High-strength aluminum alloy extruded material with excellent corrosion resistance and method of producing the same

Inactive Publication Date: 2006-11-02
THE SOC OF JAPANESE AEROSPACE +2
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

[0009] The inventors of the present invention conducted experiments and examinations in order to solve the above-described problems and to obtain a corrosion-resistant, high-strength aluminum alloy extruded product exhibiting further stable extrudability based on the proposed aluminum alloy composition and extrusion conditions. As a result, the inventors found that an aluminum alloy extrude

Problems solved by technology

However, these aluminum alloys do not necessarily exhibit sufficient corrosion resistance, and tend to produce cracks due to inferior extrudability.
Therefore, since these aluminum alloys must be extruded at a low extrusion rate, manufacturing cost is increased.
Moreover, it is difficult to extrude these aluminum alloys into a hollow product by using a porthole die or a spider die.
Therefore, since it is necessary to form a desired structure by combining solid profiles, the application range of these aluminum alloys is limited.
However, the 6000 series alloy exhibits insufficient strength in comparison with the 7000 series (Al—Zn—Mg) or 2000 series (Al—Cu) high-strength aluminum alloy.
However, these alloys do not necessarily exhibit stre

Method used

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  • High-strength aluminum alloy extruded material with excellent corrosion resistance and method of producing the same
  • High-strength aluminum alloy extruded material with excellent corrosion resistance and method of producing the same
  • High-strength aluminum alloy extruded material with excellent corrosion resistance and method of producing the same

Examples

Experimental program
Comparison scheme
Effect test

example 1

[0051] An aluminum alloy having a composition shown in Table 1 was cast by semicontinuous casting to prepare a billet with a diameter of 100 mm. The billet was homogenized at 525° C. for eight hours to prepare an extrusion billet.

[0052] The extrusion billet was heated to 480° C. and extruded by using a solid die at an extrusion ratio of 27 and an extrusion rate of 3 m / min to obtain a quadrilateral solid extruded product having a thickness of 12 mm and a width of 24 mm. The solid die had a bearing length of 6 mm, and the corners of an orifice were rounded off with a radius of 0.5 mm. A flow guide attached to the die had a quadrilateral guide hole. The distance (A) from the inner circumferential surface of the guide hole to the outer circumferential surface of the orifice was set at 15 mm, and the thickness (B) of the flow guide was set at 15 mm with respect to the billet diameter of 100 mm (B=15% of billet diameter).

[0053] The resulting solid extruded product was subjected to a sol...

example 2

[0063] The aluminum alloy A having the composition shown in Table 1 was cast by semicontinuous casting to prepare a billet with a diameter of 100 mm. The billet was homogenized at 500° C. and extruded into a quadrilateral solid extruded product (thickness: 12 mm, width: 24 mm) by using a solid die having a bearing length shown in Table 5. The extrusion temperature was 480° C. except for a specimen No. 34 (430° C.), and the extrusion rate was 3 m / min.

[0064] The solid extruded product was subjected to press quenching or quenching under conditions shown in Table 5, and was heat treated under the same conditions as in Example 1 to obtain T6 temper material. In Table 5, the quenching cooling rate is the average cooling rate from the solution heat treatment temperature to 100° C. A controlled atmosphere furnace was used for the solution heat treatment.

[0065] The resulting T6 material was used as a specimen and subjected to (1) grain size measurement in the cross section perpendicular to...

example 3

[0073] An aluminum alloy having a composition shown in Table 1 was cast by semicontinuous casting to prepare a billet with a diameter of 200 mm. The billet was homogenized at 525° C. for eight hours to prepare an extrusion billet. The extrusion billet was extruded (extrusion ratio: 20) into a tubular product having an outer diameter of 30 mm and an inner diameter of 20 mm at an extrusion temperature of 480° C. and an extrusion rate of 3 m / min by using a porthole die in which the ratio of the chamber depth D to the bridge width W was 0.5 to 0.6. The ratio of the flow speed of the aluminum alloy in the joining section of the die to the flow speed of the aluminum alloy in the non-joining section was 1.3 to 1.4.

[0074] The resulting tubular extruded product was subjected to a solution heat treatment by heating the extruded product to 530° C. at a temperature rise rate of 10° C. / sec, and subjected to water quenching within 10 seconds after completion of the solution heat treatment. The q...

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Abstract

The present invention provides a high-strength aluminum alloy extruded product exhibiting excellent corrosion resistance and secondary workability and suitably used as a structural material for transportation equipment such as automobiles, railroad vehicles, and aircrafts, and a method of manufacturing the same. The aluminum alloy extruded product has a composition containing 0.6 to 1.2% of Si, 0.8 to 1.3% of Mg, and 1.3 to 2.1% of Cu while satisfying the following conditional expressions (1), (2), (3), and (4),
3%≦Si %+Mg %+Cu %≦4%   (1)
Mg %≦1.7×Si %   (2)
Mg %+Si %≦2.7%   (3)
Cu %/2≦Mg %≦(Cu %/2)+0.6%   (4)
and further containing 0.04 to 0.35% of Cr, and 0.05% or less of Mn as an impurity, with the balance being aluminum and unavoidable impurities. The cross section of the extruded product has a recrystallized structure with an average grain size of 500 μm or less. The manufacturing method includes, when extruding the aluminum alloy into a solid product by using a solid die, extruding the aluminum alloy by using a solid die in which a bearing length (L) is 0.5 mm or more and the bearing length (L) and the thickness (T) of the solid product have a relationship expressed as “L≦5 T”, and, when extruding the aluminum alloy into a hollow product by using a porthole die or a bridge die, extruding the aluminum alloy while setting the ratio of the flow speed of the aluminum alloy in a non-joining section to the flow speed of the aluminum alloy in a joining section in a chamber, where the billet reunites after entering a port section of the die in divided flows and subsequently encircling a mandrel, at 1.5 or less.

Description

TECHNICAL FIELD [0001] The present invention relates to a high-strength aluminum alloy extruded product exhibiting excellent corrosion resistance. More particularly, the present invention relates to a method of manufacturing a high-strength aluminum alloy extruded product exhibiting excellent corrosion resistance and suitably used as a structural material for transportation equipment such as automobiles, railroad vehicles, and aircrafts. BACKGROUND ART [0002] A structural material for transportation equipment such as automobiles, railroad vehicles, and aircrafts is required to have performance such as (1) strength, (2) corrosion resistance, and (3) fracture mechanics properties (such as fatigue crack propagation resistance and fracture toughness). A recent material development trend involves overall evaluation including not only strength, but also production, assembly, and operation of the material. [0003] As high-strength aluminum alloys, an Al—Cu—Mg aluminum alloy (2000 series) an...

Claims

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Application Information

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IPC IPC(8): C22F1/04C22C21/12B21C23/00B21C23/08B21C25/02C22C21/14C22C21/16
CPCB21C23/002B21C23/08C22C21/16B21C25/025C22C21/14B21C25/02
Inventor SANO, HIDEOYOSHINO, YASUAKI
Owner THE SOC OF JAPANESE AEROSPACE
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