The invention discloses a vertical take-off and landing aircraft. The aircraft comprises a fuselage; the main wings are symmetrically arranged on the left side and the right side of the fuselage; the at least one supporting arm is symmetrically arranged below the main wings, and vertical take-off and landing power units are installed at the front end and the rear end of each supporting arm respectively and used for providing vertical take-off and landing power for the vertical take-off and landing aircraft; the empennage is positioned at the tail part of the fuselage and is provided with bilaterally symmetrical airfoils; the advancing power unit is arranged at the joint of the empennage and the tail part of the fuselage, and provides advancing power for the vertical take-off and landing aircraft; and the undercarriage is mounted at the bottom of the fuselage. According to the method, the power sources of the vertical take-off and landing aircraft in the vertical take-off and landing stage and the forward flight cruise stage are decoupled, the design difficulty of design of systems such as the structural design and the flight control algorithm of the vertical take-off and landing aircraft is lowered, and meanwhile the safety redundancy of the vertical take-off and landing aircraft on a power system is improved.

    本发明公开一种垂直起降航空器,包括:机身;对称设置在所述机身左右两侧的主翼;对称设置在所述主翼下方的至少一根支臂,所述支臂的前后两端分别安装有垂直起降动力单元,所述垂直起降动力单元用于为所述垂直起降航空器提供垂直起降的动力;位于所述机身尾部的具有左右对称翼型的尾翼;安装在所述尾翼与所述机身尾部连接处的前进动力单元,所述前进动力单元为所述垂直起降航空器提供前进的动力;以及安装在所述机身底部的起落架。本发明通过解耦垂直起降航空器在垂直起降阶段与前飞巡航阶段的动力来源,降低了垂直起降航空器结构设计、飞控算法等系统设计的设计难度,同时也提高了垂直起降航空器在动力系统上的安全冗余度。


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    Titel :

    Vertical take-off and landing aircraft


    Weitere Titelangaben:

    一种垂直起降航空器


    Beteiligte:
    LIU JUJIANG (Autor:in) / SU QINGPENG (Autor:in) / GUO XUYANG (Autor:in) / LI FU (Autor:in) / HUANG YU (Autor:in) / WANG PENG (Autor:in)

    Erscheinungsdatum :

    2022-12-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge