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拧紧力矩对线束与卡箍装配体的数值分析OACSTPCD

Numerical Analysis of Tightening Torque on Harness and Clamp Assembly

中文摘要英文摘要

采用Mooney-Rivlin本构模型描述卡箍橡胶衬垫的力学特性,借助Workbench有限元软件建立线束与卡箍装配的有限元模型,采用数值计算的方法研究不同拧紧力矩作用下线束与卡箍装配体的受力变化规律.结果表明:在卡箍耳片贴合后,不同力矩下卡箍与线束之间的受力变形特点相似,卡箍应力和接触面内的接触压力随力矩变化呈现先增大后不变的趋势.结合拉脱力试验平台,验证了仿真分析的准确性,可为飞机线束与卡箍装配研究提供参考.

The Mooney Rivlin constitutive model is used to describe the mechanical properties of the clamp rubber gasket,and the finite element model of the harness and clamp assembly is established with the help of the workbench finite element software.The stress variation law of the harness and clamp assembly under different tightening torque is studied by numerical calculation.The results show that the stress deformation characteristics between the clamp and the harness are similar under different torques after the clamp lugs are fitted.The clamp stress and the contact pressure in the contact surface show a trend of first increasing and then changing with the torque.Combined with the pull-out force test platform,the reliability of simulation analysis is verified,which provides reference for further research on aircraft harness and clamp assembly.

裴龙涛;闫静;陆珊珊;张忆鑫

南京航空航天大学机电学院,江苏南京 210016

卡箍拧紧力矩Mooney-Rivlin本构模型有限元分析

clamptightening torqueMooney-Rivlin constitutive modelfinite element analysis

《机械制造与自动化》 2024 (003)

50-53,83 / 5

国家商用飞机制造工程技术研究中心创新基金资助项目(SAMC13-JS-15-024)

10.19344/j.cnki.issn1671-5276.2024.03.010

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