Induction Heating Characteristics of Electroless Ni-Coated CFRP for Deicing and Anti-Icing
Ice accumulation on the surface of aircraft is a serious threat to flight safety and a fatal factor causing air accidents. However, traditional aircraft deicing methods no longer meet the requirements of safe flight due to changes in aircraft structural materials. In recent years, the application of...
Gespeichert in:
| Veröffentlicht in: | Coatings (Basel) 2023-09, Vol.13 (9), p.1531 |
|---|---|
| Hauptverfasser: | , , , , |
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | |
|---|---|
| container_issue | 9 |
| container_start_page | 1531 |
| container_title | Coatings (Basel) |
| container_volume | 13 |
| creator | Pang, Jie Qin, Wenfeng You, Wentao Zhong, Mian Meng, Qing’an |
| description | Ice accumulation on the surface of aircraft is a serious threat to flight safety and a fatal factor causing air accidents. However, traditional aircraft deicing methods no longer meet the requirements of safe flight due to changes in aircraft structural materials. In recent years, the application of carbon fiber-reinforced polymer (CFRP) materials in the aviation structure industry has increased. In this study, we demonstrate an economical, easy-to-prepare, and pollution-free approach to deice an aircraft through induction heating. The nickel-coated carbon fiber-reinforced polymer used as the induction heater for aircraft deicing is obtained by electroless nickel plating on the surface of the CFRP. The result shows that it takes just 110 s to achieve a temperature of 205 °C on the nickel-plated CFRP when the input voltage is 30 V, as well as melting the ice layer with a thickness of 30 mm, while the temperature of this material can reach up to 81 °C by electric heating when the input voltage is 1.5 V. Meanwhile, the nickel-plated CFRP exhibits good repeatability during the induction heating. Based on the excellent electrothermal properties, the nickel-plated CFRP polymer shows a prominent deicing ability, which provides a promising strategy for the deicing of aircraft. |
| doi_str_mv | 10.3390/coatings13091531 |
| format | Article |
| fullrecord | <record><control><sourceid>gale_proqu</sourceid><recordid>TN_cdi_proquest_journals_2869295896</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><galeid>A768249976</galeid><sourcerecordid>A768249976</sourcerecordid><originalsourceid>FETCH-LOGICAL-c352t-c12ac6673b8b714df7d817c4b297f7f5e1ac694e9451ee62c825d466333854553</originalsourceid><addsrcrecordid>eNpdUE1LAzEQDaJgqb17DHjeuvlOjmVtbUFURC9elm02qSltUpP04L83az2IM4f5fG-YB8A1qqeEqPpWhy47v0mI1Aoxgs7ACNdCVZwifP4nvwSTlLZ1MYWIRGoE3le-P-rsgodL80MCm48udjqb6FJ2OsFg4XxndI5hZ1KCj65qyjnTw2bx8gxtiPDOOD0gO9_Dmc-uWg3lFbiw3S6ZyW8cg7fF_LVZVg9P96tm9lBpwnCuNMKd5lyQtVwLRHsreomEpmushBWWGVTGihpFGTKGYy0x6ynnhBDJKGNkDG5OvIcYPo8m5XYbjtGXky2WXGHFpOJla3ra2nQ70zpvQy5fFu_N3ungjXWlPxNcYqqUGAD1CaBjSCka2x6i23fxq0V1O6je_ledfAO2SnUe</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2869295896</pqid></control><display><type>article</type><title>Induction Heating Characteristics of Electroless Ni-Coated CFRP for Deicing and Anti-Icing</title><source>Elektronische Zeitschriftenbibliothek - Frei zugängliche E-Journals</source><source>MDPI - Multidisciplinary Digital Publishing Institute</source><source>Alma/SFX Local Collection</source><creator>Pang, Jie ; Qin, Wenfeng ; You, Wentao ; Zhong, Mian ; Meng, Qing’an</creator><creatorcontrib>Pang, Jie ; Qin, Wenfeng ; You, Wentao ; Zhong, Mian ; Meng, Qing’an</creatorcontrib><description>Ice accumulation on the surface of aircraft is a serious threat to flight safety and a fatal factor causing air accidents. However, traditional aircraft deicing methods no longer meet the requirements of safe flight due to changes in aircraft structural materials. In recent years, the application of carbon fiber-reinforced polymer (CFRP) materials in the aviation structure industry has increased. In this study, we demonstrate an economical, easy-to-prepare, and pollution-free approach to deice an aircraft through induction heating. The nickel-coated carbon fiber-reinforced polymer used as the induction heater for aircraft deicing is obtained by electroless nickel plating on the surface of the CFRP. The result shows that it takes just 110 s to achieve a temperature of 205 °C on the nickel-plated CFRP when the input voltage is 30 V, as well as melting the ice layer with a thickness of 30 mm, while the temperature of this material can reach up to 81 °C by electric heating when the input voltage is 1.5 V. Meanwhile, the nickel-plated CFRP exhibits good repeatability during the induction heating. Based on the excellent electrothermal properties, the nickel-plated CFRP polymer shows a prominent deicing ability, which provides a promising strategy for the deicing of aircraft.</description><identifier>ISSN: 2079-6412</identifier><identifier>EISSN: 2079-6412</identifier><identifier>DOI: 10.3390/coatings13091531</identifier><language>eng</language><publisher>Basel: MDPI AG</publisher><subject>Aircraft accidents & safety ; Alloys ; Aluminum ; Aviation ; Carbon fiber reinforced plastics ; Carbon fiber reinforcement ; Coated fibers ; Composite materials ; Contact angle ; Deicing ; Efficiency ; Electric heating ; Electric potential ; Electroless nickel plating ; Energy consumption ; Epoxy resins ; Fiber reinforced polymers ; Flight safety ; Flying-machines ; Graphene ; Hydrophobic surfaces ; Ice accumulation ; Ice cover ; Induction heating ; Morphology ; Nickel ; Scanning electron microscopy ; Temperature ; Thickness ; Voltage</subject><ispartof>Coatings (Basel), 2023-09, Vol.13 (9), p.1531</ispartof><rights>COPYRIGHT 2023 MDPI AG</rights><rights>2023 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https://creativecommons.org/licenses/by/4.0/). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c352t-c12ac6673b8b714df7d817c4b297f7f5e1ac694e9451ee62c825d466333854553</citedby><cites>FETCH-LOGICAL-c352t-c12ac6673b8b714df7d817c4b297f7f5e1ac694e9451ee62c825d466333854553</cites><orcidid>0009-0006-0183-8077 ; 0000-0001-8614-7668</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>315,781,785,27929,27930</link.rule.ids></links><search><creatorcontrib>Pang, Jie</creatorcontrib><creatorcontrib>Qin, Wenfeng</creatorcontrib><creatorcontrib>You, Wentao</creatorcontrib><creatorcontrib>Zhong, Mian</creatorcontrib><creatorcontrib>Meng, Qing’an</creatorcontrib><title>Induction Heating Characteristics of Electroless Ni-Coated CFRP for Deicing and Anti-Icing</title><title>Coatings (Basel)</title><description>Ice accumulation on the surface of aircraft is a serious threat to flight safety and a fatal factor causing air accidents. However, traditional aircraft deicing methods no longer meet the requirements of safe flight due to changes in aircraft structural materials. In recent years, the application of carbon fiber-reinforced polymer (CFRP) materials in the aviation structure industry has increased. In this study, we demonstrate an economical, easy-to-prepare, and pollution-free approach to deice an aircraft through induction heating. The nickel-coated carbon fiber-reinforced polymer used as the induction heater for aircraft deicing is obtained by electroless nickel plating on the surface of the CFRP. The result shows that it takes just 110 s to achieve a temperature of 205 °C on the nickel-plated CFRP when the input voltage is 30 V, as well as melting the ice layer with a thickness of 30 mm, while the temperature of this material can reach up to 81 °C by electric heating when the input voltage is 1.5 V. Meanwhile, the nickel-plated CFRP exhibits good repeatability during the induction heating. Based on the excellent electrothermal properties, the nickel-plated CFRP polymer shows a prominent deicing ability, which provides a promising strategy for the deicing of aircraft.</description><subject>Aircraft accidents & safety</subject><subject>Alloys</subject><subject>Aluminum</subject><subject>Aviation</subject><subject>Carbon fiber reinforced plastics</subject><subject>Carbon fiber reinforcement</subject><subject>Coated fibers</subject><subject>Composite materials</subject><subject>Contact angle</subject><subject>Deicing</subject><subject>Efficiency</subject><subject>Electric heating</subject><subject>Electric potential</subject><subject>Electroless nickel plating</subject><subject>Energy consumption</subject><subject>Epoxy resins</subject><subject>Fiber reinforced polymers</subject><subject>Flight safety</subject><subject>Flying-machines</subject><subject>Graphene</subject><subject>Hydrophobic surfaces</subject><subject>Ice accumulation</subject><subject>Ice cover</subject><subject>Induction heating</subject><subject>Morphology</subject><subject>Nickel</subject><subject>Scanning electron microscopy</subject><subject>Temperature</subject><subject>Thickness</subject><subject>Voltage</subject><issn>2079-6412</issn><issn>2079-6412</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2023</creationdate><recordtype>article</recordtype><sourceid>ABUWG</sourceid><sourceid>AFKRA</sourceid><sourceid>AZQEC</sourceid><sourceid>BENPR</sourceid><sourceid>CCPQU</sourceid><sourceid>DWQXO</sourceid><recordid>eNpdUE1LAzEQDaJgqb17DHjeuvlOjmVtbUFURC9elm02qSltUpP04L83az2IM4f5fG-YB8A1qqeEqPpWhy47v0mI1Aoxgs7ACNdCVZwifP4nvwSTlLZ1MYWIRGoE3le-P-rsgodL80MCm48udjqb6FJ2OsFg4XxndI5hZ1KCj65qyjnTw2bx8gxtiPDOOD0gO9_Dmc-uWg3lFbiw3S6ZyW8cg7fF_LVZVg9P96tm9lBpwnCuNMKd5lyQtVwLRHsreomEpmushBWWGVTGihpFGTKGYy0x6ynnhBDJKGNkDG5OvIcYPo8m5XYbjtGXky2WXGHFpOJla3ra2nQ70zpvQy5fFu_N3ungjXWlPxNcYqqUGAD1CaBjSCka2x6i23fxq0V1O6je_ledfAO2SnUe</recordid><startdate>20230901</startdate><enddate>20230901</enddate><creator>Pang, Jie</creator><creator>Qin, Wenfeng</creator><creator>You, Wentao</creator><creator>Zhong, Mian</creator><creator>Meng, Qing’an</creator><general>MDPI AG</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>8BQ</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>ABJCF</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>D1I</scope><scope>DWQXO</scope><scope>HCIFZ</scope><scope>JG9</scope><scope>KB.</scope><scope>PDBOC</scope><scope>PIMPY</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><orcidid>https://orcid.org/0009-0006-0183-8077</orcidid><orcidid>https://orcid.org/0000-0001-8614-7668</orcidid></search><sort><creationdate>20230901</creationdate><title>Induction Heating Characteristics of Electroless Ni-Coated CFRP for Deicing and Anti-Icing</title><author>Pang, Jie ; Qin, Wenfeng ; You, Wentao ; Zhong, Mian ; Meng, Qing’an</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c352t-c12ac6673b8b714df7d817c4b297f7f5e1ac694e9451ee62c825d466333854553</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2023</creationdate><topic>Aircraft accidents & safety</topic><topic>Alloys</topic><topic>Aluminum</topic><topic>Aviation</topic><topic>Carbon fiber reinforced plastics</topic><topic>Carbon fiber reinforcement</topic><topic>Coated fibers</topic><topic>Composite materials</topic><topic>Contact angle</topic><topic>Deicing</topic><topic>Efficiency</topic><topic>Electric heating</topic><topic>Electric potential</topic><topic>Electroless nickel plating</topic><topic>Energy consumption</topic><topic>Epoxy resins</topic><topic>Fiber reinforced polymers</topic><topic>Flight safety</topic><topic>Flying-machines</topic><topic>Graphene</topic><topic>Hydrophobic surfaces</topic><topic>Ice accumulation</topic><topic>Ice cover</topic><topic>Induction heating</topic><topic>Morphology</topic><topic>Nickel</topic><topic>Scanning electron microscopy</topic><topic>Temperature</topic><topic>Thickness</topic><topic>Voltage</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Pang, Jie</creatorcontrib><creatorcontrib>Qin, Wenfeng</creatorcontrib><creatorcontrib>You, Wentao</creatorcontrib><creatorcontrib>Zhong, Mian</creatorcontrib><creatorcontrib>Meng, Qing’an</creatorcontrib><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>Materials Science & Engineering Collection</collection><collection>ProQuest Central (Alumni Edition)</collection><collection>ProQuest Central UK/Ireland</collection><collection>ProQuest Central Essentials</collection><collection>ProQuest Central</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Materials Science Collection</collection><collection>ProQuest Central Korea</collection><collection>SciTech Premium Collection</collection><collection>Materials Research Database</collection><collection>Materials Science Database</collection><collection>Materials Science Collection</collection><collection>Access via ProQuest (Open Access)</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><jtitle>Coatings (Basel)</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Pang, Jie</au><au>Qin, Wenfeng</au><au>You, Wentao</au><au>Zhong, Mian</au><au>Meng, Qing’an</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Induction Heating Characteristics of Electroless Ni-Coated CFRP for Deicing and Anti-Icing</atitle><jtitle>Coatings (Basel)</jtitle><date>2023-09-01</date><risdate>2023</risdate><volume>13</volume><issue>9</issue><spage>1531</spage><pages>1531-</pages><issn>2079-6412</issn><eissn>2079-6412</eissn><abstract>Ice accumulation on the surface of aircraft is a serious threat to flight safety and a fatal factor causing air accidents. However, traditional aircraft deicing methods no longer meet the requirements of safe flight due to changes in aircraft structural materials. In recent years, the application of carbon fiber-reinforced polymer (CFRP) materials in the aviation structure industry has increased. In this study, we demonstrate an economical, easy-to-prepare, and pollution-free approach to deice an aircraft through induction heating. The nickel-coated carbon fiber-reinforced polymer used as the induction heater for aircraft deicing is obtained by electroless nickel plating on the surface of the CFRP. The result shows that it takes just 110 s to achieve a temperature of 205 °C on the nickel-plated CFRP when the input voltage is 30 V, as well as melting the ice layer with a thickness of 30 mm, while the temperature of this material can reach up to 81 °C by electric heating when the input voltage is 1.5 V. Meanwhile, the nickel-plated CFRP exhibits good repeatability during the induction heating. Based on the excellent electrothermal properties, the nickel-plated CFRP polymer shows a prominent deicing ability, which provides a promising strategy for the deicing of aircraft.</abstract><cop>Basel</cop><pub>MDPI AG</pub><doi>10.3390/coatings13091531</doi><orcidid>https://orcid.org/0009-0006-0183-8077</orcidid><orcidid>https://orcid.org/0000-0001-8614-7668</orcidid><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 2079-6412 |
| ispartof | Coatings (Basel), 2023-09, Vol.13 (9), p.1531 |
| issn | 2079-6412 2079-6412 |
| language | eng |
| recordid | cdi_proquest_journals_2869295896 |
| source | Elektronische Zeitschriftenbibliothek - Frei zugängliche E-Journals; MDPI - Multidisciplinary Digital Publishing Institute; Alma/SFX Local Collection |
| subjects | Aircraft accidents & safety Alloys Aluminum Aviation Carbon fiber reinforced plastics Carbon fiber reinforcement Coated fibers Composite materials Contact angle Deicing Efficiency Electric heating Electric potential Electroless nickel plating Energy consumption Epoxy resins Fiber reinforced polymers Flight safety Flying-machines Graphene Hydrophobic surfaces Ice accumulation Ice cover Induction heating Morphology Nickel Scanning electron microscopy Temperature Thickness Voltage |
| title | Induction Heating Characteristics of Electroless Ni-Coated CFRP for Deicing and Anti-Icing |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-12T18%3A24%3A15IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-gale_proqu&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Induction%20Heating%20Characteristics%20of%20Electroless%20Ni-Coated%20CFRP%20for%20Deicing%20and%20Anti-Icing&rft.jtitle=Coatings%20(Basel)&rft.au=Pang,%20Jie&rft.date=2023-09-01&rft.volume=13&rft.issue=9&rft.spage=1531&rft.pages=1531-&rft.issn=2079-6412&rft.eissn=2079-6412&rft_id=info:doi/10.3390/coatings13091531&rft_dat=%3Cgale_proqu%3EA768249976%3C/gale_proqu%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=2869295896&rft_id=info:pmid/&rft_galeid=A768249976&rfr_iscdi=true |