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    COMBUSTOR TILE WITH MONOLITHIC INSERTS
    1.
    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.

    BLADE TRACK ASSEMBLY, COMPONENTS, AND METHODS
    10.
    发明申请
    BLADE TRACK ASSEMBLY, COMPONENTS, AND METHODS 有权
    叶片组件，组件和方法

    公开(公告)号：US20150016970A1

    公开(公告)日：2015-01-15

    申请号：US14458532

    申请日：2014-08-13

    申请人： Rolls-Royce North American Technologies, Inc.

    发明人： Clayton C. Smith ,  George F. Griffiths ,  Ted Joseph Freeman ,  William Westphal

    IPC分类号： F01D11/08 ,  F01D25/24

    CPC分类号： F01D11/08 ,  F01D11/005 ,  F01D25/24 ,  F05D2230/60 ,  F05D2240/11 ,  Y02T50/672 ,  Y10T29/4932

    摘要： A blade track assembly is disclosed having a variety of features. The assembly can have annular or segmented components, or a combination of the two. In one form the assembly includes blade tracks having a forward and aft edge that can be received in an opening of respective hangers. The hangers can include anti-movement features to discourage movement of a blade track. A rib can extend between hangers and in one form can be used as part of a seal assembly. Clips can be used to secure the blade track in openings of the respective hangers, as well as to discourage movement of the blade track.

    摘要翻译： 公开了具有各种特征的刀片轨道组件。 组件可以具有环形或分段部件，或两者的组合。 在一种形式中，组件包括具有可以容纳在相应悬挂器的开口中的前部和后部边缘的刀片轨道。 衣架可以包括防止运动的特征，以阻止刀片轨道的移动。 肋可以在衣架之间延伸，并且一种形式可以用作密封组件的一部分。 可以使用夹子将刀片轨道固定在各个吊架的开口中，并且阻止刀片轨道的移动。