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首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Gas-Expanded Lubricant Performance and Effects on Rotor Stability in Turbomachinery
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Gas-Expanded Lubricant Performance and Effects on Rotor Stability in Turbomachinery

机译:透平机气体膨胀润滑剂性能及其对转子稳定性的影响

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摘要

Gas-expanded lubricants (GELs) are tunable mixtures of synthetic oil and carbon dioxide that enable dynamic control of lubricant viscosity during bearing operation. This control can help reduce bearing power loss and operating temperatures while also providing direct control over bearing stiffness and damping, which can enhance rotordynamic performance. In this work, the bearing and rotordynamic performance of two representative high-speed machines was evaluated when different lubricants, including GELs, were supplied to the machine bearings. The machines chosen for this analysis, an eight-stage centrifugal compressor and a steam turbine-generator system, represent a wide range of speed and loading conditions encountered in modern turbomachinery. The fluids compared for machine performance were standard petroleum-based lubricants, polyol ester (POE) synthetic oils, and POE-based GELs. The performance simulations were carried out using a thermoelastohydrodynamic bearing model, which provided bearing stiffness and damping coefficients as inputs to finite element rotordynamic models. Several bearing performance metrics were evaluated including power loss, operating temperature, film thickness, eccentricity, and stiffness and damping coefficients. The rotordynamic analysis included an evaluation of rotor critical speeds, unbalance response, and stability. Bearing performance results for the compressor showed a 40% reduction in power loss at operating speed when comparing the GEL to the petroleum-based lubricant. The GEL-lubricated compressor also exhibited lower operating temperatures with minimal effects on film thickness. GELs were also predicted to produce lower bearing stiffness when compared to standard fluids in the compressor. Rotordynamic results for the compressor showed that the fluid properties had only minor effects on the unbalance response, while GELs were found to increase the stability margin by 43% when compared with standard fluids. The results from the turbine-generator system also demonstrated increases in low-speed bearing efficiency with the use of GELs, though at higher speeds the onset of turbulent flow in the GEL case offset these efficiency gains. Rotordynamic results for this system showed a contrast with the compressor results, with the GELs producing lower stability margins for a majority of the modes predicted due to increased bearing stiffness in the high-speed turbine bearings and negative stiffness in the lightly loaded, low-speed pinion bearings. These results suggest that GELs could be beneficial in providing control over a wide range of machine designs and operating conditions and that some machines are especially well suited for the tunability that these fluids impart.
机译:气体膨胀润滑剂(GEL)是合成油和二氧化碳的可调混合物,可在轴承运行过程中动态控制润滑剂的粘度。这种控制可以帮助减少轴承的功率损耗和工作温度,同时还可以直接控制轴承的刚度和阻尼,从而提高转子的动力性能。在这项工作中,当向机器轴承供应不同的润滑剂(包括GEL)时,评估了两个代表性的高速机器的轴承和转子动力学性能。分析所选择的机器,八级离心压缩机和蒸汽涡轮发电机系统代表了现代涡轮机械所遇到的各种速度和负载条件。比较机器性能的流体是标准石油基润滑剂,多元醇酯(POE)合成油和POE基GEL。使用热弹流体动力轴承模型进行性能模拟,该模型提供轴承刚度和阻尼系数作为有限元转子动力学模型的输入。评估了几种轴承性能指标,包括功率损耗,工作温度,薄膜厚度,偏心率以及刚度和阻尼系数。转子动力学分析包括对转子临界速度,不平衡响应和稳定性的评估。与GEL和石油基润滑剂相比,压缩机的轴承性能结果显示在运行速度下,功率损耗降低了40%。 GEL润滑的压缩机还具有较低的工作温度,并且对薄膜厚度的影响最小。与压缩机中的标准流体相比,GEL还预计会产生较低的轴承刚度。压缩机的转子动力学结果表明,流体特性对不平衡响应的影响很小,而与标准流体相比,发现GEL使稳定性裕度提高了43%。涡轮发电机系统的结果还表明,使用GEL可以降低低速轴承的效率,尽管在更高的速度下,GEL情况下湍流的产生抵消了这些效率的提高。该系统的转子动力学结果与压缩机结果形成对比,由于高速涡轮轴承的轴承刚度增加和轻载,低速轴承的负刚度增加,GEL在大多数模式下产生的稳定裕度较低小齿轮轴承。这些结果表明,GEL可能有利于在广泛的机器设计和操作条件下提供控制,并且某些机器特别适合这些流体带来的可调性。

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  • 来源
    《Journal of Engineering for Gas Turbines and Power 》 |2015年第7期| 072601.1-072601.11| 共11页
  • 作者单位

    Department of Civil and Environmental Engineering, University of Virginia, 351 McCormick Road, Charlottesville, VA 22904;

    Rotor Bearing Solutions International, LLC, 3277 Arbor Terrace, Charlottesville, VA 22911;

    Department of Mechanical and Aerospace Engineering, University of Virginia, 122 Engineer's Way, Charlottesville, VA 22904;

    Department of Mechanical and Aerospace Engineering, University of Virginia, 122 Engineer's Way, Charlottesville, VA 22904;

    Department of Civil and Environmental Engineering, University of Virginia, 351 McCormick Road, Charlottesville, VA 22904;

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