The invention discloses a power supply system for an aircraft. The power supply system comprises a plurality of main generators located in a left channel and a right channel; an auxiliary power unit (APU) starter generator (ASG) located in the right channel and used for supplying power when the main generator fails; the plurality of transformer rectifiers (TRU) are positioned on the left channel, the right channel and the emergency channel; the plurality of ATUs are positioned on the left channel, the right channel and the emergency channel; and a ram air turbine (RAT) located in the emergency aisle. A method of powering an aircraft using the power supply system is also disclosed.
本发明公开了一种用于飞机的电源系统,包括:位于左通道和右通道的多台主发电机;位于右通道的辅助动力装置(APU)起动发电机(ASG),用于在主发电机失效时供电;位于左通道、右通道和应急通道的多台变压整流器(TRU);位于左通道、右通道和应急通道的多台自耦变压器(ATU);以及位于应急通道的冲压空气涡轮(RAT)。还公开了利用电源系统来对飞机供电的方法。
Power supply system and power supply method for aircraft
用于飞机的电源系统及供电方法
2024-11-01
Patent
Electronic Resource
Chinese
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