Investigation of biogenic materials and ferroelectrets for energy harvesting on vibrating aircraft structures
In this publication the application of novel piezoelectric materials for energy harvesting on vibrating aircraft structures is investigated. These materials have significant advantages over conventional piezoelectric transducer materials like piezoceramics. In particular, biogenic materials in the f...
Gespeichert in:
| Veröffentlicht in: | CEAS aeronautical journal 2021-04, Vol.12 (2), p.331-344 |
|---|---|
| Hauptverfasser: | , , , , , |
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | 344 |
|---|---|
| container_issue | 2 |
| container_start_page | 331 |
| container_title | CEAS aeronautical journal |
| container_volume | 12 |
| creator | Holzmann, H. Weber, M. Park, Y. J. Perfetto, S. Atzrodt, H. Dafnis, A. |
| description | In this publication the application of novel piezoelectric materials for energy harvesting on vibrating aircraft structures is investigated. These materials have significant advantages over conventional piezoelectric transducer materials like piezoceramics. In particular, biogenic materials in the form of wood-based materials and ferroelectrets in the form of irradiation cross-linked polypropylene are the subject of the investigation. The material characterization in terms of mechanical and electromechanical properties is shown for both material types. For the wood materials a compression test is used as the material has load-bearing properties. The ferroelectrets provide high compliances and are therefore investigated in a tensile test for material characterisation as well as in a four-point flexural test regarding its behaviour when glued to a dynamically bending surface. Additionally an FE-model of the material model for ferroelectrets is presented, which is validated by experimental results. An estimation of the power output is given for different concepts with both kinds of materials. |
| doi_str_mv | 10.1007/s13272-021-00502-0 |
| format | Article |
| fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_2523981557</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>2523981557</sourcerecordid><originalsourceid>FETCH-LOGICAL-c2780-809d6ab351ebcf5f155994ba2cd21b8f95c0788acf71e22d3b7b9b96fb92f6da3</originalsourceid><addsrcrecordid>eNp9kM1OAyEUhYnRxEb7Aq5IXI8CU2ZgaRp_mjRxo2sCDIw0LdTLTJO-vdgxupMNh-Sc714OQjeU3FFC2vtMa9ayijBaEcJJUWdoRkUjK84lOf_Vgl2iec4bUk5D6gVfzNBuFQ8uD6HXQ0gRJ49NSL2LweKdHhwEvc1Yxw57B5Dc1tkB3JCxT4BddNAf8YeGEyL2uBAOwYA-PXQAC9oPOA8w2mEEl6_RhS9AN_-5r9D70-Pb8qVavz6vlg_ryrJWkEoQ2TXa1Jw6Yz33tPxDLoxmtmPUCC-5Ja0Q2vqWOsa62rRGGtl4I5lvOl1foduJu4f0OZbl1CaNEMtIxTirpSjEtrjY5LKQcgbn1R7CTsNRUaK-m1VTs6o0q07NKlJC9RTKxRx7B3_of1JfDvJ-SQ</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2523981557</pqid></control><display><type>article</type><title>Investigation of biogenic materials and ferroelectrets for energy harvesting on vibrating aircraft structures</title><source>SpringerNature Journals</source><creator>Holzmann, H. ; Weber, M. ; Park, Y. J. ; Perfetto, S. ; Atzrodt, H. ; Dafnis, A.</creator><creatorcontrib>Holzmann, H. ; Weber, M. ; Park, Y. J. ; Perfetto, S. ; Atzrodt, H. ; Dafnis, A.</creatorcontrib><description>In this publication the application of novel piezoelectric materials for energy harvesting on vibrating aircraft structures is investigated. These materials have significant advantages over conventional piezoelectric transducer materials like piezoceramics. In particular, biogenic materials in the form of wood-based materials and ferroelectrets in the form of irradiation cross-linked polypropylene are the subject of the investigation. The material characterization in terms of mechanical and electromechanical properties is shown for both material types. For the wood materials a compression test is used as the material has load-bearing properties. The ferroelectrets provide high compliances and are therefore investigated in a tensile test for material characterisation as well as in a four-point flexural test regarding its behaviour when glued to a dynamically bending surface. Additionally an FE-model of the material model for ferroelectrets is presented, which is validated by experimental results. An estimation of the power output is given for different concepts with both kinds of materials.</description><identifier>ISSN: 1869-5582</identifier><identifier>EISSN: 1869-5590</identifier><identifier>DOI: 10.1007/s13272-021-00502-0</identifier><language>eng</language><publisher>Vienna: Springer Vienna</publisher><subject>Aerospace Technology and Astronautics ; Aircraft ; Aircraft structures ; Aircraft vibration ; Compression tests ; Energy harvesting ; Engineering ; Investigations ; Mechanical properties ; Original Paper ; Piezoelectric ceramics ; Piezoelectric transducers ; Tensile tests</subject><ispartof>CEAS aeronautical journal, 2021-04, Vol.12 (2), p.331-344</ispartof><rights>The Author(s) 2021</rights><rights>The Author(s) 2021. This work is published under http://creativecommons.org/licenses/by/4.0/ (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c2780-809d6ab351ebcf5f155994ba2cd21b8f95c0788acf71e22d3b7b9b96fb92f6da3</citedby><cites>FETCH-LOGICAL-c2780-809d6ab351ebcf5f155994ba2cd21b8f95c0788acf71e22d3b7b9b96fb92f6da3</cites><orcidid>0000-0002-1485-5208</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://link.springer.com/content/pdf/10.1007/s13272-021-00502-0$$EPDF$$P50$$Gspringer$$Hfree_for_read</linktopdf><linktohtml>$$Uhttps://link.springer.com/10.1007/s13272-021-00502-0$$EHTML$$P50$$Gspringer$$Hfree_for_read</linktohtml><link.rule.ids>315,782,786,27931,27932,41495,42564,51326</link.rule.ids></links><search><creatorcontrib>Holzmann, H.</creatorcontrib><creatorcontrib>Weber, M.</creatorcontrib><creatorcontrib>Park, Y. J.</creatorcontrib><creatorcontrib>Perfetto, S.</creatorcontrib><creatorcontrib>Atzrodt, H.</creatorcontrib><creatorcontrib>Dafnis, A.</creatorcontrib><title>Investigation of biogenic materials and ferroelectrets for energy harvesting on vibrating aircraft structures</title><title>CEAS aeronautical journal</title><addtitle>CEAS Aeronaut J</addtitle><description>In this publication the application of novel piezoelectric materials for energy harvesting on vibrating aircraft structures is investigated. These materials have significant advantages over conventional piezoelectric transducer materials like piezoceramics. In particular, biogenic materials in the form of wood-based materials and ferroelectrets in the form of irradiation cross-linked polypropylene are the subject of the investigation. The material characterization in terms of mechanical and electromechanical properties is shown for both material types. For the wood materials a compression test is used as the material has load-bearing properties. The ferroelectrets provide high compliances and are therefore investigated in a tensile test for material characterisation as well as in a four-point flexural test regarding its behaviour when glued to a dynamically bending surface. Additionally an FE-model of the material model for ferroelectrets is presented, which is validated by experimental results. An estimation of the power output is given for different concepts with both kinds of materials.</description><subject>Aerospace Technology and Astronautics</subject><subject>Aircraft</subject><subject>Aircraft structures</subject><subject>Aircraft vibration</subject><subject>Compression tests</subject><subject>Energy harvesting</subject><subject>Engineering</subject><subject>Investigations</subject><subject>Mechanical properties</subject><subject>Original Paper</subject><subject>Piezoelectric ceramics</subject><subject>Piezoelectric transducers</subject><subject>Tensile tests</subject><issn>1869-5582</issn><issn>1869-5590</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2021</creationdate><recordtype>article</recordtype><sourceid>C6C</sourceid><recordid>eNp9kM1OAyEUhYnRxEb7Aq5IXI8CU2ZgaRp_mjRxo2sCDIw0LdTLTJO-vdgxupMNh-Sc714OQjeU3FFC2vtMa9ayijBaEcJJUWdoRkUjK84lOf_Vgl2iec4bUk5D6gVfzNBuFQ8uD6HXQ0gRJ49NSL2LweKdHhwEvc1Yxw57B5Dc1tkB3JCxT4BddNAf8YeGEyL2uBAOwYA-PXQAC9oPOA8w2mEEl6_RhS9AN_-5r9D70-Pb8qVavz6vlg_ryrJWkEoQ2TXa1Jw6Yz33tPxDLoxmtmPUCC-5Ja0Q2vqWOsa62rRGGtl4I5lvOl1foduJu4f0OZbl1CaNEMtIxTirpSjEtrjY5LKQcgbn1R7CTsNRUaK-m1VTs6o0q07NKlJC9RTKxRx7B3_of1JfDvJ-SQ</recordid><startdate>20210401</startdate><enddate>20210401</enddate><creator>Holzmann, H.</creator><creator>Weber, M.</creator><creator>Park, Y. J.</creator><creator>Perfetto, S.</creator><creator>Atzrodt, H.</creator><creator>Dafnis, A.</creator><general>Springer Vienna</general><general>Springer Nature B.V</general><scope>C6C</scope><scope>AAYXX</scope><scope>CITATION</scope><orcidid>https://orcid.org/0000-0002-1485-5208</orcidid></search><sort><creationdate>20210401</creationdate><title>Investigation of biogenic materials and ferroelectrets for energy harvesting on vibrating aircraft structures</title><author>Holzmann, H. ; Weber, M. ; Park, Y. J. ; Perfetto, S. ; Atzrodt, H. ; Dafnis, A.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c2780-809d6ab351ebcf5f155994ba2cd21b8f95c0788acf71e22d3b7b9b96fb92f6da3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2021</creationdate><topic>Aerospace Technology and Astronautics</topic><topic>Aircraft</topic><topic>Aircraft structures</topic><topic>Aircraft vibration</topic><topic>Compression tests</topic><topic>Energy harvesting</topic><topic>Engineering</topic><topic>Investigations</topic><topic>Mechanical properties</topic><topic>Original Paper</topic><topic>Piezoelectric ceramics</topic><topic>Piezoelectric transducers</topic><topic>Tensile tests</topic><toplevel>online_resources</toplevel><creatorcontrib>Holzmann, H.</creatorcontrib><creatorcontrib>Weber, M.</creatorcontrib><creatorcontrib>Park, Y. J.</creatorcontrib><creatorcontrib>Perfetto, S.</creatorcontrib><creatorcontrib>Atzrodt, H.</creatorcontrib><creatorcontrib>Dafnis, A.</creatorcontrib><collection>Springer Nature OA Free Journals</collection><collection>CrossRef</collection><jtitle>CEAS aeronautical journal</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Holzmann, H.</au><au>Weber, M.</au><au>Park, Y. J.</au><au>Perfetto, S.</au><au>Atzrodt, H.</au><au>Dafnis, A.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Investigation of biogenic materials and ferroelectrets for energy harvesting on vibrating aircraft structures</atitle><jtitle>CEAS aeronautical journal</jtitle><stitle>CEAS Aeronaut J</stitle><date>2021-04-01</date><risdate>2021</risdate><volume>12</volume><issue>2</issue><spage>331</spage><epage>344</epage><pages>331-344</pages><issn>1869-5582</issn><eissn>1869-5590</eissn><abstract>In this publication the application of novel piezoelectric materials for energy harvesting on vibrating aircraft structures is investigated. These materials have significant advantages over conventional piezoelectric transducer materials like piezoceramics. In particular, biogenic materials in the form of wood-based materials and ferroelectrets in the form of irradiation cross-linked polypropylene are the subject of the investigation. The material characterization in terms of mechanical and electromechanical properties is shown for both material types. For the wood materials a compression test is used as the material has load-bearing properties. The ferroelectrets provide high compliances and are therefore investigated in a tensile test for material characterisation as well as in a four-point flexural test regarding its behaviour when glued to a dynamically bending surface. Additionally an FE-model of the material model for ferroelectrets is presented, which is validated by experimental results. An estimation of the power output is given for different concepts with both kinds of materials.</abstract><cop>Vienna</cop><pub>Springer Vienna</pub><doi>10.1007/s13272-021-00502-0</doi><tpages>14</tpages><orcidid>https://orcid.org/0000-0002-1485-5208</orcidid><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 1869-5582 |
| ispartof | CEAS aeronautical journal, 2021-04, Vol.12 (2), p.331-344 |
| issn | 1869-5582 1869-5590 |
| language | eng |
| recordid | cdi_proquest_journals_2523981557 |
| source | SpringerNature Journals |
| subjects | Aerospace Technology and Astronautics Aircraft Aircraft structures Aircraft vibration Compression tests Energy harvesting Engineering Investigations Mechanical properties Original Paper Piezoelectric ceramics Piezoelectric transducers Tensile tests |
| title | Investigation of biogenic materials and ferroelectrets for energy harvesting on vibrating aircraft structures |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-03T23%3A06%3A25IST&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=Investigation%20of%20biogenic%20materials%20and%20ferroelectrets%20for%20energy%20harvesting%20on%20vibrating%20aircraft%20structures&rft.jtitle=CEAS%20aeronautical%20journal&rft.au=Holzmann,%20H.&rft.date=2021-04-01&rft.volume=12&rft.issue=2&rft.spage=331&rft.epage=344&rft.pages=331-344&rft.issn=1869-5582&rft.eissn=1869-5590&rft_id=info:doi/10.1007/s13272-021-00502-0&rft_dat=%3Cproquest_cross%3E2523981557%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=2523981557&rft_id=info:pmid/&rfr_iscdi=true |