The invention discloses a dismountable solar cell panel four-axis aircraft which is structurally characterized in that a solar cell panel is attached to the surface of a kt support plate; the upper end of a carbon fiber pressure bearing frame bears the solar cell panel and the kt support plate; the lower end of the carbon fiber pressure bearing frame is connected with a carbon fiber triangular pyramid arm; a motor is mounted at each of the left end and the right end of the carbon fiber triangular pyramid arm; propellers are connected onto the motors; a solar stabilized voltage supply and cache group is embedded in the middle of the carbon fiber pressure bearing frame; and the lower end of the solar stabilized voltage supply and cache group is connected with an undercarriage. The aircraft has the technical effects: (1) the aircraft carries out unmanned monitoring aloft, and has wide applications in on-site plotting and detecting fields; (2) a GPS (global position system) position finder is employed, so that the aircraft can carry out fixed positioning and is used for transportation fields of communication, express and the like; and (3) the aircraft has the advantages of zero discharge, solar driving, good flight performance, low cost, long endurance, wide application and the like.


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    Titel :

    Dismountable solar cell panel four-axis aircraft


    Beteiligte:
    CAI ZHIHUA (Autor:in) / WANG QING (Autor:in) / TAO ZEXU (Autor:in) / YUAN QIANHUI (Autor:in) / YANG ZHIJIE (Autor:in) / WANG LIBIN (Autor:in) / YAN HAILONG (Autor:in) / LI XIAOLONG (Autor:in) / YANG HUA (Autor:in)

    Erscheinungsdatum :

    22.07.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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