The invention relates to a potential energy catapulting method for an aircraft carrier aircraft, which comprises the following steps: collecting huge mechanical energy, converting the huge mechanical energy into potential energy in sections through an input energy conversion device, and dispersing and storing the potential energy in an energy storage device; potential energy in the energy storage device is released step by step, and the potential energy is converted into kinetic energy in a segmented mode through the output energy conversion device; the kinetic energy output device is started to convert kinetic energy into rotational energy in a grading mode, and the aircraft carrier aircraft is driven to take off. The method has the advantages of being large in stored energy, long in storage time, clean, free of pollution, short in launching time interval and the like, and can be particularly applied to a common aircraft carrier.

    本发明涉及一种于航母飞机的势能弹射的方法,包括采集巨大机械能通过输入能量转换装置分段转换为势能,并分散存储于储能装置中;储能装置中的势能逐级释放并通过输出能量转换装置将势能分段转换为动能;启动动能输出装置采用分级的方式将动能转换为转动能,带动航母飞机起飞。该方法具有储存能量大、储存时间长,清洁无污染,发射时间间隔短等优点,尤其是可以在普通航母上应用。


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    Titel :

    Potential energy ejection method for aircraft carrier aircraft


    Weitere Titelangaben:

    一种航母飞机的势能弹射的方法


    Beteiligte:
    LIU YOUGEN (Autor:in)

    Erscheinungsdatum :

    2022-11-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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