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Measurements Versus Predictions for the Static and Dynamic Characteristics of a Four-pad Rocker-pivot, Tilting-pad Journal Bearing

机译:测量与四垫板摇臂枢轴,可倾垫轴颈轴承静态和动态特性的预测

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摘要

Measured and predicted static and dynamic characteristics are provided for a four-pad, rocker-pivot, tilting-pad journal bearing in the load-on-pad and load-between-pad orientations. The bearing has the following characteristics: 4 pads, .57 pad pivot offset, 0.6 L/D ratio, 60.33 mm (2.375in) pad axial length, 0.08255 mm (0.00325 in) radial clearance in the load-on-pad orientation, and 0.1189 mm (0.00468 in) radial clearance in the load-between-pad orientation. Tests were conducted on a floating test bearing design with unit loads ranging from 0 to 2903 kPa (421.1 psi) and speeds from 6.8 to 13.2 krpm.For all rotor speeds, hot-clearance measurements were taken to show the reduction in bearing clearance due to thermal expansion of the shaft and pads during testing. As the testing conditions get hotter, the rotor, pads, and bearing expand, decreasing radial bearing clearance. Hot-clearance measurements showed a 16-25% decrease in clearance compared to a clearance measurement at room temperature.For all test conditions, dynamic tests were performed over a range of excitation frequencies to obtain complex dynamic stiffness coefficients as a function of frequency. The direct real dynamic stiffness coefficients were then fitted with a quadratic function with respect to frequency. From the curve fit, the frequency dependence was captured by including a virtual-mass matrix [M] to produce a frequency independent [K][C][M] model.The direct dynamic stiffness coefficients for the load-on-pad orientation showed significant orthotropy, while the load-between-pad did not. The load-between-pad showed slight orthotropy as load increased. Experimental cross-coupled stiffness coefficients were measured in both load orientations, but were of the same sign and significantly less than direct stiffness coefficients.In both orientations the imaginary part of the measured dynamic stiffness increased linearly with increasing frequency, allowing for frequency independent direct damping coefficients.Rotordynamic coefficients presented were compared to predictions from two different Reynolds-based models. Both models showed the importance of taking into account pivot flexibility and different pad geometries (due to the reduction in bearing clearance during testing) in predicting rotordynamic coefficients. If either of these two inputs were incorrect, then predictions for the bearings impedance coefficients were very inaccurate. The main difference between prediction codes is that one of the codes incorporates pad flexibility in predicting the impedance coefficients for a tilting-pad journal bearing.To look at the effects that pad flexibility has on predicting the impedance coefficients, a series of predictions were created by changing the magnitude of the pad's bending stiffness. Increasing the bending stiffness used in predictions by a factor of 10 typically caused a 3-11% increase in predicted Kxx and Kyy, and a 10-24% increase in predicted Cxx and Cyy. In all cases, increasing the calculated bending stiffness from ten to a hundred times the calculated value caused slight if any change in Kxx, Kyy, Cxx, and Cyy. For a flexible pad an increase in bending stiffness can have a large effect on predictions; however, for a more rigid pad an increase in pad bending stiffness will have a much lesser effect. Results showed that the pad's structural bending stiffness can be an important factor in predicting impedance coefficients. Even though the pads tested in this thesis are extremely stiff, changes are still seen in predictions when the magnitude of the pad?s bending stiffness is increased, especially in Cxx, and Cyy. The code without pad flexibility predicted Kxx and Kyy much more accurately than the code with pad flexibility. The code with pad flexibility predicts Cxx more accurately, while the code without pad flexibility predicted Cyy more accurately. Regardless of prediction Code used, the Kxx and Kyy were over-predicted at low loads, but predicted more accurately as load increased. Cxx, and Cyy were modeled very well in the load-on-pad orientation, while slightly overpredicted in the load-between-pad orientation. For solid pads, like the ones tested here, both codes do a decent job at predicting impedance coefficients
机译:为四块垫板,摇杆枢轴,可倾瓦块的轴颈轴承提供了测得的和预测的静态和动态特性,这些轴承在垫上载荷和垫间载荷方向上提供了支撑。轴承具有以下特征:4个垫块,0.57个垫块枢轴偏移,0.6 L / D比率,60.33毫米(2.375英寸)的垫块轴向长度,0.08255毫米(0.00325英寸)的径向载荷,以及垫片之间的负载方向的径向间隙为0.1189毫米(0.00468英寸)。测试是在浮动测试轴承设​​计上进行的,单位载荷范围为0至2903 kPa(421.1 psi),速度为6.8至13.2 krpm。对于所有转子速度,均进行了热间隙测量,以显示由于测试期间轴和轴瓦的热膨胀。随着测试条件变热,转子,轴瓦和轴承会膨胀,从而减小径向轴承游隙。热间隙测量表明,与室温下的间隙测量相比,间隙减小了16-25%。在所有测试条件下,都在一系列激励频率上进行了动态测试,以获得作为频率函数的复杂动态刚度系数。然后将直接的实际动态刚度系数与关于频率的二次函数拟合。从曲线拟合中,通过包含虚拟质量矩阵[M]来捕获频率相关性,以生成独立于频率的[K] [C] [M]模型。垫载荷方向的直接动态刚度系数显示正交各向异性显着,而垫间载荷则没有。垫间的载荷随载荷的增加而显示出轻微的正交性。在两个载荷方向上都测量了实验交叉耦合的刚度系数,但是它们的符号相同并且显着小于直接刚度系数。在两个方向上,所测得的动态刚度的虚部都随着频率的增加而线性增加,从而允许频率独立的直接阻尼将给出的转子动力系数与基于两个不同的基于雷诺兹模型的预测值进行比较。两种模型都表明在预测转子动力系数时必须考虑枢轴的柔韧性和不同的轴瓦几何形状(由于测试过程中轴承游隙的减小)的重要性。如果这两个输入中的任何一个都不正确,则轴承阻抗系数的预测将非常不准确。预测代码之间的主要区别在于,其中一个代码在预测可倾瓦块轴颈轴承的阻抗系数时结合了瓦块挠性。为了查看瓦块挠性对预测阻抗系数的影响,通过以下方法创建了一系列预测:更改垫的弯曲刚度的大小。将预测中使用的弯曲刚度提高10倍通常会导致预测的Kxx和Kyy增加3-11%,并使预测的Cxx和Cyy增加10-24%。在所有情况下,将计算的弯曲刚度从计算值的十倍增加到一百倍会导致Kxx,Kyy,Cxx和Cyy发生轻微的变化。对于柔性垫,弯曲刚度的增加可能会对预测产生很大的影响。然而,对于更刚性的垫,垫抗弯刚度的增加将具有较小的影响。结果表明,垫的结构弯曲刚度可能是预测阻抗系数的重要因素。即使本文中测试的垫极硬,但当垫的弯曲刚度增加时,在预测中仍会看到变化,特别是在Cxx和Cyy中。没有衬垫灵活性的代码比具有衬垫灵活性的代码更准确地预测Kxx和Kyy。具有填充灵活性的代码可以更准确地预测Cxx,而没有填充灵活性的代码可以更准确地预测Cyy。无论使用哪种预测代码,在低负载下Kxx和Kyy都被过度预测,但是随着负载的增加,预测会更加准确。 Cxx和Cyy在“垫上加载”方向上的建模非常好,而在“垫间加载”方向上的预测有些过高。对于实心焊盘(如此处测试的焊盘),两个代码在预测阻抗系数方面都做得不错

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    Tschoepe David 1987-;

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  • 年度 2013
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