The invention relates to the technical field of aircrafts, and particularly discloses a vertical take-off and landing aircraft which comprises a wing-body-fused lifting body fuselage, a front wing, a rear wing and a stable empennage, and a two-degree-of-freedom propelled Y3 configuration composed of the front wing, the rear wing and the fuselage, the eVTOL is composed of two fixed lift propellers installed below a front wing and in the front of the center of gravity and a two-degree-of-freedom tilting thruster installed at the tail to solve the problem that an existing eVTOL of a Y3 structure cannot give consideration to a low-speed hovering mode and a cruising mode. A tandem-lifting body pneumatic configuration and a novel Y3 power configuration are combined to solve the problem that the contradiction between high pneumatic efficiency and large cargo capacity of the aircraft is difficult to balance; and finally, through side pneumatic optimization of the fuselage, up-and-down staggered design of front and rear wing tip winglets and design of a ring wing 21, the problem that an existing configuration easily generates large pneumatic resistance is solved.

    本发明涉及飞行器技术领域,特别公开了一种垂直起降飞行器,包括翼身融合的升力体机身、前机翼和后机翼、以及安定尾翼,通过前机翼、后机翼和机身组成的二自由度推进的Y3构型,由两个安装在前机翼下方、重心前部的固定升力推进器和一个安装在尾部的二自由度倾转推力器组成来解决现有Y3构型的eVTOL无法兼顾低速悬停模态与巡航模态的问题;并且采用串列‑升力体气动构型与新型Y3动力构型相结合来解决飞行器难以平衡高气动效率和大载货量之间的矛盾的问题;最后通过机身的侧部气动优化、前、后机翼梢小翼上下错开设计、以及环翼21设计来解决现有构型容易产生较大的气动阻力的问题。


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    Titel :

    Vertical take-off and landing aircraft


    Weitere Titelangaben:

    一种垂直起降飞行器


    Beteiligte:
    LIU KUN (Autor:in) / CHEN BAIHUI (Autor:in) / LI XINLIANG (Autor:in) / QIN ZIJIE (Autor:in) / LIANG JINFENG (Autor:in) / GUO HAOCHENG (Autor:in) / MO CHONGSEN (Autor:in)

    Erscheinungsdatum :

    2024-03-05


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U