发明名称 METHOD OF REPAIRING COMBUSTION CHAMBER LINER
摘要 PROBLEM TO BE SOLVED: To provide a method of repairing a damaged annular transpiration cooling type liner for a as turbine engine combustion chamber. SOLUTION: An annular portion of the liner including a damaged region is removed from a space between an upstream section and a downstream section of the liner. A metal thin plate is molded into an annular replacement section having at least one axial joint extending to a space between the upstream end and the downstream end of a replacement section. The replacement section is formed in size and shape similar to the removed annular portion of the liner. The upstream end of the molded annular section is joined to the upstream section of the liner and the downstream end of the molded annular section is joined to the downstream section of the liner.
申请公布号 JP2002138853(A) 申请公布日期 2002.05.17
申请号 JP20010216070 申请日期 2001.07.17
申请人 GENERAL ELECTRIC CO <GE> 发明人 GILBERT FARMER;CALDWELL JAMES MICHAEL;STIVERSON STEVEN ALLEN;PATTERSON DAVID BRUCE;EMILIANOWICZ EDWARD JOHN
分类号 F02C7/00;B23K15/00;B23P6/00;F23R3/00;(IPC1-7):F02C7/00 主分类号 F02C7/00
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