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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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