| 发明名称 |
CARBURETED FUEL INJECTION SYSTEM FOR A GAS TURBINE ENGINE |
| 摘要 |
A fuel injection system for a gas turbine engine includes a vane in an airflow path within the gas turbine engine, the vane includes an air channel with an outlet in communication with the airflow path; and a fuel nozzle within the vane operable to inject fuel into the air channel to at least partial premix and prevaporize the fuel with a secondary airflow from within the vane in the air channel prior to entry into the airflow path through the outlet. A method of injecting fuel within a gas turbine engine includes at least partially premixing and prevaporizing fuel with a secondary airflow from within a vane in an air channel within the vane, the vane within an airflow path of the gas turbine engine. |
| 申请公布号 |
US2015285148(A1) |
申请公布日期 |
2015.10.08 |
| 申请号 |
US201314083040 |
申请日期 |
2013.11.18 |
| 申请人 |
United Technologies Corporation |
发明人 |
Lovett Jeffery A.;Kraus Darin A.;Phillips Scott D.;Micka Daniel J.;Magari Patrick |
| 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 vane in an airflow path within the gas turbine engine, said vane includes an air channel with an outlet in communication with the airflow path; and a fuel nozzle within said vane operable to inject fuel into said air channel to at least partial premix and prevaporize the fuel with a secondary airflow from within said vane in said air channel prior to entry into the airflow path through the outlet. |
| 地址 |
Hartford CT US |
