CH239996A - Aluminum alloy, suitable for bar turning and stamping. - Google Patents
Aluminum alloy, suitable for bar turning and stamping.Info
- Publication number
- CH239996A CH239996A CH239996DA CH239996A CH 239996 A CH239996 A CH 239996A CH 239996D A CH239996D A CH 239996DA CH 239996 A CH239996 A CH 239996A
- Authority
- CH
- Switzerland
- Prior art keywords
- alloy
- stamping
- possibility
- alloy according
- additionally
- Prior art date
Links
- 229910000838 Al alloy Inorganic materials 0.000 title claims description 5
- 229910045601 alloy Inorganic materials 0.000 claims description 15
- 239000000956 alloy Substances 0.000 claims description 15
- 238000003754 machining Methods 0.000 claims description 6
- 229910052782 aluminium Inorganic materials 0.000 claims description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 4
- 238000005242 forging Methods 0.000 claims description 4
- 229910052797 bismuth Inorganic materials 0.000 claims description 3
- 229910052793 cadmium Inorganic materials 0.000 claims description 3
- 229910052718 tin Inorganic materials 0.000 claims description 3
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 2
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims description 2
- 230000015572 biosynthetic process Effects 0.000 claims description 2
- JCXGWMGPZLAOME-UHFFFAOYSA-N bismuth atom Chemical compound [Bi] JCXGWMGPZLAOME-UHFFFAOYSA-N 0.000 claims description 2
- BDOSMKKIYDKNTQ-UHFFFAOYSA-N cadmium atom Chemical compound [Cd] BDOSMKKIYDKNTQ-UHFFFAOYSA-N 0.000 claims description 2
- 239000011248 coating agent Substances 0.000 claims description 2
- 238000000576 coating method Methods 0.000 claims description 2
- 239000012535 impurity Substances 0.000 claims description 2
- 239000000314 lubricant Substances 0.000 claims description 2
- 229910052749 magnesium Inorganic materials 0.000 claims description 2
- 239000011777 magnesium Substances 0.000 claims description 2
- 230000003647 oxidation Effects 0.000 claims description 2
- 238000007254 oxidation reaction Methods 0.000 claims description 2
- 229910052710 silicon Inorganic materials 0.000 claims description 2
- 239000010703 silicon Substances 0.000 claims description 2
- 239000000126 substance Substances 0.000 claims description 2
- 229910052716 thallium Inorganic materials 0.000 claims description 2
- BKVIYDNLLOSFOA-UHFFFAOYSA-N thallium Chemical compound [Tl] BKVIYDNLLOSFOA-UHFFFAOYSA-N 0.000 claims description 2
- 229910052751 metal Inorganic materials 0.000 description 11
- 239000002184 metal Substances 0.000 description 11
- 150000002739 metals Chemical class 0.000 description 9
- 238000007792 addition Methods 0.000 description 8
- 238000010438 heat treatment Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 2
- 229910001369 Brass Inorganic materials 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- 239000010951 brass Substances 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000000265 homogenisation Methods 0.000 description 1
- 238000003475 lamination Methods 0.000 description 1
- 229910052745 lead Inorganic materials 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000004848 polyfunctional curative Substances 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 238000007670 refining Methods 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 238000005496 tempering Methods 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 229910052726 zirconium Inorganic materials 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
- C22C21/003—Alloys based on aluminium containing at least 2.6% of one or more of the elements: tin, lead, antimony, bismuth, cadmium, and titanium
-
- 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
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Forging (AREA)
Description
Alliage d'aluminium, propre au décolletage et à l'estampage. Un alliage,d'aluminium, propre au décol letage doit présenter, ainsi qu'il est connu, les propriétés suivantes: Usinage facile avec ou sans lubrifiant, Formation :de fins copeaux facilement éli minés du nez de l'outil, Possibilité :de travail sur un tour automa tique et en particulier à des vitesses de, tra vail élevées, Surface d'usinage des pièces lisse et bril lante, Possibilité d'oxydation chimique ou élec trolytique :de cette surface, et de revêtement galvanique.
Dans certains cas, il est en outre intéres sant qu'un tel alliage se prête très facilement aux opérations de forgeage, matriçage, -estam page, normalement utilisées pour la fabrica tion :d'un très grand nombre de pièces.
La présents invention a pour objet un alliage d'aluminium renfermant, à côté de l'aluminium, outre les impuretés habituelles de ce métal, de 0,10 à<B>570</B> :de silicium et de 0,05 à 3 % de magnésium, et réunissant l'en semble des propriétés. énumérées ci-dessus.
Cet alliage peut en outre contenir de 0,3 à 4 % .d'un des métaux suivants: Plomb, étain, bismuth, cadmium, thallium, pour -augmenter la finesse -des copeaux :d'usinage.
Il peut même éventuellement renfermer à la fois plusieurs de ces métaux, avec une te neur totale comprise entre les mêmes limites de 0,3à4%.
Les propriétés; générales de l'alliage peu vent être améliorées par les additions connues pour affiner le grain, ces additions dont le taux total doit "être inférieur à 2 % peuvent comprendre un ou plusieurs des métaux sui vants Ti, V, Mo, Mn, Cr, Zr, W.
Pour augmenter les caractéristiques méca niques, tout en conservant les autres proprié tés mentionnées, on peut encore ajouter des métaux connus pour produire, au sein du mé tal, des composés :durcissants, :c'est-à-dire qui améliorent les caractéristiques mécaniques. notamment après traitement thermique.
Ces métaux peuvent être: Cu jusqu'à, <B>6%,</B> Ni 4 Zn 1() %. Les additions de Pb, Bi, Sn, Cd. T1 peu vent être faites par toutes méthodes connues: addition directe de ces métaux, soit purs, soit alliés ensemble, addition par alliage-mère con tenant de l'aluminium et un ou plusieurs des métaux d'addition, addition par réaction chi mique, les sels des métaux à ajouter étant; versés à la. surface du bain d'aluminium ou d'alliages fondus.
Les autres additions (affinantes, durcis santes) sont faites par l'un ou l'autre des pro cédés connus et en particulier par ceux énu mérés ci-dessus.
L'alliage peut être utilisé suivant les cas, soit comme alliage de fonderie, c'est-à-dire à l'état coulé, soit comme alliage dé forge, c'est à-dire après transformation mécanique telle que: forgeage, matriçage, laminage, etc. L'al liage à l'état transformé peut être utilisé écroui ou recuit. Qu'il soit à, l'état coulé ou î( l'état transformé, il peut subir un traitement thermique d'homogénéisation (chauffage entre 450 et 5î0 de 30' à 1() h.) .suivi soit d'un simple vieillissement à température ambiante.
soit d'un revenu à température plus élevée pouvant aller ,jusqu'à 300 et d'une durée va riable suivant la température utilisée e1, les caractéristiques recherchées.
A titre d'exemple, non limitatif, illustrant la. présente invention. et dans le simple but d'en faire comprendre l'intérêt, on citera la composition suivante: Fe = I),20, ô Si = 1,45% <B>Mg-</B> = 1,04 Pb = 2,56 Al = le reste.
Un tel alliage donne sur barres filée.; lorsqu'il a subi un traitement de trempe à l'eau après chauffage à 550 , suivi d'un venu à 175 : Limite élastique: L. E. = 21 kg/mm2; Résistance à la traction: R = 30,5 kg/mm'.
Allongement à la rupture: A = 19 %. Dans les conditions normales d'usinage, cet. alliage donne des copeaux identiques à ce1(x du laiton de décolletage.
Aluminum alloy, suitable for bar turning and stamping. An aluminum alloy suitable for peeling must have, as is known, the following properties: Easy machining with or without lubricant, Formation: fine chips easily removed from the nose of the tool, Possibility: of working on an automatic lathe and in particular at high working speeds, Smooth and shiny machining surface of the parts, Possibility of chemical or electrolytic oxidation: of this surface, and of galvanic coating.
In certain cases, it is also advantageous that such an alloy lends itself very easily to forging, stamping, -estam page operations, normally used for the manufacture: of a very large number of parts.
The present invention relates to an aluminum alloy containing, besides aluminum, in addition to the usual impurities of this metal, from 0.10 to <B> 570 </B>: of silicon and from 0.05 to 3% magnesium, and bringing together all the properties. listed above.
This alloy may also contain from 0.3 to 4%. Of one of the following metals: lead, tin, bismuth, cadmium, thallium, to -increase the fineness of the machining chips:
It may even possibly contain several of these metals at the same time, with a total content of between the same limits of 0.3 to 4%.
Properties; General information of the alloy can be improved by the known additions to refine the grain, these additions, the total rate of which must "be less than 2%, can comprise one or more of the following metals Ti, V, Mo, Mn, Cr, Zr, W.
To increase the mechanical characteristics, while retaining the other properties mentioned, it is also possible to add metals known to produce, within the metal, compounds: hardeners,: that is to say which improve the mechanical characteristics . especially after heat treatment.
These metals can be: Cu up to, <B> 6%, </B> Ni 4 Zn 1 ()%. The additions of Pb, Bi, Sn, Cd. T1 can be made by any known methods: direct addition of these metals, either pure or alloyed together, addition by parent alloy containing aluminum and one or more of the metals. addition metals, addition by chemical reaction, the salts of the metals to be added being; paid to the. bath surface of molten aluminum or alloys.
The other additions (refining, hardening) are made by one or the other of the known processes and in particular by those enu merited above.
The alloy can be used depending on the case, either as a foundry alloy, that is to say in the cast state, or as a forging alloy, that is to say after mechanical transformation such as: forging, stamping , lamination, etc. The bonding in the transformed state can be used cold or annealed. Whether it is in, the cast state or the transformed state, it can undergo a heat treatment of homogenization (heating between 450 and 50 from 30 'to 1 () h.). Followed either by a simple aging at room temperature.
or a higher temperature tempering which can range up to 300 and of a variable duration depending on the temperature used e1, the desired characteristics.
By way of nonlimiting example illustrating the. present invention. and for the simple purpose of making it understandable, we can cite the following composition: Fe = I), 20, ô Si = 1.45% <B> Mg- </B> = 1.04 Pb = 2 , 56 Al = the remainder.
Such an alloy gives on extruded bars .; when it has undergone a quenching treatment with water after heating to 550, followed by a come to 175: Yield strength: L. E. = 21 kg / mm2; Tensile strength: R = 30.5 kg / mm '.
Elongation at break: A = 19%. Under normal machining conditions, this. alloy gives shavings identical to ce1 (x free-cutting brass.
Claims (1)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR239996X | 1942-07-30 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CH239996A true CH239996A (en) | 1945-11-30 |
Family
ID=8883198
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CH239996D CH239996A (en) | 1942-07-30 | 1943-07-27 | Aluminum alloy, suitable for bar turning and stamping. |
Country Status (1)
| Country | Link |
|---|---|
| CH (1) | CH239996A (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1034369B (en) * | 1951-10-06 | 1958-07-17 | Gen Motors Corp | Use of aluminum alloys for plain bearings |
| DE2235168A1 (en) * | 1971-07-20 | 1973-02-01 | British Aluminium Co Ltd | ALUMINUM ALLOYS, METHOD OF MANUFACTURING AND USING THEREOF |
| DE2456866A1 (en) * | 1974-12-02 | 1976-08-12 | Sumitomo Light Metal Ind | ALUMINUM BASED ALLOY |
| DE3518407A1 (en) * | 1984-05-25 | 1985-11-28 | Sumitomo Light Metal Industries Ltd., Tokio/Tokyo | FIBER MATERIAL AND ITS USE IN PLATE HEAT EXCHANGERS WITH COOLING RIBS, SUITABLE FOR HIGH PRESSURE OPERATION |
| DE3913537A1 (en) * | 1989-04-25 | 1990-10-31 | Teves Gmbh Alfred | Aluminium alloy contg. bismuth instead of lead - to give good machinability and anodising properties |
| EP1098009A3 (en) * | 1999-11-05 | 2001-05-30 | Firma Otto Fuchs | Aluminium alloy of AlMgSi type with Sn and Mn |
| DE10249051B4 (en) * | 2001-11-07 | 2005-07-28 | Miba Gleitlager Ag | Aluminum alloy for a sliding element |
-
1943
- 1943-07-27 CH CH239996D patent/CH239996A/en unknown
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1034369B (en) * | 1951-10-06 | 1958-07-17 | Gen Motors Corp | Use of aluminum alloys for plain bearings |
| DE2235168A1 (en) * | 1971-07-20 | 1973-02-01 | British Aluminium Co Ltd | ALUMINUM ALLOYS, METHOD OF MANUFACTURING AND USING THEREOF |
| DE2456866A1 (en) * | 1974-12-02 | 1976-08-12 | Sumitomo Light Metal Ind | ALUMINUM BASED ALLOY |
| DE3518407A1 (en) * | 1984-05-25 | 1985-11-28 | Sumitomo Light Metal Industries Ltd., Tokio/Tokyo | FIBER MATERIAL AND ITS USE IN PLATE HEAT EXCHANGERS WITH COOLING RIBS, SUITABLE FOR HIGH PRESSURE OPERATION |
| DE3913537A1 (en) * | 1989-04-25 | 1990-10-31 | Teves Gmbh Alfred | Aluminium alloy contg. bismuth instead of lead - to give good machinability and anodising properties |
| EP1098009A3 (en) * | 1999-11-05 | 2001-05-30 | Firma Otto Fuchs | Aluminium alloy of AlMgSi type with Sn and Mn |
| DE19953212A1 (en) * | 1999-11-05 | 2001-05-31 | Fuchs Fa Otto | Wrought aluminum alloy |
| DE10249051B4 (en) * | 2001-11-07 | 2005-07-28 | Miba Gleitlager Ag | Aluminum alloy for a sliding element |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US10458009B2 (en) | Free-machining wrought aluminium alloy product and manufacturing process thereof | |
| US5522950A (en) | Substantially lead-free 6XXX aluminum alloy | |
| TWI700380B (en) | Free-cutting leadless copper alloy with no lead and bismuth | |
| JPWO2006016442A1 (en) | Copper-base alloy castings with refined crystal grains | |
| JP3891933B2 (en) | High strength magnesium alloy and method for producing the same | |
| JP2015519475A5 (en) | Improved free-cutting wrought aluminum alloy product and manufacturing method thereof | |
| JPH0372147B2 (en) | ||
| US9803264B2 (en) | High-plasticity free-cutting zinc alloy | |
| CN112981153B (en) | High-strength high-conductivity aluminum/aluminum alloy composite board and preparation method thereof | |
| JP3107517B2 (en) | High corrosion resistant aluminum alloy extruded material with excellent machinability | |
| CH239996A (en) | Aluminum alloy, suitable for bar turning and stamping. | |
| US3031299A (en) | Aluminum base alloy | |
| US2354006A (en) | Aluminium base alloy with protective coating | |
| JP3846702B2 (en) | Al-Mg-Si aluminum alloy extruded material for cutting | |
| US2195434A (en) | Copper alloy | |
| JP2002206132A (en) | Aluminum alloy extrusion material having excellent machinability and production method therefor | |
| JP2001181770A (en) | Aluminum-based alloy | |
| US2026545A (en) | Free cutting alloys | |
| JP3453607B2 (en) | High-strength aluminum alloy extruded material with excellent chip breaking performance | |
| JPS63312945A (en) | Non heat treatment type high strength free cutting aluminum alloy for cold forging and its production | |
| JPH0678580B2 (en) | Aluminum alloy for forging | |
| JPH1053825A (en) | Copper alloy for lead frame | |
| JP2005213629A (en) | Method for heat treatment of copper alloy, and copper alloy and material | |
| Boyko et al. | Microstructure formation and grain refinement of Al-Mg-Si-Mn casting alloys | |
| US2124572A (en) | Magnesium base alloy |