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对采用双轴承支撑的D系列鼓风机的轴承座的结构进行了分析,提出了一种用于有害气体输送风机的密封型式。通过对高压密封气体的流量和压力的计算,证明该密封型式结构简单、密封效果好。 相似文献
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通过对中国石化股份公司巴陵分公司己内酰胺生产使用的进口多级离心式压缩机轴封状况剖析,结合大修阶段备件库存状况,通过大胆实践,采用国产部件对该压缩机组一、二、三级轴封实施国产化改造,从密封机理、材料选用、工艺状况以及实际运行参数多方面论证实施国产化改造的可行性与必要性。 相似文献
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从总体布局、节流间隙宽度的确定、节流齿数的选取及腔形状的确定等四个方面,介绍了结构设计原则。阐述了泄漏速率的计算方法。最后做了几点说明。 相似文献
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济钢中厚板厂现有离心式鼓风机10台,分别用于加热炉送风,轧机主电机冷却,地下室通风,冷床钢板冷却。它们对生产的正常运行有着重要的影响。 离心式鼓风机的结构如图1。 图1 离心式鼓风机的结构简图 由图1可以看出,离心式鼓风机由机壳,叶轮,主轴,油箱,联轴器,电机组成。油箱两端为轴承座,主轴上的两盘滚动支撑轴承分别安装在两个轴承座内,轴承座外侧为轴封,防止润滑油泄漏,这种风机的结构简单,运行稳定,但是,在使用中发现,风 相似文献
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Recent studies on staggered labyrinth seals have focused on the effects of different parameters,such as the pressure ratio and rotational speed on the leakage flow rate.However,few investigations pay sufficient attention to flow details and the sealing mechanism,which would be of practical importance in designing seals having higher performance.This paper establishes a theoretical model to study the seal mechanism,thus revealing that leakage is determined by the pressure ratio and geometric structure.Numerical simulation is implemented to illustrate details of the flow field within the seal structure.Viscous dissipation is used to quantitatively investigate the contribution that each location makes to the seal performance,revealing that orifices and stagnation points are the most important positions in the seal structure,generating the most dissipation.The orifice is carefully studied by using the theoretical model.Experiments for different pressure ratios are conducted and the results match well with those of the theoretical model and numerical simulation,verifying the theoretical model and analysis of the seal mechanism.Three new designs,based on a good understanding of the seal mechanism,are presented,with one reducing leakage by 24.5%. 相似文献
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CFD Study on Stepped and Drum Balance Labyrinth Seal 总被引:2,自引:0,他引:2
The stability of rotors in turbomachines is affected by the labyrinth seal where driving forces are generated. Recent research results have shown that the preswirl has a significant influence on the rotordynamic characteristics of the straight labyrinth seal including both tooth-on-stator and tooth-on-rotor configurations. However, modern turbomachines require higher and higher pressure drop for the seal so that the eye seal is usually designed as stepped labyrinth, whereas the balance drum usually employs a tooth-interlocking labyrinth and a larger number of teeth. Both designs could generate greater forces on the rotor than the straight labyrinth seal. Therefore, it is necessary to further study the influence of preswirl on stepped and tooth-interlocking labyrinth seals. This article employed 3D calculational fluid dynamics (CFD) to solve the flow in those seals. Then the rotordynamic coefficients of the two seals at different preswirl rates were calculated based on the CFD results. The results were compared with test data and bulk flow results. A rotor stability analysis was conducted considering the balance drum seal with the coefficients predicted by the numerical method. 相似文献
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对油封表面微织构的形状进行组合设计,应用Abaqus仿真分析不同组合微织构油封的静态接触压力和变形影响矩阵;基于二维平均雷诺方程,建立考虑表面粗糙度以及唇口油膜空化现象影响的流体润滑模型,分析不同形状微织构对旋转油封密封性能的影响规律。结果表明:在相同工况下,相较于无织构油封,微织构对油封泵吸率以及油膜厚度提升较为显著,且组合型织构的提升效果优于单一三角形织构;三角形与半圆形组合织构对油封泵吸率的提升效果最佳,半圆形与方形组合织构对油封油膜厚度的提升为最佳。 相似文献
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直通式篦齿密封性能的数值模拟与试验研究 总被引:1,自引:0,他引:1
利用 FLUENT 软件对过热蒸汽分级机转轴的篦齿密封的内部流场进行数值模拟,对影响其性能的部分因素进行分析。结果表明,篦齿密封两端压差对泄漏量的影响非常明显,压差越大,泄漏量越大;篦齿密封的泄漏量随着节流间隙宽度增大而增大,但两者是非线性的关系;在齿形角不变的情况下,篦齿空腔深度小于2 mm 时对密封泄漏量的影响很大,而空腔深度大于2 mm 时对密封泄漏量的影响很小;转轴转速对泄漏量基本没有影响。通过试验验证了数值模拟方法计算篦齿密封泄漏量的可行性。 相似文献
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基于FLUENT迷宫密封动力特性分析 总被引:1,自引:0,他引:1
利用CFD有限元软件Fluent计算迷宫密封三维流场,提出一种计算密封动力特性系数的方法,并研究了偏心率、入口预旋、涡动速度对转子密封动力特性的影响.计算结果表明:入口预旋是产生交叉刚度的主要原因,入口预旋越大交叉刚度越大;主刚度和交叉阻尼与偏心率的关系基本上是线性的,而交叉刚度和主阻尼随偏心率变化呈现明显的非线性.交叉刚度和主阻尼是影响密封转子系统稳定性的重要因素. 相似文献
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基于FLUENT的迷宫密封机理研究 总被引:1,自引:0,他引:1
针对影响迷宫密封泄漏特性的三个因素:间隙宽度、齿型夹角以及空腔深宽比,计算了不同结构的内部流场,探讨了各因素对泄漏特性的影响,分析了密封机理。结果表明:迷宫密封的泄漏量随间隙的增大而增大,并得到满足泄漏量条件的最大间隙宽度cmax≈0.57mm;在一定深宽比下,存在最佳齿型角度,随着压比的增加,最佳齿型角度的影响加大;空腔深度和空腔宽度之间存在最佳匹配关系,且空腔深宽比不随间隙宽度的变化而变化。 相似文献