发明名称 Film-cooled turbine blade for a turbomachine
摘要 The turbine blade has an outer wall (1) that restricts an inner hollow space (2), in which cooling fluid (4) is provided for film cooling of the turbine blade. A passageway (3) is provided in the outer wall. The cooling fluid is flowed through the passageway from the internal hollow space to outside the turbine blade for forming a cooling film (5) on outer side of the outer wall. An edge section (14) of an inlet (10) of the passageway is formed upstream to a side (12) relative to another edge section of the inlet.
申请公布号 EP2584147(A1) 申请公布日期 2013.04.24
申请号 EP20110186219 申请日期 2011.10.21
申请人 SIEMENS AKTIENGESELLSCHAFT 发明人 HESELHAUS, ANDREAS
分类号 F01D5/18 主分类号 F01D5/18
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