• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-09-26 16:02来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

Compressor Stator Vane Control
The stator vane control system moves the inlet guide vanes and the 5th, 6th, and 7th stage variable stator vanes of the high pressure compressor (HPC). This controls the airflow through the compressor to increase compressor stability. The EEC controls the stator vane actuator and servo fuel pressure moves the actuator to move the vanes.
75-00-00

Page 5 D633W101-BEJ Jan 05/2004

AIR -GENERAL DESCRIPTION

Compressor Bleed Control
The bleed control system uses the 2.5 and 2.9 bleed valves to send air overboard that is not necessary during an engine start. The valves also bleed air during engine surge and reverse thrust conditions to increase the compressor stability. The EEC controls the 2.5 bleed valve actuator and the 2.9 bleed valve solenoid. PS3 servo air pressure closes the poppet-type 2.9 bleed valves. Servo fuel pressure moves the 2.5 bleed valve actuator to modulate the 2.5 bleed valve.
Thrust Balance Control
The LPT thrust balance control system reduces axial loads on the number 1 bearing. The thrust balance air shutoff valve sends 8th stage air to the LPT thrust balance annulus through the turbine exhaust case. The EEC controls the TVBC air shutoff valve solenoid. PS3 servo air pressure closes the poppet-type thrust balance air shutoff valve.
EFFECTIVITY BEJ ALL  75-00-00 
Page 6 
D633W101-BEJ  Sep 05/2003 


PW4000 SERIES ENGINES


777 AIRCRAFT MAINTENANCE MANUAL


AIR -GENERAL DESCRIPTION

EFFECTIVITY BEJ ALL POST SB 777-71-0032  75-00-00 
Page 7 
D633W101-BEJ  Jan 05/2004 


PW4000 SERIES ENGINES


777 AIRCRAFT MAINTENANCE MANUAL


AIR -GENERAL DESCRIPTION

EFFECTIVITY BEJ ALL  75-00-00 
Page 8 
D633W101-BEJ  Sep 05/2003 


PW4000 SERIES ENGINES


777 AIRCRAFT MAINTENANCE MANUAL

THIS PAGE IS INTENTIONALLY LEFT BLANK

75-00-00

Page 9 D633W101-BEJ Sep 05/2003

AIR -ENGINE COMPONENT LOCATIONS -LEFT

Component Locations
These engine air cooling and compressor control components are on the back of the intermediate case:
*
2.9 (start/stability) bleed valve solenoid

*
2.9 (start/stability) pneumatic relay valve

*
2.5 bleed valve actuator.


You must remove a fan exit liner segment to get access to these components.
These components are on the left side of the high pressure compressor case:
*
PS3 bleed air filters (2)

*
TVBC air shutoff valves (2)

*
TCA thermocouple probe

*
2.9 stability bleed valve and thermocouple probes (2).


EFFECTIVITY BEJ ALL  75-00-00 
Page 10 
D633W101-BEJ  Sep 05/2003 


PW4000 SERIES ENGINES


 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:777 AMM 飞机维护手册 发动机引气 Engine Air PW 777 AIRCRAFT MAINTENANCE MANUAL(4)