ROTARY-WING VEHICLE AND SYSTEM
    1.
    发明申请

    公开(公告)号:US20210009279A1

    公开(公告)日:2021-01-14

    申请号:US16509707

    申请日:2019-07-12

    Applicant: GeoScout, Inc.

    Abstract: A lift producing multi-rotor apparatus with a single gear, central drive gear unit actuating gear driven rotor-shaft units having pitch-controlled rotor heads where the rotor units are disposed directly opposite from each other, the direction of rotation of opposing rotor units are opposite from each other, and where the rotational-disk defined by each rotor overlaps two adjacent rotational disks.

    ROTARY-WING VEHICLE AND SYSTEM
    2.
    发明申请

    公开(公告)号:US20170247107A1

    公开(公告)日:2017-08-31

    申请号:US15056408

    申请日:2016-02-29

    Applicant: GeoScout, Inc.

    Abstract: An apparatus comprising a body defining a first vertical axis, two or more frame members each having a longitudinal axis and having an inner-end and an outer-end connected to the body at the inner-end and where a first horizontal geometrical plane is generally coincident with the longitudinal axis of each of the two or more frame members and where the first horizontal geometrical plane is generally orthogonal to the first vertical axis, two or more rotary-wings each comprising one or more blades whose rotation defines a first rotational axis which is configurable to be nearly parallel with the first vertical axis and comprising a second rotational axis which is configurable to be approximately parallel first horizontal geometrical plane where a first of the two or more rotary-wings having a blade-inner-end and a first blade-outer-end rotatably connected by its blade-inner-end to a first transmission is disposed substantially on the outer-end of a first of the two or more frame members, a second of the two or more rotary-wings having a blade-inner-end and a blade-outer-end rotatably connected by its blade-inner-end to a second transmission is disposed substantially on the outer-end of a second of the two or more frame members, where each of the first rotational axes is disposed on the opposite side of plane which is coincident with the first vertical axis, where the direction of rotation of a first of the two or more rotary-wings about its first rotational axis is opposite of that of the second of the two or more rotary-wings about its first rotational axis, and, where the rotational disk defined by the rotation of the blade-outer-end of the first of the two or more rotary-wings is at least partially coincident with rotational disk defined by the rotation of the blade-outer-end of the second of the two or more rotary-wings.

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