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6 o9 k! C: l% x6 Hin* x! F% W, w' R8 w; q4 g
A# r; H1 F, g- ?2 }' H& W
re1 t4 J4 E6 \3 F
A* k0 G$ p! H' Q
th
* W. b- `0 S! B9 _9 f7 Ra) f8 R( E, h @, I
A
# m$ T/ z/ g7 q9 M" cC( U% I! e0 w/ Q0 A# v
AUTOMATIC DIRECTION FINDER, A system which
. n4 R! N) V! D; G1 adetermines the direction of a radio statio
0 i. D3 u+ h1 K' f% X- e0 y% VAUTOMATIC FLIGHT CONTROL SYSTE
, K) |& [+ V. Q% F5 c; j! hc
4 a# q( p- B! b0 y6 oth
0 R: f. W- ^0 p- E/ \% [AUTOMATIC TEST
* E; Q& w+ i. E- n/ u( N1 T6 qe0 k# \& b+ }# c7 }. j
自动测试
0 ^; x, A t# H7 C见Automatic Test Equipment.2 k7 Q* m: i d; A! K0 T4 W
大气压力, _/ P/ W! t3 v% w i1 V" x/ u
由于地球周围的大气而产生的空气压力,以每平方寸多7 R# \6 Z, h7 M# z- W- e
磅(psi)或多少寸高水银柱(in Hg)或毫巴(mB)来
& d7 K/ F1 O. G- e示。: t8 j" t ]; }" r( W% u+ G3 ~
飞机姿态,
: m# j5 u& o; q6 ]. P. {5 z1 i飞机与俯仰,坡度,和偏航有关的相对方向。. x# _! Q/ j- m
音频选择面板,- i% X% R' Z$ Y4 U6 q
飞机内用来控制和选择音频通路的面板。
# v- k7 r; L' X D4 W% Z自动着陆,+ c* s* l \5 x
使用数字式飞行操作系统来进行自动着陆。4 L* K4 p( o% i% f3 S3 {
的系统。
8 m& E8 J1 I3 E,
- R6 c% W" [3 p: X& Q5 `# f系统所组成的一个系统。
1 \! a4 |9 d- n7 g在计算机控制下运作的系统测试装置。
0 C. ]9 t# N6 { u$ v7 Z; x6 B$ E少
- G2 a- u% o9 A H5 \: Z3 Z& F3 c表; }3 ~( s" I G/ o
自动定向仪(ADF),0 S) z6 W# a; p( k% G" @5 p$ N
确定无线电台方向- C5 Y# c E8 q2 @
自动飞行控制系统6 D3 J8 Q) l! ]7 p3 w$ M
由所有能引导飞机飞行的子
( S$ X4 ^/ l! p; x: O自动测试装置,# B `3 i- I2 l5 R, ^' B* p
英汉对照民用航空词典B OEING
. O' e5 N Q b8 eTECHNICAL DICTIONARY 15
% z( q& E E8 k. W" J4 w& YAUTOPILOT, A system which automatically controls- k, f _3 l8 ?
and guides the flight of an airplane.4 Y" I [- L, b- b" j1 ], t
AUTOPILOT FLIGHT DIRECTOR SYSTEM, An' w6 N+ n6 v" M, m" A5 Z0 n* {- l
tor* d/ w; ^/ {0 T
UTOTHROTTLE, A system which automatically
8 e. p' q& A/ Q/ m lontrols the throttles of an airplane.
8 S n" V: _9 wPOWER UNIT, A small turbine engine in
3 n/ }# _. y' ?. }$ h; V; v @e airplane for supplying electrical and pneumatic
" n5 P& X6 F( `$ X9 dower for systems operation on the ground or in flight.
2 {* k( |* r' `7 F: K: NVM, SEE - AIRBORNE VIBRATION MONITOR
# R1 o- A) F& JXIAL FLOW COMPRESSOR, A type of compressor
A( b, ?# r6 ~- P6 j! j) c7 rsed in a gas turbine engine in which air passes through9 _ a2 s: n6 W* v6 ~" z5 \4 y$ a
XIS, An imaginary straight line or an actual physical5 z3 Q3 O! m5 X5 E- [+ ~- S1 B# ?
omponent (such as an axle) around which a body can
, ]+ g( `6 ~5 l, [4 ?8 ^; O. C$ otate.! ?$ B6 z' D* z1 t+ v6 Z: D
仪,* L3 j, G( j+ M7 A: L. p" b+ b0 o
自
3 O6 I+ e$ O+ M自动驾驶飞行指引系统,
/ c. `8 X) w) d6 \2 ^; N* Y动驾驶和飞行指引功能的系统。
% B' a& w& K$ l p动油门,
$ i9 |0 U; w G6 @4 S5 t* R自动控制飞机油门的系统。$ f+ H* H$ K2 z5 A! _
是飞机内的小涡轮发动机,在地面或空中给各系统提供5 T5 N; Q J2 d5 P1 Z+ j# Q5 n
源和气源。3 Y9 @& F! @2 C# d+ ?7 P- q
称。
2 T# V% n% L: T& @载振动监视器,' H4 i3 d! p% {5 ?- _4 }. `
见Airborne Vibration Monitor4 S# C) `. V4 J& |" n- D2 l4 R5 x/ ]% u
integrated system containing autopilot and flight direc
6 B+ v; _# O! P+ n* Z! pfunctions.) s4 r$ F* [0 |0 Q: v# t9 s
A* w9 p1 b, W4 t6 K- S
c
8 o$ ~, @5 w1 z1 m5 ]7 IAUXILIARY
3 x3 P: e3 H, K) e1 l' ath
$ B3 W. Z$ e/ m' \/ M: up
5 j" R+ e" k- x- `) AAVIONICS, An acronym designating the field of aviation: ~ C; _0 Z0 K" N( v
electronics.
9 }% c) K) F" I# w4 k: u6 _A; ~- ?# @8 |% K! [
A
; u- L* a g ou
6 g5 e& W% c) f) Z6 k z4 a8 mthe compressor in a straight flow, front to rear.
4 \; w' I. z* B' E- H% w1 \1 i; ?A
5 E/ R# s: |& T6 n s3 ?4 }+ A7 Ic/ s2 {4 f/ [& D
ro
& S0 K& T; c p/ \% t" Y2 P自动驾驶! @( v4 c( \7 h6 [ u% k+ o: |
动操纵和引导飞机飞行的系统。
6 v" ? k8 H3 |4 M一个综合自
& ?3 Z6 @: k6 P( N自( ?; _- D4 d2 ]/ w) Q
辅助动力装置,
3 S |7 x2 J# w2 k; S2 F, `6 t* h, b电9 l- Z% z8 z5 i4 r( N; O
航空电子学,
0 {2 y+ T; k i0 k5 b是航空电子领域的一特有名
3 s5 Q$ T. L4 _6 G. ~机
9 R4 E! d7 Q( X.) d' C8 \4 X' i' i3 P! \$ K
流压缩机,
5 f9 t! P' U* v' k8 _* s一种用于燃气涡轮发动机内的压气机。空气由发动机的
& e0 k! u" H$ ~# p$ g) }+ F( l) f部流出。
9 v3 n0 T3 d; _# U* G% o线,
/ C) ]$ c+ k1 e( A, r可让物体围绕着作旋转运动的一个想像的直线或实际
- T2 V/ `& N4 P5 H+ k, |在的部件(如轴)。
: Y; R# `& g: z7 u8 }轴) j8 i& \) S+ y* S! V
前部轴向流人,压缩后,由后1 x/ _% I7 Y6 o4 }3 h
轴+ |( {( k5 b2 E
存7 p) e# l4 |, r5 A
英汉对照民用航空词典B OEING1 T$ P1 ^0 m r) I! }- s
TECHNICAL DICTIONARY 16
q+ T2 G0 c: ^9 [+ F+ jB6 l( {" Q, L( l8 u
ACKCOURSE APPROACH, An approach to a runway5 [+ a/ D# X3 ^. r) H
versed./ L0 L& q, P2 l" H; q. `# j
own on the EFIS that
1 C: o* W, _) a0 N2 t" x& Woes not readily change, for example, navigational aids.
% F. J6 g4 j, { C5 m7 F+ Zvement in the tank or reservoir.& |3 ]: ~7 m9 v( }0 o. c6 a
ALANCE TAB, A small hinged moveable part on the* }& L$ p+ u' i! C
ailing edge of a control surface (aileron, elevator,
, e* W8 K9 r% l) o4 S" J3 ]4 H航道进近,
' ]- T: ^' U, f6 v+ c6 k K相反的进近方向。当反航道进近时,无下滑
4 N* z. d* ~0 i2 L' V显示在电子飞行仪表系统上不经常改变的数据。例如:5 N# [6 h5 k8 J+ i4 s5 _, O
航设备。
/ B) g$ I2 A0 A9 u0 ?在燃油箱或滑油箱内阻止液体流动的隔板。
( o- p8 `- \$ S1 f6 k% i# X5 p% e. c动补偿片, t3 S5 u" K8 g2 {. b
铰接在操纵面后缘(副翼,方向舵,升降舵)的可动部。& q- y7 m/ O: w: `1 k
与操纵面相反,以帮助操纵面运& ?1 D0 l3 E# P6 E, n/ _
B
5 Y; I* o/ L0 xwhich is opposite the normal approach. For a
0 @3 T4 w6 ], o7 v4 I" [backcourse approach, glide slope signals are not8 V/ ^. a. Q R2 m8 F" K W
available and the sense of localizer signals must be, \7 {4 ^( ~8 l
re
# Q% k4 p: O4 j0 L$ SBACKGROUND DATA, Data sh) p% l+ P4 d% J' g
d
' c# n; O' [' c$ k5 [BAFFLE, A partition in a tank or reservoir to prevent! H$ N$ X8 W7 J- U3 K5 o) | w
fluid mo- u' C- N9 k# T
B% \0 G: Y, Y& P4 W4 H. z0 r0 a ^
tr
% ~9 h+ n- Q6 r3 ?9 h( G7 E8 S$ w& erudder).The tab moves in an opposite direction to the d" A, e$ j/ _# v# `* T" D
control surface for assisting movement of the control5 @2 \# L* r: g! j( R
surface.
4 @9 S8 o j& F$ f6 M- J: n+ C! u反
7 i8 q% ], V( x9 f6 O3 V7 Q. j与正常进近
4 K* u. \* V3 H道信号并且航道信号也必须逆反。1 N- q) [% A4 l& T$ K
背景数据,
Z' Z- [% @* s- T. D导
7 ^5 [2 i( R% G: F缓冲隔板,7 t" m3 g" E$ g. ]
随
- X% B; a! O3 E. R& k5 D随动补偿片的动作方向( g0 E. c1 m7 u. n
动,减小操纵力。
6 } u8 H" u8 B# u/ y英汉对照民用航空词典B OEING
# Z$ V: `3 {2 N! V- ^" Q* C1 jTECHNICAL DICTIONARY 17 H g, }% D4 `1 v
BALANCED FIELD LENGTH, The field length
# y3 u7 P2 l9 R6 j% o/ Eassociated with optimum aircraft performance when9 _- f. |( @% ^7 g
bstacles are not a constraint. In this case, after engine
' t8 v9 I+ t o$ Ailure at V1, the distance required to accelerate, takeoff
% X. H7 h U8 qnd reach a height of 35 feet is equal to the distance
" V0 G4 R5 }7 q C. j: ~ALLAST, A weight installed in an aircraft to maintain K# z5 I% h0 q" [5 m/ w: c5 J/ @
ALL NUT, A fixed spherical nut driven by the
% T1 \6 d+ x# ?' RAR OUT OF VIEW, A signal used to remove the flight
: t% ^6 |- h! |2 B/ i. R& O1 U* fAROMETRIC PRESSURE, The pressure of air above
) Y( x6 T6 ~3 z& L7 Y$ Ag) or6 l2 O$ }5 X6 v" m3 L. V6 G5 Z+ w
millibars (MB).
5 |0 J- |" V) Y' ~$ c/ N, pATTERY, An electrical device for changing stored
0 e3 N9 E7 P5 O( }; T' ~! M6 v! q: ?性能的场长。在此
3 @6 |" C ?( P8 G; B3 E# y况下,V1时发动机故障,要完成加速、起飞、离地35
' G( L7 I$ H: V) Y1 J1 t尺所需距离等于相同速度下完成全停所需的距离。
5 ]* n( \. a# w- j, o舱物,
4 \6 f0 {4 ?5 x% c$ u2 q/ k重心在许可范围内面装载的配重物。2 U% G" Z3 m6 l! M |) Q. v' A; t
形螺母,* g/ W7 c2 ~, l- q! S+ ~0 L
的固定的球形螺母,用以使襟翼和水平% K t M* u6 {2 U
引杆消失,! x! E% \, Z, W/ R1 k2 I* F* P' H
指引杆的信号。0 _2 p" ^; {; ~" l' l% v+ D" ?/ |$ S
压,
# O5 F9 n+ F% K' @1 E% I8 B7 B压力。通常以多少寸高水银柱(in
; g( m0 Y& w0 U3 q0 ~0 h瓶,1 `1 E1 ]8 X# Y5 _& l k( ^
的化学能转变为直流电的电气装置。
/ |: w/ K/ e2 i. zo
6 }8 p* W7 S/ A2 c8 U: kfa( b6 L# ^$ D0 M( d$ f
a
9 j- V+ p3 T( rrequired to stop from the same speed.
4 M" B8 W, q( g" aB2 R7 \ ~+ n4 ^- h; K) K1 i0 U7 {
the center of gravity within allowable limits.. h; T% A2 F! H5 M
B
# ]0 F1 {. R2 T" Yjackscrew for flap and stabilizer movement.
! s7 ~9 O9 h M y( Q1 [- j) vB) N' l- w4 p3 M8 v* J! ?/ W2 X7 _( N
director command bar(s).
2 a1 n+ q1 J: v. ^) uB' w* C+ P6 z5 W# _. q. `
zero pressure measured in inches of mercury (in H; T: ]% e4 T( G1 H+ U! v
in
W& ]5 ?$ [+ o# S+ F) P" zBASE METAL, The underlining metal to which alloying; E3 S$ H" X; P) n! @3 U
agents or metals are added.
2 _" T) ~8 F7 LB
/ r8 A2 v9 f* Pchemical energy into direct electric current.$ N2 {9 @7 A, y( i. T& N
平衡场长,/ R# d. `, z# A: i
当障碍物非限制因素使飞机达到最佳
% x( ]! B) e1 I$ T- i情) k; x4 {0 w8 I) @
英
& L& U. B' O& P) @, V( R) D压
* h( N; V' x8 ~- W5 Y为保持飞机) A% k" u1 ^) a, Z, N& A, K/ P
球6 f( o7 e2 t3 q) \2 d/ z; U
由粗重螺杆驱动
" F( y4 T0 ^8 A( l" g2 Z安定面运动。
" c5 A. T) \3 O5 C- S$ K指
# B2 n; U0 Q0 w, M" i* Y用于除去飞行9 J3 S3 U7 |! _3 I: V
气
5 x' J+ b+ n! d& W- ^# |3 b零压力以上的空气
( F; L9 t8 J) a8 `4 ~# ^2 @3 QHg)或毫巴(MB)来表示。
+ {4 U1 p6 U) U" s基底金属,
, f9 B- R( ]; @- f, i# u* }8 [指合金中的主要金属成份。
: g9 ?. w) n+ `3 n电8 A' h8 z7 O' G% ?
将储蓄
5 h! H. `0 `8 i# h英汉对照民用航空词典B OEING
. _+ M& J0 y Y7 T. C. ]( x9 ATECHNICAL DICTIONARY 18
5 U: f) F$ E, D3 |! b/ G" ?! mBATTER' M) D7 C/ w/ i# u
direct cu, ^0 G" v8 y" m% y
power su/ p' ~- q2 r1 m( S4 L% B
Y BUS, An electrical conductor supplied with; D5 H# T3 }* M7 ?9 O3 m
rrent from the battery or transformer-rectifier for- T' P2 Q r1 R- H: _& d
pply to operating components.$ R" a8 j. k' C
CHARGER, An electrical device supplied
0 n$ L4 L" i6 S8 ?1 a+ uith alternating current, which produces a direct current+ w w$ @: B' \; I& {" J+ o
utput for charging the battery on the airplane.
& k8 S* p1 P @& I" G$ b# QAY, A compartment in the airplane structure.
1 [1 o2 {% U% `) vCD, SEE - BINARY CODED DECIMAL* {4 r T1 _# O1 V2 V
EACON, A device which emits a signal for use as a
% t- w) ?7 p7 ^7 s& Juidance or warning aid.% v0 f {3 [6 m9 R/ }6 v# I
BEARING (NO. 2), The direction from an airplane to a
/ l) r2 P! Z3 g/ D* y( N3 h7 j/ nground station.
( q( G5 a, b2 k) m6 R% C3 S瓶汇流条,
7 d4 W9 [ E" D6 a" d: Y将从电瓶或变压整流器来的直流电供给工作部件的导& @( J0 g W+ Q% a, f( g- Z% i
体。4 A$ `7 i# x7 B& C2 L: j' d* r# T
瓶充电器,) d- O" L8 \+ q1 u0 ?+ M
用交流电向飞机内电瓶充电的电气装置。带有交流电的1 Z( ~- _0 q, w! W9 v4 x' M# Y
气装置,该装置产生直流电向飞机上的电瓶充电。
* f) b' I; l7 P, V1 M8 x" _& u K4 K8 w舱,
$ J0 T8 P! X- U; c5 X" I飞机结构中分隔的空间。# h- G% J, V* C$ v. l5 Q
二进制编码,
9 A" D7 u! C- G. ?" _6 I/ P" u+ y见Binary Coded Decimal, ?$ W U0 i) p( ^/ o
BATTERY% X+ v5 B$ i: g7 l4 l
w" p' v! l0 x( R& a
o
( ?% ~6 x/ v- j. I5 rB
4 a. w+ q; Z& H0 S6 N" `( `6 NB
1 a9 Z* k/ ~8 O- X! b1 o& V& WB
) J3 [4 h( c1 D1 Z" l$ kg5 F' S: V& _; ^- I" o% L4 E7 X
BEARING (NO. 1), A surface that supports a moving
' x( @/ ^/ ~6 T# `part and reduces friction between the two." ?# f: h0 l- o. O4 r" J1 n
电3 V9 w$ _2 e/ `) j9 [% c
电
" e- u: K$ P& a+ M/ |8 K0 O电' \+ e# l: K3 o7 H
电1 Y) i; _$ q/ X; `
隔) J4 _7 }7 B/ R' @. w3 I4 r
.+ V% @ P% T- A8 N( p
信标,( O$ V; s) V/ h0 N2 z+ _4 u3 g
发射引导或警告用信号的装置。 y0 Q! l) J0 b$ j' [
方位(NO.2),
* F* e1 d; I5 {6 x3 t: t1 Y3 p5 k4 a从一架飞机到地面台的方向。$ T" l( r* e! K. i! l
轴承(NO.1),5 l' Q; U+ X: c5 H
用于减轻机械转动磨擦的机械装置。$ L$ m9 i4 H' c' }, G7 ], ?
英汉对照民用航空词典B OEING
2 I6 d" J. x. y6 KTECHNICAL DICTIONARY 19
/ ~! h$ z& c% z, ]3 [! A/ D& hBELLCRANK, A double lever in the control syst& ]. ]( |8 J/ N4 c* {) e
changing direction of motion.8 ?& ^5 R8 @) B: z& k, G
em for5 n6 D* ^3 c$ w8 z
ct in the/ A7 j |% I) A6 T: o& t5 ^
neumatic system for absorbing expansion of duct due
3 V w4 X. Q0 F9 J3 |+ f1 Aheat.6 Y) P: I9 P4 \; p, m5 P# v7 _
ELLOWS (NO. 2), Corrugated folded or pleated
* U9 Y8 W" q9 L8 dontainer or compartment used to measure pressure.% A |7 n! \# C5 _& W* R
EZEL, The part of an instrument case for locking the
: J; [5 T8 w1 N; Plass.
5 M& @; b0 j Q0 B+ CIAS, The potential difference applied between two
; q* K5 \ Q. V1 ^oints for controlling a circuit.5 L* Q& E$ H3 Z
BILGE, The lowest part of an aircraft fuselage. A place
/ j9 r7 p: J' ]% w# f! }" Ywhere water, dirt and other contaminants collect.
3 H' ]. Q/ A! l, T2 ~$ u4 L& t气源系统内提供管道热胀冷缩所需要的余地的波状, h* p' B" t! e3 j! Z- u. |$ |
轫管。
2 u. H. _, a L$ W( m空膜盒,+ y* L/ U' v& n1 _
一种具有波状表面的容器。用于量测气压。, @$ t2 c0 F/ ^
嵌沟缘,
' z+ R. \7 P3 V1 L将表面玻璃固定在仪表上的圈状零件。
/ v' o/ v: k( G4 }9 ?1 R% Y) r压,+ [) n8 v4 {0 v' n, y* y
在控制电路的两点之间的电位差。' Z; h9 M, ^0 F1 F; v" ]" x4 L) ~2 w
机身腹部,* ^! B5 ] H& I9 h6 n
机身的最底部,通常水,脏物,和其他外来物集存于此。3 G* p( ~, N) {1 U* f
BELLOWS (NO. 1), A corrugated flexible du
& R2 i5 F0 u+ Pp1 Q0 W; M0 g& p# _! ?/ S- ^) o. o
to$ F" A1 x; T7 J2 I( q- ^, s
B
9 G; L3 t8 z% O5 ~ Uc
/ g% i) k6 o) d& U: z; zB% T- {! D8 [4 @0 j3 @
g. u Q/ l1 H m4 N4 j
B: m) a+ y1 ^& m4 @. ?, I
p
# X* W% h3 y3 D' @- `直角摇臂,
, Y6 E+ b. L7 O* [: a在操纵系统中改变运动方向用的双臂摇臂。
( b( b6 R, B- q1 {+ ~波纹管,, D9 \5 D/ |% r g
柔9 J. N/ Q/ t3 Y$ ~$ V' r$ Z/ q
真
) y# C9 l y" }0 O0 g) m# \镶
, _( V0 B( X. W; y, g" f# y2 ]偏
! R9 ?$ a0 l- F& u英汉对照民用航空词典B OEING
* v, E% E% e( z1 p% ~# c# BTECHNICAL DICTIONARY 209 M9 T; M9 t0 Z9 H7 M% Q' z: T
BINARY CODED DECIMAL, A system of coding each
) K; V/ L, x# g$ {4 P7 }digit in a decimal number using the binary equivalent.
: Q9 G( ^: z- j# p" QBINARY NUMBER SYSTEM, A number system using
: m( t% j9 k! ?! r1 `4 C9 x; Ds
- ]7 ^7 }! Y: x3 a, F6 MIT, In the binary number system, the smallest unit of
# c, [& \) b( p) rformation, consisting of a 0 or a 1.
- D6 v" E# y9 {1 A# X; `0 f! XITE, SEE - BUILT-IN TEST EQUIPMENT
8 @7 F6 d8 O' pLANK DISPLAY, A display that does not have any
* b7 c/ G5 E+ E8 {7 z c( \dications, normally due to failure.6 O2 ]) m" O9 Y- g+ J# h( E0 n
LACK BOX, A container for electronic circuits to record, [& V# |: n9 _$ @
ight data.
* N' j; F2 E- e! J' nLEED AIR, Air taken from the engine to power various" s4 d! I( J y4 @4 y
ircraft accessories.
_3 u) T1 M; B; M* KA valve in the pneumatic system for air
! c h, v- Z8 V8 ~9 m$ S$ F5 C B+ Msupply from the engine or auxiliary power unit to the
7 `$ I" W6 U5 \3 [pneumatic manifold. A valve on the engine for reducing D. w- _, a9 D8 `- |
pressure in the compressor section.
+ S9 o, J& S& i+ G! Z6 r$ G进制,% g/ v( x) n; C* x+ t
进制,: P9 P: a! u4 R, |8 x# s
一般用0和1)和2为底的数字系统。& L* d8 H$ `, e- s6 a% q& U
特(二进位数),
, i8 P' U/ m( W9 \1 Y二进制中的最小信息单位,包括0或1。- x2 E0 x2 J7 Q3 @- o" ^) O
内自测系统,2 B0 e# P5 ?: _- B
见Built-in Test Equipment; R# i/ K5 E y, e: M
two symbols (usually denoted 0 and 1) and having 2 a7 F" z5 V: f' V1 c1 @
its base.8 k6 w) _/ r7 M3 y# t6 R
B2 Q1 Z. q4 N3 r) S# ?2 N# X
in
& h: M$ f) U/ eB1 D5 q% K; B: i8 b
B
: d% W1 ?- F6 Y' v+ }1 E& oin4 K+ H6 Q0 D2 M: @
B! \, ]4 E* i" d$ m8 f
fl9 Q6 ~+ m7 m0 R( ]
B
( ]! T0 P Y6 M* m; {% ya: @9 V0 S- A& {4 F) |" n& Q
BLEED VALVE,. _" L4 a) c: i6 S5 s: t. l
二进制编码的十
# I: ^- h4 B* z, d) [! t, g一种编码系统。用等效二进制位数编译十进位数的每一2 N7 G$ R) r4 F! Y- W8 g$ |
位。8 `* Z. y7 W P c8 c: g9 @& M
二 w. d' O1 g7 v! q
以两个符号(
* O- J6 m+ N- [比2 F. {3 Y' i2 N" G# U% ] k. Q
机3 J/ _$ u& g* b1 r" ]
.! [/ }& t5 \' Y
白显示,
; Y- s& E1 F, E; ^6 ^通常因故障而造成的显示器上没有任何指示。
T+ W/ h* n* B* q7 E; Z匣子,7 z. `$ k. Y. }
装有用于记录飞行数据的电路系统的容器。
+ [* q8 z) Q2 r3 d% {' L2 B气,
6 y% J# X: k; W F8 r取自发动机而用以驱动飞机上之各种附件的空气。
) b" |3 d& s/ c& j气源系统内,使来自发动机或辅助动力装置的空气进人
$ o% v9 W Y) i) B7 e) l气源支管的活门。发动机上,用来降低压气机压力的活门。+ t! N& k. w5 m9 M0 y8 B. ~
空
; M( k: g* `) b N6 A3 M& B黑
+ n% K! f. h* n. ]# g引* Q& X& G. { D4 `+ R
引气活门,
8 M9 W" M" {! a6 @2 ]英汉对照民用航空词典B OEING
1 p$ K, Y7 t6 |# D9 aTECHNICAL DICTIONARY 21- e* }$ _: c d& P) F; V
BLOCKER DOOR, A device on the engine for blocking, R$ t( R, Y7 J; ^% Q" L
the normal airflow during thrust reverser operation.- u) g/ M/ O: }
LOWER, An electrically operated fan for circulating air.
! Y8 [! O- W8 ^, i% _, H% gLOWOUT PANEL, A panel in the structure between
; r% c9 ]( r( N# x( V. ]) I( Ho compartments that opens to equalize pressure in% [8 D# m+ x: [7 F
e compartments.
; E; e0 y& E0 m8 b# gODY GEAR, The landing gear attached to the
5 Y) I6 t# x4 F. y5 a- O" jgrounding.
3 [9 X* p0 A5 Q: u7 z正常的4 w2 m0 n. I4 c, a% U/ d9 t$ g2 c
气流。
* k" A# E! T( s6 M鼓风机,4 \5 V5 [+ ~7 p4 A
用来使空气循环的电动风扇。
* P3 d- s9 C6 G* A; w, S压口盖,, n$ v; B5 W* F+ m7 Q9 f
两个隔舱之间的口盖,打开后可使两舱压力相等。; [6 X* V; ~$ _) o
身起落架,
. h+ y& I! y. W. S# W身构架上的起落架。
* Y+ s5 z. u( u3 a5 C7 gB% l# t: `+ L" g% E0 }7 K
B) `+ c, U) c, w; p! Y: G
tw2 z7 |5 L& T( ~$ M" U! a
th
5 W) ?; k, w" _9 O4 PB( G, @3 o# M& t* x1 x; v
fuselage structure.
8 g% J. \0 H. ]% EBONDING JUMPER, An electrical connection between; f4 r E% C8 v1 A3 r, `$ F
a component and airplane structure for electrical" W# V' J; y% O
阻流门,8 _5 `& `, Z2 l) v
发动机上的一个装置。在反推工作时用于阻挡
) Q# e/ ]9 I! E: T5 p: L' l7 r8 @卸 Z" r) b3 w* Z s; ?
机
! W0 V3 I! A/ y& F5 I1 R装在机
' l) J, y) C& p$ @- s! T搭接片,9 E' B4 {! B$ Y, l
连接某个部件与飞机结构以形成接地的电接头。
9 ^" c7 a) [5 H英汉对照民用航空词典B OEING6 D- K. l' p) T1 L: Y# `
TECHNICAL DICTIONARY 223 _: |& U3 m5 N1 {0 l" a+ z: ]# \
BOOLEAN ALGEBRA, A mathematical system for' M* ?7 b% @0 T5 H% x9 X
writing combinations of logical statements.
2 B) F% r6 E2 }( dBOOST PUMP, An electrically operated fuel pump for @, Y/ F/ S9 d: C) Y) M0 Q+ G
fuel supply from the airplane fuel tank to the fuel5 u% E3 @5 F3 _
manifold.
& D% B, `7 s1 @BORESCOPE, An electro-optical device for looking at
g0 t4 ^0 M. Oternal parts of an engine through holes in the engine., @+ i( `0 q0 Y( [0 C
orescope ports)' k: u/ i% q6 Q# R" C
OURDON TUBE, A curved flat tube in a pressure gage$ J2 H9 t! D7 q" d) X
r moving the pointer when pressure changes inside
( c: A( f- F/ W2 h9 R# U% [on the ability of the brakes to
7 V1 f' |7 g2 q( [ S0 T9 R* gbsorb a predetermined amount of energy during a
1 h7 O V0 o1 X1 O g3 mjected takeoff.
, b3 v3 S" s# E( P/ W& F用于通过发动机内的孔(孔探口)观察发动机内部件的- L3 D# y3 i5 r( ?( F7 U3 }
光设备。. D' w9 K8 P% K2 _2 i9 I$ L
端管,
, ^5 u0 [$ \2 x4 M测压计内的弯曲扁管,管内压力的变化时它使指针移3 t9 }- {! |# b( r( Q2 c9 O
力。3 o( W) H# Z* ?9 Q1 t0 r% w
极限重量,9 P! _5 I( E, S
最# q$ d. G# J E
起飞重量。
' i" g# N: J9 Q3 m发动机滑油系统与大气相通的通气口。
, H6 G3 S$ ~: N9 c, {0 b$ f! e+ x; Z+ Din+ L* o8 e2 X( z
(b8 x0 J' A- u5 o, W4 W5 ?
B
* |* I" ^; \7 ^$ R- G) ~fo0 B3 Q& n* M3 f& S
the tube.8 s ^8 ~# ^! n% X3 |8 q
BRACKET, To enclose or surround.5 b L" x9 q; h) M
BRAKE ENERGY LIMIT WEIGHT, The maximum- z9 R0 u- Q8 R
takeoff weight based/ @& |/ o& L8 Q
a
; e7 U" M9 w8 `5 _& [& B& cre
; @6 f: U$ r. t+ t VBREATHER, A vent to ambient of the engine oil system." `3 W/ v1 j0 H- b1 q
布尔代数,
M5 Q0 {, o8 c3 P9 U2 l; G0 u7 ^一种用于编写复合逻辑命题的数学系统。- Y7 e9 V8 o( B# O, S
增压泵,
9 k: m) x3 Q. w! p+ T6 p( @ e从飞机油箱向总油管提供燃油的电动泵。
- `. u/ R# |3 ]孔探仪,
" R6 d! |6 n$ k. E. g7 L电
1 g/ j. B/ D, ^# r, d% r' s包) v: |9 I6 _0 v4 v
动,以指示压
- h& ?, l8 i, N托架,8 E8 B% } G' {; o
用于作支撑、装托、或围绕之用。
* b. U: \$ c5 V7 {刹车能量0 S% [4 k8 w/ Y0 n5 k( [" A
中断起飞过程中,取决于刹车吸收预定能量之能力的
: T5 F' \% Y, i' |% e大
) k+ G$ K7 K* N' A( B通气装置,
2 x- ]8 J4 i* S) A英汉对照民用航空词典B OEING) f- u5 Z+ _5 p* f! B. c; k
TECHNICAL DICTIONARY 23
3 b# C' @- T, M' q3 s' c) nBUFFET, Vibration of the wings and airframe resulting
. Y% V# ^; P' W, ~from unsteady airflow over the wing; caused when1 q } ~4 L; O
airspeed is too slow, the bank angle is too steep, or
' s. {' Y1 {/ d# K6 B, { \8 firspeed is too fast.* |8 T0 t7 o, ~) ~7 @/ P
UILT-IN TEST EQUIPMENT, Equipment installed on; w# |* E+ m# B( @
e airplane and in airplane systems to test the systems0 i" u x+ i& ]
ithout external test equipment.. Q) d' _9 R1 ~: s) W9 [
UFFET MARGIN, The amount of residual maneuver W: s+ \$ h N4 t$ h0 n
apability present before the onset of buffet.
' ?* E a7 t( [7 @6 NUG SPEED, A preselecteed speed to be observed
7 p3 t7 m3 k8 i1 ending sequence.
& L) g1 R( {3 sk" U* e: Q6 Q4 R( y
ng landing gear operation.
7 a+ s9 A7 f J6 ~速度太慢或太快,坡度太大,均会引起抖振。
' j6 ?3 V& y; W$ R自检设备,
5 Y% |& {; p# ?" ^5 v2 f- I5 E' V安装在飞机和飞机系统中,在无外接检测设备情况下," T9 R2 A5 h" z1 a, f: V( p) M
用于检测系统的设备。
( L& t- ?) X5 a1 z# r( u. O( u抖振裕度,
5 D3 m+ Y+ y9 t7 S. S+ v, Z飞机在遭遇抖振之前,剩余机动能力的大小。& K0 m, U4 r1 {6 D2 {
标速度,6 u& R+ P% K& s
在某些机动飞行过程中,特别是在进近和着陆时,飞机1 ?& j: ^3 K6 n) y& |5 z
预定速度。
$ c2 ] Q+ f' _3 v4 P力装置,
) v# {1 _& y4 X* j架工作的一种机械设备(弹簧或减震器)。% V" I7 g* T) Y$ h) ~4 H1 |5 c
流条,* [& G! V4 Q1 X3 z# w* A6 {; h
在部件或组件之间传输电、数据、或定时的单一电线或
/ C5 t9 q: F# k) `# Ha
0 L! T. o8 ^7 T5 J8 _1 _& d4 aB
1 u* e) W) [2 ~+ mth
+ g- _2 H( l) C: K, Rw
# z( x, W$ R& u" dB9 S/ P! m: n% m+ W
c
, t3 \% g. J9 [$ V. C. \6 l: yB9 f4 e% M p/ ^- X Q! d: m
during certain maneuvers, particularly the approach and
: n' _0 U1 i. mla2 W& k) H' t: s+ D& O V) |
BULKHEAD, A structural partition in the fuselage or
' m% k2 [: m% X8 Z/ T$ J* qwing.
; z* W" @5 x; m# A. T qBUNGEE, A mechanical device (spring or a shoc
3 L' Z2 G) ^6 Iabsorber) for assisti' d6 M) e* B, C" U2 h" g
BUS, A single wire or group of wires which transfers8 g$ j! R$ s5 B( ~- E
power, data, or timing between several units or$ g: z$ H+ E- g* z/ l; B9 D
modules.
, {, g R9 K. B; ?9 |: L& B抖振,
. q7 B; i$ n3 ]7 d* e( h+ k由于机翼上表面的不稳定气流引起的机翼和机体的振6 H3 c1 t+ L" V, h) C
动。飞行) X* O' q7 |8 E1 B' c5 _- n7 k6 }
游
% {5 | F* f+ k# V/ O所应保持的+ ]! Q& W/ }: F# n( F+ D
壁板式隔框,
8 E J7 l+ `1 d3 g) @机身或机翼内一种结构隔板。
4 L s% w Y) p% _5 G! r2 z张% P$ _* f5 Y! ]( g) J" r, O
用于协助起落2 c7 k, h, [5 h/ H% e+ [
汇0 l$ G* L: r3 z+ d7 M( X# A# q
电线组。
, O8 \# x+ r k/ R英汉对照民用航空词典B OEING. I8 |, L: |7 V2 G
TECHNICAL DICTIONARY 24 |
|