Multiport Driving Topology for a Photovoltaic Aircraft Light Transmission System Driven by Switched Reluctance Motors

In order to meet the working requirements of high performance and low cost for a photovoltaic (PV) aircraft driven by switched reluctance motors (SRMs), a multiport driving topology (MDT) is proposed. The converter is composed of an asymmetric half-bridge and a multiport power source circuit. Three...
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Autor*in:	Xiaoshu Zan [verfasserIn] Wenyuan Zhang [verfasserIn] Kai Ni [verfasserIn] Zhikai Jiang [verfasserIn] Yi Gong [verfasserIn]

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2020

Schlagwörter:	photovoltaic aircraft switched reluctance motors multiport power source circuit output torque efficiency excitation and demagnetization processes

Übergeordnetes Werk:	In: Energies - MDPI AG, 2008, 13(2020), 14, p 3687
Übergeordnetes Werk:	volume:13 ; year:2020 ; number:14, p 3687

Links:	Link aufrufen Link aufrufen Link aufrufen Journal toc

DOI / URN:	10.3390/en13143687

Katalog-ID:	DOAJ085639338

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520			\|a In order to meet the working requirements of high performance and low cost for a photovoltaic (PV) aircraft driven by switched reluctance motors (SRMs), a multiport driving topology (MDT) is proposed. The converter is composed of an asymmetric half-bridge and a multiport power source circuit. Three driving and two charging modes can be realized through simple control of the switches. The output torque and the efficiency of the system are improved, because the excitation and demagnetization processes are accelerated by increasing the commutation voltage. The battery pack can be self-charged when the system is running, and PV panels can be used to charge the battery pack to reduce energy consumption when the system is stationary. The simulation analysis and the experimental verification on an 8/6 SRM confirm the effectiveness of the MFT proposed in this paper.
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allfields	10.3390/en13143687 doi (DE-627)DOAJ085639338 (DE-599)DOAJ5f7487db0a29448b9321060f15b7fcd3 DE-627 ger DE-627 rakwb eng Xiaoshu Zan verfasserin aut Multiport Driving Topology for a Photovoltaic Aircraft Light Transmission System Driven by Switched Reluctance Motors 2020 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier In order to meet the working requirements of high performance and low cost for a photovoltaic (PV) aircraft driven by switched reluctance motors (SRMs), a multiport driving topology (MDT) is proposed. The converter is composed of an asymmetric half-bridge and a multiport power source circuit. Three driving and two charging modes can be realized through simple control of the switches. The output torque and the efficiency of the system are improved, because the excitation and demagnetization processes are accelerated by increasing the commutation voltage. The battery pack can be self-charged when the system is running, and PV panels can be used to charge the battery pack to reduce energy consumption when the system is stationary. The simulation analysis and the experimental verification on an 8/6 SRM confirm the effectiveness of the MFT proposed in this paper. photovoltaic aircraft switched reluctance motors multiport power source circuit output torque efficiency excitation and demagnetization processes Technology T Wenyuan Zhang verfasserin aut Kai Ni verfasserin aut Zhikai Jiang verfasserin aut Yi Gong verfasserin aut In Energies MDPI AG, 2008 13(2020), 14, p 3687 (DE-627)572083742 (DE-600)2437446-5 19961073 nnns volume:13 year:2020 number:14, p 3687 https://doi.org/10.3390/en13143687 kostenfrei https://doaj.org/article/5f7487db0a29448b9321060f15b7fcd3 kostenfrei https://www.mdpi.com/1996-1073/13/14/3687 kostenfrei https://doaj.org/toc/1996-1073 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_206 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2005 GBV_ILN_2009 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2055 GBV_ILN_2108 GBV_ILN_2111 GBV_ILN_2119 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 13 2020 14, p 3687
spelling	10.3390/en13143687 doi (DE-627)DOAJ085639338 (DE-599)DOAJ5f7487db0a29448b9321060f15b7fcd3 DE-627 ger DE-627 rakwb eng Xiaoshu Zan verfasserin aut Multiport Driving Topology for a Photovoltaic Aircraft Light Transmission System Driven by Switched Reluctance Motors 2020 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier In order to meet the working requirements of high performance and low cost for a photovoltaic (PV) aircraft driven by switched reluctance motors (SRMs), a multiport driving topology (MDT) is proposed. The converter is composed of an asymmetric half-bridge and a multiport power source circuit. Three driving and two charging modes can be realized through simple control of the switches. The output torque and the efficiency of the system are improved, because the excitation and demagnetization processes are accelerated by increasing the commutation voltage. The battery pack can be self-charged when the system is running, and PV panels can be used to charge the battery pack to reduce energy consumption when the system is stationary. The simulation analysis and the experimental verification on an 8/6 SRM confirm the effectiveness of the MFT proposed in this paper. photovoltaic aircraft switched reluctance motors multiport power source circuit output torque efficiency excitation and demagnetization processes Technology T Wenyuan Zhang verfasserin aut Kai Ni verfasserin aut Zhikai Jiang verfasserin aut Yi Gong verfasserin aut In Energies MDPI AG, 2008 13(2020), 14, p 3687 (DE-627)572083742 (DE-600)2437446-5 19961073 nnns volume:13 year:2020 number:14, p 3687 https://doi.org/10.3390/en13143687 kostenfrei https://doaj.org/article/5f7487db0a29448b9321060f15b7fcd3 kostenfrei https://www.mdpi.com/1996-1073/13/14/3687 kostenfrei https://doaj.org/toc/1996-1073 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_206 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2005 GBV_ILN_2009 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2055 GBV_ILN_2108 GBV_ILN_2111 GBV_ILN_2119 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 13 2020 14, p 3687
allfields_unstemmed	10.3390/en13143687 doi (DE-627)DOAJ085639338 (DE-599)DOAJ5f7487db0a29448b9321060f15b7fcd3 DE-627 ger DE-627 rakwb eng Xiaoshu Zan verfasserin aut Multiport Driving Topology for a Photovoltaic Aircraft Light Transmission System Driven by Switched Reluctance Motors 2020 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier In order to meet the working requirements of high performance and low cost for a photovoltaic (PV) aircraft driven by switched reluctance motors (SRMs), a multiport driving topology (MDT) is proposed. The converter is composed of an asymmetric half-bridge and a multiport power source circuit. Three driving and two charging modes can be realized through simple control of the switches. The output torque and the efficiency of the system are improved, because the excitation and demagnetization processes are accelerated by increasing the commutation voltage. The battery pack can be self-charged when the system is running, and PV panels can be used to charge the battery pack to reduce energy consumption when the system is stationary. The simulation analysis and the experimental verification on an 8/6 SRM confirm the effectiveness of the MFT proposed in this paper. photovoltaic aircraft switched reluctance motors multiport power source circuit output torque efficiency excitation and demagnetization processes Technology T Wenyuan Zhang verfasserin aut Kai Ni verfasserin aut Zhikai Jiang verfasserin aut Yi Gong verfasserin aut In Energies MDPI AG, 2008 13(2020), 14, p 3687 (DE-627)572083742 (DE-600)2437446-5 19961073 nnns volume:13 year:2020 number:14, p 3687 https://doi.org/10.3390/en13143687 kostenfrei https://doaj.org/article/5f7487db0a29448b9321060f15b7fcd3 kostenfrei https://www.mdpi.com/1996-1073/13/14/3687 kostenfrei https://doaj.org/toc/1996-1073 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_206 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2005 GBV_ILN_2009 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2055 GBV_ILN_2108 GBV_ILN_2111 GBV_ILN_2119 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 13 2020 14, p 3687
allfieldsGer	10.3390/en13143687 doi (DE-627)DOAJ085639338 (DE-599)DOAJ5f7487db0a29448b9321060f15b7fcd3 DE-627 ger DE-627 rakwb eng Xiaoshu Zan verfasserin aut Multiport Driving Topology for a Photovoltaic Aircraft Light Transmission System Driven by Switched Reluctance Motors 2020 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier In order to meet the working requirements of high performance and low cost for a photovoltaic (PV) aircraft driven by switched reluctance motors (SRMs), a multiport driving topology (MDT) is proposed. The converter is composed of an asymmetric half-bridge and a multiport power source circuit. Three driving and two charging modes can be realized through simple control of the switches. The output torque and the efficiency of the system are improved, because the excitation and demagnetization processes are accelerated by increasing the commutation voltage. The battery pack can be self-charged when the system is running, and PV panels can be used to charge the battery pack to reduce energy consumption when the system is stationary. The simulation analysis and the experimental verification on an 8/6 SRM confirm the effectiveness of the MFT proposed in this paper. photovoltaic aircraft switched reluctance motors multiport power source circuit output torque efficiency excitation and demagnetization processes Technology T Wenyuan Zhang verfasserin aut Kai Ni verfasserin aut Zhikai Jiang verfasserin aut Yi Gong verfasserin aut In Energies MDPI AG, 2008 13(2020), 14, p 3687 (DE-627)572083742 (DE-600)2437446-5 19961073 nnns volume:13 year:2020 number:14, p 3687 https://doi.org/10.3390/en13143687 kostenfrei https://doaj.org/article/5f7487db0a29448b9321060f15b7fcd3 kostenfrei https://www.mdpi.com/1996-1073/13/14/3687 kostenfrei https://doaj.org/toc/1996-1073 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_206 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2005 GBV_ILN_2009 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2055 GBV_ILN_2108 GBV_ILN_2111 GBV_ILN_2119 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 13 2020 14, p 3687
allfieldsSound	10.3390/en13143687 doi (DE-627)DOAJ085639338 (DE-599)DOAJ5f7487db0a29448b9321060f15b7fcd3 DE-627 ger DE-627 rakwb eng Xiaoshu Zan verfasserin aut Multiport Driving Topology for a Photovoltaic Aircraft Light Transmission System Driven by Switched Reluctance Motors 2020 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier In order to meet the working requirements of high performance and low cost for a photovoltaic (PV) aircraft driven by switched reluctance motors (SRMs), a multiport driving topology (MDT) is proposed. The converter is composed of an asymmetric half-bridge and a multiport power source circuit. Three driving and two charging modes can be realized through simple control of the switches. The output torque and the efficiency of the system are improved, because the excitation and demagnetization processes are accelerated by increasing the commutation voltage. The battery pack can be self-charged when the system is running, and PV panels can be used to charge the battery pack to reduce energy consumption when the system is stationary. The simulation analysis and the experimental verification on an 8/6 SRM confirm the effectiveness of the MFT proposed in this paper. photovoltaic aircraft switched reluctance motors multiport power source circuit output torque efficiency excitation and demagnetization processes Technology T Wenyuan Zhang verfasserin aut Kai Ni verfasserin aut Zhikai Jiang verfasserin aut Yi Gong verfasserin aut In Energies MDPI AG, 2008 13(2020), 14, p 3687 (DE-627)572083742 (DE-600)2437446-5 19961073 nnns volume:13 year:2020 number:14, p 3687 https://doi.org/10.3390/en13143687 kostenfrei https://doaj.org/article/5f7487db0a29448b9321060f15b7fcd3 kostenfrei https://www.mdpi.com/1996-1073/13/14/3687 kostenfrei https://doaj.org/toc/1996-1073 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_206 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2005 GBV_ILN_2009 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2055 GBV_ILN_2108 GBV_ILN_2111 GBV_ILN_2119 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 13 2020 14, p 3687
language	English
source	In Energies 13(2020), 14, p 3687 volume:13 year:2020 number:14, p 3687
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author	Xiaoshu Zan
spellingShingle	Xiaoshu Zan misc photovoltaic aircraft misc switched reluctance motors misc multiport power source circuit misc output torque misc efficiency misc excitation and demagnetization processes misc Technology misc T Multiport Driving Topology for a Photovoltaic Aircraft Light Transmission System Driven by Switched Reluctance Motors
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topic_title	Multiport Driving Topology for a Photovoltaic Aircraft Light Transmission System Driven by Switched Reluctance Motors photovoltaic aircraft switched reluctance motors multiport power source circuit output torque efficiency excitation and demagnetization processes
topic	misc photovoltaic aircraft misc switched reluctance motors misc multiport power source circuit misc output torque misc efficiency misc excitation and demagnetization processes misc Technology misc T
topic_unstemmed	misc photovoltaic aircraft misc switched reluctance motors misc multiport power source circuit misc output torque misc efficiency misc excitation and demagnetization processes misc Technology misc T
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title	Multiport Driving Topology for a Photovoltaic Aircraft Light Transmission System Driven by Switched Reluctance Motors
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title_full	Multiport Driving Topology for a Photovoltaic Aircraft Light Transmission System Driven by Switched Reluctance Motors
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title_sort	multiport driving topology for a photovoltaic aircraft light transmission system driven by switched reluctance motors
title_auth	Multiport Driving Topology for a Photovoltaic Aircraft Light Transmission System Driven by Switched Reluctance Motors
abstract	In order to meet the working requirements of high performance and low cost for a photovoltaic (PV) aircraft driven by switched reluctance motors (SRMs), a multiport driving topology (MDT) is proposed. The converter is composed of an asymmetric half-bridge and a multiport power source circuit. Three driving and two charging modes can be realized through simple control of the switches. The output torque and the efficiency of the system are improved, because the excitation and demagnetization processes are accelerated by increasing the commutation voltage. The battery pack can be self-charged when the system is running, and PV panels can be used to charge the battery pack to reduce energy consumption when the system is stationary. The simulation analysis and the experimental verification on an 8/6 SRM confirm the effectiveness of the MFT proposed in this paper.
abstractGer	In order to meet the working requirements of high performance and low cost for a photovoltaic (PV) aircraft driven by switched reluctance motors (SRMs), a multiport driving topology (MDT) is proposed. The converter is composed of an asymmetric half-bridge and a multiport power source circuit. Three driving and two charging modes can be realized through simple control of the switches. The output torque and the efficiency of the system are improved, because the excitation and demagnetization processes are accelerated by increasing the commutation voltage. The battery pack can be self-charged when the system is running, and PV panels can be used to charge the battery pack to reduce energy consumption when the system is stationary. The simulation analysis and the experimental verification on an 8/6 SRM confirm the effectiveness of the MFT proposed in this paper.
abstract_unstemmed	In order to meet the working requirements of high performance and low cost for a photovoltaic (PV) aircraft driven by switched reluctance motors (SRMs), a multiport driving topology (MDT) is proposed. The converter is composed of an asymmetric half-bridge and a multiport power source circuit. Three driving and two charging modes can be realized through simple control of the switches. The output torque and the efficiency of the system are improved, because the excitation and demagnetization processes are accelerated by increasing the commutation voltage. The battery pack can be self-charged when the system is running, and PV panels can be used to charge the battery pack to reduce energy consumption when the system is stationary. The simulation analysis and the experimental verification on an 8/6 SRM confirm the effectiveness of the MFT proposed in this paper.
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container_issue	14, p 3687
title_short	Multiport Driving Topology for a Photovoltaic Aircraft Light Transmission System Driven by Switched Reluctance Motors
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