Patent application number | Description | Published |
20090146014 | Actuation System for a Lift Assisting Device and Roller Bearings Used Therein - 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. | 06-11-2009 |
20110188795 | BEARING FOR FOLLOWER OR CAM - A bearing includes an inner race member having an end surface. An outer race member is disposed about the inner race member. The outer race member has an internal shoulder for engaging the end surface of the inner race member. The inner and outer race members are configured to define a raceway between them and to define a snap ring seat between them. There are cylindrical rollers in the raceway and a snap ring in the snap ring seat. The bearing may be provided as a follower head on a cam follower or may be eccentrically mounted on a drive shaft to serve as a cam. A bearing can be assembled by inserting the inner race member into the outer race member, disposing cylindrical rollers in the raceway and disposing a snap ring in the snap ring seat. | 08-04-2011 |
20110220760 | Actuation System for a Lift Assisting Device and Roller Bearings Used Therein - 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. | 09-15-2011 |
20110220762 | ACTUATION SYSTEM FOR A LIFT ASSISTING DEVICE AND ROLLER BEARINGS USED THEREIN - An aircraft wing includes a wing structure, a slat panel mounted on a track, and an actuator mechanism on the wing structure coupled to the track for moving the slat panel between a deployed position and a retracted position. Track roller bearings on the wing structure rotatably contact the track, and side roller bearings on the wing structure rotatably contact at least one side of the track. In another configuration, the actuator mechanism includes a shaft rotatably mounted on the wing structure, an actuator arm coupled to the track by a bearing linkage, and an actuator lever coupled to the shaft by a bearing linkage and to the actuator arm by a bearing linkage. At least one bearing linkage includes a spherical plain bearing. | 09-15-2011 |
20140061381 | ACTUATION SYSTEM FOR A LIFT ASSISTING DEVICE AND LINED TRACK ROLLERS USED THEREIN - An actuation system for deploying and retracting a lift assisting device of a leading edge of a wing of an aircraft including a track pivotally coupled to the lift assisting device. The track has first and second outer surfaces and side surfaces. The actuation system includes 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. The actuation system includes an actuator for actuating the lift assisting device, coupled to the shaft, between a retracted position to a deployed position along an arcuate path. The actuation system includes 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. The plurality of track roller bearings includes one or more lined track roller assembly. | 03-06-2014 |
20140131512 | SEAL AND ELECTRICAL CONDUCTOR FOR LINED TRACK ROLLERS USED ON ACTUATION SYSTEM FOR AIRCRAFT LIFT ASSISTING DEVICES - An electrical conductor for a bearing defines an annular base and is manufactured from an electrically conductive material. The electrical conductor includes a first electrical connector positioned proximate a radially outer peripheral area of the annular base. The electrical conductor includes a second electrical connector positioned proximate a radially inner peripheral area of the annular base. The second electrical connector defines one or more contact edges extending away from the annular base. The contact edge is configured for sliding electrical contact with the bearing. | 05-15-2014 |
20140339358 | ELECTRICAL CONDUCTOR FOR LINED TRACK ROLLERS USED ON ACTUATION SYSTEM FOR AIRCRAFT LIFT ASSISTING DEVICES - An electrical conductor for a bearing includes an electrically conductive spring ring having a split therein. The spring ring has a plurality of first electrical contact surfaces in electrical communication with a plurality of second electrical contact surfaces. The plurality of second electrical contact surfaces are positioned radially outward from the plurality of first electrical contact surfaces. The plurality of first electrical contact surfaces and the plurality of second electrical contact surfaces are movable relative to one another. | 11-20-2014 |