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Experimental Investigations on Vibration Characteristics for Bearing-Rotor System of Micro Gas Turbine

机译:微燃气轮机轴承转子系统振动特性的实验研究

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The dynamic characteristics of the rotor-bearing system for microgas turbine are the key factors that affect the safe and stable operation of the micro-gas turbine. This paper carried out the experimental investigations on the vibration characteristics during the speed-up process of rotating shaft, based on rotor structure of micro gas turbine generator supported by aerostatic bearings. Rotor vibration characteristics during conical whirling critical speed area, mixed control area, surge area, self-holding speed area, and bending critical speed area were analyzed. Simultaneously effects of bearing supply pressure and radial clearance on the shaft vibration characteristics were studied by experiments. The results showed that the ignition fuel flow has stepped increase when the ignition fuel valve was opened, which caused easily the rotor and bearing rubbing. And the reasonable bearing radial clearance and gas supply pressure can effectively restrain the occurring of the low frequency whirling and gas film oscillation, and improve the bearing-rotor system stability.
机译:用于微磁涡轮机的转子系统的动态特性是影响微燃气轮机安全稳定运行的关键因素。本文对旋转轴加速过程的振动特性进行了实验研究,基于空气轴承支撑的微型燃气涡轮发电机的转子结构。分析了锥形旋转临界速度区域,混合控制面积,喘振区域,自保持速度区域和弯曲临界速度区域的转子振动特性。通过实验研究了轴承供应压力和径向间隙对轴振动特性的影响。结果表明,当点火燃料阀打开时,点火燃料流动的阶梯增加,这易于易于转子和轴承摩擦。合理的轴承径向间隙和气体供应压力可以有效地抑制低频旋转和气体膜振荡的发生,并改善轴承转子系统稳定性。

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