1. 北京科技大学新材料技术研究院,北京,100083
2. 北京科技大学顺德创新学院,佛山,528399
3. 北京汽车研究总院,北京,101300
4. 无锡派克新材料科技股份有限公司,无锡,214161
纸质出版:2024
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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.
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. DOI: 10.16080/j.issn1671-833x.2024.17.059.
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.
采用粉末冶金工艺和热挤压方法制备了Al–Mg–Li合金,并通过金相显微镜、扫描电子显微镜、透射电子显微镜和拉伸试验机对合金的微观组织、断口形貌和力学性能进行了分析。研究了不同Mg/Li 比(1.3、1.8、2.5)对合金在烧结态、挤压态和T6热处理态下的微观组织和力学性能的影响。结果显示,随着Mg/Li比的增加,烧结态合金的相对密度增加,表明Mg元素对烧结过程具有促进作用。对于挤压态Al–Mg–Li合金,随着Mg/Li比的增加,合金中含Mg的析出相逐渐增多,并聚集在晶界附近,力学性能得到了很大提高,抗拉强度由285 MPa增加至407 MPa。经T6热处理后,Al–Mg–Li合金的第二相主要由δ′相和T相组成,其中δ′相是主要的强化相,均匀分布在铝基体中,而T 相在晶界处呈链状分布。研究表明,提高Mg/Li 比可以提高Al–Mg–Li合金的抗拉强度和屈服强度,但延伸率可能会有所下降。T6热处理后Al–5Mg–2Li合金可达到抗拉强度532 MPa、屈服强度473 MPa、延伸率4.5%。
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%.
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