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EVALUATION OF FRICTION DAMPING IN DOVETAIL ROOT JOINTS BASED ON DISSIPATION ENERGY ON CONTACT SURFACES

机译:基于接触表面耗散能的燕尾根节点摩擦阻尼评估

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It is necessary to increase and estimate friction damping at contact interfaces to reduce vibratory stresses in turbines. The hysteresis behavior between tangential contact force and relative displacement should be precisely estimated to improve the accuracy of fiction-damping estimates. There is a difficulty in establishing a general model of hysteresis because tangential contact stiffness depends on many parameters, such as normal contact force, contact geometry, surface roughness, and wear status.We discuss a procedure to empirically calculate friction damping in dovetail root joints using the tangential contact stiffness estimated from measured natural frequencies and the micro-slip model whose coefficients were experimentally obtained from special fretting tests. Instead of the multi-harmonic balance methods, we calculated the friction damping on the basis of the energy dissipation at contact surfaces to discuss the effects of the tangential contact stiffness on several physical values, i.e., tangential and normal contact forces, natural frequency, and micro-slip. In our model, the linear forced response analysis was conducted by taking into consideration the non-linearity between the tangential contact force and the relative displacement by defining the actual and imaginary tangential contact stiffness.We confirmed that the numerically calculated damping ratios are quantitatively in very good agreement with the measured ones under different contact angles, input gravity levels, and contact forces. This indicates that if the tangential contact stiffness is accurately estimated, friction damping with our method can be precisely estimated under different testconditions. We also showed that the estimated tangential contact stiffness for dovetail root joints are smaller than those obtained by the fretting tests at high input gravity. This is probably because the contact interface partially separates during a cyclic loading in the former case; this results in the decrease of the contact area and contact stiffness.
机译:必须增加和估算接触界面处的摩擦阻尼,以减少涡轮机中的振动应力。应精确估计切向接触力和相对位移之间的磁滞行为,以提高虚构阻尼估计的准确性。由于切向接触刚度取决于许多参数,例如法向接触力,接触几何形状,表面粗糙度和磨损状态,因此很难建立一般的磁滞模型。 我们讨论了一种程序,该程序使用根据测量的固有频率估算的切向接触刚度和微滑移模型,根据经验计算燕尾根节的摩擦阻尼,该滑移系数是通过特殊的微动试验从实验中获得的。代替多重谐波平衡方法,我们根据接触表面的能量消散来计算摩擦阻尼,以讨论切向接触刚度对几个物理值(切向和法向接触力,固有频率和振动)的影响。微滑。在我们的模型中,通过定义切线接触力的实际和假想,并考虑到切线接触力和相对位移之间的非线性,进行了线性力响应分析。 我们确认,在不同的接触角,输入重力水平和接触力下,数值计算的阻尼比与被测阻尼比在数量上非常吻合。这表明,如果精确估计切向接触刚度,则在不同的测试条件下可以精确估计本方法的摩擦阻尼 情况。我们还表明,燕尾根关节的估计切向接触刚度小于在高输入重力下通过微动试验获得的切向接触刚度。这可能是因为在前一种情况下,接触界面在循环加载过程中会部分分离;这导致接触面积和接触刚度的减小。

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