Adjustable Weight Distribution for Drone
    2.
    发明申请
    Adjustable Weight Distribution for Drone 有权
    无人机的可调重量分布

    公开(公告)号:US20160264234A1

    公开(公告)日:2016-09-15

    申请号:US14643070

    申请日:2015-03-10

    Abstract: Apparatus, methods, and systems for adjusting a center of mass of a drone may include a balance track and a repositionable weight. The balance track may extend outwardly from a central region of the drone. The balance track may include a plurality of weight-balance fixation positions. The repositionable weight may be configured to be secured at any one of the plurality of weight-balance fixation positions. Various embodiments may include receiving a weight-distribution input relating to balancing the drone. A weight-distribution balance profile may be determined, based on the weight-distribution input, for determining whether a repositionable weight should be repositioned among a plurality of weight-balance fixation positions on a balance track extending outwardly from a central region of the drone. The repositionable weight may be repositioned according to the weight-distribution balance profile.

    Abstract translation: 用于调节无人机质量中心的装置,方法和系统可以包括平衡轨道和可重定位重量。 平衡轨道可以从无人机的中心区域向外延伸。 平衡轨道可以包括多个重量平衡固定位置。 可重定位重量可以被配置为固定在多个重量平衡固定位置中的任何一个处。 各种实施例可以包括接收与平衡无人机相关的权重分布输入。 可以基于重量分布输入来确定重量分布平衡曲线,用于确定是否可以在从无人机的中心区域向外延伸的平衡轨道上的多个重量平衡固定位置之间重新定位可重新定位的重量。 可重新定位的重量可以根据重量分布平衡曲线重新定位。

    Gimbaled Universal Drone Controller
    3.
    发明申请

    公开(公告)号:US20180024570A1

    公开(公告)日:2018-01-25

    申请号:US15219116

    申请日:2016-07-25

    Inventor: Donald Hutson

    Abstract: Various embodiments are disclosed of a device for use on an unmanned aerial vehicle (drone) including two or more gimbals, a gimbal processor, an inertial measurement unit, and a communication connection. The two or more gimbals are pivotally coupled to rotate orthogonally relative to each other. An inner gimbal of the two or more gimbals may support an inner platform for receiving components thereon. An outer gimbal of the two or more gimbals may be pivotally coupled to the drone. The gimbal processor is mounted on the inner platform, wherein the gimbal processor is configured to control pivotal movement of the two or more gimbals. The inertial measurement unit may be fixed relative to the inner platform and coupled to the gimbal processor. The communication connection may be coupled to the gimbal processor and configured to exchange signals with the drone for controlling operations.

    Adjustable Weight Distribution for Drone
    4.
    发明申请
    Adjustable Weight Distribution for Drone 有权
    无人机的可调重量分布

    公开(公告)号:US20170021915A1

    公开(公告)日:2017-01-26

    申请号:US15285717

    申请日:2016-10-05

    Abstract: Apparatus, methods, and systems for adjusting a center of mass of a drone may include a balance track and a repositionable weight. The balance track may be configured to extend outwardly from a central region of the drone. The balance track may include a plurality of weight-balance fixation positions. The repositionable weight may be configured to be secured at any one of the plurality of weight-balance fixation positions. In various embodiments the repositionable weight may include an electronic component. Various embodiments may include a another balance track configured to extend outwardly from the central region along a second axis that is different from a first axis of the other balance track.

    Abstract translation: 用于调节无人机质量中心的装置,方法和系统可以包括平衡轨道和可重定位重量。 平衡轨道可以被配置为从无人机的中心区域向外延伸。 平衡轨道可以包括多个重量平衡固定位置。 可重定位重量可以被配置为固定在多个重量平衡固定位置中的任何一个处。 在各种实施例中,可重定位重量可以包括电子部件。 各种实施例可以包括另一个平衡轨道,该平衡轨道配置成沿着与另一平衡轨道的第一轴线不同的第二轴线从中心区域向外延伸。

    Unmanned Aerial Vehicle With Monolithic Wing and Twin-Rotor Propulsion/Lift Modules

    公开(公告)号:US20180281941A1

    公开(公告)日:2018-10-04

    申请号:US15474014

    申请日:2017-03-30

    Inventor: Donald Hutson

    Abstract: Various embodiments include a drone capable of operating as an airplane, a quad-copter, or a hybrid aircraft using a versatile flight performance envelope enabled by six elements of control. The drone may include a monolithic wing with a propulsion/lift module connected to each wing tip. Each propulsion/lift module may include a pivotal support structure configured to pivot around a longitudinal axis of the monolithic wing, with two pylons extending radially outwardly from the pivotal support structure and at least partially away from one another, and a propulsion units positioned on a distal end of each pylon. The pivotal support structures may be coupled to the monolithic wing via a servo motor enabling a processor to individually control rotation of each propulsion/lift module to provide roll and pitch control. Thrust and rotation of the propulsion units may be individually controlled by the processor to provide yaw, roll and pitch control.

    Adjustable weight distribution for drone
    8.
    发明授权
    Adjustable weight distribution for drone 有权
    无人机的重量分布可调

    公开(公告)号:US09469394B2

    公开(公告)日:2016-10-18

    申请号:US14643070

    申请日:2015-03-10

    Abstract: Apparatus, methods, and systems for adjusting a center of mass of a drone may include a balance track and a repositionable weight. The balance track may extend outwardly from a central region of the drone. The balance track may include a plurality of weight-balance fixation positions. The repositionable weight may be configured to be secured at any one of the plurality of weight-balance fixation positions. Various embodiments may include receiving a weight-distribution input relating to balancing the drone. A weight-distribution balance profile may be determined, based on the weight-distribution input, for determining whether a repositionable weight should be repositioned among a plurality of weight-balance fixation positions on a balance track extending outwardly from a central region of the drone. The repositionable weight may be repositioned according to the weight-distribution balance profile.

    Abstract translation: 用于调节无人机质量中心的装置,方法和系统可以包括平衡轨道和可重定位重量。 平衡轨道可以从无人机的中心区域向外延伸。 平衡轨道可以包括多个重量平衡固定位置。 可重定位重量可以被配置为固定在多个重量平衡固定位置中的任何一个处。 各种实施例可以包括接收与平衡无人机相关的权重分布输入。 可以基于重量分布输入来确定重量分布平衡曲线,用于确定是否可以在从无人机的中心区域向外延伸的平衡轨道上的多个重量平衡固定位置之间重新定位可重新定位的重量。 可重新定位的重量可以根据重量分布平衡曲线重新定位。

    Unmanned aerial vehicle with monolithic wing and twin-rotor propulsion/lift modules

    公开(公告)号:US10850835B2

    公开(公告)日:2020-12-01

    申请号:US15474014

    申请日:2017-03-30

    Inventor: Donald Hutson

    Abstract: Various embodiments include a drone capable of operating as an airplane, a quad-copter, or a hybrid aircraft using a versatile flight performance envelope enabled by six elements of control. The drone may include a monolithic wing with a propulsion/lift module connected to each wing tip. Each propulsion/lift module may include a pivotal support structure configured to pivot around a longitudinal axis of the monolithic wing, with two pylons extending radially outwardly from the pivotal support structure and at least partially away from one another, and a propulsion units positioned on a distal end of each pylon. The pivotal support structures may be coupled to the monolithic wing via a servo motor enabling a processor to individually control rotation of each propulsion/lift module to provide roll and pitch control. Thrust and rotation of the propulsion units may be individually controlled by the processor to provide yaw, roll and pitch control.

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