• CN:11-2187/TH
  • ISSN:0577-6686

机械工程学报 ›› 2026, Vol. 62 ›› Issue (4): 107-117.doi: 10.3901/JME.260136

• 材料科学与工程 • 上一篇    

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SiC铝合金复合材料梯度航天探测结构电弧增材制造

郑博1,2, 余圣甫1,2, 余振宇1,2, 孟筱灏1,2   

  1. 1. 华中科技大学材料科学与工程学院 武汉 430074;
    2. 华中科技大学材料成形与模具技术全国重点实验室 武汉 430074
  • 收稿日期:2025-02-19 修回日期:2025-08-09 发布日期:2026-04-02
  • 作者简介:郑博,男,1995年出生,博士研究生。主要研究方向为电弧增材制造。E-mail:D202080395@hust.edu.cn
    余圣甫(通信作者),男,1962年出生,博士,教授,博士研究生导师。主要研究方向为焊接、电弧增材制造。E-mail:yushengfu@hust.edu.cn
  • 基金资助:
    国家自然科学基金重大资助项目(51790174)。

Study on Wire Arc Additive Manufacturing of SiC Aluminum Alloy Composite Gradient Space Exploration Structure

ZHENG Bo1,2, YU Shengfu1,2, YU Zhenyu1,2, MENG Xiaohao1,2   

  1. 1. School of Materials Science and Engineering, Huazhong University of Science and Technology, Wuhan 430074;
    2. State Key Laboratory of Materials Processing and Die and Molud Technology, Huazhong University of Science and Technology, Wuhan 430074
  • Received:2025-02-19 Revised:2025-08-09 Published:2026-04-02

摘要: 含SiC 2 wt.%以上铝合金材料梯度航天探测结构具有良好的抗变形能力,常用于制备高超声速飞行器导引头。研制具有良好工艺性能的含SiC铝合金粉芯丝材,分析铝合金材料梯度航天探测结构特点并进行了双丝电弧增材制造工艺研究。结果表明,开发的Al-Si-SiC合金体系粉芯丝材在双丝电弧增材制造过程中,对主丝电弧稳定性影响小,沉积金属具有较高的强度和高的弹性模量。分析了铝合金材料梯度航天探测结构特点,采用分区成形策略,旁轴送丝电弧增材制造构件成型精度控制方法,制备出了SiC质量分数从2%~4%材料梯度变化的铝合金梯度航天探测结构,结构件平均尺寸偏差为±1.16 mm,在5g加速度、10 min振动测试条件下未发生明显变形、开裂现象,抗振动变形能力强。研究结果可为制备高性能陶瓷相改性航天复杂铝合金构件提供理论依据和基本数据。

关键词: 碳化硅, 材料梯度结构, 双丝电弧增材制造, 铝合金

Abstract: The gradient space exploration structure containing SiC 2 wt.% or more has good deformation resistance and is often used to prepare hypersonic vehicle seeker. The fine core wire of aluminum alloy containing SiC with good technological properties was developed, the structure characteristics of aluminum alloy material gradient space probe were analyzed, and the double wire arc additive manufacturing technology was studied. The results show that the developed Al-Si-SiC alloy system has little influence on the stability of main wire arc in the process of double wire arc additive manufacturing, and the deposited metal has high strength and high elastic modulus. The aluminum alloy gradient space detection structure was analyzed, and the aluminum alloy gradient space detection structure with SiC gradient varying from 2 wt.%-4 wt.% was prepared by adopting the zonal forming strategy and the forming precision control method of the axial wire feeding arc additive manufacturing components. The average size deviation of the structural components was ±1.16 mm. Under a 5g acceleration and a 10 min vibration test, there was no significant deformation or cracking observed, demonstrating strong resistance to vibration-induced deformation. The research results provide theoretical basis and basic data for the preparation of high performance ceramic phase modified aerospace complex aluminum alloy components.

Key words: SiC, material gradient structure, double wire arc additive manufacturing, aluminium alloy

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