发明名称 TURBINE BLADE HAVING PLATFORM AND AIRFOIL EXTENDED FROM ROOT OF PLATFORM TO TIP
摘要 PURPOSE: A turbine blade is provided to secure efficient cooling by improving the turbine blade. CONSTITUTION: A turbine blade(20) includes a platform(26) and an airfoil(22). The airfoil has a root(24) of the platform, a tip(28), a front edge(40) and a trailing edge(42), and an inner cooling passage network. The inner cooling passage network includes at least one trailing edge cavity, plural trailing edge holes(50) extended from the trailing edge to the trailing edge cavity, and plural tip holes extended from the tip to the trailing edge cavity.
申请公布号 KR20040070072(A) 申请公布日期 2004.08.06
申请号 KR20040005922 申请日期 2004.01.30
申请人 UNITED TECHNOLOGIES CORP. 发明人 CHLUS WIESLAW A.;FUNK STANLEY J.
分类号 B22C9/24;F01D5/18;F01D5/20;F02C7/00;(IPC1-7):F01D5/18 主分类号 B22C9/24
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