The invention discloses an aircraft wing folding device which is composed of an aircraft rack, a wing folding driving mechanism, a wing folding sliding rail mechanism and a main and auxiliary wing mechanism. The wing folding driving mechanism, the wing folding slide rail mechanism and the main and auxiliary wing mechanism are all fixed on the aircraft frame, and the main and auxiliary wing mechanism completes the wing folding action under the combined action of the wing folding driving mechanism and the wing folding slide rail mechanism. The problem of wing folding in a narrow space is solved, the main wing and the auxiliary wing can be unfolded into a plane in any space posture and can be contracted into an overlapped state in any space state, and the space is really saved.

    本发明公开了一种飞行器机翼折叠装置,由飞行器机架、机翼折叠驱动机构、机翼折叠滑轨机构、主辅翼机构组成;机翼折叠驱动机构、机翼折叠滑轨机构、主辅翼机构均固定于飞行器机架上,主辅翼机构在机翼折叠驱动机构和机翼折叠滑轨机构的共同作用下完成机翼折叠动作。本发明解决了狭小空间内机翼折叠问题,既可以使主辅翼在任意空间姿态下展开为平面,又可以使主辅翼在任意空间状态下收缩为重叠状态,真正节省了空间。


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    Titel :

    Aircraft wing folding device


    Weitere Titelangaben:

    一种飞行器机翼折叠装置


    Beteiligte:
    JIANG GUANGHUI (Autor:in) / GAO GUOHUA (Autor:in) / WEI JINFENG (Autor:in) / SONG CHUNXU (Autor:in)

    Erscheinungsdatum :

    29.03.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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