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SENSITIVITY ANALYSIS OF CONDENSATION MODEL CONSTANTS ON CALCULATED LIQUID FILM MOTION IN RADIAL TURBINES

机译:径向涡轮中液体膜运动的冷凝模型常数的敏感性分析

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In many technical processes, a mixture of gas and steam is used as the working fluid in radial turbines. When condensation occurs during expansion, a portion of the liquid droplets can hit the rotor blades and form a water film, which can move in a radial direction and even against the flow direction. Then, the liquid film separates in the rotor tip clearance or at the leading edge of the rotor and forms coarse water droplets. The presence of coarse water droplets in the gap between stator and rotor can cause damage to the turbine rotor. To design a radial turbine which works under condensation conditions, it is essential to know where and when condensation and film formation occur. With this information, it is possible to take action to remove the liquid or to adjust the required maintenance intervals. To examine the details of condensation and film motion, an existing flow solver is extended to capture condensation effects. Models describing nucleation and droplet growth are added to a particle-tracking algorithm. Droplets impinging on the rotor blades form a liquid film. The motion of this liquid film is calculated with a newly developed thin film solver. The calculation tool is validated against third party test rig experiments as well as numerical experiments. For many parameters, the agreement between the calculation tool and the experiments is quite satisfactory. Some results, however, show larger deviations. One of these parameters is the droplet diameter. The numerical results are generally reliable, but an experimental validation is necessary for detailed understanding of the mechanism. Before expensive experiments are conducted, it is recommended to perform a sensitivity study to emphasize important parameters. This sensitivity study is performed concerning a radial turbine for an operating point at which the liquid film travels into the tip clearance. In this paper it will be shown how the thickness and movement of the liquid film change with variation in influencing parameters. Finally, model constants that have the strongest influence on the calculated film motion are highlighted.
机译:在许多技术过程中,气体和蒸汽的混合物被用作径向涡轮中的工作流体。当在膨胀过程中发生冷凝时,一部分液滴会撞击转子叶片并形成水膜,水膜可沿径向甚至逆着流向移动。然后,液膜在转子尖端间隙中或在转子的前缘处分离,并形成粗糙的水滴。定子和转子之间的间隙中存在粗糙的水滴会损坏涡轮机转子。为了设计一种在冷凝条件下工作的径流式涡轮机,必须知道在何时何地发生冷凝和成膜。利用此信息,可以采取措施除去液体或调整所需的维护间隔。为了检查冷凝和胶片运动的细节,扩展了现有的流量求解器以捕获冷凝效果。描述成核和液滴生长的模型被添加到粒子跟踪算法中。撞击在转子叶片上的液滴形成液膜。用新开发的薄膜求解器计算该液膜的运动。该计算工具已针对第三方测试平台实验和数值实验进行了验证。对于许多参数,计算工具与实验之间的一致性非常令人满意。但是,某些结果显示出较大的偏差。这些参数之一是液滴直径。数值结果通常是可靠的,但是需要实验验证才能详细了解该机理。在进行昂贵的实验之前,建议进行敏感性研究以强调重要的参数。这项敏感性研究是针对径向涡轮机进行的,其工作点是液膜进入尖端间隙的位置。在本文中,将显示液膜的厚度和运动如何随影响参数的变化而变化。最后,突出显示对计算的胶片运动影响最大的模型常数。

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