采用透射电镜(TEM)和扫描电镜(SEM)分析了不同时效热处理制度下镍基GH99高温合金中γ'相的尺寸、形貌变化,采用维氏硬度计测试不同时效热处理制度下的合金硬度。结果表明:γ'相随着时效温度的升高和保温时间的延长而明显粗化,...采用透射电镜(TEM)和扫描电镜(SEM)分析了不同时效热处理制度下镍基GH99高温合金中γ'相的尺寸、形貌变化,采用维氏硬度计测试不同时效热处理制度下的合金硬度。结果表明:γ'相随着时效温度的升高和保温时间的延长而明显粗化,其粗化符合沉淀相粗化理论(LSW理论);随着γ'相的不断长大,部分γ'相的形貌由球形转变为立方形。经计算得到γ'相长大激活能约为248.8 k J/mol。此外发现硬度随γ'相尺寸的增大而逐渐增大,但当γ'相尺寸超过37.2 nm时,硬度随γ'相长大呈下降趋势,在750℃时得到合金的最大硬度为395.16 HV。展开更多
The effects of two-stage aging and retrogression and reaging heat treatment on the fracture toughness and stress corrosion cracking resistance of 7475 alloy were studied. The fracture toughness, conductivity and stren...The effects of two-stage aging and retrogression and reaging heat treatment on the fracture toughness and stress corrosion cracking resistance of 7475 alloy were studied. The fracture toughness, conductivity and strength of samples of nine groups under duplex aging conditions and three retrogression and reaging heat treatments were also measured. Incorporating the microstructure and property, we found that when the condition of the first order aging kept identical, the fracture toughness and stress corrosion cracking resistance increase with aging time and the second aging temperature. The optimal treatment conditions are （ 115℃×7h ＋ 185 ℃×13h） among all tested two-stage aging treatments. Although the 7475 alloy treated by RRA method shows the highest strength and its stress corrosion cracking resistance after twenty minutes retrogression can also reach the same level as those by the optimal treatment of （115℃×7h＋ 185℃×13h ）, the fracture toughness is even low.展开更多
文摘采用透射电镜(TEM)和扫描电镜(SEM)分析了不同时效热处理制度下镍基GH99高温合金中γ'相的尺寸、形貌变化,采用维氏硬度计测试不同时效热处理制度下的合金硬度。结果表明:γ'相随着时效温度的升高和保温时间的延长而明显粗化,其粗化符合沉淀相粗化理论(LSW理论);随着γ'相的不断长大,部分γ'相的形貌由球形转变为立方形。经计算得到γ'相长大激活能约为248.8 k J/mol。此外发现硬度随γ'相尺寸的增大而逐渐增大,但当γ'相尺寸超过37.2 nm时,硬度随γ'相长大呈下降趋势,在750℃时得到合金的最大硬度为395.16 HV。
文摘The effects of two-stage aging and retrogression and reaging heat treatment on the fracture toughness and stress corrosion cracking resistance of 7475 alloy were studied. The fracture toughness, conductivity and strength of samples of nine groups under duplex aging conditions and three retrogression and reaging heat treatments were also measured. Incorporating the microstructure and property, we found that when the condition of the first order aging kept identical, the fracture toughness and stress corrosion cracking resistance increase with aging time and the second aging temperature. The optimal treatment conditions are （ 115℃×7h ＋ 185 ℃×13h） among all tested two-stage aging treatments. Although the 7475 alloy treated by RRA method shows the highest strength and its stress corrosion cracking resistance after twenty minutes retrogression can also reach the same level as those by the optimal treatment of （115℃×7h＋ 185℃×13h ）, the fracture toughness is even low.
