| 发明名称 |
GAS TURBINE ENGINE BRUSH SEAL WITH SUPPORTED TIP |
| 摘要 |
As assembly is provided for a gas turbine engine. This assembly includes a component and a brush seal. The component includes a first surface and a second surface. The brush seal includes an annular bundle of bristles which extends longitudinally along an axis to a bundle tip. The bundle of bristles axially contacts the first surface at the bundle tip. The bundle of bristles proximate the bundle tip axially overlaps the second surface, and the bundle of bristles is operable to radially contact the second surface. |
| 申请公布号 |
US2016312637(A1) |
申请公布日期 |
2016.10.27 |
| 申请号 |
US201514697104 |
申请日期 |
2015.04.27 |
| 申请人 |
United Technologies Corporation |
发明人 |
Duguay Brian |
| 分类号 |
F01D11/08;F01D9/04 |
主分类号 |
F01D11/08 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An assembly for a gas turbine engine, comprising:
a component including a first surface and a second surface; and a brush seal including an annular bundle of bristles which extends longitudinally along an axis to a bundle tip; wherein the bundle of bristles axially contacts the first surface at the bundle tip; and wherein the bundle of bristles proximate the bundle tip axially overlaps the second surface, and the bundle of bristles is operable to radially contact the second surface. |
| 地址 |
Hartford CT US |
