The invention relates to the technical field of aviation aircrafts, in particular to a tilt-rotor aircraft capable of vertically taking off and landing and a working method thereof.The tilt-rotor aircraft capable of vertically taking off and landing comprises a fuselage, the fuselage is provided with a fixed wing and an empennage, the fixed wing is connected with an outer wing, and the fixed wing, the empennage and the outer wing are each provided with a plurality of rotors; the tilting assembly comprises a deflection mechanism and a locking mechanism; the butt joint assembly comprises a wing butt joint mechanism and an electrical connection mechanism; and the rotating assembly is used for driving the rotor wings to rotate. The distributed rotor design is adopted, and more stable vertical take-off and landing and horizontal flight performance is provided through cooperative work. The aircraft can be seamlessly switched between a vertical take-off and landing mode and a horizontal flight mode, the structural arrangement in the wings is simplified through the multi-section wing structural design, and the overall energy efficiency ratio of the aircraft is increased through the optimized aerodynamic layout.

    本发明涉及航空飞行器技术领域,尤其为一种可垂直起降的倾转旋翼飞行器及其工作方法,其中一种可垂直起降的倾转旋翼飞行器包括:机身,机身设置有固定翼和尾翼,固定翼连接有外翼,固定翼、尾翼和外翼上均设置有若干个旋翼;倾转组件,倾转组件包括偏转机构和锁定机构;对接组件,对接组件包括机翼对接机构和电性连接机构;转动组件,转动组件用于带动旋翼进行转动。本发明通过采用分布式旋翼设计,通过协同工作提供更稳定的垂直起降和水平飞行性能。使其能够在垂直起降和水平飞行模式之间无缝转换,多段式机翼结构设计则简化了机翼内部的结构布置,并通过优化的空气动力学布局,提升了飞行器的整体能效比。


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    Title :

    Tilt-rotor aircraft capable of vertically taking off and landing and working method of tilt-rotor aircraft


    Additional title:

    一种可垂直起降的倾转旋翼飞行器及其工作方法


    Contributors:
    ZHAO XIAOXIA (author) / GAO ZHANHANG (author)

    Publication date :

    2025-05-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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