Aircraft landing gear assembly shimmy damper

1. An aircraft landing gear assembly, said landing gear assembly comprised of a nonelastomeric outer aircraft landing gear vertical strut member having an inner axial center bore with a frictional interface inner surface segment, a nonelastomeric inner aircraft landing gear vertical strut member having an outer bonding surface segment, said nonelastomeric inner aircraft landing gear vertical strut member rotationally received in said outer aircraft landing gear vertical strut member inner axial center bore with said nonelastomeric inner aircraft landing gear vertical strut member rotatable within said outer aircraft landing gear vertical strut member, and an elastomeric surface effect damper member encompassing said nonelastomeric inner aircraft landing gear vertical strut member outer bonding surface segment, said elastomeric surface effect damper member having an inner bonding surface segment and an outer grooved elastomer surface, said elastomeric surface effect damper inner bonding surface segment bonded to said nonelastomeric inner aircraft landing gear vertical strut member outer bonding surface segment, and a surface effect lubricant, said surface effect lubricant disposed between said elastomeric surface effect damper outer grooved elastomer surface and said nonelastomeric outer aircraft landing gear vertical strut member frictional interface inner surface segment with said elastomeric surface effect damper outer grooved elastomer surface engaging said nonelastomeric outer aircraft landing gear vertical strut member frictional interface inner surface segment and inhibiting an oscillating shimmy rotation of said nonelastomeric inner aircraft landing gear vertical strut member.

2. An aircraft landing gear assembly as claimed in claim 1 , wherein said nonelastomeric inner aircraft landing gear vertical strut member is grounded to a front nose wheel with said front nose wheel and said nonelastomeric inner aircraft landing gear vertical strut member rotationally actuated by a steering input and said nonelastomeric outer aircraft landing gear vertical strut member rotationally fixed to an aircraft nose front.

3. An aircraft assembly, said assembly comprised of a nonelastomeric outer member having an inner axial center bore with a frictional interface inner surface segment, a nonelastomeric inner member having an outer bonding surface segment, said nonelastomeric inner member rotationally received in said outer member inner axial center bore with said nonelastomeric inner member rotatable within said outer member, and an elastomeric shimmy damper member encompassing said nonelastomeric inner member outer bonding surface segment, said elastomeric shimmy damper member including an elastomer having an inner bonding surface segment and an outer elastomer surface, said elastomeric damper inner bonding surface segment bonded to said nonelastomeric inner member outer bonding surface segment, and a grease, said grease disposed between said elastomeric damper outer elastomer surface and said nonelastomeric outer member frictional interface inner surface segment with said elastomeric surface effect damper outer elastomer surface engaging said nonelastomeric outer member frictional interface inner surface segment and inhibiting an oscillating shimmy rotation of said nonelastomeric inner member.

4. An aircraft assembly as claimed in claim 3 , wherein said outer elastomer surface includes a plurality of grease dams.

5. An aircraft landing gear assembly as claimed in claim 3 , wherein said elastomer surface includes a plurality of elastomer surface grooves which terminate with raised elastomer grease obstructions which radially extend outward and away from the inner bonding surface.

6. An aircraft assembly as claimed in claim 3 , wherein said assembly includes a grease inlet for injecting grease after said nonelastomeric inner member is received in said outer member inner axial center bore.

7. An aircraft assembly as claimed in claim 3 , wherein said assembly includes at least one grease dam for retaining said grease.

8. A method of making an assembly, said method comprising: providing a nonelastomeric outer member having an inner axial center bore with a frictional interface inner surface segment, providing a nonelastomeric inner member rotationally receivable in said outer member inner axial center bore with said nonelastomeric inner member rotatable within said outer member, said nonelastomeric inner member having an outer bonding surface segment, bonding an elastomer having an outer elastomer surface distal from said nonelastomeric inner member outer bonding surface segment, receiving said nonelastomeric inner member in said outer member inner axial center bore with said nonelastomeric inner member rotatable within said outer member with said elastomer surface engaging said nonelastomeric outer member frictional interface inner surface segment and inhibiting a shimmy rotation of said nonelastomeric inner member relative to said nonelastomeric outer member.

9. A method as claimed in claim 8 , said method including molding said elastomer onto said nonelastomeric inner member outer bonding surface segment with said outer elastomer surface.

10. A method as claimed in claim 8 , said method including providing a grease and a plurality of grease dams for controlling the flow of said grease along said outer elastomer surface.

11. A method as claimed in claim 8 , said method including providing a grease inlet and a grease, and injecting said grease between said outer elastomer surface and said frictional interface inner surface segment.

12. A method of making a shimmy damper, said method comprising: providing a nonelastomeric outer tubular member having an inner axial center bore with a tubular cylindrical frictional interface inner surface segment, providing a nonelastomeric inner member rotationally receivable in said outer member inner axial center bore with said nonelastomeric inner member rotatable within said outer member, said nonelastomeric inner member having an outer bonding cylindrical surface segment and an elastomer bonded to said nonelastomeric inner member outer bonding cylindrical surface segment, said elastomer having an outer elastomer surface distal from said nonelastomeric inner member outer bonding cylindrical surface segment, said outer elastomer surface including a plurality of grooves and a plurality of grease dams, receiving said nonelastomeric inner member in said outer member inner axial center bore with said nonelastomeric inner member rotatable within said outer member with said elastomer surface engaging said nonelastomeric outer member frictional interface inner surface segment and inhibiting an oscillating shimmy rotation of said nonelastomeric inner member.

13. A method as claimed in claim 12 , wherein said elastomer is molded to said nonelastomeric inner member with the outer elastomer surface having two mold flats.

14. A method as claimed in claim 12 , said method including providing a grease inlet for injecting grease after said nonelastomeric inner member is received in said outer member inner axial center bore, and wherein said elastomer surface includes a grease receiving groove, with said grease inlet proximate said elastomer surface grease receiving groove.

15. A method as claimed in claim 12 , wherein said outer elastomer surface includes a grease dam.

16. A shimmy damper for damping a rotating oscillation, said shimmy damper comprised of a nonelastomeric outer tubular member having an inner axial center bore with a tubular cylindrical frictional interface inner surface segment, a nonelastomeric inner member having an outer bonding surface segment, said nonelastomeric inner member rotationally received in said outer member inner axial center bore with said nonelastomeric inner member rotatable within said outer member, and an elastomer encompassing said nonelastomeric inner member outer bonding surface segment, said elastomer having an inner bonding surface segment and an outer elastomer surface, said elastomer inner bonding surface segment bonded to said nonelastomeric inner member outer bonding surface segment, and a grease, said grease disposed between said outer elastomer surface and said nonelastomeric outer member frictional interface inner surface segment with said outer elastomer surface engaging said nonelastomeric outer member frictional interface inner surface segment and inhibiting an oscillating shimmy rotation of said nonelastomeric inner member.

17. A method of making a damper, said method comprising: providing a nonelastomeric outer tubular member having an inner axial center bore with a tubular cylindrical frictional interface inner surface segment, providing a nonelastomeric inner member rotationally receivable in said outer member inner axial center bore with said nonelastomeric inner member rotatable within said outer member, said nonelastomeric inner member having an outer bonding cylindrical surface segment, bonding an elastomer damper member to said nonelastomeric inner member outer bonding surface segment with said elastomer damper member having an outer elastomer surface distal from said nonelastomeric inner member outer bonding surface segment, said outer elastomer surface including at least one grease dam, receiving said nonelastomeric inner member in said outer member inner axial center bore with said nonelastomeric inner member rotatable within said outer member with said elastomer damper outer elastomer surface engaging said nonelastomeric outer member frictional interface inner surface segment, providing a grease, disposing said grease between said elastomer damper outer elastomer surface and said nonelastomeric outer member frictional interface inner surface segment.

18. A damper for damping a motion, said damper comprised of a nonelastomeric outer tubular member having an inner axial center bore with a tubular cylindrical frictional interface inner contiguous smooth surface segment, a nonelastomeric inner member having an outer bonding surface segment, said nonelastomeric inner member received in said outer member inner axial center bore with said nonelastomeric inner member within said outer member, and an elastomer encompassing said nonelastomeric inner member outer bonding surface segment, said elastomer having an inner bonding surface segment and an outer elastomer surface, said elastomer inner bonding surface segment bonded to said nonelastomeric inner member outer bonding surface segment and said outer elastomer surface including a plurality of groove segments with grease dams, and a grease, said grease disposed in said groove segments and between said outer elastomer surface and said nonelastomeric outer member frictional interface inner surface segment with said outer elastomer surface engaging said nonelastomeric outer member frictional interface inner surface segment and inhibiting a rotation of said nonelastomeric inner member with said grease dams inhibiting a migration of said grease.

19. A method of making a damper, said method comprising: providing a nonelastomeric outer tubular member having an inner axial center bore, providing a nonelastomeric inner member rotationally receivable in said outer member inner axial center bore with said nonelastomeric inner member rotatable within said outer member, bonding an elastomer damper member to a nonelastomeric member bonding cylindrical surface segment with said elastomer damper member having an elastomer surface distal from said nonelastomeric member bonding surface segment, said elastomer surface including at least one grease dam, receiving said nonelastomeric inner member in said outer member inner axial center bore with said nonelastomeric inner member rotatable within said outer member with said elastomer damper elastomer surface engaging a nonelastomeric member frictional interface surface segment, providing a grease, disposing said grease between said elastomer damper elastomer surface and said nonelastomeric member frictional interface surface segment with said grease dam containing said grease, with said elastomer damper elastomer surface engagement with said nonelastomeric member frictional interface surface segment inhibiting an oscillating rotation of said nonelastomeric inner member relative to said nonelastomeric outer member.

20. A damper for damping a motion, said damper comprised of a nonelastomeric outer tubular member having an inner axial center bore, a nonelastomeric inner member, said nonelastomeric inner member rotationally received in said outer member inner axial center bore with said nonelastomeric inner member rotatable within said outer member, a nonelastomeric member bonding cylindrical surface segment and a nonelastomeric member frictional interface surface segment, and an elastomer encompassing said nonelastomeric inner member, said elastomer having a bonding surface segment and a elastomer surface, said elastomer bonding surface segment bonded to said nonelastomeric member bonding surface segment and said elastomer surface including a plurality of groove segments with grease dams, and a grease, said grease disposed in said groove segments and between said elastomer surface and said nonelastomeric member frictional interface surface segment with said elastomer surface engaging said nonelastomeric member frictional interface surface segment and inhibiting a rotation of said nonelastomeric inner member relative to said outer member with said grease dams inhibiting a migration of said grease.