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US 7,578,465 B2Granted
Aircraft front nose landing gear and method of making an aircraft landing gear
AssigneeLord Corporation
InventorsPaul J. Bachmeyer, Doug A. Hodgson
Life of this patent
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AssigneeLord Corporation
InventorsPaul J. Bachmeyer, Doug A. Hodgson
Estimating the term…
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.
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.
Dependencies are inferred from the claim text.