Fracture investigation of functionalized carbon nanotubes-grown carbon fiber fabrics/epoxy composites
Two different morphologies of carbon nanotubes (CNTs)-grown carbon fiber fabrics (CFFs) were successfully prepared by chemical vapor deposition (CVD) at different temperatures. Short-beam method was used to investigate interlaminar shear strength (ILSS) of epoxy composites reinforced by three kinds...
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| Veröffentlicht in: | Composites science and technology 2020-07, Vol.195, p.108161, Article 108161 |
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| creator | Yao, Zhiqiang Wang, Chengguo Lu, Ruijiao Su, Shunsheng Qin, Jianjie Wang, Yanxiang Ma, Ziming Wei, Huazhen Wang, Qifen |
| description | Two different morphologies of carbon nanotubes (CNTs)-grown carbon fiber fabrics (CFFs) were successfully prepared by chemical vapor deposition (CVD) at different temperatures. Short-beam method was used to investigate interlaminar shear strength (ILSS) of epoxy composites reinforced by three kinds of CFFs—desized CFFs, CNTs-grown CFFs and functionalized CNTs-grown CFFs. It was found that the morphology of CNTs affected the mechanical properties of composites. The ILSS of epoxy composites reinforced by CFFs with long and sparse CNTs was decreased by 10.4% compared with the desized CFFs/epoxy composites, while the ILSS of epoxy composites reinforced by CFFs with short and dense CNTs was almost unchanged. However, after the CNTs-grown CFFs functionalization, the ILSS of epoxy composites reinforced by CFFs with different CNTs of two morphologies were 13.78% and 23.93% higher than the desized CFFs/epoxy composites, respectively. By comprehensively analyzing the changes in oxygen-containing functional groups on the surface of CFFs, the fracture surface morphology of the composites and the relative hardness modulus distribution at the interface, a schematic model was proposed to explain the failure mechanism. |
| doi_str_mv | 10.1016/j.compscitech.2020.108161 |
| format | Article |
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Short-beam method was used to investigate interlaminar shear strength (ILSS) of epoxy composites reinforced by three kinds of CFFs—desized CFFs, CNTs-grown CFFs and functionalized CNTs-grown CFFs. It was found that the morphology of CNTs affected the mechanical properties of composites. The ILSS of epoxy composites reinforced by CFFs with long and sparse CNTs was decreased by 10.4% compared with the desized CFFs/epoxy composites, while the ILSS of epoxy composites reinforced by CFFs with short and dense CNTs was almost unchanged. However, after the CNTs-grown CFFs functionalization, the ILSS of epoxy composites reinforced by CFFs with different CNTs of two morphologies were 13.78% and 23.93% higher than the desized CFFs/epoxy composites, respectively. By comprehensively analyzing the changes in oxygen-containing functional groups on the surface of CFFs, the fracture surface morphology of the composites and the relative hardness modulus distribution at the interface, a schematic model was proposed to explain the failure mechanism.</description><identifier>ISSN: 0266-3538</identifier><identifier>EISSN: 1879-1050</identifier><identifier>DOI: 10.1016/j.compscitech.2020.108161</identifier><language>eng</language><publisher>OXFORD: Elsevier Ltd</publisher><subject>A. Carbon fibers ; B. fibre/matrix bond ; C. Crack ; Carbon fiber reinforced plastics ; Carbon fibers ; Carbon nanotubes ; Carbon-epoxy composites ; Chemical vapor deposition ; Composite materials ; E. Chemical vapor deposition (CVD) ; Fabrics ; Failure mechanisms ; Fracture surfaces ; Functional groups ; Interfacial shear strength ; Materials Science ; Materials Science, Composites ; Mechanical properties ; Morphology ; Nanotubes ; Science & Technology ; Studies ; Technology ; Textile composites</subject><ispartof>Composites science and technology, 2020-07, Vol.195, p.108161, Article 108161</ispartof><rights>2020 Elsevier Ltd</rights><rights>Copyright Elsevier BV Jul 28, 2020</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>true</woscitedreferencessubscribed><woscitedreferencescount>56</woscitedreferencescount><woscitedreferencesoriginalsourcerecordid>wos000539325600001</woscitedreferencesoriginalsourcerecordid><citedby>FETCH-LOGICAL-c349t-5ebf7ca6ea6e1de9b20d8073b7e823d6395dc76577e947bacef46adc01d420203</citedby><cites>FETCH-LOGICAL-c349t-5ebf7ca6ea6e1de9b20d8073b7e823d6395dc76577e947bacef46adc01d420203</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://dx.doi.org/10.1016/j.compscitech.2020.108161$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>315,781,785,3551,27928,27929,28252,45999</link.rule.ids></links><search><creatorcontrib>Yao, Zhiqiang</creatorcontrib><creatorcontrib>Wang, Chengguo</creatorcontrib><creatorcontrib>Lu, Ruijiao</creatorcontrib><creatorcontrib>Su, Shunsheng</creatorcontrib><creatorcontrib>Qin, Jianjie</creatorcontrib><creatorcontrib>Wang, Yanxiang</creatorcontrib><creatorcontrib>Ma, Ziming</creatorcontrib><creatorcontrib>Wei, Huazhen</creatorcontrib><creatorcontrib>Wang, Qifen</creatorcontrib><title>Fracture investigation of functionalized carbon nanotubes-grown carbon fiber fabrics/epoxy composites</title><title>Composites science and technology</title><addtitle>COMPOS SCI TECHNOL</addtitle><description>Two different morphologies of carbon nanotubes (CNTs)-grown carbon fiber fabrics (CFFs) were successfully prepared by chemical vapor deposition (CVD) at different temperatures. Short-beam method was used to investigate interlaminar shear strength (ILSS) of epoxy composites reinforced by three kinds of CFFs—desized CFFs, CNTs-grown CFFs and functionalized CNTs-grown CFFs. It was found that the morphology of CNTs affected the mechanical properties of composites. The ILSS of epoxy composites reinforced by CFFs with long and sparse CNTs was decreased by 10.4% compared with the desized CFFs/epoxy composites, while the ILSS of epoxy composites reinforced by CFFs with short and dense CNTs was almost unchanged. However, after the CNTs-grown CFFs functionalization, the ILSS of epoxy composites reinforced by CFFs with different CNTs of two morphologies were 13.78% and 23.93% higher than the desized CFFs/epoxy composites, respectively. By comprehensively analyzing the changes in oxygen-containing functional groups on the surface of CFFs, the fracture surface morphology of the composites and the relative hardness modulus distribution at the interface, a schematic model was proposed to explain the failure mechanism.</description><subject>A. Carbon fibers</subject><subject>B. fibre/matrix bond</subject><subject>C. Crack</subject><subject>Carbon fiber reinforced plastics</subject><subject>Carbon fibers</subject><subject>Carbon nanotubes</subject><subject>Carbon-epoxy composites</subject><subject>Chemical vapor deposition</subject><subject>Composite materials</subject><subject>E. Chemical vapor deposition (CVD)</subject><subject>Fabrics</subject><subject>Failure mechanisms</subject><subject>Fracture surfaces</subject><subject>Functional groups</subject><subject>Interfacial shear strength</subject><subject>Materials Science</subject><subject>Materials Science, Composites</subject><subject>Mechanical properties</subject><subject>Morphology</subject><subject>Nanotubes</subject><subject>Science & Technology</subject><subject>Studies</subject><subject>Technology</subject><subject>Textile composites</subject><issn>0266-3538</issn><issn>1879-1050</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2020</creationdate><recordtype>article</recordtype><sourceid>AOWDO</sourceid><recordid>eNqNkEtP3TAQha0KJC6U_5CKJcrFj9hOligqtBJSN-3a8mMMvoL4Yjs8-uvrNLRiiWTJo5nzjc4chL4QvCWYiIvd1saHfbahgL3bUkyXfk8E-YQ2pJdDSzDHB2iDqRAt46w_Qsc57zDGkg90g-AqaVvmBE2YniCXcKtLiFMTfePnyS61vg-_wTVWJ1MHk55imQ3k9jbF5-lf2wcDqfHapGDzBezjy2uzOIu5Osuf0aHX9xlO3_4T9Ovq68_xW3vz4_r7eHnTWtYNpeVgvLRaQH3EwWAodj2WzEjoKXOCDdxZKbiUMHTSaAu-E9pZTFy3nM5O0Nm6d5_i41zPUbs4p3pBVrTrqCCc911VDavKpphzAq_2KTzo9KoIVkuqaqfepaqW1WpNtbLnK_sMJvqqgMnCf77GytnAKBe1wou6_7h6DOVv9mOcp1LRcUWh5vUUIKk33IUEtigXwwfs_gHWjaoO</recordid><startdate>20200728</startdate><enddate>20200728</enddate><creator>Yao, Zhiqiang</creator><creator>Wang, Chengguo</creator><creator>Lu, Ruijiao</creator><creator>Su, Shunsheng</creator><creator>Qin, Jianjie</creator><creator>Wang, Yanxiang</creator><creator>Ma, Ziming</creator><creator>Wei, Huazhen</creator><creator>Wang, Qifen</creator><general>Elsevier Ltd</general><general>Elsevier</general><general>Elsevier BV</general><scope>AOWDO</scope><scope>BLEPL</scope><scope>DTL</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>8FD</scope><scope>JG9</scope></search><sort><creationdate>20200728</creationdate><title>Fracture investigation of functionalized carbon nanotubes-grown carbon fiber fabrics/epoxy composites</title><author>Yao, Zhiqiang ; Wang, Chengguo ; Lu, Ruijiao ; Su, Shunsheng ; Qin, Jianjie ; Wang, Yanxiang ; Ma, Ziming ; Wei, Huazhen ; Wang, Qifen</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c349t-5ebf7ca6ea6e1de9b20d8073b7e823d6395dc76577e947bacef46adc01d420203</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2020</creationdate><topic>A. Carbon fibers</topic><topic>B. fibre/matrix bond</topic><topic>C. Crack</topic><topic>Carbon fiber reinforced plastics</topic><topic>Carbon fibers</topic><topic>Carbon nanotubes</topic><topic>Carbon-epoxy composites</topic><topic>Chemical vapor deposition</topic><topic>Composite materials</topic><topic>E. Chemical vapor deposition (CVD)</topic><topic>Fabrics</topic><topic>Failure mechanisms</topic><topic>Fracture surfaces</topic><topic>Functional groups</topic><topic>Interfacial shear strength</topic><topic>Materials Science</topic><topic>Materials Science, Composites</topic><topic>Mechanical properties</topic><topic>Morphology</topic><topic>Nanotubes</topic><topic>Science & Technology</topic><topic>Studies</topic><topic>Technology</topic><topic>Textile composites</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Yao, Zhiqiang</creatorcontrib><creatorcontrib>Wang, Chengguo</creatorcontrib><creatorcontrib>Lu, Ruijiao</creatorcontrib><creatorcontrib>Su, Shunsheng</creatorcontrib><creatorcontrib>Qin, Jianjie</creatorcontrib><creatorcontrib>Wang, Yanxiang</creatorcontrib><creatorcontrib>Ma, Ziming</creatorcontrib><creatorcontrib>Wei, Huazhen</creatorcontrib><creatorcontrib>Wang, Qifen</creatorcontrib><collection>Web of Science - Science Citation Index Expanded - 2020</collection><collection>Web of Science Core Collection</collection><collection>Science Citation Index Expanded</collection><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Technology Research Database</collection><collection>Materials Research Database</collection><jtitle>Composites science and technology</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Yao, Zhiqiang</au><au>Wang, Chengguo</au><au>Lu, Ruijiao</au><au>Su, Shunsheng</au><au>Qin, Jianjie</au><au>Wang, Yanxiang</au><au>Ma, Ziming</au><au>Wei, Huazhen</au><au>Wang, Qifen</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Fracture investigation of functionalized carbon nanotubes-grown carbon fiber fabrics/epoxy composites</atitle><jtitle>Composites science and technology</jtitle><stitle>COMPOS SCI TECHNOL</stitle><date>2020-07-28</date><risdate>2020</risdate><volume>195</volume><spage>108161</spage><pages>108161-</pages><artnum>108161</artnum><issn>0266-3538</issn><eissn>1879-1050</eissn><abstract>Two different morphologies of carbon nanotubes (CNTs)-grown carbon fiber fabrics (CFFs) were successfully prepared by chemical vapor deposition (CVD) at different temperatures. Short-beam method was used to investigate interlaminar shear strength (ILSS) of epoxy composites reinforced by three kinds of CFFs—desized CFFs, CNTs-grown CFFs and functionalized CNTs-grown CFFs. It was found that the morphology of CNTs affected the mechanical properties of composites. The ILSS of epoxy composites reinforced by CFFs with long and sparse CNTs was decreased by 10.4% compared with the desized CFFs/epoxy composites, while the ILSS of epoxy composites reinforced by CFFs with short and dense CNTs was almost unchanged. However, after the CNTs-grown CFFs functionalization, the ILSS of epoxy composites reinforced by CFFs with different CNTs of two morphologies were 13.78% and 23.93% higher than the desized CFFs/epoxy composites, respectively. By comprehensively analyzing the changes in oxygen-containing functional groups on the surface of CFFs, the fracture surface morphology of the composites and the relative hardness modulus distribution at the interface, a schematic model was proposed to explain the failure mechanism.</abstract><cop>OXFORD</cop><pub>Elsevier Ltd</pub><doi>10.1016/j.compscitech.2020.108161</doi><tpages>10</tpages></addata></record> |
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| subjects | A. Carbon fibers B. fibre/matrix bond C. Crack Carbon fiber reinforced plastics Carbon fibers Carbon nanotubes Carbon-epoxy composites Chemical vapor deposition Composite materials E. Chemical vapor deposition (CVD) Fabrics Failure mechanisms Fracture surfaces Functional groups Interfacial shear strength Materials Science Materials Science, Composites Mechanical properties Morphology Nanotubes Science & Technology Studies Technology Textile composites |
| title | Fracture investigation of functionalized carbon nanotubes-grown carbon fiber fabrics/epoxy composites |
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