| 发明名称 |
ACCUMULATOR ASSISTED GAS TURBINE ENGINE START SYSTEM AND METHODS THEREFOR |
| 摘要 |
A gas turbine engine assembly is provided having a gas turbine engine and a fuel supply in flow communication with the gas turbine engine. An accumulator is positioned in flow communication between the fuel supply and the gas turbine engine to store fuel pressure in fuel flowing from the fuel supply to the gas turbine engine. |
| 申请公布号 |
US2016230667(A1) |
申请公布日期 |
2016.08.11 |
| 申请号 |
US201514616834 |
申请日期 |
2015.02.09 |
| 申请人 |
United Technologies Corporation |
发明人 |
Ripley David Lloyd |
| 分类号 |
F02C7/22;F04C2/10 |
主分类号 |
F02C7/22 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An accumulator assisted gas turbine engine start system for a gas turbine engine including a fuel supply, the system comprising an accumulator positioned in flow communication between a fuel supply and the gas turbine engine to store fuel pressure in fuel flowing from the fuel supply to the gas turbine engine. |
| 地址 |
Farmington CT US |
