斜齿隐藏腔型篦齿环加工工艺优化研究

Optimization of machining process for helical-tooth hidden-cavity sealing labyrinth rings

  • 摘要: 航空发动机篦齿环作为关键封严部件,其高温合金材质与隐藏腔型结构在数控加工中面临排屑困难、刀具崩损等共性挑战。现有工艺研究多集中于常规结构,对此类深腔、小倾角特征的加工策略尚不完善。本研究通过系统参数优化,建立了针对此类结构的高质量加工工艺方案。通过正交试验系统分析进给量f、切削线速度vc和切削深度am等参数的耦合作用机制。研究表明,切削深度对粗加工效率与变形控制具有决定性影响(极差分别为20.0和0.39),而进给量成为精加工表面粗糙度的主导因素(极差为0.48)。通过创新采用“从齿面两侧向中间切削”路径,有效解决了排屑不畅与扎刀问题。最终优化工艺使粗加工效率提升26.7%,精加工表面粗糙度降低37.1%。本研究为隐藏腔类复杂构件提供了可靠的工艺解决方案,对航空航天精密制造领域具有重要的工程应用价值。

     

    Abstract: As a critical sealing component in aero-engines, the labyrinth ring made of high-temperature alloy and featuring a hidden-cavity structure presents common challenges in CNC machining, such as difficult chip evacuation and tool chipping. Existing research focuses mainly on conventional configurations, leaving machining strategies for deep-cavity, low-inclination-angle features insufficiently developed. In this study, a high-quality machining solution for such structures was established through systematic parameter optimization. Orthogonal experiments were conducted to analyze the coupled effects of feed rate f, cutting speed vc, and cutting depth am. Results demonstrate that cutting depth exerts a decisive influence on roughing efficiency and deformation control, with ranges of 20.0 and 0.39, respectively, whereas feed rate dominates the surface roughness in finishing, with a range of 0.48. By innovatively implementing a "cutting from both tooth sides toward the center" strategy, issues related to chip accumulation and tool jamming were effectively mitigated. The optimized process improves roughing efficiency by 26.7% and reduces finishing surface roughness by 37.1%. This study provides a reliable machining solution for hidden-cavity complex components and demonstrates significant engineering applicability in aerospace precision manufacturing.

     

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