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Short Fiber-Reinforced Polymer Polyamide 6 Lugs and Selective Laser-Melted Ti-6Al-4V Bushing Contact Cohesive Zone Model Mode II Parameters’ Evaluation
This paper discusses an approach to estimating the parameters of the cohesive zone model (CZM) by mode II by extruding the bushing along the lug axis. This method of evaluation requires small samples, which is particularly relevant when investigating short fiber-reinforced polymers (SFRPs) with addi...
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Published in: | Computation 2024-05, Vol.12 (5), p.105 |
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creator | Sedelnikov, Andry Kurkin, Evgenii Smelov, Vitaliy Chertykovtseva, Vladislava Alekseev, Vyacheslav Gavrilov, Andrey Kishov, Evgenii Zvyagincev, Maksim Chernyakin, Sergey |
description | This paper discusses an approach to estimating the parameters of the cohesive zone model (CZM) by mode II by extruding the bushing along the lug axis. This method of evaluation requires small samples, which is particularly relevant when investigating short fiber-reinforced polymers (SFRPs) with additively manufactured embedded elements. Adhesion is investigated on the example of 30% carbon fiber-reinforced polyamide-6 molded to Ti-6Al-4V (VT6) selective laser-melted (SLM) alloy bushing in cases of a roughness Ra = 2.66 μm (vibratory finishing), Ra = 8.79 μm (sandblasting), and Ra = 10.02 (directly from SLM). The values of the maximum equivalent tangential contact stress were in a range from 1.1 MPa to 9.5 MPa, while the critical fracture energy for tangential slip was estimated at 15 N/mm for all cases. Experimental validation of the obtained CZM mode II was carried out by evaluating the load-carrying capacity of the lugs with different bushings. In both the experiment and the calculation, greater bushing roughness provides greater lug load-bearing capacity. The ribbed bushings added significant strength in the experiments, which confirmed the importance of considering the tangential mode in the contact model. The presented models can be used for the preliminary evaluation of short fiber-reinforced polyamide-6 parts with titanium-embedded elements bearing capacity. |
doi_str_mv | 10.3390/computation12050105 |
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This method of evaluation requires small samples, which is particularly relevant when investigating short fiber-reinforced polymers (SFRPs) with additively manufactured embedded elements. Adhesion is investigated on the example of 30% carbon fiber-reinforced polyamide-6 molded to Ti-6Al-4V (VT6) selective laser-melted (SLM) alloy bushing in cases of a roughness Ra = 2.66 μm (vibratory finishing), Ra = 8.79 μm (sandblasting), and Ra = 10.02 (directly from SLM). The values of the maximum equivalent tangential contact stress were in a range from 1.1 MPa to 9.5 MPa, while the critical fracture energy for tangential slip was estimated at 15 N/mm for all cases. Experimental validation of the obtained CZM mode II was carried out by evaluating the load-carrying capacity of the lugs with different bushings. In both the experiment and the calculation, greater bushing roughness provides greater lug load-bearing capacity. The ribbed bushings added significant strength in the experiments, which confirmed the importance of considering the tangential mode in the contact model. The presented models can be used for the preliminary evaluation of short fiber-reinforced polyamide-6 parts with titanium-embedded elements bearing capacity.</description><identifier>ISSN: 2079-3197</identifier><identifier>EISSN: 2079-3197</identifier><identifier>DOI: 10.3390/computation12050105</identifier><language>eng</language><publisher>Basel: MDPI AG</publisher><subject>Adhesion ; Adhesives ; Aerospace industry ; Aircraft ; Analysis ; Bearing strength ; Bond strength ; Bushings ; Carbon fiber reinforced plastics ; Carbon fibers ; Composite materials ; contact ; Contact melting ; Contact stresses ; Crack propagation ; CZM model ; Dynamic testing ; Extrusion process ; Fiber reinforced polymers ; Influence ; Injection molding ; Lasers ; Load ; Load carrying capacity ; Lugs ; Manufacturing ; Materials ; Methods ; PA6 ; Parameters ; Polyamide resins ; Polyamides ; Polymers ; Properties ; Roughness ; Sandblasting ; SFRP ; Short fibers ; SLM ; Tensile strength ; Testing ; Ti-6Al-4V ; Titanium alloys ; Titanium base alloys ; Vibratory finishing</subject><ispartof>Computation, 2024-05, Vol.12 (5), p.105</ispartof><rights>COPYRIGHT 2024 MDPI AG</rights><rights>2024 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><cites>FETCH-LOGICAL-c307t-986dce94f5d5a3fa92f63afc2bb548e0a992a6b9b69e9c048359a1981ebdd28c3</cites><orcidid>0000-0003-2698-1348 ; 0000-0002-0893-9878 ; 0000-0002-6893-1894 ; 0000-0001-9556-6290</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://www.proquest.com/docview/3059338452/fulltextPDF?pq-origsite=primo$$EPDF$$P50$$Gproquest$$Hfree_for_read</linktopdf><linktohtml>$$Uhttps://www.proquest.com/docview/3059338452?pq-origsite=primo$$EHTML$$P50$$Gproquest$$Hfree_for_read</linktohtml><link.rule.ids>314,780,784,25753,27924,27925,37012,44590,75126</link.rule.ids></links><search><creatorcontrib>Sedelnikov, Andry</creatorcontrib><creatorcontrib>Kurkin, Evgenii</creatorcontrib><creatorcontrib>Smelov, Vitaliy</creatorcontrib><creatorcontrib>Chertykovtseva, Vladislava</creatorcontrib><creatorcontrib>Alekseev, Vyacheslav</creatorcontrib><creatorcontrib>Gavrilov, Andrey</creatorcontrib><creatorcontrib>Kishov, Evgenii</creatorcontrib><creatorcontrib>Zvyagincev, Maksim</creatorcontrib><creatorcontrib>Chernyakin, Sergey</creatorcontrib><title>Short Fiber-Reinforced Polymer Polyamide 6 Lugs and Selective Laser-Melted Ti-6Al-4V Bushing Contact Cohesive Zone Model Mode II Parameters’ Evaluation</title><title>Computation</title><description>This paper discusses an approach to estimating the parameters of the cohesive zone model (CZM) by mode II by extruding the bushing along the lug axis. This method of evaluation requires small samples, which is particularly relevant when investigating short fiber-reinforced polymers (SFRPs) with additively manufactured embedded elements. Adhesion is investigated on the example of 30% carbon fiber-reinforced polyamide-6 molded to Ti-6Al-4V (VT6) selective laser-melted (SLM) alloy bushing in cases of a roughness Ra = 2.66 μm (vibratory finishing), Ra = 8.79 μm (sandblasting), and Ra = 10.02 (directly from SLM). The values of the maximum equivalent tangential contact stress were in a range from 1.1 MPa to 9.5 MPa, while the critical fracture energy for tangential slip was estimated at 15 N/mm for all cases. Experimental validation of the obtained CZM mode II was carried out by evaluating the load-carrying capacity of the lugs with different bushings. In both the experiment and the calculation, greater bushing roughness provides greater lug load-bearing capacity. The ribbed bushings added significant strength in the experiments, which confirmed the importance of considering the tangential mode in the contact model. The presented models can be used for the preliminary evaluation of short fiber-reinforced polyamide-6 parts with titanium-embedded elements bearing capacity.</description><subject>Adhesion</subject><subject>Adhesives</subject><subject>Aerospace industry</subject><subject>Aircraft</subject><subject>Analysis</subject><subject>Bearing strength</subject><subject>Bond strength</subject><subject>Bushings</subject><subject>Carbon fiber reinforced plastics</subject><subject>Carbon fibers</subject><subject>Composite materials</subject><subject>contact</subject><subject>Contact melting</subject><subject>Contact stresses</subject><subject>Crack propagation</subject><subject>CZM model</subject><subject>Dynamic testing</subject><subject>Extrusion process</subject><subject>Fiber reinforced polymers</subject><subject>Influence</subject><subject>Injection molding</subject><subject>Lasers</subject><subject>Load</subject><subject>Load carrying capacity</subject><subject>Lugs</subject><subject>Manufacturing</subject><subject>Materials</subject><subject>Methods</subject><subject>PA6</subject><subject>Parameters</subject><subject>Polyamide resins</subject><subject>Polyamides</subject><subject>Polymers</subject><subject>Properties</subject><subject>Roughness</subject><subject>Sandblasting</subject><subject>SFRP</subject><subject>Short fibers</subject><subject>SLM</subject><subject>Tensile strength</subject><subject>Testing</subject><subject>Ti-6Al-4V</subject><subject>Titanium alloys</subject><subject>Titanium base alloys</subject><subject>Vibratory 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Polyamide 6 Lugs and Selective Laser-Melted Ti-6Al-4V Bushing Contact Cohesive Zone Model Mode II Parameters’ Evaluation</title><author>Sedelnikov, Andry ; Kurkin, Evgenii ; Smelov, Vitaliy ; Chertykovtseva, Vladislava ; Alekseev, Vyacheslav ; Gavrilov, Andrey ; Kishov, Evgenii ; Zvyagincev, Maksim ; Chernyakin, Sergey</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c307t-986dce94f5d5a3fa92f63afc2bb548e0a992a6b9b69e9c048359a1981ebdd28c3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2024</creationdate><topic>Adhesion</topic><topic>Adhesives</topic><topic>Aerospace industry</topic><topic>Aircraft</topic><topic>Analysis</topic><topic>Bearing strength</topic><topic>Bond strength</topic><topic>Bushings</topic><topic>Carbon fiber reinforced plastics</topic><topic>Carbon fibers</topic><topic>Composite materials</topic><topic>contact</topic><topic>Contact melting</topic><topic>Contact stresses</topic><topic>Crack propagation</topic><topic>CZM model</topic><topic>Dynamic testing</topic><topic>Extrusion process</topic><topic>Fiber reinforced polymers</topic><topic>Influence</topic><topic>Injection molding</topic><topic>Lasers</topic><topic>Load</topic><topic>Load carrying capacity</topic><topic>Lugs</topic><topic>Manufacturing</topic><topic>Materials</topic><topic>Methods</topic><topic>PA6</topic><topic>Parameters</topic><topic>Polyamide resins</topic><topic>Polyamides</topic><topic>Polymers</topic><topic>Properties</topic><topic>Roughness</topic><topic>Sandblasting</topic><topic>SFRP</topic><topic>Short fibers</topic><topic>SLM</topic><topic>Tensile strength</topic><topic>Testing</topic><topic>Ti-6Al-4V</topic><topic>Titanium alloys</topic><topic>Titanium base alloys</topic><topic>Vibratory finishing</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Sedelnikov, Andry</creatorcontrib><creatorcontrib>Kurkin, 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Evaluation</atitle><jtitle>Computation</jtitle><date>2024-05-01</date><risdate>2024</risdate><volume>12</volume><issue>5</issue><spage>105</spage><pages>105-</pages><issn>2079-3197</issn><eissn>2079-3197</eissn><abstract>This paper discusses an approach to estimating the parameters of the cohesive zone model (CZM) by mode II by extruding the bushing along the lug axis. This method of evaluation requires small samples, which is particularly relevant when investigating short fiber-reinforced polymers (SFRPs) with additively manufactured embedded elements. Adhesion is investigated on the example of 30% carbon fiber-reinforced polyamide-6 molded to Ti-6Al-4V (VT6) selective laser-melted (SLM) alloy bushing in cases of a roughness Ra = 2.66 μm (vibratory finishing), Ra = 8.79 μm (sandblasting), and Ra = 10.02 (directly from SLM). The values of the maximum equivalent tangential contact stress were in a range from 1.1 MPa to 9.5 MPa, while the critical fracture energy for tangential slip was estimated at 15 N/mm for all cases. Experimental validation of the obtained CZM mode II was carried out by evaluating the load-carrying capacity of the lugs with different bushings. In both the experiment and the calculation, greater bushing roughness provides greater lug load-bearing capacity. The ribbed bushings added significant strength in the experiments, which confirmed the importance of considering the tangential mode in the contact model. The presented models can be used for the preliminary evaluation of short fiber-reinforced polyamide-6 parts with titanium-embedded elements bearing capacity.</abstract><cop>Basel</cop><pub>MDPI AG</pub><doi>10.3390/computation12050105</doi><orcidid>https://orcid.org/0000-0003-2698-1348</orcidid><orcidid>https://orcid.org/0000-0002-0893-9878</orcidid><orcidid>https://orcid.org/0000-0002-6893-1894</orcidid><orcidid>https://orcid.org/0000-0001-9556-6290</orcidid><oa>free_for_read</oa></addata></record> |
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subjects | Adhesion Adhesives Aerospace industry Aircraft Analysis Bearing strength Bond strength Bushings Carbon fiber reinforced plastics Carbon fibers Composite materials contact Contact melting Contact stresses Crack propagation CZM model Dynamic testing Extrusion process Fiber reinforced polymers Influence Injection molding Lasers Load Load carrying capacity Lugs Manufacturing Materials Methods PA6 Parameters Polyamide resins Polyamides Polymers Properties Roughness Sandblasting SFRP Short fibers SLM Tensile strength Testing Ti-6Al-4V Titanium alloys Titanium base alloys Vibratory finishing |
title | Short Fiber-Reinforced Polymer Polyamide 6 Lugs and Selective Laser-Melted Ti-6Al-4V Bushing Contact Cohesive Zone Model Mode II Parameters’ Evaluation |
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