发明名称 AIRFOIL COOLING ARRANGEMENT
摘要 An airfoil according to an exemplary embodiment of the present disclosure can include an airfoil body having a plurality of film cooling holes that extend through an exterior surface of the airfoil body. Each of the plurality of film cooling holes break through the exterior surface at geometric coordinates in accordance with Cartesian coordinate values of X, Y and Z as set forth in Table 1. Each of the geometric coordinates is measured from a reference point on a leading edge rail of a platform of the airfoil.
申请公布号 US2014010632(A1) 申请公布日期 2014.01.09
申请号 US201213539838 申请日期 2012.07.02
申请人 SPANGLER BRANDON W.;BERGMAN RUSSELL J. 发明人 SPANGLER BRANDON W.;BERGMAN RUSSELL J.
分类号 F01D5/18 主分类号 F01D5/18
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