Makaruk A. A., Pashkov A. A., Samoylenko O. V. Determining the deviations in the form of parts of the load-bearing structure of aircraft with shotblast hardening by the method of final-element modeling. Modern technologies. System analysis. Modeling, 2018, Vol. 59, No. 3, pp. 23–29. DOI: 10.26731/1813-9108.2018.3(59).23-29.
10.26731/1813-9108.2018.3(59).23-29
While surface peen hardening the parts of load-bearing structures of aircraft made of aluminum alloys, undesirable deformations (deviations from flatness) often takes place. These deviations after peen hardening can be determined in two ways: using the existing production experience for hardening of similar parts or using constructively similar samples containing the basic patterns of arrangement of structural elements and manufactured from the material of the part or by modeling process hardening in modern CAE-systems. The first method, using constructively similar samples, is very time-consuming and expensive. That is why, using techniques of computer finite element modeling of peen hardening to determine these deviations seems to be promising. This article contains a description of the finite element modeling technique using the nonlinear finite element analysis system to determine the total flexural deformations of a part that occurs while surface peen hardening of aircraft parts made of aluminum alloys. Using finite element modelling method for the process of shot-hardening parts allows one to significantly reduce the costs associated with the manufacture of constructively similar samples in determining the predicted deformations of hardened parts.
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