- 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
# Q$ E. M/ r) R& F" K5 Wdata information, such as altitude and airspeed, based
" e' F* k4 B9 x' C6 ion pressure and temperature measurements.
+ Z: f" g; l8 s/ M" R; V; U3 X$ ees air" L. O7 }2 E* n% v/ t3 z; B$ P
IR TRAFFIC CONTROL, A system comprised of4 b; |1 ~ i: B. p) }) f
round and airborne components used to identify, track3 P1 H* j0 E/ x9 n$ E8 ^2 c
OUND SENSOR, An electrical device operated, E# b% a6 S! D3 {7 j8 o; l
y the landing gear, which transmits on ground/in air) X6 C! n1 ?7 A6 ?# B; K; I
formation for system operation in flight or on the
, g; x+ d+ o( Q: j" P7 {7 Cround.9 q# T, N: f: ]/ J8 v. y
IRBORNE VIBRATION MONITOR, The AVM takes5 W: u6 @: k0 {6 q& Z
e signal from the engine mounted accelerometer and
, W ^: l2 u* D0 ?alculates the vibration on that engine.. n) _) M; K2 i( Y, H
corridor equipped with radio navigation/ t% C6 s& g. J$ Y1 c7 Z3 c" W8 k
aids.2 o4 z) T1 l8 A1 F- l# e) a- ~
AIRCRAFT (or ARINC) COMMUNICATIONS: ~2 I1 c, b' i# `9 w& e
ADDRESSING AND REPORTING SYSTEM, An1 l5 H& y& G, q) U; P
addressable digital data link system which permits the
6 k# n+ C( z) v' y% D& X% Aexchange of data and messages between an aircraft
% h Q" Y" Y' vand a ground-based operations center over a radio
8 E! k; j5 h O+ W: ^network.
( Q, B# z/ A4 z+ P* s# s0 H+ gAIRCRAFT CONDITION MONITORING SYSTEM, A, c( E, N8 m! j( q# B. T& q) l
system of sensors and recorders to monitor various1 Y. s, \6 {* O) z) o/ u T2 M
airplane systems' performance and status.9 X l: }0 z$ G) w$ o
机,: Z! @. h+ e' x& U( d+ c
中交通管制,0 |- h' F7 s# |. B Y% H; @! P
一个由地面设备和机载设备组成的系统。用来对飞机进5 C: { \' s8 c+ u7 B) q& d
地传感器,. y( C5 n" c2 z, Z4 ?2 y
一个由起落架操作的电气装置。用于给空中或地面的飞8 d9 ^/ g' n1 o3 M' l( J7 d/ }
系统运作传输地面/空中信息。(有些系统只能在地面
5 N+ z% M& {+ W& V+ G9 ]; L8 r用)
3 d) R* k8 z. E; @. T载振动监测器(AVM),
7 d U4 R( c/ p$ [AVM从装在发动机上的加速器取得信号后计算出该发5 |& b) b, y& l; J1 ` D* ]
机上的振动。
. q) r. Q& R- T7 R式建立的控制区域,内有无线电导航设备。
7 u0 Q8 n1 b9 [: f8 @飞机通讯寻址和报告系统,. o0 S* a1 A' ~3 N- i
有种可寻址的数据通讯系统。利用该系统可使飞机与地1 T. a2 R) }, U/ g
面操作中心通过无线电网络进行数据和信息的交换。
( |% ?9 _- b/ s. J: j+ F" B# O! {飞机状态监控系统,
1 N1 J/ S' }# a, j一个利用传感器和记录仪对各种飞机系统的性能以及$ Q* a9 T) q; D2 x
状态进行监控的系统。6 `& [! q5 m/ [# _" w
A
/ D' {* m; {, U5 c9 Ng
( x% S$ c7 v8 D& Cand locate aircraft. }" w" v8 x# l" _) U
AIR/GR* _+ M# Q3 J7 b$ y; u3 w; S
b* O, [: Q; @0 M4 d+ L8 c
in2 W! K4 ]2 u. D. t! _
g
+ ^1 D, | V2 g- F' }: AA e8 x- T8 j- ?/ D! ^: H- X' b' F! M
th
! V7 q) r2 i Q. [, \; Nc" {7 k- S, \5 `% `/ ~% s
AIR WAY, A control area or portion thereof established) N; u* A9 x5 Y! F/ ^/ X
in the form of a
' [) M! }# z/ g# D6 P大气数据计算
" z) R6 v9 o( e# _$ L7 Y根据量取压力和温度而产生大气数据资料(高度、空速
( {4 K P2 \$ c. |4 f& q等)的计算机。8 P% i5 S% y$ A' ?" M) H) P
空( ], E! v$ N1 z9 }
行识别,跟踪和定位。9 K4 `& @: O4 E7 T: ^0 k
空
6 Q# ?- R( b. [" _' i& o. m* v! @机
4 O4 B( m" o1 n: p- f使
( |; i5 T/ L& p( N: |+ R9 @3 ~机
+ c [, Y; I3 _3 L k动
6 b, G& }3 r, z! M; [航线,7 j5 l5 ~8 A" {8 }* q! a% `
以走廊形
9 q/ ^3 V4 P' c* y4 {英汉对照民用航空词典B OEING
! ~% V! F9 ^# z' T# S4 w5 bTECHNICAL DICTIONARY 6
% i- R' r* X7 l. F/ uAIRFOIL, A surface designed to obtain a useful reaction,
5 T4 h b6 o$ r* k0 w9 Q- Tsuch as lift, from the air through which it moves. Wings,/ l& j( Q. c H) z* O
stabilizers and control surfaces are airfoils.6 G! S# q$ B: s4 H4 L
AIRSPEED (IDS, TDS), The speed of the airplane
$ w8 }" Z( W9 F# |0 i% ?rough the air.
% W3 N0 l* y5 _2 nD INDEX, An adjustable pointer on the
" I7 Y; D% O; j2 Qirspeed indicator.
- N4 s& Z* s% k# l( p4 A1 g& _and legal ability
- X: e. P: Z% \% ^3 [* R# m6 ?fly.4 P8 R6 G. O; T) ^: u9 p9 P
m, for example, the procedure for finding the
; u5 u1 O4 p. J W: N( H' G) c* rquare root of a number.9 q" I2 ], m! H* H
y7 W* n6 ?' L. ~ n" b% y
re, wind,
) s; q; O2 [& A& D- D0 U! y7 R/ aand aircraft flap setting.7 q! Y* c1 [% A$ n/ Z" c& \
是翼面。
: o! E4 n" V4 Z$ |$ P' r# m速,- D2 q/ H7 J! ]0 n* ]% O( |
飞机在空气中运动的速度。
) _' b+ Z0 g6 D,) r- d7 ~( O0 [" F3 l) `* }" h
在空速表上可以调整的指针。4 q- Y& y) d" O0 W: Q! X( _" ?
机械飞行能力、和合法性的飞机状态。
* q. Z9 I# Q1 i2 r% G一步一步的解题方法。例如,计算一个数的平方根的步
5 {; t s$ N7 l# O8 u。4 B3 V6 G. R$ N" ]4 g9 W- Z
能8 j, T5 [7 o! L. ^( r" k
资料的法定文件。! G, h) }! c+ i3 g( i
翼位置成函数关系。
0 x/ ?5 S, ~% A1 ^* \th
' t; d0 A1 [5 q- rAIRSPEE
% k( y+ }, o5 e+ J2 \a5 M# [1 g, l; X; @' N @
AIRWORTHINESS, The condition of the aircraft with- O7 z0 o* T' ]. _
respect to its aerodynamic, mechanical,
8 P ]: g, H2 A9 [& d9 A, jto x+ o3 L1 V! k1 a. o/ s( [
ALGORITHM, A step-by-step procedure for solving a6 }+ {% K$ O/ u q
proble* u4 r0 x7 @" w
s
. c- C P# R$ b, a9 Z- kAIRPLANE FLIGHT MANUAL (AFM), The legal
0 E/ z$ L8 A! U" ~/ J. F$ Wdocument containing performance and operating limits,( p% _* t3 ~: A2 u a1 d0 b g
operating procedures, and takeoff and landing' j- G) f$ D6 p7 u; N$ u D
performance.6 T* |4 W+ C8 |6 _+ p$ a9 x
AIRPORT ANALYSIS, A comprehensive set of takeoff! B3 k$ C$ S& @ r. _' ~ {: \
weight limitations for a given airport runway, generall' p9 C. Q# L! O# b' E: N) ^
presented as a function of airport temperatu
5 o4 _& C# b5 k; n: X1 E) G翼面,
( w: i0 H( r. I1 Z用以从气流中获得反作用力(如升力)的表面。机翼,6 \7 K* y4 f& |
安定面和操纵面都
, f8 @( C1 D7 s; Y2 Y) ?空
; [9 z- w4 N0 v: Y3 i+ ~$ t% _空速指标
; ?$ k2 }: t' M适航性,% r( ]1 W5 ^8 ^# E- H( W+ k2 w
有关气动能力、" |3 Y3 E* Y+ P1 K6 @
演算法,
, M- _4 e& d) R5 f' N7 r骤
) m' z Q$ i) T! E m; A( p2 h# e飞机飞行手册(AFM),
4 c" G, K9 H0 L4 F, L, C包合性能极限,操作极限,操作程序,起飞和着陆性
/ v2 W# X0 s4 J% {( T& a# e" L& n等- b3 ]) c- z3 F( k
机场分析,* T/ _7 [, j6 W' T/ m1 R
一套针对给定的机场跑道的详细重量限制资料。通常与
4 K* a/ q$ k) T4 U* D: {机场温度、风、和飞机襟
# s8 x8 w# d; ]英汉对照民用航空词典B OEING
& X! x [- }; Q0 z- T6 Z0 \TECHNICAL DICTIONARY 7
, X' @6 r) ]2 ?1 P3 WAIRSPEED BUGS, Adjustable pointers on the airspeed9 C4 ~3 {$ e! {' {6 O
indicator.+ q8 P, g) U( b5 q/ f
ALLOY, A mixture of a basic metal and small amounts, v. {6 N7 h# T2 x
f other metals to change the properties of the basic( p- \- o9 N! e' [( C+ b# X
etal.
7 Q$ N& T) l3 [$ W- ~4 q& o) p+ \Minimum airplane speed.
8 ~0 c( i7 K6 U2 M% d# ue of' G4 ?2 v O( n2 F
itting airplane angle relative to
8 l3 v) j$ ?3 ?3 x5 K- pirstream for the stall warning system.
9 P) A# E( {! O4 @6 B" W, d! danother.) |. Q( q* E) b6 {3 [; ~
LTERNATE , An additional airport selected during
: k, m9 n E7 ^,
6 P/ A% S- t( w7 r6 x合金,- |+ D2 X: l4 h1 q2 j3 [3 h
在金属中加人少量其他金属,而改变其性质的一种金属1 [/ `1 y8 S+ m X# a
合物。* G" V8 w0 L7 {$ T I; K" F
飞机的最小速度。
; K0 L6 P, Z! n2 Z. P速警告系统传输飞机对2 d( [# N# Y/ ^0 H/ G* o8 f
流的相对角度。% \% J- T" y) @+ t- c! q
由一个状况改换到另一个。$ F0 g4 v- J4 u- Q0 e1 G/ W& @
降场,
0 d) L* p, U; ~1 [; Y+ c r划时,除了目标机场之外,所选的另一个机
% d) h+ L1 ^% x) `8 |: `o
! w, W7 Q+ z+ [, C4 n& J' mm% A% B) b- Y' q9 g& M2 i4 [
ALPHA SPEED,' a: v% I2 Q( c3 W# ^; z( c7 u
ALPHA VANE, A small moveable airfoil on the sid
( O; m! o8 N9 }0 x3 tthe fuselage transm
9 v3 H9 n; T& L; ~a
8 `) Q8 f% c. o5 _5 [" K ?ALTERNATE, To change from one condition to) c% N8 z4 M6 e8 R
A
) C) { p3 @+ [8 F# M5 e* q6 H9 tflight planning, usually near the destination airport, to be
0 t3 u' o5 |: L# l D" i4 ~" Mused when it is desirable to divert from the original
' o. Z- E7 x/ T4 M: Odestination airport.
2 [) n) J* |0 v! J! H5 g' P/ o' T空速游标
4 O2 G$ o1 Z8 z1 a; i! y, ]空速表上的可调指标。
+ H7 ~8 m* p9 d混& n" r+ c9 l1 S+ R/ I
迎角速度,! _6 H& E' q6 I
迎角叶片,9 m$ D& W9 O9 M# F
位于机身侧的可动小翼面。为失/ x; Q- E {6 `, \. U
气- o: N1 n" t9 C
交替,
4 W! U! Q5 c/ Y6 [备
7 J- j) ?" G* b# x* E# ] N制订飞行计
# B( n7 Y. D3 h8 g% p3 s7 M场。通常在目标机场附近,以备不去目标机场时,改降之2 g. T! L+ C2 ?/ G
用。1 `) a; Q( ` F- S
英汉对照民用航空词典B OEING
( {, Q* y I( TTECHNICAL DICTIONARY 8
8 i* K8 |* g+ H5 DALTERNATE AERODROME, An aerodrome to which
" ~8 w, |: N/ A8 D7 E Ran aircraft may proceed when it becomes either& W" z0 l( w, J. Q& r9 t. k' S
possible or inadvisable to proceed to or land at the4 U, `; o' }7 U5 A) N
erodrome of intended landing.% R7 k3 i: e3 P, }
TER SETTING, The adjustment of the altimeter2 y4 V V7 S3 {4 F6 p8 s% N
account for local variations in atmospheric pressure.3 \! e- R& m0 v$ p* p' a
LTITUDE ACQUIRE, A digital flight control system
6 i" `6 @: m4 c6 P4 ~# qode to transition from climb (or descend) to level flight.
* L; A0 [3 n, h" \( yLTITUDE ALERT, A flight deck alert occuring when the
$ k) Y* G P l3 J% o3 uirplane approaches or departs a selected altitude.
- g0 J) [. E: R* e; Y5 _7 \LTITUDE CAPABILITY, The maximum altitude at
- T3 m N% X! x$ W, D/ e9 E" t2 Ohich the airplane can be flown at for a given thrust,
% j5 y2 s: l% T o) N) J' k* Vpeed and atmosphere condition.0 y, ? J; m$ k. B# l1 H
LTITUDE HOLD (ALT HOLD), A mode of the autopilot
+ C: |: [1 T" D v% T3 A$ d; Rr flight director to maintain a selected altitude.
$ s0 F# s4 u. I2 n) {3 wirplane's altitude during VNAV operation.. H3 x( b/ v8 u/ w9 u
机场着陆时,可作着陆使用的9 I; G$ H0 V; m; W6 W v5 g
场。. G U0 U0 Q6 r
,
2 C9 B% |& @2 I" q9 ^& `根据当地大气压力变化而对高度表所做的调整。3 C; _. u* Y: M6 w% u J1 i
一种数字式飞行操纵系统,从爬升(或下降)改平的模
, X) g& w3 Q B% I。
( c- Q4 ^ u, h度警告,
% {8 a+ b9 T: F! z3 Z; E当飞机接近或偏离选定高度时,所出现的驾驶舱警告。" v5 ^& C3 V2 Y p% x
高度能力,+ y$ w( E/ F0 {7 k1 y$ V
在给定的推力,速度和大气状况下,飞机能飞达的最大
/ K5 N( X6 Z& ?9 j% V/ ~) Y7 L高度。
' M v2 Y2 ]9 }! D* V% {5 C1 q高度保持(ALT HOLD),( o9 Z5 n1 q9 o
自动驾驶仪或飞行指引仪保持在选定高度的一种方式。
- L) E7 H) n% D,
# ^/ ]+ D& x! {# Y* w3 Y7 J员对飞行高度的控制。
# z/ u) z2 N* Him
- p6 @" D# P# l6 Ha# R9 g8 n2 K. i' e# j
ALTIME8 ~- V2 X) J0 X8 T7 G4 ]
to
( T: U. A I" u; `( f! X3 V, JA0 k3 P+ `/ U3 K6 d6 l5 G$ y: z
m; K/ W! a# f' T/ ?
A( F' ^/ W$ {( a4 }, y$ y
a/ v W0 n, ]/ v5 q1 P8 ^/ P, d9 d+ j& ^
A
0 [, e$ J/ v! F% Y) d4 v% ~& Sw
; T: w1 _- n+ e- Ys
, u0 g4 ?* y) J) A mA
# |2 y; R6 T5 v7 T( `3 Mo
2 V* f9 Z3 d# d5 }3 rALTITUDE INTERVENTION, Pilot control of the8 ~7 l6 d: ~, }/ |, ]5 B) f& P2 B
a
- [: Z# M, v, m _AMBIENT, The surrounding atmosphere.
1 {5 Y2 X: `% V* t4 p/ g7 L备用机场,* w' i: u" E6 }
当不可能或不适宜在预选6 G6 i, `! z; a- e6 ]
机- b9 S, p: K6 y" f' W
高度表设定7 O$ K9 x" M" U# X
高度截获,
* i2 x5 `6 w6 m3 R0 H$ A+ C/ Z& \6 {* s式
% I5 e" @ ?" ]9 j( l* ~高
! @& X: H' N* f2 S! ~/ h高度干预
! ~/ Z( c/ l1 k1 }在垂直导航工作过程中,飞行
7 s4 g$ o( e. t, U* _周围环境(地面气层),4 P5 L) o( i! N; i% j" H) a
物体周围的环境(特别指大气)。
* m4 B4 k! E9 J/ w1 N" M) z2 h英汉对照民用航空词典B OEING
# w; b7 f! \) e4 Y5 }0 fTECHNICAL DICTIONARY 91 r+ E) }1 o4 _. u8 Z
AMBIENT PRESSURE, Pressure of air surrounding an
6 P s" ?3 K! ^& \6 A5 {3 [object, measured in pounds per square inch (psi) .: a; M( }; Y- Z& \$ D" N$ |; B& `: ^
MBIENT TEMPERATURE, Temperature of air
6 A0 \* M: U# W/ A. ^mpere.
7 M& p# u3 ^1 F+ a: @9 v- i( e6 wurrent waveform.
* L( v: q. Y4 Ig an
; W& H6 _1 G$ M8 \- ]nalog signal to a digital signal.0 A( f1 N( H1 E$ n0 h( r
ore inputs
2 | }; t, L; E( a2 E2 t; wf binary digital information and one output. The output
- U1 r2 k) q- I/ Z1 T7 J% W1 only when all of the inputs are 1. The output is 0
4 _/ \' p W; w7 Khen any one or more inputs are 0.5 w3 H. U0 [# G1 k7 ^, ^$ o
面气压),
3 ^" B- b' A# h" c2 K0 \2 _境温度,) c' U+ U; w- C1 l
气温度,用摄氏度(°C)或华氏(°F)来% z8 q- Q- a1 i) f, y. B' y3 I, |
。
" p: H3 _) w& {0 a" p) i电压或电流波形的幅度。
5 Z- r$ _6 a u) r, |: F3 q$ K性变化的信号来工作,或产生连续性变化的信号9 c" }7 R0 V' p" F' _' H6 @
统。
6 E' ]3 A' D) s6 M$ Z2 l将模拟式信号,转换成数值式。
' ~' u0 c: q2 q0 y, {一种有两个或两个以上的二进位数字信息输人,一个输$ @. z8 n# Q8 g0 H% K8 R- V; ~, |
的装置或电路。当所有输人为1,输出为1。当任何一个+ p0 s3 U5 [0 L8 S( A
一个以上的输人为0时,输出为0。
3 W& i x1 c! y9 ?! e1 {& _# ]A; z4 D" ]% N! y5 L. N; \+ X. y
surrounding an object, measured in degrees Celsius
3 p5 V- j( I8 V9 v(°C)or degrees Fahrenheit (°F).
7 o# E- \1 [3 M! K2 N% ~5 EAMPERE, A unit of electrical current. One volt across: A6 z. ^ j8 ~: a9 Z
one ohm of resistance causes current flow of one
2 i+ I( S- Q# e* p3 j/ \a
" }4 k. C2 h- g0 HAMPLITUDE, The size or magnitude of a voltage or
! j! ?$ A1 p3 ]5 h6 Jc
+ Q$ G3 o' ]6 D# {/ QANALOG, Quantities or representations that are
5 j) J$ z" @. N7 i7 G: f# Qvariable over a continuous range.6 ^( d# O/ w2 D9 y: b8 y# e5 M
ANALOG-TO-DIGITAL, The process of convertin0 }- E& b, R/ u. q8 ~
a
9 B8 u4 U6 q# N: c! w3 {9 uAND GATE, A device or circuit with two or m% u- f/ a6 i6 Q, F3 h% ]
o
' c: C7 g6 Y! Ris$ Z: j. Z0 w0 @+ x
w
/ m( E4 p2 T( w7 o& @环境压力(地
9 H; }# ?3 a. u7 Y: f) G物体周围的空气压力,用每平方英寸多少磅(psi)来5 I) t: Z$ Z; d& x/ }, O
度量。
/ I/ q% A+ y2 a! O环
; \/ l# B9 `( G6 {" B/ M物体周围的空. f" q% S1 V1 f4 d3 E' C, P4 r
度量。' u: `5 X, e) i2 H5 `7 V" g# p( I
安培,
2 k( o, [( v" [7 A4 y) {: }+ P电流的单位。
' `' j. f* D6 ^' {, p3 c1伏电压在1欧姆的电阻上所产生的电流为
) F% V2 ^3 K4 R2 r# `; ^7 l1安培
* g8 Z) e) ~' M8 i5 M. m振幅,9 U1 B$ K. C: _' ^* X% ]" A+ o
模拟式,
+ ^% B: n) @, |- y6 B1 x用连续
7 Z3 T4 `& i% C2 X {6 E- f系& ?) Y6 K7 l: }' y1 ~9 A! K
从模拟式到数字式,- T, s4 n7 a2 N8 j5 c! ]9 d
与门,% Z6 u' ^+ r) @( S
出: K' D7 X+ L0 D2 u. f
或
0 }8 y! C" E: V# {0 v$ r) r. b英汉对照民用航空词典B OEING- ]3 V# b1 D' @) X
TECHNICAL DICTIONARY 10" L, \3 x4 n9 _4 l1 S
ANEROID, A sealed flexible device containing air at low
# H2 f4 _ x* m$ j% _0 y: Dpressure, which expands or contracts during change of
% }0 j3 P8 N8 Y: B, iressure outside the device.
! d( e( ]$ X4 N; Q5 Nically% S, P! h: o8 O2 ^: I
r changing the direction
4 f0 @9 ?9 F, f8 Z, \9 _7 zf drive.
% l( |1 E1 p8 V9 p( ]of the wing chord in
2 n9 V9 n$ e: Xlation to the free stream airflow as it moves forward
3 M4 P. o! I+ vrough the air.
I4 u# Q5 w! S) E+ K4 qal axis of the+ \6 b: x. e0 g5 u
aircraft.) @" X* R% u; I' g% e }
胀或收缩。
' ]+ u s' |8 ]( m& _7 X- w# L箱。是改变驱动方向的机械装置。' k9 w2 A1 I* ]* p6 X
机翼翼弦在空气中向前运动时与自由气流之间的夹角。 E* _8 u# t( g0 q1 }* `
。
$ N+ [" u8 b/ g7 ?p+ _- R F- ~* \3 I
ANGLE GEARBOX, A part of an engine, mechan
# {, a7 x: a% f7 udriven by the compressor, which drives the accessory; c/ [- t- P* V+ y% \* d
gearbox. A mechanical device fo3 X. ^; I! n& x/ W/ Y9 U, Y
o5 L! X q, K$ h5 M6 |# ]' N
ANGLE OF ATTACK, The angle
# }2 i3 l7 m; P/ {4 Y; Are# L7 l! I9 y: l+ f9 {! a; H
th M* ?" `. n( S8 r( T- A: H. v* W
ANGLE OF INCIDENCE, The acute angle which the d! P# Y( I% A4 [$ X) s; q( S
wing chord makes with the longitudin
4 K& w. c: N! t0 p( W$ a9 i膜盒,
# s) }6 _) a0 K C4 \内含低压空气的密封弹性装置。当它周围的压力变化
2 j4 V+ y" c8 o5 V时,会膨
4 [. W% e8 t5 S- _3 l( q: h伞齿轮箱,
; S/ b% {, L$ q. z发动机的一部分。被压气机以机械方式驱动,然后驱动' @( K) D) \- m$ o( d) D1 }
附件齿轮
0 r1 s% v8 d; ~% @( \ }迎角,7 A8 @' g6 K! r4 y4 x
安装角,
+ Q9 ?2 r( z7 ^5 ?5 N! M( W: t8 o飞机的纵轴与机翼弦线所形成的锐角
$ c( G4 g( Y3 v英汉对照民用航空词典B OEING
+ I, M/ e( h: B# c0 k$ f- Y0 A+ _TECHNICAL DICTIONARY 11
/ h2 K5 a5 V2 z! r7 }ANNUNCIATIONS, Audio or visual indications used to
! d5 k0 O2 Z8 i, p. u* Hcall attention to an event that has taken place.
1 i7 F# r$ t5 [- o* B" C: C5 s! aANNUNCIATOR, A visual device consisting of a number
6 K7 [' ^- b( v k" Ply.6 d# V: K( E6 M8 X2 H
ANODE, The element toward which the principal stream$ J2 Q. L. S" z0 ` W. K
of electrons flows.
$ ~6 `, _6 w7 TANOMALY, Not normal.
+ Z& N2 S' y9 yANTENNA, A device which, used in conjunction with a
0 c9 J% K& j p% A9 @ btransmitter or receiver, is used for radiating or receiving" F( @6 M; u* x& e3 f
radio waves." Y0 {" N5 W/ F \4 `
NTI-ICING, A method of preventing ice formation on
1 j$ w5 Z9 Z* h: n; Ae wing leading edges and engine nacelles.
$ q9 E& M5 }# ` ~8 _2 v. S8 QNTI-SKID, A system for providing maximum braking% q0 Z/ | d. H b$ Y3 O
ithout skidding for any runway condition. Anti-skid
U; H8 W6 B3 k8 `& s7 Uomponents are part of the brake system.
4 s. A0 f! s/ K0 N告,
/ N) ~* k# F7 I8 r当发生事件时,以声音或目视指示形成的提示信号。5 d' q$ P- y Z4 S/ @
与之有关的电路的现有情况或已存在的
$ Y5 y" a. {! n8 i' d况
* F7 t3 `, P. u, Y- p( H* w$ A正极,( H1 u0 F2 v! ~+ D n( u
主电子流向的极位。
8 y0 R1 R; Q+ v% B. g异常,% M$ A! ?( Q1 [9 O( Q% P
不正常。, ?2 M) A1 X/ ~+ n, [3 i
天线,, d( }2 w( e% g" \- G+ x" c( v5 K! S
一种与发射机或接收机共同工作来发射或接收无线电6 [- G4 C! Z6 O* O
波的装置。* s u' W* E4 r: K
冰,
, w3 e# `' Y3 q1 R _3 a防滑系统,2 S! a5 j6 U& }$ H
一种在任何跑道状况下,都能提供最大的刹车能力而不) L2 U3 U: Y$ n* ^4 [! L
使轮胎打滑的系统。防滑部件是刹车系统的一部分。& ^" A5 y; k R% u4 Q3 a
of lights. Each light indicates the condition which exists
( _ \1 k3 Y4 Z( @7 D9 P% Qor has existed in an associated circuit and is labeled# ~; B# W9 ~. D- S0 |* B$ b' [
according
/ U r. u8 S7 u' |6 Y6 kA. a9 ^1 O1 Y6 J6 y- l( Q( h
th/ @& h3 p$ `0 n* {3 ^
A1 n1 D4 X1 i7 H, V" Z9 r9 v
w' I; [# l( R( N* d
c/ a! U u0 c! ]
通
/ M U. g! k9 `; [. i信号牌,' n& I+ g( u% x, S+ @
由一系列指示灯组成的目视装置。每个指示灯都有相应
9 b8 K$ X. C- f/ r的标记,用来显示
6 j$ x- \( e3 D A0 e' A) |情
- ]+ D; P0 ]) U0 n+ ?" s防0 C6 z! c( P" K) j1 c$ N u
防止机翼前沿和发动机短舱结冰的一种方法。* h h) L+ s/ V- M' {$ R5 j0 a% R& ?" [
英汉对照民用航空词典B OEING8 e0 L' N+ P5 v, \0 v! B
TECHNICAL DICTIONARY 12
" ^2 y5 z L R3 N3 G l) kAPPENDIX, A supplement to the Airplane Flight Manual
0 ]4 d' X' }1 ]6 n- X, Ctained in the basic manual. A$ \/ A$ \* h" c7 N
ollection of supplementary material at the end of a
0 e7 L$ P: b) t, Zook.* b: B1 z; b/ s4 { t7 }3 W+ `6 Q4 G
of the+ H' B) V) \# G; v ~
rsion link on the landing gear.
& [% R, _0 A6 q) u9 H; t& b3 YAPPROACH MODE, An autopilot/flight director mode# b7 q9 ^% p2 C: x5 @& A: }
which is a combination of localizer for roll control and
: n3 E$ K% o- p. Z9 eglide slope for pitch control. This mode is used when full, T* R( V2 u$ _- ]
instrument landing system is available.
, c1 V% k- a; J2 Z% G& BAPU, SEE - AUXILIARY POWER UNIT' w! w+ z1 w! A6 K4 b0 {' b0 z
ARINC, SEE - AERONAUTICAL RADIO
9 s2 u# l$ n( \9 t3 e! ~; }$ a+ W' a% uINCORPORATED0 B4 H! i% }* y) _& {" |
ARM, To make ready for operation.5 B, O6 N0 T5 Z* p
附录,
3 {1 V% s# Q' [' H P- H飞机飞行手册的附件,包含基本手册中未提到的飞机形
% I1 m! g0 l- d7 j" F2 v6 N态的其他性能。是附在手册末的补充材料。
' j" M% Q+ K1 p+ }* u; g2 ]" b顶销,2 L* G1 [! h% J
用于连接起落架扭力臂两部份的销子。
- L5 t6 K6 a# A5 u- f进近方式,
- D) \ Q; V5 O# w- m一种综合了控制横侧的航道信号和控制俯仰下滑信号
0 e) V: ^) E8 k的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系
8 {: ~% O8 M# i统正常时才使用。
: s- J4 u: L* G, ?; u8 a8 Y辅助动力装置,
% Z @: M" c' l3 O9 }& s& Y, T0 T/ o见Auxiliary Power Unit
! u1 P5 \6 g6 Z, U8 Dcontaining additional performance for aircraft9 n: G4 W3 b% e
configurations not con
R$ f: s& x8 V& qc4 M8 X8 X" `" `; \1 I
b6 e8 {+ u! V/ m9 @* j# v; e$ W
APEX PIN, A pin for joining the two sections
6 Z9 q% S' P2 d+ Jto k T0 _6 ~8 H0 O& s
. T& k' e7 b* X/ w) u& ~
航空无线电公司,9 g" y9 `2 F- T `
见Aeronautical Radio Incorporated.8 q9 t- _! X) U! N! ~, t0 r
预位,; y9 n4 O' L* g
部件可以开始工作的状态。
% { l' ^5 \2 h( c* Q; R英汉对照民用航空词典B OEING5 e' Q/ \4 A* J4 ?3 [+ T, V
TECHNICAL DICTIONARY 13( i$ y8 @! z, V& r4 b# l
ARC, The curved track over the ground of an aircraft. u; c4 T# _' X7 M/ S- p4 |
flying at a constant distance from a measuring+ T: d' t b# s) l z
equipment (DME).7 |8 \: h% I; p+ g9 z
in the limits of self-contained system
/ K7 R3 l) c% p. L7 l/ Sapability.5 W) I6 x$ O' |# I" R% Q% `% k
tem for opposing or restricting V6 p& m/ d6 l# w+ K6 j2 Q
ovement.$ ~ B; ]3 ^1 |$ P
SPIRATED TAT PROBE, A sensor that measures total- p! P) u( r" H1 @1 L$ x& R5 W
ir temperature when the airplane is in the air and that! i# O% M3 S% Z- ~1 n0 I5 n+ M1 `( q
easures outside air temperature when the airplane is
Y- l% A' O- H5 J0 z; w0 ~n the ground. The outside air temperature is measured% E2 u& G5 s3 H' n7 L$ v6 U
SSEMBLY, The fitting together of a complete structure
) w* K c! Q, o6 p7 t6 BSSUMED TEMPERATURE REDUCED THRUST, The2 r$ J3 A2 b# N2 [
ATC, SEE - AIR TRAFFIC CONTROL0 Z/ t6 E) V' n) s) v1 x6 R
,/ [0 B% ?. S. l& Z4 f- N( i
系统中所产生的一种用以抗拒
. z9 w' D# J- d4 `( Y( H9 b& _作或限制动作的力。
u& H, V: L1 o头,
1 n: X5 d4 D' A s5 f用来测量飞机在空中时的总大气温度和在地面时的外
# c: c, F) m% r9 h g温度。地面外界温度的测量是利用引气将外界空气吸入
& }, m. h. O! O1 P头,以达到测量的目的。
$ ^$ C2 ~) `3 g9 \ G% m2 A7 z配,
/ G6 S5 z& b! w! ]一个完整的结构或组件的过程。! [# @3 Z; x/ R2 I6 E( J+ m y2 N4 H
假设温度而得的减推力,! [* W3 X( R& n' Q
推力设定值时,假定一个比实际外界空气温6 m V, J1 N. t5 C( Z" `
空中交通管制,
2 t. q D. u/ W) x. c. t) y见Air Traffic Control
% A: m$ R/ ^$ v5 ZAREA NAVIGATION/RNAV, A method of navigation* x3 K& a+ i& }& O4 Y# |2 v+ K
that permits aircraft operations on any desired course; c4 _7 M0 R$ g
within the coverage of station-referenced navigation* j' Y+ t" h4 j/ }# e
signals or with! P E6 b; C7 {" e. A
c
& f3 G- N* E' Y; @! g' o4 UARTIFICIAL FEEL, A force developed in the flight
& \9 k: [, z' o0 Scontrol or brake sys6 T1 }9 T2 M+ f, e+ n" e% l
m
, k: ]: _3 S# |! W$ P: j0 \A* X& c* D1 Q' }- M! Z
a8 f6 H* v5 o$ d, ^9 p# ]9 I! Q
m
6 k ~. m/ a( r! jo) a" x: b! I7 E' X; u/ a
by using bleed air to draw ambient air through the* G! b3 b; U5 x3 ^6 d! e; f
sensor when the airplane is not moving.
$ X8 V) w* C( i% Z+ G! W) _& jA8 N" R5 K3 w+ s0 F
or unit.
! c9 T T& `4 @8 `$ B, c0 W% ?A
5 M# I: ]+ {) Rlower thrust obtained by setting a higher than actual
1 W$ M+ N- [9 s# BOutside Air Temperature (OAT).
5 q' y, n2 V* S弧线,
: w9 H5 _$ U" f: E7 u8 T飞机在围绕DME台等距飞行时的弧形航迹。
' X' Y- v- f/ i y& t5 E4 n区域导航,
; t$ _/ n) J5 m9 b* h, B容许飞机飞行在有电台参考的导航信号或自备系统能; n4 Q2 ]" G$ x# {7 t
力极限范围内,飞行任何预定航线的一种导航方法。
' t+ q) ~- w' S模拟感觉
% N6 X$ C' \ E' F# b) w! _, s6 I在飞行操纵系统或刹车
$ b9 R$ S9 m' p. A% z动
: N8 c* G! q/ C, z吸气式总温探 Z3 _( Y' D R5 j+ d& C
界5 `$ J. |: c9 E" B! ?
探
- h& t" c( t+ [" Q: U装
4 X, V! Y# T$ V组合成
# z. b. N1 n# D1 j: z由' c1 m1 x3 u% J: Y; G
在选择起飞
' Q- ~0 H5 M% |# `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 x }/ a& ~( U3 }8 @. B! `
磨损和维护费用。9 V P7 `" l& g" H7 T
.
& e% }) T- j: n& y英汉对照民用航空词典B OEING; j% f' `+ c+ w. R. p
TECHNICAL DICTIONARY 142 {% M% k h1 s7 O5 e( a9 i9 ?
ATE, SEE - AUTOMATIC TEST EQUIPMENT5 c8 r- ]7 l1 ~! J
ATMOSPHERIC PRESSURE, Pressure of air due to the
) d4 R* C- G. X% b# Zarth's atmosphere, expressed in pounds per square
. W% b2 p. E! x/ sch (psi) or inches of mercury (in Hg) or millibars (mB).
! p3 `! I3 D1 C+ G: ATTITUDE, The relative orientation of the airplane with" _ l' H3 a# [. ~# ^/ \. f
spect to pitch, roll, and yaw.
* H9 Z. Q% e! D* yUDIO CONTROUSELECTOR PANEL, The panel in' v* f8 N, d! Q; s9 l
e airplane which controls and selects the routing of* s$ D" k# d- Z6 l. x; F3 B6 N
udio.' v8 j- r! Y6 L# c& k6 o
UTOLAND, Automatic landing using the Digital Flight
. Y# o# f: O+ E& Fontrol System.! B' ]4 x0 C/ B) r% o
n.1 D* r. a% n: Q. n% p7 `4 x
M, A system
7 q1 P: k6 D" k. i. m& ^omposed of all necessary subsystems needed to guide7 q, Q7 A4 j6 q5 A9 @# U; G0 B6 ?
e flight of an airplane.- x1 G) x+ J! \
EQUIPMENT, System test' _# ~; T, X8 j& L4 D- k0 M
quipment that operates under computer control.
/ P5 [, c4 G, M, m I, a* h8 w装置, |
|