Multilevel Aircraft-Inverter Design Based on Wavelet PWM for More Electric Aircraft.

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Title: Multilevel Aircraft-Inverter Design Based on Wavelet PWM for More Electric Aircraft.
Authors: Catalbas, Nurbanu1 (AUTHOR) ncatalbas@ankara.edu.tr, Pakfiliz, Ahmet Gungor2 (AUTHOR) ahmetgungor.pakfiliz@ostimteknik.edu.tr, Soysal, Gokhan1 (AUTHOR) soysal@eng.ankara.edu.tr
Source: Energies (19961073). May2024, Vol. 17 Issue 9, p2054. 23p.
Subjects: Pulse width modulation transformers, Electric power distribution grids, Hybrid electric airplanes
Abstract: This paper proposes a comprehensive power system designed for the use of a more electric aircraft power distribution system. Instead of traditional Nicad battery solutions as the energy source of the aircraft power system, lithium battery structures, which are a recent and promising solution in the field of aviation power systems, are modeled and analyzed. In this study, a WPWM-based, single-phase, multi-level pure sine wave static aircraft-inverter system is designed and integrated to improve the performance of conventional aircraft power systems. In the designed power system, a boost converter structure is proposed that boosts 28 VDC-to-270 VDC voltage coming from the lithium–ion battery pack and can reach a steady state in 0.032 s. The performance of the modeled WPWM-based aircraft-inverter system, compared to SPWM Bipolar and Unipolar switching techniques commonly used in single-phase inverter designs, reveals a THD reduction of approximately 27% with WPWM, resulting in a THD value below 2% for both load current and load voltage. As a result of the study, a power system that will enable the aircraft avionics, ventilation, and navigation systems to perform better than conventional power systems and comply with aircraft electric-power characteristic standards has been designed and detailed. [ABSTRACT FROM AUTHOR]
Copyright of Energies (19961073) is the property of MDPI and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.)
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  Data: Multilevel Aircraft-Inverter Design Based on Wavelet PWM for More Electric Aircraft.
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  Data: <searchLink fieldCode="AR" term="%22Catalbas%2C+Nurbanu%22">Catalbas, Nurbanu</searchLink><relatesTo>1</relatesTo> (AUTHOR)<i> ncatalbas@ankara.edu.tr</i><br /><searchLink fieldCode="AR" term="%22Pakfiliz%2C+Ahmet+Gungor%22">Pakfiliz, Ahmet Gungor</searchLink><relatesTo>2</relatesTo> (AUTHOR)<i> ahmetgungor.pakfiliz@ostimteknik.edu.tr</i><br /><searchLink fieldCode="AR" term="%22Soysal%2C+Gokhan%22">Soysal, Gokhan</searchLink><relatesTo>1</relatesTo> (AUTHOR)<i> soysal@eng.ankara.edu.tr</i>
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  Data: <searchLink fieldCode="JN" term="%22Energies+%2819961073%29%22">Energies (19961073)</searchLink>. May2024, Vol. 17 Issue 9, p2054. 23p.
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  Data: <searchLink fieldCode="DE" term="%22Pulse+width+modulation+transformers%22">Pulse width modulation transformers</searchLink><br /><searchLink fieldCode="DE" term="%22Electric+power+distribution+grids%22">Electric power distribution grids</searchLink><br /><searchLink fieldCode="DE" term="%22Hybrid+electric+airplanes%22">Hybrid electric airplanes</searchLink>
– Name: Abstract
  Label: Abstract
  Group: Ab
  Data: This paper proposes a comprehensive power system designed for the use of a more electric aircraft power distribution system. Instead of traditional Nicad battery solutions as the energy source of the aircraft power system, lithium battery structures, which are a recent and promising solution in the field of aviation power systems, are modeled and analyzed. In this study, a WPWM-based, single-phase, multi-level pure sine wave static aircraft-inverter system is designed and integrated to improve the performance of conventional aircraft power systems. In the designed power system, a boost converter structure is proposed that boosts 28 VDC-to-270 VDC voltage coming from the lithium–ion battery pack and can reach a steady state in 0.032 s. The performance of the modeled WPWM-based aircraft-inverter system, compared to SPWM Bipolar and Unipolar switching techniques commonly used in single-phase inverter designs, reveals a THD reduction of approximately 27% with WPWM, resulting in a THD value below 2% for both load current and load voltage. As a result of the study, a power system that will enable the aircraft avionics, ventilation, and navigation systems to perform better than conventional power systems and comply with aircraft electric-power characteristic standards has been designed and detailed. [ABSTRACT FROM AUTHOR]
– Name: AbstractSuppliedCopyright
  Label:
  Group: Ab
  Data: <i>Copyright of Energies (19961073) is the property of MDPI and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract.</i> (Copyright applies to all Abstracts.)
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        Value: 10.3390/en17092054
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      – Code: eng
        Text: English
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        PageCount: 23
        StartPage: 2054
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        Type: general
      – SubjectFull: Electric power distribution grids
        Type: general
      – SubjectFull: Hybrid electric airplanes
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      – TitleFull: Multilevel Aircraft-Inverter Design Based on Wavelet PWM for More Electric Aircraft.
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            – D: 01
              M: 05
              Text: May2024
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              Y: 2024
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