BE439678A - - Google Patents
Info
- Publication number
- BE439678A BE439678A BE439678DA BE439678A BE 439678 A BE439678 A BE 439678A BE 439678D A BE439678D A BE 439678DA BE 439678 A BE439678 A BE 439678A
- Authority
- BE
- Belgium
- Prior art keywords
- zinc
- additions
- ductility
- aluminum
- corrosion
- Prior art date
Links
- 229910000838 Al alloy Inorganic materials 0.000 claims description 6
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 6
- 239000011701 zinc Substances 0.000 claims description 6
- 229910052725 zinc Inorganic materials 0.000 claims description 6
- 229910045601 alloy Inorganic materials 0.000 claims description 5
- 239000000956 alloy Substances 0.000 claims description 5
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 4
- 239000010936 titanium Substances 0.000 claims description 4
- 229910052719 titanium Inorganic materials 0.000 claims description 4
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 3
- 229910052749 magnesium Inorganic materials 0.000 claims description 3
- 239000011777 magnesium Substances 0.000 claims description 3
- 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 description 2
- 229910052710 silicon Inorganic materials 0.000 claims description 2
- 239000010703 silicon Substances 0.000 claims description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims 1
- 229910052782 aluminium Inorganic materials 0.000 claims 1
- 239000000203 mixture Substances 0.000 claims 1
- 238000007792 addition Methods 0.000 description 8
- 230000007797 corrosion Effects 0.000 description 5
- 238000005260 corrosion Methods 0.000 description 5
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 1
- 229910017708 MgZn2 Inorganic materials 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 229910001297 Zn alloy Inorganic materials 0.000 description 1
- -1 aluminum-magnesium-zinc Chemical compound 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 229910001385 heavy metal Inorganic materials 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 239000011572 manganese Substances 0.000 description 1
- 239000012768 molten material Substances 0.000 description 1
- 238000003303 reheating Methods 0.000 description 1
- 230000035945 sensitivity Effects 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000000844 transformation Methods 0.000 description 1
- 230000009466 transformation Effects 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
- 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)
- Prevention Of Electric Corrosion (AREA)
Description
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"ALLIAGES D'ALUMINIUM AMELIORABLES".
Les alliages d'aluminium améliorables contenant de faibles additions de magnésium,de manganèse et de silicium,et le cas échéant encore du titane ,ont acquis ces derniers temps une importance croissante,surtout parcequ'ils présentent certaines caractéristi- ques de résistance mécanique remarquables et une bonne résistan- ce à la corrosion. Cette dernière propriété provient de ce qu'ils sont exempts de cuivre, ou de métaux lourds similaires,qui diminuent généralement dans une forte mesure la résistance des alliages d'aluminium aux attaques chimiques.
Cependant,il manque à ces alliages d'aluminium la ductilité exigée pour une série de domaines d'applications,particulièrement
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aussi pour les transformations -car flexion,étirage,et refoule- ,ment,ce manque de ductilité s'exprimant par exemple par la faible capacité d'emboutissage . On pourrait améliorer la ductilité par de faibles additions de cuivre,mais ceci serait une mesure inap- plicable dans le présent cas,parce qu'elle met en question la résistance . la corrosion.
@
Des essai;; approfondis ont permis de faire la constatation surprenante qu'une augmentation de la ductilité est obtenu par une addition de zinc jusqu'à. 2%1,préférablement d'environ 0,1% à 0,8% , @ ,surtout en cas d'additions relativement élevées, ' malgré qu'en général le zinc, n'a pas donné de bons résultats comme composante d'alliage d'alluminium parce que par les addi- tions de zinc la sensibilité aux tensions et la corrosion était fortement augmentée.
On connaît un alliage d'aluminium-magnésium-zinc contenant le car, échéant des additions de manganèse, auquel il faut cependant ajouter des additions de magnésium considérablement plus élevées, pour y former le composé MgZn2. L'alliage constitué suivant la présente invention se distingue de¯cet alliage connu,par le fait qu'à. côté d'une résistance mécanique et d'un allongement égaux, il a une bonne capacité d'emboutissage --------- et une résistan- ce considérablement meilleure à la corrosion,surtout à l'état ramolli par...' réchauffage,particulièrement convenable pour les tra- vaux d'emboutissage.
On peut ajouter aux alliages suivant l'invention de faibles quantitésde titane(jusqu'à 0,5%),qui affinent considérablement le grain, d'où il résulte dans 'la. texture un agrandissement de la surface disponible pour le dépôt du reste de la matière en fu- sion sur leslimites des grains.L'augmentation de cette surface amené une augmentation du degré de répartition des composantes hétérogènes qui influencent la ductilité et accessoirement aussi la résistance à la corrosion. L'addition de titane agit dans le même sens que l'addition de zinc.
<Desc / Clms Page number 1>
"IMPROVABLE ALUMINUM ALLOYS".
Improved aluminum alloys containing small additions of magnesium, manganese and silicon, and possibly also titanium, have recently acquired increasing importance, above all because they exhibit certain remarkable mechanical strength characteristics and good corrosion resistance. The latter property results from the fact that they are free from copper, or similar heavy metals, which generally greatly reduce the resistance of aluminum alloys to chemical attack.
However, these aluminum alloys lack the ductility required for a variety of fields of application, particularly
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also for transformations -car bending, stretching, and upsetting, this lack of ductility being expressed for example by the low drawing capacity. The ductility could be improved by small additions of copper, but this would be an inapplicable measure in this case, because it calls into question the resistance. corrosion.
@
Tests ;; Further investigations have made it possible to make the surprising finding that an increase in ductility is obtained by adding up to zinc. 2% 1, preferably about 0.1% to 0.8%, @, especially in the case of relatively high additions, although in general zinc, has not given good results as a component of aluminum alloy because by the additions of zinc the sensitivity to stress and corrosion was greatly increased.
An aluminum-magnesium-zinc alloy is known which contains, as appropriate, additions of manganese, to which must however be added considerably higher additions of magnesium, in order to form the compound MgZn2 therein. The alloy formed according to the present invention is distinguished from this known alloy, in that. Besides equal mechanical strength and elongation, it has good drawing capacity --------- and considerably better resistance to corrosion, especially in the softened state by .. Reheating, particularly suitable for stamping work.
Small amounts of titanium (up to 0.5%) can be added to the alloys according to the invention, which considerably refine the grain, thereby resulting in the. texture an enlargement of the surface available for the deposition of the rest of the molten material on the grain boundaries. The increase in this surface leads to an increase in the degree of distribution of the heterogeneous components which influence the ductility and secondarily also the resistance to corrosion. The addition of titanium acts in the same direction as the addition of zinc.
Claims (1)
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE439678A true BE439678A (en) |
Family
ID=97621
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE439678D BE439678A (en) |
Country Status (1)
| Country | Link |
|---|---|
| BE (1) | BE439678A (en) |
-
0
- BE BE439678D patent/BE439678A/fr unknown
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