JP3800345B2 - Hot chamber castable zinc alloy - Google Patents
Hot chamber castable zinc alloy Download PDFInfo
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- JP3800345B2 JP3800345B2 JP50471196A JP50471196A JP3800345B2 JP 3800345 B2 JP3800345 B2 JP 3800345B2 JP 50471196 A JP50471196 A JP 50471196A JP 50471196 A JP50471196 A JP 50471196A JP 3800345 B2 JP3800345 B2 JP 3800345B2
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- 229910001297 Zn alloy Inorganic materials 0.000 title description 3
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 53
- 239000000956 alloy Substances 0.000 claims abstract description 53
- 239000011701 zinc Substances 0.000 claims abstract description 27
- 229910052725 zinc Inorganic materials 0.000 claims abstract description 19
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims abstract description 17
- 229910052761 rare earth metal Inorganic materials 0.000 claims abstract description 9
- 150000002910 rare earth metals Chemical class 0.000 claims abstract description 9
- 229910052751 metal Inorganic materials 0.000 claims abstract description 8
- 239000002184 metal Substances 0.000 claims abstract description 8
- 239000000203 mixture Substances 0.000 claims abstract description 8
- 229910052782 aluminium Inorganic materials 0.000 claims description 18
- 229910052802 copper Inorganic materials 0.000 claims description 15
- 238000005266 casting Methods 0.000 claims description 11
- 229910052710 silicon Inorganic materials 0.000 claims description 5
- 239000012535 impurity Substances 0.000 claims description 4
- 238000004519 manufacturing process Methods 0.000 claims description 4
- 238000000034 method Methods 0.000 claims description 4
- 238000005275 alloying Methods 0.000 claims description 3
- 230000005484 gravity Effects 0.000 claims description 2
- 229910001325 element alloy Inorganic materials 0.000 claims 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 3
- 229910052760 oxygen Inorganic materials 0.000 description 3
- 239000001301 oxygen Substances 0.000 description 3
- 235000011837 pasties Nutrition 0.000 description 3
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 229910052748 manganese Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- 238000009864 tensile test Methods 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 229910000842 Zamak Inorganic materials 0.000 description 1
- 229910000781 Zamak 5 Inorganic materials 0.000 description 1
- 229910000611 Zinc aluminium Inorganic materials 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 238000004512 die casting Methods 0.000 description 1
- 239000011888 foil Substances 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 229910052727 yttrium Inorganic materials 0.000 description 1
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C18/00—Alloys based on zinc
- C22C18/04—Alloys based on zinc with aluminium as the next major constituent
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- Manufacture Of Alloys Or Alloy Compounds (AREA)
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- Continuous Casting (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
- Refinement Of Pig-Iron, Manufacture Of Cast Iron, And Steel Manufacture Other Than In Revolving Furnaces (AREA)
- Supercharger (AREA)
- Ink Jet (AREA)
- Vertical, Hearth, Or Arc Furnaces (AREA)
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- Casting Support Devices, Ladles, And Melt Control Thereby (AREA)
- Superconductors And Manufacturing Methods Therefor (AREA)
- Conductive Materials (AREA)
- Mold Materials And Core Materials (AREA)
- Sliding-Contact Bearings (AREA)
- Ceramic Products (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
- Cooling Or The Like Of Semiconductors Or Solid State Devices (AREA)
Abstract
Description
本発明は、ホットチャンバー機(hot-chamber machine)において加圧下で鋳造され得る、AlおよびCuを含有する亜鉛をベースとする合金に関するものである。
そのような合金は文献「SAEテクニカル・ペーパー・シリーズ930788,ACuZinc:金型鋳造への使用のための改良された亜鉛合金,M.D.ハンナおよびM.S.ラシッド,国際会議および展示会デトロイト,ミシガン,1993年3月1−5日」に記載されている。この公知の合金は、「ACuZinc5」と呼ばれ、Cu5.0−6.0%、Al2.8−3.3%およびMg0.025−0.05%、残部亜鉛からなる(本明細書において全ての%は重量%である)。この合金のクリープ耐性は、長い間ホットチャンバー内で鋳造されてきたザマク(Zamak)またはZA合金のクリープ耐性に比べ実質的に優れているが、依然として比較的低い。
本発明の目的は上記公知の合金に比べ、より良好なクリープ耐性を有する最初に記載したような合金を提供することである。
このために、本発明による合金は、重量%で:Al25−30、Cu15−20、Si0.01−2、Mg0−0.1、Ti0−0.5、Cr0−0.5、Mn0−1、Nb0−0.5および希土類金属1種または金属混合物0−0.1(この組成は以下、バリアントIIと呼ばれる)を含有し、残部は亜鉛と亜鉛および上記合金化元素中に不可避に存在する不純物である。
なお、参考例の合金は、重量%で:Al15−20、Cu8−10、Si0.01−2、Mg0−0.1、Ti0−0.5、Cr0−0.5、Mn0−1、Nb0−0.5および希土類金属1種または金属混合物0−0.1(この組成は以下、バリアントIと呼ばれる)を含有し、残部は亜鉛と亜鉛および上記合金化元素中に不可避に存在する不純物である。
実際に、一方では、460℃を越えない温度で液体状態にある2種類のバリアントはホットチャンバー内で鋳造され得るような鋼に近似する低い攻撃性(aggressivity)を有すること、および他方では、鋳造状態において、バリアントIが良好なクリープ耐性および優れた引張強さを示し、鋳造状態において、バリアントIIが優れたクリープ耐性および良好な引張強さを示すことが見出されている。上に記載したAlおよびCu含量は固守されなければならず、さもなければ、合金の融点は450℃より上昇し、その結果、合金は、鋳造装置に対する腐食性が460℃以上であまりにも大きくなるので、ホットチャンバー内でもはや鋳造され得ない。ケイ素含量が0.01%より少ない場合、引張強さおよびクリープ耐性は悪化する。2%より多いケイ素含量は溶融状態で合金をあまりにペースト状にし、そしてあまりに腐食性にする。
以下の合金が既に記載されていることをここで報告することは適当である:
(a)17−19 Al,4.5−5.5 Cu,0.9−1.3 Si,0.8−1.2 Mg,残部Zn(CS−A−135802)
(b)28.6 Al,3.1 Cu,1 Si,0.1 Ca,0.2 Ni,残部Zn(GB−A−769483)
(c)20−40 Al,0−5 Cu,0−1 Si,0−0.1 Mg,0.25−2 少なくとも1種の希土類金属,残部Zn(US−A−4789522)
(d)55 Al,8 Cu,6.5 Si,4.5 Be,0.12 Ni,0.6 Ca,残部Zn(US−A−287008)。
これらの公知合金の中で、合金(c)が本発明に係る合金に最も近接している。合金(a)はホットチャンバー内で鋳造し得るにはあまりにも低いCu含量を有し、かつ、あまりにも高いMg含量を有する。合金(c)はまた、あまりに低いCu含量を有し、さらに酸化された状態でさえも、酸素に対する希土類金属の高い親和性の故に、これら希土類金属を0.25−2%含有する合金を調製することは極端に困難である。
バリアントIは有利にはAlを15−18%、好ましくは15−17%含有する。バリアントIIの好ましいAlおよびCu含量はそれぞれ25.5−28.5%および15−18%である。両方のバリアントの好ましいSi含量は0.1−1%である。両方のバリアントは、
−必要であるならば粒間耐蝕性を改良するためにMgを0.1%まで;
−必要であるならば延性を改良するためにTiを0.5%まで、Crを0.5%まで、そしてMnを1%まで;
−必要であるならば外部腐食性に対する耐性を改良するために、すなわち白色塩の形成を遅延させるためにNbを0.5%まで;および
−必要であるならば溶融状態にある合金の表面張力を低下させるために希土類金属または金属混合物を0.1%まで、含有してもよい。
0.1%より多いMg含量により、合金は溶融状態においてペースト状になり、そして固体状態で脆性になる。合金はまた、Ti、CrおよびMnに対する上記範囲から逸脱するならば、ペースト状になる。0.5%より多いNb含量および0.1%より多い希土類金属含量は、酸素に対するそれらの元素の高い親和性の故に使用が困難である。
合金を調製するために用いられるZn、AlおよびCuはそれぞれ純度≧99.99%、≧99.95%および≧99.99%を有することが望ましい。これは合金中に不純物が存在すると流動性および機械的特性に悪影響を及ぼすことが見出されているからである。純度・99.995%の亜鉛および純度・99.97%のアルミニウムが使用されることが好ましい。
合金が酸素に対する非常に高い親和性を有する金属、例えばY等を含有する場合、該金属の少なくとも一部は酸化された状態で存在してもよい。
本発明に係る合金のバリアントIIの優れたクリープ耐性および参考例の合金のバリアントIの良好なクリープ耐性は、下に記載される一連の比較試験により説明され、その結果は添付の図面に示されている。
2種類の公知合金、ザマク5およびACuZinc5が本発明に係る2種類の合金、以下「X27」と記載されるバリアントIに相当する第1の合金および以下「X28」と記載されるバリアントIIに相当する第2の合金と一緒に試験された。
これらの合金の組成は以下のとおりである:
−ザクマ5:4%Al,1%Cu,0.04%Mg,残部Zn;
−ACuZinc5:3%Al,5.5%Cu,0.04%Mg,残部Zn;
−X27:17%Al,9.5%Cu,0.5%Si,残部Zn;
−X28:27%Al,16.5%Cu,0.1%Si,残部Zn。
これらの合金の試験片はホットチャンバー機において鋳造された。
一般的な鋳造条件は以下のとおりであった:
−サイクル時間:12秒
−浴温度:420−460℃
−金属に加えた圧力:50MPa
−ピストン速度:1.2m/s
−ノズルの直径:9.5mm
−型温度:180−250℃。
これらの試験片の形状および寸法は亜鉛および亜鉛合金から製造されるシートおよび箔に対する引張試験において使用される試験片のための欧州亜鉛処理技術委員会により規定されたものである。
試験片は40MPaの荷重下100℃でクリープ試験に供された。時間(単位,時間)の関数として測定された伸び(単位,%)を示すクリープ曲線は添付の図面に示されている。
本発明に係る合金のバリアントIIが公知合金に比べより良好にクリープに耐性であることが示されている。
参考例の合金のバリアントIの優れた引張強さおよび非常に高い硬度ならびに本発明に係る合金のバリアントIIの良好な引張強さおよび適度な硬度は下の表にまとめられたデータにより示される。
引張試験は、上記のように製造された厚さ3mmの試験片に対し引張速度1cm/分で室温にて行われた。
本発明はまた、ホットチャンバー機内で加圧下鋳造することにより、AlおよびCuを含有する亜鉛がベースの合金からなる物品の製造方法に関し、該方法は上記合金が本発明の合金であり、そして上記鋳造が460℃に等しいか、またはそれより低い温度で行われることを特徴とする。
本発明の合金はホットチャンバーにおいて鋳造され得るが、それは必要に応じ、コールドチャンバーにおいて、および大気圧下で鋳造され得る。
それ故に、本発明はコールドチャンバー機内で加圧下鋳造するか、または重力鋳造することにより、AlおよびCuを含有する亜鉛がベースの合金からなる物品の製造方法に関し、該方法は上記合金が本発明の合金であることを特徴とする。The present invention relates to a zinc-based alloy containing Al and Cu that can be cast under pressure in a hot-chamber machine.
Such alloys are described in the document “SAE Technical Paper Series 930788, ACuZinc: Improved Zinc Alloy for Use in Die Casting, MD Hanna and MS Rashid, International Conference and Exhibition Detroit Michigan, March 1-5, 1993 ". This known alloy is called “ACuZinc5” and consists of Cu 5.0-6.0%, Al 2.8-3.3% and Mg 0.025-0.05%, the balance zinc (all in the present specification). % Is by weight). The creep resistance of this alloy is substantially superior to the creep resistance of Zamak or ZA alloys that have been cast in hot chambers for a long time, but is still relatively low.
The object of the present invention is to provide an alloy as described at the outset which has better creep resistance compared to the known alloys.
For this purpose, the alloys according to the invention are in weight percent: Al25-30, Cu15-20, Si0.01-2, Mg0-0.1, Ti0-0.5, Cr0-0.5, Mn0-1, Impurities that inevitably exist in zinc and zinc and the above alloying elements, containing Nb0-0.5 and one rare earth metal or metal mixture 0-0.1 (this composition is hereinafter referred to as variant II) It is.
In addition, the alloy of a reference example is weight%: Al15-20, Cu8-10, Si0.01-2, Mg0-0.1, Ti0-0.5, Cr0-0.5, Mn0-1, Nb0- 0.5 and 1 rare earth metal or metal mixture 0-0.1 (this composition is hereinafter referred to as variant I), the balance being impurities inevitably present in zinc and zinc and the alloying elements mentioned above .
In fact, on the one hand, the two variants that are in the liquid state at temperatures not exceeding 460 ° C. have low aggressivity that approximates steel such that they can be cast in a hot chamber, and on the other hand, casting It has been found that variant I exhibits good creep resistance and excellent tensile strength in the state and variant II exhibits excellent creep resistance and good tensile strength in the cast state. The Al and Cu contents described above must be adhered to, otherwise the melting point of the alloy will rise above 450 ° C, so that the alloy will be too corrosive to casting equipment above 460 ° C. So it can no longer be cast in the hot chamber. If the silicon content is less than 0.01%, the tensile strength and creep resistance deteriorate. A silicon content greater than 2% makes the alloy too pasty and too corrosive in the molten state.
It is appropriate to report here that the following alloys have already been described:
(A) 17-19 Al, 4.5-5.5 Cu, 0.9-1.3 Si, 0.8-1.2 Mg, balance Zn (CS-A-135802)
(B) 28.6 Al, 3.1 Cu, 1 Si, 0.1 Ca, 0.2 Ni, balance Zn (GB-A-769483)
(C) 20-40 Al, 0-5 Cu, 0-1 Si, 0-0.1 Mg, 0.25-2 At least one rare earth metal, the balance Zn (US-A-4789522)
(D) 55 Al, 8 Cu, 6.5 Si, 4.5 Be, 0.12 Ni, 0.6 Ca, balance Zn (US-A-287008).
Among these known alloys, the alloy (c) is closest to the alloy according to the present invention. Alloy (a) has a Cu content that is too low to be cast in a hot chamber and a Mg content that is too high. Alloy (c) also has an excessively low Cu content and, even in the oxidized state, prepared an alloy containing 0.25-2% of these rare earth metals because of the high affinity of the rare earth metals for oxygen. It is extremely difficult to do.
Variant I advantageously contains 15-18% Al, preferably 15-17%. The preferred Al and Cu contents of Variant II are 25.5-28.5% and 15-18%, respectively. The preferred Si content of both variants is 0.1-1%. Both variants are
-Up to 0.1% Mg to improve intergranular corrosion resistance if necessary;
-Ti up to 0.5%, Cr up to 0.5% and Mn up to 1% to improve ductility if necessary;
-Nb up to 0.5% to improve resistance to external corrosion if necessary, ie to delay the formation of white salts; and-Surface tension of the alloy in the molten state if necessary May be included up to 0.1% of rare earth metals or metal mixtures.
With an Mg content greater than 0.1%, the alloy becomes pasty in the molten state and becomes brittle in the solid state. The alloy also becomes pasty if it deviates from the above ranges for Ti, Cr and Mn. Nb contents greater than 0.5% and rare earth metal contents greater than 0.1% are difficult to use because of their high affinity for oxygen.
It is desirable that the Zn, Al and Cu used to prepare the alloys have a purity ≧ 99.99%, ≧ 99.95% and ≧ 99.99%, respectively. This is because it has been found that the presence of impurities in the alloy adversely affects fluidity and mechanical properties. Preferably, a purity of 99.995% zinc and a purity of 99.97% aluminum are used.
When the alloy contains a metal having a very high affinity for oxygen, such as Y, at least a portion of the metal may be present in an oxidized state.
The excellent creep resistance of variant II of the alloy according to the invention and the good creep resistance of variant I of the reference alloy are illustrated by the series of comparative tests described below, the results of which are shown in the accompanying drawings. ing.
Two types of known alloys, Zamak 5 and ACuZinc5, correspond to two types of alloys according to the present invention, a first alloy corresponding to variant I, hereinafter referred to as “X27”, and variant II, hereinafter referred to as “X28” And tested with a second alloy.
The composition of these alloys is as follows:
-Zakuma 5: 4% Al, 1% Cu, 0.04% Mg, balance Zn;
-ACuZinc5: 3% Al, 5.5% Cu, 0.04% Mg, balance Zn;
-X27: 17% Al, 9.5% Cu, 0.5% Si, balance Zn;
-X28: 27% Al, 16.5% Cu, 0.1% Si, balance Zn.
These alloy specimens were cast in a hot chamber machine.
General casting conditions were as follows:
-Cycle time: 12 seconds-Bath temperature: 420-460 ° C
-Pressure applied to the metal: 50 MPa
-Piston speed: 1.2 m / s
-Nozzle diameter: 9.5 mm
Mold temperature: 180-250 ° C.
The shape and dimensions of these specimens are those specified by the European Zinc Processing Technical Committee for specimens used in tensile tests on sheets and foils made from zinc and zinc alloys.
The specimen was subjected to a creep test at 100 ° C. under a load of 40 MPa. A creep curve showing elongation (unit,%) measured as a function of time (unit, time) is shown in the accompanying drawings.
It has been shown that variant II of the alloy according to the invention is better resistant to creep than known alloys.
The excellent tensile strength and very high hardness of variant I of the reference alloy and the good tensile strength and moderate hardness of variant II of the alloy according to the invention are shown by the data summarized in the table below.
The tensile test was performed at room temperature at a tensile speed of 1 cm / min on the test piece having a thickness of 3 mm produced as described above.
The invention also relates to a method for producing an article comprising a zinc-based alloy containing Al and Cu by casting under pressure in a hot chamber machine, wherein the method is the alloy of the invention and It is characterized in that the casting is carried out at a temperature equal to or lower than 460 ° C.
The alloy of the present invention can be cast in a hot chamber, but it can be cast in a cold chamber and under atmospheric pressure if desired.
Therefore, the present invention relates to a method for producing an article comprising a zinc-based alloy containing Al and Cu by casting under pressure in a cold chamber machine or by gravity casting, the method comprising the above-mentioned alloy according to the present invention. It is an alloy of the above.
Claims (6)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| BE9400676A BE1008479A3 (en) | 1994-07-18 | 1994-07-18 | Zinc alloy castable room hot. |
| BE9400676 | 1994-07-18 | ||
| PCT/EP1995/002820 WO1996002682A1 (en) | 1994-07-18 | 1995-07-12 | Hot chamber castable zinc alloy |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH10502705A JPH10502705A (en) | 1998-03-10 |
| JP3800345B2 true JP3800345B2 (en) | 2006-07-26 |
Family
ID=3888263
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP50471196A Expired - Fee Related JP3800345B2 (en) | 1994-07-18 | 1995-07-12 | Hot chamber castable zinc alloy |
Country Status (16)
| Country | Link |
|---|---|
| EP (1) | EP0771365B1 (en) |
| JP (1) | JP3800345B2 (en) |
| KR (1) | KR100343309B1 (en) |
| AT (1) | ATE173029T1 (en) |
| AU (1) | AU3113995A (en) |
| BE (1) | BE1008479A3 (en) |
| BR (1) | BR9507577A (en) |
| CA (1) | CA2185013C (en) |
| CZ (1) | CZ287825B6 (en) |
| DE (1) | DE69505820T2 (en) |
| DK (1) | DK0771365T3 (en) |
| ES (1) | ES2126301T3 (en) |
| FI (1) | FI114400B (en) |
| PE (1) | PE12696A1 (en) |
| PL (1) | PL178557B1 (en) |
| WO (1) | WO1996002682A1 (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR100961081B1 (en) | 2009-03-03 | 2010-06-08 | 임현규 | Zinc-aluminium alloys with high strength and low density |
| KR101955995B1 (en) * | 2017-03-21 | 2019-03-08 | 주식회사 지.에이.엠 | High strength aluminium-zinc alloy and high strength aluminium-zinc alloy casting |
| CN112522540A (en) * | 2020-12-01 | 2021-03-19 | 江苏同生特钢制造有限公司 | Zinc alloy casting and preparation method thereof |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB769483A (en) * | 1953-06-30 | 1957-03-06 | Willi Neu | Zinc aluminium alloy and process for the production thereof |
| US2870008A (en) * | 1954-11-18 | 1959-01-20 | Main Alloy Company Establishme | Zinc-aluminium alloys and the method for producing same |
| US4789522A (en) * | 1986-06-27 | 1988-12-06 | Queen's University At Kingston | Castable zinc-aluminum alloys |
-
1994
- 1994-07-18 BE BE9400676A patent/BE1008479A3/en not_active IP Right Cessation
-
1995
- 1995-07-12 AT AT95926933T patent/ATE173029T1/en not_active IP Right Cessation
- 1995-07-12 AU AU31139/95A patent/AU3113995A/en not_active Abandoned
- 1995-07-12 DK DK95926933T patent/DK0771365T3/en active
- 1995-07-12 EP EP95926933A patent/EP0771365B1/en not_active Expired - Lifetime
- 1995-07-12 KR KR1019960705161A patent/KR100343309B1/en not_active Expired - Fee Related
- 1995-07-12 JP JP50471196A patent/JP3800345B2/en not_active Expired - Fee Related
- 1995-07-12 CZ CZ199751A patent/CZ287825B6/en not_active IP Right Cessation
- 1995-07-12 BR BR9507577A patent/BR9507577A/en not_active IP Right Cessation
- 1995-07-12 PL PL95318133A patent/PL178557B1/en not_active IP Right Cessation
- 1995-07-12 WO PCT/EP1995/002820 patent/WO1996002682A1/en not_active Ceased
- 1995-07-12 CA CA002185013A patent/CA2185013C/en not_active Expired - Fee Related
- 1995-07-12 ES ES95926933T patent/ES2126301T3/en not_active Expired - Lifetime
- 1995-07-12 DE DE69505820T patent/DE69505820T2/en not_active Expired - Fee Related
- 1995-07-13 PE PE1995273756A patent/PE12696A1/en not_active Application Discontinuation
-
1997
- 1997-01-16 FI FI970177A patent/FI114400B/en active IP Right Grant
Also Published As
| Publication number | Publication date |
|---|---|
| ATE173029T1 (en) | 1998-11-15 |
| CA2185013C (en) | 2006-08-29 |
| WO1996002682A1 (en) | 1996-02-01 |
| AU3113995A (en) | 1996-02-16 |
| PE12696A1 (en) | 1996-04-23 |
| ES2126301T3 (en) | 1999-03-16 |
| PL178557B1 (en) | 2000-05-31 |
| EP0771365B1 (en) | 1998-11-04 |
| BR9507577A (en) | 1997-09-09 |
| CZ287825B6 (en) | 2001-02-14 |
| KR100343309B1 (en) | 2002-11-25 |
| DK0771365T3 (en) | 1999-07-19 |
| CZ5197A3 (en) | 1997-04-16 |
| CA2185013A1 (en) | 1996-02-01 |
| DE69505820D1 (en) | 1998-12-10 |
| FI970177A0 (en) | 1997-01-16 |
| PL318133A1 (en) | 1997-05-12 |
| DE69505820T2 (en) | 1999-07-08 |
| FI970177L (en) | 1997-01-16 |
| EP0771365A1 (en) | 1997-05-07 |
| FI114400B (en) | 2004-10-15 |
| BE1008479A3 (en) | 1996-05-07 |
| JPH10502705A (en) | 1998-03-10 |
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