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AIR DATA COMPUTER, A computer which produc
1 T7 P- }4 G/ e% X6 o& ~% w: Q& Fdata information, such as altitude and airspeed, based) [* }4 ?2 E8 w4 L! w. }( }5 j
on pressure and temperature measurements.' I8 S: E/ W4 Z m5 t% o' k
es air
( S! F v2 }+ L8 x8 ?: QIR TRAFFIC CONTROL, A system comprised of
/ C# U3 Q$ M* b3 H; \& R8 O! g0 Rround and airborne components used to identify, track2 D4 v( t/ ^$ T ^! `: d: Q% F
OUND SENSOR, An electrical device operated
, t/ W+ S* u6 A3 i' m3 Y. [y the landing gear, which transmits on ground/in air. W5 D+ G* v$ X6 {- n4 q6 F% b
formation for system operation in flight or on the
. Q1 p. K0 r% {" {& A8 Q" c3 nround.6 H4 R4 r& {! X$ A
IRBORNE VIBRATION MONITOR, The AVM takes( H, Q6 m& C& ~% H. v7 a- G8 e/ |1 }
e signal from the engine mounted accelerometer and
- Z2 V* L T; X- W6 D& P" G: X, }2 balculates the vibration on that engine.; h6 t# P' n% @
corridor equipped with radio navigation. O- I1 l3 z9 G: g/ n) u$ O
aids.
5 O) s% l- @ o$ I* C. C% oAIRCRAFT (or ARINC) COMMUNICATIONS
/ o! i& Y( R. o% \5 nADDRESSING AND REPORTING SYSTEM, An
0 R# y1 S5 e! g; `addressable digital data link system which permits the7 i5 y( l% O, O0 j
exchange of data and messages between an aircraft
9 | S) J" P& kand a ground-based operations center over a radio
) N! A* S/ ^8 w Fnetwork.
" [( A, w! t6 eAIRCRAFT CONDITION MONITORING SYSTEM, A: K9 m8 ]0 O! _- }. b
system of sensors and recorders to monitor various* X4 X1 c6 J3 e' n, D) G( `. ?/ J
airplane systems' performance and status.+ n9 S+ X/ m* B' X& J/ a
机,
) q* l i1 |' j! K/ F, F) `( B中交通管制,
1 H% W8 f2 b: [& ^3 w* u一个由地面设备和机载设备组成的系统。用来对飞机进1 S! R8 Z6 q8 ^9 B# L
地传感器,
* z0 B0 j. u' M0 C$ {" G& `一个由起落架操作的电气装置。用于给空中或地面的飞1 E' {$ V' i" U4 B5 _# t
系统运作传输地面/空中信息。(有些系统只能在地面
! C) ]5 N7 P3 z) A, n% s! n1 `& r用)4 d+ ] i: M$ Q, W9 M
载振动监测器(AVM),
4 J9 [4 Y" |' S# t+ W$ L. [: `AVM从装在发动机上的加速器取得信号后计算出该发
( f& D! n/ L9 q& ?机上的振动。# P8 a' z$ `9 i. _; l
式建立的控制区域,内有无线电导航设备。
: c4 C# H f5 J9 [飞机通讯寻址和报告系统,7 B9 q, B. m- b- }, A7 J' G
有种可寻址的数据通讯系统。利用该系统可使飞机与地 H6 m& [: v) T' G+ h# w
面操作中心通过无线电网络进行数据和信息的交换。
9 T4 K* g6 d5 n W2 v( ~飞机状态监控系统,
1 y* l0 Z0 H9 \# L一个利用传感器和记录仪对各种飞机系统的性能以及
/ f. a d, v7 L状态进行监控的系统。
5 ?4 t. H; a- N' x( Q0 b2 FA
( U! J0 X7 G9 w* Q7 \' B4 lg, o# G. x1 k8 i: A6 F
and locate aircraft.
. [. q* `/ \9 [" h: U* d. w* N1 ^: XAIR/GR
* K; m' W5 T1 q2 F. z4 r) T7 i. jb8 Y' M7 t) Z, s
in
+ p# T: _% y- [* B$ Fg
7 ]6 G, Q% @2 YA
0 k. D% P1 E# J& Xth8 V8 s9 E4 ^4 O; U. Y2 y: G
c; W! K, q$ \$ S2 q, F' \
AIR WAY, A control area or portion thereof established
r, ?4 e& m& lin the form of a
1 m% u( \; l* @# Q5 g# @大气数据计算
9 F7 U1 V v' ]根据量取压力和温度而产生大气数据资料(高度、空速- i- X7 J0 [/ G0 T! X: ?4 Q
等)的计算机。! ?. Q( k: {$ G: x* b
空7 y7 f: w% \* h9 t, A3 m
行识别,跟踪和定位。
/ `5 @' D' M3 h& E& l( r& d空2 r) Y) S% |, w9 O
机
0 D# C$ U' a7 \使
+ N. A7 R0 v9 }1 z机0 z, p4 v$ M7 h+ C2 j. g" R
动
, @7 p$ X$ A Z* m x航线,
' D9 N7 k0 A3 P5 c以走廊形
) |0 u( Y( ~3 M; p2 W5 G( |英汉对照民用航空词典B OEING
/ j: S6 ]. k. r. G3 N2 X& jTECHNICAL DICTIONARY 6
8 i) M* S( s: I, s7 T% ?. u4 _AIRFOIL, A surface designed to obtain a useful reaction,
. A" t$ I k) t0 c7 \& Nsuch as lift, from the air through which it moves. Wings,9 q% ]& ^0 S0 M8 H5 n$ Z
stabilizers and control surfaces are airfoils." H/ |' m R9 R0 c5 I
AIRSPEED (IDS, TDS), The speed of the airplane
+ H+ E+ M8 K& Z# Z7 Zrough the air.
2 x! \6 n# E1 e2 |D INDEX, An adjustable pointer on the
j/ S% I: G0 Kirspeed indicator.$ C& t9 {7 p( X: P% v" i% K
and legal ability4 P8 p Z& n# i
fly.$ K2 G% K& k4 s' P/ j$ F. u) L4 _
m, for example, the procedure for finding the
6 K: N( K) s( l" [4 [quare root of a number.
# u# n w! `2 I8 _4 F. |y$ z" ?, W; o8 a1 r( X( {" ~$ u
re, wind,6 j- ?5 {3 a' O( u( X K8 _
and aircraft flap setting.( d6 U: @ H# Z4 `! E
是翼面。
* N7 R+ s$ L6 s9 t' K% w速,# u$ m4 [8 }( H4 v8 ?% W9 T) U
飞机在空气中运动的速度。
2 p( V# ^) |( h1 _2 y,3 X1 G$ C/ h+ F. Y
在空速表上可以调整的指针。5 D3 _) Q9 b1 @, O' x
机械飞行能力、和合法性的飞机状态。
% p! m; S6 A; A% L+ U$ ^" ]- Q一步一步的解题方法。例如,计算一个数的平方根的步
; T: g$ q9 U! n7 r2 U6 A2 O; j。
' ~& I) E# @# H" o能5 Q. A2 _0 F/ c: N& s8 T& ^/ v( ]* h1 Y
资料的法定文件。
& h7 }8 _0 o+ y, z$ I0 r翼位置成函数关系。
9 ]8 d. R' l& kth% o* e8 W' g5 }0 F* T
AIRSPEE" _" V, T5 a* t1 B
a. y" L- P- X; B; w* U1 _
AIRWORTHINESS, The condition of the aircraft with' P' D/ n+ O' E- [: Y& k
respect to its aerodynamic, mechanical,$ G$ n5 z. d- V; c; s
to2 c/ @& A, z3 B, v
ALGORITHM, A step-by-step procedure for solving a
' q* A: Z* l" G9 L" k1 Iproble
^; z7 I0 f+ E; b) m# `s
/ p1 W& w6 \7 _AIRPLANE FLIGHT MANUAL (AFM), The legal
( T; A% K/ @8 y0 ?% M0 {2 q2 b" Cdocument containing performance and operating limits,3 q: p4 n" `7 e( o' w% w' N
operating procedures, and takeoff and landing* t c, o/ f$ ?. E
performance.: f/ k% \3 x& w
AIRPORT ANALYSIS, A comprehensive set of takeoff8 D( Y7 F; |$ @( d. Z8 J
weight limitations for a given airport runway, generall
9 p" k! u, b0 z. f$ dpresented as a function of airport temperatu# v/ A& o* ^" o& o1 s' o: z: J
翼面,
# o& i6 J) e& |8 u0 K6 j0 e用以从气流中获得反作用力(如升力)的表面。机翼,0 X; l4 }4 f* s; c+ A2 u2 A1 E
安定面和操纵面都
) L) i: g. G9 n空
: Q$ l! E+ r3 s1 K空速指标
3 Z7 r: M5 T2 {, ^+ h1 q- S适航性,
, Y* n1 l7 m7 ]3 \有关气动能力、
f) X, J/ `' h; Q7 Z) K2 Z演算法,4 }, R; D; k9 S2 V( ]* t$ _
骤
8 @. K" H/ p, G+ w飞机飞行手册(AFM),
. L1 m$ M" z* O, {, i; B, H包合性能极限,操作极限,操作程序,起飞和着陆性
+ o {. D4 r+ o+ a等
$ H0 X2 v# v8 {4 B机场分析,
" X' l' S4 T0 L: n! e* d一套针对给定的机场跑道的详细重量限制资料。通常与
4 o. s% |- d( M$ \ r8 _机场温度、风、和飞机襟
$ {; A* j S- g) V$ {: m( n英汉对照民用航空词典B OEING
2 c9 r; B' C7 w1 `) g2 N0 t6 }TECHNICAL DICTIONARY 7
) j, N9 Y/ W+ |* U! U/ o+ lAIRSPEED BUGS, Adjustable pointers on the airspeed! o* b! e5 r3 [2 x, f
indicator.
2 E3 z( s/ n$ B# K) c" fALLOY, A mixture of a basic metal and small amounts/ [) f. V: j; R h
f other metals to change the properties of the basic7 p0 |2 c- T4 \2 P( G- m
etal.' T+ x+ z4 f7 ^9 h; q" S' G
Minimum airplane speed.9 X+ v% G0 n2 R e1 M2 u4 l7 w
e of4 m' B0 f _- T: d S( a" |6 u+ w
itting airplane angle relative to$ J! l2 M) L- T( X; f8 S' e
irstream for the stall warning system.$ @. D' i% e1 d% S" S" ^' f4 a
another.( ?8 H4 n$ Z# ]9 \2 g1 M
LTERNATE , An additional airport selected during3 P1 Z9 |2 t3 \8 O$ g: Z2 C
,. D" e+ \9 \# m; u8 p
合金," w% ~ D7 _: B: ?
在金属中加人少量其他金属,而改变其性质的一种金属
/ h: w4 h2 G. j4 q# D9 k* N/ U合物。$ X! H1 j+ T* V* H$ N
飞机的最小速度。
. G+ v# l' @) Z% @速警告系统传输飞机对
|2 R( y: x8 v) V( Q0 R) j& ?流的相对角度。
$ @+ J% S0 k4 b+ {: K+ Q# F由一个状况改换到另一个。9 v( e; ^5 V2 Q0 W6 }! C' N
降场,! T3 S/ N- r% X- ?( c
划时,除了目标机场之外,所选的另一个机
! \0 B8 o8 O. \# ?; X$ w( Fo
9 |& L, V% U5 e) y2 f8 K7 a! hm6 N( Q, J: j1 @! o2 ?
ALPHA SPEED,: q N2 @2 ?8 z
ALPHA VANE, A small moveable airfoil on the sid
- }/ W; w' x N. `4 ~; u) othe fuselage transm
) v1 S: l- O; s7 [2 w; va8 j, m0 C7 h1 H. M% Q
ALTERNATE, To change from one condition to
% H( b, Y# I' eA; s2 s% L& r# u; e# M
flight planning, usually near the destination airport, to be% \9 `* i* t5 ?% `3 q+ Z1 c
used when it is desirable to divert from the original
. T3 \$ J, z: r) ?$ cdestination airport.
. j9 n8 D/ H" F空速游标+ S1 X w% E! `
空速表上的可调指标。
' n5 ?+ a5 Z" k混6 z: l* j, u7 N% D0 p3 ], w
迎角速度,
! w* u9 k" { {6 E迎角叶片,
4 f3 d0 O$ _( G) g% l2 {位于机身侧的可动小翼面。为失/ R2 _3 \: Z4 i" Q+ Q% ~
气+ J1 s5 z$ ~' ~
交替,5 ~$ Y: X0 i! W) {; S* L
备" G6 r2 I7 \+ u+ F
制订飞行计
$ v, z, j+ e$ n1 y8 g场。通常在目标机场附近,以备不去目标机场时,改降之! W5 L: X1 j$ H; f* z2 Q" j
用。; ~& {1 ` F6 N! C2 Z4 I5 m
英汉对照民用航空词典B OEING
O. p7 M- a' V4 e; ETECHNICAL DICTIONARY 8" _2 n( Q' M Q* Q# S2 d
ALTERNATE AERODROME, An aerodrome to which% w* q5 P" q+ I
an aircraft may proceed when it becomes either
* u+ ^! d7 _# A! qpossible or inadvisable to proceed to or land at the$ h, m% p7 B2 l: ?7 E' g1 c$ ]
erodrome of intended landing./ k e" _6 [# |& R
TER SETTING, The adjustment of the altimeter6 p7 E7 H5 ^" h
account for local variations in atmospheric pressure.
! ?/ v* X6 [* F- ILTITUDE ACQUIRE, A digital flight control system2 A$ [( N" [- V1 \8 I7 [% L
ode to transition from climb (or descend) to level flight.! F/ p& h, \3 I2 _( V. _
LTITUDE ALERT, A flight deck alert occuring when the$ D+ a) u* [2 S& J2 M% E. o* {7 W2 Q
irplane approaches or departs a selected altitude.4 ]8 z$ n, \6 u+ m. c3 }3 ~
LTITUDE CAPABILITY, The maximum altitude at3 U: Y; Y( I* d8 l
hich the airplane can be flown at for a given thrust,3 T6 l' D' O2 e8 j+ l9 o
peed and atmosphere condition.
: D- X$ G8 m Z2 O( `2 YLTITUDE HOLD (ALT HOLD), A mode of the autopilot5 c% V, \( w2 J( a! Y) E2 w% A" l
r flight director to maintain a selected altitude.' N7 O% u6 v- F0 I! [
irplane's altitude during VNAV operation.
" R# X& t0 F: U机场着陆时,可作着陆使用的
^) O/ ~! W j场。
) K" ]! m1 E M4 G,! j- ]- X, K6 Q5 o- K5 N, T
根据当地大气压力变化而对高度表所做的调整。
' z" d7 X9 E2 A t" _( n1 v. e一种数字式飞行操纵系统,从爬升(或下降)改平的模( F+ D" Y: s* ]2 y& U( s$ U5 D
。
' b% c" s; K ~. V7 r: {1 T# b$ U度警告,
8 p( K# f8 D: B8 a4 B' Z: \) q当飞机接近或偏离选定高度时,所出现的驾驶舱警告。; f9 l9 A. E3 p; \5 l1 K
高度能力,
/ V: h5 U; H4 |( F/ q) x在给定的推力,速度和大气状况下,飞机能飞达的最大* d$ T# F! V, K3 k+ U: R3 d
高度。
3 l% a! r/ E8 d0 {( L0 p5 x高度保持(ALT HOLD),: T8 H8 x& [6 ?6 G; u
自动驾驶仪或飞行指引仪保持在选定高度的一种方式。4 G p4 T3 S4 D6 G8 `; [1 R- ^
,6 r& ~7 h b6 j2 n4 d- } s8 ]9 `
员对飞行高度的控制。
& x) Z5 ]3 V5 }( jim
/ O/ ~* A- F" ?/ v' G Ea
' G& G/ u% J2 A: y3 Q) o) w0 Q& JALTIME( H. J& f+ g" G$ M
to2 G; v- J, |9 E# R. m5 C
A
- P# f7 Y& i' H$ Z( ~m" z9 H( W$ T& B B' T
A
6 s. i9 F0 d& j* ~8 F% ^+ Ja2 V( y/ E% I% A7 G3 K* X6 I
A# H: n; W5 p$ c8 t
w5 c* u% F( b) M, y0 h
s2 f8 Y1 ~, I$ R0 z5 g( w5 Y
A
3 w G6 C1 s! [! W7 zo6 v; J) l2 F4 u8 Q( C. M
ALTITUDE INTERVENTION, Pilot control of the/ \) q( S0 ?6 Z! C) U }+ w
a; {3 W. z- d) d+ S1 P* C8 d2 g
AMBIENT, The surrounding atmosphere.* z) |5 o7 b# u
备用机场,
0 H5 |2 f# h, ^8 ]4 V" S当不可能或不适宜在预选; i4 N, [9 K* \# ^4 p% G! z7 H0 l5 \
机
& Y+ B, ^0 ?0 M6 o! d+ n8 K高度表设定
( t; A. l3 b+ S7 L8 e5 j高度截获," ~/ V9 S/ o0 s& Z0 S
式
- N) w+ |" w! y8 D% }: `高
% g& o! t/ u) u; u7 K" t高度干预
- y+ @/ Y8 y; ~7 m7 q在垂直导航工作过程中,飞行
- r8 a4 q! \) T- j周围环境(地面气层),
9 f8 z) M2 O# `: M9 M& C物体周围的环境(特别指大气)。9 p+ L5 d0 H: h" ^3 W
英汉对照民用航空词典B OEING, ~ d1 x$ {- K6 ^
TECHNICAL DICTIONARY 94 W# o0 h! X. Q, S3 u
AMBIENT PRESSURE, Pressure of air surrounding an
+ y2 u9 ^9 @8 h( u0 Eobject, measured in pounds per square inch (psi) .. V" f9 b" l+ ]; {) l3 p1 m
MBIENT TEMPERATURE, Temperature of air
8 `/ ?9 E* r$ N7 [mpere.
4 V3 i& u1 h! e% j( a0 `urrent waveform.
! D8 M+ \/ p+ m, B! y+ Cg an" w- v% Z1 E* P7 O5 ^# u- u6 N
nalog signal to a digital signal.! c) m3 H% [1 d
ore inputs6 r! }5 {' }" Q: k z
f binary digital information and one output. The output
+ z% {- B3 i. l0 N1 only when all of the inputs are 1. The output is 0
: _8 L& H( C! _4 ^9 P) @0 z+ [hen any one or more inputs are 0.
; h# Z& H0 l. f6 g面气压),
& O! n) S8 t. K( T% j+ V境温度,$ F& \, a4 I5 k, _
气温度,用摄氏度(°C)或华氏(°F)来
# ?6 ~+ `/ j( w. T- x。+ D: X( i/ f9 f @) m
电压或电流波形的幅度。
3 u% v! g& x8 L性变化的信号来工作,或产生连续性变化的信号
! t, n1 w' ~. B/ J统。4 a' F. D6 }& n0 ^- K7 g) { ^
将模拟式信号,转换成数值式。
1 J" E5 K2 h$ ~. I* A! L一种有两个或两个以上的二进位数字信息输人,一个输
1 _9 z2 i# T7 M$ f8 {8 l- k的装置或电路。当所有输人为1,输出为1。当任何一个& H l# T' g% k$ j% L! ~
一个以上的输人为0时,输出为0。
/ u- S! l& P, P$ J0 y! ~4 ^A
( {8 x9 S# [" L' r6 t- jsurrounding an object, measured in degrees Celsius
$ C5 D3 Y4 V U(°C)or degrees Fahrenheit (°F).
3 S8 U; F3 |5 V; K7 w3 vAMPERE, A unit of electrical current. One volt across7 w' g9 @% i9 c/ G2 ]4 F) d9 y
one ohm of resistance causes current flow of one
% d4 I* X$ Z: [% L, |# d4 a& v& xa$ S% ~0 q7 p! _. `+ u8 e1 K- N
AMPLITUDE, The size or magnitude of a voltage or
$ w) P8 C. N |1 \; [c
! |& X, h% f9 f t$ [; xANALOG, Quantities or representations that are, K; S& ^- g! r2 o
variable over a continuous range.
- l' a3 |2 i" U& FANALOG-TO-DIGITAL, The process of convertin, T' W, Y9 W; P, X) X
a
( H7 }0 j- D6 mAND GATE, A device or circuit with two or m: Z* r1 e& y7 K1 h! Y$ {* ]: Z
o. s) ^" M; B, F- S0 j
is/ h0 C/ b9 a. D+ o$ {' M2 G; g# l
w0 s! Y; H* G% S# r) I9 ~4 ~0 A
环境压力(地
; z5 k" ]3 k# B3 l! U# ?& R物体周围的空气压力,用每平方英寸多少磅(psi)来3 [5 n* W' c& v9 g
度量。+ ?4 F( M4 a# ^6 e$ T1 A. U
环# w9 u0 v' j8 Q& G- b
物体周围的空
7 Z1 _, _+ |* p& g. ~( ~/ k, f, A度量。
+ P5 E4 I' L9 J安培,. Z& h2 m) q1 s' ?, y: y& e; d+ t4 R
电流的单位。$ Y& X% `, U+ M3 P% Z, ?( p5 O
1伏电压在1欧姆的电阻上所产生的电流为
4 M5 G" J$ y# K: }+ {! T8 `/ |' a1安培( q, k$ I; O/ ?1 l4 {0 F) W
振幅,
, C! r& \8 ^) J" F模拟式,
. N7 o- D/ ~: P5 S: ^8 E2 G' n# c用连续
; r# d u! m, b1 O- L系8 z' v# k' | L8 i
从模拟式到数字式,) r V! p3 w# z B: D( A# A. C
与门,( p2 K$ u1 g( x
出
& g2 h2 s' D$ k或" G) X* N3 s t, W$ F
英汉对照民用航空词典B OEING4 \. i0 p X3 w8 I
TECHNICAL DICTIONARY 105 ], l; ?6 T- b% |* f3 K" j5 X8 I
ANEROID, A sealed flexible device containing air at low
1 }* ^+ T+ ^: C7 Q; t+ b( `8 N" }3 hpressure, which expands or contracts during change of! |$ ~4 t A8 R, v, _" A S2 s
ressure outside the device.* E* U; z z2 ]) }6 _
ically
' ?3 [! }8 _2 ], ?0 d! Q. q1 ]! ar changing the direction& j$ c- `: l! T" ~( n
f drive.% L! _0 [( g+ x9 m7 f- G- K
of the wing chord in7 B! H Z( r$ t$ o) G. w7 e1 h% l
lation to the free stream airflow as it moves forward
, d/ u* P! b0 q4 B0 l3 prough the air.
. c4 u2 v, A l4 f) xal axis of the
. ]) z; a0 b! p( b) P2 o) vaircraft.
' h6 o" s* u( i% k! n! M胀或收缩。- q- p# v! N: m9 ?' M- ?
箱。是改变驱动方向的机械装置。
# ^- _6 y4 Y2 e$ g" R机翼翼弦在空气中向前运动时与自由气流之间的夹角。( e. b) A: [) `+ `% G0 e
。
: a& l9 V ]3 H- W& X' p' H: _p
6 q. Y4 Y7 E( t) Z4 EANGLE GEARBOX, A part of an engine, mechan
: s. l l% m* i$ C" ddriven by the compressor, which drives the accessory5 Y( r4 c; V. g7 u& T" d# [; [
gearbox. A mechanical device fo& f, O% O7 }6 n3 L Z' P! s
o& l" b3 h, r! T
ANGLE OF ATTACK, The angle, {& F0 |. _* g
re
# H& L. ]( Q2 }/ f. J0 b- x7 H6 Hth
) a4 D/ T( P0 r* p9 A! n$ _ANGLE OF INCIDENCE, The acute angle which the4 r% Q5 q; d' @9 ~/ L0 y
wing chord makes with the longitudin
3 j! |5 I/ ?0 R膜盒,
, x. I0 G, T$ T- w4 r$ L内含低压空气的密封弹性装置。当它周围的压力变化7 ~6 O3 {4 i! F
时,会膨; R1 U/ W& n7 F+ V1 }. U
伞齿轮箱,) n- v X0 |* g x* |4 X
发动机的一部分。被压气机以机械方式驱动,然后驱动
7 z% h; E4 ?' b" B5 w. K附件齿轮& P8 q- Y, x; E
迎角,' p. l: R5 S1 n; ~! z( n9 Q
安装角,# v% ^* y' O: [# F
飞机的纵轴与机翼弦线所形成的锐角
6 J$ E0 e6 C$ Y$ N3 D7 X' Z英汉对照民用航空词典B OEING O% p, G) _0 w# a! v
TECHNICAL DICTIONARY 11
. I/ e% O3 K7 Z* ]3 J1 \ANNUNCIATIONS, Audio or visual indications used to
: `, V3 Y: @9 Bcall attention to an event that has taken place.; p, E! h# Z: ~8 j
ANNUNCIATOR, A visual device consisting of a number
Z7 |8 D, i; _; B: a4 dly.% k9 O6 w6 P- @6 `9 p* L( W: ?1 g; J
ANODE, The element toward which the principal stream
- T- I' {3 W' w @0 D% oof electrons flows.
" [) K4 {0 q4 _5 ~8 ?ANOMALY, Not normal.
! ~$ o- v& \8 }0 `, \6 |ANTENNA, A device which, used in conjunction with a+ b5 o" }& K9 Y$ h! Z
transmitter or receiver, is used for radiating or receiving }& H @$ z/ y$ g8 C) N# E; z
radio waves.# I9 n" l R* @8 T: y
NTI-ICING, A method of preventing ice formation on+ S1 R& ` Y% g% q7 T" }! s: \
e wing leading edges and engine nacelles." N. b4 F' f: ^$ e4 n2 x4 @0 d. K
NTI-SKID, A system for providing maximum braking
+ r: q6 q+ d8 n X/ Eithout skidding for any runway condition. Anti-skid( Q9 e3 G4 v# P! I5 G
omponents are part of the brake system.
$ r9 [! @; m# v) A$ j告,
6 u+ j. }( r1 S! n0 \& h当发生事件时,以声音或目视指示形成的提示信号。
" x+ b; R' E0 d8 G7 a) Q与之有关的电路的现有情况或已存在的4 j! e9 f. R1 a7 ^# z5 g9 V# H* _6 h
况
& ^/ F2 s1 W, N. `% b) N' Z# T正极,1 H* ?$ h0 s" |; `
主电子流向的极位。
z6 W: O7 I. T异常,
& u% N$ n4 a& J, L不正常。
" b- |! x b. x3 D4 C @天线,
x& G$ Z& H- a' E, ^! B5 K一种与发射机或接收机共同工作来发射或接收无线电: f1 F4 F8 c' _; \2 L, f% ~
波的装置。
( ^) m; E X4 j- N0 l+ V冰,
( ?! s8 s8 e' o9 q/ x防滑系统,
& f f" _9 T, w! M一种在任何跑道状况下,都能提供最大的刹车能力而不
/ r3 x$ }; g/ n! O4 u4 n& F: n使轮胎打滑的系统。防滑部件是刹车系统的一部分。5 [- U1 b5 D% J2 r
of lights. Each light indicates the condition which exists! h/ `" c) k8 N2 c4 {
or has existed in an associated circuit and is labeled
) q, e# N* p: m- eaccording2 J* w# Q- [. _% Q. b2 R- G
A
- q2 y" P* G) M: {th
* M+ q4 i# [# [$ Y* {/ tA- H% n' P1 ^2 O1 O! e
w
8 M' N9 b+ N0 n# R: Hc* t; G! `. s" t7 l* M
通
. x; s% B. i! |& L& Y8 h8 ?$ L9 {信号牌,1 K) H9 q$ O3 m n; {/ q& u5 f
由一系列指示灯组成的目视装置。每个指示灯都有相应5 s3 P; D/ r" m- \. I
的标记,用来显示
% v( d) P2 w9 K r) m' t情) x i( k* Q& \
防: e$ y: k! s( _
防止机翼前沿和发动机短舱结冰的一种方法。
0 p4 I, g% o+ A英汉对照民用航空词典B OEING
% s4 c2 o0 w8 \7 Z1 j2 STECHNICAL DICTIONARY 12' {$ Q# b9 X2 F8 M6 t' c8 `
APPENDIX, A supplement to the Airplane Flight Manual2 q) ~( d& e* I. u" j+ Z) m$ v
tained in the basic manual. A+ g: S3 q6 k) R$ T ]5 B, G M
ollection of supplementary material at the end of a
: k. u$ `- b, f* S# Kook.6 i" x$ b. G- B; X( a
of the
0 x. K: h# h! C- e) Srsion link on the landing gear.
* I8 j3 r5 i; M& ^0 ?6 D+ oAPPROACH MODE, An autopilot/flight director mode
( P7 r7 L/ u* e8 D& twhich is a combination of localizer for roll control and
0 X! ^9 M$ Y; ~glide slope for pitch control. This mode is used when full
/ t$ I1 L' N( A. k& minstrument landing system is available." _: }* x- H) f
APU, SEE - AUXILIARY POWER UNIT/ |$ q$ q9 j" v/ c6 {1 d
ARINC, SEE - AERONAUTICAL RADIO
. D5 O) g9 t" q! \- p: HINCORPORATED
/ x0 y/ I/ e- Y3 i' v; v2 KARM, To make ready for operation.
8 z0 F4 p; e/ d3 C0 w/ v附录,% v1 Y* }+ {0 _1 g
飞机飞行手册的附件,包含基本手册中未提到的飞机形 {8 ?( r4 n$ Z" y/ b; A. |
态的其他性能。是附在手册末的补充材料。
. B' a3 q% e: L; o顶销,5 H7 G7 a4 a8 C9 j7 Z1 C+ e
用于连接起落架扭力臂两部份的销子。
1 i# o% {& h" R; O, g进近方式,
) I0 e. U& P! g: T一种综合了控制横侧的航道信号和控制俯仰下滑信号1 V; z! ~, j9 x& w2 N
的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系7 a* r$ Q$ O! O7 g/ R
统正常时才使用。
; u7 n( J. A1 F& I% H' |辅助动力装置,, y3 M/ f% @- J0 `9 a& r; ^
见Auxiliary Power Unit
* f$ p0 _9 {: Acontaining additional performance for aircraft
- R, J7 M% f6 |8 j: B! Z3 Wconfigurations not con/ Z9 o7 b/ Q" `
c
. W9 L! G2 @2 Wb
+ B& U; g: S# g! o3 d9 vAPEX PIN, A pin for joining the two sections
8 m4 V; y1 M8 g5 P6 wto
7 x2 j6 V/ K0 v/ Z: F. x# ` u2 `." |( C# H$ t. k( [3 d2 l/ C9 j
航空无线电公司,
- l$ e6 ?) h- k! o% ?* E, N3 G见Aeronautical Radio Incorporated.
3 R. M$ t* ~0 C8 o' n预位,
$ y4 G1 J7 R8 Z9 `$ x1 u* y+ F部件可以开始工作的状态。/ ^0 m, p6 s& h' z% c1 E/ S
英汉对照民用航空词典B OEING9 `7 b% z7 W" u; h8 V) W/ a
TECHNICAL DICTIONARY 13
! ?$ }$ S& V+ W" D2 Q9 ]+ o' P) uARC, The curved track over the ground of an aircraft' k: u( n% o! K8 G1 {6 b
flying at a constant distance from a measuring
9 I. C1 v/ Z X, z) H! Bequipment (DME).5 G. ?. Q" n3 o5 [: s3 `4 p6 ]* ?
in the limits of self-contained system
& _3 v4 l, j% r4 [* G* z) k; qapability.
* n& S" O) @1 ?; C! R6 ttem for opposing or restricting6 v" a+ z% `- q
ovement.
% i) {) z$ a) R9 YSPIRATED TAT PROBE, A sensor that measures total! ?! | d' I: T: N* A6 S
ir temperature when the airplane is in the air and that
- R. c, N+ r" N6 ^/ R8 U( Weasures outside air temperature when the airplane is/ ^/ t$ I+ m) l! P; J6 x* S
n the ground. The outside air temperature is measured% t6 C: w6 K( K: c: i+ L
SSEMBLY, The fitting together of a complete structure
3 q8 q' F, b1 b+ `5 ?, }# K6 n9 ESSUMED TEMPERATURE REDUCED THRUST, The
4 @0 y. I9 i" k* W$ eATC, SEE - AIR TRAFFIC CONTROL
2 ]5 e; r) o0 y3 ]7 @3 _$ \) x,
8 f. l3 D) v: s# O系统中所产生的一种用以抗拒4 O/ M$ H) i% [4 M9 k1 ~6 u7 r2 Q
作或限制动作的力。0 k5 u5 n" K' T
头,
" Q+ P5 o3 Y; o4 T' {/ S用来测量飞机在空中时的总大气温度和在地面时的外+ b: R/ a! Q, p
温度。地面外界温度的测量是利用引气将外界空气吸入
7 e5 D: n& m6 }; q' g+ S! Y头,以达到测量的目的。
1 G( _+ j- T& Y% }4 O配,) R% ?& ?4 i0 X* r1 x' h) d
一个完整的结构或组件的过程。
1 L$ A* k" B, i5 e假设温度而得的减推力,
3 }, S# u3 \1 o& t; r" R2 e推力设定值时,假定一个比实际外界空气温
3 K9 \) j' T, G" p7 g3 n c空中交通管制,8 s( f% q5 s0 m
见Air Traffic Control
w5 F3 r& u- Z# e2 w7 c: z. wAREA NAVIGATION/RNAV, A method of navigation2 _. i5 P$ S* w0 I# x
that permits aircraft operations on any desired course0 e% h+ C- M! U% U& W
within the coverage of station-referenced navigation
! y, K% ]! X0 {/ Msignals or with- d9 q$ v8 ]4 A& ~- h! t2 z
c
) L' }0 a+ @8 w! }ARTIFICIAL FEEL, A force developed in the flight
$ E/ D1 q4 u3 y& P* Vcontrol or brake sys
5 g5 X$ s' R: j& p n) Ym5 g9 P& J7 n' {; m
A- ?$ N4 G. n5 P
a
& E- R7 S7 c: J2 g1 @m
7 Y" d" W( N8 y+ p( o0 yo
2 e6 q1 H" ^4 ]0 Z$ I- ?7 Wby using bleed air to draw ambient air through the5 }9 y/ m- T5 w# x a
sensor when the airplane is not moving., X V7 K1 T7 r- L
A8 ^0 s! u! `# p4 \
or unit.' w1 Z8 l- X8 K( R
A
& x: }4 _; H& R9 F" \, dlower thrust obtained by setting a higher than actual
& f. `+ B$ m( ^( ZOutside Air Temperature (OAT).* j' R9 K9 K) z0 m
弧线,: n# [( V: t3 ~5 N9 t( G
飞机在围绕DME台等距飞行时的弧形航迹。5 r6 |! y3 k- S. B. U
区域导航,3 R4 T; B1 H- g E
容许飞机飞行在有电台参考的导航信号或自备系统能/ ]. q9 Y6 |' J. B
力极限范围内,飞行任何预定航线的一种导航方法。
: N2 c1 p% d. o5 a& S$ e* I1 M模拟感觉
* C. A: s {4 G$ R0 g在飞行操纵系统或刹车. I% H) K) w% h
动
7 z8 n- g8 f( T, T! j吸气式总温探( ~$ u( U2 w7 w; Y& F m
界 D1 m! ]+ y" t; b) B( G0 ^6 h
探
3 \2 {* A- r B3 Y2 e装; G8 p& O, M1 b4 |
组合成# u% ]9 \4 W% B7 l
由* z, S( a% G/ O3 \, T* g4 ^+ v9 }$ o- O
在选择起飞( s7 j+ b# j" S, w+ l
度高的温度而得到的推力。用这种方法可以减少发动机的
1 S. @6 f. R t) G* Y& t( l. b+ Z8 W磨损和维护费用。/ B: t' U' z- G7 h. E4 e
.
; y) W) w) P7 ?7 M6 `' P英汉对照民用航空词典B OEING2 W3 D* Z- V, \+ T# {& ]4 [
TECHNICAL DICTIONARY 14
9 l; t8 q+ S* H! ^2 Y/ MATE, SEE - AUTOMATIC TEST EQUIPMENT
4 r* }2 h, a! ?. e/ RATMOSPHERIC PRESSURE, Pressure of air due to the6 Y7 _" a* [( O& I- B. D
arth's atmosphere, expressed in pounds per square
( d' H3 i& v# U; ~; K2 L" W1 gch (psi) or inches of mercury (in Hg) or millibars (mB).7 e' m8 D( O/ w$ U; a# b* h" V
TTITUDE, The relative orientation of the airplane with
0 S4 q$ \$ D4 l- n4 ^, Vspect to pitch, roll, and yaw.
8 t( `/ d* A6 V8 f# d7 f9 x0 ~UDIO CONTROUSELECTOR PANEL, The panel in) u6 c; u4 g; |+ Z7 ^) U7 Y, E
e airplane which controls and selects the routing of& [+ [+ ?' Y" h% P l
udio.
, v8 v# V( a+ G4 {8 ]% gUTOLAND, Automatic landing using the Digital Flight
% `, o) c8 m( tontrol System.* G, g; Q/ [$ ~0 g" j y2 m
n.8 q3 G6 Q# ^8 I+ A
M, A system( s$ o# J9 m+ R" Y: ^9 c
omposed of all necessary subsystems needed to guide9 O* U& h. c" Z1 h, E+ w, f
e flight of an airplane.; ^, D6 v! n& n* d$ p% ^
EQUIPMENT, System test
: D. r& p6 {( _% v; Fquipment that operates under computer control.: W1 [) N" f; ~; _- }6 W
装置, |
|