发明名称 |
HEAT SHIELD ELEMENT FOR A GAS TURBINE |
摘要 |
Heat shield element (HS) for a gas turbine (GT) comprising an areal wall section (WS), said wall section (WS) being defined by limiting edges of the heat shield element (HS), and having a defined thickness (TH) extending radially from an inner surface (IS) to an outer surface (OS) said inner surface (IS) is exposed to a hot gas path (HGP) and said outer surface (OS) is exposed to a coolant (CO). To improve cooling efficiency, cooling channels (CC) are provided through the wall of said wall section (WS) said cooling channels (CC) comprising a first section (SI) starting at the inner surface (IS), further comprising a second section (S2) extending between the inner surface (IS) and the outer surface (OS) along a length of at least three times the thickness (TH) of the wall section (WS) at that specific area of the second section and comprising a third section (S3) joining the hot gas path so that said cooling channels (CC) connect said cavity (CV) with the hot gas path (HGP). |
申请公布号 |
WO2013011126(A3) |
申请公布日期 |
2013.05.30 |
申请号 |
WO2012EP64286 |
申请日期 |
2012.07.20 |
申请人 |
SIEMENS AKTIENGESELLSCHAFT;SZIJARTO, JANOS;GRANBERG, PER;UTRIAINEN, ESA |
发明人 |
SZIJARTO, JANOS;GRANBERG, PER;UTRIAINEN, ESA |
分类号 |
F01D11/08;F01D25/14 |
主分类号 |
F01D11/08 |
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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