| 发明名称 |
GAS TURBINE ENGINE WITH REINFORCED SPINNER |
| 摘要 |
A spinner for a gas turbine engine comprises an outer shell for defining an airflow path when mounted in a gas turbine engine. An inner surface is provided with a plurality of webs. A gas turbine engine and a fan section for a gas turbine engine are also disclosed. |
| 申请公布号 |
US2015315922(A1) |
申请公布日期 |
2015.11.05 |
| 申请号 |
US201514592942 |
申请日期 |
2015.01.09 |
| 申请人 |
United Technologies Corporation |
发明人 |
Roach James T.;Cook, III Grant O.;Kling Colin J.;O'Brien James F.;Bugaj Shari L. |
| 分类号 |
F01D9/02;F01D5/12;F01D5/02 |
主分类号 |
F01D9/02 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A spinner for a gas turbine engine comprising:
an outer shell for defining an airflow path when mounted in a gas turbine engine; and an inner surface, said inner surface being provided with a plurality of webs. |
| 地址 |
Hartford CT US |
