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运用现代CFD方法设计高效率的汽轮机 总被引:3,自引:0,他引:3
T.Thiemann A.deLazzer M.Deckers 《热力透平》2003,32(2):86-94
论述了运用现代计算流体动力学(ComputationalFluidDynamics,CFD)技术设计高效率汽轮机的方法,典型应用的实例有全三维叶片级流场、叶片汽封和排汽蜗壳计算。计算结果和实际是相符的。进一步对结构性单元和非结构单元程序的计算结果进行了比较,已证明,非结构单元CFD程序用于复杂形状的流场计算时,结果与实际相当一致,并具有独特的功能。 相似文献
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论述了运用先进的计算流体动力学(Computational Fluid Dynamics,CFD)技术设计高效率汽轮机的方法,典型应用的实例有汽轮机多级全三维流场计算、叶片汽封计算和排汽缸计算。计算结果和实际吻合很好。进一步对用结构性单(structured cotie)和非结构单元(unstructured code)的计算结果进行了比较,可看出用非结构性单元CFD程序计算复杂形状的流场时,计算结果与实测值相当一致,并证明有特别好的功能。 相似文献
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采用计算流体力学(Computational Fluid Dynamics,简称CFD)开展了汽轮机高压缸整缸的内部流场计算和低压缸末三级的变工况分析。还采用CFD分析了某空冷机组低压排汽缸流场,比较了模型排汽缸的试验和数值计算结果,又分析实际排汽缸流场的CFD计算结果,提出并验证了一个提高其静压恢复能力的优化改进措施。在总结上述成功实践的基础上,展望了基于CFD等先进技术在汽轮机行业建立新技术体系的前景。 相似文献
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本文记录了先进的计算流体动力学(简称CFD)技术在高效率汽轮机设计中的应用,计算方法是通过强词经典的型线设计和一般的汽轮机设计方面,如整个通道的应力分析及几何特性的相互关系来描述的。该方法用于典型的汽轮机设计案例,即汽轮机多级全三维流场、叶片汽封和排汽缸的计算。CFD对设计过程的支持体现在:对复杂的流动特性提供更深入的物理认识,并为进一步研究和优化提供目标。通过比较计算结果和试验结果,评定了目前技术水平下CFD的预测能力。计算结果和试验结果取得很好的一致。还对由结构化网格和非结构化网格计算所得结果进行了相互比较,不仅证明了两者极好的一致性,而且示范了采用非结构网格的CFD软件模化复杂几何形状的特殊能力。总之,发现了CFD方法具备预测现代汽轮机组中发生的复杂三维粘性流动的能力,从而在整体上获得对流体动力机械更好的理解。性能进行预测,并对流场的总体动力特性有更好的了解。因此,先进的CFD技术是西门子发电集团设计高效率汽轮机的一个基本工具。 相似文献
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汽轮机低压进汽腔室设计的优劣对机组效率有明显的影响,其对效率的影响主要有两个因素,一是腔室本身的流动情况;二是腔室出口气流角与静叶的匹配情况。采用计算流体力学(CFD)方法模拟了基于不同设计方案进汽腔室的流场情况,并根据流场参数计算了第一级的级效率。研究表明,采用切向进汽方式,并且根据腔室出口气流角匹配静叶叶型,可以提高低压缸第一级叶片的效率,降低机组热耗。未来将会有越来越多的汽轮机采用切向进汽腔室,以提高机组的效率。 相似文献
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简要介绍了计算流体力学(CFD)技术的发展与数值方法。列举CFD通用分析软件应用于汽轮机通流级分析的几个典型算例。分析结果表明,应用先进的计算流体力学(CFD)技术进行汽轮机的通流设计,可有效提高设计机组的通流级效率和设计质量。CFD技术在汽轮机通流设计中的应用缩短了产品开发周期,节约了开发成本。 相似文献
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文章从宏观通流匹配设计方面对某国产亚临界双缸双排汽凝汽式300MW汽轮机的高、中压通流的效率进行了客观分析,并在此分析基础上提出了改进设计思路,按照改进思路完成了改进设计方案,用三维CFD方法对改进前后机组的经济性水平进行了评价。改造前后的经济性分析及机组的实测热耗结果表明,改进设计后机组的经济性达到同类机组的世界先进水平。 相似文献
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T.S. Dhanasekaran Ting Wang 《International Journal of Heat and Mass Transfer》2012,55(13-14):3818-3828
To achieve higher efficiency target of the advanced turbine systems, the closed-loop steam cooling scheme is employed to cool the airfoil. It is proven from the experimental results at laboratory working conditions that injecting mist into steam can significantly augment the heat transfer in the turbine blades with several fundamental studies. The mist cooling technique has to be tested at gas turbine working conditions before implementation. Realizing the fact that conducting experiment at gas turbine working condition would be expensive and time consuming, the computational simulation is performed to get a preliminary evaluation on the potential success of mist cooling at gas turbine working conditions. The present investigation aims at validating a CFD model against experimental results in a 180-degree tube bend and applying the model to predict the mist/steam cooling performance at gas turbine working conditions. The results show that the CFD model can predict the wall temperature within 8% of experimental steam-only flow and 16% of mist/steam flow condition. Five turbulence models have been employed and their results are compared. Inclusion of radiation into CFD model causes noticeable increase in accuracy of prediction. The reflect Discrete Phase Model (DPM) wall boundary condition predicts better than the wall-film boundary condition. The CFD simulation identifies that mist impingement over outer wall is the cause for maximum mist cooling enhancement at 45° of bend portion. The computed results also reveal the phenomenon of mist secondary flow interaction at bend portion, adding the mist cooling enhancement at the inner wall. The validated CFD simulation predicts that average of 100% mist cooling enhancement can be achieved by injecting 5% mist at elevated GT working condition. 相似文献
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The aim of presented work was the prediction of the losses in the wet steam flow through the last stage of 200MW steam turbine LP part.To this end,three numerical tools were used.The first method was the streamline curvature method (SCM) used on the meridional plane with losses correlations.The next two methods,TASCflow commercial CFD code and an in-house CFD code,based on the solution of the Reynolds- averaged Navier-Stokes equations (RANS).Ap- plication of three independent numerical tools al- lowed to make the more reliable losses analysis and made possible to compare applied numerical methods with each other. For the flow modeling in the last stage of LP steam turbine the various two-phase flow models were used and compared.The equilibrium model and non-equi- librium models with homogeneous and/or heterogeneous condensation were considered.The boundary conditions at the inlet and outlet from the stage were selected in such way to get the beginning of the homogeneous condensation process in the sta- tot.It corresponded to the part load of the turbine, i.e.140MW power and pressure in condenser 2.7kPa. 相似文献
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介绍了汽轮机级组特征通流面积在工程实际应用中的相关表达式,以某火电厂310MW机组为例,对汽轮机级组特征通流面积进行分析。通过计算级组特征通流面积的偏差率和级组的相对内效率,判断汽轮机通流部分的运行状况,得出汽轮机第Ⅰ级组通流面积减小、其它级组工作正常、第7段和第8段抽汽压力测量值不准确、以及第5段和第6段抽汽口可能有热蒸汽漏入的结论,并提出在机组大修中对重点部位进行检查和处理建议。实践证明,利用级组特征通流面积进行理论分析的结果与实际相吻合。 相似文献