共查询到19条相似文献,搜索用时 171 毫秒
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针对用于可燃气体等介质回收、输送装置的传统双螺杆压缩机单向受力的不足,提出一种平衡式双螺杆压缩机。为掌握平衡式双螺杆压缩机排气区域流体运动特性,应用CFD(Computational Fluid Dynamics)技术中的SIMPLEC算法及RNG/k-ε(Renormalization-group k-ε)湍流模型,对不同排气压力下平衡式双螺杆压缩机排气过程进行了数值模拟;研究了其排气区域流体湍流动能,流动轨迹及速度矢量的分布情况,从而得到了不同工况下泄露、涡流及回流的分布及变化特征;为平衡式双螺杆压缩机排气孔口的优化设计及进一步提升其运行性能提供理论依据。 相似文献
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针对某R22半封闭螺杆制冷压缩机,通过动网格的划分建立充分考虑轴向排气孔口面积变化的排气流场模型,利用Fluent软件进行流场的动态数值模拟;将模拟得到的流场结果作为LMS的边界条件,模拟得到了双螺杆压缩机排气噪声频谱图;通过试验测量结果对模拟结果进行了验证;并进一步分析压缩机排气流道优化设计对气流脉动和噪声的影响。研究结果表明:模拟与试验的压力脉动最大值的误差在5%以内,噪声频谱的变化趋势基本一致;压缩机排气过程气流脉动主要集中在排气孔口处,并在排气腔内有明显衰减;光顺排气腔流道和增设周向排气导流槽,可有效减少排气过程的压力脉动;模拟和试验结果都表明:以模拟结果为依据的排气腔流道优化有效地降低了压缩机噪声,说明本文所述研究方法可指导半封闭双螺杆制冷压缩机的优化设计。 相似文献
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为了研究专门针对双螺杆压缩机存在转子单向受力问题而开发的一种平衡式双螺杆压缩机工作腔内齿顶间隙对其内部流场特性的影响规律,运用SCORG软件构建一种可完全兼顾实际工作间隙的工作腔流体模型,并在进行高质量代数网格划分的前提下,基于CFD(Computational Fluid Dynamics)技术对三种不同尺寸齿顶间隙的平衡式双螺杆压缩机流体模型进行内部流场特性的精确数值分析,得到了流场压力分布、速度分布以及排气压力脉动随齿顶间隙的变化规律。为平衡式双螺杆压缩机间隙优化设计及工程应用提供重要理论支撑。 相似文献
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双螺杆捏合机转子型线设计与数值模拟 总被引:1,自引:0,他引:1
利用曲面共轭原理建立双螺杆捏合机转子型线设计与螺杆转子共轭曲面啮合方程的数学模型,提出一种可对高黏度物料进行输送、混合及塑化作用的新型双螺杆捏合机螺杆转子型线,给出转子螺旋副组成齿型线参数方程,进行转子结构设计.建立双螺杆捏合机流场数值仿真模型,依据计算流体动力学理论,对非牛顿流体流动进行三维、等温稳态有限元数值分析,研究其在不同转速及中心距条件下流场压力场分布、速度场分布、最大切应力、物料流动速率等特性;依据流固耦合理论,求解捏合机内部流体和双螺杆转子结构耦合方程,研究不同工况下流体压力和扭矩对螺杆转子应力和变形影响的变化规律.研究结果为双螺杆捏合机转子型线、结构参数的设计以及工艺参数的合理设定提供理论依据. 相似文献
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Kyoung-Ku Ha Tae-Bin Jeong Shin-Hyoung Kang Hyoung-Jin Kim Kwang-Min Won Chi-Yong Park Woo-Youl Jung Kyung-Seok Cho 《Journal of Mechanical Science and Technology》2013,27(11):3287-3297
A variety of centrifugal compressors are used in various fields of industry such as aircraft, home appliances, and vehicles. Comfort and quietness are important in these uses. As a result, noise has become an important consideration in compressor design besides the conventional performance parameters such as efficiency and pressure ratio. However, compressor noise has been difficult to understand because of the lack of information. The aim of this paper is to investigate the aero-acoustic characteristics of a centrifugal compressor for the fuelcell vehicle by experiments. The existing compressor system is modified to measure the internal pressure fluctuation at the impeller inlet, the impeller outlet and the diffuser outlet. Four microphone probes are also installed to determine the external noise levels and spectra of the compressor in an airtight room according to the RPM and mass flow rate. The test results show the possibility to tell the relative noise level of a centrifugal compressor with the internal pressure data. The external microphone signals have relation to the internal pressure signals. They have similar patterns and spectra. It is a noteworthy phenomenon because it is easier and inexpensive to predict pressure behaviors than noise characteristics of centrifugal compressors. The dominant noise source is the tonal noise during normal operation. But the broadband noise component due to the turbulent flow in the compressor increases during low flow rate operation. Computational simulations are carried out to describe these phenomena and to identify noise indicators. The turbulence kinetic energy and the pressure distribution obtained from CFD results may be indicative of the relative noise intensity of the compressor. The experimental facility, instrumentation and simulation conditions are described, and the results are presented in this paper. 相似文献
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阴阳转子型线设计时存在参数修改频繁、性能实验搭建不便等问题,影响了转子型线设计效率的提高,针对以上问题,提出将
NURBS曲线和流体仿真技术应用于双螺杆压缩机转子型线设计中的新思路。以单边不对称摆线-销齿圆弧式转子型线为研究对象,开发了新型双螺杆转子型线。应用NURBS曲线构建了螺杆转子的齿廓线;建立了双螺杆压缩机原型线与新型线流场仿真模型,运用Fluent软件模拟了其在工作转速下压强与流速的分布规律。由仿真结果对新型线设计的合理性进行了预判,并为新型线的改进优化直至获得性能优良的双螺杆压缩机阴阳转子提供了参考依据。 相似文献
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高速离心压缩机旋转失速的全流场数值模拟 总被引:4,自引:1,他引:3
使用商业计算流体动力学(Computational fluid dynamics,CFD)计算软件CFX求解三维雷诺平均的Navier-Stokes方程组,结合出口气腔模型对某带无叶扩压器的离心压缩机的旋转失速现象进行数值模拟。为了准确地模拟小流量下的失速流动现象,在CFD计算中采用包括蜗壳在内的全场网格。首先使用定常计算得到该离心压缩机的稳态性能曲线,并和试验测量值进行比较。然后引入出口气腔模型,模拟离心压缩机内的旋转失速流动。在小流量下模拟得到离心压缩机内部流场的非定常流动现象。分析气腔模型不同参数对失速流动的影响,气腔体积越大,计算得到的失速频率越低。 相似文献
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针对一款典型的高压比离心压气机SRV2,采用NUMECA软件,计算其内部的流场情况,并对这些流动状态进行研究。研究表明,离心压气机中主要存在3种二次流结构,这些二次流相互作用,形成了离心压气机中常见的射流尾迹结构。该研究对于改进离心压气机设计、提高其性能具有重要意义。 相似文献
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以一种新型同步阀为研究对象,应用 UG软件建立了三维几何模型,借助 ANSYS CFX 14.5流体分析软件,用标准紊流模型模拟了阀内部流场内流体的同步分流情况及流动状态,得到了阀内部的压力场、速度场等流体状态。对阀改进前模型的数值模拟结果表明分流精度很低,同步精度不存在理论性误差,原因是结构不合理,导致节流口面积不能补偿负载压差的影响。故对阀结构改进后,分流精度得到了较大程度的提高。所得阀内部流体的压力和速度的分布情况,为合理改变同步阀结构及节流口面积函数提供了参考依据。 相似文献
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In current research on deflector jet servo valves, the receiver pressure estimated using traditional two-dimensional simulation and theoretical calculation is always lower than the experimental data; therefore, credible information about the flow field in the prestage part of the valve can hardly be obtained. To investigate this issue and understand the internal characteristics of the deflector jet valve, a realistic numerical model is constructed and a three-dimensional simulation carried out that displays a complex flow pattern in the deflector jet structure. Then six phases of the flow pattern are presented, and the defects of the two-dimensional simulation are revealed. Based on the simulation results, it is found that the jet in the deflector has a longer core area and the fluid near the shunt wedge cannot resist the impact of the high-speed fluid. Therefore, two assumptions about the flow distribution are presented by which to construct a more complete theoretical model. The receiver pressure and prestage pressure gain are significantly enhanced in the calculations. Finally, special experiments on the prestage of the servo valve are performed, and the pressure performance of the numerical simulation and the theoretical calculation agree well with the experimental data. Finally, the internal mechanism described by the theoretical and numerical models is verified. From this research,more accurate numerical and theoretical models are proposed by which to figure out the internal characteristics of the deflector jet valve. 相似文献
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用数值模拟方法对高压比大小叶片斜流式叶轮内部全三维有粘流场进行了详细分析,获得该压缩机的特性曲线和主要参数分布。计算结果表明,设计点达到设计要求值,斜流叶轮内部流动正常,满足性能要求,叶轮的小叶片在气流通道后部还有一定的改进余地。 相似文献