耦合几何与材料误差的柔性装配偏差统计分析

doi:10.7527/S1000-6893.2014.0306

Abstract

Abstract:

Compliant part is widely used in aircraft structure. Its deformation subjected to assembly forces is an important issue in assembly dimensional management for aircraft. To compensate for the deficiencies of assembly variation model concerning merely geometrical error of part, a method of statistical variation analysis for compliant assembly coupling the geometrical and material error (SVA_G&M) is proposed based on the first-order perturbation theory and the finite element method. In the SVA_G&M method, the method of influence coefficients is adopted to deduce the assembly variation regarding the source errors of part geometrical shape, material elastic modulus and Poisson's ratio, and the mean and standard deviation equations of assembly variation are formulated. Two experiments, simple sheet metals assembly and leading edge assembly of aircraft horizontal tail, are illustrated to verify the proposed method, and it is compared to the assembly process simulation of ANSYS finite element method (FEM). The result shows that the mean and standard by the SVA_G&M method has a good agreement with the FEM simulation. Meanwhile, the computing time is 30 s and 250 min respectively, which indicates that the SVA_G&M method is much more efficient than the FEM simulation. The experiments also show that material error has a considerable effect on assembly variation, in which elastic modulus plays a more important role than Poisson's ratio. Compared to assembly variation model concerning merely geometrical error, the SVA_G&M method can make more accurate and practical variation prediction of compliant assembly.

Key words: compliant assembly, material parameter, assembly variation, statistical analysis, finite element method

CLC Number:

V262.4
TH391

CHEN Hui, TAN Changbai, WANG Zhiguo. Statistical variation analysis of compliant assembly coupling geometrical and material error[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(9): 3176-3186.

References

[1] Liu S C, Hu S J, Woo T C. Tolerance analysis for sheet metal assemblies[J]. Journal of Mechanical Design, 1996, 118(1): 62-76.
[2] Hu S J, Koren Y. Stream-of-variation theory for automotive body assembly[J]. CIRP Annals-Manufacturing Technology, 1997, 46(1): 1-6.
[3] Liu S C, Hu S J. Variation simulation for deformable sheet metal assemblies using finite element methods[J]. Journal of Manufacturing Science and Engineering, 1997, 119(3): 368-374.
[4] Merkley K G, Chase K W, Perry E. An introduction to tolerance analysis of flexible systems[C]//MSC World Users' Conference. Newport Beach, CA: MSC Software Corp, 1996.
[5] Merkley K G. Tolerance analysis of compliant assemblies[D]. Provo: Brigham Young University, 1998.
[6] Bihlmaier B F. Tolerance analysis of flexible assemblies using finite element and spectral analysis[D]. Provo: Brigham Young University, 1999.
[7] Tonks M R, Chase K W. Covariance modeling method for use in compliant assembly tolerance analysis[C]//Proceedings of ASME Design Engineering Technical Conference. Salt Lake City: ASME, 2004: 1-7.
[8] Tonks M R, Chase K W, Smith C C. Predicting deformation of compliant assemblies using covariant statistical tolerance analysis[J]. Models for Computer Aided Tolerancing in Design and Manufacturing, 2007: 321-330.
[9] Mortensen A J. An integrated methodology for statistical tolerance analysis of flexible assemblies[D]. Provo: Brigham Young University, 2000.
[10] Stewart M L. Variation simulation of fixtured assembly processes for compliant structures using piecewise-linear analysis[D]. Provo: Brigham Young University, 2004.
[11] Xing Y F, Zhao X Y, Wu W W. Assembly variation analysis model based on fixture configurations for sheet metal parts[J]. Computer Integrated Manufacturing Systems, 2010, 16(2): 280-286 (in Chinese). 邢彦锋, 赵晓昱, 吴伟蔚. 基于夹具配置的薄板件装配偏差分析模型[J]. 计算机集成制造系统, 2010, 16(2): 280-286.
[12] Cheng H, Li Y, Zhang K F, et al. Efficient method of positioning error analysis for aeronautical thin-walled structures multi-state riveting[J]. The International Journal of Advanced Manufacturing Technology, 2011, 55: 217-233.
[13] Chen Z H, Du F Z, Tang X Q. Research on uncertainty in measurement assisted alignment in aircraft assembly[J]. Chinese Journal of Aeronautics, 2013, 26(6): 1568-1576.
[14] Tian W, Zhou W X, Zhou W, et al. Auto-normalization algorithm for robotic precision drilling system in aircraft component assembly[J]. Chinese Journal of Aeronautics, 2013, 26(2): 495-500.
[15] Chen Z H, Du F Z, Tang X Q. Key measurement characteristics based inspection data modeling for aircraft assembly[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(11): 2143-2152 (in Chinese). 陈哲涵, 杜福洲, 唐晓青. 基于关键测量特性的飞机装配检测数据建模研究[J]. 航空学报, 2012, 33(11): 2143-2152.
[16] Ni J, Tang W C, Xing Y. Three-dimensional precision analysis with rigid and compliant motions for sheet metal assembly[J]. The International Journal of Advanced Manufacturing Technology, 2014, 73(5-8): 805-819.
[17] Lin J, Jin S, Zheng C, et al. Compliant assembly variation analysis of aeronautical panels using unified substructures with consideration of identical parts[J]. Computer-Aided Design, 2014, 57: 29-40.
[18] Yu K G, Yang Z H. Tolerance design of automotive body sheet metal parts based on a compliant assembly variation model[J]. Journal of Shandong University: Engineering Science, 2014, 44(3): 69-74 (in Chinese). 于奎刚, 杨志宏. 基于柔性装配偏差模型的汽车车身薄板零件公差设计[J]. 山东大学学报: 工学版, 2014, 44(3): 69-74.
[19] Yu K G, Jin S, Lai X M, et al. Modeling and analysis of compliant sheet metal assembly variation[J]. Assembly Automation, 2008, 28(3): 225-234.
[20] Wang S F, Zhao H L. Reliablity analysis of railway vehicle structure based on stochastic finite element[J]. Journal of Tongji University: Natural Science, 2010, 38(11): 1631-1634 (in Chinese). 王社峰, 赵洪伦. 基于随机有限元的车辆结构可靠度分析研究[J]. 同济大学学报: 自然科学版, 2010, 38(11): 1631-1634.
[21] Chen Q, Liu X B. Stochastic finite element method and its engineering application[M]. Chengdu: Southwest Jiaotong University Press, 1993: 79-104 (in Chinese). 陈虬, 刘先斌. 随机有限元法及其工程应用[M]. 成都: 西南交通大学出版社, 1993: 79-104.

Statistical variation analysis of compliant assembly coupling geometrical and material error

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