The present invention pertains to a structural composite component, in particular for an aircraft or spacecraft, comprising: a lightning strike protection layer; and a composite battery comprising a cathode layer, wherein the lighting strike protection layer is formed integrated with the cathode layer. The invention further provides a method for configuring such a structural composite component and an aircraft or spacecraft comprising such a structural composite component.
STRUCTURAL COMPOSITE COMPONENT AND METHOD FOR CONFIGURING A STRUCTURAL COMPOSITE COMPONENT
STRUKTURELLES VERBUNDBAUTEIL UND VERFAHREN ZUR KONFIGURATION EINES STRUKTURELLEN VERBUNDBAUTEILS
COMPOSANT STRUCTUREL COMPOSITE ET PROCÉDÉ DE CONFIGURATION D'UN COMPOSANT COMPOSITE STRUCTUREL
06.12.2017
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H01M Verfahren oder Mittel, z.B. Batterien, für die direkte Umwandlung von chemischer in elektrische Energie , PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY |
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