Abstract
The efficiency of new oscillator connection diagrams in plasma ignition systems (PISs) of gas-turbine engines (GTEs) is analyzed. The most efficient oscillator connection diagram is found that reduces losses in the power circuit of the ignition system with an increased ignition capacity of the plasmatron. There are two types of discharges in the plasmatron: a continuous arc discharge and a pulsed capacitive discharge, the instantaneous power of a short capacitive discharge being several orders of magnitude higher than the instantaneous power of the arc discharge. The dynamics of discharge processes in the oscillator is estimated. Analytical expressions are presented for the main parameters of pulsed discharges: the maximum discharge current and the energy and duration of discharges.
REFERENCES
Gizatullin, F.A. and Salikhov, R.M., To determining mode oscillators part of plasma ignition system, Vestn. UGATU, 2010, vol. 14, no. 2 (37), pp. 87–89.
Kotenko, P.S. and Gizatullin, F.A., Perspektivy sovershenstvovaniya elektrooborudovaniya letatel’nykh apparatov, obshchie voprosy ekspluatatsii i remonta (Prospects for Improvement of Aircraft Electrical Equipment, General Issues of Operation and Repair), Ufa: RIK Ufa State Aviat. Tech. Univ., 2018.
Gizatullin, F.A. and Gabidullina, Z.G., Determination of oscillators parameters in gas turbine engine plasma ignition systems, Proc. Int. Conf. on Electrotechnical Complexes and Systems (ICOECS), Ufa, Russian Federation, November 16–18, 2021, IEEE, 2022, pp. 97–100. ISBN 978-166540727-4.https://doi.org/10.1109/ICOECS52783.2021.9657438.
USSR Inventor’s Certificate no. 782444.
Gizatullin, F.A., Gabidullina, Z.G., Salikhov, R.M., and Karimova, A.G., Assessing the simulation of capacitive ignition systems in gas-turbine engines, Russ. Eng. Res., 2020, vol. 40, no. 7, pp. 531–534. https://doi.org/10.3103/S1068798X20070151
Shi, X., Li, H., Ruowen, W., and Meng, X., Modeling and simulation of aviation engine ignition spark frequency disorder, Open Electr. Electron. Eng. J., 2015, vol. 9, pp.193–199.
Zhao, J. and Zhang, T., Study on spark frequency stability of aeroengine transistor ignition system, Mod. Electron. Tech., 2013, vol. 11, no. 37, pp. 116–118.
Mahajan, D.P., Narayanswamy, R., and Saxena, S.K., Novel exciter circuit for ignition of gas turbine engines in aerospace applications, IEEE Int. Conf. on Industrial Technology, Cape Town, South Africa, February 25–28, 2013, IEEE, 2013, pp. 613–617. https://doi.org/10.1109/ICIT.2013.6505741
Song, K., Liao, J., and Yang, Q., Research of modeling and simulation of aviation ignition equipment, Adv. Mater. Res., 2013, vols. 690–693, pp. 2906–2911.
RF Patent 94640.
RF Patent 132497.
RF Patent 120721.
RF Patent 86251.
RF Patent 99829.
Lefebvre, A.H. and Ballal, D.R., Gas Turbine Combustion: Alternative Fuels and Emissions, CRC Press, 2010.
Funding
This work was supported by the Russian Science Foundation under grant no. 23-29-00713, https://rscf.ru/project/23-29-00713/.
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Translated by I. Nikitin
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Farit A. Gizatullin, Zul’fiya G. Gabidullina New Connection Diagrams of Oscillators as a Part of Plasma Ignition Systems for Gas-Turbine Engines. Russ. Engin. Res. 44, 1–5 (2024). https://doi.org/10.3103/S1068798X2401012X
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DOI: https://doi.org/10.3103/S1068798X2401012X