The analysis of “more electric engine” technology to improve the environmental performance of aircraft jet engine

Maciej Henzel; Krzysztof Falkowski; Aleksander Olejnik

doi:10.1051/e3sconf/20184600029

All issues

Volume 46 (2018)

E3S Web Conf., 46 (2018) 00029

References

Open Access

Issue		E3S Web Conf. Volume 46, 2018 3^rd International Conference on Energy and Environmental Protection


Article Number		00029
Number of page(s)		8
DOI		https://doi.org/10.1051/e3sconf/20184600029
Published online		13 September 2018

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[1] Moir I., Seabridge A.: “Aircraft systems-Mechanical, electrical and avionics subsystem integration”, John Wiley & Sons, pp. 227-238, (2008) [Google Scholar]

[2] Lempke, T.A., Design and analysis of a novel low loss homopolar electrodynamic bearing, Doctoral Thesis, KTH Electrical Engineering, Stockholm., (2005) [Google Scholar]

[3] Falkowski K., Gosiewski Z.: Analytical Method of the Magnetic Forces Estimation in passive Magnetic Bearings, The 8th International Conference on Motion and Vibration Control MOVIC 2006, Korea, September (2006) [Google Scholar]

[4] Falkowski K., Henzel M., Mazurek P., Magnetic suspension system for aircraft engine, 10th International Conference on Mechatronic Systems and Materials “MSM 2014”, July 7÷10, Opole, Poland, (2014) [Google Scholar]

[5] Henzel M., Mazurek P.: “The analysis of the control system of the active magnetic bearing”, Electrodynamic and mechatronic systems, 3rd International Students Conference on Electrodynamics and Mechatronics (SCE III), IEEE, Opole (2011) [Google Scholar]

[6] Henzel M., Mazurek P. The rapid prototyping of active magnetic bearing, Advances in Intelligent Systems and Computing, Recent Advances in Automation, Robotics and Measuring Techniques, Springer, 267, pp. 155-166, (2014) [CrossRef] [Google Scholar]