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AIR DATA COMPUTER, A computer which produc
$ @) k3 V- l( d. Y: ?data information, such as altitude and airspeed, based
& |0 O0 J/ N& s4 d4 E3 `on pressure and temperature measurements.* J( U4 }/ g, G& C* G) b% X2 y
es air
# C( I$ J: O: pIR TRAFFIC CONTROL, A system comprised of
6 S/ N% G: k1 W1 i* O7 fround and airborne components used to identify, track0 Y3 _! U6 `/ ~* ~1 U
OUND SENSOR, An electrical device operated
# K% t3 b. L8 o( h% m. d3 J" Ky the landing gear, which transmits on ground/in air& G* i2 x8 ]' L- e
formation for system operation in flight or on the
' j6 O6 m c2 tround.
, v$ }/ T7 {' R9 a3 KIRBORNE VIBRATION MONITOR, The AVM takes5 x, V% k, c3 |5 m
e signal from the engine mounted accelerometer and
( s/ X/ F. K% M+ f9 {6 ?" t6 ]alculates the vibration on that engine.
* f Z' l8 f+ K( A' Xcorridor equipped with radio navigation, s6 J8 {1 K0 p# ]. Z# p7 k( n
aids.
9 n; G ?: G6 ]- D3 Y# [AIRCRAFT (or ARINC) COMMUNICATIONS
& J# H% c! t! g" @" _5 O ZADDRESSING AND REPORTING SYSTEM, An( y% X9 k8 h! z/ O, ]" @- H7 l( ?
addressable digital data link system which permits the
; d8 C" h9 l& _3 B, Texchange of data and messages between an aircraft! G) p+ Y/ z+ h
and a ground-based operations center over a radio
0 u& q3 C1 m9 D% ^) u7 e3 P( \& Mnetwork.
" X* u3 o' f& a+ y' x! L5 FAIRCRAFT CONDITION MONITORING SYSTEM, A
! ~* |; L/ Q/ N: q0 c, usystem of sensors and recorders to monitor various/ e2 O) d) C- z% u) ~2 O9 Q
airplane systems' performance and status.
" O C g2 P% n1 o机,$ L2 y8 h6 N3 N7 {5 ~% i
中交通管制,' K$ N7 _- i+ X/ }; s. V3 e$ j
一个由地面设备和机载设备组成的系统。用来对飞机进
; V+ f; \2 B$ {5 i) G) h地传感器," R2 ? I% n8 g% Q4 ^7 o( q. o
一个由起落架操作的电气装置。用于给空中或地面的飞
! w Q8 D0 o1 H) `( `! x( _( ~系统运作传输地面/空中信息。(有些系统只能在地面
, E+ t# V* c+ [9 o用)/ d4 V% |3 \0 r7 ?: G
载振动监测器(AVM),
J r% c# \$ i) j: CAVM从装在发动机上的加速器取得信号后计算出该发
5 m& r9 g( ^3 w, C' }9 S; a& R/ B机上的振动。* ?8 N% O8 w8 n+ } z X6 W
式建立的控制区域,内有无线电导航设备。
9 a0 H- O9 U6 w飞机通讯寻址和报告系统,+ [# e7 J( V& S& t; P9 g( S
有种可寻址的数据通讯系统。利用该系统可使飞机与地+ d2 x: @: @/ Y3 ~9 p. [1 M3 a9 a
面操作中心通过无线电网络进行数据和信息的交换。2 z) t3 o" f: L5 {5 ?' b5 F3 Z
飞机状态监控系统,7 _% z6 e& X# l2 ]
一个利用传感器和记录仪对各种飞机系统的性能以及
9 g% `- r1 o/ M! ?- \5 ?! C状态进行监控的系统。) B6 t4 y0 \% C6 `( i2 [
A
7 {6 E. o2 v# z& jg' {$ E' t, h& h/ U: O
and locate aircraft.
5 m% r# d" Z" `; q" f% r! h3 H3 cAIR/GR- G' D+ O0 i/ T
b7 m, G. w1 ]* m4 f7 Q
in5 Y' w# G0 n" v0 j* {+ e
g
' P5 x" U/ u( U9 o7 K, Z' VA
, S4 I y C3 y' H* c7 `0 p+ Q) a* cth
! f. l! ?/ Q% D9 ]$ V2 Yc
. y0 s+ Q1 \5 Y* N$ q3 l0 CAIR WAY, A control area or portion thereof established
/ ?9 W b. j# h& G0 H0 jin the form of a
+ Q! m" J; G# z6 C* P! b( J& ?3 A大气数据计算
" o) ^) G t7 @5 X, F2 P1 a根据量取压力和温度而产生大气数据资料(高度、空速9 z: S O; M* p( i& ]
等)的计算机。
& r4 ?! I, R0 A, [空
' d8 g' x* [. z x4 P& k行识别,跟踪和定位。
# L0 t( p& V H" O# x2 _2 c/ h) i空7 J) S @9 Q4 q7 h* K6 [
机
+ K# ~7 y; H: z0 C3 v; M0 Z5 }8 @使
' S& B+ s- N" N4 w机
! o) R9 \+ y( V! ?5 l1 Y: Z动% M/ r: H# H3 ]& y" O" k8 C
航线,5 [( T) J' X1 U8 A% H# Y" j
以走廊形
$ E V( {, @4 D8 ^/ k, I英汉对照民用航空词典B OEING
2 E' u! d0 ~7 G2 `. S1 m6 F% mTECHNICAL DICTIONARY 6
+ Q: e$ x7 R% m' V( fAIRFOIL, A surface designed to obtain a useful reaction,
7 x) h9 |8 b" _' p8 r3 W2 dsuch as lift, from the air through which it moves. Wings,
5 `+ V4 F5 x. H' E1 e7 Istabilizers and control surfaces are airfoils.' ^8 O3 h5 K' T% D8 G, b
AIRSPEED (IDS, TDS), The speed of the airplane
; T* t; I5 ^* Crough the air.# ~" B W3 o t7 a! v" c1 ^9 e
D INDEX, An adjustable pointer on the
" @/ B1 X& J d3 w# oirspeed indicator.5 g3 i- s3 S9 F( s
and legal ability
! r8 U+ L" O) [% U" lfly.* |, D8 ]5 }$ T7 E
m, for example, the procedure for finding the
7 W: E# @, \8 }; ^quare root of a number.4 j* a0 y' `: J5 R: }* s" P
y
. ], a. _( y6 O1 h1 \re, wind,
`1 ?; _* u' R# Gand aircraft flap setting.. _: k2 O( l- Y. N+ U9 F; u; O
是翼面。
+ T+ r3 ?6 V& a速,2 I) m; w! h) J) }" d* | A5 N
飞机在空气中运动的速度。
( l j+ f+ H- i) Y4 M) Y" U,
/ n. V1 l1 A: H, d7 n在空速表上可以调整的指针。" y5 s6 I$ C0 l. B0 e2 `
机械飞行能力、和合法性的飞机状态。
& B$ j! x- T t6 Z, _一步一步的解题方法。例如,计算一个数的平方根的步
5 ~- ?4 o, g, }7 z+ W% x* Q。
p# v, j" c. w) P能) ?5 ]- G2 b- D
资料的法定文件。9 V0 j: C4 D5 V' N$ {1 p- b
翼位置成函数关系。
2 |" E c) y5 p- g. U3 e$ O& Oth
+ v8 S/ I4 q% p( A$ UAIRSPEE
/ e- {* k0 y# V6 C( ?a3 ]( g t! h) g6 _) G
AIRWORTHINESS, The condition of the aircraft with- J3 `7 [6 x: P0 f' {, T, W
respect to its aerodynamic, mechanical,$ m: b, ? z8 G
to4 i" T [! b& B/ Z6 ^
ALGORITHM, A step-by-step procedure for solving a
, s, u3 w0 Y1 `8 U( D, R Vproble/ O0 Z& q& j6 V% A1 f/ [. e. c
s
* C/ w/ ]- N$ S/ m/ UAIRPLANE FLIGHT MANUAL (AFM), The legal
& z7 z$ K7 b5 c7 `document containing performance and operating limits,
1 Q* {- e1 M2 o, Hoperating procedures, and takeoff and landing- F9 n1 f1 S1 ]# z. J; J* Y) w
performance.
/ k/ A9 `% Q" e+ J6 x( W2 `AIRPORT ANALYSIS, A comprehensive set of takeoff. O" x& M U+ G6 _0 n/ ]0 c6 ~9 A
weight limitations for a given airport runway, generall
A Q. @, `0 i3 Y* |, V: R" ypresented as a function of airport temperatu7 E/ u& V6 g9 P
翼面,
4 r# \) s$ d$ I用以从气流中获得反作用力(如升力)的表面。机翼,* ^* e+ I, X+ h" K4 y! R
安定面和操纵面都$ T) V" C/ P" h" A) O
空; u+ a- A% ?: l+ q7 Q) X8 X. I2 E
空速指标
7 D$ ?" G1 |# P5 _& w2 F适航性,1 {+ j. F4 O3 K* C R6 O% \1 [: q
有关气动能力、
. y! v. Q* y. k8 b演算法,
" i' T6 G7 K+ q0 P骤
5 G2 K" b$ a$ e+ C飞机飞行手册(AFM),7 k/ x k1 }' Y" s, f! ]
包合性能极限,操作极限,操作程序,起飞和着陆性* D' [) J1 U: f, M
等: D* {4 ?& r j/ M
机场分析,0 |- z8 o1 ?8 K% l1 S
一套针对给定的机场跑道的详细重量限制资料。通常与
9 M* g. f$ t0 v V _0 u7 N机场温度、风、和飞机襟0 b u7 K! n; R4 j7 `
英汉对照民用航空词典B OEING
% Y: g* Q# }( WTECHNICAL DICTIONARY 7
! ~* L8 G" D- j$ c/ rAIRSPEED BUGS, Adjustable pointers on the airspeed! f! k6 G9 z2 M; r7 ?% M% ~' r
indicator.& E8 e1 W, n$ U1 t& b
ALLOY, A mixture of a basic metal and small amounts, m3 V" l$ s2 w' c! B/ n$ |
f other metals to change the properties of the basic/ T) Y" x1 L* y+ v+ `* N
etal.; E* ?+ c0 j, g4 B
Minimum airplane speed.0 D- c" A7 T- U& R l
e of7 e/ ]. X$ |+ j: q8 r' `
itting airplane angle relative to
9 B0 P) o; O* C# C, W1 ?, Qirstream for the stall warning system." N9 w, `+ Y. a. l! l" K
another.- h' n- _7 D0 K' ~( t. o; e
LTERNATE , An additional airport selected during
4 F( P; M, [9 {" H' Q,
4 A& A1 q6 V4 g _1 p( W L- b合金,# Z7 H; ^8 z2 X5 L8 m7 i
在金属中加人少量其他金属,而改变其性质的一种金属! \& m( H. x7 _5 b) [+ x: i0 K
合物。
( x- N. I: O3 ^) p飞机的最小速度。
+ _- ^( {2 |5 R$ b) F. j' o: e" M速警告系统传输飞机对
! b+ ^) j, ^# F) L$ O& {2 E流的相对角度。
1 X/ z4 Z2 I# {3 L: C由一个状况改换到另一个。5 N" ?" P. B8 e) l, R- D, I
降场,4 L. N) W* L( _+ T8 }
划时,除了目标机场之外,所选的另一个机& \* l( t) U4 s( F
o# Z/ C$ M* I4 _
m# N; Z0 ?5 Y2 B9 s, |
ALPHA SPEED,
' B {" J5 c7 K; e' kALPHA VANE, A small moveable airfoil on the sid
. U; B8 x, E1 u+ @! gthe fuselage transm9 x- Y5 |5 A) L
a
$ n8 f- G) D# M. r Q, X( u6 wALTERNATE, To change from one condition to
* y7 u% d& f- V4 q( k) ~0 f* QA
# E- Z0 X# F t2 [8 t8 ~, ?flight planning, usually near the destination airport, to be
9 Z7 t8 z' V$ x6 h# X! Kused when it is desirable to divert from the original" X* ?# M. h4 r( L+ K% m
destination airport.! @, x7 h9 R2 [1 D% j* |
空速游标
! H/ B+ o4 |* l0 J空速表上的可调指标。
3 X/ A* t/ @/ W% j# l% n混/ S6 s$ m5 F [! j6 K( |( N
迎角速度,$ i" ?8 h5 z+ z7 @( b* j2 x& N# V1 B
迎角叶片,
7 j) s/ k8 y+ f位于机身侧的可动小翼面。为失6 ?9 u+ {/ G2 H K1 l& R. i r
气
) ]0 J: y7 a0 e. A/ O$ L4 O) O交替," V9 l2 a1 Y ^. @4 k0 c
备" W" b: W3 s* J2 K, p% @8 `; h
制订飞行计
4 T; C+ U; l" F1 Y$ e' B4 }' q. N场。通常在目标机场附近,以备不去目标机场时,改降之9 x; ]2 t3 }: r! k
用。+ ^: T) s- s2 }/ s h: z. z4 z2 t
英汉对照民用航空词典B OEING P$ c# i" q# y; i* K. c
TECHNICAL DICTIONARY 8
0 \$ b6 M8 a. t! {: _ALTERNATE AERODROME, An aerodrome to which
. D% R# j$ c9 M5 M% p4 X. Zan aircraft may proceed when it becomes either( l9 ?- o" M8 p* N1 S
possible or inadvisable to proceed to or land at the" d9 u: T) T* z' n
erodrome of intended landing.! Z) r8 P$ m% X" d
TER SETTING, The adjustment of the altimeter! P- T( Y$ y9 W6 W3 q [
account for local variations in atmospheric pressure.
- u% P1 H- L$ @. `/ K% ULTITUDE ACQUIRE, A digital flight control system7 e1 L* Z9 p% W3 s# S0 ?$ [
ode to transition from climb (or descend) to level flight.; I' ]2 u6 Y& K. u1 N9 S( ^" t
LTITUDE ALERT, A flight deck alert occuring when the
# l# K$ B) M0 P5 l' sirplane approaches or departs a selected altitude.
@6 q& J j0 HLTITUDE CAPABILITY, The maximum altitude at
: P- T# z- |5 d# D4 q3 K: |4 thich the airplane can be flown at for a given thrust,& x- I1 ] T% K/ Y& A# D
peed and atmosphere condition.9 ]* T9 J1 f9 Q: a
LTITUDE HOLD (ALT HOLD), A mode of the autopilot) |. w, X* K: }" ~( w
r flight director to maintain a selected altitude.
[2 b2 G* s" I: U6 a( ?8 v/ dirplane's altitude during VNAV operation.- q' o: ~: w8 {) c$ m
机场着陆时,可作着陆使用的! k" {4 H& y/ h- }: V" I m& w4 f
场。
, d$ j$ u! n- q,0 T. o1 S6 q6 Q. V# a
根据当地大气压力变化而对高度表所做的调整。
+ V2 \# M, ?/ ?6 N: E/ p9 e, a一种数字式飞行操纵系统,从爬升(或下降)改平的模
$ O' S. a5 w! O% G。
' J# {+ x% ]8 g4 D8 U. i度警告,- _# D5 W# z; f: g A
当飞机接近或偏离选定高度时,所出现的驾驶舱警告。
: q: L5 N$ F% x Q5 S高度能力,$ I0 O; y; _2 i0 g! D8 K+ V6 `
在给定的推力,速度和大气状况下,飞机能飞达的最大4 S' m5 n6 s5 w ]1 c5 a
高度。 W. N) g8 U! {: z6 _' C4 q
高度保持(ALT HOLD),
( ^0 ~# @/ L, x: i8 y自动驾驶仪或飞行指引仪保持在选定高度的一种方式。
: h5 W3 T- x; b, G,: j6 |6 I1 a' w3 R! t
员对飞行高度的控制。' X% t2 b2 _/ ]- ?6 l* F3 e/ w+ }
im+ k1 h+ {2 L& Y/ `) h4 S3 i; Q
a
+ U: D$ U+ w# s2 hALTIME8 C: W7 O4 \, E% i& x8 {6 L
to* B+ |; W. {; u% {; a. G! K, ^( l( o
A* ^: a/ g3 V* b6 F2 j3 Z
m
0 r) c1 ^9 G8 C4 W& {& d1 f1 |$ bA' x# G9 a4 V* \0 Q: W, {1 ]
a
7 {! G+ z, D2 Z$ q; rA) n0 u& J/ r6 l P
w/ o% u, g/ Q3 ?9 l ?$ G
s" I1 z X9 {' _( F5 T; u
A0 e+ h9 V. a# d- ^! @: C0 J
o
9 i6 a2 G u( g9 ]' U9 \8 SALTITUDE INTERVENTION, Pilot control of the
# ~+ w- l( y4 K$ n* o/ U* za1 `, H( c) Y1 \! j* F% M
AMBIENT, The surrounding atmosphere.# H2 r: ]9 E5 r! y& f5 u6 U( f7 X
备用机场,/ t7 v# V% {5 k" h# B1 E
当不可能或不适宜在预选
" `8 f- g/ N9 ^- q) i机4 b% P* V3 H. J; q( U2 n
高度表设定
- _; K4 q0 d+ T4 _- ]: ^高度截获,6 f$ j7 `! _% T* W8 M O1 B
式
B* o0 Y$ A$ h4 U% r1 F2 Z7 X高4 ?* J2 W, k$ o' r2 a
高度干预! j+ y7 ^ \, O. q
在垂直导航工作过程中,飞行
! e$ L n* p. u* \% X1 U+ Y2 J周围环境(地面气层),
# `' z0 I8 I% E% W# V物体周围的环境(特别指大气)。
2 ]4 F6 h5 C# Z1 w8 s: q英汉对照民用航空词典B OEING" ~5 Q( t, y& C5 N% f) z
TECHNICAL DICTIONARY 9
. P( g* q- T7 X2 \9 zAMBIENT PRESSURE, Pressure of air surrounding an. N; `6 c7 d+ d1 @
object, measured in pounds per square inch (psi) .
2 _+ b% R8 r% t; l% j4 ~MBIENT TEMPERATURE, Temperature of air
; s: L1 I* R& f2 C3 ompere.
3 O2 f1 [% s4 E/ E% ~urrent waveform.8 `/ c) o+ f: G8 n5 g- K- _7 Y# F
g an
, ~8 b0 i1 [/ knalog signal to a digital signal.
" v8 H" E9 Y3 pore inputs
/ v: s" w' `$ | U2 x* Wf binary digital information and one output. The output( ?7 N1 r0 F0 T# N
1 only when all of the inputs are 1. The output is 0! Y% _( \ c) O: Q( e3 x4 S
hen any one or more inputs are 0.
2 f" L& v+ }1 _" x+ U8 Y面气压),* R; W$ ]/ {% V1 y1 `+ _) q( g
境温度,
! m; c" e, l0 J8 Y. G气温度,用摄氏度(°C)或华氏(°F)来
. O' L( c: ^2 l) m& J4 ^, O。 A- z% A2 G3 @7 e2 `/ P+ a( a
电压或电流波形的幅度。7 W/ @& l7 j* V3 A3 X
性变化的信号来工作,或产生连续性变化的信号) j: Q7 u( j9 p: e) F
统。
* K8 z: l- p9 t将模拟式信号,转换成数值式。
& I. O8 ]5 ^1 j4 n一种有两个或两个以上的二进位数字信息输人,一个输3 d K' r: N w6 f4 F
的装置或电路。当所有输人为1,输出为1。当任何一个& ^- `! d2 ~' f+ N& s% v9 D- p
一个以上的输人为0时,输出为0。' j" T0 w, Q) {
A
+ a) W2 {$ T3 _surrounding an object, measured in degrees Celsius8 m9 G8 O* D, t# z
(°C)or degrees Fahrenheit (°F).+ I3 o, Q, {! B$ v3 c5 e4 q
AMPERE, A unit of electrical current. One volt across+ y ~- e2 {$ }& {) Q
one ohm of resistance causes current flow of one; z& _( V* {5 S
a
7 `" S& O% o5 u* z* v; KAMPLITUDE, The size or magnitude of a voltage or- t6 I$ C1 X9 w9 ?3 Y
c
& b+ J4 f! K: b' f% x# U/ AANALOG, Quantities or representations that are8 m6 r% l: E! m8 g) u+ L% g9 |( o; E
variable over a continuous range.) ~- [4 p Z8 [# h
ANALOG-TO-DIGITAL, The process of convertin& Y1 F5 A. W1 Y* W- E4 H4 ]
a6 Y7 a( n$ L4 x) U4 V
AND GATE, A device or circuit with two or m
+ I( k1 y1 M/ s' c2 _# K, Yo
+ u2 ?; s- J$ a. }" b1 b; qis" a0 \& r% R* S7 L$ Y
w1 v, }' N! G. y/ d1 G
环境压力(地& g; `9 V& M0 k1 d3 B* J1 E
物体周围的空气压力,用每平方英寸多少磅(psi)来, h/ R4 I, r V" X% e: q, d" ]( k
度量。- F8 j0 Y5 [9 X
环8 u" e1 z1 w5 j1 S4 a6 T7 U5 n
物体周围的空
9 |) y2 m2 t3 b6 B度量。2 ^/ D: l) @" s9 l. u1 U: i
安培,
4 f. \* I! j. A& T7 H9 }' m5 ^( K电流的单位。
: k0 I& \6 O6 h! F1伏电压在1欧姆的电阻上所产生的电流为
8 _. `" T5 f; }3 P' T1 V* X: ^1 ]/ r1安培& e& S! F) O5 y) I7 F2 L& J! _0 D
振幅,. g( \/ o, H7 q* h4 T. J
模拟式,
0 N6 \9 ]/ f9 l+ n U5 B+ `用连续
5 c3 ?! m6 f0 |; H. ]系4 E. _ ?+ i# L1 o( }
从模拟式到数字式,& _9 m7 C! e$ z
与门,
$ {' p0 t" p# C! y8 J出' ~ o- P) X" w0 z) d+ a+ z; O
或/ g( z, W1 r: v: p2 R1 _
英汉对照民用航空词典B OEING" o- A" Y' r) T/ g$ d w! V# ?
TECHNICAL DICTIONARY 10# I! e# X- I4 K; t( W6 H
ANEROID, A sealed flexible device containing air at low" h8 q6 u$ s' d7 i7 R* J
pressure, which expands or contracts during change of& Z0 Y6 u/ @5 ~; U# Z3 r
ressure outside the device.2 i4 m! E' k1 D) M, N
ically
$ H7 @! F; A$ q: pr changing the direction8 O! a6 v f6 N2 O B
f drive.- j: \, X, c% ?* \
of the wing chord in" h V U# ?& ~2 ~3 T) q3 s
lation to the free stream airflow as it moves forward3 B+ s* ]7 o& }" B; D6 p# Q# L
rough the air.
- y' N6 O2 O1 `al axis of the9 T$ k& {# f* E1 Z' g6 ~' o
aircraft.9 Q$ `# T$ |1 N0 k5 e
胀或收缩。
. _/ i0 C6 C) Y* S6 J箱。是改变驱动方向的机械装置。8 F& `8 R, M! d
机翼翼弦在空气中向前运动时与自由气流之间的夹角。, o% K3 B0 v* e; m4 F4 e1 V
。
/ l( i, r5 ^/ A& D3 `: Jp, l8 {+ E# L* n2 K
ANGLE GEARBOX, A part of an engine, mechan
+ m7 X) |' x9 ldriven by the compressor, which drives the accessory! o9 A! y7 G3 X+ W6 z
gearbox. A mechanical device fo
o; ]' z/ o ^7 P7 h1 J$ Y) e, Go' w4 q. d1 A( t
ANGLE OF ATTACK, The angle. p) }$ o: t+ O4 S
re7 @; P+ q5 r+ G+ i1 x- n
th) Z; d, b' t# {; S f2 V
ANGLE OF INCIDENCE, The acute angle which the3 G4 X2 n+ |) ?. ~) Y% U! `+ |( C! Z
wing chord makes with the longitudin) L K5 x8 c w' y; X: @/ R! ~
膜盒,, H. ` {, L' y- d ^1 Y
内含低压空气的密封弹性装置。当它周围的压力变化' V: `3 t, f; s4 \
时,会膨 j* ?: l# @: i% X$ t% c
伞齿轮箱,
* B4 s- \/ e" e% I/ q/ Z发动机的一部分。被压气机以机械方式驱动,然后驱动
# a/ s5 u, N- O! b附件齿轮
6 z! i5 T3 i6 {: M2 B迎角,, ?- a% {3 z$ j' y+ l# }3 g9 ]
安装角,
6 B" S2 l `: V, {飞机的纵轴与机翼弦线所形成的锐角6 |2 T7 B) c) U& L9 B; g
英汉对照民用航空词典B OEING! I h9 i- ^8 ~7 E" c
TECHNICAL DICTIONARY 11
! `9 Q" T, s& D6 X8 `1 M# o7 H- B9 E/ n$ ^ANNUNCIATIONS, Audio or visual indications used to/ ~ y t* @ K6 N
call attention to an event that has taken place.$ C, i6 g9 Z& h" O0 ?! `
ANNUNCIATOR, A visual device consisting of a number
1 \7 z% l' ^1 v2 R# e) Wly.
: z0 I- U9 W6 } ~ANODE, The element toward which the principal stream
, }% S7 N! l, Q- e8 z. jof electrons flows.: d7 N2 k- j8 D0 L" i5 O
ANOMALY, Not normal.
8 b. C) s; y% q, EANTENNA, A device which, used in conjunction with a
% `9 d$ Z- g9 _8 Q$ N& Atransmitter or receiver, is used for radiating or receiving* I; S1 ]# r, T4 \% D
radio waves.
* q6 G1 @2 r( I; e& \5 ~. @NTI-ICING, A method of preventing ice formation on' _9 {" }& n- o/ q4 ?
e wing leading edges and engine nacelles.3 P0 N+ g5 w1 o% @) G5 {0 Y3 ^; p- W
NTI-SKID, A system for providing maximum braking. }( t' A$ q& \" i) G7 K% _
ithout skidding for any runway condition. Anti-skid8 R( X; g, ?- }9 p- Y+ ^) ^* n
omponents are part of the brake system.
5 h3 K! U& x+ s) ^告,
& H1 x9 f6 z( C: e9 \当发生事件时,以声音或目视指示形成的提示信号。; u1 Z( `' a N# E$ }4 ?
与之有关的电路的现有情况或已存在的
7 B* d8 r9 o d8 r1 p" e2 E况5 u. I! n% L- X( `( A- x
正极,+ b. g D4 J+ L9 ]. @$ D6 } d
主电子流向的极位。. ` l+ Z0 x1 _" G
异常,
& k! I: Z3 { E" d% h: j- `不正常。
/ ?, Z) e3 ]7 M! i- I: W天线,
" G1 u! P7 y) S; N4 T一种与发射机或接收机共同工作来发射或接收无线电
* X2 |* o' M( Y) J% I' Q波的装置。
% S" A8 H3 s' c2 v) a L3 x冰,+ ~/ K+ `7 m- b( n/ A. ~
防滑系统,( h5 F$ [# B8 R
一种在任何跑道状况下,都能提供最大的刹车能力而不" Q1 H; d' `9 u2 b! W
使轮胎打滑的系统。防滑部件是刹车系统的一部分。5 {" h/ t: k, ^8 \# k8 A3 i' M
of lights. Each light indicates the condition which exists$ \2 I6 ^! B: D
or has existed in an associated circuit and is labeled: j+ T) s/ v" p) } G
according! t' k0 C* |% _. J' z' }) O
A& d' D1 R: Q9 I
th. G* c% }" Y- D
A
! G: N- p# {0 Q/ q. W, c6 ~( nw/ x' P1 W0 @- i0 y
c
6 a i/ q) w3 D6 y6 l通1 i8 s% k: b8 b: n
信号牌,
# P n1 l) F; y" s! ~0 ]. d% Z, [由一系列指示灯组成的目视装置。每个指示灯都有相应+ K) d; y& V6 F7 e* F: Q
的标记,用来显示
! \. h( I8 _% k. L7 n$ n情' K7 B$ @2 m7 X$ }8 a
防
( S) ]: f, B! I0 M$ h9 y: T& I, m: w* z防止机翼前沿和发动机短舱结冰的一种方法。9 O: I" `* x* W* Z6 o6 }& x' c( H
英汉对照民用航空词典B OEING
H) k# [" z! r1 E2 j1 ^TECHNICAL DICTIONARY 12
/ ?5 E) t7 w( D- SAPPENDIX, A supplement to the Airplane Flight Manual
2 k) w3 w0 M; x# W. f2 y5 F- ttained in the basic manual. A
! A: p' s8 r4 sollection of supplementary material at the end of a! p2 @) J2 r. I% T* }
ook.
2 f5 D* }/ r3 ~of the' \* A# O7 t! n( j) I# v+ ?7 E* ^0 r
rsion link on the landing gear.( g- E! K2 U0 j! j
APPROACH MODE, An autopilot/flight director mode
- [- e- M4 R4 r* F5 l) L( Dwhich is a combination of localizer for roll control and
2 [) O. c, ^( G5 e3 F/ ^+ j/ Dglide slope for pitch control. This mode is used when full/ b9 W0 ]0 B3 o' w, [
instrument landing system is available.1 ~' T9 S/ u/ ]( D) X! P. o6 w: [$ i
APU, SEE - AUXILIARY POWER UNIT
5 `+ f3 `' z i% T* Z- d. PARINC, SEE - AERONAUTICAL RADIO# ~/ _5 _4 l& r- z# ]' G
INCORPORATED
: T$ ^+ }: r% P4 ?' B, `ARM, To make ready for operation.
( e. B5 ~3 N3 `, ^, r1 B+ i附录,
3 m8 K9 X8 T2 a% _# P- g飞机飞行手册的附件,包含基本手册中未提到的飞机形( W' F' h N! U% B# f9 D
态的其他性能。是附在手册末的补充材料。% \* ~" h/ m- x* c5 U
顶销,- q( f/ G- |0 |+ |. ]8 `
用于连接起落架扭力臂两部份的销子。
; b! R9 ?, w4 G8 W0 Z, i进近方式,
( s" {0 T* N+ p. u一种综合了控制横侧的航道信号和控制俯仰下滑信号9 Y# A& z" ~# {6 _+ {& B
的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系
/ e3 P* P. w$ O统正常时才使用。; R1 J1 y, X! b: q7 s1 }
辅助动力装置,
. z' y( g" S/ T见Auxiliary Power Unit$ j* F; f5 H& J" k
containing additional performance for aircraft( \; c$ ^+ J7 K
configurations not con
0 [2 _2 ^2 Q7 x5 _! I. \' ?4 I9 Q% D9 Lc
& |; s- G4 \! U& M3 i9 |b
D9 o/ Y) ?: sAPEX PIN, A pin for joining the two sections
% D1 e) P; O6 v2 D' xto/ \8 i! J: Y: t9 w8 k9 @8 a4 m
.4 i8 Q1 P2 W/ e( V/ I
航空无线电公司,
: P* _6 B. j) W; b见Aeronautical Radio Incorporated.
: z# a, c7 ~, v2 C! Z2 z预位,
4 u9 _8 X C! [& y部件可以开始工作的状态。
O+ o( O# _6 ?/ E7 h, c* K英汉对照民用航空词典B OEING
" i, e0 C l; W; p2 f0 }! \TECHNICAL DICTIONARY 13# V( ~! J' M" ]3 c/ O
ARC, The curved track over the ground of an aircraft: U; X/ m) L" B$ d3 m) Y
flying at a constant distance from a measuring
% d4 o* D2 C8 L, V! ^# u# V: Jequipment (DME).
- G4 h0 y7 N R6 X2 P1 sin the limits of self-contained system
; [$ b2 i) e/ |: Aapability.
0 i# g* W' j, {2 j. a. _ Btem for opposing or restricting* ^5 `6 e" T, p! m8 i
ovement.
' m3 [7 j+ @3 f3 L5 eSPIRATED TAT PROBE, A sensor that measures total( C$ M# |& q. H6 Z
ir temperature when the airplane is in the air and that
5 O9 F) e3 g7 A+ F; Feasures outside air temperature when the airplane is
) `+ s2 P1 m6 O5 S3 Z7 bn the ground. The outside air temperature is measured% x G+ U$ m S7 C
SSEMBLY, The fitting together of a complete structure
4 ?/ B7 f# _1 ~* L' Z0 c% sSSUMED TEMPERATURE REDUCED THRUST, The) }( |, u) t8 G2 l `* y$ T) Y0 u
ATC, SEE - AIR TRAFFIC CONTROL: B; n) {+ J8 \8 ~( v7 u
,
& c9 F+ k# n# U( |/ h" Z. e8 f q系统中所产生的一种用以抗拒6 `* K o* b, j, g/ s8 v' r1 q
作或限制动作的力。+ }3 s4 ^, J2 r' q. L
头,; j/ Q+ b I& w% Y! r1 l& h
用来测量飞机在空中时的总大气温度和在地面时的外
+ W% G1 |7 R5 D# V温度。地面外界温度的测量是利用引气将外界空气吸入6 Q; `# u& Y$ ?( @
头,以达到测量的目的。
& E" e% { D+ O; _2 t0 p& g配, Y2 A E; N1 z/ p
一个完整的结构或组件的过程。; r0 `% C& |! R9 G
假设温度而得的减推力,- K& p9 ^/ @9 k/ w
推力设定值时,假定一个比实际外界空气温( o: ?, I- _5 l/ {6 s7 g" X$ y3 W
空中交通管制,
% F! [! a2 J( k4 p* J9 t$ p见Air Traffic Control
3 ]5 u2 e2 E6 ?4 x1 @2 dAREA NAVIGATION/RNAV, A method of navigation
% s; N, [* t! p# Athat permits aircraft operations on any desired course" [% N1 L1 s2 |' V- D7 {) I
within the coverage of station-referenced navigation5 F* ]4 Y9 w0 ]7 @) D8 ~( _' u
signals or with7 m6 {/ t" N: Z, V9 g2 Q( B
c& ~8 }. T' f% H1 m
ARTIFICIAL FEEL, A force developed in the flight0 v8 \2 x8 G2 [0 e
control or brake sys k: K4 q1 x' q5 T0 o8 b
m
9 G S1 Y8 ~# c- {/ V/ pA
, f3 v$ A O. Ba
/ q3 C$ @/ U8 V9 Z$ ]m8 W3 u4 X( C7 v' c( ^
o8 y& `( [- v- V0 J) D C
by using bleed air to draw ambient air through the) H4 ~2 n- O6 Q
sensor when the airplane is not moving.
- \) n1 H" [& L9 h- A2 @A% M0 k3 P0 v* H" O p+ }: W' I7 \
or unit.
* ]3 A2 I% ~' d& E9 m" b4 oA
. {- k! f2 E6 o# {lower thrust obtained by setting a higher than actual( C2 ?$ E+ `9 j& p; a
Outside Air Temperature (OAT).
$ a; u) m' M N弧线,
+ ~5 \8 w; O! K飞机在围绕DME台等距飞行时的弧形航迹。 j$ I h! |% _) _. q. n U
区域导航,
6 z. B' U8 `, @9 t! z' ~9 o容许飞机飞行在有电台参考的导航信号或自备系统能
6 a8 \8 x. [+ U力极限范围内,飞行任何预定航线的一种导航方法。
9 u; ^3 R: h. y( G模拟感觉
! I9 \ I- I) f7 j. b在飞行操纵系统或刹车1 w+ B: @$ c2 E: ^6 }, {( b
动
5 o# W& H4 E# F1 \7 P吸气式总温探6 U1 S" d! {: S1 f: k. v
界( F. @7 a" p, i7 v8 C9 \: ]3 X# h
探
- q. d r' N; I5 q! n! e装. }% M7 L8 z4 m( i
组合成; c$ \4 ? _8 j4 n) a' S
由6 c. p* V: E- @. F2 q
在选择起飞
' m3 X% U; m! z0 S/ ]度高的温度而得到的推力。用这种方法可以减少发动机的5 E* g& K' N( ^0 C0 }1 z3 M$ T6 x5 |
磨损和维护费用。' k! _; ]2 Y9 x) \# V! Z' {
.
# x) s$ I7 v" e- s& x5 p' }- B英汉对照民用航空词典B OEING# r% X/ Z0 {4 v' A
TECHNICAL DICTIONARY 14
$ J/ V5 M$ Q1 ^ATE, SEE - AUTOMATIC TEST EQUIPMENT
2 D' x" v2 w8 k, |% B5 ^+ dATMOSPHERIC PRESSURE, Pressure of air due to the
% W. l! Q5 o9 t9 D! n6 oarth's atmosphere, expressed in pounds per square
1 B9 d. n7 T. i2 @4 F& R# B, n2 q" wch (psi) or inches of mercury (in Hg) or millibars (mB).1 l- ^9 \: x7 G# R' L. k" E% X7 n
TTITUDE, The relative orientation of the airplane with N# ^, @2 p7 y) a# T. m
spect to pitch, roll, and yaw.
' U1 k m. A* l8 J: r+ K4 WUDIO CONTROUSELECTOR PANEL, The panel in
- b. z @! R# }# [& P& re airplane which controls and selects the routing of: X) ~4 b# p1 w( `* O
udio.
( W8 F0 a/ n7 I7 k* O/ ?UTOLAND, Automatic landing using the Digital Flight. r. e+ J6 ] C/ ^) u& w7 Z% q
ontrol System., ]! g: C3 ~, r9 z/ f) J" {$ g7 y0 i
n.1 V) H& I" m1 ^- B
M, A system
/ R5 s* l, M$ S4 R) qomposed of all necessary subsystems needed to guide
% u7 _ p r9 Q5 d1 U8 |e flight of an airplane.
) f4 s& B% |0 a1 P" o4 ^& lEQUIPMENT, System test! o. l9 K8 C$ Q- ]
quipment that operates under computer control.
) t7 r8 h2 f9 K* h/ k1 R装置, |
|