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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.

Patent No.:

US 10773824 B1

PDFFull Text
Date of Patent:
Sep. 15, 2020

Filed:

Nov. 20, 2017

Structural composite component and method for configuring a structural composite component

Applicant:

Airbus Operations, S.l., Getafe (Madrid), ES;

Inventors:

Tamara Blanco Varela, Madrid, ES;

José Sanchez Gomez, Madrid, ES;

Leire Segura Martinez De Ilarduya, Madrid, ES;

Mariano Morales Monge, Madrid, ES;

Assignee:

Airbus Operations, S.L., , ES;

Attorney:

Lerner, David, Littenberg, Krumholz & Mentlik, LLP

Primary Examiner:

Danny Nguyen

Int. Cl.
CPC ...
B64D 45/02 (2006.01); B29C 70/88 (2006.01); B32B 15/02 (2006.01); H01M 2/02 (2006.01); B32B 7/06 (2019.01); B32B 15/08 (2006.01); B32B 15/14 (2006.01); B32B 15/00 (2006.01); B32B 27/00 (2006.01); B32B 9/04 (2006.01); B32B 7/02 (2019.01); B32B 5/00 (2006.01); B32B 9/00 (2006.01); B32B 3/26 (2006.01); B32B 27/06 (2006.01); B32B 7/04 (2019.01); B32B 27/28 (2006.01); B32B 7/10 (2006.01); B32B 15/04 (2006.01); B32B 5/02 (2006.01); B32B 7/00 (2019.01); B32B 15/20 (2006.01);
U.S. Cl.
CPC ...
B64D 45/02 (2013.01); B29C 70/885 (2013.01); B32B 3/26 (2013.01); B32B 5/00 (2013.01); B32B 5/02 (2013.01); B32B 7/00 (2013.01); B32B 7/02 (2013.01); B32B 7/04 (2013.01); B32B 7/06 (2013.01); B32B 7/10 (2013.01); B32B 9/00 (2013.01); B32B 9/04 (2013.01); B32B 15/00 (2013.01); B32B 15/02 (2013.01); B32B 15/04 (2013.01); B32B 15/08 (2013.01); B32B 15/14 (2013.01); B32B 15/20 (2013.01); B32B 27/00 (2013.01); B32B 27/06 (2013.01); B32B 27/28 (2013.01); H01M 2/0267 (2013.01); H01M 2/0295 (2013.01); B32B 2250/00 (2013.01); B32B 2262/00 (2013.01); B32B 2262/106 (2013.01); B32B 2307/10 (2013.01); B32B 2307/102 (2013.01); B32B 2307/20 (2013.01); B32B 2307/202 (2013.01); B32B 2307/30 (2013.01); B32B 2307/3065 (2013.01); B32B 2307/50 (2013.01); B32B 2307/558 (2013.01); B32B 2307/56 (2013.01); B32B 2307/732 (2013.01); B32B 2457/00 (2013.01); B32B 2457/10 (2013.01); B32B 2571/00 (2013.01); B32B 2605/00 (2013.01); B32B 2605/18 (2013.01);
Abstract

A structural composite component, in particular for an aircraft or spacecraft, includes: a lightning strike protection layer; and a composite battery including a cathode layer and a separation layer, wherein the lightning strike protection layer is formed integrated with the cathode layer, and wherein the separation layer is configured for providing acoustic damping, and/or fire barrier, and/or impact resistance to the structural composite component. A method for configuring such a structural composite component; and an aircraft or spacecraft including such a structural composite component are also described.

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