| 发明名称 |
GAS TURBINE ENGINE COMPONENT MATEFACE SURFACES |
| 摘要 |
An array of components in a gas turbine engine includes first and second structures respectively including first and second surfaces that are arranged adjacent to one another to provide a gap. The first and second surfaces respectively have first and second rounded edges at the gap that are arranged in staggered relationship relative to one another. |
| 申请公布号 |
US2017022839(A1) |
申请公布日期 |
2017.01.26 |
| 申请号 |
US201415039945 |
申请日期 |
2014.11.13 |
| 申请人 |
United Technologies Corporation |
发明人 |
Lewis Scott D.;Kohli Atul;Praisner Thomas J. |
| 分类号 |
F01D11/08;F01D9/02;F01D5/12 |
主分类号 |
F01D11/08 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An array of components in a gas turbine engine, comprising:
first and second structures respectively include first and second surfaces that are arranged adjacent to one another to provide a gap, the first and second surfaces respectively have first and second rounded edges at the gap that are arranged in staggered relationship relative to one another. |
| 地址 |
Farmington CT US |
