发明名称 Integral aft frame mount for a gas turbine combustor transition piece
摘要 A transition piece (110) for a gas turbine comprising a tubular body having an upstream end (112) and a downstream end (114), the downstream end (114) formed with an integral frame (116) surrounding an opening at the downstream end; and an aft mount connector 126) adapted to connect the transition piece (110) to a first stage nozzle of the gas turbine, the aft mount connector (126) formed integrally with the frame (116).
申请公布号 US5414999(A) 申请公布日期 1995.05.16
申请号 US19930147295 申请日期 1993.11.05
申请人 GENERAL ELECTRIC COMPANY 发明人 BARNES, JOHN E.
分类号 F01D9/02;(IPC1-7):F02C1/00 主分类号 F01D9/02
代理机构 代理人
主权项
地址