NO120654B - - Google Patents

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Publication number
NO120654B
NO120654B NO2276/69A NO227669A NO120654B NO 120654 B NO120654 B NO 120654B NO 2276/69 A NO2276/69 A NO 2276/69A NO 227669 A NO227669 A NO 227669A NO 120654 B NO120654 B NO 120654B
Authority
NO
Norway
Prior art keywords
titanium
alloy
copper
rolled
aluminum
Prior art date
Application number
NO2276/69A
Other languages
Norwegian (no)
Inventor
E Pelzel
Original Assignee
Stolberger Zink Ag
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 DE19681758489 external-priority patent/DE1758489C3/en
Application filed by Stolberger Zink Ag filed Critical Stolberger Zink Ag
Publication of NO120654B publication Critical patent/NO120654B/no

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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C18/00Alloys based on zinc
    • C22C18/02Alloys based on zinc with copper as the next major constituent

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Metal Rolling (AREA)
  • Superconductors And Manufacturing Methods Therefor (AREA)
  • Heat Treatment Of Steel (AREA)
  • Printing Plates And Materials Therefor (AREA)
  • Conductive Materials (AREA)

Description

Anvendelse av en finsinklegering. Application of a fine zinc alloy.

Oppfinnelsen vedrører anvendelse av en finsinklegering bestående av 0,05 til 0,25# titan, 0,02 til 0,20$ kobber, 0,005 til 0,05$ aluminium, resten finsink 99,9 til 99,995$.- The invention relates to the use of a fine zinc alloy consisting of 0.05 to 0.25# titanium, 0.02 to 0.20$ copper, 0.005 to 0.05$ aluminum, the remainder fine zinc 99.9 to 99.995$.-

Det er kjent en permanentfast sinkknalegering med inn-hold av bly fra 0 til 1$, kadmium fra 0 til 0,05$,' kobber fra 0 til 1,2$, idet denne legering er karakterisert ved at den har titan-innhold fra 0,05 til 0»25$> aluminiuminnhold på, mer enn 0,003 til mindre enn 0,05$, fortrinnsvis fra 0,01 til 0,03$, resten finsink og/eller prosess-sink, og er fri for magnesium, litium, beryllium og kalsium. A permanently fixed zinc alloy is known with a content of lead from 0 to 1%, cadmium from 0 to 0.05%, copper from 0 to 1.2%, this alloy being characterized in that it has a titanium content of 0.05 to 0»25$> aluminum content of, more than 0.003 to less than 0.05$, preferably from 0.01 to 0.03$, the balance fine zinc and/or process zinc, and is free of magnesium, lithium , beryllium and calcium.

Legeringene kan således karakteriseres som sink-titan-aluminiumtypen, fordi titaninnholdet bestemmer permanentfastheten, aluminiuminnholdet; støpeforhold og dermed økonomien. Den prakt-tiske erfaring har imidlertid ikke bare bekreftet dette, men ved finsinklegeringer av denne type fremkom dessuten ytterligere over-raskende effekter. The alloys can thus be characterized as the zinc-titanium-aluminium type, because the titanium content determines the permanent strength, the aluminum content; casting conditions and thus the economy. However, practical experience has not only confirmed this, but with fine zinc alloys of this type, additional surprising effects have also appeared.

For økning av fastheten foreslås ved de fleste titan-holdige sinkknalegeringer kobberinnhold på mer enn 0,15 til 2$ kobber. Ved fremstilling av valselegeringer med titan'og aluminium innen de angitte grenser viser det seg at ved anvendelse av finsink med en renhetsgrad på minst 99«9$ øker allerede mindre kobberinnhold under 0,2$ fastheten og har også allerede i koldvalset tilstand en betraktelig permanentfasthet og duktilitet, altså begge uten varmebehandling. Varmebehandlingen selv kan når den anvendes allerede gjennomføres ved lavere temperaturer. To increase the strength, a copper content of more than 0.15 to 2% copper is suggested for most titanium-containing zinc alloy. In the production of rolled alloys with titanium and aluminum within the specified limits, it turns out that when fine zinc is used with a purity of at least 99.9$, the strength is already increased by a small copper content of less than 0.2$ and, even in the cold-rolled state, it has a considerable permanent strength and ductility, i.e. both without heat treatment. The heat treatment itself, when used, can already be carried out at lower temperatures.

Oppfinnelsens gjenstand er følgelig anvendelsen av en finsinklegering bestående av 0,05 til 0,25$ titan, 0,02 til 0,20$ kobber, 0,005 til 0,05$ aluminium, resten finsink 99,9 til 99,995<$>; som i koldvalset tilstand permanentfast og duktil legering. Accordingly, the object of the invention is the use of a fine zinc alloy consisting of 0.05 to 0.25$ titanium, 0.02 to 0.20$ copper, 0.005 to 0.05$ aluminum, the remainder fine zinc 99.9 to 99.995<$>; as in the cold-rolled state permanently fixed and ductile alloy.

Eksempel 1. Example 1.

I en liggende kokille ble det hver gang støpt en 1000 kg blokk av 80 mm tykkelse ved 250°C valset til 8 mm og koldvalset ved værelsestemperatur fra 8 mm til 0,8 mm. Each time a 1000 kg block of 80 mm thickness was cast in a horizontal mold at 250°C, rolled to 8 mm and cold rolled at room temperature from 8 mm to 0.8 mm.

Legering med 0,5 til 0,8$ kobber Alloy with 0.5 to 0.8$ copper

0,1 til 0,15$ titan 0.1 to 0.15$ titanium

Maksimum 0,001$ aluminium Maximum 0.001$ aluminum

resten finsink the rest fine

Eksempel 2. Example 2.

I en liggende kokille ble det hver gang støpt en 1000 kg blokk av 80 mm tykkelse, ved 250°C valset til 8 mm og koldvalset ved værelsestemperatur fra 8 mm til 0,8 mm. Each time a 1000 kg block of 80 mm thickness was cast in a horizontal mould, rolled to 8 mm at 250°C and cold rolled at room temperature from 8 mm to 0.8 mm.

Legering med 0,2 til 0,5$ Kobber Alloy with 0.2 to 0.5$ Copper

0,1 til 0,15$ titan 0.1 to 0.15$ titanium

Al max. 0,001$ Al max. 0.001$

resten finsink the rest fine

Eksempel 3. Example 3.

I en liggende kokille ble det hver gang støpt en 1000 kg blokk av 80 mm tykkelse ved 250°C valset til 8 mm og koldvalset ved værelsestemperatur fra 8 mm til 0,8 mm. Each time a 1000 kg block of 80 mm thickness was cast in a horizontal mold at 250°C, rolled to 8 mm and cold rolled at room temperature from 8 mm to 0.8 mm.

Legering med 0,05 til 0,15$ kobber Alloy with 0.05 to 0.15$ copper

0,10 til 0,15$ titan 0.10 to 0.15$ titanium

0,01 til 0,02$ aluminium resten finsink 0.01 to 0.02$ aluminum the rest fine zinc

Titan-aluminium-holdige valselegeringer med lite kobberinnhold under 0,2$, fortrinnsvis 0,05 til 0jl$> har allerede ved bruddfri forarbeidelse i valset tilstand en betraktelig permanentfasthet. Dette er et avgjørende fremskritt fordi de hittil frem-stilte legeringer med høyere kobberinnhold uten aluminium etter en permanentglødning sterkt taper sigefastheten når det således be-handlede båndmateriale ved forarbeidingen ble koldformet, f.eks. ved pregning. Titanium-aluminium-containing rolling alloys with a low copper content of less than 0.2$, preferably 0.05 to 0jl$> already have a considerable permanent strength when processed without breakage in the rolled state. This is a decisive advance because the alloys with a higher copper content without aluminum that have been produced until now, after permanent annealing, greatly lose their creep strength when the band material treated in this way was cold-formed during processing, e.g. by embossing.

Den eventuelle varmebehandling av legeringen som skal anvendes ifølge oppfinnelsen kan fortrinnsvis foretas i temperatur-området fra 120 til l80°G. I samme temperaturområde kan legeringen også varmvalses. The possible heat treatment of the alloy to be used according to the invention can preferably be carried out in the temperature range from 120 to 180°G. In the same temperature range, the alloy can also be hot-rolled.

Claims (1)

Anvendelse av en f insinklegering bestående av 0,05 til 0,25$ titan, 0,02 til 0,20$ kobber, 0,005 til 0,05$ aluminium, resten finsink 99»9 til 99>995$)som i koldvalset tilstand permanentfast og duktil legering.Use of a fine zinc alloy consisting of 0.05 to 0.25$ titanium, 0.02 to 0.20$ copper, 0.005 to 0.05$ aluminum, the remainder fine zinc 99»9 to 99>995$)as in the cold-rolled condition permanently fixed and ductile alloy.
NO2276/69A 1968-06-12 1969-06-02 NO120654B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19681758489 DE1758489C3 (en) 1968-06-12 Use of a fine zinc alloy

Publications (1)

Publication Number Publication Date
NO120654B true NO120654B (en) 1970-11-16

Family

ID=5695062

Family Applications (1)

Application Number Title Priority Date Filing Date
NO2276/69A NO120654B (en) 1968-06-12 1969-06-02

Country Status (6)

Country Link
US (1) US3615379A (en)
BE (1) BE734497A (en)
FR (1) FR2010778A1 (en)
GB (1) GB1221382A (en)
NL (1) NL155598B (en)
NO (1) NO120654B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4717430A (en) * 1984-06-18 1988-01-05 Copper Development Association, Inc. Soldering compositions, fluxes and methods of use
US5945066A (en) * 1997-11-20 1999-08-31 Griffin; James D. Zinc-copper based alloy and castings made therefrom
US20040173294A1 (en) * 1998-11-17 2004-09-09 Grillo-Werke Ag Use of zinc alloys
EP3578675B1 (en) * 2018-06-07 2022-07-13 Grillo-Werke Aktiengesellschaft Highly malleable, ductile zinc strip

Also Published As

Publication number Publication date
NL155598B (en) 1978-01-16
GB1221382A (en) 1971-02-03
DE1758489A1 (en) 1971-02-11
NL6908766A (en) 1969-12-16
DE1758489B2 (en) 1974-08-08
FR2010778A1 (en) 1970-02-20
BE734497A (en) 1969-11-17
US3615379A (en) 1971-10-26

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