{"title":"用于轻质应用的 3D 打印碳纤维夹层结构的实验研究","authors":"Solaiprakash Vellaisamy , Raguraman Munusamy","doi":"10.1016/j.dt.2023.11.019","DOIUrl":null,"url":null,"abstract":"<div><p>Honeycomb sandwich structures are widely used in lightweight applications. Usually, these structures are subjected to extreme loading conditions, leading to potential failures due to delamination and debonding between the face sheet and the honeycomb core. Therefore, the present study is focused on the mechanical characterisation of honeycomb sandwich structures fabricated using advanced 3D printing technology. The continuous carbon fibres and ONYX-FR matrix materials have been used as raw materials for 3D printing of the specimens needed for various mechanical characterization testing; ONYX-FR is a commercial trade name for flame retardant short carbon fibre filled nylon filaments, used as a reinforcing material in Morkforged 3D printer. Edgewise and flatwise compression tests have been conducted for different configurations of honeycomb sandwich structures, fabricated by varying the face sheet thickness and core cell size, while keeping the core cell thickness and core height constant. Based on these tests, the proposed structure with face sheet thickness of 3.2 mm and a core cell size of 12.7 mm exhibited the highest energy absorption and prevented delamination and debonding failures. Therefore, 3D printing technology can also be considered as an alternative method for sandwich structure fabrication. However, detailed parametric studies still need to be conducted to meet various other structural integrity criteria related to the lightweight applications.</p></div>","PeriodicalId":58209,"journal":{"name":"Defence Technology(防务技术)","volume":"36 ","pages":"Pages 71-77"},"PeriodicalIF":5.0000,"publicationDate":"2024-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://www.sciencedirect.com/science/article/pii/S2214914723003070/pdfft?md5=8ad3bce54c94f4ba04fe2e576ed6f03b&pid=1-s2.0-S2214914723003070-main.pdf","citationCount":"0","resultStr":"{\"title\":\"Experimental study of 3D printed carbon fibre sandwich structures for lightweight applications\",\"authors\":\"Solaiprakash Vellaisamy , Raguraman Munusamy\",\"doi\":\"10.1016/j.dt.2023.11.019\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><p>Honeycomb sandwich structures are widely used in lightweight applications. Usually, these structures are subjected to extreme loading conditions, leading to potential failures due to delamination and debonding between the face sheet and the honeycomb core. Therefore, the present study is focused on the mechanical characterisation of honeycomb sandwich structures fabricated using advanced 3D printing technology. The continuous carbon fibres and ONYX-FR matrix materials have been used as raw materials for 3D printing of the specimens needed for various mechanical characterization testing; ONYX-FR is a commercial trade name for flame retardant short carbon fibre filled nylon filaments, used as a reinforcing material in Morkforged 3D printer. Edgewise and flatwise compression tests have been conducted for different configurations of honeycomb sandwich structures, fabricated by varying the face sheet thickness and core cell size, while keeping the core cell thickness and core height constant. 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引用次数: 0
摘要
蜂窝夹层结构广泛应用于轻质材料领域。通常情况下,这些结构要承受极端的载荷条件,从而导致面片与蜂窝芯之间的分层和脱粘可能导致失效。因此,本研究的重点是利用先进的 3D 打印技术制造蜂窝夹层结构的机械特性。连续碳纤维和ONYX-FR基体材料被用作原材料,用于三维打印各种机械特性测试所需的试样;ONYX-FR是阻燃短碳纤维填充尼龙丝的商业商品名,在Morkforged三维打印机中用作增强材料。通过改变面片厚度和芯单元尺寸,同时保持芯单元厚度和芯高度不变,对不同配置的蜂窝夹层结构进行了边缘和平面压缩测试。根据这些测试结果,面片厚度为 3.2 毫米、芯单元尺寸为 12.7 毫米的拟议结构具有最高的能量吸收能力,并能防止分层和脱粘故障。因此,3D 打印技术也可作为夹层结构制造的替代方法。不过,仍需进行详细的参数研究,以满足与轻质应用相关的其他各种结构完整性标准。
Experimental study of 3D printed carbon fibre sandwich structures for lightweight applications
Honeycomb sandwich structures are widely used in lightweight applications. Usually, these structures are subjected to extreme loading conditions, leading to potential failures due to delamination and debonding between the face sheet and the honeycomb core. Therefore, the present study is focused on the mechanical characterisation of honeycomb sandwich structures fabricated using advanced 3D printing technology. The continuous carbon fibres and ONYX-FR matrix materials have been used as raw materials for 3D printing of the specimens needed for various mechanical characterization testing; ONYX-FR is a commercial trade name for flame retardant short carbon fibre filled nylon filaments, used as a reinforcing material in Morkforged 3D printer. Edgewise and flatwise compression tests have been conducted for different configurations of honeycomb sandwich structures, fabricated by varying the face sheet thickness and core cell size, while keeping the core cell thickness and core height constant. Based on these tests, the proposed structure with face sheet thickness of 3.2 mm and a core cell size of 12.7 mm exhibited the highest energy absorption and prevented delamination and debonding failures. Therefore, 3D printing technology can also be considered as an alternative method for sandwich structure fabrication. However, detailed parametric studies still need to be conducted to meet various other structural integrity criteria related to the lightweight applications.
Defence Technology(防务技术)Mechanical Engineering, Control and Systems Engineering, Industrial and Manufacturing Engineering
CiteScore
8.70
自引率
0.00%
发文量
728
审稿时长
25 days
期刊介绍:
Defence Technology, a peer reviewed journal, is published monthly and aims to become the best international academic exchange platform for the research related to defence technology. It publishes original research papers having direct bearing on defence, with a balanced coverage on analytical, experimental, numerical simulation and applied investigations. It covers various disciplines of science, technology and engineering.