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 |
EP3077640(A1) |
申请公布日期 |
2016.10.12 |
申请号 |
EP20140867674 |
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 |
F02C7/12;F23R3/00;F23R3/06;F23R3/42 |
主分类号 |
F02C7/12 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|