Abstract
This paper is situated in the framework of future hybrid electric aircraft in which embedded weight minimization and maximization of power efficiency are the key challenges to address fuel reduction and environmental constraints. In the first part, the integrated design process aiming the overall power train optimization is described. The second part presents models specifically oriented towards the integrated design. Finally, a sensitivity analysis is carried out at the power train system level to study the influence of both electric components-specific powers and efficiencies on the Maximum Take Off Weight (MTOW) and on the fuel burn of the hybrid propulsion aircraft.
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Notes
- 1.
uHVDC means “ultra-high voltage DC” standards beyond HVDC bus (±270 V), leading to bus voltages in the range of kVs.
References
X. Roboam, B. Sareni, A. DeAndrade, More electricity in the air: toward optimized electrical networks embedded in more-electrical aircraft. IEEE Indus. Electron. Mag. 6(4), 6–17 (2012). ISSN 1932-4529
Rolls Royce, The E-FAN X programme (2018), https://www.rolls-royce.com/media/our-stories/insights/2018/paul-stein-talks-about-e-fan-x.aspx
Zunum Aero (2018), https://www.jetblueventures.com/portfolio/zunum-aero/
R.H. Jansen, C. Bowman, A. Jankovsky, R. Dyson, J. Felder, Overview of NASA electrified aircraft propulsion research for large subsonic transports, in AIAA Propulsion and Energy 2017 Forum, Atlanta, GA, United States, 10–12 July 2017
B.J. Brelje, J.R.R.A. Martins, Electric, hybrid, and turboelectric fixed-wing aircraft: a review of concepts, models, and design approaches. Prog. Aerosp. Sci. 104, 1–19 (2019)
K.R. Antcliff, M.D. Guynn, T. Marien, D.P. Wells, S.J. Schneider, M.J. Tong, Mission analysis and aircraft sizing of a hybrid-electric regional aircraft, in 54th AIAA Aerospace Sciences Meeting, American Institute of Aeronautics and Astronautics, San Diego, California, USA, Jan 2016
J. Thauvin, Exploring the design space for a hybrid-electric regional aircraft with multidisciplinary design optimisation methods, PhD Université de Toulouse, France, Oct 2018
A. Sgueglia, P. Schmollgruber, N. Bartoli, O. Atinault, E. Bénard, J. Morlier, Exploration and sizing of a large passenger aircraft with distributed electric ducted fans, in AIAA - Scitech 2018, Kissimmee, United States, 8 Jan 2018–12 Jan 2018
F. Michel, H. Fieseler, L. Allidieres, Liquid hydrogen technologies for mobil use, in WHEC, Lyon, France, 16 June 2006
Siemens, Electric propulsion components with high power densities for aviation (2015), https://nari.arc.nasa.gov/sites/default/files/attachments/Korbinian-TVFW-Aug2015.pdf
X. Yi, A. Yoon, K. Haran, Multi-physics optimization for high-frequency air-core permanent-magnet motor of aircraft application, in 2017 IEEE International Electric Machines and Drives Conference (IEMDC), Miami, FL, USA, pp. 1–8
D. Zhang, NASA SiC light-weight inverter for MW-power (SLIM)—phase I, in 55th AIAA Aerospace Sciences Meeting, AIAA, Reston, VA, 2017
Acknowledgements
This project has received funding from the European Union Horizon 2020 (cleansky 2 JTI) research and innovation programme, 2014–2024 under grant agreement No 715483.
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Pettes-Duler, M., Roboam, X., Sareni, B. (2020). Integrated Design Process and Sensitivity Analysis of a Hybrid Electric Propulsion System for Future Aircraft. In: Zamboni, W., Petrone, G. (eds) ELECTRIMACS 2019. Lecture Notes in Electrical Engineering, vol 615. Springer, Cham. https://doi.org/10.1007/978-3-030-37161-6_6
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DOI: https://doi.org/10.1007/978-3-030-37161-6_6
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