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airspace of defined dimensions within which Flight
: y" H% g; C4 f& |/ t% a3 P. VInformation Service and Alerting Service are provided.
0 C5 k; n& U. n5 q EF
6 v/ n2 i& ?) R: Z: @9 U' \d
+ g% n& `8 j2 D; O* m. q# Q: `F
i0 ^$ v+ X) _in+ q K ?9 ~" G
a
$ S! r( `5 N5 T B, e4 pF9 I, r0 u; Q/ Y: C: p6 \3 E7 U' v- n
s5 n6 F3 s/ S7 C e
s' k& P4 U- b3 A+ d3 J; {$ c
飞行指引仪自动显示(FDS),6 K9 v5 J; {6 l
当飞行指引仪的开关处于关断的位置时,自动显示的飞
* t( @' n5 E4 U- Z8 T! _% x6 z行指令。
! Z2 L( e3 u3 V) L) Q- z( N4 p飞航情报区(FIR,UIR),
, U8 m- z# T) }' q一个有飞行资料服务和警告服务的范围: _6 H5 x! U6 O2 h) p! W3 W3 `
度层。. N2 D1 I) h) \, {
50表示- i; {. s6 ~. w8 {
显示自动飞
; c/ `% m4 d- z' I2 P) t英汉对照民用航空词典B OEING# ^9 ~* R. q/ Z
TECHNICAL DICTIONARY 64
6 @" ]5 _# s* r# o4 D% A4 ~FLIGHT SPOILER, See Spoiler.
) s$ c# n& u9 r" f& iLOAT SWITCH, An electrical switch which opens or: d8 x, r" a2 T8 w" u; ` k0 Z
loses an electrical circuit depending on fluid quantity in& I* q7 ]/ s# L
e reservoir.
$ Z/ |, U: i3 Z2 FLIGHT TRAINING DEVICE: Any device having a full
( H% K3 @2 n. p6 t5 ~& M- ucale replace of instruments, flight deck area or an
5 H& z3 D1 a$ Hnclosed airplane cockpit includes the equipment and, U& E* H- D) L) r. m
rograms necessary to represent the airplane in ground
- {- \1 A0 }" t. Snd flight conditions., J1 y7 p; @ }! s( O9 S: T0 o
LOAT VALVE, A valve in a fluid reservoir which opens
% r; {5 O/ [4 {( qnd closes an inlet or outlet depending on fluid level.
4 d+ g* M* y6 n; |$ y; _LOWMETER, An electrical transmitter for measuring
9 X, O8 S" r& L( Bthe engine.
) [0 K$ `* ]/ ]% w; P2 ~ A/ LLUORESCENT LIGHT, A light emitted by a gas filled
( x: u s. t' z( Q) u. U飞行扰流板,8 C7 ]3 S! G- z/ S! Z
见Spoiler.
, F. j9 _ [" M) ^浮子电门,5 }9 a$ D% }5 J6 |
根据贮液箱内液体的量来接通或断开电路的一种电器
7 Z9 j2 j* b/ ~+ J& G, r% c开关。' w `0 V' _) ?
飞行培训设备,
, e( h( E c; C+ E( m; |. j仿仪表、驾驶舱区、或封闭驾驶舱的任何设施仿真装置。' I/ I7 y. _4 L/ E& z9 n
包括可体现飞机地面和空中状态的设备和程序。0 H5 k0 A) P* G
浮子活门,$ }4 b. r3 V, R% c/ v H
装在贮液箱内,根据液面的高低来开启和关闭进口或出, G2 F! e6 j: ~" t# J9 C
口的活门。
- f/ m- Y( {0 t2 D# C1 `! |流量表,
0 t7 h9 r; Y8 v/ h: G* P7 l用来量度流向发动机的燃油流率的电传感器。! [2 }" n1 i) O J/ e% q% ?
萤光,
* b) X: ~/ K7 o: ~由一种特制的充气管所发出的光。
% m2 _7 Z) T( \4 pF
5 {& h( _/ M# h1 p2 Wc3 I# ]8 G" r1 s8 s+ U4 F
th
5 ^. l/ L) D6 S2 W$ \+ `1 GF
2 L5 z2 A4 G+ v# zs
" g' \4 h B2 S+ F" N& M+ fe
2 b$ B4 i' d: R' Pp' E7 r% s4 M' V$ l# j/ f7 V
a# A# F$ S7 \! D9 u' ?
F
6 D8 a/ W) v3 u7 p5 }a( B% b! K0 n# e* t6 Y% U
F
- g) w t& c8 F# Z1 mthe fuel flow to3 c* p4 _+ L, m
F' Q( f n( a5 g/ L
tube.
! [7 L' G4 H2 ?英汉对照民用航空词典B OEING" I! `8 K @+ F7 X5 k! ^% X/ Z
TECHNICAL DICTIONARY 65" H5 |# B, R/ X" Y) n; y" Y* M
FMC, SEE - FLIGHT MANAGEMENT COMPUTER# x# q. M+ m. y4 ?6 H
FOD, SEE - FOREIGN OBJECT DAMAGE r. x' C% a% k. ]2 M
ORCE BALANCE VALVE, A valve controlled by the
. t8 ?- t6 {1 D# |0 e4 F1 I' l9 \OREIGN, Offside; opposite side. f3 `! N6 C8 [, w7 a: C9 W
OREIGN OBJECT DAMAGE, Internal engine damage N% y7 @& o6 P- U" T: S
ue to objects entering the engine air inlet.! i5 g. I8 M' a9 g
RM, SEE - FAULT REPORTING MANUAL8 `' b0 F- C% u) w" l: S# t l
UEL CONSERVATION, The activity of planning flight: K! ?: R3 P7 `7 j- F, j: K
ltitudes and cruise speeds so as to minimize fuel
* ?5 @7 L0 {* X. y2 m" p8 Q0 D Lonsumption.4 [+ i/ c8 X/ ~& e4 w. W
UEL CONTROL UNIT (FCU), A component on the
" l4 p" U) e' D2 K$ ^5 W- w2 mngine for controlling fuel flow for starting and engine! C( Z. f: e9 o; ^# Q
F; g, |8 P) Q5 `/ b# `& e8 x1 p
feel computer in the elevator system for hydraulic' O2 i6 s# _+ R! h
pressure supply to the elevator actuator.6 }8 w }9 R( o/ ~9 u
F
/ `" F3 X- f8 q& r/ b5 C2 D! Q- [F
! V" N& M5 f9 C [, ed4 y0 `, d1 L' ~$ Y) y" ^2 Y
F
9 D; q2 }5 }5 n# n2 HF$ `) k" ~1 O. G: |1 \/ o( f& j# u
a
0 [# l5 q( k! W- a/ Rc- V" p: m& I/ `+ f, y
F, H8 V. M7 A1 A' k3 x4 y
e4 U& N* ?1 A- e' n" s3 q
operation.9 w, V+ T4 g2 r& A+ w8 o! B
飞行管理计算机,4 s4 e$ S! ~' x3 e
见Flight Management Computer.$ B- b% L3 l8 p; U* J
外来物损坏,
+ w# e1 x9 [: I! \eign Object Damage p3 C+ p! U1 N' R. T r: b
见For .) d# R5 Y$ n# P3 c5 f6 v' y
平衡活门,; a) U7 G) B, A {/ A. R! y( I0 J
内的感觉计算机控制的活门,用来向升降
- x# z/ B( O! y1 P8 J外面的, H3 j7 A2 A( I( G
另一边的,对面的。
, A' q) A2 b; W' a7 I2 a, C外来物损坏,
8 g+ S+ `9 U% p; a9 S由进人发动机进气口的物体所引起的发动机内部。
5 J) A, J$ b N故障报告手册,4 X X$ R7 j0 e5 m, Q$ x
见Fault Reporting Manual
& a5 Q1 |. J; U8 F" Q0 N) @力! `: X: t \4 [8 B% \+ U
由升降舵系统& v8 _) G$ }6 Z) h
舵舵机提供液压力。
* ~% m) ^" ~8 e损坏
: \3 `4 y& e0 [.+ j$ {& Z* }1 U O' P& R& x: ~
约燃油,
# N) H- D K( Y- C, K为使燃油消耗最少而对飞行高度和巡航速度的计划。
3 ]: P4 ~4 u+ X6 H, P4 M" x+ |8 ^油控制装置(FCU),) v) f. V6 J- O
发动机上的一个部件。在发动机起动和运转时控制燃油" K- T: H1 B9 H7 f3 G+ ^- l
节* |9 N* }! I8 Y
燃8 [" G9 Y6 ~) T/ v) a& P" r
流量。7 T" O- h% J0 i. j$ c
英汉对照民用航空词典B OEING4 A, a) x% }+ ~# b$ h* r
TECHNICAL DICTIONARY 66
% c) t C5 @: p& u& i, @9 qFUEL FLOW, The rate at which an engine consumes" X5 W( c8 l9 j# p8 R# a) Z
UEL HEATER, A component on the engine for heating
, z3 g3 M- J! M. N7 bUEL JETTISON SYSTEM, A method for reducing
$ [9 U8 Y3 j" J. E+ {* {, n# Le3 }( e) I/ \) H' ]1 t
ULL FLIGHT SIMULATION (FFS): A flight training
' ]4 R5 O6 k* ^% {. c" tevice that incorporates full visual and motion systems
: N4 }, C i- b7 J! y/ `$ G+ Z: ^+ V! ]nd specific model airplane.
8 U1 b2 d# O) E# yULL-WAVE RECTIFIER, An electronic circuit which& S u& M1 _, W" K& y
hanges an alternating current signal into a pulsating
5 b) y, G& y- \; z3 mirect current signal.
5 h! j8 ]8 _3 g; o- m7 |or
1 C/ u. Q& a% x5 _, |AGE PRESSURE, Pressure measured in pounds per
2 D. Q* ]5 }# S3 o yGALVANIC CORROSION, A form of corrosion caused& d& @2 Y6 T" x9 S# d$ n
by the contact of dissimilar metals.
+ }; h Z& p6 `2 q& F$ E油加温器,# S* f5 @; v/ P' R1 i3 J+ S+ a
热燃油以防止发动机燃油6 s: D4 O; u1 B* N' S$ H
急放燃油系统,# O$ F4 |* f4 ^+ Y" {7 }2 a) O- H
中的燃油向外排放以减轻飞机重量的+ z# u7 B2 H1 @; o3 @
动飞行模拟机(FFS),
2 I7 B; l7 @' C& {3 t6 O4 J一种飞行训练器。它综合了完整的视景和运动系统,以* ~, g3 q& `" M# C
具体的机型。4 a+ `% O+ ^ @' ?1 y7 ^, S9 S+ Z
波整流器,
9 o7 y$ d+ q/ I6 H/ x& M用来将交流电信号变成脉冲直流电信号的电路。 Y }% _' n% _3 x4 ~
压,) S# U k W* v( c3 Y2 Q
平方英寸若干磅(psig)磅/平方英寸的计
. c+ Q, {1 z, G# v8 x6 F$ h电解腐蚀,
, ~2 m5 |. H9 F, t0 z" \/ c2 N一种由于不同种金属的接触所产生的腐蚀。* Y8 n/ k, P: E; c* ?7 `; S, s" j) J; |
fuel measured in units of weight per hour.
J; M! b! u! L' t8 OF
" F- c2 J R$ F1 C3 @0 I( r7 \fuel to prevent icing conditions in the engine fuel; y! ~! v5 b) ^
system.
. w7 V, `8 k: v O3 g! ^F/ u% x3 `2 l4 n6 Q
airplane weight by discharging fuel from the tanks to th
0 |; ~, B7 p0 D3 S3 c( ^" goutside.9 e" S ^4 y( x6 B; H( k
F* p" a' H* h' v$ s
d8 q3 {& `* h4 C/ K- w
a
7 C, x7 Y O* j/ T# }) k2 t LF4 l: P, s/ e: J; P' U8 \
c
1 @6 }6 w- r9 y6 Jd
( X' _1 x2 x v4 S0 K$ P2 k3 V, X; lG& s/ t& F1 o1 M7 y+ {1 j
GAGE, A component for showing quantity, pressure,: ]& ]/ B2 M3 t4 L
temperature by a pointer or numeric display.
5 M% C' p0 B5 ~, s/ tG5 s+ _2 V/ e0 q' I7 J
square inch gauge (psig).( G/ F3 U, f# V8 V
燃油流量,) j: A# o- y+ }, g" R
发动机消耗燃油的速率。以每小时单位重量衡量。
- L& H" n. u8 w$ Q" T2 B燃
1 @9 H. h( S( f5 J5 x4 a5 \5 P+ }发动机上的一个部件,用于加
0 z! q U8 e2 H5 h系统结冰。' o6 @3 G& O2 s! _
应/ W) h1 j7 y- N8 ?, J; N- F
一种通过将油箱
) d" U' r& v7 l% L; f9 R2 t& o方法。
) H( ?6 N; T9 w1 G7 P5 V全
' R" I. E& }. j$ ]5 s" F. ?及0 t, X' C% T" w: c1 j7 y# N9 q" g/ L
全
# z6 i1 c. }" L' |' f0 S; j) i# F7 \计量仪,4 o: L g; v4 f# j* {& ?
由指针或数字显示出数量,压力或温度的部件。
, y4 `# ], e [9 Q& X5 ~表+ l# t5 y& b! q
单位是(每
1 a# } a$ k# p& R示压力。; y4 @) ]6 x, [
英汉对照民用航空词典B OEING
. k; Y* R8 x0 [( l$ \9 cTECHNICAL DICTIONARY 67
: G0 K* T, C: e. d$ d% {- {GASKET, A seal between two flat surfaces.
8 }9 k4 T' O! u; d& nbe individually controlled for the amount5 s# a b1 W" {4 C" j
nd direction of supply.5 q$ E$ }, j8 U7 X% U/ d2 {
ATE (NO. 1), Airport location used for: G' `( V9 I0 C+ U, `, t8 B$ K6 V) f
ading/unloading passengers.
, O8 N _# j, S" qATE (NO. 2), SEE - LOGIC GATE8 B8 f! u! R% \& L
ATE VALVE, An actuator operated, sliding device in a
5 v8 ]7 a v' z6 `6 p0 N! ruct for closing and opening the duct passage.+ k2 q5 ]# d( t; h* g$ B
间的密封物。' o* ~$ F. J/ I: l+ v# `
调节供气口可控制空气的量和方向。5 r3 `7 k) h1 ~- @
登机门,0 X& }4 d8 S9 U6 Y4 b
机场内用于乘客上下飞机的通道。+ `) _: N" W; O' I: S( T5 [
逻辑门,
. z3 e& |1 z/ \' K& g* |见Logic Gate" _2 ^. ~, y# w2 ~7 S6 h. R; g1 P
GASPER AIR, An individual air supply for each
7 z& P* s X U: r) ]; Epassenger. The air outlets are in the Passenger Service
& }: m8 K: o4 p3 O3 d0 Y* wUnits and can
_ B$ a7 r* N) Y# Ya
9 y4 v6 O7 q3 e! |, [% K# ]G
8 H( q5 \! @3 H- a5 V% ?! \lo
; t0 I$ y. l. L6 P& aG( @8 [ n! n7 S2 T$ B K6 t
G
; I2 U0 U9 ~# C" N1 ^0 }d
9 l9 o& S- r6 n2 B9 v密封垫," y3 P: r/ Z! |
两个平面之
3 g( o( M- Z# j, f乘客用空气,4 X6 O( t3 ^' X, U! {; O
给每位乘客的单个空气供给。供气口装在乘客服务设备
& k4 y6 h1 C7 V' c& i6 r内,个别& I+ S5 `3 _' Q4 g2 V8 b
.
* p9 X! W+ f7 U3 I" f闸板活门," s- {; e) T! Z. S. @
管道中由作动筒操纵的滑动装置。用来关闭和打开管道2 `& X' M4 I; U- r3 A
通路。4 D$ E/ ]' S5 x
英汉对照民用航空词典B OEING& Y$ A# J+ a* E
TECHNICAL DICTIONARY 68+ I+ D& ~) p& I2 e6 ~. ]0 E
GATEWAY, A functional unit which connects networks' D4 B" b2 Z) ~+ C& J; p# S' C
r systems of different data formats.
- i f- r( H. Y7 I2 ^RS.1 ?+ w0 |7 G2 J/ V' N |2 I
ENERATOR, A mechanically driven device for
$ E% j. k/ J0 n1 W, VENERATOR BREAKER(S) (GB), A device which will
2 p$ c `) z4 P$ K: a J) R& ntor from the$ `9 u3 S4 ~! I0 K
lectrical bus(es) it powers./ h% R4 n2 ]6 N; f# c+ f
ent with
6 C$ G e a! j- so rings pivoted on axes at right angles to each other
2 l( D/ ~/ D8 g: nllowing movement in two directions used in the flap
2 H! Z) O9 C1 t1 ?% c! G! wxtension and retraction system.
% Z" D6 Q! {! O( d' G- r# @接在一起的功能
& ~* }/ _3 F J! A% J3 p件。
5 A' ^ \* e* F, t4 c4 q9 |2 k. co
: t; f; \/ c) t0 [- nGEAR DOORS, SEE LANDING GEAR DOO; p& G8 I$ E9 G0 \# D
G
0 r6 N9 @( ?/ Dproducing alternating current for airplane electrical
* G0 D5 o7 z. p3 b( F$ g. Osystem.
4 J0 \- z" X- l, V, ~# fG1 t( |/ R7 Z4 V6 u& R4 F$ Y) g
separate an electrical power genera3 q& t* e8 @, G* T
e
3 d" F9 q6 e6 bGIMBAL ASSEMBLY, A mechanical compon; n. S, K: t1 ^( R8 N6 P* y. O
tw. }7 ~, d% v! w- @/ ^7 y# a& y
a& J- D6 ^& O9 ^! i, C7 p& I9 f- C
e5 L' D4 U' M4 ~, q9 y1 j
闸门,9 `7 r2 E. H- B8 ^. p8 Y6 x
一种将数据格式不同的网络或系统联1 f8 _! z) d# f( P+ u5 H! D' G2 S) }
元! ]! i" c3 h+ T/ m( W
起落架舱门,8 D( E- u4 m( ^! }1 L: U
见Landing Gear Doors.
7 i- c/ Q) Z' }0 S4 c发电机,
1 I' m# ]. ]. f- {为飞机电器系统产生交流电的装置。5 g/ @, ~% l$ w% F+ ]$ p
电机跳开关(GB), }- u3 }3 J4 \& l* h8 K; ^
机与由它供电的汇流条断开的装置。7 k0 F, P/ z- O- j- d6 Z
襟翼的伸出和收上系统内的具有两个圆环的机械部件。
' `0 C( V) b5 N: `. o5 _- O" C9 A个圆环的旋转轴相互垂直,以使部件在两个方向都能转
5 e7 x; ~" s/ i7 H7 w1 |0 k。
. |) M2 R3 ]* ?% G0 J由机械驱动,
) ^* _ [+ i$ y0 M( J发! ]* @/ I8 K8 X! n# {# c+ t( y$ t
能将发电& r) F- b( z5 \% \0 i( J
万向架组件,
! w: [% M* G) z& R+ O7 G Z. s两
9 K: W( i4 d( A( \. j动
+ b1 l/ P* w( P/ F, ]英汉对照民用航空词典B OEING
: D* ?; \- _: z: p- m5 M9 KTECHNICAL DICTIONARY 69$ n! T0 k% W/ q6 I( @
GIRT BAR, A rod attached to the escape slide which1 }1 H, u: M ?! |% t0 C9 b$ H+ |
engages brackets on the floor for automatic slide
$ K- a8 U4 H: h: p7 @( Eperation when the doors are opened.
& w% y: o) @/ GLOPE (GS), A vertical path defined by a3 p. @3 U x0 h _6 B4 w$ ~4 ]6 L4 y
ased electronic signal used by an airplane or
2 P6 c4 |$ b/ K7 MLIDE SLOPE/GLIDE PATH INTERCEPT ALTITUDE,3 ?1 q! \) D3 i, u9 w
he intersection of the
6 d. u# j5 d( l9 V. k* xublished intercept altitude with Terminal charts by the
+ z* m: T2 E# F6 w) V3 e, @tart of the glide slope/path symbol, is the precision FAF;
+ {+ \3 T1 x0 D4 h; F. dowever, when ATC directs a lower altitude, the
% K/ Y8 U; f/ U7 k' t地6 \# f) @- H) t1 @: c
上之锁钩相齿合,以便滑梯自动工作。 N% p3 w! I! N! j6 ]+ \9 {5 y2 J3 o
滑道(GS),
; Z$ x3 u1 G( }$ h$ y由进近或着陆期间,飞机或飞行员使用的地面电子信号7 }5 ]3 A( f2 ?4 s
垂直下滑航道。3 w$ D4 o" p6 A9 @# |
滑道/下滑航径切人高度,; x! `- J( o- L( j ? i
进近时切人下滑道/下滑航径的最低高度。在: b' W* |( `/ p, B
最后进近定位点。但当空中交通管制指挥一个$ W4 ]/ x5 ~9 [, x' E F
低的高度时,由此产生的较低切人位是最后进近定位$ }) q$ a& C* l- Q3 m5 O
。1 f+ j0 M- U; E; {
o6 N. j" [* y' X) Q2 v: Z
GLIDE S
/ z6 G' W, a L* b! R( qground b
: m9 Q; M8 {, O+ Kpilot during approach or landing.$ l5 _1 l/ I, j9 F3 p, D) W( U
G
5 ]$ [- k9 A- P" W; I! y! K, iThe minimum altitude to intercept the glide slope/path
% |9 X; R! F* h6 t5 P! U% ^on a precision approach. T5 l% M' z' j6 [8 J& e- Z/ P! O3 `
p
2 a: l) a, ?8 v K1 L" |6 O Ns
) `) S8 K$ L5 c( d, ~h
5 W9 P5 q* }6 M# G: c: Lresultant lower intercept position is then the FAR.
' A4 x& ?+ A9 C3 y! G1 ?. u束缚杆,5 T3 R% U4 H- W+ @' p
连在逃离滑梯上端的杆子。在机舱门打开时,与机舱
! `7 q+ g7 y, } G+ O" o板" J2 i3 B5 w9 e& W* O4 [
下
3 P. |: D" R1 F, L9 D确立的一条
8 ~( V$ h B+ {下
8 Q4 O( P1 @$ J+ Y* c0 x在精密4 P. `+ p. m6 w- c8 T+ `5 W, P# {
Jeppesen机场图上公布的切人高度与下滑道头的交接& v9 R+ y- W p, B* F% U
点。是精密2 A5 Y6 e8 T2 @; S/ J+ ~5 _
较
$ j: S( j2 m0 B8 H点
! p, z/ ~; A# D8 Y/ G% k& s英汉对照民用航空词典B OEING
& n9 Z6 q, E# ^8 O, w( fTECHNICAL DICTIONARY 70+ p* Z8 \- \7 C8 I9 F
GLOBAL POSITIONING SYSTEM (GPS) (No. 1), A" y, u2 j+ j: h; I5 Z
pace-based radio positioning, navigation, and3 I' E( M1 V `. T" H* T6 {0 O
metransfer system being developed by U.S.A.* n% B8 x& N- G) _2 L8 w# ^% \# a
epartment of Defense. The system provides highly' V7 f( R3 }$ ]! @' r
recise% y5 I& z9 `. M0 e
nd provides a worldwide
9 V) J) ]8 T& p8 |5 I# {4 Gommon grid reference system. The GPS concept is( _% r; _7 {/ Y
redicated upon accurate and continuous knowledge of6 S. M) G/ s I6 w0 {
e spatial position of each satellite in the system with
2 D4 Y) M- l- A9 s' {& ?spect to time and distance from a transmitting satellite& u g0 M1 y; H% H! n6 B: Q' q
the user. The GPS receiver automatically selects% J8 r: }- C& F) M$ i& L
ppropriate signals from the satellite in view and4 x3 ^' @4 w6 B6 B0 K/ N
anslates these into a three-dimensional position,/ V1 }; ^) R! ^3 F; p
elocity, and time.
$ j% U; J {7 t( Y. r- HLOBAL POSITIONING SYSTEM (GPS) (No. 2), A3 A6 g/ J/ {4 [0 j
ngrange navigation system that takes navigation input6 E* X2 d0 ~/ G
om transmissions generated by a series of satellites in
( `1 c) x6 O3 hLOBAL NAVIGATION SATELLITE SYSTEMS (GNSS),6 w/ g# M; i5 W, V o3 O3 E |
ternational Civil
7 y" J) L5 d3 f6 [9 L# _, z, {viation Organization (ICAO) to encompass any1 W" D2 R' G3 a5 Z* | A
dependent satellite navigation system used by a pilot6 ?0 x: a8 D7 }9 B* B, q, L' \0 E/ Z
perform onboard position determinations from the5 r) V+ D* f) _% ~) @# e( C2 q
O-AROUND (GA), Airplane maneuver where the pilot is6 F) y8 m/ T$ I5 W/ C) z
in the final approach phase of flight and decides not to9 Z7 |/ k' `4 Y9 I) U* u
land. Thrust is applied and the landing gear retracted so# ]# M D0 y7 s8 R/ a; i( P. ?
as to climb the airplane to a safe altitude.
& V: u0 \ V. j* A- X: W! v& K mGO-AROUND THRUST, Maximum engine thrust to be/ U5 r' D4 J* }4 w5 c) P
used during the Go-Around Maneuver.
@; _* m! p9 z统(GPS)(NO.1),4 o! Z( b; H# s- v: E6 K0 u0 t
电定位,导航,和时间转移7 U; }4 y6 L6 L! ?% Q: i8 o
统。该系统在全球连接的基础上,给无数备有适当设备* U, M8 A5 Z) A$ P
户提供高度准确的位置、速度、和精密时间信息。该系
8 l3 Z& l: s% s O# L响,并提供世界通用性座标系统。全球定
6 T0 \* X, Z; r: r$ x/ F2 b* l信息之原- `6 U' ?4 a0 }$ j/ ?/ k
为基础。全球定位系统自动从所见卫星选择合适信号,, V5 ^. I8 D- l( ~* |( r- X1 v
并将这些信号转译成三维空间位置、速率、和时间。& v: i7 }; z7 d4 l+ i% N
全球定位系统(GPS)(NO.),- T& c1 t, l, G
一种使用一系列同步卫星所发射的信号作为导航输人: D. U+ w7 m0 [+ ?" c3 o
长距离导航系统。3 t n+ t4 @6 y3 D Q5 v& q
球导航卫星系统(GNSS)," `$ a6 S. t$ N) U/ t$ k3 U9 m
航组织采用的“伞形”术语。它包括飞行员
0 B9 I. F3 @4 I3 [7 ?' ?5 n料做位置判断而使用的任何独立卫
1 Z' a0 K: ~# [* ^! \导航系统。' P1 n2 E# X5 W c# w' \/ r& {
复飞(GA),
' X; O% B0 B" o1 w6 D1 h% y0 n$ g) X飞行员在最后进近阶段,决定不落地而做的机动动作。
' ]& R9 T. a6 M3 V/ Y7 J+ b# [复飞时需加油门,收起落架,以使飞机爬升至安全高度。+ O4 ^1 |% f* J* I2 Q5 {, T
复飞推力,
3 K; X. l6 F* z5 e- s6 W0 F飞机复飞期间使用的最大发动机推力。
3 Q# y& x" A' i$ Ss% h' }+ {. J, h {. Z5 W+ D1 |
ti
: o6 F% P: g% G2 r$ sD6 |9 T6 ]- v8 T3 X5 T
accurate position and velocity information, and p. U3 ?# `# ]- [# @3 }
time, on a continuous global basis, to an unlimited; v: \: U3 k4 c5 ~
number of properly equipped users. The system is
3 E! {& G. q1 y" y, q( b. hunaffected by weather, a5 \2 d3 z5 Y2 z: C
c" q' U2 y( G/ \- t
p4 J# z( j! D7 g
th
0 s) _# H) V6 k! D5 bre- Z/ g2 ~6 M( ?- V
to
$ z5 N# a' U) y+ v. C6 ea# e0 G' S8 l, O3 |
tr
; ~ c) v1 l/ B7 Mv$ M/ B/ h( z2 l6 n
G0 A7 P$ G O( |7 g
lo
2 ]6 `; S1 w, E8 }- p/ F& Q7 kfr
; B3 t- s, K& Wsynchronous orbit.
4 a; P* B: b- `2 c/ ]( k9 ]G& L, s- A( U5 G& T6 s w# A
An "umbrella" term adopted by the In1 {. R0 \- O4 v
A0 h3 r- w7 K% v) c/ v# c
in
' Q g+ d+ t7 i3 S. J- Kto
- s. V; w0 |$ c- |3 Z& |$ d; Msatellite data.
6 L8 b1 z8 d) C, Q6 W2 `全球定位系
. K% u2 W: n; x; H由美国国防部研制的空间无线
4 u# ^) P( a7 C% k1 U( F- l系
$ Z. K7 t0 L! F" J$ ]" X3 [用: U9 K9 B' A9 e1 |% t1 J% y1 }
统不受天气的影
, T3 K) o4 [2 m& |( I# a位系统概念以系统中每个卫星具备相对于发射卫星与用* N+ q0 I' P+ i( ^
户之间的时间和距离的准确且连续的空间位置
; Z0 N6 T* B& K则1 |8 L+ X! u* P& w: F& t
2
% Y% g! u; u- i* G* _的: b% m7 H6 j- ]- E: k, i
全
- F5 K2 I- C2 H+ I: E# o是国际民$ P# K+ a5 x! s! X
在飞行中根据卫星资2 D4 R+ s6 T( Y: K+ t$ X" T
星
2 c L7 e8 |( r) o. O* C英汉对照民用航空词典B OEING
; S5 w B3 _& i6 x4 Z. ATECHNICAL DICTIONARY 71, ]' O8 [" f, i3 r9 B
GRADIENT, The ratio of height gained or lost in a given
* C/ D4 Y4 G C- E7 \distance to the distance travelled.
5 x3 b/ ], \$ p6 t5 H8 H% T$ Y: Drbon! K) j* m/ a; v2 T4 p2 i0 \7 l X
r access panels, landing gear doors and flight" |/ ]# S, e. l, c
ontrols.
% ]' g- n: t$ }/ T, uIRCLE ROUTE, Is the shortest distance
( q' g2 m8 J) X( t# \9 Fetween two points on the earth's surface. It is the line5 _! H: |/ x/ i8 }2 g" ]! o' U
rmed by the surface of the earth on a plane that
- E" k* U$ Q7 u" I2 n& gasses thru the center of the earth, the departure point,
# E; J/ ~, t6 C3 I yt line
% T% w% b. b7 N5 J3 }. G) fal Conic Projection0 e! u2 G6 _6 n7 \
pproximates a great circle route." F6 x9 L" n4 K0 b: t1 M' n
GROSS WEIGHT (GW), Total weight of the entire2 |- ]" W0 @0 h0 V- [0 |
airplane, fuel, oil, cargo, passenger, etc.
; E' c5 R8 q) v& rGROUND, A part of an electrical circuit or system that2 T7 {/ }/ z5 D$ b! T
has zero voltage.( f) l( Y) E7 p* ~: b
GROUND FAULT (NO. 1), System fault that has3 g9 S3 j: ]' ?: [! n: }+ c
occurred since airplane landing.: R |3 F6 r+ x$ l
轻的材料。用以制造舱口
; i1 A- @9 \' b,起落架舱门和飞行操纵面。
" j6 w* z# O+ e7 `圆弧航线,
! ]; Z L1 d4 a4 Y, j& A地球表面两点之间的最短距离是以地球中心为圆心,在
: {2 W9 a) b4 M3 j7 G飞点和着陆点间所形成的弧线。由大圆弧航线形成的真7 S/ s$ Q& T s0 a7 g$ U
迹不断改变。在兰伯特等角曲线投影上画的直线接近大
7 [& j, p7 ?6 U G# R* O* F d0 V全重(GW),$ s9 i- w z8 M! q2 M
整架飞机的重量。包括飞机,燃油,滑油,货物,和乘
% B# f( c6 h0 u5 ~8 u客等等在内。% x* a& v& g) N8 ~9 z
地线,5 `6 |4 [7 y+ D' P! ^' `
在电路或电气系统中,具有零电压的部份。% C( ~, V+ A. R1 G; M; c
地面故障(NO.1),
6 u3 a& W) k* o {; d/ Z) V/ w自飞机着陆后所发生的系统故障。
$ V* L, B; J8 |3 aGRAPHITE, A strong, light material made from ca
8 c3 u u- ^/ z0 gfo
& w" ^& c0 U# Z+ ]" ~c# Q! f; @, `6 O& h: O
GREAT C
/ f+ D# b0 r7 t- s& q9 c4 \b- w- H0 x7 P4 S8 [9 D1 \
fo
0 J8 ?/ q' ~0 x! sp
& I: a0 n% w) j* M) u/ Uand the destination location. The true course formed by& J. u; Y1 h: I% Q* Y" p
a great circle route constantly changes. A straigh* F0 X' E. H& C4 h6 l! o
drawn on a Lambert Conform
9 e* J$ w- N/ s0 `: B6 p$ aa6 ?6 K) \9 F4 t _! h7 C. @
GROSS PERFORMANCE, Actual or measured
, ^ r- f6 E% }4 C% ]performance of the airplane./ |4 E: p5 M: c* R" e, g
梯度,2 a8 {: B! |& v' `1 y) b( K
在给定的距离内,获得或失去的高度与所经过的距离之
# Z/ J4 @% z. x比。
: T: ~# J8 K. J; d8 F3 S! c石墨,
1 q3 J9 h9 c" R, @) q4 g一种由碳纤维所制成的强而
: ~) P5 e- ~4 I3 e- R0 Z盖: U6 S+ ?+ f2 \$ V' ^
大3 W5 l& I* I; K# J* ~
起1 m# C2 Q- v- g- N
航1 m9 f1 c" d& r0 |
圆弧航线。+ J$ m# B, p) @& e5 h0 N1 B7 j
总性能,- [1 z# V( J, h1 U1 }& M
飞机实际的或量得的性能。. ]5 m4 F7 v9 S! T! k% T
英汉对照民用航空词典B OEING$ x; x9 i, q: q: h
TECHNICAL DICTIONARY 72& L+ j4 L7 Z$ l' K4 U1 [1 [
GROUND FAULT ( NO. 2), Loss of a ground connection
3 ^( J* i/ V- M' dor a short-circuit to ground.
8 R3 f0 {: t- @; k4 u. ]4 OGROUND SPEED (GS), The speed of an aircraft
- a Z7 \' b6 s7 o* S- R7 rlative to the surface of the earth.
! _, Y" s8 i# A: B, X# B. sROUND SPOILER, SEE SPOILER
# U; O) ]) F% |7 _- ?ROUND SUPPORT EQUIPMENT (GSE), Equipment' {# B4 F) S" \4 X) ]' D
sed to service, test, move, power, or repair an airplane
5 \; L( A9 B: c0 N( w' p% ]hile it is on the ground., f7 ?0 Z. A2 K+ H4 ~
ROUNDING POINT (TERMINAL), An electrical
5 }& W: U' J+ ~1 A+ V% |: Q! Honnection on the landing gear doors for electrically
. R3 E6 U& `4 t, ]! h7 Q, \rounding the airplane. An electrical connection near
' }2 v4 r: n/ [: Y! }e fueling station for electrically grounding the fueling' O0 N# V: c8 ~, a* O! l2 S, s M o
ase., e% ^! N+ R8 L) i8 Y
S, SEE - GROUND SPEED
9 S; T, h- r1 ]: G* JSE, SEE - GROUND SUPPORT EQUIPMENT4 e) [+ s; b1 }: w( w I
NO.2),3 `- G, `' g6 {( x
地速(GS),' J! b0 O) m' H8 k3 W5 S* ?; }" ^
飞机相对于地球表面的速度。2 r$ r* e K& {. m+ f
地面扰流板,# I0 g2 {+ O% ?7 R
见Spoiler
! L% f- y+ P+ ]% E/ jre
# t- S8 A3 ?2 OG
7 M/ N' |- B+ f% G8 eG
2 h; ~/ a$ F! Ku
4 @. b/ ^3 b* u7 F2 q: V. J0 {w0 X: v- {1 n J: \
G* ^+ w+ G% D& r1 \6 w4 G! u
c
- L) z: F* q# Z, k- kg. s# p/ ~6 j! M% k" G/ o$ r
th
7 s6 W% q& b& F6 D4 z) }b* |% n6 T- v: g5 l; r
G
6 G: U9 T4 _! F$ A" a( wG# p% c& V5 [# k" Z8 z+ K, G. b! D l
GUARDED SWITCH, A switch that is protected against" \% j+ O l( |9 ~2 ^
accidental movement by having a cover installed
^+ u) e7 W" [8 ~$ [directly over it.
# M" C$ R1 @6 a* ~# |地线故障(" ]) `; a5 o ~8 o% P6 k
地线脱断或某线路因短路接地。
# |. i& d k g! Q- H.. I4 M* b. C C6 C; R5 V' U, Z: v/ C
地面保障设备(GSE),$ E+ b; |! o& j6 a6 P& ^% B- p
当飞机在地面时,用于勤务,测试,搬移,动力,
$ K' `" G4 P7 k或维修用的设备。
. J8 E" n* H) N9 c+ U+ O% |! Z接地点(接头),$ I$ l1 X4 E1 \# {
是在起落架舱门上的一个使飞机电接地的电接头是在 {6 z+ }2 i, B. b4 j7 B, ?
加油口附近,使加油车或地下油库电接地的电接头。
[* @8 D$ t- f4 `" T9 b速(GS),
+ h6 t8 j5 J, s; Yeed. z% t" \: K: h; g; [
供应; ^/ B7 G4 Q) B5 k, O0 Q( t" H
。) [( i$ _- K |" O' b J
地" p* ~, m6 _6 P1 A4 `
见Ground Sp .9 d) O3 p; D9 p4 P$ f1 a3 n, J
面保障设备(GSE),
& `! n& W/ A6 B C* V见Ground Support Equipment
4 I2 E5 s |) C* p地
! o; u9 Z) H. p6 z- ?2 l.7 Y! r# V6 ~9 M- o$ w6 c& p0 [
带保护罩的开关,( s* n- c' o9 ?6 S
为防止意外拨动而直接装有罩盖的开关。: N3 D: N: Z7 `; X7 V6 t
英汉对照民用航空词典B OEING
5 T. S5 G6 H Q- e) C1 Z7 k: w W, jTECHNICAL DICTIONARY 73
! W, g* V+ }, l; o1 ^4 n* F" ~GW, SEE - GROSS WEIGHT
$ W7 L: U! X3 x( ^' R m( ~+ rH
- Q- k& b5 [# M& Q8 EHAIRLINE CRACK, A serious defect in structure; a
& s5 T" {& o6 Q+ }$ C! @3 f. R. Ycrack that shows as a very thin line.% G' B; K" v" R. d: K- T6 D
HARD-OVER, A maximum pitch or roll maneuver.
& Y# \5 I6 i( C# O8 c' m: ?& qHDG HOLD, SEE - HEADING HOLD
. ^1 v; k1 J* Q7 R, H: H6 V6 q4 r# _7 o" wEAD END, In a hydraulic actuator, reference to the
, E4 h1 k* _) {art on the piston side of the actuator.1 w5 D) Q+ z0 T$ B
HDG SEL, SEE - HEADING SELECT: [( O0 R" x- D2 _+ i/ f
H
# j% l. I, f: M3 g! Pp
: E( k! T& a N' H- y" a+ lHEADING, The direction an airplane is pointed
! v3 R) q7 t* W, ~/ R5 l4 I) ~8 Kreferenced to true north or magnetic north.
3 m R* t0 y( }/ g6 d6 m5 |. ?$ v全重(GW),
* h# _- P6 e& l& k) f9 n( p( l3 n* G见Gross Weight.2 l# `; l. a7 }+ T
细缝裂纹,
& j7 g5 H# }: A% C* u# x结构内的严重缺陷;裂纹的外观是一条很细的线。! \; }& P2 c% ?# B3 Q1 i7 E
急偏,' q1 h- W# y) r. Z6 u' z. j" H
最大俯仰或横侧操纵。
, T: s2 `& A6 K6 M0 L/ z, x: I向保持,& A2 i9 ? O! _ W
见Heading Hold
0 _4 |4 T4 p, K9 r5 w, A+ y航" R& _/ B0 p N6 I8 w. q2 z3 a
.
9 j1 S8 G7 T, e2 k航向选择;9 r+ @9 Y0 I4 V0 k
见Heading Select.
! t. J- }% r; ?6 P- Y& f顶端,
& o$ ^6 T( C. z3 ^$ z6 w# K" u3 I液压作动筒中与活塞相邻的。' d* P1 G0 j" k. A0 A
相对于真北或磁北的飞机指向。2 [1 v- G$ K- E& w- r
航向,
4 O; j# K1 N1 J' Y& M英汉对照民用航空词典B OEING
f% n8 N3 V q$ q6 _( P1 @$ h' g' u( tTECHNICAL DICTIONARY 742 t a8 i" w* z s% }, F8 ?
HEADING HOLD (HDG HOLD), A mode of the autopilot; ~6 D8 j. R. g
irplane heading.
* k1 p# ^! U+ j R9 r. Pt
% }& h+ V& d, ~$ t% a1 @e1 T8 x2 }; x% }
om
1 C- \$ }9 s7 v0 e- zg or
. |( N* o6 C6 U3 u$ H, R& [" M(HDG HOLD),* L' k4 w4 q7 W- t& D! ~+ a) s, R
(HDG SEL),
" Z* t" T7 l2 d8 K }: K交换器,
$ [( N- X& H8 Y+ k有很多通道的金属组件,气体在通道里流过时,一股气% j# }9 i& Q2 o. V' S
可被另一股气流冷却或加热。- I: M9 @. ]+ M
system that maintains the existing a
* z3 t. |1 _) W8 T$ J+ S( o+ @8 vHEADING SELECT (HDG SEL), A mode of the autopilo
5 D5 Q8 y9 b! D( Dsystem where the pilot selects the desired airplan5 K) t! M$ j! E
heading.# v# `" N9 Z( O& V/ z/ V
HEADWIND, Wind or component of wind coming fr. V4 l6 I1 ]/ ^6 l4 |" y
the direction of airplane travel.4 l& [2 D# f" J
HEAT EXCHANGER, A metal component with many! H& Q. Y4 ~8 \" j% c6 K: X) a7 ?
passages through which a fluid can flow for coolin) _, s3 J f2 m7 E& r
heating one by another.
7 M: \$ G+ n- K航向保持$ ~# p& T' W8 J2 I& t0 k
自动驾驶系统保持现在航向的方式。
$ q& j# F" M/ |" m9 Y& u! J/ ^航向选择
! t' C# M/ ~6 D9 B8 s2 o自动驾驶系统由飞行员选择航向的方式。
+ D3 q) b2 k! F顶风,
- M( C6 ^/ P d, y: o6 y7 J0 w来自飞机前方的风或风的分量。
& i3 t- _! I- U8 \4 d9 E+ o7 z热
1 K7 |$ T5 }. J& f8 w! _流( `0 n1 ]8 T6 @1 V
英汉对照民用航空词典B OEING
% ?$ {) Y! w' I% ZTECHNICAL DICTIONARY 75
; d' N5 f8 u, @, V) y3 lHEIGHT ABOVE AIRPORT (HAA), Is the parenthetical# v, c$ @' X: }
figure following MDA which, when added to the airport
% [4 ?8 X/ d. |) v/ W! a- L# \3 rlevation, will give the MDA in feet above mean sea4 P8 B, Y r. p
vel. A HAA will follow a DA or DH only when there is
7 |$ ^1 e! g0 B8 }o touchdown zone, runway end, or threshold elevation, d* _2 K% ^& k2 M1 N0 {* d i
), IS the
. k' K. G" }( ~' M: rarenthetical figure following DH, DA or MDA which,
; E+ }" B& s& mhen added to the touchdown zone, runway end, or
- @5 B+ J3 {+ \$ Lreshold elevation, will give the DH, DA or MDA in feet4 i/ y9 l! L8 f. w& T& v+ w% k
cy of one million cycles per second.3 {* _% y" {( s8 ^
EXADECIMAL NUMBERING SYSTEM, A numbering1 j6 X' Q) r; Q
ystem with sixteen as the base. The system includes
7 M* U. b/ G7 migits zero through nine, and letters A through F
! W K9 E2 I8 i* G5 Y/ e8 o' kpresenting the numbers ten through fifteen.
u9 V' W+ v1 @' s7 K1 Q8 K8 ~IGH FREQUENCY (HF), The frequency band between$ M( F7 _) }7 A$ f
场标高相加后即是 T# b1 y: L8 S4 J P
DA高于平均海平面的英尺数。只有当接地区跑道顶端或 v+ h9 A0 W! b# b' Z7 m8 X
道头标高不可得时,机场上空高度才跟着决断高度(DA
0 f4 V$ f- Z- V9 O4 }7 t6 HDH).
$ @' t+ G6 ]$ o$ U# lHAT),
9 l# ~: x7 e$ [6 ?9 i% C最低下降高度后括号中的数值。它与接地
( C; |) M8 B9 i! v7 p4 A、跑道顶端、或跑道头标高相加后即是决断高度(DA,1 P! P: U- w0 \" m7 ?9 b
H)或最低下降高度(MDA)高于平均海平面英尺数。
) Q2 m( G5 X5 k1 E3 j _2 A" N9 H i的最低天气条件同时公布的。$ g3 d ]* f0 B
率。
3 O1 m# j9 W S( J/ w A一种以16为底数的编号系统。该系统包括由数字0至
3 _1 T/ m0 L) U: d1 s+ @8 W,字母A至F代表10至15.
- O! }, _2 B+ [: U) b频(HF),' a$ U. O$ H- `
赫之间。) d) H8 @2 S& }$ b! C
e
3 f8 j; F! {. d2 Ule
% ?3 F2 A6 M6 n& [. On; @ f- `9 A4 g4 W
available.
1 j" ^4 p* p/ e. \# ^HEIGHT ABOVE TOUCHDOWN (HAT
2 ~9 e6 s e: Xp" S+ X9 G: o. K; T
w
! h8 S# q: q& h' cth6 a, |) x& t8 B
above mean sea level. HAT is published in conjunction x( k5 c3 U% y2 i- \' ?# Q3 P
with straight-in minimums.3 `% I+ j9 X6 F! h8 F- M
HERTZ (Hz), The standard radio equivalent of
]/ I( M7 Y. Q9 V2 `( X6 I4 Xfrequency in cycles per second of an electromagnetic
3 H7 h2 U/ O+ @) d6 E; cwave. One Kilohertz (kHz) is a frequency of one
& G0 E: r( q& O( e& B3 l! gthousand cycles per second. One Megahertz (MHz) is a
) \! u5 ~) p8 E* h- Z2 Sfrequen8 c8 ]/ ^8 J8 ~* R* A; v7 f8 U0 I
H$ [1 v$ k8 r/ {
s2 t4 V6 z/ B( j4 t: x
d9 e# N( J* E! o2 u
re
8 c) ?4 r! I# H+ K( @8 A) u LH: h5 Y" r2 u& t% O. M# h7 d
3 and 30 MHz.
0 u; L4 v1 g* Z$ A9 p机场上空高度(HAA),
# z# |$ N& F9 _是MDA后括号内的数值,它与机$ P+ }% z; z& C% m0 [
M5 w- ^' A) @7 _7 W" s* i# P
跑
1 M! B6 ?4 W3 M/ `7 C; f& s7 L或0 s! n- v4 ~% I U
离接地点高度(
5 e. U& h/ \7 S3 p t( S, y决断高度或! V p2 m8 I$ h* m' m* P' a+ j
区- R2 k I' v2 W9 n" y
D' {; T9 L& \, ~4 s# H/ P
接地高度是与直接进场着陆
9 A% @0 v4 t" l赫兹(HZ),
( j* F& `3 B' V单位是周期/秒的电磁波频率的标准射电当量。一千赫
+ e( c1 @- j4 w0 T) V: T8 U2 w/ t兹是每秒一千周期的频率。一兆赫是每秒一百万周期的
9 U" T" ]7 k5 D8 _2 L/ }, A% H频
; _" R( F3 L/ R* Y( m' @十六进制编号系统,
6 y+ ~) _& |: `& ~; g5 `% W9: t2 ?. _! t1 }, @4 `' x8 t
高
5 c3 _% {1 k/ k6 V( I频率带在3至30兆
2 q! e; h, W* E' U英汉对照民用航空词典B OEING: t5 X7 r# @( U& r6 S
TECHNICAL DICTIONARY 76
# z d. I' n5 [HIGH SPEED TAXIWAY/EXIT/TURNOFF (HST), A long
9 N5 a8 [* \. E. K+ Z+ Rdius taxiway designed and provided with lighting or
4 V$ ~$ W9 i9 z7 A- e8 d; Carking to define the path of aircraft, traveling at high
+ J& q, ]" F* Q5 P8 o; `9 Q2 v Jp to 60 knots), from the runway center to a5 j {( K2 i5 f( m
the center of a taxiway. Also referred to as long" x, g0 X7 n8 c/ s" _# Y3 m/ V
it or turnoff taxiway. The high speed taxiway is
, Z/ t, K& Z5 m7 _fter
, `6 N3 X8 |3 P7 Q% y mancy time.5 [5 i. J* g3 q: l w8 J
r a
6 ` t/ o% c! jeavy component during removal and installation on the9 `0 e/ ]/ O5 u; n
irplane.
) j% {+ g7 w6 @5 e$ FOLDING, Airplane maneuver to keep the airplane from
7 l0 j4 K5 `; ^7 s% `$ ]rogressing along the intended route of flight.
8 M4 M$ S: [" f; IOLDING PATTERN, The predetermined maneuver
$ [* W, l! F V( V0 S# }4 Ec control.2 k' L# \6 P0 ]. R& U
OLD/HOLDING PROCEDURE, A predetermined: I. w+ U" e. J. o
aneuver which keeps aircraft within a specified! \3 n. y1 B8 `% M8 K0 R" L
irspace while awaiting further clearance from air traffic
; |6 R0 A; D" bontrol. Also used during ground operations to keep
0 H* M0 j' O4 b3 t! q2 B. O5 N! Kircraft within a specified area or at a specified point
( A/ i$ j F. [# s9 nhile awaiting further clearance from air traffic control.
7 {8 f- A) \9 \: E8 ?' K0 N# Lhe standard holding time is one minute at or below7 Y4 B2 K* W- j
4,000 feet or FL 140 and 1 1/2 minutes above. The3 L+ ]7 l3 H4 O8 {8 g: p- S f
eparation between 1 and 1 1/2 minutes is FL 200 in
( T# k ?; C- y6 u(HST),; Z) O1 e) H) J3 m3 U9 P6 ?
道。该滑行道有灯光和标志表明飞/ _+ M5 M2 z0 H! q: r! N
从跑道中心到滑行道中心一点高速(可大到60海里)通: V( K' {7 y" ^" ?: K @$ o8 ~
的路径。也被称为大半径出口或脱离道。高速滑行道的
0 M9 C' v3 {8 E: h0 R; M2 D6 D- B计意图是加速飞机着陆后脱离跑道,从而减少跑道占用$ r( Z; F9 ~( y& [2 z( s; q1 j
时间。7 Y& c% {! g% A* l* @
安装过程中,用于放下或抬起
4 i) ^) t& D4 H! ^3 p/ @动机或重部件的装置。 Z; P7 Y6 z/ _ L& g; _+ e+ t. P
待,9 W6 k9 K5 A- }9 ^. x
使飞机不按预定航线继续飞行的机动动作。
3 z: o. v% v5 N/ k待航线,
8 D! H# V4 B/ v1 ]" x+ Y- t0 Q$ f处于指定空域内等待空中交通管制下一步调度
2 k# M. f4 z1 C% |等待程序,4 n3 u/ ]0 @5 ^$ V: Q
保持飞机在指定空域等待空中交通指挥的下一步许可4 l/ @ j9 _8 ?/ }$ z/ Y
的预定机动动作。也用在地面操纵来保持飞机在指定的地
' B: k8 V' X' f E0 h区内,或在指定点等待空中交通指挥的下一步许可。标准
* ?# }+ | `( e& G5 N的等待时间是在14,000英尺或高度层40以下时1分钟,
! F8 D% z$ |! G8 n以上为1分半钟。有些国家以飞行高度层200作1分钟和
1 x# S* w# ^: C1 o y8 B3 ~1分半钟的划分。+ ]- O! o4 G! G, s/ Z
ra3 |; D6 h& H b( P2 U
m' g$ [1 N9 ^ J6 v) n$ N/ J
speed (u
5 V/ B) z) Q' o& i! ]point on
* N+ w$ E! c2 w p* J; M! fradius ex
2 F% {. }( Y8 _, f3 v% J; Zdesigned to expedite aircraft turning off the runway a# w9 U& _0 s& O5 N
landing, thus reducing runway occup
+ j* F% G d uHOIST, A device for lowering and lifting an engine o
) [6 X+ d; x* f" {/ E. f( d4 v# Mh" q. M& e6 P6 I0 g# J# |
a6 `- R# C9 U0 ]4 k+ B6 F3 \7 l
H
6 [+ r; Q4 { }5 I1 D& _- O& Zp& h1 L3 p( {6 }& p- O
H1 {5 c, [/ W( A
which keeps aircraft within a specified air space while
, ~, a! J! @- u' ~( H( l2 ^) Uawaiting further clearance from air traffi
% g9 b+ L5 Y ?9 V9 sH- e: K/ \7 X$ m2 b `2 u4 `
m
3 t _5 r/ p6 O# D+ Q! X9 h K) ka( q/ r9 d" i; f+ q
c
3 ?5 R$ n1 U7 h: J3 ya
2 _4 K9 c( U$ \# {w/ L& H5 W4 \; r4 s
T
$ k5 V" [# d! g$ K$ A1( p& `$ s7 y9 H" Q; M/ A
s# p" n: V( e* X# d4 @
some countries.3 G# H3 r6 x' k$ k- `6 J: w: p
高速滑行道/出口
3 f5 g y& J+ M是一条半径大的滑行
6 H3 J' P. }: B& E机
# P6 D) g; ?7 a: c. \3 K过
\) _+ t& L0 |6 I设2 P- b2 n. r. n( L- j! o
的9 E! X8 w' B: p+ @* \9 s4 a
吊车,
/ K) E8 Y. I% W/ ~4 v8 ]0 G4 l在发动机或重部件拆卸和- y3 V( r) X: y0 E! E: i/ ?; M
发
3 Z8 E: T+ ~, A b% Q等
0 l n7 I9 a% A/ X. a! P等
. j9 G% y; B ?, c使飞机
+ m: A; c4 H7 r的预定机动动作。, Y& x2 N5 ]% g* Y( B8 a7 i
1- h% k, f$ i- z6 Z1 }+ _
英汉对照民用航空词典B OEING J7 Y% C5 |5 s" p
TECHNICAL DICTIONARY 77
5 K' @- e9 t3 d6 J) aHOLDING FIX, A specified fix identifiable to a pilot by
% }. v! M) C/ k3 ?9 K# a% l$ {9 INAVAIDs or visual reference to the ground used as a
# j% X+ ]+ p7 n- R/ P8 Nference point in establishing and maintaining the; D# }2 q$ y$ r9 E8 c6 e
osition of an aircraft while holding.0 m }% y% d& l. ~3 q/ b
OMB, A hexagonal material made of metal or/ |% G, w" n% K# S$ l8 Y
omex for sandwich construction of panels.2 Z U1 d3 o: q. Y: z
HORIZONTAL STABILIZER, The moveable horizontal
# I4 U# Q# l1 C6 X1 \7 Ssurface of the empennage used for pitch trim.. g4 K. D" B/ r/ y) i
HOT BATTERY BUS, A battery bus which is not
, d" ]$ G/ ^- I3 q3 oswitched and is always energized from the airplane# a) Z% L2 J1 A1 T
battery.
5 y/ ^# q: Y6 Q! @使用的一个指定
) R( ^/ y8 @% p位点。飞行员可根据导航台或地面目机参考识别该定位: C4 F+ Y8 G7 E J1 ~9 G' B9 g. P
。$ C6 p! U/ V! \* H/ a5 q
窝,9 z) }0 _8 ]2 _, ]" C7 N
一种用金属或Nomex制成的六角形材料,用以制造夹芯
& {& v( L+ u, M: a# J" i板。
/ O1 g/ f o1 O/ M- `" b& T水平安定面,
7 K c5 W a. g. t8 G0 y飞机尾翼的可动水平面,用来控制俯仰配平。
: H4 `, {6 f! ^/ y7 t热电瓶汇流条,7 y% M* O, Y7 A
无电门控制的电瓶汇流条,始终由飞机电瓶供电。4 p R6 m7 S2 {$ ^" ?
re4 `9 N4 i7 s; u/ ?4 J
p
3 z, E4 G1 h6 @HONEYC
; l; e5 F* E$ ON
$ v, a$ s# @+ T9 F等待定位点,
4 u: l; \" G; l等待过程中在建立并保持飞机位置时
# J4 L( S% S3 g6 X' m; J定, e& T. a. K/ T
点
: _* Y/ m. `. R蜂
+ E1 D& c9 D2 H7 S, P面" i; ]: f- b/ x1 U: X5 ]7 u& A
英汉对照民用航空词典B OEING a$ e0 T. x2 _* Q- H3 w' l9 O
TECHNICAL DICTIONARY 78
0 L5 o k9 w& M. }HUB CAP, An external covering to the axle of the main
0 @* I4 f- [5 a8 G( \9 C: O g% J9 ]landing gear wheels.
1 P- j' Q* q) HHYDRAULIC FUSE, A device in the hydraulic system- c3 z9 }6 ^( s9 l, m( H( z/ u
r stopping fluid flow when a leakage occurs in a line* v) C' V! u. T9 {' B; A8 M
ownstream of the fuse.. C9 W2 F1 O7 g% q& I
S, SEE - INDICATED AIRSPEED# U: S4 i! y& N7 v; T0 a% M) F* k, u
ER PLUG), An electrical device for. F2 y- Y) E0 }1 t
producing a spark in the combustion chamber.
; E7 @# s2 T! R- Y& N压保险,
' ^2 T. l" @, [( R i+ k" K液压系统内的一种装置。用于在保险的下游管线上发生
. m* n; F; l& ~. e. n; F2 O4 X2 u; w. V7 q漏时,阻止液压油流动。
4 n/ V) L& h9 u) Z5 y2 f示空速,& n+ J, S7 B0 o0 ]" W# v
见Indicated Airspeed
4 i; F$ X* F2 c, w) vfo( U0 c, s+ i8 B; f9 l
d
/ s8 C* i3 J6 JI IA6 w K, I9 ?- T/ k6 f/ `# [+ ?
IGNITER (IGNIT
0 Q- V$ w7 t& T, e轮榖帽,
0 c2 [* c+ h8 m+ t) w3 x8 d主起落架轮轴的外罩。
' k# i, L( N+ a液
; q- }& t& w* h! r6 i泄
) S: Y3 D& [: M- \指5 J9 U- ]% v1 t; M7 k1 j. D
.9 N* f0 `2 e' u' i x( c
在燃烧室内产生火花的电器。
4 I2 j F; i& C* K3 B& R: g点火器(火花塞),
8 Y0 ?; O5 i( S0 B英汉对照民用航空词典B OEING5 `% t1 o$ i5 I
TECHNICAL DICTIONARY 79
; s; A& @5 w0 S8 b$ I: ?% XIGNITION EXCITER, An electrical component for. S. _" |) H; S
supplying high voltage to the igniters for producing a8 F/ H! d, w5 [3 X. h; u
spark.
I" C6 u0 D! M( l' RIGNITION SYSTEM, A system for starting or continuing! T! z) t& a4 _! a. i
combustion of the fuel-air mixture in the engine% p" e% Y0 }: Q, G
combustion chamber.
, ^+ @, D f% b7 ~4 K% ?S, SEE - INSTRUMENT LANDING SYSTEM
$ x& L, c3 j+ GPROVED CLIMB PERFORMANCE, The rotation and
! ^' n8 }8 O( F8 B, K; c6 Blimbout speed increased above normal to increase
F C7 H z( y* T) e7 z$ G3 a6 ]; NDICATED AIRSPEED (IAS), The airspeed read6 [4 y& Z% ?5 E: T
火系统,
8 }9 @2 F; E* i1 [, w一个使油气混合物在发动机燃烧室内开始或继续燃烧
* E6 `3 G" C d8 L+ ~1 C, f7 Y* ^系统。& D- K; U, X" m, C ^! J: X
表着陆系统,' G5 d/ W, }* w$ m8 Y. d2 K0 s/ R
trument Landing System6 d9 ?8 q* R' [! b* t
ILLUMINATE, To turn on or to provide light.1 y2 P0 I5 {& w% r' P+ J! P
IL) G4 {3 a7 t+ e6 U! S
IM, @ q9 O6 J" i* Q( d4 l
c k) |9 ?: L0 v$ T( C
airplane climb performance, especially if an engine
+ S6 J3 h: X+ k4 ^( Rquits.4 P+ W. f* A. U$ |) ^# j2 g9 B
IN N$ B* Y- F K1 V$ F2 a2 e
directly from the airspeed indicator without any
! |) r! H3 r: W% c; I6 ]" vcompensation.9 y& s5 k2 Z% r: [6 k
INDICATOR, A component for showing quantity,1 a' p7 i" l9 [3 O( \! H' t
pressure, temperature or position by a pointer or
$ ?# M$ i/ n- Q. Fnumerical display. (Similar to gage (gauge)).
* C# b |0 B8 f' V点火激励器,
9 D" d2 ]" v3 C% h" ]4 Y9 s向点火器提供高电压使之产生火花的电子部件。! B/ `- a# q/ [. n3 r4 Y3 X- r
点( w6 Y$ G6 a; I- U0 Q4 ^9 {# P
的1 a* i9 L+ c* ]; m% n
照明,
6 S4 W4 p! @% j$ M( b. P( O/ W打开或提供灯光。
$ Z: l; t! t, D: O" }仪 i) S5 R8 Z/ f g
见Ins .
4 R+ q; r9 \: e" D D3 `2 |进爬升性能,
1 _6 D; e% V6 c4 ^用大于正常的抬轮和爬升速度,来改善飞机的爬升性
% E4 x5 a5 l8 s H! m一台发动机不工作时。
7 E) O. C- e7 b' D, Z示空速(IAS),
( E! m& S d$ e2 {7 H4 ]正直接从空速表上读出的空速。" H- F6 O' i! q: D: C
指示数量,压力,温度或位置的部件(与. G. V7 Z& x- d8 m% K
计量仪类似)。
$ C. N0 B( b8 V& e- x) ], e ?改
7 W) U4 S: v0 q2 s能,尤其是在& G" F! U( k* _$ W
指
" A4 y) \$ a, O' y6 m! z# d未经任何校
# m4 d$ c& D2 ?7 ?" `指示器,+ o. c& p& {5 g! w+ {0 v
用指针或数字来$ Z" {8 a) Z9 L* J; L3 h' q( @! W
英汉对照民用航空词典B OEING2 k6 s' G: w h
TECHNICAL DICTIONARY 80. ^+ E- g% [- y
INERTIAL REFERENCE SYSTEM, A self-contained,/ G3 [% F: A1 H4 {* v# d' y
navigational system based on the measurement of2 ?' j" B5 M8 v% N3 u
acceleration and attitude.
& C4 z% y# \+ K3 Z: RINFLIGHT PERFORMANCE, The performance of the- k& C* x7 Y6 I! X9 N, v0 I
ITIAL APPROACH FIX (IAF), The fix which identifies
! _- l" w- h2 }: \, `e beginning of the approach to an airport.
; z4 n2 V* s" G; i% I5 S1 Z8 }LET GUIDE VANES, A fixed set of blades in front of; V! U. K$ E- N& u1 C
n engine compressor for directing airflow to the y( R9 L9 _% Z; V0 U, v5 _
ompressor.& w8 N; U) m# ` T4 |0 J
NER LOOP CONTROL, For autopilot operation this is
3 g) C5 \4 \/ Y1 m" l' y8 ke basis control of airplane pitch and roll attitude
# J- |1 X/ g7 _6 M7 B' {4 w7 }中性能,8 z* K0 z/ @3 y) B4 d! S
飞机的性能。
* _. m( b3 F5 L h$ y: @起始进近定位点(IAF)," h4 [ L5 G/ G# K
标志向着陆机场进近开始的定位点。! N7 Q( ~& i' F$ J9 m
进口导向叶片,) c8 q7 N% a) r% c% B) a
发动机压气机前的一组固定叶片,用以引导气流进人压8 w3 b) l6 N8 X4 G
气机。
& v5 z. ^- l( a" z环路控制,
1 d2 [- J& e4 M! \* y$ U对于自动驾驶仪操作,这是无关飞行航道的飞机俯仰姿
4 W: b% A: t7 t$ u- P2 j- F+ _, }制。
, P( h1 _) g4 M3 Gaircraft while enroute.3 L& E; c# |+ H) c! V
IN# I& x, J4 v! n9 P5 x# o
th6 p( {0 {: A+ U- f7 \1 _
IN3 [; L* R" }' I, s3 u
a
" H+ a! D' I ~- ^/ L; g) x2 Sc
( X: d% ~: b! E( y a2 gIN) J/ }) s) a% v* g8 w3 q
th
) n1 u8 N$ B& A rwithout regard to flight path.
4 {2 m4 A- p% ]! |惯性基准系统,; I" {( z9 M4 J
以测量飞机的加速和姿态为基础的独立导航系统。, c: x G$ m3 C' l. |+ ~
空, B/ C) [5 q; R- v) x4 L
飞行中: ?/ G* _* H( W1 Z9 N
内
6 }2 X# R+ s3 ?7 l5 `# d态和坡度的基本控
3 q0 K4 a: O9 R. U英汉对照民用航空词典B OEING2 {, y$ }) J' E/ F# T0 e G4 r8 i6 x
TECHNICAL DICTIONARY 81
; f( s- W |8 ~INNER MARKER, A marker beacon located between
, M( Z b& \# ithe middle marker and the end of the ILS runway.
3 C' `. Y7 O7 _1 A9 EOP, SEE - INOPERATIVE
) ]$ u* Z' @$ ZOPERATIVE, Not working or operating.2 J2 B8 N7 p! S2 Z$ b% h& a2 C
STRUMENT FLIGHT RULES (IFR), Rules governing
8 D k" V- ]6 y8 D5 Y4 x! Ge procedures for conducting instrument flight. Also a0 K. b/ S; K% z' x( [7 Y
rm used by pilots and controllers to indicate type of1 y6 D: Z U }
ight plan.
. e5 j" b+ p; {) ?8 p5 W/ u8 }5 ]" fSTRUMENT LANDING SYSTEM, A precision4 b! l6 t. g' D' K: H/ t) c
strument approach system which normally consists of" I4 Y) I! e2 J+ J6 m2 d
e following airplane components: localizer receiver,9 @& R. V% }. Z5 i# Q
lide slope receiver, and marker beacon receiver.
/ x: O4 d+ z6 b) l) {/ ]9 GOLOGICAL CONDITIONS: o7 h' q/ y% H0 H. ~ T" X& J6 `9 e
MC), Meteorological conditions expressed in terms of
1 n' j0 }& |8 V& W# @: `isibility, distance from cloud, and ceiling less than the
8 N, [) C. D! e" X( @! |% S. }8 jinimums specified for visual meteorological
1 l9 o- J- L) H% f) ?; C( _* V" oitions.1 e! }" d" }. g% |+ c0 V% M" D4 l5 ]
STRUMENT RUNWAY, A runway equipped with
" n7 U7 `8 a% e* E w: Mlectronic and visual navigation aids for which a/ w5 k# z& u: n6 ^) a' r, J
recision or nonprecision approach procedure having$ W7 J4 i& M/ V
间的信标台。8 n4 n- @; C' O+ b
不工作的,
* ~) e2 Z+ M: I; M+ T见Inoperative
4 I; f) P* V" v6 `) B7 nIN$ J- D) R" n2 b7 [. Y! Y
IN
! g" Y' K3 J, e( x% s$ bIN# T' ?) b" Y* Z5 h: D0 s$ p) D
th C% g( s& P. ~, }/ y
te
1 E) P6 a5 r2 u7 ?9 l8 zfl
( D5 t% X5 y8 ?; iIN8 Y7 m! x& W8 ^" p- U. v
in' H5 e, H) z. q; T) Z ~% I8 f) W
th/ o a' e0 n( I
g
% u/ s' Y/ s1 `INSTRUMENT METEOR* D0 G! b7 |* m
(I) }) K* | |% O( a0 Z6 i4 j
v
* V7 W, d. [6 J! O5 pm
% {0 {# F% O7 Y& Z2 s/ |4 M0 Dcond
& Y9 _8 y/ g2 O7 c1 }IN3 G( K/ W. d, ^5 N' J
e
: Z" X2 S% M% `6 l7 W6 }p
- o+ ]0 o- ]- {, bstraight-in landing minimums have been established.! X. k& s5 X% A- q* G
近指点标,# h: H& s( s0 @- z
位于盲降跑道头和中台之
6 X9 D5 n: ~* m% O) W2 ]/ }3 Q& C.
% r) M. I2 {1 D不工作,
! [: c+ n+ L; Q* z+ C8 E5 z5 U不工作或无法进行操纵。# D6 d I" [- }7 X! ]
仪表飞行规则(IFR),% P- C5 p) y4 e# m8 p
仪表飞行程序所需遵守的规则。
; Y- T* R& J E' l7 o( K5 }仪表着陆系统,5 n+ x' S8 ~( o
一种精密仪表进近系统。一般由航向道信号接收机,下
* d4 [) v+ y' @1 F滑道信号接收机,和指点信标接收机所组成。! H! }7 h) r9 \$ D
以能见度,与云的距离,和云幕高低于最小规定的目视9 T- k& a. v$ }# Y
象条件的一种气象状态的表达。0 W- a# Q# p" J* T( Y& F5 F: `' H
用于以精密或非精密进近程序作订明最低天气标准直# i. u# A/ q' T+ ]' u1 O) G+ a
着陆的装备有电子和目视助航设备的跑道。
Z( H0 D0 C% p# i) v/ F仪表飞行气象条件(IMC),( c3 m2 N+ h% k" g0 a$ o0 B, c
气9 P! d1 G5 Q( ], q6 m/ e
仪表跑道,
0 A* n \3 d1 x4 T1 Z9 Z0 k线+ p- g6 i0 d/ f. p+ `: z' q; R+ Z3 A
英汉对照民用航空词典B OEING2 |( g2 U" p( \. R4 @& c
TECHNICAL DICTIONARY 82
0 l/ m" E1 U" U) u# ?# YINTEGRAL TANK, A metal container formed by the8 L4 J1 {) R9 b- }$ F( \, z7 m
lane.
2 q8 g' r0 O7 V1 ^' j+ ^5 |& ~+ Z, Xcted4 s, S7 ]7 g" y% g/ b4 E. C* v
circuits.
9 F- Z3 Q: C$ n' |8 A$ IManual, A( M: z$ u3 A) `6 u; J/ _
erformance data providing range as a function of a7 V+ \* q' a2 L" }, z. h
hange in airplane gross weight.& t, u$ P. B. S
TERNATIONAL RESERVES, Reserves required by
! p. K: H0 A& h4 w! m5 J2 ]# m( Qe applicable governing agency when flying
6 q2 `* y" X; f+ n8 NTERNATIONAL STANDARD ATMOSPHERE (ISA),( e7 b1 [/ q& ^5 |* R. A6 O# X
he hypothetical vertical distribution of atmospheric
3 {5 N3 L) I0 C( Pmperature, pressure, and density as defined by the8 J' }2 \+ s8 p
).
# V5 L0 u, j" ^- WTEGRATOR, An operational amplifier whose output5 l& j9 l5 ^9 e, m
oltage is determined by the input voltage, the input8 f( A' Q N! G* @* A6 N5 C
上7 e) D5 [" P& ]. o0 `
存燃油的金属容器。 B8 i: d& D% T2 s/ D
,; H4 Z& k7 x) c% h( }2 C9 j' E
飞机总重量的函数提供的性能数
2 g' w# N6 U6 `。
- |' }8 i$ m8 g0 K* t际航线备用油量,
4 S9 ~# y: u' k( \; u4 r6 _在国际航线飞行时,有关的政府单位所要求的备用燃油
R& x$ D7 Q q( M际标准大气(ISA),8 X( O @# Q* K8 Y7 a5 A
国际民航组织(ICAO)规定的,一种只在理论上存在* ]9 C4 G, k( ^3 ]
大气其温度,压力,和密度的垂直分布。7 h" d" L0 ^& z0 x. R- _" k
分器,' j' e0 \0 z1 D
由输人电压,输人电阻,反馈电容和时间微分而决定其
* R6 @' C. R; z; |1 j运算放大器。
P9 X! o8 @" q" Uwing structure (spars, ribs, skin) for storage of fuel on4 r6 I' T' X" a' |: C! Q! i
the airp
" F& h( u0 y% L4 VINTEGRATED CIRCUIT, A small piece of
" C, r$ b. o8 U7 f Zsemiconductive material that contains interconne
$ ~0 e% k, ~9 Y' F- ?miniaturized electronic# J M# O7 q. G5 x1 o) ]
INTEGRATED RANGE, Tabular Operations
+ B) Y( j5 x7 K5 |p5 z: K. F5 _# W; p7 f
c, O0 v$ o7 t. I/ r
IN( \8 q* C. f$ V# v& t
th. P1 `. t/ X& h2 N4 o8 F
international air route.
# r: W1 J" a n( Z# v9 _" MIN* F; { T+ X( P0 q/ a0 G
T( V( F" p" y+ [' G9 ]5 I- t2 n
te: O1 c! h: _+ Z# g2 S2 r
International Civil Aeronautical Organization (ICAO
& ?" b( _- M: GIN$ z* F) e: `* I* `8 [4 H
v5 K% ?9 z" Q% c8 {- z" N
resistance, the feedback capacitance, and time
D' n( h' D3 X) tdifferential.# S4 T- d) I( [) `
整体油箱,, R" p7 N5 \$ c/ I; H( d! L
由机翼结构件(梁、肋、蒙皮)组成,用来在飞机; i$ x2 r7 e0 P; {8 f& y
储1 m. M3 l" [8 Q+ ?& P1 {3 b. c
集成电路,+ ^2 ~+ H, V" u# C5 N' M
一小片内含相互连接的微缩电路的半导体材料。
/ A2 y; t) D5 F- H综合航程8 Z7 H! r x( j/ t! |2 ?+ ^
使用手册将航程作为' T, D' x) x8 j+ D, t1 C% x7 t/ b
据' Q2 t" Z% a, e6 M' A: Q
国! J; b: u6 v( |) p2 @
量。
/ Q; R. y# Z; w( C7 V7 K国
, S" K3 b! N: X8 E0 R; L的0 D$ }6 W! n% G( m- b& L5 l
积
1 C0 l3 P! @( x( s输出电压的" E2 t( d/ N; w Z
英汉对照民用航空词典B OEING
) I: I% I* K# P/ [TECHNICAL DICTIONARY 83
9 [) p/ v7 Y# ?* N! aINTERLOCK, A wire connected in series with an
) f q; a+ Q: |' G# `" M0 wequipment or device, or a condition that allows8 _8 B! M! w7 c( e3 y9 A5 F
operation if all requirements are met.+ j4 ^ q1 _% G5 `0 t( ]
f the United Nations whose
* U3 O1 p- [8 Ubjective is to develop the principles and techniques of
\* D' z( a% G- b8 B1 ^3 j, Sternational air navigation and to foster planning and( Z6 k( `0 T t) |# \
evelopment of international civil air transport.1 }: j: ?: m8 H/ |# Y; Z
TERROGATOR, The ground-based surveillance
% n p5 F; r9 l+ ^1 ~dar beacon transmitter-receiver, which normally scans2 K! Z; j: d1 ~: D3 t! Q8 N
ll( X% C" G8 m8 W6 Z2 W t4 A
on the mode being used to reply. The! _. c: M& C& v! N! P
plies received are mixed with the primary radar
' y; `5 s/ ~1 D' N6 cturns and displayed on the same plan position radar
. N8 Y* Y" A# J5 N3 G3 d- ^cope.
/ H {; m; u2 f) w* o9 u# VTERSECTION,
( V: v/ I% Y# |; {; l) l9 `- w( D1. A point defined by any combination of courses,9 \5 N% r0 l# K/ x( n2 r1 z9 s
radials or bearings of two or more navigational
# D1 E2 ]' O/ c+ h; U9 e4 paids." h _3 g$ |0 ~/ w) {4 n$ R* L
2. Used to describe the point where two runways Z1 }) W- h: V6 g( t N# }
cross, a taxiway and a runway cross, or two0 b7 {' _* B! \8 w" o* d; H0 f
taxiways cross.6 }2 m3 S/ p! y1 P H6 V: T
cy)
' y' W$ s. ^4 V1 u- O$ K% Ctem.6 }2 O0 q5 p% x- u8 z% ~
者8 k. ^) d9 S/ o: L+ Z+ w
当所有条件都满足时才能工作的状态。
3 Y8 r! V4 _0 u组织,- M1 Z/ U' v+ L' q. Y/ ?4 T* A' x
航的原则和技术,促进国际民航
5 f% e& K6 S- u5 a输的计划与发展为目标的联合国专业代理组织: O- ?" Q0 s" ^9 d6 X* ~$ P# \
问器,
6 J9 [7 a2 X6 e9 [一种地面监视雷达信标收发机。通常在工作时与主雷达
, ?: K) y; P% V, o# A连续的无线电信号,不断地重复要求与6 N0 g5 ?7 e# \
接收到的信号相混合,显示在同一平面位置的雷0 P3 ?6 n* R5 e! b2 e a
达屏幕上。1 I5 Q x$ @6 Y8 ^0 g3 n2 J
交叉点,
3 V+ b) u4 i: D4 `* u1. 由航线,径向方位线,或两个以上的助航设备9 W" \+ i" z5 c9 e. p4 x& K
的方位交会而确定的一点。, Z. f# K) x. x
2. 指两条跑道的,滑行道与跑道,或两条滑行道
/ i! O/ m ?7 q. g8 P+ j的交叉点。
' J: v- y; ^) n' X/ \( a J: b0 ZINTERNATIONAL CIVIL AVIATION ORGANIZATION,; ~% W% ^$ G, {# X o
A specialized agency o- q0 I' `" f' s1 V+ y# m
o
]9 B+ I' B( z! [4 K* v; F. c, din' M3 V6 } d9 x1 X5 M+ P; H
d
3 e( `4 \+ I) G3 C# @% R: AIN
% i! x+ p! ^7 H* V' `, ]ra
9 |+ H0 ~! D, N9 o7 f/ l6 `in synchronism with a primary radar, transmitting
9 i" Q& n; w3 h) ^discrete radio signals which repetitiously request a. A% X- @2 v, J1 _
transponders% B7 T5 m. W+ R O
re
+ s6 R `. y8 S3 _re
4 E% I! q, o4 ^' ?+ ]s) Z$ t& W& u! H" Q; U# _" ]
IN4 {( A: E. v" J1 E+ X4 I' b
INVERTER, An electrical device for changing direct4 t' D. f" f) c. s7 j' ]
current to alternating current for standby (emergen8 {9 {% _' s T' e3 R
power supply to electrical sys
# f8 l) W! [% Z N, @# b* c联锁,
: x. x: p& n: { F7 H; K一个以串联方式将仪器,设备联接在一起的电路。或/ e2 |. \2 N' g3 w a' N- {7 p
是% Q- f) L0 {7 Y6 M& q. n0 Q
国际民用航空# E3 a0 R$ v" ^5 F! G: Y
一个以增进国际航空导
7 I/ o; B4 L4 A6 _. \8 m e) s9 q+ `运
+ ~ q3 n$ q! w! i( H2 h! s询
5 ~5 T) K$ j5 b- X同步扫描,发射不
3 ]& C& a2 [, Y1 r7 w其工作方式一致的应答机进行回答。所接收到的回答信号
: ^- g+ z$ U! l' N3 C2 X与主雷达/ k. z& w" `: M! k7 P3 K$ v- f
变流器,
. E; u6 R# `! `" f用来将直流电变成交流电;以供电气系统备用(紧急)
6 }0 Q8 ] k# f j6 P电源的电气装置。' C3 m0 f6 |" A* j
英汉对照民用航空词典B OEING
' H5 z& M# q! s3 [1 C/ x: `5 o' fTECHNICAL DICTIONARY 840 P0 M! Q# A$ k+ v) O& H+ O8 Y
IRS, SEE - INERTIAL REFERENCE SYSTEM
& R4 c8 h) f H" `* g5 c1 Y: {ISA DEVIATION, The amount of temperature or
% m$ k* }, T4 ~6 r* f, Nsee International5 x- W; z# f! K( t0 Z6 E H0 e# }
tandard Atmosphere).0 ^7 B* T9 p7 q) P% Y1 d' I* q
LAND RESERVES, Reserves required by the
* ^1 G N h4 ?- g2 ipplicable governing agency when flying routes
1 R- R/ h. `2 f+ Setween islands with no alternate airports.
/ J1 ~2 d6 I$ i, m/ R; ACONDITION, Cabin pressure (altitude)4 n ^2 P( `& ^7 S
maining constant with changing airplane altitude." A. J* l/ f# R& e1 M
ising the
$ \) E" M `' c$ a( {+ j+ P% `a, _2 D: \$ u/ l# _: {: ^1 y H5 I! B( f
,
. i r3 X x! o1 Q# l8 Fpressure difference from ISA (
/ t y# ]) ?" u, oS3 R' u6 L4 w1 N6 |$ h2 \, W
IS N2 [4 k7 {! `
a
! H2 z- F$ o- c2 u9 K rb: J9 U W) ?1 ^3 Q/ U+ P' t, c& _
ISOBARIC6 B( x3 o- e! a5 k
re
$ j% V2 b c' G5 D! u+ WISOLATION VALVE, A valve in the system for+ z; m9 e8 H4 s! c9 G& a$ M! b
separation of the system into sections.! T$ b8 I* _# a: L
J
I& M8 ] ~& d3 \. W# K4 C7 @; q) }JACK, A mechanical or hydraulic device for ra
% B) S& L, P0 B4 I1 s* iairplane.
1 V/ d. ]! e& `7 MJACKING POINT, Location on the airplane for using3 _% p: R% W5 P4 w5 V" g1 ~4 m# C
jack.4 E1 A6 T8 ~: z4 M
惯性基准系统
" o6 L" S7 X. i0 R见Inertial Reference System./ D* K: X$ k3 X N3 N2 O
与国际标准大气之偏差,
# Q2 Y6 e8 N3 w# |( `6 x压力与国际标准大气的差值(参见国际标准
. S p8 ]/ j" y4 J- b% S' w有关政府单位要求在没有备降场的岛屿间飞行的飞机2 f3 ^# b" r' z3 ?0 \: i/ v
带的备用燃油量。
8 o/ ?8 j! y0 j; {压状况,
- E; z9 ]/ k5 }! n# A$ T在飞机改变高度时,座舱压力(即座舱高度)保持不变
8 N# ?' N* K4 s状况。 u! ~, q# u" A& D+ b. u; g
斤顶,; s2 \+ W. M( A5 c' U7 n ^) c) N
用以将飞机抬起的机械式或液压式的装置。0 s' c c7 j. [# z2 j( Z8 `. ]
温度或
$ h4 W. x" t8 m" M: D/ L; n大气)。
: ?! l1 Z5 e/ D& T0 B' E岛屿备用油量,* u6 V; K: M. R
携
( G/ A( B7 ~1 W- E1 H等' Z& j$ N$ g, R: k# I- k
的
% q8 t( y6 D0 j5 V6 b |隔离活门,) N# P @" a p* A3 b
用以将系统分隔成几个部份的活门。
0 _5 C4 P, E" l$ C5 E6 j) R/ j千
% [7 @) {$ S2 p( q( R' t千斤顶支点,: V5 a3 I* Q g, ]8 v* q4 x
飞机上可以让千斤顶吃力的位置。2 y' k; l. K# @2 ]
英汉对照民用航空词典B OEING" ?) x, T! a2 `8 v
TECHNICAL DICTIONARY 85
" H( y' a0 [! e) n. ~! uJACKSCREW, A rotating threaded rod used to drive% P- R1 U! h' M6 d5 r( s/ Z
moveable component such as a flap or stabilizer.& G* [0 J* d6 v% W
a 致动螺杆,2 R2 Z! u- c9 {; J
用来使可动部件如襟翼或水平安定面运动的能够旋转
7 J) \* i1 w! c的螺杆。( c1 Q6 q( J1 X' I
英汉对照民用航空词典B OEING
9 ]7 ]2 y& P3 H) m, qTECHNICAL DICTIONARY 86
( B- @+ ^% I1 ]6 gJET PIPE, A control component in some valves and7 t0 a& P7 T, z7 V5 l" t5 M
ET PUMP, A component in the fuel system, operated
7 _; ^2 A$ h4 i* o7 U8 mr removing water and fuel from a fuel
' \5 x* A m! E* r! ynk.9 G3 K: s% u) G3 s& o
射泵,
9 E! H" b% k1 O8 A7 i$ N, B! T内,由燃油压力来操作,用于从燃油箱中排除, k$ D' M1 ?; V7 ]. e! H7 a+ a
和燃油的部件。
& _8 M, Q# M5 s; {: S# c2 m/ ~5 Eactuators for controlling the flow of hydraulics or. G; o! V7 Y7 r& ]2 e
pneumatics.( }. ?9 ?2 D7 Y! |' }: M; N, y+ T5 l% U
J
1 A7 f" `/ b% ^; e8 zby fuel pressure, fo+ O4 g7 A7 w# p& P J* W
ta
4 T5 Y; t% Q1 B1 Q& N喷射管,; j- y! w4 q y- W! O
在有些活门和作动筒中的控制元件。用于控制液压和
% Y# M7 |$ j7 H* K+ O5 N气动的流量。
1 j) `5 x2 ~6 Q0 f, f5 a! m引
" }4 O0 W6 Y1 F4 l! |2 n2 [) ~0 f燃油系统% D q* G6 P# o1 \- P
水
8 {4 A6 p% ~3 U$ ^) H7 I8 P英汉对照民用航空词典B OEING3 ~5 _: V( V; e1 o$ ` q
TECHNICAL DICTIONARY 873 u6 k+ ] L! B; m
JOGGLE, An offset in sheet metal construction* U8 k/ s3 t* K( E% s7 l# [
designed to allow one piece to overlap, either higher or
; ?: S& e( r+ P* d$ |wer, the other piece.% g g7 H8 j [$ z! U T
OULE, A unit of electrical energy of 1 ampere of8 Q5 h9 ~$ v) R; P
urrent passing through a resistance of 1 ohm for 1
# g4 d+ ]9 Q9 q5 L0 aecond. Ignition system energy is measured in joules./ m8 m$ u: B$ B- @
UMPER WIRE, An electrical connector for temporarily
" Y+ o9 e2 x# A0 Vypassing part of an electrical current.7 P8 i; @8 F8 Q! J. n8 s/ I
UNCTION BOX, A container which serves as a joining7 [, `4 t" X: k% [ s$ D' L7 O! e
lace for electrical connections. May also contain
: [% S9 i2 |9 ~1 N& slectrical components.
* W7 g1 B1 M2 K+ o- h: u# N' WEEL BEAM, A structural beam in the fuselage center6 q9 K( }9 E2 p1 L
ection (wheel well and under wing center section) to/ W- y4 D2 V; ~) s9 ~
KEVLAR, A light, strong synthetic material for3 r8 A, k" J& Q
secondary airplane structure.
d% e+ t* D1 J5 a! o7 H; j+ O,使一件金属与另一
3 O6 @# B3 f" f' a y0 @相互叠合。* S5 _, _: ~: L7 ?! I% g
耳,
! d# u. D1 v! M6 ^0 R电能单位。一安培电流通过一欧姆电阻一秒钟所需的电
0 J: ?4 l8 n0 t0 {! @8 ?为一焦耳。点火系统的能量用焦耳度量。
$ h4 s/ x( m4 R+ V& K接线,
8 F4 `& o. s: H$ X7 w" w用来暂时旁通部份电流的电器连接件。
5 B9 g* F) W+ A) r) g) n线盒,
& d1 |. B$ |4 O* Q0 ^' |/ |/ f做为许多电接头的汇集处的容器。也可能内含电器。4 Z" X% z6 a" t4 W8 h3 s5 d) k* M9 E
梁,
1 G( u1 M! o3 z( d机身中段轮舱和翼下中段,用以防止机身弯曲的结构。
- i- {5 W9 C- f% ]KEVLAR,
) L3 M! e3 l/ b" h) M+ P一种即轻又强的人工合成材料,可供制造飞机的次要构6 B* Z I X3 @3 a% d- ]' O" ^- F4 ?
件。+ W7 D r$ F2 J8 T8 C
lo) e; ?. L1 c( X, D; K: V( N! x
J
6 U w) t& W5 j$ x( j; Hc
* o. A3 e1 k! C/ Q$ ~8 T* }s
& w& I' ?% O- j, y7 N) Q) pJ
1 J6 S: r( C+ r9 g+ _( g; db
O5 n9 \4 p4 wJ( y' u$ B2 Q" W* {5 v' a
p
9 ~3 s# M, e0 e. me
) R7 F9 W' i r* I1 b xK
$ m) i* Y8 E( ZK# G, c1 a |, k. ~/ G2 k# K
s, y9 q5 y n; ?2 X7 G3 {
prevent the fuselage from bending.+ W, F! D8 l* \% }; Y. o8 k+ s4 Z# z9 [
折接,
: t' _6 {( N9 W$ I8 p5 D一种平面金属结构设计的弥补法5 q% M0 |6 l: F' I3 k; v9 [* a
件
1 k1 c' H" S" t( M) u焦
. ~- `4 n, l3 \能
% r4 e- j) T9 i8 D$ ~2 k/ F跨
/ V7 A' F3 e2 [ T) m! |! V接
$ x+ ~" _' g+ i腹, p4 K; m" M5 [5 a) q
英汉对照民用航空词典B OEING+ V5 o+ V! T1 \, |: I! g o
TECHNICAL DICTIONARY 884 A3 e0 ?/ `: S/ Y5 r" M0 ~9 x
KILOWATT, An electrical energy unit, equal to one7 b! G; c) z; R- T. C4 ] M1 Z4 f
thousand watts, for specifying generator power output.3 a* a& \0 q2 a! T
KINK, A sharp bend, twist or dent in a section of tubing,, x. q* Y. \. t
wire bundle or angle stock.5 I0 a5 n! b2 f* Y Z
KNIFE EDGE, A very sharp edge on drilled or machined7 q% s9 V* M2 V
metal which is usually the source point for corrosive
& L3 t# V" r7 q! P- Sattack.; R* s3 E: u4 m9 Q2 q6 B( c
KNOT, One nautical mile per hour./ u, }5 ~. n! V4 v; J: `
KREUGER FLAP, A type of leading edge flap that is
b$ W4 Y4 h* [$ Yfixed on the lower side of the wing and rotates forward; D- u% R8 |9 a/ s" Q
into the airstream.
3 @8 T" Q8 |) ^2 X4 TKW, SEE - KILOWATT# Y1 a& h A2 V. K5 s
L/ l) ?1 O; ^+ P- m
LABYRINTH SEALS, Rotating and stationary; E$ e8 k8 K8 L1 d+ @% P/ \
overlapping structures which utilize differential air
& ^7 {" u# Y- P; xpressure to form an external seal. Most commonly used
( k4 H3 O$ a- b' r+ iin turbine engines.7 U q- |7 \9 u$ L9 C7 `3 [- T
扭结,/ W0 E9 M3 l2 b
在管路,电线扎,或角材中的尖角,扭转,和凹坑的部
6 K* V% a- M5 d% @, ^% p, g7 o份。
# |8 X5 \8 j1 |, }! y: w刀刃,& o1 ?/ U( @' d
钻制或机制金属的锋利边缘,通常是腐蚀的开始处。9 l( R. i+ C( z$ h' S
节(K,KT,KTS),, R% H; m5 W: j# G
每小时一海里的速度。
. ?% s2 v m2 @" L: p a& |克鲁格襟翼,- c$ A- [ i/ t' ?
一种前缘襟翼,位于机翼翼根附近,旋转前伸。
1 f* k1 |0 e0 |& P0 j: t千瓦,# ~/ R! p2 C) |1 G7 I8 G
见千瓦(Kilowatt
8 W0 `. d0 a4 j% p+ n. ~千瓦,
% o' }( |% N4 N5 U: ^电能单位。等于一千瓦。用以确定发电机的输出功率。/ q& G4 S# X* M, C# V% X
)。
2 m9 f. [6 |3 M! u( x蓖齿型密封装置,7 ?# V4 ~5 L8 ^4 w; N8 P% C
旋转并且固定的重选结构。用气压差动而造成外部的密1 y3 p/ B/ w! A+ q2 n) w
封。在涡轮发动机上最常用。
2 |; p7 |; E: G8 J6 |+ `英汉对照民用航空词典B OEING( S( N8 f3 Z* p/ k$ i. N% K
TECHNICAL DICTIONARY 89: E _8 E8 v9 i7 s. Q0 o
LAMINATED STRUCTURE, Composed of layers of a8 t( J+ C7 q7 l' s5 m3 z( `6 n
ake a
3 ^, C$ C, G2 T4 ~$ C- P6 v; Yht structure.. s' s7 I% z) p+ P: y0 X/ {
.E.D., SEE-LIGHT EMITTING DIODE.2 U7 y. Y( s5 C! x( c7 ]
ANDING GEAR, The nose and main wheels with the
' i* M# H& Y* g. a" V# ittachments for supporting the airplane on the ground.
. a' v% A9 Y+ F6 | L0 w- KLANDING GEAR DOORS, Panels operated by the- M! k. N3 z9 ~( E7 d/ I
landing gear for closing wheel wells when the landing- s$ r1 k* f4 ?. W" I
gear is retracted./ n' I% v5 ]5 V3 }/ I% m: _
LANDING WEIGHT, Gross weight of the airplane at the
: P2 H4 Z3 p3 |+ E0 ~1 X4 B# ?destination or alternate airport.
3 p. ?! }% S) V. l$ d, b! U" J发光二极管,
: Y$ j& r: ~, ~4 `( @. T: _3 I( O6 z见Light Emitting Diode
: T9 M9 S3 ]6 G2 S6 ], N4 I5 Ncomposite material bonded or cured together to m! l% m) h2 Q# @5 s
strong and lig
N7 |9 j8 `0 A; z2 jL; O9 Y) K) ?! f2 k! a( `& v
L( g& n" p# q! G0 h# L% ?' i. u% ^
a" ~$ u+ C$ v3 L, u1 O
分层结构,
8 n8 k7 v: h8 o- W( B4 j: P4 c% ~一种牢固而轻的结构。由多层的复合材料胶合或固化而
* z9 d$ z, D( J: B6 D& M! l8 P( d成。
* X! g4 @* q- W." R* @. U/ T4 o( G/ N" h+ U; t
起落架,
1 L9 r, S P: ^0 I" E* @用以在地面支撑飞机的前轮,主轮及其附件。
* c0 B, l: T) v3 }, Z9 S _起落架舱门,
/ j; _# R, ^4 S; p2 F+ Z' s9 |由起落架操作,用以在收上起落架后关闭轮舱的面板。
0 d2 S) m3 U4 F% R0 r3 r着陆重量,
5 t0 A6 Z+ g( j: k$ g飞机到目标机场或备降机场时的全重。0 I/ x7 P6 z* M4 B$ h% X1 K
英汉对照民用航空词典B OEING
0 K% b8 w9 O. y: dTECHNICAL DICTIONARY 90
* F- A, K% S' E3 b6 d2 ILANYARD, A cable for supporting or holding pan7 q& [# t& F+ Z4 U& T
open position.
& b0 |/ p! T: R) W; ^. G8 c- Qels in
, g3 B8 }5 \& W. M. j0 M4 q6 wAP JOINT, An overlapping sheet of metal, joined to the
; J7 X1 `# f" | a3 Z8 p; tdge of another sheet in aircraft structure.( e; V* y& K1 x" |$ E; e
ASER GYRO, A gyro which uses two laser light beams- p" b; ~, L0 I! m9 V- r
measure angular rotation.
+ G) A0 r5 w4 `.$ B" D! M# P, z/ D
ATITUDE, Measurement north or south of the equator
" ]& \8 b* c) b4 cs, minutes, and seconds. For INS equipped
1 A5 U( ~+ w# }9 W! B9 T6 V! Z, Rdegrees, minutes and tenth of minutes.! k0 L- {" @0 v" w1 l
l device for( e7 `, Y) o; s) {" E/ t2 _
hanging stored chemical energy into direct current.
: c T5 m" v. ]! r! V% L0 vses lead, lead oxide and sulphuric acid.5 ]' e! m+ x: h1 |; u {- s
搭接,
+ Y+ G2 q8 F% m. Y' F) _& K飞机结构中与相邻金属薄板连接的重选金属薄板。
7 z$ m( r$ S3 U! S% I激光陀螺仪,7 ~# X- v ]! d; O4 e! J, s
一种由两条激光光束来测量旋转角速度的陀螺仪。" W3 L- F1 @3 C
用以紧固或锁定的装置。
6 O z$ F7 |% g2 Z的轴。
- \8 R+ k/ d9 m( Z) Y( Q0 b方式。
( T# ]+ S% y" ]" ]* g度,5 {9 r) q8 @4 b5 ]0 s0 s- U% l
地球上与赤道平行之弧线。由赤道以北或以南度、分、# z, r% p% n' v. n
度量。对于有惯性导航系统的飞机则以度,分,和十等
0 }3 ?6 g5 }; X: t8 J& c- X度量。
0 l) P% p0 a( n; S# i/ y酸电瓶,
4 j! Y! s6 f& m0 G: B2 S将贮存的化学能转变为直流电的电气设备。它使用铅,
( r6 ^' @. o i u化铅,和硫酸。
% M' s; A" p, b2 _% V- L- cL
# h9 Z) E$ d N- m' p3 |' Ge
1 S: l5 K% Z& T I5 x- K; LL
1 K4 r4 a1 T2 gto
9 u* O4 t/ J5 Y$ {/ YLATCH, A device for fastening or locking.
: H* K: J3 c& `+ P$ iLATERAL AXIS, An axis passing through the airplane's& W7 m0 w+ u% U: X4 J M
center of gravity, from wingtip to wingtip, ~7 ], p; y0 D2 ~* E: F+ d/ }
LATERAL NAVIGATION, An autoflight mode in which3 Z+ m: y/ V7 _* T
the FMCS is used to control the airplane roll.
; Z$ o5 ~2 \# f* PL* V B. R+ I. c. i6 z+ Y
in degree
* b$ |' d" u7 l7 t+ X2 Taircraft in
9 \6 _# X2 M5 X6 i% fLEAD ACID BATTERY, An electrica3 f# G8 w. N! Z) e* l. R
c! r5 }$ N5 Q. z" C- a
U
/ O& s! F" R7 _. \牵索,
9 b. J8 I) s4 |+ \ N用以使面板保持在打开位置的钢索。6 ~$ V9 m: B+ S* U8 f
闩,3 T' j3 \) b1 f& n9 h
横轴,! h8 p$ [4 ^/ I0 A' j
通过飞机重心从一侧翼尖通向另一侧翼尖
0 ^' I: s- C' c% w0 C+ v水平导航,2 e5 R3 ]6 u; c; b, ^" x4 h
使用飞行管理计算机系统控制飞机横侧的一种自动飞# H5 ~: S/ i% ~6 r
行) G# d; Z, n- @, n! S
纬
& U* R! z: w) w% b秒& s2 B% D! Q* X/ |3 ^
分# H9 {, E8 f, ?' ~
铅
0 u' x5 B) p9 P8 A% |# `: [4 x1 _0 J氧' F' U; |2 N7 R1 J; ~ d: Y) C8 S
英汉对照民用航空词典B OEING7 J+ c0 M5 Y1 B5 {
TECHNICAL DICTIONARY 91
$ v/ U7 g0 _: S6 b6 [: ?) R+ N: p+ b0 JLEADING EDGE, The front edge of a wing, stabilizer or
, J" w1 ^ B# J; g3 [! GED, SEE - LIGHT EMITTING DIODE" ?) H- L( X/ s( x" V ]4 P
EMAC, Acronym for Leading Edge of the Mean) r* p. `& o- Y ?" q) e- x
erodynamic Chord./ z- r. I6 e* @% W
IFT, The vertical force produced by the airflow past the
7 _# r/ T& h8 n7 _4 ~8 w# Y& y+ S5 As of the wing.- o2 {. \) c2 {- i0 `' U
IGHT EMITTING DIODE, An electronic device which6 [, E& X: [0 f8 L) a- a: h
tes with red, amber or green light when supplied# n: X; Y5 q8 o; A; d4 i
ctric current.
5 Z+ |$ c9 s/ J,1 J0 y" r3 R1 E4 K X! A# t
control surface.# |8 c9 f Y( F- U+ M7 q/ K7 {
LEADING EDGE FLAP, SEE - FLAP
4 @( N/ {& v2 _# \ r: a9 ~L
1 U" u# d _4 j4 Q2 i @* TL
) o" o; `) X4 g8 H. Z- C9 VA
& g3 Q. ?0 R) M. _LEVEL-OFF ALTITUDE, Altitude of which the airflow5 Y8 {! a, v. H4 B2 Z$ _7 }
past the upper and lower surfaces of the wing.
$ M7 V9 [. [, N( x( M& R8 e8 UL
* C& O3 ]) e' Z0 supper and lower surface
& i! w/ L+ p3 `L
6 t) @8 j5 G, k; ]3 h% J0 nillumina# o9 I! ^/ x* I3 p2 s
with ele& C4 O* g. @4 N/ ^6 h+ G1 ~
前缘,5 M2 M0 t1 o6 H
机翼,安定面或操纵面的前部边缘。4 T- F: Q6 ~0 r6 T: L
前缘襟翼
; `" v" p( d, A* o2 F/ Y, n1 o& t见Flap., B0 S: v5 n6 P3 Q
发光二极管,
) z: R$ ?0 A) {) F W: _6 nht Emitting Diode' z3 ]+ [" J1 d- ^% R
见Lig .
' q: _8 r( k/ f2 F$ ]8 g均气动弦前缘,5 O4 ?. G2 w0 z5 J
平均气动弦前缘的缩写。见Leading Edge of the Mean* U* A/ Q$ u/ R
平. w5 d. M4 O9 s; ~
Aerodynamic Chord.. `( S" o2 @1 R3 e9 Y$ }) a$ y8 u
力,- ~1 y0 C! J; u' Y
过机翼上下表面所产生的垂直力。( j; O4 M' A8 O/ x* h7 [
光二极管,
* v. f. B8 ^4 b4 x6 {通电后能发出红色,琥珀色,或绿色光的电子元件。. T8 ^* A" k! B$ B
改平高度,
: |4 x2 f5 q) X3 [飞机因巡航时发动机发生故障而下降至的高度。
3 J1 B' P$ q) o9 f% K2 h' K: g$ F# R: _( g升. L0 B+ I/ l$ {/ A
气流流+ R) d% b* s5 P3 r/ {
发7 C" k! _! z Z" ?
英汉对照民用航空词典B OEING% l- M8 q2 V$ O( a+ Z
TECHNICAL DICTIONARY 923 w# o; M' S. U1 m: l# r
LIGHT PLATE, A component part of an instrument5 z. [5 g- G+ X s. v9 ?
panel for illumination of words on the panel.1 _5 J8 d2 E( ?- G: s2 t! _, ?/ a
LIGHT SWITCH, A switch which contains a light. The0 z4 F! E3 E& \$ B! w* m% n
opened or
7 m5 ?, A h" D1 J. Llosed.
; ~8 H7 j; w7 j6 U/ b# b0 ]n electric actuator which turns off electrical power to% g, z& ^+ N0 \" C, J& C
e actuator when the actuator reaches its open or; _. v/ ^. w. S* X
losed position.
$ ]3 N! S* H! n1 V" j. fIMITATIONS, Performance and operational limits
- ^9 K* N7 M- i# q6 ~$ b8 K" j5 Qsted in the Airplane Flight Manual (AFM), such as
' P8 R1 ]* p& h5 E- ]5 Z, c, E6 haximum airspeed, maximum altitude and center of0 e6 Q5 T! b( d/ {4 s6 \( E1 X
ravity constraints. j Y% b+ U2 b& y( ^7 g/ r M3 r3 o
y
3 P; Y' [" u' ^; Q2 V9 ?% Lcraft during line maintenance
; e. q" g2 C& b1 B- O9 K' |& Sperations.0 l/ O% |% p/ K7 n! A4 b
ontrol
2 Q. W8 z9 i7 x" x+ d+ Ldisplay unit allowing control of information to and from
. G0 P0 i: b. g- sthe scratch pad and designated areas of the display.- _ u A: s, N! h% n
光电门,
& I8 q' D1 L5 ]9 z* X. R/ O电门开关而决定灯的明灭。9 |. L" G9 ]' ^! Z( ^
在电作动筒内,用以在作动简到达打开或关闭位置
3 L. Q' q2 C& w5 b7 ^& k" J: G时,切断电源的机械式操作的部件。
8 C0 Z& @8 g1 ?: o, i" C* M各种极限,* O0 C3 a' Q. X, t. u0 D
飞机飞行手册(AFM)中列出的性能限度和操作极限,
2 \# y$ S7 s3 \& @) v0 M如最大空速,最大高度,和重心的限制等。1 h$ I6 s( F( J% O
在航线维修中,可以在飞机上即时拆换的部件。
8 [# p0 X2 d( m. W* o$ r; M飞机管理控制系统的控制显示器上的电门,可控制草稿
5 \% U: I. E9 J0 }" v: E; S5 B& H1 ?栏和指定显示处信息的输人和输出。
# V: a8 z$ W2 F' Vlight either turns on or off as the switch is% i0 u- D8 P. o! v8 J* P0 v, |
c& o* O) o) P' [% l7 I# R" O
LIMIT SWITCH, A mechanically operated component in
. I# g$ g. ^* u) B# D& Q4 h0 Ma5 C7 H. v, O4 P, ^
th
% Z$ U, p) w3 a" tc M- R9 b3 T; p, T5 e0 l! ~
L$ u9 r6 N' e5 _8 X, ?- y! x* g! J+ @
li
7 e7 c- X9 {4 t$ ^8 ~- e7 `" nm. O0 a( E. X o" ]& H( w
g8 v9 X7 N8 x3 G
LINE REPLACEABLE UNIT, A unit which can be readil
8 d5 S2 s- \7 u4 r ?7 v* t0 c' Gchanged on an air5 |: i' f/ R2 M- X0 [
o
M0 a2 G" a1 ]' H. hLINE SELECT KEYS, Switches on the FMCS c* a, U/ Y4 ~6 }, q+ J* Y
照明板,
( Q# v" ]) O8 l3 f8 g) y( M仪表板的一个部件,用以照亮仪表板上的文字。0 h: N. U3 |# v5 {4 ]
灯
* i% \9 Y! i+ }2 r: ~, M9 O带灯的电门。
/ C, T8 R6 X" f1 L; m极限电门,9 \( N8 z* ]! K' C& d9 _# ]; F& D
航线可换件,
w# O `3 H, |8 z$ A行选键,
. X& K! c z: _英汉对照民用航空词典B OEING5 {% G' k. H" p$ w5 X) d: ^5 \; B
TECHNICAL DICTIONARY 93
0 u3 b- C- {. n" ~" hLINEAR VARIABLE DIFFERENTIAL TRANSFORMER,
) R' p, L8 h- N/ T. insformer with a linear response.
/ _1 R: C# u) ]4 fNAV, SEE - LATERAL NAVIGATION2 Z8 ?2 F! X9 O
OAD AND TRIM SHEET, A form containing tables and
! k5 d$ n* S; @ z% d0 k8 P) M6 T0 q4 M! |harts to account for the weight and balance effect of all
1 t. ? `9 s2 a: v' e3 Tpe of an
. H5 Y6 @ Z/ p" e1 c# |( _S approach, normally located at or near the point of
7 P* F* g# A4 t% M- c: ~& aecision height.
% a! H4 a6 Y# Ber, l6 G: \( p0 i) ~& K5 W
eacon at or near the point of glide slope intercept of an
^5 D8 S8 o% N; K1 bS approach.4 `% a/ K% `" Z
ich provides
9 `% b, s8 |0 s+ ]lateral course guidance to the runway.
]; y ?' A* F7 a5 g# J' j差动变压器,
' u9 c3 M7 b' T2 V; ]3 P平导航,
5 ~# Y! I: [. n5 @- M0 |1 qvigation
2 c; r- f* a3 T7 _2 @2 |A differential tra
# F M! r. y' X. r, `& iLINK, A short connecting rod for transmitting motion.: \( V. m4 i+ i8 M8 r
L" ] f; f7 a* H+ g+ P
L
% Q7 }* x U1 h0 hc# k5 A+ S! a x8 l$ R( l
items and fuel loaded before each flight.
/ M5 X! t0 r$ {- G: z7 VLOAD FACTOR, The ratio of the lift being produced by }9 r0 D. t7 O" D
the wings to the weight of the aircraft.5 e k$ |8 G" N; ]9 [8 r- R" V
LOCATOR MIDDLE MARKER (LMM, MM), A marker
& _( S- L1 q, A( V- V" \- tbeacon that defines a point along the glide slo
& L0 B" g i# F8 a6 I* f: X5 jIL
! K8 d. E4 z) e/ x) g0 m' z" nd. {3 Y5 `& a# h. ?
LOCATOR OUTER MARKER (LOM, OM), A mark
; [5 M, M* w& Y# y4 _' M1 E/ c5 Xb
- F5 j" T* Z* n, H0 oIL
; r/ A2 A$ X, z2 O* }+ C$ zLOCALIZER, The component of an ILS wh" q; S$ \8 s4 n+ W% I u
线性可变
' h( p9 [5 ~) k# h. [具有线性反应的差动变压器。
* S% e0 g, u3 Q* B; I连杆,, [) N: O; ~+ N9 z: i
连接在两个部件之间,用以传递运动的短棒。
3 x. K3 \5 C: D水
% r# W3 `2 x3 e见Lateral Na ." S1 g$ k$ h0 C8 r8 P0 T
重和平衡表,
! H$ t( r; _( w- Z2 a9 t有着显示每个航班前飞机的各项业载和所加燃油对重0 }& V8 ]- A4 h0 p* T, K. D& j
衡影响的图表的一种表格。( O, k/ q* l4 y
,- l( j S7 h0 ?* q
附近的一点的指点标。- @- q6 I; B6 k! b- V- N0 s
近仪表着陆系统的下滑道截获点附近的指点! B0 h5 B6 a3 t0 @7 H2 _
。) X4 d" M4 ]' c8 `( k
仪表着陆系统中的一个部件。它能提供到跑道的水平航
5 ^8 q1 R+ ~9 _6 p% ~道引导。- U7 [, S& K9 M7 ^4 T* f4 t
载) c" {+ R/ @, t- e2 ~% w \
量和平- n: ]& N. H6 W3 x1 c! S' z( D0 y
装载系数
/ ^' |' E) V# o8 f, S机翼产生的升力和飞机重量的比值。
6 }+ R4 j4 f! u3 F; N) U中指点标,# @% L2 D& |0 J
用以指示仪表着陆系统进近的下滑道上通常相当于决& k1 ]/ {4 K" Y& ~
断高度或其4 w: O5 t* j7 X* f; T
远指点标,
2 Q6 p. j2 j- w位于或靠 h* ~+ |9 k' K Q- D
标# o* ]" e4 a ?
航向道,! u! O" R' B4 F7 U: A, q5 b u
英汉对照民用航空词典B OEING
$ d) H1 N( G" [/ q! s' ETECHNICAL DICTIONARY 948 q r! T% e- ]
LOCKBOLT, A steel fastener which prevents unwanted
* G1 b9 T! y" Q6 W. k, @rotation by using a collar instead of a nut.# f2 @- K6 K) n. t0 K1 y" P# Y
OGIC, A representation of complicated electrical and0 e |; x, K3 p7 o0 F: }
lectronic circuits by simple symbols called logic$ D5 e7 C4 F" p$ y
ymbols.
: U0 r$ @$ N- {8 d& MOGIC DIAGRAM, A diagram that uses logic gates to% [ U0 O- G" L4 I8 R2 V
present the function of a control circuit.
2 k- S' I1 ^$ m* x' `6 zOGIC GATE, A device or circuit which has no output2 f' h+ N+ S5 C# i7 M! f
ntil it is triggered into operation by an input signal. A$ \- J- O, ^% V
gic gate is an AND, OR, NOT, NAND, NOR, or
1 Q* C {& B, |LOGO LIGHT, A spot or flood type light mounted on
1 d$ C1 ~* X$ P* K1 }% B% U- ]aircraft structure and directed toward an airline LOGO or) \' a! X' {$ k3 `, O
other message on the fuselage or tail surface; for
1 [8 y' r6 |: Y/ w+ zvisibility during hours of darkness.
. o# }7 t" r! I,! @) j% \' g4 a
钢紧固件。! x) r8 a: s( @" Q
逻辑线路,
s; q( ?0 h/ W. n* s用简单的逻辑符号来代表复杂的电气电路和电子电路。
8 j2 o. ^7 U( |9 X逻辑电路示意图," }0 \) y' @$ M: u
一个用逻辑门来示意控制线路功能的图。
! Y' C5 `- G9 y0 Q. X: r3 i7 K逻辑门,
& s4 t5 F* V4 F& }只有当输人端有输人信号触发时,才有输出的一种元件
5 q! o u3 j1 b- W! q& |或电路。逻辑门分为:与门、或门、非门、与非门、或非
: p+ Y& M: z$ i+ _6 [门、和异或门。4 G2 o# I- g/ O- ~# J4 N
标志灯,7 J/ h6 v; x9 q3 ` j7 s
在飞机结构上装置的聚光灯或泛光灯。用于直接照在机
7 l7 s/ }) }! V' i& J1 G9 M, m身或机尾上的航空公司徽标或其他标志上,在夜航时照亮
8 j: m( Q; V# ?9 R这些标志。2 [5 W s: E( y
L1 Z5 D' [4 l5 S; ?( K' b
e
# D( ^* n+ d! x9 X6 V, ]% ms
: p! d3 u4 Z) q6 s& S( ZL( p, F3 c/ l3 o" Y
re( s' \$ ^4 ^0 v6 }$ h( E& h
L* S [, T$ M# D1 D; @" b& {, l
u: A( e- [. I+ c0 J0 {5 F
lo
9 v" i2 [2 ~6 o) y: e; B6 u5 u0 Rexclusive OR.4 I3 B6 O' d# |0 O: [& N
保险螺栓( Y# ]5 q) ~9 Q" C( X! _4 j7 d
用环圈代替螺帽以防止不必要的转动的
& i( g0 e/ E, @# P" M- K8 u; ?( {英汉对照民用航空词典B OEING
- K9 ]0 J) T$ p' oTECHNICAL DICTIONARY 958 [0 Q. O' \3 x$ t% g6 J Z+ B
LONGERON, A structural component in the horizon
3 r+ b& T- m* n' [" {direction of the fuselage or nacelle.
2 r j4 L7 S$ [4 {3 ]' btal
5 v- y6 u* w5 G* iRUISE (LRC), Cruise speed that is/ q" S% g) q; a9 S
ssociated with fuel conservation, producing fuel y. I! K% j/ C% u! X6 ]# \
ileage one percent less than the maximum fuel
* R0 ]0 F0 `. cileage available.
9 X+ p. S9 O" S& WONGITUDINAL AXIS, An axis passing through the
* m7 z7 Z& r) D- x* virplane's center of gravity, from front to rear.
6 ^2 w2 \3 i6 k ^0 L- h& s/ _not
1 i) C' [/ A4 z8 I- V3 pOUVER, An opening with slots allowing the passage of* \! P% Y# G; }7 P
远程巡航速度,9 J. }: N' @' _$ \7 p
一个与节省燃油有关的巡速度。在此巡航速度下,每; o' F- ~ k+ m; s ~" T. A! c
一单位燃油所能飞的哩程,最大的燃油量航程小百分之
! Z; C# c5 ?1 f; E9 }- A一。
# J+ I. o, q# n) b7 P纵轴,
2 l! u7 ?5 `2 i! `$ y$ L$ s8 X8 c由机头至机尾贯穿机身重心的轴。6 f! x5 f/ |: Y" \: g' {$ x+ y; w
叶窗,3 u2 M d: o: }% J( w
有多条缝的开口。
4 Z) R- w8 g: V) T7 d6 S! u2 bLONG RANGE C
# s% f5 w& y! M! I8 W( ma- p% c2 I7 f. ^0 l3 J
m$ m( d; z. r( ]9 z
m
. H' Y1 i" t5 K4 T/ R* YL: ` T* a8 X& u
a
5 i7 p$ J" b2 Z* B9 I# I$ k5 ]% hLOST MOTION DEVICE, A mechanism which does
7 F, J* M5 v( |operate a component following initial movement of! N, _8 J7 G* _; k, p d
control input.
0 d( T6 h6 @* i- ]7 A! dL
8 @& T$ t) l* m0 G: r, Vair.. o+ }3 u. h0 S& O
大梁,) i, b8 x( x, W4 b) d$ ^6 H- N- q
机身或短舱上水平方向的结构部件。
+ n/ N. V2 D; ` I V0 E, Y航6 G6 T5 {3 U' \( w$ z0 M
比% M' k& ]: F) B' z
空回装置,
2 I# Z% y* f0 t+ }在控制输人初始动作后,即不再操作部件的机制。用于( P$ p! Q8 I9 U5 A
飞行操纵系统内,以防飞机指令互相牵制。
6 X/ e N3 Q3 |1 e3 q- e: K百
# u! @/ @# @, m$ r: U9 Y/ q让空气流通的4 ~/ q4 d% N6 O+ r
英汉对照民用航空词典B OEING, L- U$ P" q0 Q# e
TECHNICAL DICTIONARY 969 X2 F% A# ~% U% r2 Y
LOW RANGE RADIO ALTIMETER, A system that
0 C8 [+ G0 i- N( cmeasures the vertical distance from the airplane to the
2 h' P" s+ X& P3 q1 \rrain.3 r' i" s% D( c( A/ B
RC, Stands for Long Range Cruise speed. Represents
. Y$ a# B" o* z( m' Q( re typical cruise speed for a given jet airplane; usually
4 ~& H! G( o' e, [- rxpressed as a Mach number.8 h' ^% T3 n; m! J4 k/ ?9 c
RRA, SEE - LOW RANGE RADIO ALTIMETER! [$ j( Q* t9 M [% v' U4 Y
RU, SEE - LINE REPLACEABLE UNIT( J/ v" X; T$ W/ ^. c. s. k, H3 @
uce friction
* c9 |6 c# {* }5 J: ietween moving parts. It can be a natural or an artificial% L E) Y' E8 C: ?- d0 t: {
aterial.( N) [! t: ~8 h" @1 {
AC, SEE - MEAN AERODYNAMIC CHORD. N: F# X M" [2 b
ft's true( D8 n# C9 u# E) e$ f
airspeed to the speed of sound at that point./ |- B# Y( r3 X! W T# F( K1 |) {& {
的系统。4 `$ A/ N s" @" K* ]! S* `' Q# X
远程巡航速度的缩写。代表喷气式飞机常见的巡航速) }0 o% }" b5 @( I
,通常以马赫数方式表示。: w6 e1 ?+ i- z! F4 l0 t. n
空无线电高度表,
; O9 B3 o# t5 V. `) x8 t1 BRadio Altimeter. ^3 L& o) c& x6 V& E
te
( Y6 s4 T; R# K, h# oL( J% f" b9 x* |5 g g `# h- e
th, b. w- {' i& D. D( \
e
9 ^1 I7 y* o( `+ m3 ^L' o& Z+ S, y: M0 @& s
L
8 h5 }( S) w, F! w2 O ZLUBRICANT, A substance used to red# p: z/ p: W5 K# @! |2 `
b, _" f$ s8 t, c$ D+ N
m3 n; X' k8 K7 Y B
LVDT, SEE - LINEAR VARIABLE DIFFERENTIAL
- f) s/ E" ^! A) rTRANSFORMER
# y+ k1 F4 X9 A4 g% ^. cM
/ W+ m! {" g6 vM/ F; ^" W. d, D# ]" O% y! u4 i
MACH NUMBER, The ratio of the aircra
* L: j- x I- S4 A2 z" t低空无线电高度表,
1 `+ x' s0 W! ?一种测量飞机至地形的垂直距离
9 s6 y/ O* N* Y0 V, H4 a, M3 x远程巡航速度,6 T. N2 F: z7 |
度! K! ^5 V0 Z( W$ A( }, F* d
低
) ^+ c0 f$ q1 Y! E见Low Range .% r2 U# ^4 c# V$ O& @4 x/ ?0 j I: a
线可换件,& V# P1 w. y5 w" v
见Line Replaceable Unit5 j% ]3 G) s5 a/ T. c! [9 W
航
Q! E5 T. h+ _ Y5 r6 A.
, @; l, G6 z0 o6 Q4 o9 g% z& [用于减轻运动物体之间产生的磨擦的物质。它可以是天7 E; T7 M2 x/ `+ |4 T! n( ?
的或人工制造的原料。
7 O; N$ w6 h2 q: T见Linear Variable Differential Transformer
' h1 V. Y# Q7 Z( |( H4 _1 ~- T: x6 L润滑剂,
8 s( r5 W' Z0 c/ c/ h! T9 L& M# h+ k然9 R; ^- Q9 @% N* x
线性可变差动变压器,6 e9 p. ?% ]( n1 r0 h4 j8 {
.. t3 s3 r9 [9 d
均气动弦,
3 P, E$ N9 D& @见Mean Aerodynamic Chord( r1 n; s# T; V: S' g
平 q) W( g: [& A9 U" ?
.
6 H% E$ _+ H& L空速与该处音速之比。
( ~. V! u4 I& C) B4 ~0 E. G$ o马赫数,) Q( U, [/ V% y* Z) `6 X
飞机真5 b. X/ p# E9 v% M# X" Q, q
英汉对照民用航空词典B OEING! }8 z* v4 x0 H1 m3 a& z6 V
TECHNICAL DICTIONARY 97
) C! { M/ W; @# D& e5 u) yMACH TRIM, Correction to airplane attitude (nose up)
1 a" o4 ~, |% j, r' E# ?% T' Tduring flight at high speed by using the horizontal/ k( i* A- R0 b1 J2 B' r1 ?
tabilizer.
5 o8 H- a/ R" D+ ]" dAGNETIC HEADING, The heading of the airplane
" B: M& f1 z) l( w, J& ]8 p9 Jlative to magnetic north.% k# o& A, s5 s7 f4 @4 w
AGNETIC VARIATION (1), The difference between
5 X8 m; T5 Q2 W) p, _9 Eagnetic and true north.
+ t( G+ D. d2 ~' U2 p: Y/ `- rnorth.6 T" K0 _" _' I) B
here is a continuous small change of direction
/ w7 D3 C5 Q$ P' n6 Rf lines of magnetic force over the surface of the earth ,. Q$ _4 ^ R3 p5 n4 Q9 u) w' o/ B
agnetic variation at most locations is not constant over
; Z" F' Y7 `4 I( xng periods of time. Lines of equal magnetic variation5 p$ @4 U8 @3 o& J( Y
e. (see3 g- J5 O: L4 N6 y
tation Declination
/ X$ N6 o1 {* m7 U# T; P$ ps
2 O5 M0 _# q4 q: J, A4 aM m7 [* f/ S/ _& Z5 v; y
re& M$ ?8 o3 m* W8 e6 y
M" f/ w- m a, d" |9 _; x
m
: U, |) j" i- `; jMAGNETIC VARIATION (2), The orientation of a& h: |0 D: g& D" R( q
horizontal magnetic compass with respect to true
$ q5 u& M+ n- | T. w/ B5 jBecause t' T- p. B! T; J. B0 v% h7 U
o9 ~ n* `) x$ `2 \7 {* H
m
* K. q/ m( k# O# O& olo
! Y) S n S5 J4 S& x: O4 X2 }(isogonics lines) are updated on Jeppesen charts every- z8 l# f* |- N2 q/ D9 N
five years in accord with worldwide practic
6 {8 j3 K6 k; y+ M$ ?S ).9 f/ u7 p3 q$ X$ U; F4 r: a
MAIN ENGINE CONTROL, A component on the engine
6 ?; @, n5 {; C3 @: o, C V O) G. iration.6 ]. s* ^ Q: |3 \- z; V" u( }
MAIN GEAR, The main wheels with the attachments for
" f$ A+ t' W: g( ^; `, nsupporting the airplane on the ground.% o: b) \7 c7 e$ d: _
MAINTENANCE, Work accomplished in support of the
! o0 D! A) L! x, Y* d) |structure and systems of an aircraft. It includes,
2 L/ T& _0 [1 O& Minspection, overhaul, repair, preservation and the2 {: o9 l; X! E( O. u4 i, [) G
replacement of parts.
6 o a% I9 [: e0 h马赫配平,
& }9 x+ N, z9 v用水平安定面对高速飞行中的飞机的俯仰姿态所做的1 U# d: d) E! B3 [8 i4 c
调整(机头朝上)。, g9 ^; H0 y4 Z4 E ]4 ~6 C" x( E: s, G
磁航向,
' ~5 T8 x& a) n# J! ?2 e: o+ J+ R相对于磁北的飞机航向。* z# l, j7 X5 |( e) \
磁差(1),
1 i: B5 r- d$ F% O真北与磁北的差别。7 p/ ~3 l* a$ K% Y( C# k
断的微量改变,磁偏角在长时间内多数是不一致的。每- v" @9 V) z3 D( L) ~4 z
五年Jeppesen手册会按照国际惯例校正等磁偏角线(等
9 X9 z: D# r+ W3 w差线)。(见基点偏差)
6 I2 e# U# `( J l主起落架,5 P7 Y: Y6 G6 p' Y# T+ h) a% \
用以在地面支撑飞机的主轮及其附件。
: o; J0 H! I5 S! T6 s维修,
% d$ K/ }' u; K) u# \, ^在保障飞机系统和结构时所做的工作。包括检查,大修,, M) Z' J* \; x: ?4 b
修理,保养和部件更换。
- A. a# I& F7 N' o. { tfor controlling fuel flow for starting and engine ope
8 A2 J/ i4 H' h! ]/ M, o6 l磁差(2),8 w% F9 j0 c3 W& ^
相对于真北的水平磁罗盘定位。因为地面的磁力线在作/ ]/ ^ C: t8 `1 L; _: y7 f& k
不$ V' @) I7 @% i9 q3 h
磁
( N+ A) I7 s( _# j& I3 B主发动机控制器,2 x* ^0 Z! L4 G) }: a
发动机上为发动机起动和运转控制燃油流量的部件。
. q, u2 R. A" f$ @英汉对照民用航空词典B OEING. P: f& \/ y: B2 a4 |% Z
TECHNICAL DICTIONARY 98$ n& R6 q# ]8 |( R
MANEUVER CAPABILITY, The ability of the aircraft to
& v2 T3 R; d* }1 O! ?' qertain load factor.: |3 _/ O, G9 ]
MANEUVER MARGIN, The amount of residual
* l; w2 L/ g+ R. D% A. v4 K; oaneuver capability present before the onset of buffet.5 w" E& b, J3 G- H! V; f1 z
MANIFOLD, A duct or chamber with several inlets and0 v( Z4 a: F3 Z( u) d8 T
outlets for air or fluid distribution.: S) V. C) O) _; S
the: h; U( k S0 V7 f* \( U: `/ B5 Z
low of
# S J! K; W& H1 ?* s8 f0 M) ke flight compartment. On specific
7 M4 `0 s7 O3 I7 y# ~ccasions it will provide conditioned air.
- H% ]) G# ^! aomponent by hand.
' ]# V$ N! t7 Q; aMANUALS, Books with instructions for proper$ c" b; x( G; H7 r) w' n) E
maintenance and operation of the airplane systems.
" [& x$ I4 e" l ZMANUFACTURED RIVET HEAD, The head of a rivet
3 b6 z6 V* a$ O; Xthat was preformed during its manufacture (see upset
& V- H! G ]; }1 Dperform certain maneuvers up to a c. c9 V6 t# n- p# }
m
3 ~5 _ N, b. W# X# BMANIFOLD INTERCONNECT VALVE, A valve in0 F& o/ p5 j* v: N% u
equipment cooling system for providing a normal f
" A& G- J5 {: c: Y7 D& S: W$ y4 Erecirculated air to th
3 }/ u. Z8 O1 r+ ko: u& e l6 \1 n$ @. g9 H
MANUAL OPERATION, Method of operating a
# G$ l3 Y% v( j. v! j; Zc
# {$ Z, d# R! H, j, _3 s4 ahead). e) }4 Q; l/ X2 [
MASS, The quantity of matter in a body. It gives the
8 w; }: b/ I0 @; [6 obody weight when it is exposed to gravity.8 k" ]. X! g" B2 c5 L
机动能力, f' P5 g3 m9 \; z# U9 B; k
飞机完成装载系数达到一特定值的机动动作的能力。
, @; S" `0 X& N, I4 _) i1 Z机动性余度,1 N7 o' X" h$ U
飞机在遭遇抖振之前,所剩的操纵能力的大小。
! a4 m1 I3 x! `总管,' F/ C. F4 ?3 _* b
用以空气或液体分布的多进口和多出口的管道或容器。
2 k! y! `1 ^ z$ M7 d6 k1 f8 O总管联接活门, D- m+ g& T5 f& y, v
设备冷却系统内的活门。用于向机舱提供正常再循环空
/ ~- ~4 _+ ~% {$ ^5 F8 B气。在特殊情况下会供给空调空气。! M6 l) B( H% J4 d& c. X
人工操作,; T, R9 G8 C' x9 C6 E
手工操纵部件的方法。
! f& g* F# a8 r- s" |! X1 Q明书。
7 m9 M+ Q3 \# b6 T5 `铆钉头,
5 D+ R) M! V( a' G在铆钉制造时已定形的铆钉头。(见膨径头)。# F, G) M2 M+ y1 S: \. O
质量,5 b& T5 g0 }0 D6 k4 h$ F
一件物体的物质数量。当该物体受到地球引力时质量产 j+ l, Z- e) x, \: V
生重量。) i; j; z% }5 s
手册,
; U4 [# m- Y" ^; j5 R: p为能正确地维护和操作飞机系统而编写的说+ C& W! ~! c* q0 N$ v
机械制造的+ C, m! H( `, @' Y8 }
英汉对照民用航空词典B OEING# d' C- d1 e) {: H
TECHNICAL DICTIONARY 99
8 ]. x! {7 P* |' v" Q7 `2 ]4 yMASS MEMORY, A memory that can store large
2 {3 k# Z" F2 o" V7 |: tamounts of information and hold that information# i( [ ^: {9 i$ s9 Q
permanently.! i) F$ v; i" }: T
AX CLIMB THRUST (MCT), Maximum engine thrust# w7 t: j# Y' D3 e
ximum engine: B0 k, X. ?" S* x* {: D: }
rust to be used continuously when one engine is+ F$ z) X# P; b$ X0 l
operative.
; U) r$ c' I' ~6 P5 qEOFF THRUST, Maximum engine thrust to be6 m R5 _" U K3 [
used during takeoff., U$ }% `- F0 P. C% y+ U
FF WEIGHT, The maximum take off7 H* O; g- P9 |2 \& k% ]/ i
weight as permitted structural limits or performance# D" Q; s& O- t4 f4 `( M
limits, whichever is lower.
# W# D8 F$ d/ g! }: @RANGE CRUISE (MRC), Cruise speed9 \* M# e9 d$ m, g; f K. F7 p
ance
( z; r- K, q* N8 }* H4 vto locate
9 \% o, {: c1 n/ L0 Kthe Center of Gravity.
% V4 F3 j, }7 o; G+ n9 ~4 ?& Y主控台,1 ^4 i0 M& I$ J$ {7 Q
控制系统操作方式的装置或系统。
" ?" k9 J( d/ ]* D% k大爬升推力(MCT),
: Y' b4 }2 Q# S! p1 [飞机爬升期间所能用的最大发动机推力。
4 B- Q9 m: O, r' c; D; S) {MCT),
. }% i2 C8 C- I7 F9 z. }2 f当一台发动机不工作时,可以连续不断地使用的最大发
2 z- K2 L- Z5 L8 H$ R- f7 a动机推力。9 L& `' m7 k, s7 H$ K1 m5 Y# D/ s
起飞期间所能用的最大发动机推力。
7 Y/ Y4 M' M: c( G2 F- K结构极限与性能极限两者中的小者许可的最大起飞重+ S2 I5 `& @* X$ L, Y
。; P5 x" e. C# N9 K
大航程巡航速度,
% I# }. ` i1 n最大的巡航速度。; B" e: O, S( o, C( L% y& E
平均气动弦,
1 i+ r( o" m# Q# s确定重心位置的基准7 r% {% y5 y/ k: |( J$ g0 Z/ P
距离。# }) q: w/ W) V/ g9 |7 f
MASTER, The device or system which controls the- h3 F4 L8 U j S( \: p4 N
system mode of operation.% P6 K% c2 v9 {/ Z1 g5 p. c5 v
M0 L# c, y, o( n9 x) C5 v
to be used during climb.& `" P+ y: }5 i: w0 F+ \# T7 g+ f
MAX CONTINUOUS THRUST (MCT), Ma- }5 I) f6 J6 Y# M8 i* I a9 T+ N; B
th
" T, B* {# ]/ A* M5 ^; qin
0 a x$ [) s. [3 I0 {$ f6 M& dMAX TAK
$ l6 ?$ j) I8 \3 F( CMAXIMUM TAKE-O' i! P7 \/ p, N, U8 V* ?, Y
MAXIMUM
7 v7 T+ Y) `, X- @6 h, x' aproducing the greatest amount of range.# y1 @1 `# J. z
MEAN AERODYNAMIC CHORD, Reference dist! }& m1 G, d6 G& U3 v( X
located at a fixed position on the aircraft used& u; m& D- D, Y
大容量存储器,7 G/ e3 k$ @- Q3 ?& C
可以储存并能永久保留大量信息的存储器。4 ]5 ? w' g/ x# d4 G7 x
最
0 p/ s% s$ d- y4 \; o5 K最大连续推力(
7 E; ^5 y$ t6 S9 G1 I4 ~: S% M最大起飞推力,
+ ^5 J6 F7 ~2 s) L! t最大起飞重量,4 `- s2 v7 }8 r7 Y, e- h. I5 e
量6 \8 c" {* P2 {) X/ Q8 f: Z
最! k, i1 U' b* L6 f$ r" i
能使飞机航程
9 n( m/ _2 B1 n5 W0 t位于飞机上一个固定位置,可用来% u6 U; K! a! ?9 |; i- n% L
英汉对照民用航空词典B OEING
. b3 e, }- h: c+ e' w, d& xTECHNICAL DICTIONARY 100
" g' V5 ^3 B' z7 ^1 PMEC (NO. 1), SEE - MAIN ENGINE CONTROL7 q' B$ l1 ?* T% v
MEC (NO. 2), SEE - MAIN EQUIPMENT CENTER! r5 d1 ~7 J- L$ F/ ]- x1 y& l
EL, SEE - MINIMUM EQUIPMENT LIST: Q! Y: U! M7 J9 o- [" I
tem the memory is where
) _: ?2 b. V6 D& f: B8 A. [" K+ e8 kformation is stored.
$ y% ^# r. |% W: }" @) ]METER, Any mechanical or electrical device that is/ V" o" c% r: I
air or0 o1 ^- C& _) B9 J0 @
point along the glide slope of an ILS approach. It is/ U' C; l q' }
normally located at or near the point of decision height.
' b, q1 q* T3 q7 n8 a' Z: ^,- S4 W, J4 G: I+ t% d/ Y$ l
见Main Engine Control P) H) t7 C& i! ^% r% C
M
* X1 @5 I' O: q/ [5 L6 Z" tMEMORY, In a digital sys7 o0 z4 d/ w2 C' S$ v8 e
in, l; F% U0 k( A9 a, ]
used to record, indicate, measure or sense a specific! s/ ~5 }$ o- b0 w r
portion of an operation.
6 w% T# U' c4 G- gMETERING VALVE, A valve for controlling flow of
4 S3 P3 p/ Y# P) ~7 zfluid.
. S( o2 x# ]9 H$ V2 R0 QMICRON, A measurement of filter effectiveness, one* h& c' y; m0 L/ F- C; I; I' e
micron equals one millionth (.000001) of a meter.6 h. g) M/ S2 V4 {' f& A4 U
MIDDLE MARKER, A marker beacon that defines a
. V! m% ^5 |$ ~ H1 g% v' a |发动机主控制
- ?- r& K1 ?; U t" B.1 C# ^$ S$ V* _4 {9 u' D0 ^; C8 D5 C6 R) S
设备中心
3 n2 {7 j4 n+ A1 C7 B* p' n见Main Equipment Center
" b1 B3 m( L4 k2 ]+ T总
% E$ ]9 a6 G, a8 F6 X6 W H.1 a; p3 E! P8 u; ~( n
低设备清单,
5 }: F3 B! e3 B2 A6 X) H Y见Minimum Equipment List
" x) k8 O" z. T* k最
7 @0 Y/ D' f; g2 V" n; u5 O.8 q: f, ~0 H5 {. C0 P
在数字系统中储存信息的地方。
8 F9 u; C* l! I9 N: Y* |0 _6 P+ c计量表,
2 k- ~3 v; Y- G, T9 G5 e# y用于记录,指示,测量,或感受一操作过程的一个特殊% _# U: I5 c3 h, U# [+ P4 Z
部份的任何一种机械或电子装置。
( K8 I( d: }4 }: B- J! Z量活门,# @& P! _6 N# A# B" A2 O
用来控制空气或液体流量的活门。
& o; j5 W. ?. y8 c5 C微米,) P7 u" D8 _+ J r" @! r
过滤器效率的计算单位。一微米等于百万分之一米。4 T) Y% n0 P9 g) l1 a0 [! w; q
在用仪表着陆系统着陆时,用来确定下滑道上一点的指
% f4 m, u b4 Q! T2 A6 w点信标。它一般位于或靠近决断高度。
6 x" w& o! E" a& P. t( w存储器;
: c+ x1 K4 F/ h计3 d1 [# }3 m9 }* q. |0 ~; R
中指点标,; }: |4 A3 i) N' Y. |7 \
英汉对照民用航空词典B OEING
- p2 I0 ^$ P6 K! J! F) ITECHNICAL DICTIONARY 1013 H# o3 m( U4 G3 P! Z! \/ k
MICRO SWITCH, A miniature mechanical device that* m5 U" y1 L1 x
completes or breaks the current path.
' _$ o! f+ o% r" U0 e% [3 G2 r.
% C( M/ ]9 m3 y! z7 @' t, {MIL, One thousandth (.001) of an inch.0 Z" r {( N/ t1 Y5 K2 c$ r
ILLIBARS, A unit of barometric pressure equal to
% U/ z( ]/ h G& O" @% x. kapproximately 0.75 millimeters of mercury.
" }. y9 Z9 u Q5 L7 d# ?The lowest1 ?' D$ Q; [' s5 M9 l
ltitude to which a descent is authorized for a
% Y# ?# ?! S& Q0 E: o6 Sonprecision approach.- c9 C& u* d9 `8 {6 \
INIMUM ENROUTE ALTITUDE (MEA), The lowest8 f# d- [; y! e/ f: m& M
ublished altitude between radio fixes that meets) a3 s* K8 v; J
bstacle clearance requirements between those fixes
& w/ Z( b, r. x8 x. I$ l: Y T5 @& _and in many countries assures acceptable navigational
" a! a% h5 w: h* gsignal coverage.
B( B" G% [, y' o* |! } B Y2 koperation of the airplane with certain systems or8 j2 w$ [" r8 H* X
subsystems inoperative.$ F6 [% e2 v# ]6 e
approach
: D- L8 W$ j8 I4 [8 lcannot be completed to a landing and results in a Go-% o7 N/ _+ v# I$ T
Around.
3 E s- E2 _& I6 P" x一个能形成或切断电流通路的特小型机械设备。6 r* {( T* i. k2 G) ~4 ]* C
话筒,
- j! I7 T+ @# v* b- [话筒一字的缩写。
9 s0 n% R& p9 r耳,
4 @+ L. o3 Q6 n一英寸。
8 G. }5 t. l ?& ?" ~+ a8 G毫巴," E) `6 f. K2 E5 r
一个度量气压的单位,一毫巴约相当于0.75毫米汞柱。
0 X& \1 o0 u3 t$ ~4 G6 r低下降高度(MDA),% p9 p, i# _6 ?
飞机作非精密进近时所准许下降的最低高度。: s- ?9 E! c3 N) K: D' P) `* v* Y
低航路高度(MEA)," `" W1 X/ ~! {' x" E; _) `
在导航用无线电定位点之间,符合越障要求的已公布1 ]9 [: u& m0 }2 N
的最低高度。在许多国家,最低航路高度保障了合格导航6 o3 @+ G6 s' x/ L! ~
信号的接收范围。
* V1 |6 L9 w" v5 y0 `+ J0 Z最低设备清单,, m6 A: ~) J. [! J D
何/ X! m. D* x+ |6 q% d4 c& [3 n
作飞机的文件。
& f4 H' z% y$ u; c$ p1 R复飞(MA or GA),
6 T: P) W6 x( K$ P# o$ o! k c飞行员因未能完成仪表进近而导致复飞所采取的一个& C0 o& v5 _6 y
机动动作。
* `4 ?1 o' ] C6 L% N7 X1 }MIKE OR MIC, A shortened form of microphone) g/ D! Y; T$ j* H+ x r* I
M
+ c& x* C* d# p/ j5 t0 IMINIMUM DESCENT ALTITUDE (MDA),1 J, L! [% r4 L5 n- K$ ]
a
9 N' `4 Z7 ]2 I1 a: en: ^& [% M7 U) r8 Y
M& \% ~8 g4 \) W# v9 t: s7 L) S2 M
p! c9 t- o- `- `3 c
o/ f- x3 N" W, H: c
MINIMUM EQUIPMENT LIST, Document prescribing" D* M- t$ a% t* a2 T
MISSED APPROACH (MA or GA), A maneuver. u I/ U3 x6 b) \5 ~& u' @: P& y
conducted by the pilot when an instrument. H5 O( I1 X2 U3 k1 s
微动电门,
# u# a4 h8 F: a) w密
D; ^/ S7 E4 v# K( G" Q8 i千分之
1 a/ [2 p1 @- {; F7 d最% a) D2 N2 ~7 e# f+ K
最
1 Z- s, O! k" k( Z+ g指定飞机在某些系统或子系统不工作的情况下,如5 u4 s6 J. f6 A; D6 i! @
操: e1 h7 P" A# B- c
英汉对照民用航空词典B OEING
& Q& G' f) w! @/ ?TECHNICAL DICTIONARY 102
' [: w4 }, q* f0 \. p8 p7 uMIX VALVE, A valve assembly with two or more0 _# G. x: U( [/ b0 l: r& m
individual valves used for airflow distribution in air4 K! c) d2 M5 d# O# p
stem.
7 k& @" T4 h: E* MMMO, The maximum Mach number at which the aircraft; M9 n, S2 y6 [/ P+ Q h+ K7 j
MODE, A specific operating state or condition; i.e.,
: q5 N8 s! H4 L: D& ?Autopilot mode, MAP mode, etc.
- U* _9 J* K4 U' Re, J$ T+ P. @! K
MODULE, A housing that contains related system
$ M/ d/ H& e& v5 z# E6 L1 g G& NMONOCOQUE, A type of construction in which the
- {4 ^$ M7 u3 nONOPOLE, A speed sensor that senses magnetic% H, O+ O" P4 z3 d0 }
pulses from a magnetic nut or gear teeth on a shaft.
: v9 d. v. I$ v# B, ~1 ahe controller." m1 Y, `) p$ K0 A
MOTOR OPERATED VALVE, A valve using an electric: X7 M! q6 w3 o/ ]1 J" o- a7 e
motor for opening, closing and modulation.. D5 a9 d% U" T+ g6 F
个以上单" l) o. u$ h) t1 b7 |6 y2 X! l& B
活门的活门组件。
% o5 J8 F5 X; J7 q; v飞机可使用的最大马赫数。, Z; m- ^! ~4 s5 X2 l" ~3 U6 F
式,MAP
0 {! {# P J9 v! J方式等等。
: J) t% `: N" z( p" z7 U7 u调制,9 u* a- l( o: Y/ V2 S( M" L
组合两个或两个以上的电子信号,使一个信号随其他信/ i9 V7 _0 D" S- U! N& |# \+ T/ X
号的变化而变化。6 _7 q% F" i4 ~- y' q/ H
组件,
7 p `8 V# Z. m1 E* ^8 p极,+ I7 k$ d# j) G
帽或齿轮轴上的磁脉冲数的速度, n3 N f `* M5 M
/分钟。
# f# a4 U0 P+ x# f用电马达来开、关和调制的活门。4 B W4 j5 \; @+ C
conditioning sy
% k- s2 K3 e: f; a5 dmay be operated.
V9 [+ U9 `0 \7 T6 y3 F. d' GMODULATION, Combining two or more electrical
' l0 }4 ?3 ?+ c1 `) T0 Isignals with the result that one signal is varied by th$ r$ E5 |7 S8 \7 p8 H
others.
; n/ j0 W' d9 P) M- O- {components.
& c7 l6 E @; Q, U+ l1 Jfuselage skin carries all the loads.: Z g! d/ p. n& i, ?, X/ z
M
+ M9 n- @8 p( L( ZThese pulses are interpreted as RPM by t
' b& t9 u' a+ C) Z混合活门,% e- D7 C) i$ P# o! }7 _
在空调系统内.用以气流分布的具有两个或两
[% w. e9 l3 r$ Q1 `5 F+ Z体
$ n, Y V+ u3 ?% dMMO,
# \8 `7 Y% V* E8 l( k1 \9 f. K方式,
! h8 a1 R' l$ u- u# |5 ~一个特定的工作状态或情况,如自动驾驶方3 K3 l) c5 F* A% h7 S
内装相关的系统部件的机体。
: a# P% D* b% f- p硬壳式,6 p. J2 Y4 m2 `" j, Y4 B
机身蒙皮承担所有载荷的结构形式。
' f$ s$ I1 q- p9 B; F! {+ v0 G0 b单
l( H' p, x, E+ {$ W一个能感应到磁螺# R1 B$ p% \8 k" p
感应器。这些脉冲可由控制器译成转; V- w' J/ k+ t- B: K
马达操作活门,
0 `" P0 c! o8 [1 J) P英汉对照民用航空词典B OEING
6 d# q1 u4 o' \TECHNICAL DICTIONARY 103$ ?7 k4 C& F9 Z' @
MSL ALTITUDE, Altitude expressed in feet measured
( b; C; C# @5 K" e$ m) q7 p5 Rom mean sea level.8 L' q* X" S D: p: D
reducing the noise of the airflow through the pneumatic
0 U- V* F+ _& Lduct.
& B! v+ K# h, t" ^7 W. OMULTIPLEXER, A device that allows two or more% X$ @! r7 k$ k) u6 S$ X* ]6 k
signals to be transmitted simultaneously on a single
" B: A& s4 O, `( |: _carrier wave, communications channel, or data bus.! v' p h2 x, e* G0 j
essure compressor rotor.
. b% F/ J& ]* R0 G; o6 d+ RN1 BLOOM, A change in engine N1 and thrust indicated: X& R4 Y5 u @* f" Q% C
N1 gages and detected by the autothrottle BITE2 d! {, x. {1 v, S: H
during throttle hold operation.7 C6 ^1 t: f( V, @* O
N2 , High pressure compressor rotor speed.1 C3 o; t/ h% g- g! ?9 R& m$ D; Y
ACELLE, A streamlined enclosure on the wing or
; \+ |/ B8 f7 I6 T! L面量起的高度。
+ I. E5 _7 [- y/ n, ]经气源管道所生的噪音
* t$ l5 q [: V) {. Z的装置。2 x( P$ {# S$ g3 {: {
多路传输器,
$ N) S. r9 v1 c$ U' p一个能让两个或两个以上的信号同时在一道传送波,一
3 Z) P% F0 T p条通讯线路,或一条资料数据总线上传递的设备。 Q+ k. Z3 R5 Z5 K9 f- t) h6 x3 T! i
N1转子转速,+ a4 X6 P% s. \( k( Q
发动机低压压气机转子的转速。4 w/ e, d( e, n# n z! V' t- n" r
N1激增,- v$ H9 T" Q1 M8 ]; X$ B
油门保持过程中,在N1表上出现的由自动油门自检探
1 P* h$ I5 @" N测到的发动机N1和推力的变化。
$ q& \! _* T% i: ^N2转子转速,7 ?. ?0 ]6 R0 A8 h6 p# Z+ ?
发动机高压压气机转子的转速。
! X+ l) I. R4 q0 s$ z4 b9 }短舱,
9 G: @+ {1 V! o, d6 ?1 E机翼或机身上为安装发动机而用的流线形壳体。- y, T5 L9 U+ c( o" }' v1 T
fr
( y+ W) e9 N/ LMUFFLER, A device in the pneumatic system for
5 L" x2 \/ c+ `# [' }N
7 H$ O$ F2 t; ~N1 , Speed of the low pr
l6 i% _ o0 b. Z$ |9 @on the6 |6 Z9 R1 i; z
N
/ ]! q8 n. L9 L$ Kfuselage for the engine.
. q+ F0 N$ c* Q( b* o' \" d平均海拔高度,
% B% s; |2 R- F0 t以英尺为单位,由平均海平& F$ F( G# Y6 u# ^7 q$ g' E
消音器,
! X# K1 X! v, S: n' C m' }0 T在气源系统内,用以减低空气流
+ z0 J! A. E/ I8 j+ q8 b5 v英汉对照民用航空词典B OEING
^+ c6 [8 f& u. S/ P" F" PTECHNICAL DICTIONARY 104
; E; K. J7 _/ P5 I2 ^5 oNAND GATE, An AND gate followed by an inverter to& o- [) k- s8 T0 y& c
form a binary circuit in which the output is logic 0 if all. G0 D8 V9 I. m/ \) Z5 b- X* v
puts are logic 1.( Q8 M0 r. Z/ e$ }
AUTICAL AIR MILES (NAM), The actual air distance
" k) _' j: Y5 j1 k4 `respect to a
3 B/ \0 q: L! c2 _tationary object.& v5 ?1 F2 }) ]( C" N0 t3 |# g
istance3 n; | z. q D% g; p& P' Y
travelled in relation to the ground expressed in nautical' o$ |( F9 ]0 X3 p9 C0 p
miles.
" ^5 [5 X6 H2 z; y: M+ K, Hnce equivalent to 6076.1 feet8 ?4 E6 p7 ^" H' Y6 _# `* b
r 1852 meters.8 T; `+ B$ [ m( P3 K
hical
* u: d/ `5 z6 u) w- w* @EGATIVE LOGIC, A form of logic in which the more$ I0 g# D# b* u% ]# i
negative level represents a logic 1.
4 c' C l, B5 @' [0 gEGATIVE RELIEF VALVE, A valve in the9 G( f' I0 h/ g6 E, j
e to be
9 ?. b2 j& E4 H5 [! X pabove airplane altitude (or cabin pressure to be below/ r5 T# e' }# i$ I! j) l- n% I2 T* N
ambient pressure).
i1 E E$ |% I% {: v, B有 ?( `: V6 l; z# Y
人为逻辑1时,输出为逻辑0。; [' o" ~- C% l3 Z/ m! J* i
海里(NAM),
& h X6 P+ C0 H" K3 y- k) P来表示的飞机在空中所飞过的实际空中飞行距. C. x" m& _! Y! s* t/ W6 E/ u
地面物体。6 K. \: x5 k; i2 L, L3 z! u
以海里来表示的飞机相对于地面所飞过的距离。% l, D d. N" A
里,3 g- P1 G0 w/ @5 c" f) s5 d# q, V
相当于6076英尺或1852米的距离单位。$ ] W" w: m0 n: H
导航,0 ]* W" r. j7 ]8 Z
反逻辑,
8 u7 Z$ ~3 g. o( i4 U* K正电压水平越是代表逻辑0,负电压水平则越是代表逻
: c' N: d/ Z5 m* X$ O- B. {释压活门,( x% l3 B7 g$ I! w4 G* W( h, ^
增压系统内,用来防止机舱高度超过飞机高度(或机舱# I. ^$ h+ j& M3 C* [0 j
压力低于外界大气压力)的活门。
! ^: f3 \' ]2 D* g Q8 Q2 Kin
, ?, R' g* z% J. s4 QN9 p% E" [2 M0 l' h% z# ~
flow expressed in nautical miles without- T: s4 T- R. @
s' B1 B5 M/ y7 ~4 w. v
NAUTICAL GROUND MILES (NGM), The d* q# i8 ]% z. ?* f' K: ~
NAUTICAL MILE, A dista
% f, @; A7 t0 L8 |o
9 [; U: F$ r5 \3 M SNAVIGATION, The art of determining the geograp: Y$ ~4 m, S6 y3 F: p4 T) D4 |
position and maintaining desired direction of an aircraft& P6 s1 X. G6 y' g, c
relative to the earth's surface.5 ~- Z2 i" h+ k1 J
N6 p' L V) k {0 u9 P2 ^
positive voltage level represents logic 0 and the more* x3 Z( `! f$ ~2 W4 r& Q
N
' @* O: U4 r8 _+ Kpressurization system for preventing cabin altitud
# f: t M8 k# k$ x$ {7 J1 K非与门,
# ~) Z% c5 T ?在与门后面紧跟着一个反向器的二进制电路,当所 ~/ {" W! ]8 f* A3 o
输
# p# G1 g; E4 E" D- O2 K* u Y e空4 ~: J B9 t; _0 O9 T
以海里
& W; n9 e' X% K/ A% G4 l离。空海里无需参考
- W0 s1 _: J* I, w; W0 [2 q地海里(NGM),4 A. M$ r$ F8 y
海
, t" g" M) l6 o' c+ s决定飞机的地理位置和保持飞机相对于地球表面所希
- a+ j+ R0 C4 d v8 x望的方向的技术。
3 G+ X" Y8 L( _) O辑1的一种逻辑形式。0 ^/ N9 r' K* j* H' p; b; P, b
负6 A# Y6 B# F) x5 l& Y$ m/ V
英汉对照民用航空词典B OEING
/ G! P+ q$ x# F8 ?TECHNICAL DICTIONARY 1050 V& W8 z& s* E1 _ w; ^9 v6 F
NEOPRENE, An oil and grease-resistant synthetic
5 p" W7 Q6 h/ s' G y& c" c& grubber. Used mostly for seals and self lock nuts, etc., W$ W/ c+ `( g A- q: c
EUTRAL SHIFT SENSOR, A sensor used for4 [) l: c+ P, p9 c( h! |
NET PERFORMANCE, Aircraft gross performance& f0 @2 }- W" [4 w
calculation4 @0 b! d! {, Q }7 ?5 T3 ?( n
purposes.
1 `+ i# _8 H& |1 \1 wNICKEL-CADMIUM BATTERY, An electrical device for
% w0 i$ i0 L$ f" Z- J4 C/ Nchanging stored chemical energy into direct current.
. T5 v$ x- }# [ses nickel hydroxide, cadmium hydroxide and' h# e7 ^4 K. s
otassium hydroxide.
$ c9 |/ c5 }, ANOBLE, A term used to explain the properties of some2 n7 D1 [/ Z0 a& k- f3 d; ]
lements that are chemically inert or inactive./ M4 G/ \! Z* }' @1 c
NOISE ABATEMENT PROCEDURE, A flight path and% v2 u2 z3 T+ N9 F3 n" @# p9 s! Z
limb profile designed to limit noise in the airport area.. G' J& {" F4 c" J- d# P; E
construction. (Nomex is a trade name.)3 l* a! d: t% ?5 s
in only
7 Q+ c# w3 A: F' m9 r0 sone direction.! K2 D% T" P8 E0 W. d& T7 m9 @
氯丁橡胶,; H! K- ^7 G$ q
一种耐油和油脂的合成橡胶。多用作密封装置或自锁螺
$ W l' D0 C7 Y, [9 p3 N ]帽,等。
. _ J) x0 O1 ^- r3 u立变换探测器,! c! G* t/ f7 N) N8 P$ u. G; x
用于探测升降舵和安定面配平状况的传感器。2 r! J5 [9 J6 s: ^8 V
性能,
: v* C' \9 b. W4 D7 E0 h" P机总性能减去由当地有关单位为了使性能计算3 t' B9 y! A8 f; E
较为保守所定的一个量后所得的性能。. K/ g) Z5 v' h. V0 |1 o
为直流电的电器元件。它使用氢氧化- {! F3 }% B. f' T* |1 ^1 Y
、氢氧化镉和氢氧化钾。
S% V- v6 R" e2 r- r0 x4 F- M1 j性,! G! n# E: G" p+ @. W$ X% C
用于解释有些元素不易起化学作用的特性的名词。
8 F3 b/ D% C! C0 V3 G4 M5 @* j低噪声程序,
0 ^1 z- x3 j5 ^0 |# O( H+ _一种为降低机场地区噪声而设计的飞行航迹和爬升剖
, Q# L* G+ u7 p。+ r1 }7 O/ A1 _2 T! P1 e
是一种类似纸的材料,用以制作蜂窝结构。(NOMEX
3 P- U+ R8 S; a8 i4 q' M( k商品名)。
: j# I8 z- E- E6 W% \+ N* r只允许向一个方向流动的活门。
H. o8 w3 W% o4 x" P9 g C4 f! eN
+ o% ^: A5 D; M8 b9 ^% M. Z* adetecting the elevator and stabilizer trim condition.
4 ], f& x8 a5 ? `7 m. L2 \: j- n4 pdegraded by an amount determined by the local
& h2 O/ H; }+ {, d- V7 |- ?governing agency for conservative4 a) U# G/ r( L# E5 X
U
" z8 j) q1 H! l+ g2 t4 W$ o9 Qp4 f, ^ w G+ o f8 W$ k2 L
e1 S" |, c1 P c# B( H5 ]$ h+ [5 ^4 Y1 U
c
+ k6 E1 Q3 u5 x$ INOMEX, Material similar to paper for honeycomb
8 o0 c. {$ U4 G! aNON-RETURN VALVE, A valve allowing flow- k& i' Q4 O6 D. h+ f% q& j4 a7 i0 \
中
- p6 X; E6 ~# X; Z6 m净
2 I9 q4 K P% Q以飞
9 R/ l! S V4 p2 \3 z; K镍镉电瓶, d! o, o9 A- d; K. Q- s# e
将储存的化学能变! Y- ]( p: }; G
镍% [: R1 I) O% l$ h0 h' E7 U
惰
8 l# m+ b N+ l8 q5 C) c; O降/ e" A3 L' Y4 P
面% _# N M2 A3 p' Y8 E
NOMEX,
0 \6 v2 z$ S" ]: R6 z/ i是3 A% o& g% k4 v* \! l# g! {- Y
单向活门," _4 B) f/ g: ]. e! m& N, {
英汉对照民用航空词典B OEING3 k+ t7 D! C( J8 {
TECHNICAL DICTIONARY 106
) H+ b2 ~; [" v' QNONDIRECTIONAL BEACON (NDB), A radio beacon
8 f O" I' q: n6 t' Ywhich transmits nondirectional signals whereby the pilot$ L) f4 k) `; ]& |- [) z# F' C
can use the ADF to determine his bearing to or from the3 P9 v: R4 I5 b6 m9 @
station.+ q4 r" a! t y ?
ONVOLATILE MEMORY, A type of memory which3 G. B) w- ^6 y0 W
does not lose its contents when power is removed.) `. @& G4 n* R( b, n9 K* I) I# d
rm4 R2 F; i% M5 ?& E
binary circuit in which the output is logic 0 if any of the$ `3 b" K8 `5 ]. c9 d$ e
inputs is logic 1." Y0 D {# p4 l7 s
NOSE CONE, A device on the front of the engine that R" i6 P% P3 N4 K- B/ Z
guides airflow to the primary airflow path of the engine.1 u. Y1 H% R3 K( H
the nacelle for air inlet to/ \+ H/ j: p$ X: Q% c- M
e engine.. D5 T1 w k6 h8 c& d' u: L
OSE DOME, Front section of the engine for& c4 H4 U7 b! F: y1 }: L
treamlining and directing airflow to the compressor.
+ d5 I, e/ k$ G. L9 y. U( ~( m),
( f* w" M3 i6 I l能够用自# a* O! ^$ _1 D
定向仪(ADF)确定他的背台或向台方位。
0 d, p q* H {+ }+ ^+ v9 n+ Z- v, I; K久性存储器,: j! X- P5 a5 R9 K9 U. H0 [, i
在失去动力或电力时不会失去记忆内容的存储器。- @8 w0 R- Y* t0 e S
在或门后面紧跟着一个反向器的二进制电路。当任何一4 o1 ]! x" _5 H3 b6 j0 i" E7 Q
输人为逻辑1时,输出为逻辑0。* O- ]" B: E0 o5 ^2 u& I
一个位于在发动机前端,用于引导气流通过发动机的主
( I& |4 Z2 m6 G; I, e6 M0 W气流通道的装置。$ S) T2 G1 U) Q# s
引导空气进人发动机的短舱前段。
. `' P! x" w6 H8 j1 t7 h4 x# f4 k% X部整流罩,
O% J& R: |0 n, C4 U" |用以整流并引导气流进人压气机的发动机前段。% x0 _% J6 [, p5 e# j+ \; j- R$ B
N
1 i: h9 D3 t1 }( WNOR GATE, An OR gate followed by an inverter to fo e7 b- u* ]" G( k8 U* r, X
a
' `6 S" K/ F/ z$ SNOSE COWL, Front section of m) V2 E3 s7 |- y5 B9 m; S+ V
th
& C8 H: Y, ] a4 gN, B# }- o3 F' ?5 q, E n
s4 k8 V& L7 w, y* \
无方向信标(NDB
# x( R$ T: g$ @) W发射无方向信号的无线电信标台。据此飞行员% T r+ x& y6 }0 a( ]
动
% N4 s J, g# Y. ~# c; j永
! s* y; Y5 j5 x) n/ a' h3 t$ g' x或非门,
/ _) V" }- O3 a; H" f0 `个
( ?& N& Q: P' i. E8 K: e进气整流锥,6 }+ e9 }4 H' f5 v! S
前整流罩,
, h1 V' P( T1 V* C6 N头, z$ ^3 }3 N' P) _1 }2 f7 S1 q& v
英汉对照民用航空词典B OEING- q! C) Y: w) s& y$ ^5 ]0 W
TECHNICAL DICTIONARY 107) z& y2 N J, a
NOSE GEAR, The front wheels with the attachments for% q* x# d( X9 {7 p1 e: z
NOT, A binary circuit with a single output that is always8 j2 R5 R3 c6 M0 }
opposite of the single input. Also called an inverter.& u. t) s# ^5 z- K% @: E. T
tion that has the shape of a "V".
6 N( L( A& Y$ W3 A# E* C: Yt.
" {+ `$ u- ^# `) o! n, F; OO-RING, A circular shaped rubber or synthetic material$ d) `$ n" s$ m# ?: `$ O E
sealing device for pneumatic and hydraulic systems.
6 a5 t. B* M0 ?; n6 t2 y) h2 MPERATURE
0 ^' j" O1 h2 S2 z& ^$ `) te7 |" n' q/ P/ [% Q' q8 g) `3 Z
in the path of flight.- y" @4 N) B" E8 e% r2 F" s: I4 I7 D
OBSTACLE CLEARANCE, The process of flying the
) ]/ M$ t* I# C% baircraft over all obstructions under the flight path.
( @ B1 w6 {& Y/ [0 ^2 ^Which obstructions are considered and the amount of% U4 P6 B" u5 n. ]
vertical altitude required above the obstructions are
) X9 C" F) P, Ndetermined by local regulatory agency.# l( Q R- |# ^9 Z0 |0 U& k/ A
非门,8 G3 s. u+ S9 N1 j
带有始终与单一输人相反的单一输出。也称作反向器。3 P1 J% T; I) {6 ]# J
一个“V”字形的缺口。
& b5 I4 @7 e, K( ]& W; _( H( h0 K喷嘴,8 R; J: I- P5 a' Z, h D+ C: d, d
形圈,
" g2 C( `" W8 ]1 k- x用于气源和液压系统,圆形的橡胶或合成材料制成的密- S0 K5 t8 E: v- o
封装置。 M- M+ f7 G9 v% j+ l, G* W5 f$ e N2 P
外界大气温度,
0 _. s$ [' x' Q/ A6 S, |& E见Outside Air Temperature
3 U5 u! Q( n' D. |( H) psupporting the airplane on the ground.5 u9 s( U. F$ b. ^7 z5 b5 _- |9 F
NOTCH, An inden
4 K' Z- L/ L- W% rNOZZLE, A shaped device for directing flow in a duc) A/ e1 h$ h" ~2 q3 u
O+ \& f4 g8 h" {6 d' p
OAT, SEE - OUTSIDE AIR TEM: n5 F( H' ?- l" u
OBSTACLE, An obstruction protruding into the airspac- A1 U' E, \- c+ k
前起落架," S, _" m; l/ R1 K8 P6 Y
用以在地面支撑飞机的前轮及其附件。6 j! F3 p. {6 y% l N9 f
凹槽,# Z, r% c& m2 {
引导管道内流动方向的具有特别形状的装置。
# P" d# K0 H: D0 JO
: o; H8 Z2 y6 d3 P. `% O, D" k) q" {.
+ q: \$ k. |$ i9 m% {% J越障,
O, j; E, y: S) w& z$ I道上所有障碍物的飞行过程。障碍物的选
; l. |+ L; O v择和飞机距离障碍物的高度要求由当地有关管理机构决- ~, }) d& Z5 G* ~0 N
定。
I. h% l i# }7 U/ p! [) |障碍物,0 u% k+ {( D( z3 w7 z' |) I
进人飞行航径上空域里的障碍物。& p! m& u# q5 H. Q
飞机飞越其航
+ n, z0 R: A& q, U' T; l1 e! c: a- M英汉对照民用航空词典B OEING
. C# o9 X* d# A! H$ DTECHNICAL DICTIONARY 108
* ]- B [+ t* @0 a/ S4 L9 NOEW, SEE - OPERATING EMPTY WEIGHT; V$ G6 t, a$ |( [8 D* C
FFSIDE, Opposite side.8 C( q( `* f- T: p$ ~9 P7 g
IL COOLER, A heat exchanger for cooling engine oil! q' J+ ^: p- M3 J# {4 E0 c' p
by fuel flow or airflow.( Z3 J0 R- k. r$ _" W; t! \
ATOR, A device used to separate unwanted
8 \( q& n; Y2 x c+ _, hir from engine oil returning to a sump or oil tank.
/ [1 B% c" x: k! @# Z# ?OIL STRAINER, Type of oil filter.
9 R4 [- H: {- ?6 ] mLEO STRUT, SEE - SHOCK STRUT# P9 j- A& o. L2 [3 N
NSIDE, Same side.
7 S, c) H( o0 a, F6 o- O# _ll weather navigation system.2 ]0 O' |4 j8 G% q: f0 O$ b I' T
ch is not
; O; ]9 s9 `# o4 a& ?& ocontinuous from power supply to ground due to a break# F! T. d/ J; @9 P! [! t
in the wiring or failure of a component.
6 l- k: C; U: M3 V! D1 a见Operating Empty Weight- w' T: y- Q( d9 R, {
O) f- K8 v. ]9 C; W+ [+ v
O8 \) a3 N" p" C2 N" v5 w8 P" u2 m1 E
OIL SEPAR
8 Z, {4 S( Q* @8 |# Z# ra( e$ w6 _0 j+ k$ V9 i2 ?
O
; n9 u- Z* a9 Y: `7 ?0 }+ f6 c4 JO: ?! f2 d7 O: z7 r9 i; G
OMEGA NAVIGATION SYSTEM (ONS), A worldwide,
7 @; V% \% A# Q$ J2 }" W; h4 }a
+ w' i6 Z; l7 N N- u0 @& ?OPEN CIRCUIT, An electrical circuit whi6 _! ]* ~# P v0 T4 Z9 ^$ B
使用空重,
9 ]% c2 ^% x2 b.
* q* O. D) k) h" Q* W C( y面,: R5 P, n7 b3 n5 J8 p3 R
油冷却器,3 I4 u' F0 y4 O; |8 ?
利用燃油或空气的流动来冷却发动机滑油的热交换器。
$ s2 _3 \2 O" j/ |油分离器,; v$ M3 f( m$ b, U+ i
一个能从回油槽或油箱发动机滑油中分离出不需要的0 _, L6 x0 H* H
气的装置。
' a- h: y: N: B M$ R滑油筛,
! }; \! T, [0 p0 s6 a p滑油油滤的一种。
\1 n" c5 Q: M$ _; x4 G液减震支柱,/ D- f. Z8 N* R& T% d+ R
见Shock Strut
# a! w# }8 X- K# w' c反
+ P' z# s: G6 z相反的一面。8 d) L# \: Q) L V' a2 S
滑
1 W Y; X, @% L- g, h$ E8 l滑3 V% L/ }: _8 t1 r; O5 d
空( a+ c8 k' W+ B+ P) }; i( e
油
( {3 o. k% D" m+ ]3 g: G.* E8 j3 T5 O( l0 j
面,, [* x: R% y% r/ U; r
相同的一面。1 u5 r/ N7 b$ D8 w% M: G: q
个全球范围内全天候的导航系统。
! M$ j7 \7 M( k, n或组件损坏而导致从电源到接地点之间
- d4 o1 [6 e9 z不通的电路。9 i$ O: W8 J' b3 w
同9 v. R$ R8 c+ s4 F
奥米加导航系统(ONS),
6 w0 f1 ~; Y b9 \' A一
+ ?2 V8 ~! w' _- C4 G5 u' }0 w开路,
( |) I! l" H/ z5 S# a+ Z, u1 T由于线路中断
2 b2 O& L5 j- i- I& m1 [( b英汉对照民用航空词典B OEING
# I# A' @/ e3 s/ R: a1 _TECHNICAL DICTIONARY 109
; G, G8 ^2 m: E$ S- [# @OPERATING EMPTY WEIGHT (OEW), The weight of
( i2 }; ^/ y- b7 X6 D- C" Jan airplane fully serviced, including the crew but without
) V4 t: v& z2 I& Hfuel and payload.
* @* j0 r, c7 D' d( K* J/ U2 P+ iPERATING ENVELOPE, Defines the environmental
9 H$ I: T5 k" w6 V! fOPTIMUM ALTITUDE, The cruise altitude which results
. y$ ?: {8 o4 V1 V' S" kin the best fuel mileage.
+ V- K0 F( c. dOR GATE, A device or circuit with two or more inputs of
" n5 C$ x, d7 _1 O- X+ X5 m Ebinary information and one output. The output is 1 when
" D0 U" C. s8 oany one or more of the inputs is 1. The output is 0 when
' M2 f4 z- d1 _all of the inputs are 0.
/ i# m/ x" s8 SORIFICE, A specified size hole in component for control2 o# I6 `6 r( {/ C- y& ~2 u b
of fluid flow from or to the component.: E* s$ [3 Y. V2 I
ORONASAL MASK, An oxygen mask covering only the
0 D% x6 ]1 S# D! S, j% jmouth and nose.% F8 a7 ^! W/ i1 `- D$ e, \
OSCILLATE, To swing back and forth with a constant
# ]) C$ Q( y. L8 C" p* |' [/ Trhythm.
4 {- V, t) C U4 ~. p! ?1 T使用空重(OEW),
7 o- V4 A' M% E' z" \# }+ g使用包线,
7 i+ @9 e8 k0 l; {4 `8 ]确定飞机准予飞行的压力高度、温度和速度的环境极
: i$ i. N. W: _7 A6 k7 F或门,
6 [8 ~0 J; H# @; g' v7 i具有两个或两个以上二进制信息输人,和一个输出的装
5 f8 y; C6 r7 g) P0 @: F置或电路。当输人端有一个或多个为逻辑1时,输出为逻# K0 r7 [4 W! F6 t) w+ j8 G5 g
辑1;当输人端都为逻辑0时,输出为逻辑0。
( v% j% s9 L1 Z* B量孔,1 r* ]7 i5 `1 B
部件上用来控制流往或流出该部件的液流的尺寸已确
5 A: ?, x4 \$ A定的孔。/ j3 h0 P2 B2 C, d J9 T p J
口鼻罩,! @& ?4 Z% i$ p! u" A
仅罩住嘴和鼻子的氧气罩。4 t$ p2 b# ]) [4 ~5 F
振荡,
- a8 l q+ Y; z& k$ G6 Y- f0 U4 S以恒定节律作前后的摇摆。
3 ^ I( t7 ]2 i: u0 t% v8 iO r5 P! l) H- I6 E% C/ X
limits of pressure altitude, temperatures and speed5 T4 w7 g9 G) I7 a" `+ M
within which the airplane is certified to operate.
' F/ Q& n/ |6 q7 ]& G" {一架勤务完毕的飞机,包括空勤人员,但不含燃油和业
; R7 V/ F% Z5 e载的重量。; r& n7 j1 o, u" B$ V J* ~! J9 S
限。
7 { D" S8 ` k最佳高度,
$ e7 m5 r3 s7 J" T9 ]: }, h& ]可获得最佳燃油哩程的巡航高度。
2 Q& y+ a ~1 P5 i- k英汉对照民用航空词典B OEING/ n' a' _8 }! b, u
TECHNICAL DICTIONARY 110- X, Q' D' n/ v
OUT OF DETENT, A condition away from neutral or a
# w+ n4 S( Y/ j: W3 i1 ^8 gOUTER LOOP CONTROL, For autopilot operation this9 L6 y1 ]5 h$ u ]/ H" i. x
is control of the airplane's flight path to a target.
* _9 J# K/ T0 HExamples are control of heading, altitude, and vertical
h; O0 B6 I2 G1 x; ?; }7 [6 {5 |: lspeed.; \: a$ D. O. C& Q& E
UTER MARKER, A marker beacon located at or near" Y g, w. f) ]9 I; p1 J" @
e glide slope intercept of an ILS approach. The OM is
- f& @( q. H9 t/ h7 inormally located four to seven miles from the runway2 A- M2 }" }# ^3 `1 n% B6 L; H
reshold on the extended centerline of the runway.; D( s" y0 S4 w- L0 J4 t/ M }) I
W VALVE, A valve in the fuselage for4 E8 m8 B0 `. m- F# a
g the airflow from the fuselage to ambient for0 x t9 l; D! B. v" z
ation control.
5 l8 W: `3 ^! K( zUTPUT, An information signal going out of a system or
4 e9 l. x8 ?& O& e. k) q4 c9 ^) _part of a system.
- }7 T: h/ m) [) x SUTSIDE AIR TEMPERATURE (OAT), Ambient, or free
* ] N9 N" X+ I2 a, mOVERHAUL, To return an aircraft or one of its% I9 ]$ F9 b% @
OVERRIDE, Operation of a component by a method
( O% R9 n' a7 x+ }8 z. o. zdifferent from normal operation.
- }) [9 B8 F" m6 U- H操纵杆离开中立或槽口位置的一种状态。
3 \( u/ I3 z/ o' Z; C4 }制,- K" \: S5 k4 ~! I8 ?
航向,高度,和垂直速度的控制。8 |0 n3 C6 K3 V5 y% L
指点标,
" q& e9 M7 Q3 r5 {- h" i位于或靠近仪表着陆系统下滑道截获点的一个指点信9 z; W( O* G5 \4 A) M
标台。它通常位于跑道中心线延长线上距离跑道头4至71 N* @2 I5 v( d
海里。# _5 i0 I( G3 l: M# p* l1 e9 |- p
流活门,3 N& z6 s# W/ S" n
机身内用以控制从机身流向外界大气的气流以进行增
% d+ Q" z6 C. ^$ k2 G控制的活门。% U$ ?- t {4 y# V3 J- t
输出,
7 N, `1 Z* @3 y! z M& n: Y' R' f从一个系统或系统的一部分出来的信息信号。$ T8 {" E! j {# d; P+ w; J' j# X1 Q
界大气温度(OAT),; u( M b6 s. `
外界环境温度或静止大气温度。
" I) l# g! L: L2 u- y4 k修,5 p) [/ k$ Y1 U( G
将飞机或飞机部件修整到近似全新或制造完成时的状' w* e4 I) [/ i! n/ r! t5 C
超控,: ]" u2 l1 @3 b, C
用不同于正常操作的方法来操作部件。 a& ?: Q9 Y2 [# I; J
notched position.: ?$ J# g1 ~- y- K0 M+ @
O
0 W* K9 B; _/ e- I, z1 u% s" cth
. j0 l1 G( u9 \1 Y6 f" t" Jth
; V) J& X3 p* s# U. O, rOUTFLO# a2 f5 E# J' c- |+ ^" b% \
controllin) `$ v" {: S! P. U/ k8 E
pressuriz1 g1 K: s0 o* C4 K) _3 W5 c
O
. c5 H% f# u# |" H8 E. ka
7 A* B' P$ A) a3 J" p p) `O% }9 L" P% ]% x! v+ `2 H2 p- o
air static temperature.
+ O" I2 l4 ^4 ucomponents to a like-new or just manufactured8 A: Y, k4 t( g0 A9 `
condition.
; Y+ A9 R8 w7 \' E脱离卡挡,
6 ?1 g$ N1 c9 M# l! M外回路控
* L; x+ W, _* Y* j7 s用于自动驾驶操作的对飞机飞往目标地的航径控制。例
, z3 t3 p( v3 P- z3 d) q如
- s/ v d4 ?8 f6 }9 G; h1 F远
* K) i" T) L' r外 [1 A! @& H% D0 _
压4 K4 Y7 i/ z: Y( b' P
外: y) F' C8 f2 l) I
翻
# l$ v& `3 |; }! }8 X! K* W态。4 B) ?+ C1 j% G: s7 A4 @
英汉对照民用航空词典B OEING& K5 ]8 c1 f0 ]% f/ Q
TECHNICAL DICTIONARY 111
1 z7 l! A2 d3 t* j9 GP. X# ~8 x7 h) r/ z0 A( a
ACK VALVE, A valve for supplying air and controlling
5 J3 J5 U/ K$ Ymanifold to the air2 R1 O9 l; L0 R" D8 e9 s) j( ?
onditioning system.
# v0 [4 W* R5 N Jll piece of any substance or
) P, C# h6 ]3 B' ephysical matter.
6 e5 R* j6 M0 L3 R/ [+ n, Q! hh. E" b/ P- {1 Y @
rovides flight crew and attendant announcements,' G1 V2 S( d+ O+ l
oarding music, and chime signals to the passenger0 I1 z' p) H+ x$ q2 k4 Z6 s( v+ G
cabin.
* Z( p0 a; [ c, T$ J0 w+ ]ASSENGER ENTERTAINMENT SYSTEM, A system
" m, I! P6 s- e2 @tertainment to' m8 T$ ^/ K" ?7 k. A$ d8 p
e passengers.
9 G+ Z2 c# l ]( D6 }, R+ VPAYLOAD, That which is carried to the destination,
0 H6 O- t& Z: A8 ^* Xuch as passengers, cargo, or mail.
3 b/ r' {1 d8 i- {* {$ _CA, SEE - POWER CONTROL ACTUATOR
4 D& Y, p! U; |/ `; R; t8 z' O3 y3 ePDCS, SEE - PERFORMANCE DATA COMPUTER
/ t* V7 j" p! PSYSTEM' F: t) }+ U4 @$ V4 F- t/ `
调组件活门,
4 A7 l3 {8 D8 g0 I! t$ `( p由气源支管向空调系统供气并控制该气流的活门。
4 t O8 k$ C; [- h- j( M5 t' g' O1 C任何物质或实体非常细小的一部份。: x- \7 V9 q/ i r* U$ v
旅客广播系统,$ O7 G; Y; m W) c& b7 `+ p
能使机组人员向客舱进行广播、播放音乐和发出谐音信
% Z! Y; F2 h: _2 k的系统。+ x4 G; ~# j0 ^; i0 a' k9 y. }; |
客娱乐系统,
4 R( \. c$ V& z* t6 [9 \# R3 e频和/或视频娱乐服务的系统。" j/ b$ o2 W a+ Y
由飞机送往目的地的载重,如乘客、货物或邮件。
% a# N7 ?4 E3 N9 a6 l$ Y% }力控制作动筒,& v) H, i& \% q, v6 h
见Power Control Actuator
" T2 T' A1 x) E& wP# Q! G% E, ~9 H9 a, f; ^. x
air flow from the pneumatic
6 i) g. @* @# |c
3 f/ R2 X) w& [- ~ |) T3 W( c0 jPARTICLE, A very sma: z" C* e+ z z" D& }
PASSENGER ADDRESS SYSTEM, A system whic
( M' L3 ]" m- e T7 ^7 ^8 Np: z3 ~# G, _7 B# ~
b
( F4 K4 t) J6 f& ~1 N- U2 WP; O- H# ~2 _$ w- z3 v" E; N' x# e/ {2 L6 J
which can provide audio and/or video en
0 y5 `' a( m4 G9 ]4 H2 t) @. Qth
1 V+ k) p$ ?; E' }s
5 E" X& p$ Y1 R* @ [1 c) pP9 v% v* o4 Y' E& Q, K o) F9 Y
PCU, SEE - POWER CONTROL UNIT y/ y* l9 M' v) M
空
$ }3 D1 Q9 f4 c, r微粒,8 v% ?% a8 M. F: n, P; u: ~5 m/ |
号
; W( d { J6 r1 v6 V+ q旅
( `8 d8 g+ q( U向旅客提供音7 T& N: q; W; p3 F5 s8 d x* s- D5 T1 F
业载,
1 Q. n! }) v3 a$ M" [/ ?动
# i% y, J/ k6 g V.
7 v( Y; i& j0 ]0 v1 oControl Unit
0 U) \( I! |7 V x6 r, D7 {' R* v% ?动力控制组件,7 }/ C6 ~& z: m) V2 d& F
见Power .* m. j4 g Z) o+ t4 S1 x
性能数据计算机系统,0 ]5 T F7 ?9 j3 n/ c$ Z9 \2 T
见Performance Data Computer System.
+ B! R; x4 {1 [, W! O* Q英汉对照民用航空词典B OEING* A d$ e! K+ P) r N1 ~3 F
TECHNICAL DICTIONARY 112
1 b' x. X7 U: r8 x, C! j& oPEEN, To cause a more corrosion resistant surface by5 X$ W5 x: |2 I" n) x
multiple impacting it with a hard material such as steel
* C, ~) Y8 V2 V$ o; Z/ n. X8 ~3 kpellets. Term for this is Shot Peening.
' D! P- e1 o5 ~3 g" A8 Z9 i& GDefines a position on the aircraft relative to the mean& ?1 z8 g/ O2 d! w$ Z8 ?
aerodynamic chord of the wing.
7 V* T: `- _( S/ b3 @6 w6 Ir as a percentage of a fixed7 m, o" L( H& o: r3 i, R: h
mount rather than revolutions per unit time.
; a8 i {5 I+ \* Gamount.5 Q' h5 i n' J. D; Q! N3 ^( E
ERFORMANCE DATA COMPUTER SYSTEM (PDC,
1 v1 P. b( g9 _: E- ?+ ~8 uPDCS), A device which provides data to achieve the
1 H. k& ~& O+ d: |4 c& xmost efficient and economical operation of the airplane.% N; g+ B. k: e) s4 I
PHASE OF FLIGHT, A portion of flight specifically
7 K4 @8 R# v/ t% f( ^0 gdevoted to accomplishing such things as takeoff, climb,
' E1 g/ {0 W9 t9 k$ z9 Fcruise, descent or landing.
& G- q% S r3 p这个过程名为喷丸硬化处理。7 I: l5 u8 V- t7 k
平均气动弦百分比,
6 w. Q% ^! G2 g; g! H- P; C+ I间转数来表示低
6 H3 k0 E5 {' c& r. F0 g压压气机转子的转速。
i3 J; c5 s9 \) l& i( s性能数据计算机系统(PDC,PDCS),$ e* ]3 Z0 e6 c( w
一个能提供数据,使飞机达到最有效和最经济的操作的 L! v6 o* F0 q' @& L" c
置。; h/ l- C5 }; `# Y" N! v
行阶段,: ]7 f7 r, Q4 H6 q2 f
飞行中负有一定任务(如起飞、爬升、巡航、下降或
- z3 u+ l# N" x8 }份。: F. p v# L, ?! B1 w
PERCENT MEAN AERODYNAMIC CHORD (% MAC),$ a& U; d% p! q1 O( c
PERCENT N 1 , Expresses the speed of the low
8 _4 a7 h$ W: p" |0 f$ Hpressure compressor roto
. j! K9 l7 p6 U/ ^. O4 L5 wa% Y& ~1 U" u; N% l& b, n/ T! _6 x: j
PERCENT N2 , Expresses the speed of the high
3 N* v+ L; ]' Vpressure compressor rotor as a percentage of a fixed k7 i8 U8 C) z
P O- U& L4 w( X6 V1 u+ A
喷九,
3 N; w) S- H( O6 F4 k' F! A9 h为形成防腐能力更强的表面,多次用诸如钢丸的坚硬材
; O b6 O2 o! ?6 g1 {料冲击表面。$ M' T9 ?* Y" g* a3 M8 ~
用来确定飞机上一点相对于机翼平均气动弦的位置。6 C5 m* I+ k) i4 p
N1百分数,
0 G9 H# v9 J5 ?' g! K. a以一定量的百分比而不以每一单位时 v8 s) D9 N4 ?2 g6 H5 O
N2百分数,
# ]& q6 }! L& O) x以一定量的百分比来表示高压压气机转子的转速。; w. k2 `6 N8 b* C) E/ }9 ~
装
9 R' a. s' K, ?. h- J飞6 _- c/ D/ E e+ N" E4 h' O
着陆)的部
8 r4 y0 g' Q) F7 A' p英汉对照民用航空词典B OEING
3 r9 K" N+ ]' B" `; B8 L" nTECHNICAL DICTIONARY 1137 d9 M2 F% _# [
PHILLIPS HEAD SCREW, A cross point screw with two
) Y- L j! p* y- m$ R7 o3 Q% Oen with a flat tipped Phillips head5 I; r/ y, I: \, n- g0 H7 p
crewdriver (see Reed and Prince).0 l8 e7 z1 O' R
ITCH, The rotation of an airplane around its lateral9 E8 K1 Y$ _% q0 Q
xis.
' I+ Q7 Z. f* H& tne
0 t- j3 I+ q0 P; i: F' p- f7 vose up and down movement controlled by the% x5 |8 Z/ K. s5 Q2 o2 V
levators (and stabilizer for trim).
9 Z$ f1 Y$ m: g# Y" k( ZITCH RATE, The rate at which the airplane moves in- J% X/ f7 i( k6 ]' f/ _
e pitch axis (nose up, nose down).
, F f5 S% s6 cTIC TUBE, A tube facing the airstream7 e4 f. X& [3 V! Z
hich measures ram and static pressure. Used by
, s0 V+ m! f: d" [( uirplane instruments.( k6 d3 p" P1 z8 b+ T) _- n
丝钉。由平
: v, M1 b* { j十字头螺丝钻驱动。4 U$ z* f( v0 q
仰,2 g/ @) M2 {# M; Z, Y
飞机绕横轴运动而造成机头的上下运动。
( h, w! I( f& ^2 f一侧通向另一侧的水平轴或横轴。升降舵控制
4 B5 ^7 t5 L: ^头绕此轴作上下的运动。(水平安定面则用以配平。)
5 J4 {, H }0 k F' P# p1 s9 T; q: n6 [俯仰率,- D9 D' [# u7 m$ v
飞机绕俯仰轴运动(机头向上或向下)的速率。( X* T# P* }) A
管,( O1 c/ f4 `8 f, O4 }3 u* Z6 F
开口面对气流以量取空气的总压和静压,供飞机仪表使4 e9 O3 {9 U* Z+ g9 W
的管道。5 L# @# H2 T6 R" }4 ^
distinct tapers. Driv6 V% [; a/ r9 L. X3 r- E& x
s
' m' @4 Q, [, g7 R, V$ C. X6 jP* ^8 @9 t3 b* x/ c' j
a3 p& S% B+ F% L0 ?4 U- p. t
PITCH AXIS, A horizontal or lateral axis passing, l% A8 K& @ s+ E% {
through the airplane from one side to the other. Airpla
( G8 d8 l% i4 b' S4 hn1 C- |* m# ~" x' n4 L5 k
e
" A! d! o2 a$ K8 Q. D0 ], QP
- r% u: Q; i& I* i7 b, Eth
6 H3 n) W& @! ePITOT STA
2 v0 S& X0 }" t4 ~9 E5 Z6 Vw
- v1 [/ B% z5 s5 v, s$ ma3 s$ D$ G3 O: U( z4 _. A. f! O. A
十字螺丝钉,
6 t& w; M2 g7 d: m3 |+ U9 h螺丝的顶面有两个明显的锥形十字四槽的螺
" `* M6 H! a* R+ [顶
: o& B5 f3 ^8 U7 W: y9 V2 z俯 d7 I; ]9 C. P' c
俯仰轴,
1 s* O5 S8 l- J3 K: ^ `$ k从飞机3 x& Y! h$ x$ v
机
% P1 p6 X9 u$ A5 y总静压& q+ Q z% B9 ~2 @4 j6 F
用
0 R6 S8 f# _# g, [3 P) w* Y1 f2 @+ }英汉对照民用航空词典B OEING6 {- C8 v3 M* d
TECHNICAL DICTIONARY 114) N4 v8 i3 M$ S! {$ A* L
PITOT T
. W* U, \. R. Y: y9 M9 Y' c( m! \* `measure
6 a; L. F- Q7 t' f7 o/ ?' YUBE, A tube facing the airstream which: H, |% A* w; K
s ram pressure.! @% p1 T" h, Z0 [1 e& N( f$ ^: M" p
PLA, SEE - POWER LEVER ANGLE+ {- B1 K, f, `+ N
r
8 x }1 ?* I4 ]' _e& i5 r0 _& {: z8 f
LEXIGLAS, A registered trade name. A transparent; l, A2 [' i* g5 v4 ~3 @- z
r any purpose. N, g; y8 @, j
NEUDRAULIC, A system or process which is a
. R$ x, D1 l* ~! S- x3 Y7 e) u: ares.& |$ ?) k# o8 z3 n8 ^
PNEUMATIC (NO. 1), Cold air, controlled and/or' W+ G) [- `# L
pressurized.! V; `0 ?8 ? {& }
托管,* d$ h- c. E6 J. x' B' R
面对气流以量取动压(冲压)的管子。
1 e) F3 Y! r, ^% c门杆角度,
' `2 u8 V/ _5 S( I. p3 M+ }见Power Lever Angle8 H( [& w6 S2 }! b% V
PLACARD, An attached sign providing information o0 Q( r& ~. L* W G) E9 b; `6 U, {
instruction.
" S0 `$ o8 k, n% e; A/ UPLENUM, An enlargement in a duct which changes th
$ G) }7 w7 {+ E7 v) q; t& f7 ?flow characteristics of moving air. Used to remove
$ B1 h8 ?3 m2 Kpulsations caused by variable airflow.9 ~* i4 N, y: n; n* _
P) P; q. k. q+ F( w0 t
acrylic plastic material used for aircraft windshields and2 {) F0 T' {& E6 M% R
side windows. JARGON TERM - sheet plastic of several
$ z* E. _* f5 b/ d/ k5 Vtypes and used fo
* I' K2 a% T" j8 [9 h$ `! ZPMC, SEE - POWER MANAGEMENT CONTROL
: A0 M) g( h4 s2 U) \0 hP
! n" @6 X |9 x$ o: ^7 Xcombination of hydraulic and pneumatic pressu
7 \- t( a" V' L& [# H( d) B7 i皮
- K8 |) f* I" s7 M6 t. A3 }油
6 G1 G, |1 N% U% D* h* c) t( H: L.7 ~# y X1 S# v9 ~2 E2 y& k
脉动。# X- o! t( Z, X5 p
机玻璃,
2 m' W/ q* ?0 h$ ]# w; [名。是飞机风档与侧风档所用的透明丙
7 Q# g( W9 @& [6 O控制,) q1 d8 F/ ]9 p5 V
标牌,9 w3 r) n- _& D" ?( h& ]# L
提供信息或说明的附贴标志。
$ T: |2 o& `! u2 T2 @整流腔,* h4 V$ w ?3 B; J! l
管道中用以改变运动气流特性的扩大部份。用于消除可
: X' u0 g% |4 V% C4 P% H. q变气流引起的8 h \4 _( p7 S7 R4 P- A/ P
有" O; b( }" |6 l, ?6 t
是一个注册商品- B X8 H9 {' i0 [* S! v; ^
烯酸塑胶制品。行家称之为多用途化学合成胶片。: r, q$ [+ H, r2 D- _
动力管理
" p+ K# q$ c# Z2 w& h2 [! c' w见Power Management Control.% m+ h1 \* k! C/ v6 K
动液压,6 C9 P* d; w7 s
推动的系统或过程。0 i7 T0 q W# I- j1 x" }- _4 I s. Q
1),
- z/ e1 |, B; q5 \。# |& {& [9 V5 ]- G# I% _- Y) ^. F
气& C& r: O, C! m {# p
由液压和气压混合
) y* H \6 y& K: ?压缩空气(NO.
: ^" z3 y. X# }8 V经控制和/或增压后的冷空气+ ?! ^+ P3 v9 [# g" L, m, U3 B. l
英汉对照民用航空词典B OEING
) j8 l' E6 X( x2 G5 wTECHNICAL DICTIONARY 115
1 n8 a- [- n, _1 s. G4 kPNEUMATIC (NO. 2), Air, controlled and/or
# ]$ F/ U* P8 i! J) ^pressurized.8 n) O" M% x* e5 N/ I+ ?) I1 _9 U$ t6 M
OP OUT INDICATOR, A device on a filter which4 A0 ]" L* q8 k# M3 W
roughout a material.+ K- ^8 T. v2 [6 Z; `
ition./ t7 K4 ~4 F1 p! e5 v$ x. Q
POSITIVE, Definite and intentional.
) B2 T/ O5 u" ~0 G& s( X c(No.2),
! c- c2 U6 a, a4 e, C/ d出指示器,1 U+ Y0 @, s2 L# c* K- N4 c
到达一定的压差时,它会从壳体内" k8 ?* Y9 |8 x! w8 E8 h
指充满整个物体的细微小孔或空隙。' Q/ U: B, C4 _
置基准的飞行管理计算机的一种操作。$ ^- d" J j- `( |# ]
肯定的,8 u( @$ k: U- U
一定而且有意的。
' Y8 f/ |8 A: B6 d" V% @3 ^9 H- Z. UP
) D0 m2 c* m& D+ Q) kprotrudes from its housing when a specific differential' n4 W) z% R2 G# @+ c7 m
pressure is reached.
& k" i% j. c% P) `! H& j% K1 I; U& {POROSITY, The term for pores or small cavities- ~$ M: y9 T- o' |/ u
th( u, P# G3 q3 J7 S% j7 p
POSITION SHIFT, An FMC operation used to change8 f( h9 a- e) b' q4 v( G* ?
the reference of present pos% ^7 ^% r7 U5 F" r$ p) [
压缩空气7 E: I0 k/ I \0 d
经控制和/或增压后的空气。7 |/ O O: H. h. c+ C4 z2 k4 R
弹
# \$ }. k `- }5 g" K' n) o9 [1 B过滤器的一个装置。, R; V! R% }, {1 _5 J
伸出来。2 n5 I1 W, D* S: U& |8 f
气孔,/ \/ W1 m* r; T8 w. t
移位,' A) s: _9 `# u/ C8 X, X; o4 Y2 H
用于改变现在位: Y) R) H7 `" U D( q2 r
英汉对照民用航空词典B OEING# i* j4 K# i$ o/ l+ Q5 c
TECHNICAL DICTIONARY 116
% T) \: _6 ]; Q# D4 {POTENTIOMETER, An electrical device for changing$ ?/ ~% z' s6 W) t: m6 `/ s
the voltage supply to an electrical circuit component. W% K6 W. F9 q0 A+ C. ]' o& @- k
r/ L+ h2 G7 Q0 h; F
bly for operation of flight controls.
& |! `1 w9 x( f, w; |$ G. TOWER LEVER ANGLE, The angular scale on the( @) B# }* k; r8 k8 Q! x y3 t, O
main engine control for showing movement of the power
$ {$ t: g( _" x9 C9 `& \( Khrottle) lever.
* z- y, I" R5 P, x' T6 C B( zOWER MANAGEMENT CONTROL, An electronic! `0 H+ [3 {( ^
ngine control.1 G- ^4 S; P, b+ Q" I
OWER TRANSFER UNIT, A hydraulic motor/pump for; I, F) T. P7 u3 z1 H
upplying hydraulic power to components when normal& l1 g. M. u8 J2 i& J
RECOOLER, A heat exchanger in the pneumatic
* d" Z% a( g: [8 rlied* D$ g) c, ]8 \) T7 ^/ R. v o/ f
作动筒,6 j4 w3 @4 T( w7 d8 U+ D D8 |
件,0 Z2 p, M- d& q1 {
油门杆角度,
/ W* D# s k6 w2 s( P+ l主发动机控制上用以指示油门杆运动的角刻度。, K6 r4 p8 }# n c
动力管理控制,' t' e. s7 y' _- ^0 H. W5 S7 Y
控制发动机的电子装置。# F/ M9 q9 Y5 z) [3 ]
力转换装置,( O/ g9 q, ?% c9 p
当无正常的液压来源可供使用时,用来向部件提供液压5 j5 E I u( y. x+ a
马达/泵。+ p0 c3 t8 d8 R5 O d V" o3 o
冷器,& B. g0 t# P P3 \1 b3 F! h
中的一个热交换器。它将发动机引气冷却后# s( v! m+ W' e( N5 R2 i! u
供给气源总管。8 u4 Y7 H' T; a$ B' n: }6 g
POWER CONTROL ACTUATOR, A hydraulic actuato
$ ?6 Q+ V+ z6 C, W- r$ K8 n: n3 Wassem5 d0 `$ X; ~* ~/ a* ^$ n- r
POWER CONTROL UNIT, A hydraulic actuator
$ X: |" n& A9 }' ]/ l6 H- iassembly for operation of flight controls.2 y3 q- m7 m# {4 f& I# _
P* g9 F, ?3 R" g4 T% p
(t
+ {* U4 T7 M+ K0 @) ~' NP6 O) T1 a4 C' k* V* m9 Z
e
9 N( Y' c4 D& x3 CP3 C7 W H, D1 u8 l9 l
s3 N5 k% L; P: s, ]+ w" w! u2 u
supply is not available.& z' L5 y6 P6 H2 i6 f3 }
P
' Q2 L, i; E3 o, v+ `0 Tsystem for cooling engine bleed air before it is supp
8 f% Q. l) E/ a7 w0 b _; Sto the pneumatic manifold.
4 e- r7 ~: ]( ]) P V% _分压器,
8 A" H+ J# Q) p( f2 b用来改变向电路部件所提供之电压的电气装置。4 i; n3 n0 E8 ` L0 p( X0 F
动力控制1 }$ O1 D. ?9 q( S
用以飞行操纵工作的液压作动筒组件。) f4 t4 |4 I* X9 H5 J& g
动力控制组! n) h5 e9 I$ [, t& V
用以飞行操纵工作的液压作动筒组件。
3 T( i8 c7 q# m }8 p* A" u动
! V; L3 n- G) Q动力的液压
$ A/ V% w+ \5 |预: D: i9 N2 U7 E- \$ V: i
在气源系统2 H6 S: O+ B6 n% u
英汉对照民用航空词典B OEING9 s! u: h( L% `& N
TECHNICAL DICTIONARY 1178 A' @0 y7 O, m, e7 ?* L* d5 U
PRECISION APPROACH PROCEDURE, A standard7 w, o9 c: z* W1 D- G! R* u% Y
edure in which an electronic
, \1 Z: Q' A9 v- S; Ilide slope/glide path is provided; e.g., ILS/MLS and+ X$ X+ u1 [ m+ v7 W6 C, |+ N
PAR.
$ d- F( z2 {* ~+ B; eRESSURE, Force per unit area usually measured in4 m4 v" D7 H# s+ ?9 o2 v% f" E0 G
ounds per square inch (psi).
9 D0 K- R" N) k$ P7 q0 jRESSURE ALTITUDE, The altitude displayed when
F$ O& H* b+ x8 O- x( [/ me barometric pressure on the altimeter is set to 29.922 g# c- h! }, h( g) j9 X2 Q& B
RESSURE REGULATING AND SHUTOFF VALVE, A
) e, D& D# r( s2 i! r3 [alve in the pneumatic system for regulating bleed air
) c: E2 `6 Z5 Z, P# z* opressure from the engine to the pneumatic manifold.2 D, k: C; I$ ^" E# r
RINTED CIRCUIT CARD, A plastic or fiberglass card7 \: B9 U! V, T& F8 r& u
ith electronic components and copper strips forming a
$ \! j9 G& b, Nircuit.# S1 } J4 S) ~& l& ^( f: L3 d
RIORITY VALVE, A valve in the hydraulic system for1 u$ {. Z+ K3 D+ s+ w: l* A
ROCEDURE TURN, A maneuver where it is. I) x R3 j9 `) ?9 O" b# |
lane
7 ~9 A7 U6 C' y# h1 iproach course.
2 S& f4 W- D2 Q精密进近程序,5 o0 E0 [/ x( o. r
己提供有电子下滑道/下滑航径的标准仪表进近程序。
$ c0 R5 Q* c& O y& }如:仪表着陆系统/微波着陆系统,以及精密进近雷达。6 v. m7 H! g% ]( g8 h
压力,
, D( n8 L: Y, Y! `4 B. e单位面积上的力。通常用磅/平方英寸(psi)来度量。, @/ Q0 {, S$ m: C
压力高度,/ x. {& i9 [, w) ^4 M% N
当高度表上的气压调至29.92英寸汞柱时显示的高度。
5 a+ `$ _5 _, M, i% s; R( r力调节和关断活门,* b# i+ Q* H" P' P& k8 D
气源系统中用以调节从发动机到气源总管的引气压力3 M; x* O; Y5 k/ q* V
的活门。
; o' Y/ ]! z, Q; N: q刷电路板,
% m5 A$ o# R% a1 x* @$ Y由电子部件和铜丝所组成电路的塑胶或纤维玻璃制, U9 B" D% Z6 u1 k: q. r6 B
薄板。
3 C) g$ _/ M0 ~8 t7 N先活门,
: C; ?2 K* ^8 Z& `,用来使各部件照合适顺序操作的活门。' [7 h# ^ ?) _0 n
序转弯,6 x5 y# p: J2 S" ]
后进近航道时所做的机动动作。
# f* O7 w' P5 t5 [5 [1 Hinstrument approach proc% X# Z% _, O6 t7 {. [
g
. s( Y( }9 ~7 `2 z9 X$ h& }' p* W6 [P6 t. _: F) a S/ P. I" M! N; J/ h- m
p
/ @4 u! O9 r' k9 K( kP' y) |8 s0 o Z* K- E
th
! Z* C+ j/ v9 ~& e' \, w* jinches of mercury.
, \7 u }% n* }/ K/ CP' r' C) n. @5 @+ \6 R
v
v& I: M7 m7 f& qP
! S6 r7 _/ v" v; fw
- y( z: g; [1 mc
. {5 v& q8 S$ A' RP
1 p5 b& Z2 u7 c2 {operation of components in proper sequence.) \6 Z8 ~! L' P7 D. [9 y/ F3 s7 A
P
# R9 ~) E0 ]9 V; Hnecessary to reverse direction to establish the airp
" S7 H# N& f, g! ron the final ap& [! `/ c3 c, O2 U; \* ~
压
5 ]) B& O: f" g( g印
$ q: Y$ O6 C7 Q5 ~5 O优
( x3 `# d' o! l+ V2 c: M. p! z4 a液压系统中4 [6 m' \+ r B8 M4 n% W
程
; {0 h% ^1 j5 z* b! r& z4 h! y在飞机必须反向建立最
# ?0 j( a3 B) y8 z8 n/ y英汉对照民用航空词典B OEING8 A# y' U* i- R) l8 u
TECHNICAL DICTIONARY 118
c1 }; I/ \- |3 GPROXIMITY SENSOR, An electromagnetic d8 c5 y# A! u3 i- ~* q4 n
senses the po
4 T& H4 N$ ~0 M! K# b- J( V7 xevice that
( l& f* C8 ~) G! ^sition of a moving actuator. The sensor6 T, M0 z" V7 V) H
as two or three wires.7 i8 V' |. @% A& d4 E
ROXIMITY SENSOR ACTUATOR, A steel plate
- P; C% o% M8 }& h% Z C2 Ecated on a moving component for operation of, \7 w, f7 I4 h! u# b
roximity sensor.3 i" v+ `: q' `% e0 T' c
ROXIMITY SWITCH, A printed circuit card for7 b7 [7 n& }5 D
transmitting sensor signals to indicating lights and, |- X0 \# W9 H3 K. G! p9 ?4 u4 F- A7 o
邻近传感器,6 h! I0 Q7 |, P( j0 A
能够感知运动中的作动筒位置的电磁装置。该传感器' `1 W% o: z6 ]0 O. v6 l8 S
有两或三根电线。
& f2 P) y4 F& c4 m$ ~邻近传感器作动器,
# m( F- e: O; ^) {8 z/ D/ W) U& p- g位于一个运动部件上,用以操作邻近传感器的钢板。
/ \+ ?6 s4 A% H# s- w近电门,
+ `6 V- p; F4 R传感器信号传输给指示灯和电路的印刷电路板。/ V( v l- A F+ [6 k2 I1 w' G
h# ]4 S& f; `/ r
P7 E' J' P2 u- @, }
lo
" t( `' g' g% X: ?5 L/ s. ?p5 @9 M* `/ h2 M% I/ j
P5 j# K+ z0 Q) ^
circuits.
6 Q3 B& J7 K, s! `& w8 ], v2 R- p' G邻
5 d. @4 o( K S8 T! b- d. m用以将% ]* A6 g8 t% g O! @" a
英汉对照民用航空词典B OEING
' u# P3 L% ~ c6 O; g* w6 g( |- kTECHNICAL DICTIONARY 119! Y& M6 t# @( j5 ]' M7 W' W
PRSOV, SEE - PRESSURE REGULATING AND. ]. Y* `. f& h* {% ]1 Q
SHUTOFF VALVE4 F* T( d/ k+ p, y, M3 t; r
TU, SEE - POWER TRANSFER UNIT/ M2 \0 U C1 ?$ B
removal of dirt from the air cleaner.' F u( _' b' h
n
1 n" O2 z! F7 n" u* V( k& n6 {$ i3 uQAD, SEE - QUICK-ATTACH-DETACH
! `; U4 G7 r9 B' J1 C; |+ eICK ENGINE CHANGE
" ]. |/ g& }9 xheight above airport elevation.9 R* e3 J# M" B2 c! L7 X
NE, Altimeter setting 29.92 inches of mercury, 1013.25 }) V: [! {/ V9 c
QNH, Altimeter setting which causes altimeter to read
5 G9 L9 s' D4 a, qheight above mean sea level.8 }& v; h( Z2 r
活门,
( q) B( d" [+ U( tP8 w) W8 \: K4 a# @6 T1 _' Z9 H
PURGE VALVE, A valve in the pneumatic system for) x! R9 H6 `' W6 p- u' P) E* y; J7 w
PYLON, A structural component for supporting a$ Z7 o) ]4 d$ P: Z
engine from the wing.
* `; U& I& W: Q0 m; t+ mQ$ q/ e8 {4 I6 f* w9 v& S+ |2 E
QEC, SEE - QU6 t# C9 M6 g) m; F0 d" Q( Y
QFE, Altimeter setting which causes altimeter to read# w$ ^) U9 n3 F- U& _; `
Q
9 Y( d; w2 J/ E8 i2 eHectopascals or 1013.2 millibars.
/ K: E( `: M0 l调压和关断+ N$ b7 `+ i) o, [' a; N
见Pressure Regulating and Shutoff Valve.
# W1 I6 r7 W: S! B/ m$ G5 A& \动力转换装置,, o5 Y. a- R- Y7 }% [% S4 J
见Power Transfer Unit.3 d& l. j" S; V
气源系统中用以清除空气清洁器中之灰尘的活门。; q6 h1 P5 t+ V2 |! c! ~
速装卸," Z% q* y) A1 Y+ x9 Z* E. M. C
见Quick-Attach-Detach
! @+ l* h) D8 N+ j除尘活门,
, R# M4 O) x+ o% U! M0 F& m* y吊架,/ }% k* e, s) P$ o% K
用以从机翼支撑发动机的结构件。
2 S- m. p' k& I7 e快
9 P( R8 \/ i8 t1 E.- A' w9 a5 Q$ h; e
见Quick Engine Change
4 O9 S& \' s! b8 f& E9 Y, U( E# H快速更换发动机,8 ^. ^4 _, }- x* ^$ S' J/ T* g8 Z
.
/ [ ?& A+ U h+ e" |9 C场面气压,
! O/ ?# A3 G& y" v8 M准高度表设定,7 \$ l$ _8 u: P' ~7 L2 ?! I4 E
2英寸汞柱,1013.2百帕斯卡,或1013.2毫1 s1 ^$ r& X; f3 g$ u# ]: S6 B
修正海平面气压,
u# @3 F3 r" G8 ~使高度表指示飞机距平均海平面之高度的高度表设定。3 J+ Y B9 m0 E/ y
使高度表指示飞机距机场标高之高度的高度表设定。' f4 H5 k ?, x
标6 W1 J2 I% ~/ M. X& e
29.9
4 n3 U" s" F( }, r. Z1 {/ l( `0 |巴的高度表设定。
! f: m2 ^* x T2 X& a! q, h英汉对照民用航空词典B OEING
8 |% H: a6 q/ P, y$ `1 N9 ~% W/ d( ~TECHNICAL DICTIONARY 120
u; e* a) ~. _- [1 ~% I- x6 L; FQUADRANT, A mechanical component shaped like a6 y+ W1 _8 m# Z. d1 j0 |
quarter of circle for transmitting cable motion in airplane# B9 m( B3 J- s/ y3 z. \
QUENCH, A heat treating process to make the surface2 ?' h3 W1 U5 C( T4 _; l
of a metal hard. The metal is taken from the furnace and/ n3 L; T* u2 t& w* G, X. M- U
QUICK ENGINE CHANGE KIT, A collection of
& k' M7 n; ?9 F5 K- ]: ne engine positions of a particular model9 ^ R& j1 l- z/ X, `
irplane.
- e4 e5 g% J3 v9 T# z! C7 q/ `ng
' @6 t5 d8 o( faccessories (hydraulic pump, fuel pump, starter) to the
: D8 g J. K! I; x8 dengine accessory gearbox.
1 @$ ]8 s1 n9 z, \S, Established the
7 S. o* o- T$ q3 E. R' r1 b/ ~minimum amount of time to cool the wheel brakes0 u9 D+ n- ~4 Q3 O
before the next take off is permitted.
* t6 B A/ ]3 s' l进油或水等液体中。
. P O: r. c2 ]# B9 L: x快速更换发动机成套设备,2 J* w, g$ X" W) q% [
置的所有部件的集合。
2 ~& V' ~' K* T* W! D4 J8 g用以将附件(如液压泵,燃油泵,起动器等)接到发动
* O& g4 S' U0 n7 y- F附件齿轮箱上的夹具。
$ z T3 c Q) G0 E8 C+ P' f快速周转极限,
0 u' C! x% T* a6 g+ _% P在下一个起飞许可之前,已确定的飞机轮刹车的最少冷3 e4 Q2 V$ n+ U) q+ Y
却时间。
% {' s, |. f6 Wcontrol systems.
1 b7 K- r/ w9 H& [dipped in a liquid such as oil or water.( ^+ ^! ~, P$ @6 v9 W" m. t& b
components allowing installation of a basic engine on to
; _: W, h* X& a G" z) Y6 ~1 h5 G, zany of th7 [1 k- Z. F! i5 V8 p. y
a
, Z8 t) y$ O+ L: l ]4 c3 Q1 LQUICK-ATTACH-DETACH, A clamp for attachi
: M9 H; X7 E- l% ]* E' Q4 EQUICK TURNAROUND LIMIT9 @! J, @5 \: m8 K$ \
扇形盘,
3 ~& h6 ?$ b: e. o( ]) r- U: R飞机操纵系统内,用以传递操纵钢索运动的扇形(四- q& n& D' T3 C, w0 ~
分之一圆)机械部件。
, C. G4 c- O8 H+ \, ^+ U淬火,
% _- H5 ?9 c7 \+ i" C; s一种使金属表面硬化的热处理过程。钢铁从熔炉里被取2 G! @; ]3 t! Q) }
出后再被泡( l% M6 r. y* K: d. s; s4 p1 S: e
用以快速地将一台基本发动机安装在一种机型的任何9 o# n( M+ }; p8 e
发动机位) a0 w) R; X* K' z
快速装卸,
5 v' a' |% ?4 Y6 G" E3 v p4 Y4 v机! S5 B4 U$ `9 J" w0 t
英汉对照民用航空词典B OEING
" i; C8 x g, T$ ETECHNICAL DICTIONARY 121
7 n4 X$ [ l' H, u u. h wQUIESCENT, Condition of an electrical circuit when no
" x- [$ ~# {0 NRACK, A place for storage of modules in the
5 P+ E7 _% K0 B/ Rlectrical/electronic equipment compartment.
: k! K2 V9 B" i2 d( Z2 _, ~ADAR, A device which measures the time between the
' ]! ^- P. C4 M3 K% v* Ptransmission and reception of radio pulses and provides ?" D: z7 K4 f' F [4 g
information on range, azimuth, and/or elevation of
% r: j/ o" \& ]6 q" N1 f" cbjects in the path of the transmitted pulses., @# G5 x9 ]9 ]9 n' `
om a
! p! \" n3 x* ]; h& y( zar.- n+ l# i2 u* I( E0 `- Y
RADIO ALTITUDE (HEIGHT) (RA), The distance of an
7 h0 @9 ~% J' k& e+ M; s! b' gaircraft above the ground, as determined by a radio
3 @ n' L6 A$ W( L& I; z3 Baltimeter system.
4 K, t9 J" F% {: R2 jRAM, SEE - RANDOM ACCESS MEMORY' Y2 z& ?& q9 `+ a% r) e" r7 Q
RAM AIR, Outside air that flows through heat
/ n) p. [ a( J8 D& x1 kexchangers in the air conditioning packs.
4 O6 B1 S+ f+ O- o0 f' ~支架,
7 Y/ n8 S$ j4 t4 v电气/电子设备舱内,用以存放组件的地方。
8 M2 a, N' e. E9 U; }雷达,
( c/ ]) O7 `* R测量无线电脉冲从传输到接收所需的时间,并提供范 _' n! c3 S3 S9 } k
围,方位,和/或脉冲信号传输途径上物体标高的装置。8 o2 f* M$ e; r6 b4 z" I6 K
由使用雷达的空中交通管制员给予飞行员的航向。/ R5 \- U* T2 C* D/ z
施发射出来的磁方位线。1 g* n2 o% O6 D
无线电高度(RA),9 Y) ^6 x. g9 |( W, f1 m5 @, t
由无线电高度表系统测定的飞机与地面的距离。
$ }( d- c: K# x+ N1 `( q随机存取存储器,1 d' B* Q8 T/ d* _# @
见Random Access Memory- [& e8 a: h) N5 w( V) ` X& B
input signal is applied to it.+ u# \/ \0 `& `0 X
R6 n* b. F9 A6 v. V/ s
e
1 y: {9 `9 X+ b# lR9 K6 x2 [( t* E, Q- ^9 \
o0 o4 ?- K; A- {* ]+ i! t
RADAR VECTORS, Headings given to the pilot fr
9 _! w0 K! C! Q; m5 Scontroller using rad
" z9 J' B$ c, F; J( W' gRADIAL, A magnetic bearing extending from a
: F k+ d; i+ ]VORNORTACITACAN navigation facility.. j+ [1 z! G L. X7 l
寂静状态,1 c# ^4 N# n9 Y% S
电路上没有输人信号的状态。
/ E; `& K& Z1 b2 o2 U0 z雷达引导,
0 P" L0 m5 D$ ]: {4 N6 Y径向线,7 m8 y: [" c x" z* O
由甚高频全向信标/塔康联合定位/塔康系统导航设4 m' M' X) u0 }- L5 G2 u
冲压空气,
0 i" U- z3 ?- ^3 W流过空调组件热交换器的外界空气。
* _: I. }7 o* v. `8 |: j英汉对照民用航空词典B OEING
% S; s! \0 L6 WTECHNICAL DICTIONARY 122
/ e5 F+ A" X6 S+ rRAM AIR TURBINE, A device which extends from the8 i2 p6 Z! Z/ l5 F
, driven by outside airflow for
9 [8 P1 y8 M$ ~' H, V" x% nmergency supply of hydraulic or electric power.1 ? I4 [2 D8 ^/ L" e
ANDOM ACCESS MEMORY, A type of memory in
$ f( Q" A! X# V6 i& E2 }data can be written into and read out of.
8 b% B1 s3 E+ d( Nused for short term memory.
9 z. \7 ]# u9 g+ FAT, SEE - RAM AIR TURBINE e/ c& u) |, k
ATIO, A specific relationship between one number
& t+ n6 c7 k4 [. Walue and another.7 w% f3 E3 V. t
ATIO CHANGER, A mechanical device for changing
% b& f( m) ]& |3 hutput speed or movement relative to input speed or
7 B( r+ \9 G7 p2 hAW DATA, Data from sensors not modified by the user
. \, F, l3 H, r2 K: r况下提
: Q1 i# f6 r. h/ Q$ b液压或电源的装置。2 ?$ a+ W* Y) E: X
机存取存储器,1 X m; y; T0 M! ^1 e! E
一种可以将数据记载和读出的存储器。一般用作短期存
; [/ \- f: p* I0 G/ n。4 \' u7 D- }0 r* \& @/ x
压空气涡轮,
9 K0 \9 L2 u. f3 k见Ram Air Turbine& ~7 b( _, w0 z1 w- Q( b
side of the fuselage6 d+ }( M w0 z7 _7 {( ^
e
7 N+ i0 z2 e- O, V9 C$ NR
/ S) ?* G- B- u8 F8 ^2 Jwhich the
2 M. k: \; Q( A( y2 jNormally, ?0 p O/ C) X* X6 q' P
R
) b) g" z) U U/ {R
+ j6 \" Q5 A0 ~3 Zv/ @0 _- T1 \. [
R( y+ X6 r9 a5 Q
o
8 Y) t& d1 |- j K' lmovement.2 O% I/ X4 Z& r1 |7 J
R- J1 l% n4 E5 n8 b5 Z2 \, l
system." p* }0 m) T# ?; A; ?$ E1 r
冲压空气涡轮, ^. P- A, f) i0 ^( Z
从机身一侧伸出,由外界气流驱动,以在紧急情
0 f( R. `* ]/ `! b# f1 ?供+ p/ u3 X, e; ]5 n+ V
随
' K3 J- n! V. G" o储3 d1 O3 G- j8 e' O+ m) S, r9 w) M
冲2 B: e* e, C2 ~$ u2 t
.& t" X) \+ G* V( Y
比率,
$ D8 j# R4 k. L. M* `! b8 h4 K _一个数值与另一个数值之间的一种特殊关系。3 T% @' R3 u Y, D8 a9 G6 h9 h0 A
率转换器,
* Y* D7 y: ]1 J- U0 J/ W! s6 W8 B: H用以改变输出速度或运动与输人速度或运动之间比率
# F- |& E7 \( r; R3 A$ P [2 F, ~始数据,
: p' B! t1 f, W( M1 _任何修正的,由传感器得来的数据。 w$ ~; _) ~0 q8 Y' p
比
' U; ~9 K0 `. @9 ^( O" i的机械装置。$ s* @0 }/ Y% }: I
原
& B" Y: F8 C) {7 s8 f0 g没有经使用系统作) H- p9 Q6 o! r; T0 F E" J- f
英汉对照民用航空词典B OEING
1 F3 \0 D' [' }( o5 I/ w% V m1 fTECHNICAL DICTIONARY 123
! e! W' x+ @6 T* ?7 }) }/ V$ O9 |) E3 RREAD-ONLY MEMORY, A memory unit in which6 |5 g" {3 v( e) D" L- m3 p) u
the computer. Under normal conditions the stored
2 \1 N' H3 ^ qinformation cannot be changed.3 {9 R% b3 [0 S6 c
ECEPTACLE, One half of a two-piece connector. It is
8 K& @6 }- F9 m; Q) rusually mounted on a support, such as a panel.
/ Y, U. ?( Z. Y, @/ fRECIRCULATED AIR, Conditioned air mixed with air" T) v9 v% `" ^( Y0 f5 R
from the passenger compartment.
: w; A, ^. z. q- V# ]" U4 ]EDUCED THRUST, A thrust level less than maximum& J/ h1 {+ r; X1 J6 n. D. O
rated thrust.; i! E. H$ Q" y: J7 l0 D. L
EED AND PRINCE SCREW, A cross point screw with0 o5 ~6 `6 |" |6 B, ]4 J8 A
a single straight line taper driven with a pointed tipped2 K- i, H6 z3 d0 B
ED SWITCH, A switch with two magnetic plates acting
% l1 O9 R7 K0 ^% e8 ?5 x* u* _8 Is contacts and operated by a magnet.: r% E( @0 \4 T& O% C( T
只读存储器,
: q5 R9 G# R7 Y. P含有由计算机永久存储着的指令或数据的存储器。在一! \" J* ~2 O# ?. V2 \% m$ {7 P
作任何的修改。
9 L- u" p0 r6 d8 R" m( }4 W; p插座,0 l/ R/ D) J$ m$ h% @
由两件组成的连接器的一半。常被安装在支架上。# S; P$ u) N9 K4 S6 ^+ v
如:仪表板。
$ m% X& b" f% b# `! S4 A) v" s. ]/ U再循环空气,
3 w7 |" r8 {" N" S7 o) \调制后的空气与客舱来的空气之混合。
4 _, k, D- ^# D! P6 ] K减推力,+ T* I& E# I$ J, l# y
额定推力小的一个推力级。; |" w7 _! h5 Z9 }- W! o
十字螺丝钉,. ~. ]& S) k }* r
的,带有一条直线锥的十字
$ h" H6 T8 r6 i舌簧电门,
7 K6 d2 }/ b* ]# J. M由一个磁体控制使两片磁片接触的电门。5 ~- d& Z$ w% C# X( K
instructions or data are permanently stored for use by! x( e, _8 L/ x j( N
R
0 Q+ f5 X5 e) i1 b; l. ~' {R* L* G: r; ?( o- L7 p
R% n6 A9 G9 m4 v* a
Reed and Prince screwdriver. (See Phillips Head.)2 U1 `- b( i& W. s
R3 x2 s4 m" ]- l6 I2 G3 A3 Q& F
a
: s# o: L0 t) k. B般情况下不能对存储信息 K9 l1 C, A/ u0 L/ w! Z# O- I
比最大
1 G$ Z5 m! S4 `与尖头十字螺旋钻配套使用
9 p( I8 S! W5 O$ x F! q( L头螺丝钉。
, ^3 x a5 ]1 ^' M" q! |英汉对照民用航空词典B OEING
" m$ n( H; f7 @" @4 E9 Y5 A1 e; D: wTECHNICAL DICTIONARY 124
/ t+ e; ]) |. o$ X7 f& m. O( @REFERENCE LINE, A line used in a chart as the- M- N& e* K6 `' p7 i
starting point for applying corrections to chart input
/ x. Q5 Z5 V3 l/ m$ U) t4 Walues. One or more reference lines may be used in" I5 ~7 u$ Y- v; L8 b8 L
uccession.
2 U+ B( x! Q: e# ?8 s' VD TAKEOFF, A takeoff which has been
* Q# j; y! m" G- r' Z.% s8 g6 e1 M$ b0 b
EGULATING VALVE, A valve for controlling pressure( V; M. k6 A/ c1 z' y$ r
ELAXED, The state of an electrical component or
, E2 z; z5 H$ [# c R; Fwitch that is deenergized.% r G: o2 u" y8 ?
RELAY, A switching device in which the contacts are
3 B" N) s# o( [) Xopened or closed in response to separate current or
f P# E# t$ e: q# t* woltage.; U! _5 x* p+ }; @
RELIEF VALVE, A valve which prevents high pressure* N0 M* m/ ~6 q7 D
a system by venting the system to ambient.
8 _; \: A, ]* v( |" p6 a起点的线。使用时可用
# [# \( u0 t) m条或连续使用多条。
5 h+ Y, i; s3 h' r) q. l! ~( W断起飞,' S3 E# M r _% V
离地前被停止的起飞。) g9 K$ M6 i% u# r1 \/ l
节活门,
. ]8 J) _- X0 R2 b制压力或流量的活门。 d `* |$ c! j& {( m. b! W
放状态,/ v9 G z% h, o' k
电器部件或电门处于关闭或没有通电的状态。0 }9 { |$ ]: ~7 i9 b4 p
继电器,: k# _+ G) U1 B7 _" }: S# Y
一种电门装置,其接触点随着单独的电流或电压开路或. g" ]2 H1 O3 [4 f
合。
' o) j+ T% W" z释压活门,
7 Z+ w# E$ }! x通过将系统与外界相通,以防系统内压力过高的活门。
$ S2 k: h6 I, ^3 u) q: vv, ^* t$ ?7 g S6 i; j! w
s
9 _ [+ l9 _+ ]+ `; f4 }1 ~0 CREFUSE
8 O# G5 m8 t" K$ dstopped before the airplane lifts off the ground3 P) J4 l/ c+ |
R
4 I$ w4 R* a2 x0 d& B+ w' u, aor flow.% v6 ]5 l) R/ w L
R
8 G- f5 N2 }/ w6 _s
& d& I5 I7 a+ C5 M/ }, rv N3 a. M9 C2 d4 r. c
in
+ v" H$ s' g2 l r9 \/ k% e; z# ^基准线,
1 W- x7 U4 |) }4 J在图表中用作修正图表输人值的; X6 i: f, J. l/ i, l' l" m) M( D
一
$ T: F0 d% Q4 O( c5 e4 [中
2 a! V* f3 G! w3 a在飞机
! Y* u0 l# K% l* I% Q调; K9 J/ _: v- P
用以控. C5 ]( C! ]+ o
释
2 _+ i; @( d2 t, L9 B. t闭
; I& t: M" D1 c3 V0 g' E英汉对照民用航空词典B OEING( d0 X! Z" p" |3 c& c% J7 U
TECHNICAL DICTIONARY 125
: y( Z* ? D. d' P, DRESERVES, The required fuel remaining on-board after4 a3 |+ A; J; T' M" d* c* e
ESERVOIR, A container for storage of fluid.) x9 t/ @8 |7 g
ESTRICTOR, An orifice for reducing the flow and
; f. D. q4 n, H- O. vressure of a fluid.
8 |9 k4 H; s) c4 r1 ]8 H& C' ~2 NESTRICTOR CHECK VALVE, Same as restrictor but% x$ z) c' j4 T% d& d
llowing flow in one direction only.+ p0 g- z6 Z- I( U0 j/ r- W
decrease the" b* ]" G y) ~
ngine thrust to idle.
- F! ~7 _: y4 d% e9 O' YREVERSION, To change to a pre-determined mode.0 ^1 ]2 |' ]7 a, _7 f
ctrical device for changing the- [; _# Z$ z* `; Y8 ?4 y
sistance in an electrical circuit.3 y4 ^7 s7 A- ~0 F
备用燃油,
* C1 a% N6 Y& W" R照规定,飞机在到达目标机场后,机上需要的剩余的燃
' v/ J9 L7 r" B! l0 L, X$ y油。6 }: u8 }0 ~1 x; w( C+ I6 `5 t& R6 z
储液箱,& i/ W5 q2 q( H2 j: I
用以储存液体的容器。5 i1 r7 h& C: \! |
限流器,5 k1 g; Z y& P6 o
用以减低液体流量和压力的量孔。8 T) }2 u3 u% u6 E( p4 h/ M& |
流单向活门,( F6 e! ]$ s% \
一个与限流器类似,但仅允许流体向单一方向流动的活
8 S: l. ?4 K; {) N; Y) w" K门。) V: ~, c& k+ N. v
门,8 ^( C$ Y2 j5 e; u* `8 x# _( w1 P
自动油门的一种方式、用于将发动机推力减小至慢车状% W7 J0 \# f6 G
。
! @- `$ f5 U6 h. U4 F0 C# w: l+ J改回到预定的方式。7 z, i5 B1 m. f5 t2 k6 _
用以改变电路内电阻的电气装置。 ]7 |5 J1 ~$ p, s+ k
arriving at the destination airport as determined by
) X- |: e' t8 G! {, k( a1 T, sregulations.
! F% h- w( c2 c+ x3 A7 \! lR
* H0 B3 L& Y8 ~; C( U! Z& nR C h0 o4 n) G
p
0 E/ [. w# S* p1 KR; D0 ]6 q1 j7 B7 b2 [
a
/ b' b8 N5 c8 q0 f/ e5 m' aRETARD, An autothrottle mode used to
# ~& a( H9 R* I; k0 a2 Ze7 ~& p. e3 b2 P, i* y6 l: D
RHEOSTAT, An ele
; R7 O5 n& x5 q+ t( G2 N3 R4 n* fre" p2 q% f! I6 d5 d$ f$ t
限
2 P# K' S- K1 L拉回油8 J8 X: p; [; n) v
态$ @( }: V3 N& D# b- `" F( Y9 s+ P
复原,
: `( g2 P2 a! O, T变阻器,
0 P4 I* N- S/ k1 J6 U# H英汉对照民用航空词典B OEING& p- {$ j. n) S- D
TECHNICAL DICTIONARY 126
0 F2 ^( R; O1 s" B0 H/ {RIB, A structural member of airfoil shape in wing,! _- K+ \7 U/ a' X! a/ ]7 m
stabilizer or control surface.$ Z2 ]. M2 N( M
IG PIN, A metal pin for inserting into a moveable
4 ]: `' ~& s2 I: {6 [' j! gomponent before adjusting the control cables and
8 f3 q1 Z G: ?3 A6 ?6 {2 t; H7 H$ @9 Enkage.! _, Q" ^8 L p0 z$ s
IGGING, An adjustment of airplane controls and doors F$ B! u! ]: T2 L
r proper operation.8 h2 H9 f/ F4 R U. B
onditioned air supply to the passenger cabin.; I& K8 z9 D. _2 Q
装销,& b1 g8 A( n7 d, _' v) m( p9 I
在调整操纵钢索和链系之前,插在可动部件内的金属) L( `4 [, z }" I5 q
。
/ X* l* m# u( O' W# i; ^校装,
; ^9 O$ k2 N& l" P, M使飞机操纵系统和舱门能正常工作而做的装配调整。( N" v' y, A) m3 l) B: \
空调系统中,将调节好的空气送到客舱的管道。3 x) [ a7 `' i0 Y# T7 L
R
# S( R+ o# ~" S7 Y! \2 L; tc9 y% q8 r4 R# [9 M; m
li
, Q6 _. m4 ] J @( {R5 l5 K- k2 F+ c9 i9 v3 S
fo7 [9 |" m+ E1 n/ v& f" _
RISER, A duct in the air conditioning system for
& e/ |# ]; A: R2 t" w# m" Nc
* |, q9 M! j) T翼肋,2 o7 m# I2 v2 ?- U: F" _
机翼、安定面或操纵面内具有翼剖面形状的结构元件。% ?! |9 E7 Y3 p! f' S( V% @* m
校
3 q9 H/ j$ {& y销
. j) I$ c! A5 B, X1 D立管,& N! o0 H& e2 \: |- r- s9 ?
英汉对照民用航空词典B OEING3 V+ s& \6 m$ e$ P9 ]9 o7 M7 g
TECHNICAL DICTIONARY 127
5 ?( h. C/ k. X2 P& X6 ?ROD END (NO. 1), In a hydraulic actuator, referen
1 i0 T$ j- }3 Z0 z( b2 K+ [the part opposite to the piston side of the actuator.
9 L" {1 `. B& g4 m6 a, d: [6 ]ce to
' @; @5 d% Z( x& fD (NO. 2), A mechanical device usually a
, p9 q3 v4 q$ e) z( wbearing, clevis or similar component attached to the end
' Z3 ^6 ?2 }! mof a link or push-pull type rod., B6 [8 l) r5 A+ b z7 z
OLL, The rotation of an airplane around its longitudinal& j, U |3 o* D
axis.
/ ?1 ~0 d4 S9 ~4 E( N `2 r* FOLL AXIS, SEE - LONGITUDINAL AXIS2 `* R1 m% ?1 s% U* u1 H
连杆端,9 l7 X7 q3 `6 H* `
杠杆端,
( @: w2 h9 C8 z* R* M# a9 B3 \一个连在活节连杆一端或推拉杆一端的通常是轴承,
- a- B0 ?/ H: Z# g8 Z) y0 O$ o) Q吊环,或类似元件的机械装置。
9 S* f4 T$ K+ E* `; u0 X+ B/ ]3 X滚,6 G1 e' w% e8 V
飞机用纵轴作为旋转轴时的运动。
. Y2 E( A4 l2 w$ U0 [横滚轴,
9 K/ f, ^% w; G( B见Longitudinal Axis: F$ x& V9 G& p: u; o+ P
ROD EN6 C0 N& d$ f5 a8 b. L# }' a; t
R1 G2 I0 L& f1 ^, h
R
+ [# z8 L7 P1 _* h- o液压作动筒活塞连杆伸出的一端。
. g# _) ~( L! ]* N% | Y' h横, }9 `* x: H. c& p9 y( z- P0 E
.
4 ?- o2 W. @2 h j0 ^' _0 E英汉对照民用航空词典B OEING! g4 c7 R9 i* a5 A; M7 }4 S/ @
TECHNICAL DICTIONARY 128
( Y. A# D' L/ |! WROLL RATE, The rate at which the airplane moves
; {5 n: I) z6 F# p; j6 Pon the roll axis (wing up, wing down).' y j# L, H3 W8 m; \" @
OLLOUT, The final phase of landing where the
. p4 }+ s6 o0 r' ~3 @/ ~OTARY VARIABLE DIFFERENTIAL TRANSDUCER,0 h) l0 B' k- O+ @% J4 B8 `0 K# J8 g9 h
ROTATE, A maneuver conducted during the takeoff9 _1 `6 s+ @0 u o" |6 Q1 L" d" I+ I# q
n
0 a' `+ Y7 Q" ?- Z9 h# F) M1 Oraise the nose of the airplane into
- N- w# r; g! o9 Z1 ue air.; p$ s8 u) k+ B) |6 d( g
OTOR, A rotating section of an engine (turbine,
8 R5 [& i2 R0 C5 M/ Pompressor) or a generator./ j! s: f2 h8 g$ h
ROUTE DISCONTINUITY, An FMC operational+ V. ]5 K6 U) j( U! b# Y: ~
condition, in which parts of a route are not joined or
0 B, x5 ?6 G/ N& h+ Q6 {) Iconnected.! k' F$ D @+ D/ g2 E
ROUTE LEGS, The portion of a route which connects+ L1 F/ \& i9 y9 }
two way-points together.
2 K( E( E' @; _3 c陆滑跑,
+ p* m# f$ G; I4 B; Q的最后阶段。此时飞机在跑道上减速。! q; l1 ^# T: ~. g ]
,; o+ U+ p! v7 o
R9 Q. C+ i2 @' t% A, R6 e A
airplane is slowing down on the runway.
5 F" A) v% l# O8 sROM, SEE - READ ONLY MEMORY
3 n* \) f/ T0 B! h7 NR
- q V" r ^7 [( {4 GA device with a rotary input and a linear response.& s, ?6 t. G/ w( q# m
ground roll. At the rotation speed, the pilot pulls back o
( Y9 U$ M4 l5 t4 R5 w% A+ c. R0 Cthe control column to3 j) [; i5 l7 i9 A) N3 M0 B, _
th: O* s6 f7 E3 g k& y
R0 W7 j: u7 D3 p- c
c$ F- B2 K4 s9 ?2 k8 ]
横滚率,
) O8 w8 D7 n. r0 X9 M9 L飞机绕横滚轴运动(机翼向上或向下)的速率。
$ p& u- l! W1 ^+ D# x着
3 j" ^ ~ f* o1 x7 T# u飞机着陆' M9 w3 {* i3 I+ y
只读存储器: g# b3 R, L6 h' k+ l8 S% \
见Read Only Memory. r, P. U e7 d: x+ z7 i
旋转可变差动传感器,
% ~% D# p I. r% O# N人和线性感应的装置。
9 K1 I- D+ h: h, D. j抬前轮,6 Y0 x" N3 I! _3 H
飞机在起飞滑跑期间所做的机动动作。在飞机达到抬前
5 R8 W* }- \# e7 g3 k$ o发动机(涡轮、压气机)或发电机的转动部份。" X- X# o2 Y8 `3 Z1 G( c
航路不连续,
" }- o7 g9 ]9 g: n1 I) i$ c一种飞行管理计算机的操作状况,航路有些部份不相连
' J( J ^6 J/ q7 I5 d% O7 K或不相通。& r( G/ W- k/ K; r D% B
航路段,
( g9 c6 m( N8 o将两个航路点连接起来的航路的一段。6 }/ ?4 V, s* _9 B5 L7 a( ?
一个具有旋转输, d* [% f0 |9 M
轮速度时,飞行员向后带操纵杆,机头上仰,前轮离地。
/ { h5 a0 y) ~% m转子,
; @4 d/ U& s5 Q# b V. I7 ~英汉对照民用航空词典B OEING E4 b4 E# t& d5 V
TECHNICAL DICTIONARY 129' F3 i, y/ J9 J o
RUDDER, A hinged moveable part on the trailing edge; _8 ]% M- S3 U8 M, L( D9 \5 | e
plane yaw (left and right)
2 s/ F% f' W) X/ ?" u# S$ g Gontrol.
% m! ]% n( O0 w) T! N4 r- L0 cRUNWAY VISUAL RANGE (RVR), The horizontal- o3 o" h2 ^' X. U
a pilot can see down the runway when flying an
% g, E) {: E- {$ E% k+ vpproach.
" ^8 e0 W* R8 y" Nof iron and iron containing metals.- h) q1 K. @ r$ q+ Y
is usually a reddish brown color.7 h( u% N5 X1 H* k
IAL
) ]- Z5 A. g: i: a) _. UTRANSDUCER
. A1 t* [4 ~- H( zS
. W+ V- L" p$ p: ?2 M% {4 E( CSAFETY RELIEF VALVE, A valve in the pressurization
& L1 k% T# T& Q; k% }+ _system for reducing cabin pressure to a safe operating
, A* Y8 K. H' C; S" A3 hpressure.
( ?# n( y" I% W! |7 nSAT, SEE - STATIC AIR TEMPERATURE2 K- t$ u$ e0 [% f% ]. S9 A/ B' S
或向右)的可动部件。. M8 w- D; G3 h) J/ W) ^' I9 l
进场时,飞行员向跑道方向望去所能看到的水平距( E' @( T- U) b: R+ |; ^1 ~
。" ?, j4 q4 [; Z4 w4 b$ w9 {/ q8 ]
铁和铁类物质的氧化物。常为褐红色。
; E5 l) u* d6 F见Rotary Variable Differential Transducer( {% C' g% J) m6 x& P8 c) u" K
of the vertical stabilizer for air
4 O! G$ f2 h3 c5 w1 tc" F1 H! y2 H! x6 R% E% V& R
distance" q7 `, O( m( R6 R
a2 g) f# @5 y% M1 B# ~
RUST, The oxidation) X0 f: e8 B: v, k# f! H
It
3 n, W" H# ~* I |7 T X' HRVDT, SEE - ROTARY VARIABLE DIFFERENT
' A3 L+ S. x+ ?: v: d5 K4 |方向舵;
* W. u; h! V0 j3 R铰连在垂直安定面后缘上,用以操纵飞机偏航(机头向
2 k% |9 G6 ~6 U1 O' j( A F3 E左
6 ?) y5 o) v! u跑道视程(RVR),9 W! Y6 `! _* y3 q: [
飞机3 w; h' A9 `/ f- Y
离: C: _; Q8 W% [8 h- O
铁锈,& d, c! ?, f8 l o( k; u
旋转可变差动传感器,
0 z9 ^' c0 X/ j; i$ Y% g.
* f$ t& V8 _; M9 z' ]安全释压活门,
1 ^1 D& I! e- [/ r v# w, d在增压系统中,使座舱压力减低至一个安全的工作压力
, W' R) O/ W9 [的活门。
* A- j% a+ U* V$ y( ?静温,
" j$ W' u5 l4 @7 ^& C见Static Air Temperature./ ^9 C/ w& o/ y0 l. _; B1 E0 V
英汉对照民用航空词典B OEING
( r8 ^& b0 W0 DTECHNICAL DICTIONARY 130
5 O1 c, x ], a, U* M! w0 ]SCAVENGE, To remove oil from the engine bearings or; w2 O4 H/ u0 w0 b [
to remove water/fuel by a pump from a tank.' K- u5 r4 ]. h9 Y1 i; l/ j! l
CHEDULE GENERATOR, An electronic component in) h$ u. Q3 ~* y2 j6 y# y
e pressurization system for controlling the operation of
/ W$ `) N) w, q. J- t) k+ Oe outflow valve.
, k' W; i6 {# wCHRAEDER VALVE, A valve for inflation of tires,) M; i! n0 H* y: I
truts and accumulators and for pressurizing the water
4 U& _" f- O& u. h- J1 GCR, SEE - SILICON CONTROLLED RECTIFIER
$ s7 T6 ~/ Y) G7 m k4 R LCRATCH PAD, An area on the FMCS control display
8 l9 i# l. T' C& ~9 d8 dunit used for showing characters activated by the
5 J/ @/ z* v1 Y: llphanumeric keys.
- D8 J, i! ^# p8 Z0 Z9 v+ e8 v" VSCSI, SEE - SMALL COMPUTER SYSTEM
+ C2 a9 B4 z# m8 c3 m! C+ ~6 H* R5 CINTERFACE
) R/ [! m, O; |/ \3 z! OSCUPPER, A shallow receptacle around a filler neck of
, s g* I9 C# j* o; _3 w( C; }a liquid tank to catch any overflow or spillage from the# {% Y2 N% t; s( {& c/ ?1 S8 h, k- f
servicing operation. The scupper is normally fitted with a
$ r0 |5 A4 o$ \( A* K4 x' y- M- Pdrain overboard." T1 e3 h# d" m* ]9 A
SEA LEVEL, The standard datum plane from which6 F& x& r. T, l4 M( P
altitude is measured.( ]- k/ u5 k k# L. J$ Z4 v" z
去油箱内的水和燃4 h* Z" h6 A4 }7 z9 }# V) @0 @
。
2 y- r# K+ L e6 ^1 K* ]6 Y; O+ S程序产生器,$ U. O8 T2 j6 O$ @! P' Q# b- y- N0 V
在增压系统中,用来控制外流活门工作的电子部件。- ?% p5 E" _3 W
chraeder活门,( `2 w: I- z0 s5 l& L- [
Schraeder公司出品的一种活门,用以为轮胎、减震支3 n% l5 Q: X. G7 {% B
充气,也用于从外面为水箱增压。. V U, z/ z6 k# X; }( |+ w' H
可控整流器,
, x$ f9 S# q0 y! v0 }$ f见Silicon Controlled Rectifier
& m: ?8 c- n2 f$ W4 k+ Z' l& ^' aS
. ?5 u( e. C+ W( ]; j7 s' j6 ith
6 n" f1 X9 _* z: f" pth
- C7 J% G$ l, D" kS
j# M7 J9 D- s; T8 X0 e0 ~& E" |s5 s, S5 x/ Z8 |8 y2 K7 s
tank from outside.
+ Y! C" m* e7 e0 SS+ S' M( B+ e' O1 v5 y
S; R( j7 h4 Y- O* F* M; s$ @ E
a' ]; c, |/ A( B3 y0 B$ Y
回油,
9 ?+ @" @, M4 B/ j: j除去发动机轴承的滑油,或用泵来除! |3 F/ w1 O+ f n S0 |+ q/ }
油4 [# h7 w) S1 N+ D) y J( q+ @
S/ d. Z3 R) ~( F! s" j" C
柱和蓄压器6 u/ A* m8 e' e+ V! j" P
硅
2 Y; M& _0 U) F% F7 [5 y% `# g.( Q4 @6 z8 g+ {! ~
稿栏,6 D; \6 f9 l6 y% p8 ]
FMCS显示器上的一个区域,用于显示由宇母—数字键6 u; N- n- l% H. ^' `# \
激发的字符。/ k" v8 D$ F* c; n" G9 F# K
小型计算机系统接口,
, S1 y4 F/ D2 r: [/ {' P+ O见Small Computer System Interface. P: c3 Y3 S! K, N; g# ]( p
草
) ^1 v: I8 q! y/ @盘1 b* T% @/ e$ z. S: _1 m8 A% X$ r
.
% S B' v9 ?2 R- B放泄孔,& g) _* Z0 H( r# M* d$ b0 Q$ Z
液体箱的加注咀边所装置的小型容器,用于接取勤务过
; f5 G. k/ _, [' b程中任何溢流的液体。一般都装有通向机舱外的排泄管
( X; s5 w+ B4 t c道。
) [. ^" G7 P3 Z3 c. q" {海平面,
8 b3 a% k5 y6 ?/ A) x6 O用作高度测量基准的标准平面。9 ^4 T! g) Q8 l6 E V
英汉对照民用航空词典B OEING0 e8 o7 P/ S- V# U" L, q( J$ D4 M% _
TECHNICAL DICTIONARY 1318 a6 k0 v4 H& n5 _: {5 V
SEA LEVEL STATIC THRUST, Maximum rated power5 E* N% q$ V. {% d) T, f. X
produced by a stationary jet engine during ambient; a. z; i. D$ C' P
onditions at sea level.0 T% T: ~" X/ v, D
s for7 v8 V0 }7 u0 z0 L7 K7 d/ H/ Z
reventing air or fluid leakage.
% {# A- K7 H0 V4 B" I3 ]: QSECTOR, A given distance between two checkpoints in
& k' P6 S( W: M/ x& m/ v; Z" E. ] P( N- W4 he flight plan.
& m4 l9 Q+ |7 K: LELCAL, SEE - SELECTIVE CALLING9 S: N8 y& R8 m0 J: \ ]4 v S. }& _% ]
SELECTIVE CALLING, A system that automatically
1 \7 x) c& O: G" _% uSELECTOR VALVE, A valve in the hydraulic system for
) R5 C) S! L! C: K- G+ do one side of the actuator
' x/ P( j) v3 }! @1 |6 znd the other side to the return line.
9 i- F: d! E, C7 h力,
7 @$ G, r% h9 m. o& n在海平面环境状态(大气温度、压力)下,一台固定住
/ n& O+ _/ E, R$ |的喷气发动机所产生的最大推力。
5 h {4 t' U. d' ~; g0 {1 u- P在两表面间防止空气或液体泄漏的元件。
% q/ u$ X! Q2 S: ]0 Y; ?航段,
- B5 L, R' v/ x6 z( E/ t( P飞行计划中,两个检查点之间的已知距离。; Q. d9 t5 G8 ]; p" N) s
择呼叫," p" D/ E7 ~1 f: d* a6 k
见Selective Calling
e# Y) E2 s C: s$ H4 l6 ?c0 @9 y; Q; o/ m) |
SEAL, A component between two surface
- v1 e0 p# J: c; d8 np
* @5 ?" v$ y' h5 v. \5 Lth
2 l9 ^( s; X7 ^+ H% {% G, M! D1 i ~S
3 ^ G5 p5 ^( \" ?2 t1 t/ ~alerts the flight crew to a call from the airline ground5 ]$ g( u% g a7 W; _
station.9 f. c& G: `/ u& X, k& s0 P
connecting hydraulic supply t3 E8 u. ?" X6 g+ U& s4 C
a
+ b$ O; Z4 [8 i' _4 m$ S% [: O. z/ u海平面静推
: d4 f$ {* i4 x5 F3 p封严,( y: R' R- \6 u5 n5 f+ r
选8 s7 P: g3 ?! x3 i
.8 @" \7 k* E8 u2 `, |* \
选择活门,
; E/ o& R! `3 J' N端连
8 m+ D6 y ]5 q8 M6 f回油端的活门。
) B6 z2 @( K/ R! ?' D选择呼叫,
; U& G- o5 v# q一个能自动将航空公司地面站呼叫报知机组的系统。3 a* l: L) c8 h7 a
液压系统中,用于将液压源一端连接作动简,另一
3 p1 M9 F7 E" F/ x2 Z接
4 j' Z1 m+ m7 z0 M* f' J- \+ E: J英汉对照民用航空词典B
( ]0 Z3 g- [' \6 qSELF SEALING COUPLING, A connection between two1 w" m4 S) W9 v" Y1 V1 c
fluid filled hoses for preventing fluid loss when the hoses6 V: w B% z- s
rated.. N3 f& a6 w" Q' a# R B& W& ~% g
SEMI-MONOCOQUE, Type of construction in which the
& b2 [' d% \+ kSENSOR, An electrical device for detecting variable
9 e+ l1 @; ]# \6 T2 m% B/ eENSOR ACTUATOR, A device for operating the8 n6 X# l$ x# W- H4 j
SERVO, An automatic control system which checks its0 Z( ?; Z4 c& G: v3 d ~+ u+ m
gainst its input so as to achieve a desired
( ]( T8 h- x" {2 _MED, Hydraulic pressure for the servo is; m1 O9 l& N" S7 Z y
resent to allow the servo to internally synchronize to
4 B: ]3 I. | r# f! {8 Te proper position, but the mechanical output of the+ B4 x# F7 N5 g+ ]# X2 T
ervo is not connected.+ k7 j# A& K* L5 A% ]# u. Q
自封接头,
# O$ ~' j5 C0 J+ \9 K5 n" L活门堵住通道,自动封闭而不
4 S H: N5 }4 X让液体流出。
4 o! T; Z3 q* G { ?/ g0 W半硬壳式结构,
8 ~7 G$ U* ?2 k6 ]6 Y; Q使蒙皮,长桁和隔框共同承受所有载荷的构造形式。
. `9 v+ \+ T m6 a感器;
! c9 S3 u% m% ]# f4 ]- d `2 G量状况并将结果以信号送至指示器和指示灯的
( t& q/ l4 F/ V/ c% \电气装置。
; A+ T/ \1 f8 K3 L8 Q# A4 X% T2 b( |1 Y传感器致动器,
% q( L& \7 `! h$ y/ C( ^3 [- n% L L。4 a8 ^) o. @# T0 A1 _
伺服系统,8 J2 x9 H5 s% P6 y- Z
能检查输出和输人数据,以便合适调控的自动控制系1 Z+ O. }2 D; s4 J
统。
4 f( d/ u/ u$ I. ]6 ^' D伺服预位,% r+ I2 \- V5 _ [2 ~2 {6 a
液压使伺服系统内部同步至适当的位置,但伺服系统的, H2 U3 I; |' f& n2 ?
机械输出还没有接通。
) C" i6 H- O6 k5 E5 V/ y+ a9 X( lare sepa
7 y" G* A- x: d+ `( i, s5 Q' _skin, stringers and frames carry all the loads.3 t8 y2 Z+ j1 n" ^: V* D
conditions and sending a signal to indicators and lights.
( ^, [" h. b6 B6 u; nS: P8 s4 H6 f7 a4 i* Z* o
sensor.
) i/ t5 J7 e. k, |1 P9 routput a2 a. l! A* Z y8 F' Q9 c
control." k0 h. Z5 b7 Z5 j' q( T ]
OEING& ?& l% j7 D. t+ ]
TECHNICAL DICTIONARY 132
3 U. V: K* `! v5 W1 c6 y, a' }: NSERVO AR
# K0 e# p6 v( h' s* n3 X5 z0 fp. O, o: Y* N6 a: A
th0 s/ @: E" c7 p/ |) Y
s! o1 c( u5 Y, v2 Q
用以连接两个充满液体的软管的特制接头。在两个管子# L% Z9 J7 A* ?# {6 R" b
分开时,接头内的弹簧即使% N8 s# W$ [6 Y* \9 j% ]
传( ^; I4 }5 I# Q$ i- H
检测变
) ^* y) o# y# f% q$ v5 f用以操作传感器的装置9 G9 \3 P1 H4 T3 R" m- ~# [7 A* Q! R
英汉对照民用航空词典B OEING2 L8 s# ?6 m0 l3 G
TECHNICAL DICTIONARY 1334 M; i- g8 I% {. R5 x
SERVO ENGAGED, The mechanical output of the
1 b8 u1 h. V5 V" Y: q6 r: T2 sservo is connected and the servo can move a surface or
4 ]2 a3 n+ U3 R4 X+ ?" A" @5 z9 aontrol5 L7 B+ c5 @, ]: a+ c& L
SET SCREW, A small screw (usually headless) used to
8 _& ]4 H: I# A, _6 c+ aeel, or knob onto a shaft and prevent4 c. Z6 f% e1 d6 b$ R- ^9 z
tation.8 S/ a4 q1 r. D! W
SHEAR, The stress exerted on a material or, assembly: v: Z/ w0 B) z
which tends to slide the mating surfaces parallel to each& t2 Z; V2 ^/ t$ {, H, s4 d
ther.5 `6 b8 u( l' o4 V$ |6 g1 V0 \7 {% q
SHIMMY, Rapid oscillations (left-right) of the landing- j6 j. l2 C$ ]# w
ear wheels.
, I5 `/ j1 V. H; P- Z预位,' S, L( w5 D5 f
伺服系统的机械输出与伺服系统已接通,伺服系统可移
& k9 i% y+ T, t& a6 A" H动一个平面或操纵。
; D6 {2 U- W; `, \0 X- n& c小螺丝钉(一般是没有钉头的)用于将滑轮,车轮,或4 d- D: k/ }$ d" m' l* e
钮紧固在轴轮上被免转动。
. O+ I9 y1 ^! R. W0 ?1 ac
/ s) f% ? | X. C. P* ^( z' ]) Sfasten a pulley, wh
- N8 Z1 `# \9 ~, jro
# [( V3 i7 o# _+ ^6 W3 u$ ZSG, SEE - SYMBOL GENERATOR5 o2 Z% j3 Z0 R8 d3 h, I" d
o8 Y: F: H! |' k0 B0 X4 i
g
( [) v6 u4 O; ^6 ]( n8 D0 c# e6 G0 L伺服系统
* |! J1 O' c5 _) N4 _定位螺丝钉,8 D9 v& z/ X! b" ]! J3 b
旋; F/ Y" `& P0 H+ H# n
符号发生器,
7 M8 n# }. R6 t. [: `) ]见Symbol Generator.
9 P% V$ Y# r: ]剪切力,0 w( l. w# h. S2 L
加在材料或组件上的应力。该力往往导致互相平行的成
' m9 p) _1 _& X# }( ]4 D8 Y, z: a对表面滑动。- A. g; L% l( x9 ~
摆振,
& g" u9 e- W1 ? Q; K" ?0 O6 ]2 K起落架轮子的快速的左右摆动。
4 O( ]1 w- o: A, k8 v& r( M$ a英汉对照民用航空词典B OEING
- w3 ~6 q1 A' Y" V% L& ^TECHNICAL DICTIONARY 134; ~) h2 d5 a. p6 j
SHIMMY DAMPER, A hydraulic device for damping
3 } E; a' S( r8 w2 X/ M2 @$ ^7 W4 oshimmy in the landing gear wheels.
3 l" h) B8 q5 I1 L E5 h9 a6 X! l7 b# Ear for) T K. E/ ]( A4 Q8 I* F
sferring oil from one
$ ?- A# G, d1 T( c- ?$ ^: hchamber to another through a metering valve.# K: {1 b0 ]. u+ M- ?9 q
,4 d& }' `, {! O2 S
一室以减, w! N, W3 N# x
着陆时产生的冲击震动的部件。
) X! c0 g, M& F+ FSHOCK STRUT, A component in the landing ge
: l5 w, z$ P; a( labsorbing landing shock by tran
$ W2 v9 @% T1 t4 n4 f! u! T减摆器,
, o2 r; i* k0 S用以缓冲起落架轮子摆振的液压装置。
7 o/ z- ~" n* h8 t减震支柱
1 q* [) E5 d* X2 t起落架上通过计量活门将油液从一室转到另
6 J& Y* B) t. L% C6 b少
$ N3 ^* Q% H1 x2 Q& g6 i英汉对照民用航空词典B OEING' g" u$ u0 s- `! Y9 ~- W. m
TECHNICAL DICTIONARY 135" v, r* ]0 v% X# ?0 q. _
SHORT CIRCUIT, A fault in an electrical circuit S2 g% u# ~. i! N, [& `' a
occurring when the power supply goes directly to
# p% o4 q5 ^3 b! Tground instead of to an electrical component.
) C1 h! n& q' NSHORT RANGE ALTITUDE, A cruise altitude chosen to. |$ ], f0 z5 F( m+ M0 @3 n4 y) H" t
inimize fuel burn during short trips.
9 W1 F/ b! M/ KHROUD, A metal covering for enclosing the APU on
4 F& Q# s/ B2 w6 U( P7 j/ w. U5 We airplane. An external tube for enclosing a fuel hose.
! Q* V7 X" h1 t0 g' THUTTLE VALVE, A valve in the hydraulic system with) M9 t+ o9 ?1 r3 I* ^3 i( \
- STANDARD INSTRUMENT DEPARTURE" @2 n3 x4 U$ {6 R$ m' u7 i
f the v" F2 q9 D. L: ]* U
r access to the components on the engine.
6 L2 U# ~1 `& X' M4 }8 y短路,
/ p# G3 j3 F& x1 H) ^短程高度,
: o0 T7 T0 i. C1 y) e. r6 D为在短途飞行中使用最少燃油而选的巡航高度。! u* S: k, V1 A, O) R5 K: ^! g
护罩,
3 {$ {: P- r5 M) G# d9 M* u飞机上包围着辅助动力装置的金属罩。包围着燃油软管
# H9 U: W! E5 G4 x9 I用活门,( l: d- n+ a3 }6 }
液压系统中,具有两个不同液压输人管和一个输出管5 | v7 N0 c* p1 K2 k
的活门。
8 V( F; ?1 |! B R; I+ W标准仪表离场,
5 M# Z% a+ `" A& o7 @% ~& c见Standard Instrument Departure
3 {: C5 y& J& B) \m" Z4 B. M$ a/ k e
S( W+ H# }5 V9 b% ~/ `$ J; s) j$ h
th: S; R. m0 W& W" D
S
9 g+ d: ^: j! k& Htwo different hydraulic supplies and one output to a
$ l( V1 V1 @( i G: s) l" Ecomponent.
% @7 R/ S; ~/ q# a* KSID, SEE& h: o7 K: r2 ?+ S# s4 ]$ F# K- K
SIDE COWL, A removable cover around the sides o8 E; Q" L( r0 t" c& G5 e# n
engine fo
! I7 L; L$ H, x! U$ _/ l电路中电源未经电气部件就直接到地线时的电路故障。5 ^( T0 k* i3 r; K L3 R
防
1 S" q$ [! m0 G的外管。8 z X1 o- W. V1 @
两
: ~7 l- {/ B9 i+ _( T/ U4 H7 I.3 p) R4 h ^9 @
机两侧,被移开后可以够到发动机部件的可卸罩* _! r* b) m" v& z
。7 v$ X" u0 A. s$ x* Q+ ]
侧整流罩,3 r& }; ]1 w; W- h+ v7 F8 k5 F
发动; H8 N: M2 F" _" k4 O
子
1 K5 M9 H; b6 ^$ d+ _8 B0 s( P& a英汉对照民用航空词典B OEING
g. |" ? _ _TECHNICAL DICTIONARY 1364 R7 X" Y+ m! m! ]
SIGHT GLASS, A glass window for observing fluid. U, L4 @- p# ^$ Q: U
quantity in the reservoir of a machine.
/ f) R' E x/ E5 [" F, that can be used to transport information for/ J- Y' \( T5 S6 o: }
communication, control, or calculation.
( }1 E, O; V0 C5 p# _) Y! v9 jILICON CONTROLLED RECTIFIER, An electronic
0 b* W8 H# N0 A t; Mdevice allowing current flow in one direction after the& w4 S6 L/ M8 T# E+ q" U
device has been pulsed at the gate.
) x _/ y8 S0 C, ^7 U' WSINGLE SHOT MULTIVIBRATOR, An electrical circuit3 m, n3 Z9 G1 F
-stable multivibrator.
, [# {+ u- [% [5 t/ M如电流或电压能用于传送、通讯、控制或) [, v7 A1 K7 Q! m( v% N. E
算需要的信息。: A7 ^' Z' p* m8 D3 n: C* p
硅控整流器,7 z2 g; l6 U( ~) C
当其控制极受到脉冲后,允许电流向单一方向流动的电" b& y: q/ o7 N. N
子装置。
. M+ `+ |7 `$ t7 Z3 B; \% U' |息多谐振荡器,
% W. a# o# y) H$ L5 ^6 u7 K输人信号触发电路时产生的脉冲的电路。又称单$ j4 g3 a% T |" d
SIGNAL, An electrical quantity, such as a current or
. y+ s, I0 ?- _: {) S6 l! E. Xvoltage" C/ A/ a/ d+ G' B5 l- d) w! I
S/ m5 y8 i3 O' p: M
which produces a pulse when triggered by an input2 c; ]/ Z/ f7 W& R( `/ V0 x
signal; a mono
8 ]0 Y2 [+ @* r1 g2 s+ `5 ?, z检查窗,6 _0 z$ @; V3 U5 \ }; l! D1 S, T
用以观察机器的储液箱内液量的玻璃窗。
8 v1 s7 {2 }5 q* C7 b信号,( r; i( W; ^; E& u4 p
电量的一种。& M/ a0 Y. B: n
计" A! r3 q" ]: q! o; d0 T K8 G( a
冲
% n' z7 U" ] g0 _! l- P当一个8 B' b z* H( a O$ {5 J
稳态多谐振荡器。& g' a3 g9 r7 o2 e) D
英汉对照民用航空词典B OEING
! C- ]# E4 K6 R* B* eTECHNICAL DICTIONARY 137- ?, W# ^+ w) ^1 ]
SIMPLIFIED FLIGHT PLANNING, Rapid determination
% k% y2 J B2 j$ @of trip time and fuel using a chart providing these data
$ b. l- H% I3 Q* R, j0 Y3 ufor the entire flight profile from brake release to landing.
! g+ Z9 A" Y# V, v3 J6 h4 s" |SLANT RANGE, The line-of-sight distance between two0 b. z7 l1 \# ~: P+ s5 w, K- B. w
points not at the same elevation.2 N3 h8 O9 l* S5 @; g3 s9 X
SLAT, A moveable part on the leading edge of the wing
' V6 d9 c7 |4 g* Pfor increasing lift at low airplane speeds.
8 @, A3 @* h: h$ b$ a+ z划,
3 c' T( Q6 Z* W迅速定出从松. i$ b* w7 W9 b3 Y* g5 S! i' | w N
车到着陆的整个飞行所需的时间和燃油的过程。( E6 r) g/ U; v5 W: v6 Z
斜距,( T2 r6 b' |, i
不在同一高度的两点之间的直线距离。; H) j: l1 ~0 [" @4 {! ^
缝翼,- }( D6 l; p$ ?5 B) q
用以在低速飞行时增加飞机升力的机翼前缘可动部件。
1 w. f$ x4 P- m简化飞行计
/ P, s/ }1 s% g# o' Q' X# Q8 m由提供旅途时间和燃油等资料的图表,来3 s# Q: u2 ?* w! F s* @1 x1 l
刹
& F5 K* y; @- t1 r- e. s2 C( T/ u英汉对照民用航空词典B OEING
; w( I; r- _. q7 ^9 H9 ]# pTECHNICAL DICTIONARY 138
( Z5 q' I+ R9 f% hSLOPE, The amount of incline a runway surface has, t' L. i3 w8 V
relative to absolute level.+ e1 ^, Z& g& `! X/ i
SLUSH, Runway contamination made up of a mixture of
, H# G, G& d5 o, U7 P6 C2 yater, snow and ice.! W- Y5 d8 v. T3 Q _
SMALL COMPUTER SYSTEM INTERFACE, An input, x0 ]1 v: h _3 f4 ~9 m+ e5 t% K
and output bus that provides a standard interface
6 [& a, s! L) @# x: vbetween a computer and peripheral devices.
# V" e; |- I- f" x1 Z, D* y8 [SMOKE DETECTOR, A device whereby the flight crew! k/ Q1 G: \: O( N. V0 C4 H
an be made aware of smoke or fire in specific areas of
) N- R3 Z1 B+ d0 a% Ithe aircraft.
* v$ G$ [+ O9 r% g2 D- t V- l1 ?SNUBBER, A part of a hydraulic actuator that slows
, f1 s! ]! Y' H0 y5 l hpiston speed by restricting flow.
0 J6 n {: O7 R$ B/ l' O- w7 KOFTWARE, The stored instructions that control the6 V4 o2 H! ]7 j( h; f! F
perations of a computer.- H4 u/ o' O& n
ng
! ] r: ^8 Q% A7 w. Fother devices.
4 J7 F9 g' ?+ vSOLENOID CONTROLLED VALVE, A valve controlled% [3 d" ]& c- t8 k3 ~
to open or close by the solenoid.
3 i; u# u. m, \) w雪泥,
9 ^ s* y+ o! ], a$ G- u积在跑道上含有冰、雪、和水的混合污染物。8 G, Q4 H( H( E3 D! g
小型计算机系统接口,: N. F5 k6 }5 e. S) r j
一个能在计算机与周围装置设施之间供给统一接口的5 ^" ]9 P3 F9 A, N& R% L1 P* ]
人和输出总线。
4 V ~# c" h4 r9 @烟雾探测器,- R. H# s" K2 L' @- f z7 G& p6 ~6 f
在机舱或任何指定区域内能测到烟雾或火并报知机组8 P6 T1 k) R$ P$ K7 O
员的装置。: O' o' ?& C/ T2 w: k/ n
冲器,
" H3 Y, B k; k液压作动筒中具有节流孔的部份。这些小孔能通过限制
1 ?+ i3 S* b, y& `9 B% E6 I液油,以减低活塞速度。4 }0 R, R6 K0 ?9 g7 I/ T! f$ R2 Y
储存在计算机的指令程序。用来控制计算机系统的工
2 S" ]0 y, Z( H9 X0 |作。
) V$ L) A$ p6 \操纵其他设施的机电装置。
7 W: u- }# A0 {0 Y# z% \* Y电磁活门,
* s+ a) `1 L+ X' h4 a用电磁线圈来控制开关的活门
# h, [2 e3 r! ?. qw8 Z( Z6 s/ v4 c* A0 u2 R. x, q
c
, R5 k" L, [+ }' ~0 f+ YS8 V: z$ n6 Z4 i/ _7 W/ H0 F
o
: a: @+ N8 `3 \. c: E9 |7 P7 _8 kSOLENOID, An electro-mechanical device for operati
% V6 m! d0 D4 M' k1 S, F斜度,
d+ d& v& H: u跑道表面相对于平面的倾斜量。: Y9 q, ?+ c* [- V
输
* ~& D4 J3 E1 { f1 ]5 ~) y人, K: R& G% b1 R* ?% V
缓3 L. f% C6 J0 u
软件,
$ \+ o6 `' { K, A% j+ D+ r电磁线圈,
+ g# I+ h( h; D用以
6 T' I$ B4 N/ I: m0 O# E5 X" T英汉对照民用航空词典B OEING
( L" u0 B" N) }+ Y- E" z( KTECHNICAL DICTIONARY 139
# l+ @0 P9 ~& B1 [( tSOLID STATE SWITCH, An electronic circuit that3 O" g- q, p& x
provides switching in a current path.) Y. y- k+ e% a3 W; V
SOUND SUPPRESSION LINER, A component in the
" y0 q7 ]0 G$ n9 p/ X( Q3 enose cowl and around the engine for absorbing engine5 F0 D* Z6 s) p; F# Z i0 k
noise./ F2 ]0 G* i: S- w
SPAR, A principal spanwise beam in the structure of a& E: \0 ^& x$ C& e
SPEED INTERVENTION, Pilot control of the speed* } h5 r2 @3 ?$ O% L8 _3 f& A
SPEED SCHEDULE, The planned speeds for a specific
" Y0 g- y+ q1 E7 Cphase of flight.
: U& M A: s i" x2 o) N晶体电门)," ?5 m& ~% h7 N$ C7 L# D# k3 Y# r
消音衬,
% _- f4 \" f& |$ ^0 p在发动机的周围及前整流罩内,用来吸收发动机噪音的5 L3 D# J; a5 D* t; K$ f
部件。
2 v2 [9 k, F8 f+ J7 Q% P4 z% t+ f梁,$ e4 v) T% Y1 s9 Z. V ^4 [
机翼、安定面或操纵面结构中的沿翼展方向的主梁。
! R' @5 v8 W) K; O) y* r3 V3 @速度干预,
$ X, G, j D9 T5 o计划速度,, m; F1 ?+ p6 U- {
为一特定飞行阶段所定的各个速度。
4 }% l* M* V1 i6 k" hwing, stabilizer or control surface.% n3 q9 c: _! L! r9 ~, O8 _2 A" I
during VNAV operation.* w6 b: g5 l3 E7 c) O
固态电门(
3 A w. Z1 B" |+ Q" f% ^3 g在电流流经途中提供开关的电路。
2 |3 D6 H5 I, v在VNAV(垂直导航)操作期间,飞行员控制速度。. f& y& C. }: W9 M
英汉对照民用航空词典B OEING
/ \( m. `) r/ W4 a+ c: XTECHNICAL DICTIONARY 140
: a c' ~9 g& t7 R% cSPIN BRAKE, A device in the nosewheel well for
; n6 E5 _" } r) H: j/ t" qstopping the wheel rotation after retraction.
8 V" y i. B; y ~: ?SPINNER, An aerodynamic fairing attached to the fan of
5 J6 D5 P1 Q- B. q# H" U; v! y( |a turbofan engine.6 l5 f- _( B7 g0 x
SPLICE (NO. 1), A connection of two airplane skin: Q& _6 \4 k: T
sections.; H* i; ^9 k# h6 T
SPLICE (NO. 2), An electrical connection between two
* M$ y% x" N0 ~9 T# f5 r* [wires.5 h& [5 g2 J9 g l% ?
前轮舱内用在起落架收起后不让前轮再转动的装置。- ~$ c5 z. E- B8 g* x
旋转罩,
% T$ l/ o9 {' G9 L3 n/ P固定在涡轮风扇发动机的风扇上的气动整流罩。& C" [. C6 q2 o: F; j
拼接,4 o6 y9 m8 n' Z$ S- C. p
飞机蒙皮与蒙皮之间的连接。
$ I( a9 \6 |3 {5 ?9 Y; h: q铰接,6 A% b8 y( D- D& M2 V
两根电线之间的电接头。! d/ [* K# s7 g# N' |0 g
停转制动器,
- I7 C: Z5 l" E4 b! r, R+ d- c1 w英汉对照民用航空词典B OEING
& S/ v$ A2 F2 M" V/ WTECHNICAL DICTIONARY 141* W) P: Z& I/ ^
SPOILER, A hinged moveable panel on top of the wing.
J0 E! o" L! r1 i: b: fFlight spoiler- assists ailerons for airplane roll( N" _+ e! k" v6 |# |$ t% h4 y
(wing up and wing down) control$ ?( n, c6 g6 [: K8 ?: K4 O
and for aerodynamic braking in- M0 r% Y" a3 K! M6 P2 C
Ground spoiler-for aerodynamic braking on the( L) N9 A; Q; a8 i: @
ground only.
; g* p/ P5 b* D2 G; y! HPRING LOADED, A condition in which one part of a9 V3 \4 e& B. q, @3 Y
evice is held in a particular relationship with another: w% J8 B) A4 R/ ~0 A
t,1 O! @/ m7 B r- I
r original position./ e' M( d- F* `, i1 @/ S8 i
SQUAT, Airplane on ground condition.
; x1 \2 G& d2 \' r$ ?3 Z% XQUAT SENSOR, SEE - AIR/GROUND SENSOR T. L0 ^& J3 H3 c7 n) ]2 u, @% s2 W- P
SQUAT SWITCH, SEE - AIR/GROUND SENSOR0 e( b3 j% D1 g- H% e" i6 e6 W
扰流板,
$ H. }) M) R5 g' P$ {+ h9 U+ t( e铰连在机翼表面上的可动翼板。& e- F! F; A& ~" M3 p* s4 u- O
飞行扰流板一功用有二。一、协助副翼来操纵飞机4 W- K3 d5 U5 P: t& v- C" F
的滚转。二、用以在飞行中或地面滑
5 r& y" |* d. [跑时作为减速器。- ?6 W' {9 `' S ]: I
地面扰流板一仅在地面时作为减速器。
+ _# ^$ B' z. x+ G簧加载的,
8 h. E0 T# [5 j4 ^; f* R& O9 X由弹簧使一个装置的两个部份保持特殊关系的一种状1 {; d! B' ~6 K* p0 @& L( I7 x7 s* e
态。该状态允许一定运动,但继而回复原位。
2 I8 ]7 A1 ~6 g' Z/ x4 P* |- t8 t; M着陆传感器,6 O% Z; k# J( ]/ e8 B1 f
und Sensor+ r9 W6 o7 x% |" N) J7 s
flight or on the ground.! u+ F# s$ G0 o' G7 z
S
! S4 h O! H8 n @d
* h! z% ?" f4 s# X/ [" upart by means of a spring. This allows some movemen$ b( x6 a; q; M1 j9 V( V7 a
but returns the parts to thei4 R' L* h/ v" w& B; Q
S; ?& G/ b! [1 ^4 G
弹8 {0 R) e* H4 C' o& {+ k9 p
着陆,
- P3 Z% ~ {" x# a6 T飞机在地面的状态。
2 Z1 G5 H+ }$ n' |$ Q见Air/Gro$ n. |" O( k$ F1 p9 e6 W3 @
着陆电门," ], X/ x+ v, k3 M/ \! L& `
见Air/Ground Sensor .# x3 V0 M$ o# M
英汉对照民用航空词典B OEING
; I' {% M& x9 t$ F& }TECHNICAL DICTIONARY 142
; y7 r) q6 D- _% G# h; W% qSQUAWK (MODE,CODE, FUNCTION), Activate2 q: F+ T6 r" c
specific modes/codes/functions on the aircraft( `3 g) S( ~1 @- I( n/ n6 A
ansponder, e.g.,” Squawk Three/Alpha, Two one zero
# L! N; C) F) i. l% R2 y( Gfive, Low".
; L7 z8 R ?% J% o$ ~6 w/ \SQUIB, An electrically operated pyrotechnic device for
^* e. x8 W, u& ^breaking a disc in the fire extinguisher bottle to release, W6 }" k& d0 q4 Q# Q, u
the extinguishing fluid. Also used for escape slide" x. v# f; G9 E' O
TABILIZER, SEE - HORIZONTAL AND VERTICAL3 M; Z. P& X, f/ O
STABILIZER: C1 _6 f4 B8 ]2 _
TABILIZER TRIM, Movement of the horizontal tail to1 p* e3 b7 \0 y! D
hange the attitude of the airplane about the pitch axis.
+ V1 p/ {, m/ x6 b- n+ OTAGE, A numbering system for the compressor and
5 C$ f3 k' {! fturbine of a jet engine.0 y8 Z( S% R3 ~6 |, m4 S
TALL, A flight condition during which lift is destroyed' e& D, S9 |3 c4 n; T3 U0 [6 H% v1 p
ue to slow airplane speed or attitude.5 q _) Z. S- i' n5 G
to enter from the top and flow
' n& v2 C5 L Aout to the system. It prevents picking up debris off the
4 [/ v& N9 w: k/ q3 Xbottom of the reservoir. It can also control fluid height in# r c# y; {( J
the reservoir.* L$ z7 }& d h7 H
能),
/ |2 c3 D7 m" @' x, ]使用飞机应答机时的一种常用的指定方式/代码/功4 O/ V) G5 n0 [* B7 H( h4 b: C) Z
能。: Q0 K5 ]' E; w3 Z
管,
1 p: L9 |; I) `7 Q& B, b: g用以爆破灭火瓶上的圆片,以释放灭火剂的电控烟火装
4 R t% b' A! e置。也用于应急滑梯放出。& r8 n+ |: r$ N) V/ _6 E, t
定面,# v) x- K J1 V3 G
见Horizontal and Vertical Stabilizer( }# M+ p2 \+ U9 R0 _
tr; M" F0 E Z& F
deployment.: @: o; E/ I6 [. T
S( h8 L; N* Q2 }/ j+ f/ x* T# m) n
S% V2 S7 U) ?) d- ] i& D4 ]
c( H' n; A+ E) H9 z* ~ W1 ]6 ~
S
# w5 k+ @" u% hS) U. |. ]8 A+ |. u6 p( d
d
# O% N$ x, }& s5 m8 NSTAND PIPE, A pipe raised up from the bottom of a3 Q( w8 Q2 Y' e) J- A
reservoir that allows fluid
5 X+ P: ~( B/ V) m! T* T发送信号(方式,代码,功9 v5 q( w: h9 i+ R& U2 ~
爆
) z- m$ H4 `) f) ~( L2 u, u安
' {) H1 l# q4 c.
) Y$ r. y7 c. ?. v {定面配平,
- ]% ?( Z1 h. c+ S为改变飞机绕俯仰轴的姿态而做的水平安定面的调整。
/ Q- E7 Z& \8 M- O: J级,9 c2 M9 b$ F0 I: r! F
用于识别喷气发动机的压气机和涡轮的各个段位的一
8 u E( h6 u) k+ R! D* K2 z种编号系统。
" ?8 D: \6 |1 f5 \失速,* o9 b1 N' B& f7 `
飞行速度过低或姿态而引起升力失去的飞行状态。5 `! V- g' N& ]4 U
回到系统中,并防止带起容器底部的碎屑。也可控制容, a) p6 H5 V7 {4 E, u! L8 B; j
器内液面的高度。
& C. v: T9 o7 F* i* y0 q安
) E/ C+ l; S3 v1 |# a$ z立式管,
$ @" A, u( a d/ @0 M6 p从容器底部立起的管道。能使液体从上流流人,然后外
7 i; e; E3 H- H: f0 S流. ?2 w" W4 V0 [0 W! O. o5 J
英汉对照民用航空词典B OEING
2 w; p/ k+ y" h, pTECHNICAL DICTIONARY 143
9 o; e4 @1 V0 T% F3 s g+ L3 t" t" sSTANDARD INSTRUMENT DEPARTURE (SID), A: f( I# {* C/ V& g6 g
IFR.
) X" @4 a; i/ zTANDARD TERMINAL ARRIVAL ROUTE (STAR), A6 ~; g7 P. Z6 v. H J2 \1 f
ublished procedure for approaching an airport IFR.
, `/ Z0 w, h( [0 K' n, Y* XTAR, SEE - STANDARD TERMINAL ARRIVAL
/ Y2 {/ d3 j7 y! {: pOUTE
2 `$ U! i) |. {) tTART VALVE, A valve in the engine start system for# \9 ~9 z& A7 ?* ~
upplying air from the pneumatic manifold to the engine
. A ]4 c! @0 M1 Ntarter.
, G" n( t+ |4 a1 ^9 e+ z# gTATIC AIR TEMPERATURE (SAT or OAT), Ambient7 T* v4 ]* l- [, M. u0 K
or outside air temperature.7 V& r5 P$ N/ ^2 `* j D
STATIC PORT, A small hole in the fuselage for sensing. v4 O# L2 a4 s5 I1 d
static pressure for airplane instruments.
4 J \) |6 u) p; p2 sSTATIC PRESSURE, Pressure in the air or fluid at rest
7 k* Z5 @5 c" w1 Umeasured in pounds per square inch.
7 E2 _* }* p9 l7 ~2 T8 zID),
0 L) m' h8 E* T; s6 [) ]用于使用仪表飞行规则离场公布的程序。" i( ~$ A* q+ ^
标准到场航线(STAR),. R* R3 {1 A" D W% z0 \
用于使用仪表飞行规则到场的公布程序。) E+ A- n1 e; d3 k* o& z+ H5 @
标准到场航线,/ w7 v- d; {1 x" w
见Standard Terminal Arrival Route6 T) I; \+ `$ m% S' o* ?
published procedure for departing an airport
( S1 r- D0 f( M! q CS
2 d8 l8 @0 G9 f# Q" M0 w8 Hp
, s# ^) I3 u$ q9 |8 F% YS
4 f' W/ v3 L% p7 oR7 c w1 \ `: u6 L& E6 r* w% `
S
1 g8 w- f. Y2 d+ y% js
0 r8 x V1 }" K6 bs1 h0 l( G6 X* f( `- I
S
' t7 k" V+ V$ m6 e; i" ^标准仪表离场(S
7 u4 c4 B( e5 _5 O2 {7 v.
6 W" U) b3 M( K7 v7 _, H) k起动活门,, C9 M* x! r" h, L' h3 `
发动机起动系统中,用以从气源总管向发动机起动器供
9 Z" H* B$ b1 N- _* n5 T% V的活门。
2 h0 n5 }6 L) e. u( n温(SAT or OAT),
; v; w9 }; Q* t, _: S环境空气或外界空气的温度。) I* m& y0 B- G
压口,
( L; t2 i0 G( \/ w% R位于机身外表,用来为飞机仪表感应静压的小孔。( @0 J. z$ T, X3 T9 x/ J
静压,
- o; ~# _0 }: \; H# @静止状态的空气或液体的压力。用磅/平方英寸来度量。" A/ `: l1 y3 U# d
气
: i: q! {9 ?8 s! m& s# `静5 ^& c6 M' ~* X# j# M
静
2 @/ m3 ]$ ]) y5 W英汉对照民用航空词典B OEING
3 r, Z; d% D0 f& [/ Y4 _! `TECHNICAL DICTIONARY 144, Y- j9 ?: Z1 U9 O7 p# Z
STATION, A vertical reference plane along the fuselage" C% A$ {+ [3 E% D" g
for measurements along the fuselage.7 ?& q& h! A/ P* k* t- M( _
TATOR, The stationary section of the compressor
+ N- ]& f1 E! [9 l2 p* d5 \& U& Setween the compressor stages in the jet engine.
8 [8 a+ P9 _+ l+ l1 ^TEERING ACTUATOR, A hydraulic actuator on the$ j' T7 X0 d/ m' I8 P6 J4 ]3 }
landing gear shock strut for steering (moving) the; u" Z3 y* j: u/ d5 b/ {1 ]8 w7 S
nosewheel left or right.; P h/ c& C1 o$ N* |' b
TEERING TILLER, A hand-operated lever in the
8 k1 t! l; ~- h9 p7 ^osewheel left or
; E/ O9 V7 h5 j% K, i3 ught.: q* ~# O' m% E) Q% a3 l, }# ]
TICK NUDGER, A device to push the control column
' Q7 A1 ?2 z8 `- yrward just before a stall occurs.6 v' O5 g9 Y+ a. N2 C
站位,, g( W$ }- F: a; U% @" Q) Y1 v
用以沿机身方向度量的垂直基准平面。
- a2 V5 a. Z( y0 Y, Y定子,+ @5 M" ~7 z8 k1 p2 q9 z3 b
喷气发动机压气机各级之间的不转动的部份。; t/ X- g5 d% u
弯作动筒,8 F+ {& h7 q$ `& X0 m
减震支柱上,用以使前轮左右转弯的液压; _' p7 {% i: c9 l* C
作动简。6 [( p( M- x# F- y/ v$ g) n+ o
轮转弯手柄,
, H) A" j; k& `8 |6 O! ?! r内用来使前轮左右转弯的手柄。
( @, Q' u' t6 a1 }8 b$ l动推杆器,
8 {( Q' v- B i, n2 X% {在失速前能将驾驶杆向前推的装置。! n; r0 R2 h* P; |6 x9 v0 `
S
R6 F$ j `! eb
2 H( E" d6 }" F5 a) s5 bS
* B' s; E$ D3 c1 u" \S6 i) ^( N* D3 B( t
control cabin for steering (moving) the n
4 E; j: {# Y) g/ Q4 x8 Lri
; U3 s0 K) j- s) ?S- d: q3 W& S$ ]- Y, B
fo
& ]7 U3 ], |4 |; k5 }) V, V0 Y0 J+ [转
1 U: \3 _/ u% D3 Q. H9 [# p一个在起落架( G+ W/ k' T/ b+ I5 }; G
前
* J2 }# u5 }8 v3 t# r驾驶舱
U; e: |: b7 D. r) v; S自" ?9 Q4 J% e; C' e2 o+ F; t
英汉对照民用航空词典B OEING" Z7 W" U% W8 X5 ?2 u
TECHNICAL DICTIONARY 145
" ~) |7 e* r4 ?: S% j6 G5 x+ {- hSTICK SHAKER, An electric motor operated devic
$ z0 m% Z$ s0 U. U9 W T: m q) nthe control column which shakes the column be
: m- A: X5 T5 @8 {) t* c- U! jstall occurs.7 z/ ]! [$ p# c
e on$ Q% C6 v; a ? C. s7 f
fore the
& Q; ?" T' s* ?# [. C) w3 M0 e2 t8 uTOPWAY, An extension beyond the end of the runway
* B, J9 U3 V+ T( B/ u% c% _hich may be used to decelerate the airplane in case of
3 J; v2 v2 ~6 P* h/ }. on aborted takeoff. It cannot be less than runway width
# Z4 m, N* u! U3 x$ c" fand must be strong enough to support the airplane
# h2 z% A6 D* W3 R9 C置。8 `; X* u$ W; W. G% s. p- }% v
速安全道,5 n9 l9 ]/ I: R
跑道两端,可用作在中断起飞时飞机减速的延伸地带。
. Z7 k) t3 f6 L2 I它的宽度不能窄于跑道,硬度也必须能够支持飞机以免结
; @4 {; H8 T& jS
4 g/ b3 B9 E8 [" K% ~' Zw
" a$ i, S* b5 da. Y/ [$ X% |9 |
without structural damage.
* W! P) ]* s1 ]4 r( m l( d- LSTRAIN, Structural material deformed slightly due to the
: r1 N* `* O! p3 [! u$ e& r6 {action and forces of stress.) \" |* d, d& G3 N) A, V
振杆器,2 i& u# ~; V: v* V1 [
驾驶杆上,在飞机失速前使驾驶杆振动的由电马达操4 I" W7 J1 q1 W7 u2 i$ g2 k8 }
作的装
% e3 A5 x# J9 i减
1 c% [6 V0 [0 @5 u& ]7 w( D构损坏。( t0 W4 j+ h. g: {
应变,
' p& \: o/ s9 W L. C2 V因应力作用和受力而轻微变形的结构材料。
' Z; x" R; Q/ @+ s+ A. u英汉对照民用航空词典B OEING
, Y3 `( M3 K$ q3 C+ z; HTECHNICAL DICTIONARY 146: `9 v$ i( k; J7 }: M, ~3 m
STRINGER, Structural components in the fuselage or+ o1 \% ~% y! X+ E
wing for transmitting skin loads to frames or wing ribs./ u* V$ P2 D! b9 t: N
STROBE LIGHT, A high intensity flashing light on the
8 N+ ^! { a; ^. {( `wing tips and empennage.
2 \/ D$ x9 e. J8 v& e( ~4 g3 dSTRUCTURAL MEMBER, The part of an aircraft' p4 T( @: v# c5 g
structure that has been designed and constructed to. [% [, ?; S& n% _
carry and accept loads and stress., ^9 x- ` q) Z; a4 I% x
STRUT, Mechanical components of the landing gear for
( E% l" B2 L% X* p( Ekeeping the gear in the extended position.
1 q+ D; G5 R- b; {% f机身或机翼中,用以将蒙皮载荷传至到隔框或翼肋的结
2 S; j! W+ U: a- t构件。( G" S8 C: {2 I, h/ ?- A z6 E
频闪灯光,$ `3 O: A/ [1 _* r5 s; l( Q7 E; g
位于翼梢和机尾的高强度的闪光灯。4 r+ G7 G' s% K
件, N6 F6 Y4 R- {5 u0 t! e" R
飞机结构的一部份。为运送和承受负载及应力而设计建
6 e' V, ~4 R% l: g, c成。! T7 h6 W- S3 {4 ?5 G3 w0 k! w
支柱,
% m5 E. l& K* R# F* @0 `2 b起落架上用以使起落架保持在伸出位置的机械式部件。5 _% n7 |, U$ r
长桁,
/ F* f# |; T6 r3 h. d7 U' Y4 Y构; D4 d- {3 f) z, d. h: M# l# g- r4 s; H. i
造 t% q7 F' b- `3 Q# q
英汉对照民用航空词典B OEING
; V1 y$ F0 Y& \. p; sTECHNICAL DICTIONARY 147
( e% `# h) B! P1 FSUMMATION UNIT, An electronic component for
4 x! o% Q1 Q% @0 l- Eadding fuel quantities in all tanks sending a signal to the) |( }) C' ]$ y
tal fuel quantity display.6 T: e% x; \% C# `# |' A
UMP, A lowest point in the engine oil system or fuel* U0 w+ U, S9 Z2 }% @
nk.
" G* [" _4 Q/ A% R" T7 k' sUPPLEMENTAL DATA, Additional data stored in the' [# M& F/ O; |
MC memory, supplementing the loaded navigation' a5 E3 j: x; H- S' r
ata base.
* `! U4 T# w" _ y- G z: T& S& `3 Un
6 x3 y) c. [8 B' Z8 {; u& [) k* d/ Feviating from normal modes.3 J0 q- { R1 s4 G3 r
SURGE, A sudden change in the airflow through the5 g6 {4 u! s1 A- A7 @
the compressor not being able
# o+ @2 O# N& z5 P4 {+ j" C. ^compress the airflow.
6 r$ D4 G$ N9 NSWAGE, To squeeze together two or more items to C; ]3 J5 X2 E8 P2 V2 d' v+ u3 B
form a permanent unit. Example: a lead or steel piece" R- k/ j. o+ I- v: [: u
on a cable which forms a stop or camlike unit. Also to$ X# ]# X1 S. x0 A C5 @0 u# d
reduce the diameter of tubing.: w" M% F% T. C& r9 W H6 Q- ~# B
SWITCH, A device which changes the condition of an4 }, D- v2 {0 @0 \- h; a' ~
electrical system from on/off or open/close.9 x* c# O& N% b, e. K
燃油总和器,
. \$ l8 S3 p; Y将所有燃油箱内的燃油量相加,并将总油量用信号传至9 C4 @4 T V& e
量显示器的电子部件。1 S! x4 {6 }3 _' a
集油槽,& ]& ?6 {- F9 C0 {, Z- `
发动机滑油系统内,或燃油箱内的最低点。
2 o6 g: X8 d8 U" e! s增补数据,2 V G+ o; y; i0 B- b6 S" \( V
飞行管理计算机存储器中的附加数据。用于补充导航数
/ A$ X3 H' X3 a1 R据库。
p9 B6 C# s; V8 C! t, _- e& Y& d,
$ C, q. ~( { {1 Q% C$ {) z附加的数字飞行控制系统方式,当偏离正常方式时使
* S! ~) p' C. ~1 ^. ^0 j( y4 N。
* f1 W7 |8 w! b2 o- R5 W过发动机的压气机的气流的突然改变,而导致# H' j( x5 \# y1 F1 v- E
气机不能压缩空气的现象。
' C8 k* Y2 ]. I1 ]. B0 |6 t陷型模,
2 O3 E" k' K1 ?! ^9 @2 ]- h挤压两件或两件以上的物体来制造一件永久性的元件。
( J9 x+ A# v7 K如:一块铅或钢在钢索上形成一个止动器或凸轮之类的4 T: n' M% s) S) m0 j6 e' ]
件。也可作减小管道的直径之用。
- z1 r, v- V' y开关;
4 T6 W* N$ m# r1 [! u( Q5 ]改变电气系统通/断或开/关的装置。
% b; B7 H! C! G: Q0 sto4 X* l4 H" N( M0 ?
S% U' N C/ ]& G) n
ta
6 y. m+ k, g8 q4 _+ KS* v$ F' b$ F) `( K% N
F
& {, d; X; Z- Od2 N( |5 ^+ a4 B+ N3 c- B6 X
SUPPLEMENTARY MODES, Additional digital flight) x6 _4 T6 j% h! Y
control system modes that are available, used whe
1 M- {* E9 _1 Z. K" Fd
4 R# G4 L+ I6 ?* D5 j7 @, bcompressor resulting in
/ y& Z# S% l5 P/ l& v' c# wto
- Q1 F- y7 `- o' l6 M6 d* a油9 H8 I" Q, d8 C; Z: E; Y
辅助方式2 A. g5 F" b. m7 ? ?8 Z* N
用* t1 ?* M- e3 I
喘振,1 X% [$ |" Y; U* D: @; J
由于通) C# }3 i4 G4 W5 \
压
# M4 S+ a3 k* O3 ?& K& K" n! M5 L例; S2 Y1 m' o: I2 d! Q
元
* z ~( T; T1 S* P英汉对照民用航空词典B OEING
( U% { @: _2 a7 W: i- hTECHNICAL DICTIONARY 148$ j$ M4 w" m3 |. {) M& X
SWIVEL, A device for rotation of components.
$ J& O; X2 D5 t: c. e5 E& X3 p G# sSWIVEL COUPLING, A junction in hydraulic7 X5 {9 j- a: o5 B5 C/ Z
bes for allowing component movement.4 H* q" z! ]$ f
YMBOL, A graphic view of an aircraft component in a
/ ~7 S( M1 s0 L& T, B; \% u4 |ery simplified format. Used on drawings to represent& f7 R4 j, b U2 H8 I J5 N
e entire component.
* Z( z& @0 \8 RSYMBOL GENERATOR, Generates the video signals7 J. n2 {; _3 P/ R* v2 y# \+ t
that are displayed on the EADI and the EHSI.
1 e- e1 `% `/ {3 s# |SYNCHRONIZER, A device or circuit to make the units
4 ~, p- h2 m6 Q3 [3 yperate in unison.7 M/ {1 z5 X# r* A4 i" V
SYNCHRONOUS, Refers to two or more things which! o1 Q: t6 M; y5 a6 i
happen in a system at the same time.' b- B& }. w- a0 ^+ @+ h
用以使部件旋转的装置。* ~ P' v( ~4 D; }) a* d( _
转动接头,' D. E; @4 l; G3 _7 d: q' B
液压管线上,使相邻的液压管能够动的接头。0 f' x4 r$ J* d- e
符号,8 B/ L7 B; U) m& L# _
飞机部件的简单示意图。用于绘图以代表部件的整个结
- y" x# y$ e) Z) s* y( |构。; P! X' V9 ?7 D9 S
符号发生器,
7 s9 v8 y7 T9 l$ {2 y为姿态指引仪和航道罗盘产生图象信号的装置。
: a9 j& J' I+ x9 v/ S- A& {( Y同步器,
: x* B' d9 i! M& E. p8 ?( \使元件操作协调一致的装置或电路。
5 {0 H7 G7 ~$ ], i. l$ ]两个以上的东西同时在一个系统中发生。- Z$ O' U# V( @: f- r2 g
tu1 o% B( Z( t* i; ^1 g- m
S
$ r# ~3 a; J- O- Bv
* j( f6 ^1 w( h+ E: R' X# C7 Vth
. B n+ `" v6 n1 o5 g; v0 A4 L7 s0 lo& [. K' k' Y( Y' c7 o
转座,# N: b( M# |7 E6 a, U$ y# ^
同步,
( i( ^+ T+ ?3 b9 I指两个或
+ t ]: }. Y7 P7 q. q3 t- D" H英汉对照民用航空词典B OEING
/ F4 g: C! P0 W# R: pTECHNICAL DICTIONARY 149: |# ~$ _3 l# n
T
: U" c- G/ [, @% ?AB, A small, hinged, moveable part on the trailing
# }) y3 Y8 B9 ~1 d3 ^dge of a control surface (aileron, elevator, rudder).
' c& t" d0 ?: Z5 ^Balance or control tab - moves in an opposite
( p# A! k2 v$ o t2 B: tdirection to the control surface for assisting
. y/ M" T ~1 Win movement of the control surface.
, @) K, S+ D. LTrim tab - provides controlled deflection of ailerons
( c, \& \. h9 m6 h0 t' w# a$ \2 f/ Sor rudder to compensate for imbalance in1 V. e# v0 ?7 {6 Y1 R9 b+ a# j" S
thrust or fuel quantity.
0 s7 A* H% X( U- g! rStabilizer trim - controlled deflection of the horizontal
6 Z2 V9 o# A7 A: G1 K# D9 q1 Rcy
{# C+ l3 w) o" x0 Nproportional to the speed of rotation.
% x! K" c& b) j& F) kTAI, SEE -THERMAL ANTI-ICING0 O# }3 v7 |. U+ M' O
TAIL PIPE, Duct at the back of the engine exhaust.
! U4 ^& v! w, m" T R }8 W7 S9 oTAIL WIND, The wind component relative to the: k3 W0 F! r/ \7 ?" P
airplane direction and coming from behind the airplane.
4 ?. B. ]% W: v! l调整片,
( G/ [& B) P4 o! S. S' q" O& ]; ^铰接在操纵面(副翼、升降舵、方向舵)后缘的可动小- L5 ]! Q& t3 B! ~: h2 L; ]
部件。 l8 b2 q) f; Q9 M
平衡或操纵调整片—与操纵面运动方向相反,用以帮
2 E7 Y4 w4 T7 z助操纵面运动。
9 x ?. D. e ?配平调整片—使副翼或方向舵作控制之下的偏转,以
- ?( r/ _/ n% G5 P- P3 H8 {补偿推力,或燃油量的不平衡。
) @8 _1 E, D0 U* s g安定面配平—使水平安定面作控制之下的偏转,以减
9 [" S7 s5 T4 |, [$ u: l# H2 \少操纵力。
' O5 t. @6 ?/ g) P4 V& H3 S机,
6 e$ r1 _7 t9 J/ K提供频率与转速成比例的电流的小发电机。
' B) ]% f( x# I9 i: }热防冰,: o5 H2 o) ^6 t6 Z
见Thermal Anti-Icing
% X- o6 \# ]. @" J% e& F( y# NT
$ Q" D" q6 P* o6 [; ge0 M. D5 o* B. ~$ g; r* v
stabilizer to reduce control force.
) Y4 G. u- l5 n. `+ ATACHOMETER GENERATOR, A small electric' H) d& e: b, D8 J1 p3 n: r) h4 J- p L
generator for supplying current at a frequen/ | Q- y3 g% x9 a* P9 X/ P6 w
测速发电1 @! L6 l3 r5 S: d4 p
.
; Q/ I5 T' _" R( P- K尾管,
* p- x1 [1 ?( N" U/ ^5 [% [发动机排气管后部,用以排出发动机的废气的管道。
G$ f8 N9 b7 i4 j4 ]顺风,
5 J) a6 i. _2 J- y& L飞机后方的来风在飞行方向上的分量。9 t' p; }! t: Z4 O: b! i" i/ _
英汉对照民用航空词典B OEING8 S( R+ l' ]3 w& l/ s
TECHNICAL DICTIONARY 150- j- N3 p. }; x8 ^) x; ]! K
TAKEOFF ANALYSIS, Analysis that evaluates the
, E$ Q- c2 C+ n1 @6 [airplane takeoff performance capability for a variety of
* i7 s3 q" u3 P, A- k4 l/ ~( o2 e) henvironmental factors at a given runway and airport.+ L! I, y, s' }9 U% I2 {! ]; B
ET PARAMETER, A specific goal such as
! w6 n* m# G6 ~7 x' Lirspeed, thrust, engine speed, altitude, temperature, or9 S: e3 f6 E. g2 q7 m
te of climb which is to be achieved.$ T6 c2 r& Y- Y1 N6 q
ASK TICKET, A computer label used for tracking the5 p8 O* B: L% f- d
ompletion of a task.
1 z2 ~; i4 ]* Z5 [( L2 YRATURE
' v+ M8 Q7 t+ p+ jAXI FUEL, Fuel burned from the time the engines are
* d' ?$ h& [) y8 u1 Mr.
3 I) N, b; |: O% c* s9 @CAS, SEE -TRAFFIC ALERT AND COLLISION
; R" u) d( e9 T+ o( v" BVOIDANCE SYSTEM' ?/ K6 B7 w7 n2 w% ~; Z- b( l
欲达到的特定目标,如空速、推力、发动机转速、高度、( f, C( c9 [+ j0 Q
度或爬升率等。
& K5 T. F, a# j3 R: L( l( o5 \工作记录单,' W7 @- {+ J0 `* C$ `9 W; [
用于追踪工作完成情况的电脑记录单。
5 o: `7 c& t% C$ f# n- X! {全温,
% h7 M ?, c, n: @ h: d& [ `, C见Total Air Temperature- G+ A- ?8 ]) E4 I4 M) g
TARG
. M( f& v$ d% ca: Q/ U0 G% I5 x9 Z% X, I
ra
" M# U9 Q/ ~: D# b% A' E: }T8 O' x& X1 R' G' A: x W. n. y' Y' N
c, j: S* j/ K3 S7 L
TAT, SEE - TOTAL AIR TEMPE9 n5 e2 X; L P( z" c" I2 B
TAXI, Movement of airplane on the ground using
( H4 c" p# _3 w' W0 h& ^% T& Fairplane engine power.0 C. ^& k' c0 F) C+ e3 Z
T
- t v. D6 w. E" Xstarted until the airplane begins the takeoff maneuve0 L: G# `1 W3 n3 {6 e& I- T
T2 d. R$ J8 W& i* ^. i
A
6 \/ r% m3 Y1 I* E& @9 u起飞分析,
' }% a# B/ p5 k& q7 X% A对飞机在一个给定的机场和跑道,在各种环境状况下的
3 V1 w0 k. }, P. T" d起飞性能能力的评估。
/ _" [$ B+ r3 ]- _目标参数,9 ]: b$ s7 I' ^! Q1 p
温0 Y7 `) F( q1 a( z. c/ }# H
·
5 ]: }3 S/ U( N5 U* Y o滑行,2 I. `6 \& O/ c5 ~
行燃油,2 d! Y4 _- b+ L. ^/ z% w: x
起动,到飞机开始作起飞动作之间,所消耗的
5 [; i" M4 }& ~4 Y7 y& x中交通警告与防撞系统,
. d5 O+ S1 l+ d. b4 R$ n+ r+ z见Traffic Alert and Collision Avoidance System
2 k9 n/ m: X/ x飞机凭借发动机推力在地面的运动。# |# d' s+ z. M4 w
滑
3 e9 b7 T9 u+ b) Y2 V/ e8 d从发动机
4 t& S: K/ g2 x' K# z燃油。/ a: t L6 H% t+ Q2 s" \/ s6 v0 z4 N
空
* I1 o/ c" Q; Y$ ~$ V.
6 P0 r* n9 v- G8 T( k' [8 ~, t英汉对照民用航空词典B OEING
% F' _+ U0 E3 {3 {% I& ATECHNICAL DICTIONARY 151
! e1 d8 \& b) M0 {TCC, SEE - TURBINE CASE COOLING
( R9 X: D2 T7 ~3 {EE, A pipe or tube connector manufactured in the! b* O' R8 ^3 Z( ]! b& J* ~' O
EFLON, A synthetic material for hydraulic and
' [$ |. b+ r9 v8 vneumatic seals.
$ X4 J0 n0 {1 _EMPERATURE INDICATION STRIP, Temperature) m2 F" K% l, x6 k; Q
ensitive tape which changes color at high temperature
: H# J# F! K+ A0 cr indicating component exposure to high
! g; n! U) c2 k# B c8 b$ V8 uTEMPERATURE INVERSION, An atmospheric
$ w3 Q1 A* b: Y1 ~7 A9 gcondition which causes the outside temperature to2 ?9 t! }5 ?( E# T9 [, j2 M8 _% i6 z
increase as the airplane altitude increases.
, b, v Z& ~* ]! }; b) ? kTENSIOMETER, An instrument used to measure the$ m P$ I8 c% c" C2 [7 O
tension applied to aircraft control cables.' T4 w/ j$ g- u3 F. e) u
冷却,
; w! g3 o3 V- W3 N$ BT6 l9 W% x- l- G3 ^
shape of a T
3 R- w l2 M; ]T
: o* ]( C" I* b; jp
: o6 G2 G4 Q! d( f3 fT
2 c, _7 ~$ Z6 t; t6 [0 y* cs2 b6 a3 N+ Q* U& Q6 [2 t3 K
fo
5 p, m7 d1 B) _: Ttemperatures.
7 I, n, d$ c; I! D$ w6 [. h涡轮机匣
1 j7 [' G( r4 s: ]% A# o见Turbine Case Cooling.
4 b; }4 Q1 T Z5 @1 q9 ~! b字接头,$ H5 Y* D- u" ^8 q
的管道连接器。
/ f( O& l0 \6 T# A6 @7 E氟隆,1 R3 `' t0 |1 ~" X
用于制造液压和气源封严的一种人工合成材料。: ^4 c9 A/ K$ Y y/ u3 ]& a5 d- t
度指示带,/ [3 h5 U+ @( [$ w; D$ e
遇高温变色,以指示部件周围高温的热敏带。
4 `; W' z( u4 R& p8 b; \逆温,
: Q! Y' l( V- i1 c& @! q6 z一种大气状态,引起外界温度随飞机高度增加而增加。
/ `3 ?: z2 R- C5 r: \$ |+ q7 o$ y张力计;
8 ]% p( z4 t6 G F: R: W+ c用于测量飞机操纵钢索上受到的张力的一种仪表。
8 ~, r9 ]) G: X; m+ c6 RT. G7 z& t' }4 q+ x5 E
制成T字形
! F: K4 }6 s; {$ i% }$ D5 w2 k" E; W泰; a8 G+ D9 Q1 v# D q1 c9 R4 p( i- I& }
温( p5 B! t* O2 n+ U3 x/ a
英汉对照民用航空词典B OEING- W1 l1 K* U0 v) N& X) V
TECHNICAL DICTIONARY 1524 d) W, x- P( Q4 N" L m
THERM
# B& q0 F; C# r5 E0 u d/ b0 \; Hformatio
' v3 R: g" m1 `. J0 v0 S* H9 ?% X8 fusing ho4 r+ ^% m0 r1 c8 u# c! v
AL ANTI-ICING, A method of preventing ice+ o/ W1 B3 U% }
n on the nose cowl and wing leading edges by
8 O, g. q8 ~6 Z At air.
. N8 g5 k$ \' b j" l/ v* s) s4 \THERMAL t
9 u( N: r4 E/ f: jin a tube fo en tube
6 U: M. V! Q, S( [+ wis pressurized with oxygen.7 Z% E# F9 j$ O
HERMAL RELIEF VALVE, A valve which opens to% j9 `2 `: k4 J7 Y6 \9 R6 l: H
ture.
1 ~/ {) ^: @5 B' q' WHERMAL SWITCH, SEE -THERMOSTATIC SWITCH2 H; }" E+ P9 t. l$ D5 B2 p
e
" g( P2 v1 I1 u2 Psistance changes with a change in temperature.) F5 Y4 T! f, P
防冰,
- Q% v( x9 B& V0 c9 |用热空气防止发动机前整流罩和机翼前缘结冰的方法。
! y1 {% P; u/ y6 a5 Y- m在管子里,使管子受氧气充压时温度不致于上升的一; W% Z2 j3 r2 U& x
个刷子形导线元件。& Y& m0 M2 t! A, n( u. X
控释压活门,
; v+ O7 i7 s& C1 b# e( a过高而打开,以减低流体压力的活门。
% o3 I q( \8 \6 E电门,# p6 K: d. q5 f4 W& N" G3 U
见Thermostatic Switch+ s$ Z( Y j' P( V
COMPENSATOR, A brush-like wire elemen9 Q3 H* i2 N3 X
r preventing temperature increase wh
% O. P: \* u% ^& ]- S" L8 WT+ E' \8 R( j; l1 F) k" k, ^
decrease fluid pressure due to high fluid tempera9 i1 P9 n z9 m0 H! \1 x+ U, e
T) ^' U" d0 F: {. I
THERMISTOR, A temperature sensitive resistor whos
% _! p! ^! \& V2 c& r9 jre4 Z9 X9 _ P" o2 q
热9 I6 Q- C& Q8 Q ^. @
热补偿器,
% ^5 M) }( \9 ~装
& ?, H% C. Z* T j% }: O W* s& t- k热$ R7 v; ?# d; X: s* v
因为流体温度
& F6 [+ G1 z# e, ^热0 {: O3 ?- x" }8 a5 W1 ?+ Z) {6 m
. q9 j- `5 p( h! g W- s3 P
,热敏电阻* ]! D3 y+ g+ a) ]
一种电阻值随温度的变化而变化的对温度敏感的电阻。) b! L, C* o3 h: @ R
英汉对照民用航空词典B OEING( g, L# |1 J: R- l
TECHNICAL DICTIONARY 153
1 |" F' O2 A2 c$ o! Y qTHERMOCOUPLE, Two different metal wires joined at
/ w9 ^; d, c z5 S; u' H# ]urrent is produced proportional to the temperature) |) r) }7 ?, s0 p( z4 f- [4 S
difference.) A" z2 w( n2 {9 N
THERMOSTAT, A component set to operate at a: g) R+ c# ?; q+ j# X
efinite temperature for controlling electric circuits and" B. V8 o- {$ J' O4 b$ a7 a
alves.
& B0 _: U$ Z5 zmperature sensitive switch which opens at a preset7 B& i' k3 g! C% B2 Z7 c
mperature.
+ p* s, z+ i' lTHR HOLD, SEE -THROTTLE HOLD2 U4 |$ V1 w3 h ?( [
即产生与温差成比例的电流。
: w: W# f" G) J% m3 d' s用来在一定温度下操作,以控制电路和活门的部件。
, r2 I& I+ a# ^$ }" S恒温电门,6 }" c2 {: y1 G: Q3 @* \& W
一个热控的、在预定温度断开的热敏电门。$ |7 d% [5 }4 s" T5 `
见Throttle Hold
: c7 ]0 o: `7 f1 [* a$ g8 [both ends for temperature measurement. When both$ c Y! [& B4 M" ]
junctions are at different temperatures, an electric/ F4 k9 i5 |3 }& a- ~7 g* Y
c6 {6 O2 E/ w' c/ {9 D
d
. f4 h) d! z, n9 F) nv
- s/ t) h" f6 @1 PTHERMOSTATIC SWITCH, A heat controlled,
6 z: c! |7 l2 i9 f9 kte" s6 s8 n7 b5 K! e1 d+ W
te
+ p6 p! f. S0 l8 R! M热电偶,: x, l' }( D$ q d+ A- w0 l+ ]- X
用来量取温度,两端相连的两根不同金属导线。当两端
/ N, F4 f; Z A之间有温差时,金属丝内
' r. c. B! d0 q y恒温器,& U( I7 N% v' [- F% r. H3 [
油门保持,
+ W5 o9 Q. ?. L! e: t1 M' f( I- U.
# e1 G( b2 F' b" W- ~英汉对照民用航空词典B OEING
. N9 f( `9 w( t4 V3 t2 V' aTECHNICAL DICTIONARY 154
8 L4 V3 i2 T) \) sTHRESHOLD (NO. 1), The bottom part of an opening in: `! f2 ]2 n w9 K& Q9 N6 E
a fuselage doorway.
' D% j3 W. L2 U2 w& i. 2), The approach end of the runway.- q/ G, D+ y9 |; |
THROTTLE LEVER ANGLE, Angle of throttle lever
8 g* X: P3 o5 g$ n. C4 S7 U0 o" pdisplacement.
6 \/ R/ p0 C1 H, v% v( iHROTTLE SPLIT, An engine control condition in which* x8 _% T- g6 T! f" a! [% v) O
the throttle lever angle is different between throttle
2 ^2 [2 U: Z% K- x: Dlevers but the engine thrusts are the same.; a/ x1 m( r k' K6 \# \
HROTTLE VALVE, A valve in the fuel control unit for
' ?2 h0 L0 c2 T) t5 Echeduling fuel flow to the engine.* ^7 I! [, m# s* }1 ?, w& L
机场跑道到场的一端。
, N; m( w9 G4 O2 f4 d. ?# O油门杆角度,
- c: \2 k+ Y4 {" i4 p9 y: h# }油门杆手柄位移的角度。( ~3 L- L8 n w; x6 a9 D
油门分叉,
7 ?" J! c6 i1 p8 I& m) R一种发动机控制状态。在这种状态下,油门杆之间的油/ h! P/ j b2 I* b
门杆角度不同,但发动机推力相同。
/ Y8 b) ^# D* ]! J+ g$ Z9 U流活门,0 y0 B/ u ^7 e1 N* X* [
燃油控制组件中,用以排定燃油流量的活门。6 z% Z' y0 t5 M3 o6 c
THRESHOLD (NO5 S, n ^9 Y2 b% H, }
THROTTLE HOLD, A mode of the autothrottle where; X6 n% e/ Q; U2 F
the thrust levers remain where placed.
! [, h# L4 t$ xT; J/ \8 ^" q) q8 t( G3 c
T6 ?5 t- [( w1 ?* z2 m4 ?5 x5 P
s
0 c) E) ^, L" h$ [7 D# D2 i门槛,; t6 X; Z* R" _$ }7 H3 M
机身舱门开口的底部。7 d% A9 E. i1 f+ l3 \
跑道头,
/ Q+ y1 p. ^3 W, p+ L# Q3 } |' H1 n油门保持,2 M3 B2 F" N8 C6 I" h
自动油门的推力手柄不改变位置的方式。
# C2 N/ o* K5 U' ?0 K节
( L( m( L8 w4 N' _2 R! X) U英汉对照民用航空词典B OEING
4 I# o7 L4 ~8 E- P3 H' GTECHNICAL DICTIONARY 155
- ^( j$ x. X6 V FTHRUST, The driving force produced by a jet engine.! e* u- i, Y6 ^
HRUST LIMIT, Maximum allowable thrust for a specific i; E$ B( |5 f# O0 s9 I
et of conditions.
' Z6 G8 k* ?2 Y+ `HRUST MODE ANNUNCIATOR, A display unit or part
6 X& T& d; h: z4 y5 Mf a display that shows the engine thrust mode.; N. b" T/ d$ A; x$ f
HRUST REVERSER, A mechanical device located in, w, z) ]- k9 ~. U; G
e fan or exhaust section of the engine for eliminating5 }# }& S, m2 A6 C. V( V+ h
rward thrust by deflecting fan air or exhaust gasses in
- T! I: p9 I& P1 o" w5 s z He forward direction can be used for stopping during; ]: l5 J% t! N- a9 s# P
landing and during an RTO.8 X6 S# J( C2 A% T5 ]
推力,
+ X1 L- K3 M2 c% }9 Z9 R力极限,) w% m6 G! [' Z, q* B8 f" Y6 d9 Y
在一组特定的状况下,发动机的最大允许推力。
$ e. c8 w$ d F3 s推力方式信号牌, O, w2 \ H- _. U
显示发动机推力方式的显示器或显示器的一部份。
$ D- f" `8 j- o6 V/ e. @反推装置,
+ }' v, O, X9 I* ]' i7 @7 y( V/ t# o位于发动机的风扇段或排气段的机械装置。该装置通过* U) Q& J8 E) S% P4 X% r) @0 V! b1 B
使风扇空气或排出之废气冲向前方,以消除发动机向前的* ~: o( }' j# P1 `
推力,并减短飞机在着陆或中断起飞时的制动距离。
% `9 f( x1 O& l$ A% B0 {* cT( N7 U1 L) F Y1 b& n7 q
s, E- @+ p$ J. l, \
T
* v$ X1 q- D) n: p) po
" u; d, D. C( A2 [3 w) X3 J! jT. l$ o5 N; s/ N$ F1 Q5 Z
th
! m1 Z' A# J2 ~9 N7 Tfo
, k$ Q- ?3 X; A/ i* ~2 {* S3 Jth: H, \) _6 p$ y `, @& m
喷气发动机的驱动力。
& k: z! r2 S3 z& @! O+ t1 u( ~推9 a) L- e9 P; w. W! j- L9 A5 I
英汉对照民用航空词典B OEING
9 r% c* r$ L! w* @- L$ J* l& cTECHNICAL DICTIONARY 156
; Z0 q5 q5 c E! F+ x; kTHRUST REVERSER COWL, A cover around the thrust
6 f8 a" v7 ^( `$ o t; A) BIME DELAY, An electrical circuit for starting/stopping
! L6 S; O8 W4 u5 q, _e flow of electric current to an operating component" X* y& N: x3 ?! r( V- p% t
r a period of time/after a period of time.
0 \( p H% f( Q$ ^9 G6 GIRE SPEED LIMIT WEIGHT, The maximum weight
~. E c* W7 p3 t, O4 F8 a: i9 ppermitted at takeoff that results in a liftoff speed equal to
: l0 j8 J/ o# v, Re rated tire speed., T4 l1 B3 }, q K0 l @
OLERANCE, The part of a specific measurement that
: I1 _2 x: X7 Lallowed to vary in dimension. Usually given in a plus
9 j" W0 X# O* e/ M( F8 n* a) p7 Y6 V) or minus (-) format.0 S& d4 _% B7 `# p( z K4 c
CLIMB, The point at which the airplane
$ x$ I/ z4 P% ?' i9 u" L$ O& breaches the cruise altitude.: i& G1 v' U& E
ts the cruise altitude and begins to" u/ G, Y5 [4 j5 o' c
descend.9 ]: u1 w# [0 ? E" s' h- M
for transmitting
+ }# H/ P' s4 y6 j! D3 Ntwisting motion to the control surfaces.
5 `3 R, P( C; W9 d,
0 y( t& z6 R" O3 d% B: C的3 l# E& w, d6 k# u
部件以进行维护。4 G& V9 E) v% l
延时电路,
. A1 b% o9 _! j$ w- ~4 i用以起动/阻止电流在某一段时间内后进人工作部件
/ v5 M# `% w( d) [3 U的电路。
2 @" Q% D; j8 q6 S: e% S轮胎速度限重,
2 |5 `& `, A# R4 J, J5 w8 o! m: u飞机起飞时,使离地速度和额定的轮胎速度相同的允许: Z; v+ V. A$ t% w% v* A
最大重量。6 X& W% ^, v" Z
公差,
T; d9 G0 O, |, R, P" y! r& Q: U特定量度容许有偏差的部份。通常以(+)或(-)2 H8 E' R7 t5 Z: h9 [/ P5 ?
的形式表示。% l _# R4 R( x% G1 S" n
爬升顶点,2 a, `2 j5 e3 |3 M+ g7 U; _; _* _: U
飞机达到巡航高度开始平飞的那一点。7 s: D. A' m7 C& @( r! h# n
下降起始点(TOP),
+ t% M- b: M' ^. E/ i" B1 ^! k飞机飞离巡航高度而开始下降的那一点。
# [% X! }- X% m% Z2 w. h操纵面的管状部件。0 }/ f; j- O# S: p+ X4 G
reverser of the engine that can be opened to access
; _ ?! y/ h" _# u% X* Ecomponents for maintenance.
, E$ X% O4 M- a: A# X% F8 NT
* a* W( S( P$ r( U% Oth
0 `6 |. e& A( J+ }fo4 Q i. W+ w' e! ~+ b9 K7 g
T
! t6 s2 {* S6 N( `5 N9 {' yth
; d8 f, e. V$ u0 ?: }% K) j" P% H- oT
0 S( v, V5 B. t3 l. |! S3 \, {is
& t! _4 f9 o; o% j2 o(+
8 F3 ^% x3 {" Q! Q5 P( F; STOP OF; P" m T$ j* B( J# o1 K |7 t
TOP OF DESCENT (TOP), The point at which the
8 H1 v9 J7 e6 D" \/ I- W7 X0 sairplane depar+ S _6 Z5 D7 D; o6 d3 G) B
TORQUE TUBE, A tubular component
7 U! o9 `" ^, i) ]% y反推整流罩
2 O! q. J+ V- W2 M% {在发动机反推装置外围的罩子。取下后可以够到内部8 _% U9 @0 ] _
扭力管,
- ]; X3 H7 P7 U' J' `; I1 O- @% @用以将扭转运动传给3 j; I7 V( h" L
英汉对照民用航空词典B OEING$ A, D X7 s# I/ A/ P, O; z
TECHNICAL DICTIONARY 157
- [( p6 M B- S: _TORSION, Twisting of a material or part caused by
: ]$ R2 |' s$ D2 J' Wexternal stress.
) u' N5 m9 C( n1 L4 D/ xORSION LINK, A hinged linkage connecting the inner: C& e+ D* A% u6 x' T
nd outer cylinders of a shock strut.4 ]6 O+ @5 B3 }7 M W2 E1 X
due to the ram
. q4 `& |! @9 J. U2 Yffect of high speed flight.2 {7 K; n% t+ O+ B* g
URE, Pressure higher than ambient+ t$ S+ S% B( _& ]4 N& C
ressure due to air flow, measured in pounds per
/ y: V6 s e3 M$ nquare inch (psi).
+ M. O3 l2 h' \/ Yer than: m' `0 J! M9 J3 g& J
mbient temperature due to the compression of air flow,9 X/ k% D: T/ |) @1 Q4 c, o% X
easured in degrees Celsius (C), or degrees' c' l* C1 S: {0 x& o8 ?% c$ C
ahrenheit (F).
- a, A2 z9 G Z$ _/ fTOUCHDOWN, The point at which an aircraft first
7 P! `# l, E% B9 I: lmakes contact with the runway.
' o' u! D/ H2 f1 u: ?) q生的扭转。9 S) V$ m- \- [. e
扭力臂,
, ^/ R5 f+ E7 S! z9 T减震支柱的内筒与外筒之间,用以防止活塞旋转的铰链% W3 f2 H- s7 `
连杆。
h0 E5 D* G: D; b# o的冲击效应 ^ K! O# Y$ s3 W1 N) i$ |0 O
引起的温度的升高的总和。5 S$ Y- I- K6 |. I
总压,
( c2 D+ q0 J- v, ]5 Q9 Z' L由于空气流动而高于环境压力的压力。常用磅/平方英4 O/ u. y+ `* ]8 V! b0 H
(psi)来度量。
! u$ Y: y. b; Q; b( o全温,
1 ~. i! ~- j: \1 N2 z( U, x由于气流的压缩而高于环境温度的空气温度。用摄氏
( t) x3 Y' d$ v9 \(°C)或华氏(°F)来量度。
8 d% z# T/ V3 |5 a9 K6 S接地,
9 I5 y' x4 U3 I飞机降落时,飞机最先接触跑道的一刻。
9 w$ m9 q0 h! h8 aT+ l) G/ l# m/ y' ]0 F" o7 m4 j
a1 J5 n0 f1 c/ ?; h5 ~
TOTAL AIR TEMPERATURE, Ambient or static air& l* ~) H6 J: q2 d4 c0 J" j1 `
temperature plus the rise of temperature
* P7 `7 v! O, v$ I, O" qe
4 \) _, [7 n1 n9 NTOTAL PRESS8 @* U( P4 \, D! {3 l. M
p2 `5 I B' `' v( q
s" X; Q E/ `6 E P0 E8 E9 t$ q
TOTAL TEMPERATURE, Temperature high# E% Y' v9 b5 r& M" ]2 W( d, }
a
) r* B7 p" S \% F; R% rm
) {. n2 V2 o2 TF* y2 j/ f1 I: @% C7 m8 i3 l5 f' f* Q
扭曲,
$ k4 [* l! u g F物体受外应力的作用所产% ^& U7 y) }6 J. e$ _; T
空气全温,+ I: H) z- I9 K, E& ?; O# c
环境温度或静空气的温度,和由于高速飞行
4 w( W% S, K& Z7 H2 {( B; M而1 Z! _9 s/ k& x$ {2 P l
寸
- J- r/ g4 P2 R6 @' F2 E英汉对照民用航空词典B OEING" A- q+ I0 _& _& z3 \
TECHNICAL DICTIONARY 1585 x0 U0 X! ^9 x9 {3 {* j
TOUCHDOWN ZONE ELEVATION (TDZE), The
; m+ P1 E' p# G3 o7 o" ?highest elevation in the first 3,000 feet of the landing
# o, T% h5 d1 L2 d, q! s0 _urface.
, H% h* G2 g( E5 ~" Yrt of nose or main landing gear for& ]* Q! g( V) q# \9 m
ttaching a tow bar to move the airplane on the ground.
/ r% ?; }% [0 I* o: u6 F$ I5 Balong.1 J. T# n( l" d, e; o( C g V
RACK (NO. 2), A navigation term that describes the5 X- w( j) H3 Z1 a; _
TRAFFIC ALERT AND COLLISION AVOIDANCE
% H2 E0 r# ^1 \( a& C3 V+ pSYSTEM, A system designed to alert the flight crew to4 O% m+ _' S; ^4 D8 A2 Z x W
potential conflicts with other transponder equipped/ G g4 x# }" ]" |+ w# s ]% P
airplanes flying in the same area.# A) _$ T6 e; s# u7 e8 |
TRAILING EDGE, The rear edge of a wing, stabilizer or4 ]2 h9 }) S$ l6 L
control surface.
7 ?; G) N4 z# pTRANSDUCER, An electrical device that either takes1 d! p8 G, V5 F6 V0 ^9 J( C
electrical energy and changes it into mechanical
9 j5 a/ d$ R* V; p0 e" w0 \# zmovement, or mechanical movement and changes it
/ M- E& y- W" s5 Minto electrical energy.
4 g4 ^; W/ m5 J# qTRANSFER GEARBOX, SEE - ANGLE GEARBOX/ D9 v/ h6 G% i, e. m
高(TDZE),
+ v* R( v9 B: N. v高标高。# \- h$ ^& Z7 x$ w3 B
前起落架或主起落架上,用以接上牵引杆以便在地面上, P2 m S, L* F* a9 ]; q4 K6 F
动飞机的部份。
8 Y! p x& i! E9 ]3 z9 u0 U轨条,) y1 m3 L5 f+ \/ [; {, g0 B
迹,8 ] Y1 C" S* i
形容飞机航迹在地面的投影。% j+ V! q7 P7 m' Z) w4 U$ v
空中交通警告与防撞系统,; e9 e" Z( Y& k
用来警告机组人员可能与其他装有应答机且在同一区; j% I. l F! u i) g; m# p
域飞行的飞机有冲突的警报系统。
! v1 `6 f2 b% i* G, v后缘,( _/ h3 ^. Y+ [1 I4 m+ B" L
机翼、安定面、或操纵面的后边缘。
) j$ K" G/ F3 T, B7 s换能器,
. C9 w( m p, k9 i9 x能将电能转换为机械运动,或将机械运动转换为电能的$ I" w6 l9 c: L, f) ~
电气部件。# V7 w' R6 k- s$ G. A+ ?
转换齿轮箱,. X3 @% T8 g% S1 |
见Angle Gearbox
! u8 m# j, Y( h$ c& {$ t7 os
9 y) U9 ?# J7 p" |$ jTOWING LUG, Pa) c, y. r/ K1 D0 x
a
$ X8 ~+ ~% m4 b: ^& nTRACK (NO. 1), A structural member for attaching fixed
+ l1 @% k1 v1 ~, {4 x3 Lcomponents to, or guiding movable components' ~* }% Z; h/ Y0 a! J
T3 X4 P" P( R! R: v5 v1 ~3 R( F' N
projection on the earth's surface of the path of an" _) _/ e, @$ ?/ j$ D
airplane.! l; P# D: @8 ]
接地区标2 d2 `6 Q" K4 j( ]" T6 L
跑道头端3,000英尺的最6 e. k6 ~. p! T0 B) W" y! k3 a
牵引环,3 X& z7 u$ i @& e2 F9 V
移2 e2 K, H8 g! e6 R' e
用以接连固定部件,或引导可动部件的构件。
" K3 }) j1 z- f航/ D- R3 S. D6 Q5 @9 e
导航术语。$ ]$ l' [3 p. ]+ ], w5 ]( G
.
$ U$ w0 ]+ n, ~ H: F9 R% C0 x英汉对照民用航空词典B OEING
; u0 [) V7 N: q; {TECHNICAL DICTIONARY 1593 p7 D; e8 z% E& f
RANSFORMER, An electrical device which uses" s% d, g6 R5 ]" @ y
RANSFORMER RECTIFIER UNIT, An electronic
; t/ K# F- j* A8 Eevice for changing alternating current to direct current
$ `0 }% Y! t6 n1 j& Z2 S D& N; Dsupply airplane electrical systems.
5 V# u& E- G2 M( V, w# A5 f% Glse signals or triggering pulses
; ]7 \! s$ M8 }/ ^. d( pnd cause component breakdowns or failures.# a( `' K" ^2 |8 z/ K% E
It consists of a base, collector
2 u3 l5 l; x) t7 I! e+ Tnd emitter. Two types of transistors are PNP and NPN.( m5 z6 R( W; d$ f' B
。% E$ Q, D4 R7 E0 X8 e4 m, `/ Y' H
变压器,' V4 n$ S# m$ ?" L% K9 U+ k
磁感应,将电能从一个电路转换到另一个电% R; o7 _& }- _. p
变压整流器,
! v- l& e* x$ \: Q/ O; l! v用来将交流电变为直流电供给飞机电气系统的电子装
G; F6 |0 w# R. Z1 h$ D置。
/ k4 f1 E* ~1 K; d# u& A瞬变,+ u, V) m' f6 r9 v& z
信号或输电线上的瞬间电涌。这种电涌常会产生一些错
/ \2 h6 H5 M; I9 \4 _误信号或触发脉冲,造成部件故障或损坏。5 m' _# [" d& W
晶体管,
# G) ]% k; B2 @ W固态电子部件。通常具有三极:基极、集
9 j1 p6 ]. I c6 T) u极、和发射极。有以下两种:* V2 T, a _+ Z8 x' r2 Z0 k$ U
PNP(正负正)基极电位低于发射极。
9 X% r% C9 v- T1 X7 s# w, O+ mNPN(负正负)基极电位高于集电极。2 t6 K5 t) `- s2 `
TRANSFER MECHANISM, A component for
# |/ A; |" Z7 J6 Xtransferring motion from one place to another.+ [' s2 a( s$ Q2 v7 f: S
T
1 j# A, y [' o4 J/ f, | ~2 r6 Yelectromagnetic induction to transfer electrical energy
, p9 J) Y' ^! A( I% V( ~4 p) @from one circuit to another circuit.
' H3 ]0 X0 l& y k2 UT( h4 j8 ]4 {. {
d
, T2 b" ~; Y# Q& Ito
, G) x& E# p1 X5 o% s! V& wTRANSIENT, A momentary surge on a signal or power$ u1 X3 D, [, K, s' B+ \* ]
line. It may produce fa
7 c6 t! G' D; m* ~+ G& Aa
8 R+ z) m f+ t5 s' tTRANSISTOR, A solid state electronic component for
0 H. R. S. W! C. A% ^use in electrical circuits.
/ Q& ?% r- {6 U% oa
- V$ B# j2 }7 I/ R6 [ D转换机构,1 D V! z! N* J. t7 F
将运动由一处转至另一处的部件
# @1 f# V" f, v一种利用电
; L9 S! [: d" {" B3 O+ _路的电器装置。" l7 Q2 k( P" U& L3 B
电路内使用的
$ [* \& B3 {3 ~- `, G" b电* p0 g. J. x2 ]$ O3 M9 i
英汉对照民用航空词典B OEING
! @" X7 R- g5 g8 F( cTECHNICAL DICTIONARY 1601 ~: T F1 _# D# b5 W9 @
TRANSITION, To change from one phase of flight to
. V: s9 r9 Y7 |& w1 z" u) {% ^9 MTRANSITION ALTITUDE, The altitude at which the8 K5 U' f, Q3 g5 {, a4 m
ltimeter setting is changed.: m6 Z. H& K* O5 ^
RANSLATING COWL, The movable outer portion of
* n, A$ g! K; f9 s# k/ Le thrust reverser cowl which is operated during
1 F' |; M7 f: Y6 R0 rverse thrust.: X" {- M7 H& |; F
RANSMITTER, An electrical component for sending( B9 K Q3 f' v0 G& Q
formation from one location to another.
* ?9 B, Y) s, f# l8 k4 jTRANSPONDER, A radio transmitter-receiver which7 O1 B* z$ R$ v' O, v
ansmits identifiable signals automatically when the" r8 f) I& g" |+ n# R1 V
TRIM, The adjustment of engine and airplane controls
0 ~( R9 V# _3 U从一个飞行阶段转成另一个飞行阶段。
; q3 t5 |0 z0 [# J0 { \过渡高度,) b$ F* L; X& v7 f; f
改变高度表设定时的飞机高度。. v2 X* y: Y: ?: D6 h* Q! Q5 B
平移整流罩,) X$ h" x) W% t& k6 v
反推过程中使用的反推整流罩外面的可动部份。
4 X" n- x) M& Y5 x发射机,7 ?. \. `" x, D( T
将信息从一处发至另一处的电气部件。
/ l( I1 W# R8 S: }5 X+ ?+ @应答机,
- K" B4 w" K9 g' U3 B) N1 D' A. ~在收到合适询问后,能自动发射可识别信号的无线电收
3 q; U0 ~; a8 _* C# a k4 v发机。
6 } z& S; M% P平,
' V! y9 R5 _, u# |动机和飞机在平衡的状况下工作而做的发动机7 J3 ~' r B/ H( s
another.
- N) o- x, g: {: F4 Ea- {" q T5 j) a0 H/ z) n1 e; t# K
T
' q6 x; [; E6 P* |4 @% k) \th
1 R) f& n; Q# z: }& D* }re. @0 ^) J6 [2 m6 G6 A5 v
T
0 B$ Z9 }# I5 n7 b- g3 hin
, w5 E O; g- w! r# Xtr
. D+ N, W3 h. q0 y! |6 yproper interrogation is received.4 Q9 x/ f) ]# g; L+ U
for a balanced condition of operation.; L( y; e& z, P/ q" W n3 k
过渡,% M/ H, T; d* W8 x: s: O% R' l
配
6 W, I, H+ `/ s9 y$ E* ]: D- w: |为使发
: Z8 S+ q" R1 m4 B, B" \和飞机操纵系统的调整。9 S& U/ V, \$ T# b- _- l# g5 X
英汉对照民用航空词典B OEING! G, O9 t# Y: p
TECHNICAL DICTIONARY 161
5 e$ T8 a( q; {3 K+ l$ l0 ]TRIM TAB, A small hinged movable part on the trailing
, S, H% Q4 @4 s. j4 A' s4 u( A7 Iedge of a control surface (aileron, rudder) (see TAB).5 U6 L! ?" y# s5 I3 ?0 B8 v' d# [
L, The total fuel consumed from brake release
, ~6 A* L. P( I/ i# zthrough climb, cruise, and descent, to landing at
5 r% l, f" {6 T( }/ V$ ndestination.
$ E7 P. K4 A7 sRUE AIRSPEED(TAS), The actual speed of the
8 k h4 R) v9 J) Y, C+ n7 o" e7 [aircraft in relation to the moving air. The true airspeed is1 Y! y$ b2 r, E/ V& `8 A
ated airspeed corrected for position
+ O$ y( B/ n. ~2 Zrror, compressibility, and temperature effects. `4 G' |' b9 e5 A
ribes( e5 X" O. D5 u
the output value for each input
0 r* J9 {% G5 d( m, o: m a7 jombination.
/ l/ s1 a" u, X铰连在副翼和方向舵等操纵面后缘的可动部份。+ _& a6 @8 i* \5 h- p, ~- }
航班燃油,) Q1 {6 H! s( R; j
一个航班由松刹车开始,经过爬升、巡航和下降,到
: u o* S4 R& a. U( m目的地着陆为止,所耗的全部燃油。
9 T/ \- _/ Q% I$ H) r变压整流装置,' |9 f9 a$ j& {# B
见Transformer Rectifier Unit9 k. G0 m: ^" E7 Q* {
TRIP FUE1 n( U( A% F! o- I5 U6 _+ o
TRU, SEE -TRANSFORMER RECTIFIER UNIT4 Z7 L) U! J& c$ v
T' l$ |, ?2 ]) r V0 I V4 D$ m
equal to the indic0 [8 X1 b/ `2 n) F: @! p- A
e H6 h2 i, d. o% c
TRUTH TABLE, in digital logic, a table which desc
4 h0 s' F4 u* Qa logic function by listing all possible combinations of
6 J: I8 Y# n7 i+ h$ `2 w5 n) Linput values and shows8 q( X# K- ]. I# k
c6 X4 ^! d# g( p9 R p
配平调整片,2 `! A' h% V1 z0 n; e }, ^+ ?, @
在
7 C: @- u% I8 K& k- f! d3 ~& j.
' H7 {- B% ]6 R i, S真空速(TAS);
" z. [7 w& B( {: {) y4 |, `对于流动中的大气的实际速度。由指示空速经过' z2 n" c) ?4 h7 t" }+ F0 E
真值表,
* x }. k" E* Z+ f8 c数学逻辑中用来表达逻辑函数的表。该表列出了所有可
* y4 ?) U* E6 a) Z9 T. }# N; g( n+ j能的输人组合,和每个输人组合所产生的输出值。
4 t! \3 a/ k; j( y8 U) s飞机相
, N6 c; v1 X3 k4 a; s9 [) z位置、压力和温度校正而得。
7 c% r2 }0 r9 D& R! m% n英汉对照民用航空词典B OEING
/ m# P' N$ f( T5 a7 C1 W2 aTECHNICAL DICTIONARY 162+ ?) ] k& n4 s- j0 _
TURBINE, A rotating part of an engine which
, a( [. s5 T* c% C& B' _kinetic energy from the combustion chamber ga
+ V" P9 J) P5 A" q3 v# s, sextracts
& T4 u8 ~) d; I3 ?ses.
# [+ s7 W/ ~- This energy is converted to turbine rotation which, v: |7 e; J+ s% z
tates the compressors and fan through a coaxial
+ w4 m+ z) [6 nhaft.
/ i4 j3 m# [" lTURBINE CASE COOLING, A method of cooling the# D0 i, m T8 _
ngine by using fan air. This cooling process is used to3 L8 Q7 Y) l5 _% c! N9 |
TURBOFAN,# h2 B/ E& m+ |: J% v5 Z5 |1 Q Z7 ~
(1). A jet engine in which the first set of blades is a
6 A3 W. }" ], q# l' I; R% J/ G8 W0 tlarge fan.' _+ `/ u! ^6 q! _, y
(2). An air driven fan/compressor used in air; c& p* C% L* A4 A# s8 N) U
conditioning system.
6 e( |9 b) _# X: V( C* W% p5 B v$ aTURBULENCE, The movement or shaking of an
7 k, ?0 G' t2 t2 xairplane caused by unstable air masses.* }* Q6 [3 _+ L# m# R$ U Z
涡轮, D$ a4 o* B) G3 U- a
发动机内,从燃烧过的高温高压气体中撷取动能的转动% k; w, M2 w+ m9 u# ?1 y
份。该动能使涡轮转动,涡轮则经由同心轴带动压气机
3 C- @( f( x4 [风扇。
1 N* t1 `; ~1 R5 q$ u涡轮机匣冷却,
( w: a' z9 K6 k4 w4 A! {用风扇空气冷却发动机的一种方法。该冷却过程被用于
3 c' I- O" d0 O, G) w效率。& s( ^, Y( O1 w5 x% j- F
(1).第一组叶片构成一个大风扇的喷气发动机。) m* v+ e+ i2 b
(2).空调系统内的由空气驱动的涡轮和压气机组合。
9 r* Y: \$ p" a9 \& R颠簸,
( _4 N# U$ T( x+ F. E& I/ [% @由不稳定的空气团造成的飞机运动或抖动。
- T0 Q+ _0 r( R) v$ ZT
+ G6 o. m1 t; Yro! [+ ?- N! @, s9 P
s
( q7 U2 z0 o* [$ Z8 R: I7 Ue* _9 u1 p( ~3 w! @
increase engine efficiency.
; Y0 ~0 Z N0 D I部, K) M6 n" n7 R/ g" U
和& v/ ~( R5 W- i* k# d* [
提高发动机
& n: B; M& M0 a6 u; C涡轮风扇,
! K! \6 x$ C1 z- M英汉对照民用航空词典B OEING! v' D! e4 l( O
TECHNICAL DICTIONARY 163' c" i: r& L: w6 h) R6 \: X
TURBULENT AIR PENETRATION SPEED, A speed
: ]' b4 `, {( i( ~0 Y$ \that provides adequate maneuver margins when flying9 y4 |3 w3 J6 B2 T
to unstable air masses.
3 m' U% z# c" c6 a+ W6 _ht7 Q1 R; l) w+ ~
stment in the control% o% c0 R R8 ~* Q2 C7 m
ables.- |- n1 E* y; \& X
UHF, SEE - ULTRA HIGH FREQUENCY' A* C$ J* m, W5 s1 ?8 m
NDERCARRIAGE, SEE - LANDING GEAR; s) _6 e% Y3 v% X4 v8 A/ U5 W* o
UNIT, One of the type, a single component.
+ ]4 Q* D# ^) M9 Y* K) T4 ^' jUPLOCK, A mechanism on the landing gear for keeping1 F( C- @6 {, N, v$ c% B, Z
the landing gear in the retracted position in the wheel
# {3 I2 ]: v" Y, d) q# L! \9 H! nwell.+ |; x o' V0 ?
速度,+ L N6 F4 w9 C! j
纵裕度的速+ N$ P3 s9 B/ y
。
1 j) @4 k" n. K- T0 Y! s调整操纵钢索张力的: r- }5 y5 ]$ z: Z* S! ]. S
械装置。# Q" k2 K9 Q$ d0 r: b
高频,) h3 ~' n: p& M$ y- h1 F
见Ultra High Frequency
/ u" l1 h* Y/ J0 U; din
3 y. K7 S8 o) f, N. TTURNBUCKLE, A mechanical device with left and rig2 n1 G/ x5 y* ?! p8 j
hand threads for tension adju' c" i8 g5 p) o! n6 t
c" [3 M" Q) p! L+ i# Z1 u6 b! o+ N# r
U, T) t2 x- Z) q
ULTRA HIGH FREQUENCY, The frequency band
" i" b% q- o8 x8 H. ^9 a5 `! ^between 300 and 3000 MHz.* ~4 r: d. G5 E4 a; u1 T
U
) F M' t2 O+ w" F, X/ P4 K9 H颠簸穿过7 o6 M5 d d$ q# t5 \! [# X
飞机飞进不稳定的空气团时,提供适当操
7 M6 z1 W4 w3 R度
0 d2 k% z. ^% R/ }松紧螺套,9 D. K s- p! i; w) _+ V
具有左旋螺纹和右旋螺纹,用以
* y) Y) W$ V7 N4 Y. a机
. r/ T1 g3 m$ F1 H超
7 _1 e" Z2 J" W* G0 S) o超高频,
0 r' _) P" v3 q; g频率带在300 MHZ至3000 MHZ之间。
6 i. |7 W; y5 G/ u( B- u起落架,' V! L7 p$ _! R' F4 M* v) g+ C% t
见Landing Gear8 c( i6 K3 s+ Q q7 ]5 k" f
单元,% f0 A% @9 P7 b2 t0 {
某一类型或某一部件。
8 j) g. m) K: y* }, d5 B0 o% f上位锁,0 C1 u" \* N. q7 l4 O% P" H
起落架上,用以将起落架保持在轮舱内收上位置的机7 {- w% A" `# H: F0 Z2 G
构。. |( `4 t0 w4 {% c* \
英汉对照民用航空词典B OEING
2 Y5 s1 m; R6 xTECHNICAL DICTIONARY 164
. f! S2 E3 Q: ^% @ ?' MUPSET HEAD, The head produced on the tail of a rivet: S# U2 e: ]' R' E1 R) e
during the installation driving process. (See
9 W+ x, q5 t4 h6 B8 v, p( m5 ^Manufactured Head.)- @" ]: U6 `- l5 _9 s
1 (TAKEOFF DECISION SPEED), Is the maximum( U7 O" i2 n: _4 C0 @
peed at which the rejected takeoff maneuver can be
# V9 |7 e d2 O0 ~1 P# kitiated and the airplane stopped within the remaining
2 q% {7 V3 {) p- R+ R4 y" D1 ^) D& xeld length under the conditions and procedures defined
% h M" j5 k- n$ Q0 `& fthe FAR's. It is the latest point in the takeoff roll where
9 d, M1 t# @& m+ Y" i5 c, s1 Qstop can be initiated.
$ y; y$ O3 V' O% u+ R$ D% o' pssure3 g9 x+ b5 k E- }! x! w
dient capability and maneuver margin.
p$ @ C9 }" ]VACUUM, A negative pressure or pressure below
4 o4 F# I* Y6 batmospheric, measured in inches or millimeters of# l" P7 C/ C9 V5 `) Z; q
ercury.
4 h Q# y4 G1 ^ C( O( \is+ s/ o: t/ [5 d' d- @4 b# f
VENT, A small hole orifice or restrictor in a component2 M- {+ D) g+ g2 f6 K, O
for allowing pressure in the component to be the same
' ]6 Y! O x& i3 |as ambient pressure.
) b8 R2 E4 v* D* u# g( d在铆钉铆接过程中,铆钉尾部一端形成的凸头(见
0 D% j c G# tManufactured Head5 I' R2 K9 h) g
V
' J* u9 C( `) _V7 C! w! ^$ R& r& g `$ a
s* t* w8 b; a) j4 x. m, @8 X( L
in- H1 G7 v" q4 J# V f# a) b3 ?
fi( E1 f: ?& ^. L1 B
in
7 v2 @3 X3 t, _4 ~6 ?( [a* w$ c5 k; X- J3 {9 J) ^" B. q1 }
V2 (TAKEOFF SAFETY SPEED), The speed flown after
4 C. ~+ t4 h/ H4 x( \; ?: D* ?( e7 itakeoff during engine-out climbout maneuvers to a7 Q; o* _! @7 G1 y! K
adequate gra
1 |9 ]. S5 o2 Mm; N1 t1 B% E* ^* n2 i& v, v# S
VAPORIZE, The mechanical process in which a liquid
7 N8 q% k# P/ u' H- i ]changed into a vapor.
4 ^" `6 u1 C/ [ Q6 ?; w; q2 dVECTOR, A heading issued to an aircraft to provide
* P1 f6 z3 T8 Y; X) Q- unavigational guidance by radar.5 i; c5 ^* M# j* R- B
铆钉镦头,3 P( k% K K/ Q! i3 `6 u0 a( _
)。
7 D8 d* O# L3 ?0 p8 P/ O$ ]. d. {" B1(起飞决断速度),
) J5 e% ^% u4 v7 y1 ~* B+ L& s* P6 S根据联邦适航条例的规则和程序,飞机能进行中断起飞. {5 X6 { L$ A+ J1 \
在剩余场长内停止的最大速度。它是在起飞滑跑时仍可
/ M4 g1 p% E& D b5 d住飞机的最后决策点。
7 O0 J3 e' g0 G速度),# q2 |1 m5 l" p3 A. X
在一发不工作起飞后的爬升中为保证足够的梯度能力
8 O9 Z8 d* u" r& A d. b- ?# w和操纵裕度所飞的速度。. u( f0 x0 V4 E8 E' u7 C4 A
若干寸(或若干毫米)/ g# |6 t. Y' v& y2 ]7 A; ]
汞柱。( ^0 K1 C% y$ D- }# t! Q
蒸发,
8 L2 ^. R$ \% n+ k; z% q: b) f1 ?+ p1 y液体汽化的物理变化过程。
& r2 P, H! n+ k1 t1 z4 n引导,$ h0 H' p; ^1 V* q1 f# d3 N9 s$ p
由雷达提供的航向,以给予飞机导航引导。# d- p2 Z1 g: f6 o) P& g0 F
通气装置,' x9 X' t4 w: k. l2 _& d9 U
部件内,用以使部件内的压力与周围环境压力相同的小- q1 h4 ]- m% a' d* F
孔、或限流器。
. b, Z( i$ h( D- ZV! P. w. ^2 A! q
且/ Y& _; T) @2 [' ~" R1 x
停, L2 E f( h4 N
V2(起飞安全; \ B- s3 T/ \9 ]) q
真空,0 o% ]( w& h( i8 L4 h$ h' i0 c
负压或比大气压力低的压力。常用
9 D+ K4 _ U( L7 @4 {英汉对照民用航空词典B OEING& @4 r3 K) f9 _6 `
TECHNICAL DICTIONARY 165: r3 o) D" p, u X8 U
VENT SCOOP, An air inlet/outlet on the bottom skin of
6 ?" a1 _; _ Y5 z/ fir
z; L4 d" I& P2 r; q9 y9 N# pVENTURI, A part of pneumatic duct with reduced flow
# C2 ?4 e. I0 B* i! Krea for airflow measurement. (Principle: As air velocity
. m( e! F7 s! K7 ?% ?, z. {creases, pressure decreases).
+ ?1 | P8 N4 u- @1 B, K8 f( lERTICAL AXIS, A vertical axis passing through the
' w2 t2 L ^( t3 iairplane from top to bottom. Airplane left and right6 Q# j. G2 h" d9 T2 g& J" |4 n( ~
trolled by the rudder.
4 f F/ j" ]* _, Q% ?: Z& `VERTICAL NAVIGATION, Functions which provide
" f' q" q- z. Rguidance signals to control the aircraft during climb or$ `! [& V0 Z& [2 K: u1 s5 i8 s
descent.5 w. ?; [0 B e; _3 ]4 H
.5 J' c$ ^; E6 m2 ~6 u+ u3 a
通气进气口,
, x. T2 U+ U3 @# l! ]5 ]- N) a位于机翼下表面蒙皮上,用以燃油箱通气和提供燃油箱# C/ x+ w# s$ ?. M0 Q' m' ]6 K( ]
内正气压的空气进出口。2 F3 p3 N: v1 |" _
文氏管,$ O9 E6 y4 q b$ }- Z5 E
气源导管上,导管截面变小以量取空气流量的那一部
5 d H5 r6 W6 P. O% e# o: J份。(原理,导管截面变小时,流速增高,压力降低。)1 D! V# Y0 N6 f& @
垂直轴,
5 F3 F: r% [/ E( E3 X+ v由飞机上部至底部的垂直轴。用以操纵方向舵,使飞# U; V3 H2 m( ` ?
右运动。6 Z' t2 k' I0 j" i5 q/ f! v& H3 T
直导航,
2 t9 s( P5 K1 R,
0 W& M5 `+ w/ J$ M2 j! {the wing for fuel tank venting and supplying positive a! l( L. C+ c" n$ G
pressure inside the fuel tank.7 k+ u. R9 e) L$ [
a7 d; z3 N! x7 u6 G
in
E: m( I8 u/ Y- f mV
: }) e" ]1 T: w& b4 E, gmovement con, I( ?$ Q1 [) D; m
VERTICAL SPEED, The rate of change of altitude8 _4 Q. _3 f- ~1 f8 |
机沿此轴作左
3 V# E9 V. B6 w6 g+ s# r垂
' @: R: t" ~# s9 k' y$ f在爬升或下降期间提供引导信号以控制飞机的功能。
" f$ q0 u9 g/ E6 Q垂直速度 K- A- l) n3 E. w1 e& a& V
飞行高度改变的速率。4 C( ?* V) Q4 c8 u9 W
英汉对照民用航空词典B* Q G' Z/ Y U9 S! {( k: L
VERY H9 f g' _ j0 x3 r# ~
OEING( d. s: _* y$ Z X5 E
TECHNICAL DICTIONARY 1664 X7 e. q" E2 D' Y& w- a# a
VERTICAL STABILIZER, A vertical surface of the( A3 ~" i- W6 M! r% E
empennage for stability/control about the vertical axis.
6 X/ M# M' }) I/ ?VERTICAL TRACK, A climb or descent profile./ H# ?" E! i' ^
IGH FREQUENCY, The frequency band/ w+ x0 D( H9 R! \* h/ \
VHF OMNI-DIRECTIONAL RANGE, A navigational
4 M3 W/ I6 R) Wsystem which tells the airplane's bearing from a VOR m1 U2 b, n) y0 t$ B- Z
round station and its deviation from a selected course
: l3 U% D; h2 b: Z. a8 Y$ u& L. @/from the station.
. w' ]7 C( v! ^7 K3 t7 mISCOSITY, In a liquid - it is the resistance to flow.
" | \8 k& Y5 w$ o" Y( ]VMO, The maximum design airspeed at which the @. F4 P4 n! ^5 b+ h$ {& S
airplane may be operated.- c- z) K- q" c0 S
在飞机尾部,用以保持飞机绕垂直轴的稳定性和控制5 x, N: l+ v% {" [2 E
的垂直面。
9 h$ v; _* P" d: F8 G1 w+ N' S垂直航迹(VTK),! \3 {: t+ e5 {% x" U
爬升或下降剖面。1 a0 h9 r: D3 ?
甚高频,, y5 H5 T5 ~) P3 R$ d) M
30 MHZ至300 MHZ之间。between 30 and 300 MHz.
% Q9 p: E( F/ CVHF, SEE - VERY HIGH FREQUENCY
( _$ a# Q) K% f: }. e( h6 og
M3 L8 V) V1 V. r. Q! qto
2 q/ G. J3 [$ {6 q' |: p& CV! M* W9 c I; f2 r/ ^- W1 ~% c
垂直安定面,
) R; u \9 j0 [5 T2 R5 J& H- J4 ~频率带在: [2 D. m$ F0 J. \2 @
甚高频,
, w& o Z( J$ ^& J0 u* f, N见Very High Frequency
# G( r' k0 O' V# t+ x, q甚高频全向信标,8 m& X/ Z& N- D5 p5 j
系统。该系统可提供飞机到VOR地面台的方
- L' C% t a/ j& l$ Z3 l" D$ V位以及飞机的向/背台飞行的航道偏离。
: X9 M. ~2 u N' L$ V3 E, o' F粘性,) W( X5 `( Q# L7 e
液体中阻碍液体流动的阻力。6 w+ e, f% C3 a, C7 F& F* G H
最大使用空速,
4 I2 M/ }! w- ^& L飞机可使用的最大设计速度。
7 T X0 T% X" P1 R" y一种导航0 @- q( j" W: |: o) G% C8 m$ q2 r
英汉对照民用航空词典B OEING
/ O+ i4 Z5 h) A1 _7 O, O uTECHNICAL DICTIONARY 167
( f8 S3 k- U: QVNAV, SEE - VERTICAL NAVIGATION
3 m' ]$ I5 K. W O' F: \6 p. PVOLATILE, The ability to vaporize readily.7 e; z9 E4 _: s7 s6 m+ n
LE MEMORY, In computers, a memory whose
9 |! V% ~+ n- J; k9 K- GOR, SEE - VHF OMNI-DIRECTIONAL RANGE
: D* Y8 O# R" r0 @- P% P. l' c% j; k; iVORTAC, A combined VOR and TACAN station.: A! Q' l0 V" H- P/ N
ORTEX CONTROL DEVICE, A small airfoil on the
) \3 i! R( J, Q1 Y5 W; Hacelle for improving airflow between nacelle and wing
/ ?+ G; p' w1 G$ m0 B' B2 Zleading edge.
+ N/ h' V" W+ w8 v; _8 _8 ?VOLATI9 D [2 O. X# F( G8 _! E9 i: _. W
contents are lost when power is removed.$ m. G( |+ h p. D3 _. U1 ^
VOLT, The unit of measurement of electromotive force.4 ^) `4 ^$ C/ U1 X4 m5 N7 W$ J
V1 i* s/ p; P% ~/ g1 Q6 ^6 b
V
9 Z* D7 j. Y c; \n1 V/ ^- b# c: h% d9 B
垂直导航,; d' K2 w+ m% ?, x3 G
见Vertical Navigation.
3 R5 k# Q, l. {$ C9 W: Q0 f易挥发的,9 s6 \! p: z8 C Z7 _$ P
随时可以蒸发的能力。0 C! K( d; P+ z7 L5 o" O
易失存储器,
4 E" m0 I- [9 R" T/ P7 _* e在计算机中,失去电源时存储内容便丢失的存储装置。" \1 N. x2 ?% ~+ z- w
伏特,
5 U! `9 t! {0 O电压的一种计量单位。
( G& L. B U5 N9 Z甚高频全向信标,' ?# P l- r; K: a9 h# o9 _- v2 G
tional Range4 Q+ e- V* Q6 g0 z
见VHF Omni-Direc .+ p! S5 }) F7 `6 _. U
VORTAC,- j8 Q+ @1 l7 K q; \$ [, y' a% Y; W
兼具VOR(甚高频全向信标)和TACAN(战术空中导- I# s9 ?% V* \7 h+ `) V. T
航系统,或称“培康”)两种导航设备的导航台。) \: l/ x- D8 k4 D" y( ]
涡流控制器,4 u' Z) a$ `9 ^5 X
发动机短舱上,用以改善短舱和机翼前缘之间的气流的3 c9 W4 \# U) a$ U
小翼片。+ O1 K! K, T+ X: N
英汉对照民用航空词典B OEING
* W3 m9 i! K: C$ QTECHNICAL DICTIONARY 168
6 }& p, d. d7 }( k* Z+ S& N8 \VORTEX GENERATOR, Small metal airfoils, located on1 o' ]8 v9 I* ~
wings and fuselage for delaying separation of the air" y: j/ N. z1 ^. h
ating local turbulence
8 _% f$ x6 s4 X6 D6 Z: }+ kortex).
+ U# ]8 j! P. |, k+ x( ]35 R, Z$ B# U V. [' w' ]
stall speed in the landing configuration.
7 u1 H' c7 V* ]) O. H装在机翼和机身表面,以在气流中产生局部紊流(涡
3 `: N0 S. B# D5 E6 F流),来推迟气流自表面分离的小金属片。- l$ P6 B* y$ ~
度),0 C2 @, _! E, E8 C* H. Z
在着陆形态时的失速速度的1.3倍。8 `( P( y! u' U A1 _! ~8 w" y
见Vertical Track
/ h8 A# [( m, D- O6 j& q$ P8 Bflowing over the surface by cre
- G* z. M8 O. \/ M1 y. f(v
0 i x# Q0 h$ y0 UVR (ROTATION SPEED), The speed at which aircraft
7 a) F/ \( D. n! V9 brotation begins in order to achieve a speed of V2 at5 n2 N) y0 T( ~$ J5 S) {: v/ k
feet above the runway.
. R7 S$ m- Q. m; S3 I8 W) | MVREF The reference speed at the 50 foot height in a9 X6 h9 S) x- y! R( K2 x) l
normal landing. This speed is generally equal to 1.3
; c8 `3 {: x6 ktimes the8 C/ Q% D4 K6 g; A1 W* a! n$ F
VTK, SEE - VERTICAL TRACK* `) m; C# T( o9 o
涡流产生器,
# S1 b; W2 c! X5 A. f Z4 JVR(抬轮速
" m) b ?% I& }- [3 z$ Z+ B4 h在该速度下飞机抬轮开始以便在跑道上空35英尺时达
' u% B9 N, t0 H9 ~3 a+ o `3 p到V2速度。
7 k! X2 a% x9 HVREF,
7 w( p( l3 `$ N* A- H, k飞机正常着陆时,高度50英尺时的基准速度。通常是飞
! w, T" y. R. w6 u4 o4 U( F机4 W) g+ k7 |, C% X+ X, R
垂直航迹,& z7 p4 H" P+ A
./ n8 a! Z- X: g+ [$ V8 _0 f
英汉对照民用航空词典B OEING
6 a' J0 ^" j: e7 u, w; c) DTECHNICAL DICTIONARY 169# b3 c" x# H; k$ A8 W
W
& O$ V0 @# g8 Q. F1 T$ v$ YWALKING BEAM, A mechanical component attached to$ \/ c& j2 e( J- w& o
the main landing gear and a hinged support which helps
# G# A$ n3 s9 i( \& F! pthe actuator during retraction of the main gear.: {, l3 o! C1 d8 ^0 k. o6 s
ATER LINE, A horizontal reference plane along the5 I H- N" \& e) J3 X( P, I, S0 N
fuselage for vertical measurements of the airplane.7 Q# y7 b0 m) ?; e4 I
WATER SEPARATOR, A component in the air
0 W3 m; s$ o/ e0 n9 C" Q8 jonditioning system for removing water from the air
" u1 H1 t* Z' z4 `+ D( Z* I动梁,7 g K6 B5 W0 X! \- C; B9 r: b0 h- i
主起落架上,一端连在减震支柱上,另一端连在铰接支5 J, a& E8 g& ^/ b
撑上,用以协助作动筒收主起落架的机械部件。; z( @, q3 w! N# \1 P4 l
线,+ x; x5 _: Y, }3 ^' i
沿着机身展向,用以量取垂直方向的距离(或长度)的' o! j& k" e: y( R' y/ s4 Z
水平基准面。+ s2 k+ U3 W$ _" S# Z1 M/ y
水器,# ~3 c2 N/ {6 k9 A8 a9 Q
空调系统内,用以在空气循环机的空气下游除去空气中, I. E) @% h5 o$ |' D7 r w3 G
W4 t# ^, V$ l: g
c
. a3 A; E/ {. A$ l$ A6 ^: Sdownstream of the air cycle machine.
' t# S$ ]# L! o4 N6 e$ s6 {+ E# `水# U( m1 s6 f, ?) |# J. O
除5 B h$ U5 X+ B; q
的水份的部件。
1 A) {, ^" n) e英汉对照民用航空词典B OEING' _( m4 l% ^1 [# E
TECHNICAL DICTIONARY 170
$ x' Q* h n5 y2 ?WATT, The basic unit of electrical power.
! Z2 C7 z3 J# }4 [' VWAYPOINT, A predetermined geographical position
/ t4 _; t% L, q) J8 {# i( rused to define a route. The waypoint is usually defined
. U) M- U2 P1 l% Xin terms of latitude and longitude.: X7 ^' N2 {- x% T. j
WEB, The portion of a beam or channel that has been, P. j6 X7 ^) b0 ]
installed between the top and bottom flanges. Its prime
/ F5 e; R$ p1 qpurpose is to furnish strength.5 o3 J) {$ X& m
WHEEL SPIN UP, Rotational acceleration of the landing, b% v4 E# v, I2 S
f the f) |( v z5 G0 G
nding gear (undercarriage) after retraction.; J+ {% n8 N* d. s# J- n8 D
电功率的一个基本单位。
7 r# ?/ u0 l: {9 h1 L' E! Z位置。通常用经、纬度来表示。
6 j% @3 }& d) c9 R# _腹板,# b& r0 B* W- r" c4 v% J
梁的横截面。常见于上横梁与下横梁连接成工字形。主
% T5 V( h3 k2 e4 C6 k2 l: t要作用是受力。3 m0 |7 i' h* b$ j
轮加速,4 e+ y5 P/ @! i4 \* Z
飞机着陆接地时,起落架轮子的旋转加速度。$ N& G. U' F/ z \6 o1 q
轮舱,2 T, R4 v9 b+ Z: M" {
飞机的一部份,用以在起落架收起之后,收藏起落架的
, j O) V2 K3 M6 m那一部份。# d0 b5 R. L* j ^4 h
gear wheels at landing touchdown., q0 K" P) O/ J8 A' F
WHEEL WELL, A part of the airplane for storage o
" H+ Z6 x" `0 l5 Q3 t$ K6 ^& ala% B4 z: j8 I( O, o# Q) Y
瓦特(瓦), A7 g5 I) r/ `* G1 h1 q$ e+ P' l* h
航路点,* z+ d2 T/ F# P/ M
用于决定航线的预定地理$ z3 k. w6 S% ]9 k; A4 K
机$ R' G+ f* ~4 m& \% K
英汉对照民用航空词典B OEING
) h- C# C7 c7 TTECHNICAL DICTIONARY 171; g4 L6 |4 d/ y( H
WIND COMPONENT, The effective wind relative to the' x& C6 F" H& T; [9 R$ Y8 @8 a
horizontal axes of the airplane.' w8 D4 G; O7 q0 J. j: o. E2 r
WINDSHEAR, A change in wind speed and/or direction
! f9 w% f9 f# x9 ]/ D! x, _: Aa short distance resulting in a tearing or shearing
) I1 Z! x( f8 weffect. It can exist in a horizontal or vertical direction and3 A" G: z" e$ N$ r+ |/ h9 C
occasionally in both.% \. `) _, ^, b2 k- O
WING CHORD PLANE, A reference plane from the tip
7 d* l# U- D7 X+ O6 }# o5 Uof the leading edge to the tip of the trailing edge of the
/ j$ Y, b8 }& R$ d( Qing.. d1 J) o" P+ ~
ING GEAR, The landing gear attached to the wing
& c; e" J% j" e& |1 Atructure. l8 U9 J1 T( {/ m# Q2 N; v0 r
ING ROOT, Part of the wing which is attached to the V! ~2 ~/ H* h8 ?* F+ i
selage.
2 `* W( p1 L3 r- F) QWORD, In a digital computer, a word is a group of bits
! G; g" I, t' Q* s; F* N# Dwith a specified length. The typical digital word is eight t/ E' x. T. s
bits long.& J+ ^4 ?3 ]1 D. w: c
风向量,
6 f. N% C( E: s( Y# q8 X; M1 x相对于飞机水平轴的有效风。" O: }7 n( s8 J# b/ \! o
风切变,
' }' T% I! t/ I: s+ {( x短距离内风力或风向的改变而形成的撕拉力和剪切力。. x9 I) m3 E. \+ J7 B
可发生在水平方向或垂直方向,有时会在两个方向上同时
0 l% {& G! H( p; X$ F& `$ ^出现。
) T: _! o, t' m0 ]3 T# p翼弦平面,9 N8 a+ B, i1 K' |& v* T) [) _
通过机翼前缘顶端和后缘顶端的参考平面。0 q- v! g! O7 H6 [- ?+ S' J
翼下起落架,) K+ m+ r/ J$ I, X, j
接连到机翼结构上的起落架。
i0 [, A. }5 `) Q* k z+ \翼根,$ v7 c: }# m% u+ a5 k# a7 H, Y5 c
机翼上,与机身相接的部份。! o3 }3 P8 e. J) _8 S
字,
! q, y# P% `5 ?# q" ?在数字计算机中,一个字是由一定长度的一组字节所组
9 I: P, i; E( r0 r成。一个典型的数字字,有8个字节。
; j8 e2 c) o, i, din
) n2 L: u1 p0 Ew5 I, R" `! J2 S( d
W
6 R5 I. {2 r( z7 }' Fs
( E1 k, P6 m! g! q: xW3 C; T7 i# r1 g6 c0 v3 l5 m
fu
" I/ Q* p$ j5 c; k/ Y英汉对照民用航空词典B OEING
& T" }' {: L8 D1 UTECHNICAL DICTIONARY 172
* ], w9 k7 O) MWRAP AR
5 Q& U' \; h0 Q; kcomputer's
2 |) l, y4 t* k' O: w9 e& aOUND, A BITE test comparing the) X$ C. A$ l( O; J3 d" o+ {
output signal with an internally stored value.
+ T% J R: ?% w5 {, ~XTK, SEE - CROSS TRACK4 {5 w8 A+ y- k' f. O" l! ~
AW AXIS, A vertical axis passing through the airplane
" }' W: L4 H/ n/ c# qfrom top to bottom. Airplane left and right movement$ R7 @/ b8 x6 j
controlled by the rudder. (See Vertical Axis).
8 r- a7 B: V4 h% k# K# O) a6 QAW DAMPER, A system that is used to move the* x1 t2 Q% {. b7 s9 {8 _- d$ ^
dder a small amount to oppose airplane yaw.7 ^' P; p5 b' [2 {, a' J
es
. N0 R- X% j+ x回测," Q% B$ |. w7 t* v4 B
自检系统对计算机的输出信号和内部的存储值进行比2 ~$ `" Q9 i4 k A& ` H! I% c
较测试。
+ f- f* z# L. U交叉航迹,/ Y, E. A5 w/ a, c4 J
见Cross Track
, d! m; J7 i) c5 r' I! UX
3 [- g1 G0 g3 m- B$ _: u- t: [.
) y, c# x4 e: W; v偏航轴,
: l+ A, b- q5 j1 t$ `3 h1 f0 t' m又称垂直轴。由飞机上部通向底部的垂直轴。飞机绕此
4 M K% x# S1 U" W2 q) _轴运动即造成机头的左右运动,这种运动是由方向舵来操
% R0 U1 w6 C1 j% C8 g5 Y纵的。! ?2 U0 g# y# y6 \- z% |) Q3 V
偏航阻尼器,3 J- p0 J1 }& }* E" ~0 G* \
用来少量移动方向舵,以抵消飞机偏航的系统。' @0 a7 U1 m2 u- z
飞机绕偏航轴运动的速率。
8 I# |9 y! t1 W0 w4 K5 x& b1 mY5 _0 P% x7 ]. [0 K
Y6 a# k) M- h! G9 H) E+ Y. L* F
Y
! l0 t1 X" h9 k* N- ^! A# C+ `4 Rru
+ e) [) {( `: qYAW RATE, The rate at which the airplane mov3 K" _1 j s1 D2 \+ G- G Q
around the vertical axis (left, right).
# n; s; p: }' z; ]4 k偏航率,
+ ]# m9 k3 a8 C- P I6 E英汉对照民用航空词典B OEING
/ N0 }. q7 Z( ]; g1 k' ?* YTECHNICAL DICTIONARY 173
& B' [1 q% ]) w) D; }" W3 MZ
$ m% w! a( [# G# J1 P" ?ENER DIODE, A special type of diode which, when5 n/ P' U) X' l+ O; I! o
ZERK FITTING, A device through which oil or grease is
\5 L. _. }. h3 c, O8 J+ Zupplied for lubrication of moving parts.
& Z& X& d* _; a- G+ A$ |; t" @* NZFW, SEE - ZERO FUEL WEIGHT' h1 N l8 }6 H4 S/ ]. ^& r
ZERO FUEL WEIGHT, The maximum allowable weight
8 X4 d, B' D; Z( m# `7 `excluding usable fuel.
6 W8 v7 l& I$ \7 F纳二极管,
" i4 O5 y, v( d8 s又称稳压二极管,是一种电子装置。正常电流可通行无& n6 f& B: M0 ?' r" u% F) P/ y
阻,但反向电流则必须在电压达到预定值之后才能通过。
! s! e- l9 m5 ^5 ]4 e在飞机电器系统内做为调压器之用。反向偏压时,它有一
E. m# p3 H3 B4 w+ |( u个恒定的电压下降。: P, N: t; Y: ]
ZERK接头,
; v7 @$ D3 \$ R# wZERK公司出品,用以接收滑油或润滑脂,以润滑活7 J2 a [3 b- }; J* n
动部件的装置。
( B8 P2 a# j) O2 n1 Z! K燃油重量,0 g3 F5 Z; \0 S, `* R {
见Zero Fuel Weight% o' G) N8 X/ g8 e! a b2 h
Z
/ r- J% U2 }$ n! ^0 D$ Z& areverse biased, has a constant voltage drop. This- k1 g+ V" U& V# `
property makes zener diodes useful as voltage# z' c: l& F5 g
regulators.
9 b. t. R. O4 A$ W% e& cs9 T* O% r$ g7 t/ S" @7 T) c9 H
齐
! E4 D( | m* Q$ X5 y无
. G2 W" b5 u' [.7 H+ P* C7 d1 E
无燃油重量,7 T/ ?; D, w% V3 x" e* z
扣除可用燃油重量之后的最大允许重量。 |
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