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Enhanced Groove Geometry for Herringbone Grooved Journal Bearings

机译:人字槽轴颈轴承的增强槽几何形状

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摘要

Although gas-lubricated herringbone grooved journal bearings (HGJB) are known for high rotordynamic stability thresholds, small clearance to diameter ratios are required for stable rotor operation. Tight clearances not only increase bearing losses but also yield challenging manufacturing and assembly tolerances, which ultimately translate into cost. Traditionally, the grooves of HGJB are of helical nature with constant cross section and pitch. The current paper aims at increasing the clearance to diameter ratio and the stability threshold of grooved bearings by introducing enhanced groove geometries. The axial evolution of groove width, depth, and local pitch are described by individual third order polynomials with four interpolation points. The expression for the smooth pressure distribution resulting from the narrow groove theory is modified to enable the calculation of bearing properties with modified groove patterns. The reduced order bearing model is coupled to a linear rigid body rotordynamic model for predicting the whirl speed map and the corresponding stability. By introducing a critical mass parameter as a measure for stability, a criterion for the instability onset is proposed. The optimum groove geometry is found by coupling the gas bearing supported rotor model with a multiobjective optimizer. By maximizing both the clearance to diameter ratio and the rotordynamic stability it is shown that with optimal groove geometry, which deviates from helicoids with constant pitch and cross section, the critical mass parameter can be improved by more than one order of magnitude compared to traditional HGJB geometries. The clearance to diameter ratio can be increased by up to 80% while keeping the same stability margin, thus reducing both losses and manufacturing constraints. The optimum groove pattern distributions (width ratio, angle, and depth) are summarized for a variety of L/D ratios and for different compressibility numbers in a first attempt to set up general design guidelines for enhanced gas-lubricated HGJB.
机译:尽管众所周知,气体润滑的人字形沟槽轴颈轴承(HGJB)具有较高的转子动态稳定性阈值,但为了使转子稳定运行,仍需要较小的游隙直径比。紧密的间隙不仅会增加轴承损耗,而且还会带来具有挑战性的制造和装配公差,最终导致成本下降。传统上,HGJB的凹槽为螺旋形,具有恒定的横截面和节距。当前的论文旨在通过引入增强的凹槽几何形状来增加带隙轴承的游隙直径比和稳定性阈值。凹槽宽度,深度和局部螺距的轴向演变是通过具有四个插值点的单个三阶多项式描述的。对由窄槽理论产生的平滑压力分布的表达式进行了修改,以便能够通过修改后的槽型来计算轴承性能。降阶轴承模型与线性刚体转子动力学模型耦合,用于预测涡旋图和相应的稳定性。通过引入临界质量参数作为稳定性的量度,提出了失稳开始的判据。通过将气体轴承支撑的转子模型与多目标优化器耦合,可以找到最佳的凹槽几何形状。通过最大化间隙直径比和转子动力学稳定性,可以看出,与最佳螺距和横截面恒定的螺旋线不同,具有最佳的槽几何形状,与传统的HGJB相比,临界质量参数可以提高一个以上的数量级几何形状。间隙直径比可以增加高达80%,同时保持相同的稳定性裕度,从而减少了损耗和制造限制。总结了各种L / D比率和不同可压缩性数值的最佳凹槽图案分布(宽度比,角度和深度),这是首次尝试为增强型气体润滑HGJB建立通用设计准则。

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  • 来源
    《Journal of Engineering for Gas Turbines and Power》 |2013年第10期|102501.1-102501.8|共8页
  • 作者

    J. Schiffmann;

  • 作者单位

    Laboratory for Applied Mechanical Design, Ecole Polytechnique Federale de Lausanne, EPFL IMT LAMD, Jaquet Droz 1, Neuchatel CH-2002, Switzerland;

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