发明名称 TURBINE BLADE HAVING SWIRLING COOLING CHANNEL AND COOLING METHOD THEREOF
摘要 PROBLEM TO BE SOLVED: To provide a turbine blade which includes a swirl portion provided at a cooling channel entrance through which cooling air is passed, thereby increasing the cooling performance of a root unit and significantly improving the stiffness of the root unit.SOLUTION: A turbine blade according to the present invention comprises a cooling channel through which cooling air is passed; and a swirl portion provided at an entrance of the cooling channel so as to form a swirl flow in the cooling air. The turbine blade may increase cooling performance of a root unit, improve the stiffness of the root unit, and significantly increase the internal heat transfer efficiency of a blade unit.
申请公布号 JP2015135113(A) 申请公布日期 2015.07.27
申请号 JP20150004768 申请日期 2015.01.14
申请人 DOOSAN HEAVY INDUSTRIES & CONSTRUCTION CO LTD 发明人 JUNG SUNG CHUL
分类号 F01D5/18;F02C7/18 主分类号 F01D5/18
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