Actuation system for a lift assisting device and roller bearings used therein
View Patent ↗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.
1. An actuation system for deploying and retracting a lift assisting device of a wing of an aircraft, the actuation system comprising:
a track pivotally coupled to the lift assisting device, the track having first and second outer surfaces and side surfaces;
a shaft rotationally coupled within the wing of the aircraft and operable, in response to flight control signals, to deploy or retract the lift assisting device;
means for actuating the lift assisting device, coupled to the shaft, between a retracted position to a deployed position along an arcuate path;
a plurality of track roller bearings rotatably contacting the first and second outer surfaces of the track to guide the track along the arcuate path; and
a plurality of side roller bearings rotatably contacting at least one side of the track to guide the track along the arcuate path
wherein the plurality of track roller bearings includes at least one lined track roller assembly comprising: an outer ring having inner bearing surfaces; and an inner split ring having a first portion and a second portion, each of the first and second portions having outer bearing surfaces, the inner split ring configured for accommodating deflection and bending of a mounting pin coupling the lined track roller bearing to the track.
2. The actuation system of claim 1 , further comprising:
a plurality of liners disposed between the inner bearing surfaces of the outer ring and the outer bearing surfaces of the inner ring.
3. The actuation system of claim 2 , wherein the liners are comprised of at least one of polytetrafluoroethylene, polyester, graphite, fabric impregnated with a polymer, urethane, polyimide, epoxy, and phenolic.
4. The actuation system of claim 2 , wherein the liners are molded and comprised of at least one of polytetrafluoroethylene, polyester, graphite, fibers in a thermosetting composite resin made from polyester, urethane, polyimide, epoxy, and phenolic.
5. The actuation system of claim 2 , further comprising:
a plurality of shields disposed about shoulder portions of an outer diameter of the outer ring and extending to an outer diameter of the inner ring.
6. The actuation system of claim 1 , wherein the first portion and the second portion of the inner split ring each include a body portion and a head portion, and wherein the head portions each have a flange for limiting axial motion of the outer ring.
7. The actuation system of claim 1 , wherein each of the plurality of track roller bearings are comprised of:
an outer ring having inner bearing surfaces;
an inner split ring having a first portion and a second portion, each of the first and second portions having outer bearing surfaces; and
a plurality of liners disposed between the inner bearing surfaces of the outer ring and the outer bearing surfaces of the inner ring;
wherein the inner rings are comprised of 17-4PH steel and the outer ring is comprised of AISI Type 422 stainless steel with a special nitriding hardening process.