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Gradient Speed Control Method to Reduce the Residual Stress on a Turbine Disk in Forging Process

机译:梯度速度控制方法,以降低涡轮机磁盘磁盘磁盘的剩余应力

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The distribution of the residual stress on the turbine disk is affected by the forging process. The residual stress will reduce fatigue life of the turbine disk and increase the assemble error to meet the production. And the process parameters such as forging speed, forging temperature and friction will all affect the residual stress. In order to reduce the residual stress and improve the service life of the turbine disk, the relationship between the forging speed and residual stress on the turbine disk in the forging process was studied in this paper. By the combination of numerical simulation method and the forging process test, the numerical model of the forging process for the superalloy turbine disk was established, and the relationship between the residual stress distribution and forging speed was analyzed and calculated. Based on this, a gradient speed control method for reducing residual stress of the turbine disk was proposed. The calculation results showed that the gradient speed controlling in the forging process of the turbine disk effectively reduced the residual stress, decreased the usage and fee of the energy, and improved the service life of the turbine disk. According to the geometrical characteristics of the turbine disk, the gradient forging speed range was designed and optimized in this research. The results show that the residual stress of the turbine disk can be greatly reduced by the optimized gradient speed control method, which is a feasible way to reduce the residual stress of the superalloy turbine disks in the forging process.
机译:涡轮盘盘上的残余应力的分布受锻造过程的影响。残余应力将降低涡轮盘疲劳寿命,并增加组装误差以满足生产。而诸如锻速,锻造温度和摩擦的过程参数将所有都影响残余应力。为了降低剩余应力并改善涡轮盘的使用寿命,本文研究了锻造过程中涡轮机盘上的锻速度和残余应力之间的关系。通过数值模拟方法和锻造工艺测试的组合,建立了超合金涡轮盘的锻造工艺的数值模型,分析并计算了残余应力分布和锻速的关系。基于此,提出了一种降低涡轮盘残余应力的梯度速度控制方法。计算结果表明,涡轮盘锻造过程中的梯度控制有效地降低了残余应力,降低了能量的使用和费用,提高了涡轮盘的使用寿命。根据涡轮盘的几何特性,在该研究中设计和优化了梯度锻造速度范围。结果表明,通过优化的梯度速度控制方法可以大大降低涡轮盘的残余应力,这是降低锻造过程中超合金涡轮机磁盘的残余应力的可行方法。

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