Patent · US Active

Structural component

US11161320B2 · kind B2 · utility

1Cited by

3References

16Claims

0Family size

Assignee

Airbus Defence and Space GmbH · DE

Inventors

Christian Karch · Schweinhub, DE
Blanka Lenczowski · Schweinhub, DE
Johannes Wolfrum · Himmelkron, DE
Yehoshua Yeshurun · Haifa, IL

Key dates

Filing date	Mar 28, 2017
Grant date	Nov 2, 2021
Priority date	—
Expiry date	Jul 18, 2038

Classification

Technology area (CPC C)Chemistry; Metallurgy
CPC primaryC08K2201/001
WIPO fieldSurface technology, coating
WIPO sectorChemistry

Abstract

A structural component, in particular 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.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.