| 发明名称 |
SWIRLER MOUNT INTERFACE FOR GAS TURBINE ENGINE COMBUSTOR |
| 摘要 |
A swirler for a combustor of a gas turbine engine includes a swirler outer body with a male snap component and/or female snap component of a snap-fit interface defined around a swirler central longitudinal axis. A bulkhead assembly for a combustor of a gas turbine engine includes a swirler mounted to a bulkhead support shell through a snap-fit interface. |
| 申请公布号 |
US2016201915(A1) |
申请公布日期 |
2016.07.14 |
| 申请号 |
US201414911205 |
申请日期 |
2014.06.30 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Williams Alexander W.;Max Seth A.;Lyons Christopher B. |
| 分类号 |
F23R3/12;F23R3/60 |
主分类号 |
F23R3/12 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A swirler for a combustor of a gas turbine engine, the swirler comprising:
a swirler outer body with at least one of a male snap component or a female snap component of a snap-fit interface. |
| 地址 |
Hartford CT US |
