The invention relates to a propulsion assembly (151) for an aircraft having a T-shaped chassis (156) with a horizontal structure (156a) and a vertical structure (156b), a gearbox (155) secured to the front of the chassis (156), and a propulsion system (150) having the following propulsion elements: an electric motor (154a) driving components of the gearbox (155), a fuel cell (154b), a tank and a cooling system (154d), the advancing element (154a-d) is fastened below the horizontal structure (156a) and against the vertical structure (156b) by fastening means. By such an arrangement, each propulsion element is readily accessible via the sides of the chassis during maintenance operations.

    本发明涉及一种用于飞行器的推进组件(151),其具有带水平结构(156a)和竖直结构(156b)的T形底架(156)、紧固到底架(156)的前部的齿轮箱(155)以及推进系统(150),推进系统具有以下推进元件:驱动齿轮箱(155)的部件的电动马达(154a)、燃料电池(154b)、储罐和冷却系统(154d),其中,推进元件(154a-d)由紧固装置紧固在水平结构(156a)下方并抵靠竖直结构(156b)。通过这样的布置,在维护操作期间容易经由底架的侧面通达每个推进元件。


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    Titel :

    Propeller propulsion assembly for aircraft


    Weitere Titelangaben:

    用于飞行器的螺旋桨推进组件


    Beteiligte:
    CASAGNE J E RU ME (Autor:in) / WINCHES FRANK (Autor:in) / SAPELA LEONARDO (Autor:in) / FUKASAKU KOSAKU (Autor:in) / AMARGEER RICHARD (Autor:in)

    Erscheinungsdatum :

    31.05.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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