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庞巴迪环球5000公务机机组操作手册 Bombardier Global-动力装置(2)

时间:2011-11-11 09:42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
  
N1, N2, EPR CMD SYNC OFF  18.10.44 
SYNC Annunciation  18.10.44 
Thrust Reverser System  18.10.45 
Thrust Reverser  18.10.46 
Reverse Thrust Operation  18.10.47 
Reverser Components  18.10.48 
Isolation Control Unit  18.10.48 
Directional Control Unit  18.10.48 
Reverse Thrust Levers  18.10.50 
Reverser System Lock-Out  18.10.51 
Starting and Ignition  18.10.52 
Starter Air Valve (SAV)  18.10.54 
Air Turbine Starter (ATS)  18.10.54 
Ignition System  18.10.55 
Engine Run Switches  18.10.56 
Engine Starting  18.10.58 
Engine Shutdown  18.10.63 
Dry Cranking  18.10.64 
Wet Cranking  18.10.64 
Starting Anomalies  18.10.65 
Auto-Relight  18.10.66 
Quick Relight  18.10.66 
Volume 2  Flight Crew Operating Manual  Rev 2A, Apr 11, 2005 
18.00.2  CSP 700.5000.6 


POWER PLANT
 
TABLE OF CONTENTS
 
Page 
DESCRIPTION 
Engine Fire Detection System  18.10.67 
Engine Limit Exceedance Display  18.10.68 
Power Plant EICAS Messages  18.10.69 
EMS CIRCUIT PROTECTION 
CB . Engine System  18.20.1 
CB . Oil System  18.20.2 
CB . Thrust Rev System  18.20.3 

Rev 2A, Apr 11, 2005 Flight Crew Operating Manual Volume 2

POWER PLANT
 
TABLE OF CONTENTS
 
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Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005

POWER PLANT
 
GENERAL
The Global 5000 airplane is powered by two BMW.Rolls Royce BR 700.710A2.20 engines, each mounted on a pylon on either side of the rear fuselage.
The engine is an axial flow, dual shaft turbofan, with a 4.0:1 bypass ratio, rated at 14,750 lbs of thrust at sea level to ISA +20.
The BR 700.710A2.20 engine contains two main rotating assemblies (spools), a single stage low pressure (LP) fan driven by a two stage turbine and a ten stage high pressure (HP) compressor, driven by a two stage turbine. The HP spool provides an external drive for the accessories mounted on the accessory gearbox.
The engine is made up of eight modules as follows:
.
Fan assembly.

.
Fan case.

.
Intermediate case.

.
HP Compressor.

.
HP Turbine and combustion chamber.

.
LP Turbine and shaft.

.
Accessory Gearbox (AGB).

.
Bypass duct.


Each engine provides bleed air extraction, from either the 5th stage or the 8th stage of compression, for Air Conditioning and Pressurization, Cowl and Wing anti-icing and/or engine starts.
 
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