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Shape-performance Integrated Design And Strengthening Mechanism Of Precipitation Strengthened FeNiCoCr-based High-entropy Alloys

Posted on:2024-08-30Degree:MasterType:Thesis
Country:ChinaCandidate:P J WangFull Text:PDF
GTID:2531307055987799Subject:Materials science
Abstract/Summary:PDF Full Text Request
The emergence of high-entropy alloys has greatly expanded the composition design space of metallic materials.By adjusting the composition and content of the main elements,alloy systems with various unique mechanical,physical,and chemical properties can be developed,providing more new options and ideas for breaking through the performance limit bottleneck of traditional structural materials.Fe Ni Co Cr HEAs are the most typical class of HEAs with excellent structural stability,mechanical properties,and corrosion resistance,but like other FCC structural alloys,Fe Ni Co Cr HEAs applications are limited by the low room temperature yield strength.Therefore,how to further improve the yield strength of Fe Ni Co Cr HEAs has become a hot topic of research.In this paper,Fe Ni Co Cr-based high entropy alloys were prepared by low-speed ball milling+hot pressing sintering method,and the effects of Si C,and Al/Ti dopants on the microstructure and properties were investigated respectively.The specific conclusions are as follows.The Fe Ni Co Cr high entropy alloys with different Si C content(0 wt%,2.5 wt%,5 wt%,and 7.5 wt%)were successfully prepared by the hot press sintering technique.The main matrix phase of the alloys is the FCC phase,and Si C reacted with Cr to form Cr7C3 secondary phase with an orthogonal crystal structure,and its content increased with increasing the Si C content.It is observed that the alloy with 7.5 wt%Si C content formed Si-rich amorphous Si O2 particles at the grain boundaries,while Ni-and Si-rich L12-structured Ni3Si nanoparticles are precipitated within the crystal.When the Si C content is less than 5 wt%,the yield strength of the HEA increased little,and the strengthening mechanism is mainly associated with the strengthening of Cr7C3 particles.With a further increase in the Si C content to 7.5 wt%,the HEAs show a yield strength of 891 MPa,respectively,which is 87.6%higher than that of the HEA without Si C.At the same time,the compressive strain still reaches 28%.Since the strengthening of Si O2 particles is predominant,the main strengthening mechanisms for the alloy are attributed to thermal mismatch and Orowan strengthening caused by the Si O2 particles at the grain boundaries.The(Fe Ni Co Cr)100-x-yAlxTiy high-entropy alloys were successfully prepared by the hot-pressure sintering technique.The matrix phases of these alloys are FCC structure,among which(Fe Ni Co Cr)93Al5Ti2,and(Fe Ni Co Cr)95Al5Ti5 alloys form nano-precipitation phase with L12-type inside the FCC matrix grains.The nanoparticles in(Fe Ni Co Cr)93Al5Ti2 alloy are irregularly rounded spheres with an average size of 8 nm and a volume ratio of 12%,and the nanoparticles in(Fe Ni Co Cr)95Al5Ti5 alloy are regular rounded squares with an average size of113 nm and a volume ratio of 48%.In addition,there are some minor phases:bulk Cr-richσphase and Fe-rich BCC structured phase in(Fe Ni Co Cr)93Al5Ti2 alloy;bulk Cr-richσphase and a small amount of fine(Ni,Al,Ti)-riched phase and Al-rich phase formed at grain boundaries in(Fe Ni Co Cr)90Al5Ti5 alloy;Cr-richσphase,Ni3Ti phase,and Ti-rich phase in(Fe Ni Co Cr)95Ti5 alloy.The(Fe Ni Co Cr)90Al5Ti5alloy has the highest true yield strength and ultimate true compressive strength of 948 MPa and1684 MPa,respectively,and maintains 46%of the true compressive strain.The high strength mainly originated from the high-density L12-type nanoprecipitation phases within the crystal.The(Fe Ni Co Cr)90Al5Ti5 alloy was quenched at 850°C and quenched at 1150°C,respectively.Both heat treatments significantly reduce the yield strength of the alloy,and the 1150℃quenching causes the largest reduction but significantly improves the plasticity of the alloy.Quenching at 850°C led to the growth of the intracrystalline nano-L12 precipitated phase into equiaxed grains with a size of more than 10 mm and the formation of a small amount of lamellar HCP structured phase.Quenching at 1150°C results in the complete dissolution of the intracrystalline nano-L12 precipitated phase.
Keywords/Search Tags:High-entropy alloy, Microstructure, Mechanical properties, Precipitation strengthening
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