The invention discloses a deformable turbojet aircraft, and relates to the technical field of aircrafts. Comprising a fuselage made of a material capable of generating large-deflection deformation, a forward deformation mechanism capable of driving the fuselage to bend upwards, a reverse deformation mechanism capable of driving the fuselage to bend downwards, a plurality of turbojet thrust mechanisms evenly distributed in the circumferential direction of the fuselage and a plurality of forward deformation mechanisms. And the reverse deformation mechanism is in communication connection with the control system of the turbojet thrust mechanism. The deformable turbojet aircraft provided by the invention can improve the loading capacity and the trafficability at the same time.

    本发明公开了一种可变形的涡喷飞行器,涉及飞行器技术领域,包括由能够产生大挠度变形的材料制成的机身、能够驱动机身向上弯曲的正向变形机构、能够驱动机身向下弯曲的反向变形机构、多个绕机身周向均匀布设的涡喷推力机构以及与正向变形机构、反向变形机构和涡喷推力机构通信连接的控制系统。本发明提供的可变形的涡喷飞行器能够同时提高载荷能力与通过性。


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    Titel :

    Deformable turbojet aircraft


    Weitere Titelangaben:

    一种可变形的涡喷飞行器


    Beteiligte:
    MA YUE (Autor:in) / YAN XIAO (Autor:in) / TANG MUCHENG (Autor:in) / BU ZHIHENG (Autor:in) / ZHOU JINGWEN (Autor:in) / HE HUI (Autor:in)

    Erscheinungsdatum :

    26.04.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



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