| 发明名称 |
COMBUSTOR QUENCH APERTURE COOLING |
| 摘要 |
An assembly is provided for a turbine engine. This turbine engine assembly includes a combustor wall. The combustor wall includes a shell, a heat shield and an annular body. The annular body extends through the combustor wall and at least partially defines a quench aperture along a centerline through the combustor wall. The shell defines a first cooling aperture radially outwards of the annular body relative to the centerline and is configured to direct air to impinge against a portion of the annular body between the heat shield and the shell. |
| 申请公布号 |
US2016290644(A1) |
申请公布日期 |
2016.10.06 |
| 申请号 |
US201415037555 |
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;F23R3/06;F02C7/18 |
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; the annular body extending through the combustor wall and at least partially defining a quench aperture along a centerline through the combustor wall; and the shell defining a first cooling aperture radially outward of the annular body relative to the center line and configured to direct air to impinge against a portion of the annular body between the heat shield and the shell. |
| 地址 |
Hartford CT US |
