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Aerodynamic journal bearing with a flexible, damped support operating at 7.2 million DN

机译:气动轴颈轴承,带柔性减震支撑,工作在720万DN

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摘要

This paper reports on the design, development and experimental validation of an aerodynamic journal bearing with a flexible, damped support operating at speeds up to 1.2 million rpm (= 7.2 million DN). In terms of the DN-number, this achievement represents to our knowledge a record for an air bearing of the self-acting type. Stabilization by means of a flexible, damped support therefore proves to be a promising solution to the dynamic stability problem ofhigh-speed gas bearings. In order to select the support parameters in an optimal way, a stability study is performed leading to the formulation of a series of dimensionless design guidelines. The proposed implementation, which makes use of elastomeric O-rings in combination with a tunable squeeze-film damper, is discussed in detail. A method for themanufacturing of miniature bearing bushes with a wave-shaped film height profile is outlined. Experiments up to 683 280 rpm are performed with an air-driven turbine and up to1 203 000 rpm with a helium-driven turbine. Deceleration experiments are conducted in order to obtain an estimation of the frictional losses of the system.
机译:本文报告了一种气动轴颈轴承的设计,开发和实验验证,该轴颈轴承具有柔韧性,减震的支撑,其转速最高为120万转/分钟(= 720万DN)。就DN编号而言,这一成就据我们所知代表了一种自作用式空气轴承的记录。因此,通过柔韧的阻尼支撑进行稳定是解决高速气体轴承动态稳定性问题的有希望的解决方案。为了以最佳方式选择支撑参数,进行了稳定性研究,从而制定了一系列无因次设计指南。拟议的实施方案,将弹性O形圈与可调式挤压膜阻尼器结合使用,将进行详细讨论。概述了一种制造具有波形薄膜高度轮廓的微型轴承衬套的方法。气动涡轮机最高可进行683 280 rpm的实验,而氦气涡轮机最高可进行1 203 000 rpm的实验。进行减速实验以获得系统的摩擦损失的估计值。

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