| 发明名称 |
CAVITY SWIRL FUEL INJECTOR FOR AN AUGMENTOR SECTION OF A GAS TURBINE ENGINE |
| 摘要 |
A fuel injection system for a gas turbine engine includes a fuel nozzle with a fuel injection aperture to inject a fuel jet and a multiple of airflow passages in the fuel nozzle to communicate a multiple of air streams to interact with the fuel jet. |
| 申请公布号 |
US2014338357(A1) |
申请公布日期 |
2014.11.20 |
| 申请号 |
US201313936876 |
申请日期 |
2013.07.08 |
| 申请人 |
United Technologies Corporation |
发明人 |
Lovett Jeffery A.;Bellows Benjamin D. |
| 分类号 |
F02C7/22 |
主分类号 |
F02C7/22 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A fuel injection system for a gas turbine engine comprising:
a fuel nozzle with a fuel injection aperture to inject a fuel jet; and a multiple of airflow passages in said fuel nozzle to communicate a multiple of air streams to interact with said fuel jet. |
| 地址 |
Hartford CT US |
