首页> 外文会议>ASME Turbine Technical Conference and Exposition >A SYSTEMATIC APPROACH TO ESTIMATE THE IMPACT OF THE AERODYNAMIC FORCE INDUCED BY ROTATING STALL IN A VANELESS DIFFUSER ON THE ROTORDYNAMIC BEHAVIOR OF CENTRIFUGAL COMPRESSORS
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A SYSTEMATIC APPROACH TO ESTIMATE THE IMPACT OF THE AERODYNAMIC FORCE INDUCED BY ROTATING STALL IN A VANELESS DIFFUSER ON THE ROTORDYNAMIC BEHAVIOR OF CENTRIFUGAL COMPRESSORS

机译:一种系统的方法来估算在离心式压缩机的旋转漫射器中旋转失速引起的空气动力学力的影响

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One of the main challenges of the present industrial research on centrifugal compressors is the need of extending the left margin of the operating range of the machines. As a result, interest is being paid in accurately evaluating the amplitude of the pressure fluctuations caused by rotating stall, which usually occurs prior to surge. The related aerodynamic force acting on the rotor can produce subsynchronous vibrations, which can prevent the machine to further operate, in case their amplitude is too high. These vibrations are often contained thanks to the stiffness of the oil journals. Centrifugal compressors design is, however, going towards alternative journal solutions having lower stiffness levels (e.g. Active Magnetic Bearings or Squeeze Film Dampers), which hence will be more sensitive to this kind of excitation: consequently, a more accurate estimation of the expected forces in presence of dynamic external forces like those connected to an aerodynamically unstable condition is needed to predict the vibration level and the compressor operability in similar conditions. Within this scenario, experimental tests were carried out on an industrial impeller operating at high peripheral Mach number. The dedicated test rig was equipped with several dynamic pressure probes that were inserted in the gas flow path; moreover, the rotor vibrations were constantly monitored with typical vibration probes located near the journal bearings. The pressure field induced by the rotating stall in the vaneless diffuser was reconstructed by means of an ensemble average approach, defining the amplitude and frequency of the external force acting on the impeller. The calculated force value was then included in the rotordynamic model of the test rig: the predicted vibrations on the bearings were compared with the measurements, showing satisfactory agreement. Finally, the prospects of the proposed approach are discussed by investigating the response of a real machine in high-pressure functioning when different choices of journal bearings are made.
机译:对离心式压缩机的目前工业研究的主要挑战之一是需要延长机器操作范围的左边缘。结果,在准确评估由旋转失速引起的压力波动的幅度时,正在支付兴趣,这通常在浪涌之前发生。作用在转子上的相关空气动力力可以产生次同步振动,这可以防止机器进一步操作,以防他们的幅度过高。由于石油期刊的刚度,通常包含这些振动。然而,离心式压缩机设计朝着具有较低刚度水平的替代轴颈溶液(例如有源磁轴承或挤压膜阻尼器),因此对这种激励更敏感:因此,更准确地估计预期力量需要具有连接到空气动力学不稳定状态的动态外力的存在来预测类似条件中的振动水平和压缩机可操作性。在这种情况下,在高周马赫数运行的工业叶轮上进行了实验测试。专用的试验台配备了几种动态压力探头,插入气流路径;此外,恒定监测转子振动,典型振动探头位于轴颈轴承附近。通过集合的平均方法重建由旋转延伸器中的旋转失速引起的压力场,限定作用在叶轮上的外力的幅度和频率。然后将计算的力值包括在测试钻机的旋转动力学模型中:将轴承上的预测振动与测量进行了比较,显示出令人满意的协议。最后,通过调查当轴颈轴承的不同选择时,通过研究现实机器在高压功能中的响应来讨论所提出的方法的前景。

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