| 发明名称 |
BLADE OUTER AIR SEAL SUPPORT STRUCTURE |
| 摘要 |
A support structure for a gas turbine engine includes an axially extending portion that forms a loop. A radially extending portion extends radially inward from the axially extending portion. A plurality of retention members are attached to at least one of the axially extending portion and the radially extending portion for retaining a blade outer air seal. |
| 申请公布号 |
US2016146053(A1) |
申请公布日期 |
2016.05.26 |
| 申请号 |
US201514931929 |
申请日期 |
2015.11.04 |
| 申请人 |
United Technologies Corporation |
发明人 |
McCaffrey Michael G. |
| 分类号 |
F01D25/28;F01D25/24;F01D11/08 |
主分类号 |
F01D25/28 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A support structure for a gas turbine engine comprising:
an axially extending portion forming a loop; a radially extending portion extending radially inward from the axially extending portion; and a plurality of retention members attached to at least one of the axially extending portion and the radially extending portion for retaining a blade outer air seal. |
| 地址 |
Hartford CT US |
