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An Experimental Investigation Into the Temperature Profile of a Compliant Foil Air Bearing

机译:顺应箔空气轴承温度分布的实验研究

摘要

A series of tests was performed to determine the internal temperature profile in a compliant bump-type foil journal air bearing operating at room temperature under various speeds and load conditions. The temperature profile was collected by instrumenting a foil bearing with nine, type K thermocouples arranged in the center and along the bearing s edges in order to measure local temperatures and estimate thermal gradients in the axial and circumferential directions. To facilitate the measurement of maximum temperatures from viscous shearing in the air film, the thermocouples were tack welded to the backside of the bumps that were in direct contact with the top foil. The mating journal was coated with a high temperature solid lubricant that, together with the bearing, underwent high temperature start-stop cycles to produce a smooth, steady-state run-in surface. Tests were conducted at speeds from 20 to 50 krpm and loads ranging from 9 to 222 N. The results indicate that, over the conditions tested, both journal rotational speed and radial load are responsible for heat generation with speed playing a more significant role in the magnitude of the temperatures. The temperature distribution was nearly symmetric about the bearing center at 20 and 30 krpm but became slightly skewed toward one side at 40 and 50 krpm. Surprisingly, the maximum temperatures did not occur at the bearing edge where the minimum film thickness is expected but rather in the middle of the bearing where analytical investigations have predicted the air film to be much thicker. Thermal gradients were common during testing and were strongest in the axial direction from the middle of the bearing to its edges, reaching 3.78 8C/mm. The temperature profile indicated the circumferential thermal gradients were negligible.
机译:进行了一系列测试,以确定在室温下在各种速度和负载条件下运行的柔顺凸点型箔式轴颈空气轴承的内部温度曲线。通过对带有9个K型热电偶的箔轴承进行测量来收集温度分布,该9个K型热电偶布置在中心并沿着轴承的边缘,以便测量局部温度并估计轴向和周向的热梯度。为了便于测量气膜中的粘性剪切产生的最高温度,将热电偶点焊到与顶箔直接接触的凸块的背面。配合轴颈上涂有高温固体润滑剂,该润滑剂与轴承一起经历了高温启停循环,以产生光滑,稳态的磨合面。测试以20至50 krpm的速度和9至222 N的负载范围进行。结果表明,在所测试的条件下,轴颈旋转速度和径向负载均是热量产生的原因,而速度在轴瓦中起着更重要的作用。温度的大小。温度分布在20和30 krpm时几乎围绕轴承中心对称,但在40和50 krpm时稍微偏向一侧。出人意料的是,最高温度并未出现在预期的最小膜厚的轴承边缘,而是发生在轴承的中间,分析研究预测该温度会大大提高空气膜的厚度。热梯度在测试期间很常见,并且在轴向上从轴承中间到边缘的强度最大,达到3.78 8C / mm。温度曲线表明周向热梯度可以忽略不计。

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