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:
May. 16, 2023

Filed:

Dec. 16, 2019
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Danilo Vukosav, Kirkland, WA (US);

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

Daniel J. Cox, Seattle, WA (US);

Jeff S. Hollowell, Everett, WA (US);

Steven D. Ingham, Everett, WA (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 1/10 (2006.01); B64C 1/06 (2006.01); B64C 1/18 (2006.01);
U.S. Cl.
CPC ...
B64C 1/10 (2013.01); B64C 1/064 (2013.01); B64C 1/068 (2013.01); B64C 1/069 (2013.01); B64C 1/18 (2013.01);
Abstract

A fuselage for an aircraft includes a pressure deck assembly extending along a roll axis of the fuselage. The pressure deck assembly includes longitudinal beams and a pressure deck. The longitudinal beams extend lengths along the roll axis of the fuselage. The pressure deck extends between the longitudinal beams along the lengths of the longitudinal beams. The pressure deck is compliant along a pitch axis of the fuselage. The fuselage includes a bulkhead extending along a yaw axis of the fuselage. The bulkhead is joined to the pressure deck assembly at a corner joint. The fuselage includes a compression chord extending a length along the pitch axis of the fuselage. The compression chord is joined between the pressure deck assembly and the bulkhead at the corner joint such that the compression chord extends on an outside of the corner joint.


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