WO2022240023A1 - Aluminum alloy, method for manufacturing same, and parts using same - Google Patents
Aluminum alloy, method for manufacturing same, and parts using same Download PDFInfo
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- WO2022240023A1 WO2022240023A1 PCT/KR2022/006090 KR2022006090W WO2022240023A1 WO 2022240023 A1 WO2022240023 A1 WO 2022240023A1 KR 2022006090 W KR2022006090 W KR 2022006090W WO 2022240023 A1 WO2022240023 A1 WO 2022240023A1
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- aluminum alloy
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- silicon
- aluminum
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- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 131
- 238000000034 method Methods 0.000 title claims abstract description 43
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 31
- 239000011572 manganese Substances 0.000 claims abstract description 36
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims abstract description 35
- 238000004512 die casting Methods 0.000 claims abstract description 35
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 35
- 239000010703 silicon Substances 0.000 claims abstract description 35
- 239000011575 calcium Substances 0.000 claims abstract description 28
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 25
- 229910052748 manganese Inorganic materials 0.000 claims abstract description 20
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims abstract description 17
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 15
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 claims abstract description 12
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 12
- 229910052791 calcium Inorganic materials 0.000 claims abstract description 12
- 239000012535 impurity Substances 0.000 claims abstract description 11
- 239000000203 mixture Substances 0.000 claims description 34
- 229910052804 chromium Inorganic materials 0.000 claims description 21
- 239000013078 crystal Substances 0.000 claims description 21
- 229910052719 titanium Inorganic materials 0.000 claims description 21
- 230000008569 process Effects 0.000 claims description 18
- 229910052726 zirconium Inorganic materials 0.000 claims description 18
- 239000000956 alloy Substances 0.000 claims description 11
- 229910045601 alloy Inorganic materials 0.000 claims description 10
- 239000000463 material Substances 0.000 claims description 10
- 229910052751 metal Inorganic materials 0.000 claims description 9
- 239000002184 metal Substances 0.000 claims description 9
- 239000011777 magnesium Substances 0.000 claims description 8
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 6
- 229910052749 magnesium Inorganic materials 0.000 claims description 6
- 238000002844 melting Methods 0.000 claims description 5
- 230000008018 melting Effects 0.000 claims description 5
- JBQYATWDVHIOAR-UHFFFAOYSA-N tellanylidenegermanium Chemical compound [Te]=[Ge] JBQYATWDVHIOAR-UHFFFAOYSA-N 0.000 claims description 5
- 238000004140 cleaning Methods 0.000 claims description 4
- 238000003825 pressing Methods 0.000 claims description 4
- 238000005260 corrosion Methods 0.000 description 28
- 230000007797 corrosion Effects 0.000 description 26
- 230000000052 comparative effect Effects 0.000 description 16
- 241000239290 Araneae Species 0.000 description 15
- 239000000047 product Substances 0.000 description 11
- 238000005406 washing Methods 0.000 description 11
- 238000011156 evaluation Methods 0.000 description 10
- 238000005266 casting Methods 0.000 description 9
- 238000001816 cooling Methods 0.000 description 8
- 229910000765 intermetallic Inorganic materials 0.000 description 8
- 239000000654 additive Substances 0.000 description 6
- 238000007743 anodising Methods 0.000 description 6
- 239000010949 copper Substances 0.000 description 6
- 239000003599 detergent Substances 0.000 description 6
- 238000010586 diagram Methods 0.000 description 6
- 239000002244 precipitate Substances 0.000 description 6
- 239000000523 sample Substances 0.000 description 6
- 230000000694 effects Effects 0.000 description 5
- 239000000843 powder Substances 0.000 description 5
- 239000002994 raw material Substances 0.000 description 5
- 150000003839 salts Chemical class 0.000 description 5
- 239000007921 spray Substances 0.000 description 5
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 4
- 229910052802 copper Inorganic materials 0.000 description 4
- 230000005484 gravity Effects 0.000 description 4
- 230000008901 benefit Effects 0.000 description 3
- 230000004907 flux Effects 0.000 description 3
- 238000007591 painting process Methods 0.000 description 3
- 239000011701 zinc Substances 0.000 description 3
- 230000000996 additive effect Effects 0.000 description 2
- 238000002474 experimental method Methods 0.000 description 2
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- ZLMJMSJWJFRBEC-UHFFFAOYSA-N Potassium Chemical compound [K] ZLMJMSJWJFRBEC-UHFFFAOYSA-N 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000007872 degassing Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000005495 investment casting Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000010309 melting process Methods 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000002161 passivation Methods 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 239000011591 potassium Substances 0.000 description 1
- 229910052700 potassium Inorganic materials 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000001902 propagating effect Effects 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D17/00—Pressure die casting or injection die casting, i.e. casting in which the metal is forced into a mould under high pressure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D21/00—Casting non-ferrous metals or metallic compounds so far as their metallurgical properties are of importance for the casting procedure; Selection of compositions therefor
- B22D21/02—Casting exceedingly oxidisable non-ferrous metals, e.g. in inert atmosphere
- B22D21/04—Casting aluminium or magnesium
-
- 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
Definitions
- the present invention can be applied to various devices such as home appliances, and relates to an aluminum alloy, a manufacturing method thereof, and parts using the same.
- Die casting also called die casting, is a precision casting method that manufactures parts having the same shape as the mold by injecting molten metal into a mold precisely processed to match the shape of the configuration of the device such as necessary parts, that is, the casting shape. can do. Parts or products produced by such die casting are also referred to as die casting castings.
- die casting can be said to be a casting method suitable for mass production.
- aluminum alloy is widely used as a material for die casting. Castings made of aluminum alloys are used in very diverse fields, and various types of aluminum alloys are used according to each main purpose.
- Aluminum alloys can be used for various parts and the like.
- various components used in a sturdy exterior material such as a TV stand and inside home appliances such as a washing machine or a refrigerator may be made of aluminum alloy.
- various mechanical properties may be required for aluminum alloys to be used in such exterior materials or various parts.
- a certain level of corrosion resistance, castability, mechanical strength, and the like may be required for aluminum alloys.
- mass productivity may be required in order to manufacture various parts with such an aluminum alloy.
- the Gravity Die-Casting (GDC) method makes mass production impossible.
- elements such as Ti, Cr, or Zr are used as additives in order to realize particle refinement for improving the corrosion properties of aluminum alloys.
- the technical problem to be solved by the present invention is to provide an aluminum alloy with improved corrosion resistance and castability, a manufacturing method thereof, and parts using the same.
- the present invention is to provide an aluminum alloy that does not require an additional painting process to enhance the corrosion resistance of the aluminum alloy, a manufacturing method thereof, and a part using the same.
- the present invention in the aluminum alloy for die casting, calcium (Ca) 2.0 to 6.0% by weight, manganese (Mn) 1.0 to 3.0% by weight, silicon (Si) 0.1 to 1.0% by weight %, iron (Fe) 0.1 to 0.5% by weight, the balance is aluminum (Al) and other unavoidable impurities, and the aluminum alloy has a crystal grain size of 10 to 50 ⁇ m.
- 1.0 to 1.5 wt% of zinc (Zn) may be further included.
- 0.01 to 0.1% by weight of magnesium may be further included.
- the content of manganese may be 0.8 to 1.5% by weight.
- the iron (Fe) content may be 0.1 to 0.3 wt%.
- the composition may not include at least one of Ti, Zr, and Cr.
- the Ti, Zr, and Cr may be materials used for grain refinement in the die casting process.
- the silicon content may be 0.1 to 0.2% by weight.
- the present invention is a die-casting part made of an aluminum alloy, wherein the aluminum alloy contains 2.0 to 6.0% by weight of calcium (Ca), 1.0 to 3.0% by weight of manganese (Mn), It is composed of 0.1 to 1.0% by weight of silicon (Si), 0.1 to 0.5% by weight of iron (Fe), the balance aluminum (Al) and other unavoidable impurities, and the crystal grain size of the aluminum alloy is 10 to 50 ⁇ m. do.
- the aluminum alloy contains 2.0 to 6.0% by weight of calcium (Ca), 1.0 to 3.0% by weight of manganese (Mn), It is composed of 0.1 to 1.0% by weight of silicon (Si), 0.1 to 0.5% by weight of iron (Fe), the balance aluminum (Al) and other unavoidable impurities, and the crystal grain size of the aluminum alloy is 10 to 50 ⁇ m. do.
- the present invention provides a method for producing an aluminum alloy using die casting, comprising: melting an ingot; molten metal cleaning step; injecting the molten alloy into the mold; Injecting by applying pressure; And including the step of opening and extruding, calcium (Ca) 2.0 to 6.0% by weight, manganese (Mn) 1.0 to 3.0% by weight, silicon (Si) 0.1 to 1.0% by weight, iron (Fe) 0.1 to 0.5% by weight, It is characterized in that it is composed of aluminum (Al) and other unavoidable impurities.
- the pressure may be 125 to 130 kgf/cm 2 .
- mechanical properties including corrosion resistance and castability of an aluminum alloy can be improved.
- an additional painting process is not required to enhance the corrosion resistance of the aluminum alloy, so the number of processes and process time can be reduced, thereby reducing costs.
- it is intended to provide an aluminum alloy in which intermetallic compounds are evenly distributed and dispersed.
- FIG. 1 is a diagram showing examples of products and parts that can be manufactured using an aluminum alloy according to an embodiment of the present invention.
- FIG. 2 is a graph showing the yield strength of specimens manufactured using an aluminum alloy according to an embodiment of the present invention.
- Figure 3 is a photograph of the results of salt spray evaluation and powder detergent evaluation for a spider manufactured through an aluminum alloy according to an embodiment of the present invention and a comparative example.
- FIG. 4 is a photograph of the surface of a spider made of an aluminum alloy according to a comparative example.
- FIG. 5 is a photograph of the surface of a spider made of an aluminum alloy according to an embodiment of the present invention.
- FIG. 6 is a conceptual diagram showing crystal grains and crack propagation of an aluminum alloy according to a comparative example.
- FIG. 7 is a conceptual diagram illustrating crystal grains and crack propagation of an aluminum alloy according to an embodiment of the present invention.
- FIG. 8 is a flow chart showing a method for manufacturing an aluminum alloy according to an embodiment of the present invention.
- an aluminum alloy for die casting may be produced by a composition containing 0.1 to 0.5% by weight, the balance of aluminum (Al) and other unavoidable impurities.
- the content of manganese in the above composition may be 0.8 to 1.5% by weight.
- the content of iron (Fe) in the above composition may be 0.1 to 0.3% by weight.
- an aluminum alloy with improved corrosion resistance and castability can be obtained using the composition presented above, but the corrosion resistance and castability of the aluminum alloy can be further improved through the content of manganese and / or iron defined in more detail as described above.
- composition of the aluminum alloy for die casting 1.0 to 1.5% by weight of zinc (Zn) may be further included.
- magnesium may be further included.
- an aluminum alloy for die casting in the aluminum alloy for die casting, calcium (Ca) 2.0 to 6.0% by weight, manganese (Mn) 0.8 to 1.5% by weight, zinc (Zn) 1.0 to 1.5% by weight, silicon
- An aluminum alloy for die casting may be manufactured by a composition including 0.1 to 1.0 wt% of (Si), 0.1 to 0.3 wt% of iron (Fe), the balance of aluminum (Al), and other unavoidable impurities.
- the composition of the aluminum alloy for die casting may not include at least one of Ti, Zr, and Cr.
- composition of the aluminum alloy for die casting may not include Ti, Zr, and Cr.
- These Ti, Zr, and Cr may be materials used for grain refinement in an aluminum die casting process.
- additives such as Ti, Cr, or Zr may be added in order to realize grain refinement for improving corrosion properties.
- an aluminum alloy can be manufactured using a high pressure die-casting (HPDC) method. As a result, it is possible to manufacture an aluminum alloy having particularly excellent corrosion resistance properties.
- HPDC high pressure die-casting
- the aluminum alloy according to the present invention may exhibit equivalent anti-corrosion properties compared to an aluminum alloy produced by the GDC method by adding a specific element as an additive.
- an aluminum alloy having excellent corrosion resistance characteristics can be implemented without adding a specific element (Ti, Cr, Zr, etc.) for grain refinement. Due to this, there are advantages such as reduction in production time by omitting the additional flux treatment process along with the effect of reducing the cost of expensive raw materials.
- composition of the aluminum alloy of the present invention a part using the same, and a manufacturing method will be described later in detail with reference to the drawings.
- FIG. 1 is a diagram showing examples of products and parts that can be manufactured using an aluminum alloy according to an embodiment of the present invention.
- an aluminum alloy according to an embodiment of the present invention may be used for parts of a washing machine 10.
- aluminum alloy can be used in various cast-type products or parts that can be manufactured through a die casting process.
- FIG. 1(B) a spider 11, which is a part that can be used in a washing machine as shown in FIG. 1(A), is shown. Also, referring to FIG. 1(C), a hub 12, which is a part that can be used in a washing machine as shown in FIG. 1(A), is shown.
- the spider 11 may be mounted on a driving unit of the washing machine 10, including a drum type and a through type, and the hub 12 may be mounted on a motor and a connection unit of the washing machine 10.
- the spider 11 and the hub 12 are parts that are continuously driven when the washing machine 10 operates, and thus require durability, and since they can always come into contact with water and detergent, corrosion resistance may also be required. Moreover, since the washing machine 10 can be visually recognized from the outside when the washing machine 10 is driven and is highly likely to come into contact with clothes, gloss characteristics may be important.
- the composition of the aluminum alloy is required to satisfy a certain level of durability, corrosion resistance, glossiness, and castability.
- the aluminum alloy according to one embodiment of the present invention may be used for exterior materials for electronic products such as TV stands in addition to the washing machine products described above.
- aluminum alloy may be applied to various parts constituting a TV stand such as a base, a bracket, and a cover.
- FIG. 2 is a graph showing the yield strength of specimens manufactured using an aluminum alloy according to an embodiment of the present invention.
- the yield strength is approximately 170 MPa in the sample prepared primarily. It can be seen that there is an improvement compared to The secondary sample may be according to the first embodiment of the present invention.
- the tertiary sample may be according to the second embodiment of the present invention.
- an embodiment of the present invention may correspond to any one or more of the first embodiment and the second embodiment.
- the silicon content of silicon (Si) is related to the gloss of aluminum alloy products, the silicon content can be reduced even if the yield strength is partially reduced within the limit allowed by the product.
- Figure 3 is a photograph of the results of salt spray evaluation and powder detergent evaluation for a spider manufactured through an aluminum alloy according to an embodiment of the present invention and a comparative example.
- composition of the aluminum alloy according to the comparative example and an embodiment of the present invention is as shown in Table 1 below.
- composition of the aluminum alloy according to one embodiment of the present invention summarized in Table 1 is approximately the same as the composition of the aluminum alloy for die casting described above.
- composition of one embodiment of the present invention summarized in Table 1 is the composition described above, calcium (Ca) 2.0 to 6.0% by weight, manganese (Mn) 1.0 to 3.0% by weight, silicon (Si) 0.1 to 1.0% by weight, iron (Fe) 0.1 to 0.5% by weight, the balance may fall within the range of the composition including aluminum (Al) and other unavoidable impurities.
- composition of the comparative example has magnesium (Mg) 2.5 to 3.0% by weight and silicon (Si) 9.6 to 10.5% by weight as the main composition, and manganese (Mn) and iron (Fe) are added in small amounts.
- the salt spray evaluation in FIG. 3 was made over 1000 hours. In addition, powder detergent evaluation was made over 456 hours.
- FIG. 4 is a photograph of the surface of a spider made of an aluminum alloy according to a comparative example.
- 5 is a surface photograph of a spider made of an aluminum alloy according to an embodiment of the present invention.
- FIG. 4 shows the results of an anodizing experiment of a spider made of an aluminum alloy according to a comparative example.
- FIG. 5 shows the results of an anodizing experiment of a spider made of an aluminum alloy according to an embodiment of the present invention.
- FIG. 6 is a conceptual diagram showing crystal grains and crack propagation of an aluminum alloy according to a comparative example
- FIG. 7 is a conceptual diagram showing crystal grains and crack propagation of an aluminum alloy according to an embodiment of the present invention.
- FIG. 6(A) schematically shows the surface shape of an aluminum alloy according to a comparative example. On the surface of these aluminum alloys, grains and grain boundaries exist. At this time, intermetallic compounds such as Al 6 Mn and Al 13 Fe 4 are mainly distributed in crystal grain boundaries having an unstable structure.
- Figure 7 (A) schematically shows the surface shape of an aluminum alloy according to an embodiment of the present invention.
- the intermetallic compound is evenly distributed or dispersed over the entire surface.
- An aluminum alloy in which such an intermetallic compound is evenly distributed or dispersed over the entire surface may be formed by crystal grain refinement.
- the grain size may be approximately 100 ⁇ m.
- the crystal grain size may be smaller than this. Referring to FIG. 7(A) , it can be seen that the size of the crystal grains is significantly reduced compared to FIG. 6 .
- the crack may stop at a certain level without continuously propagating along the grain boundary.
- the breaking strength of the aluminum alloy may be improved.
- the grain size of the aluminum alloy according to one embodiment of the present invention may be 10 to 50 ⁇ m.
- the intermetallic compound since the intermetallic compound is evenly distributed or dispersed over the entire surface of the aluminum alloy, the intermetallic compound may be located inside these crystal grains. That is, according to one embodiment of the present invention, the mechanical properties of the aluminum alloy can be improved according to the micronized grain size.
- corrosion of metals including aluminum alloy can occur in the process of pitting ⁇ propagation ⁇ re-pasivation (passivation film).
- crevice corrosion may occur mainly at grain boundaries.
- the boundaries of the grain boundaries may also become unclear (the boundaries are broken in the middle), and propagation may stop after crevice corrosion occurs.
- the aluminum alloy according to an embodiment of the present invention may not include at least one of Ti, Zr, and Cr. Characteristically, the aluminum alloy according to an embodiment of the present invention may not include all of Ti, Zr, and Cr.
- Ti, Zr, and Cr may be materials related to grain refinement, but according to an embodiment of the present invention, a desired level of grain refinement may be achieved without including Ti, Zr, and Cr.
- the grain size of the aluminum alloy according to an embodiment of the present invention may be 10 to 50 ⁇ m.
- the composition of silicon (Si) in the aluminum alloy may be 0.2% by weight or less.
- the silicon content may be 0.1 to 0.2% by weight.
- Silicon (Si) is a unique raw material and has a color (dark gray). Therefore, when the silicon content is increased, a color unique to the silicon element may appear on the surface of the alloy. For example, when the silicon content is high, stains caused by silicon or its precipitates may occur on the surface of the alloy.
- the silicon content can be suppressed when high gloss properties are used.
- the aluminum alloy when the aluminum alloy has the composition described above and the silicon content is 0.1 to 0.2% by weight, it can be used for products or parts having sufficient mechanical properties and high gloss.
- Such an aluminum alloy according to an embodiment of the present invention may be formed by having the composition described above.
- an aluminum alloy according to an embodiment of the present invention having the above characteristics can be manufactured by the manufacturing method described below together with the composition described above. Features of this manufacturing method will be described in detail below.
- FIG. 8 is a flow chart showing a method for manufacturing an aluminum alloy according to an embodiment of the present invention.
- a high pressure die-casting (HPDC) method may be used as a manufacturing method of the aluminum alloy. As a result, it is possible to manufacture an aluminum alloy having particularly excellent corrosion resistance properties.
- the aluminum alloy according to one embodiment of the present invention may exhibit equivalent anti-corrosion properties compared to an aluminum alloy produced by the GDC method by adding a specific element as an additive.
- an aluminum alloy having excellent corrosion resistance characteristics can be implemented without adding a specific element (Ti, Cr, Zr, etc.) for grain refinement. Due to this, there are advantages such as reduction in production time by omitting the additional flux treatment process along with the effect of reducing the cost of expensive raw materials.
- the step of melting the ingot (S10) may correspond to a process of melting the raw material to achieve the composition described above. This melting process may be performed at approximately 700 °C.
- the molten metal cleaning step (S20) may include a process of removing dross after introducing a degassing agent into the ingot.
- the molten alloy is injected into the mold.
- the injection process (S40) may be performed by applying pressure and pushing the molten alloy into the mold at high pressure.
- An embodiment of the present invention is characterized in that a pressure of 125 to 130 kgf/cm 2 is used for crystal grain refinement.
- a pressure of 125 to 130 kgf/cm 2 may be used in the mold process in order to achieve a desired level of crystal grain refinement without adding a specific element (Ti, Cr, Zr, etc.).
- these pressure conditions may be related to the alloy composition described above.
- Target fracture strength can be achieved using such alloy composition and/or pressure conditions. That is, crystal grain refinement can be achieved using such alloy composition and/or pressure conditions, and the intermetallic compound (Al 3 Fe/Al 4 Mn or Al 6 Mn, Al 13 Fe 4 ) is evenly dispersed, thereby increasing the strength of the aluminum alloy. can be improved.
- the cooling time of the aluminum alloy may be shorter than that of a conventional manufacturing method (usually about 10 seconds).
- the growth of crystal grains can be completed within a short time by such a fast cooling rate. Accordingly, the grain size can be miniaturized to a desired level.
- the cooling time of this aluminum alloy may correspond to 3 to 5 seconds.
- metal nuclei are created and grown, and grain boundaries that meet the growth of other nuclei must be formed at the boundary of the growth.
- the total amount of crystals of a specific material is 100, if the cooling rate is slow, for example, even with 5 nuclei, the total amount can be adjusted by grain growth. However, when the cooling rate is fast, grain growth is suppressed and the total amount cannot be matched. In this case, 5 or more nuclei are required to achieve thermodynamic equilibrium, and the total amount can be adjusted with 5 or more nuclei. In other words, crystal grains can be refined.
- the size can be miniaturized.
- mechanical properties of the aluminum alloy may be improved by such grain refinement.
- a spider or a door hinge of a washing machine may be manufactured using the improved aluminum alloy.
- the present invention it is applicable to various devices such as home appliances, and it is possible to provide an aluminum alloy, a manufacturing method thereof, and parts using the same.
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Abstract
Description
AlAl | SiSi | MgMg | CaCa | MnMn | FeFe | |
비교예comparative example | 90.0 이하90.0 or less | 9.6~10.69.6~10.6 | 2.5~3.02.5 to 3.0 | -- | 0.5~0.60.5~0.6 | 0.6~0.70.6~0.7 |
본 발명the present invention | 90.0 이상90.0 or higher | 1.0 이하below 1.0 | 0.1 이하0.1 or less | 2.0~6.02.0 to 6.0 | 1.0~3.01.0 to 3.0 | 0.5 이하less than 0.5 |
Claims (20)
- 다이캐스팅용 알루미늄 합금에 있어서,In the aluminum alloy for die casting,칼슘(Ca) 2.0 내지 6.0 중량%, 망간(Mn) 1.0 내지 3.0 중량%, 실리콘(Si) 0.1 내지 1.0 중량%, 철(Fe) 0.1 내지 0.5 중량%, 잔부 알루미늄(Al) 및 기타 불가피한 불순물을 포함하여 조성되고,Calcium (Ca) 2.0 to 6.0% by weight, manganese (Mn) 1.0 to 3.0% by weight, silicon (Si) 0.1 to 1.0% by weight, iron (Fe) 0.1 to 0.5% by weight, the balance aluminum (Al) and other unavoidable impurities made up of,상기 알루미늄 합금의 결정립 크기는 10 내지 50 ㎛인 것을 특징으로 하는 알루미늄 합금.The aluminum alloy, characterized in that the grain size of the aluminum alloy is 10 to 50 ㎛.
- 제1항에 있어서, 아연(Zn) 1.0 내지 1.5 중량%를 더 포함하는 것을 특징으로 하는 알루미늄 합금.The aluminum alloy according to claim 1, further comprising 1.0 to 1.5% by weight of zinc (Zn).
- 제1항에 있어서, 마그네슘 0.01 내지 0.1 중량%를 더 포함하는 것을 특징으로 하는 알루미늄 합금.The aluminum alloy according to claim 1, further comprising 0.01 to 0.1% by weight of magnesium.
- 제1항에 있어서, 상기 망간의 함량은 0.8 내지 1.5 중량%인 것을 특징으로 하는 알루미늄 합금.The aluminum alloy according to claim 1, wherein the manganese content is 0.8 to 1.5% by weight.
- 제1항에 있어서, 상기 철(Fe)의 함량은 0.1 내지 0.3 중량%인 것을 특징으로 하는 알루미늄 합금.The aluminum alloy according to claim 1, wherein the content of iron (Fe) is 0.1 to 0.3% by weight.
- 제1항에 있어서, 상기 조성은 Ti, Zr, 및 Cr 중 적어도 어느 하나를 포함하지 않는 것을 특징으로 하는 알루미늄 합금.The aluminum alloy according to claim 1, wherein the composition does not include at least one of Ti, Zr, and Cr.
- 제1항에 있어서, 상기 Ti, Zr, 및 Cr은 상기 다이캐스팅 공정 중에서 결정립(grain) 미세화를 위하여 이용되는 물질인 것을 특징으로 하는 알루미늄 합금.The aluminum alloy according to claim 1, wherein the Ti, Zr, and Cr are materials used for grain refinement in the die casting process.
- 제1항에 있어서, 상기 실리콘 함량은 0.1 내지 0.2 중량%인 것을 특징으로 하는 알루미늄 합금.The aluminum alloy according to claim 1, wherein the silicon content is 0.1 to 0.2% by weight.
- 알루미늄 합금으로 제작되는 다이캐스팅 부품에 있어서,In the die-casting parts made of aluminum alloy,상기 알루미늄 합금은,The aluminum alloy,칼슘(Ca) 2.0 내지 6.0 중량%, 망간(Mn) 1.0 내지 3.0 중량%, 실리콘(Si) 0.1 내지 1.0 중량%, 철(Fe) 0.1 내지 0.5 중량%, 잔부 알루미늄(Al) 및 기타 불가피한 불순물을 포함하여 조성되고, Calcium (Ca) 2.0 to 6.0% by weight, manganese (Mn) 1.0 to 3.0% by weight, silicon (Si) 0.1 to 1.0% by weight, iron (Fe) 0.1 to 0.5% by weight, the balance aluminum (Al) and other unavoidable impurities made up of,상기 알루미늄 합금의 결정립 크기는 10 내지 50 ㎛인 것을 특징으로 하는 부품.Part characterized in that the grain size of the aluminum alloy is 10 to 50 ㎛.
- 제9항에 있어서, 아연(Zn) 1.0 내지 1.5 중량%를 더 포함하는 것을 특징으로 하는 부품.10. The component according to claim 9, further comprising 1.0 to 1.5% by weight of zinc (Zn).
- 제9항에 있어서, 마그네슘 0.01 내지 0.1 중량%를 더 포함하는 것을 특징으로 하는 부품.10. The component according to claim 9, further comprising 0.01 to 0.1% by weight of magnesium.
- 제9항에 있어서, 상기 실리콘 함량은 0.1 내지 0.2 중량%인 것을 특징으로 하는 부품.10. The component according to claim 9, wherein the silicon content is between 0.1 and 0.2% by weight.
- 제9항에 있어서, 상기 조성은 Ti, Zr, 및 Cr 중 적어도 어느 하나를 포함하지 않는 것을 특징으로 하는 부품.10. The component according to claim 9, wherein the composition does not contain at least one of Ti, Zr, and Cr.
- 제9항에 있어서, 상기 망간의 함량은 0.8 내지 1.5 중량%인 것을 특징으로 하는 부품.10. The component according to claim 9, wherein the content of manganese is 0.8 to 1.5% by weight.
- 제9항에 있어서, 상기 철(Fe)의 함량은 0.1 내지 0.3 중량%인 것을 특징으로 하는 부품.10. The component according to claim 9, wherein the content of iron (Fe) is 0.1 to 0.3% by weight.
- 다이캐스팅을 이용한 알루미늄 합금의 제조 방법에 있어서,In the method for producing an aluminum alloy using die casting,잉곳 용융하는 단계;melting the ingot;용탕 클리닝 단계;molten metal cleaning step;금형에 용융된 합금을 주입하는 단계;injecting the molten alloy into the mold;압력을 가하여 사출하는 단계; 및Injecting by applying pressure; and형개 및 압출하는 단계를 포함하고,Including the steps of opening and extruding the mold,칼슘(Ca) 2.0 내지 6.0 중량%, 망간(Mn) 1.0 내지 3.0 중량%, 실리콘(Si) 0.1 내지 1.0 중량%, 철(Fe) 0.1 내지 0.5 중량%, 잔부 알루미늄(Al) 및 기타 불가피한 불순물을 포함하여 조성되는 것을 특징으로 하는 알루미늄 합금의 제조 방법.Calcium (Ca) 2.0 to 6.0% by weight, manganese (Mn) 1.0 to 3.0% by weight, silicon (Si) 0.1 to 1.0% by weight, iron (Fe) 0.1 to 0.5% by weight, the balance aluminum (Al) and other unavoidable impurities Method for producing an aluminum alloy, characterized in that the composition comprising.
- 제16항에 있어서, 상기 압력은 125 내지 130 kgf/㎠인 것을 특징으로 하는 알루미늄 합금의 제조 방법.The method of claim 16, wherein the pressure is 125 to 130 kgf/cm 2 .
- 제16항에 있어서, 상기 알루미늄 합금의 결정립 크기는 10 내지 50 ㎛인 것을 특징으로 하는 알루미늄 합금의 제조 방법.The method of claim 16, wherein the aluminum alloy has a crystal grain size of 10 to 50 μm.
- 제16항에 있어서, 상기 실리콘 함량은 0.1 내지 0.2 중량%인 것을 특징으로 하는 알루미늄 합금의 제조 방법.17. The method of claim 16, wherein the silicon content is 0.1 to 0.2% by weight.
- 제16항에 있어서, 상기 조성은 Ti, Zr, 및 Cr 중 적어도 어느 하나를 포함하지 않는 것을 특징으로 하는 알루미늄 합금의 제조 방법.17. The method of claim 16, wherein the composition does not include at least one of Ti, Zr, and Cr.
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US4126448A (en) * | 1977-03-31 | 1978-11-21 | Alcan Research And Development Limited | Superplastic aluminum alloy products and method of preparation |
JP2000355722A (en) * | 1999-06-17 | 2000-12-26 | Nippon Light Metal Co Ltd | Al-Si DIECAST PRODUCT EXCELLENT IN AIRTIGHTNESS AND WEAR RESISTANCE, AND ITS MANUFACTURE |
JP2004162140A (en) * | 2002-11-14 | 2004-06-10 | Toyota Motor Corp | Al-Mg ALLOY FOR DIE CASTING AND METHOD FOR MANUFACTURING DIE-CAST PRODUCT MADE FROM Al-Mg ALLOY |
KR20040068021A (en) * | 2003-01-23 | 2004-07-30 | 알루미늄 라인펠덴 게엠베하 | Aluminium alloy for diecasting |
CN102796925A (en) * | 2011-05-27 | 2012-11-28 | 广东鸿泰科技股份有限公司 | High-strength die-casting aluminum alloy for pressure casting |
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US4126448A (en) * | 1977-03-31 | 1978-11-21 | Alcan Research And Development Limited | Superplastic aluminum alloy products and method of preparation |
JP2000355722A (en) * | 1999-06-17 | 2000-12-26 | Nippon Light Metal Co Ltd | Al-Si DIECAST PRODUCT EXCELLENT IN AIRTIGHTNESS AND WEAR RESISTANCE, AND ITS MANUFACTURE |
JP2004162140A (en) * | 2002-11-14 | 2004-06-10 | Toyota Motor Corp | Al-Mg ALLOY FOR DIE CASTING AND METHOD FOR MANUFACTURING DIE-CAST PRODUCT MADE FROM Al-Mg ALLOY |
KR20040068021A (en) * | 2003-01-23 | 2004-07-30 | 알루미늄 라인펠덴 게엠베하 | Aluminium alloy for diecasting |
CN102796925A (en) * | 2011-05-27 | 2012-11-28 | 广东鸿泰科技股份有限公司 | High-strength die-casting aluminum alloy for pressure casting |
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