发明授权
- 专利标题: Load member for transition duct in turbine system
- 专利标题(中): 涡轮系统中过渡管的负载构件
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申请号: US13152638申请日: 2011-06-03
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公开(公告)号: US08978388B2公开(公告)日: 2015-03-17
- 发明人: James Scott Flanagan , Jeffrey Scott LeBegue , Kevin Weston McMahan , Ronnie Ray Pentecost
- 申请人: James Scott Flanagan , Jeffrey Scott LeBegue , Kevin Weston McMahan , 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, P.A.
- 主分类号: F23R3/60
- IPC分类号: F23R3/60 ; F23R3/42 ; F23R3/00 ; F01D9/02 ; F01D25/28
摘要:
A loading assembly for a turbine system is disclosed. The loading assembly includes a transition duct and a load member. The transition duct extends between a fuel nozzle and a turbine section, and has 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 load member extends from the transition duct and is configured to transfer a load between the transition duct and an adjacent transition duct along at least one of the longitudinal axis, the radial axis, or the tangential axis.
公开/授权文献
- US20120304653A1 LOAD MEMBER FOR TRANSITION DUCT IN TURBINE SYSTEM 公开/授权日:2012-12-06
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