The present disclosure provides a torque tube comprising a barrel portion disposed between a flange and a back leg, the flange extending radially inward towards an axis of rotation and the back leg extending radially outward from the barrel portion. The torque tube further comprises a channel defined by a channel wall and disposed in at least one of the barrel portion and the flange, the channel being configured to receive a sacrificial member.
TORQUE TUBE DAMPING DEVICES AND ASSEMBLIES
2017-06-22
Patent
Electronic Resource
English
TORQUE TUBE ASSEMBLIES FOR USE WITH AIRCRAFT HIGH LIFT DEVICES
European Patent Office | 2021
|Torque tube assemblies for use with aircraft high lift devices
European Patent Office | 2024
|TORQUE TUBE ASSEMBLIES FOR USE WITH AIRCRAFT HIGH LIFT DEVICES
European Patent Office | 2019
|Torque tube assemblies for use with aircraft high lift devices
European Patent Office | 2018
|