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.
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
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