Please use this identifier to cite or link to this item: https://doi.org/10.21256/zhaw-27151
Publication type: Conference paper
Type of review: Peer review (publication)
Title: A methodology for preliminary performance estimation of a hybrid-electric tilt-wing aircraft for emergency medical services
Authors: Barra, Federico
Capone, Pierluigi
Guglieri, Giorgio
et. al: No
DOI: 10.1109/ICUAS48674.2020.9214025
10.21256/zhaw-27151
Proceedings: 2020 International Conference on Unmanned Aircraft Systems (ICUAS)
Page(s): 1636
Pages to: 1643
Conference details: International Conference on Unmanned Aircraft Systems (ICUAS), Athens, Greece, 1-4 September 2020
Issue Date: 2020
Publisher / Ed. Institution: IEEE
ISBN: 978-1-7281-4278-4
ISSN: 2575-7296
Language: English
Subjects: Hybrid-Electric; eVTOL; Aircraft propulsion; Medical service; Turbine; Battery; Airplane; Helicopter
Subject (DDC): 629: Aeronautical, automotive engineering
Abstract: This paper aims to provide a simple methodology to preliminary size a hybrid-electric propulsion system for large scale piloted, optionally piloted or unmanned tilt-wing aircraft. In this work, the author refers to three mission profile representative of an Emergency Medical Service (EMS) operation and estimate the performance of the aircraft along the mission. Thus, based on some assumptions on battery technology, architecture of the hybrid system and mission safety requirements, a methodology for preliminary performance estimation is described and results for a baseline architecture are presented. Based on present and near future battery technology (in terms of charge/discharge rates and energy density), the present study shows how safety requirements can strongly affect the overall size of the power-plant system and impact the feasibility of hybrid-electric technology in aeronautical applications.
URI: https://digitalcollection.zhaw.ch/handle/11475/27151
Fulltext version: Accepted version
License (according to publishing contract): Not specified
Departement: School of Engineering
Organisational Unit: Centre for Aviation (ZAV)
Appears in collections:Publikationen School of Engineering

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Barra, F., Capone, P., & Guglieri, G. (2020). A methodology for preliminary performance estimation of a hybrid-electric tilt-wing aircraft for emergency medical services [Conference paper]. 2020 International Conference on Unmanned Aircraft Systems (ICUAS), 1636–1643. https://doi.org/10.1109/ICUAS48674.2020.9214025
Barra, F., Capone, P. and Guglieri, G. (2020) ‘A methodology for preliminary performance estimation of a hybrid-electric tilt-wing aircraft for emergency medical services’, in 2020 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE, pp. 1636–1643. Available at: https://doi.org/10.1109/ICUAS48674.2020.9214025.
F. Barra, P. Capone, and G. Guglieri, “A methodology for preliminary performance estimation of a hybrid-electric tilt-wing aircraft for emergency medical services,” in 2020 International Conference on Unmanned Aircraft Systems (ICUAS), 2020, pp. 1636–1643. doi: 10.1109/ICUAS48674.2020.9214025.
BARRA, Federico, Pierluigi CAPONE und Giorgio GUGLIERI, 2020. A methodology for preliminary performance estimation of a hybrid-electric tilt-wing aircraft for emergency medical services. In: 2020 International Conference on Unmanned Aircraft Systems (ICUAS). Conference paper. IEEE. 2020. S. 1636–1643. ISBN 978-1-7281-4278-4
Barra, Federico, Pierluigi Capone, and Giorgio Guglieri. 2020. “A Methodology for Preliminary Performance Estimation of a Hybrid-Electric Tilt-Wing Aircraft for Emergency Medical Services.” Conference paper. In 2020 International Conference on Unmanned Aircraft Systems (ICUAS), 1636–43. IEEE. https://doi.org/10.1109/ICUAS48674.2020.9214025.
Barra, Federico, et al. “A Methodology for Preliminary Performance Estimation of a Hybrid-Electric Tilt-Wing Aircraft for Emergency Medical Services.” 2020 International Conference on Unmanned Aircraft Systems (ICUAS), IEEE, 2020, pp. 1636–43, https://doi.org/10.1109/ICUAS48674.2020.9214025.


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