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ELECTRICAL Table of Contents May 06/2005 Flight Crew Operating Manual Volume 2 REV 2 CSP 100-6 07-00-01 Introduction ......................................................................................................................... 07-01-01 Electrical System................................................................................................................. 07-01-03 Description................................................................................................................. 07-01-03 Components and Operation....................................................................................... 07-01-03 Engine and APU Generators ..................................................................................... 07-01-03 External Power........................................................................................................... 07-01-03 Batteries.....................................................................................................................07-01-05 Power Centers ........................................................................................................... 07-01-05 Secondary Power Centers ......................................................................................... 07-01-06 Hydraulic Motor Driven Generator (HMDG) (Optional) .............................................. 07-01-06 Circuit Breaker Panels ............................................................................................... 07-01-06 Cockpit Floor Heaters ................................................................................................ 07-01-06 CB 1 Pilot Circuit Breaker Panel (Typical) ................................................................. 07-01-07 CB 2 Copilot Circuit Breaker Panel (Typical) ............................................................. 07-01-08 CB 3 Left Side Equipment Rack Circuit Breaker Panel (Typical)............................... 07-01-09 CB 4 Right Side Equipment Rack Circuit Breaker Panel (Typical) ............................07-01-10 CB 5 Left DC Power Center Circuit Breaker Panel (Typical) ..................................... 07-01-11 CB 6 Right DC Power Center Circuit Breaker Panel (Typical)................................... 07-01-11 Direct Current System.........................................................................................................07-01-12 DC Electrical System ................................................................................................ 07-01-12 DC Primary Architecture ............................................................................................07-01-13 Controls and Indications......................................................................................................07-01-14 External Power Control Panel.................................................................................... 07-01-14 Electrical Summary Page........................................................................................... 07-01-15 Electrical Control Panel.............................................................................................. 07-01-16 Electrical Synoptic Page ............................................................................................07-01-17 EICAS Messages....................................................................................................... 07-01-18 REV 2
ELECTRICAL Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6 07-01-01 REV 1 INTRODUCTION Primary DC electrical power is provided by two engine-driven generators and one APU-driven generator supplying 28 volt power to a split bus electrical system. An automatic electrical load-shedding system prevents generator overload and prolongs battery duration during a single or dual generator failure. Two main batteries power essential avionics, communication, and instrumentation. A separate battery powers the independent standby instrument system. An optional hydraulically driven electrical generator is available to provide electrical power generation in the event all engine and APU generator power is lost. A ground power unit can be connected to the aircraft to provide electrical power if desired. The only AC electrical power requirements are for passenger convenience. This power is provided by inverters located in the aft accessory compartment. The electrical system incorporates a split, multiple bus system for power distribution interconnected by contactors, fuses, and circuit breakers. These react automatically to isolate a malfunctioning circuit. ELECTRICAL Volume 2 Flight Crew Operating Manual Sep 13/2004 07-01-02 CSP 100-6 REV 1 INTRODUCTION (Cont) RIGHT CIRCUIT BREAKER PANEL www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：Bombardier_Challenger_Global_00-Electrical
