- 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 produc
5 h9 L8 S% W, ?# i6 ^4 _data information, such as altitude and airspeed, based& N8 I6 X5 Z4 w
on pressure and temperature measurements.
+ n4 Y* c. E: p: Wes air
# K1 c m. C l; F1 vIR TRAFFIC CONTROL, A system comprised of$ G. H7 {( B9 v, e5 }7 }7 M+ F
round and airborne components used to identify, track
5 d& D) @+ X" R6 VOUND SENSOR, An electrical device operated
3 t/ K$ ^( s$ N7 H0 a% A$ {y the landing gear, which transmits on ground/in air
' f3 X0 B- j0 M o! G3 tformation for system operation in flight or on the, q; Q2 B/ ~! J( f
round.
1 Z' S' P& c8 X: n+ J) TIRBORNE VIBRATION MONITOR, The AVM takes, K& L' }; `- p# [
e signal from the engine mounted accelerometer and0 W- q k! N9 r$ R
alculates the vibration on that engine.
# {, l1 h9 [' q, r/ rcorridor equipped with radio navigation7 I' ^* l% O3 o: @
aids.
]' M! h$ [: E- L* Z5 E& D5 gAIRCRAFT (or ARINC) COMMUNICATIONS
2 c$ Q2 P8 H& _! x) j7 Z5 PADDRESSING AND REPORTING SYSTEM, An6 `4 V( v: X2 [2 G
addressable digital data link system which permits the" `% c. H6 A0 E# M5 @( U. |
exchange of data and messages between an aircraft7 p6 I A5 Z1 D! R& P" n0 h5 s
and a ground-based operations center over a radio/ a. b# Z8 ^% _, \, D3 V
network.
' _+ b8 l; \! o* V5 m3 j6 T' S# VAIRCRAFT CONDITION MONITORING SYSTEM, A
: w7 s+ q$ X6 H7 [* usystem of sensors and recorders to monitor various7 F) c, D8 j: M8 ]$ M
airplane systems' performance and status.9 A) |8 x$ {) b
机,1 y: Y' r9 b0 n7 ^; b3 \5 X
中交通管制,
5 q% s8 D/ L. D' q一个由地面设备和机载设备组成的系统。用来对飞机进2 {) m5 l: ^$ y5 t
地传感器,& B/ T) K' k$ D, A1 |: b
一个由起落架操作的电气装置。用于给空中或地面的飞
/ U- n0 F3 s* ~% R系统运作传输地面/空中信息。(有些系统只能在地面
$ `% h/ t0 o1 [6 m用)* `! X8 Y5 q" _7 G6 C& I- i) t
载振动监测器(AVM),
* K$ q6 ~. ^, ]0 x6 a1 JAVM从装在发动机上的加速器取得信号后计算出该发* l4 ^1 K A4 b/ V9 f/ l
机上的振动。5 G/ ~ W: X( z. Z B! w) ]5 f) g/ U) g
式建立的控制区域,内有无线电导航设备。4 W1 z, ~3 w: i
飞机通讯寻址和报告系统,: D4 X. }, h) I) R) u" P
有种可寻址的数据通讯系统。利用该系统可使飞机与地
& _, L7 A0 \! x面操作中心通过无线电网络进行数据和信息的交换。9 D9 ~) W4 h- T
飞机状态监控系统,% I+ e# k, K5 v4 W% L% G' d
一个利用传感器和记录仪对各种飞机系统的性能以及% G8 ^7 `2 C j* Y( m
状态进行监控的系统。1 E0 ]$ ?; T9 ?& [; Q: J0 V
A. [& I0 y1 Q. r" Y9 B0 w1 b
g
1 }" ^+ f& i, I) @1 I- T9 rand locate aircraft.& j0 w9 r6 m$ V: h
AIR/GR
2 U. t7 r: |3 t5 b& w) C, ?& [& E; ?b" ^. S$ d! J6 {' m4 @3 }
in
" T0 \3 \' P9 s* `g
0 P& R: D9 a. C+ gA
* Q/ P+ l# g) J7 mth
4 @ V& h6 w9 }c \5 E0 [: P) J1 K3 I
AIR WAY, A control area or portion thereof established
$ B0 A( s- O/ Zin the form of a+ A `5 w2 e1 s) o4 J3 [
大气数据计算
. n* N- T7 Q0 [根据量取压力和温度而产生大气数据资料(高度、空速
; H: h/ f7 F0 s# |/ I8 X等)的计算机。
" U" U p% y* G4 |; k空
z# Q; j4 O$ a* E4 [行识别,跟踪和定位。4 z H; r) X: ?# j' p. f9 G
空
1 y6 i$ j S- x4 Q* m' b机' @8 P! n/ q' F
使5 o9 |- x6 D9 a0 e
机
3 K( j/ L3 v( L7 F/ ?动
& s* F# @% y4 e- M3 N航线,
# @" }4 I1 _; d以走廊形
( d7 a& d( P6 V% Y& e w英汉对照民用航空词典B OEING
( A) r0 t8 U4 M* ^TECHNICAL DICTIONARY 6
/ d2 A/ v' ]* ^) T4 [9 H L5 DAIRFOIL, A surface designed to obtain a useful reaction,( J8 S& k% `- d, D% B
such as lift, from the air through which it moves. Wings,
7 G x& V) I, S$ i5 Q# v3 rstabilizers and control surfaces are airfoils.# t# e5 x5 F+ P9 P" {
AIRSPEED (IDS, TDS), The speed of the airplane
! i( I! R/ e$ g/ R& Y; [rough the air.
! z- G, a) a7 {- H P9 ]D INDEX, An adjustable pointer on the4 m/ n7 H( \& f6 F: ~ H
irspeed indicator.0 f; V; u; D+ b9 S- w6 A
and legal ability
; a$ d' s, t+ l- R. J0 R: Mfly.
% H/ {& `9 }0 p# |- a4 Tm, for example, the procedure for finding the
. a: C' \* d, m5 vquare root of a number.
! l0 x: h5 f* by
& x; i8 T8 L9 J/ f/ [+ p; Ire, wind,2 Z* ?! ]5 Q) ?- z
and aircraft flap setting./ c; D3 ]2 T3 c- x# P
是翼面。) n9 M! f0 K- o1 f! X
速,
6 n. ?" P, n2 T' Y! q8 q- W飞机在空气中运动的速度。
( x0 g! B7 x& Y% X& M/ f,, U) ?/ y$ ] m# I# S9 F/ h
在空速表上可以调整的指针。- r9 i( }1 a0 T% L( v- H# [
机械飞行能力、和合法性的飞机状态。: p6 p% L. M ]
一步一步的解题方法。例如,计算一个数的平方根的步7 n, O5 v* ~ G5 b
。5 k- Z6 y/ O2 s x- L) A
能% s1 h0 f' I6 t& M8 Q9 c5 J
资料的法定文件。
- K& e# j% _. O) Z翼位置成函数关系。5 O1 z' Z/ G! ?3 G( h; b" i
th
+ t2 r3 ^! F1 i' x. X1 dAIRSPEE
1 y0 T. x. c1 a% o& e0 v/ n$ Xa" v. ^) U$ Y/ W% \/ _
AIRWORTHINESS, The condition of the aircraft with7 }! T1 p" k2 `/ v0 o; w% p
respect to its aerodynamic, mechanical,
V5 u& H; f! ?0 @6 h0 sto
' j; n, E; ?8 @* x! FALGORITHM, A step-by-step procedure for solving a; Y4 T( e0 g, \
proble
% {3 \9 U4 M' Ss6 z: d# T7 h* k( `, v8 S0 Q) h
AIRPLANE FLIGHT MANUAL (AFM), The legal7 J$ T( O Y8 d, t8 Z0 T! _
document containing performance and operating limits,
3 S" X/ E; I0 N. P: ]+ Aoperating procedures, and takeoff and landing
0 k+ Y. ]5 p% A T5 Hperformance.
4 @; i/ L) s0 s' z) DAIRPORT ANALYSIS, A comprehensive set of takeoff
$ G! V4 ~, m* c: j" Bweight limitations for a given airport runway, generall
0 r; p* M! o# n0 l; ]# ppresented as a function of airport temperatu9 n$ d% s6 c7 L d* W, s7 ~
翼面,
w& j, a n* \5 `+ {- d, \% J4 S6 T用以从气流中获得反作用力(如升力)的表面。机翼,' {5 s% ?) t# a! Z
安定面和操纵面都
1 {( U/ q s% z9 ?5 t空
9 k% q! Z" S- F/ ^& Y! w! Z空速指标6 D4 `% A- N! h" ^! q& y/ Y
适航性,
! }: j X5 m A有关气动能力、! Q$ q! s; P @0 Y- \4 K* b- R
演算法,
, p2 i: `# K( q骤
: L& {7 i, z3 A" [& w飞机飞行手册(AFM),( L! Q" u2 r# \8 X0 s
包合性能极限,操作极限,操作程序,起飞和着陆性' q6 v! L: ^0 r, L4 v* T3 s# R
等
- W: t; w, j/ C& U& Z机场分析,
: R+ [+ h: M3 w: t一套针对给定的机场跑道的详细重量限制资料。通常与; p5 e7 E. Y4 Q
机场温度、风、和飞机襟1 B0 Y# P1 s6 ], `: n0 F
英汉对照民用航空词典B OEING% L4 n; ^& x+ G- w7 V; b# x
TECHNICAL DICTIONARY 7' A0 i }6 N- B
AIRSPEED BUGS, Adjustable pointers on the airspeed/ y0 w1 g1 U" a8 b; r
indicator.
1 Z' [; K! z$ c% F6 N6 K5 R/ WALLOY, A mixture of a basic metal and small amounts
8 T8 V! ?! Y# w. y+ _2 C4 v5 P+ Kf other metals to change the properties of the basic
" ]9 Y h! Z9 l E; Tetal.
/ ~9 K% |5 c+ W7 I* Q: _* \/ ~Minimum airplane speed.* ^ s& S+ _3 Z
e of$ r4 m) y* _% h e
itting airplane angle relative to8 ]# U7 c8 Y% z2 f: C$ V& q
irstream for the stall warning system.0 }( n2 }$ ?3 z6 y' Y: _8 O
another.0 [% r. ]1 T0 u8 w5 a
LTERNATE , An additional airport selected during
- `! G1 I/ l8 q6 [. K,
+ d6 _9 G! g! Y6 Z合金,
/ \ n, i, y+ S7 Q( T9 b在金属中加人少量其他金属,而改变其性质的一种金属1 X6 E9 X. ^" r1 W0 U) C
合物。+ ]/ Z6 P2 N1 F3 Z$ J$ G/ Q) e
飞机的最小速度。
* Z4 J* k6 w- N) J- e速警告系统传输飞机对
) e' Y" Z. m. K; Z! E' n1 A流的相对角度。
, Z' b* V Y3 k' V. |; ~由一个状况改换到另一个。7 y3 b. P, G5 p1 h' ^
降场,3 ] V/ ~, U, S" t, S
划时,除了目标机场之外,所选的另一个机. u: B1 f6 K2 Z" z: [( u- r0 ^
o
, I. S& n1 \ N9 ]8 P5 q. bm# W( I6 G5 D* |7 Q
ALPHA SPEED,; r$ E2 P1 A. l5 p" {
ALPHA VANE, A small moveable airfoil on the sid
! f) a$ g. M; w; }the fuselage transm3 j9 N& L$ \0 {, q
a
4 Q0 j! ]" L2 {) O' }ALTERNATE, To change from one condition to! Z/ S9 X( p8 y" C) d: n4 H/ _
A
* {1 i: X! D6 u% Z2 |flight planning, usually near the destination airport, to be% q( E i: w* O( J, p9 }
used when it is desirable to divert from the original
2 C( S) V) q9 `5 L/ mdestination airport.
( s8 N7 E; s, u( w. F空速游标; h/ d) p X1 J6 G
空速表上的可调指标。
8 m, I) O2 @$ _, x# s' K混
; Q8 Y" X& o k8 k7 |* w& _6 G! {迎角速度,7 a. n8 Y- F% J# ^! k
迎角叶片,
8 z4 b+ _, y5 k/ s2 Q/ I位于机身侧的可动小翼面。为失9 ^& l {2 K: O- H
气( ]1 B1 X! K* O
交替,: [; i7 Z: g9 T3 }. z
备
' r) J0 r! C, t" s2 _2 H" [制订飞行计. v$ y7 j# u* J+ ]4 t, h9 m0 F' [
场。通常在目标机场附近,以备不去目标机场时,改降之! D0 n+ Q' i9 U% r4 |8 L2 a* S
用。
! q$ i$ K6 Z4 h& x1 u英汉对照民用航空词典B OEING
0 F" w+ c7 X8 {; Z* l5 ?1 f# J3 VTECHNICAL DICTIONARY 8
0 u8 ?3 {5 M% d0 A9 F C+ N3 {ALTERNATE AERODROME, An aerodrome to which$ {" F; K( }' Z! p
an aircraft may proceed when it becomes either
' B9 V3 f Q( Bpossible or inadvisable to proceed to or land at the
; q& v, L6 s; n9 ~8 H. h$ lerodrome of intended landing.
+ v0 Y! s$ W" M8 ETER SETTING, The adjustment of the altimeter
& ~, o0 g6 M# Y/ j# n) q% Uaccount for local variations in atmospheric pressure.! L7 l0 h1 w* s9 D: Q
LTITUDE ACQUIRE, A digital flight control system9 S% O! v) ?; f( i5 {: @+ e7 v6 X
ode to transition from climb (or descend) to level flight.) M2 V+ v P! V5 A3 R X1 i
LTITUDE ALERT, A flight deck alert occuring when the
, i( J/ y! R" J& ^$ p" Airplane approaches or departs a selected altitude.
& A# h5 V/ {) g% f) E; _LTITUDE CAPABILITY, The maximum altitude at N+ ~' I/ Q- z& b7 H! {
hich the airplane can be flown at for a given thrust,/ |$ _; Y( K' b( L2 h' i" U* ~8 h& H
peed and atmosphere condition.) S" \( v8 {6 A% j# q' ~0 L: l
LTITUDE HOLD (ALT HOLD), A mode of the autopilot" k, }" }3 G0 ?7 t2 i
r flight director to maintain a selected altitude.
$ s$ G ?4 f1 I4 R3 Oirplane's altitude during VNAV operation.* T c) o' ~, y; _" U4 V
机场着陆时,可作着陆使用的
7 a' S8 U& N% j% W! T4 s9 T场。
3 p5 Y- A) M4 H* V,% b! D4 J! K+ D6 @
根据当地大气压力变化而对高度表所做的调整。
; _' z' Y, V1 l2 J9 n) \一种数字式飞行操纵系统,从爬升(或下降)改平的模
& W t! J$ q& w5 L( z7 O" s。
( k2 }+ Q" I! @- p- u度警告,
0 n4 ]% n' \$ f3 a" Y# f当飞机接近或偏离选定高度时,所出现的驾驶舱警告。
* T( m6 @8 X7 e- Y) v8 a2 i5 @+ J高度能力,
k6 I9 |( Z+ }9 O在给定的推力,速度和大气状况下,飞机能飞达的最大% n2 G' V% H( h9 P1 G& J+ S1 @
高度。4 e) u j6 h% q" w" o7 Q
高度保持(ALT HOLD),
' l7 S! x$ _2 r* i3 a自动驾驶仪或飞行指引仪保持在选定高度的一种方式。$ I9 D& s0 }; S7 \( h
,
0 `6 i! Y4 y" m& P员对飞行高度的控制。
0 d! `/ N. G( Zim
, o3 W# q9 ~* N. W/ ]1 ]) Da
' ]; g; r0 ^. R1 U6 ?ALTIME
( I B/ i% P& | B+ K3 qto: G* R. N) r8 i
A# I f% ^5 t* h9 X
m1 v, e6 K/ [2 j2 }! a! Y( y' s
A' v! l+ J* T7 c' c$ g E
a7 v9 `, { e/ P; @, t0 e
A
2 c% C2 R! r. C4 e5 e1 t. Uw
) d, p% c8 W( w- As" j$ K2 l& T8 h2 L. A! L3 h- w
A& u S( Q! c% w' k7 S+ C! i
o
) c4 E, S) P' I: {2 fALTITUDE INTERVENTION, Pilot control of the
- ?, X0 W4 D) K/ c2 w ?a
- L" \% R& m' ]$ SAMBIENT, The surrounding atmosphere.
' O# R( Y: [% s9 W/ d备用机场,
9 m( s6 q" |/ a2 j& N1 ^9 g* j* @ K6 J当不可能或不适宜在预选
; I6 p; A8 S# i, ^, H机) Y5 O" ]/ X6 y6 v _3 O7 q/ g
高度表设定 ^2 r" ]/ f) L! C
高度截获,! a% U6 ^$ M" Z' E% t
式
5 N0 `( P/ c5 G+ P; X# Z5 j5 X9 T高7 ^8 r- {. Z x/ \, a6 D# I
高度干预
& C) B3 g# v" u$ F" ~在垂直导航工作过程中,飞行# j1 J- V( F- H, w) k$ u5 U
周围环境(地面气层),
s) V3 F) U/ E" I物体周围的环境(特别指大气)。
7 R9 E* t9 I/ x6 W: f' @英汉对照民用航空词典B OEING$ c" q! @% ^* g; y- R' _
TECHNICAL DICTIONARY 9/ W1 ^. c2 S4 z7 e4 P4 ^
AMBIENT PRESSURE, Pressure of air surrounding an
8 q6 h6 |# J' ?( hobject, measured in pounds per square inch (psi) .
$ Z5 \! B3 e6 b% n/ MMBIENT TEMPERATURE, Temperature of air
9 L1 d0 \/ m1 Z! l+ H7 g, Wmpere.
; v' s4 I, ?9 _- Gurrent waveform.
$ m4 k4 m+ j- U7 n/ ]3 \2 s/ Mg an! z$ ~" A/ x$ }% `% y) K z
nalog signal to a digital signal./ e% }+ z$ P* ? e- ]
ore inputs p5 r1 z* d d
f binary digital information and one output. The output
8 f) o1 H* S! H9 V4 t! o1 only when all of the inputs are 1. The output is 08 X7 \' J8 ~ U9 I' k
hen any one or more inputs are 0.- C5 [) h( K& P
面气压),0 z6 q# Y2 ] E/ R" [1 a
境温度,
! h/ {: x( E$ ]3 n/ `# F; @1 X气温度,用摄氏度(°C)或华氏(°F)来9 y6 u% N: z. C* s# @& p* H4 E
。0 Z- ^% b7 p- Y& t" U( L
电压或电流波形的幅度。- h) G& ], h, K
性变化的信号来工作,或产生连续性变化的信号# ?: Z3 C/ J% _1 R5 b& ^
统。( Q5 M" T' l( d# X! D
将模拟式信号,转换成数值式。( i3 J) ]* f6 ?7 M
一种有两个或两个以上的二进位数字信息输人,一个输7 Y% B6 g k( I* b
的装置或电路。当所有输人为1,输出为1。当任何一个
1 w9 V, L! K) n5 N一个以上的输人为0时,输出为0。
( v2 Q8 a# @8 ^" o/ m: { q: r5 h+ Q LA
, Z' n& E8 j, Y' ^, d) Msurrounding an object, measured in degrees Celsius8 M& r f) J) [
(°C)or degrees Fahrenheit (°F).
8 i& L! R+ ]. z# EAMPERE, A unit of electrical current. One volt across
' y) H% t( P- lone ohm of resistance causes current flow of one) E4 a3 t3 s8 S9 R4 m- B$ R. [
a
: ]8 _# N ^5 RAMPLITUDE, The size or magnitude of a voltage or
1 m h6 f# N% V7 x7 jc
$ c/ ~) n6 n aANALOG, Quantities or representations that are$ P8 t1 x. a8 E3 A- S7 T9 W% U% }7 h- P
variable over a continuous range.. Y) M* Z& P3 e/ ~
ANALOG-TO-DIGITAL, The process of convertin4 ^7 Y+ }9 h5 E- U6 `' o) ~7 }
a' B6 ]9 k0 b, F1 V2 S$ F
AND GATE, A device or circuit with two or m
; }. R9 C' n! o# \3 P- f- Fo( {$ f; }$ D1 D$ _
is; @3 K: x. ?7 Z; i# @# o* d2 |9 _2 q6 X
w
N* } O% [, Q( V; @环境压力(地
2 X% {. G5 {& l- s. R' E: f6 N% u3 e N物体周围的空气压力,用每平方英寸多少磅(psi)来
# E0 Z C9 F# c/ x' y度量。
% I$ t/ m5 e5 M6 }7 j环
" K7 E9 P& V& k. T0 f7 h q% i物体周围的空9 X* j8 L7 G O! z0 n y& X+ V
度量。
/ ^6 O& @6 {" o2 G! c* B. A: O安培,
& }; O5 W! L% v* x! c电流的单位。
, M$ \! U, P& a5 O# r* F3 e) `9 y1伏电压在1欧姆的电阻上所产生的电流为% b* n- r g4 |4 U
1安培$ k6 L7 {+ L: O
振幅,
$ }$ C Z# E! u# Z* z; C模拟式,
3 P* T. A6 ?, I8 }用连续! [; ~9 {" l' U: T# ^5 S
系
e/ j& S8 J! a2 u% I从模拟式到数字式,
1 f6 z, c0 b% o与门,9 A7 t5 |: g7 l7 {) D
出/ }0 U4 |3 e( `7 `& |
或$ k, G4 ^, l4 K4 D: b1 W/ x0 j+ F5 X
英汉对照民用航空词典B OEING/ Y- [9 A7 K( [" x$ q
TECHNICAL DICTIONARY 10
1 H8 V% o" k( B B# vANEROID, A sealed flexible device containing air at low
l1 @# j, Z) ^# H7 S5 {pressure, which expands or contracts during change of1 ?; Y% @( l1 v- t
ressure outside the device.
9 y% f# T0 I: y f! L# h1 D/ }ically# B4 b1 e: j. V+ O6 J. n
r changing the direction3 _; \' H" m* O; e3 }) z
f drive.$ e! K9 h: T3 Z2 C: r/ b
of the wing chord in$ t; }# W% a4 @) t/ d
lation to the free stream airflow as it moves forward
6 U( `8 W$ o, r; m* T. mrough the air.
1 N! r! A* g+ i) b$ S- J Fal axis of the
1 ^! f1 x. H$ w% W! T2 H/ Maircraft.6 d; @- E% _% H( n4 x- P$ B
胀或收缩。% l3 C5 A7 P& c% `' W" B
箱。是改变驱动方向的机械装置。5 j+ U) i4 F/ a3 h' Z
机翼翼弦在空气中向前运动时与自由气流之间的夹角。
$ U6 p4 ^4 Z' h9 q Q- ^6 v。) j% U5 I; h& G8 e& d+ U4 r
p
J& x& q' a$ d* f! y+ dANGLE GEARBOX, A part of an engine, mechan
. H" s" N d) I0 ddriven by the compressor, which drives the accessory
3 Z& |2 R# n7 W6 b Tgearbox. A mechanical device fo
9 s$ d7 g7 u: T6 e/ K0 l8 S0 g* lo
& P: Q8 T+ Z X/ c8 F- d4 YANGLE OF ATTACK, The angle
" U0 i, I3 i9 V1 Qre
, w3 b) z Q0 vth) x& F6 b9 m. M3 q" b
ANGLE OF INCIDENCE, The acute angle which the
( P0 b8 c! {, b7 G! m' Jwing chord makes with the longitudin$ ]7 f8 V- R: }8 q
膜盒,% p3 `) T3 v( l9 F, K
内含低压空气的密封弹性装置。当它周围的压力变化
; W& P3 K& j, q, f8 b, j( ]* D时,会膨
0 T @# Z5 |) {. t8 e伞齿轮箱,' n4 l. W8 B( J! T
发动机的一部分。被压气机以机械方式驱动,然后驱动" H' D3 Q1 \3 {! B, C; J
附件齿轮! r9 n! h% m! \+ W$ _
迎角,
# P! f: G$ M/ o6 [5 _& {安装角,
: D" |/ Y- v+ y* P8 ]3 h飞机的纵轴与机翼弦线所形成的锐角
1 A' ?5 t8 z# ?- C ?英汉对照民用航空词典B OEING
! s4 [" {: p2 M0 ?) [ W, ]TECHNICAL DICTIONARY 11
* v1 [ A# u1 T3 ~! I n' kANNUNCIATIONS, Audio or visual indications used to9 ^+ i1 h' Q9 V6 B2 j C1 {
call attention to an event that has taken place.5 j2 x' t+ {% I, d( \
ANNUNCIATOR, A visual device consisting of a number% e ?# c1 p( f- a, N. ~/ K
ly.
. [+ |6 w# V. m r% W) b8 BANODE, The element toward which the principal stream0 F( @# ~! k0 M* ]$ ]1 K
of electrons flows./ g' h' s4 ^$ P% X3 a* x$ E
ANOMALY, Not normal.
( z9 J* {( z$ {8 m8 `$ K6 JANTENNA, A device which, used in conjunction with a
, i+ b' a) G, Z, R1 atransmitter or receiver, is used for radiating or receiving
/ L" I C! p/ n8 t- I. j2 U9 Jradio waves.' c) ]3 h7 m2 { \" `
NTI-ICING, A method of preventing ice formation on
$ i M- a4 Z: }* Je wing leading edges and engine nacelles.7 P: m) t' T9 D4 q8 O# P' I
NTI-SKID, A system for providing maximum braking5 ]0 M& f# m3 t9 B* s0 o# k, E2 m
ithout skidding for any runway condition. Anti-skid
% Z8 F6 y$ H w' Q8 {omponents are part of the brake system.
^# T f8 h N3 R0 q告,
1 y6 [; W: w8 `6 S& n当发生事件时,以声音或目视指示形成的提示信号。
* p8 N' Z% L! [0 t与之有关的电路的现有情况或已存在的
& ^. I& h. V( t0 X5 v8 O况" E: h$ o' q0 {. e9 ~
正极, }4 v" V9 s7 O
主电子流向的极位。 H0 v& O( l9 @' g( n) x6 ^
异常,; o L/ `" G( y
不正常。
- ], \, J2 H, N+ j( ]天线,: C0 u1 g @( V) B; W' D9 B
一种与发射机或接收机共同工作来发射或接收无线电6 R4 M: a+ L7 S4 d" V, [7 Y6 x
波的装置。4 {0 b# t) O% P+ l0 h
冰,
" w2 g! v$ t5 _0 ?防滑系统,) {5 X5 A; R6 d
一种在任何跑道状况下,都能提供最大的刹车能力而不
6 r( h9 E' J& z使轮胎打滑的系统。防滑部件是刹车系统的一部分。* q9 F7 s! {$ l: u
of lights. Each light indicates the condition which exists
5 y' Q4 X/ J# t% r& b, Hor has existed in an associated circuit and is labeled
! U" c5 H+ m) M9 ^$ [0 o- n* c2 paccording
( m/ C3 ?. }! P" YA
: D0 S! y+ w" J! K m% \3 M. Q: o) rth; O1 t" q( u9 y" `8 o3 u' \& T" u( J
A) u5 c# T- H. e: H) _: v/ Q) b
w
, k8 W( G& d1 v6 E3 ic
& l4 F5 K, Z0 {9 n$ H, r通4 G1 h& h2 A$ V- s; q3 _+ n- [
信号牌,
$ d5 P% d }' m% }+ a: s! B# A7 A由一系列指示灯组成的目视装置。每个指示灯都有相应
5 z% `& o% ^8 C" z的标记,用来显示! M+ v Y# k' A$ _% i4 V
情
, e( r N/ @, O0 j3 G) `防
9 Z3 I6 T) Y' o2 `6 j+ y" M防止机翼前沿和发动机短舱结冰的一种方法。) s5 Z' f7 ?7 E( H
英汉对照民用航空词典B OEING
' L3 J/ [- ?2 l, Z" f rTECHNICAL DICTIONARY 12
" B1 Y/ I, @4 F4 B0 M. zAPPENDIX, A supplement to the Airplane Flight Manual; ^1 ~4 s# k0 k' u- U* B
tained in the basic manual. A$ H; x+ n4 T a( k) Q
ollection of supplementary material at the end of a
+ t. N1 @, o$ Q J: Wook./ p5 `3 _' R) |
of the C9 V$ S/ l5 j4 L8 p* b
rsion link on the landing gear.
! H% h$ h9 s7 ^APPROACH MODE, An autopilot/flight director mode
' k# ^1 w# ~1 X* G9 w0 l3 G- Fwhich is a combination of localizer for roll control and
7 S/ W$ R0 j, ~5 w/ u8 {glide slope for pitch control. This mode is used when full7 Q1 @3 O4 A& h( `
instrument landing system is available.* m( \( J" B8 k. o% l9 j
APU, SEE - AUXILIARY POWER UNIT( ]2 r( S$ j! s6 G; f% T6 m
ARINC, SEE - AERONAUTICAL RADIO. k* {/ S; F; |3 g
INCORPORATED- z5 l# v7 e8 T. h4 R
ARM, To make ready for operation.$ j* h* U X8 d. v- D# v* Y [% H
附录,. T1 P1 l7 R6 x9 |
飞机飞行手册的附件,包含基本手册中未提到的飞机形
( }2 Y5 ^6 c* u9 g态的其他性能。是附在手册末的补充材料。
+ d" P* ]3 _% P# ?9 ]顶销,2 Z3 H* W- o6 e2 s
用于连接起落架扭力臂两部份的销子。
5 T3 M/ S8 m7 w2 [; B8 c- [进近方式,4 U2 q+ ]7 |" g1 Z" a0 L4 K
一种综合了控制横侧的航道信号和控制俯仰下滑信号
; g. f% X$ O& [* V; K4 I的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系
/ ^! x8 p' C/ R/ K5 g B% t0 [- }统正常时才使用。: x8 z J! T% U7 Q- X& u
辅助动力装置," T8 w9 z0 M( B0 E' B
见Auxiliary Power Unit: M+ U0 w& M. a( p
containing additional performance for aircraft3 F0 X V; x5 {7 O# [) x0 q
configurations not con4 o# t! k- i+ {) t
c0 S$ r! M8 w/ q4 R+ W6 q" [2 @7 ^
b
" \8 {2 D% [, @/ x" x; |* {" v' @APEX PIN, A pin for joining the two sections- W* I2 t! Q- Q* p
to) S7 A/ H( t8 r5 u [) x7 t
.& w' t6 s3 P% p7 r' q3 J& r; F7 {' v, y' l
航空无线电公司,
# w: \* B9 }. \) d3 r% R见Aeronautical Radio Incorporated.8 a2 Y$ O Q# A* h" u4 X, M
预位,8 F- {- ]5 c( @; ]
部件可以开始工作的状态。
/ P1 W9 J6 Q2 ] }英汉对照民用航空词典B OEING; c! d4 j/ u; c- W
TECHNICAL DICTIONARY 13% V: d$ y% f2 t. h! `3 ^
ARC, The curved track over the ground of an aircraft
' D; I4 } w7 G5 D D# Bflying at a constant distance from a measuring+ M4 s0 M$ E3 H+ E' U5 m
equipment (DME).
! t, S/ I3 n# E% _$ e2 cin the limits of self-contained system3 x* `/ R% T0 z7 h% L
apability.
+ w* B& u' E( I/ k: Z' Q1 utem for opposing or restricting3 p/ C& U- A0 F( E, |- m
ovement.4 d) I5 b0 I* I7 s1 z/ L/ Y7 T
SPIRATED TAT PROBE, A sensor that measures total
3 H; v! ]5 Y+ F, J6 c3 u7 Y' X9 X% `1 Xir temperature when the airplane is in the air and that# v4 ]9 l4 Z" E3 U$ @
easures outside air temperature when the airplane is& ~) \( _" T8 E* ]. ~2 J* h
n the ground. The outside air temperature is measured& U/ b' p( P" l: C7 {# _- E
SSEMBLY, The fitting together of a complete structure
3 J3 \7 |. U; Z' PSSUMED TEMPERATURE REDUCED THRUST, The; a+ r$ L7 C; p! S' D7 t' N
ATC, SEE - AIR TRAFFIC CONTROL
. I1 f8 W J. c,& S' `% A* ^; k v
系统中所产生的一种用以抗拒
* T) O3 w7 ~" O- p, f1 S0 ]& V0 V作或限制动作的力。
1 k, F% {5 L' ~( |头,* Q/ \, @/ w8 F
用来测量飞机在空中时的总大气温度和在地面时的外0 t. a6 z$ Y- O1 ]$ X2 I$ d
温度。地面外界温度的测量是利用引气将外界空气吸入
1 M$ Q6 m8 @. o% I头,以达到测量的目的。
3 Z y% V' [) K) K: {配,+ k. m$ ^2 p9 C# I9 o
一个完整的结构或组件的过程。
' l* ?; K. e$ K) u8 h假设温度而得的减推力,
0 T1 f3 W N0 l* X+ Z5 ~0 U推力设定值时,假定一个比实际外界空气温
) \0 f. h' [9 {2 C空中交通管制,. b0 B( r, y. ^- b3 H& t* X
见Air Traffic Control9 @" M# Q) X8 @; L7 D
AREA NAVIGATION/RNAV, A method of navigation: s2 ^. a7 q7 S6 O. S
that permits aircraft operations on any desired course
% W4 a1 o- s! _0 a' n" Nwithin the coverage of station-referenced navigation; q$ _3 N; G H' F z f9 t* ?3 C
signals or with
7 W# R/ F$ U! W* r) Tc* d) V7 |( B" V! o+ r0 z! a
ARTIFICIAL FEEL, A force developed in the flight, Q% f$ G' B m+ j7 z
control or brake sys; \4 \' ]. n9 M7 f) X0 a! B2 Q/ D0 f
m
& ^' K- \7 @7 `A
% |6 ?7 {+ c/ ua# C& @, k; f) g1 m
m5 d; F! `# j L
o6 m, D' l6 c v9 o( J( ~/ s8 U8 _( F1 Z
by using bleed air to draw ambient air through the. s' g/ [ G8 E+ H# k' y w) g! \
sensor when the airplane is not moving.4 Z& B( U; s1 ]
A
( S( W w6 I# W/ h& ~2 c' wor unit.! S' l5 C# b* ?; M0 ~7 g0 D+ d8 V
A/ t- l9 j4 E) P: k* ]; v% `; ^
lower thrust obtained by setting a higher than actual
6 f: F+ r# m" ]6 H% zOutside Air Temperature (OAT).7 m% ~: B* N; W0 X' w4 Q$ Z
弧线,& @2 N6 D5 Q. K2 v! x
飞机在围绕DME台等距飞行时的弧形航迹。( p) G+ w+ I" C6 g5 A7 b$ N8 {
区域导航,
+ T {; S& Q$ l# x' C |容许飞机飞行在有电台参考的导航信号或自备系统能
+ [4 @; L% s5 h, G力极限范围内,飞行任何预定航线的一种导航方法。
# B1 B) C9 N) N+ [, Q模拟感觉
2 ]1 C: [) L) N9 p# U! y/ F在飞行操纵系统或刹车
: o1 Y; D# v# _ o, c动
4 v0 ~; V. |# v3 n% U/ B吸气式总温探" P, V1 r9 y* j+ V
界
9 ]& s* L" j8 r* ~0 w# J探2 q1 v0 E1 g% E- C. _; {. P
装
/ S5 J7 J1 w" E! `5 E组合成
8 i# i/ x$ ]* e" ~9 D由' F+ g' d) X! ? Q
在选择起飞
0 r. p+ T# {- B( T度高的温度而得到的推力。用这种方法可以减少发动机的
. I' }- }- o" {9 L# \& U2 ^- V磨损和维护费用。
% G7 W/ p: H0 C+ S: D.
]# |" H+ _6 ~# j; w* ~英汉对照民用航空词典B OEING
X4 `9 p- j& t& KTECHNICAL DICTIONARY 14/ i2 C0 J. H- ~) l
ATE, SEE - AUTOMATIC TEST EQUIPMENT
# ~$ @$ |0 _ gATMOSPHERIC PRESSURE, Pressure of air due to the
2 g& ?+ z$ I$ {9 p4 m" Zarth's atmosphere, expressed in pounds per square
& B2 [" _) |2 v: P6 dch (psi) or inches of mercury (in Hg) or millibars (mB).2 h- a8 \. w. P( ~6 V6 f
TTITUDE, The relative orientation of the airplane with. j. X/ }+ u4 T( X1 U0 e
spect to pitch, roll, and yaw.# S- O; j b# u
UDIO CONTROUSELECTOR PANEL, The panel in4 z' w0 y8 ~2 s- C# g4 E; r& z) x
e airplane which controls and selects the routing of# B! K' d+ o. g, B
udio.1 x# [9 B# A9 ^4 P2 T8 L: p+ J
UTOLAND, Automatic landing using the Digital Flight
; G/ u6 T$ t" ?7 ~! f ~( }ontrol System.7 V& f6 m' E. B" a
n.: J0 C2 ^& ]* [, g
M, A system( G. f+ m$ w- T2 d" C2 ]' t1 X
omposed of all necessary subsystems needed to guide
; [: [8 i- M. ge flight of an airplane.! e; |: e3 i# f; V: Q# D* L! s
EQUIPMENT, System test; z, k, Q6 A1 D; a6 b# H, G/ ]/ h
quipment that operates under computer control./ V' ]5 M8 g- q, g
装置, |
|