首页|电弧增材制造铝锂合金组织与性能研究

电弧增材制造铝锂合金组织与性能研究

扫码查看
铝锂合金是新一代航空航天用轻质合金材料.本文采用电弧增材制备了含Si铝锂合金试样,并对比了沉积态以及T6 态时含Si铝锂合金微观组织及力学性能.试验结果显示,单道薄壁沉积态含Si铝锂合金α-Al平均尺寸约21.2 μm,SEM及XRD结果显示微观组织中存在大量微米级共晶Si相以及含Cu、Li共晶相.T6态热处理后,粗大Al2Cu相及部分共晶硅组织逐渐回溶至基体中,增材试样硬度由 96HV提升至 138HV,相对提升 43.8%.T6 态试样在 0°、45°、90°方向上抗拉强度分别为 402 MPa、350 MPa、330 MPa,沉积态试样在 3 个方向的抗拉强度分别为160 MPa、134 MPa、142 MPa,T6态试样力学性能显著提升.
Research on Microstructure and Mechanical Properties of Wire Arc Additive Manufactured Aluminum-Lithium Alloy
Lithium aluminum(Al-Li)alloy is a new-generation lightweight alloy material used in aerospace applications.In this study,arc additive manufacturing was used to fabricate aluminum-lithium-silicon alloy.A comparison was made between the microstructure and mechanical properties of the alloy in the as-deposited sample and the T6 heat-treated sample.The experimental results show that the average size of the α-Al phase in the single-pass thin-walled deposited aluminum-lithium-silicon alloy was approximately 21.2 μm.SEM and XRD results revealed the presence of a large amount of micrometer-scale eutectic Si phase and eutectic phases containing Cu and Li in the microstructure.After T6 heat treatment,the coarse Al2Cu phase and some eutectic silicon structures gradually dissolved into the matrix.The hardness of the additive sample increased from 96HV to 138HV,representing a relative increase of 43.8%.The tensile strength in the 0°,45°,and 90° directions was 402 MPa,350 MPa,and 330 MPa,respectively.The as-deposited samples exhibited tensile strengths of 160 MPa,134 MPa,and 142 MPa in three directions,whereas the T6 heat-treated samples showed significantly improved mechanical properties.

Wire arc additive manufactureAl-Li alloysMicrostructureMechanical propertiesTensile strength

张睿泽、谢勇、罗志伟、严振宇、李瑞卿、蒋日鹏、李安庆

展开 >

首都航天机械有限公司,北京 100076

中南大学,长沙 410000

电弧增材制造 铝锂合金 微观组织 力学性能 抗拉强度

2024

航空制造技术
北京航空制造工程研究所

航空制造技术

CSTPCD北大核心
影响因子:0.403
ISSN:1671-833X
年,卷(期):2024.67(21)