Hybrid Cooling System for Thermal Management in Electric Aerial Vehicles 2024-26-0468

Continuous improvements and innovations towards sustainability in the aviation industry has brought interest in electrified aviation. Electric aircrafts have short missions in which the temporal variability of thermal loads are high. Lithium-ion (Li-ion) batteries have emerged as prominent power source candidate for electric aircrafts and Urban Air Mobility (UAM). UAMs and Electric aircrafts have large battery packs with battery capacity ranging in hundreds or thousands of kWh. If the battery is exposed to temperatures outside the optimum range, the life and the performance of the battery reduces drastically. Hence, it is crucial to have a Thermal Management System (TMS) which would reduce the heat load on battery in addition to cabin, and machinery thermal loads. Thermal management can be done through active or passive cooling. Adding a passive cooling system like Phase Change Material (PCM) to the TMS reduces the design maximum thermal loads. However, the added weight of the PCM module may at times outweigh the benefit of weight reduction. This research shows a study of thermal management of electric aircrafts/UAMs using Vapor Cycle System (VCS), Phase Change Material (PCM) and combination thereof (Hybrid). The TMS of three representative UAM/electric aircrafts of different capacities are simulated, and the results will help us conclude the best method of cooling that can be applied to electric aerial vehicles with varying passenger capacity depending on its heat loads. The analysis of the results quantifies the impact of the architecture on the weight, power, and size metrics and determines the viability limits of each of the three architectures.