! c3 t: z* Y% d) {7 R
The lowest
4 k+ F/ M" t! l& m) rltitude to which a descent is authorized for a, v m1 R; L, _* `$ e, u
onprecision approach.) U) _/ M u& R i: u \' o- |
INIMUM ENROUTE ALTITUDE (MEA), The lowest
- E8 p8 E, f- }ublished altitude between radio fixes that meets
" V r* }% L( |4 [) V7 J. sbstacle clearance requirements between those fixes
/ Q# e# Z7 h7 X. M1 ]5 Kand in many countries assures acceptable navigational: I4 k9 S' N: I
signal coverage.
8 q8 B4 e% x: c9 v b4 u. noperation of the airplane with certain systems or
! w- P9 }+ z- }6 T" T7 {3 \" tsubsystems inoperative.
4 }6 u+ V: V' s0 m' h; {! _$ happroach0 E+ V9 p" \% c+ G" Q
cannot be completed to a landing and results in a Go-
9 p4 V' Z' z& tAround.
& \& A, R: C; F) C一个能形成或切断电流通路的特小型机械设备。
' B/ {$ P: K7 S3 }2 U0 f话筒,9 C3 M0 f5 i$ D" r& B/ B
话筒一字的缩写。
* x5 S) `" V8 _% s. x1 f" y7 t% C耳,
, L% b% ^: ? O l5 Z一英寸。
5 V6 }2 Q: j u, f( o k0 r4 m毫巴,
j7 N+ A; \1 {2 \# }: f2 R一个度量气压的单位,一毫巴约相当于0.75毫米汞柱。
7 e2 {; P- t' s+ t! w2 W) _ `低下降高度(MDA),
1 G5 K( K3 \' j* U飞机作非精密进近时所准许下降的最低高度。
. J( j, ^6 f6 G低航路高度(MEA),
% T F. f5 U+ ~& P在导航用无线电定位点之间,符合越障要求的已公布
; C' q- t: R* p9 Z8 [& v" t! |的最低高度。在许多国家,最低航路高度保障了合格导航& e1 f# T7 q; i
信号的接收范围。* h; O6 C( R: m# r0 }
最低设备清单,
! u( J$ a3 J) [何9 D( U4 r/ C$ f0 K [7 q7 c/ N
作飞机的文件。, {& d+ H. U: ^( [8 X5 h
复飞(MA or GA),
6 S: I* Q c$ K# s' ?8 E飞行员因未能完成仪表进近而导致复飞所采取的一个" @( C6 {/ L* {6 X, s" b
机动动作。
) ?( L( G2 P8 C$ ^8 CMIKE OR MIC, A shortened form of microphone
0 G" Z, _0 _3 U( {M
I: j$ w1 x9 j1 q- v aMINIMUM DESCENT ALTITUDE (MDA),: I/ Q ^& A2 ~3 r+ b
a9 F. ], e8 B0 [9 m# I- g5 x
n
* G7 w& P. y) ZM
4 e" ]3 e- s- d! Dp
1 A! h7 e# b- g+ a* Go' k! h c. r. o" V
MINIMUM EQUIPMENT LIST, Document prescribing
# P3 L/ K" s/ x7 Q# LMISSED APPROACH (MA or GA), A maneuver- V6 H) ?" r, X! P+ B1 X) P' l
conducted by the pilot when an instrument
3 W/ ^: A2 Q. _ c$ x微动电门,
- Z3 p) a: I" I密8 t0 L0 P; }8 c7 F: _; M
千分之
' Q/ Z. D {% d% h1 ~1 }& d) E最6 [; \! W3 F; j2 @
最; q; T3 h3 Q9 @2 {- P# a- m
指定飞机在某些系统或子系统不工作的情况下,如# n/ ^" S; O# G% b" l% p
操9 Q4 U' c( }, m) S, P2 \1 p7 w
英汉对照民用航空词典B OEING
+ A, O: S$ i1 `+ k4 xTECHNICAL DICTIONARY 1022 M) T: P l* Y0 E
MIX VALVE, A valve assembly with two or more
6 K7 ~2 a5 Y* k- [& |individual valves used for airflow distribution in air
2 ^5 _' t% u) l. _& |1 Jstem.5 d f+ b8 _' E$ O, e" r2 ]+ H
MMO, The maximum Mach number at which the aircraft
' q0 a7 ]6 | ~3 tMODE, A specific operating state or condition; i.e.,3 t, h: _5 ?2 E+ I2 b( d7 h. Y/ M) r
Autopilot mode, MAP mode, etc.
+ w$ E' A, ^. ]% g, `# qe
8 I; A& L9 N+ O5 [, @4 MMODULE, A housing that contains related system) n+ b) j; Y% g% y. M6 }% @
MONOCOQUE, A type of construction in which the5 O" F+ [$ ]9 M, N7 a9 H
ONOPOLE, A speed sensor that senses magnetic
, d" {, ~6 O& ^' f5 t! kpulses from a magnetic nut or gear teeth on a shaft.
/ k! C8 x9 c/ g5 E2 ?he controller.4 U) v- ]0 r9 y. c1 i
MOTOR OPERATED VALVE, A valve using an electric
) B* K/ @8 m! V9 Z0 f/ D8 @motor for opening, closing and modulation.
! x5 { I$ Q( }. _! k; k* `( T8 H个以上单
* U3 X, |* O* l/ H活门的活门组件。" y: L6 W W! Y9 V$ R
飞机可使用的最大马赫数。+ h4 a4 Q+ g1 s% w" x* y- B- B
式,MAP& z, @* b# [, i
方式等等。4 ?' c, ]( T+ T+ M, _
调制,5 Q, r! m. ~# J% B% d q
组合两个或两个以上的电子信号,使一个信号随其他信
5 a. T5 r: m7 t* Y5 p号的变化而变化。
) X9 s: r8 K% f. [9 H$ ~组件, L7 ^, {' `0 z" g" Q
极,
; Z* c2 X7 `$ v/ \: D帽或齿轮轴上的磁脉冲数的速度
) [4 Z w/ e' n/分钟。
# W0 t+ V& l* h. |. ]用电马达来开、关和调制的活门。
1 Z, r% M' j5 H |& ?, O) Z% |conditioning sy. A; _ F; O! b* I( p
may be operated.
0 N+ `2 M$ B: {# r7 s! ]) ZMODULATION, Combining two or more electrical
# y4 k3 m' K6 s6 b+ n" ~signals with the result that one signal is varied by th
: d& K& d5 i T$ G# l. [2 Eothers.
" ?; j8 V5 V' O& |( Q8 ccomponents.3 S( r& s& \4 T( k2 D8 V |& ^
fuselage skin carries all the loads.
- k0 \0 q0 D2 H* W" K @0 x6 AM
) }3 [" B: i# @; a+ n- \8 iThese pulses are interpreted as RPM by t
2 A6 i; O y2 M混合活门,
# B/ H! y3 h$ I( m( L在空调系统内.用以气流分布的具有两个或两2 I) b; ]! `4 j( w* X+ C6 c
体+ m+ S. K+ X( U, y2 M! p$ @6 w
MMO,
; C x* ~5 k5 d# M7 z方式,
A$ n! ~% n' n; w* a. A0 X: I+ w一个特定的工作状态或情况,如自动驾驶方
, G6 G+ p/ S: ]0 v4 `内装相关的系统部件的机体。) Z. C1 F; ?5 E8 V* j
硬壳式,: F1 `: G" M% U: Z" j/ ]8 \* F5 y# L4 _
机身蒙皮承担所有载荷的结构形式。; q$ h1 {4 C6 _7 ~! Z* v4 _
单6 U- x: p3 k, w' L. J2 L
一个能感应到磁螺
3 H9 S; L0 F) C感应器。这些脉冲可由控制器译成转
1 U3 Z4 ^2 I9 b4 ^9 l+ G' s马达操作活门,
9 p8 o( `! ]. O2 l- m英汉对照民用航空词典B OEING: L7 a2 W, f [3 ^$ Z4 U, d, T
TECHNICAL DICTIONARY 103
8 D8 _: d) ~: y% {* g, |2 @/ qMSL ALTITUDE, Altitude expressed in feet measured/ W5 r/ M+ t0 ^, W
om mean sea level.
8 z7 l2 G, @ @* K! R( R) nreducing the noise of the airflow through the pneumatic& Y. M- P; |$ q. ?1 y9 s
duct.6 O1 U* `# Q% ? ]
MULTIPLEXER, A device that allows two or more w$ m3 }; ?* b& R2 Y3 d( V
signals to be transmitted simultaneously on a single
! I( r% Z8 |7 m1 h7 acarrier wave, communications channel, or data bus.3 J1 _( U% A$ V5 T' W
essure compressor rotor.
; p( _) w* |3 |N1 BLOOM, A change in engine N1 and thrust indicated8 ?' e: J' X$ T
N1 gages and detected by the autothrottle BITE' T9 e& ~( Y* \2 s) Q$ R- U; w
during throttle hold operation.
+ n" Q, ], Z1 x( {; O- Q$ {N2 , High pressure compressor rotor speed.
- `$ W' Z5 w6 ~5 QACELLE, A streamlined enclosure on the wing or
/ T0 r7 C) A; b$ ^) M0 P; X, O面量起的高度。) d5 q4 u% Q5 X; [
经气源管道所生的噪音
7 h* f8 k" T# G A/ d$ n! [的装置。" ?7 [0 E8 y3 A8 h' ?
多路传输器,
7 b$ N; s9 f& M% {8 L" E. U一个能让两个或两个以上的信号同时在一道传送波,一
7 Q1 u% X4 [4 I( r) x条通讯线路,或一条资料数据总线上传递的设备。/ }3 F8 R0 i! |4 J
N1转子转速,5 r% q3 c; }6 Y
发动机低压压气机转子的转速。
1 v! [ y6 \3 b( M9 F0 q( Q! mN1激增,# N$ L( S' V& V- h2 @
油门保持过程中,在N1表上出现的由自动油门自检探
( o, t# t) ?8 E, A; p测到的发动机N1和推力的变化。
4 Z B* e, ], U: l" v1 l- Y" [N2转子转速,: a8 Q( M- h7 n, N" S
发动机高压压气机转子的转速。- {3 m: Y& o- O) @$ j8 x% ^3 M, d
短舱,& ?! H) b4 L& [
机翼或机身上为安装发动机而用的流线形壳体。' J4 C) K" @ v( C
fr9 V8 a0 w' t, ~
MUFFLER, A device in the pneumatic system for
% e7 C; C% `# J2 X( r. aN
5 T5 ~5 ?5 c7 S4 N9 _- ^8 S0 JN1 , Speed of the low pr
2 B* ~* {1 d. f7 H2 `4 Y5 |+ E( Lon the$ k! g2 g5 ~ ^) x7 S
N
- Y+ R: ]) o; j/ J* k% efuselage for the engine.
: l! k* _) J9 m, i6 s平均海拔高度,
3 [) T8 [* Y& G% d1 x以英尺为单位,由平均海平( i* ` g" {, K- `
消音器,
1 S" E3 Z( t* S1 f. Z在气源系统内,用以减低空气流; `9 y% k) x. X; d
英汉对照民用航空词典B OEING5 Z J0 }5 q( I. Z8 Z0 s5 c3 J! Y
TECHNICAL DICTIONARY 1045 }% G+ T- c) L" T
NAND GATE, An AND gate followed by an inverter to
6 u& K6 C& o9 F' Wform a binary circuit in which the output is logic 0 if all
! T# V! h) y x2 ^+ P) p* c* hputs are logic 1.2 H" M4 ]1 R( o& _
AUTICAL AIR MILES (NAM), The actual air distance* B2 |8 }% A$ M) j9 C* V* f/ ]
respect to a! I" \* s$ X" v" v5 k# N
tationary object.
# |- {/ n" W/ r7 p$ G+ iistance
8 i) W8 S2 i- |0 ~; Q1 ftravelled in relation to the ground expressed in nautical
7 s' u/ n9 y1 {+ E: omiles.
4 J) A3 U( c: ance equivalent to 6076.1 feet) w S L9 [: d0 ], A6 P
r 1852 meters.
6 K4 y+ R$ G; D- Q8 j" Lhical
7 ?# c3 n2 |# P3 r9 C( zEGATIVE LOGIC, A form of logic in which the more
5 D! F5 ^, e6 S/ V+ h" R6 ~negative level represents a logic 1.
1 v* A" X- N4 F- ~5 H' n) fEGATIVE RELIEF VALVE, A valve in the
6 o1 Q6 ?# P V q) n! t# B/ de to be! A. R' [+ o6 Z/ z/ {
above airplane altitude (or cabin pressure to be below
5 x" q# k) p, U- k/ Pambient pressure).
! g, u# g* q( S" L8 F有
! k) U' Z9 j' h; ^- V" q0 {& m/ l4 j人为逻辑1时,输出为逻辑0。" d6 a( W1 @( `) ~* A
海里(NAM),( t5 V" g5 A* Q; y e) _/ I
来表示的飞机在空中所飞过的实际空中飞行距) W0 N% e2 }. P' j' @- t
地面物体。% |( E6 X) x% g0 M# B9 V- J
以海里来表示的飞机相对于地面所飞过的距离。
% U4 F& B. F# T, \里,
/ W7 E+ D ]% ?* l相当于6076英尺或1852米的距离单位。" |' H. D( ?8 Q6 i0 |' x7 D, L6 E8 Q
导航,! ~- ^) F# H6 @8 M9 N
反逻辑,
+ M% c2 t) S% O8 u- W正电压水平越是代表逻辑0,负电压水平则越是代表逻' c4 W1 w2 w. N2 r1 m
释压活门,3 u2 S( p1 z% A/ p; [6 c+ g
增压系统内,用来防止机舱高度超过飞机高度(或机舱) M( [1 B' b- Y7 r3 E
压力低于外界大气压力)的活门。
7 a/ [+ T4 P: R! din7 E6 p c7 o: k' D
N
w8 p6 C- \0 f0 c6 L" q" o( Z9 r* vflow expressed in nautical miles without
* M& H5 q2 K$ O! n- }8 hs
0 s* T# }, |; r; n% w* a+ nNAUTICAL GROUND MILES (NGM), The d' T1 k7 l) C( H5 d8 F1 }) e
NAUTICAL MILE, A dista
4 ?0 Y3 n7 o7 Uo( D% S; a% f( a4 X1 F) h
NAVIGATION, The art of determining the geograp
/ B# U7 E: t" d+ bposition and maintaining desired direction of an aircraft
# d+ H" s9 E8 n l5 Prelative to the earth's surface.3 g+ ]" \) n7 C' }
N) b7 L$ g% [( j; K8 V# ~
positive voltage level represents logic 0 and the more
8 b! x6 Z' S1 W" A( JN
. N/ h' m& L$ Apressurization system for preventing cabin altitud
) o1 Q! X- s2 ~+ M7 U5 x' |非与门,0 w9 v1 J( y- s: t, ~( n
在与门后面紧跟着一个反向器的二进制电路,当所- T9 J |8 [2 _8 m& m
输
u% b- B4 x3 T& B$ J空
- _8 B8 k# ?5 E) i. b% _2 p( K以海里8 V7 a5 b! [1 y, B1 G' f, ^- H
离。空海里无需参考
7 g. d! b5 t+ F2 z' q* D; D& ?地海里(NGM),
1 i+ ~' P' f' G$ {6 y海 ~. N. A7 {+ r5 f) D8 j
决定飞机的地理位置和保持飞机相对于地球表面所希
& o; k+ h- O# k, H9 o望的方向的技术。. A8 d7 r0 [& r- s
辑1的一种逻辑形式。
( J* W2 P3 v) }9 [, G( Q& x' l负
* D8 P5 [( ?# W2 N: d r1 e英汉对照民用航空词典B OEING: G( b* y0 W( o) d1 m* s
TECHNICAL DICTIONARY 1053 R E O0 N) v* ?; ^( I
NEOPRENE, An oil and grease-resistant synthetic
/ S1 C: ^9 N4 ]* w/ Lrubber. Used mostly for seals and self lock nuts, etc.& D3 a, u) g; w# P$ f4 g
EUTRAL SHIFT SENSOR, A sensor used for
8 q+ V8 [' k7 D+ e( cNET PERFORMANCE, Aircraft gross performance1 Y7 \% H) V- E& r# N
calculation
- w L+ t3 N- D$ npurposes.! G; @% C+ S! a: |+ q" x
NICKEL-CADMIUM BATTERY, An electrical device for
7 @7 y% m9 x/ [) } }0 ~changing stored chemical energy into direct current.
8 Y, I' ` R R3 u2 P) w$ @, A2 @ses nickel hydroxide, cadmium hydroxide and' I/ g, y" p7 _) @
otassium hydroxide.
3 N/ o6 _. U. jNOBLE, A term used to explain the properties of some! n/ I! R) t4 x3 e {9 Z6 ~' W8 `1 I- q
lements that are chemically inert or inactive.& S0 X; T/ {. O* F. t4 ?% k
NOISE ABATEMENT PROCEDURE, A flight path and
# v& H: [; p! p2 {' F# plimb profile designed to limit noise in the airport area.2 V4 g: O6 J3 v$ K. N- g
construction. (Nomex is a trade name.)
. f0 t! I7 _. c# r3 [in only6 H5 n1 C) G# Z" A$ q9 |. x
one direction.
; {6 a* a. s0 h& _( U0 R3 \氯丁橡胶,, X; f& h) r' J& B' e, n& U# l1 |
一种耐油和油脂的合成橡胶。多用作密封装置或自锁螺) [! G$ z0 Y4 @4 V- O2 m5 }' h4 [
帽,等。8 K. J, b6 }9 }) n
立变换探测器,
' e. O9 h2 o* l用于探测升降舵和安定面配平状况的传感器。4 P6 @* W7 ]' N! R! b0 @
性能,+ s/ a# L" J; m/ A6 @: s
机总性能减去由当地有关单位为了使性能计算
; M1 u! C1 m0 ~较为保守所定的一个量后所得的性能。4 W! Y6 I! @: @4 F$ ^4 ~
为直流电的电器元件。它使用氢氧化5 k$ [7 g0 B& l: e! I+ i5 W
、氢氧化镉和氢氧化钾。) Q0 y p# Z6 [) W
性,% i6 ]! k1 Z7 p- d2 {. R: r
用于解释有些元素不易起化学作用的特性的名词。5 c3 o. [( }9 s9 j+ |( Y
低噪声程序,
/ F2 g" {1 D9 Z& P3 S一种为降低机场地区噪声而设计的飞行航迹和爬升剖) x- y$ l( X3 n: Q9 Q9 W0 P% _
。+ W F# i1 i. g7 T& y
是一种类似纸的材料,用以制作蜂窝结构。(NOMEX
% |' h$ d# [3 _1 `0 T; D% _6 l商品名)。/ K" ~: T# d/ j( }: R/ c
只允许向一个方向流动的活门。0 L+ f# N" C& k& n2 p
N0 f5 R* D! {/ t9 T: M. T
detecting the elevator and stabilizer trim condition.
# W, T: l5 m( d+ [! Mdegraded by an amount determined by the local8 G* @1 K# \- C3 I! G+ ~
governing agency for conservative
1 x" ?6 W5 w+ S" lU7 t! A: j Q# O
p# B! _" L- Q9 q+ l+ \7 n/ Q
e: o0 m* u; K n% T
c
8 F- p: R% e6 V: |& q: x/ g$ VNOMEX, Material similar to paper for honeycomb
3 \5 q+ x+ n: f6 a" C' A+ VNON-RETURN VALVE, A valve allowing flow
" s0 {7 E- r K- M中
. [# Y0 b! N$ o! U7 z4 C, k4 y净
o& p. t O2 U) r6 t( H以飞6 q$ Q. |7 A9 B, p
镍镉电瓶,
4 e/ q8 N5 c7 l将储存的化学能变0 c' k% u; \, E/ K1 D% o
镍
% x, a; \8 H' a惰
% B5 W) U1 `# d6 l' N1 e+ a降8 T' W T* E9 B4 m
面
/ K2 g8 x1 D2 H5 rNOMEX,. y7 \( `+ `" o" ^2 n8 J
是
' E- v! n# [: v* n单向活门,
9 ]) p$ [2 A( n, K英汉对照民用航空词典B OEING/ m% q6 U, C% ^, o
TECHNICAL DICTIONARY 106
- N# f3 l1 ?3 ^ f8 ~. M( sNONDIRECTIONAL BEACON (NDB), A radio beacon
/ c8 I& ]) f2 q( B9 [6 {which transmits nondirectional signals whereby the pilot- ~, E2 O8 r* Y. j7 p1 Z0 e
can use the ADF to determine his bearing to or from the# ^4 T' b+ G# l
station.
& G7 c5 Y5 B* P% p# L# q+ p( UONVOLATILE MEMORY, A type of memory which7 f' e W9 l2 ~' R/ _
does not lose its contents when power is removed.+ S7 Z+ r8 q4 m$ b$ n" K7 g
rm
& E, d, I3 Z# ^9 }4 Z% ~% ^binary circuit in which the output is logic 0 if any of the6 C" e8 A# f8 b/ n
inputs is logic 1.
8 ~1 G! h+ M$ R* A! O" mNOSE CONE, A device on the front of the engine that; k- s% Q1 [) C4 I' g7 U
guides airflow to the primary airflow path of the engine.
6 X: q& U( I2 M% L! e! Tthe nacelle for air inlet to6 _4 }' K8 o" _7 E* J
e engine.5 Z9 J0 A8 Z' Y/ W
OSE DOME, Front section of the engine for
$ d: [$ ~- _) E2 p6 p. \ }treamlining and directing airflow to the compressor.( f, \6 E0 s$ }8 l& N6 v( K2 V' P
),
; H+ \ M! ~5 }# C0 B能够用自$ p* F! ^- g% [8 I
定向仪(ADF)确定他的背台或向台方位。& i; s6 |3 E# E5 G
久性存储器,9 _# v* }" i0 t. n( y" \
在失去动力或电力时不会失去记忆内容的存储器。
; t2 Z; \, N ?7 }3 x8 x( M. n5 D在或门后面紧跟着一个反向器的二进制电路。当任何一8 z! W9 t, T& _) G* ]/ g4 d# i3 F
输人为逻辑1时,输出为逻辑0。
u. b U! e4 v& V7 f r9 v8 a: j6 g一个位于在发动机前端,用于引导气流通过发动机的主 h2 q- c* d% q8 ?+ H* v8 d
气流通道的装置。) T2 O2 r% c, v' g
引导空气进人发动机的短舱前段。& {) R6 ?% l% X/ [
部整流罩,( x1 P" J& z* g2 L1 [2 y
用以整流并引导气流进人压气机的发动机前段。
5 a- c4 y+ R% w9 `- eN
: b6 G, ^2 A4 gNOR GATE, An OR gate followed by an inverter to fo0 i+ Z5 |" [; _: d* H$ j/ o! v" X
a7 X1 [1 w3 f' S1 y, F; x4 V
NOSE COWL, Front section of" _% I* {/ k% [3 p6 ]
th @- Q; i U; s1 x2 @" r
N
j6 r( P2 Z: _9 X6 ms
, r5 j! _* L# n* A无方向信标(NDB
, ~0 g& Z# V! m发射无方向信号的无线电信标台。据此飞行员* s) n7 U" c, D& c0 i7 I& X
动( ]: k& E+ }* J! i ?
永
; n$ U. Y5 W V9 ]或非门,2 T8 T+ O6 Z3 C2 A% g3 F( b9 F
个
) c1 w- U0 y6 }) |进气整流锥,
2 H. q5 T8 S8 y前整流罩,! p( F# \ Q. F7 X+ F" q
头
# f3 b$ o9 j& p5 K英汉对照民用航空词典B OEING
+ \+ [" P8 q8 _* l( x% r8 f( n# z5 YTECHNICAL DICTIONARY 107. Z2 N: x! s5 m4 i9 a9 @; [- Q
NOSE GEAR, The front wheels with the attachments for6 i% p2 w4 g; U& g/ Q+ [
NOT, A binary circuit with a single output that is always/ p6 J' O- A0 g1 s
opposite of the single input. Also called an inverter.
+ F" t: }9 j" r1 l2 t, gtion that has the shape of a "V".
9 m; ~$ N3 `- Q$ v8 `* S9 E2 I B- Pt.& b$ ]& N% {5 E6 F, J! s5 @6 c
O-RING, A circular shaped rubber or synthetic material+ _4 b1 B g/ J c3 A! k
sealing device for pneumatic and hydraulic systems.4 P6 p' e: j" K) W
PERATURE
! I* l9 t1 f1 V& b8 ge
* v9 O9 w) _# C0 ~# cin the path of flight., n# _# G* M, `' d+ c3 [
OBSTACLE CLEARANCE, The process of flying the& Q. q) F5 s& N2 s1 V
aircraft over all obstructions under the flight path.
' t( }0 j3 e0 [$ `Which obstructions are considered and the amount of( N/ l+ P6 A6 Q2 n. ^
vertical altitude required above the obstructions are
5 ]$ ]# J z, idetermined by local regulatory agency.6 p- @! m# G6 n% x
非门,- n7 p! `* s2 g2 |+ e
带有始终与单一输人相反的单一输出。也称作反向器。# b0 F" r" _' e) w: g/ W! G6 z
一个“V”字形的缺口。
. u/ e1 G9 M8 M+ Y' b1 O" C' Y& \喷嘴,
- `$ x7 T7 b# [8 I形圈,
" c9 e) b6 E3 ] j- {' n用于气源和液压系统,圆形的橡胶或合成材料制成的密
+ i, p! P- @( T1 r$ S f封装置。
. _7 G. T' N. g/ { ^4 E: u; `外界大气温度,9 [: t% J6 d( {: ]
见Outside Air Temperature4 ^6 K4 D% W8 j+ B5 c9 ^" R
supporting the airplane on the ground.7 w4 I9 P5 K. a: W: J8 `! A& e$ R9 Q
NOTCH, An inden
' c3 K+ Q1 Z: ]/ Y7 J3 JNOZZLE, A shaped device for directing flow in a duc: \% z* O3 A- S( W( ^. m2 D
O
" T7 x9 c% ^" l6 hOAT, SEE - OUTSIDE AIR TEM
( C* A5 z' O# {0 G7 o3 TOBSTACLE, An obstruction protruding into the airspac
; A) _" ]" ~- r2 R% A前起落架,
8 g- q' t; c# A用以在地面支撑飞机的前轮及其附件。
/ s3 u3 z3 A- m) \% ^( ]1 N凹槽,# q4 L) C0 v1 B' l; Y# R4 c! k
引导管道内流动方向的具有特别形状的装置。
7 H) T3 I1 o, V! i7 P" [O v: n% o/ ?# C8 [% V8 a
.2 j9 X$ m$ ]! p1 [
越障,, l! c2 ]7 y/ v' T
道上所有障碍物的飞行过程。障碍物的选2 u; {0 ^& h; b+ Y
择和飞机距离障碍物的高度要求由当地有关管理机构决/ v& K; n! Z! E( P* H+ F
定。3 k$ P* O9 }7 G- d2 m& V1 I0 z
障碍物,. V: w# o' g' w8 @% r* v
进人飞行航径上空域里的障碍物。8 k* P% @6 n4 ]0 Q
飞机飞越其航( I; c/ \0 V9 N/ Q; W% G- S
英汉对照民用航空词典B OEING- s8 V: K' j; p6 Y$ S
TECHNICAL DICTIONARY 108
& P% A- J/ v/ ~% `9 b: AOEW, SEE - OPERATING EMPTY WEIGHT
8 J) Q8 X9 F5 u$ PFFSIDE, Opposite side.
) s; `: R5 {3 N5 w) {& KIL COOLER, A heat exchanger for cooling engine oil
& G6 E) [* B7 ]( l; J7 rby fuel flow or airflow.
; v( K1 O6 q1 }+ U2 X! }& [- gATOR, A device used to separate unwanted7 p: M M u- D. T; u) ^+ Y$ o7 h
ir from engine oil returning to a sump or oil tank.% A1 Q6 I$ m w" r+ ] j6 l
OIL STRAINER, Type of oil filter.
! w' k8 S1 v' _LEO STRUT, SEE - SHOCK STRUT. V) U! f6 w5 p: @
NSIDE, Same side.
1 F" T8 V/ R- G' i$ J( m- Rll weather navigation system.+ `! l+ I! @& G
ch is not
; l- q" c' o: Acontinuous from power supply to ground due to a break/ O* ~; H. a2 E
in the wiring or failure of a component.
8 Z) v( k, [! F见Operating Empty Weight
~% v) Q# t% M, k6 i9 XO
0 v, }& B$ C/ P( a8 OO
$ n, w! [0 c, W) j2 c) ?. ]OIL SEPAR
4 [/ p5 A+ T/ b$ P& Ca( v- P7 Y& F% U( a% n+ W. k+ k! _
O& H8 u, _+ R, L6 x/ x! S
O
9 \/ b; Y& t I9 q' d& p: }OMEGA NAVIGATION SYSTEM (ONS), A worldwide,
0 c5 Z! e. s; m+ s2 _8 ma- m+ `5 E7 q2 y
OPEN CIRCUIT, An electrical circuit whi4 Q" }! W* f& S4 ^0 { z' _5 B- o
使用空重,$ P. q- @6 i9 R7 A% u, [- {# A
.: W8 j( v2 {3 e4 f, ?
面,0 r8 D* Y5 k7 X7 k3 X! J: Y! |
油冷却器,
1 j( I' C" `# @3 T$ A# W5 v利用燃油或空气的流动来冷却发动机滑油的热交换器。9 j2 l* r/ c) @- n( O" e% W
油分离器,. S' G! J* _7 O g k7 t
一个能从回油槽或油箱发动机滑油中分离出不需要的
2 w4 J5 B: S( R5 G气的装置。
) v6 O/ y4 ]+ }5 W. a- c5 @/ R滑油筛,4 E* q% r* w7 v; x. f) R- {
滑油油滤的一种。- H9 Q+ B' a. b# p6 R" X
液减震支柱,0 v$ T. g0 M5 N
见Shock Strut
) @/ o1 ?& l$ e3 U- R反
( L; g' j0 M& M; P0 n8 b相反的一面。
1 J0 r8 R! j4 T0 Z滑
5 C( l0 ?$ ~6 B9 J) l滑1 O% x; D; M0 M6 ]0 g5 w! ]% N4 ^9 k
空8 s; f) w2 o8 s
油1 Y K, Y' l# K! R; e1 F5 @& C
.; g7 e7 d5 `4 T; e, X7 p% R
面,0 f6 s) v' u+ Y) s
相同的一面。
9 r- I4 J5 r. t6 `1 N7 S3 [/ H" N个全球范围内全天候的导航系统。
7 N1 t5 k- O: [' f' H# v# t或组件损坏而导致从电源到接地点之间
; M4 j) x& ?7 D0 X S0 R. p% E0 W不通的电路。' J4 p) D+ ]& p" v1 u/ O, \
同
& Z2 ] W. V4 `) i% k- l* M( X奥米加导航系统(ONS),- L9 r+ M6 D- w) Y8 k' _
一
0 Z; p- j! M- t0 m& ~+ j" |# g开路,& i9 M+ H; ?* d! v$ E6 r. o
由于线路中断2 V- u# A1 {+ U' W$ e
英汉对照民用航空词典B OEING* T1 W0 m% h3 x
TECHNICAL DICTIONARY 109
v. Q% A; Z) ~0 O% \5 _5 g* [OPERATING EMPTY WEIGHT (OEW), The weight of
, u, p! o$ X2 K3 Uan airplane fully serviced, including the crew but without/ t- \* |( B% e p0 L8 c9 K
fuel and payload.# ]) c) _: k, B
PERATING ENVELOPE, Defines the environmental5 M* N) b- o7 ~9 f+ E7 B
OPTIMUM ALTITUDE, The cruise altitude which results" z( b/ _/ M0 D! \+ a
in the best fuel mileage.
$ h) \8 f) T; D- i+ O3 U5 N: `OR GATE, A device or circuit with two or more inputs of: W0 Q3 T9 B- o
binary information and one output. The output is 1 when) c; k' Z4 w/ |9 L" A
any one or more of the inputs is 1. The output is 0 when
4 l+ e4 J3 {% \- b# _9 Rall of the inputs are 0.! o% k% X) g4 B! E6 y1 `
ORIFICE, A specified size hole in component for control
4 s @7 C" |% Z0 rof fluid flow from or to the component.
x/ k7 Z8 o; j4 s& \ORONASAL MASK, An oxygen mask covering only the
) L' d$ j! C/ D5 K; ?mouth and nose.
5 ?8 L6 c" @4 D: OOSCILLATE, To swing back and forth with a constant2 P& G9 y+ Q7 n9 p1 s5 [5 [- z
rhythm.# v; N6 J5 D1 C2 d# E2 L: |
使用空重(OEW),/ v' W, m D8 [* `) Y* A
使用包线,) J, L; W$ X5 }5 M* S6 `
确定飞机准予飞行的压力高度、温度和速度的环境极
) ~' P6 {; \& n3 `0 ^+ c5 N4 r. z或门,6 } ?, \* n; t3 W' V" t/ d9 A
具有两个或两个以上二进制信息输人,和一个输出的装& h6 A# k) ?1 m- J: H; j, V" g
置或电路。当输人端有一个或多个为逻辑1时,输出为逻& `8 x D: A# h* E! \
辑1;当输人端都为逻辑0时,输出为逻辑0。9 [" ?7 Y8 |) x$ X4 G0 |
量孔,+ C$ k$ H8 S- X
部件上用来控制流往或流出该部件的液流的尺寸已确5 ^3 ~5 Y# ^6 y! C9 k7 M
定的孔。' m4 W9 q/ l" q1 T7 ~
口鼻罩,
0 q; ?" ^4 g- u- G3 |仅罩住嘴和鼻子的氧气罩。
: w) }9 d/ m* }6 _% N振荡,
2 k2 R( T! J+ D' b以恒定节律作前后的摇摆。/ H) ?9 P% L- j) v. \) l% X/ h
O% g5 o$ a4 k+ E6 H! D+ r% K, ?
limits of pressure altitude, temperatures and speed
y; @- |; x& w2 L5 z8 Iwithin which the airplane is certified to operate.$ X+ q4 E% D ^9 I9 d0 O, [
一架勤务完毕的飞机,包括空勤人员,但不含燃油和业4 `8 Y& P- C. u! L; e3 l+ o
载的重量。
$ I3 b6 @4 I4 `0 c ?) S1 _限。
N2 [3 g/ [, w" O3 e5 O0 P最佳高度,
8 A i) C7 R+ S, @9 S可获得最佳燃油哩程的巡航高度。
: u. P9 |' n5 l% F" [& g英汉对照民用航空词典B OEING
. t% }" a; x4 d1 n4 UTECHNICAL DICTIONARY 110
, n% H p, q. ^/ }' B# {OUT OF DETENT, A condition away from neutral or a
1 }6 p3 S( A$ p5 m% qOUTER LOOP CONTROL, For autopilot operation this* s- z$ w1 \7 @$ W
is control of the airplane's flight path to a target.! D3 F* d |: h. P
Examples are control of heading, altitude, and vertical
+ x' R' A- I; q% L! Y3 C+ |speed." R( p+ w* R% l
UTER MARKER, A marker beacon located at or near M. V! _$ t$ g$ C
e glide slope intercept of an ILS approach. The OM is2 ]/ ~8 U. I: q+ J3 c$ m0 P# _9 b
normally located four to seven miles from the runway
# D0 @5 E8 U- K7 ]reshold on the extended centerline of the runway.
7 v1 O- ]4 a/ t2 JW VALVE, A valve in the fuselage for
3 \8 F" o( @# q: c$ u# Sg the airflow from the fuselage to ambient for
6 v2 _# i4 d4 Ration control.
( C: t2 o9 p, oUTPUT, An information signal going out of a system or
0 O i+ Q$ q& s7 Bpart of a system.
/ f) V0 S. k- i* `- v. B: VUTSIDE AIR TEMPERATURE (OAT), Ambient, or free
8 u- G( a) ~5 VOVERHAUL, To return an aircraft or one of its
! e0 w- c, c( DOVERRIDE, Operation of a component by a method& r& W8 O9 i+ L8 A
different from normal operation.
8 f. F- ?. D5 w+ w0 K5 M操纵杆离开中立或槽口位置的一种状态。
Y% a: b) f6 t制,7 G( @( b2 t0 `
航向,高度,和垂直速度的控制。 F: |& u" A4 w8 c# |6 m
指点标,0 |' ]4 m5 `, Z2 p" g2 u5 B* `
位于或靠近仪表着陆系统下滑道截获点的一个指点信
! f( l. b. l2 U( ]4 `标台。它通常位于跑道中心线延长线上距离跑道头4至7! o/ l2 J/ o" J; F
海里。
! u" b0 S2 k9 J7 ]0 N5 r流活门,
, Q' C$ U+ }# c8 j机身内用以控制从机身流向外界大气的气流以进行增
. k6 {! t. V9 @% ~6 B& h% H7 l控制的活门。" g5 r) q/ X. ?
输出,
0 }: r/ j+ T$ K9 ~! u从一个系统或系统的一部分出来的信息信号。
& N5 V7 {/ U, }: s8 y% l( ?界大气温度(OAT),; o6 l( k$ k6 f! _
外界环境温度或静止大气温度。1 N( Z+ e- y+ `. Q! q7 V3 F( B
修,# T3 k2 d* O; c. Q; ? R/ L! j
将飞机或飞机部件修整到近似全新或制造完成时的状/ K1 U/ F. p7 ]+ e# a
超控,8 @, Q1 M( E2 z2 Q" i
用不同于正常操作的方法来操作部件。( v& K) d' [; Z+ B2 E- u
notched position.
T' }2 p, Y* g+ a& P* {6 iO$ F1 R' T" |) o% R8 P; d
th, G$ x3 Z, s- x& n3 q' s
th
7 a. Q* }* h2 p( j. kOUTFLO
/ v* N$ d3 s% n# }controllin& M \: {3 O5 J& J6 _7 p
pressuriz, w3 C5 w' N' y% Z! f; W
O
" F) H; J- b; Q8 m8 V( ta
* R6 n' w. ?8 l& _1 I zO
: n* o- ?* S d/ t5 `9 ~+ j8 z# Gair static temperature.
0 i0 [3 y0 j' n" r2 vcomponents to a like-new or just manufactured8 W D6 [3 Z1 B0 f
condition.% S7 q1 Q4 ^# P0 |# r
脱离卡挡,
* [5 h" N8 I4 E k# s9 h/ H$ X外回路控8 t7 T* x9 ~- X8 o* @+ k6 {9 z
用于自动驾驶操作的对飞机飞往目标地的航径控制。例
9 E9 n: l" @" `如
' n* d$ r# C2 m! F; W远2 e! X8 W" U( {( d' ?' Z
外7 S. G% P+ y& G v5 y1 s
压
# S. a7 \* R/ U外
: o D+ e4 k: K* s: P翻
+ a+ Q1 @1 |8 L) ]) l( L* D: T态。( n, m( v. ^) T* m
英汉对照民用航空词典B OEING, h( F- B! k; R' C
TECHNICAL DICTIONARY 111
+ l( d% b! Y7 N4 L; q0 x. t8 J7 ^P
9 {- i% p4 K3 b9 G8 i5 A# o5 pACK VALVE, A valve for supplying air and controlling
6 J. n8 h; i6 [8 Umanifold to the air
4 w; C% p) v- p' W/ t5 uonditioning system.! O, W7 k$ y5 d& ?# y5 O; E
ll piece of any substance or" {7 N6 p8 | R% J3 a" \1 r9 V, ~
physical matter.
0 X6 x, Y" q8 r6 F' hh
( i I& t% u& @rovides flight crew and attendant announcements,% ]8 I4 Y9 z( e8 T3 o' [
oarding music, and chime signals to the passenger3 `) K! H% w% q7 j
cabin.
/ j2 N3 F' e, n, oASSENGER ENTERTAINMENT SYSTEM, A system
8 q5 t1 j* S0 A; ktertainment to
! d8 B& `1 u& ?) g3 Ue passengers.
6 I3 s7 e7 Q2 s9 ZPAYLOAD, That which is carried to the destination, D4 n/ Q4 s7 A' J! T+ [" X* N
uch as passengers, cargo, or mail.
' S4 @ z& t2 gCA, SEE - POWER CONTROL ACTUATOR0 ^( u+ ^, L$ K P5 V! T
PDCS, SEE - PERFORMANCE DATA COMPUTER: ]3 a8 Q- x6 z
SYSTEM- I M# i* r0 O. m# H
调组件活门,8 E0 G) ^: m4 N
由气源支管向空调系统供气并控制该气流的活门。
9 Z$ t0 [( G- H9 z# D任何物质或实体非常细小的一部份。
0 L A7 O- D" r; }旅客广播系统,
, }4 c' ~ o8 l! C' a/ H能使机组人员向客舱进行广播、播放音乐和发出谐音信; b$ f- N% p- Y/ N+ B4 g, n
的系统。
8 W, T7 |: S1 h) P a1 ]3 L客娱乐系统,
: H+ E" q$ y; D! a0 z频和/或视频娱乐服务的系统。
8 E! y j M2 m' t# T. } s7 ]由飞机送往目的地的载重,如乘客、货物或邮件。: C% Y# r& V. Y, B4 F# P
力控制作动筒,, |( `# A4 I3 k# N D- _3 J0 f
见Power Control Actuator! l( d* \/ D. ^1 G
P
) f2 l- A" z" r( r n' oair flow from the pneumatic5 [9 U! C4 K6 k9 w1 J
c
1 w0 ?! i& G6 X6 I& }; s2 oPARTICLE, A very sma
/ v5 P2 `% f! ~PASSENGER ADDRESS SYSTEM, A system whic
( I7 T0 @+ V& hp
8 [0 N5 U* M( c8 }3 S6 E$ @b
1 |8 {' R$ Y: F( oP
6 p, B& d* e2 d, J8 c( k* ]& I( cwhich can provide audio and/or video en4 t% t# l1 a8 \: ? A, @+ I: t4 n
th7 k, D7 T. D/ C+ `7 M/ P
s
3 i' p a4 n) C# H1 [) {& q9 bP
; i9 k$ I- P1 m& D8 P! s; |0 @: NPCU, SEE - POWER CONTROL UNIT/ q8 I2 {( w2 Z
空# f8 h' u" i* L6 S0 J6 ~
微粒,* a% ]! X. y6 j4 u( l
号+ ^( y) c& h/ r+ U/ i' F* s, Q
旅
6 R" h7 d, X9 x! z, C' V向旅客提供音
. X* R1 i* v+ j业载,
' |+ N6 d/ b3 U# l' {动
$ B8 ~1 m+ G- t) L2 M. ~.$ K* c% s9 L8 G9 \
Control Unit4 C4 | E7 L/ I( F7 I3 V
动力控制组件,, L Z/ x- h' c, f8 V
见Power .* [' g/ c- z- S
性能数据计算机系统,
, X7 E+ f. E1 Y S见Performance Data Computer System.
9 o1 Y" R* i U- E' ^7 [) _, M英汉对照民用航空词典B OEING. J9 o9 @ Z$ V+ h B: o1 L
TECHNICAL DICTIONARY 112 ~% a2 Y3 ^1 i, y
PEEN, To cause a more corrosion resistant surface by9 r, q: u" c$ Z6 y: o% y' h
multiple impacting it with a hard material such as steel$ k4 H* a! C8 c* s' [2 ]! U8 B3 X
pellets. Term for this is Shot Peening.3 X6 ~# Y- v8 M4 m6 o6 X
Defines a position on the aircraft relative to the mean
; X/ j# `0 e& F! U f d laerodynamic chord of the wing.
" X% M3 ]8 p2 M3 X' n9 x1 ~6 nr as a percentage of a fixed
6 k! |+ S& L; kmount rather than revolutions per unit time.
' b: o3 X- v4 f7 Uamount.) ]0 ^+ _4 ~( Q" [
ERFORMANCE DATA COMPUTER SYSTEM (PDC,2 C/ a6 }4 i. ~" Y4 U
PDCS), A device which provides data to achieve the
) P, D7 F. o( v& wmost efficient and economical operation of the airplane.- ?7 h B# E. i7 H: l
PHASE OF FLIGHT, A portion of flight specifically6 r, L' D: ]: V( i2 s0 f! L: N1 m
devoted to accomplishing such things as takeoff, climb,
( y7 i: E' m% y4 M6 F. j2 @cruise, descent or landing.
]% n; t6 V0 D( R/ [5 o; F- c这个过程名为喷丸硬化处理。
2 ~$ o3 ^, Q- x3 `$ d5 p0 F+ I平均气动弦百分比,# a* U3 ?- u9 O9 y
间转数来表示低2 G" {% J+ V0 A5 h
压压气机转子的转速。' f7 ^! W1 g) {- u
性能数据计算机系统(PDC,PDCS),) D( M! P/ l. `$ Q, |" M
一个能提供数据,使飞机达到最有效和最经济的操作的
: I% ?* E. [" ]- Q- a6 _/ a置。
* {3 R* ^1 [# Z: D7 u* V行阶段,& \+ P: Y$ V6 y$ B2 T" ^. {4 y
飞行中负有一定任务(如起飞、爬升、巡航、下降或/ Z1 X3 m9 {! [ o) @4 L0 ]( T6 u
份。
/ d. v' o2 X# I1 \: {PERCENT MEAN AERODYNAMIC CHORD (% MAC),
; @8 U9 g" n' z: _% jPERCENT N 1 , Expresses the speed of the low5 l* T1 \7 z) x& ^0 U N# c! Y* @
pressure compressor roto
) n' _& X- }- M$ ]; _- H Ua
# ]! A0 P' ]: ] |9 b* G4 zPERCENT N2 , Expresses the speed of the high9 {) j! T: U8 r* o' g
pressure compressor rotor as a percentage of a fixed
( M- O( b' G @$ W7 u2 ^P
; j( A4 U1 _" s喷九,
# W- [( E. |- \4 n6 M; d; l为形成防腐能力更强的表面,多次用诸如钢丸的坚硬材
: H V3 r# N6 @) _* c料冲击表面。1 V8 v6 E/ }" ~/ e6 E
用来确定飞机上一点相对于机翼平均气动弦的位置。
' U5 B' g" O) g, u# b! H+ Y0 g0 |N1百分数,
4 R0 c! k5 `6 `以一定量的百分比而不以每一单位时7 R1 @2 m$ |% K6 W
N2百分数,2 s- ?% Q9 @4 S
以一定量的百分比来表示高压压气机转子的转速。
3 u# }. X# d0 V7 D( ^装
$ F# ~: L1 x: n S3 H* G4 t飞
7 `, {- i5 T% o7 c5 x8 Z9 w& w8 T着陆)的部
$ i+ s" H- c' n* c7 T英汉对照民用航空词典B OEING
0 u c+ K; [% W& w9 ?TECHNICAL DICTIONARY 113& H) |+ Y7 D) C4 t% z
PHILLIPS HEAD SCREW, A cross point screw with two0 Y' T' K, ]: C% u& l4 P! q& A& o
en with a flat tipped Phillips head
' I' R# E4 G4 ?crewdriver (see Reed and Prince).
3 p- w$ }2 l) N: VITCH, The rotation of an airplane around its lateral
7 ^7 A6 c& }* |. V6 o# N9 k1 Nxis., {1 B1 s$ @; t4 J6 |- B
ne
3 _' Q2 C5 V6 yose up and down movement controlled by the, u7 z6 g; W, Z. z4 }- i* ^0 P0 {
levators (and stabilizer for trim).
& L) v# u8 S; e5 r- R9 |% s NITCH RATE, The rate at which the airplane moves in
5 w" x7 m9 M2 }0 }' L, ee pitch axis (nose up, nose down).
$ @8 }# {5 A& c. v/ l* j2 JTIC TUBE, A tube facing the airstream/ N/ I" h2 q7 d5 K8 n- f
hich measures ram and static pressure. Used by
( \* N+ m8 U6 u7 i' |, jirplane instruments. G* Z# e- i9 b4 T, X( L0 J
丝钉。由平
3 p4 k- S9 i. n4 m- n; W5 S/ G7 a十字头螺丝钻驱动。
% K/ |9 u1 x- `$ Y" v0 a8 t' k* j仰,
) z9 C8 R# V/ y) }8 D3 z2 j. R+ l飞机绕横轴运动而造成机头的上下运动。4 q/ A% P) I$ T
一侧通向另一侧的水平轴或横轴。升降舵控制" b& G5 }) x$ x# D0 r
头绕此轴作上下的运动。(水平安定面则用以配平。)/ p0 t' U" i D* B7 C
俯仰率,. O$ N6 S% R3 N
飞机绕俯仰轴运动(机头向上或向下)的速率。6 e4 d3 z# `: N' Z2 v; S
管,
2 f3 R/ X: i* v# j3 r$ G5 \开口面对气流以量取空气的总压和静压,供飞机仪表使
& v" E% N) _6 ~, m N, P4 v7 l8 p5 h的管道。 x e* Z/ ~9 I- M4 i, t
distinct tapers. Driv; X; K0 c# w1 O( z, y
s
/ p% c8 \2 z3 {P
8 b- `. @7 k9 ea
- O7 ^; [1 l. ^0 m7 g. z6 b- rPITCH AXIS, A horizontal or lateral axis passing; `* ]; R6 ~6 Z! M7 q
through the airplane from one side to the other. Airpla) m5 D) B( d# U2 `( T
n) I# {0 f; c/ J M1 i
e& B: u8 p% ]+ P+ b1 W
P
( u$ h+ ^3 I3 ~th% B( @* |, Z0 \; ]5 A. L
PITOT STA2 G6 N) {9 V" s! V
w
; J# ~5 b9 D' h# e& ya
7 O" Q% C# \) `7 H十字螺丝钉,( ]' ]9 b' I5 g8 N5 E, ?
螺丝的顶面有两个明显的锥形十字四槽的螺
3 w% E U k* h6 M1 s3 u7 B& \顶) G3 {4 X9 }9 x p
俯
' q" k9 B) q: R俯仰轴,: C6 Y/ h0 I% D- V) `( Z
从飞机5 @$ I0 c9 \; V5 X
机
* c. ^* h9 V1 J3 U总静压
. M+ p; E( R2 ?/ {2 o0 G' o用2 m7 M5 P7 z+ ]' e, B
英汉对照民用航空词典B OEING% H: v2 B1 d8 i/ I$ u; j
TECHNICAL DICTIONARY 114
6 j1 @! d6 Z7 ` [' E4 F GPITOT T' p, D3 F M, j1 u
measure
0 H$ C9 K1 R" k; ?7 f/ ?! R$ UUBE, A tube facing the airstream which. Z8 W# c0 s1 C/ O; Q* ^. W3 e6 l3 I
s ram pressure.
: [( l$ z$ ^ r1 O9 I: R% A% ~PLA, SEE - POWER LEVER ANGLE
. q- I( g9 S0 H& E, Kr
2 |5 F) J* J# V4 Q, T3 |e; P6 W3 b, P4 b9 K* z
LEXIGLAS, A registered trade name. A transparent( J' Y! c) g: G* n8 z2 X7 g
r any purpose.
; p v" ?( I# n1 K% ~. |$ `NEUDRAULIC, A system or process which is a
4 k/ W. `" R1 [& yres.9 W) a5 b# k* Y4 H! V- N/ w
PNEUMATIC (NO. 1), Cold air, controlled and/or/ k1 i8 ~3 [& f& ^2 C
pressurized.
6 I3 P0 @) E. P2 \5 t9 [托管,
9 q! \9 ?; Q& {6 W. ~面对气流以量取动压(冲压)的管子。
+ I5 M. n. r2 E* o; T) ?# v& b门杆角度,
" Y4 s* S/ O" R- E6 t6 Y9 e- x见Power Lever Angle
4 d( t$ X# n y, R; y; ]PLACARD, An attached sign providing information o
R( A4 P+ C3 B, ]- U$ k4 {instruction.
1 g' l& N1 w Q4 C; ^3 TPLENUM, An enlargement in a duct which changes th
: W! y, y" X2 K9 yflow characteristics of moving air. Used to remove
4 y: Z6 R7 t6 @6 Apulsations caused by variable airflow.
5 |4 e7 x3 N; n8 z" H7 |P
6 x( L9 _- q# M7 W, m0 yacrylic plastic material used for aircraft windshields and
: c' g1 A. A! \- ]! m# [0 p& dside windows. JARGON TERM - sheet plastic of several* y: ?' l0 I$ `3 J
types and used fo
/ N- S, w& h6 o+ [PMC, SEE - POWER MANAGEMENT CONTROL
( S/ }0 \" V( F- r1 \9 JP+ G- [2 y& f3 Z+ t, ?, o+ }8 L3 s
combination of hydraulic and pneumatic pressu
0 s4 d* T2 K0 a& ]* e K1 ^皮7 C- J& W! B- v% T2 T1 d
油
7 T+ z7 _* b+ b6 ?.
! t' S0 ` M. d' d: P, r脉动。
1 r Q0 ?4 H$ ~5 z% Y机玻璃,3 a+ A5 H2 p+ J. w2 J
名。是飞机风档与侧风档所用的透明丙
/ S: Q6 K7 y, {) Y7 v6 p p控制,
. `! K+ `! M1 L标牌,
, x6 G8 e% s! S! m X提供信息或说明的附贴标志。
! Y3 U5 |- v0 \( t M# R整流腔,
& O$ K& v+ B1 [. W9 b9 A9 X2 \管道中用以改变运动气流特性的扩大部份。用于消除可. m$ S% i0 M4 x O( V
变气流引起的
' |3 E% h; `2 Q" h$ Y$ G有. }9 g, ?& ^2 w" S1 A
是一个注册商品
4 H& d: S; F9 B/ c烯酸塑胶制品。行家称之为多用途化学合成胶片。
* D$ a4 q! ]0 V3 d- ^% G动力管理
, L) w; V0 r' f) t0 D见Power Management Control.3 f' O# `4 ~- Y# |4 W! A9 a
动液压,* i" y4 c* C4 |* V& B, j
推动的系统或过程。
" f& W1 A9 A4 \2 q, y1),
" `$ R( L5 Q6 c0 w: ?* m8 E。' B. k( |4 q% a7 d* h& ~) o
气' ~4 p4 v* U3 z" Q8 `
由液压和气压混合9 }, o, l: f- f. w+ N
压缩空气(NO.
% a/ Q& P6 |% W' F N+ s经控制和/或增压后的冷空气
* |. ^ D) H* v; b' ]% K! q B英汉对照民用航空词典B OEING
' E) u% b4 y a, e. KTECHNICAL DICTIONARY 115
. `* ^# q2 `9 I) \PNEUMATIC (NO. 2), Air, controlled and/or
v1 d6 m2 ^8 B4 D" C; M8 X6 a0 o# R Fpressurized.
/ V- d1 f' o* C3 X! yOP OUT INDICATOR, A device on a filter which/ j# H1 Q: I( ]( Y% v* p" ~
roughout a material.
0 ]4 m/ G, `4 y& \5 {6 p$ Tition.3 K9 d; d) } K; _2 R
POSITIVE, Definite and intentional.
. Q% v4 Q- U( J! t6 s+ t(No.2),
% y2 ]/ h2 J9 z& g出指示器,
/ ~ C9 o$ c* D/ q, q Y8 t到达一定的压差时,它会从壳体内
2 g6 b' G1 g* [- b- e指充满整个物体的细微小孔或空隙。8 {3 \& J) g: b6 S7 i
置基准的飞行管理计算机的一种操作。( a/ O( B1 h; x7 _
肯定的,+ K/ [; M6 F& K' ?+ V
一定而且有意的。 ?# v. \4 Q- t/ h
P& f& p- Q, G3 G& g* Q
protrudes from its housing when a specific differential
9 d9 `2 w$ k1 }1 Spressure is reached.$ s( Z; l9 C% r& V
POROSITY, The term for pores or small cavities6 R; b& @( O- M2 X6 E
th
9 g3 A5 K; s- B# n% GPOSITION SHIFT, An FMC operation used to change
9 @( c" M) a; W% I+ |, Vthe reference of present pos9 T# T9 B# K7 V- w/ Z- W. L1 s
压缩空气
- B( `5 O. r; u7 f5 M( \经控制和/或增压后的空气。6 k. |/ v" F" v( ]6 i7 G
弹, j. T7 h' m" ]$ o9 g
过滤器的一个装置。* u* m9 Q! L6 u; \& ], V
伸出来。9 i6 s1 L- G- B2 S
气孔,+ ~0 D9 ]* e5 J9 Y% n
移位,
: p+ [/ u/ B8 P9 z( J: B+ ~1 l用于改变现在位/ W+ n- \+ N6 q* B
英汉对照民用航空词典B OEING
2 ~! R4 D' Z6 w: n4 X9 L& }TECHNICAL DICTIONARY 116
- U A3 e! p# y( d5 _; S2 |3 OPOTENTIOMETER, An electrical device for changing
. t- B/ K O* E# pthe voltage supply to an electrical circuit component.+ `5 p' y2 M; h" I3 P
r( P8 h3 A: ]8 g
bly for operation of flight controls.
& t+ v2 u5 {# i0 o0 J3 d+ w2 r* cOWER LEVER ANGLE, The angular scale on the6 q7 u" b9 r: O) v. Y) O
main engine control for showing movement of the power; v- G) X3 l! P Y5 K
hrottle) lever.# ]2 n! b5 q/ a- T' s: \% N
OWER MANAGEMENT CONTROL, An electronic
1 Y- L4 [# {, V. rngine control.
3 S& _4 C/ J! P# i/ @+ `. g6 Q1 xOWER TRANSFER UNIT, A hydraulic motor/pump for
4 j( i8 z* x) u8 `. F( {upplying hydraulic power to components when normal
! w9 F( [8 X, ?+ |+ pRECOOLER, A heat exchanger in the pneumatic
, G1 n" t/ |2 Y) y. _7 z- s/ ~3 Llied3 s/ \. }, `: Q6 T0 v% x! p
作动筒,
9 `- i8 k0 ^1 @件,
0 x2 d- z- [& Q) L油门杆角度,1 |7 {/ i# \$ x6 ?
主发动机控制上用以指示油门杆运动的角刻度。
# L+ w! y# ~/ t- x+ @: }7 s动力管理控制,
9 J: b6 p1 W/ O, S3 n6 F/ p控制发动机的电子装置。# f+ }% R/ e5 ^' z; v, A5 m
力转换装置,
$ e! P: r3 {7 V1 `9 ~当无正常的液压来源可供使用时,用来向部件提供液压8 f; o b( B7 T4 [ K( [" s
马达/泵。
4 Y! O: E3 ?+ O1 x7 G冷器,
1 V# ]8 ]7 t" d中的一个热交换器。它将发动机引气冷却后. w9 ~! Y! u0 u# l7 I
供给气源总管。1 J% ^6 i) p1 V6 S2 v" z+ i
POWER CONTROL ACTUATOR, A hydraulic actuato
. O+ ?+ D D$ N$ S, P4 R# h3 }7 sassem
/ v- l8 ?5 }8 L' u$ wPOWER CONTROL UNIT, A hydraulic actuator$ [3 B9 g' y5 i0 Z. U( Y
assembly for operation of flight controls.+ R8 X) A" v8 R! a, D% L
P
6 }* @' J6 D4 h) ^1 n9 ](t
( R' `" D$ ]. Q, |P; l3 n7 O, g K" U( w
e# A& x1 p1 ]( Q$ m, v3 D
P; T- e! O! S# _. A8 e9 D2 m
s/ @$ m, [* Q7 Z2 T
supply is not available.- B, S0 B; F( V. M1 Y* ]1 V5 o
P
+ O$ \$ }6 R& g" w0 b: l ?/ S6 Lsystem for cooling engine bleed air before it is supp
/ l% b& L0 g+ C2 U [8 |) a2 wto the pneumatic manifold.
; @: I4 J. u+ u, g* b分压器,
% Y8 ~; H7 ^+ q& C. x用来改变向电路部件所提供之电压的电气装置。9 \% p0 s& Q J% I: V
动力控制
# ]& @ C3 F, @( I; n4 Q" L用以飞行操纵工作的液压作动筒组件。
0 U% Y5 g8 a6 J! ^动力控制组
/ m, C8 n3 Z/ V3 G. C1 t) F用以飞行操纵工作的液压作动筒组件。8 V% A; i p- h, c( F! m
动 B/ m& |, W0 V
动力的液压
/ n0 _, H- s. G% U! K预
8 `+ `5 q* E& J1 w# H. L2 [3 G: V- I在气源系统
# f' n. M8 z9 z6 S; V英汉对照民用航空词典B OEING
+ l) O; _$ U6 t6 a9 z. [: x( jTECHNICAL DICTIONARY 117
1 ^2 t% H; K% C) K2 nPRECISION APPROACH PROCEDURE, A standard
6 x" J2 R% B& {, J. U; w! Gedure in which an electronic
# F g" O: T& {$ ?) j. Clide slope/glide path is provided; e.g., ILS/MLS and L8 t9 |: {4 M% Y3 H
PAR.- V: f# d) U: ~' c+ i* o
RESSURE, Force per unit area usually measured in
3 k+ \" t% O( B9 P# ^ounds per square inch (psi).
( y7 E; K% ~+ q( \RESSURE ALTITUDE, The altitude displayed when
& F8 I- Y1 X+ {/ b" d; r0 Xe barometric pressure on the altimeter is set to 29.925 ^( j" ]. E, C- P9 B+ m2 g, Z
RESSURE REGULATING AND SHUTOFF VALVE, A
) t5 Y; O7 Z8 ^- Nalve in the pneumatic system for regulating bleed air7 s9 R" d) W- |1 t, J9 q, A0 i
pressure from the engine to the pneumatic manifold.+ w2 }( w! m' r4 C
RINTED CIRCUIT CARD, A plastic or fiberglass card
) q3 P1 ]) y8 j x; I8 D6 \9 p- Yith electronic components and copper strips forming a
. E3 |8 Q& H9 X; Dircuit.- d( T. i9 o. r1 M6 g
RIORITY VALVE, A valve in the hydraulic system for
# R& ~/ b2 p! u- w; [) I7 NROCEDURE TURN, A maneuver where it is
* i+ b8 ]9 s) q6 l0 c0 @$ ?lane
' ~+ }) U- p8 j5 @+ Iproach course.; ?4 k% j; S- v
精密进近程序,
6 S# v/ N- Q% d1 k己提供有电子下滑道/下滑航径的标准仪表进近程序。" A" L5 ^% X: n9 C9 ]
如:仪表着陆系统/微波着陆系统,以及精密进近雷达。
' J$ K4 r* y5 ^- P( u; c7 I压力,* m/ @/ {' D3 q, y, M6 r
单位面积上的力。通常用磅/平方英寸(psi)来度量。
$ c$ S+ l$ B& P( P" N( g# R压力高度,
* v. E# N: s$ ~2 R- i当高度表上的气压调至29.92英寸汞柱时显示的高度。
9 R: G, i6 c: I( a# _$ O& t力调节和关断活门," N+ Y" x5 K9 L0 b) s# T5 a$ E
气源系统中用以调节从发动机到气源总管的引气压力
' u, g/ a, _+ u1 I的活门。
2 z/ J' }3 x+ I# u' d# f刷电路板,
S! b/ `5 r+ i- h; m3 Q1 ^由电子部件和铜丝所组成电路的塑胶或纤维玻璃制
4 A5 ~/ Q' f$ Z# j5 s% N5 v薄板。+ a9 E$ V+ s5 i& g) U
先活门, P4 s& w! V9 I2 z7 {; }/ j
,用来使各部件照合适顺序操作的活门。- Q/ s ]0 k, T# l! d8 Y
序转弯,; `, e: K) R1 ^. R. o+ s4 c, G
后进近航道时所做的机动动作。
# q8 k( i( V1 a) x) q. rinstrument approach proc
; {* J+ B1 W; {g, v, n2 n Q+ X2 f! S2 D5 _8 J
P {6 K" ^$ ^: x; @# a1 X
p
, V7 B; F9 n! V* q7 {- ?: mP
9 S1 m- o9 c3 k( yth
0 l! G* N1 C4 c9 y6 S1 sinches of mercury.8 S/ x$ _/ v" G2 S6 [$ H8 `& Y2 A
P9 |: v# E) m% }* k4 R# W4 d' P% h. G
v8 X* v+ J! Y# m; X/ l: o( u& G
P: _5 d2 _. [& S3 l3 l* D0 u2 x
w
9 Y6 T, J; v, A8 f) ?c
2 C: K6 \& B. Y9 J- X- RP4 S/ E; P4 B: _) {- h# w% c
operation of components in proper sequence.- e' P7 O/ V; F
P Y' L X0 C8 `* M0 _, q& J
necessary to reverse direction to establish the airp7 X! t( a* O3 x8 k9 W2 f4 |
on the final ap
9 F: d0 W8 y: s' Q, Q q7 `' I压/ `% o6 l3 Y( W( C9 W
印
) t, S( X* m7 n$ M/ F优
3 |0 K+ w5 C6 M% z液压系统中; z) e. G8 E5 e* O. \1 I) `! J* C
程5 l% o; O6 J3 Z) F3 K* @
在飞机必须反向建立最) e, g/ y8 ]/ r3 ~5 |
英汉对照民用航空词典B OEING' F- z# C3 ^: q! n. r& H$ ]
TECHNICAL DICTIONARY 1182 o5 d* X; v+ ]4 K# x/ k2 ~0 Y
PROXIMITY SENSOR, An electromagnetic d
2 U" {6 Y& O9 L, s) b: f" l/ G+ h1 r0 Y3 psenses the po* h7 K: f' Q' @( y% V" B
evice that% ~5 ?+ e* f2 y
sition of a moving actuator. The sensor# [9 y. v+ [( O6 t
as two or three wires.
7 C' j! f4 ?; s+ Y* F( KROXIMITY SENSOR ACTUATOR, A steel plate
9 I1 z- x7 c8 V* N7 N. N% I/ `cated on a moving component for operation of
' `! i, t8 U9 r1 Z3 zroximity sensor.
# y7 U$ r5 D- G# r2 j! V5 U8 S" y' NROXIMITY SWITCH, A printed circuit card for
/ p4 D3 M' o- _- T1 s4 i6 S2 Xtransmitting sensor signals to indicating lights and7 l& q' T! q# h! ?, s [) ^
邻近传感器,0 H! X% p; M& A7 r$ b: K
能够感知运动中的作动筒位置的电磁装置。该传感器. w: z- S- H3 N" E) ]
有两或三根电线。1 ?; @" W" Q0 y. T9 I ~' b; g/ f' z
邻近传感器作动器,( r1 B/ @# H2 F" H) J
位于一个运动部件上,用以操作邻近传感器的钢板。1 g5 K/ p4 W5 i! ^1 t3 t
近电门,- {4 K$ z+ J* I2 Y
传感器信号传输给指示灯和电路的印刷电路板。
' @# n0 ]( Q( rh
1 f: s3 P0 J( f' @# `P- M1 k8 h9 J0 |" P4 V6 g( L E
lo+ K# _: i8 J8 K" }; u+ E6 H
p
) a" D! g. }+ b \: ~P$ t! L2 X3 H) Q1 \' t- x
circuits.4 ?+ |) n2 {* w" K3 h2 p- j
邻; a* F, j8 V* e
用以将+ V- v; U0 ]8 [( u2 t" g( x0 J
英汉对照民用航空词典B OEING. N+ @; O# W4 m |8 @
TECHNICAL DICTIONARY 119' Z. e# a! D9 @' b8 n$ e
PRSOV, SEE - PRESSURE REGULATING AND# g- x# R, }( h5 s% S L- `
SHUTOFF VALVE
! z# h$ w% M! R& l2 oTU, SEE - POWER TRANSFER UNIT
+ L, C6 Q) V) w. J' jremoval of dirt from the air cleaner.
K9 P8 R; i: Jn
( `. g% L! D7 G4 x. oQAD, SEE - QUICK-ATTACH-DETACH
! r* X; V! G; |ICK ENGINE CHANGE, k6 ?5 t1 I7 n: J; v! y/ E- b$ @$ |
height above airport elevation.# @ f6 W) r3 a
NE, Altimeter setting 29.92 inches of mercury, 1013.2" S5 z8 m9 Z& Z; E/ `% O2 V
QNH, Altimeter setting which causes altimeter to read/ Q' p& S |2 z8 H6 s+ Q
height above mean sea level.
G6 y; L0 W+ S ]- S4 m1 v( V活门,
- s0 m- `$ N! s+ z$ |- M$ eP" D% t' U: a; h, K
PURGE VALVE, A valve in the pneumatic system for0 K) T; A3 g3 P' m/ H9 u) _+ @0 o m% l
PYLON, A structural component for supporting a
6 @; C, |0 d2 `engine from the wing.( X* t" G* {5 `+ h/ _& K0 n
Q4 W$ W5 C* X- \9 Q
QEC, SEE - QU
, d9 ]' Z6 E x- W& d- AQFE, Altimeter setting which causes altimeter to read2 C4 r) Y9 w ~; L* ]1 P k* O
Q
3 W+ S+ r$ W0 g: ]" e; P! {Hectopascals or 1013.2 millibars.+ j" |. k0 Q0 ], K
调压和关断
- T% z! c; e7 x( F3 s9 j见Pressure Regulating and Shutoff Valve.
* y: Q4 a5 U {* |8 J) \动力转换装置,
1 A/ {# z" O. x; c1 S见Power Transfer Unit.
: Y) {# \: U; @, p# p7 ]气源系统中用以清除空气清洁器中之灰尘的活门。, ~4 W+ T: Q' E6 n2 y7 \
速装卸,0 `* O8 \2 V% `7 W G
见Quick-Attach-Detach
5 {1 O5 i5 o4 `4 T4 t除尘活门,
7 ]0 D1 S' Q$ D/ ~吊架,
1 u. b& F b q8 }用以从机翼支撑发动机的结构件。
' [( L- ^; u8 d快 Q/ {( L/ B( W1 |" E
.
- X6 E; F6 ?8 T: @( a7 y3 z" K* I见Quick Engine Change
2 p! u6 K) z: b+ W+ [) y& z* M快速更换发动机,
. f) O6 T5 U5 q3 L.
8 q( O! G" X$ d! X8 L+ b场面气压,
$ }+ @& F3 K/ G- ^/ g3 a+ f准高度表设定,
7 \5 a+ @8 Y6 I ]+ |1 b& F2英寸汞柱,1013.2百帕斯卡,或1013.2毫
$ z( R4 x7 g% P1 Y+ A修正海平面气压,# P/ P% ^6 M5 H5 _ s% A7 j
使高度表指示飞机距平均海平面之高度的高度表设定。
y0 E) N, c) O0 C" r) ^) v使高度表指示飞机距机场标高之高度的高度表设定。
& t! z) h+ q g2 C$ Z8 j标
; O& k- x9 w/ r) `29.9
% ?" C- W5 L- f; l巴的高度表设定。' s: X3 d' E, V) h1 p% I7 i* \; p! x
英汉对照民用航空词典B OEING* O" E/ H8 h2 l
TECHNICAL DICTIONARY 120
/ O6 u+ e- E; p# M/ a* H1 ?% pQUADRANT, A mechanical component shaped like a
7 R0 G7 {( q# O+ T8 G' z$ @quarter of circle for transmitting cable motion in airplane, R, `: \: P$ x7 A, k' B, j
QUENCH, A heat treating process to make the surface
; x/ F/ p6 D! G2 bof a metal hard. The metal is taken from the furnace and. D9 z6 e" h; x% [/ w6 Z
QUICK ENGINE CHANGE KIT, A collection of
6 D( z/ e6 H- `3 t2 Me engine positions of a particular model
3 x8 R O) w! n) firplane.
% _0 c3 x* H% B! v, o; d9 e2 Q5 Nng
2 K" y9 Y0 `# E' ?5 M. Baccessories (hydraulic pump, fuel pump, starter) to the
* N; x2 p. z( s7 E. nengine accessory gearbox.6 S U" K I/ P! w- ?, I$ l; V3 K" \& J
S, Established the
; t7 q0 S. P* B+ wminimum amount of time to cool the wheel brakes
4 @: y' _" O) N$ O" ?" Obefore the next take off is permitted.
7 M. r, f/ A/ P$ n5 {, d进油或水等液体中。# \0 h! ~9 l$ Z5 z, O% Y, h0 s
快速更换发动机成套设备,& X4 C4 I+ p/ H' u8 s" |
置的所有部件的集合。. B; R' [; r! o; a! r) S h/ K$ q) `
用以将附件(如液压泵,燃油泵,起动器等)接到发动 g5 }! ]0 T5 y- ?3 `2 j2 r
附件齿轮箱上的夹具。
1 z+ ^1 L& t5 W; k4 r9 D2 L' e快速周转极限,
3 ^' z; W; A0 w3 @, O在下一个起飞许可之前,已确定的飞机轮刹车的最少冷
- f4 [! V/ R2 U# T3 g7 p却时间。
% I& a9 M7 r& T+ s2 Q; C: Ucontrol systems.
7 P4 V: @2 q2 {# j% t" J2 I Xdipped in a liquid such as oil or water., U F4 b: J# q. X/ s% m \3 m
components allowing installation of a basic engine on to. A- f; q V& F( r' N
any of th3 v) B: C# D7 B+ C! U
a* ?* z5 d) d" m' ^4 }5 H
QUICK-ATTACH-DETACH, A clamp for attachi
7 n+ V3 V7 R, K0 aQUICK TURNAROUND LIMIT [* U! _0 @' b2 v
扇形盘,- m; @- N- K# O, A
飞机操纵系统内,用以传递操纵钢索运动的扇形(四
* m% Q4 N) M- \2 k分之一圆)机械部件。0 m0 U4 Q, u6 y$ Q
淬火,, P A: s# \2 a, E9 u
一种使金属表面硬化的热处理过程。钢铁从熔炉里被取
3 u5 Y9 o% P" S9 ~2 w2 J9 y: u出后再被泡
4 c/ \) t; R5 |* }2 S$ N用以快速地将一台基本发动机安装在一种机型的任何
/ R! {+ y, M7 u2 d发动机位
* V6 J% {% R" M! K# i: ]. b* W1 I快速装卸,
" {$ [# @; a: H0 ~. |9 o机6 y# x! O* B6 A9 L5 Q
英汉对照民用航空词典B OEING
2 H) s3 B( C. NTECHNICAL DICTIONARY 121& z3 X( c' p9 j2 s; z& K. l9 @3 ^5 o
QUIESCENT, Condition of an electrical circuit when no% V1 P5 }: j; _
RACK, A place for storage of modules in the
3 z3 I# T7 Q" L( \3 \* glectrical/electronic equipment compartment." b4 e1 l: n9 W& h) r( p
ADAR, A device which measures the time between the) z0 Z0 M" j% n( ^; S/ M/ R
transmission and reception of radio pulses and provides
0 b- z' V; o* Z5 a/ w- q4 Yinformation on range, azimuth, and/or elevation of
. v- B$ K" B2 }* Y6 \bjects in the path of the transmitted pulses.( r# G2 ~3 C" _2 ^. V7 J
om a( m9 O( i: U) j4 H9 v! J
ar. E3 [- G2 v- k! P+ r6 k- L
RADIO ALTITUDE (HEIGHT) (RA), The distance of an* C9 B$ ]& E; T0 }% J1 d
aircraft above the ground, as determined by a radio8 X w, F7 W5 Y6 l
altimeter system.! I. [! U) x8 P; q+ L: \$ [
RAM, SEE - RANDOM ACCESS MEMORY
% b ^# l z* A) D2 T6 sRAM AIR, Outside air that flows through heat# v' I* G- [1 [* @! d F
exchangers in the air conditioning packs.
( j7 a j! O- l支架,
; X8 q- R. D4 x$ }& R电气/电子设备舱内,用以存放组件的地方。
) S# z$ T3 Y$ j雷达,2 \+ t6 i& M6 H8 v4 Y! `
测量无线电脉冲从传输到接收所需的时间,并提供范9 Y2 \' I) t8 a; g' P% @; P: W, F
围,方位,和/或脉冲信号传输途径上物体标高的装置。& } V1 d$ K, [7 _; A" t7 [
由使用雷达的空中交通管制员给予飞行员的航向。" W1 O7 {8 u3 D5 W
施发射出来的磁方位线。
- }& v- ]$ b7 f P无线电高度(RA),* v% P P9 g1 \5 c6 V' p0 h
由无线电高度表系统测定的飞机与地面的距离。6 R0 C' E2 O4 F
随机存取存储器,
- I& H& {! V9 \( p: f$ u8 c见Random Access Memory
/ I, U6 {7 W! Dinput signal is applied to it.
! W) O4 n; d9 ^6 q; HR
% a* v3 n4 I4 v0 c* b0 Je
2 V( J) P$ G; F1 P- k# N$ bR
) r/ Y# [0 S: @; p! W% p1 ao
8 h* u* M0 H; ?' V- C# { A+ V" URADAR VECTORS, Headings given to the pilot fr
6 o4 u, G' [: `controller using rad9 x* E$ ]3 r1 k2 J$ E/ S
RADIAL, A magnetic bearing extending from a0 H0 g3 V! a/ w/ c+ e+ M0 A3 t2 S
VORNORTACITACAN navigation facility.1 N* A# n0 O7 ?. i3 a6 A
寂静状态,/ i' k- b: A' Y; R, W$ U W
电路上没有输人信号的状态。$ S# K d/ t" v! b
雷达引导,3 J# J0 a' y8 R5 |5 F
径向线,/ x' Z4 l: i' U$ L* @5 L
由甚高频全向信标/塔康联合定位/塔康系统导航设$ v& } e! @" {, j X1 G
冲压空气,
' M8 l- W4 E; F3 s流过空调组件热交换器的外界空气。
) Q d; d! s- R" f4 n; b3 Q" y4 m英汉对照民用航空词典B OEING
3 O6 F( k9 {3 D- u) c& uTECHNICAL DICTIONARY 122
: {* D$ q6 k+ e0 MRAM AIR TURBINE, A device which extends from the( ] w n" }9 k6 Z1 Z
, driven by outside airflow for
: e1 X1 `, P7 d+ g# A+ W+ A0 h. v: I- }mergency supply of hydraulic or electric power.: P$ q, v8 b% Y* V8 e
ANDOM ACCESS MEMORY, A type of memory in! h. o! d: [* |
data can be written into and read out of.
/ B9 K$ p2 `1 ~5 g3 T8 w2 v7 lused for short term memory.
& D3 J/ U6 n7 ~4 }AT, SEE - RAM AIR TURBINE) O9 r E$ R0 c* f' p
ATIO, A specific relationship between one number
! g" v+ E7 W: O; X: `alue and another.
: s; E/ b2 G4 E' BATIO CHANGER, A mechanical device for changing
! Z x% `' G" A" E$ @) q6 a6 n% Eutput speed or movement relative to input speed or& C; Z" P) I# w; u) H
AW DATA, Data from sensors not modified by the user
& [% J7 ]6 t" w0 V. C" v. m5 r况下提
0 }# r8 C: {, j, I3 j3 I液压或电源的装置。
- [) @; ]$ J- A5 {* J( x机存取存储器,8 P/ U+ g: h+ }+ I) {# H- h
一种可以将数据记载和读出的存储器。一般用作短期存
- H% `; e. J- H! L6 C9 r2 u。
$ g; @/ d3 {+ I9 k压空气涡轮,
1 u7 U# B- T: b$ H9 |" v3 c见Ram Air Turbine
m: Z+ O" j) {& g5 v( M. e9 Tside of the fuselage
1 W7 p; R: G( _2 Ve: }, W: O- m, k& s& A" I
R4 K @% B4 T6 R: s; m: ]2 x- Y
which the h, ~8 ?# t1 e: k' z; i
Normally% p& @: Y M* J/ w6 z
R3 p! O' p2 W& ]7 y" G* X* x. K9 Y+ C
R
2 r/ s6 m% j- n3 W( L: qv
/ z) b& `# b1 A2 i4 c3 _" I! P% jR
2 U8 f# a* X n( To
7 T1 i. `- I" [# ^% D% \movement.* y. W! l+ Z& D1 b( Q" t+ g
R
* R Y/ E* ^4 @7 F0 R2 \7 F6 ksystem.' D$ |2 f' Z# [6 N1 b3 _
冲压空气涡轮,+ R3 [( k, B) @, R5 W0 V) p, {
从机身一侧伸出,由外界气流驱动,以在紧急情
& p: X+ b, |: Q5 ?+ b9 k% f供
4 I4 A( F5 y3 h8 C随
! Y7 I0 k' q4 w! }储
3 K. d9 y3 x. ?7 q9 P冲! m: s' S1 G/ J) Q
.: t2 f! U5 n: }1 M: ?% j
比率,
# h" r& k" Z2 E8 M" [9 N一个数值与另一个数值之间的一种特殊关系。
4 d! Z3 N# v6 @6 z% G) f/ p率转换器,: w) M o& U* b2 N- t5 [
用以改变输出速度或运动与输人速度或运动之间比率8 h0 i. P) `& ?/ e5 |) e
始数据,: E1 m9 G* `9 @+ i! z) N5 g
任何修正的,由传感器得来的数据。
" \3 O8 E, b3 G# T! Y- `9 e& s比8 [* x: L$ z, n- n
的机械装置。
. p6 t, [: q; w4 U- l原3 c' a5 p' S& A/ F/ J( J* B4 @( O4 b
没有经使用系统作5 L! o0 B# |9 H3 ~1 P, s1 L
英汉对照民用航空词典B OEING( Q( t; b* O' v o; u4 y
TECHNICAL DICTIONARY 123' ^" |8 n$ \' s: R
READ-ONLY MEMORY, A memory unit in which) p" q% t/ {/ B+ H0 Y
the computer. Under normal conditions the stored; H* ?8 ?4 Z& {- Y
information cannot be changed.5 P7 g# S1 y+ ]: ^
ECEPTACLE, One half of a two-piece connector. It is1 n% M+ f4 k7 p/ t' B* D. C
usually mounted on a support, such as a panel.+ O; E' k6 W" P6 ~ U/ b- P; F
RECIRCULATED AIR, Conditioned air mixed with air
2 X3 M7 }! A0 }) k2 g; U+ ?* Dfrom the passenger compartment.
' q& E: H% l/ E1 |- k B6 r/ e6 Z0 |" eEDUCED THRUST, A thrust level less than maximum
/ P+ q+ G- l5 {) p: m" M9 Zrated thrust.0 b- |; b) |& h8 J3 b# Y1 j
EED AND PRINCE SCREW, A cross point screw with2 f/ m+ L0 t7 {( J) S- Q
a single straight line taper driven with a pointed tipped: Q( o& ]0 t5 P- e
ED SWITCH, A switch with two magnetic plates acting
$ \( {0 I# z! o0 r" A$ w, V* N$ }s contacts and operated by a magnet.6 {( n9 U+ b& \1 E9 H% H
只读存储器,
& C2 ~* @+ H! k含有由计算机永久存储着的指令或数据的存储器。在一+ J2 V1 ?, ^7 S3 ]8 M3 h8 f
作任何的修改。
& |& B4 q. U7 T6 Q插座,
, p X6 ]# T. N* I8 z3 j由两件组成的连接器的一半。常被安装在支架上。
8 v$ n/ s4 x! \7 r, r8 w% c如:仪表板。$ n- x7 N" i( [& Z
再循环空气,
5 F2 h, k* o+ P- Y; w6 ~5 y调制后的空气与客舱来的空气之混合。
B0 b+ C0 h, G& w, @6 `$ @, K- d) `7 i减推力,
& w3 i" o4 p' F# G, L6 e额定推力小的一个推力级。+ E( M$ d. }/ L4 Q, s* Y: i. q
十字螺丝钉,/ B9 J/ E: U, J0 m. c3 V
的,带有一条直线锥的十字, z5 d0 y; w- x; p2 O, }2 L/ E
舌簧电门, W. l5 {* P" V7 |
由一个磁体控制使两片磁片接触的电门。
+ m2 M% U/ ^0 c; G- u+ r* Rinstructions or data are permanently stored for use by8 h0 f* n! d+ [& q0 k' T' C3 J
R5 i0 L$ c. `( F8 \; A" e
R
; T7 J& T" w, h& k; ~% n' d" B5 @R
9 e8 a# W7 I4 Y6 Q( }) zReed and Prince screwdriver. (See Phillips Head.)
- b- E6 z0 W5 |: p+ K0 @R
% u5 b3 V: w$ B3 o) a& L5 ca( _9 _1 x% ]9 m0 |4 N
般情况下不能对存储信息' K; O* T4 ]& c- O4 i
比最大
: e8 `. T- @; c与尖头十字螺旋钻配套使用) j% w3 I1 F- R& w8 B# O0 D
头螺丝钉。- R& {: q4 G5 c9 s$ @
英汉对照民用航空词典B OEING
6 X z5 M1 r. B3 G' j) G2 b7 aTECHNICAL DICTIONARY 124
: w8 s* h1 j! t& G! YREFERENCE LINE, A line used in a chart as the4 m' t, j( Z3 e0 Q
starting point for applying corrections to chart input; g( y! [( K- w7 Q* }8 |; ^2 D- n
alues. One or more reference lines may be used in
5 H. v1 H' ]/ j: B+ G6 ~uccession.! J' A0 t* C. E5 e# H0 F# ^: }
D TAKEOFF, A takeoff which has been( d# g, h3 o4 e( `
.
4 ~ j& I4 v1 f+ FEGULATING VALVE, A valve for controlling pressure
% z# e8 m7 h h) Y w: yELAXED, The state of an electrical component or A- @3 \* b, Q$ l+ `$ I
witch that is deenergized.
. N0 t# T# z, e, oRELAY, A switching device in which the contacts are
) E" {2 [, u/ k5 R. U0 \9 ^9 V" x; s2 Jopened or closed in response to separate current or
/ _, i; K8 I8 |$ poltage.
& f# h% }4 u' {- M+ sRELIEF VALVE, A valve which prevents high pressure) o \" n; h. N: O* ^, A
a system by venting the system to ambient.1 |2 n* C0 u9 i( j7 z2 \
起点的线。使用时可用) i, \# j3 G) @7 p
条或连续使用多条。
& z6 `$ c3 A- S9 ^断起飞,: N3 o8 d0 Z* j" k' I e
离地前被停止的起飞。
2 D2 @+ ?6 n; c7 G! }节活门,9 q" u6 y6 P8 n4 G4 ~$ D: P$ g, _
制压力或流量的活门。
) P0 M8 M% ?$ V0 L" p放状态,
A0 I' M8 S- Y2 F2 @电器部件或电门处于关闭或没有通电的状态。 a. g4 n* o+ t7 O) G& m
继电器,9 _3 E& s# V! d) ^( C/ R
一种电门装置,其接触点随着单独的电流或电压开路或; v, X }& M3 I) B2 V. \
合。" Z7 k0 r: d C! I
释压活门,1 X) _9 B% Z, _) H0 o
通过将系统与外界相通,以防系统内压力过高的活门。
# @3 ^$ m. B# P! H# {v
; C& s7 n/ L5 u4 h- b" i6 Ys" f7 \; J& f* B$ R1 F" a
REFUSE
* e( F/ h2 s2 E" H: ustopped before the airplane lifts off the ground
) l; |- k0 f& `' B0 dR. d0 o% p+ @; w- Q
or flow.
! d r' m1 K q, U: aR
4 i' s* t' |( z3 U. `5 |s) T6 L( n$ C# g# [' p* j; G, j! J" A$ T
v
5 F' f0 [7 O. p7 }" ^/ hin6 B- ]. V7 g' {0 D! b6 x) {
基准线,# A# O" B- P5 n2 v
在图表中用作修正图表输人值的
- W. t$ x# T: \/ i6 ?9 Y5 a* D. z一# q7 S- a& ^- [& V
中
" P, b8 j" ^4 U在飞机; v: E9 q! h Y" V# F
调: w5 D( v/ [0 W$ ]7 ]* |
用以控7 ]; h$ ?: c- V% j0 ^
释
8 w( a4 \: L0 L) D闭: b' |+ C. J3 Y
英汉对照民用航空词典B OEING/ t( D# e: s: p: [9 d6 a+ d- r
TECHNICAL DICTIONARY 125
1 D/ K. [0 t- F$ ~& BRESERVES, The required fuel remaining on-board after1 l; q m% |6 D! a3 A4 q. g% D' _
ESERVOIR, A container for storage of fluid. j) p6 n `" N
ESTRICTOR, An orifice for reducing the flow and5 e, p, s& D) u/ o1 U+ }3 l
ressure of a fluid.
. Q$ c* W- a6 k( Y/ e& QESTRICTOR CHECK VALVE, Same as restrictor but: P/ |# k+ O# @! }4 Q" r
llowing flow in one direction only.
$ a c, f8 R8 E, G6 u! q, R& \decrease the
) T% h# J- |0 F0 ?/ P/ Wngine thrust to idle.! x1 l$ p& {5 V" [8 ^; G; j& d4 ^
REVERSION, To change to a pre-determined mode.
/ `+ |* a/ R9 }# T& s* Ectrical device for changing the
7 S( }1 X& j0 [: |sistance in an electrical circuit.
4 H6 E+ T( B+ ^3 C备用燃油,! m8 e* z5 o! v; J# E8 x; E
照规定,飞机在到达目标机场后,机上需要的剩余的燃
6 {0 {/ ~, h& I* n油。5 h3 g6 E! l# O
储液箱,
* T0 S: c! @+ B6 R& {+ Q用以储存液体的容器。
/ @5 ~4 T3 X# K6 c4 L# @限流器,
8 \' `- r) g# o) W用以减低液体流量和压力的量孔。
" L% A: ~! u' y% ^* w) w流单向活门,. M" ^$ e5 W `+ D7 Z
一个与限流器类似,但仅允许流体向单一方向流动的活
; _4 P# y" A* @门。: h% U& i7 |7 K, u- {# J
门,
1 {9 h! u+ r) F" d. G自动油门的一种方式、用于将发动机推力减小至慢车状
# d& d8 z& o, ]! R+ @6 {' S6 V。
& k) d! R* y& a' m改回到预定的方式。3 ] O' g( m. @' @+ }# A0 f7 Z
用以改变电路内电阻的电气装置。
' V5 t) h% y/ Y% W2 q; K7 ^arriving at the destination airport as determined by
A2 t/ E+ e- d, v: ?4 Dregulations.
# U& b4 y9 l% V1 p0 U4 @R7 i J# t& N$ d2 @) P( e+ u$ o
R- H" _8 k- c( g9 o2 P( u( @2 c
p/ {% H7 P6 E! S6 _
R
% O( w) t2 v$ Z V5 y, |8 Oa
. r; A; Q2 c( z/ a/ |1 L+ lRETARD, An autothrottle mode used to A [2 P+ m; n8 n
e6 o% ~# I& |, F, j/ E$ n% w
RHEOSTAT, An ele1 |% K: K1 E G- F7 E3 R
re2 {4 x) |# N! ]- ?
限
. c& S2 p) s, W9 {' X# z拉回油
' C, T% ^. l( F* d4 z态$ o- i! `; A: J* M
复原,! f3 }2 j7 W s7 m" E% f7 G& E$ z
变阻器,
, Q) f1 _$ a: H# c- D英汉对照民用航空词典B OEING
; `0 [& o& e9 h, s9 uTECHNICAL DICTIONARY 1262 D6 a% U+ M% H
RIB, A structural member of airfoil shape in wing,
7 u5 D% D. S+ \4 L) bstabilizer or control surface.2 m% r$ s0 i, ?4 ] {
IG PIN, A metal pin for inserting into a moveable
6 p: ^: K3 M# m6 Z' @omponent before adjusting the control cables and0 g6 n" ?$ `/ I* u0 v
nkage.
: x9 M" t, e& S( ~; GIGGING, An adjustment of airplane controls and doors6 F* ?/ _9 b5 V W2 L2 z! f( ]
r proper operation.
, r1 h. P# y7 f4 Q" \6 x* G5 yonditioned air supply to the passenger cabin.
- @" P! R# ?9 @9 Q. V* S装销,. H. p6 p! ~, W4 P
在调整操纵钢索和链系之前,插在可动部件内的金属& \8 @9 T. m- q5 n* Q
。
8 l# E/ z5 y+ H0 [# I, {( @4 M- z校装,+ p$ C- m( F. t9 _
使飞机操纵系统和舱门能正常工作而做的装配调整。/ K+ p2 q9 V( ~
空调系统中,将调节好的空气送到客舱的管道。
8 ~( k7 h% c' w6 P4 QR9 L& b u" `1 k) M' x
c
2 M+ a/ y7 s; h) R) Z4 Q5 f% q8 N; s Rli) X7 Y$ ~/ n- z: O
R
" I5 x2 }7 @0 X; `# vfo
# ^8 R7 M- j; V" E* G3 _2 r( F8 c# aRISER, A duct in the air conditioning system for7 r% a* V* s% f6 |# N1 Y, b7 j
c
% [0 ? [! G" S- W; N% P( B* ]2 z翼肋,) N# X7 E) B% F* x5 i. ?
机翼、安定面或操纵面内具有翼剖面形状的结构元件。% {1 I4 g( `5 ?
校4 l+ E7 O- q, X" u' {# t; ]
销( D7 c0 w: B# W/ a/ a4 S' F% N
立管," w3 }; X- O/ I- |7 E
英汉对照民用航空词典B OEING9 ~/ y* J: m1 `9 F$ y
TECHNICAL DICTIONARY 127
* F3 u* D4 ?( I! z# S0 TROD END (NO. 1), In a hydraulic actuator, referen
+ i2 z% X+ M) F- K) N. |6 c" O3 Gthe part opposite to the piston side of the actuator.6 i$ N E# x3 a( k/ r! p
ce to
2 B3 s( N: x! D: i& G$ A$ |8 d+ dD (NO. 2), A mechanical device usually a
* L5 i0 I5 u8 [) E3 a5 ~- l% Ibearing, clevis or similar component attached to the end3 S) X( x/ o2 A- V
of a link or push-pull type rod.
' c O; A$ p! n# N1 D* p6 ]% NOLL, The rotation of an airplane around its longitudinal, H. r+ d' j4 h) f0 t
axis.: d) G; U2 l D0 T2 C
OLL AXIS, SEE - LONGITUDINAL AXIS/ k( M( y _ `, K7 E6 E$ {6 w
连杆端,
( @; i2 x% d0 R# O$ U* B) x: Z! N7 a# k* u杠杆端,
) S$ D0 x @/ {8 ?一个连在活节连杆一端或推拉杆一端的通常是轴承,9 t6 a X8 A+ l8 l5 ~" Z+ a
吊环,或类似元件的机械装置。; n! ? \1 |& m
滚,: y4 ]5 Y8 J# S6 W* ^
飞机用纵轴作为旋转轴时的运动。
7 ~& o, O3 H3 e" n4 U! w& L) G' b横滚轴,# M a- h& I2 l& h
见Longitudinal Axis' e7 X8 }! l6 q/ q7 k! T/ t' F- _1 R
ROD EN# J# }; r1 l" n; M
R
6 q2 \" r1 m' c8 V4 y0 [R5 |3 `- R4 W1 I# ]
液压作动筒活塞连杆伸出的一端。
! l" z! p( V% x' S( V2 H横
# ]) A! t5 T3 O.: g. d4 @2 t1 z
英汉对照民用航空词典B OEING
7 V& `! O% F) [TECHNICAL DICTIONARY 128
8 q0 e( O& ]' ^/ }8 w8 B3 J+ |4 C3 iROLL RATE, The rate at which the airplane moves
1 r. M3 T4 ] ? Don the roll axis (wing up, wing down).
+ Y5 p: v6 I( I3 rOLLOUT, The final phase of landing where the
* w9 ~3 I% j7 x* P: S* ]1 G) hOTARY VARIABLE DIFFERENTIAL TRANSDUCER,
3 i6 e/ B! o9 M3 y& R+ dROTATE, A maneuver conducted during the takeoff9 ^5 O8 [+ |% {/ u- U x i
n
: I( Y# }& w( }raise the nose of the airplane into& W# S9 b9 ]' [
e air.: P1 ]- p; S, U$ P3 A7 G" F
OTOR, A rotating section of an engine (turbine,
3 L% O) e6 S* vompressor) or a generator.5 ]: c9 [. l& i. D% v/ }
ROUTE DISCONTINUITY, An FMC operational* b9 G8 P9 s' r3 O+ Z# \3 H- I
condition, in which parts of a route are not joined or* ~ ~3 A5 ?7 U% W4 w
connected.' Q4 L% S, @3 U: z5 R V* ~: p
ROUTE LEGS, The portion of a route which connects
' R) p. g+ I. l5 F5 z5 f; Ftwo way-points together.
% z5 K" W: Q2 @$ ]5 N7 Y: [陆滑跑,1 c. Z! U1 Z7 v8 e
的最后阶段。此时飞机在跑道上减速。
' S6 a/ p1 T0 n5 o,
! v) I( R" E- h9 @R+ m+ B8 z" @& i& \( @
airplane is slowing down on the runway.
. @, k- S. v8 G JROM, SEE - READ ONLY MEMORY
2 N `. d" b: @/ Z( V# E2 y% m- s% ~8 b# [R
0 b* @9 \( B; y: X9 e7 P4 c1 NA device with a rotary input and a linear response.; N0 x5 R% e1 }4 ~
ground roll. At the rotation speed, the pilot pulls back o
- i! U& c. @ o9 cthe control column to2 F: L& g8 F0 g5 X6 l: b& Y
th2 g$ X# e% x9 z& }9 R9 O
R
9 j# i+ R2 a2 R2 v Z2 G: mc+ U9 m5 e! g" X0 R5 |3 R
横滚率,
5 R$ m8 m9 {8 ^飞机绕横滚轴运动(机翼向上或向下)的速率。; O2 [8 v: m1 k
着; `& y) |* d1 w0 Z
飞机着陆0 j; ?/ ^5 L e) \0 S
只读存储器
' M& `- V$ x+ p/ ?# Y见Read Only Memory
' Z) c. T* t3 B4 L2 a" H0 E旋转可变差动传感器, L0 X0 T3 w. P( j- @8 G: n3 N
人和线性感应的装置。
# [& R8 S* n( k% U3 u8 V, x. R抬前轮,! e$ c4 k! d$ m
飞机在起飞滑跑期间所做的机动动作。在飞机达到抬前
9 P- _2 q. m3 O发动机(涡轮、压气机)或发电机的转动部份。! u2 F& z7 ?% s/ V. f
航路不连续,
; n( X$ `" _) h5 Y! C0 A, Z/ f一种飞行管理计算机的操作状况,航路有些部份不相连3 O9 g& A8 @' \, ]* e4 s
或不相通。
4 ?3 d7 `# F! b! k航路段,
* }% H- M& M: E; z' y" m' x7 ^- G* [将两个航路点连接起来的航路的一段。3 \7 h" O( g& C) t% j5 x
一个具有旋转输; @1 f6 l! u0 ?' Y2 y5 z- ]
轮速度时,飞行员向后带操纵杆,机头上仰,前轮离地。" h% G/ b" i. b5 w* D
转子,
3 _) [4 A/ s7 D9 d英汉对照民用航空词典B OEING8 S; I* `# o& T3 P
TECHNICAL DICTIONARY 129. \# w+ n0 c) ~ s0 f
RUDDER, A hinged moveable part on the trailing edge' H9 Z c4 i" t8 }4 k' p) c2 D
plane yaw (left and right)
1 i4 }& B8 x4 ]2 L- R0 N1 z" hontrol.- V `4 Z- X( g5 f
RUNWAY VISUAL RANGE (RVR), The horizontal8 I) }" X$ S3 W
a pilot can see down the runway when flying an
& ?1 F' q9 [) Kpproach. a8 t @: \6 Y0 F
of iron and iron containing metals.
& M1 h+ O! f: iis usually a reddish brown color.
2 k) i' ^9 M( z* y5 z2 ]: eIAL
; h: H% n" b0 N6 \8 j+ UTRANSDUCER/ I# J0 t# f& C' l1 q
S
5 f" y2 q) f L- d4 U2 J- WSAFETY RELIEF VALVE, A valve in the pressurization
( k; n9 }7 R: ^3 d' D2 L/ ssystem for reducing cabin pressure to a safe operating+ C9 e: K( q, F0 [9 e) [; T
pressure., X7 z+ ] R. F% |0 X& O% {
SAT, SEE - STATIC AIR TEMPERATURE
7 S7 j% b! d" b% _或向右)的可动部件。 y: U1 C8 ~; N3 {" w3 c# h
进场时,飞行员向跑道方向望去所能看到的水平距. K! K/ W. W" A# f$ X) b
。
5 I( Q. n& }. A铁和铁类物质的氧化物。常为褐红色。
* K+ X* k! {6 F6 A* }' B见Rotary Variable Differential Transducer
* ]3 S: k: g; A/ [of the vertical stabilizer for air
1 A& k" o/ U+ Y w. hc
6 _. ^) a* V7 Hdistance) B) [$ F! D% w* T. b$ B/ j+ j
a) _% m/ l2 F( K6 Y$ S Y8 H; f
RUST, The oxidation- O: ^) h$ q) u" s& L# p" t
It4 R( D) @1 b" A# f2 [& M
RVDT, SEE - ROTARY VARIABLE DIFFERENT/ @) [0 [' R5 V+ j! A+ L, E; e4 R
方向舵;
: e: F8 y3 ]5 y" N' l1 ~+ y铰连在垂直安定面后缘上,用以操纵飞机偏航(机头向. e6 m4 A5 L- L |
左
, ]/ p8 y5 t2 Q跑道视程(RVR),
3 F5 a( i. c6 d# w, R, N飞机
4 `3 j8 V* n$ u. B- z+ h. n; R: P8 B. i离6 H X9 y, G2 u
铁锈,4 T' x. @% ]7 U0 Y8 N
旋转可变差动传感器,
( d4 W4 |- j- L( r.1 Z" U, Y, y/ V5 h: J, v4 p4 m
安全释压活门,. a) ~6 T5 f% A* i6 m) d
在增压系统中,使座舱压力减低至一个安全的工作压力
Q0 W/ ?' Q+ l, F, y的活门。
# K/ {3 y% Y3 n; j! Z& T静温,
, U( [" s0 E$ r2 T, l- C见Static Air Temperature.
! B8 d4 J; B+ @- S英汉对照民用航空词典B OEING
9 H/ j4 E, O' n. |/ v xTECHNICAL DICTIONARY 130' y1 E% i) S" v% Q6 K
SCAVENGE, To remove oil from the engine bearings or# ^9 V1 n+ \2 f. R+ o5 Z! f
to remove water/fuel by a pump from a tank.# c! L+ R* p9 r0 S$ w1 J* {# Z% d
CHEDULE GENERATOR, An electronic component in) [6 X6 R3 O$ V8 [2 [1 l
e pressurization system for controlling the operation of( [! W' O0 |% K0 M
e outflow valve.
' e. H* F) X" y* gCHRAEDER VALVE, A valve for inflation of tires,5 ~( ~% l& ?* L
truts and accumulators and for pressurizing the water0 N B" p1 f6 _# I3 E# G
CR, SEE - SILICON CONTROLLED RECTIFIER( M5 u" f5 d# m s- w
CRATCH PAD, An area on the FMCS control display
$ w6 U2 s& m7 |: O6 x' Kunit used for showing characters activated by the
% ?2 E5 O* v9 Z% f/ _lphanumeric keys.
9 y, Q2 x: s) K8 `7 Y" E g BSCSI, SEE - SMALL COMPUTER SYSTEM
0 [& z; d$ [& q4 `; S% IINTERFACE
$ m5 ?# g+ T1 q; |7 J1 Z3 RSCUPPER, A shallow receptacle around a filler neck of
# ^* I* {& X9 H& c8 ~a liquid tank to catch any overflow or spillage from the! h3 f5 e$ S, g7 c
servicing operation. The scupper is normally fitted with a2 g& e) K3 U" O0 z1 ], l1 ~
drain overboard.. W) M& T" ]7 L3 \
SEA LEVEL, The standard datum plane from which
3 ~5 U% P" ?7 p. L b! N% ?% Z8 ` Waltitude is measured.* q% y+ c0 `1 i+ }
去油箱内的水和燃
\5 W, e7 r, u1 J' C* w6 V7 W。. U# W# j7 B$ w7 T+ p; c' B3 t) R
程序产生器,) |6 z5 c' O, Y& [, x0 X+ o9 x
在增压系统中,用来控制外流活门工作的电子部件。- R. R4 ~' \+ y+ B2 \! y$ f) ]
chraeder活门,
2 ~) k1 M3 S* y* V* MSchraeder公司出品的一种活门,用以为轮胎、减震支/ G5 R l$ U/ c4 |+ c/ `$ I, i5 J
充气,也用于从外面为水箱增压。) k4 J; Y( M9 a5 ~* s, D, i# p( \
可控整流器,0 `( p. Y6 O, P5 r$ J
见Silicon Controlled Rectifier' j# s& z/ |5 x
S
; \1 T1 J: K3 Jth
5 ]7 r' ?- X$ F% |: ^; q# z7 ^th0 l, h& P2 t1 |/ f- o! h% R
S
+ c! @8 L9 F% u8 u) e* {" t. h$ as
* g( y5 B' H5 z; ^) x) o4 n& Ntank from outside.2 q( s! O6 x5 r c5 M3 Q
S
1 ^4 D* {" E* Y1 M5 {S' X0 t0 L' G, u1 h' k# E
a( j: Z1 N( g9 w& [5 e
回油,$ n) G* n) B7 m' R" E5 l7 t% ^
除去发动机轴承的滑油,或用泵来除# p! k' J1 M7 n9 ]/ m0 @3 g
油
" P4 }4 l2 s! I- RS1 ]) {: h- W, z+ e/ @
柱和蓄压器
( c4 N5 F5 P7 @- w硅; S! L3 c. N" g, t
.
9 F( n6 g* E+ r! G稿栏,
: ^; V0 F! P/ UFMCS显示器上的一个区域,用于显示由宇母—数字键
7 c% a+ F- r a9 p激发的字符。& J0 B- u+ k! Y
小型计算机系统接口,0 [; l/ h8 `( y. A9 q# P
见Small Computer System Interface9 q+ l0 a8 D! Y/ \3 P
草
G0 {: U/ j4 K' U4 z# r- R盘: q- v5 K9 w- i
.
* u8 e3 p+ a; }6 S/ X# Y放泄孔,
. U4 ]5 V6 R. f' |: u! t6 x液体箱的加注咀边所装置的小型容器,用于接取勤务过
; ?. {( K2 D4 C8 x7 W程中任何溢流的液体。一般都装有通向机舱外的排泄管
' Y9 p% ?$ l3 y, N道。
0 d; S) P: Y4 V海平面,
7 A0 D# b6 k2 E0 b) s9 _用作高度测量基准的标准平面。
. }' K4 \1 ^0 P# \英汉对照民用航空词典B OEING% J/ G3 A% O Z
TECHNICAL DICTIONARY 1314 Z z1 a W* j, D9 K8 z
SEA LEVEL STATIC THRUST, Maximum rated power( Z0 o6 ]* |( G/ ~, q
produced by a stationary jet engine during ambient' h ~& Z- A! H, b9 V! x1 E. ~3 C }1 c
onditions at sea level.% p6 v, @; m0 a
s for
* d, I1 A* J/ ereventing air or fluid leakage.) U m( l6 k/ D2 u6 z
SECTOR, A given distance between two checkpoints in3 D( ]) ~ P; P2 d7 t' ?( S6 c( n
e flight plan.
: V- \, D/ r& @- C# HELCAL, SEE - SELECTIVE CALLING
7 v, S1 O" r( s+ ]SELECTIVE CALLING, A system that automatically
/ H. I% p$ ]: ~" B- ySELECTOR VALVE, A valve in the hydraulic system for
- I0 T( f2 f$ }0 W+ X u- Wo one side of the actuator! w+ f! E% r6 E( d) ]& {1 y; P
nd the other side to the return line.9 h$ d+ L# k7 t- U' S
力,8 _: E9 i" T8 h; z: x5 a4 X
在海平面环境状态(大气温度、压力)下,一台固定住
; G; n9 M: d7 o的喷气发动机所产生的最大推力。
- }: _0 P2 {2 B5 _! O2 E# I, R在两表面间防止空气或液体泄漏的元件。! \5 n2 U9 d% u3 r* T9 p8 g4 d
航段,$ T! y. N) [% y
飞行计划中,两个检查点之间的已知距离。7 F: O7 v/ q3 ]8 y. |% x3 C
择呼叫,
: I" ]9 C* f" G4 n" Y见Selective Calling
( X- T+ c9 C" K4 T! b7 M5 K+ y$ \c
: I9 Q6 g; |! ?: h! TSEAL, A component between two surface
6 ]1 ^: I" e3 ]p# v7 g) e k" p- X* x8 K
th- a& G* P( @& k4 |# w& }5 D5 I
S
2 L* _; O. V# yalerts the flight crew to a call from the airline ground' j! \0 L; v9 D- @0 p% U
station.
@6 a4 Z0 S+ x C* Sconnecting hydraulic supply t
0 U8 C+ j. Y& R. c4 M. ~9 b7 `/ _7 u4 ba# {8 | c# A' ^* q2 q3 k4 \
海平面静推
/ B' C4 K1 k! ] B3 F封严,# n# M+ _5 }* c+ @
选( k9 L$ ^9 F+ O2 E s4 ]- h
.
: ~8 p J% u! H0 t. G选择活门,
. N8 t- D4 Z5 e" Q6 |6 h0 U$ p0 \端连
0 X- k# _% L) r- }回油端的活门。" o4 [7 X4 W2 U1 i7 O
选择呼叫,
$ }) I B- K( Z1 Q- h& v一个能自动将航空公司地面站呼叫报知机组的系统。- Z! G7 C8 n4 ~
液压系统中,用于将液压源一端连接作动简,另一& _; u# z, _# `8 h
接
8 M1 E: [# y7 W: X, X& T' C英汉对照民用航空词典B
" M6 \( q) _3 V* Y- {6 USELF SEALING COUPLING, A connection between two! I( P5 P. c5 o5 Y3 B& o
fluid filled hoses for preventing fluid loss when the hoses
2 w3 F2 _; F6 A7 A4 o3 ?% F# T1 N1 Trated.
6 L' Y1 M5 `8 KSEMI-MONOCOQUE, Type of construction in which the: p8 C) ~$ [# ^; m3 `
SENSOR, An electrical device for detecting variable
3 @* O* A8 W" ?; v" C5 z- L) qENSOR ACTUATOR, A device for operating the4 A( O* T# L) K1 l$ {+ B) g
SERVO, An automatic control system which checks its( D. ?8 E) I G: V( }! y
gainst its input so as to achieve a desired8 }# R" u+ J5 ^: P& g
MED, Hydraulic pressure for the servo is
* Z0 t: ]6 E% ]- }; nresent to allow the servo to internally synchronize to
% [. h; [& L7 D9 ?0 ]e proper position, but the mechanical output of the/ l6 f% D: L5 k! K( r5 i7 M0 x8 J: q
ervo is not connected.
k" Y7 x" h+ A/ w) }% X: F自封接头,
* @, Q( |- V0 C5 E6 ~' ]活门堵住通道,自动封闭而不8 _1 [: S. |% M$ ]) N( A
让液体流出。
4 B4 Q, g, ]1 \* y" u j9 h半硬壳式结构,! @! U" u' s% h; `. L% D9 I
使蒙皮,长桁和隔框共同承受所有载荷的构造形式。
7 P7 w I$ k5 Q0 p, S" n/ X感器;4 m W! k2 L, ?/ v `% c; c
量状况并将结果以信号送至指示器和指示灯的7 y' a" T0 @5 t- v+ G) Y
电气装置。! P5 n! X" E5 R3 K
传感器致动器,
. ?4 {3 s* m8 {。, E: k0 G9 [: b( a- q
伺服系统,
& w' j. ?" r# ]5 A+ w/ \: ^能检查输出和输人数据,以便合适调控的自动控制系
3 H% P* A0 r* r- f6 _+ f+ F统。
; r1 I0 ^ D( ]; v0 i0 r伺服预位,% y& q) ]/ p" U7 M: s
液压使伺服系统内部同步至适当的位置,但伺服系统的5 r I6 J2 r- S/ E0 }5 B
机械输出还没有接通。% ]0 p( J3 l8 i* i+ x$ W
are sepa8 a) N4 |; ~ e) G) X! y3 K* x0 B
skin, stringers and frames carry all the loads.- w- i8 y5 `( w
conditions and sending a signal to indicators and lights.3 J, k' r/ Z% `2 D# N1 ~
S
1 _( R# k& l4 v$ ?$ |sensor.
" s/ j% w8 M$ a* y1 `output a$ U; t4 u3 g: f% T {
control.
1 f2 y1 C7 x- w' u2 ?% xOEING
3 N. _0 ~0 w, `+ }6 S7 L( E% ITECHNICAL DICTIONARY 132( V8 o4 z# |, }0 t8 E3 `1 J
SERVO AR# w# ~' C5 D, n
p8 f7 Z2 W* z6 l: g- C' `% }& k
th9 U! o5 k$ L f2 O) |; D
s/ A. }% ?& l8 O0 X( J- j
用以连接两个充满液体的软管的特制接头。在两个管子
5 F. ]( J9 C( V分开时,接头内的弹簧即使
5 l7 } v! s; N* K* [; ^传
. p0 m- {: b5 T& h) R5 Q检测变
, p: U6 r5 i& M7 r* _8 T3 n" r/ F# o用以操作传感器的装置
6 a6 m, H4 B$ b2 {' R英汉对照民用航空词典B OEING
4 e/ Y/ o9 s* N2 B# ~! ]TECHNICAL DICTIONARY 133
' R6 p* ^6 m+ J) P X) ]! XSERVO ENGAGED, The mechanical output of the
- X* k$ ?. p* q8 w4 R: }( n# B6 Dservo is connected and the servo can move a surface or
2 @8 p! t( m* }. |0 A" O, n% Control
& V& Q2 D1 h( |, @SET SCREW, A small screw (usually headless) used to
; x0 Z9 y% I- O9 e9 s3 u% x' A- M* Deel, or knob onto a shaft and prevent
+ f$ C) l$ [0 a. z' Itation.8 `* h* f5 \6 m9 d2 U S) C9 t6 s
SHEAR, The stress exerted on a material or, assembly
8 N& Z' ]& ?" c- Q0 h4 i! F8 F$ Q: nwhich tends to slide the mating surfaces parallel to each
( R: `/ B2 R1 [5 Y1 Rther.: {- [ G8 w* C) d- r/ s( g4 M
SHIMMY, Rapid oscillations (left-right) of the landing
6 A! D2 u8 x- o3 B/ q- rear wheels.
0 r8 Y; D# r* N& g预位,7 n5 y; [9 {$ ~! Q% {/ B# \
伺服系统的机械输出与伺服系统已接通,伺服系统可移
/ A2 ]* f. e4 Z5 C" |动一个平面或操纵。
: L/ k- [+ a) t B5 i+ `. x小螺丝钉(一般是没有钉头的)用于将滑轮,车轮,或
; _6 ~. J2 o' D! G钮紧固在轴轮上被免转动。
; T2 @ ^5 ~8 O0 ^c
( V7 ]7 b! s& p$ V+ i. xfasten a pulley, wh; h' e. Y3 l0 H7 L6 \6 D
ro
3 q( M4 d1 n# j4 M( ASG, SEE - SYMBOL GENERATOR
+ B9 P$ \1 q9 p) ho1 p" l7 P4 |3 W: o, N
g
$ i/ x8 v- [+ ~% O3 f伺服系统
7 t1 e2 j6 p" g9 s% k定位螺丝钉,
+ U, R# B0 s2 H6 R" V% ?/ T旋, Q6 Q) S3 o# G, R( P
符号发生器,% X% Z7 b2 g+ z6 [; M% p2 |: B, y
见Symbol Generator.
, H- u. m& T2 P- }: u$ d7 S剪切力,
- M g: C9 @" E K6 G: _加在材料或组件上的应力。该力往往导致互相平行的成# G7 W5 a6 c) X* e: z
对表面滑动。
/ ?1 q, E u* f* W% e摆振,& H' z$ c- H% ?1 A4 c7 ? _: v. J5 T" j
起落架轮子的快速的左右摆动。
& M5 T& i, ]8 g3 t! N) w: j英汉对照民用航空词典B OEING x; b' U; X9 Y4 x& a) _
TECHNICAL DICTIONARY 1345 b& p, }( {$ |7 J% N
SHIMMY DAMPER, A hydraulic device for damping! g3 \7 R3 ~( _! i9 r2 f
shimmy in the landing gear wheels.. j2 R) r# e$ v+ N
ar for2 B: V% h; c2 s0 i3 C8 r; w
sferring oil from one9 E& u3 R, k6 A* [+ ^9 N6 z
chamber to another through a metering valve.6 e" q3 s- a! T, L5 n$ u- X
,) x. Q7 _% f7 }7 c3 V
一室以减
: L- B3 o/ z) t9 R* y着陆时产生的冲击震动的部件。
$ H, e1 f, d& k1 E1 WSHOCK STRUT, A component in the landing ge {0 }) s4 y9 k3 R
absorbing landing shock by tran
9 K' |* Z8 q: [1 x# e减摆器,
$ w( D1 f1 k m- k0 m% N用以缓冲起落架轮子摆振的液压装置。; u K* a/ X5 P( v4 T6 B& l! V2 J
减震支柱# t7 B4 p/ f5 t
起落架上通过计量活门将油液从一室转到另+ I: ^ S2 U O$ C% l& R
少
P/ u2 V1 z4 o英汉对照民用航空词典B OEING
1 h9 @; b$ U1 e; }2 ATECHNICAL DICTIONARY 135( B, U" m7 d( r: ~6 s
SHORT CIRCUIT, A fault in an electrical circuit' G0 |1 B0 }! [. I, ?+ A
occurring when the power supply goes directly to) B7 k( k7 c8 S. q& j7 _% ]
ground instead of to an electrical component.8 {8 N. U0 b6 ~$ O
SHORT RANGE ALTITUDE, A cruise altitude chosen to
3 {+ k7 Z" B5 U( X* e5 hinimize fuel burn during short trips.9 l. R! D( y. K
HROUD, A metal covering for enclosing the APU on8 a$ C5 ~ n7 Y5 S" D% F* t
e airplane. An external tube for enclosing a fuel hose.) ]8 \9 b9 }9 C" c& `
HUTTLE VALVE, A valve in the hydraulic system with
/ e, l/ A) u. m- STANDARD INSTRUMENT DEPARTURE, r6 K4 ]* A( v1 |. `- R3 F
f the
0 K4 N) i+ e, i, v3 u8 R1 _r access to the components on the engine.
- T, Y1 J5 U1 K5 @- L短路,
+ c1 x+ f5 i- c6 J+ B# N短程高度,
, H+ s1 }0 o* ?% }4 G/ G. B% ?6 N为在短途飞行中使用最少燃油而选的巡航高度。
' r! s/ G5 K! R- F L, k9 R护罩,* J( k" s" Y9 s* }6 W2 g
飞机上包围着辅助动力装置的金属罩。包围着燃油软管 B1 u( |+ N' y; S
用活门,
# L; y; `7 u4 e) r# T2 c) g7 ]液压系统中,具有两个不同液压输人管和一个输出管 B# z" v N6 v1 e
的活门。
$ n2 n4 u6 M' u6 J8 G5 q4 V标准仪表离场,+ C& M0 D$ p3 j
见Standard Instrument Departure4 L7 @! t/ P- ?1 a4 u
m# B% i; c: K' T: D, O; F
S1 ^; p' ? L% |* r; ]9 f
th
4 A6 q# g8 k. \ CS8 x9 k2 ]5 x% g3 \+ Q
two different hydraulic supplies and one output to a
5 X) F' H7 U8 }! h" y& o( tcomponent.
8 n- O" \5 r- |/ l, {% s7 dSID, SEE) D6 @1 G8 ~+ X1 o5 g
SIDE COWL, A removable cover around the sides o
% ]) X5 N8 n2 e7 u. w0 uengine fo Y8 a/ ?- S c8 J( J [, ~" v
电路中电源未经电气部件就直接到地线时的电路故障。: d0 p1 Y. `. f N
防
. z$ c9 D3 q/ s% e" q- _* Y- h& B的外管。
6 D0 a( J3 l* q. z. O* G6 F( i两
. W: s q* m6 K.
3 V! r% U" w- s* z9 Z9 N: m机两侧,被移开后可以够到发动机部件的可卸罩
% D8 x- t" G5 y* k( F8 ?) Q。# }& x b! v* Q L
侧整流罩,; g- N0 u3 a/ s/ ~4 w- V1 _
发动
/ W% s2 s! \$ U( i3 A子
. y6 M8 Z, J! y# b% u. [ }0 ]英汉对照民用航空词典B OEING- R$ J; F1 K: a5 G X- h
TECHNICAL DICTIONARY 136
4 a k& o. {7 M( P2 oSIGHT GLASS, A glass window for observing fluid
# z& g6 S% p1 M5 Rquantity in the reservoir of a machine.
' ^4 ?- s+ F. u$ n! p, that can be used to transport information for+ V) H! v( O3 b, g; i; X
communication, control, or calculation.- g: l6 t8 k- w5 }9 S ^
ILICON CONTROLLED RECTIFIER, An electronic( @1 I8 i; b1 ?% C! d1 ?8 d: [; y- x9 R
device allowing current flow in one direction after the
, M* N# G, G+ T+ ^5 \device has been pulsed at the gate.% c, h0 J. q/ Q" e6 p) B
SINGLE SHOT MULTIVIBRATOR, An electrical circuit5 w1 ^: A* s- X# }. r G, Y' Z
-stable multivibrator.
: p2 d# c) M' J+ Q如电流或电压能用于传送、通讯、控制或6 J% [% u5 n" P6 Z0 f) ~9 G
算需要的信息。" ]: Z! [9 C$ d
硅控整流器,
! R. R* E' k2 |" L5 C& |当其控制极受到脉冲后,允许电流向单一方向流动的电
! @2 \3 P# Z- t$ U7 ~+ r子装置。
% N7 p3 ^ A, B$ x' h5 q息多谐振荡器,) x& k: c [' E& H8 |8 m
输人信号触发电路时产生的脉冲的电路。又称单8 B7 u9 a9 x4 m4 P5 M/ q2 |# C
SIGNAL, An electrical quantity, such as a current or2 X) t) |: L* D0 {
voltage
/ A) _4 [: H1 z, p, WS8 R2 U! q$ d! _0 ~5 t+ o' [
which produces a pulse when triggered by an input% U5 R% y5 Z, E7 A
signal; a mono
$ l" b: T- X, P+ [) t6 d0 y检查窗,7 s1 t2 h: ? Y% s1 v3 J& g* i' A
用以观察机器的储液箱内液量的玻璃窗。
! ^) q3 T# X. K1 o$ o' S+ R0 b信号,- b# W: x" r: ~
电量的一种。+ |+ I _" d, \7 c& z8 k
计8 k1 [9 U: A( H# V [7 Y
冲
! H( w$ b1 _) h. [- K0 L# |3 P* v当一个
9 i# r1 E6 E9 q$ A; g' U" G5 p稳态多谐振荡器。
. b+ c% j" z9 x英汉对照民用航空词典B OEING) `9 j5 m2 H+ U& g' r+ j
TECHNICAL DICTIONARY 137& G% Q; Q1 K( _7 f( i% G
SIMPLIFIED FLIGHT PLANNING, Rapid determination
1 M2 d- u1 x0 T/ v' S$ Yof trip time and fuel using a chart providing these data
3 X- a9 {, W+ s3 x! [- Yfor the entire flight profile from brake release to landing.- z3 q2 y7 x* D: Y3 F
SLANT RANGE, The line-of-sight distance between two7 `% q) f* S) Y& L% _8 D
points not at the same elevation.
4 q4 \: S7 o- ESLAT, A moveable part on the leading edge of the wing
0 V) @* K7 D2 ~8 K5 [; H ^- B+ q/ Q. {for increasing lift at low airplane speeds.5 j0 y0 b, l6 _, P! q' t
划,
' P0 k$ ?7 V% H4 |0 U迅速定出从松3 [. R) q# e! H J
车到着陆的整个飞行所需的时间和燃油的过程。6 C: r" b" y; a# V; u
斜距,6 I7 y5 H4 x2 p2 ?, w+ {
不在同一高度的两点之间的直线距离。
& s, d7 t1 b+ t! [缝翼,; [9 [! x- P2 _1 @$ _: M6 l
用以在低速飞行时增加飞机升力的机翼前缘可动部件。- D: l: S$ R4 X
简化飞行计# k3 e2 Q% q# p8 Y
由提供旅途时间和燃油等资料的图表,来
% _: G# u9 j2 E* A刹) p/ h0 H, D& P7 ]! i: |( F
英汉对照民用航空词典B OEING
$ v1 J' @; ?, G7 b% QTECHNICAL DICTIONARY 138+ C! S9 ~( E5 d% }' s
SLOPE, The amount of incline a runway surface has
7 m M! `( X. l1 Krelative to absolute level.- F' g$ ~6 V( W2 j" M; S
SLUSH, Runway contamination made up of a mixture of
8 M; _; P$ C( n' yater, snow and ice.
! O/ c4 r/ R9 X$ m3 ySMALL COMPUTER SYSTEM INTERFACE, An input4 E$ | ]$ n. l0 f8 O
and output bus that provides a standard interface
9 p/ W, N; _, J J1 F; sbetween a computer and peripheral devices.
, ~) \" t! O! O! OSMOKE DETECTOR, A device whereby the flight crew
* A( `3 @1 e8 Z/ F# K: Nan be made aware of smoke or fire in specific areas of( [ p. n* c3 d, h9 W
the aircraft.6 p, `( p' W, S# ?6 F! ]
SNUBBER, A part of a hydraulic actuator that slows! n- h; z q! J: I3 @+ W- C
piston speed by restricting flow.6 n5 ~8 X# m7 d# {& o% o. ^
OFTWARE, The stored instructions that control the% T9 p5 ^5 N# `: V
perations of a computer.
$ M6 b/ h7 i/ C0 ^" q dng
) a8 I$ n0 H& X- E7 C' j( Y" iother devices.$ C) @4 v1 A0 b! Q5 _4 b, K
SOLENOID CONTROLLED VALVE, A valve controlled
3 N& { g0 }/ R9 K: ito open or close by the solenoid.$ \0 P$ E! w q3 ]) O/ U# a. k$ V
雪泥,
7 T8 d' }% d% q% D C0 [; [积在跑道上含有冰、雪、和水的混合污染物。: c8 _% y% ?. O8 b
小型计算机系统接口,
: P: p1 c, `7 f! p6 w# L& g一个能在计算机与周围装置设施之间供给统一接口的* ~' l/ p3 i1 E# g
人和输出总线。
% M# F7 b0 }2 c- |烟雾探测器,2 M* X6 m1 t6 N5 \. L
在机舱或任何指定区域内能测到烟雾或火并报知机组2 l* A& {4 [$ q& g& M
员的装置。$ f5 _, u$ a! Y! F8 M
冲器,8 H& d; o& q5 m" Z' j+ `
液压作动筒中具有节流孔的部份。这些小孔能通过限制! c \2 P. i: c# A/ D
液油,以减低活塞速度。
4 Y; }: @0 b5 V2 Z9 [储存在计算机的指令程序。用来控制计算机系统的工
6 t1 z& h* Q' ]- b" C4 W作。* s3 S+ Q: @5 r) Y3 }6 a
操纵其他设施的机电装置。) j5 ~9 V8 e0 g: S$ _. W
电磁活门,# H. W9 b5 a! ?( t* t
用电磁线圈来控制开关的活门7 Q8 S% L) U' c
w ~9 f9 e, [5 p. g+ ?, W
c! f6 g k; t, p- ^: O ~) G/ v
S
' ~, m5 ~& B* H6 C/ k6 |o# G7 @( D/ V1 k T8 i1 e
SOLENOID, An electro-mechanical device for operati# F8 ~2 D/ W6 V% @6 J9 c
斜度,5 T3 z/ q$ J3 Y) J. H
跑道表面相对于平面的倾斜量。5 x* X! Z- t' F) x# |, O' u6 F
输- e, L k4 C& o. D( x( D
人9 w3 p) a! O2 ~ K; a# n
缓
" s" f) Y( b: O9 a( U软件,
9 j9 L; S1 I. I0 d电磁线圈,
* x% N9 x8 Z( ?8 m用以% {5 p1 s b- Z9 n' A
英汉对照民用航空词典B OEING
+ \+ L( |1 R/ C+ QTECHNICAL DICTIONARY 139
6 r! [) O& p. e( K" j% d" n& L9 }SOLID STATE SWITCH, An electronic circuit that
! |9 C8 i* g! \5 @0 \& tprovides switching in a current path.
0 \: S/ Z, E$ d0 U3 RSOUND SUPPRESSION LINER, A component in the
: R4 ~, ?2 \) b3 Y2 ~7 Cnose cowl and around the engine for absorbing engine
* G5 e+ n' t- X1 M& Dnoise.
$ m# }9 `; E. T& H; ySPAR, A principal spanwise beam in the structure of a
& o; H9 o6 X% F- O- j: d8 ASPEED INTERVENTION, Pilot control of the speed9 _# }. l8 V4 c4 R) D
SPEED SCHEDULE, The planned speeds for a specific
* B7 @& N/ H: Z% w& J" kphase of flight.$ c) \) I3 \: d" `
晶体电门),6 G0 g5 O9 O8 b( D) b, I& b
消音衬,
$ }0 N' N' {3 X! }在发动机的周围及前整流罩内,用来吸收发动机噪音的
. m1 {+ B8 W( X8 r- I" [部件。 v1 [% C1 \9 K9 O' }$ Z0 c; O
梁,
1 B/ {2 {" K- g4 I: n机翼、安定面或操纵面结构中的沿翼展方向的主梁。
( y V; x# f4 d5 R6 s; \: T速度干预, t9 G' W7 U" Q0 H3 b! ^( S9 ]
计划速度,
" f& E* H+ e. I& ?9 i9 C, x为一特定飞行阶段所定的各个速度。7 `' M% y. F3 ]% o' B2 v& a
wing, stabilizer or control surface.
# a: |% x; f$ Pduring VNAV operation.
* F! m' M; F+ V# _- A6 ?固态电门(
6 D' t" q2 z$ E3 C在电流流经途中提供开关的电路。
% m- D- M( E6 ^, c) Q& i0 v2 X; m% E在VNAV(垂直导航)操作期间,飞行员控制速度。- n) T" G/ q; r4 u* W
英汉对照民用航空词典B OEING- l2 n: H# v4 g" c
TECHNICAL DICTIONARY 140
+ O% ]4 q. A, T+ K0 s' [SPIN BRAKE, A device in the nosewheel well for
' i4 P3 z+ U, x7 w3 g7 ?# Tstopping the wheel rotation after retraction.
8 ?4 e" C- F, q. XSPINNER, An aerodynamic fairing attached to the fan of& n- Z/ n* B, C" m m: o
a turbofan engine.- j. g7 Z1 c$ Z6 w! D
SPLICE (NO. 1), A connection of two airplane skin( X! w. `0 N5 D
sections.
0 t' }3 t7 |1 i& r7 A' }SPLICE (NO. 2), An electrical connection between two. V: g T9 e9 ]- h) Y3 c1 H
wires.9 Y0 R4 z( ` d# }. w0 l7 U1 t! [
前轮舱内用在起落架收起后不让前轮再转动的装置。4 a2 v0 {8 r; n% \7 G8 o, n3 ^$ D. R! P
旋转罩,
8 h% c% X1 x- [# }4 m固定在涡轮风扇发动机的风扇上的气动整流罩。& I/ r0 M ]6 b% V
拼接,# a, X2 i" i* _ y- x* m
飞机蒙皮与蒙皮之间的连接。
5 l" f# \( E) A' t* F( e- l: `铰接,% S$ |" x+ r; l/ H5 h; ~ H% k8 p
两根电线之间的电接头。/ L) b3 b! {- H* i: C
停转制动器,% A* O: y& C+ o% S
英汉对照民用航空词典B OEING$ y# h/ Z, C0 Y( Y- [1 [7 a7 q1 b
TECHNICAL DICTIONARY 141
8 B0 i7 z+ W* B8 o5 D/ a+ ^SPOILER, A hinged moveable panel on top of the wing.
% w1 ]! b! x! ~( VFlight spoiler- assists ailerons for airplane roll6 j$ y3 y T# p/ L
(wing up and wing down) control
9 r, I6 h1 F" K1 B; Land for aerodynamic braking in
: L' k* h. I: X. Q5 q. l' Q% D; Z0 qGround spoiler-for aerodynamic braking on the6 C( \2 r% q' P! t, ?
ground only.% D( N) }- f2 \7 _3 x' p0 u8 E5 w
PRING LOADED, A condition in which one part of a
1 k" a u; C4 P% vevice is held in a particular relationship with another
& w; k5 S0 L+ I, P; |( at,
) t( f* N j, Y1 Wr original position.+ r/ `! w' s( b0 R7 d6 F1 c7 k
SQUAT, Airplane on ground condition.
0 M- w3 s) T& v0 E. \% l( m" q1 @QUAT SENSOR, SEE - AIR/GROUND SENSOR
- z. f' `: K$ HSQUAT SWITCH, SEE - AIR/GROUND SENSOR
$ ^& }7 S" R' [0 e* H( y7 P& R- u扰流板,
- z! s/ W- |& ?& R铰连在机翼表面上的可动翼板。
2 v+ U* p' \7 G+ U9 J7 r0 A- C飞行扰流板一功用有二。一、协助副翼来操纵飞机- a8 U" U; {9 W/ J/ _* l2 A
的滚转。二、用以在飞行中或地面滑9 l' J* ^+ ~6 B
跑时作为减速器。
7 P3 j" y Z1 `- I地面扰流板一仅在地面时作为减速器。
) M3 R" a' D1 u( G簧加载的,5 t3 ~5 w7 [8 k" x$ N
由弹簧使一个装置的两个部份保持特殊关系的一种状: `. J3 b8 e7 z* L
态。该状态允许一定运动,但继而回复原位。
' G. W/ l& Z7 X& K" c5 C& j# G8 H着陆传感器, @; G' H ^8 o$ u
und Sensor' E/ d- o( Q5 s+ M) C
flight or on the ground.& @( O, _$ X' b' h( G4 _
S
; E" q- V4 ?8 fd
% h6 e- P/ h. F, ^part by means of a spring. This allows some movemen4 {- [9 c; S( u M) k
but returns the parts to thei9 G4 H& ]) _ y
S
# e* B4 n$ g+ b5 i& e弹
7 n, M- h2 H: v W5 L着陆,
2 @0 }' f1 h0 d6 w& o& m( J/ ^飞机在地面的状态。
( j* F& ]5 f8 q. v/ [! M# A见Air/Gro
) Z* v9 l, K0 V) {$ z) _着陆电门,$ S3 Y5 [' d" _
见Air/Ground Sensor .
4 M1 x3 ?* ~0 i( t' s$ `英汉对照民用航空词典B OEING1 I" _ {& {3 T7 o" R
TECHNICAL DICTIONARY 142
& s5 a5 T0 l/ M" O/ r, XSQUAWK (MODE,CODE, FUNCTION), Activate
b! _+ ` O6 F3 Qspecific modes/codes/functions on the aircraft$ X0 l! h! F% U& V/ T7 L/ x" R
ansponder, e.g.,” Squawk Three/Alpha, Two one zero+ ^5 o' n3 N( _0 O/ J4 A% S1 |9 @$ s/ }
five, Low".
1 y4 P% n# J0 i9 J# qSQUIB, An electrically operated pyrotechnic device for
- L5 U0 u) H5 x, T& D% nbreaking a disc in the fire extinguisher bottle to release
' ~4 @' F/ _1 ~2 Lthe extinguishing fluid. Also used for escape slide
; S: b4 _' |( Q/ O: F4 XTABILIZER, SEE - HORIZONTAL AND VERTICAL- e* Y ?+ C4 U. }, i: \0 ]" @" S
STABILIZER
; j0 f- B" V& E7 ~TABILIZER TRIM, Movement of the horizontal tail to) c8 A5 N6 V2 j, W& _" N
hange the attitude of the airplane about the pitch axis.
; `8 d3 E1 h; X$ FTAGE, A numbering system for the compressor and' k7 D, s1 M5 k- |$ ^
turbine of a jet engine.
6 x6 N+ D! l @, W, VTALL, A flight condition during which lift is destroyed
0 _, t, }3 H/ R# ~& b6 ]- P6 z: Lue to slow airplane speed or attitude.
H+ O" |% j* A; Y! F+ f1 ?; Q$ Jto enter from the top and flow
( K* G( i; ?3 D; a! Iout to the system. It prevents picking up debris off the$ J) R/ s5 G1 A+ H |. p
bottom of the reservoir. It can also control fluid height in
, [% i6 u/ H; y, i: U/ N6 A. Ythe reservoir.
5 a' j' ^# B( G6 V0 R) R0 o o" f能),
6 z1 h& I3 C- U使用飞机应答机时的一种常用的指定方式/代码/功
$ e: Z5 _* E. Y2 k3 M能。
& \ ?" p( G9 Q6 X, u管, M5 w ?" _' h" ]/ T
用以爆破灭火瓶上的圆片,以释放灭火剂的电控烟火装
* W7 `* i2 @# D8 U( @置。也用于应急滑梯放出。
8 A/ H' e5 D4 [. U定面,
) [. t& \2 x( U. r3 k/ K见Horizontal and Vertical Stabilizer& V2 O3 T* c8 S- b
tr
& F2 ^: Q2 G+ t- D0 D2 |deployment.
) v$ d& Q% c0 B1 }3 B" h( [S( j. I3 q7 _* o/ M9 }+ x% g3 j
S2 {, M% z% t$ F9 J
c7 b6 J6 q. t+ z) E7 s5 `
S
! i( S! |% U B* a" n! e; yS& ^3 ~/ n7 l9 V9 B1 U$ x8 O% S& |
d9 K7 G" b; h/ v9 j% q( _
STAND PIPE, A pipe raised up from the bottom of a+ m ^! ^/ p4 U
reservoir that allows fluid
$ J; A. v. p# P9 i) n1 ~发送信号(方式,代码,功- Z& j$ W5 U( }* u, _- ~0 W
爆, {1 r8 z; ~: Z9 W
安8 k: K6 `# J, O Z$ N6 K+ }
.5 `9 }1 D. x9 L- Z
定面配平,; K8 _2 Z: A! j, P4 B
为改变飞机绕俯仰轴的姿态而做的水平安定面的调整。
( o# V; G* H4 X级,7 p _. b% T! v2 G* J
用于识别喷气发动机的压气机和涡轮的各个段位的一, n. `( S# a/ j; @/ a, Q
种编号系统。
, a- g1 c; \. v4 L: b. M) m失速,1 N% X5 n( q( i0 c6 F* m" N$ |
飞行速度过低或姿态而引起升力失去的飞行状态。5 J- k6 X7 T8 x
回到系统中,并防止带起容器底部的碎屑。也可控制容# q0 t& z+ ^3 G
器内液面的高度。
' k! ^3 p N, H4 O' L. j$ \安- _. Y) R! u, H* m6 c
立式管,
& E9 E) _( U3 ` ?从容器底部立起的管道。能使液体从上流流人,然后外
8 ~6 j6 i" x2 t流
% Q$ S8 B' \) S) ^2 J$ t英汉对照民用航空词典B OEING
, J) C1 q8 V- C, ~3 U( n- ZTECHNICAL DICTIONARY 143
% _% E& \9 A, C8 Y- r2 ~& ZSTANDARD INSTRUMENT DEPARTURE (SID), A8 o7 R) T% j) F
IFR.
: v) ]# b7 H3 p6 `8 S% X: Q8 sTANDARD TERMINAL ARRIVAL ROUTE (STAR), A
7 D: k8 M/ j8 t* Z) Oublished procedure for approaching an airport IFR.
- x& c) p" |: h8 vTAR, SEE - STANDARD TERMINAL ARRIVAL! z( E8 K. G, y- i5 a* a
OUTE X1 T& [8 [1 z0 ~2 u' t) i- M6 ^
TART VALVE, A valve in the engine start system for
* g" L( X' b) [upplying air from the pneumatic manifold to the engine$ n" o4 h0 f& ?! D
tarter.! K, q9 t1 l6 I* |* e4 t1 g1 i. V
TATIC AIR TEMPERATURE (SAT or OAT), Ambient6 t2 P, f; j; L* y4 b
or outside air temperature.
4 d/ x' Q/ x) B. e* R0 MSTATIC PORT, A small hole in the fuselage for sensing9 {* {5 U( R {4 L' F
static pressure for airplane instruments.1 ?# k0 D' ^9 _! p. v
STATIC PRESSURE, Pressure in the air or fluid at rest
7 x8 ]) b \! f% g7 ?# omeasured in pounds per square inch.
* c" [+ k4 e- ~" `2 ]ID),
7 Z5 M/ f% z. g" M用于使用仪表飞行规则离场公布的程序。
4 L# Z; L: Y( T! X- O7 ^标准到场航线(STAR),5 J m* f. |/ m0 h0 T8 `1 d
用于使用仪表飞行规则到场的公布程序。
( g5 D; a. W' ]% a* c标准到场航线,* ~" W R) q: k0 ]
见Standard Terminal Arrival Route
# C- Z/ W* }9 \0 ipublished procedure for departing an airport
3 m) j# Q/ A# \7 @! v) E' J% hS
& Z9 [. p# d. H7 Gp4 P$ l2 |5 G6 m% e5 [& s0 D
S
. X8 ?. ]& A# B( Z( bR
8 M4 q6 J B3 e* C: o+ r& tS4 M/ _- V7 u: g( i( Z7 k! r2 ?
s$ I# \! ?6 z+ n6 M
s+ n; M1 g# a# C; x- t! ?- S/ K( P
S7 }- R; {0 S- }8 ^+ o
标准仪表离场(S
9 R* q# a! \' z6 q5 K [.
# @3 P: F+ P& \$ }- d; y, e起动活门,4 ?3 ^* f/ }" n8 N' j+ T
发动机起动系统中,用以从气源总管向发动机起动器供
- p: u; e4 l n& P的活门。
7 _, S4 z0 P2 V0 g温(SAT or OAT),9 _# Z: A0 m; e/ g- E7 n+ i1 z H
环境空气或外界空气的温度。
& r8 @* K( `& ]压口,
0 l1 i3 B' D8 D% L0 }) r位于机身外表,用来为飞机仪表感应静压的小孔。
5 H: i7 ]# Q) w( \0 v静压,' r! o1 W- g" L B) t" y+ M
静止状态的空气或液体的压力。用磅/平方英寸来度量。7 z9 a- t: F5 x$ S8 s
气
" w0 X# ?; ]& }! I- c静
. X5 ?* d9 Z9 ]2 c; ^静
& {, ~8 T1 _& p' \1 p' {英汉对照民用航空词典B OEING9 d' G5 z1 r+ Z5 `/ I' k2 A: m% j
TECHNICAL DICTIONARY 144
" e+ J& \; c% B' \& X$ M wSTATION, A vertical reference plane along the fuselage" F5 {, j% L: C- h5 U+ J- A
for measurements along the fuselage./ ^1 g7 Z+ m& [1 `" M9 |+ h
TATOR, The stationary section of the compressor, |, a# `% b1 w/ f
etween the compressor stages in the jet engine.
+ _/ ?, [0 c& J- ]* m, MTEERING ACTUATOR, A hydraulic actuator on the
. T3 C4 T/ y+ J; e! p E# z; zlanding gear shock strut for steering (moving) the
: k5 R* @1 C- Y1 o* q/ e' C- jnosewheel left or right.
/ }+ D4 V/ {: p& NTEERING TILLER, A hand-operated lever in the$ h& S0 A( _/ ~0 L$ G- t
osewheel left or4 Q* t( e6 h+ g5 X4 P3 L8 L
ght.
0 }$ c4 v" w7 U TTICK NUDGER, A device to push the control column( h9 c% p4 _2 u, q) a
rward just before a stall occurs.! S: `. B' z3 a( |3 V* S
站位,8 J" r" b9 N, `& M" v! D. a
用以沿机身方向度量的垂直基准平面。 i- b% V5 h: R! Q# F6 [. r( l3 ~0 F
定子,; K& P; u; h/ X4 v7 @/ n
喷气发动机压气机各级之间的不转动的部份。9 M1 _; c9 N2 I: Z) I: l- l
弯作动筒,) L H! W0 d) u$ H
减震支柱上,用以使前轮左右转弯的液压
4 [/ U3 c& K: y' n; t作动简。% M$ U( s! v3 V$ H7 v9 H4 G( d
轮转弯手柄,
) b8 K* k4 O) E9 R! M内用来使前轮左右转弯的手柄。, k$ x! B5 l: ^9 z0 o& p; @
动推杆器,; z! \4 h7 ]( g" q$ ^5 r
在失速前能将驾驶杆向前推的装置。9 P. {1 ]. [/ F+ {
S, f: ?$ m* d# s
b2 M+ p8 k( v, I& @2 `
S
! {; Z# L/ `4 E0 {8 @S3 X$ D8 ]& ~. Y( k* |
control cabin for steering (moving) the n8 X) E9 o6 c/ M1 E& K: b- R; ~: M
ri2 K8 l: Q. j0 S4 N9 [
S
& X- m! L. {& i) l/ V* O, afo
9 p+ R( }2 D u" z8 y4 a9 @, X0 Z转
6 m) n3 E; }. u+ ~) B一个在起落架
! K: y% R: t3 ^8 _) B2 J前- j3 P/ f/ m& ]: _0 d( h
驾驶舱
$ _4 X5 L" Q$ L$ ~4 H" K9 z自- O* ?" j$ {: }: R; T3 [
英汉对照民用航空词典B OEING
+ Y& b3 Y% n8 Q( R8 C8 q {TECHNICAL DICTIONARY 145
0 M) X3 ]& K! QSTICK SHAKER, An electric motor operated devic
k5 O- r, {; Nthe control column which shakes the column be
# q8 C' L& f6 J$ k: w. A1 Ostall occurs.
1 J* s X( D6 d2 M6 @$ F8 fe on' M% p, t# D- I, N& [( l0 \+ ?
fore the
! T) V1 w8 J# X* \# w% u3 j5 h3 ~TOPWAY, An extension beyond the end of the runway! B2 r3 N/ f) N& [
hich may be used to decelerate the airplane in case of' R1 c$ A" {! u" G! ^" n& ?6 a
n aborted takeoff. It cannot be less than runway width
! _) l x* G! [% @- v, Vand must be strong enough to support the airplane3 L; y6 a1 W2 A# L: p' s
置。
( E( ?; T0 k% k7 L( T5 K' x+ s速安全道,
+ T, G, i0 z6 a0 L$ k9 c0 j: q3 V跑道两端,可用作在中断起飞时飞机减速的延伸地带。
, [; { @: S0 W/ C它的宽度不能窄于跑道,硬度也必须能够支持飞机以免结
( B& F5 D( a& Z" c3 J% O0 C; kS
3 k; b9 C5 E- I5 \. T; gw X! G& h2 g5 Y# E
a
" u2 i4 a; L# fwithout structural damage.2 P2 ^5 _% x% s" M
STRAIN, Structural material deformed slightly due to the
) p4 n% \" n z/ paction and forces of stress.
6 X; o8 S- x, }/ P x振杆器,2 w Z+ n# h7 X8 a l% D
驾驶杆上,在飞机失速前使驾驶杆振动的由电马达操
1 N" Q& r z0 O4 h {+ [. w% m2 g. E作的装1 z4 `. P7 a. o+ a
减
$ c s* P' G2 g- y* ] d( h构损坏。! J" Q" e; a ]; t: ?: \
应变,6 V8 b; J8 {) P) x# F- m" C* O
因应力作用和受力而轻微变形的结构材料。# j* @- Y- C# ^# Q& m; y" F6 j' \- P
英汉对照民用航空词典B OEING
2 b( W% z4 A) y6 S1 [" k7 e6 u8 vTECHNICAL DICTIONARY 146& h7 R3 U% E8 ] q1 }
STRINGER, Structural components in the fuselage or
$ a. C' q2 J& x; F7 ]. hwing for transmitting skin loads to frames or wing ribs.
7 F. Z& S# X" Z" CSTROBE LIGHT, A high intensity flashing light on the; U) y' A, _0 W' D+ u7 a
wing tips and empennage.
6 a/ H& Q8 s0 rSTRUCTURAL MEMBER, The part of an aircraft ^" p3 v2 Z. u: f( g) ?
structure that has been designed and constructed to( R) L, E) C# B3 M, C# K2 n
carry and accept loads and stress.9 P! Z( C* N9 a ]" G0 I
STRUT, Mechanical components of the landing gear for
$ R" M% r! p. P6 U) j" l: y. Okeeping the gear in the extended position.
! r! P: ?( |; l' D机身或机翼中,用以将蒙皮载荷传至到隔框或翼肋的结
4 o6 [7 i! @4 b# Q. E) S% P7 E构件。
/ ?/ A0 I8 u6 X# y- U0 ]+ U频闪灯光,
! b" O" S/ k. ]. M+ k. v位于翼梢和机尾的高强度的闪光灯。: X# ]) E9 m$ s( U Q R
件,! R. m' M0 V" b d6 k8 V$ g4 l% J
飞机结构的一部份。为运送和承受负载及应力而设计建* c; h9 ?' T4 n
成。- @% ^* p* U4 N' S& U4 e( O# Z
支柱,
. y+ q* Y x% W# A" S起落架上用以使起落架保持在伸出位置的机械式部件。
! M1 F3 j6 ]7 a2 z* B长桁,! h# {% ^6 F. I; f* Q: `2 k
构' a8 x9 A9 G# A; [; `$ P' I5 D
造/ d! x. _' R) Y8 [' j
英汉对照民用航空词典B OEING: L/ P. f6 P1 D0 s2 n8 r# h/ X w
TECHNICAL DICTIONARY 147
8 D$ t, e- L% O5 gSUMMATION UNIT, An electronic component for
( n/ D1 B; N2 ?7 P7 D2 ]adding fuel quantities in all tanks sending a signal to the
: z- q+ k8 x# ]* T9 j7 ]tal fuel quantity display.9 r, X& Y0 v, S: }8 S& ?/ Y
UMP, A lowest point in the engine oil system or fuel
2 A) k! f* w1 r) {3 ^nk.8 m0 q4 Z; {9 ~3 A8 A1 A" L
UPPLEMENTAL DATA, Additional data stored in the
" g; ?! l" k C- YMC memory, supplementing the loaded navigation
% A0 Y! f0 @ {- ], c4 R& Vata base.+ d* f% G* J* x6 p' D& ?
n
! |. O0 a1 v" e3 {9 s* U2 e: y) |eviating from normal modes.
4 i6 i/ h: t' h5 u2 j. jSURGE, A sudden change in the airflow through the: o0 H: g$ ^% l; O7 L( M0 U
the compressor not being able
/ m% _% W4 B2 E% X, [compress the airflow.
S+ n, y; g4 S* l& cSWAGE, To squeeze together two or more items to* x3 e8 _- T A) X1 [
form a permanent unit. Example: a lead or steel piece6 W7 n$ o$ Q* l1 D4 j$ R
on a cable which forms a stop or camlike unit. Also to/ l9 H6 K6 r$ p
reduce the diameter of tubing.
: { |' O, b4 n6 ?( a. C* BSWITCH, A device which changes the condition of an; z* ?" `$ Y0 L* Q W
electrical system from on/off or open/close." X1 z5 ], F* d; @0 i8 G" D
燃油总和器,
) b0 N: F s+ ?9 U+ `6 a将所有燃油箱内的燃油量相加,并将总油量用信号传至" N! Z8 `) @! @' ~' e
量显示器的电子部件。9 ?, v+ Q4 }0 v! p- i4 `
集油槽,7 S4 g0 O- `% c% [; @) n' j G8 T/ h- Y
发动机滑油系统内,或燃油箱内的最低点。7 K9 O6 N. r0 h
增补数据, ]8 v$ n0 U, t
飞行管理计算机存储器中的附加数据。用于补充导航数
. E5 n. g Z2 m5 K) t4 D据库。' }( l8 }* ~& K2 ^! p" Y
,( L' ]$ F( V( k4 _9 x4 _; S
附加的数字飞行控制系统方式,当偏离正常方式时使
6 j; R- ?& p1 l+ A/ [。
0 W' e: z% g# j9 J, i& P% s过发动机的压气机的气流的突然改变,而导致
) k# D1 Y% i" j& z( s/ o$ Y, |气机不能压缩空气的现象。( e( f4 _ J0 b3 U+ p
陷型模,. D, d& H; X) [3 [ q
挤压两件或两件以上的物体来制造一件永久性的元件。
) ~* Q; i. x0 Y如:一块铅或钢在钢索上形成一个止动器或凸轮之类的; t( _# b6 t6 R2 L) \! r. |* {
件。也可作减小管道的直径之用。5 J5 u$ p6 d; v0 M
开关;
: o9 w# e) M+ N* Q2 Q( M改变电气系统通/断或开/关的装置。
. t' }7 d y9 J2 T( ~3 K; [- b2 Lto- N0 F# T* L* a7 I- E
S
! I! h4 ~0 V- T/ O* U, uta# h2 w4 x! p0 S7 l' d" C% K4 W. n
S
' b% M& k/ _& Y1 PF
& N% `: [$ l" J# vd
8 x/ ^; n8 W5 ISUPPLEMENTARY MODES, Additional digital flight0 E7 t) f6 f3 o7 I% U
control system modes that are available, used whe6 m% q( q2 T+ b$ z: T
d c/ N/ c5 G. |3 T* t4 K) W. ?
compressor resulting in
2 E* X6 U- q* F5 y+ [+ u6 H3 lto
$ ~/ E. ^' v9 A+ n油; d" m! u" Q- X1 ~' F
辅助方式
& z% J! y& N. y7 A$ \( B/ Y用
( Y5 w- k- W' P- K5 _! b喘振,1 s9 @- B6 E4 r" Q1 { A
由于通
3 R6 D$ B* ~ Q5 L$ o/ U" \! \压. H6 p# Z, D# |! @2 Q
例
! S6 D- `, C( g/ c& |+ Z: {元) `& i; v1 S5 v4 M% L5 }; a* R( b
英汉对照民用航空词典B OEING
5 V& Q" U {. zTECHNICAL DICTIONARY 148, E: G0 ~# ~ p1 M1 t' a/ d
SWIVEL, A device for rotation of components.
& _0 u* z0 |4 t- z& |; D' pSWIVEL COUPLING, A junction in hydraulic
+ ~6 M7 I7 E2 C6 K8 S4 p- q, ibes for allowing component movement.. h P3 `6 h. k! R. b; ?1 v
YMBOL, A graphic view of an aircraft component in a4 s# S' d" H% N! F3 f2 Z9 {9 j
ery simplified format. Used on drawings to represent
4 u: M' R- @+ S1 G4 g; h9 L& h4 Qe entire component. U0 a. b% B4 Z# i U; x1 Z% J
SYMBOL GENERATOR, Generates the video signals* x: r3 G: [& U- X
that are displayed on the EADI and the EHSI.
1 s) q8 x S: c3 }; wSYNCHRONIZER, A device or circuit to make the units6 P- I& e z; j# D
perate in unison.
" i+ I$ I6 M# k2 {8 J eSYNCHRONOUS, Refers to two or more things which) Q* w- H% C6 E5 p# c
happen in a system at the same time.9 m1 U+ |8 M! L7 V. Q2 e' D: W, G
用以使部件旋转的装置。$ G! A* ^ u- S& j3 v
转动接头,
- v0 t( q1 O$ v液压管线上,使相邻的液压管能够动的接头。
1 `( l. X A. E7 o7 L$ N# z符号,
; }) G. a( K& M+ A飞机部件的简单示意图。用于绘图以代表部件的整个结! a$ y- i% W1 E% J$ G* t
构。
5 V N6 _, o6 f: P符号发生器,5 N. h7 d; l: j# X& }
为姿态指引仪和航道罗盘产生图象信号的装置。1 i5 Y6 j" q4 a. x- |+ y
同步器,: [& w9 w+ |+ h: A2 }, H, j
使元件操作协调一致的装置或电路。- t7 R; _- a- }# p1 ]5 b. L
两个以上的东西同时在一个系统中发生。
8 r6 c4 {/ l. p8 b! G& E+ G" Ttu
- e9 O; F6 S3 e" rS; |0 Q$ v# d: o+ {/ n2 i7 T
v
- \* ~2 i# I. X9 A, U1 m# Q$ Ath, e! s- U' N: M }+ Q
o$ Z4 {! N' J+ i; n# y. r% w
转座,
' [7 U0 K( J+ L8 u; A同步,
3 l5 t) R7 A% r" Q9 }5 z指两个或
) M8 Q% t3 B1 N英汉对照民用航空词典B OEING7 X* [2 D" h9 L p! N9 b" \
TECHNICAL DICTIONARY 149
. M& F0 q7 q% D+ g0 A9 f% w. ZT
( a, D6 h W. W' ]) xAB, A small, hinged, moveable part on the trailing B( L" ^# z/ e
dge of a control surface (aileron, elevator, rudder).
( _6 b+ ~+ I( EBalance or control tab - moves in an opposite5 z; ^4 ], i7 p/ A
direction to the control surface for assisting
8 k7 s5 i9 t: |! g4 D. k" jin movement of the control surface.* ?7 S+ m4 s1 S( f. |8 d
Trim tab - provides controlled deflection of ailerons
4 E: G4 J6 {# {* y) }or rudder to compensate for imbalance in' }, F) H+ X( a" p4 Z/ F
thrust or fuel quantity.
. n* q9 L$ i6 R& eStabilizer trim - controlled deflection of the horizontal$ y4 M! S4 r9 f. w: Q
cy2 X1 U3 F( I5 @. N
proportional to the speed of rotation.: j7 w3 s% w' Q
TAI, SEE -THERMAL ANTI-ICING
6 n. V5 E* |' Z9 |$ l) cTAIL PIPE, Duct at the back of the engine exhaust.
. ~8 ?/ D- Y9 l7 Z1 zTAIL WIND, The wind component relative to the
" {" M5 \/ F8 g# U k/ Sairplane direction and coming from behind the airplane.
6 }9 Q8 r0 c& `: `! ]9 `! d" [1 ?. X; L调整片,
. t S& H6 L/ X9 n; |铰接在操纵面(副翼、升降舵、方向舵)后缘的可动小/ A' B2 B' T4 K3 a4 }! w9 Q
部件。
8 e2 m2 ]. G5 t/ [4 Q3 \: g& p5 B* c平衡或操纵调整片—与操纵面运动方向相反,用以帮* A8 o0 Z p& `. X; m8 a% u2 a
助操纵面运动。8 G2 T+ u0 K/ b' S' ^
配平调整片—使副翼或方向舵作控制之下的偏转,以
+ M) f, P3 g/ v补偿推力,或燃油量的不平衡。' [/ L# _1 j) D7 a
安定面配平—使水平安定面作控制之下的偏转,以减7 J: |0 G V' C9 a4 ~- a K
少操纵力。
3 _3 y6 F' n0 J5 w$ r% i/ U机,
" }; l' p" [ q8 |0 |提供频率与转速成比例的电流的小发电机。$ T' a- H" D3 C* y4 {7 d
热防冰,& C5 T6 {: w K& U3 L' ?4 V/ P
见Thermal Anti-Icing
) t" C" v- q! I8 XT$ Z A: H- o# R
e0 Z4 F" K7 _6 f8 u V
stabilizer to reduce control force.
+ `- E: s e4 {0 u A* U& a( ~TACHOMETER GENERATOR, A small electric. J( d" v) Z3 f0 w, Q
generator for supplying current at a frequen
9 f/ n, K1 J9 ?% q) h, J3 q9 M& {测速发电
B ^! R0 R8 a1 v8 e! X" H: \.
% n9 Z6 J& W0 h/ @3 w8 O尾管,3 A+ U9 }9 T h0 T
发动机排气管后部,用以排出发动机的废气的管道。) O- q$ w8 i% t) X' o [& ^
顺风,
; k# o9 f K! p0 F6 D' l飞机后方的来风在飞行方向上的分量。
, V6 n5 v) e; a$ u. X& T英汉对照民用航空词典B OEING$ _2 k7 e, |. F( R, ]
TECHNICAL DICTIONARY 150
. ~! o5 g% l F6 K6 G! ATAKEOFF ANALYSIS, Analysis that evaluates the% ]- `4 i/ V' _1 {) q3 k1 _
airplane takeoff performance capability for a variety of! L& @/ A3 G+ E4 S% w. U
environmental factors at a given runway and airport.7 W0 `- R3 E/ U# l
ET PARAMETER, A specific goal such as. L8 t5 o' K7 ?" p
irspeed, thrust, engine speed, altitude, temperature, or
/ r Z* n3 u3 u- \) Q6 t1 cte of climb which is to be achieved.
: Z1 [; b" V3 I }3 ]0 g8 nASK TICKET, A computer label used for tracking the
- _' V$ Q' Y" P1 ^ompletion of a task.) d) ` t; y" w
RATURE
j( z* F2 G& S( ~( @( J1 N; ]AXI FUEL, Fuel burned from the time the engines are
8 m. I! i6 k. |5 e8 zr.
9 d# U4 S; o/ ?+ i/ `CAS, SEE -TRAFFIC ALERT AND COLLISION
# C# l3 ~3 Q* g; i/ y3 Y7 H5 TVOIDANCE SYSTEM
% j; T8 U# G- Y ]" m' T( q欲达到的特定目标,如空速、推力、发动机转速、高度、/ _! q& G: k/ u7 F
度或爬升率等。$ d2 h/ W$ \, r7 x( W3 Z
工作记录单,
, p% ~8 N* w" s+ L2 N+ [% e, O) u用于追踪工作完成情况的电脑记录单。
: ]7 s" k9 C+ `( ]. w0 i" ~全温,
; ?) a; W2 o% ?# O- N" `见Total Air Temperature
5 `7 R6 e( _& k: k$ L3 j+ QTARG
; e$ T% T& `0 Q j5 D$ o; Ja
9 L5 u* g1 S% G' dra `# `1 N1 R3 J6 i# ~8 j
T
4 E8 G3 N6 `4 T) W; z( ic
, B& E$ w! K7 j H/ o* aTAT, SEE - TOTAL AIR TEMPE
: j2 ~2 R" b+ Q$ U, Q; U. ZTAXI, Movement of airplane on the ground using
3 e( j( l: y7 V& q! f2 Aairplane engine power. [9 L) N. }8 X' c8 T' ~0 C
T' E8 `1 w) ^: C8 B3 g8 w8 g
started until the airplane begins the takeoff maneuve
- |- y' X" r0 k% d BT
# }: N+ [5 i/ Y5 z" P8 C0 T, VA$ N4 }+ V; o; ~1 M; _( _& h- F3 ~
起飞分析, f. p8 P! \( F! ~; Q/ M
对飞机在一个给定的机场和跑道,在各种环境状况下的8 j* ?+ c3 a' @
起飞性能能力的评估。
8 ]& g# o1 {1 p. L" C, ~+ n6 P目标参数,
! a; J$ ?# ]8 a' z温- m6 { E8 S6 y
·9 X7 u1 W/ [ t$ v7 P
滑行,7 B' }4 q* S! d) @$ H
行燃油,4 Q9 h# u6 d3 j9 g6 o% |
起动,到飞机开始作起飞动作之间,所消耗的
, ^7 m" t: p# m( s d" Q中交通警告与防撞系统,
# Y$ s* _; p7 v6 ~0 \$ r: {. w见Traffic Alert and Collision Avoidance System
. R5 o. |8 g% `- V' A飞机凭借发动机推力在地面的运动。
$ g$ N! p+ {& h8 H2 L6 l滑
+ R) l0 ~5 ]9 [从发动机' O9 f- P. L; T- C/ Y
燃油。
% B! u. Q3 Q% q空- e3 n3 Q9 @3 B, m3 J
.8 K& | D8 ?" Z/ U$ K0 j2 h3 H
英汉对照民用航空词典B OEING9 |) Z% K8 p) I( j' ^
TECHNICAL DICTIONARY 151
. r/ z. j7 R; @8 r7 h9 u: l KTCC, SEE - TURBINE CASE COOLING
1 i& ]% E7 g# P+ H! A! f+ Z6 _/ I6 o5 ^EE, A pipe or tube connector manufactured in the0 ^, U; ~/ j& ^' @& N1 f" J
EFLON, A synthetic material for hydraulic and3 c1 @' \8 ]( W& H6 p' c
neumatic seals.; T# m+ {9 k+ n3 ?3 v2 Y. V6 @
EMPERATURE INDICATION STRIP, Temperature
& k/ ?1 e5 d% s# Gensitive tape which changes color at high temperature
: _. |- r: T4 k2 J* _r indicating component exposure to high
* S- X) n& ^! U# gTEMPERATURE INVERSION, An atmospheric
: ~( E- V8 S5 d% k& t" _condition which causes the outside temperature to
0 w4 l# l4 r) s% c$ w; q" U4 E4 w+ Zincrease as the airplane altitude increases.) P. p4 r1 Y; K$ S
TENSIOMETER, An instrument used to measure the
; E, p0 j+ Z8 C5 m8 V, V G9 U$ U' }tension applied to aircraft control cables.* Q4 |; v- M$ \' K2 Q, }( X/ u* O4 i
冷却,3 ]4 @/ w" V/ C& ^" H0 d) \
T) b: Q3 }& b+ m/ g2 b6 e4 Z
shape of a T# g& P/ v1 t/ j0 [
T# c. ^0 r, @% r/ R! h7 ]$ M$ I# T% Y
p
% o( ~0 E- H) X5 Z1 lT
$ {; L1 E4 d8 @. D- gs+ W; O7 e% a+ C; j: o( g/ `) Z$ k7 B& c
fo
! v6 P& E8 p9 T$ ktemperatures.
6 z: o& n* L- e2 m4 _涡轮机匣
2 N( X& }5 s' H6 A见Turbine Case Cooling.$ z6 N, x6 b. J5 G# ~5 h* m% X4 F
字接头,
# Z! i& e e1 d0 P+ F的管道连接器。
: v# a1 F. {2 a" X3 D氟隆,
) C( j* X2 K5 s* P. O4 h1 x8 a# }. s用于制造液压和气源封严的一种人工合成材料。
9 J9 c, x) L; F1 [ ? X度指示带,
0 B5 p5 X4 Y2 T3 e6 x+ T4 }遇高温变色,以指示部件周围高温的热敏带。7 A3 f. b: u3 c9 ^1 R
逆温,
) \5 ^9 d( F/ X一种大气状态,引起外界温度随飞机高度增加而增加。
9 M3 d k8 m7 ]8 [$ m4 _6 V. T张力计;0 y* S2 i" t& s3 i
用于测量飞机操纵钢索上受到的张力的一种仪表。0 ?+ B T7 V5 Q) T9 g0 P
T# h' @: S7 D) w% a$ ?
制成T字形% I5 G& p5 C2 u# g0 b2 V" S1 a7 \
泰- G' d T( s" X+ X$ j
温( I/ w7 E/ m$ b( g& k$ Y
英汉对照民用航空词典B OEING
$ K/ b" }5 N. ^, |1 l" l) F& q& i8 FTECHNICAL DICTIONARY 1527 h1 I m( k! y% r. E
THERM
4 N/ c1 Z* G) s0 y) Pformatio
! e" X4 a6 m& r1 R4 z8 {) D6 ]using ho
0 F/ n# s+ F6 s! rAL ANTI-ICING, A method of preventing ice# S, l6 j" r% T4 l# O7 y2 g
n on the nose cowl and wing leading edges by9 H9 ~9 J D& Q+ ^
t air.
3 v" B' v/ c2 S" P5 W! i' F2 ^THERMAL t
: b" ]- V- h |( e3 a" b8 ~0 Zin a tube fo en tube& [! t" o/ r4 Y7 I4 z0 r
is pressurized with oxygen.4 ~7 [1 \; V( b
HERMAL RELIEF VALVE, A valve which opens to
5 F; T+ L9 n6 `: }, tture.( {' w, E; r: |8 m9 ~' v! N
HERMAL SWITCH, SEE -THERMOSTATIC SWITCH1 B6 x4 p. E' i+ v
e/ P4 s$ g( F( o+ }: h: Z
sistance changes with a change in temperature.
3 U7 l4 l" d2 w* z* k1 g防冰,
( e5 w4 g) g- w; J/ }4 G用热空气防止发动机前整流罩和机翼前缘结冰的方法。
" `, `6 _! J, y3 Q4 J在管子里,使管子受氧气充压时温度不致于上升的一
. E! d- t7 O' ?6 \, g, H* v个刷子形导线元件。9 S4 a/ O' J, {, F- A" i( J( w. m
控释压活门,
$ {! U g: g- Q( ?; J% H过高而打开,以减低流体压力的活门。
* B. Z0 k' g- F9 A' R% n电门,
0 z6 ~9 j8 K' K- {见Thermostatic Switch4 [; L; z! @+ h3 L4 Z/ J$ m
COMPENSATOR, A brush-like wire elemen
! j& G. s& t, ]r preventing temperature increase wh
# \, x2 a) P# j1 ~T
+ V; I0 A, X* v; Ddecrease fluid pressure due to high fluid tempera
. v! W( u- R$ U8 |T1 I" [$ Y) s. K: [8 K* p' j1 D4 C
THERMISTOR, A temperature sensitive resistor whos1 g8 D& ^* n) `8 e" g
re$ l9 E# Q2 q; _' }/ N( z; I4 L
热
# t' S F" J$ [$ l6 O热补偿器,1 l1 n1 t( s5 c1 G8 P' S
装' e7 m, E" t% ~( Q" }# M7 _6 f
热' p, B$ [8 W6 j# u, T
因为流体温度
% X& f3 w2 _2 v# d1 i4 b热
+ G V9 h( `% @% k$ V.
6 K- ~% _2 T3 Y' g,热敏电阻
; b, X/ y e, M5 Q( y一种电阻值随温度的变化而变化的对温度敏感的电阻。6 N3 U* q5 n- X$ a4 @7 l
英汉对照民用航空词典B OEING
, R2 Y/ A- t% o: `1 K" l: KTECHNICAL DICTIONARY 1531 J. r i- Q% e: v7 J% i
THERMOCOUPLE, Two different metal wires joined at
U* @ m) V& ~% e* }urrent is produced proportional to the temperature: {+ G1 q( V8 _, Q$ u0 N
difference.
$ r; x3 I; w- B: j6 ~: ]+ l* n8 yTHERMOSTAT, A component set to operate at a
+ x* W4 L4 d3 F1 H3 G" H( q Kefinite temperature for controlling electric circuits and
1 ~0 z$ Y+ g" K* U7 z( Q. o" zalves.: x' k: g Z- ?* ]6 F
mperature sensitive switch which opens at a preset# p9 l) b4 O+ r5 e, {7 C5 C! I, ~
mperature.
. E+ k% Q$ ~1 O' ?: _THR HOLD, SEE -THROTTLE HOLD7 l) O6 a( A- _$ y
即产生与温差成比例的电流。9 C. t' w" |+ y9 Z
用来在一定温度下操作,以控制电路和活门的部件。: F. \% I' r) b: T2 s: V
恒温电门,
- b- V ^0 c( [- y- T. G一个热控的、在预定温度断开的热敏电门。6 I! i) t8 E4 T9 ?6 U
见Throttle Hold5 U9 X4 ^8 D+ w5 E
both ends for temperature measurement. When both- C# l6 S$ b" R, M& x. o/ j T
junctions are at different temperatures, an electric
# f* a3 I: D# o) n$ L% x5 t0 a) ic
5 w& N% @5 t6 \& B$ H& C5 Cd
6 d& ]; r& e9 L' h, Uv ^( p- f: a$ e O w
THERMOSTATIC SWITCH, A heat controlled,7 J1 M9 S4 z$ G0 z
te0 `" g; K8 _3 w1 N4 b2 |
te
( \( y4 h! H" d3 H" v热电偶,( z4 g& w& M$ Y" I& b7 l' e
用来量取温度,两端相连的两根不同金属导线。当两端, I$ B: {2 p ?1 w$ x U6 e: V
之间有温差时,金属丝内. W% F8 q% m9 x7 Z' W, r# L9 G
恒温器,& K# n3 U: _8 |7 Y7 A2 \# }* t
油门保持,
7 C- `- G7 ?2 ~- g.( ]: k3 k% o# R! h
英汉对照民用航空词典B OEING; x; l( i$ y( G2 a' `4 o
TECHNICAL DICTIONARY 1542 } F, M# A* A+ b) v1 w B
THRESHOLD (NO. 1), The bottom part of an opening in
( R* C3 \5 t6 H# m- d) _a fuselage doorway.
$ @. ~) |9 Z: Y, A, h% U) ]+ z. q3 @1 c. 2), The approach end of the runway.1 M' z0 ~" }6 l, v, g0 H
THROTTLE LEVER ANGLE, Angle of throttle lever
$ n+ I) A2 N. ^9 U. g3 odisplacement.
" R3 r. q; A SHROTTLE SPLIT, An engine control condition in which/ }- ~" f/ O2 b# m/ X4 f
the throttle lever angle is different between throttle/ A" M7 I3 C' J* U8 h
levers but the engine thrusts are the same.. A( ?# V2 e. P |
HROTTLE VALVE, A valve in the fuel control unit for
: V e+ ^- H) g, g, ocheduling fuel flow to the engine.8 L N- R' E+ x1 k. W; r
机场跑道到场的一端。8 s& k: G7 D$ g: e
油门杆角度,2 L7 |3 N1 j0 U7 o1 u# |4 T* W, y
油门杆手柄位移的角度。; v+ n& }0 j2 r+ L9 G. ]3 T0 q
油门分叉,/ o- X$ M. R, I) g+ l
一种发动机控制状态。在这种状态下,油门杆之间的油8 M# E' L( q$ \
门杆角度不同,但发动机推力相同。7 } d! a# ?# K: S/ g5 r- o9 c
流活门,
0 o; h7 z) G! _% o3 y6 C燃油控制组件中,用以排定燃油流量的活门。; ]7 w) [7 s+ y; t/ k
THRESHOLD (NO
& @* `! X, {; k. }1 f: c |THROTTLE HOLD, A mode of the autothrottle where
' n& e: y: Y' H. |4 Wthe thrust levers remain where placed./ {: I, F {# N2 _* s
T8 k. m$ y! f( w- Q3 I3 N
T
3 g9 @$ J0 @' l0 [6 k8 ^! Ws. s" f* u, a; _
门槛,
( k/ O1 I9 @7 a机身舱门开口的底部。
$ K3 o1 a3 ?8 S" O4 M& n( {, y. [跑道头,
" g& G1 R, I7 k9 v, E3 {: q3 J油门保持,
4 I$ s& a0 M2 y7 @: [% X _自动油门的推力手柄不改变位置的方式。
5 d3 s7 P: X6 q; P+ z0 S6 X节+ d' l" { d, F4 y& r. { ~% d8 u/ ]
英汉对照民用航空词典B OEING
7 ~; {$ h8 |0 FTECHNICAL DICTIONARY 155$ k0 L# U1 G# }- u! s' s
THRUST, The driving force produced by a jet engine.
7 t8 ]% z" _% l7 M6 i4 h# U2 GHRUST LIMIT, Maximum allowable thrust for a specific+ A& q& Y7 \9 A7 o$ j6 r/ G I) ^
et of conditions.
0 o3 o% H/ I! m- p6 dHRUST MODE ANNUNCIATOR, A display unit or part
& B8 j. X1 P9 Yf a display that shows the engine thrust mode.: a' j* i# Z6 v1 d, W n
HRUST REVERSER, A mechanical device located in
* G- n8 k+ `# g5 m( g" E% C/ d4 k: C' Ke fan or exhaust section of the engine for eliminating
5 h' Y8 N0 A+ @7 H; @9 q% \9 ?rward thrust by deflecting fan air or exhaust gasses in
6 y5 m8 n- c9 H8 y4 M `e forward direction can be used for stopping during- o' u* I1 i2 O* ~* C3 g; T3 I
landing and during an RTO.9 @- [* Y7 \9 H; g
推力,1 g2 R' _0 ]5 u! ?/ X1 S
力极限,% |& G: l3 \0 k9 g5 u+ y
在一组特定的状况下,发动机的最大允许推力。
5 e. S4 V1 e: A1 p推力方式信号牌,
9 d- d, u9 O8 U9 `6 i/ e显示发动机推力方式的显示器或显示器的一部份。
/ M, _4 G; q% D" c2 s1 }, a Y反推装置,
3 J& r9 z! {- I0 _' R* }位于发动机的风扇段或排气段的机械装置。该装置通过4 x4 }3 G; G m3 U
使风扇空气或排出之废气冲向前方,以消除发动机向前的 h: l6 O8 c* I) c* W
推力,并减短飞机在着陆或中断起飞时的制动距离。
" I- [: {) x- i) Q9 _9 p6 X, \) k7 DT5 s! n% Z3 O: \* h0 G' u) T
s7 \0 t! c( J9 `* S7 n: z; `2 l" L
T: D/ i6 T' s T7 R( ~# `
o
k: x' }0 ^3 m% |: }% pT
3 X3 A' e9 A# `( C2 r! [; ^8 xth
' d/ n6 N9 a: @& Q) E8 p8 L. Mfo
) v& W0 S1 _* h H% x! w1 Pth
4 X) k8 z9 b' d3 E$ s喷气发动机的驱动力。9 D G4 Q6 T- }" a" N( G8 N, h. A
推- p$ q: S# q: B! K0 Y" k! ~
英汉对照民用航空词典B OEING
* a- U! b/ n. b/ uTECHNICAL DICTIONARY 156
/ s4 V2 R# T" X( zTHRUST REVERSER COWL, A cover around the thrust+ ?. e% @4 T1 L$ p8 I- C
IME DELAY, An electrical circuit for starting/stopping8 a6 K5 Q$ X" q+ g# @2 h9 V) k
e flow of electric current to an operating component( I, X# t0 j# [( f( J6 |
r a period of time/after a period of time." i+ B, ?4 W+ D7 q
IRE SPEED LIMIT WEIGHT, The maximum weight
, I% I' {0 Y: Tpermitted at takeoff that results in a liftoff speed equal to
( R# ~7 y4 f0 c3 [5 u9 ]) Ge rated tire speed.
3 D0 f d/ m i/ AOLERANCE, The part of a specific measurement that- F T; H, W( u5 c) E; h
allowed to vary in dimension. Usually given in a plus% n% u1 P- V1 ?3 U M/ F. b+ C
) or minus (-) format. {: |6 D) P' Y$ V
CLIMB, The point at which the airplane
& U: W6 K o/ dreaches the cruise altitude.$ I& p! ~) r; H
ts the cruise altitude and begins to t( M4 U3 {5 h, K5 V Y# [& R
descend.0 i7 h; Y& p/ h7 C( t+ E
for transmitting
4 ]2 }* h6 ~1 htwisting motion to the control surfaces.1 e6 G5 B e; |( Z9 ^
,
8 e+ p$ u* E4 M& @* o* w) N0 k的/ W+ t( A2 P K0 |6 W/ w
部件以进行维护。
$ x( u7 w8 S) Q- T8 G+ U. S延时电路,
$ }* \; U$ g" V用以起动/阻止电流在某一段时间内后进人工作部件
8 F: t. _2 E& s' ]0 |的电路。
, i2 D9 I1 e# \) g" e4 l1 G轮胎速度限重,
8 x+ d3 Z9 P0 q9 z飞机起飞时,使离地速度和额定的轮胎速度相同的允许! E1 F; J2 R, i ?5 z5 X
最大重量。 a3 K' N( S% A. `& L' Q
公差,$ h$ b- t# T8 a8 y
特定量度容许有偏差的部份。通常以(+)或(-)
; h& U6 _8 n `的形式表示。4 h, `; L; d2 s8 t- j+ m& R+ n! C
爬升顶点,1 R+ i/ R' V* w( N
飞机达到巡航高度开始平飞的那一点。
$ u/ Y% }* y# C5 F下降起始点(TOP),
/ \- i' i0 k$ y# s: k飞机飞离巡航高度而开始下降的那一点。2 U; t: I1 \6 _) h6 g/ h% }8 a* x
操纵面的管状部件。% y/ j! \6 }7 c4 i5 u9 ~4 L! x
reverser of the engine that can be opened to access
& b/ O' S) a0 l6 Xcomponents for maintenance.; x7 r5 P% ` r+ Z6 V) o. [9 v
T
, r# S; a% F' Kth* ?! r# @- ^8 Z
fo
/ T: J4 {8 ?( W7 V% O% DT! O6 C2 U* b `3 a
th( m' C+ h% L* V# z3 _: p
T8 i6 R" c. b8 q1 \% Y9 M
is
+ y* n6 p& u) z1 T(+
4 r, T* D9 B' A& z2 H6 R6 MTOP OF
3 [- N3 [$ o( T- vTOP OF DESCENT (TOP), The point at which the
$ S( ?4 u9 G& b2 g; H* Y5 F( cairplane depar% P& l4 M0 a1 h
TORQUE TUBE, A tubular component0 \' Z3 d1 \2 K( T5 v% ~9 x0 ]4 N
反推整流罩
$ T7 G( E! m; g5 B在发动机反推装置外围的罩子。取下后可以够到内部( q' Y) W" _9 Q
扭力管,
' Y, |$ J: d( H) l1 H用以将扭转运动传给: L8 Z" U* f% j7 b: P+ S
英汉对照民用航空词典B OEING: r3 V6 _( B5 L" i
TECHNICAL DICTIONARY 157% N4 `3 t( @. B
TORSION, Twisting of a material or part caused by
6 F1 f; {6 J: C# v7 \1 C; n, Sexternal stress./ U X6 v& \6 V8 n( [
ORSION LINK, A hinged linkage connecting the inner
# }) l# H8 m* L: c8 ?" q# |7 Ond outer cylinders of a shock strut.1 |7 J- _& P* r. K0 b* I
due to the ram, U0 R U' q+ Y! ?
ffect of high speed flight.. @0 x) H0 @6 m/ `) p; k
URE, Pressure higher than ambient
8 ~2 X5 |' r N+ z0 Y" cressure due to air flow, measured in pounds per! ?2 G. h% \# U; j3 e
quare inch (psi).
/ ^7 h2 A. E# {5 [8 J- F7 c- [; ger than
3 {* r7 l+ C2 ^5 ]8 x, |! |( ~& E0 Gmbient temperature due to the compression of air flow,
2 Q2 x/ F( r% b/ M" Eeasured in degrees Celsius (C), or degrees
' Z; T$ l* e. H4 ~ahrenheit (F).6 ?( m; ?5 X g2 j
TOUCHDOWN, The point at which an aircraft first
) g- E" @! ?8 s& N0 gmakes contact with the runway., U& L/ l% |+ G+ I
生的扭转。
8 n& X3 I+ }& k: a- I/ g. D扭力臂,/ S2 J7 x, p4 `0 o: f- p' @6 _
减震支柱的内筒与外筒之间,用以防止活塞旋转的铰链
' g+ h$ i( u7 k连杆。
$ i6 ^* }0 H2 k9 Z+ V7 ?( a3 y1 f的冲击效应 r( s0 ~' y; f/ j- s: Q
引起的温度的升高的总和。' [, x4 ~* s$ }- ]5 B8 z; [3 m
总压,
0 k3 k& P8 O3 @3 {$ w) s由于空气流动而高于环境压力的压力。常用磅/平方英
+ t1 A. z2 [, q! E! A7 }2 B(psi)来度量。* F' }; l4 R& B" r# N
全温,
( l0 x x {* {1 m8 u. W) R8 ^- \; C由于气流的压缩而高于环境温度的空气温度。用摄氏6 `8 U/ y9 F' I( E
(°C)或华氏(°F)来量度。
W6 n) L4 w7 A/ o接地,& l( Q9 J* s* g+ N0 c5 Y+ L
飞机降落时,飞机最先接触跑道的一刻。
9 x4 ~+ m; ?' `/ ?: j. @T
9 i. T" q/ m4 a4 F5 ha
- q' x' g% g, Q! C9 B: f/ sTOTAL AIR TEMPERATURE, Ambient or static air
" p9 c: F8 U( x% W+ ztemperature plus the rise of temperature0 ^5 e- Q3 X. D; o
e5 v" o; a, _! i. r4 A# g
TOTAL PRESS
) r" O) N4 ?# sp* s" A4 _ \. K! N# u
s
& C9 |8 l6 `4 M/ sTOTAL TEMPERATURE, Temperature high
7 f( P. ^$ b" za
$ i; y0 X4 _" h, ~5 o, {, ym
) `* |4 k5 b; t" e0 _* eF
0 H# a7 f0 h$ B' A/ k扭曲,) w& R1 V3 j2 w6 E; J4 W/ N* A
物体受外应力的作用所产1 T7 H; ~# W4 B8 A2 F w' o) A; P
空气全温,
* v. y b/ N8 B$ C( \& N环境温度或静空气的温度,和由于高速飞行8 p& n" t* [) E: D2 j
而
% S" K: a# R1 o寸: ]8 `0 J y3 C; |7 q, _- R
英汉对照民用航空词典B OEING
7 D+ b+ S2 w! f5 |' sTECHNICAL DICTIONARY 1587 t6 s3 [; u! S2 C, s
TOUCHDOWN ZONE ELEVATION (TDZE), The
5 @8 G6 u" J9 w7 h5 K' a# Fhighest elevation in the first 3,000 feet of the landing
" y1 `) \- d( u) I& E7 ~urface.) @2 {5 a- Y6 x5 `$ { I* Y N
rt of nose or main landing gear for
! }- j, P8 d, B5 t- p# C9 E1 F: Nttaching a tow bar to move the airplane on the ground.$ R! E; i6 y; g, x7 T8 v1 K
along.
) I/ J9 l( U2 X3 oRACK (NO. 2), A navigation term that describes the& u# E3 T1 D! `6 k6 d0 \
TRAFFIC ALERT AND COLLISION AVOIDANCE
8 M/ |5 R, e3 e' k1 s% B RSYSTEM, A system designed to alert the flight crew to
2 O9 S9 E, C* Gpotential conflicts with other transponder equipped
, m" \: j% l8 ?0 s) l' E' Lairplanes flying in the same area." e+ c f' v4 {' `! {
TRAILING EDGE, The rear edge of a wing, stabilizer or
0 J# Y* d! ?; H& n! Pcontrol surface.
( U5 K$ i3 u/ j; \ lTRANSDUCER, An electrical device that either takes1 r, p0 L1 M7 K$ D8 q5 Z
electrical energy and changes it into mechanical
) c2 D! \" y: a$ ~" u4 emovement, or mechanical movement and changes it$ V, Q; W& M2 D( e, Y6 g. @1 H
into electrical energy.
: P) Y% l, h! d( D( PTRANSFER GEARBOX, SEE - ANGLE GEARBOX \) D% U. ~0 J
高(TDZE),' G% w8 \9 ?% j8 \8 C! t
高标高。
' _) y$ y& G6 ]3 B" q& G- t前起落架或主起落架上,用以接上牵引杆以便在地面上
1 p- B# P8 `5 `! W( D" r0 C0 S1 m动飞机的部份。
& X% w, W- E# O4 m3 O轨条,3 t+ |' t* @6 \! V
迹,
$ _# Y- l& h7 w; W形容飞机航迹在地面的投影。
4 S8 M# F9 _6 Q& n9 D空中交通警告与防撞系统,' I8 ^, l; G7 j: e: Y% ~& Q
用来警告机组人员可能与其他装有应答机且在同一区
7 M1 G8 e6 Q; D/ w+ N域飞行的飞机有冲突的警报系统。
- g; v, Y+ G) R后缘,7 z; V$ p% b/ b7 `) K2 z ]
机翼、安定面、或操纵面的后边缘。
# Y8 e) `0 `0 i& g换能器,
2 K+ O5 Q/ d8 f/ R7 x/ _7 t能将电能转换为机械运动,或将机械运动转换为电能的
- ~% `1 b& Z. l( t8 p5 a, m电气部件。; J7 [. |1 Z1 Y7 `( h
转换齿轮箱,+ z1 x$ |* y L1 D
见Angle Gearbox4 G0 q: H" [3 @& t' {2 J
s
! c; `( ~- g9 R7 o; N/ rTOWING LUG, Pa
# H$ v6 a- b2 na
6 N% H6 t9 X2 ] lTRACK (NO. 1), A structural member for attaching fixed
& j; w4 {2 S" D6 gcomponents to, or guiding movable components3 o9 [3 S9 J$ O1 ?' F3 D
T
2 `1 u, H2 j4 p9 j9 k8 `projection on the earth's surface of the path of an( @/ `" ]8 }* Z3 j4 @- m/ g
airplane.
6 D2 g8 |8 q$ n0 w0 @8 `接地区标
6 ^. w6 H1 f9 H/ x跑道头端3,000英尺的最1 @4 s+ w& ? s
牵引环,5 d+ L( y) S2 P1 u9 i
移
! H9 Z# p+ O4 n9 u v1 f9 K4 I, a用以接连固定部件,或引导可动部件的构件。
# ~% b& {( [- p- ]+ r航
$ j+ q9 O1 d1 v' ]: K导航术语。
& D7 y2 a, T7 i) s/ Y& l1 Z) u.& t0 d5 v) k7 v
英汉对照民用航空词典B OEING
* ?* t. B1 m: u+ t' [TECHNICAL DICTIONARY 159
4 q( |4 p2 k1 M+ }# ^6 hRANSFORMER, An electrical device which uses
: C# ?: S, k& p' u( A. T# n% f$ F0 pRANSFORMER RECTIFIER UNIT, An electronic
' |( n) q! N7 [ \& hevice for changing alternating current to direct current: }* x. f8 s6 j F1 P2 F
supply airplane electrical systems.+ j, Z9 U$ v i+ k3 S# ?
lse signals or triggering pulses
/ b ^: T' Y- W4 L* Q7 S' a/ }nd cause component breakdowns or failures.
/ a5 g) E8 W- ?' I. }" \2 K1 u3 NIt consists of a base, collector
+ N$ R& `: `5 Y) G1 y% J" tnd emitter. Two types of transistors are PNP and NPN.
0 {" R7 s% s. L9 r. T* a, x。
* C$ X+ m8 P! r变压器," R0 A1 @$ j6 u p& ?
磁感应,将电能从一个电路转换到另一个电3 B- L$ _* q% I3 k/ E6 x" I
变压整流器,! e! r3 H% y: {
用来将交流电变为直流电供给飞机电气系统的电子装7 Z! J+ `: |( n' Z/ @1 s/ v
置。
. a9 ^. D0 T& S$ w A瞬变,# j5 L: O! t, o J& J* z5 K
信号或输电线上的瞬间电涌。这种电涌常会产生一些错
. W" h, D" L( X3 `: ~误信号或触发脉冲,造成部件故障或损坏。
: O' @$ Z4 a. i7 r, ]/ P& y' v晶体管,4 G8 y# R3 Q+ w
固态电子部件。通常具有三极:基极、集
. \4 [. u/ X) E" m( f8 v' U极、和发射极。有以下两种:& ]. U1 z# y/ C2 s2 h. D
PNP(正负正)基极电位低于发射极。7 v- B& w9 z7 s* t4 R
NPN(负正负)基极电位高于集电极。
$ n8 C" n4 V1 Y8 HTRANSFER MECHANISM, A component for# w8 i- a2 f) _) P: @) o
transferring motion from one place to another., f* m, q0 g3 }# W" x. G
T; ^4 ?, n5 T. d. Z: @1 I) I. I4 g
electromagnetic induction to transfer electrical energy/ O5 Z% E5 Z( [( T: @, E
from one circuit to another circuit.
& E: H6 c7 {2 ?8 K. R, D% x" g/ {T
7 M: v2 T: C, Q5 d; D9 Ud
' y( f# v6 s5 c K3 ito, v: O0 x n- A* k8 Q2 f& U' f2 B$ A
TRANSIENT, A momentary surge on a signal or power
- B" Z" [' y" v4 Eline. It may produce fa1 s0 S1 J# p5 a
a6 P( b! j- g) P: F
TRANSISTOR, A solid state electronic component for
% \3 f, e4 C7 a2 R cuse in electrical circuits. Q+ }! l; s0 v: K5 {) [8 j0 h0 q1 L' p
a
4 g$ E# R1 T& q9 B. ?' P. `转换机构,
" b7 N0 @' j0 x将运动由一处转至另一处的部件% H8 c5 X6 J. D1 p( r) ~# o# B8 q
一种利用电
3 v* W' L( g, S1 e, a路的电器装置。- x# h* L; V* m2 }3 S2 I
电路内使用的# F# h2 i/ ^5 u3 B6 c/ [, f
电( ?5 x) R7 k s4 W
英汉对照民用航空词典B OEING) \: A, j6 }( v: d7 T
TECHNICAL DICTIONARY 160/ `9 j; |; `* _& m( b( i
TRANSITION, To change from one phase of flight to! E6 v: H) `% z. j3 w" Z
TRANSITION ALTITUDE, The altitude at which the/ a, Q) R( U: t! ~# p
ltimeter setting is changed.
- E; W0 t8 V3 ^+ h2 }* bRANSLATING COWL, The movable outer portion of+ {3 s* J; O8 D/ o1 ^7 T
e thrust reverser cowl which is operated during( n7 s( U e( o0 T$ X3 X' a
verse thrust.
3 g( R4 t+ R0 D! `RANSMITTER, An electrical component for sending8 n9 `' z5 N( @) \- D# ~* @
formation from one location to another., G0 y2 W9 r% D! S" T0 M
TRANSPONDER, A radio transmitter-receiver which" b. a9 u7 m: h. f; T
ansmits identifiable signals automatically when the4 ~' k* c* c" l( R" T
TRIM, The adjustment of engine and airplane controls
* r: G4 e4 Z. p5 |. ?从一个飞行阶段转成另一个飞行阶段。
. m# `: z3 e2 z3 V& W过渡高度,) d7 c; C0 w9 L
改变高度表设定时的飞机高度。7 A* }( Q4 G% \' U& v
平移整流罩,0 c% E( {/ v" B; m* l
反推过程中使用的反推整流罩外面的可动部份。
/ f- o- l: c# w% o. k4 `8 A9 s发射机,
( `1 ^2 v' Q) e$ }& Y8 w' P将信息从一处发至另一处的电气部件。
3 M4 h' `" a: G! s应答机,, n9 t% P+ }3 a2 i
在收到合适询问后,能自动发射可识别信号的无线电收
3 b5 B& L7 E0 b. T9 K; Z. r+ [ @# y发机。
0 U" o6 k; k9 O( \1 H, s平,% x$ G. x& L# p# z& Q; i. c
动机和飞机在平衡的状况下工作而做的发动机6 a+ r6 b% M* d0 o
another.
5 U2 K B0 `0 H9 n6 ^* Da
9 p g d8 d! | GT6 W1 |4 J8 r2 E% J
th
, I! ?& b( U9 v5 a. Are
1 Q1 @3 ~6 j1 f7 s5 \# WT
, n2 O1 z" d& v* Rin
3 P4 x9 ~1 m8 H' r; ltr
( q3 A, \; ]+ A0 y& m$ T- ^, u! zproper interrogation is received.
/ ]6 W O B" J* Q# b- jfor a balanced condition of operation.
$ b% o* [2 R4 X6 j, S5 V+ @2 i+ h/ Y) P过渡,
4 e0 G5 z5 _" ]. `* i" Q- q$ Q. V配2 o1 R0 \2 s# R; F( J
为使发& n. @+ ?8 r8 J ~, C
和飞机操纵系统的调整。
6 F. @! \ e1 A. D英汉对照民用航空词典B OEING6 X3 E5 H& b4 U6 \1 |
TECHNICAL DICTIONARY 161
7 D% ~6 @% l9 tTRIM TAB, A small hinged movable part on the trailing9 @3 [- Y0 P- e5 d
edge of a control surface (aileron, rudder) (see TAB).% H" f% L8 u9 u+ U+ j$ }
L, The total fuel consumed from brake release
' Z" [6 ]; q, c* \2 k5 ]through climb, cruise, and descent, to landing at
2 h/ W" J! B3 R1 s% r* ~; Hdestination.6 A3 |7 C. P! O' V8 Q
RUE AIRSPEED(TAS), The actual speed of the9 B9 |- @7 I% o
aircraft in relation to the moving air. The true airspeed is
. d% y& i0 m% c8 h7 Kated airspeed corrected for position
|7 P3 I* P$ r3 `" ]$ q$ L1 d0 [rror, compressibility, and temperature effects.
5 B, k# X! ~5 ]& g+ n% \# iribes: o* \7 I- \. q. o
the output value for each input
d9 X5 T) x) Z g C+ M. k$ Hombination." X1 k- {1 M% V2 Z! K
铰连在副翼和方向舵等操纵面后缘的可动部份。4 R$ U9 P# P$ F: e2 E
航班燃油,6 I' J y$ W% w9 i
一个航班由松刹车开始,经过爬升、巡航和下降,到
' @- ^9 K' L* e& A; J' c: C; V目的地着陆为止,所耗的全部燃油。' E; n2 m: b- O
变压整流装置,$ \: O0 g9 J, |3 P
见Transformer Rectifier Unit Y! O1 J: @! g9 _& S1 j
TRIP FUE0 u4 ]" {9 M9 \, d+ c# J
TRU, SEE -TRANSFORMER RECTIFIER UNIT7 }% @3 K5 y2 a. D8 t! L
T
+ w; f, M. O6 b& l6 W) dequal to the indic
2 h. N Q: u& p1 ]: J- Ue
* A1 H8 `/ P5 A! `- |+ V$ T. pTRUTH TABLE, in digital logic, a table which desc
5 M' _) d# l; {: Wa logic function by listing all possible combinations of
7 C' D- |5 }3 F p0 Uinput values and shows
( a% c! r1 f6 h) }9 F. q7 `, Ec0 m2 h$ f+ _# [2 V
配平调整片,
9 _4 j, n6 n+ J" P/ `! U在
7 c8 L) X& M2 f ^$ d+ l2 l.: ^$ B; E! o3 s9 F1 T; \% y: o
真空速(TAS);
$ o3 k9 C8 a) a6 p! Y$ R对于流动中的大气的实际速度。由指示空速经过" O3 `7 g B, T1 ]+ j
真值表,1 h. S! G v9 y0 l; G$ j) W8 k# L( O/ a0 s
数学逻辑中用来表达逻辑函数的表。该表列出了所有可+ b3 |3 {6 o- K
能的输人组合,和每个输人组合所产生的输出值。
$ J4 ]: E" d8 F, Y飞机相! m! R+ g, L( f" w5 x
位置、压力和温度校正而得。" n8 Q% M! a) `0 d3 w
英汉对照民用航空词典B OEING! K" S- o+ j: t( A7 ?
TECHNICAL DICTIONARY 162
; p$ ?1 n& u6 h- L8 r4 h: B. y& N2 eTURBINE, A rotating part of an engine which
6 x4 W Q7 U$ {9 N+ B- P- kkinetic energy from the combustion chamber ga
" {* o; @- F; m3 Q$ k$ X8 v0 f5 bextracts
# `! B _( Y5 X5 k! |ses.
4 P. B. i! A) H+ ]his energy is converted to turbine rotation which
" A/ t% i$ w. q$ h% l0 x3 t* states the compressors and fan through a coaxial
' B. j9 I8 _; C+ qhaft.
9 c! ?0 a& L! @# p; u) {+ UTURBINE CASE COOLING, A method of cooling the) \9 P- V/ P5 {. a2 l
ngine by using fan air. This cooling process is used to r( T- ?8 o7 r# t5 r6 a
TURBOFAN,
' @, S/ g; L$ e, v4 z9 S! M$ j(1). A jet engine in which the first set of blades is a: ^4 Y3 N* s# ?
large fan.+ U _( m. O, a% ^: b
(2). An air driven fan/compressor used in air+ c% w4 F/ y4 u0 X8 K- r4 @/ i7 G
conditioning system.
, E* i6 z! m- n# B* f$ B L3 zTURBULENCE, The movement or shaking of an) ^) U+ q& Y! N/ b/ e. e
airplane caused by unstable air masses.. Z% b- E. _- s! z. z
涡轮,. U1 X4 H5 H2 a# s
发动机内,从燃烧过的高温高压气体中撷取动能的转动8 x/ }& l" z6 W' s* v! i
份。该动能使涡轮转动,涡轮则经由同心轴带动压气机2 b9 e$ N* R2 W6 S4 N/ G
风扇。
/ o' B1 L. w+ s9 T& K0 K7 d涡轮机匣冷却,
+ p8 C3 c2 s' d8 [/ R; _用风扇空气冷却发动机的一种方法。该冷却过程被用于! B4 V/ e8 u# w) K9 `8 ^
效率。
5 c4 v7 p7 J( J(1).第一组叶片构成一个大风扇的喷气发动机。, d" S* ]" v0 N9 M7 e, Y' p' ?
(2).空调系统内的由空气驱动的涡轮和压气机组合。
4 R6 o3 r7 I( e- w' `颠簸,
4 J+ L0 y2 E6 ^* f由不稳定的空气团造成的飞机运动或抖动。
* {3 f# y$ x- w; g/ c2 \' |T1 e: V H k; j' b) B8 P" N
ro# }4 D. J- X, s
s
2 X% @/ B2 m/ N E% Qe& [7 Y/ ~3 z0 k
increase engine efficiency.
3 s9 e! d* C% H7 d: d/ v! @部: C+ Z+ k$ H" K- B U
和
' _! y* B0 I5 v提高发动机
& B+ i( R6 w* U V涡轮风扇,0 s/ N3 \+ N& _% ?3 a; q# H* L1 Q
英汉对照民用航空词典B OEING
1 {2 D+ n+ ~2 XTECHNICAL DICTIONARY 163
3 a3 _" A! R {) R7 O+ m& aTURBULENT AIR PENETRATION SPEED, A speed
, M! D: X0 ~" E9 D9 j) tthat provides adequate maneuver margins when flying5 R4 S v4 j9 D3 M2 h; Y. S
to unstable air masses./ D! b# U: U6 a+ D
ht
, s: Y5 ? x, w: `- \0 ?- V: e0 Wstment in the control% M, j% e r: R0 B
ables.
# |) O( F; k6 B" { yUHF, SEE - ULTRA HIGH FREQUENCY" y* O. g0 _. W/ |( m
NDERCARRIAGE, SEE - LANDING GEAR
; F/ }2 N3 t9 l, f1 l( AUNIT, One of the type, a single component.% R* \9 C$ F# Y- K' _
UPLOCK, A mechanism on the landing gear for keeping
+ v! C5 P+ Z0 Sthe landing gear in the retracted position in the wheel
( L* p; O5 S0 \9 a7 vwell.
) H6 k0 x+ S, K8 \" `* D: a速度,
+ Q( j" K( |+ \* Q9 A纵裕度的速
3 \; u' T* Y' o) g。# m# E7 \5 p7 x2 M* d0 J
调整操纵钢索张力的: h: L: R/ C u* M
械装置。
1 B; k" n! H9 \- d高频,
; R8 V& r0 e# g9 i见Ultra High Frequency
- ]0 o" C3 W" I2 V8 @" Fin, w4 ?: d: @+ ^+ G* q7 x
TURNBUCKLE, A mechanical device with left and rig1 i" @2 q/ G: u3 {, V/ I' D
hand threads for tension adju3 g) p4 m5 T, n, T o5 ?. |
c
; `9 [7 K% ~' U8 U$ r$ g0 DU
# B; j. u) S8 e- d& {5 M3 B% EULTRA HIGH FREQUENCY, The frequency band% p6 ~# D$ ^3 z* m, N' y: V
between 300 and 3000 MHz.' W) s/ N! D; R& T" t
U
0 `2 u3 @% R( O' ?+ B8 l颠簸穿过6 V/ u- c) O- r# X* i9 {4 |; R
飞机飞进不稳定的空气团时,提供适当操
" `& \ F0 a5 ^. k& u$ Y度
2 k% x5 h( v1 p6 Y7 W; r: h松紧螺套,
+ f P; m. K8 A# Q具有左旋螺纹和右旋螺纹,用以% K+ a v* x/ z# G8 O$ l( r/ O
机
& [# {. q5 u" F) l超5 ]! u0 E& Y' a, Z+ v- w' j
超高频,2 P" \# I) L! Y, [$ f
频率带在300 MHZ至3000 MHZ之间。7 F$ [1 F5 a; a
起落架,( _# G3 }6 k7 o+ {( X; n% M6 v
见Landing Gear1 P0 V- b; j- M! `2 ]& k
单元,
* i+ |5 J1 m4 a' M7 y某一类型或某一部件。
: X4 t( b3 m* d* v7 \6 E/ L上位锁,3 {$ n3 ^1 S& P$ I; q1 f" M. G; g1 o% _
起落架上,用以将起落架保持在轮舱内收上位置的机3 s# X g: H5 K- C
构。
1 {5 c. T6 B5 S2 J' Q英汉对照民用航空词典B OEING" S5 l, {8 |1 K- [! d/ J t
TECHNICAL DICTIONARY 164
" _* g; Q- d% D6 \3 U! SUPSET HEAD, The head produced on the tail of a rivet. j( t4 R$ t: p
during the installation driving process. (See% g% W. _, @: k% T1 f9 U
Manufactured Head.)
. W. q( E; X! V) T' B) t5 s1 (TAKEOFF DECISION SPEED), Is the maximum' P3 M' F6 E; a* @1 d
peed at which the rejected takeoff maneuver can be
, c7 Y! ^4 H8 qitiated and the airplane stopped within the remaining
1 p, O5 R/ m( T$ held length under the conditions and procedures defined. V& J. @. i$ j* r& p% X8 Q& v
the FAR's. It is the latest point in the takeoff roll where
5 s9 w& X7 j! u/ lstop can be initiated.
7 P2 e2 u( D, e) ^' b1 e% C9 ?5 ]1 Hssure9 O, a5 }6 r, N \) J9 r
dient capability and maneuver margin.
- o% a7 l. X o! BVACUUM, A negative pressure or pressure below
8 F0 x; t6 M1 V+ _atmospheric, measured in inches or millimeters of
) l. K% x$ L, p4 eercury.
6 H1 f7 ~9 a+ u: K- w1 m9 |* _5 ris
5 E( ^. P- ]. a8 N0 KVENT, A small hole orifice or restrictor in a component5 I( F. s2 j7 E- ~) A. |/ S; f9 y1 M0 d
for allowing pressure in the component to be the same
* e2 L+ |3 a' }, N: W O/ ~as ambient pressure.8 `' z8 Q6 @. x2 l
在铆钉铆接过程中,铆钉尾部一端形成的凸头(见
/ j3 d" @. ?' bManufactured Head5 K% Y, I% X( E" {* H k
V
# x6 Q" _: a V, `$ D0 G5 oV
& g( j7 d' ~4 D$ }+ x# Cs% n& F: ]5 C8 w8 h. W, @" K4 @+ ^
in
; F" R4 P; e+ R4 d( sfi
7 q; Q( j& `! H" t$ F' qin
0 e! w4 Z; P' e- t4 S- T3 oa
2 F( W1 |! }# Y: p ?& iV2 (TAKEOFF SAFETY SPEED), The speed flown after! a+ M) c0 H* p' t. |3 Y7 N3 G# i. C
takeoff during engine-out climbout maneuvers to a
' W( t2 ~* A* c8 u! {! B4 Qadequate gra
: A1 i0 A1 Z$ X8 xm. X' i) W+ P, V" d7 H
VAPORIZE, The mechanical process in which a liquid
' ? ]$ W9 f- ichanged into a vapor.
0 q; G8 c/ a, @VECTOR, A heading issued to an aircraft to provide ~! r& ^: j7 l5 {( @: ]3 S
navigational guidance by radar.; k! A; t1 w4 S
铆钉镦头,
* \7 W2 V+ k7 r6 v)。
% X. q6 G- \5 @1 [1(起飞决断速度),; t+ U) [* p/ b1 O; M
根据联邦适航条例的规则和程序,飞机能进行中断起飞! n* ?, Z; d, G; x/ f/ V7 o
在剩余场长内停止的最大速度。它是在起飞滑跑时仍可
, |( E1 w; `5 L, q住飞机的最后决策点。4 l5 l0 o. ^& Z: i# {
速度),
; o) ?2 U8 P$ H! M/ o8 f在一发不工作起飞后的爬升中为保证足够的梯度能力- W+ r. s& o3 @1 R0 y4 ~8 b
和操纵裕度所飞的速度。; Y1 H+ Z% O. n7 W" G
若干寸(或若干毫米)2 `# i% P1 k3 W" d; Q7 a* B
汞柱。; {( e7 n f$ x
蒸发,
- E/ v* p2 M+ R' C8 `8 @液体汽化的物理变化过程。: t: V- C" ?$ q2 P* _5 K5 ]
引导,9 ] ]' W& _- l: J
由雷达提供的航向,以给予飞机导航引导。) V2 H1 ~9 D! d7 X
通气装置,
; V l. i- ?: C! ]部件内,用以使部件内的压力与周围环境压力相同的小
( P2 n( f) L2 f3 \! _* q7 l孔、或限流器。0 a3 r \$ f. h
V# f8 M6 v0 Z, V- l$ m5 s
且/ W0 V( M" ~% D% Y% [- z
停
! b A! L$ x! I- VV2(起飞安全
( E7 M, l6 D q+ G1 r; w* k4 L5 t真空,
7 O. S8 e) n0 l; @负压或比大气压力低的压力。常用7 o+ ?5 a0 H. q& Z9 B! w8 o) V
英汉对照民用航空词典B OEING
3 W( G9 t8 ^* o9 l9 ]% ^TECHNICAL DICTIONARY 165; S, K! J6 V/ |. E( s% j
VENT SCOOP, An air inlet/outlet on the bottom skin of
' l- j0 q3 K& J2 dir" g9 J# A& v r6 e
VENTURI, A part of pneumatic duct with reduced flow
5 H+ j: @! @0 I% R6 f I; Nrea for airflow measurement. (Principle: As air velocity
5 S6 a$ I" X* \, O2 m$ K/ [1 ocreases, pressure decreases).
/ T4 A3 ]( K+ t9 e cERTICAL AXIS, A vertical axis passing through the# `) B! q) |' z, g7 Y
airplane from top to bottom. Airplane left and right P. X1 t. Y1 e ~$ Q$ F
trolled by the rudder.
U9 o3 Z6 y4 l) d; |, S- FVERTICAL NAVIGATION, Functions which provide1 F% X ^, h( l) R3 W5 U2 k1 L
guidance signals to control the aircraft during climb or. }/ {/ ~& W8 K, Y- q( W
descent.
5 L1 ]5 ]2 c/ a./ u. T' ?: D% k- @# G$ g
通气进气口,
+ }3 ~- r4 G/ x7 d0 o& W: L* `位于机翼下表面蒙皮上,用以燃油箱通气和提供燃油箱
a! `5 K6 [; e/ Q! _. L& R内正气压的空气进出口。
2 y6 e# d- m" [9 M文氏管,5 ?- h9 Q" K$ z! v9 g
气源导管上,导管截面变小以量取空气流量的那一部
' N& o& _) R U% F- D5 g+ r份。(原理,导管截面变小时,流速增高,压力降低。)7 F- E9 ?# ~3 i2 Z
垂直轴,
4 [- R% Y8 K4 t4 [2 G- r由飞机上部至底部的垂直轴。用以操纵方向舵,使飞
2 G4 b# l$ e, i; g) P5 A. i右运动。
' C' X( o4 |+ _9 W直导航,2 N* S1 ^- S! U0 `; u
,
, u" y$ v/ A2 B" h3 f2 u$ qthe wing for fuel tank venting and supplying positive a
1 G( _ f9 B6 Wpressure inside the fuel tank.
4 [- v4 m" }1 x+ \( e- l3 ? Ra5 u7 s$ z; r2 }3 H' ?
in
3 Z$ V# n) R% O: n/ Z( zV
+ T% u7 Y3 E4 h h3 ~movement con) d; k3 a/ ^& ^9 K
VERTICAL SPEED, The rate of change of altitude
* z& T. h& K! D) i机沿此轴作左4 ^2 b k! R3 W# x/ s$ B$ H
垂3 k& K. s2 m1 }4 R/ _# a/ {0 R1 S/ t
在爬升或下降期间提供引导信号以控制飞机的功能。1 ~0 A. b& T: E; Q" J% y- L
垂直速度9 t0 ?# G& Q4 q) u. v
飞行高度改变的速率。
4 T+ M2 |7 n1 e7 t- [: I3 ]英汉对照民用航空词典B9 A0 N1 j$ q6 I: V- j
VERY H7 D* {/ Y$ N4 ^+ ~1 ?
OEING
; U! i" p$ x* D5 PTECHNICAL DICTIONARY 166
9 d3 v) {) Y, B2 B. j/ [VERTICAL STABILIZER, A vertical surface of the" h% c2 b9 b: X7 Q: C8 {
empennage for stability/control about the vertical axis., [1 I' g X' S
VERTICAL TRACK, A climb or descent profile.3 V8 ?9 v. H, P9 ^
IGH FREQUENCY, The frequency band
5 m, @/ K, b; |4 dVHF OMNI-DIRECTIONAL RANGE, A navigational
! q9 w' m0 s- l, u0 h# Dsystem which tells the airplane's bearing from a VOR3 r5 V/ q& E. d2 N
round station and its deviation from a selected course% R. h- Z* J( B- t5 c4 d: t
/from the station.
1 a2 }% h: N. HISCOSITY, In a liquid - it is the resistance to flow.
! x1 ~ \4 ?+ B- BVMO, The maximum design airspeed at which the; n2 c# y, n" v P$ h8 ^! d
airplane may be operated.& p l. s4 t- t; u. \/ e
在飞机尾部,用以保持飞机绕垂直轴的稳定性和控制: R. x! U& ]* I
的垂直面。
# J. I( V2 A& a- L z垂直航迹(VTK),8 d# o$ i3 |2 [8 b! E' j1 j1 @4 x
爬升或下降剖面。
+ W: `7 @* H* D7 V$ z甚高频,
/ V" {1 T) |6 ]30 MHZ至300 MHZ之间。between 30 and 300 MHz.) P& Z% U, b$ f" Y1 u# G
VHF, SEE - VERY HIGH FREQUENCY
; M/ F9 _' Z9 F$ y8 Rg1 y& E% U2 x/ z' I, K ~
to
6 o. b" M' S3 O8 v( KV) L3 f0 @& K6 }- H
垂直安定面,
, ?( B/ A, I# x# ?频率带在1 j0 u) ?" m8 A. l9 Y2 U
甚高频,
8 [' w8 m' {- \8 Z7 w见Very High Frequency2 |7 N, z5 R% S8 r7 V j* B& H0 |
甚高频全向信标,8 x7 I) _8 y1 ` ^8 v, B
系统。该系统可提供飞机到VOR地面台的方+ o) `/ j# A4 y, c6 ]
位以及飞机的向/背台飞行的航道偏离。$ r1 {5 g5 h! P( y
粘性,7 E$ `% ^9 B3 C
液体中阻碍液体流动的阻力。
& [7 c1 B; _' `" N9 z& A最大使用空速,
$ w, e* L& E! g v飞机可使用的最大设计速度。
4 R' `1 @* ^! f2 L+ ] X! ^0 I一种导航+ ]9 o: j+ J! `- H
英汉对照民用航空词典B OEING: a0 T" o/ I) C0 y
TECHNICAL DICTIONARY 167
. c0 J* k/ ]2 A' m! T2 k( tVNAV, SEE - VERTICAL NAVIGATION
0 {9 ~& w. ^1 F# I J( fVOLATILE, The ability to vaporize readily.
6 k4 T6 _& p6 x' s1 f- r: A+ ^& ?LE MEMORY, In computers, a memory whose
6 L$ s7 u, Y, G3 oOR, SEE - VHF OMNI-DIRECTIONAL RANGE
- s, s6 Q0 l5 R, P3 cVORTAC, A combined VOR and TACAN station.
8 B& \ Z! r/ p* [* HORTEX CONTROL DEVICE, A small airfoil on the
4 G! O+ R$ V+ d2 z$ p# Iacelle for improving airflow between nacelle and wing
* I$ i$ e4 t/ ~3 g! Vleading edge.4 \( b' N6 K' x; ?/ r3 N1 ?
VOLATI
! H9 e! N8 J7 d# zcontents are lost when power is removed.
6 T- v2 m7 \' \& g# O4 P$ |+ yVOLT, The unit of measurement of electromotive force.
2 `! ?, F6 V- r$ T0 M% O2 c4 `V' b2 n7 Q R8 p9 f' V
V1 d2 h" O! J$ J7 G- j7 G) p. k
n/ ?+ |0 U2 ~& [5 U9 ]
垂直导航,* }" Q+ }% V$ \9 t# i' \, g
见Vertical Navigation.; j" U2 V2 U* s! w4 G
易挥发的,+ g5 i1 }# x% ]/ e- x
随时可以蒸发的能力。8 \; R" L# \) S' d
易失存储器,& v+ w4 @* {" _# P" g* Y$ _4 N
在计算机中,失去电源时存储内容便丢失的存储装置。
- s+ z. l5 E4 e% m" ~3 }伏特,: o* A( {4 ~. ?0 ]2 t2 j
电压的一种计量单位。4 J- r q! b$ Y+ W$ p
甚高频全向信标,
( b) _6 q9 l( L; H1 f: E W; Dtional Range
Q+ A: `4 q' G( i: d4 q见VHF Omni-Direc .
+ i- Q/ K' T& J/ h1 o) ~# c! hVORTAC,+ f E3 Y8 v/ V# E
兼具VOR(甚高频全向信标)和TACAN(战术空中导
- e5 K/ Z4 N8 r! D- }; j; m航系统,或称“培康”)两种导航设备的导航台。1 a9 h0 Q0 t7 b2 T% D
涡流控制器,
; ]0 b; [) I! G$ x' m8 C& @发动机短舱上,用以改善短舱和机翼前缘之间的气流的! S& `- F8 E* V3 {+ v& l; N
小翼片。
2 \9 g* Q$ N2 m6 J& S英汉对照民用航空词典B OEING
5 {( m7 \& ^* ^4 J! aTECHNICAL DICTIONARY 168
; T! O( H+ k4 OVORTEX GENERATOR, Small metal airfoils, located on8 [* S; g _( A: w% @! d
wings and fuselage for delaying separation of the air- j/ |$ H' q m# o
ating local turbulence" l5 H- s9 U6 K1 X- }
ortex).; r. @, e9 }. _& y( M; v
35
2 ^5 V% V4 z* P2 t2 s% ~0 m. m+ ustall speed in the landing configuration.0 O% c% O' i/ T" B
装在机翼和机身表面,以在气流中产生局部紊流(涡
& W8 O7 V- ~4 y3 j! t流),来推迟气流自表面分离的小金属片。( d/ Y7 `4 | l9 T7 o0 Y- ]3 P5 g
度),
, n5 o9 S9 y. s$ R* x+ j( C在着陆形态时的失速速度的1.3倍。
1 P- Y6 W; L1 ]* Z见Vertical Track
6 m W2 Q2 z7 U" t3 ~3 O; C5 Zflowing over the surface by cre
/ h% i/ l0 [7 F5 S(v
# E9 r* B {: H5 ?- s1 tVR (ROTATION SPEED), The speed at which aircraft
" M$ f$ A* d! `rotation begins in order to achieve a speed of V2 at
. O: e4 s# u3 q5 ]/ p, afeet above the runway.
0 x4 E; z- ~( }VREF The reference speed at the 50 foot height in a# j8 s) d' h9 X2 I& i' R
normal landing. This speed is generally equal to 1.3
( v. ?, u3 X! r! Mtimes the3 b: w# V( T% B- Q3 x! t& r7 l) A
VTK, SEE - VERTICAL TRACK4 G, t0 m9 o/ @/ z
涡流产生器,
0 @0 k. v+ O/ l# _# ]; d$ BVR(抬轮速
# ?& m d) C5 A在该速度下飞机抬轮开始以便在跑道上空35英尺时达
0 }! G$ N( K) ~7 c到V2速度。. Z) q# M! ]4 k. S
VREF,- X( U( I; s8 g1 s9 d8 N
飞机正常着陆时,高度50英尺时的基准速度。通常是飞
9 l! J% m3 y1 h( M3 Q+ ?% B7 T机1 O, D7 u: Q" M" f2 d! a0 Q: I
垂直航迹,
9 m3 H7 \0 P$ [1 K J.# I- A. m) _: [1 t
英汉对照民用航空词典B OEING; o; E7 u/ e- X" ]3 G
TECHNICAL DICTIONARY 1696 u; p+ S m& P# X
W
6 z& t' N5 h8 ?2 @8 RWALKING BEAM, A mechanical component attached to4 O: X* k R1 e/ f8 p
the main landing gear and a hinged support which helps* b: G7 h) e1 `: Q, f& ?8 e
the actuator during retraction of the main gear., w! p5 g% {/ I( C5 M# |
ATER LINE, A horizontal reference plane along the$ ?, L, | j8 x1 o% [
fuselage for vertical measurements of the airplane.7 m) A, {, j* Y. A1 B0 r
WATER SEPARATOR, A component in the air: c* R/ ^+ l: ?0 ~, a" B2 o" Y
onditioning system for removing water from the air( o1 f& U, \& Q6 e
动梁,
. j" \. {/ h! _. c8 _3 [主起落架上,一端连在减震支柱上,另一端连在铰接支1 ], C( a! O" ^; G" C/ h! |
撑上,用以协助作动筒收主起落架的机械部件。
& L4 u% o8 Y" U" N9 [! C线,
# o4 |4 @1 A; P+ N* S) J. ]% S" l沿着机身展向,用以量取垂直方向的距离(或长度)的5 `* @6 `- m! I8 z/ o! T
水平基准面。
1 O9 _) K1 q4 c, U* d水器,# T7 M* z$ {/ [/ h- I9 [8 S8 R: a
空调系统内,用以在空气循环机的空气下游除去空气中
8 {# ^) i4 T) K; }& c) ^W x' z, ?1 I7 R* q7 m7 V0 u4 ]
c
/ |2 f. z5 D1 A. l' m; \ rdownstream of the air cycle machine.
5 V' n& O$ X2 N' x$ a水
* b5 V% |; D# f7 u; C. D9 T x除$ Y- J3 |. T, y/ q# v$ X8 m
的水份的部件。1 r* ~: M! j% k. i
英汉对照民用航空词典B OEING
7 S; ^' |% H" X! P( L2 g, E- {TECHNICAL DICTIONARY 170
8 a0 f8 |9 O) gWATT, The basic unit of electrical power.; t: {7 _% R$ Z/ B6 I! J& B$ b
WAYPOINT, A predetermined geographical position
" d# Q6 p! s8 [! _' `used to define a route. The waypoint is usually defined
! A. V3 s2 `( N0 G. q2 Bin terms of latitude and longitude.2 R' [, N: h/ q" l
WEB, The portion of a beam or channel that has been% [; f- h) ]2 [3 N+ |
installed between the top and bottom flanges. Its prime$ P6 G H- s, N: w4 M; E; i
purpose is to furnish strength.
9 j U. i9 A6 K/ X( H$ O! KWHEEL SPIN UP, Rotational acceleration of the landing
: G# T! q: R0 A- f4 z: _/ gf the+ n8 O5 ~8 A- J
nding gear (undercarriage) after retraction.) j7 o/ Q2 N. p
电功率的一个基本单位。
& n' B! @- \3 U% v位置。通常用经、纬度来表示。
4 C; D8 R# \/ a$ n6 i9 k腹板,
+ J/ R, F# u9 e: p( G; q4 u梁的横截面。常见于上横梁与下横梁连接成工字形。主
1 p6 W7 F; N, O- R要作用是受力。
* u* k6 k$ U( r2 d) j! R0 A2 ~轮加速,
/ H( j; ^' ]3 {* U: U9 [2 J飞机着陆接地时,起落架轮子的旋转加速度。
/ T0 C7 @- Q8 f, P0 X- s# N6 F7 F轮舱,: q( p4 ^: y1 o5 q: Y
飞机的一部份,用以在起落架收起之后,收藏起落架的
( `# m7 H3 [; M! K那一部份。0 s7 a! c+ G" R+ g% w
gear wheels at landing touchdown.5 D8 P+ O' I/ P( H; ^$ D
WHEEL WELL, A part of the airplane for storage o
7 `& P! f R; y: ala# @" A$ P2 w9 P% T m6 \1 L. v- P
瓦特(瓦)," t4 K7 j6 n/ |) X0 E' {
航路点,9 K/ `) u9 Z8 _/ b4 Q& ~" F. \1 B
用于决定航线的预定地理
/ M6 P2 k4 b! e) T4 r机
, k% V7 F9 O1 ]+ p# V英汉对照民用航空词典B OEING+ z0 t3 w( o4 M
TECHNICAL DICTIONARY 171
% x6 Y4 e1 {( u7 A* ~WIND COMPONENT, The effective wind relative to the
; W# o) V; Z$ y: G2 H( \horizontal axes of the airplane.3 r; i2 u. x% \# r+ D
WINDSHEAR, A change in wind speed and/or direction0 w# h2 ~6 m% h+ y/ z. n( C
a short distance resulting in a tearing or shearing
- k, E" f- y2 Qeffect. It can exist in a horizontal or vertical direction and; _" t4 o5 G% k/ q4 `
occasionally in both.9 c o5 N5 `- _
WING CHORD PLANE, A reference plane from the tip
! O+ z+ {7 Z$ y8 z3 gof the leading edge to the tip of the trailing edge of the7 {& a: h- n# o
ing. u( K |1 X; L+ O6 i* }
ING GEAR, The landing gear attached to the wing
# b! S9 ^* _. v' Dtructure.- ]& z2 |" H0 p% k3 _
ING ROOT, Part of the wing which is attached to the* e/ ^: U/ W1 @" p0 J
selage.
* G( ~0 r" x }' KWORD, In a digital computer, a word is a group of bits: }+ R( D" l8 w O
with a specified length. The typical digital word is eight
( @# D8 z @3 ?# Fbits long.
7 M; v& g# ~5 [) H7 ^2 k9 r风向量,
+ C; @# F9 s, u相对于飞机水平轴的有效风。
0 L, C# S2 Z2 H' H风切变,
* U. p, d) B) Q9 m% \! n7 X短距离内风力或风向的改变而形成的撕拉力和剪切力。
/ f k& @3 _: h- P8 j) Z M可发生在水平方向或垂直方向,有时会在两个方向上同时6 t! \6 f2 Q9 m$ S/ j
出现。- y( b* X, B$ H2 q1 s
翼弦平面,
. ]9 K o1 v) ?9 e- @通过机翼前缘顶端和后缘顶端的参考平面。& X4 M6 P0 p) V# |0 ~; `7 C/ V f
翼下起落架,
$ [4 c0 ^: H. P; S& t9 j! A7 Z接连到机翼结构上的起落架。
, F+ D( s7 v+ {! X翼根,
# h5 v8 d8 B% `( N- e* R机翼上,与机身相接的部份。: A; H, w2 |2 S. ]8 m8 V
字,# F$ k& _# V7 v) R0 \$ k/ N1 E. {, |
在数字计算机中,一个字是由一定长度的一组字节所组7 F! ?( q) j$ M" ^
成。一个典型的数字字,有8个字节。
) f8 q, L9 x& A% C6 Qin
6 @3 i1 t! p k6 e7 A% gw
& c# y. g8 l: x+ q9 M3 wW
. s/ J1 k5 O( w \- e3 x/ L& Ss- v* ?! f$ l L. ^
W. `8 o6 l% f6 T z: j: c9 v& q" O
fu
5 r1 _# Z* M. {% w) I; G英汉对照民用航空词典B OEING
: C( C. z: E8 W3 O9 r1 _: D7 ETECHNICAL DICTIONARY 172, R+ P+ O0 c& Y: [* f, R
WRAP AR
- L' C" v! C% o, wcomputer's
4 X9 o3 \( y. L$ F. T. YOUND, A BITE test comparing the
# o# Q; ^( n/ {2 _( koutput signal with an internally stored value.6 d* z6 b' |) u+ W7 S/ |
XTK, SEE - CROSS TRACK6 x, A* N9 C) v5 O
AW AXIS, A vertical axis passing through the airplane/ g2 |5 u6 T8 i# r5 W+ O% n
from top to bottom. Airplane left and right movement
0 u% w5 _) \# h. ^ W; c. I, }controlled by the rudder. (See Vertical Axis).3 p: A- B& O: y: g+ P( u+ k
AW DAMPER, A system that is used to move the
( g) c5 ^0 `, W7 F" A$ ?dder a small amount to oppose airplane yaw.
1 Y0 }* K% O* \8 w# c& Ies
4 h7 ]7 R+ T y1 g- a回测,
/ }; d) {( E) a7 ^( ? f! Z自检系统对计算机的输出信号和内部的存储值进行比8 f* K; w7 s. x6 t0 s
较测试。3 L, c _7 @% q _' k% i7 a
交叉航迹,% }1 Y+ ^# X+ M5 q( L
见Cross Track+ F9 k: j+ R; n5 w+ o% M
X/ e) |- g1 m) n& G- N
.( \$ M2 i4 w, Z/ Y7 b. I4 w
偏航轴,* c7 s/ P% L5 \" j
又称垂直轴。由飞机上部通向底部的垂直轴。飞机绕此# e( N% F7 u! b2 V. u9 R
轴运动即造成机头的左右运动,这种运动是由方向舵来操
6 J8 W. M3 }% u' r纵的。% L9 L' P- ~" }+ w& q: ^8 i
偏航阻尼器,- @. r; P: a5 |
用来少量移动方向舵,以抵消飞机偏航的系统。( a, r# g) j6 {7 W' ~# z, l
飞机绕偏航轴运动的速率。
* U4 `) d; L2 R& C$ `& p' zY0 H. K) \9 Q/ i6 W
Y
7 p3 {9 j2 ~2 {7 x+ ?7 SY' f: ?& D: U. k2 i
ru
- w( \1 H$ R8 M- W6 d4 iYAW RATE, The rate at which the airplane mov
$ d# V! |2 \( k! W+ Xaround the vertical axis (left, right).( M w ]+ u9 s4 t3 U
偏航率,
2 a0 h6 F' ^% C% ]' q英汉对照民用航空词典B OEING$ ]5 a- }( j$ n: K" S
TECHNICAL DICTIONARY 173
7 B2 @ K/ Q; h5 |4 b OZ }) W2 g+ O- `4 s0 x* }, y
ENER DIODE, A special type of diode which, when
: X" i1 {& L, n6 [5 {ZERK FITTING, A device through which oil or grease is. E! @8 O& D$ u- l9 [3 p. \/ J
upplied for lubrication of moving parts.
. g) a1 x, T' w* M, t. R/ }ZFW, SEE - ZERO FUEL WEIGHT
/ ?- H4 A% e/ \4 T; D' s4 qZERO FUEL WEIGHT, The maximum allowable weight
) h2 i: n: u9 f. J# Uexcluding usable fuel.
9 ^' b( v9 @; l! m2 C纳二极管,# V2 e$ k* d/ I3 [7 H* ]* ^, q
又称稳压二极管,是一种电子装置。正常电流可通行无
4 G- A5 w! N) O1 R5 U阻,但反向电流则必须在电压达到预定值之后才能通过。
0 x Y3 P" z( I: z1 n) A在飞机电器系统内做为调压器之用。反向偏压时,它有一, w( ]+ l5 B4 b0 v% F
个恒定的电压下降。
" l& q7 |5 l5 q$ \ZERK接头,
. O! y+ P/ `2 PZERK公司出品,用以接收滑油或润滑脂,以润滑活, |. a: T1 R2 T8 d& U
动部件的装置。9 I9 d) W/ ~0 H0 J' O' v
燃油重量,9 S5 V# J; `3 K
见Zero Fuel Weight
% e* B) R/ k6 u! e' \+ o' nZ
& {: v( w) b2 C6 r6 `( j$ I! c. Kreverse biased, has a constant voltage drop. This9 l& E% t% {! K. P( D _
property makes zener diodes useful as voltage
/ X! U4 N$ A- g+ N# R/ H! Qregulators.! ~7 I# |* `2 z! L5 J/ T( p
s& l( b1 ]/ i X! H8 r% Q
齐/ N0 y+ x9 b. n! g
无
, y: k. y" `5 O' ~" J.
$ X: U* t B& B# I$ j! z无燃油重量,
, V1 T7 z" D4 w& L* R* k扣除可用燃油重量之后的最大允许重量。 |
|