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AIR DATA COMPUTER, A computer which produc) u5 Q: o9 y) Z
data information, such as altitude and airspeed, based
9 h! d* Z, F/ l& P* ~" Lon pressure and temperature measurements.
2 H Z2 j3 D/ a6 ees air
- c9 D+ t" f5 N% w7 R5 m( @8 J9 }# k! |IR TRAFFIC CONTROL, A system comprised of& D m% H) ~% [+ q# D
round and airborne components used to identify, track
* u6 a# u9 Z5 S. d" P5 q, wOUND SENSOR, An electrical device operated
) d, U3 c* A1 A' Z! M% [6 _6 Wy the landing gear, which transmits on ground/in air
, p! m+ t; t8 N3 z% q: bformation for system operation in flight or on the Q# c- P/ S' P. K: t+ k& }
round.8 _: @* w6 ]" ?, y: e
IRBORNE VIBRATION MONITOR, The AVM takes1 x$ u+ c5 N4 E4 }; N. u& C/ q
e signal from the engine mounted accelerometer and
( }: e3 {" {8 p malculates the vibration on that engine.
! ?- B& [, l4 F: ?) @corridor equipped with radio navigation* r4 Y; o! C1 L8 }' z3 K9 P# Z* o
aids.* P$ T& I2 G- v& Y8 w/ J
AIRCRAFT (or ARINC) COMMUNICATIONS$ H: S. N. `. l+ s/ L1 h+ l
ADDRESSING AND REPORTING SYSTEM, An9 G7 z9 E r1 Q) M1 E, H7 U2 j7 @
addressable digital data link system which permits the
2 Q# R; }* H( t% Q( N3 U5 |exchange of data and messages between an aircraft& |& j) y5 [- ?" G
and a ground-based operations center over a radio
' e8 q, ?2 y: A% Y, L/ Znetwork.
9 j4 H. T' C) XAIRCRAFT CONDITION MONITORING SYSTEM, A* ^# s9 f- O" @* b
system of sensors and recorders to monitor various5 q: M: T/ t8 r" A: I
airplane systems' performance and status.% I0 t- D5 J3 N3 w! I
机,& O% U3 Q k, F& Z/ {
中交通管制,7 Y/ u" w' Y X6 }" L e
一个由地面设备和机载设备组成的系统。用来对飞机进
8 M$ Q7 B7 I1 x/ c/ C1 |地传感器,
& n G$ m% G& G0 x一个由起落架操作的电气装置。用于给空中或地面的飞% ~% P7 ^, W# A# [
系统运作传输地面/空中信息。(有些系统只能在地面+ E0 K1 S: S/ G% J; U& d
用)
& E5 g5 \9 E; i& A1 z3 v; ], B载振动监测器(AVM),
, s5 h% N0 p% A R j) mAVM从装在发动机上的加速器取得信号后计算出该发) _& ]7 [+ i. h, L% [
机上的振动。
5 I3 y1 P' h2 t5 `" d7 Y- ~% e a( N式建立的控制区域,内有无线电导航设备。6 ~$ Y- C3 u( {) v" s
飞机通讯寻址和报告系统,+ @! l! d$ e' S7 g+ | N- f
有种可寻址的数据通讯系统。利用该系统可使飞机与地, l' `( y8 A2 O" V2 T# D
面操作中心通过无线电网络进行数据和信息的交换。
" k/ ?7 w/ C8 o0 P0 ~8 m% J飞机状态监控系统,
6 g0 `0 q5 `8 Y9 J3 N2 \4 ^" P9 L一个利用传感器和记录仪对各种飞机系统的性能以及
; P0 p6 l8 _. c) }状态进行监控的系统。
( Q# E! C3 y; `& U9 FA, d8 ?0 v. k9 D& v& j/ V8 P3 R
g
. \ K: ~# f2 E: t( Gand locate aircraft.
1 x2 e) d6 L# k6 FAIR/GR
, _4 B" ^3 x% l5 d Db; o g \& d; f: e5 Y
in
# y+ P% n( `1 d: R6 w; a+ `g
3 T/ g9 K7 `* Z R. F0 C2 PA
% u% N0 R {, \3 H0 u, ~th
* [4 X P% W5 T3 U3 Q. A. @c2 k( l4 l+ L s0 `: o) q
AIR WAY, A control area or portion thereof established
9 z4 C8 h. a Qin the form of a
' l% U: o; x% E2 d" x3 l5 U大气数据计算/ s: ]6 c g# a4 I3 r6 H: W
根据量取压力和温度而产生大气数据资料(高度、空速
1 r& K; b& ]# G ^# [等)的计算机。
9 O) r% b; Z1 Z! A0 t0 Q空
( u1 ]6 X$ D: |6 b6 n1 v, D7 r8 W行识别,跟踪和定位。
3 I. `: F$ U+ v; m2 D6 E7 R: k* g空
4 @! Z4 u) c3 J$ i机: a: F9 k/ P& ^! D7 H
使
- o( J8 d( |& d0 {) X {0 B% ]/ N机- @+ h! n. C" ?5 a# w
动+ u! e) S$ s* d- t
航线,
) N( u" C; q n以走廊形
# \! q: j) M8 n! o+ Z英汉对照民用航空词典B OEING
0 y; D ]) |. W L7 ZTECHNICAL DICTIONARY 6: U' n' Z! e, Z
AIRFOIL, A surface designed to obtain a useful reaction,3 g0 X) \2 D& h
such as lift, from the air through which it moves. Wings,* W" P7 T# H$ m" A# a- i% W
stabilizers and control surfaces are airfoils.
6 V% d! E5 n: W* G! n3 i# OAIRSPEED (IDS, TDS), The speed of the airplane
. ]0 J3 i2 K* x# B5 m5 a# ^3 zrough the air.! h) e4 v$ \+ D7 I1 h
D INDEX, An adjustable pointer on the
+ F$ @/ O/ f1 M1 i( ?$ r# C' N2 virspeed indicator.# l) A* A$ h% k' o
and legal ability
, e( y! q' [0 d9 F" T3 W: i3 j; gfly.
9 J* t# `7 S4 x* \5 Dm, for example, the procedure for finding the/ H6 _8 L2 G6 D6 `: G8 F& F1 D
quare root of a number.
$ R8 r- j1 W3 r \4 jy
4 e0 k: m5 O) B/ @re, wind,' O6 Z: d/ ?$ b! z7 k
and aircraft flap setting.
4 h& g; C) \* y3 m: }. u是翼面。" Q0 o* ?8 Z( [6 _
速,
, I6 ~! I0 B" B2 Q飞机在空气中运动的速度。
6 L) a M, P4 U$ M# C) S" q2 ^+ J,3 F0 _$ C' W; @( x9 H
在空速表上可以调整的指针。+ U0 y5 T8 d/ O( s9 a
机械飞行能力、和合法性的飞机状态。8 u' ]* L& L9 ~; h! O! z* G
一步一步的解题方法。例如,计算一个数的平方根的步
, a$ X* f' W- n; j' b) Q0 c。
( ]' }3 j. ]. h7 @9 d6 h% e3 z能. X6 f% v" F& }
资料的法定文件。( v4 I! `% ~% G/ o# K
翼位置成函数关系。6 T4 d' B2 c+ Q8 p9 U( ~5 L2 F
th* Z& P% r& F& H. X9 s2 Q) U
AIRSPEE
) T: |* U2 ^, F" F" E* k. ^7 ya
5 g; W% C( z3 t. o/ w1 pAIRWORTHINESS, The condition of the aircraft with4 }5 s; y( X0 e2 y, e( a; _/ [; E
respect to its aerodynamic, mechanical,3 U5 s; d2 e) m3 f7 {
to* l3 z* a( M5 J6 n
ALGORITHM, A step-by-step procedure for solving a( a6 X2 T6 l% }5 Y9 o a, P* A8 U
proble% z" Y' t% D" {2 o
s
5 m7 ^7 U( S1 z) l( N+ J1 L1 l' s9 aAIRPLANE FLIGHT MANUAL (AFM), The legal
: \ E' i! K: s8 @/ Pdocument containing performance and operating limits,
) g$ D A w& a; m/ coperating procedures, and takeoff and landing8 E- Q- l1 l1 d' Q- I
performance." R- Q* F7 `: i' D {( v5 T7 J
AIRPORT ANALYSIS, A comprehensive set of takeoff
5 x' T) M$ K+ _- b! Fweight limitations for a given airport runway, generall
3 `* c3 F/ A& t) m2 F; Mpresented as a function of airport temperatu
0 y: V& |- O. o) d5 c翼面,: ^% }+ x4 X7 S+ N& S
用以从气流中获得反作用力(如升力)的表面。机翼,
5 g: [# l( G7 [& q3 R安定面和操纵面都6 N, c# g) A; C/ ]/ r$ Y
空
# B- o) W6 M) p7 k" |3 v" D空速指标
2 y8 {* |$ M4 R: C8 t6 V# q d, z适航性,
# Y- H* p& K; O有关气动能力、
3 N1 t& R6 L1 d% H$ q" a演算法,6 B& _" N) K8 ?. e
骤
+ F, _9 `! x" M8 U/ t# U飞机飞行手册(AFM),- D W8 B( w% E6 Y, r& q2 X
包合性能极限,操作极限,操作程序,起飞和着陆性) J, f% R! ]; p1 m2 R0 h( C
等
# H/ `' @2 B& {; l) ^机场分析,/ C; `! Z3 F) W0 ]* X0 m; ]
一套针对给定的机场跑道的详细重量限制资料。通常与7 E ?: q1 t' a, R. S2 e
机场温度、风、和飞机襟
G) ]( z9 S' U' O% ]; b; a英汉对照民用航空词典B OEING' P# X8 a$ \8 J* ^
TECHNICAL DICTIONARY 7
5 x+ D- Q" k% R; y# m- ~) g" c/ p NAIRSPEED BUGS, Adjustable pointers on the airspeed$ l* }+ ^ ?( N; T" E6 v5 `$ S
indicator.
L8 M4 Q' a- w6 E: q* n7 A# R) _ALLOY, A mixture of a basic metal and small amounts+ H& X) {: Q2 c6 c- F# Y
f other metals to change the properties of the basic9 P9 I) N2 d& @& A
etal.
) N5 Y+ M7 T v1 [7 y. kMinimum airplane speed.
1 y4 x5 i0 A+ Z7 P- }e of4 L! n- s7 w2 G2 X
itting airplane angle relative to
; @# Y3 G1 D: \0 e, i" hirstream for the stall warning system.& z9 W2 }1 N6 ?
another.' z: X& I8 Z7 n: Z. I; a
LTERNATE , An additional airport selected during0 d: Q% A* m: L9 D5 U
,
4 p! P& d$ w) q2 |* u1 A* q T# Q合金,/ Q+ ] V% Z5 P# {& `6 Y7 l( X
在金属中加人少量其他金属,而改变其性质的一种金属
8 L% o0 E& W4 h' B; E$ M合物。- |) x$ W% }7 G4 v) _6 ?. O
飞机的最小速度。$ _- D2 v [: `5 O
速警告系统传输飞机对
- |/ A d6 q3 c流的相对角度。5 n( k1 w( f$ R! L3 o) U
由一个状况改换到另一个。3 v8 m0 a; E7 _8 l
降场,2 A4 E) k; H, Q1 h& x+ J D( V9 u
划时,除了目标机场之外,所选的另一个机0 j6 `+ y& J% e7 C6 F
o
0 J. h5 e8 j# m# q5 z. Gm
2 [% x3 `2 D' W& I4 rALPHA SPEED,. s7 u0 E0 [7 Q2 T/ G. M
ALPHA VANE, A small moveable airfoil on the sid! t+ d; l. |: k( i$ J
the fuselage transm* r. p5 X J/ o9 A1 z8 v2 p
a
- w {+ i/ u8 H2 O( sALTERNATE, To change from one condition to
5 l' z" O0 V4 X9 `# r3 ]A
0 w3 g, o1 U) r6 A R Hflight planning, usually near the destination airport, to be
5 q: _9 L! u; Sused when it is desirable to divert from the original
5 @3 T% x5 ]) |# `destination airport.6 @) t Z1 Z. k* ~
空速游标$ m+ o& D2 s0 }1 i
空速表上的可调指标。1 K& w' v% Z, |
混
I% J! p8 s6 Q C9 D' x迎角速度,
- H2 f+ C/ k8 l. v: V2 `) Y. j迎角叶片,
6 q' V# N$ M7 i8 e+ A1 G- E- k位于机身侧的可动小翼面。为失& P! g& {3 g+ k# L! m4 R' b+ z
气
; n: e3 y, J+ q9 ^5 I交替,
- o4 R5 L" f: R6 z( U9 m+ z3 P备
w( G8 Z. T; Q1 a制订飞行计
4 S u: f+ }. g场。通常在目标机场附近,以备不去目标机场时,改降之
8 L% F0 u0 L2 Z5 @% @, k3 N用。
; j+ s, P; h, Y, H5 U英汉对照民用航空词典B OEING! J* m; g! W+ _: U$ t! P
TECHNICAL DICTIONARY 8) p$ b& q& _( s# `, M& D* {, K
ALTERNATE AERODROME, An aerodrome to which
1 V# n) z$ u+ d2 y4 E: Gan aircraft may proceed when it becomes either/ B0 m. K: ]) C7 G) @
possible or inadvisable to proceed to or land at the
2 Y% E" N8 l# Q; I& [. Yerodrome of intended landing.
- \1 G& U$ r4 u3 y9 z6 GTER SETTING, The adjustment of the altimeter
7 Y; T/ w. e/ r; l( Haccount for local variations in atmospheric pressure.2 }9 b) h% t! k8 u
LTITUDE ACQUIRE, A digital flight control system. Q0 U( b9 Z# w# }2 U! i
ode to transition from climb (or descend) to level flight.' H6 n( }0 \$ [8 b1 ]4 g
LTITUDE ALERT, A flight deck alert occuring when the: Z) R1 U& D' t- q9 U
irplane approaches or departs a selected altitude., p8 k$ \, j; s. s t
LTITUDE CAPABILITY, The maximum altitude at) r% g& t/ P; h2 L$ t8 ^- L
hich the airplane can be flown at for a given thrust,
1 z$ l; q. \4 u6 j$ E4 X7 mpeed and atmosphere condition.( \7 r9 |2 M$ p! ~
LTITUDE HOLD (ALT HOLD), A mode of the autopilot
! e) G/ Q% b* {r flight director to maintain a selected altitude.
4 S& ]" R4 t o7 n) C: r% Dirplane's altitude during VNAV operation.
5 ~1 @& k: U# e' U: _0 v机场着陆时,可作着陆使用的( x A1 Q3 z# r, K! N+ N( h
场。( a) t; L/ h) o9 I G
,
8 E0 o# D, X) q6 h) t3 U: l0 B' t根据当地大气压力变化而对高度表所做的调整。2 V9 x5 x: s& W2 |7 F
一种数字式飞行操纵系统,从爬升(或下降)改平的模; U, V! Z5 A: N/ d1 O
。
% O5 A( _# ~4 j2 n' ~5 b度警告,- r3 U: p3 U/ q& J0 o* P
当飞机接近或偏离选定高度时,所出现的驾驶舱警告。
9 z& C, O7 q. `8 G% U M高度能力,: E0 o1 C3 N+ t0 y
在给定的推力,速度和大气状况下,飞机能飞达的最大1 S g' a% M3 }* Q+ r h
高度。
' L1 {0 j7 ~4 B, l5 g4 h( r# L) [高度保持(ALT HOLD),7 s) C2 @! c ]6 I7 J
自动驾驶仪或飞行指引仪保持在选定高度的一种方式。
( y9 ?% t$ {# p1 Y1 t8 Y6 M* g5 _; l,7 K* t- U. R; M5 M, i( B' _
员对飞行高度的控制。
7 N0 h) ?) D8 `( j0 him* N' Z0 B; C: t. u* f) c
a% A+ ~( r8 w& O1 Y/ O4 b
ALTIME. s! w4 P& Z/ H- G" X0 T
to9 n' n3 [& p4 C4 F" B
A' u, |, E8 [- K; u- G7 ~
m
3 \$ _; |/ f' C+ |5 h& Z& fA4 h6 m m/ [( X$ i
a
' C `- s/ a t ~A$ k* n" T9 ?# D1 n0 E
w
' k" r9 E: w8 s; K+ w1 y$ s; Is: z: P$ J& U' w5 d f0 H4 E% X+ J
A
2 |, D8 H! k1 {' d& X! m6 |# Jo
* t0 l5 t. D$ S7 F/ {- `* c) `' KALTITUDE INTERVENTION, Pilot control of the Y( l$ B& m8 U; M6 e3 v$ a. d
a) W, a9 V: X/ g, l/ W9 [7 g& s/ Q1 a
AMBIENT, The surrounding atmosphere./ J9 U7 r- x# n+ {; b/ I
备用机场,
7 }/ S! f- Y% J当不可能或不适宜在预选5 y" a% u! w% o+ o: s2 ]
机! X9 J' Y$ k/ ?& S' b" o& g4 t$ s {
高度表设定( c5 e9 r0 R8 z
高度截获,$ i8 ? g7 ]$ T& L* U9 g: g
式, m+ S b' r0 G
高
- c* p8 @: l7 ]' h: G D. T高度干预: O3 E& e0 ~$ P
在垂直导航工作过程中,飞行; _6 T, P* A" C1 k7 I2 w
周围环境(地面气层),
: G8 }* |4 b* h& g. l" [" K物体周围的环境(特别指大气)。
- G, Y, O V* K! X" g% K英汉对照民用航空词典B OEING
! c# \/ T' X3 E' TTECHNICAL DICTIONARY 9
6 z& T* _8 P% e# m" z$ NAMBIENT PRESSURE, Pressure of air surrounding an3 q9 n; V0 Z% @
object, measured in pounds per square inch (psi) . M& } ^( b* k
MBIENT TEMPERATURE, Temperature of air
8 T+ X6 t* \) n- h- Vmpere.
5 u, q6 h( J! Surrent waveform.9 _- R2 j* Z2 C6 u/ P) z4 i) p2 |" f
g an
/ H/ N# ^: X) Y7 ]- s ]/ ^8 gnalog signal to a digital signal.& o* g2 b. \) J; a7 b* O$ Z
ore inputs4 B7 v5 m6 a7 i* G, c; \& l; ~8 ?
f binary digital information and one output. The output2 u3 A3 x& m. x4 m
1 only when all of the inputs are 1. The output is 0
$ z- h- i* [4 ^: Vhen any one or more inputs are 0.
: H- X! Q2 r. y6 A `6 M( d4 a8 _; M面气压),5 e+ W. Y( E: j' S5 i& _# ?
境温度,% R0 _+ }6 a k) U
气温度,用摄氏度(°C)或华氏(°F)来1 ~5 k& N# J! [3 N, t: ^
。
0 C" Z1 w" K1 `4 M3 G) ` N' V' S3 Z1 [电压或电流波形的幅度。4 [- A% F1 o7 j" U( h- d+ y
性变化的信号来工作,或产生连续性变化的信号7 H$ I: }: M7 Z7 Q, A, v& p$ T4 @
统。
; _; v5 u M7 S将模拟式信号,转换成数值式。
; {: |/ ~) {* S4 J' k) e) i0 |: p一种有两个或两个以上的二进位数字信息输人,一个输! U* A2 J/ D9 K* h! z3 G
的装置或电路。当所有输人为1,输出为1。当任何一个$ O7 _; p2 ?/ o3 r8 _: u8 T
一个以上的输人为0时,输出为0。" L% Z( T" {- ?( O
A
1 l9 E! D+ R0 m) \+ G; fsurrounding an object, measured in degrees Celsius) Y, \- @( Z, h- ]8 ]( h. N* m
(°C)or degrees Fahrenheit (°F).- H! [ B. H0 y* `4 b, R; C
AMPERE, A unit of electrical current. One volt across
1 Q! i7 o- p) V8 F1 M& Gone ohm of resistance causes current flow of one
( s, p& N3 a: \* @a- j2 H' z9 X0 o- L$ K; j9 x& b
AMPLITUDE, The size or magnitude of a voltage or9 c/ b1 O' H& `$ ]4 g5 a c: E
c
7 a4 B" Q, h D- d* i$ F: sANALOG, Quantities or representations that are
- Z; F+ m! i9 t/ M% ^variable over a continuous range.
/ v& @8 n0 N% p9 A" R4 XANALOG-TO-DIGITAL, The process of convertin9 B+ [/ _) M0 R! b$ B+ y# K9 G
a
* \& W2 u* I7 X* q' c* }AND GATE, A device or circuit with two or m$ w/ {. k5 {7 O- m- l2 E
o& S2 O' ^. m% ]
is
2 q4 I/ e* n: F j# a% K1 Pw
* \! [4 R6 @$ r环境压力(地
- g3 T$ {7 h4 A% z6 t5 @物体周围的空气压力,用每平方英寸多少磅(psi)来: _( @, j' S5 y* j% E; ]
度量。. o, x! K8 [- \* X, X4 b7 B: ?
环
+ a' w; F* C+ j6 \$ i6 |# k* c物体周围的空. Q2 Y1 o# C- G) O0 d1 O: z
度量。
- w, v) P4 ?( j! _# A" `安培,; h4 j' Z, O& }. ]
电流的单位。
! i+ h. x, i0 N1伏电压在1欧姆的电阻上所产生的电流为* I* f" m8 d5 Q4 Q# ]9 \
1安培9 t c/ q9 W$ D( Z& V4 I
振幅,
" ?3 t1 @+ f* L* z" n模拟式,* W; L" I( Q6 O% N/ b J* \- I
用连续
7 c6 P! h( q1 i4 `$ }系: p8 M: j. m+ k2 G
从模拟式到数字式,
# B! }% {5 F* K+ k& g与门,
8 h& Q" O3 U/ s8 a5 u出
& }1 A4 z& E# I3 c2 J, S) c; T或
% t) D: D0 L6 l, t/ o英汉对照民用航空词典B OEING
; W" H& X6 W- _. r h( E7 bTECHNICAL DICTIONARY 10
; [* \/ p% |; P# {* l9 W$ LANEROID, A sealed flexible device containing air at low: M0 h0 [5 E; e8 j2 H- Z# X2 h
pressure, which expands or contracts during change of6 f: }$ E( J6 Z9 U$ ~0 R3 p$ ]
ressure outside the device.
! B2 w/ y+ |# N9 Y7 Nically+ W: [# O; H& z5 F6 `4 W5 L2 q
r changing the direction f5 d/ c! e$ _+ ?) P+ P
f drive.4 A1 G! l1 t8 {' \
of the wing chord in5 v' f: a1 z# G' I+ b, H
lation to the free stream airflow as it moves forward
9 A1 K$ K& X" E# _rough the air.
' c& O5 ]# x; z/ \& Z9 Dal axis of the& F* W+ F6 e3 u% O8 e0 s! m
aircraft.
8 p! ?& A& {* k8 }; Y* Z胀或收缩。
. R; G0 f! O& ?' u+ u* Q箱。是改变驱动方向的机械装置。$ A8 c+ C# Z0 p6 g7 O+ l" Y
机翼翼弦在空气中向前运动时与自由气流之间的夹角。
. l4 C% a& {8 n( m. J。
4 r- L$ T \0 Q4 u+ N: jp
% x0 ~9 q# N' wANGLE GEARBOX, A part of an engine, mechan
9 T& u* }1 c' ~& s8 ]% R7 Z" ndriven by the compressor, which drives the accessory1 w* g) L( }- S5 E) s
gearbox. A mechanical device fo
% [ N! }$ i0 m7 ?9 G! j" n% Bo9 n' H, Y C: \2 C
ANGLE OF ATTACK, The angle% t% x5 y8 l9 s/ C2 K
re
% R+ p1 x$ W/ q/ s0 gth
' T9 Z9 k2 u O! N% L; _& nANGLE OF INCIDENCE, The acute angle which the$ g; v3 {7 k/ w: O- Y F
wing chord makes with the longitudin
% B8 }5 D4 n! x, r3 V" F; @6 d膜盒," R8 I, p* g* M' }8 V$ L* I0 I
内含低压空气的密封弹性装置。当它周围的压力变化
5 d6 @8 [ r" s p# j' m$ \时,会膨
) j& _& s1 P% T h: N/ l伞齿轮箱,, Q# j8 G- r* X! X0 j# i# I7 M
发动机的一部分。被压气机以机械方式驱动,然后驱动& v( T: Q% v+ } w- a( x7 \
附件齿轮
0 _& b! j! _8 ^6 Z+ i6 [" K+ M3 G迎角,
P& e4 Q& Q, t4 v0 q安装角,
' P: U- T8 L0 h飞机的纵轴与机翼弦线所形成的锐角
% A4 p- O# N9 L2 B2 Z, Q2 {英汉对照民用航空词典B OEING
& j# b) K' d4 P0 o( S" mTECHNICAL DICTIONARY 11& |% T5 R) ~6 [3 r& ~+ m
ANNUNCIATIONS, Audio or visual indications used to
2 `+ C5 v$ V- y: Q. _& S' j8 Z( Tcall attention to an event that has taken place.
- O- E) Q2 J! X# rANNUNCIATOR, A visual device consisting of a number
( I7 J7 v/ X* aly.
+ O" c9 H' l, J7 ]3 N( oANODE, The element toward which the principal stream
& z9 Y2 b" P; r& }: hof electrons flows.2 O; h0 D3 Q' N. Q% m D3 X
ANOMALY, Not normal./ T4 B9 C# ]% d
ANTENNA, A device which, used in conjunction with a
/ S/ J3 V$ W: Ptransmitter or receiver, is used for radiating or receiving! o$ |( [7 K5 U) z) {* c1 _1 x
radio waves.% e. t7 Y: V. ]# B
NTI-ICING, A method of preventing ice formation on
2 M4 B+ e( _( Z. ke wing leading edges and engine nacelles.- c! L. B) b' P
NTI-SKID, A system for providing maximum braking% s/ k `8 J/ D+ {3 q4 m
ithout skidding for any runway condition. Anti-skid
% Y2 C0 g R1 `- h N& Q& J( domponents are part of the brake system.9 P _1 z5 e$ c3 _) }" W. U: K( h
告,
- ?" |/ I; G* v, i2 I, M当发生事件时,以声音或目视指示形成的提示信号。
" G. ]! j' W: }; I% H7 D: s {/ `与之有关的电路的现有情况或已存在的% K1 M5 D* N2 l
况
0 m) @- M+ Q @ F- R正极," b2 n0 j2 I+ \/ ^9 T
主电子流向的极位。
( u# |0 o# M5 A异常,# v" Q# u" h' K4 p! R
不正常。
' k; e- }1 H5 ^8 I- o1 y k/ u# x, I7 {天线,
4 A3 g+ p/ R. |( }9 R7 | h- P一种与发射机或接收机共同工作来发射或接收无线电
6 I5 l3 a8 F+ V% x+ X) X7 G9 |波的装置。% H9 {' ~% |& f' @+ [* p
冰,
' {" ~4 S- \2 m6 U, P9 B+ z6 `3 t防滑系统,
1 h, o. w) c4 z* Y% @一种在任何跑道状况下,都能提供最大的刹车能力而不
1 q: e- b3 a$ b( i2 x+ ]使轮胎打滑的系统。防滑部件是刹车系统的一部分。4 F/ i: m$ p1 K7 v' ]
of lights. Each light indicates the condition which exists* G2 M& i2 e2 |$ d9 N3 ~
or has existed in an associated circuit and is labeled+ O; l1 D# ?+ V
according
+ Y& a9 X# l5 QA
+ W! l6 x- L0 l1 c- hth
* o7 J7 c- ^+ ^1 ^A
3 W, y, P( F' H; }- m3 nw
: e! z. j9 x% E- U. I, ^3 x, E4 fc
% l5 S: W- @* g- Y通
0 _, x2 F' S& v信号牌,
% n2 r, M$ w, m9 v" T6 W* h由一系列指示灯组成的目视装置。每个指示灯都有相应
( j. a1 E1 ?% w, X* F; s2 n的标记,用来显示' \: {! q4 k6 T" i; T7 u
情
+ u# B1 r: F% @7 v0 p防
x* y2 d5 T, D7 z7 g防止机翼前沿和发动机短舱结冰的一种方法。
( x. I4 ^, W8 e j英汉对照民用航空词典B OEING8 o0 _$ h( h7 H1 H. k' ?4 \
TECHNICAL DICTIONARY 12
. r( K& |8 O- K* qAPPENDIX, A supplement to the Airplane Flight Manual u9 @' S& V2 c
tained in the basic manual. A
3 C Y( N3 G+ k' D5 q1 Y; rollection of supplementary material at the end of a6 n K: `$ v5 U2 d* ^; ]" S
ook.
4 W! m& C6 h0 ^8 U" kof the
0 S3 ]* I: d3 u0 _8 Q" `* frsion link on the landing gear.
( u' Q& Q2 f- p" a! S/ iAPPROACH MODE, An autopilot/flight director mode$ I! F r8 I% A5 t/ m, |' Z
which is a combination of localizer for roll control and* l( o" b7 l* D* R; l% R2 |4 @
glide slope for pitch control. This mode is used when full
# {# Q3 M3 f x( m W% {instrument landing system is available.( z% m! Q8 h( A) x: y2 I
APU, SEE - AUXILIARY POWER UNIT
9 Y9 X$ x. m) g/ r- fARINC, SEE - AERONAUTICAL RADIO
1 h( F5 d) V% l" Q9 v! y' UINCORPORATED
. U0 A* A+ n) m% z# A$ n* n: `ARM, To make ready for operation.6 V$ v( k2 [. J: e
附录,
2 x) @. V; E6 y& q; L飞机飞行手册的附件,包含基本手册中未提到的飞机形* E! C0 S1 Z! y7 f8 p
态的其他性能。是附在手册末的补充材料。
2 r( [( P9 V0 ~. ~顶销,& R( O- m3 q. x& D2 o
用于连接起落架扭力臂两部份的销子。
; z o7 `+ i0 a进近方式,- [* L0 {1 b1 ^/ U6 i; }. C5 d
一种综合了控制横侧的航道信号和控制俯仰下滑信号
. ^; H# i' B& P" U( U的自动驾驶/飞行指引方式。这种方式是在全仪表着陆系
: s5 C2 h' b+ d6 U统正常时才使用。
! o( `1 m S3 d辅助动力装置,
* H! @& s, I# s. B; U' l( s见Auxiliary Power Unit
8 ?# q5 n6 ]* ^* Fcontaining additional performance for aircraft
7 s2 t$ P! v! j% c: C9 iconfigurations not con
6 s6 m7 J$ ?6 |; c+ S+ h& D& }6 Q" H& U Qc
) c& v% P$ t3 z6 Ib! O1 K! f X9 b6 z
APEX PIN, A pin for joining the two sections
" O7 K& f q$ ~; r( gto
, k( y0 f$ s6 q6 v" y& D9 i6 H7 g.
& r7 h' E5 h7 k* u* N航空无线电公司,
: f3 v' f* v/ f- U$ `- `7 `7 \: S% W见Aeronautical Radio Incorporated.2 f, F0 Z* d; d, T! G
预位,
. `& B! B1 Y5 a! K部件可以开始工作的状态。
3 r1 f9 A% V) l# [英汉对照民用航空词典B OEING
8 g4 L3 N( q7 J6 r* ATECHNICAL DICTIONARY 13/ ~ b6 i C, l, T! H
ARC, The curved track over the ground of an aircraft
) \4 K* M" p/ U5 J" N3 b+ nflying at a constant distance from a measuring
/ R6 X, _0 h- T/ P Y1 zequipment (DME).
: N2 s, ^7 J% t0 Y0 m; ?in the limits of self-contained system7 I2 t1 A9 g1 I [) h& {
apability.
" u0 o2 D! C' i7 m( Atem for opposing or restricting$ R; Q1 f6 B9 ~) D
ovement.
( F3 s' b* U) F5 }& }5 Z8 z6 oSPIRATED TAT PROBE, A sensor that measures total" z, ?4 U. C M! M8 O9 W, p9 k- ?4 b' _
ir temperature when the airplane is in the air and that
* Y2 K# L5 s8 j- c$ W- ~7 Heasures outside air temperature when the airplane is! {- @& G5 u b
n the ground. The outside air temperature is measured% J- `8 _6 ?. c. _, @
SSEMBLY, The fitting together of a complete structure
, B4 d( h( v' N E$ h# r3 ]SSUMED TEMPERATURE REDUCED THRUST, The1 P+ ]0 R4 g8 L2 `
ATC, SEE - AIR TRAFFIC CONTROL
. j# b5 g" D/ U4 x,
6 V0 Z4 P' M9 [3 x% f# U6 X系统中所产生的一种用以抗拒
/ M o: ^1 C, B7 r9 v作或限制动作的力。/ [+ D; h% i# X" U! W2 W9 @
头,
+ m. U- h' C e2 k/ ~7 C) ]用来测量飞机在空中时的总大气温度和在地面时的外
R- d) l5 }: L/ ]温度。地面外界温度的测量是利用引气将外界空气吸入; }7 F3 w' r8 q- i" U0 @
头,以达到测量的目的。
8 ^4 r, }" c, m1 }! B: U. t配,
% n6 {# D, O' [, ~5 z* B7 a7 y一个完整的结构或组件的过程。
( E1 h' A+ O/ s5 V \- c/ }假设温度而得的减推力,$ r, C7 S9 W' Y( {
推力设定值时,假定一个比实际外界空气温& u5 |/ m5 u9 W( O3 ]7 g; G6 o
空中交通管制,; V5 }3 b. F5 {1 Z! ^+ C. `1 ^# @& H
见Air Traffic Control
" J) J \' X, q: b eAREA NAVIGATION/RNAV, A method of navigation) S9 }+ y! w& z" _
that permits aircraft operations on any desired course% Y q4 x; Q/ x, m n( w3 I# z9 G
within the coverage of station-referenced navigation
, {5 U; A0 n& D1 E, C, lsignals or with; m" j9 v! L( D
c8 N! I- N5 l; R, L
ARTIFICIAL FEEL, A force developed in the flight% H7 |, R9 P; g! w7 ~2 ~
control or brake sys
' f2 Z" i- N: K# }! p/ Bm
9 q4 q0 P- o7 k; e0 `8 l: vA/ M) l( k v* h) V% K
a9 i- m5 P! [- U. r6 {
m
. ?1 n! O! w2 i6 y7 ?3 No
8 Z$ ]: m+ H! tby using bleed air to draw ambient air through the! O4 a2 n* f5 s+ g
sensor when the airplane is not moving.% f* x/ d. `# l/ s0 w
A8 |: t8 W% r w8 P
or unit.
. D* G: Z& V* ^/ K; M* e' K( b6 wA
7 x, F6 F8 d, hlower thrust obtained by setting a higher than actual9 r& v7 P1 c6 B; ]# I
Outside Air Temperature (OAT)., \% }' A- [$ q
弧线,
* h8 b6 j: J& K' N飞机在围绕DME台等距飞行时的弧形航迹。
- H* ~) Q, f# k区域导航,
+ c$ @$ ]3 p( d# j' o/ z容许飞机飞行在有电台参考的导航信号或自备系统能% E9 U4 }! W) A5 q J6 r
力极限范围内,飞行任何预定航线的一种导航方法。2 y* P5 m/ p2 N$ y) V9 B6 d
模拟感觉
, u. r2 J' G5 z) l: W" {9 }在飞行操纵系统或刹车8 t; B* Q( U' r1 _9 b* k0 c
动( A0 | G" A! q0 R0 g6 D4 X8 w' U
吸气式总温探
' R3 o& U2 | U: f+ L( q9 V9 C界
, n" S6 N) w( j' V: S探5 M; i6 P4 o: T( |7 o- m r: X
装2 G& ?6 I# I, L8 D7 E, |
组合成
) g% ^) b. \- ~0 B3 m由
* e4 Q6 B# y4 V- a在选择起飞
! n8 v' `6 E( _3 C度高的温度而得到的推力。用这种方法可以减少发动机的( [% K# O, o# F( i
磨损和维护费用。
" d0 a9 `' g9 |5 G+ l.1 @: K' [% _6 x# M$ l0 b# B6 o, G
英汉对照民用航空词典B OEING
9 ^- i0 J ?- k/ f4 @& qTECHNICAL DICTIONARY 14
& X4 y: a- [/ Y/ H; `. m3 v& W& TATE, SEE - AUTOMATIC TEST EQUIPMENT
* a! M* b6 d$ \1 H4 g7 Q8 O {6 \ATMOSPHERIC PRESSURE, Pressure of air due to the
. L8 V2 F- Y9 ]( Rarth's atmosphere, expressed in pounds per square" @. |: F- o* ~; U& a s
ch (psi) or inches of mercury (in Hg) or millibars (mB).
: F+ ]6 w d- S) \TTITUDE, The relative orientation of the airplane with" v- V0 [8 k+ [" M
spect to pitch, roll, and yaw.
2 o& e7 J1 o# x7 T8 `0 S. `UDIO CONTROUSELECTOR PANEL, The panel in0 S. O/ Y3 g: ]3 o5 e6 F
e airplane which controls and selects the routing of$ P- ~- K( m6 x: w6 j, d
udio.: h- w/ _8 Y6 y* ]
UTOLAND, Automatic landing using the Digital Flight2 E# E/ B: e# W' b
ontrol System.% O7 l, h3 e* D
n.
2 v* G0 ?' X$ WM, A system
& g4 ]1 W7 {* d0 f$ y. aomposed of all necessary subsystems needed to guide; F" u( g0 c) Q9 K
e flight of an airplane.# I. r B7 u$ b' _
EQUIPMENT, System test
* Q! _6 j( g0 l1 Q! Iquipment that operates under computer control.
7 ?- m; W' s9 v装置, |
|