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AIR DATA COMPUTER, A computer which produc
, `( z, Q0 z: U1 udata information, such as altitude and airspeed, based
9 e: O, _1 x( b" w, ton pressure and temperature measurements.
2 _9 N2 P" S) C0 @4 K' [0 Oes air/ Z @5 t" C) i
IR TRAFFIC CONTROL, A system comprised of9 w: n; [- A) M) h' k
round and airborne components used to identify, track/ C( Z2 g) H+ H8 v" D y
OUND SENSOR, An electrical device operated0 q5 ]; d$ J4 j1 A5 s+ C6 C
y the landing gear, which transmits on ground/in air$ J1 T- r7 p+ r& L
formation for system operation in flight or on the
3 I0 ? z4 p" m5 iround.- R7 K: G2 v: v) T
IRBORNE VIBRATION MONITOR, The AVM takes( `( P# N$ m5 d8 P, ]" j3 ]
e signal from the engine mounted accelerometer and4 q- i0 w! r8 }4 w3 M J# [
alculates the vibration on that engine.9 f; W# Z T( Y6 T! j
corridor equipped with radio navigation% h. v: W1 W7 H6 x
aids.' l# b& z# |* u9 r! g0 t% O: |
AIRCRAFT (or ARINC) COMMUNICATIONS
0 v2 I0 d4 `+ M# r$ R6 u+ nADDRESSING AND REPORTING SYSTEM, An
9 a; \( ~ L# y: N7 _9 Zaddressable digital data link system which permits the
2 W- g* ]$ V( C' b, |exchange of data and messages between an aircraft: O% R$ w X* c5 J: r+ T
and a ground-based operations center over a radio
2 y' I& F5 o7 F5 z! i/ Q4 ]network." q. i, j g2 H! A2 t2 D# P, O
AIRCRAFT CONDITION MONITORING SYSTEM, A% |" \/ s& K3 j# @6 e$ x6 G
system of sensors and recorders to monitor various) p* v3 a" u0 K. c' n( g3 C
airplane systems' performance and status.
+ p2 h9 v& _( r/ B7 m6 ^7 |机,! {/ v% `" I0 L. e
中交通管制,
8 t$ Q+ I8 L/ j5 {& F& b一个由地面设备和机载设备组成的系统。用来对飞机进
; T, ^! i8 O! ]7 v/ [1 s# b5 g! ~地传感器,* j( Z5 d9 u1 u; |$ G+ t4 m( u8 r* A
一个由起落架操作的电气装置。用于给空中或地面的飞) S5 w; K: D) S6 u
系统运作传输地面/空中信息。(有些系统只能在地面* \+ Y/ B% `6 u8 V
用)
' Q; c# a4 G. }5 s; m; [) V5 R5 |载振动监测器(AVM),
7 h! o5 z7 Y7 U" D" s, v0 g# eAVM从装在发动机上的加速器取得信号后计算出该发0 y3 u0 @& t0 B l
机上的振动。
) z1 {% R. W, K7 K% W式建立的控制区域,内有无线电导航设备。) ^0 |4 N2 ^0 O [
飞机通讯寻址和报告系统,: p! j! K- a5 R, e
有种可寻址的数据通讯系统。利用该系统可使飞机与地
* I s; s+ |8 p3 S N; @$ H, _% E* t面操作中心通过无线电网络进行数据和信息的交换。* I; R, ?/ E) i1 m
飞机状态监控系统,( p/ U2 o4 E. ?' [/ j+ h
一个利用传感器和记录仪对各种飞机系统的性能以及' H; Q" e8 {, U. s
状态进行监控的系统。, T5 b- r% W( Y4 a; ]& Y# N
A
+ T: e4 d/ k! O. d1 p1 X( @# N' ?g5 N% X+ z0 \! l8 S* @6 p2 ^# G4 h2 O: A
and locate aircraft.
, e! B& m4 }2 K; }AIR/GR
4 Z3 R1 B: F9 y: wb1 L6 C3 i/ U% X9 j$ w
in2 }" g- W, f# ]% _7 D" F& M6 j
g
0 i- D `- d6 w; J4 zA; n8 _4 ]; ]5 D7 w7 f* Q
th( y1 G# Q2 `6 W" t* T6 N, [
c3 f8 W: g: v" @$ j/ v# a+ ]( Y: O2 F# z
AIR WAY, A control area or portion thereof established) f; [6 C/ i5 o" ^$ w( U6 o3 j
in the form of a
& r, N9 o- }, @2 V大气数据计算( m2 c+ h ~4 k+ ]6 s
根据量取压力和温度而产生大气数据资料(高度、空速1 W- N( N" `! `1 y
等)的计算机。
+ X8 g8 }. C7 s( y0 V; H' H空
* V/ }) E( i! h1 M行识别,跟踪和定位。
/ d6 Z& i% O2 v8 N. r! F# J# C9 A空
; @ A c& J7 d机# N% E& r* j. ?9 N& a, f0 @
使
' S& j( X1 ]' B- n机
+ F$ T0 S/ O% r. q1 R! j动
: {, a. A, ^) J+ y" ~; S航线,
* p; J# W- L b以走廊形
7 V( q" Z n5 X' \7 y英汉对照民用航空词典B OEING( ?5 j. l4 u# S( Q% s% z
TECHNICAL DICTIONARY 6* A( L0 H( ?% b6 V, D* U0 H& p% F
AIRFOIL, A surface designed to obtain a useful reaction,' G) O, D+ a6 R: _ w$ [
such as lift, from the air through which it moves. Wings,
. e5 A: i, b) E4 b- rstabilizers and control surfaces are airfoils.) W: c6 W8 V1 U) U9 a
AIRSPEED (IDS, TDS), The speed of the airplane
7 e7 g4 y) m9 s: L _1 Z1 ]rough the air.
# Y) E+ d. {' K5 g. R" n [D INDEX, An adjustable pointer on the
- F" f2 P: k5 R/ kirspeed indicator.
0 i2 [8 s. z" `7 w9 ^5 Yand legal ability) F9 h3 p0 P1 B1 s: M
fly.
0 K. R. s3 m8 F- @: }5 Rm, for example, the procedure for finding the
/ P0 e% ]( Z3 i) z" N% B6 \2 C) Qquare root of a number.% j9 S# D5 y0 m
y! i! |9 }+ x, D
re, wind,3 {( [' J `: F+ r2 a' _
and aircraft flap setting.9 C; \; B7 V3 X. K
是翼面。
0 Q! c8 }2 H8 P速,; r4 t. A0 y: g* V- G' s- M/ V2 c8 q
飞机在空气中运动的速度。
% i# Z) {4 G3 G,
- m- A9 x3 l8 w在空速表上可以调整的指针。0 g) Y9 E: Q \/ \, T# d, Z
机械飞行能力、和合法性的飞机状态。
" }' ]0 C+ u; N) ~4 T# T! d, C- p一步一步的解题方法。例如,计算一个数的平方根的步
- L! Y1 R) J; i. G3 l% u5 r3 c8 N9 T。
: ^2 F; u; W8 j# {2 h能
n! q! ^% u4 m) H/ x资料的法定文件。
6 C1 N8 E- i4 C5 x1 \. j翼位置成函数关系。
+ ?3 E$ D. f v3 z) H* Hth$ r k, B0 {1 M; `) J
AIRSPEE
; M3 j( O6 O6 Ia
$ l8 c \1 N8 bAIRWORTHINESS, The condition of the aircraft with, S! {+ k8 u" T! ]9 L1 k
respect to its aerodynamic, mechanical,
% s+ p( D) D d) \to
, c% v4 O7 [! B/ [) u% UALGORITHM, A step-by-step procedure for solving a' b' U7 A, Y# ? e7 t3 k# c
proble. t3 Q( I: ?# s( L( d9 t
s
* G/ E/ m7 h3 X$ Q- Y( \3 h$ L7 W* OAIRPLANE FLIGHT MANUAL (AFM), The legal
$ ~# e; a: ]' V* m+ `document containing performance and operating limits,1 Q; y- t/ C d! l& s1 @5 c
operating procedures, and takeoff and landing
- ?) C# M1 D. ~performance.
& @1 S9 s6 H# E" u8 a- t& TAIRPORT ANALYSIS, A comprehensive set of takeoff( C6 e9 u: q8 o# p$ X0 c: G
weight limitations for a given airport runway, generall' A& V! p- V1 j$ z
presented as a function of airport temperatu
6 q# D* g$ F: d+ m b翼面,. _2 \% c% z, r' T0 X# s
用以从气流中获得反作用力(如升力)的表面。机翼, d* k% G, ?# y& i! M4 _4 q( ?
安定面和操纵面都
+ p+ d, \& ~5 U, V% b4 n2 i u7 {空
0 |) `+ d' t) c. I: x! j2 P0 L- b空速指标; V/ `. F4 n+ k m9 j
适航性,
% r6 l! Q( g0 e& t; p有关气动能力、6 e& R) W+ v) \% h7 [7 I
演算法,: r9 D/ l; N0 S- ]
骤! t, d9 n9 E, M: k5 u
飞机飞行手册(AFM),
m" m) D7 j( K3 _包合性能极限,操作极限,操作程序,起飞和着陆性: a* s, r, M/ A% b, `' ~
等
: i; k' e* @! j" s$ B2 Z9 h机场分析,
' J4 l' m8 K" Y6 u一套针对给定的机场跑道的详细重量限制资料。通常与* M4 |9 ], M) U# P/ z2 w0 ~& e
机场温度、风、和飞机襟
7 s9 ~3 e( }! {英汉对照民用航空词典B OEING
( V! l/ m; Y6 C5 XTECHNICAL DICTIONARY 72 K" X& k1 Z1 z5 d
AIRSPEED BUGS, Adjustable pointers on the airspeed
+ h' o0 }. P0 I; p1 c6 Eindicator.
6 p. L% x5 |: `. p( X3 a/ |0 t9 ]: IALLOY, A mixture of a basic metal and small amounts0 }% r' P6 ~8 |
f other metals to change the properties of the basic
2 ^9 Q5 @- F+ p" l6 Hetal.. a# ]; z* H7 r, s" `
Minimum airplane speed.
. w1 F2 K" }, U0 x3 @ he of
& u! L7 c6 h. T1 D" J# Citting airplane angle relative to
$ b# I8 e5 }+ s& |1 t& ]) i4 tirstream for the stall warning system.. ?: U5 F: a! p) ]
another.
8 s, @$ N' J1 J! O; {LTERNATE , An additional airport selected during
8 R" N5 {+ V0 Q8 @3 Y,
6 }% e9 \5 f% m1 S( g2 C' Q f1 W合金,0 d" i- g0 q4 ~* W' a0 O
在金属中加人少量其他金属,而改变其性质的一种金属
- [! F3 ^4 `: A# ]合物。) u- J! x r# m! R( _
飞机的最小速度。
3 G' I+ g& a; ^8 A速警告系统传输飞机对1 f5 \# N! L' V J
流的相对角度。
: M( n6 r' \. w" K* {% ]/ j1 T3 r, ^# X由一个状况改换到另一个。5 L3 }+ P# z- S' c5 e6 s3 F! s
降场,9 D% I2 h" p+ S* L& N* |
划时,除了目标机场之外,所选的另一个机. @ Q: j7 H- ^- [
o) [/ J+ O( T, Q/ ^! ]1 o
m
; e# C1 q' u" KALPHA SPEED,
" R8 G, |9 c3 D8 [' R& R4 S7 }ALPHA VANE, A small moveable airfoil on the sid
B; d) V6 O/ ^8 u% o& F' Ithe fuselage transm
) O6 ?7 V. g: A da
8 L9 ^" Y$ R3 P7 j6 PALTERNATE, To change from one condition to
8 v. D: Q7 l4 q0 VA
- U8 T7 O9 n& b# Iflight planning, usually near the destination airport, to be( I5 q% k$ ?3 f* I4 I& M
used when it is desirable to divert from the original: W% g+ c1 a3 f( Y! {
destination airport.! k( o; b4 L5 A0 j+ e7 ~5 b& G% }$ K
空速游标
7 e% I. B, b9 }& Y: g' O空速表上的可调指标。
; @; A: R' C; n. u" }2 q混) D U8 S& ^2 `- v+ d
迎角速度,
% f3 M8 c4 @1 q6 `0 t' U7 t迎角叶片,$ f0 X7 a8 ~4 K' o
位于机身侧的可动小翼面。为失% i, ~7 Y2 B3 D' O' B, u
气
; a( Q; t3 Q& d% h1 m8 x2 t交替,
: o2 W$ z8 t! y/ r* v# X备& U7 ^ v& h9 ~* x; V
制订飞行计( [% M1 N! b$ l
场。通常在目标机场附近,以备不去目标机场时,改降之; T9 \! f, W9 A7 P; Q
用。
6 @* ]! w3 Z v- k# O- R; K1 Q英汉对照民用航空词典B OEING3 p2 r: M9 a6 N" b; H" p" f0 m
TECHNICAL DICTIONARY 8
& s# H5 T. c) Z+ B! x( r" GALTERNATE AERODROME, An aerodrome to which! l4 z+ Q$ B& j; |% B3 q
an aircraft may proceed when it becomes either- ?% d% v1 E4 k1 y# s1 G9 G: I* ?
possible or inadvisable to proceed to or land at the
5 ~" ^) {+ z. k5 \- J7 {erodrome of intended landing.! \1 n2 u. ]- U. l# M4 }, q3 a
TER SETTING, The adjustment of the altimeter9 w/ W o* h$ ]
account for local variations in atmospheric pressure., `; D/ Y5 ~0 i5 L6 q! ^& j- P
LTITUDE ACQUIRE, A digital flight control system% Y$ G! x% W3 J7 D/ h) U
ode to transition from climb (or descend) to level flight.
) s' r! }8 Y4 E5 |# `8 C2 _' k! U4 l6 f5 w) PLTITUDE ALERT, A flight deck alert occuring when the
. B7 B; [9 J4 V- `! Eirplane approaches or departs a selected altitude.
5 e1 u8 V! H3 F9 A0 t3 [- f# _2 xLTITUDE CAPABILITY, The maximum altitude at
& j& t+ p' H o4 Qhich the airplane can be flown at for a given thrust,3 i) |# S' K6 s/ N# z
peed and atmosphere condition.$ N# i' Y4 T4 R. |
LTITUDE HOLD (ALT HOLD), A mode of the autopilot+ O' Y) R2 {+ x
r flight director to maintain a selected altitude.4 [5 o) {0 f7 y5 _5 b: j
irplane's altitude during VNAV operation.
# b3 y1 I$ O: m0 z+ q机场着陆时,可作着陆使用的
5 _: D6 r0 f, X8 S5 z1 o1 _场。: x% ]% M1 ^* W5 t$ D# S
,
* ]4 i; D6 n7 y& a" h根据当地大气压力变化而对高度表所做的调整。# `& m& T, y- Y+ F" t$ ^ o
一种数字式飞行操纵系统,从爬升(或下降)改平的模0 a, b& _$ U* v2 k/ M( I1 ]
。
! t9 z' Z" s6 Z: \度警告,+ ~" {( T0 a( L5 y* q& s
当飞机接近或偏离选定高度时,所出现的驾驶舱警告。
( V% W- t$ f6 E" i) y1 J高度能力,
3 t+ {4 _4 v- J; U, V在给定的推力,速度和大气状况下,飞机能飞达的最大
0 T8 Z$ K1 ^3 A' ?+ N. }, [高度。3 A9 j% ?* ~9 s
高度保持(ALT HOLD),( K0 X) t7 m+ N% @ D: w4 i
自动驾驶仪或飞行指引仪保持在选定高度的一种方式。
' f, e2 ]2 z8 W/ S,
- h4 b) }0 [% U. |* P" H6 \2 O# p员对飞行高度的控制。8 ?6 [8 J: @9 |+ |
im
9 s3 X- d. `! }9 {# @a
4 X4 G- r9 f& {$ UALTIME1 d8 ?2 Y, ~6 s- o7 x* [
to! N, k& y6 E, ?- P( O
A
0 t+ }5 e7 w# o! |% S4 B w8 l$ }1 sm
) p# C, N7 D$ y' I/ Z! tA
( ]3 S) f7 _, ?) T/ za
+ o5 \0 }0 U4 S3 n* u- TA
8 U& p$ A7 v" D9 o- U- Vw
0 i& v4 b |4 ]4 os/ c5 X, w5 g9 F2 n7 h
A1 L( I+ k; O0 i) Z) \7 t7 B$ y
o1 `# O1 Q. r. d, o0 @1 t1 u
ALTITUDE INTERVENTION, Pilot control of the
! V2 H5 {# n+ ^% A& w# Qa- s4 H8 q; F |0 [& O. X0 Z( ?
AMBIENT, The surrounding atmosphere./ M/ W3 `2 _# f7 U5 w
备用机场,
i& ~( e+ [/ r$ A4 G8 @7 j; e当不可能或不适宜在预选
- _7 t3 z3 j; {: t7 e机5 E; _) l: r+ ~# w; E0 E
高度表设定$ {; J; a2 t6 z( v) Q3 M5 P
高度截获,
, J3 e) u! T, Y {& [6 m式' ?/ a5 v" e. }* _% }( h! E
高0 b9 i5 i% c4 H0 D& ?& L
高度干预
9 i" T7 Y6 ?. X( M在垂直导航工作过程中,飞行
) X9 j' M0 P0 P F; Q5 B周围环境(地面气层),
# g5 w1 l; q& {, ^' g& H1 r% x物体周围的环境(特别指大气)。/ P# o* m1 | s3 Z' }9 k4 [8 P8 N
英汉对照民用航空词典B OEING
6 g7 }& d4 k) o T# n( [: `% UTECHNICAL DICTIONARY 99 P4 `/ T1 {) O$ Z
AMBIENT PRESSURE, Pressure of air surrounding an f' n& ?$ B9 ^3 f! m+ }3 I, B
object, measured in pounds per square inch (psi) .
5 e* N2 ~" h: y! _. N2 r2 qMBIENT TEMPERATURE, Temperature of air
9 L& ]2 l) x; _2 H! Rmpere.
! H, _! `8 K; K1 C" }2 T/ f- N, lurrent waveform.1 c. \& p* I. G! p
g an
) ~, B5 _0 b# L- @nalog signal to a digital signal.+ J/ M# Q& d2 W; M4 M
ore inputs+ y2 f: C& W% J6 s# C% z& X
f binary digital information and one output. The output. J4 f6 W+ r8 T7 M
1 only when all of the inputs are 1. The output is 0' L3 d: }- q. d& i) M
hen any one or more inputs are 0.4 w* Y& J1 b1 v2 t/ E' \
面气压),
! x( ]$ |7 J% J N境温度,
! C- A, y; x! }/ c3 @气温度,用摄氏度(°C)或华氏(°F)来
( B0 L* x, e- J' q+ u$ g/ `。3 {+ L- U8 x- J2 Z! `7 g
电压或电流波形的幅度。- I1 c! v; y* F8 }0 ~# [& T( R1 ?& A
性变化的信号来工作,或产生连续性变化的信号6 ]$ F( S. i% m$ ]9 E# s
统。$ `( T+ x5 F: D1 e: k9 @
将模拟式信号,转换成数值式。* ]' R6 f$ P/ q6 v
一种有两个或两个以上的二进位数字信息输人,一个输
# a8 y& E' h8 q( d, h( N的装置或电路。当所有输人为1,输出为1。当任何一个( r+ `8 E6 u; k( x& a& W
一个以上的输人为0时,输出为0。
% ~9 `- N3 g1 m+ i4 g* AA7 w7 [$ B& \1 }% ^* ?
surrounding an object, measured in degrees Celsius R# e% ^" ~* T6 [5 x5 ^5 c) s
(°C)or degrees Fahrenheit (°F).0 f/ k3 c- Q0 c9 w$ @! W
AMPERE, A unit of electrical current. One volt across
$ }' A; v/ T6 hone ohm of resistance causes current flow of one' ]5 R; W1 E& P& M% @% P0 T8 {
a
) C& `9 J% Y' nAMPLITUDE, The size or magnitude of a voltage or
, a( k0 Y5 q1 u0 Yc+ n' J! ?2 ]2 U. ~8 [0 n
ANALOG, Quantities or representations that are
. k1 Z' ~" W# f- f7 [variable over a continuous range.
/ ?) k# D5 P2 W8 { bANALOG-TO-DIGITAL, The process of convertin
+ e1 ~' h8 E% X/ ca P4 R' \3 d# b3 ]- x; d) u9 K
AND GATE, A device or circuit with two or m1 G! |# F, i# Z |0 Z
o) x1 ^: R* {& D) h: o3 a3 x+ ~( L
is: r: N1 y; W$ H1 o+ k, W0 R
w
) ^# a' g! r; N- H: Q" G% u/ c环境压力(地
0 ?, ^$ M! g/ A5 f& w+ o物体周围的空气压力,用每平方英寸多少磅(psi)来& h! F0 I! l" P4 f; S8 B
度量。7 u# z3 K. O4 m4 K$ l8 D+ K9 l
环
# `- V- D4 ~5 ^物体周围的空/ x- T g* C* Q# M% i7 V( \
度量。
- F6 |9 [/ x5 W0 [0 x) {安培,
8 q6 u+ _' n4 A% o: q电流的单位。- J4 v1 f: N8 b" r; L
1伏电压在1欧姆的电阻上所产生的电流为, \ b; m x/ Y, X
1安培
! Q+ s5 S" H! d) H振幅,
U+ d( q: V" P1 _% z模拟式,
+ ?4 g% Y% h/ K8 ~# m5 }用连续
5 @- c6 V, C7 V系0 E$ f4 l/ H6 |$ a4 ]
从模拟式到数字式,
. P5 O4 J1 e; `: f# Z& K与门,
1 N8 M3 f+ p! i; j; n出
/ r4 j$ Q- J- e6 T% @3 ]/ l, k% W或' T8 q+ W9 ^( T) r1 y0 \8 P" ^( I
英汉对照民用航空词典B OEING- j7 y& H3 N( _% p: J3 m h
TECHNICAL DICTIONARY 105 d7 \2 A- g. N9 ? f* ?! q1 v* I/ n
ANEROID, A sealed flexible device containing air at low% G& S8 X( q7 a8 e
pressure, which expands or contracts during change of3 C O/ p2 X" o& ^0 U) G, p8 R; s# s V
ressure outside the device.6 s8 I* m; [+ L3 m6 F
ically
3 C# K) V3 \# R5 t% z- E3 mr changing the direction
0 ~0 D% v/ p7 W! E+ z0 \5 \f drive.
, h! H5 f2 L8 p+ }9 aof the wing chord in! X2 D7 b. U$ D2 `- i
lation to the free stream airflow as it moves forward
+ g! } m! i4 t. C3 D4 T2 lrough the air.4 b' t& G, o- G$ M3 O
al axis of the5 ^- y7 U; X j3 ?: }; w* j! }
aircraft.
2 g& {( l9 ]2 o5 C/ c) f胀或收缩。
9 F* Q( |: u0 j# p3 ^5 a5 T7 A6 i- D箱。是改变驱动方向的机械装置。
% o# I Q. j8 C* p4 t& W% K机翼翼弦在空气中向前运动时与自由气流之间的夹角。
! u. s1 e& ~4 G9 B, J8 O。% {, {+ B$ r! g# c
p
; }( n" n+ f3 j# p0 J BANGLE GEARBOX, A part of an engine, mechan y [$ Z6 h& G D
driven by the compressor, which drives the accessory: y" B0 }- D) w
gearbox. A mechanical device fo) B# {0 @3 x9 T" r; C' Y
o9 J$ y& x0 @- t: X* _' c4 k6 Y8 l, |8 c( D
ANGLE OF ATTACK, The angle
2 C6 k! m% I" [( @, y3 cre8 s. }& H3 G2 i y! b
th* e4 G6 i1 a# ~7 t! \" A
ANGLE OF INCIDENCE, The acute angle which the
0 J0 X0 V# S+ L7 rwing chord makes with the longitudin
" u& d) _9 |+ J8 {膜盒," M# n' [$ H( r! H) I+ v
内含低压空气的密封弹性装置。当它周围的压力变化+ _9 |) g( @7 ~3 u+ { x
时,会膨# Y1 i1 H: `+ @' ~# W
伞齿轮箱,
* P) o. L5 c& k- Y+ H发动机的一部分。被压气机以机械方式驱动,然后驱动2 u' A* Q& T& `0 }6 |
附件齿轮6 S" [9 G6 p1 A/ ^6 w+ H
迎角,
. j% E; a' l3 A/ ^8 n5 m ~安装角,
' d+ l! `- P8 s* N: l飞机的纵轴与机翼弦线所形成的锐角
; W& d! t' L, S- p' \/ D英汉对照民用航空词典B OEING) ^5 ~, H! \5 h
TECHNICAL DICTIONARY 11! Y! N: d3 S" s; Q- e% j# L
ANNUNCIATIONS, Audio or visual indications used to U7 L8 }. C9 G0 z2 k" w9 X! b
call attention to an event that has taken place.
9 S2 j; Y/ e( _6 HANNUNCIATOR, A visual device consisting of a number5 F5 f# f! o P
ly.
- c% N+ z- g! X7 Z2 vANODE, The element toward which the principal stream
# D. C, w8 X @5 P0 ?& T6 c; zof electrons flows.1 T3 c/ @9 Q1 a
ANOMALY, Not normal.2 Z! N1 S3 C. X- e
ANTENNA, A device which, used in conjunction with a
" f# m$ t R5 B( T% d9 ltransmitter or receiver, is used for radiating or receiving* ~6 C2 m7 `# y4 z, k1 ~
radio waves.
1 [/ N+ t7 t1 x8 g* ^NTI-ICING, A method of preventing ice formation on
2 \# H- L) _% ]$ ]e wing leading edges and engine nacelles.
. C( b d. p+ V' U, B4 kNTI-SKID, A system for providing maximum braking
% V( P( c' Y+ o; F4 [' Lithout skidding for any runway condition. Anti-skid
" L) N' Z$ p. M/ S0 U! A* B, `omponents are part of the brake system.
% y* `3 N4 ~/ } b告,$ b# G3 c2 k# n+ S6 s- N7 W5 i; _2 O- l
当发生事件时,以声音或目视指示形成的提示信号。
3 z- h r4 ~9 k {" Q0 O与之有关的电路的现有情况或已存在的
0 } p" Q( E2 B- e e1 b* B况4 S; a2 T6 ?$ I
正极,
' _: I* R( v* n, v4 s! d% P$ N主电子流向的极位。
6 Z! i; {0 [& c$ V9 A1 ]异常,3 M# z$ y3 f8 |! I, r, d* G: k
不正常。
/ C. f- U' `# Q9 Z% J' H天线,
. Q+ a8 x& \5 D1 K) W一种与发射机或接收机共同工作来发射或接收无线电5 }5 b" o! Y# I/ ~9 ]% w
波的装置。& S8 U6 F, v9 F( p$ ~. X
冰,: V0 ]2 \/ H. B- u# I% D, J% g
防滑系统,
; G' Y3 u* I: A; E. a一种在任何跑道状况下,都能提供最大的刹车能力而不
$ r( |3 Z. s' g9 z' @1 ?6 n* k! B+ l使轮胎打滑的系统。防滑部件是刹车系统的一部分。
7 W7 C; Y4 C: ]+ Nof lights. Each light indicates the condition which exists( L/ ^ o1 T* ~ J
or has existed in an associated circuit and is labeled+ N5 @' E) P( A: f( M, Y. \
according
C/ M+ b* s$ PA; }) A5 U) ^3 v! t9 D g
th: j, C8 `! C$ a6 g E
A
, {# X# R, v; N- |9 H) Cw
( j: Y( |& l+ ]0 L) o- L5 {c
7 b4 p2 A8 y8 {9 T' z: n+ `: u通
1 F4 _* @- \) Q' k+ W9 W信号牌,! r1 h" f5 \# l; G8 X$ R& w
由一系列指示灯组成的目视装置。每个指示灯都有相应) ^* i @4 Y' q' K {
的标记,用来显示
* p8 ^/ h3 G: n! G情
) q6 V2 q+ n ~4 k防6 A+ Q& x4 s$ a* g$ n2 A D$ a
防止机翼前沿和发动机短舱结冰的一种方法。
1 [# v, w3 \, Z英汉对照民用航空词典B OEING
) c, n- L9 z( m0 ~1 B+ i0 |TECHNICAL DICTIONARY 12
2 ]* O5 u/ b: FAPPENDIX, A supplement to the Airplane Flight Manual
* `1 C" R3 |$ x# t3 v( ktained in the basic manual. A
. W. p4 J8 f9 R: I3 c* C/ \ollection of supplementary material at the end of a
! L2 v- ^+ e j9 z: n9 P/ ]ook.
* H+ b; P0 n0 k. }, \, [" J/ hof the
j \( u! N( m7 v5 k9 Rrsion link on the landing gear.
# _6 T" }* j$ Q: Z0 @: YAPPROACH MODE, An autopilot/flight director mode3 d% K8 ]" n4 D. N& e
which is a combination of localizer for roll control and
0 g, C* a, h0 O Cglide slope for pitch control. This mode is used when full" }* S( j2 F! [! b
instrument landing system is available.( }% p4 k; _" A% n
APU, SEE - AUXILIARY POWER UNIT/ c9 n6 j) _! z
ARINC, SEE - AERONAUTICAL RADIO
9 i" w8 V3 X' u' ?* bINCORPORATED
0 V8 C% N( U8 I8 ~% n' ~ARM, To make ready for operation.
# L. V7 J5 \7 X' k8 ?( F3 |附录,& Q u$ A3 I; y; \: m7 u- k
飞机飞行手册的附件,包含基本手册中未提到的飞机形7 }5 z# k0 Z; V! }) e! u. |
态的其他性能。是附在手册末的补充材料。
0 U4 ?1 g) ^) q3 X! ]; q顶销,8 P# z( i) `5 L
用于连接起落架扭力臂两部份的销子。
! o: w! t/ @; y6 a" Y3 Z进近方式,) u' f' y4 y0 N8 _
一种综合了控制横侧的航道信号和控制俯仰下滑信号
y3 i, c- Z# t, l" @5 {& s' F6 g的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系 Z+ B" w# q9 h1 B+ g% K5 e
统正常时才使用。 c; H& o5 i! s/ W! }, ?( u& u
辅助动力装置,
! t& S! E2 Y& }) o8 E: r见Auxiliary Power Unit
& a F C4 e7 a8 u- Z" v2 acontaining additional performance for aircraft
. F; F' o4 c$ E pconfigurations not con
) `+ V# w* |+ D# f" E( ~c+ R& Y4 _ ?% G) Y' \
b# o: N* e3 w- E* P4 y4 `, ^
APEX PIN, A pin for joining the two sections- k0 O% p. {5 e. \4 V( ]( [' H
to( v( |; y5 U2 J. d+ w+ U
.1 C+ ?0 }- z6 ]1 @- ]
航空无线电公司,7 x# c$ U* y% {" m* P
见Aeronautical Radio Incorporated.
2 ~8 e; e1 l6 @6 f- e预位,- A( L0 p" R; [5 }
部件可以开始工作的状态。3 G% R' U3 L4 X4 M" k8 d. x
英汉对照民用航空词典B OEING
3 W+ b/ _; |7 \' fTECHNICAL DICTIONARY 13
: p$ o. T o8 tARC, The curved track over the ground of an aircraft
: [9 M' H. M2 p5 q) Tflying at a constant distance from a measuring
- u( ?0 Z' {$ r* L. \% J0 Qequipment (DME).5 T, g. ^* }0 T- p; x
in the limits of self-contained system
# l) d( F" z6 z& C& Fapability.) F* f) |, I8 I6 J/ S& D8 I, Y
tem for opposing or restricting8 d- ]: m" V8 e5 S& J8 w
ovement.& }: @& ~; J- m4 L( H/ X
SPIRATED TAT PROBE, A sensor that measures total
/ h. ?/ Z/ I+ a3 M9 ]0 ?8 }$ xir temperature when the airplane is in the air and that
' W4 u) J1 E) {, E/ R3 f8 Aeasures outside air temperature when the airplane is
( M" J( D& ^& K4 yn the ground. The outside air temperature is measured7 p m' J* C0 H; I8 n A
SSEMBLY, The fitting together of a complete structure
; J9 K/ o' y. Q d3 W) F( _SSUMED TEMPERATURE REDUCED THRUST, The
2 M# d: d# `1 {, `4 ~0 pATC, SEE - AIR TRAFFIC CONTROL) T7 V5 z2 W4 x7 x) k
,0 `! g7 }0 T; s# f- I
系统中所产生的一种用以抗拒
/ ^! O. z* i x6 C8 G! E- c; q作或限制动作的力。/ M2 @* p+ \; \1 Q
头,
' b7 f' R, B& z% I7 l3 c; K- ?用来测量飞机在空中时的总大气温度和在地面时的外6 d% F9 m2 [# ^ X3 Z$ M E& _' d
温度。地面外界温度的测量是利用引气将外界空气吸入2 F0 Q d+ {! D! u' @) B; r o& g1 W
头,以达到测量的目的。
8 m5 \, t+ E' ~1 B配,, @2 B0 m7 q# B1 f5 W3 z3 s4 ~+ s
一个完整的结构或组件的过程。1 C. S; c$ D4 Z3 f) x8 Z
假设温度而得的减推力,
' m) I) E, ]% s7 K* q推力设定值时,假定一个比实际外界空气温8 }2 [( C7 V3 I; k# R- j
空中交通管制,
5 ~9 }9 Y( P H$ R5 y9 ]4 b/ l0 P见Air Traffic Control
) d+ O; A* L" w9 ^3 _6 a& GAREA NAVIGATION/RNAV, A method of navigation
6 L7 {! Q& L2 a' m0 v8 I+ S/ Ithat permits aircraft operations on any desired course
3 W- [. I A- P% h: j$ s; c! V" ewithin the coverage of station-referenced navigation
8 n0 A# J2 u; k. j; w+ }* F# |( Vsignals or with i `0 W# c, r: t5 P* y
c+ T' J) q% w6 R- B( T* O% u
ARTIFICIAL FEEL, A force developed in the flight- W( ?4 E' v7 b) |/ @
control or brake sys+ a5 P' S9 s) @
m! w+ V2 W/ X8 V1 v
A3 l0 t* w* K1 @* j ~! R0 i
a
# f" O$ \% {+ J% r5 ?3 V7 ]m" x4 V6 O+ `3 Y% B% z' N6 F6 f& h* N
o
/ O1 _2 z8 W7 Fby using bleed air to draw ambient air through the
. c/ x- a, Y- i+ ~4 F$ z' ~8 Usensor when the airplane is not moving.& X; I1 S4 g& d0 m6 q0 _0 \
A) N4 F0 y) ^; U3 I
or unit.
. A9 ^" Y! }7 V* h8 x: ^A
. @% j$ _9 W# K9 Blower thrust obtained by setting a higher than actual. t; V: N8 G5 D# b2 N# u
Outside Air Temperature (OAT). H- f {. O5 X, Y7 }$ B
弧线,$ ?8 ?, Z5 h7 M1 k6 \. r) m5 Z
飞机在围绕DME台等距飞行时的弧形航迹。
; S% J- f; ~+ F: g& {2 p# ]区域导航,
! A* Y) B4 l1 @2 T容许飞机飞行在有电台参考的导航信号或自备系统能
/ Y* S& i5 \ o. `6 J力极限范围内,飞行任何预定航线的一种导航方法。
1 |) |) e, C; }+ K模拟感觉
* i/ r% x# u. n: e$ a5 {6 [, Q在飞行操纵系统或刹车
- ~# V2 x/ p6 Y6 t: {: q5 B" A动
/ Y, l, \7 u$ a# x% p3 P吸气式总温探. Z( R$ ?; ~+ K( Y( Y
界! |* n/ h: ^9 M/ a) {+ B
探
2 Q# e- a s# C" W8 B7 l装
1 y( r8 Y2 F; N$ c组合成
' Q% J; c l% n3 p- n$ l; a8 c由
/ a! n/ }/ Y- ]4 D! u在选择起飞
3 B/ s4 n, O! a. t" Y度高的温度而得到的推力。用这种方法可以减少发动机的* d, o( Z/ P1 K4 I
磨损和维护费用。
- }' P$ p; h+ w+ ^- `; b.
" c. F# O6 j& }3 x: N英汉对照民用航空词典B OEING; T6 @/ p! D% u6 E" P
TECHNICAL DICTIONARY 14/ I% P- P6 o- O: P, a- I- ~. k
ATE, SEE - AUTOMATIC TEST EQUIPMENT/ p# c" J/ \3 t- f1 K
ATMOSPHERIC PRESSURE, Pressure of air due to the0 w& } e" @$ C2 X3 F
arth's atmosphere, expressed in pounds per square
( c3 s/ G. l+ J1 P) sch (psi) or inches of mercury (in Hg) or millibars (mB).$ |( o+ q4 n/ D j* L6 ^9 r" N
TTITUDE, The relative orientation of the airplane with" z8 J8 E/ @2 X" V- A
spect to pitch, roll, and yaw.
& s# I F! j) b! q: NUDIO CONTROUSELECTOR PANEL, The panel in* G- ]0 g! u5 d4 t8 s5 A. m
e airplane which controls and selects the routing of
" v2 w6 G' g! N! ^8 o e+ V0 Gudio.) g) a+ J2 V# }7 W- G! D, _
UTOLAND, Automatic landing using the Digital Flight
: @' [; E6 d. V* ~4 _; control System.$ G/ D0 K9 q& A3 _, i
n.
8 F% X- k% a4 {# _$ |M, A system+ Q" _1 O# }6 n$ V# c, F
omposed of all necessary subsystems needed to guide7 c( Y4 @; x6 B6 B7 f. \6 e3 J
e flight of an airplane.+ Z0 [5 Y8 `- F+ }$ t
EQUIPMENT, System test
7 |% {$ Z- o: {) k, o' J# @- @3 Uquipment that operates under computer control.) Q* h, m6 ]* m* J! D$ ^
装置, |
|