Invention Application
US20170059158A1 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
- Patent Title: WEAR PAD SYSTEM FOR TURBINE COMBUSTION SYSTEMS AND METHOD FOR COUPLING WEAR PAD INTO TURBINE COMBUSTION SYSTEM
- Patent Title (中): 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
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Application No.: US14833388Application Date: 2015-08-24
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Publication No.: US20170059158A1Publication Date: 2017-03-02
- Inventor: Kyle Lee Kidder , Tiffany Marie Craig , Eunice Delia Garza
- Applicant: General Electric Company
- Main IPC: F23R3/00
- IPC: F23R3/00 ; B23P15/00 ; F23R3/60

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.
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