高级检索

航空压气机叶片增材修复最优热输入分析

Research on optimal heat input for blade repair of aero compressor

  • 摘要: 建立了压气机叶片MPAW增材修复传热模型,首先通过分析合金的热物性,计算出叶片MPAW增材修复的热输入范围,得到了不同热输入下熔池的温度分布. 之后创建了增材高度与送丝速度的数学模型,求解出不同送丝速度下的增材高度,并通过对焊缝截面温度分布的数值分析,进一步缩小热输入范围,得到试验参数. 最后通过数值分析及试验对比,揭示了合金修复区组织形貌与热输入率的演化规律,得到了最优的热输入和匹配的焊接参数.结果表明,试验结果与理论模型吻合度较好,验证了理论方法的有效性. 对于1 mm厚度的超薄压气机叶片的增材修复,采用研究得到的焊接参数,可达到最优热输入率,实现较好的增材形貌和增材修复效果.

     

    Abstract: A heat transfer model for MPAW additive manufacturing repair of compressor blades was established. Firstly, the heat input range was calculated by analyzing the thermal properties of the alloy, and the temperature distribution of molten pool under different heat input was obtained. After that, the mathematical model of the additive manufacturing height and wire feeding speed was established, and the height under different wire feeding speed was solved. Through the numerical analysis of temperature distribution of weld cross-section, the heat input range was further reduced and the experimental parameters were obtained. Finally, with numerical analysis and experimental comparison, the evolution law of microstructure and heat input rate of the alloy repair zone was revealed, and the optimal heat input and welding parameters were obtained. The experimental results are in good agreement with the theoretical model, which verifies the effectiveness of the theoretical method. The results show that the optimal heat input rate can be achieved by using the welding parameters obtained, and the better additive manufacturing morphology and repair effect can be achieved.

     

/

返回文章
返回