大深径比管件反型腔孔径自适应标定方法

Adaptive calibration method for bore diameter measurement of reverse cavities in tubular components with large depth-to-diameter ratios

  • 摘要: 起落架、炮管等大长径比管件的型腔普遍具有多级变径阶梯孔等几何特征,针对现有测量方法因难以补偿轴线偏心与机械偏心导致孔径测量精度低的问题,提出一种自适应孔径标定方法。首先,分析测量误差来源;然后,研究不同孔径测量的偏心误差补偿算法,提出精密集成测量方案及自适应孔径标定方法;最后,研制起落架深孔反型腔多孔径集成自动测量设备。试验结果表明,在ϕ135~175 mm的孔径测量中,通过自适应孔径标定方法后平均绝对误差减小至0.017~0.020 mm,较未标定前的平均绝对误差减小了57.5%~66.4%。该方法实现了起落架深孔反型腔多级变径阶梯孔的精密测量,为起落架的精密制造和精度控制提供了有力技术支持。

     

    Abstract: The internal cavities of components with large length-to-diameter ratios, such as landing gear struts and gun barrels, commonly feature geometric characteristics like multi-stage stepped holes with variable diameters. To address the issue of low measurement accuracy in existing methods, which arises from difficulties in compensating for axis eccentricity and mechanical eccentricity, an adaptive bore diameter calibration method is proposed. Firstly, the sources of measurement errors were analyzed. Secondly, an eccentricity error compensation algorithm for measuring different diameters was investigated, and a precision integrated measurement scheme along with the adaptive bore diameter calibration method was proposed. Finally, an integrated automatic measurement device for multiple diameters in the deep-hole reverse cavity of landing gear struts was developed. Experimental results demonstrate that for diameter measurements within the range of ϕ135−175 mm, the mean absolute error is reduced to 0.017−0.020 mm after applying the adaptive calibration method, which represents a reduction of 57.5%−66.4% compared to the error before calibration. Precise measurement of multi-stage variable-diameter stepped holes in the deep-hole reverse cavity of landing gear struts is achieved, providing strong technical support for the precision manufacturing and accuracy control of landing gear.

     

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