CN104160049B - Mar proof, extrudability, the aluminium alloy of forging excellent processability - Google Patents
Mar proof, extrudability, the aluminium alloy of forging excellent processability Download PDFInfo
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- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 33
- 238000005242 forging Methods 0.000 title abstract description 24
- 239000000463 material Substances 0.000 claims abstract description 55
- 230000005496 eutectics Effects 0.000 claims abstract description 31
- 239000012535 impurity Substances 0.000 claims abstract description 4
- 230000003287 optical effect Effects 0.000 claims description 6
- 239000013078 crystal Substances 0.000 claims description 5
- 239000002344 surface layer Substances 0.000 claims description 4
- 238000005457 optimization Methods 0.000 abstract 1
- 230000000052 comparative effect Effects 0.000 description 19
- 230000000694 effects Effects 0.000 description 15
- 238000001125 extrusion Methods 0.000 description 13
- 239000000203 mixture Substances 0.000 description 13
- 238000009721 upset forging Methods 0.000 description 10
- 229910052710 silicon Inorganic materials 0.000 description 7
- 238000000034 method Methods 0.000 description 6
- 238000005496 tempering Methods 0.000 description 6
- 229910052802 copper Inorganic materials 0.000 description 5
- 239000000956 alloy Substances 0.000 description 4
- 238000011156 evaluation Methods 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- 229910045601 alloy Inorganic materials 0.000 description 3
- 238000009826 distribution Methods 0.000 description 3
- 235000012438 extruded product Nutrition 0.000 description 3
- 229910052749 magnesium Inorganic materials 0.000 description 3
- 238000009864 tensile test Methods 0.000 description 3
- 229910019018 Mg 2 Si Inorganic materials 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 239000011856 silicon-based particle Substances 0.000 description 2
- 229910018125 Al-Si Inorganic materials 0.000 description 1
- 229910021364 Al-Si alloy Inorganic materials 0.000 description 1
- 229910018520 Al—Si Inorganic materials 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- 239000000498 cooling water Substances 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000012208 gear oil Substances 0.000 description 1
- 238000000265 homogenisation Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000010687 lubricating oil Substances 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 230000003746 surface roughness Effects 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/02—Alloys based on aluminium with silicon as the next major constituent
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C23/00—Extruding metal; Impact extrusion
- B21C23/002—Extruding materials of special alloys so far as the composition of the alloy requires or permits special extruding methods of sequences
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J1/00—Preparing metal stock or similar ancillary operations prior, during or post forging, e.g. heating or cooling
- B21J1/003—Selecting material
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/02—Alloys based on aluminium with silicon as the next major constituent
- C22C21/04—Modified aluminium-silicon alloys
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
- C22F1/043—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with silicon as the next major constituent
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Forging (AREA)
- Extrusion Of Metal (AREA)
Abstract
Description
技术领域technical field
本发明涉及在汽车、家电制品等中作为压缩机等部件使用的耐磨损性、挤出性、锻造加工性优良的铝合金。The present invention relates to an aluminum alloy excellent in wear resistance, extrudability, and forgeability used as components such as compressors in automobiles, home appliances, and the like.
背景技术Background technique
用于汽车、家电制品等中的压缩机等的铝合金要求耐磨损性等。例如,用于压缩机的铝合金为了提高耐磨损性、缩小热膨胀率,使用添加有10质量%(以下简称为%)以上Si的Al-Si合金。在专利文献1中记载了耐疲劳性和非烧结性优良的滑动用铝合金。在该铝合金中Si作为有助于非烧结性、耐磨损性的必须元素添加1~15%。但是,记载了Si的添加量超过15%时,铝合金发生脆化。Aluminum alloys used for compressors and the like in automobiles, home appliances, and the like are required to have wear resistance and the like. For example, an aluminum alloy used in a compressor is an Al-Si alloy to which 10% by mass (hereinafter simply referred to as %) or more of Si is added in order to improve wear resistance and reduce thermal expansion coefficient. Patent Document 1 describes an aluminum alloy for sliding that is excellent in fatigue resistance and non-sintering properties. In this aluminum alloy, Si is added in an amount of 1 to 15% as an essential element contributing to non-sinterability and wear resistance. However, it is described that when the amount of Si added exceeds 15%, the aluminum alloy becomes embrittled.
【现有技术文献】[Prior Art Literature]
【专利文献】【Patent Literature】
【专利文献1】日本特开平03-006345[Patent Document 1] Japanese Patent Application Laid-Open No. 03-006345
发明内容Contents of the invention
【发明要解决的课题】【Problems to be solved by the invention】
上述用于压缩机等的铝合金要求耐磨损性、膨胀系数等优良,因此,大量添加Si。但是,这样的铝合金虽然耐磨损性、膨胀系数等提高,但有可能挤出性等加工性降低和表面性状变差等。这是由于,铝合金具有所添加的各组成的成分浓度越高越难以加工的倾向。特别是为了提高耐磨损性而添加的Si在挤出工序、锻造工序中的加工工序中使生产率降低。实际上,这样的铝合金相对于对使用的部件所要求的耐磨损性、膨胀系数等而言具有该特性为必要以上的过量的规格的情况也不少。即,这些铝合金不一定需要耐磨损性等显著优良,因此,从生产率的观点出发,就耐磨性等必要特性而言,最好是根据用途来控制其成为最佳状态。The aluminum alloys used in compressors and the like are required to be excellent in wear resistance, expansion coefficient, etc., and therefore, a large amount of Si is added. However, although such an aluminum alloy has improved wear resistance, expansion coefficient, etc., there is a possibility that processability such as extrudability may decrease, and surface properties may deteriorate. This is because the aluminum alloy tends to be difficult to process as the concentration of each component added increases. In particular, Si added to improve wear resistance reduces productivity in the processing steps in the extrusion process and the forging process. In fact, such aluminum alloys often have excessive specifications that are more than necessary in terms of wear resistance, expansion coefficient, and the like required for components used. That is, these aluminum alloys do not necessarily need to be remarkably excellent in wear resistance and the like. Therefore, from the viewpoint of productivity, it is preferable to control the necessary properties such as wear resistance to an optimum state according to the application.
因此,通过将根据需要而要求的特性与生产率进行调和,不降低生产率而得到在成本方面具有优良效果的铝合金。Therefore, an aluminum alloy having an excellent effect in terms of cost can be obtained without lowering productivity by reconciling properties required as needed with productivity.
因此,在生产时尽量抑制生产率变差,同时得到的铝合金具有必要特性,在这两者之间保持平衡的铝合金的开发成为课题。Therefore, it is an issue to develop an aluminum alloy that maintains a balance between the reduction in productivity during production as much as possible and the obtained aluminum alloy having necessary properties.
鉴于上述情况,本发明的目的在于,提供能够生产在Al-Si系合金中挤出性以及锻造加工性优良、并且保持耐磨损性的可用于制造锻造物的铝合金。In view of the above circumstances, an object of the present invention is to provide an aluminum alloy that can be used for producing forgings that is excellent in extrudability and forging workability among Al-Si-based alloys and that maintains wear resistance.
【用于解决问题的方法】【Methods used to solve the problem】
本发明人进行了深入的研究,结果得到如下见解:通过调节各组成的添加量,并且控制共晶Si尺寸,得到将必要特性与生产率进行调和后的铝合金。即发现,通过下述方法实现上述本发明的目的。As a result of intensive studies, the present inventors obtained the insight that an aluminum alloy in which necessary characteristics and productivity are balanced can be obtained by adjusting the addition amount of each component and controlling the size of eutectic Si. That is, it was found that the object of the present invention described above is achieved by the following means.
即,根据本发明,提供一种耐磨损性、挤出性、锻造加工性优良的铝合金,其特征在于,含有Si5.5~7.0质量%(以下记为%)、Cu1.0~2.0%、Mg0.4~0.8%、Cr0.05~0.15%、Ni0.05~0.25%,余量由Al和不可避免的杂质构成,在与挤出材料的长度方向垂直的截面上将中央部的共晶Si尺寸设为Sc,将表层侧部的共晶Si尺寸设为Ss时,Sc-Ss≤15μm2,并且共晶Si尺寸是20μm2以下的粒数为1000~3000个/mm2。That is, according to the present invention, there is provided an aluminum alloy excellent in wear resistance, extrudability, and forgeability, characterized in that it contains Si5.5-7.0% by mass (hereinafter referred to as %), Cu1.0-2.0 %, Mg0.4~0.8%, Cr0.05~0.15%, Ni0.05~0.25%, and the balance is composed of Al and unavoidable impurities. When the eutectic Si size is Sc and the eutectic Si size at the surface side is Ss, Sc-Ss≤15 μm 2 , and the number of eutectic Si particles with a eutectic Si size of 20 μm 2 or less is 1000 to 3000/mm 2 .
优选提供耐磨损性、挤出性、锻造加工性优良的铝合金,其还含有Sr 0.01~0.05%。It is preferable to provide an aluminum alloy excellent in wear resistance, extrudability, and forgeability, which further contains 0.01 to 0.05% of Sr.
【发明效果】【Invention effect】
本发明可以提供通过适当控制铝合金的各组成以及共晶Si尺寸而能够生产挤出性以及锻造加工性优良、并且保持耐磨损性的用于制造挤出材料、锻造材料的铝合金材料。The present invention can provide an aluminum alloy material for producing extruded materials and forged materials that is excellent in extrudability and forging processability and maintains wear resistance by appropriately controlling the various compositions of the aluminum alloy and the size of the eutectic Si.
附图说明Description of drawings
【图1】是对由挤出而制造的挤出品进行锻造加工的图。[ Fig. 1 ] is a diagram of forging an extruded product produced by extrusion.
具体实施方式detailed description
以下,对本发明的实施方式进行说明。Embodiments of the present invention will be described below.
首先,对本发明的铝合金中的各添加元素进行说明。First, each additional element in the aluminum alloy of the present invention will be described.
Si通过生成Si化合物而有助于磨损性。另外,Si与Mg一起形成Mg2Si,Si是有助于强度的元素。Si的添加量低于5.5%时,强度、耐磨损性的效果弱。超过7.0%时,表面性状变差,挤出性降低。Si contributes to abrasiveness by forming a Si compound. In addition, Si forms Mg 2 Si together with Mg, and Si is an element contributing to strength. When the amount of Si added is less than 5.5%, the effects of strength and wear resistance are weak. When it exceeds 7.0%, surface properties will deteriorate and extrudability will fall.
Cu有助于强度提高。Cu的添加量低于1.0%时,强度提高的效果小,超过2.0%时,挤出加工性、耐腐蚀性变差。Cu contributes to strength improvement. When the amount of Cu added is less than 1.0%, the effect of improving the strength is small, and when it exceeds 2.0%, extrusion processability and corrosion resistance deteriorate.
Mg与Si一起形成Mg2Si,有助于强度提高。Mg的添加量低于0.4%时,其效果小。超过0.8%时,挤出加工性降低。优选Mg为0.55~0.65%。Mg forms Mg 2 Si together with Si and contributes to an increase in strength. When the added amount of Mg is less than 0.4%, the effect is small. When exceeding 0.8%, extrusion processability will fall. Preferably, Mg is 0.55 to 0.65%.
Cr对晶粒微小化有效,有助于强度提高。Cr的添加量低于0.05%时,该效果小。超过0.15%后,其效果没有大幅变化。优选Cr为0.07~0.10%。Cr is effective for miniaturization of crystal grains and contributes to improvement of strength. When the amount of Cr added is less than 0.05%, this effect is small. After exceeding 0.15%, the effect does not change significantly. Cr is preferably 0.07 to 0.10%.
Ni对耐热性、耐磨损性提高有效,也有助于强度提高。Ni的添加量低于0.05%时,其效果小。超过0.25%后,其效果没有大幅变化,并且导致挤出性变差。优选Ni为0.07~0.13%。Ni is effective for improving heat resistance and wear resistance, and also contributes to improving strength. When the amount of Ni added is less than 0.05%, the effect is small. When it exceeds 0.25%, the effect does not change greatly, and extrudability deteriorates. Ni is preferably 0.07 to 0.13%.
Sr的添加而有助于机械性质的提高。Sr用于结晶后的Si的改良处理,通过添加Sr,结晶后的Si成为微小的形态。Sr的添加量优选为0.01~0.05%。Sr的添加量低于0.01%时,其效果小。超过0.05%时,其效果没有大幅变化。The addition of Sr contributes to the improvement of mechanical properties. Sr is used for improvement treatment of crystallized Si, and by adding Sr, crystallized Si becomes a fine form. The added amount of Sr is preferably 0.01 to 0.05%. When the added amount of Sr is less than 0.01%, the effect is small. When it exceeds 0.05%, the effect does not change significantly.
Fe、Mn被添加时,与其他元素生成化合物,会导致各添加元素的效果变差,因此,本发明中的铝合金为0.5%以下。When Fe and Mn are added, they will form compounds with other elements, and the effect of each added element will be reduced. Therefore, the aluminum alloy in the present invention is 0.5% or less.
另外,本发明的铝合金除了上述元素之外,还含有不可避免的杂质和Al。例如,在不损害发明效果的范围内,可以少量含有Ti、Zr、Zn。不损害发明效果的范围是指0.05%以下。In addition, the aluminum alloy of the present invention contains unavoidable impurities and Al in addition to the above elements. For example, Ti, Zr, and Zn may be contained in small amounts within the range that does not impair the effects of the invention. The range that does not impair the effect of the invention means 0.05% or less.
共晶Si对表面性状、耐磨损性产生影响,因此,这些特性的均一性是由挤出材料以及锻造材料的共晶Si的尺寸和分布来决定的。即,本发明的铝合金通过控制Si等各组成的含量,获得优良的挤出性以及锻造加工性,另外,通过控制共晶Si的尺寸和分布,防止由表面性状以及部位的原因而造成的特性上的偏差。由此,通过本发明,能够以高生产率得到特性均一的挤出材料以及锻造材料。Since eutectic Si affects surface properties and wear resistance, the uniformity of these properties is determined by the size and distribution of eutectic Si in extruded materials and forged materials. That is, the aluminum alloy of the present invention obtains excellent extrudability and forgeability by controlling the content of various components such as Si, and in addition, by controlling the size and distribution of eutectic Si, it prevents defects caused by surface properties and parts. Deviations in characteristics. Thus, according to the present invention, extruded materials and forged materials with uniform properties can be obtained with high productivity.
通过将Ss和Sc控制为Sc-Ss≤15μm2,使得挤出材料的表面性状好,并且能够抑制挤出表层侧部与中央部的耐磨损性特性的分布不均。关于共晶Si尺寸,Ss指的是以在与挤出材料的长度方向垂直的截面上距表层50μm的深度为基准、在光学显微镜的100倍的视野中观察中心侧时的共晶Si尺寸。Ss是在同一视野中以中心角每隔90度测定4个部位,以其中的最大的值为准。Sc指的是在光学显微镜100倍的视野中观察到的挤出材料截面的中心部的共晶Si尺寸。本发明中的共晶Si尺寸是指共晶Si的结晶面积。By controlling Ss and Sc so that Sc-Ss≦15 μm 2 , the surface properties of the extruded material can be improved, and uneven distribution of wear resistance properties between the side and center of the extruded surface layer can be suppressed. Regarding the size of the eutectic Si, Ss refers to the size of the eutectic Si when the central side is observed in the field of view of 100 times of an optical microscope at a depth of 50 μm from the surface layer on a cross-section perpendicular to the longitudinal direction of the extruded material. Ss is measured at 4 locations at intervals of 90 degrees at the central angle in the same field of view, and the largest value among them shall prevail. Sc refers to the size of the eutectic Si at the center of the cross-section of the extruded material observed in a 100-fold field of view of an optical microscope. The eutectic Si size in the present invention refers to the crystal area of eutectic Si.
另外,通过使挤出材料中的共晶Si尺寸为20μm2以下,能够抑制表面的粗糙度。另外,为了得到耐磨损性,共晶Si的粒数为1000~3000个/mm2。共晶Si的尺寸20μm2以下的粒数低于1000个/mm2时,锻造后的耐磨损性的效果小。共晶Si的粒数超过3000个/mm2时,阻碍挤出性以及锻造加工性。In addition, by setting the size of the eutectic Si in the extruded material to 20 μm 2 or less, surface roughness can be suppressed. In addition, in order to obtain wear resistance, the number of eutectic Si grains is 1000 to 3000 grains/mm 2 . When the number of eutectic Si grains with a size of 20 μm 2 or less is less than 1000/mm 2 , the effect on wear resistance after forging is small. When the number of eutectic Si particles exceeds 3000/mm 2 , extrudability and forging workability are hindered.
需要说明的是,关于本发明中的铝合金的制造条件以及调质都没有特别限定,调质在通常的制造条件下根据用途选择即可。It should be noted that neither the production conditions nor the tempering of the aluminum alloy in the present invention are particularly limited, and the tempering may be selected according to the application under normal production conditions.
在使用挤出品作为锻造品的情况下,锻造工序中的加工性会对材料的硬度产生影响。由此,本发明的挤出品的调质优选为F、T1、O,进一步优选的调质为O。When an extruded product is used as a forged product, the workability in the forging process affects the hardness of the material. Therefore, the tempering of the extruded product of the present invention is preferably F, T1, O, and the more preferable tempering is O.
另外,锻造后的调质分别根据需要的特性来选择即可,但本发明中优选为T6。In addition, the quenching and tempering after forging may be selected according to the required characteristics, but T6 is preferable in the present invention.
【实施例】【Example】
基于实施例详细说明本发明,但本发明不限于此。The present invention will be described in detail based on examples, but the present invention is not limited thereto.
首先,在700℃~740℃的范围内加热,将表1所示的组成的合金熔解,得到铝合金熔液,使用金属模具进行铸造。以冷却水量达到70~100L/分钟的方式进行控制。First, by heating in the range of 700°C to 740°C, the alloys having the compositions shown in Table 1 were melted to obtain molten aluminum alloys, which were cast using metal molds. Control so that the amount of cooling water reaches 70 to 100 L/min.
得到直径220mm的铸块后,对该铸块实施在490℃下进行4小时加热的匀质化处理。将该铸块通过500℃的1个孔挤出,制得直径30mm的挤出圆棒。After obtaining an ingot with a diameter of 220 mm, the ingot was subjected to a homogenization treatment by heating at 490° C. for 4 hours. This ingot was extruded through one hole at 500° C. to obtain an extruded round rod with a diameter of 30 mm.
该样品的挤出材料,以在与长度方向垂直的截面上距表层50μm的深度为基准,在光学显微镜的100倍的视野中观察中心侧。在同一视野中以中心角每隔90度测定4个部位,测定其最大的共晶Si尺寸(Ss)。另外,对挤出材料截面的中心部在光学显微镜100倍的视野中观察共晶Si尺寸(Sc)。需要说明的是,共晶Si粒尺寸和个数通过旭化成Engineering株式会社制软件“图像分析软件A像くん”进行分析。关于表面性状,用HB的铅笔划表面时,将没有刮到的情况设为合格“○”,将刮到的情况设为不合格“×”。将结果示于表2。达到规定值的情况为合格,规定值以外的情况为不合格。The extruded material of this sample was observed on the central side with a 100-fold field of view of an optical microscope based on a depth of 50 μm from the surface layer on a cross-section perpendicular to the longitudinal direction. Four locations were measured at intervals of 90 degrees at a central angle in the same field of view, and the largest eutectic Si size (Ss) was measured. In addition, the eutectic Si size (Sc) was observed in the field of view of 100 times of an optical microscope at the central portion of the cross section of the extruded material. In addition, the size and number of eutectic Si grains were analyzed by the software "image analysis software A like-kun" manufactured by Asahi Kasei Engineering Co., Ltd. Regarding the surface properties, when the surface was scratched with an HB pencil, the case where there was no scratch was set as pass "◯", and the case where scratch was set as fail "x". The results are shown in Table 2. If it reaches the specified value, it is acceptable, and if it is outside the specified value, it is unqualified.
接着,将该挤出圆棒在400℃下进行5小时的退火处理,得到O材。在锻造评价时,确认了共晶Si尺寸、以及个数在发明的范围内。Next, the extruded round rod was annealed at 400° C. for 5 hours to obtain an O material. In the forging evaluation, it was confirmed that the size and number of eutectic Si were within the range of the invention.
接着,将该挤出圆棒沿长度方向以100mm的长度切割,实施加工率80%的镦锻。将锻造品在520℃下进行2小时的固溶处理后,立刻用50℃的温水进行淬火。再在180℃下进行10小时的人工时效处理,得到T6的调质。Next, this extruded round bar was cut to a length of 100 mm in the longitudinal direction, and subjected to upset forging with a working ratio of 80%. After the forged product was subjected to solution treatment at 520°C for 2 hours, it was immediately quenched with warm water at 50°C. Then artificial aging treatment was carried out at 180° C. for 10 hours to obtain T6 tempering.
在此,镦锻的加工率是图1中用(r1-r2)/r1×100进行计算而得到的值。Here, the machining rate of upset is a value calculated by (r1-r2)/r1×100 in FIG. 1 .
对这样得到的上述试验合金锻造品进行拉伸试验、镦锻后的外观观察、以及磨损试验。将其结果示于表3。Tensile tests, appearance observations after upset forging, and wear tests were performed on the above-mentioned test alloy forged products thus obtained. The results are shown in Table 3.
(1)镦锻后的外观(1) Appearance after forging
观察80%镦锻后的外观,将没有观察到裂纹的情况设为合格(=标记为“○”),将观察到裂纹的情况设为不合格(=标记为“×”)。The appearance after 80% upset was observed, and when no cracks were observed, it was judged to be acceptable (=marked with “◯”), and when cracks were observed, it was judged to be unacceptable (=marked with “×”).
(2)拉伸试验(2) Tensile test
拉伸试验片以挤出棒的长度方向为试验片的长度方向的方式采集,制作JIS4号试验片,进行试验。作为评价,将拉伸强度(TS)为300MPa以上设为合格,将低于该值设为不合格。The tensile test pieces were collected so that the longitudinal direction of the extruded rod was the longitudinal direction of the test piece, and JIS No. 4 test pieces were prepared and tested. As an evaluation, a tensile strength (TS) of 300 MPa or more was regarded as acceptable, and a value lower than this value was regarded as unacceptable.
(3)磨损试验(3) Wear test
通过大越式磨损试验来评价比磨损量。在此,作为试验条件,润滑油为齿轮油(75W-90),使对象材料为SCM415,使摩擦距离为1200m,使载荷为19kgf。作为摩擦试验的评价,将比磨损量为5.0×10-9以下设为合格,将超过该值设为不合格。The specific wear amount was evaluated by a Ohkoshi wear test. Here, as test conditions, the lubricating oil is gear oil (75W-90), the object material is SCM415, the friction distance is 1200m, and the load is 19kgf. As an evaluation of the friction test, a specific wear amount of 5.0×10 -9 or less was regarded as acceptable, and a value exceeding this value was regarded as unacceptable.
【表1】【Table 1】
【表2】【Table 2】
【表3】【table 3】
根据表1以及表2,本发明例的挤出材料1~10的表面性状好,比较例11~17的挤出材料的表面性状不良。According to Table 1 and Table 2, the surface properties of the extruded materials 1 to 10 of the examples of the present invention are good, and the surface properties of the extruded materials of Comparative Examples 11 to 17 are poor.
本发明例1~10由于组成在优选的范围内,因此,表面性状好。即,表面光滑,因此挤出性良好、能够以高生产率进行制造。In Examples 1 to 10 of the present invention, since the compositions were within the preferable range, the surface properties were good. That is, since the surface is smooth, extrudability is good, and it can manufacture with high productivity.
比较例11~14、16以及17的挤出材料由于组成在优选的范围外,因此这些挤出材料就表面性状而言存在刮到的情况,挤出加工性差。Since the extruded materials of Comparative Examples 11 to 14, 16 and 17 had compositions outside the preferred range, these extruded materials may be scratched in terms of surface properties, and extrusion processability was poor.
比较例11的挤出材料的Si的含量多,另外,Sc-Ss的值大。因此该挤出材料就表面性状而言存在刮到的情况,挤出加工性差。The extruded material of Comparative Example 11 had a large Si content and a large value of Sc—Ss. Therefore, the extruded material may be scratched in terms of surface properties, and extrusion processability is poor.
比较例12的挤出材料的Si的含量少,另外,Sc-Ss的值大。因此该挤出材料就表面性状而言存在刮到的情况,挤出加工性差。The extruded material of Comparative Example 12 had a small Si content and a large value of Sc—Ss. Therefore, the extruded material may be scratched in terms of surface properties, and extrusion processability is poor.
比较例13的挤出材料的Si以及Cu的含量少。因此该挤出材料就表面性状而言存在刮到的情况,挤出加工性差。The extruded material of Comparative Example 13 contained little Si and Cu. Therefore, the extruded material may be scratched in terms of surface properties, and extrusion processability is poor.
比较例14的挤出材料的Si、Cu、Mg、以及Cr的含量多。因此该挤出材料就表面性状而言存在刮到的情况,挤出加工性差。The extruded material of Comparative Example 14 contained many Si, Cu, Mg, and Cr contents. Therefore, the extruded material may be scratched in terms of surface properties, and extrusion processability is poor.
比较例16的挤出材料的Sr在优选范围外,共晶Si尺寸为20μm2以下的数目多。因此该挤出材料就表面性状而言存在刮到的情况,挤出加工性差。In the extruded material of Comparative Example 16, Sr was out of the preferred range, and the number of eutectic Si with a size of 20 μm 2 or less was large. Therefore, the extruded material may be scratched in terms of surface properties, and extrusion processability is poor.
比较例17的挤出材料在组成中Si的含量多,Mg的含量少,另外,Sc-Ss的值大。因此该挤出材料就表面性状而言存在刮到的情况,挤出加工性差。The extruded material of Comparative Example 17 had a composition with a large Si content, a small Mg content, and a large value of Sc—Ss. Therefore, the extruded material may be scratched in terms of surface properties, and extrusion processability is poor.
比较例15的挤出材料的组成在范围内,但Sc-Ss的值大,因此该挤出材料就表面性状而言存在刮到的情况,挤出加工性差。The composition of the extruded material of Comparative Example 15 was within the range, but the value of Sc-Ss was large, so the extruded material may be scratched in terms of surface properties, and the extrusion processability was poor.
根据表3,本发明例1~10的镦锻后的外观、拉伸强度、比磨损量全部良好,比较例11~17不良。According to Table 3, the appearance after upset forging, tensile strength, and specific wear amount of Examples 1 to 10 of the present invention are all good, while Comparative Examples 11 to 17 are not good.
本发明例1~10的锻造材料的拉伸强度、比磨损量好。另外,锻造加工性优良,因此,镦锻后的外观好。The forged materials of Examples 1 to 10 of the present invention were superior in tensile strength and specific wear. In addition, forging workability is excellent, so the appearance after upset forging is good.
比较例11的锻造材料在组成中Si的含量多,因此,在镦锻后的外观上观察到裂纹。即,锻造加工性差,作为锻造材料不良。The forged material of Comparative Example 11 had a large Si content in the composition, so cracks were observed in the appearance after upset forging. That is, the forging workability is poor, and it is not good as a forging material.
比较例12的锻造材料在组成中Si的含量少,因此,拉伸强度变差,耐磨损性变差。另外,根据表2,挤出材料的共晶Si尺寸为20μm2以下的数目少,因此,耐磨损性变差。In the forged material of Comparative Example 12, the Si content in the composition was small, so the tensile strength deteriorated and the wear resistance deteriorated. Also, according to Table 2, the number of extruded materials having a eutectic Si size of 20 μm 2 or less was small, and thus the abrasion resistance deteriorated.
比较例13的锻造材料在组成中Si以及Cu的含量少,因此,拉伸强度变差,耐磨损性变差。比较例14的锻造材料在组成中Si、Cu、Mg、以及Cr的含量多,因此,在镦锻后的外观上观察到裂纹。即,锻造加工性差,作为锻造材料不良。In the forged material of Comparative Example 13, the content of Si and Cu in the composition was small, so the tensile strength deteriorated and the wear resistance deteriorated. The forged material of Comparative Example 14 contained many Si, Cu, Mg, and Cr contents in the composition, so cracks were observed in the appearance after upset forging. That is, the forging workability is poor, and it is not good as a forging material.
比较例15的锻造材料的组成在范围内,镦锻后的外观、拉伸强度、比磨损量全部良好,但根据表2,比较例15的挤出材料的挤出加工性差,生产率不好。因此,比较例15的锻造材料的生产率差。The composition of the forged material of Comparative Example 15 was within the range, and the appearance after upset forging, tensile strength, and specific wear amount were all good. However, according to Table 2, the extrusion processability of the extruded material of Comparative Example 15 was poor, and the productivity was not good. Therefore, the productivity of the forged material of Comparative Example 15 was poor.
比较例16的锻造材料在组成中Si、Cu以及Sr的含量多,另外,根据表2,挤出材料的共晶Si尺寸为20μm2以下的数目多,因此,在镦锻后的外观上观察到裂纹。即,锻造加工性差,作为锻造材料不良。The forged material of Comparative Example 16 has a large content of Si, Cu, and Sr in the composition. In addition, according to Table 2 , there are many extruded materials whose eutectic Si size is 20 μm or less. to the crack. That is, the forging workability is poor, and it is not good as a forging material.
比较例17的锻造材料在组成中Si的含量多,Mg的含量少,因此,在镦锻后的外观上观察到裂纹。即,锻造加工性差,作为锻造材料不良。The forged material of Comparative Example 17 has a composition with a large Si content and a small Mg content, so cracks were observed in the appearance after upset forging. That is, the forging workability is poor, and it is not good as a forging material.
【符号的说明】【Description of symbols】
1 完成切割的挤出棒(锻造前)1 extruded rod finished cutting (before forging)
2 锻造机2 forging machine
r1 镦锻前的材料高度r1 material height before upset forging
r2 镦锻后的材料高度r2 material height after upset forging
3 旋转环3 swivel ring
4 评价材料(铝合金)4 Evaluation material (aluminum alloy)
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