| 发明名称 |
GAS TURBINE SYSTEM AND METHOD |
| 摘要 |
A fuel supply system is provided having a first fuel gas compressor configured to be driven by a motor and a second fuel gas compressor configured to be driven by a shaft of a gas turbine system. The first fuel gas compressor and the second fuel gas compressor are configured to supply a pressurized fuel flow to a combustor of the gas turbine system, and the first fuel gas compressor and the second fuel gas compressor are coupled to one another in series. |
| 申请公布号 |
US2017082033(A1) |
申请公布日期 |
2017.03.23 |
| 申请号 |
US201414768433 |
申请日期 |
2014.06.10 |
| 申请人 |
WU Wenjie;YU Ping;DIDDI Pradeep Kumar;BIGI Manuele;SNIDER David August;CARDENAS Manuel Moises;GENERAL ELECTRIC COMPANY |
发明人 |
Wu Wenjie;Yu Ping;Diddi Pradeep Kumar;Bigi Manuele;Snider David August;Cardenas Manuel Moises |
| 分类号 |
F02C9/26;F04D29/54;F02C7/36;F01D21/00;F02C3/04;F02C7/22 |
主分类号 |
F02C9/26 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A system, comprising:
a fuel supply system, comprising:
a first fuel gas compressor coupled to a compressor shaft and configured to pressurize a fuel for a gas turbine system;a first clutch configured to selectively engage the compressor shaft with a motor shaft of a motor; anda second clutch configured to selectively engage the compressor shaft with a turbine shaft of the gas turbine system. |
| 地址 |
Shanghai CN |
