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AIR DATA COMPUTER, A computer which produc
( o. f1 L7 j9 `& _: j# ~data information, such as altitude and airspeed, based/ `; P0 g3 D% Y7 Y
on pressure and temperature measurements.) M9 ~2 p2 b& n! z
es air
3 j4 n1 I6 d8 K% ]; _0 U, ~3 IIR TRAFFIC CONTROL, A system comprised of5 d F" j- s- Q' [3 A7 s
round and airborne components used to identify, track
8 ^) _9 D4 U- D) V. y' [4 ~7 QOUND SENSOR, An electrical device operated0 J$ a6 F) R$ \% ?# j# W7 b* A
y the landing gear, which transmits on ground/in air
3 [5 }0 ?# {+ |0 Z% W: Q* Kformation for system operation in flight or on the( H- s% ]+ r! T# S
round.2 S; e. T/ Z% e9 P. a) a5 v9 ^, q
IRBORNE VIBRATION MONITOR, The AVM takes
3 @4 v1 ` N0 h) F0 q; ~ de signal from the engine mounted accelerometer and
* r6 K% F9 O! I Falculates the vibration on that engine.
; A9 {1 F, W9 L/ Rcorridor equipped with radio navigation
& ?0 n! J& A( ]aids. {& B) V# k( p0 v0 r
AIRCRAFT (or ARINC) COMMUNICATIONS+ t+ E1 q c$ O" ~& H. W
ADDRESSING AND REPORTING SYSTEM, An' L, N7 P( o9 L" T1 Q7 o! ]3 P4 c; [4 d
addressable digital data link system which permits the8 _3 y. p" M, H0 ~1 H
exchange of data and messages between an aircraft# @7 H8 Y6 L1 y4 }4 |: \# l* A
and a ground-based operations center over a radio- A- K9 [6 C/ c2 ^/ z0 }( v6 s
network.% Y' K# V; d; d
AIRCRAFT CONDITION MONITORING SYSTEM, A
# Y' b* u. V# G+ u: Nsystem of sensors and recorders to monitor various
0 j' j X& l6 \& Nairplane systems' performance and status.% l) h, i- g& j
机,
- Y3 z- z! I; ]$ \中交通管制,
* j. I. I! Y8 Z( b X一个由地面设备和机载设备组成的系统。用来对飞机进
+ ]+ o! ]0 u$ Y地传感器,
3 S" U- {: D1 L0 w# U# z2 `- h一个由起落架操作的电气装置。用于给空中或地面的飞
5 ^9 m) E, f- x1 a! Q$ z* J _系统运作传输地面/空中信息。(有些系统只能在地面
2 c ~& u3 ?" _( f) s8 m9 \用). Q6 G4 X! A1 p& u6 Y
载振动监测器(AVM),
~- ?2 y. n9 z: u& zAVM从装在发动机上的加速器取得信号后计算出该发; u- K! A- x% F. K
机上的振动。
* X; f( g4 {- N) M9 @# H- G式建立的控制区域,内有无线电导航设备。
- o8 I- C4 |, D5 H% W- q# s飞机通讯寻址和报告系统,% i0 B8 `- N$ _8 _& `; a
有种可寻址的数据通讯系统。利用该系统可使飞机与地
; i4 h* q( o" c) f. O& c面操作中心通过无线电网络进行数据和信息的交换。4 c8 J) C" k _& ?: F
飞机状态监控系统,
" O; r+ G: _" p9 h一个利用传感器和记录仪对各种飞机系统的性能以及
& m. N/ Y- O" A" m7 r2 T状态进行监控的系统。3 j' G5 l2 q5 D4 A: Z- Z; M
A
5 g/ P2 G6 a; \g
1 ^- F- g+ M2 u- T7 l! t$ u% Tand locate aircraft.! m: _+ ^7 A0 C$ N, ^0 r- {, j
AIR/GR
3 T/ u2 c8 W/ M$ ]" P1 b: ob
' w! j e: a; M8 U9 ^* Ein9 ~. W# O* S1 l2 Q$ D
g! l$ H# D( b" x" }
A
7 v4 ~, ]1 S( i; e$ ]th
7 P' I, O1 f( \% {* [c
2 C7 i( [/ I6 \AIR WAY, A control area or portion thereof established
& J0 ^" d: M) u& s$ B; pin the form of a
, _, }3 [* I' K- T大气数据计算
- t; h3 g% M7 N( s: O9 p根据量取压力和温度而产生大气数据资料(高度、空速$ o3 S0 a4 @, \0 ]. Z' E/ T
等)的计算机。4 @2 H2 ^6 |2 f: O
空
5 b% c7 E" w: c( h0 T. V行识别,跟踪和定位。8 M- u/ ?3 H( T9 }; ~8 w6 X
空
9 p, o4 {- X2 _机- f7 }- ?$ n0 J/ ?
使
0 _7 h0 _ D/ w) e* m7 Y机5 Y# |- C( ~! H: n j
动
3 E( x! \5 S0 P. @4 w# k+ e航线,
# C8 t9 g0 w' r4 w) B6 ?以走廊形; v* |( _- G8 v% I9 X; s+ A) C
英汉对照民用航空词典B OEING0 e! `' }% q4 c" a. z0 h
TECHNICAL DICTIONARY 6; z2 K( e- A* M/ k/ V
AIRFOIL, A surface designed to obtain a useful reaction,
* l3 G1 v6 R O; s: s+ g$ ~+ Esuch as lift, from the air through which it moves. Wings,
/ Y8 z" D0 G) u, ^4 E8 l9 X) {+ Zstabilizers and control surfaces are airfoils.
: x0 S3 g4 _. `, y( i2 G/ m) BAIRSPEED (IDS, TDS), The speed of the airplane) X4 u0 Z& Y$ t
rough the air.
4 B" O3 n) a ^. k6 f% e% rD INDEX, An adjustable pointer on the; \' [9 F9 k$ z$ O+ ?- y
irspeed indicator.% M, Q! S) h2 |3 q
and legal ability6 }- v6 S) F$ k& g- c6 n
fly.7 l7 C& w& t. E& e* M8 q+ \
m, for example, the procedure for finding the: q4 h2 \9 \) s; s# [; @
quare root of a number., q7 p% t& l f/ F* w
y
- ]0 [6 G! ^* r }) k2 Q1 C% t9 ]re, wind,
5 J9 X* p! M, O1 |! Oand aircraft flap setting.5 _- k& I% Q3 M% l1 H/ ]0 \# b
是翼面。. e) n0 S; D, o% V4 b
速,* \% ^, b5 v; s8 I3 D
飞机在空气中运动的速度。
b/ C/ t8 h& _,1 F" k0 ? h% h; r. n8 ]% ` U( \( U
在空速表上可以调整的指针。
7 a# R4 ]4 j# N) X) C机械飞行能力、和合法性的飞机状态。' S5 z3 H+ r1 h w. m8 p
一步一步的解题方法。例如,计算一个数的平方根的步
0 ?* o4 U9 x" V2 O- y; p- \。% u2 m' A4 U# w3 g5 B
能
" H- }& K: H! ^5 a- j资料的法定文件。3 M- q$ S: V* Z7 m' L0 b' R- g4 I
翼位置成函数关系。' m6 s) S+ |0 }% [
th
" Q3 \/ \3 v* @9 H6 U$ x# FAIRSPEE" ^$ f8 v! y' Y0 l, [3 b1 u4 [8 M I
a; T3 j, o# _+ ~6 {! J
AIRWORTHINESS, The condition of the aircraft with; v6 }) [/ X9 @" H- T* p
respect to its aerodynamic, mechanical,
" F% w$ S1 @& O6 H& y; ]0 Oto, F2 {2 O5 i! ?+ r( ~5 p9 `2 \
ALGORITHM, A step-by-step procedure for solving a
1 y7 J8 f" P+ L6 Xproble% d9 {8 o( B7 k) b8 C# \7 }
s
& T8 q* a i4 f9 a' K$ @AIRPLANE FLIGHT MANUAL (AFM), The legal1 P4 t$ A2 Q% Z4 l8 ]
document containing performance and operating limits,. h9 t( p" j e
operating procedures, and takeoff and landing+ j; x6 v$ F# d, ]% U6 |
performance.
$ q% \, g3 l9 j1 ]AIRPORT ANALYSIS, A comprehensive set of takeoff! b# A1 X: j* M1 Q
weight limitations for a given airport runway, generall
: s! n. }8 |. B- ]4 `presented as a function of airport temperatu0 X3 G* v1 {1 d, c2 V
翼面,8 y4 L& I* F" g$ t
用以从气流中获得反作用力(如升力)的表面。机翼,
8 |" [% F- O$ E1 l4 B i* j! m安定面和操纵面都# d. n2 D0 P3 _$ M5 q! w' _
空# [; T a! C: W- y0 x
空速指标/ o( ^5 w( I+ C% }: U) @
适航性,% }& X% k* R: f9 B. q8 S$ F
有关气动能力、
8 S3 D& k8 h* u! X& P! q演算法,) F) L' Q9 ~: Y3 p
骤
6 F% o$ Q# `+ f4 a& C飞机飞行手册(AFM)," k; {1 s | \5 @/ T; J8 [9 N
包合性能极限,操作极限,操作程序,起飞和着陆性4 \9 s% j+ v: O; Z/ S! k1 \2 S
等: Q$ e4 R5 C, u
机场分析,/ X, [# m) R' w3 b" B( D! p$ J, b
一套针对给定的机场跑道的详细重量限制资料。通常与- ^/ ~% B4 ~) ?
机场温度、风、和飞机襟! s7 I0 `, l" {$ c3 |5 @+ c
英汉对照民用航空词典B OEING. h, T [$ _: h9 w3 c! Y
TECHNICAL DICTIONARY 7, d9 E. P" r8 V s5 _8 O$ d9 d
AIRSPEED BUGS, Adjustable pointers on the airspeed; o# A5 g4 o; D
indicator.4 d% X! ^$ V1 d H, m# O
ALLOY, A mixture of a basic metal and small amounts, Q# o& X1 z2 C" _9 v
f other metals to change the properties of the basic# E8 w" a; y5 L
etal.
2 J/ F$ \- M& ?7 vMinimum airplane speed.& \+ t0 a& N( a! r% R
e of
% `/ Y7 Z! }2 {itting airplane angle relative to# W0 W# W% o/ k
irstream for the stall warning system.$ o! e; @1 x/ T
another.% S* ~+ D5 X+ S
LTERNATE , An additional airport selected during/ S3 Z6 ~0 b' ]0 C
,0 \: b/ j d/ U( \) W# n
合金,6 q- h( C3 D5 C8 r. _2 v8 y
在金属中加人少量其他金属,而改变其性质的一种金属
& j5 I- b/ p2 V+ U2 k4 E合物。+ h4 K& G! |7 v2 u3 T% ]5 c0 y3 Z
飞机的最小速度。
) Z% e1 }& n2 }! h速警告系统传输飞机对* m3 F& f" [! f( y( ^
流的相对角度。, K. r% ?5 a& J( ]' q2 C
由一个状况改换到另一个。6 k$ y5 Y9 t- S
降场,
; e/ b! W% u% B% F8 q6 v划时,除了目标机场之外,所选的另一个机
9 Y2 n0 Q( C% N- {o
. \) a; a" M( s& w) n9 Wm
7 Y9 q+ C0 d0 E8 b1 J8 ~' ^ALPHA SPEED," y) }) {: d& {
ALPHA VANE, A small moveable airfoil on the sid
0 @' z; P0 _0 I9 u7 }% Kthe fuselage transm: h+ o! i4 v! h3 Y) ?, a" B4 f. t$ r
a8 p* t9 M6 I! l* s8 I) a0 t R8 v/ \. I
ALTERNATE, To change from one condition to) T' U0 }6 I4 b9 w, T' n& b
A
! U* o A( W. D( A* Mflight planning, usually near the destination airport, to be0 ^1 p; k# S" x- U
used when it is desirable to divert from the original) V1 j! [* b1 O) @
destination airport.$ O( s/ r8 X( }. V& {1 [& M7 w
空速游标
6 z" t' y$ r) ?8 R空速表上的可调指标。
) h, c" |: \- ]7 m1 S* f# [; r) Q0 Z混
0 ?7 j8 m- S% _' p* b/ t迎角速度,$ x0 `. I* @' p: ?6 R2 u9 I% }2 N
迎角叶片,* u1 S# H, T+ f
位于机身侧的可动小翼面。为失4 H- C ]7 \" t
气+ ]3 \( N4 p! A# T; z) U$ n! y
交替,
# b& }$ C w ]2 Z备1 t, I, }1 ]& k# N: y* d
制订飞行计
# C4 \8 H/ }; @# [3 E场。通常在目标机场附近,以备不去目标机场时,改降之6 k) X2 b7 n5 W' @- D) Y
用。, {% {- _1 b9 u, \6 m2 y2 V; g
英汉对照民用航空词典B OEING
: I2 ?1 [; O+ n& LTECHNICAL DICTIONARY 8
* I/ J5 a6 C& `8 x) mALTERNATE AERODROME, An aerodrome to which
/ |7 t2 \; }* F6 uan aircraft may proceed when it becomes either
: I$ g# Y+ e1 Spossible or inadvisable to proceed to or land at the: \# \/ c2 z" o5 t) C3 i
erodrome of intended landing.; V; V. u% j f
TER SETTING, The adjustment of the altimeter
8 e& r0 j4 R# xaccount for local variations in atmospheric pressure.+ [3 C* n% O, Y4 T0 g: n
LTITUDE ACQUIRE, A digital flight control system
+ a* |- Y% W. ?% x7 Sode to transition from climb (or descend) to level flight.
1 f( H1 v# u7 f) U+ y1 J6 o& ]8 ]LTITUDE ALERT, A flight deck alert occuring when the' D5 T8 h2 a/ [6 G: o3 h& k3 W
irplane approaches or departs a selected altitude.
. T2 C) a% y; G8 a; S* oLTITUDE CAPABILITY, The maximum altitude at8 W: J, X, @* U
hich the airplane can be flown at for a given thrust,
3 w# d6 Z7 ], G. w8 e5 N9 A( Dpeed and atmosphere condition.+ q3 u; K8 B9 d z8 p u; N) n
LTITUDE HOLD (ALT HOLD), A mode of the autopilot
6 A. }* v; x+ O, v/ B9 E8 Yr flight director to maintain a selected altitude.% Q3 w1 V5 d4 ?
irplane's altitude during VNAV operation.
' i$ H+ |! c/ o, i }* p机场着陆时,可作着陆使用的: X$ c' | k; ^; X+ v, ?" g
场。& B2 ~1 L9 B! g. H
,
( S5 I" Y3 R; F9 O5 W根据当地大气压力变化而对高度表所做的调整。
5 [ o! R( r l一种数字式飞行操纵系统,从爬升(或下降)改平的模
* k, y. ^& U0 F% _) a, x。
2 G( e$ ^ q5 `4 ~度警告,
! A& l: e9 ?+ y' d& |9 B& l# ^当飞机接近或偏离选定高度时,所出现的驾驶舱警告。
/ J/ H" W# K* C8 Y8 ^( d高度能力,
' |7 c0 i+ F1 I0 c# R/ n3 t在给定的推力,速度和大气状况下,飞机能飞达的最大8 \1 E0 S$ O$ I$ |( W4 H( W
高度。
) K$ V8 h- _1 t' j2 `7 B) y$ k高度保持(ALT HOLD),
" L1 {& _- Q! X0 f6 p9 `自动驾驶仪或飞行指引仪保持在选定高度的一种方式。9 T* ]% e! O6 \8 ]" H
, ~. v X7 i& _- z6 |( W/ d3 T
员对飞行高度的控制。( ]3 P" Q1 l& Q7 D- D* a
im
% w! Z* _6 S- t& \a
5 H7 p. Y5 v# U0 W9 p! JALTIME* k) n1 n* j& G( k0 T. c
to
1 d2 S! g' M8 G2 fA& \; k( t6 U4 t1 D2 C3 C1 \
m
2 Q. H& |( {3 uA8 r4 T4 a$ ]& l# s7 [1 m0 Y: F; ~
a
" `" `( G3 I' S# f3 O9 s2 _% S- K: K5 uA+ C, t7 ?* g- U# ]0 Q
w1 {2 Y& ^$ [4 x( V. u* Y
s
0 X9 ~' K! K' K3 xA; s5 S8 Q A+ r' P/ T3 b9 h E4 W
o3 n5 q. E( j! A
ALTITUDE INTERVENTION, Pilot control of the
* H1 Y$ o- \6 E8 T& c; }! R9 |a
. z9 T( C) g+ A8 ~8 }AMBIENT, The surrounding atmosphere.% o, l: Z6 Z: Q4 t
备用机场,
# B4 ?# `* @$ ^% z3 a# ~当不可能或不适宜在预选! r9 ~5 g1 y2 U" {' V
机3 N+ c9 |+ ?3 `
高度表设定
$ Q* L$ `1 b; P/ b. g0 e高度截获,; z4 n+ h4 h5 Z& D
式- K% [3 m }/ n: x
高
l$ \) L6 V | K4 @高度干预
. z) c1 p3 V. P/ h- J7 x在垂直导航工作过程中,飞行: M" U% V0 Q* E a% S
周围环境(地面气层),$ F0 P" Q( B+ B4 r
物体周围的环境(特别指大气)。+ o0 j6 K1 A& P8 i4 w
英汉对照民用航空词典B OEING D# M+ b/ L9 u! p2 [+ t: `; \
TECHNICAL DICTIONARY 9* a. N/ }! P X
AMBIENT PRESSURE, Pressure of air surrounding an. r( T" O. T( x% M! O
object, measured in pounds per square inch (psi) .0 P& b7 I" A& L1 q% W9 U
MBIENT TEMPERATURE, Temperature of air) b: s0 D$ w* h+ m- v
mpere.
! W G5 c/ X4 B2 ^% {urrent waveform.3 Y/ a2 c% `; d
g an
% [5 |% a; i, ?3 O( P" ^2 z7 p. Hnalog signal to a digital signal. `7 j# L% U' W( Y4 j* j( {- ] Z( g
ore inputs
6 P9 G. Q" W- E5 d" Gf binary digital information and one output. The output! {( e/ q! k. N( W9 H E1 f6 E
1 only when all of the inputs are 1. The output is 09 ~1 ]7 {7 @, c
hen any one or more inputs are 0. Y6 A- ?7 y- {1 _* n4 T; G& J# @
面气压),- h2 \# `# n) A$ `
境温度,
! a) R6 D. W3 p, K/ K气温度,用摄氏度(°C)或华氏(°F)来7 U/ c+ h# X2 D/ n. A! t) ~: I$ `
。
2 r) F; @! O+ g& X电压或电流波形的幅度。
( J$ e6 Y7 O' i0 ^5 k: i7 e7 m$ C& f性变化的信号来工作,或产生连续性变化的信号
. Q) s ]& M; ~9 a统。( Q8 v$ p( d2 k$ u. Z6 l
将模拟式信号,转换成数值式。+ T- p, |* @3 t E8 y
一种有两个或两个以上的二进位数字信息输人,一个输1 k, c' f: k9 N \# Q! e* h/ h- P4 ]; l
的装置或电路。当所有输人为1,输出为1。当任何一个
5 S: R% N8 o" `+ q) A0 @2 _3 @一个以上的输人为0时,输出为0。" }( F5 I, o8 _- O2 j2 T
A: N1 E. C9 f6 T% Q8 v; }+ Z% m9 Z
surrounding an object, measured in degrees Celsius
2 B+ G6 m9 d2 E2 B, x$ N+ y# q9 F }3 _(°C)or degrees Fahrenheit (°F).
+ V7 o2 `! u- b+ f7 z/ ~( yAMPERE, A unit of electrical current. One volt across. ?% N. }- s7 g8 f
one ohm of resistance causes current flow of one
7 l7 Y% g8 p- D* d, S/ Z) Ja
) s% i. p7 k6 f: p. @$ ]AMPLITUDE, The size or magnitude of a voltage or
/ y1 J2 x3 v2 ac
' s! D. j6 V; d W* GANALOG, Quantities or representations that are) W$ {7 q& w6 H' O4 B
variable over a continuous range.) v3 ^" R2 m$ t y8 a8 n
ANALOG-TO-DIGITAL, The process of convertin
* M. z' c; o0 M& j/ ]a
% r9 x/ X$ t5 K/ H, `# t, l1 X( SAND GATE, A device or circuit with two or m
" x$ l7 g9 q% U) j: o* A+ ~o
a( ^. ~8 R2 ]is* ?' P0 i3 F2 d# n, ^
w
* q) p( j9 t9 E U0 {环境压力(地
0 y4 i' A0 N* s& n6 `, D0 {# R物体周围的空气压力,用每平方英寸多少磅(psi)来9 X+ `. h a; D: S4 v) p" d
度量。: n0 s% S, r j \4 z
环
8 ~2 X5 Y Z% }- {+ ~物体周围的空
* H7 x- h; _" l度量。
( z$ n6 O1 \8 q6 Q9 C o7 ?$ r$ t安培,, M; T% C8 Y2 L# v
电流的单位。/ a, i" S+ r, y) l
1伏电压在1欧姆的电阻上所产生的电流为$ E* I Y2 h7 j
1安培2 G2 B) ]) W3 J" X9 c
振幅,
/ G7 g k4 U. z: W! D& L e模拟式,- P0 g. y" a/ K6 Z4 Z/ u0 k
用连续
: r9 \% Q4 j7 O$ ]系/ ~1 F: y- [" m+ K9 E& B: M: Y
从模拟式到数字式,
9 ^/ J! S( `9 l: Z' n$ M与门,
5 D% q/ j( O- v: C5 p2 j出
# w9 @# x) d: m或
* J p) t( z- i! M3 I+ O英汉对照民用航空词典B OEING: Q# i1 ]* w0 f3 W9 t
TECHNICAL DICTIONARY 101 z/ n3 O/ I d- @* j' i: I
ANEROID, A sealed flexible device containing air at low
! X% P1 D- `8 ^& opressure, which expands or contracts during change of
$ B* {: M2 U1 b `; ]ressure outside the device.
( v8 O" ?! t" o: ]! Vically
- [% v- ?1 A3 } Y1 i5 Zr changing the direction
]/ q, L+ l X' L2 h3 Af drive.
; u$ T$ d/ ?0 J: ]( D, G5 E/ _of the wing chord in
4 P9 \; i ~! X1 e3 Jlation to the free stream airflow as it moves forward
% C+ H$ |7 P7 Rrough the air.
5 q+ q4 |8 D, B% _al axis of the
6 W+ x, c) O Gaircraft. t0 G, P0 v, u% w$ i% e* n0 D
胀或收缩。8 k0 V' f; i7 {
箱。是改变驱动方向的机械装置。
% @8 q+ i( V' B% s, b机翼翼弦在空气中向前运动时与自由气流之间的夹角。
) d& D+ C: S2 Z+ n2 f+ }2 x0 ~。
( ~% P$ K) ]2 U9 k' lp: L& P1 Q5 I) E
ANGLE GEARBOX, A part of an engine, mechan
" \6 ]/ `& P* p! K7 u9 Adriven by the compressor, which drives the accessory1 o, t9 e7 }* S \- ^4 q+ P- U$ T
gearbox. A mechanical device fo
% I% W$ q) x# }" r# n+ Zo
) y" }2 }8 D" L9 ~! ~ANGLE OF ATTACK, The angle
+ A! k2 O8 }' N$ F6 s: p# U& }re
9 p5 B( ~- I' Jth0 j! a2 H6 [; k9 H5 N
ANGLE OF INCIDENCE, The acute angle which the
8 e( `$ ?0 l. D8 U/ i# D5 e0 hwing chord makes with the longitudin+ \1 R4 h7 b3 n. i* k- [& Q
膜盒,
U7 y4 `/ {7 s3 [5 o内含低压空气的密封弹性装置。当它周围的压力变化
: R. c0 q) g, C- j; o/ R时,会膨
! q. P3 T* t5 c" F6 _9 d/ s伞齿轮箱,
% k' b8 [1 X# V" q/ ~9 ]+ P V发动机的一部分。被压气机以机械方式驱动,然后驱动
; [: R+ ~$ I) h M附件齿轮
+ z# ^. D8 U7 ?5 M! {8 K. {* Q迎角,6 g2 ^1 }. K! r% g$ p2 E
安装角,* M9 a; @5 k2 R0 z _4 Q8 `
飞机的纵轴与机翼弦线所形成的锐角1 c* w1 @* U0 f6 P$ x; u
英汉对照民用航空词典B OEING/ b# w( P5 f4 N* f
TECHNICAL DICTIONARY 11# K+ N/ J+ z a1 e$ [9 ]* j
ANNUNCIATIONS, Audio or visual indications used to
' U5 @* w( D- f, ^3 ucall attention to an event that has taken place.
- W$ S7 _# s- b1 c" @4 kANNUNCIATOR, A visual device consisting of a number
3 y* K/ H6 E0 a# q5 Yly.1 k4 Q! U: Q; c" w; g( k
ANODE, The element toward which the principal stream
. z- i( X# c& z: l4 y8 d9 nof electrons flows.
! i! A3 C; B& ?1 m6 YANOMALY, Not normal.- E9 j. t, w2 \; ]. \/ q- p0 M
ANTENNA, A device which, used in conjunction with a( T/ z4 V0 [0 u2 S+ V) s
transmitter or receiver, is used for radiating or receiving$ L* O1 w# n9 ^# R& X
radio waves.
D' P: w" _" Z9 W* tNTI-ICING, A method of preventing ice formation on
' v& b0 Q9 @: q& x7 x8 z8 Ae wing leading edges and engine nacelles.
, i) C; L' M) uNTI-SKID, A system for providing maximum braking5 a; `2 f& Z) g% N
ithout skidding for any runway condition. Anti-skid
* y/ M! \9 e. N momponents are part of the brake system.
( G! x# V1 x0 d6 y6 X2 ~告," Q1 T) _; K4 [$ |$ [
当发生事件时,以声音或目视指示形成的提示信号。
5 d$ D) v" j7 K/ z与之有关的电路的现有情况或已存在的6 y8 H. g4 `- g) N
况! l7 G" M' g2 F! n7 |1 W5 s. o
正极,5 _: u8 C% P) d v. L1 S( @3 R
主电子流向的极位。; k" D7 M3 g, K2 m; A
异常,
) T* `& m1 P: h; a7 ]不正常。
, E$ H4 [( r/ d. Z, A天线,% ]! l+ U& m: ]6 G6 F& L
一种与发射机或接收机共同工作来发射或接收无线电. X) R: y8 x+ V+ G2 J
波的装置。1 C! Y$ N/ q5 C- v, {6 D( Q
冰,
/ L! V, ~) S `0 z- Q4 X, _防滑系统,1 p7 {' ]! W6 j# D8 l' |
一种在任何跑道状况下,都能提供最大的刹车能力而不( N( f, R' E2 b* R- E7 n. Y: m V
使轮胎打滑的系统。防滑部件是刹车系统的一部分。
# S3 O; c8 \- _. D- oof lights. Each light indicates the condition which exists" {' B2 H! Y2 ]% T* y
or has existed in an associated circuit and is labeled
2 T$ e- j1 W" T1 O- A, A$ t0 x% Gaccording
" I2 _9 n- [+ A0 y6 e5 vA, J" k4 A! u! v* i: r! _
th
3 g+ d! x+ O9 ]! ^" e" l1 qA
/ _$ U1 K: @8 }! @' j/ ^w
( _- P3 z( H5 x6 |c
$ I) N7 F: X' S9 m2 V通
7 O' p7 o+ A, s; a& m信号牌,. A5 x" O- j" b4 K* p* g3 h
由一系列指示灯组成的目视装置。每个指示灯都有相应
7 V9 I. p8 r: e L5 w+ v2 W! y9 P* _的标记,用来显示! t" e L, b; b. o
情- d: [9 N6 \: C' z5 D& s
防2 A8 \' E g& o7 f Y
防止机翼前沿和发动机短舱结冰的一种方法。
& S. e9 z) k+ \- j英汉对照民用航空词典B OEING
4 ~* l, a; W; f( b+ ]TECHNICAL DICTIONARY 12
$ E# L/ B7 _. g1 {2 B# bAPPENDIX, A supplement to the Airplane Flight Manual4 P: i: x. p, J+ B p+ H. u
tained in the basic manual. A
) D* ]; [+ O5 f& u" k! l) j, c* ]ollection of supplementary material at the end of a& \* b3 E: j5 ~& s% M: ?/ D
ook.
2 I2 a8 I5 `6 {- ]of the- t+ K/ B4 n T# B. X
rsion link on the landing gear.+ o6 B; ~6 a; ~+ e* c1 o! B
APPROACH MODE, An autopilot/flight director mode3 _5 ^3 }* n# N" V! f' d
which is a combination of localizer for roll control and
5 y7 {7 \' N1 T# Oglide slope for pitch control. This mode is used when full
0 k/ m5 `% K, {9 B+ z# u0 ?$ |instrument landing system is available.4 i# J. e& V4 F* M8 Z
APU, SEE - AUXILIARY POWER UNIT' P7 K) Y& b E. R6 a2 B6 h2 C
ARINC, SEE - AERONAUTICAL RADIO' H# A+ }. P5 p* g, G
INCORPORATED
6 s: a$ K; K1 s% g1 Y" t' P8 E. i6 ~ARM, To make ready for operation.1 k g$ b/ O M' \
附录,* Y8 B( w( Z" C/ ^
飞机飞行手册的附件,包含基本手册中未提到的飞机形
8 H0 d3 G' Z7 s& T x态的其他性能。是附在手册末的补充材料。
6 ?% u/ ^& V7 H7 a' L顶销,
: K3 w& C* Y' ]( E用于连接起落架扭力臂两部份的销子。
9 Z6 D+ L1 |8 P5 E; j2 t6 W% k$ a) s进近方式,3 W0 I! U+ q1 _3 W9 V
一种综合了控制横侧的航道信号和控制俯仰下滑信号
( D! N* v0 F r( m4 M1 v, j0 U, q的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系. n% T* l8 l1 t. |# F
统正常时才使用。
& a5 v4 j7 F) I! r$ ?% Q辅助动力装置,
: k' Q6 D6 W, M' Y6 j* X; h见Auxiliary Power Unit
" d. G( R" g7 ^/ Lcontaining additional performance for aircraft
4 N$ |( H3 \8 T* g$ yconfigurations not con8 y G5 m1 P6 f& \
c$ J5 [0 A" s4 B
b
% Y i% {; ~$ Y! S1 |+ }" CAPEX PIN, A pin for joining the two sections
0 z0 X+ S, n( N, y) \6 c: V. fto" ?' ^. b$ g' C4 t$ q4 T
.
; w7 {! Z" M, @) D航空无线电公司,! h- H7 Q9 P- m" N3 A
见Aeronautical Radio Incorporated.: a7 e% @! B6 L
预位,
+ Z& @ D0 y1 t5 Q7 y' J部件可以开始工作的状态。* G# U4 X. V6 f
英汉对照民用航空词典B OEING ]* _5 M4 i9 F5 {0 L
TECHNICAL DICTIONARY 13! ^' G1 h. Q5 G( L0 x% d; i
ARC, The curved track over the ground of an aircraft4 [. p+ T1 [! i7 M
flying at a constant distance from a measuring; [: \& [9 h# |1 S7 h4 I8 S' ^- I
equipment (DME).$ O9 E6 S- B3 l6 X+ ^% D l' w- I
in the limits of self-contained system9 t& t7 j g, H, F: L; Z
apability.; [7 i# ~4 t- K- ^! f( t4 U4 |
tem for opposing or restricting
- g0 f, S! y* L3 Uovement.2 K. i7 c/ s% q. u1 q/ F- P
SPIRATED TAT PROBE, A sensor that measures total. s& ~; T- ?' R5 \0 V v) F* c1 k8 H
ir temperature when the airplane is in the air and that
, l! d; f/ ^8 h, g$ veasures outside air temperature when the airplane is/ e3 R5 f0 N* R/ l4 u2 a$ A
n the ground. The outside air temperature is measured
3 A$ D0 J' |% G- I$ D- e0 F" E) G8 QSSEMBLY, The fitting together of a complete structure; D2 h2 [1 ^1 F5 c& X
SSUMED TEMPERATURE REDUCED THRUST, The) r8 h2 o& r8 L7 f4 O
ATC, SEE - AIR TRAFFIC CONTROL, h3 q2 J4 |# e2 A
,/ m, b" u% Y0 a# T/ c1 P9 {% s
系统中所产生的一种用以抗拒
9 e0 x5 x! O# ^8 j作或限制动作的力。) P- E7 n5 ~0 g- {+ L6 u) Q7 i. \
头,
5 D4 u3 w: J, g' F+ }用来测量飞机在空中时的总大气温度和在地面时的外& X! J# }; S; X2 F0 n/ r
温度。地面外界温度的测量是利用引气将外界空气吸入
3 f. q4 w( M* |- Y- w: ^# v头,以达到测量的目的。) `$ w0 K, Y- `) ~; a: C
配,8 T; X2 q; n3 y5 N% b+ C
一个完整的结构或组件的过程。
2 w' m9 |5 E9 @8 O2 ]假设温度而得的减推力,9 Q) |6 z* T! C+ p& K% F
推力设定值时,假定一个比实际外界空气温( c" E/ W4 H6 I
空中交通管制,+ j& p6 V4 s7 [+ D
见Air Traffic Control
6 O2 r4 i( ^9 U& e% u2 m& jAREA NAVIGATION/RNAV, A method of navigation
. ]# n+ t, t% u' Rthat permits aircraft operations on any desired course
V. Q( y: `2 U, {, Dwithin the coverage of station-referenced navigation
+ j/ P8 J. r/ _# Dsignals or with
% l5 V( ]* c3 i8 b" b. v, o) o% qc
+ c6 t, k6 X! @8 @5 L) F) HARTIFICIAL FEEL, A force developed in the flight
2 \3 S9 Q9 Z/ ~ m9 q4 A- \4 hcontrol or brake sys/ F$ A" M- S7 x0 ?3 E$ m! c/ x
m
. L7 T' x6 |6 }1 FA/ `. Z, g% n0 m( r5 } a
a* c8 V# o+ ?5 X9 d1 C& ~+ l
m
$ f" S1 p, v& W$ ~" Zo
8 Y1 V, F8 x" `0 ^+ |! Yby using bleed air to draw ambient air through the
X+ y. t# y6 K1 Dsensor when the airplane is not moving.) r0 I: v. p9 N. T8 U
A5 C& L& g2 q& m0 i/ b8 S
or unit. c q% Q3 m6 K+ I; k# h1 F! u
A
( _# A% K0 l; v" i5 ?lower thrust obtained by setting a higher than actual1 _& `+ z9 A! t7 Y
Outside Air Temperature (OAT).1 k) d; k) ^0 R& K0 c
弧线, p, ?! s, u) p! |+ c
飞机在围绕DME台等距飞行时的弧形航迹。2 C/ U& ~! C% K1 _& ~+ E& d
区域导航,' ] T. m+ A, f5 }, v% e! V, b
容许飞机飞行在有电台参考的导航信号或自备系统能
' ]+ E) u% m) t0 L S- r- C力极限范围内,飞行任何预定航线的一种导航方法。
8 _/ y, T4 \" y6 h模拟感觉( e* p) B4 V6 W& G
在飞行操纵系统或刹车
; \& j; E1 d( t动# N3 u1 V& v9 N: W# m) o' H
吸气式总温探8 a" V& o+ C9 |8 F5 F, i3 D5 g
界
1 r3 L! y3 a! k探
* t+ G: v6 t( w) g' {6 y装
; J; R# {9 P; B9 u( i2 {5 x组合成
* N% e% ^$ J; v" j: ~' c4 s由% b5 A3 A" m: L. y
在选择起飞8 U. k6 A; A8 r( O
度高的温度而得到的推力。用这种方法可以减少发动机的
4 |; }1 v1 W1 F4 X8 T* }磨损和维护费用。. Z. Q X+ P! Y" [5 Z% O
.
) t& `. u( }, d: {/ m英汉对照民用航空词典B OEING
$ P- g# G9 z$ H) |TECHNICAL DICTIONARY 14
; d7 n. n8 y4 b) L/ S' z+ {ATE, SEE - AUTOMATIC TEST EQUIPMENT/ o# M% p5 U- x
ATMOSPHERIC PRESSURE, Pressure of air due to the, m& ?) w+ s/ A4 ~% L
arth's atmosphere, expressed in pounds per square
0 c6 H& n6 a9 Y/ @9 ]ch (psi) or inches of mercury (in Hg) or millibars (mB).
/ n( C* N) O. v$ l2 m5 `- hTTITUDE, The relative orientation of the airplane with6 K+ T: i* P5 @8 b8 f) T( }
spect to pitch, roll, and yaw.
# B3 X9 M. O" e7 \( ]. F! O* PUDIO CONTROUSELECTOR PANEL, The panel in5 A2 q( \ G0 Q' |. N$ a
e airplane which controls and selects the routing of
]8 o4 ]9 h! H( zudio.( f* x, b6 P" P8 ]% T& O0 C/ f/ z. C) Q
UTOLAND, Automatic landing using the Digital Flight
# m% T; ^& k- J; @6 ]$ Yontrol System.# ~$ S# r7 B ]0 E+ M5 m3 l
n.
! r2 I( t' Y; I+ R5 _. g( kM, A system
! u( i% c/ h3 c! }3 e) womposed of all necessary subsystems needed to guide
5 _1 Z- L+ x4 e1 G- P) ?e flight of an airplane.5 G: W3 k6 q( }) i/ j# N/ ^
EQUIPMENT, System test
" c" a: W$ ]$ Z5 Cquipment that operates under computer control.
2 z& Y, W2 U7 t2 T0 }( [/ H/ J; u装置, |
|