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AIR DATA COMPUTER, A computer which produc; l4 N$ ` U. P6 _
data information, such as altitude and airspeed, based
2 B5 n9 H% u+ R: ^: Y. don pressure and temperature measurements.; _4 \! R7 ^8 R' Y5 \ t, \' @& h3 n: m
es air
7 d: C( J% _6 w7 T+ _IR TRAFFIC CONTROL, A system comprised of
6 \! z; [7 T( L- f3 T) |round and airborne components used to identify, track6 g1 ~" A4 v, e- I; l0 b5 @
OUND SENSOR, An electrical device operated" `8 A& ~& S" S
y the landing gear, which transmits on ground/in air
) [& [/ q6 S* G3 q5 E9 l" d# yformation for system operation in flight or on the; `7 Q! V' r( _ y& X% D
round.
8 p7 h- K3 ^+ s* x* FIRBORNE VIBRATION MONITOR, The AVM takes. |5 s& T; p& |7 Z# N2 U8 a3 q9 N
e signal from the engine mounted accelerometer and1 T7 f; h' R( d4 A
alculates the vibration on that engine.
- Y$ r: I2 s+ j& u0 z0 ?3 a `/ Lcorridor equipped with radio navigation, n5 E- b9 `; P8 @+ b
aids.
$ y1 e$ N! R' m0 C- a/ @$ ?0 ZAIRCRAFT (or ARINC) COMMUNICATIONS
9 c4 u0 {+ }/ u6 }- S. C5 f! LADDRESSING AND REPORTING SYSTEM, An; B# u/ K4 G! l- {* M6 W
addressable digital data link system which permits the
+ Y5 f& s) i/ y& h, Cexchange of data and messages between an aircraft0 _* {+ m- |! K* V% N) L, [
and a ground-based operations center over a radio
: c- n' i/ @8 G( o' ?network.
) U0 q6 B% K- f3 x1 t. BAIRCRAFT CONDITION MONITORING SYSTEM, A$ @1 z! \: c ~- G ~! P& ]3 |4 x5 h
system of sensors and recorders to monitor various
: y5 y* m5 w6 t7 K' J5 x: Wairplane systems' performance and status.2 w7 G$ A. q- p6 o5 D* _
机,
. k5 X% C5 ]2 @; s( b' I中交通管制,0 I+ Q: ^# R0 l4 p# e$ a- w
一个由地面设备和机载设备组成的系统。用来对飞机进' A# M8 e. C% J" H9 ]
地传感器,; _. S! s6 v, d" U$ F4 s
一个由起落架操作的电气装置。用于给空中或地面的飞3 K7 V9 ]- a' k7 p: a
系统运作传输地面/空中信息。(有些系统只能在地面3 n$ }1 }9 Z6 ^
用)
5 x' {9 u0 X( K4 n( \载振动监测器(AVM),- j2 u$ H9 Q3 s
AVM从装在发动机上的加速器取得信号后计算出该发" E7 \8 Z- [8 y9 i4 D
机上的振动。' I$ d- A6 `) l7 o
式建立的控制区域,内有无线电导航设备。. G/ ~1 g# B) x
飞机通讯寻址和报告系统,+ W" b7 n; N, f7 x8 w
有种可寻址的数据通讯系统。利用该系统可使飞机与地
7 q* G5 Z- K# z3 p4 y2 ?面操作中心通过无线电网络进行数据和信息的交换。
& @* B9 l) d- u; A飞机状态监控系统,
- k( u% T4 f5 I+ H: Y2 O: b! ~& s, X一个利用传感器和记录仪对各种飞机系统的性能以及( l+ [9 \: {/ u& r7 o
状态进行监控的系统。) e" m7 j) D3 o) L& _
A
2 U% s4 y& [. L, E. g3 rg/ D) M2 ] I2 s9 E( w @; ^
and locate aircraft.
3 b% u, D0 q; z' r6 ~AIR/GR+ l$ c _5 e7 q/ k1 v. k2 r4 Y
b
% m$ K1 }" `; S- T3 A; i- @. o" lin
3 R& q; s' W9 ^8 Y$ Tg' p& q# X! f; W& W* ]
A+ k( m8 S3 k1 r; {% V
th
+ O T' P! f" h8 {/ H/ Wc
$ n8 ?0 V! V8 c' v; _, iAIR WAY, A control area or portion thereof established
1 @! Y- y. E+ _( ? Lin the form of a
( M9 M" R1 ^" [6 j d大气数据计算
$ j U$ D. A& \% l) U. S' M+ D根据量取压力和温度而产生大气数据资料(高度、空速
) W7 ~$ q6 v/ n/ K X等)的计算机。; _8 x' e) Z" e d2 T2 }2 E
空& v+ j: a! {, z, H" c" _3 E
行识别,跟踪和定位。! `- \0 j% [. z6 f( u, H) N
空
6 J# m4 Y7 J0 | ^1 \7 l机) r( }/ ^/ M. H7 Z$ g; a% r% P. a. i
使' P2 f4 I9 ~0 `/ u4 |/ I( c+ E3 w
机' N4 e2 z/ O/ t; u7 ~5 j z; e# x
动- k* w& b# E# _2 M
航线," ^# N$ ]4 d0 @' w% ` v7 ~8 Y9 A
以走廊形& O& b" B! }3 c1 X1 e" T9 x( Y* |
英汉对照民用航空词典B OEING8 m @' {# _4 ?0 ^" h
TECHNICAL DICTIONARY 6
! Z, z" j O1 A5 W+ U6 |* RAIRFOIL, A surface designed to obtain a useful reaction,& i a% ?" z. o) z
such as lift, from the air through which it moves. Wings,$ x7 f6 c. a) G# k/ B1 {/ w; w0 `
stabilizers and control surfaces are airfoils.
+ h' i; c8 v, GAIRSPEED (IDS, TDS), The speed of the airplane4 E- Z5 c. D8 L3 d8 s. E3 k5 L
rough the air.
- ]1 }3 S R. K2 c( ]: s3 sD INDEX, An adjustable pointer on the
+ R: t2 X' T* pirspeed indicator.
: T6 @0 v2 L- A: v6 z% M) W9 band legal ability
- @0 \" V, h. l: h8 _fly.9 M& T9 E% ?' }- d6 S4 y2 R/ ~
m, for example, the procedure for finding the
' ]) o7 T( ^6 k$ }1 n9 s4 Uquare root of a number.# e: {3 h+ D" T0 r% s+ ~
y. U. d+ j6 g0 k# v+ a
re, wind,
' p/ f- x. R: d' O% E% v0 {+ Y, qand aircraft flap setting.
( P& L+ M( M& x8 ^& R, V是翼面。8 l4 t+ l% V, y6 _% D- ]
速,( x) }: l, x7 T2 t* m% i
飞机在空气中运动的速度。
8 @- ~, N" D1 H; S,! |8 F/ w5 o3 F9 k% l2 r
在空速表上可以调整的指针。3 C$ o. l# A, t$ L, N7 J, L' {6 X
机械飞行能力、和合法性的飞机状态。9 n$ \. H% ~7 b+ n/ J3 }
一步一步的解题方法。例如,计算一个数的平方根的步
& l4 N" ]8 u; e; Z。) ^7 C* |# T6 C
能
; D4 J" L) q. A( v: ~资料的法定文件。
0 L( A; D8 i+ K( K$ x翼位置成函数关系。
+ e1 h/ V5 `) {3 s, ith
5 v, E- U' w! `( t( i5 t4 j: i7 yAIRSPEE1 d7 b9 I+ u4 j2 K4 L+ g4 ~
a
8 [/ P! ^7 q; }; }AIRWORTHINESS, The condition of the aircraft with) p& E) J: _4 X- ] w1 c; o" g
respect to its aerodynamic, mechanical,
( [+ `7 n) Z7 F, j, q& X4 Oto! Y$ |( c @- o+ D6 s
ALGORITHM, A step-by-step procedure for solving a6 K) @. R- I+ S9 |$ s3 [
proble
6 T3 u) J# q8 M$ s Ws7 A m, V$ L# U# t
AIRPLANE FLIGHT MANUAL (AFM), The legal
{0 c/ @6 g1 y8 s5 Y/ @document containing performance and operating limits, j" R/ a( y. ]. U. K9 z' }7 k
operating procedures, and takeoff and landing7 {" R! g( ~+ k; M/ B- E
performance.
9 ~. w- f" b# P3 b4 f* s: \! Y( iAIRPORT ANALYSIS, A comprehensive set of takeoff
. l, ]1 @9 f2 G5 D" c; k/ x% tweight limitations for a given airport runway, generall: m, V! D3 F: k8 U
presented as a function of airport temperatu
; v2 h- A/ b+ n% L翼面,2 W$ C: o' q# B
用以从气流中获得反作用力(如升力)的表面。机翼,7 c. N% v0 F) C' g1 ~5 f/ ^% S7 v
安定面和操纵面都# y% Z" d, ~3 {7 f# z. \
空
: j/ {6 Y( Y3 t$ l u空速指标( b2 W" N1 ?' P
适航性,4 j w( p v0 w, I
有关气动能力、
' j$ [/ H& z: ?+ D( Z2 u* b0 L演算法,* u ?$ e1 h* ]7 n; T1 d1 @; }- a
骤# x1 K4 I8 ~3 q A8 U
飞机飞行手册(AFM),9 i b: H3 u9 s( L
包合性能极限,操作极限,操作程序,起飞和着陆性8 c% ?0 g7 ^! ^
等 U% o7 q% ]' G7 K7 _
机场分析,
1 L& I( B! s' G ]( h一套针对给定的机场跑道的详细重量限制资料。通常与
6 [/ v1 O9 h' J7 y) S机场温度、风、和飞机襟- K- G# O' g% A# ]5 U7 R
英汉对照民用航空词典B OEING8 E" T2 x# _) z, q; \
TECHNICAL DICTIONARY 7$ L& H) h2 Y. a
AIRSPEED BUGS, Adjustable pointers on the airspeed' @4 h: v5 N0 V
indicator.
0 ~% ~+ U3 l+ Y, @ALLOY, A mixture of a basic metal and small amounts# I) \/ ?7 p3 T* N1 t5 l N
f other metals to change the properties of the basic
0 y; q6 R% @ g2 l- }etal.. D' Q) r9 P" S* [# t4 }: |
Minimum airplane speed.6 }: Z: H/ B) j6 c% W
e of. r n3 G: Z2 Y8 B+ a
itting airplane angle relative to
' ?# X; W, E; w7 Yirstream for the stall warning system.
. o' l% y) J& b! b3 _another.
, [ N5 l7 U4 K4 U; mLTERNATE , An additional airport selected during3 |8 L& z9 t; u; p+ {
,$ E" {1 m. ~' }$ Z a5 Q
合金,
4 P& p' ^2 [; X' A, R在金属中加人少量其他金属,而改变其性质的一种金属
+ }( a* Z. a- e1 B; |9 O |合物。
) ^: ^# k& i* d4 X$ [飞机的最小速度。
) H: G8 u3 N" p4 v速警告系统传输飞机对; T. X, A& C9 c' g; o/ O# f, C
流的相对角度。% b& r- M; w8 t+ o1 J
由一个状况改换到另一个。7 z$ y' m0 C# H# m& j: a0 p
降场,3 M* M5 [- G/ \0 f' q) v
划时,除了目标机场之外,所选的另一个机: ?- d2 p0 g5 P w/ W
o; ^) J" t, {+ ]
m
( Z$ Q2 i7 L, M6 L( G' XALPHA SPEED,: h1 B% M; L3 ~4 h
ALPHA VANE, A small moveable airfoil on the sid
% J- m/ i/ S4 z6 S# I" N6 nthe fuselage transm2 T) g4 T* c& W
a
' N/ j; Q+ H4 o+ U7 Q5 Y6 A9 U3 |ALTERNATE, To change from one condition to" ^2 p+ u1 o0 ]) E* m0 V! f: d$ s
A
- `% w: @# s3 {flight planning, usually near the destination airport, to be
: r- i8 P6 M5 P" b* ?! |1 sused when it is desirable to divert from the original, f* Q4 h; \* l$ e3 j6 X
destination airport.
* k: j1 l1 S' `, E2 ^/ K空速游标
7 M0 U8 @, l7 a* Y空速表上的可调指标。
, |% j p, ^* t% d混
1 l% k; O, f' a; p( A E迎角速度,
6 C! @& E8 q. U/ R2 W迎角叶片,
! P" L6 A/ }5 L- O+ h* s: c位于机身侧的可动小翼面。为失+ |+ B# e9 p; H1 s4 O0 @. k1 Z
气4 q0 h3 k8 v5 ^8 ~- c! M5 r8 p
交替,
+ r$ V8 j# k- B* j# P备: B. K n( d0 i$ W% G: j
制订飞行计' g9 m' b6 O: A6 t
场。通常在目标机场附近,以备不去目标机场时,改降之6 D$ X k" j. X2 y" K" l! q) Q
用。
9 n* n% ]+ x/ e( i5 h0 ~英汉对照民用航空词典B OEING
5 R9 p! A/ u1 ^& \ F4 [6 ATECHNICAL DICTIONARY 8( X/ g3 J& _0 K" ^
ALTERNATE AERODROME, An aerodrome to which9 I! A V, S! ~. j' B- {5 j1 Z
an aircraft may proceed when it becomes either2 e2 c' d: H3 q2 X$ U6 T2 F3 s u
possible or inadvisable to proceed to or land at the
' s# j* t7 w+ J. merodrome of intended landing.
# G8 J! i2 B/ x; yTER SETTING, The adjustment of the altimeter
- ?7 A. p/ }1 f) i% g3 s' t& ^account for local variations in atmospheric pressure.
: y8 _& [; D5 ]4 \5 k JLTITUDE ACQUIRE, A digital flight control system
- v6 r5 p( J2 x" o7 Pode to transition from climb (or descend) to level flight.
# p# V- b* E; n; fLTITUDE ALERT, A flight deck alert occuring when the0 `0 z) o, n; C: r% y8 f: B4 z
irplane approaches or departs a selected altitude.$ G) u) g$ @4 ^% {1 A8 E
LTITUDE CAPABILITY, The maximum altitude at! h" C8 U6 s: x- x
hich the airplane can be flown at for a given thrust,
2 k# Z# |7 @7 D3 Cpeed and atmosphere condition.
, P) u5 r( Q4 I$ T. }4 PLTITUDE HOLD (ALT HOLD), A mode of the autopilot" G1 }+ J' X( i; y( e
r flight director to maintain a selected altitude.' S! E1 l) Z4 P3 L* l6 \4 D9 D
irplane's altitude during VNAV operation.
; h1 C4 k7 S0 q: z4 G机场着陆时,可作着陆使用的7 b: G) V$ R/ B4 L. G
场。
- j9 i$ D8 R9 _, s& k,
+ { m+ o: F3 f2 r根据当地大气压力变化而对高度表所做的调整。
8 [9 i1 c( B. l" U9 C0 b一种数字式飞行操纵系统,从爬升(或下降)改平的模0 [# n. s% {! _. W8 \& h
。
5 F2 P5 G y9 `, q度警告,
% n3 K! w: n4 y4 B9 ]当飞机接近或偏离选定高度时,所出现的驾驶舱警告。. D% m% H7 o" @3 o! Y' Q+ W
高度能力,. z2 ~& h$ a; `: U. x9 ?' c
在给定的推力,速度和大气状况下,飞机能飞达的最大) a% V" r/ ^; I' K ]7 K
高度。
/ C; e: N# g8 }5 t! g高度保持(ALT HOLD),
4 o0 q9 E. o" ^自动驾驶仪或飞行指引仪保持在选定高度的一种方式。1 E0 t* ]' [: C0 a( U v
,
* ^0 a) `, M; d/ {1 {! t员对飞行高度的控制。# D! M+ A$ F- c4 G) U
im
) q/ @! o; N; ~5 m% ka% S) g* O- w% |. o+ e) v! [
ALTIME
. r3 g6 S: V S2 }9 Z& f4 n+ x; l vto
- m, f# C- B/ p5 U$ c: M( tA. O9 u" y) Q4 c) A7 y* L
m0 O! q$ R" O! @9 U# e) s# p5 [
A5 G, }, X" ?5 i( E
a* R5 X+ _+ P( K. R
A4 ?- s# _( }/ t: D
w
5 V5 Q$ F5 V- N* w& Ks" m* _ Z3 r" D! A. r
A1 a+ b" s3 j2 Z+ W9 W; i& M
o- Y0 S+ T( _" r( o
ALTITUDE INTERVENTION, Pilot control of the6 |3 d/ x9 f l& P# l
a
) Y- E4 M& l/ qAMBIENT, The surrounding atmosphere.
2 Q7 C. B) e/ ]$ x* \1 Z0 x备用机场,
) g- k( o2 `) S8 M, @& l4 c当不可能或不适宜在预选
0 o( G( D4 A' _4 y Q机 b9 J+ k G2 N0 N% |" @7 S' d
高度表设定
2 Y3 O( ` s6 u" M6 P' q. q+ x/ ?6 Q高度截获,
7 w8 F- f, F! ]- g+ J3 `/ t式
& Q+ `! g& n7 c( N* v% C2 c7 h6 e5 A高
7 q% z! Z; m3 L5 q& P, I高度干预+ e7 \/ U3 r5 }3 ]
在垂直导航工作过程中,飞行
& D7 |" G5 `( q7 A8 X* q' i3 V周围环境(地面气层),4 C3 k. j8 w3 h7 @5 a0 |$ Z
物体周围的环境(特别指大气)。
4 N4 i$ \* l" Z; H) n英汉对照民用航空词典B OEING
5 r# p% b; G/ v! o$ q, dTECHNICAL DICTIONARY 9
% |: j, ]+ t8 [% ~AMBIENT PRESSURE, Pressure of air surrounding an
" N% k4 z9 \" r" n) G( x. M" R, Qobject, measured in pounds per square inch (psi) .
7 w* h$ D. b+ m7 {* CMBIENT TEMPERATURE, Temperature of air8 Y3 A3 @ x2 P
mpere.
1 l1 h) I* s( v# _! Kurrent waveform.. ~- p% f u4 k
g an" Y) t0 ?& j( G) p" |3 \8 E
nalog signal to a digital signal.
, e- f, b o2 v, s: V" \ore inputs
6 s1 O( l) G4 `" uf binary digital information and one output. The output
2 a1 q2 e# m: Q) O% b1 only when all of the inputs are 1. The output is 0
% C5 {) d9 a+ V' F; g1 Nhen any one or more inputs are 0.
1 d$ E+ f# A: v+ ?4 e/ Z# q面气压),
3 z) ^# B* b& r" C( L* E; d- G境温度,
! p* F2 Z. F' ^! M, ?8 n1 c气温度,用摄氏度(°C)或华氏(°F)来
3 r- v! O7 [) M4 F {& F( j。
$ v3 {+ P1 _2 F2 }7 x( R电压或电流波形的幅度。5 F$ Y! j) t. J: Q% Z3 ]
性变化的信号来工作,或产生连续性变化的信号
" [7 l. r* ?; ~& w3 N0 v; f统。9 t# r. ~. ^3 R9 i& ?( }9 F
将模拟式信号,转换成数值式。6 c+ {4 T- R8 y0 \0 w8 w
一种有两个或两个以上的二进位数字信息输人,一个输% I/ R, r) z$ x% s. G
的装置或电路。当所有输人为1,输出为1。当任何一个* m) z8 }+ F( h3 v8 l/ f
一个以上的输人为0时,输出为0。7 \6 `9 C* i1 i: y, c/ I
A3 T d; |7 g6 k- F
surrounding an object, measured in degrees Celsius
2 o8 B, W4 f+ x+ S" C; V(°C)or degrees Fahrenheit (°F).
6 m+ } \) J E; t& ?6 PAMPERE, A unit of electrical current. One volt across* r! e1 t" S; o7 J6 w
one ohm of resistance causes current flow of one
9 E' r- s; Y# I/ v% U5 {" ma
8 ^( P6 F1 i. i9 s" Q6 D8 `AMPLITUDE, The size or magnitude of a voltage or- D6 D' Y t5 S4 @0 _7 D M
c, Y# v$ x, s% H# W: B# C
ANALOG, Quantities or representations that are
- J. J$ O H6 `% t/ Kvariable over a continuous range.
# p! |% \; Q% t7 YANALOG-TO-DIGITAL, The process of convertin
" k/ t2 Q$ L" R! e/ `a* n, |7 [ ]1 A0 M2 O
AND GATE, A device or circuit with two or m/ g# R+ z+ y( x: S: n' i7 {; W
o
( \. d) [: Y, l: ? K! cis
' |6 `8 `4 a }w
1 B0 o& l* q7 \! g- `2 l1 i环境压力(地
5 F3 F# L4 U* G( z物体周围的空气压力,用每平方英寸多少磅(psi)来) d2 X" y- k/ o7 V5 i
度量。
2 g U% E# @8 b+ l+ V环
& E) Q4 x# A9 `; V# a4 [" @8 n* }物体周围的空: x- H( C l2 L n) h" x
度量。& W1 } ^) H! X7 V o
安培,
, S. s7 v1 x, \9 C( d' V) }' |电流的单位。% k: r3 l/ X& p5 ?* M. ^- [6 [
1伏电压在1欧姆的电阻上所产生的电流为' v7 j2 U8 O- Q# K1 [. f$ _
1安培
. O! w; d' K) A- e+ F% @9 W振幅,% i, a( G4 z* B" F, h. Y& n
模拟式," t3 F" _6 M/ h V
用连续
$ n( K9 w' I/ W; ?" h系
* r2 k" E8 M+ i+ g8 s* H& S从模拟式到数字式,
( K& I8 [# A. p% [与门,: @+ p, `6 J+ P6 q! P8 U
出
3 D# f& d' l, |) O( i0 l或0 ]1 T* {/ S1 ~* C& j) s' B# c0 h
英汉对照民用航空词典B OEING) N* p6 b9 X8 o5 {. q1 q
TECHNICAL DICTIONARY 10% R" M# [! {' Q9 G$ E
ANEROID, A sealed flexible device containing air at low) L" ?+ ~7 n2 R; |" u( T. i* A: V$ p
pressure, which expands or contracts during change of
/ N+ q3 z& ^- d% cressure outside the device.
- d( u3 J- V, v7 V9 a' aically
r" U! u4 d' s m7 W- _7 N1 Ur changing the direction! X B, Q1 R1 {9 J W9 c
f drive.: F. h- S: g4 d5 p5 i7 r
of the wing chord in( f# X7 D! k* a
lation to the free stream airflow as it moves forward
& [% s0 f- R+ S9 d3 q6 ?rough the air.3 }, D6 U! M; H i3 {! U
al axis of the
5 N& k0 F5 V1 Z6 o4 @aircraft.5 @$ X! q5 Q* x
胀或收缩。4 m$ D. ^; n [! W: e9 M5 l
箱。是改变驱动方向的机械装置。7 C4 g; d: O, F& ^
机翼翼弦在空气中向前运动时与自由气流之间的夹角。
" G9 K' X: x6 s# g。$ f7 ?4 S+ @ x3 A# }, T8 d
p
5 t6 p5 q" h' p) {' G$ ~ANGLE GEARBOX, A part of an engine, mechan; y4 f8 |7 V) v, V9 r
driven by the compressor, which drives the accessory5 X" B% f) F" e' i' [+ S% j# m
gearbox. A mechanical device fo
$ I4 w8 y8 _0 d4 F' K8 qo" f% W( m) k3 \0 X/ h
ANGLE OF ATTACK, The angle5 d6 P% e1 L0 E0 r( k
re
+ g4 z- W( n3 l e+ _( Fth
/ I6 w3 w- d4 LANGLE OF INCIDENCE, The acute angle which the m" N% _9 _, }5 T% `
wing chord makes with the longitudin7 R n: G3 k" N- T7 d' L7 R- }
膜盒,4 c b$ W! Q0 u- w+ X; R" S
内含低压空气的密封弹性装置。当它周围的压力变化! |& n. A- T) ?' F' ^# U
时,会膨9 v6 D/ _ @5 a, T
伞齿轮箱,/ W! o; C- d Y* [
发动机的一部分。被压气机以机械方式驱动,然后驱动
) n' p X( m5 o( e4 h2 i附件齿轮5 L4 i+ G( I1 k% K
迎角,
; p. u2 k5 E) `( @) k安装角,
$ K" y9 \( j$ T0 _4 u飞机的纵轴与机翼弦线所形成的锐角
; O, p9 A$ e3 `0 M英汉对照民用航空词典B OEING/ t0 k4 C) w+ a# r2 M' Y$ B) J
TECHNICAL DICTIONARY 11: E2 D# C( `3 P. v% f- J$ Y3 J% `
ANNUNCIATIONS, Audio or visual indications used to2 y2 {$ c3 P- |. s
call attention to an event that has taken place.
2 q: t) y; Q1 u0 oANNUNCIATOR, A visual device consisting of a number$ M( M1 Z: E l9 A3 f
ly.
) ^/ ^! t# d- [ Y. j6 y7 U3 ZANODE, The element toward which the principal stream
- ]/ x) ]6 ^9 I$ F+ W5 Kof electrons flows.
, d' r9 i. l5 u; D% mANOMALY, Not normal.
8 t; s0 L9 ?9 YANTENNA, A device which, used in conjunction with a
: U9 t- z: |; Z, c4 ], c- Stransmitter or receiver, is used for radiating or receiving$ O' k: Z0 a' U: W* T( O! h* D
radio waves.
( b; Q0 N. A9 @; i, ]NTI-ICING, A method of preventing ice formation on( f* m$ B1 E# p$ L4 g& R" y
e wing leading edges and engine nacelles.
, y0 \4 C5 U5 L# E3 ~9 l/ r7 ONTI-SKID, A system for providing maximum braking9 h: R+ f" [( o5 N) n
ithout skidding for any runway condition. Anti-skid
; k: ~ z) a+ z/ y' ?omponents are part of the brake system.) j: K8 t1 C$ x4 J- d
告,/ J8 e6 E# i* [
当发生事件时,以声音或目视指示形成的提示信号。% d6 [- K0 |& H) C4 M! c2 F
与之有关的电路的现有情况或已存在的3 t) M7 I/ i4 f. Q, [, c) n7 `
况9 c8 C5 A$ m6 N9 C, h
正极,
% r6 J: F# z* E主电子流向的极位。
6 P+ ^2 P0 t0 y1 A" {8 q异常,; Y2 o8 @* E7 h ^. g( e
不正常。1 b& u5 Y9 c8 g+ M4 x; w9 A4 M
天线,
% t3 v! K: F1 _一种与发射机或接收机共同工作来发射或接收无线电+ T& v9 Y% X. I6 f, i
波的装置。- @4 Y5 m' a/ c, e) B0 w% ^8 O
冰,3 `9 B! ?' e b; |' c a5 k3 y
防滑系统,* Q/ f& ^) D0 {9 j+ k8 j
一种在任何跑道状况下,都能提供最大的刹车能力而不9 K, d) f0 N2 y5 x9 I4 {
使轮胎打滑的系统。防滑部件是刹车系统的一部分。 N# b* T$ o6 e% g" W$ O h; ^. p- H8 G
of lights. Each light indicates the condition which exists4 W" _' T2 G. v o; a
or has existed in an associated circuit and is labeled3 ~9 p4 b; h% c6 h; Z$ `
according
% ~5 W, U0 u) HA1 b% X: z$ o" Z, B* i
th
_/ P, L9 @# K2 [$ C% b! q# jA0 y& z1 B0 w: }! J* Q1 m
w
% j, W1 }( `% g8 y) }: j# Ic/ n" W2 k1 P2 L) _" `. o' o
通
- w" \5 Y% l+ E2 w; C \' y' j3 t C( D; D信号牌,6 N; r1 v" v/ p" v ^, z, m
由一系列指示灯组成的目视装置。每个指示灯都有相应
! {# D3 v2 l! |( X% z& w' H! j的标记,用来显示7 Q3 S: H4 X: G6 A0 U& H
情
6 G6 s4 a! C' w防* v# ^- y: s" J2 c6 i" w
防止机翼前沿和发动机短舱结冰的一种方法。
4 ~ g3 O7 w$ b+ T: s- `英汉对照民用航空词典B OEING- [/ i- _( R0 o2 [% h3 d" I
TECHNICAL DICTIONARY 12( u H/ Z" S3 r) F1 I: p3 f
APPENDIX, A supplement to the Airplane Flight Manual
4 z7 Y, g2 @1 @- v' `tained in the basic manual. A
5 B8 X% o I/ |4 mollection of supplementary material at the end of a5 F0 f4 _, v5 Y2 C: a
ook.0 c2 v, j! U: z; o- C/ v D
of the
" b# a; w" c4 y8 E4 B5 ~0 T9 ]* t' Qrsion link on the landing gear.. D0 L( c( v I2 W! g
APPROACH MODE, An autopilot/flight director mode& j: V& u, I# Q. {, z3 q
which is a combination of localizer for roll control and
! g+ n% N& w/ N8 @( [glide slope for pitch control. This mode is used when full( g5 T9 g. @8 U+ u+ ?
instrument landing system is available., f, @ O$ ~0 l2 D% f8 L5 R
APU, SEE - AUXILIARY POWER UNIT/ ]% b' j8 t, V% ]- h W2 l/ D6 N
ARINC, SEE - AERONAUTICAL RADIO
/ @+ x3 i9 Y x1 P f$ g, F; m. NINCORPORATED
% f* Q* p: V# O1 V% \ARM, To make ready for operation.4 n% p8 c+ R' i# e
附录,# {. }+ b9 e- T8 H! W( V s/ i
飞机飞行手册的附件,包含基本手册中未提到的飞机形
* n& z, n* n+ A8 n4 P/ e态的其他性能。是附在手册末的补充材料。
/ h- B6 W$ W& c$ |2 X/ T; D7 P顶销,! M. @- m7 U2 k3 M2 D k
用于连接起落架扭力臂两部份的销子。& J! K. A/ H* u8 h
进近方式,
- o" h' {2 |2 X/ n G' e; V, K一种综合了控制横侧的航道信号和控制俯仰下滑信号
6 u/ L! |" ]! n' k! F8 J6 x6 z9 p的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系
; n- n3 L$ d: j6 t; m统正常时才使用。
' F4 G& P" G7 V4 L- }- k, L辅助动力装置,8 n5 N5 u& k. j% G* [8 I8 I! e- m \
见Auxiliary Power Unit
9 a2 S- b/ b; c( h" ~9 k: d5 Rcontaining additional performance for aircraft4 X3 B" j: K7 t3 x" C2 v
configurations not con
4 G J1 q7 Y& B& j4 U+ Ec9 [1 G3 {4 q& ~% O5 I2 e" z8 D
b& Q! I" M7 Q% g9 J3 _8 s/ f
APEX PIN, A pin for joining the two sections9 E& \8 V" A2 _) f3 ?1 B
to, B# {5 b$ Y2 W, a. S# [7 L+ O+ O
.7 u; ~- n3 Q9 F4 n" _
航空无线电公司,
9 A4 z1 r) S6 n. ]; s见Aeronautical Radio Incorporated.7 R5 _' _9 E/ ^
预位,
1 B n; @( I8 m1 |' I3 W部件可以开始工作的状态。
' `+ F, x# o, R4 T. i英汉对照民用航空词典B OEING
: g3 Q( y; j; S, {3 d( ^* uTECHNICAL DICTIONARY 13
! U2 k; _) }* \, Y. ?4 o; qARC, The curved track over the ground of an aircraft
5 o. w6 c& Y8 Q/ o: H- b wflying at a constant distance from a measuring- D* m; W& a4 U+ e
equipment (DME).
' m; H8 w: `" Cin the limits of self-contained system0 g0 @# [$ X7 V$ P3 s+ r+ W4 J2 f
apability.% _: o5 f7 [- t1 G0 v
tem for opposing or restricting
. o3 i0 L! q6 ^ovement.
9 [0 D% g/ ^, T! A& ~SPIRATED TAT PROBE, A sensor that measures total0 w: S6 x+ U2 p, i! J
ir temperature when the airplane is in the air and that' Z8 U; a# ?. c. q8 E( c. h* F
easures outside air temperature when the airplane is
! D; W' b# G9 g8 J. f$ |9 c4 ^* Yn the ground. The outside air temperature is measured
( d# n6 |1 u( v4 {0 ^SSEMBLY, The fitting together of a complete structure+ k! y' f/ L& C8 ?. H, C
SSUMED TEMPERATURE REDUCED THRUST, The
5 l/ n; W. c' |: J1 `8 }+ u3 v& iATC, SEE - AIR TRAFFIC CONTROL
/ g$ C+ A; E! p% Z4 ^,
4 f: D* `1 F- j! a0 |* @2 P系统中所产生的一种用以抗拒
& g9 R& r; x6 q3 H作或限制动作的力。
$ g7 }' R b8 i) G" {0 q6 E头,9 D X# u$ s0 y
用来测量飞机在空中时的总大气温度和在地面时的外! L5 \3 G9 Z$ ~- Y) A# `! x. S& y1 |
温度。地面外界温度的测量是利用引气将外界空气吸入8 W" `: R6 Z5 n* M
头,以达到测量的目的。8 \" a Q8 z$ j1 I+ D7 m8 @
配,% [4 o0 b0 V4 Y/ k$ m6 {, \
一个完整的结构或组件的过程。
! B V0 m; T. Y( j6 h j2 k假设温度而得的减推力,: U" u" j3 l6 `, w' u9 A b
推力设定值时,假定一个比实际外界空气温
+ X! J1 @; |0 r9 B5 o9 v# Q空中交通管制,. b5 u2 C2 L- }+ {6 y
见Air Traffic Control8 q* z! U8 h# k# _. ?! S; v
AREA NAVIGATION/RNAV, A method of navigation
9 g7 o' [/ Z4 }2 cthat permits aircraft operations on any desired course
! L/ h& W3 p. W4 _0 C+ kwithin the coverage of station-referenced navigation: U3 `7 S* ]( I, r/ k/ ~# `& \/ s
signals or with
2 @7 e9 j* Z1 N A5 e5 ~* M' [( cc
3 f, m' U! s; W& a/ r/ zARTIFICIAL FEEL, A force developed in the flight
/ R8 j, }8 S/ v& o8 u* qcontrol or brake sys9 X: o4 [ B' j& u- I
m) r# ]* L4 ?# d: M) K- w
A; q8 l6 X5 c6 K0 N
a
9 ^3 _0 e1 Y8 i% Bm. P5 F% U) @) t3 E6 m5 [. m
o: N; R, h" B$ C/ O# V
by using bleed air to draw ambient air through the
1 U2 s# x1 }" J7 K# U$ e8 Y# Qsensor when the airplane is not moving.* L) B w" M/ E* G, v+ J
A1 D. {; }" s% R
or unit.
! P8 g: I& g j% ^A
! K3 I. {/ q Z# Q. k" M# E# Klower thrust obtained by setting a higher than actual
4 G. c% P( Q6 k& y# @Outside Air Temperature (OAT).+ ]& i: [6 ]8 G5 c& t% n9 G+ e1 T
弧线,
" h) o" V/ b( t+ k飞机在围绕DME台等距飞行时的弧形航迹。: I' v ^ \2 `% b1 f
区域导航,4 S1 y3 n1 T2 @" m9 k7 p) C" ?) N
容许飞机飞行在有电台参考的导航信号或自备系统能
5 y/ d6 U( c) x( f- o/ e力极限范围内,飞行任何预定航线的一种导航方法。8 l3 a- ^5 i0 _, d; c
模拟感觉8 t/ m# T3 v/ ]0 ^; ]- h1 I
在飞行操纵系统或刹车 g) L: \2 @; l( `7 p# x
动
2 g! q0 j0 k" u& U5 J吸气式总温探
4 k* p4 F4 _7 Q6 T4 Z1 J" Z% K界 @* A& V6 T" j& S3 }* A U
探
; @# K) [' ` ]. H H装
4 l: d' i2 ~; K- _, O: K* X组合成; |4 r; x4 i6 K7 w; h( L7 F- B3 A
由
* f$ e( A- x# y0 y& r, y' l) R9 ?# O, ~在选择起飞; L0 U6 Z( w7 X; C. E: {
度高的温度而得到的推力。用这种方法可以减少发动机的
6 g' Y5 t$ v+ b' o5 _磨损和维护费用。
+ L( x' y- I1 N; r& U, r, W4 k' q.
) `) D7 j) g# V: W英汉对照民用航空词典B OEING
) ?# J3 L8 [: g9 j3 ^TECHNICAL DICTIONARY 140 {: G+ i9 ^% t5 C
ATE, SEE - AUTOMATIC TEST EQUIPMENT# `, }! x% A) w0 m+ N2 }1 B
ATMOSPHERIC PRESSURE, Pressure of air due to the
9 O q$ w( t' O5 g1 ]* L4 D7 @. |arth's atmosphere, expressed in pounds per square
& R- q" E: e9 }+ p; gch (psi) or inches of mercury (in Hg) or millibars (mB).
6 l/ {) _. O2 h, n' YTTITUDE, The relative orientation of the airplane with( u! a4 Y3 S+ a- I
spect to pitch, roll, and yaw.( s/ a: _; J5 h& B- F/ o2 N( i
UDIO CONTROUSELECTOR PANEL, The panel in
6 H" u) b5 q: M9 }, ?4 N* Xe airplane which controls and selects the routing of
" ~6 `' `) H! M+ T- E' audio.
8 Y3 D' f6 K& B `UTOLAND, Automatic landing using the Digital Flight6 z3 n+ ?) }% S' B. s$ o- D, a
ontrol System.
2 g( d6 V9 G f/ o" K' Gn.
8 S+ \! K; q2 e0 x: v( DM, A system
6 F# `/ |0 u9 `( {. z5 `9 l. Yomposed of all necessary subsystems needed to guide* G7 s' {; {% d5 e8 H8 i
e flight of an airplane., p& Z. q9 f; X# }
EQUIPMENT, System test
3 |- v* ?4 c( ~# vquipment that operates under computer control.
0 i) T5 s3 L. o+ _装置, |
|