| 发明名称 |
Trichannel airfoil leading edge cooling |
| 摘要 |
A turbine blade includes an airfoil having a leading edge flow chamber disposed behind a leading edge in front of a pair of side channels. The leading edge channel receives coolant from the pressure side channel in isolation from the suction side channel.
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| 申请公布号 |
US2003026698(A1) |
申请公布日期 |
2003.02.06 |
| 申请号 |
US20010921432 |
申请日期 |
2001.08.02 |
| 申请人 |
FLODMAN DAVID ALLEN;REDDY BHANU MAHASAMUDRAM;GLEDHILL MARK DOUGLAS |
发明人 |
FLODMAN DAVID ALLEN;REDDY BHANU MAHASAMUDRAM;GLEDHILL MARK DOUGLAS |
| 分类号 |
F01D5/18;(IPC1-7):F01D5/18 |
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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