Method for integrally molding metal and resin and metal-resin composite structure obtainable by the same

Abstract

A method for integrally molding a metal and a resin and a metal-resin composite structure obtainable by the same are provided. The method comprises forming a nanopore in a surface of a metal sheet; melting a thermoplastic resin on the surface of the metal sheet formed with the nanopore; and injection molding the thermoplastic resin onto the surface of the metal sheet. The thermoplastic resin includes a mixture of a main resin and a polyolefin resin, the main resin is a polycarbonate, and the polyolefin resin has a melting point of about 65 C. to about 105 C.

Claims

1. A method for integrally molding a metal and a resin, comprising: forming nanopores on a surface of a metal sheet; forming corrosion pores on the surface of the metal sheet, thereby to form a double-layer pore structure including the corrosion pores and the nanopores, the corrosion pores being in communication with the nanopores and the corrosion pores having a larger diameter than the nanopores; melting a thermoplastic resin; and injection molding the melted thermoplastic resin onto the surface of the metal sheet through the nanopores and the corrosion pores, wherein the melted thermoplastic resin composition is fixedly attached to the metal sheet, wherein the thermoplastic resin includes a mixture of a main resin and a polyolefin resin, the main resin is a polycarbonate, and the polyolefin resin has a melting point of about 65 C. to about 105 C.

2. The method according to claim 1, wherein forming the nanopores on the surface of the metal sheet comprises: anodizing the surface of the metal sheet to form an oxide layer on the surface of the metal sheet, where the oxide layer includes the nanopores.

3. The method according to claim 2, wherein the oxide layer has a thickness of about 1 m to about 10 m, and the nanopores have an average diameter of about 10 nm to about 100 nm and an average depth of about 0.5 m to about 9.5 m.

4. The method according to claim 2, wherein anodizing the surface of the metal sheet comprises: placing a pretreated metal sheet as an anode in a H.sub.2SO.sub.4 solution with a concentration of about 10 wt % to about 30 wt %; and electrolyzing the metal sheet at a temperature of about 10 C. to about 30 C. at a voltage of about 10V to about 100V for about 1 minute to about 40 minutes to form the oxide layer with a thickness of about 1 m to about 10 m on the surface of the metal sheet.

5. The method according to claim 2, wherein forming the corrosion pores on the surface of the metal sheet comprises: immersing the metal sheet including the oxide layer on the surface thereof in an etching solution to form the corrosion pores on an outer surface of the oxide layer.

6. The method according to claim 5, wherein the corrosion pores have an average diameter of about 200 nm to about 2000 nm and an average depth of about 0.5 m to about 9.5 m.

7. The method according to claim 5, wherein the etching solution corrodes the oxide layer.

8. The method according to claim 1, wherein based on 100 weight parts of the thermoplastic resin, the amount of the main resin is about 95 weight parts to about 99 weight parts, and the amount of the polyolefin resin is about 1 weight part to about 5 weight parts.

9. The method according to claim 8, wherein based on 100 weight parts of the thermoplastic resin, the thermoplastic resin further contains about 1 weight part to about 5 weight parts of a flow improver, and the flow improver is a cyclic polyester.

10. The method according to claim 1, wherein the polyolefin resin is a grafted polyethylene.

11. The method according to claim 1, wherein the metal is at least one selected from the group consisting of aluminum, stainless steel and magnesium.

12. A method for integrally molding a metal and a resin, comprising: A) forming nanopores on a surface of a metal sheet by anodizing the surface of the metal sheet to form an oxide layer on the surface of the metal sheet, wherein the oxide layer includes the nanopores; B) immersing the metal sheet including the oxide layer on the surface thereof in an etching solution to form corrosion pores on an outer surface of the oxide layer, wherein the corrosion pores and the nanopores form a double-layer pore structure and the corrosion pores are in communication with the nanopores; C) melting a thermoplastic resin; and D) injection molding the melted thermoplastic resin onto the surface of the metal sheet formed with the nanopores and corrosion pores wherein the melted thermoplastic resin composition is fixedly attached to the metal sheet, wherein the thermoplastic resin includes a mixture of a main resin and a polyolefin resin, the main resin is a polycarbonate, and the polyolefin resin has a melting point of about 65 C. to about 105 C., and wherein the nanopores have an average diameter of about 10 nm to about 100 nm and the corrosion pores have an average diameter of about 200 nm to about 2000 nm.

Description

DETAILED DESCRIPTION

(1) Reference will be made in detail to embodiments of the present disclosure. The embodiments described herein are explanatory, illustrative, and used to generally understand the present disclosure. The embodiments shall not be construed to limit the present disclosure.

(2) According to a first aspect of the present disclosure, a method for integrally molding a metal and a resin is provided. The method comprises steps of: A) forming a nanopore in a surface of a metal sheet; and B) melting a thermoplastic resin on the surface of the metal sheet formed with the nanopore, and then injection molding the thermoplastic resin onto the surface of the metal sheet, in which the thermoplastic resin is a mixture of a main resin and a polyolefin resin, the main resin is a polycarbonate, and the polyolefin resin has a melting point of about 65 C. to about 105 C.

(3) Because the resins used in the prior art are all highly crystalline resins, the surface of the prior art plastic layer may be difficult to treat. In the present disclosure, a non-crystalline polycarbonate, which has a surface gloss and a toughness both superior to those of the highly crystalline resins in the prior art, is used as an injection molding material, and a polyolefin resin with a melting point of about 65 C. to about 105 C. is also used. Therefore, injection molding at a specific mould temperature may not be required during the molding. Subsequent annealing treatment may also not be required. The molding process may be simplified. And it may be ensured that the obtained metal-resin composite structure has high mechanical strength and good surface treatment characteristics, thus solving the problem of the conventional techniques and enhancing the light transmittance of plastic articles.

(4) In the present disclosure, the mechanism of the metal-resin integrally molding is as follows: a nanoscale micropore is formed on the surface of the metal sheet; a resin composition is melted on the surface of the metal sheet, where a part of the melted resin composition permeates into the nanoscale micropore; and then the metal and the resin composition are integrally injection molded.

(5) Particularly, in step A), forming a nanopore on a surface of a metal sheet comprises: anodizing the surface of the metal sheet to form an oxide layer on the surface of the metal sheet, in which the oxide layer is formed with the nanopore. The anodizing technique is well known to those skilled in the art. In some embodiments, anodizing the surface of the metal sheet may comprise: placing a pretreated metal sheet as an anode in a H.sub.2SO.sub.4 solution with a concentration of about 10 wt % to about 30 wt %; and electrolyzing the metal at a temperature of about 10 C. to about 30 C. at a voltage of about 10V to about 100V for about 1 min to about 40 min to form the oxide layer with a thickness of about 1 m to about 10 m on the surface of the metal sheet. An anodizing apparatus may be those known in the art, such as, an anodizing bath.

(6) By anodizing, the oxide layer formed with the nanopore is formed on the surface of the metal sheet. Preferably, the oxide layer has a thickness of about 1 m to about 10 m, more preferably about 1 m to about 5 m.

(7) According to an embodiment, the nanopore has a diameter of about 10 nm to about 100 nm. According to a further embodiment, the nanopore has a diameter of about 20 nm to about 80 nm. According to a still further embodiment, the nanopore has a diameter of about 20 nm to about 60 nm. According to an embodiment, the nanopore has a depth of about 0.5 m to about 9.5 m. According to a further embodiment, the nanopore has a depth of about 0.5 m to about 5 m. The structure of the nanopore enhances the filling of the melted resin composition in the nanopore. The nanopore with such depth may be filled with the melted resin in a conventional injection molding process, which, while retaining the bonded area between the resin and the oxide layer, may further improve the bonding force between the resin and the metal because there are no voids or gaps in the nanopore.

(8) In one preferred embodiment, in step A), forming a nanopore in a surface of a metal sheet may further comprise a step of: immersing the metal sheet formed with the oxide layer on the surface thereof in an etching solution to form a corrosion pore in an outer surface of the oxide layer. The corrosion pore is communicated with the nanopore. The corrosion pore and the nanopore form a double-layer three-dimensional pore structure, thereby enhancing the permeability of the resin composition, improving the bonding force between the resin composition and the metal, and thus further facilitating the molding.

(9) According to an embodiment, the corrosion pore has a diameter of about 200 nm to about 2000 nm. According to a further embodiment, the corrosion pore has a diameter of about 200 nm to about 1000 nm. According to a still further embodiment, the corrosion pore has a diameter of about 400 nm to about 1000 nm. According to an embodiment, the corrosion pore has a depth of about 0.5 m to about 9.5 m. According to a further embodiment, the corrosion pore has a depth of about 0.5 m to about 5 m. The structure of the corrosion pore facilitates direct injection of the resin composition and the bonding between the resin composition and the alloy during the injection molding.

(10) The etching solution may be a solution that corrodes the oxide layer. Generally, the etching solution may be a solution that dissolves the oxide layer. The concentration of the etching solution may be adjusted as desired. The etching solution may be an acid/base etching solution. Preferably, the etching solution may be a single basic solution with a pH of about 10 to about 13 or a complex buffer solution. The single basic solution with a pH of about 10 to about 13 may be at least one selected from the group consisting of a Na.sub.2CO.sub.3 aqueous solution, a NaHCO.sub.3 aqueous solution, and a NaOH aqueous solution, preferably a Na.sub.2CO.sub.3 aqueous solution and/or a NaHCO.sub.3 aqueous solution, thus allowing the corrosion pores to be uniformly distributed in the surface of the oxide layer and to have uniform diameter, and achieving better bonding performance between the resin layer and an aluminum alloy substrate as well as higher tensile strength and better integral bonding of an aluminum alloy composite structure. The Na.sub.2CO.sub.3 aqueous solution and/or the NaHCO.sub.3 aqueous solution may have a solid content of about 0.1 wt % to about 15 wt %. The complex buffer solution may be a mixed solution of a soluble hydrophosphate and a soluble base, for example, an aqueous solution of sodium dihydrogen phosphate and sodium hydroxide. The aqueous solution of sodium dihydrogen phosphate and sodium hydroxide may have a solid content of about 0.1 wt % to about 15 wt %.

(11) Immersing the metal sheet formed with the oxide layer on the surface thereof in an etching solution may comprise repeatedly immersing the metal sheet in the etching solution 2 to 10 times with each immersing time of about 1 minute to 60 minutes, and cleaning the metal sheet with deionized water after each immersing. Cleaning the metal sheet may comprise placing the metal sheet in a washing bath to wash the metal sheet for about 1 minute to about 5 minutes, or placing the metal sheet in a washing bath to place the metal sheet for about 1 min to about 5 minutes.

(12) It has been found by the inventors through many experiments that in the present disclosure, by using a polyolefin resin with a melting point of about 65 C. to about 105 C. in the non-crystalline main resin, the flowing capability of the resin in the nano on the surface of the metal sheet may be enhanced, thus ensuring strong adhesive force between the metal and the plastic as well as high mechanical strength of the metal-resin composite structure. Preferably, based on 100 weight parts of the thermoplastic resin, the amount of the main resin is about 95 weight parts to about 99 weight parts, and the amount of the polyolefin resin is about 1 weight part to about 5 weight parts.

(13) It has also been found by the inventors that by using a flow improver in the thermoplastic resin, the flowing capability of the resin may be enhanced, thus further enhancing the adhesive force between the metal and the plastic as well as the injection molding performance of the resin. Preferably, based on 100 weight parts of the thermoplastic resin, the thermoplastic resin further contains about 1 weight part to about 5 weight parts of a flow improver. Preferably, the flow improver is a methyl methacrylate composition.

(14) In the present disclosure, the main resin is a polycarbonate (PC), which may be selected from any straight chain polycarbonate and/or any branched chain polycarbonate commonly used in the prior art. For example, the polycarbonate may be PC IR2500 or IR2200 available from Idemitsu Kosan Co., Ltd., without special limits.

(15) In the present disclosure, the polyolefin resin has a melting point of about 65 C. to about 105 C. Preferably, the polyolefin resin may be a grafted polyethylene. More preferably, the polyolefin resin may be a grafted polyethylene with melting point of about 100 C. or about 105 C.

(16) In the present disclosure, the metal may be any metal known, and may be selected according to the specific application. For example, the metal may be at least one selected from the group consisting of aluminum, stainless steel and magnesium.

(17) According to a second aspect of the present disclosure, a metal-resin composite structure is also provided, which is obtained by the method according to the first aspect of the present disclosure.

(18) In the metal-resin composite structure according to an embodiment of the present disclosure, the metal sheet and the plastic layer are integrally formed, providing strong adhesive force and high mechanical strength. As shown in Table 1, each metal-resin composite structure has a fracture strength of about 15 MPa to about 20 MPa, an impact strength of about 350 J/m to about 400 J/m and a light transmittance of about 50% to about 52%.

(19) The present disclosure provides further details of the embodiments with reference to examples thereof. It would be appreciated that particular examples described herein are merely used to understand the present disclosure. The examples shall not be construed to limit the present disclosure. The raw materials used in the examples and the comparative examples are all commercially available, without special limits.

Example 1

Pretreatment

(20) A commercially available A5052 aluminum alloy plate with a thickness of 1 mm was cut into 18 mm45 mm rectangular sheets, which were then immersed in a 40 g/L NaOH aqueous solution. The temperature of the NaOH aqueous solution was 40 C. After 1 minute, the rectangular sheets were washed with water and dried to obtain pretreated aluminum alloy sheets.

(21) (2) Surface Treatment 1:

(22) Each aluminum alloy sheet as an anode was placed in an anodizing bath containing a 20 wt % H.sub.2SO.sub.4 solution, the aluminum alloy was electrolyzed at a voltage of 20V at 18 C. for 10 min, and then the aluminum alloy sheet was blow-dried.

(23) The cross section of the aluminum alloy sheet after the surface treatment 1 was observed by a metalloscope, to find out that an aluminum oxide layer with a thickness of 5 m was formed on the surface of the electrolyzed aluminum alloy sheet. The surface of the aluminum alloy sheet after the surface treatment 1 was observed by an electron microscope, to find out that a nanopore with a diameter of about 40 nm to about 60 nm and a depth of 1 m was formed in the aluminum oxide layer.

(24) (3) Surface Treatment 2:

(25) 500 ml of 10 wt % sodium carbonate solution (pH=12) with a temperature of 20 C. was prepared in a beaker. The aluminum alloy sheet after step (2) was immersed in the sodium carbonate solution, taken out after 5 minutes, and placed in a beaker containing water to be immersed for 1 minute. The process was repeated for 5 times. After water immersing for the last time, the aluminum alloy sheet was blow-dried.

(26) The surface of the aluminum alloy sheet after the surface treatment 2 was observed by an electron microscope, to find out that a corrosion pore with a diameter of 300 nm to 1000 nm and a depth of 4 m was formed in the surface of the immersed aluminum alloy sheet. It may also be observed that there was a double-layer three-dimensional pore structure in the aluminum oxide layer, and the corrosion pore was communicated with the nanopore.

(27) (4) Molding:

(28) 95 weight parts of a straight chain polycarbonate PC (IR2200 available from Idemitsu Kosan Co., Ltd.), 3 weight parts of a flow improver (TP003 available from Mitsubishi Rayon Co., Ltd.) and 2 weight parts of a grafted polyethylene with a melting point of 65 C. (Lotader AX8900 available from Arkema Group) were weighed, and mixed uniformly to obtain a resin mixture. Then, using an injection molding machine, the melted resin mixture was injection molded on the surface of the aluminum alloy sheet after step (3), to obtain a metal-resin composite structure S1 in this example.

Example 2

(29) A metal-resin composite structure S2 in this example was prepared by a method which is substantially the same as the method in Example 1, with the following exceptions.

(30) In step (1), instead of the aluminum alloy plate in Example 1, a commercially available magnesium alloy plate with a thickness of 3 mm was cut into 18 mm45 mm rectangular sheets.

(31) In step (2), each magnesium alloy sheet as an anode was placed in an anodizing bath containing a 20 wt % H.sub.2SO.sub.4 solution. The magnesium alloy was electrolyzed at a voltage of 15V at 18 C. for 10 min. And then the magnesium alloy sheet was blow-dried.

(32) The cross section of the magnesium alloy sheet after the surface treatment 1 was observed by a metalloscope, to find out that a magnesium oxide layer with a thickness of 5 m was formed on the surface of the electrolyzed magnesium alloy sheet. The surface of the magnesium alloy sheet after the surface treatment 1 was observed by an electron microscope, to find out that a nano micropore with a diameter of 20 nm to 40 nm and a depth of 1 m was formed in the magnesium oxide layer.

(33) The surface of the magnesium alloy sheet after the surface treatment 2 was observed by an electron microscope, to find out that a corrosion pore with a diameter of 300 nm to 1000 nm and a depth of 4 m was formed in the surface of the immersed magnesium alloy sheet. It may also be observed that there was a double-layer three-dimensional pore structure in the magnesium oxide layer, and the corrosion pore was communicated with the nanopore.

(34) After the above steps, the metal-resin composite structure S2 in this example was obtained.

Example 3

(35) A metal-resin composite structure S3 in this example was prepared by a method which is substantially the same as the method in Example 1, with the following exceptions.

(36) In step (2), each aluminum alloy sheet as an anode was placed in an anodizing bath containing a 20 wt % H.sub.2SO.sub.4 solution, the aluminum alloy was electrolyzed at a voltage of 40V at 18 C. for 10 min, and then the aluminum alloy sheet was blow-dried.

(37) The cross section of the aluminum alloy sheet after the surface treatment 1 was observed by a metalloscope, to find out that an aluminum oxide layer with a thickness of 5 m was formed on the surface of the electrolyzed aluminum alloy sheet. The surface of the aluminum alloy sheet after the surface treatment 1 was observed by an electron microscope, to find out that a nanopore with a diameter of 60 nm to 80 nm and a depth of 1 m was formed in the aluminum oxide layer.

(38) The surface of the aluminum alloy sheet after the surface treatment 2 was observed by an electron microscope, to find out that a corrosion pore with a diameter of 300 nm to 1000 nm and a depth of 4 m was formed in the surface of the immersed aluminum alloy sheet. It may also be observed that there was a double-layer three-dimensional pore structure in the aluminum oxide layer, and the corrosion pore was communicated with the nanopore.

(39) After the above steps, the metal-resin composite structure S3 in this example was obtained.

Example 4

(40) A metal-resin composite structure S4 in this example was prepared by a method which is substantially the same as the method in Example 2, with the following exceptions.

(41) In step (4), 98 weight parts of a straight chain polycarbonate PC (IR2200 available from Idemitsu Kosan Co., Ltd.) and 2 weight parts of a grafted polyethylene with a melting point of 105 C. (Lotader 4210 available from Arkema Group) were weighed, and mixed uniformly to obtain a resin mixture. Then, using an injection molding machine, the melted resin mixture was injection molded on the surface of the aluminum alloy sheet after step (3), to obtain a metal-resin composite structure S4 in this example.

Comparative Example 1

(42) A metal-resin composite structure DS1 in this example was prepared by a method which is substantially the same as the method in Example 1, with the following exceptions.

(43) In step (4), 97 weight parts of a straight chain polycarbonate PC (IR2200 available from Idemitsu Kosan Co., Ltd.) and 3 weight parts of a flow improver (TP003 available from Mitsubishi Rayon Co., Ltd.) were weighed, and mixed uniformly to obtain a resin mixture. Then, using an injection molding machine, the melted resin mixture was injection molded on the surface of the aluminum alloy sheet after step (3), to obtain a metal-resin composite structure DS1 in this example.

Comparative Example 2

(44) A metal-resin composite structure DS2 in this example was prepared by a method which is substantially the same as the method in Example 1, with the following exceptions.

(45) In step (4), 84 weight parts of polyphenylene sulfide PPS (PPS-HCl available from Sichuan Deyang Chemical Co., Ltd., China), 3 weight parts of a flow improver, i.e., a cyclic polyester (CBT100), 8 weight parts of a grafted polyethylene with a melting point of 105 C. (Lotader AX8900 available from Arkema Group) and 5 weight parts of a toughener (Lotader AX8840 available from Arkema Group) were weighed, and mixed uniformly to obtain a resin mixture. Then, using an injection molding machine, the melted resin mixture was injection molded on the surface of the aluminum alloy sheet after step (3) to obtain an injection molded metal-resin composite structure, which was annealed at 180 C. for 1 hour to obtain a metal-resin composite structure DS2 in this example.

(46) Performance Test

(47) 1) The metal-resin composite structures S1-S4 and DS1-DS4 were fixed on a universal testing machine for tensile test to obtain maximum loads thereof respectively. The test results were shown in Table 1.

(48) 2) The impact strength of standard samples of the metal-resin composite structures S1-S4 and DS1-DS4 was tested using a cantilever beam impact tester according to the method disclosed in ASTM D256.

(49) 3) 40.0 mm40.0 mm2.0 mm square samples were made of the resin mixtures in Examples 1-4 and Comparative Examples 1-2 respectively, and the light transmittance of the square samples were tested using a spectrophotometer respectively.

(50) The test results were shown in Table 1.

(51) TABLE-US-00001 TABLE 1 Fracture Impact Light Fracture Impact Light Strength Strength Transmittance Strength Strength Transmittance Sample (MPa) (J/m) (%) Sample (MPa) (J/m) (%) S1 22 350 50 S2 20 350 50 S3 19 350 50 S4 19 400 52 DS1 10 500 55 DS2 20 130

(52) It may be seen from the test results in Table 1 that the metal-resin composite structures S1-S4 have a fracture strength of about 19 MPa to about 22 MPa, which indicates that the bonding force between the metal sheet and the plastic layer in the metal-resin composite structures S1-S4 is very strong; the metal-resin composite structures S1-S4 have an impact strength of about 350 J/m to about 400 J/m, which indicates that the metal-resin composite structures S1-S4 have high mechanical strength; and the metal-resin composite structures S1-S4 have a light transmittance of about 50% to about 52%, which may meet the requirement of light transmission applications.

(53) By comparing the test results of the metal-resin composite structure S1 with the test results of the metal-resin composite structure DS2, it may be seen that the toughness of the polyphenylene oxide resin used in the prior art is very poor, the toughness of the polyphenylene oxide resin after modified with a toughener is still poor, and the metal-resin composite structure DS2 is unable to meet the requirement of the light transmission applications.

(54) Although explanatory embodiments have been shown and described, it would be appreciated by those skilled in the art that the above embodiments can not be construed to limit the present disclosure, and changes, alternatives, and modifications can be made in the embodiments without departing from spirit, principles and scope of the present disclosure.