发明名称 Turbine shroud segment seal
摘要 A ring seal for sealing an annular gap defined between opposed surfaces of concentric inner and outer annular engine parts in a gas turbine engine. The ring seal being wholly disposed within the annular gap and having a wave pattern with alternating peaks. The ring seal radially inwardly loads the inner engine part and provides a fluid seal between the inner and outer engine parts.
申请公布号 US7207771(B2) 申请公布日期 2007.04.24
申请号 US20040965234 申请日期 2004.10.15
申请人 PRATT & WHITNEY CANADA CORP. 发明人 SYNNOTT REMY;BLAIS DANY
分类号 F04D29/08 主分类号 F04D29/08
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