Actuation system for a lift assisting device and roller...

Details Actuation system for a lift assisting device and roller... Actuation system for a lift assisting device and roller...

B - Operations, Transporting

64

C

B64C 13/28 (2006.01) B64C 13/34 (2006.01) F16C 31/04 (2006.01)

Patent

CA 2643029

An actuation system for deploying and retracting a lift assisting device of a wing of an aircraft, is presented. The actuation system includes a track pivotally coupled to the lift assisting device, a shaft rotating in response to flight control signals to deploy or retract the lift assisting device, means for actuating the lift assisting device between a retracted position and a deployed position along an arcuate path, a plurality of track roller bearings and a plurality of side roller bearings. The roller bearings rotatably contact the track to guide the track along the arcuate path. The track roller bearings are comprised of an outer ring, a split inner ring and liners disposed between bearing surfaces of the outer and the inner rings. The split inner ring is configured for accommodating deflection and bending of a mounting pin coupling the track roller bearing in proximity to the track.

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