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时间:2011-09-26 16:02来源:蓝天飞行翻译 作者:航空
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AIR -ENGINE BEARING COOLING -GENERAL DESCRIPTION

EFFECTIVITY BEJ ALL  75-22-00 
Page 5 
D633W101-BEJ  Sep 05/2002 


AIR -ENGINE BEARING COOLING -NO. 3 BEARING BUFFER AIR COOLER

Component Location
The cooler is on the intermediate case below the fan exit liner at the 2:00 position.
Functional Description
The No. 3 bearing buffer air cooler is a flow-through air-to-air type heat exchanger. The cooler uses 4th stage air to cool the 12th stage HPC bleed air. The cooled air flows through an external tube back to the No. 3 bearing compartment.
EFFECTIVITY BEJ ALL  75-22-00 
Page 6 
D633W101-BEJ  Sep 05/2002 

 

AIR -ENGINE BEARING COOLING -NO. 3 BEARING BUFFER AIR COOLER

EFFECTIVITY BEJ ALL POST SB 777-71-0032  75-22-00 
Page 7 
D633W101-BEJ  Jan 05/2004 

 

AIR -ENGINE BEARING COOLING -NO. 3 BEARING BUFFER AIR COOLER

EFFECTIVITY BEJ ALL  75-22-00 
Page 8 
D633W101-BEJ  Sep 05/2003 


PW4000 SERIES ENGINES


777 AIRCRAFT MAINTENANCE MANUAL

THIS PAGE IS INTENTIONALLY LEFT BLANK

75-23-00

Page 1 D633W101-BEJ Sep 05/2002

AIR -ENGINE EXTERNAL ACCESSORY COOLING -GENERAL DESCRIPTION

Purpose
The engine external accessory cooling uses fan air to cool specific engine components and the nacelle zone between the engine and the thrust reverser.
General Description
BEJ ALL POST SB 777-71-0032
Tubes send fan air to these components:
*
Ignition exciters (2)

*
Exciter-to-igniter plug cables (2)

*
Igniter plugs (2)

*
Turbine vane cooling (TVC) air valve actuator

*
Oil pressure transmitter

*
Permanent magnet alternator

*
Pneumatic starter.


BEJ ALL
Tubes send fan air to these components:
*
Ignition exciters (2)

*
Exciter-to-igniter plug cables (2)

*
Igniter plugs (2)

*
Oil pressure transmitter

*
Permanent magnet alternator

*
Pneumatic starter.


The nacelle zone ventilation shutoff valve is on the left thrust reverser. It controls the flow of fan air around the high pressure compressor and the diffuser cases.
The EEC controls the nacelle zone vent ventilation valve as a function of altitude. A dual LVDT supplies position feedback to the EEC. Fault data goes to AIMS.
EFFECTIVITY BEJ ALL  75-23-00 
Page 2 
D633W101-BEJ  Jan 05/2004 

 

AIR -ENGINE EXTERNAL ACCESSORY COOLING -GENERAL DESCRIPTION

EFFECTIVITY BEJ ALL POST SB 777-71-0032  75-23-00 
Page 3 
D633W101-BEJ  Jan 05/2004 


 
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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(8)