计算机集成制造系统 ›› 2013, Vol. 19 ›› Issue (05 ): 1009-1014.

• 产品创新开发技术 • 上一篇    下一篇

基于关键特征的飞机大部件对接位姿调整技术

刘继红,庞英仲,邹成   

  1. 北京航空航天大学机械工程及自动化学院
  • 出版日期:2013-05-31 发布日期:2013-05-31
  • 基金资助:
    国家科技支撑计划资助项目(2011BAF13B11)。

Adjusting position-orientation of large components based on key features

  • Online:2013-05-31 Published:2013-05-31
  • Supported by:
    Project supported by the National Key Technology R&D Program,China (No.2011BAF13B11)

摘要: 为实现飞机大部件姿态的自动调整,必须先获得大部件的空间姿态表达,进而确定具有6个自由度的调整向量。为此,针对大部件外形面装配误差累积,采用以大部件外形面测量点作为对接基准点进行姿态拟合的传统对接方法难以获得正确对接位置的问题,提出基于关键特征的大部件对接位姿调整方法。该方法首先确定对接大部件的关键特征,获得大部件的对接向量,然后通过优化协调尺寸误差分配建立满足装配质量要求的最优对接矩阵,确定对接过程中的大部件位姿,以提高对接精度与效率。通过在飞机平垂尾对接中的运用,并与一般位姿计算方法比较,验证了该方法的有效性。

关键词: 飞机装配, 关键特征, 误差分配, 自动对接

Abstract: To realize automatic adjustment of large aircraft components,the postures of large components were expressed and the adjustment vectors with six degrees of freedom were determined.For the assembly variation accumulation on the surface of large components,it was difficult to obtain the correct assembly vector with the traditional method,which took the measured points on the surface of large components as assembly reference points to calculate large components'postures.A new method based on key features of large components was proposed.The key characteristics of large component were identified and the assembly vector was obtained.By optimizing the tolerance distribution,the optimal assembly matrix satisfying assembly quality requirements was established.This method defined component postures accurately and improved the assembly quality and efficiency.Through the application of assembling horizontal stabilizer and vertical stabilizer,and comparison with the conventional posture adjusting method,the validity of the method was verified.

Key words: aircraft assembly, key characteristic, tolerance distribution, automatic assembly

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