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RESEARCH ON STRUCTURAL DESIGN AND ANALYSIS OF S-CO_2 TURBINE IMPELLER

机译:S-CO_2透平叶轮结构设计与分析研究

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The Brayton cycle with supercritical carbon (S-CO_2) as working medium is one of the most promising new nuclear power systems. Turbine is the key device during the working process in the Brayton power cycle. The turbine structural presents small size and extremely high rotational speed for the special physical properties of S-CO_2, which increase the difficulty for the structural design and strength safety significantly. According to the aerodynamic design and optimization results of 200 kW S-CO_2 radial inflow turbine, this paper proposes a detail structural design and analysis method for turbine impeller. Based on the three-dimensional blade profile data and meridional planes data, key structural design parameters are chosen and the parametric geometry model is established by CAD tools. On this basis, numerical simulation models of turbine are established to analyze the structural strength in detail. Then the influence of parameters on the turbine impeller strength is studied by a series of finite element numerical procedures. The influence mechanisms of key structural design parameters on impeller strength are discussed. Moreover, the final model of turbine impeller is obtained by parameter comparison and selection. The results show that for the initial model, the maximum von-Mises equivalent stress is 400.10 MPa, the maximum radial deformation is 0.0333 mm and the maximum axial deformation is 0.0770 mm. For the final model, the maximum von-Mises equivalent stress is 294.26 MPa, the maximum radial deformation is 0.0279 mm and the maximum axial deformation is 0.0769 mm. The maximum von-Mises equivalent stress and maximum radial deformation of structural decreases 26.45 % and 16.22 % respectively compared with the initial model. As a result, the impeller structural strength safety margin is obviously improved by the parameter analysis.
机译:以超临界碳(S-CO_2)为工作介质的布雷顿循环是最有前途的新型核动力系统之一。涡轮机是布雷顿(Brayton)动力循环中工作过程中的关键设备。涡轮机结构由于S-CO_2的特殊物理特性而具有较小的尺寸和极高的转速,这大大增加了结构设计的难度和强度安全性。根据200 kW S-CO_2径向进水涡轮的气动设计和优化结果,提出了一种详细的涡轮叶轮结构设计和分析方法。基于三维叶片轮廓数据和子午面数据,选择关键的结构设计参数,并通过CAD工具建立参数化几何模型。在此基础上,建立了水轮机数值模拟模型,对结构强度进行了详细分析。然后通过一系列有限元数值程序研究了参数对涡轮叶轮强度的影响。讨论了关键结构设计参数对叶轮强度的影响机理。此外,通过参数比较和选择获得了涡轮叶轮的最终模型。结果表明,对于初始模型,最大von-Mises当量应力为400.10 MPa,最大径向变形为0.0333 mm,最大轴向变形为0.0770 mm。对于最终模型,最大冯·米塞斯等效应力为294.26 MPa,最大径向变形为0.0279毫米,最大轴向变形为0.0769毫米。与初始模型相比,结构的最大von-Mises等效应力和最大径向变形分别降低了26.45%和16.22%。结果,通过参数分析,明显提高了叶轮结构强度的安全裕度。

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