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Feasibility study for a fuel cell-powered unmanned aerial vehicle with a 75 kg payload

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EN
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EN
Among the possible electric powerplants currently driving low-payload UAVs (up to around 10 kg of payload), batteries offer certain clear benefits, but for medium-payload operation such as aerotaxis and heavy-cargo transportation UAVs, battery capacity requirements restrict their usage due to high weight and volume. In light of this situation, fuel cell (FC) systems (FCS) offer clear benefits over batteries for the medium-payload UAV segment (> 50 kg). Nevertheless, studies regarding the application of FCS powerplants to this UAV segment are limited and the in-flight performance has not been clearly analysed. In order to address this knowledge gap, a feasibility analysis of these particular applications powered by FCS is performed in this study. A validated FC stack model (40 kW of maximum power) was integrated into a balance of plant to conform an FCS. As a novelty, the management of the FCS was optimized to maximize the FCS efficiency at different altitudes up to 12500 ft, so that the operation always implies the lowest H2 consumption regardless of the altitude. In parallel, an UAV numerical model was developed based on the ATLANTE vehicle and characterized by calculating the aerodynamic coefficients through CFD simulations. Then, both models were integrated into a 0D-1D modelling platform together with an energy management strategy optimizer algorithm and a suitable propeller model. With the preliminary results obtained from the FCS and UAV models, it was possible to ascertain the range and endurance of the vehicle. As a result, it was concluded that the combination of both technologies could offer a range over 600 km and an endurance over 5 h. Finally, with the integrated UAV-FCS model, a flight profile describing a medium altitude, medium endurance mission was designed and used to analyse the viability of FC-powered UAV. The results showed how UAVs powered by FCS are viable for the considered aircraft segment, providing competitive values of specific range and endurance.
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13--30
Opis fizyczny
Bibliogr. 20 poz., rys., tab., wykr., wzory
Twórcy
  • CMT-Motores Térmicos. Universitat Politècnica de València. Camino de Vera s/n, 46022 Valencia, Spain
  • CMT-Motores Térmicos. Universitat Politècnica de València. Camino de Vera s/n, 46022 Valencia, Spain
  • CMT-Motores Térmicos. Universitat Politècnica de València. Camino de Vera s/n, 46022 Valencia, Spain
  • CMT-Motores Térmicos. Universitat Politècnica de València. Camino de Vera s/n, 46022 Valencia, Spain
Bibliografia
  • [1] European Commission, 2019, “A European Green Deal: Striving to be the first climate-neutral continent”, URL https://ec.europa.eu/info/strategy/priorities-2019-2024/european-green-deal_en.
  • [2] European Commission, “European Partnership for Clean Aviation”, URL https://ec.europa.eu/info/law/better-regulation/have-your-say/initiatives/11904-European-Partnership-for-Clean-Aviation_en.
  • [3] Chiaramonti, D. “Sustainable Aviation Fuels: the challenge of decarbonization.” Energy Procedia Vol. 158 (2019). pp. 1202-1207 DOI 10.1016/j.egypro.2019.01.308. Innovative Solutions for Energy Transitions.
  • [4] Lee, S., Kim, G. and Bae, C. “Effect of injection and ignition timing on a hydrogen-lean stratified charge combustion engine.” International Journal of Engine Research. OnlineFirst (2021). DOI 10.1177/14680874211034682.
  • [5] Caton, P.A. and Pruitt, J.T. “Homogeneous charge compression ignition of hydrogen in a single-cylinder diesel engine.” International Journal of Engine Research Vol. 10 No. 1. (2009). pp. 45-63. DOI 10.1243/14680874JER02208.
  • [6] Christo, F.C., Levy, Y., Costa, M. and Balelang, G.A. “Effect of jet momentum flux and heat density on NOx emission in a flameless gas turbine combustor.” Aerospace Science and Technology Vol. 119 (2021). p. 107137. DOI 10.1016/j.ast.2021.107137.
  • [7] Baroutaji, A., Wilberforce, T., Ramadan, M. and Olabi, A.G. “Comprehensive investigation on hydrogen and fuel cell technology in the aviation and aerospace sectors.” Renewable and Sustainable Energy Reviews Vol. 106 (2019). pp. 31-40. DOI 10.1016/j.rser.2019.02.022.
  • [8] Molina, S., Novella, R., Pla, B. and Lopez-Juarez, M. “Optimization and sizing of a fuel cell range extender vehicle for passenger car applications in driving cycle conditions.” Applied Energy Vol. 285 (2021) p. 116469. DOI 10.1016/j.apenergy.2021.116469.
  • [9] Desantes, J.M., Novella, R., Pla, B. and Lopez-Juarez, M. “Impact of fuel cell range extender powertrain design on greenhouse gases and NOx emissions in automotive applications.” Applied Energy Vol. 302 (2021). p. 117526. DOI 10.1016/j.apenergy.2021.117526.
  • [10] Terada, I. and Nakagawa, H. “Polymer Electrolyte Fuel Cell.” Kobunshi Vol. 57 No. 7 (2008). pp. 498-501. DOI 10.1295/kobunshi.57.498.
  • [11] Murschenhofer, D., Kuzdas, D., Braun, S. and Jakubek, S., “A real-time capable quasi-2D proton exchange membrane fuel cell model.” Energy Conversion and Management, Vol. 162 (2018). pp. 159-175. DOI 10.1016/j.enconman.2018.02.028.
  • [12] Corbo, P., Migliardini, F. and Veneri, O. “Experimental analysis of a 20 kWe PEM fuel cell system in dynamic conditions representative of automotive applications.” Energy Conversion and Management Vol. 49 No. 10 (2008). pp. 2688-2697. DOI 10.1016/j.enconman.2008.04.001.
  • [13] Corbo, P., Migliardini, F. and Veneri, O. “Experimental analysis and management issues of a hydrogen fuel cell system for stationary and mobile application.” Energy Conversion and Management Vol. 48 No. 8 (2007). pp. 2365-2374. DOI 10.1016/j.enconman.2007.03.009.
  • [14] Teng, T., Zhang, X., Dong, H. and Xue, Q. “A comprehensive review of energy management optimization strategies for fuel cell passenger vehicle.” International Journal of Hydrogen Energy Vol. 45 No. 39 (2020). pp. 20293-20303. DOI 10.1016/j.ijhydene.2019.12.202.
  • [15] Burress, T.A., Campbell, S.L., Coomer, C.L., Ayers, C.W., Wereszczak, A.A., Cunningham, J.P., Marlino, L.D, Seiber, L.E. and Lin, H., “Evaluation of the 2010 Toyota Prius Hybrid Synergy Drive System.”, Oak Ridge National Laboratory, Tennessee, USA. (2011).
  • [16] Airbus Defence & Space. “Atlante: tactical fixed wing multirole UAS for maximized operational capability and mission flexibility.” (2014) URL https://www.airbus.com/content/dam/products-and-solutions/unmanned-air-systems/atlante/atlante-brochure.pdf.
  • [17] Cassidian. “Atlante: Tactical Unmanned Aerial System for National Security.” (2014) URL https://www.airtn.eu/downloads/atlante-para-airtn_v2.pdf.
  • [18] Rivard, E., Trudeau, M. and Zaghib, K. “Hydrogen storage for mobility: A review.” Materials Vol. 12 No. 12 (2019). DOI 10.3390/ma12121973.
  • [19] U.S. Department Of Energy. “DOE Technical Targets for Fuel Cell Systems and Stacks for transportation Applications.” (2015). URL https://www.energy.gov/eere/fuelcells/doe-technical-targets-fuel-cell-systems-and-stacks-transportation-applications.
  • [20] Howell, D., Cunningham, B., Duong, T. and Faguy, P. “Overview of the DOE VTO Advanced Battery R&D Program.” U.S. Department Of Energy (2016).
Uwagi
1. This research has been partially funded by the Spanish Ministry of Science, Innovation, and University through the University Faculty Training (FPU) program (FPU19/00550). This work is part of the project PID2020-11946RA-I00 funded by MCIN/AEI/ . Part of the research was also funded by Generalitat Valenciana and by “ERDF A way of making Europe” through grant number IDIFEDER/2021/039, as part of the program “Subvenciones para Infraestructuras y Equipamiento de I+D+i”. It was also partially funded by the Conselleria d’Innovació, Universitats, Ciència i Societat Digital of the Generalitat Valenciana through grant with expedient number GV/2021/069 of the program for “Grupos de Investigación Emergentes GV/2021”. The hydrogen activities were also funded by grant EQC2019-005968-P funded by MCIN/AEI/ and by “ERDF A way of making Europe”.
2. Opracowanie rekordu ze środków MEiN, umowa nr SONP/SP/546092/2022 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2022-2023).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-3172573d-d5f6-41ae-bfe4-9b61aa9fcf5c
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