Thermal Cycling Durability of Bonded PZT Transducers Used for the SHM of Reusable Launch Vehicles
In the context of recent reusable launch vehicles (RLV) developments, the SHM methods could be useful to help fast and economic revalidation of RLVs between launches, provided that the SHM transducers keep their functionality under extreme environmental conditions during flight. This paper focuses o...
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| creator | Mastromatteo, Loïc Gaverina, Ludovic Lavelle, Florian Roche, Jean-Michel Irisarri, François-Xavier |
| description | In the context of recent reusable launch vehicles (RLV) developments, the SHM methods could be useful to help fast and economic revalidation of RLVs between launches, provided that the SHM transducers keep their functionality under extreme environmental conditions during flight.
This paper focuses on the thermal cycling durability of PZT piezoelectric transducers bonded on a Carbon Fiber Reinforce Polymer (CFRP) composite plate. The temperature cycles are set to be representative of the thermal loadings that the structure of a launcher could experience under a thermal barrier: limited number of cycles ( |
| doi_str_mv | 10.1007/978-3-031-07258-1_73 |
| format | Book Chapter |
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This paper focuses on the thermal cycling durability of PZT piezoelectric transducers bonded on a Carbon Fiber Reinforce Polymer (CFRP) composite plate. The temperature cycles are set to be representative of the thermal loadings that the structure of a launcher could experience under a thermal barrier: limited number of cycles (<10) of short duration (<10 min) and high temperatures for thermoset-matrix composites (150 ∘\documentclass[12pt]{minimal}
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\begin{document}$$^\circ $$\end{document}C/min) and gradients through the plate thickness to best reproduce flight conditions. To our knowledge, very few research studies have been carried out so far on the resistance of SHM systems under such environment.
The degradation of the system formed by the composite plate, the adhesive and the PZT transducer is studied, in comparison with the state of reference before cycling, with three different approaches. First, electromechanical impedance is measured during the entire thermal cycling. Then the functionality of a guided wave SHM system is evaluated based on the emission and reception of Lamb waves between PZTs attached to the surface of the plate. Finally, Laser vibrometry is used to provide a mapping of the emitted Lamb waves propagation and to identify possible debondings or changes of amplitudes of waveforms after the thermal cycles.</description><identifier>ISSN: 2366-2557</identifier><identifier>ISBN: 9783031072574</identifier><identifier>ISBN: 303107257X</identifier><identifier>EISSN: 2366-2565</identifier><identifier>EISBN: 9783031072581</identifier><identifier>EISBN: 3031072588</identifier><identifier>DOI: 10.1007/978-3-031-07258-1_73</identifier><identifier>OCLC: 1334104224</identifier><identifier>LCCallNum: TH3301-3411</identifier><language>eng</language><publisher>Switzerland: Springer International Publishing AG</publisher><subject>Carbon Fiber Reinforce Polymer (CFRP) ; Chemical Sciences ; Composite ; Durability ; Electro-mechanical impedance (EMI) ; Engineering Sciences ; Guided waves (GW) ; Laser Doppler Vibrometry (LDV) ; Physics ; Reusable launch vehicle (RLV)</subject><ispartof>European Workshop on Structural Health Monitoring, 2022, Vol.254, p.727-736</ispartof><rights>The Author(s), under exclusive license to Springer Nature Switzerland AG 2023</rights><rights>Distributed under a Creative Commons Attribution 4.0 International License</rights><woscitedreferencessubscribed>false</woscitedreferencessubscribed><orcidid>0009-0004-0032-4133</orcidid><relation>Lecture Notes in Civil Engineering</relation></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Uhttps://ebookcentral.proquest.com/covers/7018137-l.jpg</thumbnail><linktopdf>$$Uhttps://link.springer.com/content/pdf/10.1007/978-3-031-07258-1_73$$EPDF$$P50$$Gspringer$$H</linktopdf><linktohtml>$$Uhttps://link.springer.com/10.1007/978-3-031-07258-1_73$$EHTML$$P50$$Gspringer$$H</linktohtml><link.rule.ids>230,775,776,780,789,881,27904,38234,41421,42490</link.rule.ids><backlink>$$Uhttps://hal.science/hal-03772283$$DView record in HAL$$Hfree_for_read</backlink></links><search><contributor>Rizzo, Piervincenzo</contributor><contributor>Milazzo, Alberto</contributor><contributor>Rizzo, Piervincenzo</contributor><contributor>Milazzo, Alberto</contributor><creatorcontrib>Mastromatteo, Loïc</creatorcontrib><creatorcontrib>Gaverina, Ludovic</creatorcontrib><creatorcontrib>Lavelle, Florian</creatorcontrib><creatorcontrib>Roche, Jean-Michel</creatorcontrib><creatorcontrib>Irisarri, François-Xavier</creatorcontrib><title>Thermal Cycling Durability of Bonded PZT Transducers Used for the SHM of Reusable Launch Vehicles</title><title>European Workshop on Structural Health Monitoring</title><description>In the context of recent reusable launch vehicles (RLV) developments, the SHM methods could be useful to help fast and economic revalidation of RLVs between launches, provided that the SHM transducers keep their functionality under extreme environmental conditions during flight.
This paper focuses on the thermal cycling durability of PZT piezoelectric transducers bonded on a Carbon Fiber Reinforce Polymer (CFRP) composite plate. The temperature cycles are set to be representative of the thermal loadings that the structure of a launcher could experience under a thermal barrier: limited number of cycles (<10) of short duration (<10 min) and high temperatures for thermoset-matrix composites (150 ∘\documentclass[12pt]{minimal}
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\begin{document}$$^\circ $$\end{document}C/min) and gradients through the plate thickness to best reproduce flight conditions. To our knowledge, very few research studies have been carried out so far on the resistance of SHM systems under such environment.
The degradation of the system formed by the composite plate, the adhesive and the PZT transducer is studied, in comparison with the state of reference before cycling, with three different approaches. First, electromechanical impedance is measured during the entire thermal cycling. Then the functionality of a guided wave SHM system is evaluated based on the emission and reception of Lamb waves between PZTs attached to the surface of the plate. Finally, Laser vibrometry is used to provide a mapping of the emitted Lamb waves propagation and to identify possible debondings or changes of amplitudes of waveforms after the thermal cycles.</description><subject>Carbon Fiber Reinforce Polymer (CFRP)</subject><subject>Chemical Sciences</subject><subject>Composite</subject><subject>Durability</subject><subject>Electro-mechanical impedance (EMI)</subject><subject>Engineering Sciences</subject><subject>Guided waves (GW)</subject><subject>Laser Doppler Vibrometry (LDV)</subject><subject>Physics</subject><subject>Reusable launch vehicle (RLV)</subject><issn>2366-2557</issn><issn>2366-2565</issn><isbn>9783031072574</isbn><isbn>303107257X</isbn><isbn>9783031072581</isbn><isbn>3031072588</isbn><fulltext>true</fulltext><rsrctype>book_chapter</rsrctype><creationdate>2022</creationdate><recordtype>book_chapter</recordtype><recordid>eNpVkU2P0zAQhs2nWJb-Aw6-cgiMPU7GPS7lo0hFIOhy4GJNXGcTyCbFTpD673G2CImTpWfexxq9I8RzBS8VAL1aky2wAFQFkC5toRzhPbHKGDO8Y-q-uNBYVYUuq_LBfzMyD__NSnosnipEo8BobZ6IVUo_AEATKtLqQvC-DfGWe7k5-b4bbuSbOXLd9d10kmMjX4_DIRzk5-97uY88pMPsQ0zyOmXYjFFObZBftx-X6JcwJ677IHc8D76V30Lb-T6kZ-JRw30Kq7_vpbh-93a_2Ra7T-8_bK52RauBpsKHytQlkSkRIFiqy8ZqX-XNA-dtTc1rtn4NynBVGcCDBWgs6IoZStKIl-LF-d-We3eM3S3Hkxu5c9urnVsYIJHWFn-rnNXnbMrB4SZEV4_jz-QUuOUALrfpMAvK3ZXtlgNkyZylYxx_zSFNLiyWD8MUufctH6fcjSNQViE5MpAti38A1QiAqw</recordid><startdate>2022</startdate><enddate>2022</enddate><creator>Mastromatteo, Loïc</creator><creator>Gaverina, Ludovic</creator><creator>Lavelle, Florian</creator><creator>Roche, Jean-Michel</creator><creator>Irisarri, François-Xavier</creator><general>Springer International Publishing AG</general><general>Springer International Publishing</general><scope>FFUUA</scope><scope>1XC</scope><orcidid>https://orcid.org/0009-0004-0032-4133</orcidid></search><sort><creationdate>2022</creationdate><title>Thermal Cycling Durability of Bonded PZT Transducers Used for the SHM of Reusable Launch Vehicles</title><author>Mastromatteo, Loïc ; Gaverina, Ludovic ; Lavelle, Florian ; Roche, Jean-Michel ; Irisarri, François-Xavier</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-h207t-ce64b57745300e87b5f82c6341ea2734ba9a8c9014a66403d800f8026aa057233</frbrgroupid><rsrctype>book_chapters</rsrctype><prefilter>book_chapters</prefilter><language>eng</language><creationdate>2022</creationdate><topic>Carbon Fiber Reinforce Polymer (CFRP)</topic><topic>Chemical Sciences</topic><topic>Composite</topic><topic>Durability</topic><topic>Electro-mechanical impedance (EMI)</topic><topic>Engineering Sciences</topic><topic>Guided waves (GW)</topic><topic>Laser Doppler Vibrometry (LDV)</topic><topic>Physics</topic><topic>Reusable launch vehicle (RLV)</topic><toplevel>online_resources</toplevel><creatorcontrib>Mastromatteo, Loïc</creatorcontrib><creatorcontrib>Gaverina, Ludovic</creatorcontrib><creatorcontrib>Lavelle, Florian</creatorcontrib><creatorcontrib>Roche, Jean-Michel</creatorcontrib><creatorcontrib>Irisarri, François-Xavier</creatorcontrib><collection>ProQuest Ebook Central - Book Chapters - Demo use only</collection><collection>Hyper Article en Ligne (HAL)</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Mastromatteo, Loïc</au><au>Gaverina, Ludovic</au><au>Lavelle, Florian</au><au>Roche, Jean-Michel</au><au>Irisarri, François-Xavier</au><au>Rizzo, Piervincenzo</au><au>Milazzo, Alberto</au><au>Rizzo, Piervincenzo</au><au>Milazzo, Alberto</au><format>book</format><genre>bookitem</genre><ristype>CHAP</ristype><atitle>Thermal Cycling Durability of Bonded PZT Transducers Used for the SHM of Reusable Launch Vehicles</atitle><btitle>European Workshop on Structural Health Monitoring</btitle><seriestitle>Lecture Notes in Civil Engineering</seriestitle><date>2022</date><risdate>2022</risdate><volume>254</volume><spage>727</spage><epage>736</epage><pages>727-736</pages><issn>2366-2557</issn><eissn>2366-2565</eissn><isbn>9783031072574</isbn><isbn>303107257X</isbn><eisbn>9783031072581</eisbn><eisbn>3031072588</eisbn><abstract>In the context of recent reusable launch vehicles (RLV) developments, the SHM methods could be useful to help fast and economic revalidation of RLVs between launches, provided that the SHM transducers keep their functionality under extreme environmental conditions during flight.
This paper focuses on the thermal cycling durability of PZT piezoelectric transducers bonded on a Carbon Fiber Reinforce Polymer (CFRP) composite plate. The temperature cycles are set to be representative of the thermal loadings that the structure of a launcher could experience under a thermal barrier: limited number of cycles (<10) of short duration (<10 min) and high temperatures for thermoset-matrix composites (150 ∘\documentclass[12pt]{minimal}
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\begin{document}$$^\circ $$\end{document}C). The heating is generated using a CO2 laser in order to obtain the steep thermal ramps (60 ∘\documentclass[12pt]{minimal}
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\begin{document}$$^\circ $$\end{document}C/min) and gradients through the plate thickness to best reproduce flight conditions. To our knowledge, very few research studies have been carried out so far on the resistance of SHM systems under such environment.
The degradation of the system formed by the composite plate, the adhesive and the PZT transducer is studied, in comparison with the state of reference before cycling, with three different approaches. First, electromechanical impedance is measured during the entire thermal cycling. Then the functionality of a guided wave SHM system is evaluated based on the emission and reception of Lamb waves between PZTs attached to the surface of the plate. Finally, Laser vibrometry is used to provide a mapping of the emitted Lamb waves propagation and to identify possible debondings or changes of amplitudes of waveforms after the thermal cycles.</abstract><cop>Switzerland</cop><pub>Springer International Publishing AG</pub><doi>10.1007/978-3-031-07258-1_73</doi><oclcid>1334104224</oclcid><tpages>10</tpages><orcidid>https://orcid.org/0009-0004-0032-4133</orcidid></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 2366-2557 |
| ispartof | European Workshop on Structural Health Monitoring, 2022, Vol.254, p.727-736 |
| issn | 2366-2557 2366-2565 |
| language | eng |
| recordid | cdi_hal_primary_oai_HAL_hal_03772283v1 |
| source | Springer Books |
| subjects | Carbon Fiber Reinforce Polymer (CFRP) Chemical Sciences Composite Durability Electro-mechanical impedance (EMI) Engineering Sciences Guided waves (GW) Laser Doppler Vibrometry (LDV) Physics Reusable launch vehicle (RLV) |
| title | Thermal Cycling Durability of Bonded PZT Transducers Used for the SHM of Reusable Launch Vehicles |
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