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 |
Files in This Item:
File | Description | Size | Format | |
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2020_Barra-etal_Methodology-for-preliminary-performance-estimation-hybrid-electric-tilt-wing-aircraft_AMM.pdf | Accepted Version | 972.2 kB | Adobe PDF | View/Open |
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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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