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:
Sep. 29, 2015

Filed:

Nov. 26, 2012
Applicant:

The Boeing Company, Chicago, IL (US);

Inventor:

John H. Moselage, III, Renton, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 1/26 (2006.01); B64C 3/18 (2006.01); B64C 1/06 (2006.01); B64C 3/20 (2006.01); B64C 1/00 (2006.01);
U.S. Cl.
CPC ...
B64C 1/26 (2013.01); B64C 1/061 (2013.01); B64C 1/065 (2013.01); B64C 1/068 (2013.01); B64C 3/182 (2013.01); B64C 3/185 (2013.01); B64C 3/20 (2013.01); B64C 2001/0072 (2013.01); Y02T 50/433 (2013.01); Y10T 29/49622 (2015.01);
Abstract

Apparatus and methods provide for the reinforcement of various components of an aircraft utilizing vertically-oriented circumferential stringers. According to embodiments described herein, barrel skin of an aircraft fuselage may be reinforced using stringers that are vertically-oriented and circumferential. According to additional embodiments, the wing stringers of a wing can be aligned with circumferential stringers. According to further embodiments, the wing may also have one or more wing spars having an elliptical aperture. The shape of the elliptical may be configured for attachment to a fuselage so that an outer surface of the aperture is disposed proximate to an inner surface of the fuselage.


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