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Centrifugal multi-wing type ventilator performance improvement and Numerical simulation

机译:离心式多翼式通风机性能改进及数值模拟

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The existing and mature CFD technology is applied in this paper. Through the simulation of the prototype, it's found that there are obvious vortices in the cochlea part of the centrifugal multi-wing type ventilator. Two schematic plans are adopt to improve efficiency of the centrifugal multi-wing type ventilator. These vortices can cause high energy loss. At the same time, they increase noise of the ventilator and affect efficiency. The first scheme is to increase radius of the cochlea. The second scheme is to change the cochlea into tilted. Some experiments of the velocity of outlet of the centrifugal multi-wing type ventilator also have been carried on which are in order to make some comparison. It can be found that unsuitable change of the cochlea radius caused more disorder airflow rather than improve the cochlea vortices. So the conclusion obtained is that the key issue is to find the suitable radius of the cochlea in design of the centrifugal multi-wing type ventilator. During the design of tilted cochlea, a satisfying outcome is obtained.
机译:本文采用了现有的,成熟的CFD技术。通过对样机的仿真,发现离心式多翼式通风机的耳蜗部分存在明显的涡旋。为了提高离心式多翼式通风机的效率,采用了两个示意图。这些旋涡会导致高能量损失。同时,它们会增加呼吸机的噪音并影响效率。第一种方案是增加耳蜗的半径。第二种方案是将耳蜗变成倾斜的。为了进行比较,还对离心式多翼式通风机的出口速度进行了一些实验。可以发现,耳蜗半径的不适当改变导致更多的无序气流,而不是改善了耳蜗涡。因此得出的结论是,关键问题是在离心式多翼式呼吸机的设计中找到合适的耳蜗半径。在倾斜耳蜗的设计过程中,获得了令人满意的结果。

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