DOWNHOLE POWER AND COMMUNICATIONS SYSTEM(S) AND METHOD(S) OF USING SAME

    公开(公告)号:US20240344429A1

    公开(公告)日:2024-10-17

    申请号:US18756784

    申请日:2024-06-27

    申请人: Bosko GAJIC

    发明人: Bosko GAJIC

    IPC分类号: E21B41/00 E21B47/13 H02N11/00

    摘要: Apparatus, method(s), and system(s) according to which electric power is generated in one or more coils by rotating a magnetic field generated by one or more permanent magnets. The one or more coils are connected to a collar. The collar is positioned downhole in an oil and gas wellbore. The one or more permanent magnets are connected to a rotor positioned within an internal passageway of the collar. A fluid is communicated along the internal passageway of the collar. The rotor, and thus the magnetic field generated by the one or more permanent magnets, are rotated using the fluid communicated along the internal passage.

    ACTUATOR FOR CAMERA
    7.
    发明公开
    ACTUATOR FOR CAMERA 审中-公开

    公开(公告)号:US20240231031A9

    公开(公告)日:2024-07-11

    申请号:US18317187

    申请日:2023-05-15

    IPC分类号: G02B7/02 G03B17/17 H02N11/00

    摘要: The embodiment disclosed herein is an actuator for camera comprising a lens module emitting light towards an image sensor; a housing enclosing the lens module; and a patterned member disposed on the internal surface of the housing wherein the internal surface is the one between the lens module and the image sensor. The patterned member comprises protrusions arranged in repetition along an optical axis, in which each protrusion extends lengthwise along a direction perpendicular to the optical axis.

    MAGNETIC MULTI-POLE PROPULSION ARRAY SYSTEM
    9.
    发明公开

    公开(公告)号:US20240124163A1

    公开(公告)日:2024-04-18

    申请号:US18084519

    申请日:2022-12-19

    IPC分类号: B64G1/40 H02N11/00

    CPC分类号: B64G1/409 H02N11/006

    摘要: A magnetic multi-pole propulsion array system is applied to at least one external cathode and includes a plurality of magnetic multi-pole thrusters connected adjacent to each other. Each magnetic multi-pole thruster includes a propellant provider, a discharge chamber, an anode and a plurality of magnetic components. The propellant provider outputs propellant. The discharge chamber is connected with the propellant provider to accommodate the propellant. The anode is disposed inside the discharge chamber to generate an electric field. The plurality of magnetic components is respectively disposed on several sides of the discharge chamber. One of the several sides of the discharge chamber of the magnetic multi-pole thruster is applied for one side of a discharge chamber of another magnetic multi-pole thruster.