发明名称 |
Serpentine Cooling of Nozzle Endwall |
摘要 |
A gas turbine nozzle section of a gas turbine may include an inner endwall with a leading edge. A serpentine passage may be configured substantially within the leading edge. The serpentine passage may have an inlet and an outlet. Air may be received at the inlet and exhausted at the outlet, cooling the leading edge. |
申请公布号 |
US2014072400(A1) |
申请公布日期 |
2014.03.13 |
申请号 |
US201213608269 |
申请日期 |
2012.09.10 |
申请人 |
DILLARD DANIEL JACKSON;PORTER CHRISTOPHER DONALD;GENERAL ELECTRIC COMPANY |
发明人 |
DILLARD DANIEL JACKSON;PORTER CHRISTOPHER DONALD |
分类号 |
B64D33/04 |
主分类号 |
B64D33/04 |
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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