| 发明名称 |
FAN CONTAINMENT CASE WITH THERMALLY CONFORMING LINER |
| 摘要 |
A fan section of a gas turbine engine includes a fan containment case assembly includes an outer case of an aluminum alloy. The outer case extends circumferentially around an axial centerline. A thermally conforming liner assembly is located inwardly of the outer case. The thermally conforming liner assembly includes a circumferential liner of an aluminum alloy. A ballistic liner is located between the outer case and the thermally conforming liner assembly. |
| 申请公布号 |
US2014286748(A1) |
申请公布日期 |
2014.09.25 |
| 申请号 |
US201213714821 |
申请日期 |
2012.12.14 |
| 申请人 |
United Technologies Corporation |
发明人 |
Costa Mark W.;Robertson, JR. Thomas J.;Lussier Darin S. |
| 分类号 |
F01D21/04 |
主分类号 |
F01D21/04 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A fan section of a gas turbine engine comprising:
a fan containment case assembly including: an outer case of an aluminum alloy, wherein the outer case extends circumferentially around an axial centerline; a thermally conforming liner assembly located inwardly of the outer case, wherein the thermally conforming liner assembly includes a circumferential liner of an aluminum alloy; and a ballistic liner located between the outer case and the thermally conforming liner assembly. |
| 地址 |
US |
