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AIR DATA COMPUTER, A computer which produc/ I- d, w* _9 O* O( G) U
data information, such as altitude and airspeed, based# B% T m5 |5 n, q; n9 J
on pressure and temperature measurements.
9 S" ^- o: [2 i& i3 F- E+ Pes air' I/ J3 G9 k3 q7 q5 B" m. m$ A* W
IR TRAFFIC CONTROL, A system comprised of3 p+ n5 i. _7 f, `
round and airborne components used to identify, track6 s# B2 M& C( l/ e) f9 Q
OUND SENSOR, An electrical device operated. `, b2 i: v/ T" g. z/ X. ]
y the landing gear, which transmits on ground/in air
5 |7 p7 F& {. |* wformation for system operation in flight or on the
' [9 [* H1 o9 S% i! V, sround.
1 A ` Z. |+ y8 ~0 p5 `2 xIRBORNE VIBRATION MONITOR, The AVM takes% Q. w1 u/ W5 `1 X& Q8 j6 C+ [
e signal from the engine mounted accelerometer and
# J! y' N3 G, R1 Balculates the vibration on that engine.
9 V+ x! H& f2 X/ B( fcorridor equipped with radio navigation! G; V# ^/ \2 l
aids.( n7 L: V' O% P$ y+ [, |0 I$ j: B# b* n
AIRCRAFT (or ARINC) COMMUNICATIONS* H, W; H: A8 O5 N9 b; |
ADDRESSING AND REPORTING SYSTEM, An1 M$ u& T- C4 e( Z7 k6 n/ i
addressable digital data link system which permits the
1 k& |4 ?/ O& E- f1 H9 nexchange of data and messages between an aircraft7 }6 g& H9 V, C/ B, a
and a ground-based operations center over a radio
; K5 A; x$ [" m" c5 { o% b7 `network.: f/ _( _' x: W$ V
AIRCRAFT CONDITION MONITORING SYSTEM, A- [5 z- x" A: {6 M$ [" |' i
system of sensors and recorders to monitor various1 U- T9 \ ~: K& z3 q6 {5 f' h" l
airplane systems' performance and status.5 M4 d& Y! l0 i ]4 W
机,/ N. Z3 R- C" Q0 M
中交通管制,
+ K' G$ L) m+ u @一个由地面设备和机载设备组成的系统。用来对飞机进1 E5 K7 L1 }. n2 M
地传感器,
! A( ^9 N z- Y一个由起落架操作的电气装置。用于给空中或地面的飞
2 r- `& D* f( p- F' c7 M系统运作传输地面/空中信息。(有些系统只能在地面2 {* V6 O1 J3 d' Z/ m2 ]. x+ o
用)
. E8 Y! k5 \1 s& ?% D载振动监测器(AVM),& K/ U) \) C! Q: B2 V" X$ [- _
AVM从装在发动机上的加速器取得信号后计算出该发
& H( O* c: C* b机上的振动。
' N- X* ~5 i9 e1 Y' n4 }式建立的控制区域,内有无线电导航设备。
" z! l; X8 ]: x; W' ?% Z1 ]飞机通讯寻址和报告系统,
: Q5 u3 e. `. x有种可寻址的数据通讯系统。利用该系统可使飞机与地5 p" P- B2 ^ J! g& R
面操作中心通过无线电网络进行数据和信息的交换。
+ h# Q. E- i4 N" S, O# V0 K' N# I飞机状态监控系统,
) H0 e& |' G2 K S$ a( W6 L9 h" g( I一个利用传感器和记录仪对各种飞机系统的性能以及% Z1 N2 |* q0 e
状态进行监控的系统。
7 I! r. m* l0 Y/ |# M# c+ pA# |; f1 q2 |; Z# m' k! |" U8 B
g
/ Y" Y2 A" D5 `. C( C4 V! J' Q, Vand locate aircraft.* X& x' V9 J2 u: ]$ r% l0 ]
AIR/GR
2 B8 k4 i" M4 Z; l9 Jb
6 V0 z x, `' g" F4 ~$ Win
2 Y4 S% G/ R/ A9 T' O* w- P2 m( vg- Z# u6 F* M2 }: `/ s+ f) ~9 B, @# l
A
* ~. G0 _2 ^7 {* Yth+ M/ V6 u) v5 h. v* W. P; ?' j
c9 N, U( G, N) I
AIR WAY, A control area or portion thereof established q# M& Z/ i5 C$ u
in the form of a5 J `8 P: M; O% j( A, V& e
大气数据计算, T' i& x& V% Q* U
根据量取压力和温度而产生大气数据资料(高度、空速5 h. a# [, }$ n
等)的计算机。
0 J' D T/ O5 H: v$ t/ x4 w空/ S$ z9 |6 x# P) H' v+ Y( t" @: v9 x
行识别,跟踪和定位。, ^; o1 m/ I' R2 z; L$ i+ U
空$ x6 E9 r% x& s2 R3 G
机0 Q' e! z$ t1 m ?
使
$ a' E/ D4 f) T0 u' ~; B# s机
) @$ i- l6 L3 m! I1 P动7 s- f! p1 v ~4 i
航线,
- Q) [( ]* I4 H3 U+ J" J以走廊形5 Y( M: z6 H' e! j2 F1 s6 v, S
英汉对照民用航空词典B OEING
& U8 h1 [) n- xTECHNICAL DICTIONARY 6% {7 Q/ q. b; O4 V* ^3 x( g+ U
AIRFOIL, A surface designed to obtain a useful reaction,; k7 D1 n7 C4 u% c
such as lift, from the air through which it moves. Wings,& J- w1 H5 w7 k
stabilizers and control surfaces are airfoils. L; p- y5 h* k# a- @7 g
AIRSPEED (IDS, TDS), The speed of the airplane1 j6 T. p" a/ s8 G U. i
rough the air.
6 |" g% d$ B: V1 ?& w) B: W8 M" d oD INDEX, An adjustable pointer on the
" Z0 h& }6 r; r+ A7 |- |# `irspeed indicator.
; C. i* a& o. `3 K, Z1 Cand legal ability/ U+ X/ W+ I6 _
fly.' k: N8 {5 G( [* l) u: w0 c3 t
m, for example, the procedure for finding the
. C' p9 n8 F1 b) dquare root of a number.
2 J. i0 G$ g2 S( ~# r v2 o- cy
* G' Z; u4 v& p9 Q) C* d0 X4 cre, wind,9 I- `, N; ~3 J9 S
and aircraft flap setting.2 A8 L; _" B% `. u
是翼面。4 ~) _( c# K9 n* g) M) D
速,
( I7 Z7 s+ }# F! F0 e$ h0 e0 H0 [飞机在空气中运动的速度。2 l; S: a' G! n& T, z
,5 b7 v' b/ [' o4 F, F& I' h
在空速表上可以调整的指针。
& u3 W$ {3 _! C$ z9 s& H1 z机械飞行能力、和合法性的飞机状态。7 R x+ m1 Z Z! R
一步一步的解题方法。例如,计算一个数的平方根的步
1 D3 @* C7 T4 K) I9 V/ |5 Y。6 n, ~$ l9 i. w, O; t9 N" D
能3 t6 ~7 m( N& u$ b Q$ R( e
资料的法定文件。
( |8 W O: e3 {7 D2 c翼位置成函数关系。7 q5 e* v0 d6 Z. N) m
th
5 r: u% f' t: EAIRSPEE
& J2 X0 M/ G4 c9 ~; Ba
3 N9 D% ?6 d8 U# A2 C# @, ]; { q5 WAIRWORTHINESS, The condition of the aircraft with' x( S/ w+ j& E% ^
respect to its aerodynamic, mechanical, V* }; ^& N5 v( D- z
to
+ @' r2 x# M' z# JALGORITHM, A step-by-step procedure for solving a
# Y+ b$ Y0 l! p0 e3 N" Mproble& @, L; H- n A3 C; {' D& b
s
0 r1 R0 m8 m/ l: d+ M, ^$ k qAIRPLANE FLIGHT MANUAL (AFM), The legal" R2 B% y# U! N2 k5 ? l3 H
document containing performance and operating limits,
7 p' M3 T# Z. G/ ^1 s- A) p$ Noperating procedures, and takeoff and landing2 s( B# |3 l9 V
performance.# q9 `# m6 m8 Y5 }# N7 f4 J, e
AIRPORT ANALYSIS, A comprehensive set of takeoff
$ c4 ?1 M. j! Pweight limitations for a given airport runway, generall
& k; Y1 k2 R R0 q. Qpresented as a function of airport temperatu
9 k: S; y( a2 r0 k/ U! Z K翼面,8 D' Z/ T& q; z+ u. E
用以从气流中获得反作用力(如升力)的表面。机翼,& R% m; K, b z: J5 O3 T- b9 g
安定面和操纵面都
2 E* R) m& A% \空6 \$ B# Z/ `& K. O' b8 ~ B( D ] P
空速指标/ n6 M5 D3 b" Y# z9 b8 C" o
适航性,
( Y: _5 W3 Y7 N8 a# ]; i1 h有关气动能力、& E; `5 `4 \0 D5 F/ C! ]
演算法,' i; N9 ?, B9 R+ d6 _8 J
骤
3 W9 |3 u. H0 ]6 X( E飞机飞行手册(AFM),
! F# _0 p4 z$ M/ T包合性能极限,操作极限,操作程序,起飞和着陆性
: g# |& ~/ j: Z2 M) g等, b5 E' U. C6 P( f. Q, R- d7 Y
机场分析,
! {+ h% v' b0 ]; s4 e一套针对给定的机场跑道的详细重量限制资料。通常与
% Y/ L( h6 q7 |$ n机场温度、风、和飞机襟
; I6 [3 H& m7 D' D9 \英汉对照民用航空词典B OEING% y# G. C; {% @) g: @& v% v
TECHNICAL DICTIONARY 7
! |* Z$ r% z5 J9 l1 @) l; O- u0 Y5 hAIRSPEED BUGS, Adjustable pointers on the airspeed( v6 p6 K# d/ f% L% W( Z2 @
indicator.* w4 t z J0 z" o) H
ALLOY, A mixture of a basic metal and small amounts
# L1 m% y, B' U6 h: _( S- Cf other metals to change the properties of the basic
' C2 c: G L# ~& k& E8 wetal.) c& o1 a# Y, Z0 W, F
Minimum airplane speed., V! Y3 j! r! ?! ^ h& l% z
e of8 k0 c7 D3 c! G2 k9 D
itting airplane angle relative to3 n! j1 l; o2 U1 j, P6 q, r+ q2 h! P
irstream for the stall warning system.
8 G! @5 s, z0 j) L% ganother.
/ y- S( I; |6 V9 bLTERNATE , An additional airport selected during
( Y! c. f# k/ i+ n0 K& r' T,0 \6 e( P6 D% h# ^6 I; ?
合金,# Z7 `6 ^. c! p2 m' b7 d) f3 e+ K
在金属中加人少量其他金属,而改变其性质的一种金属
( v5 r: x8 {$ p8 i5 L% y6 S; v合物。0 u% j. H' r2 d/ [6 E5 K+ ~
飞机的最小速度。/ a( u- V; j& R$ j$ G% w/ T
速警告系统传输飞机对$ S2 L, F/ Y+ P! L5 X
流的相对角度。( a" S8 `9 W& I
由一个状况改换到另一个。) t- ^8 ~+ G; l5 I* T
降场,
; h& B& z; i9 M l2 ?划时,除了目标机场之外,所选的另一个机
" H* y U4 L' U: h/ r1 R7 p- m* Xo
& e$ `+ w9 S8 P$ w C1 Mm2 }* }$ G: W: j) D( i
ALPHA SPEED,! Z, I) V/ }; ~* Y4 M; o& w
ALPHA VANE, A small moveable airfoil on the sid
5 R8 j8 T+ @/ k7 kthe fuselage transm
+ w- W; o& ~ D) a9 va' J7 I. Z# d3 t; Q4 J; C
ALTERNATE, To change from one condition to
3 d9 O! J, L( g7 ?- ?- eA# R& w) g% W1 t9 Q: O5 |
flight planning, usually near the destination airport, to be
" ~3 T1 _1 [( N2 X7 h$ lused when it is desirable to divert from the original8 l5 f+ ]* M2 J L
destination airport.
! T. E) o7 x! L2 u( y1 z1 D空速游标6 O3 T+ z/ n( b8 K
空速表上的可调指标。
0 @. S2 t. o( z0 F9 s- e) k0 @( [混+ d0 d5 }1 `( m
迎角速度,/ z3 u* v, U! j/ v
迎角叶片,
! Q+ z' f& }: E. \0 |: @; E位于机身侧的可动小翼面。为失% p$ b( o6 W/ R" U" ^ W! @& r
气
" j+ l( {. W/ u; P1 g5 K交替,
& D/ z! R0 _' l* D0 P备6 u$ R1 V* R4 w _- X! e. d5 f
制订飞行计/ c( a4 U* b% ~) n( t" C
场。通常在目标机场附近,以备不去目标机场时,改降之
7 R, [3 Z/ n. @/ [+ k用。4 Q! O& v3 Y0 m) m7 P- E0 W
英汉对照民用航空词典B OEING
2 }) D1 Q+ _4 B% @4 S4 LTECHNICAL DICTIONARY 8
% O+ C: u. _' `* y7 B. vALTERNATE AERODROME, An aerodrome to which
. v8 I: c1 ]7 ^( m' V" Nan aircraft may proceed when it becomes either
0 v8 A' x# B. G2 T) ipossible or inadvisable to proceed to or land at the5 {! g& o- U3 F
erodrome of intended landing.
" q* r5 d) p6 m' c$ d5 e* ^TER SETTING, The adjustment of the altimeter
' x; D) c, F$ Xaccount for local variations in atmospheric pressure.. e9 e6 ]* N9 `' g! ]# M+ [8 E/ F
LTITUDE ACQUIRE, A digital flight control system
# A4 N, p, Q/ dode to transition from climb (or descend) to level flight., m" O2 V- E M
LTITUDE ALERT, A flight deck alert occuring when the
0 j3 L3 [' F7 f# l- i; Virplane approaches or departs a selected altitude.
0 a) f0 t* v* y5 _- jLTITUDE CAPABILITY, The maximum altitude at$ s& f* s# F5 K# b0 W) q
hich the airplane can be flown at for a given thrust,- h- l! B6 [& _9 M$ q F/ }, v
peed and atmosphere condition.
! P, I! a& f/ q. @* nLTITUDE HOLD (ALT HOLD), A mode of the autopilot- @* v2 F3 Z: ~% Z
r flight director to maintain a selected altitude.
+ x9 q5 ^1 g% w% Z! {$ ^' {; G- {2 wirplane's altitude during VNAV operation.
2 G& c% B+ C! ~1 C7 H机场着陆时,可作着陆使用的
) ^8 r. S' T8 c$ Y! Z# z场。! R9 k7 A s3 j/ s2 q
,
% }. W& R2 }3 J根据当地大气压力变化而对高度表所做的调整。
3 Y$ G6 h% f z( v& e; ?% z& f& K6 B一种数字式飞行操纵系统,从爬升(或下降)改平的模
$ [3 I' a# \9 @: _8 ]3 L+ P。8 U) i9 i$ x3 d: b! S# Q
度警告,
( Y# j6 _! ` ~: A( P当飞机接近或偏离选定高度时,所出现的驾驶舱警告。
, ]& S# q. t0 l9 ~7 H0 ~% V高度能力,# ^, f9 R) q1 W& s" e
在给定的推力,速度和大气状况下,飞机能飞达的最大
! B4 z8 v; P: `$ k高度。
) i0 V* J3 D& i& u+ Y) X高度保持(ALT HOLD),4 }; t7 H- }5 \: s, F5 }& b0 j" [1 d; m
自动驾驶仪或飞行指引仪保持在选定高度的一种方式。
+ y& n% s7 B( [4 f,& L% |# S: E0 }" A% N
员对飞行高度的控制。
3 \ ?# ?& ]: Y7 Q: U9 U7 i Z# Vim
' m/ R) C, b; g5 K9 Va$ R" h* }& S$ h: B0 m" o/ c
ALTIME
) F# Y6 l. D6 l: a7 pto
, E y/ |; `+ l5 i# IA' z R/ E8 U5 d, K& A+ F
m
" l9 I1 _8 k/ ` V' k6 A3 o/ X# OA! d& Y- V8 ^* D6 A) U# \
a$ z, D9 z/ G$ y0 ^
A" g% y9 d$ ?8 ^ D" r4 k
w
" P7 C& r5 D2 m" }, }s
+ O( V6 D Z& K0 k9 {7 e6 mA* c+ g8 K7 w7 O& G6 Y; @
o
) A' H: D) r; W, P g& ^( C& yALTITUDE INTERVENTION, Pilot control of the
* C: J$ M/ F6 v; Z4 F( q a; y- s* La7 Q3 A' `$ D& d0 d# }& v* U
AMBIENT, The surrounding atmosphere.2 C4 c0 P+ Z4 C5 c+ E+ E
备用机场,
, e/ H( ^$ }0 a# m6 o当不可能或不适宜在预选
* V; X- _- Y# k8 z& E* \机
7 t: m$ A( d, a& {- K- Y- ]$ d: }高度表设定& f7 t& d7 I' |) J% Q
高度截获,
2 ]0 L' C0 j4 u) ?式; D3 X3 H! C. i6 h q
高
" O/ d; w8 t5 U( b( L7 g( a高度干预+ B% \% ~ g+ f6 Z# f6 ~
在垂直导航工作过程中,飞行, J$ q5 D, U' b! _
周围环境(地面气层),
; _$ [. m. n: j* V3 c- z物体周围的环境(特别指大气)。/ v" d2 A- l0 s" b
英汉对照民用航空词典B OEING
3 G" r/ \& U* }' U! MTECHNICAL DICTIONARY 9
( Y) G- |% O. K0 k k& I/ F% m/ CAMBIENT PRESSURE, Pressure of air surrounding an
! u( x# e6 s* `* P3 g' c! J6 R, {object, measured in pounds per square inch (psi) .1 g! w `, V* ^ Q! V
MBIENT TEMPERATURE, Temperature of air
% Y0 a% q1 _; E( F* C0 ompere.
' i* c$ a6 u2 n/ eurrent waveform.* g* U- N; a+ \# \
g an
7 y7 M( o3 H: y* g$ u0 Pnalog signal to a digital signal.
* b7 _9 j9 g$ Q- r) e; p. }ore inputs
) d4 I. f! N) Wf binary digital information and one output. The output, C* @/ h9 a! n4 u9 T* H
1 only when all of the inputs are 1. The output is 0
1 y& Z- z- {5 G4 Khen any one or more inputs are 0.
# n' y7 G# X/ g8 k面气压),( f- C4 G" {" f
境温度,
7 e2 p0 l& }/ d, D- E气温度,用摄氏度(°C)或华氏(°F)来
0 G3 [$ k6 d- n) R- t {8 ?。
( Q- X# z$ ~# a电压或电流波形的幅度。! f1 j" s: \' Y% ?4 v
性变化的信号来工作,或产生连续性变化的信号 A' S5 Y1 B+ O/ B2 C3 x4 a
统。
) A) M8 C1 _+ ?将模拟式信号,转换成数值式。
8 W, ]! |# T# ?2 g一种有两个或两个以上的二进位数字信息输人,一个输
) k3 d5 f2 s2 _2 r- Q6 @; U( b的装置或电路。当所有输人为1,输出为1。当任何一个+ V* p6 h' G' `0 U0 r, c
一个以上的输人为0时,输出为0。. W" d. ?8 ~- q/ A
A, ~7 ~" ~+ Y! s- N
surrounding an object, measured in degrees Celsius
9 _! D% X2 [- u& d$ z6 X(°C)or degrees Fahrenheit (°F)." E) W" A; |$ Y$ m4 c {2 b
AMPERE, A unit of electrical current. One volt across
) u- W8 p" y( k' V; oone ohm of resistance causes current flow of one* t% q/ J& _ }0 F, F; L
a
6 g& ~" E. n4 K, M$ Z; x o+ kAMPLITUDE, The size or magnitude of a voltage or
- T, C$ f9 T" [5 \+ ]c7 R9 Z l- S" _& a
ANALOG, Quantities or representations that are
6 T, k4 [1 L" o1 N/ S* Yvariable over a continuous range.
! M& Q) y! \1 L% G0 ^2 j, w; bANALOG-TO-DIGITAL, The process of convertin
& h) [7 n \! s7 F% k( @a
/ V( o6 k: Q6 W# N: f4 K; W) H& XAND GATE, A device or circuit with two or m
! Q7 a0 f- }! Q9 I: K) d5 U* Co
: v9 m9 F% b# Y1 ?4 h `is# M, F7 s5 }2 r9 i
w& F, M v1 C3 V1 ^6 l# n5 m
环境压力(地8 V5 a1 _# v/ @
物体周围的空气压力,用每平方英寸多少磅(psi)来/ x7 y! c6 C F3 T- E8 D
度量。
/ x( y# ~7 x5 Y& L/ Y2 X环& ?& u. [4 o B
物体周围的空" B; y" |7 V3 x. x3 [% N0 O
度量。2 a+ h) ~# h0 F3 S2 T1 l
安培,2 D- _' k6 d* i7 B% H, s4 z
电流的单位。8 Y( Z0 d. g' X G6 t L
1伏电压在1欧姆的电阻上所产生的电流为. N3 T! @' c1 e# _2 t2 G q
1安培
4 P+ [1 A+ c. g9 j- k# `振幅,
' W4 _* l% a: r3 k. K: e# V模拟式,% I; ~: Q1 p$ e, z4 }" U; ^( O
用连续
; ~* B5 K! M- p- F3 r& k系
; i6 W: [! N6 t# v' t& U从模拟式到数字式,: b4 E! ~3 h' s
与门,
) r2 ]+ `$ X% K( a9 t出
8 A% U$ W- g! o6 ]! h0 n2 p" h& @或8 i* X5 A7 u1 E( h
英汉对照民用航空词典B OEING+ M' I5 K2 [# c% K! G3 R6 {
TECHNICAL DICTIONARY 10( y) F$ R1 H4 r" k. _, X
ANEROID, A sealed flexible device containing air at low0 _/ ^% n: c- W6 E( C# K9 u
pressure, which expands or contracts during change of8 \+ W! O" W1 e, ?% a+ |/ R) ~: M- Q
ressure outside the device.
$ Y9 p# V+ C1 o% cically+ r# E% P! E2 [ V
r changing the direction$ c5 z& p, d4 z) y8 Z+ T- x% w
f drive.1 D* }" d. q2 { M
of the wing chord in
* E/ j. P( ]( ?lation to the free stream airflow as it moves forward8 I: Z( v( l5 |( ?3 C
rough the air.6 H- S- B- y \
al axis of the
4 t J: I% L5 b4 \5 O# |: M' ]aircraft.
, C. D* V3 H4 ?胀或收缩。
3 B$ }# C6 `, ]( g; I$ o3 F& a箱。是改变驱动方向的机械装置。
* d( n! O( c+ k# g% ^机翼翼弦在空气中向前运动时与自由气流之间的夹角。0 Z" N* L `9 V# @
。/ U/ W: n" r$ D' V* u* X4 g" X
p
" C# }& k% i& y# M5 pANGLE GEARBOX, A part of an engine, mechan* J# _% s- a% P6 {" r3 d
driven by the compressor, which drives the accessory
: `# s, }1 l) f; Sgearbox. A mechanical device fo
, K, i a& L; U( H( M5 `4 `o6 N: {$ V f7 O- b3 r3 N7 e
ANGLE OF ATTACK, The angle
$ b0 F' i5 n7 A( Qre8 F7 i6 { A5 C# e( v
th
) i1 O1 |3 m9 {# @6 mANGLE OF INCIDENCE, The acute angle which the+ d. l# R" r n1 `- o! [4 n
wing chord makes with the longitudin
/ y7 N n/ x" W膜盒,; ~# l6 ]# v Z9 [; {
内含低压空气的密封弹性装置。当它周围的压力变化' r3 ?; d8 Q) R" q. {: Q4 f
时,会膨0 S& B% W( x, J& _" X9 Y
伞齿轮箱,+ {! T+ C$ L. P# |
发动机的一部分。被压气机以机械方式驱动,然后驱动
, p. G* t% t: x7 D& S附件齿轮
I* }* e% A' y. ^& {迎角,1 I( g9 Y( V* `) Y
安装角,
# V) t# i: Y( q飞机的纵轴与机翼弦线所形成的锐角
' U! E% z$ q4 e8 B英汉对照民用航空词典B OEING9 a% k- c t) S+ N/ G5 G
TECHNICAL DICTIONARY 11
6 W( ?# H2 B. M0 H NANNUNCIATIONS, Audio or visual indications used to9 O9 J3 Y7 E! ]/ \" S
call attention to an event that has taken place.! T) @) i: V/ d, \
ANNUNCIATOR, A visual device consisting of a number
* A, o w9 z0 J0 Z# C% s3 kly.' i4 Q( O, D: U2 W
ANODE, The element toward which the principal stream' V# o- U2 r: ]$ V/ I
of electrons flows.
# X, j' n- @ x1 a2 ]3 F ~ANOMALY, Not normal.; J2 {5 l$ M0 J* z8 M
ANTENNA, A device which, used in conjunction with a
) T. |0 u# N& y! w. ]5 x$ Otransmitter or receiver, is used for radiating or receiving) [- T& w- B2 R
radio waves.
# p# K1 |$ q: F' BNTI-ICING, A method of preventing ice formation on' |9 @% g0 q- J& t
e wing leading edges and engine nacelles.
- u2 u6 [+ U' {2 U* R. q" f7 jNTI-SKID, A system for providing maximum braking
2 \7 o' H3 \+ u4 _/ n H( G' b" rithout skidding for any runway condition. Anti-skid3 ]+ [. f1 ~1 M5 J2 e, l( _
omponents are part of the brake system.
; Z: Y* R' x1 ~3 c: L: F: A9 {& X告,) _* a) V) y) m4 O0 G7 |
当发生事件时,以声音或目视指示形成的提示信号。
. Y' L+ ~6 c" R9 k; s. Z4 T与之有关的电路的现有情况或已存在的# Z- D4 {3 P4 c7 D4 R* H
况
) f7 o, q3 Y- `" ]正极,
! n: V6 i$ d. n0 z; [6 }主电子流向的极位。
8 R/ v: x6 r+ g3 k) l9 a异常,
) W8 C# g4 f% F$ B6 Y- c, l8 C4 r不正常。- g2 @( W5 F0 h% N4 t) B, \
天线,
* U B& G; e; d& Y; p一种与发射机或接收机共同工作来发射或接收无线电+ F" I; J5 Y; P1 X
波的装置。9 r% g# ?7 s# M1 ^7 R7 q
冰,
4 r# O+ G; }! n, {( y3 [7 n: S3 C防滑系统,
3 E- w3 Z* T( a9 I1 [" [* ?! ^一种在任何跑道状况下,都能提供最大的刹车能力而不7 ]4 Q* H! o+ C! E1 r% G( w4 V5 U
使轮胎打滑的系统。防滑部件是刹车系统的一部分。
. g+ w' D4 l! w/ q6 P$ Eof lights. Each light indicates the condition which exists* z; N9 I# \( j8 ^. K
or has existed in an associated circuit and is labeled
9 W/ a1 V9 J4 W5 h6 i, Baccording* v1 W! m! _- C+ H5 ?! u+ L
A
^5 y( F t! l. I- l; }9 rth
/ _5 \/ Y. n3 a |" cA
3 j% G/ O9 B; ?+ x. ]8 d) hw
% J+ Z8 l" u- {0 s8 |0 uc
9 h; y; Q9 j0 v \. [通
( l3 G$ H6 E" ^7 r* H, ?信号牌,
+ R. T. y8 u' m1 g5 h9 ~2 M* _由一系列指示灯组成的目视装置。每个指示灯都有相应
( C- W R1 z2 c+ j5 h的标记,用来显示
3 Q) A! |! z4 }) V( K2 m2 ^- ?/ W情. D* x2 i- @& ?/ D
防) _1 h7 _. D! Z
防止机翼前沿和发动机短舱结冰的一种方法。. f, n u" n% b0 n/ K+ r1 h
英汉对照民用航空词典B OEING/ P1 F( ?2 i! f! n- `/ X
TECHNICAL DICTIONARY 125 j( l! ~/ z; I
APPENDIX, A supplement to the Airplane Flight Manual
- M, D6 e1 b+ E. D7 rtained in the basic manual. A
( ]$ D8 [ b/ q7 `, tollection of supplementary material at the end of a
& p# N: C8 y3 X8 Vook.
' y% H/ ?& O2 @4 R; vof the
( `" z) s B' d) Jrsion link on the landing gear.
2 G! S% R1 _2 H( e8 h" vAPPROACH MODE, An autopilot/flight director mode) v1 }: Q8 ^8 n2 m2 ~# g; ~
which is a combination of localizer for roll control and
/ F# F' N. r5 G0 U" ^& E5 @glide slope for pitch control. This mode is used when full
$ o1 |" n5 O/ \! Finstrument landing system is available.% m6 v2 s5 [. L1 l4 X h9 ?1 H
APU, SEE - AUXILIARY POWER UNIT
( n, ]- c. p& e+ W" CARINC, SEE - AERONAUTICAL RADIO
* Q/ K+ w3 U0 tINCORPORATED4 A, H. z1 T, q8 j& ]- O* ]3 s
ARM, To make ready for operation.
' _0 O0 |+ j* v) g: v附录,- j6 W6 r {) k9 g
飞机飞行手册的附件,包含基本手册中未提到的飞机形
h/ v" i% x1 K {2 K6 x态的其他性能。是附在手册末的补充材料。' Q; C$ G. I: R" Y! t9 C2 t. N
顶销,
. J* T* e1 t( l: O用于连接起落架扭力臂两部份的销子。3 ?4 p' A* ?, |- q/ I/ ]1 s
进近方式,
. n, g+ V+ a) E- O# x4 `/ `9 p# P一种综合了控制横侧的航道信号和控制俯仰下滑信号
: W2 n/ Q' I# Q7 {* h. \' X- J+ r的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系
& S- B( i4 p' @2 r统正常时才使用。! {- p* r0 V$ P6 |
辅助动力装置,
1 c7 I0 W# o6 x- Q" H. h; o8 ~2 s见Auxiliary Power Unit
# l1 o5 m( w4 v. ucontaining additional performance for aircraft
0 x' g0 x; [6 {$ \4 Bconfigurations not con
3 h2 W+ T7 }- D) \3 Gc$ C- C9 r" X6 y3 U' R6 p* t% J2 k S
b
$ K* T8 P) g/ G. c- ?" pAPEX PIN, A pin for joining the two sections
: a; q* c- ]$ S/ [" Wto* R8 G& h8 k9 p7 B+ u; T8 [
., d% K0 K! t# o4 C f
航空无线电公司,6 I7 {% n8 |% G9 l6 Z% N
见Aeronautical Radio Incorporated.
0 P$ E5 W H" {0 W8 L5 w预位,! ]# L' f& m5 o4 F3 f7 u
部件可以开始工作的状态。
/ e' O6 K3 M! P4 ?% M7 q4 l英汉对照民用航空词典B OEING
( {) ?; Y+ I& q( k% v( rTECHNICAL DICTIONARY 131 T8 U. U4 k/ A& s2 ^- @" r) O" p
ARC, The curved track over the ground of an aircraft1 A0 c5 k+ A5 b; R* z4 n: G
flying at a constant distance from a measuring
; C V( m8 x& [7 \equipment (DME).
, |* o7 {: `: N: o( b9 oin the limits of self-contained system
# R" [* D e/ ~; p9 }apability." J4 q# P" `0 T) N
tem for opposing or restricting
4 l1 D1 Q$ r; u- V, povement.
3 O4 u, `3 ]' tSPIRATED TAT PROBE, A sensor that measures total- A& d! H) K: o" a9 M0 u/ E
ir temperature when the airplane is in the air and that
% ~# m g% s; M& @9 c9 k% {) D/ Oeasures outside air temperature when the airplane is9 d& o5 v# L# z* L; n2 ]) o
n the ground. The outside air temperature is measured
" L4 J P/ B/ i' n, N: U3 _SSEMBLY, The fitting together of a complete structure. @# d4 Q' r, x. A+ a
SSUMED TEMPERATURE REDUCED THRUST, The4 r) c% Q) w) v; n7 ?, z5 L0 c/ v
ATC, SEE - AIR TRAFFIC CONTROL* [* [7 p7 S* T D, ~
,
; M7 [9 Z& ]3 F: o, R% I: _3 }系统中所产生的一种用以抗拒
1 X8 D' M$ S* \- L) _" @ ]$ e作或限制动作的力。
( H# [" t; \" p4 s. h( T头,
4 x( b8 N4 I0 Q+ g: z( u用来测量飞机在空中时的总大气温度和在地面时的外
) C9 s' k& t4 i; I/ a6 [温度。地面外界温度的测量是利用引气将外界空气吸入- Y& e6 L' g4 |: y" {/ H
头,以达到测量的目的。% ^1 m' V8 M3 A/ Q' }
配,
2 k9 z* {2 B/ _$ ?8 c8 ]一个完整的结构或组件的过程。
/ B, d( T3 j: K6 ] M z8 q假设温度而得的减推力,
7 k. y2 n1 V8 g2 E9 Z/ y, X推力设定值时,假定一个比实际外界空气温
T! o6 P5 r% v空中交通管制,
8 a8 L, F4 n$ u8 g* Q见Air Traffic Control& E- U+ f9 o: ~- ]0 S* }
AREA NAVIGATION/RNAV, A method of navigation6 [) ]1 ~/ a( r8 ^1 B; h
that permits aircraft operations on any desired course1 t* p" ^( ?5 k+ e+ m
within the coverage of station-referenced navigation
; ~0 w7 G9 t& T) Y8 msignals or with
* I# w' I& @& T" m* r1 @c& r a% {# w# X O
ARTIFICIAL FEEL, A force developed in the flight( n& V! l% ^% B, r* k
control or brake sys
8 m% A$ \& h$ om
* D- f, o" W# J4 ~& cA
' n) J7 T! U* O. @5 ~a7 P/ B# e2 o! L1 L
m% |# a9 B% K6 V: P8 f$ D+ C5 n
o
1 ~7 \: e) ~3 d- e b- Nby using bleed air to draw ambient air through the
+ K; V& I% W V# ]: p' h2 Jsensor when the airplane is not moving.
+ N' p7 W! |; r+ _$ ?1 M0 KA! x' u" s/ Z- k4 y8 F
or unit.
4 R! v. |1 R3 G% V' J( ^1 n7 cA' z5 t5 A* B& N# j# Q f2 U
lower thrust obtained by setting a higher than actual
+ e" O- u( n5 e& HOutside Air Temperature (OAT).
3 I# A7 R" K3 q& y- `弧线, p" ]- B3 k [! X) k/ }+ z
飞机在围绕DME台等距飞行时的弧形航迹。
; p$ i8 R+ E3 q" c" k) {: n# v5 a8 H区域导航,
5 F8 ?- a* d/ z% y容许飞机飞行在有电台参考的导航信号或自备系统能
! s$ \4 t1 L- r: k力极限范围内,飞行任何预定航线的一种导航方法。
! L# t o8 c7 P" N模拟感觉) V1 L4 ^0 m, x
在飞行操纵系统或刹车5 I" l2 k+ s6 F6 V- t5 t5 ^
动9 x7 \: Z8 S% ^4 B B' t
吸气式总温探' i% E! f3 H& E% N7 o7 Z
界; r$ H; \7 j- f, F) c+ A' T
探
: n$ L, |4 ^; |* L' G装4 _/ V7 |$ P$ Y- _
组合成
/ ^5 m0 I# r$ P$ S% x( E由
9 S/ C4 _( E" J2 s- }; @在选择起飞! U% { i: f& e( V6 P
度高的温度而得到的推力。用这种方法可以减少发动机的
' I% j+ K6 G( G# O磨损和维护费用。1 a# s' L4 i$ r9 m
.
# ]4 H% t) ~6 E/ t9 ~8 y英汉对照民用航空词典B OEING) l5 x f& d( @+ v% T5 y
TECHNICAL DICTIONARY 143 }3 ^& [9 T4 x+ L+ G
ATE, SEE - AUTOMATIC TEST EQUIPMENT
G- g% t. X4 j' g8 {- P0 K) A4 wATMOSPHERIC PRESSURE, Pressure of air due to the
$ K- r y, [3 e. T8 v" f1 Tarth's atmosphere, expressed in pounds per square
& Z0 w3 Z: i$ y3 A% G0 C$ pch (psi) or inches of mercury (in Hg) or millibars (mB).4 I. `0 l% a8 n: F
TTITUDE, The relative orientation of the airplane with
0 g" r. @8 f$ t* `/ Gspect to pitch, roll, and yaw.( m3 p! R+ g# J* Y# @% F4 I7 w
UDIO CONTROUSELECTOR PANEL, The panel in' E1 R; @9 Q& \* M a; _
e airplane which controls and selects the routing of
8 K' E$ r% `+ c; n! Sudio.' d6 R, ^3 P w& D" Z: J& g
UTOLAND, Automatic landing using the Digital Flight- e4 ?( U" |, z+ p
ontrol System.
" H/ V% r, q. xn.3 ~* X( o: m5 G0 u* c) `+ k
M, A system5 F' m# S# X7 p5 v, b& @2 R8 b! {
omposed of all necessary subsystems needed to guide2 r4 A6 _) f2 h% Z* W( d
e flight of an airplane.
. m8 J/ g$ p h1 P. {" r9 v/ I5 dEQUIPMENT, System test
& X$ t. \# X( ?, H* e* K+ squipment that operates under computer control.
/ v( w5 x" N# |# c! V V* K/ j' M装置, |
|