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Aerostatic and Aerodynamic Performance of an In-Pump Spirally Grooved Thrust Bearing: Analysis and Comparisons to Static Load Experiments

机译:泵内螺旋沟槽止推轴承的空气静力和空气动力性能:静载荷实验的分析和比较

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摘要

The combined effects of external pressurization and in-pump spiral grooves are studied according to the incompressible Whipple analysis; the results are examined in terms of nondimensional parameters that bring out the interaction between the action of the spiral groove self-pressurization and that of the external pressurization through orifices. It is found that the interaction is significant when the supply pressure level to the orifices is near the peak pressure that can be reached by the spiral grooves alone. An optimized interacting design can improve the bearing stiffness. Away from the optimized interacting design, one of the two actions would dominate and the other one would cause a detraction of the bearing performance. As speed is sufficiently high, the pressurization action of spiral grooves causes the reduction of orifice flow and even its reversal. At such a condition the orifices are merely leakage paths that detract from the self-pressurization action of the spiral grooves. These predicted trends are qualitatively substantiated by tests.
机译:根据不可压缩的Whipple分析,研究了外部增压和泵内螺旋槽的综合作用。根据无量纲参数检查结果,该参数可显示出螺旋槽自加压的作用与通过孔的外部加压之间的相互作用。发现当孔口的供应压力水平接近仅由螺旋槽可达到的峰值压力时,相互作用是显着的。优化的相互作用设计可以提高轴承刚度。除了优化的交互设计之外,这两个动作之一将占主导,而另一个动作将导致轴承性能下降。当速度足够高时,螺旋凹槽的加压作用会导致孔口流量减少甚至逆转。在这样的条件下,孔口仅仅是泄漏路径,其损害了螺旋槽的自加压作用。这些预测的趋势通过测试定性地证实。

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