发明名称 |
TURBINE BLADE IMPINGEMENT BAFFLE |
摘要 |
13DV-101370 An impingement-cooled gas turbine blade includes an impingement baffle which, during engine operation, is subject only to shear loading. A tubular baffle body is provided with a pair of mounting flanges which are bonded between a forward portion of the turbine blade and an aft portion of the turbine blade. The bond extends from the blade dovetail to the blade tip.
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申请公布号 |
CA2072386(A1) |
申请公布日期 |
1993.03.01 |
申请号 |
CA19922072386 |
申请日期 |
1992.06.25 |
申请人 |
CORSMEIER, ROBERT J.;MACLIN, HARVEY M. |
发明人 |
CORSMEIER, ROBERT J.;MACLIN, HARVEY M. |
分类号 |
F01D5/14;F01D5/18;F02C7/18;(IPC1-7):F01D5/18 |
主分类号 |
F01D5/14 |
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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