| 发明名称 |
COOLING A QUENCH APERTURE BODY OF A COMBUSTOR WALL |
| 摘要 |
An assembly is provided for a turbine engine. A combustor wall of the turbine engine assembly includes a shell, a heat shield and an annular body engaged with the shell and the heat shield. The annular body extends through the combustor wall. The annular body at least partially defines a quench aperture along a centerline through the combustor wall. The annular body also at least partially defines a cooling aperture in fluid communication with the quench aperture. At least a portion of the cooling aperture extends radially outward from the quench aperture relative to the centerline. |
| 申请公布号 |
US2016290643(A1) |
申请公布日期 |
2016.10.06 |
| 申请号 |
US201415035356 |
申请日期 |
2014.12.04 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Cunha Frank J.;Kostka, Jr. Stanislav |
| 分类号 |
F23R3/00;F02C7/24;F02C7/18;F23R3/04 |
主分类号 |
F23R3/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An assembly for a turbine engine, the assembly comprising:
a combustor wall including a shell, a heat shield and an annular body engaged with the shell and the heat shield; the annular body extending through the combustor wall and at least partially defining a quench aperture along a centerline through the combustor wall, and a cooling aperture in fluid communication with the quench aperture; wherein at least a portion of the cooling aperture extends radially outward from the quench aperture relative to the centerline. |
| 地址 |
Hartford CT US |
