An assembly for a gas turbine engine includes an intermediate case and a gearbox. The intermediate case defines an annular transition duct. The gearbox comprises a plurality of lobes and is integrally formed with the annular transition duct.
申请公布号
US2012159966(A1)
申请公布日期
2012.06.28
申请号
US201213414118
申请日期
2012.03.07
申请人
SUCIU GABRIEL L.;MERRY BRIAN D.;DYE CHRISTOPHER M.;UNITED TECHNOLOGIES CORPORATION
发明人
SUCIU GABRIEL L.;MERRY BRIAN D.;DYE CHRISTOPHER M.
