The invention discloses a wing tilting device of a multi-propeller tilting wing configuration aircraft and the aircraft. A torque transmission mechanism comprises a tubular beam, a tubular beam tilting adapter and a tilting adapter which are fixedly connected; a torque transmission assembly in the driving mechanism is hinged to the tilting connector, torque output by the steering engine is transmitted to a torque transmission mechanism, and the tubular beam is driven to rotate around the axis of the tubular beam. The two ends of the tubular beam are symmetrically provided with a set of fuselage connecting assemblies, bearings of the fuselage connecting assemblies are arranged on the tubular beam in a sleeving mode, and loads of the wings are transmitted to the fuselage through the tubular beam; a wing mounting tube in the wing connecting assembly penetrates through a central through hole of the tubular beam, and two ends of the wing mounting tube are respectively inserted into wings on two sides and are fixedly connected with the wings; the two wing tilting adapters are fixed at the two ends of the tubular beam and are fixedly connected with the wings at the corresponding positions. The wing tilting mechanism solves the problems that an existing wing tilting mechanism requires a steering engine to bear large torque in a fixed wing mode and a helicopter mode, the requirement for the steering engine is high, and the service life of the steering engine is shortened.

    本发明公开一种多桨倾转机翼构型飞行器的机翼倾转装置以及飞行器,扭矩传输机构包括固连的管梁、管梁倾转转接头和倾转接头;驱动机构中扭矩传输组件与倾转接头铰接,将舵机输出的扭矩传输至扭矩传输机构,带动管梁绕其自身轴线转动;管梁的两端对称设置有一组机身连接组件,机身连接组件的轴承套装在管梁上,通过管梁将机翼的载荷传递到机身上;机翼连接组件中的机翼安装管穿过管梁的中心通孔,两端分别插入两侧机翼并与机翼固定连接;管梁两端固定2个机翼倾转转接件,并与对应位置的机翼固定连接。本发明实施例解决了现有机翼倾转机构,在固定翼模式及直升机模式下要求舵机承受较大扭矩,对舵机的要求较高,降低了舵机的使用寿命等问题。


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    Title :

    Wing tilting device of multi-propeller tilting wing configuration aircraft and aircraft


    Additional title:

    一种多桨倾转机翼构型飞行器的机翼倾转装置以及飞行器


    Contributors:
    LIU JIFU (author) / MA DONGLIN (author) / LUO JUN (author) / HOU XIANGMIN (author) / FU LICHUN (author)

    Publication date :

    2024-02-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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