Compact structure for accessory gearbox of an aircraft turbine engine

    公开(公告)号:US10323576B2

    公开(公告)日:2019-06-18

    申请号:US14903468

    申请日:2014-07-09

    申请人: HISPANO SUIZA

    摘要: An aircraft drive chain including a plurality of main gears engaging with each other, a first main gear including a wall defining an inner space, an outer set of gear teeth being placed on an outer surface of the wall, the outer set of gear teeth engaging with at least one second main gear, a gear system being built into the inner space, the first main gear and the gear system being jointly configured so as to form a gearbox or reducer and ensure mechanical power transfer between a drive member and a slave member, the gear system being mounted onto the wall with a decoupling member.