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首页> 外文期刊>Journal of nuclear engineering and radiation science >Numerical Modeling and Experimental Validation of a Supercritical CO2-Lubricated Hydrodynamic Journal Bearing
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Numerical Modeling and Experimental Validation of a Supercritical CO2-Lubricated Hydrodynamic Journal Bearing

机译:超临界CO2-润滑流体动力轴颈轴承的数值建模与实验验证

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摘要

The supercritical carbon dioxide (sCO(2)) Brayton cycle is an attractive thermal cycle for compact power generation applications due to its high efficiency and power density. Hydrodynamic gas journal bearings are attractive for this application due to their simplicity. Lubricating the bearings with sCO(2) from the primary loop would be ideal, as this would eliminate the need for a separate lubricant source or complex seals and pumps to reduce the bearing lubricant pressure below the operating pressure of the primary loop. However, few studies in the literature have examined the behavior of a hydrodynamic journal bearing lubricated with supercritical fluid and none have experimentally demonstrated the operation of such a bearing. This paper describes the development of a simple numerical model of a hydrodynamic journal bearing operating under laminar conditions. The model incorporates the real gas properties of sCO(2) and therefore can be used to qualitatively investigate the impact of operation near the critical point and the scaling relationships between inlet pressure and the bearing drag and stiffness. The model predictions are compared to results that would be obtained by assuming constant fluid properties in order to assess the effects on bearing performance of the large gradients in properties that occur near the critical point and to determine over what range of inlet conditions the constant-property simplification is valid. The modeling results show that bearing drag and stiffness rise linearly throughout the subcritical regime, but sharply rise by approximately 50% at the critical pressure. However, the behavior predicted by the real gas model closely matches those obtained from the constant-property model (CPM) for all conditions that are more than 3 kPa away from the critical pressure. To validate the prediction that bearing operation follows the same scaling relationships near the critical pressure as at low pressure, a test assembly consisting of a turbomachine driven by a motor and supported on tilt-pad hydrodynamic gas journal bearing was operated in a CO2 environment at 35 degrees C with pressures up to 7.336 MPa. The bearing operated smoothly and did not exhibit signs of instability such as whirl. Coast down measurements were conducted to estimate the bearing drag at various pressures up to 5.612 MPa. The bearing coefficient of friction, f, inferred from these tests increased with system pressure from 0.359 at atmospheric pressure to 0.619 at 5.612 MPa. The peak bearing Reynolds number during operation was approximately 400. These results indicate that hydrodynamic bearing operation using sCO(2) is possible without significant reduction in bearing performance; however, further testing should be carried out in order to validate the model results concerning bearing stiffness.
机译:超临界二氧化碳(sCO(2))布雷顿循环因其高效率和高功率密度而成为紧凑型发电应用中极具吸引力的热循环。流体动力气体径向滑动轴承由于其简单性,在这种应用中很有吸引力。从一回路使用sCO(2)润滑轴承是理想的,因为这样就不需要单独的润滑油源或复杂的密封件和泵,从而将轴承润滑油压力降低到一回路的工作压力以下。然而,文献中很少有研究考察超临界流体润滑的流体动力滑动轴承的行为,也没有实验证明这种轴承的运行。本文描述了在层流条件下工作的流体动力滑动轴承的简单数值模型的发展。该模型结合了sCO(2)的真实气体特性,因此可用于定性研究临界点附近运行的影响,以及入口压力与轴承阻力和刚度之间的比例关系。将模型预测结果与通过假设恒定流体性质获得的结果进行比较,以评估临界点附近出现的较大性质梯度对轴承性能的影响,并确定恒定性质简化在何种进口条件范围内有效。模拟结果表明,轴承阻力和刚度在整个亚临界区呈线性上升,但在临界压力下急剧上升约50%。然而,实际气体模型预测的行为与从恒定特性模型(CPM)中获得的结果非常吻合,适用于距离临界压力超过3 kPa的所有条件。为了验证轴承在临界压力附近的运行遵循与低压下相同的缩放关系的预测,在35°C的CO2环境下,压力高达7.336 MPa的条件下,对一个试验组件进行了操作,该组件由一台由电机驱动的涡轮机械组成,并支撑在倾斜垫流体动力气体径向轴承上。轴承运行平稳,没有出现旋转等不稳定迹象。进行滑行测量,以估计在高达5.612 MPa的各种压力下的轴承阻力。从这些试验中推断出的摩擦承载系数f随着系统压力的增加而增加,从大气压力下的0.359增加到5.612 MPa下的0.619。运行期间的峰值轴承雷诺数约为400。这些结果表明,在不显著降低轴承性能的情况下,使用sCO(2)进行流体动力轴承操作是可行的;然而,应进行进一步测试,以验证有关轴承刚度的模型结果。

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