发明名称 STRUCTURAL STATOR AIRFOIL
摘要 An airfoil comprises a leading edge, a trailing edge, and pressure and suction surfaces defined therebetween. An inner platform is coupled to a root section of the airfoil, with a curvilinear gusset extending along a lower surface of the inner platform, opposite the root section. An outer platform is coupled to a tip section of the airfoil, with a multi-lobed gusset extending along an upper surface of the inner platform, opposite the tip section.
申请公布号 US2013121833(A1) 申请公布日期 2013.05.16
申请号 US201113295724 申请日期 2011.11.14
申请人 LUCASHU JOHN P.;REINHARDT GREGORY E.;DITOMASSO JOHN C.;UNITED TECHNOLOGIES CORPORATION 发明人 LUCASHU JOHN P.;REINHARDT GREGORY E.;DITOMASSO JOHN C.
分类号 F01D5/14;F01D5/30 主分类号 F01D5/14
代理机构 代理人
主权项
地址