A layered optimization management method for an all-electric aircraft energy system is characterized in that a set of control management system is designed for an energy architecture of a double-generator all-electric load, and the control management system comprises a flight management computer, an energy system management center, a load management center, a bottom layer controller, various sensors, generators and loads; the bottom layer controller comprises a generator controller and a power distribution and protection device. The control strategy is controlled according to the health state, and the flight safety of the aircraft is guaranteed; according to a full-electric aircraft generator grid-connected design, management control is carried out by taking efficiency as a control target on the basis of flight safety, and the energy efficiency of the system is improved.

    一种全电飞机能源系统分层优化管理方法,是针对双发电机全电负载的能源架构设计一套控制管理系统,所述控制管理系统包括飞管计算机、能源系统管理中心、负载管理中心、底层控制器、多种传感器、发电机和负载;所述的底层控制器包括发电机控制器以及配电及保护装置。本发明控制策略根据健康状态进行控制,保证飞机飞行安全;根据全电飞机发电机并网设计,在飞行安全基础上以效率为控制目标进行管理控制,提高系统能源效率。


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    Title :

    Layered optimization management method for energy system of all-electric aircraft


    Additional title:

    一种全电飞机能源系统分层优化管理方法


    Contributors:
    LI ZHENGHONG (author) / LIU RUI (author) / AI FENGMING (author) / BI WENYAN (author) / ZUO LINXUAN (author) / WANG GUAN (author) / LIN PENG (author) / YU XIKUI (author) / MIAO YUE (author) / WU TAO (author)

    Publication date :

    2023-10-10


    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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