- 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% v b+ w" p( Z2 z
data information, such as altitude and airspeed, based3 W3 e @+ r' U3 e, b, L
on pressure and temperature measurements.6 a; t+ D/ e& `$ c' i {0 P8 b
es air& t e/ N# A0 ?
IR TRAFFIC CONTROL, A system comprised of
]6 Z# ?- n& @% j/ wround and airborne components used to identify, track4 F8 Y" r1 [1 r+ Z: w1 I( [$ _9 T6 }5 ~
OUND SENSOR, An electrical device operated
. B0 L3 X" g' k" ^, Py the landing gear, which transmits on ground/in air- D" @' Q7 @2 X
formation for system operation in flight or on the
: ^7 ^( |4 w! v; eround.
7 p3 U$ T9 x, J6 D, M6 `: vIRBORNE VIBRATION MONITOR, The AVM takes
- f( f9 ?- u5 }& g9 M' Y2 m/ x8 `, `e signal from the engine mounted accelerometer and
9 _2 A0 Y* p I* E" Zalculates the vibration on that engine.3 g4 Y0 Z" g3 D
corridor equipped with radio navigation
3 v; V2 Q4 ^: n) g4 `* uaids.& Y2 n: g! j$ i- s$ ?
AIRCRAFT (or ARINC) COMMUNICATIONS7 P3 Q' m2 k, W0 T
ADDRESSING AND REPORTING SYSTEM, An
% I3 Z% y6 L+ K8 v+ r2 Gaddressable digital data link system which permits the
' O3 s( l( {% v! t0 V* R( [. G( x5 zexchange of data and messages between an aircraft
9 h9 }. F1 N" M0 r0 e. Yand a ground-based operations center over a radio) W: ?8 p+ B; |9 [& w7 x4 a
network.: M0 Y# C$ T. m, V5 G: \
AIRCRAFT CONDITION MONITORING SYSTEM, A
\6 g3 T0 h8 }system of sensors and recorders to monitor various
' v4 E, ]3 h6 H/ O$ x5 ~airplane systems' performance and status.
4 j! H) k* z2 X& a [! m& \: `机,
4 f% H- I8 w' W8 C0 e# x中交通管制,4 H" \, ~9 T4 ]- g4 E( G; L5 I( F' {
一个由地面设备和机载设备组成的系统。用来对飞机进# j5 k5 t0 s2 i
地传感器,
0 ^' `) X% x) q+ j9 U一个由起落架操作的电气装置。用于给空中或地面的飞
8 R' [" X$ G* L+ K/ @系统运作传输地面/空中信息。(有些系统只能在地面" o, o- d( o9 B. r" z" g0 U
用)
5 }" v# P* Z0 `载振动监测器(AVM),/ u0 T2 ?) l+ |3 w9 S
AVM从装在发动机上的加速器取得信号后计算出该发/ x; S) C: f5 L! u' R& q) t
机上的振动。0 a* _$ K7 c9 u- r6 N% n) \& r
式建立的控制区域,内有无线电导航设备。
" x; U6 P/ @+ p q, U飞机通讯寻址和报告系统,7 r$ A) C# b' x+ z. ]* b
有种可寻址的数据通讯系统。利用该系统可使飞机与地, ?/ w" o% U% Z4 ]: m& P/ y! K
面操作中心通过无线电网络进行数据和信息的交换。- i$ N; [- _ ~! I
飞机状态监控系统,! M' O S% C; d1 L8 P6 k* `
一个利用传感器和记录仪对各种飞机系统的性能以及
x$ q% y% [3 j" u( t+ R状态进行监控的系统。" B0 V3 |" P q+ J& V; Q) |( x3 {
A
8 Z y$ M& }6 g9 c/ u- g. X0 Cg
3 w9 l( z) _# l. @and locate aircraft.( k/ o" S& G8 f! s, d/ N, H
AIR/GR
( c4 F4 L- x" Mb, q- |( o& q/ O s9 ]0 u5 z+ a% G
in- g. w( C/ z3 t
g7 z# r, W/ O3 ~ |
A
) t4 O& J& e6 L& Hth3 h& B) I* N" v; e. m8 D9 r0 j) q
c
1 s4 s% k. ?' y& P9 u) @' c) @1 M; WAIR WAY, A control area or portion thereof established
& ?3 ?* G @* u, Rin the form of a m3 O* U( q9 Z7 Q
大气数据计算
- P% i, f5 n# k$ @& J根据量取压力和温度而产生大气数据资料(高度、空速4 w& f; v8 H: e: {) e( f1 p
等)的计算机。0 M. n P2 \: V n6 x
空
: R8 H2 w/ ]1 w* s- o( J* Q行识别,跟踪和定位。
% i# G. T6 Y1 m( j" B8 j空
" B/ w9 r0 U$ x9 _' e; J/ C% i. V3 n机
- q" k. s8 A: `; s使! B8 v. Q3 e+ p7 a. t: Y5 s5 f
机* Q: {5 T( d3 Y. r
动
) _+ I3 _5 B. _0 m3 t3 \- {1 _# H航线,
: h. D- w V8 l; Y以走廊形, G4 z/ F7 q$ ~: y% V* ~
英汉对照民用航空词典B OEING
6 M# r- S# l; {1 T6 TTECHNICAL DICTIONARY 6
- g, b: {% R7 ?: N: lAIRFOIL, A surface designed to obtain a useful reaction,
/ W9 a3 u) |9 Zsuch as lift, from the air through which it moves. Wings,
+ c% B _0 J* D; P, [+ T. ?4 Astabilizers and control surfaces are airfoils.0 ]- A( ]/ f8 l. z6 h5 v
AIRSPEED (IDS, TDS), The speed of the airplane
?3 b6 }$ t4 k+ k$ _rough the air.5 G" G: E# S( s7 C) G
D INDEX, An adjustable pointer on the
$ p5 @' X Q& \: O5 }4 D# Yirspeed indicator.
, r# t& J6 n7 N2 `3 I: Rand legal ability: j! G' W! R7 T( `4 T
fly.
6 K: [" w. k" Q$ c5 km, for example, the procedure for finding the
: N8 L( a3 ] @1 s3 \quare root of a number.
6 A/ l6 z7 G/ Z! G! o1 m1 K" L% yy5 g8 ?9 v: Z) i( N/ y3 O
re, wind,
1 e: \/ b% G6 o# P6 a( Zand aircraft flap setting.
- E# [8 L2 W0 N$ o是翼面。
. v3 m ~. o5 K6 y' b- h% J, d; v$ f速,
2 b3 E$ _: `2 F0 i1 n. u! _8 N飞机在空气中运动的速度。
2 _1 ]% J* _1 M# ~9 h6 ?6 J,$ {0 d' d$ W" J4 @2 S w
在空速表上可以调整的指针。
+ z& K6 W; ^, n机械飞行能力、和合法性的飞机状态。
, E; z" c. x8 l- @# k一步一步的解题方法。例如,计算一个数的平方根的步
5 `: c3 ]2 x5 n, t& Y! {。/ Q+ }( X. ~. X, r( s) }$ k7 |
能# ~/ A$ }- L' [6 c
资料的法定文件。
5 h+ i4 _3 J5 j& a1 e翼位置成函数关系。
2 C7 H# @4 ^* m1 I/ A' w2 N* Fth
; T0 x0 x9 ?( nAIRSPEE
# i! \/ g+ ` K5 g' U3 i( ]% _a' f% r! |5 R; H9 q3 }8 ~ P
AIRWORTHINESS, The condition of the aircraft with
, B, g# l. p' z0 H0 krespect to its aerodynamic, mechanical,
1 v; B" B. m( rto
6 A- C u9 A1 LALGORITHM, A step-by-step procedure for solving a
1 s. O7 `* J: Y$ R$ t7 I, qproble& K' _- c1 @5 n4 m- W: k5 o- ^: i
s
8 `* P& z0 Y" v2 J# CAIRPLANE FLIGHT MANUAL (AFM), The legal4 e% X7 J C, Q7 u' g
document containing performance and operating limits,2 X; O& N3 ], D( l
operating procedures, and takeoff and landing
4 s" Q: T4 P$ B* w# ]performance.$ q5 |* a6 }( r. G
AIRPORT ANALYSIS, A comprehensive set of takeoff/ R: o& m5 R; G/ W2 A, O" ~
weight limitations for a given airport runway, generall
3 p' B4 V% c; Y" r/ M; p- A) Bpresented as a function of airport temperatu3 c, c# P# D+ z$ N* N
翼面,
" y; S4 ]8 J0 H/ G! l用以从气流中获得反作用力(如升力)的表面。机翼,2 z' y6 k3 _' R2 s) ~1 B
安定面和操纵面都' F" O! G- t* J) p6 ]& |3 i) b
空2 K2 b- }0 ?( u8 \. [
空速指标/ c" Z4 Q( O* B/ ^: v8 R; n7 T
适航性,4 W" x1 k' R8 W# n2 ^6 g
有关气动能力、
! Q1 m6 X! N3 a5 v8 @) f% D演算法,
' m2 ^6 @1 _5 T* n: G* V骤8 H- r7 t+ M' {
飞机飞行手册(AFM),
9 _+ Z c" G. S& u包合性能极限,操作极限,操作程序,起飞和着陆性
+ o1 P) V' _8 ~9 b: {' X等' s9 r) h, t, R5 b
机场分析,# B9 G0 ^7 q3 W8 ?: Y) I% V2 d
一套针对给定的机场跑道的详细重量限制资料。通常与
! ?. }3 z* u, y3 U |* g/ |机场温度、风、和飞机襟" ~# P& k, Y. J* X5 k6 R8 `0 A
英汉对照民用航空词典B OEING5 ?% b# I1 `9 [. Q$ e+ u {$ ?
TECHNICAL DICTIONARY 7
/ \0 @8 ~1 F& v/ b+ u/ lAIRSPEED BUGS, Adjustable pointers on the airspeed
3 D( P% |3 N9 m2 j" uindicator.
3 I1 K* q2 y6 n, n. hALLOY, A mixture of a basic metal and small amounts
" q+ [. E+ @* D! E8 Vf other metals to change the properties of the basic
4 l" M' f" Y& c( K, m }etal.
" t; R% d3 D2 m0 U- g& X% A; J! ^Minimum airplane speed.- e, P; n( P$ i: I5 w3 e% B
e of; V, M+ R6 o* k1 B
itting airplane angle relative to& A# S/ x4 q+ {9 O
irstream for the stall warning system.
: l# P2 m# O5 W2 v" R& aanother.8 [0 e( e0 |+ o& j; E: ~& k
LTERNATE , An additional airport selected during( r+ |2 U+ P- d' K# y
,) Z6 k0 }3 m! I) _( ^% U
合金,
: U: c" x2 U$ P; Q) G在金属中加人少量其他金属,而改变其性质的一种金属
6 a+ t6 T$ I0 ^! a' q# j* n+ g合物。: K, X2 l# e! T3 C u- T# s
飞机的最小速度。+ d' N# m& c+ j3 x7 A
速警告系统传输飞机对
& o! _2 V. N) z" x+ ~5 h! \! S" r: q流的相对角度。0 @7 p: C) P, Z; Y7 u* ~$ q
由一个状况改换到另一个。
; _7 q$ y- y) h' z1 { o+ I. e降场,$ T, p/ s4 Q. N# o
划时,除了目标机场之外,所选的另一个机
! L# v' C4 U+ Z" y& B# G7 uo
6 \& m9 M4 e0 L$ Y+ e8 am
. k# M; O2 `7 |7 |% |ALPHA SPEED,
4 _% J) s d @' P8 YALPHA VANE, A small moveable airfoil on the sid
7 A, m7 a5 N( c2 `' F- C/ bthe fuselage transm
( h/ n) x- D4 x/ m/ a" o3 f. Y8 A \a
; ]6 w! K( J3 ~( o- z# VALTERNATE, To change from one condition to
3 {2 g( X: z; O( y8 S" y/ s! hA
y7 E7 D, ^! W% j& b1 t7 h& aflight planning, usually near the destination airport, to be' U# a/ u2 D) u8 m9 V
used when it is desirable to divert from the original4 B) }5 n7 R. u/ `$ G
destination airport.3 Q) O0 E! T$ e0 i
空速游标
0 U; q% s" F. D' [, R4 f$ I1 d; w空速表上的可调指标。
/ O* w6 G: b9 h- x2 N" N混
( h4 J1 V C- ~+ i: b迎角速度,* u' O4 z+ e8 d; X! i
迎角叶片,: W4 } F3 V) R @
位于机身侧的可动小翼面。为失2 ], `8 Q8 W) V- A$ |: N4 }
气/ M; v5 w- h% m0 a3 I" k
交替,0 L& z6 v5 F6 e' L" ?, c
备( j9 e. x* I" q( \% g
制订飞行计
* S$ n0 _- m! V! f" G, g2 t% F场。通常在目标机场附近,以备不去目标机场时,改降之
6 y, u; Q/ J2 x' Q s用。* n) v8 G: C5 ~& b# W. Z9 T
英汉对照民用航空词典B OEING L: P0 X+ \8 U1 B# _
TECHNICAL DICTIONARY 8- H) [$ m* S; q' p2 s# j/ E/ t
ALTERNATE AERODROME, An aerodrome to which
5 S1 x9 i0 u7 ]6 X# \an aircraft may proceed when it becomes either
( k/ E6 m' i Y x& tpossible or inadvisable to proceed to or land at the
D: \- {9 @/ cerodrome of intended landing.9 C+ D$ h" f7 X+ m
TER SETTING, The adjustment of the altimeter
x3 c7 {& T' B2 P( L4 Y( s) z6 Aaccount for local variations in atmospheric pressure.6 s3 n. J- b' l0 X$ D! c+ x
LTITUDE ACQUIRE, A digital flight control system9 q5 k" A% }2 P# B. B; @ R- X; Y6 `
ode to transition from climb (or descend) to level flight.
8 @, {$ A) e: t5 v0 s$ R$ sLTITUDE ALERT, A flight deck alert occuring when the- Q. l. o9 ?7 b( o7 n; M0 H
irplane approaches or departs a selected altitude.5 [7 t( `, A7 `8 }% D
LTITUDE CAPABILITY, The maximum altitude at5 p" P: s- O% M2 L* F
hich the airplane can be flown at for a given thrust,
" r! k: R( `. O. Cpeed and atmosphere condition.
' E" H1 r& i; _: a3 K: G% O3 |1 OLTITUDE HOLD (ALT HOLD), A mode of the autopilot
. ]' }) T L8 Z3 qr flight director to maintain a selected altitude.
' R& `7 B8 j# m8 Virplane's altitude during VNAV operation.
& H* g$ `6 Q& x机场着陆时,可作着陆使用的4 X" S( u( K% a5 c& l5 y+ b) u; E
场。; _9 x* M1 G% b% P
,# p- K6 I* d# Y( h3 M5 Q; D- q
根据当地大气压力变化而对高度表所做的调整。
# X9 A1 n) b$ ]8 S: ^6 A一种数字式飞行操纵系统,从爬升(或下降)改平的模) F0 _7 { L8 r9 m1 f% F4 W
。
5 _+ H6 F$ J0 \" W% c6 Q5 y度警告,
- P( `' ~6 I8 K9 [( u& J当飞机接近或偏离选定高度时,所出现的驾驶舱警告。, x) Y, Q) D- c/ k" w
高度能力,: @5 ?, ]- U' d7 G5 y% |" a/ Q$ A4 P
在给定的推力,速度和大气状况下,飞机能飞达的最大
5 N: T& z; Y; I9 V2 O. F; @7 D高度。* }% V+ B7 e% G( E
高度保持(ALT HOLD),
6 L) N4 u* @7 a. w自动驾驶仪或飞行指引仪保持在选定高度的一种方式。 b- o7 T4 J1 A6 Z( G
,
( [/ X, }/ \3 O! b5 n, k3 v员对飞行高度的控制。& T/ J+ j8 \1 S; M9 Y
im0 d* v& X1 R5 n$ I2 }* x
a
, B* k) `# ~, l, W, UALTIME
8 ^( X0 L: C, ]* ~( {' D% sto
7 r0 _" |4 X f) uA
$ N$ s9 a" d) lm
' h: H, I0 m* x' Z+ ]A
; K' K1 T/ _/ \& m/ \, oa
4 D+ R+ l* b' x. p! G9 ]& l3 QA
" p! V4 U- l+ N8 v$ q+ h: Hw
& h2 F. V i4 k1 U1 q9 Fs
0 D+ Q6 N3 |1 m+ j6 ]+ r/ ]" MA. w N; g5 ~' Y0 ]" A; i
o6 b! }9 D1 v& }9 N- K! S' C3 C
ALTITUDE INTERVENTION, Pilot control of the
f; R; W U. j+ Q. ha
* J0 H, k) s$ Q; L( ]$ d+ ?! rAMBIENT, The surrounding atmosphere.- h& J; A. F6 \% A' l! h1 X k3 ]. e
备用机场,. `9 U: U3 f8 ~2 t& C, w1 X- b0 P
当不可能或不适宜在预选1 e" P7 U$ w$ O7 o9 w- k3 n9 p
机 {3 C2 P1 l/ A& t, } W
高度表设定$ R$ }. ~% }, f* P
高度截获,) l l3 v+ E; B' `
式/ {2 m+ ^' n K
高9 T1 r' n+ j' ^" O- R
高度干预
2 [' L( w- r* X& s- d6 c在垂直导航工作过程中,飞行
) ~: e a2 c3 D& O9 H, x周围环境(地面气层),
f: e1 r( e5 i# X: G# k物体周围的环境(特别指大气)。& l7 Y! w! ? ]6 T. q. a( o& m
英汉对照民用航空词典B OEING
( c; s. r: n& g# sTECHNICAL DICTIONARY 9
0 X; s3 ?- X: X5 p$ kAMBIENT PRESSURE, Pressure of air surrounding an3 r: @$ y; ^& a. _" P" A
object, measured in pounds per square inch (psi) .
) w( U- }1 M/ Z: i# U# `MBIENT TEMPERATURE, Temperature of air9 D( O8 T" O0 p0 a6 j# ^( h+ Y2 P9 H
mpere.
3 w f* z: n0 e# murrent waveform.0 m: |/ J9 s' C" P4 x- y6 E
g an
, C2 H% S3 i' e: c8 J0 I N% \nalog signal to a digital signal.
" e$ u7 P9 X1 S$ U2 fore inputs
; l2 g; A4 ~4 \9 @1 n0 @* w. Vf binary digital information and one output. The output% } L2 N* {2 }: L- B& w( g: p2 o
1 only when all of the inputs are 1. The output is 0
' ]* r, s7 ~4 e" K3 [4 nhen any one or more inputs are 0.5 e/ w3 [8 b- x7 ]" D2 R
面气压)," C- c1 y8 P) X t0 |
境温度,
6 V2 ^9 J2 G* y% {气温度,用摄氏度(°C)或华氏(°F)来
1 I/ x/ h# X, g, A) p。
- b& k5 M7 J2 c+ f: O$ l电压或电流波形的幅度。
6 e) V3 F! A% _* ?# E性变化的信号来工作,或产生连续性变化的信号& k0 R3 _6 n& p
统。- o$ N4 |% r7 z( \, J3 u6 F' o
将模拟式信号,转换成数值式。
% W4 m2 r U0 C' L一种有两个或两个以上的二进位数字信息输人,一个输
7 d* z- I' U f% P的装置或电路。当所有输人为1,输出为1。当任何一个5 M- c8 ~( |( M& ^* `
一个以上的输人为0时,输出为0。3 `2 r, F6 y! b
A
+ R5 ^: B6 ^; Y/ N& lsurrounding an object, measured in degrees Celsius
" m8 R" c3 M5 W9 ](°C)or degrees Fahrenheit (°F).
: ?) O8 d" K, y; dAMPERE, A unit of electrical current. One volt across+ R* d9 w+ N9 H- c. X. M
one ohm of resistance causes current flow of one7 o4 }5 ]! ?" A0 |4 {- C& J
a, J0 x0 V. [1 Y# a7 l
AMPLITUDE, The size or magnitude of a voltage or
/ T9 x2 d" n' [, @% r2 e3 `7 N& Gc! Y: O# Y# `) r3 L% ^4 l5 f
ANALOG, Quantities or representations that are
$ B4 E0 ?( f1 X* k8 S+ ~7 Kvariable over a continuous range.
2 P* R+ \$ q6 BANALOG-TO-DIGITAL, The process of convertin
) ~$ m3 Y8 {7 va
0 i% u J. H8 X2 N0 `% |AND GATE, A device or circuit with two or m
: F* a o; a8 `4 T1 Yo
0 e5 ]# j3 ]# I" ]' Eis
; _/ n& G5 b5 R1 r0 k$ L0 {4 vw
0 x' {7 X% \( t, u/ k8 }6 w& I x% D环境压力(地
, [: ?% h- S' v1 i9 Q物体周围的空气压力,用每平方英寸多少磅(psi)来
2 X# |) c! r$ ]- O) ?% T6 s度量。3 |" d7 C4 S1 a) a, r% w
环* t! a6 \# T _* f, d) q
物体周围的空
- Z7 |0 o% L- t- f* u1 u1 q2 r度量。
/ ~8 r- g6 i) Z- Z1 v* i5 f安培,
+ G6 E: g+ `9 ~" o电流的单位。
) D/ {5 S2 z$ j' [1伏电压在1欧姆的电阻上所产生的电流为
3 q0 w4 E6 E$ T1 y' P$ Z1安培
1 Q+ c' V. _! f5 V3 Q. ^" ^7 b$ b振幅,
H. a1 Q( m5 c2 a. p" J( Q模拟式,
/ T0 L. j9 K8 ^* V( b( o- E$ H. a, N用连续$ B' u) A) E- K, [9 a3 @
系
6 n: }2 m% e' R% ^( |: ^% P s从模拟式到数字式, v3 f5 i1 M. w# y/ f6 ]1 v% C
与门,
3 A" [; E. m7 Z出
. D1 h3 L- x& k或
7 N, ?0 L. K+ w# }) q/ k' `! S英汉对照民用航空词典B OEING
) n+ g2 X I, V8 K. Q) aTECHNICAL DICTIONARY 10+ J0 h& l4 j. \% u5 m
ANEROID, A sealed flexible device containing air at low
3 s/ w2 {/ W& v) R% d; Tpressure, which expands or contracts during change of2 p W+ ]; S2 l& s! ]% k
ressure outside the device.
! S7 `. L; ~0 ~7 G& ?7 Y( ~. Y3 C8 eically) Q5 j% e* J: X, ~% G N
r changing the direction
. ], B* ?3 \5 r: vf drive.
/ l) }7 ~- B5 W9 L7 t- W# B# Dof the wing chord in* \6 g* Y3 G G% C
lation to the free stream airflow as it moves forward5 }% A, M+ f# |0 G2 y
rough the air.$ Z& q, ^' q$ b2 C7 F
al axis of the
' \$ @; c. I0 Taircraft.
, s6 \8 E7 W6 |4 U. D* H胀或收缩。( |7 D" W& V t | Z' U
箱。是改变驱动方向的机械装置。
. Q: E" m4 d+ E7 C! h: L( D机翼翼弦在空气中向前运动时与自由气流之间的夹角。! u3 s! \. d8 N, C
。& _- r' N* [7 G M/ C# g; z
p
( P; `1 M$ L$ i: ~1 D; J+ ?; nANGLE GEARBOX, A part of an engine, mechan
. O& H/ [, l6 ]8 u& [# U$ r, xdriven by the compressor, which drives the accessory
# { T3 V# |! L5 w$ e3 r: `gearbox. A mechanical device fo
+ G- q; A- L: S6 v3 x' qo7 t5 |( @* R: t4 n5 ]7 d+ V
ANGLE OF ATTACK, The angle
' |% L; k: j8 [re0 g/ f* h* x* H; T! d5 C
th, {- g& x2 H) w; A3 S; `- {& o
ANGLE OF INCIDENCE, The acute angle which the
) ?& m& t7 Q) ]& `1 Mwing chord makes with the longitudin! R) o0 u; d. G* @: E
膜盒,8 I a" c5 k7 H
内含低压空气的密封弹性装置。当它周围的压力变化
1 L% P& g y5 E- H' O% {时,会膨
0 f# }% \5 j* j/ F+ B6 O伞齿轮箱,( T% M9 |$ a5 ?* ]4 ^5 `
发动机的一部分。被压气机以机械方式驱动,然后驱动+ k* T3 O' f/ N1 ^
附件齿轮) ] @, k$ P7 E+ j1 p* R( h
迎角,% f$ S3 Q/ r- |" M- ]
安装角,5 @! M$ ^$ f7 z$ V1 v% a
飞机的纵轴与机翼弦线所形成的锐角
. w0 M% Y+ K% v1 Y6 j E英汉对照民用航空词典B OEING; l* n/ E" m; j5 @. O8 o
TECHNICAL DICTIONARY 11
; y+ \! }1 q& I0 KANNUNCIATIONS, Audio or visual indications used to( |2 F$ q. q* k8 R3 @, w
call attention to an event that has taken place.
1 m" t. X/ X- i7 t! x" [( XANNUNCIATOR, A visual device consisting of a number8 B* ~% M4 t" P2 H; c
ly.$ L) ~ m/ v7 c/ g S0 u& ?9 r# R/ W1 ]
ANODE, The element toward which the principal stream/ k8 p/ e" ^1 W" B
of electrons flows.
& S5 d, x9 X8 b' z7 s2 ~/ ^8 IANOMALY, Not normal.
" b2 C( [9 j3 E2 f KANTENNA, A device which, used in conjunction with a
% X7 v$ t! J6 N7 a( F7 a! otransmitter or receiver, is used for radiating or receiving3 ^/ u! N! ?, h& q7 ]
radio waves.
1 Y: H( D5 M) q" ^: @NTI-ICING, A method of preventing ice formation on9 f9 a) M5 C: J M3 G$ Q) z0 S; J
e wing leading edges and engine nacelles.
\) m8 `$ l% MNTI-SKID, A system for providing maximum braking$ ]) ?2 u4 K2 ^; z* ?$ j5 C. d& V
ithout skidding for any runway condition. Anti-skid! M( M8 | k# O
omponents are part of the brake system.
( Y% ?9 O; h. ]6 W& @3 f告,
( o* L- Z! y! |7 F当发生事件时,以声音或目视指示形成的提示信号。
7 O. A2 D) O) }" p) n3 A- t与之有关的电路的现有情况或已存在的
: [. y& W. J" P: N! }! O: w况2 |9 o6 N \+ y! u4 m) O, D
正极,% E* u8 E6 F J0 S3 Q2 Y
主电子流向的极位。
9 }" N! Y' B9 g* M异常,9 M. q6 Q! t$ R% h( G: G' F
不正常。 \# Z8 C1 m* m* n$ W
天线,/ S) \) j/ i% Q3 ~- [* _6 m
一种与发射机或接收机共同工作来发射或接收无线电
; z, ?, v. e) z7 C波的装置。
; k0 V" @4 \$ S! Q冰,; D4 A* T4 D( P# [5 k& R4 F/ ? O
防滑系统,
" R U3 B2 a3 S9 _9 R0 }4 X& i* z一种在任何跑道状况下,都能提供最大的刹车能力而不 B% x+ V3 b9 i8 w5 @3 n2 p
使轮胎打滑的系统。防滑部件是刹车系统的一部分。
3 C$ H V3 a9 _! b4 _5 aof lights. Each light indicates the condition which exists
6 G( p; B& Q3 i" L$ |or has existed in an associated circuit and is labeled
6 q! }6 k) `: daccording
' L1 O# u, J( u+ T' i6 h* @A- g% |5 S$ j6 d
th
! ~/ y7 U/ D4 t' J* x+ _( VA
) |9 _4 D6 u7 k! q9 F* Zw
# H' B# l8 m" C; C7 i# ^c- @ M+ k& B7 n5 G' z
通3 k; j0 T+ J8 S
信号牌,
* G. O6 k& [" K7 U/ M* T/ X由一系列指示灯组成的目视装置。每个指示灯都有相应9 g$ e Q1 j# c- ~) G! q5 S7 ^" \
的标记,用来显示
8 O6 A$ Z& m$ s: q/ t情
2 Z# p0 @8 ^. a6 E+ v8 x. m防
7 n+ _/ s2 B& \' Q" j防止机翼前沿和发动机短舱结冰的一种方法。
, {0 _7 ?4 D$ O2 G2 u4 g' @& ]英汉对照民用航空词典B OEING
4 q _* l/ z7 R3 ATECHNICAL DICTIONARY 12
$ p W! Q B2 g5 [0 e/ L5 S7 zAPPENDIX, A supplement to the Airplane Flight Manual7 O9 _( E- Y3 b" X) e$ L
tained in the basic manual. A) ]0 _7 i* `0 z; g, `- u9 G- o# @
ollection of supplementary material at the end of a! @- j$ z$ H" T: y1 h* K* O2 e
ook.- D" m, w! _; T
of the ^7 Q" u: u7 n5 x/ l
rsion link on the landing gear.
: A7 D. A! z7 Q. _2 NAPPROACH MODE, An autopilot/flight director mode" b7 m. v8 m8 U" K, p
which is a combination of localizer for roll control and/ j) N, F, R4 q9 g3 s
glide slope for pitch control. This mode is used when full
4 P9 n4 u6 t8 ]instrument landing system is available.
! E4 L5 R+ Y( [2 z# p1 T& j; i( GAPU, SEE - AUXILIARY POWER UNIT
7 k" W5 p* m( E5 N# E! QARINC, SEE - AERONAUTICAL RADIO
/ R, i$ ^6 Q9 YINCORPORATED. s5 E7 T. K1 M" I& R
ARM, To make ready for operation./ E2 h% H* |- W. s' k9 u; w. C
附录,
: m n9 Z8 F9 i9 w飞机飞行手册的附件,包含基本手册中未提到的飞机形& N; d: \$ D& @% P9 z7 m7 S
态的其他性能。是附在手册末的补充材料。! E( g$ [, y% T9 c
顶销,
* Y) [" i' Y: p9 R$ ^2 e, k用于连接起落架扭力臂两部份的销子。1 [5 u4 l ] A4 s* J0 M- q
进近方式,
; v8 q8 \: {) q+ t6 O/ I2 _一种综合了控制横侧的航道信号和控制俯仰下滑信号
: _; P4 y Q9 T0 Z X' _; o# X 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 }1 R2 s4 I+ u* b5 p+ r. O+ R) Z统正常时才使用。
" e* {5 a9 a o& d' }) `9 J辅助动力装置,, p. s- b9 c1 ]% R" I3 j. R( K d
见Auxiliary Power Unit
2 x9 z; l, a/ w* k5 i( M' f/ Wcontaining additional performance for aircraft$ v$ ^. X" I3 a6 ~
configurations not con- y2 B0 @1 y, n6 W9 X2 D3 {8 S6 b
c; s. C8 P- m7 ]
b9 H- `5 t8 |9 J# p6 }3 n
APEX PIN, A pin for joining the two sections& u: M8 g) C5 ]/ T# M& w
to' l6 {% X+ X# t6 D: I, Y6 j* r
.6 ~' S) }5 G& |
航空无线电公司,
6 Z' f1 J1 T0 |( K- k7 T; F见Aeronautical Radio Incorporated.3 }0 v6 p( j; ?( S/ y7 Q, f1 B
预位,' K6 j( M, X" ?6 u
部件可以开始工作的状态。# a5 J6 l' E& ?: l5 x6 h6 k2 M- T
英汉对照民用航空词典B OEING
" a5 x6 r* M& F: qTECHNICAL DICTIONARY 13. @9 C; B5 w9 b( r G
ARC, The curved track over the ground of an aircraft
) \7 A0 u( P% c4 B! d! `' Qflying at a constant distance from a measuring5 b$ g% [& c0 v6 ~+ q* Z6 M
equipment (DME).
- G: k0 K$ B0 c1 P. _( E9 Fin the limits of self-contained system
1 s7 X, a% x P% z4 X9 [% `! kapability.
% I6 j% b/ W7 w6 G$ ttem for opposing or restricting
1 R4 t9 f0 U0 `+ N2 o! h6 }ovement.
9 c h1 \0 r6 c0 O- NSPIRATED TAT PROBE, A sensor that measures total8 P T( j& n' d1 Y( y( B# z
ir temperature when the airplane is in the air and that: |& D7 J& F" s' ]# S5 E
easures outside air temperature when the airplane is( k& Z) ?6 s& b( c- J }
n the ground. The outside air temperature is measured
5 b. G0 i% |' K G' W6 T& Z" K5 |SSEMBLY, The fitting together of a complete structure
1 z- e5 C& m$ k' M: b, b, h- `3 W3 g0 [SSUMED TEMPERATURE REDUCED THRUST, The
9 D6 d( s! D$ ] B/ `' }6 f( WATC, SEE - AIR TRAFFIC CONTROL
u4 Q, Q p6 F( S, \7 u. S( q,/ Q2 G `: j( K* s7 ?/ U9 `4 C
系统中所产生的一种用以抗拒( M. w0 E0 c/ y+ ~# q
作或限制动作的力。- H) s4 d8 J' W/ z8 Y3 L
头,
C: k; J& m( m- u7 }1 B3 M用来测量飞机在空中时的总大气温度和在地面时的外6 \; N2 U$ z2 G# [/ S& ]
温度。地面外界温度的测量是利用引气将外界空气吸入
8 m( r- W1 X# n: s: O, Y9 Z/ g头,以达到测量的目的。
4 k& ]( I6 }: A5 L' u* F配,
: O. R( v' _7 K0 d% B) k: K$ u一个完整的结构或组件的过程。
4 }9 i% Y1 K$ }# o! ]' E假设温度而得的减推力,4 @/ c1 l: ]& N2 B5 v4 b
推力设定值时,假定一个比实际外界空气温
( E& z2 S. `3 E e空中交通管制,
, b0 u1 b) W5 r$ j( Z% _6 G见Air Traffic Control; y; z- @' c, G/ [' y+ `" B
AREA NAVIGATION/RNAV, A method of navigation
2 k2 m: _+ W, K) J+ E- k$ {& othat permits aircraft operations on any desired course
2 ]0 L( p, G! S5 n. _. Wwithin the coverage of station-referenced navigation
2 I7 A4 S$ |4 ?5 ]# t, Esignals or with
}% c* a& B/ }: X, H! uc+ Q3 F3 F& f& q. F1 R0 b# R
ARTIFICIAL FEEL, A force developed in the flight
U. k7 L5 x) Ycontrol or brake sys
$ e4 |, j. }" |( x- M1 `9 p y1 ym
4 t3 h) B0 m/ x3 o9 S& t+ hA5 G- l! A/ R' S
a4 Z0 m1 f$ ]7 F* G# b
m+ n* J6 p" E% W+ \0 X+ H; L
o7 ~, ~* I1 \) Q# t/ W: G, G3 n0 Y
by using bleed air to draw ambient air through the
/ f/ f/ i. }4 ?0 Msensor when the airplane is not moving.; O( r( K1 ?- L$ l2 W' W% F0 u
A
& l' I7 Q$ x" y/ L: O0 m0 B5 ?* S- hor unit." |$ I% J; N: k
A
* @/ v/ N+ w& y5 _; x- r- ilower thrust obtained by setting a higher than actual
1 Q; C: M7 ?/ a) y1 q* rOutside Air Temperature (OAT).* q% V: O4 c" R; w8 t, H {# m% P$ l
弧线,8 R4 r% k2 }9 q' R
飞机在围绕DME台等距飞行时的弧形航迹。! a/ r1 j9 s- Z( c* P
区域导航,1 `% Z2 x) Y, b$ d. k" Z4 S
容许飞机飞行在有电台参考的导航信号或自备系统能3 P2 h4 K9 E& k( T
力极限范围内,飞行任何预定航线的一种导航方法。
: W3 O# D# v6 N$ l& L. @ J模拟感觉1 W" A9 h. r5 D9 F, ~7 h
在飞行操纵系统或刹车- ~0 f; |. W! O! a
动
# q0 O$ Y0 f! f" n/ K4 Z吸气式总温探7 v) K m W9 D5 U0 l* S4 O$ Z
界
/ K$ |' j, ^% |7 b7 p H; N. \探$ M& s* ]5 u- S( d' v. Z
装0 W2 V8 H: M' i2 m% l$ n2 J
组合成
7 P- B$ `2 w4 ~6 d$ `# K6 @; {由
( {6 g ~% v4 f @在选择起飞
. m+ g8 i3 b+ X' w' M2 s+ v度高的温度而得到的推力。用这种方法可以减少发动机的
7 c5 D9 O) c& D; h$ G磨损和维护费用。& f- s; h U; l0 Z. H0 S4 I
. c/ c# {0 a* F3 s6 s$ {% y
英汉对照民用航空词典B OEING0 b8 v/ \! c. g/ h
TECHNICAL DICTIONARY 14
# a6 L5 w3 d$ G) g0 eATE, SEE - AUTOMATIC TEST EQUIPMENT. [- _' b4 w$ N$ W
ATMOSPHERIC PRESSURE, Pressure of air due to the
4 |3 f; L3 I+ r: X; oarth's atmosphere, expressed in pounds per square# U* W2 Q" S0 _- J0 A$ m7 q4 R6 f
ch (psi) or inches of mercury (in Hg) or millibars (mB).
7 Y9 K$ {* J, Q" s1 N% N' CTTITUDE, The relative orientation of the airplane with
' I6 O3 g9 I" N) r" L( Q6 ispect to pitch, roll, and yaw.3 b5 O5 z' E7 }, J q
UDIO CONTROUSELECTOR PANEL, The panel in
9 }5 Q! @" Q8 [; Z+ O! w" de airplane which controls and selects the routing of
5 f8 C ?3 f/ V/ `3 Xudio.# M0 z; A2 \8 c2 s$ r' T9 b# p! ^
UTOLAND, Automatic landing using the Digital Flight
: E! C6 k! f4 P0 M0 W3 R, oontrol System.
' F9 ~4 W: P& |" C% sn.
6 y8 a. h2 S& k: K0 g2 mM, A system
; {# [& n- v; ?5 A+ e3 Y7 [% T/ zomposed of all necessary subsystems needed to guide
4 w' u9 I2 M0 C8 a4 E7 B5 l Ue flight of an airplane.5 q( B6 c4 n4 M
EQUIPMENT, System test
0 h( S: v6 m. F# Y u! r, Vquipment that operates under computer control.
* r. r( w. r/ d: M7 r装置, |
|