The invention discloses a tilting ducted unmanned aerial vehicle, which comprises a fuselage, side wings are arranged in the middle of the fuselage, a horizontal empennage and a vertical empennage are arranged on the rear portion of the fuselage, tilting ducted fans are arranged on the side wings and the horizontal empennage, and a driving device connected with the tilting ducted fans is arranged on the fuselage. Tilting ducted fans are arranged on side wings and a horizontal tail wing of the tilting ducted unmanned aerial vehicle. During take-off and landing, the tilting ducted fans are perpendicular to the airfoil, airflow flows downwards to provide lift force, so that the tilting ducted unmanned aerial vehicle realizes vertical take-off and landing, and the requirements of the unmanned aerial vehicle on running and the surrounding environment are reduced. During level flight, the tilting ducted fans are parallel to airfoils, airflow flows backwards to provide thrust, the side wings of the unmanned aerial vehicle generate lift force, it is guaranteed that the tilting ducted unmanned aerial vehicle can fly at a high speed, and the tilting ducted unmanned aerial vehicle has the advantages of being high in speed and large in task radius.

    本发明公开了一种倾转涵道无人机,包括机身,机身的中部设有侧翼,机身的后部设有水平尾翼和垂直尾翼,侧翼和水平尾翼均设有倾转涵道风扇,机身设有与倾转涵道风扇相连的驱动装置。倾转涵道无人机的侧翼和水平尾翼均设有倾转涵道风扇。在起降时,倾转涵道风扇垂直翼面,气流向下流动提供升力,使倾转涵道无人机实现垂直起降,降低了无人机对跑到及周遭环境的要求。在平飞时,倾转涵道风扇平行翼面,气流向后流动提供推力,无人机的侧翼产生升力,保证倾转涵道无人机可高速飞行,使其具备速度快、任务半径大的优点。


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    Titel :

    Tilting ducted unmanned aerial vehicle


    Weitere Titelangaben:

    一种倾转涵道无人机


    Beteiligte:
    LI YIDONG (Autor:in) / CHEN ANQIANG (Autor:in) / TIAN HAO (Autor:in) / DENG JIE (Autor:in) / WANG BING (Autor:in)

    Erscheinungsdatum :

    2021-07-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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