发明名称 Banked platform turbine blade
摘要 A turbine blade includes an airfoil and integral platform at the root thereof. The platform is contoured in elevation from a bank adjacent the pressure side of the airfoil to a trough commencing behind the airfoil leading edge.
申请公布号 US8647067(B2) 申请公布日期 2014.02.11
申请号 US20080330783 申请日期 2008.12.09
申请人 PANDEY VIDHU SHEKHAR;CLEMENTS JEFFREY DONALD;LEE CHING-PANG;GENERAL ELECTRIC COMPANY 发明人 PANDEY VIDHU SHEKHAR;CLEMENTS JEFFREY DONALD;LEE CHING-PANG
分类号 B63H1/26;B63H1/16 主分类号 B63H1/26
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