首页> 外文会议>ASME turbo expo: turbomachinery technical conference and exposition >A CFD BASED APPROACH FOR ESTIMATION OF ROTOR DYNAMIC COEFFICIENTS FOR LIQUID ANNULAR SEALS IN TURBOMACHINERY
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A CFD BASED APPROACH FOR ESTIMATION OF ROTOR DYNAMIC COEFFICIENTS FOR LIQUID ANNULAR SEALS IN TURBOMACHINERY

机译:基于CFD的涡轮机环形密封圈转子动力系数估计方法。

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Seals are used to control leakage across stages in pumps and other rotating machinery such as turbomachines. However, while acting to control leakage, the seals generate a reaction force on the rotating members. The rotordynamic forces produced by fluid impact the stability behaviour of the highspeed turbomachinery, therefore precise estimation of rotordynamic parameters is important to ensure vibrational stability and desired dynamic performance of rotors having annular seals. Studies on seals have so far mainly focused on bulk flow model based on Hirs turbulent lubrication theory for calculating leakage flow rate and rotordynamic coefficients. However, it is incapable to deal complex geometries and is less efficient in predicting precise rotor dynamic parameters for high speed rotating systems due to its basic assumptions. The experiments performed for calculating rotordynamic coefficients show their dependence on many physical and mechanical properties such as working fluid properties, pressure drop, seal clearance, rotor speed, eccentricity and misalignments. With the latest high performance computing facilities it is now relatively easy to simulate the flow in seal and evaluate the dynamic coefficients at high rotational speeds and with complex geometries. This paper proposes a 3-D CFD based transient stimulation method to capture the experimental conditions in virtual environment. The fluid force is calculated by integrating pressure to the rotor surface and the stiffness and damping coefficients are evaluated by appropriate curve fitting of fluid forces for various eccentricity values. The coefficients obtained from the present method show better correlation with experimental data compared to the existing steady state CFD and theoretical models. Variation of these rotordynamic coefficients with eccentricity helps in assessing the safe design of turbomachinery.
机译:密封件用于控制泵和其他旋转机械(例如涡轮机)中各级的泄漏。然而,在用于控制泄漏的同时,密封件在旋转构件上产生反作用力。由流体产生的转子动力会影响高速涡轮机械的稳定性,因此精确估计转子动力学参数对于确保具有环形密封件的转子的振动稳定性和所需的动态性能很重要。迄今为止,对密封件的研究主要集中在基于Hirs湍流润滑理论的大流量模型上,用于计算泄漏流量和转子动力学系数。但是,由于其基本假设,它无法处理复杂的几何形状,并且在预测高速旋转系统的精确转子动态参数方面效率较低。用于计算转子动力系数的实验表明,它们取决于许多物理和机械特性,例如工作流体特性,压降,密封间隙,转子速度,偏心率和偏心。使用最新的高性能计算设备,现在相对容易地模拟密封中的流动并评估高转速和复杂几何形状下的动态系数。本文提出了一种基于3-D CFD的瞬态刺激方法,以捕获虚拟环境中的实验条件。通过将压力积分到转子表面来计算流体力,并通过针对各种偏心率值对流体力进行适当的曲线拟合来评估刚度和阻尼系数。与现有的稳态CFD和理论模型相比,从本方法获得的系数与实验数据具有更好的相关性。这些转子动力系数随偏心率的变化有助于评估涡轮机械的安全设计。

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