Chenzhou Liang , Shanyong Xuan , Hailong Yang , Yimeng Shan , Xuefeng Yao
{"title":"带状修复层合板固化残余应力的数值分析","authors":"Chenzhou Liang , Shanyong Xuan , Hailong Yang , Yimeng Shan , Xuefeng Yao","doi":"10.1016/j.compstruct.2025.119420","DOIUrl":null,"url":null,"abstract":"<div><div>Among the current repair technologies for aircraft composite structures, scarfed repair with composite patches using vacuum bag curing technology is considered to be a repair method that takes both efficiency and reliability into account. During the molding process of composite material patches, process stresses arise in the patch. Determination of residual process stresses is a primary task for the modeling of the repair process. To achieve this objective, a numerical simulation framework is developed to model the curing deformation and residual stresses that arise in the scarf-repaired structure during the composite patch curing process. The framework incorporates the curing reaction, resin modulus variation, and volume changes during the repair process. Subsequently, the distribution of process-induced stress and deformation in repaired structures were analyzed. Finally, the effects of different heating rates and maximum curing temperatures on curing deformation and residual stresses were explored. The results showed that increasing the curing temperature and heating rate can shorten the repair time, but at the expense of increasing residual stresses in repaired structures.</div></div>","PeriodicalId":281,"journal":{"name":"Composite Structures","volume":"370 ","pages":"Article 119420"},"PeriodicalIF":7.1000,"publicationDate":"2025-06-23","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Numerical analysis of curing residual stresses in scarf-repaired laminates\",\"authors\":\"Chenzhou Liang , Shanyong Xuan , Hailong Yang , Yimeng Shan , Xuefeng Yao\",\"doi\":\"10.1016/j.compstruct.2025.119420\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>Among the current repair technologies for aircraft composite structures, scarfed repair with composite patches using vacuum bag curing technology is considered to be a repair method that takes both efficiency and reliability into account. During the molding process of composite material patches, process stresses arise in the patch. Determination of residual process stresses is a primary task for the modeling of the repair process. To achieve this objective, a numerical simulation framework is developed to model the curing deformation and residual stresses that arise in the scarf-repaired structure during the composite patch curing process. The framework incorporates the curing reaction, resin modulus variation, and volume changes during the repair process. Subsequently, the distribution of process-induced stress and deformation in repaired structures were analyzed. Finally, the effects of different heating rates and maximum curing temperatures on curing deformation and residual stresses were explored. The results showed that increasing the curing temperature and heating rate can shorten the repair time, but at the expense of increasing residual stresses in repaired structures.</div></div>\",\"PeriodicalId\":281,\"journal\":{\"name\":\"Composite Structures\",\"volume\":\"370 \",\"pages\":\"Article 119420\"},\"PeriodicalIF\":7.1000,\"publicationDate\":\"2025-06-23\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Composite Structures\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S0263822325005859\",\"RegionNum\":2,\"RegionCategory\":\"材料科学\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"MATERIALS SCIENCE, COMPOSITES\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Composite Structures","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0263822325005859","RegionNum":2,"RegionCategory":"材料科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"MATERIALS SCIENCE, COMPOSITES","Score":null,"Total":0}
Numerical analysis of curing residual stresses in scarf-repaired laminates
Among the current repair technologies for aircraft composite structures, scarfed repair with composite patches using vacuum bag curing technology is considered to be a repair method that takes both efficiency and reliability into account. During the molding process of composite material patches, process stresses arise in the patch. Determination of residual process stresses is a primary task for the modeling of the repair process. To achieve this objective, a numerical simulation framework is developed to model the curing deformation and residual stresses that arise in the scarf-repaired structure during the composite patch curing process. The framework incorporates the curing reaction, resin modulus variation, and volume changes during the repair process. Subsequently, the distribution of process-induced stress and deformation in repaired structures were analyzed. Finally, the effects of different heating rates and maximum curing temperatures on curing deformation and residual stresses were explored. The results showed that increasing the curing temperature and heating rate can shorten the repair time, but at the expense of increasing residual stresses in repaired structures.
期刊介绍:
The past few decades have seen outstanding advances in the use of composite materials in structural applications. There can be little doubt that, within engineering circles, composites have revolutionised traditional design concepts and made possible an unparalleled range of new and exciting possibilities as viable materials for construction. Composite Structures, an International Journal, disseminates knowledge between users, manufacturers, designers and researchers involved in structures or structural components manufactured using composite materials.
The journal publishes papers which contribute to knowledge in the use of composite materials in engineering structures. Papers deal with design, research and development studies, experimental investigations, theoretical analysis and fabrication techniques relevant to the application of composites in load-bearing components for assemblies, ranging from individual components such as plates and shells to complete composite structures.