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:
Apr. 14, 2025

Filed:

Oct. 05, 2022
Applicant:

Airbus Defence and Space Gmbh, Taufkirchen, DE;

Inventors:

Christian Karch, Taufkirchen, DE;

Kay Dittrich, Taufkirchen, DE;

Matthias Bleckmann, Taufkirchen, DE;

Thomas Schuster, Taufkirchen, DE;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 45/02 (2005.12); B32B 1/00 (2005.12); B32B 3/08 (2005.12); B32B 5/02 (2005.12); B32B 15/14 (2005.12); H02G 13/00 (2005.12); B32B 15/20 (2005.12);
U.S. Cl.
CPC ...
B64D 45/02 (2012.12); B32B 1/00 (2012.12); B32B 3/08 (2012.12); B32B 5/02 (2012.12); B32B 15/14 (2012.12); H02G 13/80 (2012.12); B32B 15/20 (2012.12); B32B 2255/06 (2012.12); B32B 2255/205 (2012.12); B32B 2260/021 (2012.12); B32B 2260/046 (2012.12); B32B 2262/101 (2012.12); B32B 2262/106 (2012.12); B32B 2307/202 (2012.12); B32B 2307/212 (2012.12); B32B 2307/712 (2012.12); B32B 2605/18 (2012.12);
Abstract

A structural part for lightning strike protection, preferably of an aircraft includes a first structure element, wherein the first structure element includes a conducting material and is adapted to conduct electric currents into a grounded conducting airframe structure, and a second structure element, wherein the second structure element includes an outer layer with a first surface, wherein the outer layer includes a composite, preferably carbon-fibre reinforced plastic, CFRP or glass-fibre reinforced plastic GFRP. The structural part further includes a first elongated, preferably wedge-shaped, electrical conductor, with a first end and a second end, wherein the first end of the first elongated electrical conductor is connected to the first structure element and extends through the second structure element to the first surface, so that the second end of the first elongated electrical conductor serves as a lightning receptor without impairing the radar cross section of the aircraft.


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