The invention relates to the technical field of aircraft structure design, in particular to an actuating folding wing and an aircraft. The actuation folding wing provided by the embodiment of the invention comprises an actuator, an inner wing box and an outer wing box, the actuator is provided with a fixed connecting piece and a driving piece which are rotationally connected, and the inner wing box is connected with the fixed connecting piece, so that the actuator is fixedly connected with the inner wing box. The outer wing box is connected with the driving part so that the driving part can drive the outer wing box to rotate around the shaft, the inner wing box serves as a supporting end of the folding wing, the outer wing box serves as a wing surface folding end, then the outer wing box can rotate by a preset angle relative to the inner wing box according to requirements, the folding and unfolding functions of the folding end are achieved, and the problem of adaptability of a high-aspect-ratio wing to an airport can be effectively solved. The aircraft provided by the invention comprises the actuating folding wing, so that the aircraft also has the technical effects.

    本申请涉及飞机结构设计技术领域,尤其涉及一种作动折叠翼及飞行器。本申请实施例提供的作动折叠翼,包括作动器、内翼盒以及外翼盒。作动器具有转动连接的固定连接件和驱动件,内翼盒与固定连接件连接,以使作动器与内翼盒紧固连接。外翼盒与驱动件连接,以使驱动件驱动外翼盒绕轴转动,内翼盒为折叠翼的支持端,外翼盒为翼面折叠端,进而外翼盒可根据需求相对内翼盒转动预设角度,实现折叠端的折叠与展开功能,可有效地解决了大展弦比机翼与机场适应性的问题。本申请提供的飞行器,包括上述的作动折叠翼,因此也具有上述的技术效果。


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    Title :

    Actuating folding wing and aircraft


    Additional title:

    作动折叠翼及飞行器


    Contributors:
    ZHANG GUANGXIN (author) / LIU TIANQI (author) / XI XIAOBO (author) / WANG YIFAN (author) / GAO LIMIN (author)

    Publication date :

    2024-03-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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