首页> 外文会议>ASME Turbo Expo: Turbomachinery Technical Conference and Exposition >EXPERIMENTAL AND NUMERICAL STUDY ON PRESSURE LOSSES AND FLOW FLUCTUATIONS IN A HIGH-PRESSURE VALVE ASSEMBLY OF STEAM TURBINE GOVERNING SYSTEM
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EXPERIMENTAL AND NUMERICAL STUDY ON PRESSURE LOSSES AND FLOW FLUCTUATIONS IN A HIGH-PRESSURE VALVE ASSEMBLY OF STEAM TURBINE GOVERNING SYSTEM

机译:汽轮机控制系统高压阀组件压力损耗和流量波动的实验与数值研究

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Aerodynamic measurements and numerical simulations carried out on a model of a high-pressure valve assembly used for nozzle governing of a turbine with 135MW output are described in this paper. Aim of the study is to investigate effects of control valve's strainers on pressure losses and unsteadiness in the flow field. It is an important task since undesirable flow fluctuations can lead to operational reliability issues. Measurements were carried out in the Aerodynamic laboratory of the Institute of Thermomechanics of the Czech Academy of Sciences (IT) where an aerodynamic tunnel is installed. Numerical simulations were carried out in the Doosan Skoda Power (DSP) Company using ANSYS software tools. The experimental model consists of one of two identical parts of the real valve assembly. It means it consists of an inlet pipeline, a stop valve, a valve chamber with two independent control valves, its diffusers and outlet pipelines. The numerical model consists of both assembly parts and includes also an A-wheel control stage in order to simulate the real turbine operating points. The different lifts of the main cone in each control valve for its useful combinations were investigated. Results were evaluated on the model with control valve's strainers, which were historically used in order to stabilize the flow, and without them. The results of the experimental measurement were compared with the numerical results in the form of pressure losses prediction. From measured pressure fluctuations, it was found out where and for which conditions a danger of flow instabilities occurs. It can be concluded that there is a border, in terms of operating conditions, where the flow field starts to be unstable and this border is different dependent of the fact whether the control valve's strainers are used or not. Therefore, the areas of safe and danger operational reliability can be predicted. The influence of the control valve's strainers on the maximal amplitude of periodic fluctuations appears only for the cases when valves are highly overloaded. For normal operating conditions, there is no difference. As a result, the control valve's strainers do not have to be used in standard applications of valve assemblies. Furthermore, a loss model for valve pressure loss estimation could be updated. Therefore, a pressure loss should be predicted with a sufficient accuracy for each new turbine bid with similar valve assemblies.
机译:本文描述了用于用135MW输出的涡轮机的喷嘴控制的高压阀组件的模型上进行的空气动力学测量和数值模拟。该研究的目的是研究控制阀过滤器对流场中压力损失和不稳定的影响。这是一个重要的任务,因为不良流动波动可能导致操作可靠性问题。测量是在捷克科科学院的热机械研究所(IT)的空气动力学实验室进行了测量,其中安装了空气动力学隧道。使用ANSYS软件工具在Doosan Skoda Power(DSP)公司中进行了数值模拟。实验模型包括真实阀组件的两个相同部件中的一个。这意味着它由入口管道,止动阀,具有两个独立控制阀的阀室,其漫射器和出口管道组成。数值模型包括两个组装部件,并且还包括一个轮子控制级,以便模拟真正的涡轮机操作点。研究了每个控制阀中的主要锥体的不同升降机以其有用的组合。结果是在历史上使用的控制阀过滤器的模型中评估了历史上,以稳定流动,而无需它们。将实验测量结果的结果与压力损失预测的形式的数值结果进行了比较。从测量的压力波动中,它发现了在其中发生了流动不稳定性的危险的地方。可以得出结论,在运行条件方面存在边界,其中流场开始不稳定,这种边界不同的取决于是否使用了控制阀的过滤器。因此,可以预测安全和危险的操作可靠性的领域。控制阀的过滤器对周期性波动最大幅度的影响仅在阀门高度过载时仅出现。对于正常的操作条件,没有区别。结果,控制阀的过滤器不必用于阀组件的标准应用中。此外,可以更新用于阀压力损失估计的损耗模型。因此,应以具有相似瓣膜组件的每个新涡轮机竞标的足够精度来预测压力损失。

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