STRUCTURAL FIBRE-REINFORCED COMPONENT WITH LIGHTNING STRIKE PROTECTION BY USING CARBON NANO TUBE MATS AND METALLIC LAYERS

The present invention pertains to a structural component (1), in particular for an aircraft, spacecraft or rocket (10), comprising: a ply (2) of fiber reinforced polymer; a first carbon nano tube mat (3); and a metallic layer (4), wherein the carbon nano tube mat (3) and the metallic layer (4) are a...

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Bibliographische Detailangaben
Hauptverfasser:	Karch, Christian, Wolfrum, Johannes, Lenczowski, Blanka, Yeshurun, Yehoshua
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F,C08G AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CHEMISTRY COMPOSITIONS BASED THEREON COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERAL PROCESSES OF COMPOUNDING MANUFACTURE OR TREATMENT OF NANOSTRUCTURES MEASUREMENT OR ANALYSIS OF NANOSTRUCTURES METALLURGY NANOTECHNOLOGY ORGANIC MACROMOLECULAR COMPOUNDS PARACHUTES PERFORMING OPERATIONS SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS SPECIFIC USES OR APPLICATIONS OF NANOSTRUCTURES THEIR PREPARATION OR CHEMICAL WORKING-UP TRANSPORTING WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL WORKING-UP
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Beschreibung
Zusammenfassung:	The present invention pertains to a structural component (1), in particular for an aircraft, spacecraft or rocket (10), comprising: a ply (2) of fiber reinforced polymer; a first carbon nano tube mat (3); and a metallic layer (4), wherein the carbon nano tube mat (3) and the metallic layer (4) are arranged on the ply (2) of fiber reinforced polymer to form a hybrid lightning strike protection layer (5). The invention further pertains to 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 comprising such a structural component.