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    AERIAL VEHICLE WITH FRAME ASSEMBLIES
    31.
    发明申请
    AERIAL VEHICLE WITH FRAME ASSEMBLIES 有权
    具有框架组合的空中客车

    公开(公告)号：US20160152316A1

    公开(公告)日：2016-06-02

    申请号：US15012068

    申请日：2016-02-01

    Applicant: SZ DJI TECHNOLOGY Co., LTD

    Inventor： Tao Wang ,  Tao Zhao ,  Hao Du ,  Mingxi Wang

    IPC: B64C1/06 ,  B64C27/08 ,  B64D47/08 ,  B64C39/02

    CPC classification number: B64C1/063 ,  A63H27/12 ,  B64C1/00 ,  B64C1/061 ,  B64C25/32 ,  B64C27/08 ,  B64C39/024 ,  B64C39/028 ,  B64C2025/325 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/14 ,  B64C2201/146 ,  B64C2201/165 ,  B64D47/00 ,  B64D47/08 ,  G05D1/042

    Abstract: Systems, devices, and methods for a transformable aerial vehicle are provided. In one aspect, a transformable aerial vehicle includes: a central body and at least two transformable frames assemblies respectively disposed on the central body, each of the at least two transformable frame assemblies having a proximal portion pivotally coupled to the central body and a distal portion; an actuation assembly mounted on the central body and configured to pivot the at least two frame assemblies to a plurality of different vertical angles relative to the central body; and a plurality of propulsion units mounted on the at least two transformable frame assemblies and operable to move the transformable aerial vehicle.

    Abstract translation: 提供了可变形飞行器的系统，装置和方法。 一方面，可变形飞行器包括：中心体和分别设置在中心体上的至少两个可变形框架组件，所述至少两个可变形框架组件中的每一个具有枢转地联接到中心体的近侧部分和远端部分 ; 驱动组件，其安装在所述中心主体上并且构造成将所述至少两个框架组件相对于所述中心体枢转到多个不同的垂直角度; 以及安装在所述至少两个可变形框架组件上并可操作以移动所述可变形飞行器的多个推进单元。

    Aerial vehicle with frame assemblies
    33.
    发明授权
    Aerial vehicle with frame assemblies 有权
    具有框架组件的空中车辆

    公开(公告)号：US09284052B1

    公开(公告)日：2016-03-15

    申请号：US14944042

    申请日：2015-11-17

    Applicant: SZ DJI TECHNOLOGY CO., Ltd

    Inventor： Tao Wang ,  Tao Zhao ,  Hao Du ,  Mingxi Wang

    IPC: B64C29/00 ,  B64C39/02 ,  B64C27/08 ,  B64C1/00 ,  A63H27/00

    CPC classification number: B64C1/063 ,  A63H27/12 ,  B64C1/00 ,  B64C1/061 ,  B64C25/32 ,  B64C27/08 ,  B64C39/024 ,  B64C39/028 ,  B64C2025/325 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/14 ,  B64C2201/146 ,  B64C2201/165 ,  B64D47/00 ,  B64D47/08 ,  G05D1/042

    Abstract: Systems, devices, and methods for a transformable aerial vehicle are provided. In one aspect, a transformable aerial vehicle includes: a central body and at least two transformable frames assemblies respectively disposed on the central body, each of the at least two transformable frame assemblies having a proximal portion pivotally coupled to the central body and a distal portion; an actuation assembly mounted on the central body and configured to pivot the at least two frame assemblies to a plurality of different vertical angles relative to the central body; and a plurality of propulsion units mounted on the at least two transformable frame assemblies and operable to move the transformable aerial vehicle.

    Abstract translation: 提供了可变形飞行器的系统，装置和方法。 一方面，可变形飞行器包括：中心体和分别设置在中心体上的至少两个可变形框架组件，所述至少两个可变形框架组件中的每一个具有枢转地联接到中心体的近侧部分和远端部分 ; 驱动组件，其安装在所述中心主体上并且构造成将所述至少两个框架组件相对于所述中心体枢转到多个不同的垂直角度; 以及安装在所述至少两个可变形框架组件上并可操作以移动所述可变形飞行器的多个推进单元。

    PAYLOAD MOUNTING PLATFORM
    35.
    发明申请
    PAYLOAD MOUNTING PLATFORM 有权

    公开(公告)号：US20160023778A1

    公开(公告)日：2016-01-28

    申请号：US14877435

    申请日：2015-10-07

    Applicant: SZ DJI TECHNOLOGY Co., Ltd

    Inventor： Tao Zhao ,  Xi Feng Zhao ,  Yong Wang ,  Li Zhou ,  Tao Wang

    IPC: B64D47/08 ,  G03B17/56

    CPC classification number: B64D47/08 ,  B64C39/024 ,  B64C2201/127 ,  B64C2201/128 ,  F16M11/10 ,  F16M11/18 ,  F16M11/2028 ,  F16M11/42 ,  G03B15/006 ,  G03B17/561

    Abstract: Systems, devices, and methods are provided relating to improved mounting platforms for supporting a payload on a movable object. In one aspect, an apparatus for supporting a payload comprises: a first support member coupled to the payload and configured to rotate the payload; a second support member coupled to the first support member and configured to rotate the first support member relative to the second support member; and a flexible member electrically coupling the first and second support members, wherein a length of the flexible member winds around a portion of the first support member or second support member, such that the length winds up around the portion when the first support member is rotated in a first direction and unwinds from the portion when the first support member is rotated in a second direction.

    APPARATUS, SYSTEMS, AND METHODS FOR DETECTING PROJECTILE HITS ON A SURFACE
    39.
    发明申请
    APPARATUS, SYSTEMS, AND METHODS FOR DETECTING PROJECTILE HITS ON A SURFACE 有权
    用于检测表面上的投影仪的装置，系统和方法

    公开(公告)号：US20150321094A1

    公开(公告)日：2015-11-12

    申请号：US14683115

    申请日：2015-04-09

    Applicant: SZ DJI TECHNOLOGY CO., LTD.

    Inventor： Ji Dong Wei ,  Sheng Yang Chen ,  Tao Wang ,  Ji Yuan Ao ,  Yi Jun Guan

    IPC: A63F13/27 ,  A63F13/21

    CPC classification number: A63F13/27 ,  A63F13/02 ,  A63F13/21 ,  A63F13/28 ,  A63H2200/00

    Abstract: A sensing apparatus may be provided capable of detecting a hit by a projectile, such as a BB pellet. The sensing apparatus may include a surface and accelerometer to detect the acceleration of the surface. A processor may determine whether a projectile hit has occurred. The sensing apparatus may be mounted onto a vehicle. The vehicle may be a robot capable of participating in a game. The robot game may occur within a facility.

    Abstract translation: 可以提供能够检测诸如BB颗粒之类的抛射体的撞击的感测装置。 感测装置可以包括表面和加速度计，以检测表面的加速度。 处理器可以确定是否发生了弹丸命中。 感测装置可以安装在车辆上。 车辆可以是能够参与游戏的机器人。 机器人游戏可能发生在设施内。

    Flight control for flight-restricted regions
    40.
    发明授权
    Flight control for flight-restricted regions 有权

    公开(公告)号：US09176501B2

    公开(公告)日：2015-11-03

    申请号：US14262563

    申请日：2014-04-25

    Applicant: SZ DJI TECHNOLOGY CO., LTD

    Inventor： Mingyu Wang ,  Tao Wang ,  Jianyu Song

    IPC: G05D1/00 ,  G05D1/02 ,  G08G5/00 ,  B64C39/02

    Abstract: Systems, methods, and devices are provided for providing flight response to flight-restricted regions. The location of an unmanned aerial vehicle (UAV) may be compared with a location of a flight-restricted region. If needed a flight-response measure may be taken by the UAV to prevent the UAV from flying in a no-fly zone. Different flight-response measures may be taken based on the distance between the UAV and the flight-restricted region and the rules of a jurisdiction within which the UAV falls.

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