High reliability model of mechanical response in drilling of CFRP/Al stacks
CFRP/Al laminate material is widely used in aerospace due to its advantages of light weight and high machinability. For assembling, crowded assembly holes need to be drilled for CFRP/Al laminate products. However, the damages of burr, delamination, and tearing appear frequently in drilling without p...
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| Veröffentlicht in: | International journal of advanced manufacturing technology 2023-03, Vol.125 (1-2), p.645-660 |
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| creator | Gong, Qinghong Li, Liang Yuan, Xinman Hu, Zhiqin Chen, Jie Ma, Ke |
| description | CFRP/Al laminate material is widely used in aerospace due to its advantages of light weight and high machinability. For assembling, crowded assembly holes need to be drilled for CFRP/Al laminate products. However, the damages of burr, delamination, and tearing appear frequently in drilling without precise guidance by mechanical response model. In order to reduce the machining damages, in this paper, a high-reliability mechanical response model is established for each stage in laminate materials drilling to ascertain the matching method between materials, tools, and cutting parameters. The theoretical expression of drilling thrust based on the thin plate theory is established considering the influence of cutting parameters, and further corrected with the cutting parameter correction terms to predict drilling thrust force, and further guiding the optimization of drilling parameters. According to the experimental results, the proposed model has a reliability greater than 97.3% and a prediction deviation lower than 13.2% in CFRP/Al laminate material drilling thrust force prediction. In the cutting with optimized parameters from the proposed model, the inlet orifice of the laminated material has no flanging burr, and the CFRP layer exit orifice has no defects as burr, delamination, or tearing. |
| doi_str_mv | 10.1007/s00170-022-10750-x |
| format | Article |
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For assembling, crowded assembly holes need to be drilled for CFRP/Al laminate products. However, the damages of burr, delamination, and tearing appear frequently in drilling without precise guidance by mechanical response model. In order to reduce the machining damages, in this paper, a high-reliability mechanical response model is established for each stage in laminate materials drilling to ascertain the matching method between materials, tools, and cutting parameters. The theoretical expression of drilling thrust based on the thin plate theory is established considering the influence of cutting parameters, and further corrected with the cutting parameter correction terms to predict drilling thrust force, and further guiding the optimization of drilling parameters. According to the experimental results, the proposed model has a reliability greater than 97.3% and a prediction deviation lower than 13.2% in CFRP/Al laminate material drilling thrust force prediction. In the cutting with optimized parameters from the proposed model, the inlet orifice of the laminated material has no flanging burr, and the CFRP layer exit orifice has no defects as burr, delamination, or tearing.</description><identifier>ISSN: 0268-3768</identifier><identifier>EISSN: 1433-3015</identifier><identifier>DOI: 10.1007/s00170-022-10750-x</identifier><language>eng</language><publisher>London: Springer London</publisher><subject>Assembling ; CAE) and Design ; Computer-Aided Engineering (CAD ; Cutting parameters ; Cutting tools ; Delamination ; Drilling ; Engineering ; Flanging ; Industrial and Production Engineering ; Machinability ; Machining ; Mathematical models ; Mechanical analysis ; Mechanical Engineering ; Media Management ; Optimization ; Orifices ; Original Article ; Plate theory ; Reliability ; Reliability analysis ; Tearing ; Thin plates ; Thrust ; Weight reduction</subject><ispartof>International journal of advanced manufacturing technology, 2023-03, Vol.125 (1-2), p.645-660</ispartof><rights>The Author(s), under exclusive licence to Springer-Verlag London Ltd., part of Springer Nature 2022. Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c314t-8f34917a764eecbe591fec641d2635aade01d9f315ef07aacd423f691df265c73</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://link.springer.com/content/pdf/10.1007/s00170-022-10750-x$$EPDF$$P50$$Gspringer$$H</linktopdf><linktohtml>$$Uhttps://link.springer.com/10.1007/s00170-022-10750-x$$EHTML$$P50$$Gspringer$$H</linktohtml><link.rule.ids>314,776,780,27903,27904,41467,42536,51298</link.rule.ids></links><search><creatorcontrib>Gong, Qinghong</creatorcontrib><creatorcontrib>Li, Liang</creatorcontrib><creatorcontrib>Yuan, Xinman</creatorcontrib><creatorcontrib>Hu, Zhiqin</creatorcontrib><creatorcontrib>Chen, Jie</creatorcontrib><creatorcontrib>Ma, Ke</creatorcontrib><title>High reliability model of mechanical response in drilling of CFRP/Al stacks</title><title>International journal of advanced manufacturing technology</title><addtitle>Int J Adv Manuf Technol</addtitle><description>CFRP/Al laminate material is widely used in aerospace due to its advantages of light weight and high machinability. For assembling, crowded assembly holes need to be drilled for CFRP/Al laminate products. However, the damages of burr, delamination, and tearing appear frequently in drilling without precise guidance by mechanical response model. In order to reduce the machining damages, in this paper, a high-reliability mechanical response model is established for each stage in laminate materials drilling to ascertain the matching method between materials, tools, and cutting parameters. The theoretical expression of drilling thrust based on the thin plate theory is established considering the influence of cutting parameters, and further corrected with the cutting parameter correction terms to predict drilling thrust force, and further guiding the optimization of drilling parameters. According to the experimental results, the proposed model has a reliability greater than 97.3% and a prediction deviation lower than 13.2% in CFRP/Al laminate material drilling thrust force prediction. In the cutting with optimized parameters from the proposed model, the inlet orifice of the laminated material has no flanging burr, and the CFRP layer exit orifice has no defects as burr, delamination, or tearing.</description><subject>Assembling</subject><subject>CAE) and Design</subject><subject>Computer-Aided Engineering (CAD</subject><subject>Cutting parameters</subject><subject>Cutting tools</subject><subject>Delamination</subject><subject>Drilling</subject><subject>Engineering</subject><subject>Flanging</subject><subject>Industrial and Production Engineering</subject><subject>Machinability</subject><subject>Machining</subject><subject>Mathematical models</subject><subject>Mechanical analysis</subject><subject>Mechanical Engineering</subject><subject>Media Management</subject><subject>Optimization</subject><subject>Orifices</subject><subject>Original Article</subject><subject>Plate theory</subject><subject>Reliability</subject><subject>Reliability analysis</subject><subject>Tearing</subject><subject>Thin plates</subject><subject>Thrust</subject><subject>Weight reduction</subject><issn>0268-3768</issn><issn>1433-3015</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2023</creationdate><recordtype>article</recordtype><sourceid>AFKRA</sourceid><sourceid>BENPR</sourceid><sourceid>CCPQU</sourceid><sourceid>DWQXO</sourceid><recordid>eNp9kEFLwzAYhoMoOKd_wFPBc1y-pE3a4xjOiQNF9ByyNOkys3YmHWz_3swK3jx9h_d53w8ehG6B3AMhYhIJAUEwoRQDEQXBhzM0gpwxzAgU52hEKC8xE7y8RFcxbhLOgZcj9LxwzToLxju1ct71x2zb1cZnnc22Rq9V67TyKY-7ro0mc21WB-e9a5sTMpu_vU6mPou90p_xGl1Y5aO5-b1j9DF_eJ8t8PLl8Wk2XWLNIO9xaVlegVCC58bolSkqsEbzHGrKWaFUbQjUlWVQGEuEUrrOKbO8gtpSXmjBxuhu2N2F7mtvYi833T606aWkQhRAqzKvEkUHSocuxmCs3AW3VeEogciTNDlIk0ma_JEmD6nEhlJMcNuY8Df9T-sbRQpvaA</recordid><startdate>20230301</startdate><enddate>20230301</enddate><creator>Gong, Qinghong</creator><creator>Li, Liang</creator><creator>Yuan, Xinman</creator><creator>Hu, Zhiqin</creator><creator>Chen, Jie</creator><creator>Ma, Ke</creator><general>Springer London</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope><scope>8FE</scope><scope>8FG</scope><scope>ABJCF</scope><scope>AFKRA</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>DWQXO</scope><scope>HCIFZ</scope><scope>L6V</scope><scope>M7S</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope><scope>PTHSS</scope></search><sort><creationdate>20230301</creationdate><title>High reliability model of mechanical response in drilling of CFRP/Al stacks</title><author>Gong, Qinghong ; Li, Liang ; Yuan, Xinman ; Hu, Zhiqin ; Chen, Jie ; Ma, Ke</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c314t-8f34917a764eecbe591fec641d2635aade01d9f315ef07aacd423f691df265c73</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2023</creationdate><topic>Assembling</topic><topic>CAE) and Design</topic><topic>Computer-Aided Engineering (CAD</topic><topic>Cutting parameters</topic><topic>Cutting tools</topic><topic>Delamination</topic><topic>Drilling</topic><topic>Engineering</topic><topic>Flanging</topic><topic>Industrial and Production Engineering</topic><topic>Machinability</topic><topic>Machining</topic><topic>Mathematical models</topic><topic>Mechanical analysis</topic><topic>Mechanical Engineering</topic><topic>Media Management</topic><topic>Optimization</topic><topic>Orifices</topic><topic>Original Article</topic><topic>Plate theory</topic><topic>Reliability</topic><topic>Reliability analysis</topic><topic>Tearing</topic><topic>Thin plates</topic><topic>Thrust</topic><topic>Weight reduction</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Gong, Qinghong</creatorcontrib><creatorcontrib>Li, Liang</creatorcontrib><creatorcontrib>Yuan, Xinman</creatorcontrib><creatorcontrib>Hu, Zhiqin</creatorcontrib><creatorcontrib>Chen, Jie</creatorcontrib><creatorcontrib>Ma, Ke</creatorcontrib><collection>CrossRef</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>Materials Science & Engineering Collection</collection><collection>ProQuest Central UK/Ireland</collection><collection>ProQuest Central</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Central Korea</collection><collection>SciTech Premium Collection</collection><collection>ProQuest Engineering Collection</collection><collection>Engineering Database</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central China</collection><collection>Engineering Collection</collection><jtitle>International journal of advanced manufacturing technology</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Gong, Qinghong</au><au>Li, Liang</au><au>Yuan, Xinman</au><au>Hu, Zhiqin</au><au>Chen, Jie</au><au>Ma, Ke</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>High reliability model of mechanical response in drilling of CFRP/Al stacks</atitle><jtitle>International journal of advanced manufacturing technology</jtitle><stitle>Int J Adv Manuf Technol</stitle><date>2023-03-01</date><risdate>2023</risdate><volume>125</volume><issue>1-2</issue><spage>645</spage><epage>660</epage><pages>645-660</pages><issn>0268-3768</issn><eissn>1433-3015</eissn><abstract>CFRP/Al laminate material is widely used in aerospace due to its advantages of light weight and high machinability. For assembling, crowded assembly holes need to be drilled for CFRP/Al laminate products. However, the damages of burr, delamination, and tearing appear frequently in drilling without precise guidance by mechanical response model. In order to reduce the machining damages, in this paper, a high-reliability mechanical response model is established for each stage in laminate materials drilling to ascertain the matching method between materials, tools, and cutting parameters. The theoretical expression of drilling thrust based on the thin plate theory is established considering the influence of cutting parameters, and further corrected with the cutting parameter correction terms to predict drilling thrust force, and further guiding the optimization of drilling parameters. According to the experimental results, the proposed model has a reliability greater than 97.3% and a prediction deviation lower than 13.2% in CFRP/Al laminate material drilling thrust force prediction. In the cutting with optimized parameters from the proposed model, the inlet orifice of the laminated material has no flanging burr, and the CFRP layer exit orifice has no defects as burr, delamination, or tearing.</abstract><cop>London</cop><pub>Springer London</pub><doi>10.1007/s00170-022-10750-x</doi><tpages>16</tpages><oa>free_for_read</oa></addata></record> |
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| subjects | Assembling CAE) and Design Computer-Aided Engineering (CAD Cutting parameters Cutting tools Delamination Drilling Engineering Flanging Industrial and Production Engineering Machinability Machining Mathematical models Mechanical analysis Mechanical Engineering Media Management Optimization Orifices Original Article Plate theory Reliability Reliability analysis Tearing Thin plates Thrust Weight reduction |
| title | High reliability model of mechanical response in drilling of CFRP/Al stacks |
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