SYSTEM FOR COUPLING A AT LEAST ONE RING GEAR OF A GEARBOX WITH A STATIC PART IN AN AIRCRAFT TURBO ENGINE

摘要

A system for coupling at least one ring gear of a gearbox with at least one static part of a geared turbofan engine through a connector device, in particular a ring-like connector device, arranged radially between the at least one ring gear and the at least one static part, with two first torque link devices coupling the ring gear with the connector device, the two first torque link devices being arranged between the ring gear and the connector device, in particular opposite to each other on a first axis; two second torque link devices for coupling the connector device to the at least one static part, the two second torque link devices being arranged between the connector device and the at least one static part, in particular opposite to each other on a second axis.