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带有ERSFD的航空弧齿锥齿轮动态特性

任鸿飞 王三民 邹浩然 陈鹏 张旭阳

任鸿飞, 王三民, 邹浩然, 等. 带有ERSFD的航空弧齿锥齿轮动态特性[J]. 航空动力学报, 2024, 39(2):20220240 doi: 10.13224/j.cnki.jasp.20220240
引用本文: 任鸿飞, 王三民, 邹浩然, 等. 带有ERSFD的航空弧齿锥齿轮动态特性[J]. 航空动力学报, 2024, 39(2):20220240 doi: 10.13224/j.cnki.jasp.20220240
REN Hongfei, WANG Sanmin, ZOU Haoran, et al. Dynamic characteristic of aviation spiral bevel gear with ERSFD[J]. Journal of Aerospace Power, 2024, 39(2):20220240 doi: 10.13224/j.cnki.jasp.20220240
Citation: REN Hongfei, WANG Sanmin, ZOU Haoran, et al. Dynamic characteristic of aviation spiral bevel gear with ERSFD[J]. Journal of Aerospace Power, 2024, 39(2):20220240 doi: 10.13224/j.cnki.jasp.20220240

带有ERSFD的航空弧齿锥齿轮动态特性

doi: 10.13224/j.cnki.jasp.20220240
详细信息
    作者简介:

    任鸿飞(1998-),男,博士生,主要从事齿轮系统动力学、发动机故障诊断和健康监控等方面的研究

  • 中图分类号: V232.8

Dynamic characteristic of aviation spiral bevel gear with ERSFD

  • 摘要:

    将弹性环式挤压油膜阻尼器(ERSFD)引入弧齿锥齿轮传动(SBGD)系统中以改善其动态特性。基于广义雷诺方程建立内外油膜控制方程,并通过半解析方法得到弹性环的变形,获得ERSFD油膜力后基于径向基(RBF)神经网络建立其近似模型,建立带有ERSFD支撑的8自由度SBGD系统双向流固耦合动力学模型,借助分时迭代方法获得系统稳态响应。结果表明:内油膜压力沿圆周分段式分布,且沿偏移线为非对称分布;ERSFD的存在有效削弱了油膜力与偏心率之间的非线性关系;弹性环凸台厚度的增加,使系统振动响应的幅值整体下降,并抑制了5200~8200 r/min转速范围内系统的混沌行为,有效改善了SBGD系统动态特性。

     

  • 图 1  流体动力润滑示意图

    Figure 1.  Schematic diagram of hydrodynamic lubrication

    图 2  ERSFD模型示意图

    Figure 2.  Schematic diagram of ERSFD model

    图 3  内油膜上下表面速度示意图

    Figure 3.  Schematic diagram of the velocity of the upper and lower surfaces of the inner oil film

    图 4  弹性环受力示意图

    Figure 4.  Schematic diagram of the force of the elastic ring

    图 5  流体计算域示意图

    Figure 5.  Schematic diagram of the fluid computational domain

    图 6  RBF神经网络拟合效果图

    Figure 6.  RBF neural network fitting effect diagram

    图 7  SBGD系统动力学模型

    Figure 7.  Dynamic model of SBGD system

    图 8  计算流程图

    Figure 8.  Calculation flow chart

    图 9  内油膜压力分布示意图

    Figure 9.  Schematic diagram of inner oil film pressure distribution

    图 10  β = π/4时油膜分力及油膜压力随偏心率的变化曲线

    Figure 10.  Variation curves of oil film component force and oil film pressure with eccentricity for β = π/4

    图 11  不同凸台厚度下,主动轮横向振动位移响应随转速变化分岔图

    Figure 11.  Bifurcation diagram of the lateral vibration displacement response of the pinion with the change of rotational speed under different boss thicknesses

    图 12  主动轮转速为2200 r/min下,不同凸台厚度对应的系统振动响应

    Figure 12.  Vibration response of the system corresponding to different boss thicknesses when the pinion speed is 2200 r/min

    图 13  主动轮转速5800 r/min下,不同凸台厚度对应的系统振动响应

    Figure 13.  Vibration response of the system corresponding to different boss thicknesses when the pinion speed is 5800 r/min

    图 14  主动轮转速7600 r/min下,不同凸台厚度对应的系统振动响应

    Figure 14.  Vibration response of the system corresponding to different boss thicknesses when the pinion speed is 7600 r/min

    表  1  计算时间成本

    Table  1.   Calculate time cost

    方法耗时/s
    数值求解2.280
    RBF网络回归0.00764
    下载: 导出CSV

    表  2  ERSFD相关参数

    Table  2.   ERSFD related parameters

    参数数值
    凸台数8
    凸台对应角度/(°)π/4
    弹性环长度/mm20
    渗油孔数8
    流体黏度/(Pa·s)0.01844
    内油膜初始间隙/mm0.2
    外油膜初始间隙/mm0.2
    下载: 导出CSV

    表  3  SBGD相关参数

    Table  3.   SBGD related parameters

    参数数值及说明
    主动轮从动轮
    齿数4753
    质量/kg0.81.5
    转动惯量/(kg·mm210403120
    旋向左旋右旋
    偏心距/μm0.5
    压力角/(°)20
    中点螺旋角/(°)20
    轴交角/(°)108
    齿宽/mm30
    平均传动误差/mm0.02
    平均啮合刚度/108 (N/m)3
    啮合阻尼/(N·s/m)1000
    径向支承刚度/108 (N/m)3
    径向支撑阻尼/(N·s/m)500
    轴向支承刚度/108 (N/m)5
    轴向支撑阻尼/(N·s/m)500
    下载: 导出CSV
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  • 收稿日期:  2022-04-23
  • 网络出版日期:  2023-08-09

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