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:
Jul. 24, 2018

Filed:

Jul. 13, 2016
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Richard R. Rosman, Seattle, WA (US);

Bernhard Dopker, Bellevue, WA (US);

Wallace Chi-Hua Chan, Bothell, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 1/12 (2006.01); B29C 65/56 (2006.01); B29C 65/00 (2006.01); B64C 1/00 (2006.01); B29L 31/30 (2006.01); B29K 105/08 (2006.01); B29K 307/04 (2006.01);
U.S. Cl.
CPC ...
B64C 1/12 (2013.01); B29C 65/562 (2013.01); B29C 66/532 (2013.01); B29C 66/721 (2013.01); B29C 66/1122 (2013.01); B29C 66/21 (2013.01); B29C 66/7392 (2013.01); B29C 66/7394 (2013.01); B29K 2105/08 (2013.01); B29K 2307/04 (2013.01); B29L 2031/3082 (2013.01); B64C 2001/0072 (2013.01); Y02T 50/433 (2013.01); Y10T 29/49696 (2015.01); Y10T 403/70 (2015.01); Y10T 403/7075 (2015.01);
Abstract

A method of forming a direct bearing joint includes coupling a first load-bearing structure to a second load-bearing structure. The second load-bearing structure includes a first structural feature comprising a first arcuate shape. The method also includes coupling a composite skin including a second structural feature comprising a second arcuate shape to the second load-bearing structure. The composite skin is coupled to the second load-bearing structure such that the first and second structural features are mated against each other to facilitate distributing compressive loads from the second load-bearing structure into the composite skin.


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