A mid-turbine frame (12) is connected to at least one mount (16) of a gas turbine engine for transferring a first load from a first bearing (18) and a second load from a second bearing (20) to the mount (16). The mid-turbine frame (12) includes a first load structure (22), a second load structure (26), and a plurality of struts (24). The first load structure (22) combines the first load and the second load into a combined load. The second load structure (26) transfers the combined load to the mount (16). The struts (24) are connected between the first load structure (22) and the second load structure (26) and transfer the combined load from the first load structure (22) to the second load structure (26).
申请公布号
EP1930555(A3)
申请公布日期
2012.08.08
申请号
EP20070254594
申请日期
2007.11.27
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
KUMAR, KESHAVA B.;SOMANATH, NAGENDRA;SOWA, WILLIAM A.