发明名称 METHOD OF MANUFACTURING TURBINE BLADE
摘要 PROBLEM TO BE SOLVED: To guarantee the high-yield manufacturing of a turbine blade having cavities. SOLUTION: A core element 10 is joined to a separate core element and/or casting mold via a plurality of almost cylindrical spacers 14. A blade material is cast in the casting mold. After removing the core element 10 and the spacers 14, an opening formed by the spacers 14 and the cavities 4 and 6 formed by the core element 10 remain in the turbine blade 1. The opening is closed by a blocking element.
申请公布号 JP2002349285(A) 申请公布日期 2002.12.04
申请号 JP20020098225 申请日期 2002.04.01
申请人 SIEMENS AG 发明人 ESSER WINFRIED;HAENDLER MICHAEL;TIEMANN PETER
分类号 F01D5/18;B22C21/14;F01D9/02;F02C7/00;(IPC1-7):F02C7/00 主分类号 F01D5/18
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