CN116162900A - Titanium nitride-based self-release carbon lubricating composite coating and preparation method and application thereof - Google Patents
Titanium nitride-based self-release carbon lubricating composite coating and preparation method and application thereof Download PDFInfo
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Abstract
Description
技术领域technical field
本发明涉及摩擦磨损防护技术领域,特别涉及一种氮化钛基自释放碳润滑复合涂层及其制备方法和应用。The invention relates to the technical field of friction and wear protection, in particular to a titanium nitride-based self-releasing carbon lubricating composite coating and its preparation method and application.
背景技术Background technique
TiN(Titanium Nitride,氮化钛)是一种具有高硬度、高耐磨性的陶瓷材料,是当今最成熟的工程材料之一,具有广泛的技术应用。长期以来,一直作为保护性和装饰性的涂层应用于模具制造、汽车工业、航空航天等多个领域。然而,氮化钛涂层缺乏润滑性能,具有较高的摩擦系数,限制了其在润滑减摩领域中的应用。TiN (Titanium Nitride, titanium nitride) is a ceramic material with high hardness and high wear resistance. It is one of the most mature engineering materials today and has a wide range of technical applications. For a long time, it has been used as a protective and decorative coating in many fields such as mold manufacturing, automotive industry, and aerospace. However, titanium nitride coating lacks lubricity and has a high coefficient of friction, which limits its application in the field of lubrication and friction reduction.
发明内容Contents of the invention
有鉴于此,本发明目的在于提供一种氮化钛基自释放碳润滑复合涂层及其制备方法和应用。本发明制备的氮化钛基自释放碳润滑复合涂层具有优异的润滑减摩耐磨效果。In view of this, the object of the present invention is to provide a titanium nitride-based self-releasing carbon lubricating composite coating and its preparation method and application. The titanium nitride-based self-releasing carbon lubricating composite coating prepared by the invention has excellent lubricating, friction-reducing and wear-resisting effects.
为了实现上述发明目的,本发明提供以下技术方案:In order to achieve the above-mentioned purpose of the invention, the present invention provides the following technical solutions:
本发明提供了一种氮化钛基自释放碳润滑复合涂层的制备方法,包括以下步骤:The invention provides a preparation method of a titanium nitride-based self-releasing carbon lubricating composite coating, comprising the following steps:
在基底上沉积多孔氮化钛涂层;所述沉积为多弧离子镀沉积,以钛金属靶为靶材,以氮气为工作气体,所述沉积的过程中,基底法线与钛金属靶法线的夹角为75~85°;Deposit a porous titanium nitride coating on the substrate; the deposition is multi-arc ion plating deposition, with a titanium metal target as the target material, and nitrogen as the working gas. During the deposition process, the substrate normal and the titanium metal target method The included angle of the line is 75-85°;
将所述多孔氮化钛涂层浸泡在碳源水溶液中进行水热处理,得到复合有碳前驱体的氮化钛涂层;Soaking the porous titanium nitride coating in an aqueous carbon source solution for hydrothermal treatment to obtain a titanium nitride coating composited with a carbon precursor;
将所述复合有碳前驱体的氮化钛涂层在保护气氛下进行碳化,得到所述氮化钛基自释放碳润滑复合涂层。The titanium nitride coating compounded with the carbon precursor is carbonized in a protective atmosphere to obtain the titanium nitride-based self-releasing carbon lubricating composite coating.
优选地,所述沉积的条件包括:靶基距为40~60mm,真空度为0.2~1.0Pa,氮气的气流量为100~800sccm,弧电流为75~85A,沉积时间为30~35min。Preferably, the deposition conditions include: target-base distance of 40-60 mm, vacuum degree of 0.2-1.0 Pa, nitrogen flow rate of 100-800 sccm, arc current of 75-85A, and deposition time of 30-35 min.
优选地,所述沉积多孔氮化钛涂层之前,还包括在所述基底上沉积钛层。Preferably, before depositing the porous titanium nitride coating, depositing a titanium layer on the substrate is also included.
优选地,所述钛层的厚度为400~500nm。Preferably, the thickness of the titanium layer is 400-500 nm.
优选地,所述碳源水溶液中的碳源为小分子糖;所述碳源水溶液的浓度为195~200g/L。Preferably, the carbon source in the carbon source aqueous solution is small molecule sugar; the concentration of the carbon source aqueous solution is 195-200 g/L.
优选地,所述水热处理的温度为150~200℃,时间为150~240min。Preferably, the temperature of the hydrothermal treatment is 150-200° C., and the time is 150-240 minutes.
优选地,所述保护气氛为氩气或氮气;所述保护气氛的气流量为60~150sccm。Preferably, the protective atmosphere is argon or nitrogen; the gas flow of the protective atmosphere is 60-150 sccm.
优选地,所述碳化的温度为500~600℃,时间为120~240min。Preferably, the temperature of the carbonization is 500-600° C., and the time is 120-240 minutes.
本发明提供了以上技术方案所述制备方法制备得到的氮化钛基自释放碳润滑复合涂层,包括沉积在基底上的多孔氮化钛涂层和填充在所述多孔氮化钛涂层的孔隙中的碳润滑相,所述多孔氮化钛涂层的孔为纳米尺度。The invention provides a titanium nitride-based self-releasing carbon lubricating composite coating prepared by the preparation method described in the above technical scheme, including a porous titanium nitride coating deposited on a substrate and a porous titanium nitride coating filled in the porous titanium nitride coating. A carbon lubricating phase in the pores, the pores of the porous titanium nitride coating are nanoscale.
本发明提供了以上技术方案所述氮化钛基自释放碳润滑复合涂层在润滑减摩中的应用。The invention provides the application of the titanium nitride-based self-releasing carbon lubricating composite coating in the above technical solution in lubricating and reducing friction.
本发明提供了一种氮化钛基自释放碳润滑复合涂层的制备方法,包括以下步骤:在基底上沉积多孔氮化钛涂层;所述沉积为多弧离子镀沉积,以钛金属靶为靶材,以氮气为工作气体,所述沉积的过程中,基底法线与钛金属靶法线的夹角为75~85°;将所述多孔氮化钛涂层浸泡在碳源水溶液中进行水热处理,得到复合有碳前驱体的氮化钛涂层;将所述复合有碳前驱体的氮化钛涂层在保护气氛下进行碳化,得到所述氮化钛基自释放碳润滑复合涂层。本发明采用斜角沉积(基底法线与钛金属靶法线的夹角为75~85°),通过在涂层沉积过程中加强自阴影效应的影响,使氮化钛的生长方向朝钛金属靶材的入射方向倾斜,获得多孔(具体为多孔柱状)的氮化钛硬质耐磨涂层;通过对多孔结构的氮化钛涂层进行水热填碳,将碳前驱体填充到氮化钛涂层纳米尺度的孔隙中;再通过碳化,将碳前驱体转化为碳润滑相,实现碳润滑相在氮化钛涂层中的储存。本发明将斜角沉积、多弧离子镀技术和水热碳包覆相结合制备出氮化钛基自释放碳润滑复合涂层,能够在滑动摩擦中将氮化钛纳米孔中的碳持续供给至摩擦接触面,提供减摩润滑效果;并且,本发明采用多弧离子镀沉积法制备氮化钛基硬质涂层,结合力好,耐磨性强,能够保护碳润滑相免受不同形式的失效,提高复合涂层的摩擦寿命。进一步地,本发明可以通过调整沉积角度和沉积时的工作气压(即氮气的气流量),对氮化钛涂层的孔隙率进行调控,实现碳填充量的可控制备,进而实现对复合涂层寿命的控制。The invention provides a preparation method of a titanium nitride-based self-releasing carbon lubricating composite coating, comprising the following steps: depositing a porous titanium nitride coating on a substrate; the deposition is multi-arc ion plating deposition, and a titanium metal target is used as the target material, using nitrogen as the working gas, during the deposition process, the angle between the normal line of the substrate and the normal line of the titanium metal target is 75-85°; the porous titanium nitride coating is soaked in the carbon source aqueous solution Carrying out hydrothermal treatment to obtain a titanium nitride coating compounded with a carbon precursor; carbonizing the titanium nitride coating compounded with a carbon precursor under a protective atmosphere to obtain the titanium nitride-based self-releasing carbon lubricating composite coating. The present invention adopts oblique angle deposition (the included angle between the normal of the substrate and the normal of the titanium metal target is 75-85°), and by strengthening the influence of the self-shadowing effect during the coating deposition process, the growth direction of titanium nitride is made towards the titanium metal The incident direction of the target is inclined to obtain a porous (specifically porous columnar) titanium nitride hard wear-resistant coating; by filling the porous titanium nitride coating with hydrothermal carbon, the carbon precursor is filled to the nitriding In the nanoscale pores of the titanium coating; and then through carbonization, the carbon precursor is converted into a carbon lubricating phase to realize the storage of the carbon lubricating phase in the titanium nitride coating. The invention combines oblique angle deposition, multi-arc ion plating technology and hydrothermal carbon coating to prepare a titanium nitride-based self-releasing carbon lubricating composite coating, which can continuously supply carbon in titanium nitride nanopores during sliding friction To the friction contact surface, anti-friction lubrication effect is provided; and, the present invention adopts multi-arc ion plating deposition method to prepare titanium nitride-based hard coating, which has good bonding force and strong wear resistance, and can protect the carbon lubricating phase from different forms failure and improve the friction life of the composite coating. Further, the present invention can adjust the porosity of the titanium nitride coating by adjusting the deposition angle and the working pressure during deposition (i.e., the gas flow rate of nitrogen gas), so as to realize the controllable preparation of the carbon filling amount, and then realize the composite coating Layer lifetime control.
本发明提供了以上技术方案所述制备方法制备得到的氮化钛基自释放碳润滑复合涂层,本发明提供的氮化钛基自释放碳润滑复合涂层为摩擦诱导碳润滑相释放的氮化钛基涂层,碳的填充大大提高了涂层的减摩耐磨润滑性能,在滑动摩擦中氮化钛纳米孔中的碳能够持续供给至摩擦接触面,提供减摩润滑效果。The present invention provides a titanium nitride-based self-releasing carbon lubricating composite coating prepared by the preparation method described in the above technical scheme. The titanium nitride-based self-releasing carbon lubricating composite coating provided by the present invention is nitrogen released from the friction-induced carbon lubricating phase. Titanium nitride-based coating, carbon filling greatly improves the anti-friction and wear-resistant lubrication performance of the coating. During sliding friction, the carbon in the titanium nitride nanopores can be continuously supplied to the friction contact surface, providing anti-friction and lubrication effects.
附图说明Description of drawings
图1为本发明氮化钛基自释放碳润滑复合涂层的制备流程图;Fig. 1 is the preparation flowchart of titanium nitride-based self-releasing carbon lubricating composite coating of the present invention;
图2为本发明实施例中氮化钛基自释放碳润滑复合涂层的减摩润滑机理示意图;Fig. 2 is the schematic diagram of the anti-friction lubrication mechanism of the titanium nitride-based self-releasing carbon lubricating composite coating in the embodiment of the present invention;
图3为实施例3和对比例1中制备的多孔氮化钛涂层与致密氮化钛涂层表面及截面的扫描电镜图,图3中,(a)和(c)分别对应于实施例3和对比例1的表面,(b)和(d)分别对应于实施例3和对比例1的截面;Fig. 3 is the scanning electron micrograph of porous titanium nitride coating and dense titanium nitride coating surface and section prepared in embodiment 3 and comparative example 1, among Fig. 3, (a) and (c) correspond to embodiment respectively 3 and the surface of Comparative Example 1, (b) and (d) correspond to the section of Embodiment 3 and Comparative Example 1 respectively;
图4为实施例3中在80°沉积角下由多弧离子镀沉积获得的氮化钛涂层的XRD图谱;Fig. 4 is the XRD spectrum of the titanium nitride coating obtained by multi-arc ion plating deposition under 80 ° of deposition angle in embodiment 3;
图5为实施例1~3制备的氮化钛基自释放碳润滑复合涂层和对比例1制备的氮化钛致密涂层复合碳的摩擦系数曲线。Fig. 5 is the friction coefficient curve of the titanium nitride-based self-releasing carbon lubricating composite coating prepared in Examples 1-3 and the titanium nitride dense coating composite carbon prepared in Comparative Example 1.
具体实施方式Detailed ways
本发明提供了一种氮化钛基自释放碳润滑复合涂层的制备方法,包括以下步骤:The invention provides a preparation method of a titanium nitride-based self-releasing carbon lubricating composite coating, comprising the following steps:
在基底上沉积多孔氮化钛涂层;所述沉积为多弧离子镀沉积,以钛金属靶为靶材,以氮气为工作气体,所述沉积的过程中,基底法线与钛金属靶法线的夹角为75~85°;Deposit a porous titanium nitride coating on the substrate; the deposition is multi-arc ion plating deposition, with a titanium metal target as the target material, and nitrogen as the working gas. During the deposition process, the substrate normal and the titanium metal target method The included angle of the line is 75-85°;
将所述多孔氮化钛涂层浸泡在碳源水溶液中进行水热处理,得到复合有碳前驱体的氮化钛涂层;Soaking the porous titanium nitride coating in an aqueous carbon source solution for hydrothermal treatment to obtain a titanium nitride coating composited with a carbon precursor;
将所述复合有碳前驱体的氮化钛涂层在保护气氛下进行碳化,得到所述氮化钛基自释放碳润滑复合涂层。The titanium nitride coating compounded with the carbon precursor is carbonized in a protective atmosphere to obtain the titanium nitride-based self-releasing carbon lubricating composite coating.
图1为本发明氮化钛基自释放碳润滑复合涂层的制备流程图。下面结合图1进行详细说明。Fig. 1 is a flow chart of the preparation of the titanium nitride-based self-releasing carbon lubricating composite coating of the present invention. The detailed description will be described below with reference to FIG. 1 .
本发明在基底上沉积多孔氮化钛涂层。本发明对所述基底没有特别的要求,采用本领域技术人员熟知的基底即可,如金属基底。在本发明中,所述沉积为多弧离子镀沉积,以钛金属靶(也可称为钛金属沉积靶)为靶材,以氮气为工作气体,所述沉积的过程中,基底法线与钛金属靶法线的夹角(所述夹角称为沉积角)为75~85°,优选为80°;所述钛金属靶优选为纯度为99.7%的圆形钛金属靶。在本发明中,所述沉积的条件优选包括:靶基距(靶材中心和基底中心的垂直距离)为40~60mm,优选为45~55mm;真空度为0.2~1.0Pa,优选为0.25~0.85Pa;氮气的气流量为100~800sccm,优选为150~500sccm;弧电流为75~85A,优选为75~80A;沉积时间为30~35min,优选为30~32min。The present invention deposits a porous titanium nitride coating on a substrate. The present invention has no special requirements on the substrate, and a substrate well known to those skilled in the art can be used, such as a metal substrate. In the present invention, the deposition is multi-arc ion plating deposition, with a titanium metal target (also referred to as a titanium metal deposition target) as the target material, and nitrogen as the working gas. During the deposition process, the substrate normal and The included angle of the normal line of the titanium metal target (the included angle is referred to as the deposition angle) is 75-85°, preferably 80°; the titanium metal target is preferably a circular titanium metal target with a purity of 99.7%. In the present invention, the deposition conditions preferably include: the target-base distance (the vertical distance between the center of the target and the center of the substrate) is 40-60mm, preferably 45-55mm; the degree of vacuum is 0.2-1.0Pa, preferably 0.25- 0.85Pa; nitrogen flow rate is 100-800sccm, preferably 150-500sccm; arc current is 75-85A, preferably 75-80A; deposition time is 30-35min, preferably 30-32min.
在本发明中,所述多弧离子镀沉积的装置(即镀膜机)包括腔体和设置在所述腔体内的转架盘和钛金属靶,所述转架盘和钛金属靶单向竖直放置于腔体的内部;所述转架盘上设有基底,所述转架盘可施加偏压,用于在镀膜过程中,通过合理控制偏压实现辉光清洗;所述钛金属靶用于轰击清洗基底和完成镀膜。In the present invention, the device for multi-arc ion plating deposition (i.e. coating machine) includes a cavity and a turntable disk and a titanium metal target arranged in the cavity, and the turntable disk and the titanium metal target are unidirectionally vertical Placed directly inside the chamber; the turntable is provided with a base, and the turntable can be biased to achieve glow cleaning by reasonably controlling the bias during the coating process; the titanium metal target For bombardment cleaning of substrates and finishing coatings.
在本发明中,所述多弧离子镀沉积的具体操作优选包括以下步骤:In the present invention, the specific operation of the multi-arc ion plating deposition preferably includes the following steps:
(a)将钛金属靶单向竖直放置于所述装置的腔体内部;(a) placing the titanium metal target unidirectionally vertically inside the cavity of the device;
(b)将基底超声清洗后放入所述腔体内部,调整靶基距为40~60mm和沉积角为75~85°;(b) putting the substrate into the cavity after ultrasonic cleaning, adjusting the target base distance to 40-60 mm and the deposition angle to 75-85°;
(c)抽取所述腔体内部的空气,使得腔体内部为真空状态;(c) extracting the air inside the cavity so that the inside of the cavity is in a vacuum state;
(d)在所述真空状态下,对腔体真空内部进行加热,并以第一气流量通入高纯氩气,在第一负偏压下对基底进行辉光放电清洗;(d) In the vacuum state, heating the vacuum interior of the cavity, and passing high-purity argon gas into the first gas flow, and performing glow discharge cleaning on the substrate under the first negative bias voltage;
(e)将所述高纯氩气的流量降低至第二气流量,开启所述钛金属靶,在第二负偏压下对基底进行轰击清洗;(e) reducing the flow rate of the high-purity argon gas to the second gas flow rate, opening the titanium metal target, and bombarding and cleaning the substrate under the second negative bias;
(f)将氮气通入所述真空腔体内,将真空度维持在0.2~1.0Pa,沉积多孔氮化钛涂层。(f) blowing nitrogen gas into the vacuum cavity, maintaining the vacuum degree at 0.2-1.0 Pa, and depositing a porous titanium nitride coating.
在本发明中,所述超声清洗优选包括依次进行的第一超声清洗和第二超声清洗;所述第一超声清洗优选在石油醚中进行,清洗时间优选为10~15min;所述第二超声清洗优选在无水乙醇中进行,清洗时间优选为10~15min;所述超声清洗后,优选将所得基底烘干。在本发明中,所述真空状态的真空度优选为4.0~5.0×10-3Pa,更优选为4.5~5.0×10- 3Pa;所述加热的温度优选为150~250℃,更优选为200~250℃;所述第一气流量优选为600~800sccm,更优选为700~800sccm;所述第一负偏压优选为-1000~-1200V,更优选为-1100~-1200V,所述辉光放电清洗的时间优选为10~15min,更优选为12~15min。在本发明中,所述第二气流量优选为150~200sccm,更优选为150~170sccm;所述第二负偏压优选为-750~-850V,更优选为-750~-800V,所述轰击清洗的时间优选为3~5min,更优选为4~5min。In the present invention, the ultrasonic cleaning preferably includes the first ultrasonic cleaning and the second ultrasonic cleaning carried out in sequence; the first ultrasonic cleaning is preferably carried out in petroleum ether, and the cleaning time is preferably 10 to 15 minutes; the second ultrasonic cleaning The cleaning is preferably performed in absolute ethanol, and the cleaning time is preferably 10-15 minutes; after the ultrasonic cleaning, the obtained substrate is preferably dried. In the present invention, the vacuum degree of the vacuum state is preferably 4.0 to 5.0×10 -3 Pa, more preferably 4.5 to 5.0× 10 -3 Pa ; the heating temperature is preferably 150 to 250°C, more preferably 200-250°C; the first gas flow is preferably 600-800 sccm, more preferably 700-800 sccm; the first negative bias voltage is preferably -1000--1200V, more preferably -1100--1200V, the The time for glow discharge cleaning is preferably 10-15 minutes, more preferably 12-15 minutes. In the present invention, the second air flow is preferably 150-200 sccm, more preferably 150-170 sccm; the second negative bias voltage is preferably -750-850V, more preferably -750-800V, the The bombardment cleaning time is preferably 3-5 minutes, more preferably 4-5 minutes.
在本发明中,所述沉积多孔氮化钛涂层之前,还优选在所述基底上沉积钛层,具体是在步骤(e)之后进行钛层沉积,由于偏置电压(即第二负偏压下)的影响,形成结构致密的钛层,然后再进行步骤(f)中的多孔氮化钛涂层沉积。在本发明中,所述钛层的厚度优选为400~500nm,所述钛层作为过渡层,有利于提高膜基结合力。In the present invention, before the deposition of the porous titanium nitride coating, it is also preferred to deposit a titanium layer on the substrate, especially after step (e), because the bias voltage (i.e. the second negative bias Under the influence of compression), a titanium layer with a dense structure is formed, and then the porous titanium nitride coating deposition in step (f) is carried out. In the present invention, the thickness of the titanium layer is preferably 400-500 nm, and the titanium layer is used as a transition layer, which is beneficial to improve the bonding force of the film base.
本发明将基体进行多弧离子镀,并采用斜角沉积技术(基底法线与钛金属靶法线的夹角为75~85°)在基体表面沉积多孔结构的氮化钛硬质耐磨涂层。所述斜角沉积技术是通过改变基体相对于靶材的方向,在沉积过程中增加自阴影效应的影响,在沉积涂层的同时获得特定的具有自由分离的纳米柱结构的多孔涂层,该技术获得的多孔硬质膜除了起到承载作用,还可以作为微库储存固体润滑剂,一方面保护固体润滑剂免受失效,另一方面还能够在摩擦过程中将固体润滑剂及时地释放到摩擦接触表面,减小滑动过程中的摩擦和磨损,避免涂层过早失效,延长运动部件的服役时间。In the present invention, the substrate is subjected to multi-arc ion plating, and the oblique-angle deposition technique (the angle between the normal line of the substrate and the normal line of the titanium metal target is 75-85°) is used to deposit the titanium nitride hard wear-resistant coating with a porous structure on the surface of the substrate. layer. The oblique angle deposition technique is to change the direction of the substrate relative to the target, increase the influence of the self-shadowing effect during the deposition process, and obtain a specific porous coating with a freely separated nano-column structure while depositing the coating. The porous hard film obtained by the technology can not only play a load-bearing role, but also store solid lubricants as micro-reservoirs. On the one hand, it protects the solid lubricants from failure, and on the other hand, it can release the solid lubricants in time during the friction process. Frictional contact surfaces, reducing friction and wear during sliding, avoiding premature failure of coatings, and prolonging the service life of moving parts.
得到多孔氮化钛涂层后,本发明将所述多孔氮化钛涂层浸泡在碳源水溶液中进行水热处理,得到复合有碳前驱体的氮化钛涂层。在本发明中,所述碳源水溶液中的碳源优选为小分子糖,本发明对所述小分子糖没有特别的要求,本领域技术人员熟知的小分子糖均可,如葡萄糖、蔗糖、果糖等;所述碳源水溶液的浓度优选为195~200g/L,更优选为198g/L。在本发明中,所述水热处理的温度优选为150~200℃,更优选为170~200℃,时间优选为150~240min,更优选为180~200min。在所述水热处理的过程中,小分子糖发生焦糖化反应,脱水生成焦糖,并裂解产生小分子醛酮类物质,即所述碳前驱体。本发明通过水热法将碳前驱体填充到多孔氮化钛涂层的纳米孔中。After the porous titanium nitride coating is obtained, the present invention soaks the porous titanium nitride coating in a carbon source aqueous solution for hydrothermal treatment to obtain a titanium nitride coating compounded with carbon precursors. In the present invention, the carbon source in the carbon source aqueous solution is preferably a small molecular sugar. The present invention has no special requirements for the small molecular sugar, and any small molecular sugar well known to those skilled in the art can be used, such as glucose, sucrose, fructose, etc.; the concentration of the carbon source aqueous solution is preferably 195-200 g/L, more preferably 198 g/L. In the present invention, the temperature of the hydrothermal treatment is preferably 150-200°C, more preferably 170-200°C, and the time is preferably 150-240min, more preferably 180-200min. In the process of the hydrothermal treatment, the small molecular sugar undergoes caramelization reaction, dehydrates to form caramel, and cracks to produce small molecular aldehydes and ketones, that is, the carbon precursor. The invention fills the carbon precursor into the nanopores of the porous titanium nitride coating through a hydrothermal method.
得到复合有碳前驱体的氮化钛涂层后,本发明将所述复合有碳前驱体的氮化钛涂层在保护气氛下进行碳化,得到所述氮化钛基自释放碳润滑复合涂层。在本发明中,所述保护气氛优选为氩气或氮气,所述氩气或氮气优选为高纯氩气或高纯氮气;所述保护气氛的气流量优选为60~150sccm,更优选为80~100sccm。在本发明中,所述碳化的温度优选为500~600℃,更优选为550℃,时间优选为120~240min,更优选为180~200min,所述碳化优选在管式炉中进行,在本发明中,所述碳化也可称为热处理。本发明通过所述碳化,将碳前驱体转化为碳润滑相,实现碳润滑相在氮化钛涂层中的储存。After obtaining the titanium nitride coating compounded with the carbon precursor, the present invention carbonizes the titanium nitride coating compounded with the carbon precursor under a protective atmosphere to obtain the titanium nitride-based self-releasing carbon lubricating composite coating layer. In the present invention, the protective atmosphere is preferably argon or nitrogen, and the argon or nitrogen is preferably high-purity argon or high-purity nitrogen; the gas flow rate of the protective atmosphere is preferably 60 to 150 sccm, more preferably 80 ~100 sccm. In the present invention, the carbonization temperature is preferably 500-600°C, more preferably 550°C, the time is preferably 120-240min, more preferably 180-200min, and the carbonization is preferably carried out in a tube furnace. In the invention, the carbonization may also be referred to as heat treatment. The present invention converts the carbon precursor into a carbon lubricating phase through the carbonization, and realizes the storage of the carbon lubricating phase in the titanium nitride coating.
本发明在制备硬质耐磨的氮化钛涂层的同时,获得了多孔的结构,通过碳的填充大大提高了涂层的减摩耐磨润滑效果,降低了涂层的磨损率;并且,多弧离子镀沉积的氮化钛基硬质涂层的结合力好,且具有优良的耐磨性能,更有利于提高复合涂层的承载能力;此外本发明还可通过调整沉积角度和沉积时的工作气压,实现涂层孔隙率的可控,从而实现碳填充量的可控制备,进而实现对复合涂层寿命的控制。The invention obtains a porous structure while preparing a hard and wear-resistant titanium nitride coating, greatly improves the anti-friction and wear-resistant lubrication effect of the coating through carbon filling, and reduces the wear rate of the coating; and, The titanium nitride-based hard coating deposited by multi-arc ion plating has good bonding force and excellent wear resistance, which is more conducive to improving the bearing capacity of the composite coating; in addition, the present invention can also adjust the deposition angle and deposition time The working air pressure can be controlled to control the porosity of the coating, thereby realizing the controllable preparation of the carbon filling amount, and then realizing the control of the life of the composite coating.
本发明提供了以上技术方案所述制备方法制备得到的氮化钛基自释放碳润滑复合涂层,包括沉积在基底上的多孔氮化钛涂层和填充在所述多孔氮化钛涂层的孔隙中的碳润滑相,所述多孔氮化钛涂层的孔为纳米尺度。在本发明中,所述多孔氮化钛涂层的孔隙率优选为7~14%。在本发明中,所述基底与多孔氮化钛涂层之间还优选沉积有钛层。本发明提供的氮化钛基自释放碳润滑复合涂层为摩擦诱导碳润滑相释放的氮化钛基涂层,碳的填充大大提高了涂层的减摩耐磨润滑性能,在滑动摩擦中氮化钛纳米孔中的碳能够持续供给至摩擦接触面,提供减摩润滑效果,图2为本发明实施例中氮化钛基自释放碳润滑复合涂层的减摩润滑机理示意图。本发明提供的氮化钛基自释放碳润滑复合涂层能够在润滑减摩中广泛有效的应用。The invention provides a titanium nitride-based self-releasing carbon lubricating composite coating prepared by the preparation method described in the above technical scheme, including a porous titanium nitride coating deposited on a substrate and a porous titanium nitride coating filled in the porous titanium nitride coating. A carbon lubricating phase in the pores, the pores of the porous titanium nitride coating are nanoscale. In the present invention, the porosity of the porous titanium nitride coating is preferably 7-14%. In the present invention, a titanium layer is preferably deposited between the substrate and the porous titanium nitride coating. The titanium nitride-based self-releasing carbon lubricating composite coating provided by the present invention is a titanium nitride-based coating that is released from the friction-induced carbon lubricating phase. The filling of carbon greatly improves the friction-reducing and wear-resistant lubrication performance of the coating. The carbon in the titanium nitride nanopores can be continuously supplied to the frictional contact surface to provide anti-friction lubrication effect. Figure 2 is a schematic diagram of the anti-friction lubrication mechanism of the titanium nitride-based self-releasing carbon lubricating composite coating in the embodiment of the present invention. The titanium nitride-based self-releasing carbon lubricating composite coating provided by the invention can be widely and effectively applied in lubricating and reducing friction.
下面结合实施例对本发明提供的氮化钛基自释放碳润滑复合涂层及其制备方法和应用进行详细的说明,但是不能把它们理解为对本发明保护范围的限定。The titanium nitride-based self-releasing carbon lubricating composite coating provided by the present invention and its preparation method and application will be described in detail below in conjunction with the examples, but they should not be understood as limiting the protection scope of the present invention.
实施例1Example 1
采用纯度为99.7%的圆形Ti金属沉积靶,单向竖直放置,弧电流为80A。选用304不锈钢作为涂层生长的样品基底,304不锈钢基底为20mm×20mm×2mm的块体;所述样品基底依次在石油醚、无水乙醇中各超声清洗15min,烘干后放入腔体。将所述样品基底的沉积角(样品基底法线与Ti金属沉积靶法线的夹角)调整为80°,靶基距调整为45mm。A circular Ti metal deposition target with a purity of 99.7% was used, placed vertically in one direction, and the arc current was 80A. 304 stainless steel was selected as the sample substrate for coating growth, and the 304 stainless steel substrate was a block of 20mm×20mm×2mm; the sample substrate was ultrasonically cleaned in petroleum ether and absolute ethanol for 15 minutes each, dried and put into the cavity. The deposition angle of the sample substrate (the angle between the normal of the sample substrate and the normal of the Ti metal deposition target) was adjusted to 80°, and the distance between the target and the substrate was adjusted to 45 mm.
实验前,先将腔体真空度抽取至5.0×10-3Pa,预加热到200℃,先通入高纯氩气800sccm,在-1200V偏压下,辉光放电清洗基底15min,氩气流量降低至150sccm,开启Ti金属沉积靶,在-800V偏压下对基底轰击5min。预先沉积Ti层(厚度为400~500nm)作为过渡层,以提高膜基结合力;将氮气通入所述真空腔体内,沉积氮化钛层,氮化钛层沉积时间为30min,沉积氮化钛时,氮气气流量为150sccm,真空度为2.5~2.7×10-1Pa,形成多弧离子镀制备的具有多孔结构的氮化钛硬质涂层(即多孔氮化钛涂层)。Before the experiment, the vacuum degree of the cavity was pumped to 5.0×10 -3 Pa, preheated to 200°C, and 800 sccm of high-purity argon gas was introduced first. Under the bias voltage of -1200V, the substrate was cleaned by glow discharge for 15 minutes. Decrease to 150 sccm, turn on the Ti metal deposition target, and bombard the substrate for 5 minutes under the bias voltage of -800V. Pre-deposit a Ti layer (400-500nm in thickness) as a transition layer to improve the bonding force of the film base; pass nitrogen gas into the vacuum chamber to deposit a titanium nitride layer. The deposition time of the titanium nitride layer is 30min, and the deposition time of the nitrided For titanium, the flow rate of nitrogen gas is 150 sccm, and the degree of vacuum is 2.5-2.7×10 -1 Pa to form a titanium nitride hard coating with a porous structure (ie, a porous titanium nitride coating) prepared by multi-arc ion plating.
将具有多孔结构的氮化钛涂层的样品转移到葡萄糖水溶液中进行水热处理,所述葡萄糖水溶液中一水葡萄糖浓度为198g/L,水热温度为200℃,水热时间为180min。The titanium nitride-coated sample with a porous structure was transferred to an aqueous glucose solution for hydrothermal treatment. The concentration of glucose monohydrate in the aqueous glucose solution was 198g/L, the hydrothermal temperature was 200°C, and the hydrothermal time was 180min.
将水热处理后的样品转移到管式炉,在高纯氩气环境下进行高温热处理,所述热处理温度为550℃,热处理时间为180min,高纯氩气的气流量为80sccm,在基底上形成孔隙率为7.5%的氮化钛基自释放碳润滑复合涂层,记为M1。Transfer the hydrothermally treated sample to a tube furnace, and perform high-temperature heat treatment in a high-purity argon environment. The heat treatment temperature is 550°C, the heat treatment time is 180min, and the gas flow rate of the high-purity argon gas is 80 sccm. The titanium nitride-based self-releasing carbon lubricating composite coating with a porosity of 7.5% is denoted as M1.
实施例2Example 2
采用纯度为99.7%的圆形Ti金属沉积靶,单向竖直放置,弧电流为80A。选用304不锈钢作为涂层生长的样品基底,304不锈钢基底为20mm×20mm×2mm的块体;所述样品基底依次在石油醚、无水乙醇中各超声清洗15min,烘干后放入腔体。将所述样品基底的沉积角(样品基底法线与Ti金属沉积靶法线的夹角)调整为80°,靶基距调整为45mm。A circular Ti metal deposition target with a purity of 99.7% was used, placed vertically in one direction, and the arc current was 80A. 304 stainless steel was selected as the sample substrate for coating growth, and the 304 stainless steel substrate was a block of 20mm×20mm×2mm; the sample substrate was ultrasonically cleaned in petroleum ether and absolute ethanol for 15 minutes each, dried and put into the cavity. The deposition angle of the sample substrate (the angle between the normal of the sample substrate and the normal of the Ti metal deposition target) was adjusted to 80°, and the distance between the target and the substrate was adjusted to 45 mm.
实验前,先将腔体真空度抽取至5.0×10-3Pa,预加热到200℃,先通入高纯氩气800sccm,在-1200V偏压下,辉光放电清洗基底15min,氩气流量降低至150sccm,开启Ti金属沉积靶,在-800V偏压下对基底轰击5min。预先沉积Ti层(厚度为400~500nm)作为过渡层,以提高膜基结合力;将氮气通入所述真空腔体内,沉积氮化钛层,氮化钛沉积时间为30min,沉积氮化钛时,氮气气流量为300sccm,真空度为5.0~5.2×10-1Pa,形成多弧离子镀制备的具有多孔结构的氮化钛硬质涂层(即多孔氮化钛涂层)。Before the experiment, the vacuum degree of the cavity was pumped to 5.0×10 -3 Pa, preheated to 200°C, and 800 sccm of high-purity argon gas was introduced first. Under the bias voltage of -1200V, the substrate was cleaned by glow discharge for 15 minutes. Decrease to 150 sccm, turn on the Ti metal deposition target, and bombard the substrate for 5 minutes under the bias voltage of -800V. Pre-deposit a Ti layer (thickness is 400-500nm) as a transition layer to improve the bonding force of the film base; pass nitrogen gas into the vacuum chamber to deposit a titanium nitride layer, the deposition time of titanium nitride is 30min, and deposit titanium nitride At this time, the flow rate of nitrogen gas is 300 sccm, and the degree of vacuum is 5.0-5.2×10 -1 Pa to form a titanium nitride hard coating with a porous structure (ie, a porous titanium nitride coating) prepared by multi-arc ion plating.
将具有多孔结构的氮化钛涂层的样品转移到葡萄糖水溶液中进行水热处理,所述葡萄糖水溶液中一水葡萄糖浓度为198g/L,水热温度为200℃,水热时间为180min。The titanium nitride-coated sample with a porous structure was transferred to an aqueous glucose solution for hydrothermal treatment. The concentration of glucose monohydrate in the aqueous glucose solution was 198g/L, the hydrothermal temperature was 200°C, and the hydrothermal time was 180min.
将水热处理后的样品转移到管式炉,在高纯氩气环境中进行高温热处理,所述热处理温度为550℃,热处理时间为180min,高纯氩气的气流量为80sccm,在基底上形成孔隙率为9.3%的氮化钛基自释放碳润滑复合涂层,记为M2。Transfer the hydrothermally treated sample to a tube furnace, and perform high-temperature heat treatment in a high-purity argon environment. The heat treatment temperature is 550°C, the heat treatment time is 180min, and the high-purity argon gas flow rate is 80 sccm, forming on the substrate The titanium nitride-based self-releasing carbon lubricating composite coating with a porosity of 9.3% is denoted as M2.
实施例3Example 3
采用纯度为99.7%的圆形Ti金属沉积靶,单向竖直放置,弧电流为80A。选用304不锈钢作为涂层生长的样品基底,304不锈钢基底为20mm×20mm×2mm的块体;所述样品基底依次在石油醚、无水乙醇中各超声清洗15min,烘干后放入腔体。将所述样品基底的沉积角(样品基底法线与Ti金属沉积靶法线的夹角)调整为80°,靶基距调整为45mm。A circular Ti metal deposition target with a purity of 99.7% was used, placed vertically in one direction, and the arc current was 80A. 304 stainless steel was selected as the sample substrate for coating growth, and the 304 stainless steel substrate was a block of 20mm×20mm×2mm; the sample substrate was ultrasonically cleaned in petroleum ether and absolute ethanol for 15 minutes each, dried and put into the cavity. The deposition angle of the sample substrate (the angle between the normal of the sample substrate and the normal of the Ti metal deposition target) was adjusted to 80°, and the distance between the target and the substrate was adjusted to 45 mm.
实验前,先将腔体真空度抽取至5.0×10-3Pa,预加热到200℃,先通入高纯氩气800sccm,在-1200V偏压下,辉光放电清洗基底15min,氩气流量降低至150sccm,开启Ti金属沉积靶,在-800V偏压下对基底轰击5min。预先沉积Ti层(厚度为400~500nm)作为过渡层,以提高膜基结合力;将氮气通入所述真空腔体内,沉积氮化钛层,氮化钛层沉积时间为30min,沉积氮化钛时,氮气气流量为500sccm,真空度为7.9~8.1×10-1Pa,形成多弧离子镀制备的具有多孔结构的氮化钛硬质涂层(即多孔氮化钛涂层)。Before the experiment, the vacuum degree of the cavity was pumped to 5.0×10 -3 Pa, preheated to 200°C, and 800 sccm of high-purity argon gas was introduced first. Under the bias voltage of -1200V, the substrate was cleaned by glow discharge for 15 minutes. Decrease to 150 sccm, turn on the Ti metal deposition target, and bombard the substrate for 5 minutes under the bias voltage of -800V. Pre-deposit a Ti layer (400-500nm in thickness) as a transition layer to improve the bonding force of the film base; pass nitrogen gas into the vacuum chamber to deposit a titanium nitride layer. The deposition time of the titanium nitride layer is 30min, and the deposition time of the nitrided For titanium, the flow rate of nitrogen gas is 500 sccm, and the degree of vacuum is 7.9-8.1×10 -1 Pa to form a titanium nitride hard coating with a porous structure (ie porous titanium nitride coating) prepared by multi-arc ion plating.
将具有多孔结构的氮化钛涂层的样品转移到葡萄糖水溶液中进行水热处理,所述葡萄糖水溶液中一水葡萄糖浓度为198g/L,水热温度为200℃,水热时间为180min。The titanium nitride-coated sample with a porous structure was transferred to an aqueous glucose solution for hydrothermal treatment. The concentration of glucose monohydrate in the aqueous glucose solution was 198g/L, the hydrothermal temperature was 200°C, and the hydrothermal time was 180min.
将水热处理后的样品转移到管式炉,在高纯氩气环境下进行高温热处理,所述热处理温度为550℃,热处理时间为180min,高纯氩气的气流量为80sccm,在基底上形成孔隙率为13.7%的氮化钛基自释放碳润滑复合涂层,记为M3。Transfer the hydrothermally treated sample to a tube furnace, and perform high-temperature heat treatment in a high-purity argon environment. The heat treatment temperature is 550°C, the heat treatment time is 180min, and the gas flow rate of the high-purity argon gas is 80 sccm. The titanium nitride-based self-releasing carbon lubricating composite coating with a porosity of 13.7%, is denoted as M3.
对比例1Comparative example 1
为了作为对比,采用多弧离子镀技术制备致密的氮化钛涂层,采用纯度为99.7%的圆形Ti金属沉积靶,单向竖直放置,弧电流为80A。选用304不锈钢作为涂层生长的样品基底,304不锈钢基底为20mm×20mm×2mm的块体;所述样品基底依次在石油醚、无水乙醇中各超声清洗15min,烘干后放入腔体。将所述样品基底的沉积角(样品基底法线与Ti金属沉积靶法线的夹角)调整为0°,靶基距调整为45mm。For comparison, a dense titanium nitride coating was prepared by multi-arc ion plating technology, using a circular Ti metal deposition target with a purity of 99.7%, placed vertically in one direction, and the arc current was 80A. 304 stainless steel was selected as the sample substrate for coating growth, and the 304 stainless steel substrate was a block of 20mm×20mm×2mm; the sample substrate was ultrasonically cleaned in petroleum ether and absolute ethanol for 15 minutes each, dried and put into the cavity. The deposition angle of the sample substrate (the angle between the normal of the sample substrate and the normal of the Ti metal deposition target) was adjusted to 0°, and the distance between the target and the substrate was adjusted to 45 mm.
实验前,先将腔体真空度抽取至5.0×10-3Pa,预加热到200℃,先通入高纯氩气800sccm,在-1200V偏压下,辉光放电清洗基底15min,氩气流量降低至150sccm,开启Ti金属沉积靶,在-800V偏压下对基底轰击5min。预先沉积Ti层(厚度为400~500nm)作为过渡层,以提高膜基结合力;将氮气通入所述真空腔体内,沉积氮化钛层,氮化钛沉积时间为30min,沉积氮化钛时,氮气气流量为500sccm,真空度为7.9~8.1×10-1Pa,形成多弧离子镀制备的具有致密结构的氮化钛硬质涂层(即致密氮化钛涂层)。Before the experiment, the vacuum degree of the cavity was pumped to 5.0×10 -3 Pa, preheated to 200°C, and 800 sccm of high-purity argon gas was introduced first. Under the bias voltage of -1200V, the substrate was cleaned by glow discharge for 15 minutes. Decrease to 150 sccm, turn on the Ti metal deposition target, and bombard the substrate for 5 minutes under the bias voltage of -800V. Pre-deposit a Ti layer (thickness is 400-500nm) as a transition layer to improve the bonding force of the film base; pass nitrogen gas into the vacuum chamber to deposit a titanium nitride layer, the deposition time of titanium nitride is 30min, and deposit titanium nitride At this time, the flow rate of nitrogen gas is 500 sccm, and the degree of vacuum is 7.9-8.1×10 -1 Pa to form a titanium nitride hard coating with a dense structure (ie, a dense titanium nitride coating) prepared by multi-arc ion plating.
将具有致密结构的氮化钛涂层的样品转移到葡萄糖水溶液中进行水热处理,所述葡萄糖水溶液中一水葡萄糖浓度为198g/L,水热温度为200℃,水热时间为180min。The sample with dense titanium nitride coating was transferred to aqueous glucose solution for hydrothermal treatment. The concentration of glucose monohydrate in the aqueous glucose solution was 198g/L, the hydrothermal temperature was 200°C, and the hydrothermal time was 180min.
将水热处理后的样品转移到管式炉,在高纯氩气环境中进行高温热处理,所述热处理温度为550℃,热处理时间为180min,高纯氩气的气流量为80sccm,在基底上形成结构致密的氮化钛基复合涂层(氮化钛致密涂层复合碳),记为M4。Transfer the hydrothermally treated sample to a tube furnace, and perform high-temperature heat treatment in a high-purity argon environment. The heat treatment temperature is 550°C, the heat treatment time is 180min, and the high-purity argon gas flow rate is 80 sccm, forming on the substrate Titanium nitride-based composite coating with dense structure (titanium nitride dense coating composite carbon), denoted as M4.
图3为实施例3和对比例1中制备的多孔氮化钛涂层与致密氮化钛涂层表面及截面的扫描电镜图对比图,图3中,(a)和(c)分别对应于实施例3和对比例1的表面,(b)和(d)分别对应于实施例3和对比例1的截面。图3的结果表明,随着沉积角的引入,氮化钛涂层的表面由致密结构转变成了多孔结构,氮化钛涂层的截面由致密结构转变为了纳米柱自由分离的结构。Fig. 3 is the scanning electron micrograph contrast figure of porous titanium nitride coating and dense titanium nitride coating surface and section prepared in embodiment 3 and comparative example 1, among Fig. 3, (a) and (c) correspond to respectively The surfaces of Example 3 and Comparative Example 1, (b) and (d) correspond to the cross-sections of Example 3 and Comparative Example 1, respectively. The results in Figure 3 show that with the introduction of the deposition angle, the surface of the titanium nitride coating changes from a dense structure to a porous structure, and the cross-section of the titanium nitride coating changes from a dense structure to a structure in which nanopillars are freely separated.
图4为实施例3中在80°沉积角下由多弧离子镀沉积获得的氮化钛涂层的XRD图谱,图4中,氮化钛涂层具有多晶结构,并表现出了(220)的择优取向。Fig. 4 is the XRD spectrum of the titanium nitride coating obtained by multi-arc ion plating deposition under 80 ° of deposition angles in embodiment 3, among Fig. 4, titanium nitride coating has polycrystalline structure, and has shown (220 ) preference orientation.
图5为实施例1~3制备的氮化钛基自释放碳润滑复合涂层和对比例1制备的氮化钛致密涂层复合碳的摩擦系数曲线,图5中的M1、M2、M3和M4分别对应于实施例1、实施例2、实施例3和对比例1。摩擦测试条件为:旋转半径4mm,载荷2N,对磨球(材质Al2O3)直径8mm,转速200r/min。图5所示测试结果:在摩擦磨损测试中,M1最初的摩擦系数为0.2,并随着时间逐渐增加,在6000s左右涂层失效;M2最初的摩擦系数为0.2,在2000~7000s区间内摩擦系数稳定在0.4,在7800s左右涂层失效;M3最初的摩擦系数为0.2,在2000~9000s区间内摩擦系数稳定在0.4,在9500s左右涂层失效;M4最初的摩擦系数为0.2,随后迅速升高至0.85,该涂层并没有表现出良好的润滑效果。根据摩擦测试结果可以看出,本发明可以在氮化钛纳米孔中实现碳的填充,从而降低氮化钛基复合涂层的摩擦系数。Fig. 5 is the friction coefficient curve of the titanium nitride-based self-releasing carbon lubricating composite coating prepared in Examples 1 to 3 and the titanium nitride dense coating composite carbon prepared in Comparative Example 1, M1, M2, M3 and M4 corresponds to Example 1, Example 2, Example 3 and Comparative Example 1, respectively. The friction test conditions are: radius of rotation 4mm, load 2N, diameter of counter ball (material Al 2 O 3 ) 8mm, rotation speed 200r/min. The test results shown in Figure 5: In the friction and wear test, the initial friction coefficient of M1 is 0.2, and gradually increases with time, and the coating fails at about 6000s; The coefficient is stable at 0.4, and the coating fails around 7800s; the initial friction coefficient of M3 is 0.2, and the friction coefficient is stable at 0.4 in the range of 2000-9000s, and the coating fails around 9500s; the initial friction coefficient of M4 is 0.2, and then rises rapidly. As high as 0.85, the coating did not exhibit a good lubricating effect. According to the friction test results, it can be seen that the present invention can realize carbon filling in the titanium nitride nanopores, thereby reducing the friction coefficient of the titanium nitride-based composite coating.
由以上实施例可以看出,本发明通过斜角沉积在氮化钛涂层中引入纳米孔阵列,可有效在水热处理中留存碳,涂层的纳米孔阵列是由斜角沉积中的自阴影效应所致,不需要后期的机械加工过程,其便捷性优于微织构制造工艺;氮化钛多孔涂层的孔隙率随工作气压的增加而增大,填充碳的氮化钛多孔涂层能够有效降低氮化钛的摩擦系数。本发明将斜角沉积、多弧离子镀和水热碳包覆相结合制备出多孔氮化钛涂层复合碳的润滑涂层,能够在涂层磨损时,及时向摩擦接触面释放补充润滑物碳,有效地减小了氮化钛的摩擦系数,增加了氮化钛的耐磨寿命。It can be seen from the above examples that the present invention introduces the nanopore array into the titanium nitride coating through oblique angle deposition, which can effectively retain carbon in the hydrothermal treatment. The nanopore array of the coating is formed by the self-shadowing in the oblique angle deposition. Due to the effect, there is no need for later mechanical processing, and its convenience is better than that of the micro-texture manufacturing process; the porosity of the titanium nitride porous coating increases with the increase of the working pressure, and the carbon-filled titanium nitride porous coating It can effectively reduce the friction coefficient of titanium nitride. The invention combines oblique-angle deposition, multi-arc ion plating and hydrothermal carbon coating to prepare a porous titanium nitride-coated composite carbon lubricating coating, which can release supplementary lubricants to the frictional contact surface in time when the coating is worn. Carbon effectively reduces the friction coefficient of titanium nitride and increases the wear life of titanium nitride.
以上所述仅是本发明的优选实施方式,应当指出,对于本技术领域的普通技术人员来说,在不脱离本发明原理的前提下,还可以做出若干改进和润饰,这些改进和润饰也应视为本发明的保护范围。The above is only a preferred embodiment of the present invention, it should be pointed out that, for those of ordinary skill in the art, without departing from the principle of the present invention, some improvements and modifications can also be made, and these improvements and modifications can also be made. It should be regarded as the protection scope of the present invention.
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Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104616910A (en) * | 2015-01-09 | 2015-05-13 | 东南大学 | Carbon-coating titanium based nano array material and preparation method and application thereof |
| CN105483631A (en) * | 2015-12-18 | 2016-04-13 | 中国科学院兰州化学物理研究所 | Preparation method for nano porous crystalline-state inorganic film material |
| CN105506566A (en) * | 2015-12-18 | 2016-04-20 | 中国科学院兰州化学物理研究所 | Preparation method of elastic hard lubricating nano composite thin-film material |
| CN106086787A (en) * | 2016-06-15 | 2016-11-09 | 济宁学院 | Ti‑TiN+MoS2/Ti laminated composite coating tool and its preparation process |
| US20180017122A1 (en) * | 2016-07-15 | 2018-01-18 | Borgwarner Inc. | Friction material |
| CN108385080A (en) * | 2018-04-28 | 2018-08-10 | 华南理工大学 | It is used to prepare the substrate and preparation method, the preparation method of foraminous die plate of foraminous die plate |
| CN108620111A (en) * | 2017-03-16 | 2018-10-09 | 中国科学院金属研究所 | A kind of nano silicon nitride titanium matrix composite and its preparation method and application |
| CN109809428A (en) * | 2017-11-20 | 2019-05-28 | 中国科学院大连化学物理研究所 | A kind of composite material with carbon layer supported on the surface of inorganic carrier and preparation method thereof |
-
2023
- 2023-03-02 CN CN202310186808.2A patent/CN116162900A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104616910A (en) * | 2015-01-09 | 2015-05-13 | 东南大学 | Carbon-coating titanium based nano array material and preparation method and application thereof |
| CN105483631A (en) * | 2015-12-18 | 2016-04-13 | 中国科学院兰州化学物理研究所 | Preparation method for nano porous crystalline-state inorganic film material |
| CN105506566A (en) * | 2015-12-18 | 2016-04-20 | 中国科学院兰州化学物理研究所 | Preparation method of elastic hard lubricating nano composite thin-film material |
| CN106086787A (en) * | 2016-06-15 | 2016-11-09 | 济宁学院 | Ti‑TiN+MoS2/Ti laminated composite coating tool and its preparation process |
| US20180017122A1 (en) * | 2016-07-15 | 2018-01-18 | Borgwarner Inc. | Friction material |
| CN108620111A (en) * | 2017-03-16 | 2018-10-09 | 中国科学院金属研究所 | A kind of nano silicon nitride titanium matrix composite and its preparation method and application |
| CN109809428A (en) * | 2017-11-20 | 2019-05-28 | 中国科学院大连化学物理研究所 | A kind of composite material with carbon layer supported on the surface of inorganic carrier and preparation method thereof |
| CN108385080A (en) * | 2018-04-28 | 2018-08-10 | 华南理工大学 | It is used to prepare the substrate and preparation method, the preparation method of foraminous die plate of foraminous die plate |
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