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    TIP RAIL COOLING INSERT FOR TURBINE BLADE TIP COOLING SYSTEM AND RELATED METHOD
    4.
    发明申请
    TIP RAIL COOLING INSERT FOR TURBINE BLADE TIP COOLING SYSTEM AND RELATED METHOD 有权

    公开(公告)号：US20210017864A1

    公开(公告)日：2021-01-21

    申请号：US16876615

    申请日：2020-05-18

    Applicant: General Electric Company

    Inventor： Mark Steven Honkomp ,  Mark Lawrence Hunt ,  Frederick Whitfield Dantzler ,  Yan Cui ,  Ethan Conrad Schaeffer

    IPC: F01D5/18

    Abstract: A tip rail cooling insert for attaching into a tip rail pocket in a tip rail of a turbine blade is disclosed. The insert includes a first inner layer defining at least one first insert cooling channel therein, the first inner layer including a pair of spaced legs defining a first coolant collection plenum with at least the tip rail pocket for directing coolant from at least one internal cooling cavity in the turbine blade to the at least one first insert cooling channel. Each of the pair of spaced legs has an angled outer end configured to accommodate rounded inner corners of the tip rail pocket. A first outer layer is on a first side of the first inner layer, and a second outer layer is on a second side of the first inner layer.

    METHOD OF REPAIRING SUPERALLOY COMPONENTS USING PHASE AGGLOMERATION
    6.
    发明申请
    METHOD OF REPAIRING SUPERALLOY COMPONENTS USING PHASE AGGLOMERATION 审中-公开

    公开(公告)号：US20200346294A1

    公开(公告)日：2020-11-05

    申请号：US16402163

    申请日：2019-05-02

    Applicant: General Electric Company

    Inventor： Brian Leslie Henderson ,  Paul Albert Cook ,  Yan Cui ,  Daniel James Dorriety

    IPC: B23K1/20 ,  C22F1/10

    Abstract: A method of repairing a superalloy component includes subjecting the superalloy component, including a repair area, to a phase agglomeration cycle, which includes stepped heating and controlled cooling of the component. The method further includes applying weld material to the repair area to create a weld surface; and covering the weld surface with brazing material. The component is then subjected to a braze cycle to produce a brazed component. The brazed component is cleaned, and the cleaned component is subjected to a restorative heat treatment to restore the microcrystalline structure and mechanical properties of the component.

    Method and fixture for counteracting tensile stress
    8.
    发明授权
    Method and fixture for counteracting tensile stress 有权

    公开(公告)号：US10508316B2

    公开(公告)日：2019-12-17

    申请号：US15475661

    申请日：2017-03-31

    Applicant: GENERAL ELECTRIC COMPANY

    Inventor： Yan Cui ,  Srikanth Chandrudu Kottilingam ,  Brian Lee Tollison ,  Brian Leslie Henderson ,  Cem Murat Eminoglu

    IPC: C21D1/30 ,  C22F1/10 ,  C22F1/18 ,  C22F1/08

    Abstract: A method for counteracting tensile stress in an article is disclosed, including heating the article and applying compressive stress to the article along a compressive stress vector, the compressive stress vector including a compressive stress vector component opposite in direction to a tensile stress vector of a thermally-induced tensile stress of the article. The compressive stress is applied by thermally-induced autogenous pressure by a fixture contacting the article. A fixture for counteracting tensile stress is disclosed, including a first compression member and a second compression member, and a position lock connecting the first compression member to the second compression member and reversibly fixing the first compression member relative to the second compression member. The first compression member and the second compression member include compressive surfaces having mating conformations for surfaces of an article. The position lock includes a material composition.

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