Open Access

Investigating the Fatigue Behaviour of TiO2 Nanoparticle Reinforced AA7071 Aluminium Alloy

K. Sabari, sabarik246@gmail.com
Department of Mechanical Engineering, Saveetha School of Engineering, Saveetha Institute of Medical and Technical Sciences, Chennai, TN, India
K. Ch. Sekhar, Department of Mechanical Engineering, Lendi Institute of Engineering and Technology, Jonnada, Vizianagaram, AP, India M. Thirunavukkarasu, Department of Automobile Engineering, Dr.Mahalingam College of Engineering and Technology, Coimbatore, TN, India DVSSSV Prasad, Department of Mechanical Engineering, Aditya College of Engineering (A), Surampalem, AP, India G. Rathinasabapathi, Department of Mechanical Engineering, Panimalar Engineering College, Chennai, TN, India Nageswara Rao Medikondu Department of Mechanical Engineering, Koneru Lakshmaiah Education Foundation, Vaddeswaram, AP, India


J. Environ. Nanotechnol., Volume 13, No 2 (2024) pp. 127-134

https://doi.org/10.13074/jent.2024.06.242635

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Abstract

Aluminium metal matrix nanocomposites have become a major focus in the industry as they possess exceptional strength and ductility. The experiment included incorporating TiO2 nanoparticles into the AA7071 alloy at a volume ratio of 5 wt. % using the stir casting technique. The matrix was infused with TiO2 nanoparticles, which had an average particle size of 30 ± 5 nm, using a powder injection method. A study was carried out to assess the influence of different levels of TiO2 on the durability of the material, both before and after undergoing heat treatment. The results indicated that the fatigue properties of AA7071 were enhanced after heat treatment when TiO2 nanoparticles were incorporated. After undergoing heat treatment, a 5 wt. % TiO2 addition resulted in a significant improvement in fatigue properties, leading to a noteworthy 14.71% increase in fatigue life when compared to the base sample. The observed improvement may be ascribed to the larger quantity of finely dispersed precipitates that are evenly distributed after the heat treatment procedure. The fatigue strength of the matrix in composite materials showed a discrepancy of just 4% between the experimental and numerical values. Furthermore, the research found that the absence or decrease in the size of the area without precipitates inside the space between dendrites happened after the aging process. Nevertheless, despite the inclusion of 5 weight percent of titanium and the use of heat treatment, the creation of Al2CuMg precipitates remained unachievable. However, the formation of the Al3TiCu and Al7TiCu phases occurred.

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