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    COMBUSTOR TILE WITH MONOLITHIC INSERTS
    3.
    发明申请
    COMBUSTOR TILE WITH MONOLITHIC INSERTS 审中-公开

    公开(公告)号：US20170138597A1

    公开(公告)日：2017-05-18

    申请号：US15217444

    申请日：2016-07-22

    申请人： Rolls-Royce North American Technologies Inc. ,  Rolls-Royce Corporation ,  Rolls-Royce High Temperature Composites Inc.

    发明人： Ted Joseph Freeman ,  Bruce E. Varney ,  Andrew Joseph Lazur

    IPC分类号： F23R3/00 ,  F01D9/04

    摘要： An annular assembly for a gas turbine engine and a method of making the annular assembly. The annular assembly comprises a supporting member comprising metal and including a support hole therethrough, and a liner tile made of ceramic matrix composite material. A plurality of the liner tile form an annular liner to shield hot combustion gases produced by the gas turbine engine. The liner tile is disposed adjacent the supporting member. A connecting member comprising ceramic material has a base element and a stem. The base element is embedded in the liner tile during construction of the liner tile to form an integrated structure therewith. A distal end of the stem passes through the support hole and is mated with a retaining member to retain the liner tile adjacent the supporting member.

    Combustor tile with monolithic inserts
    5.
    发明授权
    Combustor tile with monolithic inserts 有权

    公开(公告)号：US10767863B2

    公开(公告)日：2020-09-08

    申请号：US15217444

    申请日：2016-07-22

    申请人： Rolls-Royce North American Technologies Inc. ,  Rolls-Royce Corporation ,  Rolls-Royce High Temperature Composites Inc.

    发明人： Ted Joseph Freeman ,  Bruce E. Varney ,  Andrew Joseph Lazur

    IPC分类号： F23R3/00 ,  F01D9/04 ,  F23M5/04

    摘要： An annular assembly for a gas turbine engine and a method of making the annular assembly. The annular assembly comprises a supporting member comprising metal and including a support hole therethrough, and a liner tile made of ceramic matrix composite material. A plurality of the liner tile form an annular liner to shield hot combustion gases produced by the gas turbine engine. The liner tile is disposed adjacent the supporting member. A connecting member comprising ceramic material has a base element and a stem. The base element is embedded in the liner tile during construction of the liner tile to form an integrated structure therewith. A distal end of the stem passes through the support hole and is mated with a retaining member to retain the liner tile adjacent the supporting member.

    Forming a surface layer on a ceramic matrix composite article
    7.
    发明授权
    Forming a surface layer on a ceramic matrix composite article 有权

    公开(公告)号：US10774010B2

    公开(公告)日：2020-09-15

    申请号：US15499946

    申请日：2017-04-28

    申请人： Rolls-Royce High Temperature Composites, Inc.

    发明人： Sungbo Shim ,  Andrew Joseph Lazur ,  Robert Shinavski

    IPC分类号： C04B41/00 ,  C04B41/89 ,  C04B41/52 ,  C04B35/80 ,  F01D5/28 ,  B05D7/24 ,  B05D3/00 ,  B05D7/22

    摘要： Techniques for infiltrating a CMC substrate may include infiltrating the CMC substrate with a first slurry to at least partially fill at least some inner spaces of the CMC substrate, where the first slurry includes first solid particles, drying the first slurry to form an infiltrated CMC including the first solid particles, depositing a second slurry including a carrier material and second solid particles on a surface of the infiltrated CMC, where the second solid particles include a plurality of fine ceramic particles, a plurality of coarse ceramic particles, and a plurality of diamond particles, drying the second slurry to form an article having an outer surface layer including the second solid particles on the infiltrated CMC, and infiltrating the article with a molten infiltrant to form a composite article.

    FORMING A SURFACE LAYER ON A CERAMIC MATRIX COMPOSITE ARTICLE
    8.
    发明申请
    FORMING A SURFACE LAYER ON A CERAMIC MATRIX COMPOSITE ARTICLE 审中-公开

    公开(公告)号：US20170313629A1

    公开(公告)日：2017-11-02

    申请号：US15499946

    申请日：2017-04-28

    申请人： Rolls-Royce High Temperature Composites, Inc.

    发明人： Sungbo Shim ,  Andrew Joseph Lazur ,  Robert Shinavski

    IPC分类号： C04B41/00 ,  C04B35/80

    摘要： The disclosure describes techniques for infiltrating a CMC substrate with a first slurry to at least partially fill at least some inner spaces of the CMC substrate, where the first slurry comprises first solid particles, drying the first slurry to form an infiltrated CMC including the first solid particles, depositing a second slurry including a carrier material and second solid particles on a surface of the infiltrated CMC, where the second solid particles comprise a plurality of fine ceramic particles, a plurality of coarse ceramic particles, and a plurality of diamond particles, drying the second slurry to form an article having an outer surface layer comprising the second solid particles on the infiltrated CMC, and infiltrating the article with a molten infiltrant to form a composite article.

    Textile material joining technique
    10.
    发明授权
    Textile material joining technique 有权

    公开(公告)号：US10696008B2

    公开(公告)日：2020-06-30

    申请号：US14141962

    申请日：2013-12-27

    申请人： Rolls-Royce Corporation

    发明人： Andrew Joseph Lazur

    IPC分类号： B32B3/06 ,  B32B5/02 ,  D03D1/00 ,  D03D3/04

    摘要： Techniques for joining textile materials are provided. In one non-limiting form, a system includes a woven structure having a first woven layer and at least a first section and a second section. The first section includes a first fringe portion and a first set of fibers, and the second section includes a second fringe portion and a second set of fibers. The fibers of the first and second sets of fibers are configured in the first and second fringe portions to provide an interlocking arrangement between the first and second sections. Further embodiments, forms, features, and aspects shall become apparent from the description and drawings.