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。


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    Title :

    Power supply system and power supply method for aircraft


    Additional title:

    用于飞机的电源系统及供电方法


    Contributors:
    ZHANG GENG (author) / YANG YIWEI (author) / CHEN GUANGLIN (author) / YAN LINFANG (author) / XU YIHAO (author) / WANG BANGTING (author)

    Publication date :

    2024-11-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung



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