发明名称 COOLED SNUBBER STRUCTURE FOR TURBINE BLADES
摘要 A turbine blade assembly in a turbine engine. The turbine blade assembly includes a turbine blade and a first snubber structure. The turbine blade includes an internal cooling passage containing cooling air. The first snubber structure extends outwardly from a sidewall of the turbine blade and includes a hollow interior portion that receives cooling air from the internal cooling passage of the turbine blade.
申请公布号 US2011194943(A1) 申请公布日期 2011.08.11
申请号 US201113023651 申请日期 2011.02.09
申请人 MAYER CLINTON A;CAMPBELL CHRISTIAN X;WHALLEY ANDREW;MARRA JOHN J 发明人 MAYER CLINTON A.;CAMPBELL CHRISTIAN X.;WHALLEY ANDREW;MARRA JOHN J.
分类号 F01D5/18;B21K25/00 主分类号 F01D5/18
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