WO2017075740A1 - 一种车辆轴承用镀镍碳化硅颗粒增强铜基复合材料及其制备方法 - Google Patents

一种车辆轴承用镀镍碳化硅颗粒增强铜基复合材料及其制备方法 Download PDF

Info

Publication number
WO2017075740A1
WO2017075740A1 PCT/CN2015/000859 CN2015000859W WO2017075740A1 WO 2017075740 A1 WO2017075740 A1 WO 2017075740A1 CN 2015000859 W CN2015000859 W CN 2015000859W WO 2017075740 A1 WO2017075740 A1 WO 2017075740A1
Authority
WO
WIPO (PCT)
Prior art keywords
nickel
silicon carbide
plated silicon
composite material
based composite
Prior art date
Application number
PCT/CN2015/000859
Other languages
English (en)
French (fr)
Inventor
孙飞
赵勇
埃里克斯•高登
Original Assignee
苏州金仓合金新材料有限公司
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 苏州金仓合金新材料有限公司 filed Critical 苏州金仓合金新材料有限公司
Publication of WO2017075740A1 publication Critical patent/WO2017075740A1/zh

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C1/00—Making non-ferrous alloys
    • C22C1/10—Alloys containing non-metals
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C32/00—Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C9/00—Alloys based on copper

Definitions

  • the invention relates to a copper matrix composite material, in particular to a nickel-plated silicon carbide particle reinforced copper matrix composite material for vehicle bearings and a preparation method thereof.
  • Nano-SiC is a kind of nano-material prepared on the basis of common silicon carbide materials through certain technical conditions. Nano-SiC has high purity, small particle size, uniform distribution, large specific surface area, high surface activity, low bulk density, excellent mechanical, thermal, electrical and chemical properties, ie high hardness, high wear resistance and good Self-lubricating, high thermal conductivity, low thermal expansion coefficient and high temperature strength. Therefore, it can be used for addition to an alloy to improve the strength, hardness, and the like of the base alloy, but silicon carbide is used as a non-metal compound, the molten matrix alloy does not wet the reinforcing particles, and the interfacial reaction between the phase particles and the matrix alloy is prone to occur.
  • the degree of bonding (ie, compatibility) of the interface largely determines the properties of the composite; at the same time, due to the lower density of silicon carbide (3.2 g/cm 3 ), and heavy metals (copper) When the alloy and iron alloy solution are fused, serious floating will occur, which will lead to serious segregation of the composite material, which will affect the performance and application of the composite. Therefore, a new medium must be sought to facilitate the fusion of silicon carbide and heavy metals so that the two can be fully integrated to facilitate the next production process.
  • Tin-lead bronze (ZCuSn 10 Pb 10 ) is a cast copper alloy with good lubricity, wear resistance and corrosion resistance. It is mainly used to manufacture sliding bearings with high surface pressure and side pressure, such as rolls and vehicle bearings. Impacted parts with a load peak of 60 MPa, and bimetallic bushings of internal combustion engines with a peak of up to 100 MPa, as well as piston pin bushings, friction plates, etc. However, the application in impact parts with a load higher than 60 MPa is limited. Therefore, in order to extend the service life of tin-lead bronze (ZCuSn 10 Pb 10 ) in vehicle bearings and corresponding friction plates, tin-lead bronze (ZCuSn 10 Pb 10 ) is improved. The relevant performance is essential.
  • an object of the present invention is to provide a nickel-plated silicon carbide particle-reinforced copper-based composite material for a vehicle bearing and a preparation method thereof, and a nickel-plated silicon carbide particle-reinforced copper base for a vehicle bearing prepared
  • the composite material has a significant improvement in strength and hardness, and expands the application of the original tin-lead bronze (ZCuSn 10 Pb 10 ) in impact parts with a load of 100 MPa.
  • a nickel-plated silicon carbide particle-reinforced copper-based composite material for a vehicle bearing wherein the composition of the copper-based composite material comprises nickel-plated silicon carbide particles (Ni-SiC), rare earth, tin-lead bronze (ZCuSn 10 Pb 10 ), wherein the copper base
  • Ni-SiC nickel-plated silicon carbide particles
  • ZCuSn 10 Pb 10 tin-lead bronze
  • the copper base The composition of each component of the composite material is as follows: nickel-plated silicon carbide particles (Ni-SiC): 15-20%, rare earth: 0.05-0.5%, tin-lead bronze (ZCuSn 10 Pb 10 ): 79.5-84.95%.
  • composition of each component of the copper-based composite material is: nickel-plated silicon carbide particles (Ni-SiC): 16-18%, rare earth: 0.1-0.4%, tin-lead bronze (ZCuSn 10 Pb 10 ): 81.6-83.9%.
  • the nickel-plated silicon carbide particles are produced by a known chemical method, and the nickel-plated silicon carbide particles have a particle diameter in the range of 0.5 ⁇ m to 35 ⁇ m.
  • the rare earth contains 20% by weight of lanthanum (La) and 15% by weight of cerium (Ce).
  • a method for preparing a nickel-plated silicon carbide particle-reinforced copper-based composite material for a vehicle bearing comprising the following steps:
  • Step 1 mixing the nickel-plated silicon carbide particles with the rare earth in a predetermined ratio
  • Step 2 The electrolytic copper, tin ingot and lead ingot are in accordance with the requirements of national standard GB/T1176-2013 at 500. Melting in a medium-frequency electric furnace of kilogram capacity;
  • Step 3 Perform component detection on the smelted copper alloy solution by using a Spike direct reading spectrometer
  • Step 4 placing the nickel-plated silicon carbide and rare earth mixture pre-mixed in step 1 on the smelted copper alloy solution, and stirring with a graphite rod;
  • Step 5 Pour the stirred copper alloy solution into the holding furnace, and open the vibration device of the holding furnace;
  • Step 6 heat preservation, then open the casting device and cast the blank profile according to the predetermined product shape
  • Step 7 The finished blank profile is surface treated and packaged into a warehouse.
  • the melting temperature in the step 2 is from 1000 ° C to 1100 ° C, and the melting time is from 1.5 to 2 hours.
  • the stirring rate in the step 4 is 3 times/second, and the stirring time is 15-20 minutes.
  • the temperature of the holding furnace in the step 5 is 1100 ° C to 1150 ° C
  • the vibration frequency of the vibration device is set to 25-30 times / sec
  • the time of the vibration device is set to 25-30 minutes.
  • the holding time in the step 6 is 1-1.5 hours
  • the holding temperature is 900 ° C - 1000 ° C
  • the casting temperature is 850 ° C - 900 ° C:
  • the nickel-bearing silicon carbide particle-reinforced copper-based composite material for vehicle bearing of the invention is selected from the nickel-plated nano-silicon carbide material and the rare earth material, and is uniformly distributed in the existing alloy material by a certain technical means, and the nickel-plated nano-scale carbonization is utilized. Silicon high hardness, high wear resistance and good self-lubricating and high temperature strength properties, and through its good wettability, strengthen the combination with the original tin-lead bronze (ZCuSn 10 Pb 10 ) alloy to achieve tin-lead bronze ( Further improvement in the properties of ZCuSn 10 Pb 10 ) alloy materials.
  • the nickel-plated silicon carbide particle-reinforced copper-based composite material for vehicle bearing prepared by the method of the invention has higher strength and hardness, so that it can be extended to impact parts with a load of 100 MPa, and extended in the bearing and corresponding under the same conditions.
  • the age of use in the friction lining is not limited.
  • the invention provides a nickel-plated silicon carbide particle-reinforced copper-based composite material for a vehicle bearing, wherein the composition of the copper-based composite material comprises nickel-plated silicon carbide particles (Ni-SiC), rare earth, tin-lead bronze (ZCuSn 10 Pb 10 ), wherein The composition of each component of the copper matrix composite is by weight: nickel-plated silicon carbide particles (Ni-SiC): 15-20%, rare earth: 0.05-0.5%, tin-lead bronze (ZCuSn 10 Pb 10 ): 79.5-84.95 %.
  • the nickel-plated silicon carbide particles are obtained by a known chemical method, and the nickel-plated silicon carbide particles have a particle diameter in the range of 0.5 ⁇ m to 35 ⁇ m.
  • the rare earth contains 20% by weight of lanthanum (La) and 15% by weight of cerium (Ce).
  • the casting of tin-lead bronze (ZCuSn 10 Pb 10 ) is in accordance with the national standard GB/T 1176-2013.
  • the invention provides a method for preparing a nickel-plated silicon carbide particle reinforced copper matrix composite material for a vehicle bearing, comprising the following steps:
  • Step 1 mixing the nickel-plated silicon carbide particles with the rare earth in a predetermined ratio
  • Step 2 The electrolytic copper, tin ingot and lead ingot are smelted in a medium-frequency electric furnace of 500 kg capacity according to the requirements of national standard GB/T1176-2013, the melting temperature is 1000 ° C -1100 ° C, and the melting time is 1.5-2 hours;
  • Step 3 Using a Spike direct reading spectrometer to carry out component detection on the smelted copper alloy solution to determine that the chemical composition of the copper alloy solution is within the requirements of the national standard, and to ensure that the copper alloy solution accounts for less than 80% of the volume of the melting furnace;
  • Step 4 Place the nickel-plated silicon carbide and rare earth mixture pre-mixed in step 1 on the smelted copper alloy solution, and stir with a graphite rod.
  • the stirring rate is 3 times/second, and the stirring time is 15-20. minute;
  • Step 5 Pour the stirred copper alloy solution into the holding furnace, and turn on the vibration device of the holding furnace.
  • the vibration frequency of the vibration device is set to 25-30 times/second, and the time of the vibration device is set to 25-30 minutes.
  • the temperature of the holding furnace is 1100 ° C - 1150 ° C;
  • Step 6 Insulation for 1-1.5 hours, holding temperature of 900 ° C -1000 ° C, and opening the casting device, casting temperature is 850 ° C -900 ° C, casting the blank profile according to the predetermined product shape;
  • Step 7 The finished blank profile is surface treated and packaged into a warehouse.
  • Embodiment 1 is a diagrammatic representation of Embodiment 1:
  • Ni-SiC nickel-plated silicon carbide particles
  • rare earth 0.05%
  • tin-lead bronze ZCuSn 10 Pb 10
  • the nickel-plated silicon carbide particles are obtained by a known chemical method, and the nickel-plated silicon carbide particles have a particle diameter of 0.5 ⁇ m.
  • the rare earth contains 20% by weight of lanthanum (La) and 15% by weight of cerium (Ce).
  • the casting of tin-lead bronze (ZCuSn 10 Pb 10 ) is in accordance with the national standard GB/T 1176-2013.
  • the nickel-plated silicon carbide particles are mixed with the rare earth in a predetermined ratio.
  • the electrolytic copper, tin ingot and lead ingot are smelted in a medium-frequency electric furnace of 500 kg capacity according to the requirements of the national standard GB/T1176-2013, the melting temperature is 1000 ° C, and the melting time is 1.5 hours.
  • the Spike direct reading spectrometer is used to test the composition of the smelted copper alloy solution to determine the chemical composition of the copper alloy solution within the requirements of the national standard, and to ensure that the copper alloy solution accounts for less than 80% of the volume of the melting furnace.
  • the pre-mixed nickel-plated silicon carbide and rare earth mixture was placed on the smelted copper alloy solution and stirred with a graphite rod at a stirring rate of 3 times/second and a stirring time of 15 minutes.
  • the stirred copper alloy solution is poured into the holding furnace, and the vibration device of the holding furnace is turned on.
  • the vibration frequency of the vibration device is set to 25 times/second, the time of the vibration device is set to 25 minutes, and the temperature of the holding furnace is set. It is 1100 ° C.
  • the temperature was maintained for 1 hour, the holding temperature was 900 ° C, and the casting apparatus was opened, and the casting temperature was 850 ° C, and the blank profile was cast in accordance with the predetermined product shape.
  • the finished blank profile is surface treated and packaged into the warehouse.
  • Nickel SiC particle reinforced copper matrix composites have a longer life span than the original tin-lead bronze (ZCuSn 10 Pb 10 ) for two years in vehicle bearings and corresponding friction linings.
  • Embodiment 2 is a diagrammatic representation of Embodiment 1:
  • Ni-SiC nickel-plated silicon carbide particles
  • rare earth 0.1%
  • tin-lead bronze ZCuSn 10 Pb 10
  • the nickel-plated silicon carbide particles are obtained by a known chemical method, and the nickel-plated silicon carbide particles have a particle diameter of 10 ⁇ m.
  • the rare earth contains 20% by weight of lanthanum (La) and 15% by weight of cerium (Ce).
  • the casting of tin-lead bronze (ZCuSn 10 Pb 10 ) is in accordance with the national standard GB/T 1176-2013.
  • the nickel-plated silicon carbide particles are mixed with the rare earth in a predetermined ratio.
  • the electrolytic copper, tin ingot and lead ingot are smelted in a medium-frequency electric furnace of 500 kg capacity according to the requirements of the national standard GB/T1176-2013, the melting temperature is 1030 ° C, and the melting time is 1.6 hours.
  • the Spike direct reading spectrometer is used to test the composition of the smelted copper alloy solution to determine the chemical composition of the copper alloy solution within the requirements of the national standard, and to ensure that the copper alloy solution accounts for less than 80% of the volume of the melting furnace.
  • the pre-mixed nickel-plated silicon carbide and rare earth mixture was placed on the smelted copper alloy solution and stirred with a graphite rod at a stirring rate of 3 times/second and a stirring time of 16 minutes.
  • the stirred copper alloy solution is poured into the holding furnace, and the vibration device of the holding furnace is turned on.
  • the vibration frequency of the vibration device is set to 26 times/second, the time of the vibration device is set to 26 minutes, and the temperature of the holding furnace is set. It is 1120 ° C.
  • the insulation was held for 1.2 hours, the holding temperature was 930 ° C, and the casting apparatus was started.
  • the casting temperature was 860 ° C, and the blank profile was cast in accordance with the predetermined product shape.
  • the finished blank profile is surface treated and packaged into the warehouse.
  • Nickel SiC particle reinforced copper matrix composites have a longer life span than the original tin-lead bronze (ZCuSn 10 Pb 10 ) for 2.5 years in vehicle bearings and corresponding friction linings.
  • Embodiment 3 is a diagrammatic representation of Embodiment 3
  • Ni-SiC nickel-plated silicon carbide particles
  • rare earth 0.3%
  • tin-lead bronze ZCuSn 10 Pb 10
  • the nickel-plated silicon carbide particles are obtained by a known chemical method, and the nickel-plated silicon carbide particles have a particle diameter of 18 ⁇ m.
  • the rare earth contains 20% by weight of lanthanum (La) and 15% by weight of cerium (Ce).
  • the casting of tin-lead bronze (ZCuSn 10 Pb 10 ) is in accordance with the national standard GB/T 1176-2013.
  • the nickel-plated silicon carbide particles are mixed with the rare earth in a predetermined ratio.
  • the electrolytic copper, tin ingot and lead ingot were smelted in a medium-frequency electric furnace of 500 kg capacity according to the requirements of the national standard GB/T1176-2013, the melting temperature was 1060 ° C, and the melting time was 1.9 hours.
  • the Spike direct reading spectrometer is used to test the composition of the smelted copper alloy solution to determine the chemical composition of the copper alloy solution within the requirements of the national standard, and to ensure that the copper alloy solution accounts for less than 80% of the volume of the melting furnace.
  • the pre-mixed nickel-plated silicon carbide and rare earth mixture was placed on the smelted copper alloy solution and stirred with a graphite rod at a stirring rate of 3 times/second and a stirring time of 17 minutes.
  • the stirred copper alloy solution is poured into the holding furnace, and the vibration device of the holding furnace is turned on.
  • the vibration frequency of the vibration device is set to 28 times/second, the time of the vibration device is set to 28 minutes, and the temperature of the holding furnace is set. It is 1130 ° C.
  • the insulation was maintained for 1.3 hours, the holding temperature was 960 ° C, and the casting apparatus was opened, and the casting temperature was 880 ° C, and the blank profile was cast in accordance with the predetermined product shape.
  • the finished blank profile is surface treated and packaged into the warehouse.
  • Nickel SiC particle reinforced copper matrix composites have a longer life span than the original tin-lead bronze (ZCuSn 10 Pb 10 ) for three years in vehicle bearings and corresponding friction linings.
  • Embodiment 4 is a diagrammatic representation of Embodiment 4:
  • Ni-SiC nickel-plated silicon carbide particles
  • rare earth 0.4%
  • tin-lead bronze ZCuSn 10 Pb 10
  • the nickel-plated silicon carbide particles are obtained by a known chemical method, and the nickel-plated silicon carbide particles have a particle diameter of 25 ⁇ m.
  • the rare earth contains 20% by weight of lanthanum (La) and 15% by weight of cerium (Ce).
  • the casting of tin-lead bronze (ZCuSn 10 Pb 10 ) is in accordance with the national standard GB/T 1176-2013.
  • the nickel-plated silicon carbide particles are mixed with the rare earth in a predetermined ratio.
  • the electrolytic copper, tin ingot and lead ingot were smelted in a medium-frequency electric furnace of 500 kg capacity according to the requirements of the national standard GB/T1176-2013, the melting temperature was 1080 ° C, and the melting time was 1.8 hours.
  • the Spike direct reading spectrometer is used to test the composition of the smelted copper alloy solution to determine the chemical composition of the copper alloy solution within the requirements of the national standard, and to ensure that the copper alloy solution accounts for less than 80% of the volume of the melting furnace.
  • the pre-mixed nickel-plated silicon carbide and rare earth mixture was placed on the smelted copper alloy solution and stirred with a graphite rod at a stirring rate of 3 times/second and a stirring time of 19 minutes.
  • the stirred copper alloy solution is poured into the holding furnace, and the vibration device of the holding furnace is turned on.
  • the vibration frequency of the vibration device is set to 29 times/second, and the time of the vibration device is set to 29 minutes, and the temperature of the holding furnace is set. It is 1140 ° C.
  • the insulation was heated for 1.4 hours, the holding temperature was 980 ° C, and the casting apparatus was started.
  • the casting temperature was 890 ° C, and the blank profile was cast in accordance with the predetermined product shape.
  • the finished blank profile is surface treated and packaged into the warehouse.
  • Nickel SiC particle reinforced copper matrix composites have a longer life span than the original tin-lead bronze (ZCuSn 10 Pb 10 ) in vehicle bearings and corresponding friction linings for 4 years.
  • Embodiment 5 is a diagrammatic representation of Embodiment 5:
  • Ni-SiC nickel-plated silicon carbide particles
  • rare earth 0.5%
  • tin-lead bronze ZCuSn 10 Pb 10
  • the nickel-plated silicon carbide particles are obtained by a known chemical method, and the nickel-plated silicon carbide particles have a particle diameter of 35 ⁇ m.
  • the rare earth contains 20% by weight of lanthanum (La) and 15% by weight of cerium (Ce).
  • the casting of tin-lead bronze (ZCuSn 10 Pb 10 ) is in accordance with the national standard GB/T 1176-2013.
  • the nickel-plated silicon carbide particles are mixed with the rare earth in a predetermined ratio.
  • the electrolytic copper, tin ingot and lead ingot are smelted in a medium-frequency electric furnace of 500 kg capacity according to the requirements of the national standard GB/T1176-2013, the melting temperature is 1100 ° C, and the melting time is 2 hours.
  • the Spike direct reading spectrometer is used to test the composition of the smelted copper alloy solution to determine the chemical composition of the copper alloy solution within the requirements of the national standard, and to ensure that the copper alloy solution accounts for less than 80% of the volume of the melting furnace.
  • the pre-mixed nickel-plated silicon carbide and rare earth mixture was placed on the smelted copper alloy solution and stirred with a graphite rod at a stirring rate of 3 times/second and a stirring time of 20 minutes.
  • the stirred copper alloy solution is poured into the holding furnace, and the vibration device of the holding furnace is turned on.
  • the vibration frequency of the vibration device is set to 30 times/second, the time of the vibration device is set to 30 minutes, and the temperature of the holding furnace is set. It is 1150 ° C.
  • the insulation was heated for 1.5 hours, the holding temperature was 1000 ° C, and the casting apparatus was started.
  • the casting temperature was 900 ° C, and the blank profile was cast in accordance with the predetermined product shape.
  • the finished blank profile is surface treated and packaged into the warehouse.
  • the strength and hardness of the nickel-plated silicon carbide particle-reinforced copper matrix composites prepared for vehicle bearings are increased by 38% and 43%, respectively, compared with the original tin-lead bronze (ZCuSn 10 Pb 10 ).
  • the use of nickel-silicon carbide reinforced copper matrix composites in vehicle bearings and corresponding friction linings has been extended by 3.5 years compared to the original tin-lead bronze (ZCuSn 10 Pb 10 ).

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Electroplating Methods And Accessories (AREA)
  • Sliding-Contact Bearings (AREA)

Abstract

一种车辆轴承用镀镍碳化硅颗粒增强铜基复合材料，其成分包含镀镍碳化硅颗粒(Ni-SiC)、稀土、锡铅青铜(ZCuSn10Pb10)，其中各成分组成按重量百分比分别为：镀镍碳化硅颗粒(Ni-SiC)：15-20％，稀土：0.05-0.5％，锡铅青铜(ZCuSn10Pb10)：79.5-84.95％。还提供了一种该车辆轴承用镀镍碳化硅颗粒增强铜基复合材料的制备方法。

Description

一种车辆轴承用镀镍碳化硅颗粒增强铜基复合材料及其制备方法 技术领域
本发明涉及铜基复合材料，特别是涉及一种车辆轴承用镀镍碳化硅颗粒增强铜基复合材料及其制备方法。
背景技术
纳米碳化硅是一种通过一定的技术条件，在普通碳化硅材料的基础上制备出的一种纳米材料。纳米碳化硅具有纯度高、粒径小、分布均匀、比表面积大、高表面活性、松装密度低，极好的力学、热学、电学和化学性能，即具有高硬度、高耐磨性和良好的自润滑、高热传导率、低热膨胀系数及高温强度大等特点。因此可用于添加到合金当中以提高母基合金的强度、硬度等，但是碳化硅作为非金属化合物，熔融的基体合金对增强粒子不湿润，以及增强相颗粒与基体合金之间容易发生界面反应，由于界面是复合材料极其重要的组成部分，界面的结合程度(即相容性)很大程度决定了复合材料的性质；同时由于碳化硅密度较低(3.2g/cm3)，与重金属(铜合金、铁合金)溶液融合时会产生严重的上浮，导致复合材料偏析问题严重，从而影响复合材料的性能及应用。因此必须寻求一种新的介质以便于碳化硅与重金属的融合而使二者之间能够充分融合，从而便于下一步生产处理。
锡铅青铜(ZCuSn10Pb10)是一种润滑性、耐磨性和耐腐蚀性较好的铸造铜合金，主要用于制造表面压力高又存在侧压力的滑动轴承，如轧辊、车辆轴承、负载峰值达60MPa的受冲击零件，和最高峰值达100MPa的内燃机双金属轴瓦，以及活塞销套、摩擦片等。但是在负载高于60MPa的冲击零件中的应用受到了限制，因此为了延长锡铅青铜(ZCuSn10Pb10)在 车辆轴承及相应摩擦片中的使用年限，提高锡铅青铜(ZCuSn10Pb10)的相关性能是必不可少的。
发明内容
针对上述现有技术中存在的问题，本发明的目的在于提供一种车辆轴承用镀镍碳化硅颗粒增强铜基复合材料及其制备方法，所制备的车辆轴承用镀镍碳化硅颗粒增强铜基复合材料在强度和硬度方面具有明显提升，拓展原锡铅青铜(ZCuSn10Pb10)在负载100MPa的冲击零件中的应用。
为了实现上述发明目的，本发明采用的技术方案如下：
一种车辆轴承用镀镍碳化硅颗粒增强铜基复合材料，铜基复合材料的成分包含镀镍碳化硅颗粒(Ni-SiC)、稀土、锡铅青铜(ZCuSn10Pb10)，其中，铜基复合材料的各成分组成按重量百分比分别为：镀镍碳化硅颗粒(Ni-SiC)：15-20％，稀土：0.05-0.5％，锡铅青铜(ZCuSn10Pb10)：79.5-84.95％。
进一步地，铜基复合材料的各成分组成按重量百分比分别为：镀镍碳化硅颗粒(Ni-SiC)：16-18％，稀土：0.1-0.4％，锡铅青铜(ZCuSn10Pb10)：81.6-83.9％。
进一步地，镀镍碳化硅颗粒是通过已知的化学方法制得，镀镍碳化硅颗粒的粒径在0.5μm-35μm范围内。
进一步地，稀土中包含重量百分比20％的镧(La)和重量百分比15％的铈(Ce)。
进一步地，锡铅青铜(ZCuSn10Pb10)的铸造是按照国标GB/T 1176-2013的标准。
一种上述车辆轴承用镀镍碳化硅颗粒增强铜基复合材料的制备方法，包含以下步骤：
步骤1：将镀镍碳化硅颗粒与稀土按照预订比例混合；
步骤2：将电解铜、锡锭、铅锭按照国标GB/T1176-2013的要求在500 公斤容量的中频电炉中熔炼；
步骤3：采用斯派克直读光谱仪对熔炼完成的铜合金溶液进行成分检测；
步骤4：将步骤1中预混合完成的镀镍碳化硅、稀土的混合物放置于熔炼完成的铜合金溶液之上，并用石墨棒进行搅拌；
步骤5：将搅拌完成的铜合金溶液倒入保温炉中，并开启保温炉的振动装置；
步骤6：保温，然后开启铸造装置并按照预定的产品形状铸造毛坯型材；
步骤7：将铸造完成的毛坯型材进行表面处理，包装入库。
进一步地，步骤2中的熔炼温度为1000℃-1100℃，熔炼时间为1.5-2小时。
进一步地，步骤4中的搅拌速率为3次/秒，搅拌时间为15-20分钟。
进一步地，步骤5中的保温炉的温度为1100℃-1150℃，振动装置的振动频率设定为25-30次/秒，振动装置的时间设定为25-30分钟。
进一步地，步骤6中的保温时间为1-1.5小时，保温温度为900℃-1000℃，铸造温度为850℃-900℃：
本发明的车辆轴承用镀镍碳化硅颗粒增强铜基复合材料，选取镀镍的纳米碳化硅材料及稀土材料并通过一定的技术手段均匀分布在现有的合金材料中，利用镀镍纳米级碳化硅高硬度、高耐磨性和良好的自润滑及高温强度大的性能，并通过其良好的润湿性，加强与原锡铅青铜(ZCuSn10Pb10)合金的结合，实现锡铅青铜(ZCuSn10Pb10)合金材料的性能的进一步提升。利用本发明方法制备的车辆轴承用镀镍碳化硅颗粒增强铜基复合材料具有更高的强度和硬度，从而可拓展应用于负载100MPa的冲击零件中，并且在同等条件下延长在车辆轴承及相应摩擦片中的使用年限。
具体实施方式
为了使本发明的目的、技术方案及优点更加清楚明白，下面结合实施例及附图，对本发明进行进一步详细说明。应当理解，此处所描述的具体实施例仅用以解释本发明，并不用于限定本发明。
本发明提供的车辆轴承用镀镍碳化硅颗粒增强铜基复合材料，铜基复合材料的成分包含镀镍碳化硅颗粒(Ni-SiC)、稀土、锡铅青铜(ZCuSn10Pb10)，其中，铜基复合材料的各成分组成按重量百分比分别为：镀镍碳化硅颗粒(Ni-SiC)：15-20％，稀土：0.05-0.5％，锡铅青铜(ZCuSn10Pb10)：79.5-84.95％。镀镍碳化硅颗粒是通过已知的化学方法制得，镀镍碳化硅颗粒的粒径在0.5μm-35μm范围内。稀土中包含重量百分比20％的镧(La)和重量百分比15％的铈(Ce)。锡铅青铜(ZCuSn10Pb10)的铸造是按照国标GB/T 1176-2013的标准。
本发明提供的车辆轴承用镀镍碳化硅颗粒增强铜基复合材料的制备方法，包含以下步骤：
步骤1：将镀镍碳化硅颗粒与稀土按照预订比例混合；
步骤2：将电解铜、锡锭、铅锭按照国标GB/T1176-2013的要求在500公斤容量的中频电炉中熔炼，熔炼温度为1000℃-1100℃，熔炼时间为1.5-2小时；
步骤3：采用斯派克直读光谱仪对熔炼完成的铜合金溶液进行成分检测，以确定铜合金溶液的化学成分在国标要求范围之内，并保证铜合金溶液占熔炼炉体积的80％以下；
步骤4：将步骤1中预混合完成的镀镍碳化硅、稀土的混合物放置于熔炼完成的铜合金溶液之上，并用石墨棒进行搅拌，搅拌速率为3次/秒，搅拌时间为15-20分钟；
步骤5：将搅拌完成的铜合金溶液倒入保温炉中，并开启保温炉的振动装置，振动装置的振动频率设定为25-30次/秒，振动装置的时间设定为25-30分钟，保温炉的温度为1100℃-1150℃；
步骤6：保温1-1.5小时，保温温度为900℃-1000℃，并开启铸造装置，铸造温度为850℃-900℃，按照预定的产品形状铸造毛坯型材；
步骤7：将铸造完成的毛坯型材进行表面处理，包装入库。
实施例一：
按重量百分比为：镀镍碳化硅颗粒(Ni-SiC)：15％，稀土：0.05％，锡铅青铜(ZCuSn10Pb10)：84.95％准备原料。其中镀镍碳化硅颗粒是通过已知的化学方法制得，镀镍碳化硅颗粒的粒径为0.5μm。稀土中包含重量百分比20％的镧(La)和重量百分比15％的铈(Ce)。锡铅青铜(ZCuSn10Pb10)的铸造是按照国标GB/T 1176-2013的标准。
首先，将镀镍碳化硅颗粒与稀土按照预订比例混合。
其次，将电解铜、锡锭、铅锭按照国标GB/T1176-2013的要求在500公斤容量的中频电炉中熔炼，熔炼温度为1000℃，熔炼时间为1.5小时。
其次，采用斯派克直读光谱仪对熔炼完成的铜合金溶液进行成分检测，以确定铜合金溶液的化学成分在国标要求范围之内，并保证铜合金溶液占熔炼炉体积的80％以下。
其次，将预混合完成的镀镍碳化硅、稀土的混合物放置于熔炼完成的铜合金溶液之上，并用石墨棒进行搅拌，搅拌速率为3次/秒，搅拌时间为15分钟。
其次，将搅拌完成的铜合金溶液倒入保温炉中，并开启保温炉的振动装置，振动装置的振动频率设定为25次/秒，振动装置的时间设定为25分钟，保温炉的温度为1100℃。
其次，保温1小时，保温温度为900℃，并开启铸造装置，铸造温度为850℃，按照预定的产品形状铸造毛坯型材。
最后，将铸造完成的毛坯型材进行表面处理，包装入库。
制备的车辆轴承用镀镍碳化硅颗粒增强铜基复合材料的强度和硬度与原锡铅青铜(ZCuSn10Pb10)相比，分别提高了28％和30％，在同等条件下车辆轴承用镀镍碳化硅颗粒增强铜基复合材料在车辆轴承及相应摩 擦片中的使用年限比原锡铅青铜(ZCuSn10Pb10)的使用年限延长了2年。
实施例二：
按重量百分比为：镀镍碳化硅颗粒(Ni-SiC)：16％，稀土：0.1％，锡铅青铜(ZCuSn10Pb10)：83.9％准备原料。其中镀镍碳化硅颗粒是通过已知的化学方法制得，镀镍碳化硅颗粒的粒径为10μm。稀土中包含重量百分比20％的镧(La)和重量百分比15％的铈(Ce)。锡铅青铜(ZCuSn10Pb10)的铸造是按照国标GB/T 1176-2013的标准。
首先，将镀镍碳化硅颗粒与稀土按照预订比例混合。
其次，将电解铜、锡锭、铅锭按照国标GB/T1176-2013的要求在500公斤容量的中频电炉中熔炼，熔炼温度为1030℃，熔炼时间为1.6小时。
其次，采用斯派克直读光谱仪对熔炼完成的铜合金溶液进行成分检测，以确定铜合金溶液的化学成分在国标要求范围之内，并保证铜合金溶液占熔炼炉体积的80％以下。
其次，将预混合完成的镀镍碳化硅、稀土的混合物放置于熔炼完成的铜合金溶液之上，并用石墨棒进行搅拌，搅拌速率为3次/秒，搅拌时间为16分钟。
其次，将搅拌完成的铜合金溶液倒入保温炉中，并开启保温炉的振动装置，振动装置的振动频率设定为26次/秒，振动装置的时间设定为26分钟，保温炉的温度为1120℃。
其次，保温1.2小时，保温温度为930℃，并开启铸造装置，铸造温度为860℃，按照预定的产品形状铸造毛坯型材。
最后，将铸造完成的毛坯型材进行表面处理，包装入库。
制备的车辆轴承用镀镍碳化硅颗粒增强铜基复合材料的强度和硬度与原锡铅青铜(ZCuSn10Pb10)相比，分别提高了32％和33％，在同等条件下车辆轴承用镀镍碳化硅颗粒增强铜基复合材料在车辆轴承及相应摩擦片中的使用年限比原锡铅青铜(ZCuSn10Pb10)的使用年限延长了2.5年。
实施例三：
按重量百分比为：镀镍碳化硅颗粒(Ni-SiC)：17％，稀土：0.3％，锡铅青铜(ZCuSn10Pb10)：82.7％准备原料。其中镀镍碳化硅颗粒是通过已知的化学方法制得，镀镍碳化硅颗粒的粒径为18μm。稀土中包含重量百分比20％的镧(La)和重量百分比15％的铈(Ce)。锡铅青铜(ZCuSn10Pb10)的铸造是按照国标GB/T 1176-2013的标准。
首先，将镀镍碳化硅颗粒与稀土按照预订比例混合。
其次，将电解铜、锡锭、铅锭按照国标GB/T1176-2013的要求在500公斤容量的中频电炉中熔炼，熔炼温度为1060℃，熔炼时间为1.9小时。
其次，采用斯派克直读光谱仪对熔炼完成的铜合金溶液进行成分检测，以确定铜合金溶液的化学成分在国标要求范围之内，并保证铜合金溶液占熔炼炉体积的80％以下。
其次，将预混合完成的镀镍碳化硅、稀土的混合物放置于熔炼完成的铜合金溶液之上，并用石墨棒进行搅拌，搅拌速率为3次/秒，搅拌时间为17分钟。
其次，将搅拌完成的铜合金溶液倒入保温炉中，并开启保温炉的振动装置，振动装置的振动频率设定为28次/秒，振动装置的时间设定为28分钟，保温炉的温度为1130℃。
其次，保温1.3小时，保温温度为960℃，并开启铸造装置，铸造温度为880℃，按照预定的产品形状铸造毛坯型材。
最后，将铸造完成的毛坯型材进行表面处理，包装入库。
制备的车辆轴承用镀镍碳化硅颗粒增强铜基复合材料的强度和硬度与原锡铅青铜(ZCuSn10Pb10)相比，分别提高了36％和38％，在同等条件下车辆轴承用镀镍碳化硅颗粒增强铜基复合材料在车辆轴承及相应摩擦片中的使用年限比原锡铅青铜(ZCuSn10Pb10)的使用年限延长了3年。
实施例四：
按重量百分比为：镀镍碳化硅颗粒(Ni-SiC)：18％，稀土：0.4％，锡铅青铜(ZCuSn10Pb10)：81.6％准备原料。其中镀镍碳化硅颗粒是通过已知 的化学方法制得，镀镍碳化硅颗粒的粒径为25μm。稀土中包含重量百分比20％的镧(La)和重量百分比15％的铈(Ce)。锡铅青铜(ZCuSn10Pb10)的铸造是按照国标GB/T 1176-2013的标准。
首先，将镀镍碳化硅颗粒与稀土按照预订比例混合。
其次，将电解铜、锡锭、铅锭按照国标GB/T1176-2013的要求在500公斤容量的中频电炉中熔炼，熔炼温度为1080℃，熔炼时间为1.8小时。
其次，采用斯派克直读光谱仪对熔炼完成的铜合金溶液进行成分检测，以确定铜合金溶液的化学成分在国标要求范围之内，并保证铜合金溶液占熔炼炉体积的80％以下。
其次，将预混合完成的镀镍碳化硅、稀土的混合物放置于熔炼完成的铜合金溶液之上，并用石墨棒进行搅拌，搅拌速率为3次/秒，搅拌时间为19分钟。
其次，将搅拌完成的铜合金溶液倒入保温炉中，并开启保温炉的振动装置，振动装置的振动频率设定为29次/秒，振动装置的时间设定为29分钟，保温炉的温度为1140℃。
其次，保温1.4小时，保温温度为980℃，并开启铸造装置，铸造温度为890℃，按照预定的产品形状铸造毛坯型材。
最后，将铸造完成的毛坯型材进行表面处理，包装入库。
制备的车辆轴承用镀镍碳化硅颗粒增强铜基复合材料的强度和硬度与原锡铅青铜(ZCuSn10Pb10)相比，分别提高了40％和45％，在同等条件下车辆轴承用镀镍碳化硅颗粒增强铜基复合材料在车辆轴承及相应摩擦片中的使用年限比原锡铅青铜(ZCuSn10Pb10)的使用年限延长了4年。
实施例五：
按重量百分比为：镀镍碳化硅颗粒(Ni-SiC)：20％，稀土：0.5％，锡铅青铜(ZCuSn10Pb10)：79.5％准备原料。其中镀镍碳化硅颗粒是通过已知的化学方法制得，镀镍碳化硅颗粒的粒径为35μm。稀土中包含重量百分比20％的镧(La)和重量百分比15％的铈(Ce)。锡铅青铜(ZCuSn10Pb10) 的铸造是按照国标GB/T 1176-2013的标准。
首先，将镀镍碳化硅颗粒与稀土按照预订比例混合。
其次，将电解铜、锡锭、铅锭按照国标GB/T1176-2013的要求在500公斤容量的中频电炉中熔炼，熔炼温度为1100℃，熔炼时间为2小时。
其次，采用斯派克直读光谱仪对熔炼完成的铜合金溶液进行成分检测，以确定铜合金溶液的化学成分在国标要求范围之内，并保证铜合金溶液占熔炼炉体积的80％以下。
其次，将预混合完成的镀镍碳化硅、稀土的混合物放置于熔炼完成的铜合金溶液之上，并用石墨棒进行搅拌，搅拌速率为3次/秒，搅拌时间为20分钟。
其次，将搅拌完成的铜合金溶液倒入保温炉中，并开启保温炉的振动装置，振动装置的振动频率设定为30次/秒，振动装置的时间设定为30分钟，保温炉的温度为1150℃。
其次，保温1.5小时，保温温度为1000℃，并开启铸造装置，铸造温度为900℃，按照预定的产品形状铸造毛坯型材。
最后，将铸造完成的毛坯型材进行表面处理，包装入库。
制备的车辆轴承用镀镍碳化硅颗粒增强铜基复合材料的强度和硬度与原锡铅青铜(ZCuSn10Pb10)相比，分别提高了38％和43％，在同等条件下车辆轴承用镀镍碳化硅颗粒增强铜基复合材料在车辆轴承及相应摩擦片中的使用年限比原锡铅青铜(ZCuSn10Pb10)的使用年限延长了3.5年。
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。

Claims (10)

  1. 一种车辆轴承用镀镍碳化硅颗粒增强铜基复合材料，其特征在于，所述铜基复合材料的成分包含镀镍碳化硅颗粒Ni-SiC、稀土、锡铅青铜ZCuSn10Pb10，其中，所述铜基复合材料的各成分组成按重量百分比分别为：所述镀镍碳化硅颗粒Ni-SiC：15-20％，所述稀土：0.05-0.5％，所述锡铅青铜ZCuSn10Pb10：79.5-84.95％。
  2. 根据权利要求1所述的车辆轴承用镀镍碳化硅颗粒增强铜基复合材料，其特征在于，所述铜基复合材料的各成分组成按重量百分比分别为：所述镀镍碳化硅颗粒Ni-SiC：16-18％，所述稀土：0.1-0.4％，所述锡铅青铜ZCuSn10Pb10：81.6-83.9％。
  3. 根据权利要求1所述的车辆轴承用镀镍碳化硅颗粒增强铜基复合材料，其特征在于，所述镀镍碳化硅颗粒的粒径在0.5μm-35μm范围内。
  4. 根据权利要求1所述的车辆轴承用镀镍碳化硅颗粒增强铜基复合材料，其特征在于，所述稀土中包含重量百分比20％的镧和重量百分比15％的铈。
  5. 根据权利要求1所述的车辆轴承用镀镍碳化硅颗粒增强铜基复合材料，其特征在于，所述锡铅青铜ZCuSn10Pb10的铸造是按照国标GB/T1176-2013的标准。
  6. 一种上述权利要求1-5中任一项所述的车辆轴承用镀镍碳化硅颗粒增强铜基复合材料的制备方法，其特征在于，包含以下步骤：
    步骤1：将所述镀镍碳化硅颗粒与所述稀土按照预订比例混合；
    步骤2：将电解铜、锡锭、铅锭按照国标GB/T1176-2013的要求在500公斤容量的中频电炉中熔炼；
    步骤3：采用斯派克直读光谱仪对熔炼完成的铜合金溶液进行成分检测；
    步骤4：将所述步骤1中预混合完成的所述镀镍碳化硅、所述稀土的 混合物放置于所述熔炼完成的铜合金溶液之上，并用石墨棒进行搅拌；
    步骤5：将搅拌完成的铜合金溶液倒入保温炉中，并开启所述保温炉的振动装置；
    步骤6：保温，然后开启铸造装置并按照预定的产品形状铸造毛坯型材；
    步骤7：将铸造完成的毛坯型材进行表面处理，包装入库。
  7. 根据权利要求6所述的车辆轴承用镀镍碳化硅颗粒增强铜基复合材料的制备方法，其特征在于，所述步骤2中的熔炼温度为1000℃-1100℃，熔炼时间为1.5-2小时。
  8. 根据权利要求6所述的车辆轴承用镀镍碳化硅颗粒增强铜基复合材料的制备方法，其特征在于，所述步骤4中的搅拌速率为3次/秒，搅拌时间为15-20分钟。
  9. 根据权利要求6所述的车辆轴承用镀镍碳化硅颗粒增强铜基复合材料的制备方法，其特征在于，所述步骤5中的所述保温炉的温度为1100℃-1150℃，所述振动装置的振动频率设定为25-30次/秒，所述振动装置的时间设定为25-30分钟。
  10. 根据权利要求6所述的车辆轴承用镀镍碳化硅颗粒增强铜基复合材料的制备方法，其特征在于，所述步骤6中的保温时间为1-1.5小时，保温温度为900℃-1000℃，铸造温度为850℃-900℃。
PCT/CN2015/000859 2015-11-02 2015-12-04 一种车辆轴承用镀镍碳化硅颗粒增强铜基复合材料及其制备方法 WO2017075740A1 (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN201510733156.5A CN105220006A (zh) 2015-11-02 2015-11-02 一种车辆轴承用镀镍碳化硅颗粒增强铜基复合材料及其制备方法
CN201510733156.5 2015-11-02

Publications (1)

Publication Number Publication Date
WO2017075740A1 true WO2017075740A1 (zh) 2017-05-11

Family

ID=54989271

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2015/000859 WO2017075740A1 (zh) 2015-11-02 2015-12-04 一种车辆轴承用镀镍碳化硅颗粒增强铜基复合材料及其制备方法

Country Status (2)

Country Link
CN (1) CN105220006A (zh)
WO (1) WO2017075740A1 (zh)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114807894A (zh) * 2022-05-18 2022-07-29 湖南工业职业技术学院 一种表面改性碳化硅颗粒增强铜基复合材料及其制备方法

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106191515A (zh) * 2016-08-09 2016-12-07 苏州列治埃盟新材料技术转移有限公司 一种化学镀镍碳化硅颗粒与铜铝复合的材料及其制备方法
CN106435252B (zh) * 2016-12-14 2018-08-03 苏州金仓合金新材料有限公司 一种碳化硅增强锑锡铜合金棒及其制造方法
CN107312950A (zh) * 2017-06-22 2017-11-03 苏州天兼新材料科技有限公司 一种镀镍碳化硅铜基合金材料及其制备方法
CN107119205B (zh) * 2017-06-22 2019-03-05 苏州天兼新材料科技有限公司 一种替代铍青铜的铜合金材料及其制备方法
CN111020269A (zh) * 2019-12-09 2020-04-17 苏州列治埃盟新材料技术转移有限公司 一种用于海洋工程机械高强度镀镍碳化硅铜基合金新材料
CN111850341A (zh) * 2020-07-31 2020-10-30 苏州天兼新材料科技有限公司 一种石油工程设备用高强度铜合金材料及其制备方法

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101748348A (zh) * 2009-12-04 2010-06-23 湖南大学 一种制备高性能陶瓷颗粒增强金属基复合材料的方法
CN102134664A (zh) * 2010-12-20 2011-07-27 昆明理工大学 一种均匀弥散颗粒增强金属基复合材料及其制备方法
CN102537065A (zh) * 2012-02-23 2012-07-04 杭州钱王机械有限公司 一种铜基重载自润滑船用轴承及其制备方法
CN103451634A (zh) * 2013-07-29 2013-12-18 洛阳德欣石化科技有限公司 一种微米碳化硅粉体表面的化学镀镍方法
CN104164589A (zh) * 2014-08-06 2014-11-26 中国兵器科学研究院宁波分院 一种高强耐磨铜合金及其制备方法
CN104630544A (zh) * 2015-01-27 2015-05-20 苏州金仓合金新材料有限公司 一种高速铁路用复合铜基新型合金材料及其制备方法

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100462184C (zh) * 2006-11-09 2009-02-18 上海交通大学 用于点焊电极的表面改性的颗粒增强铜基复合材料
CN101452773A (zh) * 2007-12-04 2009-06-10 美红 铜基SiCp稀土金属陶瓷复合电触头材料

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101748348A (zh) * 2009-12-04 2010-06-23 湖南大学 一种制备高性能陶瓷颗粒增强金属基复合材料的方法
CN102134664A (zh) * 2010-12-20 2011-07-27 昆明理工大学 一种均匀弥散颗粒增强金属基复合材料及其制备方法
CN102537065A (zh) * 2012-02-23 2012-07-04 杭州钱王机械有限公司 一种铜基重载自润滑船用轴承及其制备方法
CN103451634A (zh) * 2013-07-29 2013-12-18 洛阳德欣石化科技有限公司 一种微米碳化硅粉体表面的化学镀镍方法
CN104164589A (zh) * 2014-08-06 2014-11-26 中国兵器科学研究院宁波分院 一种高强耐磨铜合金及其制备方法
CN104630544A (zh) * 2015-01-27 2015-05-20 苏州金仓合金新材料有限公司 一种高速铁路用复合铜基新型合金材料及其制备方法

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114807894A (zh) * 2022-05-18 2022-07-29 湖南工业职业技术学院 一种表面改性碳化硅颗粒增强铜基复合材料及其制备方法

Also Published As

Publication number Publication date
CN105220006A (zh) 2016-01-06

Similar Documents

Publication Publication Date Title
WO2017075740A1 (zh) 一种车辆轴承用镀镍碳化硅颗粒增强铜基复合材料及其制备方法
WO2016119095A1 (zh) 一种高速铁路用复合铜基新型合金材料及其制备方法
CN106521252B (zh) 列车制动盘用碳化硅颗粒增强铝基复合材料及制备方法
CN103305742B (zh) 一种纳米级碳化硅铜基合金材料制备方法
WO2017133415A1 (zh) 一种高导热压铸铝合金及其制备方法
CN101514409B (zh) 原位Mg2Si颗粒增强金属基复合材料的制备方法
CN103243280B (zh) 一种碳纤维增强铝基复合材料及其制备方法
Dong et al. Microstructures and properties of A356–10% SiC particle composite castings at different solidification pressures
CN102699081B (zh) 一种铝硅铁合金发动机缸套的半固态触变挤压成形方法
CN103343274A (zh) 高导热金刚石颗粒混杂增强石墨铝复合材料及其制备工艺
Tang et al. Preparation and interface investigation of Fe/Al2O3P composite activated by Ni and Ti
CN109468487B (zh) 一种碳化钨增强铜基粉末冶金摩擦材料及其制备方法
CN105586503A (zh) 铜石墨复合材料及其制备方法
CN110453113A (zh) 一种氧化铯改性石墨烯增强铝合金复合材料的方法
WO2018028089A1 (zh) 一种应用于核电和风电的铸造材料及其制作方法
WO2017070806A1 (zh) 一种高强度碳化钛颗粒增强铜基复合材料及其制备方法
CN103146984B (zh) 一种高强度灰铸铁用孕育剂及其制备方法
CN106636823B (zh) 一种新型镁合金复合材料的制备方法
WO2017075741A1 (zh) 一种高速机车齿轮用高强度纳米级碳化硅铜基复合合金新材料
CN106191514A (zh) 一种多用途的铜基复合材料及其制备方法
CN114959409A (zh) 一种颗粒增强无铟可溶铝基复合材料制备方法
CN104726727A (zh) 高强度合金材料的制备方法
CN107399976B (zh) 一种离心大型棒材轧辊端盖用耐火材料及端盖制造方法
CN111378863B (zh) 一种二氧化硅气凝胶增强铜基复合材料及其制备方法
CN112853183A (zh) 一种高导热颗粒增强镁基复合材料及其制备方法

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: 15907582

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: 15907582

Country of ref document: EP

Kind code of ref document: A1