The invention relates to the technical field of unmanned aerial vehicles, and particularly discloses a long-endurance large-load-ratio combined vertical take-off and landing unmanned aerial vehicle which comprises a fixed-wing task aircraft and a vertical take-off and landing propeller. The vertical take-off and landing propulsion machine is used for assisting the fixed-wing task aircraft to take off and land, a docking device is arranged on the vertical take-off and landing propulsion machine, and the docking device is used for being docked with the fixed-wing task aircraft when the fixed-wing task aircraft takes off and lands; the fixed-wing task aircraft is provided with a front fuselage and a rear fuselage, a hinged connecting piece is arranged between the front fuselage and the rear fuselage, and the front fuselage and the rear fuselage are connected through the hinged connecting piece. The front fuselage and the rear fuselage are respectively provided with a first wing and a second wing, and the first wing and the second wing are in tandem wing layout; according to the combined vertical take-off and landing unmanned aerial vehicle with the long endurance and the large load ratio, autonomous take-off and landing in a narrow space are achieved, take-off and landing are not limited by sites, and the combined vertical take-off and landing unmanned aerial vehicle has very important significance on future development of the unmanned aerial vehicle.

    本发明涉及无人机技术领域,具体公开一种长航时大载荷比的组合式垂直起降无人机,包括固定翼任务机和垂直起降推进机;垂直起降推进机用于协助固定翼任务机起飞和降落,垂直起降推进机上配置有对接装置,对接装置用于在固定翼任务机起飞和降落时与固定翼任务机对接;固定翼任务机具有前机身和后机身,前机身和后机身之间配置有铰接连接件,前机身和后机身通过铰接连接件连接;前机身和后机身上分别具有第一机翼和第二机翼,第一机翼和第二机翼为串列翼布局;该长航时大载荷比的组合式垂直起降无人机实现了其在狭小空间的自主起降,起飞与降落不必受到场地的限制,对无人机在未来发展有着十分重要的意义。


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    Titel :

    Combined vertical take-off and landing unmanned aerial vehicle with long endurance and large load ratio


    Weitere Titelangaben:

    一种长航时大载荷比的组合式垂直起降无人机


    Beteiligte:
    LIU KUN (Autor:in) / CAO MINGZHI (Autor:in) / WANG CHUNQIANG (Autor:in) / CHEN BAIHUI (Autor:in) / WEI JINGBO (Autor:in)

    Erscheinungsdatum :

    2023-11-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



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