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
┣━━┻━━━━━━━━━━━━━━━━━━━━━━━━━┫ ┃ ┃
┃~ i t L_AC ESS FEED-┏━━━━━━━━━━━━━━━━┳━━━━━━┳━━━━━━━━━┓
┃I -~ A318 ┃ELECTRICAL ┃1.24.10 P 3 ┃
┃ .*,,.8, ,, ~L,~ A319 ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃
┃ ┃ ┣━━━━┳━━━━┫
┃ A~7-~'M" A321 ┃DESCRIPTION ┃SEQ 001 ┃REV 23 ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━┻━━━━┻━━━━┛
AC GENERATORS
MAIN GENERATORS
Two three-phase AC generators (GEN 1, GEN 2), one driven by each main engine through
an integrated drive, supply aircraft electrical power. Each generator can supply up to 90
KVA of power at 115 and 200 volts and 400 hertz.
A third generator (APU GEN), driven directly by the APU and producing the same output
as each main engine generator, can replace either or both main engine generators at any
time.
A Generator Control Unit (GCU) controls the output of each generator. The main functions
of each GCU are :
- Control the frequency and voltage of the generator output.
- Protect the network by controlling the associated Generator Line Contactor (GLC).
EXTERNAL POWER
A ground power connector near the nose wheel allows ground power to be supplied to all
bus bars.
A Ground Power Control unit (GPCU) protects the network by controlling the external power
contactor.
EMERGENCY GENERATOR
The blue hydraulic circuit drives an emergency generator that automatically supplies
emergency AC power to the aircraft electrical system if all three main generators fail. This
generator supplies 5 KVA of three-phase 115/200-volt 400-hertz power.
A Generator Control Unit (GCU) :
- keeps the emergency generator at a constant speed
- controls the generator's output voltage
- protects the network by controlling the emergency generator line contactor
- controls the emergency generator start-up
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃ ┃ ┃1.24.10 P 4 ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃I ~-Z A318 ┃ DESCRIPTIONLECTRICAL ┃SEQ 100 1 ┃I REV 31 ┃
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
AIRBUS A320 Flight Crew Operating Manual2(156)
