More electric aircraft challenges: A study on 270 V/90 V interleaved bidirectional DC–DC converter

The concept of more electric aircraft (MEA) has gained increased importance in the aviation industry to make the aircraft energy efficient and reduce carbon footprints. MEA facilitates transition towards clean energy and accomplishing the United Nations’ net-zero emission goal by 2050. An efficient...

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Main Authors: Mustafa Tahir, Shoaib Ahmed Khan, Tahir Khan, Muhammad Waseem, Danish Khan, Andres Annuk
Format: Article
Language:English
Published: Elsevier 2022-11-01
Series:Energy Reports
Subjects:
Online Access:http://www.sciencedirect.com/science/article/pii/S2352484722012240
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author Mustafa Tahir
Shoaib Ahmed Khan
Tahir Khan
Muhammad Waseem
Danish Khan
Andres Annuk
author_facet Mustafa Tahir
Shoaib Ahmed Khan
Tahir Khan
Muhammad Waseem
Danish Khan
Andres Annuk
author_sort Mustafa Tahir
collection DOAJ
description The concept of more electric aircraft (MEA) has gained increased importance in the aviation industry to make the aircraft energy efficient and reduce carbon footprints. MEA facilitates transition towards clean energy and accomplishing the United Nations’ net-zero emission goal by 2050. An efficient and reliable dc–dc converter is an indispensable part of the MEA that interfaces 270VDC and 28VDC bus bars in aircraft applications. Dual Active Bridge is a well-known and promising topology for this application; however, the problem of current and voltage ripples deteriorates the life of the battery and filtering components. In addition, the mentioned voltage levels demand high voltage gain, which makes design challenging. To reduce the voltage gain requirement along with ripple minimization, a two-stage bidirectional converter is proposed by combing a three-phase interleaved buck-boost converter with Dual Active Bridge. The three-phase interleaved bidirectional converter is modelled and analysed using the state-space averaging method, and a controller is established. Simulation results demonstrate the efficacy of the design. The research carried out in this paper can serve as a reference and offer future research directions using the proposed idea, which might assist other researchers in developing an efficient design, eventually facilitating the MEA and carbon footprint reduction.
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spelling doaj.art-591751a16c7f43dbb14f51436fb8a0862023-01-20T04:25:41ZengElsevierEnergy Reports2352-48472022-11-01811331140More electric aircraft challenges: A study on 270 V/90 V interleaved bidirectional DC–DC converterMustafa Tahir0Shoaib Ahmed Khan1Tahir Khan2Muhammad Waseem3Danish Khan4Andres Annuk5College of Electrical Engineering, Zhejiang University, No. 38 Zheda Road, Xihu District, Hangzhou 310027, China; Corresponding authors.College of Electrical Engineering, Zhejiang University, No. 38 Zheda Road, Xihu District, Hangzhou 310027, ChinaCollege of Electrical Engineering, Zhejiang University, No. 38 Zheda Road, Xihu District, Hangzhou 310027, ChinaCollege of Electrical Engineering, Zhejiang University, No. 38 Zheda Road, Xihu District, Hangzhou 310027, China; Corresponding authors.College of Electrical Engineering, Zhejiang University, No. 38 Zheda Road, Xihu District, Hangzhou 310027, ChinaChair of Energy Application Engineering, Institute of Forestry and Engineering, Estonian University of Life Sciences, 51006 Tartu, EstoniaThe concept of more electric aircraft (MEA) has gained increased importance in the aviation industry to make the aircraft energy efficient and reduce carbon footprints. MEA facilitates transition towards clean energy and accomplishing the United Nations’ net-zero emission goal by 2050. An efficient and reliable dc–dc converter is an indispensable part of the MEA that interfaces 270VDC and 28VDC bus bars in aircraft applications. Dual Active Bridge is a well-known and promising topology for this application; however, the problem of current and voltage ripples deteriorates the life of the battery and filtering components. In addition, the mentioned voltage levels demand high voltage gain, which makes design challenging. To reduce the voltage gain requirement along with ripple minimization, a two-stage bidirectional converter is proposed by combing a three-phase interleaved buck-boost converter with Dual Active Bridge. The three-phase interleaved bidirectional converter is modelled and analysed using the state-space averaging method, and a controller is established. Simulation results demonstrate the efficacy of the design. The research carried out in this paper can serve as a reference and offer future research directions using the proposed idea, which might assist other researchers in developing an efficient design, eventually facilitating the MEA and carbon footprint reduction.http://www.sciencedirect.com/science/article/pii/S2352484722012240More electric aircraft (MEA)Interleaved bidirectional converter (IBC)ElectrificationClean energyGreen energy
spellingShingle Mustafa Tahir
Shoaib Ahmed Khan
Tahir Khan
Muhammad Waseem
Danish Khan
Andres Annuk
More electric aircraft challenges: A study on 270 V/90 V interleaved bidirectional DC–DC converter
Energy Reports
More electric aircraft (MEA)
Interleaved bidirectional converter (IBC)
Electrification
Clean energy
Green energy
title More electric aircraft challenges: A study on 270 V/90 V interleaved bidirectional DC–DC converter
title_full More electric aircraft challenges: A study on 270 V/90 V interleaved bidirectional DC–DC converter
title_fullStr More electric aircraft challenges: A study on 270 V/90 V interleaved bidirectional DC–DC converter
title_full_unstemmed More electric aircraft challenges: A study on 270 V/90 V interleaved bidirectional DC–DC converter
title_short More electric aircraft challenges: A study on 270 V/90 V interleaved bidirectional DC–DC converter
title_sort more electric aircraft challenges a study on 270 v 90 v interleaved bidirectional dc dc converter
topic More electric aircraft (MEA)
Interleaved bidirectional converter (IBC)
Electrification
Clean energy
Green energy
url http://www.sciencedirect.com/science/article/pii/S2352484722012240
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