The invention discloses a power management method for an aviation series hybrid electric propulsion system. The aviation series-connection hybrid electric propulsion system comprises an aero-engine, a generator, a battery, a motor, a transmission and a propeller, efficiency is introduced into the aviation series-connection hybrid electric propulsion system as an evaluation index for the first time, and a system power management scheme is optimized in combination with the rotating speed of a variable power turbine. Compared with the prior art, the efficiency of the aero-engine can be improved, the loss is reduced, the optimal scheme of expected power distribution of the aero-engine and the battery under the determined voyage is obtained, and the performance of the hybrid electric propulsion aircraft is improved.

    本发明公开了一种航空串联混合电推进系统功率管理方法。所述航空串联混合电推进系统包括航空发动机、发电机、电池、电机、传动及推进器,本发明方法首次在航空串联混合电推进系统中引入㶲效率作为评价指标,并结合可变动力涡轮转速进行系统功率管理方案的优化。相比现有技术,本发明能够提高航空发动机的㶲效率,减少㶲损失,得到确定航程下航空发动机与电池期望功率分配的最优方案,提升混合电推进飞行器性能。


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    Title :

    Power management method for aviation series hybrid electric propulsion system


    Additional title:

    一种航空串联混合电推进系统功率管理方法


    Contributors:
    GU JIANGWEI (author) / XI JUNJIE (author) / WANG YONG (author) / ZHANG HAIBO (author)

    Publication date :

    2023-11-10


    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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