考虑设计与非设计工况下叶轮与螺旋机匣特性的螺旋机匣设计新方法及CFD数值验证

P. Epple, M. Fritsche, M. Steppert, Michael Steber
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摘要

用于工业应用的径向风扇通常与螺旋外壳一起操作,也称为蜗壳。蜗壳的作用是收集叶轮出口的空气,并将其输送到风机出口。在蜗壳内,叶轮的切向速度分量在蜗壳出口处转化为直线速度分量。在蜗壳内,静压随蜗壳横截面积的增大而增大。当流体流出叶轮时,流量基本上由径向速度分量乘以叶轮出口面积给出。而蜗壳内的流量基本由叶轮出口处和蜗壳内考虑角动量守恒的切向速度分量给出。因此,只有一个工作点,即蜗壳的设计点,在这里叶轮内的流量与蜗壳内的流量相匹配。在文献中,蜗壳的设计仅在设计点进行,并且通常计算蜗壳的横截面积,使流量从隔舌到蜗壳出口呈线性分布。本文提出了一种考虑设计点流量和非设计点流量的扩展理论方法。在设计点上,考虑特定叶轮的特性,即在叶轮出口处的径向和切向速度分量来设计蜗壳。此外,在蜗壳的设计过程中还考虑了叶轮的非设计特性,即其径向和切向速度分量。叶轮内流量与蜗壳内流量仅在设计点匹配,在非设计点叶轮内流量与蜗壳内流量不匹配。这对叶轮-蜗壳单元的设计过程有重要的影响。每个蜗壳还必须与特定的叶轮相匹配。在数值部分,考虑到特定叶轮的特性,设计了一个普通蜗壳。利用商用Navier-Stokes求解器ANSYS CFX对蜗壳和整机风扇的性能进行了研究。对计算结果和蜗壳内以及叶轮-蜗壳单元内的流动情况进行了详细的分析,并与新蜗壳理论预测的结果进行了比较。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
New Design Method for Spiral Casings Considering the Properties of the Impeller and Spiral Casing at Design and Off-Design Conditions and Numerical Verification With CFD
Radial fans for industrial applications are very commonly operated with a spiral casing, also called volute. The function of the volute is to collect the air from the impellers outlet and to transport it to the fans outlet. In the volute the tangential velocity component of the impeller is transformed in a straight velocity component at the volute’s outlet. In the volute the static pressure is increased according to the cross sectional area of the volute. When the flow exits the impeller the flow rate is given basically by the radial velocity component times the outlet area of the impeller. In the volute, however, the flow rate is basically given by the tangential velocity component at the impeller exit and in the volute considering the conservation of angular momentum. Hence, there is only one operating point, i.e. the design point of the volute, where the flow rate in the impeller matches the flow rate in the volute. In the literature the design of the volute is performed at the design point only and the cross sectional area of the volute is usually computed distributing the flow rate linearly from the tongue to the exit of the volute. In this work an extended theoretical approach was developed considering the design point flow rate and off design flow rates. At the design point, the properties of the specific impeller, i.e. it’s radial and its tangential velocity components at the impeller’s exit are considered to design the volute. Furthermore, also the off-design characteristics of the impeller, i.e. its radial and tangential velocity components are considered in the design process of the volute. The flow rates in the impeller and in the volute match only at the design point, at off-design points the flow rates in the impeller and in the volute are different. This has an important impact on the design process of impeller – volute units. Each volute has also to be matched to the specific impeller. In the numerical part a usual volute was designed considering the properties of a particular impeller. The performance of the volute and of complete fan was investigated with the commercial Navier–Stokes Solver ANSYS CFX. A detailed analysis of the results and the flow conditions in volute as well as in the impeller-volute unit and a comparison with the results predicted by the new volute theory is given.
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