METHOD FOR MANUFACTURING AN INTEGRALLY-FORMED ALLOY STRUCTURE HAVING A BRAZING SURFACE

Abstract

A method for manufacturing an integrally-formed alloy structure having a brazing surface includes the following steps. Firstly, a magnesium-containing alloy is provided. Next, the magnesium-containing alloy is heat treated to obtain a vacuum heat-treated alloy structure. Then, the top surface of the vacuum heat-treated alloy structure is reduced to expose the brazing surface. Finally, the integrally-formed alloy structure having the brazing surface is formed.

Description

CROSS-REFERENCE TO RELATED PATENT APPLICATION

This Application is a Continuation-in-Part of application Ser. No. 16/713,793 filed Dec. 13, 2019, now pending, and entitled “ALLOY STRUCTURE HAVING A LOW MAGNESIUM CONTENT SURFACE,” the entire disclosures of which are incorporated herein by reference.

FIELD OF THE DISCLOSURE

The present disclosure relates to a method for manufacturing an alloy structure, and more particularly to a method for manufacturing an integrally-formed alloy structure having a brazing surface.

BACKGROUND OF THE DISCLOSURE

Aluminum alloy is the most widely used metal material in industrial application. Aluminum alloy has the advantages of low density, high strength, high thermal conductivity, and good processability. With the application of aluminum alloys in the fields of aerospace, automotive, and machinery manufacturing, demands on the brazeability of aluminum alloys continue to increase, and the quality of brazing would directly affect the use of relevant components.

The main element that provides a strengthening effect in aluminum alloys is magnesium (Mg). However, excess magnesium content in aluminum alloys may be one of the reasons that causes poor brazing, which leads to inconsistent yield rates of the joint.

In view of this, the inventor of the present disclosure has been engaged in the development and design of related products for years, and in response to the above-mentioned inadequacies, the present disclosure provides an alloy structure having a low magnesium content surface that can effectively improve on the inadequacies with a more sensible design.

SUMMARY OF THE DISCLOSURE

In response to the above-referenced technical inadequacies, the present disclosure provides a method for manufacturing an integrally-formed alloy structure having a brazing surface for brazing.

In one aspect, the present disclosure provides a method for manufacturing an integrally-formed alloy structure having a brazing surface, including: providing a magnesium-containing alloy; heat treating the magnesium-containing alloy in a vacuum furnace; obtaining a vacuum heat-treated alloy structure including a magnesium-rich layer, a magnesium-deficient layer and an original magnesium-content layer, wherein the magnesium-rich layer is integrally formed on the magnesium-deficient layer, the magnesium-deficient layer is integrally formed on the original magnesium-content layer, the magnesium-rich layer has a higher magnesium content than the original magnesium-content layer, and the magnesium-deficient layer has a lower magnesium content than the original magnesium-content layer; and performing a surface reduction treatment on the vacuum heat-treated alloy structure to reduce the magnesium-rich layer to expose the brazing surface of the magnesium-deficient layer underneath the magnesium-rich layer, so as to form the integrally-formed alloy structure having the brazing surface.

In certain embodiments, the vacuum heat-treated alloy structure is formed at a temperature of between 500° C. and 600° C.

In certain embodiments, the vacuum heat-treated alloy structure is formed by maintaining the temperature for a period of time longer than 30 minutes.

In certain embodiments, the vacuum heat-treated alloy structure is formed at a vacuum degree of lower than 10⁻⁴ torr.

In certain embodiments, a thickness of the magnesium-deficient layer is formed more than 10 μm.

In certain embodiments, the magnesium-containing alloy is a 6000-series aluminum alloy containing magnesium.

One of the advantages of the present disclosure is that the method of the present disclosure can strengthen the brazeability of the surface of the alloy structure by including steps of: heat treating a magnesium-containing alloy in a vacuum furnace, obtaining a vacuum heat-treated alloy structure including a magnesium-rich layer, a magnesium-deficient layer and an original magnesium-content layer, and performing a surface reduction treatment on the vacuum heat-treated alloy structure to reduce the magnesium-rich layer to expose the brazing surface of the magnesium-deficient layer underneath the magnesium-rich layer.

These and other aspects of the present disclosure will become apparent from the following description of the embodiment taken in conjunction with the following drawings and their captions, although variations and modifications therein may be affected without departing from the spirit and scope of the novel concepts of the disclosure.

BRIEF DESCRIPTION OF THE DRAWINGS

The present disclosure will become more fully understood from the following detailed description and accompanying drawings.

FIG. 1 is a schematic view of the alloy structure having a low magnesium content surface of the present disclosure.

FIG. 2 is a schematic view of a treatment method of an alloy surface of the present disclosure.

DETAILED DESCRIPTION OF THE EXEMPLARY EMBODIMENTS

The present disclosure is more particularly described in the following examples that are intended as illustrative only since numerous modifications and variations therein will be apparent to those skilled in the art. Like numbers in the drawings indicate like components throughout the views. As used in the description herein and throughout the claims that follow, unless the context clearly dictates otherwise, the meaning of “a”, “an”, and “the” includes plural reference, and the meaning of “in” includes “in” and “on”. Titles or subtitles can be used herein for the convenience of a reader, which shall have no influence on the scope of the present disclosure.

The terms used herein generally have their ordinary meanings in the art. In the case of conflict, the present document, including any definitions given herein, will prevail. The same thing can be expressed in more than one way. Alternative language and synonyms can be used for any term(s) discussed herein, and no special significance is to be placed upon whether a term is elaborated or discussed herein. A recital of one or more synonyms does not exclude the use of other synonyms. The use of examples anywhere in this specification including examples of any terms is illustrative only, and in no way limits the scope and meaning of the present disclosure or of any exemplified term. Likewise, the present disclosure is not limited to various embodiments given herein. Numbering terms such as “first”, “second” or “third” can be used to describe various components, signals or the like, which are for distinguishing one component/signal from another one only, and are not intended to, nor should be construed to impose any substantive limitations on the components, signals or the like.

Referring to FIG. 1, an embodiment of the present disclosure provides an alloy structure having a low magnesium content surface, as shown in FIG. 1, the alloy structure having a low magnesium content surface of the present disclosure includes an alloy layer 10 having an original magnesium content and a magnesium-deficient layer 20 formed on the alloy layer 10, in which the magnesium-deficient layer has a low magnesium content surface, which strengthens the brazeability of the alloy and improves the yield rate of the joint.

In this embodiment, the original magnesium-content layer (alloy layer 10) is an aluminum alloy with Mg, a magnesium alloy, or a titanium alloy, but the present disclosure is not limited thereto.

In this embodiment, the magnesium-deficient layer 20 and the original magnesium-content layer 10 are integrally formed. Specifically, the low magnesium content surface 201 of the magnesium-deficient layer 20 is formed by removing the surface of the vacuum heat-treated aluminum alloy. Moreover, the magnesium content of the magnesium-deficient layer 20 is less than the magnesium content of the original magnesium-content layer 10.

Further, the aluminum alloy used to make the alloy structure having a low magnesium content surface may include elements such as silicon, copper, lead, aluminum, manganese, nickel, iron, tin, magnesium and others, and unavoidable impurities. The so-called unavoidable impurities are substances that are unavoidably mixed in the raw materials, but do not affect the characteristics of the aluminum alloy, and therefore are regarded as acceptable impurities. The silicon element can be used to increase the strength of the aluminum alloy, the copper element can be used to enhance the hardness of the aluminum alloy, and the lead element can be used to enhance the workability of the aluminum alloy.

Moreover, referring to FIG. 2, the integrally-formed alloy structure having a low magnesium content surface (brazing surface) of the present disclosure can be obtained by an alloy surface treatment method, which mainly includes the following steps:

(a) Vacuum heat treatment: providing a magnesium-containing alloy M on a fixture P and placing it in a vacuum furnace (not shown in the figure), raising the temperature under a heating rate 15° C./min, preferably heating the temperature to 500° C.˜600° C. (if another alloy is used, the temperature is based on the temperature at which the elements on the surface of the alloy becomes active), maintaining the temperature between 500° C. and 600° C. for a period of time (temperature-maintained time) of longer than 30 minutes, and then cooling for a cooling time of less than 120 minutes. The vacuum degree of the vacuum heat treatment is preferably lower than 10⁻⁴ torr. In addition, the magnesium-containing alloy M can also be placed on the fixture P and placed in a protective atmosphere furnace (not shown in the figure), and heated in a protective atmosphere (such as N₂, Ar), the oxygen content preferably being less than 50 ppm.

(b) Obtaining a vacuum heat-treated alloy structure including a magnesium-rich layer 30a having a high magnesium content surface, a magnesium-deficient layer 20a, and an original magnesium-content layer 10a. The magnesium-rich layer 30a is integrally formed on the magnesium-deficient layer 20a, and the magnesium-deficient layer 20a is integrally formed on the original magnesium-content layer 10a. The magnesium-rich layer 30a has a higher magnesium content than the original magnesium-content layer 10a, and the magnesium-deficient layer 20a has a lower magnesium content than the original magnesium-content layer 10a. The magnesium content of the magnesium-rich layer 30a is 0.1-100%. In addition, the thickness of the magnesium-deficient layer 20a depends on the vacuum degree and the temperature-maintained time and maintained temperature of the vacuum heat treatment. The thickness of the magnesium-deficient layer 20a is thicker when the vacuum degree is higher, the temperature-maintained time is longer and the maintained temperature is higher. Further, in the vacuum heat-treated alloy structure, an area from the lower edge of the magnesium-deficient layer 20a to the place where the original magnesium-content layer 10a contacts the fixture P can be an aluminum alloy with the original magnesium content, that is, surfaces of the aluminum alloy that are not exposed and in contact with vacuum will not form the magnesium rich layer 30a nor the magnesium deficient layer 20a.

(c) Surface reduction treatment: the obtained vacuum heat-treated alloy structure is subjected to a surface reduction treatment to reduce/remove the magnesium-rich layer 30a, and a brazing surface (low magnesium content surface) of the magnesium-deficient layer 20a underneath the magnesium-rich layer 30a can be obtained afterward. The brazing surface is a low magnesium content surface 201a of the magnesium-deficient layer 20a, and the magnesium-deficient layer 20a would disappear due to non-vacuum baking above 50° C. in a subsequent process, wherein the higher the temperature, the faster the rate of disappearance will be. Therefore, the magnesium-deficient layer 20a should have a thickness of at least greater than 10 μm to be suitable for brazing. In addition, the surface reduction method can be non-heating thinning methods such as pickling, alkali cleaning, grinding, polishing, etching, or others, or other thinning methods under vacuum or a protective atmosphere or an inert atmosphere, such as plasma cleaning.

Further, the magnesium-containing alloy M of this embodiment can be a 6000-series aluminum alloy containing magnesium (Mg). Due to the Mg element, the 6000-series aluminum alloy has higher strength than a 3000-series or a 1000-series aluminum alloy without Mg element (pure aluminum). Moreover, after softening by high temperature, the 6000-series aluminum alloy can still be used to restore its strength and hardness by a heat treatment process. This method and structure of the present would only slightly change the surface element concentration, and would not greatly affect the overall element content, which effectively maintains the original characteristics of 6000-series aluminum alloys, such as to be able to be heat treated and have strong strength. This method and structure of the present further makes the 6000-series aluminum alloys have a low-magnesium surface similar to the 3000-series and the 1000-series aluminum alloys which have high brazeability.

It should be noted that the method and the alloy structure of the present disclosure can be applied to aluminum alloys as well as other magnesium-containing alloys. In addition, this method and alloy structure are not limited to the removing of the magnesium content, other elements that easily volatilize in the vacuum or accumulate on the alloy surface, such as zinc, are also applicable. In other words, the present disclosure can not only strengthen the brazeability of aluminum alloys, but can also be applied to other alloys that need to reduce easily oxidized solid solution elements on the surface, such as magnesium and zinc.

One of the advantages of the present disclosure is that the method of the present disclosure can strengthen the brazeability of the surface of the alloy structure by including steps of: heat treating a magnesium-containing alloy in a vacuum furnace, obtaining a vacuum heat-treated alloy structure including a magnesium-rich layer, a magnesium-deficient layer and an original magnesium-content layer, and performing a surface reduction treatment on the vacuum heat-treated alloy structure to reduce the magnesium-rich layer to expose the brazing surface of the magnesium-deficient layer underneath the magnesium-rich layer.

Furthermore, the magnesium-deficient layer manufactured by the method of the present disclosure can have a thickness of greater than 10 μm to be suitable for brazing.

The foregoing description of the exemplary embodiments of the disclosure has been presented only for the purposes of illustration and description and is not intended to be exhaustive or to limit the disclosure to the precise forms disclosed. Many modifications and variations are possible in light of the above teaching.

The embodiments were chosen and described in order to explain the principles of the disclosure and their practical application so as to enable others skilled in the art to utilize the disclosure and various embodiments and with various modifications as are suited to the particular use contemplated. Alternative embodiments will become apparent to those skilled in the art to which the present disclosure pertains without departing from its spirit and scope.

Claims

1. A method for manufacturing an integrally-formed alloy structure having a brazing surface, comprising:

providing a magnesium-containing alloy;

heat treating the magnesium-containing alloy in a vacuum furnace;

obtaining a vacuum heat-treated alloy structure, wherein the vacuum heat-treated alloy structure includes a magnesium-rich layer, a magnesium-deficient layer and an original magnesium-content layer, the magnesium-rich layer is integrally formed on the magnesium-deficient layer, the magnesium-deficient layer is integrally formed on the original magnesium-content layer, the magnesium-rich layer has a higher magnesium content than the original magnesium-content layer, and the magnesium-deficient layer has a lower magnesium content than the original magnesium-content layer; and

performing a surface reduction treatment on the vacuum heat-treated alloy structure to reduce the magnesium-rich layer to expose the brazing surface of the magnesium-deficient layer underneath the magnesium-rich layer, so as to form the integrally-formed alloy structure having the brazing surface.

2. The method according to claim 1, wherein the vacuum heat-treated alloy structure is formed at a temperature of between 500° C. and 600° C.

3. The method according to claim 2, wherein the vacuum heat-treated alloy structure is formed by maintaining the temperature for a period of time longer than 30 minutes.

4. The method according to claim 3, wherein the vacuum heat-treated alloy structure is formed at a vacuum degree of lower than 10−4 torr.

5. The method according to claim 1, wherein a thickness of the magnesium-deficient layer is formed more than 10 μm.

6. The method according to claim 1, wherein the magnesium-containing alloy is a 6000-series aluminum alloy containing magnesium.