发明名称 |
Support assembly for a turbine system and corresponding turbine system |
摘要 |
<p>A support assembly (100) for a turbine system (10) is disclosed. The support assembly (100) includes a transition duct (50) extending between a fuel nozzle and a turbine section. The transition duct (50) has an inlet (52), an outlet (54), and a passage (56) extending between the inlet (52) and the outlet (54) and defining a longitudinal axis (90), a radial axis (94), and a tangential axis (92). The outlet (54) of the transition duct (50) is offset from the inlet (52) along the longitudinal axis. The support assembly (100) further includes a plurality of protrusions (102) extending from the transition duct (50). The plurality of protrusions (102) are configured to allow movement of the transition duct (50) about at least one axis. A corresponding turbine system is also provided.</p> |
申请公布号 |
EP2543824(B1) |
申请公布日期 |
2014.12.03 |
申请号 |
EP20120174844 |
申请日期 |
2012.07.03 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
LEBEGUE, JEFFREY SCOTT;MCMAHAN, KEVIN WESTON;PENTECOST, RONNIE RAY;FLANAGAN, JAMES SCOTT |
分类号 |
F01D9/02;F02C3/14 |
主分类号 |
F01D9/02 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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