WO2017070806A1 - High-strength titanium carbide particle-reinforced copper-based composite material and preparation method therefor - Google Patents

High-strength titanium carbide particle-reinforced copper-based composite material and preparation method therefor Download PDF

Info

Publication number
WO2017070806A1
WO2017070806A1 PCT/CN2015/000866 CN2015000866W WO2017070806A1 WO 2017070806 A1 WO2017070806 A1 WO 2017070806A1 CN 2015000866 W CN2015000866 W CN 2015000866W WO 2017070806 A1 WO2017070806 A1 WO 2017070806A1
Authority
WO
WIPO (PCT)
Prior art keywords
titanium carbide
copper
composite material
purity
based composite
Prior art date
Application number
PCT/CN2015/000866
Other languages
French (fr)
Chinese (zh)
Inventor
孙飞
赵勇
埃里克斯⋅高登
Original Assignee
苏州列治埃盟新材料技术转移有限公司
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by 苏州列治埃盟新材料技术转移有限公司 filed Critical 苏州列治埃盟新材料技术转移有限公司
Publication of WO2017070806A1 publication Critical patent/WO2017070806A1/en

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/02Making non-ferrous alloys by melting
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C9/00Alloys based on copper
    • C22C9/02Alloys based on copper with tin as the next major constituent

Definitions

  • the invention relates to a particle reinforced copper matrix composite material and a preparation method thereof, in particular to a high strength titanium carbide particle reinforced copper matrix composite material for a high speed turbine of a locomotive.
  • the national standard copper alloy material ZCuSn 10 Pb 1 is a multi-purpose tin bronze material with high hardness, excellent wear resistance, easy to produce seizure, good casting performance and machinability, in the atmosphere and fresh water. It has good corrosion resistance and is mainly used for manufacturing wear parts with high load (below 20MPa) and high sliding speed (8m/s), such as connecting rods, bushings, bushings, gears, turbines, etc.
  • high load below 20MPa
  • 8m/s high sliding speed
  • the material needs to increase its corresponding strength while meeting the manufacturing requirements of high-speed locomotive parts, so as to reduce the amount of wear in a certain period of time, thereby increasing its service life and reducing replacement.
  • the frequency of parts and components reduces the corresponding operating costs and saves resources.
  • the high-purity titanium carbide powder is a titanium carbide material prepared by reacting titanium dioxide and carbon black in a carbon tube furnace or a frequency-modulated vacuum furnace through a hydrogen gas at a high temperature of 1600 ° C to 1800 ° C. Because titanium carbide has high hardness, high strength, good chemical stability, no hydrolysis, high temperature oxidation resistance, etc., it is an important raw material for the production of hard alloys, which can be used to manufacture wear-resistant materials, cutting tool materials, mechanical parts, etc. It can also produce bismuth of tin, lead, cadmium, zinc and other metals.
  • the new copper-based alloy composites that combine the advantages of high-purity titanium carbide and copper alloy ZCuSn 10 Pb 1 can meet the material requirements of high-speed turbines and other components of the locomotive to a certain extent.
  • the object of the present invention is to provide an effective improvement of the strength, wear resistance and corrosion resistance of the copper alloy ZCuSn 10 Pb 1 by improving the volume ratio between the high-purity titanium carbide and the copper alloy ZCuSn 10 Pb 1 and the preparation conditions.
  • a high-strength titanium carbide particle reinforced copper-based composite material for a high-speed turbine of a locomotive consisting of the following volume percentage components: high-purity titanium carbide with a purity greater than 98% 0.05-1.5%, copper alloy ZCuSn 10 Pb 1 98.5- 99.95%.
  • the high strength titanium carbide particle reinforced copper matrix composite of the present invention is composed of a volume percentage component of high purity titanium carbide 0.05% having a purity greater than 98% and a copper alloy ZCuSn 10 Pb 1 99.95%.
  • the high strength titanium carbide particle reinforced copper matrix composite of the present invention consists of a volume percent component of high purity titanium carbide 0.8% with a purity greater than 98% and a copper alloy ZCuSn 10 Pb 1 99.2%.
  • the high strength titanium carbide particle reinforced copper matrix composite of the present invention consists of a volume percent component of high purity titanium carbide 1.5% having a purity greater than 98% and a copper alloy ZCuSn 10 Pb 1 98.5%.
  • the high-purity titanium carbide is a powder particle.
  • the copper alloy ZCuSn 10 Pb 1 is composed of the following components by weight: 9.0-11.5% of tin ingot, 0.5-1.0% of phosphor bronze alloy, ⁇ 0.75% of total impurity, and the balance being copper.
  • the invention provides a preparation method of a high-strength titanium carbide particle reinforced copper-based composite material for a high-speed turbine of a locomotive, which has the following steps:
  • the finished high-strength titanium carbide particle reinforced copper-based composite material is kept in an electric furnace for a period of 1-1.5 hours; then the high-strength titanium carbide particle-reinforced copper-based composite material is cast into a high casting method.
  • Intensity particle reinforced copper-based alloy composite bar, casting temperature is 1150-1200 ° C;
  • the volume fraction of the high-purity titanium carbide particles is 0.05%.
  • the volume fraction of the high-purity titanium carbide particles is 0.8%.
  • step 3 the volume fraction of the high-purity titanium carbide particles is 1.5%.
  • the invention uniformly distributes the high-purity titanium carbide powder in the copper alloy ZCuSn 10 Pb 1 material by the above-mentioned technical means, and utilizes the high hardness of the titanium carbide, the strength is strong, the chemical stability is good, the hydrolysis is not good, and the high-temperature oxidation resistance is good to make up.
  • 1 is a disadvantage of the copper alloy material ZCuSn 10 Pb, copper alloys achieve ZCuSn 10 Pb 1 further improve performance of the materials.
  • the high-strength titanium carbide particle reinforced copper-based composite material obtained by the invention has higher strength, hardness, wear resistance and corrosion resistance, and is applied to wear-resistant parts working under high load and high sliding speed, thereby Extend the service life of connecting rods, bushings, bushings, gears, and turbines.
  • FIG. 1 is a flow chart of a method of the present invention for a high strength titanium carbide particle reinforced copper matrix composite for a high speed turbine of a locomotive.
  • the high-strength titanium carbide particle reinforced copper-based composite material for a high-speed turbine of a locomotive according to Embodiment 1 of the present invention, wherein the volume percentage of each component is 0.05% of high-purity titanium carbide powder having a purity of more than 98%, and the copper alloy ZCuSn 10 Pb 1 99.95%.
  • the method for preparing a high-strength titanium carbide particle reinforced copper-based composite material for a high-speed turbine of a locomotive according to Embodiment 1 of the present invention has the following steps (as shown in FIG. 1):
  • composition of the prepared copper alloy ZCuSn 10 Pb 1 liquid is detected by using a Spike direct reading spectrometer to determine the chemical composition within the requirements of the national standard;
  • the finished high-strength titanium carbide particle reinforced copper-based composite material is kept in an electric furnace for 1 hour; then the high-strength titanium carbide particle-reinforced copper-based composite material is cast into high-strength particle reinforcement by continuous casting.
  • Copper-based alloy composite bar, casting temperature is 1150 ° C;
  • the high-strength titanium carbide particle-reinforced copper-based composite material for a high-speed turbine of a locomotive according to Embodiment 2 of the present invention wherein the volume percentage of each component is 0.8% of high-purity titanium carbide powder having a purity of more than 98%, and the copper alloy ZCuSn 10 Pb 1 99.2%.
  • the method for preparing a high-strength titanium carbide particle reinforced copper-based composite material for a high-speed turbine of a locomotive according to Embodiment 2 of the present invention has the following steps (as shown in FIG. 1):
  • composition of the prepared copper alloy ZCuSn 10 Pb 1 liquid is detected by using a Spike direct reading spectrometer to determine the chemical composition within the requirements of the national standard;
  • the finished high-strength titanium carbide particle reinforced copper-based composite material is kept in an electric furnace for 1 hour; then the high-strength titanium carbide particle-reinforced copper-based composite material is cast into high-strength particle reinforcement by continuous casting.
  • Copper-based alloy composite bar, casting temperature is 1150 ° C;
  • a high-strength titanium carbide particle-reinforced copper-based composite material for a high-speed turbine of a locomotive according to Embodiment 3 of the present invention wherein a volume percentage of each component is 1.5% of a high-purity titanium carbide powder having a purity of more than 98%, and a copper alloy ZCuSn 10 Pb 1 98.5%.
  • the method for preparing a high-strength titanium carbide particle reinforced copper-based composite material for a high-speed turbine of a locomotive according to Embodiment 3 of the present invention has the following steps (as shown in FIG. 1):
  • composition of the prepared copper alloy ZCuSn 10 Pb 1 liquid is detected by using a Spike direct reading spectrometer to determine the chemical composition within the requirements of the national standard;
  • the finished high-strength titanium carbide particle reinforced copper matrix composite material is carried out in an electric furnace Insulation, the time is 1.5h; then the high-strength titanium carbide particle-reinforced copper-based composite material is cast into a high-strength particle-reinforced copper-base alloy composite bar by continuous casting, and the casting temperature is 1200 ° C;
  • the copper alloy material with the traditional element cadmium and titanium is composed of cadmium containing 0.025% by weight of the total weight of the alloy material, titanium of 0.025% by weight of the total weight of the alloy material, and copper alloy ZCuSn 10 Pb accounting for 99.95% of the total weight of the alloy material. 1 .
  • the above copper alloy material is prepared by a conventional heat treatment process, that is, a heat treatment process such as repeated annealing, tempering, and bonfire.
  • the copper alloy material with traditional elements of cadmium and titanium is composed of cadmium which is 0.5% of the total weight of the alloy material, 1.0% of the total weight of the alloy material, and the copper alloy ZCuSn 10 Pb which accounts for 98.5% of the total weight of the alloy material. 1 .
  • the above copper alloy material is prepared by a conventional heat treatment process, that is, a heat treatment process such as repeated annealing, tempering, and bonfire.

Abstract

A high-strength titanium carbide particle-reinforced copper-based composite material for a high-speed turbine of a locomotive and a preparation method therefor. The material is composed of the following components by volume percentage: 0.05% - 1.5% of high-purity titanium carbide with a purity of greater than 98%, and 98.5% - 99.95% of a copper alloy ZCuSn10Pb1. The high-strength titanium carbide particle-reinforced copper-based composite material is prepared by undergoing the steps of stirring, smelting, casting and the like.

Description

一种高强度碳化钛颗粒增强铜基复合材料及其制备方法High-strength titanium carbide particle reinforced copper matrix composite material and preparation method thereof 技术领域Technical field
本发明涉及一种颗粒增强铜基复合材料及其制备方法,特别是涉及一种用于机车高速涡轮的高强度碳化钛颗粒增强铜基复合材料。The invention relates to a particle reinforced copper matrix composite material and a preparation method thereof, in particular to a high strength titanium carbide particle reinforced copper matrix composite material for a high speed turbine of a locomotive.
背景技术Background technique
国标铜合金材料ZCuSn10Pb1是一种多用途的锡青铜材料,其硬度高、耐磨性极好、不易产生咬死现象、有较好的铸造性能和可切削性、在大气和淡水中具有良好耐蚀性,主要用于制造高负荷(20MPa以下)和高滑动速度(8m/s)下工作的耐磨零件,如连杆、衬套、轴瓦、齿轮、涡轮等。但是随着我国高速铁路的迅速发展,该材料在满足高速机车零部件的制造要求的同时,需要提高其相应的强度,以减少其在一定时间段的磨损量,从而提高其使用年限,减少更换零部件频率,降低相应的运行成本,节约资源。The national standard copper alloy material ZCuSn 10 Pb 1 is a multi-purpose tin bronze material with high hardness, excellent wear resistance, easy to produce seizure, good casting performance and machinability, in the atmosphere and fresh water. It has good corrosion resistance and is mainly used for manufacturing wear parts with high load (below 20MPa) and high sliding speed (8m/s), such as connecting rods, bushings, bushings, gears, turbines, etc. However, with the rapid development of China's high-speed railway, the material needs to increase its corresponding strength while meeting the manufacturing requirements of high-speed locomotive parts, so as to reduce the amount of wear in a certain period of time, thereby increasing its service life and reducing replacement. The frequency of parts and components reduces the corresponding operating costs and saves resources.
高纯度的碳化钛粉体是一种由二氧化钛与炭黑在通氢气的碳管炉或调频真空炉内,1600℃-1800℃高温下反应制得的一种碳化钛材料。由于碳化钛具有高硬度,强度大,化学稳定好,不水解,高温抗氧化性好等优势,因此它是硬质合金生产的重要原料,可用于制造耐磨材料、切削刀具材料、机械零件等,还可制作熔炼锡、铅、镉、锌等金属的坩埚。The high-purity titanium carbide powder is a titanium carbide material prepared by reacting titanium dioxide and carbon black in a carbon tube furnace or a frequency-modulated vacuum furnace through a hydrogen gas at a high temperature of 1600 ° C to 1800 ° C. Because titanium carbide has high hardness, high strength, good chemical stability, no hydrolysis, high temperature oxidation resistance, etc., it is an important raw material for the production of hard alloys, which can be used to manufacture wear-resistant materials, cutting tool materials, mechanical parts, etc. It can also produce bismuth of tin, lead, cadmium, zinc and other metals.
综上,将高纯度碳化钛和铜合金ZCuSn10Pb1二者优势结合在一起的新型铜基合金复合材料一定能够在一定程度上满足机车高速涡轮等部件对材料的要求。In summary, the new copper-based alloy composites that combine the advantages of high-purity titanium carbide and copper alloy ZCuSn 10 Pb 1 can meet the material requirements of high-speed turbines and other components of the locomotive to a certain extent.
发明内容Summary of the invention
本发明的目的在于,通过改进高纯度碳化钛和铜合金ZCuSn10Pb1之间 体积配比以及制备条件,提供一种有效提高铜合金ZCuSn10Pb1强度、耐磨性和耐腐蚀性的高强度碳化钛颗粒增强铜基复合材料及其制备方法。The object of the present invention is to provide an effective improvement of the strength, wear resistance and corrosion resistance of the copper alloy ZCuSn 10 Pb 1 by improving the volume ratio between the high-purity titanium carbide and the copper alloy ZCuSn 10 Pb 1 and the preparation conditions. Strength titanium carbide particle reinforced copper matrix composite material and preparation method thereof.
为实现上述发明目的,本发明所提供的技术方案是:In order to achieve the above object, the technical solution provided by the present invention is:
一种用于机车高速涡轮的高强度碳化钛颗粒增强铜基复合材料,由如下体积百分比的组分组成:纯度大于98%的高纯度碳化钛0.05-1.5%,铜合金ZCuSn10Pb1 98.5-99.95%。A high-strength titanium carbide particle reinforced copper-based composite material for a high-speed turbine of a locomotive consisting of the following volume percentage components: high-purity titanium carbide with a purity greater than 98% 0.05-1.5%, copper alloy ZCuSn 10 Pb 1 98.5- 99.95%.
优选地,本发明的高强度碳化钛颗粒增强铜基复合材料,由如下体积百分比的组分组成:纯度大于98%的高纯度碳化钛0.05%,铜合金ZCuSn10Pb1 99.95%。Preferably, the high strength titanium carbide particle reinforced copper matrix composite of the present invention is composed of a volume percentage component of high purity titanium carbide 0.05% having a purity greater than 98% and a copper alloy ZCuSn 10 Pb 1 99.95%.
优选地,本发明的高强度碳化钛颗粒增强铜基复合材料,由如下体积百分比的组分组成:纯度大于98%的高纯度碳化钛0.8%,铜合金ZCuSn10Pb1 99.2%。Preferably, the high strength titanium carbide particle reinforced copper matrix composite of the present invention consists of a volume percent component of high purity titanium carbide 0.8% with a purity greater than 98% and a copper alloy ZCuSn 10 Pb 1 99.2%.
优选地,本发明的高强度碳化钛颗粒增强铜基复合材料,由如下体积百分比的组分组成:纯度大于98%的高纯度碳化钛1.5%,铜合金ZCuSn10Pb1 98.5%。Preferably, the high strength titanium carbide particle reinforced copper matrix composite of the present invention consists of a volume percent component of high purity titanium carbide 1.5% having a purity greater than 98% and a copper alloy ZCuSn 10 Pb 1 98.5%.
进一步地,所述高纯度碳化钛为粉体颗粒。Further, the high-purity titanium carbide is a powder particle.
进一步地,所述铜合金ZCuSn10Pb1由如下重量百分比的组分组成:锡锭9.0-11.5%,磷铜合金0.5-1.0%,杂质总和≤0.75%,其余为铜。Further, the copper alloy ZCuSn 10 Pb 1 is composed of the following components by weight: 9.0-11.5% of tin ingot, 0.5-1.0% of phosphor bronze alloy, ≤0.75% of total impurity, and the balance being copper.
本发明提供一种用于机车高速涡轮的高强度碳化钛颗粒增强铜基复合材料的制备方法具有以下步骤:The invention provides a preparation method of a high-strength titanium carbide particle reinforced copper-based composite material for a high-speed turbine of a locomotive, which has the following steps:
1)制备铜合金ZCuSn10Pb1:将电解铜、磷铜合金,锡锭按照上述的重量比例放入电炉中熔炼,熔炼中铜合金液体体积小于电炉体积的90%;熔炼温度为1150-1200℃,时间为5-6h;1) Preparation of copper alloy ZCuSn 10 Pb 1 : Electrolytic copper, phosphor bronze alloy, and tin ingot are smelted in an electric furnace according to the above weight ratio, the volume of the copper alloy liquid in the smelting is less than 90% of the volume of the electric furnace; the melting temperature is 1150-1200. °C, the time is 5-6h;
2)使用斯派克直读光谱仪对制备的铜合金ZCuSn10Pb1液体进行成分检测,以确定其化学组成在上述的范围之内;2) using a Spike direct reading spectrometer to perform a component test on the prepared copper alloy ZCuSn 10 Pb 1 liquid to determine that its chemical composition is within the above range;
3)将高纯度碳化钛颗粒按体积百分比为0.05-1.5%放入上述铜合金ZCuSn10Pb1液体的表面,开启工频电炉的震动装置并同时用石墨棒进行搅 拌,使二者均匀混合;进一步升高电炉温度至1200-1250℃并保持50-60min;3) placing high-purity titanium carbide particles in a volume percentage of 0.05-1.5% on the surface of the above-mentioned copper alloy ZCuSn 10 Pb 1 liquid, turning on the vibration device of the power frequency electric furnace and simultaneously stirring with a graphite rod to uniformly mix the two; Further raising the temperature of the electric furnace to 1200-1250 ° C and maintaining 50-60 min;
4)将制作完成的高强度碳化钛颗粒增强铜基复合材料在电炉中进行保温,时间为1-1.5h;之后采用连续铸造的方式将此高强度碳化钛颗粒增强铜基复合材料铸造成高强度颗粒增强铜基合金复合棒材,铸造温度为1150-1200℃;4) The finished high-strength titanium carbide particle reinforced copper-based composite material is kept in an electric furnace for a period of 1-1.5 hours; then the high-strength titanium carbide particle-reinforced copper-based composite material is cast into a high casting method. Intensity particle reinforced copper-based alloy composite bar, casting temperature is 1150-1200 ° C;
5)将铸造完成之后的高强度颗粒增强铜基合金复合棒材进行表面车加工处理,并按照出厂标准包装。5) The high-strength particle-reinforced copper-based alloy composite bar after casting is surface-processed and packaged according to the factory standard.
进一步地,步骤3中,所述高纯度碳化钛颗粒的体积百分比为0.05%。Further, in the step 3, the volume fraction of the high-purity titanium carbide particles is 0.05%.
进一步地,步骤3中,所述高纯度碳化钛颗粒的体积百分比为0.8%。Further, in the step 3, the volume fraction of the high-purity titanium carbide particles is 0.8%.
进一步地,步骤3中,所述高纯度碳化钛颗粒的体积百分比为1.5%。Further, in step 3, the volume fraction of the high-purity titanium carbide particles is 1.5%.
采用上述技术方案,本发明的有益效果有:With the above technical solutions, the beneficial effects of the present invention are as follows:
本发明将高纯度碳化钛粉体通过上述技术手段均匀分布在铜合金ZCuSn10Pb1材料中,利用碳化钛高硬度,强度大,化学稳定好,不水解,高温抗氧化性好的性能,弥补了铜合金ZCuSn10Pb1材料的缺点,实现铜合金ZCuSn10Pb1材料的性能的进一步提升。本发明所得到的高强度碳化钛颗粒增强铜基复合材料具有更高的强度、硬度、耐磨性以及耐腐蚀性,将其应用在高负荷和高滑动速度下工作的耐磨零件中,从而延长连杆、衬套、轴瓦、齿轮、涡轮机的使用寿命。The invention uniformly distributes the high-purity titanium carbide powder in the copper alloy ZCuSn 10 Pb 1 material by the above-mentioned technical means, and utilizes the high hardness of the titanium carbide, the strength is strong, the chemical stability is good, the hydrolysis is not good, and the high-temperature oxidation resistance is good to make up. 1 is a disadvantage of the copper alloy material ZCuSn 10 Pb, copper alloys achieve ZCuSn 10 Pb 1 further improve performance of the materials. The high-strength titanium carbide particle reinforced copper-based composite material obtained by the invention has higher strength, hardness, wear resistance and corrosion resistance, and is applied to wear-resistant parts working under high load and high sliding speed, thereby Extend the service life of connecting rods, bushings, bushings, gears, and turbines.
附图说明DRAWINGS
图1是本发明的用于机车高速涡轮的高强度碳化钛颗粒增强铜基复合材料的方法的流程图。1 is a flow chart of a method of the present invention for a high strength titanium carbide particle reinforced copper matrix composite for a high speed turbine of a locomotive.
具体实施方式detailed description
以下结合附图和实施例对本发明提供的高强度碳化钛颗粒增强铜基复合材料及其制备方法作进一步说明,但并非限制本发明的应用范围。The high-strength titanium carbide particle reinforced copper-based composite material provided by the present invention and its preparation method are further described below with reference to the accompanying drawings and embodiments, but are not intended to limit the scope of application of the present invention.
实施例1Example 1
本发明实施例1的用于机车高速涡轮的高强度碳化钛颗粒增强铜基复合材料,各组分的体积百分比为纯度大于98%的高纯度碳化钛粉体0.05%,铜合金ZCuSn10Pb1 99.95%。The high-strength titanium carbide particle reinforced copper-based composite material for a high-speed turbine of a locomotive according to Embodiment 1 of the present invention, wherein the volume percentage of each component is 0.05% of high-purity titanium carbide powder having a purity of more than 98%, and the copper alloy ZCuSn 10 Pb 1 99.95%.
本发明实施例1的用于机车高速涡轮的高强度碳化钛颗粒增强铜基复合材料的制备方法,具有以下步骤(如图1所示):The method for preparing a high-strength titanium carbide particle reinforced copper-based composite material for a high-speed turbine of a locomotive according to Embodiment 1 of the present invention has the following steps (as shown in FIG. 1):
1)制备铜合金ZCuSn10Pb1:按照国标GB/T 1176-1987的标准将电解铜、磷铜合金,锡锭按照重量比例放入电炉中熔炼,熔炼中铜合金液体体积小于电炉体积的90%;熔炼温度为1150℃,时间为5h;1) Preparation of copper alloy ZCuSn 10 Pb 1 : Electrolytic copper, phosphor bronze alloy and tin ingot are smelted in an electric furnace according to the standard GB/T 1176-1987. The volume of the copper alloy liquid in the smelting is less than 90% of the volume of the electric furnace. %; melting temperature is 1150 ° C, time is 5h;
2)使用斯派克直读光谱仪对制备的铜合金ZCuSn10Pb1液体进行成分检测,以确定其化学组成在国标要求范围之内;2) The composition of the prepared copper alloy ZCuSn 10 Pb 1 liquid is detected by using a Spike direct reading spectrometer to determine the chemical composition within the requirements of the national standard;
3)将高纯度碳化钛放入上述铜合金ZCuSn10Pb1液体的表面,开启工频电炉的震动装置并同时用石墨棒进行搅拌,使二者均匀混合;进一步升高电炉温度至1200℃并保持50min;3) Put high-purity titanium carbide into the surface of the above-mentioned copper alloy ZCuSn 10 Pb 1 liquid, turn on the vibration device of the power frequency electric furnace and simultaneously stir with a graphite rod to uniformly mix the two; further increase the temperature of the electric furnace to 1200 ° C and Hold for 50 minutes;
4)将制作完成的高强度碳化钛颗粒增强铜基复合材料在电炉中进行保温,时间为1h;之后采用连续铸造的方式将此高强度碳化钛颗粒增强铜基复合材料铸造成高强度颗粒增强铜基合金复合棒材,铸造温度为1150℃;4) The finished high-strength titanium carbide particle reinforced copper-based composite material is kept in an electric furnace for 1 hour; then the high-strength titanium carbide particle-reinforced copper-based composite material is cast into high-strength particle reinforcement by continuous casting. Copper-based alloy composite bar, casting temperature is 1150 ° C;
5)将铸造完成之后的高强度颗粒增强铜基合金复合棒材进行表面车加工处理,并按照出厂标准包装。5) The high-strength particle-reinforced copper-based alloy composite bar after casting is surface-processed and packaged according to the factory standard.
实施例2Example 2
本发明实施例2的用于机车高速涡轮的高强度碳化钛颗粒增强铜基复合材料,各组分的体积百分比为纯度大于98%的高纯度碳化钛粉体0.8%,铜合金ZCuSn10Pb1 99.2%。The high-strength titanium carbide particle-reinforced copper-based composite material for a high-speed turbine of a locomotive according to Embodiment 2 of the present invention, wherein the volume percentage of each component is 0.8% of high-purity titanium carbide powder having a purity of more than 98%, and the copper alloy ZCuSn 10 Pb 1 99.2%.
本发明实施例2的用于机车高速涡轮的高强度碳化钛颗粒增强铜基复合材料的制备方法,具有以下步骤(如图1所示):The method for preparing a high-strength titanium carbide particle reinforced copper-based composite material for a high-speed turbine of a locomotive according to Embodiment 2 of the present invention has the following steps (as shown in FIG. 1):
1)制备铜合金ZCuSn10Pb1:按照国标GB/T 1176-1987的标准将电解铜、磷铜合金,锡锭按照重量比例放入电炉中熔炼,熔炼中铜合金液体体 积小于电炉体积的90%;熔炼温度为1150℃,时间为5.5h;1) Preparation of copper alloy ZCuSn 10 Pb 1 : Electrolytic copper, phosphor bronze alloy and tin ingot are smelted in an electric furnace according to the standard GB/T 1176-1987. The volume of the copper alloy liquid in the smelting is less than 90% of the volume of the electric furnace. %; melting temperature is 1150 ° C, time is 5.5h;
2)使用斯派克直读光谱仪对制备的铜合金ZCuSn10Pb1液体进行成分检测,以确定其化学组成在国标要求范围之内;2) The composition of the prepared copper alloy ZCuSn 10 Pb 1 liquid is detected by using a Spike direct reading spectrometer to determine the chemical composition within the requirements of the national standard;
3)将高纯度碳化钛放入上述铜合金ZCuSn10Pb1液体的表面,开启工频电炉的震动装置并同时用石墨棒进行搅拌,使二者均匀混合;进一步升高电炉温度至1225℃并保持55min;3) placing high-purity titanium carbide on the surface of the above-mentioned copper alloy ZCuSn 10 Pb 1 liquid, turning on the vibration device of the power frequency electric furnace and simultaneously stirring with a graphite rod to uniformly mix the two; further raising the temperature of the electric furnace to 1225 ° C and Hold for 55 minutes;
4)将制作完成的高强度碳化钛颗粒增强铜基复合材料在电炉中进行保温,时间为1h;之后采用连续铸造的方式将此高强度碳化钛颗粒增强铜基复合材料铸造成高强度颗粒增强铜基合金复合棒材,铸造温度为1150℃;4) The finished high-strength titanium carbide particle reinforced copper-based composite material is kept in an electric furnace for 1 hour; then the high-strength titanium carbide particle-reinforced copper-based composite material is cast into high-strength particle reinforcement by continuous casting. Copper-based alloy composite bar, casting temperature is 1150 ° C;
5)将铸造完成之后的高强度颗粒增强铜基合金复合棒材进行表面车加工处理,并按照出厂标准包装。5) The high-strength particle-reinforced copper-based alloy composite bar after casting is surface-processed and packaged according to the factory standard.
实施例3Example 3
本发明实施例3的用于机车高速涡轮的高强度碳化钛颗粒增强铜基复合材料,各组分的体积百分比为纯度大于98%的高纯度碳化钛粉体1.5%,铜合金ZCuSn10Pb1 98.5%。A high-strength titanium carbide particle-reinforced copper-based composite material for a high-speed turbine of a locomotive according to Embodiment 3 of the present invention, wherein a volume percentage of each component is 1.5% of a high-purity titanium carbide powder having a purity of more than 98%, and a copper alloy ZCuSn 10 Pb 1 98.5%.
本发明实施例3的用于机车高速涡轮的高强度碳化钛颗粒增强铜基复合材料的制备方法,具有以下步骤(如图1所示):The method for preparing a high-strength titanium carbide particle reinforced copper-based composite material for a high-speed turbine of a locomotive according to Embodiment 3 of the present invention has the following steps (as shown in FIG. 1):
1)制备铜合金ZCuSn10Pb1:按照国标GB/T 1176-1987的标准将电解铜、磷铜合金,锡锭按照重量比例放入电炉中熔炼,熔炼中铜合金液体体积小于电炉体积的90%;熔炼温度为1200℃,时间为6h;1) Preparation of copper alloy ZCuSn 10 Pb 1 : Electrolytic copper, phosphor bronze alloy and tin ingot are smelted in an electric furnace according to the standard GB/T 1176-1987. The volume of the copper alloy liquid in the smelting is less than 90% of the volume of the electric furnace. %; melting temperature is 1200 ° C, time is 6h;
2)使用斯派克直读光谱仪对制备的铜合金ZCuSn10Pb1液体进行成分检测,以确定其化学组成在国标要求范围之内;2) The composition of the prepared copper alloy ZCuSn 10 Pb 1 liquid is detected by using a Spike direct reading spectrometer to determine the chemical composition within the requirements of the national standard;
3)将高纯度碳化钛放入上述铜合金ZCuSn10Pb1液体的表面,开启工频电炉的震动装置并同时用石墨棒进行搅拌,使二者均匀混合;进一步升高电炉温度至1250℃并保持60min;3) Put high-purity titanium carbide into the surface of the above-mentioned copper alloy ZCuSn 10 Pb 1 liquid, turn on the vibration device of the power frequency electric furnace and simultaneously stir with a graphite rod to uniformly mix the two; further increase the temperature of the electric furnace to 1250 ° C and Hold for 60 minutes;
4)将制作完成的高强度碳化钛颗粒增强铜基复合材料在电炉中进行 保温,时间为1.5h;之后采用连续铸造的方式将此高强度碳化钛颗粒增强铜基复合材料铸造成高强度颗粒增强铜基合金复合棒材,铸造温度为1200℃;4) The finished high-strength titanium carbide particle reinforced copper matrix composite material is carried out in an electric furnace Insulation, the time is 1.5h; then the high-strength titanium carbide particle-reinforced copper-based composite material is cast into a high-strength particle-reinforced copper-base alloy composite bar by continuous casting, and the casting temperature is 1200 ° C;
5)将铸造完成之后的高强度颗粒增强铜基合金复合棒材进行表面车加下处理,并按照出厂标准包装。5) The high-strength particle-reinforced copper-based alloy composite bar after casting is subjected to surface car treatment and packaged according to the factory standard.
比较例1Comparative example 1
添加传统元素镉、钛的铜合金材料,由以下组分组成:占合金材料总重量0.025%的镉,占合金材料总重量0.025%的钛,占合金材料总重量99.95%的铜合金ZCuSn10Pb1。通过传统的热处理工艺,即反复退火、回火及蘸火等热处理工艺,制备得到上述铜合金材料。The copper alloy material with the traditional element cadmium and titanium is composed of cadmium containing 0.025% by weight of the total weight of the alloy material, titanium of 0.025% by weight of the total weight of the alloy material, and copper alloy ZCuSn 10 Pb accounting for 99.95% of the total weight of the alloy material. 1 . The above copper alloy material is prepared by a conventional heat treatment process, that is, a heat treatment process such as repeated annealing, tempering, and bonfire.
比较例2Comparative example 2
添加传统元素镉、钛的铜合金材料,由以下组分组成:占合金材料总重量0.5%的镉,占合金材料总重量1.0%的钛,占合金材料总重量98.5%的铜合金ZCuSn10Pb1。通过传统的热处理工艺,即反复退火、回火及蘸火等热处理工艺,制备得到上述铜合金材料。The copper alloy material with traditional elements of cadmium and titanium is composed of cadmium which is 0.5% of the total weight of the alloy material, 1.0% of the total weight of the alloy material, and the copper alloy ZCuSn 10 Pb which accounts for 98.5% of the total weight of the alloy material. 1 . The above copper alloy material is prepared by a conventional heat treatment process, that is, a heat treatment process such as repeated annealing, tempering, and bonfire.
本发明的高强度碳化钛颗粒增强铜基复合材料以及上述比较例1和2的传统铜合金材料的机械性能如表1所示。 The mechanical properties of the high-strength titanium carbide particle-reinforced copper-based composite material of the present invention and the conventional copper alloy materials of Comparative Examples 1 and 2 described above are shown in Table 1.
表1Table 1
Figure PCTCN2015000866-appb-000001
Figure PCTCN2015000866-appb-000001
由上表1可见,通过本发明的采用碳化钛颗粒增强铜基复合材料(实施例1-3)相较于传统的含镉、钛的铜合金材料,其强度有明显提高,耐磨性和耐腐蚀性也得到了显著提高。It can be seen from the above Table 1 that the strength of the copper-based composite material (Example 1-3) using the titanium carbide particles of the present invention is significantly improved compared with the conventional copper alloy materials containing cadmium and titanium, and the wear resistance and Corrosion resistance has also been significantly improved.
以上所述实施例仅表达了本发明的实施方式,其描述较为具体和详细,但并不能因此而理解为对本发明专利范围的限制。应当指出的是,对于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。 The above-mentioned embodiments are merely illustrative of the embodiments of the present invention, and the description thereof is not to be construed as limiting the scope of the invention. It should be noted that a number of variations and modifications may be made by those skilled in the art without departing from the spirit and scope of the invention.

Claims (10)

  1. 一种用于机车高速涡轮的高强度碳化钛颗粒增强铜基复合材料,其特征在于,由如下体积百分比的组分组成:纯度大于98%的高纯度碳化钛0.05-1.5%,铜合金ZCuSn10Pb198.5-99.95%。A high-strength titanium carbide particle reinforced copper-based composite material for a high-speed turbine of a locomotive, characterized by comprising: a high-purity titanium carbide having a purity of more than 98%, 0.05-1.5%, a copper alloy ZCuSn 10 Pb 1 98.5-99.95%.
  2. 根据权利要求1所述的高强度碳化钛颗粒增强铜基复合材料,其特征在于,由如下体积百分比的组分组成:纯度大于98%的高纯度碳化钛0.05%,铜合金ZCuSn10Pb199.95%。The high-strength titanium carbide particle-reinforced copper-based composite material according to claim 1, which is composed of the following components by volume: high-purity titanium carbide having a purity of more than 98% 0.05%, copper alloy ZCuSn 10 Pb 1 99.95 %.
  3. 根据权利要求1所述的高强度碳化钛颗粒增强铜基复合材料,其特征在于,由如下体积百分比的组分组成:纯度大于98%的高纯度碳化钛0.8%,铜合金ZCuSn10Pb199.2%。The high-strength titanium carbide particle-reinforced copper-based composite material according to claim 1, which is composed of the following components by volume: high-purity titanium carbide having a purity of more than 98% 0.8%, copper alloy ZCuSn 10 Pb 1 99.2 %.
  4. 根据权利要求1所述的高强度碳化钛颗粒增强铜基复合材料,其特征在于,由如下体积百分比的组分组成:纯度大于98%的高纯度碳化钛1.5%,铜合金ZCuSn10Pb198.5%。The high-strength titanium carbide particle-reinforced copper-based composite material according to claim 1, which is composed of the following components by volume: high-purity titanium carbide having a purity of more than 98%: 1.5%, copper alloy ZCuSn 10 Pb 1 98.5 %.
  5. 根据权利要求1-4中任一项的高强度碳化钛颗粒增强铜基复合材料,其特征在于,所述高纯度碳化钛为粉体颗粒。The high-strength titanium carbide particle-reinforced copper-based composite material according to any one of claims 1 to 4, wherein the high-purity titanium carbide is a powder particle.
  6. 根据权利要求1-4中任一项的高强度碳化钛颗粒增强铜基复合材料,其特征在于,所述铜合金ZCuSn10Pb1由如下重量百分比的组分组成:锡锭9.0-11.5%,磷铜合金0.5-1.0%,杂质总和≤0.75%,其余为铜。The high-strength titanium carbide particle-reinforced copper-based composite material according to any one of claims 1 to 4, wherein the copper alloy ZCuSn 10 Pb 1 is composed of the following components by weight: 9.0-11.5% of tin ingot, Phosphorus copper alloy 0.5-1.0%, the total impurity is ≤0.75%, and the rest is copper.
  7. 一种用于机车高速涡轮的高强度碳化钛颗粒增强铜基复合材料的制备方法,其特征在于,具有以下步骤:A method for preparing a high-strength titanium carbide particle reinforced copper-based composite material for a high-speed turbine of a locomotive, characterized in that the method has the following steps:
    1)制备铜合金ZCuSn10Pb1:将电解铜、磷铜合金,锡锭按照权利要求6所述的重量比例放入电炉中熔炼,熔炼中铜合金液体体积小于电炉体积的90%;熔炼温度为1150-1200℃,时间为5-6h;1) preparing copper alloy ZCuSn 10 Pb 1 : electrolytic copper, phosphor bronze alloy, tin ingot according to the weight ratio of claim 6 is placed in an electric furnace for melting, the volume of the copper alloy liquid in the melting is less than 90% of the volume of the electric furnace; the melting temperature It is 1150-1200 ° C, the time is 5-6h;
    2)使用斯派克直读光谱仪对制备的铜合金ZCuSn10Pb1液体进行成分检测,以确定其化学组成在权利要求6所述的范围之内;2) performing component detection on the prepared copper alloy ZCuSn 10 Pb 1 liquid using a Spike direct reading spectrometer to determine that its chemical composition is within the scope of claim 6;
    3)将高纯度碳化钛颗粒按体积百分比为0.05-1.5%放入上述铜合金 ZCuSn10Pb1液体的表面,开启工频电炉的震动装置并同时用石墨棒进行搅拌,使二者均匀混合;进一步升高电炉温度至1200-1250℃并保持50-60min;3) placing high-purity titanium carbide particles in a volume percentage of 0.05-1.5% on the surface of the above-mentioned copper alloy ZCuSn 10 Pb 1 liquid, turning on the vibration device of the power frequency electric furnace and simultaneously stirring with a graphite rod to uniformly mix the two; Further raising the temperature of the electric furnace to 1200-1250 ° C and maintaining 50-60 min;
    4)将制作完成的高强度碳化钛颗粒增强铜基复合材料在电炉中进行保温,时间为1-1.5h;之后采用连续铸造的方式将此高强度碳化钛颗粒增强铜基复合材料铸造成高强度颗粒增强铜基合金复合棒材,铸造温度为1150-1200℃;4) The finished high-strength titanium carbide particle reinforced copper-based composite material is kept in an electric furnace for a period of 1-1.5 hours; then the high-strength titanium carbide particle-reinforced copper-based composite material is cast into a high casting method. Intensity particle reinforced copper-based alloy composite bar, casting temperature is 1150-1200 ° C;
    5)将铸造完成之后的高强度颗粒增强铜基合金复合棒材进行表面车加工处理,并按照出厂标准包装。5) The high-strength particle-reinforced copper-based alloy composite bar after casting is surface-processed and packaged according to the factory standard.
  8. 根掘权利要求7所述的制备方法,其特征在于,步骤3中,所述高纯度碳化钛颗粒的体积百分比为0.05%。The preparation method according to claim 7, wherein in step 3, the volume fraction of the high-purity titanium carbide particles is 0.05%.
  9. 根据权利要求7所述的制备方法,其特征在于,步骤3中,所述高纯度碳化钛颗粒的体积百分比为0.8%。The preparation method according to claim 7, wherein in step 3, the volume fraction of the high-purity titanium carbide particles is 0.8%.
  10. 根据权利要求7所述的制备方法,其特征在于,步骡3中,所述高纯度碳化钛颗粒的体积百分比为1.5%。 The production method according to claim 7, wherein in step 3, the volume fraction of the high-purity titanium carbide particles is 1.5%.
PCT/CN2015/000866 2015-10-30 2015-12-04 High-strength titanium carbide particle-reinforced copper-based composite material and preparation method therefor WO2017070806A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN201510728060.XA CN105256170A (en) 2015-10-30 2015-10-30 High-strength titanium carbide particle-reinforced copper-based composite material and preparation method thereof
CN201510728060.X 2015-10-30

Publications (1)

Publication Number Publication Date
WO2017070806A1 true WO2017070806A1 (en) 2017-05-04

Family

ID=55096095

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2015/000866 WO2017070806A1 (en) 2015-10-30 2015-12-04 High-strength titanium carbide particle-reinforced copper-based composite material and preparation method therefor

Country Status (2)

Country Link
CN (1) CN105256170A (en)
WO (1) WO2017070806A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115198211A (en) * 2022-07-05 2022-10-18 贵州航天天马机电科技有限公司 Toughening method of TiCx-Cu cermet
CN117025014A (en) * 2023-07-28 2023-11-10 浙江大学 Preparation method of neodymium-iron-boron magnet anti-corrosion composite slurry

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105671397A (en) * 2016-01-23 2016-06-15 中山百鸥医药科技有限公司 Worm gear of grain packing machine for processing omega-3 fish oil soft capsules
CN110439581B (en) * 2019-09-04 2021-12-03 郑州机械研究所有限公司 Wear-resistant material, wear-resistant cutter ring and shield tunneling machine

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61149449A (en) * 1984-12-24 1986-07-08 Sumitomo Electric Ind Ltd Composite material for lead frame for semiconductor device and its production
JPH02118002A (en) * 1988-10-27 1990-05-02 Komatsu Ltd Sintered laminating body for copper alloy powder sheet
CN1718795A (en) * 2005-07-11 2006-01-11 合肥波林新材料有限公司 Leadless copper base high temperature self lubricating composite material
CN104630544A (en) * 2015-01-27 2015-05-20 苏州金仓合金新材料有限公司 Novel composite copper-based alloy material for high speed railway and preparation method of novel composite copper-based alloy material

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100336929C (en) * 2005-01-12 2007-09-12 中国科学院金属研究所 In-situ produced titanium carbide dispersion strengthening copper based composite material and method for preparing the same

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61149449A (en) * 1984-12-24 1986-07-08 Sumitomo Electric Ind Ltd Composite material for lead frame for semiconductor device and its production
JPH02118002A (en) * 1988-10-27 1990-05-02 Komatsu Ltd Sintered laminating body for copper alloy powder sheet
CN1718795A (en) * 2005-07-11 2006-01-11 合肥波林新材料有限公司 Leadless copper base high temperature self lubricating composite material
CN104630544A (en) * 2015-01-27 2015-05-20 苏州金仓合金新材料有限公司 Novel composite copper-based alloy material for high speed railway and preparation method of novel composite copper-based alloy material

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115198211A (en) * 2022-07-05 2022-10-18 贵州航天天马机电科技有限公司 Toughening method of TiCx-Cu cermet
CN117025014A (en) * 2023-07-28 2023-11-10 浙江大学 Preparation method of neodymium-iron-boron magnet anti-corrosion composite slurry
CN117025014B (en) * 2023-07-28 2024-04-16 浙江大学 Preparation method of neodymium-iron-boron magnet anti-corrosion composite slurry

Also Published As

Publication number Publication date
CN105256170A (en) 2016-01-20

Similar Documents

Publication Publication Date Title
CN107099708B (en) A kind of graphene rare earth aluminium alloy height leads the preparation method of material
WO2017070806A1 (en) High-strength titanium carbide particle-reinforced copper-based composite material and preparation method therefor
CN103526085A (en) Wear-proof aluminum alloy
CN113278846B (en) Wear-resistant copper-nickel-tin alloy and preparation method thereof
CN104630556A (en) Ultrahigh-strength high-toughness high corrosion-resisting CuNiSiNbSn elastic copper alloy and preparation method thereof
CN105908218B (en) A kind of high pure rare earth metals and its production and use
CN104862552A (en) Novel aluminum alloy and preparation method thereof
CN109112367B (en) Graphene-reinforced Al-Si-Mg cast aluminum alloy and preparation method thereof
WO2018028094A1 (en) Silicon carbide, antimony, tin, zinc and copper composite material for high-speed railway locomotive and preparation method therefor
CN107130157B (en) A kind of rare earth antifriction alloy
JP2022512995A (en) A type of alloy material and its production process
CN105177348A (en) High-strength titanium carbide copper-based composite material and preparation method thereof
CN104946925A (en) Treatment technology of copper aluminum alloy material for bus duct
CN103789569B (en) Bearing holder material and manufacture method thereof
CN113249630A (en) Forging and pressing process of high-entropy alloy
CN112410597A (en) Preparation method of nano WC dispersion strengthened copper
WO2018028091A1 (en) Copper-based composite material for mechanical part and preparation method therefor
WO2017075741A1 (en) Novel high-strength nanoscale silicon carbide copper-based composite alloy material for high-speed locomotive gears
CN103436751A (en) Corrosion-resistant casting aluminum alloy for pump shell and manufacturing method thereof
CN105200264A (en) High-strength titanium diboride particle enhanced copper-based composite and preparation method thereof
CN105256169A (en) High-strength nanometer silicon carbide strengthening copper-based composite material and preparing method thereof
WO2017070808A1 (en) Titanium carbide particle-reinforced copper-based composite alloy material
CN105385888A (en) High-strength particle copper-based composite alloy new material for high-load connecting rod of haulage motor
CN105220000A (en) A kind of high strength titanium diboride particle enhanced copper-based composite material and preparation method thereof
CN112342436B (en) Nanoparticle reinforced ZTC4 titanium alloy and preparation method thereof

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 15906872

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 15906872

Country of ref document: EP

Kind code of ref document: A1