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AIR DATA COMPUTER, A computer which produc3 ]* m X! E7 G& G5 B
data information, such as altitude and airspeed, based
( L6 n% W N0 _* Y6 I( yon pressure and temperature measurements.# f8 Z6 k( g$ s, F$ Y8 K3 h3 Z
es air3 E6 L: B+ C) H" C" {, {# N- m
IR TRAFFIC CONTROL, A system comprised of# ], G$ F8 J6 o; F: e$ c8 ?- k9 L
round and airborne components used to identify, track5 g1 o$ s4 X" Q' m
OUND SENSOR, An electrical device operated
8 g6 k/ L' n# S: o% ny the landing gear, which transmits on ground/in air O# d. G: p5 b, C$ P
formation for system operation in flight or on the
2 Z5 f# a4 p; ]0 N8 Around.
7 |; [* ~" ~8 S' v- `8 E5 hIRBORNE VIBRATION MONITOR, The AVM takes
1 _, l+ R2 Y1 K Q: d4 Ne signal from the engine mounted accelerometer and& _/ i9 F" y8 t6 E" ?% ~- D
alculates the vibration on that engine.- ^7 G! V) U0 k o I4 O- ^
corridor equipped with radio navigation
6 |+ E* f: B8 a. F6 Xaids.9 {: a0 A9 e2 @ @
AIRCRAFT (or ARINC) COMMUNICATIONS0 @6 Z' ^9 ]! f; T
ADDRESSING AND REPORTING SYSTEM, An
8 M7 @: Q! T: X) ]2 Waddressable digital data link system which permits the
7 H6 ~; _0 W7 g4 M5 }) B) Q, @exchange of data and messages between an aircraft
. A8 d( P" f% a [) {3 yand a ground-based operations center over a radio
" m W0 Z" z. M; ]network.1 c; T$ x' h/ |
AIRCRAFT CONDITION MONITORING SYSTEM, A
e! s% R" g1 l% A* }$ k+ Csystem of sensors and recorders to monitor various* |9 `2 ^7 ?7 ^: Y6 ?# ?4 p
airplane systems' performance and status.
; G3 Y& Y) M2 b( W% _$ J m2 E机,
" {: h: G7 ]( U, r* o* g" q0 @中交通管制,
7 z. n6 S# e9 B( M2 o" G一个由地面设备和机载设备组成的系统。用来对飞机进
. P1 u+ A' j. J( [4 C地传感器,
8 P7 B$ Y" ~$ O' B3 c% R一个由起落架操作的电气装置。用于给空中或地面的飞% @3 w- I7 e! L- c- |3 g
系统运作传输地面/空中信息。(有些系统只能在地面 H5 X# q1 M, a7 c
用): r* S0 M4 c( N5 b1 q
载振动监测器(AVM),
7 m3 |6 o- \. L. n: E+ ]9 VAVM从装在发动机上的加速器取得信号后计算出该发
4 T3 K8 \* D) R机上的振动。1 }% f9 W' f7 Y0 B
式建立的控制区域,内有无线电导航设备。. F& O& W( U) z$ d. B
飞机通讯寻址和报告系统,* B4 l3 |% n5 }. X- P
有种可寻址的数据通讯系统。利用该系统可使飞机与地) y. A: [! M8 g1 o# }
面操作中心通过无线电网络进行数据和信息的交换。
# m4 A L h, ]3 z飞机状态监控系统,
- p' X V8 J8 g: Q: \3 c: J# W4 ?一个利用传感器和记录仪对各种飞机系统的性能以及
1 o# [: c! i1 M: r- Y/ E4 i, I状态进行监控的系统。9 K/ v1 G3 b) N+ i
A& A" a& t% a8 K
g
' A2 P+ g W: l7 @8 b; iand locate aircraft.
; I8 g, H. R: PAIR/GR
: ?$ L0 f6 r+ X$ U, ]b
% p. r! E% }% z+ y) M) h. y/ f7 zin
! c0 g' [9 M' b r$ ^5 eg, m3 [& u1 v' H& t+ f+ r# U! a9 J
A) \9 a! @% u& ]. |1 v
th
$ T2 i, t* c4 `6 Ec
7 q+ J4 e$ H0 |! j- P- `AIR WAY, A control area or portion thereof established
7 I1 q! Z. l$ g$ Z B3 }in the form of a
A+ ?$ [) g! I8 `5 y+ R' t2 h& m0 ~大气数据计算
3 m' b5 G: f: x: T根据量取压力和温度而产生大气数据资料(高度、空速
, w/ b+ T5 K0 v, M3 M等)的计算机。
3 a8 b' _/ K, y8 ~空
8 P( @6 D+ s+ V3 E4 m3 O行识别,跟踪和定位。# [ l! ~( _, z1 {0 ?
空
2 o& t6 x/ F+ Y% P0 j# e: t& j机6 s6 Z1 o% `/ b5 B0 X
使7 _: @/ H. z; w
机
0 ]* P7 R5 }, P8 P5 |动7 e3 C4 y" T# U" A
航线,
# t0 j: ~! A' k0 Q以走廊形
& q1 G, O4 l, T! i& ]英汉对照民用航空词典B OEING( c) d1 i- o4 C3 O( g
TECHNICAL DICTIONARY 6
9 w% f/ V% p% UAIRFOIL, A surface designed to obtain a useful reaction,$ L0 g: W7 d' ]% ^: e g
such as lift, from the air through which it moves. Wings,
/ _, l$ b: v) \/ P' wstabilizers and control surfaces are airfoils.
$ {* y$ C, `5 Z& `AIRSPEED (IDS, TDS), The speed of the airplane3 a# m' Z5 |$ r( m/ H
rough the air.
! r# M3 K7 M' o+ N" j5 t5 xD INDEX, An adjustable pointer on the
& X Q; `/ L: t, wirspeed indicator.
$ r5 ]5 X8 u' {' R/ A! _and legal ability6 c' z" g. \' r& E/ J0 ^( C: Q
fly.
+ A, [. W0 c& o9 C& u5 [+ Lm, for example, the procedure for finding the
3 y" q7 x0 f6 I8 p! E% bquare root of a number.& O. e* N% d; v- E7 ?8 D+ e& I; E
y+ b: `6 C0 q" R3 c( l" L
re, wind,8 R4 d" |3 T- ]6 ?4 x, D
and aircraft flap setting.
- R! v |% A3 y是翼面。% v& s5 D3 d, Y; @# j
速,
; t; v" P5 {& ^" s) u, C飞机在空气中运动的速度。
. p" k! _, _' p,
, v. x5 @1 W7 S在空速表上可以调整的指针。2 d/ r, [$ @* p4 q0 p1 I
机械飞行能力、和合法性的飞机状态。, _* y3 t+ n0 M, Q# Q, {: B% t
一步一步的解题方法。例如,计算一个数的平方根的步
/ k8 s" E3 ~8 f5 h。
- F( [# q3 Y+ y. I% D0 C% P" r9 X能
. R+ [) T; W+ f; X& U" C资料的法定文件。
! S8 w+ c* v; ?; [3 w翼位置成函数关系。9 u$ S) A9 l! R3 Y0 I% [
th
5 Z; r& G; O& {0 j. G% XAIRSPEE$ f/ Y: x. w& [6 i2 v+ T) R
a6 N% p0 @9 u4 y6 @
AIRWORTHINESS, The condition of the aircraft with
}( Y1 L7 P/ q% [respect to its aerodynamic, mechanical,
( z" m" c, A4 T( n3 o4 \to( @, j Q6 B, w( \) R9 X0 y
ALGORITHM, A step-by-step procedure for solving a
+ O% p# t, J8 l0 m3 n; }proble
9 V2 I8 x9 D# w( n# w# ?s/ ^+ W$ S. Y1 N- ?, B
AIRPLANE FLIGHT MANUAL (AFM), The legal8 R) |/ a+ ~, e1 V6 z) E
document containing performance and operating limits,! b3 N1 M# {$ g# J. `/ e! E2 k
operating procedures, and takeoff and landing
* G& k3 ~% J6 iperformance.
) o( q: `2 d9 a$ {7 F3 s8 JAIRPORT ANALYSIS, A comprehensive set of takeoff
* x+ ^4 a* W7 {! e; ~& n( p7 Q8 Sweight limitations for a given airport runway, generall
! ~; [( p2 X K3 L3 jpresented as a function of airport temperatu
( D k# i' t2 C( |" d翼面,
. V; W5 j3 s$ ^, T8 c4 ~0 y7 `用以从气流中获得反作用力(如升力)的表面。机翼,2 R9 X% L! d1 Y4 d
安定面和操纵面都
2 _' T0 I9 I; I# X6 t7 J; i7 T( X9 A8 q空
1 m& X- h* g# A9 G空速指标& S) i: |# T# T3 J) E5 ?( r
适航性,6 t) n- M+ @3 Y: q M1 a: G5 a
有关气动能力、
3 `' t9 S0 f' ^7 }/ t; W1 d/ Y' X$ p演算法,2 h K6 B5 L3 a) m( A
骤: ?7 }5 ~5 X. e7 Y( L; t0 ~0 V W
飞机飞行手册(AFM),4 z$ B! {9 y d
包合性能极限,操作极限,操作程序,起飞和着陆性
, Q4 y; f* G3 R4 G& \等
6 U# T1 m3 a! g7 g' B( t机场分析,
e* Q$ J6 X! J) C一套针对给定的机场跑道的详细重量限制资料。通常与1 ~( Y8 `4 B* _; i S6 q* Q8 v
机场温度、风、和飞机襟$ X3 g8 L" I8 a% j6 [; e
英汉对照民用航空词典B OEING
5 g# z* P$ @- h. u$ q$ K* MTECHNICAL DICTIONARY 7# U* K: [- m) H' e4 |, f, I
AIRSPEED BUGS, Adjustable pointers on the airspeed& |+ v' L8 o$ E
indicator.! [( p$ }/ f) _0 q" e
ALLOY, A mixture of a basic metal and small amounts
8 p8 V% Y& ^& ?6 ]% yf other metals to change the properties of the basic
; ?% G; r" u* x1 g h& ~# `$ Aetal.7 P" `+ D3 l( l$ c' i
Minimum airplane speed.
2 T' @1 S! Y% Q( I9 o" t5 y( Ne of5 Q5 b; E* n) C) ]. D5 C3 G
itting airplane angle relative to2 W; B! R& T! s, a; Y/ R
irstream for the stall warning system.. E' b) Z( a- b8 P/ @
another.; O* x+ x( Q& t% L& ]' r
LTERNATE , An additional airport selected during
$ _0 ~6 @5 b9 B* Z,
9 s5 O) B3 a0 v' ?8 Q8 F合金,
* s6 H$ N% U$ w/ t在金属中加人少量其他金属,而改变其性质的一种金属
. l! j6 F# @! Y6 k q9 W( n合物。
! y1 O4 s7 }% ~3 k飞机的最小速度。( x) y! X% R0 c# F G7 J
速警告系统传输飞机对1 W' a# ]. A7 M/ e/ G/ q% @& c
流的相对角度。
8 g' j/ Z6 k& T% [' V由一个状况改换到另一个。- n$ U: c" F* w+ `. G8 Y- C! Y
降场,
9 ]3 h& v' r: E9 n划时,除了目标机场之外,所选的另一个机
& e% H. \$ }+ j/ g5 L, Lo
% ?# w3 @( q5 }* G* ~1 D4 W* `m
/ ]4 n, K( p0 A# pALPHA SPEED,1 p; P( A% r& G7 E5 |/ i
ALPHA VANE, A small moveable airfoil on the sid
( z8 b" j4 m2 {. m( W+ }# [: Tthe fuselage transm
/ H! a4 F. r/ B9 n* Ea& g, U1 I+ G/ c8 c1 f5 K
ALTERNATE, To change from one condition to8 c) ^$ G8 `! h" K% n- F
A- K; K5 T: p- y, [6 v! Y
flight planning, usually near the destination airport, to be6 V$ z3 y& i6 D9 _1 T
used when it is desirable to divert from the original
- g7 t* s! V% M. p4 C" L2 H' Pdestination airport.
^0 U6 u+ H. n- H, L空速游标8 C- D% x/ d9 w# ?8 F
空速表上的可调指标。5 s% ?) H6 F# j& A+ [' ~
混; R) ~+ i5 ^& q8 Y
迎角速度,4 B0 q( B# u3 y1 `
迎角叶片,
+ ?1 s; v5 }5 q+ }& i' b- H位于机身侧的可动小翼面。为失: J% }$ o. h) D4 |, M. b
气
4 \7 t4 g" W# K# d$ u交替,
) L1 S u+ p* \备
+ y# l+ s$ Z ~; ]- L2 Y; C! A( K制订飞行计& _8 v6 A& M2 u2 n" x& z6 E1 p6 ?
场。通常在目标机场附近,以备不去目标机场时,改降之/ \3 F- c$ e) j* r
用。
6 N* H% Q# }3 @. ^& a/ `. f. a3 q英汉对照民用航空词典B OEING
+ \6 M/ |1 [% f( B5 J) uTECHNICAL DICTIONARY 8
1 Q8 p; R8 T9 P+ zALTERNATE AERODROME, An aerodrome to which, T; S" X0 K i. ^
an aircraft may proceed when it becomes either: v" z) t, I+ D" P# o
possible or inadvisable to proceed to or land at the
# P$ R$ W( t; ^2 V+ serodrome of intended landing.
; ~; S( h' k; N+ u# w8 hTER SETTING, The adjustment of the altimeter
$ N5 J) \6 j8 Uaccount for local variations in atmospheric pressure.* ]# z! R1 V% c2 }+ N! \
LTITUDE ACQUIRE, A digital flight control system
2 X" }7 N" K' c' N w1 tode to transition from climb (or descend) to level flight.
t) w1 c# w1 n7 O. Q4 k! H2 }* @LTITUDE ALERT, A flight deck alert occuring when the$ W; e3 f% S& I
irplane approaches or departs a selected altitude.
' {. N8 [* o9 I3 J2 N# G9 L- r: w+ B9 tLTITUDE CAPABILITY, The maximum altitude at6 g* D) F- @2 g" p0 y( [
hich the airplane can be flown at for a given thrust,& c% Q& }! B, |9 |& X
peed and atmosphere condition./ e; \- g5 _% S
LTITUDE HOLD (ALT HOLD), A mode of the autopilot0 j+ I6 u p5 s F5 @- L. a$ z
r flight director to maintain a selected altitude.
4 W3 M3 H/ O4 L+ p+ J% Y# yirplane's altitude during VNAV operation.
6 F/ _! t) ~+ p+ q r- a1 f# p机场着陆时,可作着陆使用的
+ V! `" h7 U0 ^& x8 w$ d, t8 b场。; K8 K7 G. \; J8 g; ~' V
,6 E1 }- g" M! l1 S
根据当地大气压力变化而对高度表所做的调整。) P# }7 h8 U# v) i2 x+ U
一种数字式飞行操纵系统,从爬升(或下降)改平的模
/ ]+ K& J: y. m# ~' b! i/ {。
* ^3 q3 P( i) q3 @0 R度警告,
* R( | C' `2 G R7 a- q5 b* B! }当飞机接近或偏离选定高度时,所出现的驾驶舱警告。 t/ o7 k6 x9 L M# v8 _( A }
高度能力,# L; I( K2 n7 g
在给定的推力,速度和大气状况下,飞机能飞达的最大
1 A6 F U( \& A, T7 i0 x高度。
( j9 d, w2 e7 d% C& O: H高度保持(ALT HOLD),
( q: J" J. m, l, \" N8 [) ?自动驾驶仪或飞行指引仪保持在选定高度的一种方式。
; [) q5 x! X& z( r! w8 S9 J, f,! r, M# T; _/ u7 Q# ^! ^3 |) E1 K
员对飞行高度的控制。" y2 i, a0 f; f- O
im
7 r6 u, y- R, Ja6 `( ?- B: @4 Q3 O
ALTIME
/ i5 T7 l# O9 j+ L$ Fto
3 x. G. V5 g# k$ |7 R; r5 x* fA5 F' }9 C* ?( y/ u/ [! S
m
: C0 N$ Q7 b. g+ N0 vA, I7 V* G" U3 h
a
1 [4 x% R! y/ r; o' Z2 e5 EA0 K. }! Q w9 \3 m+ t
w
+ a$ r) n% L1 K- ?+ T9 {5 Es3 {; X$ {. }# I+ Q5 Z' c
A @3 l- W5 X/ ~. E
o
; I" ?$ k0 q) L. t4 @ALTITUDE INTERVENTION, Pilot control of the
1 n u0 e. l' Ma
8 `. @3 J9 }) n2 \! K% B9 LAMBIENT, The surrounding atmosphere.
9 I0 d! Z- M* A3 d( n( N备用机场,
7 l& d1 n3 s+ E) c( F当不可能或不适宜在预选
# m! i% {% J) m% x z ], F机
4 h% d. l2 n8 l高度表设定! W3 S2 Z, Z" u. M5 \
高度截获,
; ]. R( }" w8 Z5 \5 e式, O- }' h& b/ Z# d) w. m! V
高
5 E; Y. u& K9 u5 k9 o高度干预; N- o- n8 r4 o
在垂直导航工作过程中,飞行
- n+ h V# u. ^3 Z周围环境(地面气层),
' \7 Y. V/ f" N4 W, c3 ]2 L* ]( D4 Q物体周围的环境(特别指大气)。
# L# o1 s, g0 J5 B英汉对照民用航空词典B OEING
# W6 {3 v& b+ ]2 z* \9 y# W5 tTECHNICAL DICTIONARY 9
& T- V3 T) V1 m9 g5 C% `' h5 y. y1 lAMBIENT PRESSURE, Pressure of air surrounding an& j5 g0 v, n1 t7 r; j* @
object, measured in pounds per square inch (psi) .9 |6 ^. k: _# X$ I1 r, p; ^# T
MBIENT TEMPERATURE, Temperature of air0 \" u* W! a) d( i
mpere.9 Y3 ]0 C5 |! _. f) w
urrent waveform.
* P. w& f( c2 `g an
# ?- ?" d# w* r8 Gnalog signal to a digital signal.
" c$ g- a! \. h, Qore inputs1 F; I. w& ]& H9 a$ p# ?% u7 u; g
f binary digital information and one output. The output
; k4 L& b8 T* K1 only when all of the inputs are 1. The output is 0
. a8 T7 j8 u3 D% }5 ohen any one or more inputs are 0.6 m. U: w$ A. ]) y0 r
面气压),& n% g5 P0 Z; ], g# [
境温度,
8 i3 l* c$ d8 t5 [2 g( y. v气温度,用摄氏度(°C)或华氏(°F)来
1 {: m+ ^' I$ c- m4 o) [。
. P: W- f& E' D( r& I! \电压或电流波形的幅度。( n) ?! p* X' H! D X, Y0 f
性变化的信号来工作,或产生连续性变化的信号* |7 w5 {! Q3 z( x4 Y
统。$ a1 b1 L- o3 P! \$ A
将模拟式信号,转换成数值式。
& a9 U9 e. z( U一种有两个或两个以上的二进位数字信息输人,一个输
% e1 @- {3 Q; _的装置或电路。当所有输人为1,输出为1。当任何一个
# a+ p- w: p; C- z7 c# ~# V5 ^一个以上的输人为0时,输出为0。
- X y7 [4 i1 z2 z0 \( q; E% [A/ b! {% t2 U- _% U4 P4 b4 ^
surrounding an object, measured in degrees Celsius$ q0 x1 _; Z6 H( E l. v. p
(°C)or degrees Fahrenheit (°F).
8 ]4 _6 ? W- k5 r8 zAMPERE, A unit of electrical current. One volt across
7 Y5 i( K* a4 b4 \* d* i; done ohm of resistance causes current flow of one
) A: d$ i; I$ S5 _' A7 va1 m/ u/ |, V% D% w0 @' u
AMPLITUDE, The size or magnitude of a voltage or
+ y9 B. R- a9 z, B: z8 q; Ec, j9 {6 m5 @9 E
ANALOG, Quantities or representations that are
6 S- ~5 j( O* x" |* T( @variable over a continuous range.
4 D7 L" a w" l8 \; n- `8 BANALOG-TO-DIGITAL, The process of convertin+ r1 d% |2 X. M ?9 I
a
( W* n [; ]$ }5 m9 t. |" b [AND GATE, A device or circuit with two or m
# q) r( o% `5 ^o" g% P" f# z3 y
is! g) z; I1 n5 I# t( P$ ~2 a
w0 \. d! c2 y0 x- s# _4 [
环境压力(地1 L: ~0 g5 S9 c
物体周围的空气压力,用每平方英寸多少磅(psi)来% {4 s j+ D. M" a
度量。
6 E! s: o8 N: i/ _( l {' E" p环; Q7 H' F" ?4 q) k( [$ A
物体周围的空+ O& |( e5 s0 ~: I6 I! j
度量。! Q2 \$ `4 q# \
安培,2 f9 J$ T4 ?0 b0 z( E; @
电流的单位。
7 E/ ^' B. u# x1伏电压在1欧姆的电阻上所产生的电流为: e$ o# E3 S Z
1安培* Y5 k ~3 D! s6 N( ]
振幅,
% u# R% g" a8 Q模拟式,* S0 ~, v- U' L+ X f+ V' d
用连续* y$ s' E' G! @; i1 s5 d3 o I
系* c7 r" C3 w/ d8 @! Q& G
从模拟式到数字式,0 I: H/ Z1 l* a6 ?" k3 N
与门,
+ Y% ~% e2 X$ `+ c出; Z5 q( f. i) S+ f
或
6 r" G7 E$ r& R英汉对照民用航空词典B OEING
8 L2 k9 ~- y4 X! ~+ K' t. cTECHNICAL DICTIONARY 109 h% R- {& \9 c( S$ a7 N" O$ F: `, r
ANEROID, A sealed flexible device containing air at low
6 K0 B" h* \, ~( M* V2 Mpressure, which expands or contracts during change of
f! L: x2 \* Kressure outside the device." d: r+ T% K; G, s/ n; e
ically
$ p+ Z' L/ {0 Y, Xr changing the direction
- C! ?* u% w' a4 k/ }f drive.- `% L6 b( }9 R- }7 j: H6 g
of the wing chord in
. W* h9 p9 R, z& Z" _1 ]lation to the free stream airflow as it moves forward, w8 y6 J1 d8 Z1 D* t+ p4 ?. ^, r
rough the air.. [- W! l6 z( L0 j# |4 O
al axis of the
! L6 ]6 q: H& F4 G; xaircraft., ^1 ~( i0 T' t5 K' e
胀或收缩。
+ v* h$ C5 b8 m" a4 s箱。是改变驱动方向的机械装置。
& T0 a; S3 @0 w7 z机翼翼弦在空气中向前运动时与自由气流之间的夹角。
; S$ b: N7 i8 n。% l3 T. g; {+ X4 h4 R9 A' W. ?
p1 h) j' }7 y6 k
ANGLE GEARBOX, A part of an engine, mechan
. S, \7 S+ M' ]- Ndriven by the compressor, which drives the accessory
5 ~8 j6 z f# g) R l1 M$ @gearbox. A mechanical device fo, K# i. s: q& c, k4 n" R
o3 M: ~8 P5 N# ?+ S
ANGLE OF ATTACK, The angle# \3 ]- m) G8 G0 \
re
5 p- Y$ N2 e) } P/ o" C# u( z/ Rth
5 x- P+ T2 \% m. {4 |0 |! l. QANGLE OF INCIDENCE, The acute angle which the
3 q' U0 C, u0 Y; D/ awing chord makes with the longitudin. r( ~. S9 P9 |' U% ]5 L. y7 J; k6 O
膜盒,
& g* D6 e# r' H7 V0 t! ~4 J内含低压空气的密封弹性装置。当它周围的压力变化4 Y( Z4 a+ u1 _. l0 r
时,会膨 s6 r& {, ]/ B$ p# {' g* M
伞齿轮箱,7 v+ T N4 ] Q
发动机的一部分。被压气机以机械方式驱动,然后驱动, U8 Z6 c% I4 K7 ~
附件齿轮- d9 k& E7 j& ^1 O1 {2 {
迎角,
. _. m4 |! i$ ^; q1 b安装角,
+ k8 X6 |" }5 i1 T$ C: o飞机的纵轴与机翼弦线所形成的锐角
0 m$ A4 R' B8 [0 S! V6 [0 p英汉对照民用航空词典B OEING8 l) A. D# f& l6 w3 ]: G9 k* g/ H, Z* y
TECHNICAL DICTIONARY 11' Y$ m6 Y" F; d9 |( w7 ?" I. G7 n6 e
ANNUNCIATIONS, Audio or visual indications used to
8 E3 s& ]( Y7 n5 `1 P3 u0 H! Fcall attention to an event that has taken place.
0 l Q5 a9 j1 V) c, ^0 KANNUNCIATOR, A visual device consisting of a number
( d6 x. y. _5 B2 E7 a6 ely.. R' u: t/ t- t* n8 M
ANODE, The element toward which the principal stream
" A7 ]2 d% Y1 b* Qof electrons flows.
$ v# |) Y% x+ aANOMALY, Not normal.
# k( e! H \+ M' y" mANTENNA, A device which, used in conjunction with a
5 Q$ Q7 e. ~+ d/ {5 ktransmitter or receiver, is used for radiating or receiving# ]+ B2 Y; O6 b6 n/ e3 P n
radio waves." c4 {3 B0 y5 R) d' l5 H! z
NTI-ICING, A method of preventing ice formation on
" X+ e+ h/ W( D% u6 c/ V4 l7 }e wing leading edges and engine nacelles.
8 `9 f5 a+ I, fNTI-SKID, A system for providing maximum braking1 D+ g, O- p8 J0 _( b: O
ithout skidding for any runway condition. Anti-skid8 H6 f" }: r$ Z% Q4 c! x G: w- p8 g
omponents are part of the brake system.
. k* N4 z6 a5 D告, `8 b6 y" {5 U1 }
当发生事件时,以声音或目视指示形成的提示信号。
7 u$ ]. ? o3 z5 Q' [8 _1 _与之有关的电路的现有情况或已存在的
6 H: k9 Z- @' Y' u况2 \0 g" p+ S, h1 w
正极,
2 X' E8 J6 w4 N主电子流向的极位。
% y1 ?# ~: A6 B0 z异常,0 x( t8 d/ I+ G4 G8 t7 z* C
不正常。. L9 q& e2 K) |6 y+ Z: @
天线,5 P% y& x: B4 ]* s4 |
一种与发射机或接收机共同工作来发射或接收无线电4 h/ H! l p) Y: A* @4 ]
波的装置。
) z4 e# F9 a: n' r冰,4 F1 ?: e0 @7 R5 E# F6 B( H0 V
防滑系统,
) _* t5 H( m3 x" V6 A9 F! }, y一种在任何跑道状况下,都能提供最大的刹车能力而不# O; a. x H/ m; _+ f
使轮胎打滑的系统。防滑部件是刹车系统的一部分。0 F/ F2 ]7 @1 M" c6 `
of lights. Each light indicates the condition which exists# w( j) U4 n: L3 a H) ~
or has existed in an associated circuit and is labeled' q8 I" @- S" F2 v& f& y
according- W- |: J% D' t* ?
A; Y6 S( D$ L2 U4 Z0 B* ]
th3 ?5 _% k A7 a
A, n! ]8 r& M8 h6 C6 E
w
( A6 e2 {4 N$ Dc3 W" T! G" ]4 Y/ Q% L$ G
通/ M# ?1 U, B& U
信号牌,4 S5 T- G& r9 l; r+ x, l0 O
由一系列指示灯组成的目视装置。每个指示灯都有相应9 H- V8 v# o. C' k' A( b
的标记,用来显示
+ n; i% {% u, J4 b情
$ m' x2 v* e- ~6 n1 ^防1 ~# N, h7 i" q8 a6 }! d j, W
防止机翼前沿和发动机短舱结冰的一种方法。! {( n1 r7 @2 ^
英汉对照民用航空词典B OEING5 N: _! ]. D" V: u. I" z' _
TECHNICAL DICTIONARY 12. R3 I* y' R% ^2 d8 {' o) \* q
APPENDIX, A supplement to the Airplane Flight Manual
* y$ L+ n; \1 c8 F+ S, i: }: O) Ftained in the basic manual. A4 Z5 s( n1 P- \2 F. J0 n1 Q
ollection of supplementary material at the end of a- K8 `$ H8 q* z$ w- _. X
ook.7 q7 H) V$ g! Q% h4 {5 s* A; ~' }" W/ C
of the. r; o- m8 _( A( l" V' q) d% C2 f
rsion link on the landing gear.: S- Q6 D& s9 E, C R) d7 l/ i0 l
APPROACH MODE, An autopilot/flight director mode6 f' d2 n# o: w1 Q, Y6 ~3 \
which is a combination of localizer for roll control and( |; n( ~9 W" n" q2 v" b
glide slope for pitch control. This mode is used when full# w2 |- x& p; ^; |3 w! D0 @
instrument landing system is available.1 j, F2 e# j4 o( q0 {6 n0 B
APU, SEE - AUXILIARY POWER UNIT( H: u/ e0 J: D) I; y) ^
ARINC, SEE - AERONAUTICAL RADIO% P+ V, _# n- b7 s
INCORPORATED
- b9 `( [8 [& @0 kARM, To make ready for operation.1 H4 Z0 t4 p* y/ Q1 ]6 b# @7 d. Q/ V
附录,# y! A, }0 {( D( Y# [+ S% D' m
飞机飞行手册的附件,包含基本手册中未提到的飞机形
2 t+ @& B, Z; F* @; U& h2 {- A态的其他性能。是附在手册末的补充材料。' Z3 Y9 E; h1 Z# m `
顶销,
5 R* C( B5 S$ M用于连接起落架扭力臂两部份的销子。- a& M0 D6 K" e; y; h
进近方式,
$ U) @ v2 x# T) { P一种综合了控制横侧的航道信号和控制俯仰下滑信号
3 p1 p$ p6 z/ ]% j+ O' c的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系
; L# [1 m+ B9 @, m0 e统正常时才使用。/ W+ [& h, W8 \) b0 a) _) Y! w! ?5 e
辅助动力装置,
0 q' |; v# x7 E8 h, k见Auxiliary Power Unit1 T1 A: E2 _& X2 F
containing additional performance for aircraft) F4 v: G4 L2 }3 v
configurations not con
$ g: d" T5 i; g1 ~/ Q& U1 s9 oc0 u" w$ ^4 c/ O1 A; P% p
b7 e& S7 h% ~, P* E
APEX PIN, A pin for joining the two sections% j" l5 W2 G$ p0 A( p Z4 S
to0 [* k- w, l4 G; s I% I
.
9 D6 n. }9 q1 w$ e4 J% T# ?航空无线电公司,
+ R8 Y8 ]" ]; W( \; k见Aeronautical Radio Incorporated.
: K8 o8 f9 ?+ Y: P: P7 h6 o' E4 r1 b预位,7 J6 Q# g+ L. `- K
部件可以开始工作的状态。2 @' f2 d$ k4 Y
英汉对照民用航空词典B OEING
% r& ?- w% `+ zTECHNICAL DICTIONARY 13' Q3 s7 d0 ~' C7 p
ARC, The curved track over the ground of an aircraft1 v: V8 `' K' v( x* w$ N9 C/ w8 B
flying at a constant distance from a measuring% ~9 w0 I$ S, T6 A( V
equipment (DME).1 m3 m, W9 [) S. F4 b3 F" ^& Y
in the limits of self-contained system* w9 [% ]9 e, T" D
apability.) H5 H; D& E5 a3 U9 Z" \/ T/ q
tem for opposing or restricting! G; R% ]5 L8 |% C+ e) d3 q
ovement.
4 q* f! }; r% v. G- j6 z8 G% MSPIRATED TAT PROBE, A sensor that measures total
/ H. Z8 r1 z1 }5 L; Y* `/ u! ^) Jir temperature when the airplane is in the air and that
$ h9 b5 b; y$ M, Z9 ^easures outside air temperature when the airplane is
! @. \0 x U! Q3 yn the ground. The outside air temperature is measured
" t2 u4 P6 j0 iSSEMBLY, The fitting together of a complete structure
& \, i7 \7 |1 K9 XSSUMED TEMPERATURE REDUCED THRUST, The/ H1 F1 ~4 k& f6 ^
ATC, SEE - AIR TRAFFIC CONTROL
0 T# K. i' V6 Z' s/ A7 \/ },
# R* D1 y7 K, x t6 e系统中所产生的一种用以抗拒0 L- Y2 v0 C9 x( D. q
作或限制动作的力。
; G$ \" \, t1 x/ N& K4 O头,
+ ?0 y r) U8 `7 m) ]; j. d7 U; `* h用来测量飞机在空中时的总大气温度和在地面时的外
, x& r0 @; y/ U X5 ~' W0 M温度。地面外界温度的测量是利用引气将外界空气吸入& T6 u% n6 ?! \
头,以达到测量的目的。
$ J) ?6 B2 v# _配,
# d0 N. a. G! X. u" t9 N一个完整的结构或组件的过程。1 ^: }% V8 O2 I+ r
假设温度而得的减推力,4 `$ A: d: ^8 M2 z& Q' l, }" I" U
推力设定值时,假定一个比实际外界空气温( p% K; v8 i2 j& p
空中交通管制,( }* V/ L1 o. U3 s; ? ]0 y
见Air Traffic Control
. ]' i% A; ~) M ?AREA NAVIGATION/RNAV, A method of navigation0 d* X2 s, v) `. ~! f4 E6 a
that permits aircraft operations on any desired course
& c: Y9 p9 A% m4 Jwithin the coverage of station-referenced navigation
* v0 I% U) B: [1 ]5 ^signals or with+ b% S9 g7 |* {% R. W7 G* U
c; @& a+ I0 {6 H* t* K
ARTIFICIAL FEEL, A force developed in the flight, N; x0 S- a. H* g) Y2 H
control or brake sys) {' K- A9 T" @3 q/ P
m
, ^7 q2 w! ?' y" U- G7 j# ?# B) x% `A
0 K! A2 S! }' e9 k q" N: Za
6 V) ]1 I; @9 l# w. N+ x) ym* R5 O% I) n3 T$ |( f
o) H; O8 u. }. r1 M
by using bleed air to draw ambient air through the
- c% N* C) N- H" o/ Xsensor when the airplane is not moving.- ?. S! j) b" Z/ x
A
# b( a) `; o. e. ror unit.
. \, D( R& G" d/ `3 y5 k6 KA
/ u! T1 z8 d7 |$ ?" glower thrust obtained by setting a higher than actual
3 f9 V+ H( q I- c5 _: R. COutside Air Temperature (OAT).
3 U6 s1 A5 q# I2 d; X' M: o! ]弧线,
* v" A. d+ p& P$ U" E飞机在围绕DME台等距飞行时的弧形航迹。
6 L0 X; O9 r" U) a' B区域导航,7 M: m5 E& N4 W z
容许飞机飞行在有电台参考的导航信号或自备系统能( d/ Z% u7 `: b
力极限范围内,飞行任何预定航线的一种导航方法。" ]! p/ S2 H4 O8 t
模拟感觉
9 B& Y: S2 N8 S% }在飞行操纵系统或刹车
% V& r9 A- R2 E* k动
0 i7 l* B ]- Y, `: d吸气式总温探
1 l5 U5 c0 g+ b6 M5 g界
) \6 l( \3 r9 Q& |8 }9 u( \+ o探
" ^) ~& }0 D* {1 i* S6 _- P装& a8 C$ P# l$ k+ b1 a
组合成3 F; L0 u H$ v6 g f m
由. u3 ?+ B! O% d! E v0 R
在选择起飞
% g. N4 ~) K' @9 V0 _: @度高的温度而得到的推力。用这种方法可以减少发动机的
+ n8 {6 W6 ^) P: } G磨损和维护费用。
4 g: R+ l/ q7 R.
# u. V5 j7 G* b+ e0 }9 C英汉对照民用航空词典B OEING
. ?, ^9 a0 N# G# gTECHNICAL DICTIONARY 145 x" R ^6 n- x" [5 X
ATE, SEE - AUTOMATIC TEST EQUIPMENT
1 Y1 `8 {7 N" m! VATMOSPHERIC PRESSURE, Pressure of air due to the
% e4 ?. X# z1 }. x- varth's atmosphere, expressed in pounds per square
/ u' x9 b0 F Lch (psi) or inches of mercury (in Hg) or millibars (mB).2 ~% y8 D6 G/ m0 Z' O+ `, w
TTITUDE, The relative orientation of the airplane with! B6 g+ e. N7 \ N' W
spect to pitch, roll, and yaw.
' W) v7 N$ F* d. S$ ^; R) Z JUDIO CONTROUSELECTOR PANEL, The panel in
# J$ Y: d8 T4 `% H) j) ^9 h2 f2 G1 oe airplane which controls and selects the routing of: \! _1 O1 @' q7 {/ P: g& A
udio.! R; Q" q) m/ u8 p
UTOLAND, Automatic landing using the Digital Flight: ]1 j% I( |* M8 {- m1 p2 r& R4 |
ontrol System.+ ^6 Y; k7 G4 @6 c8 [; {
n., S- j8 u6 V. M5 M7 V
M, A system8 Q8 ?% a" e( R0 D) g8 [
omposed of all necessary subsystems needed to guide! [5 j& U9 h# d3 E
e flight of an airplane.
0 X( Q+ g2 Y( VEQUIPMENT, System test
5 ]2 |) t6 \; _2 r. fquipment that operates under computer control.
6 p: S( z$ f1 {, v: a' k+ }& v8 h' Y装置, |
|