The invention discloses a foldable wing type tilting ducted unmanned aerial vehicle which comprises a fuselage, wings, empennages, canards, front ducts, rear ducts and foldable wing mechanisms, the wings are mounted in the middle of the fuselage, the empennages are mounted at the tail of the fuselage, the canards are mounted at the head of the fuselage, the two front ducts are symmetrically arranged at the two ends of the canards, and the two rear ducts are symmetrically arranged at the two ends of the canards. The two rear ducts are symmetrically arranged at the two ends of the empennage, the two folding wing mechanisms are symmetrically arranged in the middle of the wings, and the undercarriage is a front three-point type retractable undercarriage. The rollover problem caused by gust is avoided, the space occupied by shutdown is reduced, the space utilization rate of airports and naval vessels is increased, and transportation is convenient.

    本发明公开了一种可折叠机翼式倾转涵道无人机,包括机身、机翼、尾翼、鸭翼、前置涵道、后置涵道、折叠机翼机构,机翼安装在机身中部,尾翼安装在机身尾部,鸭翼安装在机身头部,两个前置涵道对称设于鸭翼的两端,两个后置涵道对称设置于尾翼两端,两个折叠机翼机构对称设于机翼中部,起落架为前三点式可收放起落架。本发明避免了突风引起的侧翻问题,减少了停机占用的空间,提高了机场、舰艇空间利用率,且便于运输。


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    Titel :

    Foldable wing type tilting ducted unmanned aerial vehicle


    Weitere Titelangaben:

    一种可折叠机翼式倾转涵道无人机


    Beteiligte:
    LIU YAOLONG (Autor:in) / XU SHANGRU (Autor:in) / ZHANG JIFA (Autor:in) / ZHENG YAO (Autor:in)

    Erscheinungsdatum :

    2024-01-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



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