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. 11, 2021

Filed:

Nov. 08, 2018
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Kim A. Linton, Garden Grove, CA (US);

James P. Dobberfuhl, Clinton, WA (US);

Jaime E. Baraja, San Pedro, CA (US);

Hsi-Yung T. Wu, Cypress, CA (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 3/18 (2006.01); B64F 5/10 (2017.01); B64C 3/26 (2006.01);
U.S. Cl.
CPC ...
B64C 3/185 (2013.01); B64F 5/10 (2017.01); B64C 3/182 (2013.01); B64C 3/187 (2013.01); B64C 3/26 (2013.01);
Abstract

An example aircraft wing includes a first skin, a second skin opposite to the first skin, and a composite spar. The composite spar includes a double-flanged spar cap, a single-flanged spar cap, a spar web connecting the double-flanged spar cap and the single-flanged spar cap, and a tear strap. The double-flanged spar cap includes an inward-facing flange and a first outward-facing flange, and the inward-facing flange and the first outward-facing flange are integrated with the first skin during a co-curing process. The single-flanged spar cap includes a second outward-facing flange that is attached to the second skin. The tear strap is stitched to an inner side of the spar web along at least a portion of a length of the composite spar.


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