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螺头/螺母约束状态对螺纹松动特性的影响

张功平 刘文光 黄政 李可昊 成龙

张功平, 刘文光, 黄政, 等. 螺头/螺母约束状态对螺纹松动特性的影响[J]. 航空动力学报, 2025, 40(5):20230675 doi: 10.13224/j.cnki.jasp.20230675
引用本文: 张功平, 刘文光, 黄政, 等. 螺头/螺母约束状态对螺纹松动特性的影响[J]. 航空动力学报, 2025, 40(5):20230675 doi: 10.13224/j.cnki.jasp.20230675
ZHANG Gongping, LIU Wenguang, HUANG Zheng, et al. Effect of bolthead/nut constraint state on thread loosening characteristics[J]. Journal of Aerospace Power, 2025, 40(5):20230675 doi: 10.13224/j.cnki.jasp.20230675
Citation: ZHANG Gongping, LIU Wenguang, HUANG Zheng, et al. Effect of bolthead/nut constraint state on thread loosening characteristics[J]. Journal of Aerospace Power, 2025, 40(5):20230675 doi: 10.13224/j.cnki.jasp.20230675

螺头/螺母约束状态对螺纹松动特性的影响

doi: 10.13224/j.cnki.jasp.20230675
基金项目: 国家自然科学基金(52365012); 江西省自然科学基金(20224ACB204015)
详细信息
    作者简介:

    张功平(1998-),男,硕士生,主要从事螺栓连接结构振动松动研究。E-mail:1974675619@qq.com

    通讯作者:

    刘文光(1978-),男,教授、硕士生导师,博士,主要从事结构动力学和疲劳寿命预测研究。E-mail:liuwg14@nchu.edu.cn

  • 中图分类号: V232;TH131.3;TH122

Effect of bolthead/nut constraint state on thread loosening characteristics

  • 摘要:

    为研究螺头/螺母约束状态对螺纹松动特性的影响,提出了约束螺头或螺母的两种螺纹连接防松结构,建立了单搭接单螺栓连接结构的精细有限元模型,分析了横向振动条件下不同防松模型螺纹松动的过程,并进一步讨论了不同模型在不同加载、螺纹面摩擦因数、承压面摩擦因数等条件下的螺纹松动特性,通过螺纹松动试验验证了防松效果。结果表明:在相同条件下,对于未约束螺头和螺母的普通连接结构,在振动前期螺栓预紧力损失最大,最容易发生松动;对于约束螺头的新型连接结构,其螺栓预紧力衰退最慢、损失最少,具有很好的防松效果;而对于约束螺母的连接结构,其螺纹松动最快,不具有防松效果;工程中可以考虑设计螺头被约束的连接结构,以提高螺纹连接防松能力。

     

  • 图 1  螺头/螺母不同约束状态下的螺栓连接结构

    Figure 1.  Bolted joint structures with different constraint states of the bolthead/nut

    图 2  螺栓连接结构有限元模型

    Figure 2.  Finite element model of bolted joint structure

    图 3  拧紧加载示意图

    Figure 3.  Tightening loading schematic

    图 4  横向振动位移载荷施加过程

    Figure 4.  Transverse vibration displacement load application process

    图 5  有限元方法施加预紧力与理论值的比较

    Figure 5.  Comparison of preload obtained by finite element method and theoretical value

    图 6  螺栓预紧力与旋松角度随加载次数的变化

    Figure 6.  Variation of preload and loosening angle with the vibration cycles

    图 7  螺纹面黏结-滑移接触状态变化

    Figure 7.  Variation of sticking-sliping contact state of thread surfaces

    图 8  不同最大振动幅值下螺栓预紧力的变化

    Figure 8.  Variation of preload for different maximum vibration amplitudes

    图 9  不同最大振动幅值下振动40次后预紧力损失比

    Figure 9.  Preload loss ratio after 40 vibrations with different maximum vibration amplitudes

    图 10  不同螺纹面摩擦因数下螺栓预紧力的变化

    Figure 10.  Variation of preload with different thread surface friction factors

    图 11  不同螺纹面摩擦因数下40次振动后预紧力损失比

    Figure 11.  Preload loss ratio after 40 vibrations with different thread surface friction factors

    图 12  不同承压面摩擦因数下螺栓预紧力的变化

    Figure 12.  Variation of preload with different friction factors of bearing surface

    图 13  不同承压面摩擦因数下40次振动后预紧力损失比

    Figure 13.  Preload loss ratio after 40 vibrations with different friction factors of bearing surface

    图 14  横向振动试验装置图

    Figure 14.  Transverse vibration tester

    图 15  螺头/螺母不同约束状态试验装配效果图

    Figure 15.  Effect of test assembly of bolthead/nut under different constraint states

    图 16  不同初始预紧力下螺栓预紧力的变化

    Figure 16.  Variation of preload with different initial preloads

    图 17  不同最大振动幅值下螺栓预紧力的变化

    Figure 17.  Variation of preload for different maximum vibration amplitudes

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出版历程
  • 收稿日期:  2023-10-26
  • 网络出版日期:  2024-04-15

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