CN111283212B - Tungsten alloy material with stripping self-sharpening structure and preparation method and application thereof - Google Patents
Tungsten alloy material with stripping self-sharpening structure and preparation method and application thereof Download PDFInfo
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- 239000000956 alloy Substances 0.000 title claims abstract description 46
- 229910001080 W alloy Inorganic materials 0.000 title claims abstract description 41
- 238000002360 preparation method Methods 0.000 title claims abstract description 15
- 239000000843 powder Substances 0.000 claims abstract description 74
- OWUGOENUEKACGV-UHFFFAOYSA-N [Fe].[Ni].[W] Chemical compound [Fe].[Ni].[W] OWUGOENUEKACGV-UHFFFAOYSA-N 0.000 claims abstract description 48
- UQSXHKLRYXJYBZ-UHFFFAOYSA-N Iron oxide Chemical compound [Fe]=O UQSXHKLRYXJYBZ-UHFFFAOYSA-N 0.000 claims abstract description 36
- 229910001030 Iron–nickel alloy Inorganic materials 0.000 claims abstract description 30
- 230000009467 reduction Effects 0.000 claims abstract description 21
- 229910000480 nickel oxide Inorganic materials 0.000 claims abstract description 18
- QGLKJKCYBOYXKC-UHFFFAOYSA-N nonaoxidotritungsten Chemical compound O=[W]1(=O)O[W](=O)(=O)O[W](=O)(=O)O1 QGLKJKCYBOYXKC-UHFFFAOYSA-N 0.000 claims abstract description 18
- GNRSAWUEBMWBQH-UHFFFAOYSA-N oxonickel Chemical compound [Ni]=O GNRSAWUEBMWBQH-UHFFFAOYSA-N 0.000 claims abstract description 18
- 229910001930 tungsten oxide Inorganic materials 0.000 claims abstract description 18
- 239000011812 mixed powder Substances 0.000 claims abstract description 13
- 238000001816 cooling Methods 0.000 claims abstract description 12
- 238000000280 densification Methods 0.000 claims abstract description 12
- 238000003825 pressing Methods 0.000 claims abstract description 12
- 238000002156 mixing Methods 0.000 claims abstract description 8
- 238000009413 insulation Methods 0.000 claims abstract 2
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims description 12
- 238000005096 rolling process Methods 0.000 claims description 11
- 229910045601 alloy Inorganic materials 0.000 claims description 9
- 238000005245 sintering Methods 0.000 claims description 8
- 229910052786 argon Inorganic materials 0.000 claims description 6
- 239000001257 hydrogen Substances 0.000 claims description 6
- 229910052739 hydrogen Inorganic materials 0.000 claims description 6
- 239000000203 mixture Substances 0.000 claims description 6
- 239000002245 particle Substances 0.000 claims description 6
- 239000002826 coolant Substances 0.000 claims description 4
- 238000011068 loading method Methods 0.000 claims description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 4
- 238000010438 heat treatment Methods 0.000 claims description 2
- 230000006698 induction Effects 0.000 claims description 2
- 125000004435 hydrogen atom Chemical class [H]* 0.000 claims 1
- 238000006722 reduction reaction Methods 0.000 abstract description 21
- 238000005516 engineering process Methods 0.000 abstract description 5
- 239000003638 chemical reducing agent Substances 0.000 abstract description 3
- 238000013000 roll bending Methods 0.000 abstract 2
- 238000010008 shearing Methods 0.000 abstract 1
- 238000000034 method Methods 0.000 description 16
- 230000008569 process Effects 0.000 description 8
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 4
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 3
- 239000002994 raw material Substances 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical group [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 150000002431 hydrogen Chemical class 0.000 description 2
- 230000002401 inhibitory effect Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- 238000004321 preservation Methods 0.000 description 2
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- 239000010937 tungsten Substances 0.000 description 2
- 235000001674 Agaricus brunnescens Nutrition 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000032798 delamination Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 238000007731 hot pressing Methods 0.000 description 1
- 239000007791 liquid phase Substances 0.000 description 1
- 238000000691 measurement method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
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Abstract
Description
技术领域technical field
本发明涉及钨合金制备技术领域,具体涉及一种剥层自锐结构钨合金材料及其制备方法和应用。The invention relates to the technical field of tungsten alloy preparation, in particular to a stripping self-sharpening structure tungsten alloy material and a preparation method and application thereof.
背景技术Background technique
高密度钨合金作为一种结构材料,主要用于穿甲弹弹芯等军工领域,其强度和塑性的匹配性(绝热剪切性能)是决定子弹穿甲性能的关键条件。若强度过高、塑性较低则穿甲过程中易脆断,反之强度较低、塑性过高则易出现“蘑菇”状弹头,子弹失去自锐性和穿甲性能。现有的无压液相烧结、热压烧结、二步烧结、简单塑性变形等方法对于钨合金材料绝热剪切性能的调控水平很有限。因此,寻找一种有效方法,优化钨合金材料强度和塑性的匹配性,对于提高其绝热剪切性能等穿甲性能至关重要。As a structural material, high-density tungsten alloy is mainly used in military fields such as armor-piercing bullet cores. The matching of strength and plasticity (adiabatic shear performance) is the key condition to determine the armor-piercing performance of bullets. If the strength is too high and the plasticity is low, it will be brittle during the armor-piercing process. On the contrary, if the strength is low and the plasticity is too high, a "mushroom"-shaped warhead will easily appear, and the bullet loses self-sharpening and armor-piercing performance. The existing methods such as pressureless liquid phase sintering, hot pressing sintering, two-step sintering, and simple plastic deformation are very limited in regulating the adiabatic shear properties of tungsten alloy materials. Therefore, finding an effective method to optimize the matching of strength and plasticity of tungsten alloy materials is crucial for improving its armor-piercing properties such as adiabatic shear performance.
发明内容SUMMARY OF THE INVENTION
本发明的目的在于提供一种剥层自锐结构钨合金材料及其制备方法和应用,本发明提供的方法充分发挥化学还原和塑变的技术优势,能够优化钨合金材料强度和塑性的匹配性,使得到的剥层自锐结构钨合金材料具有较好的绝热剪切性能。The purpose of the present invention is to provide a peeling self-sharpening structure tungsten alloy material and its preparation method and application. The method provided by the present invention gives full play to the technical advantages of chemical reduction and plastic deformation, and can optimize the matching of the strength and plasticity of the tungsten alloy material. , so that the obtained stripped self-sharp structure tungsten alloy material has better adiabatic shear performance.
为了实现上述发明目的,本发明提供以下技术方案:In order to achieve the above-mentioned purpose of the invention, the present invention provides the following technical solutions:
一种剥层自锐结构钨合金材料的制备方法,包括以下步骤:A preparation method of a peeling self-sharpening structure tungsten alloy material, comprising the following steps:
将氧化钨粉末、氧化镍粉末和氧化铁粉末混合后所得混合粉末进行脉冲还原等离子射流处理和冷却处理,得到钨镍铁预合金粉末;The mixed powder obtained by mixing tungsten oxide powder, nickel oxide powder and iron oxide powder is subjected to pulse reduction plasma jet treatment and cooling treatment to obtain tungsten-nickel-iron pre-alloy powder;
将所述钨镍铁预合金粉末进行四级对辊成形处理,得到板型钨镍铁合金;The tungsten-nickel-iron pre-alloyed powder is subjected to four-level roll forming treatment to obtain a plate-shaped tungsten-nickel-iron alloy;
将所述板型钨镍铁合金进行滚弯变形处理,得到变形钨镍铁合金;rolling and deforming the plate-shaped tungsten-nickel-iron alloy to obtain a deformed tungsten-nickel-iron alloy;
将所述变形钨镍铁合金进行温压致密处理,得到剥层自锐结构钨合金材料。The deformed tungsten-nickel-iron alloy is subjected to warm-pressing and densification treatment to obtain a tungsten alloy material with a peeled-off self-sharp structure.
优选地,按质量分数计,所述氧化钨粉末的用量为91.67~96.89%,氧化镍粉末的用量为2.11~5.33%,氧化铁粉末的用量为1~3%。Preferably, in terms of mass fraction, the dosage of the tungsten oxide powder is 91.67-96.89%, the dosage of the nickel oxide powder is 2.11-5.33%, and the dosage of the iron oxide powder is 1-3%.
优选地,所述脉冲还原等离子射流处理的等离子源为氩气和氢气的混合气,脉冲电流为2.3~4.1A,脉冲频率为6.8~11.5Hz;以所述混合粉末的质量计,所述脉冲还原等离子射流处理的处理效率为7s/g。Preferably, the plasma source for the pulse reduction plasma jet treatment is a mixture of argon and hydrogen, the pulse current is 2.3-4.1A, and the pulse frequency is 6.8-11.5Hz; based on the mass of the mixed powder, the pulse The treatment efficiency of the reducing plasma jet treatment was 7 s/g.
优选地,所述冷却处理采用的冷却介质为3℃循环水。Preferably, the cooling medium used in the cooling treatment is circulating water at 3°C.
优选地,所述四级对辊成形处理的操作条件包括:四级对辊直径级配为4:2.5:2.3:2,出坯速度为0.3~1.6cm/s,按坯体运行方向温度升温梯度为3~6℃/cm,最高烧结温度为1410~1600℃。Preferably, the operating conditions of the four-stage roll forming process include: the four-stage roll diameter gradation is 4:2.5:2.3:2, the blanking speed is 0.3-1.6 cm/s, and the temperature is increased according to the running direction of the blank. The gradient is 3~6℃/cm, and the maximum sintering temperature is 1410~1600℃.
优选地,所述滚弯变形处理的横向变形速度为3~6mm/min,纵向变形速度为0.05~0.14mm/min。Preferably, the transverse deformation speed of the rolling deformation treatment is 3-6 mm/min, and the longitudinal deformation speed is 0.05-0.14 mm/min.
优选地,所述温压致密处理的压力为3.6~5.8GPa,压力的加载速率为120~240MPa/min,温度为560~740℃,保温保压时间为2~5min。Preferably, the pressure of the warm-pressing densification treatment is 3.6-5.8 GPa, the loading rate of the pressure is 120-240 MPa/min, the temperature is 560-740°C, and the heat preservation and pressure holding time is 2-5 min.
本发明提供了上述技术方案所述制备方法制备得到的剥层自锐结构钨合金材料。The present invention provides a stripped self-sharp structure tungsten alloy material prepared by the preparation method described in the above technical solution.
优选地,所述剥层自锐结构钨合金材料的莫氏硬度≥7.4,屈服强度≥2150MPa,绝热剪切应变率≤5.6%,晶粒的平均粒度≤1.5μm。Preferably, the Mohs hardness of the peeled self-sharpening tungsten alloy material is ≥7.4, the yield strength is ≥2150 MPa, the adiabatic shear strain rate is ≤5.6%, and the average grain size is ≤1.5 μm.
本发明提供了上述技术方案所述剥层自锐结构钨合金材料在军工领域中的应用。The invention provides the application of the stripped self-sharpening structure tungsten alloy material in the field of military industry.
本发明提供了一种剥层自锐结构钨合金材料的制备方法,包括以下步骤:将氧化钨粉末、氧化镍粉末和氧化铁粉末混合后所得混合粉末进行脉冲还原等离子射流处理和冷却处理,得到钨镍铁预合金粉末;将所述钨镍铁预合金粉末进行四级对辊成形处理,得到板型钨镍铁合金;将所述板型钨镍铁合金进行滚弯变形处理,得到变形钨镍铁合金;将所述变形钨镍铁合金进行温压致密处理,得到剥层自锐结构钨合金材料。针对现有技术中常见手段难以有效协调钨合金强度和塑性矛盾的问题,本发明通过采用脉冲还原等离子射流技术、四级对辊成形处理、滚弯变形处理和温压致密处理,充分发挥化学还原和塑变的技术优势,能够优化钨合金材料强度和塑性的匹配性,使得到的剥层自锐结构钨合金材料具有较好的绝热剪切性能。具体的,采用脉冲还原等离子射流技术,有利于实现氧化钨粉末、氧化镍粉末和氧化铁粉末的快速、高纯度还原,抑制粉末长大,均化钨镍铁原子分布;四级对辊成形处理和滚弯变形处理分别为快、慢塑性变形技术,二者配合可以调控晶界面积和晶粒位向关系,为得到剥层自锐结构提供基础;温压致密处理用于去除塑性变形组织的内应力,避免应力集中效应。此外,本发明提供的方法具有成分控制精度高、工艺稳定性好和重复性强的优势,可实现钨合金材料的性能优化,扩展其应用范围。实施例的结果显示,采用本发明提供的方法制备得到的钨合金材料具有剥层自锐结构,莫氏硬度≥7.4,屈服强度≥2150MPa,绝热剪切应变率≤5.6%,晶粒的平均粒度≤1.5μm。The invention provides a method for preparing a tungsten alloy material with a peeling self-sharp structure, which comprises the following steps: performing pulse reduction plasma jet treatment and cooling treatment on the mixed powder obtained by mixing tungsten oxide powder, nickel oxide powder and iron oxide powder to obtain tungsten-nickel-iron pre-alloy powder; subjecting the tungsten-nickel-iron pre-alloy powder to four-stage roll forming treatment to obtain a plate-shaped tungsten-nickel-iron alloy; subjecting the plate-shaped tungsten-nickel-iron alloy to rolling deformation treatment to obtain a deformed tungsten-nickel-iron alloy ; The deformed tungsten-nickel-iron alloy is subjected to temperature-compression densification treatment to obtain a tungsten alloy material with a peeling self-sharp structure. In view of the problem that it is difficult to effectively coordinate the contradiction between the strength and plasticity of tungsten alloys by common means in the prior art, the present invention gives full play to chemical reduction by adopting pulse reduction plasma jet technology, four-stage roll forming treatment, rolling deformation treatment and warm pressing densification treatment. The technical advantages of plastic deformation and plastic deformation can optimize the matching of strength and plasticity of tungsten alloy materials, so that the obtained tungsten alloy materials with peeling self-sharp structure have good adiabatic shear performance. Specifically, the use of pulse reduction plasma jet technology is conducive to realizing rapid and high-purity reduction of tungsten oxide powder, nickel oxide powder and iron oxide powder, inhibiting powder growth, and homogenizing the distribution of tungsten, nickel and iron atoms; four-stage roll forming treatment and rolling deformation treatment are fast and slow plastic deformation technologies, respectively. The combination of the two can control the relationship between grain boundary area and grain orientation, providing a basis for obtaining a self-sharpening structure of delamination. Internal stress to avoid stress concentration effects. In addition, the method provided by the invention has the advantages of high composition control precision, good process stability and strong repeatability, can realize the performance optimization of the tungsten alloy material, and expand its application range. The results of the examples show that the tungsten alloy material prepared by the method provided by the present invention has a self-sharpening structure, Mohs hardness ≥ 7.4, yield strength ≥ 2150 MPa, adiabatic shear strain rate ≤ 5.6%, and the average grain size of the grains. ≤1.5μm.
具体实施方式Detailed ways
本发明提供了一种剥层自锐结构钨合金材料的制备方法,包括以下步骤:The invention provides a preparation method of a peeling self-sharpening structure tungsten alloy material, comprising the following steps:
将氧化钨粉末、氧化镍粉末和氧化铁粉末混合后所得混合粉末进行脉冲还原等离子射流处理和冷却处理,得到钨镍铁预合金粉末;The mixed powder obtained by mixing tungsten oxide powder, nickel oxide powder and iron oxide powder is subjected to pulse reduction plasma jet treatment and cooling treatment to obtain tungsten-nickel-iron pre-alloy powder;
将所述钨镍铁预合金粉末进行四级对辊成形处理,得到板型钨镍铁合金;The tungsten-nickel-iron pre-alloyed powder is subjected to four-level roll forming treatment to obtain a plate-shaped tungsten-nickel-iron alloy;
将所述板型钨镍铁合金进行滚弯变形处理,得到变形钨镍铁合金;rolling and deforming the plate-shaped tungsten-nickel-iron alloy to obtain a deformed tungsten-nickel-iron alloy;
将所述变形钨镍铁合金进行温压致密处理,得到剥层自锐结构钨合金材料。The deformed tungsten-nickel-iron alloy is subjected to warm-pressing and densification treatment to obtain a tungsten alloy material with a peeled-off self-sharp structure.
在本发明中,若无特殊说明,所用原料以及设备均为本领域技术人员熟知的市售商品。In the present invention, unless otherwise specified, the raw materials and equipment used are commercially available commodities well known to those skilled in the art.
本发明将氧化钨粉末、氧化镍粉末和氧化铁粉末混合后所得混合粉末进行脉冲还原等离子射流处理和冷却处理,得到钨镍铁预合金粉末。在本发明中,按质量分数计,所述氧化钨粉末的用量优选为91.67~96.89%,氧化镍粉末的用量优选为2.11~5.33%,氧化铁粉末的用量优选为1~3%。在本发明中,所述氧化钨粉末、氧化镍粉末和氧化铁粉末的粒度优选独立地为2~6μm;本发明对所述氧化钨粉末、氧化镍粉末和氧化铁粉末的来源没有特殊限定,采用本领域技术人员熟知的市售商品即可。本发明对氧化钨粉末、氧化镍粉末和氧化铁粉末的混合方式不作特殊限定,能够实现三者均匀混合即可。In the present invention, the mixed powder obtained by mixing tungsten oxide powder, nickel oxide powder and iron oxide powder is subjected to pulse reduction plasma jet treatment and cooling treatment to obtain tungsten-nickel-iron pre-alloy powder. In the present invention, in terms of mass fraction, the dosage of the tungsten oxide powder is preferably 91.67-96.89%, the dosage of the nickel oxide powder is preferably 2.11-5.33%, and the dosage of the iron oxide powder is preferably 1-3%. In the present invention, the particle sizes of the tungsten oxide powder, the nickel oxide powder and the iron oxide powder are preferably independently 2-6 μm; the present invention does not specifically limit the sources of the tungsten oxide powder, the nickel oxide powder and the iron oxide powder, Commercially available products well known to those skilled in the art may be used. The present invention does not specifically limit the mixing mode of the tungsten oxide powder, the nickel oxide powder and the iron oxide powder, as long as the three can be uniformly mixed.
将氧化钨粉末、氧化镍粉末和氧化铁粉末混合后,本发明将所得混合粉末进行脉冲还原等离子射流处理和冷却处理,得到钨镍铁预合金粉末。在本发明中,所述脉冲还原等离子射流处理的等离子源优选为氩气和氢气的混合气;所述氩气和氢气的体积比优选为6:4;脉冲电流优选为2.3~4.1A,更优选为2.4~3.5A,进一步优选为2.5~3.1A;脉冲频率优选为6.8~11.5Hz,更优选为6.9~10.5Hz,进一步优选为7.0~7.5Hz;以所述混合粉末的质量计,所述脉冲还原等离子射流处理的处理效率优选为7s/g。在本发明中,所述冷却处理采用的冷却介质优选为3℃循环水。本发明采用脉冲还原等离子射流技术实现氧化钨粉末、氧化镍粉末和氧化铁粉末的还原,脉冲还原等离子射流技术以高脉冲电流为能量激发介质、以氩气和氢气的混合气为高能等离子源,通过高能还原和快速冷却方法,可以将氧化钨粉末、氧化镍粉末和氧化铁粉末快速、高纯度还原,抑制粉末长大,均化钨镍铁原子分布。After mixing the tungsten oxide powder, the nickel oxide powder and the iron oxide powder, in the present invention, the obtained mixed powder is subjected to pulse reduction plasma jet treatment and cooling treatment to obtain tungsten-nickel-iron pre-alloy powder. In the present invention, the plasma source for the pulse reduction plasma jet treatment is preferably a mixture of argon and hydrogen; the volume ratio of the argon and hydrogen is preferably 6:4; the pulse current is preferably 2.3-4.1A, more The pulse frequency is preferably 2.4-3.5A, more preferably 2.5-3.1A; the pulse frequency is preferably 6.8-11.5Hz, more preferably 6.9-10.5Hz, further preferably 7.0-7.5Hz; based on the mass of the mixed powder, the The treatment efficiency of the pulse reduction plasma jet treatment is preferably 7 s/g. In the present invention, the cooling medium used in the cooling treatment is preferably circulating water at 3°C. The invention adopts the pulse reduction plasma jet technology to realize the reduction of the tungsten oxide powder, the nickel oxide powder and the iron oxide powder. Through high-energy reduction and rapid cooling methods, tungsten oxide powder, nickel oxide powder and iron oxide powder can be reduced quickly and with high purity, inhibiting powder growth and homogenizing the distribution of tungsten, nickel and iron atoms.
得到钨镍铁预合金粉末后,本发明将所述钨镍铁预合金粉末进行四级对辊成形处理,得到板型钨镍铁合金。在本发明中,所述四级对辊成形处理的操作条件包括:四级对辊直径级配优选为4:2.5:2.3:2;出坯速度优选为0.3~1.6cm/s,更优选为0.4~0.6cm/s;按坯体运行方向温度升温梯度优选为3~6℃/cm,更优选为4~5℃/cm;最高烧结温度优选为1410~1600℃,更优选为1450~1600℃,进一步优选为1490~1500℃。在本发明中,所述四级对辊成形处理采用的对辊的材质优选为硬质合金。本发明对钨镍铁预合金粉末进行四级对辊成形处理,通过感应加热方式逐步加热钨镍铁预合金粉末,达到加压烧结的目的。在本发明中,所述四级对辊成形处理优选在四级对辊成形一体装置中进行。After the tungsten-nickel-iron pre-alloy powder is obtained, the present invention performs a four-stage roll forming process on the tungsten-nickel-iron pre-alloy powder to obtain a plate-shaped tungsten-nickel-iron alloy. In the present invention, the operating conditions of the four-stage paired roll forming process include: the four-stage paired roll diameter gradation is preferably 4:2.5:2.3:2; the blanking speed is preferably 0.3-1.6 cm/s, more preferably 0.4~0.6cm/s; according to the running direction of the green body, the temperature gradient is preferably 3~6°C/cm, more preferably 4~5°C/cm; the maximum sintering temperature is preferably 1410~1600°C, more preferably 1450~1600°C °C, more preferably 1490 to 1500 °C. In the present invention, the material of the pair of rolls used in the four-stage paired roll forming process is preferably cemented carbide. In the present invention, the pre-alloyed powder of tungsten-nickel-iron is subjected to four-stage roll forming treatment, and the pre-alloyed powder of tungsten-nickel-iron is gradually heated by induction heating to achieve the purpose of pressure sintering. In the present invention, the four-stage roll forming process is preferably performed in an integrated four-stage roll forming apparatus.
得到板型钨镍铁合金后,本发明将所述板型钨镍铁合金进行滚弯变形处理,得到变形钨镍铁合金。在本发明中,所述滚弯变形处理的横向变形速度优选为3~6mm/min,更优选为4~5mm/min;纵向变形速度优选为0.05~0.14mm/min,更优选为0.07~0.08mm/min。After the plate-shaped tungsten-nickel-iron alloy is obtained, in the present invention, the plate-shaped tungsten-nickel-iron alloy is subjected to rolling deformation treatment to obtain a deformed tungsten-nickel-iron alloy. In the present invention, the transverse deformation speed of the rolling deformation treatment is preferably 3-6 mm/min, more preferably 4-5 mm/min; the longitudinal deformation speed is preferably 0.05-0.14 mm/min, more preferably 0.07-0.08 mm/min.
得到变形钨镍铁合金后,本发明将所述变形钨镍铁合金进行温压致密处理,得到剥层自锐结构钨合金材料。在本发明中,所述温压致密处理的压力优选为3.6~5.8GPa,更优选为3.8~4.8GPa;压力的加载速率优选为120~240MPa/min,更优选为140~210MPa/min;温度优选为560~740℃;保温保压时间优选为2~5min,更优选为3~4min。After the deformed tungsten-nickel-iron alloy is obtained, in the present invention, the deformed tungsten-nickel-iron alloy is subjected to a temperature pressing and densification treatment to obtain a tungsten alloy material with a peeling self-sharp structure. In the present invention, the pressure of the warm-pressing densification treatment is preferably 3.6-5.8GPa, more preferably 3.8-4.8GPa; the loading rate of the pressure is preferably 120-240MPa/min, more preferably 140-210MPa/min; the temperature Preferably, the temperature is 560-740° C.; the temperature-preservation and pressure-holding time is preferably 2-5 min, more preferably 3-4 min.
本发明提供了上述技术方案所述制备方法制备得到的剥层自锐结构钨合金材料。在本发明中,所述剥层自锐结构钨合金材料的莫氏硬度≥7.4,屈服强度≥2150MPa,绝热剪切应变率≤5.6%,晶粒的平均粒度≤1.5μm。The present invention provides a stripped self-sharp structure tungsten alloy material prepared by the preparation method described in the above technical solution. In the present invention, the Mohs hardness of the peeling self-sharp structure tungsten alloy material is ≥7.4, the yield strength is ≥2150MPa, the adiabatic shear strain rate is ≤5.6%, and the average grain size of the crystal grains is ≤1.5 μm.
本发明提供了上述技术方案所述剥层自锐结构钨合金材料在军工领域中的应用,如具体可以用于制备穿甲弹弹芯。The present invention provides the application of the stripped self-sharpening structure tungsten alloy material in the field of military industry, for example, it can be specifically used for preparing armor-piercing bullet cores.
下面将结合本发明中的实施例,对本发明中的技术方案进行清楚、完整地描述。显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。The technical solutions of the present invention will be clearly and completely described below with reference to the embodiments of the present invention. Obviously, the described embodiments are only some, but not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.
实施例1Example 1
(1)按质量百分比计,取92.70%氧化钨粉末(粒度为2~6μm)、5.33%氧化镍粉末(粒度为2~6μm)和1.97%氧化铁粉末(粒度为2~6μm)混合均匀,将所得混合粉末进行脉冲还原等离子射流处理和冷却处理,得到钨镍铁预合金粉末;其中,操作条件包括:等离子源为氩气和氢气的混合气,所述氩气和氢气的体积比为6:4;脉冲电流为2.3A,脉冲频率为6.8Hz;以所述混合粉末的质量计,所述脉冲还原等离子射流处理的处理效率为7s/g;冷却介质为3℃循环水;(1) In terms of mass percentage, take 92.70% tungsten oxide powder (particle size of 2-6 μm), 5.33% nickel oxide powder (particle size of 2-6 μm) and 1.97% iron oxide powder (particle size of 2-6 μm) and mix them evenly, The obtained mixed powder is subjected to pulse reduction plasma jet treatment and cooling treatment to obtain tungsten-nickel-iron pre-alloyed powder; wherein, the operating conditions include: the plasma source is a mixture of argon and hydrogen, and the volume ratio of the argon and hydrogen is 6 : 4; the pulse current is 2.3A, and the pulse frequency is 6.8Hz; based on the mass of the mixed powder, the treatment efficiency of the pulse reduction plasma jet treatment is 7s/g; the cooling medium is 3°C circulating water;
(2)将所述钨镍铁预合金粉末送入四级对辊成形一体装置中进行成形,得到板型钨镍铁合金;其中,操作条件包括:四级对辊直径级配为4:2.5:2.3:2,出坯速度为0.3cm/s,按坯体运行方向温度升温梯度为3℃/cm,最高烧结温度为1410℃;(2) the tungsten-nickel-iron pre-alloyed powder is sent into the four-stage paired roll forming integrated device to be formed to obtain a plate-shaped tungsten-nickel-iron alloy; wherein, the operating conditions include: the four-stage paired roll diameter gradation is 4:2.5: 2.3:2, the blanking speed is 0.3cm/s, the temperature gradient in the running direction of the blank is 3°C/cm, and the maximum sintering temperature is 1410°C;
(3)将所述板型钨镍铁合金进行滚弯变形处理,得到变形钨镍铁合金;其中,操作条件包括:横向变形速度为3mm/min,纵向变形速度为0.05mm/min;(3) rolling and deforming the plate-shaped tungsten-nickel-iron alloy to obtain deformed tungsten-nickel-iron alloy; wherein, the operating conditions include: the transverse deformation speed is 3mm/min, and the longitudinal deformation speed is 0.05mm/min;
(4)将所述变形钨镍铁合金在双向超重压装置中进行温压致密处理,得到剥层自锐结构钨合金材料;其中,操作条件包括:压力为3.6GPa,压力的加载速率为120MPa/min,温度为560℃,保温保压时间为2min。(4) The deformed tungsten-nickel-iron alloy is subjected to temperature pressing and densification treatment in a two-way super-heavy pressure device to obtain a peeling self-sharp structure tungsten alloy material; wherein, the operating conditions include: the pressure is 3.6GPa, and the loading rate of the pressure is 120MPa/ min, the temperature was 560 °C, and the holding time was 2 min.
实施例2~8Examples 2 to 8
按照实施例1的方法制备剥层自锐结构钨合金材料,原料配比以及各步骤的操作参数如表1所示(表1中未列的操作条件或参数与实施例1相同)。The peeling self-sharp structure tungsten alloy material was prepared according to the method of Example 1. The ratio of raw materials and the operating parameters of each step are shown in Table 1 (the operating conditions or parameters not listed in Table 1 are the same as those of Example 1).
表1实施例1~8中原料配比以及各步骤的操作参数The ratio of raw materials and the operating parameters of each step in Examples 1 to 8 of Table 1
对实施例1~8制备的剥层自锐结构钨合金材料的莫氏硬度、屈服强度(GB T228.1-2010)、绝热剪切应变率以及晶粒的粒度进行测定,结果见表2;其中,绝热剪切应变率的测量方法为:用线切割将各实施例制备的剥层自锐结构钨合金材料加工成下底直径为4mm、上底直径为1mm、高为5mm的圆台试样,上底朝下放置在515BHN高硬度钢板上,用锻锤以0.5~1.5GPa的瞬间冲击力锤击圆台试样的下底,测量产生初始剥层裂纹需要的应变率。The Mohs hardness, yield strength (GB T228.1-2010), adiabatic shear strain rate and grain size of the peeled self-sharp structure tungsten alloy materials prepared in Examples 1-8 were measured, and the results are shown in Table 2; Among them, the measurement method of the adiabatic shear strain rate is: using wire cutting to process the peeled self-sharp structure tungsten alloy material prepared in each embodiment into a circular table sample with a lower bottom diameter of 4 mm, an upper bottom diameter of 1 mm and a height of 5 mm , placed on the 515BHN high-hardness steel plate with the upper bottom facing down, hammer the lower bottom of the round table sample with a forging hammer with an instantaneous impact force of 0.5-1.5 GPa, and measure the strain rate required to generate the initial peeling crack.
表2实施例1~8制备的剥层自锐结构钨合金材料的性能及质量指标检测结果Table 2 Performance and quality index test results of the peeled self-sharp structure tungsten alloy materials prepared in Examples 1 to 8
本发明制备的钨合金材料具有剥层自锐结构,且由表2可知,所述钨合金材料的莫氏硬度≥7.4,屈服强度≥2150MPa,绝热剪切应变率≤5.6%,晶粒的平均粒度≤1.5μm。The tungsten alloy material prepared by the present invention has a peeling self-sharpening structure, and it can be seen from Table 2 that the Mohs hardness of the tungsten alloy material is greater than or equal to 7.4, the yield strength is greater than or equal to 2150MPa, the adiabatic shear strain rate is less than or equal to 5.6%, and the average grain size is less than or equal to 5.6%. Particle size≤1.5μm.
以上所述仅是本发明的优选实施方式,应当指出,对于本技术领域的普通技术人员来说,在不脱离本发明原理的前提下,还可以做出若干改进和润饰,这些改进和润饰也应视为本发明的保护范围。The above are only the preferred embodiments of the present invention. It should be pointed out that for those skilled in the art, without departing from the principles of the present invention, several improvements and modifications can be made. It should be regarded as the protection scope of the present invention.
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Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1563443A (en) * | 2004-03-30 | 2005-01-12 | 上海大学 | Equipment for intensifying hydrogen reductiion for metallic oxide |
CN104722770A (en) * | 2015-04-16 | 2015-06-24 | 柳州豪祥特科技有限公司 | Method for preparing tungsten-molybdenum powder |
CN106694897A (en) * | 2016-12-27 | 2017-05-24 | 中国兵器科学研究院宁波分院 | Method for preparing tungsten-based high-density alloy nano-composite powder and block material made of nano-composite powder |
CN110465666A (en) * | 2019-09-16 | 2019-11-19 | 陕西理工大学 | The preparation method of nano-interface and ultra micro crystal grain tungsten alloy material |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2006348349A (en) * | 2005-06-16 | 2006-12-28 | Katsuyoshi Kondo | Magnesium alloy-powder raw material, high proof-stress magnesium alloy, method for manufacturing magnesium alloy-powder raw material and method for manufacturing high proof-stress magnesium alloy |
-
2020
- 2020-03-27 CN CN202010227146.5A patent/CN111283212B/en active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1563443A (en) * | 2004-03-30 | 2005-01-12 | 上海大学 | Equipment for intensifying hydrogen reductiion for metallic oxide |
CN104722770A (en) * | 2015-04-16 | 2015-06-24 | 柳州豪祥特科技有限公司 | Method for preparing tungsten-molybdenum powder |
CN106694897A (en) * | 2016-12-27 | 2017-05-24 | 中国兵器科学研究院宁波分院 | Method for preparing tungsten-based high-density alloy nano-composite powder and block material made of nano-composite powder |
CN110465666A (en) * | 2019-09-16 | 2019-11-19 | 陕西理工大学 | The preparation method of nano-interface and ultra micro crystal grain tungsten alloy material |
Non-Patent Citations (5)
Title |
---|
变形对钨合金微观组织性能及绝热剪切敏感性的影响;李淑华等;《特种铸造及有色合金》;20061015;第25卷(第11期);664-667 * |
郎利辉等.钨基合金的预强化和后期强化技术.《锻压技术》.2012,第37卷(第04期), * |
钨及其合金塑性加工的研究进展;李萍等;《稀有金属材料与工程》;20160215;第45卷(第02期);529-536 * |
钨基合金的预强化和后期强化技术;郎利辉等;《锻压技术》;20120825;第37卷(第04期);第1页-第4页 * |
钨基合金穿、破甲材料的研究进展;范景莲等;《中国钨业》;20070228;第22卷(第01期);25-29 * |
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