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庞巴迪挑战者605公务机机组操作手册 CL605-防冰和排雨 ICE and RAIN PROTECTION

时间:2011-10-29 11:01来源:蓝天飞行翻译 作者:公务机 点击:
  


 ICE AND RAIN PROTECTION Table of Contents  Vol. 2  14.00.1 
Oct 05/06 

CHAPTER 14 - ICE AND RAIN PROTECTION
TABLE OF CONTENTS
Page
TABLE OF CONTENTS 14.00.1
DESCRIPTION
General 14.10.1 Wing Anti-Ice System 14.10.1 Description 14.10.1 Components and Operation 14.10.2 Engine Cowl Anti-Ice System 14.10.4 Description 14.10.4 Components and Operation 14.10.5 Windshield/Window Anti-Ice System 14.10.6 Description 14.10.6 Components and Operation 14.10.7 Air Data Probes and Sensors Anti-Icing 14.10.8 Description 14.10.8 Components and Operation 14.10.9 Ice Detection System 14.10.10 Description 14.10.10 Components and Operation 14.10.11 Controls and Indicators 14.10.11 ANTI-ICE Panel 14.10.12 EICAS Messages 14.10.13 EICAS Messages – Wing Anti-Ice System 14.10.13 EICAS Messages – Engine Cowl Anti-Ice System 14.10.13 EICAS Messages – Windshield/Window Anti-Ice System 14.10.13 EICAS Messages – Air Data Probes and Sensors Anti-Icing 14.10.14 EICAS Messages – Ice Detection System 14.10.14
SUMMARY
Power Supply and Circuit Breaker Summary 14.20.1
LIST OF ILLUSTRATIONS
DESCRIPTION
Figure 14.10.1 Wing Anti-Ice System 14.10.2 Figure 14.10.2 Wing Anti-Ice Components 14.10.3 Figure 14.10.3 Cowl Anti-Ice System 14.10.5


 ICE AND RAIN PROTECTION Table of Contents  Vol. 2  14.00.2 
Oct 05/06 

Page 
LIST OF ILLUSTRATIONS 
DESCRIPTION 
Figure 14.10.4  Windshield/Window Anti-Ice System  14.10.7 
Figure 14.10.5  Air Data Probes and Sensors Anti-Icing System  14.10.9 
Figure 14.10.6  Ice Detectors  14.10.11 
Figure 14.10.7  ANTI-ICE Panel  14.10.12 

 

 ICE AND RAIN PROTECTION Description  Vol. 2  14.10.1 
Oct 05/06 

There are four anti-iced areas on the Challenger 605:
.
Wing leading edges;

.
Engine cowls;

.
Windshields and windows; and

.
Air data probes.


The wing leading edges and the engine intake cowls are anti-iced using engine 14th-stage bleed air. The windshields, windows and air data probes are anti-iced using electrical power. An ice detector system provides EICAS indications of ice accumulation.
Anti-icing of the aircraft tail surfaces is not required.
WING ANTI-ICE SYSTEM
Description
The left and right wing leading edges are anti-iced using pressure-regulated 14th-stage bleed air, distributed by wing anti-ice ducting and piccolo tubes. The system is controlled by the WING ANTI-ICE switch, located on the ANTI-ICE panel. The WING ANTI-ICE switch normally controls the left and right wing anti-ice valves, via wing-mounted control sensors and the wing anti-ice controller. An isolation valve allows both wings to be anti-iced from a single bleed source via a crossover duct. Panel lights and EICAS messages provide indications of system status during operation.
 
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