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2.4 kW Three-Phase Inverter for Aircraft Application-Hardware Implementation

  • K. M. Pandav
  • S. B. MahajanEmail author
  • Padmanaban Sanjeevikumar
  • S. M. Badave
  • R. M. Pachagade
Chapter
Part of the Lecture Notes in Electrical Engineering book series (LNEE, volume 436)

Abstract

In this article 2.4 kW, three-phase inverter for aircraft application is articulated. When aircraft above 1000 m altitude, power amplifiers are employed to increase the strength of signal during transmission. The circuitry consist of input filter, three-phase output obtained by connecting three single-phase H-bridge inverter, transformers and LC filters at the star connected load end. The (THD) of proposed three-phase inverter is 2.8%. The Total Harmonics Distortion (THD) of the circuit is reduced by using sinusoidal pulse width modulation technique (SPWM). The component size is reduced by using high frequency modulating signal (400 Hz). The proposed circuit performance is verified with experimental and simulation result. The experimental and simulation result confirms the feasibility of proposed converter.

Keywords

Three-phase inverter H-Bridge Aircraft application High frequency Sinusoidal pulse width modulation (SPWM) 

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Copyright information

© Springer Nature Singapore Pte Ltd. 2018

Authors and Affiliations

  • K. M. Pandav
    • 1
  • S. B. Mahajan
    • 1
    Email author
  • Padmanaban Sanjeevikumar
    • 2
  • S. M. Badave
    • 1
  • R. M. Pachagade
    • 1
  1. 1.Department of Electrical & Electronics EngineeringMarathwada Institute of TechnologyAurangabadIndia
  2. 2.Department of Electrical & Electronics EngineeringUniversity of JohannesburgAuckland ParkSouth Africa

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