IDiyas

For the Inventor, By the Inventor

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 11969983 B1

PDFFull Text
Date of Patent:
Apr. 30, 2024

Filed:

Oct. 06, 2021

Structural component

Applicant:

Airbus Defence and Space Gmbh, Taufkirchen, DE;

Inventors:

Christian Karch, Taufkirchen, DE;

Blanka Lenczowski, Taufkirchen, DE;

Johannes Wolfrum, Taufkirchen, DE;

Yehoshua Yeshurun, Taufkirchen, DE;

Assignee:

Airbus Defence and Space GmbH, Taufkirchen, DE;

Attorney:

KDW Firm PLLC

Primary Examiner:

Peter Y Choi

Int. Cl.
CPC ...
B32B 5/02 (2006.01); B29C 70/02 (2006.01); B29C 70/88 (2006.01); B32B 5/26 (2006.01); B32B 7/04 (2019.01); B32B 15/08 (2006.01); B32B 15/14 (2006.01); B32B 15/18 (2006.01); B32B 15/20 (2006.01); B32B 27/12 (2006.01); B32B 27/30 (2006.01); B32B 37/14 (2006.01); B64D 45/02 (2006.01); B82Y 30/00 (2011.01); C08J 5/00 (2006.01); C08J 5/24 (2006.01);
U.S. Cl.
CPC ...
B32B 5/022 (2013.01); B29C 70/021 (2013.01); B29C 70/885 (2013.01); B32B 5/26 (2013.01); B32B 7/04 (2013.01); B32B 15/08 (2013.01); B32B 15/14 (2013.01); B32B 15/18 (2013.01); B32B 15/20 (2013.01); B32B 27/12 (2013.01); B32B 27/308 (2013.01); B32B 37/14 (2013.01); B64D 45/02 (2013.01); B82Y 30/00 (2013.01); C08J 5/005 (2013.01); C08J 5/243 (2021.05); B32B 2250/40 (2013.01); B32B 2255/02 (2013.01); B32B 2260/021 (2013.01); B32B 2260/046 (2013.01); B32B 2262/106 (2013.01); B32B 2307/202 (2013.01); B32B 2307/204 (2013.01); B32B 2307/212 (2013.01); B32B 2307/308 (2013.01); B32B 2307/50 (2013.01); B32B 2307/546 (2013.01); B32B 2307/732 (2013.01); B32B 2571/00 (2013.01); B32B 2605/18 (2013.01); C08K 2201/001 (2013.01);
Abstract

A structural component for an aircraft, spacecraft or rocket has a ply of fiber reinforced polymer, a first carbon nanotube mat; and a metallic layer, wherein the carbon nanotube mat and the metallic layer are arranged on the ply of fiber reinforced polymer to form a hybrid lightning strike protection layer. A component for manufacturing such a structural component, a method for manufacturing a component of this type, a method for manufacturing a structural component and an aircraft or spacecraft with such a structural component are described.

Find Patent Forward Citations

Loading…