发明名称 COMBUSTOR HEAT SHIELD SEALING
摘要 A method and an apparatus for reducing airflow leakage between a combustor liner and a rail of a heat shield mounted to an inner surface of the combustor liner. The method comprises locally deforming the combustor liner in sealing engagement with the rail by applying a pressure on the outer surface of the combustor liner over the rail of the heat shield. A tool, such as a sealing clip, may be mounted in pressing engagement with the outer surface of the combustor liner to apply forces locally on the liner over the rail of the heat shield.
申请公布号 US2016040878(A1) 申请公布日期 2016.02.11
申请号 US201414455185 申请日期 2014.08.08
申请人 Pratt & Whitney Canada Corp. 发明人 HAYEK Daniel;HERBORTH Jason;WANG Yen-Wen
分类号 F23R3/00;F02C7/20;B23P19/04 主分类号 F23R3/00
代理机构 代理人
主权项 1. A method of providing a seal between a combustor liner and a rail of a heat shield mounted to an inner surface of the combustor liner, the method comprising: locally deforming the combustor liner in sealing engagement with the rail by applying a pressure on the outer surface of the combustor liner over the rail of the heat shield.
地址 Longueuil CA