Design and application of optimum toroidal shaped electromagnetic energy harvesters for unmanned aerial vehicles
This study presents the design and implementation of electromagnetic energy harvesters for the purpose of charging unmanned aerial vehicles (UAVs) battery. In the study, the designed harvesters are analyzed through finite element method (FEM) simulations. In the FEM analysis, common and self‐inducta...
Gespeichert in:
Veröffentlicht in: | International journal of numerical modelling 2024-05, Vol.37 (3), p.n/a |
---|---|
Hauptverfasser: | , |
Format: | Artikel |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | n/a |
---|---|
container_issue | 3 |
container_start_page | |
container_title | International journal of numerical modelling |
container_volume | 37 |
creator | Balcı, M. Şamil Dalcalı, Adem |
description | This study presents the design and implementation of electromagnetic energy harvesters for the purpose of charging unmanned aerial vehicles (UAVs) battery. In the study, the designed harvesters are analyzed through finite element method (FEM) simulations. In the FEM analysis, common and self‐inductance values, as well as magnetic flux density values of the harvesters, are calculated at specific current values. Inductance values are also theoretically calculated for comparison. Subsequently, an experimental setup is established to test the designed harvesters. After winding the core, the induced voltage and the power transferred to the load by the harvesters are measured. Curve fitting is performed after the measurements with different load resistances to find the maximum power transferred to the load. Through curve fitting, the maximum power obtained at each current value and at which load resistance this power is harvested are determined. Considering the intention of using the designed cores to charge UAVs and the importance of weight in UAV flight, the weights of each core, both without winding and after winding, are measured, and their costs are calculated. Taking all these criteria into account, the performance of the harvesters is demonstrated, and those among the used cores that are the most suitable for UAVs are identified in the study. |
doi_str_mv | 10.1002/jnm.3260 |
format | Article |
fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_3069011385</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>3069011385</sourcerecordid><originalsourceid>FETCH-LOGICAL-c1840-7209359485a4d576efd3b7c6e25f3b79ad6d024f606bd58a1eacc2cc970bdf733</originalsourceid><addsrcrecordid>eNp10DtPwzAQB3ALgUQpSHwESywsKec4zxGVtwosMFuufW5dJXawk6J-e1LKynQ3_O6hPyGXDGYMIL3ZuHbG0wKOyIRBXScsheyYTKCqs4TzEk7JWYwbAOAsTyeku8NoV45Kp6nsusYq2VvvqDfUd71th5b2PnirZUPjWnaoKTao-uBbuXLYW0XRYVjt6FqGLcYeQ6TGBzq4Vjo3conBjsNbXFvVYDwnJ0Y2ES_-6pR8Ptx_zJ-Sxfvj8_x2kShWZZCUKdQ8r7Mql5nOywKN5stSFZjmZmxqqQsNaWYKKJY6ryRDqVSqVF3CUpuS8ym5Ouztgv8axsfExg_BjScFh6IGxniVj-r6oFTwMQY0ogu2lWEnGIh9nmLMU-zzHGlyoN-2wd2_Try8vf76H6uQeNU</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>3069011385</pqid></control><display><type>article</type><title>Design and application of optimum toroidal shaped electromagnetic energy harvesters for unmanned aerial vehicles</title><source>Wiley Online Library All Journals</source><creator>Balcı, M. Şamil ; Dalcalı, Adem</creator><creatorcontrib>Balcı, M. Şamil ; Dalcalı, Adem</creatorcontrib><description>This study presents the design and implementation of electromagnetic energy harvesters for the purpose of charging unmanned aerial vehicles (UAVs) battery. In the study, the designed harvesters are analyzed through finite element method (FEM) simulations. In the FEM analysis, common and self‐inductance values, as well as magnetic flux density values of the harvesters, are calculated at specific current values. Inductance values are also theoretically calculated for comparison. Subsequently, an experimental setup is established to test the designed harvesters. After winding the core, the induced voltage and the power transferred to the load by the harvesters are measured. Curve fitting is performed after the measurements with different load resistances to find the maximum power transferred to the load. Through curve fitting, the maximum power obtained at each current value and at which load resistance this power is harvested are determined. Considering the intention of using the designed cores to charge UAVs and the importance of weight in UAV flight, the weights of each core, both without winding and after winding, are measured, and their costs are calculated. Taking all these criteria into account, the performance of the harvesters is demonstrated, and those among the used cores that are the most suitable for UAVs are identified in the study.</description><identifier>ISSN: 0894-3370</identifier><identifier>EISSN: 1099-1204</identifier><identifier>DOI: 10.1002/jnm.3260</identifier><language>eng</language><publisher>Chichester, UK: John Wiley & Sons, Inc</publisher><subject>Curve fitting ; Design ; Energy harvesting ; finite element analysis ; Finite element method ; Flux density ; Induced voltage ; Inductance ; Load resistance ; Magnetic flux ; Maximum power ; toroidal core ; Unmanned aerial vehicles ; Winding</subject><ispartof>International journal of numerical modelling, 2024-05, Vol.37 (3), p.n/a</ispartof><rights>2024 John Wiley & Sons Ltd.</rights><rights>2024 John Wiley & Sons, Ltd.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c1840-7209359485a4d576efd3b7c6e25f3b79ad6d024f606bd58a1eacc2cc970bdf733</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://onlinelibrary.wiley.com/doi/pdf/10.1002%2Fjnm.3260$$EPDF$$P50$$Gwiley$$H</linktopdf><linktohtml>$$Uhttps://onlinelibrary.wiley.com/doi/full/10.1002%2Fjnm.3260$$EHTML$$P50$$Gwiley$$H</linktohtml><link.rule.ids>314,780,784,1416,27923,27924,45573,45574</link.rule.ids></links><search><creatorcontrib>Balcı, M. Şamil</creatorcontrib><creatorcontrib>Dalcalı, Adem</creatorcontrib><title>Design and application of optimum toroidal shaped electromagnetic energy harvesters for unmanned aerial vehicles</title><title>International journal of numerical modelling</title><description>This study presents the design and implementation of electromagnetic energy harvesters for the purpose of charging unmanned aerial vehicles (UAVs) battery. In the study, the designed harvesters are analyzed through finite element method (FEM) simulations. In the FEM analysis, common and self‐inductance values, as well as magnetic flux density values of the harvesters, are calculated at specific current values. Inductance values are also theoretically calculated for comparison. Subsequently, an experimental setup is established to test the designed harvesters. After winding the core, the induced voltage and the power transferred to the load by the harvesters are measured. Curve fitting is performed after the measurements with different load resistances to find the maximum power transferred to the load. Through curve fitting, the maximum power obtained at each current value and at which load resistance this power is harvested are determined. Considering the intention of using the designed cores to charge UAVs and the importance of weight in UAV flight, the weights of each core, both without winding and after winding, are measured, and their costs are calculated. Taking all these criteria into account, the performance of the harvesters is demonstrated, and those among the used cores that are the most suitable for UAVs are identified in the study.</description><subject>Curve fitting</subject><subject>Design</subject><subject>Energy harvesting</subject><subject>finite element analysis</subject><subject>Finite element method</subject><subject>Flux density</subject><subject>Induced voltage</subject><subject>Inductance</subject><subject>Load resistance</subject><subject>Magnetic flux</subject><subject>Maximum power</subject><subject>toroidal core</subject><subject>Unmanned aerial vehicles</subject><subject>Winding</subject><issn>0894-3370</issn><issn>1099-1204</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2024</creationdate><recordtype>article</recordtype><recordid>eNp10DtPwzAQB3ALgUQpSHwESywsKec4zxGVtwosMFuufW5dJXawk6J-e1LKynQ3_O6hPyGXDGYMIL3ZuHbG0wKOyIRBXScsheyYTKCqs4TzEk7JWYwbAOAsTyeku8NoV45Kp6nsusYq2VvvqDfUd71th5b2PnirZUPjWnaoKTao-uBbuXLYW0XRYVjt6FqGLcYeQ6TGBzq4Vjo3conBjsNbXFvVYDwnJ0Y2ES_-6pR8Ptx_zJ-Sxfvj8_x2kShWZZCUKdQ8r7Mql5nOywKN5stSFZjmZmxqqQsNaWYKKJY6ryRDqVSqVF3CUpuS8ym5Ouztgv8axsfExg_BjScFh6IGxniVj-r6oFTwMQY0ogu2lWEnGIh9nmLMU-zzHGlyoN-2wd2_Try8vf76H6uQeNU</recordid><startdate>202405</startdate><enddate>202405</enddate><creator>Balcı, M. Şamil</creator><creator>Dalcalı, Adem</creator><general>John Wiley & Sons, Inc</general><general>Wiley Subscription Services, Inc</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SC</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>JQ2</scope><scope>KR7</scope><scope>L7M</scope><scope>L~C</scope><scope>L~D</scope></search><sort><creationdate>202405</creationdate><title>Design and application of optimum toroidal shaped electromagnetic energy harvesters for unmanned aerial vehicles</title><author>Balcı, M. Şamil ; Dalcalı, Adem</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c1840-7209359485a4d576efd3b7c6e25f3b79ad6d024f606bd58a1eacc2cc970bdf733</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2024</creationdate><topic>Curve fitting</topic><topic>Design</topic><topic>Energy harvesting</topic><topic>finite element analysis</topic><topic>Finite element method</topic><topic>Flux density</topic><topic>Induced voltage</topic><topic>Inductance</topic><topic>Load resistance</topic><topic>Magnetic flux</topic><topic>Maximum power</topic><topic>toroidal core</topic><topic>Unmanned aerial vehicles</topic><topic>Winding</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Balcı, M. Şamil</creatorcontrib><creatorcontrib>Dalcalı, Adem</creatorcontrib><collection>CrossRef</collection><collection>Computer and Information Systems Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>ProQuest Computer Science Collection</collection><collection>Civil Engineering Abstracts</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Computer and Information Systems Abstracts Academic</collection><collection>Computer and Information Systems Abstracts Professional</collection><jtitle>International journal of numerical modelling</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Balcı, M. Şamil</au><au>Dalcalı, Adem</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Design and application of optimum toroidal shaped electromagnetic energy harvesters for unmanned aerial vehicles</atitle><jtitle>International journal of numerical modelling</jtitle><date>2024-05</date><risdate>2024</risdate><volume>37</volume><issue>3</issue><epage>n/a</epage><issn>0894-3370</issn><eissn>1099-1204</eissn><abstract>This study presents the design and implementation of electromagnetic energy harvesters for the purpose of charging unmanned aerial vehicles (UAVs) battery. In the study, the designed harvesters are analyzed through finite element method (FEM) simulations. In the FEM analysis, common and self‐inductance values, as well as magnetic flux density values of the harvesters, are calculated at specific current values. Inductance values are also theoretically calculated for comparison. Subsequently, an experimental setup is established to test the designed harvesters. After winding the core, the induced voltage and the power transferred to the load by the harvesters are measured. Curve fitting is performed after the measurements with different load resistances to find the maximum power transferred to the load. Through curve fitting, the maximum power obtained at each current value and at which load resistance this power is harvested are determined. Considering the intention of using the designed cores to charge UAVs and the importance of weight in UAV flight, the weights of each core, both without winding and after winding, are measured, and their costs are calculated. Taking all these criteria into account, the performance of the harvesters is demonstrated, and those among the used cores that are the most suitable for UAVs are identified in the study.</abstract><cop>Chichester, UK</cop><pub>John Wiley & Sons, Inc</pub><doi>10.1002/jnm.3260</doi><tpages>21</tpages></addata></record> |
fulltext | fulltext |
identifier | ISSN: 0894-3370 |
ispartof | International journal of numerical modelling, 2024-05, Vol.37 (3), p.n/a |
issn | 0894-3370 1099-1204 |
language | eng |
recordid | cdi_proquest_journals_3069011385 |
source | Wiley Online Library All Journals |
subjects | Curve fitting Design Energy harvesting finite element analysis Finite element method Flux density Induced voltage Inductance Load resistance Magnetic flux Maximum power toroidal core Unmanned aerial vehicles Winding |
title | Design and application of optimum toroidal shaped electromagnetic energy harvesters for unmanned aerial vehicles |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-12T18%3A26%3A45IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Design%20and%20application%20of%20optimum%20toroidal%20shaped%20electromagnetic%20energy%20harvesters%20for%20unmanned%20aerial%20vehicles&rft.jtitle=International%20journal%20of%20numerical%20modelling&rft.au=Balc%C4%B1,%20M.%20%C5%9Eamil&rft.date=2024-05&rft.volume=37&rft.issue=3&rft.epage=n/a&rft.issn=0894-3370&rft.eissn=1099-1204&rft_id=info:doi/10.1002/jnm.3260&rft_dat=%3Cproquest_cross%3E3069011385%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=3069011385&rft_id=info:pmid/&rfr_iscdi=true |