| 发明名称 |
FUEL SYSTEM FOR TONE CONTROL AND OPERABILITY |
| 摘要 |
Aspects of the disclosure are directed to controlling a distribution of fuel to a plurality of nozzles associated with at least one aircraft engine by: determining a state of operation associated with the at least one aircraft engine, causing a valve coupled to a fuel supply and each of the nozzles to open when it is determined that the state of operation indicates a high power state relative to at least one threshold, and causing the valve to close when it is determined that the state of operation indicates a low power state relative to the at least one threshold. |
| 申请公布号 |
US2016195024(A1) |
申请公布日期 |
2016.07.07 |
| 申请号 |
US201514884487 |
申请日期 |
2015.10.15 |
| 申请人 |
United Technologies Corporation |
发明人 |
Hoke James B.;Van Anthony |
| 分类号 |
F02C9/26 |
主分类号 |
F02C9/26 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method for controlling a distribution of fuel to a plurality of nozzles associated with at least one aircraft engine, the method comprising:
determining a state of operation associated with the at least one aircraft engine; causing a valve coupled to a fuel supply and each of the nozzles to open when it is determined that the state of operation indicates a high power state relative to at least one threshold; and causing the valve to close when it is determined that the state of operation indicates a low power state relative to the at least one threshold. |
| 地址 |
Hartford CT US |
