| 发明名称 |
TURBINE ENGINE WITH A TURBO-COMPRESSOR |
| 摘要 |
A turbine engine is provided that includes a first rotor, a second rotor and a combustor section. The first rotor includes a first set of compressor blades. The second rotor is adjacent the first rotor. The second rotor includes a second set of compressor blades and a set of turbine blades respectively connected to the second set of compressor blades. The combustor section is configured to receive air compressed by the first and the second sets of compressor blades. The combustor section is also configured to provide combustion products to the set of turbine blades. |
| 申请公布号 |
US2016356218(A1) |
申请公布日期 |
2016.12.08 |
| 申请号 |
US201514622383 |
申请日期 |
2015.02.13 |
| 申请人 |
United Technologies Corporation |
发明人 |
Kupratis Daniel B.;Sheridan William G. |
| 分类号 |
F02C6/12;F01D9/04;F02C7/36;F04D29/54;F02C3/04;F01D5/12;F04D29/32 |
主分类号 |
F02C6/12 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A turbine engine, comprising:
a first rotor including a first set of compressor blades; a second rotor adjacent the first rotor, the second rotor including a second set of compressor blades and a set of turbine blades respectively connected to the second set of compressor blades; and a combustor section configured to receive air compressed by the first and the second sets of compressor blades and provide combustion products to the set of turbine blades. |
| 地址 |
Hartford CT US |
