发明名称 Turbine airfoil with platform cooling
摘要 Convective cooling of gas turbine engine airfoil platforms is enhanced by grooving the interface of the platforms with corresponding platform-to-platform seals, thereby accelerating cooling airflow over the platform surfaces.
申请公布号 US2009116953(A1) 申请公布日期 2009.05.07
申请号 US20070982578 申请日期 2007.11.02
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 SPANGLER BRANDON W.;PAAUWE CORNEIL S.;LEHANE CHRISTOPHER J.;TRACY ANITA L.;WIEDEMER JOHN D.;HJELM SCOTT D.
分类号 F02C7/18;F02C7/28 主分类号 F02C7/18
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