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Key Deviation Source Diagnosis for Aircraft Structural Component Assembly Driven by Small Sample Inspection Data

ZHU Yongguo1;DENG Bin1;HUO Zhengshu1; ZHOU Jiehua2   

  1. 1. School of Aeronautical Manufacturing Engineering, Nanchang Hangkong University, Nanchang,330063
    2. School of Information Engineering, Nanchang Hangkong University, Nanchang,330063
  • Online:2019-11-25 Published:2019-11-26

小样本检测数据驱动的飞机结构件装配关键偏差源诊断

朱永国1;邓斌1;霍正书1;周结华2   

  1. 1.南昌航空大学航空制造工程学院,南昌,330063
    2.南昌航空大学信息工程学院,南昌,330063
  • 基金资助:
    国家自然科学基金资助项目(51565042,51865037);
    江西省重点研发计划资助项目(20171BBE50007);
    江西省自然科学基金资助项目(20181BAB206029);
    江西省教育厅基金资助项目(GJJ180532)

Abstract: There were many transitive relationships among aircraft structural component assembly quality and the deviation sources such as nonlinearity, multilevel strong coupling and large uncertainty, which could not be directly built to identify the key deviation sources using the equation of assembly dimension chain. Thus, the measurement information theory was introduced, and a key deviation source diagnosis was presented for aircraft structural component assembly driven by small sample inspection data based on the integrated use of the entropy weight method and the synthetic grey correlation. Firstly, the potential informations were mined from assembly quality inspection data and entropy method was used to measure assembly quality attribute differences. Secondly, the correlation between each deviation source and the assembly quality was quantized by the synthetic grey correlation. Thirdly, the synthetic grey correlation between each deviation sources and assembly quality was modified by the weight of assembly quality attribute. Finally, according to the modified correlation, each deviation source was sorted to determine the key deviation source which affected assembly quality quantitatively. The case of assembly application verifies the accuracy and computational feasibility of the key deviation source diagnosis method based on entropy method and synthetic grey correlation.

Key words: aircraft, assembly, deviation source, small sample, entropy weight, synthetic grey correlation

摘要: 飞机结构件的装配质量与其偏差源之间呈现非线性、多层级强耦合、不确定度大的传递关系,不能通过构建装配尺寸链方程的方法诊断出影响装配质量的关键偏差源,为此,以装配偏差实测数据为基础,引入测量信息论,将熵权法和灰色综合关联度进行融合,提出小样本数据驱动的影响结构件装配质量的关键偏差源诊断方法。挖掘结构件装配质量检测数据的潜在信息,利用熵权法对结构件装配质量属性进行差异化度量;利用灰色综合关联度量化结构件各偏差源与结构件装配质量之间的关联度;利用装配质量属性权重对各偏差源与装配质量之间的灰色综合关联度进行修正;最后,按照修正后的关联度对各偏差源的重要程度进行排序,量化确定影响结构件装配质量的关键偏差源。装配应用案例证明了基于熵权法和灰色综合关联度的装配质量关键偏差源诊断方法的准确性和计算可行性。

关键词: 飞机, 装配, 偏差源, 小样本, 熵权, 灰色综合关联度

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