WO2011062447A2 - 알루미늄 합금 및 이의 제조 방법 - Google Patents
알루미늄 합금 및 이의 제조 방법 Download PDFInfo
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- WO2011062447A2 WO2011062447A2 PCT/KR2010/008213 KR2010008213W WO2011062447A2 WO 2011062447 A2 WO2011062447 A2 WO 2011062447A2 KR 2010008213 W KR2010008213 W KR 2010008213W WO 2011062447 A2 WO2011062447 A2 WO 2011062447A2
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/02—Making non-ferrous alloys by melting
- C22C1/026—Alloys based on aluminium
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/02—Making non-ferrous alloys by melting
- C22C1/03—Making non-ferrous alloys by melting using master alloys
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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
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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
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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
- C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
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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
- C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
- C22C21/08—Alloys based on aluminium with magnesium as the next major constituent with silicon
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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
- C22C21/10—Alloys based on aluminium with zinc as the next major constituent
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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
- C22C21/12—Alloys based on aluminium with copper as the next major constituent
Definitions
- the present invention relates to an aluminum alloy and a method for producing the same.
- magnesium is one of the major alloying elements.
- the addition of magnesium increases the strength of aluminum alloys, favors surface treatment and improves corrosion resistance.
- oxides or inclusions are mixed into the aluminum molten metal by the magnesium having high chemically oxidizing property, thereby causing a problem of deteriorating molten metal quality.
- a method of applying a molten surface with a protective gas such as SF 6 may be used when magnesium is added.
- the present invention is to provide an aluminum alloy having excellent alloying properties and manufacturing method while being environmentally friendly.
- the present invention is to provide a processed product using such an aluminum alloy. This problem has been presented by way of example, and the scope of the present invention is not limited by this problem.
- the manufacturing method of the aluminum alloy of one embodiment of the present invention is provided. It provides a magnesium mother alloy and aluminum containing a calcium-based compound. A molten metal in which the magnesium mother alloy and the aluminum are dissolved is formed. The molten metal is cast.
- the magnesium mother alloy may be prepared by using pure magnesium or a magnesium alloy as a base material, and adding a calcium-based additive to the base material.
- the magnesium base alloy may be formed by dissolving a base metal to form a base metal melt and adding a calcium-based additive to the base metal melt.
- the magnesium master alloy may include forming by dissolving the base material and the calcium-based additive together.
- the magnesium mother alloy may further include stirring the base metal melt to exhaust at least a portion of the calcium-based additive.
- the calcium-based additive may be reduced in the magnesium molten metal
- the calcium-based compound is any one or more of the Mg-Ca compound, Al-Ca compound and Mg-Al-Ca compound It may include.
- it may further comprise the step of adding iron (Fe) to 1.0 wt% or less (greater than zero).
- the aluminum alloy of one embodiment of the present invention may be an aluminum alloy produced by any one or a combination of the above-described manufacturing methods.
- An aluminum alloy according to another aspect of the present invention includes an aluminum base and a calcium-based compound present in the aluminum base. Magnesium is dissolved in the aluminum base.
- the aluminum base has a plurality of regions forming a boundary and separated from each other, and at least a portion of the calcium-based compound may be present in the boundary or the region.
- the region may be grains and the boundary may be grain boundaries.
- the region may be an image region defined by different images, and the boundary may be an image boundary.
- the calcium-based compound may include any one or more of Mg-Ca compound, Al-Ca compound and Mg-Al-Ca compound.
- the Mg-Ca compound may include Mg 2 Ca
- the Al-Ca compound may include any one or more of Al 2 Ca and Al 4 Ca
- the Mg-Al-Ca compound is (Mg , Al) 2 Ca.
- iron (Fe) may be further included in 1.0 wt% or less (greater than zero).
- the average size of the grain or phase region in the aluminum matrix may exhibit a smaller value than the aluminum alloy which is manufactured under the same conditions and does not have the calcium-based compound.
- the tensile strength of the aluminum alloy may exhibit a larger value than the aluminum alloy without the calcium-based compound, furthermore the greater tensile It can have a greater or equivalent level of elongation with strength.
- the manufacturing method of the aluminum alloy according to the embodiments of the present invention in the process of adding magnesium in the aluminum molten metal stably even if the amount of protective gas, such as SF 6 used conventionally or not significantly reduced Aluminum casting process can be performed. Therefore, while being able to easily increase the content of magnesium added in the aluminum can have advantages in terms of environmental and cost.
- protective gas such as SF 6 used conventionally or not significantly reduced Aluminum casting process
- the aluminum alloy cast therefrom due to the improvement of the quality of the molten aluminum can significantly reduce the content of impurities as compared to the prior art can exhibit better mechanical properties.
- the aluminum alloy prepared by the manufacturing method according to the embodiments of the present invention as the calcium-based compound added with the addition of the magnesium mother alloy is dispersed in the matrix, causing a dispersion strengthening effect and grain refinement effect, such as mechanical mechanical of the aluminum alloy Properties can be significantly improved.
- magnesium content can be increased in the aluminum alloy, even when the iron content is decreased, sintering occurring during die casting of aluminum can be prevented, and corrosion resistance and elongation deterioration due to iron can be prevented.
- FIG. 1 is a flow chart showing an embodiment of a method for producing a magnesium mother alloy added to the molten aluminum in the manufacture of an aluminum alloy according to the present invention.
- Figure 3 is a flow chart showing an embodiment of the aluminum alloy manufacturing method according to the present invention.
- Figure 4 is a result of observing the molten surface of the aluminum alloy (a) and the aluminum alloy (b) with the addition of the mother alloy prepared by adding calcium oxide (CaO) in accordance with an embodiment of the present invention .
- Figure 7 shows the results of observing the structure of the aluminum alloy to which the magnesium mother alloy to which calcium oxide (CaO) is added in accordance with an embodiment of the present invention in EPMA (a), and aluminum, calcium as a component mapping result using EPMA , Mapping results of magnesium and oxygen ((b) to (e)) are shown.
- FIG. 9 is a schematic diagram illustrating a process of decomposing calcium oxide in the upper layer of the magnesium molten metal when calcium oxide is added to the molten magnesium.
- an aluminum alloy is prepared by preparing a mother alloy to which a predetermined additive is added and then adding the mother alloy to aluminum.
- the mother alloy may be used as a base material pure magnesium or magnesium alloy, all of which is referred to as magnesium mother alloy.
- pure magnesium is defined as a practical meaning that contains no intentionally added alloying elements, and includes impurities that are inevitably added during the manufacture of magnesium.
- a magnesium alloy is an alloy prepared by intentionally adding another alloy element to magnesium, for example, the alloy element may include aluminum.
- Magnesium alloys containing aluminum as alloying elements may also be referred to as magnesium-aluminum alloys.
- the magnesium-aluminum alloy may include not only aluminum as an alloy element but also other alloy elements other than aluminum.
- FIG. 1 is a flowchart showing a method of manufacturing a magnesium mother alloy in the method of manufacturing an aluminum alloy according to an embodiment of the present invention.
- Pure magnesium or magnesium alloy may be used as the base material of the magnesium mother alloy.
- Calcium-based additives added to the base material include calcium-containing compounds such as calcium oxide (CaO), calcium cyanide (CaCN 2 ), calcium carbide (CaC 2 ), calcium hydroxide (Ca (OH) 2 ) and calcium carbonate (CaCO 3 It may include any one or more of).
- a method of preparing a magnesium master alloy may include a magnesium molten metal forming step (S1), an additive adding step (S2), a stirring and maintaining step (S3), a casting step (S4), and a cooling step (S5).
- S1 magnesium molten metal forming step
- S2 additive adding step
- S3 stirring and maintaining step
- S4 casting step
- S5 cooling step
- the magnesium may be placed in a crucible and the magnesium may be melted to form a molten magnesium.
- the crucible may be heated to 600 to 800 ° C. to melt magnesium. If the heating temperature is less than 600 ° C., the molten magnesium is hardly formed. If the heating temperature is more than 800 ° C., there is a risk that the magnesium molten metal is ignited.
- the calcium-based additive may be added to the molten metal of the base metal.
- the size of the calcium-based additive may be 0.1 to 500 ⁇ m. The size of these additives of less than 0.1 ⁇ m is difficult and expensive to make realistically. If the size of the additive exceeds 500 ⁇ m, such an additive may not react with the magnesium molten metal.
- the calcium-based additive may be added at 0.0001 to 30 parts by weight based on 100 parts by weight of the magnesium mother alloy. If the additive is less than 0.0001 parts by weight, the effect by the additive (hardness increase, oxidation decrease, ignition temperature increase and protective gas decrease) may be small. In addition, if the additive exceeds 30 parts by weight, the original magnesium properties may be weakened.
- the molten magnesium can be stirred or maintained for an appropriate time.
- the stirring or holding time may be in the range of 1 to 400 minutes. If the stirring and holding time is less than 1 minute, the additives are not sufficiently mixed in the magnesium molten metal, and if it exceeds 400 minutes, the stirring and holding time of the magnesium molten metal may be unnecessarily long.
- a small amount of additional protective gas may be selectively provided to prevent ignition of the molten magnesium.
- the protective gas conventional SF6, SO2, CO2, HFC-134a, Novec TM 612, inert gas and equivalents thereof, or a mixed gas thereof may be used.
- a protective gas is not necessarily required and may not be provided.
- the oxidation resistance of magnesium in the molten metal is increased to increase the ignition temperature, so that The amount can be significantly reduced or eliminated. Therefore, according to the magnesium master alloy manufacturing method, it is possible to reduce the environmental pollution by reducing or eliminating the use of a protective gas, such as SF 6 regulated.
- the calcium oxide in the upper portion of the molten magnesium in the stirring and holding step (S3) can be decomposed into oxygen and calcium.
- the decomposed oxygen is discharged out of the magnesium molten metal as gas (O 2 ) or floated on the magnesium molten metal as dross or sludge.
- the decomposed calcium reacts with other elements in the molten metal to form various compounds.
- the reaction environment can be created so that the calcium-based additive reacts on the surface of the molten metal rather than incorporated into the magnesium molten metal.
- the calcium-based additive added may remain on the surface of the molten metal for as long as possible and may be stirred on the upper layer of the magnesium molten metal in order to maintain the exposure to the atmosphere.
- Table 1 shows the results of measuring the residual amount of calcium oxide according to the stirring method when calcium oxide was added to the AM60B magnesium molten metal.
- the size of the added calcium oxide was 70 ⁇ m, and 5, 10, 15 wt% of calcium oxide was added.
- the upper layer stirring, internal stirring, and stirring of the molten magnesium were selected. From Table 1, when stirring the upper portion of magnesium, it can be seen that most of the added calcium oxide is reduced to calcium unlike the other cases.
- the agitation can be carried out at the upper layer within 20% of the total depth of the melt from the magnesium melt surface, preferably at about 10% of the total depth of the melt.
- stirring is performed at a depth of 20% or more, decomposition of the calcium-based additive on the surface becomes less likely to occur.
- the time for stirring may vary depending on the temperature of the molten metal and the state of the injected powder, and it is preferable to sufficiently stir until the added calcium-based additive is completely consumed in the molten metal. Exhaustion here means that the decomposition of the calcium-based additives is substantially completed.
- the decomposition of calcium-based additives in the molten magnesium and the calcium cone produced by such decomposition can further promote the reaction of forming various compounds in the magnesium molten metal.
- the magnesium molten metal is cast into a mold (S4), cooled, and the solidified mother alloy is separated from the mold (S5).
- the temperature of the mold in the casting step (S4) may have a temperature range of room temperature (for example, 25 °C) to 400 °C.
- the cooling step (S5) after the mold is cooled to room temperature, the mother alloy can be separated from the mold, but even when the mother alloy is completely solidified before the room temperature, the mother alloy can be separated from the mold.
- the mold may use any one selected from a mold, a ceramic mold, a graphite mold, and an equivalent thereof.
- the casting method may include sand casting, die casting, gravity casting, continuous casting, low pressure casting, squeeze casting, lost wax casting, thixo casting, and the like. .
- Gravity casting may refer to a method of injecting a molten alloy into the mold using gravity
- low pressure casting may refer to a method of injecting molten metal into the mold by applying pressure to the molten surface of the molten alloy using gas.
- Thixocasting is a casting technique in a semi-melt state that combines the advantages of conventional casting and forging.
- the present invention does not limit the type of mold and the manner of casting.
- the magnesium master alloy thus prepared may have a base having a plurality of regions that form a boundary and are separated from each other.
- the plurality of regions separated from each other may be a plurality of grains typically divided into grain boundaries, and as another example, the plurality of regions may be a plurality of phase regions defined by two or more different phase boundaries.
- the base of the magnesium mother alloy may be present by dispersing the calcium-based compound produced in the mother alloy manufacturing process.
- the calcium-based compound may be produced by reacting the calcium-based additive added in the base metal melt in the additive addition step S2 with other elements in the magnesium base metal, for example, magnesium and / or aluminum.
- the calcium-based additive is reduced to calcium in the process of adding and stirring the calcium-based additive to the magnesium molten metal.
- the calcium-based additives are thermodynamically more stable than magnesium, it is expected that the calcium-based additives will not be separated from the molten magnesium.
- experiments by the inventors have shown that such calcium-based additives are reduced in the molten magnesium.
- the reduced calcium can then react with other elements in the matrix, for example magnesium and / or aluminum, to form calcium-based compounds.
- the calcium-based additive is a source of calcium used to form the calcium-based compound formed in the magnesium mother alloy and is an additive element added to the base metal molten metal during the production of the mother alloy, and the calcium-based compound is supplied from the calcium-based additive.
- Calcium is a newly produced compound by reacting with other elements in the base metal.
- Calcium has a certain degree of solubility for magnesium, but it has been found that only some of the calcium reduced from the calcium-based additives in the molten magnesium, as in the present invention, is partially dissolved in the magnesium base and most of them form calcium-based compounds.
- the calcium-based compound that can be produced may be an Mg-Ca compound, for example, Mg 2 Ca.
- the base material of the magnesium master alloy is a magnesium alloy, for example, a magnesium-aluminum alloy
- the calcium compound that can be produced may include any one or more of an Mg-Ca compound, an Al-Ca compound, and an Mg-Al-Ca compound.
- the Mg-Ca compound may be Mg 2 Ca
- the Al-Ca compound may include any one or more of Al 2 Ca and Al 4 Ca
- the Mg-Al-Ca compound may be (Mg, Al) 2 Ca.
- Calcium-based compounds have a high probability of being distributed in grain boundaries, which are boundaries between grains, or in boundary boundaries, which are boundaries between phase regions.
- This boundary portion is an open structure compared to the inside of the grain or phase region, and has a relatively high energy, which can provide a favorable position for nucleation and growth of calcium-based compounds.
- EMA Electron Probe Micro Analyzer
- (a) shows the microstructure of the magnesium master alloy observed using back scattering electrons.
- the magnesium master alloy exhibits a region surrounded by a compound (white portion), that is, a polycrystalline microstructure. At this time, the compound (white part) is formed along the grain boundary.
- (B) to (d) of FIG. 2 are results of mapping the components of the compound (white portion) region to EPMA, showing the distribution regions of aluminum, calcium and oxygen, respectively. As shown in (b) and (c) of FIG. 2, aluminum and calcium were detected in the compound, respectively, but oxygen was not detected as shown in (d).
- the Al-Ca compound produced by the reaction of calcium separated from calcium oxide (CaO) with aluminum contained in the base material is distributed in the grain boundary of the magnesium mother alloy.
- the Al-Ca compound may be Al 2 Ca or Al 4 Ca, which is an intermetallic compound.
- the above EPMA results show that Al-Ca compounds are mainly distributed in the grain boundaries of the magnesium mother alloy, which is more likely to be distributed in the grain boundaries than in the grains due to the nature of the grain boundaries having an open structure as grain boundaries. It is interpreted because.
- the results of the analysis are not limited to the present invention, because all the calcium-based compounds are distributed only in the grain boundaries, and in some cases, such calcium-based compounds may be found inside the grains.
- the magnesium master alloy thus prepared may be used for the purpose of being added to an aluminum alloy.
- calcium supplied from the calcium-based additive added during the alloying process includes a calcium-based compound formed by reaction with magnesium and / or aluminum.
- These calcium-based compounds are all intermetallic compounds and have a melting point higher than that of aluminum (658 ° C.).
- the melting point of Al 2 Ca or Al 4 Ca, which is an Al—Ca compound is 1079 ° C. and 700 ° C., respectively, which is higher than that of aluminum.
- the calcium-based compound when the mother alloy containing such a calcium-based compound is added to the aluminum molten metal, the calcium-based compound can be maintained without melting in the molten metal, when casting the molten metal to produce an aluminum alloy, the calcium in the aluminum alloy System compounds may be included.
- Such a manufacturing method may include providing a magnesium mother alloy and aluminum containing a calcium-based compound, forming a molten magnesium alloy and an aluminum melt, and casting the molten metal.
- a molten magnesium alloy and a molten aluminum it can be formed by first dissolving aluminum to form an aluminum molten metal, and then adding and dissolving a magnesium mother alloy containing a calcium-based compound in the aluminum molten metal.
- the molten aluminum may be formed by mounting aluminum and magnesium master alloy together in a melting apparatus such as a crucible and then heating and dissolving them together.
- FIG. 3 is a flowchart of a method of manufacturing an aluminum alloy using a method of first forming an aluminum molten metal as an embodiment of a method of manufacturing an aluminum alloy according to the present invention, and then adding and dissolving the magnesium mother alloy prepared by the method described above. .
- the method for producing an aluminum alloy includes an aluminum molten metal forming step (S11), a magnesium mother alloy addition step (S12), a stirring and holding step (S13), a casting step (S14), and a cooling step (S15). It may include.
- the aluminum is placed in a crucible and heated in a range of 600 to 900 ° C. to form aluminum molten metal.
- aluminum may be any one selected from pure aluminum, an aluminum alloy, and an equivalent thereof.
- the aluminum alloy is, for example, 1000 series, 2000 series, 3000 series, 4000 series, 5000 series, 6000 series, 7000 series and 8000 series Wrought aluminum or 100 series, 200 series, 300 series, 400 series It may be any one selected from among 500 series, 700 series casting aluminum.
- Aluminum alloys have been developed in various types according to their use, and the types of aluminum alloys are classified according to the standards of the Aluminum Association of America in almost every country today.
- Table 2 shows the composition of the main alloying elements by the alloy series in thousand units, and adds another improvement element to each alloy series to further subdivide the four-digit number and attach the alloy name.
- the first number indicates the alloy series representing the main alloying elements as above, the second number indicates the base alloy as 0, the modified alloy as 1 ⁇ 9, and the newly developed new alloy is labeled with N.
- 2xxx is a base alloy of Al-Cu series aluminum
- 21xx ⁇ 29xx is an improved alloy of Al-Cu series base alloy
- 2Nxx is a new alloy developed outside the association standard.
- the third and fourth numbers indicate the purity of aluminum in the case of pure aluminum, and the alloy name of the Alcoa company used in the past for alloys.
- 1080 represents at least 99.80% Al and 1100 represents 99.00% Al.
- the main configuration of this aluminum alloy is shown in Table 3 below.
- the magnesium master alloy addition step (S12) the magnesium master alloy prepared by the method described above is added to the aluminum molten metal.
- the magnesium mother alloy used in the magnesium mother alloy addition step (S12) may be added 0.0001 to 30 parts by weight based on 100 parts by weight of aluminum. If the added magnesium master alloy is less than 0.0001 parts by weight, the effect of the addition of the magnesium master alloy (hardness, corrosion resistance, weldability) may be small. In addition, when the magnesium master alloy exceeds 30 parts by weight, the original aluminum alloy may be weakened or not shown.
- the magnesium master alloy may be added in bulk form.
- the magnesium master alloy may be added in various forms such as powder form and granule form.
- the size of the magnesium master alloy may be appropriately selected depending on the dissolution conditions and does not limit the scope of this embodiment.
- the calcium compound contained in the magnesium master alloy is also provided in the molten aluminum.
- the calcium-based compound provided into the molten aluminum may include any one or more of an Mg-Ca compound, an Al-Ca compound, and an Mg-Al-Ca compound.
- a small amount of protective gas may be additionally provided to prevent oxidation of the magnesium mother alloy.
- the protective gas may use conventional SF6, SO2, CO2, HFC-134a, Novec TM 612, inert gas and equivalents thereof, or a mixed gas thereof, thereby inhibiting oxidation of the magnesium master alloy.
- such a protective gas is not necessarily required and may not be provided. That is, in the case of adding a magnesium mother alloy containing a calcium-based compound as in the embodiment of the present invention, the resistance to ignition is increased by increasing the oxidation resistance of the magnesium mother alloy, and magnesium that does not contain a conventional calcium-based compound is added. Compared with the case of addition, the presence of impurities such as oxides in the molten metal is significantly reduced. Therefore, according to the aluminum alloy production method of the present invention, the cleanliness of the aluminum molten metal is greatly improved even without using a protective gas can significantly improve the quality of the molten metal.
- the aluminum molten metal can be stirred or maintained.
- the molten aluminum can be stirred or maintained for 1 to 400 minutes. If the stirring and holding time is less than 1 minute, the magnesium mother alloy is not sufficiently mixed with the aluminum molten metal. If the stirring and holding time is more than 400 minutes, the stirring and holding time of the aluminum molten metal may be unnecessarily long.
- the molten aluminum is put into a mold and cast (S14), cooled, and then the solidified aluminum alloy is separated from the mold (S15).
- the temperature of the mold in the casting step (S14) may have a temperature range of room temperature (for example, 25 °C) to 400 °C.
- the cooling step (S15) after the mold is cooled to room temperature, the aluminum alloy may be separated from the mold, but even when the aluminum alloy is solidified even before the room temperature, the aluminum alloy may be separated from the mold. Since the casting method has been described in detail with respect to the magnesium mother alloy production method will be omitted.
- the aluminum alloys produced are 1000 series, 2000 series, 3000 series, 4000 series, 5000 series, 6000 series, 7000 series and 8000 series wrought aluminum or 100 series, 200 series, 300 series, 400 series, 500 It can be any one selected from the series, 700 series casting aluminum.
- the mechanical properties of the cast aluminum alloy are remarkably improved due to the improvement in cleanliness of the molten aluminum. That is, due to the improvement of the cleanliness of the molten metal, there is no impurities such as oxides or inclusions in the aluminum alloy cast therefrom that deteriorate the mechanical properties, and bubbles in the cast aluminum alloy are also significantly reduced.
- the inside of the cast aluminum alloy has a cleaner state than the conventional one, the aluminum alloy according to the present invention not only has excellent yield strength and tensile strength as compared with the conventional one, but also has very good mechanical properties such that the elongation is further improved. Have.
- the loss in the molten magnesium of aluminum added to the aluminum is reduced, and even if a smaller amount of magnesium is added, it is possible to manufacture substantially the same amount of magnesium contained in the aluminum alloy, which is economical aluminum.
- the alloy can be manufactured.
- the magnesium mother alloy according to the present invention when added to the molten aluminum, the magnesium instability in the molten aluminum is significantly improved compared to the conventional, it is possible to easily increase the content of magnesium compared to the conventional.
- Magnesium can be dissolved in aluminum up to 15% by weight and can improve the mechanical properties of aluminum alloys when dissolved. For example, adding magnesium to a 300 series or 6000 series aluminum alloy may improve the strength and elongation of the aluminum alloy.
- oxides and inclusions caused by magnesium may be mixed in the molten metal and degrade the quality of the aluminum alloy. This problem is exacerbated as the amount of magnesium added increases. Even if it is difficult to stably increase the content of magnesium added to the aluminum molten metal.
- the magnesium mother alloy can be stably added to the molten aluminum in accordance with the present invention, it is possible to easily increase the content of magnesium in the aluminum alloy as compared with the conventional art and to secure castability while increasing the proportion of magnesium. Therefore, by adding the magnesium master alloy according to the present invention to the 300 series or 6000 series aluminum alloy, it is possible to suppress the incorporation of oxides or inclusions and to improve not only castability but also strength and elongation. Available 500 series or 5000 series aluminum alloys can be used.
- the aluminum alloy according to the present invention can easily increase the solid solution of magnesium to 0.1% by weight or more, as well as 5% by weight or more, even 6% by weight or even more than 10% by weight to 15%.
- the stability of magnesium in this aluminum alloy can also work advantageously in the waste recycling of the aluminum alloy.
- a process of reducing it to a required ratio hereinafter referred to as de-megging process
- de-megging process a process of reducing it to a required ratio
- the aluminum alloy prepared by using a magnesium mother alloy containing a calcium-based compound has a technical, environmental, and cost advantage because it is possible to maintain a magnesium ratio of 0.3% by weight or more.
- the aluminum alloy according to the present invention may further include a step of adding a small amount of iron (Fe) after, for example, the aluminum molten metal forming step (S11) or the master alloy addition step (S12).
- the amount of iron added at this time may have a smaller value than in the prior art. That is, in the case of casting, for example, die-casting an aluminum alloy, a problem arises that the mold is damaged due to the occurrence of sintering between the mold made of an iron-based metal and the aluminum casting material. 1.0 to 1.5 wt.% Of iron has been added to the aluminum alloy. However, the addition of iron may cause another problem that the corrosion resistance and elongation of the aluminum alloy is reduced.
- the aluminum alloy according to the present invention may have a high content of magnesium, and when a high content of magnesium is added, a significantly smaller proportion of iron is added to the mold, which has appeared in the related art. Sedimentation problems can be greatly improved. Therefore, it is possible to solve the problems of corrosion resistance and elongation reduction that are conventionally found in die cast aluminum alloy castings.
- the content of iron (Fe) added in the process of manufacturing the above-described aluminum alloy may be 1.0% by weight or less (greater than 0) relative to the aluminum alloy, more strictly 0.2% by weight or less (greater than 0). Accordingly, the base of the aluminum alloy may include iron in the corresponding composition range.
- the aluminum alloy prepared according to the manufacturing method of the present invention includes an aluminum base and a calcium-based compound present in the aluminum base, wherein magnesium may be dissolved in the aluminum base. Magnesium may be dissolved in the aluminum matrix of 0.1 to 15% by weight.
- the aluminum base may have a solid solution of less than or equal to the solid solution limit, for example, 500 ppm or less.
- the calcium reduced from the calcium-based additives added in the magnesium master alloy is mostly present as a calcium-based compound, and only a part of it is dissolved in the magnesium matrix.
- the magnesium master alloy is added to the molten aluminum, as the dissolved calcium in the magnesium master alloy is diluted, the amount of calcium dissolved in the base of the actual aluminum alloy also has a small value below the solid solution limit.
- the aluminum alloy according to the present invention has a structure in which the calcium base compound is separately formed on the aluminum base while the calcium base is dissolved in the aluminum base at or below the solid solution limit, for example, 500 ppm or less.
- the aluminum base may have a plurality of regions that form a boundary and are separated from each other.
- the calcium-based compound may exist within the boundary or region.
- An aluminum base may be defined as referring to a metallic structure in which aluminum is the main component, and in which other alloying elements are dissolved or in which other compounds other than calcium-based compounds are formed as separate phases.
- the plurality of regions separated from each other may be a plurality of grains typically divided into grain boundaries, and as another example, the plurality of regions may be a plurality of phase regions defined by two or more different phase boundaries.
- the aluminum alloy according to the present invention may have an effect of improving the mechanical properties resulting from the calcium-based compound formed in the magnesium mother alloy.
- the calcium compound contained in the magnesium master alloy is also added to the molten metal.
- the calcium compound is an intermetallic compound formed by the reaction between calcium and other metal elements. All have a melting point higher than that of aluminum.
- the calcium-based compound when the mother alloy containing such a calcium-based compound is added to the aluminum molten metal, the calcium-based compound can be maintained without melting in the molten metal, and when casting the molten metal to produce an aluminum alloy, the calcium in the aluminum alloy System compounds may be included.
- Such a calcium-based compound may be dispersed and distributed in the fine particle side in the aluminum alloy.
- the calcium-based compound is a high-strength material compared to aluminum known as an intermetallic compound, and therefore, the strength of the aluminum alloy may be increased due to the dispersion distribution of the high-strength material.
- the calcium-based compound may provide a place where nucleation occurs in the process of the aluminum alloy is phased from the liquid phase to the solid phase.
- the transition from the liquid phase to the solid phase during the solidification of the aluminum alloy is in the form of nucleation and growth, and at this time, the calcium-based compound and the liquid phase as the calcium-based compound itself functions as a heterogeneous nucleation site.
- nucleation occurs preferentially for transition to the solid phase.
- the nucleated solid phase grows while forming around the calcium compound.
- the calcium-based compound When the calcium-based compound is distributed in a plurality, the solid phases grown at the interface of each calcium-based compound meet each other to form a boundary, and the boundary thus formed may form a grain boundary or an boundary boundary. Therefore, when the calcium-based compound functions as a nucleation site, the calcium-based compound is present inside the grains or the phase region, and the grains or the phase region may have a smaller effect than the case where the calcium-based compound does not exist. Will be.
- the calcium-based compound may be distributed in a grain boundary which is a boundary between grains or an upper boundary which is a boundary between phase regions.
- This boundary portion is an open structure compared to the inside of the grain or phase region, and has a relatively high energy, which can provide a favorable position for nucleation and growth of calcium-based compounds.
- the calcium-based compound When the calcium-based compound is distributed in the grain boundary or the boundary of the aluminum alloy, the calcium-based compound acts as an obstacle of grain boundary or the boundary boundary, and the movement of the grain boundary or the boundary boundary is suppressed to reduce the average size of the grain or the boundary boundary. have.
- such a calcium-based compound may have a finer and smaller grain or phase region size on average.
- the refinement of the grain or phase region due to such a calcium-based compound can bring about an effect of improving the strength and elongation of the aluminum alloy.
- Aluminum bases are also available in 1000 series, 2000 series, 3000 series, 4000 series, 5000 series, 6000 series, 7000 series and 8000 series plastic processing (Wrought) aluminum or 100 series, 200 series, 300 series, 400 series, 500 series, 700 It may be any one selected from the series casting aluminum.
- the total amount of calcium in the aluminum alloy according to the present invention may be present in an amount of 0.0001 to 10 parts by weight based on 100 parts by weight of aluminum.
- the total amount of calcium is the sum of the calcium present in the aluminum base and the calcium-based compound dissolved in the aluminum base.
- the magnesium mother alloy prepared by adding the calcium-based additive as described above most of the calcium reduced from the calcium-based additive forms a calcium-based compound without being dissolved in the magnesium matrix. Therefore, when the magnesium master alloy is added to produce aluminum, the amount of calcium dissolved in the magnesium master alloy shows a small value, so that the amount of calcium employed in the aluminum base through the magnesium master alloy is very low, for example, 500 ppm or less. Have.
- the aluminum matrix may have from 0.1 to 15% by weight of magnesium dissolved, further 5 to 15% or more, further 6 to 15% by weight and even more 10 to 15% by weight.
- the amount of magnesium added in the molten aluminum can be stably increased. Higher doses of magnesium also increase. This increase in magnesium capacity can greatly contribute to the improvement of aluminum alloy strength due to solid solution strengthening and heat treatment, and exhibits excellent castability and excellent mechanical properties compared to conventional commercial alloys.
- Table 4 shows an aluminum alloy prepared by adding magnesium oxide (CaO) added to aluminum as a calcium-based additive (Experimental Example 1) and prepared by adding pure magnesium without adding a calcium-based additive to aluminum. This table compares the casting characteristics of an aluminum alloy (Comparative Example 1).
- Experimental Example 1 was prepared by adding 305 g of magnesium mother alloy to 2750 g of aluminum, and Comparative Example 1 was prepared by adding 305 g of pure magnesium to 2750 g of aluminum.
- the magnesium mother alloy used in Experimental Example 1 used a magnesium-aluminum alloy as a base material, and the weight ratio of calcium oxide (CaO) to the base material was 0.3.
- FIG. 5 is a result of comparing the casting surface of the aluminum alloy according to Experimental Example 1 and Comparative Example 1.
- the surface of the cast material of the aluminum alloy to which the magnesium master alloy of Experimental Example 1 (a) was added is cleaner than the cast material of the aluminum alloy to which pure magnesium was added in Comparative Example 1 (b). .
- the ignition phenomenon is suppressed and a clean surface can be obtained.
- FIG. 6 is an energy dispersive spectroscopy (EDS) analysis result of a scanning electron microscope (SEM) of aluminum alloys according to Experimental Example 1 and Comparative Example 1.
- EDS energy dispersive spectroscopy
- SEM scanning electron microscope
- Table 5 shows the mechanical properties of the aluminum alloys (Experimental Examples 2 and 3) prepared by adding a magnesium master alloy containing calcium oxide (CaO) to the commercially available aluminum alloys 7075 and 6061, respectively. It is a table compared with the comparative examples 2 and 3).
- the specimens according to Experimental Examples 2 and 3 were subjected to T6 heat treatment by extrusion after casting, and the data of Comparative Examples 2 and 3 refer to values in the ASM standard (T6 heat treatment data).
- the aluminum alloy according to the experimental example of the present invention exhibits higher values in tensile strength and yield strength, it can be seen that the elongation is superior or equivalent to that of the commercial aluminum alloy. In general, when the strength is increased in the alloy, the elongation is relatively decreased. However, the aluminum alloy according to the experimental example of the present invention exhibits the ideal characteristics in that the elongation is also increased along with the increase in strength. It was mentioned above that this result may be related to the improvement of the cleanliness of the molten aluminum alloy.
- Grain refinement in the aluminum alloy of Experimental Example 3 is determined by the growth of the grain boundary is suppressed by the calcium-based compound distributed in the grain boundary, or because the calcium-based compound functioned as nucleation sites during coagulation. It is judged that the aluminum alloy according to the embodiment of the present invention is one of the causes showing excellent mechanical properties.
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Abstract
Description
5wt%CaO 첨가 | 10wt%CaO 첨가 | 15wt%CaO 첨가 | ||
합금 내 CaO 잔량 | 교반하지 안음 | 4.5wt%CaO | 8.7wt%CaO | 13.5wt%CaO |
용탕 내부 교반 | 1.2wt%CaO | 3.1wt%CaO | 5.8wt%CaO | |
용탕 상층부 교반(본 발명) | 0.001wt%CaO | 0.002wt%CaO | 0.005wt%CaO |
합금 계열 | 주요 합금 성분 |
1000계열 알루미늄 | 순순하 알루미늄 |
2000계열 알루미늄 | Al-Cu-(Mg)계 알루미늄 합금 |
3000계열 알루미늄 | Al-Mn계 알루미늄 합금 |
4000계열 알루미늄 | Al-Si계 알루미늄 합금 |
5000계열 알루미늄 | Al-Mg계 알루미늄 합금 |
6000계열 알루미늄 | Al-Mg-Si계 알루미늄 합금 |
7000계열 알루미늄 | Al-Zn-Mg-(Cu)게 알루미늄 합금 |
8000계열 알루미늄 | 기타 |
등급 번호 | 첨가금속(원소기호),단위 % | 용도 | ||||||
Si | Cu | Mn | Mg | Cr | Zn | 기타 | ||
1100 | 0.12 | Si 1%, Fe 다량 | 금속박판, 주방용기 | |||||
1350 | 기타 0.5% 정도 | 전도물질 | ||||||
2008 | 0.7 | 0.9 | 0.4 | 자동차용 금속판 | ||||
2014 | 0.8 | 4.4 | 0.8 | 0.5 | 비행기 외부, 트럭프레임 | |||
2024 | 4.4 | 0.6 | 1.5 | 비행기 외부, 트럭 휠 | ||||
2036 | 2.6 | 0.25 | 0.45 | 자동차용 금속판 | ||||
2090 | 2.7 | Li 2.2, Zr 0.12 | 비행기 금속 | |||||
2091 | 2.2 | 1.5 | Li 2.0, Zr 0.12 | 비행기 금속 | ||||
2219 | 6.3 | 0.3 | V 0.1,Zr 0.18, Ti 0.06 | 우주선용 금속, 용접가능 | ||||
2519 | 5.9 | 0.3 | 0.2 | V 0.1, Zr 0.18 | 군사장비, 우주선용 금속, 용접가능 | |||
3003 | 0.12 | 1.1 | 일반적 용도, 주방용기 | |||||
3004 | 1.1 | 1.0 | 일반적 용도, 금속캔 | |||||
3105 | 0.6 | 0.5 | 건축자재 | |||||
5052 | 2.5 | 0.25 | 일반적 용도 | |||||
5083 | 0.7 | 4.4 | 0.15 | 내열/내압용기 | ||||
5182 | 0.35 | 4.5 | 금속캔, 자동차용 금속 | |||||
5252 | 2.5 | 차체 외장용 | ||||||
6009 | 0.8 | 0.33 | 0.33 | 0.5 | 자동차용 금속판 | |||
6010 | 1.0 | 0.33 | 0.33 | 0.8 | 자동차용 금속판 | |||
6013 | 0.8 | 0.8 | 0.5 | 1.0 | 우주선용 금속 | |||
6061 | 0.6 | 0.25 | 1.0 | 0.20 | 일반적 목적 | |||
6063 | 0.4 | 0.7 | 일반적 목적, 사출형성 | |||||
6201 | 0.7 | 0.8 | 전도물질 | |||||
7005 | 0.45 | 1.4 | 0.13 | 4.5 | Zr 0.14 | 트럭차체, 열차 | ||
7075 | 1.6 | 2.5 | 0.25 | 5.6 | 비행기용 금속 | |||
7150 | 2.2 | 2.3 | 6.4 | Zr 0.12 | 우주선용 금속 | |||
8090 | 1.3 | 0.9 | Li 2.4, Zr 0.12 | 우주선용 금속 |
실험예1 | 비교예1 | |
Dross양(용탕표면에 뜨는 불순물) | 206g | 510g |
Al 합금 내의 Mg 함량 | 4.89% | 2.65% |
용탕 유동성 | 좋음 | 나쁨 |
경도(HR하중 60kg, 1/16"강구) | 92.6 | 92 |
인장강도 (MPa) | 항복강도(MPa) | 연신율(%) | |
실험예 2 | 670 | 600 | 12 |
비교예 2 | 572 | 503 | 11 |
실험예 3 | 370 | 330 | 17 |
비교예 3 | 310 | 276 | 17 |
Claims (40)
- 칼슘계 화합물을 포함하는 마그네슘 모합금 및 알루미늄을 제공하는 단계;상기 마그네슘 모합금 및 상기 알루미늄이 용해된 용탕을 형성하는 단계; 및상기 용탕을 주조하는 단계;를 포함하는, 알루미늄 합금 제조방법.
- 제 1 항에 있어서, 상기 용탕을 형성하는 단계는상기 알루미늄을 용해하여 알루미늄 용탕을 형성하는 단계; 및상기 알루미늄 용탕에 상기 마그네슘 모합금을 첨가하여 용해하는 단계;를 포함하는, 알루미늄 합금 제조방법.
- 제 1 항에 있어서, 상기 용탕을 형성하는 단계는상기 마그네슘 모합금 및 상기 알루미늄을 장착하는 단계; 및상기 마그네슘 모합금 및 상기 알루미늄을 같이 용해하는 단계;를 포함하는, 알루미늄 합금 제조방법.
- 제 1 항 있어서, 상기 마그네슘 모합금은 상기 알루미늄 100 중량부에 대해서 0.0001 내지 30 중량부인, 알루미늄 합금 제조방법.
- 제 1 항에 있어서, 상기 마그네슘 모합금은 순수 마그네슘 또는 마그네슘 합금을 모재로 하고, 상기 모재에 칼슘계 첨가제를 첨가하여 제조한 것인, 알루미늄 합금 제조방법.
- 제 5 항에 있어서, 상기 마그네슘 합금은 알루미늄을 포함하는 것인, 알루미늄 합금 제조방법.
- 제 5 항에 있어서, 상기 마그네슘 모합금은상기 모재를 용해하여 모재 용탕을 형성하는 단계; 및상기 모재 용탕에 상기 칼슘계 첨가제를 첨가하는 단계;를 포함하여 형성하는, 알루미늄 합금 제조 방법.
- 제 5 항에 있어서, 상기 마그네슘 모합금은상기 모재 및 상기 칼슘계 첨가제를 같이 용해하는 단계를 포함하여 형성하는, 알루미늄 합금 제조 방법.
- 제 7 항에 있어서, 상기 마그네슘 모합금은 상기 칼슘계 첨가제의 적어도 일부를 소진시키기 위하여 상기 모재 용탕을 교반하는 단계를 더 포함하여 형성하는, 알루미늄 합금 제조 방법.
- 제 9 항에 있어서, 상기 교반하는 단계는 상기 칼슘계 첨가제가 실질적으로 잔류되지 않도록 상기 모재 용탕의 표면으로부터 용탕 전체 깊이의 20%이하의 상층부에서 수행하는, 알루미늄 합금 제조 방법.
- 제 6 항에 있어서, 상기 칼슘계 첨가제는 산화칼슘(CaO), 시안화칼슘(CaCN2), 탄화칼슘(CaC2), 수산화칼슘(Ca(OH)2) 및 탄산칼슘(CaCO3) 중 어느 하나 이상을 포함하는, 알루미늄 합금 제조방법.
- 제 11 항에 있어서, 상기 칼슘계 화합물은 상기 칼슘계 첨가제로부터 공급되는 칼슘과 상기 모재의 마그네슘 또는 알루미늄이 반응하여 생성된 것인, 알루미늄 합금 제조방법.
- 제 12 항에 있어서, 상기 칼슘계 화합물은 Mg-Ca 화합물, Al-Ca 화합물 및 Mg-Al-Ca 화합물 중 어느 하나 이상을 포함하는, 알루미늄 합금 제조방법.
- 제 13 항에 있어서, 상기 Mg-Ca 화합물은 Mg2Ca을 포함하는, 알루미늄 합금.
- 제 13 항에 있어서, 상기 Al-Ca 화합물은 Al2Ca 및 Al4Ca 중 어느 하나 이상을 포함하는, 알루미늄 합금 제조방법.
- 제 13 항에 있어서, 상기 Mg-Al-Ca 화합물은 (Mg,Al)2Ca을 포함하는, 알루미늄 합금 제조방법.
- 제 5 항에 있어서, 상기 칼슘계 첨가제는 상기 모재 100 중량부에 대해 0.0001 내지 30 중량부의 범위에서 첨가되는, 알루미늄 합금 제조방법.
- 제 1 항에 있어서, 상기 알루미늄은 순수 알루미늄 또는 알루미늄 합금인, 알루미늄 합금 제조방법.
- 제 1 항에 있어서, 철(Fe)을 1.0 중량% 이하(0% 초과)로 첨가하는 단계를 더 포함하는, 알루미늄 합금 제조방법.
- 제 19 항에 있어서, 상기 철(Fe)을 0.2 중량% 이하로 첨가하는, 알루미늄 합금 제조방법.
- 제 1 항 내지 20 항 중 어느 하나의 항에 따른 알루미늄 합금 제조방법에 의해 제조된 알루미늄 합금.
- 제 21 항에 있어서, 상기 알루미늄 합금은 1000 계열, 2000 계열, 3000 계열, 4000 계열, 5000 계열, 6000 계열, 7000계열 및 8000 계열 소성 가공용(Wrought) 알루미늄 또는 100 계열, 200 계열, 300계열, 400 계열, 500 계열 및 700 계열 주조용(Casting) 알루미늄 중에서 선택된 어느 하나를 포함하는, 알루미늄 합금.
- 알루미늄 기지; 및상기 알루미늄 기지에 존재하는 칼슘계 화합물;을 포함하고,상기 알루미늄 기지에는 마그네슘이 고용된, 알루미늄 합금.
- 제 23 항에 있어서, 상기 마그네슘은 상기 알루미늄 기지에 0.1 내지 15 중량% 고용된, 알루미늄 합금.
- 제 23 항에 있어서, 상기 알루미늄 기지는 칼슘이 고용한도 이하로 고용된, 알루미늄 합금.
- 제 25 항에 있어서, 상기 칼슘은 500 ppm 이하로 고용된, 알루미늄 합금.
- 제 23 항에 있어서, 상기 알루미늄 기지는 경계를 이루며 서로 구분되는 복수개의 영역을 가지며 상기 경계에는 상기 칼슘계 화합물이 존재하는, 알루미늄 합금.
- 제 23 항에 있어서, 상기 알루미늄 기지는 경계를 이루며 서로 구분되는 복수개의 영역을 가지며 상기 영역 내에 상기 칼슘계 화합물이 존재하는, 알루미늄 합금.
- 제 27 항 또는 제 28 항에 있어서, 상기 영역은 결정립이고, 상기 경계는 결정립계인, 알루미늄 합금.
- 제 27 항 또는 제 28 항에 있어서, 상기 영역은 서로 다른 상에 의해 한정되는 상영역이며, 상기 경계는 상경계인, 알루미늄 합금.
- 제 23 항에 있어서, 칼슘계 화합물은 Mg-Ca 화합물, Al-Ca 화합물 및 Mg-Al-Ca 화합물 중 어느 하나 이상을 포함하는, 알루미늄 합금.
- 제 31 항에 있어서, 상기 Mg-Ca 화합물은 Mg2Ca을 포함하는, 알루미늄 합금.
- 제 31 항에 있어서, 상기 Al-Ca 화합물은 Al2Ca 및 Al4Ca 중 어느 하나 이상을 포함하는, 알루미늄 합금.
- 제 31 항에 있어서, 상기 Mg-Al-Ca 화합물은 (Mg,Al)2Ca을 포함하는, 알루미늄 합금.
- 제 23 항에 있어서, 상기 알루미늄 기지는 1000 계열, 2000 계열, 3000 계열, 4000 계열, 5000 계열, 6000 계열, 7000계열 및 8000 계열 소성 가공용(Wrought) 알루미늄 또는 100 계열, 200 계열, 300계열, 400 계열, 500 계열 및 700 계열 주조용(Casting) 알루미늄 중에서 선택된 어느 하나를 포함하는, 알루미늄 합금.
- 제 23 항에 있어서, 철(Fe)을 1.0 중량% 이하(0% 초과)로 더 포함하는, 알루미늄 합금.
- 제 36 항에 있어서, 철(Fe)을 0.2 중량% 이하로 더 포함하는, 알루미늄 합금.
- 제 27 항 또는 제 28 항에 있어서, 상기 영역의 평균크기가, 동일조건으로 제조된 알루미늄 합금으로서 상기 칼슘계 화합물을 갖지 않는 알루미늄 합금에 비해 더 작은, 알루미늄 합금.
- 제 23 항에 있어서, 인장강도가 동일조건으로 제조된 알루미늄 합금으로서 상기 칼슘계 화합물을 갖지 않는 알루미늄 합금에 비해 더 큰, 알루미늄 합금.
- 제 23 항에 있어서, 동일조건으로 제조된 알루미늄 합금으로서 상기 칼슘계 화합물을 갖지 않는 알루미늄 합금에 비해 인장강도는 더 크고 연신율은 더 크거나 동등한, 알루미늄 합금.
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JP (2) | JP5639449B2 (ko) |
CN (1) | CN102071342B (ko) |
AU (1) | AU2010322540B2 (ko) |
CA (1) | CA2721752C (ko) |
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Families Citing this family (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA2721761C (en) * | 2009-11-20 | 2016-04-19 | Korea Institute Of Industrial Technology | Aluminum alloy and manufacturing method thereof |
CA2721752C (en) * | 2009-11-20 | 2015-01-06 | Korea Institute Of Industrial Technology | Aluminum alloy and manufacturing method thereof |
CA2794962C (en) * | 2010-03-29 | 2019-02-26 | Korea Institute Of Industrial Technology | Magnesium-based alloy with superior fluidity and hot-tearing resistance and manufacturing method thereof |
KR101388922B1 (ko) | 2010-07-28 | 2014-04-24 | 자동차부품연구원 | 철-망간 전율고용체를 포함하는 알루미늄 합금 및 그 제조방법 |
KR101273577B1 (ko) * | 2010-10-19 | 2013-06-11 | 한국생산기술연구원 | 알루미늄 합금 다이캐스팅재 및 그 제조방법 |
KR101402897B1 (ko) | 2011-05-20 | 2014-06-02 | 한국생산기술연구원 | 합금제조방법 및 이에 의해 제조된 합금 |
KR101434262B1 (ko) * | 2012-04-20 | 2014-08-28 | 한국생산기술연구원 | 알루미늄 합금 및 이의 제조 방법 |
KR101434263B1 (ko) * | 2012-04-20 | 2014-08-28 | 한국생산기술연구원 | 알루미늄 합금 및 이의 제조 방법 |
WO2013157903A1 (ko) * | 2012-04-20 | 2013-10-24 | 한국생산기술연구원 | 알루미늄 합금 및 이의 제조 방법 |
KR20140063959A (ko) | 2012-11-19 | 2014-05-28 | 한국생산기술연구원 | 아연합금 및 이의 제조방법 |
CN102978340A (zh) * | 2012-11-26 | 2013-03-20 | 张桂芬 | 一种炼钢脱氧剂及其制备方法 |
JP6283240B2 (ja) * | 2013-05-23 | 2018-02-21 | 株式会社神戸製鋼所 | アルミニウム合金板、接合体及び自動車用部材 |
US9643651B2 (en) | 2015-08-28 | 2017-05-09 | Honda Motor Co., Ltd. | Casting, hollow interconnecting member for connecting vehicular frame members, and vehicular frame assembly including hollow interconnecting member |
US11149332B2 (en) | 2017-04-15 | 2021-10-19 | The Boeing Company | Aluminum alloy with additions of magnesium and at least one of chromium, manganese and zirconium, and method of manufacturing the same |
US11098391B2 (en) | 2017-04-15 | 2021-08-24 | The Boeing Company | Aluminum alloy with additions of magnesium, calcium and at least one of chromium, manganese and zirconium, and method of manufacturing the same |
MX2019014060A (es) * | 2017-05-30 | 2020-02-05 | Obshchestvo S Ogranichennoy Otvetstvennostyu Obedinennaya Kompaniya Rusal Inzhenerno Tekh Tsentr | Aleacion de elevada resistencia a base de aluminio. |
KR101961468B1 (ko) * | 2017-09-29 | 2019-04-15 | (주)한국주조산업 | 알루미늄합금용 Al-Mg-Ca 모합금 및 그 제조방법 |
DE102018125521A1 (de) | 2018-10-15 | 2020-04-16 | Achenbach Buschhütten GmbH & Co. KG | Verfahren zur Herstellung eines hochfesten Aluminium-Legierungsblechs |
WO2020160682A1 (en) * | 2019-02-07 | 2020-08-13 | Equispheres Inc. | Alloys with a low density of precipitates for use in applications that include remelting processes, and preparation process thereof |
CN112662921B (zh) * | 2020-12-04 | 2022-03-25 | 成都慧腾创智信息科技有限公司 | 一种高强韧压铸铝硅合金及其制备方法 |
CN113564438A (zh) * | 2021-07-15 | 2021-10-29 | 烟台南山学院 | 一种经济型阻燃大变形铝合金材料及其制备方法 |
CN113667870B (zh) * | 2021-08-09 | 2022-03-25 | 江西理工大学 | 一种高应力腐蚀抗性铝铜锂合金材料 |
KR102585807B1 (ko) * | 2023-01-12 | 2023-10-06 | (주)코리아마그네슘 | 탄산칼슘의 분산원리, 그래핀 및 탄소나노튜브를 이용한 고강도 알루미늄 합금 |
KR102585806B1 (ko) * | 2023-01-12 | 2023-10-06 | (주)코리아마그네슘 | 탄산칼슘의 분산 원리를 이용한 Mg 고강도 경량 합금 |
KR102585810B1 (ko) * | 2023-04-18 | 2023-10-05 | 오재부 | 다이캐스팅용 고강도-저팽창 합금 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS53125918A (en) * | 1977-04-11 | 1978-11-02 | Nippon Keikinzoku Sougou Kenki | Aluminum alloy for casting |
JPH06145865A (ja) * | 1992-11-10 | 1994-05-27 | Nippon Light Metal Co Ltd | Ca系助剤を併用する初晶Siの微細化 |
JPH06306521A (ja) * | 1993-04-27 | 1994-11-01 | Nippon Light Metal Co Ltd | 鋳物用過共晶Al−Si系合金及び鋳造方法 |
US20050011591A1 (en) * | 2002-06-13 | 2005-01-20 | Murty Gollapudi S. | Metal matrix composites with intermettalic reinforcements |
KR100681539B1 (ko) * | 2005-02-25 | 2007-02-12 | 한국생산기술연구원 | 산화칼슘이 첨가된 마그네슘 합금 및 그의 제조방법 |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH502440A (de) | 1967-09-21 | 1971-01-31 | Metallgesellschaft Ag | Verfahren zur Herstellung von strontium- und/oder bariumhaltigen Vorlegierungen für die Veredelung von Aluminiumlegierungen |
GB1430758A (en) | 1972-08-23 | 1976-04-07 | Alcan Res & Dev | Aluminium alloys |
US4286984A (en) * | 1980-04-03 | 1981-09-01 | Luyckx Leon A | Compositions and methods of production of alloy for treatment of liquid metals |
US4929511A (en) * | 1983-12-06 | 1990-05-29 | Allied-Signal Inc. | Low temperature aluminum based brazing alloys |
US5074936A (en) * | 1989-04-05 | 1991-12-24 | The Dow Chemical Company | Amorphous magnesium/aluminum-based alloys |
FR2741359B1 (fr) | 1995-11-16 | 1998-01-16 | Gm Metal | Alliage-mere d'aluminium |
JPH11323456A (ja) * | 1998-05-08 | 1999-11-26 | Kobe Steel Ltd | アルミニウム合金鋳塊の製造方法 |
US6412164B1 (en) | 2000-10-10 | 2002-07-02 | Alcoa Inc. | Aluminum alloys having improved cast surface quality |
US8123877B2 (en) * | 2003-01-31 | 2012-02-28 | Kabushiki Kaisha Toyota Jidoshokki | Heat-resistant magnesium alloy for casting heat-resistant magnesium alloy cast product, and process for producing heat-resistant magnesium alloy cast product |
JP4415098B2 (ja) | 2005-03-16 | 2010-02-17 | 独立行政法人産業技術総合研究所 | 難燃性マグネシウム合金押出材の製造方法及びその押出材 |
JP2006322062A (ja) | 2005-04-19 | 2006-11-30 | Daiki Aluminium Industry Co Ltd | 鋳造用アルミニウム合金および同アルミニウム合金鋳物 |
JP4539572B2 (ja) * | 2006-01-27 | 2010-09-08 | 株式会社豊田中央研究所 | 鋳造用マグネシウム合金および鋳物 |
JP5321960B2 (ja) | 2009-01-06 | 2013-10-23 | 日本軽金属株式会社 | アルミニウム合金の製造方法 |
CA2721752C (en) * | 2009-11-20 | 2015-01-06 | Korea Institute Of Industrial Technology | Aluminum alloy and manufacturing method thereof |
CA2721761C (en) * | 2009-11-20 | 2016-04-19 | Korea Institute Of Industrial Technology | Aluminum alloy and manufacturing method thereof |
-
2010
- 2010-11-17 CA CA2721752A patent/CA2721752C/en active Active
- 2010-11-18 US US12/949,152 patent/US9200348B2/en active Active
- 2010-11-19 WO PCT/KR2010/008213 patent/WO2011062447A2/ko active Application Filing
- 2010-11-19 JP JP2010259038A patent/JP5639449B2/ja active Active
- 2010-11-19 AU AU2010322540A patent/AU2010322540B2/en active Active
- 2010-11-22 EP EP10251974.1A patent/EP2339037B1/en active Active
- 2010-11-22 CN CN2010106109480A patent/CN102071342B/zh active Active
- 2010-11-22 EP EP13179478.6A patent/EP2677049B1/en active Active
- 2010-11-22 PL PL13179478T patent/PL2677049T3/pl unknown
-
2012
- 2012-10-16 JP JP2012228604A patent/JP5879244B2/ja active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS53125918A (en) * | 1977-04-11 | 1978-11-02 | Nippon Keikinzoku Sougou Kenki | Aluminum alloy for casting |
JPH06145865A (ja) * | 1992-11-10 | 1994-05-27 | Nippon Light Metal Co Ltd | Ca系助剤を併用する初晶Siの微細化 |
JPH06306521A (ja) * | 1993-04-27 | 1994-11-01 | Nippon Light Metal Co Ltd | 鋳物用過共晶Al−Si系合金及び鋳造方法 |
US20050011591A1 (en) * | 2002-06-13 | 2005-01-20 | Murty Gollapudi S. | Metal matrix composites with intermettalic reinforcements |
KR100681539B1 (ko) * | 2005-02-25 | 2007-02-12 | 한국생산기술연구원 | 산화칼슘이 첨가된 마그네슘 합금 및 그의 제조방법 |
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AU2010322540B2 (en) | 2014-05-01 |
US9200348B2 (en) | 2015-12-01 |
JP2011104655A (ja) | 2011-06-02 |
CN102071342A (zh) | 2011-05-25 |
EP2339037B1 (en) | 2013-09-18 |
WO2011062447A3 (ko) | 2011-11-03 |
EP2677049A1 (en) | 2013-12-25 |
US20110123390A1 (en) | 2011-05-26 |
EP2339037A1 (en) | 2011-06-29 |
CA2721752C (en) | 2015-01-06 |
JP5879244B2 (ja) | 2016-03-08 |
CN102071342B (zh) | 2013-10-23 |
JP5639449B2 (ja) | 2014-12-10 |
EP2677049B1 (en) | 2017-08-23 |
PL2677049T3 (pl) | 2018-02-28 |
CA2721752A1 (en) | 2011-05-20 |
JP2013066936A (ja) | 2013-04-18 |
AU2010322540A1 (en) | 2012-06-07 |
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