A case (30) for a gas turbine engine includes a single-piece case (30) that includes a combustor case portion (30a) and a turbine case portion (30b) that is integrally formed with the combustor case portion (30a) as one piece (30). In one example, the single-piece case (30) includes a transition duct/mid-turbine frame case portion (30c) which is integrally formed with the combustor and turbine case portions (30a,30b).
申请公布号
EP2078826(A2)
申请公布日期
2009.07.15
申请号
EP20090250053
申请日期
2009.01.09
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
ALVANOS, IOANNIS;MERRY, BRIAN D.;SUCIU, GABRIEL L.