发明名称 Dichtung für Turbinenschaufelplattformen
摘要 A seal for a turbine blade in a gas turbine engine has a sealing portion 72 with two subportions 80,82, where the subportions 80,82 are longitudinally offset from one another, so that the seal may provide sealing for adjacent turbine blades having longitudinally offset inner platform surfaces. <IMAGE>
申请公布号 DE69728508(D1) 申请公布日期 2004.05.13
申请号 DE1997628508 申请日期 1997.12.23
申请人 UNITED TECHNOLOGIES CORP., HARTFORD 发明人 HOUSTON, DAVID P.;AIREY, DAVID;PELLAND, NATALIE A.
分类号 F01D5/30;F01D11/00 主分类号 F01D5/30
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