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庞巴迪挑战者605公务机机组操作手册 CL605-辅助动力装置 AUXILIARY_POWER_UNIT

时间:2011-10-27 15:29来源:蓝天飞行翻译 作者:公务机 点击:
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
  


 AUXILIARY POWER UNIT Table of Contents  Vol. 2  05.00.1 
Oct 05/06 

CHAPTER 5 - AUXILIARY POWER UNIT 
TABLE OF CONTENTS 
Page 
TABLE OF CONTENTS  05.00.1 
DESCRIPTION 
General  05.10.1 
APU Enclosure  05.10.1 
Power Section and Accessory Gearbox  05.10.2 
Description  05.10.2 
Components and Operation  05.10.2 
Generator Adapter  05.10.3 
Description  05.10.3 
Components and Operation  05.10.4 
Air Intake and Exhaust  05.10.6 
Description  05.10.6 
Components and Operation  05.10.6 
APU Fuel Distribution  05.10.8 
Description  05.10.8 
Components and Operation  05.10.8 
Start and Ignition  05.10.12 
Description  05.10.12 
Components and Operation  05.10.12 
Pneumatic Supply  05.10.20 
Description  05.10.20 
Components and Operation  05.10.20 
Controls and Indicators  05.10.21 
EICAS Messages  05.10.24 
SUMMARY 
Power Supply and Circuit Breaker Summary  05.20.1 
LIST OF ILLUSTRATIONS 
DESCRIPTION 
Figure 05.10.1 Auxiliary Power Unit (APU)  05.10.1 
Figure 05.10.2 APU Power Section and Accessory Gearbox  05.10.3 
Figure 05.10.3 APU Generator Adapter  05.10.5 
Figure 05.10.4 Air Intake, Exhaust and Indication  05.10.7 

 

 AUXILIARY POWER UNIT Table of Contents  Vol. 2  05.00.2 
Oct 05/06 

Page 
LIST OF ILLUSTRATIONS 
DESCRIPTION 
Figure 05.10.5  APU Fuel Pump and Shutoff Valve  05.10.9 
Figure 05.10.6  Negative.G Shutoff Valve and FCU  05.10.11 
Figure 05.10.7  APU Start and Ignition  05.10.13 
Figure 05.10.8  APU Start  05.10.15 
Figure 05.10.9  APU Normal Shutdown  05.10.17 
Figure 05.10.10  APU Protective/Emergency Shutdowns and Faults  05.10.19 
Figure 05.10.11  APU Pneumatic Supply  05.10.21 
Figure 05.10.12  APU Panel and EICAS Indications  05.10.22 
Figure 05.10.13  EICAS and Synoptic Page Color Coding  05.10.23 

 

 AUXILIARY POWER UNIT Description  Vol. 2  05.10.1 
Oct 05/06 

A Honeywell 36–150(CL) constant-speed gas turbine auxiliary power unit (APU) is installed within a fire-resistant compartment in the aft equipment bay.
The APU drives a generator, providing AC electrical power, that serves as a backup AC power source up to an altitude of 20,000 feet. The APU also provides pressurized bleed air to the 10th-stage manifold for engine starting up to 15,000 feet. In-flight APU bleed air extraction for air conditioning is not permitted above 15,000 feet.
 
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