CH312660A - Heat-treatable light metal alloy and process for their production - Google Patents
Heat-treatable light metal alloy and process for their productionInfo
- Publication number
- CH312660A CH312660A CH312660DA CH312660A CH 312660 A CH312660 A CH 312660A CH 312660D A CH312660D A CH 312660DA CH 312660 A CH312660 A CH 312660A
- Authority
- CH
- Switzerland
- Prior art keywords
- light metal
- metal alloy
- sep
- treatable
- heat
- Prior art date
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
- C22C21/08—Alloys based on aluminium with magnesium as the next major constituent with silicon
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Refinement Of Pig-Iron, Manufacture Of Cast Iron, And Steel Manufacture Other Than In Revolving Furnaces (AREA)
Description
Vergütbare Leichtmetall-Legierung und Verfahren zu deren Herstellung Vorliegende Erfindung betrifft eine ver- gütba.re Leichtmetall-Legierung, die folgende Zusammensetzung aufweist Cu 0,9-1,70/0. Si 6,3-6,7 0/0 Mg 0,2-0e4% Mn0,2-0,7 % Fe 0,4-1,8% Rest Aluminium.
Diese vergütbare Leichtmetall-Legierung hat den Vorteil, da:ss sie sieh für sehr kom plizierte und giesstechniseh sehr schwierig zu vergiessende Gussteile eignet.
Mit dieser vergütbaren Leichtmetall Legie rung können Festigkeitswerte bis ungefähr 35 kg/mm2 mit einer Dehnung bis 3,51/o sowie Brinellhärten bis 130 kglmm2 erzielt werden. Schon im unvergüteten Zustand können Brinellhärten von 80 kg/mm2 erreicht. werden..
Die erfindungsgemässe Legierung besitzt auch einen besonders guten Widerstand ge- (ren Verschleiss.
Weiterhin hat die vergütbare Leichtme- tall-Legierung besondere Vorteile hinsicht lich ihrer mechanischen Bearbeitbarkeit, indem auf sämtliche bisher erforderliche Zu satzmittel, wie Terpentin und dergleichen, verzichtet werden kann.
Die Herstellung der erfindungsgemässen Legierung erfolgt zweckmässig derart, dass die Leiehtmetall-Legierung unter Verwen- dune einer Vorlegierung aus gleichen Ge wichtsteilen Kupfer und Aluminium er schmolzen wird, wobei die höher schmelzen- den Bestandteile zuletzt zugesetzt werden.
Aus <I>f</I> ührungsbeispieZ Aus gleichen Gewiehtsteilen Aluminium und Kupfer wird eine Vorlegierung erzeugt, indem. in geschmolzenes Aluminium (rein) die gleiche Gewiehtsmenge Kupfer eingetra gen wird.
Zur Herstellung der Legierung selbst werden
EMI0001.0059
89 <SEP> kg <SEP> Reinaluminium <SEP> erschmolzen.
<tb> Alsdann <SEP> werden
<tb> 0,400 <SEP> kg <SEP> Magnesium,
<tb> 3 <SEP> <SEP> der <SEP> Al-Cu-Vorlegierung,
<tb> 0,300 <SEP> <SEP> Mangan,
<tb> 0,800 <SEP> <SEP> Eisen <SEP> und
<tb> 6,500 <SEP> <SEP> Silizium <SEP> nacheinander <SEP> zugesetzt.
<tb> 100 <SEP> kg,.
Heat treatable light metal alloy and process for its production The present invention relates to a heat treatable light metal alloy which has the following composition Cu 0.9-1.70 / 0. Si 6.3-6.7 0/0 Mg 0.2-0e4% Mn0.2-0.7% Fe 0.4-1.8% balance aluminum.
This heat treatable light metal alloy has the advantage that it is suitable for very complicated cast parts that are very difficult to cast in terms of casting technology.
With this heat treatable light metal alloy, strength values of up to about 35 kg / mm2 with an elongation of up to 3.51 / o and Brinell hardnesses of up to 130 kg / mm2 can be achieved. Brinell hardnesses of 80 kg / mm2 can be achieved even in the non-tempered state. will..
The alloy according to the invention also has a particularly good resistance to wear.
Furthermore, the heat treatable light metal alloy has particular advantages with regard to its mechanical workability, in that all the additives previously required, such as turpentine and the like, can be dispensed with.
The alloy according to the invention is expediently produced in such a way that the light metal alloy is melted using a master alloy composed of equal parts by weight of copper and aluminum, with the higher-melting components being added last.
FROM <I> f </I> EXAMPLE A master alloy is produced from the same weighted parts aluminum and copper by. The same weight of copper is entered in molten aluminum (pure).
Be used to manufacture the alloy itself
EMI0001.0059
89 <SEP> kg <SEP> pure aluminum <SEP> melted.
<tb> Then become <SEP>
<tb> 0.400 <SEP> kg <SEP> magnesium,
<tb> 3 <SEP> <SEP> of the <SEP> Al-Cu master alloy,
<tb> 0.300 <SEP> <SEP> manganese,
<tb> 0.800 <SEP> <SEP> iron <SEP> and
<tb> 6.500 <SEP> <SEP> silicon <SEP> added one after the other <SEP>.
<tb> 100 <SEP> kg ,.
Claims (1)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH312660T | 1955-08-11 |
Publications (1)
Publication Number | Publication Date |
---|---|
CH312660A true CH312660A (en) | 1956-02-15 |
Family
ID=4494945
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH312660D CH312660A (en) | 1955-08-11 | 1955-08-11 | Heat-treatable light metal alloy and process for their production |
Country Status (1)
Country | Link |
---|---|
CH (1) | CH312660A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2003080883A1 (en) * | 2002-03-19 | 2003-10-02 | Spx Corporation | Aluminum alloy |
-
1955
- 1955-08-11 CH CH312660D patent/CH312660A/en unknown
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2003080883A1 (en) * | 2002-03-19 | 2003-10-02 | Spx Corporation | Aluminum alloy |
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