| 发明名称 |
COMBUSTOR WALL FOR A GAS TURBINE ENGINE AND METHOD OF ACOUSTIC DAMPENING |
| 摘要 |
A vascular wall of a combustor that may be for a gas turbine engine includes a first face defining at least in-part a combustion chamber, a second face defining at least in-part a cooling air plenum, and a vascular lattice structure located between the first and second faces for distributing cooling air from the plenum and to the chamber. The vascular lattice structure may be configured to enhance cooling air flow where needed whiling providing structural support. The orientation of the vascular lattice structure may further contribute toward acoustic dampening. |
| 申请公布号 |
US2016153658(A1) |
申请公布日期 |
2016.06.02 |
| 申请号 |
US201514805963 |
申请日期 |
2015.07.22 |
| 申请人 |
United Technologies Corporation |
发明人 |
Xu JinQuan |
| 分类号 |
F23R3/00;F02C7/24;F23R3/04 |
主分类号 |
F23R3/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A combustor wall comprising:
a first face defining at least in-part a combustion chamber; a second face defining at least in-part a cooling air plenum; and a vascular lattice structure located between the first and second faces for distributing cooling air from the plenum and to the chamber. |
| 地址 |
Hartford CT US |
