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    FIXTURE FOR SECURING COMPONENT TO BE DRILLED AND METHOD OF DRILLING SAME
    1.
    发明申请
    FIXTURE FOR SECURING COMPONENT TO BE DRILLED AND METHOD OF DRILLING SAME 审中-公开
    用于固定钻头的组件的固定装置及其钻孔方法

    公开(公告)号：US20170056980A1

    公开(公告)日：2017-03-02

    申请号：US14833396

    申请日：2015-08-24

    申请人： General Electric Company

    发明人： Tiffany Marie Craig ,  Charles Van Buchan

    IPC分类号： B23B49/02

    CPC分类号： B23B49/02 ,  B23B2215/76 ,  B25B5/003 ,  B25B5/147 ,  B25B5/163

    摘要： A first aspect of the invention provides for a fixture for securing a component to be drilled. The fixture may comprise: a support structure positioning the component thereon; a template substantially surrounding the component configured to locate a position on the component that is to be drilled, the template being positioned on the support structure and having at least one hole therethrough; and a centering device positioned on the support structure configured to center the component within the template.

    摘要翻译： 本发明的第一方面提供一种用于固定要钻探的部件的固定装置。 该固定装置可以包括：将部件定位在其上的支撑结构; 基本上围绕所述部件的模板，所述模块被构造成定位要被钻探的部件上的位置，所述模板定位在所述支撑结构上并且具有穿过其中的至少一个孔; 以及定位在所述支撑结构上的定心装置，其被配置为使所述部件在所述模板内居中。

    WEAR PAD SYSTEM FOR TURBINE COMBUSTION SYSTEMS AND METHOD FOR COUPLING WEAR PAD INTO TURBINE COMBUSTION SYSTEM
    2.
    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

    申请人： General Electric Company

    发明人： Kyle Lee Kidder ,  Tiffany Marie Craig ,  Eunice Delia Garza

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

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

    摘要： 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.

    摘要翻译： 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。