发明名称 Full ring inner air-seal with locking nut
摘要 A vane assembly has a vane including an inner platform with a mount rail extending radially inwardly toward an engine center axis. An air seal is attached to the inner platform. The air seal has a single-piece ring extending circumferentially about the engine center axis. A ring nut secures the air seal to the inner platform. A biasing member cooperates with the ring nut and air seal to seal fore and aft locations on the vane.
申请公布号 US9327368(B2) 申请公布日期 2016.05.03
申请号 US201213628298 申请日期 2012.09.27
申请人 United Technologies Corporation 发明人 Hagan Benjamin F.
分类号 F01D11/00;F01D11/02;B23P15/04;F02C7/28;F01D11/04;F01D11/10;F01D9/06 主分类号 F01D11/00
代理机构 Carlson, Gaskey & Olds, PC 代理人 Carlson, Gaskey & Olds, PC
主权项 1. A turbine section comprising: at least first and second turbine rotors each carrying turbine blades for rotation about a central axis, said first and second turbine rotors each having at least one rotating seal at a radially inner location; a vane assembly including a vane extending from a platform; an air seal attached to the vane assembly, the air seal comprising a ring extending circumferentially about the axis; a ring nut received on the air seal for axially securing the air seal to the vane assembly; and a biasing member reacting against the ring nut to prevent the ring nut from being removed from the air seal once the ring nut is installed.
地址 Hartford CT US