The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Mar. 03, 2015

Filed:

Dec. 13, 2007
Applicants:

Paul Joseph Bachmeyer, Cary, NC (US);

Doug Hodgson, Fuquay-Varina, NC (US);

Darrin M. Jones, Derby, KS (US);

Nicholas V. Anderson, Haysville, KS (US);

Inventors:

Paul Joseph Bachmeyer, Cary, NC (US);

Doug Hodgson, Fuquay-Varina, NC (US);

Darrin M. Jones, Derby, KS (US);

Nicholas V. Anderson, Haysville, KS (US);

Assignee:

Textron Innovations, Inc., Providence, RI (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 25/00 (2006.01); B64C 25/50 (2006.01); F16F 7/02 (2006.01);
U.S. Cl.
CPC ...
B64C 25/505 (2013.01); F16F 7/02 (2013.01); F16F 2224/025 (2013.01);
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.


Find Patent Forward Citations

Bachmeyer, Paul. (2015). Aircraft landing gear assembly shimmy damper (U.S. Patent No. 8967534). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/8967534

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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