A hybrid electric propulsion system and method are provided. More specifically, the present disclosure relates to a control system for a hybrid electric propulsion system of an aircraft configured to rapidly and automatically take action in response to a rapid electrical load change on a torque source, such as an engine. A method for operating a hybrid electric propulsion system of an aircraft is also provided.

    提供了一种混合电动推进系统和方法。更具体地,本公开涉及用于飞行器的混合电动推进系统的控制系统,其被构造为响应于扭矩源(例如发动机)上的快速电负载变化而快速且自动地采取动作。还提供了用于操作飞行器的混合电动推进系统的方法。


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    Titel :

    Fault tolerant hybrid electric propulsion system for aircraft


    Weitere Titelangaben:

    用于飞行器的容错性混合电动推进系统


    Beteiligte:

    Erscheinungsdatum :

    27.06.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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