CN104372283A - Plasma sprayed TiN coating layer having relatively good hardness and toughness - Google Patents
Plasma sprayed TiN coating layer having relatively good hardness and toughness Download PDFInfo
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- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 title claims abstract description 79
- 239000011247 coating layer Substances 0.000 title 1
- 238000000576 coating method Methods 0.000 claims abstract description 116
- 239000011248 coating agent Substances 0.000 claims abstract description 113
- 239000000843 powder Substances 0.000 claims abstract description 41
- 239000002245 particle Substances 0.000 claims abstract description 16
- 238000005054 agglomeration Methods 0.000 claims abstract description 12
- 230000002776 aggregation Effects 0.000 claims abstract description 12
- 239000011148 porous material Substances 0.000 claims abstract description 8
- OGIDPMRJRNCKJF-UHFFFAOYSA-N titanium oxide Inorganic materials [Ti]=O OGIDPMRJRNCKJF-UHFFFAOYSA-N 0.000 claims abstract description 8
- 239000000758 substrate Substances 0.000 claims abstract description 7
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 claims abstract description 6
- 238000009826 distribution Methods 0.000 claims abstract description 6
- 230000007547 defect Effects 0.000 claims abstract description 5
- 238000005507 spraying Methods 0.000 claims description 32
- 238000000034 method Methods 0.000 claims description 21
- 239000007789 gas Substances 0.000 claims description 13
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims description 12
- 239000007921 spray Substances 0.000 claims description 9
- 238000002360 preparation method Methods 0.000 claims description 7
- 229910052786 argon Inorganic materials 0.000 claims description 6
- 229910010413 TiO 2 Inorganic materials 0.000 claims description 4
- 239000011230 binding agent Substances 0.000 claims description 3
- 239000001257 hydrogen Substances 0.000 claims description 3
- 229910052739 hydrogen Inorganic materials 0.000 claims description 3
- 239000002994 raw material Substances 0.000 claims description 3
- 238000000889 atomisation Methods 0.000 claims description 2
- 238000001035 drying Methods 0.000 claims 1
- 125000004435 hydrogen atom Chemical class [H]* 0.000 claims 1
- 238000002156 mixing Methods 0.000 claims 1
- 238000007750 plasma spraying Methods 0.000 abstract description 10
- 238000007373 indentation Methods 0.000 description 8
- 238000005516 engineering process Methods 0.000 description 7
- 238000005229 chemical vapour deposition Methods 0.000 description 6
- 238000005240 physical vapour deposition Methods 0.000 description 6
- 238000002441 X-ray diffraction Methods 0.000 description 5
- 239000000463 material Substances 0.000 description 5
- 238000012360 testing method Methods 0.000 description 5
- 238000006243 chemical reaction Methods 0.000 description 4
- 238000005488 sandblasting Methods 0.000 description 4
- 238000007751 thermal spraying Methods 0.000 description 4
- 238000005260 corrosion Methods 0.000 description 3
- 230000007797 corrosion Effects 0.000 description 3
- 238000000151 deposition Methods 0.000 description 3
- 230000008021 deposition Effects 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 238000011160 research Methods 0.000 description 3
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000011068 loading method Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000003647 oxidation Effects 0.000 description 2
- 238000007254 oxidation reaction Methods 0.000 description 2
- 238000007747 plating Methods 0.000 description 2
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 238000005524 ceramic coating Methods 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 229910052593 corundum Inorganic materials 0.000 description 1
- 239000010431 corundum Substances 0.000 description 1
- 238000007656 fracture toughness test Methods 0.000 description 1
- 239000008187 granular material Substances 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 150000002431 hydrogen Chemical class 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 230000035755 proliferation Effects 0.000 description 1
- 238000001878 scanning electron micrograph Methods 0.000 description 1
- 238000001228 spectrum Methods 0.000 description 1
- 239000013077 target material Substances 0.000 description 1
Classifications
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
- C23C4/10—Oxides, borides, carbides, nitrides or silicides; Mixtures thereof
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Coating By Spraying Or Casting (AREA)
Abstract
一种硬度和韧性较好的等离子喷涂TiN涂层,本发明公开了一种TiN团聚粉沫,该粉末包括原子分数为Ti-72%和N-28%,其团聚后形成粒径为40~80μm球状团聚体。本发明还提供了一种TiN涂层,该TiN涂层是由TiN团聚粉末制备得到;该涂层的三强峰相为TiN相,还存在部分TiO、TiO2和Ti3O氧化物相;该涂层中存在明暗相层状分布,在层状结构内部和层状结构结合处有少量孔隙;涂层与基体结合处无裂纹等微观缺陷,结合良好。本发明采用超音速等离子喷涂TiN涂层,硬度较高,可以达到1210HV0.1,高的硬度可以提高涂层的耐磨性,涂层的断裂韧性较大,可以提高涂层内断裂力学性能,延长涂层的疲劳寿命。
A plasma-sprayed TiN coating with good hardness and toughness. The invention discloses a TiN agglomerated powder. The powder includes atomic fractions of Ti-72% and N-28%, and the particle size formed after agglomeration is 40~ 80 μm spherical aggregates. The present invention also provides a TiN coating, which is prepared from TiN agglomerated powder; the three-peak phase of the coating is the TiN phase, and there are also some TiO, TiO2 and Ti3O oxide phases; the coating There is a layered distribution of light and dark phases in the coating, and there are a small amount of pores inside the layered structure and at the junction of the layered structure; there are no microscopic defects such as cracks at the junction of the coating and the substrate, and the combination is good. The invention adopts supersonic plasma spraying TiN coating, the hardness is high, can reach 1210HV 0.1 , the high hardness can improve the wear resistance of the coating, the fracture toughness of the coating is large, can improve the fracture mechanical properties of the coating, prolong the Coating fatigue life.
Description
技术领域 technical field
本发明涉及材料技术研究领域,具体的涉及一种等离子涂层。 The invention relates to the field of material technology research, in particular to a plasma coating. the
背景技术 Background technique
TiN涂层具有低的摩擦系数和高的硬度,以及良好的耐腐蚀性被广泛应用为装饰涂层、耐磨涂层、耐腐蚀涂层。目前,许多研究者通过反应热喷涂、化学气相沉积(CVD)、物理气相沉积(PVD)、电弧镀、等技术制备了TiN涂层,并对涂层的沉积过程,显微结构和性能进行了研究。采用CVD、PVD等技术制备的TiN涂层厚度较薄,降低涂层的机械性能;而利用热喷涂反应技术可以制备较厚的TiN涂层,但涂层内含有较多的孔隙,脆性较大,涂层质量不易控制。采用等离子喷技术直接喷涂TiN粉末可以在短时间内制备较厚的涂层,同时在喷涂过程TiN发生氧化,产生Ti的氧化物相,可以提高涂层的韧性。 TiN coating has low coefficient of friction, high hardness, and good corrosion resistance, and is widely used as decorative coating, wear-resistant coating, and corrosion-resistant coating. At present, many researchers have prepared TiN coatings by reactive thermal spraying, chemical vapor deposition (CVD), physical vapor deposition (PVD), arc plating, etc. Research. The thickness of the TiN coating prepared by CVD, PVD and other technologies is thin, which reduces the mechanical properties of the coating; while the thermal spraying reaction technology can be used to prepare a thicker TiN coating, but the coating contains more pores and is more brittle. , The coating quality is not easy to control. The direct spraying of TiN powder by plasma spraying technology can prepare a thicker coating in a short time. At the same time, TiN is oxidized during the spraying process to produce Ti oxide phase, which can improve the toughness of the coating. the
等离子喷涂技术被广泛应用于制备金属、陶瓷和复合涂层以抵抗磨损、腐蚀和高温。在喷涂过程中,易产生氧化物和孔隙等微观缺陷,这是由于熔融颗粒在熔化和飞行以及与基体表面接触过程中与周围介质发生了化学反应,使得喷涂材料出现氧化,而且还由于熔融颗粒的陆续堆叠和部分颗粒的反弹散失,在颗粒之间不可避免的出现孔隙。涂层内氧化物含量和孔隙率等微观缺陷是评判涂层质量的重要标准,有学者对等离子喷涂过程中氧化物的控制和孔隙率对涂层性能的影响进行了研究,通过控制合适的工艺参数能够显著改善涂层的微观结构和性能。TiN高温下易分解氧化,的活性较大,在等离子喷涂过程中与其它介质反应生成Ti的氧化物,Ti的氧化物相相比TiN相硬度和强度较低,TiN涂层内氧化物含量直接影响了涂层性能。断裂韧性是材料抵抗断裂破坏的能力,采用压痕法对涂层断裂韧性的测量已得到广泛应用,涂层硬度和断裂韧性是涂层抵抗裂纹增殖和发生断裂的主要指标,直接影响了涂层的服役性能和 寿命。 Plasma spraying technology is widely used to prepare metal, ceramic and composite coatings to resist wear, corrosion and high temperature. During the spraying process, it is easy to produce microscopic defects such as oxides and pores. This is due to the chemical reaction of the molten particles with the surrounding medium during melting and flight and contact with the surface of the substrate, which makes the sprayed material oxidized, and also due to the molten particles. The continuous stacking and the rebound of some particles are lost, and pores inevitably appear between the particles. Microscopic defects such as oxide content and porosity in the coating are important criteria for judging the quality of the coating. Some scholars have studied the influence of oxide control and porosity on the performance of the coating during the plasma spraying process. By controlling the appropriate process parameter can significantly improve the microstructure and properties of the coating. TiN is easy to decompose and oxidize at high temperature, and has a high activity. It reacts with other media to form Ti oxides during the plasma spraying process. The Ti oxide phase has lower hardness and strength than the TiN phase, and the oxide content in the TiN coating is directly affect the coating performance. Fracture toughness is the ability of materials to resist fracture damage. The measurement of coating fracture toughness by indentation method has been widely used. Coating hardness and fracture toughness are the main indicators of coating resistance to crack proliferation and fracture, which directly affect the coating. service performance and lifespan. the
目前,许多研究者通过反应热喷涂、化学气相沉积(CVD)、物理气相沉积(PVD)、电弧镀、等技术制备了TiN涂层,并对涂层的沉积过程,显微结构和性能进行了研究。采用CVD、PVD等技术制备的TiN涂层厚度较薄,降低涂层的机械性能;而利用热喷涂反应技术可以制备较厚的TiN涂层,但涂层内含有较多的孔隙,脆性较大,涂层质量不易控制。而采用等离子直接喷涂TiN粉末,即可以保证涂层的厚度,同时,TiN涂层内Ti的氧化物相可以提高涂层的韧性,从而得到韧性和硬度都较好的TiN涂层。 At present, many researchers have prepared TiN coatings by reactive thermal spraying, chemical vapor deposition (CVD), physical vapor deposition (PVD), arc plating, etc. Research. The thickness of the TiN coating prepared by CVD, PVD and other technologies is thin, which reduces the mechanical properties of the coating; while the thermal spraying reaction technology can be used to prepare a thicker TiN coating, but the coating contains more pores and is more brittle. , The coating quality is not easy to control. The direct spraying of TiN powder by plasma can ensure the thickness of the coating. At the same time, the oxide phase of Ti in the TiN coating can improve the toughness of the coating, thus obtaining a TiN coating with better toughness and hardness. the
发明内容 Contents of the invention
为了解决上述问题,本发明的目的是提供一种TiN涂层。 In order to solve the above problems, the object of the present invention is to provide a TiN coating. the
为了实现本发明的目的,本发明提供了一种TiN团聚粉沫,该粉末包括原子分数为Ti-72%和N-28%,其团聚后形成粒径为40~80μm球状团聚体。 In order to realize the object of the present invention, the present invention provides a kind of TiN agglomeration powder, and this powder comprises atomic fraction is Ti-72% and N-28%, after its agglomeration forms spherical agglomerate with particle diameter of 40-80 μ m. the
进一步地,本发明还提供了一种TiN涂层,该TiN涂层是由TiN团聚粉沫制备得到。 Further, the present invention also provides a TiN coating, which is prepared from TiN agglomerated powder. the
并且,该涂层的三强峰相为TiN相,还存在部分TiO、TiO2和Ti3O氧化物相;该涂层中存在明暗相层状分布,在层状结构内部和层状结构结合处有少量孔隙;涂层与基体结合处无裂纹等微观缺陷,结合良好。 Moreover, the three-peak phase of the coating is the TiN phase, and there are also some TiO, TiO2 and Ti3O oxide phases; there is a layered distribution of light and dark phases in the coating, and a small amount of Pores; there are no microscopic defects such as cracks at the junction of the coating and the substrate, and the combination is good. the
优选地,所述的TiN涂层是由以下方法制备: Preferably, the TiN coating is prepared by the following method:
一种制备TiN涂层的方法,其包括如下步骤: A method for preparing a TiN coating, comprising the steps of:
(1)制备TiN团聚粉末:该粉末包括原子分数为Ti-72%和N-28%,其团聚后形成粒径为40~80μm球状团聚体; (1) Preparation of TiN agglomerated powder: the powder includes atomic fractions of Ti-72% and N-28%, which form spherical aggregates with a particle size of 40-80 μm after agglomeration;
(2)模具表面预处理; (2) Mold surface pretreatment;
(3)喷涂:利用等离子喷枪进行喷涂,喷涂参数为,喷涂主气为氩气,气体流量为38L·min-1-42L·min-1;次气为氢气气体流量为12L·min-1-16L·min-1;送粉气为氩气,喷涂距离为100-140mm;送粉量为40g·min-1,喷涂电压为41KW-50KW;喷涂电流为500A-600A; (3) Spraying: Utilize a plasma spray gun for spraying, the spraying parameters are, the main gas for spraying is argon, the gas flow rate is 38L·min −1 -42L·min −1 ; the secondary gas is hydrogen, and the gas flow rate is 12L·min −1 −1 16L·min -1 ; the powder feeding gas is argon, the spraying distance is 100-140mm; the powder feeding amount is 40g·min -1 , the spraying voltage is 41KW-50KW; the spraying current is 500A-600A;
(4)制得TiN涂层:该涂层三强峰相为TiN相,还存在部分TiO、TiO2 和Ti3O氧化物相。 (4) Preparation of TiN coating: the three-peak phase of the coating is TiN phase, and part of TiO, TiO 2 and Ti 3 O oxide phases also exist.
其中,所述TiN团聚粉沫是由以下方法制备: Wherein, the TiN agglomerated powder is prepared by the following method:
(1-1)TiN粉末原料进行雾化; (1-1) TiN powder raw material is atomized;
(1-2)对雾化后的TiN粉末和粘结剂进行混料加入到团聚设备内进行团聚,并对团聚后的粉末进行干燥,冷却; (1-2) The atomized TiN powder and binder are mixed and added to the agglomeration equipment for agglomeration, and the agglomerated powder is dried and cooled;
(1-3)将团聚后的粉末通过-200目~400目粉末筛,得到的TiN团聚粉末粒径为40-80微米球状团聚体。 (1-3) Pass the agglomerated powder through a powder sieve of -200 mesh to 400 mesh, and the obtained TiN agglomerated powder has a particle size of 40-80 micron spherical agglomerates. the
本发明的有益效果如下: The beneficial effects of the present invention are as follows:
本发明直接对TiN粉末进行喷涂,可以再零件表面直接制备耐磨陶瓷涂层,涂层中Ti氧化物的出现,提高了涂层的韧性。直接喷涂TiN涂层可以避免传统的采用反应喷涂TiN层较大的脆性和工艺复杂,需要较多的人力和物力资源。 The invention directly sprays the TiN powder, and can directly prepare a wear-resistant ceramic coating on the surface of the part, and the appearance of Ti oxide in the coating improves the toughness of the coating. Direct spraying of TiN coating can avoid the greater brittleness and complicated process of traditional reaction spraying TiN layer, which requires more manpower and material resources. the
本发明采用超音速喷涂TiN涂层,涂层较致密,有少量空隙,与基体结合良好,厚度约200μm,采用压痕法测量涂层断裂韧性为 The present invention adopts supersonic spraying TiN coating, the coating is denser, has a small amount of voids, is well combined with the substrate, and has a thickness of about 200 μm. The fracture toughness of the coating is measured by indentation method as
本发明采用等离子喷涂TiN粉末制备的TiN涂层,该方法可以采用粉末直接喷涂,操作方便,易于推广,大大的节约了成本。 The invention adopts the TiN coating prepared by plasma spraying TiN powder, and the method can be directly sprayed by powder, which is convenient to operate, easy to popularize, and greatly saves cost. the
本发明采用超音速等离子喷涂TiN涂层,硬度较高,可以达到1210HV0.1,高的硬度可以提高涂层的耐磨性,涂层的断裂韧性较大,可以提高涂层内断裂力学性能,延长涂层的疲劳寿命。 The invention adopts supersonic plasma spraying TiN coating, the hardness is high, can reach 1210HV 0.1 , the high hardness can improve the wear resistance of the coating, the fracture toughness of the coating is large, can improve the fracture mechanical properties of the coating, prolong the Coating fatigue life.
附图说明 Description of drawings
图1本发明实施例1制得的TiN涂层; The TiN coating that Fig. 1 embodiment of the present invention 1 makes;
图2涂层的XRD测试结果; The XRD test result of Fig. 2 coating;
图3涂层的SEM扫描形貌; The SEM scanning morphology of the coating in Fig. 3;
图4涂层硬度测试结果; Fig. 4 coating hardness test result;
图5断裂韧性测试压痕形貌; Figure 5 Fracture toughness test indentation morphology;
图6不同孔隙率对涂层硬度的影响; The influence of Fig. 6 different porosity on coating hardness;
图7不同氧化物含量对涂层断裂韧性的影响。 Figure 7 Effect of different oxide contents on the fracture toughness of the coating. the
具体实施方式 Detailed ways
下面结合附图及其具体实施方式详细介绍本发明。但本发明的保护范围并不局限于以下实例,应包含权利要求书中的全部内容。 The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments thereof. But the scope of protection of the present invention is not limited to the following examples, and should include all content in the claims. the
以下实施例中所使用的均为常规仪器和设备。 All used in the following examples are conventional instruments and equipment. the
实施例1涂层的制备 The preparation of embodiment 1 coating
涂层的制备过程分为制备TiN团聚粉末,模具表面预处理,喷涂参数优化,喷涂四个阶段,四个阶段步骤如下: The preparation process of the coating is divided into four stages: preparation of TiN agglomerated powder, mold surface pretreatment, spraying parameter optimization, and spraying. The steps of the four stages are as follows:
(1)制备TiN团聚粉末; (1) Prepare TiN agglomerated powder;
(1-1)以粉末粒径为1-5μm的TiN粉末为原料进行雾化; (1-1) Atomize TiN powder with a particle size of 1-5 μm as raw material;
(1-2)对雾化后的TiN粉末和粘结剂进行混料加入到雾化设备内进行团聚,并对团聚后的粉末进行干燥,造粒成形; (1-2) Mix the atomized TiN powder and binder into the atomization equipment for agglomeration, dry the agglomerated powder, and granulate;
(1-3)将团聚后的粉末通过-200目~+400目粉末筛,得到的TiN团聚粉末粒径为40-80微米的微米球状团聚体。 (1-3) passing the agglomerated powder through a -200 mesh to +400 mesh powder sieve to obtain a TiN agglomerated powder with a particle size of 40-80 micron micron spherical agglomerates. the
该粉末包括原子分数为Ti-72%和N-28%,其团聚后形成粒径为40~80μm球状团聚体。 The powder includes atomic fractions of Ti-72% and N-28%, and after agglomeration, spherical agglomerates with a particle diameter of 40-80 μm are formed. the
(2)模具表面预处理; (2) Mold surface pretreatment;
(2-1)对模具表面首先进行磨削处理,使模具表面的粗糙度达到Ra=0.8μm; (2-1) Grinding the mold surface first, so that the roughness of the mold surface reaches Ra=0.8μm;
(2-2)然后对模具表面进行酒精或丙酮清洗,去除模具表面的油污; (2-2) Carry out alcohol or acetone cleaning to mold surface then, remove the oil stain on mold surface;
(2-3)对模具表面进行喷砂处理,喷砂材料选用粒径小于700μm的棕刚玉,喷砂气压为0.7MPa,喷砂角度为45°,喷枪离模具表面距离为0.15m。 (2-3) Perform sandblasting on the surface of the mold. The sandblasting material is brown corundum with a particle size of less than 700 μm. The sandblasting air pressure is 0.7MPa, the sandblasting angle is 45°, and the distance between the spray gun and the mold surface is 0.15m. the
(3)喷涂 (3) Spraying
(3-1)喷涂设备采用超音速等离子喷枪,喷涂参数为,喷涂主气为氩气(38L·min-1),次气为氢气(16L·min-1),送粉气为氩气,喷涂距离为125mm,送粉量为40g·min-1,喷涂电压为46KW,喷涂电流为540A; (3-1) The spraying equipment adopts a supersonic plasma spray gun, and the spraying parameters are as follows: the main spraying gas is argon (38L·min -1 ), the secondary gas is hydrogen (16L·min -1 ), and the powder feeding gas is argon, The spraying distance is 125mm, the powder feeding volume is 40g·min -1 , the spraying voltage is 46KW, and the spraying current is 540A;
(3-2)在喷涂参数下,利用超音速等离子喷枪对工件表面进行喷涂,扫描过程采用“井”字扫描,扫描速度为1.25m/min; (3-2) Under the spraying parameters, use a supersonic plasma spray gun to spray on the surface of the workpiece. The scanning process uses "well" character scanning, and the scanning speed is 1.25m/min;
(3-3)根据沉积速度对工件表面进行4~6次“井”字扫描,得到厚度约为200μm厚度的涂层; (3-3) Carry out 4 to 6 "well" scans on the surface of the workpiece according to the deposition rate to obtain a coating with a thickness of about 200 μm;
(4)制得TiN涂层 (4) Prepare TiN coating
(4-1)TiN粉末熔点约为2950℃,喷涂粉末TiN团聚粉末在等离子束的高温下熔化,超音速等离子喷涂设备可以使熔化粉末具有高的飞行速度,可以形成较致密的涂层; (4-1) The melting point of TiN powder is about 2950°C. Spray powder TiN agglomerated powder is melted at the high temperature of the plasma beam. The supersonic plasma spraying equipment can make the molten powder have a high flying speed and form a denser coating;
(4-2)喷涂粉末由于沉积到基体上,熔化颗粒在飞行过程中,与周围的空气发生了反应,产生了氧化,生成了TiO,Ti3O,TiO2氧化物,Ti的氧化物相比TiN相强度和硬度较低,可以提高涂层的韧性。 (4-2) Due to the deposition of the spray powder on the substrate, the molten particles reacted with the surrounding air during the flight, resulting in oxidation, and formed TiO, Ti 3 O, TiO 2 oxides, Ti oxide phases It has lower strength and hardness than TiN phase, which can improve the toughness of the coating.
制得的TiN涂层如图1所示,涂层较致密,有少量空隙,与基体结合良好,厚度约200μm,采用压痕法测量涂层断裂韧性为 The prepared TiN coating is shown in Figure 1. The coating is relatively dense, has a small amount of voids, and is well combined with the substrate. The thickness is about 200 μm. The fracture toughness of the coating measured by the indentation method is
实施例2实施例1中涂层的性能 The performance of coating in embodiment 2 embodiment 1
为了测量涂层中相成分和相结构,采用BRUKER公司D8型X射线分析衍射仪(XRD)对实施例1制得的涂层进行相成分分析,衍射靶材为Cu靶,波长为0.154056nm,测试结果如图2所示所示。 In order to measure phase composition and phase structure in coating, adopt BRUKER company D8 type X-ray analysis diffractometer (XRD) to carry out phase composition analysis to the coating that embodiment 1 makes, diffraction target material is Cu target, and wavelength is 0.154056nm, The test results are shown in Figure 2. the
图2所示为TiN涂层XRD图谱,经过对比PDF卡片,图中的三强峰相为TiN相,TiN相具有强烈的(200)取向,存在部分TiO、TiO2和Ti3O氧化物相,这是由于等离子喷涂过程中TiN高温下发生了氧化,生成了Ti的氧化物。涂层内TiO和Ti3O亚稳相的存在是由于等离子喷涂过程中TiN的氧化不充分沉积形成。TiN相三强峰的强度远大于氧化物相的强度,说明涂层中主要为TiN相。 Figure 2 shows the XRD spectrum of the TiN coating. After comparing the PDF card, the three strong peak phases in the figure are the TiN phase. The TiN phase has a strong (200) orientation, and there are some TiO, TiO 2 and Ti 3 O oxide phases. , which is due to the oxidation of TiN at high temperature during the plasma spraying process to form Ti oxides. The existence of TiO and Ti 3 O metastable phases in the coating is due to the insufficient deposition of TiN during the plasma spraying process. The intensity of the triple peak of the TiN phase is much greater than that of the oxide phase, indicating that the coating is mainly composed of the TiN phase.
为了确定涂层中各元素的分布情况,采用Nova NanoSEM450型扫描电子显微镜所采用的EDS能谱仪对TiN涂层进行了元素分析,具体如图3和表1所示,以确定涂层中各相之间的结合情况。 In order to determine the distribution of each element in the coating, the EDS energy spectrometer used in the Nova NanoSEM450 scanning electron microscope was used to analyze the elements of the TiN coating, as shown in Figure 3 and Table 1, to determine the elements in the coating. The connection between the phases. the
表1涂层EDS结果 Table 1 Coating EDS results
从截面扫描照片图3中可以看出,涂层中存在明暗相层状分布,在层状结构内部和层状结构结合处有少量孔隙。从元素面扫描分布图中可以看出Ti元素在整个截面中分布较均匀,N元素和O元素呈区域性分布,SEM图片中颜色较暗的A区富含成分为Ti和N,以及少量的O,相反,颜色较亮的B区富含成分为Ti、O和少量的N。结合XRD结果,可以分析A区主要成分为TiN相,而B区的主要成分为Ti氧化物相和少量TiN相。A和B颜色的不同,主要可能是氧化物相含量的不同所致。 It can be seen from the cross-sectional scanning photo in Figure 3 that there is a layered distribution of light and dark phases in the coating, and there are a small amount of pores inside the layered structure and at the junction of the layered structure. From the element surface scanning distribution diagram, it can be seen that the Ti element is evenly distributed in the entire section, and the N element and O element are regionally distributed. In the SEM image, the darker A area is rich in Ti and N, and a small amount of O, on the contrary, the brighter B region is rich in Ti, O and a small amount of N. Combined with the XRD results, it can be analyzed that the main component of area A is TiN phase, while the main component of area B is Ti oxide phase and a small amount of TiN phase. The difference in color between A and B may be mainly due to the difference in the content of the oxide phase. the
采用HVS-1000型数显维氏硬度计测试涂层显微硬度,显微硬度加载载荷为100g,加载时间15S,测试点个数为10个点,涂层的平均硬度达到1210HV0.1,可以看出涂层具有较高的硬度,具体如图4所示。 HVS-1000 digital display Vickers hardness tester is used to test the microhardness of the coating. The microhardness load is 100g, the loading time is 15S, the number of test points is 10 points, and the average hardness of the coating reaches 1210HV 0.1 . You can see The resulting coating has relatively high hardness, as shown in Figure 4.
采用HVS-1000型数显维氏硬度计压出压痕,如图5和表2所示,并利用压痕法的如下公式计算了涂层的断裂韧性: The HVS-1000 digital display Vickers hardness tester was used to press out the indentation, as shown in Figure 5 and Table 2, and the fracture toughness of the coating was calculated using the following formula of the indentation method:
式(1)中:a为对角线压痕长度的一半;P为加载载荷;式(2)中:E为杨氏模量;c为从压痕中心到裂纹边径向裂纹的长度。 In formula (1): a is half of the length of the diagonal indentation; P is the loading load; in formula (2): E is Young's modulus; c is the length of the radial crack from the center of the indentation to the edge of the crack. the
表2 涂层断裂韧性KIC计算参数 Table 2 Calculation parameters of coating fracture toughness K IC
涂层内喷涂参数对孔隙率和氧化物的影响,对硬度和断裂韧性也有影响 Influence of spraying parameters in the coating on porosity and oxides, also on hardness and fracture toughness
涂层内氧化物和孔隙率对硬度的影响趋势图如图6所示,可以看出,三种工艺下,随涂层内和孔隙率增大,涂层硬度呈明显降低趋势。孔隙率较小时涂层的硬度最高,为1402HV0.1。 The trend diagram of the influence of oxide and porosity in the coating on the hardness is shown in Figure 6. It can be seen that under the three processes, the hardness of the coating decreases significantly with the increase of the inner and porosity of the coating. When the porosity is small, the hardness of the coating is the highest, which is 1402HV0.1. the
涂层内氧化物和孔隙率对断裂韧性的影响趋势,如图7所示。可以看出,随氧化物含量增加涂层的断裂韧性呈先增加后降低的趋势,,在氧化物含量为16%左右时,涂层的断裂韧性值最大,为 The influence trend of oxide and porosity in the coating on fracture toughness is shown in Fig. 7. It can be seen that as the oxide content increases, the fracture toughness of the coating increases first and then decreases. When the oxide content is about 16%, the fracture toughness of the coating is the largest, which is
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,在不脱离本发明技术原理的前提下,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 technical principle of the present invention, some improvements and modifications can also be made. These improvements and modifications It should also be regarded as the protection scope of the present invention. the
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US15/102,976 US10047014B2 (en) | 2014-10-13 | 2015-10-13 | Plasma-sprayed tin coating having excellent hardness and toughness, the preparation method therefor, and a mold coated with said tin coating |
PCT/CN2015/091811 WO2016058513A2 (en) | 2014-10-13 | 2015-10-13 | Plasma-sprayed tin coating having excellent hardness and toughness, the preparation method therefor, and a mold coated with said tin coating |
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WO2016058513A3 (en) * | 2014-10-13 | 2016-06-16 | 王海斗 | PLASMA-SPRAYED TiN COATING HAVING EXCELLENT HARDNESS AND TOUGHNESS, THE PREPARATION METHOD THEREFOR, AND A MOLD COATED WITH SAID TiN COATING |
US10047014B2 (en) | 2014-10-13 | 2018-08-14 | Zhiguo XING | Plasma-sprayed tin coating having excellent hardness and toughness, the preparation method therefor, and a mold coated with said tin coating |
CN106676454A (en) * | 2015-11-04 | 2017-05-17 | 中国人民解放军装甲兵工程学院 | Method for improving anti-fatigue performance of coating through three-layer patterning coupling action |
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