多级轴流压气机全工况特性数值模拟

采用一种快速求解三维粘性流场的计算方法求解某多级轴流压气机内部流场及全工况特性。该方法以ＬＵ－ＳＧＳ－ＧＥ隐式格式和 ＭＵＳＣＬ ＴＶＤ迎风格式为基础，结合壁面函数方法和简单的混合长度湍流模型，使用多重网格迭代加速收敛技术对三维可压缩雷诺平均Ｎａｖｉｅ－Ｓｔｏｋｅｓ方程进行求解．叶列间参数的传递采用混合平面方法并应用了微机网络并行计算技术．首先对一个五排压气机（进口导叶加两级）进行了全工况特性计算，并对计算结果做了详细分析．然后对前三排（进口导叶加一级）进行了全工况特性计算并与五排联赛的计算结果进行了对比，对多级环境对单级性能的影响机理做了初步探讨。     

A method for calculating the absorption coefficient of a multi-layer absorbent using the electro-acoustic analogy

A theoretical method for calculating the absorption coefficient of the multi-layer absorbers composed of perforated plates, airspaces and porous materials is proposed. Initially, for multi-layer absorbers composed either of perforated plates and airspaces or perforated plates and porous materials, the acoustic impedance is calculated using an electro-acoustic analogy. Then, for multi-layer absorbers composed of perforated plates, airspaces and porous materials, the acoustic impedance is calculated using an iterative method. Finally, theoretical calculations for the absorption coefficient of three types of multi-layer absorbers composed of different materials and including perforated plates are carried out. The results are validated by experimental results.     

低速离心压气机的全工况数值模拟和校核

本文选用不同的计算模型和网格数目在全流量域对NASA低速离心压气机进行了数值模拟,通过与实验数据的对比检验了计算结果的精度,为具有无叶扩压器结构的低压离心压气机确定了合理的计算方案。同时通过计算结果的观察和对比,分析了小流量下叶轮内部流场的部分变化特征。     

涡旋压缩机空调系统数值化设计新途径

本文提出了楼用涡旋压缩机空调系统数值化设计的新途径,将房间瞬时热负荷与能力可连续调节的空调系统结合在一起,实现了真正意义上的空调数值化设计。文章从设计原理和实验两方面对空调数值化设计进行了分析,并对理论计算结果与实验结果做了对比。     

热力学第二定律演示仪

在热力学统计物理学的学习中，我们曾经学过十分重要的两条定律，即为热力学第一、第二定律，并且进行了这两个定律的实验演示。本主要介绍一种效果十分显的热力学第二定律演示仪。     

叶片尾缘掠型对离心压气机特性影响研究

针对叶片尾缘掠型对离心压气机特性影响开展了数值仿真与试验验证的研究工作,详细分析了尾缘掠型对压气机特性的影响规律和压气机叶轮内部流动特征,研究结果表明:尾缘掠型能够提升压气机出口的总压,使离心压气机压比变高,自由掠叶型相比于斜掠叶型,压比会进一步提升。叶片尾缘掠型能够有效抑制尾缘流动分离与叶间泄漏效应的结合效果,降低流动分离强度和分离区域,提升叶轮的稳定工作范围与效率。试验验证结果表明采用自由掠型尾缘叶轮,压比随着转速的升高提升幅度变大,最多提升了9.14%,喘振线明显向左偏移,运行流量范围拓宽。尾缘掠型能够有效提升压气机压比和稳定工作范围,是改善压气机特性的有效手段。     

Toward improved simulation tools for compressible turbomachinery: assessment of residual-based compact schemes for the transonic compressor NASA Rotor 37

Residual-based compact schemes of second- and third-order accuracy are applied to a challenging three-dimensional flow through a transonic compressor. The proposed schemes provide almost mesh-converged solutions in good agreement with experimental data on relatively coarse grids, which allow achieving a given accuracy level with computational cost reductions by a factor between 2 and 4 with respect to standard solvers.     

Experimental analysis of pressure distribution in a twin screw compressor for multiphase duties

This paper presents the results of an experimental investigation of pressure distribution inside working chamber of a twin screw compressor for multiphase duties. A mathematical model for describing the pressure distribution inside working chamber is proposed. By means of a small pressure transducer embedded into the groove at the root of the rotor, the pressure distributions of a multiphase compressor under various running conditions have been recorded successfully to verify the model. It is found that the pressure curve during the discharge process has a higher level under the conditions of the lower gas void fraction, higher discharge pressure, higher rotational speed and higher inlet pressure. The pressure distribution calculated by model in this paper shows good agreement with the data recorded by a small pressure sensor in a prototype multiphase compressor at the high gas void fractions under different operating conditions.     

制冷系统中双转子压缩机建模与性能分析

双转子压缩机主要用于热泵制冷系统中,该系统以CO2作为制冷剂,具有无毒、不易燃等特点,但是CO2体系制冷效能较低.为了提高制冷效能,有必要对双转子压缩机进行建模和分析.主要对CO2压缩机的工作过程进行了建模和分析,并编制仿真分析程序,对双转子压缩机模型第一、二级内部压力进行了连续测量,给出了详细的性能分析结果,给出了双...     

低温制冷机用线性压缩机效率的理论及实验研究

为了提高低温制冷机整机效率,基于力的平衡及电压平衡方程理论,分析了线性压缩机电机效率及电功转化为活塞表面声功效率的影响因素;并对线性压缩机效率进行了实验测量;理论与实验吻合较好;电机效率、电功转化为声功效率测量值与理论值偏差分别在3%及7%以内.最后对冷指确定时线性压缩机的优化设计方法进行了总结.