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AIR DATA COMPUTER, A computer which produc2 N( k1 T) x5 M6 g3 |2 T
data information, such as altitude and airspeed, based* |* Q0 Y5 O4 A; W/ f5 _2 Q
on pressure and temperature measurements.
; `, _* k& g( P) E3 @/ C9 Wes air% Q, F: l; L7 `; `3 l
IR TRAFFIC CONTROL, A system comprised of
5 ?: u( |( Q1 B7 v8 i a$ y0 m7 Nround and airborne components used to identify, track
2 |6 \5 c3 Y7 G( W" s9 L( tOUND SENSOR, An electrical device operated
/ F$ A! @5 y9 Yy the landing gear, which transmits on ground/in air6 r9 k6 |% z. u& u! E a
formation for system operation in flight or on the% z# w5 \: w5 g4 Z
round.5 b: G+ L7 L' }# @5 s0 ]( [/ K
IRBORNE VIBRATION MONITOR, The AVM takes! }3 O' T4 Z3 g8 R2 M6 Q! x
e signal from the engine mounted accelerometer and% i6 g. R: W- g8 v5 [+ D
alculates the vibration on that engine.) C6 }$ }4 c8 j( o
corridor equipped with radio navigation
/ q% c2 m2 `2 ` J4 X. g$ F* vaids.
: n6 n9 V# g8 l1 L4 O/ O4 V1 j: bAIRCRAFT (or ARINC) COMMUNICATIONS
+ Y$ p3 x6 X1 o( H4 P: b( y6 R* E" |ADDRESSING AND REPORTING SYSTEM, An
! Y, R: I/ ^( {2 j, Caddressable digital data link system which permits the
1 w0 W0 _2 s# h8 {3 E) H+ aexchange of data and messages between an aircraft- O8 f k* |% T* G2 n' P
and a ground-based operations center over a radio" J" U1 B% f4 G3 }; i$ ~
network.* ` d8 x2 K1 a/ m/ `
AIRCRAFT CONDITION MONITORING SYSTEM, A
5 _' e* k& e7 L2 ]/ b5 tsystem of sensors and recorders to monitor various) k2 t% m6 z! Z/ x& U) u4 \6 m
airplane systems' performance and status.5 u' Y) b! i( J
机,
& @0 W$ G4 `' N- ^% N中交通管制,7 ^* E* {) U+ T% J" B
一个由地面设备和机载设备组成的系统。用来对飞机进
0 e4 K) n$ b' k; r4 G& |地传感器,
5 T- F) b# i5 m- K+ K一个由起落架操作的电气装置。用于给空中或地面的飞
" R$ F# l+ |" i# b系统运作传输地面/空中信息。(有些系统只能在地面* X4 s5 _: m7 [9 a0 w' X3 f
用)
$ z' r v0 ^1 R" P' D+ g4 \: E载振动监测器(AVM),
5 H" p- p* H) \8 \% z; uAVM从装在发动机上的加速器取得信号后计算出该发
m/ }6 h1 i! \% L q# d机上的振动。
& g, ] m6 D9 P% K式建立的控制区域,内有无线电导航设备。6 ]( G# p$ C X. m. P1 C
飞机通讯寻址和报告系统,5 v* r% j: P, `2 X: D& L/ I
有种可寻址的数据通讯系统。利用该系统可使飞机与地
1 k% k# C6 D- z" d9 z k D面操作中心通过无线电网络进行数据和信息的交换。
8 O6 L% ~; |+ g飞机状态监控系统,: J& i5 n% O% P* A y$ f5 e9 F
一个利用传感器和记录仪对各种飞机系统的性能以及
* U( k& L6 _+ f1 [8 g8 g, d状态进行监控的系统。. \: e! B+ c( @& _2 T
A5 Y" K1 a# J# I3 a9 W' G4 V. |7 q
g
! z1 a8 A3 D( o" x) q0 j& L+ u1 j; @and locate aircraft.7 ]0 H8 x, ?8 {2 {& H: h; j. M
AIR/GR
X2 k8 J$ B& z% A. yb# ^, A* s$ j5 y
in j8 E$ e( ]. a% L" v$ f' W& H3 @: V
g
) ~) ^! T4 t7 [, {, J+ IA
1 {7 O2 `+ Y, wth3 E3 @* M6 t8 J# x, y
c
" A- j& }7 e0 g( H) Y* {, [* MAIR WAY, A control area or portion thereof established
. c* E7 `2 J( w( lin the form of a
A- Y0 c* o" Z0 W$ g! S大气数据计算& f0 q, Y( F Z# C# i2 {
根据量取压力和温度而产生大气数据资料(高度、空速
6 ?2 t7 B2 q1 o! w+ T等)的计算机。
$ S' g/ c8 Q& Z7 Z) e# i1 k, M9 j空
: i5 Z7 k4 t# s% \行识别,跟踪和定位。
2 G# a8 N% ^0 D( v空8 I% @7 e+ R' u2 R. S% M1 r& Z
机8 ^# s9 k9 R6 O- Q9 ^
使
2 {) w6 G, h* i) I- b" `4 C( g机
! j2 p' F) t9 q动
' M# W. m1 u" v; L& n6 E4 [/ D航线,/ {2 Z4 ~" d. j( i4 ?% B
以走廊形* g! m$ C% e) `) Z+ _/ ]% p1 Z" }
英汉对照民用航空词典B OEING
Z) r6 x D0 l9 ~! [( k; q5 `8 cTECHNICAL DICTIONARY 6
`% j ]+ H# m! _AIRFOIL, A surface designed to obtain a useful reaction,
5 m2 ^0 c2 E0 ?& G- k# l; L }such as lift, from the air through which it moves. Wings,4 G# x% ~2 ~( C. `+ h5 E& k
stabilizers and control surfaces are airfoils.
0 v0 i- n7 q. m) SAIRSPEED (IDS, TDS), The speed of the airplane
# D o0 a* _& L0 K& Frough the air.
& v* O) K9 e* FD INDEX, An adjustable pointer on the
- @3 J3 T( q) c q3 ]7 d1 Mirspeed indicator.. C* H3 B; H, Q5 ]- d
and legal ability
4 u5 p5 f1 F3 @- x/ Mfly.
" O: L' T" j6 D5 q' y! _m, for example, the procedure for finding the5 \" \% O* y1 E8 D* W* g& ] f/ r- ~
quare root of a number.3 o* |3 H9 ~3 D+ u: l
y# ?) x# W, H/ U# I$ d- M
re, wind,* K' ]% y. G6 G8 _1 v
and aircraft flap setting.8 i% ~# t$ P: ~) Z* T% A# T( u, L
是翼面。
! |) p, r3 E: m' G @* R ?) E& b速,
, ^+ Q- D1 P$ |8 n6 J飞机在空气中运动的速度。
# G7 Q/ }$ [8 \- W7 {4 `8 @) ]2 [, u,7 K% I T+ N2 K8 z% Z& X* l( d
在空速表上可以调整的指针。, d& v& y, {' U$ q0 I! B
机械飞行能力、和合法性的飞机状态。1 G% n0 }+ }$ n: G I# y. ^/ Y
一步一步的解题方法。例如,计算一个数的平方根的步: }* {; F& B( `6 Q. \' Y
。
' J8 p2 n$ @0 a7 i能7 C1 o+ k$ q6 w6 y+ i6 i9 k
资料的法定文件。7 \' ~6 K: O' [
翼位置成函数关系。
( K9 |! Y L: Y1 Fth
1 H0 Y9 \5 q2 D' B6 ?AIRSPEE
# l" W4 U6 [* Q0 R7 V; C0 ^a
4 U0 G4 o' X0 L) U- m8 J V6 H# _AIRWORTHINESS, The condition of the aircraft with! q" M) L* A3 D. ]" O# z8 O' |
respect to its aerodynamic, mechanical,
/ S! R4 A6 A dto. e: v' }9 E, d
ALGORITHM, A step-by-step procedure for solving a
) K% y' b, `( Iproble
2 {3 [, \, D, o$ C& v% I3 V" us# l j. o( ?) N) d
AIRPLANE FLIGHT MANUAL (AFM), The legal
% y- |/ l; G v3 F- Ydocument containing performance and operating limits,
6 _/ V' Z8 R+ v% q$ y/ E) b' e! zoperating procedures, and takeoff and landing2 y E- b3 e$ M3 \8 w, J
performance.
5 M% x0 k& M8 n" k3 ]AIRPORT ANALYSIS, A comprehensive set of takeoff; u7 q1 P) z, M& c6 v
weight limitations for a given airport runway, generall
$ v: B' _: c' ?5 v/ d& c: k% xpresented as a function of airport temperatu
6 J! V6 r$ D' B' Z! H4 V; ]8 T7 X翼面,
* \- m6 {. ~2 a$ Z- ^" I! V用以从气流中获得反作用力(如升力)的表面。机翼,
5 q6 L, g2 r& M* d' D安定面和操纵面都- [" V( V) j+ o7 \( v3 _
空
9 U! h% J% u0 a; _+ U2 N! |* F空速指标
& z; P% W, _( y; c适航性,
0 k6 f2 j- j: f4 Y; u+ `有关气动能力、
1 ?, z2 A: B# [" s7 i5 \' Q演算法,' s& R0 `4 ~# |1 R, y% y4 Y1 a2 a9 X
骤
( P5 p& \2 z! b* O飞机飞行手册(AFM),
7 ^3 V1 C; `, U& ~包合性能极限,操作极限,操作程序,起飞和着陆性! r9 R2 D! |% c* ]
等
6 c' o0 k* g7 `* j$ l( ~机场分析,
" |( c3 |" ?7 S. _8 l一套针对给定的机场跑道的详细重量限制资料。通常与. i5 F$ {. C& z+ p. S
机场温度、风、和飞机襟
, y0 q' s4 e u6 S英汉对照民用航空词典B OEING
8 N/ H, J$ \. Q" e; a- Z, PTECHNICAL DICTIONARY 7
7 v9 E8 o: t7 C' d7 ?& X$ XAIRSPEED BUGS, Adjustable pointers on the airspeed
; T3 W, ~6 _, {5 D0 ^indicator.& y! ~7 [" N# |* F- t' d+ h
ALLOY, A mixture of a basic metal and small amounts
* P' k, D3 k1 U, e8 hf other metals to change the properties of the basic: U c% R1 V7 l7 K$ Y$ |* o9 D* r2 G
etal.& o, p0 J1 E' A* k+ s1 W
Minimum airplane speed./ L6 \, @# K# {% \3 s+ m8 ^: O
e of
. z) M$ x r# u1 g9 _itting airplane angle relative to
5 a4 p/ c& k2 R3 e A! y; sirstream for the stall warning system.+ u6 `) m5 j) I& t' v3 B
another.
; e& C8 R# a" v3 `7 K0 `LTERNATE , An additional airport selected during8 F" ?/ x- ? u W) y
,! K) U2 o- Q( n; j2 }* S$ p! H
合金,
F3 e, P* S7 A* g; z在金属中加人少量其他金属,而改变其性质的一种金属/ C1 i& a' q8 ]+ a- n- Y
合物。, ^: v; w- a: C
飞机的最小速度。
7 T+ g( L( K7 |$ \) E* f# g0 P速警告系统传输飞机对
/ S2 Y M: a; d0 {$ l( T流的相对角度。) j. M+ I( l: _. _& x
由一个状况改换到另一个。
8 A' N2 S h& ~: y降场,. M- Z, Z o) }' w2 W0 b7 M6 L
划时,除了目标机场之外,所选的另一个机
- V6 j+ P$ t" q( n4 `( ~o
9 ^$ h/ e7 K. O! qm+ _' f+ ]# T+ Z" P, B
ALPHA SPEED,
U) w+ d5 Q/ rALPHA VANE, A small moveable airfoil on the sid
7 z' Y; [2 l+ M6 j* Lthe fuselage transm2 d0 G- T5 s/ ~! z3 r B
a; j; @- W m# u( p
ALTERNATE, To change from one condition to
; z6 a+ g7 t7 S; g6 I DA
( P( B# y+ p- e3 Z' `* Lflight planning, usually near the destination airport, to be( w& [9 O: L$ J
used when it is desirable to divert from the original& G1 J$ ^3 q: {: X
destination airport.
8 {9 y% k0 I/ Y* e空速游标
1 g, p b' U5 h# A1 |- F, i空速表上的可调指标。" w2 e. Q8 o" y
混0 J1 |. w; Z' R6 M# S$ G8 A
迎角速度,! q2 f) `2 {, {7 R
迎角叶片,
: v1 p0 X0 ^6 i6 M位于机身侧的可动小翼面。为失$ k# T: c) d# Y( g4 o2 Y9 e
气
1 y: S7 ^. ^2 [3 j: X交替,
1 a( `2 ~0 m# Y* D, b' V备! Y( [' s( d3 g) G
制订飞行计
" X6 u* J- b$ J6 Y5 e场。通常在目标机场附近,以备不去目标机场时,改降之* F. O! l) y7 @& m# y
用。+ R; p1 P, E3 ~3 P
英汉对照民用航空词典B OEING: a3 [- v. V2 g6 v( k
TECHNICAL DICTIONARY 8
) W: S5 J% W% M, c8 HALTERNATE AERODROME, An aerodrome to which' K8 F5 M6 i2 S: k* O- P [3 y
an aircraft may proceed when it becomes either
2 {8 r! X% a6 e; E( x: fpossible or inadvisable to proceed to or land at the0 L2 t4 }9 {9 p8 [! P
erodrome of intended landing.
0 s+ v: x: l8 B' }TER SETTING, The adjustment of the altimeter
3 }+ Z( ]1 K2 Y: @1 J( G: e' L+ Vaccount for local variations in atmospheric pressure.1 a5 k1 S3 P$ M) J
LTITUDE ACQUIRE, A digital flight control system5 |' D1 ~' o4 l" ^
ode to transition from climb (or descend) to level flight.
% {. R1 P: z4 hLTITUDE ALERT, A flight deck alert occuring when the
; l- b' J; D5 o( E U0 A0 w$ o1 @/ Mirplane approaches or departs a selected altitude.' C/ x( ?6 ]! u* N' o' T8 i0 W
LTITUDE CAPABILITY, The maximum altitude at: d' H, f4 f! U7 z; k4 c5 D0 U
hich the airplane can be flown at for a given thrust,
, d' B. K$ o6 K1 n: t+ x7 x5 Q% T! Dpeed and atmosphere condition.
! x7 U E9 D( KLTITUDE HOLD (ALT HOLD), A mode of the autopilot
' q" W; B- H6 M/ d( }r flight director to maintain a selected altitude.$ n/ N1 y4 e8 m8 M1 k& @
irplane's altitude during VNAV operation.1 K# W3 x: }: A" @: a
机场着陆时,可作着陆使用的8 b' h. j, l, v# b
场。
2 d- T- F, s& C1 U- g,
8 I; R3 h/ x: b5 H4 e2 ]7 d6 y( _根据当地大气压力变化而对高度表所做的调整。( R1 l0 M0 ?- r! w' z1 d6 [$ y# @
一种数字式飞行操纵系统,从爬升(或下降)改平的模! C5 q1 P4 c7 U2 M9 \2 T: a
。. ]. ]- [' g% Q8 D* T! W
度警告,: F! E+ N ?# b0 B: q
当飞机接近或偏离选定高度时,所出现的驾驶舱警告。
" Y. D9 J# O+ j' d& I( |. j高度能力,- |' [; k2 b7 q# E# c
在给定的推力,速度和大气状况下,飞机能飞达的最大
6 ?6 H/ l" M3 X& y高度。
' e2 z/ u# l' x8 g高度保持(ALT HOLD),
. v: X/ K9 O: B- M* I, r l1 y% d自动驾驶仪或飞行指引仪保持在选定高度的一种方式。# v/ {& a4 u+ `
,. m, Q% Z# m- F( ~4 }
员对飞行高度的控制。
) a! [, ~! m |4 X6 \6 [# Gim5 C% h$ j( i4 u0 \' K8 ]
a
) ~6 k, p4 F4 k& HALTIME
# r( P5 P8 J4 Q. p/ vto
. B$ M# O1 L( E* ?% S+ V$ OA4 ^) [' r, V- P% z. B5 L( k
m! t1 H3 G8 L) ^' D+ z
A
8 w2 z3 H7 i, F: y* _0 Ja
3 J/ t5 E3 i1 R [+ w/ qA6 G2 }' r/ |6 I/ g
w
" t$ I& H+ D) K( B& s* Ms
/ g# I$ f+ U, h+ ?+ sA
/ i u% J1 H, B# P) p- ^4 to
' N6 `/ Z& T; fALTITUDE INTERVENTION, Pilot control of the
' Q& Z" a7 L1 l d% Ma3 a4 Z& ]; R( O% I- v
AMBIENT, The surrounding atmosphere.
2 }5 u# h! Y. ^& Z; n9 G5 s4 p, b备用机场,- A- b( Y. b+ P6 M- g3 [0 L( `
当不可能或不适宜在预选
* {9 c. R2 H) F" g5 G机
! P: [) M4 z$ Y2 ?% \& A0 q# e高度表设定0 c+ Q+ ^5 s5 u( q7 P1 i, f" w2 j
高度截获,* M" L- i4 @9 U5 C- x3 R, ]5 V1 k/ z
式
) ]& f! d: I0 w+ ]' z; @. X高) r; A" ]' _! i1 e
高度干预% p# L, X3 S4 w4 J
在垂直导航工作过程中,飞行7 [5 ^) `8 }; H g6 J, b- s) \1 ^
周围环境(地面气层),
. E# O4 D1 V; D) u+ @物体周围的环境(特别指大气)。: g+ P4 q) i1 G* l2 C) w
英汉对照民用航空词典B OEING- y0 E! O1 U* u5 w; [% K
TECHNICAL DICTIONARY 9# W/ N- s/ ^$ X/ r- ]- K
AMBIENT PRESSURE, Pressure of air surrounding an: n* F$ f* n- p( Z9 _: I# k
object, measured in pounds per square inch (psi) .
+ n. ]3 E/ |$ z9 WMBIENT TEMPERATURE, Temperature of air
2 ^/ ~: \ h' a2 wmpere.- I8 ?# T2 D, _* t( B
urrent waveform.
9 u3 f/ t4 q. F2 b8 \g an
, E1 A) ]1 v& s( f, j& Nnalog signal to a digital signal.
V$ t0 \4 h" o" Vore inputs
4 k1 R2 e. F/ J6 j0 ]" zf binary digital information and one output. The output
/ R2 K- C% r! B& y1 only when all of the inputs are 1. The output is 0
$ ]# b, p% o- E2 Qhen any one or more inputs are 0.; _7 D j2 ]- |4 x W8 T
面气压),
) ~, m1 P* j4 H; F) G境温度,# G5 x1 v9 e3 ^; z
气温度,用摄氏度(°C)或华氏(°F)来
& ]- D( i. p! x. u; @5 s6 \( v: f, \。! d: ~+ R2 U; i9 Q) Y7 P6 x
电压或电流波形的幅度。( j3 v; e" A: E
性变化的信号来工作,或产生连续性变化的信号: G: F* o' f7 Q! v7 W3 n
统。6 v: }# ~5 a1 M& H+ z: I* l
将模拟式信号,转换成数值式。
! @* o( i9 W- H: |一种有两个或两个以上的二进位数字信息输人,一个输+ Q' Z6 n! ^) h
的装置或电路。当所有输人为1,输出为1。当任何一个
) B9 F' N; L1 G: d) ?" [一个以上的输人为0时,输出为0。( f$ _" N E n! u6 t5 @" b, T
A
( s! Q0 R! h/ `' D9 V8 R3 Y2 ?8 psurrounding an object, measured in degrees Celsius
) g7 f2 p" c8 L1 _5 c( P(°C)or degrees Fahrenheit (°F).
3 G, f8 D7 }# h; w6 v% `AMPERE, A unit of electrical current. One volt across4 d! M: _( s9 s) k7 u. O: r; s
one ohm of resistance causes current flow of one
2 p7 B. k# m# oa4 ?( W; Q' i$ C3 b& l- E$ C `! n
AMPLITUDE, The size or magnitude of a voltage or
# c* N& m1 I6 d& m( H# Yc$ `! l# I) K- Y6 z# O0 A
ANALOG, Quantities or representations that are
& a( n/ U) u* C; e6 l+ {variable over a continuous range.
; {* O- [. Y l* r8 lANALOG-TO-DIGITAL, The process of convertin7 I( I, x9 O) h* y8 R4 B6 E4 s# q
a3 w" e: V% m. J; {
AND GATE, A device or circuit with two or m
; D; ]3 E9 S) h: n7 co. [" W, O- [* U1 }& I
is* d7 x6 c" x6 Y1 {
w* x v0 P5 a6 i! f
环境压力(地
5 s/ i6 s; |+ ~: P物体周围的空气压力,用每平方英寸多少磅(psi)来# _( R% ^9 M6 H* \! W
度量。
; @! R, @" J ?! @1 T7 X6 f/ r环
& d# a7 G& l: X( H9 v7 r物体周围的空
, F. p% z3 R' r- G, y! a# P度量。
- E/ T. \4 v; F+ X" {* f/ Y安培,
' M1 [3 K* h4 B/ R; K9 x Z: \1 I$ t电流的单位。
% g+ k8 T, L- y7 K+ T1伏电压在1欧姆的电阻上所产生的电流为
" d# o. k0 s. I; X3 W; A1安培5 |$ e9 N# p/ S" ~4 }( c
振幅,9 X7 k4 q- a2 T+ q
模拟式,
4 C9 f% P0 c: a) I+ W用连续
8 h4 k" G3 o" d7 h! B系0 H1 a. A- \7 q1 T
从模拟式到数字式,4 q) _6 o5 R$ F" d+ L9 E$ o& I
与门,
R5 S2 m7 `! H% r出3 _: o8 e2 |: ?, b) P
或
) z& e% F& D& ?英汉对照民用航空词典B OEING
; x2 p7 ^# b+ DTECHNICAL DICTIONARY 10+ r( X3 D' W' K" H
ANEROID, A sealed flexible device containing air at low3 a8 H4 L7 p: {1 Z
pressure, which expands or contracts during change of- l1 s1 n2 C% w
ressure outside the device.4 V) M; y3 B' b7 r) ~
ically0 Z; r& S0 ]7 K' {* }. K2 J
r changing the direction$ R7 n# C: {; h( U( Z0 o
f drive.
5 F3 P. W8 |3 L/ E/ \4 n; X s# Eof the wing chord in* T+ E- A7 u+ i- `8 c
lation to the free stream airflow as it moves forward
, p+ H9 g% h; ?) K0 }rough the air.
. d1 B: B5 q) N: H3 Sal axis of the
/ L, h& V/ o/ N0 y+ T0 N1 A. yaircraft.2 l% t# A/ K+ l! ]1 K6 j' j2 `
胀或收缩。" i6 T8 s y0 P4 g; e$ v
箱。是改变驱动方向的机械装置。8 t. \5 y" c& X0 T Q' S
机翼翼弦在空气中向前运动时与自由气流之间的夹角。* O5 r5 L. U( |1 E$ O
。
) k, P; _3 c' dp& H; I0 ?9 s! x
ANGLE GEARBOX, A part of an engine, mechan
' g7 \" |! E# {# d$ w) udriven by the compressor, which drives the accessory
; o7 s* Q4 k; Q* P. n. Qgearbox. A mechanical device fo
; H3 j0 G* f% H, _/ [- eo# G! S" c7 h5 n: D
ANGLE OF ATTACK, The angle9 J% B+ z9 i( R! S- @
re% }9 u9 i6 H' }7 i4 o8 o4 h, N
th
' i5 P$ m7 K, z% lANGLE OF INCIDENCE, The acute angle which the6 t7 ?7 w. v4 F( u6 V2 C
wing chord makes with the longitudin% l- r, a* h# a: F7 d& _3 I
膜盒,
+ r6 q9 f5 D. M5 j# a内含低压空气的密封弹性装置。当它周围的压力变化
5 j2 p6 U8 Z& H: [, G7 y时,会膨
$ f4 d. ^2 z6 j5 O4 t- C伞齿轮箱,' U+ e9 f7 s. X. N2 ?9 e
发动机的一部分。被压气机以机械方式驱动,然后驱动$ }; G. G# S4 V/ s5 a: v4 P! E0 p
附件齿轮8 H( G; a- ?0 N& b# h( i
迎角,; u7 Z0 @" b0 \% j: A$ s# I
安装角,' y8 G( _4 u. v/ {1 ?) J+ a
飞机的纵轴与机翼弦线所形成的锐角; q# t; p' r' R" X4 P
英汉对照民用航空词典B OEING% |- L/ Z& @; [* ?! @' q
TECHNICAL DICTIONARY 113 ]: W7 q% r7 q5 n, Q& j
ANNUNCIATIONS, Audio or visual indications used to
3 R, M9 J& D2 _+ J% m6 [9 mcall attention to an event that has taken place.6 V! z0 k9 A' `7 z
ANNUNCIATOR, A visual device consisting of a number9 w; T2 ^# ?! Y
ly.
/ |0 H3 O! F. b3 `# zANODE, The element toward which the principal stream
* { B1 D9 `2 K7 Q' o3 Tof electrons flows.2 @+ m1 |- z! |+ O* H( }
ANOMALY, Not normal.# n: Z- V' d# T- a9 z0 d7 @
ANTENNA, A device which, used in conjunction with a
2 s) U: H3 ?9 F* _) Y/ U% j- s* `transmitter or receiver, is used for radiating or receiving
9 v9 Y; I$ r3 F$ u7 [: |radio waves.
8 F) q: ~! B3 P9 t3 FNTI-ICING, A method of preventing ice formation on
+ x* p* C" D2 V% ]9 z( ~e wing leading edges and engine nacelles.
3 F7 n; s$ n4 k2 R: q! m" iNTI-SKID, A system for providing maximum braking
% [* c* W9 r, k& f1 j; Uithout skidding for any runway condition. Anti-skid1 O7 Z, T3 r3 a* `9 U A! z
omponents are part of the brake system.' V0 B) A1 L" L
告,
( w# s! A: L9 e当发生事件时,以声音或目视指示形成的提示信号。/ g$ w9 L: X- }$ T, H3 N2 A" K
与之有关的电路的现有情况或已存在的
7 F: z* H* i8 L9 O- A: r, I5 ]" s, i$ s况
4 r# ]8 a p/ B- ?6 i( x/ p8 i1 E4 e正极,% k, @' u' r: W: X; ] p# C& Q
主电子流向的极位。9 [5 Q6 J+ c0 S- B
异常,! ]3 h0 _( U) I7 C9 ]+ r- W
不正常。
1 O2 k+ p! @9 t1 P8 v天线,; v; C3 }# z% h: A
一种与发射机或接收机共同工作来发射或接收无线电! i, \4 f' F8 s/ V8 V' o
波的装置。
$ V0 }. x$ b- n8 W+ q) o" [ h& h' d冰,9 k6 h1 _ d* Q) f" a J& _6 ~
防滑系统,
& }- ~: h" ~2 m: l* Y. W一种在任何跑道状况下,都能提供最大的刹车能力而不
1 C/ V; x) @, @9 d6 E$ c使轮胎打滑的系统。防滑部件是刹车系统的一部分。
8 f2 u( w+ `, n! o* G: |of lights. Each light indicates the condition which exists# [" b+ K) m9 X5 W5 p
or has existed in an associated circuit and is labeled A! Q( ^- X* h" I. a
according
8 I. {* n" T# BA2 k) N$ u' A4 }/ ~
th- ?) \" a/ z* v+ R- h* S* x4 ~$ M# k
A( N1 U. J/ j3 e* _8 L. b
w+ a% b1 c6 X! A. ?3 c% C& n
c. i0 r1 P+ a+ H( K2 }2 O
通, z/ x. r' g, T# w* Q0 L9 a# L
信号牌,
8 g. ^6 N9 U/ ^# Z# E- y" P: |由一系列指示灯组成的目视装置。每个指示灯都有相应
7 y+ F1 J: h4 d( }5 G5 @的标记,用来显示
' L: ^" Y5 h* W' @! C情
2 {1 G" d! o6 d7 \防
$ d- F1 [1 u8 T$ g3 }) S6 }9 L防止机翼前沿和发动机短舱结冰的一种方法。0 b- m* e% ?7 u: J- w; y# R
英汉对照民用航空词典B OEING& X9 z5 u6 ~, r& W9 i) J$ z" y
TECHNICAL DICTIONARY 12
0 N: l6 ]4 j0 L" ~/ jAPPENDIX, A supplement to the Airplane Flight Manual
+ f# S/ \9 {9 f" stained in the basic manual. A/ ?6 { ]7 R) D: P2 _! D, z0 _3 Y. `- b
ollection of supplementary material at the end of a2 k5 z$ T5 c g
ook.
$ R0 d( H( ^6 a; Vof the# v; l7 a" s* J( h
rsion link on the landing gear.
. v7 _$ B4 G7 a4 z" HAPPROACH MODE, An autopilot/flight director mode
4 @6 y& r0 o" t! w& ]7 lwhich is a combination of localizer for roll control and
3 A: N! |& _; o$ \7 Q$ y7 Iglide slope for pitch control. This mode is used when full
' S( ]( V" Y9 g) k% F" u; D- winstrument landing system is available.
0 c" Y! R! c7 |8 `% kAPU, SEE - AUXILIARY POWER UNIT
9 s3 @( e# m$ J7 o. A8 gARINC, SEE - AERONAUTICAL RADIO U7 L. O n! S+ D; W; A, t
INCORPORATED
+ [* A8 Q2 Z$ j: e) K* L) WARM, To make ready for operation.
3 z8 s# J, q' B附录,# |' }) l2 I- I/ D, R, Y6 e
飞机飞行手册的附件,包含基本手册中未提到的飞机形
# y1 o* ]% U/ B1 \; O6 v. q' J: k态的其他性能。是附在手册末的补充材料。
9 D/ B1 O! D3 G/ l8 N4 {' v9 @顶销,, ^5 c% r$ P+ q1 `7 F
用于连接起落架扭力臂两部份的销子。
* t7 ]9 n) a9 m8 j进近方式,3 y$ `3 W+ i" t, o1 d
一种综合了控制横侧的航道信号和控制俯仰下滑信号3 V G3 e. L% V# X. Z, }. D* v
的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系$ T% G) i7 }! [4 o) ^
统正常时才使用。& m/ o+ F& h$ X. Q6 z3 `0 H8 {
辅助动力装置,3 |% _1 r" r0 ?' z: R( B7 |% v
见Auxiliary Power Unit
7 C- H9 @* a3 R! I3 G6 J. bcontaining additional performance for aircraft$ U1 |& k2 V1 ^- [; a
configurations not con1 {5 J2 o0 g6 S1 @7 b" C* h
c
1 X$ H* P/ D w% ~2 sb- G* C# k9 U0 g# w( d4 I1 @8 ~$ r
APEX PIN, A pin for joining the two sections
/ e. G' {$ O7 P; k* w, z# zto
* P$ W* J$ K" u.$ z" U$ Y' U8 Z. _5 B$ s8 ^
航空无线电公司,
d6 _( Z9 U/ @5 { V9 N见Aeronautical Radio Incorporated.
$ }% B$ E2 v/ c5 e( g预位,
! e# d' A. i; W$ ?7 o1 M$ ]部件可以开始工作的状态。# g; D. m) M% I P s
英汉对照民用航空词典B OEING- i, | e" e3 Y% R! `
TECHNICAL DICTIONARY 13
1 l. Y4 Z, P" C; l) T! MARC, The curved track over the ground of an aircraft5 D+ `( @1 N/ t% S% b2 y: }, g
flying at a constant distance from a measuring
) ], F5 |4 Z. f4 |0 l0 Y2 _3 Wequipment (DME).
9 P! B" G2 J- s( Q( d Xin the limits of self-contained system: p$ S3 K% J- j4 P
apability.
; v( x( m; |( S7 K& x' Ktem for opposing or restricting$ @% N3 c% E3 @9 V- J
ovement.
, m* @6 [9 B6 I; b( QSPIRATED TAT PROBE, A sensor that measures total
) D+ C/ H" h$ p& \* `$ j1 V% D% Cir temperature when the airplane is in the air and that
" _4 \4 g7 C/ m& L6 Feasures outside air temperature when the airplane is
' ]. S. ?2 z& _n the ground. The outside air temperature is measured
: v2 [! `' n( k& A4 ?+ ~; E& }8 DSSEMBLY, The fitting together of a complete structure
8 t% N- I: g- p) n1 v$ `SSUMED TEMPERATURE REDUCED THRUST, The
: P5 |3 L, K( G0 D5 Q% W! ?' H0 A. aATC, SEE - AIR TRAFFIC CONTROL2 a; f8 r. S# H: J7 m
,5 V; n4 x6 U! e9 `4 Y v. T/ }
系统中所产生的一种用以抗拒% U, k f+ R! C
作或限制动作的力。. t, e; R) o( y# A
头,
' n, `1 d# E+ F& g$ D$ H. T5 {用来测量飞机在空中时的总大气温度和在地面时的外* r3 ^" c0 {: |
温度。地面外界温度的测量是利用引气将外界空气吸入
8 Z0 y+ K2 \3 h) `头,以达到测量的目的。
) C9 C# S7 Y! n7 Y* I配,
/ K& {9 W; j6 x. r2 \一个完整的结构或组件的过程。$ r) f4 ?5 d: Z, d
假设温度而得的减推力,3 K$ _% }, U( M+ N: w c0 [: [& V3 x
推力设定值时,假定一个比实际外界空气温: z$ U( ~3 `( Y" G6 X0 }
空中交通管制,! @9 d' S* J% ?9 N1 K/ v
见Air Traffic Control+ ]; H1 {/ z/ w' o$ O
AREA NAVIGATION/RNAV, A method of navigation
" ?5 ^. o; g Y9 v3 z: ?: p* j/ kthat permits aircraft operations on any desired course
$ `( ~. x1 E8 } D( ^- P3 Iwithin the coverage of station-referenced navigation* p. J. b: i6 I" w" T
signals or with
$ e0 g) P a5 M7 S% ]8 gc: q: T' M2 l3 z) l; _3 ]
ARTIFICIAL FEEL, A force developed in the flight
' r7 q& c. J+ s/ i; P0 econtrol or brake sys* @3 X9 e" D; Z" [5 S: D' V5 g
m4 R: ?/ D1 h" Y0 Q1 A
A
! a: J' Y: s9 `" u+ C# N0 d. d+ ra2 {+ r, _+ v3 Q1 n2 g- R% Q9 {
m
9 ^5 `+ U3 c# X- e' {o/ }8 H5 x# ?: @
by using bleed air to draw ambient air through the
$ V) n+ k1 ]4 e% h( e1 _sensor when the airplane is not moving.4 X- M5 f& f0 u+ Y: I L* f
A1 w& ^ {2 X6 ?6 m7 R
or unit.' z0 [& M: m1 o( q8 V! {
A) {9 v: ?4 K9 Y. T) ?( j% c
lower thrust obtained by setting a higher than actual
. P( m$ M0 @$ B4 COutside Air Temperature (OAT).9 Y( q0 E6 `6 c
弧线,* t$ U2 O! ~5 S/ F
飞机在围绕DME台等距飞行时的弧形航迹。6 u6 y8 \" }% J% T$ o2 x
区域导航,9 N# h0 J- a, j: u. [
容许飞机飞行在有电台参考的导航信号或自备系统能+ M" N$ z1 n1 P7 Z. Q
力极限范围内,飞行任何预定航线的一种导航方法。1 `0 V3 l* K8 q% z, `3 N/ a& T
模拟感觉5 B7 l2 O# r' m# G
在飞行操纵系统或刹车2 i) |) K# v: B9 j# c6 J# A, N9 s
动
' M# X" p- D- p) `0 G3 _吸气式总温探: _/ I8 m; Q& u3 U; s
界
0 Z1 C; W. w( F9 h# e1 P! A ]探
+ M% e3 z" ^5 \4 `装: h8 ^ M H a% n# `& {
组合成
8 l: M3 n3 D7 B2 w2 Y# E$ `: l由
; v/ J5 _1 ^! B+ y- ]* `# Q在选择起飞
b7 X5 Z9 R) V. G! h( p, J9 z- 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! `% H F7 e7 l/ \( W
磨损和维护费用。
3 l( \! Z+ @% o7 |.# @2 p$ l! o& n
英汉对照民用航空词典B OEING, O4 a7 [ y* @6 j
TECHNICAL DICTIONARY 14
% p1 g) t. }' P( E4 f7 h3 D2 IATE, SEE - AUTOMATIC TEST EQUIPMENT! t& l* @9 G/ p- \
ATMOSPHERIC PRESSURE, Pressure of air due to the
% f( y2 I6 Q6 U! sarth's atmosphere, expressed in pounds per square
1 B# ~3 O! e) k4 dch (psi) or inches of mercury (in Hg) or millibars (mB).
5 v# z3 ]/ B3 n! ~4 UTTITUDE, The relative orientation of the airplane with1 A; m1 b. N6 b9 r0 m( M7 o& Z# S
spect to pitch, roll, and yaw.1 [# n1 Y. g. o
UDIO CONTROUSELECTOR PANEL, The panel in0 I- x: I0 ~. `% m
e airplane which controls and selects the routing of
# L: M$ ]2 X4 Q( u* D) C$ judio.
, L- A' [$ I* O" L0 ~+ @1 h8 ?. TUTOLAND, Automatic landing using the Digital Flight
5 [) I) F3 t; }; J- tontrol System.( h/ X) w$ ?. E2 Q' G4 J6 g
n.
8 V" P2 c0 @; I, Y4 u+ k: nM, A system
0 B, o# x2 x- i, q7 P$ |omposed of all necessary subsystems needed to guide
* c! G3 m2 c+ ~' W# ?e flight of an airplane.1 K0 v Y) L( G0 F
EQUIPMENT, System test# x$ p- F/ ^/ s% k: [7 T
quipment that operates under computer control.5 V9 W& K: t% Q- q" N0 }- Y
装置, |
|