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Series Hybrid Configuration Based Proposed Architecture Model for Hybrid Electric Aircraft Using SimulinkMatlab

Author

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  • MEGHANA .R
  • Kiran Kumar .D
  • Lakshmikanth Reddy

Abstract

Due to demand for optimization of various aircraft performance parameters, decrease in operating and maintenance cost and to reduce gas emission Hybrid Electric Aircraft (HEA) concept has been put forward. Rapid growth in the field of power electronics, electric motor and conversion system has made Hybrid Electric Aircraft possible. Being more advantageous series hybrid configuration is used to build basic architecture model. Architecture consists of two power sources one is engine driven generator other is the battery. Electric motor drive plays an very important role in series hybrid configuration as it is the only torque source to meet the aircraft performance such as acceleration. The proposed system presents groundwork of the hybrid electric system architecture and reduced fuel consumption compared to existing convention aircraft system. MATLAB software is used to design the basic structure of hybrid electric aircraft architecture and the simulation results shown and analysis of overall system performance is done accordingly.

Suggested Citation

  • MEGHANA .R & Kiran Kumar .D & Lakshmikanth Reddy, 2018. "Series Hybrid Configuration Based Proposed Architecture Model for Hybrid Electric Aircraft Using SimulinkMatlab," International Journal of Scientific Research in Computer Science, Engineering and Information Technology, International Journal of Scientific Research in Computer Science, Engineering and Information Technology, vol. 4(6), pages 875-881, May.
    • Handle: RePEc:jbh:ijsrcs:v4:y2018:i6:id:hcseit1846165
    Note: Article URL: https://ijsrcseit.com/CSEIT1846165
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