李楠,王强,牛文娟,郭楠,葛书恺,黄亮亮,王金,李申奥,韩鹏.超音速激光沉积硬质铝合金的疲劳性能研究[J].表面技术,2024,53(13):55-63.
LI Nan,WANG Qiang,NIU Wenjuan,GUO Nan,GE Shukai,HUANG Liangliang,WANG Jin,LI Shen'ao,HAN Peng.Fatigue Properties of Hard Al Alloy Fabricated by Supersonic Laser Deposition[J].Surface Technology,2024,53(13):55-63
超音速激光沉积硬质铝合金的疲劳性能研究
Fatigue Properties of Hard Al Alloy Fabricated by Supersonic Laser Deposition
投稿时间:2024-04-30  修订日期:2024-06-24
DOI:10.16490/j.cnki.issn.1001-3660.2024.13.006
中文关键词:  冷喷涂  超音速激光沉积  涂层  修复  疲劳
英文关键词:cold spraying  supersonic laser deposition  coating  repair  fatigue
基金项目:陕西省重点研发计划项目(2023GXLH-050)
作者单位
李楠 西安建筑科技大学 冶金工程学院,西安 710055;陕西省冶金工程技术研究中心,西安 710055 
王强 西安建筑科技大学 冶金工程学院,西安 710055;陕西省冶金工程技术研究中心,西安 710055 
牛文娟 西安建筑科技大学 冶金工程学院,西安 710055;陕西省冶金工程技术研究中心,西安 710055 
郭楠 西安建筑科技大学 冶金工程学院,西安 710055;陕西省冶金工程技术研究中心,西安 710055 
葛书恺 西安建筑科技大学 冶金工程学院,西安 710055;陕西省冶金工程技术研究中心,西安 710055 
黄亮亮 西安建筑科技大学 冶金工程学院,西安 710055;陕西省冶金工程技术研究中心,西安 710055 
王金 西安建筑科技大学 冶金工程学院,西安 710055;陕西省冶金工程技术研究中心,西安 710055 
李申奥 西安建筑科技大学 冶金工程学院,西安 710055;陕西省冶金工程技术研究中心,西安 710055 
韩鹏 西安建筑科技大学 冶金工程学院,西安 710055;陕西省冶金工程技术研究中心,西安 710055 
AuthorInstitution
LI Nan School of Metallurgical Engineering, Xi'an University of Architecture and Technology, Xi'an 710055, China;Shaanxi Research Center of Metallurgical Engineering, Xi'an 710055, China 
WANG Qiang School of Metallurgical Engineering, Xi'an University of Architecture and Technology, Xi'an 710055, China;Shaanxi Research Center of Metallurgical Engineering, Xi'an 710055, China 
NIU Wenjuan School of Metallurgical Engineering, Xi'an University of Architecture and Technology, Xi'an 710055, China;Shaanxi Research Center of Metallurgical Engineering, Xi'an 710055, China 
GUO Nan School of Metallurgical Engineering, Xi'an University of Architecture and Technology, Xi'an 710055, China;Shaanxi Research Center of Metallurgical Engineering, Xi'an 710055, China 
GE Shukai School of Metallurgical Engineering, Xi'an University of Architecture and Technology, Xi'an 710055, China;Shaanxi Research Center of Metallurgical Engineering, Xi'an 710055, China 
HUANG Liangliang School of Metallurgical Engineering, Xi'an University of Architecture and Technology, Xi'an 710055, China;Shaanxi Research Center of Metallurgical Engineering, Xi'an 710055, China 
WANG Jin School of Metallurgical Engineering, Xi'an University of Architecture and Technology, Xi'an 710055, China;Shaanxi Research Center of Metallurgical Engineering, Xi'an 710055, China 
LI Shen'ao School of Metallurgical Engineering, Xi'an University of Architecture and Technology, Xi'an 710055, China;Shaanxi Research Center of Metallurgical Engineering, Xi'an 710055, China 
HAN Peng School of Metallurgical Engineering, Xi'an University of Architecture and Technology, Xi'an 710055, China;Shaanxi Research Center of Metallurgical Engineering, Xi'an 710055, China 
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中文摘要:
      目的 通过冷喷涂(Cold Spraying)和超音速激光沉积(Supersonic Laser Deposition)技术对预制缺口的硬质铝合金试样进行修复。方法 通过扫描电子显微镜、电子背散射衍射检测器和X射线衍射仪等,研究了不同工艺对修复层微观结构和晶粒细化的影响,对修复后试样的疲劳性能进行了测试。结果 冷喷涂和超音速激光沉积涂层中均未发现粉末材料的相变。7075铝合金颗粒在冷喷涂和超音速激光沉积过程中的严重塑性变形导致了双峰晶粒结构。激光辅助加热提高了喷涂颗粒的塑性变形能力,使涂层的平均晶粒尺寸降至0.92 μm,其中局部动态再结晶是晶粒细化的主要原因。另外,超音速激光沉积层的平均显微硬度为196HV,高于冷喷涂涂层和基体。超音速激光沉积修复试样的疲劳极限为(135±15) MPa,远高于冷喷涂和未修复前的试样,这归因于修复涂层内聚和黏合强度的增加。结论 激光的引入可以改善7075铝合金颗粒的塑性变形能力,从而提高了修复层的显微硬度和修复件的疲劳极限。
英文摘要:
      High-quality repair of damaged components during aircraft service is crucial to aircraft maintenance industry. Apart from fulfilling the dimensional requirement, restoring the fatigue properties of repaired parts has always been a challenging problem. Cold spraying is a unique coating preparation technology characterized by low-temperature solid-state deposition, and the temperature during the spraying process is much lower than the melting temperature of the original powder material, which can effectively avoid adverse effects such as oxidation, phase transition and thermal cracking caused by high-temperature coating technologies such as laser cladding and arc spraying. The deposition and formation of cold spraying coatings are based on the plastic deformation of metal powder materials under high-speed impact, and powder materials need to have good plasticity, such as copper and aluminum. However, due to the lack of ductility in hard aluminum alloy powder, the repair of structural components such as frame beams made of hard aluminum alloy suffers from insufficient coating substrate adhesion and limited coating strength, which leads to low coating density and low deposition efficiency. Supersonic laser deposition technology is a new coating preparation technology developed on the basis of cold spraying technology and laser irradiation synchronous heating technology, which can achieve effective deposition of high-strength and high hardness powder materials. It can effectively improve the interface bonding strength of the coating substrate and the strength of the coating itself. Research has shown that laser assisted heating achieves the goal of using low-cost nitrogen gas instead of helium to prepare high-quality coatings while reducing coating preparation costs and expanding the selection range of deposition materials. Supersonic laser deposition technology can improve the deposition efficiency of traditional cold spraying while retaining the characteristics of solid-state deposition in cold spraying technology. In addition, compared to laser cladding coatings, supersonic laser deposition technology has advantages such as fine structure, phase stability, less dilution and good sliding wear resistance. In the present study, the pre-notched hard Al alloy samples were repaired by cold spraying and supersonic laser deposition. The effect of different processes on the microstructure, phase composition, crystallographic characteristics of deformed grains in the coatings was studied. The fatigue properties of the repaired specimens were tested. The results showed that no phase transformation of powder material was found in the cold spraying and supersonic laser deposition coatings. Severe plastic deformation of 7075 Al alloy particles during cold spraying and supersonic laser deposition resulted in bimodal grain structure. Laser assisted heating improved the plastic deformation ability of sprayed particles and reduced the average grain size of the coating to 0.92 μm, and the localized dynamic recrystallization was responsible for such refinement. In addition, the microhardness of supersonic laser deposition layer was 196HV, which was higher than that of cold spray coating and substrate. The fatigue limit of the sample repaired by supersonic laser deposition was (135±15) MPa, which was much higher than that of the sample repaired by cold spraying. This was attributed to the enhanced cohesive and adhesive bonding strength of repaired coatings. Therefore, the study provides a novel approach for high-quality repair of damaged aircraft components.
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