| 发明名称 |
FILM COOLING A COMBUSTOR WALL OF A TURBINE ENGINE |
| 摘要 |
An assembly is provided for a turbine engine. This turbine engine assembly includes a combustor wall including a shell and a heat shield. The combustor wall defines first and second cavities between the shell and the heat shield. The heat shield defines a first outlet and an elongated second outlet. The first outlet is fluidly coupled with the first cavity. The second outlet is fluidly coupled with the second cavity. The combustor wall defines one of the cavities with a tapered geometry. |
| 申请公布号 |
US2017009988(A1) |
申请公布日期 |
2017.01.12 |
| 申请号 |
US201515113558 |
申请日期 |
2015.02.03 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Cunha Frank J.;Kostka, JR. Stanislav |
| 分类号 |
F23R3/00;F02C7/12 |
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 and a heat shield, the combustor wall defining first and second cavities between the shell and the heat shield; the heat shield defining a first outlet and an elongated second outlet, the first outlet fluidly coupled with the first cavity, and the second outlet fluidly coupled with the second cavity; wherein the combustor wall defines one of the cavities with a tapered geometry. |
| 地址 |
Hartford CT US |
