01.1 - Aircraft Design and Integrated System (Basics and Theory)
FUEL-BASED THERMAL MANAGEMENT SYSTEM ARCHITECTURES AND TANK TEMPERATURE EVOLUTION MODELS FOR AVIATION
S. Favre¹, F. Di Fede, Leonardo Labs, Leonardo S.p.A., Italy; E. Brusa¹, C. Delprete¹; ¹Politecnico di Torino, Italy
Development of a dynamic, system level, model for the evaluation of thermal endurance associated with fuel-based Thermal Management Systems (F-TMS) in the aerospace sector. A hybrid-electric regional transport aircraft is taken as a reference, while TMS performance is investigated over multiple parameters, architectures, and degrees of hybridization.