EP3196323B1 - Druckgussprodukt aus aluminiumlegierung - Google Patents
Druckgussprodukt aus aluminiumlegierung Download PDFInfo
- Publication number
- EP3196323B1 EP3196323B1 EP14904322.6A EP14904322A EP3196323B1 EP 3196323 B1 EP3196323 B1 EP 3196323B1 EP 14904322 A EP14904322 A EP 14904322A EP 3196323 B1 EP3196323 B1 EP 3196323B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- aluminum alloy
- alloy
- corrosion resistance
- die casting
- castability
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- 229910000838 Al alloy Inorganic materials 0.000 title claims description 83
- 238000004512 die casting Methods 0.000 claims description 31
- 229910052712 strontium Inorganic materials 0.000 claims description 8
- 239000012535 impurity Substances 0.000 claims description 7
- 229910052719 titanium Inorganic materials 0.000 claims description 7
- 229910052791 calcium Inorganic materials 0.000 claims description 6
- 229910052708 sodium Inorganic materials 0.000 claims description 6
- 229910052796 boron Inorganic materials 0.000 claims description 5
- 238000005260 corrosion Methods 0.000 description 31
- 230000007797 corrosion Effects 0.000 description 31
- 230000000052 comparative effect Effects 0.000 description 22
- 229910045601 alloy Inorganic materials 0.000 description 21
- 239000000956 alloy Substances 0.000 description 21
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 18
- 239000011651 chromium Substances 0.000 description 17
- 239000010949 copper Substances 0.000 description 16
- 239000000463 material Substances 0.000 description 13
- 239000011777 magnesium Substances 0.000 description 11
- 230000000694 effects Effects 0.000 description 10
- 239000010936 titanium Substances 0.000 description 10
- 229910052742 iron Inorganic materials 0.000 description 8
- 230000004048 modification Effects 0.000 description 8
- 238000012986 modification Methods 0.000 description 8
- 229910052804 chromium Inorganic materials 0.000 description 7
- 229910052710 silicon Inorganic materials 0.000 description 7
- 238000012360 testing method Methods 0.000 description 7
- 238000011282 treatment Methods 0.000 description 7
- 230000005496 eutectics Effects 0.000 description 6
- 230000008018 melting Effects 0.000 description 6
- 238000002844 melting Methods 0.000 description 6
- 239000011575 calcium Substances 0.000 description 5
- 238000005266 casting Methods 0.000 description 5
- 229910052802 copper Inorganic materials 0.000 description 5
- 239000013078 crystal Substances 0.000 description 5
- 229910052749 magnesium Inorganic materials 0.000 description 5
- 238000000034 method Methods 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- 239000011734 sodium Substances 0.000 description 5
- 229910052782 aluminium Inorganic materials 0.000 description 4
- 239000002994 raw material Substances 0.000 description 4
- 150000003839 salts Chemical class 0.000 description 4
- 239000000243 solution Substances 0.000 description 4
- 239000007921 spray Substances 0.000 description 4
- 229910052748 manganese Inorganic materials 0.000 description 3
- 238000005259 measurement Methods 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 230000002265 prevention Effects 0.000 description 3
- 239000010703 silicon Substances 0.000 description 3
- 239000011856 silicon-based particle Substances 0.000 description 3
- RZVAJINKPMORJF-UHFFFAOYSA-N Acetaminophen Chemical compound CC(=O)NC1=CC=C(O)C=C1 RZVAJINKPMORJF-UHFFFAOYSA-N 0.000 description 2
- 229910018134 Al-Mg Inorganic materials 0.000 description 2
- 229910021364 Al-Si alloy Inorganic materials 0.000 description 2
- 229910018467 Al—Mg Inorganic materials 0.000 description 2
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- 229910017060 Fe Cr Inorganic materials 0.000 description 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 2
- 229910000676 Si alloy Inorganic materials 0.000 description 2
- 230000032683 aging Effects 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- TZCXTZWJZNENPQ-UHFFFAOYSA-L barium sulfate Chemical compound [Ba+2].[O-]S([O-])(=O)=O TZCXTZWJZNENPQ-UHFFFAOYSA-L 0.000 description 2
- 239000010953 base metal Substances 0.000 description 2
- 230000015556 catabolic process Effects 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 238000006731 degradation reaction Methods 0.000 description 2
- 239000005297 pyrex Substances 0.000 description 2
- 230000001105 regulatory effect Effects 0.000 description 2
- 239000006104 solid solution Substances 0.000 description 2
- 229910018566 Al—Si—Mg Inorganic materials 0.000 description 1
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 1
- DGAQECJNVWCQMB-PUAWFVPOSA-M Ilexoside XXIX Chemical compound C[C@@H]1CC[C@@]2(CC[C@@]3(C(=CC[C@H]4[C@]3(CC[C@@H]5[C@@]4(CC[C@@H](C5(C)C)OS(=O)(=O)[O-])C)C)[C@@H]2[C@]1(C)O)C)C(=O)O[C@H]6[C@@H]([C@H]([C@@H]([C@H](O6)CO)O)O)O.[Na+] DGAQECJNVWCQMB-PUAWFVPOSA-M 0.000 description 1
- 229910019752 Mg2Si Inorganic materials 0.000 description 1
- 229910018594 Si-Cu Inorganic materials 0.000 description 1
- 229910018619 Si-Fe Inorganic materials 0.000 description 1
- 229910008465 Si—Cu Inorganic materials 0.000 description 1
- 229910008289 Si—Fe Inorganic materials 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- CSDREXVUYHZDNP-UHFFFAOYSA-N alumanylidynesilicon Chemical compound [Al].[Si] CSDREXVUYHZDNP-UHFFFAOYSA-N 0.000 description 1
- 229910052787 antimony Inorganic materials 0.000 description 1
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 description 1
- 238000012512 characterization method Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000002425 crystallisation Methods 0.000 description 1
- 230000008025 crystallization Effects 0.000 description 1
- 238000006356 dehydrogenation reaction Methods 0.000 description 1
- 238000009472 formulation Methods 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 239000011572 manganese Substances 0.000 description 1
- 230000007935 neutral effect Effects 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- CIOAGBVUUVVLOB-UHFFFAOYSA-N strontium atom Chemical compound [Sr] CIOAGBVUUVVLOB-UHFFFAOYSA-N 0.000 description 1
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
- C22C21/02—Alloys based on aluminium with silicon as the next major constituent
-
- 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
- B22D21/002—Castings of light metals
- B22D21/007—Castings of light metals with low melting point, e.g. Al 659 degrees C, Mg 650 degrees C
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/02—Alloys based on aluminium with silicon as the next major constituent
- C22C21/04—Modified aluminium-silicon alloys
Definitions
- the present invention relates to an aluminum alloy for die casting having improved castability and corrosion resistance, and an aluminum alloy die cast produced using the alloy.
- Aluminum alloys are lightweight and have various properties such as excellent thermal conductivity and high corrosion resistance, and therefore are widely used as materials for components in various fields such as automobiles, industrial machines, aircrafts, and electrical home appliances.
- One of such fields is the field of aluminum alloys for die casting, and representative examples thereof include ADC12 that is an Al-Si-Cu based alloy for die casting specified by Japanese Industrial Standards JIS H5302 (hereinafter simply referred to as "ADC12").
- ADC12 has satisfactory fluidity and filling characteristic during casting (die casting), and therefore has been frequently used for usage applications such as cases and covers such as cylinder head covers, cylinder blocks, and carburetors for automobiles, or die cast components other than those for automobiles.
- ADC12 is poor in corrosion resistance
- a process for improving corrosion resistance such as anodic oxidation, is required if ADC12 is used under an environment where it is easily corroded, which causes problems in terms of labor, cost, and the like.
- ADC5 and ADC6 that are Al-Mg based alloys for die casting specified by Japanese Industrial Standards JIS H5302 (hereinafter simply referred to as "ADC5" and “ADC6”) are excellent in corrosion resistance, but are poor in fluidity because of a large solidification range and therefore are likely to cause cracks in die-cast products. That is, since the Al-Mg based alloys are significantly inferior in castability to ADC12, usage applications thereof are likely to be disadvantageously limited to products with simple structures.
- Patent Literature 1 discloses an aluminum alloy for die casting that contains: Si by 9.0 to 12.0 wt%; Mg by 0.20 to 0.80 wt%; Mn+Fe by 0.7 to 1.1 wt%, in which Mn/Fe ratio is not less than 1.5; Cu as an impurity that is regulated to be not more than 0.5 wt%; and a remaining portion of the aluminum alloy that consists of aluminum and unavoidable impurities.
- the amounts of Mn, Fe, and Cu have great influence on corrosion resistance of the aluminum alloy, and the corrosion resistance is greatly improved as compared to that of ADC12 by, for example, regulating the amount of Cu to be not more than 0.5 wt%.
- JP 2001 200326 A describes an aluminum alloy containing, by weight, 7 to 13% Si, 0.001 to 0.2% Fe, at least one of Mn and Cr by 0.001 to 0.25%, 0.003 to 0.03% Sr, 0.005 to 0.03% Ti, and the balance Al with inevitable impurities.
- Patent Literature 1 can improve corrosion resistance of an aluminum alloy to a level approximately equal to that of AC4C that is an Al-Si-Mg based alloy for die casting specified by Japanese Industrial Standards JIS H5202, mechanical properties of the aluminum alloy in comparison with ADC12 are uncertain.
- Patent Literature 1 provides castability about 80% of that of ADC12 when compared in flow length, it is difficult to say that the castability reaches a level approximately equal to that of ADC12.
- a main objective of the present invention is to provide: an aluminum alloy for die casting, having castability and mechanical properties equivalent to those of ADC12 and corrosion resistance equivalent to that of ADC6; and an aluminum alloy die cast produced using the alloy.
- a aspect of the present invention is an aluminum alloy die cast obtained through die-casting an aluminum alloy for die casting containing: Cu by not more than 0.10 wt%; Si by 12.0 to 15.0 wt%; Mg by not more than 1.00 wt%; Fe by 0.05 to 1.00 wt%; Cr by 0.10 to 0.50 wt%; and optionally Sb by 0.05 to 0.20 wt%, Ti by 0.05 to 0.30 wt%, B by 1 to 50 ppm and/or at least one selected from Na, Sr, and Ca by 30 to 200 ppm, with the remaining portion of the aluminum alloy being Al and unavoidable impurities.
- Si is contained by 12.0 to 15.0 wt% to improve castability of the alloy, the content ratio of Cu that is considered to have most influence on corrosion resistance is suppressed to not more than 0.10 wt%, and Cr that effectively improves corrosion resistance and anti-seizing characteristic is contained by 0.10 to 0.50 wt%. Therefore, it is possible to obtain an alloy having castability and mechanical properties comparable to those of ADC12, and high corrosion resistance comparable to that of ADC6.
- an ingot of an aluminum alloy for die casting having not only excellent castability and mechanical properties but also excellent corrosion resistance can be produced safely and easily.
- At least one selected from Na, Sr, and Ca is added by 30 to 200 ppm, or Sb is added by 0.05 to 0.20 wt%.
- adding Ti by 0.05 to 0.30 wt% or adding B by 1 to 50 ppm is also preferable. By doing so, crystal grains of the aluminum alloy can be miniaturized even when the amount of Si is particularly small and when a casting method having a low cooling rate is used. As a result, stretching of the aluminum alloy can be improved.
- the aluminum alloy die cast obtained through die-casting the aluminum alloy for die casting of the present invention can be mass produced with satisfactory castability and is superior not only in mechanical properties such as yield strength and stretching but also in corrosion resistance, the aluminum alloy die cast is most suitable for usage applications, such as structural components for automobiles, which are used outdoor for long hours.
- an aluminum alloy for die casting having castability and mechanical properties equivalent to those of ADC12 and corrosion resistance equivalent to that of ADC6; and an aluminum alloy die cast produced using the alloy.
- An aluminum alloy for die casting of the present invention (hereinafter, also simply referred to as "aluminum alloy”) mainly contains Cu (copper) by not more than 0.10 wt%, Si (silicon) by 12.0 to 15.0 wt%, Mg (magnesium) by not more than 1.00 wt%, Fe (iron) by 0.05 to 1.00 wt%, Cr (chromium) by 0.10 to 0.50 wt%, and Al (aluminum) and unavoidable impurities as a remaining portion of the aluminum alloy.
- aluminum alloy mainly contains Cu (copper) by not more than 0.10 wt%, Si (silicon) by 12.0 to 15.0 wt%, Mg (magnesium) by not more than 1.00 wt%, Fe (iron) by 0.05 to 1.00 wt%, Cr (chromium) by 0.10 to 0.50 wt%, and Al (aluminum) and unavoidable impurities as a remaining portion of
- Cu copper
- Cu improves mechanical strength and hardness of the aluminum alloy, but on the other hand, significantly degrades corrosion resistance of the aluminum alloy. Therefore, in order to improve corrosion resistance of the aluminum alloy, the content of Cu, except Cu mixed as an impurity, needs to be reduced.
- the content ratio of Cu with respect to the whole weight of the aluminum alloy is not more than 0.10 wt%. If more strict corrosion resistance is required of the aluminum alloy die cast using the alloy, the content ratio of Cu with respect to the whole weight of the aluminum alloy is preferably not more than 0.08 wt%, and more preferably, not more than 0.05 wt%.
- Si silicon is an important element that contributes to improvement of fluidity, reduction in liquidus temperature, and the like when the aluminum alloy is molten, thereby to improve castability.
- the content ratio of Si with respect to the whole weight of the aluminum alloy is preferably within a range of 12.0 to 15.0 wt% as described above.
- the content ratio of Si is less than 12.0 wt%, melting temperature and casting temperature of the aluminum alloy increase, and sufficient fluidity cannot be ensured during die casting since fluidity of the aluminum alloy reduces when the aluminum alloy is molten.
- the content ratio of Si is more than 15.0 wt%, castability is degraded due to reduced fluidity and increased liquidus temperature.
- Mg manganesium mainly exists as Mg 2 Si or in a solid-solution state in an Al base material in the aluminum alloy, and is a component that provides yield strength and tensile strength to the aluminum alloy but, when being contained by an excessive amount, has an adverse effect on castability and corrosion resistance.
- the content ratio of Mg with respect to the whole weight of the aluminum alloy is preferably within a range not more than 1.00 wt% as described above.
- the presence of Mg within the above range can improve mechanical properties of the aluminum alloy such as yield strength and tensile strength, without greatly affecting corrosion resistance.
- the content ratio of Mg is more than 1.00 wt%, stretching of the alloy is reduced, which results in degraded quality of an aluminum alloy die cast produced by using the alloy.
- Fe iron
- Fe is known to have a seizing prevention effect during die casting.
- Fe causes crystallization of a needle like crystal in the form of Al-Si-Fe, reduces toughness of the aluminum alloy, and, when being added in a large quantity, causes melting at a suitable temperature to be difficult.
- the content ratio of Fe with respect to the whole weight of the aluminum alloy is preferably within a range of 0.05 to 1.00 wt% as described above.
- the content ratio of Fe is less than 0.05 wt%, the seizing prevention effect during die casting becomes insufficient, whereas when the content ratio of Fe is more than 1.00 wt%, although the seizing prevention effect becomes sufficient, toughness of the alloy reduces and the melting temperature rises to cause degradation of castability.
- Cr chromium mainly exists in a molten state when the aluminum alloy is molten, and when the aluminum alloy is solid, exists in a solid-solution state in an Al phase or in a crystallized state as a Cr based compound. Similar to Fe and Mn described above, Cr is used for preventing seizing of the aluminum alloy and a mold during die casting, and for improving corrosion resistance of the alloy.
- the content ratio of Cr with respect to the whole weight of the aluminum alloy is preferably within the range of 0.10 to 0.50 wt% as described above.
- the content ratio of Cr is less than 0.10 wt%, the effect of improving corrosion resistance of the alloy becomes insufficient, whereas when the content ratio of Cr is more than 0.50 wt%, although corrosion resistance becomes sufficient, liquidus temperature increases and fluidity reduces to cause degradation of castability.
- At least one element selected from Na (sodium), Sr (strontium), Ca (calcium), and Sb (antimony) may be added as a modification material.
- a modification material By adding such a modification material, it is possible to reduce the size of eutectic Si particles, and further improve toughness and strength of the aluminum alloy.
- the addition ratio of the modification material with respect to the whole weight of the aluminum alloy is preferably within a range of 30 to 200 ppm when the modification material is Na, Sr, and Ca, and within a range of 0.05 to 0.20 wt% when the modification material is Sb.
- the addition ratio of the modification material is less than 30 ppm (0.05 wt% in the case with Sb)
- miniaturizing eutectic Si particles in the aluminum alloy becomes difficult
- the addition ratio of the modification material is more than 200 ppm (0.20 wt% in the case with Sb)
- eutectic Si particles in the aluminum alloy are sufficiently miniaturized, and no further addition effect can be obtained even when the added amount is increased.
- At least one of Ti (titanium) and B (boron) may be added instead of or together with the modification material.
- Ti and B titanium
- crystal grains of the aluminum alloy are miniaturized, and stretching of the alloy can be improved. It should be noted that such an advantageous effect becomes significant when the amount of Si is particularly small or when a casting method having a low cooling rate is used.
- the addition ratios of Ti and B with respect to the whole weight of the aluminum alloy are preferably within a range of 0.05 to 0.30 wt% and a range of 1 to 50 ppm, respectively.
- the addition ratio of Ti is less than 0.05 wt% or the addition ratio of B is less than 1 ppm, miniaturizing the crystal grains in the aluminum alloy becomes difficult, whereas when the addition ratio of Ti is more than 0.30 wt% or the addition ratio of B is more than 50 ppm, the crystal grains in the aluminum alloy are sufficiently miniaturized, and no further addition effect can be obtained even when the added amount is increased.
- the aluminum alloy for die casting according to the present invention When the aluminum alloy for die casting according to the present invention is to be produced, first, a raw material designed to contain, at the predetermined ratio described above, each of the elemental components of Al, Cu, Si, Mg, Fe, and Cr is prepared. Next, the raw material is placed in a melting furnace such as a sealed melting furnace or a melting furnace with a fore hearth to melt the elemental components. The molten raw material, i.e., the molten metal of the aluminum alloy is subjected to refinement treatments such as a dehydrogenation treatment and an inclusion removal treatment, if necessary. Then, the refined molten metal is casted in a predetermined mold and solidified in order to form the molten metal of the aluminum alloy into an alloy base metal ingot or the like.
- a melting furnace such as a sealed melting furnace or a melting furnace with a fore hearth to melt the elemental components.
- the molten raw material i.e., the molten metal of the
- a solution treatment and an aging treatment, etc. are performed if necessary.
- a solution treatment and an aging treatment, etc. are performed if necessary.
- castability during die casting was evaluated by the following method, in addition to measuring liquidus temperature of the alloy. That is, the alloy ingot was molten, and a flow length of the solution was measured at a temperature 100°C higher than the alloy liquidus temperature.
- Table 1 shows the elemental compositions, salt spray measurement results, and mechanical properties of aluminum alloys, which are the objects of the present invention, in Examples 1 to 9 and Comparative Examples 1 to 9.
- Elemental composition (wt%) Salt spray test result (mg/dm 2 /day) Physical property measurement result Cu Si Mg Fe Cr Tensile strength (MPa) Stretching (%) 0.2%-yield strength (MPa)
- Example 1 0.01 12.17 0.01 0.21 0.19 1.4 257 2.8 138
- Example 2 0.01 12.36 0.21 0.20 0.19 0.9 283 3.3 147
- Example 3 0.01 12.43 0.42 0.21 0.19 1.1 288 2.9 155
- Example 4 0.01 12.50 0.62 0.21 0.19 1.2 295 2.3 176
- Example 5 0.01 12.39 0.98 0.21 0.19 1.0 296 1.6 206
- Example 6 0.00 12.46 0.22 0.15 0.40 0.8
- Example 7 0.00 12.56 0.23 0.43 0.40 0.8
- Example 8 0.00 12.56 0.21 0.45
- Table 2 shows the elemental compositions, liquidus temperatures, and flow lengths of aluminum alloys, which are the objects of the present invention, in Examples 10 to 14 and Comparative Examples 10 and 11.
- Elemental composition (wt%) Liquidus temperature (°C) Flow length (mm) Notes Cu Si Mg Fe Cr Example 10 0.00 12.27 0.00 0.20 0.19 581 492 Approximate to Example 1
- Example 11 0.00 12.38 0.19 0.21 0.20 582 494 Approximate to Example 2
- Example 12 0.00 12.40 0.39 0.21 0.20 582 483 Approximate to Example 3
- Example 13 0.00 12.54 0.59 0.21 0.21 584 482 Approximate to Example 4
- Example 14 0.00 12.38 0.95 0.22 0.20 585 445 Approximate to Example 5 Comparative Example 10 1.90 10.76 0.20 0.84 0.08 571 330
- Comparative Example 11 0.02 0.54 3.55 0.50 0.03 635 333
- ADC6 Elemental composition (wt%) Liquidus temperature (°C
- Examples 1 to 9 are compared with Comparative Example 2 corresponding to ADC12, it is found that the aluminum alloys of Examples 1 to 9 have corrosion resistances significantly higher than corrosion resistance of Comparative Example 2, and have mechanical properties approximately equal to mechanical properties of Comparative Example 2.
- liquidus temperatures of Examples 10 to 14 are significantly lower than liquidus temperature of Comparative Example 11 corresponding to ADC6, and are approximately equal to liquidus temperature of Comparative Example 10 corresponding to ADC12.
- flow lengths of Examples 10 to 14 are significantly longer than those of Comparative Examples 10 and 11. That is, the aluminum alloys of the Examples 10 to 14 are superior in castability during die casting to the aluminum alloys of Comparative Examples 10 to 11.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
- Continuous Casting (AREA)
- Moulds For Moulding Plastics Or The Like (AREA)
Claims (5)
- Aluminiumlegierungsdruckguss, der durch Druckgießen einer Aluminiumlegierung zum Druckgießen erlangt ist, aufweisend: höchstens 0,10 Gew.% Cu; 12,0 bis 15,0 Gew.% Si; höchstens 1,00 Gew.% Mg; 0,05 bis 1,00 Gew.% Fe; 0,10 bis 0,50 Gew.% Cr; und optional 0,05 bis 0,20 Gew.% Sb, 0,05 bis 0,30 Gew.% Ti, 1 bis 50 ppm B und/oder 30 bis 200 ppm von zumindest einem ausgewählt aus Na, Sr und Ca, wobei der Rest der Aluminiumlegierung Al und unvermeidbare Unreinheiten sind.
- Aluminiumlegierungsdruckguss gemäß Anspruch 1, umfassend 30 bis 200 ppm von zumindest einem ausgewählt aus Na, Sr und and Ca.
- Aluminiumlegierungsdruckguss gemäß Anspruch 1 oder 2, umfassend 0,05 bis 0,20 Gew.% Sb.
- Aluminiumlegierungsdruckguss gemäß einem der Ansprüche 1 bis 3, umfassend 0,05 bis 0,30 Gew.% Ti.
- Aluminiumlegierungsdruckguss gemäß einem der Ansprüche 1 bis 4, umfassend 1 bis 50 ppm B.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL14904322T PL3196323T3 (pl) | 2014-10-23 | 2014-12-15 | Produkt odlewany kokilowo ze stopu aluminium |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2014216640 | 2014-10-23 | ||
PCT/JP2014/006238 WO2016063320A1 (ja) | 2014-10-23 | 2014-12-15 | ダイカスト用アルミニウム合金およびこれを用いたアルミニウム合金ダイカスト |
Publications (3)
Publication Number | Publication Date |
---|---|
EP3196323A1 EP3196323A1 (de) | 2017-07-26 |
EP3196323A4 EP3196323A4 (de) | 2017-08-09 |
EP3196323B1 true EP3196323B1 (de) | 2019-02-06 |
Family
ID=55760396
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP14904322.6A Active EP3196323B1 (de) | 2014-10-23 | 2014-12-15 | Druckgussprodukt aus aluminiumlegierung |
Country Status (9)
Country | Link |
---|---|
US (1) | US20170314101A1 (de) |
EP (1) | EP3196323B1 (de) |
JP (1) | JP5969713B1 (de) |
KR (1) | KR101935243B1 (de) |
CN (1) | CN107075622A (de) |
MX (1) | MX2017004376A (de) |
MY (1) | MY179378A (de) |
PL (1) | PL3196323T3 (de) |
WO (1) | WO2016063320A1 (de) |
Families Citing this family (4)
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MY183152A (en) * | 2015-04-15 | 2021-02-16 | Daiki Aluminium Ind Co Ltd | Aluminum alloy for die casting, and aluminum alloy die cast produced using same |
CN107779695A (zh) * | 2017-11-01 | 2018-03-09 | 道然精密智造无锡有限公司 | 一种高流动耐腐蚀的无链自行车壳体制造方法 |
US20190185967A1 (en) * | 2017-12-18 | 2019-06-20 | GM Global Technology Operations LLC | Cast aluminum alloy for transmission clutch |
CN113564431B (zh) * | 2021-08-10 | 2022-04-08 | 广州立中锦山合金有限公司 | 一种轮毂用高强度铝合金及其制备方法 |
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JP4145454B2 (ja) * | 2000-01-18 | 2008-09-03 | 住友電気工業株式会社 | 耐摩耗性アルミニウム合金長尺体およびその製造方法 |
JP4191370B2 (ja) * | 2000-03-02 | 2008-12-03 | 株式会社大紀アルミニウム工業所 | 高熱伝導加圧鋳造用合金と該合金鋳物 |
JP2002105571A (ja) * | 2000-10-03 | 2002-04-10 | Ryoka Macs Corp | 熱伝導性に優れたヒートシンク用アルミニウム合金材 |
JP4413106B2 (ja) * | 2004-08-30 | 2010-02-10 | 三菱樹脂株式会社 | ヒートシンク用アルミニウム合金材及びその製造法 |
JP2007070716A (ja) * | 2005-09-09 | 2007-03-22 | Daiki Aluminium Industry Co Ltd | 加圧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 |
MY155638A (en) * | 2009-01-27 | 2015-11-13 | Daiki Aluminium Industry Co Ltd | An aluminum alloy for pressure casting and an alumium alloy cast made of the same |
WO2012101805A1 (ja) * | 2011-01-27 | 2012-08-02 | 日本軽金属株式会社 | 高電気抵抗アルミニウム合金 |
-
2014
- 2014-12-15 EP EP14904322.6A patent/EP3196323B1/de active Active
- 2014-12-15 JP JP2015558290A patent/JP5969713B1/ja active Active
- 2014-12-15 PL PL14904322T patent/PL3196323T3/pl unknown
- 2014-12-15 CN CN201480082837.3A patent/CN107075622A/zh active Pending
- 2014-12-15 MY MYPI2017701407A patent/MY179378A/en unknown
- 2014-12-15 WO PCT/JP2014/006238 patent/WO2016063320A1/ja active Application Filing
- 2014-12-15 KR KR1020177011719A patent/KR101935243B1/ko active IP Right Grant
- 2014-12-15 US US15/520,650 patent/US20170314101A1/en not_active Abandoned
- 2014-12-15 MX MX2017004376A patent/MX2017004376A/es unknown
Non-Patent Citations (1)
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Also Published As
Publication number | Publication date |
---|---|
US20170314101A1 (en) | 2017-11-02 |
KR20170063891A (ko) | 2017-06-08 |
MY179378A (en) | 2020-11-05 |
MX2017004376A (es) | 2018-01-30 |
JPWO2016063320A1 (ja) | 2017-04-27 |
WO2016063320A1 (ja) | 2016-04-28 |
EP3196323A1 (de) | 2017-07-26 |
PL3196323T3 (pl) | 2019-08-30 |
JP5969713B1 (ja) | 2016-08-17 |
KR101935243B1 (ko) | 2019-01-04 |
CN107075622A (zh) | 2017-08-18 |
EP3196323A4 (de) | 2017-08-09 |
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