The bolted joint structure is one of the most prevalent forms of connection in
mechanical systems, and is instrumental in the assembly of such systems
due to its advantages of straightforward disassembly and assembly. This
paper proposes an inverse identification method for the material parameters
of the virtual layer of the joint interface, taking into account the range of
bolt preload force. The Sumali-like bolted joint model is the focus of this
research, and the virtual material layer method is employed to model the joint
interface with equivalent chemical parameters. Initially, a comparison is
made between the experimental and computational modal analysis results.
Subsequently, the establishment of a parametric model, the introduction of an
objective function, and the execution of multi-objective genetic algorithm-based
optimization follows. Finally, the virtual material parameters are solved so as to
complete the correction of the simulation parameters of the specimen material.
The effects of different preload forces on the virtual material parameters
are also discussed. The outcomes demonstrate that the total error of the
secondary identification is 7.48%, which is reduced by approximately 59.3% in
comparison with the inverse identification. This substantial improvement
in accuracy serves to verify the correctness and feasibility of the proposed
method.
Keywords
virtual material, range of application of pre-tightening
torque, joint surface, reverse parameter identification,
multi-objective genetic algorithm
School of Mechatronics
Engineering
Shenyang Aerospace University
Shenyang, 110136
China
Key Laboratory of Rapid Development
and Manufacturing Technology for Aircraft (Shenyang Aerospace
University)
Ministry of Education
Shenyang 110136
China
School of Mechatronics
Engineering
Shenyang Aerospace University
Shenyang, 110136
China
Key Laboratory of Rapid Development
and Manufacturing Technology for Aircraft (Shenyang Aerospace
University)
Ministry of Education
Shenyang 110136
China
School of Mechatronics
Engineering
Shenyang Aerospace University
Shenyang, 110136
China
Key Laboratory of Rapid Development
and Manufacturing Technology for Aircraft (Shenyang Aerospace
University)
Ministry of Education
Shenyang 110136
China