US3337377A - Process for the treatment of magnesium-silicon aluminum alloys - Google Patents

Process for the treatment of magnesium-silicon aluminum alloys Download PDF

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Publication number
US3337377A
US3337377A US331381A US33138163A US3337377A US 3337377 A US3337377 A US 3337377A US 331381 A US331381 A US 331381A US 33138163 A US33138163 A US 33138163A US 3337377 A US3337377 A US 3337377A
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United States
Prior art keywords
alloys
percent
magnesium
weight
treatment
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Expired - Lifetime
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US331381A
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English (en)
Inventor
Bonmarin Jacques
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Pechiney SA
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Pechiney SA
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/06Alloys based on aluminium with magnesium as the next major constituent
    • C22C21/08Alloys based on aluminium with magnesium as the next major constituent with silicon

Definitions

  • the aluminum alloys which con- In the process according to the invention a quantity of tain magnesium and silicon are capable of being given tin between 0.001 and 0.1 percent and. preferably between improved mechanical properties by quenching from atem- 0.005 and 0.1 percent is added to the aluminum alloy perature at which the metal is entirely or almost entirely containing magnesium and silicon.
  • Typical alloys accordin the state of solid solution. This rapid cooling is then ing to the invention have the following compositions: followed by a natural or artifical aging.
  • Such alloys are magnesium 0 2 to 2% employed either in the cast state or in the transformed si1ic0n 0 2 to'5% state obtained by operations resulting from hot working to 0.1%: or h Such. as forgmg forming rohihg impurities-iron up to 0.5%, others up to 0.2% each, trudlng drawlng and wire-drawing.
  • the mechamcal characteristlcs obtained after quenchaluminum balance ing and artifical aging, or tempering, are proportionally higher for a quenching of given intensity when the time pfeferredhhow whlch are modlfieh 1h accordahfie Wlth elapsed between these two operations is shorter. It is the 1115mm lhventlon have the f llowing compositions;
  • tin is added in amounts of 0.01 percent and 0.1 percent to an alloy, the composition of which is as follows:
  • the alloy to which no tin is added and the two alloys containing the addition are cast into billets, then extruded under the same conditions Without previous homogenization of the billets.
  • the bars which are obtained are heated for two hours to 560 C., and then quenched in water. They are then subjected to an annealing operation which lasts hours at a temperature of 175 C. The annealing is conducted either immediately after the quenching or after an increasingly long period of time.
  • tion are suitable for use in combination with a wide variety of aluminum-magnesium-silicon alloys.
  • the fol- 4 lowing comprises a list of additional elements which may be included in such alloys and which will not affect the improvements provided by the tin additions:
  • alloys of the type described can be utilized. It will be apparent, however, that such additions are contemplated only where they do not interfere with the function of the tin additions described herein.
  • magnesium is present in said alloys in amounts between 0.4 and 1.0 percent by weight
  • silicon is present in said alloys in amounts between 0.4 and 0.8 percent by weight
  • aid iron is present in said alloys in amounts up to 0.5 percent by weight.
  • alloys contain up to 6 percent by weight manganese, up to 6 percent by weight chromium, up to 1 percent by weight titanium, up to 1 percent by weight zirconium, up to 1 percent by weight vanadium and up to 0.1 percent by weight boron.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
US331381A 1962-12-20 1963-12-18 Process for the treatment of magnesium-silicon aluminum alloys Expired - Lifetime US3337377A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR919280A FR1351498A (fr) 1962-12-20 1962-12-20 Procédé pour l'amélioration des alliages d'aluminium contenant du magnésium et du silicium et alliages obtenus

Publications (1)

Publication Number Publication Date
US3337377A true US3337377A (en) 1967-08-22

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US331381A Expired - Lifetime US3337377A (en) 1962-12-20 1963-12-18 Process for the treatment of magnesium-silicon aluminum alloys

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US (1) US3337377A (en:Method)
BE (1) BE641527A (en:Method)
FR (1) FR1351498A (en:Method)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4043840A (en) * 1976-07-09 1977-08-23 Swiss Aluminium Ltd. Aluminum alloys possessing improved resistance weldability
US4244756A (en) * 1978-03-22 1981-01-13 Sumitomo Light Metal Industries, Ltd. Fin stocks for use in heat exchanger made of aluminum alloy and production method thereof
FR2547037A1 (fr) * 1982-03-10 1984-12-07 Sumitomo Precision Prod Co Echangeur a plaques ailettees pour l'emploi a ultra-haute pression
US4861388A (en) * 1986-08-20 1989-08-29 Alcan International Limited Method for contact conductor for electric vehicles
US20190136355A1 (en) * 2012-02-23 2019-05-09 Amag Rolling Gmbh Age-hardenable aluminum alloy and method for improving the ability of a semi-finished or finished product to age artificially

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2076587A (en) * 1935-03-09 1937-04-13 George K Parsons Convertible washing machine construction
US2081951A (en) * 1934-08-15 1937-06-01 Aluminum Co Of America Aluminum-magnesium alloys

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2081951A (en) * 1934-08-15 1937-06-01 Aluminum Co Of America Aluminum-magnesium alloys
US2076587A (en) * 1935-03-09 1937-04-13 George K Parsons Convertible washing machine construction

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4043840A (en) * 1976-07-09 1977-08-23 Swiss Aluminium Ltd. Aluminum alloys possessing improved resistance weldability
US4244756A (en) * 1978-03-22 1981-01-13 Sumitomo Light Metal Industries, Ltd. Fin stocks for use in heat exchanger made of aluminum alloy and production method thereof
FR2547037A1 (fr) * 1982-03-10 1984-12-07 Sumitomo Precision Prod Co Echangeur a plaques ailettees pour l'emploi a ultra-haute pression
US4861388A (en) * 1986-08-20 1989-08-29 Alcan International Limited Method for contact conductor for electric vehicles
US20190136355A1 (en) * 2012-02-23 2019-05-09 Amag Rolling Gmbh Age-hardenable aluminum alloy and method for improving the ability of a semi-finished or finished product to age artificially
US10774409B2 (en) * 2012-02-23 2020-09-15 Amag Rolling Gmbh Age-hardenable aluminum alloy and method for improving the ability of a semi-finished or finished product to age artificially

Also Published As

Publication number Publication date
FR1351498A (fr) 1964-02-07
BE641527A (en:Method) 1964-06-19

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