QI Miao, CHEN Cunguang, SUN Chunfang, LI Xin, YANG Fang, LIU Qiyuan, LIU Xinhua, GUO Zhimeng. Microstructure and Mechanical Properties of Powder Metallurgy Al–Mg–Li Alloys With Different Mg/Li Ratios[J]. Aeronautical Manufacturing Technology, 2024, 67(17): 59-67.
QI Miao, CHEN Cunguang, SUN Chunfang, LI Xin, YANG Fang, LIU Qiyuan, LIU Xinhua, GUO Zhimeng. Microstructure and Mechanical Properties of Powder Metallurgy Al–Mg–Li Alloys With Different Mg/Li Ratios[J]. Aeronautical Manufacturing Technology, 2024, 67(17): 59-67. DOI: 10.16080/j.issn1671-833x.2024.17.059.
Microstructure and Mechanical Properties of Powder Metallurgy Al–Mg–Li Alloys With Different Mg/Li Ratios
Al–Mg–Li alloy was prepared using powder metallurgy and hot extrusion methods. The microstructure
fracture morphology and mechanical properties of the alloy were analyzed using metallographic microscopy
scanning electron microscopy
transmission electron microscopy
and a tensile testing machine. The effects of different Mg/Li ratios (1.3
1.8
2.5) on the microstructure and mechanical properties of the alloy in the sintered
extruded
and T6 heat-treated states were investigated. The results revealed that an increase in the Mg/Li ratio led to an increase in the relative density of the sintered alloy
indicating the promoting effect of Mg on the sintering process. For the extruded Al–Mg–Li alloy
as the Mg/Li ratio increased
the precipitation of Mg-containing phases gradually increased and clustered near the grain boundaries
resulting in improved mechanical properties
the tensile strength of which increased from 285 MPa to 407 MPa. After T6 heat treatment
the second phase in the Al–Mg–Li alloy mainly consisted of δ′ phase and T phase. The δ′ phase
as the main strengthening phase
was uniformly distributed in the aluminum matrix
while the T phase exhibited a chain-like distribution along the grain boundaries. Increasing the Mg/Li ratio enhanced the tensile strength and yield strength of the alloy
but it may lead to a decrease in elongation. For instance
the Al–5Mg–2Li alloy after T6 heat treatment exhibited a tensile strength of 532 MPa