The performance of hydrogen PEM fuel cell systems can be optimized by means of pressurization of the cathode air, especially in aviation, where at in-flight conditions the pressure of the ambient air is significantly lower as at on-ground conditions. To provide the inlet air at optimal conditions (p, T, rH) during flight, an air supply system is required and in an all-electric aircraft the compression should happen by means of an electric centrifugal compressor. A challenge for the operation of a pressurised fuel cell system at high altitudes is the control of the compression system. Any unstable operation like compressor surge has to be avoided, since it can damage both the fuel cell stack and the compressor itself. For the development of such an air supply system, a combined experimental and modeling approach was chosen.A hydrogen PEM fuel cell system was characterized at nominal and at low cathode pressures to obtain the behavior at flight relevant conditions and an experimental air supply system containing electric compressor, intercooler, humidifier, cathode volume and throttle valve at the outlet has been set up and used for the development, parameterization, and validation of a model for the compression system. The model is based on the Greitzer model 1,2, and has been extended to also represent the additional components between the compressor and the throttle valve (intercooler, humidifier, and cathode volume) 3. It is now able to predict the transient response of the entire air supply system to changes in the reference values of compressor speed and valve opening angle and the resulting mass flow changes and pressures within the individual components.The model and the data from the fuel cell system were used for the development of improved control strategies, that make it possible to operate the system safely in a wide range of operating conditions. Unstable situations, like compressor surge, are avoided by these control strategies even in the highly varying conditions during a flight. The developed control strategies are verified on the hardware of the experimental setup and tested under realistic flight conditions in a low-pressure climate chamber.References Greitzer, E. M. Surge and Rotating Stall in Axial Flow Compressors—Part I: Theoretical Compression System Model. Journal of Engineering for Power 98, 190–198 (1976).Gravdahl, J. T. & Egeland, O. Compressor Surge and Rotating Stall. (Springer London, London, 1999). doi:10.1007/978-1-4471-0827-6.Frank, D., Bauer, C. & Willich, C. Modeling of the cathode air supply for a pressurized hydrogen fuel cell system in airborne applications. Proceedings of the Aerospace Europe Conference 2023 (2023) doi:10.13009/EUCASS2023-218.
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