The invention discloses a tilting type electric vertical take-off and landing aircraft with foldable airfoils and an operation method. Comprising a fuselage, a fixed section wing arranged on the fuselage, a folding section wing connected to the fixed section wing through a wing folding assembly, a vertical fin arranged at the tail of the fuselage, a fixed section horizontal tail arranged on the vertical fin and a folding section horizontal tail connected to the fixed section horizontal tail through a horizontal tail folding assembly. The conversion of the aircraft among a folding mode, a helicopter mode and a fixed-wing aircraft mode can be realized under the action of the wing folding assembly and the horizontal tail folding assembly, a front-end rotor wing is arranged on the fixed-section wing, a middle-end rotor wing is arranged on the folding-section wing, and a rear-end rotor wing is arranged on the folding-section horizontal tail. When the aircraft is parked on the ground, the folding section wings and the folding section horizontal tail can be folded, so that the parking space needed by the aircraft is reduced, the requirement for special infrastructures is lowered, the cost is saved, the aircraft can be more easily integrated into the current limited space of a city, and the operation flexibility is enhanced.

    本发明公开了一种翼面可折叠的倾转类电动垂直起降飞行器及操作方法,包括机身、设置在机身上的固定段机翼、通过机翼折叠组件连接在固定段机翼上的折叠段机翼、设置在机身尾部的垂尾、设置在垂尾上的固定段平尾以及通过平尾折叠组件连接在固定段平尾上的折叠段平尾,通过机翼折叠组件、平尾折叠组件的作用可实现飞行器在折叠模式、直升机模式以及固定翼飞机模式间的转换,固定段机翼上设置有前端旋翼,折叠段机翼上设置有中端旋翼,折叠段平尾上设置有后端旋翼。本飞行器在地面停放时,折叠段机翼、折叠段平尾可折叠,从而减小飞行器所需停放空间,降低对专用基础设施的需求,从而节省成本,使其更容易融入城市当前有限的空间,增强了操作灵活性。


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    Title :

    Tilting type electric vertical take-off and landing aircraft with foldable airfoils and operation method of tilting type electric vertical take-off and landing aircraft


    Additional title:

    一种翼面可折叠的倾转类电动垂直起降飞行器及操作方法


    Contributors:
    MOU XIAOWEI (author) / WU XIMING (author) / SUN XIUWEN (author) / LI BO (author) / XU YUE (author) / LI ZHIQUAN (author) / SHI JINSHUAI (author) / LI YINGHUI (author)

    Publication date :

    2025-03-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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