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 |
EP2971552(A1) |
申请公布日期 |
2016.01.20 |
申请号 |
EP20140768813 |
申请日期 |
2014.02.21 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
MURDOCK, JAMES, R. |
分类号 |
F01D5/22;F01D5/14;F01D11/00;F02C7/00 |
主分类号 |
F01D5/22 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|