Solid Mechanics and Vehicle Conceptual Design

Application of DFR Method to Optimal Fatigue Design of Structures

  • CHEN Binqi ,
  • ZENG Jianjiang ,
  • WANG Yiding ,
  • TONG Mingbo
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  • College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Received date: 2012-06-19

  Revised date: 2012-08-21

  Online published: 2012-09-18

Abstract

A new method to analyze fatigue reliability based on detail fatigue rating (DFR) is presented which integrates finite element analysis and fatigue analysis. Fatigue reliability calculating software (FEM-DFR) is written with the help of finite element analysis. The agreement between the simulation results calculated by FEM-DFR and the experimental data proves the effectiveness of the method. On this basis, a general platform which integrates Patran/Nastran, FEM-DFR and iSIGHT is developed to overcome the shortcomings of long time-consumption and low efficiency of structure fatigue optimization. A detailed bracket of an actuator cylinder is optimized on the platform. The results show that the platform is stable, data transmission is smooth, operational efficiency is high, and the optimized quality is good.

Cite this article

CHEN Binqi , ZENG Jianjiang , WANG Yiding , TONG Mingbo . Application of DFR Method to Optimal Fatigue Design of Structures[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013 , 34(5) : 1122 -1128 . DOI: 10.7527/S1000-6893.2013.0201

References

[1] Venter G, Haftka R T, Chirehdast M. Response surface approximations for fatigue life prediction. AIAA-1997-1331,1997.
[2] Shim H J, Kim J K. Consideration of fatigue life optimization of pulley in power-steering system. Materials Science and Engineering: A, 2008,483-484: 452-455.
[3] Tang Y C, Zhou X H, Chen J. Preform tool shape optimization and redesign based on neural network response surface methodology. Finite Elements in Analysis and Design, 2008, 44(8): 462-471.
[4] Xue C J, Tan W, Xu F J, et al. Structural fatigue life optimization method based on response surface model. Journal of Nanjing University of Science and Technology, 2011, 35(6): 843-846. (in Chinese) 薛彩军, 谭伟, 徐奋进, 等. 基于响应面模型的结构疲劳寿命优化方法. 南京理工大学学报, 2011, 35(6): 843-846.
[5] Zhang C C, Yao W X. Anti-fatigue optimal design based on response surface model. Journal of Nanjing University of Aeronautics & Astronautics, 2007, 39(1): 37-40. (in Chinese) 张成成, 姚卫星. 基于响应面的结构抗疲劳优化设计方法. 南京航空航天大学学报, 2007, 39(1): 37-40.
[6] Liu G L, Shen H J, Ren L. Response surface model applicable to the fatigue optimal design of structures. Mechanical Engineering & Automation, 2009, 10(5): 61-63. (in Chinese) 刘根林, 沈海军, 任亮. 响应面模型在结构疲劳优化设计中的应用. 机械工程与自动化, 2009, 10(5): 61-63.
[7] Mrzyglod M, Zielinski A P. Parametric structural optimization with respect to the multiaxial high-cycle fatigue criterion. Structural and Multidisciplinary Optimization, 2007, 33(2): 161-171.
[8] Liu Y S, Liu J, Shao X J, et al. Effect of roughness on fatigue life of open holes. Key Engineering Materials, 2007, 348-349: 757-760.
[9] Goranson U G. Fatigue issues in aircraft maintenance and repairs. International Journal of Fatigue, 1997, 19(93): 3-21.
[10] Mohaghegh M. Evolution of structures design philosophy and criteria. Journal of Aircraft, 2005, 42(4): 814-831.
[11] Liu Y S, Yuan X K, Liu J, et al. Research on structure detail fatigue rating DFR and testing method. Experimental Technology and Management, 2008, 25(1): 27-29. (in Chinese) 刘永寿, 袁修开, 刘军, 等. 结构细节疲劳额定值DFR及其试验方法的研究. 实验技术与管理, 2008, 25(1): 27-29.
[12] Dong Y M, Liu W T, Yang C. Military aircraft durability design method based on detail fatigue rating. Acta Aeronautica et Astronautica Sinica, 2010, 31(12): 2357-2364. (in Chinese) 董彦民, 刘文珽, 杨超. 军用飞机结构耐久性设计的细节疲劳额定值方法. 航空学报, 2010, 31(12): 2357-2364.
[13] Huang X, Liu J Z, Ma S J, et al. Sensitivity analysis of the parameters in detail fatigue rating equation. Acta Aeronautica et Astronautica Sinica, 2012, 33(5): 863-870. (in Chinese) 黄啸, 刘建中, 马少俊,等. 细节疲劳额定强度计算参量取值敏感性研究. 航空学报, 2012, 33(5): 863-870.
[14] Yuan H S, Xu Z N. Analysis of internal force for joints by PATRAN/NASTRAN software. Civil Aircraft Design & Research, 2003(2): 15-18. (in Chinese) 袁华生, 徐仲年. 使用PATRAN/NASTRAN软件进行连接件内力分析. 民用飞机设计与研究, 2003(2): 15-18.
[15] Zhang C C, Yao W X, Ye B. Equivalent stress severity factor approach for fatigue of multi-fastener plate. Acta Aeronautica et Astronautica Sinica, 2009, 30(2): 271-275. (in Chinese) 张成成, 姚卫星, 叶彬. 连接件疲劳寿命分析的等效SSF法. 航空学报, 2009, 30(2): 271-275.
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