增压器叶轮根部裂纹、缩孔缺陷解决及尺寸精度控制

Resolution of Cracks and Shrinkage Cavity Defects at Turbocharger Impeller Root & Dimensional Accuracy Control

  • 摘要:   
      本文旨在解决涡轮增压器叶轮铸造过程中的裂纹、缩孔缺陷及尺寸精度难题。文章从机理分析→工艺适配优化设计→实验验证研究,通过理论建模、实验测试与行业需求对接相结合,形成 "结构 - 工艺 - 性能 - 应用" 的闭环研究,揭示叶轮叶片根部裂纹与轮毂缩孔的萌生机理;建立适配叶轮结构特性的高精度铸造工艺体系;实现叶轮制造缺陷率由40%降至 3% 以下、合格率提升至 95% 以上,且工艺具备批量生产能力。
      本文旨在解决涡轮增压器叶轮铸造过程中的裂纹、缩孔缺陷及尺寸精度难题。文章从机理分析→工艺适配优化设计→实验验证研究,通过理论建模、实验测试与行业需求对接相结合,形成 "结构 - 工艺 - 性能 - 应用" 的闭环研究,揭示叶轮叶片根部裂纹与轮毂缩孔的萌生机理;建立适配叶轮结构特性的高精度铸造工艺体系;实现叶轮制造缺陷率由40%降至 3% 以下、合格率提升至 95% 以上,且工艺具备批量生产能力。

     

    Abstract: This paper aims to address the challenges of cracks, shrinkage defects, and dimensional accuracy in the casting process of turbocharger impellers. Through a closed-loop research framework integrating "structure-process-performance-application," the study combines theoretical modeling, experimental testing, and industry requirements. It reveals the initiation mechanisms of cracks at the blade root and shrinkage cavities in the hub; establishes a high-precision casting process system tailored to impeller structural characteristics; and achieves a reduction in manufacturing defect rates from 40% to below 3%, with qualification rates exceeding 95%, while ensuring the process is suitable for mass production.

     

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