2021
DOI: 10.21285/1814-3520-2021-1-8-16
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Methodology for calculating the technological parameters of preventive deformation of the hardened parts of the "wall" type

Abstract: The article aims to establish the effect of preventive deformation on the accuracy of aircraft parts made from the thermally hardened aluminium alloy 1933T2, after blasting hardening. Determination of the impact of preventive deformation was carried out by analysing structural parts of the "wall" type produced using various technological sequences. Sample 1 was produced using a standard manufacturing sequence: milling – blasting hardening – blasting correction. Sample 2 was produced as follows: milling – preve… Show more

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