首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Forward Blade Sweep Applied to Low-Speed Axial Fan Rotors of Controlled Vortex Design: An Overview
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Forward Blade Sweep Applied to Low-Speed Axial Fan Rotors of Controlled Vortex Design: An Overview

机译:前叶片扫掠应用于受控涡流设计的低速轴流风机转子:概述

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An over-view is given on the research maintained by the author about the design aspects of three-dimensional blade passage flow in low-speed axial flow industrial fan rotors, affected by spanwise changing design blade circulation due to controlled vortex design (CVD), blade forward sweep (FSW), and their combination. It was pointed out that, comparing the CVD method to the free vortex design, the fluid in the blade suction side boundary layer has an increased inclination to migrate radially outward, increasing the near-tip blockage and loss. It was concluded that the benefit of FSW, in terms of moderating loss near the tip, can be better utilized for the rotors of the CVD, in comparison to the free vortex design. Compared to the free vortex design, the FSW applied to the blades of the CVD was found to also be especially beneficial in loss reduction away from the end-walls, via shortening the flow paths on the suction side-in any case being elongated by the radially outward flow due to CVD-and thus, reducing the effect of wall skin friction. The necessity of correcting the swept blades was pointed out for matching with the prescribed CVD circulation distribution.
机译:作者概述了低速轴流工业风扇转子中三维叶片通道流动的设计方面的研究,该研究受到受控涡流设计(CVD)引起翼展方向变化的设计叶片循环的影响,刀片前掠(FSW)及其组合。要指出的是,将CVD方法与自由涡流设计相比,叶片吸力侧边界层中的流体具有增加的倾斜度,以径向向外迁移,从而增加了近端堵塞和损失。结论是,与自由涡流设计相比,FSW的好处是在尖端附近的适度损耗方面可以更好地用于CVD的转子。与自由涡流设计相比,发现通过将CVD叶片上的FSW缩短,可以缩短吸气侧的流路,从而特别有利于减少CVD叶片上的FSW,无论如何通过将FSW延长由于CVD径向向外流动,因此减少了壁皮肤摩擦的影响。指出了校正扫掠叶片的必要性以与规定的CVD循环分布相匹配。

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