发明名称 Brush seal for turbine
摘要 A brush seal for a turbine including an annular layer of filaments having a generally L-shape including an axial portion of the filaments and a radial portion of filaments, wherein a first end of the filaments is at an end of the radial portion and faces a rotating component of the turbine and a second end region of the filaments is at an end of the axial portion of the filaments and is fastened to a stationary component of the turbine.
申请公布号 US9322287(B2) 申请公布日期 2016.04.26
申请号 US201414294812 申请日期 2014.06.03
申请人 General Electric Company 发明人 Zheng Xiaoqing;Mack Michael Dennis;Mukhopadhyay Debabrata
分类号 F16J15/32;F01D11/02;F01D11/00;F04D29/08 主分类号 F16J15/32
代理机构 Nixon & Vanderhye P.C. 代理人 Nixon & Vanderhye P.C.
主权项 1. A brush seal for a turbine having a rotating axis, the brush seal comprising: an annular layer of filaments being L-shaped in cross section and including an axial portion of the filaments extending in a direction substantially parallel to the rotating axis and a radial portion extending in a direction substantially perpendicular to the rotating axis, wherein a first end of the filaments is at an end of the radial portion and faces a rotating component of the turbine and a second end region of the filaments includes an end of the axial portion of the filaments and is configured to be fastened to a stationary component of the turbine, and annular side rails which sandwiched the second end region of the filaments, wherein the side rails are coaxial and aligned along a common radius, and one of the annular side rails seats in a step or groove in a stationary annular structure which supports the filaments.
地址 Schenectady NY US