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AIR DATA COMPUTER, A computer which produc
, y% G& c$ L+ _+ {2 Z: T j* ~data information, such as altitude and airspeed, based% [( `1 Y" `( P+ N$ d
on pressure and temperature measurements.
( Y* u4 d1 }, P8 u- ^. q: d% nes air
2 ?2 S ^+ ]/ \7 m1 O a9 R5 CIR TRAFFIC CONTROL, A system comprised of. d4 Y+ U) m5 h& O ]
round and airborne components used to identify, track
& r( k: r) X# Q% j$ b5 M1 vOUND SENSOR, An electrical device operated
+ R1 V$ a. e( Z6 ?# j0 U4 U% N' [8 v% Xy the landing gear, which transmits on ground/in air
1 V0 Y- v; X1 |7 G2 P3 } Mformation for system operation in flight or on the
r' z1 O+ Z! y3 ?7 Wround.$ E1 p) {4 `2 P# y. i& ` m
IRBORNE VIBRATION MONITOR, The AVM takes
Z& c' i4 K# ^9 S( h" te signal from the engine mounted accelerometer and% n! L3 k) g1 @. \: l$ Y
alculates the vibration on that engine.
0 v* B; j% Z: l8 f" Jcorridor equipped with radio navigation) L; f5 C' r- l+ {4 H! a4 c
aids.
8 o' `5 T$ e A, DAIRCRAFT (or ARINC) COMMUNICATIONS
+ L/ Y1 y3 v2 J. _- r) q" z# F0 HADDRESSING AND REPORTING SYSTEM, An
! [' }/ y7 ?) I% Jaddressable digital data link system which permits the3 _. F8 L# |2 p9 F1 D w' b m
exchange of data and messages between an aircraft- p- u/ N K. K6 C" T1 e- L5 c
and a ground-based operations center over a radio+ }' h0 w" x: m8 M
network.
1 d; R% K, i, x/ q+ @4 {8 DAIRCRAFT CONDITION MONITORING SYSTEM, A
4 F& M5 a% H* nsystem of sensors and recorders to monitor various% h% h+ {) B4 @& F9 M* `: {7 Z
airplane systems' performance and status.
! Y$ d. r: x# [: c+ m/ E机,6 `6 p6 r% P7 N
中交通管制,' U8 M) j! T+ F# I
一个由地面设备和机载设备组成的系统。用来对飞机进
' c+ S+ A' E( }8 W! T. R: f- C地传感器,, ?$ ?1 ~2 c, Y+ ^( M
一个由起落架操作的电气装置。用于给空中或地面的飞
* M% v2 ^) c# D+ J' h3 A5 T f系统运作传输地面/空中信息。(有些系统只能在地面
. H' s ?& f& o. l$ ], @# k" n用)
- c; n- n. y X5 Q% x7 w6 c载振动监测器(AVM),. S2 m2 `! {+ x# [. s& I l1 ?8 p
AVM从装在发动机上的加速器取得信号后计算出该发; C, l$ D4 s6 |1 |' J
机上的振动。
4 m: l2 | g5 u* \6 F9 U9 k- u式建立的控制区域,内有无线电导航设备。( n9 X3 D& r T% X! a% v: s6 _
飞机通讯寻址和报告系统,) ^( c1 _7 }& {3 a: B8 S4 `, y. t
有种可寻址的数据通讯系统。利用该系统可使飞机与地
% R( O; q; e5 E面操作中心通过无线电网络进行数据和信息的交换。
: h4 l9 ?( ]" ^1 I! Q$ B' o飞机状态监控系统," w% Y) g/ a. ^# j! n! C: e+ e( _
一个利用传感器和记录仪对各种飞机系统的性能以及! @7 N7 w7 y8 o4 F, R; X
状态进行监控的系统。
' c+ b3 ?; U3 H; o+ nA
8 L0 y& B/ w; \( G, gg( Y! t1 @, g3 j& _
and locate aircraft.
9 F; G0 N0 W4 hAIR/GR
7 Z" [8 z' T/ h- k0 r5 `8 P3 @, `b
& A+ O# f. T! u$ ]) ~in
+ l9 R! X! _+ b2 c z% Z# Vg
3 G; G9 C3 u4 V7 {- j5 pA
, s# J" ?1 K, Oth& ~9 y- Z( Y. q# T( T( X3 p* b( \
c [. ^' V. z B. e
AIR WAY, A control area or portion thereof established9 L, P9 J$ h( F' T2 F( z
in the form of a
5 {4 O( s( u( V, s8 {' W大气数据计算
5 n+ @0 K( W, Z+ G+ X根据量取压力和温度而产生大气数据资料(高度、空速
/ O* g$ |7 g- H5 `" [7 r z等)的计算机。
4 q9 s6 H$ ]2 d$ f( W* H# ~- }空
6 L% H. f/ O1 B行识别,跟踪和定位。4 h, ]7 {+ Y- l L8 W
空
/ W j% ^! K1 z8 q) b7 m机
9 n( R; q: T: b4 Q$ T8 b5 D使0 N7 g# x. X% u% I
机3 Z; T! k, M5 L. ^% I; T
动
' n2 t2 }5 M& M6 w; }* s4 H航线,! ^ L* ~ g: [2 T% `6 x
以走廊形4 L# z9 T* e4 d0 {0 o' i! Q( W
英汉对照民用航空词典B OEING9 a q# w$ q6 s& l
TECHNICAL DICTIONARY 6% J ]* H% R5 ^: F4 L1 k8 z; J
AIRFOIL, A surface designed to obtain a useful reaction, J" `, G* @* ]/ a* A
such as lift, from the air through which it moves. Wings,
* T3 p! w9 c+ ~7 Rstabilizers and control surfaces are airfoils.9 e" u [' ], e; ?5 e) V+ F, {0 D' L# ]
AIRSPEED (IDS, TDS), The speed of the airplane
( l3 Y- A6 ]" Hrough the air.
, H* S, P8 `4 L9 YD INDEX, An adjustable pointer on the( q( Y' M( {) r
irspeed indicator.. T Q/ p+ a' W. C$ v2 t3 W
and legal ability1 v: O! D, K: e. E
fly.- s; E3 E* X5 _- ~1 Z( q' f7 |
m, for example, the procedure for finding the2 P! X) L. ?" n A* Y: y7 S
quare root of a number.
0 x3 ^2 k8 l5 Y: Y) ^3 a6 }& Oy
: Q7 d/ U' p/ T! d) c8 \4 W m# `* Dre, wind,, K4 j$ _& h: V9 U5 n( t
and aircraft flap setting.
9 i+ y P& v# p4 f是翼面。+ |" _% u8 W0 x8 i" Z7 P% U9 w
速,) R9 @/ g$ U+ m& |) O, E) U
飞机在空气中运动的速度。
9 I! d- t. `* @: R2 e; x; R, Q( M1 H6 I, ~6 ~* C& { C
在空速表上可以调整的指针。; ^3 | D8 m, i6 M/ `) ~. u
机械飞行能力、和合法性的飞机状态。
0 S/ s0 ?; R* _: f) t一步一步的解题方法。例如,计算一个数的平方根的步4 \: X4 H& A& E* b
。
2 a( F) d0 ]7 F2 u# z: T8 w能" ^3 K8 n7 h2 d8 d
资料的法定文件。
" A0 m& [% z3 O2 T0 o翼位置成函数关系。0 [- e4 Y2 `- u
th1 F! Y1 _0 P2 D% j
AIRSPEE X- O, a2 C, u( ]4 |
a% z4 S( |& U/ Y9 ]8 @
AIRWORTHINESS, The condition of the aircraft with! g" q# L6 }9 M- b1 h& i) d
respect to its aerodynamic, mechanical,
1 L# L- M' H6 E1 Ato
4 x# L! N3 U! _- ]9 bALGORITHM, A step-by-step procedure for solving a3 M& W- G0 A I0 z* T% L# L! g
proble
+ P6 \+ B- p* m" q, t' L( _" Hs
0 d/ ]! u9 F t, n/ @9 _AIRPLANE FLIGHT MANUAL (AFM), The legal
: u, M* q: T$ n% T& ydocument containing performance and operating limits,
4 v3 } e8 m4 M& p/ {% z9 [operating procedures, and takeoff and landing b: E6 S: Y( P6 W9 Z6 B& O
performance.
$ U9 U" Q6 |: G6 h" `; z8 k2 iAIRPORT ANALYSIS, A comprehensive set of takeoff
9 z7 Q: [* n! f8 U' I, }weight limitations for a given airport runway, generall" u ^2 G" q, o2 ]
presented as a function of airport temperatu, }) w2 k/ p0 G. ~; M9 W/ \
翼面,1 e/ I7 F4 x. c& Y; L' i
用以从气流中获得反作用力(如升力)的表面。机翼,3 G. A3 H8 |) m" M$ Q ~
安定面和操纵面都5 X) s3 N2 Z2 {( ]. `' r
空
+ u' s! L- ?0 e* B+ @' h* f' P空速指标
+ A' v5 }: _$ I9 W1 x0 C8 K* D适航性,
% {1 _0 y/ ?0 l) v+ i1 p有关气动能力、
/ A' ^* f! K7 S! n1 J" M演算法,! s7 o8 a- q" H5 ~6 H# `3 h3 y* J
骤
7 @7 M; E$ C& W* c飞机飞行手册(AFM),
9 g) c9 M, h# Q! Y# W/ w* W8 i包合性能极限,操作极限,操作程序,起飞和着陆性% U9 p8 ?4 M* w/ n& y
等
6 I) L$ [2 S$ h机场分析,9 N) O! }+ }& r: R9 g/ V" V" _
一套针对给定的机场跑道的详细重量限制资料。通常与
( y5 `7 B; G0 j机场温度、风、和飞机襟
1 J) p) z5 b1 |英汉对照民用航空词典B OEING& V3 B" E& g( j) j9 X3 ~8 j
TECHNICAL DICTIONARY 7# l# P) U% w( z1 `" {
AIRSPEED BUGS, Adjustable pointers on the airspeed
6 k& O8 G4 d& i. mindicator.
5 M* j% s5 Z6 R6 E5 \ALLOY, A mixture of a basic metal and small amounts8 u+ F4 D) i6 @+ x" F" j* e
f other metals to change the properties of the basic
2 \5 v2 Q5 x5 y7 ?etal.
. C! R! h8 C0 O% g7 bMinimum airplane speed.
8 C% @$ l5 v1 ^4 Xe of$ _* J$ {" o$ B) o7 t
itting airplane angle relative to
~0 r5 Z$ M5 s( [ ^& zirstream for the stall warning system.9 ?" Z, A7 n* w8 X3 O& F& E& x7 f/ @
another.! x5 d( |6 e. c2 R
LTERNATE , An additional airport selected during
* B0 K7 D1 x0 r& n4 @,
: j8 k1 \+ ~# I6 e5 I7 m- W) J合金,
7 X& R, ]- ]8 _4 o0 m在金属中加人少量其他金属,而改变其性质的一种金属
! _9 C: `4 D" \; ]/ W合物。
6 i# }( C# N' E4 C' X5 ]飞机的最小速度。
. C: J' ?0 K# g速警告系统传输飞机对
1 Y9 y- n; x; r. m. [; w% b% G流的相对角度。
- P) L2 J O+ W x由一个状况改换到另一个。
# P6 t# ?+ ^5 C: `% F降场,
; C, r9 a0 D- a1 F* h) @划时,除了目标机场之外,所选的另一个机
5 k2 T- Q" ~' P; Q, F; `! G, ~o
& X+ C6 W5 a% v+ w( s5 Jm) ^; K# C( l" }; r/ q3 M
ALPHA SPEED,3 l, z1 S0 i8 X+ ^. |
ALPHA VANE, A small moveable airfoil on the sid
( M& \/ D# X1 Uthe fuselage transm
: q6 }9 p0 B6 W: G) R ba+ G% v, ~/ o2 k. b7 g
ALTERNATE, To change from one condition to9 O4 E' L8 T, D
A" W* W& K3 n1 i8 Y+ B0 b
flight planning, usually near the destination airport, to be
6 \$ p7 |' k: R0 h, f' v8 D1 |used when it is desirable to divert from the original* l8 D$ R6 O' o
destination airport.' K. J6 V* ^/ }* H! F. @
空速游标
( \" E$ B1 i7 O B, a6 {: t) s& [空速表上的可调指标。
5 X/ |0 h9 { x; ~) O) _& Z8 v混
7 B. X2 K4 o* k8 y5 C迎角速度,
" w7 N/ t/ q' P迎角叶片,
- W+ G$ B1 i, @$ ]# x$ W* `; V) N* {位于机身侧的可动小翼面。为失) m) D o2 q$ A5 z/ r; ?- X
气- O0 i. A8 R9 P& f0 f
交替,
0 |7 B1 V0 K3 m. }2 I9 y备
. O& ^! t& P- p# S& F$ ~制订飞行计
$ Z3 G0 R7 t0 Y( J4 X4 ^3 g5 F) w场。通常在目标机场附近,以备不去目标机场时,改降之
+ v5 ]" ?+ D/ i9 r; c& H) m0 B4 q用。
! ~, g' i' K4 N, P: N英汉对照民用航空词典B OEING$ a* A! T& i6 a! y8 R
TECHNICAL DICTIONARY 8
@9 p" p \; v, _ALTERNATE AERODROME, An aerodrome to which% }' H( N( ]8 _3 e# P1 e4 s/ T
an aircraft may proceed when it becomes either
6 q! a. o5 P3 ~# \" q9 Opossible or inadvisable to proceed to or land at the
5 F% W6 I3 r7 Oerodrome of intended landing.
( q1 @; }) W- r' t, nTER SETTING, The adjustment of the altimeter
u O, l: }, O9 K/ haccount for local variations in atmospheric pressure. Q7 y L; Z. ]4 I9 V
LTITUDE ACQUIRE, A digital flight control system
& O# G" k; F0 H5 lode to transition from climb (or descend) to level flight. r3 Z; ^8 t |2 p1 |
LTITUDE ALERT, A flight deck alert occuring when the. ]2 R# i5 e1 l8 E
irplane approaches or departs a selected altitude.) L" B+ X4 l+ H6 A. K( a% r5 h
LTITUDE CAPABILITY, The maximum altitude at
/ U- c8 o; F' Hhich the airplane can be flown at for a given thrust,
9 g/ e% Y1 O) c$ Q3 O( r8 I9 p3 w/ ? Fpeed and atmosphere condition.2 u8 b) q8 W) ]7 M
LTITUDE HOLD (ALT HOLD), A mode of the autopilot
, c7 e& l& u- `: s7 b2 ?r flight director to maintain a selected altitude.! ]8 m3 u% [; }! I
irplane's altitude during VNAV operation.
1 V7 Z" l+ Z5 _! V8 F机场着陆时,可作着陆使用的
8 m( k1 ]. @" [, s3 U场。8 `0 L2 k' i I) d3 r2 d7 j
,
+ _3 u. U% @0 r7 Y6 Q! P/ l根据当地大气压力变化而对高度表所做的调整。9 Y" B/ @5 P3 x+ q. } P
一种数字式飞行操纵系统,从爬升(或下降)改平的模' i* q; |0 w7 H& b3 V
。( a6 E( H* i% u; |; _6 D
度警告,4 }+ H% I A4 R0 S
当飞机接近或偏离选定高度时,所出现的驾驶舱警告。
2 I3 f n/ {0 s% Z5 L高度能力,: u. K G2 d* J: T; C
在给定的推力,速度和大气状况下,飞机能飞达的最大$ q, }# h6 M) p4 z
高度。
9 ~* F! L0 v' U$ F4 |. |4 _1 U高度保持(ALT HOLD),
9 _( b `$ A/ q, b. S6 g& Z6 F自动驾驶仪或飞行指引仪保持在选定高度的一种方式。. Q; R) z" m6 y2 |6 j* e
,
* b; d' B* s/ I; o% @1 C* W员对飞行高度的控制。6 i) W$ a! P( R( m( U9 s
im5 C" }6 ~9 w Y' L- V& }' Y( Q; T
a) O8 C2 Q+ K" K. G4 v% j0 I/ U
ALTIME) F" X1 I& W# r2 E3 c
to
# X1 x' j) R5 s0 VA
0 W( e0 f3 R! b! R$ N! cm
. z/ c- c6 @# J! V$ P& pA# f) ^% N- Z8 d; t" `
a
& a/ Z9 S( U- o4 P3 N; M: A+ cA
" c/ N0 r8 h6 J- f: C# Mw
' |& v* z9 V6 O' s! f2 Is+ a E+ W7 r+ z: l! a
A
" \5 P* f/ Q. ~7 fo
/ L) i% Y+ j4 y- nALTITUDE INTERVENTION, Pilot control of the/ q0 i# R& k' x% m k2 I
a
& r. c2 f) _: F1 h2 T' B+ mAMBIENT, The surrounding atmosphere.3 r3 ~7 o7 `% Y, z8 V2 o
备用机场,! X/ _: ~8 Q6 Z% N
当不可能或不适宜在预选
- t$ E! m/ u |机
' E* G# @0 H! H8 @ w4 u: K高度表设定
A* L! z6 P+ d8 |8 A, f高度截获,
% ~" m' A% T& _' d( _. i式
1 A* k/ ^; ?' `4 }4 N) Q5 p高
9 D) a G7 A; x" _: p; f J高度干预
" }* c6 n/ Q* L在垂直导航工作过程中,飞行. U, [0 g& V) R4 `) G" v9 ?
周围环境(地面气层),* G9 |7 V/ Y% G7 k# K% N
物体周围的环境(特别指大气)。9 g* D, T9 i. s% u
英汉对照民用航空词典B OEING
/ E# L8 g/ A0 v5 @3 [7 gTECHNICAL DICTIONARY 9& }$ S- b* C# \7 [3 I: f" z
AMBIENT PRESSURE, Pressure of air surrounding an' ?+ H" L2 |1 d2 [6 V
object, measured in pounds per square inch (psi) .' f, _* `: `" l; _4 e
MBIENT TEMPERATURE, Temperature of air
q/ y) W. {3 ]! t& cmpere.! U& Z3 F0 W* G
urrent waveform.
9 y% |: `9 a4 O; g: }, pg an
7 N' }! b: y8 c7 inalog signal to a digital signal.. F, L) l5 C7 @. ~0 A
ore inputs
. h4 I3 S( l$ ?" B. ]f binary digital information and one output. The output- |' v! J @' J: N) X# I- D
1 only when all of the inputs are 1. The output is 0
9 r) j4 A. \5 h# L/ h0 vhen any one or more inputs are 0.4 \& Q$ I9 \ [. C; Z
面气压),, d0 ?4 P& A* g& ?% O+ `0 W) M4 o
境温度,
3 _/ A6 q2 u& k; B/ v' ?/ k2 t气温度,用摄氏度(°C)或华氏(°F)来7 b% o/ L0 v5 P+ Z! B6 d* ^0 \
。
: ~; ^8 o6 N+ Q/ |9 K电压或电流波形的幅度。2 _) g7 m7 H0 A& g
性变化的信号来工作,或产生连续性变化的信号) D1 T& a/ a, N4 d! |% G1 g
统。
' }8 m m+ N2 b/ \+ m将模拟式信号,转换成数值式。
. k) ?5 B+ M, x一种有两个或两个以上的二进位数字信息输人,一个输
+ F$ x9 m+ y( P7 I的装置或电路。当所有输人为1,输出为1。当任何一个3 U8 }0 f( s9 s9 z8 ]; F9 \
一个以上的输人为0时,输出为0。: p% I3 z; F2 Z4 i: E
A
; T' s, Y; |0 y+ p9 i2 Xsurrounding an object, measured in degrees Celsius
& u3 B- {1 T! K2 w(°C)or degrees Fahrenheit (°F).
: ^" q9 N {. BAMPERE, A unit of electrical current. One volt across
$ _7 }- a" q3 T' K" a8 m6 Z6 xone ohm of resistance causes current flow of one
* `% K% J% k( N! B2 o* G# I" Ga- N. a( m1 }2 _- K
AMPLITUDE, The size or magnitude of a voltage or
6 [' v! ~! M" v! jc
1 O9 N( X7 g1 |) wANALOG, Quantities or representations that are: F, W0 [' [# L, k8 c" U/ u
variable over a continuous range.% b! c' T% t$ }4 M2 A! L
ANALOG-TO-DIGITAL, The process of convertin
( B" b, _" m, Z, T; x$ Pa
7 u+ N% i+ r, L* N1 B6 Y. B: ]AND GATE, A device or circuit with two or m
: R* j! t$ V% [1 Fo0 C+ k/ X c9 ]. Y3 m$ L) }' Z
is q. t& v4 I7 S- {, A7 j7 R. N2 \! d
w
) x- ]% c6 Q- T: s7 T% |6 Z% ~环境压力(地
- C2 b' H/ T) q$ m7 [物体周围的空气压力,用每平方英寸多少磅(psi)来
6 R' ~1 E8 }* w; @度量。
" j3 L- b- P6 V, V% j D: l环
& U4 T* x, r0 |物体周围的空8 c# p! V5 n0 T; r& e6 q
度量。* y' n* A" `( G9 N- u0 g! ], l
安培,' s, l+ J" I9 y8 w5 k8 D' Q
电流的单位。1 C# u; l7 J* n* f
1伏电压在1欧姆的电阻上所产生的电流为* \' E6 D& K5 o7 b7 }; {5 D, O
1安培
5 s) i- S4 @( B; h [/ t, r% A振幅,7 ?/ s x; h- s6 X# @
模拟式,
/ u! Y! s5 i; E+ V! U" ~' n+ f用连续: O& i M' S0 A" F7 x
系0 |1 A5 i( C0 k% M2 ]7 i: N# V
从模拟式到数字式,
f( S& i: S! D& D( _' y: {! _与门,
5 S8 e' A( \6 w+ |出
; {3 z% Q$ b; k7 Y# a7 y9 ?或
0 p, R' A: A2 d$ v英汉对照民用航空词典B OEING* h3 S$ v' w$ q, i! B
TECHNICAL DICTIONARY 10
* f2 L, q- c8 K' U& I$ Z6 s8 OANEROID, A sealed flexible device containing air at low
: w$ [" F& K8 ?' N R- }# gpressure, which expands or contracts during change of4 N4 M8 z: X" q" g- b7 R
ressure outside the device.9 B8 w ^5 v& s
ically
8 i6 F# `) m0 j# G! K5 ~; V* k D- Sr changing the direction) l) m0 B/ T! m
f drive.
' ~7 O. ]) x$ ]of the wing chord in
0 ?. F# H! \: Q3 I+ \lation to the free stream airflow as it moves forward* w8 Y9 p& S, p2 m2 w- p% [
rough the air.2 ?# T Q* S/ z# ~/ b
al axis of the. i3 T* S. o# D) q1 [
aircraft.
! W" J1 A& V7 e胀或收缩。
; [0 T5 c! y$ C0 h箱。是改变驱动方向的机械装置。+ `& _) n8 V' F+ F
机翼翼弦在空气中向前运动时与自由气流之间的夹角。
7 J$ t4 @; q8 W% O/ z# N。
- g" `& o% z$ j9 ~6 c8 qp
' { x0 B; W+ K" v$ {7 uANGLE GEARBOX, A part of an engine, mechan
" j- O& T% g, n- \/ E2 n- mdriven by the compressor, which drives the accessory O% z" w4 |9 |3 A2 Q
gearbox. A mechanical device fo3 b: M8 k2 g: N, v
o# d. m# C3 g" ]6 w3 c2 M
ANGLE OF ATTACK, The angle# N1 q4 C8 s' U" t
re
) b9 C# b0 Z* Z- P2 Mth0 G5 W0 c5 m& N* v! ^) K8 A
ANGLE OF INCIDENCE, The acute angle which the) h" G1 |. W( ~
wing chord makes with the longitudin8 X+ i* n7 _4 R% e
膜盒,5 o3 J( [! G, K) r& `6 L- S+ e
内含低压空气的密封弹性装置。当它周围的压力变化
# D- g7 D2 d$ Z0 h q$ ~* Q时,会膨9 T {- D/ o6 L5 }
伞齿轮箱,
3 O6 C) n! a- I0 C发动机的一部分。被压气机以机械方式驱动,然后驱动
# a- t( T m; x附件齿轮
' A4 z) m+ ^" E# u7 d4 E迎角,% B6 M# k' F& b2 s/ \( s
安装角," C9 U# A- q4 V! V" Y# t2 R
飞机的纵轴与机翼弦线所形成的锐角
9 b! H2 d) r2 G0 ]/ Z* J+ ^英汉对照民用航空词典B OEING2 R! [* B r5 w7 O' H* k
TECHNICAL DICTIONARY 118 t3 _1 U1 }# ^! Y
ANNUNCIATIONS, Audio or visual indications used to
* ^' x; `: @7 o/ j7 x6 L9 }call attention to an event that has taken place.
+ h0 N5 [7 @- w) U) @6 a7 gANNUNCIATOR, A visual device consisting of a number
: J b7 U% [# S I) ]ly.
9 r) h+ _: w6 R% h9 F6 {ANODE, The element toward which the principal stream- G$ `7 @3 I' ?+ h9 w. N! m
of electrons flows.& b0 C1 ~& I% d
ANOMALY, Not normal.5 ?; q7 ?7 V6 E6 N% c1 d4 ?
ANTENNA, A device which, used in conjunction with a
4 d$ V: v+ d3 I" D1 ?; gtransmitter or receiver, is used for radiating or receiving6 p/ x( m& R4 i
radio waves.
9 H) W2 ]* G& f" M1 N4 x5 w- D$ [NTI-ICING, A method of preventing ice formation on
8 i. T6 E: g+ l- ye wing leading edges and engine nacelles.
5 ^- u. u# P" W' @# q8 qNTI-SKID, A system for providing maximum braking" D: w% p& t6 K8 M/ x; {2 J
ithout skidding for any runway condition. Anti-skid% U0 n) K6 L2 }" ~: `2 p
omponents are part of the brake system.
: Y; _4 o5 C/ I7 {告,
& y+ V8 h! |' k, ]0 E当发生事件时,以声音或目视指示形成的提示信号。# _6 H# M3 E% {( E
与之有关的电路的现有情况或已存在的
! r/ \8 M' H) C% j* B/ P6 m# C. w况' J! ], ]: O# }& O5 J0 e
正极,
! {+ f3 }- b' X$ f8 T- s- I主电子流向的极位。 H S; K- j9 D
异常,
1 z$ b+ X X Q/ R不正常。
I$ U; V$ m$ m5 u% m2 i! g5 g天线,4 P/ _! [0 J7 B v4 G
一种与发射机或接收机共同工作来发射或接收无线电
. L& ~, V7 ~$ T波的装置。8 F: s6 j5 e" C! l) s2 Z
冰,9 Y: U. C8 [7 P4 E
防滑系统,
" ?/ C- ~/ j- J2 K一种在任何跑道状况下,都能提供最大的刹车能力而不
z1 I$ L) A& `7 a. ~9 ?使轮胎打滑的系统。防滑部件是刹车系统的一部分。1 \; R, x* t$ t
of lights. Each light indicates the condition which exists9 ?4 R. W. j: H9 V, D( o
or has existed in an associated circuit and is labeled
" P% I( ^9 B( i! Faccording
. Q/ W7 Y- z9 @! l" dA7 t4 }* B- i9 Z& e& B4 f3 S4 J
th6 d$ {6 f6 p, p% ^
A) I# ^8 y P. E! a' e9 {4 {
w( G) l; Y' s) l" ]2 I
c
+ P; c$ d5 }; Q. {$ K5 `. R通
' c- h2 A- U5 j4 O2 a) H$ R) h, O. r信号牌,
; j0 |/ K+ y5 R由一系列指示灯组成的目视装置。每个指示灯都有相应
V7 _6 {* C! m5 o的标记,用来显示4 S! m" l% m/ ^" r
情
2 G0 c; a- a& F& [4 w防
- M9 }+ \& s9 W9 P. |防止机翼前沿和发动机短舱结冰的一种方法。
: t5 K' C; p0 N) I) |英汉对照民用航空词典B OEING# w8 _+ m3 C4 A! T+ s+ V' K
TECHNICAL DICTIONARY 12
n: d; G5 f5 Z5 h" z8 cAPPENDIX, A supplement to the Airplane Flight Manual6 i3 Z3 }+ b6 F( c: d5 z
tained in the basic manual. A5 ?( z) \. q' {; c$ Z$ j
ollection of supplementary material at the end of a
4 W4 M" y( {6 l+ U1 j7 jook.
$ H+ ~7 d" M0 }0 Q2 B: c* }of the
7 n- `* k: P- @5 x- jrsion link on the landing gear.: o/ ^8 w1 e9 l3 S) I) z
APPROACH MODE, An autopilot/flight director mode
3 R" M+ `, b& _ W+ g6 t# r( x! h Qwhich is a combination of localizer for roll control and/ d2 d7 U& G4 R; N' s
glide slope for pitch control. This mode is used when full
6 X! F/ I8 i1 A( V, B8 H7 oinstrument landing system is available.8 H0 l& @. @, t7 J1 r" s* d
APU, SEE - AUXILIARY POWER UNIT
3 R6 e. ~5 z2 I3 l0 o' G" lARINC, SEE - AERONAUTICAL RADIO
9 o5 R* n: R( [; Q8 nINCORPORATED
2 p: Q9 P+ Q6 ^. @ARM, To make ready for operation.
1 V# V8 e. ?, K1 T附录,
0 R# X' r \2 z+ V飞机飞行手册的附件,包含基本手册中未提到的飞机形$ `$ ^) P+ [4 y
态的其他性能。是附在手册末的补充材料。
# ^( w3 Q" X3 c1 s0 U: ~% H顶销, Z6 d1 @1 @7 q! M
用于连接起落架扭力臂两部份的销子。
) w; r1 ?% |; ~: H9 { E6 X3 V进近方式,
: c+ C# Y) N2 o' |3 j一种综合了控制横侧的航道信号和控制俯仰下滑信号
, s* h8 I% R- N$ ~' A的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系- I. Y Q( [# {% U6 x% M# R Z
统正常时才使用。7 O1 v D3 t& ?6 {* \7 t: j
辅助动力装置,
8 B/ ]% B9 L1 b E e见Auxiliary Power Unit; I8 }* s: ~7 v5 |
containing additional performance for aircraft
2 o5 o2 f. W) o, E( yconfigurations not con
' d+ T8 u* ?4 E' Xc" B0 @, S i1 y% J& c
b
8 C1 N7 W7 }( mAPEX PIN, A pin for joining the two sections& O2 r( N/ i& a" E8 m" N M7 @
to
/ E! B4 \ m y' B. E, k.1 p* U3 t! T9 Y5 K: l1 e
航空无线电公司,$ S$ q3 P0 }, x
见Aeronautical Radio Incorporated. P1 V3 a7 ~8 s! V& [# {$ f
预位,8 j" l/ c/ t: c7 J. U; s
部件可以开始工作的状态。9 x# n9 I# [+ |7 I
英汉对照民用航空词典B OEING, _6 n( \; k/ H" O8 v) n
TECHNICAL DICTIONARY 13( E" F8 S' J0 |4 G
ARC, The curved track over the ground of an aircraft; `' ]) P! E/ @' N
flying at a constant distance from a measuring& ~* k1 G6 }; c( E1 K0 `+ p
equipment (DME).
( r/ l, A/ _5 K5 P6 m$ H) h {in the limits of self-contained system
1 _" u3 P5 {. O8 Hapability.3 i% n3 O( v" W2 N h
tem for opposing or restricting6 ~9 j+ |5 x7 S$ {& `- t
ovement.
3 O. R- U: C2 D+ D2 x1 rSPIRATED TAT PROBE, A sensor that measures total! L- m2 c; w; [2 W2 u
ir temperature when the airplane is in the air and that; r6 b, r3 Z7 D' E- |! T
easures outside air temperature when the airplane is
6 F/ J# U" p- ?& \9 R+ En the ground. The outside air temperature is measured
& o- X6 N, b+ w2 ]8 o1 \7 tSSEMBLY, The fitting together of a complete structure0 r' h5 _2 \1 M9 a, C
SSUMED TEMPERATURE REDUCED THRUST, The
2 i4 b; r( q& N5 ~, F( LATC, SEE - AIR TRAFFIC CONTROL- R `/ v1 \4 k [6 Z
,5 l1 I2 I8 A" e8 N0 c
系统中所产生的一种用以抗拒8 D, A7 i+ ^' Y6 {4 b, ^, P
作或限制动作的力。
3 G* z$ u( E6 J L头," h+ G& G) O# N- r: d
用来测量飞机在空中时的总大气温度和在地面时的外
4 x. q2 N9 |* W9 i1 A0 A; o温度。地面外界温度的测量是利用引气将外界空气吸入, y+ `2 W! f! B/ O1 B) ~6 Y: }
头,以达到测量的目的。
1 G+ ~7 c2 U6 ]: r配,
4 v' e1 e3 |% ~8 f一个完整的结构或组件的过程。
9 R* Y# O3 `; a假设温度而得的减推力,$ S" I8 \- }' J
推力设定值时,假定一个比实际外界空气温
" I/ n6 g9 P6 m# {3 `1 {2 T/ a$ d空中交通管制,
7 x8 o( L3 y/ k见Air Traffic Control! K& E' m. Q/ j+ Z7 G5 `
AREA NAVIGATION/RNAV, A method of navigation5 y7 R! E K2 t( j- ]
that permits aircraft operations on any desired course
! R1 r- O, N' t! Q/ Lwithin the coverage of station-referenced navigation& H) _6 u6 Y o7 ]- ^3 E2 }! n
signals or with/ q3 N) M& k# _: u
c/ F9 c; L* {3 g& Z- w# ^
ARTIFICIAL FEEL, A force developed in the flight
M- o4 d; E9 R# icontrol or brake sys
1 Z5 V9 a* P3 y) x' c2 Y& F1 um/ T# U0 _2 Z* U0 F5 {
A* t& ]: z4 J/ {5 _" j1 F |
a5 P$ L4 b0 N; J
m
6 p8 q# i. G, B+ U$ u- Co
6 i4 }% Y8 |8 s4 w0 K) @8 R. ~: e7 y6 kby using bleed air to draw ambient air through the
4 N( b- ~$ n0 R7 Y, b! xsensor when the airplane is not moving.
# @4 R, c9 ~7 F" ~4 R% CA
7 D# y( }# g; B: f9 Qor unit.
9 N3 L T# b- i6 _A4 l& n3 S2 h% l* {) H7 d9 H) r
lower thrust obtained by setting a higher than actual* \' \& L/ K: x7 Q5 w1 \5 ^
Outside Air Temperature (OAT).
2 k5 p! L& T @6 a( X( ?弧线,
% P+ Q7 u8 R( K6 K3 u/ F飞机在围绕DME台等距飞行时的弧形航迹。9 _7 F {' d9 I- h
区域导航,
; J: L: b3 Q, {: C! X* V容许飞机飞行在有电台参考的导航信号或自备系统能2 \! c$ P& ~2 g& D# i
力极限范围内,飞行任何预定航线的一种导航方法。, O2 D- t: d9 X; G2 D
模拟感觉
* R! _( \. H0 X+ V% q+ c4 b在飞行操纵系统或刹车
# f7 ]8 `; M1 g动: X+ l4 b" ?& B; G2 e6 \9 t9 A8 q
吸气式总温探
2 X( {, ^7 a8 x8 J7 U, m9 C" q界: |$ i% S3 K7 K! V
探$ a# {5 t. a* j; @) ?
装
1 K' i8 B* Y' y! A, l$ y组合成1 W9 [* [7 W7 T- A% x
由9 z4 m6 F, |4 |, }1 m6 s. N
在选择起飞
* S! T6 K& G* R8 z度高的温度而得到的推力。用这种方法可以减少发动机的
8 w2 k# ^8 N7 G! E磨损和维护费用。
- f2 `$ {# @- R( d.
7 c. C9 r3 s) D* j英汉对照民用航空词典B OEING
. z$ J" S* V) z; [! u; n( uTECHNICAL DICTIONARY 14
0 J* U$ ?! D; |8 I; ]ATE, SEE - AUTOMATIC TEST EQUIPMENT
$ B+ C( C8 o, Z l2 l* ^ATMOSPHERIC PRESSURE, Pressure of air due to the
3 m" d' u9 r: S% M6 Zarth's atmosphere, expressed in pounds per square
. v" E2 u* }6 ^ch (psi) or inches of mercury (in Hg) or millibars (mB).5 s/ N& y% Q! p8 ]# w
TTITUDE, The relative orientation of the airplane with+ V- G$ C$ k3 I
spect to pitch, roll, and yaw.
" b* ]( x/ l( y5 R: v6 DUDIO CONTROUSELECTOR PANEL, The panel in# {; n2 @$ `% J# R+ ^' P- T
e airplane which controls and selects the routing of+ l) K2 b* n5 z$ U
udio.
8 X8 E+ a* K, n7 U8 n$ g. JUTOLAND, Automatic landing using the Digital Flight
* U P" ]7 ?7 n9 Oontrol System.
% `3 ]" A7 X% e. rn.# U5 b# W' g* M4 v/ w) T, O, ^/ s6 d& m# Q
M, A system
2 C3 ]# C; K1 V) }omposed of all necessary subsystems needed to guide
* p/ k1 |4 I# D! ` q5 _e flight of an airplane.
/ h1 t& {/ V" u5 }# G6 I6 wEQUIPMENT, System test, T2 g2 R) ]9 a8 m0 D1 V: k
quipment that operates under computer control.
. W$ H f6 N0 @% o7 P装置, |
|