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庞巴迪环球5000公务机机组操作手册 Bombardier Global-辅助动力装置

时间:2011-11-03 12:04来源:蓝天飞行翻译 作者:公务机
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TABLE OF CONTENTS 
CHAPTER 5 
Page 
TABLE OF CONTENTS  05.00.1 
DESCRIPTION 
General  05.10.1 
APU Access and Component Location  05.10.2 
APU Compartment  05.10.2 
APU General Arrangement  05.10.3 
APU System Schematic  05.10.3 
Lubrication  05.10.4 
Oil Pressure  05.10.4 
Gravity Oil Fill  05.10.4 
Oil Replenishment System  05.10.4 
Oil Replenishment System Filling  05.10.6 
Oil Replenishment Panel  05.10.7 
Operation  05.10.7 
Fuel Control and Indication  05.10.8 
Airframe Fuel  05.10.8 
Ignition  05.10.9 
Start System  05.10.9 
Speed Indication  05.10.9 
Temperature Indication  05.10.9 
Hourmeter/Cycle Counter  05.10.9 
ECU Component Control Schematic  05.10.10 
Control System  05.10.10 
Pneumatic  05.10.10 
APU System Operating Modes  05.10.12 
ECU Power-up  05.10.12 
Start Mode  05.10.12 
On-speed Mode  05.10.12 
Cooldown Mode  05.10.12 
Shutdown Mode  05.10.12 
APU System Operating Sequence  05.10.12 
APU Starting  05.10.12 
APU Door Positioning  05.10.12 
APU Loading  05.10.13 
APU Shutdown  05.10.13 
APU Door Operation and Indication  05.10.14 
Door Operation  05.10.14 
Door Indication  05.10.14 

Rev 3, Apr 25, 2005 Flight Crew Operating Manual Volume 2

AUXILIARY POWER UNIT
 
TABLE OF CONTENTS 
Page 
DESCRIPTION 
APU RPM and EGT Indications  05.10.14 
APU Fire Protection  05.10.15 
APU Control Panel  05.10.15 
Start Sequence  05.10.16 
Normal Shutdown  05.10.16 
Emergency Shutdown  05.10.16 
APU Emergency Shut-off Buttons  05.10.17 
Restart After Emergency ShutDown  05.10.17 
Protective Shutdowns  05.10.18 
System Overview Schematic  05.10.19 
Electrical Power and Distribution  05.10.20 
Start Control Schematic  05.10.20 
FADEC Inputs and Outputs  05.10.21 
ECU Schematic  05.10.22 
EICAS Messages  05.10.23 
EMS CIRCUIT PROTECTION 
CB . APU System  05.20.1 

Volume 2 Flight Crew Operating Manual Rev 3, Apr 25, 2005
GENERAL
An Allied-Signal RE 220 gas turbine Auxiliary Power Unit (APU) is installed in a fire proof enclosure in the tail cone of the airplane (beneath the airplane rudder and elevator control systems) and has a fire detection element system (see Fire Protection System Chapter 9). The APU is installed outside of the main engine rotor burst zone which enhances airplane high altitude operation.
 
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