Abstract: A ballnut assembly is provided in which a locknut (20), which is normally unloaded becomes loaded in the event of failure of a primary load path. This loading causes relative motion between locking nut (24) and the threads of a shaft (8) such that on clearance there between is eliminated. This causes frictional forces to initiate a lock-up of the locknut.
Type:
Grant
Filed:
August 6, 2002
Date of Patent:
August 16, 2005
Assignee:
Smiths Wolverhampton Limited
Inventors:
Jonathan Davies, Brian Farley, Neil Venables
Abstract: An aircraft flight surface actuator has at least one eccentric cam mechanism, the eccentric cam mechanism imparting movement onto the flight surface.