发明名称 GAS TURBINE WITH WELDED COMBUSTOR LINERS
摘要 In order to provide an annular combustion chamber (3) which can be heated without thermal distortion, expands without distortion, and is reliably closed, and for repairs can be opened and permanently closed again and can be reconditioned, the inner and/or outer shell (8, 7) of an annular combustion chamber (3) is produced from a rotationally symmetrical sheet metal. For assembly, the shells are cut open along a split line (16), and the lower half of the inner and of the outer shell (8, 7) is introduced into the lower casing half of a gas turbine. After the insertion of the rotor, the two upper shell halves can likewise be inserted and be connected to the lower halves by welding. In order to improve the service life of the split line weld seam (21), film cooling of the weld seam is routed by an indentation. This may be implemented, for example, by welded-in split line elements (15) which are also suitable for retrofitting.
申请公布号 US2010205973(A1) 申请公布日期 2010.08.19
申请号 US20100724550 申请日期 2010.03.16
申请人 TSCHUOR REMIGI;SCHNEIDER LOTHAR;MARKOVIC ALEN;HAEHNLE HARTMUT 发明人 TSCHUOR REMIGI;SCHNEIDER LOTHAR;MARKOVIC ALEN;HAEHNLE HARTMUT
分类号 F02C7/18;B23P6/00 主分类号 F02C7/18
代理机构 代理人
主权项
地址