Feasibility Study on the Effect of Blade Inclination for Heavy Duty Centrifugal Fans – Aerodynamic Aspects

T. Biedermann, Youssef Moutamassik, F. Kameier
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Abstract

With a special focus on the industrial feasibility and the manufacturability, a recently proposed novel approach to centrifugal impeller blade inclination is adopted and investigated through extensive CFD analysis. The fan blades, originally aligned perpendicular to the impeller backplate, are inclined in either forward or backward direction. For the presented study, an industrially proven fan design is chosen for testing. Compared to the original design, the inclined fan blades possess an increased total blade area and at the same time providing variable inflow angles at the leading edges of the blades. These two factors are expected to alter the fan characteristic curves in providing an increased range of optimum performance while maintaining high aerodynamic efficiency. The results obtained show a clear trend in aerodynamic performance with the degree of inclination, where the characteristic curves rotate at about the design point, allowing local improvements either at overload conditions or part-load conditions of the fan. Moreover, the trends obtained show the tendency to agree well with the rudimentary models published in previous studies, even though it appears to be affected by the fan volute and the point of operation as well.
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重型离心风机叶片倾角影响的可行性研究——气动方面
针对离心叶轮叶片倾角的工业可行性和可制造性,本文采用了一种新的计算方法,并对其进行了广泛的CFD分析。原本垂直于叶轮背板的风扇叶片,在向前或向后的方向上倾斜。对于提出的研究,一个工业证明的风扇设计被选择进行测试。与原来的设计相比,倾斜风扇叶片增加了叶片的总面积,同时在叶片的前缘提供了可变的入流角。预计这两个因素将改变风扇的特性曲线,在保持高空气动力学效率的同时,提供更大范围的最佳性能。得到的结果表明,气动性能随倾斜度的变化有明显的趋势,特性曲线在设计点附近旋转,使得风机在过载或部分负载条件下都能得到局部改善。此外,所获得的趋势显示出与先前研究中发表的基本模型非常一致的趋势,即使它似乎也受到风机蜗壳和操作点的影响。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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