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转子叶片-机匣系统中微观摩擦表面粗糙度的影响分析

张莹 倪欢

张莹, 倪欢. 转子叶片-机匣系统中微观摩擦表面粗糙度的影响分析[J]. 航空动力学报, 2025, 40(X):20250216 doi: 10.13224/j.cnki.jasp.20250216
引用本文: 张莹, 倪欢. 转子叶片-机匣系统中微观摩擦表面粗糙度的影响分析[J]. 航空动力学报, 2025, 40(X):20250216 doi: 10.13224/j.cnki.jasp.20250216
ZHANG Ying, NI Huan. Analysis on influence of microscopic friction roughness in rotor blade-casing system[J]. Journal of Aerospace Power, 2025, 40(X):20250216 doi: 10.13224/j.cnki.jasp.20250216
Citation: ZHANG Ying, NI Huan. Analysis on influence of microscopic friction roughness in rotor blade-casing system[J]. Journal of Aerospace Power, 2025, 40(X):20250216 doi: 10.13224/j.cnki.jasp.20250216

转子叶片-机匣系统中微观摩擦表面粗糙度的影响分析

doi: 10.13224/j.cnki.jasp.20250216
基金项目: 国家自然科学基金民航联合基金重点项目(U2233201),国家自然科学基金(52172360)
详细信息
    作者简介:

    张莹(1983-),女,副教授,博士,主要研究方向为航空发动机故障诊断、飞机发动机健康管理、双稳随机共振。E-mail:caucezy@163.com

    通讯作者:

    倪欢(2002-),男,硕士生,主要研究方向为航空发动机碰摩。E-mail:3428289418@qq.com

  • 中图分类号: V233.1

Analysis on influence of microscopic friction roughness in rotor blade-casing system

  • 摘要:

    聚焦于叶片-机匣系统的微观摩擦表面粗糙度,通过理论分析、数值模拟,深入探讨了从摩擦的瞬态到碰摩周期性演化的规律及其机制。研究发现,表面粗糙度显著影响初始接触应力和温度,且随表面粗糙度增加,初始应力峰值和温度上升幅度增大,表明表面粗糙度对瞬态摩擦热效应有显著影响。在周期性碰摩阶段,应力和温度趋于稳定,但表面粗糙度仍影响其分布均匀性。通过优化表面粗糙度,可有效调控摩擦行为,减少能量损耗与磨损,提升发动机效率和可靠性。本文创新性地提出了基于分形接触理论和弹塑性变形阶段的耦合模型,与传统模型相比,该模型能够更准确地描述复杂表面形态下的接触情况,全面考虑微凸体在弹塑性变形阶段的复杂行为,完整呈现摩擦过程中的力学响应全貌。这一改进显著提升模拟精度,为跨尺度力学行为研究提供了一种思路和方法。

     

  • 图 1  单个微凸体接触变形简图

    Figure 1.  Schematic diagram of contact deformation of a single microconvex body

    图 2  实际粗糙表面

    Figure 2.  Actual rough surface

    图 3  微观摩擦模型示意图

    Figure 3.  Schematic representation of the microscopic friction model

    图 4  不同表面粗糙度下叶片应力的时域曲线

    Figure 4.  Time domain curve of blade stress under different surface roughness

    图 5  不同表面粗糙度下叶片应力分布云图

    Figure 5.  Cloud map of blade stress distribution under different surface roughness

    图 6  不同表面粗糙度下叶片温度的时域曲线

    Figure 6.  Time-domain curve of leaf temperature at different surface roughness

    图 7  不同表面粗糙度下叶片温度分布云图

    Figure 7.  Cloud map of leaf temperature distribution under different surface roughness

    图 8  不同机匣表面粗糙度下叶片应力的时域曲线

    Figure 8.  Time domain curve of blade stress under different casing surface roughness

    图 9  不同机匣表面粗糙度下叶片应力分布云图

    Figure 9.  Cloud diagram of blade stress distribution under different casing surface roughness

    图 10  不同机匣表面粗糙度下叶片温度时域曲线

    Figure 10.  Time domain curve of blade temperature under different casing roughness

    图 11  不同机匣表面粗糙度下叶片温度分布云图

    Figure 11.  Cloud diagram of blade temperature distribution under different casing roughness

    图 12  宏观转子叶片-机匣系统有限元模型

    Figure 12.  Finite element model of a macroscopic rotor blade-casing system

    图 13  碰摩点温度和应力时域曲线

    Figure 13.  Time-domain curves of friction point temperature and stress

    图 14  叶片等效应力云图

    Figure 14.  Equivalent stress contour of the blade

    表  1  TC4 合金和结构钢材料参数

    Table  1.   Material parameters of TC4 alloy and structural steel

    材料 弹性模量/
    GPa
    泊松比 密度/
    (kg/m3
    表面粗糙度/
    μm
    TC4合金 110 0.34 4430 0.1~0.4
    结构钢 210 0.29 7850 0.4~1.6
    下载: 导出CSV

    表  2  TC4 合金和结构钢表面粗糙度划分标准

    Table  2.   TC4 Alloy and structural steel surface roughness classification standards

    材料 表面粗糙度/μm 对应加工条件
    TC4合金 0.1 精密加工条件(符合航空发动机
    叶片的高标准表面处理要求)
    0.2 高精度的工业加工水平
    (精密车削或铣削)
    0.3 一般的机械加工精度
    0.4 相对粗糙的表面状态
    结构钢 0.4 较高精度标准
    (精细车削或铣削加工)
    0.8 常见的机械加工精度
    1.2 一般的加工精度
    1.6 低精度的加工
    下载: 导出CSV
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  • 收稿日期:  2025-05-06
  • 网络出版日期:  2025-10-16

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