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AIR DATA COMPUTER, A computer which produc9 _+ Z% y# d9 n
data information, such as altitude and airspeed, based/ ~7 c+ k. ] x' q
on pressure and temperature measurements.
8 v8 H# L; A- wes air6 Y, @/ q4 |# b4 ?5 H
IR TRAFFIC CONTROL, A system comprised of. l' Y! k" W- P& E9 b% C, i
round and airborne components used to identify, track) q4 V# [& f: W" i F
OUND SENSOR, An electrical device operated
+ n3 f7 j; r6 v+ d1 ~( Ty the landing gear, which transmits on ground/in air: |0 F( j9 c8 r$ v+ Y6 C+ S6 b
formation for system operation in flight or on the* m, b7 S( t6 G9 y0 b; q8 V8 D0 A
round.
) p( {3 N+ e% X& zIRBORNE VIBRATION MONITOR, The AVM takes& u9 A3 F( w# \, v6 ^% s: b/ H& @
e signal from the engine mounted accelerometer and
u9 H! l; y4 `- P2 ?9 b/ Ualculates the vibration on that engine.
9 }- [) ~. S0 g( O3 `8 c. tcorridor equipped with radio navigation e4 D7 C9 P" }. Z9 M
aids.$ S9 E. R" X- @$ {
AIRCRAFT (or ARINC) COMMUNICATIONS
& _; l4 x0 f6 m! [; N8 PADDRESSING AND REPORTING SYSTEM, An2 I( l% X2 X+ a! ?9 H5 f
addressable digital data link system which permits the; O# V+ W7 z/ y* V& a7 x' k
exchange of data and messages between an aircraft
. c% _$ Z- K" l' x. _and a ground-based operations center over a radio
8 t# @6 L" D& o$ P' V! m. @ }" cnetwork.
+ ?9 ]: R0 d. ^' ~3 |& x. b8 dAIRCRAFT CONDITION MONITORING SYSTEM, A2 X0 s' P9 `: S- Y3 a
system of sensors and recorders to monitor various8 O+ h" t6 i5 ]) C4 A5 I
airplane systems' performance and status.
6 A+ i) K# A& V$ W* i/ G机,8 c/ X4 z9 H# ~. g+ a9 U; A5 q
中交通管制,7 E0 r9 h- X" j; V1 v. F s3 v
一个由地面设备和机载设备组成的系统。用来对飞机进1 H6 N& c! P' L* T. X: p; Y+ K
地传感器,
% q0 X8 P; D3 X" X; F一个由起落架操作的电气装置。用于给空中或地面的飞
: P5 z: E; B# d# G系统运作传输地面/空中信息。(有些系统只能在地面
3 m0 y1 M6 I( G4 |: R5 {' o用)
9 W8 B& b) F0 X4 G7 v载振动监测器(AVM),; C+ N1 h3 R8 F1 h5 A
AVM从装在发动机上的加速器取得信号后计算出该发; D- E0 e8 ^7 y4 H4 p) b
机上的振动。 ?3 H3 C8 w9 ~ s3 J5 \9 K
式建立的控制区域,内有无线电导航设备。* Q3 b" j% }. o+ [5 x
飞机通讯寻址和报告系统,+ P" J, C6 g1 `- V+ t2 |0 O
有种可寻址的数据通讯系统。利用该系统可使飞机与地
* L$ J+ h, K! D7 |0 E0 a) k面操作中心通过无线电网络进行数据和信息的交换。6 f+ [( P0 Z8 G5 M
飞机状态监控系统,
) i; L% a! e7 p% X# _2 q: a一个利用传感器和记录仪对各种飞机系统的性能以及1 Y0 y* X4 b4 B
状态进行监控的系统。% b" U7 r/ Q- R5 W# D7 S
A
4 `& P; F& d2 y) Kg
- D8 q3 V3 R' |- B) Hand locate aircraft.
: s* |! }4 i' Y3 A0 `+ K pAIR/GR; E7 o) i" n F/ \2 `
b" v/ R+ A) y' q# p5 Z1 \( s
in
, I# G# d1 x6 W/ \( r& a% R) u8 `g
( \ D _: E2 |5 @5 g* dA# ^, g7 w: `/ H- u
th
, ]5 n8 [, Q; G8 @% u* |c0 X( c- i) b* e+ x9 d
AIR WAY, A control area or portion thereof established( V2 q9 N/ b$ L; r: r9 H
in the form of a
7 j0 H) @2 \, e& V: C" F大气数据计算
! @" q5 a9 z" I根据量取压力和温度而产生大气数据资料(高度、空速; T) u7 [( H K8 {
等)的计算机。
3 ?* Q% K& ], S- U空
6 @/ L* d8 A% W, y: p: G& x7 k行识别,跟踪和定位。) |3 C, S6 P2 e, V; t4 t f& c8 H
空
& m5 j% H, }8 Y) e, {; b机
* M$ K; T n% @% {! K- B使* E. {* _3 `, e' v' k
机2 C {" n* w' `0 \. W: l6 n
动+ n( o$ s+ i& n! n
航线,
/ D- e5 y* @$ Y4 L以走廊形
% d' H+ i0 O) W3 Y) O# L4 a英汉对照民用航空词典B OEING
' k6 _/ s% y' o1 a4 B v/ g# u- T6 PTECHNICAL DICTIONARY 6
1 u0 ? m: i6 c1 ^AIRFOIL, A surface designed to obtain a useful reaction,% r' e8 a. B5 |" H' x
such as lift, from the air through which it moves. Wings,
2 u" z6 r: n+ q+ E! G: Bstabilizers and control surfaces are airfoils.& ~1 V6 Q$ `! q! q6 {$ h3 \9 a, R
AIRSPEED (IDS, TDS), The speed of the airplane1 `5 M- b& Q$ Q: @3 y# Q) W
rough the air.7 @6 J9 ~# o) ~/ q: i0 Z7 M, t1 c$ n
D INDEX, An adjustable pointer on the
+ o6 m+ k& g- H8 `6 sirspeed indicator.
# z: h$ V3 X l! t0 o( Qand legal ability" u2 A! }8 b3 t3 q- u4 }0 D; C
fly.# B7 i( u6 s0 `0 S4 }& M- F
m, for example, the procedure for finding the/ E' k' l Z* X# m$ S) c
quare root of a number.4 p# i7 I# ^( I
y
2 q! ?7 @6 E2 E* |1 A0 \5 {re, wind,4 _, g4 ?3 A! P2 O1 l1 J# g7 w
and aircraft flap setting.
# R* O4 U2 @/ B是翼面。
& V) y" o6 x0 H3 V/ d6 ?. M+ K w速,
; P A( U% c7 f' }7 U飞机在空气中运动的速度。
1 k9 {+ u- s& U: B9 C4 }/ u,0 E" u9 l' \: g/ J
在空速表上可以调整的指针。% L3 ^. j# @7 N2 }/ R
机械飞行能力、和合法性的飞机状态。2 K4 i- A, B1 p3 S0 V
一步一步的解题方法。例如,计算一个数的平方根的步+ Q, x i* D- m) F
。
2 t/ b; n1 M# z能* M, W/ N3 P4 E8 F6 c. J. m' D* f, [) R
资料的法定文件。
! y$ }- Y2 y6 K4 q) Y翼位置成函数关系。9 X I' Q- b4 {6 j7 P
th( o' m. K1 M% i9 W# H4 |6 _" ~' {
AIRSPEE4 f* `. H3 S B) Q8 D8 ?" a
a
- O/ ~7 y1 J' H- I: V2 c8 U* s5 jAIRWORTHINESS, The condition of the aircraft with
& h0 Y# {4 M" W# a9 s# g7 Frespect to its aerodynamic, mechanical,
' a% Z; H$ X/ x8 Q$ vto
5 A, R( H6 N- O, p% U' UALGORITHM, A step-by-step procedure for solving a
* e0 G* f- m1 I! I0 V( \5 gproble- M. t7 U K) A0 m
s0 A) X. _, W- b
AIRPLANE FLIGHT MANUAL (AFM), The legal& G: H; O, y1 Y- I9 D
document containing performance and operating limits,
5 k& s! A% ]/ _& z0 d7 ooperating procedures, and takeoff and landing
. U% {% S' U2 M' O6 operformance.% Z* F5 q. l: {; V" h
AIRPORT ANALYSIS, A comprehensive set of takeoff0 d1 f8 J3 {7 j* o5 T9 ]' ? d
weight limitations for a given airport runway, generall
* H2 ^2 h. V" C6 F; z( J; c# G; X8 Xpresented as a function of airport temperatu R# F$ Z5 s( Q- ^( ^
翼面,
: q# B) d, Q1 j+ X" ~! D* Z用以从气流中获得反作用力(如升力)的表面。机翼,
+ X" \" X* }8 u6 L安定面和操纵面都# @: r: {( O! r3 ?9 _8 L* L
空
# s) {8 H3 ^+ Z: g- L+ a% B L* c! O空速指标" C5 B7 r) a1 p% m% `% `3 Z+ z9 |+ d; E
适航性,& g4 p9 H! y" N" A
有关气动能力、! @. D/ C2 [; B* x
演算法,/ Q2 f& d$ N. Y5 T% _) j
骤; A3 Q% V! H. P, |7 w( K8 N4 ~) {
飞机飞行手册(AFM),
4 Y! ?9 [2 i: Y包合性能极限,操作极限,操作程序,起飞和着陆性
$ W6 c! O( S. x2 C等4 p' L# K: f) ^" x t
机场分析,
- J R( H: _) n J; s一套针对给定的机场跑道的详细重量限制资料。通常与
0 T0 U6 T, z* L- k: L; @& }& i% w3 y机场温度、风、和飞机襟3 j. m4 r' D& a
英汉对照民用航空词典B OEING1 _' p3 }: ]) l, f- C
TECHNICAL DICTIONARY 7
7 I% P% y1 J. i: Z- nAIRSPEED BUGS, Adjustable pointers on the airspeed+ ]( K# J% V. F- t* f9 q! w
indicator.
& B/ t5 Q! N2 X n# W4 P" lALLOY, A mixture of a basic metal and small amounts
& C# Z+ x- Z" d8 w6 wf other metals to change the properties of the basic
, ~7 D7 h" M9 |etal.( @# n# f0 x) c b5 q
Minimum airplane speed.$ B% x( ~" j: z2 ]
e of
! Y% u( h/ }# X" v% Y9 k7 N% a$ gitting airplane angle relative to
5 D; j$ w4 L8 y$ y! A) H9 rirstream for the stall warning system.
7 o$ }! q2 q- \ G1 `another.
1 H7 h' c' b: v1 u8 ~LTERNATE , An additional airport selected during
5 C7 f: q' J1 L+ X, c) ~5 O,
$ z9 k6 `; @& R3 M/ y Z$ o合金,9 g0 e4 o' b9 k9 |
在金属中加人少量其他金属,而改变其性质的一种金属
1 H+ q; u+ N3 |! p! w3 [1 x合物。
. e- p$ n h7 o X9 {8 z飞机的最小速度。1 ]6 P( x3 Y+ ~, m
速警告系统传输飞机对
) l1 f/ Z( i5 T. T3 f流的相对角度。
+ ]( h0 V; r. l9 A+ y5 s( U由一个状况改换到另一个。, Q+ t4 A5 O. m8 V
降场,) t' ~9 j/ p* D+ ?" P' w; j; z" E3 e, ^
划时,除了目标机场之外,所选的另一个机
* ^% B' ^) ~' Q' `% `o1 f) w% Y5 o$ s4 O
m7 j$ H. k3 {# P, D+ |# I# q
ALPHA SPEED,8 C: |' w* R- V7 a
ALPHA VANE, A small moveable airfoil on the sid
, ^0 N8 o3 x! c/ xthe fuselage transm) ^" ?$ q8 x# Y2 f
a
5 m, ^+ Y6 \: V+ TALTERNATE, To change from one condition to2 c! `4 F, b1 w3 H5 e( O: t
A/ E# ~% Y, s3 x7 \
flight planning, usually near the destination airport, to be ]( e( k. B" Y7 t
used when it is desirable to divert from the original
% C; {* i* F/ x- `destination airport.
; |5 T( M, I4 U; F" @& F7 m! P2 K空速游标: P) p1 x) G7 {6 e
空速表上的可调指标。
& t1 g, Y$ _" K混/ K# H! s0 T* c; [4 u3 d4 }3 ]
迎角速度,; c, O" n# I" u/ e1 L2 x7 x; w
迎角叶片,
* ?8 l; A! b$ m# V+ p& E3 a位于机身侧的可动小翼面。为失
2 P& ], ?+ G7 n$ l1 _气6 _( q7 u' L- q$ I
交替,
% _, ~. e7 j+ ^: d9 g" j. d备
6 o8 W- V9 ]% @) w, K5 I制订飞行计
4 F7 S( D+ @# g8 h4 m& C- ?# O/ g7 N场。通常在目标机场附近,以备不去目标机场时,改降之
7 x) P Z8 D5 O/ Y+ e4 p- S用。; q8 X/ V# l4 n& a) f; h
英汉对照民用航空词典B OEING' P* k5 f2 t3 G4 x7 s
TECHNICAL DICTIONARY 8/ q/ C6 e5 C3 ~* @
ALTERNATE AERODROME, An aerodrome to which$ G4 a& Z9 |! \6 R3 C
an aircraft may proceed when it becomes either
" z! T; ]; @& e7 apossible or inadvisable to proceed to or land at the9 r Q& w; r0 H: _ I0 \; s1 q
erodrome of intended landing. ~; x$ o* U# b1 C) u' k. j8 G
TER SETTING, The adjustment of the altimeter! l/ R& x; w( B/ [
account for local variations in atmospheric pressure.
9 j* }6 p! L1 h7 }) D" DLTITUDE ACQUIRE, A digital flight control system% ]; y7 s. B3 U1 J, t
ode to transition from climb (or descend) to level flight.8 ] ?3 X k0 ^9 ?# }
LTITUDE ALERT, A flight deck alert occuring when the
$ z. O( _8 C. r* a) n" t8 Eirplane approaches or departs a selected altitude. n. K0 x# R' k* `+ U8 l4 _! b v' }
LTITUDE CAPABILITY, The maximum altitude at
' i; s1 z0 X" E$ K2 R* E* ^4 Lhich the airplane can be flown at for a given thrust,# v- O* K7 x$ V ^$ @$ \
peed and atmosphere condition.
0 a, x: c2 J, x5 cLTITUDE HOLD (ALT HOLD), A mode of the autopilot
4 E* j5 U/ V* D! ~r flight director to maintain a selected altitude.
8 W! e% z) ^% \! kirplane's altitude during VNAV operation.0 {% r6 W5 g1 U2 \. u
机场着陆时,可作着陆使用的 h/ m7 m y) X
场。
5 Q1 A" e; F! f,$ x6 o4 F2 N1 {9 \/ R
根据当地大气压力变化而对高度表所做的调整。. l! b+ ?' o9 B( g! ?
一种数字式飞行操纵系统,从爬升(或下降)改平的模/ l: _' p" [ p( G) D- V% a4 Z& u# r% P
。
e4 Q9 m' [- {' T0 u, H6 {* u$ ?+ n度警告,
& e* ?$ F/ }8 d2 c* ^( D当飞机接近或偏离选定高度时,所出现的驾驶舱警告。
/ ^8 i- X* a6 s! H4 m& g& J高度能力,
F5 ?3 p1 y" v# a4 D在给定的推力,速度和大气状况下,飞机能飞达的最大! e0 d8 p2 K( J4 T7 k! d. T1 H
高度。, G" [5 A. V; h) j$ D N
高度保持(ALT HOLD),0 K! n: w' Q- H2 T+ s. v% w
自动驾驶仪或飞行指引仪保持在选定高度的一种方式。
7 q& l) W k8 [& N$ p2 M1 @' [! ],
7 C) e: v0 t" m员对飞行高度的控制。/ ?$ w6 k' |8 x2 {, c6 A7 Q4 H
im
* V, g7 D1 W# B+ Wa1 T7 L' W# y( v1 s% q
ALTIME
, c8 n+ X4 t. d* A& V- z1 Sto4 m5 C+ l( T0 n
A
, i9 }' z) ~% t' ~, O$ C- q1 ~) J- I2 r! um7 u3 Y C' k4 m- Q( w/ l/ Q
A' L4 f7 Z# U& M. K
a: Q/ v) [# i7 r' ?; e ^. o
A& `: g5 v R. c8 w& L+ l
w5 } _9 H- N# n. E" o( B+ ~
s& E( `0 e a3 R+ l* Z
A6 D% w8 E/ m& J+ m! l
o/ P6 w8 v; p8 P% a
ALTITUDE INTERVENTION, Pilot control of the
& j l2 {2 r7 Ua
1 E; N- G' u3 ^# EAMBIENT, The surrounding atmosphere.9 r4 _8 ]' k3 h* v0 e2 A: Z0 H
备用机场,) G+ u; N! f0 u# d8 c6 |2 v
当不可能或不适宜在预选9 V3 U5 l$ z4 m: v
机
0 C' `3 E6 P. l! s. g高度表设定
1 n8 P. X, M+ K4 m$ A$ j9 n2 N高度截获,
8 W2 P3 |0 F \* u$ Q, ~5 h& p- t式
p% B7 Z) ]6 M. z- W高
7 M5 l3 j2 L7 L高度干预
: }6 O6 j6 A0 J- q0 k在垂直导航工作过程中,飞行
, E! A* K( ]$ M. k9 d. S周围环境(地面气层),! L% h: o0 ^9 }' R2 k7 M6 @
物体周围的环境(特别指大气)。- j2 u4 r7 _+ ~% A9 Q
英汉对照民用航空词典B OEING
/ `* h# t; ~4 }9 s. L' I* STECHNICAL DICTIONARY 9
9 Z. J- d' v* p. U* HAMBIENT PRESSURE, Pressure of air surrounding an
& i! e& B' M' V+ i0 ~object, measured in pounds per square inch (psi) .( x9 v# D) c, `3 H' m; l9 C$ }
MBIENT TEMPERATURE, Temperature of air
: c0 y. c) N2 Y' |mpere.
# z2 S: E! O2 _8 e9 Iurrent waveform.
9 N0 @7 z0 u2 ~5 z( h) X1 ]g an* O$ B5 x' {: u, o: p! d
nalog signal to a digital signal., Q1 Q$ V! ]( E! J+ L8 A6 ^
ore inputs7 ^+ k* f3 ^4 ~* M0 r/ ?3 [
f binary digital information and one output. The output
& m. Z+ E% J3 E) h. W; o1 only when all of the inputs are 1. The output is 0
2 C, e! \: [ a, t+ B( j6 ohen any one or more inputs are 0.0 p! @, t$ B' E2 a, B1 a" S6 i6 f3 `
面气压),
# ] O! F7 t# @- v/ @9 G# o境温度,$ M7 U$ o, D' u) w: {
气温度,用摄氏度(°C)或华氏(°F)来; L5 p/ T% b; U) Z# z Y" n
。
1 {5 h$ O) V8 T2 m9 ^电压或电流波形的幅度。5 Z$ G( b X$ S0 l' A
性变化的信号来工作,或产生连续性变化的信号6 q' ~1 i& ?- @: j6 k
统。6 u2 H% e! C+ T* J: ~
将模拟式信号,转换成数值式。' U2 d# O( r. K! A, C* J! v
一种有两个或两个以上的二进位数字信息输人,一个输% S. G8 [. C/ X
的装置或电路。当所有输人为1,输出为1。当任何一个4 ~0 w7 `& ^) K* [/ L e3 M# m. t- B
一个以上的输人为0时,输出为0。% R+ a, H! }5 r$ c, N0 |
A
. ]2 @! a& V2 |+ C8 P- }) E# ~. Dsurrounding an object, measured in degrees Celsius
) N& B8 c2 N* Q1 ~(°C)or degrees Fahrenheit (°F).0 x- {! t3 y9 l2 z
AMPERE, A unit of electrical current. One volt across
( g2 S9 |3 Y% V# Zone ohm of resistance causes current flow of one# s5 c$ q+ Y7 s# S
a
4 K9 \/ S3 _' n: [( x/ BAMPLITUDE, The size or magnitude of a voltage or0 M9 e1 J# \2 L4 i; @
c7 N* U3 d- P7 S& B/ h9 @7 j1 i
ANALOG, Quantities or representations that are
8 c8 U% D$ n- |" ]& bvariable over a continuous range.2 Q6 @9 G6 r- U* g8 N* M
ANALOG-TO-DIGITAL, The process of convertin, A$ {" ?$ s9 R
a, w( b8 Q& s" d+ U C4 N9 p
AND GATE, A device or circuit with two or m1 @. m! f; T: A- P4 `( A( b
o& Y5 |" B5 |; r* N1 K
is3 X# }$ V. o6 B
w
* x8 W9 l1 [$ l4 }! {, o/ c; p环境压力(地5 C9 D' H% z9 [& u& U: Q
物体周围的空气压力,用每平方英寸多少磅(psi)来' u. s* z$ ~1 ~% D8 _6 _
度量。4 Z: F7 j4 {1 \+ A
环' x4 R! N* c6 a- a
物体周围的空# @( {" @" t7 d( N
度量。
4 H# Y, i2 S0 d+ q% {) l! d安培,/ k1 {+ q5 e1 |/ i2 J" N
电流的单位。3 a" M% N: N3 N4 ] Y
1伏电压在1欧姆的电阻上所产生的电流为" q( C8 H6 H6 z Z8 ^8 K
1安培2 l( T* d* c! \( W2 Z
振幅,( C8 {0 d! T; _& b$ W
模拟式,' c' _( T$ z3 p; z* q5 z. o
用连续
9 P' y( D6 P% V6 ^+ G" M# a系8 `% |- j! v) J4 J
从模拟式到数字式,
% ^# z0 y; ~ }$ I与门,2 W( T0 G% y" _* p1 W
出1 K5 H6 u9 G" v# t/ u
或
7 L: z" v8 D7 A" L7 ?, r( k# Q英汉对照民用航空词典B OEING0 {9 A, i/ G# Y9 y
TECHNICAL DICTIONARY 10
: p) I$ c0 w8 OANEROID, A sealed flexible device containing air at low
; e }$ J- [! G) e2 K6 B" Ypressure, which expands or contracts during change of
, |& o( `/ P8 b$ mressure outside the device.2 H& {3 M2 l6 c% f* `# B
ically
! ^& j% B* M4 K+ _3 K, c5 Nr changing the direction
( @4 i# y" z4 Qf drive. u% s! t* o4 s0 j
of the wing chord in* `: j4 s& x. _$ _
lation to the free stream airflow as it moves forward
% a* K$ n0 Y7 d, Q& @9 F4 yrough the air. q* i' a0 ~+ k' Y
al axis of the
& H. e0 ~, I4 R& H' g/ y6 |5 Laircraft.* U2 I, |# u" m. {+ _ Z
胀或收缩。
; s- C6 h- P3 F! e0 ]箱。是改变驱动方向的机械装置。
{/ n! p1 i4 i+ c( B机翼翼弦在空气中向前运动时与自由气流之间的夹角。! N1 d" B, \8 G/ t3 q
。
0 X, Z- ?! q0 v Q, ~6 F! E; u0 jp
3 ?7 E) ~3 _* K6 d# ~ANGLE GEARBOX, A part of an engine, mechan
: i3 G' L* j4 A$ w/ s4 Z( ydriven by the compressor, which drives the accessory
, K$ O- P5 O# T3 Q) E- Ngearbox. A mechanical device fo; b% c* p1 B- @9 Q3 \; q. b1 ^- w& i
o
5 Y g" r( u' T/ I0 \6 j( UANGLE OF ATTACK, The angle
$ s. z: Q4 V2 w. tre; ^ f- ~- a4 B3 n T
th
$ m- q7 I% ~3 e2 G: ]( l5 }% u" H- CANGLE OF INCIDENCE, The acute angle which the3 l( C! q- h+ W0 T
wing chord makes with the longitudin
2 I5 \7 {1 o7 p8 K膜盒,
p3 K8 X6 o& \- r7 V# U$ O内含低压空气的密封弹性装置。当它周围的压力变化, m: M2 Y' [4 v: @9 \% T
时,会膨, p1 J! x" a" k0 c8 b
伞齿轮箱,8 W1 f, O4 ~! ~
发动机的一部分。被压气机以机械方式驱动,然后驱动
. j# q! Q+ R. b& }* I, [附件齿轮
% C! a& K3 M$ \4 n迎角,
( A- p/ Q. Z" z5 X4 O安装角,
. u1 D2 | y. ?+ X飞机的纵轴与机翼弦线所形成的锐角
" f: _* Q$ E+ n0 a$ r, m- i# b英汉对照民用航空词典B OEING
/ u* A+ U8 o0 L) m4 Q+ z" QTECHNICAL DICTIONARY 11. i, R* Z* R4 y2 I3 v \
ANNUNCIATIONS, Audio or visual indications used to
2 P# I+ ]/ ~9 O1 Ccall attention to an event that has taken place.
" B# X9 Q7 Q. M. d% c. DANNUNCIATOR, A visual device consisting of a number
& U% _/ t5 s2 h7 A- [& O* Oly.
7 q6 t! H: K# {$ a; l. y* oANODE, The element toward which the principal stream
1 g. L" n# B. o5 }( J+ B2 Wof electrons flows.+ r% D2 p: p5 F) Q4 O
ANOMALY, Not normal.
* a- n% }7 v' H( {3 t8 r+ xANTENNA, A device which, used in conjunction with a8 b, y6 G0 a2 H+ ^
transmitter or receiver, is used for radiating or receiving
, W( i3 c5 m' c' ]3 b1 ^0 Cradio waves.$ ~: x8 A6 O2 @" R$ `
NTI-ICING, A method of preventing ice formation on
* G F) g0 {9 ~5 Ye wing leading edges and engine nacelles.- H$ s5 B- I! E o( v* e4 C
NTI-SKID, A system for providing maximum braking& X4 ^% L1 o. c! E: s. K
ithout skidding for any runway condition. Anti-skid+ Z: t! F" V6 ?' j6 ?( ?& H( x4 w6 f# ]
omponents are part of the brake system.
/ [/ j: ]) r4 s告,) j9 ?: ? D8 c* B7 I. @) @( S
当发生事件时,以声音或目视指示形成的提示信号。0 q( j' p( b; _" d# K
与之有关的电路的现有情况或已存在的
, p' q$ D; u; L8 W0 {) t况
1 Y$ ]7 F% O9 A ]8 d正极,5 a, t6 s# W, [$ ^8 ^6 E& Q. c3 A
主电子流向的极位。8 W# { }! h. \& X
异常,# l/ J% p8 `2 b, u% f) O( N
不正常。( Z' }$ Z) |4 R
天线,1 f" U# X$ _0 Q! P d
一种与发射机或接收机共同工作来发射或接收无线电9 h4 A/ F: ]1 x9 v! W" L8 ] M
波的装置。
; X: z( z+ z& P冰,
7 S, o+ V( s' P, W" R1 c7 `$ S防滑系统,, l# S! _( j! G' h; s5 R3 @
一种在任何跑道状况下,都能提供最大的刹车能力而不2 L$ v) L2 l9 T' w1 T9 O
使轮胎打滑的系统。防滑部件是刹车系统的一部分。1 z+ E2 R# ]5 x. U* N2 Q6 C+ S0 d
of lights. Each light indicates the condition which exists
2 k7 I) q5 _" y% A- n/ yor has existed in an associated circuit and is labeled9 c" o9 b$ C6 H7 j$ ~
according
. z* w- G# u' \. x$ \8 w) E9 _5 @A$ P5 v! N- `: X0 d
th
' Y9 ?4 r) ~% `9 kA N& _4 M. m# |2 m" l! n, K% A. P5 M
w
" V0 n. \( R: a& X4 c% ?c! q$ ~5 V7 q6 c; z4 J
通+ _' U' p) V- @: P j
信号牌,
8 j2 t: v+ P7 D由一系列指示灯组成的目视装置。每个指示灯都有相应( H, K+ {# p% [8 w9 J5 P
的标记,用来显示. g; l3 ]; c, H
情
9 i; n9 I. R' X) `+ n9 V( V防
) u! U( h3 K- r2 U/ ~防止机翼前沿和发动机短舱结冰的一种方法。3 e; x* ~7 {6 @9 P1 y$ U
英汉对照民用航空词典B OEING
/ O% y" J5 @6 I0 K; t' ~1 |0 J ]TECHNICAL DICTIONARY 12) A) Y. l5 d7 G0 g- @
APPENDIX, A supplement to the Airplane Flight Manual
" R' E* o5 c* |tained in the basic manual. A
- p: i8 T& p1 s, V3 L* A& oollection of supplementary material at the end of a
+ A F4 `9 b% pook.7 L7 d Z) W7 d- N) K/ ^# |
of the
, `# u" ]" Z' U3 }rsion link on the landing gear.; [* N( E6 u- x; y
APPROACH MODE, An autopilot/flight director mode
, T5 F; A& `2 u9 _6 {which is a combination of localizer for roll control and6 a. {$ v# M6 U- f8 T
glide slope for pitch control. This mode is used when full
. Z0 _! W$ R% f8 w7 z! Minstrument landing system is available.
4 {* }$ [1 k5 L" X) C( WAPU, SEE - AUXILIARY POWER UNIT
) t) p6 s9 X8 _/ a N+ S: CARINC, SEE - AERONAUTICAL RADIO9 [& r+ S. Z9 g1 X
INCORPORATED
9 v" O8 M" b$ G$ U# O. I6 O/ ZARM, To make ready for operation.0 j P8 [- [0 o) u |0 j
附录,
' U- t1 C6 x4 H0 M) p飞机飞行手册的附件,包含基本手册中未提到的飞机形+ h! e, t% Y3 i D1 K% n l. x
态的其他性能。是附在手册末的补充材料。0 {7 E$ R3 [. s
顶销,
5 { J8 X- r; I( g# M用于连接起落架扭力臂两部份的销子。
9 Z. q! M( \2 ?8 l8 X5 L9 J进近方式,
# m3 b4 f2 f" D$ |一种综合了控制横侧的航道信号和控制俯仰下滑信号
6 G Y! w6 t, v- b' b% I# S1 j的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系
% g8 l2 ^6 U0 c( s3 i- e1 S. D( i统正常时才使用。! H8 X @) j. F; W- A, m% p5 B
辅助动力装置,. G" J3 i+ T& k2 s
见Auxiliary Power Unit6 F) n/ {% Z# j) O6 m
containing additional performance for aircraft
@/ A+ g$ ? `3 b3 tconfigurations not con7 l2 |* j- ?5 _" Q
c) |- u4 p. N. E& Z" q4 c+ Q
b3 i/ s+ L0 i8 r
APEX PIN, A pin for joining the two sections! g5 V: J- n! n- Q4 _8 V
to7 x+ U; z5 a# d% L8 r
.
8 s5 i% t" p7 N7 r5 }7 v航空无线电公司," A+ ^1 p$ Z+ P1 i
见Aeronautical Radio Incorporated.
& x. I) }" Q; i- m- H$ I$ T3 Z0 `1 J预位,% L$ e1 m5 v" e; B ^: t- `( J
部件可以开始工作的状态。7 _9 i! h2 }9 B; h. I. m" |
英汉对照民用航空词典B OEING6 o" u/ f9 w" F! B w
TECHNICAL DICTIONARY 131 D$ g. Q4 z7 i# I3 h2 d0 ^
ARC, The curved track over the ground of an aircraft, l" F3 a! P3 I* u+ `
flying at a constant distance from a measuring+ M% T! P) b" m) `! c
equipment (DME).
2 ]5 E/ s& E3 |- _/ C0 B1 O7 }in the limits of self-contained system
1 D% x2 h3 l3 sapability.! u' P7 V4 D; c4 `( l# I
tem for opposing or restricting3 L8 R! p# a9 L m
ovement.
8 v. M8 {( j# h" }* Z) ]SPIRATED TAT PROBE, A sensor that measures total* d5 f( ~, ~. P/ t
ir temperature when the airplane is in the air and that9 A1 I! q$ R6 `% Y2 q7 \3 K! {
easures outside air temperature when the airplane is
3 v R# M5 s9 |2 r3 S, c% G0 fn the ground. The outside air temperature is measured
4 i/ I+ \$ a. t. S9 Z& p( LSSEMBLY, The fitting together of a complete structure
6 m' z3 W2 g3 P- ~* h' MSSUMED TEMPERATURE REDUCED THRUST, The
# A1 i4 ?" @- H! NATC, SEE - AIR TRAFFIC CONTROL
1 Y7 g. [" g4 P0 v& J/ V,) G( q- r/ l, [# E8 G
系统中所产生的一种用以抗拒, J- c$ K# a5 }
作或限制动作的力。
" b7 X9 L6 H9 N% v) |( f, @3 M头,
8 n9 @% i# S7 o用来测量飞机在空中时的总大气温度和在地面时的外
+ `# I0 b1 e" ~7 K- e6 J% t温度。地面外界温度的测量是利用引气将外界空气吸入
6 y" l6 G D" R y' M头,以达到测量的目的。3 v& `8 y- h: }. k, f! Z
配,
" [. ^7 M$ I _5 A2 H7 I5 P& D一个完整的结构或组件的过程。
, L9 z' B" x; d假设温度而得的减推力,
. s. \+ z. W8 t p+ d1 [. w9 ^0 {推力设定值时,假定一个比实际外界空气温
" E' e- i u1 q' |5 L空中交通管制,9 y9 Q# K- x& y, Y/ {/ ]7 Q
见Air Traffic Control
2 T9 S9 s( F2 A, yAREA NAVIGATION/RNAV, A method of navigation1 ^/ J h2 r% {# ?& Q
that permits aircraft operations on any desired course
- s+ ~% k% I- ?9 j+ F1 S% `within the coverage of station-referenced navigation
S7 r& s& @: Y/ q9 Psignals or with
; `+ v3 | R% rc
) W2 G% U1 {& b" tARTIFICIAL FEEL, A force developed in the flight
9 U9 C, _4 y. K, gcontrol or brake sys9 \" s! i- [% ?
m
0 B# x: E7 v5 c% ~4 ^A1 Y2 x) Q }- Y6 ^
a1 c" [8 d4 g& K) u
m+ A O* O+ F/ _, W r/ T. y2 g, R/ O
o) K& Q. M1 S/ q, K
by using bleed air to draw ambient air through the4 T+ n1 X3 d' F" w5 V; m: h
sensor when the airplane is not moving.
4 }& G& z' ^' L3 F9 O- ?1 v0 S+ `A) G$ D9 x' g B, D* f
or unit.- L5 R6 o/ n- f4 n$ b
A$ P- l' o/ P: r! q
lower thrust obtained by setting a higher than actual
0 c$ z& h! i* Z+ P6 ?% ^2 V& mOutside Air Temperature (OAT).
) y4 M/ ]& U T# p# L* q弧线,
% b" i! A" i! _3 r4 `7 b飞机在围绕DME台等距飞行时的弧形航迹。% ~3 C: V/ F% s$ L) M
区域导航,
. O2 \3 I) N$ v: }容许飞机飞行在有电台参考的导航信号或自备系统能
% [9 R0 C0 L% b# |力极限范围内,飞行任何预定航线的一种导航方法。# t& U1 J" j4 }' L; I. E
模拟感觉; O3 p+ l: M- f& x; j/ b
在飞行操纵系统或刹车4 M* Z" r8 b8 u" J; z& |
动
( ]. ~, C5 w! h) R- S吸气式总温探
3 I% @+ {/ c0 f% U, ~5 X' U( O: [界
1 X7 p- M6 [" _; @探8 M$ T: u# r: g
装
1 S% Y+ J R" K8 w- D组合成) | [1 |$ `8 v
由
7 ]$ j6 n* f" w9 F6 ~在选择起飞
: f8 D l2 x4 x1 f, F! q度高的温度而得到的推力。用这种方法可以减少发动机的
; n3 f4 X$ m. u2 H8 m0 X4 [磨损和维护费用。
0 D7 h6 ^ f/ |& i% a6 B.
M; a! [4 e9 N: U英汉对照民用航空词典B OEING$ x* Z" J+ p6 U) t9 U1 {$ ]
TECHNICAL DICTIONARY 14
4 X8 A+ K0 o; M. i. r* Q/ P0 y+ tATE, SEE - AUTOMATIC TEST EQUIPMENT Z0 Z) s6 Z0 _, v, Z
ATMOSPHERIC PRESSURE, Pressure of air due to the7 p; W' \, j( n+ ^1 D
arth's atmosphere, expressed in pounds per square
' L0 u6 Y- @5 |" jch (psi) or inches of mercury (in Hg) or millibars (mB).
, i4 X. S# U( ]- \% [, f9 @TTITUDE, The relative orientation of the airplane with! z7 s- z' B4 _% l) }# h
spect to pitch, roll, and yaw.# E- Z) r$ b* Y
UDIO CONTROUSELECTOR PANEL, The panel in
5 t% U/ E4 u3 n1 q/ {" f# G+ ye airplane which controls and selects the routing of
) g5 n& R2 m& m5 K( R0 g- v, h6 _, |udio.
, ^' l* c) {. q u6 ? @UTOLAND, Automatic landing using the Digital Flight
7 i* N6 [* X2 N% Z" Control System./ ~6 ]- h$ g& T+ z" n
n.
3 e" ?8 G8 M7 c, [: L# U3 n$ ?M, A system7 d4 P+ x2 Z1 ^% Z- [+ V4 V7 X
omposed of all necessary subsystems needed to guide& _: E' x- ^. n# o0 ~8 o: v
e flight of an airplane.& R) a$ @* l, v" v) I
EQUIPMENT, System test
- }& G8 ?# h4 k! j5 Q2 iquipment that operates under computer control.
& t/ ~+ v/ F+ M! ?' g装置, |
|