The invention relates to an emergency-assisting helicopter power system and a transmission method. The helicopter power system comprises a turboshaft engine unit, the turboshaft engine unit comprises a plurality of turboshaft engines, each turboshaft engine comprises a turboshaft engine body and an electric starter rotationally connected with the turboshaft engine body, and the turboshaft engine body is further rotationally connected with a transmission system. The system further comprises an auxiliary motor and an airborne power unit. Through the arrangement of the airborne power unit, the emergency power demand, the starting power supply power demand and the helicopter power demand can be met, and meanwhile the weight and design complexity of a turboshaft engine and a transmission system can be reduced; the turboshaft engine and the airborne power unit form a fuel-electric hybrid propulsion system, so that the fuel utilization rate can be effectively improved, and the voyage of the helicopter is further improved.

    本发明涉及一种辅助应急的直升机动力系统及传动方法。所述直升机动力系统包括涡轴发动机组,所述涡轴发动机组包括若干涡轴发动机,所述涡轴发动机包括涡轴发动机本体和与所述涡轴发动机本体转动连接的电起动机,所述涡轴发动机本体还转动连接有传动系统,还包括辅助电机和机载电力单元。本发明通过机载电力单元的设置,可满足应急功率需求、起动电源功率需求、直升机用电需求,同时还可以减小涡轴发动机和传动系统的重量和设计复杂度;通过所述涡轴发动机与机载电力单元构成油电混合推进系统,可有效提高燃油利用率,进而提高直升机航程。


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    Title :

    Electrically-assisted emergency helicopter power system and transmission method


    Additional title:

    一种电辅助应急的直升机动力系统及传动方法


    Contributors:
    RUAN HUABO (author) / GUO QINGLIN (author) / SU ZHIMIN (author) / WANG XU (author) / CHENG BENLIN (author) / LI WEI (author)

    Publication date :

    2023-11-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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