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. 24, 2019

Filed:

Aug. 16, 2016
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Max U. Kismarton, Renton, WA (US);

Clayton L. Munk, Maple Valley, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 3/20 (2006.01); B29C 70/30 (2006.01); B64C 3/18 (2006.01); B64C 3/26 (2006.01); B29L 31/30 (2006.01);
U.S. Cl.
CPC ...
B64C 3/20 (2013.01); B29C 70/30 (2013.01); B64C 3/182 (2013.01); B64C 3/185 (2013.01); B64C 3/26 (2013.01); B29L 2031/3076 (2013.01);
Abstract

Systems and methods are provided for structurally supporting an aircraft wing. The system comprises a section of aircraft wing that includes skin. The skin surrounds an internal volume of the wing and comprises layers of Carbon Fiber Reinforced Polymer (CFRP) having fiber orientations aligned to bear shear stresses applied to the wing. The section of aircraft wing also includes planked stringers that are laterally oriented within the wing, contact the skin within the internal volume, are attached to the skin, and comprise layers of CFRP having fiber orientations that are aligned to bear bending at the wing. Furthermore, the section includes spars that are positioned between planked stringers on an upper portion of the wing and planked stringers on a lower portion of the wing, wherein the spars are aligned with the planked stringers.


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