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基于数字孪生的航空发动机配合界面装配分析

李瑾岳,张鹏飞,徐茂程,赵罡   

  1. 北京航空航天大学
  • 收稿日期:2023-10-31 修回日期:2024-02-14 出版日期:2024-04-19 发布日期:2024-04-19
  • 通讯作者: 张鹏飞

Assembly analysis of aero-engine mating interface based on Digital Twin

  • Received:2023-10-31 Revised:2024-02-14 Online:2024-04-19 Published:2024-04-19
  • Contact: Peng-Fei Zhang

摘要: 随着航空发动机零部件加工精度和质量稳定性的提升,装配精度逐渐成为影响产品精度的关键因素。目前已有基于数学模型的装配误差分析方法,能够实现配合界面形位偏差对产品最终装配偏差影响的预测。然而,这些方法受到建模方法的限制,对配合界面的几何物理信息进行了简化拟合。虽然能够增加计算分析的便捷性,但是也导致其无法足够准确的表征表面形貌偏差特征,进而导致无法准确分析其对装配的影响。特别是面向航空发动机等精密机械产品,装配配合界面形貌的微小几何偏差会在大载荷条件下对产品质量和稳定性产生重要影响。因此,本文提出了一种基于数字孪生技术的装配偏差分析方法。该方法以数字孪生技术为框架,使用肤面模型作为特征表面的建模方法,结合实测数据驱动的多因素计算机仿真模型,实现装配界面变动对装配精度影响的综合分析。开发了发动机装配界面试验件,并通过对比试验和模拟结果,验证所提出数字孪生方法的有效性。

关键词: 航空发动机, 配合界面, 数字孪生, 装配分析, 形貌测量, 数字化仿真

Abstract: With the improvement of machining accuracy and quality stability of aero-engine parts, assembly accuracy has gradually become the critical factor affecting product accuracy. In order to predict the influence of the form and posi-tion deviation of the mating surface on the final assembly deviation of the product, a large number of assembly error analysis methods based on mathematical models have been developed. However, most of the existing methods have greatly simplified the geometrical and physical information of the mating interface due to the limitation of the modeling method, although the convenience of calculation and analysis can be increased, these methods are not able to accurately characterize the deviation of the surface morphology and analyze its influence on the assembly. Especially for precision mechanical products such as aero-engines, small deviations can have an important impact on product quality and stability under large load conditions. Therefore, an assembly deviation analysis method based on Digital Twin technology is proposed in this paper. This solution uses the Digital Twin technology as the framework, uses the Skin Model Shapes as the modeling method of the feature surface, and combines the data-driven multi-factor computer simulation model to realize the comprehensive analysis of influence of the assembly mating surface deviation on the assembly accuracy. An engine assembly interface test workpieces are made, and the effectiveness of the proposed Digital Twin method is verified by comparing the experiment and simulation re-sults.

Key words: Aero-engine, Maing interface, Digital Twin, Assembly analysis, Surface Measurement, Digital simulation

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