Gimbal, photographing assembly and unmanned aerial vehicle (UAV) that have gimbal

    公开(公告)号:US10809600B2

    公开(公告)日:2020-10-20

    申请号:US16733886

    申请日:2020-01-03

    Abstract: The present invention relates to the technical field of aircrafts, and provides a gimbal, a photographing assembly and an unmanned aerial vehicle (UAV) that have the gimbal. The gimbal includes: a first rotating member and a second rotating member. The first rotating member includes a first drive apparatus, the first drive apparatus including a first rotating portion, and the second rotating member includes a second drive apparatus and a first connecting arm, the second drive apparatus including a second fixing portion and a second rotating portion that may rotate relative to the second fixing portion, the first connecting arm being fixedly connected between the first rotating portion and the second fixing portion, and the first connecting arm is integrally formed with the first rotating portion and the second fixing portion.

    Arm and unmanned aerial vehicle
    3.
    发明授权

    公开(公告)号:US10730619B2

    公开(公告)日:2020-08-04

    申请号:US15848910

    申请日:2017-12-20

    Inventor: Feng Ni

    Abstract: The present invention relates to the field of air vehicle technologies and provides an arm, a power assembly and an unmanned aerial vehicle. The arm includes a principal arm and an auxiliary arm. The principal arm is mounted on the vehicle body and the principal arm can rotate relative to the vehicle body. One end of the auxiliary arm is connected to the principal arm. The auxiliary arm can rotate relative to the principal arm. In the foregoing manner, an unmanned aerial vehicle having the arm is compact in structure, small in volume and easy to carry after being folded.

    Unmanned aerial vehicle
    4.
    发明授权

    公开(公告)号:US11498677B2

    公开(公告)日:2022-11-15

    申请号:US17122612

    申请日:2020-12-15

    Abstract: The present invention discloses an unmanned aerial vehicle, including: a fuselage; a battery accommodation cavity, disposed on the fuselage; a battery pack, including at least two battery blocks and mounted inside the battery accommodation cavity; a battery circuit board, electrically connected to the battery blocks in the battery pack; and a functional module, electrically connected to the battery circuit board, the battery blocks in the battery pack supplying power to the functional module via the battery circuit board at the same time. By using the solution of the present invention, endurance of the unmanned aerial vehicle is increased.

    Undercarriage and unmanned aerial vehicle (UAV) having undercarriage

    公开(公告)号:US11485483B2

    公开(公告)日:2022-11-01

    申请号:US16731941

    申请日:2019-12-31

    Inventor: Feng Ni

    Abstract: Embodiments of the present invention relate to the technical field of aircrafts, and provide an undercarriage and an unmanned aerial vehicle (UAV) having the undercarriage. The undercarriage includes a power assembly and an undercarriage body. The power assembly includes a connecting member and a drive apparatus for driving the connecting member to reciprocate. The undercarriage body includes a plurality of hinged connecting rods, the plurality of hinged connecting rods constituting at least one parallelogram mechanism, and projections of at least two of the hinged connecting rods on a side face of the fuselage are staggered. The undercarriage body is connected to the connecting member, and when the connecting member reciprocates, the undercarriage body is driven to be folded or unfolded. In the foregoing manner, driven by the reciprocating motion of the connecting member, the undercarriage body may be retracted and folded on two sides or in an interior of the fuselage, so that the undercarriage may be retracted and folded during flight of the UAV, thereby avoiding unnecessary resistance in the air.

    Unmanned aerial vehicle
    6.
    发明授权

    公开(公告)号:US10906643B2

    公开(公告)日:2021-02-02

    申请号:US16518175

    申请日:2019-07-22

    Abstract: The present invention discloses an unmanned aerial vehicle, including: a fuselage; a battery accommodation cavity, disposed on the fuselage; a battery pack, including at least two battery blocks and mounted inside the battery accommodation cavity; a battery circuit board, electrically connected to the battery blocks in the battery pack; and a functional module, electrically connected to the battery circuit board, the battery blocks in the battery pack supplying power to the functional module via the battery circuit board at the same time. By using the solution of the present invention, endurance of the unmanned aerial vehicle is increased.

    Antenna and unmanned aerial vehicle

    公开(公告)号:US10707572B2

    公开(公告)日:2020-07-07

    申请号:US15989907

    申请日:2018-05-25

    Inventor: Feng Ni

    Abstract: The present invention discloses an antenna and an unmanned aerial vehicle, where the antenna is applied to the unmanned aerial vehicle and the unmanned aerial vehicle includes a camera apparatus, the antenna including an antenna body and a bending part connected to the antenna body; and the bending part bends to a direction avoiding a field of view of the camera apparatus. Based on the foregoing technical solutions, in the embodiments of the present invention, it can be ensured that the antenna has a certain effective length to obtain a relatively strong radio signal, and avoids a shooting vision of the camera apparatus at the same time, so that images satisfying user demands are obtained.

    Unmanned aerial vehicle
    8.
    发明授权

    公开(公告)号:US10266264B2

    公开(公告)日:2019-04-23

    申请号:US16003589

    申请日:2018-06-08

    Abstract: The present invention discloses an unmanned aerial vehicle, including: a fuselage; a battery accommodation cavity, disposed on the fuselage; a battery pack, including at least two battery blocks and mounted inside the battery accommodation cavity; a battery circuit board, electrically connected to the battery blocks in the battery pack; and a functional module, electrically connected to the battery circuit board, the battery blocks in the battery pack supplying power to the functional module via the battery circuit board at the same time. By using the solution of the present invention, endurance of the unmanned aerial vehicle is increased.

    Unmanned aerial vehicle
    9.
    发明授权

    公开(公告)号:US11091249B2

    公开(公告)日:2021-08-17

    申请号:US15845372

    申请日:2017-12-18

    Inventor: Feng Ni

    Abstract: Embodiments of the present invention relate to the field of aircraft technologies, and provide an unmanned aerial vehicle including an unmanned aerial vehicle body and a landing gear. The landing gear is entirely accommodated in the unmanned aerial vehicle body when being in a folded state. When being folded, the landing gear in the present invention is entirely accommodated in the unmanned aerial vehicle body, and therefore neither causes unnecessary resistance in air nor blocks an aerial photographing field of view in an aerial photographing process of the unmanned aerial vehicle. In addition, when the unmanned aerial vehicle is not in use, the landing gear is accommodated in the unmanned aerial vehicle body, so that the unmanned aerial vehicle is very compact in structure and easy to accommodate and carry.

    Unmanned aerial vehicle
    10.
    发明授权

    公开(公告)号:US11492112B2

    公开(公告)日:2022-11-08

    申请号:US16747180

    申请日:2020-01-20

    Inventor: Feng Ni

    Abstract: The present invention relates to the field of air vehicle technologies and provides an unmanned aerial vehicle (UAV), including a vehicle body and arms connected to the vehicle body. The arm is hinged to the vehicle body by using a spherical hinge portion and may be folded or unfolded relative to the vehicle body. Through the forgoing manner, the arm is connected to the vehicle body of the UAV by using the spherical hinge. The arm can be folded and unfolded smoothly without interference, which conforms to known operation habits of users, so that after the entire UAV is folded, the structure becomes more compact and easier to carry. In addition, it can be effectively avoided that the UAV is damaged due to impact in the carrying process.

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