| 发明名称 | Gas turbine engine with fan-tied inducer section | ||
| 摘要 | A gas turbine engine includes a shaft, a speed change device driven by the shaft, and a fan including a fan rotor driven by the speed change device. At least one inducer stage is positioned aft of the fan and is coupled for rotation with the fan rotor. | ||
| 申请公布号 | US9103227(B2) | 申请公布日期 | 2015.08.11 |
| 申请号 | US201213406819 | 申请日期 | 2012.02.28 |
| 申请人 | United Technologies Corporation | 发明人 | Kupratis Daniel Bernard;Schwarz Frederick M. |
| 分类号 | F02C3/10;F01D15/12;F02C7/36;F02K3/072;F02C7/047 | 主分类号 | F02C3/10 |
| 代理机构 | Carlson, Gaskey & Olds, PC | 代理人 | Carlson, Gaskey & Olds, PC |
| 主权项 | 1. A gas turbine engine comprising: a shaft defining an axis of rotation; a speed reduction device driven by the shaft; a fan including a fan rotor driven by the speed reduction device; and at least one inducer stage positioned aft of the fan and coupled for rotation with the fan rotor. | ||
| 地址 | Hartford CT US | ||