新型飞机用铝合金薄壁件的选区激光熔化成形研究

赵鑫; 虞雨洭; 吴圣川; 齐世文; 李飞; 李光俊

doi:10.7512/j.issn.1001-2303.2021.03.01

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新型飞机用铝合金薄壁件的选区激光熔化成形研究
Selective laser melted aluminum alloy thin-walled parts of new generation aircraft structures
2021年51卷第3期页码：1-7
纸质出版：2021
DOI： 10.7512/j.issn.1001-2303.2021.03.01
稿件说明：

移动端阅览

赵鑫, 虞雨洭, 吴圣川, 等. 新型飞机用铝合金薄壁件的选区激光熔化成形研究[J]. 电焊机, 2021,51(3):1-7. DOI： 10.7512/j.issn.1001-2303.2021.03.01.

ZHAO Xin, YU Yukuang, WU Shengchuan, et al. Selective laser melted aluminum alloy thin-walled parts of new generation aircraft structures[J]. Eletric Welding Machine2021, 51(3): 1-7. DOI： 10.7512/j.issn.1001-2303.2021.03.01.

摘要

高效率、短流程、一体化成形复杂金属件对新型飞机结构优化、成本降低具有重要意义。针对飞机用复杂薄壁零件开展选区激光熔化(Selective Laser Melting

SLM)成形AlSi10Mg合金设计优化和工艺研究

讨论了激光功率、扫描间距、保护气氛和热处理温度对成形质量的影响。结果表明

在较优工艺参数下

SLM成形AlSi10Mg合金组织致密

孔洞少

沉积态室温拉伸性能相较于铸件有明显提高;零件内部与表面质量良好

热处理后零件侧壁各方向尺寸与设计值正负偏差在0.2 mm以内

满足新型飞机复杂零件装配设计要求。

Abstract

High efficiency

short process and integrated forming of complex precision metallic parts are of great significance to the structural optimization and cost reduction of advanced aircrafts. In this work

the structural design optimization and processing adaptability of AlSi10Mg alloy thin-walled metallic components for new aircrafts were performed using selective laser melting（SLM）. The influence of laser power

hatch spacing

shielding gas and heat treatment on the manufacturing quality was discussed in details. The results show that under a set of optimized processing parameters

AlSi10Mg alloy formed by SLM shows a dense structure and fewer pores

and its deposited tensile properties at room temperature are superior to those of castings. The internal and surface qualities of the obtained parts are also good

and the geometry accuracy of the side walls after heat treatment is within 0.2 mm

which meets the assembly design requirements of complex new aircraft parts.