首页|飞行器结构密封胶界面性能表征与失效过程

飞行器结构密封胶界面性能表征与失效过程

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密封胶是飞行器结构的重要组成部分,是结构密封安全性的基本保障.如果密封胶的性能参数不达标,则可能达不到其设计目标.对新型HM109改性聚硫密封胶进行测试分析,利用有限元软件开展模拟计算,使用Cohesive单元实现对密封胶层的模拟.通过观察胶层失效过程,确定飞行器密封结构在大载荷情况下密封胶层失效的过程;通过对比试验结果和模拟计算结果,验证有限元分析的可靠性.结果表明:试验所测得的参数应用于有限元模拟所得结果与试验结果基本一致,拉伸和剪切模拟最大载荷与试验平均结果误差分别约为3.74%、1.50%,模拟结果具有可靠性.
Interface Properties Characterization and Failure Process of Structural Sealant of Aircrafts
Sealant is an important component of aircraft structures and the basic guarantee of structural seal safety.If the performance parameters of sealant are not up to standard,it's impossible to achieve the design goal.A new HM109 modified polysulfide sealant was tested and analyzed,and simulation calculation was carried out by finite element simulation software,with Cohesive element used to simulate the sealant layer.By observing the failure process of the sealant layer,the failure process of the sealant layer of aircraft seal structure under heavy load was determined.The reliability of finite element simulation analysis was verified by comparing the test results with the simulation results.The results show that the measured parameters are applied to the finite element simulation,and the simulation results are basically consistent with the test results.The error between the simulated results and the average test results is about 3.74%and 1.5%,and the simulation results are reliable.

sealantperformance testfinite element analysisseal failure

陈鑫、李振威、徐明鸽、贺译贤、陶林

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北京强度环境研究所,北京 100076

天津航天瑞莱科技有限公司,天津 300462

同济大学 航空航天与力学学院,上海 200092

密封胶 性能测试 有限元分析 密封失效

国家自然科学基金青年基金上海市青年科技英才"扬帆计划"项目

5230210823YF1448800

2024

失效分析与预防
南昌航空大学 北京航空材料研究院

失效分析与预防

影响因子:0.352
ISSN:1673-6214
年,卷(期):2024.19(2)
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