EP3589766A1 - Alliages de moulage d'al-mg-si-mn-fe - Google Patents
Alliages de moulage d'al-mg-si-mn-feInfo
- Publication number
- EP3589766A1 EP3589766A1 EP19773328.0A EP19773328A EP3589766A1 EP 3589766 A1 EP3589766 A1 EP 3589766A1 EP 19773328 A EP19773328 A EP 19773328A EP 3589766 A1 EP3589766 A1 EP 3589766A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- aluminum casting
- casting alloy
- new aluminum
- alloys
- aluminum
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 249
- 239000000956 alloy Substances 0.000 title claims abstract description 249
- 238000005266 casting Methods 0.000 title claims abstract description 197
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 191
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 191
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 77
- 229910052742 iron Inorganic materials 0.000 claims abstract description 55
- 229910052748 manganese Inorganic materials 0.000 claims abstract description 47
- 229910052749 magnesium Inorganic materials 0.000 claims abstract description 41
- 239000012535 impurity Substances 0.000 claims abstract description 24
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 23
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 15
- 229910052720 vanadium Inorganic materials 0.000 claims abstract description 15
- 229910052712 strontium Inorganic materials 0.000 claims abstract description 14
- 229910052726 zirconium Inorganic materials 0.000 claims abstract description 14
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 29
- 239000010703 silicon Substances 0.000 claims description 29
- 238000005336 cracking Methods 0.000 claims description 26
- 150000001875 compounds Chemical class 0.000 claims description 17
- 230000035939 shock Effects 0.000 claims description 3
- 229910000838 Al alloy Inorganic materials 0.000 abstract description 7
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 61
- 239000011777 magnesium Substances 0.000 description 41
- 239000011572 manganese Substances 0.000 description 36
- 239000000203 mixture Substances 0.000 description 15
- 239000010936 titanium Substances 0.000 description 13
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 10
- 239000011651 chromium Substances 0.000 description 9
- 101100072002 Arabidopsis thaliana ICME gene Proteins 0.000 description 8
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 8
- 230000015572 biosynthetic process Effects 0.000 description 8
- 239000002245 particle Substances 0.000 description 5
- 238000005476 soldering Methods 0.000 description 5
- 230000007423 decrease Effects 0.000 description 4
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 3
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 3
- 229910052735 hafnium Inorganic materials 0.000 description 3
- VBJZVLUMGGDVMO-UHFFFAOYSA-N hafnium atom Chemical compound [Hf] VBJZVLUMGGDVMO-UHFFFAOYSA-N 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 229910052706 scandium Inorganic materials 0.000 description 3
- SIXSYDAISGFNSX-UHFFFAOYSA-N scandium atom Chemical compound [Sc] SIXSYDAISGFNSX-UHFFFAOYSA-N 0.000 description 3
- CIOAGBVUUVVLOB-UHFFFAOYSA-N strontium atom Chemical compound [Sr] CIOAGBVUUVVLOB-UHFFFAOYSA-N 0.000 description 3
- 230000008685 targeting Effects 0.000 description 3
- GPPXJZIENCGNKB-UHFFFAOYSA-N vanadium Chemical compound [V]#[V] GPPXJZIENCGNKB-UHFFFAOYSA-N 0.000 description 3
- 229910021365 Al-Mg-Si alloy Inorganic materials 0.000 description 2
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 2
- 230000006978 adaptation Effects 0.000 description 2
- 238000004512 die casting Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000000523 sample Substances 0.000 description 2
- 229910018125 Al-Si Inorganic materials 0.000 description 1
- 229910018520 Al—Si Inorganic materials 0.000 description 1
- 229910019752 Mg2Si Inorganic materials 0.000 description 1
- 229910000676 Si alloy Inorganic materials 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 230000005496 eutectics Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000007734 materials engineering Methods 0.000 description 1
- 238000010120 permanent mold casting Methods 0.000 description 1
- 239000011164 primary particle Substances 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 238000007670 refining Methods 0.000 description 1
- 229910000679 solder Inorganic materials 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 238000012360 testing method Methods 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
- C22C21/06—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
-
- 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
-
- 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
- C22F1/047—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with magnesium as the next major constituent
Definitions
- Aluminum alloys are useful in a variety of applications.
- Aluminum casting (foundry) alloys for instance, are used in dozen of industries, including, for instance, the automotive and consumer electronics industries.
- the present disclosure relates to new aluminum casting (foundry) alloys and associated products.
- the new aluminum casting alloys generally comprise (and in some instances consist of or consist essentially of) from 2.5 to 5.0 wt. % Mg, from 0.70 to 2.5 wt. % Si, where the weight ratio of magensium to silicon (Mg/Si) is from 1.7: 1 to 3.6: 1, from 0.40 to 1.5 wt. % Mn, from 0.10 to 0.60 wt. % Fe, optionally up to 0.15 wt. % Ti, optionally up to 0.10 wt. % Sr, and optionally up to 0.15 wt.
- Mg/Si magensium to silicon
- the new aluminum casting alloys may realize an improve combination of properties, such as an improved combination of two or more of strength, ductility, castability, die soldering resistance and quality index, among others.
- the new aluminum casting alloys generally include from 2.5 to 5.0 wt. % Mg. In one embodiment, a new aluminum casting alloy includes not greater than 4.75 wt. % Mg. In another embodiment, a new aluminum casting alloy includes not greater than 4.60 wt. % Mg. In one embodiment, anew aluminum casting alloy includes at least 2.75 wt. % Mg. In another embodiment, a new aluminum casting alloy includes at least 3.0 wt. % Mg.
- the new aluminum casting alloys generally include from 0.70 to 2.5 wt. % Si.
- a new aluminum casting alloy includes at least 0.80 wt. % Si.
- a new aluminum casting alloy includes at least 0.90 wt. % Si.
- a new aluminum casting alloy includes at least 0.95 wt. % Si.
- a new aluminum casting alloy includes at least 1.00 wt. % Si.
- a new aluminum casting alloy includes at least 1.05 wt. % Si.
- a new aluminum casting alloy includes at least 1.10 wt. % Si.
- a new aluminum casting alloy includes at least 1.15 wt.
- anew aluminum casting alloy includes at least 1.20 wt. % Si. In one embodiment, a new aluminum casting alloy includes not greater than 2.4 wt. % Si. In another embodiment, a new aluminum casting alloy includes not greater than 2.3 wt. % Si. In yet another embodiment, a new aluminum casting alloy includes not greater than 2.2 wt. % Si. In another embodiment, a new aluminum casting alloy includes not greater than 2.1 wt. % Si. In yet another embodiment, a new aluminum casting alloy includes not greater than 2.0 wt. % Si.
- the weight ratio of magensium to silicon in the new aluminum casting alloys is generally from 1.7: 1 to to 3.6: 1 (wt. % Mg / wt. % Si). In one embodiment, the weight ratio of magensium to silicon in the new aluminum casting alloy is at least 1.8: 1. In another embodiment, the weight ratio of magensium to silicon in the new aluminum casting alloy is at least 1.85: 1. In one embodiment, the weight ratio of magensium to silicon in the new aluminum casting alloy is not greater than 3.6: 1. In another embodiment, the weight ratio of magensium to silicon in the new aluminum casting alloy is not greater than 3.5: 1.
- a new aluminum casting alloy includes an amount of magnesiumn and silicon sufficient to facilitate production of a crack-free cast product (e.g., a crack-free high pressure die cast product).
- a crack-free product is a product sufficiently free of cracks so that it can be used for its intended purpose.
- a new aluminum casting alloy includes an amount of magnesiumn and silicon sufficient to realize a hot cracking tendency index (HCTI) of not greater than 0.30, such as any of the low HCTI values disclosed herein.
- HCTI hot cracking tendency index
- the new aluminum casting alloys generally include from 0.40 to 1.5 wt. % Mn.
- anew aluminum casting alloy includes at least 0.45 wt. % Mn.
- a new aluminum casting alloy includes at least 0.50 wt. % Mn.
- anew aluminum casting alloy includes at least 0.55 wt. % Mn.
- a new aluminum casting alloy includes at least 0.60 wt. % Mn.
- a new aluminum casting alloy includes not greater than 1.45 wt. % Mn.
- a new aluminum casting alloy includes not greater than 1.40 wt. % Mn.
- a new aluminum casting alloy includes not greater than 1.35 wt. % Mn. In another embodiment, a new aluminum casting alloy includes not greater than 1.30 wt. % Mn. In yet another embodiment, a new aluminum casting alloy includes not greater than 1.25 wt. % Mn. In another embodiment, a new aluminum casting alloy includes not greater than 1.20 wt. % Mn.
- the new aluminum casting alloys generally include from 0.10 to 0.60 wt. % Fe.
- a new aluminum casting alloy includes at least 0.12 wt. % Fe.
- a new aluminum casting alloy includes at least 0.15 wt. % Fe.
- anew aluminum casting alloy includes at least 0.20 wt. % Fe.
- a new aluminum casting alloy includes at least 0.25 wt. % Fe.
- a new aluminum casting alloy includes at least 0.30 wt. % Fe.
- a new aluminum casting alloy includes at least 0.35 wt. % Fe.
- a new aluminum casting alloy includes not greater than 0.55 wt. % Fe.
- a new aluminum casting alloy includes not greater than 0.50 wt. % Fe.
- a new aluminum casting alloy includes not greater than 0.45 wt. % Fe.
- a new aluminum casting alloy includes an amount of iron and manganse sufficient to facilitate formation of alpha phase particles while restricting formation of beta phase particles. In one embodiment, at least due to the iron content, a new aluminum casting alloy includes not greater than 0.012 wt. % of P-A15FeSi compounds. In another embodiment, anew aluminum casting alloy includes not greater than 0.010 wt. % of -Al5FeSi compounds. In yet another embodiment, a new aluminum casting alloy includes not greater than 0.008 wt. % of -Al5FeSi compounds. In another embodiment, a new aluminum casting alloy includes not greater than 0.006 wt. % of P-A15FeSi compounds.
- a new aluminum casting alloy includes not greater than 0.004 wt. % of P-A15FeSi compounds. In another embodiment, a new aluminum casting alloy includes not greater than 0.002 wt. % of P-A15FeSi compounds. In yet another embodiment, a new aluminum casting alloy includes not greater than 0.001 wt. % of P-A15FeSi compounds. In another embodiment, anew aluminum casting alloy includes not greater than 0.0005 wt. % of -Al5FeSi compounds.
- a new aluminum casting alloy may include an amount of magensium, silicon, manganese and iron sufficient to satisfy the following requirements:
- the new aluminum casting alloys may optionally include up to 0.15 wt. % Ti.
- a new aluminum casting alloy includes at least 0.01 wt. % Ti.
- a new aluminum casting alloy includes at least 0.03 wt. % Ti.
- a new aluminum casting alloy includes at least 0.05 wt. % Ti.
- a new aluminum casting alloy includes at least 0.07 wt. % Ti.
- a new aluminum casting alloy includes not greater than 0.13 wt. % Ti.
- a new aluminum casting alloy includes not greater than 0.115 wt. % Ti.
- a new aluminum casting alloy includes not greater than 0.10 wt.
- a new aluminum casting alloy include an amount of titanium sufficient to faciltiate grain refining while resticting / avoiding formation of primary titanium-containing particles.
- titanium is included in a new aluminum casting alloy as an impurity.
- the new aluminum casting alloys may optionally include up to 0.10 wt. % Sr.
- a new aluminum casting alloy includes an amount of strontium sufficient to faciltiate modification of the Mg 2 Si eutectic while resticting / avoiding formation of primary strontium-containing particles.
- a new aluminum casting alloy includes at least 0.005 wt. % Sr.
- a new aluminum casting alloy includes not greater than 0.08 wt. % Sr.
- a new aluminum casting alloy includes not greater than 0.05 wt. % Sr.
- strontium is included in a new aluminum casting alloy as an impurity.
- the new aluminum casting alloys may optionally include up to 0.15 wt. % of any of Zr, Sc, Hf, V, and Cr.
- anew aluminum casting alloy includes an amount of zirconiun, scandium, hafnium, vanadium, and/or chromium sufficient to facilitate solid solution strenghtening while resticting / avoiding formation of primary particles containing zirconium, scandium, hafnium, vanadium, and chromium.
- a new aluminum casting alloy includes at least 0.01 wt. % of any of Zr, Sc, Hf, V, and Cr.
- a new aluminum casting alloy includes at least 0.03 wt.
- a new aluminum casting alloy includes at least 0.05 wt. % of any of Zr, Sc, Hf, V, and Cr. In one embodiment, a new aluminum casting alloy includes not greater than 0.10 wt. % of any of Zr, Sc, Hf, V, and Cr.
- zirconium is included in a new aluminum casting alloy as an impurity.
- scandium is included in a new aluminum casting alloy as an impurity.
- hafnium is included in a new aluminum casting alloy as an impurity.
- vanadium is included in a new aluminum casting alloy as an impurity.
- chromium is included in a new aluminum casting alloy as an impurity.
- the balance of the new aluminum casting alloys is generally aluminum and unavoiable impurities.
- anew aluminum casting alloy comprises not greater than 0.30 wt. % of the unavoiable impurities, and wherein the new aluminum casting alloy comprises not greater than 0.10 wt. % of any one element of the unavoiable impurities.
- a new aluminum casting alloy comprises not greater than 0.15 wt. % of the unavoiable impurities, and wherein the new aluminum casting alloy comprises not greater than 0.05 wt. % of any one element of the unavoiable impurities.
- a new aluminum casting alloy comprises not greater than 0.10 wt. % of the unavoiable impurities, and wherein the new aluminum casting alloy comprises not greater than 0.03 wt. % of any one element of the unavoiable impurities.
- the new aluminum casting alloys may be cast using any suitable casting method.
- a new alumimum casting alloy is a direct chill cast as an ingot or billet.
- a new aluminum casting alloy is shape cast into a shape cast product (e.g., a complex shape cast product, such as a complex automotive compontent).
- the shape cast product is an automotive structural component.
- the shape cast product is a door frame.
- the shape cast product is a shock tower.
- the shape cast product is a tunnel structure for an automobile.
- the shape casting comproses high pressure die casting. In another embodiment, the shape casting comprises permanent mold casting.
- the new aluminum casting alloys do not require a solution heat treatment step.
- the new aluminum casting alloys may be provided, therefore, in the appopriate temper, such as in the F temper or the T5 temper.
- the new aluminum casting alloys may realize an improved combination of properties, such as an improved combination of at least two of strength, ductility, castability, die soldering resistance and quality index.
- Mechanical properties may be measured in accordance with ASTM E8 and B557 (e.g., when directionally solidified). Castability may be measured using the HCTI method described herein. Die soldering resistance may be determined by casting the alloy.
- a new aluminum casting alloy realizes an ultimate tensile strength of at least 200 MPa. In another enbodiment, a new aluminum casting alloy realizes an ultimate tensile strength of at least 210 MPa. In yet another enbodiment, a new aluminum casting alloy realizes an ultimate tensile strength of at least 220 MPa. In another enbodiment, a new aluminum casting alloy realizes an ultimate tensile strength of at least 230 MPa.
- a new aluminum casting alloy realizes a tensile yield strength of at least 100 MPa. In another enbodiment, a new aluminum casting alloy realizes an tensile yield strength of at least 105 MPa. In yet another enbodiment, a new aluminum casting alloy realizes an tensile yield strength of at least 110 MPa. In another enbodiment, a new aluminum casting alloy realizes an tensile yield strength of at least 115 MPa. In another enbodiment, a new aluminum casting alloy realizes an tensile yield strength of at least 120 MPa. In another enbodiment, a new aluminum casting alloy realizes an tensile yield strength of at least 125 MPa. Any of the above tensile yield strength values may be realized with any of the above ultimate tensile strength values.
- anew aluminum casting alloy realizes an elongation of at least 7%. In another embodiment, a new aluminum casting alloy realizes an elongation of at least 8%. In yet another embodiment, a new aluminum casting alloy realizes an elongation of at least 9%. In another embodiment, a new aluminum casting alloy realizes an elongation of at least 10%. In yet another embodiment, a new aluminum casting alloy realizes an elongation of at least 11%. In another embodiment, a new aluminum casting alloy realizes an elongation of at least 12%. In yet another embodiment, a new aluminum casting alloy realizes an elongation of at least 13%. In another embodiment, a new aluminum casting alloy realizes an elongation of at least 14%.
- a new aluminum casting alloy realizes an elongation of at least 15%. In another embodiment, a new aluminum casting alloy realizes an elongation of at least 16%, or higher. Any of the above elongation values may be realized with any of the above ultimate tensile strength or tensile yield strength values.
- a new aluminum casting alloy realizes a HCTI of not greater than 0.30. In another embodiment, a new aluminum casting alloy realizes a HCTI of not greater than 0.25. In yet another embodiment, a new aluminum casting alloy realizes a HCTI of not greater than 0.20. In another embodiment, a new aluminum casting alloy realizes a HCTI of not greater than 0.15, or lower.
- a new aluminum casting alloy is die soldering resistant wherein the as-cast aluminum alloy product is removed from the die without damage to the cast product and/or without sticking to the die. Die soldering can occur during high pressure die casting wherein molten aluminum solders to the die surface. In some embodiments, the new aluminum casting alloys described herein may be cast without being soldered to the die.
- FIG. 1 is a graph showing silicon content versus hot cracking tendency index for Example 1 alloys.
- FIG. 2 is a graph showing silicon content versus hot cracking tendency index for Example 2 alloys.
- FIG. 3 is a graph showing silicon content versus hot cracking tendency index for Example 3 alloys.
- FIG. 4 is a graph showing manganese content versus hot cracking tendency index for Example 4 alloys.
- FIG. 5a is a graph showing beta phase content (shown in wt. %) as a function of Mn and Fe content based on ICME modeling; the amounts of 3.6 wt. % Mg and 1.5 wt % Si were kept constant.
- FIG. 5b is a graph showing alpha phase content (shown in wt. %) as a function of Mn and Fe content based on ICME modeling; the amounts of 3.6 wt. % Mg and 1.5 wt % Si were kept constant.
- FIG. 6 is a graph showing beta phase content (shown in wt. %) as a function of Fe content based on ICME modeling; the amounts of 3.6 wt. % Mg, 1.5 wt % Si and 0.5 wt. % Mn were kept constant.
- FIG. 7a is a graph showing ultimate tensile strength (MPa) versus iron content (wt. %) for Example 6 alloys.
- FIG. 7b is a graph showing elongtion (%) versus iron content (wt. %) for Example 6 alloys.
- FIG. 7c is a graph showing tensile yield strength (MPa) versus iron content (wt. %) for Example 6 alloys.
- FIG. 7d is a graph showing quality index (Q in MPa) versus iron content (wt. %) for Example 6 alloys.
- FIG. 8a is a graph showing HCI (computed hot cracking index) as a function of Si and Mg content based on ICME modeling; the amounts of 0.70 wt. % Mn and 0.25 wt. % Fe were kept constant.
- FIG. 8b is a graph showing non-equilibrium solidificaiton temperature range (in °C) as a function of Si and Mg content based on ICME modeling; the amounts of 0.70 wt. % Mn and 0.25 wt. % Fe were kept constant.
- FIG. 8c is a graph showing showing HCI (computed hot cracking index) as a function of Si and Mn content based on ICME modeling; the amounts of 4.0 wt. % Mg and 0.25 wt. % Fe were kept constant.
- FIG. 8d is a graph showing showing HCI (computed hot cracking index) as a function of Si and Fe content based on ICME modeling; the amounts of 4.0 wt. % Mg and 0.70 wt. % Mn were kept constant.
- Table 2 Five tests per alloy were conducted and at various connection sizes. Table 2, below, provides the hot cracking results. In the below table,“C” means cracked during casting,“OK” means casting was successful without cracking, and“NF” means the pencil probe mold was not completely filled.
- the hot cracking tendency index (“HCTI”) of each alloy was calculated in accordance with the results. Table 2 also lists the calculated HCTI for each alloy.
- the hot cracking tendency index (HCTI) of an alloy is defined as
- the HCTI value will be 0. If cracking is found in all 7 connection rods (from 4 mm to 16 mm), the HCTI value will be 1. Therefore, a smaller HCTI indicates a higher hot cracking resistance for a specific alloy.
- FIG. 1 shows a plot of the silicon content versus the determined HCTI value.
- alloys having from about 1 to about 2 wt. % Si at similar amounts of Fe, Mn, Mg and Ti realized improved hot cracking resistance.
- the Mg/Si ratio for these alloys is from about 2.0 to 3.0.
- Alloy A4 with 1.56 wt. % Si had a Mg to Si ratio of 2.26.
- Example 2 [0044] Four additional alloys were cast and their hot cracking susceptibility was determined, as per Example 1. Like Example 1, the silicon content was again varied, but using a lower nominal amount of magnesium and manganese. The compositions of the Example 2 alloys are shown in Table 3, below. The HCTI results for the Example 2 alloys are shown in the below figure. Alloy B2 showed the best hot cracking resistance. The Mg/Si ratio for this alloy is about 2.65.
- FIG. 2 shows the experimental measured hot cracking tendency indexes of the Al- 2.5Mg-l. lMn-x%Si alloys. Alloy B2, with 0.96 wt. % Si and 2.54 wt. % Mg, showed the best hot cracking resistance. The Mg/Si ratio for this alloy is about 2.65.
- Example 3 The compositions of the Example 3 alloys are shown in Table 4, below.
- the HCTI results for the Example 3 alloys are shown in FIG. 3. As shown, the HCTI for all alloys is generally good. The lowest HCTI was realized by alloy C3 with a Mg/Si ratio of 2.22.
- the Mg/Si weight ratio
- the Mg/Si should be from about 1.7 to about 3.6, preferably from about 2.0 to about 3.0 to facilitate hot cracking resistance.
- Example 4 Four additional alloys were cast and their hot cracking susceptibility was determined, as per Example 1. This time, the manganese content was varied, targeting a nominal magnesium amount of 3.6 wt. % and a nominal silicon amount of 1.5 wt. %.
- the compositions of the Example 4 alloys are shown in Table 5, below.
- the HCTI results for the Example 4 alloys are shown in FIG. 4. As shown, the HCTI for all alloys is generally good. Alloy D4 with 1.20 wt. % Mn realized the best HCTI results.
- Example 5 The compositions of the Example 5 alloys are shown in Table 6, below.
- the HCTI results for the Example 5 alloys are shown in the below figure. As shown, the HCTI for all alloys is generally good. Alloy E4 with 0.29 wt. % Fe realized the best HCTI results.
- FIGS. 5a, 5b and 6 show the correlation between manganese and iron content and the volume fraction on b-AEFeSi and a- AhsFeM SE phase particles (for a Al-3.6Mg-l.5Si alloys).
- Adding Mn to the Al-Mg-Si alloys can promote formation of a-AhsFeM SE phase and restrict or prevent formation of b- AEFeSi phase.
- a Al-3.6Mg-l.5Si alloy with from 0.4 to 0.6 wt. % Mn using increased iron amounts decreases the amount of b-AEFeSi phase.
- the amount of b-AEFeSi phase decreases from about 0.018 wt. % to essentially 0 wt. % by increasing iron from 0.15 wt. % to 0.4 wt. %.
- alloys having improved properties e.g., elongation
- the first group (F) targeted a nominal magnesium amount of 3.6 wt. %, a nominal silicon amount of 1.5 wt. %, and a nominal manganese amount of 0.90 wt. %.
- the second group (G) targeted a nominal magnesium amount of 4.0 wt. %, a nominal silicon amount of 1.7 wt. %, and a nominal manganese amount of 0.65 wt. %.
- the compositions of the Example 6 alloys are shown in Table 7, below.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Continuous Casting (AREA)
- Refinement Of Pig-Iron, Manufacture Of Cast Iron, And Steel Manufacture Other Than In Revolving Furnaces (AREA)
- Mold Materials And Core Materials (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
Abstract
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP23175753.5A EP4234123A3 (fr) | 2018-05-07 | 2019-05-06 | Alliages de moulage d'al-mg-si-mn-fe |
Applications Claiming Priority (2)
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US201862667930P | 2018-05-07 | 2018-05-07 | |
PCT/US2019/030924 WO2019217319A1 (fr) | 2018-05-07 | 2019-05-06 | Alliages de moulage d'al-mg-si-mn-fe |
Related Child Applications (1)
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EP23175753.5A Division EP4234123A3 (fr) | 2018-05-07 | 2019-05-06 | Alliages de moulage d'al-mg-si-mn-fe |
Publications (3)
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---|---|
EP3589766A1 true EP3589766A1 (fr) | 2020-01-08 |
EP3589766A4 EP3589766A4 (fr) | 2020-09-02 |
EP3589766B1 EP3589766B1 (fr) | 2023-06-28 |
Family
ID=68466843
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
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EP23175753.5A Withdrawn EP4234123A3 (fr) | 2018-05-07 | 2019-05-06 | Alliages de moulage d'al-mg-si-mn-fe |
EP19773328.0A Active EP3589766B1 (fr) | 2018-05-07 | 2019-05-06 | Alliages de moulage d'al-mg-si-mn-fe |
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EP23175753.5A Withdrawn EP4234123A3 (fr) | 2018-05-07 | 2019-05-06 | Alliages de moulage d'al-mg-si-mn-fe |
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US (1) | US20190352745A1 (fr) |
EP (2) | EP4234123A3 (fr) |
JP (1) | JP7438134B2 (fr) |
KR (1) | KR20200140917A (fr) |
CN (1) | CN110603341A (fr) |
CA (1) | CA3099043A1 (fr) |
DE (1) | DE202019105466U1 (fr) |
ES (1) | ES2949017T3 (fr) |
MX (1) | MX2020011679A (fr) |
PL (1) | PL3589766T3 (fr) |
WO (1) | WO2019217319A1 (fr) |
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KR102441402B1 (ko) | 2016-11-16 | 2022-09-07 | 현대자동차주식회사 | 버스시트의 슬라이딩장치 |
Family Cites Families (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1384264A (en) | 1972-02-09 | 1975-02-19 | Honsel Werke Ag | Structural parts produced from aluminium-containing alloys |
JPS60245759A (ja) * | 1984-05-21 | 1985-12-05 | Nippon Light Metal Co Ltd | 鋳物用アルミニウム合金 |
CH689143A5 (de) * | 1994-06-16 | 1998-10-30 | Rheinfelden Aluminium Gmbh | Aluminium-Silizium Druckgusslegierung mit hoher Korrosionsbestaendigkeit, insbesondere fuer Sicherheitsbauteile. |
JP2002105611A (ja) | 2000-09-26 | 2002-04-10 | Ahresty Corp | ダイカスト鋳造による自動車部品の製造方法 |
JP3724362B2 (ja) | 2000-11-02 | 2005-12-07 | 日本軽金属株式会社 | ダイカスト用アルミニウム合金 |
FR2827306B1 (fr) * | 2001-07-10 | 2004-10-22 | Pechiney Aluminium | Alliage d'aluminium a haute ductilite pour coulee sous pression |
US20030143102A1 (en) * | 2001-07-25 | 2003-07-31 | Showa Denko K.K. | Aluminum alloy excellent in cutting ability, aluminum alloy materials and manufacturing method thereof |
US20050199318A1 (en) * | 2003-06-24 | 2005-09-15 | Doty Herbert W. | Castable aluminum alloy |
JP2009108409A (ja) * | 2007-10-12 | 2009-05-21 | Hitachi Metals Ltd | 靭性に優れた鋳造用Al−Mg系アルミニウム合金及びそれからなる鋳造部材 |
JP5355320B2 (ja) * | 2009-09-10 | 2013-11-27 | 日産自動車株式会社 | アルミニウム合金鋳物部材及びその製造方法 |
JP5368968B2 (ja) | 2009-12-28 | 2013-12-18 | 株式会社神戸製鋼所 | ヒートインシュレータ用アルミニウム合金板およびその製造方法 |
EP2471967B1 (fr) * | 2010-12-28 | 2014-07-09 | Casa Maristas Azterlan | Procédé pour obtenir des propriétés mécaniques améliorées dans des moulages d'aluminium recyclés dépourvus de phases bêta en forme de plaquettes |
AT511397B1 (de) * | 2011-05-03 | 2013-02-15 | Sag Motion Ag | Verfahren zur raffination und gefügemodifikation von aimgsi-legierungen |
JP5882380B2 (ja) | 2013-04-09 | 2016-03-09 | 株式会社神戸製鋼所 | プレス成形用アルミニウム合金板の製造方法 |
JP6229130B2 (ja) | 2013-10-08 | 2017-11-15 | 国立大学法人富山大学 | 鋳造用アルミニウム合金及びそれを用いた鋳物 |
WO2015085433A1 (fr) * | 2013-12-13 | 2015-06-18 | Rio Tinto Alcan International Limited | Alliage de coulée à base d'aluminium doté de performances améliorées à haute température |
WO2017210916A1 (fr) | 2016-06-10 | 2017-12-14 | GM Global Technology Operations LLC | Alliage à base d'aluminium contenant du magnésium pour pièces coulées à paroi mince |
CN106191572B (zh) * | 2016-06-29 | 2018-03-09 | 余姚市弘顺机械有限公司 | 一种汽车配件用铝合金和汽车配件的压铸方法 |
JP6836266B2 (ja) | 2016-12-27 | 2021-02-24 | 学校法人常翔学園 | Al−Mg−Si系アルミニウム合金鋳造板およびその製造方法 |
-
2019
- 2019-05-06 KR KR1020207034302A patent/KR20200140917A/ko not_active Application Discontinuation
- 2019-05-06 CA CA3099043A patent/CA3099043A1/fr active Pending
- 2019-05-06 EP EP23175753.5A patent/EP4234123A3/fr not_active Withdrawn
- 2019-05-06 PL PL19773328.0T patent/PL3589766T3/pl unknown
- 2019-05-06 DE DE202019105466.2U patent/DE202019105466U1/de active Active
- 2019-05-06 ES ES19773328T patent/ES2949017T3/es active Active
- 2019-05-06 MX MX2020011679A patent/MX2020011679A/es unknown
- 2019-05-06 EP EP19773328.0A patent/EP3589766B1/fr active Active
- 2019-05-06 CN CN201980002032.6A patent/CN110603341A/zh active Pending
- 2019-05-06 JP JP2020561716A patent/JP7438134B2/ja active Active
- 2019-05-06 WO PCT/US2019/030924 patent/WO2019217319A1/fr unknown
- 2019-05-07 US US16/405,061 patent/US20190352745A1/en active Pending
Also Published As
Publication number | Publication date |
---|---|
EP4234123A3 (fr) | 2023-09-27 |
MX2020011679A (es) | 2020-12-10 |
ES2949017T3 (es) | 2023-09-25 |
DE202019105466U1 (de) | 2020-01-13 |
KR20200140917A (ko) | 2020-12-16 |
CN110603341A (zh) | 2019-12-20 |
US20190352745A1 (en) | 2019-11-21 |
EP3589766A4 (fr) | 2020-09-02 |
JP7438134B2 (ja) | 2024-02-26 |
JP2021523291A (ja) | 2021-09-02 |
EP3589766B1 (fr) | 2023-06-28 |
WO2019217319A1 (fr) | 2019-11-14 |
CA3099043A1 (fr) | 2019-11-14 |
PL3589766T3 (pl) | 2023-07-31 |
EP4234123A2 (fr) | 2023-08-30 |
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