| 发明名称 |
GAS TURBINE ENGINE NOISE REDUCING NOSE CONE |
| 摘要 |
A fan section for a gas turbine engine includes a fan hub and a nose cone section operatively mounted to the fan hub. The nose cone section includes a noise attenuation feature. |
| 申请公布号 |
US2016032832(A1) |
申请公布日期 |
2016.02.04 |
| 申请号 |
US201414766825 |
申请日期 |
2014.02.13 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Gilson Jonathan;Sawyers-Abbott Nigel David |
| 分类号 |
F02C7/045;F01D25/24;F01D5/02 |
主分类号 |
F02C7/045 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A fan section for a gas turbine engine comprising;
a fan hub; and a nose cone section operatively mounted to the fan hub, the nose cone section including a noise attenuation feature. |
| 地址 |
Hartford, CT US |
