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 |