CN104004942A - TiC particle-reinforced nickel-based composite material and preparation method thereof - Google Patents
TiC particle-reinforced nickel-based composite material and preparation method thereof Download PDFInfo
- Publication number
- CN104004942A CN104004942A CN201410191342.6A CN201410191342A CN104004942A CN 104004942 A CN104004942 A CN 104004942A CN 201410191342 A CN201410191342 A CN 201410191342A CN 104004942 A CN104004942 A CN 104004942A
- Authority
- CN
- China
- Prior art keywords
- powder
- composite material
- tic
- particle
- based composite
- 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.)
- Granted
Links
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 title claims abstract description 136
- 239000002131 composite material Substances 0.000 title claims abstract description 53
- 229910052759 nickel Inorganic materials 0.000 title claims abstract description 53
- 238000002360 preparation method Methods 0.000 title claims abstract description 28
- 239000002245 particle Substances 0.000 claims abstract description 68
- 239000000843 powder Substances 0.000 claims abstract description 66
- 239000000956 alloy Substances 0.000 claims abstract description 36
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 35
- 238000000034 method Methods 0.000 claims abstract description 30
- 230000006698 induction Effects 0.000 claims abstract description 15
- 238000005266 casting Methods 0.000 claims abstract description 11
- 238000002844 melting Methods 0.000 claims abstract description 11
- 230000008018 melting Effects 0.000 claims abstract description 11
- 238000003786 synthesis reaction Methods 0.000 claims abstract description 11
- 239000000463 material Substances 0.000 claims abstract description 10
- 230000015572 biosynthetic process Effects 0.000 claims abstract description 9
- 239000000376 reactant Substances 0.000 claims abstract description 6
- 239000000203 mixture Substances 0.000 claims abstract description 4
- 239000011208 reinforced composite material Substances 0.000 claims abstract description 4
- 229910000990 Ni alloy Inorganic materials 0.000 claims abstract description 3
- 239000011812 mixed powder Substances 0.000 claims description 17
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims description 12
- 238000003723 Smelting Methods 0.000 claims description 6
- 229910052786 argon Inorganic materials 0.000 claims description 6
- 239000007789 gas Substances 0.000 claims description 5
- 238000006243 chemical reaction Methods 0.000 claims description 3
- 238000002156 mixing Methods 0.000 claims description 3
- 238000003825 pressing Methods 0.000 claims description 3
- 238000009694 cold isostatic pressing Methods 0.000 claims description 2
- 238000011068 loading method Methods 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 abstract description 6
- 229910000601 superalloy Inorganic materials 0.000 abstract description 5
- 238000009826 distribution Methods 0.000 abstract description 3
- 239000010936 titanium Substances 0.000 description 15
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 6
- 238000005516 engineering process Methods 0.000 description 6
- 238000011065 in-situ storage Methods 0.000 description 6
- 239000011159 matrix material Substances 0.000 description 5
- 230000002787 reinforcement Effects 0.000 description 5
- 229910052782 aluminium Inorganic materials 0.000 description 4
- 238000007670 refining Methods 0.000 description 4
- 229910052719 titanium Inorganic materials 0.000 description 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 238000005728 strengthening Methods 0.000 description 3
- 229910002056 binary alloy Inorganic materials 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 239000011156 metal matrix composite Substances 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000004663 powder metallurgy Methods 0.000 description 2
- 239000002994 raw material Substances 0.000 description 2
- 238000009827 uniform distribution Methods 0.000 description 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- 229910000861 Mg alloy Inorganic materials 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000011195 cermet Substances 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000005049 combustion synthesis Methods 0.000 description 1
- 238000005056 compaction Methods 0.000 description 1
- 239000011246 composite particle Substances 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000001513 hot isostatic pressing Methods 0.000 description 1
- 238000007731 hot pressing Methods 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000010970 precious metal Substances 0.000 description 1
- 229910001404 rare earth metal oxide Inorganic materials 0.000 description 1
- 229910052702 rhenium Inorganic materials 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
- 238000001308 synthesis method Methods 0.000 description 1
- 230000002194 synthesizing effect Effects 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
Landscapes
- Powder Metallurgy (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
Abstract
本发明提供了一种TiC颗粒增强镍基复合材料,其特征在于,所述材料包含的组份及百分含量为:TiC颗粒体积百分比为3%-30%,其余为母合金;所述母合金为所有镍合金中的一种;所述方法以预制块生坯Ni-Ti-C作为颗粒合成反应物,其中该合成反应物的组成为Ni粉、Ti粉和C粉,Ni粉质量百分含量为5-50%,Ti粉与C粉的摩尔比为1∶1,将预制块生坯与母合金一同添加至真空感应炉中熔炼制备TiC颗粒增强复合材料。本发明有效地解决了传统制备成本高、工艺复杂以及颗粒形貌多样与分布不均匀以及致密度差等问题,具有成本低廉和工艺简单的特点,并且该方法可用于制造镍基高温合金大型复杂铸件。The invention provides a TiC particle-reinforced nickel-based composite material, which is characterized in that the components and percentages contained in the material are: the volume percentage of TiC particles is 3%-30%, and the rest is master alloy; the master alloy The alloy is one of all nickel alloys; the method uses prefabricated block green body Ni-Ti-C as particle synthesis reactant, wherein the composition of the synthesis reactant is Ni powder, Ti powder and C powder, and the quality of Ni powder is 100%. The TiC powder content is 5-50%, the molar ratio of Ti powder and C powder is 1:1, and the prefabricated block green body and master alloy are added into a vacuum induction furnace for melting to prepare TiC particle reinforced composite material. The invention effectively solves the traditional problems of high preparation cost, complex process, various particle shapes, uneven distribution, and poor density, and has the characteristics of low cost and simple process, and the method can be used to manufacture large and complex nickel-based superalloys. casting.
Description
技术领域technical field
本发明涉及复合材料领域,具体地,涉及一种TiC颗粒增强镍基复合材料及其制备方法。The invention relates to the field of composite materials, in particular to a TiC particle-reinforced nickel-based composite material and a preparation method thereof.
背景技术Background technique
镍基高温合金由于其优良高温性能,已成为目前制造先进航空发动机和燃气轮机热端部件的主要材料,主要包括机匣类承力件、涡轮叶片、燃烧室、涡轮盘及部分压气机叶片等。航空航天技术飞速发展要求飞行器的复杂零部件可承受更高使用温度,开发具有更高耐热温度的镍基高温复合材料制备技术对提高发动机热效率至关重要,可降低燃料消耗率,提升发动机性能,提高飞机航程,具有节能减排效应。因此对更高使用温度的铸造镍基高温合金材料需求迫切。Due to its excellent high-temperature performance, nickel-based superalloys have become the main materials for manufacturing advanced aero-engines and gas turbine hot-end components, mainly including casing-like load-bearing parts, turbine blades, combustion chambers, turbine disks, and some compressor blades. The rapid development of aerospace technology requires complex parts of aircraft to withstand higher operating temperatures. The development of nickel-based high-temperature composite materials with higher heat-resistant temperatures is crucial to improving the thermal efficiency of engines, which can reduce fuel consumption and improve engine performance. , improve the flight range of the aircraft, and have the effect of energy saving and emission reduction. Therefore, there is an urgent need for cast nickel-based superalloy materials with higher service temperature.
目前常见的K4169铸造镍基合金的耐热温度为650℃,超过650℃时其主要高温强化相γ’’将会溶解或转变为δ相,失去高温强化效果。目前国内外主要通过添加大量Co、W、Re等稀缺贵金属来提高镍基合金高温性能,而本发明是通过添加低成本第二相增强颗粒制备镍基复合材料来提升材料高温性能。At present, the heat-resistant temperature of the common K4169 cast nickel-based alloy is 650 °C. When it exceeds 650 °C, its main high-temperature strengthening phase γ’’ will dissolve or transform into δ phase, losing the high-temperature strengthening effect. At present, at home and abroad, the high-temperature performance of nickel-based alloys is mainly improved by adding a large amount of scarce precious metals such as Co, W, and Re. However, the present invention improves the high-temperature performance of the material by adding low-cost second phase reinforcement particles to prepare nickel-based composite materials.
颗粒增强复合材料能有效提高基础合金材料的耐磨性、高温性能,颗粒增强法被广泛用于制备金属基复合材料。上海交通大学吕维洁等人利用TiC、TiB以及稀土氧化物作为强化相制备了钛基复合材料(专利公开号ZL02111575.3、ZL02112260.1以及ZL200510029075.3等)。采用颗粒增强制备铝基复合材料的报道较多,米国发等人发明的一种制备颗粒增强铝基复合材料的方法(ZL201210413996.x),王宏明等人发明的一种电流与磁场复合作用下合成颗粒增强复合材料的方法(ZL201110037708.0)等。吉林大学王慧远等人通过原位自生法将TiC颗粒添加至镁合金和钢中以提高合金的耐磨性能。由于受基体材料性能限制,镁基、铝基、钛基以及铁基复合材料的高温性能始终无法超越镍基高温合金材料。Particle-reinforced composites can effectively improve the wear resistance and high-temperature performance of basic alloy materials, and the particle-reinforced method is widely used to prepare metal matrix composites. Lu Weijie from Shanghai Jiaotong University and others prepared titanium-based composite materials using TiC, TiB and rare earth oxides as strengthening phases (patent publication numbers ZL02111575.3, ZL02112260.1 and ZL200510029075.3, etc.). There are many reports on the preparation of aluminum matrix composites using particle reinforcement. A method for preparing particle reinforced aluminum matrix composites invented by Mi Guofa et al. (ZL201210413996.x), and a method invented by Wang Hongming et al. Methods for synthesizing particle-reinforced composite materials (ZL201110037708.0), etc. Wang Huiyuan of Jilin University and others added TiC particles to magnesium alloys and steels to improve the wear resistance of the alloys through the in situ autogenous method. Due to the limitation of the performance of the matrix material, the high-temperature performance of magnesium-based, aluminum-based, titanium-based and iron-based composite materials has always been unable to surpass that of nickel-based superalloy materials.
关于颗粒增强制备金属基复合材料的专利和文献较多,但TiC颗粒增强制备镍基合金复合材料制备的文献很少。具有代表性的有哈尔滨工业大学张幸红等人利用自蔓延高温燃烧合成(SHS)结合热等静压制备TiC-Ni基金属陶瓷材料,该方法受技术设备限制,只能制备Ni含量较低的复合材料,若Ni含量超过70%将无法发生SHS合成反应。由于该制备技术的原料都为粉末,需压制成型,制备形状复杂的工件困难,成品的致密度远不如铸造工艺制备的工件,并且该技术生产成本高。华北电力大学的包艳蓉等人在金属热处理上发表的文章《热压原位合成TiC-xNi复合材料的组织与性能》介绍了一种采用粉末冶金法制备镍基复合材料材料的方法,但通过粉末冶金法制备的工件对成品形貌与材料的致密度存在一定的局限性。此外,华北电力大学的刘宗德等人在《MaterialsScience and Engineering A》上发表的一篇关于原位自生法制备镍基复合材料,该方法的工艺流程是:首先将Ti与C混合粉末压制成预制块,再通过Ti-C预制块与电解镍在真空感应炉中加热熔炼制备TiC颗粒增强镍基复合材料,结果显示TiC颗在铸锭中分布不均匀,且颗粒形貌有方形与针状两种,该工艺制备的TiC颗粒增强镍基复合材料性能不稳定。此外,该TiC颗粒增强镍基复合材料的颗粒制备原料为Ti粉与C粉组成的二元体系,Ti-C二元体系发生合成反应的温度点高,高温金属Ni的熔点,接近Ti的熔点,不利于颗粒尺寸控制与均匀分布。刘宗德等人还发明了一种原位反应合成TiCx颗粒增强镍基复合材料的制备方法(ZL200910091602.1),该方法将Ti、C、Al、Fe和Mo混合粉末用镍箔包起,压制成块之后加入真空中频感应炉内,与电解镍一起熔炼浇铸,制备出致密度接近100%,高温强度与硬度明显提高的TiCx颗粒增强镍基复合材料。该工艺所用的镍基体以金属镍粉末为主,价格昂贵,且需要用镍箔包裹混合粉末压制成块,工艺复杂,不适宜产业化大生产。There are many patents and literatures on the preparation of metal matrix composites by particle reinforcement, but there are few literatures on the preparation of nickel-based alloy composites by TiC particle reinforcement. Representative ones include Zhang Xinghong from Harbin Institute of Technology and others who used self-propagating high-temperature combustion synthesis (SHS) combined with hot isostatic pressing to prepare TiC-Ni-based cermet materials. This method is limited by technical equipment and can only prepare composite materials with low Ni content. material, if the Ni content exceeds 70%, the SHS synthesis reaction cannot occur. Because the raw materials of this preparation technology are all powders, which need to be pressed and formed, it is difficult to prepare workpieces with complex shapes, and the density of the finished product is far lower than that of workpieces prepared by casting technology, and the production cost of this technology is high. Bao Yanrong of North China Electric Power University and others published an article on metal heat treatment "The microstructure and properties of in-situ synthesis of TiC-xNi composite materials by hot pressing", which introduced a method of preparing nickel-based composite materials by powder metallurgy, but The workpiece prepared by powder metallurgy has certain limitations on the shape of the finished product and the density of the material. In addition, Liu Zongde and others from North China Electric Power University published an article on the in-situ self-generation method for the preparation of nickel-based composites on "Materials Science and Engineering A". The process of this method is: firstly, the mixed powder of Ti and C is pressed into a prefabricated block , and then Ti-C prefabricated blocks and electrolytic nickel were heated and smelted in a vacuum induction furnace to prepare TiC particle-reinforced nickel-based composite materials. The results showed that the distribution of TiC particles in the ingot was uneven, and the particle shapes were square and needle-like. , the properties of TiC particle reinforced nickel-based composites prepared by this process are not stable. In addition, the TiC particle-reinforced nickel-based composite particle preparation raw material is a binary system composed of Ti powder and C powder. The synthesis reaction temperature of the Ti-C binary system is high, and the melting point of the high-temperature metal Ni is close to the melting point of Ti. , is not conducive to particle size control and uniform distribution. Liu Zongde and others also invented a preparation method for in-situ reaction synthesis of TiC x particle-reinforced nickel-based composites (ZL200910091602.1). In this method, the mixed powder of Ti, C, Al, Fe and Mo is wrapped with nickel foil, pressed After forming a block, put it into a vacuum medium-frequency induction furnace, melt and cast it together with electrolytic nickel, and prepare a TiC x particle-reinforced nickel-based composite material with a density close to 100% and a significantly improved high-temperature strength and hardness. The nickel matrix used in this process is mainly metallic nickel powder, which is expensive, and the mixed powder needs to be wrapped with nickel foil and pressed into blocks. The process is complex and not suitable for industrialized mass production.
发明内容Contents of the invention
针对现有技术中的缺陷,本发明的目的是提供一种TiC颗粒增强镍基复合材料及其制备方法,工艺简单、成本低,并可调控复合材料中TiC颗粒的尺寸与数量。In view of the defects in the prior art, the object of the present invention is to provide a TiC particle reinforced nickel-based composite material and its preparation method, which has simple process and low cost, and can control the size and quantity of TiC particles in the composite material.
根据本发明的一个方面,提供一种TiC颗粒增强镍基复合材料,所述材料包含的组份及含量为:TiC颗粒体积百分含量为3%-30%,其余为母合金;所述母合金为所有镍合金中的一种。According to one aspect of the present invention, there is provided a TiC particle-reinforced nickel-based composite material, the components and contents of which are: the TiC particle volume percentage is 3%-30%, and the rest is a master alloy; the master alloy The alloy is one of all nickel alloys.
优选地,所述TiC颗粒是通过Ni-Ti-C预制块生坯反应生成,Ni-Ti-C预制块生坯的组成为Ni粉、Ti粉和C粉,Ni粉质量百分含量为5-50%,Ti粉与C粉的摩尔比为1:1。更优选地,Ni粉质量百分含量为20-30%。Preferably, the TiC particles are produced by reacting a Ni-Ti-C prefabricated block green body, the composition of the Ni-Ti-C prefabricated block green body is Ni powder, Ti powder and C powder, and the mass percentage of Ni powder is 5 -50%, the molar ratio of Ti powder to C powder is 1:1. More preferably, the mass percentage of Ni powder is 20-30%.
优选地,所述Ni粉粒径为200-800目、纯度≥99.5%。Preferably, the Ni powder has a particle size of 200-800 mesh and a purity of ≥99.5%.
优选地,所述Ti粉粒径为200-800目、纯度≥99.5%。Preferably, the particle size of the Ti powder is 200-800 mesh, and the purity is ≥99.5%.
优选地,所述C粉粒径为≤2000目、纯度≥99.5%。Preferably, the C powder has a particle size of ≤2000 mesh and a purity of ≥99.5%.
优选地,所述TiC颗粒体积百分含量为3-10%,更进一步的,为4-7%,在该范围内可以获得性能更好的TiC颗粒增强镍基复合材料。Preferably, the volume percentage of the TiC particles is 3-10%, further, 4-7%. Within this range, a TiC particle-reinforced nickel-based composite material with better performance can be obtained.
优选地,所述TiC颗粒的尺寸小于10微米,更优选地,TiC颗粒的尺寸小于5微米。Preferably, the size of the TiC particles is less than 10 microns, more preferably, the size of the TiC particles is less than 5 microns.
优选地,所述TiC颗粒的形貌为等轴状、球状或立方状,更优选地,为球状。Preferably, the shape of the TiC particles is equiaxed, spherical or cubic, more preferably spherical.
根据本发明的另一个方面,提供一种上述TiC颗粒增强镍基复合材料的制备方法,所述方法以预制块生坯(Ni-Ti-C)作为颗粒合成反应物,与母合金一同添加至真空感应炉中熔炼制备TiC颗粒增强复合材料,具体包括以下步骤:According to another aspect of the present invention, there is provided a method for preparing the above-mentioned TiC particle-reinforced nickel-based composite material. The method uses prefabricated block green body (Ni-Ti-C) as a particle synthesis reactant, and adds it together with the master alloy to Melting and preparing TiC particle-reinforced composite materials in a vacuum induction furnace specifically includes the following steps:
⑴按照各组份的质量百分比称取Ni粉、Ti粉、C粉以及母合金;(1) Weigh Ni powder, Ti powder, C powder and master alloy according to the mass percentage of each component;
⑵采用搅拌设备将步骤⑴配比好的粉末混合均匀;⑵Use mixing equipment to mix the powder with good ratio in step ⑴ evenly;
⑶将步骤⑵混合均匀的粉末压制成Ni-Ti-C预制块生坯;(3) Pressing the uniformly mixed powder in step (2) into a Ni-Ti-C prefabricated block green body;
⑷将生坯预制块与母合金一同置入真空感应炉内熔炼浇铸成锭。(4) Put the green prefabricated block and the master alloy together into a vacuum induction furnace for melting and casting into an ingot.
优选地,所述步骤⑵中:采用搅拌机、混料机或球磨机等混合方法将Ni粉、Ti粉和C粉混合均匀。Preferably, in the step (2): Ni powder, Ti powder and C powder are uniformly mixed using a mixing method such as a mixer, a mixer or a ball mill.
优选地,所述步骤⑶中:采用冷等静压成型方法将混合粉末制备成Ni-Ti-C预制块生坯,生坯压制致密度为50-90%。Preferably, in the step (3): cold isostatic pressing is used to prepare the mixed powder into a Ni-Ti-C prefabricated block green body, and the compaction density of the green body is 50-90%.
更优选地,所述步骤⑶中:将步骤⑵中混合均匀的粉末装入模具内,施加50-100MPa的压力,加压时间为10-20秒,制备成Ni-Ti-C预制块生坯,其致密度为50-90%。More preferably, in the step (3): put the uniformly mixed powder in the step (2) into the mold, apply a pressure of 50-100 MPa, and pressurize for 10-20 seconds, and prepare a Ni-Ti-C prefabricated block green body , and its density is 50-90%.
优选地,所述步骤⑷,具体如下:Preferably, the step (4) is specifically as follows:
①装样:将制备的预制块生坯与母合金一同置入真空感应炉内熔炼;①Sample loading: put the prepared prefabricated block green body and master alloy together into a vacuum induction furnace for melting;
②熔炼气氛:将炉内真空度抽至1×10-2-1×10-4Pa,通入氩气,使其压强为0.01-0.08MPa,②Smelting atmosphere: the vacuum degree in the furnace is evacuated to 1×10 -2 -1×10 -4 Pa, and argon gas is introduced to make the pressure 0.01-0.08MPa,
③熔炼浇铸:将炉内温度升至1450-1800℃,精炼3-8分钟后浇铸成锭,得到所述TiC颗粒增强镍基复合材料。③Smelting and casting: raise the temperature in the furnace to 1450-1800°C, refine for 3-8 minutes, and then cast into ingots to obtain the TiC particle-reinforced nickel-based composite material.
本发明方法利用预制块生坯(Ni-Ti-C体系)作为反应物,将其与镍基母合金一起熔炼,成功制备TiC颗粒增强镍基复合材料。生坯预制块真空感应加热至反应温度,合成形貌规则(球状)、尺寸合理(<10μm)且与基体界面干净的TiC颗粒,并且通过感应搅拌,使TiC颗粒均匀分布于基础合金内。该技术有效地解决了传统TiC颗粒增强镍基复合材料制备成本高、工艺复杂以及颗粒形貌多样与分布不均匀以及致密度差等问题。本发明采用原位合成法与传统的熔炼浇铸相结合的工艺,是一种成本低廉和工艺简单的TiC颗粒增强镍基复合材料制备方法,并且该方法可用于制造镍基高温合金大型复杂铸件。本发明通过调整原位合成反应物(Ni-Ti-C预制块生坯)的组成,可以控制复合材料中的颗粒尺寸、形貌以及数量。The method of the invention uses the prefabricated block green body (Ni-Ti-C system) as a reactant, melts it together with the nickel-based master alloy, and successfully prepares the TiC particle-reinforced nickel-based composite material. The green prefabricated block is heated to the reaction temperature by vacuum induction, and TiC particles with regular shape (spherical), reasonable size (<10 μm) and clean interface with the matrix are synthesized, and the TiC particles are evenly distributed in the base alloy by induction stirring. This technology effectively solves the problems of traditional TiC particle-reinforced nickel-based composite materials, such as high preparation cost, complex process, various particle shapes, uneven distribution, and poor density. The invention adopts the process of combining the in-situ synthesis method with the traditional smelting and casting, and is a low-cost and simple process for preparing TiC particle reinforced nickel-based composite materials, and the method can be used to manufacture large-scale complex castings of nickel-based superalloys. The invention can control the particle size, shape and quantity in the composite material by adjusting the composition of the in-situ synthesis reactant (Ni-Ti-C prefabricated block green body).
与现有技术相比,本发明具有如下的有益效果:Compared with the prior art, the present invention has the following beneficial effects:
①本发明不用镍箔包裹混合粉末,可以通过工艺简单且成本低廉的方法制备高性能的镍基复合材料;① The present invention does not wrap the mixed powder with nickel foil, and can prepare a high-performance nickel-based composite material through a simple and low-cost method;
②本发明制备的球状TiC颗粒形貌规则、尺寸合理、分布均匀;②The spherical TiC particles prepared by the present invention have regular appearance, reasonable size and uniform distribution;
③本发明可以调整预制块生坯的添加量控制复合材料内增强体的含量(3%-30%),以此制备不同性能的镍基复合材料,以此满足不同需求;③ The present invention can adjust the addition amount of the prefabricated block green body to control the content of reinforcement in the composite material (3%-30%), so as to prepare nickel-based composite materials with different performances to meet different needs;
④本发明由于是熔炼浇铸成型,因此可以生产制备高致密度、大尺寸、复杂外形的产品。④ The present invention can produce products with high density, large size and complex shape because it is smelted and casted.
具体实施方式Detailed ways
下面结合具体实施例对本发明进行详细说明。以下实施例将有助于本领域的技术人员进一步理解本发明,但不以任何形式限制本发明。应当指出的是,对本领域的普通技术人员来说,在不脱离本发明构思的前提下,还可以做出若干变形和改进。这些都属于本发明的保护范围。以下实施例中没有详细说明的部分均可以采用现有技术实现。The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several modifications and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention. Parts that are not described in detail in the following embodiments can be implemented using existing technologies.
实施例1:制备TiC体积百分含量为3%的镍基复合材料Example 1: Preparation of a nickel-based composite material with a volume percentage of TiC of 3%
①混合粉末的制备:按配比称取镍粉末(纯度:99.5%,粒度:-200目)、钛粉末(纯度:99.5%,粒度:-200目)和C粉末(纯度:99.5%,粒度:-12500目),Ni粉50wt.%,Ti粉与C粉的摩尔比为1:1,将三种粉末用自制搅拌机混合均匀;① Preparation of mixed powder: Weigh nickel powder (purity: 99.5%, particle size: -200 mesh), titanium powder (purity: 99.5%, particle size: -200 mesh) and C powder (purity: 99.5%, particle size: -12500 order), Ni powder 50wt.%, the mol ratio of Ti powder and C powder is 1:1, three kinds of powders are mixed homogeneously with self-made mixer;
②生坯制备:混合粉末装入内径为Ф50mm的模具内,施加100MPa的压力,加压时间为20秒,制备成Ф50mm×10mm的生坯预制块,其致密度为90%;②Green body preparation: put the mixed powder into a mold with an inner diameter of Ф50mm, apply a pressure of 100MPa for 20 seconds, and prepare a green prefabricated block of Ф50mm×10mm with a density of 90%;
③熔炼浇铸:将生坯预制块与K4169母合金一起置入真空感应熔炼炉中,生坯与K4169母合金的质量百分比约为1:55。炉内真空度抽至1×10-4Pa,通入氩气,使其压强为0.01MPa。开始熔炼,炉内温度升至1450℃,精炼3分钟后浇铸成锭;③Smelting and casting: Put the prefabricated block of the green body and the K4169 master alloy into a vacuum induction melting furnace, and the mass percentage of the green body and the K4169 master alloy is about 1:55. The vacuum in the furnace was evacuated to 1×10 -4 Pa, and argon was introduced to make the pressure 0.01MPa. Start smelting, the temperature in the furnace rises to 1450°C, and cast into ingots after refining for 3 minutes;
该实施例中50%Ni-Ti-C体系反应合成尺寸在3μm左右的球状TiC颗粒,且颗粒均匀分布于基础合金,其体积百分含量占3%左右。In this embodiment, 50% Ni-Ti-C system reacts to synthesize spherical TiC particles with a size of about 3 μm, and the particles are uniformly distributed in the base alloy, and the volume percentage thereof accounts for about 3%.
实施例2:制备TiC体积百分含量为5%的镍基复合材料Example 2: Preparation of a nickel-based composite material with a volume percentage of TiC of 5%
①混合粉末的制备:按配比称取镍粉末(纯度:99.5%,粒度:-400目)、钛粉末(纯度:99.5%,粒度:-400目)和C粉末(纯度:99.5%,粒度:-8000目),Ni粉10wt.%,Ti粉与C粉的摩尔比为1:1,将三种粉末用混料机混合均匀;① Preparation of mixed powder: Weigh nickel powder (purity: 99.5%, particle size: -400 mesh), titanium powder (purity: 99.5%, particle size: -400 mesh) and C powder (purity: 99.5%, particle size: -8000 order), Ni powder 10wt.%, the mol ratio of Ti powder and C powder is 1:1, three kinds of powders are mixed with mixer;
②生坯制备:混合粉末装入内径为Ф50mm的模具内,施加80MPa的压力,加压时间为15秒,制备成Ф50mm×12mm的生坯预制块,其致密度为70%;②Green body preparation: put the mixed powder into a mold with an inner diameter of Ф50mm, apply a pressure of 80MPa for 15 seconds, and prepare a green prefabricated block of Ф50mm×12mm with a density of 70%;
③熔炼浇铸:将生坯预制块与K4169母合金一起置入真空感应熔炼炉中,生坯与K4169母合金的质量百分比约为1:26。炉内真空度抽至0.6×10-3Pa,通入氩气,使其压强为0.04MPa。开始熔炼,炉内温度升至1650℃,精炼5分钟后浇铸成锭;③Smelting and casting: Put the prefabricated block of the green body and the K4169 master alloy into the vacuum induction melting furnace, and the mass percentage of the green body and the K4169 master alloy is about 1:26. The vacuum in the furnace was evacuated to 0.6×10 -3 Pa, and argon gas was introduced to make the pressure 0.04MPa. Start smelting, the temperature in the furnace rises to 1650°C, and cast into ingots after 5 minutes of refining;
该实施例中10%Ni-Ti-C体系反应合成尺寸在小于8μm的球状TiC颗粒,颗粒均匀分布于基础合金,其体积百分含量占5%左右。In this embodiment, 10% Ni-Ti-C system reacts to synthesize spherical TiC particles with a size less than 8 μm, and the particles are uniformly distributed in the base alloy, and its volume percentage accounts for about 5%.
实施例3:制备TiC颗粒体积百分含量为15%的镍基复合材料Example 3: Preparation of a nickel-based composite material with a volume percentage of TiC particles of 15%
①混合粉末的制备:按配比称取镍粉末(纯度:99.5%,粒度:-400目)、钛粉末(纯度:99.5%,粒度:-400目)和C粉末(纯度:99.5%,粒度:-8000目),Ni粉20wt.%,Ti粉与C粉的摩尔比为1:1,将三种粉末用混料机混合均匀;① Preparation of mixed powder: Weigh nickel powder (purity: 99.5%, particle size: -400 mesh), titanium powder (purity: 99.5%, particle size: -400 mesh) and C powder (purity: 99.5%, particle size: -8000 order), Ni powder 20wt.%, the mol ratio of Ti powder and C powder is 1:1, three kinds of powders are mixed with mixer;
②生坯制备:混合粉末装入内径为Ф50mm的模具内,施加75MPa的压力,加压时间为15秒,制备成Ф50mm×13mm的生坯预制块,其致密度为65%;②Green body preparation: put the mixed powder into a mold with an inner diameter of Ф50mm, apply a pressure of 75MPa for 15 seconds, and prepare a green prefabricated block of Ф50mm×13mm with a density of 65%;
③熔炼浇铸:将生坯预制块与K4202母合金一起置入真空感应熔炼炉中,生坯与K4202母合金的质量百分比约为1:7.5。炉内真空度抽至0.6×10-3Pa,通入氩气,使其压强为0.04MPa。开始熔炼,炉内温度升至1650℃,精炼5分钟后浇铸成锭;③Smelting and casting: Put the prefabricated block of the green body and the K4202 master alloy into a vacuum induction melting furnace, and the mass percentage of the green body and the K4202 master alloy is about 1:7.5. The vacuum in the furnace was evacuated to 0.6×10 -3 Pa, and argon gas was introduced to make the pressure 0.04MPa. Start smelting, the temperature in the furnace rises to 1650°C, and cast into ingots after 5 minutes of refining;
该实施例中20%Ni-Ti-C体系反应合成尺寸在小于8μm的球状TiC颗粒,颗粒均匀分布于K4202基础合金,其体积百分含量占15%左右。In this embodiment, 20% Ni-Ti-C system reacts to synthesize spherical TiC particles with a size less than 8 μm, and the particles are uniformly distributed in the K4202 base alloy, and its volume percentage accounts for about 15%.
实施例4:制备TiC颗粒体积百分含量为30%的镍基复合材料Example 4: Preparation of a nickel-based composite material with a volume percentage of TiC particles of 30%
①混合粉末的制备:按配比称取镍粉末(纯度:99.5%,粒度:-800目)、钛粉末(纯度:99.5%,粒度:-800目)和C粉末(纯度:99.5%,粒度:-2000目),Ni粉5wt.%,Ti粉与C粉的摩尔比为1:1,将三种粉末用球磨机混合均匀;① Preparation of mixed powder: Weigh nickel powder (purity: 99.5%, particle size: -800 mesh), titanium powder (purity: 99.5%, particle size: -800 mesh) and C powder (purity: 99.5%, particle size: -2000 order), Ni powder 5wt.%, the mol ratio of Ti powder and C powder is 1:1, three kinds of powders are mixed with ball mill;
②生坯制备:混合粉末装入内径为Ф50mm的模具内,施加50MPa的压力,加压时间为10秒,制备成Ф50mm×15mm,致密度为50%的生坯预制块;②Green body preparation: put the mixed powder into a mold with an inner diameter of Ф50mm, apply a pressure of 50MPa for 10 seconds, and prepare a green prefabricated block of Ф50mm×15mm with a density of 50%;
③熔炼浇铸:将生坯预制块与K4169母合金一起置入真空感应熔炼炉中,生坯与K4169母合金的质量百分比约为1:36。炉内真空度抽至1×10-2Pa,通入氩气,使其压强为0.08MPa。开始熔炼,炉内温度升至1800℃,精炼8分钟后浇铸成锭;③Smelting and casting: Put the prefabricated block of the green body and the K4169 master alloy into a vacuum induction melting furnace, and the mass percentage of the green body and the K4169 master alloy is about 1:36. The vacuum in the furnace was evacuated to 1×10 -2 Pa, and argon was introduced to make the pressure 0.08MPa. Start smelting, the temperature in the furnace rises to 1800°C, and cast into ingots after 8 minutes of refining;
该实施例中5%Ni-Ti-C体系反应合成尺寸在小于10μm的球状TiC颗粒,颗粒均匀分布于基础合金,其体积百分含量占30%左右。In this embodiment, 5% Ni-Ti-C system reacts to synthesize spherical TiC particles with a size less than 10 μm, and the particles are uniformly distributed in the base alloy, and its volume percentage accounts for about 30%.
以上对本发明的具体实施例进行了描述。需要理解的是,本发明并不局限于上述特定实施方式,本领域技术人员可以在权利要求的范围内做出各种变形或修改,这并不影响本发明的实质内容。Specific embodiments of the present invention have been described above. It should be understood that the present invention is not limited to the specific embodiments described above, and those skilled in the art may make various changes or modifications within the scope of the claims, which do not affect the essence of the present invention.
Claims (14)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201410191342.6A CN104004942B (en) | 2014-05-07 | 2014-05-07 | TiC particle-reinforced nickel-based composite material and preparation method thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201410191342.6A CN104004942B (en) | 2014-05-07 | 2014-05-07 | TiC particle-reinforced nickel-based composite material and preparation method thereof |
Publications (2)
Publication Number | Publication Date |
---|---|
CN104004942A true CN104004942A (en) | 2014-08-27 |
CN104004942B CN104004942B (en) | 2017-01-11 |
Family
ID=51365848
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201410191342.6A Active CN104004942B (en) | 2014-05-07 | 2014-05-07 | TiC particle-reinforced nickel-based composite material and preparation method thereof |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN104004942B (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106058291A (en) * | 2016-07-01 | 2016-10-26 | 中国科学院上海硅酸盐研究所 | Connector material for solid oxide fuel cell and preparation method of connector material |
CN106319288A (en) * | 2015-07-03 | 2017-01-11 | 中国科学院上海硅酸盐研究所 | Directly-introduced and in-situ generated TiC particle commonly-enhanced nickel-base composite and preparing method and application thereof |
CN108486402A (en) * | 2018-03-07 | 2018-09-04 | 上海交通大学 | A kind of TiN particle enhanced nickel base composite materials and preparation method thereof |
CN108504886A (en) * | 2017-02-24 | 2018-09-07 | 中国科学院上海硅酸盐研究所 | A kind of preparation method of TiC-C nickel-base alloys self-lubricating composite |
CN113718132A (en) * | 2021-08-31 | 2021-11-30 | 华中科技大学 | Ni alloy for refining grains by solute interaction and preparation method thereof |
CN114525425A (en) * | 2022-02-21 | 2022-05-24 | 大连理工大学 | MC type carbide reinforced nickel-based superalloy composite material, preparation method and application thereof |
CN115475947A (en) * | 2022-10-17 | 2022-12-16 | 吉林大学 | Preparation method and application of transition metal carbide particles with {100} crystal face cube surfaces |
CN116334422A (en) * | 2023-03-17 | 2023-06-27 | 西安航天发动机有限公司 | Forming method capable of realizing grain refinement of K4202 superalloy |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2076019A (en) * | 1980-05-16 | 1981-11-25 | Metallurg Ind Inc | Erosion-resistant Alloys |
CN1091473A (en) * | 1993-11-08 | 1994-08-31 | 武汉工业大学 | Autoreaction-fusion technology prepares metal-base composites |
CN1281053A (en) * | 2000-07-27 | 2001-01-24 | 钢铁研究总院 | Process for preparing ceramic-phase diffusion enhanced alloy and particle enhanced metal-base composition |
-
2014
- 2014-05-07 CN CN201410191342.6A patent/CN104004942B/en active Active
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2076019A (en) * | 1980-05-16 | 1981-11-25 | Metallurg Ind Inc | Erosion-resistant Alloys |
CN1091473A (en) * | 1993-11-08 | 1994-08-31 | 武汉工业大学 | Autoreaction-fusion technology prepares metal-base composites |
CN1281053A (en) * | 2000-07-27 | 2001-01-24 | 钢铁研究总院 | Process for preparing ceramic-phase diffusion enhanced alloy and particle enhanced metal-base composition |
Non-Patent Citations (2)
Title |
---|
张幸红等: "工艺参数对Ti-C-Ni体系燃烧合成过程的影响", 《粉末冶金技术》, vol. 18, no. 1, 31 December 2000 (2000-12-31) * |
张辛红等: "Ni含量对SHS法合成TiC-Ni基金属陶瓷的影响", 《复合材料学报》, vol. 16, no. 4, 31 October 1999 (1999-10-31), pages 25 * |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106319288A (en) * | 2015-07-03 | 2017-01-11 | 中国科学院上海硅酸盐研究所 | Directly-introduced and in-situ generated TiC particle commonly-enhanced nickel-base composite and preparing method and application thereof |
CN106058291A (en) * | 2016-07-01 | 2016-10-26 | 中国科学院上海硅酸盐研究所 | Connector material for solid oxide fuel cell and preparation method of connector material |
CN106058291B (en) * | 2016-07-01 | 2018-12-07 | 中国科学院上海硅酸盐研究所 | A kind of metallic interconnection materials and preparation method thereof for solid oxide fuel cell |
CN108504886A (en) * | 2017-02-24 | 2018-09-07 | 中国科学院上海硅酸盐研究所 | A kind of preparation method of TiC-C nickel-base alloys self-lubricating composite |
CN108486402A (en) * | 2018-03-07 | 2018-09-04 | 上海交通大学 | A kind of TiN particle enhanced nickel base composite materials and preparation method thereof |
CN113718132A (en) * | 2021-08-31 | 2021-11-30 | 华中科技大学 | Ni alloy for refining grains by solute interaction and preparation method thereof |
CN114525425A (en) * | 2022-02-21 | 2022-05-24 | 大连理工大学 | MC type carbide reinforced nickel-based superalloy composite material, preparation method and application thereof |
CN115475947A (en) * | 2022-10-17 | 2022-12-16 | 吉林大学 | Preparation method and application of transition metal carbide particles with {100} crystal face cube surfaces |
CN115475947B (en) * | 2022-10-17 | 2024-01-12 | 吉林大学 | Preparation method and application of transition metal carbide particles with cubic {100} crystal planes on the surface |
CN116334422A (en) * | 2023-03-17 | 2023-06-27 | 西安航天发动机有限公司 | Forming method capable of realizing grain refinement of K4202 superalloy |
Also Published As
Publication number | Publication date |
---|---|
CN104004942B (en) | 2017-01-11 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN104004942B (en) | TiC particle-reinforced nickel-based composite material and preparation method thereof | |
CN104120291B (en) | A kind of TiC, TiB2The preparation method of particle enhanced nickel base composite material | |
CN107829007B (en) | A method for preparing high-entropy alloy bulk by high-entropy alloy and powder metallurgy | |
CN103240412B (en) | Method for preparing powder super-alloy by near net shape | |
CN109338172A (en) | A kind of high-entropy alloy reinforced 2024 aluminum matrix composite material and preparation method thereof | |
CN105734324A (en) | Preparing method for powder metallurgy high-entropy alloy based composite material | |
CN102534334B (en) | A kind of preparation method of high-strength and high-toughness molybdenum alloy | |
CN108441706B (en) | A kind of high-entropy alloy reinforced nickel-aluminum composite material and preparation method thereof | |
CN107760897A (en) | To hydrogenate method of the titanium sponge as raw material manufacture titanium and titanium alloy and its parts | |
CN107130125A (en) | A kind of preparation method of high-entropy alloy | |
CN103938005B (en) | Airflow milling titanium hydride powder prepares the method for superfine crystal particle titanium or titanium alloy | |
CN1958817A (en) | Method for preparing alloy material of high niobium-titanium-aluminum by discharging plasma agglomeration | |
CN100432267C (en) | High-strength magnesium based composite material and preparation method thereof | |
CN103433488B (en) | Preparation method of titanium nitride-ferrous metal ceramics | |
CN103143709B (en) | Method for manufacturing TiAl intermetallic compound component based on Ti elemental powder and Al elemental powder | |
CN108251670B (en) | Preparation method of high-temperature-resistant intermetallic compound alloy | |
CN112705717A (en) | Preparation method of in-situ generated nitride enhanced high-entropy alloy-based powder material | |
CN105624536A (en) | Preparation method of Fe-Al-Mn-C alloy | |
CN108396199A (en) | A kind of cobalt chrome-nickel material and its method for preparing powder metallurgy | |
CN104294070B (en) | A kind of low-temperature sintering preparation is containing the method for Mg aluminium alloy | |
CN107620004A (en) | A kind of method for preparing powder metallurgy of Fe Mn Al series alloys | |
CN103834847A (en) | High-density non-magnetic balance block as well as powder metallurgy preparation method and application thereof | |
CN102732747A (en) | Method for preparing Ti-24Nb-8Sn alloy by using TiH2 powder as raw material though powder metallurgy | |
CN107012368A (en) | A kind of method that utilization powder metallurgic method prepares high-strength degradable aluminium alloy | |
CN111349838A (en) | Preparation method of high-entropy alloy composite material |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant |