发明名称 BLADE TIP COOLING GROOVE
摘要 An example turbine blade includes a blade having an airfoil profile extending radially toward a blade tip. A shelf is established in the blade tip. A sealing portion of the blade tip extends radially past a floor of the shelf. The sealing portion extends from a blade tip leading edge to a blade tip trailing edge. A groove is established in the blade tip. The groove extends from adjacent the shelf to adjacent the blade tip trailing edge. The groove is configured to communicate a fluid from a position adjacent the shelf to a position adjacent the blade tip trailing edge.
申请公布号 US2010232979(A1) 申请公布日期 2010.09.16
申请号 US20090402571 申请日期 2009.03.12
申请人 PAAUWE CORNEIL S;SPANGLER BRANDON W 发明人 PAAUWE CORNEIL S.;SPANGLER BRANDON W.
分类号 F01D5/18;F01D11/08 主分类号 F01D5/18
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