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Modelling and Dynamic Analysis of the Spiral Bevel Gear-Shaft-Bearing-Gearbox Coupling System

机译:螺旋锥齿轮轴轴承齿轮耦合系统的建模与动态分析

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To accurately study the dynamic characteristics of the spiral bevel gear transmission system in a helicopter tail transmission system, the finite element model of the gear shaft was established by a Timoshenko beam element, and the mechanical model of the spiral bevel gear was created by the lumped mass method. The substructure method is employed to extract the dynamic parameters from the gearbox's finite element model, and the dynamic model of the spiral bevel gear-shaft-bearing-gearbox coupling system was built according to the interface coordination conditions. In the model, the influences of time-varying stiffness, a time-varying transmission error, gearbox flexibility, unbalance excitation, and a flexible shaft and bearing support on the system vibration were taken into account simultaneously. On this basis, the dynamic differential equations of the full coupling system of the spiral bevel gear were derived, and the effects of the gearbox flexibility, the shaft angle, and the unbalance on the dynamic properties of the system were analysed. The results show that the gearbox flexibility can reduce the gear meshing force and bearing force, in which there is a more significant impact on the bearing force. The shaft angle affects the position, size, and direction of the system's axis trajectory. Meanwhile, the meshing force and the bearing force of the system are also varied because of the various pitch angles of the driving and driven gears under different shaft angles. The unbalance of the gear shaft has an effect on the vibration of the spiral bevel gear transmission system in all directions, wherein the influence on the torsional vibration is the most significant, and the influence increases as the unbalance rises. The unbalance of the gear shaft also affects the meshing force and bearing force, which increases as the rotational speed rises. This research provides a theoretical basis to optimize dynamic performance and reduce the vibration and noise of a spiral bevel gear full coupling system.
机译:为了准确研究直升机尾传动系统中螺旋锥齿轮传动系统的动态特性,齿轮轴的有限元模型由TIMOSHENKO梁元件建立,螺旋锥齿轮的机械模型由集成产生质量方法。采用子结构方法从变速箱的有限元模型中提取动态参数,并且根据界面配位条件建立螺旋锥齿轮轴轴承齿轮箱联轴器耦合系统的动态模型。在该模型中,同时考虑时变刚度,时变误差,齿轮箱柔性,不平衡激励和柔性轴和轴承支撑的影响。在此基础上,得出了螺旋锥齿轮的全耦合系统的动态微分方程,并分析了齿轮箱柔性,轴角和不平衡对系统动态性质的影响。结果表明,齿轮箱灵活性可以减少齿轮啮合力和轴承力,在此内部对轴承力产生更大的影响。轴角影响系统轴轨迹的位置,尺寸和方向。同时,由于驱动和从动齿轮在不同的轴角下的各种俯仰角,也改变了系统的啮合力和轴承力。齿轮轴的不平衡对所有方向的螺旋锥齿轮传动系统的振动有影响,其中对扭转振动的影响是最显着的,并且随着不平衡升高的影响,影响增加。齿轮轴的不平衡也影响啮合力和承载力,随着旋转速度升高而增加。本研究提供了理论依据,可优化动态性能,降低螺旋锥齿轮全耦合系统的振动和噪音。

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  • 来源
    《Mathematical Problems in Engineering》 |2019年第19期|9065215.1-9065215.16|共16页
  • 作者单位

    Nanjing Univ Aeronaut & Astronaut Natl Key Lab Sci & Technol Helicopter Transmiss Nanjing 210016 Jiangsu Peoples R China;

    Nanjing Univ Aeronaut & Astronaut Natl Key Lab Sci & Technol Helicopter Transmiss Nanjing 210016 Jiangsu Peoples R China;

    Nanjing Univ Aeronaut & Astronaut Natl Key Lab Sci & Technol Helicopter Transmiss Nanjing 210016 Jiangsu Peoples R China;

    AECC Hunan Aviat Powerplant Res Inst Zhuzhou 412000 Peoples R China;

    AECC Hunan Aviat Powerplant Res Inst Zhuzhou 412000 Peoples R China;

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