• 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


777 AIRCRAFT MAINTENANCE MANUAL


AIR -ENGINE COMPONENT LOCATIONS -LEFT

EFFECTIVITY BEJ ALL  75-00-00 
Page 11 
D633W101-BEJ  Sep 05/2003 


AIR -ENGINE COMPONENT LOCATIONS -RIGHT

Component Locations
These engine air cooling and compressor control components are on the back of the intermediate case:
*
TVBC air shutoff valve solenoid

*
TVBC pneumatic relay valve

*
Number 3 bearing buffer air cooler.


You must remove a fan exit liner segment to get access to these components.
BEJ ALL POST SB 777-71-0032
These components are on the right side of the high pressure compressor and turbine cases:
*
Thrust balance air shutoff valve

*
2.9 start bleed valve and thermocouple probes (2)

*
TVBC pneumatic relay valve

*
TVBC air shutoff valve solenoid

*
PS3 bleed air filters (2)

*
TVC air valve

*
TVC air valve actuator

*
TVBC air shutoff valve

*
Variable stator vane actuator

*
TCC HPT manifolds

*
TCC HPT collector

*
TCC HPT air valve

*
TCC LPT manifolds

*
TCC LPT collector

*
TCC inlet duct.


BEJ ALL
These components are on the right side of the high pressure compressor and turbine cases:
*
Thrust balance air shutoff valve

*
2.9 start bleed valve and thermocouple probes (2)

*
TVBC pneumatic relay valve

*
TVBC air shutoff valve solenoid

*
PS3 bleed air filters (2)

*
TVBC air shutoff valve

*
Variable stator vane actuator

*
TCC HPT manifolds

*
TCC HPT collector

*
TCC HPT air valve

*
TCC LPT manifolds

*
TCC LPT collector

*
TCC inlet duct.


EFFECTIVITY BEJ ALL  75-00-00 
Page 12 
D633W101-BEJ  Jan 05/2004 


PW4000 SERIES ENGINES


777 AIRCRAFT MAINTENANCE MANUAL


AIR -ENGINE COMPONENT LOCATIONS -RIGHT

EFFECTIVITY BEJ ALL POST SB 777-71-0032  75-00-00 
Page 13 
D633W101-BEJ  Jan 05/2004 


PW4000 SERIES ENGINES


777 AIRCRAFT MAINTENANCE MANUAL


AIR -ENGINE COMPONENT LOCATIONS -RIGHT

EFFECTIVITY BEJ ALL  75-00-00 
Page 14 
D633W101-BEJ  Sep 05/2003 


AIR -FUNCTIONAL DESCRIPTION

General
During engine operation, the cooling and airflow control systems operate automatically.
Compressor Stator Vane Control
The IGV, and the 5th, 6th, and 7th stage variable stator vanes control the airflow through the HPC. The EEC controls the variable stator vane actuator as a function of:
 
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(5)