发明名称 Turbine interstage seal system
摘要 A system includes a multi-stage turbine. The multi-stage turbine has an interstage seal extending axially between a first turbine stage and a second turbine stage. The interstage seal has an upper body that extends from an upstream seating arm to a downstream seating arm. The upstream and downstream seating arms are designed to constrain movement of the interstage seal along a radial direction of the multi-stage turbine. The interstage seal also has a lower body that extends from a seating end to a hook end. The seating end is designed to constrain movement of the interstage seal along the radial direction. The hook end has a protrusion that extends crosswise relative to a base of the lower body. The hook end is designed to constrain movement of the interstage seal along the radial direction and an axial direction of the multi-stage turbine.
申请公布号 US9540940(B2) 申请公布日期 2017.01.10
申请号 US201213418281 申请日期 2012.03.12
申请人 General Electric Company 发明人 Liotta Gary Charles;Potter Brian Denver
分类号 F01D11/00 主分类号 F01D11/00
代理机构 Fletcher Yoder, P.C. 代理人 Fletcher Yoder, P.C.
主权项 1. A system, comprising: a multi-stage turbine, comprising: an interstage seal extending in an axial direction relative to a rotational axis of the multi-stage turbine between a first turbine stage and a second turbine stage, wherein the interstage seal comprises: an upper body extending from an upstream seating arm to a downstream seating arm, wherein the upstream and downstream seating arms are configured to constrain movement of the interstage seal along a radial direction relative to the rotational axis of the multi-stage turbine; anda lower body extending from a seating end to a hook end, wherein the seating end is configured to constrain movement of the interstage seal along the radial direction, and the hook end comprises an integral protrusion extending crosswise relative to a base of the lower body, wherein the hook end is configured to constrain movement of the interstage seal along the radial direction and the axial direction, the integral protrusion is axially constrained in an upstream direction and a downstream direction by a groove adjacent a lower support of a second rotor wheel of the second turbine stage, and the lower body comprises a hollow region that is axially and radially enclosed relative to the rotational axis of the multi-stage turbine.
地址 Schenectady NY US