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DESCRIPTION General 14−10−1 Bleed/AntiIce Synoptic 14−10−2 Components 14−10−2 AntiIce Panel 14−10−3 Ice Detection 14−10−4 Ice Detection Indication 14−10−5 Pneumatic AntiIcing 14−10−6 Cowl AntiIcing (CAI) 14−10−6 Engine Spinner 14−10−6 Cowl AntiIce Valves 14−10−6 CAI Operation 14−10−7 Wing AntiIcing (WAI) 14−10−8 Wing AntiIce Valves (WAIV) 14−10−8 WAI Operation 14−10−9 Crossbleed Valve (CBW) 14−10−9 WAI Failure Indications 14−10−10 Wing AntiIce Overheat 14−10−10 Wing AntiIce Fail 14−10−10 Wing AntiIce Low Heat 14−10−11 Slat AntiIcing 14−10−12 Slat AntiIce Operation 14−10−12 Electrical AntiIcing 14−10−13 Air Data Probes and Sensors 14−10−13 HBMU 14−10−13 Probes 14−10−15 Windshield Heat 14−10−16 Windshield Temperature Controller 14−10−16 Windshield Heat Panel 14−10−17 Modes of Operation 14−10−17 WarmUp Mode 14−10−17 Normal Regulating Mode 14−10−17 Windshield/Window Failure Indication 14−10−17 EICAS Philosophy 14−10−18 Ice and Rain EICAS Messages 14−10−19 ICE AND RAIN PROTECTION TABLE OF CONTENTS CHAPTER 14 14−00−1 Rev 3, Apr 25, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 14−00−1 Page TABLE OF CONTENTS EMS CIRCUIT PROTECTION CB − Ice System 14−20−1 ICE AND RAIN PROTECTION TABLE OF CONTENTS Flight Crew Operating Manual Rev 2A, Apr 11, 2005 CSP 700−5000−6 Volume 2 14−00−2 Page GENERAL Thermal antiicing, electrical antiicing, ice detection and alerting systems are provided for airplane ice and rain protection. Selections for antiice functions are made on the ANTIICE panel, located on the overhead panel. GF1410_001 AUTO OFF ON AUTO OFF ON AUTO OFF ON L COWL WING R COWL ANTI−ICE AUTO FROM L FROM R WING XBLEED Ice Detection Independent ice detection probes (2), located on the fuselage, sense the formation of ice. If ice is detected, the ice detectors automatically turn on the electrical heat to the various probes, signalling the Bleed Management Controllers (BMC) to activate wing antiice and operate a relay in the ANTIICE Control panel to activate cowl antiice. Pneumatic AntiIcing Hot air antiicing, provided by engine bleed air, through piccolo ducting, wing antiice valves and cowl antiice valves, prevents the formation of ice on the wing leading edge, slats and the engine intake cowls. Electrical AntiIcing Electrical antiicing is provided for Pitot Static Probes, Ice Detectors, Total Air Temperature (TAT) Probes, Heater/Brake Temperature Monitoring Units (HBMUs) and Angle of Attack (AOA) Vanes. Selections for the Pilot’s and Copilot’s Windshields and Side Windows heating, are made on the WINDSHIELD HEAT panel, located on the overhead panel. GF1410_002 R WINDSHIELD HEAT OFF/ ON RESET L OFF/ ON RESET Antiice system data is displayed on the BLEED /ANTIICE synoptic page and any faults or failures are displayed on EICAS and CAIMS. ICE AND RAIN PROTECTION Rev 3, Apr 25, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 14−10−1 BLEED/ANTI-ICE SYNOPTIC GF1410_003 WING ANTIICE CROSS BLEED VALVE (CBW) WING ANTIICE VALVE (WAIV) COWL ANTIICE VALVE (CAIV) For more information on BLEED System, refer to Chapter 2, AIR CONDITIONING and PRESSURIZATION. LP HP L R APU HP LP COND AIR BLEED/ANTIICE 40 PSI 40 PSI COMPONENTS CBW CAIV WAIV BMC ANTIICING TEMPERATURE SENSORS ICE DETECTORS PICCOLO DUCTS GF1410_004 TO EICAS ICE AND RAIN PROTECTION Flight Crew Operating Manual Rev 3, Apr 25, 2005 CSP 700−5000−6 Volume 2 14−10−2 ANTI-ICE PANEL Controls are provided on the ANTIICE www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：Bombardier_Global_000-Ice_and_Rain_Protection
