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| Naji, M. |
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| Motta, Antonella |
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| Aletan, Dirar |
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| Mohamed, Tarek |
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| Ertürk, Emre |
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| Taccardi, Nicola |
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| Kononenko, Denys |
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| Petrov, R. H. | Madrid |
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| Alshaaer, Mazen | Brussels |
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| Bih, L. |
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| Casati, R. |
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| Muller, Hermance |
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| Kočí, Jan | Prague |
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| Šuljagić, Marija |
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| Kalteremidou, Kalliopi-Artemi | Brussels |
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| Azam, Siraj |
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| Ospanova, Alyiya |
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| Blanpain, Bart |
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| Ali, M. A. |
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| Popa, V. |
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| Rančić, M. |
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| Ollier, Nadège |
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| Azevedo, Nuno Monteiro |
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| Landes, Michael |
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| Rignanese, Gian-Marco |
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Guida, Michele
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (8/8 displayed)
- 2024Validation of Experimental Data for the Application of the Magnesium Alloy “Elektron 43”
- 2023SOLIFLY D4.1 - Airworthiness assessment for structural batteries
- 2022VALIDITY AND APPLICABILITY OF THE SCALING EFFECTS FOR LOW VELOCITY IMPACT ON COMPOSITE PLATES
- 2021CleanSky2 SOLIFLY - Developing structural batteries towards aeronautic application
- 2020DYNAMIC BUCKLING INVESTIGATION OF AIRCRAFT COMPOSITE STANCHIONS SUBJECTED TO CYCLIC LOADING CONDITIONS
- 2020Characterization of Adhesives Bonding in Aircraft Structurescitations
- 2020Dynamic Pulse Buckling of Composite Stanchions in the Sub-Cargo Floor Area of a Civil Regional Aircraftcitations
- 2019Analysis of the impact dynamics of shape memory alloy hybrid composites for advanced applicationscitations
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document
SOLIFLY D4.1 - Airworthiness assessment for structural batteries
Abstract
Electrification of aircraft systems is key for increasing efficiency and reducing climate impact of air transport towards the European net-zero goal. The functional integration of structural capabilities and electrical energy storage in the form of structural batteries (SB) is considered as a low TRL technology with the potential to reduce the impact of battery energy storage on the overall aircraft weight. So far, structural batteries have been mainly studied at material level, largely neglecting their integration into aircraft structures.The CleanSky2 THT project SOLIFLY is developing further structural batteries for aeronautical applications with two cell concepts, one with coated carbon fibres acting as structural and electrically conductive components, and another with laminate structural electrodes. The project puts particular emphasis on their integration into CFRP laminates that are compatible with aeronautical manufacturing processes.This report fixes some general considerations about certification requirements on composite material structures and the current trend of certification agencies to move towards a performance-based regulations. This document may represent a reference for structural composite batteries, for which there are still no well-defined certification requirements. Assuming this approach is valid, an airworthy solution for certification of composite structures with embedded structural batteries is given, providing an innovative interpretation of existing regulations, in compliance with current trends.