An aircraft power system includes: a turbocharger including: a compressor for supplying combustion air to an internal combustion engine; a turbine operatively connected to the internal combustion engine to receive an exhaust flow from the internal combustion engine and convert energy of the exhaust flow into rotational power; and a turbine shaft operably connecting the turbine to the compressor to transfer at least some of the rotational power to the compressor. A generator is operably connected to the turbine shaft to receive at least some of the rotational power from the turbine shaft to generate electrical power. At least one electrically powered air mover is electrically connected to the generator to receive at least some of the power to generate thrust.

    一种飞行器动力系统包括:涡轮增压器,所述涡轮增压器包括:压缩机,所述压缩机用于向内燃发动机供应燃烧空气;涡轮,所述涡轮可操作地连接到内燃发动机以从所述内燃发动机接收排气流并将所述排气流的能量转换为旋转动力;以及涡轮轴,所述涡轮轴将所述涡轮可操作地连接到所述压缩机以将至少一些所述旋转动力传递到所述压缩机。发电机可操作地连接到所述涡轮轴以从所述涡轮轴接收至少一些所述旋转动力以产生电力。至少一个电动空气增流器电连接到所述发电机以接收至少一些所述电力以产生推力。


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    Title :

    Electric distributed propulsion using exhaust gas recovery power


    Additional title:

    使用排气回收动力的电动分布式推进


    Contributors:

    Publication date :

    2022-09-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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