The growing concern about climate change and the contemporary increase in mobility require-ments call for faster, cheaper, safer, and cleaner means of transportation. The retrofitting of fos-sil-fueled piston-engine ultralight aerial vehicles to hydrogen power systems is an option re-cently proposed in this direction. The goal of this investigation is a comparative analysis of the environmental impact of conventional and hydrogen-based propulsive systems. As a case study, a hybrid electric configuration consisting of a fuel cell with a nominal power of about 30kW, a 6kWh LFP battery, and a pressurized hydrogen vessel is proposed to replace a piston-prop con-figuration for an ultralight aerial vehicle. Both power systems are modeled with a backward ap-proach that allows the efficiency of the main components to be evaluated based on load and alti-tude at every moment of the flight with a time step of 1 s. A typical 90-minute flight mission is considered for the comparative analysis which is performed in terms of direct and indirect emis-sions of carbon dioxide, water, and pollutant substances. For the hydrogen-based configuration, two possible strategies are adopted for the use of the battery: charge sustaining and charge de-pleting. Moreover, the effect of altitude on the parasitic power of the fuel cell compressor, and consequently on the net efficiency of the fuel cell system, is taken into account. The results showed that, even if the use of hydrogen confines the direct environmental impact to the emis-sion of water (in a similar quantity to the fossil fuel case), the indirect emissions associated with the production, transportation, and delivery of hydrogen and electricity compromises the de-sired achievement of pollutant-free propulsion in terms of equivalent emissions of CO2 and VOCs, if hydrogen is obtained from natural gas reforming. However, in the case of green hy-drogen from electrolysis with wind energy, the total (direct and indirect) emissions of CO2 can be reduced up to 1/5 of the fossil fuel case. The proposed configuration has the additional ad-vantage of eliminating the problem of lead which is used as an additive in the AVGAS 100LL.

Energy Consumption and Saved Emissions of a Hydrogen Power System for Ultralight Aviation: A Case Study

Donateo, Teresa
Investigation
;
Bonatesta, Andrea Graziano
Data Curation
;
Ficarella, Antonio
Funding Acquisition
;
Lecce, Leonardo
Resources
2024-01-01

Abstract

The growing concern about climate change and the contemporary increase in mobility require-ments call for faster, cheaper, safer, and cleaner means of transportation. The retrofitting of fos-sil-fueled piston-engine ultralight aerial vehicles to hydrogen power systems is an option re-cently proposed in this direction. The goal of this investigation is a comparative analysis of the environmental impact of conventional and hydrogen-based propulsive systems. As a case study, a hybrid electric configuration consisting of a fuel cell with a nominal power of about 30kW, a 6kWh LFP battery, and a pressurized hydrogen vessel is proposed to replace a piston-prop con-figuration for an ultralight aerial vehicle. Both power systems are modeled with a backward ap-proach that allows the efficiency of the main components to be evaluated based on load and alti-tude at every moment of the flight with a time step of 1 s. A typical 90-minute flight mission is considered for the comparative analysis which is performed in terms of direct and indirect emis-sions of carbon dioxide, water, and pollutant substances. For the hydrogen-based configuration, two possible strategies are adopted for the use of the battery: charge sustaining and charge de-pleting. Moreover, the effect of altitude on the parasitic power of the fuel cell compressor, and consequently on the net efficiency of the fuel cell system, is taken into account. The results showed that, even if the use of hydrogen confines the direct environmental impact to the emis-sion of water (in a similar quantity to the fossil fuel case), the indirect emissions associated with the production, transportation, and delivery of hydrogen and electricity compromises the de-sired achievement of pollutant-free propulsion in terms of equivalent emissions of CO2 and VOCs, if hydrogen is obtained from natural gas reforming. However, in the case of green hy-drogen from electrolysis with wind energy, the total (direct and indirect) emissions of CO2 can be reduced up to 1/5 of the fossil fuel case. The proposed configuration has the additional ad-vantage of eliminating the problem of lead which is used as an additive in the AVGAS 100LL.
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11587/524446
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