Design of hybrid-electric aircraft with fault-tolerance considerations. Marciello, V., Orefice, F., Nicolosi, F., Ciliberti, D., & Della vecchia , P. Chinese Journal of Aeronautics, 36(2):160–178, February, 2023. ![Design of hybrid-electric aircraft with fault-tolerance considerations [link]](https://bibbase.org/img/filetypes/link.svg "link")
Paper doi abstract bibtex The potential benefits of hybrid-electric or all-electric propulsion have led to a growing interest in this topic over the past decade. Preliminary design of propulsion systems and innovative configurations has been extensively discussed in literature, but steps towards higher levels of technological readiness, optimisation algorithms based on reliable weight estimation and simulation-based mission analysis are required. This paper focuses on the integration of a method for evaluating the lateral-directional controllability of an aircraft within a design chain that integrates aero-propulsive interactions, accurate modelling of the fuel system, and mid-fidelity estimation of the structural weight. Furthermore, the present work proposes a strategy for powerplant management in scenarios with an inoperative chain element. Benefits of hybrid-electric propulsion on the design of the vertical tail plane are evaluated involving the analysis of multiple failure scenarios and certification requirements. The proposed application concerns a commuter aircraft.
@article{marciello_design_2023,
title = {Design of hybrid-electric aircraft with fault-tolerance considerations},
volume = {36},
copyright = {All rights reserved},
issn = {1000-9361},
url = {https://www.sciencedirect.com/science/article/pii/S1000936122001066},
doi = {10.1016/j.cja.2022.05.014},
abstract = {The potential benefits of hybrid-electric or all-electric propulsion have led to a growing interest in this topic over the past decade. Preliminary design of propulsion systems and innovative configurations has been extensively discussed in literature, but steps towards higher levels of technological readiness, optimisation algorithms based on reliable weight estimation and simulation-based mission analysis are required. This paper focuses on the integration of a method for evaluating the lateral-directional controllability of an aircraft within a design chain that integrates aero-propulsive interactions, accurate modelling of the fuel system, and mid-fidelity estimation of the structural weight. Furthermore, the present work proposes a strategy for powerplant management in scenarios with an inoperative chain element. Benefits of hybrid-electric propulsion on the design of the vertical tail plane are evaluated involving the analysis of multiple failure scenarios and certification requirements. The proposed application concerns a commuter aircraft.},
number = {2},
urldate = {2023-08-14},
journal = {Chinese Journal of Aeronautics},
author = {Marciello, Valerio and Orefice, Francesco and Nicolosi, Fabrizio and Ciliberti, Danilo and Della vecchia, Pierluigi},
month = feb,
year = {2023},
keywords = {Distributed electric propulsion, Hybrid-electric aircraft, Failure management, Fault-tolerance analysis, Lateral-directional controllability},
pages = {160--178},
file = {ScienceDirect Full Text PDF:C\:\\Users\\danci\\Zotero\\storage\\N4S5TYE7\\Marciello et al. - 2023 - Design of hybrid-electric aircraft with fault-tole.pdf:application/pdf;ScienceDirect Snapshot:C\:\\Users\\danci\\Zotero\\storage\\X2EJS2KE\\S1000936122001066.html:text/html},
}
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