Thermal management for electric aviation: An product development approach
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Examensarbete för masterexamen
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Lithium-ion batteries (LIB’s) are gaining momentum as a suitable and sustainable
solution which can be utilised in many different applications and market. In order
to be used in electric aircraft the batteries have to be lightweight, they also should
also be safe enough to support second-line of defense during an electrical outage. As
the global electric aircraft markets are expected to reach 27.7 billion USD by 2030.
Battery industry is also expected to evolve and grow as the need evolves.
The safety, lifetime and reliability of LIBs are directly dependent on the operating
cell temperature, which makes the thermal characterization of battery cells vital.
Therefore, understanding the different thermal effects within the battery is of ut most importance for selecting the correct battery thermal management systems
(BTMS). Understanding the heat distribution through the cell is important, as the
cells exhibit orthotropic properties. This master thesis deals with understanding the
dependence of different cooling strategies on the cell by creating a thermal model
of a Li-ion pouch cell determining temperature distribution within the cell volume.
A commercial CFD tool was utilised for performing the necessary simulations. The
simulations were based on the heat generated during high discharge profiles. To
validate the simulated results, experimental tests were conducted based on the pre defined profiles and the results are will be utilized to further improve the simulation
approach and calibrate the model to improve its accuracy and reliability.
It was observed that the thermal resistance is the highest only when the terminals
are cooled and the lowest when the cells are cooled radially. The heating tests also
showed similar trends in the thermal resistance characterisation. while comparing
the experimental and simulated results the difference in maximum temperatures was
found to be approximately 5%, with the experimental temperatures being higher
than the simulated results. As the tests were carried out only on a specific discharge case while repeating the experiments for other discharge profiles might give
a different perspective and more valuable information.
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Ämne/nyckelord
Thermal management, CFD, electric aviation, experimental validation, cooling, heating