High strength and high rigidity aluminum-based alloy and...

Metal treatment – Process of modifying or maintaining internal physical... – Heating or cooling of solid metal

Reexamination Certificate

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Details

C075S338000, C164S046000

Reexamination Certificate

active

06331218

ABSTRACT:

BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention relates to an aluminum-based alloy for use in a wide range of applications such as in a structural material for aircraft, vehicles, and ships, and for engine parts. In addition, the present invention may be employed in sashes, roofing materials, and exterior materials for use in construction, or as material for use in marine equipment, nuclear reactors, and the like.
2. Description of Related Art
As prior art aluminum-based alloys, alloys incorporating various components such as Al—Cu, Al—Si, Al—Mg, Al—Cu—Si, Al—Cu—Mg, and Al—Zn—Mg are known. In all of the aforementioned, superior anti-corrosive properties are obtained at a light weight, and thus the aforementioned alloys are being widely used as structural material for machines in vehicles, ships, and aircraft, in addition to being employed in sashes, roofing materials, exterior materials for use in construction, structural material for use in LNG tanks, and the like.
However, the prior art aluminum-based alloys generally exhibit disadvantages such as a low hardness and poor heat resistance when compared to material incorporating Fe. In addition, although some materials have incorporated elements such as Cu, Mg, and Zn for increased hardness, disadvantages remain such as low anti-corrosive properties.
On the other hand, recently, experiments have been conducted in which a fine metallographic structure of aluminum-based alloys is obtained by means of performing quick-quench solidification from a liquid-melt state, resulting in the production of superior mechanical strength and anti-corrosive properties.
In Japanese Patent Application, First Publication No. 1-275732, an aluminum-based alloy comprising a composition AlM
1
X with a special composition ratio (wherein M
1
represents an element such as V, Cr, Mn, Fe, Co, Ni, Cu, Zr and the like, and X represents a rare earth element such as La, Ce, Sm, and Nd, or an element such as Y, Nb, Ta, Mm (misch metal) and the like), and having an amorphous or a combined amorphous/fine crystalline structure, is disclosed.
This aluminum-based alloy can be utilized as material with a high hardness, high strength, high electrical resistance, anti-abrasion properties, or as soldering material. In addition, the disclosed aluminum-based alloy has a superior heat resistance, and may undergo extruding or press processing by utilizing the superplastic phenomenon observed near crystallization temperatures.
However, he aforementioned aluminum-based alloy is disadvantageous in that high costs result from the incorporation of large amounts of expensive rare earth elements and/or metal elements with a high activity such as Y. Namely, in addition to the aforementioned use of expensive raw materials, problems also arise such as increased consumption and labor costs due to the large scale of the manufacturing facilities required to treat materials with high activities. Furthermore, this aluminum-based alloy having the aforementioned composition tends to display insufficient resistance to oxidation and corrosion.
SUMMARY OF THE INVENTION
It is an object of the present invention to provide an aluminum-based alloy, possessing superior strength, rigidity, and anti-corrosive properties, which comprises a composition in which rare earth elements or high activity elements such as Y are not incorporated, thereby effectively reducing the cost, as well as, the activity described in the aforementioned.
In order to solve the aforementioned problems, the present invention provides a high strength and high rigidity aluminum-based alloy consisting essentially of a composition represented by the general formula Al
100−(a+b)
Q
a
M
b
(wherein Q is at least one metal: element selected from the group consisting of V, Mo, Fe, W, Nb, and Pd; M is at least one metal element selected from the group consisting of Mn, Fe, Co, Ni, and Cu; and a and b, which represent a composition ratio in atomic percentages, satisfy the relationships 1≦a≦8, 0<b<5, and 3≦a+b≦8) having a metallographic structure comprising a quasi-crystalline phase, wherein the difference in the atomic radii between Q and M exceeds 0.01 Å, and said alloy does not contain rare earths.
According to the present invention, by adding a predetermined amount of V, Mo, Fe, W, Nb, and/or Pd to Al, the ability of the alloy to form a quasi-crystalline phase is improved, and the strength, hardness, and toughness of the alloy is also improved. Moreover, by adding a predetermined amount of Mn, Fe, Co, Ni, and/or Cu, the effects of quick-quenching are enhanced, the thermal stability of the overall metallographic structure is improved, and the strength and hardness of the resulting alloy are also increased. Fe has both quasi-crystalline phase forming effects and alloy strengthening effects.
The aluminum-based alloy according to the present invention is useful as materials with a high hardness, strength, and rigidity. Furthermore, this alloy also stands up well to bending, and thus possesses superior properties such as the ability to be mechanically processed.
Accordingly, the aluminum-based alloys according to the present invention can be used in a wide range of applications such as in the structural material for aircraft, vehicles, and ships, as well as for engine parts. In addition, the aluminum-based alloys of the present invention may be employed in sashes, roofing materials, and exterior materials for use in construction, or as materials for use in marine equipment, nuclear reactors, and the like.


REFERENCES:
patent: 5433978 (1995-07-01), Shield et al.
patent: 5858131 (1999-01-01), Inoue et al.
patent: 6017403 (2000-01-01), Masumoto et al.
patent: 710730 (1996-05-01), None
patent: 693363 (1994-04-01), None
patent: 6256875 (1994-09-01), None

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