Multi-Objective Optimization for Improving Weight and Fault Characteristics of a DC HTS Cable in Cryo-Electric Aircraft

The aim of the presented study is to optimize the different classes of high-temperature superconducting (HTS) DC cables for improving their performances in a cryo-electric aircraft considering their weight, peak temperature during faults, and the ratio of current passing through each tape to the cri...

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Main Authors: Alireza Sadeghi, Mohammad Yazdani-Asrami
Format: Article
Language:English
Published: MDPI AG 2022-11-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/9/12/753
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author Alireza Sadeghi
Mohammad Yazdani-Asrami
author_facet Alireza Sadeghi
Mohammad Yazdani-Asrami
author_sort Alireza Sadeghi
collection DOAJ
description The aim of the presented study is to optimize the different classes of high-temperature superconducting (HTS) DC cables for improving their performances in a cryo-electric aircraft considering their weight, peak temperature during faults, and the ratio of current passing through each tape to the critical current of HTS tapes. These terms were interpreted into three objective functions, and a multi-objective optimization algorithm known as non-dominated sorting genetic algorithm II was used to find the optimal solution clusters. The cable optimization was conducted for different former materials by changing the former thickness and radius. Results showed that the DC HTS cables with aluminum former have the lowest weight while cables with copper formers have the best thermal performance against faults.
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spelling doaj.art-c858899b58a04290ae2e5b39701aabb72023-11-24T12:37:25ZengMDPI AGAerospace2226-43102022-11-0191275310.3390/aerospace9120753Multi-Objective Optimization for Improving Weight and Fault Characteristics of a DC HTS Cable in Cryo-Electric AircraftAlireza Sadeghi0Mohammad Yazdani-Asrami1Department of Electrical Engineering, Shahrood University of Technology, Shahrood 3619995161, IranPropulsion, Electrification & Superconductivity Group, James Watt School of Engineering, University of Glasgow, Glasgow G12 8QQ, UKThe aim of the presented study is to optimize the different classes of high-temperature superconducting (HTS) DC cables for improving their performances in a cryo-electric aircraft considering their weight, peak temperature during faults, and the ratio of current passing through each tape to the critical current of HTS tapes. These terms were interpreted into three objective functions, and a multi-objective optimization algorithm known as non-dominated sorting genetic algorithm II was used to find the optimal solution clusters. The cable optimization was conducted for different former materials by changing the former thickness and radius. Results showed that the DC HTS cables with aluminum former have the lowest weight while cables with copper formers have the best thermal performance against faults.https://www.mdpi.com/2226-4310/9/12/753aviationelectrificationcablelossheat capacityhigh temperature superconductor
spellingShingle Alireza Sadeghi
Mohammad Yazdani-Asrami
Multi-Objective Optimization for Improving Weight and Fault Characteristics of a DC HTS Cable in Cryo-Electric Aircraft
Aerospace
aviation
electrification
cable
loss
heat capacity
high temperature superconductor
title Multi-Objective Optimization for Improving Weight and Fault Characteristics of a DC HTS Cable in Cryo-Electric Aircraft
title_full Multi-Objective Optimization for Improving Weight and Fault Characteristics of a DC HTS Cable in Cryo-Electric Aircraft
title_fullStr Multi-Objective Optimization for Improving Weight and Fault Characteristics of a DC HTS Cable in Cryo-Electric Aircraft
title_full_unstemmed Multi-Objective Optimization for Improving Weight and Fault Characteristics of a DC HTS Cable in Cryo-Electric Aircraft
title_short Multi-Objective Optimization for Improving Weight and Fault Characteristics of a DC HTS Cable in Cryo-Electric Aircraft
title_sort multi objective optimization for improving weight and fault characteristics of a dc hts cable in cryo electric aircraft
topic aviation
electrification
cable
loss
heat capacity
high temperature superconductor
url https://www.mdpi.com/2226-4310/9/12/753
work_keys_str_mv AT alirezasadeghi multiobjectiveoptimizationforimprovingweightandfaultcharacteristicsofadchtscableincryoelectricaircraft
AT mohammadyazdaniasrami multiobjectiveoptimizationforimprovingweightandfaultcharacteristicsofadchtscableincryoelectricaircraft