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. 15, 2020

Filed:

Mar. 27, 2018
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Akif O. Bolukbasi, Mesa, AZ (US);

Timothy R. Gleason, Mesa, AZ (US);

Peter Holemans, Sewell, NJ (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 37/32 (2006.01); B32B 1/02 (2006.01); B32B 3/28 (2006.01); B32B 5/14 (2006.01); B32B 5/18 (2006.01); B32B 15/20 (2006.01); B32B 27/32 (2006.01); B32B 7/022 (2019.01); B64C 1/00 (2006.01); B32B 3/30 (2006.01); B32B 5/26 (2006.01); B60K 15/03 (2006.01); B32B 3/18 (2006.01); B32B 5/24 (2006.01); B32B 15/04 (2006.01); B32B 27/06 (2006.01); B64D 37/02 (2006.01); B60K 15/063 (2006.01);
U.S. Cl.
CPC ...
B64D 37/32 (2013.01); B32B 1/02 (2013.01); B32B 3/18 (2013.01); B32B 3/28 (2013.01); B32B 3/30 (2013.01); B32B 5/145 (2013.01); B32B 5/18 (2013.01); B32B 5/245 (2013.01); B32B 5/26 (2013.01); B32B 7/022 (2019.01); B32B 15/046 (2013.01); B32B 15/20 (2013.01); B32B 27/065 (2013.01); B32B 27/32 (2013.01); B60K 15/03 (2013.01); B60K 15/03177 (2013.01); B64C 1/00 (2013.01); B64D 37/02 (2013.01); B32B 2250/40 (2013.01); B32B 2260/023 (2013.01); B32B 2260/046 (2013.01); B32B 2262/106 (2013.01); B32B 2266/06 (2013.01); B32B 2266/08 (2013.01); B32B 2305/022 (2013.01); B32B 2307/558 (2013.01); B32B 2307/56 (2013.01); B32B 2439/40 (2013.01); B32B 2605/18 (2013.01); B60K 2015/03407 (2013.01); B60K 2015/0631 (2013.01); B60Y 2200/50 (2013.01); B60Y 2306/01 (2013.01); B64D 2037/325 (2013.01);
Abstract

Typical composite panels are brittle and unable to support transverse pressure loads that might be imposed on the panels. For example, the use of typical panels around fuel tanks of a vehicle are unable to support transverse pressure loads that might be imposed on the fuel tanks during a crash of the vehicle or a ballistic impact to the fuel tanks. In the embodiments described herein, panels include face sheets that are bonded to a foam core. The foam core includes a corrugated core sheet that is formed from a highly ductile material, such as Polyethylene or Aluminum. When a transverse pressure load is imposed on the panel, core crush of the foam occurs as the core sheet elongates from its original corrugated shape to a curve shape during deformation. This allows the panel to dissipate the energy of the transverse pressure load applied to the panel.


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