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    Sleeve assemblies and methods of fabricating same
    1.
    发明授权
    Sleeve assemblies and methods of fabricating same 有权

    公开(公告)号：US11359815B2

    公开(公告)日：2022-06-14

    申请号：US16814360

    申请日：2020-03-10

    Applicant: General Electric Company

    Inventor： Kyle Lee Kidder ,  Zsolt Czirle

    IPC: F23R3/60 ,  F02C7/28 ,  F23R3/00 ,  F23R3/46

    Abstract: A sleeve assembly for a combustion system includes a first duct including a first circumferential surface and a second duct including a second circumferential surface. The first circumferential surface radially overlaps the second circumferential surface such that the first duct and the second duct collectively define a continuous combustion chamber therein. The continuous combustion chamber is configured to receive high temperature gases flowing therethrough. The sleeve assembly further includes a wear insert removably coupled to the first circumferential surface and extending radially therefrom to engage the second circumferential surface.

    WEAR PAD SYSTEM FOR TURBINE COMBUSTION SYSTEMS AND METHOD FOR COUPLING WEAR PAD INTO TURBINE COMBUSTION SYSTEM
    6.
    发明申请
    WEAR PAD SYSTEM FOR TURBINE COMBUSTION SYSTEMS AND METHOD FOR COUPLING WEAR PAD INTO TURBINE COMBUSTION SYSTEM 审中-公开
    用于涡轮机燃烧系统的磨损系统和用于将磨损垫片连接到涡轮机燃烧系统中的方法

    公开(公告)号：US20170059158A1

    公开(公告)日：2017-03-02

    申请号：US14833388

    申请日：2015-08-24

    Applicant: General Electric Company

    Inventor： Kyle Lee Kidder ,  Tiffany Marie Craig ,  Eunice Delia Garza

    IPC: F23R3/00 ,  B23P15/00 ,  F23R3/60

    CPC classification number: F23R3/002 ,  B23P15/00 ,  B23P2700/13 ,  F01D9/023 ,  F23R3/46 ,  F23R3/60 ,  F23R2900/00012 ,  F23R2900/00017 ,  F23R2900/03044

    Abstract: An aspect of the invention provides for a wear pad system for a turbine combustion system including a transition piece (TP) forward ring, an impingement sleeve substantially surrounding the TP forward ring, and a gap between the TP forward ring and the impingement sleeve, the wear pad system comprising: a wear pad extending through a hole in the impingement sleeve and through the gap to contact the TP forward ring, the wear pad having a radially outer portion and a radially inner portion, the radially outer portion in contact with a radially outer surface of the impingement sleeve and the radially inner portion in contact with a radially outer surface of the TP forward ring.

    Abstract translation: 本发明的一个方面提供了一种用于涡轮机燃烧系统的磨损系统，其包括过渡件（TP）前环，基本上围绕TP前进环的冲击套筒以及TP前进环和冲击套筒之间的间隙， 磨损垫系统，包括：磨损垫，其延伸穿过冲击套筒中的孔并且穿过间隙以接触TP前进环，所述磨损垫具有径向外部部分和径向内部部分，所述径向外部部分与径向外部接触 冲击套筒的外表面和与TP前进环的径向外表面接触的径向内部。

    System for Protecting an Inner Wall of a Combustor
    10.
    发明申请
    System for Protecting an Inner Wall of a Combustor 审中-公开
    用于保护燃烧室内壁的系统

    公开(公告)号：US20140157783A1

    公开(公告)日：2014-06-12

    申请号：US13710395

    申请日：2012-12-10

    Applicant: GENERAL ELECTRIC COMPANY

    Inventor： Kyle Lee Kidder ,  Jerome D. Brown

    IPC: F23R3/00

    CPC classification number: F23R3/002 ,  F23R3/005 ,  F23R3/007 ,  F23R3/06 ,  F23R2900/00019 ,  F23R2900/03041 ,  F23R2900/03042 ,  Y02T50/675 ,  Y02T50/6765

    Abstract: In a first embodiment a system, including a gas turbine combustor, including an inner wall disposed about a combustion chamber, and an outer wall disposed about the inner wall, wherein a coolant flow path extends between the inner and outer walls, wherein the inner wall comprises a material blocking a plurality of openings, and the plurality of openings are configured to open after the material is consumed or depleted to define a plurality of coolant passages through the inner wall.

    Abstract translation: 在第一实施例中，包括燃气轮机燃烧器的系统，包括围绕燃烧室设置的内壁，以及围绕内壁设置的外壁，其中冷却剂流动路径在内壁和外壁之间延伸，其中内壁 包括阻挡多个开口的材料，并且多个开口构造成在材料消耗或耗尽之后打开以限定穿过内壁的多个冷却剂通道。

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