| 发明名称 |
INNER DIFFUSER CASE FOR A GAS TURBINE ENGINE |
| 摘要 |
A combustor section of a gas turbine engine has a diffuser case with a structural cone having variable wall thicknesses strategically located for reducing localized stress in the cone. |
| 申请公布号 |
US2016265371(A1) |
申请公布日期 |
2016.09.15 |
| 申请号 |
US201415029474 |
申请日期 |
2014.10.31 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Dale Timothy;Bhanderi Swati G. |
| 分类号 |
F01D9/02;F23R3/10 |
主分类号 |
F01D9/02 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A diffuser case for use in a gas turbine engine, the diffuser case comprising:
a structural cone having a variable wall thickness configured to reduce thermal induced stress. |
| 地址 |
Hartford CT US |
