聚合物微晶格缓冲结构 自由冲击吸收

Louis Catar, Ilyass Tabiai, David St-Onge
{"title":"聚合物微晶格缓冲结构 自由冲击吸收","authors":"Louis Catar, Ilyass Tabiai, David St-Onge","doi":"arxiv-2408.02909","DOIUrl":null,"url":null,"abstract":"The uncrewed aerial systems industry is rapidly expanding due to advancements\nin smaller electronics, smarter sensors, advanced flight controllers, and\nembedded perception modules leveraging artificial intelligence. These\ntechnological progress have opened new indoor applications for UAS, including\nwarehouse inventory management, security inspections of public spaces and\nfacilities, and underground exploration. Despite the innovative designs from\nUAS manufacturers, there are no existing standards to ensure UAS and human\nsafety in these environments. This study explores developing and evaluating\nmicro-lattice structures for impact resistance in lightweight UAS. We examine\npatch designs using Face-Centered Cubic (FCC), Diamond (D), Kelvin (K), and\nGyroid (GY) patterns and detail the processes for creating samples for impact\nand compression tests, including manufacturing and testing protocols. Our evaluation includes compression and impact tests to assess structural\nbehavior, revealing the influence of geometry, compactness, and material\nproperties. Diamond and Kelvin patterns were particularly effective in load\ndistribution and energy absorption over the compression tests. Impact tests\ndemonstrated significant differences in response between flexible and rigid\nmaterials, with flexible patches exhibiting superior energy dissipation and\nstructural integrity under dynamic loading. The study provides a detailed analysis of specific energy absorption (SEA)\nand efficiency, offering insights into optimal micro-lattice structure designs\nfor impact resistance in lightweight UAS applications.","PeriodicalId":501083,"journal":{"name":"arXiv - PHYS - Applied Physics","volume":null,"pages":null},"PeriodicalIF":0.0000,"publicationDate":"2024-08-06","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Polymer Micro-Lattice buffer structure Free Impact absorption\",\"authors\":\"Louis Catar, Ilyass Tabiai, David St-Onge\",\"doi\":\"arxiv-2408.02909\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The uncrewed aerial systems industry is rapidly expanding due to advancements\\nin smaller electronics, smarter sensors, advanced flight controllers, and\\nembedded perception modules leveraging artificial intelligence. These\\ntechnological progress have opened new indoor applications for UAS, including\\nwarehouse inventory management, security inspections of public spaces and\\nfacilities, and underground exploration. Despite the innovative designs from\\nUAS manufacturers, there are no existing standards to ensure UAS and human\\nsafety in these environments. This study explores developing and evaluating\\nmicro-lattice structures for impact resistance in lightweight UAS. We examine\\npatch designs using Face-Centered Cubic (FCC), Diamond (D), Kelvin (K), and\\nGyroid (GY) patterns and detail the processes for creating samples for impact\\nand compression tests, including manufacturing and testing protocols. Our evaluation includes compression and impact tests to assess structural\\nbehavior, revealing the influence of geometry, compactness, and material\\nproperties. Diamond and Kelvin patterns were particularly effective in load\\ndistribution and energy absorption over the compression tests. Impact tests\\ndemonstrated significant differences in response between flexible and rigid\\nmaterials, with flexible patches exhibiting superior energy dissipation and\\nstructural integrity under dynamic loading. The study provides a detailed analysis of specific energy absorption (SEA)\\nand efficiency, offering insights into optimal micro-lattice structure designs\\nfor impact resistance in lightweight UAS applications.\",\"PeriodicalId\":501083,\"journal\":{\"name\":\"arXiv - PHYS - Applied Physics\",\"volume\":null,\"pages\":null},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2024-08-06\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"arXiv - PHYS - Applied Physics\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/arxiv-2408.02909\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"arXiv - PHYS - Applied Physics","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/arxiv-2408.02909","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0

摘要

由于小型电子设备、更智能的传感器、先进的飞行控制器和利用人工智能的嵌入式感知模块的进步,无人驾驶航空系统行业正在迅速扩大。这些技术进步为无人机系统开辟了新的室内应用领域,包括仓库库存管理、公共场所和设施的安全检查以及地下勘探。尽管无人机系统制造商进行了创新设计,但目前还没有确保无人机系统和人类在这些环境中安全的标准。本研究探讨了开发和评估轻型无人机系统抗冲击的微格结构。我们研究了使用面心立方(FCC)、钻石(D)、开尔文(K)和甲状腺(GY)图案的补丁设计,并详细介绍了创建用于冲击和压缩测试的样品的过程,包括制造和测试协议。我们的评估包括压缩和冲击测试,以评估结构行为,揭示几何形状、密实度和材料特性的影响。在压缩试验中,菱形和开尔文图案在负载分布和能量吸收方面尤为有效。冲击测试表明,柔性材料和刚性材料在响应上存在显著差异,柔性补丁在动态加载下表现出更优越的能量耗散和结构完整性。该研究详细分析了比能量吸收(SEA)和效率,为轻型无人机应用中抗冲击的最佳微晶格结构设计提供了启示。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
Polymer Micro-Lattice buffer structure Free Impact absorption
The uncrewed aerial systems industry is rapidly expanding due to advancements in smaller electronics, smarter sensors, advanced flight controllers, and embedded perception modules leveraging artificial intelligence. These technological progress have opened new indoor applications for UAS, including warehouse inventory management, security inspections of public spaces and facilities, and underground exploration. Despite the innovative designs from UAS manufacturers, there are no existing standards to ensure UAS and human safety in these environments. This study explores developing and evaluating micro-lattice structures for impact resistance in lightweight UAS. We examine patch designs using Face-Centered Cubic (FCC), Diamond (D), Kelvin (K), and Gyroid (GY) patterns and detail the processes for creating samples for impact and compression tests, including manufacturing and testing protocols. Our evaluation includes compression and impact tests to assess structural behavior, revealing the influence of geometry, compactness, and material properties. Diamond and Kelvin patterns were particularly effective in load distribution and energy absorption over the compression tests. Impact tests demonstrated significant differences in response between flexible and rigid materials, with flexible patches exhibiting superior energy dissipation and structural integrity under dynamic loading. The study provides a detailed analysis of specific energy absorption (SEA) and efficiency, offering insights into optimal micro-lattice structure designs for impact resistance in lightweight UAS applications.
求助全文
通过发布文献求助,成功后即可免费获取论文全文。 去求助
来源期刊
自引率
0.00%
发文量
0
期刊最新文献
Ultrafast cascade charge transfer in multi bandgap colloidal quantum dot solids enables threshold reduction for optical gain and stimulated emission p-(001)NiO/n-(0001)ZnO Heterostructures based Ultraviolet Photodetectors Normal/inverse Doppler effect of backward volume magnetostatic spin waves Unattended field measurement of bird source level Fabrication of Ultra-Thick Masks for X-ray Phase Contrast Imaging at Higher Energy
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 联系我们:info@booksci.cn
Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。
Copyright © 2023 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1