| Al-Li alloys not only have low density,high ratio strength and low fatigue crack expansion rate,but also have good low-temperature mechanical property and processing performance.Due to their light weight and high strength,Al-Li alloys have become one of the most potential materials in aeronautics and aerospace field.Alloying and heat-treatment could improve the microstructure and mechanical property of Al-Li alloys.At the same time,due to the complexity of some service environments,the Al-Li alloy sometimes needs to serve in a wet or salty environment for a long time.The precipitates of Al-Li alloy not only has an significant impact on the mechanical property of Al-Li alloys,but also affects the corrosion resistance of Al-Li alloys.Therefore,in this thesis,the research has been conducted on precipitates evolution of the novel Al-Cu-Li-Mg-Ag-Mn alloys during homogenization treatment,the microstructure and corrosion resistance of the aged alloys.The main conclusions of this thesis are as follows:(1)There were Al2Cu Li phase,Al3Li phase and Al7Cu4Li phase in the homogenized Al-5Cu-1Li-0.6Mg-0.5Ag-0.5Mn alloys.Al7Cu4Li phase were dissolved with increase of homogenization temperature and holding time.Al2Cu phase and Al2Cu Li phase coarsened during the homogenization process.Moreover,it could be found that there was segregation of Ce and La elements at the Cu-rich precipitates,and the segregation could not be removed by homogenization treatment.(2)The homogenized Al-5Cu-1Li-0.6Mg-0.5Ag-0.5Mn alloy was subjected to a two-stage aging treatment.Peak-age Al-5Cu-1Li-0.6Mg-0.5Ag-0.5Mn alloy,which had gone through aging treatment at 120°C for 4 hours and 180°C for 6 hours,was mainly composed ofα-Al,Al2Cu Li,Al2Cu,Al3Li and Al20Cu2Mn3 precipitates,and needle-like Al2Cu Li,Al2Cu precipitates and dot-like Al3Li precipitates were tiny and scattered.(3)Tafel polarization of the peak-age Al-5Cu-1Li-0.6Mg-0.5Ag-0.5Mn alloys revealed the corrosion potential and corrosion current density to be-651m V and 5.861μA/cm2,respectively.The over-age alloy had more positive corrosion potential of-618 m V but presented higher corrosion current of16.368μA/cm2.It was found that the peak-age alloy has better corrosion resistance by comparing the corrosion surfaces of peak-age alloy and over-age alloy.(4)The homogenized Al-4.5Cu-1Li-0.4Mg-0.4Ag-0.4Mn-0.5Zn alloys were mainly composed of Al(α),Al2Cu Li,Al3Li and Al7Cu4Li precipitates.All precipitates coarsened with increase of homogenization temperature and holding time.Moreover,it was found that there was segregation of Zn elements at Cur-rich precipitates.(5)Peak-age Al-4.5Cu-1Li-0.4Mg-0.4Ag-0.4Mn-0.5Zn alloys was mainly composed by Al2Cu Li precipitates and Al20Cu2Mn3 precipitates.Comparing with the homogenized alloy,the needle-like Al2Cu Li precipitates were scattered and smaller.It was found that there were segregation of Zn and Mn at Cu-rich precipitates at Cu-rich precipitates.Al20Cu2Mn3 precipitates was small and dispersed,with an average size of approximately 100 nm.(6)For the aged Al-4.5Cu-1Li-0.4Mg-0.4Ag-0.4Mn-0.5Zn alloy,Tafel polarization testing of the peak-age alloy in a 3.5%Na Cl solution revealed the corrosion potential and corrosion current density to be-611 m V and 2.005μA/cm2,respectively.The over-age alloy had more negative corrosion potential of-653 m V.It was found that the peak-age alloy has better corrosion resistance by comparing the corrosion surfaces of peak-age alloy and over-age alloy.And alloying with Zn element could improve the corrosion resistance of the aged alloys. |