DRONE HAVING A COUPLED PROPULSION SUPPORT
    2.
    发明申请

    公开(公告)号:US20170129601A1

    公开(公告)日:2017-05-11

    申请号:US15345292

    申请日:2016-11-07

    Applicant: PARROT DRONES

    Abstract: The invention relates to a rotary-wing drone (10) comprising a drone body (30) that comprises an electronic circuit board controlling the flight of the drone, four link arms (36) comprising a propulsion unit (38) at their ends, two propulsion units each having a propeller (12) that rotates in the clockwise direction and two propulsion units each having a propeller that rotates in the anticlockwise direction, the propulsion units that have propellers that rotate in the same direction being positioned on the same diagonal line. The drone comprises a propulsion support (32) comprising the link arms (36) and a central hub (34), two pairs of symmetrical link arms each extending on either side of the central hub, the central hub (34) being capable of being coupled to the drone body (30), and the propulsion support (32) having at least one torsional bending direction extending in the horizontal plane.

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