发明名称 Combustion Chamber/Venturi Configuration and Assembly Method
摘要 A two-stage gas turbine combustor is disclosed that incorporates an improved assembly and disassembly methodology that results in improved inspection and repair techniques. The combustor includes an upper liner, lower liner, cap assembly, and a venturi assembly that directs cooling air into the combustion chamber for use in the combustion process, wherein a venturi assembly is inserted within an upper liner and an upper liner is then inserted in a lower liner. The venturi assembly, upper liner, and lower liner are fixed together with a plurality of easily removable retaining pins. The improved assembly allows for easier inspection and repair of the upper liner, lower liner, and venturi assembly.
申请公布号 US2004112058(A1) 申请公布日期 2004.06.17
申请号 US20020248079 申请日期 2002.12.17
申请人 POWER SYSTEMS MFG, LLC 发明人 GARRIDO MIGUEL A.;MILLER SHAWN
分类号 F23R3/00;F23R3/60;(IPC1-7):F23R3/04 主分类号 F23R3/00
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