A structural component for an aircraft including at least one heatable component section having a layer structure including an inner base structure, at least one heating layer having carbon allotropes embedded in a matrix material, at least one first group of consecutive layers including at least one anode layer, at least one first insulating layer, and at least one cathode layer having an electroactive coating. The first group of layers are arranged between the inner base structure and the at least one heating layer, and at least one protective layer is arranged outside the heating layer. The first group of layers constitute a structural battery. The at least one anode layer and the at least one cathode layer are electrically connectable with the heating layer.
Structural component for an aircraft with integrated heating layer and structural battery
2024-04-09
Patent
Electronic Resource
English
IPC: | 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 / H05B ELECTRIC HEATING , Elektrische Heizung |
STRUCTURAL COMPONENT FOR AN AIRCRAFT WITH INTEGRATED HEATING LAYER AND STRUCTURAL BATTERY
European Patent Office | 2021
|Structural component for aircraft and aircraft with structural component
European Patent Office | 2023
|Aircraft structural component and method of manufacturing aircraft structural component
European Patent Office | 2024
|AIRCRAFT OR SPACECRAFT HAVING A STRUCTURAL COMPONENT WITH A BATTERY ARRANGEMENT INTEGRATED THEREIN
European Patent Office | 2020
|