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Characterization of unsteady loading due to impeller-diffuser interaction in centrifugal compressors

机译:由离心压缩机中的叶轮 - 扩散器相互作用引起的非稳态载荷的表征

摘要

Time dependent simulations are used to characterize the unsteady impeller blade loading due to imipeller-diffuser interaction in centrifugal compressor stages. The capability of simulations are assessed by comparing results against unsteady pressure and velocity measurements in the vaneless space. Simulations are shown to be adequate for identifying the trends of unsteady impeller blade loading with operating and design parameters. However they are not sufficient for predicting the absolute magnitude of loading unsteadiness. Errors of up to 14% exist between absolute values of flow quantities. Evidence suggests that the k - e turbulence model used is inappropriate for centrifugal compressor flow and is the significant source of these errors. The unsteady pressure profile on the blade surface is characterized as the sum of two superimposing pressure components. The first component varies monotonically along the blade chord. The second component can be interpreted as an acoustic wave propagating upstream. Both components fluctuate at the diffuser vane passing frequency, but at a different phase angle. The unsteady loading is the sum of the fluctuation amplitude of each component minus a value that is a function of the phase relationship between the pressure component fluctuations. Simulation results for different compressor designs are compared. Differences observed are primarily attributed to the amplitude of pressure fluctuation on the pressure side of the blade and the wavelength of the pressure disturbance propagating upstream. Lower pressure side pressure fluctuations are associated with a weaker pressure non-uniformity at the diffuser inlet as a result of a lower incidence angle into the diffuser. The wavelength of the pressure disturbance propagating upstream sets the domain on the blade surface in which the phase relationship between pressure component fluctuations is favorable. A longer wavelength increases the domain over which this phase relationship is such that the amplitude of unsteadiness is reduced.
机译:基于时间的仿真用于表征由于离心压缩机级中的叶轮-扩压器相互作用而引起的不稳定叶轮叶片负载。通过将结果与无叶片空间中的非恒定压力和速度测量值进行比较,可以评估仿真能力。结果表明,通过仿真可以充分识别带有工作参数和设计参数的叶轮叶片不稳定负载的趋势。但是,它们不足以预测载荷不稳定的绝对幅度。流量的绝对值之间存在高达14%的误差。有证据表明,所使用的k-e湍流模型不适用于离心压缩机流量,并且是这些误差的重要来源。叶片表面上的非恒定压力曲线的特征是两个叠加压力分量之和。第一分量沿叶片弦单调变化。第二分量可以解释为在上游传播的声波。这两个分量都以扩压器叶片通过频率波动,但相位角不同。非稳定载荷是每个分量的波动幅度之和减去一个值,该值是压力分量波动之间的相位关系的函数。比较了不同压缩机设计的仿真结果。观察到的差异主要归因于叶片压力侧的压力波动幅度和上游传播的压力扰动波长。较低的压力侧压力波动与在扩散器入口处的较弱的压力不均匀性有关,这是由于进入扩散器的入射角较小的结果。在上游传播的压力扰动的波长设定了叶片表面上的区域,在该区域中压力分量波动之间的相位关系良好。较长的波长增加了该相位关系所在的域,从而减小了不稳定的幅度。

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