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AIR DATA COMPUTER, A computer which produc) O# n: H8 P( `7 Y. ]" D
data information, such as altitude and airspeed, based
% k8 O6 i/ o: z1 r+ W6 }on pressure and temperature measurements.( p5 @ R! w% Z" C! P! @
es air. c- j+ [0 }! Z; K
IR TRAFFIC CONTROL, A system comprised of1 h! Q; N9 q1 N9 g" K3 Z
round and airborne components used to identify, track
0 o2 K/ T5 E2 J B; P# _1 i$ R: }OUND SENSOR, An electrical device operated
' X# e N* t* I& Qy the landing gear, which transmits on ground/in air
# v8 q; M4 D$ `5 {formation for system operation in flight or on the
7 i) Q6 `* i! i5 S4 vround.0 a: X( z5 I8 s2 y2 y' K/ @
IRBORNE VIBRATION MONITOR, The AVM takes% c4 n0 t! s% ^1 p
e signal from the engine mounted accelerometer and
& O7 B; F$ j7 M7 f# s3 ^# K; d# Z+ Jalculates the vibration on that engine.0 D y5 L4 e$ D7 Y1 j9 k
corridor equipped with radio navigation
% d* t; |/ t2 K% Xaids.
6 G8 _ l# k8 j& E0 {& JAIRCRAFT (or ARINC) COMMUNICATIONS
7 i! ?0 L& U- I% |. N9 J. aADDRESSING AND REPORTING SYSTEM, An# `4 x1 _ D- i% y# E3 a3 C
addressable digital data link system which permits the) P' S) I% S) k! N2 w- n8 o
exchange of data and messages between an aircraft( z3 }' }2 v9 N8 q% b- r
and a ground-based operations center over a radio
* I# r. T( m4 ?5 \1 I( enetwork.! }/ f& T# G$ J- W8 k/ ^
AIRCRAFT CONDITION MONITORING SYSTEM, A
5 Q* {' `1 _; Psystem of sensors and recorders to monitor various
! l0 H d/ _4 W1 d. M9 jairplane systems' performance and status.
" ~% p7 R7 v$ p+ m3 J. W! e机,: x: `- ~7 J1 \0 s
中交通管制, Q6 w+ K) t/ x- F" P
一个由地面设备和机载设备组成的系统。用来对飞机进
' F% }0 [( f3 V" g0 G Y地传感器,- b: q2 o; w$ r2 j) N& W( i
一个由起落架操作的电气装置。用于给空中或地面的飞3 V3 h% \% U5 f/ M
系统运作传输地面/空中信息。(有些系统只能在地面! r4 D8 F: A" L9 j$ n3 F% m
用)% K$ K! h. s0 C( o, C# j$ n4 N
载振动监测器(AVM),
; q2 ^! w. h/ b& W) u2 qAVM从装在发动机上的加速器取得信号后计算出该发! X6 W, m2 D$ a. f$ ^6 F7 `
机上的振动。
1 \# j' X: m2 g式建立的控制区域,内有无线电导航设备。/ H) \9 G7 T& v D$ e/ G9 g
飞机通讯寻址和报告系统,
/ ]" E% g2 }* P* m! d+ L! g5 G有种可寻址的数据通讯系统。利用该系统可使飞机与地* U1 e) G; O1 k5 Q
面操作中心通过无线电网络进行数据和信息的交换。3 |. R/ l8 f: `4 ~
飞机状态监控系统,5 _% Q3 x! {& N# Y* p
一个利用传感器和记录仪对各种飞机系统的性能以及 |! A; U: g; E" G: b! N
状态进行监控的系统。+ e0 G4 h4 A- o) `" z
A5 l. Q7 S4 ]+ h7 Q4 B
g
& }0 u4 c1 `2 W/ Wand locate aircraft. B$ W/ ]9 q0 M2 `& f& N" t; j
AIR/GR
. k, n* }% h4 R+ [0 rb
2 C5 z/ v2 J& j% jin
) b7 q! D# n3 j, U5 Dg
4 S ?6 I+ o h+ LA
: T/ K% r. i$ M, z ? m6 o- dth
. H, H B! H% p& n8 e; |9 m9 K4 Hc! ^* F5 T& d) [9 {5 _ {4 y
AIR WAY, A control area or portion thereof established
# W" P4 @# K* q4 G: [! ~3 X6 fin the form of a
3 M6 ^0 V0 e1 _3 U6 K2 k$ e大气数据计算
+ T- \" ?3 Y6 `6 F/ a7 w根据量取压力和温度而产生大气数据资料(高度、空速$ D J: D8 x2 K' |) q
等)的计算机。
2 U+ {6 Q0 _$ [" ~) C k% g! n空
( Z$ @( ?5 w- M: W$ Q* ` }0 B行识别,跟踪和定位。
& N/ D4 ^1 u! m' P空
# j6 j6 ^: d% {$ ^0 m, L; R机/ g; U' [& W! r4 a4 f& s }
使
3 Y/ a8 x" h0 \; L$ e! @' w/ Z机
( k$ L5 x3 D. y1 y& ~' R; ~动/ E& | t" A- w6 Q
航线,
; ?9 y8 V- J8 A5 Q) |. ]$ }: `, f/ G, [以走廊形" i1 O1 p: p$ b; a+ j5 V6 A
英汉对照民用航空词典B OEING# g8 g6 [% H' U$ q3 S! ]
TECHNICAL DICTIONARY 6
* D c7 k3 V1 [AIRFOIL, A surface designed to obtain a useful reaction,/ W5 S& G4 D6 x! A; U; t
such as lift, from the air through which it moves. Wings,( x7 D5 k5 e7 T+ a
stabilizers and control surfaces are airfoils.
8 @/ H j. \4 ]AIRSPEED (IDS, TDS), The speed of the airplane5 o" b4 a( `& e# ?8 ]
rough the air.& A5 Z; `! R+ }+ U: |' w
D INDEX, An adjustable pointer on the0 P F; |* J% `7 ^- `5 q; p
irspeed indicator.
9 E8 P, R4 x5 X7 ~and legal ability4 M9 @" d/ @8 m `
fly./ P2 |: U4 m! U
m, for example, the procedure for finding the
+ f. |+ H' P3 X7 H8 n- jquare root of a number.
. J) v3 z9 ~. e. q0 _, [- X( Ly* k" c' k* y& b/ t* @$ J! l
re, wind,
3 B W# g3 f1 p" w/ Qand aircraft flap setting.# k0 Z0 k" O7 e! b1 ?5 U
是翼面。6 n" k; X; u7 N6 G: p6 y' r
速,
; D2 |, U7 O6 F+ {- A7 C/ C飞机在空气中运动的速度。4 D9 e8 s* B, h! P3 A: g& i+ K( V3 x
,9 H/ P6 \: x+ b- Y7 @, J0 ~
在空速表上可以调整的指针。
- y6 s% z9 {- A o" g( Y( m机械飞行能力、和合法性的飞机状态。- t0 h. q4 ~6 c: B( O1 T
一步一步的解题方法。例如,计算一个数的平方根的步/ L8 M4 z/ Z. \& c5 |+ K( t
。 b4 `- w4 ^4 R
能- w4 Y5 a- R5 z8 `
资料的法定文件。5 l: z% k) C! a8 f8 e
翼位置成函数关系。
& K. x' W l) s1 x2 xth. _+ c; W' s Z! h( q
AIRSPEE
n6 n- f" @+ `6 w. P+ Ea2 \- B6 t3 e k1 V
AIRWORTHINESS, The condition of the aircraft with2 d( N* a" F: W5 G
respect to its aerodynamic, mechanical,
# F9 S4 z- w* Z) zto
: D( F" G% ]$ kALGORITHM, A step-by-step procedure for solving a8 Y u2 ] V. ?! @$ v. M
proble u' g1 Q( V4 W8 l! s, h% N9 Y' `
s6 T0 r) L' u$ P% a3 b6 Q; Q9 l
AIRPLANE FLIGHT MANUAL (AFM), The legal
, ?; ~8 ]* j6 D! m% wdocument containing performance and operating limits,% L; m" e, B* e ?' j% n" y! f/ E# B1 X: [
operating procedures, and takeoff and landing7 a# J; i* s. ?! w% ?8 F) N# {" I
performance.5 r# S9 k8 ]$ U% J
AIRPORT ANALYSIS, A comprehensive set of takeoff! ~1 w6 a* {; U( P
weight limitations for a given airport runway, generall
7 g+ t* [% S) t4 K+ |: ^presented as a function of airport temperatu
& s: b) p R6 ?! ] l c) ?翼面,
1 d: B ]$ j9 W4 V# r- P( T用以从气流中获得反作用力(如升力)的表面。机翼,
0 `9 {. u* _2 F4 d3 [9 k+ \1 l安定面和操纵面都
. j8 O2 x& a6 p$ x" ?7 S空
9 W% u) X- [8 q0 B7 H4 Z空速指标
+ {4 t( H' O' z) }适航性,
7 K2 b5 `3 _7 `0 W有关气动能力、
) `5 C) C% v' C- A0 {演算法,
( M! Z: u% w* x% L+ L4 B骤1 g" T. K* f5 [- v% b$ q
飞机飞行手册(AFM),
& r0 R6 K3 e4 t2 x6 ~6 j4 t+ y% z包合性能极限,操作极限,操作程序,起飞和着陆性
, F9 S4 t* I& L) @; Z1 Y等
9 X$ B; F8 B9 B8 {3 R7 t机场分析,1 C% G& G! m/ s9 W9 _
一套针对给定的机场跑道的详细重量限制资料。通常与
" l' X6 V0 `7 x6 l, f B机场温度、风、和飞机襟6 P" W1 d' Y( W
英汉对照民用航空词典B OEING
1 r9 ?; d3 x* y M* h- \TECHNICAL DICTIONARY 75 t8 i' v) Y6 C4 d T0 `# A9 S
AIRSPEED BUGS, Adjustable pointers on the airspeed3 W5 L$ P& R9 B4 f' l
indicator.
4 h5 v7 m+ e0 l4 E% OALLOY, A mixture of a basic metal and small amounts
! u. Y, F' y( V# @' Y( N' j, uf other metals to change the properties of the basic
, r4 ^ m ?- n" |, a% F( Aetal.
5 p! K; C. L/ {2 G* T, QMinimum airplane speed.9 \, d; M' V* d3 m7 U/ j! P
e of {) X# p1 u+ w$ h% ?
itting airplane angle relative to) D$ N% ^3 C! ^' @+ d
irstream for the stall warning system.
: P. J# o# l3 n. ^another.
$ N6 O2 m0 U6 x3 m* _+ q XLTERNATE , An additional airport selected during
8 e/ Q8 E4 V# T. @" m% z,) e; y& g, h; F: |8 J+ S6 N
合金,
5 t: M \1 l3 @6 j在金属中加人少量其他金属,而改变其性质的一种金属
! z: A- a4 a9 m- ?% F- d5 x0 D合物。
5 i8 Q K) O# K- L8 t飞机的最小速度。5 k a' a. W. N
速警告系统传输飞机对% S1 T# ]" i7 S7 ?$ A( M+ G9 G) ?
流的相对角度。7 }, a# d- t* o3 B; \
由一个状况改换到另一个。
! o: @ Q0 _# b g4 g- D" l9 f% T% a* j降场,& v% Q6 ?7 P8 K' J- B
划时,除了目标机场之外,所选的另一个机
% F# ~) s) M# w7 w; po
% f- Z0 q/ q1 H$ m# N: d \m
, h& w5 f0 K2 b! G% ~ALPHA SPEED,: C! n6 z t1 X6 O4 O# G
ALPHA VANE, A small moveable airfoil on the sid2 i8 x! }. P! |
the fuselage transm
- w5 y! L' Y4 R G- h5 Ra5 B; L$ W6 I$ z- B! {/ Q/ G4 Z# ~
ALTERNATE, To change from one condition to
( A. e" J k3 fA
, S. ]- l% ~- aflight planning, usually near the destination airport, to be6 L8 L) V v3 X, K; M, w% q
used when it is desirable to divert from the original* G5 B8 Y( a0 Y4 R* c! Q6 D+ E8 V! I
destination airport.
! h, K6 w2 r+ @$ b) _% z4 |空速游标
) d, w% t" P' O: G9 ^* _; y# q! d9 V空速表上的可调指标。
9 o5 n7 P- h; e& Q混( x" }4 J1 l. J
迎角速度,& v# ^- {0 A1 N1 b" s: Z. @
迎角叶片,
7 \! J' e9 `0 h, @- ~& H% ]位于机身侧的可动小翼面。为失; u. G' w; S5 A3 l8 t0 s
气
. V9 c0 g- z- n { \交替,
" @; k1 J4 F. G备, A+ V$ V5 D) [3 E, m: P" X
制订飞行计: r, n" V9 ?( X$ a, b5 `
场。通常在目标机场附近,以备不去目标机场时,改降之4 S+ k+ R- M+ ?- ^
用。
* a1 u1 ]. \+ f英汉对照民用航空词典B OEING
' H3 f4 N1 j! @: qTECHNICAL DICTIONARY 8! l$ w* B: i$ }0 H
ALTERNATE AERODROME, An aerodrome to which
2 j8 N( b. n& }5 l7 han aircraft may proceed when it becomes either6 Y& ~) ]& V( H# G
possible or inadvisable to proceed to or land at the
5 N% T6 C0 b+ B d4 derodrome of intended landing.
' a3 Y5 q. B, R h5 T9 C) UTER SETTING, The adjustment of the altimeter
! {8 y1 c$ i5 q' j! K+ ~6 Iaccount for local variations in atmospheric pressure.
) G( u( D( N. c& N% \, i& jLTITUDE ACQUIRE, A digital flight control system6 m6 {$ s8 E$ y7 J
ode to transition from climb (or descend) to level flight.: F6 M. g2 i( ]' `$ G% U
LTITUDE ALERT, A flight deck alert occuring when the7 A5 `( \9 J. `
irplane approaches or departs a selected altitude.* m( h/ {9 j! L* D. L: t( w. _
LTITUDE CAPABILITY, The maximum altitude at
5 n- C8 ]2 i+ l# Y! U7 Dhich the airplane can be flown at for a given thrust,1 J9 J; s1 h) w' d6 ^& A4 L" D" K( V
peed and atmosphere condition.
6 }2 M7 p" W, ?LTITUDE HOLD (ALT HOLD), A mode of the autopilot
$ f2 @ ~$ [# G) U. vr flight director to maintain a selected altitude.: Q" T: W4 ~( J, i" r4 R% J3 L* s
irplane's altitude during VNAV operation.* {* R* Z+ _9 O( K
机场着陆时,可作着陆使用的2 {6 d/ P8 q% {* _) S2 C
场。
: m" {" P2 h/ t7 K3 Z* H. j,
8 G; G9 z$ W) [8 @: Z- A6 {根据当地大气压力变化而对高度表所做的调整。
0 m; | V5 s1 {: H3 h# K8 @* K一种数字式飞行操纵系统,从爬升(或下降)改平的模7 A6 K+ z( x6 s
。
* y. T# Q8 ?3 D0 y8 i7 |度警告,
! _+ v2 T- R" k当飞机接近或偏离选定高度时,所出现的驾驶舱警告。
( @$ n2 R ^6 G高度能力,
: M8 R& d: M/ {/ g6 c& O9 P在给定的推力,速度和大气状况下,飞机能飞达的最大" C# @: H# b( F8 G C2 P$ a: @ w, s
高度。
6 Z. e/ e1 |2 n8 l N高度保持(ALT HOLD),7 M0 E; a3 s* H
自动驾驶仪或飞行指引仪保持在选定高度的一种方式。+ T) D0 D2 ~* _3 ?, K) v' |
,
$ {; a# @5 M/ Y* a员对飞行高度的控制。% X. L7 I0 ~* C/ z: @, [ ^+ k
im1 o+ k" y+ E$ k5 E; ]5 ^
a9 _/ \+ S. S+ W
ALTIME
, Q: z# A7 W c: H0 `/ a: A4 nto
; M7 J" J/ J# H, ~4 w$ ?. mA( z& x: L7 G7 L1 i9 r) x& M
m
* g: B6 \- m& t2 QA
6 i+ c) U, N+ N' I+ J5 ?a
: s2 C. O2 \9 x1 \' W3 V, _A1 a3 |; A3 ]1 |; p% J d
w
: o% g, j1 ?) F P. c) v; ks
3 h2 }6 C. G- X; {! ~1 ]A
/ G+ f* w, Q. ~" |o
# {8 g( u) s) c/ b4 o$ @2 @3 AALTITUDE INTERVENTION, Pilot control of the- f- O( x/ E: ^' f8 |* D/ n6 F
a
i. t5 h$ o) oAMBIENT, The surrounding atmosphere.# O: X* X% @( r; t: b2 k
备用机场,2 O1 G/ H' B" T0 v- g( w9 {
当不可能或不适宜在预选
. w/ g% H, V7 S8 i9 g& p: h机
$ q/ s$ E4 Y' k高度表设定; H3 F) I4 ~, X; r5 G' u( b b
高度截获,4 l( T2 Y% N2 Y" ]
式( i- s6 }; D" s. |' ?
高7 s& e; ]; I) |
高度干预
$ h* c/ d3 J! g5 D4 T在垂直导航工作过程中,飞行7 U- Q4 M( k* b6 P; B
周围环境(地面气层),* P' g0 q, o) o8 s% e. F$ s0 X
物体周围的环境(特别指大气)。
2 i+ V$ {$ G2 \+ l英汉对照民用航空词典B OEING
a; V/ S1 N/ ]; H! C" KTECHNICAL DICTIONARY 9% k, m' I( f0 U* f# D& R$ V! B
AMBIENT PRESSURE, Pressure of air surrounding an
# w+ J/ r! c1 }& hobject, measured in pounds per square inch (psi) .; m6 r5 k5 x" U0 f
MBIENT TEMPERATURE, Temperature of air0 G8 A( U6 K6 e! _/ |) e: |
mpere.
' u7 J- J# f% E; Y6 h9 burrent waveform.; D& j1 y5 c8 l5 T, f& a
g an
4 F& H+ J8 W7 _0 a/ F* T7 e2 snalog signal to a digital signal.! c* K, h/ x) p: Y( v( [: N1 L
ore inputs: D; N! `$ I2 S; p* p
f binary digital information and one output. The output) p' Q$ J/ p3 c" m
1 only when all of the inputs are 1. The output is 0
% u1 `3 @& ~5 X& Vhen any one or more inputs are 0.
& E8 m! m1 G5 p( Q面气压),7 a2 m7 U+ f! t% D. r: g' ?
境温度,. |. U, J7 s% Q5 M! M" A
气温度,用摄氏度(°C)或华氏(°F)来$ Q5 k; ]" C0 ^- d' g. F! g
。
4 b4 e$ x& {( H& M0 l电压或电流波形的幅度。+ W0 @7 M' ?1 y
性变化的信号来工作,或产生连续性变化的信号1 x: m3 v# K8 a
统。$ N" m9 m; E2 b2 ^
将模拟式信号,转换成数值式。& C: B+ U4 Q( _; F- g5 H
一种有两个或两个以上的二进位数字信息输人,一个输8 X* l7 d$ T7 ^5 S+ @* h" \
的装置或电路。当所有输人为1,输出为1。当任何一个
: f2 ]& B" V6 z' B6 `8 E$ n一个以上的输人为0时,输出为0。* J* F2 i0 l# h. m
A
: B+ m0 l2 o" p0 I7 G' j) msurrounding an object, measured in degrees Celsius1 M0 c, k5 F2 ~! x$ v2 T. H
(°C)or degrees Fahrenheit (°F).5 P! n& s; j! Z
AMPERE, A unit of electrical current. One volt across+ s' b" [. m u9 C* ~
one ohm of resistance causes current flow of one
! K( @; ]4 u3 @% u; W' ?. [a
9 O. S/ B2 Z/ `7 f: FAMPLITUDE, The size or magnitude of a voltage or' | D/ }$ y+ ^
c
2 i8 w. B. ]( @6 TANALOG, Quantities or representations that are
2 @- z3 y! H- R7 D; m, c1 ]variable over a continuous range.
1 M+ a% w* X1 u7 q0 ?/ lANALOG-TO-DIGITAL, The process of convertin' E( M: }1 [7 \
a" V, n% n/ M) f* Z
AND GATE, A device or circuit with two or m* U. w ~7 U, Y& d9 l
o1 j5 D& r; o6 Y' K- Z( I
is. f, a; j! B: j5 v3 o J' W( S
w1 u1 ]- ~. F6 d% s' c. L& d
环境压力(地
+ }! S$ F" v5 e+ ?1 h物体周围的空气压力,用每平方英寸多少磅(psi)来
* M3 v$ n7 T5 o9 U: P9 ^度量。
/ O; p- g4 k, @/ ^1 X0 _. U环: Q. K2 O7 j% r
物体周围的空
5 I5 }' W! q7 ?/ {度量。! f i$ ?% w6 d* I# V6 _7 k
安培,8 j; ]7 f3 E! @( D2 s- O7 ~7 H: o+ V
电流的单位。
7 @7 o$ A# @7 d/ B/ ]4 _; e6 J+ t) s5 s1伏电压在1欧姆的电阻上所产生的电流为
% {: {% F9 u V1 T1安培& u6 s8 v' L: ?$ M5 c. {
振幅,
A. u6 b+ u4 g1 J" m8 @4 j模拟式,+ w1 }5 s8 S. H8 C; F" W
用连续! `# k4 {9 g7 G- h$ P" G7 g9 }' s
系
7 S8 v( P$ a8 v* f从模拟式到数字式,% }* `) h' ?, q5 G' r4 g
与门,$ c: Z8 J, r6 |+ Z1 _. P
出
) Y* {( P2 t) f9 \! S. Y7 x. h( i或
) I+ |: E8 W, f英汉对照民用航空词典B OEING9 N: X4 ?3 P, I" |( d
TECHNICAL DICTIONARY 10' B) W7 Z) l& z- I6 q2 Y
ANEROID, A sealed flexible device containing air at low
7 h7 O9 N4 V) n/ z- D/ ]" P1 Cpressure, which expands or contracts during change of
1 d7 r) `* @4 U/ f: l% `! E- Y) h( Vressure outside the device.4 \4 k2 V# {5 Q# O" V7 d+ _
ically j; H j, F {8 v; n2 g
r changing the direction
! h/ P7 h0 w5 O( a$ D6 If drive.
, ~$ p2 M' O4 G8 k3 U0 e7 Oof the wing chord in; k& ]8 X/ A5 r5 s6 i! _
lation to the free stream airflow as it moves forward8 S9 [: t- R ]7 P% F( O2 |
rough the air.
+ P/ M! u9 F3 }' T$ U; G8 \al axis of the; ?3 `2 z- B% p( P$ |+ e
aircraft.
6 @) }0 |8 n& `. d& N8 u0 ^4 |% T- L胀或收缩。
3 B. P. x4 n5 {: i箱。是改变驱动方向的机械装置。5 g7 A) J0 p e" C& w
机翼翼弦在空气中向前运动时与自由气流之间的夹角。
( m' s8 G8 a H& I* X9 s。
7 H+ T& G4 N' qp
) m$ H% J" j; O- A4 \3 L. f! V5 vANGLE GEARBOX, A part of an engine, mechan! Z1 }! e0 L3 \0 d
driven by the compressor, which drives the accessory
3 A+ p4 h! n7 _/ L4 q1 Jgearbox. A mechanical device fo
% h& ?) U; j/ L V* R" d) ]& Oo
* O8 [% H1 v) H, hANGLE OF ATTACK, The angle
; Q. g1 w) [7 Cre
) B% z A0 G* dth
: P) ^1 K$ }/ PANGLE OF INCIDENCE, The acute angle which the7 q% F$ T% m: B! s) v* C: A
wing chord makes with the longitudin
9 G; L3 s8 \% Z5 D e' g0 D/ |膜盒,
, x! P) v {2 C- M! l) ~' u; h内含低压空气的密封弹性装置。当它周围的压力变化6 w7 K$ w4 S7 G4 G4 ?2 ^* R
时,会膨
9 w, ^' ?# J& d6 a1 U" |伞齿轮箱,0 ]3 F6 o9 M2 k7 \
发动机的一部分。被压气机以机械方式驱动,然后驱动; b+ K. r1 Z! ]
附件齿轮8 i- { G. O2 c( U* U# [
迎角,
9 W' B+ X7 u( n% U9 B3 b$ X安装角,- K) l; j: b e$ c) U1 n# {
飞机的纵轴与机翼弦线所形成的锐角( F* R( Z% Z8 F& w
英汉对照民用航空词典B OEING
. O+ P" v1 g7 J0 yTECHNICAL DICTIONARY 11' `' n3 i+ i3 v5 `3 \& g0 d: d8 d
ANNUNCIATIONS, Audio or visual indications used to/ Y( [; |( [: i
call attention to an event that has taken place.8 E: j* \+ ~6 x% s5 _ W! k6 Y! [
ANNUNCIATOR, A visual device consisting of a number, q0 K2 ? Z b" Z5 _# a# E
ly.
- e7 @; ?6 G2 g# |ANODE, The element toward which the principal stream0 i1 n0 A7 B9 E3 n; X- L
of electrons flows.
% `- |3 a" K% F* L/ n4 S; P4 \ANOMALY, Not normal.( F) ~6 F! r4 S8 r- l
ANTENNA, A device which, used in conjunction with a
" |* h6 \' d& K; p7 m' W* Ytransmitter or receiver, is used for radiating or receiving
0 x$ |' a# |# m) lradio waves." c3 N; g& x% [' c* J; j, [6 W
NTI-ICING, A method of preventing ice formation on
, V s# t1 F6 r7 e! }6 d9 ~e wing leading edges and engine nacelles.
+ B# C2 O% r+ H+ ]& |8 P, YNTI-SKID, A system for providing maximum braking5 u) ` Q6 m. x. n
ithout skidding for any runway condition. Anti-skid) v, _& }% r9 e% k2 z; C
omponents are part of the brake system.7 [9 h$ i. p( R) @! n, p
告,6 d1 t9 O" c3 u4 l
当发生事件时,以声音或目视指示形成的提示信号。! t2 v! {8 B& u# ^9 z
与之有关的电路的现有情况或已存在的3 V$ f* v! T$ \2 x# F8 a
况9 _& ?8 a0 U' Q0 B, ^
正极," P1 C- E6 k+ d0 _) J
主电子流向的极位。3 w% A5 {* u! e6 k0 S6 e; m9 B! [
异常," f5 _+ a: A2 q% [: x$ h
不正常。5 t# K) ^- D$ F+ F
天线,: I" Q; g' h1 M. A9 `
一种与发射机或接收机共同工作来发射或接收无线电* R; `; ~& Y8 l4 t" B+ U' o6 i/ e
波的装置。 j* R7 I6 }% D
冰,
3 p9 k/ K3 z. \! b3 A2 W& ]- K防滑系统,2 B' f* O, |9 i. P5 g
一种在任何跑道状况下,都能提供最大的刹车能力而不! N m8 e% n! ]& I$ k
使轮胎打滑的系统。防滑部件是刹车系统的一部分。
3 m$ H. C% i$ L0 t- ~0 u4 H0 Y* Gof lights. Each light indicates the condition which exists
0 T% |: x& b. a$ G. r' t, ror has existed in an associated circuit and is labeled
7 h8 |* u- b, b" Iaccording
: @- i8 g, d9 W; b& GA, p) a; |5 _& o$ q' y* b0 w) t
th
- }4 }& y, C- B( e/ ]. b# ]2 BA' `5 l4 _) G* ?, d5 j* \
w
$ ~8 n4 n1 k3 `6 S, ~c1 M7 d1 a6 A" [9 e! j
通
4 b. j; k3 ?+ C3 B' ~( B信号牌,
E" V4 J( S3 z+ H4 N/ `由一系列指示灯组成的目视装置。每个指示灯都有相应' K5 I4 k9 W2 F- d6 W- m
的标记,用来显示
& i7 e, O8 v) d4 q" e' A5 [情
7 j# |% F7 o" O6 u! L防4 k0 Q: e" G' H5 O# A' K
防止机翼前沿和发动机短舱结冰的一种方法。
9 m" L- N' P( q1 C- \英汉对照民用航空词典B OEING1 i$ k) a' y7 c- F2 ?3 z& P5 o
TECHNICAL DICTIONARY 123 N) R* X( O; ?3 h/ E
APPENDIX, A supplement to the Airplane Flight Manual( h7 g1 \6 G9 D% `
tained in the basic manual. A
L/ }- j9 j* C* [2 J m. |7 @5 `ollection of supplementary material at the end of a
3 A) [; ?5 @8 P' R. N/ ~ook.+ x7 I! u) J: t( h; Z
of the& i6 d) ]2 z' R; ?& C# U
rsion link on the landing gear.7 ~1 Y& p9 E0 i) [ F' z0 q: @
APPROACH MODE, An autopilot/flight director mode% m9 w8 ]# ]* K3 D
which is a combination of localizer for roll control and
4 Q3 {, D" d2 ~% @3 q% n, k/ N& tglide slope for pitch control. This mode is used when full% f5 K! }* O9 m
instrument landing system is available.+ P/ X! h& s2 k- P: F/ M7 ^! `. \0 `
APU, SEE - AUXILIARY POWER UNIT
) y: u4 N, u/ R# b/ T4 u3 gARINC, SEE - AERONAUTICAL RADIO0 J" e# a8 _$ m9 G7 d
INCORPORATED# z' r. V) T ? G# Y
ARM, To make ready for operation.2 k% Z. S! Z# T+ R4 ]
附录,
2 _8 ]0 W2 O0 l* h飞机飞行手册的附件,包含基本手册中未提到的飞机形
3 a, C$ P6 T/ M4 j2 u态的其他性能。是附在手册末的补充材料。 q7 P7 Q/ d/ w6 K( Z* ~4 m$ e0 _
顶销,* v! Q O# p, r3 X, W+ D T
用于连接起落架扭力臂两部份的销子。) N4 @# R1 v- M2 c5 p& _4 [
进近方式,
, U* H- e# y ]9 I7 m一种综合了控制横侧的航道信号和控制俯仰下滑信号
5 P4 C- N# _7 C& I1 f的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系
9 D r i J& d" V: U: z统正常时才使用。
2 {3 R" ?) i5 p$ ?辅助动力装置,
+ ~% j3 Z4 X8 u U" k7 q* o9 L见Auxiliary Power Unit
# p2 s4 l+ }& {; ?( kcontaining additional performance for aircraft) k/ s/ C' v- I8 S2 ~2 C
configurations not con
8 i% C3 [* O* Ac
- K% U* }2 U$ M2 D3 Yb( }8 r8 ?: s/ D3 B# n/ t9 a! k
APEX PIN, A pin for joining the two sections S- T7 V1 z0 y
to
& ~, R0 B7 w% x9 i. @.
7 _6 g c, ^8 A% z航空无线电公司,
; k# x+ ?2 t5 J% q2 K见Aeronautical Radio Incorporated./ a5 z( k$ a" D0 h
预位," h4 ?7 j% s3 o
部件可以开始工作的状态。
4 a+ H x: u% n+ }* N& T英汉对照民用航空词典B OEING* w: @' w1 N9 ^9 T0 {% s
TECHNICAL DICTIONARY 13
( z8 y( g* u8 \5 {2 A f+ z2 ]8 VARC, The curved track over the ground of an aircraft( D# e; ~8 s" F, x+ k' V3 w
flying at a constant distance from a measuring
- @3 W6 y# q) c5 S" F: iequipment (DME).5 X9 ]+ A2 }9 ?' L
in the limits of self-contained system
2 x, e" e Z- V! G% b! I( lapability.
8 E1 P* f! j" j+ stem for opposing or restricting
0 n/ P( @; B$ S3 ]. R% Povement.
- e! }& S4 p: ^9 c: DSPIRATED TAT PROBE, A sensor that measures total
) M# n) i/ }5 Cir temperature when the airplane is in the air and that% U1 [, h: s4 y) G; _+ `& D4 R
easures outside air temperature when the airplane is
7 F- U" J# v& r5 \n the ground. The outside air temperature is measured( p) A% H! s) X- k% E i/ r$ T
SSEMBLY, The fitting together of a complete structure
+ P* D. O; y; P- q- sSSUMED TEMPERATURE REDUCED THRUST, The5 X. K4 O3 l; N! T. N' \- {
ATC, SEE - AIR TRAFFIC CONTROL# W) N6 u4 Y1 E; a* h# j% z
,
* s$ m/ h9 q! K5 W- J \系统中所产生的一种用以抗拒
8 x: h4 j6 U1 C# E* B; ]作或限制动作的力。9 t8 {! }& a) c) W- G6 W* w
头,
* \! b- n+ q% R* y' k; b用来测量飞机在空中时的总大气温度和在地面时的外
" v2 r3 |3 Q: ?0 T$ e温度。地面外界温度的测量是利用引气将外界空气吸入
- H B( o; b$ F+ ^头,以达到测量的目的。% N6 g& s4 }* b3 J* _% d# X
配,
$ O% }) P( z( }' Q( p, Z一个完整的结构或组件的过程。
, R/ L. A/ u [; P+ w5 J( b假设温度而得的减推力,
" |- S* e' X- I8 o: A$ t- N推力设定值时,假定一个比实际外界空气温
( Y5 _" D+ k+ G1 M* k9 d" j空中交通管制,
) J4 M0 q5 v5 o见Air Traffic Control4 M b1 v9 E. L- U2 k% G, L- {
AREA NAVIGATION/RNAV, A method of navigation
* d1 D0 _* A3 ]that permits aircraft operations on any desired course
2 S, x' G6 h6 Q3 c& _8 twithin the coverage of station-referenced navigation
0 q) f% I, P; ? c# t" Ysignals or with
# o K% v `4 Bc! W& P4 ~/ m u+ F3 B' t, X$ a
ARTIFICIAL FEEL, A force developed in the flight3 w: |5 u: ^1 o
control or brake sys% q" I$ G* T; u" d1 W: l
m) k6 `( U3 |1 K9 Y) O# P4 @# k) u
A
6 z- F% ~! t! ]$ b' f. Ya
3 U. K$ E& e* ?& e6 b; i g, ^- Gm& C# X5 Q; k. e- E
o
7 C# Y! r6 w4 [ Wby using bleed air to draw ambient air through the" h6 v0 h5 U' r c/ a2 [' [# M' O
sensor when the airplane is not moving.
7 y5 {7 q) {; F7 p3 tA9 W% {- ^+ G) E2 |% W2 M
or unit.: g N. y: l& G4 X( @: S) q
A
! V; @9 R+ ]1 k: T3 V5 Nlower thrust obtained by setting a higher than actual
" m; `; [7 L" i i' lOutside Air Temperature (OAT). Y% J+ v$ n, K- p8 C& U$ C% v
弧线,, m+ n* }+ K, l& m3 d3 @- G
飞机在围绕DME台等距飞行时的弧形航迹。# {& [) X) i( P( L$ I
区域导航,
1 a8 _8 z: T/ \; Y" h容许飞机飞行在有电台参考的导航信号或自备系统能
" Q7 p5 d6 c4 p/ {6 N( R/ x力极限范围内,飞行任何预定航线的一种导航方法。" G$ `# D, ?6 m! A' }, E2 {- Q
模拟感觉- f, R. u& ^& Q7 i; n9 m
在飞行操纵系统或刹车9 w+ }, C, q3 t1 z q! F0 G
动
. G$ t# G2 w$ g/ p1 C) h# P' Y吸气式总温探
! q+ Z( Z2 ?' z! t界
9 M1 t" \' V+ J6 H3 F9 i探
2 {6 |/ ~, D# V* _: |, }% `装; N6 `0 _' A8 Z. F1 K
组合成( J4 n0 I" p% K
由
9 _7 s, }" H0 @5 `在选择起飞6 k. o' S$ |0 |
度高的温度而得到的推力。用这种方法可以减少发动机的
) F4 A( |2 g# M7 y磨损和维护费用。
3 ~! {8 `9 ?+ {+ Z! Z.& u9 B1 W0 r* y( O7 f: S) ~; \5 r! Z
英汉对照民用航空词典B OEING
J, c! ]! h9 lTECHNICAL DICTIONARY 14
# G7 r$ L n) j( s6 h; v7 bATE, SEE - AUTOMATIC TEST EQUIPMENT
% A/ K/ l" a; r* k X4 vATMOSPHERIC PRESSURE, Pressure of air due to the; q, u3 _' |8 R; i
arth's atmosphere, expressed in pounds per square
$ |% r+ H8 Y: \ch (psi) or inches of mercury (in Hg) or millibars (mB).
, [$ @ Q( v3 I; c- K$ hTTITUDE, The relative orientation of the airplane with1 g* x u7 K% f% a* F# v1 d7 z
spect to pitch, roll, and yaw.0 E1 R% J8 h4 f$ O: `
UDIO CONTROUSELECTOR PANEL, The panel in
T! a# C9 s! J5 k3 O! i% M0 we airplane which controls and selects the routing of" }6 h- d9 U; e( `
udio.
( O; Y u) M, @7 KUTOLAND, Automatic landing using the Digital Flight: o) B, P* Y1 _4 b$ c: q9 H
ontrol System.
6 J0 P( X& O9 K, e" \6 {: t; Cn.( J- n8 E' F% N3 x. C
M, A system7 {, \' F- y3 d4 q0 r$ i
omposed of all necessary subsystems needed to guide* x1 K4 {) P p8 Y; c& G, n
e flight of an airplane.
! W$ `* d' |/ Y: O' _- ]EQUIPMENT, System test) y' Q8 l! [; t+ s" W
quipment that operates under computer control.
* J: N1 p4 i' f装置, |
|