WO2014170946A1 - PRODUCTION METHOD FOR Al-Mg-Si-BASED ALUMINIUM ALLOY MEMBER FOR RESIN BONDING, AND Al-Mg-Si-BASED ALUMINIUM ALLOY MEMBER FOR RESIN BONDING OBTAINED USING SAID METHOD - Google Patents

PRODUCTION METHOD FOR Al-Mg-Si-BASED ALUMINIUM ALLOY MEMBER FOR RESIN BONDING, AND Al-Mg-Si-BASED ALUMINIUM ALLOY MEMBER FOR RESIN BONDING OBTAINED USING SAID METHOD Download PDF

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WO2014170946A1
WO2014170946A1 PCT/JP2013/061217 JP2013061217W WO2014170946A1 WO 2014170946 A1 WO2014170946 A1 WO 2014170946A1 JP 2013061217 W JP2013061217 W JP 2013061217W WO 2014170946 A1 WO2014170946 A1 WO 2014170946A1
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Prior art keywords
aluminum alloy
resin
alloy member
aluminium alloy
resin bonding
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PCT/JP2013/061217
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French (fr)
Japanese (ja)
Inventor
正憲 遠藤
誠己 飯野
みゆき 吉田
昌司 磯部
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日本軽金属株式会社
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Priority to PCT/JP2013/061217 priority Critical patent/WO2014170946A1/en
Publication of WO2014170946A1 publication Critical patent/WO2014170946A1/en

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    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23FNON-MECHANICAL REMOVAL OF METALLIC MATERIAL FROM SURFACE; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL; MULTI-STEP PROCESSES FOR SURFACE TREATMENT OF METALLIC MATERIAL INVOLVING AT LEAST ONE PROCESS PROVIDED FOR IN CLASS C23 AND AT LEAST ONE PROCESS COVERED BY SUBCLASS C21D OR C22F OR CLASS C25
    • C23F1/00Etching metallic material by chemical means
    • C23F1/10Etching compositions
    • C23F1/14Aqueous compositions
    • C23F1/16Acidic compositions
    • C23F1/20Acidic compositions for etching aluminium or alloys thereof
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D21/00Casting non-ferrous metals or metallic compounds so far as their metallurgical properties are of importance for the casting procedure; Selection of compositions therefor
    • B22D21/002Castings of light metals
    • B22D21/007Castings of light metals with low melting point, e.g. Al 659 degrees C, Mg 650 degrees C
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/06Alloys based on aluminium with magnesium as the next major constituent
    • C22C21/08Alloys based on aluminium with magnesium as the next major constituent with silicon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • C22F1/043Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with silicon as the next major constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • C22F1/047Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with magnesium as the next major constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • C22F1/05Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys of the Al-Si-Mg type, i.e. containing silicon and magnesium in approximately equal proportions

Definitions

  • the present invention relates to a method of manufacturing an aluminum alloy member for resin bonding made of an Al-Mg-Si-based aluminum alloy and an aluminum alloy member obtained by this method, and is not particularly limited, but in a harsh environment. Manufacturing method of resin-bonded Al-Mg-Si based aluminum alloy member suitable for many applications including automotive parts, household appliance parts, industrial equipment parts, etc., which are exposed, and obtained by this method.
  • the present invention relates to an Al-Mg-Si aluminum alloy member for resin bonding.
  • Aluminum alloys are lightweight and have excellent workability, as well as excellent mechanical properties, and excellent thermal conductivity, electrical conductivity, corrosion resistance, etc., so they are used for building materials, home appliance materials, vehicles and ships. It is used for a large number of applications such as materials, and especially for Al-Mg-Si-based aluminum alloys, it is excellent in thermal conductivity and conductivity, so that it can be cooled, such as a heat sink using high thermal conductivity. It is widely used for parts and electrical and electronic parts such as busbars and electric wires that use high conductivity. Especially in recent years, in the case of the former use, it is necessary to insulate part of it. In the case of the latter application, it is required to partially insulate a resin that is partially insulative. Sought to join To have.
  • the present inventors previously provided a fine uneven shape on the surface of the aluminum alloy member by hydrochloric acid etching treatment, and using this uneven shape, the resin molded body was joined to the surface of the aluminum alloy member during resin molding.
  • an aluminum / resin injection molded product (aluminum-resin) that retains excellent adhesion and airtightness even in harsh environments such as temperature, humidity, and dust, and also exhibits excellent durability and heat resistance.
  • Patent Document 1 A method for producing a composite was provided (Patent Document 1).
  • the Al-Mg-Si aluminum alloy contains a relatively large amount of Si, and this Si is a chemical other than hydrofluoric acid. Si hardly dissolves on the surface of the aluminum alloy member during the etching process of Al-Mg-Si based aluminum alloy and deposits on the surface of the aluminum alloy member. As a result, there is a problem of adversely affecting the bondability between the aluminum and the resin.
  • this Al-Mg-Si aluminum alloy is not only excellent in corrosion resistance and extrusion processability, but also has high mechanical properties obtained by heat treatment, and also has good anodizing properties, so it is constant.
  • heat treatment solution treatment
  • aging treatment fine Mg 2 Si intermetallic compounds are deposited, making them suitable for various applications such as building materials, housings for home appliances, and parts for vehicles and ships.
  • the Al-Mg-Si-based aluminum alloy sheet is hardened at 500 ° C or higher, and tempered at 200 to 400 ° C.
  • the Mg 2 Si intermetallic compound precipitated in the tempering treatment to an etching treatment to dissolve and remove with an acid aqueous solution, and providing a photosensitive film (photosensitive layer) on the roughened surface formed by the etching treatment
  • Aluminum alloy It is known to produce an aluminum support for a lithographic printing plate support that has excellent adhesion between a metal plate and a photosensitive film (Patent Document 3), and is further subjected to homogenization treatment and hot rolling to obtain a surface.
  • An Al-Mg-Si-based aluminum alloy plate with an exposed Mg 2 Si crystallized material is formed, and this aluminum alloy plate is anodized or etched to desorb the Mg 2 Si crystallized product.
  • resin-coated can barrels where the surface is coated with a polyester, polyolefin, or polyamide resin film with good adhesion using the anchor effect of recesses or holes formed by the separation of Mg 2 Si crystals
  • An aluminum alloy plate is also known (Patent Document 4).
  • the Mg 2 Si crystallized product produced by the heat treatment has various forms such as an acicular phase, a rod-like intermediate phase ⁇ ′, and a plate-like stable phase ⁇ depending on the conditions of the heat treatment. Therefore, the uneven shape formed after etching changes depending on the heat treatment conditions and is not stable.
  • automobiles such as heat sink members for electric and electronic parts, aluminum base heat dissipation bases for LED lighting, water jacket members for liquid cooling units, etc. Adhesion strength and air tightness at the metal-resin interface when exposed to harsh environments such as industrial parts, home appliance parts, industrial equipment parts, etc. The development of metal-resin composites with good properties has been demanded.
  • the present inventors further improved the shear strength at the Al-Mg-Si aluminum alloy-resin molded body interface, and improved the adhesion strength and air tightness at this interface, under severe conditions.
  • a surface treatment layer with an extremely fine uneven shape of crosshead type or expanded metal type is formed on the surface by solution treatment of the aluminum alloy base material under the prescribed conditions and aging treatment under the prescribed conditions.
  • an object of the present invention is to maintain excellent adhesion and airtightness between aluminum and resin by bonding a resin molded body to the surface of an aluminum alloy member made of an Al-Mg-Si based aluminum alloy.
  • -Mg-Si-based aluminum alloys with excellent durability, extrudability, and mechanical properties, and aluminum-resin composites suitable for various applications that are exposed to harsh environments Another object of the present invention is to provide a method for producing an Al—Mg—Si based aluminum alloy member for resin bonding suitable for the purpose.
  • Another object of the present invention is an aluminum which is manufactured by the above-described method and has excellent adhesion and airtightness, as well as excellent durability, extrudability and mechanical properties, and is suitable for various applications. -To provide an Al-Mg-Si-based aluminum alloy member for resin bonding suitable for manufacturing a resin composite.
  • an aluminum alloy base material made of an Al—Mg—Si based aluminum alloy having a Mn content of less than 0.05% by mass is subjected to a solution treatment under conditions of 500 to 600 ° C. and 1 to 20 hours. Then, after cooling, an aging treatment is performed under conditions of 150 to 300 ° C. and 1 to 20 hours, and then an etching treatment with an acidic etchant composed of sulfuric acid and / or an aqueous solution of nitric acid is performed, and the surface of the aluminum alloy substrate is applied.
  • a method for producing an Al—Mg—Si based aluminum alloy member for resin bonding characterized by providing a surface treatment layer.
  • the present invention provides an Al—Mg—Si based aluminum alloy for resin bonding, which is obtained by the above method and has a surface treatment layer having an extremely fine concavo-convex structure of a crosshead type or an expanded metal type on the surface. It is a member.
  • the “cross-head type ultra-fine concavo-convex structure” means a concavo-convex structure in which the tip portion of a part or all of the many convex portions forming the fine concavo-convex structure has a substantially cross shape.
  • the “expanded metal type extremely fine concavo-convex structure” refers to a case in which the fine concavo-convex structure has an expanded metal-like structure in which metal fibers are entangled in a network.
  • Mg is 0.2% by mass or more and 4.0% by mass or less, preferably 0.3% by mass or more and 1.5% by mass.
  • Si content is 0.1% by mass or more and 2.5% by mass or less, preferably 0.3% by mass or more and 1.5% by mass or less.
  • Mg content is less than 0.2% by mass, there is a problem that Mg 2 Si does not sufficiently precipitate, and conversely, when it exceeds 4.0% by mass, there arises a problem that castability deteriorates.
  • the Si content is less than 0.1% by mass, there is a problem that Mg 2 Si does not sufficiently precipitate. Conversely, if the Si content exceeds 2.5% by mass, Si melts during solution treatment, which causes blistering. As a result, there is a danger that the solution treatment at a high temperature becomes difficult. Further, when the Mn content is 0.05% by mass or more, this Mn is preferentially combined with Si to form coarse precipitates (Al—Mn—Si alloy), and as a result, Al—Mg. The shear strength at the interface between the Si-aluminum alloy and the resin molded body is remarkably reduced, and the adhesion strength and airtightness at this interface are also reduced.
  • an aluminum alloy substrate made of the Al-Mg-Si-based aluminum alloy as described above is subjected to a solution treatment under the conditions of 500 ° C. or higher and 600 ° C. or lower and 1 hour or longer and 20 hours or shorter.
  • Mg and Si are dissolved in Al to form Mg 2 Si intermetallic compounds. If the temperature condition at this time is lower than 500 ° C., Mg and Si in the alloy cannot be dissolved in Al, whereas if it is higher than 600 ° C., Al itself melts.
  • an aging treatment is performed again under the conditions of 150 ° C. or more and 300 ° C. or less and 1 hour or more and 20 hours or less, and the solution treatment is generated.
  • Mg 2 Si intermetallic compound in a desired shape that is, a shape of Mg 2 Si intermetallic compound suitable for obtaining a surface treatment layer of a desired cross-head type or expanded metal type fine concavo-convex structure by subsequent etching treatment.
  • Mg 2 Si intermetallic compound in a desired shape that is, a shape of Mg 2 Si intermetallic compound suitable for obtaining a surface treatment layer of a desired cross-head type or expanded metal type fine concavo-convex structure by subsequent etching treatment.
  • Mg 2 Si having a desired shape does not precipitate.
  • it is higher than 300 ° C. Mg 2 Si is excessively enlarged and the dispersibility is lowered.
  • the temperature condition when the above temperature condition is less than 200 ° C., it is transformed into an Mg 2 Si intermetallic compound suitable for obtaining a surface treatment layer of a cross-head type ultra fine concavo-convex structure by etching treatment, In addition, when the temperature is 200 ° C. or higher, it tends to be transformed into an Mg 2 Si intermetallic compound suitable for obtaining a surface treatment layer having an expanded metal type fine concavo-convex structure by etching treatment, and an Al—Mg—Si based aluminum alloy -From the viewpoint of improving the shear strength at the interface of the resin molded body, the temperature condition is preferably 200 ° C or higher and 300 ° C or lower.
  • the aluminum alloy substrate thus prepared is then subjected to an etching treatment using an acidic etching solution composed of an aqueous solution of sulfuric acid and / or nitric acid, and Mg 2 Si present on the surface of the aluminum alloy substrate.
  • An intermetallic compound is dissolved, and a surface treatment layer of a desired crosshead type or expanded metal type extremely fine uneven structure is formed on the surface of the aluminum alloy substrate.
  • the sulfuric acid and / or nitric acid aqueous solution used as the acidic etching solution has an acid concentration of 1% by weight to 60% by weight, preferably 5% by weight to 50% by weight in the case of sulfuric acid aqueous solution.
  • the acid concentration should be 5 to 60% by weight, preferably 10 to 50% by weight. It is preferable to add a nitric acid aqueous solution having an acid concentration of 5% by weight to 30% by weight to a sulfuric acid aqueous solution having an acid concentration of 5% by weight to 50% by weight. If the acid concentration of the acidic etching solution is lower than the above range, the reaction may not proceed sufficiently and the dissolution amount may be insufficient.
  • the reaction rate becomes too fast and it is difficult to control the dissolution amount. become.
  • chromic acid for the purpose of controlling the amount of dissolution, chromic acid, phosphoric acid, acetic acid, oxalic acid, ascorbic acid, benzoic acid, butyric acid, citric acid, formic acid, lactic acid, Acids other than sulfuric acid and nitric acid such as isobutyric acid, malic acid, propionic acid, and tartaric acid may be added.
  • the processing temperature is usually 20 ° C. or higher and 90 ° C. or lower, preferably 30 ° C. or higher and 80 ° C. or lower, and the processing time is usually 1 minute or longer and 20 minutes or shorter. Hereinafter, it is preferably 5 minutes or more and 15 minutes or less. If the processing temperature under the processing conditions of this etching process is lower than 20 ° C., the reaction may not proceed sufficiently and the amount of dissolution may be insufficient. On the other hand, if the processing temperature is higher than 90 ° C., the reaction rate becomes too high and Control becomes difficult.
  • the processing time of the etching process is shorter than 1 minute, the reaction may not proceed sufficiently and the amount of dissolution may be insufficient. On the other hand, if the processing time is longer than 20 minutes, the production efficiency decreases and the mass productivity deteriorates. .
  • this aluminum is used for the purpose of degreasing, surface adjustment, and removal of surface deposits and contaminants.
  • the acid aqueous solution used for this purpose include those prepared with commercially available acidic degreasing agents, mineral acids such as sulfuric acid, nitric acid, hydrofluoric acid, and phosphoric acid, organic acids such as acetic acid and citric acid, and these acids.
  • a 1 to 50% by weight aqueous solution of an acid such as that prepared by using an acid reagent such as a mixed acid obtained by mixing the above
  • examples of the alkaline aqueous solution include a commercially available alkaline degreasing agent. It is preferable to use a 1 to 50% by weight aqueous solution of an alkali such as one prepared, one prepared with an alkali reagent such as caustic soda, or one prepared by mixing these materials. In both cases, the alkaline aqueous solution is preferably about 0.5 to 10 minutes.
  • the trace of the Mg 2 Si intermetallic compound dissolved by the above etching treatment becomes a concave portion, and the surface of the aluminum alloy member has a fine crosshead type or expanded metal type.
  • a surface treatment layer having a concavo-convex structure is formed, and this surface treatment layer exhibits excellent aluminum resin bondability with the resin molded body.
  • the surface treatment layer of the cross head type or expanded metal type ultra fine uneven structure observed on the surface of the aluminum alloy member is formed by the following mechanism. Is done. That is, in the Al—Mg—Si based aluminum alloy containing Mg and Si, the crystal structure of the produced Mg 2 Si intermetallic compound depends on the temperature conditions during solution treatment and aging treatment, as shown in FIG. The transformation is as follows: needle shape (a) ⁇ rod shape (b) ⁇ plate shape (c) ⁇ random cubic shape (d).
  • the crystal structure of this random cubic shape (d) is formed by overlapping the plate-like (c) crystals of Mg 2 Si intermetallic compound, but the crosshead type ultra-fine uneven structure is such a random cube precipitating Mg 2 Si intermetallic compound having a crystal structure of the shape (d), expressing the Mg 2 Si intermetallic compound when dissolved in an aqueous solution of sulfuric acid and / or nitric acid.
  • the crosshead type ultra-fine uneven structure is such a random cube precipitating Mg 2 Si intermetallic compound having a crystal structure of the shape (d), expressing the Mg 2 Si intermetallic compound when dissolved in an aqueous solution of sulfuric acid and / or nitric acid.
  • it is better to sufficiently quench and increase the temperature during the aging treatment In order to prevent precipitation, it is preferable to make quenching insufficient or to lower the temperature during the aging treatment.
  • the surface treatment layer of the expanded metal type ultra-fine concavo-convex structure is obtained when the above plate-like (c) Mg 2 Si intermetallic compound crystals are dissolved without being overlapped and dissolved by etching treatment.
  • the higher the temperature during the aging treatment the more the Mg 2 Si intermetallic compound precipitates. Therefore, the higher the temperature during the aging treatment, the larger the expanded metal type electrode after the etching treatment. It is considered that a fine uneven structure is easily developed.
  • the abundance ratio of the crosshead type uneven structure observed in the surface treatment layer of the aluminum alloy member [ie, scanning electron microscope (Hitachi FE-SEM, S-4500 type) ) Is used to observe the SEM image (FIG. 2 in the case of Example 1), and the result is obtained by image processing as shown in FIG.
  • the area ratio is calculated as the existence ratio of the cross-head concavo-convex structure] is usually 20% to 90%, preferably 35% to 80%. If the ratio of the concave portion on the surface of the aluminum alloy member is lower than 20%, the amount of resin entering the concave portion may be insufficient, which may cause a problem of adversely affecting the resin bonding property.
  • Example 2 the same measuring method [Namely, SEM image (FIG. 5 in the case of Example 2) using a scanning electron microscope (Hitachi FE-SEM, S-4500 type))
  • the presence ratio of the expanded metal structure was calculated from the area ratio of the concave portion in the measurement visual field 0.1 mm square obtained by image processing as shown in FIG.
  • it is 10% or more, preferably 20% or more, improvement in bonding strength and airtightness can be obtained.
  • the aluminum alloy member obtained by the method of the present invention has a surface treatment layer of an extremely fine concavo-convex structure of a crosshead type or an expanded metal type formed on the surface thereof.
  • the resin molded body is formed on the necessary part of the aluminum alloy member by injection molding of a thermoplastic resin using a so-called aluminum alloy member that is injected into a mold and injects a predetermined thermoplastic resin into the mold and solidifies.
  • an aluminum-resin composite is manufactured by bonding, an excellent aluminum resin bonding property is exhibited.
  • thermoplastic resin used in producing the aluminum-resin composite using the aluminum alloy member of the present invention various thermoplastic resins can be used alone, but the aluminum alloy of the present invention is used.
  • the thermoplastic resin is preferably a polypropylene resin, a polyethylene resin, an acrylonitrile-butadiene-styrene copolymer, for example.
  • ABS polycarbonate resin
  • PC polyamide resin
  • PA polyarylene sulfide resin
  • PPS polyphenylene sulfide
  • PES polyacetal resin
  • liquid crystalline resin polyester such as polyethylene terephthalate (PET) and polybutylene terephthalate (PBT) Resin
  • PET polyethylene terephthalate
  • PBT polybutylene terephthalate
  • Resin polyoxymethylene resin
  • PET polyethylene terephthalate
  • PBT polybutylene terephthalate
  • PBT polybutylene terephthalate
  • Examples include syndiotactic polystyrene resin and a mixture of two or more of these thermoplastic resins, and adhesion between an aluminum shaped body and a resin molded body, mechanical strength, heat resistance, dimensional stability (resistance resistance)
  • fillers such as fibrous, granular, and plate-like materials and various elastomer components to these thermoplastic resins. It is good.
  • Fillers added to thermoplastic resins include inorganic fiber fillers such as glass fibers, carbon fibers, metal fibers, asbestos fibers and boron fibers, and high melting point organic fibers such as polyamides, fluororesins and acrylic resins. And powder fillers such as silica powder, glass beads, glass powder, inorganic powders such as calcium carbonate, and plate fillers such as glass flakes, silicates such as talc and mica, etc. In addition, it is added in an amount of 250 parts by weight or less, preferably 20 parts by weight or more and 220 parts by weight or less, more preferably 30 parts by weight or more and 100 parts by weight or less with respect to 100 parts by weight of the thermoplastic resin.
  • inorganic fiber fillers such as glass fibers, carbon fibers, metal fibers, asbestos fibers and boron fibers
  • high melting point organic fibers such as polyamides, fluororesins and acrylic resins.
  • powder fillers such as silica powder, glass beads, glass powder, inorganic powders
  • the elastomer component added to the thermoplastic resin examples include urethane type, core shell type, olefin type, polyester type, amide type, and styrene type elastomers.
  • the melting temperature of the thermoplastic resin at the time of injection molding, etc. it is selected in consideration of 30 parts by weight or less, preferably 3 to 25 parts by weight based on 100 parts by weight of the thermoplastic resin.
  • the added amount of the elastomer component exceeds 30 parts by weight, a further effect of improving the adhesion strength is not seen, and problems such as a decrease in mechanical properties occur.
  • This blending effect of the elastomer component is particularly prominent when a polyester resin is used as the thermoplastic resin.
  • thermoplastic resin for producing the aluminum-resin composite of the present invention includes known additives generally added to thermoplastic resins, that is, flame retardants, colorants such as dyes and pigments, antioxidants, Stabilizers such as ultraviolet absorbers, plasticizers, lubricants, lubricants, mold release agents, crystallization accelerators, crystal nucleating agents, and the like can be appropriately added according to the required performance.
  • thermoplastic resin performed by setting the aluminum alloy member in the injection mold
  • molding conditions required for the thermoplastic resin to be used can be adopted. It is important that the molten thermoplastic resin surely enters and solidifies into the concave part of the aluminum alloy member, and the mold temperature and cylinder temperature are compared within the range that the type and physical properties of the thermoplastic resin and the molding cycle allow.
  • the lower limit temperature must be 90 ° C. or higher, preferably 130 ° C. or higher, especially for the mold temperature, but the upper limit is 100 depending on the type of thermoplastic resin used.
  • the temperature ranges from °C to a temperature about 20 °C lower than the melting point or softening point of the thermoplastic resin (if the elastomer component is added, the higher melting point or softening point). Good it is. Further, the lower limit mold temperature is preferably set so as not to be lowered by 140 ° C. or more from the melting point of the thermoplastic resin.
  • the aluminum-resin composite manufacturing method performed using the aluminum alloy member of the present invention is not limited to the above-described thermoplastic resin injection integral molding method, and a thermocompression bonding method may be employed. That is, first, an aluminum alloy member is heated to a temperature of about 90 to 300 ° C. in accordance with the melting temperature of the thermoplastic resin to be used, and a thermoplastic resin molding is pressed against the surface of the aluminum alloy member under pressure. A desired aluminum-resin composite is produced by melting a part of the surface of the molded body to enter the concave portion of the surface of the aluminum alloy member, and further cooling under pressure.
  • a resin molded body is bonded to the surface of an aluminum alloy member made of an Al-Mg-Si-based aluminum alloy, thereby maintaining excellent adhesion and airtightness between the aluminum and the resin, and Al-Mg -Manufacturing Al-Mg-Si-based aluminum alloy members for resin bonding suitable for manufacturing aluminum-resin composites having the inherent durability, extrudability, and mechanical properties of Si-based aluminum alloys Can do.
  • the produced aluminum-resin composite has excellent adhesion and airtightness, it can be used in harsh environments such as automobile parts, home appliance parts, industrial equipment parts and the like. Suitable for various applications where there is an opportunity to be exposed.
  • FIG. 1 is an explanatory diagram for explaining a mechanism (estimation) for forming a surface treatment layer having an extremely fine uneven structure of a crosshead type or an expanded metal type in the method of the present invention.
  • FIG. 2 is a photograph showing an SEM image obtained when the surface of the aluminum alloy member obtained in Example 1 of the present invention was observed with a scanning electron microscope.
  • FIG. 3 is a photograph showing a processed image after the image processing of the SEM image of FIG.
  • FIG. 4 is a photograph showing an SEM image obtained when the resin-side surface shape of the aluminum-resin composite obtained in Example 1 after complete aluminum removal was observed with a scanning electron microscope.
  • FIG. 5 is a photograph showing an SEM image of the same aluminum alloy member surface as in FIG. 2 obtained in Example 2 of the present invention.
  • FIG. 6 is a photograph showing an SEM image in which a part of FIG. 5 is enlarged.
  • FIG. 7 is a photograph similar to FIG. 3 showing the processed image after the image processing of the SEM image of FIG.
  • FIG. 8 is a photograph showing a processed image after image processing in which only the expanded metal structure portion in the SEM image of FIG. 5 is extracted by image processing.
  • FIG. 9 is a photograph showing an SEM image of the resin-side surface shape similar to that of FIG. 4 obtained in Example 2.
  • FIG. 10 is a photograph showing an SEM image of the same aluminum alloy member surface as in FIG. 2 obtained in Example 3 of the present invention.
  • FIG. 11 is a photograph similar to FIG. 3 showing a processed image after image processing of the SEM image of FIG.
  • FIG. 12 is a photograph showing an SEM image of the resin-side surface shape similar to FIG. 4 obtained in Example 3.
  • FIG. 13 is a photograph showing an SEM image of the same aluminum alloy member surface as in FIG. 2 obtained in Example 4 of the present invention.
  • FIG. 14 is a photograph showing an SEM image in which a part of FIG. 13 is enlarged.
  • FIG. 15 is a photograph similar to FIG. 3 showing the processed image after the image processing of the SEM image of FIG.
  • FIG. 16 is a photograph similar to FIG. 8 showing a processed image after image processing in which only the expanded metal structure in the SEM image of FIG. 13 is extracted by image processing.
  • FIG. 17 is a photograph showing an SEM image of the resin-side surface shape similar to FIG. 4 obtained in Example 4.
  • FIG. 18 is a photograph showing an SEM image of the same aluminum alloy member surface as in FIG. 2 obtained in Example 5 of the present invention.
  • FIG. 19 is a photograph similar to FIG. 3 showing the processed image after the image processing of the SEM image of FIG.
  • FIG. 20 is a photograph showing an SEM image of the resin-side surface shape similar to that of FIG. 4 obtained in Example 5.
  • FIG. 20 is a photograph showing an SEM image of the resin-side surface shape similar to that of FIG. 4 obtained in Example 5.
  • FIG. 21 is a photograph showing an SEM image of the same aluminum alloy member surface as in FIG. 2 obtained in Example 6 of the present invention.
  • FIG. 22 is a photograph similar to FIG. 3 showing a processed image after the image processing of the SEM image of FIG.
  • FIG. 23 is a photograph showing an SEM image of the resin-side surface shape similar to FIG. 4 obtained in Example 6.
  • FIG. 24 is a photograph showing an SEM image of the same aluminum alloy member surface as in FIG. 2 obtained in Comparative Example 1 of the present invention.
  • FIG. 25 is a photograph similar to FIG. 3 showing a processed image after the image processing of the SEM image of FIG.
  • FIG. 26 is a photograph showing an SEM image of the resin-side surface shape similar to that of FIG. 4 obtained in Comparative Example 1.
  • FIG. 27 is a photograph showing an SEM image of the same aluminum alloy member surface as in FIG. 2 obtained in Comparative Example 2 of the present invention.
  • FIG. 28 is a photograph similar to FIG. 3 showing the processed image after the image processing of the SEM image of FIG.
  • FIG. 29 is a photograph showing an SEM image of the resin-side surface shape similar to that of FIG. 4 obtained in Comparative Example 2.
  • FIG. 29 is a photograph showing an SEM image of the resin-side surface shape similar to that of FIG. 4 obtained in Comparative Example 2.
  • FIG. 30 is an explanatory view showing an aluminum resin test piece (aluminum-resin composite) for a shear fracture load measurement test produced using the aluminum alloy member obtained in each example and each comparative example.
  • FIG. 31 is an explanatory diagram for explaining a state in which an aluminum resin test piece is fixed to a test piece fixing jig of a shear fracture load measurement tester and a shear fracture load is measured.
  • Example 1 Preparation of aluminum alloy base material After casting an Al-Mg-Si based aluminum alloy containing Si: 0.21% by mass, Mg: 0.42% by mass, and Mn: 0.01% by mass in a casting furnace, extrusion processing Then, a flat bar (aluminum alloy base material) having a size of 2050 mm ⁇ 800 mm ⁇ 3 mm was formed.
  • the heat-treated aluminum alloy base material obtained above was immersed in 30 wt% nitric acid aqueous solution at room temperature for 1 minute, then thoroughly washed with ion-exchanged water, and then immersed in 5 wt% sodium hydroxide aqueous solution at 50 ° C for 1 minute. Then, it was washed with water and further pretreated by immersing it in a 30 wt% nitric acid aqueous solution at room temperature for 1 minute and then washing with water.
  • the pre-treated aluminum alloy base material after the heat treatment was subjected to an etching treatment in which it was immersed in a 10 wt% -sulfuric acid aqueous solution at 30 ° C. for 10 minutes and then washed with water.
  • the aluminum alloy member of Example 1 was produced by drying for a minute.
  • the surface of the aluminum alloy member of Example 1 obtained in this way was observed with a scanning electron microscope (Hitachi FE-SEM, model S-4500), and thereafter image processing was performed to obtain a length of 0.
  • the existence ratio (area ratio) of the concave portion having a size of 1 to 10.0 ⁇ m was calculated.
  • using an X-ray diffraction apparatus Riviere RAD-rR, the integrated diffraction strength value of the intermetallic compound existing on the surface of the obtained aluminum alloy base material was measured, and the result showed that The ratio of Mg 2 Si intermetallic compound was determined.
  • FIG. 2 shows the SEM image of the surface of the aluminum alloy member obtained at this time
  • FIG. 3 shows the processed image after the image processing
  • Table 1 shows the result.
  • Example 1 An aluminum-resin composite of Example 1 was prepared in which the resin molded body 2 was integrally bonded with an area of 40 mm ⁇ 10 mm ⁇ 5 mm. Two aluminum-resin composites of Example 1 were prepared for the resin side surface observation and for the shear fracture load measurement test.
  • Example 4 Observation of the resin-side surface of the aluminum-resin composite
  • the aluminum-resin composite obtained in Example 1 was immersed in a 10 wt% -sodium hydroxide aqueous solution at 80 ° C. for 10 hours to completely cover the aluminum side of the aluminum-resin composite.
  • the surface of the obtained specimen is observed with a scanning electron microscope (Hitachi FE-SEM, S-4500 type), and an aluminum-resin composite is obtained.
  • the shape of the surface of the resin molded body side at the aluminum-resin bonding interface was examined, and the existence ratio of the concavo-convex structure of the crosshead type or the expanded metal type was examined.
  • the SEM image of the resin molded body surface obtained at this time is shown in FIG. 4 and the results are shown in Table 1.
  • Examples 2 to 5 and Comparative Examples 1 and 2 After casting an Al—Mg—Si based aluminum alloy having the composition shown in Table 1 for Mg, Si, and Mn in a casting furnace, a flat bar (aluminum alloy substrate) was formed in the same manner as in Example 1, and then The aluminum alloy members of Examples 2 to 6 and Comparative Examples 1 and 2 were prepared in the same manner as in Example 1 except that solution treatment, aging treatment, and etching treatment with an aqueous sulfuric acid solution were performed under the conditions shown in Table 1. Prepared.
  • Example 6 The post-heat treatment aluminum alloy base material obtained in the same manner as in Example 1 is subjected to the same pretreatment as in Example 1, and then immersed in a 10 wt% nitric acid aqueous solution at 30 ° C. for 10 minutes and then washed with water. And then washed with water and dried with hot air at 80 ° C. for 5 minutes to produce an aluminum alloy member.
  • FIG. 5 shows an SEM image of the surface of the aluminum alloy member obtained in Example 2
  • FIG. 6 shows an enlarged image of the SEM image
  • FIG. 7 shows a processed image after the image processing
  • FIG. FIG. 8 shows a processed image obtained by extracting only the expanded metal structure portion in FIG. 8,
  • FIG. 9 shows an SEM image of the surface of the resin molded body.
  • FIG. 10 shows the SEM image of the surface of the aluminum alloy member obtained in Example 3
  • FIG. 11 shows the processed image after the image processing
  • FIG. 12 shows the SEM image of the surface of the resin molded body.
  • FIG. 13 shows an SEM image of the surface of the aluminum alloy member obtained in Example 4
  • FIG. 14 shows an enlarged image of the SEM image
  • FIG. 15 shows a processed image after the image processing
  • FIG. 16 shows a processed image obtained by extracting only the metal structure portion by image processing
  • FIG. 17 shows an SEM image of the surface of the resin molded body.
  • FIG. 18 shows the SEM image of the surface of the aluminum alloy member obtained in Example 5
  • FIG. 19 shows the processed image after the image processing
  • FIG. 20 shows the SEM image of the surface of the resin molded body.
  • FIG. 21 shows an SEM image of the surface of the aluminum alloy member obtained in Example 6,
  • FIG. 22 shows a processed image after the image processing, and
  • FIG. 23 shows an SEM image of the surface of the resin molded body.
  • FIG. 24 shows the SEM image of the surface of the aluminum alloy member obtained in Comparative Example 1
  • FIG. 25 shows the processed image after the image processing
  • FIG. 26 shows the SEM image of the surface of the resin molded body.
  • the SEM image of the aluminum alloy member surface obtained in Comparative Example 2 is shown in FIG. 27, the processed image after the image processing is shown in FIG. 28, and the SEM image of the resin molded body surface is shown in FIG.

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Abstract

Provided is a production method for an Al-Mg-Si-based aluminium alloy member for resin bonding, said method being suitable for producing, by bonding a resin moulded body to a surface of the Al-Mg-Si-based aluminium alloy member, an aluminium/resin composite which maintains excellent adhesive properties and airtightness between the aluminium and resin therein, which exhibits excellent durability with respect to the original aluminium alloy therein, excellent extrusion processing properties, and excellent mechanical properties, and which is suitable for a variety of uses wherein exposure to severe environments may occur. In this production method for an Al-Mg-Si-based aluminium alloy member for resin bonding, an Al-Mg-Si-based aluminium alloy substrate having an Mn content of less than 0.05 mass% is: subjected to solution treatment under conditions in which the temperature is 500-600˚C for a period of 1-20 hours; subsequently subjected to ageing treatment under conditions in which the temperature is 150-300˚C for a period of 1-20 hours; and subjected thereafter to etching using an aqueous solution of sulphuric acid and/or nitric acid to impart a surface-treated layer upon a surface of the aluminium alloy substrate.

Description

樹脂接合用Al-Mg-Si系アルミ合金部材の製造方法及びこの方法で得られた樹脂接合用Al-Mg-Si系アルミ合金部材Method for producing Al-Mg-Si based aluminum alloy member for resin bonding and Al-Mg-Si based aluminum alloy member for resin bonding obtained by this method
 この発明は、Al-Mg-Si系アルミニウム合金からなる樹脂接合用のアルミ合金部材の製造方法及びこの方法で得られたアルミ合金部材に係り、特に限定するものではないが、過酷な環境下に曝される機会のある自動車用部品、家電機器用部品、産業機器用部品等を始めとする多くの用途に好適な樹脂接合用Al-Mg-Si系アルミ合金部材の製造方法及びこの方法で得られた樹脂接合用Al-Mg-Si系アルミ合金部材に関する。 The present invention relates to a method of manufacturing an aluminum alloy member for resin bonding made of an Al-Mg-Si-based aluminum alloy and an aluminum alloy member obtained by this method, and is not particularly limited, but in a harsh environment. Manufacturing method of resin-bonded Al-Mg-Si based aluminum alloy member suitable for many applications including automotive parts, household appliance parts, industrial equipment parts, etc., which are exposed, and obtained by this method The present invention relates to an Al-Mg-Si aluminum alloy member for resin bonding.
 アルミニウム合金は、軽量で加工性に富むほか機械的性質にも優れ、しかも、優れた熱伝導性、導電性、耐食性等の特性を有することから、建築材料、家電機器用材料、車両・船舶用材料等の極めて多くの用途に供されており、特にAl-Mg-Si系アルミニウム合金については、熱伝導性及び導電性に優れていることから、例えば高熱伝導性を利用したヒートシンク等の放冷部品や高導電性を利用したブスバー、電線等の電気電子部品等の用途に多用されており、そして、特に近年においては、前者の用途の場合には、その一部を断熱したい等のニーズから、部分的に断熱性に富む樹脂を接合することが求められ、また、後者の用途の場合には、その一部を電気的に絶縁したい等のニーズから、部分的に絶縁性に富む樹脂を接合することが求められている。 Aluminum alloys are lightweight and have excellent workability, as well as excellent mechanical properties, and excellent thermal conductivity, electrical conductivity, corrosion resistance, etc., so they are used for building materials, home appliance materials, vehicles and ships. It is used for a large number of applications such as materials, and especially for Al-Mg-Si-based aluminum alloys, it is excellent in thermal conductivity and conductivity, so that it can be cooled, such as a heat sink using high thermal conductivity. It is widely used for parts and electrical and electronic parts such as busbars and electric wires that use high conductivity. Especially in recent years, in the case of the former use, it is necessary to insulate part of it. In the case of the latter application, it is required to partially insulate a resin that is partially insulative. Sought to join To have.
 そして、このような用途に用いられ、部分的に樹脂を接合すること(部分的な樹脂化)が求められる場合、これまではビス止めや接着剤等の手段が採用されていたが、これらの手段による部分的な樹脂化には、製造工程での工程数が増加するほか、重量増加の原因にもなり、これらビス止めや接着剤等の手段を必要としないアルミ-樹脂接合技術の開発が求められていた。 And when it is used for such applications and it is required to partially join the resin (partial resinization), means such as screws and adhesives have been used so far. In addition to the increase in the number of steps in the manufacturing process, the partial resinization by means also leads to an increase in weight, and the development of aluminum-resin bonding technology that does not require these means such as screws and adhesives. It was sought after.
 そこで、本発明者らは、先に塩酸系エッチング処理によりアルミ合金部材の表面に微細な凹凸形状を付与し、この凹凸形状を利用して樹脂成形時にアルミ合金部材の表面に樹脂成形体を接合し、これによって温度や湿度、粉塵等において過酷な環境下でも優れた密着性及び気密性を保持すると共に、優れた耐久性や耐熱性をも発揮するアルミ・樹脂射出一体成形品(アルミ-樹脂複合体)の製造方法を提供した(特許文献1)。しかしながら、Al-Mg-Si系アルミニウム合金にこのアルミ-樹脂接合技術をそのまま適用した場合には、Al-Mg-Si系アルミニウム合金が比較的多量のSiを含み、このSiがフッ酸以外の薬品にはほとんど溶解しないことから、Al-Mg-Si系アルミニウム合金のエッチング処理の際にSiがアルミ合金部材の表面で溶け残って堆積し、成形された樹脂成形体との間の密着性が損なわれ、アルミ-樹脂間の接合性に悪影響を及ぼすという問題があった。 Therefore, the present inventors previously provided a fine uneven shape on the surface of the aluminum alloy member by hydrochloric acid etching treatment, and using this uneven shape, the resin molded body was joined to the surface of the aluminum alloy member during resin molding. As a result, an aluminum / resin injection molded product (aluminum-resin) that retains excellent adhesion and airtightness even in harsh environments such as temperature, humidity, and dust, and also exhibits excellent durability and heat resistance. A method for producing a composite was provided (Patent Document 1). However, when this aluminum-resin bonding technology is applied to an Al-Mg-Si aluminum alloy as it is, the Al-Mg-Si aluminum alloy contains a relatively large amount of Si, and this Si is a chemical other than hydrofluoric acid. Si hardly dissolves on the surface of the aluminum alloy member during the etching process of Al-Mg-Si based aluminum alloy and deposits on the surface of the aluminum alloy member. As a result, there is a problem of adversely affecting the bondability between the aluminum and the resin.
 ところで、このAl-Mg-Si系アルミニウム合金は、耐食性や押出加工性に優れているだけでなく、熱処理によって高い機械的性質が得られ、また、陽極酸化処理特性も良好であることから、一定の熱処理(溶体化処理)と時効処理とを施すことにより微細なMg2Siの金属間化合物を析出させ、建築材、家電製品の筐体、車両・船舶等の部材等の様々な用途に適したアルミニウム合金材とすることが知られており(特許文献2)、また、このようなAl-Mg-Si系のアルミニウム合金板に500℃以上での焼入れ処理、200~400℃での焼戻し処理、及び、焼戻し処理で析出したMg2Si金属間化合物を酸水溶液で溶解して除去するエッチング処理を施し、エッチング処理で形成された粗面化表面上に感光膜(感光層)設けることにより、アルミニウム合金板と感光膜との間の密着性に優れた平版印刷版支持体用アルミニウム支持体を製造することが知られており(特許文献3)、更に、均質化処理及び熱間圧延を経て表面にMg2Si晶出物が露出したAl-Mg-Si系のアルミニウム合金板を形成し、このアルミニウム合金板に陽極酸化処理又はエッチング処理を施してMg2Si晶出物を脱離させ、このMg2Si晶出物が離脱して形成された凹部又は脱離穴によるアンカー効果を利用して表面にポリエステル系、ポリオレフィン系、又はポリアミド系の樹脂フィルムを密着性良く被覆した樹脂被覆缶胴用アルミニウム合金板も知られている(特許文献4)。 By the way, this Al-Mg-Si aluminum alloy is not only excellent in corrosion resistance and extrusion processability, but also has high mechanical properties obtained by heat treatment, and also has good anodizing properties, so it is constant. By applying heat treatment (solution treatment) and aging treatment, fine Mg 2 Si intermetallic compounds are deposited, making them suitable for various applications such as building materials, housings for home appliances, and parts for vehicles and ships. (Alternatively, it is known that the Al-Mg-Si-based aluminum alloy sheet is hardened at 500 ° C or higher, and tempered at 200 to 400 ° C.) And, by subjecting the Mg 2 Si intermetallic compound precipitated in the tempering treatment to an etching treatment to dissolve and remove with an acid aqueous solution, and providing a photosensitive film (photosensitive layer) on the roughened surface formed by the etching treatment, Aluminum alloy It is known to produce an aluminum support for a lithographic printing plate support that has excellent adhesion between a metal plate and a photosensitive film (Patent Document 3), and is further subjected to homogenization treatment and hot rolling to obtain a surface. An Al-Mg-Si-based aluminum alloy plate with an exposed Mg 2 Si crystallized material is formed, and this aluminum alloy plate is anodized or etched to desorb the Mg 2 Si crystallized product. For resin-coated can barrels where the surface is coated with a polyester, polyolefin, or polyamide resin film with good adhesion using the anchor effect of recesses or holes formed by the separation of Mg 2 Si crystals An aluminum alloy plate is also known (Patent Document 4).
 しかしながら、これらの特許文献3~4の場合においても、熱処理によって生成するMg2Si晶出物がこの熱処理の条件によって針状相、棒状中間相β’、板状安定相β等の種々の形態をとることから、熱処理条件によってエッチング後に形成される凹凸形状が変化して安定せず、例えば、電気電子部品向けヒートシンク部材、LED照明用アルミベース放熱基盤、液冷ユニット向けウォータージャケット部材等の自動車用部品、家電機器用部品、産業機器用部品等の如く過酷な環境下に曝された際における金属-樹脂の界面での密着強度及び気密性が必ずしも充分ではなく、より優れた密着強度及び気密性を持つ金属-樹脂複合体の開発が要請されていた。 However, even in these Patent Documents 3 to 4, the Mg 2 Si crystallized product produced by the heat treatment has various forms such as an acicular phase, a rod-like intermediate phase β ′, and a plate-like stable phase β depending on the conditions of the heat treatment. Therefore, the uneven shape formed after etching changes depending on the heat treatment conditions and is not stable. For example, automobiles such as heat sink members for electric and electronic parts, aluminum base heat dissipation bases for LED lighting, water jacket members for liquid cooling units, etc. Adhesion strength and air tightness at the metal-resin interface when exposed to harsh environments such as industrial parts, home appliance parts, industrial equipment parts, etc. The development of metal-resin composites with good properties has been demanded.
WO2009/151、099A1号公報WO2009 / 151, 099A1 publication 特開平10-088,300号公報Japanese Patent Laid-Open No. 10-088,300 特開昭59-220,395号公報JP 59-220,395 特開2000-309,839号公報JP 2000-309,839 A
 そして、本発明者らは、Al-Mg-Si系アルミニウム合金が有する特性を損なうことなく、例えば過酷な環境下に曝される機会のある自動車用部品、家電機器用部品、産業機器用部品等の多くの用途において使用するのに好適な樹脂接合用Al-Mg-Si系アルミ合金部材の製造方法について種々検討を重ねる中で、意外なことには、機械的強度の改善に有効なMnの含有量が0.05質量%以上になると、製造されたアルミ-樹脂複合体のAl-Mg-Si系アルミニウム合金-樹脂成形体の界面での剪断強度が顕著に低下し、また、この界面での密着強度及び気密性が低下することを見い出した。 And the present inventors do not impair the characteristics of Al-Mg-Si-based aluminum alloys, for example, automotive parts, household appliance parts, industrial equipment parts, etc. that are exposed to harsh environments. As a result of various studies on a method for producing an Al-Mg-Si-based aluminum alloy member for resin bonding suitable for use in many applications, it is surprising that Mn is effective for improving mechanical strength. When the content is 0.05% by mass or more, the shear strength of the manufactured aluminum-resin composite at the Al-Mg-Si-based aluminum alloy-resin molded body interface is significantly reduced. It has been found that the adhesion strength and airtightness of the resin deteriorate.
 そこで、本発明者らは、更にこのAl-Mg-Si系アルミニウム合金-樹脂成形体の界面での剪断強度の向上を図り、この界面での密着強度及び気密性を改善して過酷な環境下に曝される機会のある多くの用途に好適な樹脂接合用Al-Mg-Si系アルミ合金部材を開発すべく鋭意検討した結果、Mnの含有量が0.05質量未満のAl-Mg-Si系アルミ合金基材を所定の条件下で溶体化処理すると共に所定の条件下で時効処理を行なうことにより、表面にクロスヘッド型又はエキスパンドメタル型の極微細な凹凸形状を有する表面処理層を形成することができ、これによって、この表面処理層の上に設けられる樹脂成形体との間の界面での剪断強度を改善できることを見い出し、本発明を完成した。 Therefore, the present inventors further improved the shear strength at the Al-Mg-Si aluminum alloy-resin molded body interface, and improved the adhesion strength and air tightness at this interface, under severe conditions. As a result of intensive investigations to develop resin-bonded Al-Mg-Si based aluminum alloy members suitable for many applications that are exposed to exposure to Al-Mg-Si with an Mn content of less than 0.05 mass A surface treatment layer with an extremely fine uneven shape of crosshead type or expanded metal type is formed on the surface by solution treatment of the aluminum alloy base material under the prescribed conditions and aging treatment under the prescribed conditions Thus, the present inventors have found that the shear strength at the interface with the resin molded body provided on the surface treatment layer can be improved, thereby completing the present invention.
 従って、本発明の目的は、Al-Mg-Si系アルミニウム合金からなるアルミ合金部材の表面に樹脂成形体を接合することにより、アルミ-樹脂間において優れた密着性及び気密性を保持すると共にAl-Mg-Si系アルミニウム合金本来の優れた耐久性、押出加工性、及び機械的特性を有し、過酷な環境下に曝される機会のある種々の用途に適したアルミ-樹脂複合体を製造するのに好適な樹脂接合用Al-Mg-Si系アルミ合金部材の製造方法を提供することにある。 Therefore, an object of the present invention is to maintain excellent adhesion and airtightness between aluminum and resin by bonding a resin molded body to the surface of an aluminum alloy member made of an Al-Mg-Si based aluminum alloy. -Mg-Si-based aluminum alloys with excellent durability, extrudability, and mechanical properties, and aluminum-resin composites suitable for various applications that are exposed to harsh environments Another object of the present invention is to provide a method for producing an Al—Mg—Si based aluminum alloy member for resin bonding suitable for the purpose.
 また、本発明の目的は、上記の方法によって製造され、優れた密着性及び気密性を有すると共に優れた耐久性、押出加工性、及び機械的特性をも有し、種々の用途に適したアルミ-樹脂複合体の製造に好適な樹脂接合用Al-Mg-Si系アルミ合金部材を提供することにある。 Another object of the present invention is an aluminum which is manufactured by the above-described method and has excellent adhesion and airtightness, as well as excellent durability, extrudability and mechanical properties, and is suitable for various applications. -To provide an Al-Mg-Si-based aluminum alloy member for resin bonding suitable for manufacturing a resin composite.
 すなわち、本発明は、Mnの含有量が0.05質量%未満であるAl-Mg-Si系アルミニウム合金からなるアルミ合金基材を500~600℃及び1~20時間の条件で溶体化処理し、次いで冷却した後に150~300℃及び1~20時間の条件で時効処理を行った後、硫酸及び/又は硝酸の水溶液からなる酸性エッチング液によるエッチング処理を施し、前記アルミ合金基材の表面に表面処理層を付与することを特徴とする樹脂接合用Al-Mg-Si系アルミ合金部材の製造方法である。 That is, in the present invention, an aluminum alloy base material made of an Al—Mg—Si based aluminum alloy having a Mn content of less than 0.05% by mass is subjected to a solution treatment under conditions of 500 to 600 ° C. and 1 to 20 hours. Then, after cooling, an aging treatment is performed under conditions of 150 to 300 ° C. and 1 to 20 hours, and then an etching treatment with an acidic etchant composed of sulfuric acid and / or an aqueous solution of nitric acid is performed, and the surface of the aluminum alloy substrate is applied. A method for producing an Al—Mg—Si based aluminum alloy member for resin bonding, characterized by providing a surface treatment layer.
 また、本発明は、上記の方法によって得られ、表面にクロスヘッド型又はエキスパンドメタル型の極微細な凹凸構造の表面処理層を有することを特徴とする樹脂接合用Al-Mg-Si系アルミ合金部材である。ここで、本発明において「クロスヘッド型の極微細な凹凸構造」とは、微細な凹凸構造を形成する多数の凸部の一部又は全部においてその先端部分が略々十字架形状を有する凹凸構造である場合をいい、また、本発明において「エキスパンドメタル型の極微細な凹凸構造」とは、微細な凹凸構造があたかも金属繊維が網目状に絡まり合ってエキスパンドメタル様の構造を呈する場合をいう。 In addition, the present invention provides an Al—Mg—Si based aluminum alloy for resin bonding, which is obtained by the above method and has a surface treatment layer having an extremely fine concavo-convex structure of a crosshead type or an expanded metal type on the surface. It is a member. Here, in the present invention, the “cross-head type ultra-fine concavo-convex structure” means a concavo-convex structure in which the tip portion of a part or all of the many convex portions forming the fine concavo-convex structure has a substantially cross shape. In addition, in the present invention, the “expanded metal type extremely fine concavo-convex structure” refers to a case in which the fine concavo-convex structure has an expanded metal-like structure in which metal fibers are entangled in a network.
 本発明において、前記アルミ合金基材を構成するAl-Mg-Si系アルミニウム合金については、Mgを0.2質量%以上4.0質量%以下、好ましくは0.3質量%以上1.5質量%以下の範囲で含有すると共に、Siを0.1質量%以上2.5質量%以下、好ましくは0.3質量%以上1.5質量%以下の範囲で含有し、Mnの含有量については、できるだけ少ないのがよく、0.05質量%未満、好ましくは0.04質量%未満であるのがよい。Mgの含有量が0.2質量%より少ないとMg2Siが十分に析出しないという問題があり、反対に、4.0質量%より多くなると鋳造性が低下するという問題が生じる。また、Siの含有量が0.1質量%より少ないとMg2Siが十分に析出しないという問題があり、反対に、2.5質量%より多くなると溶体化処理時にSiが溶融することによりブリスターが発生する危険が生じ、高い温度での溶体化処理が困難になるという問題が生じる。更に、Mnの含有量が0.05質量%以上になると、このMnが優先的にSiと結合して粗大な析出物(Al-Mn-Si系合金)を形成するため、結果としてAl-Mg-Si系アルミニウム合金-樹脂成形体の界面での剪断強度が顕著に低下し、また、この界面での密着強度及び気密性が低下する。 In the present invention, regarding the Al—Mg—Si based aluminum alloy constituting the aluminum alloy base material, Mg is 0.2% by mass or more and 4.0% by mass or less, preferably 0.3% by mass or more and 1.5% by mass. In addition, the Si content is 0.1% by mass or more and 2.5% by mass or less, preferably 0.3% by mass or more and 1.5% by mass or less. , It should be as little as possible, less than 0.05% by weight, preferably less than 0.04% by weight. When the Mg content is less than 0.2% by mass, there is a problem that Mg 2 Si does not sufficiently precipitate, and conversely, when it exceeds 4.0% by mass, there arises a problem that castability deteriorates. Further, if the Si content is less than 0.1% by mass, there is a problem that Mg 2 Si does not sufficiently precipitate. Conversely, if the Si content exceeds 2.5% by mass, Si melts during solution treatment, which causes blistering. As a result, there is a danger that the solution treatment at a high temperature becomes difficult. Further, when the Mn content is 0.05% by mass or more, this Mn is preferentially combined with Si to form coarse precipitates (Al—Mn—Si alloy), and as a result, Al—Mg. The shear strength at the interface between the Si-aluminum alloy and the resin molded body is remarkably reduced, and the adhesion strength and airtightness at this interface are also reduced.
 本発明においては、上記の如きAl-Mg-Si系アルミニウム合金からなるアルミ合金基材を、先ず、500℃以上600℃以下及び1時間以上20時間以下の条件で溶体化処理し、合金中のMg及びSiをAl中に固溶化させ、Mg2Si金属間化合物を生成させる。この際の温度条件が、500℃より低いと合金中のMg及びSiをAl中に固溶させることができず、反対に、600℃より高くなるとAl自体が溶融してしまう。 In the present invention, first, an aluminum alloy substrate made of the Al-Mg-Si-based aluminum alloy as described above is subjected to a solution treatment under the conditions of 500 ° C. or higher and 600 ° C. or lower and 1 hour or longer and 20 hours or shorter. Mg and Si are dissolved in Al to form Mg 2 Si intermetallic compounds. If the temperature condition at this time is lower than 500 ° C., Mg and Si in the alloy cannot be dissolved in Al, whereas if it is higher than 600 ° C., Al itself melts.
 また、本発明においては、上記の溶体化処理が終了して一旦冷却した後に、再び、150℃以上300℃以下及び1時間以上20時間以下の条件で時効処理を行ない、溶体化処理で生成したMg2Si金属間化合物を所望の形状、すなわち次のエッチング処理により所望のクロスヘッド型又はエキスパンドメタル型の極微細な凹凸構造の表面処理層を得るのに適したMg2Si金属間化合物の形状に変態化させる。この際の温度条件が、150℃より低いと所望の形状を有するMg2Siが析出せず、反対に、300℃より高くなるとMg2Siが肥大化し過ぎて分散性が低下する。 Further, in the present invention, after the above solution treatment is completed and once cooled, an aging treatment is performed again under the conditions of 150 ° C. or more and 300 ° C. or less and 1 hour or more and 20 hours or less, and the solution treatment is generated. Mg 2 Si intermetallic compound in a desired shape, that is, a shape of Mg 2 Si intermetallic compound suitable for obtaining a surface treatment layer of a desired cross-head type or expanded metal type fine concavo-convex structure by subsequent etching treatment. To metamorphose. If the temperature condition at this time is lower than 150 ° C., Mg 2 Si having a desired shape does not precipitate. On the other hand, if it is higher than 300 ° C., Mg 2 Si is excessively enlarged and the dispersibility is lowered.
 そして、この時効処理において、上記の温度条件が200℃未満であるとエッチング処理によりクロスヘッド型の極微細な凹凸構造の表面処理層を得るのに適したMg2Si金属間化合物に変態し、また、200℃以上であるとエッチング処理によりエキスパンドメタル型極微細な凹凸構造の表面処理層を得るのに適したMg2Si金属間化合物に変態する傾向にあり、Al-Mg-Si系アルミニウム合金-樹脂成形体の界面での剪断強度の向上を図るという観点からは、好ましくは温度条件を200℃以上300℃以下にするのがよい。 And in this aging treatment, when the above temperature condition is less than 200 ° C., it is transformed into an Mg 2 Si intermetallic compound suitable for obtaining a surface treatment layer of a cross-head type ultra fine concavo-convex structure by etching treatment, In addition, when the temperature is 200 ° C. or higher, it tends to be transformed into an Mg 2 Si intermetallic compound suitable for obtaining a surface treatment layer having an expanded metal type fine concavo-convex structure by etching treatment, and an Al—Mg—Si based aluminum alloy -From the viewpoint of improving the shear strength at the interface of the resin molded body, the temperature condition is preferably 200 ° C or higher and 300 ° C or lower.
 このようにして調製されたアルミ合金基材については、次に、硫酸及び/又は硝酸の水溶液からなる酸性エッチング液を用いてエッチング処理を行い、このアルミ合金基材の表面に存在するMg2Si金属間化合物を溶解し、アルミ合金基材の表面に所望のクロスヘッド型又はエキスパンドメタル型の極微細な凹凸構造の表面処理層を形成せしめる。 The aluminum alloy substrate thus prepared is then subjected to an etching treatment using an acidic etching solution composed of an aqueous solution of sulfuric acid and / or nitric acid, and Mg 2 Si present on the surface of the aluminum alloy substrate. An intermetallic compound is dissolved, and a surface treatment layer of a desired crosshead type or expanded metal type extremely fine uneven structure is formed on the surface of the aluminum alloy substrate.
 ここで、酸性エッチング液として用いる硫酸及び/又は硝酸の水溶液については、硫酸水溶液の場合にはその酸濃度が1重量%以上60重量%以下、好ましくは5重量%以上50重量%以下であるのがよく、また、硝酸水溶液の場合にはその酸濃度が5重量%以上60重量%以下、好ましくは10重量%以上50重量%以下であるのがよく、更に、硫酸・硝酸混合水溶液の場合には酸濃度が5重量%以上50重量%以下である硫酸水溶液中に酸濃度が5重量%以上30重量%以下である硝酸水溶液を添加するのがよい。酸性エッチング液の酸濃度が上記範囲より低いと反応が十分に進まず溶解量が不十分になる虞があり、反対に、上記範囲より高くなると反応速度が速くなり過ぎて溶解量の制御が困難になる。なお、上記の酸性エッチング液については、溶解量を制御する等の目的のため、必要によりクロム酸、リン酸、酢酸、シュウ酸、アスコルビン酸、安息香酸、酪酸、クエン酸、ぎ酸、乳酸、イソブチル酸、リンゴ酸、プロピオン酸、酒石酸等の硫酸及び硝酸以外の酸を添加してもよい。 Here, the sulfuric acid and / or nitric acid aqueous solution used as the acidic etching solution has an acid concentration of 1% by weight to 60% by weight, preferably 5% by weight to 50% by weight in the case of sulfuric acid aqueous solution. In the case of an aqueous nitric acid solution, the acid concentration should be 5 to 60% by weight, preferably 10 to 50% by weight. It is preferable to add a nitric acid aqueous solution having an acid concentration of 5% by weight to 30% by weight to a sulfuric acid aqueous solution having an acid concentration of 5% by weight to 50% by weight. If the acid concentration of the acidic etching solution is lower than the above range, the reaction may not proceed sufficiently and the dissolution amount may be insufficient. On the other hand, if the acid concentration is higher than the above range, the reaction rate becomes too fast and it is difficult to control the dissolution amount. become. For the above acidic etching solution, for the purpose of controlling the amount of dissolution, chromic acid, phosphoric acid, acetic acid, oxalic acid, ascorbic acid, benzoic acid, butyric acid, citric acid, formic acid, lactic acid, Acids other than sulfuric acid and nitric acid such as isobutyric acid, malic acid, propionic acid, and tartaric acid may be added.
 また、上記の酸性エッチング液を用いたエッチング処理の処理条件については、処理温度が通常20℃以上90℃以下、好ましくは30℃以上80℃以下であって、処理時間が通常1分以上20分以下、好ましくは5分以上15分以下であるのがよい。このエッチング処理の処理条件における処理温度が20℃より低いと反応が十分に進まず溶解量が不十分になる虞があり、反対に、90℃より高くなると反応速度が速くなり過ぎて溶解量の制御が困難になる。同様に、エッチング処理の処理時間が1分より短いと反応が十分に進まず溶解量が不十分になる虞があり、反対に、20分より長くなると生産効率が低下して量産性が悪くなる。 In addition, with respect to the processing conditions of the etching process using the above acidic etching solution, the processing temperature is usually 20 ° C. or higher and 90 ° C. or lower, preferably 30 ° C. or higher and 80 ° C. or lower, and the processing time is usually 1 minute or longer and 20 minutes or shorter. Hereinafter, it is preferably 5 minutes or more and 15 minutes or less. If the processing temperature under the processing conditions of this etching process is lower than 20 ° C., the reaction may not proceed sufficiently and the amount of dissolution may be insufficient. On the other hand, if the processing temperature is higher than 90 ° C., the reaction rate becomes too high and Control becomes difficult. Similarly, if the processing time of the etching process is shorter than 1 minute, the reaction may not proceed sufficiently and the amount of dissolution may be insufficient. On the other hand, if the processing time is longer than 20 minutes, the production efficiency decreases and the mass productivity deteriorates. .
 本発明において、以上のようにして得られたアルミ合金基材の表面にコンタミ等が残渣している場合には、脱脂や表面調整、表面付着物・汚染物等の除去を目的に、このアルミ合金基材のエッチング処理に先駆けて、酸水溶液に浸漬した後にアルカリ水溶液に浸漬する前処理を行うのがよい。この目的で使用される酸水溶液としては、例えば、市販の酸性脱脂剤で調製したもの、硫酸、硝酸、フッ酸、リン酸等の鉱酸や酢酸、クエン酸等の有機酸や、これらの酸を混合して得られた混合酸等の酸試薬を用いて調製したもの等の酸の1~50重量%水溶液が用いるのがよく、また、アルカリ水溶液としては、例えば、市販のアルカリ性脱脂剤により調製したもの、苛性ソーダ等のアルカリ試薬により調製したもの、又はこれらのものを混合して調製したもの等のアルカリの1~50重量%水溶液が用いるのがよく、更に、浸漬時間については、酸水溶液及びアルカリ水溶液のいずれの場合も0.5~10分間程度であるのがよい。 In the present invention, when contaminants or the like remain on the surface of the aluminum alloy substrate obtained as described above, this aluminum is used for the purpose of degreasing, surface adjustment, and removal of surface deposits and contaminants. Prior to the etching treatment of the alloy substrate, it is preferable to perform a pretreatment of immersing in an aqueous alkali solution after immersing in an aqueous acid solution. Examples of the acid aqueous solution used for this purpose include those prepared with commercially available acidic degreasing agents, mineral acids such as sulfuric acid, nitric acid, hydrofluoric acid, and phosphoric acid, organic acids such as acetic acid and citric acid, and these acids. It is preferable to use a 1 to 50% by weight aqueous solution of an acid such as that prepared by using an acid reagent such as a mixed acid obtained by mixing the above, and examples of the alkaline aqueous solution include a commercially available alkaline degreasing agent. It is preferable to use a 1 to 50% by weight aqueous solution of an alkali such as one prepared, one prepared with an alkali reagent such as caustic soda, or one prepared by mixing these materials. In both cases, the alkaline aqueous solution is preferably about 0.5 to 10 minutes.
 本発明により得られたアルミ合金部材は、上記のエッチング処理によって溶解されたMg2Si金属間化合物の跡が凹状部となってこのアルミ合金部材の表面にクロスヘッド型又はエキスパンドメタル型の極微細な凹凸構造の表面処理層を形成し、この表面処理層により樹脂成形体との間に優れたアルミ樹脂接合性を発現する。 In the aluminum alloy member obtained by the present invention, the trace of the Mg 2 Si intermetallic compound dissolved by the above etching treatment becomes a concave portion, and the surface of the aluminum alloy member has a fine crosshead type or expanded metal type. A surface treatment layer having a concavo-convex structure is formed, and this surface treatment layer exhibits excellent aluminum resin bondability with the resin molded body.
 そして、本発明のアルミ合金部材において、アルミ合金部材の表面に観察されるクロスヘッド型又はエキスパンドメタル型の極微細な凹凸構造の表面処理層は、次のようなメカニズムによって形成されるものと推定される。
 すなわち、MgとSiとを含むAl-Mg-Si系アルミニウム合金では、溶体化処理及び時効処理の際の温度条件により、図1に示すように、生成したMg2Si金属間化合物の結晶構造が針状(a)→棒状(b)→板状(c)→ランダムな立方体形状(d)の如く変態する。このランダムな立方体形状(d)の結晶構造はMg2Si金属間化合物の板状(c)結晶が重なり合って形成されるが、クロスヘッド型の極微細な凹凸構造は、このようなランダムな立方体形状(d)の結晶構造を有するMg2Si金属間化合物を析出させ、このMg2Si金属間化合物を硫酸及び/又は硝酸の水溶液で溶解させた場合に発現する。ここで、ランダムな立方体形状(d)の結晶構造を有するMg2Si金属間化合物を析出させるためには、焼き入れを十分に行ない、かつ、時効処理の際の温度を高くするのがよく、反対に、析出させないためには、焼き入れを不十分にし、あるいは時効処理の際の温度を低くするのがよい。また、Al-Mg-Si系アルミニウム合金において、Mnの含有量が多い場合には、MnがAl-Mn-Si系アルミニウム合金を作ってMg2Si金属間化合物の形成が阻害されるので、焼き入れが不十分になる可能性が高くなる。この場合には、時効処理の際の温度を上げても針状(a)→棒状(b)→板状(c)への変態が起こらず、結果としてアルミ-樹脂間の接合性にプラスに寄与するクロスヘッド型の極微細な凹凸構造を発現させることができない。また、エキスパンドメタル型の極微細な凹凸構造の表面処理層は、上記の板状(c)のMg2Si金属間化合物の結晶が重なり合わずに分散した状態のままエッチング処理により溶解した場合に形成されるものと考えられ、また、時効処理の際の温度が高いほどMg2Si金属間化合物の析出量が多くなるので、時効処理の際の温度が高いほどエッチング処理後にエキスパンドメタル型の極微細な凹凸構造が発現し易くなると考えられる。
And in the aluminum alloy member of the present invention, it is estimated that the surface treatment layer of the cross head type or expanded metal type ultra fine uneven structure observed on the surface of the aluminum alloy member is formed by the following mechanism. Is done.
That is, in the Al—Mg—Si based aluminum alloy containing Mg and Si, the crystal structure of the produced Mg 2 Si intermetallic compound depends on the temperature conditions during solution treatment and aging treatment, as shown in FIG. The transformation is as follows: needle shape (a) → rod shape (b) → plate shape (c) → random cubic shape (d). The crystal structure of this random cubic shape (d) is formed by overlapping the plate-like (c) crystals of Mg 2 Si intermetallic compound, but the crosshead type ultra-fine uneven structure is such a random cube precipitating Mg 2 Si intermetallic compound having a crystal structure of the shape (d), expressing the Mg 2 Si intermetallic compound when dissolved in an aqueous solution of sulfuric acid and / or nitric acid. Here, in order to precipitate the Mg 2 Si intermetallic compound having a crystal structure of a random cubic shape (d), it is better to sufficiently quench and increase the temperature during the aging treatment, On the other hand, in order to prevent precipitation, it is preferable to make quenching insufficient or to lower the temperature during the aging treatment. In addition, in the Al-Mg-Si-based aluminum alloy, if the Mn content is large, Mn forms an Al-Mn-Si-based aluminum alloy and the formation of Mg 2 Si intermetallic compound is hindered. There is a high possibility of insufficient insertion. In this case, even if the temperature during the aging treatment is increased, the transformation from needle-like (a) → rod-like (b) → plate-like (c) does not occur, and as a result, the bondability between the aluminum and the resin is positive. It is not possible to develop a contributing crosshead-type extremely fine uneven structure. In addition, the surface treatment layer of the expanded metal type ultra-fine concavo-convex structure is obtained when the above plate-like (c) Mg 2 Si intermetallic compound crystals are dissolved without being overlapped and dissolved by etching treatment. The higher the temperature during the aging treatment, the more the Mg 2 Si intermetallic compound precipitates. Therefore, the higher the temperature during the aging treatment, the larger the expanded metal type electrode after the etching treatment. It is considered that a fine uneven structure is easily developed.
 また、本発明により得られたアルミ合金部材において、アルミ合金部材の表面処理層に観察されるクロスヘッド型凹凸構造の存在比率〔すなわち、走査型電子顕微鏡(日立製FE-SEM、S-4500形)を用いてSEM像(実施例1の場合の図2)を観察し、その結果を実施例1の場合の図3のように画像処理して求められる測定視野0.1mm角における凹状部の面積比率をクロスヘッド型凹凸構造の存在比率として算出〕については、通常20%以上90%以下、好ましくは35%以上80%以下であるのがよい。アルミ合金部材の表面における凹状部の存在比率が20%より低いと凹部に入り込む樹脂量が不十分になり、樹脂接合性に悪影響を及ぼすという問題が生じる虞があり、反対に、90%より高くなると凹部に入り込んだ樹脂を支えるためのアルミ部が極端に少なくなり、結果として樹脂接合性に悪影響を及ぼすという問題が生じる虞が生じる。また,実施例2及び実施例4については、同様の測定方法〔すなわち、走査型電子顕微鏡(日立製FE-SEM、S-4500形)を用いてSEM像(実施例2の場合の図5)を観察し、その結果を実施例2の場合の図8のように画像処理して求められる測定視野0.1mm角における凹状部の面積比率〕によりエキスパンドメタル構造の存在比率を算出した。通常10%以上好ましくは20%以上であると、接合強度及び気密性の向上が得られる。 Further, in the aluminum alloy member obtained by the present invention, the abundance ratio of the crosshead type uneven structure observed in the surface treatment layer of the aluminum alloy member [ie, scanning electron microscope (Hitachi FE-SEM, S-4500 type) ) Is used to observe the SEM image (FIG. 2 in the case of Example 1), and the result is obtained by image processing as shown in FIG. The area ratio is calculated as the existence ratio of the cross-head concavo-convex structure] is usually 20% to 90%, preferably 35% to 80%. If the ratio of the concave portion on the surface of the aluminum alloy member is lower than 20%, the amount of resin entering the concave portion may be insufficient, which may cause a problem of adversely affecting the resin bonding property. Then, the aluminum part for supporting the resin that has entered the recess is extremely reduced, and as a result, there is a possibility that a problem of adversely affecting the resin bondability may occur. Moreover, about Example 2 and Example 4, the same measuring method [Namely, SEM image (FIG. 5 in the case of Example 2) using a scanning electron microscope (Hitachi FE-SEM, S-4500 type)) Then, the presence ratio of the expanded metal structure was calculated from the area ratio of the concave portion in the measurement visual field 0.1 mm square obtained by image processing as shown in FIG. Usually, when it is 10% or more, preferably 20% or more, improvement in bonding strength and airtightness can be obtained.
 本発明の方法により得られたアルミ合金部材は、その表面に形成されたクロスヘッド型又はエキスパンドメタル型の極微細な凹凸構造の表面処理層により、例えばこのアルミ合金部材を射出成形用金型内にセットし、この金型内に溶融した所定の熱可塑性樹脂を射出して固化させる、いわゆるアルミ合金部材を用いた熱可塑性樹脂の射出一体成形により、アルミ合金部材の必要な部分に樹脂成形体を接合してアルミ-樹脂複合体を製造した際に、優れたアルミ樹脂接合性を発揮する。 The aluminum alloy member obtained by the method of the present invention has a surface treatment layer of an extremely fine concavo-convex structure of a crosshead type or an expanded metal type formed on the surface thereof. The resin molded body is formed on the necessary part of the aluminum alloy member by injection molding of a thermoplastic resin using a so-called aluminum alloy member that is injected into a mold and injects a predetermined thermoplastic resin into the mold and solidifies. When an aluminum-resin composite is manufactured by bonding, an excellent aluminum resin bonding property is exhibited.
 ここで、本発明のアルミ合金部材を用いたアルミ-樹脂複合体を製造する際に使用される熱可塑性樹脂としては、各種の熱可塑性樹脂を単独で用いることができるが、本発明のアルミ合金部材を用いて製造されるアルミ-樹脂複合体に求められる物性、用途、使用環境等を考慮すると、熱可塑性樹脂としては、好ましくは、例えばポリプロピレン樹脂、ポリエチレン樹脂、アクリロニトリル・ブタジエン・スチレン共重合体(ABS)、ポリカーボネート樹脂(PC)、ポリアミド樹脂(PA)、ポリフェニレンスルフィド(PPS)等のポリアリーレンサルファイド樹脂、ポリアセタール樹脂、液晶性樹脂、ポリエチレンテレフタレート(PET)やポリブチレンテレフタレート(PBT)等のポリエステル系樹脂、ポリオキシメチレン樹脂、ポリイミド樹脂、シンジオタクティックポリスチレン樹脂等やこれらの熱可塑性樹脂の2種以上の混合物が挙げられ、また、アルミ形状体と樹脂成形体との間の密着性、機械的強度、耐熱性、寸法安定性(耐変形、反り等)、電気的性質等の性能をより改善するために、より好ましくは、これらの熱可塑性樹脂に繊維状、粉粒状、板状等の充填剤や、各種のエラストマー成分を添加するのがよい。 Here, as the thermoplastic resin used in producing the aluminum-resin composite using the aluminum alloy member of the present invention, various thermoplastic resins can be used alone, but the aluminum alloy of the present invention is used. Considering the physical properties required for the aluminum-resin composite produced using the members, applications, usage environment, etc., the thermoplastic resin is preferably a polypropylene resin, a polyethylene resin, an acrylonitrile-butadiene-styrene copolymer, for example. (ABS), polycarbonate resin (PC), polyamide resin (PA), polyarylene sulfide resin such as polyphenylene sulfide (PPS), polyacetal resin, liquid crystalline resin, polyester such as polyethylene terephthalate (PET) and polybutylene terephthalate (PBT) Resin, polyoxymethylene resin, polyimide resin, Examples include syndiotactic polystyrene resin and a mixture of two or more of these thermoplastic resins, and adhesion between an aluminum shaped body and a resin molded body, mechanical strength, heat resistance, dimensional stability (resistance resistance) In order to further improve performance such as deformation, warpage, and electrical properties, it is preferable to add fillers such as fibrous, granular, and plate-like materials and various elastomer components to these thermoplastic resins. It is good.
 また、熱可塑性樹脂に添加される充填剤としては、ガラス繊維、カーボン繊維、金属繊維、アスベスト繊維、硼素繊維等の無機質繊維充填剤や、ポリアミド、フッ素樹脂、アクリル樹脂等の高融点有機質繊維充填剤や、石英粉末、ガラスビーズ、ガラス粉、炭酸カルシウムを始めとする無機粉体類等の粉状充填剤や、ガラスフレーク、タルクやマイカ等の珪酸塩類等の板状充填剤等が例示され、熱可塑性樹脂100重量部に対して250重量部以下、好ましくは20重量部以上220重量部以下、より好ましくは30重量部以上100重量部以下の範囲で添加される。この充填剤の添加量が250重量部を超えると、流動性が低下しアルミ形状体の凹部へ進入し難くなり良好な密着強度を得られなかったり、機械的特性の低下を招くという問題が生じる。 Fillers added to thermoplastic resins include inorganic fiber fillers such as glass fibers, carbon fibers, metal fibers, asbestos fibers and boron fibers, and high melting point organic fibers such as polyamides, fluororesins and acrylic resins. And powder fillers such as silica powder, glass beads, glass powder, inorganic powders such as calcium carbonate, and plate fillers such as glass flakes, silicates such as talc and mica, etc. In addition, it is added in an amount of 250 parts by weight or less, preferably 20 parts by weight or more and 220 parts by weight or less, more preferably 30 parts by weight or more and 100 parts by weight or less with respect to 100 parts by weight of the thermoplastic resin. When the added amount of the filler exceeds 250 parts by weight, there is a problem that the fluidity is lowered and it is difficult to enter the concave portion of the aluminum shaped body, and good adhesion strength cannot be obtained or the mechanical properties are deteriorated. .
 また、熱可塑性樹脂に添加されるエラストマー成分としては、ウレタン系、コアシェル型、オレフィン系、ポリエステル系、アミド系、スチレン系等のエラストマーが例示され、射出成形時の熱可塑性樹脂の溶融温度等を考慮して選択され、また、熱可塑性樹脂100重量部に対して30重量部以下、好ましくは3~25重量部の範囲で使用される。このエラストマー成分の添加量が30重量部を超えると、更なる密着強度向上効果が見られず機械的特性の低下等の問題が生じる。このエラストマー成分の配合効果は、熱可塑性樹脂としてポリエステル系樹脂を用いた場合に特に顕著に現れる。 Examples of the elastomer component added to the thermoplastic resin include urethane type, core shell type, olefin type, polyester type, amide type, and styrene type elastomers. The melting temperature of the thermoplastic resin at the time of injection molding, etc. In addition, it is selected in consideration of 30 parts by weight or less, preferably 3 to 25 parts by weight based on 100 parts by weight of the thermoplastic resin. When the added amount of the elastomer component exceeds 30 parts by weight, a further effect of improving the adhesion strength is not seen, and problems such as a decrease in mechanical properties occur. This blending effect of the elastomer component is particularly prominent when a polyester resin is used as the thermoplastic resin.
 更に、本発明のアルミ-樹脂複合体を製造するための熱可塑性樹脂には、一般に熱可塑性樹脂に添加される公知の添加剤、すなわち難燃剤、染料や顔料等の着色剤、酸化防止剤や紫外線吸収剤等の安定剤、可塑剤、潤滑剤、滑剤、離型剤、結晶化促進剤、結晶核剤等を、要求される性能に応じて適宜添加することができる。 Further, the thermoplastic resin for producing the aluminum-resin composite of the present invention includes known additives generally added to thermoplastic resins, that is, flame retardants, colorants such as dyes and pigments, antioxidants, Stabilizers such as ultraviolet absorbers, plasticizers, lubricants, lubricants, mold release agents, crystallization accelerators, crystal nucleating agents, and the like can be appropriately added according to the required performance.
 本発明において、アルミ合金部材を射出成形用金型内にセットして行う熱可塑性樹脂の射出成形については、用いられる熱可塑性樹脂に求められる成形条件を採用し得るものであるが、射出成形時に溶融した熱可塑性樹脂がアルミ合金部材の凹状部内に確実に進入して固化することが重要であり、金型温度やシリンダー温度を熱可塑性樹脂の種類や物性、更には成形サイクルの許す範囲で比較的高めに設定するのが好ましく、特に金型温度については、下限温度を90℃以上、好ましくは130℃以上にする必要があるが、上限は、使用する熱可塑性樹脂の種類に応じて、100℃から当該熱可塑性樹脂の融点又は軟化点(エラストマー成分が添加される場合にはどちらか高い方の融点又は軟化点)より20℃程度低い温度までの範囲であるのがよい。また、下限金型温度は、熱可塑性樹脂の融点から140℃以上低くならないように設定するのが好ましい。 In the present invention, for the injection molding of the thermoplastic resin performed by setting the aluminum alloy member in the injection mold, molding conditions required for the thermoplastic resin to be used can be adopted. It is important that the molten thermoplastic resin surely enters and solidifies into the concave part of the aluminum alloy member, and the mold temperature and cylinder temperature are compared within the range that the type and physical properties of the thermoplastic resin and the molding cycle allow. The lower limit temperature must be 90 ° C. or higher, preferably 130 ° C. or higher, especially for the mold temperature, but the upper limit is 100 depending on the type of thermoplastic resin used. The temperature ranges from ℃ to a temperature about 20 ℃ lower than the melting point or softening point of the thermoplastic resin (if the elastomer component is added, the higher melting point or softening point). Good it is. Further, the lower limit mold temperature is preferably set so as not to be lowered by 140 ° C. or more from the melting point of the thermoplastic resin.
 なお、本発明のアルミ合金部材を用いて行われるアルミ-樹脂複合体の製造方法については、上記の熱可塑性樹脂の射出一体成形法に限らず、熱圧着法を採用してもよい。すなわち、先ず、使用する熱可塑性樹脂の溶融温度に応じてアルミ合金部材を90~300℃程度の温度に加熱し、その表面に熱可塑性樹脂性の樹脂成形体を加圧下に押し当て、この樹脂成形体の表面の一部を溶融させてアルミ合金部材表面の凹状部内に侵入させ、更に加圧下に冷却することにより所望のアルミ-樹脂複合体を製造する。 Note that the aluminum-resin composite manufacturing method performed using the aluminum alloy member of the present invention is not limited to the above-described thermoplastic resin injection integral molding method, and a thermocompression bonding method may be employed. That is, first, an aluminum alloy member is heated to a temperature of about 90 to 300 ° C. in accordance with the melting temperature of the thermoplastic resin to be used, and a thermoplastic resin molding is pressed against the surface of the aluminum alloy member under pressure. A desired aluminum-resin composite is produced by melting a part of the surface of the molded body to enter the concave portion of the surface of the aluminum alloy member, and further cooling under pressure.
 本発明によれば、Al-Mg-Si系アルミニウム合金からなるアルミ合金部材の表面に樹脂成形体を接合することにより、アルミ-樹脂間において優れた密着性及び気密性を保持すると共にAl-Mg-Si系アルミニウム合金本来の優れた耐久性、押出加工性、及び機械的特性を有するアルミ-樹脂複合体を製造するのに好適な樹脂接合用Al-Mg-Si系アルミ合金部材を製造することができる。しかも、製造されたアルミ-樹脂複合体は、優れた密着性及び気密性を有するものであるから、例えば自動車用部品、家電機器用部品、産業機器用部品等を始めとする過酷な環境下に曝される機会のある種々の用途に適している。 According to the present invention, a resin molded body is bonded to the surface of an aluminum alloy member made of an Al-Mg-Si-based aluminum alloy, thereby maintaining excellent adhesion and airtightness between the aluminum and the resin, and Al-Mg -Manufacturing Al-Mg-Si-based aluminum alloy members for resin bonding suitable for manufacturing aluminum-resin composites having the inherent durability, extrudability, and mechanical properties of Si-based aluminum alloys Can do. Moreover, since the produced aluminum-resin composite has excellent adhesion and airtightness, it can be used in harsh environments such as automobile parts, home appliance parts, industrial equipment parts and the like. Suitable for various applications where there is an opportunity to be exposed.
図1は、本発明方法において、クロスヘッド型又はエキスパンドメタル型の極微細な凹凸構造の表面処理層が形成されるメカニズム(推定)を説明するための説明図である。FIG. 1 is an explanatory diagram for explaining a mechanism (estimation) for forming a surface treatment layer having an extremely fine uneven structure of a crosshead type or an expanded metal type in the method of the present invention.
図2は、本発明の実施例1で得られたアルミ合金部材の表面を走査型電子顕微鏡で観察した際に得られたSEM画像を示す写真である。FIG. 2 is a photograph showing an SEM image obtained when the surface of the aluminum alloy member obtained in Example 1 of the present invention was observed with a scanning electron microscope.
図3は、図2のSEM画像の画像処理後の処理画像を示す写真である。FIG. 3 is a photograph showing a processed image after the image processing of the SEM image of FIG.
図4は、実施例1で得られたアルミ-樹脂複合体のアルミ完全除去後の樹脂側表面形状を走査型電子顕微鏡で観察した際に得られたSEM画像を示す写真である。FIG. 4 is a photograph showing an SEM image obtained when the resin-side surface shape of the aluminum-resin composite obtained in Example 1 after complete aluminum removal was observed with a scanning electron microscope.
図5は、本発明の実施例2で得られた図2と同様のアルミ合金部材表面のSEM画像を示す写真である。FIG. 5 is a photograph showing an SEM image of the same aluminum alloy member surface as in FIG. 2 obtained in Example 2 of the present invention.
図6は、図5の一部を拡大したSEM画像を示す写真である。FIG. 6 is a photograph showing an SEM image in which a part of FIG. 5 is enlarged.
図7は、図5のSEM画像の画像処理後の処理画像を示す図3と同様の写真である。FIG. 7 is a photograph similar to FIG. 3 showing the processed image after the image processing of the SEM image of FIG.
図8は、図5のSEM画像おけるエキスパンドメタル構造部のみを画像処理により抽出した画像処理後の処理画像を示す写真である。FIG. 8 is a photograph showing a processed image after image processing in which only the expanded metal structure portion in the SEM image of FIG. 5 is extracted by image processing.
図9は、実施例2で得られた図4と同様の樹脂側表面形状のSEM画像を示す写真である。FIG. 9 is a photograph showing an SEM image of the resin-side surface shape similar to that of FIG. 4 obtained in Example 2.
図10は、本発明の実施例3で得られた図2と同様のアルミ合金部材表面のSEM画像を示す写真である。FIG. 10 is a photograph showing an SEM image of the same aluminum alloy member surface as in FIG. 2 obtained in Example 3 of the present invention.
図11は、図10のSEM画像の画像処理後の処理画像を示す図3と同様の写真である。FIG. 11 is a photograph similar to FIG. 3 showing a processed image after image processing of the SEM image of FIG.
図12は、実施例3で得られた図4と同様の樹脂側表面形状のSEM画像を示す写真である。FIG. 12 is a photograph showing an SEM image of the resin-side surface shape similar to FIG. 4 obtained in Example 3.
図13は、本発明の実施例4で得られた図2と同様のアルミ合金部材表面のSEM画像を示す写真である。FIG. 13 is a photograph showing an SEM image of the same aluminum alloy member surface as in FIG. 2 obtained in Example 4 of the present invention.
図14は、図13の一部を拡大したSEM画像を示す写真である。FIG. 14 is a photograph showing an SEM image in which a part of FIG. 13 is enlarged.
図15は、図13のSEM画像の画像処理後の処理画像を示す図3と同様の写真である。FIG. 15 is a photograph similar to FIG. 3 showing the processed image after the image processing of the SEM image of FIG.
図16は、図13のSEM画像におけるエキスパンドメタル構造部のみを画像処理により抽出した画像処理後の処理画像を示す図8と同様の写真である。FIG. 16 is a photograph similar to FIG. 8 showing a processed image after image processing in which only the expanded metal structure in the SEM image of FIG. 13 is extracted by image processing.
図17は、実施例4で得られた図4と同様の樹脂側表面形状のSEM画像を示す写真である。FIG. 17 is a photograph showing an SEM image of the resin-side surface shape similar to FIG. 4 obtained in Example 4.
図18は、本発明の実施例5で得られた図2と同様のアルミ合金部材表面のSEM画像を示す写真である。FIG. 18 is a photograph showing an SEM image of the same aluminum alloy member surface as in FIG. 2 obtained in Example 5 of the present invention.
図19は、図18のSEM画像の画像処理後の処理画像を示す図3と同様の写真である。FIG. 19 is a photograph similar to FIG. 3 showing the processed image after the image processing of the SEM image of FIG.
図20は、実施例5で得られた図4と同様の樹脂側表面形状のSEM画像を示す写真である。20 is a photograph showing an SEM image of the resin-side surface shape similar to that of FIG. 4 obtained in Example 5. FIG.
図21は、本発明の実施例6で得られた図2と同様のアルミ合金部材表面のSEM画像を示す写真である。FIG. 21 is a photograph showing an SEM image of the same aluminum alloy member surface as in FIG. 2 obtained in Example 6 of the present invention.
図22は、図21のSEM画像の画像処理後の処理画像を示す図3と同様の写真である。22 is a photograph similar to FIG. 3 showing a processed image after the image processing of the SEM image of FIG.
図23は、実施例6で得られた図4と同様の樹脂側表面形状のSEM画像を示す写真である。FIG. 23 is a photograph showing an SEM image of the resin-side surface shape similar to FIG. 4 obtained in Example 6.
図24は、本発明の比較例1で得られた図2と同様のアルミ合金部材表面のSEM画像を示す写真である。FIG. 24 is a photograph showing an SEM image of the same aluminum alloy member surface as in FIG. 2 obtained in Comparative Example 1 of the present invention.
図25は、図24のSEM画像の画像処理後の処理画像を示す図3と同様の写真である。25 is a photograph similar to FIG. 3 showing a processed image after the image processing of the SEM image of FIG.
図26は、比較例1で得られた図4と同様の樹脂側表面形状のSEM画像を示す写真である。FIG. 26 is a photograph showing an SEM image of the resin-side surface shape similar to that of FIG. 4 obtained in Comparative Example 1.
図27は、本発明の比較例2で得られた図2と同様のアルミ合金部材表面のSEM画像を示す写真である。FIG. 27 is a photograph showing an SEM image of the same aluminum alloy member surface as in FIG. 2 obtained in Comparative Example 2 of the present invention.
図28は、図27のSEM画像の画像処理後の処理画像を示す図3と同様の写真である。FIG. 28 is a photograph similar to FIG. 3 showing the processed image after the image processing of the SEM image of FIG.
図29は、比較例2で得られた図4と同様の樹脂側表面形状のSEM画像を示す写真である。29 is a photograph showing an SEM image of the resin-side surface shape similar to that of FIG. 4 obtained in Comparative Example 2. FIG.
図30は、各実施例及び各比較例で得られたアルミ合金部材を用いて作製されたせん断破壊荷重測定試験用のアルミ樹脂試験片(アルミ-樹脂複合体)を示す説明図である。FIG. 30 is an explanatory view showing an aluminum resin test piece (aluminum-resin composite) for a shear fracture load measurement test produced using the aluminum alloy member obtained in each example and each comparative example.
図31は、せん断破壊荷重測定試験機の試験片固定用冶具にアルミ樹脂試験片を固定し、せん断破壊荷重を測定する際の様子を説明するための説明図である。FIG. 31 is an explanatory diagram for explaining a state in which an aluminum resin test piece is fixed to a test piece fixing jig of a shear fracture load measurement tester and a shear fracture load is measured.
 以下、本発明の実施例及び比較例に基づいて、本発明の実施の形態を具体的に説明する。 Hereinafter, embodiments of the present invention will be described in detail based on examples and comparative examples of the present invention.
〔実施例1〕
 1.アルミ合金基材の調製
 Si:0.21質量%、Mg:0.42質量%、及びMn:0.01質量%を含むAl-Mg-Si系アルミニウム合金を鋳造炉で鋳造した後、押出加工を行い、2050mm×800mm×3mmの大きさのフラットバー(アルミ合金基材)を成形した。
[Example 1]
1. Preparation of aluminum alloy base material After casting an Al-Mg-Si based aluminum alloy containing Si: 0.21% by mass, Mg: 0.42% by mass, and Mn: 0.01% by mass in a casting furnace, extrusion processing Then, a flat bar (aluminum alloy base material) having a size of 2050 mm × 800 mm × 3 mm was formed.
 2.アルミ合金部材の調製
 上で得られたフラットバーについて、520℃及び1時間の条件で溶体化処理を施した後、大気雰囲気下で室温まで自然放冷し、次いで190℃及び3時間の条件で時効処理を実施した。また、得られた溶体化処理及び時効処理後(熱処理後)のフラットバーから、大きさ40mm×40mm×3mmの熱処理後アルミ合金基材を切り出した。
2. Preparation of aluminum alloy member The flat bar obtained above was subjected to solution treatment under conditions of 520 ° C. and 1 hour, then allowed to naturally cool to room temperature in an air atmosphere, and then at 190 ° C. and 3 hours. An aging treatment was performed. Further, from the obtained flat bar after the solution treatment and aging treatment (after heat treatment), a post-heat treatment aluminum alloy substrate having a size of 40 mm × 40 mm × 3 mm was cut out.
 上で得られた熱処理後アルミ合金基材について、30wt%-硝酸水溶液に常温で1分間浸漬した後にイオン交換水で十分に水洗し、次いで5wt%-水酸化ナトリウム水溶液に50℃で1分間浸漬した後に水洗し、更に、30wt%-硝酸水溶液に常温で1分間浸漬した後に水洗する前処理を施した。 The heat-treated aluminum alloy base material obtained above was immersed in 30 wt% nitric acid aqueous solution at room temperature for 1 minute, then thoroughly washed with ion-exchanged water, and then immersed in 5 wt% sodium hydroxide aqueous solution at 50 ° C for 1 minute. Then, it was washed with water and further pretreated by immersing it in a 30 wt% nitric acid aqueous solution at room temperature for 1 minute and then washing with water.
 次に、この前処理を施した熱処理後アルミ合金基材について、10wt%-硫酸水溶液中に30℃で10分間浸漬した後に水洗するエッチング処理を施し、次いで水洗した後に、80℃の熱風で5分間乾燥させ、実施例1のアルミ合金部材を作製した。 Next, the pre-treated aluminum alloy base material after the heat treatment was subjected to an etching treatment in which it was immersed in a 10 wt% -sulfuric acid aqueous solution at 30 ° C. for 10 minutes and then washed with water. The aluminum alloy member of Example 1 was produced by drying for a minute.
 このようにして得られた実施例1のアルミ合金部材について、その表面を走査型電子顕微鏡(日立製FE-SEM、S-4500形)で観察し、その後、画像処理を行って長さ0.1~10.0μmの大きさを有する凹状部について、その存在比率(面積比率)を算出した。また、X線回析装置(リガク製 RAD-rR)を用い、得られたアルミ合金基材の表面に内在する金属間化合物の積分回析強度値を測定し、その結果からアルミ合金基材中のMg2Si金属間化合物の割合を求めた。この時に得られたアルミ合金部材表面のSEM画像を図2に、また、その画像処理後の処理画像を図3にそれぞれ示すと共に、結果を表1に示す。 The surface of the aluminum alloy member of Example 1 obtained in this way was observed with a scanning electron microscope (Hitachi FE-SEM, model S-4500), and thereafter image processing was performed to obtain a length of 0. The existence ratio (area ratio) of the concave portion having a size of 1 to 10.0 μm was calculated. In addition, using an X-ray diffraction apparatus (Rigaku RAD-rR), the integrated diffraction strength value of the intermetallic compound existing on the surface of the obtained aluminum alloy base material was measured, and the result showed that The ratio of Mg 2 Si intermetallic compound was determined. FIG. 2 shows the SEM image of the surface of the aluminum alloy member obtained at this time, FIG. 3 shows the processed image after the image processing, and Table 1 shows the result.
 3.アルミ-樹脂複合体の調製
 以上のようにして得られた実施例1のアルミ合金部材を射出成形機(NISSEI社製ST10R2V)の金型内にセットし、熱可塑性樹脂として、充填剤を含むポリフェニレンスルフィド樹脂(ポリプラスチックス社製PPS、グレード名1140A6)を用い、射出時間(保圧時間を含む)5秒、射出速度60mm/秒、保圧力90MPa、成形温度310℃、及び金型温度180℃の成形条件で射出成形し、図30に示すように、40mm×40mm×3mmの大きさのアルミ合金部材1の表面に、長辺長さ40mm×短辺長さ10mm×高さ5mmの大きさの樹脂成形体2が40mm×10mm×5mmの面積で一体的に接合された実施例1のアルミ-樹脂複合体を調製した。この実施例1のアルミ-樹脂複合体については、樹脂側表面観察用とせん断破壊荷重測定試験用のために2つ作製した。
3. Preparation of aluminum-resin composite The aluminum alloy member of Example 1 obtained as described above was set in a mold of an injection molding machine (ST10R2V manufactured by NISSEI), and polyphenylene containing a filler as a thermoplastic resin. Using sulfide resin (PPS manufactured by Polyplastics Co., Ltd., grade name 1140A6), injection time (including pressure holding time) 5 seconds, injection speed 60 mm / second, pressure holding pressure 90 MPa, molding temperature 310 ° C., mold temperature 180 ° C. As shown in FIG. 30, the surface of the aluminum alloy member 1 having a size of 40 mm × 40 mm × 3 mm has a size of 40 mm long side × 10 mm short side × 5 mm height. An aluminum-resin composite of Example 1 was prepared in which the resin molded body 2 was integrally bonded with an area of 40 mm × 10 mm × 5 mm. Two aluminum-resin composites of Example 1 were prepared for the resin side surface observation and for the shear fracture load measurement test.
 4.アルミ-樹脂複合体の樹脂側表面の観察
 実施例1で得られたアルミ-樹脂複合体を10wt%-水酸化ナトリウム水溶液に80℃で10時間浸漬し、アルミ-樹脂複合体のアルミ側を完全に除去し、樹脂側表面観察用の試験体を作製し、得られた試験体の表面を走査型電子顕微鏡(日立製FE-SEM、S-4500形)で観察し、アルミ-樹脂複合体におけるアルミ-樹脂接合界面における樹脂成形体側表面の形状を調べ、クロスヘッド型又はエキスパンドメタル型の凹凸構造の存在比率を調べた。この時に得られた樹脂成形体表面のSEM画像を図4に示すと共に、結果を表1に示す。
4). Observation of the resin-side surface of the aluminum-resin composite The aluminum-resin composite obtained in Example 1 was immersed in a 10 wt% -sodium hydroxide aqueous solution at 80 ° C. for 10 hours to completely cover the aluminum side of the aluminum-resin composite. The surface of the obtained specimen is observed with a scanning electron microscope (Hitachi FE-SEM, S-4500 type), and an aluminum-resin composite is obtained. The shape of the surface of the resin molded body side at the aluminum-resin bonding interface was examined, and the existence ratio of the concavo-convex structure of the crosshead type or the expanded metal type was examined. The SEM image of the resin molded body surface obtained at this time is shown in FIG. 4 and the results are shown in Table 1.
 5.剪断破壊荷重測定試験
 次に、剪断強度測定試験機(島津製作所製:100kNオートグラフ)を用い、図31に示すように、その試験片固定用治具3に上記のせん断破壊加重測定試験用のアルミ樹脂試験片を図示外のボルトで固定し、接合部から0.1mm離れた位置で樹脂成形体2上に押しジグ4を当て、この押しジグ4により樹脂成形体2に剪断荷重を加え、アルミ部材試験片1と樹脂成形体2との間の接合部の剥離状態(剪断強度)を調べた。この時の剥離形態について、樹脂成形体2の樹脂がアルミ部材試験片1側に接合面積の70%以上の割合で残る「凝集破壊」である場合を最良好(◎)とし、また、樹脂がアルミ部材試験片1側に一部でも残る「凝集破壊」である場合を良好(○)とし、更に、樹脂がアルミ部材試験片1側に残らずに剥離が接合界面で発生した場合を不良(×)として評価した。結果は最良好(◎)であった。
 結果を表1に示す。
5. Next, using a shear strength measurement tester (manufactured by Shimadzu Corporation: 100 kN autograph), as shown in FIG. An aluminum resin test piece is fixed with a bolt (not shown), a pressing jig 4 is applied on the resin molded body 2 at a position 0.1 mm away from the joint, and a shear load is applied to the resin molded body 2 by the pressing jig 4. The peeled state (shear strength) of the joint between the aluminum member test piece 1 and the resin molded body 2 was examined. As for the peeling form at this time, the case where the resin of the resin molded body 2 is “cohesive failure” remaining at a ratio of 70% or more of the bonding area on the aluminum member test piece 1 side is the best ((). The case of “cohesive failure” that remains even partially on the aluminum member test piece 1 side is judged as good (◯), and the case where the resin does not remain on the aluminum member test piece 1 side and peeling occurs at the joining interface is defective ( X). The result was the best (◎).
The results are shown in Table 1.
〔実施例2~5及び比較例1、2〕
 Mg、Si、及びMnについて表1に示す組成を有するAl-Mg-Si系アルミニウム合金を鋳造炉で鋳造した後、実施例1と同様にしてフラットバー(アルミ合金基材)を成形し、次いで表1に示す条件で溶体化処理、時効処理、及び硫酸水溶液でのエッチング処理を施した以外は、実施例1と同様にして実施例2~6及び比較例1、2の各アルミ合金部材を調製した。
[Examples 2 to 5 and Comparative Examples 1 and 2]
After casting an Al—Mg—Si based aluminum alloy having the composition shown in Table 1 for Mg, Si, and Mn in a casting furnace, a flat bar (aluminum alloy substrate) was formed in the same manner as in Example 1, and then The aluminum alloy members of Examples 2 to 6 and Comparative Examples 1 and 2 were prepared in the same manner as in Example 1 except that solution treatment, aging treatment, and etching treatment with an aqueous sulfuric acid solution were performed under the conditions shown in Table 1. Prepared.
〔実施例6〕
 実施例1と同様にして得られた熱処理後アルミ合金基材について、実施例1と同様の前処理を行った後、10wt%-硝酸水溶液中に30℃で10分間浸漬した後に水洗するエッチング処理を施し、次いで水洗した後に、80℃の熱風で5分間乾燥させ、アルミ合金部材を作製した。
Example 6
The post-heat treatment aluminum alloy base material obtained in the same manner as in Example 1 is subjected to the same pretreatment as in Example 1, and then immersed in a 10 wt% nitric acid aqueous solution at 30 ° C. for 10 minutes and then washed with water. And then washed with water and dried with hot air at 80 ° C. for 5 minutes to produce an aluminum alloy member.
 このようにして調製された各実施例2~6及び比較例1、2のアルミ合金部材について、上記実施例1と同様にして、凹状部の存在比率とクロスヘッド型又はエキスパンドメタル型の凹凸構造の有無を調べると共に、アルミ部材試験片1と樹脂成形体2との間の接合部の剥離状態(剪断強度)を調べて評価した。
 結果を表1に示す。
For the aluminum alloy members of Examples 2 to 6 and Comparative Examples 1 and 2 prepared in this manner, the presence ratio of the concave portions and the concavo-convex structure of the crosshead type or the expanded metal type are the same as in Example 1 above. And the peeling state (shear strength) of the joint between the aluminum member test piece 1 and the resin molded body 2 was examined and evaluated.
The results are shown in Table 1.
Figure JPOXMLDOC01-appb-T000001
Figure JPOXMLDOC01-appb-T000001
 また、実施例2で得られたアルミ合金部材表面のSEM画像を図5に、その一部を拡大した画像を図6に、その画像処理後の処理画像を図7に、図5のSEM画像におけるエキスパンドメタル構造部のみを画像処理により抽出した処理画像を図8に、また、樹脂成形体表面のSEM画像を図9にそれぞれ示す。
 実施例3で得られたアルミ合金部材表面のSEM画像を図10に、その画像処理後の処理画像を図11に、また、樹脂成形体表面のSEM画像を図12にそれぞれ示す。
Further, FIG. 5 shows an SEM image of the surface of the aluminum alloy member obtained in Example 2, FIG. 6 shows an enlarged image of the SEM image, FIG. 7 shows a processed image after the image processing, and FIG. FIG. 8 shows a processed image obtained by extracting only the expanded metal structure portion in FIG. 8, and FIG. 9 shows an SEM image of the surface of the resin molded body.
FIG. 10 shows the SEM image of the surface of the aluminum alloy member obtained in Example 3, FIG. 11 shows the processed image after the image processing, and FIG. 12 shows the SEM image of the surface of the resin molded body.
 実施例4で得られたアルミ合金部材表面のSEM画像を図13に、その一部を拡大した画像を図14に、その画像処理後の処理画像を図15に、図13のSEM画像におけるエキスパンドメタル構造部のみを画像処理により抽出した処理画像を図16に、また、樹脂成形体表面のSEM画像を図17にそれぞれ示す。
 実施例5で得られたアルミ合金部材表面のSEM画像を図18に、その画像処理後の処理画像を図19に、また、樹脂成形体表面のSEM画像を図20にそれぞれ示す。
FIG. 13 shows an SEM image of the surface of the aluminum alloy member obtained in Example 4, FIG. 14 shows an enlarged image of the SEM image, FIG. 15 shows a processed image after the image processing, and an expanded view in the SEM image of FIG. FIG. 16 shows a processed image obtained by extracting only the metal structure portion by image processing, and FIG. 17 shows an SEM image of the surface of the resin molded body.
FIG. 18 shows the SEM image of the surface of the aluminum alloy member obtained in Example 5, FIG. 19 shows the processed image after the image processing, and FIG. 20 shows the SEM image of the surface of the resin molded body.
 実施例6で得られたアルミ合金部材表面のSEM画像を図21に、その画像処理後の処理画像を図22に、また、樹脂成形体表面のSEM画像を図23にそれぞれ示す。 FIG. 21 shows an SEM image of the surface of the aluminum alloy member obtained in Example 6, FIG. 22 shows a processed image after the image processing, and FIG. 23 shows an SEM image of the surface of the resin molded body.
 そして、比較例1で得られたアルミ合金部材表面のSEM画像を図24に、その画像処理後の処理画像を図25に、また、樹脂成形体表面のSEM画像を図26にそれぞれ示す。
 また、比較例2で得られたアルミ合金部材表面のSEM画像を図27に、その画像処理後の処理画像を図28に、また、樹脂成形体表面のSEM画像を図29にそれぞれ示す。
24 shows the SEM image of the surface of the aluminum alloy member obtained in Comparative Example 1, FIG. 25 shows the processed image after the image processing, and FIG. 26 shows the SEM image of the surface of the resin molded body.
Moreover, the SEM image of the aluminum alloy member surface obtained in Comparative Example 2 is shown in FIG. 27, the processed image after the image processing is shown in FIG. 28, and the SEM image of the resin molded body surface is shown in FIG.

Claims (6)

  1.  Mnの含有量が0.05質量%未満であるAl-Mg-Si系アルミニウム合金からなるアルミ合金基材を500~600℃及び1~20時間の条件で溶体化処理し、次いで冷却した後に150~300℃及び1~20時間の条件で時効処理を行った後、硫酸及び/又は硝酸の水溶液からなる酸性エッチング液によるエッチング処理を施し、前記アルミ合金基材の表面に表面処理層を付与することを特徴とする樹脂接合用Al-Mg-Si系アルミ合金部材の製造方法。 An aluminum alloy base material made of an Al—Mg—Si based aluminum alloy having a Mn content of less than 0.05% by mass is subjected to a solution treatment under conditions of 500 to 600 ° C. and 1 to 20 hours, and then cooled to 150%. After performing an aging treatment under conditions of ˜300 ° C. and 1˜20 hours, an etching treatment with an acidic etchant composed of an aqueous solution of sulfuric acid and / or nitric acid is performed to provide a surface treatment layer on the surface of the aluminum alloy substrate. A method for producing an Al—Mg—Si based aluminum alloy member for resin bonding, characterized in that:
  2.  前記時効処理の処理温度が200~300℃である請求項1に記載の樹脂接合用Al-Mg-Si系アルミ合金部材の製造方法。 The method for producing an Al-Mg-Si-based aluminum alloy member for resin bonding according to claim 1, wherein the aging treatment temperature is 200 to 300 ° C.
  3.  Al-Mg-Si系アルミニウム合金が、Mgを0.2~4.0質量%の範囲で含有すると共に、Siを0.1~2.5質量%の範囲で含有する請求項1又は2に記載の樹脂接合用Al-Mg-Si系アルミ合金部材の製造方法。 The Al-Mg-Si-based aluminum alloy contains Mg in a range of 0.2 to 4.0% by mass and Si in a range of 0.1 to 2.5% by mass. The manufacturing method of the Al-Mg-Si type aluminum alloy member for resin joining as described.
  4.  時効処理終了後エッチング処理に先駆けて、酸水溶液に浸漬した後にアルカリ水溶液に浸漬する前処理を施す請求項1~3のいずれかに記載の樹脂接合用Al-Mg-Si系アルミ合金部材の製造方法。 The production of an Al-Mg-Si based aluminum alloy member for resin bonding according to any one of claims 1 to 3, wherein after the aging treatment, prior to the etching treatment, a pretreatment of immersing in an aqueous alkaline solution and then in an alkaline aqueous solution is performed. Method.
  5.  エッチング処理の処理条件が、20~90℃及び処理時間1~20分である請求項1~4の何れかに記載の樹脂接合用Al-Mg-Si系アルミ合金部材の製造方法。 The method for producing an Al-Mg-Si aluminum alloy member for resin bonding according to any one of claims 1 to 4, wherein the processing conditions of the etching process are 20 to 90 ° C and a processing time of 1 to 20 minutes.
  6.  請求項1~5に記載のいずれかの方法によって得られ、表面にクロスヘッド型又はエキスパンドメタル型の極微細な凹凸構造の表面処理層を有することを特徴とする樹脂接合用Al-Mg-Si系アルミ合金部材。 An Al-Mg-Si for resin bonding, which is obtained by the method according to any one of claims 1 to 5 and has a surface treatment layer having an extremely fine concavo-convex structure of a crosshead type or an expanded metal type on the surface. Aluminum alloy members.
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