The invention discloses an unmanned power parafoil with an adjustable mounting angle. The unmanned power parafoil comprises an electric winding mechanism, a suspension compartment and a parachute canopy, wherein the electric winding mechanism is arranged in the suspension compartment; a plurality of parachute ropes are arranged on the parachute canopy, and the parachute canopy is connected with the electric winding mechanism through the parachute ropes; the electric winding mechanism comprises a motor, a transmission mechanism, a left winding drum and a right winding drum; the motor is connected with an input end of the transmission mechanism; the transmission mechanism is provided with a two-way output shaft; two ends of the two-way output shaft are respectively connected with a winding-drum shaft arranged in the left winding drum, and a winding-drum shaft arranged in the right winding drum; an operation band is uniformly wound on each of the winding drums; the parachute bands are divided into four strands; two strands of parachute ropes are respectively connected with two ends of the operation band in the left winding drum, and the other two strands of parachute ropes are respectively connected with two ends of the operation band in the right winding drum. During flight, a mounting angle is adjusted in real time, so that the power parafoil can easily take off or land; the flying speed and the flying height of the power parafoil can be flexibly controlled when the power parafoil flies in air.


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    Titel :

    Unmanned power parafoil with adjustable mounting angle


    Beteiligte:
    LI QI (Autor:in) / ZHOU QINGYAN (Autor:in) / TIAN RUDONG (Autor:in)

    Erscheinungsdatum :

    02.12.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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