发明名称 |
Cooled turbomachinery element and casting method thereof |
摘要 |
<p>A cooling channel (41) is provided in the outer wall of the blade that is impinged upon by a working medium (A). A cooling fluid (KF) flows along the longitudinal axis of the cooling channel. A device is provided in the cooling channel for imparting a swirl on the flowing cooling fluid. Preferably, at least one turbulator element (47) is provided on the inner surface of the cooling channel. Independent claims are included for a gas turbine and for a method of casting a cooled component.</p> |
申请公布号 |
EP1621730(A1) |
申请公布日期 |
2006.02.01 |
申请号 |
EP20040017673 |
申请日期 |
2004.07.26 |
申请人 |
SIEMENS AKTIENGESELLSCHAFT |
发明人 |
DELLMANN, JUERGEN;LANG, GERNOT |
分类号 |
F01D5/18;F01D25/24;F23R3/00 |
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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