US2003143101A1PendingUtilityA1
Aluminum die casting alloy, aluminum die cast product and production process
Est. expiryOct 25, 2020(expired)· nominal 20-yr term from priority
Inventors:Sanji KitaokaYukio KuramasuSyuichi AsakunoKenji TsushimaMasahiko ShiodaHiroshi KambeShinichiro SumiTakaaki Ikari
C22F 1/047C22C 21/08
48
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Claims
Abstract
An aluminum alloy for die casting, contains, in terms of mass percentage: Si in the range of 1.0˜3.5 %; Mg in the range of 2.5˜4.5 %; Mn in the range of 0.3˜1.5%; Fe in the range equal to or less than 0.15%; Ti in the range of equal to or less than 0.20%; and the balance of aluminum and inevitable impurities. A die cast product having good strength and elongation in a high strain rate region is produced from the aluminum alloy without the need for solution heat treatment.
Claims
exact text as granted — not AI-modifiedWhat is claimed is:
1 . An aluminum alloy for die casting, comprising, in terms of mass ratio:
silicon in the range of 1.0˜3.5%; magnesium in the range of 2.5˜4.5%; manganese in the range of 0.3˜1.5%; iron in the range equal to or less than 0.15%; a further constituent comprising titanium in the range of equal to or less than 0.20%; and the balance of aluminum and inevitable impurities.
2 . The aluminum alloy as claimed in claim 1 , wherein the further constituent consists of titanium, and the aluminum alloy consists essentially, in terms of mass ratio, of:
silicon in the range of 1.0˜3.5%; magnesium in the range of 2.5˜4.5%; manganese in the range of 0.3˜1.5%; iron in the range equal to or less than 0.15%; titanium in the range of equal to or less than 0.20%; and the balance of aluminum and inevitable impurities.
3 . The aluminum alloy as claimed in claim 2 , wherein the Ti content is 0.10% or more.
4 . The aluminum alloy as claimed in claim 1 , wherein the further constituent consists of titanium and boron, and the aluminum alloy consists essentially, in terms of mass ratio, of:
silicon in the range of 1.0˜3.5%; magnesium in the range of 2.5˜4.5%; manganese in the range of 0.3˜1.5%; iron in the range equal to or less than 0.15%; titanium in the range of 0.05˜0.20%; boron in the range of 0.001˜0.10%; and the balance of aluminum and inevitable impurities.
5 . The aluminum alloy as claimed in claim 1 , wherein the further constituent consists of titanium and zirconium, and the aluminum alloy consists essentially, in terms of mass ratio, of
silicon in the range of 1.0˜3.5%; magnesium in the range of 2.5˜4.5%; manganese in the range of 0.3˜1.5%; iron in the range equal to or less than 0.15%; titanium in the range equal to or smaller than 0.20%; zirconium in the range of 0.05˜0.30%; and the balance of aluminum and inevitable impurities.
6 . The aluminum alloy as claimed in claim 1 , wherein the Mn content is equal to or more than 1.0%.
7 . The aluminum alloy as claimed in claim 1 , wherein the Si content is equal to or more than 2.5%.
8 . The aluminum alloy as claimed in claim 1 , wherein the Si content is equal to or less than 2.0%.
9 . The aluminum alloy as claimed in claim 1 , wherein a ratio of the Mg content in mass %, to the Si content in mass % is equal to or smaller than 2.0.
10 . The aluminum alloy as claimed in claim 1 , wherein a ratio of the Mg content in mass %, to the Si content in mass % is equal to or greater than 1.8.
11 . A product comprising an aluminum die casting of the aluminum alloy as claimed in claim 1 .
12 . The product as claimed in claim 11 , wherein the product is a part of a motor vehicle.
13 . A production process comprising:
preparing an aluminum alloy comprising, in terms of mass ratio,
silicon in the range of 1.0˜3.5%,
magnesium in the range of 2.5˜4.5%,
manganese in the range of 0.3˜1.5%,
iron in the range equal to or less than 0.15%,
a further constituent comprising titanium in the range equal to or less than 0.20%, and
the balance of aluminum and inevitable impurities; and
forming the aluminum alloy into a fixed shape by die casting operation.
14 . The production process as claimed in claim 13 , wherein the die casting is vacuum die casting.
15 . The production process as claimed in claim 13 , wherein a ratio of the Mg content in mass % to the Si content in mass % of the aluminum alloy is equal to or greater than 1.8; and the production process further comprises heat-treating a die-casting obtained by the die casting operation, in the temperature range of 130° C.˜300° C. after the die casting operation.
16 . The production process as claimed in claim 15 , wherein the operation of heat-treating is one of an artificial aging operation and a stabilizing operation.
17 . The production process as claimed in claim 15 , wherein the operation of heat-treating comprises at least one of an annealing operation, and a baking operation of baking a coating layer.
18 . The production process as claimed in claim 13 , wherein a ratio of the Mg content in mass % to the Si content in mass % of the aluminum alloy is equal to or smaller than 2.0; and the production process further comprises stabilizing treatment in the temperature range of 150° C.˜400° C. of stabilizing a die-casting obtained by the die casting operation.
19 . A product comprising an aluminum die casting produced by the production process as claimed in claim 13 .
20 . The product as claimed in claim 19 , wherein the product is one of A pillar, B pillar, C pillar, roof, space frame node, and fitting for suspension of a motor vehicle.
21 . The product as claimed in claim 19 , wherein the product is one of suspension arm, sub-frame and link for suspension.Join the waitlist — get patent alerts
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