首页> 外文会议>International compressor engineering conference at purdue;2008 ICECP >Effects of Surface Roughness upon Gas Leakage Flow through Small Clearances in CO_2 Scroll Compressors
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Effects of Surface Roughness upon Gas Leakage Flow through Small Clearances in CO_2 Scroll Compressors

机译:表面粗糙度对CO_2涡旋压缩机小间隙气体泄漏流的影响

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This study presents empirical values of the friction factor for CO_2 gas leakage through thin rectangular cross-sectional openings of small axial and radial clearances between the orbiting and fixed scrolls of scroll compressors. Leakage flow experiments are conducted for different relative roughness of leakage channel surface. The pressure drop due to leakage is measured using a maximum pressure of 3 MPa. The Darcy-Weisbach equation for incompressible, viscous fluid flow through the thin rectangular cross-section is applied to calculate the pressure drop characteristics, where the empirical friction factors are determined and plotted on a Moody diagram. As a result, it is shown that the empirical friction factors for both axial and radial clearance leakage flows take on essentially the same values, strongly dependent on the relative roughness of leakage channel surface. Subsequently, the empirical friction factor is incorporated into computer simulations for a CO_2 scroll compressor with small cooling capacity to determine its optimal performance. As a result, it is shown that CO_2 scroll compressors can achieve higher performance levels by increasing the relative roughness of scroll wrap surfaces.
机译:这项研究提出了通过涡旋压缩机在动涡旋盘和固定涡旋盘之间轴向和径向间隙较小的矩形横截面细小矩形开口而泄漏CO_2气体的摩擦因数的经验值。针对泄漏通道表面的不同相对粗糙度进行泄漏流实验。由于泄漏造成的压降是使用3 MPa的最大压力测量的。通过不可压缩的粘性流体流过细长矩形横截面的Darcy-Weisbach方程来计算压降特性,确定经验摩擦因子并将其绘制在穆迪图中。结果表明,轴向和径向间隙泄漏流的经验摩擦系数取基本相同的值,强烈取决于泄漏通道表面的相对粗糙度。随后,将经验摩擦因数结合到具有较小冷却能力的CO_2涡旋压缩机的计算机模拟中,以确定其最佳性能。结果表明,CO_2涡旋压缩机可以通过增加涡旋涡卷表面的相对粗糙度来达到更高的性能水平。

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