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Vibration of planetary gears having an elastic continuum ring gear.

机译:具有弹性连续齿圈的行星齿轮的振动。

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摘要

The primary goal of this work is to develop mathematical models for planetary gears having an elastic ring gear to conduct numerical and analytical studies to understand the modal properties, parametric instability, and nonlinear gear dynamic behaviors.;First, natural frequencies and vibration modes are determined as closed-form expressions for a ring having a circumferentially varying foundation of very general description through perturbation and Galerkin analyses. The simple eigensolution expressions explicitly show the parameter dependencies, lead to natural frequency splitting rules for degenerate unperturbed eigenvalues at both first and second orders of perturbation, and identify which nodal diameter Fourier components contaminate a given n nodal diameter base mode of the free ring. As an application and as the motivating problem for the study, the natural frequencies and vibration modes of a ring gear used in helicopter planetary gears with unequally spaced planets are investigated.;Second, the distinctive modal properties of equally spaced planetary gears with elastic ring gears are analytically studied through perturbation and a candidate mode method based on an elastic-discrete model. Two perturbations are used to obtain closed-form expressions of all the eigenfunctions. In the Discrete Planetary Perturbation (DPP), the unperturbed system is a discrete planetary gear with a rigid ring. In the Elastic Ring Perturbation (ERP), the unperturbed system is an elastic ring supported by the ring-planet mesh springs; the sun, planet and carrier motions are treated as small perturbations. All vibration modes are classified into rotational, translational, planet and purely ring modes. The well defined properties of each type of mode are analytically determined. All modal properties are verified numerically. Also the modal properties of planetary gears having diametrically opposed planets and an elastic ring gear are studied through the candidate mode method. Two types of modes are found: rotational and translational modes.;Fourth, the parametric instability of planetary gears having elastic continuum ring gears is analytically investigated based on the elastic-discrete model. By using the structured modal properties of planetary gears and the method of multiple scales, the instability boundaries are obtained as simple expressions in terms of mesh parameters. Instability existence rules for in-phase and sequentially phased planet meshes are also discovered. For in-phase planet meshes, instability existence depends only on the type of gear mesh deformation. For sequentially phased planet meshes, the number of teeth on the sun (or the ring) and the type of gear mesh deformation govern the instability existence. The instability boundaries are validated numerically.;Finally, the nonlinear dynamics of planetary gears having an elastic ring gear is studied. The frequency-response functions are presented for primary, subharmonic, and superharmonic resonances. The tooth separation phase between meshes depends on the mode type excited and the position of the planets. The resonances associated with a translational or planet mode are investigated. Parametric instability rule and mesh deflection phase expression are confirmed in the numerical simulation for both in-phase and sequentially phased planets. Response of planetary gears having commensurate natural frequencies is also studied.
机译:这项工作的主要目的是开发具有弹性齿圈的行星齿轮的数学模型,以进行数值和分析研究,以了解模态特性,参数不稳定性和非线性齿轮动力学行为。首先,确定固有频率和振动模式通过微扰和Galerkin分析,对具有周向变化基础的环的封闭形式进行了概括性描述。简单的本征解表达式明确显示了参数的依存关系,从而导致了自然的频率分裂规则,使得在第一阶和第二阶扰动下退化的非扰动本征值,并确定哪个节点直径傅立叶分量会污染给定的自由环的n节点直径基础模式。作为研究的一个应用和动机问题,研究了等距行星齿轮直升飞机行星齿轮中使用的齿圈的固有频率和振动模式。第二,等距弹性齿圈行星齿轮的独特模态特性通过摄动和基于弹性离散模型的候选模式方法进行分析研究。使用两个扰动来获得所有本征函数的闭式表达式。在离散行星扰动(DPP)中,无扰动系统是具有刚性环的离散行星齿轮。在弹性环扰动(ERP)中,无扰动系统是由环形行星网状弹簧支撑的弹性环。太阳,行星和行星架的运动被视为小扰动。所有振动模式都分为旋转,平移,行星和纯环形模式。通过分析确定每种模式的定义明确的属性。所有模态特性均通过数字验证。还通过候选模式方法研究了具有直径相对的行星齿轮和弹性齿圈的行星齿轮的模态特性。发现了两种模式:旋转模式和平移模式。第四,基于弹性离散模型,对具有弹性连续齿圈的行星齿轮的参数不稳定性进行了分析研究。通过使用行星齿轮的结构化模态特性和多尺度方法,可以根据网格参数将不稳定性边界作为简单表达式获得。还发现了同相和相序行星网的不稳定性存在规则。对于同相行星网,不稳定性的存在仅取决于齿轮网变形的类型。对于相继定序的行星网格,太阳(或环)上的齿数和齿轮啮合变形的类型决定了不稳定性的存在。最后,对具有弹性齿圈的行星齿轮的非线性动力学进行了研究。给出了用于主,次谐波和超谐波谐振的频率响应函数。网格之间的齿分离阶段取决于激发的模式类型和行星的位置。研究了与平移或行星模式相关的共振。在同相行星和相继行星的数值模拟中,确定了参数不稳定性规则和网格变形相位表达式。还研究了具有适当固有频率的行星齿轮的响应。

著录项

  • 作者

    Wu, Xionghua.;

  • 作者单位

    The Ohio State University.;

  • 授予单位 The Ohio State University.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2010
  • 页码 239 p.
  • 总页数 239
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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