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STEAM FLOW AND HEAT TRANSFER IN THE INTERMEDIATE PRESSURE CYLINDER OF THE ULTRA-SUPERCRITICAL STEAM TURBINE

机译:超超临界汽轮机中间压力缸中的蒸汽流量和传热

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The cooling protection of the hot end is the key technique for ultra-supercritical steam turbine. Tangential direction cooling chamber has a simple form and stable cooling effectiveness. The influence of inlet Mach number, turbulent Prandtl number, rotational speed, and inlet turbulence intensity on cooling effect of the structure in ideal air model have been made by previous work. The cooling mechanism and the flow characteristic in the ideal air chamber were investigated. In this paper, the focus of the study is to investigate the flow and heat transfer characteristics of the tangential direction cooling chamber in the real steam model. The cooling chamber coupled with the whole steel shaft are simulated. Different boundary condition are compared. The heat transfer coefficients of the hub are acquired at some different rotational speeds and different hub conditions. The distribution of heat transfer coefficients and wall temperature are mainly affected by the viscous force and the velocity gradient near the hub.
机译:热端的冷却保护是超超临界汽轮机的关键技术。切向方向冷却室具有简单的形式和稳定的冷却效果。在先前的工作中,入口马赫数,湍流普朗特数,转速和入口湍流强度对理想空气模型结构的冷却效果的影响。研究了理想气室中的冷却机构和流动特性。在本文中,研究的重点是研究真实蒸汽模型中切向方向冷却室的流动和传热特性。模拟与整个钢轴联接的冷却室。比较不同的边界条件。在一些不同的旋转速度和不同的轮毂条件下获取集线器的传热系数。传热系数和壁温的分布主要受粘性力的影响和枢轴附近的速度梯度。

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