Solid Rocket Motor Propellant Manufacture and Configurations

    公开(公告)号:US20200377428A1

    公开(公告)日:2020-12-03

    申请号:US16427663

    申请日:2019-05-31

    Inventor: Dustin W. Davis

    Abstract: A method for manufacturing a solid propellant includes: forming a tool of layers of a first material wherein cuts in the layers form a first interior chamber in the tool; using the tool to mold a second material in the first interior chamber; removing the molded second material from the tool; using the molded second material to mold an interior chamber in a rocket propellant grain; and removing the molded second material from the rocket propellant grain.

    CAST-IN FILM COOLING HOLE STRUCTURES
    19.
    发明申请

    公开(公告)号:US20200086380A1

    公开(公告)日:2020-03-19

    申请号:US16131695

    申请日:2018-09-14

    Abstract: A core element of an investment core for use in a casting process used to produce an airfoil includes an investment core body, an extension connected to and protruding from the investment core body, and a connection portion connected to the investment core body and to the extension. The investment core body comprises a ceramic material. A shape of the extension comprises a tube with a centerline axis passing through a center of the extension. A shape of a cross-section of the extension taken along a plane perpendicular to the extension centerline axis comprises an ellipse. The extension is connected to the investment core body by the connection portion.

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