| 发明名称 |
Injection Molded Composite Fan Platform |
| 摘要 |
A fan platform for a gas turbine engine may include an outer flow path surface extending between a first side and a second side. An inner surface extends between the first side and the second side, and faces radially oppositely the outer flow path surface. A plurality of platform hooks may extend radially inwardly from the inner surface. |
| 申请公布号 |
US2016053636(A1) |
申请公布日期 |
2016.02.25 |
| 申请号 |
US201414506830 |
申请日期 |
2014.02.21 |
| 申请人 |
United Technologies Corporation |
发明人 |
Murdock James R. |
| 分类号 |
F01D25/28;B29C45/00 |
主分类号 |
F01D25/28 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A fan platform for a gas turbine engine, the fan platform comprising:
an outer flow path surface extending between a first side and a second side; an inner surface extending between the first side and the second side, the inner surface facing radially oppositely the outer flow path surface; and a plurality of platform hooks extending radially inwardly from the inner surface. |
| 地址 |
Hartford CT US |
