The invention provides a separation type hybrid lift high-speed aircraft which comprises a fuselage and wings, vertical tails are symmetrically arranged on the upper portion and the lower portion of the tail of the fuselage respectively, the separation type hybrid lift high-speed aircraft further comprises four propelling power devices, the four propelling power devices are installed on the two wings and the two vertical tails respectively, the fuselage is a lift body fuselage, and the two wings and the two vertical tails are symmetrically arranged on the fuselage. The two sides of the fuselage and the wings are in smooth transition and are fused into a whole, and a wing body fusion body is formed. The aircraft has the beneficial effects that the wing body is combined with the fixed wing surface with the large lift-drag ratio and the propeller, stable transition and operation of the aircraft in the vertical take-off and landing stage and the forward flight stage are achieved to the maximum extent, the flight modes can be flexibly converted, vertical take-off and landing, hovering and forward flight are achieved, and the aircraft has a wide application prospect. And moreover, switching between a fixed wing mode and a rotor wing mode can be realized according to task requirements, so that the optimal flight efficiency and performance are realized.

    本发明提供一种分离式混合升力高速飞行器,包括机身和机翼,所述机身尾部上下各对称设置有一个垂直尾翼,还包括四个推进动力装置,四个所述推进动力装置分别安装于两个机翼和两个垂直尾翼上,所述机身为升力体机身,所述机身两侧与机翼光滑过渡,融合于一体,形成翼身融合体。本发明的有益效果是:本发明由翼身融合大升阻比固定翼面与螺旋桨相结合,最大限度地实现了飞行器在垂直起降阶段和前飞阶段的平稳过渡和运行,可灵活转换飞行模式,实现垂直起降、悬停和向前飞行,而且可以根据任务需求在固定翼和旋翼模式之间切换,以实现最佳的飞行效率和性能。


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    Title :

    Separated hybrid lift high-speed aircraft


    Additional title:

    一种分离式混合升力高速飞行器


    Contributors:
    SU RUI (author) / MA CHAO (author) / JIN PENGLEI (author)

    Publication date :

    2025-03-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U




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