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AIR DATA COMPUTER, A computer which produc
' S {% W O! c) O$ z2 d, `; Z: }, _data information, such as altitude and airspeed, based9 {7 S4 J% U! ] S$ R
on pressure and temperature measurements.
0 k- I$ \3 u+ O* o5 bes air
* h3 b& A7 m3 D9 j- ^3 b3 Z' V wIR TRAFFIC CONTROL, A system comprised of# l9 c. B) ]5 ?
round and airborne components used to identify, track
+ S/ X; _. }" F8 n5 @ sOUND SENSOR, An electrical device operated% s7 e' K! V9 @# g% W
y the landing gear, which transmits on ground/in air
5 e3 X" z2 J4 a. G. E9 ?8 Q: Bformation for system operation in flight or on the
) b# V" P! e. n- f8 A6 p6 o$ _round., P: p5 c% f. b
IRBORNE VIBRATION MONITOR, The AVM takes* K7 k) W+ Y& [) E
e signal from the engine mounted accelerometer and
3 o" T: s2 ?) r3 palculates the vibration on that engine.
9 s2 ~# m. i1 i' U4 _7 i& D |corridor equipped with radio navigation" G4 q7 d. G/ W0 m- v0 ^# [
aids.3 o! u$ W! N2 P, a7 @
AIRCRAFT (or ARINC) COMMUNICATIONS1 E- G: t+ {+ J4 q; o- ]
ADDRESSING AND REPORTING SYSTEM, An9 u: N* Q7 p1 d- i' `! F
addressable digital data link system which permits the7 V2 z3 @) h. J
exchange of data and messages between an aircraft1 Y* ^$ l! Q# [: J& C
and a ground-based operations center over a radio/ i# Q+ m# i0 W, y8 E' X
network.& {5 L5 d" D- c4 g$ G6 T/ M
AIRCRAFT CONDITION MONITORING SYSTEM, A
: d5 N2 E7 h0 ?system of sensors and recorders to monitor various8 |% \; U) c2 a7 j+ v y
airplane systems' performance and status.( `% }1 O& I! W" { q# e8 m
机,7 d9 n+ h. z+ R1 b8 C* m3 S
中交通管制,
* t0 e9 d5 D6 M- p$ X8 b* o一个由地面设备和机载设备组成的系统。用来对飞机进
% l3 G- g7 R, ^4 _地传感器,
1 Z. c, H: p9 D一个由起落架操作的电气装置。用于给空中或地面的飞
$ Q4 S3 T4 q, @' ]1 {- ^) O- T系统运作传输地面/空中信息。(有些系统只能在地面
# @7 ]- K% c. J9 }/ t用)
3 z* w- }5 p6 o. K8 j: |) E载振动监测器(AVM),
9 \6 L' g! G. u: L1 Y1 ?0 h5 PAVM从装在发动机上的加速器取得信号后计算出该发
% R. M- S" N* ~0 V7 q, }4 T机上的振动。
5 @. d2 c3 C' [, ?0 K式建立的控制区域,内有无线电导航设备。4 X( p+ `; r6 r9 P' i
飞机通讯寻址和报告系统,% F7 e+ K5 r9 @5 S l8 Z4 z
有种可寻址的数据通讯系统。利用该系统可使飞机与地
' p- ~8 s: b8 K- D" Y面操作中心通过无线电网络进行数据和信息的交换。
$ ?. f* s9 Z1 ?4 T% Y' x0 V) ~8 @飞机状态监控系统,
- K3 i) [# F9 f2 o: e& X一个利用传感器和记录仪对各种飞机系统的性能以及+ R: R& ]8 B, l& Z) w) Y
状态进行监控的系统。8 y: i6 w! y9 M' G8 p' P6 x$ a
A
0 {: E6 v2 m1 P1 O" w" Eg
: Y% Y; d) r; v! Qand locate aircraft.
X. \0 R& J+ N$ AAIR/GR+ h% \) m2 I8 k8 V* G0 a. N
b
# R/ d5 ], I5 Qin1 G& ^; X1 z2 ` s
g' a. C3 q4 \% u- {
A$ y0 p- M2 b; h
th
6 c4 q9 t5 u; t; W+ Nc
7 [3 f& P. J3 \7 \6 BAIR WAY, A control area or portion thereof established7 {) g+ J+ d9 @4 l
in the form of a8 f; X: E/ C% m* |
大气数据计算
+ w F3 C$ o; n5 r1 {1 d, s4 C根据量取压力和温度而产生大气数据资料(高度、空速
, X7 l' M8 Y: }6 s y! O% x( v- j等)的计算机。" s$ v x2 s. i. q+ U
空
, v7 d: ]4 {' b' ^8 U* ]3 E- P行识别,跟踪和定位。
' i5 [% \* ~( r: K空
7 T7 H* v! X) h! l! e& G {机
n6 o9 h: E I2 ?* X. `7 V使
2 x" H" Z) }& k4 j' b机
4 P& K8 n9 P2 A8 i. O动, w3 C% M" T, S3 {. G
航线,
5 `2 B) U! l* v; D4 X+ a I以走廊形
( V# ? ?' R+ J+ V% @4 o英汉对照民用航空词典B OEING: B. p$ D" _1 Y9 E* J! N7 U
TECHNICAL DICTIONARY 6! r" c$ Q6 L2 e; D* A
AIRFOIL, A surface designed to obtain a useful reaction,
- o6 L( b# a# @8 y1 [. {" ]such as lift, from the air through which it moves. Wings,, H" u0 B' N9 m! P
stabilizers and control surfaces are airfoils.: n; [" n5 n2 B, m# E3 H/ ?* n- g
AIRSPEED (IDS, TDS), The speed of the airplane: ~% j: E, V5 W% U7 }( R
rough the air.: T! L+ @0 }& U5 _
D INDEX, An adjustable pointer on the
: @' G8 ?! R4 T" X7 xirspeed indicator.: A- H7 t( f, K/ U. }9 X6 ]
and legal ability, |; l0 X$ p7 E2 F6 t7 b
fly.$ s/ N# M2 S6 g2 r4 y s, T9 j
m, for example, the procedure for finding the9 G+ x2 B, A0 X& D. H
quare root of a number.
8 N2 z* d2 {2 H" k0 Zy* a/ C/ J% o. W# s7 a) y0 C. y# w& o. f
re, wind,
0 \* C$ n2 b- w7 t. sand aircraft flap setting. `3 {) c# j7 W0 R$ G2 m. L( _( A
是翼面。% `' h$ g" O6 F* }! ^$ @& T
速,
; S& p" v6 w0 h飞机在空气中运动的速度。
* q5 Y4 y0 q, B3 H. f,
) h0 }0 F( x6 [7 K/ L2 Z. x在空速表上可以调整的指针。& `4 ]: v$ E/ r' u! @
机械飞行能力、和合法性的飞机状态。
9 p( q) ?, Z- ]2 B; a一步一步的解题方法。例如,计算一个数的平方根的步
3 e9 b! H; J% Q- v! R, C。
* r+ G0 h' l! ~$ ~& T, c能, u' O0 B9 U" P5 W% Z& s7 R, m
资料的法定文件。1 D2 ^ d, q u
翼位置成函数关系。
( E2 z N- a) X5 S; q: kth
$ v% x0 B0 z* hAIRSPEE
& J# e5 ^0 }; O- S6 ra4 z* F6 u2 o- x+ Z6 m
AIRWORTHINESS, The condition of the aircraft with
; {$ @# R5 o- X, Trespect to its aerodynamic, mechanical,
2 S% Z% m/ y' C" O$ h) q4 |- _to
2 J: Q8 ]; @* M8 oALGORITHM, A step-by-step procedure for solving a
3 l' M3 l8 k% o5 ]. s. W1 @2 E5 @proble4 s; t9 x: h+ v8 f. N; v
s6 E% Z, f1 ]( S) e! j
AIRPLANE FLIGHT MANUAL (AFM), The legal
. ?2 ~" v: I- T8 odocument containing performance and operating limits,
1 e' H; \7 b$ s2 G3 q" Z) ]operating procedures, and takeoff and landing
) D1 L$ E" b/ W' a! c7 Uperformance.9 C3 H" U6 _* G4 ^1 k& Q
AIRPORT ANALYSIS, A comprehensive set of takeoff
0 N0 k& n, k; p3 m( x+ G2 n& Uweight limitations for a given airport runway, generall
) }4 t1 ~# B) q/ Gpresented as a function of airport temperatu. Q& _: y I, K
翼面,
" ~: W g" d4 p$ R用以从气流中获得反作用力(如升力)的表面。机翼,- `* ?. c7 d9 b- ]- r
安定面和操纵面都1 ~; @9 z" V, Q$ R
空$ S4 e; v5 l" I
空速指标* b: n0 x( [4 f5 x" k6 Q
适航性,
( \% h$ i+ ?) e) l% T有关气动能力、/ m3 U% A0 b6 D: s0 g
演算法," u* k* D/ W$ f8 K5 x
骤+ d- w. a- [) r; P; f
飞机飞行手册(AFM),( ?0 I j; i7 Z; l7 L6 j
包合性能极限,操作极限,操作程序,起飞和着陆性
& I6 h# A$ V \) d! z等
+ a" N% i6 t# c+ u机场分析,
4 E* f- l2 J y. X; M/ P h一套针对给定的机场跑道的详细重量限制资料。通常与
2 k4 x! E; S8 \' C机场温度、风、和飞机襟8 J ^" |6 j$ T0 g# M% }, ]
英汉对照民用航空词典B OEING
2 F/ ^" w4 ^4 [$ K! Z0 mTECHNICAL DICTIONARY 7
! T; b8 A1 z1 T. ~$ o1 F8 JAIRSPEED BUGS, Adjustable pointers on the airspeed9 d+ u; K7 n; A- B
indicator.0 J$ N' t! M" i, O8 H( z, t
ALLOY, A mixture of a basic metal and small amounts6 u5 \8 M% A. v4 y; x
f other metals to change the properties of the basic
" T$ `+ H) c5 |" ~% a* S8 yetal.
3 W# t( S/ o+ WMinimum airplane speed.
2 s0 S0 b# ^! w+ Y9 \e of
& s) F5 @1 R+ h0 \" I( R5 H1 xitting airplane angle relative to
& {! c) M8 q3 h: s: u: M# j0 Virstream for the stall warning system.% Y) q* D- S* }. S3 Q* G" t7 S
another.
' y9 f' @$ u: vLTERNATE , An additional airport selected during1 y9 u. ^) a" x6 c0 |
,
$ S& s! a1 [5 e/ W合金,
5 k! Y: k/ B% p* M* g) d: a/ b5 x/ a在金属中加人少量其他金属,而改变其性质的一种金属* J# S5 U9 n' k5 V4 K
合物。
+ I8 d9 W( B6 Y, y6 Y7 Z2 c4 b+ A飞机的最小速度。
0 V; C( u; E h/ c速警告系统传输飞机对5 J% k: a r4 i0 `
流的相对角度。
4 ?9 ^& m# x3 z由一个状况改换到另一个。! v9 B4 S5 A: {7 g) C3 t
降场,8 Y3 |/ V& N( |/ h. A- g! t
划时,除了目标机场之外,所选的另一个机
( w# J; k* }4 j& So
% ^9 S/ X' F. L# N7 Km
I+ T$ T5 m& t0 s% S: }' o" _. wALPHA SPEED,* M7 A2 b0 P1 A% z6 T: M7 w2 p0 s
ALPHA VANE, A small moveable airfoil on the sid; k' B ]% E& R, L
the fuselage transm
$ Q+ |+ f; c# }0 J6 M/ L. ha
0 [# k: k/ D/ KALTERNATE, To change from one condition to) }* P5 t5 @: G
A( n" v- T1 m) ?
flight planning, usually near the destination airport, to be
' o+ t |6 p+ I9 M- Y( Pused when it is desirable to divert from the original1 e6 Z* l/ L. ]- b$ F
destination airport.
S1 a, |+ x0 L1 W0 f+ ?空速游标* ^6 j4 }" Y C9 e5 F5 \1 R/ ?
空速表上的可调指标。
: H- H+ P9 c; t: o, W: K. @6 b混
3 `. r$ l7 ?6 K6 K& V7 t4 n: v迎角速度,2 L: R" p" |7 E. Z& g
迎角叶片,
- s* Q! I' P) W. W4 r9 D位于机身侧的可动小翼面。为失
- A) z1 i8 B1 i2 L0 x& ?) ]气+ o' `- F6 M" O1 |9 F% K& s. g5 J
交替,. N' @1 e6 d, _4 L
备
; [* q8 C7 J, t3 |$ X- }: u制订飞行计7 v9 q- A2 Z* g- h( ~# J7 W
场。通常在目标机场附近,以备不去目标机场时,改降之
8 d- {* M% d+ D! N用。
% b! _4 Q, C+ O' ^英汉对照民用航空词典B OEING
# h( i' r# N7 B2 [TECHNICAL DICTIONARY 8
( ^( M2 ]3 J* ` WALTERNATE AERODROME, An aerodrome to which
. ^/ `3 _4 S4 c( N" \an aircraft may proceed when it becomes either0 q+ ]7 N1 X% K% _- q" G
possible or inadvisable to proceed to or land at the
' e7 T! |4 N7 V1 V1 ?8 l- _erodrome of intended landing.
+ e3 Q" `/ a0 d4 u6 Z( ?+ ETER SETTING, The adjustment of the altimeter* @- P8 Y0 ]- F9 H5 b1 R1 i- I
account for local variations in atmospheric pressure.
9 Q3 |( I( K! U( m& P% G3 TLTITUDE ACQUIRE, A digital flight control system
0 u! E) n% _& `0 B. vode to transition from climb (or descend) to level flight.. s& I( s8 i0 i: O
LTITUDE ALERT, A flight deck alert occuring when the2 Q9 f) q3 O! g% R( ^
irplane approaches or departs a selected altitude. h' S) ~( R! R2 J1 o
LTITUDE CAPABILITY, The maximum altitude at! p' f+ W0 y% r& W: E+ Y" y
hich the airplane can be flown at for a given thrust,
+ @' q# f G- e) M6 d$ D% ?. Z" \$ bpeed and atmosphere condition.+ @1 A: l! Y D
LTITUDE HOLD (ALT HOLD), A mode of the autopilot
8 D7 k$ s( P3 g1 c. H3 s5 ?) Pr flight director to maintain a selected altitude.9 X H* X. N4 `& D, \% m4 J
irplane's altitude during VNAV operation.
# {) P7 R. `% B6 O A机场着陆时,可作着陆使用的
" W' d% m! e0 f$ G7 k场。
4 G1 ^' E$ \# U/ c$ l, g,# R, u2 R; E/ u/ o; {7 p j; Z# E
根据当地大气压力变化而对高度表所做的调整。1 \# U$ S+ K; l( X m
一种数字式飞行操纵系统,从爬升(或下降)改平的模
# k7 s4 R. v/ e/ U1 y% a。5 {/ v/ y; ?" v
度警告,' w/ s/ o9 ~; s; k
当飞机接近或偏离选定高度时,所出现的驾驶舱警告。3 P2 E$ k3 w& b- l
高度能力,
8 z7 X7 J( H0 b: w4 D1 V$ L A1 F在给定的推力,速度和大气状况下,飞机能飞达的最大
2 ?) N6 V; U/ Q0 u! {2 V/ }高度。6 N, k* y8 ~; p, `- C1 I3 f
高度保持(ALT HOLD),
3 H3 F! ~1 N: C% Q自动驾驶仪或飞行指引仪保持在选定高度的一种方式。" Z' P, O& S4 w, z: w
,
9 l7 r) w$ X4 ^3 @& w" L7 Q员对飞行高度的控制。
$ Z8 @ g; B4 ?0 E% Zim0 p% G E3 [8 N/ r9 c! h5 s
a
8 D- ^" r& w+ C4 W& n- uALTIME
* s* N; ?1 }" B( b$ o; [3 s5 jto
( b; Z+ B5 g ]- ]4 tA0 _( b9 K3 _- W. d* x
m. u5 m" f# _8 ?8 b4 o5 G
A
1 |2 V3 F$ R: o9 E( aa. Z) c# Z8 e4 _# E1 I0 I
A9 O \2 ?6 ?# D4 l q# F; G
w
$ }7 Q5 _) i+ M! D* S* ~s6 b$ q4 {3 r0 m4 H* g8 \
A
: X0 @9 N% b% zo
0 C$ F( K# _* A& r XALTITUDE INTERVENTION, Pilot control of the
2 y3 ?* n/ |# q- s; _* N4 Za" _" Q3 o% r8 d7 Y o, a1 x
AMBIENT, The surrounding atmosphere.
1 A+ w5 z0 Y. O' V% C: ^: v备用机场,* Y/ i' j/ |8 [$ T. [! q
当不可能或不适宜在预选5 U; u! V- \/ ^* [- Z D0 s
机2 o2 \" a& g2 s0 l; ?; v/ `
高度表设定% E. X: @" A( N5 a5 v4 m9 a
高度截获,1 p$ c9 r H$ l. D
式6 d7 i3 d* c( Z- c0 s# x* @9 ^3 S
高
1 T( o0 {( A! C0 |+ p高度干预
, B! A6 U% r. Z3 R. i- C0 H' o$ C, z在垂直导航工作过程中,飞行
# Y8 r# M! E" r3 |9 s) H周围环境(地面气层),
4 l* ^" m; A1 J, e/ Z物体周围的环境(特别指大气)。- s7 c/ Q! R3 Z% V7 [5 \
英汉对照民用航空词典B OEING2 T0 f- N; h; X+ L1 b
TECHNICAL DICTIONARY 90 |2 N- O4 `9 C5 r f- w& M" i
AMBIENT PRESSURE, Pressure of air surrounding an
( f/ q: G3 S d# Qobject, measured in pounds per square inch (psi) .
7 ?1 ]. u, T0 D# q$ B0 I! nMBIENT TEMPERATURE, Temperature of air
# D/ J" B1 a; v5 q( Rmpere.) l) ]) _ N3 X1 B- O# X8 k" X
urrent waveform.- w+ N) v, S8 z( N2 J2 U
g an: ^+ K8 U9 b' \# t. ]5 k2 ]! M
nalog signal to a digital signal.8 k. m R# o( O+ C5 Z! Z
ore inputs
, J3 i3 A* M% P( J, H; wf binary digital information and one output. The output
) |! p, N) N6 v8 O" z5 X/ `' j1 only when all of the inputs are 1. The output is 0
1 j8 M3 {3 ]# A {6 d) s8 Lhen any one or more inputs are 0.
( C" b4 b$ i) H* \' V面气压),% B9 V% ~6 M _3 _* ]! v* y
境温度,% I8 l# T4 f3 x% Q5 f+ p5 j
气温度,用摄氏度(°C)或华氏(°F)来 ^" }: D, {; D, q
。
2 Y7 C8 L6 j* C( @' D$ s" S Y电压或电流波形的幅度。
# _2 |+ {) n: _1 k性变化的信号来工作,或产生连续性变化的信号- I, n }; T7 d! Q
统。! g; Y2 Q* W# y6 u" H, I
将模拟式信号,转换成数值式。 y2 c" b* s, ^9 Y, k7 C
一种有两个或两个以上的二进位数字信息输人,一个输
) G' I! `. i4 i7 B; `& D# V的装置或电路。当所有输人为1,输出为1。当任何一个9 L, {0 f4 k, U5 w% R
一个以上的输人为0时,输出为0。
( V. o5 ?0 o0 L& VA
/ M" E; E1 I" M! V9 X u* csurrounding an object, measured in degrees Celsius
+ @# a: `8 W/ g+ U(°C)or degrees Fahrenheit (°F).
2 w* A" R6 F- ~6 IAMPERE, A unit of electrical current. One volt across. L2 H! t9 x5 b$ z+ |
one ohm of resistance causes current flow of one5 @) K0 U$ a3 p7 F( E6 D6 K% D
a' z+ V, B* `- n2 R, ]
AMPLITUDE, The size or magnitude of a voltage or: O5 _ a6 G n
c" L: }, i" M E" a6 m9 [- x
ANALOG, Quantities or representations that are6 D3 j# S8 \; J& D2 `
variable over a continuous range.
# y$ d( t% `3 d8 U% GANALOG-TO-DIGITAL, The process of convertin
6 Z2 F9 ^0 Y3 ?6 M' Na* V2 r2 K$ i6 s7 P; e% N
AND GATE, A device or circuit with two or m( G! h/ Y% L) \5 |. ]
o. A0 l y2 c9 n
is
( T+ x. D# o6 e! t5 c2 `# o3 lw
3 L. Z" j3 C1 z' D环境压力(地* s! x9 \9 H' N/ I# ?$ Z' T
物体周围的空气压力,用每平方英寸多少磅(psi)来) C; A) M5 J! M$ j. L3 q! M
度量。
6 o' c; y- m- c8 b) W, [环/ r; o# n1 b- |
物体周围的空
9 n e1 l9 W _! |5 W0 `( k7 q度量。/ o @ [# C) {. N* K n7 ?8 |
安培,
T+ s$ y: V# D! C. J' f. f电流的单位。- }2 ~4 w5 _( H* P @
1伏电压在1欧姆的电阻上所产生的电流为3 {% A/ ~2 {2 ?) J
1安培, z5 `" `6 m4 t' w0 a# q+ n" u
振幅,, s8 X& j' q6 }/ o& u
模拟式,& x& I a S2 @$ S7 k
用连续
- L4 Z W5 M+ i系, k/ X+ x1 B& S$ r
从模拟式到数字式,# Z* B1 r& G5 v) g$ s
与门,3 n1 T& |* z( L
出
: K; r' l4 L, J. E或
& e; t- p, a6 P# v. t6 e9 C+ f英汉对照民用航空词典B OEING
+ m6 `4 V! C9 j. _: Z5 @6 uTECHNICAL DICTIONARY 107 m$ C" C9 E; o
ANEROID, A sealed flexible device containing air at low# b. J; t4 P1 |
pressure, which expands or contracts during change of
* _# J. C0 q. Y b5 Nressure outside the device.
- ?$ E% b* h9 B& y Dically
5 ?4 |% w' G7 w0 O8 {r changing the direction1 |) \+ I' H3 o: O9 p
f drive.& Y3 ]0 J$ N; Z+ c4 j
of the wing chord in
3 ]( m( Z y8 G" v ]( ilation to the free stream airflow as it moves forward4 I6 V5 m! l0 N
rough the air.& Y* g" D: [. g" T( q. R
al axis of the
6 r: z+ P z8 Uaircraft.! R ^( N0 p% [# z
胀或收缩。
* ?1 B9 u s. K7 ~, [箱。是改变驱动方向的机械装置。& d! p4 ^2 J" C5 @
机翼翼弦在空气中向前运动时与自由气流之间的夹角。" J9 S4 Q$ o1 ~4 G
。. E' ^( g* {/ P$ D# a6 C; v
p! X4 Q. a2 O" N! K* F2 Q4 ?$ j* K0 {8 Y
ANGLE GEARBOX, A part of an engine, mechan
* Q! m, T, r6 Y2 j: sdriven by the compressor, which drives the accessory
! s! u l. p# C1 agearbox. A mechanical device fo
( j1 M+ J* B So3 Z3 q0 q: u3 A+ a3 r) {
ANGLE OF ATTACK, The angle
; ^- f' |+ j6 v8 _% C2 l$ Rre/ i) g, U* j8 u$ q
th+ T0 I- v4 ^( b1 W- o, j
ANGLE OF INCIDENCE, The acute angle which the
# Y, T: S' e" s) _9 ywing chord makes with the longitudin
; H! u, ?( G+ r膜盒,$ ^- @1 B' T2 e
内含低压空气的密封弹性装置。当它周围的压力变化
( f! U' |+ \( {/ Y' @时,会膨
5 E: a+ u x/ A, E- P6 o9 V P7 e+ |伞齿轮箱,
& } K8 Y: I8 w" q w发动机的一部分。被压气机以机械方式驱动,然后驱动. t6 i) I/ B$ j! m. n- `
附件齿轮
$ |( y H1 O, R' D0 v迎角,! {6 s0 b9 A* z6 \1 S
安装角,& Y+ R5 B; l/ v2 X0 R2 Z) I. }
飞机的纵轴与机翼弦线所形成的锐角
- d- d6 K- _7 B( O$ m# p$ W英汉对照民用航空词典B OEING) K6 N4 s1 N0 l6 }2 l+ X
TECHNICAL DICTIONARY 11
1 O% |/ X8 _: Z [/ H8 sANNUNCIATIONS, Audio or visual indications used to+ l1 A! M+ d4 c! U, Z! H: A' |' {/ a
call attention to an event that has taken place.
8 Z9 m6 ^) O, e; E5 N( F- yANNUNCIATOR, A visual device consisting of a number: d. P# C. i% j$ O6 S l( W: C- A
ly.
l1 F) S5 |1 q q; l) W% cANODE, The element toward which the principal stream% U: s( d' R; @
of electrons flows.) G) F: Y+ c6 }* \* I' d: ^
ANOMALY, Not normal.( [# z+ c; g! F! N
ANTENNA, A device which, used in conjunction with a1 d4 }" Q" b6 K8 y$ S
transmitter or receiver, is used for radiating or receiving
/ U* [, n/ g# Qradio waves.. A B, X' H" x t" B2 a
NTI-ICING, A method of preventing ice formation on5 G( A; [2 ~( J" x( ^( u
e wing leading edges and engine nacelles.. {( D4 _# D2 A, G* u6 _" `
NTI-SKID, A system for providing maximum braking6 ~3 K: l. Z# N( {# @
ithout skidding for any runway condition. Anti-skid: o; A* w+ `! X1 b- L2 }
omponents are part of the brake system.7 s% G0 `8 N7 q; R4 M
告,
: c! E# }$ I7 r2 G& U- W当发生事件时,以声音或目视指示形成的提示信号。3 Q8 q* Y- r, f* U3 r
与之有关的电路的现有情况或已存在的
! C [. W$ p2 j& F+ D- m% S况
& j8 c1 z9 L6 {$ a+ U正极,5 o; j, E3 S# @/ l( B
主电子流向的极位。9 @' ]7 {* u2 Z# D
异常,! M0 V E. V9 }# e' V# ~
不正常。
! Y/ X ~- l( t天线,
) J; a% P6 y0 c$ M6 g: p一种与发射机或接收机共同工作来发射或接收无线电
' U3 n& V# @/ l2 B! T6 L4 P- ~波的装置。
! t" D2 i5 ]9 o' f+ d# G6 M; F- E冰,2 O$ k$ b! O9 P% b
防滑系统,: u) X7 V$ Z; r3 p7 F4 F- T4 B
一种在任何跑道状况下,都能提供最大的刹车能力而不1 T2 u" ~1 \$ @* Q7 z
使轮胎打滑的系统。防滑部件是刹车系统的一部分。& u0 J/ t; u1 m3 T" L7 m2 J3 `
of lights. Each light indicates the condition which exists
" I0 F3 F7 E" O2 F& V- P$ gor has existed in an associated circuit and is labeled
9 V& ~5 n6 B% A9 L4 @# q6 q- u" Vaccording
$ G/ ]! g( `; W$ M E6 vA
( W. B; A, \; F: N# [0 O" @& G1 Sth
0 n2 M6 m" Y! `5 D; dA5 ?: i9 V. W$ J3 [
w v/ ~0 g% | X
c" q n) v1 u6 P) t M6 |: M" J q
通
, C5 O$ L5 t4 g+ W5 `" U& `信号牌,
/ i! \; p8 c. {1 x由一系列指示灯组成的目视装置。每个指示灯都有相应. C4 P/ V. Z% z9 u5 c4 ^
的标记,用来显示( A: A! `* m& r' x3 P/ U1 T
情
$ y: p8 c; z# W* |4 b8 ?防
* N* B+ r- B0 t! j防止机翼前沿和发动机短舱结冰的一种方法。" F* Q; X {1 V' n- E; h
英汉对照民用航空词典B OEING; O/ @ E6 x1 d5 j' B( V0 \
TECHNICAL DICTIONARY 12
9 Q) {) M2 k1 A4 b) c. CAPPENDIX, A supplement to the Airplane Flight Manual% I) |- J2 _( {: w
tained in the basic manual. A9 G# G0 z/ d, \) c6 g+ d
ollection of supplementary material at the end of a
- e. y( }$ ]; L6 Iook.# [4 |8 H b R9 ~- h1 _9 B
of the r: r+ {: p0 \, i, }
rsion link on the landing gear.
0 }; {( _) g: HAPPROACH MODE, An autopilot/flight director mode
2 j( f4 d" k; v* zwhich is a combination of localizer for roll control and) _+ ^2 U0 V. c- B
glide slope for pitch control. This mode is used when full, V8 u1 l6 G" S
instrument landing system is available.
1 O& H- h$ g9 ^2 a5 m+ K! `1 I2 t, YAPU, SEE - AUXILIARY POWER UNIT
4 w5 h2 g& |' E3 i! K6 @ARINC, SEE - AERONAUTICAL RADIO" C, S$ |6 p$ k% P$ ]
INCORPORATED
! k( m% g/ Z+ }& t3 f; v# ZARM, To make ready for operation.$ j8 j6 A6 m% u, @7 M# L" K
附录,
" i2 O- }$ n i% T飞机飞行手册的附件,包含基本手册中未提到的飞机形/ D- U7 w- D9 w* t* |
态的其他性能。是附在手册末的补充材料。" o* |% X( b3 w, w: K$ ? ?7 S
顶销,
% Y1 l7 D" l d6 `/ W8 ^7 V! I9 m用于连接起落架扭力臂两部份的销子。- y W h! G. C. b
进近方式,2 E( d8 |, s2 Q( O5 {& e7 H
一种综合了控制横侧的航道信号和控制俯仰下滑信号
* y" S7 Q* W! K的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系' X2 c }% `) Q& T
统正常时才使用。1 \$ C8 k. f# X
辅助动力装置,4 E6 v# K( u4 U o5 l0 s" l# p
见Auxiliary Power Unit0 q# A$ m2 k5 }0 h
containing additional performance for aircraft
" x7 t/ Q# Y0 Q: Sconfigurations not con7 d5 g- f* `5 P. p& M9 g
c/ J3 C; s2 K( X. v. _
b0 u0 F- _' h0 [: x1 Z0 }
APEX PIN, A pin for joining the two sections
: q6 `3 r% y5 Ito4 N1 z! ?: Z$ k. \: ^
.9 U; a1 O M5 U! I5 | X7 _
航空无线电公司,' _& c& m; L0 W
见Aeronautical Radio Incorporated.: d# S3 [$ S! O% ?
预位,
7 y: f4 ^- a5 e0 O* V& K& _$ Y) H部件可以开始工作的状态。
1 |( X& }. u7 q- O英汉对照民用航空词典B OEING
% F0 K: _. y# `TECHNICAL DICTIONARY 13
" Q) F) Z, v7 [ARC, The curved track over the ground of an aircraft
) G7 c5 _% w0 q# \7 Iflying at a constant distance from a measuring V5 v, x4 [0 C) Z6 n
equipment (DME).
6 g7 S( \8 ?; }' T* P, ^2 l6 b6 rin the limits of self-contained system
8 U/ j# t. ?2 r% z7 T+ g) o, ?: Wapability.
; O9 L1 d" s2 y5 @/ T2 t8 Ctem for opposing or restricting! X( s, P" J( ]! H4 u
ovement.0 c9 ~9 p A/ E. P" ]' a5 _6 i
SPIRATED TAT PROBE, A sensor that measures total
& V6 O( E! p5 X! B$ a# Mir temperature when the airplane is in the air and that
, L# b0 V; @2 A! v: p9 Teasures outside air temperature when the airplane is* I( g7 g5 U5 o& u: G4 i% S
n the ground. The outside air temperature is measured
; c0 @7 R, S6 Y" m2 x3 @SSEMBLY, The fitting together of a complete structure
2 _& \3 X+ B: F3 l' h& H, iSSUMED TEMPERATURE REDUCED THRUST, The
0 q; i% ^' x( f- [8 Q8 UATC, SEE - AIR TRAFFIC CONTROL+ n# y. \- Q) T; J+ s
,
0 d7 V P. r4 D* p系统中所产生的一种用以抗拒
2 a' q/ r6 u& ?4 p; \. f \0 Q作或限制动作的力。
8 _9 ?" N3 x% `0 O# z5 o头,/ m! S: ?) a/ X+ @- p! ~$ o
用来测量飞机在空中时的总大气温度和在地面时的外 J, T* b# B3 Q5 N1 ?2 c6 h
温度。地面外界温度的测量是利用引气将外界空气吸入: x5 k4 d3 t4 Z/ V5 N m
头,以达到测量的目的。
$ ~1 b. U( y! R+ V+ [: q& Y! \! \配,$ i! k* K2 R% V U8 k
一个完整的结构或组件的过程。* |1 y# q) [% y$ }
假设温度而得的减推力,
3 V! I" b, c2 ^0 @推力设定值时,假定一个比实际外界空气温
, |4 ^+ v4 i% X* m f. C* F空中交通管制,
7 g* r9 {- P, [8 D% Z4 Q' w$ {见Air Traffic Control, O" o7 P0 V; }! e1 ^+ d2 X7 W
AREA NAVIGATION/RNAV, A method of navigation: ? E' _ [8 @1 D- g( x5 w
that permits aircraft operations on any desired course8 I( j" v# [& W+ r4 M, y# W2 J2 @2 E
within the coverage of station-referenced navigation
9 c3 Z! H$ h$ ?signals or with
+ X5 X+ Z, I! B- k9 P0 q" C4 y# B0 @c+ \3 \+ ?7 C* A# C2 F4 d7 L# h
ARTIFICIAL FEEL, A force developed in the flight
; C9 K! X/ c* z2 tcontrol or brake sys8 m& @7 g7 b* E" F8 N; C) ~
m
. Q* v+ |1 W; B6 _- X* xA
% m1 g3 U* a0 X7 ya/ P3 l. a. ?* J, v: B6 z
m+ V: u! U5 X1 @8 V4 {. i
o9 U! k- [: _, u! G+ \1 _/ }( B
by using bleed air to draw ambient air through the" J, L8 z5 v& g4 A( U8 x& R- x
sensor when the airplane is not moving.
$ X! \3 _ A# K: W8 ]: uA
7 u' `- b; {, O& e4 C& B" C& Q* Bor unit.1 M0 y+ |6 s- J c
A
1 }5 J! j) c9 N0 [5 alower thrust obtained by setting a higher than actual: @! x6 |1 f- F9 b0 b9 ?" r
Outside Air Temperature (OAT).: G- R, y& O8 ]1 Q. _. G
弧线,4 Z) G" r+ }5 b& n U& r
飞机在围绕DME台等距飞行时的弧形航迹。
, m! _6 m9 l) S+ K区域导航,
; ^! z9 a h* @* i容许飞机飞行在有电台参考的导航信号或自备系统能
) G- M6 C. t" ?力极限范围内,飞行任何预定航线的一种导航方法。
* F& _; x) X+ L1 b模拟感觉
$ P1 l) k6 ], ~* Z3 N在飞行操纵系统或刹车
1 s% ^- g! F+ ^: [9 D, c+ L e* q动: o8 }( z& N$ h/ U7 N
吸气式总温探
+ v# b1 T& y2 i' r0 A* k界
2 p' |! u4 I8 }) b探
. K( C: _$ y( ?# s8 j& {装
/ K+ o7 ?. f0 [2 k3 V0 Y& T! d( D组合成. f. {# Q& m9 P6 ^0 E* }0 \5 C5 s
由* W( U5 ]( z, K
在选择起飞
3 c; q- u- c: m1 W度高的温度而得到的推力。用这种方法可以减少发动机的
5 i* ]' Y6 l; {8 }6 t' x# W磨损和维护费用。
g9 a* b' V. r3 k& \6 @: Z' u.: w [1 }+ |/ M9 G
英汉对照民用航空词典B OEING
7 A- \ s8 |. J+ v4 \TECHNICAL DICTIONARY 14, H, q( o8 |& {6 g: i
ATE, SEE - AUTOMATIC TEST EQUIPMENT$ q2 y, v" v0 \& U4 _3 J
ATMOSPHERIC PRESSURE, Pressure of air due to the
6 Y/ l2 Q# Y+ |1 Warth's atmosphere, expressed in pounds per square& ?) w- K' Y. ?' T$ k
ch (psi) or inches of mercury (in Hg) or millibars (mB).
4 U0 k1 G6 K p# eTTITUDE, The relative orientation of the airplane with; a2 z2 H7 {: K% u
spect to pitch, roll, and yaw.- F- _) E: V- F2 O, ?1 _
UDIO CONTROUSELECTOR PANEL, The panel in
" e7 `/ [. J+ w+ C5 Ne airplane which controls and selects the routing of
/ M, C+ S/ V+ W9 Q. d- P, kudio.
. O$ |7 Y2 z9 X8 Q% B2 ]5 h; sUTOLAND, Automatic landing using the Digital Flight
# E0 {% i& f$ d4 i5 a H k8 U/ ~ontrol System.% g8 n2 {& I& \9 G
n.
: S( r n" N" a1 g/ }7 {M, A system/ C, D, M7 }6 V$ {' M, V1 g
omposed of all necessary subsystems needed to guide
; F) X) e Q: i3 R& X& H. ?e flight of an airplane.7 T' g& a9 ] e- d9 T6 }
EQUIPMENT, System test
: `4 c. y2 V6 z( Kquipment that operates under computer control.
9 p: ]& ^* g# G0 g0 g7 M2 L; {装置, |
|