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
US8192143(B2)
申请公布日期
2012.06.05
申请号
US20080154200
申请日期
2008.05.21
申请人
SUCIU GABRIEL L;MERRY BRIAN D.;DYE CHRISTOPHER M.;UNITED TECHNOLOGIES CORPORATION