发明名称 Attachment Faces for Clamped Turbine Stator of a Gas Turbine Engine
摘要 An airfoil fairing shell for a gas turbine engine includes an airfoil section between an outer vane endwall and an inner vane endwall, at least one of the outer vane endwall and the inner vane endwall including a radial attachment face, a suction side tangential attachment face, a pressure side tangential attachment face, and an axial attachment face.
申请公布号 US2016069201(A1) 申请公布日期 2016.03.10
申请号 US201514841943 申请日期 2015.09.01
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 Carr Jesse M.;Dube Bryan P.
分类号 F01D9/04 主分类号 F01D9/04
代理机构 代理人
主权项 1. An airfoil fairing shell for a gas turbine engine comprising: an airfoil section between an outer vane endwall and an inner vane endwall, at least one of said outer vane endwall and said inner vane endwall including a radial attachment face, a suction side tangential attachment face, a pressure side tangential attachment face, and an axial attachment face.
地址 Hartford CT US