| 发明名称 |
FUEL MANAGEMENT SYSTEM FOR A TURBINE ENGINE |
| 摘要 |
A system is provided for a turbine engine that includes a fuel injector and an actuator. The system includes a fuel management system configured to receive fuel from a flow path. The fuel management system is also configured to provide a first portion of the fuel received from the flow path to the fuel injector at a first temperature, and a second portion of the fuel received from the flow path to the actuator at a second temperature different than the first temperature. |
| 申请公布号 |
US2016201563(A1) |
申请公布日期 |
2016.07.14 |
| 申请号 |
US201414914178 |
申请日期 |
2014.09.10 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Stearns Ethan K.;Crawley, Jr. Clifton J. |
| 分类号 |
F02C7/224;F23R3/28 |
主分类号 |
F02C7/224 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A system for a turbine engine including a fuel injector and an actuator, the system comprising:
a fuel management system configured to receive fuel from a flow path and provide a first portion of the fuel received from the flow path to the fuel injector at a first temperature, and a second portion of the fuel received from the flow path to the actuator at a second temperature different than the first temperature. |
| 地址 |
Hartford CT US |
