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    PAYLOAD MOUNTING PLATFORM
    61.
    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.

    Self-tightening rotor
    64.
    发明授权
    Self-tightening rotor 有权
    自紧式转子

    公开(公告)号：US09057273B2

    公开(公告)日：2015-06-16

    申请号：US14167735

    申请日：2014-01-29

    Applicant: SZ DJI TECHNOLOGY CO., LTD

    Inventor： Tao Wang ,  Tao Zhao ,  Zhi Gang Ou

    IPC: F01D5/02 ,  B64C11/04 ,  A63H27/00

    CPC classification number: B64C27/32 ,  A63H27/001 ,  A63H27/02 ,  B64C11/02 ,  B64C11/04 ,  B64C27/08 ,  B64C27/14 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/108 ,  F01D5/025

    Abstract: Systems, methods, and devices for propelling self-propelled movable objects are provided. In one aspect, a rotor assembly for a self-propelled movable object comprises: a hub comprising a first fastening feature; a drive shaft comprising a second fastening feature and directly coupled to the hub by a mating connection of the first and second fastening features, wherein the drive shaft is configured to cause rotation of the hub such that the mating connection of the first and second fastening features is tightened by the rotation; and a plurality of rotor blades coupled to the hub and configured to rotate therewith to generate a propulsive force.

    Abstract translation: 提供了用于推进自行式移动物体的系统，方法和装置。 一方面，一种用于自推进可移动物体的转子组件包括：毂，包括第一紧固特征; 驱动轴，其包括第二紧固特征并且通过所述第一和第二紧固特征的匹配连接直接联接到所述轮毂，其中所述驱动轴构造成引起所述轮毂的旋转，使得所述第一和第二紧固特征 被旋转收紧; 以及多个转子叶片，其联接到所述毂并且被配置为随其旋转以产生推进力。

    TRANSFORMABLE AERIAL VEHICLE
    66.
    发明申请
    TRANSFORMABLE AERIAL VEHICLE 有权
    可转换的航空汽车

    公开(公告)号：US20140263823A1

    公开(公告)日：2014-09-18

    申请号：US14167679

    申请日：2014-01-29

    Applicant: SZ DJI TECHNOLOGY CO., Ltd

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

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

    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。

    AIRCRAFT CONTROL APPARATUS, CONTROL SYSTEM AND CONTROL METHOD
    68.
    发明申请
    AIRCRAFT CONTROL APPARATUS, CONTROL SYSTEM AND CONTROL METHOD 有权

    公开(公告)号：US20220144430A1

    公开(公告)日：2022-05-12

    申请号：US17585886

    申请日：2022-01-27

    Applicant: SZ DJI Technology Co., LTD

    Inventor： Tao Wang ,  Tao Zhao

    IPC: B64C39/02 ,  A63H30/04 ,  B64C13/20 ,  B64D47/08 ,  G05D1/00

    Abstract: An aircraft control system and control method are disclosed. The system comprises a remote control apparatus with a first control rod and a flight controller associated with an aircraft. The first control rod is configured to move in a first movement direction to control a motion of the aircraft in a first motion direction when an external force is applied on the first control rod and after a withdrawal of the external force, the first control rod returns to a preset position. The remote control apparatus operates to generate one or more control signals corresponding to the withdrawal of the external force. The flight controller controls the aircraft to maintain a flight state based on said control signals and one or more state signals, which are generated based on a measurement of the flight state by a flight controller associated with the aircraft state measurement sensors carried by the aircraft.

    Self-tightening rotor
    69.
    发明授权
    Self-tightening rotor 有权

    公开(公告)号：US11267565B2

    公开(公告)日：2022-03-08

    申请号：US16995792

    申请日：2020-08-17

    Applicant: SZ DJI TECHNOLOGY CO., LTD.

    Inventor： Tao Wang ,  Tao Zhao ,  Zhi Gang Ou

    IPC: B64C27/32 ,  B64C39/02 ,  A63H27/00 ,  B64C11/02 ,  B64C11/04 ,  F01D5/02 ,  B64C27/08 ,  B64C27/14

    Abstract: An aerial vehicle includes an aerial vehicle body, and first and second rotor assemblies. The first rotor assembly includes a first hub coupled to first blades, and a first drive shaft coupled to the first hub via fastening features. The first drive shaft is configured to rotate the first hub in a first direction such that the first blades rotate in a first rotation plane. The second rotor assembly includes a second hub coupled to second blades, and a second drive shaft coupled to the second hub via fastening features. The second drive shaft is configured to rotate the second hub in a second direction opposite to the first direction, such that the second blades rotate in a second rotation plane. The first and second rotation planes are at opposite sides of the aerial vehicle body.

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