Actuation system for a lift assisting device and lined track rollers used therein

• US 10,023,302 B2
• Filed: 12/19/2012
• Issued: 07/17/2018
• Est. Priority Date: 12/06/2007
• Status: Active Grant

• Current Assignee: Roller Bearing Company of America Incorporated (RBC Bearings Incorporated)
• Original Assignee: Roller Bearing Company of America Incorporated (RBC Bearings Incorporated)
• Inventors: Gyuricsko, Frederick S., Phoenix, Jay, Fredericksen, Arnold E., Cowles, Jr., John H.
• Primary Examiner(s): Collins, Timothy D
• Assistant Examiner(s): Dixon, Keith L
• Application Number:
  US13/719,541
• Publication Number:
  US 20140061381A1
• Time in Patent Office: 2,036 Days
• Field of Search: 244214, 244215, 244213, 244218
• CPC Class Codes: B64C 9/02 Mounting or supporting thereof
• CPC Class Codes: B64C 9/22 at the front of the wing
• CPC Class Codes: F16C 11/02 Trunnions; Crank-pins fastening crank-pins to webs, crank-pins integral with cranks F16C3/06, F16C3/22
• CPC Class Codes: F16C 13/006 Guiding rollers, wheels or the like, formed by or on the outer element of a single bearing or bearing unit, e.g. two adjacent bearings, whose ratio of length to diameter is generally less than one
• CPC Class Codes: F16C 23/041 with edge relief
• CPC Class Codes: F16C 2326/43 Aeroplanes; Helicopters in general B64C
• CPC Class Codes: F16C 29/045 having rolling elements journaled in one of the moving parts
• CPC Class Codes: Y02T 50/40 Weight reduction

Abstract

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.

Claims

1. An actuation system for deploying and retracting a lift assisting device of a leading edge 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; and

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,

wherein each of the track roller bearings comprises an inner ring having an outer bearing surface and an outer ring having an inner bearing surface, the inner ring being disposed at least partially in the outer ring and at least one of the track roller bearings has a self lubricating liner secured to at least one of the outer bearing surface and the inner bearing surface, to carry loads transmitted to the track roller bearing from the track.

2. The actuation system of claim 1, wherein at least one of the plurality of track roller bearings is in rotational contact with an upper surface of the track and at least one of the track roller bearings is in rotational contact with a lower surface of the track.

3. The actuation system of claim 1, wherein the all of the plurality of track roller bearings have one of the self lubricating liners secured to at least one of the outer bearing surface and the inner bearing surface.

4. The actuation system of claim 1, wherein the means for actuating is comprised of:

an actuator arm coupled to the track; and

an actuator lever coupled to the shaft and to the actuator arm;

wherein when the shaft rotates in a first direction the actuator lever drives the actuator arm to move the track and the lift assisting device from the retracted to the deployed position along the arcuate path, and when the shaft rotates in a second direction the actuator lever drives the actuator arm to move the track and the lift assisting device from the deployed position to the retracted position along the arcuate path.

5. The actuation system of claim 1, wherein the actuation system further includes a mounting web enclosing at least a portion of the track and wherein the plurality of track roller bearings are coupled to the mounting web.

6. The actuation system of claim 5, wherein the track roller bearings are coupled to the mounting web with opposing bushings, a mounting pin and a nut.

7. The actuation system of claim 6, wherein the opposing bushings are comprised of eccentric bushings and the nut is comprised of a castellated nut to allow adjustment to the track at fit-up.

8. The actuation system of claim 1 further comprising a plurality of side roller bearings rotatably contacting at least one side of the track to guide the track along the arcuate path.

9. The actuation system of claim 8 wherein each of the plurality of the side roller bearings comprise an inner ring having an outer bearing surface and an outer ring having an inner bearing surface, the inner ring being disposed at least partially in the outer ring at least one of the side roller bearings has one of the self lubricating liners secured to at least one of the outer bearing surface and the inner bearing surface.

10. The actuation system of claim 1, wherein the at least one track roller bearing having the self lubricating liner has no balls, no needles and no cage.

11. The actuation system of claim 1, wherein the securing of the liner comprises at least one of by bonding and by an adhesive.