Simulation of the automatic riveting process with the aircraft structures

The paper considers the process of forming high-resource rivet joints in the aircraft structures using the automatic riveting mode. It provides the main typical operations and principles of ensuring high quality of this process in accordance with technical requirements for a modern aircraft, and notes the advantages and disadvantages. Main stages of the technological process in assembling the aircraft fuselage panels are developed. Computer simulation of the rivet joint is performed in the MSC.Marc software.
EDN: BSQMIW, https://elibrary/bsqmiw

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