| 发明名称 |
FUEL INJECTOR FOR HIGH ALTITUDE STARTING AND OPERATION OF A GAS TURBINE ENGINE |
| 摘要 |
A fuel injector for a combustor of a gas turbine engine includes an air swirler adjacent to a pressure atomizer. |
| 申请公布号 |
US2015354459(A1) |
申请公布日期 |
2015.12.10 |
| 申请号 |
US201414764469 |
申请日期 |
2014.01.30 |
| 申请人 |
Hamilton Sundstrand Corporation |
发明人 |
Chen Daih-Yeou;Hu Xiaolan;Peffley James;Lee Hanjie |
| 分类号 |
F02C7/26;F23R3/28 |
主分类号 |
F02C7/26 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A fuel injector for a combustor of a gas turbine engine comprising:
a pressure atomizer; and an air swirler adjacent to said pressure atomizer. |
| 地址 |
Windsor Locks CT US |
