| 发明名称 |
Pressure Seal With Non-Metallic Wear Surfaces |
| 摘要 |
A gas turbine engine has a first component and a second component. The first and second components have a high-pressure chamber on one side and a low pressure chamber on an opposed side. A three sided seal has one side facing each of the first and second components, and a third side facing a third component. At least one non-metallic wear surface is between one of the three sides of the seal and the facing component. |
| 申请公布号 |
US2016146032(A1) |
申请公布日期 |
2016.05.26 |
| 申请号 |
US201615011720 |
申请日期 |
2016.02.01 |
| 申请人 |
United Technologies Corporation |
发明人 |
Burd Steven W. |
| 分类号 |
F01D11/02;F16J15/447 |
主分类号 |
F01D11/02 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A gas turbine engine comprising:
a first component and a second component, said first and second components having a high-pressure chamber on one side, and a low pressure chamber on an opposed side, and a three sided seal having one side facing each of said first and second components, and having a third side facing a third component, and there being at least one non-metallic wear surface between one of said three sides of said seal and said facing component. |
| 地址 |
Hartford CT US |
