首页|电脉冲复合激光冲击对316L不锈钢摩擦磨损及耐腐蚀性能的影响

电脉冲复合激光冲击对316L不锈钢摩擦磨损及耐腐蚀性能的影响

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不锈钢具有良好的力学性能,在航空航天、能源开发等领域受到广泛应用,但其硬度低、耐磨性较差.本文利用脉冲电流对 316L不锈钢进行处理然后进行激光冲击强化(Electro-pulsing combining laser shock peening,EP-LSP),并对比激光冲击强化(Laser shock peening,LSP)进行分析.研究不同工艺对显微硬度、表面形貌、摩擦磨损等特性的影响.LSP和EP-LSP处理后试样的显微硬度比原试样分别提升 26.1%和 38.3%.在相同的摩擦条件下,LSP和EP-LSP处理后试样的磨损率比原试样减小 12.3%和 30.0%.原始试样主要为黏着磨损与疲劳磨损,LSP及EP-LSP处理后试样主要为磨粒磨损,EP-LSP试样犁沟细小且深度较浅.EP-LSP试样腐蚀试验中,腐蚀电位超过1.1 V电流密度逐渐增大,大于原始试样的0.4 V和LSP试样的0.7 V,表明EP-LSP试样钝化区域最大,耐腐蚀性最好.
Effect of Electro-pulsing Combining Laser Shock on Wear and Corrosion Resistance Properties of 316L Stainless Steel
Stainless steel is widely used in aerospace,energy development and other fields for its good mechanical properties,but its hardness and wear resistance is lower.In this study,316L stainless steel is treated by electro-pulsing combining laser shock peening(EP-LSP)and laser shock peening(LSP),respectively.The effects of different processes on micro-hardness,surface morphology,friction and wear were investigated.The micro-hardness of the samples treated with LSP and EP-LSP was respectively increased by 26.1%and 38.3%,compared with the as-built samples.The wear rate of the samples treated with LSP and EP-LSP is reduced by 12.3%and 30.0%under the same friction conditions.The original samples mainly have adhesive and fatigue wear,the LSP and EP-LSP samples mainly have abrasive wear,and the furrow of EP-LSP samples is small and shallow.The current density of the EP-LSP sample increases gradually when the potential exceeds 1.1 V,which is larger than 0.4 V of the original sample and 0.7 V of the LSP sample,indicating that the passivated area of the EP-LSP sample is the largest and the corrosion resistance is the best.

316L stainless steelElectro-pulsingLaser shock peeningFriction and wearCorrosion resistance

张硕文、江熔、秦秀、王汝家、张文武

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中国科学院宁波材料技术与工程研究所,宁波 315201

浙江省航空发动机极端制造技术研究重点实验室,宁波 315201

宁波大学,宁波 315000

316L不锈钢 脉冲电流 激光冲击强化 摩擦磨损 耐腐蚀性

国家自然科学基金宁波市自然科学基金中国博士后科学基金面上项目

523054372022J3072022M723254

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(9)