发明名称 |
Alabe de turbina |
摘要 |
The invention relates to a turbine blade comprising a profiled vane around which working gas flows. The working gas cross-flows a front edge of the vane and flows away on a rear edge of the vane. The vane has a first and a second channel system for guiding two media separated from the turbine blade. Combustion taking place inside is reduced in a safe manner to maintain the service life of the turbine blade and to prevent damage in the gas turbine, such that a first outlet connected to the first channel system is arranged in the region of the rear edge for blowing out the first media into the working gas and a second outlet connected to the second channel system is arranged in the region of the rear edge for blowing out the second medium.
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申请公布号 |
ES2426349(T3) |
申请公布日期 |
2013.10.22 |
申请号 |
ES20070726359T |
申请日期 |
2007.02.13 |
申请人 |
SIEMENS AKTIENGESELLSCHAFT |
发明人 |
BEECK, ALEXANDER RALPH;HOFFMANN, STEFAN |
分类号 |
F01D5/18;F01D5/14;F01D9/06;F02C3/16;F02K3/08 |
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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