Design Engineering of High-Energy Absorbent Aircrew Helmet Using 3D Woven Structural Composite

IF 2.3 4区 材料科学 Q3 MATERIALS SCIENCE, COMPOSITES Applied Composite Materials Pub Date : 2024-09-04 DOI:10.1007/s10443-024-10261-w
Omender Singh, Shivangi Shukla, Jaya Sharma, B. K. Behera
{"title":"Design Engineering of High-Energy Absorbent Aircrew Helmet Using 3D Woven Structural Composite","authors":"Omender Singh, Shivangi Shukla, Jaya Sharma, B. K. Behera","doi":"10.1007/s10443-024-10261-w","DOIUrl":null,"url":null,"abstract":"<p>This study investigated the effectiveness of 3D woven structural composite-based aircrew helmets comprising a 3D woven solid shell and a 3D woven honeycomb liner. This research adopted a structured sequence of steps to integrate desired aircrew helmet properties. The study involved the analysis of 3D woven structural composites through quasistatic compression and dynamic impact tests to assess their compressive strength and impact energy properties, respectively. Initially, the study focuses on optimizing the honeycomb liner by adjusting its structural parameters to improve the compressive strength. The research then delved into the critical role of impact energy, aiming to enhance load transfer to the liner for maximal impact energy absorption. Key findings highlight that the L2T2H3 honeycomb liner configuration, when combined with the OR8L3M shell, significantly improves the protective performance by exhibiting superior impact energy, cushioning properties, and compressive strength. Factors such as weave architecture, impactor geometry, impactor velocity, and face sheet thickness were found to influence the energy absorption capacity, emphasizing the importance of structural design optimization. The combined use of helmet shell and liner components demonstrated superior energy absorption capabilities compared to individual components. This combination suggests a successful approach for achieving enhanced performance in aircrew helmets. By analyzing compressive strength and impact energy, this research contributes to the ongoing efforts to enhance the performance of aircrew helmets, thereby ensuring improved safety and protection for aircrew members operating in high-risk environments.</p>","PeriodicalId":468,"journal":{"name":"Applied Composite Materials","volume":null,"pages":null},"PeriodicalIF":2.3000,"publicationDate":"2024-09-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Applied Composite Materials","FirstCategoryId":"88","ListUrlMain":"https://doi.org/10.1007/s10443-024-10261-w","RegionNum":4,"RegionCategory":"材料科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q3","JCRName":"MATERIALS SCIENCE, COMPOSITES","Score":null,"Total":0}
引用次数: 0

Abstract

This study investigated the effectiveness of 3D woven structural composite-based aircrew helmets comprising a 3D woven solid shell and a 3D woven honeycomb liner. This research adopted a structured sequence of steps to integrate desired aircrew helmet properties. The study involved the analysis of 3D woven structural composites through quasistatic compression and dynamic impact tests to assess their compressive strength and impact energy properties, respectively. Initially, the study focuses on optimizing the honeycomb liner by adjusting its structural parameters to improve the compressive strength. The research then delved into the critical role of impact energy, aiming to enhance load transfer to the liner for maximal impact energy absorption. Key findings highlight that the L2T2H3 honeycomb liner configuration, when combined with the OR8L3M shell, significantly improves the protective performance by exhibiting superior impact energy, cushioning properties, and compressive strength. Factors such as weave architecture, impactor geometry, impactor velocity, and face sheet thickness were found to influence the energy absorption capacity, emphasizing the importance of structural design optimization. The combined use of helmet shell and liner components demonstrated superior energy absorption capabilities compared to individual components. This combination suggests a successful approach for achieving enhanced performance in aircrew helmets. By analyzing compressive strength and impact energy, this research contributes to the ongoing efforts to enhance the performance of aircrew helmets, thereby ensuring improved safety and protection for aircrew members operating in high-risk environments.

Abstract Image

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
使用三维编织结构复合材料的高能量吸收空勤人员头盔设计工程
本研究调查了基于三维编织结构复合材料的空勤人员头盔的有效性,该头盔由三维编织实心外壳和三维编织蜂窝衬垫组成。这项研究采用了一系列结构化步骤,以整合所需的空勤人员头盔特性。研究包括通过准静态压缩和动态冲击试验对三维编织结构复合材料进行分析,分别评估其抗压强度和冲击能量特性。最初,研究重点是通过调整蜂窝衬垫的结构参数来优化蜂窝衬垫,从而提高抗压强度。随后,研究深入探讨了冲击能量的关键作用,旨在加强对衬垫的载荷传递,以最大限度地吸收冲击能量。主要研究结果表明,L2T2H3蜂窝衬垫配置与OR8L3M外壳相结合,可显著提高防护性能,表现出卓越的冲击能量、缓冲性能和抗压强度。研究发现,编织结构、撞击器几何形状、撞击器速度和面片厚度等因素都会影响能量吸收能力,从而强调了结构设计优化的重要性。与单个部件相比,头盔外壳和衬垫部件的组合使用显示出更出色的能量吸收能力。这种组合是提高空勤人员头盔性能的成功方法。通过分析抗压强度和冲击能量,这项研究有助于不断提高空勤人员头盔的性能,从而确保改善在高风险环境中工作的空勤人员的安全和保护。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 去求助
来源期刊
Applied Composite Materials
Applied Composite Materials 工程技术-材料科学:复合
CiteScore
4.20
自引率
4.30%
发文量
81
审稿时长
1.6 months
期刊介绍: Applied Composite Materials is an international journal dedicated to the publication of original full-length papers, review articles and short communications of the highest quality that advance the development and application of engineering composite materials. Its articles identify problems that limit the performance and reliability of the composite material and composite part; and propose solutions that lead to innovation in design and the successful exploitation and commercialization of composite materials across the widest spectrum of engineering uses. The main focus is on the quantitative descriptions of material systems and processing routes. Coverage includes management of time-dependent changes in microscopic and macroscopic structure and its exploitation from the material''s conception through to its eventual obsolescence.
期刊最新文献
Cutting Force Model of SiCp/Al Composites in Ultrasonic Elliptical Vibration Assisted Cutting with Negative Rake Angle Experimental and Simulation Analysis of the Mechanical Deterioration Mechanisms in SiCp/A356 Composites Under Thermal Cycling Load Design Engineering of High-Energy Absorbent Aircrew Helmet Using 3D Woven Structural Composite Numerical Simulation and Preforming Parameters Optimization of Carbon-Kevlar Hybrid Woven Reinforcement Materials Based on Genetic Algorithm Low Velocity Impact Response of Carbon Fiber Composite Laminates with Surface Glass Fibers
×
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