The invention discloses a deformable wing parallel guide rail distributed driving telescopic mechanism, and relates to the technical field of aviation equipment technologies. The problems that an existing high-speed aircraft deformation wing cannot meet the deformation and bearing requirements of the high-speed aircraft deformation wing, and the contradiction between the height of a small wing type structure and a high-reliability large-tolerance telescopic mechanism cannot be solved are solved. A distributed motor provides rotation driving input for a driving transmission mechanism, the inner side of a nut is spirally connected with a lead screw, and then a telescopic wing is driven to achieve telescopic movement; meanwhile, on one hand, the multiple double-dovetail-groove cantilever guide rail assemblies fixedly connected with the telescopic wing inner plate do follow-up motion; and on the other hand, the second-stage cantilever guide rail assembly fixedly connected with the telescopic wing inner plate conducts follow-up movement. According to the mechanism, high-reliability large-tolerance linear motion of the wing under a heavy load condition can be realized, the functions of deformation driving, supporting, motion guiding and the like are provided for the wing, and the aerodynamic performance of an aircraft under different flight conditions and flight tasks is improved.

    一种变形翼并联导轨分布式驱动伸缩机构,它涉及航空设备技术技术领域。本发明解决了现有高速飞行器变形翼存在无法满足高速飞行器变形翼的变形与承载要求,且无法解决小翼型结构高度与高可靠大容差伸缩机构之间的矛盾的问题。本发明的分布式电机对驱动传动机构提供旋转驱动输入,丝母内侧与丝杆螺旋连接,进而带动伸缩翼实现伸缩运动;与此同时,一方面,与伸缩翼内板固定连接的多个双燕尾槽悬臂导轨组件进行随动运动;另一方面,与伸缩翼内板固定连接的二级悬臂导轨组件进行随动运动。本发明可实现大负载条件下机翼的高可靠大容差直线运动,为机翼提供变形驱动、支撑、运动导向等功能,提高飞行器在不同飞行条件、飞行任务下的气动性能。


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    Titel :

    Deformable wing parallel guide rail distributed driving telescopic mechanism


    Weitere Titelangaben:

    一种变形翼并联导轨分布式驱动伸缩机构


    Beteiligte:
    XIAO HONG (Autor:in) / GUO HONGWEI (Autor:in) / LI CHUNFENG (Autor:in) / JIANG YANG (Autor:in) / YANG GUANG (Autor:in)

    Erscheinungsdatum :

    2021-12-31


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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