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Casing wall static pressure distribution behavior in a centrifugal compressor with asymmetric inlet/outlet structures

机译:具有不对称进/出口结构的离心压缩机的机壳壁静压力分布特性

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Asymmetric structures of the bent inlet pipes and outlet volute are typically adopted in centrifugal compressors. By using asymmetric inlet/outlet structures, the uniformity of the compressor's internal flow field in the circumferential direction will be changed. The static pressure distribution behavior around the casing wall is significantly influenced by the coupling effect of the bent inlet pipe and outlet volute. In the present work, three compressors were numerically and experimentally investigated. One compressor had a straight inlet pipe, and the other two had bent inlet pipes. Seventy-two static pressure sensors were mounted around the casing wall to obtain the static pressure distribution at different flow rates for three rotational speeds. The results show that at high rotational speeds with large flow rate conditions, when the static pressure waves induced by the bent pipe and volute act on the same circumferential position, the casing wall static pressure will be increased at the corresponding position. Furthermore, this high static pressure will further influence the static pressure values at other circumferential positions and leads to a more nonuniform circumferential static pressure distribution. Near the design flow rate, when the high static pressure strips, which are induced by both the bent pipe and volute impact different circumferential positions, the high static pressure strip induced by the volute will be weakened. As a result, the high static pressure strip induced by the volute cannot propagate upstream into the impeller. At small flow rate under designed rotational speed, the influence of the volute tongue on the casing pressure distribution will be enhanced. At small flow rate under low rotational speed, the casing pressure distributions of the three models were almost the same because the secondary flow effect of the bent pipe diminishes as the flow rate reduces.
机译:离心压缩机通常采用弯曲的入口管和出口蜗壳的不对称结构。通过使用不对称的入口/出口结构,将改变压缩机内部流场在圆周方向上的均匀性。弯曲的入口管和出口蜗壳的耦合作用显着影响套管壁周围的静压分布行为。在目前的工作中,对三台压缩机进行了数值和实验研究。一台压缩机的进气管是笔直的,另外两台的进气管是弯曲的。在外壳壁周围安装了72个静压传感器,以在三种转速下以不同的流量获得静压分布。结果表明,在大流量条件下的高转速下,当弯管和蜗壳产生的静压力波作用在同一圆周位置上时,相应位置的套管壁静压力将增大。此外,该高静压力将进一步影响其他圆周位置处的静压力值,并导致更不均匀的圆周静压力分布。在设计流量附近,由弯管和蜗壳共同引起的高静压带冲击不同的圆周位置时,蜗壳引起的高静压带会减弱。结果,由蜗壳引起的高静压带不能向上游传播到叶轮中。在设计转速下的小流量下,蜗壳舌片对套管压力分布的影响将增强。在低转速下的小流量下,三个模型的套管压力分布几乎相同,这是因为随着流量的减小,弯管的次级流量效应会减小。

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