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
Links
- 229910045601 alloy Inorganic materials 0.000 claims description 12
- 239000000956 alloy Substances 0.000 claims description 12
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 11
- 229910052802 copper Inorganic materials 0.000 claims description 11
- 239000010949 copper Substances 0.000 claims description 11
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 10
- 239000010936 titanium Substances 0.000 claims description 10
- 229910052719 titanium Inorganic materials 0.000 claims description 10
- 229910052782 aluminium Inorganic materials 0.000 claims description 9
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 9
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 7
- 229910001297 Zn alloy Inorganic materials 0.000 claims description 7
- 239000011701 zinc Substances 0.000 claims description 7
- 229910052725 zinc Inorganic materials 0.000 claims description 7
- 238000010438 heat treatment Methods 0.000 description 3
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 1
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 1
- 241001424392 Lucia limbaria Species 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- UQZIWOQVLUASCR-UHFFFAOYSA-N alumane;titanium Chemical compound [AlH3].[Ti] UQZIWOQVLUASCR-UHFFFAOYSA-N 0.000 description 1
- 238000000137 annealing Methods 0.000 description 1
- 229910052790 beryllium Inorganic materials 0.000 description 1
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 description 1
- 229910052793 cadmium Inorganic materials 0.000 description 1
- BDOSMKKIYDKNTQ-UHFFFAOYSA-N cadmium atom Chemical compound [Cd] BDOSMKKIYDKNTQ-UHFFFAOYSA-N 0.000 description 1
- 229910052791 calcium Inorganic materials 0.000 description 1
- 239000011575 calcium Substances 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 238000004049 embossing Methods 0.000 description 1
- 229910052744 lithium Inorganic materials 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- -1 zinc-titanium-aluminium Chemical compound 0.000 description 1
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
- C22C18/02—Alloys based on zinc with copper as the next major constituent
Landscapes
- 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)
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)
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 |
-
1969
- 1969-06-02 NO NO2276/69A patent/NO120654B/no unknown
- 1969-06-03 GB GB27989/69A patent/GB1221382A/en not_active Expired
- 1969-06-09 NL NL6908766.A patent/NL155598B/en not_active IP Right Cessation
- 1969-06-11 US US832508A patent/US3615379A/en not_active Expired - Lifetime
- 1969-06-12 BE BE734497D patent/BE734497A/xx not_active IP Right Cessation
- 1969-06-12 FR FR6919530A patent/FR2010778A1/fr active Pending
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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