| 发明名称 |
GEARED TURBINE ENGINE |
| 摘要 |
A turbine engine is provided that includes a fan rotor, a first compressor rotor, a second compressor rotor, a third compressor rotor, a first turbine rotor, a second turbine rotor, a third turbine rotor and a gear train. The fan rotor and the first compressor rotor are connected to the first turbine rotor through the gear train. The second compressor rotor is connected to the second turbine rotor. The third compressor rotor is connected to the third turbine rotor. |
| 申请公布号 |
US2016245184(A1) |
申请公布日期 |
2016.08.25 |
| 申请号 |
US201514626534 |
申请日期 |
2015.02.19 |
| 申请人 |
United Technologies Corporation |
发明人 |
Schwarz Frederick M.;Sheridan William G. |
| 分类号 |
F02C7/36;F02C3/04 |
主分类号 |
F02C7/36 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A turbine engine, comprising:
a fan rotor, a first compressor rotor, a second compressor rotor, a third compressor rotor, a first turbine rotor, a second turbine rotor, a third turbine rotor and a gear train; wherein the fan rotor and the first compressor rotor are connected to the first turbine rotor through the gear train, wherein the second compressor rotor is connected to the second turbine rotor, and wherein the third compressor rotor is connected to the third turbine rotor. |
| 地址 |
Hartford CT US |
