A hybrid aircraft power plant includes a turbine engine having a first shaft configured to output power from the turbine engine, a bypass fan, and an electric machine. The hybrid aircraft power plant further includes a first mechanism configured to selectively engage the first shaft with a second shaft connected to the electric machine such that power is output from the turbine engine to the electric machine. The hybrid aircraft power plant further includes a second mechanism configured to selectively engage the first shaft with a third shaft connected to the bypass fan to output power from the turbine engine to the bypass fan.

    一种混合动力航空器动力装置包括涡轮发动机、旁路风扇和电机,该涡轮发动机具有配置成从涡轮发动机输出动力的第一轴杆。混合动力航空器动力装置进一步包括第一机构,该第一机构配置成选择性地将第一轴杆与连接到电机的第二轴杆接合,使得动力从涡轮发动机输出到电机。混合动力航空器动力装置进一步包括第二机构,该第二机构配置成选择性地将第一轴杆与连接旁路风扇的第三轴杆接合,以将动力从涡轮发动机输出到旁路风扇。


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    Title :

    Parallel hybrid power device with turbofan engine core


    Additional title:

    带有涡扇发动机核心的并联混合动力装置



    Publication date :

    2024-09-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen



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