Optimization of the Energy Storage of Series-Hybrid Propelled Aircraft by Means of Integer Differential Evolution
The possibility of realizing full electric or hybrid electric propulsion for aircraft has been considered due to the constant growth in the use of electric technologies in aircraft and the availability of high-power-density electrical machines and converters. In this paper, an optimized design appro...
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Language: | English |
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MDPI AG
2019-05-01
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Series: | Aerospace |
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Online Access: | https://www.mdpi.com/2226-4310/6/5/59 |
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author | Liviu Sevastian Bocii Luigi Pio Di Noia Renato Rizzo |
author_facet | Liviu Sevastian Bocii Luigi Pio Di Noia Renato Rizzo |
author_sort | Liviu Sevastian Bocii |
collection | DOAJ |
description | The possibility of realizing full electric or hybrid electric propulsion for aircraft has been considered due to the constant growth in the use of electric technologies in aircraft and the availability of high-power-density electrical machines and converters. In this paper, an optimized design approach is proposed with reference to the optimal trade-off between energy storage system sizing and the fuel mass of a series of hybrid aircraft. The problem is approached using an integer optimization algorithm based on differential evolution and by mixing both the flight mechanics and the electrical issues inherent to hybrid flights. This method has been validated by means of implementing numerical simulations and the results are reported and discussed in the paper. |
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format | Article |
id | doaj.art-f9b5bef623ef4e00911c644a54aeece7 |
institution | Directory Open Access Journal |
issn | 2226-4310 |
language | English |
last_indexed | 2024-12-21T07:40:06Z |
publishDate | 2019-05-01 |
publisher | MDPI AG |
record_format | Article |
series | Aerospace |
spelling | doaj.art-f9b5bef623ef4e00911c644a54aeece72022-12-21T19:11:21ZengMDPI AGAerospace2226-43102019-05-01655910.3390/aerospace6050059aerospace6050059Optimization of the Energy Storage of Series-Hybrid Propelled Aircraft by Means of Integer Differential EvolutionLiviu Sevastian Bocii0Luigi Pio Di Noia1Renato Rizzo2Department of Automation, Industrial, Textile and Transportation Engineering, Aurel Vlaicu University of Arad, 310130 Arad, RomaniaDepartment of Electrical Engineering and Information Technologies, University of Naples Federico II, 80125 Naples, ItalyDepartment of Electrical Engineering and Information Technologies, University of Naples Federico II, 80125 Naples, ItalyThe possibility of realizing full electric or hybrid electric propulsion for aircraft has been considered due to the constant growth in the use of electric technologies in aircraft and the availability of high-power-density electrical machines and converters. In this paper, an optimized design approach is proposed with reference to the optimal trade-off between energy storage system sizing and the fuel mass of a series of hybrid aircraft. The problem is approached using an integer optimization algorithm based on differential evolution and by mixing both the flight mechanics and the electrical issues inherent to hybrid flights. This method has been validated by means of implementing numerical simulations and the results are reported and discussed in the paper.https://www.mdpi.com/2226-4310/6/5/59batterydifferential evolutionelectric propulsionhybrid electric aircraftoptimization |
spellingShingle | Liviu Sevastian Bocii Luigi Pio Di Noia Renato Rizzo Optimization of the Energy Storage of Series-Hybrid Propelled Aircraft by Means of Integer Differential Evolution Aerospace battery differential evolution electric propulsion hybrid electric aircraft optimization |
title | Optimization of the Energy Storage of Series-Hybrid Propelled Aircraft by Means of Integer Differential Evolution |
title_full | Optimization of the Energy Storage of Series-Hybrid Propelled Aircraft by Means of Integer Differential Evolution |
title_fullStr | Optimization of the Energy Storage of Series-Hybrid Propelled Aircraft by Means of Integer Differential Evolution |
title_full_unstemmed | Optimization of the Energy Storage of Series-Hybrid Propelled Aircraft by Means of Integer Differential Evolution |
title_short | Optimization of the Energy Storage of Series-Hybrid Propelled Aircraft by Means of Integer Differential Evolution |
title_sort | optimization of the energy storage of series hybrid propelled aircraft by means of integer differential evolution |
topic | battery differential evolution electric propulsion hybrid electric aircraft optimization |
url | https://www.mdpi.com/2226-4310/6/5/59 |
work_keys_str_mv | AT liviusevastianbocii optimizationoftheenergystorageofserieshybridpropelledaircraftbymeansofintegerdifferentialevolution AT luigipiodinoia optimizationoftheenergystorageofserieshybridpropelledaircraftbymeansofintegerdifferentialevolution AT renatorizzo optimizationoftheenergystorageofserieshybridpropelledaircraftbymeansofintegerdifferentialevolution |