EP0119180A2 - Legierung auf Zinkbasis mit Duktilität - Google Patents

Legierung auf Zinkbasis mit Duktilität Download PDF

Info

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
Application number
EP84870009A
Other languages
English (en)
French (fr)
Other versions
EP0119180B1 (de
EP0119180A3 (en
Inventor
André Skenazi
Dimitri Coutsouradis
André Rasquin
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Centre de Recherches Metallurgiques CRM ASBL
Original Assignee
Centre de Recherches Metallurgiques CRM ASBL
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority claimed from BE6/47778A external-priority patent/BE895892A/fr
Priority claimed from BE6/47872A external-priority patent/BE897789A/fr
Application filed by Centre de Recherches Metallurgiques CRM ASBL filed Critical Centre de Recherches Metallurgiques CRM ASBL
Priority to AT84870009T priority Critical patent/ATE41447T1/de
Publication of EP0119180A2 publication Critical patent/EP0119180A2/de
Publication of EP0119180A3 publication Critical patent/EP0119180A3/fr
Application granted granted Critical
Publication of EP0119180B1 publication Critical patent/EP0119180B1/de
Expired legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C18/00Alloys based on zinc
    • C22C18/04Alloys 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)
EP84870009A 1983-02-11 1984-01-20 Legierung auf Zinkbasis mit Duktilität Expired EP0119180B1 (de)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Cited By (1)

* Cited by examiner, † Cited by third party
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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