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:
Nov. 06, 2018

Filed:

Apr. 04, 2015
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Robert G. Hill, Everett, WA (US);

James R. Schnelz, Seattle, WA (US);

Monte D. Wright, Kenmore, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16C 17/12 (2006.01); B64D 27/26 (2006.01); F16C 35/02 (2006.01); F16C 11/04 (2006.01); F16C 17/02 (2006.01); F16C 7/02 (2006.01);
U.S. Cl.
CPC ...
F16C 17/12 (2013.01); B64D 27/26 (2013.01); F16C 11/045 (2013.01); F16C 17/02 (2013.01); F16C 35/02 (2013.01); B64D 2027/262 (2013.01); F16C 7/02 (2013.01); F16C 2326/43 (2013.01);
Abstract

An offset bushing for a structural member may include a tubular body having a cylindrical inner surface and a cylindrical outer surface. The cylindrical inner surface may have an inner diameter defining an inner axis. The cylindrical outer surface may have an outer diameter defining an outer axis. The inner axis may be spaced apart from the outer axis to define a linear offset. The offset bushing may include a bushing indexing feature configured to align with a member indexing feature of a member when the offset bushing is installed in a member bore. Alignment of the bushing indexing feature with the member indexing feature may cause the linear offset to be oriented substantially parallel to a loading axis of a load on the member.


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