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AIR DATA COMPUTER, A computer which produc; @4 W1 B4 V1 K; W7 y
data information, such as altitude and airspeed, based
1 |/ x& M0 Q1 ]% n9 \4 Oon pressure and temperature measurements.
1 D% \/ h4 M& k% {8 Pes air
9 Y2 T$ C: i$ bIR TRAFFIC CONTROL, A system comprised of" @8 N: s$ o5 c# W" L
round and airborne components used to identify, track5 [$ V$ w( `- e1 ?9 F% F: l
OUND SENSOR, An electrical device operated
1 g) n! a* ]; ?, B0 m& Sy the landing gear, which transmits on ground/in air2 I" V8 A8 R2 n! P5 B( t* }
formation for system operation in flight or on the
4 i' d( S, t6 E& [( mround.
+ q4 n' N1 H+ M2 _IRBORNE VIBRATION MONITOR, The AVM takes
- q6 b" D$ l% ]e signal from the engine mounted accelerometer and
+ c D: b; D+ U ]8 U ]alculates the vibration on that engine.- ~9 d( d2 |" w$ P2 Q- U9 N; P# @
corridor equipped with radio navigation
1 P! R; Z2 V# K1 }' gaids.
: R# z2 i% v |AIRCRAFT (or ARINC) COMMUNICATIONS
# n5 h6 @7 Z. \3 }( a" EADDRESSING AND REPORTING SYSTEM, An
, ~1 d( Y9 ~- m- C7 y7 \addressable digital data link system which permits the$ v5 h6 x( ]. w# \
exchange of data and messages between an aircraft% ]1 e/ v% d" B- V
and a ground-based operations center over a radio# K# i0 L) o& e' _% G& {! G
network.
1 m$ \, w7 B0 \% O4 R' W3 OAIRCRAFT CONDITION MONITORING SYSTEM, A% U4 @' T6 v+ Y( v' E5 J
system of sensors and recorders to monitor various
5 b e; L4 i1 h" V1 Mairplane systems' performance and status. M0 w7 |+ K) D" Y% U2 O, _0 `
机,) f# ?; n% x& E6 i% F* t
中交通管制,
! Q1 @' ^% e7 v" B% c& u一个由地面设备和机载设备组成的系统。用来对飞机进
! l. \& e! j$ [! a地传感器,
% {! d8 s/ R/ |+ n5 n4 X一个由起落架操作的电气装置。用于给空中或地面的飞+ g0 T1 ]# q2 \& S5 L
系统运作传输地面/空中信息。(有些系统只能在地面
$ j# ? E& A( A用)% D1 [' y, z2 D
载振动监测器(AVM),
% X& {" U# F7 ]8 OAVM从装在发动机上的加速器取得信号后计算出该发* s5 Y, F% r2 T: S
机上的振动。+ `) o. V& {. j% w
式建立的控制区域,内有无线电导航设备。* o. [. q& \6 p7 K
飞机通讯寻址和报告系统,7 S" B$ z0 T8 _, j5 X
有种可寻址的数据通讯系统。利用该系统可使飞机与地& u3 V+ K5 l2 K( s8 b8 p" _* n# S
面操作中心通过无线电网络进行数据和信息的交换。* x4 e- }, `3 _$ I8 ^( z t- E/ |$ h
飞机状态监控系统,( c1 L, Y, q; D/ V6 y+ T
一个利用传感器和记录仪对各种飞机系统的性能以及
# T, E9 F: s% Z状态进行监控的系统。' f% ^% o Z) j6 T
A5 E. R5 B# i# g, @0 |# E1 N
g
+ V* F( s5 E$ X" `6 ~! R& Xand locate aircraft.
4 H$ a4 [" r& _8 NAIR/GR
& _( _! c" U0 y3 T+ H5 g: _b
* O& d w) v) u( Y! Yin( x% o0 c5 Q: T* y8 F
g6 n$ b) {) [3 m& {! N, F3 f- O" [
A
7 H P( h0 Q( M7 I; c; uth
; z5 A( A( v" N; w2 F- ]$ |c
! f& \, d' J. mAIR WAY, A control area or portion thereof established$ u6 l3 p; z8 E, x4 y5 V) o u
in the form of a
. h( \) ~9 a: U# n q% m大气数据计算/ W' d% v7 R8 g: a$ }% b
根据量取压力和温度而产生大气数据资料(高度、空速
) O; z. B" K0 c$ c/ K2 x% `0 C等)的计算机。
8 T0 l' _/ X0 ^9 q( J' [! ?空8 _: t7 f: o7 I
行识别,跟踪和定位。
: C& ~$ u) @' F! ?2 v5 [: p空
* e K& N8 M, G机$ ?; X" d* q$ I' d( M4 N
使. k& G* ^, E/ }) k+ u
机
! m, z7 }- _! f" O动9 z7 @+ R3 Q! k
航线,2 S2 ]9 v+ k: l. C0 }
以走廊形- e. R- j4 M: A8 {/ ^! {
英汉对照民用航空词典B OEING; v3 T9 U5 v% ^7 `2 f4 T7 D
TECHNICAL DICTIONARY 6
& C# j" ~0 K% F& hAIRFOIL, A surface designed to obtain a useful reaction,
& ~9 ?7 R- p+ Ksuch as lift, from the air through which it moves. Wings,
/ x; J6 P7 i, K/ F* A' [2 jstabilizers and control surfaces are airfoils.) u8 W: ? \) J9 v
AIRSPEED (IDS, TDS), The speed of the airplane9 ^; v' R) ?& j- j2 ?
rough the air.) B. a2 i/ g# ?5 f$ h% v
D INDEX, An adjustable pointer on the
# Q7 w |" S- b/ L( ~+ |* }irspeed indicator.% I- {4 n- E2 A7 J8 T* H3 D
and legal ability. S8 J' {0 o) |2 D" t
fly.
! R3 P6 O# C# ~7 x( um, for example, the procedure for finding the6 @! f7 L9 K& x
quare root of a number.5 w) J5 a- m( f. s' {' {
y* n# v% [5 e2 ~9 d, J
re, wind,
1 a3 D; m$ G J1 gand aircraft flap setting.9 a; l6 A8 t# q8 q
是翼面。
9 }, G/ |" w, n9 K7 o速,
: B7 j2 y$ t5 N飞机在空气中运动的速度。, B& } w) a2 K+ p& w% A
,
: \; Y7 j( H( N0 Q+ e7 l在空速表上可以调整的指针。
; T3 s% B6 V+ |1 X机械飞行能力、和合法性的飞机状态。
" B1 ?5 b7 @) o& r一步一步的解题方法。例如,计算一个数的平方根的步2 C3 S5 ]# w7 E" \6 ]
。
3 c! X1 t! _9 X9 K' c能0 n- y# z$ A2 @! o {( T9 @
资料的法定文件。! f/ ^# h0 D) Y0 B( f
翼位置成函数关系。
$ v' u4 w" V; ^9 r' _th0 I9 M; d/ _, K3 z3 [
AIRSPEE
' n( Y/ W% O0 S, }' ua- w% e: Z Z% {. _
AIRWORTHINESS, The condition of the aircraft with) q( U; J0 M) _! n7 ^" J! h
respect to its aerodynamic, mechanical,3 [' w3 O, s" y A& a8 P9 V
to
* h3 M. g+ z9 J6 }" L' H+ V8 HALGORITHM, A step-by-step procedure for solving a1 [" m7 B1 H& n# e/ U
proble
) a% r! C2 U k7 x" K$ P% M+ P4 bs/ ?: x# i+ S/ H9 w. P, ~* I' K4 O
AIRPLANE FLIGHT MANUAL (AFM), The legal
, s9 w1 W% J8 V3 M) Fdocument containing performance and operating limits,
% T1 L4 C( C3 ]# Y' eoperating procedures, and takeoff and landing
3 |% ^8 Z( B" f3 Cperformance.- ?8 Z; U- |+ i. T6 ]9 l
AIRPORT ANALYSIS, A comprehensive set of takeoff
9 y1 M! @* w$ u8 O0 eweight limitations for a given airport runway, generall
: Z7 ?6 ~& H$ e/ x& q8 `. Rpresented as a function of airport temperatu
' G6 x: }1 |5 |7 e; h6 S翼面,
8 H' t: W% J) x8 M用以从气流中获得反作用力(如升力)的表面。机翼,; o9 q5 C, i3 b3 Z
安定面和操纵面都
: {; H$ z3 E7 i: L. q9 o" ~空
^+ E5 t; f% k+ Q f+ `4 h空速指标( e' \ S, f1 r( ?9 N% M% L
适航性,
/ G- m8 z6 z+ H9 k3 I有关气动能力、+ `" a/ x2 j1 d$ t
演算法,; [6 F# Y2 S& F% b8 v6 X
骤1 n) K2 c5 d u, `
飞机飞行手册(AFM), f8 V% m; Y5 ^, g- A5 ^* i6 E: i B
包合性能极限,操作极限,操作程序,起飞和着陆性- r1 V4 q- h c5 a7 V
等
$ {; ]* w+ J4 @* A0 ~* M机场分析,
0 D* L( x: t% s$ V# W- k0 a一套针对给定的机场跑道的详细重量限制资料。通常与
# O1 T- c; y" [机场温度、风、和飞机襟
4 k" X: [: F/ ~$ H6 v英汉对照民用航空词典B OEING
7 G: l, q* d% p$ OTECHNICAL DICTIONARY 74 J7 ]5 E- h7 ]* u# w
AIRSPEED BUGS, Adjustable pointers on the airspeed
2 S6 d! X0 X3 s4 \ Bindicator.# D, U. Y- C% E8 v1 s0 b7 ~
ALLOY, A mixture of a basic metal and small amounts
% t" {" U+ ]2 I8 H, ?# y' ef other metals to change the properties of the basic
" _3 `0 R1 r/ n( W& Jetal., x: A. C7 a( }/ k
Minimum airplane speed.
$ Y! O6 K. [8 e+ O0 G% V% X3 e4 a# @e of
8 [, D. N4 q$ c; c. N) s; Y gitting airplane angle relative to! z. h5 J& k' g! R5 G7 [5 v
irstream for the stall warning system.
; G5 p" }6 P7 P! a* R4 b- Kanother.
- f6 w/ L: G( p, V: H% M' F; g! dLTERNATE , An additional airport selected during
3 h5 x! P' D4 P5 J& _+ V,5 X: i' \! Y2 T5 Q/ b
合金,* e; k( V/ W, K {2 y0 ~/ Z) t. M
在金属中加人少量其他金属,而改变其性质的一种金属2 B4 `& n# i |9 g( d4 V8 ?5 ]
合物。
Y" q5 o/ [0 b& n% `# {5 ^4 g飞机的最小速度。) ?, n6 m* n. n6 y+ h9 O
速警告系统传输飞机对& l$ N& |6 [0 C6 ~
流的相对角度。" r: j- m7 W( y( e
由一个状况改换到另一个。5 ~: S6 i$ F- \; ^, p
降场,3 Y$ |7 Y9 O: Y5 M8 r! ]: ]
划时,除了目标机场之外,所选的另一个机% s# e& o w7 \! x1 P
o
( {1 z* V; B6 x6 N+ zm
8 H# A; e8 k* x, kALPHA SPEED,. q8 f2 j7 I( N5 b. A. h& C
ALPHA VANE, A small moveable airfoil on the sid
! D3 g7 x- v3 E: S! n V; U7 Rthe fuselage transm
W$ q- G: h( k1 K1 ha
3 X0 ?# k: ]/ U# f9 zALTERNATE, To change from one condition to$ s, Y9 h6 D* k% ^
A5 h6 t7 z7 ~( j! f: e; Q9 \
flight planning, usually near the destination airport, to be
4 x: g( h& r) d' `! x) k' v: cused when it is desirable to divert from the original* U; W# v2 V3 t' x1 U9 v# P
destination airport.& {+ k; F8 F) g) S
空速游标' ^2 L' x3 s3 E& R2 @
空速表上的可调指标。/ x) \: i. t+ L9 q- U6 H
混
2 n9 b. |1 P0 ^# |9 C迎角速度,' o W/ M" b' E. D4 P
迎角叶片,9 k( n6 z5 Q' K7 K$ n8 {/ a
位于机身侧的可动小翼面。为失
R- W2 x9 i( W+ N e: T气2 m0 M& f `5 D2 F
交替,+ Z- a3 k* y0 j& |2 v `7 _. ?
备( f& a, ]! `, ^
制订飞行计
8 F+ S6 U8 T2 j场。通常在目标机场附近,以备不去目标机场时,改降之
" V% {% ^8 u4 ]5 @3 H用。
3 s- }5 x* }( H0 h) N9 b+ }* h% P英汉对照民用航空词典B OEING
! t5 c2 \; v& CTECHNICAL DICTIONARY 8: {3 V& [3 Z& f6 t5 C
ALTERNATE AERODROME, An aerodrome to which7 H3 @7 n2 N/ e; j/ G) g( i8 G
an aircraft may proceed when it becomes either
2 C7 ?0 y5 y+ M' ~7 K0 tpossible or inadvisable to proceed to or land at the. i& M' Q) h& K$ [. k6 d
erodrome of intended landing.3 d. J8 r4 c; d3 B: v. A
TER SETTING, The adjustment of the altimeter: V& Q [5 y' W0 {& O7 ~& i. h# K# w
account for local variations in atmospheric pressure.
9 v# e) S; C+ r& cLTITUDE ACQUIRE, A digital flight control system
; ^# A { a0 V' Qode to transition from climb (or descend) to level flight.) L0 ?/ i' P% [4 W
LTITUDE ALERT, A flight deck alert occuring when the+ f- D& C# W7 R* {" ?
irplane approaches or departs a selected altitude.
7 c5 c/ i' x6 I. ?LTITUDE CAPABILITY, The maximum altitude at
* v4 D! l; Z; M& B9 [! i5 v- _hich the airplane can be flown at for a given thrust,
. h0 g! Y8 N- Speed and atmosphere condition.
2 P3 b9 J% i/ R) uLTITUDE HOLD (ALT HOLD), A mode of the autopilot
* p [6 U& i6 u2 j2 ^, h+ Ar flight director to maintain a selected altitude.( N O! H+ l5 N5 n
irplane's altitude during VNAV operation.* @& e' S. g3 s4 W7 d6 o0 X& g
机场着陆时,可作着陆使用的8 m. V8 V% D# k% U% d- ?
场。. J1 v8 g9 Q8 S) f0 ?6 s+ G
," ?0 y. D* _9 R% A% O, N+ ~
根据当地大气压力变化而对高度表所做的调整。
$ g3 k+ _1 ]) n4 k一种数字式飞行操纵系统,从爬升(或下降)改平的模
) |# g# w2 _" E。
' \7 X( E+ D. d; g, V1 I. E0 i度警告,
# _! o* P7 h* n; x. E0 `当飞机接近或偏离选定高度时,所出现的驾驶舱警告。, _ k8 ^ z8 u3 Y3 u" ?6 E- ~
高度能力,/ n1 y( m- V9 b1 @
在给定的推力,速度和大气状况下,飞机能飞达的最大
v3 U, p0 s; ]1 Z2 ?" C/ K9 m) q2 F高度。. x1 t' B0 H; `. B
高度保持(ALT HOLD),
) V# g0 Q! @, F$ a% R0 B& ]! `自动驾驶仪或飞行指引仪保持在选定高度的一种方式。+ E/ ~ L; z7 \9 h" M. q/ c
,' W3 a. E4 K. C, J/ Y
员对飞行高度的控制。
- w# q' l& c Y; g4 m) g& sim
* G8 c; h7 G! P/ x; _a
5 T) J- ~( A) }3 `ALTIME
; e7 q/ @$ g1 }0 S" N% wto$ ]* _9 u, j% i7 V2 w" D
A9 h. h) ~1 D! d
m
/ |0 ^9 k- V' C: }8 E; z" O7 OA o8 S: e; _0 I* T/ S5 R
a( s% e1 U% G. m% |; R
A( v% {8 q. T# y, P1 |* R! e
w; P: I( I, ^1 }
s
- i7 b. s0 A4 A& S! U- B6 gA0 e. @, m. x b
o: Y4 \. `2 R; v- c
ALTITUDE INTERVENTION, Pilot control of the
* p g2 S/ u0 v7 R0 x' f% sa
6 D( _, F( ]1 |8 N2 SAMBIENT, The surrounding atmosphere.
0 e+ e# h ]8 h) S, R备用机场,
- N# T7 W" y+ _0 z+ ]; L/ O当不可能或不适宜在预选
; B$ ^9 ]. n2 r1 K- D机2 x2 |: C' K/ L$ h
高度表设定* Q# X1 l2 `1 s2 A) f( b1 p& m
高度截获,1 F) ^+ I/ l9 }! {2 R
式
& r% G- C, J2 p& Q4 S# }- @高' X% A$ R J9 K. O/ q
高度干预
/ u8 R) ^3 Z- t; O在垂直导航工作过程中,飞行
4 z% Z. M( `5 @周围环境(地面气层),/ D' v! X6 Y- W2 ]/ n, j
物体周围的环境(特别指大气)。
' [% S. c J, j4 [) N4 F英汉对照民用航空词典B OEING/ c# a2 ~3 V7 \: k/ L# C
TECHNICAL DICTIONARY 96 j2 C+ d [# X) ^
AMBIENT PRESSURE, Pressure of air surrounding an X/ e$ y1 d4 m- W; z7 H
object, measured in pounds per square inch (psi) .
1 t4 f% {# E2 C/ ~% H' o( z6 ?MBIENT TEMPERATURE, Temperature of air, |* @- o9 [$ Y2 ]- W9 ]
mpere., S4 z8 f( a) o4 u( [. G+ z
urrent waveform.1 C( P+ C. ~3 R0 }& ?
g an' {, U6 Y( N( C E: `& q
nalog signal to a digital signal.& z/ g1 x: r8 b; e& ^0 Y+ `
ore inputs: ~; m; `( T* [) G
f binary digital information and one output. The output
& Q3 q1 I& K r; |/ p1 only when all of the inputs are 1. The output is 0; G. f' j- v* {
hen any one or more inputs are 0.
' O$ ^; U& k) S+ ]8 t* d! p面气压),
6 R F/ @0 W/ _境温度,5 J6 \7 b) F8 I3 @
气温度,用摄氏度(°C)或华氏(°F)来
0 `0 O3 k& z. R& k3 Q# z。
& v! `6 N1 o5 T9 r b3 G' |, v电压或电流波形的幅度。
' T( }3 q8 v' n性变化的信号来工作,或产生连续性变化的信号
& P+ ^: E; Y/ }! y! h6 c1 r统。
9 r7 }/ V7 P' s: h% o3 E将模拟式信号,转换成数值式。( K- I/ G! g3 @/ z* [
一种有两个或两个以上的二进位数字信息输人,一个输
7 _$ ?% k3 `5 ^7 o9 T6 r( x的装置或电路。当所有输人为1,输出为1。当任何一个
1 \( w. B2 x* Q: o* E一个以上的输人为0时,输出为0。
1 K2 c; m) \1 n' ~+ |A
6 q7 {, u; a' p5 [4 P' n' usurrounding an object, measured in degrees Celsius
2 q: \2 U K0 u* r5 ](°C)or degrees Fahrenheit (°F).
7 v& t6 }# S9 e& K8 uAMPERE, A unit of electrical current. One volt across
' x2 v' m% q+ \one ohm of resistance causes current flow of one
$ B. p+ d+ ?, F. x/ G G$ ka
& z. h& ] l( T, B& p% }+ |AMPLITUDE, The size or magnitude of a voltage or$ ~0 m) B. m$ A
c
; `" h0 d% L) aANALOG, Quantities or representations that are
2 F g: R& I- ^9 G6 w% Ovariable over a continuous range.+ J ?( u5 O# h0 U$ L
ANALOG-TO-DIGITAL, The process of convertin; M4 V) L5 W* g, y0 K
a
7 a K- ~, s# D! Q: C. E1 r$ q5 \AND GATE, A device or circuit with two or m
4 Q1 L; c! h) i) D, ?o
* ], b9 h2 G0 W+ w3 N) fis5 n; Q' ]4 P7 X. Q
w
2 v' T- v$ x' R环境压力(地- E4 \% ?, ]: b. p2 L
物体周围的空气压力,用每平方英寸多少磅(psi)来
' ^9 s7 v ~ R2 y度量。! i4 ~: S) ^5 E
环
& T+ W4 x% u+ M; V物体周围的空- \7 l7 o; _, L. D9 Y8 A& u
度量。
C1 k3 y1 `0 [( ^1 K安培,& l! I( O( H0 T! a
电流的单位。6 O7 u8 Z* p& ~$ ~% f; E
1伏电压在1欧姆的电阻上所产生的电流为
$ x" x% Q. a2 L- J1安培2 p P5 |& |# Q1 e* M) {
振幅,
8 K, u% T+ y0 @0 X9 C; @模拟式,, l, o7 F5 ^6 U+ s% B+ d
用连续
4 b' o% v: d$ p- l4 N3 O/ R O系& ^: W0 ?, \- i7 i
从模拟式到数字式,
+ `$ [! c( N8 t! A4 B与门,8 Z2 z9 |) m; X1 i3 x/ N
出
8 x5 M9 H: V" L' y- C% J, s b& M或0 i+ V9 r7 }0 U& @
英汉对照民用航空词典B OEING
# U( H! ]7 h+ ]( ?8 x" n* d2 v2 f$ aTECHNICAL DICTIONARY 10' W$ H; X# Y" L S. u0 S
ANEROID, A sealed flexible device containing air at low$ O7 I; d4 U7 Y6 }
pressure, which expands or contracts during change of
, y: \/ L# L8 h6 e6 S# T) Pressure outside the device.) C# U. W+ q) S2 d$ J3 K
ically
% b3 `8 M4 v7 ?# gr changing the direction
7 q4 r2 s n4 ~( P9 T' ?9 {f drive.: C3 ?: c4 i% y. ^4 I! W
of the wing chord in
$ F- M5 a9 Z, K/ Y5 v( u klation to the free stream airflow as it moves forward
/ b$ p, N: F8 K3 F* R8 G+ trough the air.
; P% R) `$ Z7 I+ m, _al axis of the
: a& J, k% t; Paircraft.
! I# i0 g% q6 y( `+ B( E- n5 M8 T胀或收缩。& |5 E, S/ D* h% h! Y
箱。是改变驱动方向的机械装置。% Z. z$ ?" t2 U& O
机翼翼弦在空气中向前运动时与自由气流之间的夹角。# Z* H( M8 N. N# I# B9 t- L
。
9 m+ ?/ J8 ]7 n9 N0 w$ qp7 f1 s7 p+ v% q- f
ANGLE GEARBOX, A part of an engine, mechan, l) A4 X; s9 U
driven by the compressor, which drives the accessory
+ B4 E. o. [# j7 X* A& Z" o) J: w) Qgearbox. A mechanical device fo
4 S |0 M5 p/ v1 fo
6 {8 K7 F. P. y+ i. yANGLE OF ATTACK, The angle% n6 R4 v+ l9 o( ` |5 W
re& S r% }: h# d8 Z: A: @/ u
th+ _' G" \1 E6 N5 `
ANGLE OF INCIDENCE, The acute angle which the
( y1 b8 g- _4 Z7 {8 z/ Swing chord makes with the longitudin
! T& K6 r" E" p- k- J膜盒," N- z, b$ {5 @& @! |" e$ _8 ~
内含低压空气的密封弹性装置。当它周围的压力变化
# v6 _# _9 M: T6 ^时,会膨4 a: I6 Z2 o6 l) e# q b8 w
伞齿轮箱,7 A: O- U% G/ `/ Q* }: z. a$ p
发动机的一部分。被压气机以机械方式驱动,然后驱动
7 M; x2 {7 H- U }$ [( I附件齿轮
7 D7 {+ h- x6 P0 T2 P& y1 d' x迎角,1 S* Z0 R9 z0 y$ b
安装角,8 {& @. s( J3 S- A; G0 b
飞机的纵轴与机翼弦线所形成的锐角
$ ]- W& |+ ?) \5 C/ k% A, [英汉对照民用航空词典B OEING2 Z# V+ G; R2 e$ l7 d: P- J7 r
TECHNICAL DICTIONARY 11( Z- ~0 ^0 |, ~
ANNUNCIATIONS, Audio or visual indications used to
0 p) C% C) j$ }6 I @0 j+ jcall attention to an event that has taken place.4 K* U$ m# d, W) [
ANNUNCIATOR, A visual device consisting of a number
7 B6 a9 C, \5 n: I: \ly./ N" C6 X7 P2 E
ANODE, The element toward which the principal stream/ y6 Y% J% u$ q! N8 B) J" X
of electrons flows.5 a! B* D9 B$ |; T& h) G) j
ANOMALY, Not normal.8 C. a6 e# e& c" C
ANTENNA, A device which, used in conjunction with a
; j! [: N0 h& D9 Stransmitter or receiver, is used for radiating or receiving6 A" z# N! F8 c" X. p6 I
radio waves.
& u6 a; P3 `: sNTI-ICING, A method of preventing ice formation on
3 `+ k( d1 w" h3 e; [ we wing leading edges and engine nacelles.1 y+ ~ B5 h+ ~/ y. s" m" A
NTI-SKID, A system for providing maximum braking2 C* n+ J8 n) }7 E; l1 F
ithout skidding for any runway condition. Anti-skid, w' \. d; V' W& ]7 ^$ a
omponents are part of the brake system.2 X1 ]2 v# g' C6 q7 N
告,
+ [* C' e# v, G8 |( c当发生事件时,以声音或目视指示形成的提示信号。
/ B; q2 u, e- W8 W6 f2 U与之有关的电路的现有情况或已存在的9 Y" x! I6 Z0 o+ L6 W
况5 y* \2 g" s- S- Y7 S( A8 B
正极,; v- ^) i6 h1 J4 f& E
主电子流向的极位。' @) @; f+ j- a9 [) j! k: u
异常,1 q. c( N$ p) D- `( C' r
不正常。1 a* A6 V$ ?) K& t" h& b- ^) k
天线,
* B$ l" Z2 f6 `5 n一种与发射机或接收机共同工作来发射或接收无线电$ K9 F# Q& p' T) z: m1 T0 v
波的装置。
3 u$ w4 f: W$ ?( f5 B冰,& u' ^! c5 ]9 l
防滑系统,3 W3 ^4 e* q( v+ E+ G' c5 k
一种在任何跑道状况下,都能提供最大的刹车能力而不
- L, C; b0 F" b使轮胎打滑的系统。防滑部件是刹车系统的一部分。
9 b; z( A- c1 [: _1 R f: ]of lights. Each light indicates the condition which exists5 \- N. D6 k4 [* o& {% ?/ }+ J% l q
or has existed in an associated circuit and is labeled! \5 X$ L8 l) D; Z, `+ E. ?3 d b
according( i7 x- H5 @/ G
A# n: {5 d: D( M- ~
th
/ @. z3 n% O5 R: F! @. S5 RA
+ {% |- l0 x8 C7 a( G4 Dw
8 |( }* u: E2 n9 ?2 `/ R Cc
! X& ~. V- |( ^; u5 Y$ n通
! I! k6 _1 Q5 i: a& J5 e3 [, A) ~信号牌,
# w4 D4 A% m0 D& ^由一系列指示灯组成的目视装置。每个指示灯都有相应 `2 M1 h1 ~. F5 `: A/ b3 X
的标记,用来显示
% y+ }6 \0 z$ r6 O( T1 d* M( E情
& y" N. I7 Q8 B$ ^9 {+ ?防2 O( O( t3 O. X; q
防止机翼前沿和发动机短舱结冰的一种方法。, [/ i( P8 B7 T/ h2 D0 V) J1 @8 P
英汉对照民用航空词典B OEING
7 C2 V/ E6 g2 c$ NTECHNICAL DICTIONARY 12
. b; z' I( n8 \/ uAPPENDIX, A supplement to the Airplane Flight Manual
3 m; \) X5 K1 u) Y& l2 |tained in the basic manual. A
$ v. ]% J1 o3 L6 N" q! Nollection of supplementary material at the end of a
{& ?7 A+ U9 \3 N, v1 Dook." M5 S8 ]) ?# \) u- K. K
of the. d* E3 G k2 g( D& V6 w
rsion link on the landing gear.- z" k, i- V+ M) V6 q/ k+ p8 |) ^
APPROACH MODE, An autopilot/flight director mode
* |1 r3 N- T. Uwhich is a combination of localizer for roll control and: v, X' w5 `( r: z2 _: n" X- w
glide slope for pitch control. This mode is used when full; ^. j- r \- ?% O; E. M
instrument landing system is available.
+ d9 T0 J- Z; A- Z) cAPU, SEE - AUXILIARY POWER UNIT
' R/ n% J8 f6 {" YARINC, SEE - AERONAUTICAL RADIO
; k3 Z" m* a# c6 BINCORPORATED2 O* _( O6 g0 S3 C, X# `
ARM, To make ready for operation., U% V0 s9 }- R6 ~, m* R
附录,0 B. k* X; V) e$ V Z5 n3 b6 [' c, V
飞机飞行手册的附件,包含基本手册中未提到的飞机形. J2 q. B: ~& J1 _8 }
态的其他性能。是附在手册末的补充材料。
/ a4 m% w/ w; T顶销,* u+ {# \* W0 {+ \3 v7 O
用于连接起落架扭力臂两部份的销子。
$ f1 v% g3 O- t3 x" M进近方式,* s( }7 ~8 [6 B
一种综合了控制横侧的航道信号和控制俯仰下滑信号7 E8 m. @1 U J) \! O: D
的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系
& w' A! ], i$ q( Z \统正常时才使用。( W- ]4 Y7 {0 X* q% [
辅助动力装置,7 j m" E& h0 U' d
见Auxiliary Power Unit
+ U9 X4 J) `1 t% b+ w, wcontaining additional performance for aircraft/ G8 q4 m' w7 g N6 U! b
configurations not con1 z: g( @3 F' s: R8 A' S
c* M- l. U: z( C1 Q. x2 y2 u9 w4 `
b2 P4 q* l4 X; l) S4 g3 c
APEX PIN, A pin for joining the two sections7 A1 q. ?* b9 R- t/ B5 X$ z
to
) C. a9 v, W4 K# |.
, j) i* A+ ?1 I航空无线电公司,- m6 }! ?, E& X& J$ ~5 k# u6 l
见Aeronautical Radio Incorporated.
8 M7 Y; o, ]% `9 `& P1 {3 }* [3 n9 S预位,
: D; c4 j2 |2 G3 P, N$ s& W8 b$ n部件可以开始工作的状态。4 {3 q1 A* `* q% M9 i8 l
英汉对照民用航空词典B OEING2 T* Z8 p d2 s/ ~5 m+ h
TECHNICAL DICTIONARY 13; b: ~; o9 I [
ARC, The curved track over the ground of an aircraft9 }3 |& n5 c/ g. E0 q6 p2 a
flying at a constant distance from a measuring
" }) ?) B6 B% q- }equipment (DME).; R% O' D# R1 \* m* v1 F
in the limits of self-contained system; L9 i( Q8 l2 T: Y
apability. J" V2 J$ e8 L7 f
tem for opposing or restricting8 N! S# J2 q: ^/ Y; s! }
ovement.% k; K6 G, N7 ?; ^; Q
SPIRATED TAT PROBE, A sensor that measures total* v: F2 V: w. M9 Z8 G! c$ G
ir temperature when the airplane is in the air and that ~' W/ F$ i+ J- Y1 ~$ H
easures outside air temperature when the airplane is
$ t& D1 }0 m* `8 k" {n the ground. The outside air temperature is measured& v W! l' Y. h- U/ ~0 n+ N4 G
SSEMBLY, The fitting together of a complete structure) a- N3 J# P) t8 z K) A" h# d
SSUMED TEMPERATURE REDUCED THRUST, The
& _3 E" Y8 E& U/ P' h DATC, SEE - AIR TRAFFIC CONTROL
8 I9 X* O3 O },- j' ^$ R1 `- t$ o7 S
系统中所产生的一种用以抗拒
9 d: f; H+ o6 N z0 h作或限制动作的力。
. _ \) y3 ]: K. b& `头, @) g- n: d0 \
用来测量飞机在空中时的总大气温度和在地面时的外
) J% g% T! Z9 F. T- |% G温度。地面外界温度的测量是利用引气将外界空气吸入
0 S! a/ i: D- b# @头,以达到测量的目的。2 X1 P, p' ?9 E) {; x3 x
配,
. ^5 [6 D7 p. r& z. e$ M' w9 n. B一个完整的结构或组件的过程。
! j8 E6 Y- f% I+ P0 a% O假设温度而得的减推力,
9 @& r+ q; \( u _4 K$ Y推力设定值时,假定一个比实际外界空气温6 s+ _& m' d4 g7 K, c
空中交通管制," Z- Z% z& n3 \3 F! V4 ^! L/ }
见Air Traffic Control
1 }3 \. y" U$ u+ tAREA NAVIGATION/RNAV, A method of navigation
( G2 ^: }: h5 E0 \2 N0 Lthat permits aircraft operations on any desired course
`9 F6 T* R8 A7 pwithin the coverage of station-referenced navigation% p' I4 ^2 g& q1 j6 K( t
signals or with. y! c% X. e* c" o, Y" \( G7 K. m
c
9 }5 d2 j7 ]" y3 i7 iARTIFICIAL FEEL, A force developed in the flight5 A D' V8 S7 q7 j1 f+ w- `& r
control or brake sys v/ I( E; O% |1 t5 |
m
/ h, j% E% o# N( m: XA1 S( ?. S1 \/ _2 Q- K ]) g
a0 U, f( t7 |: {; S% S- N, ]
m
2 K/ t- K) ^0 p1 [* ^o! [0 E9 b9 V1 ?
by using bleed air to draw ambient air through the
8 n) C8 e+ Z" R" V/ d( d5 i6 d _sensor when the airplane is not moving.
% x/ e5 S* a( K6 y/ a4 r: y& ?A5 [0 p2 y0 X3 ~
or unit.
( D0 P' o% |. DA( w2 h1 p& X" D, P8 E3 C1 ~
lower thrust obtained by setting a higher than actual
- z' X; v1 k5 L" P$ xOutside Air Temperature (OAT)." ]8 L$ x+ J6 A* L
弧线,. S6 |% W4 j' |
飞机在围绕DME台等距飞行时的弧形航迹。" z3 |0 A8 | j7 D1 [) [& ?
区域导航,# c. h. i$ E" r1 n$ H0 X3 [
容许飞机飞行在有电台参考的导航信号或自备系统能- o" }7 M4 Y" `! ~3 Y2 G3 \
力极限范围内,飞行任何预定航线的一种导航方法。, }8 \# ~3 V2 y/ c5 s
模拟感觉
, a$ F6 }2 k/ _. h在飞行操纵系统或刹车
( a- T! i9 U( c7 r C动# g: ~4 Q4 M6 D1 E: A
吸气式总温探. S2 X- [1 n% U" e" H
界
; ~4 U7 |+ d# V* W9 c探# q. _; ~/ n0 G ^ ]4 x
装
7 D& c9 v2 k, ]组合成
! t- D" a5 ?8 y/ t# g由
* G, i& A% f, F在选择起飞
- ?/ B' S" `. Y/ P度高的温度而得到的推力。用这种方法可以减少发动机的
2 U' J0 i+ [3 ^' _( p7 I( z0 m磨损和维护费用。
# a |/ ?1 z" n5 V% A- G.3 l0 t2 |$ X% j) Y9 [
英汉对照民用航空词典B OEING0 Y6 ]% O6 g3 ~* s! i+ \$ w) S3 I. g
TECHNICAL DICTIONARY 146 d; Q$ B5 U1 m, d N% |# o( n
ATE, SEE - AUTOMATIC TEST EQUIPMENT; {' I" m$ @, J5 h+ n: W: `
ATMOSPHERIC PRESSURE, Pressure of air due to the1 e. R* _) @$ E7 y# S
arth's atmosphere, expressed in pounds per square+ H# |6 N' _) F% G. n3 t% [
ch (psi) or inches of mercury (in Hg) or millibars (mB).
1 w! e. T3 W p# @* V- YTTITUDE, The relative orientation of the airplane with
# ~. |) R; ?. Q \+ E$ T- G6 t# Gspect to pitch, roll, and yaw.' E" Z. g, }. ?4 I1 w
UDIO CONTROUSELECTOR PANEL, The panel in
7 j+ `; Y4 k; C8 V8 pe airplane which controls and selects the routing of
( z) N0 {* p6 ~% E& P* Q6 M& pudio.
4 S0 g0 ?* i$ \/ F8 A: I: J2 @" SUTOLAND, Automatic landing using the Digital Flight* w3 u! }9 ], b3 l p0 \: @6 j
ontrol System.9 `6 _1 c8 w4 A2 V
n.
- ?# Y$ _9 k5 [# @M, A system w0 @+ c; p) e0 O* r0 k, Q8 h
omposed of all necessary subsystems needed to guide7 K" S/ H, r. K: w. k
e flight of an airplane.
: a2 X* J8 K$ q' Q% Z% P+ [EQUIPMENT, System test* K6 a; s7 B/ x! y6 S
quipment that operates under computer control.8 J. E& W; y' m6 @( B
装置, |
|