发明授权
- 专利标题: Flexible metallic seal for transition duct in turbine system
- 专利标题(中): 涡轮机系统中过渡管的柔性金属密封
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申请号: US13292389申请日: 2011-11-09
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公开(公告)号: US08701415B2公开(公告)日: 2014-04-22
- 发明人: James Scott Flanagan , Jeffrey Scott LeBegue , Kevin Weston McMahan , Daniel Jackson Dillard , Ronnie Ray Pentecost
- 申请人: James Scott Flanagan , Jeffrey Scott LeBegue , Kevin Weston McMahan , Daniel Jackson Dillard , Ronnie Ray Pentecost
- 申请人地址: US NY Schenectady
- 专利权人: General Electric Company
- 当前专利权人: General Electric Company
- 当前专利权人地址: US NY Schenectady
- 代理机构: Dority & Manning, PA
- 主分类号: F02C1/00
- IPC分类号: F02C1/00 ; F16J15/02 ; F01D5/00
摘要:
A turbine system is disclosed. In one embodiment, the turbine system includes a transition duct. The transition duct includes an inlet, an outlet, and a passage extending between the inlet and the outlet and defining a longitudinal axis, a radial axis, and a tangential axis. The outlet of the transition duct is offset from the inlet along the longitudinal axis and the tangential axis. The transition duct further includes an interface member for interfacing with a turbine section. The turbine system further includes a flexible metallic seal contacting the interface member to provide a seal between the interface member and the turbine section.
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