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AIR DATA COMPUTER, A computer which produc4 U4 O- a, J( w
data information, such as altitude and airspeed, based
7 g8 }6 M/ s+ K& g& |on pressure and temperature measurements. q6 F+ ?7 V y0 H1 y0 Y1 C4 j
es air% z6 t- L8 l0 `2 O! O* m
IR TRAFFIC CONTROL, A system comprised of
, |) E7 c, [7 Bround and airborne components used to identify, track( h; d% s- m3 _! ?8 H: f, m
OUND SENSOR, An electrical device operated7 T$ m* I3 J' w. w2 W, f0 v" z* d2 J A, y
y the landing gear, which transmits on ground/in air9 e9 d" T- K* u( ]. r
formation for system operation in flight or on the( b2 x0 _$ J9 O. c
round.# i, c. W+ j: S/ Z
IRBORNE VIBRATION MONITOR, The AVM takes0 ~: H. b$ k9 Z; v
e signal from the engine mounted accelerometer and- V6 n7 e; v9 O7 h
alculates the vibration on that engine.& c% S) y4 V1 e- m0 ?
corridor equipped with radio navigation- e# B: V; }+ }2 R; G/ Y$ \- ]6 u! Q
aids.
8 F. G0 g- @5 RAIRCRAFT (or ARINC) COMMUNICATIONS3 w( z. M" g3 C5 S
ADDRESSING AND REPORTING SYSTEM, An
" n- w0 m3 b$ G5 h O2 baddressable digital data link system which permits the
! `5 u6 l- f6 |0 qexchange of data and messages between an aircraft
+ Z# V+ K+ \5 b) U3 xand a ground-based operations center over a radio
0 v: l ~" z- s: O: Jnetwork.
: `& T$ j$ d. g% ?( IAIRCRAFT CONDITION MONITORING SYSTEM, A
4 r1 v6 }5 D7 t0 m6 usystem of sensors and recorders to monitor various. j. l* O" f. x( p; N9 } k
airplane systems' performance and status.
+ b) o I5 ~% A ^- X机,
- a5 ^6 {2 c# v ]4 G中交通管制, e. N+ b" [, }: C. E
一个由地面设备和机载设备组成的系统。用来对飞机进
d2 ?3 x- i& B地传感器,& c- }$ N d b8 v+ K
一个由起落架操作的电气装置。用于给空中或地面的飞+ ^! b, p1 W! T% H( |2 i
系统运作传输地面/空中信息。(有些系统只能在地面
) d8 S7 ^" G9 |' C用)8 u7 j( a3 Y# i& ~4 W' S3 t
载振动监测器(AVM), X9 f7 _- D! Z/ e1 `8 M4 {6 T
AVM从装在发动机上的加速器取得信号后计算出该发4 ?0 z3 V8 U- w& G0 N7 Z6 H* o, T4 U
机上的振动。) C% {% ]3 u( Y, r( y8 q
式建立的控制区域,内有无线电导航设备。5 z' ^" |; W! n) n" e: O
飞机通讯寻址和报告系统,' a* R+ o* O- i, _7 Z( l/ X
有种可寻址的数据通讯系统。利用该系统可使飞机与地7 h7 Y2 r/ k7 b. u/ P; n- s/ L/ h9 Q& h9 d
面操作中心通过无线电网络进行数据和信息的交换。 O; P- ]9 M7 V" X$ s
飞机状态监控系统,& w+ ^5 _) v% X9 v3 ~; W
一个利用传感器和记录仪对各种飞机系统的性能以及( X% y% r8 C6 R* n+ G
状态进行监控的系统。
1 w" }! t9 Z! H+ E, K6 ~A, m7 U% p8 p1 M: `# S( a
g) @7 b$ I7 z* a
and locate aircraft. a/ n+ k" U3 W. N
AIR/GR
5 `+ F* O$ s( ~& J9 c% gb. f2 j7 U {) k
in
& S' x3 y" {4 b) U- O& bg6 \9 c S7 O# v6 y" o
A$ b) X m% ^' k* V7 y2 u, |
th
3 g, Z6 I/ x! L5 |1 H9 @, ^c
3 o- W# j) K" s. W% I V) aAIR WAY, A control area or portion thereof established
% ?, `1 y4 }4 B' T. ~* j& }in the form of a
. U. C S5 E$ o1 K# k: O大气数据计算) j! V6 i4 X! Q9 \
根据量取压力和温度而产生大气数据资料(高度、空速
% m u: p4 P% d等)的计算机。
/ q* e5 b D, F# N& k- y' K) c空
$ y& p1 {6 s% T/ f( E' _行识别,跟踪和定位。% A7 C9 S! }' J+ v8 W4 P$ Z' C" C
空
4 a' e! }: w' R: B8 [# O. `机
3 H* T& k# N5 I; k( D使
- d" u0 q& ~5 w6 K机# J7 `9 U s' l) V* r i
动
* b, H/ x' J8 o. b航线,$ M" o9 T* B0 z" K
以走廊形. E; C$ b, O1 u2 F5 X! ^6 ]
英汉对照民用航空词典B OEING' i9 v/ g+ p* T; t0 q4 r. u o
TECHNICAL DICTIONARY 6
k& v# d- a$ R, [3 |: l9 |AIRFOIL, A surface designed to obtain a useful reaction,
3 U% b( _8 E" }" H3 h9 q/ { gsuch as lift, from the air through which it moves. Wings,
4 N6 m; K* H' c7 _% hstabilizers and control surfaces are airfoils.
4 p+ s+ N. d8 K B( |4 `AIRSPEED (IDS, TDS), The speed of the airplane
+ P6 A8 c( e" }$ B2 @# Grough the air.% r5 G+ ^9 d# C5 R
D INDEX, An adjustable pointer on the
6 u4 }' O! T0 {3 m2 p1 ^$ d8 Eirspeed indicator.* N4 [/ k: [* J( T# G) s
and legal ability
- l5 m% T9 l( Dfly.+ r7 I: r5 j- v$ Z0 f
m, for example, the procedure for finding the
" K# K9 E. s: xquare root of a number.
- J8 r2 r& N. W6 L. Z6 h3 ?y o/ H5 l- F( r! l) D" T' H7 |
re, wind,
! g- H4 s, }4 s7 j. b8 yand aircraft flap setting.
: R" C3 w n% t是翼面。( P4 M1 D0 h7 l8 ?1 G R. {
速,
8 F, x' O- D, o飞机在空气中运动的速度。" M) s( t2 @' N
,) l+ h9 D3 e4 g$ v g
在空速表上可以调整的指针。& G1 L0 n" l2 _1 b: K9 h
机械飞行能力、和合法性的飞机状态。$ E$ z- A9 d& ^( Q, J" u
一步一步的解题方法。例如,计算一个数的平方根的步1 E5 d* i' Q' s* `' [. p
。! J4 ]7 n ^5 U8 |& F4 c: `
能9 i$ Y% s& c7 Y. m1 p: X( o; @
资料的法定文件。4 Q3 H6 R$ k" P9 N' l8 u
翼位置成函数关系。
* M, d: |# P$ D( i1 N( Ath
& {- I2 E3 k$ s1 ^AIRSPEE5 a4 b3 [; Y7 G7 Z
a8 C" Z2 S* y, z" j% B( C
AIRWORTHINESS, The condition of the aircraft with
7 |& Q( f* k+ X) ]9 C2 ^" u; brespect to its aerodynamic, mechanical,
}3 I, G3 @! f% K" Y! M9 M* Rto! Y. g! a, @: b& a) m
ALGORITHM, A step-by-step procedure for solving a
# K1 e2 s* L& {* ]" f, O+ Cproble
2 d6 ?+ F8 _5 i! b. g1 Ss
3 g7 e; `3 ?/ j* i4 b& j' a5 r% KAIRPLANE FLIGHT MANUAL (AFM), The legal
0 e7 f5 w) f4 K: j4 Ldocument containing performance and operating limits,
+ {0 P7 ^0 f8 v; p1 Poperating procedures, and takeoff and landing5 K- W# `9 k* b$ D! [+ u
performance. o. @. q. {- |5 u
AIRPORT ANALYSIS, A comprehensive set of takeoff, e6 a4 E# ]& v, I
weight limitations for a given airport runway, generall1 r; g! G; A: Q9 ^5 C
presented as a function of airport temperatu" b' S1 W3 c! l" z% M# }" m
翼面,: y2 n j8 B y; \6 H& I
用以从气流中获得反作用力(如升力)的表面。机翼,
! u+ i' m% ~, d安定面和操纵面都4 E. }+ N" ?. T9 x1 [/ T
空& C v' F ` h7 a- m0 C6 `
空速指标. b# w0 g- w$ p
适航性,
3 J+ N7 b/ _9 n8 k+ }# W有关气动能力、9 ]% x* K/ D y E3 m# ?+ {
演算法,
' u+ z3 O1 X$ H$ V( X骤
# l) h, [7 _' r4 Z1 O3 x1 K2 G飞机飞行手册(AFM),$ H8 L/ X, o6 E: B. o4 d
包合性能极限,操作极限,操作程序,起飞和着陆性) F7 \3 t. _9 z" ~0 o
等. o& X" V6 Q1 _" R5 b
机场分析,2 g9 A5 E; ]# _+ F# D, ?
一套针对给定的机场跑道的详细重量限制资料。通常与! _. F$ |! s5 U L7 e T
机场温度、风、和飞机襟: I, a% E2 y: I7 S, p, ^. u
英汉对照民用航空词典B OEING! w$ w0 a; r9 g# E1 ~
TECHNICAL DICTIONARY 70 R' G0 ~2 N5 Q
AIRSPEED BUGS, Adjustable pointers on the airspeed. A& s4 h' Z0 I
indicator.
4 s1 ~3 _2 ?- {" Y+ m' eALLOY, A mixture of a basic metal and small amounts' k' i& v& H2 G. `' a. n
f other metals to change the properties of the basic
- ~) b9 e3 Y1 p$ M5 Oetal.
! O4 ]$ n* H" kMinimum airplane speed.( ~8 @; Y/ `% y. C) z2 j3 g! d
e of8 B1 W3 x$ i! o
itting airplane angle relative to. d8 i7 D# p3 P2 @3 c
irstream for the stall warning system." ~9 h3 H& D. _3 [6 s3 w
another.
& O1 F: x# _: b% uLTERNATE , An additional airport selected during0 T. f* m2 C5 s( E: h( L
,
8 @! @/ ~& C6 r: R3 _合金,$ T& E7 y: z5 V" a' O% [7 D- m
在金属中加人少量其他金属,而改变其性质的一种金属& \' g4 f' j% a0 e
合物。
6 O" v* A: A" m0 y# R; D$ s2 S [飞机的最小速度。, y/ V O1 w! S
速警告系统传输飞机对
) K z, q9 M1 x; n! Z. c流的相对角度。1 C4 [7 |" V; ^
由一个状况改换到另一个。
9 C* D/ ]; f( ]$ K+ W4 N7 u降场,+ g+ `' ~, p9 T& O
划时,除了目标机场之外,所选的另一个机* c. f/ q/ p7 v* R% [* b/ K
o0 f$ y3 ^. Y" a% W' r
m! _0 b- t5 Z, _; O6 P# {
ALPHA SPEED,0 m* F9 J0 ~/ \+ i5 R
ALPHA VANE, A small moveable airfoil on the sid& i6 K5 o) V: x q( x, o% X
the fuselage transm T+ J; x6 D% _# U" j* T. ~+ _8 t/ l( W: F
a
+ u, q3 M: v- F# ^1 JALTERNATE, To change from one condition to/ S# G3 \, o/ h+ z6 r' L! z( g
A
$ L* F4 X, f2 R5 yflight planning, usually near the destination airport, to be
! D: t) `5 X6 x/ ?& b9 vused when it is desirable to divert from the original
U0 ]( h, l) j( a2 ldestination airport.9 N0 u0 P+ {. p/ x" ^% D
空速游标' U Z: P( Q! b, F( g& L' x
空速表上的可调指标。
+ S+ C# L* E; e8 V6 b混2 d' q; f4 y+ d7 O. @- p
迎角速度,
m2 M5 _. p. M3 F迎角叶片,
3 W; x3 ] v8 p! l; V' Z& K位于机身侧的可动小翼面。为失+ X+ ^8 j8 d5 `
气1 D( }: ^6 P9 \% [+ S
交替,+ X, ^$ W ]: s3 O. @8 r4 D. u7 r
备. f( O$ m, r8 W( A7 P; v* i+ s
制订飞行计
# @+ U, [9 H) {& ^% v O, |/ i% X& I场。通常在目标机场附近,以备不去目标机场时,改降之! s; W- I" C: {! I# ^ D! ~) T
用。
* ~9 n! l6 V# D. r英汉对照民用航空词典B OEING
: R) r2 K% d; ^5 Y$ [' W! Q$ T3 DTECHNICAL DICTIONARY 89 f8 g( ?. s0 @( \9 j: J
ALTERNATE AERODROME, An aerodrome to which
' ?: W5 O7 F& f0 {6 l7 y/ kan aircraft may proceed when it becomes either8 m8 a( u; l; K% ]& U7 b
possible or inadvisable to proceed to or land at the p4 d" {# E4 N0 w0 c3 d. k$ I
erodrome of intended landing.. Y R5 |+ Q- {: a L T, E6 j
TER SETTING, The adjustment of the altimeter
! \1 ^5 F5 I) ~, u" Iaccount for local variations in atmospheric pressure./ p9 h& Y$ Y7 C* ^& Q
LTITUDE ACQUIRE, A digital flight control system+ o" v. }$ f. A5 e+ w" x7 N+ B
ode to transition from climb (or descend) to level flight.' i( Q- |# E) r! {% ~
LTITUDE ALERT, A flight deck alert occuring when the% |$ K% `- x: x& x
irplane approaches or departs a selected altitude.) U; ]% z" |' P0 Z
LTITUDE CAPABILITY, The maximum altitude at2 D0 g; L, r$ ]) T
hich the airplane can be flown at for a given thrust,9 w) T: A" A" ~! Q7 L( r; a
peed and atmosphere condition.
$ Q9 a& e+ G$ _9 G& V# ZLTITUDE HOLD (ALT HOLD), A mode of the autopilot
/ ~& M4 F$ s! j: \* ^% fr flight director to maintain a selected altitude.! S' N* b) e: T+ W7 B: s
irplane's altitude during VNAV operation.
0 j: r, x8 m/ M, X: i7 P& U# K机场着陆时,可作着陆使用的
+ J0 e; v9 L( z( g# e1 v; H8 l场。
; Z0 s- `- W0 l,
" U- {1 Q$ [- w( S( r0 f* C根据当地大气压力变化而对高度表所做的调整。
8 L' N+ N1 l7 u+ H. X一种数字式飞行操纵系统,从爬升(或下降)改平的模
! Q" U# [ g3 E。
) W# A, n9 P( v3 [- K( x' { s度警告,
% G3 [, J7 {% J8 C2 Z当飞机接近或偏离选定高度时,所出现的驾驶舱警告。
7 _% g0 f# ]/ T# L. s/ b- T高度能力,
% O) a6 x! v* L& ~ P9 v在给定的推力,速度和大气状况下,飞机能飞达的最大4 o9 [9 T& B/ M$ d0 |
高度。
* w+ e1 W. z [# H! Y高度保持(ALT HOLD),
0 v0 n. R# f( N! b- h自动驾驶仪或飞行指引仪保持在选定高度的一种方式。
0 w7 m; Z: r' j4 T2 C, h& B: J, V: A, w+ L! b3 G$ M
员对飞行高度的控制。
! Y4 Z8 f1 h% O" p4 ~! I* z/ Kim
# K# @: p/ R+ q' m( d' }" oa
* B) j0 s4 a- e, ~7 F8 FALTIME
! s* \ P0 Q6 Z: @+ B( ~+ Kto# Y7 k4 ]& E& d1 H0 H
A9 w2 X1 h" Z& N& q) H& M& K
m5 G4 b$ }+ j: V' M) P
A
3 P' p% Y$ j8 M' E; u" F" T! Da
, Y6 R4 w6 G: a' MA0 e8 Y3 o$ e+ r; _7 d* S7 {. _
w8 P# Z+ p& ]2 M4 E
s3 x+ o4 |6 u2 t$ L+ x! p( f- K
A
2 g# Z% i. `6 N1 p# L' xo
4 }; Q4 k W7 @5 I: JALTITUDE INTERVENTION, Pilot control of the1 I' e$ f* g) g
a
* F7 Q4 P0 D& [+ _( uAMBIENT, The surrounding atmosphere.
6 E: x5 H) \/ n" K2 c6 @备用机场,6 {, ]/ y8 E0 J U5 @: ^1 s
当不可能或不适宜在预选
3 C. D1 ^# q ~& J% s; }机: X( _. I2 U" B2 e% n8 b
高度表设定
# \! \+ \7 k0 x8 K# `% t高度截获,
; R$ V" S& F+ ^% C& F: w式( C* _2 S$ w9 e6 d
高
( e; x4 y6 h, O" z( f( H高度干预& d q% d% Q! y8 [# n
在垂直导航工作过程中,飞行4 p5 s. M4 F- N! x
周围环境(地面气层),: @- ~7 g5 J; U
物体周围的环境(特别指大气)。7 N6 U+ c. ]. b1 [' I! ~3 F
英汉对照民用航空词典B OEING
* w5 @+ L/ Y1 O0 F9 \' G0 [1 ]* KTECHNICAL DICTIONARY 9" _* N8 v, ^5 M2 \7 ~) e
AMBIENT PRESSURE, Pressure of air surrounding an& A/ X2 g+ s' k
object, measured in pounds per square inch (psi) .. D8 N# A( @$ Z3 l# S7 y7 l
MBIENT TEMPERATURE, Temperature of air" m$ U" s/ A3 `- E2 c
mpere.& f, K4 z# I! ]5 |! y9 a
urrent waveform.! \1 t+ b! q. l. o
g an0 u |. `# c' c* P# ~2 [) N
nalog signal to a digital signal.
, y. C% |% h: u! k ^+ ?, ?ore inputs
[9 M" D5 S2 V2 \: Af binary digital information and one output. The output! p! j+ Q" a6 i' y3 S
1 only when all of the inputs are 1. The output is 0# O) |; L( y* D# Y8 U' |
hen any one or more inputs are 0.& |- `* G/ y" \$ Y6 Y! [
面气压),
% d* q6 g9 `# E7 d {7 i1 s' Z' ]境温度,
$ h) B% X5 C& N' ], Z气温度,用摄氏度(°C)或华氏(°F)来
; ?' ~) `* z. X+ e% O( `3 p, @。( u4 k; h5 `. j4 D- w. ~6 U
电压或电流波形的幅度。
& A0 j& o. z7 q0 G性变化的信号来工作,或产生连续性变化的信号8 V. w# `+ l- R4 s1 R
统。
* V+ u! e+ w2 v7 a; ~9 D将模拟式信号,转换成数值式。
. l2 y7 x6 o& x一种有两个或两个以上的二进位数字信息输人,一个输
7 H% _9 D# x: a7 o的装置或电路。当所有输人为1,输出为1。当任何一个9 d" ^5 O' X0 l% S8 q) q B- r! W
一个以上的输人为0时,输出为0。
0 D* F- t! F; S2 G9 LA4 V/ w. l* u u. B) T8 ^4 @
surrounding an object, measured in degrees Celsius+ ?! t# i) g& F% V6 a3 x
(°C)or degrees Fahrenheit (°F).
( x3 M1 @0 J% B, m$ B1 pAMPERE, A unit of electrical current. One volt across7 T" q2 \0 W( p+ a1 o% k
one ohm of resistance causes current flow of one; a, d' [5 v+ @8 F, s, b J& ?
a
! w& b/ H/ k* F$ ~3 {AMPLITUDE, The size or magnitude of a voltage or, x% Y1 ~9 |9 M6 E8 G3 Y
c9 H. X9 G4 ]4 j5 V; `4 n: v7 n
ANALOG, Quantities or representations that are8 ^1 l; a, H4 M7 s$ V& i6 a
variable over a continuous range.( ^: B7 X& f+ [/ W
ANALOG-TO-DIGITAL, The process of convertin6 W! z2 O% N r% U, j$ O: i+ y' B
a
1 @- Q1 A$ C- X* bAND GATE, A device or circuit with two or m
3 W$ b1 n. Y- Y9 \* {o$ `5 ~ Q# j* O2 |8 s9 F
is
$ Z; j- Z7 p/ P$ lw9 J7 [1 s$ T- K1 b
环境压力(地, ?6 x5 D$ j+ X) t+ X7 F8 x$ f$ I
物体周围的空气压力,用每平方英寸多少磅(psi)来
; C e) y, V& f, k4 n/ `/ J4 D1 ]度量。! r4 r8 O" c/ w3 k
环 L! r1 e4 c P8 J9 j
物体周围的空- g# e6 U) M9 ~- M4 a/ V4 @
度量。3 P3 j' R0 q; d; ]; `1 c& G
安培,
( I( G1 Z( c9 v$ A/ Q电流的单位。
B0 [3 N& X, w! R$ \1 ?. e1伏电压在1欧姆的电阻上所产生的电流为
; o- J1 E6 m9 ]4 d/ m3 _8 q* B1安培
: |& Y# V) }& R( a& m* O振幅,
* k' ]1 |( A I) {8 y模拟式,# x; D8 s3 n4 E/ P; U
用连续1 r' F9 z/ o: r" J
系" d- Y/ a* T9 z& m
从模拟式到数字式,4 [" j: n6 ^5 q G/ G
与门,
! `4 ^4 f* M. S出( O: i; u( o: u' m% g w
或
9 t8 Z! G, M3 @0 a9 S! F! g+ Q4 b英汉对照民用航空词典B OEING
- a& ^/ O4 k3 u% W8 C0 [! qTECHNICAL DICTIONARY 10
& u9 r ^; ? k$ xANEROID, A sealed flexible device containing air at low
6 Z, t% f3 r; X% y- e& u5 Cpressure, which expands or contracts during change of
e- H6 ^# k) g0 {ressure outside the device.
, j, ?, y0 {: x/ H! @) Sically
7 k$ r- w8 v8 k; @r changing the direction
7 b' T+ N; C9 G& ?, T q: Xf drive.
) }: S& A* |( I. u# M6 ^8 Cof the wing chord in
: E5 Q: V# F/ `: ?8 r0 X: xlation to the free stream airflow as it moves forward7 t+ d. L1 Q3 O% @2 V2 f
rough the air." G9 \4 o( m1 R
al axis of the
. d' z' {8 g2 gaircraft.2 z" W( j% o8 q9 ^, I
胀或收缩。% F; [2 Y. o* s e3 I+ a: U6 t1 k
箱。是改变驱动方向的机械装置。
8 K* T: K3 V3 X: j- I7 Z3 {7 W5 k机翼翼弦在空气中向前运动时与自由气流之间的夹角。! P* g5 Z* r/ r. n
。/ M1 Z9 ~8 O* ^1 A0 j1 k
p
3 J8 v& H c' n- DANGLE GEARBOX, A part of an engine, mechan
+ V" j$ p4 f4 ~0 G: udriven by the compressor, which drives the accessory" h. U* U( I2 A# A% E
gearbox. A mechanical device fo- |5 d6 m4 |1 ?8 i2 @2 ?
o. N! [0 ]+ P4 U" @- l0 W E, g0 S" E3 w
ANGLE OF ATTACK, The angle
, B' T+ |6 q: y/ Tre
3 o! ~- T3 l& c2 X4 {6 V+ ]th, x, Z$ [6 `5 {0 ]/ h s! b$ G
ANGLE OF INCIDENCE, The acute angle which the, b+ e0 ~) e8 w' O, P) O
wing chord makes with the longitudin0 I: f: O ^; ]7 c1 x; u
膜盒,
# J( n( c2 h0 d内含低压空气的密封弹性装置。当它周围的压力变化" h' N2 i0 j j7 @+ M0 n! R3 L* ~
时,会膨, f( y! H1 X+ k0 Z9 ^0 O' Q
伞齿轮箱,- e* X- d: Y. w5 G, j" ^# [
发动机的一部分。被压气机以机械方式驱动,然后驱动% l; A; z* k* @
附件齿轮
8 i7 m+ X4 f9 H" I0 M迎角,, k6 O6 n8 j& o* V/ ?
安装角,
! e! I0 x" s( {飞机的纵轴与机翼弦线所形成的锐角
! Y# b: u1 t# `! G英汉对照民用航空词典B OEING
2 C! u) m# k8 ~TECHNICAL DICTIONARY 11& O& E! Y' j7 d5 \" d1 k U7 Q
ANNUNCIATIONS, Audio or visual indications used to
: t4 S& Y9 C- m9 D) jcall attention to an event that has taken place.. |1 T4 p+ d0 t, x. f& t
ANNUNCIATOR, A visual device consisting of a number
6 i x6 D8 ]3 q, l5 qly.
/ ?7 ?( p8 v- k3 LANODE, The element toward which the principal stream
* i/ i8 d' Q: u8 jof electrons flows.0 ?$ q5 N" f6 B) S7 Z
ANOMALY, Not normal.- B) o2 a* f3 T/ Q! O
ANTENNA, A device which, used in conjunction with a& j. p5 P& H1 Q6 W. W- W% ^; |. o
transmitter or receiver, is used for radiating or receiving& x- Z4 @8 C0 b2 l$ {- w
radio waves.. x8 T' R$ p# |
NTI-ICING, A method of preventing ice formation on
# y8 {7 t6 p8 ]& }0 m! [e wing leading edges and engine nacelles.; W8 L$ l0 k9 Q6 f5 D, C# s! @2 i2 T' W
NTI-SKID, A system for providing maximum braking
2 Y" B2 M) U- z. @6 Jithout skidding for any runway condition. Anti-skid0 p& ^) H* T+ r; X& u# r5 S" b0 R% h
omponents are part of the brake system.
" O+ l3 K6 @' V" ^5 {+ d/ ]1 b! ^告,
# o' w; r6 x5 d d! Q! s当发生事件时,以声音或目视指示形成的提示信号。
' A6 q5 g8 ]- F6 b" H与之有关的电路的现有情况或已存在的
* O! h$ t4 V+ m3 C$ \8 ?况
' o! f' V' J4 l0 J1 C正极,( q5 [- D. E5 f- N
主电子流向的极位。+ U! `$ n' M1 a, q) ~0 @
异常,
P! C' F+ ?" O7 b0 Q不正常。/ X1 ~" c, f d- W. c9 {- C7 G
天线,
/ C6 m0 Z8 {) ~/ j一种与发射机或接收机共同工作来发射或接收无线电
9 ?) L W w) l9 g, L波的装置。
$ X$ |( _, q. P( B% o' @冰,
, _7 a$ q* p5 l4 I* x" S+ L& b! k防滑系统,; S( R+ [, B+ w% [9 t
一种在任何跑道状况下,都能提供最大的刹车能力而不
/ i) B$ d$ S V/ u! ~# l2 r使轮胎打滑的系统。防滑部件是刹车系统的一部分。; c8 ]: l% ?% ~! a5 @! I' t
of lights. Each light indicates the condition which exists% z3 M( X0 s. E/ I& X( n- m
or has existed in an associated circuit and is labeled- h% i6 ?+ n" |1 ^! u$ r! }! \- U' S6 [
according
' F' |! L' [3 R" [* M! IA
9 o+ H2 ^3 P- H9 W0 x, P) Uth: o. f( C, X; O9 S
A
: ?# S3 f5 K I& f! `/ _1 uw
9 Q! N0 E, i# e4 d; k% |c
. Z _. W3 o+ M# F% w" n$ f通 f* W/ A5 L) U( w4 T
信号牌,
2 C# A& \8 b( `7 f) R由一系列指示灯组成的目视装置。每个指示灯都有相应* ?% [# \$ e7 O5 p2 f; J
的标记,用来显示* T6 A9 ?" Y! r
情4 P! i; ~% l$ g
防
( Y/ F) a# A, t9 P0 w防止机翼前沿和发动机短舱结冰的一种方法。
[4 v+ d3 P& p/ g5 ?$ m& u7 P英汉对照民用航空词典B OEING
% {1 n3 S9 f: i& l0 A% [* vTECHNICAL DICTIONARY 12
0 _' f( ?4 J" w+ `$ ]) h# T" sAPPENDIX, A supplement to the Airplane Flight Manual
. w3 t `- l9 h5 I* Jtained in the basic manual. A
! {* X6 W: }* n' U. t1 z D5 }ollection of supplementary material at the end of a
& F; x4 }/ M# zook.
5 c& [$ I0 u! @; d2 r# n7 aof the- A, ]0 J( ?; q) Z; k n4 [+ a
rsion link on the landing gear.
" H6 _) F- i. b* O7 w) zAPPROACH MODE, An autopilot/flight director mode# L9 G: S$ ~3 X
which is a combination of localizer for roll control and
# o, E$ \9 h7 s+ s6 H& gglide slope for pitch control. This mode is used when full
& |, _6 L) G4 w0 s6 D, binstrument landing system is available.
7 S6 M* y" @ L5 L! ^1 pAPU, SEE - AUXILIARY POWER UNIT. l2 J/ S+ u& J3 W5 r/ d
ARINC, SEE - AERONAUTICAL RADIO
! z) W: Q8 p/ B1 @' tINCORPORATED
$ l B* T- w* D% [ARM, To make ready for operation.
# p$ z2 r% B' c: ~8 l+ h4 [附录,
& X6 e5 @7 [. x! M# ?6 {飞机飞行手册的附件,包含基本手册中未提到的飞机形
5 ?( q6 _* P% E' c; M4 E* b( M3 s态的其他性能。是附在手册末的补充材料。& _" X5 \* I$ ~5 ]: c5 S/ ~$ j! l
顶销,
( C+ k0 O' p' z8 ?/ h用于连接起落架扭力臂两部份的销子。" u. u* f4 R! A6 o! ?+ c( Z2 W* L
进近方式,
+ g3 C1 R7 U) n0 L一种综合了控制横侧的航道信号和控制俯仰下滑信号- ?1 ?1 l: J; z9 t) d
的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系( F9 W v" X! a8 {+ ^# a
统正常时才使用。
* b2 U8 b" h& r$ l6 j辅助动力装置,3 d3 Q& ~' R" \0 F6 I' g7 j; k3 E' U
见Auxiliary Power Unit$ q6 m( i$ q7 I R: [; a/ n U/ N
containing additional performance for aircraft$ Q& Q" Y. `1 Z$ [& X" S* x
configurations not con; V4 O8 P |7 w. S* u: S2 f
c
7 Z8 b- G5 l, T# n6 n/ k' jb
- n6 d% k& z- x5 c: F; A' ^APEX PIN, A pin for joining the two sections; a; K# H% F2 h$ P; a7 g
to# ]$ e* \/ Z z- B7 O: o
.' B6 |8 J8 E; S/ A% ?4 n9 ~3 k2 M
航空无线电公司,
( O. v) `. t* M, P! E0 f B见Aeronautical Radio Incorporated. e0 i3 J; y1 \1 \! D& `
预位,# J; v1 `% v8 ]9 F1 Q, I1 E' L
部件可以开始工作的状态。
5 d" l) @8 Y( E w: M0 [英汉对照民用航空词典B OEING
6 F( W9 O5 j" P1 j. {: a |% f# eTECHNICAL DICTIONARY 138 a5 m' g( N/ v/ s' ~; M
ARC, The curved track over the ground of an aircraft8 g+ z z' X1 _: ]
flying at a constant distance from a measuring& z- I, |- x C N( |( y a8 m
equipment (DME).3 m: t2 t7 _2 J2 C. I9 F2 H
in the limits of self-contained system
6 w: R0 a8 x; [; W4 \# capability.
% C4 R" A2 o' y" ]7 ~" X$ P1 ctem for opposing or restricting
9 b& ]/ F0 y. v+ ^! D4 G$ Sovement.
& F, e+ Y; h7 _. R& tSPIRATED TAT PROBE, A sensor that measures total
0 d1 j+ K' L* n& \9 o$ @8 Pir temperature when the airplane is in the air and that$ H: |/ K3 S2 d3 @" I+ L8 T* b
easures outside air temperature when the airplane is
2 j" Y) n# r: _ u. }n the ground. The outside air temperature is measured0 n1 P( b4 X% n5 {: \3 L
SSEMBLY, The fitting together of a complete structure) C* h: f9 ?& d9 ^2 u
SSUMED TEMPERATURE REDUCED THRUST, The O. z) G d: h0 j3 j8 a, w) B
ATC, SEE - AIR TRAFFIC CONTROL
- l7 D3 E$ w3 n) A+ ]) W,% V) }- p7 b' D- }* F; V
系统中所产生的一种用以抗拒$ G+ R/ o, r6 p+ L8 ^& l' f: q
作或限制动作的力。' L F' x: Q( c7 g" ^5 `$ q+ B$ d
头,
; r$ `9 {" ?; _: J+ L用来测量飞机在空中时的总大气温度和在地面时的外: ~; c2 I% Z/ z- H2 g6 J
温度。地面外界温度的测量是利用引气将外界空气吸入
6 a1 S8 p) ?2 g+ T, }9 ?头,以达到测量的目的。
# I, O1 D0 g5 s配,+ E5 Q; g& P1 j- b* m9 h2 r
一个完整的结构或组件的过程。! ]% J! T3 R) M1 Z; n4 B
假设温度而得的减推力,$ G C& J2 _* Q, g8 l. {8 i) Q' J
推力设定值时,假定一个比实际外界空气温6 n- v+ m' ^8 l6 L
空中交通管制," W8 u) S$ E1 q" ]/ v
见Air Traffic Control7 i! b4 }( c! d
AREA NAVIGATION/RNAV, A method of navigation2 u3 x: Q' O- ]2 o# m! B: ?, R! Z
that permits aircraft operations on any desired course, M% }4 z3 G% ]" R( G1 n4 g4 l1 b
within the coverage of station-referenced navigation
' U& U) p5 Y/ O3 w% n# g1 `( A K1 Dsignals or with
$ r% M3 w9 K$ J( sc, ~* T$ V; s# f% r
ARTIFICIAL FEEL, A force developed in the flight0 f% P1 M7 ^/ |9 m9 B3 S8 M
control or brake sys! \+ P* T$ y+ {8 t G& S$ K: I# [
m4 ?* z5 X3 a- T Q9 }; M$ `
A
, f, }/ s8 W+ z1 pa* E4 G$ q q4 H5 w: L
m
0 w& [7 S- q5 a, m8 J: a& H3 G {o" G }$ ~0 y! ]$ n8 j: L( {
by using bleed air to draw ambient air through the
8 S+ N& {6 w/ D7 osensor when the airplane is not moving.
" ?+ N' {/ I: U5 ~; P4 [0 RA
5 u' T) u& U) x5 `* Qor unit.3 c( E/ r# X8 w% G/ V% p( I
A. D% K9 \$ M3 E' W% H
lower thrust obtained by setting a higher than actual b) d w0 D4 I# b5 ^
Outside Air Temperature (OAT).
" ^$ ~! a' q$ Y弧线,
( N0 P# @( ]/ a7 x+ Z% v飞机在围绕DME台等距飞行时的弧形航迹。
8 q% G" w, l9 t区域导航,; ^6 Y2 X) v, ] z. D8 b" G8 b
容许飞机飞行在有电台参考的导航信号或自备系统能
) S m) G4 ~( Y; z9 k! W$ W力极限范围内,飞行任何预定航线的一种导航方法。
8 }7 S! L% P Z模拟感觉
! h& T( [* S" h: K& x在飞行操纵系统或刹车2 U/ N2 r; z* v) n9 l
动5 F9 e* N# A" Q- p3 U$ p7 J
吸气式总温探
8 \# s7 F$ V/ t5 t6 q- k: v界; ]! {- p4 C2 S& z
探
/ {8 O$ o" D$ P" O. E7 Y装4 E2 f/ O) s+ m+ m
组合成9 S! d1 t5 c4 }5 _3 t7 I
由
6 I* J$ k' b$ E2 j在选择起飞
8 {0 v4 T1 f6 c- T2 @度高的温度而得到的推力。用这种方法可以减少发动机的
) ]2 g z6 ]/ p7 n7 p6 v; W5 |2 `磨损和维护费用。6 {) l1 y& P$ d8 i
.) j Y/ t. m p3 ^) W
英汉对照民用航空词典B OEING! H! r- _* L' N+ q# V) Z: e4 @
TECHNICAL DICTIONARY 143 K6 {2 c O6 j# e8 m8 `
ATE, SEE - AUTOMATIC TEST EQUIPMENT H: I6 R; Q* u$ N
ATMOSPHERIC PRESSURE, Pressure of air due to the9 F# {* o0 S4 {. _& ?+ p% U, k1 y
arth's atmosphere, expressed in pounds per square
9 K" F1 v) c' \$ f4 ych (psi) or inches of mercury (in Hg) or millibars (mB).
: B8 C7 n1 K5 H, A# o5 ~" G* E) YTTITUDE, The relative orientation of the airplane with
, s$ \; [" ^9 f: c. m- jspect to pitch, roll, and yaw.3 R- f2 {. j% F( x( e2 j8 ]# e( R
UDIO CONTROUSELECTOR PANEL, The panel in, n2 u z9 v) B; T( g) S
e airplane which controls and selects the routing of
+ z8 q6 H/ n) u7 L6 r' y( Vudio.5 L( g1 e" T0 {/ f, t, g
UTOLAND, Automatic landing using the Digital Flight! W' l0 f" Q S' P2 A
ontrol System.
: e$ J( m2 i% _2 P- P/ \n.3 V) U) ?$ A2 f+ H
M, A system! C `0 Y" z% p- ~: q
omposed of all necessary subsystems needed to guide+ G1 n' s6 T+ _7 m$ ~- x) w s |
e flight of an airplane.3 Q0 y% i; |0 F9 v
EQUIPMENT, System test
) Z/ w& c* u9 y3 I$ ~quipment that operates under computer control.4 P: j5 ? ?% m9 ?6 X# E! g
装置, |
|