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AIR DATA COMPUTER, A computer which produc: O; ?$ T# } p0 K2 V
data information, such as altitude and airspeed, based' J* J1 N7 y+ j9 K2 ^* Z
on pressure and temperature measurements.
6 j( O5 ]+ B8 I" ?' g6 {es air
" M0 [. Z* ]- C+ [. E& j( S/ J) ^IR TRAFFIC CONTROL, A system comprised of
+ v' u: Y. B0 rround and airborne components used to identify, track
7 ?3 I/ r9 h: Q: ^, E6 cOUND SENSOR, An electrical device operated7 }4 n& w7 \" U: \% F* k
y the landing gear, which transmits on ground/in air! b) i# \1 c- y6 _+ H
formation for system operation in flight or on the. p: o+ i7 ^( i, |4 s8 Q& }
round.# Z, o) g$ ~# d' [0 ?/ h4 W
IRBORNE VIBRATION MONITOR, The AVM takes
4 n# f. G3 o! f, v7 ^" P, n: Ce signal from the engine mounted accelerometer and
! y( k% f; u& f6 B6 H6 v) k( `alculates the vibration on that engine.4 _9 u. m7 S7 _1 W5 K8 L7 |
corridor equipped with radio navigation; o6 G& a v: p% @: A
aids.
. q C) ?# h, xAIRCRAFT (or ARINC) COMMUNICATIONS$ \1 I( p0 J' Z1 [2 C/ A3 E
ADDRESSING AND REPORTING SYSTEM, An
; k5 s9 H3 G1 X# Q1 A N; Paddressable digital data link system which permits the( f. l8 l4 j& E2 j- l
exchange of data and messages between an aircraft
2 _* c2 E$ z! m$ o& [5 q0 wand a ground-based operations center over a radio' V) y$ y3 ~/ {' s3 U
network.* ]: B6 n: |3 v
AIRCRAFT CONDITION MONITORING SYSTEM, A% H l$ h& w6 ?" [
system of sensors and recorders to monitor various( O2 e. T% {1 u- s$ _, f
airplane systems' performance and status.: u4 e2 X# i) a" h# U9 r) }7 Z
机, r% _4 U8 p0 k
中交通管制,
" _9 ^( r J/ y. ]3 n1 |" r2 n一个由地面设备和机载设备组成的系统。用来对飞机进
) H) ]0 d( L- t4 `地传感器,6 l6 b; f+ k8 A" f, ]: ^5 E- _, K
一个由起落架操作的电气装置。用于给空中或地面的飞( a. l- `9 t5 B7 ~/ v) ~" |7 h: U1 O9 y% g
系统运作传输地面/空中信息。(有些系统只能在地面
k q5 K# R8 s# j7 l; a7 l O用)+ s, S/ A, U0 s8 h' J1 s
载振动监测器(AVM),
" m$ E. u8 r$ ~AVM从装在发动机上的加速器取得信号后计算出该发# O6 p% v1 ]% {# o
机上的振动。) K8 H9 f! \/ A
式建立的控制区域,内有无线电导航设备。/ A( S2 }1 y/ o7 c9 r: l4 X
飞机通讯寻址和报告系统,, _3 b9 U' v7 u V6 y
有种可寻址的数据通讯系统。利用该系统可使飞机与地
( S2 F9 l: U, i. B2 L面操作中心通过无线电网络进行数据和信息的交换。! I8 ]8 l. Q0 L0 F0 I2 k
飞机状态监控系统,0 K2 q/ b( Q! ]- k
一个利用传感器和记录仪对各种飞机系统的性能以及! f2 [" }9 O/ B# y
状态进行监控的系统。' E, _! l' _5 i& E' {5 n( T! o! h/ E& ~
A# c9 @9 ?) E8 Y6 x
g
% X( Y) A0 J, n, r, m- K0 oand locate aircraft.6 o& p: S8 P% f, b( h' }, J
AIR/GR4 R3 g+ v1 J* e# F6 t; H
b' k1 M& i# ^% E! `) L; p
in9 P& i' _! r( w
g
# y0 j0 n" A t* B# C: ?+ S5 PA
2 U$ }0 o% h T0 J: `" pth
7 `$ M( c: ] P* ~/ b- T+ Hc& m' T, L6 q* ]7 A1 Q4 C8 p
AIR WAY, A control area or portion thereof established
/ x1 ~0 x4 W# h T, ^) \9 Rin the form of a1 F+ k) ` A4 @$ a3 ?* ~# p
大气数据计算
; ~; x0 Z; P( m1 n8 F根据量取压力和温度而产生大气数据资料(高度、空速" \; r: T7 l6 D2 W
等)的计算机。
9 e# J3 K8 T: }空
6 m# f" a5 d5 q+ K G j行识别,跟踪和定位。
/ l( L+ C8 i; I! D空
2 D5 @* n/ X, v$ d5 Y机
7 ?; w" t" x( h* X& @3 n+ o' Z使& S, X' D6 W1 i; ]/ T6 @
机/ I6 M) Z( z0 L& m; e! K: L
动3 m% O8 i; S e: }' `+ m
航线,0 v8 O2 c- m* U% H8 r. ?
以走廊形
6 [1 q H5 a) i英汉对照民用航空词典B OEING" n% ~9 H9 j* L2 a* ^+ O. Z
TECHNICAL DICTIONARY 6
5 E- q! c3 e9 r2 x9 z/ x& aAIRFOIL, A surface designed to obtain a useful reaction," |! F+ }5 d% d6 A' Z
such as lift, from the air through which it moves. Wings,( m+ [# y3 I: m0 e& g) ?
stabilizers and control surfaces are airfoils.
1 d* f0 ~$ T8 |AIRSPEED (IDS, TDS), The speed of the airplane: r) o4 Z( j2 i [- p" P$ N. K
rough the air.9 X1 V6 q9 | q. O' A$ O; ?
D INDEX, An adjustable pointer on the
: E, U+ B8 b( `& @& uirspeed indicator.
7 S3 I& z2 ~& x: k1 vand legal ability2 [% s4 S" j H. \% x3 t% ?" P
fly.1 [* }% _" u! N; i
m, for example, the procedure for finding the
# q& J& q7 k6 W1 p& fquare root of a number.; e, N# X# M( Y4 s: u) _6 A
y
- S; `! w/ p# \4 y! ]0 Hre, wind,
3 v6 n" T( A- [9 ^+ @8 J& a+ dand aircraft flap setting.
8 a% R# S$ o7 v; a& k7 h9 |是翼面。+ e! i3 f7 ?! d) v+ r0 }' L
速,3 W! m h8 g7 g& `
飞机在空气中运动的速度。
. U. N4 T& h2 R( v, `/ f,3 c2 Y+ z/ C' F k- t$ B4 t
在空速表上可以调整的指针。1 M$ M% m4 @ e B) m1 Y4 G4 N; y! W
机械飞行能力、和合法性的飞机状态。' a" y7 x u8 D
一步一步的解题方法。例如,计算一个数的平方根的步
' r+ K2 f8 M, ?。& u0 X1 i# O+ H- G& r; Q
能
8 I) U7 Z! k& q9 v资料的法定文件。$ g+ w8 c0 z2 {3 } U% s. M! |
翼位置成函数关系。
+ y3 k/ Z1 p( `# Vth
5 T4 L3 Y \3 _0 QAIRSPEE4 F: {' i( v6 S. w: ~! e* X2 U
a
3 ?5 ?. E2 m% ?5 N) t# g8 I' tAIRWORTHINESS, The condition of the aircraft with# t: o/ Z& R& S( N! z' X
respect to its aerodynamic, mechanical,
& k% R3 V& H# K/ vto8 k$ [# @, t0 b; ^6 y
ALGORITHM, A step-by-step procedure for solving a
, h' s8 d8 \3 jproble
* D) A, Q+ A: i% d3 y) I1 ms \3 C" L8 q# j8 o2 _
AIRPLANE FLIGHT MANUAL (AFM), The legal
7 c# M7 k; G. fdocument containing performance and operating limits,( U# \" b% |( x" Z2 s( b" ]
operating procedures, and takeoff and landing3 z+ X4 d# F1 j4 C
performance.+ G. L! x0 v( S
AIRPORT ANALYSIS, A comprehensive set of takeoff
2 [$ |5 z; r' F8 _: M0 u; S1 f, `% eweight limitations for a given airport runway, generall
0 T, \: Z) L: G$ M! a/ R; P: Ipresented as a function of airport temperatu
( \' F$ t3 @! ]% l0 t翼面,; J3 K+ D. Y( N; T$ r" j
用以从气流中获得反作用力(如升力)的表面。机翼,
% J4 K2 H8 a; |8 L1 ^# B+ }# ?$ M安定面和操纵面都) S$ o5 z& p6 h
空# p3 ~/ V2 w: E% M+ s( ?6 o& H
空速指标5 J- K8 w6 R: v; A& } l
适航性,
9 W; l3 q/ G; c& u: P: ^5 }, J" C有关气动能力、0 T+ I5 ^2 c( v; T* v
演算法,, i) @6 Y6 ~( E+ a" \( I
骤, M' `$ O" `, B& B& t
飞机飞行手册(AFM),: k+ C; W8 l/ A$ O, s2 @$ H
包合性能极限,操作极限,操作程序,起飞和着陆性
: s) W8 e, W9 Z) s$ t等- @: y- k/ | p' w! N
机场分析," P1 T7 p, x; @3 [; M& r
一套针对给定的机场跑道的详细重量限制资料。通常与
; |. L# v! E* C# K' ^( Y, ~& {4 Z机场温度、风、和飞机襟
; {9 R" a- H6 w! x8 A4 D# y5 Y英汉对照民用航空词典B OEING/ a$ K |/ _" Y+ h* O
TECHNICAL DICTIONARY 7
6 W. ^7 i9 V7 \$ ~% g6 `+ ?AIRSPEED BUGS, Adjustable pointers on the airspeed9 I; |! N' x/ S9 l
indicator.$ N4 Z0 e3 d" |2 [
ALLOY, A mixture of a basic metal and small amounts: w7 V. M4 ?- k
f other metals to change the properties of the basic9 R* j2 Z; ~) c
etal. A2 M8 a3 D1 H3 s, h' g1 m
Minimum airplane speed.
9 `; m: r3 C! r0 H: {e of
5 T& }# }' R! ^8 b& r) witting airplane angle relative to
' a+ u4 I! {. U# Z: Iirstream for the stall warning system.! Z4 t, d2 `) {
another.
# c& T! x W) ]4 R' _, B) uLTERNATE , An additional airport selected during
5 \8 G# {" F9 | i9 [$ S0 N8 g,9 f F( x. L. a! Q6 P
合金,% x* h8 F" X/ p. ^3 C
在金属中加人少量其他金属,而改变其性质的一种金属
' n/ i: u+ b' g合物。
5 E) i% K- E0 ^) g飞机的最小速度。) w9 s [ \: s% G5 @
速警告系统传输飞机对
( b. |0 d( P' ?7 f; v# B! {1 r流的相对角度。
0 a" ?. e# s. Q8 |$ c6 z由一个状况改换到另一个。
# M3 f* G" u) \( r降场,
7 f. N& I9 K3 N" G$ E+ |划时,除了目标机场之外,所选的另一个机; z4 K8 Z z' [7 p& h8 R4 S: q
o
) ^8 ]) _4 \! g, F* }# R& O3 Jm: l" n& d( x5 n
ALPHA SPEED,) N: E3 n8 Y1 ^4 J- u
ALPHA VANE, A small moveable airfoil on the sid
6 Z) V3 N2 b( v1 b: g) @0 Cthe fuselage transm
' b$ J4 H" r/ i; u" xa- @' i' i' G1 d& G
ALTERNATE, To change from one condition to
4 _( L( {% w) }/ @. s Q% OA
' T. D7 H1 Q; {+ T/ bflight planning, usually near the destination airport, to be0 p, O" w6 \9 l
used when it is desirable to divert from the original
7 V9 u9 H! _8 V. \9 |destination airport.
+ K( i- [- _, @; ?空速游标2 ~+ u' R$ s* ~* g4 ^ [3 e! M1 `
空速表上的可调指标。) l) o+ c6 B6 l# }
混
; U! D" F8 \/ x' A: u迎角速度,. F$ a3 W1 {% n- X: `! Q/ P
迎角叶片,
/ j$ E. P& z" q1 m9 ^3 j6 d! M位于机身侧的可动小翼面。为失! _* G. [2 s% @8 ?& m ^
气
) g/ `6 b. [( z3 Q$ q' U7 k交替,9 g' e; B$ A* y7 Y. H9 G' n
备7 V- \4 \/ L, j
制订飞行计
) B5 z( a9 ]5 e' S, j$ x. P场。通常在目标机场附近,以备不去目标机场时,改降之, G3 O5 @2 c/ ~4 y+ F) ]# z( e
用。
* U6 J9 c7 x! w3 I! w6 E英汉对照民用航空词典B OEING- S1 d; C4 ~! K% r. O, W
TECHNICAL DICTIONARY 81 p O: C# m$ f2 R, L
ALTERNATE AERODROME, An aerodrome to which5 m* J/ I ^0 {+ U
an aircraft may proceed when it becomes either
' C3 s) g! A( N5 ^possible or inadvisable to proceed to or land at the/ c0 |; ?5 y* M n% [
erodrome of intended landing.
! x) o8 W _: T! \TER SETTING, The adjustment of the altimeter
1 X) Z4 Q; B9 V) Q& U' @5 A6 Caccount for local variations in atmospheric pressure.
7 G6 n. [5 `3 k" j' X" ^* }3 hLTITUDE ACQUIRE, A digital flight control system
" x8 e- I6 m2 ]" xode to transition from climb (or descend) to level flight.9 Q3 u2 o' `- g2 W, c% r
LTITUDE ALERT, A flight deck alert occuring when the, v* O+ O! H9 \. j+ A
irplane approaches or departs a selected altitude.
) ~" ~3 Z# e* X. j8 Z1 RLTITUDE CAPABILITY, The maximum altitude at d# j8 C: |$ n$ q$ r8 i
hich the airplane can be flown at for a given thrust,# C! A3 a7 s7 b
peed and atmosphere condition.+ ^* h9 k F+ _) x7 l
LTITUDE HOLD (ALT HOLD), A mode of the autopilot- |- i% T9 u0 h, T% ~
r flight director to maintain a selected altitude.
7 B) i* Z1 Y" eirplane's altitude during VNAV operation.) r4 T- w) o; V' u8 P5 g
机场着陆时,可作着陆使用的
% @& u a) w g! o, j场。8 o0 F+ a9 w- X( L; b ]
,
) E2 n1 x& s0 `& d7 W$ X根据当地大气压力变化而对高度表所做的调整。
0 l0 L4 F8 R0 N1 K D5 L一种数字式飞行操纵系统,从爬升(或下降)改平的模3 |7 E& \6 P3 J7 @( ?
。9 H" b: A) ^$ g! U& P4 V' E
度警告,6 A g0 p, A: i! ~* N) h k
当飞机接近或偏离选定高度时,所出现的驾驶舱警告。
' d. D+ h0 {0 U' C高度能力,1 o( D- x0 m1 T8 i; }0 E8 {
在给定的推力,速度和大气状况下,飞机能飞达的最大
( {& p+ A* G: i% a高度。
5 M6 Y0 R1 J. C: H( Y& y! H9 s) |高度保持(ALT HOLD),) Y; S# q. z; y% J# e- V) z
自动驾驶仪或飞行指引仪保持在选定高度的一种方式。& e1 _7 `# w$ j% \8 d+ z6 e A$ ^
,$ ?7 O! H+ T8 D0 m/ X+ h4 ?
员对飞行高度的控制。
7 s( H& S! @/ c- n5 h, i/ ~. _( kim0 f1 ~$ j8 C/ V( O) w* j! v
a2 c. g0 ^1 Z9 p6 o
ALTIME
& d" Z, T5 d5 v! u4 Gto! L5 v- P- [# P* c b6 _
A; M! N2 X7 g0 O; d" q
m& j, I3 U6 K" F6 g% m, a
A9 K9 ?) ^% Q9 O2 J
a6 h! n& V' E# Q2 k" g6 g5 q
A% m- q+ O2 c8 i7 W, A, |3 e
w
/ q8 g9 c% n7 S' u0 V* Ts
$ z7 e8 Q }4 m- ~A. _6 g# Y5 \1 Y4 y0 d0 [0 h( P
o
- L$ r. t% r# D( \ALTITUDE INTERVENTION, Pilot control of the
9 A) J6 b. n0 z' ^% E& u: S- ^* da
+ E9 K$ A$ q eAMBIENT, The surrounding atmosphere.
+ O& j, Z# T5 X7 z$ e备用机场,
. E; e1 ^1 L# \. q" O当不可能或不适宜在预选) v0 a& |. n4 }6 a# z# F
机
$ c2 g$ k4 A1 i高度表设定
' {) p; q# t5 P高度截获,
0 d/ U* D5 o3 q2 l式/ ~# p5 z2 R7 c# H! C- f8 g
高5 Z2 M3 J0 I: h/ a! d& D
高度干预
' {3 ?8 I8 ^ G) Q在垂直导航工作过程中,飞行
' g8 j/ G4 u8 n7 d周围环境(地面气层),
8 f" _: i' l, p- D" ^物体周围的环境(特别指大气)。+ Q. ^2 M. d& H9 S& l
英汉对照民用航空词典B OEING
8 W0 M3 {6 e' {( u' C( z' XTECHNICAL DICTIONARY 98 ?, K) [; s. q* i) I3 [
AMBIENT PRESSURE, Pressure of air surrounding an
) P5 ?, p& a& E8 tobject, measured in pounds per square inch (psi) .
$ [! b) R3 a; e* R9 a0 OMBIENT TEMPERATURE, Temperature of air
6 V# c" L- f- t, z: lmpere.
3 N w1 p' A; t. Yurrent waveform.3 c4 r4 _# h9 E, K9 h( s0 Q2 \4 K: [
g an/ i0 ?" \, d, A
nalog signal to a digital signal.
9 Q5 J/ g8 S) tore inputs3 g6 u; H: d/ Q! _- u- R# Y( n8 g) l% j+ o
f binary digital information and one output. The output
4 K& q* O8 |1 i0 n* n1 only when all of the inputs are 1. The output is 03 `* x' c" P5 k, V+ q+ \, `! n
hen any one or more inputs are 0.
P9 Z3 _$ ?7 R/ Y0 n7 p; L! M面气压),; a$ u# `. b5 W& i. s' A5 [& |
境温度,% H7 n! @: R+ |" y \
气温度,用摄氏度(°C)或华氏(°F)来2 Y9 N/ D8 @; b
。
K' A5 }4 F3 `- m' J8 [电压或电流波形的幅度。/ t& g( D% {7 @: d/ \
性变化的信号来工作,或产生连续性变化的信号) y0 e2 h9 F: e+ D* a- R& |7 D5 f# r
统。# M) b0 @/ R3 T) z+ W1 f! }
将模拟式信号,转换成数值式。
" C) n: E4 @' h" J9 |& C) d一种有两个或两个以上的二进位数字信息输人,一个输
5 `4 i6 |4 Y" f" q' A, g的装置或电路。当所有输人为1,输出为1。当任何一个& {! L/ K2 q) y( ]. e
一个以上的输人为0时,输出为0。1 E* ]& M5 Q1 U( M1 L
A- f& i8 K8 [: ^7 v _9 a+ G
surrounding an object, measured in degrees Celsius7 f' W1 _8 x Q
(°C)or degrees Fahrenheit (°F).' K' ]: C- E& T
AMPERE, A unit of electrical current. One volt across
! I( Y) X0 Y' d+ E% Z) m" Fone ohm of resistance causes current flow of one
+ y; V& ~* U8 Z0 M; `! @4 q( Qa! [ J4 r6 [ O# I% n
AMPLITUDE, The size or magnitude of a voltage or1 f: L4 |$ e0 _# r
c
8 D6 w5 d/ V) ], A# ]& l" |1 QANALOG, Quantities or representations that are! c, b" v- M+ d: C% h/ M
variable over a continuous range." d7 j4 w( N7 ~4 X) B* N- @/ J/ D6 |
ANALOG-TO-DIGITAL, The process of convertin
! P( R8 Q8 b) Pa
/ e7 A A7 u2 \( {$ N' ?AND GATE, A device or circuit with two or m% h& M Q' i$ z: u
o
7 _8 k- T2 p' |. q9 P0 a7 q% pis
! `3 C, g3 j. X- r4 P- g: S; Qw# A6 P2 N B$ a* a9 R- Z9 a
环境压力(地
6 f3 R- L) \% W1 G1 J5 Y' Z2 g* E物体周围的空气压力,用每平方英寸多少磅(psi)来
0 B6 e& t6 @5 m! P; f* D度量。: j% T. R# o) V5 K: z
环
4 _: ] R1 c( \) W* @0 P物体周围的空- ~4 X7 ~# ^' R* E* j2 Y
度量。
# d, m* {9 b4 b! b安培,
3 S# D; u3 Z7 d电流的单位。6 l6 k3 t" @% K. T* `) _4 a
1伏电压在1欧姆的电阻上所产生的电流为
* |* D; M2 R8 B. t" b$ Y% B, G4 E! w1安培
+ a r1 e% A' B振幅,3 B% f: W, v2 R! ?1 }' Q
模拟式,
9 F+ ~' M8 |- [7 u用连续
2 R, x& S# b! R8 G系
4 m; j; v0 ~: r' q; J# D从模拟式到数字式,* f$ k e- j3 Z' T+ B4 j- m' s* }
与门,
! ~, R2 S0 P1 T# b: [0 G2 }+ A出5 ^6 M/ R! E; x% ^! K4 z6 w9 A
或5 |1 L/ \0 _2 S. z: _
英汉对照民用航空词典B OEING, j& f1 `' H z* l
TECHNICAL DICTIONARY 10
' ?- L& ^; c' _, \0 R% tANEROID, A sealed flexible device containing air at low. I2 r4 S7 }, I, v( O N0 U
pressure, which expands or contracts during change of( t2 o; m9 C% y$ l2 O
ressure outside the device.
0 u4 Z5 M# |( {* c" ]ically: b$ e5 B; P1 N0 G* R b
r changing the direction/ a1 N+ K/ X5 n/ H
f drive.7 O0 }& r7 j: Q$ r. ?
of the wing chord in; C- a5 \. M$ M% i0 p9 G
lation to the free stream airflow as it moves forward0 }& @, d* W+ C$ a
rough the air.# I$ h/ z0 d! w3 b3 |
al axis of the
# Y. l/ n1 g% C* x' zaircraft.0 N. F# _2 T9 o( i, F
胀或收缩。
7 a1 u" o& h( S& x( m4 b. P5 k箱。是改变驱动方向的机械装置。* ^8 e# V d, w
机翼翼弦在空气中向前运动时与自由气流之间的夹角。% u1 ?5 o2 @ A; t8 [! I
。
3 L5 M7 v6 Z% g$ N# k# T- r5 H' {p5 `: Y) x1 V% j3 O
ANGLE GEARBOX, A part of an engine, mechan
+ f# P6 b, H8 Z8 t+ `5 jdriven by the compressor, which drives the accessory: G# z# Q! D |% k- r% r4 X
gearbox. A mechanical device fo8 o0 ?5 ^1 `6 w+ X- R8 W
o2 ?$ n* S9 z4 k" t b0 v6 Q
ANGLE OF ATTACK, The angle7 R# W( h1 n+ g" t
re
* |' O. h: d2 ^: {/ Lth7 b6 m2 t' j5 V5 e- `/ e, z |
ANGLE OF INCIDENCE, The acute angle which the ^* R x" }) u7 T7 v% B
wing chord makes with the longitudin2 f5 Z4 w0 L/ Q4 {) \. R: U
膜盒,
4 [- {: ^) p9 F内含低压空气的密封弹性装置。当它周围的压力变化: R! L6 R6 w. \8 n- s. D, D
时,会膨
: L( {+ E0 m2 P. k, d( b伞齿轮箱,
; f0 |, K# P0 T发动机的一部分。被压气机以机械方式驱动,然后驱动
2 j; d+ |- \+ m附件齿轮
( l, W! x3 x0 @ a迎角," t1 M: Y1 X5 d0 x K
安装角,
( A' j2 z7 x* y1 ?飞机的纵轴与机翼弦线所形成的锐角2 q, n- d$ s2 j: C T8 ]! }0 ~% I
英汉对照民用航空词典B OEING
: u5 a4 x& ?! L0 lTECHNICAL DICTIONARY 119 E* x. O4 d# x6 Q6 K# Z! P M
ANNUNCIATIONS, Audio or visual indications used to# f- [' b1 H5 S) \% L, G# S6 r
call attention to an event that has taken place.) p# _' |3 G- P1 U8 ?3 j
ANNUNCIATOR, A visual device consisting of a number
5 r) u: ^' l% r. Hly.5 n' |4 x3 e+ G8 ~8 f& X& y
ANODE, The element toward which the principal stream
& I n& y- q5 M% Qof electrons flows.
/ _$ g5 Y. b( u7 f6 N7 g6 |2 WANOMALY, Not normal.4 c U8 f5 H2 a* Z# P
ANTENNA, A device which, used in conjunction with a1 K* e# y6 i/ |) m4 `2 A
transmitter or receiver, is used for radiating or receiving9 b0 l8 `3 ?: t! Z
radio waves.
) D1 m( m! k4 X$ z# a/ {NTI-ICING, A method of preventing ice formation on
0 t1 ?/ q( k+ {) l9 r! be wing leading edges and engine nacelles.0 z2 r$ C! @/ B5 ~# R& m9 d
NTI-SKID, A system for providing maximum braking3 u. ]$ _9 f4 E; P! C' {- _
ithout skidding for any runway condition. Anti-skid. l0 B7 T, }1 @. a3 R! a3 C6 l" @
omponents are part of the brake system.7 \' a3 Z+ {0 F- x
告,. Y* d+ G- F8 U7 e
当发生事件时,以声音或目视指示形成的提示信号。0 o; T, x$ P4 |, Z# ?
与之有关的电路的现有情况或已存在的
7 c" y2 v" D r5 w2 s3 b2 ]况( y1 r6 @, e* o" |0 u) W9 ~
正极,
' m$ O8 d t: Q+ {2 R' N2 ^5 S主电子流向的极位。4 A% B0 U2 }* y+ i* _9 A
异常,1 s; R8 \, P8 P9 Z# K
不正常。
/ k( {6 I A$ {$ e天线,
. M4 b8 f. P' c# n: f9 P( |$ x0 J5 V一种与发射机或接收机共同工作来发射或接收无线电
/ R8 s2 s3 M3 `6 F1 z( Y5 ]2 v2 u波的装置。
; V7 m6 s. B2 |* g4 I n7 w; i k冰,: t. ]5 J* N$ F. H7 Y
防滑系统,! `7 J8 |: a% M& Y$ c* U7 O
一种在任何跑道状况下,都能提供最大的刹车能力而不( o! `2 y2 G- O% z, c
使轮胎打滑的系统。防滑部件是刹车系统的一部分。' p$ v3 e; F- J
of lights. Each light indicates the condition which exists
1 c! f' Y# z4 m$ I7 uor has existed in an associated circuit and is labeled5 i( a' }- V7 I5 s
according
+ S) |% @- Z* E. A7 BA
. ]3 G* e# O6 z+ i- S; _th2 R- e9 w! O& n/ \- K" ~
A
7 |. a" Z$ U& gw
* i/ m9 E7 u0 Q0 \1 v; _1 Hc' Q8 |9 a% c0 { P% o
通! A" g9 f& [' N4 ~
信号牌,1 F3 A1 ^0 y# U' \! p# T
由一系列指示灯组成的目视装置。每个指示灯都有相应
4 a4 M# @2 ~! ]+ J' N* u, O7 f2 A; L% j9 J的标记,用来显示. i- O* f! u. s2 \5 l! h" U
情$ M: z7 e* F9 s' O0 X, Q+ E
防4 [4 L9 a+ h; R
防止机翼前沿和发动机短舱结冰的一种方法。6 n3 U: }4 A" x7 J: O
英汉对照民用航空词典B OEING- i" m) [ G" s
TECHNICAL DICTIONARY 12$ f7 O" t3 Z" X$ s8 Q+ O
APPENDIX, A supplement to the Airplane Flight Manual
! m' c; P6 g# P5 _tained in the basic manual. A2 R: [) X3 j3 ?; M, E1 W, @
ollection of supplementary material at the end of a
" t; n F* \6 f; r% J. h5 Y7 Nook., C7 ? P8 K/ ?# m
of the
* N/ q0 Z5 l& x1 A% f) ersion link on the landing gear.
4 J; P( Z! O: J" |3 mAPPROACH MODE, An autopilot/flight director mode
# }1 f, [; K7 S4 y/ @, ^which is a combination of localizer for roll control and
% A. z5 q/ x, x. B3 L6 hglide slope for pitch control. This mode is used when full' W f2 @- I. Q& S
instrument landing system is available.2 @5 ~* P$ I- T" G9 l( a7 t0 c: [
APU, SEE - AUXILIARY POWER UNIT: j- M9 b( t1 T7 E
ARINC, SEE - AERONAUTICAL RADIO
6 P- N- T) K& b- w" XINCORPORATED; C! `4 { u# _! A
ARM, To make ready for operation.! G/ u$ J/ W0 }: {
附录,% k6 F5 O! g. j( C* u4 ?* h# h
飞机飞行手册的附件,包含基本手册中未提到的飞机形
* [& k4 n" c, ^" h. o7 l; Q; Q- a态的其他性能。是附在手册末的补充材料。3 J9 N9 d, H0 [; I
顶销,
5 r; O5 I# @7 x' N/ y/ ~6 y; Z, j用于连接起落架扭力臂两部份的销子。' X( D1 E# N& B% S; K
进近方式,0 U" T- `! D3 S% n2 B
一种综合了控制横侧的航道信号和控制俯仰下滑信号
9 ^! M; Z/ K4 s的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系
4 Q9 `3 u# {0 D/ r统正常时才使用。' a) x( o5 z0 i+ ~ M
辅助动力装置,
4 |5 n) M4 Q$ H8 P+ s8 M见Auxiliary Power Unit
3 T$ h/ f& U, @" c6 @6 n% d9 [containing additional performance for aircraft% t. @# z7 C* j6 Q
configurations not con
2 W: Q: H' ?0 U9 H f% ac( z, G# p) k2 J3 q4 n
b6 t! i+ N, Z" y4 ~' q: d
APEX PIN, A pin for joining the two sections
* F* j! T5 K* o. d/ xto, F6 |& t! x. O6 u8 F( i( S
.
0 c' g, j9 Z$ h, w" Y9 R! H( n* ^航空无线电公司,8 S& j+ D: I8 r( ?5 j
见Aeronautical Radio Incorporated.: I* z' j" A" H
预位,3 T% s$ c. C/ j; [' a
部件可以开始工作的状态。; {! L; M* c; p1 o
英汉对照民用航空词典B OEING# u8 w3 [4 i9 P% x& Q- c' S' Q# y
TECHNICAL DICTIONARY 13
1 A, Q# @& ?, lARC, The curved track over the ground of an aircraft
4 A8 y7 Q5 J0 s' Cflying at a constant distance from a measuring
- Z& ]" c$ @$ p9 P$ j. t4 m" \equipment (DME).
0 m. [. k5 ^, A1 a+ K6 x' z6 ~in the limits of self-contained system
Q% q% S* j* O# f$ _apability.
& B* Y. K% G9 W9 j: Gtem for opposing or restricting' d, a) k U6 e2 d/ w
ovement.. {* Y) f' B* P4 Y
SPIRATED TAT PROBE, A sensor that measures total1 t! q1 ^* l# A3 j4 S' V# ^
ir temperature when the airplane is in the air and that
8 j; u) s5 Y2 b1 ~easures outside air temperature when the airplane is
4 D% M& T3 u* C) K! M0 Qn the ground. The outside air temperature is measured* v5 I# {. d% a \: T
SSEMBLY, The fitting together of a complete structure
, R4 }6 Q/ x0 F0 X- D+ ?1 \, c$ {SSUMED TEMPERATURE REDUCED THRUST, The& Z& H$ L! X; Y1 t6 E; p0 s9 I
ATC, SEE - AIR TRAFFIC CONTROL! ~# ^* i9 R% f
,
, D( }6 `0 |' M5 i; ]系统中所产生的一种用以抗拒- P2 U1 s8 M" U4 B3 @; b9 \
作或限制动作的力。
0 b& S+ l5 C. a$ C- K头,
$ K: M$ I1 a: D" r% ?" `: ^用来测量飞机在空中时的总大气温度和在地面时的外
0 ^" z$ V0 _: z3 u! u" K温度。地面外界温度的测量是利用引气将外界空气吸入
" p R5 w& B: X& v头,以达到测量的目的。
0 ^' m# ?$ v8 F7 C/ L配,
5 V: T- o+ p( a* T6 O( G一个完整的结构或组件的过程。2 a# s/ J" i) E$ @8 X% o
假设温度而得的减推力,
1 D0 G6 P; r9 j7 S' A推力设定值时,假定一个比实际外界空气温( {6 Z' {( g' B" m# a- ~
空中交通管制,
: `. T/ n. p4 o见Air Traffic Control& E: ?2 G# c3 K% W, C1 V0 ^# x
AREA NAVIGATION/RNAV, A method of navigation9 L' a S6 m) R
that permits aircraft operations on any desired course% W, g" _1 v1 T% L! [( m+ J$ G
within the coverage of station-referenced navigation
r$ v1 c4 F5 M: s( x* ~# xsignals or with! ~, [, a0 r2 s! s/ f
c
$ e; p5 I( t; m9 X" ~/ oARTIFICIAL FEEL, A force developed in the flight
. N/ H: T5 q9 Q) {3 `7 Rcontrol or brake sys
- h8 N% t8 B+ Om
. w* R6 z# \1 O% DA$ }/ M1 M2 p% Z7 {" p% ^2 [! g& e" J
a
6 J6 H. f, R1 e- d+ }) j& dm) T S! Z" f" c' S. ~# N a# o
o j5 O) z) t/ e" n; a0 I( ?: L
by using bleed air to draw ambient air through the" c4 A+ i3 {3 y( D
sensor when the airplane is not moving.1 C! @+ V) B1 k5 Z/ T
A( n$ F# P+ a. P5 e& e
or unit.
$ d' W" M' l' P9 E; h1 S' q1 g, ]A
5 Y9 ^4 N2 {5 H" r" }lower thrust obtained by setting a higher than actual3 R* W {1 r! x |0 u! d
Outside Air Temperature (OAT)./ v* }$ l* H; X; O# C
弧线,
7 l" P5 _' L% G- m- x1 G飞机在围绕DME台等距飞行时的弧形航迹。; o( L( R; l1 z$ W1 i
区域导航,
1 G2 N: n% D" y容许飞机飞行在有电台参考的导航信号或自备系统能: M3 U4 L+ [6 ~. B) _ q
力极限范围内,飞行任何预定航线的一种导航方法。6 l. r8 _. x: ]) o3 V- @
模拟感觉! X) k! j: y4 Z; q7 C+ {. l
在飞行操纵系统或刹车
: V s f* Z. } K动9 x& O8 h% r R: F) l7 y
吸气式总温探4 E# d# G% x8 v' o9 X+ c& ~2 C
界
' A, i4 E' n( i) O探, }$ c4 E' E3 y# F d
装
% H: y T2 M1 Z; l组合成2 `* [0 O* F( y: I/ O$ C2 ~3 G" F
由
+ K1 e1 g, ?' L4 h- v) f在选择起飞3 d: Y8 \8 `# Y q9 E, Q5 N5 K' K" @
度高的温度而得到的推力。用这种方法可以减少发动机的1 h8 G1 v: K( G4 o j# j8 H
磨损和维护费用。1 y2 Y+ O) h, v$ n1 Q1 E
.
( x1 `- G5 d1 }6 J英汉对照民用航空词典B OEING6 y v( [( Y! t, t3 j6 J- l
TECHNICAL DICTIONARY 147 g! {2 I3 R; I+ N; h
ATE, SEE - AUTOMATIC TEST EQUIPMENT* O* C3 V$ k2 K& l* ]$ M5 F0 R
ATMOSPHERIC PRESSURE, Pressure of air due to the
1 a) E7 \. U1 C* a7 Xarth's atmosphere, expressed in pounds per square8 C J0 q% B% `$ N: B c
ch (psi) or inches of mercury (in Hg) or millibars (mB).3 }2 x6 h+ ]8 S5 P% J, B
TTITUDE, The relative orientation of the airplane with
" S& o# v+ T& s7 |% z* l8 l Rspect to pitch, roll, and yaw.2 ~) Y- t- m; }; j
UDIO CONTROUSELECTOR PANEL, The panel in
4 o. @3 u2 i, u5 B9 A! ne airplane which controls and selects the routing of
6 R) P* u, ?2 m5 T5 uudio.
$ w# C! ?8 @; D8 r1 |" N- ~3 mUTOLAND, Automatic landing using the Digital Flight S4 e4 j& L9 Y. v X" H
ontrol System., h6 X G" E8 E% v! `0 F
n.& W8 q+ V0 w3 r1 {4 a
M, A system
3 i( `( [- N1 O. qomposed of all necessary subsystems needed to guide
0 ?2 g5 }6 h$ T# B+ @2 P1 s1 t! w4 He flight of an airplane., i3 x1 d+ ^) g
EQUIPMENT, System test+ P6 H+ p! l% B& j. @
quipment that operates under computer control.+ u# ^3 e+ P, M6 T7 k1 O( T
装置, |
|