发明名称 |
Open-cooled component for a gas turbine, combustion chamber, and gas turbine |
摘要 |
An open-cooled component for a gas turbine is provided. The component includes an outer wall that is subjected to a hot gas and at least partially defines a first cavity for a first means. The outer wall is provided with through-openings which open up into the cavity on one side and into a hot gas chamber on the other. The inventive component also includes at least one second cavity for admixing a second means, said second cavity is connected to the through-openings in a fluid-connected manner. A combustion chamber for a gas turbine, and to a gas turbine including one such component is also provided.
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申请公布号 |
US2010083665(A1) |
申请公布日期 |
2010.04.08 |
申请号 |
US20090631940 |
申请日期 |
2009.12.07 |
申请人 |
HOFFMANN STEFAN |
发明人 |
HOFFMANN STEFAN |
分类号 |
F02C1/00;F01D5/18;F01D25/12;F23M5/08;F23R3/00;F23R3/30 |
主分类号 |
F02C1/00 |
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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