发明名称 Turbine blade trip strip orientation
摘要 <p>A turbine component (20c) includes a coolant passage (42) and a plurality of trip members (50) that extend within the coolant passage (42). Each of the plurality of trip members (50) includes an orientation relative to an expected flow direction through the coolant passage (42). At least three of the trip members (50) have orientations that are different from each other. For example, the orientations of the trip members (50) may progressively transition along the length of the coolant passage (42).</p>
申请公布号 EP1944469(A2) 申请公布日期 2008.07.16
申请号 EP20070254923 申请日期 2007.12.18
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 PIETRASZKIEWICZ, EDWARD F.;DOWNS, JAMES P.
分类号 F01D5/18 主分类号 F01D5/18
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