Invention Grant
- Patent Title: Aircraft landing gear assembly shimmy damper
- Patent Title (中): 飞机起落架组件摆动阻尼器
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Application No.: US11956118Application Date: 2007-12-13
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Publication No.: US08967534B2Publication Date: 2015-03-03
- Inventor: Paul Joseph Bachmeyer , Doug Hodgson , Darrin M. Jones , Nicholas V. Anderson
- Applicant: Paul Joseph Bachmeyer , Doug Hodgson , Darrin M. Jones , Nicholas V. Anderson
- Applicant Address: US RI Providence
- Assignee: Textron Innovations, Inc.
- Current Assignee: Textron Innovations, Inc.
- Current Assignee Address: US RI Providence
- Agency: Lathrop & Gage LLP
- Main IPC: B64C25/00
- IPC: B64C25/00 ; B64C25/50 ; F16F7/02

Abstract:
An aircraft vehicular assembly is provided that includes a nonelastomeric outer tubular member having an inner axial center bore with a tubular cylindrical frictional interface contiguous smooth inner surface segment, and a nonelastomeric inner member having an outer bonding surface segment. The nonelastomeric inner member is rotationally received in the outer member inner axial center bore with the nonelastomeric inner strut member rotatable within said outer member. An elastomer encompasses the nonelastomeric inner strut member outer bonding surface segment. The elastomer has an inner bonding surface segment and an outer grooved elastomer surface, the inner bonding surface segment is bonded to the nonelastomeric inner member outer bonding surface segment.
Public/Granted literature
- US20090152396A1 Aircraft Landing Gear Assembly Shimmy Damper Public/Granted day:2009-06-18
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