The invention discloses a ground effect aircraft which is provided with a ground effect wing, a plurality of wingtip buoys and a control system. The ground-effect wings may include a front ground-effect wing and a rear ground-effect wing. The ground-effect wings may generate a stabilizing moment on at least one wingtip buoy to stabilize the ground-effect aircraft. A plurality of wingtip pontoons may be dynamically coupled to the body. A plurality of wingtip pontoons may be dynamically coupled to each other. The dynamic coupling may allow the wingtip pontoons to move relatively independently of the body and one another to stabilize the ground effect aircraft. The ground effect aircraft may include a stabilizing wing.

    本发明公开了一种地效飞行器,具有地效机翼、多个翼梢浮筒以及控制系统。地效机翼可以包括前地效机翼和后地效机翼。地效机翼可以在至少一个翼梢浮筒上产生稳定力矩,以稳定该地效飞行器。多个翼梢浮筒可以动态联接到本体。多个翼梢浮筒可以彼此动态联接。动态联接可以允许翼梢浮筒相对独立于本体和彼此运动,从而稳定该地效飞行器。该地效飞行器可以包括稳定翼。


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    Titel :

    Ground effect aircraft


    Weitere Titelangaben:

    地效飞行器


    Beteiligte:

    Erscheinungsdatum :

    14.06.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B60V Luftkissenfahrzeuge , AIR-CUSHION VEHICLES / B64C AEROPLANES , Flugzeuge / B63B Schiffe oder sonstige Wasserfahrzeuge , SHIPS OR OTHER WATERBORNE VESSELS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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    LU RONGFEI / ZHAO YONGSHENG / ZHOU JIAN et al. | Europäisches Patentamt | 2023

    Freier Zugriff