| 发明名称 |
GAS TURBINE ENGINE DRIVEN BY SUPERCRITICAL POWER GENERATION SYSTEM |
| 摘要 |
A gas turbine engine includes a shaft having a first air compressor coupled thereto, a combustor positioned to receive compressed air from the first compressor, and a power source coupled to the shaft, the power source powered by a working fluid other than the compressed air. |
| 申请公布号 |
US2015354450(A1) |
申请公布日期 |
2015.12.10 |
| 申请号 |
US201514729318 |
申请日期 |
2015.06.03 |
| 申请人 |
Rolls-Royce Corporation |
发明人 |
Vaisman Igor;Bastnagel Thomas E. |
| 分类号 |
F02C3/13;F02C7/143;F02C3/04 |
主分类号 |
F02C3/13 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A gas turbine engine, comprising:
a shaft having a first air compressor coupled thereto; a combustor positioned to receive compressed air from the first compressor; and a power source coupled to the shaft, the power source powered by a working fluid other than the compressed air. |
| 地址 |
Indianapolis IN US |
