KR20050081168A - Casting of an aluminium alloy - Google Patents
Casting of an aluminium alloy Download PDFInfo
- Publication number
- KR20050081168A KR20050081168A KR1020050005296A KR20050005296A KR20050081168A KR 20050081168 A KR20050081168 A KR 20050081168A KR 1020050005296 A KR1020050005296 A KR 1020050005296A KR 20050005296 A KR20050005296 A KR 20050005296A KR 20050081168 A KR20050081168 A KR 20050081168A
- Authority
- KR
- South Korea
- Prior art keywords
- weight
- casting
- alloy
- casting according
- alloy comprises
- 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.)
- Withdrawn
Links
- 238000005266 casting Methods 0.000 title claims abstract description 26
- 229910000838 Al alloy Inorganic materials 0.000 title claims description 7
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 37
- 239000000956 alloy Substances 0.000 claims abstract description 37
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 9
- 239000011651 chromium Substances 0.000 claims abstract description 7
- 239000010949 copper Substances 0.000 claims abstract description 7
- 239000011777 magnesium Substances 0.000 claims abstract description 7
- 239000010936 titanium Substances 0.000 claims abstract description 7
- 229910052749 magnesium Inorganic materials 0.000 claims abstract description 6
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 5
- 229910052802 copper Inorganic materials 0.000 claims abstract description 5
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 5
- 229910052726 zirconium Inorganic materials 0.000 claims abstract description 5
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims abstract description 4
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims abstract description 4
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims abstract description 4
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims abstract description 4
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims abstract description 4
- 229910052790 beryllium Inorganic materials 0.000 claims abstract description 4
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 claims abstract description 4
- 239000012535 impurity Substances 0.000 claims abstract description 4
- 229910052742 iron Inorganic materials 0.000 claims abstract description 4
- 239000010703 silicon Substances 0.000 claims abstract description 4
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 4
- 229910052720 vanadium Inorganic materials 0.000 claims abstract description 4
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims abstract description 4
- 239000011701 zinc Substances 0.000 claims abstract description 4
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims abstract description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 3
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 3
- 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 claims abstract description 3
- 229910052725 zinc Inorganic materials 0.000 claims abstract description 3
- 239000011572 manganese Substances 0.000 claims description 5
- 238000004519 manufacturing process Methods 0.000 claims description 4
- 229910000968 Chilled casting Inorganic materials 0.000 claims description 3
- 238000007528 sand casting Methods 0.000 claims description 3
- 230000002349 favourable effect Effects 0.000 claims 1
- 230000000052 comparative effect Effects 0.000 description 4
- 238000004512 die casting Methods 0.000 description 4
- 239000000203 mixture Substances 0.000 description 4
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- CSDREXVUYHZDNP-UHFFFAOYSA-N alumanylidynesilicon Chemical compound [Al].[Si] CSDREXVUYHZDNP-UHFFFAOYSA-N 0.000 description 2
- 238000001723 curing Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000005242 forging Methods 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 229910052748 manganese Inorganic materials 0.000 description 2
- 238000009716 squeeze casting Methods 0.000 description 2
- 230000002459 sustained effect Effects 0.000 description 2
- 229910000789 Aluminium-silicon alloy Inorganic materials 0.000 description 1
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 238000000137 annealing Methods 0.000 description 1
- 238000000889 atomisation Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000013007 heat curing Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 238000007670 refining Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 230000008646 thermal stress Effects 0.000 description 1
- 238000010117 thixocasting Methods 0.000 description 1
Classifications
-
- A—HUMAN NECESSITIES
- A47—FURNITURE; DOMESTIC ARTICLES OR APPLIANCES; COFFEE MILLS; SPICE MILLS; SUCTION CLEANERS IN GENERAL
- A47K—SANITARY EQUIPMENT NOT OTHERWISE PROVIDED FOR; TOILET ACCESSORIES
- A47K10/00—Body-drying implements; Toilet paper; Holders therefor
- A47K10/24—Towel dispensers, e.g. for piled-up or folded textile towels; Toilet paper dispensers; Dispensers for piled-up or folded textile towels provided or not with devices for taking-up soiled towels as far as not mechanically driven
- A47K10/32—Dispensers for paper towels or toilet paper
- A47K10/34—Dispensers for paper towels or toilet paper dispensing from a web, e.g. with mechanical dispensing means
- A47K10/38—Dispensers for paper towels or toilet paper dispensing from a web, e.g. with mechanical dispensing means the web being rolled up with or without tearing edge
- A47K10/3809—Dispensers for paper towels or toilet paper dispensing from a web, e.g. with mechanical dispensing means the web being rolled up with or without tearing edge with roll spindles which are not directly supported
- A47K10/3827—Dispensers for paper towels or toilet paper dispensing from a web, e.g. with mechanical dispensing means the web being rolled up with or without tearing edge with roll spindles which are not directly supported with a distribution opening which is parallel to the rotation axis
-
- 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
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Public Health (AREA)
- Health & Medical Sciences (AREA)
- Body Structure For Vehicles (AREA)
- Continuous Casting (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
- Secondary Cells (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
- Superconductors And Manufacturing Methods Therefor (AREA)
- Conductive Materials (AREA)
- Cookers (AREA)
- Compressor (AREA)
- Refinement Of Pig-Iron, Manufacture Of Cast Iron, And Steel Manufacture Other Than In Revolving Furnaces (AREA)
- Casings For Electric Apparatus (AREA)
Abstract
다음 성분의 합금으로 구성된 양호한 내열성을 갖는 주물.Castings with good heat resistance consisting of alloys of the following components:
2-4 중량%의 마그네슘,2-4% by weight magnesium,
0.9-1.5 중량%의 규소,0.9-1.5 weight percent silicon,
0.1-0.4 중량%의 망간,0.1-0.4% by weight manganese,
0.1-0.4 중량%의 크롬,0.1-0.4% by weight of chromium,
최대 0.2 중량%의 철,Up to 0.2% by weight of iron,
최대 0.1 중량%의 구리,Up to 0.1% by weight of copper,
최대 0.2 중량%의 아연,Up to 0.2% by weight of zinc,
최대 0.2 중량%의 티타늄,Up to 0.2 wt% titanium,
최대 0.3 중량%의 지르코늄,Up to 0.3% zirconium,
최대 0.008 중량%의 베릴륨,Up to 0.008% beryllium,
최대 0.5 중량%의 바나듐, 및Vanadium up to 0.5% by weight, and
각각이 최대 0.02 중량%을 이루지만 전체가 0.2 중량%를 넘지않은 기타 성분과 생산유발불순물, 및 나머지의 알루미늄.Other components and impurities which produce up to 0.02% by weight but not more than 0.2% by weight in total, and the remainder of aluminum.
Description
본 발명은 양호한 내열성을 갖는 알루미늄합금의 주물에 관한 것이다.The present invention relates to a casting of an aluminum alloy having good heat resistance.
오늘날 열적 응력을 받는 부품에 대해서는 통상적으로 AlSi 합금이 사용되며, 이러한 합금에 Cu를 첨가함으로써 내열성을 얻는다. 그러나 구리는 열크랙 성향을 증가시키고 주조성에 대하여 좋지 않은 영향을 준다. 특히 내열성이 요구되는 분야로는 자동차의 실린더 헤드분야가 있다. 예로서, F.J.Feikus, "Optimisation of Aluminium Silicon Casting Alloys for Cylinder Heads". Giesserei-Praxis 1999, Vol.2, pages 50-57를 참조하기 바란다.AlSi alloys are commonly used for today's thermally stressed parts, and heat resistance is obtained by adding Cu to these alloys. However, copper increases the heat crack propensity and adversely affects castability. In particular, an area where heat resistance is required is an automobile cylinder head field. See, eg, F. J. Feikus, "Optimisation of Aluminum Silicon Casting Alloys for Cylinder Heads". See Giesserei-Praxis 1999, Vol. 2, pages 50-57.
특허문헌 WO-A-0043560에는 다이캐스팅, 스퀴즈(squeeze) 캐스팅, 틱소포밍(thixoforming) 및 틱소포징(thixoforging) 공정으로 안전부품을 생산하기 위한 알루미늄합금으로서, 2.5-7.0 중량%의 Mg, 1.0-3.0 중량%의 Si, 0.3-0.49 중량%의 Mn, 0.1-0.3 중량%의 Cr, 최대 0.15 중량%의 Fe, 최대 0.00005 중량%의 Ca, 최대 0.00005 중량%의 Na, 최대 0.0002 중량%의 P, 및 각각이 최대 0.02 중량%를 갖는 기타 성분의 불순물과 나머지는 알루미늄으로 이루어진 알루미늄합금이 기술되어 있다.Patent document WO-A-0043560 discloses an aluminum alloy for the production of safety parts by die casting, squeeze casting, thixoforming and thixoforging processes. Wt% Si, 0.3-0.49 wt% Mn, 0.1-0.3 wt% Cr, up to 0.15 wt% Fe, up to 0.00005 wt% Ca, up to 0.00005 wt% Na, up to 0.0002 wt% P, and Impurities of other components, each having a maximum of 0.02% by weight, and an aluminum alloy consisting of the remainder are described.
본 발명은 열적응력을 받는 부품의 제조에 적합한 것으로, 양호한 내열성을 갖는 알루미늄합금을 제공하는데 그 목적이 있다. 이 합금은 특히 중력다이캐스팅, 저압칠드캐스팅 및 샌드캐스팅에 적합하다. The present invention is suitable for the production of parts subjected to thermal stress, and an object thereof is to provide an aluminum alloy having good heat resistance. This alloy is particularly suitable for gravity die casting, low pressure chilled casting and sand casting.
상기 합금으로 주조되는 부품은 높은 연성과 관련하여 고강도를 가져야 한다. 이러한 부품의 바람직한 기계적인 특성은 다음과 같이 정의된다.Parts cast from the alloy should have high strength with respect to high ductility. Preferred mechanical properties of these parts are defined as follows.
항복강도 Rp0.2 > 170MPaYield strength Rp0.2> 170 MPa
인장강도 Rm > 230MPaTensile Strength Rm> 230 MPa
파단 연신율 A5 > 6%Elongation at break A5> 6%
이러한 합금이 사용되는 분야의 특수성 때문에, 이 합금은 부식성이 가능한 한 낮게 유지되어야 하며, 양호한 피로강도를 가져야 한다. 합금의 주조성은 현재 이용되고 있는 AlSiCu 주조합금보다 양호하여야 하고 열 크랙(heat cracks)이 발생되지 않아야 한다. Because of the specificity of the field in which these alloys are used, these alloys should be kept as low as corrosive and have good fatigue strength. The castability of the alloy should be better than the AlSiCu main alloys currently in use and no heat cracks would be generated.
본 발명에서 "주물"이라 함은 주조로서만 제조되는 순수 주물과, 예비성형된 주물, 및 냉간이나 열간 성형으로 최종 칫수로 성형된 제품을 포함한다. In the present invention, the term "casting" includes pure castings which are produced only by casting, preformed castings, and products molded into final dimensions by cold or hot forming.
순수 주물의 예로서는 샌드캐스팅, 중력다이캐스팅, 저압칠드캐스팅, 다이캐스팅, 틱소캐스팅 또는 스퀴즈캐스팅으로 제조되는 것이 있다. Examples of pure castings are sand casting, gravity die casting, low pressure chilled casting, die casting, thixocasting or squeeze casting.
세이핑(shaping)에 의하여 예비성형된 주물에서 수행되는 성형작업으로는 단조와 반용융단조가 있다. Molding operations performed in castings preformed by shaping include forging and semi-melting forging.
본 발명에 따른 목적은 다음의 조성을 갖는 알루미늄합금에 의하여 달성된다.The object according to the invention is achieved by an aluminum alloy having the following composition.
2-4 중량%의 마그네슘,2-4% by weight magnesium,
0.9-1.5 중량%의 규소,0.9-1.5 weight percent silicon,
0.1-0.4 중량%의 망간,0.1-0.4% by weight manganese,
0.1-0.4 중량%의 크롬,0.1-0.4% by weight of chromium,
최대 0.2 중량%의 철,Up to 0.2% by weight of iron,
최대 0.1 중량%의 구리,Up to 0.1% by weight of copper,
최대 0.2 중량%의 아연,Up to 0.2% by weight of zinc,
최대 0.2 중량%의 티타늄,Up to 0.2 wt% titanium,
최대 0.3 중량%의 지르코늄,Up to 0.3% zirconium,
최대 0.008 중량%의 베릴륨,Up to 0.008% beryllium,
최대 0.5 중량%의 바나듐,Vanadium up to 0.5% by weight,
각각이 최대 0.02 중량%를 이루지만 전체가 0.2 중량%을 넘지않은 기타 성분과 생산유발불순물, 및 나머지의 알루미늄.Other components, production impurities, and the remainder of aluminum, each up to 0.02% by weight but not more than 0.2% by weight in total.
각 합금원소는 다음의 조성범위를 갖는 것이 바람직하다.Each alloy element preferably has the following composition range.
Mg 2.5-3.5 중량%, 특히 2.7-3.3 중량%,Mg 2.5-3.5 wt%, especially 2.7-3.3 wt%,
Si 0.9-1.3 중량%,Si 0.9-1.3 wt%,
Mn 0.15-0.3 중량%,Mn 0.15-0.3 wt%,
Cr 0.15-0.3 중량%,Cr 0.15-0.3 wt%,
Ti 0.05-0.15 중량%,Ti 0.05-0.15 wt%,
Fe 최대 0.15 중량%,Fe max 0.15% by weight,
Cu 최대 0.05 중량%,Up to 0.05 wt% Cu,
Be 0.002-0.005 중량%,Be 0.002-0.005 wt%,
V 0.01-0.1 중량%, 및V 0.01-0.1 wt%, and
Zr 0.1-0.2 중량%.Zr 0.1-0.2 wt%.
합금원소의 효과는 다음과 같다.The effect of the alloying element is as follows.
마그네슘과 결합된 규소는 특히, 열경화가 요구되는 경우에 경화가 이루어질 수 있도록 한다. 예를 들어, T6 상태로 열처리 하는 경우, 즉 550℃에서 12시간 어 닐링을 행하고 160-170℃에서 8 내지 10시간 동안 인공시효를 행할 경우에 적합하다.Silicon combined with magnesium allows the curing to take place, especially when heat curing is required. For example, it is suitable for heat treatment in a T6 state, that is, annealing at 550 ° C. for 12 hours and artificial aging at 160-170 ° C. for 8 to 10 hours.
망간과 크롬의 조합은 180℃까지의 지속온도에서 양호한 내열성을 갖게 한다.The combination of manganese and chromium gives good heat resistance at sustained temperatures up to 180 ° C.
티타늄과 지르코늄은 미립화(grain refining)를 위하여 사용된다. 양호한 미립화는 실질적으로 주조성의 개선에 기여한다.Titanium and zirconium are used for grain refining. Good atomization substantially contributes to the improvement of castability.
바나듐과 함께 베릴륨은 드로스(dross)의 형성을 줄여준다.Beryllium together with vanadium reduces the formation of dross.
본 발명에 따른 주물의 응용분야는 열적인 응력을 받는 부품, 특히 압력용기, 콤프레샤 하우징, 및 자동차의 실린더 헤드와 같은 엔진부품 등이 포함된다.Applications of the castings according to the invention include components which are thermally stressed, in particular pressure vessels, compressor housings, engine parts such as automobile cylinder heads and the like.
본 발명을 첨부도면에 의거하여 보다 상세히 설명하면 다음과 같다. Referring to the present invention in more detail based on the accompanying drawings as follows.
아래의 표1에 나타낸 조성을 갖도록 한 본 발명의 합금 AlMg3SiMnCr과 이에 비교되는 비교합금으로서 F.J.Feikus, "Optimisation of Aluminium Silicon Casting Alloys for Cylinder Heads". Giesserei-Praxis 1999, Vol.2, pages 50-57에 소개된 합금 AlSi7MgCu1을 지속적인 온도부하에서 온도에 따라 비교하였다. As an alloy AlMg 3 SiMnCr of the present invention having a composition shown in Table 1 below and a comparative alloy, F.J.Feikus, "Optimisation of Aluminum Silicon Casting Alloys for Cylinder Heads". The alloy AlSi7MgCu1, presented in Giesserei-Praxis 1999, Vol. 2, pages 50-57, was compared with temperature at constant temperature loading.
표 1 : 합금의 화학조성(중량%) Table 1 : Chemical Composition of Alloys (wt%)
본 발명에 따른 합금을 Deiz의 시험환봉몰드에서 직경이 16 mm 인 환봉으로 주조하였다. 500 시간동안의 지속적인 온도부하에서의 다양한 온도에서, T6(165℃/6시간) 상태에서 시험환봉에 대한 항복강도(Rp0.2), 인장강도(Rm) 및 연신율(A5)이 측정되었다. 이에 상응하는 비교합금에 대한 값은 상기한 F.J.Feikus의 논문으로부터 얻었다. 그 결과를 도 1에 나타내었다. The alloy according to the invention was cast into round bars of 16 mm diameter in a test rod mold of Deiz. At various temperatures with a continuous temperature load of 500 hours, the yield strength (Rp0.2), tensile strength (Rm) and elongation (A5) for the test rods were measured at T6 (165 ° C / 6 hours). Values for the corresponding comparative alloys were obtained from the above paper by F.J.Feikus. The results are shown in FIG.
본 발명에 따른 합금 AlMg3SiMnCr은 항복강도와 인장강도에 있어서는 비교합금 AlSi7MgCu1의 최고값에 이르지는 않았으나, 그 온도특성에 있어서는 "적은 변성"을 보였다. 이러한 변성은 온도에 있어서 가벼운 변화라 할지라도 기계적인 특성에는 큰 변화를 나타내기 때문에 작업에 있어서 파열결과를 초래한다. 본 발명에 따른 합금의 항복강도는 180℃ 부근까지는 거의 동일한 레벨로 유지되고 200℃까지는 점진적으로 하강하였다가 200℃ 이상에서는 연속적으로 감소하기 시작하였다. 이러한 연속적인 감소는 그 기울기가 합금 AlSi7MgCu1 보다는 작았다. The alloy AlMg3SiMnCr according to the present invention did not reach the maximum value of the comparative alloy AlSi7MgCu1 in yield strength and tensile strength, but exhibited "little modification" in temperature characteristics. This change results in a rupture result in the work because even a light change in temperature shows a large change in the mechanical properties. The yield strength of the alloy according to the present invention was maintained at about the same level up to around 180 ° C. and gradually decreased to 200 ° C. and then started to decrease continuously above 200 ° C. This continuous decrease was less than that of the alloy AlSi7MgCu1.
파단 연신율에 있어서, 본 발명에 따른 합금은 180℃ 까지는 거의 일정한 값을 갖는다. 높은 값의 연신율은 양호한 파단/파괴특성을 제공한다. 가시적인 변형이 부품의 파단에 앞서 먼저 나타난다. 180℃ 이상에서는 연신율이 연속적으로 증가하였다. 비교합금 AlSi7MgCu1에 있어서는 분명한 경화효과를 보였다. 낮은 값의 연신율은 파단성에 바람직하지 않다. 즉, 부품이 약간만 변형되거나 전혀 변형되지 않기 때문에 최대값의 부하에서는 징후없이 부품이 파단되어 버린다.In elongation at break, the alloy according to the invention has an almost constant value up to 180 ° C. High values of elongation provide good break / break characteristics. Visible deformation occurs first before the part breaks. Above 180 ° C., the elongation increased continuously. The comparative alloy AlSi7MgCu1 showed a clear curing effect. Low values of elongation are undesirable for fracture. In other words, since the part is slightly deformed or not deformed at all, the part breaks without any sign at the maximum load.
도 1 내지 도 3은 본 발명에 따른 합금과 종래기술의 합금을 비교하기 위하여, 각각 500시간의 지속된 온도부하에서의 시간에 따른 인장강도, 항복강도 및 연신율을 보인 그래프이다.1 to 3 are graphs showing tensile strength, yield strength and elongation with time at a sustained temperature load of 500 hours, respectively, in order to compare the alloy according to the present invention with the prior art alloy.
Claims (13)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CH?00195/04? | 2004-02-11 | ||
| CH1952004 | 2004-02-11 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| KR20050081168A true KR20050081168A (en) | 2005-08-18 |
Family
ID=34683119
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| KR1020050005296A Withdrawn KR20050081168A (en) | 2004-02-11 | 2005-01-20 | Casting of an aluminium alloy |
Country Status (12)
| Country | Link |
|---|---|
| US (1) | US20050173032A1 (en) |
| EP (1) | EP1564308B1 (en) |
| JP (1) | JP2005226161A (en) |
| KR (1) | KR20050081168A (en) |
| CN (1) | CN1654694A (en) |
| AT (1) | ATE338149T1 (en) |
| BR (1) | BRPI0500277A (en) |
| CA (1) | CA2496140A1 (en) |
| DE (1) | DE502005000072D1 (en) |
| ES (1) | ES2270403T3 (en) |
| MX (1) | MXPA05001576A (en) |
| NO (1) | NO20050682L (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR102716443B1 (en) * | 2024-01-10 | 2024-10-15 | 티아이엘씨 주식회사 | SUV luggage board |
Families Citing this family (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE502006000145D1 (en) * | 2005-08-22 | 2007-11-29 | Rheinfelden Aluminium Gmbh | Heat-resistant aluminum alloy |
| KR100691328B1 (en) | 2006-02-07 | 2007-03-12 | (주)새서울경금속 | Die-cast aluminum alloy |
| WO2010114063A1 (en) * | 2009-03-31 | 2010-10-07 | 日立金属株式会社 | Al-mg-si-type aluminum alloy for casting which has excellent bearing force, and casted member comprising same |
| WO2011031183A1 (en) * | 2009-09-14 | 2011-03-17 | Anisimov Oleg Vladimirovich | Method for producing a construction material from an aluminium-based alloy |
| KR101388922B1 (en) | 2010-07-28 | 2014-04-24 | 자동차부품연구원 | Aluminum alloys including Fe-Mn solid solution and method of manufacturing the same |
| GB201205655D0 (en) | 2012-03-30 | 2012-05-16 | Jaguar Cars | Alloy and method of production thereof |
| US20150030496A1 (en) * | 2013-07-26 | 2015-01-29 | M&C Corporation | Aluminum alloy wire and wire assembly parts |
| CN103436755B (en) * | 2013-08-23 | 2015-09-23 | 北京艾路浦科技发展有限公司 | A kind of rust-preventing aluminum alloy material |
| CN103469024B (en) * | 2013-09-24 | 2015-06-24 | 天津那诺机械制造有限公司 | Special aluminum-alloy material for liquid die-forging molding of aluminum-alloy wheels of heavy-duty vehicle and molding method |
| CN103725938B (en) * | 2013-11-27 | 2016-01-13 | 余姚市吴兴铜业有限公司 | A kind of High-performance aluminum alloy automobile part |
| KR101606525B1 (en) * | 2014-10-29 | 2016-03-25 | 주식회사 케이엠더블유 | Aluminum alloy for die casting having excellent corrosion resistance |
| CN105256192A (en) * | 2015-11-13 | 2016-01-20 | 无锡清杨机械制造有限公司 | Aluminium alloy panel and preparation method thereof |
| US20190177818A1 (en) * | 2016-06-10 | 2019-06-13 | GM Global Technology Operations LLC | Magnesium-containing, aluminum-based alloy for thin-wall castings |
| EP3339465B1 (en) * | 2016-12-23 | 2020-01-15 | Brunswick Corporation | Method for solution heat treating with pressure |
| CN109593996A (en) * | 2018-12-28 | 2019-04-09 | 宁波合力模具科技股份有限公司 | A kind of high tough squeeze casting Al mg-si master alloy and preparation method thereof |
| WO2020185920A1 (en) | 2019-03-13 | 2020-09-17 | Novelis Inc. | Age-hardenable and highly formable aluminum alloys, monolithic sheet made therof and clad aluminum alloy product comprising it |
| JP7238545B2 (en) * | 2019-03-29 | 2023-03-14 | 株式会社アイシン | Method for manufacturing aluminum alloy and cast parts |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2129352C3 (en) * | 1971-06-14 | 1982-03-18 | Honsel-Werke Ag, 5778 Meschede | Use of AlMgSi casting alloys for cylinder heads subject to alternating thermal loads |
| JP3006446B2 (en) * | 1994-12-12 | 2000-02-07 | 日本軽金属株式会社 | Heat-treated thin aluminum extruded profile and method for producing the same |
| JP3734317B2 (en) * | 1996-10-09 | 2006-01-11 | 古河スカイ株式会社 | Method for producing Al-Mg-Si alloy plate |
| JPH10130768A (en) * | 1996-10-30 | 1998-05-19 | Furukawa Electric Co Ltd:The | Direct cast rolled sheet of Al-Mg-Si alloy for forming and method for producing the same |
| AT407533B (en) * | 1999-01-22 | 2001-04-25 | Aluminium Lend Gmbh | ALUMINUM ALLOY |
| EP1118685A1 (en) * | 2000-01-19 | 2001-07-25 | ALUMINIUM RHEINFELDEN GmbH | Aluminium cast alloy |
| JP2003129156A (en) * | 2001-10-22 | 2003-05-08 | Kobe Steel Ltd | Al ALLOY SHEET SUPERIOR IN FORMABILITY FOR STRETCH FLANGE AND MANUFACTURING METHOD THEREFOR |
| FR2833616B1 (en) * | 2001-12-17 | 2004-07-30 | Pechiney Aluminium | HIGH DUCTILITY AND RESILIENCE ALUMINUM ALLOY PRESSURE CAST PART |
-
2005
- 2005-01-04 US US11/029,130 patent/US20050173032A1/en not_active Abandoned
- 2005-01-20 KR KR1020050005296A patent/KR20050081168A/en not_active Withdrawn
- 2005-01-31 BR BR0500277-0A patent/BRPI0500277A/en not_active Application Discontinuation
- 2005-02-01 AT AT05100655T patent/ATE338149T1/en not_active IP Right Cessation
- 2005-02-01 ES ES05100655T patent/ES2270403T3/en not_active Expired - Lifetime
- 2005-02-01 DE DE502005000072T patent/DE502005000072D1/en not_active Expired - Lifetime
- 2005-02-01 EP EP05100655A patent/EP1564308B1/en not_active Expired - Lifetime
- 2005-02-08 CA CA002496140A patent/CA2496140A1/en not_active Abandoned
- 2005-02-09 MX MXPA05001576A patent/MXPA05001576A/en unknown
- 2005-02-09 NO NO20050682A patent/NO20050682L/en not_active Application Discontinuation
- 2005-02-10 JP JP2005033891A patent/JP2005226161A/en active Pending
- 2005-02-16 CN CNA2005100090259A patent/CN1654694A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR102716443B1 (en) * | 2024-01-10 | 2024-10-15 | 티아이엘씨 주식회사 | SUV luggage board |
Also Published As
| Publication number | Publication date |
|---|---|
| EP1564308B1 (en) | 2006-08-30 |
| BRPI0500277A (en) | 2005-09-27 |
| CN1654694A (en) | 2005-08-17 |
| ES2270403T3 (en) | 2007-04-01 |
| ATE338149T1 (en) | 2006-09-15 |
| DE502005000072D1 (en) | 2006-10-12 |
| CA2496140A1 (en) | 2005-08-11 |
| MXPA05001576A (en) | 2005-08-19 |
| NO20050682L (en) | 2005-08-12 |
| EP1564308A1 (en) | 2005-08-17 |
| JP2005226161A (en) | 2005-08-25 |
| US20050173032A1 (en) | 2005-08-11 |
| NO20050682D0 (en) | 2005-02-09 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| KR101295458B1 (en) | Aluminium alloy and use of an aluminium alloy | |
| KR20050081168A (en) | Casting of an aluminium alloy | |
| CN1320144C (en) | Casting alloy | |
| JP5345056B2 (en) | Heat-treatable high-strength aluminum alloy | |
| US4834941A (en) | Heat-resisting high-strength Al-alloy and method for manufacturing a structural member made of the same alloy | |
| AU2003255687B2 (en) | Part cast from aluminium alloy with high hot strength | |
| CA2556645C (en) | High temperature aluminium alloy | |
| US4840683A (en) | Al-Cu-Li-Mg alloys with very high specific mechanical strength | |
| US6306342B2 (en) | Aluminum casting alloy | |
| JP2000144296A (en) | High-strength and high-toughness aluminum alloy forged material | |
| CN101311283A (en) | High-temperature aluminium alloy | |
| US20180010214A1 (en) | High strength high creep-resistant cast aluminum alloys and hpdc engine blocks | |
| US20040045638A1 (en) | Safety component moulded in a1-si alloy | |
| CN109811206B (en) | Cast aluminum alloy | |
| EP2072628A1 (en) | High strength crash resistant aluminium alloy | |
| CN100503857C (en) | Aluminum alloy material, its manufacturing method and its application | |
| JP2002348631A (en) | Aluminum-zinc-magnesium cast forging aluminum alloy, aluminum-zinc-magnesium cast forged product, and method of manufacturing the same | |
| JPH08295977A (en) | High strength aluminum alloy extruded material with excellent fatigue strength and motorcycle front fork outer tube material made of the extruded material | |
| EP3342890B1 (en) | Aluminium casting alloy | |
| CN113234970A (en) | Er-containing high-strength and high-toughness cast aluminum-silicon alloy and preparation method thereof | |
| JP2001226731A (en) | Aluminum-zinc-magnesium cast forging aluminum alloy, aluminum-zinc-magnesium cast forged product, and method of manufacturing the same | |
| US20050238529A1 (en) | Heat treatable Al-Zn-Mg alloy for aerospace and automotive castings | |
| JPH06330264A (en) | Production of aluminum alloy forged material excellent in strength and toughness | |
| JP2002226934A (en) | Aluminum alloy for diecasting | |
| US6623570B2 (en) | AlMgSi casting alloy |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PA0109 | Patent application |
Patent event code: PA01091R01D Comment text: Patent Application Patent event date: 20050120 |
|
| PG1501 | Laying open of application | ||
| PC1203 | Withdrawal of no request for examination | ||
| WITN | Application deemed withdrawn, e.g. because no request for examination was filed or no examination fee was paid |