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Simulation of Ni-Based Super-Alloy and Optimizing of Its Mechanical Properties in a Near-Shaped Turbine Blade Part

机译:镍基超合金涡轮叶片零件的模拟及其力学性能的优化

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This paper presents simulation of a Ni-based super-alloy during filling of a near-shaped turbine blade part to optimize its mechanical properties. Since geometrical shape of the airfoil is so complicated, a simple near-shaped part was made by plexiglass to water modeling. Condition and parameters of water modeling were obtained from the Procast software simulation. The flow pattern of the transparent systems, recorded by a high speed video camera, was analyzed. Air bubble amounts were quantitatively measured by an image analysis software. Quantified results were used to compare two systems in terms of ability to prevent bubble formation and entrainment. Both water modeling and computer simulating methods indicated that highest turbulences in bottom- and top-poured systems form in first initially pouring times. According to the water modeling results amount of bubble values was 40 and 18 percent for top-poured and bottom-poured systems, respectively. Then the Ni-base super-alloy IN939 is poured by investment casting in bottom- and top-poured systems and compared with each other. The results stated that bottom-poured system had higher mechanical properties compared to top-poured one. Ultimate tensile strength for the former was 820 MPa while for the part which was cast by bottom-poured system it was 850 MPa.
机译:本文介绍了一种镍基超级合金在近形涡轮叶片零件填充过程中的模拟,以优化其机械性能。由于机翼的几何形状非常复杂,因此通过有机玻璃到水的模型制作了一个简单的近形零件。水模型的条件和参数是从Procast软件仿真中获得的。分析了由高速摄像机记录的透明系统的流动模式。通过图像分析软件定量测量气泡量。量化结果用于比较两种系统在防止气泡形成和夹带方面的能力。水模型和计算机模拟方法均表明,在底部和顶部浇注系统中,在最初的最初浇注时间中形成了最高湍流。根据水模型结果,顶部注入和底部注入系统的气泡值分别为40%和18%。然后,通过熔模浇铸将镍基超级合金IN939浇铸在底部和顶部浇铸的系统中,并进行相互比较。结果表明,与顶部浇注的系统相比,底部浇注的系统具有更高的机械性能。前者的极限抗拉强度为820 MPa,而底部浇铸的零件的极限抗拉强度为850 MPa。

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