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Design and Development of Turbodrill Blade Used in Crystallized Section

机译:结晶截面使用的涡轮机刀片的设计与开发

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Turbodrill is a type of hydraulic axial turbomachinery which has a multistage blade consisting of stators and rotors. In this paper, a turbodrill blade that can be applied in crystallized section under high temperature and pressure conditions is developed. On the basis of Euler equations, the law of energy transfer is analyzed and the output characteristics of turbodrill blade are proposed. Moreover, considering the properties of the layer and the bole-hole conditions, the radical size, the geometrical dimension, and the blade profile are optimized. A computational model of a single-stage blade is built on theANSYS CFDinto which the three-dimensional model of turbodrill is input. In light of the distribution law of the pressure and flow field, the functions of the turbodrill blade are improved and optimized. The turbodrill blade optimization model was verified based on laboratory experiments. The results show that the design meets the deep hard rock mineral exploration application and provides good references for further study.
机译:Turbodrill是一种液压轴流式涡轮机,具有由定子和转子组成的多级刀片。在本文中,开发了一种在高温和压力条件下可以在结晶截面中施加的涡轮机叶片。在欧拉方程的基础上,分析了能量转移规律,提出了涡轮机刀片的输出特性。此外,考虑到层和泡孔条件的性质,自由基尺寸,几何尺寸和叶片轮廓被优化。在Theansys CFdinto上建立了单级刀片的计算模型,该摩擦仪的三维模型被输入。鉴于压力和流场的分配定律,涡轮机刀片的功能得到改善和优化。基于实验室实验验证了Turbodrill刀片优化模型。结果表明,该设计符合深厚岩石矿物勘探应用,并为进一步研究提供良好的参考。

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