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ON THE FAILURE OF A GAS FOIL BEARING: HIGH TEMPERATURE OPERATION WITHOUT COOLING FLOW

机译:气体箔轴承失效的研究:高温运行而无冷却流

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Implementing gas foil bearings (GFBs) in micro gas turbine engines is a proven approach to improve system efficiency and reliability. Adequate thermal management for operation at high temperatures, such as in a gas turbine or a turbocharger, is important to control thermal growth of components and to remove efficiently mechanical energy from the rotor mainly. The paper presents a test rotor supported on GFBs operating with a heated shaft and reports components temperatures and shaft motions at an operating speed of 37 krpm. An electric cartridge heater loosely inserted in the hollow rotor warms the test system. Thermocouples and non-contact infrared thermometers record temperatures on the bearing sleeve and rotor OD, respectively. No forced cooling air flow streams were supplied to the bearings and rotor, in spite of the high temperature induced by the heater on the shaft outer surface. With the rotor spinning, the tests consisted in heating the rotor to a set temperature, recording the system component temperatures until reaching thermal equilibrium in -60 minutes, and stepping the heater set temperature by 200 °C. The experiments proceeded without incident, the heater set temperature equaled 600 °C and 10 minutes into the test, noise became apparent and the rotor stopped abruptly. The unusual operating condition, without cooling flow and a too large increment in rotor temperature, reaching 250 °C, led to the incident which destroyed one of the foil bearings. Post-test inspection evidenced seizure of the hottest bearing (closest to the heater) with melting of the top foil at the locations where it rests on the underspring crests (bumps). Analysis reveals a notable reduction in bearing clearance as the rotor temperature increases until seizure occurs. Upon contact between the rotor and top foil, dry-friction quickly generated vast amounts of energy that melted the protective coating and metal top foil. Rather than a reliability issue with the foil bearings the experimental results show poor operating procedure and ignorance on the system behavior (predictions). A cautionary tale and a lesson in humility follow.
机译:在微型燃气轮机中实施气体箔轴承(GFB)是提高系统效率和可靠性的行之有效的方法。对于在高温下(例如在燃气轮机或涡轮增压器中)运行的适当热管理,对于控制组件的热增长并主要有效地从转子中去除机械能很重要。本文介绍了一个在带有加热轴的GFB上支撑的测试转子,并以37 krpm的运行速度报告了组件的温度和轴的运动。松散地插入空心转子中的电筒加热器使测试系统变热。热电偶和非接触式红外温度计分别记录轴承套和转子外径上的温度。尽管加热器在轴外表面上产生了高温,但仍未向轴承和转子提供强制的冷却气流。在转子旋转的情况下,测试包括将转子加热到设定温度,记录系统组件温度,直到-60分钟达到热平衡,然后将加热器设定温度步进200°C。实验进行时没有发生意外,加热器设定温度等于600°C,并且在测试开始10分钟后,出现了明显的噪音,转子突然停止了运转。异常的工作条件,没有冷却流以及转子温度升高到250°C太大,导致事故损坏了一个箔轴承。测试后的检查表明,最热的轴承(最靠近加热器)被卡住了,并且顶部箔片在靠在弹簧顶部(凸点)上的位置熔化了。分析表明,随着转子温度升高直至发生咬合,轴承的游隙显着减小。转子与顶部箔片接触后,干摩擦迅速产生大量能量,使保护涂层和金属顶部箔片熔化。实验结果显示,不良的操作程序和对系统行为(预测)的了解不大,而不是箔轴承的可靠性问题。接下来是一个警告性的故事和谦卑的教训。

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