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材料导报  2026, Vol. 40 Issue (4): 25020059-10    https://doi.org/10.11896/cldb.25020059
  金属与金属基复合材料 |
飞行器运输振动下GH4169/WC激光熔覆复合涂层摩擦磨损性能研究
林婕1, 张海瑞1, 丁昊昊2,*, 姚鑫宇2, 姚重阳1, 王尧1
1 中国运载火箭技术研究院, 北京 100076
2 西南交通大学轨道交通运载系统全国重点实验室, 成都 610031
Friction and Wear Behavior of GH4169/WC Laser Cladding Composite Coating Under Aircraft Transportation Vibration
LIN Jie1, ZHANG Hairui1, DING Haohao2,*, YAO Xinyu2, YAO Chongyang1, WANG Yao1
1 China Academy of Launch Vehicle Technology, Beijing 100076, China
2 State Key Laboratory of Rail Transit Vehicle System, Southwest Jiaotong University, Chengdu 610031, China
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摘要 针对飞行器机构在运输、转载、挂飞等工况下的磨损失效问题,结合激光熔覆技术制备GH4169/WC复合涂层,开展激光熔覆工艺参数优化研究以及材料在运输振动工况下的常温干摩擦磨损行为和机理研究。基于田口-灰色关联理论,建立了GH4169/WC复合材料激光熔覆工艺参数优化方法,对激光熔覆工艺参数进行优化。以实际地面运输试验数据作为输入,开展飞行器机构动力学仿真与有限元分析,确定磨损试验中接触应力、滑动速度等试验参数。利用往复摩擦磨损试验机开展不同接触参数下的摩擦磨损试验,对比GH4169/WC复合涂层与单一GH4169材料的耐磨性能,分析磨损形貌和磨损量随接触应力与滑动速度的变化规律和机理。结合田口-灰色关联理论成功将多响应目标转化为单一灰色关联度,实现了激光熔覆工艺的优化。优化后的激光功率为650 W,扫描速度为2 mm/s,送粉速率为4.7 g/min。并且预测的灰色关联度(0.669 7)与实验值(0.672 9)吻合较好,误差仅为0.5%。同时,与单一GH4169镍基高温合金相比,GH4169/WC复合涂层磨损深度以及对磨副磨损量均得到了降低。田口-灰色关联法能够快速准确地实现复合材料激光熔覆工艺参数优化,有效提高熔覆层质量,为激光熔覆复合材料的工业应用提供了理论依据。同时,利用激光熔覆技术制备GH4169/WC复合涂层能够提高材料耐磨性能,改善飞行器在运输、转载、挂飞等工况下的磨损失效问题。
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林婕
张海瑞
丁昊昊
姚鑫宇
姚重阳
王尧
关键词:  激光熔覆工艺优化  GH4169/WC复合涂层  田口-灰色关联法  摩擦磨损  磨损机理    
Abstract: Wear-induced failure of GH4169 nickel-based superalloy components in aircraft transport, transfer, and suspendedflight operations constitutes a critical engineering challenge requiring urgent resolution. The advent of high-power lasers has facilitated the application of laser cladding technology in metal-ceramic composite coatings to enhance material wear resistance. However, limited research exists regarding laser cladding composite coatings, particularly concerning laser cladding parameters of composite coatings and the wear resistance characteristics and underlying mechanisms of composite coatings. Therefore, in the present study, GH4169/WC composite coating was deposited by laser cladding, and the process parameters were optimized by Taguchi-grey relational analysis. Furthermore, the dry slip wear behavior and its mechanism were systematically studied under vibration conditions simulating the operation of airborne equipment at ambient temperature. The main results demonstrate that the Taguchi-grey relation method effectively consolidates multi-response objectives into a singular grey relational grade (GRG), achieving the optimization of laser cladding process parameters. The optimized laser power, scanning speed and powder feeding rate are 650 W, 2 mm/s, and 4.7 g/min, respectively. Notably, the predicted GRG (0.669 7) exhibits excellent agreement with experimental results (0.672 9), the prediction error is only 0.5%. Compared with GH4169 substrate, the composite coating reduces the wear depth by 38.2% and mass loss by 41.5%. In addition, with the increase in contact stress, the wear depth and wear amount of the material increases. And with the increase in sli-ding speed, the oxidation wear degree of the material gradually increases. The present study validated the efficacy of Taguchi-grey relation method in laser cladding optimization and elucidated the wear resistance mechanisms in metal-ceramic composite coatings, thereby providing theoretical foundations and experimental basis for enhancing the wear resistance of aerospace components.
Key words:  laser cladding process optimization    GH4169/WC composite coating    taguchi-grey relation method    friction and wear    wear mec-hanism
出版日期:  2026-02-25      发布日期:  2026-02-13
ZTFLH:  TH117  
基金资助: 中央高校基本科研业务费专项资金(2682024GF022)
通讯作者:  * 丁昊昊,西南交通大学机械工程学院副教授、硕士研究生导师。主要从事服役损伤失效机制与控制技术方面的研究。haohaoding@swjtu.edu.cn   
作者简介:  林婕,中国运载火箭技术研究院硕士研究生,研究方向为飞行器总体设计和摩擦学。
引用本文:    
林婕, 张海瑞, 丁昊昊, 姚鑫宇, 姚重阳, 王尧. 飞行器运输振动下GH4169/WC激光熔覆复合涂层摩擦磨损性能研究[J]. 材料导报, 2026, 40(4): 25020059-10.
LIN Jie, ZHANG Hairui, DING Haohao, YAO Xinyu, YAO Chongyang, WANG Yao. Friction and Wear Behavior of GH4169/WC Laser Cladding Composite Coating Under Aircraft Transportation Vibration. Materials Reports, 2026, 40(4): 25020059-10.
链接本文:  
https://www.mater-rep.com/CN/10.11896/cldb.25020059  或          https://www.mater-rep.com/CN/Y2026/V40/I4/25020059
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