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转子螺栓连接结构界面滑移损伤机理及影响因素研究

吕东晓 陈雪骑 王东 马艳红 洪杰

吕东晓, 陈雪骑, 王东, 等. 转子螺栓连接结构界面滑移损伤机理及影响因素研究[J]. 航空动力学报, 2025, 40(1):20230027 doi: 10.13224/j.cnki.jasp.20230027
引用本文: 吕东晓, 陈雪骑, 王东, 等. 转子螺栓连接结构界面滑移损伤机理及影响因素研究[J]. 航空动力学报, 2025, 40(1):20230027 doi: 10.13224/j.cnki.jasp.20230027
LYU Dongxiao, CHEN Xueqi, WANG Dong, et al. Mechanism and influential factors research of slip damage in rotor bolted joint structures[J]. Journal of Aerospace Power, 2025, 40(1):20230027 doi: 10.13224/j.cnki.jasp.20230027
Citation: LYU Dongxiao, CHEN Xueqi, WANG Dong, et al. Mechanism and influential factors research of slip damage in rotor bolted joint structures[J]. Journal of Aerospace Power, 2025, 40(1):20230027 doi: 10.13224/j.cnki.jasp.20230027

转子螺栓连接结构界面滑移损伤机理及影响因素研究

doi: 10.13224/j.cnki.jasp.20230027
基金项目: “两机”重大专项基础研究项目(2017-Ⅳ-0011-0048,2017-Ⅶ-0010-0104); 国家自然科学基金(52075018)
详细信息
    作者简介:

    吕东晓(1998-),女,硕士生,研究方向为转子动力学、整机振动故障

    通讯作者:

    陈雪骑(1991-),男,助理研究员,博士,研究方向为转子动力学、整机振动故障排故、界面损伤力学。E-mail:chenxueqi@buaa.edu.cn

  • 中图分类号: V232.4

Mechanism and influential factors research of slip damage in rotor bolted joint structures

  • 摘要:

    针对转子法兰-螺栓连接结构及其所处的载荷环境,考虑了其定位端面和定心柱面变形交互影响的力学过程,并提出了滑移损伤定量评估方法,基于此分析了复杂载荷作用下界面滑移损伤力学过程及其关键影响因素。研究表明:由于转子螺栓连接结构的界面非连续性,其定位端面和定心柱面间不同方向上的变形会交互影响,并且会受到工艺和装配特征参数的影响,实际发动机中由于上述参数随机特性,会导致连接结构界面滑移损伤具有显著的非确定性,引起连接结构发生附加变形并影响转子不平衡状态。

     

  • 图 1  航空发动机典型螺栓连接结构及其载荷

    Figure 1.  Typical bolt joint in an aero engine and its applied loads while operating

    图 2  螺栓连接结构柱面轴向滑移

    Figure 2.  Axial slip between centering cylinders of bolt joint

    图 3  螺栓连接结构端面径向滑移

    Figure 3.  Radial slip between end-faces of bolt joints

    图 4  涡轮前螺栓连接结构有限元模型

    Figure 4.  Finite element model of turbine front bolted connection structure

    图 5  载荷边界条件及加载方式示意图

    Figure 5.  Schematic diagram of load boundary condition and loading method

    图 6  装配-最大工作-卸载状态下各界面接触状态

    Figure 6.  Contact state of various fields under state of assembly-maximum working-unloading

    图 7  装配-最大工作-卸载状态下各界面接触特征表征参数变化

    Figure 7.  Change of characterization parameters of contact characteristics of various surfaces in state of assembly-maximum working-unloading

    图 8  左定心柱面径向滑移特征随转速的变化

    Figure 8.  Changes of axial slip characteristics of left centering cylinder with rotating speed

    图 9  左定位端面轴向滑移特征随转速的变化

    Figure 9.  Changes of axial slip characteristics of left positioning end face with rotating speed

    图 10  定心柱面过盈量对界面接触特征的影响(装配状态)

    Figure 10.  Influence of interference of centering cylinder on interface contact characteristics (assembling condition)

    图 11  定心柱面过盈量对界面接触特征的影响(最大工作状态)

    Figure 11.  Influence of interference of centering cylinder on interface contact characteristics(maximum working condition)

    图 12  定心柱面过盈状态对定心柱面轴向滑移的影响

    Figure 12.  Influence of interference of centering cylinder on axial slip of centering cylinder

    图 13  螺栓预紧力对界面接触特征的影响 (装配状态)

    Figure 13.  Influence of bolt preload on interface contact characteristics (assembling condition)

    图 14  螺栓预紧力对界面接触特征的影响(最大工作状态)

    Figure 14.  Influence of bolt preload on interface contact characteristics (maximum working condition)

    图 15  螺栓预紧力对定心柱面轴向滑移的影响

    Figure 15.  Influence of bolt preload on axial slip of centering cylinder

    表  1  定心柱面过盈量

    Table  1.   Interference of centering cylinder mm

    计算状态最小过盈中间过盈最大过盈
    左侧定心柱面0.100.200.30
    右侧定心柱面0.050.100.15
    下载: 导出CSV

    表  2  螺栓初始预紧力设置

    Table  2.   Bolt initial preload setting N

    计算状态 螺栓初始预紧力
    最小状态 19600
    中间状态 24500
    最大状态 29400
    下载: 导出CSV
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出版历程
  • 收稿日期:  2023-01-12
  • 网络出版日期:  2024-07-25

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