Overview and Weighted Evaluation of Cooling Concepts for High Power Electric Machines in Electrified Aircraft Propulsion Systems

Kurzfassung

The electrifcation of commercial aircrafts is one key strategy to mitigate aviation-related emissions and hence climate change effects. This requires high power electric motors with low weight and volume for aircraft propulsion. The critical enablers of those MW-class high specifc power electric machines are highly capable cooling systems, allowing to increase current densities and/or rotational speeds to obtain more power output, while maintaining geometrical extents and mass. Such cooling technology requires to be highly suitable for aviation purposes, leading to high demands on cooling effectiveness, energy effciency, additional mass, safety and reliability as well as costs and durability. Consequently, the goal of this paper is to perform an assessment of such technologies based on aviation-adjusted weighted criteria. As frst step, an overview of electric motor cooling methods and relevant literature is established. To condense the obtained information, an ensuing classifcation and categorization according to different methodical approaches is performed. Subsequently, the selected assessment criteria are weighted through pairwise comparison, followed by the evaluation of each cooling concept based on the weighted criteria. Concept-specifc evaluation parameters are obtained, enabling the comparison of technologies and the selection of preferred variants. Promising options turn out to be the cooling by cooling channels, the hollow conductor cooling and the heat pipe cooling. Among these, the channel cooling stands out due to its decent overall criteria fulfllment. As different cooling approaches have different strengths and weaknesses, a combination of these variants seems expedient to realize a highly capable electric machine cooling system. After further investigation, such as refnement of the literature-based evaluation, analytical assessment, as well as numerical validation, informed design choices can be made. This can potentially lead to an increase in electric motor power density, enabling electric aircraft propulsion and electrifcation of aviation. Thus, aviation-induced CO2 emissions could be reduced and adverse impact on climate could be mitiga