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Project graduation (2). Effect of Thermo-Mechanical Treatment (TMT) on Hardness and Mechanical Properties for Heat-Treated Al-Mg-Si (6082) and Al-Cu-Li- Zr (8090) alloys: Experimental Correlation Using (DOE) Method using Minitab Software. By: Abdullah alshehri Yousif albalawy
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Project graduation (2) Effect of Thermo-Mechanical Treatment (TMT) on Hardness and Mechanical Properties for Heat-Treated Al-Mg-Si (6082) and Al-Cu-Li-Zr (8090) alloys: Experimental Correlation Using (DOE) Method using Minitab Software By: Abdullah alshehri Yousifalbalawy Ali alshahrani Supervisor: Dr. Saleh A. Al Kahtani Dr. MahmoudM.Tash College of Engineering
Introduction Thermomechanical treatment is one such combination of heat treatment and mechanical working, which yield high strength materials, an improvement in fatigue, creep, corrosion resistance and fracture toughness coupled with good formability. TMT is applicable to both ferrous and non-ferrous materials. For non-ferrous alloys, TMT is commonly applied to the age harden able alloys. The process consists of plastic deformation of alloys followed by aging treatment. This is in contrast to TMT of steels, which entails plastic deformation with simultaneous phase transformation. Different types of steels (carbon steels and low alloy steel, low and medium alloy high strength steels, mar aging steels, tool steels and high-speed steels) have been successfully subjected to thermomechanical treatments. Greater mechanical strength and an increase in toughness as well as dimensional stability are obtained with such treatment.
The objective -The effect of heat- treatment (TMT) on the aging and mechanical behavior of Al-Cu-Mg-Li-Zr and Al-Mg-Si alloys (8090 and 6082) are investigated i.e. the combined effect of cold work and aging parameters on the hardness of heat-treated 6082 and 8090 alloys are analysed. -Correlation between metallurgical parameters, hardness and mechanical properties of Al-Cu-Mg-Li-Zr and Al-Mg-Si alloys (8090 and 6082) using Mintab software are investigated. -Correlation between the hardness results and the different metallurgical factors for these alloys at both quantitative and qualitative are analyzed.
CONCLUSIONS • 1-Aging carried out for the Al-Cu-Mg-Li-Zr alloy under investigation, revealed that at 170C with intermediate cold work of 50% reduction yields peak hardness at 10 hours. • 2- Aging carried out for the Al-Cu-Mg-Li-Zr alloy under investigation, revealed that at 385C with intermediate cold work of 27-50% reduction yields peak hardness at (15-20 minutes). This could be attributed to bands of • fine precipitates, which appear in those specimens. • 3-Optimum mechanical properties (strength and ductility) can be attained for LTMT specimens aged at 170C for 10 hours with cold work of 50% reduction. This could be attributed to the recovery and recrystallization effects