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

时间:2011-10-31 12:02来源:蓝天飞行翻译 作者:公务机 点击:
  


 POWER PLANT Table of Contents  Vol. 2  19.00.1 
Oct 05/06 

TABLE OF CONTENTS
Page
TABLE OF CONTENTS 19.00.1

DESCRIPTION
General 19.10.1 Flat-Rated Thrust 19.10.1 Engine Construction 19.10.1 Description 19.10.1 Engine Fuel System 19.10.3 Description 19.10.3 Components and Operation 19.10.3 Automatic Performance Reserve System 19.10.5 Description 19.10.5 Operation 19.10.6 Engine Oil System 19.10.6 Description 19.10.6 Components and Operation 19.10.6 Engine Bleed Air System 19.10.11 Description 19.10.11 Components and Operation 19.10.11 Engine Starting System 19.10.12 Description 19.10.12 Components and Operation 19.10.13 Ignition System 19.10.15 Description 19.10.15 Operation 19.10.15 Vibration Monitoring System 19.10.16 Description 19.10.16 Operation 19.10.17 Thrust Levers 19.10.17 Description 19.10.17 Operation 19.10.17 Thrust Reverser System 19.10.19 Description 19.10.19 Operation 19.10.19 Controls and Indicators 19.10.23 Engine Starting 19.10.23 Engine Speed Controls 19.10.24


 POWER PLANT Table of Contents  Vol. 2  19.00.2 
Oct 05/06 

Page

DESCRIPTION
Thrust Levers 19.10.25 Reverse Thrust 19.10.26 Oil System 19.10.26 EICAS Page 19.10.27
EICAS Messages 19.10.31

SUMMARY
Power Supply and Circuit Breaker Summary 19.20.1

LIST OF ILLUSTRATIONS
DESCRIPTION
Figure 19.10.1 Flow Distribution 19.10.2 Figure 19.10.2 Engine Fuel System . Schematic 19.10.4 Figure 19.10.3 ENGINE CONTROL Panel 19.10.5 Figure 19.10.4 ENGINE CONTROL Panel 19.10.6 Figure 19.10.5 Oil System Schematic 19.10.8 Figure 19.10.6 Oil Replenishment System 19.10.10 Figure 19.10.7 Engine Bleed Air System . Schematic 19.10.12 Figure 19.10.8 Starting System . Schematic 19.10.13 Figure 19.10.9 Engine Start/Ignition Panel 19.10.14 Figure 19.10.10 Ignition System 19.10.16 Figure 19.10.11 ENGINE CONTROL Panel 19.10.17 Figure 19.10.12 Thrust Levers 19.10.19 Figure 19.10.13 Thrust Reverser Operation 19.10.21 Figure 19.10.14 GND SPOILERS/THRUST REVERSER Panel 19.10.22 Figure 19.10.15 Engine Start/Ignition Panel 19.10.23 Figure 19.10.16 ENGINE CONTROL Panel 19.10.24 Figure 19.10.17 Thrust Levers 19.10.25 Figure 19.10.18 GND SPOILERS/THRUST REVERSER Panel 19.10.26 Figure 19.10.19 Impending Bypass and Chip Detector Annunciators (JB5) 19.10.26 Figure 19.10.20 N1 Indications 19.10.27 Figure 19.10.21 ITT Indications 19.10.28 Figure 19.10.22 N2 Indications 19.10.29 Figure 19.10.23 Engine Secondary Indications 19.10.30


 POWER PLANT Description  Vol. 2  19.10.1 
Oct 05/06 

The Challenger 605 is equipped with two General Electric CF34-3B high-bypass ratio turbofan engines.
The dual-assembly engine consists of a fan rotor (N1) and a compressor rotor (N2). The N1 rotor is
comprised of a single-stage fan connected through a shaft to a four-stage low-pressure turbine. The N2 rotor is a 14-stage axial flow compressor connected through a shaft to a two-stage high-pressure turbine. The accessory gearbox is mechanically driven by the N2 compressor.
 
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