The invention provides a combined-separate stratospheric aircraft system scheme. The system scheme mainly comprises a high-altitude balloon, a solar powered unmanned air vehicle and a connecting rope, wherein the high-altitude balloon comprises a bag main body and a cable net structure which is outside the bag main body; and the solar powered unmanned air vehicle is the core of the whole platform and mainly comprises a structure subsystem, an energy subsystem, an avionic flight control subsystem, a propelling subsystem and a loading subsystem, which are arranged on a stabilizer of the solar powered unmanned air vehicle. According to the combined-separate stratospheric aircraft system scheme provided by the invention, the platform takes off through the high-altitude balloon; and the high-altitude balloon is separated from the solar powered unmanned air vehicle through an explosion device after the platform reaches a fixed flying height. The solar powered unmanned air vehicle flies for a long time through parts carried on the unmanned air vehicle and returns to a fixed point through its avionic flight control subsystem after the flying task is finished. Through the adoption of the combined-separate stratospheric aircraft system scheme provided by the invention, the performance of the solar powered unmanned air vehicle during executing the flying task can be greatly improved.


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    Titel :

    Combined-separate stratospheric aircraft system scheme


    Beteiligte:
    ZHU MING (Autor:in) / SUN KANGWEN (Autor:in)

    Erscheinungsdatum :

    07.10.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64B LIGHTER-THAN-AIR AIRCRAFT , Luftfahrzeuge leichter als Luft / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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