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.:
Date of Patent:
Jul. 14, 2015
Filed:
Mar. 25, 2011
Applicants:
Stefan Tacke, Buxtehude, DE;
Thorsten Roming, Himmelpforten, DE;
Inventors:
Stefan Tacke, Buxtehude, DE;
Thorsten Roming, Himmelpforten, DE;
Assignee:
Airbus Operations GmbH, Hamburg, DE;
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B32B 3/24 (2006.01); B64C 1/06 (2006.01); B32B 1/00 (2006.01); B32B 3/26 (2006.01); B32B 15/08 (2006.01); B64C 1/00 (2006.01);
U.S. Cl.
CPC ...
B64C 1/062 (2013.01); B32B 1/00 (2013.01); B32B 3/266 (2013.01); B32B 15/08 (2013.01); B32B 2262/106 (2013.01); B32B 2307/558 (2013.01); B32B 2307/56 (2013.01); B32B 2307/714 (2013.01); B32B 2605/18 (2013.01); B64C 2001/0072 (2013.01); Y02T 50/433 (2013.01); Y10T 428/24132 (2015.01); Y10T 428/24331 (2015.01);
Abstract
In the case of a fiber composite component for energy absorption in the event of a crash for an aircraft or spacecraft, the fiber composite component is formed as a laminate construction made of CFRP layers and at least one integrated metal foil portion which is corrosion-resistant with respect to the CFRP layers. A fuselage structure portion of an aircraft or spacecraft is formed using at least one fiber composite component of this type. An aircraft or spacecraft comprises a fuselage structure portion of this type.