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A study of heat transfer between the walls and gas inside the cylinder of a reciprocating compressor.

机译:往复式压缩机气缸壁与气体之间的传热研究。

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摘要

A numerical model of the flow and heat transfer inside the cylinder of a reciprocating compressor is used to analyze the heat transfer between the wall and the gas. A control volume finite-difference technique is used in conjunction with the SIMPLER algorithm to solve the ensemble averaged equations for conservation of mass, momentum and energy. Turbulence closure is obtained with a version of the k-;The numerical model is tested by computing the flow and heat transfer in a Helium-filled gas spring operating over a wide range of speeds, and comparing the numerical results with recent measurements by other researchers. At low speeds the flow is laminar and hysteresis loss is controlled by conduction. At higher speeds the flow is turbulent and the roll up of a corner vortex between the piston and the cylinder wall is observed. For both high and low speeds a significant phase difference occurs between the heat transfer at the gas-wall interface, and the difference between the bulk gas temperature and the cylinder wall temperature. Overall, the predictions of hysteresis loss are in very good agreement with the experiments, except for the highest speed tested (1000 RPM) where the magnitude of the hysteresis loss is small.;The numerical model is used to simulate a single-cylinder reciprocating compressor operating at 1750 RPM, using Refrigerant 12 as the working fluid. Results of the compressor simulations show that the flow field inside the cylinder is dominated by a large vortex driven by the jet of gas from the suction port. This vortex thoroughly mixes the gas so that the temperature field is relatively uniform, except for steep gradients near the walls. Parameter studies show that completely eliminating the heat transfer results in slight performance gains: a 1 percent increase in mass flow rate, and a 1.6 percent decrease in work input per unit mass. Large reductions in cylinder wall temperature have the same effect as eliminating the heat transfer. Design changes that affect the suction jet do not significantly change the heat transfer between the walls and the gas.
机译:往复式压缩机气缸内部的流动和传热的数值模型用于分析壁和气体之间的传热。控制体积有限差分技术与SIMPLER算法结合使用,以求解整体平均方程,以守恒质量,动量和能量。通过使用k-版本获得湍流闭合;通过计算在各种速度下运行的充氦气弹簧中的流动和传热并将该数值结果与其他研究人员的最新测量结果进行比较,来测试数值模型。在低速下,流动是层流的,磁滞损耗由传导控制。在较高的速度下,流动是湍流的,并且观察到活塞和气缸壁之间的拐角涡旋卷起。对于高速和低速两者,在气壁界面处的传热与本体气体温度与气缸壁温度之间的差之间会出现明显的相位差。总体而言,磁滞损耗的预测与实验非常吻合,除了最高测试速度(1000 RPM)时磁滞损耗的幅度很小。;数值模型用于模拟单缸往复式压缩机使用制冷剂12作为工作流体以1750 RPM的转速运行。压缩机模拟的结果表明,气缸内部的流场受来自吸入口的气体射流驱动的大涡旋支配。该涡流充分混合了气体,因此,除了壁附近的陡峭梯度外,温度场相对均匀。参数研究表明,完全消除传热会导致轻微的性能提升:每单位质量的质量流量增加1%,功输入减少1.6%。气缸壁温度的大幅度降低与消除热传递具有相同的效果。影响吸力射流的设计变更不会显着改变壁与气体之间的热传递。

著录项

  • 作者单位

    University of Minnesota.;

  • 授予单位 University of Minnesota.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 1989
  • 页码 250 p.
  • 总页数 250
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机械、仪表工业;
  • 关键词

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