EN
Single Phase Series Active Filter Load Compensation for Aircraft Applications
Öz
Aircraft technology is moving toward what is known as More Electric Aircraft. This technology aims to increase the amount of electrical power equipment rather than mechanical or hydraulic equipment. This paper present an analytical method of calculating reactive and harmonic current and using this current as a reference to feed a series active filter to compensate the harmonic currents generated by a nonlinear load.
Anahtar Kelimeler
Kaynakça
- M H Taha, “Active rectifier using DQ control for aircraft application” IEMDC 2007; PP 1306-1310.
- M H Taha, S Skinner, S Gami, M Holme and G Raimondi “ Variable frequency to constant frequency converter for aircraft application” PEMD 2002, PP235-240
- Kamala Kant Mishra, Rajesh Gupta, “ Load compensation for single phase using series active filter” IJEST Vol 3, No 3 , 2011 , pp 83-93
- J.Sebastian Tepper, Juan W. Dixon,” A simple frequency – independent method for calculating the reactive and harmonics current in nonlinear load”IEEE Trans on Indust Elect, Vol. 43 No.6 Decem 1996. Pp 647-65
- Marko Dimitrijevic and Vanco Litovski “ Quantitave Analysis of reactive power calculation for small non-linear load” Proceeding of small system simulation symposium 2012, Nis
- Juan Dixon, Luis Morán, José Rodríguez, Ricardo Domke, “Reactive Power Compensation Technologies, State of–the-Art Review”, IEEE Proc. vol. 93, no. 12, pp. 2144-2164, 2005.
- R. S. Herrera, P. Salmeron, and H. Kim, “Instantaneous reactive power theory applied to active power filter compensation: Different approaches, assessment, and experimental results”, IEEE Trans. Ind. Electron., vol. 55, no. 1, pp. 184–196, Jan. 2008.
- L. Hongda and K. Cao, “Active power filter simulation based on instantaneous reactive power theory and the PWM hysteresis control mode”, 978-1-4244-8161-3/11/ IEEE, 2011.
Ayrıntılar
Birincil Dil
İngilizce
Konular
-
Bölüm
-
Yazarlar
Yayımlanma Tarihi
4 Haziran 2015
Gönderilme Tarihi
4 Haziran 2015
Kabul Tarihi
-
Yayımlandığı Sayı
Yıl 2015 Cilt: 1 Sayı: 2
APA
Taha, M. (2015). Single Phase Series Active Filter Load Compensation for Aircraft Applications. International Journal of Engineering Technologies IJET, 1(2), 72-77. https://doi.org/10.19072/ijet.105716
AMA
1.Taha M. Single Phase Series Active Filter Load Compensation for Aircraft Applications. IJET. 2015;1(2):72-77. doi:10.19072/ijet.105716
Chicago
Taha, Mohammad. 2015. “Single Phase Series Active Filter Load Compensation for Aircraft Applications”. International Journal of Engineering Technologies IJET 1 (2): 72-77. https://doi.org/10.19072/ijet.105716.
EndNote
Taha M (01 Haziran 2015) Single Phase Series Active Filter Load Compensation for Aircraft Applications. International Journal of Engineering Technologies IJET 1 2 72–77.
IEEE
[1]M. Taha, “Single Phase Series Active Filter Load Compensation for Aircraft Applications”, IJET, c. 1, sy 2, ss. 72–77, Haz. 2015, doi: 10.19072/ijet.105716.
ISNAD
Taha, Mohammad. “Single Phase Series Active Filter Load Compensation for Aircraft Applications”. International Journal of Engineering Technologies IJET 1/2 (01 Haziran 2015): 72-77. https://doi.org/10.19072/ijet.105716.
JAMA
1.Taha M. Single Phase Series Active Filter Load Compensation for Aircraft Applications. IJET. 2015;1:72–77.
MLA
Taha, Mohammad. “Single Phase Series Active Filter Load Compensation for Aircraft Applications”. International Journal of Engineering Technologies IJET, c. 1, sy 2, Haziran 2015, ss. 72-77, doi:10.19072/ijet.105716.
Vancouver
1.Mohammad Taha. Single Phase Series Active Filter Load Compensation for Aircraft Applications. IJET. 01 Haziran 2015;1(2):72-7. doi:10.19072/ijet.105716