Abstract
This paper presents the experimental results of a study on ion thrust under magnetic flux density in atmospheric conditions. This study demonstrates that magnetic flux density perpendicular to the direction of ion flow generates a Lorentz-force. The effect of this electromagnetic force on the flow rate distribution was measured via experimentation. Consequently, it was confirmed that the magnetic flux density by the magnets increased the thrust force by 46% compared to the case without magnetic flux density. On the other hand, the discharge current was reduced by 11% due to the third electrode effect of the magnets.
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References
Drew D, Contreras DS, Pister KSJ (2017) First thrust from a microfabricated atmospheric ion engine. In: 2017 IEEE 30th international conference on micro electro mechanical system 346–349
Gilmore CK, Barrett SRH (2015) Electrohydrodynamic thrust density using positive corona-induced ionic winds for in atmosphere propulsion. Proc R Soc A 471(2175):1–24
Kim SK, Yu MJ, Choi SW (2010) Preliminary design of ECR ion thruster. Aerospace Eng Technol 9(2):14–21
Einat M, Kalderon R (2014) High efficiency Lifter based on the biefeld-brown effect. AIP Adv 4(7):1–20
Ma C, Lu R, Ye B (2013) Surface aerodynamic model of the lifter. J Electrostat 71:134–139
Zhao L, Adamiak K (2006) EHD gas flow in electrostatic levitation unit. J Electrostat 64:639–645
Pekarek S (2010) DC corona discharge ozone production enhanced by magnetic field. Euro Phys J D 56:91–98
Ferreira JL, Monteiro KMFP, Damasio HJ, Kostov KG (1998) Magnetic field enhanced plasma reactor for pollutant gases control by corona discharge. Combust Sci Technol 140:1–11
Park JY, Kim GH, Kim JD, Koh HS, Lee DC (1998) NOx removal using DC corona discharge with magnetic field. Combustion Sci Technol 133:65–77
Ulaby F (2001) Fundamentals of applied electromagnetics, 2001 media edition. Prentice Hall, pp 187–189
Xu D, Sheng L, Wang H, Sun Y, Zhang X, Mi J (2007) Study of magnetically enhanced corona pre-charger. J Electrostat 65:101–106
Karimov AR, Murad PA (2018) Plasma thruster using momentum exchange in crossed magnetic fields. IEEE Trans Plasma Sci 46(4):882–887
Mi J, Xu D, Sun Y, Du S, Chen Y (2008) Influence of magnetic fields on negative corona discharge currents. J Electrostat 66:457–462
Moon JD, Jung HJ, Jung JS (2007) Effect of cylindrical third electrode of a point-plate type plasma reactor on corona discharge and ozone generation characteristics. Trans Korean Inst Electr Eng 56(5):933–937
Kim YJ, Kang HW (2016) Development and performance evaluation of HVLS Fan for energy saving of logistic centers. KLRA 26(6):25–34
Park JY, Kim GH, Kim JD, Koh HS, Lee DC (1998) NOx removal using DC corona discharge with magnetic field. Combust Sci Technol 133:65–77
Acknowledgements
This research was supported by Basic Science Research Program through the National Research Foundation of Korea(NRF) funded by the Ministry of Education(NRF-2017R1D1A3B03031043).
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Kim, JG., Jung, JS. Application of a Magnetic Flux in the Corona Discharge Region to Improve Ion Thrust via Ion Acceleration. J. Electr. Eng. Technol. 14, 1683–1688 (2019). https://doi.org/10.1007/s42835-019-00204-y
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DOI: https://doi.org/10.1007/s42835-019-00204-y