Battery housing apparatus and unmanned aerial vehicle

    公开(公告)号:US11088414B2

    公开(公告)日:2021-08-10

    申请号:US16397555

    申请日:2019-04-29

    Abstract: The present disclosure discloses a battery housing apparatus. The apparatus includes a housing body and a battery locking mechanism. The housing body is configured with at least one battery compartment for housing a battery. The battery locking mechanism is disposed on the housing body and configured to indicate whether the battery is mounted in place during a process of mounting the battery in the battery compartment and to lock the battery in the battery compartment after the battery is mounted in place.

    Rotor-wing assembly and unmanned aerial vehicle

    公开(公告)号:US11524775B2

    公开(公告)日:2022-12-13

    申请号:US16401930

    申请日:2019-05-02

    Abstract: A rotor-wing assembly includes a motor, a propeller, and a connection assembly connecting the propeller to the motor. The motor includes a rotating portion. The connection assembly includes a locking member and a reinforcing member arranged between the propeller and the motor. The locking member locks the propeller to the rotating portion. A first end of the reinforcing member is mounted at the rotating portion. A second end of the reinforcing member opposite to the first end is engaged with the locking member, to reinforce the locking member to lock the propeller to the rotating portion.

    Servo, control method, and unmanned aerial vehicle

    公开(公告)号:US11249491B2

    公开(公告)日:2022-02-15

    申请号:US16395875

    申请日:2019-04-26

    Abstract: An unmanned aerial vehicle (UAV) includes a central part, a frame assembly, and a propulsion assembly mounted to the frame assembly. The UAV also includes a servo mounted to the central part. The servo includes a driving apparatus, a control apparatus operably coupled with the driving apparatus, and a sensor configured to obtain operating parameters of the driving apparatus. The operating parameters include operating positions of the driving apparatus. The control apparatus is configured to control the driving apparatus to rotate to a predetermined position and stay at the predetermined position based on the operating positions of the driving apparatus obtained by the sensor.

    Transformable aerial vehicle
    7.
    发明授权

    公开(公告)号:US10287004B2

    公开(公告)日:2019-05-14

    申请号:US15389087

    申请日:2016-12-22

    Inventor: Di Ou Wenlong Liang

    Abstract: A transformable aerial vehicle includes a fuselage and a body frame. The fuselage includes a transmission mechanism including a leadscrew, at least two nuts threadedly connected to the leadscrew and connected to each other, and a nut adapter sleeved on one of the at least two nuts. The body frame includes a main support arm connected to the nut adapter, a crossbar connected to the main support arm, and a rotary power mechanism mounted on the crossbar.

    Aerial vehicle and a signal line protection assembly thereof

    公开(公告)号:US10513329B2

    公开(公告)日:2019-12-24

    申请号:US16297193

    申请日:2019-03-08

    Inventor: Di Ou

    Abstract: A signal line protection assembly connecting to a propulsion system of an aerial vehicle includes a foot stand and a protection sleeve. The foot stand includes a foot stand sleeve including a bearing member and a receiving portion. The bearing member has a first side and a second side that is opposite to the first side. The first side is configured to bear the propulsion system, and the receiving portion is arranged at the second side. The protection sleeve is configured to receive a signal line. At least a portion of the protection sleeve is received in the receiving portion.

    Aerial vehicle and a signal line protection assembly thereof

    公开(公告)号:US10227131B2

    公开(公告)日:2019-03-12

    申请号:US15816353

    申请日:2017-11-17

    Inventor: Di Ou

    Abstract: A signal line protection assembly connecting to a propulsion system of an aerial vehicle includes a foot stand and a protection sleeve. The foot stand includes a foot stand sleeve including an electronic speed controller compartment arranged below a motor of the propulsion system and forming a closed space to receive an electronic speed controller of the aerial vehicle. The protection sleeve is configured to receive a power line for the electronic speed controller. At least a portion of the protection sleeve is received in the electronic speed controller compartment.

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