| 发明名称 |
GAS TURBINE ENGINE COMBUSTOR |
| 摘要 |
A swirler assembly for a gas turbine engine includes an outer annular injector which at least partially surrounds an inner injector and an air-assist atomizer upstream of said inner injector. |
| 申请公布号 |
US2016040881(A1) |
申请公布日期 |
2016.02.11 |
| 申请号 |
US201414773971 |
申请日期 |
2014.03.13 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Cunha Frank;Erbas-Sen Nurhak |
| 分类号 |
F23R3/06;F23R3/26;F23R3/14 |
主分类号 |
F23R3/06 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A swirler for a combustor of a gas turbine engine comprising:
an inner injector; an outer annular injector which at least partially surrounds said inner injector; and an air-assist atomizer upstream of said inner injector. |
| 地址 |
Hartford CT US |
