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AIR DATA COMPUTER, A computer which produc
) ]& e+ A5 [1 i! f7 \data information, such as altitude and airspeed, based
- V" s+ b/ Q( B- Q5 w- ~on pressure and temperature measurements.
* V+ M" Y4 l, \5 g8 zes air/ U* U4 s% t# |1 s( F
IR TRAFFIC CONTROL, A system comprised of
: o9 t" o4 f4 N) [round and airborne components used to identify, track( W/ g! h8 b3 {$ e6 E
OUND SENSOR, An electrical device operated
1 Y* I4 t7 Y' I& a. r. Ty the landing gear, which transmits on ground/in air: [) V. o, w* V5 d. q! l/ t
formation for system operation in flight or on the1 X( [( _1 d1 M2 z
round.! L2 q& U0 u: Y. p, u$ o' ^, \
IRBORNE VIBRATION MONITOR, The AVM takes
8 e, D2 P# F* w5 ^e signal from the engine mounted accelerometer and
$ @8 M' D: ?# r! s+ jalculates the vibration on that engine.
4 K$ R6 a( s0 H6 O) i+ Gcorridor equipped with radio navigation
! I) u/ R+ d8 N6 qaids.! E) X: f0 a2 ~% }# I
AIRCRAFT (or ARINC) COMMUNICATIONS
% I3 W s: V+ G E: X; k! e7 eADDRESSING AND REPORTING SYSTEM, An
, ~1 v) j1 Z" x, o" i. ^6 T0 i7 [addressable digital data link system which permits the! b4 F& [# L j2 i8 c1 M# `
exchange of data and messages between an aircraft1 m- B/ l9 T: {3 c3 M" w) Z5 t
and a ground-based operations center over a radio+ U$ k/ }; u# Z+ P% m- v' J
network.
; g4 c, B/ V' p* rAIRCRAFT CONDITION MONITORING SYSTEM, A
' o, O+ h3 r8 `5 H! Y. lsystem of sensors and recorders to monitor various' g, r3 a6 c* U2 H3 c
airplane systems' performance and status.
" f5 e$ u7 J3 N5 D) z8 x3 n机,0 q- `4 O2 `: R! ?8 G9 ~2 q
中交通管制,) l$ r2 ^) p" B) c
一个由地面设备和机载设备组成的系统。用来对飞机进- E2 P; w* |. F6 ]3 {$ |. }
地传感器,
O8 G' G" F6 f+ P& C* c" e* R* T一个由起落架操作的电气装置。用于给空中或地面的飞( o: X# q1 s) E) F8 v, X
系统运作传输地面/空中信息。(有些系统只能在地面& R2 e/ ~7 N: f3 D) f# o* Y+ }9 a
用)9 A7 _: c7 a& `0 x
载振动监测器(AVM),
6 d' k9 v* V$ }( o/ \AVM从装在发动机上的加速器取得信号后计算出该发
; t* Z( n% o6 W机上的振动。, _- _6 B6 H$ E/ ^/ Y7 r
式建立的控制区域,内有无线电导航设备。
2 O" n- |7 ^4 N& y" c; k9 j) h飞机通讯寻址和报告系统,; ~+ D- |3 |( v, O
有种可寻址的数据通讯系统。利用该系统可使飞机与地
' o6 S2 _! t1 g( m" `面操作中心通过无线电网络进行数据和信息的交换。1 C1 D9 _2 x' C" ~, X1 Y. {8 x
飞机状态监控系统, B2 @4 A! c8 ]( j
一个利用传感器和记录仪对各种飞机系统的性能以及$ F; f2 A/ R' D( J0 I2 L
状态进行监控的系统。& E6 M b1 [ @7 b" u5 M
A
, l: w, D( S, X$ r4 A# t" m6 \5 Rg
/ {3 h5 r9 k; xand locate aircraft.# |) n$ T& Y" G
AIR/GR
2 R6 I0 W& N( Zb9 \6 K) x2 k% k# n0 q4 X
in
6 F/ T5 Y3 W+ r/ [g
' Z5 g* O/ M& S! A, a; m, h. ~! ?A
+ A( |' D) V7 y" U8 D" f% f3 kth
8 t* d5 k& }# B3 J# ic8 B' W+ p" ~% {8 F& L0 w8 ]: K
AIR WAY, A control area or portion thereof established
- l3 [. M& A2 l$ a- din the form of a9 ]. ? [0 R, J/ V( q
大气数据计算* i2 r2 e3 S3 y0 y8 S! _4 O7 }. z9 Y/ a
根据量取压力和温度而产生大气数据资料(高度、空速# K9 E2 }" |9 a4 A
等)的计算机。0 r# o7 A b1 `4 v" w
空
$ W9 b S: g+ \行识别,跟踪和定位。8 o2 N; [4 x. U0 @; Y, c% ?
空: R& ]' _% \1 U0 u7 `' ~
机
, H- I1 a P Z: [/ a使
6 F* \3 R2 e0 T' T机 u2 T% \7 ^( K( {' s& w* e- Y# N
动3 |2 {/ ?1 T- Y$ Z* ?* p
航线,
' J% G2 h) S, U" H ~以走廊形
- D3 a" E: F" v# `) x8 e' X2 Y2 z英汉对照民用航空词典B OEING* J; v" Z* Z( T3 v# j" u8 W" V
TECHNICAL DICTIONARY 6; ^& Y) C h4 k: V- c0 c( p, h! H
AIRFOIL, A surface designed to obtain a useful reaction,
& R5 {& S w' I5 g3 g. T* T. U: Zsuch as lift, from the air through which it moves. Wings,# }0 p. s& N b
stabilizers and control surfaces are airfoils.
3 M4 ?+ s0 w+ u1 U6 L( y5 j6 yAIRSPEED (IDS, TDS), The speed of the airplane) L3 O7 q F- L0 a1 B' T1 |, @
rough the air.
. h, S. F4 D. J. ]# iD INDEX, An adjustable pointer on the
' e" s! t0 o, o/ U) Iirspeed indicator.0 N) h% x E1 u
and legal ability2 N5 n- x: p; l7 o, v# t
fly.& I, a3 [. D: s, f
m, for example, the procedure for finding the: ?- J4 T, ]" ~3 c( O
quare root of a number., S8 P4 K7 ?* A2 @) Z; R- A
y
& g9 u0 x/ v! o4 K4 pre, wind,, A' q6 G5 @& X @& J1 M
and aircraft flap setting.% I$ b7 I3 a; z( P! z
是翼面。+ d4 E& H$ \2 ^# V& q
速, D# {. u9 }# ~3 c3 ?3 o
飞机在空气中运动的速度。( I$ ~( J+ j& E" t
,
& E* u+ d2 y: C4 V0 k在空速表上可以调整的指针。9 V8 @7 R$ K( i/ F5 E" k+ q
机械飞行能力、和合法性的飞机状态。
( i& `) B- w! y8 y! J! n一步一步的解题方法。例如,计算一个数的平方根的步
], n7 i8 @2 q。8 z* G7 L/ ]/ P: m& \) }6 s5 J1 d
能7 A! F% i9 b2 A0 e8 v
资料的法定文件。
& |4 C! K1 t6 U" [翼位置成函数关系。
- \# O I9 X: { X0 W! ^9 P( Zth
6 K3 [5 s' d9 O( ~) p9 cAIRSPEE" {0 h* r9 ?1 e( c9 G9 g
a
* q% i) J- {3 ?8 G6 m3 G* t1 ?# VAIRWORTHINESS, The condition of the aircraft with" ^ L" N( H) S* N& |, x4 y
respect to its aerodynamic, mechanical,
: }! U, `1 ^8 {) j! X0 eto
6 u- y. {. B6 W1 s4 `ALGORITHM, A step-by-step procedure for solving a
) I2 r: D5 _$ _( x3 ^* J- g% Qproble9 l* r' R& w* q. U
s+ n4 F7 a$ o D5 {; U: t( z, f
AIRPLANE FLIGHT MANUAL (AFM), The legal. K5 C/ L9 Z3 K& W6 c: L. `
document containing performance and operating limits,
' n' x- U6 m. M& E4 ]operating procedures, and takeoff and landing
( W: r P9 J7 hperformance.
1 W6 V& G( J( b0 y ] g5 C x! fAIRPORT ANALYSIS, A comprehensive set of takeoff
0 s$ X! P: L9 p+ s2 |/ B5 i1 Zweight limitations for a given airport runway, generall
& V. \( D) p3 u! S& q, Zpresented as a function of airport temperatu
# b8 _+ t( F, R翼面,0 F( e! Z. ], Z2 _# g; k# s5 T- W
用以从气流中获得反作用力(如升力)的表面。机翼,! H5 W4 w8 U# @! {9 D$ S$ y
安定面和操纵面都3 d! ^6 y1 ]/ D, I
空
b% ?) \) |/ J9 v空速指标. S* e5 q8 S+ P
适航性,6 f. Z8 r" W6 w8 F) f0 P
有关气动能力、; C+ k1 @: h! S- G, V1 \ u
演算法,
# z- s' r) e- f; p5 M2 v骤7 h% H6 F' Y" R9 D, @- b
飞机飞行手册(AFM),3 L. D7 _: s7 |4 ~4 U. U
包合性能极限,操作极限,操作程序,起飞和着陆性
+ A% V0 H9 |: n等
& K/ K3 N+ d7 b) B* C) w机场分析, O% U7 d1 F1 M' p
一套针对给定的机场跑道的详细重量限制资料。通常与7 p8 E. J% k( p
机场温度、风、和飞机襟4 {# w, z# M. G5 K4 P% f: Y
英汉对照民用航空词典B OEING
* y* m6 [5 |* H* J* rTECHNICAL DICTIONARY 7
" A4 K& m: \" ~. V6 J8 ]6 C, aAIRSPEED BUGS, Adjustable pointers on the airspeed
! J4 t+ ~3 o- Z+ v4 j- R$ P2 O' eindicator.
6 }' ^6 V; n3 A; V7 p0 ]ALLOY, A mixture of a basic metal and small amounts* A# s h) Z" X. t7 H; j0 g( B
f other metals to change the properties of the basic
: J) G9 z! \: retal.7 ^( u6 r _& I: ?& L
Minimum airplane speed.' s$ [+ Z% } {! b! s" `7 v
e of
1 u c( x, E7 v; r' v+ B5 w/ _# Hitting airplane angle relative to
+ h5 d1 F* q! X& u1 dirstream for the stall warning system.
; r/ L0 v# [( b/ ~another.
% q" C) Y# r$ e6 }* D3 A* ]LTERNATE , An additional airport selected during/ K. r5 v7 I8 u* W/ R- [9 P1 Z
,
: L1 K1 Y, _2 W V& j; n3 B( d合金,3 B" ~1 c' ^; [# i4 m
在金属中加人少量其他金属,而改变其性质的一种金属! l1 K# D. E: k! J! m9 I7 x* G" ]3 w
合物。
7 b! a5 y& [7 P0 g! n5 N飞机的最小速度。
! d% `5 q/ n/ M5 l$ N" a速警告系统传输飞机对/ ]$ j2 u# Z9 L* b4 C
流的相对角度。3 h& b$ T" [) x
由一个状况改换到另一个。- e4 d0 z( z! \' m# s
降场,
+ Q& q Y3 q. W$ M: V% [6 f6 W" H划时,除了目标机场之外,所选的另一个机- i' q' _) z7 J6 |5 m! W: V l% m
o
: w# _$ z; b( G! q# |% N0 `+ o; Ym
8 U! a5 t: d3 i( ?( i6 _ALPHA SPEED,* f) k2 e, ^% j" {, \3 D
ALPHA VANE, A small moveable airfoil on the sid
& n) P- j" o4 ithe fuselage transm
$ F) D- B6 Y7 G+ sa
V& e' \( B! h1 {ALTERNATE, To change from one condition to
. s @. P: |' } S, UA7 k9 u6 V; }/ D% n7 k/ [( x$ @& W
flight planning, usually near the destination airport, to be
2 t/ i( x/ ?- [; n( D2 i# [used when it is desirable to divert from the original
% g l) ] {/ h" ?destination airport.
. F) t3 M) M( U- H$ B空速游标
1 Y- h3 y9 S6 l空速表上的可调指标。/ `5 x5 ^4 \! i6 F8 [( B# I
混) z% g/ c# o! r; J3 A3 @
迎角速度,% _: d: @$ l: \6 L
迎角叶片,# f l; A7 [/ J k m# r/ t- b7 n
位于机身侧的可动小翼面。为失
" M. ^' C6 R8 u% t2 T L( E气/ f s$ W9 B+ C( G: A4 ]% g
交替,/ E) I* W2 C/ W0 J9 y) k! {9 z
备
' N6 R& E! \4 K( S制订飞行计) M7 I& n- f6 ?& G' I5 @
场。通常在目标机场附近,以备不去目标机场时,改降之6 U, ^7 M$ R2 H D' J3 @8 w M$ V2 m
用。* L9 @+ F; S' B# u I. X
英汉对照民用航空词典B OEING
3 `; F' R( p" f0 F! _2 x% m) \TECHNICAL DICTIONARY 84 A! c X1 i) _& n) Z- O$ @
ALTERNATE AERODROME, An aerodrome to which1 w1 s; v' ?! q
an aircraft may proceed when it becomes either$ P0 S2 C2 a- p% r" v" u" [/ Q
possible or inadvisable to proceed to or land at the1 ~2 k8 W; d6 S9 t7 F; O( i2 U
erodrome of intended landing. n' B% @8 p7 Q( X% D1 i
TER SETTING, The adjustment of the altimeter
5 ]: `- L- w4 ^- R1 J0 Taccount for local variations in atmospheric pressure. ]+ c) Y5 J' h. v. T! Q+ t
LTITUDE ACQUIRE, A digital flight control system
) }: n& w" v$ I7 ~; x* Jode to transition from climb (or descend) to level flight.1 a' Y0 E- e/ j8 R2 M. M
LTITUDE ALERT, A flight deck alert occuring when the5 {# a" {$ E! q3 b$ R. L3 A
irplane approaches or departs a selected altitude.1 x- t ?' ]2 j# t) f, b; p9 n
LTITUDE CAPABILITY, The maximum altitude at* N& j: g* _& O1 L' X4 b& ]
hich the airplane can be flown at for a given thrust,1 c% J5 n( { n
peed and atmosphere condition.
/ `% N5 o7 i5 C0 u( [ @5 zLTITUDE HOLD (ALT HOLD), A mode of the autopilot
( K% X' g L% B/ Q; t5 Rr flight director to maintain a selected altitude.* N0 b' O3 g% Z6 ^- ]4 \
irplane's altitude during VNAV operation.
1 h. k, o3 n# O+ w T1 ^* f" _ l机场着陆时,可作着陆使用的. l* ~+ v1 u9 `9 P5 y% V* V
场。( p) M. A* h+ V9 N
,
) U) H5 w5 X8 L: m# d0 }* h3 Q2 j根据当地大气压力变化而对高度表所做的调整。) M) i. \9 c7 o3 F" K2 p$ A9 J: E
一种数字式飞行操纵系统,从爬升(或下降)改平的模
( h1 _& ?, y" y: V; S. d。
- n; b1 @. ]; h度警告,. v( J2 ^% ^, I/ Y& v5 N r
当飞机接近或偏离选定高度时,所出现的驾驶舱警告。& w* H* m/ v# v/ L) h/ P; A
高度能力,
* i: l7 N) v; a9 Q+ y# e- i在给定的推力,速度和大气状况下,飞机能飞达的最大1 n( D" I( r% Z3 ~& J! h& `$ c
高度。4 J! W" {" A) o2 `4 ]
高度保持(ALT HOLD),
9 [2 w6 l; U9 Z N自动驾驶仪或飞行指引仪保持在选定高度的一种方式。( x, U3 }7 B( A+ \) k* x% Y) _
,
3 Q$ ^$ T$ U$ J8 E员对飞行高度的控制。
3 A4 Y! V! X% Y5 ]( Iim
) i" k! {) G; J. `a! p# V# V* P0 a; Q8 t
ALTIME
# a# ~) o' ~. J& Bto; H- G) p+ e6 a- I
A" \5 ^+ r4 y) _% Y- O
m8 y8 l- M! V' R
A
, V4 G. t; f8 b4 Za
; b& B( M9 }! t# r; t* tA! J* H# P1 H3 ~) C
w
' [! @4 N+ n2 [4 T5 gs
* z# {' F1 L! q3 w; X1 ?% c* PA
0 `; p- S8 ~1 h6 C! lo
( s2 I* a* w# C# J+ W4 a5 M5 qALTITUDE INTERVENTION, Pilot control of the
2 d+ f$ x9 t4 Va( h3 C( H3 k/ Y( Y: Q" N# m$ k
AMBIENT, The surrounding atmosphere.. J0 ~( L7 r/ ^
备用机场,2 E; I" i) s0 Y" U7 L
当不可能或不适宜在预选
; b. ~. ^# C9 m8 r3 b机
. ` }# N, G) k! D5 l) O4 ~高度表设定
9 ~( _$ I4 o, Z( m) d3 |# O高度截获,2 P$ G+ _. S( M" H. J
式
: C* \' |: G* H6 Q; D1 t0 u+ U; G$ G6 T高1 G5 _. a+ x- b, Z
高度干预
3 G$ t+ d6 x: K$ Z6 ~2 R2 ^在垂直导航工作过程中,飞行/ e5 i% j3 }4 U, o9 R* c* ~
周围环境(地面气层),
6 i; x' {8 ^, [! M6 [0 E3 i* f/ Y9 P3 X物体周围的环境(特别指大气)。
3 e. S9 {1 O/ W) Z英汉对照民用航空词典B OEING
3 r1 Y2 [" f( W X& M2 pTECHNICAL DICTIONARY 9
) B9 y( c( Y$ z* OAMBIENT PRESSURE, Pressure of air surrounding an
" e( u5 v3 i G" A% K: n/ K: N2 lobject, measured in pounds per square inch (psi) .
" n! ^' i8 p% EMBIENT TEMPERATURE, Temperature of air- w/ d* ~5 x: ]7 N; X. _
mpere." E( `0 e0 x0 _; d
urrent waveform.
3 f5 s; i/ a& @# Hg an) v9 [: {" @! B, C. Y
nalog signal to a digital signal.
5 |7 Q6 Y: e) R/ j2 Tore inputs
: K& L( L% y+ O4 |: a, _! ]f binary digital information and one output. The output
# D/ ^+ D: E5 s8 s0 H$ ^) k1 only when all of the inputs are 1. The output is 0
% ]7 O) T- C' h2 W7 ^6 @6 |hen any one or more inputs are 0.! e8 j4 ~. m) i* p
面气压),; ^" S& ^/ k4 M9 r9 J
境温度,3 ~3 i2 q" a( D4 p/ [
气温度,用摄氏度(°C)或华氏(°F)来
! s5 F( z/ _" K6 Z$ U: X。
0 ~6 S+ D' a9 V电压或电流波形的幅度。
: l3 D8 k- ], @! _5 n9 w性变化的信号来工作,或产生连续性变化的信号7 J) G, S3 e; t$ U+ y9 p
统。
: n: o2 } x* L& R! ^将模拟式信号,转换成数值式。& t. e8 ~$ n8 @9 _7 W- L z5 ~( }. ?
一种有两个或两个以上的二进位数字信息输人,一个输
9 _9 Q) X y4 l w! i. c' i4 p8 G# o2 N的装置或电路。当所有输人为1,输出为1。当任何一个" I* Q, d" [' g4 u! {2 w
一个以上的输人为0时,输出为0。
, }* ~) J& k$ ~! m. G6 kA
; R! M9 Y. {& r- ?) \1 Msurrounding an object, measured in degrees Celsius# j6 F: w# p8 o& X$ S, l2 {% s
(°C)or degrees Fahrenheit (°F).8 e: g: A& q8 k! S
AMPERE, A unit of electrical current. One volt across
0 [5 e/ ?7 u# K- Mone ohm of resistance causes current flow of one+ @: ^5 ~) _7 K9 U6 b- P$ `1 U
a
8 K' r3 H# i9 O$ F. o1 qAMPLITUDE, The size or magnitude of a voltage or
; r: G- f" s( F9 N% ?1 P/ T7 mc F6 }8 U; f; K( ]- {2 B
ANALOG, Quantities or representations that are
! `# z, f" v3 ?1 E: i3 A1 @variable over a continuous range.3 z& V# D! |+ l# S3 ?5 Z+ a
ANALOG-TO-DIGITAL, The process of convertin0 }, D- g0 ]9 S( f9 o
a
9 v! j/ [6 W) O D: A% @AND GATE, A device or circuit with two or m0 N: @1 D @6 N
o
% G5 o* i! `, [% pis
' g8 m' k" C; p# ?3 z0 ~# }2 cw
9 B6 e/ G! z+ P3 I环境压力(地5 Y( x& Y1 g2 l) s
物体周围的空气压力,用每平方英寸多少磅(psi)来
) Y( m( T$ m0 Q. V; u5 p" Q度量。
+ k) Y; z% I" R6 F( X$ T环
8 N/ m# F, h4 Q9 p物体周围的空
# Y$ R8 g% x3 Q/ |# y度量。3 v) M: c8 ^# O* G) n
安培,
* `! Q# `6 f& |4 i& o" }电流的单位。
$ G6 J9 G3 R% D- h/ C/ n( ^' S1伏电压在1欧姆的电阻上所产生的电流为
2 l4 `3 f3 u" N$ _1安培
5 R( N% I G( i振幅,: p: n0 H' I b& W3 p
模拟式,
- D/ C% K5 R, T; P; e8 X5 V- O用连续
5 v5 g% A- W/ A5 D1 _1 E+ h" H系
0 e, A2 a# ]! g从模拟式到数字式,
4 M# {- \2 }, ~6 l" x8 y/ b与门,9 G1 h! ?4 g7 D$ P- C" O
出
7 G7 L g% Q( B2 }8 Z或
! p; P4 X+ T" y$ k( T0 ^9 u英汉对照民用航空词典B OEING: }9 j9 {7 e0 c
TECHNICAL DICTIONARY 10+ Z n' W" j9 x! j. D
ANEROID, A sealed flexible device containing air at low/ h& V. C$ V l
pressure, which expands or contracts during change of
- z# `5 }4 X0 x* c( I |" N( E" Gressure outside the device.
# z' @% f7 e, L) b4 t/ iically1 m- `' z" C1 q0 Q0 M- s
r changing the direction5 j$ M/ m, s$ d9 Q. C
f drive.
# U/ s1 p; t$ D9 I7 |of the wing chord in9 a4 u$ J' L& [% ^" ~5 X
lation to the free stream airflow as it moves forward
$ c, B2 t# ]; jrough the air., `6 L9 R: M+ x+ Z
al axis of the# D$ p+ _+ _' h: a/ f- ]3 x: G
aircraft.0 `! ]2 u3 _7 ]1 {; O
胀或收缩。
" m' P# f& f% Z7 d& U, e% u' y箱。是改变驱动方向的机械装置。
/ Q. Y9 ? P- d1 _机翼翼弦在空气中向前运动时与自由气流之间的夹角。9 K2 U7 A1 Y; S/ a; b2 h
。- K- h7 m6 t4 F0 L
p
, @+ ?, x$ B3 \) c1 _ANGLE GEARBOX, A part of an engine, mechan
9 V: I4 j+ ]; {driven by the compressor, which drives the accessory8 u. h6 l' F! E8 ?" Q6 C! Q+ m7 c; [
gearbox. A mechanical device fo
7 m# k' z$ o( J: d+ v7 X( S. Po
2 R! g, r; @* F# D% Y1 }ANGLE OF ATTACK, The angle$ S# k8 ^1 t- O: g. k ^ j
re5 h9 a* P* b/ n+ }9 e6 b
th
4 o9 H; M+ S" U% a( k* iANGLE OF INCIDENCE, The acute angle which the! G% W* f- Y7 c; w! k
wing chord makes with the longitudin
# }, A7 @, c: I; X膜盒,
8 _9 s. y. A# T; w& b内含低压空气的密封弹性装置。当它周围的压力变化8 @7 w# F0 N) j( G
时,会膨2 k- M g; A$ P2 d, m& ^
伞齿轮箱,
) V6 Q w, s- \# _( }发动机的一部分。被压气机以机械方式驱动,然后驱动
7 L- c- s6 c: z6 i2 h附件齿轮4 @- n" F# ?3 e! `* B6 f
迎角,
: n5 M4 w# I4 {% t, R3 ~1 f/ l安装角,8 c: t* ^* u$ T9 R
飞机的纵轴与机翼弦线所形成的锐角+ l& C+ H& l7 Z1 v
英汉对照民用航空词典B OEING/ \) }7 a; F' r+ L2 k
TECHNICAL DICTIONARY 11
5 }" ^7 x6 h: P2 ~4 Z) B6 mANNUNCIATIONS, Audio or visual indications used to
: G3 \; ?, [2 h- F% o: P; n1 tcall attention to an event that has taken place.( }9 \6 ^) p, k% M$ o; v( A8 }
ANNUNCIATOR, A visual device consisting of a number1 X8 D3 G. I, i5 [! `; O* t, ?+ U
ly.
8 ^- ^1 s! x/ {/ c% U& gANODE, The element toward which the principal stream; P/ j: O% b5 B* m( Z
of electrons flows.6 }9 Q- h/ v( x! M" K3 m
ANOMALY, Not normal.
+ u+ s$ J# x" pANTENNA, A device which, used in conjunction with a
5 t( G, L4 L( H) ~' \2 m ]transmitter or receiver, is used for radiating or receiving
; X% b4 O% T/ ], |5 o/ n- vradio waves.2 Y# \1 p( n9 P3 b" m" g+ Z8 {
NTI-ICING, A method of preventing ice formation on
. b5 p6 ` Q( x. Pe wing leading edges and engine nacelles.
- k9 d8 D$ I4 z* [7 i/ yNTI-SKID, A system for providing maximum braking% m0 V" X3 i" a7 @' m5 g2 o5 O$ b
ithout skidding for any runway condition. Anti-skid
* m& d' y% @4 Z* \; ] _omponents are part of the brake system.+ M9 [9 T5 d; L6 O+ U0 T
告,
) v: j" K4 @1 N; ?6 s Y当发生事件时,以声音或目视指示形成的提示信号。
* Y8 K. f( \; U5 O. N6 m与之有关的电路的现有情况或已存在的5 t5 e/ }3 |" W8 l
况& u! I+ r$ N5 }2 i
正极,
. K* X0 k% p% J7 a( [6 N8 ?1 h0 ^主电子流向的极位。
- l: T9 l" I7 L3 v3 C& F异常,' O6 \4 u3 D1 l5 K0 {6 b
不正常。
1 E/ T0 J# T y% v$ u" c$ J7 b天线,
9 m* }; f, {3 ]+ E9 i一种与发射机或接收机共同工作来发射或接收无线电8 B* ^, Q9 U% Z3 E; U( Z2 x
波的装置。) L% T' Q6 w2 e/ Q; H% A$ L) Y
冰,
p) F1 ^5 i0 i! e; r: L防滑系统,. a+ n" j5 V% q) D5 o/ D7 A
一种在任何跑道状况下,都能提供最大的刹车能力而不' S$ [% r& v f
使轮胎打滑的系统。防滑部件是刹车系统的一部分。# x, H! {- @+ e8 T& M
of lights. Each light indicates the condition which exists
4 `& \) A# R. j/ i! Z0 v' a* e+ Eor has existed in an associated circuit and is labeled9 Q+ I; P# h& f) ~5 E. P
according. F4 |7 i) U. a& ~& [; C; t. E
A
6 o, O/ y( p- v- v3 Qth% A7 W: ^/ X c. o% a* V
A
& @* e8 O i, Z: G$ ^! Tw
2 c# _$ o; H: ]7 W5 Oc
5 l/ O& w) J$ `1 a0 L+ k, A2 }# U通
; A2 L$ b2 Q; a信号牌,4 k! Y8 f. p& [, H6 i
由一系列指示灯组成的目视装置。每个指示灯都有相应$ D1 Z$ y0 m8 O( s; |) l; q
的标记,用来显示
2 J H9 @6 M: g3 g* b情
; m6 |( R8 V& U防* e7 p8 c" J: S; m* [0 C# E
防止机翼前沿和发动机短舱结冰的一种方法。) j6 Y k' L; {& ~' ?4 N
英汉对照民用航空词典B OEING
% n8 n% H+ B9 C dTECHNICAL DICTIONARY 12
1 {$ q5 I1 v( T& m) d( p. w/ IAPPENDIX, A supplement to the Airplane Flight Manual
4 A! W! E/ o1 W) z% n1 }& X$ otained in the basic manual. A
) B' A" |1 @$ _9 j- u/ p rollection of supplementary material at the end of a4 j1 W7 F0 o) f6 _7 b
ook.
6 d3 I$ A" t+ x3 [! v6 g9 vof the9 s, P( ?/ |7 M' _9 L
rsion link on the landing gear.' }* x/ S6 Z& B6 D
APPROACH MODE, An autopilot/flight director mode
+ k& X" H' l/ b" @8 Iwhich is a combination of localizer for roll control and5 \( B! X+ u8 H) L) d
glide slope for pitch control. This mode is used when full
: w; c3 N3 B0 } J4 [( tinstrument landing system is available.9 |3 C8 i: J8 r* k( o
APU, SEE - AUXILIARY POWER UNIT
) l/ b) N9 f+ ?5 y/ JARINC, SEE - AERONAUTICAL RADIO7 n+ s. e) T$ _! |" Z
INCORPORATED& e/ h" w7 D6 {
ARM, To make ready for operation./ @, q4 {9 b9 y+ d$ j
附录,
! V5 a& W7 B( x; ^; \: v飞机飞行手册的附件,包含基本手册中未提到的飞机形- Y% ]" M0 V' s! S" S/ h
态的其他性能。是附在手册末的补充材料。
4 V0 @' {0 t7 _0 T" W/ r" f顶销,
9 g w8 r9 x6 s0 \9 j2 {; n用于连接起落架扭力臂两部份的销子。: A9 U" c$ p- s0 q% m* ^, f1 Y$ ]
进近方式,
) L; o, l9 u) D( N5 Q" c: y: H一种综合了控制横侧的航道信号和控制俯仰下滑信号
& n# n2 U# W# U m9 j* w的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系
$ _, F4 r# {* m7 z) Z% R1 r统正常时才使用。$ W1 v6 a% e* V& q
辅助动力装置,7 [8 e5 H; H/ Q; M# s3 J: N9 b- W
见Auxiliary Power Unit
- t4 D, R% {3 U2 Y( H. B8 lcontaining additional performance for aircraft# _ |* q7 f4 X+ g2 |& {
configurations not con
4 j4 W1 C0 Z# _% [9 n& P3 o- Fc
0 B- ?" C+ u' l& S; D4 s" @ eb
a/ q. `& c3 F8 @6 a6 w6 dAPEX PIN, A pin for joining the two sections0 t" z! v3 h0 {: I5 h/ v0 N& Q
to Q# I, p9 j8 \! E5 b
.! e# R) K5 B& p3 e
航空无线电公司,8 u$ A8 I, }& q x+ ? \8 t5 k5 V
见Aeronautical Radio Incorporated.
; o$ |4 f: S% k1 L; a3 }+ e预位,
' d6 h, ]8 O; W0 \9 T, V部件可以开始工作的状态。
" ?* p' p3 R2 ~) Q0 r8 c4 s5 ^: E& s英汉对照民用航空词典B OEING
# ~1 d# t$ H2 K5 i! m' j- c2 m) ~TECHNICAL DICTIONARY 13
: P2 R7 ^: w; t; V+ b4 zARC, The curved track over the ground of an aircraft
a5 r! B. D6 F+ g6 tflying at a constant distance from a measuring* S9 q7 w- {0 K& N2 Z
equipment (DME).8 n. ?3 g1 P8 _8 K
in the limits of self-contained system) A7 L L @& y: B+ L; Z
apability.
/ `/ e3 Q) k/ s) b J, Ptem for opposing or restricting1 m9 }: O }" y8 L8 B6 f* P. ~8 O. U; ?
ovement.
. B* k/ T. k( k* B3 R+ hSPIRATED TAT PROBE, A sensor that measures total
0 o; t5 U9 p4 x4 t6 ^! E9 ?) Oir temperature when the airplane is in the air and that
# u: X+ M/ i3 f: v& W1 j% seasures outside air temperature when the airplane is
. T6 c. B7 {( E) \2 On the ground. The outside air temperature is measured
3 k! g0 F# p( i5 Q' jSSEMBLY, The fitting together of a complete structure1 P" p- W' V* u1 M7 y4 q9 S6 |
SSUMED TEMPERATURE REDUCED THRUST, The6 N, N g) s: i2 }% s' |
ATC, SEE - AIR TRAFFIC CONTROL6 H6 f8 @4 G5 E5 J% C/ A
,9 F1 M# \+ x1 l
系统中所产生的一种用以抗拒- B V2 f4 d$ _1 C
作或限制动作的力。
0 Z; S2 V' V: j2 ^4 n头,3 c2 l& j9 ^( p& G/ B, v' O
用来测量飞机在空中时的总大气温度和在地面时的外
" X7 }" T* p1 k# h7 a9 I2 O温度。地面外界温度的测量是利用引气将外界空气吸入3 K7 S% ?) \5 k
头,以达到测量的目的。1 x3 ^9 F* a' o! v2 g7 A$ ]1 p+ \
配,& T- x9 c3 j9 B5 w: B) `
一个完整的结构或组件的过程。
7 f- ]8 g* i' f1 g W7 B假设温度而得的减推力,
8 T; I8 B6 u3 Z D/ f, D推力设定值时,假定一个比实际外界空气温
; M2 e, Y, E4 O$ G( _3 I空中交通管制,# b [8 q6 D1 I
见Air Traffic Control
8 S* R8 J# ^: G+ D3 l) xAREA NAVIGATION/RNAV, A method of navigation
4 A/ T$ Y. _' P' W ]that permits aircraft operations on any desired course
# G* J$ R/ {# D0 f' T3 w, lwithin the coverage of station-referenced navigation8 Y) Q4 F: l& _+ K7 o
signals or with& Q' T$ j: E7 Q A- d
c
8 H7 C0 o' p0 {# \1 {0 l$ `ARTIFICIAL FEEL, A force developed in the flight! L( J4 ]& N, }- D; O
control or brake sys, U9 m' {( P1 W2 j' a
m9 x- P3 T b* E+ e
A
7 e: C$ e$ w, T7 u" e$ p! {6 R( {a
$ |( n# H. Y" D9 C' g5 C- U3 Um! h, Q; J: @, W$ w/ v' u# j) c
o
/ V# _4 Q) C" q; H* \" Qby using bleed air to draw ambient air through the$ u/ _6 ]# @! e& \; `
sensor when the airplane is not moving.. |- e! Q+ J) |8 a5 t8 ]' y
A& J9 M% j, u. C4 b
or unit.( H4 G k: g3 Z5 h% Y7 _8 w" V2 i
A% T3 I/ e2 T6 v" G
lower thrust obtained by setting a higher than actual) ~$ r0 N, ^. @1 e$ Q, L# _
Outside Air Temperature (OAT).$ y0 @ R6 w5 f
弧线,& f; u8 c6 q" \6 J' K# Q* Y1 N' p
飞机在围绕DME台等距飞行时的弧形航迹。' D: K8 F v# h# b# D A1 Y) P% C
区域导航,, k7 j% p3 I) `2 x0 n( I
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" w- y* u5 w1 x力极限范围内,飞行任何预定航线的一种导航方法。
1 D! r7 A4 B! i1 |0 m模拟感觉: h8 r" m' ?" [) f# W9 u+ \6 f
在飞行操纵系统或刹车+ K1 x3 r) ]6 f# L" {
动2 M( }8 _, x# r
吸气式总温探# G$ _& r) E" r# J& k
界9 `7 w. v! [! C) i/ F# y
探
- }7 N" i: ^' g8 x" q装
* I1 q& w; K# V% H6 i/ ~) \组合成% n& O/ f0 v. a+ |& w
由6 S/ C, ^! M: j
在选择起飞0 }3 q& }, F% o! _- K, ]" 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& k$ Q0 V& d7 g/ L# d. m
磨损和维护费用。
) A, u3 P9 E4 j, q" z.# G& q- O7 n$ y& w
英汉对照民用航空词典B OEING
. u4 H, E/ e* l2 p; H% n, NTECHNICAL DICTIONARY 14' ]! v4 q6 y( v! t" n
ATE, SEE - AUTOMATIC TEST EQUIPMENT
`) r9 V" v2 M8 `2 Y" D" b. JATMOSPHERIC PRESSURE, Pressure of air due to the' Q+ @9 @2 y. j3 Q5 u6 [8 T# S
arth's atmosphere, expressed in pounds per square
. I+ z# S0 Q! m [& kch (psi) or inches of mercury (in Hg) or millibars (mB).
8 a! m& o1 i2 u4 X8 HTTITUDE, The relative orientation of the airplane with
J; `: |" F: `) p1 yspect to pitch, roll, and yaw.* w. L0 }" b c2 c2 l( j+ R$ C$ h
UDIO CONTROUSELECTOR PANEL, The panel in9 F3 |4 A7 y" y+ n8 o7 Y
e airplane which controls and selects the routing of4 ~! t+ c X- ~9 B
udio.
9 ~* W% M% N7 p. J0 B+ \UTOLAND, Automatic landing using the Digital Flight
/ |+ ^+ z. r/ U9 F$ Z \; sontrol System.
2 I2 ^ ~' P: L) an.
. u/ `# J" J5 ZM, A system4 s+ i: J6 H- T; A2 b( {
omposed of all necessary subsystems needed to guide
$ U' d$ |: q0 Ie flight of an airplane.4 V' N& L- h" {. e3 v8 L( M
EQUIPMENT, System test* S' S% s! z6 f1 u: T3 Y& i
quipment that operates under computer control.
/ i: Z9 g X: a5 I装置, |
|