- 注册时间
- 2008-9-13
- 最后登录
- 1970-1-1
- 在线时间
- 0 小时
- 阅读权限
- 200
- 积分
- 0
- 帖子
- 24482
- 精华
- 4
- UID
- 9
  
|
AIR DATA COMPUTER, A computer which produc1 Z& y& `! y0 }) z4 D
data information, such as altitude and airspeed, based0 r& P+ M, a3 h/ q( E
on pressure and temperature measurements.
! K. K# t6 j/ Y, j# [ C! xes air; t% f/ `* p' A S/ o% N
IR TRAFFIC CONTROL, A system comprised of
# i5 i5 y7 ?2 Wround and airborne components used to identify, track
! s- U. t/ G) e5 i* r# BOUND SENSOR, An electrical device operated0 g4 z4 a! }5 U( O$ ^1 f- A
y the landing gear, which transmits on ground/in air
+ v4 X# H. \3 u1 Q$ _5 gformation for system operation in flight or on the' y5 ?4 L4 O2 K/ P9 E! n
round., G, r& a4 r2 E3 D& w
IRBORNE VIBRATION MONITOR, The AVM takes( W5 M$ [. T( D' r9 e( W' r. [& D
e signal from the engine mounted accelerometer and
2 y' `9 f& r7 M9 j! e8 ?: oalculates the vibration on that engine.% V5 j- O; H/ ?0 V+ [
corridor equipped with radio navigation
1 T0 b% H+ i( D7 r0 j, maids.
+ z0 Y6 A' r* T( B+ T0 O$ p# uAIRCRAFT (or ARINC) COMMUNICATIONS
) \. P8 J* ~. n6 a! [ADDRESSING AND REPORTING SYSTEM, An' o- \8 s9 K4 n7 E% y3 k
addressable digital data link system which permits the7 ~ t' }2 E0 G1 s: b" h( G; k! X
exchange of data and messages between an aircraft' Y* T& H! D) R) w6 Q+ P
and a ground-based operations center over a radio1 c) N1 |8 ]* Y9 X) a2 X
network./ N8 @) ]% q7 P8 B- j+ w
AIRCRAFT CONDITION MONITORING SYSTEM, A6 J/ j% P0 a/ X
system of sensors and recorders to monitor various; o6 a( n0 Y1 u. B& U: H. M
airplane systems' performance and status.) q1 E, t S: M4 W( Y
机,
" C, I1 w3 N( a中交通管制,1 @! h+ A( Z- s7 J
一个由地面设备和机载设备组成的系统。用来对飞机进( [ a" [: L2 {( d" u* U$ X
地传感器,
2 g5 H* t; H9 W* w% Y一个由起落架操作的电气装置。用于给空中或地面的飞
6 \4 { @) M2 h系统运作传输地面/空中信息。(有些系统只能在地面0 y, q. ~9 K+ ?
用)
$ w6 v" r, D# W& w, D5 S载振动监测器(AVM),
a* u# w% x9 [( m: y) TAVM从装在发动机上的加速器取得信号后计算出该发3 z6 b* g# _" {5 ^
机上的振动。2 A7 M( z' F$ {+ P9 C: c! [
式建立的控制区域,内有无线电导航设备。' [2 b8 a7 g6 T
飞机通讯寻址和报告系统,
2 @* y7 u9 R& T' Z9 G* A4 R# q* H0 S有种可寻址的数据通讯系统。利用该系统可使飞机与地
. N! f! P2 P& l2 D1 f1 R/ h面操作中心通过无线电网络进行数据和信息的交换。, s; o/ `. O. I
飞机状态监控系统, P% K% B* {3 ?) G4 w3 @8 v C
一个利用传感器和记录仪对各种飞机系统的性能以及
8 Y9 _7 [% U' F" O( W状态进行监控的系统。9 z2 C, v( l1 q' _
A9 {6 t0 ]4 d' ^( | Q! f
g
9 ~, ?7 r5 g2 P" G" d7 n$ I' Uand locate aircraft.' x. V3 A" N- l! ^0 e+ G. l
AIR/GR4 ~1 ~! L5 l1 v: t4 }" ?: w
b1 `; T9 @4 \3 V4 d
in
1 l0 I% q2 E: F7 j1 b- Sg
! D$ n& S$ f' |3 N5 e: KA
: A! I( q! k" W' G( |th
) }+ v! f2 L# }- @c
- K! n$ W0 d; c% U0 JAIR WAY, A control area or portion thereof established; l, A. W Q% _) b2 J, {' l
in the form of a# d8 _& I: Y1 ]6 G! H4 k
大气数据计算
9 Q8 R( i9 R8 |, V& x根据量取压力和温度而产生大气数据资料(高度、空速
. O, h" A( | a等)的计算机。0 p$ d) z* ^5 y+ @ Z0 `% q
空
0 ^1 l1 G$ g) m行识别,跟踪和定位。2 H* g; L" p4 F
空
$ i2 t1 w) ]6 A! ^3 a2 X机
( t. a/ g8 q L. |- I0 r: V' T使$ V! x* N) a0 i" Y4 P* _
机8 p5 C! A( x. p% _* T
动
6 Y/ g# B" N! U, L7 C航线,- _/ f! A* ^/ x# V R8 t+ m
以走廊形
: x3 I) z8 o- H* n) d英汉对照民用航空词典B OEING' t9 @% O' B9 b3 I1 {$ k
TECHNICAL DICTIONARY 68 B5 W: I' @6 N5 t6 F1 c5 P- b k9 N
AIRFOIL, A surface designed to obtain a useful reaction,
) V2 U! ]- e! r4 m' A3 M, ~such as lift, from the air through which it moves. Wings,
\: @3 \1 ?. x7 Z+ U3 w8 Pstabilizers and control surfaces are airfoils. q. T0 [8 j% J/ |$ ^; l
AIRSPEED (IDS, TDS), The speed of the airplane
2 b' \1 W% V1 ~rough the air.
8 ~9 m* W# R7 e" k2 wD INDEX, An adjustable pointer on the
8 }% z0 p8 s+ F3 o' H, _# Oirspeed indicator.: @: O6 x$ Z4 `& ^; A6 F4 P
and legal ability) o8 M, C' w0 Y
fly.
( F, B# W, @' G, fm, for example, the procedure for finding the
4 |8 j" D1 B mquare root of a number. D/ s% O) a) P; p+ A7 v$ S- ^
y
+ a9 R% } ~; x1 ore, wind,
: {& Y. c8 m! m- o4 {! F( sand aircraft flap setting. l2 N9 Z1 `8 h3 r& h$ ^# g
是翼面。2 ^5 e$ }& O7 T1 p
速,
6 p' ?4 ]) V U% h6 b* j8 G/ a飞机在空气中运动的速度。
2 a3 |0 w' j2 j2 H$ H& },
5 Z$ o$ S+ ?/ U! F7 C在空速表上可以调整的指针。8 h( r: u; e' U
机械飞行能力、和合法性的飞机状态。
7 c+ K4 B( [0 T8 D! P一步一步的解题方法。例如,计算一个数的平方根的步6 \. E" v+ E# n% x
。
2 F# G! @6 q5 c f能
4 T/ B m* G7 t4 F& n资料的法定文件。: l( s# @1 q: S' g& X
翼位置成函数关系。+ j W" N/ ~5 F; A8 ?
th4 d/ j1 e, z" ]
AIRSPEE
6 ~( t+ k m+ X$ ba
( ~) m' G+ w6 d8 c8 k9 v/ p7 HAIRWORTHINESS, The condition of the aircraft with
1 Q2 @' S$ H2 h3 Vrespect to its aerodynamic, mechanical,! ^4 F5 S6 l2 J3 v) t" u& |, b5 D
to, E- Z( A7 {; `( c
ALGORITHM, A step-by-step procedure for solving a
9 b9 g& ?, P: w& Qproble
8 S0 r- l0 c5 z* Is6 v8 {2 T) o+ U. Q: D% A' k$ ]
AIRPLANE FLIGHT MANUAL (AFM), The legal& @) L- ^& n& {) U: Q, M
document containing performance and operating limits,
4 d: Q0 a) r% h7 j1 K5 B1 Eoperating procedures, and takeoff and landing& t0 w" ^4 ~6 y. d% q) L( j$ a
performance.: D7 f: }) d$ h& t! f4 j, C
AIRPORT ANALYSIS, A comprehensive set of takeoff
* l+ b: [; N. m9 v fweight limitations for a given airport runway, generall* m& T( |# @7 z) A) ^% c+ n+ j
presented as a function of airport temperatu) K# m8 N! ~0 _; l! e! X
翼面,
9 T$ u- i+ y8 i$ T. n0 c7 C; [* V Q用以从气流中获得反作用力(如升力)的表面。机翼,2 @) i# w. w4 e [- z
安定面和操纵面都
9 c' s% L; d( F, m# M" u空
' O$ R9 [5 d& H1 v/ x6 w5 Y空速指标" u. }2 D) K# A Z3 T, J+ {8 e g6 K
适航性,
* J" ^( A6 ~0 B* `; e9 d有关气动能力、2 t4 I% o9 ^, ~# j' R2 |8 B' X
演算法,& M: ?2 y0 G" F; h
骤0 h5 u; X4 y& g. v. e# u
飞机飞行手册(AFM),
4 E1 ?) F9 b( l( }3 n/ {包合性能极限,操作极限,操作程序,起飞和着陆性, l' y- ^! `+ _) o4 S) k% w: J; c
等! Z+ C8 P9 T) o, E/ J7 v8 W# Y$ P
机场分析,# d5 q% w4 h( l
一套针对给定的机场跑道的详细重量限制资料。通常与/ S4 I# }' a8 c9 G. y
机场温度、风、和飞机襟" }0 h' t7 O$ J; r
英汉对照民用航空词典B OEING
7 a( D$ j6 t! }% O6 u* B0 L! fTECHNICAL DICTIONARY 7
8 n2 p( E/ p! t3 h' B/ H2 ~7 PAIRSPEED BUGS, Adjustable pointers on the airspeed
0 \, d7 X& C% l, k5 k5 p* O: Jindicator.6 Y' U# [1 @0 ^
ALLOY, A mixture of a basic metal and small amounts/ M, P7 W7 `* {' B7 E; W: J
f other metals to change the properties of the basic/ c! G; l: H& }
etal.
5 r! Z7 Z3 J/ B$ y% CMinimum airplane speed. ^* s+ f/ p/ g7 u
e of: U7 }* O/ C8 y9 I. _/ y3 T' t
itting airplane angle relative to! l& G$ g* t0 i# J. Q E
irstream for the stall warning system.! E, a( Q: p5 P9 k5 b! v
another.
/ I2 \; @) {$ u3 vLTERNATE , An additional airport selected during$ ~4 u5 U Q& z# W) E
,
& i* g- d' L# j$ f+ Q4 y合金,' l. B% }! l% D* Q: S) k. z9 t: E
在金属中加人少量其他金属,而改变其性质的一种金属
( E, u9 q% B6 r$ }& X合物。
5 k# K4 o+ B" v飞机的最小速度。
8 e1 p* X- f% Q9 `1 c速警告系统传输飞机对
& R0 [8 F5 L3 v流的相对角度。
/ b+ \! V# C0 z5 B9 H8 y由一个状况改换到另一个。) p' ?* V7 `! L
降场,1 m- k+ M- i' w5 }. I" D9 G
划时,除了目标机场之外,所选的另一个机0 ]2 i# R [. a h b% R l
o
$ g0 l H3 I* P9 g8 S2 Lm/ I' X# P7 V; d0 w
ALPHA SPEED,
, `# _4 _& E! Z# i8 aALPHA VANE, A small moveable airfoil on the sid' g% J* I3 s& N' J) t- |" y( s+ e
the fuselage transm
; T& R& C8 q* S8 La; x4 {+ N9 [( g4 h' A* G4 f9 l5 r
ALTERNATE, To change from one condition to5 u6 U& T! U9 c+ y
A
$ Z; V) ]$ ]9 N" t: I/ Eflight planning, usually near the destination airport, to be1 m& t, H' k8 w! n
used when it is desirable to divert from the original
- z% T- f* p* M* i! Xdestination airport.8 \$ \( w! X- g. f/ W0 ~
空速游标
, X, [. F5 s3 d6 Z9 p* s/ q6 |空速表上的可调指标。! t" G: T, Z, j3 u( y1 a$ I
混
, l7 Z) C1 G' g$ t9 `9 t迎角速度,
# X' R. h% j' V9 t# |迎角叶片,
: t6 L# W, i6 P/ {- N: Z4 @' z位于机身侧的可动小翼面。为失
, S% k# ~& T* g" Q; x* h( \" v气1 D R& z5 p' R# M* ?! Q; u2 v, q
交替,% k2 H0 E1 I, P6 M, n l* q
备
" K l2 l: ~3 z% N制订飞行计
; W0 z& y6 f; u0 @场。通常在目标机场附近,以备不去目标机场时,改降之3 o; ~" I$ c/ r0 T8 ]8 {- J
用。0 o5 }* l/ m. F& b
英汉对照民用航空词典B OEING
" }$ x5 z0 P8 |. d3 ]9 U8 h7 STECHNICAL DICTIONARY 86 h( `+ T) u4 L9 J' F0 k* u) r
ALTERNATE AERODROME, An aerodrome to which
# x1 g( G6 X! O/ b% ?* l% San aircraft may proceed when it becomes either
: o1 q; R2 d% i3 Z" p. ]' npossible or inadvisable to proceed to or land at the
: \' D: Y. S7 \, h4 aerodrome of intended landing.- N3 s9 x1 o5 w- t+ u: x- D
TER SETTING, The adjustment of the altimeter
) `; p- [$ b# w8 f) B: _! T; haccount for local variations in atmospheric pressure.6 w5 c1 S1 @; z5 q
LTITUDE ACQUIRE, A digital flight control system
3 ^6 k; y8 r' X$ b. vode to transition from climb (or descend) to level flight.$ T q, i8 Z1 H
LTITUDE ALERT, A flight deck alert occuring when the) E9 a; y- V% H: Z' s7 G( C. g1 W
irplane approaches or departs a selected altitude.2 S: Z5 U/ r& \0 d
LTITUDE CAPABILITY, The maximum altitude at3 C, z6 j- E+ I$ F) [ @
hich the airplane can be flown at for a given thrust,
/ |# p, ~5 L8 E2 p s+ Qpeed and atmosphere condition.3 [( O$ I% A# p1 `+ ]: z1 z
LTITUDE HOLD (ALT HOLD), A mode of the autopilot; }, Q! U' L2 ~# _3 u7 q' L/ F
r flight director to maintain a selected altitude.
4 w3 D1 L2 w. W- Jirplane's altitude during VNAV operation.
1 t* ?; N4 k! C) x6 f机场着陆时,可作着陆使用的/ d6 w5 }4 \% Z' D: x/ X
场。) g9 b" E; [( G6 Q7 W V. s
,
$ R4 l. t. X5 Y4 M x; o根据当地大气压力变化而对高度表所做的调整。
1 {+ }: u) z4 ^! r! ^1 Q一种数字式飞行操纵系统,从爬升(或下降)改平的模
% t0 ~$ |: ^& A。6 U/ o* [1 l2 q2 c
度警告,8 D6 c2 c% t, x* c( C4 b" N: {( S
当飞机接近或偏离选定高度时,所出现的驾驶舱警告。$ H2 C! F& R7 g3 q
高度能力,
! ?, G) ?; I6 C* O0 ~在给定的推力,速度和大气状况下,飞机能飞达的最大( M8 X& j% l+ C; {6 o
高度。3 R8 _2 S* _- I$ _0 I n
高度保持(ALT HOLD),9 F( N/ J$ j7 X( t `6 _1 m
自动驾驶仪或飞行指引仪保持在选定高度的一种方式。
6 s+ j$ g" k- @7 N5 ~& q,' X$ T* I. w7 D4 B! Y; y
员对飞行高度的控制。, e% g+ E+ C0 g0 P* m2 z$ B* N
im
2 c X5 Y7 d+ r4 w/ U8 Wa
# K& S+ X/ V- W: C X2 K- GALTIME
- [0 W7 C P, y v* A+ R2 R# Ito( ]6 e# P& w% F% a. K9 `
A
Y0 Y5 L: ^: K) m( @0 n) sm
, G$ ^- E9 z; nA
- q. A8 y4 h: ^- O7 h2 za
$ i+ C1 m# o6 H5 @A: w( h( B( a; q; e4 Z4 y
w2 Q s. Z+ W1 ^/ `
s
) u9 }' F9 y& K) r0 x9 t6 J0 IA
1 h6 ?% c* v/ N ao
! i4 L" e; c1 U/ Q; x& u# y$ |ALTITUDE INTERVENTION, Pilot control of the
1 d. P& |( ]1 `9 w: ~' [8 Za
: q7 x1 S2 o4 a# K9 MAMBIENT, The surrounding atmosphere.7 K' n( H* {1 ]2 G9 V0 m. P7 C
备用机场,5 l0 Z7 L6 Q2 A @- C% k
当不可能或不适宜在预选+ O f8 N9 `: ]- m$ Y3 O
机
% C _/ o7 o9 D4 B. h- y7 ~) g5 k/ Z高度表设定8 _& r/ C- y& g- L
高度截获,
" m! \' j& m( R6 W! ~; _式
x& {2 [, x3 A* \$ r' d高
/ ~3 f8 J% N7 b/ f" y7 `+ @高度干预
+ q4 ?7 m0 Y* G1 l1 ^& _在垂直导航工作过程中,飞行" D9 Y- W, W* Q: d+ g
周围环境(地面气层), f* R2 B5 E& I+ M
物体周围的环境(特别指大气)。
3 U) `+ H, t- w \3 b6 X英汉对照民用航空词典B OEING& Z2 A+ c# Z& b: m$ V
TECHNICAL DICTIONARY 9" ?& Y* F3 c7 Q; a/ Z) g
AMBIENT PRESSURE, Pressure of air surrounding an
1 y, D$ e# x/ T9 iobject, measured in pounds per square inch (psi) .* i: {& n& {0 U$ r
MBIENT TEMPERATURE, Temperature of air
% s z7 b; Q6 _7 r) Nmpere.
+ P7 v3 a/ @, p; c8 gurrent waveform.' k" }8 {# y! Q$ X+ ]$ m" i
g an) M2 x x% q/ |' Z I$ q" C
nalog signal to a digital signal.
0 n6 r- z' j# U G% h- @ore inputs/ q. S% p9 T# v4 @2 [
f binary digital information and one output. The output* }7 E& ?/ F9 T- I" T
1 only when all of the inputs are 1. The output is 0% P2 [9 P# \4 r7 ]. a/ B
hen any one or more inputs are 0.; o" N- y j) u
面气压),: ]& E# Z7 l+ y0 L
境温度,' J+ h& O1 @! A6 }. t" A$ y
气温度,用摄氏度(°C)或华氏(°F)来: g. \- P% ~) B; v* a
。
+ z9 ^- Q8 x8 i6 ]$ C4 i% e电压或电流波形的幅度。
1 O Q8 e' |2 m性变化的信号来工作,或产生连续性变化的信号; _( ~3 |; ?8 U1 P
统。
) l j4 S5 x/ O6 l$ d6 i将模拟式信号,转换成数值式。
; h1 o. m* j' \/ F一种有两个或两个以上的二进位数字信息输人,一个输
& V3 u( }* E" D$ {6 v/ f; y的装置或电路。当所有输人为1,输出为1。当任何一个- @* D/ l9 q5 d8 _, p# `
一个以上的输人为0时,输出为0。& L& i. a2 W9 c3 B
A
4 b7 e6 Y: Z( B/ j; q5 usurrounding an object, measured in degrees Celsius
7 T7 I1 q! v8 R; O# e% b. Z(°C)or degrees Fahrenheit (°F).% U/ `1 Y: p8 b+ L4 K R' L
AMPERE, A unit of electrical current. One volt across
' j5 k1 W7 o* v; qone ohm of resistance causes current flow of one% u: W l/ u+ b9 h, U; E
a4 y4 L+ B- v# z, s6 d: ]/ O
AMPLITUDE, The size or magnitude of a voltage or
3 ~: a& X3 Q4 M) Z2 b; `$ [c7 r, k. Q8 P& R, B
ANALOG, Quantities or representations that are
) N6 T e; J8 \0 w+ K# a' B, |variable over a continuous range., |8 u% ]! F( T8 c' \& r2 a
ANALOG-TO-DIGITAL, The process of convertin1 w6 e3 X2 {+ i8 B4 V1 N2 C
a" x+ M6 N- v( o1 c! R
AND GATE, A device or circuit with two or m
g: l9 t# p c1 Po
4 x! w; U v, K) F& pis
. |: g! h$ j# Z. O) Q* fw# V5 p* a+ ^/ ]/ y
环境压力(地
* W5 Q# y) `4 _( ~& z物体周围的空气压力,用每平方英寸多少磅(psi)来% k1 A) q+ N0 r4 X' w
度量。# u# v6 `+ r# {
环
" M! S( W/ S" S9 h! V物体周围的空+ S: g* w% L( [
度量。 f- K) r: W2 D* F( k% H& G
安培,
* {+ j% L- o( I% E1 k& h5 H$ t电流的单位。
+ M7 Y* `6 z3 n6 p4 f& [2 P* Z1伏电压在1欧姆的电阻上所产生的电流为9 G* a7 n3 H! Z! H
1安培
+ C* z( g9 k* z/ r- e& F) c振幅,' z& t/ w$ g: g+ x
模拟式,0 I* s4 W- x! H: M( f& V
用连续% o5 d: c% j: L3 h4 K6 a# e
系
3 U# b$ ~) p. R" D7 i" U F从模拟式到数字式,
; X4 ^& x4 x+ ?! C! n与门,
2 p$ e' @$ c, L/ p- L5 m出( ^- s) r, e( a
或( d( H) |/ I! s
英汉对照民用航空词典B OEING
$ f4 z6 r! v7 ]+ e5 Z5 j( b5 L0 ^TECHNICAL DICTIONARY 102 B8 K4 s8 w3 k
ANEROID, A sealed flexible device containing air at low1 M, n) ?0 [' g+ q: Y, D
pressure, which expands or contracts during change of
3 D7 ]1 i- T8 X: K+ i/ C; }ressure outside the device.5 g0 G9 T. i; ^2 ^8 `
ically
0 i5 h# ?& [: Fr changing the direction
2 v5 L5 O% x5 ^$ y* N! Zf drive.
i) `! b3 i% R' m! z0 g; Zof the wing chord in; u( z1 Z; w9 C& ]
lation to the free stream airflow as it moves forward
/ M' U+ a: t" d" M; ^9 Zrough the air.6 o9 ]' j2 f# `7 V
al axis of the0 @5 x4 V1 V i# H% P( t
aircraft.4 G4 M1 O+ w$ @/ x
胀或收缩。9 `5 B# {( @' e. _ ~& H
箱。是改变驱动方向的机械装置。8 f- X3 @/ L( t x$ R( Y( R9 @
机翼翼弦在空气中向前运动时与自由气流之间的夹角。
( D% ^. H& g" J7 H。
% @. z5 ~+ B7 @. qp
* E* v' B8 M K# G. }ANGLE GEARBOX, A part of an engine, mechan
8 ^' s% G) t! c* Pdriven by the compressor, which drives the accessory
6 W7 Y1 Q, L7 j t4 h& o5 Pgearbox. A mechanical device fo0 t% N7 u' L/ M: D" m. W- d
o
% C: N3 `. m( N$ g% K5 VANGLE OF ATTACK, The angle
2 F" ^: F! J$ [2 p8 Tre
* g; C' }- v9 k e; V6 mth
7 j, z7 W1 h8 K p, O4 [ANGLE OF INCIDENCE, The acute angle which the
4 V) `- \. G* i' M% T3 l+ nwing chord makes with the longitudin
* i) X$ k! N9 D$ a* |膜盒,
6 o5 q! t, E2 ~2 H, m2 c' x, U/ M内含低压空气的密封弹性装置。当它周围的压力变化
2 A$ P: ~# G% y: ~( y时,会膨% N$ v' J7 L& w+ r( R+ U- _7 T
伞齿轮箱,8 T5 _9 g- k4 k; o+ o- k
发动机的一部分。被压气机以机械方式驱动,然后驱动& u# Q. G2 M) i% b% @
附件齿轮
! V+ y7 F _3 r0 u5 p迎角,
* Q! i9 B z$ l# a' T5 o1 v安装角,
, h0 }5 W- C6 Z& j( ^# o飞机的纵轴与机翼弦线所形成的锐角
) o0 D, i& i: E: c( h" g英汉对照民用航空词典B OEING
' E3 T! X2 y: ]: h' n8 L, ?TECHNICAL DICTIONARY 117 Z7 c" X. R0 |7 _. l, }
ANNUNCIATIONS, Audio or visual indications used to9 u( d2 F9 p3 h/ F
call attention to an event that has taken place.
+ _ `" b W$ qANNUNCIATOR, A visual device consisting of a number
% _9 E8 z/ \9 c% n6 Lly.6 h: P/ f5 O' b0 B
ANODE, The element toward which the principal stream
& r' J- D9 \- ?5 x" n) J' W2 z! Nof electrons flows.
3 P4 m. o# t6 H0 V4 V, m; o3 }5 uANOMALY, Not normal.% P+ m1 t' J; u u, C/ f0 ?" E
ANTENNA, A device which, used in conjunction with a& M' _: `* P9 K& u3 Q9 W. \
transmitter or receiver, is used for radiating or receiving5 u+ _3 h' V$ i0 T/ _$ [
radio waves.
: U* b8 w9 Y4 ^NTI-ICING, A method of preventing ice formation on
# i |: K% R1 i+ F4 se wing leading edges and engine nacelles.6 l0 W) T. \; d' \
NTI-SKID, A system for providing maximum braking3 K8 |, Q1 Q- V( z) X
ithout skidding for any runway condition. Anti-skid1 E7 i3 U' r# g
omponents are part of the brake system.; M( Z& y" o- u
告,
; M0 Q3 W$ g/ |2 B3 h当发生事件时,以声音或目视指示形成的提示信号。, k! o% ^* e3 i0 w/ n' Q. u
与之有关的电路的现有情况或已存在的. L b, @3 N' f' ?' }0 \& k4 c
况5 U$ r: Z$ l; T" e$ K% E1 f
正极,
( T: h& Z& B2 L0 n# a. C主电子流向的极位。7 Q; i3 N6 ^1 O, U4 W
异常,6 x1 h k4 L) U7 N' E; t
不正常。. @" b; j. u, b
天线,1 p7 _7 N; N6 x7 v5 y
一种与发射机或接收机共同工作来发射或接收无线电
) l, |) n0 G* X) A7 f波的装置。2 D5 o8 q) a9 I( ~7 g
冰, M2 F O0 v) ]+ t
防滑系统,
3 X; i$ C4 ?( S# S* `一种在任何跑道状况下,都能提供最大的刹车能力而不
8 W! d# b4 n9 \- p& V! n m使轮胎打滑的系统。防滑部件是刹车系统的一部分。
/ s' c5 @8 Z1 u. Gof lights. Each light indicates the condition which exists
6 [1 y6 i9 {9 i0 F: Z9 P( por has existed in an associated circuit and is labeled9 m' U6 W6 `$ j5 {8 d' ]4 }$ [
according
2 E5 ]# q, w3 G- pA
0 r# X, A4 G$ [& Fth2 e) n$ z- g i/ S. V/ f' ^
A) o1 K5 h0 y* V/ k* P: Q
w
0 ~3 C4 L6 j3 u- T k6 Z8 wc
' m; _% D" @$ Y2 T7 \ N8 N5 r通% i H1 b- t1 T5 c% C$ S* X* X
信号牌,
8 M' @* ]8 _- Q; d1 L% O5 o' b# R由一系列指示灯组成的目视装置。每个指示灯都有相应
3 n+ y F& [5 L3 |: a的标记,用来显示
* c: q4 _/ t6 g- o9 {+ @' V情( p! S" f: W# P
防( c4 @4 f9 {, D6 t) P/ X& \5 K
防止机翼前沿和发动机短舱结冰的一种方法。
! K5 k# O. C6 N4 v; F! h英汉对照民用航空词典B OEING
: E% m; F# V# z* r5 I5 t4 TTECHNICAL DICTIONARY 12
. g( l0 o% S1 p1 fAPPENDIX, A supplement to the Airplane Flight Manual
2 E3 G, j8 d: z. Y% O9 q; V5 ]4 ctained in the basic manual. A
. P7 l8 o6 D/ J1 g& p+ Nollection of supplementary material at the end of a; D) e$ y* O- @" {% t
ook., p! d6 U, [- A, W, Q
of the# O% ]: T* D$ m! r5 n& K2 q# ~( e
rsion link on the landing gear., n: L/ y3 Q) ]7 {# T+ c7 B6 L# u
APPROACH MODE, An autopilot/flight director mode1 ? C+ A. w; P- J d( k
which is a combination of localizer for roll control and
' U9 ], j: T- }# \. iglide slope for pitch control. This mode is used when full
, n$ q0 l( H$ x; N; _. vinstrument landing system is available.: ^: O2 J. \" t r x* ]( w, \
APU, SEE - AUXILIARY POWER UNIT* ]. n9 o! C* A6 h% j
ARINC, SEE - AERONAUTICAL RADIO: i) H7 l' A, Q% e; Q7 I
INCORPORATED, H6 A. `# Y7 a( @6 o3 o" _4 N( ?
ARM, To make ready for operation.9 g& ?, T1 _# J' E5 {
附录,9 E% U: f2 X" A5 I! F& k- T( {! H! f
飞机飞行手册的附件,包含基本手册中未提到的飞机形# y. T) c8 D; I. k6 M) V
态的其他性能。是附在手册末的补充材料。
. M6 x) n& j4 n' i# C6 v7 E' B顶销,* z8 Z% v) v4 }1 c; o
用于连接起落架扭力臂两部份的销子。+ ^+ h5 j0 |+ u2 |2 w% |1 w
进近方式,
( S0 Y! d3 d; k9 U- a7 @. ^5 Q' D一种综合了控制横侧的航道信号和控制俯仰下滑信号1 q: @2 B& G6 u' n" S& J: ~5 o( D
的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系' v/ |; O4 i/ F o2 V+ D/ G
统正常时才使用。
5 i } C1 V" `, P* d! ]# I辅助动力装置,
2 }! O, k* s' O4 `见Auxiliary Power Unit3 z( M* _: z: j9 @2 ]
containing additional performance for aircraft
# L$ w m& y1 X- n6 [configurations not con
( `- V* C' o5 C$ U+ M' F8 Yc
: G# D* }/ ^, s3 N/ O. q; D1 e7 _b
2 W: ^5 Q5 w) ]. HAPEX PIN, A pin for joining the two sections. N# N# P2 I Q4 g q
to# T5 P+ B- e& A" \* |& }
., H; O1 _! T1 v: l8 B! @7 d7 @$ R4 O
航空无线电公司,5 Y0 b$ k( `* Y
见Aeronautical Radio Incorporated.
1 y. c; J1 @) |; x预位,
9 z$ ^% a& a' h& u9 m6 ~6 d& f部件可以开始工作的状态。
# `3 @6 t8 |, N% X- Z$ w英汉对照民用航空词典B OEING$ `$ B9 q" C J/ v$ [1 Z$ @# y$ R
TECHNICAL DICTIONARY 13
9 [( ^$ k2 @5 s$ S9 b5 \2 e- m2 KARC, The curved track over the ground of an aircraft0 F/ S2 D* z# {; W+ _7 c5 c2 A
flying at a constant distance from a measuring, u% g4 E: |( u% }! O
equipment (DME).
( g2 l/ F5 k8 r* |0 Gin the limits of self-contained system
% H( t- t: | r% aapability.
7 @. \; B4 X3 V* xtem for opposing or restricting; v6 p+ @2 G1 U% B* Y
ovement.
, {3 c, R- c' r2 [/ c2 `8 d9 TSPIRATED TAT PROBE, A sensor that measures total9 x% N8 U; e) E- b6 L" X$ z
ir temperature when the airplane is in the air and that
, F+ t u& C, x8 `) heasures outside air temperature when the airplane is
& l* _0 F5 Y+ |0 b3 Fn the ground. The outside air temperature is measured
H1 Q5 Y- [ B4 WSSEMBLY, The fitting together of a complete structure3 H; a* s. g' s- @% V; d |9 w* g
SSUMED TEMPERATURE REDUCED THRUST, The! g/ W! A( O: x; |; a
ATC, SEE - AIR TRAFFIC CONTROL
1 x( v- V% ^5 ^5 i% t% o2 F8 w,3 q. W% q/ ^$ _, q9 q: J
系统中所产生的一种用以抗拒0 z- N% p- a2 ^! Y" [- O0 }' a! s
作或限制动作的力。
& Q- O1 }+ m" d头,
$ o9 G2 K+ k" e0 ]4 L! i+ R5 V用来测量飞机在空中时的总大气温度和在地面时的外
) J# A# p- D5 k+ c! |温度。地面外界温度的测量是利用引气将外界空气吸入( U# C' [# Y5 p3 |) G3 b/ K! x
头,以达到测量的目的。; v5 f7 z, S. s% I2 E, ]; ~ l, W
配, M0 ?) y ]; w4 a: a( _# ]
一个完整的结构或组件的过程。7 q" w+ @$ {0 l
假设温度而得的减推力,
+ @2 T1 ~- D: |+ _7 c推力设定值时,假定一个比实际外界空气温
5 g) J- a {' b; F k3 E空中交通管制,
6 l' l; @) W2 V; G O+ D9 Y% B见Air Traffic Control
& h. O% P5 t. @$ sAREA NAVIGATION/RNAV, A method of navigation
2 B Z3 [, m+ K, fthat permits aircraft operations on any desired course
) S' `$ N6 p& v ewithin the coverage of station-referenced navigation S' B4 @8 K# g
signals or with
, R1 j% `* k2 t/ M2 [( {, lc+ I& q$ ?( F5 b Q, Q
ARTIFICIAL FEEL, A force developed in the flight( x0 r# {6 `( y0 x5 Z. P
control or brake sys, L! u1 o! P3 k; f9 T$ R, f% \* | w
m$ p* ~7 E0 [! P9 \! @/ g
A: }: m1 g" o( ?/ z& q" O
a5 ^+ c% P- l6 }- f7 `2 s# D: a
m
: ], ?9 W- o# `- l+ Y& Qo
# [+ [; J9 J/ _by using bleed air to draw ambient air through the
1 F. q/ N" {2 o7 W6 L: q% }6 [sensor when the airplane is not moving.
+ H: T) x- V* w9 B3 b1 TA8 ~: W9 [( t; A, Z& B$ G- P
or unit.2 Z2 }( g$ e) @, `6 a) G
A- Y4 u( @$ v2 O, }
lower thrust obtained by setting a higher than actual) B- p% v3 N+ w$ h0 v% O
Outside Air Temperature (OAT). c7 J; [; A4 _: n+ {" P! f R5 p G/ B# c8 g
弧线,
7 Q: a. N$ z0 c( l飞机在围绕DME台等距飞行时的弧形航迹。& ?8 A8 |- n& N( p
区域导航,' G3 r4 k4 S, k! A: y* o
容许飞机飞行在有电台参考的导航信号或自备系统能+ x* b7 w( o6 h) H$ b: t
力极限范围内,飞行任何预定航线的一种导航方法。
1 j7 \2 B1 D3 u; @2 m模拟感觉
: j- H$ ^! V2 ^在飞行操纵系统或刹车
1 r+ H" y6 U; C% p+ Y7 n动
! y2 g; x' Q) I- q. S) O吸气式总温探
, Y" G3 i- d: D/ z3 L/ K3 Y界/ N. \2 f5 _: d
探6 P, d" J! |0 W7 D6 o/ C2 a8 {& C8 `
装! m4 u- Z% B7 _; V1 ~9 l
组合成 A ^& L% J H2 f4 Y$ B
由
2 a/ C# Q, Q0 W0 Z+ f2 U6 O在选择起飞$ p& O' T d! O5 j
度高的温度而得到的推力。用这种方法可以减少发动机的3 r3 g- c& m+ }
磨损和维护费用。
- ^1 S+ L+ ^2 R5 n- i X.
; [/ {- d# W# J: v* p% V- i: @英汉对照民用航空词典B OEING
* J6 w# R7 L4 FTECHNICAL DICTIONARY 143 i2 a# q8 ~0 {) v7 C9 b* j
ATE, SEE - AUTOMATIC TEST EQUIPMENT
3 @ ?8 b) g6 J* z5 TATMOSPHERIC PRESSURE, Pressure of air due to the8 q& }2 i0 z6 [
arth's atmosphere, expressed in pounds per square% j1 X; Z7 v+ j- V5 H9 ^" w3 l) q
ch (psi) or inches of mercury (in Hg) or millibars (mB).
: s# D. t# S( l0 Q XTTITUDE, The relative orientation of the airplane with6 ~. W% ^' R& I! c8 ?8 z) z
spect to pitch, roll, and yaw.
1 |3 b4 {1 z/ @0 Y" Q' qUDIO CONTROUSELECTOR PANEL, The panel in3 Y6 o7 r* X7 Y1 S2 v9 ~5 z/ H; E
e airplane which controls and selects the routing of' f% b8 @# {* `9 l* q
udio.
* K1 N* J, E7 Q, P3 N7 o- v) C( FUTOLAND, Automatic landing using the Digital Flight
8 g$ X# v! \8 g) y+ sontrol System.
2 s g. R1 E& i6 I9 Wn.* ^& l/ v9 V% r2 \& @, [/ Q* x
M, A system
5 _% @3 `8 }. V+ M: J9 `: y: Jomposed of all necessary subsystems needed to guide3 N8 N5 S8 U8 W; s) m
e flight of an airplane.
- ?0 _5 O2 A i& _) eEQUIPMENT, System test
2 `$ `6 ^0 z2 f% g2 D3 equipment that operates under computer control.0 Z! ]2 R4 ^# L$ }
装置, |
|