BE400249A - - Google Patents
Info
- Publication number
- BE400249A BE400249A BE400249DA BE400249A BE 400249 A BE400249 A BE 400249A BE 400249D A BE400249D A BE 400249DA BE 400249 A BE400249 A BE 400249A
- Authority
- BE
- Belgium
- Prior art keywords
- cold
- alloys
- worked
- annealing
- aluminum
- Prior art date
Links
- 229910045601 alloy Inorganic materials 0.000 claims description 8
- 239000000956 alloy Substances 0.000 claims description 8
- 238000000137 annealing Methods 0.000 claims description 6
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 5
- 238000000034 method Methods 0.000 claims description 4
- 229910000838 Al alloy Inorganic materials 0.000 claims description 3
- 229910000861 Mg alloy Inorganic materials 0.000 claims description 3
- 239000011701 zinc Substances 0.000 claims description 3
- 229910052725 zinc Inorganic materials 0.000 claims description 3
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 2
- 229910052751 metal Inorganic materials 0.000 claims description 2
- 239000002184 metal Substances 0.000 claims description 2
- 150000002739 metals Chemical class 0.000 claims description 2
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 claims 1
- 238000001953 recrystallisation Methods 0.000 claims 1
- 229910052782 aluminium Inorganic materials 0.000 description 3
- 239000011777 magnesium Substances 0.000 description 3
- 239000011572 manganese Substances 0.000 description 3
- 239000003518 caustics Substances 0.000 description 2
- 231100001010 corrosive Toxicity 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 229910052749 magnesium Inorganic materials 0.000 description 2
- 229910052748 manganese Inorganic materials 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000002425 crystallisation Methods 0.000 description 1
- 230000008025 crystallization Effects 0.000 description 1
- 239000013535 sea water Substances 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
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
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Metal Rolling (AREA)
Description
<Desc/Clms Page number 1>
"Procédé pour augmenter la résistance à la corrosion des alliages d'aluminium et de magnésium travaillés à froid".
On. sait que le travail à froid des alliages d'aluminium et de magnésium, utilisables dans 1'industrie, présente l'inconvé- nient suivant : ces alliages étant mis en contact avec des milieux corrosifs, l'eau de mer en particulier, il se produit, à la longue, des modifications de structure qui provoquent la formation de fis- sures ou d'écaillés et par suite un ac croissement de l'attaque par 1'agent corrosif.
Ces phénomènes se manifestent de façon analogue pour les alliages, également connus, qui contiennent en faible quantité, outre l'aluminium et le magnésium, d'autres métaux tels que du zinc et/ou du manganèse destinés à augmenter leurs proprié-
EMI1.1
tés d1-r6sistance. pour .supprimer ces inconvénients, conformément à la pré-
<Desc/Clms Page number 2>
sente invention, on soumet les alliages, moulés froid, ' un traitement de recuit à des températures inférieures à celle re à laquelle pour une même durée de recuit commencerait la/cris- tallisation.
La valeur de la température et la-durée du trai- tement varient dans certaines limites, suivant la composition @ de l'alliage et la nature de son traitement préalable par dé- formation à froid ; en général, on a constaté qu'un recuit à 150-200 0 environ, pendant à peu près une heure, donne de bons résultats. Le recuit provoque une modification telle de la structure de l'alliage, que la résistance mécanique, à l'action des corrosifs des pièces d'usinage travaillées à froid est con- sidérablement accrue, et qu'il ne se forme pratiquement plus de fissures ni d'écailles.
Voici, à titre d'exemples non limitatifs, deux compositions d'alliages sur lesquels on a expérimenté avec un succès parti- culièremet frappant le procédé de traitement conforme à l'in- vention ; Ce sont : 1) 7 % d'Al, 1% de Zn, 0,3 de Mn, le reste étant du Mg 2) 9% de Mg, 0,5 % de Mn, le reste étant de l'aluminium.
Le procédé de traitement conforme à l'invention s'appli- que particulièrement bien aux t8les laminées, profilés, etc.., qui soiit somises à froid (comme suite au travail à. chaud) à un laminagp ou à tout autre travail d'usinage complémentaire.
<Desc / Clms Page number 1>
"Process for increasing the corrosion resistance of cold worked aluminum and magnesium alloys".
We. knows that the cold working of aluminum and magnesium alloys, which can be used in industry, has the following drawback: these alloys being brought into contact with corrosive media, seawater in particular, it is over time produces structural changes which lead to the formation of cracks or flakes and hence increased attack by the corrosive agent.
These phenomena are manifested in a similar way for the alloys, also known, which contain in small quantities, in addition to aluminum and magnesium, other metals such as zinc and / or manganese intended to increase their properties.
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resistance tees. to eliminate these drawbacks, in accordance with the pre-
<Desc / Clms Page number 2>
According to this invention, the cold-cast alloys are subjected to an annealing treatment at temperatures below that at which, for the same annealing time, crystallization would begin.
The value of the temperature and the duration of the treatment vary within certain limits, depending on the composition of the alloy and the nature of its pretreatment by cold deformation; in general it has been found that annealing at about 150-200 0 for about an hour gives good results. Annealing causes such a change in the structure of the alloy that the mechanical resistance to the action of corrosives of the cold-worked machining parts is considerably increased, and practically no more cracks are formed. no scales.
Here are, by way of nonlimiting examples, two alloy compositions on which the treatment process according to the invention has been tested with particularly striking success; These are: 1) 7% Al, 1% Zn, 0.3 Mn, the remainder being Mg 2) 9% Mg, 0.5% Mn, the remainder being aluminum.
The treatment process according to the invention is particularly suitable for rolled sheets, sections, etc., which are cold (as a result of hot work), laminated or any other cold work. additional machining.
Claims (1)
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE400249A true BE400249A (en) |
Family
ID=66401
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE400249D BE400249A (en) |
Country Status (1)
| Country | Link |
|---|---|
| BE (1) | BE400249A (en) |
-
0
- BE BE400249D patent/BE400249A/fr unknown
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