BATTERY HOUSING APPARATUS AND UNMANNED AERIAL VEHICLE

    公开(公告)号:US20190259998A1

    公开(公告)日:2019-08-22

    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.

    UNMANNED AERIAL VEHICLE
    3.
    发明申请

    公开(公告)号:US20190256215A1

    公开(公告)日:2019-08-22

    申请号:US16401854

    申请日:2019-05-02

    Abstract: An unmanned aerial vehicle (UAV) includes a fuselage, an electrical component, and an adapter arranged at the fuselage. The fuselage includes a battery compartment for accommodating a battery. The battery compartment includes an electrical connector for electrically coupling to the battery. The adapter is electrically coupled to the electrical connector and includes an access unit electrically coupled to the electrical connector and an adapting unit detachably coupled to the access unit. The adapting unit is configured to be electrically connected to the access unit when the adapting unit is coupled to the access unit. The adapting unit is electrically coupled to the electrical component through an adapting conductive wire to conduct power from the battery to the electrical component.

    LOCKING MECHANISM, PROPELLER, MOTOR, PROPULSION SYSTEM ASSEMBLY, AND AIRCRAFT

    公开(公告)号:US20210276691A1

    公开(公告)日:2021-09-09

    申请号:US17328770

    申请日:2021-05-24

    Abstract: A propulsion system assembly includes a propeller, a motor configured to drive the propeller to rotate, and a locking mechanism configured to detachably lock the propeller to the motor. The propeller includes one of a first body and a second body. The motor includes another one of the first body and the second body. The locking mechanism includes a coupling member including a femoral position groove, a fastener configured to fix the coupling member to the second body, and a locking member configured to lock the first body to the coupling member and the second body. A bottom portion of the first body that contacts the coupling member includes a protruding rib configured to fit with the femoral position groove to restrain the first body from rotating relative to the coupling member.

    BATTERY HOUSING APPARATUS AND UNMANNED AERIAL VEHICLE

    公开(公告)号:US20210376414A1

    公开(公告)日:2021-12-02

    申请号:US17397239

    申请日:2021-08-09

    Abstract: An unmanned aerial vehicle (UAV) includes a housing body and a battery locking mechanism disposed on the housing body. The housing body includes a battery compartment configured to receive a battery. The battery locking mechanism is configured to lock the battery in the battery compartment after the battery is mounted in place. The battery locking mechanism includes a locking assembly configured to be dislocated by the battery in a process of mounting the battery in the battery compartment and to be restored to lock the battery in the battery compartment after the battery is mounted in place, and an indicator assembly disposed on the housing body and configured to indicate whether the battery is mounted in place. The locking assembly includes a locking slider configured to tightly contact with the battery to lock the battery in a direction of a battery insertion.

    ROTOR-WING ASSEMBLY AND UNMANNED AERIAL VEHICLE

    公开(公告)号:US20190256204A1

    公开(公告)日:2019-08-22

    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.

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