发明名称 Combustor and cap assemblies for combustors in a gas turbine
摘要 The cap assembly of a turbine combustor includes a plurality of burner tubes sealed against fuel nozzles extending in the tubes. These piston seals are coated with a high velocity oxygen fuel coating to extend their service life. The outer cap body assembly includes concentric seal rings each with cantilevered convex fingers circumferentially offset from one another to seal between the cap assembly casing and the inner liner. The cap assembly casing is provided with a plurality of holes at predetermined locations about the casing to minimize or eliminate response to combustion dynamics.
申请公布号 US2006230763(A1) 申请公布日期 2006.10.19
申请号 US20050104549 申请日期 2005.04.13
申请人 GENERAL ELECTRIC COMPANY 发明人 JOHNSON JERE A.;BAILEY MARK;BERRY ROBERT R.;BEITZ STEWART W.;MONAGHAN JAMES C.
分类号 F23R3/42 主分类号 F23R3/42
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