Xingxing Huang , Shuncheng Zhang , Kang Han , Zhenyu Lu , Liang Guo , Ming Sun
{"title":"大型车身散热器的温度适应性分析和测试","authors":"Xingxing Huang , Shuncheng Zhang , Kang Han , Zhenyu Lu , Liang Guo , Ming Sun","doi":"10.1016/j.csite.2024.105476","DOIUrl":null,"url":null,"abstract":"<div><div>This paper addresses the issue of thermal stress release in large-scale body-mounted radiator for China space station telescope under extreme temperature differences of 80 °C. To address this challenge, an innovative floating combined stress release support mechanism is proposed. Initially, the stress release mechanism for the radiator is designed with an “orthogonal + parallel” layout based on key factors such as radiator size, operating conditions, and thermal stress. Subsequently, through this layout design, specific modeling is conducted for the fixed support point, line-degree-of-freedom release mechanism, and plane-degree-of-freedom release mechanism of the stress release support mechanism. Utilizing elastic mechanics theory, the deformation of the radiator cooling panel is determined to be 2.51 mm, leading to the design of a support mechanism with a release capacity of 5 mm. Finally, the effectiveness of the design is verified through finite element simulation analysis and experimental validation. Thermal-elastic simulation analysis reveals that the strain of the radiator cooling panel under an 80 °C temperature load is 2.75 mm, representing an error of 8 % compared to the theoretical calculation. The maximum stress of 315 MPa in the radiator cooling panel and 873 MPa in the support mechanism are less than the yield strength of the respective materials. Experimental results indicate that during a temperature change of 30 °C, the lateral deformation of the radiator is 0.85 mm, differing by 17.48 % from the simulation analysis result of 1.03 mm for a ΔT of 30 °C. These errors fall within an acceptable range and meet the design requirements. The results strongly confirm that the designed stress release support mechanism can effectively release thermal stress in large-scale body-mounted radiator while ensuring that the deformation of the radiator remains within the safe range of the sliding distance of the stress release support mechanism.</div></div>","PeriodicalId":9658,"journal":{"name":"Case Studies in Thermal Engineering","volume":"64 ","pages":"Article 105476"},"PeriodicalIF":6.4000,"publicationDate":"2024-11-12","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Analysis and testing of temperature adaptability of large-scale body-mounted radiator\",\"authors\":\"Xingxing Huang , Shuncheng Zhang , Kang Han , Zhenyu Lu , Liang Guo , Ming Sun\",\"doi\":\"10.1016/j.csite.2024.105476\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>This paper addresses the issue of thermal stress release in large-scale body-mounted radiator for China space station telescope under extreme temperature differences of 80 °C. To address this challenge, an innovative floating combined stress release support mechanism is proposed. Initially, the stress release mechanism for the radiator is designed with an “orthogonal + parallel” layout based on key factors such as radiator size, operating conditions, and thermal stress. Subsequently, through this layout design, specific modeling is conducted for the fixed support point, line-degree-of-freedom release mechanism, and plane-degree-of-freedom release mechanism of the stress release support mechanism. Utilizing elastic mechanics theory, the deformation of the radiator cooling panel is determined to be 2.51 mm, leading to the design of a support mechanism with a release capacity of 5 mm. Finally, the effectiveness of the design is verified through finite element simulation analysis and experimental validation. Thermal-elastic simulation analysis reveals that the strain of the radiator cooling panel under an 80 °C temperature load is 2.75 mm, representing an error of 8 % compared to the theoretical calculation. The maximum stress of 315 MPa in the radiator cooling panel and 873 MPa in the support mechanism are less than the yield strength of the respective materials. Experimental results indicate that during a temperature change of 30 °C, the lateral deformation of the radiator is 0.85 mm, differing by 17.48 % from the simulation analysis result of 1.03 mm for a ΔT of 30 °C. These errors fall within an acceptable range and meet the design requirements. The results strongly confirm that the designed stress release support mechanism can effectively release thermal stress in large-scale body-mounted radiator while ensuring that the deformation of the radiator remains within the safe range of the sliding distance of the stress release support mechanism.</div></div>\",\"PeriodicalId\":9658,\"journal\":{\"name\":\"Case Studies in Thermal Engineering\",\"volume\":\"64 \",\"pages\":\"Article 105476\"},\"PeriodicalIF\":6.4000,\"publicationDate\":\"2024-11-12\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Case Studies in Thermal Engineering\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S2214157X24015077\",\"RegionNum\":2,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"THERMODYNAMICS\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Case Studies in Thermal Engineering","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S2214157X24015077","RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"THERMODYNAMICS","Score":null,"Total":0}
Analysis and testing of temperature adaptability of large-scale body-mounted radiator
This paper addresses the issue of thermal stress release in large-scale body-mounted radiator for China space station telescope under extreme temperature differences of 80 °C. To address this challenge, an innovative floating combined stress release support mechanism is proposed. Initially, the stress release mechanism for the radiator is designed with an “orthogonal + parallel” layout based on key factors such as radiator size, operating conditions, and thermal stress. Subsequently, through this layout design, specific modeling is conducted for the fixed support point, line-degree-of-freedom release mechanism, and plane-degree-of-freedom release mechanism of the stress release support mechanism. Utilizing elastic mechanics theory, the deformation of the radiator cooling panel is determined to be 2.51 mm, leading to the design of a support mechanism with a release capacity of 5 mm. Finally, the effectiveness of the design is verified through finite element simulation analysis and experimental validation. Thermal-elastic simulation analysis reveals that the strain of the radiator cooling panel under an 80 °C temperature load is 2.75 mm, representing an error of 8 % compared to the theoretical calculation. The maximum stress of 315 MPa in the radiator cooling panel and 873 MPa in the support mechanism are less than the yield strength of the respective materials. Experimental results indicate that during a temperature change of 30 °C, the lateral deformation of the radiator is 0.85 mm, differing by 17.48 % from the simulation analysis result of 1.03 mm for a ΔT of 30 °C. These errors fall within an acceptable range and meet the design requirements. The results strongly confirm that the designed stress release support mechanism can effectively release thermal stress in large-scale body-mounted radiator while ensuring that the deformation of the radiator remains within the safe range of the sliding distance of the stress release support mechanism.
期刊介绍:
Case Studies in Thermal Engineering provides a forum for the rapid publication of short, structured Case Studies in Thermal Engineering and related Short Communications. It provides an essential compendium of case studies for researchers and practitioners in the field of thermal engineering and others who are interested in aspects of thermal engineering cases that could affect other engineering processes. The journal not only publishes new and novel case studies, but also provides a forum for the publication of high quality descriptions of classic thermal engineering problems. The scope of the journal includes case studies of thermal engineering problems in components, devices and systems using existing experimental and numerical techniques in the areas of mechanical, aerospace, chemical, medical, thermal management for electronics, heat exchangers, regeneration, solar thermal energy, thermal storage, building energy conservation, and power generation. Case studies of thermal problems in other areas will also be considered.