共查询到20条相似文献,搜索用时 15 毫秒
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螺旋式离心泵叶轮动平衡问题的优化设计 总被引:1,自引:0,他引:1
叙述了针对现有处理螺旋式离心泵叶轮动平衡问题所存在的不足,通过借助于三维CAD手段对叶轮进行优化设计,较好地解决了动平衡的问题,实现了既可减少叶轮的加工去重量,降低制作成本,改善泵加工质量,又可提高泵的工作效率,真正地达到以低的消耗.生产出高质、节能的螺旋式离心泵产品。 相似文献
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离心压缩机叶轮的形状优化设计 总被引:2,自引:0,他引:2
提出一种新的优化方法离心叶轮的形状优化问题,即在遗传算法中加入自适应算子调节个体变异概率,来保证搜索的全局性和种群的多样性。并在寻优过程中加入生物生长来加快其寻优速度。最后,采用遗传算法和改进的遗传算法-生物生长法两种方法,对叶轮进行优化设计。计算结果表明改进的遗传算法-生物生长法,在较少的优化时间得到最优解。 相似文献
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离心压缩机属于技术门槛高,且需整合多学科关键技术的透平机械。本文主要描述了整体齿轮式离心压缩机的设计理念、流程及关键气动参数的取值分析,并利用商用软件结合工程实例阐述单级整体齿轮式离心压缩机主要气动部件的设计流程、参数输出及实物机的验证。 相似文献
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N. V. Sokolov T. V. Maksimov M. B. Khadiev V. A. Futin 《Russian Engineering Research》2017,37(4):287-291
The equipment for dynamic tests of sliding thrust bearings is considered. The test data are analyzed for a thrust bearing with motionless pads in a centrifugal compressor with a semiclosed impeller in pumping mode. 相似文献
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基于Workbench整体叶轮流固耦合强度分析 总被引:1,自引:0,他引:1
作为许多动力机械的核心部件的叶轮,其强度及可靠性的问题日渐突出。叶轮工作时,流体力和高速旋转时的离心力为其主要载荷。基于Workbench软件对整体叶轮的内部流场和工作压力分布进行数值模拟;使用ANSYS CFX进行复杂几何形状叶轮的流体动力分析,得到了整体叶轮的流场和工作压力场及流体载荷在叶轮内部产生的等效应力分布图,并耦合了旋转离心载荷等,研究了在高压工况情况下,叶轮的载荷组成和流固耦合下的叶轮强度。 相似文献
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针对传统离心泵叶轮设计步骤繁琐的不足,提出了基于SolidWorks的三维参数化离心泵叶轮注塑模设计方法。简单介绍了SolidWorks的主要功能模块及离心泵叶轮模具设计的流程,详细阐述了离心泵叶轮模具设计的步骤。设计中,叶轮采用尼龙6/10材料,其拔模斜度为1.5°,收缩率为1%。通过对模具各零部件的造型与实时修改,实现了离心泵叶轮模具的参数化设计,并完成了模具的虚拟装配及加工出详图的快速输出。本方法对工程设计具有一定的实用价值。 相似文献
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Yong-sik Choi Jun-ho Lee Weui-bong Jeong Il-Geun Kim 《Journal of Mechanical Science and Technology》2010,24(7):1371-1377
In refrigerator designs, the linear compressor is preferable to the recipro-type compressor, due to its higher energy efficiency.
The linear compressor’s valve system, however, causes significant noise, not only in the steady state but also in the transient
state. To accurately predict the behavior of the suction and discharge valve system in both states, the interaction between
the fluid flowing through the valves and the structural deformation of the valves needs to be understood. In the present study,
the steady-state behaviors of the valve system were numerically analyzed using ADINA software, which takes fluid-structure
interaction (FSI) into account. This computational analysis thereafter was experimentally validated. The effects of a pre-load
of the conical compression spring on the dynamic characteristics of the valve system also were analyzed. 相似文献
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Sarhan Karray Zied Driss Hedi Kchaou Mohamed Salah Abid 《Journal of Mechanical Science and Technology》2011,25(7):1749-1760
A coupling algorithm is used to compute the equilibrium of a flexible anchor impeller in a stirred vessel. This coupling algorithm is based on a partitioned approach, which consists of three relatively independent modules: the computational fluid dynamics (CFD), the computational structure dynamics (CSD) and the interface. In the CFD module, the Euler formulation was used to account for the moving boundary. In the CSD module, the updated Lagrangian formulation for solving the motion of non-linear structure was used and a static study was adopted. In the interface module, an exchange of the forces and displacements was allowed. The numerical results, such as the velocity field, the turbulent kinetic energy, its dissipation rate, the turbulent viscosity and the mechanical deformation, have been presented. Particularly, we are interested in the study of the static behavior of the anchor impeller and the evolution of the displacement field of the arms during various iterations of our coupling algorithm. Accordingly, if the anchor impeller undergoes a deformation due to the flexion of the arms of the anchor impeller, the numerical results changes slightly from iteration to another. At the end of certain iteration, the anchor impeller becomes deformed and the velocity field is preserved. These results confirm that the fluid has a significant effect on the deformation of the arms of the anchor impeller during mixing depending on the velocity of the anchor impeller and the fluid flow. The numerical results were validated by a comparison with literature data. 相似文献
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Cavitation is one of the most important performance of centrifugal pumps. However, the current optimization works of centrifugal pump are mostly focusing on hydraulic efficiency only, which may result in poor cavitation performance. Therefore, it is necessary to find an appropriate solution to improve cavitation performance with acceptable efficiency. In this paper, to improve the cavitation performance of a centrifugal pump with a vaned diffuser, the influence of impeller geometric parameters on the cavitation of the pump is investigated using the orthogonal design of experiment(DOE) based on computational fluid dynamics. The impeller inlet diameter D_1, inlet incidence angle Δβ, and blade wrap angle φ are selected as the main impeller geometric parameters and the orthogonal experiment of L_9(3*3) is performed. Three-dimensional steady simulations for cavitation are conducted by using constant gas mass fraction model with second-order upwind, and the predicated cavitation performance is validated by laboratory experiment. The optimization results are obtained by the range analysis method to improve cavitation performance without obvious decreasing the efficiency of the centrifugal pump. The internal flow of the pump is analyzed in order to identify the flow behavior that can affect cavitation performance. The results show that D_1 has the greatest influence on the pump cavitation and the final optimized impeller provides better flow distribution at blade leading edge. The final optimized impeller accomplishes better cavitation and hydraulic performance and the NPSHR decreases by 0.63 m compared with the original one. The presented work supplies a feasible route in engineering practice to optimize a centrifugal pump impeller for better cavitation performance. 相似文献
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Design a small flow back-to-back two-stage centrifugal compressor in the aviation turbocharger, the compressor is compact structure, small axial length, light weighted. Stationary parts have a great influence on their overall performance decline. Therefore, the stationary part of the back-to-back two-stage centrifugal compressor should pay full attention to the diffuser, bend, return vane and volute design. Volute also impact downstream return vane, making the flow in circumferential direction is not uniformed, and several blade angle of attack is drastically changed in downstream of the volute with the airflow can not be rotated to required angle. Loading of high-pressure rotor blades change due to non-uniformed of flow in circumferential direction, which makes individual blade load distribution changed, and affected blade passage load decreased to reduce the capability of work, the tip low speed range increases. 相似文献