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從一個(gè)飛行階段轉(zhuǎn)成另一個(gè)飛行階段。
過渡高度，
改變高度表設(shè)定時(shí)的飛機(jī)高度。
平移整流罩，
反推過程中使用的反推整流罩外面的可動部份。
發(fā)射機(jī)，
將信息從一處發(fā)至另一處的電氣部件。
應(yīng)答機(jī)，
在收到合適詢問后，能自動發(fā)射可識別信號的無線電收
發(fā)機(jī)。
平，
動機(jī)和飛機(jī)在平衡的狀況下工作而做的發(fā)動機(jī)
another.
a
T
th
re
T
in
tr
proper interrogation is received.
for a balanced condition of operation.
過渡，
配
為使發(fā)
和飛機(jī)操縱系統(tǒng)的調(diào)整。
英漢對照民用航空詞典 B OEING
TECHNICAL DICTIONARY 161
TRIM TAB, A small hinged movable part on the trailing
edge of a control surface (aileron, rudder) (see TAB).
L, The total fuel consumed from brake release
through climb, cruise, and descent, to landing at
destination.
RUE AIRSPEED(TAS), The actual speed of the
aircraft in relation to the moving air. The true airspeed is
ated airspeed corrected for position
rror, compressibility, and temperature effects.
ribes
the output value for each input
ombination.
鉸連在副翼和方向舵等操縱面后緣的可動部份。
航班燃油，
一個(gè)航班由松剎車開始，經(jīng)過爬升、巡航和下降，到
目的地著陸為止，所耗的全部燃油。
變壓整流裝置，
見 Transformer Rectifier Unit
TRIP FUE
TRU, SEE -TRANSFORMER RECTIFIER UNIT
T
equal to the indic
e
TRUTH TABLE, in digital logic, a table which desc
a logic function by listing all possible combinations of input values and shows
c
配平調(diào)整片，
在
．
真空速（TAS）；
對于流動中的大氣的實(shí)際速度。由指示空速經(jīng)過
真值表，
數(shù)學(xué)邏輯中用來表達(dá)邏輯函數(shù)的表。該表列出了所有可
能的輸人組合，和每個(gè)輸人組合所產(chǎn)生的輸出值。
飛機(jī)相
位置、壓力和溫度校正而得。
英漢對照民用航空詞典 B OEING
TECHNICAL DICTIONARY 162
TURBINE, A rotating part of an engine which kinetic energy from the combustion chamber ga
extracts
ses.
his energy is converted to turbine rotation which
tates the compressors and fan through a coaxial
haft.
TURBINE CASE COOLING, A method of cooling the
ngine by using fan air. This cooling process is used to
TURBOFAN,
(1). A jet engine in which the first set of blades is a
large fan.
(2). An air driven fan/compressor used in air
conditioning system.
TURBULENCE, The movement or shaking of an
airplane caused by unstable air masses.
渦輪，
發(fā)動機(jī)內(nèi)，從燃燒過的高溫高壓氣體中擷取動能的轉(zhuǎn)動
份。該動能使渦輪轉(zhuǎn)動，渦輪則經(jīng)由同心軸帶動壓氣機(jī)
風(fēng)扇。
渦輪機(jī)匣冷卻，
用風(fēng)扇空氣冷卻發(fā)動機(jī)的一種方法。該冷卻過程被用于
效率。
（1）．第一組葉片構(gòu)成一個(gè)大風(fēng)扇的噴氣發(fā)動機(jī)。
（2）．空調(diào)系統(tǒng)內(nèi)的由空氣驅(qū)動的渦輪和壓氣機(jī)組合。
顛簸，
由不穩(wěn)定的空氣團(tuán)造成的飛機(jī)運(yùn)動或抖動。
T
ro
s
e
increase engine efficiency.
部
和
提高發(fā)動機(jī)
渦輪風(fēng)扇，
英漢對照民用航空詞典 B OEING
TECHNICAL DICTIONARY 163
TURBULENT AIR PENETRATION SPEED, A speed
that provides adequate maneuver margins when flying
to unstable air masses.
ht
stment in the control
ables.
UHF, SEE - ULTRA HIGH FREQUENCY
NDERCARRIAGE, SEE - LANDING GEAR
UNIT, One of the type, a single component.
UPLOCK, A mechanism on the landing gear for keeping
the landing gear in the retracted position in the wheel
well.
速度，
縱裕度的速
。
調(diào)整操縱鋼索張力的
械裝置。
高頻，
見 Ultra High Frequency
in
TURNBUCKLE, A mechanical device with left and rig
hand threads for tension adju
c
U
ULTRA HIGH FREQUENCY, The frequency band
between 300 and 3000 MHz.
U
顛簸穿過
飛機(jī)飛進(jìn)不穩(wěn)定的空氣團(tuán)時(shí)，提供適當(dāng)操
度
松緊螺套，
具有左旋螺紋和右旋螺紋，用以
機(jī)
超
超高頻，
頻率帶在300 MHZ至 3000 MHZ之間。
起落架，
見 Landing Gear
單元，
某一類型或某一部件。
上位鎖，
起落架上，用以將起落架保持在輪艙內(nèi)收上位置的機(jī)
構(gòu)。
英漢對照民用航空詞典 B OEING
TECHNICAL DICTIONARY 164
UPSET HEAD, The head produced on the tail of a rivet
during the installation driving process. (See
Manufactured Head.)
1 (TAKEOFF DECISION SPEED), Is the maximum
peed at which the rejected takeoff maneuver can be
itiated and the airplane stopped within the remaining
eld length under the conditions and procedures defined
the FAR's. It is the latest point in the takeoff roll where
stop can be initiated.
ssure
dient capability and maneuver margin.
VACUUM, A negative pressure or pressure below
atmospheric, measured in inches or millimeters of
　
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