[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

CN110629012A - A method for ultrahigh strain rate plastic deformation strengthening in metals - Google Patents

A method for ultrahigh strain rate plastic deformation strengthening in metals Download PDF

Info

Publication number
CN110629012A
CN110629012A CN201810658115.8A CN201810658115A CN110629012A CN 110629012 A CN110629012 A CN 110629012A CN 201810658115 A CN201810658115 A CN 201810658115A CN 110629012 A CN110629012 A CN 110629012A
Authority
CN
China
Prior art keywords
sample
plastic deformation
strain rate
ultrasonic
ultra
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN201810658115.8A
Other languages
Chinese (zh)
Other versions
CN110629012B (en
Inventor
李玉胜
王帅卓
周浩
魏康
李建生
毛庆忠
高波
刘艳芳
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nanjing Tech University
Original Assignee
Nanjing Tech University
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 Nanjing Tech University filed Critical Nanjing Tech University
Priority to CN201810658115.8A priority Critical patent/CN110629012B/en
Publication of CN110629012A publication Critical patent/CN110629012A/en
Application granted granted Critical
Publication of CN110629012B publication Critical patent/CN110629012B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D10/00Modifying the physical properties by methods other than heat treatment or deformation

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Investigating Or Analyzing Materials By The Use Of Ultrasonic Waves (AREA)

Abstract

本发明为一种在金属中实现超高应变速率塑性变形强化的方法,通过超声波共振实现超高应变速率的塑性变形。使超声波在局部产生共振得到极高极快的应力波,从而产生具有超高应变速率的塑性变形,根据金属材料的塑性变形理论,其可以实现金属材料内部微观结构的变化,最终实现了材料强化。该方法将高能的超声波通过金属材料内部,并使其在金属材料局部发生共振,从而产生超高频的应力正弦波,由于其应力峰值远高于材料的屈服强度,使材料发生超高应变速率的塑性变形。

The invention is a method for realizing superhigh strain rate plastic deformation strengthening in metal, and realizes superhigh strain rate plastic deformation through ultrasonic resonance. Ultrasonic waves are locally resonated to obtain extremely high and fast stress waves, resulting in plastic deformation with ultra-high strain rates. According to the plastic deformation theory of metal materials, it can achieve changes in the internal microstructure of metal materials, and finally achieve material strengthening. . This method passes high-energy ultrasonic waves through the interior of the metal material and makes it resonate locally in the metal material, thereby generating an ultra-high-frequency stress sine wave. Because the stress peak value is much higher than the yield strength of the material, the material undergoes an ultra-high strain rate. plastic deformation.

Description

一种在金属中实现超高应变速率塑性变形强化的方法A method for ultrahigh strain rate plastic deformation strengthening in metals

技术领域technical field

本发明为一种在金属中实现超高应变速率塑性变形强化的方法,涉及金属强化领域。The invention relates to a method for realizing ultra-high strain rate plastic deformation strengthening in metals, and relates to the field of metal strengthening.

背景技术Background technique

塑性变形会导致金属材料内部微观结构发生变化,位错发生增殖、运动、重排与湮灭等等。剧烈塑性变形可使金属材料晶粒细化至亚微米甚至纳米级,能够有效制备出力学性能优异、致密度高、无污染的块体超细晶材料。常见的剧烈塑性变形方式有高压扭转、旋锻、等通道挤压(ECAP)等,传统的塑性变形方式如锻造、轧制或挤压等,也可以对金属材料进行较大塑性变形并使其微观组织发生明显改变。剧烈塑性变形处理过的金属具有高强度、高硬度和良好的摩擦性能,成为金属及金属基复合材料的非常重要的强化手段之一。Plastic deformation will lead to changes in the internal microstructure of metal materials, dislocation proliferation, movement, rearrangement and annihilation, etc. Severe plastic deformation can refine the grains of metal materials to submicron or even nanometer level, and can effectively prepare bulk ultrafine-grained materials with excellent mechanical properties, high density, and pollution-free. Common severe plastic deformation methods include high-pressure torsion, rotary forging, equal channel extrusion (ECAP), etc. Traditional plastic deformation methods such as forging, rolling or extrusion, etc., can also perform large plastic deformation on metal materials and make them Significant changes occurred in the microstructure. Metals treated with severe plastic deformation have high strength, high hardness and good friction properties, and become one of the very important strengthening methods for metals and metal matrix composites.

Wu等人在《Proceedings of the National Academy of Sciences of theUnited States of America》(PNAS,2015,112(47):14501–14505)上发表了名为“Heterogeneous lamella structure unites ultrafine-grain strength with coarse-grain ductility”,公开一种具有高强高塑性的异质层状结构的纯钛,这种结构是通过大的塑性变形引入了丰富的微观结构,经过简单的热处理得到一种由硬的超细晶和软的再结晶组成的异构纯钛。该方法制得的新型金属钛棒材通过异质结构的变形协调作用,能够在一定程度上兼得超细晶的高强度和粗晶的高韧性,提升金属钛的综合性能。Wu et al published a paper entitled "Heterogeneous lamella structure units ultrafine-grain strength with coarse-grain ductility", which discloses a pure titanium with a heterogeneous layered structure with high strength and high plasticity. This structure introduces a rich microstructure through large plastic deformation. Soft recrystallized composition of isomerically pure titanium. The novel titanium metal rod prepared by the method can achieve both the high strength of the ultrafine grain and the high toughness of the coarse grain to a certain extent through the deformation coordination effect of the heterogeneous structure, and improve the comprehensive performance of the titanium metal.

中国发明专利申请号:99122670.4公开了一种采用刚性丸粒钢球对金属材料表面撞击,使基体表面产生了剧烈塑性变形,其变形时具有较高的应变速率,从而实现表面组织细化至纳米尺寸。其局限性是:只能对金属材料表面进行塑性变形而不能使材料的整体组织发生改变。Chinese invention patent application number: 99122670.4 discloses a method of impacting the surface of metal materials with rigid shot steel balls, causing severe plastic deformation on the surface of the substrate, with a high strain rate during deformation, so as to realize the refinement of the surface structure to nanometer size. Its limitation is that it can only plastically deform the surface of the metal material without changing the overall structure of the material.

中国发明专利一种等通道挤压装置申请号:200710030188.4公开了一种整体剧烈塑性变形制备超细晶材料的方法,通过挤压力的作用,使得金属材料发生纯剪切塑性变形,从而引入丰富的微观组织,细化晶粒。其局限性是:被加工材料整体外观发生变形,且其在塑性变形的过程中应变速率不高。A Chinese invention patent for an equal-channel extrusion device application number: 200710030188.4 discloses a method for preparing ultra-fine-grained materials by overall severe plastic deformation. Through the action of extrusion force, pure shear plastic deformation of metal materials occurs, thereby introducing rich Microstructure, refine the grain. Its limitations are: the overall appearance of the processed material is deformed, and its strain rate is not high during the plastic deformation process.

发明内容Contents of the invention

本发明目的在于提供一种在金属中实现超高应变速率塑性变形强化的方法。The purpose of the present invention is to provide a method for realizing ultra-high strain rate plastic deformation strengthening in metals.

实现本发明目的具体方案如下:Realize the specific scheme of the object of the present invention as follows:

一种在金属中实现超高应变速率塑性变形强化的方法,该方法为:A method of achieving ultrahigh strain rate plastic deformation strengthening in metals by:

步骤1,将金属材料根据其密度及弹性模量加工成所需外形样品的外形,满足超声波可以在变形区域产生共振,形成超高频的应力波;Step 1. Process the metal material into the shape of the desired shape sample according to its density and elastic modulus, so that the ultrasonic wave can resonate in the deformation area to form an ultra-high frequency stress wave;

步骤1中,所述的样品为中部等截面板状的拉伸试样,所述的样品满In step 1, the sample is a tensile sample with a central equal-section plate, and the sample is full of

足超声波可以在变形区域产生共振需要其谐振长度L3满足以下公式:Foot ultrasound can generate resonance in the deformed region, and its resonance length L3 needs to satisfy the following formula :

采用试样纵向的振动方程U(x)为:The longitudinal vibration equation U(x) of the sample is:

其中:in:

试样谐振长度L3为:The resonant length L3 of the sample is:

板状试样最大应力幅为:The maximum stress amplitude of the plate sample is:

位移应力系数为:The displacement stress coefficient is:

A0=μIA 0 =μI

其中L1为试样塑性变形区的半长度,L2圆弧过度端的平行距离为,b1为试样塑性变形区的厚度,b2为连接端的厚度,;E为弹性模量;ρ为密度;超高应变速率加载系统的谐振频率f=20kHz。C为纵波波速;w为角速度;μ为设备对应的位移放大系数,本发明使用的设备μ=16;I为设备电源提供的电流(可以调节);α1,β1,k为物理推导过程量,其可以被基础量表示。Where L 1 is the half length of the plastic deformation zone of the sample, L 2 is the parallel distance of the arc transition end, b 1 is the thickness of the plastic deformation zone of the sample, b 2 is the thickness of the connecting end, E is the modulus of elasticity; ρ is Density; the resonant frequency f=20kHz of the ultra-high strain rate loading system. C is the longitudinal wave velocity; w is the angular velocity; μ is the displacement amplification factor corresponding to the equipment, and the equipment used in the present invention μ=16; I is the current provided by the equipment power supply (can be adjusted); α 1 , β 1 , k are physical derivation processes Quantities, which can be represented by base quantities.

步骤2:将加工好的样品与超声设备相连接,选择超声波功率。Step 2: Connect the processed sample to the ultrasonic equipment and select the ultrasonic power.

步骤2具体为:超声波加载的峰值应高于试样材料的屈服强度Step 2 is specifically: the peak value of ultrasonic loading should be higher than the yield strength of the sample material

步骤3:确保样品一端通过内螺纹与超声设备放大器底端连接,另一端自由。Step 3: Make sure that one end of the sample is connected to the bottom of the ultrasound equipment amplifier through the internal thread, and the other end is free.

步骤4:开始超声共振,机械振动的纵波传到试样自由端后发生反射,反射波的频率与入射波产生谐振,沿样品轴向形成超高频应力的载荷,对样品形成塑性变形。Step 4: Start ultrasonic resonance, the longitudinal wave of mechanical vibration is transmitted to the free end of the sample and then reflected, the frequency of the reflected wave resonates with the incident wave, forming a load of ultra-high frequency stress along the axial direction of the sample, and forming plastic deformation on the sample.

步骤4中,试样采用冷却液进行循环冷却。In step 4, the sample is cooled by circulating cooling liquid.

由于超高频交变载荷作用下,材料的内摩擦生热较为明显,防止温度过高导致塑性变形所产生的变形组织发生回复再结晶。Under the action of ultra-high frequency alternating load, the internal friction heat generation of the material is more obvious, so as to prevent the recovery and recrystallization of the deformed structure caused by plastic deformation caused by excessive temperature.

本发明与现有技术相比具有显著优点如下:Compared with the prior art, the present invention has significant advantages as follows:

(1)共振时极高的频率,使得单次加载时间非常之短,从而使其应变速率非常高,因此本发明对金属进行塑性变形时所达到的应变速率远远超过了传统冷变形方式。(1) The extremely high frequency during resonance makes the single loading time very short, so that the strain rate is very high, so the strain rate achieved by the present invention when plastically deforming metal far exceeds the traditional cold deformation method.

(2)本发明采用处理方式对金属的外形改变极小,可以在基本不改变外形的情况下强化金属材料,而传统的变形手段则对样品外形尺寸有一个较大的改变。(2) The present invention adopts the processing method to change the shape of the metal very little, and can strengthen the metal material without changing the shape basically, while the traditional deformation means has a large change to the shape of the sample.

(3)本发明在金属材料塑性变形处理过程中,金属材料的一端是一直裸露在外,故而可将其裸露端浸泡在液氮中进行持续深冷塑性变形,这是传统塑性变形方式无法做到的。(3) During the plastic deformation treatment process of the metal material, one end of the metal material is always exposed, so the exposed end can be soaked in liquid nitrogen for continuous cryogenic plastic deformation, which cannot be achieved by traditional plastic deformation methods of.

(4)本发明操作流程简单,可控性好,效率高。(4) The present invention has simple operation process, good controllability and high efficiency.

附图说明Description of drawings

图1为本发明的变形设计试样示意图。Fig. 1 is a schematic diagram of a deformed design sample of the present invention.

图2为超高应变速率加载装置示意图。Figure 2 is a schematic diagram of the ultra-high strain rate loading device.

图3为谐振部位任意点的应力与时间的关系图。Figure 3 is a graph showing the relationship between stress and time at any point in the resonance part.

图4为本发明塑性变形强化后的316L不锈钢金相图。Fig. 4 is a metallographic diagram of 316L stainless steel after plastic deformation strengthening of the present invention.

图5为本发明塑性变形强化后的铝合金金相图。Fig. 5 is a metallographic diagram of the aluminum alloy after plastic deformation strengthening according to the present invention.

图6为本发明塑性变形强化后的紫铜金相图。Fig. 6 is a metallographic diagram of red copper after plastic deformation strengthening in the present invention.

图7为本发明塑性变形强化后的铜铬锆合金相图。Fig. 7 is a phase diagram of the copper-chromium-zirconium alloy after plastic deformation strengthening of the present invention.

具体实施方式Detailed ways

下面结合附图及实施例对本发明做进一步说明Below in conjunction with accompanying drawing and embodiment the present invention will be further described

实施例1Example 1

316L不锈钢的超高速率塑性变形处理。Ultra-high rate plastic deformation treatment of 316L stainless steel.

1.将316L不锈钢切割为如附图1所示的试验样品,并使用砂纸将表面打磨光滑。给定316L不锈钢样品的相关参数:f=20kHz,E=206GPa,ρ=7.85g/cm3,L1=25mm,L2=20mm,b1=3mm,b2=12mm根据步骤1中相关公式1. Cut 316L stainless steel into a test sample as shown in Figure 1, and use sandpaper to smooth the surface. Given the relevant parameters of the 316L stainless steel sample: f=20kHz, E=206GPa, ρ=7.85g/cm 3 , L1=25mm, L2=20mm, b1=3mm, b2=12mm According to the relevant formula in step 1

其中:in:

试样谐振长度L3为:The resonant length L3 of the sample is:

经过计算得到谐振长度L3=8.78mmAfter calculation, the resonance length L3 = 8.78mm

2.设置超声波参数,根据参数的设置标准,超声波加载的峰值应高于试样材料的屈服强度,根据步骤2可知,峰值比原始材料的屈服强度高的越多一般来说强化越明显,已知所采用的316L不锈钢的屈服强度约为300MPa,将载荷峰值设置为390MPa,根据载荷的峰值通过公式计算出加载电流I。2. Set the ultrasonic parameters. According to the parameter setting standard, the peak value of ultrasonic loading should be higher than the yield strength of the sample material. According to step 2, the more the peak value is higher than the yield strength of the original material, the more obvious the strengthening is generally. It is known that the yield strength of the 316L stainless steel used is about 300MPa, the peak value of the load is set to 390MPa, and the loading current I is calculated by the formula according to the peak value of the load.

A0=μI(μ=16)A 0 =μI(μ=16)

经计算得I=2.5安培Calculated I = 2.5 ampere

3.对316L不锈钢试样进行了20分钟的超高应变速率的塑性变形,变形期间以水作为冷却液不断喷洒其表面使其温度不至于过度升高。3. The 316L stainless steel sample was plastically deformed at an ultra-high strain rate for 20 minutes. During the deformation, water was used as a cooling liquid to continuously spray its surface so that the temperature would not rise excessively.

对处理后的316L不锈钢试样变形部位进行表征结果如下:The characterization results of the deformed part of the treated 316L stainless steel sample are as follows:

附图4中,左图为处理前316L不锈钢原始样品金相图,右图为经超高应变速率塑性变形后的316L不锈钢金相图In accompanying drawing 4, the left picture is the metallographic diagram of the original 316L stainless steel sample before treatment, and the right picture is the metallographic picture of the 316L stainless steel after plastic deformation at an ultra-high strain rate

从金相图可以看出,经本发明所处理的316L不锈钢内部出现了大量的变形组织,可见其发生了明显的塑性变形。It can be seen from the metallographic diagram that a large number of deformed structures appear inside the 316L stainless steel treated by the present invention, which shows that it has undergone obvious plastic deformation.

b.硬度测试b. Hardness test

使用维氏显微硬度硬度仪对原始316L不锈钢材料及经本发明处理过的316L不锈钢材料进行测试,结果显示原始样的维氏硬度约为160Hv,经超高应变速率塑性变形后其维氏硬度达到了220Hv。显示出了明显的硬度提升。Use the Vickers microhardness tester to test the original 316L stainless steel material and the 316L stainless steel material processed by the present invention, the results show that the Vickers hardness of the original sample is about 160Hv, and its Vickers hardness after plastic deformation at an ultra-high strain rate Reached 220Hv. A significant increase in hardness is shown.

实施例2Example 2

5A02铝合金的超高速率塑性变形处理。Ultra-high rate plastic deformation treatment of 5A02 aluminum alloy.

1.将5A02铝合金切割为如附图1所示的试验样品,并使用砂纸将表面打磨光滑。给定5A02铝合金样品的相关参数:f=20kHz,E=71GPa,ρ=2.7g/cm3,L1=24mm,L2=20mm,,b1=6mm,b2=14mm1. Cut the 5A02 aluminum alloy into a test sample as shown in Figure 1, and use sandpaper to smooth the surface. Given the relevant parameters of the 5A02 aluminum alloy sample: f=20kHz, E=71GPa, ρ=2.7g/cm 3 , L1=24mm, L2=20mm, b1=6mm, b2=14mm

根据步骤1中相关公式According to the relevant formula in step 1

其中:in:

试样谐振长度L3为:The resonant length L3 of the sample is:

经过计算得到谐振长度L3=10mm。The resonant length L3=10mm is obtained through calculation.

2.设置超声波参数,根据参数的设置标准,超声波加载的峰值应高于试样材料的屈服强度,根据步骤2可知,峰值比原始材料的屈服强度高的越多一般来说强化越明显,已知所采用的5A02铝合金的屈服强度约为120MPa,将载荷峰值设置为200MPa。2. Set the ultrasonic parameters. According to the parameter setting standard, the peak value of ultrasonic loading should be higher than the yield strength of the sample material. According to step 2, the more the peak value is higher than the yield strength of the original material, the more obvious the strengthening is generally. It is known that the yield strength of the 5A02 aluminum alloy used is about 120MPa, and the peak load is set to 200MPa.

根据载荷的峰值通过公式计算出加载电流I。According to the peak value of the load, the loading current I is calculated by the formula.

A0=μI(μ=16)A 0 =μI(μ=16)

经计算得I=1.8安培Calculated I = 1.8 ampere

3.对5A02铝合金试样进行了约10分钟的超高应变速率的塑性变形,变形期间以水作为冷却液不断喷洒其表面使其温度不至于过度升高。3. The 5A02 aluminum alloy sample was plastically deformed at an ultra-high strain rate for about 10 minutes. During the deformation, water was used as a cooling liquid to continuously spray its surface so that the temperature would not rise excessively.

对处理后的5A02铝合金试样变形部位进行表征结果如下:The characterization results of the deformed parts of the treated 5A02 aluminum alloy sample are as follows:

附图5中,左图为处理前5A02铝合金原始样品偏光显微镜金相图,右图为经超高应变速率塑性变形后的5A02铝合金金相图In attached drawing 5, the left picture is the metallographic picture of the original sample of 5A02 aluminum alloy before treatment, and the right picture is the metallographic picture of the 5A02 aluminum alloy after plastic deformation at an ultra-high strain rate

从金相图可以看出,经本发明所处理的5A02铝合金内部出现了大量的变形组织,组织明显细化,可见其发生了明显的塑性变形。It can be seen from the metallographic diagram that a large number of deformed structures appear inside the 5A02 aluminum alloy treated by the present invention, and the structure is obviously refined, which shows that it has undergone obvious plastic deformation.

b.硬度测试b. Hardness test

使用维氏显微硬度硬度仪对原始5A02铝合金材料及经本发明处理过的5A02铝合金材料进行测试,结果显示原始样的维氏硬度约为60Hv,经超高应变速率塑性变形后其维氏硬度达到了100Hv。显示出了明显的硬度提升。Vickers microhardness tester is used to test the original 5A02 aluminum alloy material and the 5A02 aluminum alloy material processed by the present invention, and the results show that the Vickers hardness of the original sample is about 60Hv, and it is maintained after plastic deformation at an ultra-high strain rate. Its hardness has reached 100Hv. A significant increase in hardness is shown.

实施例3Example 3

紫铜的超高速率塑性变形处理。Ultra-high rate plastic deformation treatment of copper.

1.将紫铜切割为如附图1所示的试验样品,并使用砂纸将表面打磨光滑。1. Cut the red copper into test samples as shown in Figure 1, and use sandpaper to smooth the surface.

给定紫铜样品的相关参数:f=20kHz,E=108GPa,ρ=8.9g/cm3,L1=16mm,L2=12mm,b1=3mm,b2=10mm。Given the relevant parameters of the red copper sample: f=20kHz, E=108GPa, ρ=8.9g/cm 3 , L1=16mm, L2=12mm, b1=3mm, b2=10mm.

根据步骤1中相关公式According to the relevant formula in step 1

其中:in:

试样谐振长度L3为:The resonant length L3 of the sample is:

经过计算得到谐振长度,L3=9.4mmAfter calculation, the resonance length is obtained, L3=9.4mm

2.设置超声波参数,根据参数的设置标准,超声波加载的峰值应高于试样材料的屈服强度,根据步骤2可知,峰值比原始材料的屈服强度高的越多一般来说强化越明显,已知所采用的紫铜的屈服强度约为120MPa,将载荷峰值设置为300MPa。根据载荷的峰值通过公式计算出加载电流I。2. Set the ultrasonic parameters. According to the parameter setting standard, the peak value of ultrasonic loading should be higher than the yield strength of the sample material. According to step 2, the more the peak value is higher than the yield strength of the original material, the more obvious the strengthening is generally. It is known that the yield strength of the copper used is about 120MPa, and the peak load is set to 300MPa. According to the peak value of the load, the loading current I is calculated by the formula.

A0=μI(μ=16)A 0 =μI(μ=16)

经计算得I=2.2安培Calculated I = 2.2 ampere

3.对紫铜试样进行了约5分钟的超高应变速率的塑性变形,变形期间以水作为冷却液不断喷洒其表面使其温度不至于过度升高。3. The copper sample was plastically deformed at an ultra-high strain rate for about 5 minutes. During the deformation, water was used as a cooling liquid to continuously spray its surface so that the temperature would not rise excessively.

对处理后的紫铜试样变形部位进行表征结果如下:The results of characterization of the deformed part of the treated red copper sample are as follows:

附图6中,左图为处理前紫铜原始样品偏光显微镜金相图,右图为经超高应变速率塑性变形后的紫铜金相图In accompanying drawing 6, the left picture is the metallographic image of the original copper sample before treatment under the polarizing microscope, and the right picture is the metallographic picture of the copper after plastic deformation at an ultra-high strain rate

从金相图可以看出,经本发明所处理的紫铜内部出现了大量的变形组织,组织明显细化,可见其发生了明显的塑性变形。It can be seen from the metallographic diagram that a large amount of deformed structures appear inside the red copper treated by the present invention, and the structures are obviously refined, which shows that it has undergone obvious plastic deformation.

b.硬度测试b. Hardness test

使用维氏显微硬度硬度仪对原始紫铜及经本发明处理过的紫铜进行测试,结果显示原始样的维氏硬度约为60Hv,经超高应变速率塑性变形后其维氏硬度达到了110Hv。显示出了明显的硬度提升。The Vickers microhardness tester was used to test the original red copper and the red copper treated by the present invention, and the results showed that the Vickers hardness of the original sample was about 60Hv, and the Vickers hardness of the original sample reached 110Hv after plastic deformation at an ultra-high strain rate. A significant increase in hardness is shown.

实施例4Example 4

铜铬镐合金的超高速率塑性变形处理。Ultrahigh-rate plastic deformation processing of copper-chromium pick alloys.

1.将铜铬镐合金切割为如附图1所示的试验样品,并使用砂纸将表面打磨光滑。给定铜铬镐合金样品的相关参数:f=20kHz,E=110GPa,ρ=8.9g/cm3,L1=16mm,L2=12mm,b1=3mm,b2=11mm1. Cut the copper-chromium pick alloy into test samples as shown in Figure 1, and use sandpaper to polish the surface smoothly. Relevant parameters of a given copper-chromium pickaxe alloy sample: f=20kHz, E=110GPa, ρ=8.9g/cm 3 , L1=16mm, L2=12mm, b1=3mm, b2=11mm

根据步骤1中相关公式According to the relevant formula in step 1

其中:in:

试样谐振长度L3为:The resonant length L3 of the sample is:

经过计算得到谐振长度L3=8.7mm。The resonant length L3=8.7mm is obtained through calculation.

2.设置超声波参数,根据参数的设置标准,超声波加载的峰值应高于试样材料的屈服强度,根据步骤2可知,峰值比原始材料的屈服强度高的越多一般来说强化越明显,已知所采用的铜铬镐合金的屈服强度约为120MPa,将载荷峰值设置为300MPa。2. Set the ultrasonic parameters. According to the parameter setting standard, the peak value of ultrasonic loading should be higher than the yield strength of the sample material. According to step 2, the more the peak value is higher than the yield strength of the original material, the more obvious the strengthening is generally. It is known that the yield strength of the copper-chromium alloy used is about 120MPa, and the peak load is set at 300MPa.

根据载荷的峰值通过公式计算出加载电流I。According to the peak value of the load, the loading current I is calculated by the formula.

A0=μI(μ=16)A 0 =μI(μ=16)

经计算得I=2.2安培Calculated I = 2.2 ampere

3.对铜铬镐合金试样进行了约5分钟的超高应变速率的塑性变形,变形期间以水作为冷却液不断喷洒其表面使其温度不至于过度升高。3. The copper-chromium pickaxe alloy sample was plastically deformed at an ultra-high strain rate for about 5 minutes. During the deformation, water was used as a cooling liquid to continuously spray its surface so that the temperature would not rise excessively.

对处理后的铜铬镐合金试样变形部位进行表征结果如下:The results of characterizing the deformed part of the treated copper-chromium pickaxe alloy sample are as follows:

附图7中,左图为处理前铜铬锆合金原始样品偏光显微镜金相图,右图为经超高应变速率塑性变形后的铜铬锆合金相图In accompanying drawing 7, the left picture is the polarizing microscope metallographic picture of the original copper-chromium-zirconium alloy sample before treatment, and the right picture is the phase picture of the copper-chromium-zirconium alloy after plastic deformation at an ultra-high strain rate

从金相图可以看出,经本发明所处理的铜铬锆合金内部出现了大量的变形组织,组织明显细化,可见其发生了明显的塑性变形。It can be seen from the metallographic diagram that a large number of deformed structures appear inside the copper-chromium-zirconium alloy treated by the present invention, and the structure is obviously refined, which shows that it has undergone obvious plastic deformation.

b.硬度测试b. Hardness test

使用维氏显微硬度硬度仪对原始铜铬锆合金及经本发明处理过的铜铬锆合金进行测试,结果显示原始样的维氏硬度约为90Hv,经超高应变速率塑性变形后其维氏硬度达到了140Hv。显示出了明显的硬度提升。Use the Vickers microhardness tester to test the original copper-chromium-zirconium alloy and the copper-chromium-zirconium alloy processed by the present invention. The results show that the Vickers hardness of the original sample is about 90Hv. Its hardness has reached 140Hv. A significant increase in hardness is shown.

本发明中,共振频率的选择,共振频率越高,单次加载时间就越短,根据应变速率计算公式dε/dt,其中ε为应变,t为时间,dε可以从所需强化的金属材料的工程应力应变曲线中获得,具体是从明显屈服点到谐振时应力幅值对应的强度点为实际应变,dt则是与系统的谐振频率有关,其在一个周期加载时间为1/f,dt则是实际发生塑性变形的那一段的时间tσ-tMAX如附图3所示,那么根据设备20000Hz的谐振频率,其△t经计算在10-6级别,当实际的应力峰值达到材料屈服强度的1.3倍以上,其平均应变速率可达到103。当应变不变情况下,时间越短应变速率越高。要增加应变速率可以通过不断提升谐振频率的方法来获得。In the present invention, the selection of the resonant frequency, the higher the resonant frequency, the shorter the single loading time, according to the strain rate calculation formula dε/dt, wherein ε is the strain, t is the time, and dε can be obtained from the metal material to be strengthened Obtained from the engineering stress-strain curve, specifically, the strength point corresponding to the stress amplitude from the apparent yield point to resonance is the actual strain, dt is related to the resonance frequency of the system, and its loading time in one cycle is 1/f, and dt is is the time t σ -t MAX during which plastic deformation actually occurs. More than 1.3 times of that, the average strain rate can reach 10 3 . When the strain remains constant, the shorter the time, the higher the strain rate. To increase the strain rate can be obtained by continuously increasing the resonance frequency.

2:应力幅值,应力幅值在步骤1中已经给出了相关计算公式,其主要由超声发生器的加载电流决定,通过所需的应力幅值经计算便能得到所需加的载电流。其选择的关键在于共振区域超声波的应力幅值对应的载荷必须远远超过样品的屈服强度。2: Stress amplitude, the relevant calculation formula of the stress amplitude has been given in step 1, which is mainly determined by the loading current of the ultrasonic generator, and the required loading current can be obtained by calculating the required stress amplitude . The key to its selection is that the load corresponding to the stress amplitude of the ultrasonic wave in the resonance region must far exceed the yield strength of the sample.

超声波是一种机械波,机械振动的纵波传到试样自由端后发生反射,反射波的频率与入射波的频率一致,两列干涉波产生谐振,因此沿试样轴向形成超高频应力的载荷。试样一端通过内螺纹与放大器底端连接,另一端自由(详见附图2)。由步骤1,2可知,试样中部平行段的应力幅值最大,为塑性变形区。Ultrasound is a kind of mechanical wave. The longitudinal wave of mechanical vibration is transmitted to the free end of the sample and then reflected. The frequency of the reflected wave is consistent with the frequency of the incident wave. The two columns of interference waves resonate, so the UHF stress is formed along the axial direction of the sample. load. One end of the sample is connected to the bottom of the amplifier through an internal thread, and the other end is free (see Figure 2 for details). From steps 1 and 2, it can be seen that the stress amplitude of the parallel section in the middle of the sample is the largest, which is the plastic deformation zone.

Claims (5)

1. A method for achieving ultra-high strain rate plastic deformation strengthening in metal, characterized by:
step 1, processing a metal material into the shape of a sample with a required shape according to the density and the elastic modulus of the metal material, so that ultrasonic waves can generate resonance in a deformation area to form ultrahigh-frequency stress waves;
and 2, connecting the processed sample with ultrasonic equipment, and selecting ultrasonic power.
And 3, ensuring that one end of the sample is connected with the bottom end of the ultrasonic equipment amplifier through the internal thread and the other end is free.
And 4, starting ultrasonic resonance, reflecting longitudinal waves of mechanical vibration after the longitudinal waves are transmitted to the free end of the sample, generating resonance between the frequency of the reflected waves and the frequency of the incident waves, forming a load of ultrahigh frequency stress along the axial direction of the sample, and forming plastic deformation on the sample.
2. The method of achieving ultra-high strain rate plastic deformation strengthening in metals of claim 1, wherein in step 1, the sample is a tensile specimen with a middle uniform-section plate shape.
3. The method of claim 1 or 2, wherein the sample has a resonant length L required for the ultrasonic wave to resonate in the deformation region3The following formula is satisfied:
using the vibration equation U (x) of the longitudinal direction of the sample as: using the vibration equation U (x) of the longitudinal direction of the sample as:
wherein:
sample resonant length L3Comprises the following steps:
the maximum stress amplitude of the plate-shaped sample is as follows:
the displacement stress coefficient is:
A0=μI
wherein b is1、b2、L1、L2For given design parameters, L1Is the half length of the plastic deformation zone of the specimen, L2The parallel distance of the arc transition ends is b1Thickness of the plastically deformed region of the specimen, b2Is the thickness of the connecting end; e is the modulus of elasticity; rho is density; the resonant frequency f of the ultrahigh strain rate loading system is 20 kHz; c is the longitudinal wave velocity; w is the angular velocity; mu is a displacement amplification coefficient corresponding to the equipment, and the equipment mu used in the invention is 16; i is the current provided by the equipment power supply; alpha is alpha1,β1And k is a physical derivation process quantity, which can be represented by a basic quantity.
4. The method for achieving ultra-high strain rate plastic deformation strengthening in metals according to claim 1, wherein step 2 specifically comprises: the peak of the ultrasonic loading should be above the yield strength of the sample material.
5. The method of achieving ultra-high strain rate plastic deformation strengthening in metals of claim 1, wherein in step 4, the sample is cooled by circulating a cooling fluid.
CN201810658115.8A 2018-06-25 2018-06-25 Method for realizing ultrahigh strain rate plastic deformation strengthening in metal Active CN110629012B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810658115.8A CN110629012B (en) 2018-06-25 2018-06-25 Method for realizing ultrahigh strain rate plastic deformation strengthening in metal

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810658115.8A CN110629012B (en) 2018-06-25 2018-06-25 Method for realizing ultrahigh strain rate plastic deformation strengthening in metal

Publications (2)

Publication Number Publication Date
CN110629012A true CN110629012A (en) 2019-12-31
CN110629012B CN110629012B (en) 2021-05-07

Family

ID=68966810

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810658115.8A Active CN110629012B (en) 2018-06-25 2018-06-25 Method for realizing ultrahigh strain rate plastic deformation strengthening in metal

Country Status (1)

Country Link
CN (1) CN110629012B (en)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0666142A1 (en) * 1994-02-04 1995-08-09 Gec Alsthom Electromecanique Sa Method and device for the surface treatment and for the pre-stressing of the inner wall of a cavity
US6843957B2 (en) * 1998-09-03 2005-01-18 U.I.T., L.L.C. Ultrasonic impact methods for treatment of welded structures
CN1924030A (en) * 2005-08-30 2007-03-07 宝山钢铁股份有限公司 Metal surface nanolizing method of supersonic wave high-energy surface machinery processing
CN201212054Y (en) * 2008-07-10 2009-03-25 北京有色金属研究总院 Ultrasonic wave surface strengthening treatment device for metal material surface treatment
RU2442841C2 (en) * 2010-05-27 2012-02-20 Государственное образовательное учреждение высшего профессионального образования "Национальный исследовательский Томский политехнический университет" Method for preparation of raw piece surface using ultrasonic oscillations
CN102560078A (en) * 2010-12-24 2012-07-11 北京有色金属研究总院 Steel and iron material surface nanometering method
CN108441612A (en) * 2018-03-28 2018-08-24 中国石油大学(华东) Two-phase section is plastically deformed and ultrasonic coupling realizes carbon steel surface modification device and technique

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0666142A1 (en) * 1994-02-04 1995-08-09 Gec Alsthom Electromecanique Sa Method and device for the surface treatment and for the pre-stressing of the inner wall of a cavity
US6843957B2 (en) * 1998-09-03 2005-01-18 U.I.T., L.L.C. Ultrasonic impact methods for treatment of welded structures
CN1924030A (en) * 2005-08-30 2007-03-07 宝山钢铁股份有限公司 Metal surface nanolizing method of supersonic wave high-energy surface machinery processing
CN201212054Y (en) * 2008-07-10 2009-03-25 北京有色金属研究总院 Ultrasonic wave surface strengthening treatment device for metal material surface treatment
RU2442841C2 (en) * 2010-05-27 2012-02-20 Государственное образовательное учреждение высшего профессионального образования "Национальный исследовательский Томский политехнический университет" Method for preparation of raw piece surface using ultrasonic oscillations
CN102560078A (en) * 2010-12-24 2012-07-11 北京有色金属研究总院 Steel and iron material surface nanometering method
CN108441612A (en) * 2018-03-28 2018-08-24 中国石油大学(华东) Two-phase section is plastically deformed and ultrasonic coupling realizes carbon steel surface modification device and technique

Also Published As

Publication number Publication date
CN110629012B (en) 2021-05-07

Similar Documents

Publication Publication Date Title
Vinogradov et al. Fatigue of severely deformed metals
Han et al. A superior combination of strength-ductility in CoCrFeNiMn high-entropy alloy induced by asymmetric rolling and subsequent annealing treatment
Zhou et al. A comparative study of mechanical and microstructural characteristics of aluminium and titanium undergoing ultrasonic assisted compression testing
Karaman et al. The effect of severe marforming on shape memory characteristics of a Ti-rich NiTi alloy processed using equal channel angular extrusion
WO2019100809A1 (en) High strength and toughness filamentous grain pure titanium and preparation method therefor
CN110241367A (en) A Method of Strengthening and Toughening Aluminum Alloy Based on Pulse Current
CN107130197B (en) A kind of deformation heat treatment method of Ultra-fine Grained AZ80 magnesium alloys
Zhou et al. Tensile behavior of nickel with gradient microstructure produced by laser shock peening
Jung et al. Enhancement of fatigue life of aluminum alloy affected by the density of pulsed electric current
Ye et al. RETRACTED-Effect of electropulsing treatment on the microstructure, texture, and mechanical properties of cold-rolled Ti–6Al–4V alloy
Xie et al. Effects of ultrasonic vibration on performance and microstructure of AZ31 magnesium alloy under tensile deformation
Yuan et al. Hot forming-quenching integrated process with cold-hot dies for 2A12 aluminum alloy sheet
Sajadifar et al. Cyclic deformation response of ultra-fine grained titanium at elevated temperatures
Li et al. Research on microstructure evolution and deformation behaviors of AZ31 Mg alloy sheets processed by a new severe plastic deformation with different temperatures
Li et al. Effect of pulse current on the tensile deformation of SUS304 stainless steel
ZHANG et al. Effects of stacking fault energy on the deformation mechanisms and mechanical properties of face-centered cubic metals
Zhang et al. Achieving high ductility and strength in magnesium alloy through cryogenic-hot forming
Rong et al. Microstructure and mechanical properties of rolled Mg-12Gd-3Y-0.4 Zr alloy sheets
CN110629012A (en) A method for ultrahigh strain rate plastic deformation strengthening in metals
Ghorbani et al. Microstructural evolution and room temperature mechanical properties of AZ31 alloy processed through hot constrained compression
Huang et al. Effect of thermal deformation parameters on the microstructure, texture, and microhardness of 5754 aluminum alloy
CN111394670A (en) Method for enhancing mechanical property of aluminum alloy based on ultrasonic cyclic resonance effect
Hwang et al. Dynamic deformation behavior of ultrafine-grained low-carbon steels fabricated by equal-channel angular pressing
YUAN et al. Influence of hydrogen content on room temperature compressive properties of Ti–6Al–4V alloy at high strain rate
Kwak et al. Processing and mechanical properties of fine grained magnesium by equal channel angular pressing

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant