According to the compound flapping wing structure aircraft, through the compound structural design of wings, after the structures of the wings are improved, the wings have two or more forms during flapping, the wind resistance of the wings can be greatly reduced through one hollow-out mode, the lift force of the wings is optimized through one full filling mode, and the energy conversion and utilization rate is improved, the wings are provided with certain rigid structures and cambered surface structures and can work together with turbofans and the like, when the flight speed is increased, the wings have natural lift force, and the cruise speed is fully optimized.

    一种复式扑翼结构飞行器,通过对机翼的复式结构设计,使机翼在改善结构后,扑动时具备二种或多种形态,一种镂空使其风阻可以大大降低,一种机翼充分填充,优化机翼的升力,提高能量的转化和利用率,且机翼具备一定的刚性结构和弧面结构,可与涡扇等共同工作,当飞行速度提升时,机翼具备自然的升力,充分优化巡航速度。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Compound flapping wing structure aircraft


    Weitere Titelangaben:

    复式扑翼结构飞行器


    Erscheinungsdatum :

    2022-02-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Flat-flapping-wing flapping-wing aircraft

    WANG ZHICHENG | Europäisches Patentamt | 2015

    Freier Zugriff

    Flapping-wing aircraft

    SHUANG FENG / CAI YU / ZHANG ZHENHONG et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    Flapping wing aircraft

    XU JINGGE / YUAN SHUO / HU JIAXUN et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Four-wing flat-flapping flapping-wing aircraft

    WANG ZHICHENG | Europäisches Patentamt | 2015

    Freier Zugriff

    Flapping wing aircraft

    CHEN XIN / PENG LIHONG / ZHANG TONG et al. | Europäisches Patentamt | 2023

    Freier Zugriff