CN111169113A - Metal composite board - Google Patents
Metal composite board Download PDFInfo
- Publication number
- CN111169113A CN111169113A CN201811330644.1A CN201811330644A CN111169113A CN 111169113 A CN111169113 A CN 111169113A CN 201811330644 A CN201811330644 A CN 201811330644A CN 111169113 A CN111169113 A CN 111169113A
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- China
- Prior art keywords
- metal
- plate
- metal plate
- aluminum alloy
- series
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/20—Layered products comprising a layer of metal comprising aluminium or copper
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B33/00—Layered products characterised by particular properties or particular surface features, e.g. particular surface coatings; Layered products designed for particular purposes not covered by another single class
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
- B32B9/04—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B9/041—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material of metal
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/54—Yield strength; Tensile strength
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/558—Impact strength, toughness
Abstract
The invention discloses a metal composite plate, which consists of three layers of metal plates combined with each other, wherein the three layers of metal plates comprise: the first metal plate in the middle layer, and the second metal plate and the third metal plate which are respectively combined on two opposite surfaces of the first metal plate, wherein the first metal plate is an aluminum alloy plate or a magnesium alloy plate which is processed by 6-8 series high temperature T4, the second metal plate and the third metal plate are aluminum alloy plates which are processed by 1-5 series high temperature T4, and the outer side surfaces of the second metal plate and the third metal plate are provided with a metal oxide layer. The metal composite plate is easy to machine and form and supports coloring treatment, and is suitable for manufacturing shells of electronic products and products manufactured by adopting a stamping process.
Description
Technical Field
The invention relates to a composite metal plate in the field of metal materials, in particular to a metal composite plate with a three-layer structure.
Background
Light weight, thinness, shortness, and smallness are design goals of current electronic products, and sufficient mechanical strength needs to be maintained in addition to the goals, so that the use of metal materials for manufacturing housings of electronic products has become mainstream. At present, the metal materials for manufacturing the electronic product shell are mainly aluminum alloys, and magnesium aluminum alloys and titanium alloys are also common metal materials for manufacturing the electronic product shell.
The conventional technology generally extrudes aluminum alloy to a base material or performs die-casting molding, then the aluminum alloy is manufactured into a shell of an electronic product through a mechanical cutting process, and then the shell is subjected to anodic oxidation treatment to obtain the final required shell. Thin metal plate or strip products cannot be produced by extrusion, the extruded products can only meet the requirement of thinning and shelling through a large amount of machining, and the production process is complex. The die-casting product has large machining amount, die-casting waste is easy to oxidize and has high impurity content, and a plurality of defects are easy to generate in the forming process, so that the production cost of the product is increased.
In order to solve the problem of manufacturing the shell by adopting an extrusion or die-casting process, the shell of the electronic product can be quickly formed by adopting a thin metal plate or metal strip through a stamping process, and the shell of the electronic product can be light and thin through simple machining, grinding, sand blasting and polishing treatment. At present, a commonly used 6-8 series aluminum alloy sheet or strip can be changed into a hard roll/plate material after being treated by high-temperature T4, and is not easy to be formed by a stamping process.
Disclosure of Invention
The invention aims to solve the technical problem of providing a metal composite plate which is easy to machine and form and has enough mechanical strength.
The invention provides an embodiment structure of a metal composite plate, which consists of three layers of metal plates combined with each other, wherein the three layers of metal plates comprise: the first metal plate in the middle layer, and the second metal plate and the third metal plate which are respectively combined on the opposite first surface and the opposite second surface of the first metal plate, wherein the first metal plate is 6-8 series aluminum alloy plates or magnesium alloy plates which pass through a high-temperature T4 processing procedure, the second metal plate and the third metal plate are 1-5 series aluminum alloy plates which pass through a high-temperature T4 processing procedure, the outer side surfaces of the second metal plate and the third metal plate are provided with a metal oxide layer as the outer side surface of the metal composite plate, the total thickness of the second metal plate and the third metal plate accounts for 10% -90% of the total thickness of the metal, and the thickness of the first metal plate accounts for 90% -10% of the total thickness of the metal composite plate.
As the preferable structure of the metal composite plate of the invention, the treatment temperature of the aluminum alloy plate of 6-8 series passing through the high temperature T4 treatment process is 440-660 ℃, and the treatment temperature of the aluminum alloy plate of 1-5 series passing through the high temperature T4 treatment process is 450-650 ℃.
The metal composite plate has the beneficial effects that the first metal plate is formed by adopting 6-8 series aluminum alloy plate soft materials and then is treated by high-temperature T4, so that the metal composite plate is easy to process and deform and has enough mechanical strength; the second metal plate and the third metal plate are made of 1-5 series aluminum alloy and are subjected to T4 treatment simultaneously to form soft materials which are easy to punch and form or bend. On the other hand, 1-5 series aluminum alloy is adopted as the outer layer structure of the metal composite plate, so that the anode treatment and the subsequent coloring treatment can be carried out, and the problem of attractiveness can be solved. 6-8 series aluminum alloy plates or magnesium alloy plates are used as the middle layer of the metal composite plate, so that the problem that the anode aluminum plate is insufficient in compression resistance, tensile strength and yield strength can be solved.
Drawings
The drawings described herein are for illustration purposes only and are not intended to limit the scope of the present disclosure in any way. In addition, the shapes, the proportional sizes, and the like of the respective members in the drawings are merely schematic for facilitating the understanding of the present invention, and do not specifically limit the shapes, the proportional sizes, and the like of the respective members of the present invention. Those skilled in the art, having the benefit of the teachings of this invention, may choose from the various possible shapes and proportional sizes to implement the invention as a matter of case.
Fig. 1 is an exploded view of one embodiment of the metal composite panel of the present invention.
Fig. 2 is a cross-sectional view of the construction of one embodiment of the metal composite plate of the present invention.
Description of reference numerals:
10. a first metal plate
11. First surface
12. Second surface
20. Second metal plate
21. Metal oxide layer
30. Third metal plate
31. Metal oxide layer
Detailed Description
The details of the present invention can be more clearly understood in conjunction with the accompanying drawings and the description of the embodiments of the present invention. However, the specific embodiments of the present invention described herein are for the purpose of illustration only and are not to be construed as limiting the invention in any way. Any possible variations based on the present invention may be conceived by the skilled person in the light of the teachings of the present invention, and these should be considered to fall within the scope of the present invention.
Referring to fig. 1 and 2, an exploded view and a sectional view of an embodiment of the metal composite plate according to the present invention are shown.
An embodiment construction of the metal composite panel of the present invention is composed of three metal plates bonded to each other, the three metal plates including: the first metal plate 10 in the middle layer, and the second metal plate 20 and the third metal plate 30 respectively combined on the opposite first surface 11 and second surface 12 of the first metal plate 10, wherein the first metal plate 10 is a 6-8 series aluminum alloy plate or magnesium alloy plate processed by a high temperature T4 process, the second metal plate 20 and the third metal plate 30 are a 1-5 series aluminum alloy plate processed by a high temperature T4 process, wherein the outer side surfaces of the second metal plate 20 and the third metal plate 30 respectively have a metal oxide layer 21 and a metal oxide layer 31 as the outer side surface of the metal composite plate, the total thickness of the second metal plate 20 and the third metal plate 30 accounts for 10% -90% of the total thickness of the metal composite plate, and the thickness of the first metal plate 10 accounts for 90% -10% of the total thickness of the metal composite plate.
As the preferable structure of the metal composite plate of the invention, the treatment temperature of the aluminum alloy plate of 6-8 series passing through the high temperature T4 treatment process is 440-660 ℃, and the treatment temperature of the aluminum alloy plate of 1-5 series passing through the high temperature T4 treatment process is 450-650 ℃. Wherein the first metal plate 10, the second metal plate 20 and the third metal plate 30 are heated and rolled (without interface additives) to form the metal composite plate of the present invention.
The aluminum alloy plates of the 1-5 series through the high-temperature T4 processing procedure and the 6-8 series through the high-temperature T4 processing procedure are aluminum alloy plates manufactured by processing the 1 XXXXXX-8 XXXX series aluminum alloy marked according to the international brand naming principle through the existing aluminum alloy material tempering procedure code T4.
The aluminum alloy material tempering procedure T4 treatment is not unknown to professionals in the technical field of aluminum alloy materials, and the T4 treatment sequence is solutionizing heat treatment natural aging, namely the aluminum alloy is naturally aged and hardened to a stable state without cold working after the solutionizing heat treatment.
For example, the aluminum alloy sheet of 1XXX series is determined to have the lowest aluminum content according to the last two digits of the series, for example, the last two digits of 1050 series are 50, and the aluminum content must reach more than 99.5% according to the international designation principle, so that the aluminum is qualified. The series 1 to 5 and the series 6 to 8 of the present invention are the aluminum alloy materials expressed by the first digit of the international designation principle, and therefore, it should be understood by those skilled in the art of aluminum alloy materials. Generally speaking, the first digit represents the alloy elements mainly added in the aluminum alloy material, wherein the 1 series is pure aluminum according with the international designation principle; 2, the series of main added alloy elements are copper; the 3 series of main added alloy elements are manganese or manganese and magnesium; the 4 series of main added alloy elements are silicon; the 5 series of main added alloy elements are magnesium; the 6 series of main added alloy elements are silicon and magnesium; the 7 series of main added alloy elements are zinc and magnesium; the 8 series is a new alloy not belonging to the above alloy series.
Although the present invention has been described with reference to the above embodiments, it should be understood that various changes and modifications can be made therein by those skilled in the art without departing from the spirit and scope of the invention.
Claims (2)
1. A metal composite plate, characterized in that said metal composite plate is composed of three metal plates bonded to each other, the three metal plates comprising: the first metal plate in the middle layer, and the second metal plate and the third metal plate which are respectively combined on the opposite first surface and second surface of the first metal plate, wherein the first metal plate is 6-8 series aluminum alloy plates or magnesium alloy plates which pass through a high temperature T4 processing procedure, the second metal plate and the third metal plate are 1-5 series aluminum alloy plates which pass through a high temperature T4 processing procedure, the second metal plate and the third metal plate are used as the outer side surface of the metal composite plate and are provided with a metal oxide layer, the total thickness of the second metal plate and the third metal plate accounts for 10-90% of the total thickness of the metal composite plate, and the thickness of the first metal plate accounts for 90-10% of the total thickness of the metal composite plate.
2. The metal composite plate according to claim 1, wherein the treatment temperature of the aluminum alloy plate of 6 to 8 series through the high temperature T4 treatment process is 440 to 660 ℃, and the treatment temperature of the aluminum alloy plate of 1 to 5 series through the high temperature T4 treatment process is 450 to 650 ℃.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201811330644.1A CN111169113A (en) | 2018-11-09 | 2018-11-09 | Metal composite board |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201811330644.1A CN111169113A (en) | 2018-11-09 | 2018-11-09 | Metal composite board |
Publications (1)
Publication Number | Publication Date |
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CN111169113A true CN111169113A (en) | 2020-05-19 |
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Family Applications (1)
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CN201811330644.1A Pending CN111169113A (en) | 2018-11-09 | 2018-11-09 | Metal composite board |
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Citations (9)
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---|---|---|---|---|
CN1832825A (en) * | 2003-08-29 | 2006-09-13 | 克里斯铝轧制品有限公司 | High strength aluminium alloy brazing sheet, brazed assembly and method for producing the same |
US20090202860A1 (en) * | 2006-05-02 | 2009-08-13 | Aleris Aluminum Duffel Bvba | Clad sheet product |
CN101530860A (en) * | 2009-04-13 | 2009-09-16 | 西安建筑科技大学 | Method for preparing aluminum-magnesium ultrafine crystal composite plate with multilayer structure |
CN101885251A (en) * | 2009-04-30 | 2010-11-17 | 美铝公司 | The multi-alloy composite sheet that is used for automotive panels |
US20140193666A1 (en) * | 2011-09-15 | 2014-07-10 | Hydro Aluminium Rolled Products Gmbh | Aluminium Composite Material with AlMgSi Core Layer |
CN104870113A (en) * | 2012-10-30 | 2015-08-26 | 海德鲁铝业钢材有限公司 | Aluminum composite material and forming method |
CN105563933A (en) * | 2015-12-16 | 2016-05-11 | 银邦金属复合材料股份有限公司 | Three-layer aluminum alloy composite board |
CN106335247A (en) * | 2016-08-24 | 2017-01-18 | 银邦金属复合材料股份有限公司 | Aluminum honeycomb structure plate for carrier gas soldering, and production method thereof |
CN106735660A (en) * | 2016-12-14 | 2017-05-31 | 无锡银邦防务科技有限公司 | A kind of soldering cellular board panel high strength alumin ium alloy composite plate, core, clad and skin material |
-
2018
- 2018-11-09 CN CN201811330644.1A patent/CN111169113A/en active Pending
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1832825A (en) * | 2003-08-29 | 2006-09-13 | 克里斯铝轧制品有限公司 | High strength aluminium alloy brazing sheet, brazed assembly and method for producing the same |
US20090202860A1 (en) * | 2006-05-02 | 2009-08-13 | Aleris Aluminum Duffel Bvba | Clad sheet product |
CN101530860A (en) * | 2009-04-13 | 2009-09-16 | 西安建筑科技大学 | Method for preparing aluminum-magnesium ultrafine crystal composite plate with multilayer structure |
CN101885251A (en) * | 2009-04-30 | 2010-11-17 | 美铝公司 | The multi-alloy composite sheet that is used for automotive panels |
US20140193666A1 (en) * | 2011-09-15 | 2014-07-10 | Hydro Aluminium Rolled Products Gmbh | Aluminium Composite Material with AlMgSi Core Layer |
CN104870113A (en) * | 2012-10-30 | 2015-08-26 | 海德鲁铝业钢材有限公司 | Aluminum composite material and forming method |
CN105563933A (en) * | 2015-12-16 | 2016-05-11 | 银邦金属复合材料股份有限公司 | Three-layer aluminum alloy composite board |
CN106335247A (en) * | 2016-08-24 | 2017-01-18 | 银邦金属复合材料股份有限公司 | Aluminum honeycomb structure plate for carrier gas soldering, and production method thereof |
CN106735660A (en) * | 2016-12-14 | 2017-05-31 | 无锡银邦防务科技有限公司 | A kind of soldering cellular board panel high strength alumin ium alloy composite plate, core, clad and skin material |
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Application publication date: 20200519 |
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