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:
Apr. 09, 2024

Filed:

Mar. 03, 2022
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Michael R. Rush, Mukilteo, WA (US);

Orion P. Watson, Kirkland, WA (US);

Daniel H. Fletcher, Lake Forest Park, WA (US);

Ryan A. Fear, Kirkland, WA (US);

Brent E. Beneke, Mukilteo, WA (US);

David H. Leibov, Seattle, WA (US);

Patricia W. Estell, Woodinville, WA (US);

Norma L Alvarez-Quinones, Seattle, WA (US);

Soo H. Teoh, Mill Creek, WA (US);

Jesse R. Wiseman, Snohomish, WA (US);

Mark E. Shadell, Seattle, WA (US);

Mark R. Mclaughlin, Snohomish, WA (US);

Emmett A. Salisbury, Everett, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 1/26 (2006.01); B64C 1/06 (2006.01); B64C 3/18 (2006.01); B64F 5/10 (2017.01);
U.S. Cl.
CPC ...
B64C 1/26 (2013.01); B64F 5/10 (2017.01); B64C 1/064 (2013.01); B64C 3/185 (2013.01);
Abstract

An assembly integrates an aft wing spar root fitting to an aircraft fuselage when joining the aircraft wing to the aircraft body. The assembly provides structural strength to the connection between the aircraft wing and the aircraft body, provides corrosion prevention and provides improved inspection capabilities and repair capabilities to the aircraft wing and aircraft body connection.


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