发明名称 Method of producing a turbine blade
摘要 In a method of producing a turbine blade in hollow section, an especially low defect or scrap rate is to be ensured. To this end, a first core element is connected via a number of approximately cylindrical spacers to a further core element and/or to a casting mold, the cavities left in the casting mold by the core elements being filled by blade material, and the openings remaining in the turbine blade after the removal of the core elements and the spacers and produced by the spacers being closed by stopper elements.
申请公布号 US2002157251(A1) 申请公布日期 2002.10.31
申请号 US20020117633 申请日期 2002.04.04
申请人 ESSER WINFRIED;HAENDLER MICHAEL;TIEMANN PETER 发明人 ESSER WINFRIED;HAENDLER MICHAEL;TIEMANN PETER
分类号 F01D5/18;B22C21/14;F01D9/02;F02C7/00;(IPC1-7):B21K3/04;B21D53/78;B23P15/02 主分类号 F01D5/18
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