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
EP2932052(A4)
申请公布日期
2016.02.17
申请号
EP20130862300
申请日期
2013.12.10
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
COSTA, MARK W.;ROBERTSON, THOMAS J.;LUSSIER, DARIN S.