SRM复合材料壳体固化过程参数的全局敏感性分析

Qun Liang, Xi-ping Feng, Kun Zhang, Jian Li, Shu-hua Chen, Xiao Hou
{"title":"SRM复合材料壳体固化过程参数的全局敏感性分析","authors":"Qun Liang,&nbsp;Xi-ping Feng,&nbsp;Kun Zhang,&nbsp;Jian Li,&nbsp;Shu-hua Chen,&nbsp;Xiao Hou","doi":"10.1007/s42423-021-00072-7","DOIUrl":null,"url":null,"abstract":"<div><p>The case for modern solid rocket motor (SRM) is a complex compose structure with fiber reinforced resin matrix composite, insulation layer and metal connections, the case forming process is a multi-physical–chemical process which involving heat transfer, chemical reaction and structure deformation. During the cure process, temperature determines whether the case cure completely and the uniformity of temperature field is an important factor in causing residual thermal stress and shrinkage stress, so temperature field is the key to the mutual coupling effect of each physical and chemical process, and the basis to analyze the cure process of the case. During the cure process of case, fluctuation of cure temperature, cure time or heat transfer of hot air in the furnace may occur, which make the actual forming process of case deviate from the ideal cure process. In order to investigate the sensitive degree of thermal cycle, convective heat transfer coefficient and thermal properties to cure uniformity during cure process of composite case, the influence rule of the three factors on uniformity of temperature and cure degree fields were analyzed by numerical simulation. A thermal-chemical model was built for a simplified composite SRM case firstly, and the model was verified. Then, the influence degree of the three factors on cure uniformity of composite case was analyzed and quantized by the Morris global sensitivity analysis method. The results show that he sensitivity order of the uniformity of temperature field for the four parameters is: thermal diffusion coefficient &gt; heat transfer coefficient &gt; duration time &gt; cure temperature. Besides, he temperature and duration time of the fourth dwell stage have less effect on the cure uniformity of composite case than that of heat transfer coefficient. Therefore, it is a challenge to design a thermal cycle that can not only guarantee the vulcanization of EPDM insulation layer, but also improve the cure uniformity.</p></div>","PeriodicalId":100039,"journal":{"name":"Advances in Astronautics Science and Technology","volume":"4 1","pages":"19 - 26"},"PeriodicalIF":0.0000,"publicationDate":"2021-04-03","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://sci-hub-pdf.com/10.1007/s42423-021-00072-7","citationCount":"0","resultStr":"{\"title\":\"Global Sensitivity Analysis of Parameters During Cure Process of SRM Composite Case\",\"authors\":\"Qun Liang,&nbsp;Xi-ping Feng,&nbsp;Kun Zhang,&nbsp;Jian Li,&nbsp;Shu-hua Chen,&nbsp;Xiao Hou\",\"doi\":\"10.1007/s42423-021-00072-7\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><p>The case for modern solid rocket motor (SRM) is a complex compose structure with fiber reinforced resin matrix composite, insulation layer and metal connections, the case forming process is a multi-physical–chemical process which involving heat transfer, chemical reaction and structure deformation. During the cure process, temperature determines whether the case cure completely and the uniformity of temperature field is an important factor in causing residual thermal stress and shrinkage stress, so temperature field is the key to the mutual coupling effect of each physical and chemical process, and the basis to analyze the cure process of the case. During the cure process of case, fluctuation of cure temperature, cure time or heat transfer of hot air in the furnace may occur, which make the actual forming process of case deviate from the ideal cure process. In order to investigate the sensitive degree of thermal cycle, convective heat transfer coefficient and thermal properties to cure uniformity during cure process of composite case, the influence rule of the three factors on uniformity of temperature and cure degree fields were analyzed by numerical simulation. A thermal-chemical model was built for a simplified composite SRM case firstly, and the model was verified. Then, the influence degree of the three factors on cure uniformity of composite case was analyzed and quantized by the Morris global sensitivity analysis method. The results show that he sensitivity order of the uniformity of temperature field for the four parameters is: thermal diffusion coefficient &gt; heat transfer coefficient &gt; duration time &gt; cure temperature. Besides, he temperature and duration time of the fourth dwell stage have less effect on the cure uniformity of composite case than that of heat transfer coefficient. Therefore, it is a challenge to design a thermal cycle that can not only guarantee the vulcanization of EPDM insulation layer, but also improve the cure uniformity.</p></div>\",\"PeriodicalId\":100039,\"journal\":{\"name\":\"Advances in Astronautics Science and Technology\",\"volume\":\"4 1\",\"pages\":\"19 - 26\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2021-04-03\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"https://sci-hub-pdf.com/10.1007/s42423-021-00072-7\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Advances in Astronautics Science and Technology\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://link.springer.com/article/10.1007/s42423-021-00072-7\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Advances in Astronautics Science and Technology","FirstCategoryId":"1085","ListUrlMain":"https://link.springer.com/article/10.1007/s42423-021-00072-7","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

现代固体火箭发动机壳体是一个由纤维增强树脂基复合材料、绝缘层和金属连接组成的复杂结构,壳体的形成过程是一个涉及传热、化学反应和结构变形的多物理-化学过程。在固化过程中,温度决定了固化体是否完全固化,温度场的均匀性是造成残余热应力和收缩应力的重要因素,因此温度场是各个物理化学过程相互耦合作用的关键,也是分析固化体固化过程的基础。在壳体的固化过程中,可能会出现固化温度、固化时间或炉内热空气传热的波动,使壳体的实际成型过程偏离理想的固化过程。为了研究复合材料固化过程中热循环、对流传热系数和热性能对固化均匀性的敏感程度,通过数值模拟分析了三个因素对温度场和固化度场均匀性的影响规律。首先建立了一个简化的复合材料SRM壳的热化学模型,并对该模型进行了验证。然后,采用Morris全局灵敏度分析方法,对三个因素对复合材料固化均匀性的影响程度进行了分析和量化。结果表明,四个参数对温度场均匀性的灵敏度阶为:热扩散系数 >; 传热系数 >; 持续时间 >; 固化温度。此外,第四停留阶段的温度和持续时间对复合材料固化均匀性的影响小于对传热系数的影响。因此,设计一种既能保证三元乙丙橡胶绝缘层硫化,又能提高固化均匀性的热循环是一项挑战。
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
Global Sensitivity Analysis of Parameters During Cure Process of SRM Composite Case

The case for modern solid rocket motor (SRM) is a complex compose structure with fiber reinforced resin matrix composite, insulation layer and metal connections, the case forming process is a multi-physical–chemical process which involving heat transfer, chemical reaction and structure deformation. During the cure process, temperature determines whether the case cure completely and the uniformity of temperature field is an important factor in causing residual thermal stress and shrinkage stress, so temperature field is the key to the mutual coupling effect of each physical and chemical process, and the basis to analyze the cure process of the case. During the cure process of case, fluctuation of cure temperature, cure time or heat transfer of hot air in the furnace may occur, which make the actual forming process of case deviate from the ideal cure process. In order to investigate the sensitive degree of thermal cycle, convective heat transfer coefficient and thermal properties to cure uniformity during cure process of composite case, the influence rule of the three factors on uniformity of temperature and cure degree fields were analyzed by numerical simulation. A thermal-chemical model was built for a simplified composite SRM case firstly, and the model was verified. Then, the influence degree of the three factors on cure uniformity of composite case was analyzed and quantized by the Morris global sensitivity analysis method. The results show that he sensitivity order of the uniformity of temperature field for the four parameters is: thermal diffusion coefficient > heat transfer coefficient > duration time > cure temperature. Besides, he temperature and duration time of the fourth dwell stage have less effect on the cure uniformity of composite case than that of heat transfer coefficient. Therefore, it is a challenge to design a thermal cycle that can not only guarantee the vulcanization of EPDM insulation layer, but also improve the cure uniformity.

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
CiteScore
1.20
自引率
0.00%
发文量
0
期刊最新文献
Research on Overload Characteristics of Projectile Penetrating Layered Protective Structures with High-Velocity Video Information-Based Liquid Rocket Engine Fault Simulation Test Method under Complex Environment Preface Game Strategies Against High Orbit Surveillance Satellites Orbital Rendezvous Guidance Strategy for Time-Sensitive Missions
×
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