Improving the efficiency of fuel cell systems for aircraft propulsion: A comparative study of turbo-compressor and conventional systems
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
Published online on January 28, 2026
Abstract
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Ahead of Print.
In this study, the advantages and limitations of implementing a turbo-compressor system in a fuel cell propulsion architecture were examined. By integrating a turbine into the conventional air supply line, the system recovers exhaust energy, increasing ...
In this study, the advantages and limitations of implementing a turbo-compressor system in a fuel cell propulsion architecture were examined. By integrating a turbine into the conventional air supply line, the system recovers exhaust energy, increasing ...