Microstructure and Mechanical Properties of Powder Metallurgy Al–Mg–Li Alloys With Different Mg/Li Ratios
QI Miao1, CHEN Cunguang1, 2, SUN Chunfang1, 3, LI Xin1, YANG Fang1, 2, 4, LIU Qiyuan4, LIU Xinhua1, GUO Zhimeng1, 2
1. Institute for Advanced Materials and Technology, University of Science and Technology Beijing, Beijing 100083, China;
2. Shunde Innovation School, University of Science and Technology Beijing, Foshan 528399, China;
3. Beijing General Automotive Research Institute, Beijing 101300, China;
4. Wuxi Paike New Materials Technology Co., Ltd., Wuxi 214161, China)
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, a yield strength of 473 MPa, and an elongation of 4.5%.
祁妙,陈存广,孙春芳,李鑫,杨芳,刘其源,刘新华,郭志猛. 不同Mg/Li比对粉末冶金Al–Mg–Li合金显微组织及力学性能的影响[J]. 航空制造技术, 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.