发明名称 |
Microcircuit airfoil mainbody |
摘要 |
A cooling circuit disposed within a first wall portion and a second wall portion of a wall for use in a gas turbine engine is provided. The cooling circuit includes a plurality of inlet apertures disposed in the first wall portion to provide a flow path of cooling air into the cooling circuit, a first exit slot disposed in the second wall portion to provide a cooling air flow path out of the cooling circuit, a plurality of pedestals arranged in rows extending within the between the first wall portion and the second wall portion and a first elongated pedestal disposed radially and extending between the first and second wall portions. The first elongated pedestal is positioned between the pedestals and the first exit slot.
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申请公布号 |
US2005031450(A1) |
申请公布日期 |
2005.02.10 |
申请号 |
US20030637352 |
申请日期 |
2003.08.08 |
申请人 |
CUNHA FRANK J.;SANTELER KEITH A. |
发明人 |
CUNHA FRANK J.;SANTELER KEITH A. |
分类号 |
F01D5/18;F02C7/18;(IPC1-7):F01D5/08 |
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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