Numerical study on the heat effect on the drilling damage of Ti/CFRP stacks

Carbon fiber reinforced plastics (CFRP) has strong sensitivity to temperature, as the stacking sequence is titanium alloy (Ti) to CFRP, the damage of CFRP is more severe due to the accumulation of cutting heat. In this study, a stress‐strain constitutive model of CFRP with the effect of thermal stre...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Polymer composites 2024-07, Vol.45 (10), p.9487-9500
Hauptverfasser: Chen, Chen, Zhao, Qing, Wang, Aixu, Shi, Zhanli, Bai, Yu
Format: Artikel
Sprache:eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page 9500
container_issue 10
container_start_page 9487
container_title Polymer composites
container_volume 45
creator Chen, Chen
Zhao, Qing
Wang, Aixu
Shi, Zhanli
Bai, Yu
description Carbon fiber reinforced plastics (CFRP) has strong sensitivity to temperature, as the stacking sequence is titanium alloy (Ti) to CFRP, the damage of CFRP is more severe due to the accumulation of cutting heat. In this study, a stress‐strain constitutive model of CFRP with the effect of thermal stress is proposed. On the basis, a simulation model of drilling Ti/CFRP stacks is established to explore the heat effect on the drilling damage. Based on the results, it can be concluded that the burr of Ti at hole exit is generally low due to the support of CFRP, and the burr height increases by 56.61% as the temperature rises from 182.02 to 355.69 °C. Besides, the intralaminar damage of CFRP is mainly caused by the fiber tensile failure and matrix tensile failure, and the matrix tensile failure is more affected by temperature. Moreover, delamination of CFRP decreases slightly with the reduce of drilling temperature. In addition, serious damage of CFRP on the hole wall usually occurs within the cutting angle of 90° to 135°, and pit defects can be reduced in a lower drilling temperature. Highlights A thermal effect stress‐strain constitutive model of CFRP is proposed. Ti/CFRP drilling model is developed based on the proposed constitutive model. Fiber and matrix tensile failure are main form of intralaminar damage of CFRP. Matrix tensile failure is more sensitive to temperature. Simulation model for drilling of Ti/CFRP stacks with heat effect.
doi_str_mv 10.1002/pc.28422
format Article
fullrecord <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_3073877511</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>3073877511</sourcerecordid><originalsourceid>FETCH-LOGICAL-c2542-848562090e5b41a45ad75c64ed66b12acfd5b16230ffd67d1e3f1945c9a479b13</originalsourceid><addsrcrecordid>eNp10MtKw0AUBuBBFKxV8BEG3LhJO_dJlhKsikWL1PUwmUubmjZxJkHy9qZGl64OHL5z4QfgGqMZRojMGzMjKSPkBEwwZ2mCuMhOwQQRSZKUZvIcXMS4GyQWgk7A80u3d6E0uoKx7WwP6wNstw5unW6h896Z9q9lQ1lV5WEDrd7rjYO1h-tyni_eVsOoNh_xEpx5XUV39Vun4H1xv84fk-Xrw1N-t0wM4Wz4gqVcEJQhxwuGNePaSm4Ec1aIAhNtvOUFFoQi762QFjvqcca4yTSTWYHpFNyMe5tQf3YutmpXd-EwnFQUSZpKyfFR3Y7KhDrG4LxqQrnXoVcYqWNUqjHqJ6qBJiP9KivX_-vUKh_9N2i7Z1o</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>3073877511</pqid></control><display><type>article</type><title>Numerical study on the heat effect on the drilling damage of Ti/CFRP stacks</title><source>Wiley Online Library Journals Frontfile Complete</source><creator>Chen, Chen ; Zhao, Qing ; Wang, Aixu ; Shi, Zhanli ; Bai, Yu</creator><creatorcontrib>Chen, Chen ; Zhao, Qing ; Wang, Aixu ; Shi, Zhanli ; Bai, Yu</creatorcontrib><description>Carbon fiber reinforced plastics (CFRP) has strong sensitivity to temperature, as the stacking sequence is titanium alloy (Ti) to CFRP, the damage of CFRP is more severe due to the accumulation of cutting heat. In this study, a stress‐strain constitutive model of CFRP with the effect of thermal stress is proposed. On the basis, a simulation model of drilling Ti/CFRP stacks is established to explore the heat effect on the drilling damage. Based on the results, it can be concluded that the burr of Ti at hole exit is generally low due to the support of CFRP, and the burr height increases by 56.61% as the temperature rises from 182.02 to 355.69 °C. Besides, the intralaminar damage of CFRP is mainly caused by the fiber tensile failure and matrix tensile failure, and the matrix tensile failure is more affected by temperature. Moreover, delamination of CFRP decreases slightly with the reduce of drilling temperature. In addition, serious damage of CFRP on the hole wall usually occurs within the cutting angle of 90° to 135°, and pit defects can be reduced in a lower drilling temperature. Highlights A thermal effect stress‐strain constitutive model of CFRP is proposed. Ti/CFRP drilling model is developed based on the proposed constitutive model. Fiber and matrix tensile failure are main form of intralaminar damage of CFRP. Matrix tensile failure is more sensitive to temperature. Simulation model for drilling of Ti/CFRP stacks with heat effect.</description><identifier>ISSN: 0272-8397</identifier><identifier>EISSN: 1548-0569</identifier><identifier>DOI: 10.1002/pc.28422</identifier><language>eng</language><publisher>Hoboken, USA: John Wiley &amp; Sons, Inc</publisher><subject>Carbon fiber reinforced plastics ; Constitutive models ; Cutting parameters ; Damage accumulation ; Drilling ; drilling damage ; Failure ; Heat ; heat effect ; High temperature effects ; simulation ; Simulation models ; Stacking sequence (composite materials) ; Stacks ; Strain ; Thermal stress ; Ti/CFRP stacks ; Titanium alloys ; Titanium base alloys</subject><ispartof>Polymer composites, 2024-07, Vol.45 (10), p.9487-9500</ispartof><rights>2024 Society of Plastics Engineers.</rights><rights>2024 Society of Plastics Engineers</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c2542-848562090e5b41a45ad75c64ed66b12acfd5b16230ffd67d1e3f1945c9a479b13</cites><orcidid>0009-0007-1349-8062</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://onlinelibrary.wiley.com/doi/pdf/10.1002%2Fpc.28422$$EPDF$$P50$$Gwiley$$H</linktopdf><linktohtml>$$Uhttps://onlinelibrary.wiley.com/doi/full/10.1002%2Fpc.28422$$EHTML$$P50$$Gwiley$$H</linktohtml><link.rule.ids>314,776,780,1411,27903,27904,45553,45554</link.rule.ids></links><search><creatorcontrib>Chen, Chen</creatorcontrib><creatorcontrib>Zhao, Qing</creatorcontrib><creatorcontrib>Wang, Aixu</creatorcontrib><creatorcontrib>Shi, Zhanli</creatorcontrib><creatorcontrib>Bai, Yu</creatorcontrib><title>Numerical study on the heat effect on the drilling damage of Ti/CFRP stacks</title><title>Polymer composites</title><description>Carbon fiber reinforced plastics (CFRP) has strong sensitivity to temperature, as the stacking sequence is titanium alloy (Ti) to CFRP, the damage of CFRP is more severe due to the accumulation of cutting heat. In this study, a stress‐strain constitutive model of CFRP with the effect of thermal stress is proposed. On the basis, a simulation model of drilling Ti/CFRP stacks is established to explore the heat effect on the drilling damage. Based on the results, it can be concluded that the burr of Ti at hole exit is generally low due to the support of CFRP, and the burr height increases by 56.61% as the temperature rises from 182.02 to 355.69 °C. Besides, the intralaminar damage of CFRP is mainly caused by the fiber tensile failure and matrix tensile failure, and the matrix tensile failure is more affected by temperature. Moreover, delamination of CFRP decreases slightly with the reduce of drilling temperature. In addition, serious damage of CFRP on the hole wall usually occurs within the cutting angle of 90° to 135°, and pit defects can be reduced in a lower drilling temperature. Highlights A thermal effect stress‐strain constitutive model of CFRP is proposed. Ti/CFRP drilling model is developed based on the proposed constitutive model. Fiber and matrix tensile failure are main form of intralaminar damage of CFRP. Matrix tensile failure is more sensitive to temperature. Simulation model for drilling of Ti/CFRP stacks with heat effect.</description><subject>Carbon fiber reinforced plastics</subject><subject>Constitutive models</subject><subject>Cutting parameters</subject><subject>Damage accumulation</subject><subject>Drilling</subject><subject>drilling damage</subject><subject>Failure</subject><subject>Heat</subject><subject>heat effect</subject><subject>High temperature effects</subject><subject>simulation</subject><subject>Simulation models</subject><subject>Stacking sequence (composite materials)</subject><subject>Stacks</subject><subject>Strain</subject><subject>Thermal stress</subject><subject>Ti/CFRP stacks</subject><subject>Titanium alloys</subject><subject>Titanium base alloys</subject><issn>0272-8397</issn><issn>1548-0569</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2024</creationdate><recordtype>article</recordtype><recordid>eNp10MtKw0AUBuBBFKxV8BEG3LhJO_dJlhKsikWL1PUwmUubmjZxJkHy9qZGl64OHL5z4QfgGqMZRojMGzMjKSPkBEwwZ2mCuMhOwQQRSZKUZvIcXMS4GyQWgk7A80u3d6E0uoKx7WwP6wNstw5unW6h896Z9q9lQ1lV5WEDrd7rjYO1h-tyni_eVsOoNh_xEpx5XUV39Vun4H1xv84fk-Xrw1N-t0wM4Wz4gqVcEJQhxwuGNePaSm4Ec1aIAhNtvOUFFoQi762QFjvqcca4yTSTWYHpFNyMe5tQf3YutmpXd-EwnFQUSZpKyfFR3Y7KhDrG4LxqQrnXoVcYqWNUqjHqJ6qBJiP9KivX_-vUKh_9N2i7Z1o</recordid><startdate>20240710</startdate><enddate>20240710</enddate><creator>Chen, Chen</creator><creator>Zhao, Qing</creator><creator>Wang, Aixu</creator><creator>Shi, Zhanli</creator><creator>Bai, Yu</creator><general>John Wiley &amp; Sons, Inc</general><general>Blackwell Publishing Ltd</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>8FD</scope><scope>JG9</scope><orcidid>https://orcid.org/0009-0007-1349-8062</orcidid></search><sort><creationdate>20240710</creationdate><title>Numerical study on the heat effect on the drilling damage of Ti/CFRP stacks</title><author>Chen, Chen ; Zhao, Qing ; Wang, Aixu ; Shi, Zhanli ; Bai, Yu</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c2542-848562090e5b41a45ad75c64ed66b12acfd5b16230ffd67d1e3f1945c9a479b13</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2024</creationdate><topic>Carbon fiber reinforced plastics</topic><topic>Constitutive models</topic><topic>Cutting parameters</topic><topic>Damage accumulation</topic><topic>Drilling</topic><topic>drilling damage</topic><topic>Failure</topic><topic>Heat</topic><topic>heat effect</topic><topic>High temperature effects</topic><topic>simulation</topic><topic>Simulation models</topic><topic>Stacking sequence (composite materials)</topic><topic>Stacks</topic><topic>Strain</topic><topic>Thermal stress</topic><topic>Ti/CFRP stacks</topic><topic>Titanium alloys</topic><topic>Titanium base alloys</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Chen, Chen</creatorcontrib><creatorcontrib>Zhao, Qing</creatorcontrib><creatorcontrib>Wang, Aixu</creatorcontrib><creatorcontrib>Shi, Zhanli</creatorcontrib><creatorcontrib>Bai, Yu</creatorcontrib><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Technology Research Database</collection><collection>Materials Research Database</collection><jtitle>Polymer composites</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Chen, Chen</au><au>Zhao, Qing</au><au>Wang, Aixu</au><au>Shi, Zhanli</au><au>Bai, Yu</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Numerical study on the heat effect on the drilling damage of Ti/CFRP stacks</atitle><jtitle>Polymer composites</jtitle><date>2024-07-10</date><risdate>2024</risdate><volume>45</volume><issue>10</issue><spage>9487</spage><epage>9500</epage><pages>9487-9500</pages><issn>0272-8397</issn><eissn>1548-0569</eissn><abstract>Carbon fiber reinforced plastics (CFRP) has strong sensitivity to temperature, as the stacking sequence is titanium alloy (Ti) to CFRP, the damage of CFRP is more severe due to the accumulation of cutting heat. In this study, a stress‐strain constitutive model of CFRP with the effect of thermal stress is proposed. On the basis, a simulation model of drilling Ti/CFRP stacks is established to explore the heat effect on the drilling damage. Based on the results, it can be concluded that the burr of Ti at hole exit is generally low due to the support of CFRP, and the burr height increases by 56.61% as the temperature rises from 182.02 to 355.69 °C. Besides, the intralaminar damage of CFRP is mainly caused by the fiber tensile failure and matrix tensile failure, and the matrix tensile failure is more affected by temperature. Moreover, delamination of CFRP decreases slightly with the reduce of drilling temperature. In addition, serious damage of CFRP on the hole wall usually occurs within the cutting angle of 90° to 135°, and pit defects can be reduced in a lower drilling temperature. Highlights A thermal effect stress‐strain constitutive model of CFRP is proposed. Ti/CFRP drilling model is developed based on the proposed constitutive model. Fiber and matrix tensile failure are main form of intralaminar damage of CFRP. Matrix tensile failure is more sensitive to temperature. Simulation model for drilling of Ti/CFRP stacks with heat effect.</abstract><cop>Hoboken, USA</cop><pub>John Wiley &amp; Sons, Inc</pub><doi>10.1002/pc.28422</doi><tpages>14</tpages><orcidid>https://orcid.org/0009-0007-1349-8062</orcidid></addata></record>
fulltext fulltext
identifier ISSN: 0272-8397
ispartof Polymer composites, 2024-07, Vol.45 (10), p.9487-9500
issn 0272-8397
1548-0569
language eng
recordid cdi_proquest_journals_3073877511
source Wiley Online Library Journals Frontfile Complete
subjects Carbon fiber reinforced plastics
Constitutive models
Cutting parameters
Damage accumulation
Drilling
drilling damage
Failure
Heat
heat effect
High temperature effects
simulation
Simulation models
Stacking sequence (composite materials)
Stacks
Strain
Thermal stress
Ti/CFRP stacks
Titanium alloys
Titanium base alloys
title Numerical study on the heat effect on the drilling damage of Ti/CFRP stacks
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-22T02%3A54%3A41IST&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=Numerical%20study%20on%20the%20heat%20effect%20on%20the%20drilling%20damage%20of%20Ti/CFRP%20stacks&rft.jtitle=Polymer%20composites&rft.au=Chen,%20Chen&rft.date=2024-07-10&rft.volume=45&rft.issue=10&rft.spage=9487&rft.epage=9500&rft.pages=9487-9500&rft.issn=0272-8397&rft.eissn=1548-0569&rft_id=info:doi/10.1002/pc.28422&rft_dat=%3Cproquest_cross%3E3073877511%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=3073877511&rft_id=info:pmid/&rfr_iscdi=true