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AIR DATA COMPUTER, A computer which produc
$ y, n8 \/ }1 H' _data information, such as altitude and airspeed, based
/ W, X2 T4 D0 |4 I" hon pressure and temperature measurements.: Z( A" N# ^( U# B9 n
es air% W6 h& D3 T; y6 U
IR TRAFFIC CONTROL, A system comprised of
( U+ D/ v X3 z& }round and airborne components used to identify, track
6 ^" t4 e+ Z' E- L4 m" WOUND SENSOR, An electrical device operated4 h* T3 W# c% {
y the landing gear, which transmits on ground/in air
4 v3 h4 ~) e6 w. g# jformation for system operation in flight or on the, t" S+ c- l5 g. P' F4 Z* ^# W
round.
4 ~! K- }5 \2 e9 e2 w0 ?0 N2 }IRBORNE VIBRATION MONITOR, The AVM takes
* i0 ^# w( o# g9 me signal from the engine mounted accelerometer and% g" P* m' A; g _8 E; E+ k" J
alculates the vibration on that engine.( a& @3 @3 W. ^0 K. D, {
corridor equipped with radio navigation
8 s5 O; z2 L" `2 ~6 @5 ]aids.! c' u. s! x- B. g6 k
AIRCRAFT (or ARINC) COMMUNICATIONS
+ ^: N( U2 f' _/ p- Z& HADDRESSING AND REPORTING SYSTEM, An
- y8 F' b) q" m! |3 raddressable digital data link system which permits the8 P0 u: |' ~: { G
exchange of data and messages between an aircraft
- I: w* t( O9 K2 M, N4 C; _and a ground-based operations center over a radio$ A( i! f* l) ]
network.
$ @5 I4 Y8 t: ]AIRCRAFT CONDITION MONITORING SYSTEM, A4 r% c) R' E; f% ?5 c
system of sensors and recorders to monitor various2 z9 F9 B Z$ D; G$ u+ J
airplane systems' performance and status.6 v& \, t u' d3 C' p- T
机,
6 m- y9 m! ?* s0 V+ @中交通管制,
: E( J, w. r- Q1 a) ^: N/ Z一个由地面设备和机载设备组成的系统。用来对飞机进
, R+ }# t/ r( ^$ d地传感器,/ p0 k! V3 Q& j5 y2 S& [ w
一个由起落架操作的电气装置。用于给空中或地面的飞: X' H2 Z* l7 H: g2 U, k7 K+ j
系统运作传输地面/空中信息。(有些系统只能在地面
' c. b8 ]3 H7 J: i5 R用)2 T) w+ a4 d8 n$ d T" k: g6 S
载振动监测器(AVM),
, ?, t5 h5 X+ m" n; TAVM从装在发动机上的加速器取得信号后计算出该发. t$ x6 N8 E+ s" H% I) K6 v+ a
机上的振动。4 ~0 l, g& h+ Z' r
式建立的控制区域,内有无线电导航设备。6 T# S7 |3 K! _$ e& E
飞机通讯寻址和报告系统,. z. o/ q ~# e- J( p" a
有种可寻址的数据通讯系统。利用该系统可使飞机与地
8 {1 S) Q3 C# D. Q- W3 i1 m) J3 K面操作中心通过无线电网络进行数据和信息的交换。
. q" x; W9 i0 N8 h飞机状态监控系统, u/ ]9 E, V5 ^% ?$ y A- H+ w
一个利用传感器和记录仪对各种飞机系统的性能以及
. s2 ?/ S+ z5 K2 R* H状态进行监控的系统。3 O# C% S E; k
A
* c3 J) a' Y- j* ~g
) |7 y8 K) E. M, j2 R; E5 mand locate aircraft.
3 Z4 F! X9 ~# ~' R1 g& PAIR/GR
d$ v, O8 e- I0 Z; e2 {b# |' W0 j% ?5 ~ u/ c! L! o' j
in7 C# A. l2 i& Q
g
" w s# x9 W4 {- ^- c. U1 W) Y: \, mA( G% X: \# }4 V* z2 W' c4 C
th9 X! y8 r" d# ^6 n
c
$ i ^; ?5 `) C' ]$ J! H3 ]- xAIR WAY, A control area or portion thereof established
& X0 ?" g5 o6 ?/ Y" q/ Hin the form of a
+ I, K! p& @" _1 Q' o- P大气数据计算3 ?" c# @! N, M1 Q& Z; ]5 m' }9 I
根据量取压力和温度而产生大气数据资料(高度、空速
9 n/ O2 h# F; z等)的计算机。7 {7 Z) \$ Q* P6 o4 A- S7 m8 s
空
1 e( U( b+ B7 s$ y2 T: e行识别,跟踪和定位。
! ~: o* S$ P) p0 h1 Y% e3 w+ t) }空
1 A; k2 o! y: u* c1 Y! S机
1 g1 N" y% c" @4 G: i使
+ r+ a' a, X& q A机
9 b$ G' Y1 K7 o6 [$ p动
2 x; q3 ?. j0 ~4 t! z航线,* y7 ]" f$ f, b$ w- r: }
以走廊形
; Y% G/ w0 _$ U/ c英汉对照民用航空词典B OEING P4 N) Z; o/ v
TECHNICAL DICTIONARY 6
3 l& \% k; |7 N: p/ p% FAIRFOIL, A surface designed to obtain a useful reaction,
8 P! r) L6 G3 ]( n6 Y/ U* ]7 zsuch as lift, from the air through which it moves. Wings,2 e4 P C1 r; t# B4 i* f# W
stabilizers and control surfaces are airfoils.
- M5 [" g9 `6 |; R; u: g7 BAIRSPEED (IDS, TDS), The speed of the airplane5 b4 i7 c. W3 h8 u# @/ Q4 B- b& T. S
rough the air.: z5 Y" F3 V+ W# i' G0 M& W- B1 ^
D INDEX, An adjustable pointer on the
& `5 k" ~ ~& r. c( O4 rirspeed indicator.
" G1 @+ E: ]0 h& P. q1 nand legal ability
% T- K; @3 z D6 K, X) `: a0 qfly.
+ g! v/ l+ n/ n5 u% D6 zm, for example, the procedure for finding the
2 x: D- y/ N' l9 G9 x7 n \1 Pquare root of a number.
- O6 @% e; ]9 B* P9 g2 \y( N9 h$ d* H0 `7 \
re, wind,
; X- x! j' M; ^9 d, Y8 ?and aircraft flap setting.
) g! _1 d3 o9 _; _1 e' k5 K0 S是翼面。! O6 u) T" b7 [! w; K+ x
速,4 {" }0 x7 ~# H
飞机在空气中运动的速度。
/ M8 f: K8 L1 |* V( J! V* a6 u9 E2 A,8 o, R% Q; O/ ], |
在空速表上可以调整的指针。
' [; M. b6 p* J8 s机械飞行能力、和合法性的飞机状态。6 w# j7 Q$ F; ?6 i: n
一步一步的解题方法。例如,计算一个数的平方根的步
8 h' o I: \5 m) D$ d- U8 i。
5 m* R5 M4 {7 {$ V9 T7 e能- ?9 M; s8 b f" ?* D6 Q& x
资料的法定文件。% R8 F! H" w' X4 ]9 \
翼位置成函数关系。
& q) M+ x H1 O1 ^th/ I. |& a. w8 ^" m( P, T
AIRSPEE$ @! J2 u4 d: v
a
# F: P K+ M9 y3 KAIRWORTHINESS, The condition of the aircraft with% J5 e; m6 x. A. b& q. P
respect to its aerodynamic, mechanical,
6 E4 @1 }9 l6 D8 A$ w# Y# |% s: j: hto
K& E* w |2 @, ?ALGORITHM, A step-by-step procedure for solving a" O: u4 Q" T2 `9 {/ n
proble' {, _) O; x2 } Q- N
s) p6 Q- C- p* f
AIRPLANE FLIGHT MANUAL (AFM), The legal
$ p$ |8 K' L7 r. W. C% {document containing performance and operating limits,: u2 ^9 F5 V, x" w% B
operating procedures, and takeoff and landing) j! _ s- k0 K! t4 R
performance.8 S, ^( p2 C2 N- h. i9 Z
AIRPORT ANALYSIS, A comprehensive set of takeoff' u1 N A/ K& a1 @, o* ^9 N
weight limitations for a given airport runway, generall
$ T% u2 I; p: o& b4 J3 apresented as a function of airport temperatu
/ C0 g8 U2 X' {+ r翼面,
8 F" C. x* u- \% i: o0 K7 m2 G( o4 N) Y用以从气流中获得反作用力(如升力)的表面。机翼,; o: h3 K8 g7 j5 Z3 t
安定面和操纵面都
& T! K' O& n: s1 n' D空( V3 a3 k+ \* ?9 e8 f
空速指标
- s* }% W% ?" ~+ O N适航性,- e% V! y% u* l, E) X& N
有关气动能力、
& s2 {! i- X5 C" }7 }7 M演算法,2 _8 _4 @! n, E) u6 B6 O$ h2 J
骤. e8 F! q, _5 B& a1 {8 i7 ~
飞机飞行手册(AFM),
3 s: O6 B: m+ e/ D包合性能极限,操作极限,操作程序,起飞和着陆性# l: T1 D2 K( L
等
* v7 ] Y* y) k5 F/ O2 l/ x& X机场分析,
0 N0 n6 n1 A3 z% y4 s' U一套针对给定的机场跑道的详细重量限制资料。通常与6 P6 C ]8 v, z6 H, o
机场温度、风、和飞机襟
8 q6 M5 C1 C6 O) K6 a2 s! S; X7 i5 h英汉对照民用航空词典B OEING7 ?, b5 a( L# n( o3 n' }. e
TECHNICAL DICTIONARY 7$ m# D1 }1 J4 S5 H; G; l& R4 u
AIRSPEED BUGS, Adjustable pointers on the airspeed8 t7 V) L5 F" q% H; B' l3 A. Q
indicator.
/ S) T/ B2 G0 P& \- e5 ?ALLOY, A mixture of a basic metal and small amounts
& f$ g7 `- m7 ^ w+ E' v% vf other metals to change the properties of the basic
4 _+ }! A) b2 D5 A# u; y" eetal.8 |6 D. ^) [2 k( {+ Z& _( ^! A
Minimum airplane speed.: z9 C8 B) a& B2 |1 f$ J+ N
e of2 ~3 ?7 K9 [% O) I, J
itting airplane angle relative to% Z3 u" h' Q: `, K O) X) J
irstream for the stall warning system.) F0 b& Y, v, j/ f* D ?( V: a
another.
2 B( X& h; N2 |6 O) w8 X `LTERNATE , An additional airport selected during2 F- H0 u, ?/ d1 H
,4 v- {2 d9 B: J- @
合金,
" @3 G' t& |; l% P( x1 H在金属中加人少量其他金属,而改变其性质的一种金属/ { c1 W9 ~' Z1 B K# \" M
合物。
7 ?4 V% H6 a6 S, `飞机的最小速度。/ @& ~" Z$ I, k3 D6 ?
速警告系统传输飞机对0 \2 ^6 b& {% O4 |& T
流的相对角度。
) p- J0 r, V. b$ q由一个状况改换到另一个。$ T" Q+ f6 i9 d) K& }
降场,2 m. A' t% i9 w/ W
划时,除了目标机场之外,所选的另一个机, A; P, ?$ o. z) W: w; V0 r! V
o
6 ^ a, _& ]: B( @7 F, Tm3 \0 ~! F/ x' w4 \ C) i7 g% Z6 `1 b' X
ALPHA SPEED,
2 ?8 a# F. z$ t& F9 gALPHA VANE, A small moveable airfoil on the sid
2 `) h# K( f% ^6 F. D9 v+ N5 \the fuselage transm4 a7 K, q/ z2 i
a2 J$ l" i! t2 @; K$ T0 j, ?0 A
ALTERNATE, To change from one condition to- n4 h% t# T( D F1 K
A
! D. h0 M# \' @' A2 h Kflight planning, usually near the destination airport, to be, W1 r6 I4 o! [/ c% X9 [) [/ i
used when it is desirable to divert from the original f6 c9 v& D8 U) Z! L
destination airport.: Y, D R" k5 J% G `
空速游标$ \ I* ~. t4 }; b- u) }/ n
空速表上的可调指标。, d! z3 g9 ]: b. c" h% R
混
9 G% Z) a9 w) Q9 [* W迎角速度,0 L% b, O% ~% I! W _6 N8 x
迎角叶片,
0 O7 r7 z% p! P; R位于机身侧的可动小翼面。为失
' l* {* I9 x0 |$ M气
& L5 \9 E" O: j+ R% x9 J1 o交替,
0 {2 m5 D# Y3 C备) _9 ], v5 K# @/ U2 k2 d3 x" T
制订飞行计
$ Z$ T' q2 A$ x场。通常在目标机场附近,以备不去目标机场时,改降之
0 E2 x/ j: O/ o, J& e5 m用。
- C/ T8 u/ U8 F5 I英汉对照民用航空词典B OEING
: {4 _& r/ C; \% \6 w/ g1 CTECHNICAL DICTIONARY 85 E) M0 \# t0 j9 v5 n
ALTERNATE AERODROME, An aerodrome to which$ C8 C) x; [, \+ I0 U, L
an aircraft may proceed when it becomes either
6 }0 Y8 `/ ^1 ?/ i4 B1 gpossible or inadvisable to proceed to or land at the
1 {: g, S% h. k8 serodrome of intended landing.
" D" E' h+ z% r5 O" \TER SETTING, The adjustment of the altimeter
4 q& O) P/ t; j& c3 haccount for local variations in atmospheric pressure.
- r8 o0 v5 I( T* ?LTITUDE ACQUIRE, A digital flight control system
% O1 R1 X2 J: ]+ l/ Z# e8 wode to transition from climb (or descend) to level flight.* F" b- Z1 O+ [7 R
LTITUDE ALERT, A flight deck alert occuring when the5 b' y n; R8 S& L
irplane approaches or departs a selected altitude.
) K: K! g5 r; G1 ELTITUDE CAPABILITY, The maximum altitude at
% f% d1 h0 V! M* |$ Rhich the airplane can be flown at for a given thrust,( b, P3 J- ?( k! ]0 _
peed and atmosphere condition.: C$ t( @' t8 a9 v
LTITUDE HOLD (ALT HOLD), A mode of the autopilot7 z- A4 @4 N6 ?1 o! A1 S. ~; u8 W3 J
r flight director to maintain a selected altitude.* ]8 f' Y2 \5 L# P, X {
irplane's altitude during VNAV operation.9 G; N# T& `! ~
机场着陆时,可作着陆使用的 n* O& a/ _9 n4 c5 u- `
场。$ o9 t J+ {+ M% z
," C+ }% `8 G" x5 i3 A+ v7 [
根据当地大气压力变化而对高度表所做的调整。
) `2 J+ @7 c% W+ F一种数字式飞行操纵系统,从爬升(或下降)改平的模. l: y3 s4 N/ p c$ i# ^
。" i" @ |! A1 Y2 _5 A
度警告,
$ A& Y! L! w* b9 ~! d当飞机接近或偏离选定高度时,所出现的驾驶舱警告。+ |/ p. P$ i0 }$ F }
高度能力,
9 J3 V/ S$ _! i0 q) w在给定的推力,速度和大气状况下,飞机能飞达的最大
' P! U( W* J! h. T0 i- k高度。
2 I+ X. E0 D" W3 X高度保持(ALT HOLD),5 \1 M0 s# [) P) S+ i2 `
自动驾驶仪或飞行指引仪保持在选定高度的一种方式。
2 w4 T3 P1 L' [: I,0 B5 {. ^" H8 `$ P" W5 A$ g) q
员对飞行高度的控制。1 [3 l) d3 U+ j9 ]
im; T: ^9 \/ c9 }4 a9 x9 \
a
[- A; M# j6 u' x# FALTIME6 ]7 n2 D* [+ k1 n( d
to' }$ r. J5 h: d& B8 E: k9 q: X
A. \* y. Z0 {2 d4 T% @
m; g4 r' u e2 z1 z6 x! o
A
# |3 G7 w U% z! R1 m1 @a6 M6 N: O f/ v
A( p: X: G! e$ U% E% a! j% P7 \
w! W0 ^2 W0 z& U7 v( Q
s% A/ Q) A- D+ U, w
A
" n& q% v8 x I! \$ s8 X& K# ao. q+ A- ^' }& G! k8 E$ i
ALTITUDE INTERVENTION, Pilot control of the4 a, Y# d6 H" l* c9 \. ?% f
a* m6 M( ^5 X3 n+ J3 |% V
AMBIENT, The surrounding atmosphere./ j4 V& N1 i- v& O
备用机场,
1 A$ d: @8 R: @$ H; O, x当不可能或不适宜在预选
) A& Q5 I, @" s0 T4 R机
! d0 w- ?- e9 v8 X) f% S高度表设定
( {: T% ~, a( [% P$ }2 d! ~1 b; g高度截获,
$ F. A/ |" y$ t; K8 |2 ^式4 ?0 C! d9 a) Y* H7 ?% k* v8 K
高9 ]/ R9 {/ L( [) A; R r \
高度干预3 t$ X- Y7 L- B5 m4 b/ V
在垂直导航工作过程中,飞行
; e, p) [! Q$ ?& W2 G周围环境(地面气层),1 s$ ~+ ~: H9 h8 V; z/ ?/ H5 Z4 O! L
物体周围的环境(特别指大气)。8 ]( ?" N7 i( U" x/ N5 b4 ~
英汉对照民用航空词典B OEING
|/ [ h6 U8 O& bTECHNICAL DICTIONARY 9
( w, A% r4 \. T$ }AMBIENT PRESSURE, Pressure of air surrounding an
2 S: F! t( s/ X9 H- e! Zobject, measured in pounds per square inch (psi) .$ U0 A9 P4 a6 a5 ^
MBIENT TEMPERATURE, Temperature of air
; r# R; C+ i% c3 g1 mmpere." u/ p* ]* B* X: {* n8 C! K9 @
urrent waveform.
& Y9 W1 R5 V' e/ F* jg an: |4 Z) c. @) n3 C& K: y7 ?
nalog signal to a digital signal.
* S8 B" R9 H' oore inputs
! P6 R( l' l* t) g9 x( l8 Df binary digital information and one output. The output9 G7 l9 @5 P, |0 |7 |5 Z) X; c
1 only when all of the inputs are 1. The output is 0" |$ l) S" O! }) b0 G3 Z4 C' s1 D, i
hen any one or more inputs are 0./ Y6 W2 ? D$ G7 H: D, {
面气压), ^, E- O4 W7 s1 F% F4 ?! J$ @5 |
境温度,7 Y+ v) m' i2 `$ i# k' M2 q' O
气温度,用摄氏度(°C)或华氏(°F)来
0 S0 k7 D" Y3 U$ k7 u8 \3 ^' J; L。
* ^ o" F6 M `( d电压或电流波形的幅度。/ d- I& b: h- t! ]0 a$ c- ]9 g; l s# S$ j
性变化的信号来工作,或产生连续性变化的信号
3 |; n4 V0 t2 U, {# f! I统。# A! ]) O0 d! Q) d! r' `
将模拟式信号,转换成数值式。
3 [- j5 \, j* U2 k: J, c V% |/ L4 w一种有两个或两个以上的二进位数字信息输人,一个输
. k0 B( X' \( q1 U) @的装置或电路。当所有输人为1,输出为1。当任何一个7 C; f& i# }6 j
一个以上的输人为0时,输出为0。) _" N, N) G0 P# h
A& e: P( u. A9 ^ W
surrounding an object, measured in degrees Celsius
[$ b/ n0 u& [7 |) f# O2 c(°C)or degrees Fahrenheit (°F).! W/ a7 w. w/ C' u3 s" U$ }! ^
AMPERE, A unit of electrical current. One volt across ~9 [ v$ N3 @$ d
one ohm of resistance causes current flow of one0 g: J* S* r" {. I, `7 N
a
2 E/ T/ B1 m8 X' K: ^; X' _! ]7 ^AMPLITUDE, The size or magnitude of a voltage or# n0 K. j' w+ S A. Q! |: u# C
c9 G. L8 ]: |, g' R
ANALOG, Quantities or representations that are6 N; _% A, |) | C0 Y
variable over a continuous range.
7 y9 m, o% i" h/ K$ UANALOG-TO-DIGITAL, The process of convertin' t9 L9 ]! o9 T/ q
a% l) G4 g/ Q" F
AND GATE, A device or circuit with two or m
$ _( v/ [! ]" G/ y2 Mo
) x8 y3 [; i$ B+ a% w3 Fis8 g3 S2 }3 S, ~8 b3 r
w1 k8 \0 U* Q0 L X$ |& P1 t, F
环境压力(地 E9 g9 \% C+ r9 j
物体周围的空气压力,用每平方英寸多少磅(psi)来& n. q) ~. Z; V9 w/ R
度量。
, T1 Q* x0 t1 r: Z2 p环
5 d2 F% r; S# ]# ]' B$ M/ E物体周围的空
& @% x A0 x; Z/ i度量。
5 C4 ]6 I, j' U. Z: t9 W安培,
# _% ]9 e5 W9 E3 }6 t$ X电流的单位。
$ E2 T T% T' [1伏电压在1欧姆的电阻上所产生的电流为4 K' [% b; G: x8 @% o' x, y1 N4 v! F
1安培
1 K9 e) `6 f! W- v& ]振幅,
7 X4 r0 X" K3 j$ _3 J5 b7 k模拟式,
5 Q! ~! d0 t) O+ ]8 U- f5 w用连续) T0 A% @& Z6 x+ A4 |
系
5 e& O5 i% V9 ^2 g( u从模拟式到数字式,3 [, u8 r u! q g' @& m
与门,
$ M, V% \& n' j, w出
' R( q; O. |1 G" w3 q! U或
6 h2 ?; Z3 A% A/ I8 a3 V( H, y英汉对照民用航空词典B OEING
/ Y3 h0 X$ M# E3 L0 STECHNICAL DICTIONARY 101 X' ^, r. }1 d' p& p7 [5 q* ~
ANEROID, A sealed flexible device containing air at low
( O( D& Z2 i' Q: X: h. t" Tpressure, which expands or contracts during change of
2 ~% k o& L7 F& Pressure outside the device.5 @% M, L; D. P% p z$ x
ically$ w" K$ q3 I8 j: X4 Y* q& T" Q. V, g, a% r
r changing the direction
5 n; q/ g# ~' S) q, xf drive.
3 |( b' e3 n2 T! b9 q% Dof the wing chord in( }! ]1 J' {$ V: }5 R3 D( b. @
lation to the free stream airflow as it moves forward
9 d e# z8 k3 g, orough the air.
0 V) [+ U7 V& M- t7 V$ ual axis of the
" a2 a1 M+ a: Y! {) A( x4 A- waircraft.' M, ~- N# {0 m- n5 \8 k2 i, x
胀或收缩。
# X- `- T: P. ^& e7 q7 c6 T箱。是改变驱动方向的机械装置。 C; K% X ]: G# w
机翼翼弦在空气中向前运动时与自由气流之间的夹角。
, y( R4 A% }% H' b+ l; V。% |; S: d9 f7 w- _0 F4 n6 {6 H
p
1 z O( v4 ^% q/ U$ ~; iANGLE GEARBOX, A part of an engine, mechan
2 T9 }0 B4 c! m. ~/ M% Ndriven by the compressor, which drives the accessory8 @# `( `2 k# D ^7 n
gearbox. A mechanical device fo3 r! G/ b' h9 E7 t9 Z7 s1 y
o& l% m# n4 H8 |7 E
ANGLE OF ATTACK, The angle
6 o- i8 A8 m; f* Vre
* y, Z6 z- X5 `3 `( W9 @th
* g6 {3 |- j' N& X; B) p% IANGLE OF INCIDENCE, The acute angle which the' g- _2 \8 f' e A7 X& A* W
wing chord makes with the longitudin
Y4 P4 ~7 m1 }; n膜盒,
- K' U' O! G, j0 T S2 R& b7 Q内含低压空气的密封弹性装置。当它周围的压力变化, o: \7 S5 t6 [# ^0 B3 j0 X5 c
时,会膨
) {* X* q, x/ ~) ^# ]: q- ^伞齿轮箱, V6 K1 V, ^& _4 P6 f U$ y( j& ?
发动机的一部分。被压气机以机械方式驱动,然后驱动
9 H( ^8 n7 n, ^+ g9 n6 I T附件齿轮0 @, T" ], N6 i
迎角,0 t/ s/ I6 \/ _8 i) `
安装角,/ ]" x2 ^+ F0 E) T: C
飞机的纵轴与机翼弦线所形成的锐角
9 e$ X8 n" h' y+ c5 _. @1 u2 c英汉对照民用航空词典B OEING
8 V: C T- Y5 f- u/ CTECHNICAL DICTIONARY 112 u z0 _& N9 Y6 o, x% z& ], Q, w
ANNUNCIATIONS, Audio or visual indications used to! W* u4 h: V* u) |5 a t
call attention to an event that has taken place.
+ c: B: B7 C8 X/ M( t$ Y5 Z1 s: w: ^ANNUNCIATOR, A visual device consisting of a number
" u: M0 r ~- X5 N$ f" h0 Lly.
8 T9 x2 E! }2 G6 i8 H; a0 V6 zANODE, The element toward which the principal stream3 j( |& D# N9 Z- K# x
of electrons flows. M. A4 D$ B5 J B: d$ L
ANOMALY, Not normal.0 T& ^( ]. q2 I- [
ANTENNA, A device which, used in conjunction with a
) X* H0 o3 h2 n, m' ?, Btransmitter or receiver, is used for radiating or receiving
- ]3 t( u3 r# Z0 h! i# wradio waves.( V; S/ d" l" X& C
NTI-ICING, A method of preventing ice formation on
5 o" r# @# n- R- x9 k0 ~e wing leading edges and engine nacelles.8 m: M: {! Z; r7 }
NTI-SKID, A system for providing maximum braking& G. x/ A; @4 ^& Y0 D2 S8 b R
ithout skidding for any runway condition. Anti-skid
% [! t$ l0 `9 |) p x0 i, Momponents are part of the brake system.
3 M! c4 m8 X. ~/ ~" P% c告,
. @, Y4 W$ K( K当发生事件时,以声音或目视指示形成的提示信号。* o/ M7 Q) n! ?1 E( |( f. {1 X( w
与之有关的电路的现有情况或已存在的
s. i/ q9 V! s. E' G况, w5 }. X. u& ]- g
正极,1 Z5 A9 I; k8 v% _
主电子流向的极位。& D+ z% Z8 H* [
异常,
! }/ G9 h o" k: g4 K) n不正常。
! n7 f+ |/ W4 R) E5 N& t4 u9 L天线," W, r8 g! L5 N5 m3 A& e/ N
一种与发射机或接收机共同工作来发射或接收无线电' {9 y P% k- Z4 |: g
波的装置。, T8 Z6 J# y0 z" l0 M! x
冰,
+ p* @/ J b; ]2 u% k0 z防滑系统,
" b5 x* E. Y% x, `8 o& `- z一种在任何跑道状况下,都能提供最大的刹车能力而不
9 r5 ?6 v7 L( i6 P1 I使轮胎打滑的系统。防滑部件是刹车系统的一部分。- H; o$ m9 O8 C2 G
of lights. Each light indicates the condition which exists
0 c) j% f' ]9 l" T1 j2 J! _or has existed in an associated circuit and is labeled
6 }# }, p* E* g% U% Y# taccording
6 U4 b4 ~( ?0 k- a, w0 w% H1 W& ?A
+ j {1 n+ Q9 O/ W( mth2 r' p: k$ Q% X+ |. J5 g' P3 P
A
' [; ^, R8 j: h' E8 pw7 U. t7 t, ^ S% _0 F
c1 p, \ F) I0 n9 a+ P2 C, b) K" H& Q
通, n- e5 t/ C) ]% ]: T6 t0 v, G: _* Y. I p
信号牌,
6 v# G$ `" g/ g9 s9 Z7 f4 W由一系列指示灯组成的目视装置。每个指示灯都有相应
- Z, l, k, b2 P7 ^6 `的标记,用来显示 X% b8 W0 a; I8 a9 w
情
4 W* V/ Q3 E3 T4 w防
7 P' b7 G5 t0 e) f3 ^$ W6 I/ E防止机翼前沿和发动机短舱结冰的一种方法。8 ^. F4 Q4 r! y5 W
英汉对照民用航空词典B OEING
) _ a, Y+ c% a4 B6 m0 FTECHNICAL DICTIONARY 12& j# \& T9 | I! d2 n/ w
APPENDIX, A supplement to the Airplane Flight Manual
1 P/ z% s2 v* D% ^tained in the basic manual. A
1 `+ l$ E) q+ Gollection of supplementary material at the end of a+ u& l, u% i t% n) a; e" C) P$ w& h
ook.
0 ~' I! F: D" s7 _- Bof the
; | z: X2 i2 ]: Z$ h: {* Srsion link on the landing gear.6 u: C" J3 J$ f1 c
APPROACH MODE, An autopilot/flight director mode
' A; b! J, z" R8 Mwhich is a combination of localizer for roll control and
* n/ ]" x' g! T! K' L8 _/ Vglide slope for pitch control. This mode is used when full! R# C1 p, {3 t2 z* s5 ]. f4 l9 E
instrument landing system is available.6 s+ m$ e% e: y& l/ w
APU, SEE - AUXILIARY POWER UNIT
3 I4 e4 c( D+ _8 h I# @ARINC, SEE - AERONAUTICAL RADIO: {: J5 W& @+ f$ _
INCORPORATED( L2 D8 u! \5 b) h3 Z
ARM, To make ready for operation.
9 ?8 z- Z. v4 H3 S附录,
+ u: i0 q- P8 W$ L6 w: N飞机飞行手册的附件,包含基本手册中未提到的飞机形
5 u5 J: f( y/ K6 W7 o态的其他性能。是附在手册末的补充材料。
# \% Q3 V* L9 z8 r. V顶销,4 n2 D& O% X6 K: h$ _7 c; k+ j& _# w
用于连接起落架扭力臂两部份的销子。
6 P8 w* h$ P Y; A! ~/ O8 r1 s进近方式,
" L7 B% ^+ d3 d一种综合了控制横侧的航道信号和控制俯仰下滑信号$ |, p2 W* \2 _
的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系6 R1 A6 d- z0 w# f: Z T3 k
统正常时才使用。
6 S) T o3 {+ m辅助动力装置,
F: S/ d" s1 l7 M/ q+ Q% F T7 W- J见Auxiliary Power Unit2 w* J: f; e2 m% B) n
containing additional performance for aircraft8 n( h) w. B! Q7 ~& P% u
configurations not con- [0 u# S! g) t+ p) ^8 \( ^$ V
c
7 E { R$ l' k& G3 \9 Db
( T$ E ]6 e1 _; g# EAPEX PIN, A pin for joining the two sections
1 k; E2 C, r# T+ \to: z5 _+ [1 Q7 k
.
& J% N$ V$ R0 H0 [2 @* S航空无线电公司,
7 M t& a+ [0 z9 N5 t见Aeronautical Radio Incorporated.
& w. W7 w6 I p6 c& Q预位,. ?6 }9 c" ]6 C5 \( j, i$ i. B
部件可以开始工作的状态。
" d& K% ]; Y/ W' b英汉对照民用航空词典B OEING
! q$ f8 y. L8 M0 ~' I* Z9 j' Q uTECHNICAL DICTIONARY 132 c2 C4 Z6 C1 I) j# N
ARC, The curved track over the ground of an aircraft, Z3 f- [% L* N! t
flying at a constant distance from a measuring
) a) E) e5 Y/ \equipment (DME).+ a0 ^- D9 U% ^$ I4 i6 l1 @- s
in the limits of self-contained system
/ G% k: ?/ S' g4 [, gapability.
2 O- ^! v4 k$ Utem for opposing or restricting: p9 Q9 }7 C0 D9 r& ~1 a% O, a
ovement.0 m6 w6 @- T' Q
SPIRATED TAT PROBE, A sensor that measures total
* i9 n" E" l( k$ vir temperature when the airplane is in the air and that
* U7 y$ [4 n5 _ Reasures outside air temperature when the airplane is; y% a* j t' F! v$ C' p8 n2 e0 r
n the ground. The outside air temperature is measured2 R: h- O; z* W) V
SSEMBLY, The fitting together of a complete structure& }6 Q0 {9 \, i4 L& s7 ]& g
SSUMED TEMPERATURE REDUCED THRUST, The
7 y( ~+ h! O& R; Z) `0 SATC, SEE - AIR TRAFFIC CONTROL
6 ]8 X. K. Z% h8 V7 U) a8 ~! [9 w/ g,- _8 e5 x3 ^7 R$ }5 o4 x S
系统中所产生的一种用以抗拒
! n! @7 h) L$ K: Z7 j作或限制动作的力。
8 M- p+ a% ~4 d' K头,) W& n9 |# _: {8 c
用来测量飞机在空中时的总大气温度和在地面时的外
2 D( e5 c1 Y- v2 y温度。地面外界温度的测量是利用引气将外界空气吸入
- j6 U5 J* C9 P' f头,以达到测量的目的。6 k, Q1 O# C5 \( N
配,' ^' } w3 q5 [0 W/ T
一个完整的结构或组件的过程。
% n& f4 S3 |" x, S8 i4 V& `假设温度而得的减推力,
; {8 S/ r2 j3 e/ B推力设定值时,假定一个比实际外界空气温
+ }; z- ]% L$ m空中交通管制," ^0 _ Y* z& B7 V5 Z8 L7 L4 c
见Air Traffic Control
$ N# y) W) v6 G( MAREA NAVIGATION/RNAV, A method of navigation
1 f. ?, [) Q9 ^5 X6 I( G# Hthat permits aircraft operations on any desired course
# A' U G' w/ n) P, |% ewithin the coverage of station-referenced navigation8 w2 Y5 o9 b9 G$ M2 ]9 }
signals or with1 V) q+ N' W: H
c
$ X; a4 \& q% J' W4 g6 bARTIFICIAL FEEL, A force developed in the flight' y- Z5 k% a" K; ^
control or brake sys# _1 z8 b* H# M9 V) F" k
m
' `+ L& M3 n I) I/ l- s7 DA( u3 u# e7 v- ? Y* s7 l
a7 @5 h5 T N& K5 M+ J
m
" }! F4 h/ L$ p! x4 Z. Mo
4 \+ K* t8 I6 m0 L0 Jby using bleed air to draw ambient air through the
% o$ ]3 y2 Z3 r9 y9 U5 Vsensor when the airplane is not moving.& m. ]* j- W8 @
A+ e: B% `& b+ Y9 h! G- h
or unit.% W0 c, X, ~# h$ `- |; u
A
) F: w6 _% d5 V) x) B: {) wlower thrust obtained by setting a higher than actual! W+ j& q+ @& _( D$ X
Outside Air Temperature (OAT).
! q* ]+ Z' O, R( q. G+ u8 E弧线,+ t1 P) C) p; ], g' H/ A2 R
飞机在围绕DME台等距飞行时的弧形航迹。% q1 B$ w0 @* {. l
区域导航,3 H2 J6 B Y: H' ?, j
容许飞机飞行在有电台参考的导航信号或自备系统能
! ], K X9 \# I. X7 }2 Q( I$ [力极限范围内,飞行任何预定航线的一种导航方法。6 F6 {2 @1 x. V
模拟感觉
! F2 n7 v4 C A/ \6 T在飞行操纵系统或刹车9 I( B' w' T T: R
动" N6 ~9 F. i& j' L4 d% g! m- h
吸气式总温探% ^9 h- @$ p$ A/ X" ?
界
7 h2 C! S: e- @2 e, U3 d探: H- ]' g% A- ?5 D4 S
装
( j% s2 m2 d w2 X3 s i组合成
3 U U1 p: W) d& r. y' K由
1 N, h! s, s# h) E' L在选择起飞
4 u# p1 D; A8 q( x* L/ Z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 U' |8 }; t& d! |' g4 g6 o6 p6 e磨损和维护费用。
$ Y3 k* ^# ^; ].7 e: v& Q* R2 `; \2 q2 J
英汉对照民用航空词典B OEING- e1 ]$ J9 w3 r6 Y- P$ k" ^1 h
TECHNICAL DICTIONARY 14. I O! l4 Q5 ~1 ?9 A7 O
ATE, SEE - AUTOMATIC TEST EQUIPMENT$ z' o; q9 A' ]% J) d1 z/ L
ATMOSPHERIC PRESSURE, Pressure of air due to the. b. X+ _) y" C5 A& M* @
arth's atmosphere, expressed in pounds per square
* E( L( k* S* r9 Xch (psi) or inches of mercury (in Hg) or millibars (mB).2 e3 A) X2 P& L
TTITUDE, The relative orientation of the airplane with
) K% l9 d P3 A% q! A$ l2 G Aspect to pitch, roll, and yaw.
2 p. z* R7 |7 B* X- A/ l6 QUDIO CONTROUSELECTOR PANEL, The panel in
% I: u: f$ u6 g1 Y# R, ~. E; c9 Ne airplane which controls and selects the routing of4 K9 {9 s. d* v( `- c
udio.+ p7 K4 e2 A+ Q/ h6 c: B. o) x& v r
UTOLAND, Automatic landing using the Digital Flight
1 V# G) G: \' F( f' aontrol System.6 n3 K$ \" ` P5 E8 _2 T2 C- _
n.
2 G5 E. F& x Q2 p* e- o7 O. tM, A system
7 U- j" J# d( ]5 [omposed of all necessary subsystems needed to guide W7 e8 D+ k2 w# w/ g" d* q
e flight of an airplane.7 b0 V E8 ^' `6 z; A
EQUIPMENT, System test
4 ~1 D2 N# J" {/ qquipment that operates under computer control.
7 ?8 ~6 @; _+ O4 O/ U装置, |
|