Volume 47 Issue 11
Nov.  2021
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SHAN Meijuan, ZHAO Libin. Reliability-based design optimization method of CFRP bolted joints[J]. Journal of Beijing University of Aeronautics and Astronautics, 2021, 47(11): 2249-2255. doi: 10.13700/j.bh.1001-5965.2020.0425(in Chinese)
Citation: SHAN Meijuan, ZHAO Libin. Reliability-based design optimization method of CFRP bolted joints[J]. Journal of Beijing University of Aeronautics and Astronautics, 2021, 47(11): 2249-2255. doi: 10.13700/j.bh.1001-5965.2020.0425(in Chinese)

Reliability-based design optimization method of CFRP bolted joints

doi: 10.13700/j.bh.1001-5965.2020.0425
Funds:

National Natural Science Foundation of China 11772028

China Postdoctoral Science Foundation 2020M680325

More Information
  • Corresponding author: ZHAO Libin, E-mail: lbzhao@buaa.edu.cn
  • Received Date: 12 Aug 2020
  • Accepted Date: 20 Nov 2020
  • Publish Date: 20 Nov 2021
  • Bolted joints are the weak points of composite structures. Therefore, the design of bolted joints is one of crucial issues in the design of composite structure. In this paper, a probability analysis model for the failure load of a Carbon Fiber Reinforced Polymer (CFRP) composite bolted joint was built by combining the modified characteristic curve method and the statistical model of random parameters. The key influence parameters were regarded as the design variables, the reliability index was considered as the constraint, and the mass of the joint was the design goal. Accordingly, a reliability-based design optimization method was developed for the CFRP bolted joint. The orthogonal test design method was used to establish the reliability-based optimal design calculation scheme. The optimization results show that, when the key influence parameters XC is 2 450 MPa, tply is 0.174 mm, and E11 is 225 GPa, the best design of the joint is obtained. According to this scheme, when the external load is 17.5 kN, the reliability of the joint is increased from 0.998 to above 0.999 999, and the mass of the joint is reduced by 6.44%.

     

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