The invention relates to a lifting and floating integrated aircraft and a control method. The lifting and floating integrated aircraft has aerodynamic lifting force and air buoyancy at the same time, is supported by an external rigid support framework, and adopts a fuselage of a sweepback wing type pneumatic layout, foldable rigid truss frames, rotatable power systems, a payload, a battery system and a flight control device; each rotatable power system consists of an engine beam, an engine rod, an engine and a steering engine. According to the lifting and floating integrated aircraft disclosed by the invention, the sweepback wing type layout is adopted, a pocket body is filled with floating and lifting gas such as helium, and besides, the lifting and floating integrated aircraft has aerodynamic lifting force and air buoyancy at the same time.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Lifting and floating integrated aircraft and control method


    Beteiligte:
    ZHANG WEIPING (Autor:in) / WANG HUA (Autor:in) / ZHAI XIAOLI (Autor:in) / SU JIECHAO (Autor:in) / SHEN LINPING (Autor:in)

    Erscheinungsdatum :

    06.01.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64B LIGHTER-THAN-AIR AIRCRAFT , Luftfahrzeuge leichter als Luft



    Separable airship wing type lifting and floating integrated aircraft

    MA DONGLI / SUN FUDONG / YANG MUQING et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Rolling adjusting method for double-hull lifting and floating integrated aircraft

    MA DONGLI / SUN FUDONG / YANG MUQING et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Variable gravity center device suitable for lifting and floating integrated aircraft and pitching control method

    YANG MUQING / SUN FUDONG / MA DONGLI et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Floating and lifting integrated airship layout

    HWANG YONG-TAE / YIN TAO / XU SONGDING et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Wing and fuselage connecting structure of near space lifting and floating integrated aircraft

    SUN FUDONG / YANG MUQING / MA DONGLI et al. | Europäisches Patentamt | 2024

    Freier Zugriff