An accessory system for a gas turbine engine includes a main case which defines an accessory gearbox axis. A cover is removably mountable to the main case and a first gear set at least partially within the cover along a first accessory axis transverse to the accessory gearbox axis.
申请公布号
US2012117982(A1)
申请公布日期
2012.05.17
申请号
US201113103152
申请日期
2011.05.09
申请人
SUCIU GABRIEL L.;DYE CHRISTOPHER M.;DUONG HUNG;SNAPE NATHAN
发明人
SUCIU GABRIEL L.;DYE CHRISTOPHER M.;DUONG HUNG;SNAPE NATHAN