The invention belongs to the technical field of design of parallel combined engine auxiliary power systems of aircrafts, and particularly relates to a parallel combined engine auxiliary power system of an aircraft and a control method of the parallel combined engine auxiliary power system of the aircraft. The system has higher energy utilization efficiency, lower internal thermal load and higher accessory efficiency, and can bring remarkable improvement and beneficial effects to an aircraft energy scheme.

    本申请属于飞机并联组合发动机辅助动力系统设计技术领域,具体涉及一种飞机并联组合发动机辅助动力系统及操控方法,采用电传动架构,相比于现有机械液压的系统架构,具有更高的能源利用效率、更低的内部热负荷和更高的附件效率,可为飞机能源方案带来显著的改进和有益效果。


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    Title :

    Airplane parallel combination engine auxiliary power system and control method


    Additional title:

    一种飞机并联组合发动机辅助动力系统及操控方法


    Contributors:
    LIU XUYANG (author) / GUO SHUAIFAN (author) / HE JIAQIAN (author)

    Publication date :

    2024-05-17


    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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