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Hybrid Design Method for High-efficient and Low-Noise Multiple-sectioned Impeller of Backward-bladed Turbo Blower

机译:后叶片涡轮风机高效低噪声多段叶轮的混合设计方法

摘要

The present invention relates to a design method and a low noise implementation method of a turbo-type rear-wing three-dimensional impeller used in a centrifugal blower (fan) or a scrollless plenium blower (fan), in particular, the three-dimensional impeller and two-dimensional impeller unit shroud and back plate It combines in the middle height of to overcome the difficulty of manufacturing the injection mold of the three-dimensional impeller to achieve high efficiency, and also to reduce the low noise and load noise after applying the lean angle corresponding to 2.5 dimensions in the low noise method Design method, the rear curvature has more than one curvature radius other than the curvature on the rotating surface so that lift fluctuation caused by the vortex generated in the rear stage is amplified, and the noise emitted from the rear stage is canceled near the rear stage to make noise emission. Backward curvature design method to weaken, phase of vortex at the low and high point of tooth-shaped rear end is 360˚ Or, it is a multiple of it, and the toothed rear design method for reducing the rear noise by canceling the vortex and the curvature of the leading edge of the shroud inlet are adjusted to adjust the vane pass frequency of the turbofan and its harmonic frequency noise. The present invention relates to a method of realizing low noise by combining a method of designing curvature of the leading edge and the like.;Blower, multiple impeller, turbo type, rear wing, high efficiency, low noise design, rear noise
机译:离心式鼓风机(风扇)或无涡旋式鼓风机(风扇)中使用的涡轮式尾翼三维叶轮的设计方法和低噪声实现方法技术领域叶轮和二维叶轮单元护罩和背板结合在中间高度,克服了制造三维叶轮注塑模具难以获得高效率的要求,并降低了应用后的低噪音和负荷噪音在低噪声方法设计方法中,对应于2.5维的倾斜角,后曲率具有一个以上的曲率半径,而不是旋转表面上的曲率,从而放大了由后级产生的涡流引起的升力波动,并且从后级发出的噪音在后级附近被抵消,从而发出噪音。向后弯曲的设计方法可以减弱,在齿形后端的低点和高点处的涡流相位为360°或是它的倍数,而有齿的后部设计方法可通过消除涡流来减少后部噪音调节护罩入口前缘的曲率,以调节涡轮风扇的叶片通过频率及其谐波频率噪声。本发明涉及通过组合设计前缘的曲率等的方法来实现低噪声的方法。鼓风机,多叶轮,涡轮型,后翼,高效,低噪声设计,后噪声

著录项

  • 公开/公告号KR100719103B1

    专利类型

  • 公开/公告日2007-05-17

    原文格式PDF

  • 申请/专利权人

    申请/专利号KR20050089093

  • 发明设计人 이승배;박덕준;김남욱;

    申请日2005-09-26

  • 分类号F04D29/66;G06F17/50;

  • 国家 KR

  • 入库时间 2022-08-21 20:32:13

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