Invention Grant
- Patent Title: Support assembly for transition duct in turbine system
- Patent Title (中): 涡轮机系统过渡管支撑组件
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Application No.: US13176183Application Date: 2011-07-05
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Publication No.: US08650852B2Publication Date: 2014-02-18
- Inventor: Jeffrey Scott LeBegue , Kevin Weston McMahan , Ronnie Ray Pentecost , James Scott Flanagan
- Applicant: Jeffrey Scott LeBegue , Kevin Weston McMahan , Ronnie Ray Pentecost , James Scott Flanagan
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Dority & Manning, PA
- Main IPC: F02C3/00
- IPC: F02C3/00

Abstract:
A support assembly for a turbine system is disclosed. The support assembly includes a transition duct extending between a fuel nozzle and a turbine section. The transition duct 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. The support assembly further includes an annular contact member extending from the transition duct. The contact member is configured to allow movement of the transition duct about at least one axis.
Public/Granted literature
- US20130008178A1 SUPPORT ASSEMBLY FOR TRANSITION DUCT IN TURBINE SYSTEM Public/Granted day:2013-01-10
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