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《汽轮机技术》2017,(5)
为研究核电汽轮机高压级内非定常流动对湿蒸汽凝结流动液滴直径、压力以及湿汽损失等参数分布的影响,采用湿蒸汽非平衡凝结相变模型,对定常与非定常流动状态下湿蒸汽自发凝结流动进行三维数值分析。结果表明:非定常凝结流动趋于稳定时,各项参数的分布呈现周期性变化规律。非定常流动的动静干涉现象导致周向流场具有非均匀性,湿蒸汽级内的轴端功率下降0.266%。非定常流动过程中的静叶尾迹现象致使下游动叶通道内自发凝结的液滴直径减小。非定常凝结流动的压力位势作用使得动叶出口平均压力提高。非定常流动引起湿蒸汽凝结的热力学损失与制动损失分别升高62.27%和1.88%,疏水损失降低0.233%。 相似文献
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采用遗传算法及人工神经网络的优化算法,把某汽轮机末级常规静叶片改型设计成海豚仿生型叶片。利用两相均质数值方法和湿蒸汽平衡相变模型,以商用软件CFX为计算平台,模拟了常规原型与新设计的海豚型叶栅流场。通过对计算结果进行比较,分析该海豚型叶片与常规叶片在气动性能上的异同,探索海豚型叶片是如何通过改变叶栅流道内蒸汽湿度的分布状况来更好地适应叶栅内湿蒸汽跨音速流动。 相似文献
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为分析自发射流条件下非定常尾迹对叶顶间隙流动、S1流面和S2流面上流场参数、叶尖泄漏比和动叶载荷变化的影响,采用数值模拟方法,以Durham叶栅为原型,将动、静叶栅流场通过滑移网格技术耦合,开展非定常计算。结果表明:在静叶非定常尾迹的影响下,转子区域流场内的流动、叶尖间隙泄漏比及叶片周向载荷均呈现出周期性变化的特征;考虑非定常效应和端壁相对运动效应,相较于无叶尖射流,单孔叶尖自发射流可使泄漏比降低4.57%,比定常计算预测的泄漏比低3.43%,表明要想准确获得叶尖射流条件下的叶栅流动特性和叶尖泄漏抑制效果,其间的非定常效应不可忽略。 相似文献
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在某汽轮机除湿级的空心静叶上设计了不同的热蒸汽喷射缝,应用两相均质混合模型和湿蒸汽平衡相变模型,对具有缝隙的叶栅流场进行了全三维定常的数值计算。引入参数的方法进行能量转化过程的经济性评估。结果表明:尾缘喷射热蒸汽时,同一喷射流量下,缝隙宽度越大,有效效率越高。同时,在较大缝隙宽度下,有一个最佳的喷射流量,此时的有效效率最高。压力面中部喷射热蒸汽时,在喷射流量比小于6%下,各方案的有效效率均比无热蒸汽喷射的原型要高。同一喷射流量下,顺主流喷射且缝隙宽度越大,其有效效率越高。 相似文献
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针对平原河网地区汇流模拟困难且成果难以校验的特点,提出一种与平原河网非恒定流计算模型相耦合的汇流模型。模型提出概化单元的概念,并通过水量平衡方程和水动力方程加以数学表达。实例验证结果表明,该模型能有效模拟田间径流与骨干河网相互影响的实际情况。 相似文献
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There are two difficulties encountered in modeling valveless micropumps using lumped-element methods. The pressure loss coefficient for fluidic diodes used in valveless pumps to rectify flow depends on the flow direction. A problem arises in choosing the proper loss correlation because the flow direction is not known a priori. Another problem is the quadratic form of the equation for the flow through the fluidic diodes, which brings about multiple solutions. The above problems become even more serious in multi-chamber cases. They are overcome in this study by suitably formulating the flow resistance. In addition, the flow inertia is accounted for in the unsteady model. The steady and unsteady models are evaluated by comparing with CFD simulations, which also serve to illustrate the flow field in more detail. It is shown that, compared with the steady model, the variation of the flow rate and pressure predicted by the unsteady model behaves in a close manner to those obtained by multidimensional calculations. 相似文献
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David Afungchui Baddreddinne Kamoun Ali Helali Abdellatif Ben Djemaa 《Renewable Energy》2010,35(1):307-313
The aim of this paper is to numerically explore the non-linear two-dimensional unsteady potential flow over a Savonius rotor and to develop a code for predicting its aerodynamics performances. In the model developed, the rotor is represented in a median plane by two semicircles, displaced along their common diameter. The two semicircles can be considered to produce lifting effects. As a result, they are modelled by a collection of discrete vortices on their contours. The flow field is then governed by the Laplace equation. The versatile Neumann boundary condition, applied over the contour of the semicircles and the Kutta Joukowsky condition applied at the four extremities of the semicircles have been used in the modelling. The torque distribution of the stationary rotor and the unsteady pressure field on the blades of the rotating rotor, predicted by the code developed, have been compared and validated by some experimental data. 相似文献
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稳态与非稳态下旋风分离器气相流场数值模拟方法研究 总被引:1,自引:0,他引:1
为了研究旋风分离器气相流场的特性,在稳态与非稳态下,采用雷诺应力方程模型(RSM)对一台气一固旋风分离器气相流场进行了数值模拟和计算,其中旋风分离器网格划分采用混合网格分块划分技术,对流项分别采用不同阶格式进行离散,将数值模拟结果与试验数据进行了比较.结果表明:在非稳态下,动量(Momentum)方程采用二阶迎风格式(SOU),湍动能走、耗散率£采用高阶的Quick离散格式,雷诺应力项(Reynolds stresses)采用一阶迎风格式(FOU)是模拟旋风分离器气相流场的最佳选择. 相似文献
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用数值模拟的方法对大功率蒸汽轮机抽汽口(从通流部分到抽汽管)的流场进行了研究,给出了流场模拟的数学模型及其解法。详细描述了从通流部分到抽汽管的各段内流场的结构。指出:由于抽汽的影响,在通流部分外径处抽汽缝进口前壁的位置形成了一个惯性涡区,相对于抽汽道其它部分来说,该旋涡区所造成的流动损失最大;在通流部分不但出现了参数的径向不均匀分布,也出现了参数的周向不均匀分布;集气室内形成了一对旋转方向相反的螺旋涡,并将计算结果与实验结果进行了比较。 相似文献