The use of co-extrusion technology for the production of a new thermal energy storage system with the operationg working temperature in the range 550°C-600°C to be applied in aerospace applications

Stampa multi-materiale per sistemi di accumulo termico

SETTEN, EUGENIA
2023/2024

Abstract

The use of co-extrusion technology for the production of a new thermal energy storage system with the operationg working temperature in the range 550°C-600°C to be applied in aerospace applications
2023
Multi-materials 3D printing for thermal energy storage systems
Thermal energy
3D printing
Core-shell structure
Al2O3 ink
316L ink
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/20.500.12608/77541