发明名称 TURBINE AIRFOIL COOLING PASSAGE WITH DIAMOND TURBULATOR
摘要 <p>The present invention relates to a turbulator having a diamond-shaped configuration where a front portion of the turbulator is a mirror image of a rear portion of the turbulator; and where the turbulator has an application to cool flow channels on a blade of a gas turbine engine. An array of the diamond-shaped turbulators is positioned in rows relative to the flow of the cooling air such that the turbulator in one of the rows is positioned relative to the gap between two turbulators in an adjacent row to break up the flow of air flowing between the turbulators.</p>
申请公布号 KR20150063950(A) 申请公布日期 2015.06.10
申请号 KR20140170763 申请日期 2014.12.02
申请人 SIEMENS ENERGY, INC. 发明人 LIANG GEORGE
分类号 F01D5/18;F02C7/18;F15D1/12 主分类号 F01D5/18
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