Page 79 - 《摩擦学学报》2020年第5期
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第 40 卷     第 5 期                        摩  擦  学  学  报                                  Vol 40   No 5
            2020  年 9  月                                 Tribology                                   Sept, 2020


            DOI: 10.16078/j.tribology.2020004



                   微量Ag元素对TiAlN涂层摩擦学性能的影响




                                               1
                                                        2*
                                                                         1
                                                                1
                                       王泽勇 , 冯长杰 , 师  超 , 刘光明 , 王  景             1
                                           (1. 南昌航空大学 材料学院,江西 南昌 330063;
                                         2. 沈阳航天航空大学 材料学院,辽宁 沈阳 110136)
                摘   要: 采用电弧离子镀技术利用Ti 50 Al 50 、Ti 50 Al 49 Ag 1 、Ti 50 Al 45 Ag 5 合金靶沉积制备出了TiAlN及不同Ag含量的
                TiAlAgN涂层. 利用球-盘式摩擦磨损试验机研究了室温、200、400和600 ℃等温度下的摩擦学性能;通过扫描电子显
                微镜(SEM)、X射线衍射仪(XRD)、显微硬度计、表面轮廓仪和划痕仪对磨损前后涂层的表面形貌、微观结构、硬度及
                涂层结合力进行了分析. 结果表明:TiAlN、TiAlAgN(Ag原子百分数0.12%)、TiAlAgN(Ag原子百分数0.30%)涂层的
                厚度分别为为4.18、5.31和4.69 μm,硬度分别为HV 0.2  2 049.4、HV 0.2  1 672.9、HV 0.2  1 398.5;TiAlN、TiAlAgN涂层的
                衍射峰位与面心立方的TiN相同,掺入Ag后TiAlN涂层的择优取向变为N(220)面. 三种涂层在不同温度下的磨损机
                理主要为黏着磨损与磨粒磨损. 室温时TiAlN涂层的摩擦系数比其他两种涂层要小约0.3,200 ℃时三种涂层的磨损
                率较大,400 ℃时掺Ag涂层的耐磨效果达到最佳. 此外,当Ag原子百分数在0.12%~0.30%范围时,随着Ag含量增加,
                涂层的结合力降低.
                关键词: 电弧离子镀; 涂层; 结合力; 黏着磨损; 磨粒磨损
                中图分类号: TG174,TG444                 文献标志码: A                文章编号: 1004-0595(2020)05–0634–13


                  Effect of Trace Ag on Tribological Properties of TiAlN coating


                                        1              2*         1               1           1
                           WANG Zeyong , FENG Changjie , SHI Chao , LIU Guangming , WANG Jing
                            (1. School of Materials, Nanchang Hang kong University, Jiangxi Nanchang 330063,China
                    2. School of Materials, Shenyang University of Aeronautics and Astronautics, Liaoning Shenyang 110136,China)
                 Abstract: TiAlN and TiAlAgN coatings with different Ag contents were prepared by arc ion plating with Ti 50 Al 50 ,
                 Ti 50 Al 49 Ag 1 , Ti 50 Al 45 Ag 5  alloy targets in this paper. The tribological properties were studied by using a ball-on-disk
                 tribo-meter at room temperature, 200 ℃, 400 ℃ and 600 ℃.The surface morphology, microstructure, hardness and
                 adhesion of the coatings before and after wear were determined by scanning electron microscope, X-ray diffraction,
                 microhardness   tester,   surface   profiler   and   scratch   tester.   The   results   showed   that   the   thickness   of   TiAlN,
                 TiAlAgN(0.12%Ag,atomic percentage), TiAlAgN(0.30%Ag,atomic percentage) coating was 4.18 μm, 5.31 μm and
                 4.69 μm. The hardness was HV 0.2  2 049.4, HV 0.2  1 672.9, HV 0.2  1 398.5, respectively. The diffraction peaks of TiAlN
                 and TiAlAgN coatings were the same as those of FCC TiN, and the preferential orientation of N(220) for TiAlN coating
                 was found after adding Ag. The wear mechanism of the three coatings at elevated temperatures was identified as
                 adhesive wear and abrasive wear. At room temperature, the friction coefficient of TiAlN coating was about 0.3, which
                 was lower than that of the other two coatings. The wear rate of the three coatings was higher at 200 ℃, and the best wear
                 resistance was obtained at 400 ℃. In addition, as the Ag contents were between 0.12%~0.30%, the adhesion of the
                 coating decreased.
                 Key words: arc ion plating; coating; adhesion; adhesion wear; abrasive wear


            Received 3 January 2020, revised 2 April 2020, accepted 9 April 2020, available online 28 September 2020.
            *Corresponding author. E-mail: chjfengniat@126.com, Tel: +86-24-89724198.
            The  project  was  supported  by  the  National  Natural  Science  Foundation  of  China  (51365041, 51961028)  and  Talent  project  of
            Shenyang Aerospace University(19YB05).
            国家自然科学基金项目(51365041,51961028)和沈阳航空航天大学人才引进项目(19YB05)资助.
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