The invention discloses a novel light-weight power system applied to an aircraft, and relates to the technical field of novel power systems, the power system is used for providing power for propellers of the aircraft, a novel driving mode combining an engine and a power motor is adopted, fuel consumption is reduced, meanwhile, the flight smoothness of the aircraft can be improved, and the service life of the aircraft is prolonged. The engine and the propeller adopt the design scheme of parallel shafts, the characteristic of different shafts is met, and the propeller is suitable for being applied to airplanes. The lower transmission cavity is used for rotationally supporting the input shaft, and a double-end supporting mode can be adopted, so that the power transmission stability is guaranteed. When the whole machine cruising battery is insufficient, the output power can be improved for a long time to drive the power motor under the fixed rotating speed of the engine, and the battery electricity is compensated through power generation.

    本发明公开了一种应用于飞机的轻量化新型动力系统,涉及新型动力系统技术领域,动力系统用于为飞机的螺旋桨提供动力,采用发动机和动力电机结合的新型驱动方式,降低了燃油消耗,同时可以提高飞机飞行的平顺性,发动机和螺旋桨采用了平行轴的设计方案,满足了不同轴的特点,适配于飞机应用。下传动腔用于对输入轴进行旋转支撑,可以采用双端支撑的形式,保证动力传递稳定性。在整机巡航电池电量不足时,发动机固定转速下,可长时间提高输出功率驱动动力电机,通过发电来补偿电池的电量。


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    Title :

    Novel lightweight power system applied to airplane


    Additional title:

    一种应用于飞机的轻量化新型动力系统


    Contributors:
    SHI FANGHUI (author) / ZHOU KUN (author) / DONG XIANGLONG (author) / WENG LISHA (author) / LIU JIANFENG (author) / PAN ZHIXIN (author)

    Publication date :

    2025-03-07


    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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