초록 ▼

An aircraft vehicular front wheel landing gear assembly is provided that includes a nonelastomeric outer upper strut tubular member having an inner axial center bore with a tubular cylindrical frictional interface inner surface segment, and a nonelastomeric inner lower strut member having an outer b

An aircraft vehicular front wheel landing gear assembly is provided that includes a nonelastomeric outer upper strut tubular member having an inner axial center bore with a tubular cylindrical frictional interface inner surface segment, and a nonelastomeric inner lower strut member having an outer bonding surface segment. The nonelastomeric inner member is rotationally received in the outer strut member inner axial center bore with the nonelastomeric inner strut member rotatable within said outer strut member. The assembly includes an elastomeric surface effect damper member encompassing the nonelastomeric inner strut member outer bonding surface segment. The elastomeric surface effect damper member has an inner bonding surface segment and an outer elastomer surface, the inner bonding surface segment is bonded to the nonelastomeric inner strut member outer bonding surface segment. The assembly includes a surface effect lubricant disposed between the elastomeric surface effect damper outer elastomer surface and the nonelastomeric outer strut member frictional interface inner surface segment with the elastomeric surface effect damper outer elastomer surface engaging the nonelastomeric outer strut member frictional interface inner surface segment and inhibiting an oscillating shimmy rotation.

대표청구항 ▼

The invention claimed is: 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 gea

The invention claimed is: 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 landing gear assembly as claimed in claim 1, wherein said elastomeric surface effect damper member outer grooved elastomer surface has an upper end and a distal lower end with an elastomer surface groove traversing said elastomer surface from said upper end to said distal lower end. 4. An aircraft landing gear assembly as claimed in claim 1, wherein said elastomeric surface effect damper member outer grooved elastomer surface has an upper end and a distal lower end with a helical elastomer surface groove traversing said elastomer surface from said upper end to said distal lower end. 5. An aircraft landing gear assembly as claimed in claim 1, wherein said elastomeric surface effect damper member outer grooved elastomer surface includes a helical elastomer surface groove. 6. An aircraft landing gear assembly as claimed in claim 1, wherein said elastomeric surface effect damper member outer grooved elastomer surface includes an elastomer surface groove.