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Investigation of Radial Gas Bearings with Longitudinal Micro-Grooves of Various Transverse Profiles

机译:各种横向型材纵向微槽径向气体轴承的研究

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For a radial gas bearing with two lines of compressed gas supply into the working gap with blind micro-grooves of a constant and variable depth of the following profiles: triangular or stepped, with the increasing or decreasing depth of the micro-groove in the direction of movement of the compressed gas - radial lifting force, gas consumption and performance ranges were founded. In the study of the effect of blind micro-grooves of different transverse profiles (seven options) on the characteristics of radial bearings the, authors used the methods of cyclic sweep (grooves of a triangular transverse profile) and the method of splines (stepped grooves). The calculations with optimal design parameters (maximum ratio of the radial lifting force to the gas flow rates) showed that the radial bearing with longitudinal micro-grooves of various transverse profiles, the depth of which decreases in the direction of gas flow, has a significantly greater radial lifting force (by 54% at P_H = 5; λ = 2; ae = 0.25; a = 0.676) compared with a suspension with the grooves of a constant depth and efficient in the range of practical use of supports, unlike the suspensions with micro-grooves with a minimum depth in the area of compressed gas supply.
机译:对于具有两条压缩气体的径向气体轴承进入工作间隙,其具有以下轮廓的恒定和可变深度的盲微槽:三角形或阶梯,在方向上增加或减小微槽的深度建立了压缩气体径向提升力,煤气消耗和性能范围的运动。在研究不同横向型材(七种选项)对径向轴承特性的影响中,作者使用了循环扫描(三角形横曲面的凹槽)的方法和花键的方法(阶梯式凹槽)。具有最佳设计参数的计算(径向提升力与气流速率的最大比率)显示,径向轴承具有各种横向轮廓的纵向微槽,其深度在气流方向上减小,具有显着的方向更大的径向提升力(P_H = 5的54%;λ= 2; ae = 0.25; a = 0.676)与悬浮液在恒定深度和高效的悬架中,与悬浮液不同,与悬架不同在压缩气体供应面积中具有最小深度的微槽。

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