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Composite materials with thermo-mechanical functionality for future integrated propulsion systems (C01)

Subject Area Lightweight Construction, Textile Technology
Term since 2023
Project identifier Deutsche Forschungsgemeinschaft (DFG) - Project number 498601949
 
The higher weight of novel energy storage solutions in aircraft call for a higher lightweight potential as well as load-path oriented orthotropic design options. Furthermore, new functionalities such as optimized heat distribution zones are also required. Hence, the project will examine the potential of structure-integrated thermal management by using hybrid laminates with continuous (fiber reinforced polymers doped with graphene materials) and discrete (fiber metal laminates, hybridization) functionalization. The investigations will include experimental and numerical methods that are suitable to design and validate dedicated intra- and interlaminar heat flux paths of these composite materials with realistic boundary conditions e.g. for the known thermal convection in a dedicated test chamber.
DFG Programme CRC/Transregios
Major Instrumentation Thermographic camera system incl. control and data acquisition
Applicant Institution Technische Universität Braunschweig
 
 

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