EP0119180A2 - Legierung auf Zinkbasis mit Duktilität - Google Patents
Legierung auf Zinkbasis mit Duktilität Download PDFInfo
- Publication number
- EP0119180A2 EP0119180A2 EP84870009A EP84870009A EP0119180A2 EP 0119180 A2 EP0119180 A2 EP 0119180A2 EP 84870009 A EP84870009 A EP 84870009A EP 84870009 A EP84870009 A EP 84870009A EP 0119180 A2 EP0119180 A2 EP 0119180A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- content
- alloy
- ppm
- boron
- titanium
- 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
Classifications
-
- 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
Definitions
- the present invention relates to zinc-based alloys with improved ductility.
- a zinc alloy intended for gravity casting is known in particular having a breaking load of the order of 400 MPa. This value was reached by assuring the alloy an aluminum content of about 27%, with additions of copper and magnesium. The ductility of this alloy is however poor, because its elongation is, under the best casting conditions, between 4 and 8%. The same is true of other known alloys, containing approximately 35% of aluminum and additions, in particular of copper.
- the present invention relates to a zinc-based alloy, intended for gravity casting and having improved ductility properties.
- the elongation is clearly improved, while the breaking load remains at least equal to that of the alloys containing 27% or 35% of aluminum.
- a zinc alloy, object of the present invention containing 25% to 40% of aluminum, 0.5% to 5% of copper and up to 0.1% of magnesium, has a content of boron between 5 ppm and 0.1%, and preferably between 0.005% and 0.050%.
- a first particular modality consists in adding to the alloy of titanium in a content of between 25 ppm and 0.5%, and preferably between 0.005% and 0.050%.
- an alloy in accordance with the invention contains, in addition to boron, zirconium and / or strontium in a content of less than 0.1%.
- a zinc alloy which is the subject of the present invention containing 25% to 40% of aluminum, 0.5% to 5% of copper and up to 0.1% of magnesium, has a total content of rare earths, preferably lanthanum and cerium, between 5 ppm and 0.1%, and preferably between 0.005% and 0.050%.
- rare earths can also be in the form of the mixture called mischmetall which contains either about 60% - 90% La, 6% - 10% Ce, the balance being made up of other earths rare and other residual elements (Fe, Mg, Al, Si), i.e. 45% - 60% Ce, the balance being made up of other rare earths or other residual elements (Fe, Mg, Al, Si).
- the table below illustrates the effect of the additions, in accordance with the invention, which have just been described, on the breaking load and on the elongation of a zinc-based alloy containing 27% aluminum, 1% copper and 0.02% magnesium.
- Alloy A is the previously known alloy; it has a low ductility, expressed by an elongation of between 4% and 8%.
- the Blet B 2 alloys in accordance with the first variant of the invention show that an addition of boron within the limits indicated makes it possible to very significantly increase the value of the elongation, and consequently to improve the ductility without altering the load. alloy breakage.
- the alloys C1 and C2 meeting the first particular modality of this first variant also exhibit increased elongation; in addition, the breaking load is slightly increased in the case of the alloy C 1 , whose boron and titanium contents respect the preferential ratio of 1: 5.
- the alloy C 3 has a breaking load markedly improved, but the elongation remained at that of the reference alloy, despite the presence of boron. This behavior seems to be explained by the formation of intermetallic compounds of boron and titanium, which counteract the beneficial effect of boron on elongation, when the titanium contents are high.
- Alloy D I which corresponds to the second particular modality of the first variant, has a significantly higher breaking load than the basic alloy, associated with elongations which are also improved.
- the alloys E 1 and E 2 in accordance with the second variant of the invention, show that an addition of lanthanum or cerium within the limits indicated, makes it possible to raise very significantly significantly the value of the elongation, and consequently of improving the ductility, without altering the breaking load of the alloy.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Conductive Materials (AREA)
- Heat Treatment Of Sheet Steel (AREA)
- Electrolytic Production Of Metals (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AT84870009T ATE41447T1 (de) | 1983-02-11 | 1984-01-20 | Legierung auf zinkbasis mit duktilitaet. |
Applications Claiming Priority (6)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| BE6/47778A BE895892A (fr) | 1983-02-11 | 1983-02-11 | Alliages a base de zinc a ductilite amelioree |
| BE6047778 | 1983-02-11 | ||
| BE6047844 | 1983-07-05 | ||
| BE6047844 | 1983-07-05 | ||
| BE6047872 | 1983-09-20 | ||
| BE6/47872A BE897789A (fr) | 1983-09-20 | 1983-09-20 | Alliage a base de zinc a proprietes ameliorees |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| EP0119180A2 true EP0119180A2 (de) | 1984-09-19 |
| EP0119180A3 EP0119180A3 (en) | 1986-04-30 |
| EP0119180B1 EP0119180B1 (de) | 1989-03-15 |
Family
ID=27159694
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP84870009A Expired EP0119180B1 (de) | 1983-02-11 | 1984-01-20 | Legierung auf Zinkbasis mit Duktilität |
Country Status (3)
| Country | Link |
|---|---|
| EP (1) | EP0119180B1 (de) |
| DE (1) | DE3477206D1 (de) |
| WO (1) | WO1993013230A1 (de) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101698912B (zh) * | 2009-11-06 | 2011-08-17 | 湖南华康新材料有限公司 | 适于连续挤压的铜合金代用材料高性能变形锌基合金 |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE10131344C1 (de) * | 2001-06-28 | 2002-11-21 | Grillo Werke Ag | Zinklegierungen für den Zinkguss oder Zinkdruckguss und Verfahren zu deren Herstellung |
| US7241350B2 (en) * | 2002-12-03 | 2007-07-10 | Greenkote (Israel) Ltd. | Corrosion resistant poly-metal diffusion coatings and a method of applying same |
| CN104651686A (zh) * | 2015-03-16 | 2015-05-27 | 靖江新舟合金材料有限公司 | 一种合金锭以及制备方法 |
| CN104651687B (zh) * | 2015-03-16 | 2016-10-05 | 靖江新舟合金材料有限公司 | 一种合金锌锭以及制备方法 |
| CN106399755B (zh) * | 2016-12-12 | 2018-05-04 | 福州大学 | 一种环保型锌铝阻尼合金及其制备方法 |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1490696A (en) * | 1923-04-26 | 1924-04-15 | Golyer Anthony G De | Zinc alloy |
| CH328148A (de) * | 1952-06-30 | 1958-02-28 | Wilhelm Dr Neu | Zink-Aluminium-Legierung, Verfahren zur Herstellung und Verwendung einer solchen Legierung |
| GB790309A (en) * | 1954-11-18 | 1958-02-05 | Wilhelm Neu | Zinc-aluminium alloys and the production thereof |
| FR1140750A (fr) * | 1956-02-03 | 1957-08-12 | Procédé de fabrication d'alliage de zinc-aluminium-cuivre avec des additions telles que silicium, bore, carbone, nickel et d'autres métaux | |
| BE769480A (fr) * | 1971-07-02 | 1972-01-03 | Centre Rech Metallurgique | Perfectionnements aux alliages zinc-aluminium. |
| DE2142685A1 (de) * | 1971-08-26 | 1973-03-01 | Metallgesellschaft Ag | Superplastische zinklegierung |
-
1984
- 1984-01-20 DE DE8484870009T patent/DE3477206D1/de not_active Expired
- 1984-01-20 EP EP84870009A patent/EP0119180B1/de not_active Expired
- 1984-02-08 WO PCT/BE1984/000003 patent/WO1993013230A1/fr not_active Ceased
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101698912B (zh) * | 2009-11-06 | 2011-08-17 | 湖南华康新材料有限公司 | 适于连续挤压的铜合金代用材料高性能变形锌基合金 |
Also Published As
| Publication number | Publication date |
|---|---|
| EP0119180B1 (de) | 1989-03-15 |
| WO1993013230A1 (fr) | 1993-07-08 |
| DE3477206D1 (en) | 1989-04-20 |
| EP0119180A3 (en) | 1986-04-30 |
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