CN102560338B - A kind of cermet coating and preparation method thereof - Google Patents
A kind of cermet coating and preparation method thereof Download PDFInfo
- Publication number
- CN102560338B CN102560338B CN201010580583.1A CN201010580583A CN102560338B CN 102560338 B CN102560338 B CN 102560338B CN 201010580583 A CN201010580583 A CN 201010580583A CN 102560338 B CN102560338 B CN 102560338B
- Authority
- CN
- China
- Prior art keywords
- coating
- phase
- preparation
- substrate
- metal
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 238000000576 coating method Methods 0.000 title claims abstract description 149
- 239000011248 coating agent Substances 0.000 title claims abstract description 138
- 238000002360 preparation method Methods 0.000 title claims abstract description 69
- 239000011195 cermet Substances 0.000 title abstract description 36
- 150000004767 nitrides Chemical class 0.000 claims abstract description 38
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 31
- 239000000956 alloy Substances 0.000 claims abstract description 31
- 229910052751 metal Inorganic materials 0.000 claims abstract description 29
- 239000002184 metal Substances 0.000 claims abstract description 28
- 238000000034 method Methods 0.000 claims abstract description 22
- 230000007797 corrosion Effects 0.000 claims abstract description 14
- 238000005260 corrosion Methods 0.000 claims abstract description 14
- 239000007789 gas Substances 0.000 claims abstract description 13
- 239000011159 matrix material Substances 0.000 claims abstract description 10
- 239000000463 material Substances 0.000 claims abstract description 8
- 229910000905 alloy phase Inorganic materials 0.000 claims abstract description 5
- 239000006104 solid solution Substances 0.000 claims abstract description 5
- 239000000758 substrate Substances 0.000 claims description 51
- 238000000151 deposition Methods 0.000 claims description 31
- 230000008021 deposition Effects 0.000 claims description 29
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 24
- 238000005524 ceramic coating Methods 0.000 claims description 18
- 229910052757 nitrogen Inorganic materials 0.000 claims description 15
- 239000000203 mixture Substances 0.000 claims description 9
- 238000004140 cleaning Methods 0.000 claims description 8
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 claims description 6
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims description 6
- 239000000126 substance Substances 0.000 claims description 6
- 238000005137 deposition process Methods 0.000 claims description 5
- 239000013077 target material Substances 0.000 claims description 5
- 229910052786 argon Inorganic materials 0.000 claims description 4
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 claims description 3
- 238000002844 melting Methods 0.000 claims description 3
- 230000008018 melting Effects 0.000 claims description 3
- 238000005498 polishing Methods 0.000 claims description 3
- 239000007787 solid Substances 0.000 claims description 3
- 238000002203 pretreatment Methods 0.000 claims description 2
- 238000004506 ultrasonic cleaning Methods 0.000 claims description 2
- 239000000376 reactant Substances 0.000 claims 4
- 239000000470 constituent Substances 0.000 claims 3
- 238000012986 modification Methods 0.000 claims 2
- 230000004048 modification Effects 0.000 claims 2
- 238000001816 cooling Methods 0.000 claims 1
- 238000013461 design Methods 0.000 claims 1
- 230000000694 effects Effects 0.000 claims 1
- 239000012530 fluid Substances 0.000 claims 1
- 238000002347 injection Methods 0.000 claims 1
- 239000007924 injection Substances 0.000 claims 1
- 238000004020 luminiscence type Methods 0.000 claims 1
- 238000012423 maintenance Methods 0.000 claims 1
- 238000002156 mixing Methods 0.000 claims 1
- 238000012545 processing Methods 0.000 claims 1
- 230000001105 regulatory effect Effects 0.000 claims 1
- 230000002000 scavenging effect Effects 0.000 claims 1
- 238000010583 slow cooling Methods 0.000 claims 1
- 238000009504 vacuum film coating Methods 0.000 claims 1
- 230000003647 oxidation Effects 0.000 abstract description 23
- 238000007254 oxidation reaction Methods 0.000 abstract description 23
- 238000005240 physical vapour deposition Methods 0.000 abstract description 7
- 239000012495 reaction gas Substances 0.000 abstract description 6
- 238000005728 strengthening Methods 0.000 abstract description 6
- 238000004519 manufacturing process Methods 0.000 abstract description 5
- 239000002245 particle Substances 0.000 abstract description 5
- 238000000137 annealing Methods 0.000 abstract description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 36
- 238000005516 engineering process Methods 0.000 description 17
- 238000007733 ion plating Methods 0.000 description 17
- 229910052759 nickel Inorganic materials 0.000 description 13
- 239000010408 film Substances 0.000 description 12
- 229910000601 superalloy Inorganic materials 0.000 description 12
- 239000011651 chromium Substances 0.000 description 10
- 229910052782 aluminium Inorganic materials 0.000 description 9
- 229910052804 chromium Inorganic materials 0.000 description 9
- 238000001755 magnetron sputter deposition Methods 0.000 description 8
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 8
- 230000035939 shock Effects 0.000 description 7
- 230000004584 weight gain Effects 0.000 description 7
- 235000019786 weight gain Nutrition 0.000 description 7
- 150000002500 ions Chemical class 0.000 description 5
- 238000012360 testing method Methods 0.000 description 5
- FAPWRFPIFSIZLT-UHFFFAOYSA-M Sodium chloride Chemical compound [Na+].[Cl-] FAPWRFPIFSIZLT-UHFFFAOYSA-M 0.000 description 4
- 229910003266 NiCo Inorganic materials 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 3
- 229910000734 martensite Inorganic materials 0.000 description 3
- 238000004544 sputter deposition Methods 0.000 description 3
- 239000010959 steel Substances 0.000 description 3
- WGLPBDUCMAPZCE-UHFFFAOYSA-N Trioxochromium Chemical compound O=[Cr](=O)=O WGLPBDUCMAPZCE-UHFFFAOYSA-N 0.000 description 2
- 239000010406 cathode material Substances 0.000 description 2
- 229910000423 chromium oxide Inorganic materials 0.000 description 2
- 239000013078 crystal Substances 0.000 description 2
- 238000000227 grinding Methods 0.000 description 2
- 238000010884 ion-beam technique Methods 0.000 description 2
- 239000011253 protective coating Substances 0.000 description 2
- 150000003839 salts Chemical class 0.000 description 2
- 239000011780 sodium chloride Substances 0.000 description 2
- 238000001771 vacuum deposition Methods 0.000 description 2
- 229910000967 As alloy Inorganic materials 0.000 description 1
- 229910008326 Si-Y Inorganic materials 0.000 description 1
- 229910006773 Si—Y Inorganic materials 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 230000008033 biological extinction Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000005253 cladding Methods 0.000 description 1
- 239000008199 coating composition Substances 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 238000010891 electric arc Methods 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 238000002513 implantation Methods 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 238000007750 plasma spraying Methods 0.000 description 1
- 238000004321 preservation Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 229910052761 rare earth metal Inorganic materials 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 238000004227 thermal cracking Methods 0.000 description 1
- 239000010409 thin film Substances 0.000 description 1
- 229910052727 yttrium Inorganic materials 0.000 description 1
Images
Landscapes
- Physical Vapour Deposition (AREA)
Abstract
一种金属陶瓷涂层:由金属相母体和弥散分布纳米晶氮化物相颗粒组成;所述金属相(b)为含固溶强化合金组元的合金相或者纯金属;氮化物相(c)弥散分布于金属相(b)中,其中氮化物(c)的体积分数为5~60%。一种金属陶瓷涂层制备方法,具体使用真空物理气相沉积类型方法;制备过程包含三个步骤:(1)零件必须置于真空室(e)内,(2)在真空室(e)内通入反应气体(f),(3)使靶(g)表面的物质形成气相(h)。本发明所述涂层具有较高的断裂韧性、抗氧化性能和耐腐蚀性能,具有较高的氧化膜的粘附性,较好的硬度和耐磨性。涂层制备工艺简单,制备后不需要经过真空退火等后续处理,具有较高的生产效率。
A cermet coating: composed of a metal phase matrix and dispersed nanocrystalline nitride phase particles; the metal phase (b) is an alloy phase or pure metal containing solid solution strengthening alloy components; the nitride phase (c) It is dispersed in the metal phase (b), and the volume fraction of the nitride (c) is 5-60%. A method of preparing a cermet coating, specifically using a vacuum physical vapor deposition type method; the preparation process includes three steps: (1) the part must be placed in the vacuum chamber (e), (2) the vacuum chamber (e) is passed through Into the reaction gas (f), (3) to make the material on the surface of the target (g) form a gas phase (h). The coating of the invention has higher fracture toughness, oxidation resistance and corrosion resistance, higher adhesion of oxide film, better hardness and wear resistance. The coating preparation process is simple, no subsequent treatment such as vacuum annealing is required after preparation, and the production efficiency is high.
Description
技术领域 technical field
本发明涉及高温防护技术,特别提供了一种金属陶瓷涂层及其制备方法。 The invention relates to high temperature protection technology, and in particular provides a cermet coating and a preparation method thereof.
背景技术 Background technique
MCrAlY涂层是较为理想的包覆涂层。由于其具有良好的抗高温氧化性能和抗热腐蚀性能,以及很好的韧性和抗热疲劳强度,被广泛地应用于航空发动机、燃气轮机等的涡轮叶片上。MCrAlY涂层的优点在于其成分选择的多样性,即可以根据不同的工作环境和不同基体材料选择合适的涂层成分,不受基体化学成分和微观结构限制。但是MCrAlY涂层硬度及耐磨性有待于提高。目前MCrAlY涂层的主要制备方法有物理气相沉积和等离子喷涂。 MCrAlY coating is an ideal cladding coating. Because of its good high temperature oxidation resistance and thermal corrosion resistance, as well as good toughness and thermal fatigue resistance, it is widely used in turbine blades of aero-engines, gas turbines, etc. The advantage of MCrAlY coating lies in the diversity of its composition selection, that is, the appropriate coating composition can be selected according to different working environments and different substrate materials, and is not limited by the chemical composition and microstructure of the substrate. But the hardness and wear resistance of MCrAlY coating need to be improved. At present, the main preparation methods of MCrAlY coatings are physical vapor deposition and plasma spraying.
与MCrAlY涂层相比,氮化物涂层硬度高,并且具有优异的耐磨性。但是氮化物涂层的热稳定性不高,抗热裂性能差,因此在高温防护领域的应用研究较少。近年来,CrN, CrAlN涂层由于具有很高的硬度和耐磨性,良好的抗高温氧化性和抗腐蚀性而得到人们的广泛关注。但是,氮化物涂层的韧性差,氧化后,涂层表面的氧化物在高温下受到热循环和机械作用易剥落,加速涂层的失效,因此氮化物涂层与基体的结合强度及其韧性也有待于提高。最近Lin 等利用脉冲非平衡磁控溅射的方法制备了不同Al含量的CrAlN涂层,其表现出较好的高温性能,降低了AISI304不锈钢在800oC的氧化速率。同时研究发现随着Al含量的增加,CrAlN涂层的抗氧化性逐渐提高,并且Al的加入有效地抑制了高温环境下涂层中含氮量的减少,使涂层在800oC经1h退火处理仍维持25Gpa的硬度值。但是,该涂层在高温下伴随氧化物的形成会发生分解,仅能提供短期的防护[参见文献J. Lin, et al. A study of the oxidation behavior of CrN and CrAlN thin films in air using DSC and TGA analyses [J]. Surface & Coatings Technology, 202 (2008): 3272-3283.]。 Compared with MCrAlY coating, nitride coating has high hardness and has excellent wear resistance. However, the thermal stability of the nitride coating is not high, and the thermal cracking resistance is poor, so the application research in the field of high temperature protection is less. In recent years, CrN, CrAlN coatings have attracted widespread attention due to their high hardness and wear resistance, good high temperature oxidation resistance and corrosion resistance. However, the toughness of the nitride coating is poor. After oxidation, the oxide on the surface of the coating is easily peeled off by thermal cycles and mechanical action at high temperature, which accelerates the failure of the coating. Therefore, the bonding strength and toughness of the nitride coating to the substrate It also needs to be improved. Recently, Lin et al. used pulsed unbalanced magnetron sputtering to prepare CrAlN coatings with different Al contents, which showed better high temperature performance and reduced the oxidation rate of AISI304 stainless steel at 800 o C. At the same time, it was found that with the increase of Al content, the oxidation resistance of CrAlN coating gradually improved, and the addition of Al effectively suppressed the decrease of nitrogen content in the coating under high temperature environment, so that the coating was annealed at 800 o C for 1h The treatment still maintains a hardness value of 25Gpa. However, this coating decomposes at high temperatures with oxide formation and provides only short-term protection [see J. Lin, et al. A study of the oxidation behavior of CrN and CrAlN thin films in air using DSC and TGA analyzes [J]. Surface & Coatings Technology, 202 (2008): 3272-3283.].
目前,高温合金的氮化物防护涂层,或因为其韧性差,与基体的结合强度低,结构不致密,或因为热稳定性不高等问题而不能够对高温合金起到有效的腐蚀防护作用,远达不到工业应用要求。因此,发展具有高抗氧化性、高抗腐蚀性、高热稳定性、高耐磨性和高韧性的新型的高温防护涂层,仍是高温合金防护领域亟待解决的问题。 At present, the nitride protective coatings of superalloys cannot effectively protect superalloys from corrosion due to their poor toughness, low bonding strength with the substrate, lack of compact structure, or low thermal stability. Far from meeting the requirements of industrial applications. Therefore, the development of new high-temperature protective coatings with high oxidation resistance, high corrosion resistance, high thermal stability, high wear resistance and high toughness is still an urgent problem to be solved in the field of superalloy protection.
发明内容 Contents of the invention
本发明的目的在于提供一种金属陶瓷涂层及其制备方法。该金属陶瓷涂层由金属相母体和弥散分布纳米晶氮化物相颗粒组成。该金属陶瓷涂层的显微硬度、耐磨性、抗1000℃高温氧化性均比MCrAlY涂层(M=Ni, Co, 或NiCo)提高一倍以上,适用于金属工件。该制备方法为采用合金为靶材和氮气为反应气体的真空物理气相沉积类型方法,包括但不限于多弧离子镀、磁控溅射。可通过调整合金靶材成分及真空室温度、通入的气体压力、基体偏压等控制参数,以获得满足硬度、耐磨性、抗氧化性和抗热腐蚀性等不同要求的涂层。涂层制备工艺简单,制备后不需要经过真空退火等后续处理,具有较高的生产效率。 The object of the present invention is to provide a cermet coating and a preparation method thereof. The cermet coating is composed of a metal phase matrix and dispersed nanocrystalline nitride phase particles. The microhardness, wear resistance, and high temperature oxidation resistance of the cermet coating are more than double that of the MCrAlY coating (M=Ni, Co, or NiCo), and are suitable for metal workpieces. The preparation method is a vacuum physical vapor deposition method using an alloy as a target material and nitrogen as a reaction gas, including but not limited to multi-arc ion plating and magnetron sputtering. Coatings that meet different requirements such as hardness, wear resistance, oxidation resistance, and hot corrosion resistance can be obtained by adjusting control parameters such as alloy target composition, vacuum chamber temperature, gas pressure, and substrate bias. The coating preparation process is simple, no subsequent treatment such as vacuum annealing is required after preparation, and the production efficiency is high.
本发明一种金属陶瓷涂层,其特征在于:该金属陶瓷涂层由金属相母体和弥散分布纳米晶氮化物相颗粒组成; A cermet coating of the present invention is characterized in that: the cermet coating is composed of a metal phase matrix and dispersedly distributed nanocrystalline nitride phase particles;
所述金属相(b)为含固溶强化合金组元的合金相或者纯金属,当为纯金属时其中包括但不限于Ni; The metal phase (b) is an alloy phase containing solid solution strengthening alloy components or a pure metal, including but not limited to Ni when it is a pure metal;
氮化物相(c) 弥散分布于金属相(b)中,其中氮化物(c)的体积分数为5~60 %。 The nitride phase (c) is dispersed in the metal phase (b), and the volume fraction of the nitride (c) is 5-60%.
所述金属陶瓷涂层,其特征在于:氮化物相(c)含至少一种金属元素;氮化物相(c)晶粒尺寸≤80nm。 The cermet coating is characterized in that: the nitride phase (c) contains at least one metal element; the grain size of the nitride phase (c) is ≤80nm.
本发明还要求保护金属陶瓷涂层制备方法,其特征在于: The present invention also claims a method for preparing a cermet coating, characterized in that:
制备后的成品由金属相母体和弥散分布纳米晶氮化物相颗粒组成;所述金属相(b)为含固溶强化合金组元的合金相或者纯金属,当为纯金属时其中包括但不限于Ni;氮化物相(c) 弥散分布于金属相(b)中,其中氮化物(c)的体积分数为5~60 %; The prepared finished product is composed of a metal phase matrix and dispersed nanocrystalline nitride phase particles; the metal phase (b) is an alloy phase or a pure metal containing solid solution strengthening alloy components, and when it is a pure metal, it includes but not Limited to Ni; the nitride phase (c) is dispersed in the metal phase (b), and the volume fraction of the nitride (c) is 5-60%;
具体使用真空物理气相沉积类型方法,包括但不限于多弧离子镀、磁控溅射等; Specific use of vacuum physical vapor deposition methods, including but not limited to multi-arc ion plating, magnetron sputtering, etc.;
制备过程包含三个步骤:(1)零件必须置于真空室(e)内,(2)在真空室(e)内通入反应气体(f),(3)使靶(g)表面的物质形成气相(h)。 The preparation process consists of three steps: (1) the part must be placed in the vacuum chamber (e), (2) the reaction gas (f) is introduced into the vacuum chamber (e), (3) the substance on the surface of the target (g) A gas phase (h) is formed.
所述金属陶瓷涂层制备方法,其特征在于: The preparation method of the cermet coating is characterized in that:
制备过程中,反应气体(f)必须含氮气,也可同时通氩气等其他气体,通入的反应气体量应使真空室的气压≥0.2Pa; During the preparation process, the reaction gas (f) must contain nitrogen, and other gases such as argon can also be passed at the same time, and the amount of reaction gas introduced should make the pressure of the vacuum chamber ≥ 0.2Pa;
靶的材料为合金,数量≥1;靶的合金组元含不易形成或不形成氮化物的合金组元,包括但不限于Ni等; The material of the target is an alloy, and the quantity is ≥1; the alloy components of the target contain alloy components that are not easy to form or do not form nitrides, including but not limited to Ni, etc.;
在制备过程中要求能够通过改变靶的化学成分以调节金属陶瓷涂层(a)的氮化物相(c)体积分数;制备过程中要求能够调节真空室温度、通入的气体压力、基体偏压等控制参数以调节金属陶瓷涂层(a)中的氮化物相(c)体积分数。 During the preparation process, it is required to be able to adjust the volume fraction of the nitride phase (c) of the cermet coating (a) by changing the chemical composition of the target; during the preparation process, it is required to be able to adjust the temperature of the vacuum chamber, the gas pressure introduced, and the bias voltage of the substrate and other control parameters to adjust the volume fraction of the nitride phase (c) in the cermet coating (a).
所述金属陶瓷涂层制备方法,进一步优选的要求是: In the preparation method of the cermet coating, further preferred requirements are:
制备步骤如下:(1)合金靶材的制备:采用真空熔炼的方法制备多组元合金作为阴极靶材;(2) 工件前处理:镀膜前对试样进行常规的打磨、镜面抛光处理,最后分别用丙酮和酒精超声波清洗,吹干备用;(3) 涂层制备:所述金属陶瓷涂层的制备方法采用多弧离子镀; The preparation steps are as follows: (1) Preparation of alloy target: adopt vacuum melting method to prepare multi-component alloy as cathode target; (2) Workpiece pretreatment: before coating, the sample is subjected to conventional grinding and mirror polishing treatment, and finally Ultrasonic cleaning with acetone and alcohol respectively, drying for later use; (3) coating preparation: the preparation method of the cermet coating adopts multi-arc ion plating;
涂层制备过程具体为: The coating preparation process is specifically as follows:
首先将样品置于真空镀膜室的样品架上,抽真空后通入纯度99.99%的Ar和纯度99.99% 的N2,通入的反应气体量应使真空室的气压≥0.2Pa;然后利用促发电极,采用电弧放电的方法,在固体阴极靶材表面产生强烈发光的阴极弧斑,使靶材金属直接蒸发并电离;同时对基片施加一定的负偏压,使离子束加速;N2和从阴极弧斑放出的阴极物质的离子混合形成等离子体,经负偏压加速后沉积在基片上形成金属陶瓷涂层,具体参数为: First place the sample on the sample rack of the vacuum coating chamber, and then pass in Ar with a purity of 99.99% and N 2 with a purity of 99.99% after vacuuming. The generator electrode adopts the method of arc discharge to generate a strong luminous cathode arc spot on the surface of the solid cathode target, so that the target metal is directly evaporated and ionized; at the same time, a certain negative bias is applied to the substrate to accelerate the ion beam; N 2 It mixes with the ions of the cathode material emitted from the cathode arc spot to form a plasma, which is accelerated by a negative bias and deposited on the substrate to form a cermet coating. The specific parameters are:
离子清洗:真空度:P﹤6×10-3Pa,电弧电流:65-72A,基片负偏压:600V,清洗时间:3min; Ion cleaning: vacuum: P﹤6×10 -3 Pa, arc current: 65-72A, substrate negative bias: 600V, cleaning time: 3min;
涂层沉积:真空度:P﹤6×10-3Pa,电弧电流:65-72A,电弧电压:18-22V,基片负偏压:100-500V,基片温度:200-300oC,Ar流量为8-20sccm,N2流量为100-400sccm,靶材与基体距离:200mm,沉积时间:1-5h。 Coating deposition: vacuum degree: P﹤6×10 -3 Pa, arc current: 65-72A, arc voltage: 18-22V, substrate negative bias voltage: 100-500V, substrate temperature: 200-300 o C, The flow of Ar is 8-20sccm, the flow of N 2 is 100-400sccm, the distance between the target and the substrate: 200mm, the deposition time: 1-5h.
有关参数控制的具体要求如下: The specific requirements for parameter control are as follows:
(1)在涂层沉积前,通入纯度99.99%高纯Ar和纯度99.99% N2,对基片进行离子清洗和注入作用,同时使阴极靶材表层氮化,有效地减少沉积初期大颗粒的产生; (1) Before coating deposition, high-purity Ar with a purity of 99.99% and N 2 with a purity of 99.99% are introduced to perform ion cleaning and implantation on the substrate, and at the same time nitride the surface of the cathode target to effectively reduce large particles at the initial stage of deposition production;
(2)在涂层沉积过程中,严格将弧电流控制在65-72A之间,Ar流量在8-20sccm之间,其数值过高或过低都会导致涂层熔滴剧增或熄弧等现象。根据不同工件材料,严格控制基片的温度:200-300oC,温度过低,涂层与基体的结合力下降,温度过高将导致基体软化;装有工件的样品架在离子清洗、涂层沉积的过程中保持18 rpm/min的速度自转,以保证涂层沉积均匀; (2) During the coating deposition process, strictly control the arc current between 65-72A, and the Ar flow rate between 8-20sccm, if the value is too high or too low, it will lead to a sharp increase of coating droplets or arc extinction, etc. Phenomenon. According to different workpiece materials, strictly control the temperature of the substrate: 200-300 o C, if the temperature is too low, the bonding force between the coating and the substrate will decrease, and if the temperature is too high, the substrate will soften; During the layer deposition process, the speed of rotation at 18 rpm/min is maintained to ensure uniform coating deposition;
(3)在涂层沉积过程中,调整N2流量:调控范围100-400sccm,基片偏压:调控范围100-500V,沉积时间:1-5h;以获得厚度、硬度、耐磨性、抗氧化性和抗热腐蚀性要求不同的涂层; (3) During the coating deposition process, adjust the N 2 flow rate: the control range is 100-400sccm, the substrate bias voltage: the control range is 100-500V, the deposition time: 1-5h; to obtain the thickness, hardness, wear resistance, resistance Oxidation and hot corrosion resistance require different coatings;
(4)在沉积结束后,使真空室缓慢降温,待工件完全冷却后取出,以防止工件受热氧化。 (4) After the deposition is completed, the temperature of the vacuum chamber is slowly cooled, and the workpiece is taken out after it is completely cooled to prevent the workpiece from being oxidized by heat.
本发明的金属陶瓷涂层,具有如下特征: The cermet coating of the present invention has the following characteristics:
1. 本发明的金属陶瓷涂层由金属相和氮化物组成,氮化物的体积分数为5~60 %。该金属陶瓷涂层以金属相作为基体,以纳米尺度的氮化物作为强化相,形成氮化物弥散分布于基体相的复合结构。金属相可为纯金属或含固溶强化合金组元的合金相,弥散分布的氮化物晶粒尺寸小于80nm。 1. The cermet coating of the present invention is composed of metal phase and nitride, and the volume fraction of nitride is 5-60%. The cermet coating uses a metal phase as a matrix and a nanoscale nitride as a strengthening phase to form a composite structure in which the nitride is dispersed in the matrix phase. The metal phase can be pure metal or an alloy phase containing solid-solution strengthening alloy components, and the grain size of the dispersed nitride is less than 80nm.
2. 本发明的金属陶瓷涂层以金属相作为基体,使涂层具有较高的断裂韧性、抗氧化性能和耐腐蚀性能,同时由于金属相中固溶的稀土元素,如Y,能有效的提高氧化膜的粘附性,从而有效提高了涂层的抗热裂性能;弥散分布于基体相的氮化物为强化相,使该金属陶瓷涂层具有较高的硬度和耐磨性。本发明中的金属陶瓷涂层的显微硬度、耐磨性、抗1000℃高温氧化性均比MCrAlY涂层(M=Ni, Co, 或NiCo)提高一倍以上。 2. The metal-ceramic coating of the present invention uses the metal phase as the matrix, so that the coating has high fracture toughness, oxidation resistance and corrosion resistance, and at the same time, due to the solid-dissolved rare earth elements in the metal phase, such as Y, it can effectively The adhesion of the oxide film is improved, thereby effectively improving the thermal crack resistance of the coating; the nitride dispersed in the matrix phase is a strengthening phase, so that the cermet coating has higher hardness and wear resistance. The microhardness, wear resistance and high-temperature oxidation resistance of the cermet coating in the present invention are more than double that of the MCrAlY coating (M=Ni, Co, or NiCo).
本发明所述的金属陶瓷涂层的制备方法,确定真空物理气相沉积类型方法,包括但不限于多弧离子镀、磁控溅射等作为所述金属陶瓷的制备技术,所述方法特征在于:(1)采用单一的合金靶或多个合金靶,(2)采用合金靶时,合金靶中含不易形成或不形成氮化物的合金组元,包括但不限于Ni等,(3)可通过调节真空物理气相沉积参数和合金靶的化学成分,获得满足厚度、硬度、耐磨性、抗氧化性和抗热腐蚀性等不同要求的涂层。 The preparation method of the cermet coating of the present invention determines the type of vacuum physical vapor deposition method, including but not limited to multi-arc ion plating, magnetron sputtering, etc. as the preparation technology of the cermet, and the method is characterized in that: (1) A single alloy target or multiple alloy targets are used, (2) when an alloy target is used, the alloy target contains alloy components that are not easy to form or do not form nitrides, including but not limited to Ni, etc., (3) can be passed Adjust the vacuum physical vapor deposition parameters and the chemical composition of the alloy target to obtain coatings that meet different requirements such as thickness, hardness, wear resistance, oxidation resistance and hot corrosion resistance.
本发明的一种金属陶瓷涂层的制备方法,可通过调整真空室温度、氮气流量、基片负偏压,沉积时间等工艺参数,以获得厚度、硬度、耐磨性、抗氧化性和抗热腐蚀性等不同要求的涂层。该金属陶瓷涂层适用于金属工件,不受材料的结构,成分等因素限制。涂层制备工艺简单,制备后不需要经过真空退火等后续处理,具有较高的生产效率。 The preparation method of a cermet coating of the present invention can obtain thickness, hardness, wear resistance, oxidation resistance and resistance Coatings with different requirements such as hot corrosion. The metal-ceramic coating is suitable for metal workpieces and is not limited by factors such as material structure and composition. The coating preparation process is simple, no subsequent treatment such as vacuum annealing is required after preparation, and the production efficiency is high.
本发明中采用真空物理气相沉积类型方法,包括但不限于多弧离子镀、磁控溅射等制备的金属陶瓷涂层的显微硬度、耐磨性、抗1000℃高温氧化性均比MCrAlY涂层(M=Ni, Co, 或NiCo)提高一倍以上。本发明的一种金属陶瓷涂层的制备方法,可通过调整氮气流量、基片负偏压,沉积时间等工艺参数,以获得厚度、硬度、耐磨性、抗氧化性和抗热腐蚀性等不同要求的涂层。涂层制备工艺简单,制备后不需要经过真空退火等后续处理,具有较高的生产效率。 In the present invention, vacuum physical vapor deposition methods, including but not limited to multi-arc ion plating, magnetron sputtering, etc., are adopted in the microhardness, wear resistance, and high temperature oxidation resistance of MCrAlY coatings compared to MCrAlY coatings. layer (M=Ni, Co, or NiCo) more than doubled. The preparation method of a cermet coating of the present invention can obtain thickness, hardness, wear resistance, oxidation resistance and thermal corrosion resistance, etc. Coatings with different requirements. The coating preparation process is simple, no subsequent treatment such as vacuum annealing is required after preparation, and the production efficiency is high.
附图说明 Description of drawings
下面结合附图及实施方式对本发明作进一步详细的说明: Below in conjunction with accompanying drawing and embodiment the present invention is described in further detail:
图1为采用多弧离子镀技术在马氏体耐热钢1Cr16Ni2MoN基体上制备该金属陶瓷涂层的TEM眀场像照片; Fig. 1 adopts multi-arc ion plating technology to prepare the TEM field image photo of this cermet coating on the martensitic heat-resistant steel 1Cr16Ni2MoN substrate;
图2为采用多弧离子镀技术在镍基高温合金K417基体上制备该金属陶瓷涂层的显微照片; Fig. 2 is the photomicrograph that adopts multi-arc ion plating technology to prepare this cermet coating on nickel base superalloy K417 substrate;
图3为采用多弧离子镀技术在镍基高温合金K417基体上制备的金属陶瓷涂层在1000oC恒温氧化100h的显微照片; Figure 3 is a photomicrograph of a cermet coating prepared on a nickel-based superalloy K417 substrate by multi-arc ion plating technology and oxidized at a constant temperature of 1000 o C for 100 h;
图4为采用多弧离子镀技术在镍K417基体上制备的金属陶瓷涂层在900oC, NaCl/Na2SO4(25:75wt.%)环境中热腐蚀80h显微照片; Figure 4 is a photomicrograph of the cermet coating prepared on the nickel K417 substrate by multi-arc ion plating technology in the environment of 900 o C, NaCl/Na 2 SO 4 (25:75wt.%) hot corrosion for 80h;
图5为采用多弧离子镀技术在玻璃基体上制备金属陶瓷涂层的TEM眀场像照片。 Figure 5 is a TEM field image photo of a cermet coating prepared on a glass substrate by using multi-arc ion plating technology.
具体实施方式 Detailed ways
实施例1 Example 1
以马氏体耐热钢1Cr16Ni2MoN为基体,采用多弧离子镀技术为该陶瓷涂层的制备方法,其制备工艺如下: The martensitic heat-resistant steel 1Cr16Ni2MoN is used as the substrate, and the multi-arc ion plating technology is used as the preparation method of the ceramic coating. The preparation process is as follows:
(1)合金靶材(以NiCrAlSiY合金靶为例)的制备:采用真空熔炼的方法制备的Ni-Cr-Al-Si-Y多组元合金作为阴极靶材,其合金成分为:8~13wt.% Al,20~26 wt.% Cr, 0.5~1.0 wt.% Si,约0.5 wt.% Y,余量为Ni, 并且Al和Cr的总含量为31~37 wt.%; (1) Preparation of alloy target (taking NiCrAlSiY alloy target as an example): Ni-Cr-Al-Si-Y multi-component alloy prepared by vacuum melting method is used as cathode target material, and its alloy composition is: 8~13wt .% Al, 20-26 wt.% Cr, 0.5-1.0 wt.% Si, about 0.5 wt.% Y, the balance being Ni, and the total content of Al and Cr is 31-37 wt.%;
(2) 零件前处理:镀膜前对零件进行常规的打磨、镜面抛光处理,最后分别用丙酮和酒精超声波清洗,吹干备用; (2) Pre-treatment of parts: Before coating, the parts are subjected to conventional grinding and mirror polishing, and finally ultrasonically cleaned with acetone and alcohol respectively, and dried for later use;
(3) 涂层制备:将样品置于真空镀膜室的样品架上,抽真空后通入高纯Ar(纯度99.99%)和N2(纯度99.99%),利用促发电极,采用电弧放电的方法,在NiCrAlSiY固体阴极靶材表面产生强烈发光的阴极弧斑,使靶材金属直接蒸发并电离。同时对基片施加一定的负偏压,使离子束加速。N2和从阴极弧斑放出的阴极物质的离子混合形成等离子体,经偏压加速后沉积在基片上形成金属陶瓷涂层,具体参数为: (3) Coating preparation: the sample is placed on the sample holder of the vacuum coating chamber, and high-purity Ar (purity 99.99%) and N 2 (purity 99.99%) are introduced after vacuuming. In this method, an intensely luminescent cathode arc spot is generated on the surface of the NiCrAlSiY solid cathode target, so that the target metal is directly evaporated and ionized. At the same time, a certain negative bias voltage is applied to the substrate to accelerate the ion beam. N2 mixes with the ions of the cathode material emitted from the cathode arc spot to form a plasma, which is accelerated by a bias voltage and deposited on the substrate to form a cermet coating. The specific parameters are:
离子清洗:真空度:P﹤6×10-3Pa,电弧电流:65-72A,基片负偏压:600V,清洗时间:3min。 Ion cleaning: vacuum: P﹤6×10 -3 Pa, arc current: 65-72A, substrate negative bias: 600V, cleaning time: 3min.
涂层沉积:真空度:P﹤6×10-3Pa,电弧电流:65-72A,基片负偏压:100V,基片温度:210oC,Ar流量为8sccm,N2流量为225sccm,靶材与基体距离:200mm,沉积时间:3h。 Coating deposition: vacuum degree: P﹤6×10 -3 Pa, arc current: 65-72A, substrate negative bias voltage: 100V, substrate temperature: 210 o C, Ar flow rate is 8 sccm, N2 flow rate is 225 sccm, target Material and substrate distance: 200mm, deposition time: 3h.
涂层的TEM眀场相如图1所示,晶粒尺寸小于30nm的氮化物弥散分布于涂层基体相Ni上,氮化物的体积分数约为35%。沉积速率为183.3nm/min,涂层为γ-Ni,CrN和AlN相。涂层的含氮量为19.43at%, Al和Cr的含量分别为:14.40 at.%、18.60 at.%。涂层的硬度为889.6 HV25gf,加载10N时涂层的磨损量为11.0×10-3mm3/m。 The TEM field phase of the coating is shown in Figure 1. Nitride with a grain size smaller than 30nm is diffusely distributed on the matrix phase Ni of the coating, and the volume fraction of nitride is about 35%. The deposition rate is 183.3nm/min, and the coating is γ-Ni, CrN and AlN phases. The nitrogen content of the coating is 19.43 at%, and the Al and Cr contents are: 14.40 at.% and 18.60 at.%, respectively. The hardness of the coating is 889.6 HV 25gf , and the wear amount of the coating is 11.0×10 -3 mm 3 /m when the load is 10N.
实施例2 Example 2
以镍基高温合金K417为基体,采用多弧离子镀技术为该陶瓷涂层的制备方法,其制备工艺如下: The nickel-based superalloy K417 is used as the substrate, and the multi-arc ion plating technology is used as the preparation method of the ceramic coating. The preparation process is as follows:
(1) 合金靶材的制备同实施例1; (1) The preparation of the alloy target is the same as in Example 1;
(2) 零件前处理同实施例1; (2) Part pretreatment is the same as embodiment 1;
(3) 涂层制备:涂层沉积时基片负偏压为300V, 其他工艺参数同实施例1。 (3) Coating preparation: The substrate negative bias voltage was 300V during coating deposition, and other process parameters were the same as in Example 1.
涂层沉积速率为148.9nm/min,涂层为γ-Ni,CrN和AlN相,其微观结构如图2所示。涂层的含氮量为15.40 at.%, Al和Cr的含量分别为14.88 at.%和16.87 at.%。涂层的硬度为970.2 HV25gf,加载10N时涂层的磨损量为6.96×10-3mm3/m。样品经1000oC恒温氧化100h,涂层表面生成了一层很薄的连续致密的氧化铝膜,样品单位面积氧化增重:0.34mg/cm2。 The deposition rate of the coating is 148.9nm/min, and the coating is γ-Ni, CrN and AlN phases, and its microstructure is shown in Figure 2. The nitrogen content of the coating is 15.40 at.%, and the Al and Cr contents are 14.88 at.% and 16.87 at.%, respectively. The hardness of the coating is 970.2 HV 25gf , and the wear amount of the coating is 6.96×10 -3 mm 3 /m when the load is 10N. After the sample was oxidized at a constant temperature of 1000 o C for 100 hours, a thin continuous and dense aluminum oxide film was formed on the surface of the coating, and the oxidation weight gain per unit area of the sample was 0.34mg/cm 2 .
实施例3 Example 3
以镍基高温合金K438为基体,采用多弧离子镀技术为该陶瓷涂层的制备方法,制备工艺同实施例2。 The ceramic coating is prepared by using the nickel-based superalloy K438 as the substrate and adopting multi-arc ion plating technology, and the preparation process is the same as that in Example 2.
涂层沉积速率为145.4 nm/min,涂层为γ-Ni,CrN和AlN相。涂层的含氮量为16.35 at.%, Al和Cr的含量分别为14.18 at.%和16.14 at.%。涂层的硬度为980.6 HV25gf,加载10N时涂层的磨损量为6.04×10-3mm3/m。样品经1000oC恒温氧化100h,涂层表面生成了一层很薄的连续致密的氧化铝膜,样品单位面积氧化增重:0.37mg/cm2。 The deposition rate of the coating is 145.4 nm/min, and the coating is γ-Ni, CrN and AlN phases. The nitrogen content of the coating is 16.35 at.%, and the Al and Cr contents are 14.18 at.% and 16.14 at.%, respectively. The hardness of the coating is 980.6 HV 25gf , and the wear amount of the coating is 6.04×10 -3 mm 3 /m when the load is 10N. After the sample was oxidized at a constant temperature of 1000 o C for 100 hours, a thin continuous and dense aluminum oxide film was formed on the surface of the coating, and the oxidation weight gain per unit area of the sample was 0.37mg/cm 2 .
实施例4 Example 4
以镍基高温合金K417为基体,采用多弧离子镀技术为该陶瓷涂层的制备方法,其制备工艺如下: The nickel-based superalloy K417 is used as the substrate, and the multi-arc ion plating technology is used as the preparation method of the ceramic coating. The preparation process is as follows:
(1) 合金靶材的制备同实施例1; (1) The preparation of the alloy target is the same as in Example 1;
(2) 零件前处理同实施例1; (2) Part pretreatment is the same as embodiment 1;
(3) 涂层制备:涂层沉积时基片负偏压为400V, 其他工艺参数同实施例1。 (3) Coating preparation: The substrate negative bias voltage was 400V during coating deposition, and other process parameters were the same as in Example 1.
涂层沉积速率为112.8 nm/min,涂层为γ-Ni,CrN和AlN相。涂层的含氮量为14.01 at.%, Al和Cr的含量分别为14.91 at.%和17.87 at.%。涂层的硬度为824.7 HV25gf,加载10N时涂层的磨损量为8.46×10-3mm3/m。样品经1000oC恒温氧化100h微观结构如图3所示,涂层表面生成了一层很薄的连续致密的氧化铝膜,氧化膜厚度为:1.25μm,100h样品单位面积氧化增重:0.33mg/cm2。 The deposition rate of the coating is 112.8 nm/min, and the coating is γ-Ni, CrN and AlN phases. The nitrogen content of the coating is 14.01 at.%, and the Al and Cr contents are 14.91 at.% and 17.87 at.%, respectively. The hardness of the coating is 824.7 HV 25gf , and the wear amount of the coating is 8.46×10 -3 mm 3 /m when the load is 10N. The microstructure of the sample was oxidized at 1000 o C for 100 hours, as shown in Figure 3. A thin continuous and dense aluminum oxide film was formed on the coating surface. mg/cm 2 .
实施例5 Example 5
以镍基高温合金K417为基体,采用多弧离子镀技术为该陶瓷涂层的制备方法,其制备工艺如下: The nickel-based superalloy K417 is used as the substrate, and the multi-arc ion plating technology is used as the preparation method of the ceramic coating. The preparation process is as follows:
(1) 合金靶材的制备同实施例1; (1) The preparation of the alloy target is the same as in Example 1;
(2) 零件前处理同实施例1; (2) Part pretreatment is the same as embodiment 1;
(3) 涂层制备:涂层沉积时N2流量为300sccm,其他工艺参数同实施例1。 (3) Coating preparation: N flow during coating deposition was 300 sccm, and other process parameters were the same as in Example 1.
涂层沉积速率为236.7 nm/min,涂层为γ-Ni,CrN和AlN相。涂层的含氮量为20.08 at.%, Al和Cr的含量分别为10.97 at.%和18.64 at.%。涂层的硬度为787.4 HV25gf,加载10N时涂层的磨损量为8.78×10-3mm3/m。样品经1000oC恒温氧化100h,涂层表面生成了一层很薄的连续致密的氧化铝膜,样品单位面积氧化增重:0.45mg/cm2。 The deposition rate of the coating is 236.7 nm/min, and the coating is γ-Ni, CrN and AlN phases. The nitrogen content of the coating is 20.08 at.%, and the Al and Cr contents are 10.97 at.% and 18.64 at.%, respectively. The hardness of the coating is 787.4 HV 25gf , and the wear amount of the coating is 8.78×10 -3 mm 3 /m when the load is 10N. After the sample was oxidized at a constant temperature of 1000 o C for 100 hours, a thin continuous and dense aluminum oxide film was formed on the surface of the coating, and the oxidation weight gain per unit area of the sample was 0.45mg/cm 2 .
实施例6 Example 6
以镍基高温合金K417为基体,采用多弧离子镀技术为该陶瓷涂层的制备方法,其制备工艺如下: The nickel-based superalloy K417 is used as the substrate, and the multi-arc ion plating technology is used as the preparation method of the ceramic coating. The preparation process is as follows:
(1) 合金靶材的制备同实施例1; (1) The preparation of the alloy target is the same as in Example 1;
(2) 零件前处理同实施例1; (2) Part pretreatment is the same as embodiment 1;
(3) 涂层制备:沉积时间为5h,其他工艺参数同实施例1。 (3) Coating preparation: the deposition time is 5h, and other process parameters are the same as in Example 1.
涂层厚度为28μm。在1000oC预氧化1h后,涂层经涂25%NaCl+75%Na2SO4(wt.%)盐,涂盐量为1.5-2.5 mg/cm2,900oC热腐蚀试验80h后氧化膜厚度为3.3μm,显微结构照片如图4所示,涂层表面生成单一的氧化铝膜。80h样品单位面积增重:0.27mg/cm2。试验100h后氧化膜厚度为4.5μm,因涂层中的Al大量消耗,不足以形成连续的保护性氧化铝膜,Cr向外扩散生成氧化铬,生成的氧化膜形成外层为氧化铬,内层为氧化铝的双层结构。100h样品单位面积增重:1.7mg/cm2。 The coating thickness was 28 μm. After pre-oxidation at 1000 o C for 1 hour, the coating was coated with 25%NaCl+75%Na 2 SO 4 (wt.%) salt, the amount of salt applied was 1.5-2.5 mg/cm 2 , after 80 hours of hot corrosion test at 900 o C The thickness of the oxide film is 3.3 μm, and the microstructure photo is shown in Figure 4. A single aluminum oxide film is formed on the surface of the coating. Weight gain per unit area of sample at 80h: 0.27mg/cm 2 . After 100 hours of testing, the thickness of the oxide film was 4.5 μm. Due to the large consumption of Al in the coating, it was not enough to form a continuous protective aluminum oxide film. Cr diffused outwards to form chromium oxide, and the outer layer of the formed oxide film was chromium oxide. The layer is a double-layer structure of alumina. 100h sample weight gain per unit area: 1.7mg/cm 2 .
实施例7 Example 7
以马氏体耐热钢1Cr16Ni2MoN为基体,采用多弧离子镀技术为该陶瓷涂层的制备方法,其制备工艺同实施例2。 The martensitic heat-resistant steel 1Cr16Ni2MoN is used as the substrate, and the multi-arc ion plating technology is used as the preparation method of the ceramic coating, and the preparation process is the same as that in Example 2.
将CrN涂层与所制备的金属陶瓷涂层进行抗裂性比较,将样品在800oC进行热震试验,保温10min后取出淬火,热震14次发现,镀有CrN涂层的样品表面边角处出现剥落现象,而镀有金属陶瓷涂层的试样未出现剥落现象。将样品在1000oC进行热震试验,保温10min后取出淬火。每隔两次试验对样品进行称重,通过光学显微镜观察发现,经过一次热震后CrN涂层表面出现严重的剥落现象,而本发明所制备的金属陶瓷涂层经过十次热震后涂层表面未出现剥落现象。镀有CrN涂层的样品经过2次和10次热震后涂层单位面积质量变化分别为:0.0144mg/cm2和-0.3515 mg/cm2。 镀有该金属陶瓷涂层的样品经过2次和10次热震后涂层单位面积质量变化分别为为:0.0091mg/cm2和0.0401 mg/cm2。 The crack resistance of the CrN coating was compared with that of the prepared cermet coating. The sample was subjected to a thermal shock test at 800 o C. After holding for 10 minutes, it was taken out and quenched. After 14 thermal shocks, it was found that the surface edge of the sample coated with CrN coating was The peeling phenomenon appeared at the corner, but the sample coated with cermet coating did not appear peeling phenomenon. The sample was subjected to a thermal shock test at 1000 o C, and after 10 minutes of heat preservation, it was taken out and quenched. The sample is weighed every two tests, and it is found by optical microscope observation that serious peeling occurs on the surface of the CrN coating after one thermal shock, while the cermet coating prepared by the present invention is coated after ten thermal shocks. There is no peeling phenomenon on the surface. After 2 and 10 thermal shocks, the mass changes per unit area of the CrN-coated samples were 0.0144 mg/cm 2 and -0.3515 mg/cm 2 , respectively. After 2 and 10 thermal shocks, the mass changes per unit area of the samples coated with the cermet coating were 0.0091 mg/cm 2 and 0.0401 mg/cm 2 respectively.
实施例8 Example 8
以镍基高温合金K438为基体,采用磁控溅射技术为该陶瓷涂层的制备方法,其制备工艺如下: The nickel-based superalloy K438 is used as the substrate, and the magnetron sputtering technology is used as the preparation method of the ceramic coating. The preparation process is as follows:
(1) 合金靶材的制备同实施例1; (1) The preparation of the alloy target is the same as in Example 1;
(2) 零件前处理同实施例1; (2) Part pretreatment is the same as embodiment 1;
(3) 涂层制备:以氮气(纯度为99.99%)为反应气体,以氩气(纯度为99.99%)为溅射气体。将零件放入磁控溅射反应腔内,腔内真空度达到6×10-3Pa,腔体加热到200oC,对基体刻蚀30min后开始沉积。工艺参数为:溅射压力为0.20Pa,基体偏压为300V,靶基距离为150mm,N2流量为450 sccm,溅射功率为2kw,沉积时间为4h。 (3) Coating preparation: Nitrogen (purity: 99.99%) is used as the reaction gas, and argon (purity: 99.99%) is used as the sputtering gas. Put the parts into the magnetron sputtering reaction chamber, the vacuum degree in the chamber reaches 6×10 -3 Pa, the chamber is heated to 200 o C, and the substrate is etched for 30 minutes before deposition. The process parameters are: the sputtering pressure is 0.20Pa, the substrate bias is 300V, the target-substrate distance is 150mm, the N 2 flow rate is 450 sccm, the sputtering power is 2kw, and the deposition time is 4h.
涂层沉积速率为62.5 nm/min,涂层以柱状晶的形式存在,为γ-Ni,CrN和AlN相。涂层的含氮量为14.40 at.%, Al和Cr的含量分别为16.88 at.%和16.95 at.%。涂层的硬度为981.2 HV25gf,加载10N时涂层的磨损量为6.67×10-3mm3/m。样品经1000oC恒温氧化100h,涂层表面生成了一层很薄的连续致密的氧化铝膜,样品单位面积氧化增重:0.41mg/cm2。 The deposition rate of the coating is 62.5 nm/min, and the coating exists in the form of columnar crystals, which are γ-Ni, CrN and AlN phases. The nitrogen content of the coating is 14.40 at.%, and the Al and Cr contents are 16.88 at.% and 16.95 at.%, respectively. The hardness of the coating is 981.2 HV 25gf , and the wear amount of the coating is 6.67×10 -3 mm 3 /m when the load is 10N. After the sample was oxidized at a constant temperature of 1000 o C for 100 hours, a thin continuous and dense aluminum oxide film was formed on the surface of the coating, and the oxidation weight gain per unit area of the sample was 0.41mg/cm 2 .
实施例9 Example 9
以镍基高温合金K417为基体,采用磁控溅射技术为该陶瓷涂层的制备方法,其制备工艺同实施例8。 The nickel-based superalloy K417 is used as the substrate, and the magnetron sputtering technology is used as the preparation method of the ceramic coating, and the preparation process is the same as that in Example 8.
涂层沉积速率为59.5 nm/min,涂层以柱状晶的形式存在,为γ-Ni,CrN和AlN相。涂层的含氮量为14.82 at.%, Al和Cr的含量分别为15.97 at.%和17.05 at.%。涂层的硬度为984.2 HV25gf,加载10N时涂层的磨损量为6.83×10-3mm3/m。样品经1000oC恒温氧化100h,涂层表面生成了一层很薄的连续致密的氧化铝膜,样品单位面积氧化增重:0.43mg/cm2。 The deposition rate of the coating is 59.5 nm/min, and the coating exists in the form of columnar crystals, which are γ-Ni, CrN and AlN phases. The nitrogen content of the coating is 14.82 at.%, and the Al and Cr contents are 15.97 at.% and 17.05 at.%, respectively. The hardness of the coating is 984.2 HV 25gf , and the wear amount of the coating is 6.83×10 -3 mm 3 /m when the load is 10N. After the sample was oxidized at a constant temperature of 1000 o C for 100 hours, a thin continuous and dense aluminum oxide film was formed on the surface of the coating, and the oxidation weight gain per unit area of the sample was 0.43mg/cm 2 .
Claims (2)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201010580583.1A CN102560338B (en) | 2010-12-09 | 2010-12-09 | A kind of cermet coating and preparation method thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201010580583.1A CN102560338B (en) | 2010-12-09 | 2010-12-09 | A kind of cermet coating and preparation method thereof |
Publications (2)
Publication Number | Publication Date |
---|---|
CN102560338A CN102560338A (en) | 2012-07-11 |
CN102560338B true CN102560338B (en) | 2014-01-08 |
Family
ID=46406929
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201010580583.1A Expired - Fee Related CN102560338B (en) | 2010-12-09 | 2010-12-09 | A kind of cermet coating and preparation method thereof |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN102560338B (en) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103184451B (en) * | 2013-03-28 | 2015-08-05 | 常州大学 | A kind of preparation technology of anti-oxidant conductive spinel coating |
KR20160092357A (en) * | 2015-01-27 | 2016-08-04 | 삼성전자주식회사 | Amorphous and nano nitride composite thin film, method for forming the same and electronic divice with the same |
CN108796461B (en) * | 2018-06-20 | 2020-12-11 | 暨南大学 | A composite metal-ceramic coating for high temperature alloy protection and preparation method thereof |
CN112663001B (en) * | 2020-12-14 | 2022-07-01 | 中国兵器工业第五九研究所 | A kind of titanium alloy blade protective coating and preparation method thereof |
CN114277350A (en) * | 2021-12-28 | 2022-04-05 | 东北大学 | A kind of nanometer high temperature protective coating with stable structure and preparation method thereof |
CN115323324B (en) * | 2022-07-28 | 2024-12-13 | 中国科学院金属研究所 | A wear-resistant, corrosion-resistant, and oxidation-resistant fiber crystal chromium-nitrogen thick film and preparation method thereof |
CN115368166A (en) * | 2022-07-29 | 2022-11-22 | 中国航发北京航空材料研究院 | Ceramic microsphere coated nickel coating and preparation method thereof |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1791692A (en) * | 2003-05-20 | 2006-06-21 | 埃克森美孚研究工程公司 | Erosion-corrosion resistant nitride cermets |
CN101230448A (en) * | 2008-01-31 | 2008-07-30 | 沈阳大学 | Preparation method of multi-component superhard reaction film of titanium-aluminum-chromium-silicon-yttrium-nitride multi-arc ion plating |
-
2010
- 2010-12-09 CN CN201010580583.1A patent/CN102560338B/en not_active Expired - Fee Related
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1791692A (en) * | 2003-05-20 | 2006-06-21 | 埃克森美孚研究工程公司 | Erosion-corrosion resistant nitride cermets |
CN101230448A (en) * | 2008-01-31 | 2008-07-30 | 沈阳大学 | Preparation method of multi-component superhard reaction film of titanium-aluminum-chromium-silicon-yttrium-nitride multi-arc ion plating |
Also Published As
Publication number | Publication date |
---|---|
CN102560338A (en) | 2012-07-11 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN102560338B (en) | A kind of cermet coating and preparation method thereof | |
JP3124966B2 (en) | Manufacturing method of thermal protection film | |
CN103409722B (en) | Method for preparing anti-erosion coating on surface of aero engine air compressor blade | |
CN101230448B (en) | Preparation method of multi-component superhard reaction film of titanium-aluminum-chromium-silicon-yttrium-nitride multi-arc ion plating | |
CN104928638A (en) | AlCrSiN-based multilayer nanometer composite cutter coating layer and preparation method thereof | |
CN104401089B (en) | High-temperature coating comprising nickel-chromium-oxygen active diffusion barrier layer and preparation method | |
KR20070067607A (en) | High Strength Ni-Plat-Al-Hf Bond Coating | |
CN108359927B (en) | NiCr/Al2O3Preparation method of composite coating | |
CN104278234B (en) | Preparation technology for self-lubricating coating with wide temperature range of room temperature to 800 DEG C | |
Badini et al. | Cyclic oxidation in burner rig of TiAlN coating deposited on Ti-48Al-2Cr-2Nb by reactive HiPIMS | |
CN101307424B (en) | Process for preparing zirconia coating | |
CN106756819A (en) | A kind of MCrAlY high-temperature protection coatings preparation method | |
CN111560584A (en) | High-performance thermal barrier coating of aero-engine blade and multi-process combined preparation method | |
CN101698363A (en) | TiN/(TiN+CrN)/CrAlN nano composite coating and preparation method thereof | |
CN101787516A (en) | MCrAlY coating with excellent oxidation resistance and preparation method thereof | |
CN110241387A (en) | A preparation method of CrAlN coating based on HIPIMS technology | |
CN106868450A (en) | A kind of utilization modulates the method that high-power impulse magnetron sputtering prepares AlTiN hard coats | |
CN112663001B (en) | A kind of titanium alloy blade protective coating and preparation method thereof | |
CN112981325B (en) | Thermal protection coating and preparation method and application thereof | |
CN108823544A (en) | Based on nitridation titanium compound film and preparation method thereof | |
CN209024637U (en) | A kind of nitridation titanium compound film | |
CN103614698B (en) | A kind of High-temperature antioxidant niobium alloy compound coating and preparation method thereof | |
CN111485204A (en) | Method for preparing anti-solid particle erosion ceramic coating by using plasma | |
CN115522169B (en) | Composite deposition method of oxide hard coating and coated cutter | |
CN106119796A (en) | A kind of preparation method of amorphous diamond coatings |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140108 |
|
CF01 | Termination of patent right due to non-payment of annual fee |