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
US2009290976(A1)
申请公布日期
2009.11.26
申请号
US20080154200
申请日期
2008.05.21
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
SUCIU GABRIEL L.;MERRY BRIAN D.;DYE CHRISTOPHER M.
