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冲击载荷下法兰连接螺栓结构强度评估方法

陈景阳 李百洋

陈景阳, 李百洋. 冲击载荷下法兰连接螺栓结构强度评估方法[J]. 航空动力学报, 2025, 40(5):20230560 doi: 10.13224/j.cnki.jasp.20230560
引用本文: 陈景阳, 李百洋. 冲击载荷下法兰连接螺栓结构强度评估方法[J]. 航空动力学报, 2025, 40(5):20230560 doi: 10.13224/j.cnki.jasp.20230560
CHEN Jingyang, LI Baiyang. Strength evaluation method of flange connection bolt structure under impact load[J]. Journal of Aerospace Power, 2025, 40(5):20230560 doi: 10.13224/j.cnki.jasp.20230560
Citation: CHEN Jingyang, LI Baiyang. Strength evaluation method of flange connection bolt structure under impact load[J]. Journal of Aerospace Power, 2025, 40(5):20230560 doi: 10.13224/j.cnki.jasp.20230560

冲击载荷下法兰连接螺栓结构强度评估方法

doi: 10.13224/j.cnki.jasp.20230560
基金项目: 国家重点研发计划(2021YFB3302200)
详细信息
    作者简介:

    陈景阳(1986-),男,高级工程师,硕士,主要从事航空发动机结构强度研究。E-mail:chen34040219@163.com

  • 中图分类号: V232.7;O344.5

Strength evaluation method of flange connection bolt structure under impact load

  • 摘要:

    针对冲击载荷下法兰连接螺栓结构强度评估方法研究开展研究。设计并加工动态力学性能材料试验件,通过试验获取螺栓材料动态力学行为模型,试验表明螺栓用材料IN718具有明显的应变率强化效应,在中高应变率条件下,材料的屈服强度和抗拉强度均有所提高;设计并加工断裂力学模型标定试验件,通过试验表明不同应力状态下材料断裂力学试验表明螺栓用材料的断裂应变与材料所受应力空间状态相关。并建立考虑应力三轴度和罗德角的螺栓材料断裂力学模型。最终基于上述材料试验结果结合仿真建立起螺栓冲击载荷下强度评估方法。通过冲击试验结果与评估分析结果对比表明,在给定冲击载荷条件下,所建立的综合考虑螺栓材料动态力学性能和断裂力学性能的评估结果与试验结果吻合,在1500 J冲击能量下,螺栓未发生断裂。而传统力学评估方法结果表明螺栓发生断裂,评估结果偏于保守。

     

  • 图 1  冲击载荷下螺栓强度评估流程

    Figure 1.  Process for evaluating bolt strength under impact load

    图 2  IN718动态力学性能试验件

    Figure 2.  IN718 specimen in dynamic testing

    图 3  不同应变率下应力-塑性应变曲线

    Figure 3.  Stress-plastic strain curves under different strain rates

    图 4  应变率与抗拉强度、屈服强度的关系

    Figure 4.  Relationship between strain rate and tensile strength, yield strength

    图 5  4种反应不同受力状态的试样(单位:mm)

    Figure 5.  Four types of test specimens with different stress states (unit:mm)

    图 6  各组试验载荷-位移曲线

    Figure 6.  Load-displacement curves for each group of tests

    图 7  断裂模型标定流程

    Figure 7.  Calibration process of facture model

    图 8  断裂模型标定仿真模型

    Figure 8.  Calibration finite element model of facture model

    图 9  试验与仿真载荷-位移曲线对比

    Figure 9.  Comparison of test and simulation displacement-load curves

    图 10  试验与仿真断裂模式对比

    Figure 10.  Comparison of test and simulation fracture modes

    图 11  考虑应变率效应的MMC 3D断裂面

    Figure 11.  MMC 3D-fracture surface with considering strain rate effect

    图 12  仿真模型

    Figure 12.  Finite element model

    图 13  材料模型

    Figure 13.  Material model

    图 14  接触边界条件

    Figure 14.  Contact boundary conditions

    图 15  仿真计算结果

    Figure 15.  Simulation results

    图 16  试验件

    Figure 16.  Test specimens

    图 17  冲击载荷加载装置

    Figure 17.  Impact load loading device

    图 18  试验后螺栓试验件形貌

    Figure 18.  Morphology of bolt test specimens after testing

    图 19  2000 J冲击能量下仿真与试验结果对比

    Figure 19.  Comparison of simulation and test results under 2000 J impact energy

    图 20  2 500 J冲击能量下仿真与试验结果对比

    Figure 20.  Comparison of simulation and test results under 2 500 J impact energy

    表  1  各试样应力三轴度、罗德角与等效断裂应变

    Table  1.   Stress triaxiality,Lode parameter and effective fracture strain

    试样 $ \eta $ $ \bar {\theta } $ $ {\varepsilon }_{{\mathrm{f}}} $
    颈缩平板试样SG1 0.47 0.94 0.13
    颈缩棒材试样SG2 0.61 0.99 0.17
    标准拉伸试样SG3 0.33 1.00 0.274
    纯剪切试样SG4 0 0 0.435
    下载: 导出CSV

    表  2  MMC断裂模型参数

    Table  2.   Fracture parameters of MMC model

    材料 A n c1 c2 c3
    IN718 1651.9 0.0621 0.223 2472.5 1.98
    下载: 导出CSV

    表  3  两种评估方案结果对比

    Table  3.   Comparison of results between two evaluation projects

    方案 冲击
    能量/J
    等效前端
    载荷/kN
    螺栓失效
    情况
    螺栓等效应力/
    MPa
    1 1500 502 未断裂 1638
    2 1500 502 全部断裂 1204
    下载: 导出CSV
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  • 收稿日期:  2023-09-03
  • 网络出版日期:  2024-09-03

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