• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-09-26 11:58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

IDG AOC Valve
The EEC uses a torque motor driver to control the position of the integrated drive generator (IDG) air/oil cooler valve. The EEC receives feedback of the valve position.
Backup Generator AOC Valve
The EEC uses a torque motor driver to control the position of the backup generator air/oil cooler valve. The EEC receives feedback of the valve position.
2.5 Bleed Valve
The EEC uses a torque motor driver to control the 2.5 bleed valve actuator. The EEC receives feedback of the actuator position.
EFFECTIVITY
BEJ ALL

VSV
The EEC uses a torque motor driver to control the variable stator vane (VSV) actuator. The EEC receives feedback of the actuator position.

2.9 Bleed Valves
The EEC uses a solenoid driver to control the pneumatically operated 2.9 bleed valves. The EEC receives feedback of the valve position from thermocouple probes.
TCA Valves
The EEC uses a solenoid driver to control the pneumatically operated turbine cooling air (TCA) valves. The EEC uses a torque motor driver to control the actuator of the fourth valve. The EEC receives feedback of the actuator position.
TCC Valves
The EEC uses a torque motor driver to control the turbine case cooling (TCC) valves actuator. The EEC receives feedback of the actuator position.
Nacelle Zone Vent Valve
The EEC uses a solenoid driver to control the position of the nacelle zone vent valve. The EEC receives feedback of the valve position.
73-21-00

Page 17 D633W101-BEJ Sep 05/2002

ENGINE FUEL CONTROL -ENGINE INTERFACES
Programming Plug
The programming plug selects the EEC rating logic with pins. It attaches to the EEC.
EFFECTIVITY BEJ ALL  73-21-00 
Page 18 
D633W101-BEJ  Sep 05/2002 


PW4000 SERIES ENGINES

 

777 AIRCRAFT MAINTENANCE MANUAL


ENGINE FUEL CONTROL -ENGINE INTERFACES

EFFECTIVITY BEJ ALL  73-21-00 
Page 19 
D633W101-BEJ  Sep 05/2002 


ENGINE FUEL CONTROL -PMA

General
The permanent magnet alternator (PMA) supplies power to the EEC. It also supplies an analog N2 speed signal to the EEC. The PMA attaches to the front of the main gearbox.
Physical Description
The PMA contains two three-phase coils for power. It also contains two single-phase coils for N2 speed signals. Fan air cools the PMA and the gearbox turns it.
Functional Description
Each EEC channel gets power from one of the alternator coils when the engine gets to 5 percent N2. Each EEC channel also gets an analog N2 speed signal from one of the speed sensor coils. The EEC sends analog and digital N2 speed signals to airplane systems.
Training Information Point
You should use the special removal tool when you remove the PMA rotor. The tool will prevent damage to the PMA carbon seal in the main gearbox. Seal damage can cause high oil consumption.
 
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 发动机和燃油控制 Engine Fuel and Control PW 777 AIRCRAFT MAINTENANCE MANUAL(13)