Estudo da influência da topologia dos furos na taxa de propagação de trincas
Keywords:
holes, cracks, loading, fracture toughnessAbstract
The drilling process for bolted or riveted joints of components is very common in the naval, aeronautical, mechanical and civil industries. In this context, the present work aims to study, through computer simulation, the influence of hole geometry (through, chamfered and rounded) on crack propagation when submitted to static and dynamic loads. For the static crack evaluation, failure was considered when the stress intensity factor (FIT) exceeds the fracture toughness of the material (KIc). In the case of fatigue, the condition of small crack tip plastification zone and the Paris Law were considered for determining region II of the dadN x DeltaK curve. Initially, a parametric analysis of the hole geometry was performed to obtain a topology that would result in less discontinuity of the stress field and consequently less influence on static crack growth. The best performing topology was then used to study the fatigue crack growth rate considering the Paris Law. The numerical tests were performed on a 7075-T6 aluminum specimen resulting in dadN x DeltaK curves with good agreement with the literature.
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Gaspari , R.S.; Reis,E. ; Chaves , R.S ; Técnicas Para Identificação Do Estágio Inicial e/Ou Acompanhamento de Trinca Ocasionada Por Fadiga Mecânica. Anais Do IX Congresso Nacional de Engenharia Mecânica, no. March 2018.
Fuchs, H.O.; Stephens, R.I.; Saunders H.; Metal Fatigue in Engineering. Journal of Engineering Materials and Technology.1980, Volume 103.
Zhao, T.; Yanyao, J.; Fatigue of 7075-T651 Aluminum Alloy. International Journal of Fatigue 2008, Volume 30.
Moreno, J.R.S; Ribeiro, C.; Junior, E.M; Computational Study of Fatigue Fracture in Rivet Housing of an Aeronautical Aluminum Alloy 7075-T6. International Journal of Advanced Engineering Research and Science 2018, Volume 5.
Reifsnider, K.L.; Fazzino, P.; Majumdar, P.K.; Xing, L.; Material State Changes as a Basis for Prognosis in Aeronautical Structures. Aeronautical Journal 2009, Volume 113.
Martinetti, A.M.D.; Singh, S.; Applications and Challenges of Maintenance and Safety Engineering in Industry 2020.
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