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Drive unit characteristics of a completely electrical passenger aircraft

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Języki publikacji
EN
Abstrakty
EN
Aviation has, over the years, become an inseparable element of human life. Airplanes are very commonly used for various tasks, such as transport of passengers and goods, military attack and defence, rescue, recreation and so on. In spite of the many advantages of aviation, one cannot ignore its disadvantages. The most important disadvantages of aviation are the emissions that cause atmospheric pollution and noise. Additionally, one should remember about the decreasing stocks of non-renewable fuels. These drawbacks affect human health and the natural environment. Therefore, a good alternative to conventional drive units in aircraft may turn out to be electric drive units in the near future. The aim of this article is to check the extent to which today’s knowledge and technology allow the use of electric drive units instead of conventional aircraft drive units. This article presents the concept of electric aircraft, from the electric drive unit to its power supply system. The feasibility of designing an electric jet drive unit for a passenger aircraft was analysed based on the performances of PZL 104 Wilga 35 and Boeing B787 Dreamliner.
Wydawca
Rocznik
Strony
59--71
Opis fizyczny
Bibliogr. 14 poz., rys., tab.
Twórcy
  • Department of Mechanics, Machines and Energy Processes, Faculty of Mechanical and Power Engineering, Wroclaw University of Science and Technology, Wroclaw, Poland
Bibliografia
  • Bozhko, S., Hill, C. and Yang, T. (2018). More electric aircraft: systems and modeling. In: Webster J. G. ed., Wiley Encyclopedia of Electrical and Electronics Engineering. Hoboken: John Wiley & Sons, Inc. DOI: https://doi.org/10.1002/047134608X.W8367
  • Burke, K. A. (2003). Fuel cells for space science applications. NASA Glenn Research Center, Cleveland, Ohio. In: First International Energy Conversion Engineering Conference. Portsmouth, 17–21 August 2003.
  • Cable, T. L., Farmer, S. C., Eckel, A. J. and Setlock, J. A. (2009). Regenerative performance of the NASA symmetrical solid oxide fuel cell design. International Journal of Applied Ceramic Technology, 8(1), pp. 1–12.
  • Climate Change Authority. (2014). Light vehicle emissions standards for australia research report, <http://www.climatechangeauthority.gov.au/files/files/Light%20Vehicle%20Report/Lightvehiclesreport.pdf> [available 02/07/2020].
  • Dzierżanowski, P., Kordziński, W., Łyżwiński, M., Otyś, J., Szczeciński, S. and Wiatrek, R. (1983). Aviation Drives - Turbine Jet Engines. Warsaw: Transport and Communication Publishers.
  • Eco-Healthy Child Care. (2016). Noise pollution, <https://cehn.org/wp-content/uploads/2015/12/Noise_Pollution_9_16.pdf> [available 02/07/2020].
  • Gieras, J. F. (2008). Advancements in Electric Machines. Berlin-Heidelberg: Springer, pp. 247–249.
  • Jaroszewicz, A. (2017). Analysis of the possibility of use of a solid oxide fuel cell as an auxiliary power unit for modern passenger aircraft. Scientific Letters of Rzeszow University of Technology – Mechanics, 89(1), pp. 45–62.
  • Maré, J. C. and Fu J. (2017). Review on signal-by-wire and power-by-wire actuation for more electric aircraft. Chinese Journal of Aeronautics, 30(3), pp. 857–870.
  • Mueller, J.-K., Bensmann A., Bensmann B., Fischer T., Kadyk T., Narjes G., Kauth F., Ponick B., Seume J. R., Krewer, U., Hanke-Rauschenbach, R. and Mertens, A. (2018). Design considerations for the electrical power supply of future civil aircraft with active high-lift systems. Energies, 11(1), pp. 1–21.
  • Roque, A., Sousa, D. M., Fernão Pires, V. and Margato, E. (2017). Superconductivity and their applications. In: International Conference on Renewable Energies and Power Quality. Malaga, 4–6 April 2017.
  • Tariq, M., Maswood, A. I., Gajanayake, C. J. and Gupta, A. K. (2017). Aircraft batteries: current trend towards more electric aircraft. IET Electrical Systems in Transportation, 7(2), pp. 93–103.
  • Wolkiewicz, M. and Skowron, M. (2017). Diagnostic system for induction motor stator winding faults based on axial flux. Power Electronics and Drives, 2(2), pp. 137–150.
  • Yang, Z., Qu, J., Yingchuan, M.A. and Shi, X. (2015). Modeling and simulation of power distribution system in more electric aircraft. Journal of Electrical and Computer Engineering, 2015(8), pp. 1–7.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-1f356e88-d30f-4d07-b7fb-b3e852f3e0d3
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