TW201035330A - Aluminum alloy member with excellent jointability to resin, and production method thereof - Google Patents

Aluminum alloy member with excellent jointability to resin, and production method thereof Download PDF

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TW201035330A
TW201035330A TW98145276A TW98145276A TW201035330A TW 201035330 A TW201035330 A TW 201035330A TW 98145276 A TW98145276 A TW 98145276A TW 98145276 A TW98145276 A TW 98145276A TW 201035330 A TW201035330 A TW 201035330A
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Taiwan
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alloy
resin
less
eutectic
aluminum
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TW98145276A
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Chinese (zh)
Inventor
Hiroshi Horikawa
Masanori Endo
Masaki Iino
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Nippon Light Metal Co
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Publication of TW201035330A publication Critical patent/TW201035330A/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
    • B22D21/02Casting exceedingly oxidisable non-ferrous metals, e.g. in inert atmosphere
    • B22D21/04Casting aluminium or magnesium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/02Alloys based on aluminium with silicon as the next major constituent

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Injection Moulding Of Plastics Or The Like (AREA)
  • ing And Chemical Polishing (AREA)

Abstract

This invention provides an aluminum alloy part having an extremely complicated surface to exhibit an enhanced jointability to a composite resin member. The aluminum alloy part is an Al alloy member obtained by imposing a cast member of an Al-Si series alloy to surface chemical etching with an acid solution. The Al alloy member has multiple recesses over a portion or the whole of the surface; and the recesses have a mean opening width of above 0.1 to below 30μm, the inside surface of each recess having multiple protrusions consisting of an eutectic Si crystal The protrusions consisting of an eutectic Si crystal have sizes of above 0.1 to below 10μm that are equivalent to sphere particle diameter, while portions where only Si is distributed account for above 5 to below 80% of the total of the eutectic portions as determined by elemental analysis for Si and Al through X-ray fluorescence mapping.

Description

201035330 六、發明說明: 【發明所屬之技術領域】 本么月係關㈣以製造與高強度熱可龍樹脂組成物一 體化之構造物之樹脂黏合性優異的銘合金構件及其製 法。 【先前技術】 ο 將異種材質之銘構件與合成樹月旨一體化的铭-樹脂複合 f化製品、編器等之廣泛領域。 物V,,,' 樹脂複合材,係使用藉由黏著劑之介存 物貝壓黏鋁構件和樹脂構件者。 但是,最近,提柰古T人士 予以-體化的方法、。例^子黏著劑而將高強度的工程樹脂 至少一面,以射以^利文獻1中,提㈣在紹薄板的 的方法,其特_ 職独製造I樹脂複合體201035330 VI. Description of the Invention: [Technical Fields of the Invention] This is a technique for producing an alloy having excellent resin adhesion to a structure in which a high-strength heat-resistant resin composition is integrated and a method for producing the same. [Prior Art] ο A wide range of products such as f-products and encoders that combine the components of different materials with the synthetic tree. The material V,,, 'resin composite material is a pressure-sensitive aluminum member and a resin member which are used as a filler by an adhesive. However, recently, the method of cultivating the people of T. For example, the high-strength engineering resin is applied to at least one side of the adhesive to produce the I resin composite in the literature.

G _法設錢一j馳薄録面,預先以 具的可動金屬模具如/、人將核薄板安裝於金屬模 押密合並封閉模型 11疋金屬換具側將上述粗链面層壓 具所形成的模腔内,射層與顧押之固定金屬模 樹脂層。内射出樹脂並在链薄板的至少一面成形出 合=::::取得使_編構件-_ 用於要求強力為有用的技術,但此種複合材若欲應 方 098145276 點者力(固著力)和剛性之機械性構造物 201035330 面,則不夠充分。 於是,追求以強力黏著力將作為樹脂構件之強度高的物質 黏著的鋁-樹脂複合體。 例如,於專利文獻2、3,提案有可達成上述要求之鋁-樹 脂複合體的製造方法。 [先前技術文獻] [專利文獻] [專利文獻1]日本專利特開2000-176962號公報 [專利文獻2] WO 2004/041533號公報 [專利文獻3]日本專利特開2007-182071號公報 【發明内容】 (發明所欲解決之問題) 例如,於上述專利文獻3中,提案有一種由經過浸潰於從 氨、肼、及水溶性胺化合物中選出之1種以上水溶液中之步 驟且在電子顯微鏡觀察下被數平均内徑1〇〜80ηιη之凹部覆 蓋表面的鋁合金零件,以及在上述鋁合金零件之上述表面以 射出成形固著、主成分為聚醯胺樹脂且次要成分為耐衝擊性 改良材之樹脂成分組成的熱可塑性合成樹脂組成物零件所 構成的金屬樹脂複合.體。 此複合體係藉由作成為使鋁合金零件表面以超微細凹部 和孔的開口部所覆蓋的形狀’則可使聚醯胺系樹脂組成物強 固黏者。 098145276 201035330 但是’上述專利文獻2、3所提案的複合體,均無法發揮 可承受使用作為機械構造物的強黏著力。 本發明係為了解決此種課題而提案者,經由使用特定合金 系的銘合金讀’將其表面減複雜化,以提供提高了盆盘 •複合化樹脂構件間之點合性的紹合金零件為其目的。…、 (解決問題之手段) ο 本=之樹脂黏合性優異之銘合金構件’係為了達成此目 的,而屬於在其一部八* , 刀表面或全面具有複數個凹狀部的 Al-Si系I呂合金構件, y 硪凹狀部係於内面具有複數個由共晶 石夕結晶所構成之凸部, 其特徵為,上述由共晶矽結晶所構成 的凸部具有相當球粒徑 仫為以上且10#m以下之尺 •寸且根據螢光X射綠之繪圖分析進行石夕元素及紹元素分 析夺在,、曰曰邛/刀所存在之僅有矽的分佈部位佔有5%以上 且80%以下。 ❹ 又本發明之樹月旨點合性優異之铭合金構件表面,係形成 具有複數個上述由技曰 、 ”明矽結晶所構成之凸部之平均開口寬 度為0.1 V m以上且 β m以下的凹狀部,且除了此等凹狀 部以外’關於初晶a、Aw、 部分’形成有下述凹狀部:於銘合 金構^的厚度方向㈣中,在垂直其厚度方向上,且在通過 卩之最间°卩的$線與通過最深部之底線之間的中間線 上,以掃描型電 礙鏡觀察所測定之平均開口寬度為0.1 /zm以上且3〇#m以 下之尺寸,深度為O.lem以上且30 098145276 5 201035330 以下之尺寸的複數凹狀部。 上述由共晶矽結晶所構成的凸部,較佳係在上述凹狀部内 面以0.001g/m2以上且ig/m2以下的量突出、析出。 作為構成上述樹脂黏合性優良之鋁合金構件的鋁合金,較 佳係含有Si : 5.0質量%以上且is質量%以下、Fe : i 3質 篁/ί>以下、Cu· 5.0質量%以下、Mg : 1.5質量%以下、Ni : 1.5質量%以下,且殘餘部分具有A1以及由不可避免之雜質 所構成之成分組成的銘合金。 本發明之樹脂黏合性優良之鋁合金構件,係在將具有上述 成分組成之鋁合金炼融液予以鑄造而製造鋁合金構件時,在 鑄造時的共晶Si凝固溫度為755。(:以上且780。(:以下之領域 中,使冷卻速度為〇.rC/秒鐘以上且1〇〇〇c/秒鐘以下而取 得。 將鑄造之鑄物體整形成指定形狀、尺寸後,對表面以酸系 液施以化學蝕刻處理,則可取得具有上述表面特性的鋁合金 構件。 又,本發明之樹脂黏合性優異的鋁合金構件,係對表面先 以酸系液之化學㈣處理,並且使用氧化銘微粒子或㈣微 粒子所構㈣絲子倾㈣處理,於化縣形成凹凸形 狀’則取得黏合強度更高的紹-樹脂複合體。 作為表面上所形成的凹凸形狀,較佳係表面粗链度之^ 值成為1〜100/zm之尺寸。 098145276 6 201035330 (發明效果) 根據本發明,對用以製造複合體之鋁合金構件表面,賦予 經複雜化的凹凸形狀。因此,例如以射出成形法等對其表面 _ 黏合樹脂構件時’藉由上述複雜化之凹凸形狀可有效發揮錨 固效果,可輕易取得黏合強度高的鋁-樹脂複合體。 並且’作為銘合金素材,因為可使用Al-Si系的鑄造合金, 故可廉價製造形狀自由度高的複合體。又,如此所製造的鋁 〇樹脂複*體,係在紹合金構件與樹脂成形體之間之界面(銘 树月曰界面)的密合強度和氣密性極高,且即使曝露於嚴苛之 %境下仍可保持其優良的密合強度及氣密性,並可長期維持 高可靠性。 . 因此’本發明之鋁·樹脂複合體,可適當使用於例如以汽 車用之各種感應器零件、家電機器用之各種開關零件、各種 產業機器用之冷凝器零件等為首之廣泛領域中的金属-樹脂 〇 -體成料件’特別適#使驗賴脂成雜由㉝合金構件 的。I5刀表面以突合狀態突出,並要求高黏合強度的金屬_ 樹脂一體成形零件。 •【實施方式】 本發月者等人對於在製造纟呂_樹脂複合體時,提高與複合 化树月曰構件間之黏合性、改善銘合金零件之表面性狀的對策 重複致力檢討。 於提同與树月曰構件間之黏合性上,有效的是在紹合金零件 098145276 7 201035330 表面形成錨固效果高的凹凸。但是,對於金屬組成範圍廣且 金屬組織複雜的A1鑄造用合金而言,將難以形成錨固效果 南的凹凸。 於是’本發明發現,在Al-Si系鑄造用合金中’藉由將特 定組成之生成、與其後的蝕刻處理予以組合’則可在其表面 形成錨固效果高的凹凸。 以下詳細說明。 首先,說明關於在Al-Si系合金構件表面容易形成複雜化 凹凸的基本原理。 將實用上常用之具有亞共晶-共晶附近組成的Al-Si系合 金之熔融液於鑄型内凝固時,如圖1所見般,呈現出薄片狀 之Al-Si共晶部⑺埋入於初晶α -Al(l)間的形態。於是,Al-Si 共晶部(2)係由共晶〇:-Α1(3)與共晶Si(4)所構成的形態。 若將具有此種金屬組織的Al-Si系合金構件以鹽酸等之酸 液進行化學性蝕刻處理,則使Al-Si共晶部的共晶α_Α1(3) 選擇性溶解。其係因共晶α _A1的Α1純度比其他部分更低。 其結果,成為由埋入於初晶α·Α1(1)間之薄片狀共晶部變 成僅殘存共晶Si(4)’在成為凹部之初晶α_Αι間的空隙部(5) 中所殘存的si突出於上述凹部壁的形態(參照圖2)。 圖3為示出以掃描電子顯微鏡觀察後述實施例所用之試 料表面之結果。可知Si結晶在初h_A1間所形成之凹狀部 内部中突出,形成凸部。 098145276 8 201035330 本^明係欲在初晶α-Al間之殘存Si突出壁面 』、毛揮黏合樹脂構件時的錯固機能。 、狀 :有效表現上述錯固效果,有效的是使所形成 燮窄,日祐办 X的四狀部 使大出的Si結晶所形成的凸部變窄且多。 的 、,,。日曰所形成的凸部變窄且多時,雖亦依賴素# Αι & 系合金的Si含#,但必腳整製造條件,尤其是凝1 冷卻速度和化學蝕刻條件。 的G _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ In the formed cavity, the shot layer and the fixed metal mold resin layer. The resin is injected and formed on at least one side of the chain sheet. =:::: The technique for making the _-member is used to require strength. However, if the composite is intended to be 098,145,276 points (fixing force) And the rigid mechanical structure 201035330 is not enough. Then, an aluminum-resin composite in which a material having high strength as a resin member is adhered with a strong adhesive force is pursued. For example, Patent Documents 2 and 3 propose a method for producing an aluminum-resin composite which can achieve the above requirements. [Patent Document 1] [Patent Document 1] Japanese Patent Laid-Open Publication No. 2000-176962 (Patent Document 2) WO 2004/041533 (Patent Document 3) Japanese Patent Laid-Open Publication No. 2007-182071 (Problems to be Solved by the Invention) For example, in the above Patent Document 3, there is proposed a step of immersing in one or more aqueous solutions selected from ammonia, hydrazine, and a water-soluble amine compound, and in the electron Under the microscope, the aluminum alloy parts covered by the concave portion having the average inner diameter of 1 〇 to 80 ηηη, and the surface of the above aluminum alloy part are fixed by injection molding, the main component is polyamine resin and the secondary component is impact resistant. A metal-resin composite body composed of a thermoplastic resin composition component composed of a resin component of a modified material. In the composite system, the polyamine-based resin composition can be strongly adhered by forming a shape in which the surface of the aluminum alloy part is covered by the ultra-fine concave portion and the opening of the hole. 098145276 201035330 However, the composites proposed in the above Patent Documents 2 and 3 are not capable of exerting a strong adhesive force as a mechanical structure. In order to solve such a problem, the present invention proposes to reduce the surface of the alloy by using a special alloy-based alloy, to provide a sintered alloy part having improved dot-to-cell composite resin members. Its purpose. ..., (the means to solve the problem) ο This is an alloy component with excellent resin adhesion. In order to achieve this, it belongs to Al-Si which has a plurality of concave portions on its surface. The y 合金 alloy member has a plurality of convex portions composed of eutectic crystals on the inner surface, and the convex portion composed of the eutectic cerium crystal has a substantially spherical particle size. For the above and the size of 10#m or less and according to the analysis of the fluorescent X-ray green, the analysis of the elements of the Shixia element and the Shao element is carried out, and the only part of the distribution of the 曰曰邛/knife is 5%. Above and below 80%. Further, in the surface of the alloy member which is excellent in the point of the present invention, the average opening width of the convex portion having a plurality of the above-mentioned techniques and "alum crystals" is 0.1 V m or more and β m or less. In addition to the concave portions, the concave portion is formed with respect to the primary crystal a, Aw, and the portion: in the thickness direction (4) of the alloy structure, in the thickness direction thereof, and The average opening width measured by scanning type electric mirror is 0.1 / zm or more and 3 〇 #m or less in the middle line between the most straight line of the 卩 and the bottom line passing through the deepest part. The plurality of concave portions having a depth of O.lem or more and 30 098145276 5 201035330 or less. The convex portion composed of the eutectic crystal is preferably 0.001 g/m 2 or more and ig/ on the inner surface of the concave portion. The aluminum alloy having an aluminum alloy member having excellent resin adhesion is preferably contained in an amount of not less than 5.0% by mass and equal to or less by mass, and Fe: i 3 mass 篁 / ί Cu·5.0% by mass or less, Mg: 1.5% by mass Ni: 1.5% by mass or less, and the residual portion has an alloy composed of A1 and a component composed of unavoidable impurities. The aluminum alloy member having excellent resin adhesion of the present invention is an aluminum having the above composition. When the alloy smelting liquid is cast to produce an aluminum alloy member, the eutectic Si solidification temperature at the time of casting is 755. (: 780 or more.): In the following fields, the cooling rate is 〇.rC/sec or more. The obtained cast object is formed into a predetermined shape and size, and then subjected to chemical etching treatment on the surface of the acid-based liquid, whereby an aluminum alloy member having the above surface characteristics can be obtained. The aluminum alloy member excellent in the adhesiveness of the resin of the present invention is treated with the chemical (4) of the acid-based liquid on the surface, and is treated with the oxidized fine particles or (4) fine particles (four) the silk tilting (four) treatment, and the concave and convex shape is formed in the chemical county. Then, a smear-resin composite having a higher adhesive strength is obtained. As the uneven shape formed on the surface, it is preferable that the value of the surface roughness is 1 to 100/zm. 098145276 6 20103 5330 (Effect of the Invention) According to the present invention, the surface of the aluminum alloy member for manufacturing the composite body is provided with a complicated concavo-convex shape. Therefore, for example, when the surface of the aluminum alloy member is bonded by an injection molding method or the like, the resin member is adhered to The uneven shape can effectively exhibit an anchoring effect, and an aluminum-resin composite having a high bonding strength can be easily obtained. And as an alloy material of the name, since an Al-Si-based casting alloy can be used, it is possible to inexpensively manufacture a shape having a high degree of freedom. Further, the aluminum-ruthenium resin composite body produced in this manner is excellent in adhesion strength and airtightness at the interface between the member of the Shao alloy and the resin molded body (Mingshu Yueqi interface), and even if exposed It can maintain its excellent adhesion strength and air tightness under strict conditions and maintain high reliability for a long time. Therefore, the aluminum-resin composite of the present invention can be suitably used in various fields such as various sensor parts for automobiles, various switch parts for home electric appliances, and condenser parts for various industrial machines. - Resin 〇-body forming part 'Special # 使 使 验 验 验 验 使 使 使 。 。 。 。 。 。 。 The surface of the I5 blade protrudes in a protruding state, and a metal-resin integrally formed part of high adhesion strength is required. • [Embodiment] The person in charge of this month has repeatedly reviewed the measures to improve the adhesion to the composite tree member and improve the surface properties of the alloy parts when manufacturing the _ _ resin composite. In the adhesion between the member and the tree raft member, it is effective to form a bump with high anchoring effect on the surface of the alloy part 098145276 7 201035330. However, for an alloy for A1 casting having a wide metal composition range and a complicated metal structure, it is difficult to form an unevenness of the anchoring effect in the south. Then, the present invention has found that in the Al-Si-based casting alloy, by combining the formation of a specific composition and the subsequent etching treatment, irregularities having a high anchoring effect can be formed on the surface. The details are as follows. First, the basic principle that the complicated unevenness is easily formed on the surface of the Al-Si-based alloy member will be described. When a molten metal of an Al-Si alloy having a composition near the hypoeutectic-eutectic in a practical use is solidified in a mold, as shown in Fig. 1, a flaky Al-Si eutectic portion (7) is buried. The form between the primary crystal α - Al (l). Then, the Al-Si eutectic portion (2) is a form composed of eutectic 〇: -Α1 (3) and eutectic Si (4). When the Al-Si-based alloy member having such a metal structure is chemically etched with an acid solution such as hydrochloric acid, the eutectic α_Α1(3) in the Al-Si eutectic portion is selectively dissolved. It is due to the lower purity of Α1 of eutectic α _A1 than other parts. As a result, the flaky eutectic portion embedded between the primary crystal α·Α1(1) remains as only the remaining eutectic Si(4)′ remains in the void portion (5) between the primary crystal α_Αι which is the concave portion. The si protrudes from the shape of the above-mentioned recess wall (refer to FIG. 2). Fig. 3 is a view showing the results of observing the surface of the sample used in the examples described later by a scanning electron microscope. It is understood that the Si crystal protrudes inside the concave portion formed between the initial h_A1 to form a convex portion. 098145276 8 201035330 This is a system that is intended to be a residual wall of the Si in the primary crystal α-Al. Shape: It is effective to express the above-mentioned staggering effect, and it is effective to make the formation narrow, and the four portions of the X-ray X can narrow the convex portion formed by the large Si crystal. of ,,,. When the convex portion formed by the corona is narrowed and long-term, it depends on the Si-containing # of the alloy of the prime, and the manufacturing conditions of the alloy, especially the condensation cooling rate and the chemical etching condition. of

後述關於較佳的製造條件,係說明有效發揮錯固機能 部的尺寸、分佈狀態。 以掃描型電子顯微鏡(日立製FE-SEM、S-4500型)觀察鋁 合金構件之表面構造時,由共晶Si結晶所構成之凸部尺寸 必須以相當球粒徑計為G ] # m以上幻 么士曰 1 * ^ A v»〇 gg 尺寸若未$ 0.1㈣以下之尺寸,則由共晶s i結晶所構成之 凸部本身易f折,無法發揮銷固作用,另—方面,即使於The preferred manufacturing conditions will be described later to effectively exhibit the size and distribution state of the erecting function portion. When the surface structure of the aluminum alloy member is observed by a scanning electron microscope (FE-SEM, S-4500 type), the size of the convex portion composed of the eutectic Si crystal must be G > # m or more in terms of the equivalent spherical particle diameter.幻么士曰1 * ^ A v»〇 gg If the size is less than 0.1 (four) or less, the convex portion formed by the eutectic si crystal itself is easily folded, and the pinning effect cannot be exerted. On the other hand, even

Si結晶尺寸為超過1G#m之情況,亦因尺寸過大而無法發 揮錨固作用。 殘存Si大出壁面的凹狀部,較佳係在銘合金構件之 厚度方向剖面中,在垂直其厚度方向上,且在通過凹凸部之 最高部的頂線與通過最深部之底線之間的中間線上,以掃描 型電子顯微鏡觀察所測定之平均開口寬度為01_以上且 30//m以下,較佳為〇.5//喊上且、m以下,更佳為i P以上且1〇//m以下之尺寸,深度為〇._以上且如 098145276 9 201035330 以下之尺寸為佳。 m’則射出成形時 g m以下,杈佳為0.5 “ m以上且2〇〆m 此凹狀部的平均開口寬度若窄於0.1/z 熔融樹脂難以進入,並在叙纟金構件與樹脂成形體的界面 生微小的空隙’而難以取得優良的密合強度和氣密性,相=When the crystal size of Si is more than 1G#m, it is too large to be anchored. The concave portion of the Si-out wall surface is preferably in the thickness direction cross section of the alloy member, in the thickness direction thereof, and between the top line passing through the highest portion of the uneven portion and the bottom line passing through the deepest portion. On the middle line, the average opening width measured by scanning electron microscope observation is 01_ or more and 30//m or less, preferably 〇.5// shouting and m or less, more preferably i P or more and 1 〇. The size below //m, the depth is 〇._ above and the size below 098145276 9 201035330 is better. m' is not less than gm at the time of injection molding, and preferably 0.5" m or more and 2 〇〆m. The average opening width of the concave portion is narrower than 0.1/z. The molten resin is difficult to enter, and the bismuth metal member and the resin molded body are The interface has tiny gaps' and it is difficult to obtain excellent adhesion strength and air tightness.

3〇#m,則在鋁成形體之表面處理(蝕刻處理)時溶解反應過 剩進行’產生材料表面缺落或者材料之板厚減少量增大的問 於本發明中,關於殘存Si於壁面突出之複數個凹狀部的 密度,較佳係每0.1mm正方中,平均開口寬度〇 5"m以上 且20"m以下、以及深度〇,5"m以上且2〇/zm以下範圍内 之1種或2種以上之尺寸者,以5個以上且200個以下左右 之範圍存在。 又,殘存Si於壁面突出之複數個凹狀部,於其一部分或 全部中,亦可具有在内部壁面形成至少丨個以上之内部凹狀 部的雙重凹狀部構造,又,亦可具有在内部壁面形成至少j 個以上之内部突起部的内部凹凸構造,更且,亦可並存此等 雙重凹狀部構造和内部凹凸構造。藉由在殘存Si於壁面突 098145276 10 201035330 出之複數個凹狀部的一部分或全部中,存在此種雙重凹狀部 構造和内部凹凸構造,則使鋁合金構件的凹狀部與樹脂成形 體的嵌入部相互強固黏合,於鋁合金構件與樹脂成形體之間 發揮更加優異的密合強度和氣密性。 更且,將上述鋁合金構件表面構造,以能量分散型X射 線分析裝置(堀場製作所製EMAX_7000)之繪圖分析而進行 石夕兀素及銘兀素分析時,必須使在共晶部分所存在之僅有 ❹^的分佈部位佔有5%以上且_以下。Si分佈部位未滿5% 則無法發揮有效的_效果。相反地,若超過8G%,則亦益 法忽略形成凹狀部壁面之初晶α_Αΐ的溶解,成為上述壁面 溶解,且Si結晶堆穑於 法發揮錨固效果。狀部内的狀態,對於樹脂成分無 由共晶Si結晶所構成之凸部的突出量,較佳係於 狀部内面以0.001以卜B ,, 〇 #。—去且1g/m以下之份量突出、析出為 若二;"7則難以表現有效的錨固效果。相反地, 另外’凸部的突出量,後 晶,使用刷子削落後,對於使^冓件表面上所形成的si結 晶粒子根據重量法所測定;J用0.1/mPC職器採取的結 此處’針對上述財經由共之選擇性溶解所 098145276 11 201035330 2共晶W吉晶突出部的凹狀部,合併說明有效發揮銷固機 能之在初晶α _A1所形成的凹狀部。起因於銘構件之表面凹 凸部而形成的複數凹狀部,較佳係在銘合金構件之厚度方向 剖面中,在垂直其厚度方向上,且在通過凹凸部之最高部的 頂線與通過最深部之底線之間的中間線上,以掃描型電子顯 微鏡觀察所測定之平均開口寬度為〇.km以上且3〇_以 :;。較佳為。·5一上且2。_以下’更佳為1㈣上 且Π)㈣以下之尺寸,深度為01_以上且、姐以下, 較佳為0.5# m以上且2〇#m以下之尺寸。 此凹狀部的平均開口寬度若窄於g 時炼轉脂難以進入,在銘合金構件與__胃== 取得優良的密合強度和氣密性,相反地: = = = :材料表面之 性降低的原因二;度不足之製品並且成為生產 又關於深度,若淺於o.l/zm, 得充分之樹脂成形體的嵌入部,相反地’若使其产亦難以取 ㈣則核成形體之表面處理(侧 ^30 題。 缺洛或者材料之板厚減少量增大的問 於本發日种,於_独合金構件 之複數個凹狀部之密 又凹凸部而形成 _侧 &度,可依母⑸細正方_,平均開口 12 201035330 寬度〇.5/zm以上且20#m以下及深度〇 5"m以上且2〇 μ m以下範圍内之1種或2種以上尺寸者,以$個以上且 200個以下左右之範圍存在。 又,鋁合金構件之複數個凹狀部,係於其一部分或全部 中,亦可具有在内部壁面形成至少1個以上之内部凹狀部的 雙重凹狀部構造,又,亦可具有在内部壁面形成至少丨個以 上之内部突起部的内部凹凸構造,更且,亦可並存此等雙重 〇 凹狀部構造和内部凹凸構造。藉由在鋁合金構件之複數個凹 狀部的一部分或全部中,存在此種雙重凹狀部構造和内部凹 凸構造’則使鋁合金構件的凹狀部與樹脂成形體的嵌入部相 互強固黏合,並且於銘合金構件與樹脂成形體之間發揮更力 優異的密合強度和氣密性。 其次,說明關於本發明對象之Al-Si系合金的較佳入金矣 C)3〇#m, when the surface treatment (etching treatment) of the aluminum formed body is excessive, the dissolution reaction is excessive, and the surface of the material is missing or the amount of decrease in the thickness of the material is increased. In the present invention, the remaining Si is protruded from the wall surface. The density of the plurality of concave portions is preferably 1 in the range of 0.1 mm or more, the average opening width 〇 5 " m or more and 20 " m, and the depth 〇, 5 " m or more and 2 〇 / zm or less; The type or the two or more types are present in a range of about 5 or more and 200 or less. Further, a plurality of concave portions in which Si remains on the wall surface may have a double concave portion structure in which at least one or more internal concave portions are formed on the inner wall surface in part or all of the surface, or may have The inner wall surface has an inner concavo-convex structure in which at least j or more internal protrusions are formed, and the double concave portion structure and the inner concavo-convex structure may be coexisted. By having such a double concave portion structure and an internal concavo-convex structure in a part or all of a plurality of concave portions which are formed by the residual Si in the wall surface protrusion 098145276 10 201035330, the concave portion of the aluminum alloy member and the resin molded body are formed. The embedded portions are strongly bonded to each other, and exhibit more excellent adhesion strength and airtightness between the aluminum alloy member and the resin molded body. In addition, when the surface structure of the above-mentioned aluminum alloy member is analyzed by the drawing analysis of the energy dispersive X-ray analyzer (EMAX_7000 manufactured by Horiba, Ltd.), it is necessary to have the eutectic portion. Only the distribution of ❹^ accounts for more than 5% and below _. If the Si distribution is less than 5%, the effective effect cannot be achieved. On the other hand, if it exceeds 8 G%, it is also possible to neglect the dissolution of the primary crystal α_Αΐ which forms the wall surface of the concave portion, and the above-mentioned wall surface is dissolved, and the Si crystal stacking method exerts an anchoring effect. In the state in the shape, the amount of protrusion of the convex portion composed of the eutectic Si crystal is not included in the resin component, and it is preferable that the inner surface of the portion is 0.001 or B, and 〇 #. - Going and the amount below 1g/m is prominent and precipitated as two; "7 is difficult to express an effective anchoring effect. Conversely, in addition, the amount of protrusion of the convex portion, the back crystal, which is used after the brush is cut off, is determined by the gravimetric method for the si crystal particles formed on the surface of the electrode; J is taken here with a 0.1/m PC device. 'The concave portion of the eutectic W-shaped protrusion of the 098145276 11 201035330 2 for the selective dissolution of the above-mentioned financial resources, and the concave portion formed by the primary crystal α_A1 which effectively exhibits the pinning function. The plurality of concave portions formed by the surface uneven portions of the member are preferably in the thickness direction cross section of the alloy member, in the thickness direction thereof, and at the top line passing through the highest portion of the uneven portion and passing through the deepest portion The average opening width measured by scanning electron microscope observation on the middle line between the bottom lines of the parts is 〇.km or more and 3〇_以:;. Preferably. · 5 one and 2. Preferably, the following dimensions are 1 (four) and Π) (4) the following dimensions, and the depth is 01_ or more and less than the sister, preferably 0.5 # m or more and 2 〇 #m or less. If the average opening width of the concave portion is narrower than g, it is difficult to enter the refining fat, and the alloy member and the __ stomach == obtain excellent adhesion strength and airtightness. Conversely: = = = : material surface property The reason for the decrease is 2; the product of insufficient degree is produced and the depth is, if it is shallower than ol/zm, the embedding portion of the resin molded body is sufficient, and conversely, if it is made difficult to produce (4), the surface of the core molded body Treatment (side ^30 questions. If the amount of reduction in the thickness of the material or the increase in the thickness of the material is increased in the present day, the _ side & degree is formed in the dense and concave portions of the plurality of concave portions of the _ alloy member. According to the mother (5) thin square _, the average opening 12 201035330 width 〇.5/zm or more and 20#m or less and depth 〇5 " m or more and 2 〇 μ m or less within the range of one or more than More than or equal to 200 or less. The plurality of concave portions of the aluminum alloy member may be formed in part or all of the inner wall surface, and may have a double recessed portion formed on the inner wall surface. The concave portion structure, in addition, may have at least 丨 formed on the inner wall surface The inner concavo-convex structure of the inner protrusions described above may further include such a double concavity-and-concave structure and an inner concavo-convex structure. This may be present in a part or all of a plurality of concave portions of the aluminum alloy member. In the double concave portion structure and the internal concavo-convex structure, the concave portion of the aluminum alloy member and the embedded portion of the resin molded body are strongly bonded to each other, and the adhesion strength and gas are more excellent between the alloy member and the resin molded body. Next, a description will be given of a preferred gold alloy for the Al-Si alloy of the object of the present invention.

本發明較佳係含有Si : 5.0質量%以上且18質量%以下 較佳為6.0質量%以上且12 5質量%以下,F .質量% 以下、較佳為0.9質量%以下,Cu: 5.0質量%以下± ° a广、較佳為 4.5質量%以下,Mg: j 5質量%以下、較佳為ι 曰‘、、、 -.χτ. .貝里%以 下’Nl: L5質量%以下、較佳為1.1質量%以下,殘餘部八 具有A1以及由不可避免之雜質所構成之成分組成的合金刀 為對象。以下說明其理由。 作The present invention preferably contains Si: 5.0% by mass or more and 18% by mass or less, preferably 6.0% by mass or more and 125% by mass or less, F.% by mass or less, preferably 0.9% by mass or less, and Cu: 5.0% by mass. The following is ± ° a wide, preferably 4.5% by mass or less, Mg: j 5 mass % or less, preferably ι 曰 ', , -. χτ. . . . . . . . . . . . . . . . . . . . The alloy knives having a residual portion 8 having A1 and a component composed of unavoidable impurities are targeted for 1.1% by mass or less. The reason is explained below. Make

Si : 5.0質量%以上且18質量%以下 098145276 13 201035330Si : 5.0% by mass or more and 18% by mass or less 098145276 13 201035330

Si係用於增加母材強度、降低熱膨脹率、提高鑄造性等 而添加。尤其是於本發明中,伴隨共晶組織内之共晶α_Α1 的選擇性溶解所形成之由共晶Si所造成的突出部,對於樹 脂黏合性的幫助最騎要。Si未滿5.G%,則Si f過少,無 法取得充分的共晶組織,無法表現有效的錨固效果。另一方 面’若超過18%,則因初曰曰曰si白勺大量析出而阻礙錯固效果。 Fe : 1.3質量%以下The Si system is added for increasing the strength of the base material, lowering the coefficient of thermal expansion, improving the castability, and the like. Particularly in the present invention, the protrusion formed by the eutectic Si formed by the selective dissolution of the eutectic α_Α1 in the eutectic structure is most suitable for the adhesion of the resin. When Si is less than 5. G%, Sif is too small, and a sufficient eutectic structure cannot be obtained, and an effective anchoring effect cannot be exhibited. If the other side is more than 18%, the large-scale precipitation of the first-time si will hinder the staggering effect. Fe : 1.3% by mass or less

Fe係用於防止對於金屬模具燒結而添加。但,以若超過 1.3質量%,則引起急劇的強度降低,進而無法避免樹脂黏 合後之鋁-樹脂複合體的強度降低。Fe is used to prevent addition to the metal mold. However, if it exceeds 1.3% by mass, a sharp decrease in strength is caused, and the strength of the aluminum-resin composite after resin bonding cannot be prevented from being lowered.

Cu : 5.0質量%以下Cu : 5.0% by mass or less

Cu係用於增加母材強度以及提高切削性而添加。但,cu 若超過5.0質量%,則發生鑄造性降低,又,樹脂黏合後之 鋁-樹脂複合體的耐餘性顯著降低。Cu is added for increasing the strength of the base material and improving the machinability. However, when the cu exceeds 5.0% by mass, the castability is lowered, and the durability of the aluminum-resin composite after the resin is bonded is remarkably lowered.

Mg : 1.5質量%以下Mg : 1.5% by mass or less

Mg係用於增加母材強度以及提高樹脂黏合後之鋁-樹脂 複合體的耐蝕性而添加。但,Mg若超過丨5質量%,則發 生熔融液氧化’產生大量氣體。The Mg system is added for increasing the strength of the base material and improving the corrosion resistance of the aluminum-resin composite after the resin is bonded. However, if Mg exceeds 5% by mass, the melt is oxidized to generate a large amount of gas.

Ni : 1.5質量%以下Ni : 1.5% by mass or less

Ni係用於使高溫強度安定化而添加。但,见若超過^ $ 質量% ’則鑄造性及時效硬化性降低。 不可避免雜質Μη : 〇.65質量%以下、Zn : 3 〇質量%以下 098145276 14 201035330 不可避免雜質為多,無法避免其等混入若超 過㈣質量%,則树的切削性降低。另—方面’ Zn若超 過3.0質量%,則樹脂魏合後之銘_樹脂複合體的耐錄降 低。因此’作為不_免雜質之·、〜較佳係限制於上述 量以下。 Ο 接著,說明使用具有上述成分組成之A1_si系紹合金,製 造本發明之樹脂黏合性優異之鋁合金構件的方法。 合金炫融液的調製方法並無特別限制。若進行通常的溶解 即足夠。 本發明所用之A1-Si系合金因&含量較多,且熔融溫度 低,故較佳係鱗轉作成目_狀。峰得精細度高且安 定之機械特性醜點而言,較佳雜用料法。鑄入條件亦 無特別限制。 Ο 如上述,於取得複雜化之表面性狀上,較佳係使凝固後之 結晶組織纖細。由此意義而言,於矯造時之共晶Si凝固溫 度為755°c以上a 7帆以下之領域中,冷却速度必須設為 0.1C/秒鐘以上且1〇〇aC/秒鐘以下。 冷却逮度未滿G.1 口秒鐘,則結晶_變大,即❹後施 以化學性_處理亦在共晶Si結晶所構成之凸部尺寸,分 佈狀虹無法轉^者,顿轉著料«。相反地,冷 =度若超過靴騎,_急劇冷卻使得共晶&結晶 隻成過細,無法發揮錨固效果。 098145276 201035330 為了整理所得鑄造品的形狀、尺寸’將熔液通道等不需要 部分切斷除去後’視需要予以削面整理樹脂黏合面。 作為在已整理樹脂黏合面之鑄造品之樹脂黏合面表面 上’形成具有所需凹凸部之鋁合金構件的方法,可列舉例 如,將鋁合金材浸漬於鹽酸、 鱗酸、硫酸、醋酸、草酸、抗 壞企酸、笨曱酸、丁酸、檸檬酸、甲酸、乳酸、異丁酸、蘋 果酸、丙醆、酒石酸等之酸溶液所構成的蝕刻液中,並對此 鋁合金材表面形成指定之凹凸部的蝕刻處理方法。 作為曰此目的所用之钱刻液,以酸溶液型式,可列舉酸濃度 0.1重上且80重量%以下、較佳為i重量。以上且刈 重量%以下之鹽酸溶液、械溶液、稀硫酸溶液、醋酸溶液 =。、和酸濃度5重量%以上且3G重量%以下、較佳為⑺重 里%以上且2〇重量%以下的草酸溶液等。 更加促進共“_A1溶解之目㈣言,亦可在此等 酸溶液中添加i化物。作為_化物,可列舉例如氣化納 二氣化鎂侧等之氣化物、和氣化㈣之氟化物和 漠化鉀等化物等,考慮安全性㈣較佳為氯化物,更 且’姓刻液中之鹵離子濃度,通常為〇1七公升 上 且300g/L以下、較佳為lg/L以上且丨取以下,若未滿 離子的效果小,_起共^仏_, 產生無柄成具有Sl結晶^部之凹狀部㈣題 3〇〇机之情況’在喊雜之表面處理(_處理)時溶解反 098145276 201035330 應急劇進行,因此發生難以控制之選擇性 形成之凹狀部及Si結晶突出部的問題。Ni is used to stabilize the high temperature strength and to add it. However, if it exceeds ^$% by mass, the castability and time-effective hardenability are lowered. Inevitable impurity Μη : 〇.65 mass% or less, Zn: 3 〇 mass% or less 098145276 14 201035330 Inevitably, there are many impurities, and if it is not more than (4) mass%, the machinability of the tree is lowered. On the other hand, if the Zn exceeds 3.0% by mass, the resin-recombined _ resin composite has a low resistance to degradation. Therefore, it is preferable to limit the amount to be less than the above amount. Next, a method of producing an aluminum alloy member excellent in resin adhesion of the present invention using an A1_si system having the above-described composition will be described. The preparation method of the alloy smelting liquid is not particularly limited. It is sufficient if the usual dissolution is carried out. The A1-Si-based alloy used in the present invention has a high content of & and a low melting temperature, so that the scaly is preferably converted into a shape. In terms of the fineness of the peak and the ugly mechanical properties of the stability, the miscellaneous material method is preferred. There are no special restrictions on the casting conditions. Ο As described above, in order to obtain a complicated surface property, it is preferred to make the crystal structure after solidification fine. In this sense, in the field where the eutectic Si solidification temperature during the preparation is 755 ° C or more and a 7 or less, the cooling rate must be 0.1 C / sec or more and 1 〇〇 a C / sec or less. If the cooling arrest is less than G.1 for 2 seconds, the crystal _ becomes larger, that is, after the enthalpy is chemically treated, the convex portion size formed by the eutectic Si crystal is also formed, and the distribution rainbow cannot be rotated. Feeding «. Conversely, if the cold = degree exceeds the boots, the _ sharp cooling makes the eutectic & crystallization too fine to achieve the anchoring effect. 098145276 201035330 In order to arrange the shape and size of the obtained cast product, the part of the melt passage is not required to be cut and removed, and the resin bonding surface is trimmed as necessary. As a method of forming an aluminum alloy member having a desired uneven portion on the surface of the resin bonding surface of the cast product of the resin bonding surface, for example, the aluminum alloy material is immersed in hydrochloric acid, scaly acid, sulfuric acid, acetic acid, oxalic acid. An etching solution composed of an acid solution such as anti-bad acid, alum acid, butyric acid, citric acid, formic acid, lactic acid, isobutyric acid, malic acid, propylene glycol, tartaric acid, etc., and formed on the surface of the aluminum alloy material The etching method of the specified uneven portion. As the money engraving liquid used for this purpose, the acid solution type may have an acid concentration of 0.1% by weight and 80% by weight or less, preferably i by weight. Above and below 5% by weight of hydrochloric acid solution, mechanical solution, dilute sulfuric acid solution, acetic acid solution =. And an oxalic acid solution having an acid concentration of 5 wt% or more and 3 wt% or less, preferably (7) wt% or more and 2 wt% or less. Further, it is also possible to add a compound to the acid solution of the "_A1". Considering safety (4), preferably chloride, and the concentration of halide ions in the surname, usually 〇17 liters and 300 g/L or less, preferably lg/L or more. Take the following, if the effect of the full ion is small, _ a total of ^ 仏 _, resulting in a sessile into the concave part of the Sl crystal ^ (4) problem 3 之 machine's situation in the surface of the shouting (_ processing When the dissolution anti-098145276 201035330 should be carried out rapidly, there is a problem that the concave portion and the Si crystal protruding portion which are selectively formed are difficult to control.

❹ 另外,於本發明中,作為在銘合金構件表面形成所需之凹 狀部的⑽Μ ’叫酸和超過⑽重量%濃度之濃硫酸等氧 化力強的酸溶液、和氫氧化姊氫氧化鉀等之驗性溶性並不 適當。派硫酸权氧化力較_酸職,對純合金具有生 成皮膜能力,反而在紹合金構件的表面形成強固的氧化皮 膜,亚且難以將氧化歧溶解。又,氫氧化納和氫氧化卸等 驗性溶液,對純合金的溶解機構為全面溶解型,神由所 需之共晶Ml的性溶_成贿部及81結晶的 部 於本發明中,關於使用上述钱刻液對銘合金構件表面進行 触刻處理時的處理條件,係根據所使狀_液之種類、酸 濃度、㈣子濃料、和在銘合金構件上應形成之複數個凹 狀部的數目和尺寸等而異,通常,於鹽酸溶液之情況中,以 浴溫20°C以上且8(TC以下浸潰時間!分鐘以上且4〇分鐘以 下,於磷酸溶液之情況,以浴溫2〇t以上且6(rc#下浸潰 時間1分鐘以上且60分鐘以下,於硫酸溶液之情況中,以 浴溫2(TC以上且7(TC以下浸漬時間!分鐘以上且5〇分鐘以 下,於草酸溶液之情況中,以浴溫2〇°c以上且5〇ΐ以下浸 潰時間1分鐘以上且20分鐘以下,於醋酸溶液之情況中, 以浴溫20°C以上且80°c以下浸潰時間i分鐘以上且3〇分鐘 098145276 17 201035330 以下之範圍。使用之餘刻爾濃度和浴溫愈 理的效果愈顯著,可進行短時間處理,關於心*處 t則溶解速編恤共^A1=之未滿 及Si突出部的生成時需要長時間,χ ^/解之凹狀部 叫,又,於超過8(rc 中,溶解反應急劇進行並且難化制凹狀部及^皿 關於浸潰時間’未滿1分鐘則難以控制共晶α·Α1選胸生i =因相反地超過⑽分鐘之浸潰時間,則成&產性降二 又,於本㈣之以雜紐㈣刻處理中,亦 之溶液重複數次餘刻處理以形成所需的凹狀部。不问 在進行上述之化學钮刻處理 狀部之前,可進行均勾之侧處理、面施以凹 之目的下,亦可在IS合金構件4 3 σ提1固效果 讀仟表面,以喷擊處理形成 於金属組織複雜之無鑷造用合金中,在進行化學 。 時,於紹合金構件表面發线刻不均,且有時難以㈣2 敍刻處理。於噴擊處对,料轉介㈣触而在銘合金 構件的最表面重複發生局部之塑性變形及塑性變形所伴隨 的急熱、急冷’使表面組織微細化、均勻化。因此,在喷擊 處理後進行化學Μ刻處理,可形成均勾的凹狀部。 又由於喷擊處理後之紹表面被粗面化,因此經由在其後 施以化學期處理形成凹狀部的雙重粗面化處理,則可提高 樹脂黏合性。 098145276 18 201035330 於喷擊處理中’有·所謂葉輪之翼輪之離心力將 予以投射的射擊喷擊處理’以及使用空調機壓麵由壓縮= 氣將投射材抑投射的氣衝處理,均可雜合金構、、、空 面凹凸。 予表 〇 作為喷擊的方式,以空氣噴嘴式的喷擊為佳。喷擊處理、 方式甲’空氣喷嘴式為特佳的理由在於,相較於射擊式,的 列舉介質的能壓力高,例如相較时射壓力_射擊可 擊’可使介質以更強壓力彳驗“,結果可形賴於均=噴 名虫刻處理而言較佳的表面組織,彳士 二之 但由成本和效率之觀IfcA 言,亦可選定射擊喷擊處理。 而 經由喷擊處理可在銘合金構件 间形成表面粗糙声 Rz(Rz :以 JIS B 0601-1994 為其淮—丄 ^ 1卷旱之切平均祕度)為 以上且100/zm以下、較伟^ 1 ^ Λ 為上且50_以下 之凹凸。 「 〇 未滿1 // m則無法得到表面凹几命主 凸興表面組織的均勻 超過100/zm則隨著生產性降低 右 料變形等問題 ^ as '内〇卩應力的增加,而有材 縳鐵般之金屬微粒 了對鋁合金構件賦 視成本和效率而利 又,作為投射材,可列舉砂、氧化鋁、 子和樹脂材料,可根據各別目的使用。為 予凹凸,以硬度尚的氧化鋁為佳,亦可重 用鑄鐵般之金屬微粒子。 藉由以喷擊處理形成凹凸部 則鋁合金構件 的表面積變 098145276 19 201035330 大,韻刻處理液對於襲共晶部之共晶的反應性增 兩,故具有易於形成更多所需之凹狀部的效果。又,除了亦 可減低_處理㈣雜㈣,村除㉔合金構件表面的 污垢等。 又’於本發财,如上述般勒合金材如侧處理而形 成具有凹狀部之|§合金構件時,或者,於噴擊處理後施以钱 刻處理㈣成具有凹狀部種合金構件時,視需要,亦可對 此钱刻處叫或餅纽前種合金料面,在縣和調整 表面、除去表面附著物、污染物等目的之下,施以酸溶液之 酸處理、及/或、鹼溶液之鹼處理的前處理。 此處,作為此前處理所用之酸溶液,例如可使用以市售之 酸性脫脂劑調製者,可使用硫酸、硝酸、氟酸、-酸等之無 機酸和醋酸、擰檬酸等之有機酸、和混合此等酸所得之混合 酸等酸試藥所調製者等,又,作秘溶液,例如可使用以市 售之驗性脫㈣調製者、可使用以苛性納等之驗試藥調製 者、或混合其等所調製者等。 關於使用上述酸溶液及/或鹼溶液進行前處理之操作方法 及處理條件’可與習知使用此種酸溶液或鹼溶液所進行之前 處理之操作方法及處理條件相同,例如,可根據浸潰法、喷 霧法等之方法進行。 另一方面,在化學蝕刻處理前未進行噴擊處理之情況,較 佳係於化學蝕刻處理後進行超音波處理。 098145276 20 201035330 擊處理之情況,發生壓鑄之成形步驟 之表面金屬組織 時,時無法,溶解,而發_不:一 間:==二的浴溫、或延長浸潰時 生共晶si⑨日称 但隨私溶解量的增加,將發 ❹ Ο 合性非常,i、,難叫得轉 其與A1合金的密 進行超音波餘,將最表财’可在_處理後 除丰λ^Α^-L· 9在的堆積共晶Si結晶選擇性 僅使有助於樹_合性之表面凹部内的共晶Si結晶 又,在 狀Si且發二^之_處理過度進行、未取得所需之凸 可贿料料域理作為應 心的處置性措%,#此可僅除去堆積Si層,並且使所需的 凸狀Si依然突㈣存。 “的 方面亦可為以含有I化物離子之溶液將Si溶解除 去的方法,但此情況僅除去堆積Si層,難以控制僅使所· 之凸狀Si依然突出殘存,故不佳。 其次,於銘合金材之表面施以上述之前處理後、或施以形 成凹狀部之關處理後’視需要亦可進行水洗處理,於此水 洗處理中可使用玉業时、地下水、自來水、離子交換水等, 可根據所製造之is合金構料以適#選擇。更且,關於已施 098145276 21 201035330 :=和餘刻處理的紹合金材,視需要進行乾燥處理, 而關於此乾燥處理,除了 了為在至溫下放置的自然乾燥以 二可使用吹風機、乾燥機、烤爐等進行強制乾燥。 最後’間单說明關於本發明之提高了與樹脂構件間之黏合 性之鋁合金零件的使用態樣。 本發明之I呂合金構件係在藉上述各專利文獻所記載之射 出成形法製造銘·樹脂複合體時,被使用作為素独合金形 狀物。即’準備射出成形金屬模具,打開可動金屬模具並對 八方插人本發明之|呂合金構件,將可動金屬模具關閉後, 射出所A的熱可雜合成樹脂組成物,其後若打開可動金屬 模具並且脫模’料取得所需_删旨複合體。 於本發明中,特佳之射出一體成形品,係包含在紹合金構 件之彳刀表面上’將熱可塑性樹脂射出成形並且以突合狀 態結合之樹脂成形體的鋁_樹脂複合體。 此處’關於用以製造本發明之樹脂複合體的熱可塑性 树脂,可單獨使用各種熱可塑性樹脂,若考慮本發明之紹_ 樹脂複合體所要求之物性、料、使料境等,則作為熱可 塑性樹脂,較佳可列舉例如聚丙烯樹脂、聚乙稀樹脂、丙烯 腈-丁二烯-苯乙烯共聚合體(ABS)、聚碳酸酯樹脂(pc)、聚 醯胺樹脂(PA)、聚硫苯(pps)等之聚伸芳基硫樹脂、聚縮醛 樹脂、液晶性樹脂、聚對笨二曱酸乙二酯(pET)和聚對苯二 曱酸丁二酯(PBT)等之聚酯系樹脂、聚氧亞曱基樹脂、聚醯 098145276 22 201035330 亞胺樹脂、對聽苯乙_料和此等熱可塑性樹脂之^ =以上的混合物’又’為了更加改善銘合金構件與樹脂成形 體間之密合性、機械強度、耐熱性、尺寸安定性(耐變形、 曲勉等)、電性質等性能,更佳係在此等熱可塑性樹脂中添 加纖維狀、粉粒狀、板狀箄 寺之填充劑、和各種彈性體成分為 佳0 、處作為在熱可塑性樹脂中添加的填充劑,可例示玻璃 〇戴♦ 纖維、金屬纖維、石棉纖維、硼纖維等之無機質纖 維填充劑、和聚醯胺、氟樹脂、丙稀酸系樹脂等之高溶點有 機質纖維填充劑、和石英粉末、玻璃珠粒、玻璃粉、碳酸鈣 -: …機粍體類等之粉狀填充劑、和玻璃片、滑石和雲母 次'力員專之板狀填充劑等,相對於熱可塑性樹脂100 重=份’添力口 250重量份以下、較佳為2〇重量份以上且22〇 重里伤以下、更佳為30重量份以上且100重量份以下之範 〇 、真充劑的添加量若超過250重量份,則流動性降低且 、進入紹合金構件的凹部,而有無法取得良好的密合強 度或導致機械特性降低的問題。 又,作為熱可塑性樹脂中所添加的彈性體成分,可例示胺 基甲酸乙π 4 曰糸、核殼型、烯烴系、聚酯系、醯胺系、苯乙烯 等之彈性體,考慮射出成形時之熱可塑性樹脂的熔融溫度等 而選擇’又’相對於熱可塑性樹脂100重量份,使用30重 里伤以下’較佳為3重量份以上且25重量份以下之範圍。 098145276 23 201035330 此彈性體成分之添加量若超過3〇旦 強度更加提高的效果,產生機械特性::等相密合 體成分的配合效果係在使用聚^旨系樹脂作為。此祕 之情況中特別顯著。 ‘、’、…、可塑性樹脂 更且’在用於製造本發明 脂複合體之熱 脂中,可根據要求之性能適當添 ' 叙在熱可塑性樹脂中所 添加的么知添加劑,即難燃劑、染料和顏料 氧化劑和紫外線吸收劑等之安定劑、可塑劑、潤滑 脫模劑、結晶化促進劑、結晶核劑等。 於本發明中,關於雜合金構件安裝於射出柄用金屬模 具内而進行之熱可㈣樹脂的射出成形,可採用所用之熱可 塑性樹脂所要求的成形條件,但重要的是射出成形時炫融的 熱可塑性樹脂可確實進入鋁合金構件的凹狀部内並且固 化’較佳係將金屬模具溫度和汽缸溫度設定為熱可塑性樹脂 之種類和物性、以及成形周期所容許之範圍中的較高者,尤 其是金屬模具溫度,必須使下限溫度為9(TC以上、較佳為 130C以上’上限較佳係根據使用之熱可塑性樹脂的種類, 為由100°C至較該熱可塑性樹脂之熔點或軟化點(於添加彈 性體成分之情況係其中較高者的炫點或軟化點)低2〇°c左右 之溫度為止的範圍。又,金屬模具溫度之下限較佳係設定為 不較熱可塑性樹脂之熔點低14〇°C以上。 又,關於製造本發明之鋁-樹脂複合體之手段並非限於射 098145276 24 201035330 出成形法,亦可採用熱壓黏法。即,將上述鋁合金構件以 90°C〜300°C左右之範圍加熱’並在其表面將熱可塑性樹脂所 構成的樹脂構件,施加壓力並按壓,亦可取得所需之鋁-樹 脂複合體。 [實施例] 實施例1 : [A1合金試驗片之調製] ◎ 將含有 Si: 11 質量%、Fe: 0.71 質量%、(:11: 2.46 質量%、 Μη : 0.36 質量%、Mg : 0.29 質量%、Zn : 0.79 質量%、Ni : 0.72質量%之A1合金、熔融液’以180mmxl50mmx3mm之尺 寸進行壓鑄鑄入。另外,此時之設定條件為金屬模具溫度·· 17〇°C、熔融液溫度:720°C、射出速度:1.7m/s、製品填充 時間:10ms、製品内平均流速:llm/s。另外,鑄造時的冷 卻速度為40 C/秒鐘。 Ο 由所付之禱物,切出尺寸37.5mm><37.5mmx3mm的A1合 金片’並對此A1合金片’將鑄肌面由兩面各削面〇 3mm, 製作尺寸37.5mmx37.5mmx2.4mm的Ai合金試驗片。 • 其次,對於上述A1合金試驗片,於在5wt%鹽酸溶液中添 加了 54g/L之氯化鋁六水合物而調製之蝕刻液中,實施以 40°C浸潰10分鐘之蝕刻處理後予以水洗,並以12〇ΐ之熱 風乾無5分鐘,製作铭合金構件。 [紹合金構件之矽結晶的觀察] 098145276 25 201035330 將所得之A1合金試驗片表面,❹掃描 立製職m、s_45G")進行觀察’觀察^日顯細日 又,根據重量法測定其析出量。 相的尺寸, 所觀察之紹合金構件的表面,係例如圖3 所示,在紹表面所形成之凹狀部内部突出析广 的凸部。又,關於此種凸部的形狀 觀察處亦相同。又’將A1合金試驗片表面所形成晶, 使用刷子將其刷落後’對採集的結晶粒子藉由使曰 /Z m PC膜遽器之重量法進行測定。 所測疋之銘合金構件之某區域表面中所觀察到之凹狀部 的平均開口寬寬及内部突出析出的共⑽結晶尺寸及其分 佈,係凹狀部之平均開口寬度為〇·1_以上且·m以 下’相當球粒徑為〇·1/zm以上且1()"m以下,且對於上述 銘合金構件之表面以能量分散型X射線分析裝置(堀場製作 所製EMAX-7000)之緣圖分析進行石夕元素及銘元素分析,結 果,在共晶部分所存在之僅有以之分佈部位佔有45%。又, 鋁合金構件表面所形成之共晶矽析出量為每im正方為 0.001克以上,1克以下。關於此突出析出之矽結晶尺寸、 分佈及份量,即使改變觀察處亦幾乎全部無變化。 [剪切破壞荷重測定試驗] 將如上述處理所得之實施例1的鋁合金構件安裝於射出 成形機(NISSEI公司製ST10R2V)的金屬模具内,使用含有 098145276 26 201035330 填充劑的聚硫苯樹脂(Polyplastics公司製PPS等級名 1140A6)作為熱可塑性樹脂,並以射出時間(包含保壓時間)5 秒鐘、射出速度60mm/秒鐘、保壓力90MPa、成形溫度 310°C、及金屬模具溫度18〇t之成形條件進行射出成形, 如圖4所示般,製作在37.5mmx37.5mmx2.4mm尺寸的銘合 金構件(6)表面,使具有長度15mmx厚度3mmx高度6mm尺 寸且固黏在上述A1合金試驗片表面之樹脂成形體(7)—體化 Ο 之剪切強度測定試驗用的鋁-樹脂試驗片(鋁-樹脂複合體)。 使用剪切強度測定試驗機(島津製作所製:1〇〇ΚΝFurther, in the present invention, as the desired concave portion formed on the surface of the alloy member, (10) Μ 'acid and acid solution having a strong oxidizing power such as concentrated sulfuric acid exceeding (10)% by weight concentration, and cesium hydroxide potassium hydroxide It is not appropriate to test the solubility. The oxidizing power of the sulphuric acid has a stronger ability to produce a film for the pure alloy, and instead forms a strong oxidized film on the surface of the slag alloy member, and it is difficult to dissolve the oxidized lag. Further, the sodium hydroxide and the oxidizing agent are decomposed, and the dissolving mechanism for the pure alloy is a fully soluble type, and the eutectic M1 of the desired eutectic Ml is formed in the present invention. The processing conditions when the surface of the alloy member is subjected to the etch treatment using the above-mentioned money engraving liquid are based on the type of the liquid, the acid concentration, the (four) sub-concentrate, and the plurality of depressions to be formed on the alloy member. The number and size of the shapes vary, and usually, in the case of a hydrochloric acid solution, the bath temperature is 20° C. or more and 8 (the immersion time of TC or less is less than or equal to 4 minutes and less than 4 minutes, and in the case of a phosphoric acid solution, The bath temperature is 2 〇t or more and 6 (the immersion time of rc# is 1 minute or more and 60 minutes or less. In the case of a sulfuric acid solution, the bath temperature is 2 (TC or more and 7 (the immersion time of TC or less! Minutes or more and 5 〇) In the case of an oxalic acid solution, the bathing temperature is 2 〇 ° C or more and the immersion time of 5 〇ΐ or less is 1 minute or more and 20 minutes or less, and in the case of an acetic acid solution, the bath temperature is 20 ° C or more and 80 minutes or less. Below the °c, the dipping time is more than i minutes and 3 minutes 098145276 17 201035330 The range below. The effect of the remaining engraving concentration and the bath temperature is more remarkable, and the treatment can be performed for a short period of time. When the heart* is t, the dissolving speed is a total of ^A1=the undershoot and the formation of the Si protrusion. It takes a long time, χ ^ / solution of the concave part called, and, in more than 8 (rc, the dissolution reaction is sharp and difficult to make the concave part and ^ dish about the dipping time ' less than 1 minute is difficult to control Crystal α·Α1 selects the chest i = because the opposite is more than (10) minutes of the impregnation time, then the & production declines two, in this (four) to the hybrid (four) engraving treatment, the solution is repeated several times The treatment is performed to form a desired concave portion. It is also possible to perform the side treatment of the uniform hook and the concave surface before the chemical buttoning treatment portion described above, or the IS alloy member 4 3 σ 1 The solid effect is read on the surface of the crucible, and is formed by a spray treatment in a complex metal alloy with a metal structure. When the chemical is applied, the surface of the Yu Shao alloy member is unevenly lined, and sometimes it is difficult to perform the (4) 2 engraving treatment. At the point of the slamming, the material is referred to (4) and the surface is repeated on the outermost surface of the alloy member. The rapid heat and rapid cooling accompanying the physical deformation and the plastic deformation make the surface structure finer and uniform. Therefore, after the blasting treatment, chemical engraving treatment is performed to form a concave portion of the hook. Since the surface of the surface is roughened, the resin adhesion can be improved by the double roughening treatment which is formed by the chemical treatment to form the concave portion thereafter. 098145276 18 201035330 In the spray treatment, there is a so-called impeller. The centrifugal force of the wing wheel will be used for the projection of the shot and the air pressure of the air conditioner, and the air pressure is used to compress the projection material. The method of hitting is preferably an air nozzle type spray. The reason why the spray treatment and the method of the 'air nozzle type are particularly good is that the energy of the enumerated medium is higher than that of the shooting type, for example, the pressure of the shot can be made stronger by the pressure of the shot. "The results can be determined by the better surface structure of the spray treatment, and the gentleman's view of cost and efficiency, IfcA, can also be selected for shooting and spraying. The rough surface sound Rz (Rz: JIS B 0601-1994 for the Huai-丄^1 drought) is above and below 100/zm, and Weiwei ^ 1 ^ Λ is Up and down 50_ below the bump. "If you are less than 1 / 4 m, you can't get the surface concave. The uniformity of the surface of the main convex surface is more than 100/zm, and the right material is deformed with the decrease of productivity. The increase of the enthalpy stress, and the iron-like metal particles have a good effect on the cost and efficiency of the aluminum alloy component. As the projection material, sand, alumina, sub- and resin materials can be cited, and can be used according to the purpose. For the unevenness, it is better to use alumina with a hardness, but also heavy Cast iron-like metal particles. The surface area of the aluminum alloy member is changed by the spray treatment to form a concave and convex portion. 098145276 19 201035330 Large, the reaction of the rhyme processing liquid to the eutectic portion of the eutectic portion is increased by two, so it is easy to form. The effect of the concave part required more. In addition, it can also reduce the _ treatment (four) miscellaneous (four), the dirt on the surface of the alloy parts of the 24 parts of the village, etc. Also in the fortune, as described above, the alloy material is formed as a side treatment. When there is a concave part of the § alloy member, or after the smear treatment, the money is processed (4) into a concave-shaped alloy member, if necessary, the money may be called or the cake The alloy material surface is treated with acid treatment of acid solution and/or alkali treatment of alkali solution under the purpose of county and adjusting surface, removing surface deposits, pollutants, etc. Here, as the previous treatment For the acid solution, for example, a commercially available acidic degreaser can be used, and an inorganic acid such as sulfuric acid, nitric acid, hydrofluoric acid or acid, an organic acid such as acetic acid or citric acid, or the like can be used. Mixed acid For the preparation of the drug, etc., the secret solution may be, for example, a commercially available tester (four) modulator, a tester that can be used with caustic soda, or a mixture thereof. The operation method and processing conditions of the pretreatment of the acid solution and/or the alkali solution may be the same as those of the conventional treatment using the acid solution or the alkali solution, for example, according to the dipping method, On the other hand, in the case where the spraying treatment is not performed before the chemical etching treatment, it is preferable to perform the ultrasonic treatment after the chemical etching treatment. 098145276 20 201035330 The formation of the die casting occurs in the case of the treatment When the surface of the metal structure of the step, the time can not dissolve, and the hair _ no: one: == two bath temperature, or prolonged immersion when the eutectic si9 said, but with the increase of the amount of private dissolution, will be ❹ Ο It is very synonymous, i, it is difficult to call it with the denseness of the A1 alloy for ultrasonic, and it will be the most versatile in the eutectic Si crystallization after the _ treatment is removed λ^Α^-L·9 Sex only helps the tree The eutectic Si crystal in the surface concave portion is further processed in the form of Si and the hair is not processed, and the required convex brittle material is not obtained as a countermeasure. #This can only remove the accumulation. The Si layer, and the desired convex Si remains (4). "The aspect may be a method of dissolving and removing Si in a solution containing an I compound ion. However, in this case, it is not preferable to remove the Si layer, and it is difficult to control only the convex Si remains prominent, which is not preferable. The surface of the alloyed metal material may be subjected to a water-washing treatment after the above-mentioned previous treatment or after the treatment of forming the concave portion, and the jade industry, ground water, tap water, and ion-exchanged water may be used in the water washing treatment. Etc., according to the manufactured alloy composition, it is suitable for selection. Moreover, regarding the applied 098145276 21 201035330:= and the remaining alloy material, the drying treatment is carried out as needed, and the drying treatment is excluded. For the natural drying to the temperature, the forced drying can be carried out using a hair dryer, a dryer, an oven, etc. Finally, the use of the aluminum alloy parts of the present invention for improving the adhesion to the resin member is explained. The I-lu alloy member of the present invention is used as a plain alloy shape when the inscription resin composite is produced by the injection molding method described in each of the above patent documents. 'Prepare to shoot the forming metal mold, open the movable metal mold, and insert the |Lu alloy member of the present invention into the eight sides, close the movable metal mold, and then project the heat-mixable synthetic resin composition of the A, and then open the movable metal mold. Further, in the present invention, a particularly excellent injection-molded article is formed by injection molding a thermoplastic resin onto a trowel surface of a slag alloy member and combining it in a protruding state. Aluminum-resin composite of a resin molded body. Here, as for the thermoplastic resin used for producing the resin composite of the present invention, various thermoplastic resins may be used alone, and the physical properties required for the resin composite of the present invention are considered. For the thermoplastic resin, for example, a polypropylene resin, a polyethylene resin, an acrylonitrile-butadiene-styrene copolymer (ABS), or a polycarbonate resin (pc) is preferable. Poly-arylene resin, polyacetal resin, polyacetal resin, liquid crystalline resin, polyethylene terephthalate (pET) and poly(p-phenylene terephthalate), polyacetamide resin (PA), polythiobenzene (pps), etc. Polyester resin such as butyl phthalate (PBT), polyoxyalkylene based resin, polyfluorene 098145276 22 201035330 imine resin, benzophenone and a mixture of these thermoplastic resins In addition, in order to further improve the adhesion between the alloy member and the resin molded body, mechanical strength, heat resistance, dimensional stability (resistance to deformation, koji, etc.), electrical properties, etc., it is preferable to use these thermoplastic resins. Adding a filler of a fibrous form, a powdery form, a slab-shaped sacred temple, and various elastomer components is preferable as a filler added to the thermoplastic resin, and examples thereof include glass ray-forming fibers, metal fibers, and asbestos. Inorganic fiber filler such as fiber or boron fiber, and high-melting point organic fiber filler such as polyamine, fluororesin or acrylic resin, and quartz powder, glass beads, glass powder, calcium carbonate- ... A powdery filler such as a carcass or the like, and a plate-shaped filler such as a glass piece, a talc, and a mica sub-manufacturer, are preferably 250 parts by weight or less with respect to the thermoplastic resin 100. 2 parts by weight When the amount of the additive is more than 30 parts by weight, more preferably 30 parts by weight or more and 100 parts by weight or less, and the amount of the true charge is more than 250 parts by weight, the fluidity is lowered and the concave portion of the alloy member is entered. There is a problem that a good adhesion strength cannot be obtained or a mechanical property is lowered. In addition, examples of the elastomer component to be added to the thermoplastic resin include elastomers such as urethane ruthenium hydride, core-shell type, olefin type, polyester type, guanamine type, and styrene, and injection molding is considered. In the case of the melting temperature of the thermoplastic resin, etc., the amount of 'again' is preferably 30 parts by weight or less and preferably 25 parts by weight or less with respect to 100 parts by weight of the thermoplastic resin. 098145276 23 201035330 When the amount of the elastomer component added exceeds 3 , the strength is further improved, and mechanical properties are produced: the mixing effect of the phase-intimate component is used as the resin. This secret is particularly significant. ', ', ..., plasticity resin, and 'in the thermal grease used for the production of the lipid composite of the present invention, the additive which is added to the thermoplastic resin, that is, the flame retardant, can be appropriately added according to the required properties. , stabilizers, plasticizers, lubricating release agents, crystallization accelerators, crystal nucleating agents, etc. of dyes and pigment oxidants and ultraviolet absorbers. In the present invention, the injection molding of the heat-resistant (tetra) resin which is performed by attaching the hetero-alloy member to the mold for the injection handle can be carried out by the molding conditions required for the thermoplastic resin to be used, but it is important to smear during injection molding. The thermoplastic resin can surely enter the concave portion of the aluminum alloy member and cure 'better, setting the mold temperature and the cylinder temperature to the higher of the kind and physical properties of the thermoplastic resin, and the range allowed by the molding cycle, In particular, the temperature of the metal mold must be such that the lower limit temperature is 9 (TC or more, preferably 130 C or more). The upper limit is preferably from 100 ° C to the melting point or softening of the thermoplastic resin depending on the type of thermoplastic resin used. The point (in the case where the elastomer component is added is the higher or higher soft point or softening point) is lower than the temperature of about 2 ° C. Further, the lower limit of the mold temperature is preferably set to be less thermoplastic resin. The melting point is lower than 14 ° C. Further, the means for producing the aluminum-resin composite of the present invention is not limited to shot 098145276 24 201035330 A thermocompression bonding method may be employed, that is, the aluminum alloy member is heated in a range of about 90 ° C to 300 ° C and a resin member composed of a thermoplastic resin is applied to the surface thereof, and pressure is applied thereto. The desired aluminum-resin composite was obtained. [Examples] Example 1: [Preparation of A1 alloy test piece] ◎ Si: 11% by mass, Fe: 0.71% by mass, (: 11: 2.46% by mass, Μη) : 0.36 mass%, Mg: 0.29 mass%, Zn: 0.79 mass%, Ni: 0.72 mass% of the A1 alloy, and the melt 'casting and casting in a size of 180 mm x 150 mm x 3 mm. The setting conditions at this time are the mold temperature. · 17 ° ° C, melt temperature: 720 ° C, injection speed: 1.7 m / s, product filling time: 10 ms, average flow rate within the product: llm / s. In addition, the cooling rate during casting is 40 C / sec Ο From the prayers, cut out the A1 alloy sheet of size 37.5mm><37.5mmx3mm' and the slab surface of the A1 alloy sheet is smashed by 3mm from both sides to make a size of 37.5mmx37.5mmx2.4mm Ai alloy test piece. • Second, for the above A1 alloy test The etching solution prepared by adding 54 g/L of aluminum chloride hexahydrate to a 5 wt% hydrochloric acid solution was subjected to an etching treatment at 40 ° C for 10 minutes, followed by water washing, and a hot air of 12 Torr. Drying for 5 minutes, making the alloy parts. [Observation of the crystallization of the alloy components] 098145276 25 201035330 The surface of the obtained A1 alloy test piece, ❹ scan the standing m, s_45G") to observe 'observation ^ day fine Further, the amount of precipitation was measured by a gravimetric method. The size of the phase, the surface of the alloy member to be observed, is as shown in Fig. 3, and the convex portion is formed inside the concave portion formed on the surface. Further, the shape of the convex portion is also observed. Further, the crystal formed on the surface of the A1 alloy test piece was brushed with a brush. The collected crystal particles were measured by the weight method of the 曰/Z m PC film device. The average opening width and the total (10) crystal size and distribution of the concave portion observed in the surface of a certain region of the alloy member of the 疋之铭 alloy member, and the average opening width of the concave portion is 〇·1_ The above-mentioned "m" is equivalent to 〇·1/zm or more and 1 ()"m or less, and an energy dispersive X-ray analyzer (EMAX-7000 manufactured by Horiba, Ltd.) is used for the surface of the above-mentioned alloy member. The analysis of the edge of the map carried out the analysis of the elements of Shi Xi and the elements of the Ming Dynasty. As a result, only the distribution portion of the eutectic portion was 45%. Further, the amount of eutectic cerium precipitated on the surface of the aluminum alloy member is 0.001 g or more and 1 g or less per im square. Regarding the apparent crystal size, distribution, and amount of the precipitate, almost no change was observed even if the observation site was changed. [Shear failure load measurement test] The aluminum alloy member of Example 1 obtained as described above was attached to a metal mold of an injection molding machine (ST10R2V manufactured by NISSEI Co., Ltd.), and a polythiobenzene resin containing a filler of 098145276 26 201035330 ( Polyplastics PPS grade name 1140A6) is used as a thermoplastic resin with an injection time (including dwell time) of 5 seconds, an injection speed of 60 mm/sec, a holding pressure of 90 MPa, a forming temperature of 310 ° C, and a mold temperature of 18 〇. The forming conditions of t were injection-molded, as shown in Fig. 4, and the surface of the alloy member (6) having a size of 37.5 mm x 37.5 mm x 2.4 mm was fabricated to have a length of 15 mm x a thickness of 3 mm x a height of 6 mm and was adhered to the above A1 alloy test. Resin molded body (7) on the surface of the sheet - an aluminum-resin test piece (aluminum-resin composite) for the shear strength measurement test. Shear strength measurement test machine (made by Shimadzu Corporation: 1〇〇ΚΝ)

Autograph),如圖5所示般,於此試驗片固定用夾具⑻上, 將上述之剪切破壞加重測定試驗用鋁_樹脂試驗片以螺旋(9) 固定,由距黏合部〇. 1 m m之位置壓住並以夾具(1 〇)施加剪切 荷重’調查銘合金構件(6)與樹脂成形體(7)間之黏合部的剝 離狀怨。剝離形態係將在鋁合金構件(6)側上即使殘留一部 〇分樹脂之凝集破壞情況,視為良好(〇),更且,將樹脂在鋁 合金構件(6)側上相對於黏合面積為殘留7〇%以上之凝集破 壞情況,視為最良好(◎),又,將樹脂不殘留於鋁合金構件 側並且於黏合界面發生之情況,評估為不良(χ)時,結果為 最良好(@)>。 結果示於表1。 實施例2 : 由實施例1所製作之Α1合金壓鑄鑄物,切出尺寸 098145276 27 201035330 37.5mmx37.5mmx3mm之A1合金片,並對於此A1合金片, 僅單侧削面0.6mm,製作單面具有鑄肌面之尺寸 37,5mmx37.5mmx2.4mm的A1合金試驗片。對於此A1合金 試驗片的鑄肌面使用粒徑125〜149/zm之#100的氧化鋁微 粒子(組成;Al2〇3: 96.6wt%、Ti02 : 2.4wt%、Si02 : 0.6wt°/〇、 及其他)實施氣衝處理,使表面粗糙度值Rz值為5 後, 於在2wt%鹽酸溶液中添加了 54g/L之氣化鋁六水合物而調 製的蝕刻液中,施以4(TC浸潰15分鐘之蝕刻處理後、予以 水洗,並以12(TC之熱風乾燥5分鐘,製作鋁合金構件。 同實施例1進行銘纟*構件之石夕、结晶觀察時,所測定之銘 合金構件之某區域表面中觀察到的凹狀部的平均開口寬户 及内部突出析出之共晶雜晶的尺寸及其分佈,係凹狀部= 平均開口寬度為(U㈣以上且、㈣下,更且相當球粒 徑為以上且1G//m以下’且在共晶部分所存在 有Sl之分佈部位佔有55%。 又’紹合金構件表面所形成之共晶石夕析出量為每以 為0.001克以上,i克以下’關於突出 •V η /V « /、、、口 日日尺寸、 刀佈及份量,即使改變觀察處亦幾乎全部無變 接著’同上述實施例i處理,使用樹脂製作^ 試驗用之鋁-樹脂試驗片(鋁_樹脂複合體),並實扩疋 樹脂試驗片的剪切強度測定試驗,分別進行坪估施上述鋁-結果與實施例1之結果共同示於表1。 098145276 28 201035330 實施例3 : 由實施例i所製作之A1合金壓鑄鑄物,切出尺寸 37.5mmx37.5mmx3mm之A1合金片,並對於此…合金片, 僅單侧削面0.6mm,製作單面具有鑄肌面之尺寸 37,5mmx37.5mmx2.4inm的A1合金試驗片。對於此ai合金 試驗片的鑄肌面,於在2wt%鹽酸溶液中添加了 5勉几之氣 化!呂六水合物而調製之關液中,施以阶浸潰8分鐘之 〇敍翁理後、予财洗,並以12叱之熱風乾燥5分鐘,製 作鋁合金構件。 同實施例i進行銘合金構件之石夕結晶觀察時,所測定之紹 合金構件之某區域表面中觀察到之凹狀部的平均開口寬度 及内部突出析出之共晶雜晶的尺寸及其分佈,係凹狀部二 平均開口寬度為(U"m以上且3〇㈣以下,更且相當球粒 ❹ 徑為0.1 " m以上且1G“ m以下,且在共日日日部分所存在之僅 有Si之分佈部位估有30%。 又,銘合金構件表面所形成之共轉析出量為每^正方 為0.001克以上,1克以下,關於突出析 /、、'口日日尺丁 ' 分佈及份量’即使改魏察場所錢乎全部無變化。 接著,同上述實施例1處理,使用樹脂分別製作剪切強度 測定試驗用之鋁-樹脂試驗片(鋁_樹脂複合體),並實施上2 鋁-樹脂試驗片的剪切強度測定試驗,並且進行評估。 結果與實施例1之結果共同示於表1。 098145276 29 201035330 實施例4 : 除了將樹脂射出成形時的金屬模具溫度變更成吻。、 外,同上述實施例1進行處理,製作齡金構件,其次 上述實施例1進行處理,使用樹脂製作剪切強度測定試人同 之銘-樹脂試驗片,並實施剪切強度測定試驗,並進行驗用 結果與實施例1之結果共同示於表1。 估 實施例5 : 冋上迅貫; 〜u化杜,眾邗Ai令、金試驗片, a 於在5wt%硫酸溶液中添加了 5哪之氣化奸水人^欠’ 製之罐中’施以4吖浸潰8分鐘之姓刻處理=而調 洗,並以赃之熱風乾燥5分鐘,製作齡金予以水 同實施例1進行1呂合金構件之石夕結晶觀察時,所測定之冷 及内部突出析出之ί日到之凹狀部的平均開口寬度 ,、曰日矽結晶的尺寸及其分佈 平均開口寬度為(U"ma 且凹=的 徑為O.Mm以上且1〇// 下更且相當球粒 上且10/m以下’且在共晶部 僅有Si之分佈部位佔有35%。 中所存在之 又,銘合金構件表面所 為議克以上Μ克以下析出里為每lm正方 分佈及份㈣出切結晶尺寸、 Π 更改邊硯察處亦幾乎全部無 接著,同上述實施例p 測定試驗狀㉟樹^ 使㈣料作剪切強度 用之銘儀4驗片⑽-樹腊複合體)’並實施上述 098145276 30 201035330 鋁-樹脂試驗片的剪切強度測定試驗,並且予以評估。 結果與實施例1之結果共同示於表1。 實施例6 : 〇 同上述實⑽例1進行處理,製作A1合金試驗片,其文, 於在5wt%磷酸溶液中添加了 54机之氯化納六水合物^周 製之_液中’施卩贼浸漬10分鐘之關處理後予^ 洗’並以not:之熱風乾燥5分鐘,製倾合金構件。w 同實施例1進行銘合金構件之石夕結晶觀察時,所测定之銘 合金構件之某區域表面中觀察到之凹狀部的平均開口寬产 及内部突出析出之共㈣結晶的尺寸及其分佈,係、凹狀部= :均開口寬度為上且,瓜以下更且相當球粒 徑為0.1# m以上幻0"m以下,且在共晶部分 僅有Si之分佈部位佔有40%。Autograph), as shown in Fig. 5, on the test piece fixing jig (8), the above-mentioned aluminum-resin test piece for shear breaking and weighting test is fixed by a spiral (9), and is 1 mm from the adhesive portion. The position is pressed and the shear load is applied by the jig (1 〇) to investigate the peeling of the adhesive portion between the alloy member (6) and the resin molded body (7). The peeling form is considered to be good even if a part of the resin is left on the side of the aluminum alloy member (6), and the resin is on the side of the aluminum alloy member (6) with respect to the bonded area. In the case of agglomerated damage of 7 % by weight or more, it is considered to be the best ( ◎ ), and the resin does not remain on the side of the aluminum alloy member and occurs at the bonding interface. When the evaluation is poor (χ), the result is the best. (@)>. The results are shown in Table 1. Example 2: The Α1 alloy die-casting cast produced by Example 1 was cut out to form an A1 alloy sheet having a size of 098145276 27 201035330 37.5 mm x 37.5 mm x 3 mm, and the single-sided noodle was 0.6 mm on the A1 alloy sheet, and one side was produced. A1 alloy test piece having a size of 37, 5 mm x 37.5 mm x 2.4 mm of the cast muscle surface. For the cast muscle surface of this A1 alloy test piece, #100 alumina fine particles having a particle diameter of 125 to 149/zm were used (composition; Al2〇3: 96.6 wt%, Ti02: 2.4 wt%, SiO 2 : 0.6 wt ° / 〇, And other) performing an air blasting treatment, and after the surface roughness value Rz is 5, 4 (TC) is applied to an etching solution prepared by adding 54 g/L of vaporized aluminum hexahydrate to a 2 wt% hydrochloric acid solution. After immersing for 15 minutes, it was washed with water, and dried with hot air of 12 (TC for 5 minutes to prepare an aluminum alloy member. The same as in Example 1 was carried out on the stoneware of the member, and the crystal was observed. The average opening width of the concave portion observed in the surface of a certain portion of the member and the size and distribution of the eutectic crystals precipitated inside the concave portion are concave portions = the average opening width is (U (four) or more, and (four) lower, And the equivalent spherical particle size is above and below 1 G//m' and the distribution of S1 in the eutectic portion is 55%. The amount of eutectic precipitate formed on the surface of the alloy member is 0.001 g per liter. Above, i grams below 'About the highlights•V η /V « /,,, day size, knife cloth and The amount, even if the observation position is changed, is almost completely unchanged. Then, the aluminum-resin test piece (aluminum-resin composite) for the test is fabricated by using the resin, and the shear of the test piece is expanded. In the strength measurement test, the aluminum was evaluated and the results are shown in Table 1. Together with the results of Example 1, 098145276 28 201035330 Example 3: A1 alloy die-casting cast from Example i, cut out to a size of 37.5 mm x 37 .5mmx3mm A1 alloy sheet, and for this... alloy sheet, only one side of the face is 0.6mm, and a single-sided A1 alloy test piece having a cast muscle surface size of 37, 5mm x 37.5mm x 2.4inm is produced. For this ai alloy test piece Casting the muscle surface, in the 2wt% hydrochloric acid solution added 5 勉 several gasification! Lu Liu hydrate and prepared in the liquid, applied to the order of 8 minutes of 〇 翁 翁 翁 翁 翁 翁 翁 翁 翁 翁 翁 翁 翁 翁 翁 翁 翁 翁 翁 翁 翁 翁 翁 翁 翁 翁 翁 翁 翁 翁 翁The aluminum alloy member was produced by drying in a hot air of 12 Torr for 5 minutes. When the crystallization of the alloy member was observed in the same manner as in Example i, the average opening width of the concave portion observed in the surface of a certain portion of the alloy member was measured. And a total of internal precipitation The size and distribution of the crystallites are the average opening width of the concave portion 2 (U"m or more and 3〇(4) or less, and the equivalent spheroid diameter is 0.1 " m or more and 1G" m or less, and The distribution of only Si in the daily and daily parts is estimated to be 30%. In addition, the amount of co-rotation formed on the surface of the alloy member is 0.001 g or more per gram, less than 1 gram, about the prominent analysis / , 'Day and day ruler' distribution and weight 'even if the change to Weicha site money is all unchanged. Next, in the same manner as in the above-mentioned Example 1, an aluminum-resin test piece (aluminum-resin composite) for shear strength measurement test was prepared using a resin, and a shear strength measurement test of the upper 2 aluminum-resin test piece was carried out, and to evaluate. The results are shown together with the results of Example 1 in Table 1. 098145276 29 201035330 Example 4: The temperature of the mold at the time of injection molding of the resin was changed to a kiss. In addition, the same procedure as in the above Example 1 was carried out to prepare an ageing member, and then the above Example 1 was treated, and a shear strength measurement tester-in-resin test piece was prepared using a resin, and a shear strength measurement test was performed, and The results of the test were shown together with the results of Example 1 in Table 1. Estimate Example 5: 迅上迅; 〜uhuadu, Zhongyi Ai order, gold test piece, a added 5 in the 5wt% sulfuric acid solution, which is the gasification of the water After 4 minutes of dipping for 8 minutes, it was washed and dried by hot air for 5 minutes, and the age of gold was prepared and observed in the same manner as in Example 1 for the crystallization of the alloy. The average opening width of the concave portion of the cold and the inner protruding, the size of the 矽 矽 crystal and the average opening width of the distribution are (U"ma and the diameter of the concave = O.Mm or more and 1〇/ / Lower and quite spheroidal and below 10/m' and only 35% of the distribution of Si in the eutectic part. In the presence of the alloy, the surface of the alloy component is considered to be less than the above. The lm square distribution and parts (4) the cut crystal size, Π change the edge of the observation point, almost all without the same, the same as the above example p test test shape 35 tree ^ (4) material for the shear strength of the instrument 4 (10) - "Tree wax complex") and carry out the shear strength measurement test of the above-mentioned 098145276 30 201035330 aluminum-resin test piece, and Be assessed. The results are shown together with the results of Example 1 in Table 1. Example 6: The same procedure as in the above Example (10) was carried out to prepare an A1 alloy test piece, which was added to a 5 wt% phosphoric acid solution to add 54 machine sodium chloride hexahydrate. After the thief was immersed for 10 minutes, it was treated with a 'wash' and dried with a hot air of not: for 5 minutes to pour the alloy member. w When the crystallization of the alloy member of the alloy was observed in the same manner as in the first embodiment, the average opening width of the concave portion observed in the surface of a certain portion of the alloy member to be measured and the size of the total (4) crystal of the internal protrusion and the Distribution, system, concave portion =: The average opening width is above, and the ball diameter is more than 0.1# m or more below the melon, and only 40% of the distribution portion of Si in the eutectic portion is occupied.

又’銘合金構件表面所形成之共晶石夕析出量為每lm正方 為0.001克以上,i克以下,關於突出析出之石夕結晶尺寸、 分佈及份量,即使改變觀察處亦幾乎全部無變化°。阳 、接著,同上述實施m進行處理,使用樹料作剪切強度 測定試驗用之鋁-樹脂試驗片(鋁_樹脂複合體),並實施上述 鋁-樹脂試驗片的剪切強度測定試驗,並且 了 Μ評估。 結果與實施例1之結果共同示於表1。 實施例7 : 同上述實關1進行纽,㈣A1合錢料,其次 098145276 31 201035330 於在5wt%草酸溶液中添加了 5邮之氯化紹六水合物而調 製之關液中,施以5〇t浸潰2〇純之敍刻處理後予以水 洗並以120 C之熱風乾燥5分鐘,製作|呂合金構件。 同實施例1進行銘合金構件之石夕結晶觀察時,所測定之叙 合金構件之某區域表面中觀察到之凹狀部的平均開口寬度 及内4大出析出之共晶梦結晶的尺寸及其分佈,係凹狀部的 :句開口見度為O.l^m以上且3〇_以下,更且相當球粒 徑為0.1 # m以上且1 〇 "、 #以下,且在共晶部分中所存在之 僅有Si之分佈部位佔有3〇%。 又’銘合金構件表面所形成之共轉析出量為每Μ正方 為0.001克以上,1克以下 a# 曰 哥於犬出析出之矽結晶尺寸、 分佈及份1,即使改轡翻寂:忐 核察處亦幾乎全部無變化。 接者,同上述實施例丨進行 处里,使用樹脂製作剪切強度 /貝J疋忒驗用之鋁-樹脂試驗片 4g Η ή^-τ· 曰歿&體),並實施上述 鋁-¼月曰忒驗片的剪切強度 姓吳盘眘Μ ! 疋式驗,並且予以評估。 、、、。果與貫施例1之結果共同示於表i。 實施例8 : 同上述實施m進行處理 於5wt%鹽酸溶液中施以阶心主°金魏片,其次, 以水洗’並以12吖之熱風乾:二:分鐘之蝕刻處理後予 同實施例1進行叙合金構件之石夕Γ曰=作1呂合金構件。 合金構件之某區域表面中 、、°曰曰觀-時’所測定之鋁 中歲察到之凹狀部的平均開 098145276 見及 32 201035330 及内部突出析出之共晶矽結晶的尺寸及其分佈,係凹狀部的 平均開口寬度為0.1 /zm以上且30#m以下,更且相當球粒 徑為0.1 A m以上且10/zm以下,且在共晶部分中所存在之 僅有Si之分佈部位佔有40%。 又,鋁合金構件表面所形成之共晶矽析出量為每lm正方 為0.001克以上,1克以下,關於突出析出之矽結晶尺寸、 分佈及份量,即使改變觀察處亦幾乎全部無變化。 0 接著,同上述實施例1處理,使用樹脂製作剪切強度測定 試驗用之鋁-樹脂試驗片(鋁-樹脂複合體),並實施上述鋁-樹脂試驗片的剪切強度測定試驗,並且予以評估。 結果與實施例1之結果共同示於表1。 實施例9 : [A1合金試驗片之調製] 將含有Si: 11質量%、Fe: 0.71質量%、(:11: 2.46質量%、 Q Μη : 0.36 質量%、Mg : 0.29 質量%、Zn : 0.79 質量%、Ni : 0.72質量%之A1合金溶融液,以180mmx150mmxl.6mm之 尺寸進行壓鑄鑄入。另外,此時之設定條件為金屬模具溫 度:170°C、熔融液溫度:720°C、射出速度:1.7m/s、製品 填充時間:l〇ms、製品内平均流速:llm/s。另外,鑄造時 的冷卻速度為90°C/秒鐘。 由所得之鑄物,切出尺寸37.5mmx37.5mmxl.6mm的A1 合金片,並對此A1合金片,將鑄肌面由兩面各削面0.3mm, 098145276 33 201035330 製作尺寸37.5mmx37.5職χ1画的ai合金試驗片。 八人對於上述A1合金試驗片,於在5加%鹽酸溶液中添 加了 5填之氯化銘六水合物而調製之钱刻液中On the other hand, the amount of eutectic precipitate formed on the surface of the alloy member is 0.001 gram or more per lm square, below i gram, and the size, distribution, and amount of the crystal of the prominent precipitation are almost unchanged even if the observation is changed. °. Yang, followed by the above-mentioned treatment m, using a tree material as an aluminum-resin test piece (aluminum-resin composite) for shear strength measurement test, and performing a shear strength measurement test of the above-mentioned aluminum-resin test piece, And the evaluation. The results are shown together with the results of Example 1 in Table 1. Example 7: The above-mentioned real-time 1 is carried out, (4) A1 combined materials, and then 098145276 31 201035330 is added to 5% of the oxalic acid solution to add 5 chlorinated hexahydrate to the blister solution, and 5 施 is applied. After tipping 2 〇 pure etched, it was washed with water and dried with hot air of 120 C for 5 minutes to make a | When the crystallization of the alloy member was carried out in the same manner as in the first embodiment, the average opening width of the concave portion observed on the surface of a certain region of the alloy member and the size of the eutectic dream crystal which was precipitated within the four major portions and The distribution is concave: the opening of the sentence is above Ol^m and 3〇_, and the equivalent spherical particle size is 0.1 # m or more and 1 〇", #以下, and in the eutectic portion The only distribution of Si present is 3%. Moreover, the amount of co-rotation formed on the surface of the 'Metal alloy component is 0.001 g or more per square, and less than 1 g a# 曰 于 于 犬 犬 犬 犬 犬 犬 犬 犬 犬 犬 犬 犬 犬 犬 犬 犬 犬 犬 犬 犬 犬 犬 犬 犬 犬 犬 犬 犬 犬 犬 犬 犬 犬Almost all of the inspections remained unchanged. In the same manner as in the above embodiment, the aluminum-resin test piece 4g Η - - - - - - - - amp amp 使用 使用 使用 使用 使用 使用 使用 使用 使用 使用 铝 铝 铝 铝 铝 铝 铝 铝 铝 铝 铝 铝 铝 铝 铝 铝 铝 铝 铝 铝 铝 铝The shear strength of the 1⁄4 month test piece is surnamed Wu Panshen Μ 疋 test and evaluated. , ,,. The results are shown in Table i together with the results of Example 1. Example 8: Treatment with the above-mentioned embodiment m was carried out in a 5 wt% hydrochloric acid solution, and a step-centered gold-wet film was applied. Secondly, it was washed with water and dried with a hot air of 12 Torr: a two-minute etching treatment was given to the same example. 1 Conducting the alloy component of the stone Γ曰 Γ曰 = as a 1 Lu alloy component. The average opening of the concave portion observed in the aluminum of the surface of a certain part of the alloy member, 曰曰 - - 时 098 098 098 098 098 098 098 098 098 098 098 098 098 098 098 098 098 098 098 098 098 098 098 098 098 098 098 098 098 098 098 098 098 098 098 098 098 098 The average opening width of the concave portion is 0.1 /zm or more and 30#m or less, and the equivalent spherical particle diameter is 0.1 A m or more and 10/zm or less, and only Si is present in the eutectic portion. The distribution site accounts for 40%. Further, the amount of eutectic cerium precipitated on the surface of the aluminum alloy member was 0.001 g or more and 1 g or less per lm square, and the crystal size, distribution, and amount of the ruthenium which were precipitated were almost unchanged even when the observation was changed. 0. Next, in the same manner as in the above-mentioned Example 1, an aluminum-resin test piece (aluminum-resin composite) for shear strength measurement test was prepared using a resin, and the shear strength measurement test of the above-mentioned aluminum-resin test piece was carried out, and Evaluation. The results are shown together with the results of Example 1 in Table 1. Example 9: [Preparation of A1 alloy test piece] Si: 11% by mass, Fe: 0.71% by mass, (:11: 2.46% by mass, Q Μ η: 0.36% by mass, Mg: 0.29% by mass, Zn: 0.79) Mass A, Ni: 0.72% by mass of the A1 alloy molten solution was die-cast cast in a size of 180 mm x 150 mm x 1.6 mm. In addition, the setting conditions at this time were a mold temperature of 170 ° C, a melt temperature of 720 ° C, and injection. Speed: 1.7 m/s, product filling time: l〇ms, average flow rate in the product: llm/s. In addition, the cooling rate during casting was 90 ° C / sec. From the obtained casting, the size was cut out to 37.5 mm x 37 .5mmxl.6mm A1 alloy sheet, and for this A1 alloy sheet, the cast muscle surface is made of 0.3mm, 098145276 33 201035330 on both sides, and the ai alloy test piece with the size of 37.5mmx37.5 is used for 1 painting. Eight people for the above A1 The alloy test piece is prepared by adding 5 chlorinated hexahydrate to the 5% hydrochloric acid solution.

’施以40°C 浸潰7分鐘之㈣處賴予財洗,並以i2Q 5分鐘,製作鋁合金構件。 ”、、L钇爍 同實施例1進行銘合令错放 .金構件之矽結晶觀察時,所測定之鋁 合金構件之某區域表面中觀致5| 中硯察到之凹狀部的平均開口寬户 及内部突出析出之共晶矽結晶又 才及刀佈,係凹狀部的 榻見度為^以上且30⑽以下,更且相當球粒 徑為0.1心以上且1(^"下,且在共晶部 僅有Si之分佈部位佔有4〇〇/〇。 斤存在之 又,1呂合金構件表面所形成之共晶石夕析出量為每lm正方 為0.001克以上,1克町,關於突出析k料 分佈及份量,即使改變觀察處亦幾乎全部無變化”日尺寸、 接著,同上述實施m處理.,使用樹脂製作^切 試驗用之鋁-樹脂試驗片(鋁-樹脂複合體),、、7涟度則疋 樹脂試驗片的剪切強度測定試驗,並且予‘,上述銘-結果與實施例1之結果共同示於表丨。平估 實施例10 : [A1合金試驗片之調製] 將含有Si . 6.9質量〇/〇、Fe : 〇 38質 0 ' Mg : 〇 29 暂· | %、Cu ·· 0.01 質量%、Ni : 〇.〇1 質 呂 貝 1 、 1合金溶融液, 098145276 34 201035330 以180mmxl5〇mm><3.0mm之尺寸進行壓鑄鑄入。另外,此 時之設定條件為金屬模具溫度:17〇°c、熔融液溫度:720。(:、 射出速度:1.7m/s、製品填充時間:i〇ms、製品内平均流速: llm/s 另外,鑄造時的冷卻速度為4〇〇c/秒鐘。 由所得之鑄物,切出尺寸37.5mmx37 5mmx3mm的乂合 金片’並對此A1合金片,將鑄肌面由兩面各削面〇 3jnm, 製作尺寸37.5mmx37.5mmx2.4mm的A1合金試驗片。 ❸ 其次,對於上述A1合金試驗片,於在5wt%鹽酸溶液中添 加了 54g/L之氯化铭六水合物而調製之餘刻液中,施以 浸潰7分鐘之钱刻處理後予以水洗,並以12〇t>c之熱風乾燥 5分鐘’製作鋁合金構件。 时補1進行合金構件之㈣晶觀察時,所測定之紹 合金構件之某區域表面中觀察到之凹狀部的平均開口寬度 及内部突出析出之共晶雜晶的尺寸及其分佈,係凹狀部的 ❹平均開口寬度為0.1,以上13〇_以下,更且相當球粒 徑為O.^m以上且10_以下,且在共晶部分中所存在之 僅有Si之分佈部位佔有35〇/〇。 - 又’銘合金構件表面所形成之共晶石夕析出量為每lm正方 為0.001克以上,1克以下,關於突出析出之雜晶尺寸、 分佈及份量,即使改變觀察處亦幾乎全部無變化。 接者’同上述實施例i進行處理,使用樹脂製作剪切強度 測定試驗用之銘樹脂試驗片.樹脂複合體),並實施上述 098145276 35 201035330 I呂-樹脂試驗片的剪切強度測定試驗,並且予以評估。 結果與實施例1之結果共同示於表1。 實施例11 : 由實施例1所製作之A1合金壓鑄鑄物,切出尺寸 37.5mmx37.5mmx3.0mm之A1合金片,並對於此A1合金 片’將每肌面由兩面各削面〇.3mm,製作尺寸 37.5mmx37.5mmx2.4mm 的 A1 合金試驗片。 其-人’對於上述A1合金試驗片,於在2wt%鹽酸溶液中添 加了 54g/L之氣化鋁六水合物而調製之蝕刻液中,施以4〇它 浸潰35分鐘之蝕刻處理後予以水洗,並以12〇它之熱風乾 燥5分鐘,製作鋁合金構件。 同實施例1進行銘合金構件之石夕結晶觀察時,所测定之銘 合金構件之某區域表面中觀察到之凹狀部的平均開口 及内部突出析出之共晶傾晶的尺寸及其分佈,係立又 平均開口寬度為0.1/Zin以上且3〇//m以下,更且卷15的 徑為0.1# m以上幻〇"m以下,且在共晶部分田球粒 僅有Si之分佈部位佔有75%。 斤存在之 又,銘合金構件表面所形成之共砂析出 為〇._克以上,1克以下,關於突出析出切Z h正方 分佈及份量,即使改變觀察處亦幾乎全部晶尺寸、 接著’同上述實施们進行處理,使用樹。 測定試驗用之1呂-樹脂試驗片(銘-樹脂複合體)剪切強度 098145276 ’並實施上述 36 201035330 铭-樹脂試驗片的剪㈣度測定試驗,並对以評估。 結果與實施例1之結果共同示於表 實施例12 : 由實施例1所製作之A1合金㈣鑄物,切出尺寸 37.5mmx37.5mmx3.0mm之匐合金片,並對於此ai合金 片’將鑄肌面由兩面A 0 , 谷削面0.3mm,製作尺寸 37.5mmx37.5mmx2.4mm的八^式驗片'After 40 ° C, it was dipped for 7 minutes (4), and it was made to be washed, and an aluminum alloy member was produced by i2Q for 5 minutes. ", L 钇 同 同 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施 实施The eutectic crystals which are widely formed in the opening and the inside are only knives, and the visibility of the concave portion is ^ or more and 30 (10) or less, and the equivalent spherical particle size is 0.1 or more and 1 (^" In the eutectic portion, only the distribution portion of Si occupies 4 〇〇 / 〇. In the presence of jin, the eutectic precipitate formed on the surface of the 1 Lu alloy member is 0.001 g or more per lm square, 1 gram. Regarding the analysis of the distribution and the amount of the k-material, almost all of the observations were not changed. The daily size, and then the m treatment was carried out as described above, and the aluminum-resin test piece (aluminum-resin composite) for the test was made using the resin. The shear strength measurement test of the ruthenium resin test piece, and the results of the above-mentioned results are shown together with the results of Example 1. The evaluation example 10: [A1 alloy test The modulation of the film] will contain Si. 6.9 mass 〇 / 〇, Fe : 〇 38 mass 0 ' Mg : 〇 29 Temp. · %, Cu ······························································································· The setting conditions at this time are the mold temperature: 17 ° C, and the melt temperature: 720. (:, ejection speed: 1.7 m/s, product filling time: i 〇 ms, average flow rate in the product: llm / s The cooling rate at the time of casting was 4 〇〇c/sec. From the obtained cast, a bismuth alloy sheet having a size of 37.5 mm x 37 5 mm x 3 mm was cut out, and the A1 alloy sheet was made, and the cast muscle surface was cut from the sides by 3 jnm. A1 alloy test piece having a size of 37.5 mm x 37.5 mm x 2.4 mm. ❸ Next, in the above A1 alloy test piece, in a residual solution prepared by adding 54 g/L of chlorinated hexahydrate to a 5 wt% hydrochloric acid solution, After being treated by dipping for 7 minutes, it was washed with water and dried by hot air of 12 〇t>c for 5 minutes to make an aluminum alloy member. When the (four) crystal of the alloy member was observed, the measured alloy member was measured. The average opening width of the concave portion observed in the surface of a certain area and The size and distribution of the eutectic crystals which are prominently precipitated in the interior, the average opening width of the concave portion of the concave portion is 0.1, or more, 13 Å or less, and the equivalent spherical particle diameter is 0.5 m or more and 10 Å or less. The distribution of only Si in the eutectic portion occupies 35 〇 / 〇. - The amount of eutectic precipitate formed on the surface of the alloy member is 0.001 g or more per lm square, less than 1 gram. The size, distribution and amount of the precipitated crystals are prominently changed, and almost no change is observed even if the observation position is changed. The receiver was treated in the same manner as in the above Example i, and the resin test piece for the shear strength measurement test was used to form a resin composite. The shear strength measurement test of the above-mentioned 098145276 35 201035330 I-lu resin test piece was carried out. And to be assessed. The results are shown together with the results of Example 1 in Table 1. Example 11: The A1 alloy die-casting cast produced by Example 1 was cut out of an A1 alloy sheet having a size of 37.5 mm x 37.5 mm x 3.0 mm, and the surface of each of the A1 alloy sheets was cut by 3 mm from each side. An A1 alloy test piece having a size of 37.5 mm x 37.5 mm x 2.4 mm was produced. In the above-mentioned A1 alloy test piece, an etching solution prepared by adding 54 g/L of vaporized aluminum hexahydrate to a 2 wt% hydrochloric acid solution was subjected to an etching treatment of 4 Å and it was immersed for 35 minutes. It was washed with water and dried with a hot air of 12 Torr for 5 minutes to prepare an aluminum alloy member. In the same manner as in the first embodiment, the average opening of the concave portion and the size and distribution of the eutectic crystals precipitated inside the concave portion observed in the surface of a certain portion of the alloy member were measured. The average opening width of the system is 0.1/Zin or more and 3〇//m or less, and the diameter of the coil 15 is 0.1# m or more, and the distribution of the spherulites in the eutectic portion is only Si. The site accounts for 75%. In the presence of the pound, the co-sand precipitate formed on the surface of the alloy member is 〇._gram or more, less than 1 gram, and the square distribution and the amount of the cut Z h are prominently precipitated, even if the observation point is changed, almost all crystal sizes, then 'the same The above implementations process and use the tree. The test 1 ru-resin test piece (Ming-resin composite) shear strength 098145276 ′ was used and the above-mentioned 36 201035330 Ming-resin test piece shear test was performed and evaluated. The results are shown together with the results of Example 1 in Table Example 12: The A1 alloy (four) cast produced by Example 1 was cut out of a bismuth alloy sheet having a size of 37.5 mm x 37.5 mm x 3.0 mm, and the ai alloy sheet was The cast muscle surface is made up of two sides A 0 and a chamfered surface of 0.3 mm to make an eight-piece test piece with a size of 37.5 mm x 37.5 mm x 2.4 mm.

Ο 其次,對於上述A1合金詁私u > n 驗片,於在5wt%鹽酸溶液中添 加了 54g/L之氯化鋁六水合物 丄 i μ 0物而調製之蝕刻液中,施以40 °C浸潰2分鐘之蝕刻處理後予 故卞Μ水洗,並以丨別艽之熱風乾 燥5分鐘,製作鋁合金構件。 同實施例1進行鋁合金構件夕η 午之石夕結晶觀察時,所測定之鋁 合金構件之某區域表面中觀窣_ 丨士 規①到之凹狀部的平均開口寬度 及内部突出析料叫尺找其分佈,係凹狀部的 :均開口寬度為(U㈣以上且、m以下,更且相當球粒 徑為0.1#m以上且l〇//m以下,g + u ” 且在共晶部分中所存Ο Next, for the above-mentioned A1 alloy u u & n , , , , , , 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 在 40 40 40 40 40 40 40 40 40 40 40 40 40 40 40 40 40 40 40 40 40 40 40 After etching at ° C for 2 minutes, it was washed with water and dried by hot air for 5 minutes to prepare an aluminum alloy member. When the aluminum alloy member was observed in the same manner as in the first embodiment, the average opening width of the concave portion of the surface of the surface of the aluminum alloy member measured in the surface of the aluminum alloy member was measured. It is called the ruler to find its distribution, and the concave part is: the width of the opening is (U (four) or more, and m or less, and the equivalent spherical particle size is 0.1#m or more and l〇//m or less, g + u ” Stored in the crystal part

僅有Si之分佈部位佔有1〇%。 I 又,鋁合金構件表面所形成之共晶矽析出量為每1 為0.001克以上,1克以下,關於突出析出之石’、、、=曰lm正方 分佈及份量,即使改變觀察處亦幾乎全部無織化。日日尺寸、 接著,同上述實施例1進行處理,使用樹脂製作剪+ 測定試驗用之鋁-樹脂試驗片(鉈-樹脂複八 '強度 °體),並實施上述 098145276 37 201035330 銘-樹脂試驗片的剪切強度測定試驗,並且予以評估。 結果與實施例1之結果共同示於表1。 實施例13 : [A1合金試,檢片之調製] 將含有Si : 9.0質量%、:Fe : 〇 72質量%、Cu : 2.54質量 %、Mn : 0·36 質量%、Mg : 0.29 質量%、Zn : 0.71 質量%、 Nl:〇.69 質量%之 A1 合金熔融液,以 I80mmxl50mmx3.0mm 之尺寸進行壓鑄鑄入。另外,此時之設定條件為金屬模具溫 度:170°C、熔融液溫度:72(rc、射出速度:i.7m/s、製品 填充時間:l0ms、製品内平均流速:llm/s。另外,鑄造時 的冷卻速度為4CTC/秒鐘。 由所传之轉物’切出尺寸37.5mm><37.5mmx3mm的A1合 士此A1合金片’將缚肌面由兩面各削面〇.3min, 製作尺寸37.5mmx37 5mmx2 4jnm的A1合金試驗片。 人對於上述A1合金試驗片,於在5wt〇/〇鹽酸溶液中添 加了 54g/L之氣她六水合物而調製之姓刻液中Only the distribution of Si accounts for 1%. I, the amount of eutectic bismuth formed on the surface of the aluminum alloy member is 0.001 gram or more and 1 gram or less per 1 part, and the square distribution and the amount of the stone ', 、, 曰lm which are prominently precipitated, even if the observation point is changed, All are not woven. The daily size, and then the same as in the above-mentioned Example 1, the aluminum-resin test piece for the shear + measurement test was prepared using a resin, and the above-mentioned 098145276 37 201035330 Ming-resin test was carried out. The shear strength of the sheet was measured and evaluated. The results are shown together with the results of Example 1 in Table 1. Example 13: [A1 alloy test, preparation of test piece] Si: 9.0 mass%, :Fe: 〇72 mass%, Cu: 2.54 mass%, Mn: 0·36 mass%, Mg: 0.29 mass%, Zn: 0.71% by mass, Nl: 69.69% by mass of the A1 alloy melt, which was die-cast in a size of I80 mm x 150 mm x 3.0 mm. Further, the setting conditions at this time were a mold temperature of 170 ° C, a melt temperature of 72 (rc, an injection speed: i.7 m/s, a product filling time: 10 ms, and an average flow velocity in the product: llm/s. The cooling rate at the time of casting was 4 CTC/sec. From the transferred material 'cut size 37.5 mm> <37.5 mm x 3 mm A1 alloy A1 alloy sheet', the binding muscle surface was cut from both sides for 3 minutes. A1 alloy test piece with a size of 37.5mmx37 5mmx2 4jnm. For the above A1 alloy test piece, a surrogate was prepared by adding 54g/L of her hexahydrate to a 5wt〇/〇 hydrochloric acid solution.

,施以40°G 燥5分鐘’製作鋁合金構件。 同實施例1進行銘合金構件 浸潰Η)分鐘之關處理後予财洗,並以丨赃之熱風乾 之矽結晶觀察時,所測定之鋁The aluminum alloy member was produced by applying 40 °G for 5 minutes. In the same manner as in the first embodiment, the alloy of the alloy was immersed and immersed in a minute after the treatment, and the aluminum was measured by the crystallization of the hot air.

平均開口見度為以上且 的尺寸及其分佈,係凹狀部的 L 3〇em以下,更且相當球粒 098145276 38 201035330 徑為0.1 μ m以上且l〇" m以下,且在共晶部分中所存在之 僅有Si之分佈部位佔有4〇〇/。。 又,銘合金構件表面所形成之共晶石夕析出量為每lm正方 為0.001克以上’ 1克以下,關於突出析出之石夕結晶尺寸、 分佈及份量,即使改變觀察處亦幾乎全部無變化。 接著,同上述實施例1進行處理,使用樹脂製作剪切強度 測定試驗用之鋁-樹脂試驗片(鋁_樹脂複合體),並實施上述 〇 鋁·樹脂試驗片的剪切強度測定試驗,並且予以評估。 結果與實施例1之結果共同示於表1。 實施例14 : [A1合金試驗片之調製] 將含有Si : 9.0質量%、Fe : 〇 71質量%、Cu : 2 %質量 °/〇、Μη : 0.34 質量 %、Mg : 〇 29 質量%、Zn : 〇 69 質量%、 Νι . 〇,68質量%之A1合金熔融液,鑄入於銅製之JIS船型 Ο金屬杈具中,製作鑄物製品。另外,此時之設定條件為金屬 模具溫度:120°C、熔融液溫度:72〇乞。又,鑄造時的冷卻 速度為2.5 C/秒鐘。 由所得之鱗物製品,切出尺寸37.5mmx37.5mmx5mm的 A1合金片,並對此A1合金片,由兩面削面2.6mm,製作尺 寸 37.5mmx37.5mmx2.4mm 的 A1 合金試驗片。The average opening visibility is above and the size and distribution thereof are below the L 3 〇em of the concave portion, and the equivalent globule 098145276 38 201035330 has a diameter of 0.1 μm or more and l〇" m or less, and is in the eutectic The only Si distribution in the part is 4〇〇/. . In addition, the amount of eutectic precipitate formed on the surface of the alloy member is 0.001 g or more per lm, which is less than 1 g, and the crystal size, distribution, and amount of the precipitated crystal are almost unchanged even if the observation is changed. . Then, the aluminum-resin test piece (aluminum-resin composite) for shear strength measurement test was prepared by using the resin in the same manner as in the above-mentioned Example 1, and the shear strength measurement test of the above-described yttrium aluminum resin test piece was carried out, and To be assessed. The results are shown together with the results of Example 1 in Table 1. Example 14: [Preparation of A1 alloy test piece] Si: 9.0% by mass, Fe: 〇71% by mass, Cu: 2% by mass/〇, Μη: 0.34% by mass, Mg: 〇29% by mass, Zn : 〇69% by mass, Νι. 〇, 68% by mass of the A1 alloy melt, which was cast into a JIS ship-type enamel metal cookware made of copper to produce a cast product. Further, the setting conditions at this time were a mold temperature of 120 ° C and a melt temperature of 72 °. Further, the cooling rate at the time of casting was 2.5 C/sec. From the obtained scaly product, an A1 alloy piece having a size of 37.5 mm x 37.5 mm x 5 mm was cut out, and an A1 alloy test piece having a size of 37.5 mm x 37.5 mm x 2.4 mm was produced from the A1 alloy piece by 2.6 mm on both sides.

其次’對於上述A1合金試驗片,於在5wt%鹽酸溶液中添 加了 54g/L之氣化鋁六水合物而調製之蝕刻液中,施以4(TC 098145276 39 201035330 浸漬⑺分叙㈣處賴h核,如 燥5分鐘,製作鋁合金構件。 c之…几釭 八=Γ1進行銘合金構件之梦結晶觀察時,所測定之紹 區域表面中觀察到之凹狀部的平均開口寬度 ^析出之共晶⑪結晶的尺寸及其分佈,係凹狀部的 徑為。」…上且i。二:。=’更⑽ . 下且在,、晶部分中所存在之 僅有Si之分佈部位佔有。 又’銘,件表面所形成之共晶石夕析出量為每&正方 t以上,1克以下,關於突出析出之㈣晶尺寸、 /刀佈及伤1 ’即使改變觀察處亦幾乎全部無變化。 接著’同上述實施例!進行處理,使用樹脂製作剪切強度 測定試驗用之链-樹脂試驗片(銘_樹脂複合體),並實施上述 鋁-樹脂試驗片的剪切強度測定試驗,並且予以評估。 結果與實施例1之結果共同示於表j。 實施例15 : [A1合金試驗片之調製] 將含有Si : 9.0質量% ' Fe : 〇 71質量%、Cu : 2私質量 % > Μη : 0.34 ft% > Mg : 0.29 f *〇/〇 . Zn : 0.69 f *〇/〇 . Ni . 0.68貝里/〇之A1合金熔融液,鑄入於銅製之JIS船型 金屬松具中,製作鑄物製品。另外,此時之設定條件為金屬 模具溫度:350°C、熔融液溫度:720〇c。又,鑄造時的冷卻 098145276 40 201035330 速度為0.25°C/秒鐘。 由所得之禱物製品,切出尺寸37.5mmx37.5mm><5mm的 A1合金片’並對此A1合金片,由兩面削面2.6mm,製作尺 寸 37.5mmx37.5mmx2.4mm 的 A1 合金試驗片。 其次’對於上述A1合金試驗片’於在5wt%鹽酸溶液中添 加了 54g/L之氯化鋁六水合物而調製之蝕刻液中,施以4〇。〇 浸潰10分鐘之钱刻處理後予以水洗,並以12〇。(;之熱風乾 〇 燥5分鐘,製作鋁合金構件。 同實施例1進行紹合金構件之石夕結晶觀察時,所測定之在 合金構件之某區域表面中觀察到之凹狀部的平均開口寬^ 及内部突㈣k共Μ結W尺找其分佈,係凹狀部ό 平均開口寬度為0.1 # m以上且3〇 " m丨、,丁 川以111以下,更且相當球雄Next, for the above A1 alloy test piece, in an etching solution prepared by adding 54 g/L of vaporized aluminum hexahydrate to a 5 wt% hydrochloric acid solution, 4 (TC 098145276 39 201035330 impregnation (7) is divided (4) h core, such as drying for 5 minutes, to make aluminum alloy components. c... a few Γ Γ = Γ 1 When performing the dream crystal of the Ming alloy component, the average opening width of the concave portion observed in the surface of the measured area is determined. The size and distribution of the crystals of the eutectic crystal 11 are the diameters of the concave portions. "... and i. 2: . = 'more (10). Under and in the crystal portion, only the distribution of Si exists. Occupy. Also, the amount of eutectic precipitate formed on the surface of the part is equal to or greater than the square t, less than 1 gram, and the (4) crystal size, / knife cloth and wound 1 ' In the same manner as in the above-mentioned embodiment, the chain-resin test piece (inscription_resin composite) for shear strength measurement test was prepared using a resin, and the shear strength measurement of the above-mentioned aluminum-resin test piece was carried out. Test and evaluate it. The results of Example 1 are collectively shown in Table J. Example 15: [Preparation of A1 alloy test piece] Si was contained: 9.0% by mass of 'Fe: 〇71% by mass, Cu: 2 pp% > Μη: 0.34 ft % > Mg : 0.29 f *〇/〇. Zn : 0.69 f *〇/〇. Ni . 0.68 Berry/〇 A1 alloy melt, cast into copper JIS ship-type metal looser to make cast products In addition, the setting conditions at this time were a mold temperature of 350 ° C and a melt temperature of 720 ° C. Further, the cooling at the time of casting was 098145276 40 201035330 and the speed was 0.25 ° C / sec. An A1 alloy sheet having a size of 37.5 mm x 37.5 mm >< 5 mm was cut out, and an A1 alloy test piece having a size of 37.5 mm x 37.5 mm x 2.4 mm was produced from the A1 alloy sheet by 2.6 mm on both sides. Next, 'for the above A1 alloy test The sheet was applied to an etchant prepared by adding 54 g/L of aluminum chloride hexahydrate to a 5 wt% hydrochloric acid solution, and was subjected to a crucible for 10 minutes, washed with water, and washed with 12 〇. (;; The hot air is dried and dried for 5 minutes to make an aluminum alloy member. The stone of the alloy member is the same as in the embodiment 1. In the case of crystallization, the average opening width of the concave portion observed in the surface of a certain region of the alloy member and the internal protrusion (four) k total enthalpy knot were found to be distributed, and the average opening width of the concave portion was 0.1. #m以上和3〇" m丨,, Dingchuan is below 111, and is quite quite male

徑為0.1/zm以上且1〇am以下,θ力丛曰A 在/、日日部分中所存在3 僅有Si之分佈部位佔有45%。When the diameter is 0.1/zm or more and 1〇am or less, the distribution of the θ force cluster 曰A in the / day part is 35%, and only the distribution portion of Si is 45%.

G 又,鋁合金構件表面所形成之共晶矽析出量為每1正方 為0.001克以上,1克以下,關於突出析出之矽結曰1寸 分佈及份量,即使改變觀察處亦幾乎全部無變VQBa 、 接著,同上述實施例1進行處理,使 1之用树脂製作剪切強度 測定試驗用之銘-樹脂試驗片(鋁_樹脂禮人 ,Α σ體),並實施上述 I呂-樹脂式驗片的剪切強度測定試驗,拍 、予以評估。 結果與實施例1之結果共同示於表1。 實施例16 : 098145276 41 201035330 由貫施例1所製作之A1合金壓鑄鏵物,切出尺寸 37.5mmx37.5mmx3mm之A1合金片,並對於此A1合金片, 僅單側削面0.6mm,製作單面具有鑄肌面之尺寸 37.5mmx37.5mmx2.4mm的A1合金試驗片。對於此A1合金 試驗片的鑄肌面,使用粒徑1〇〇〜120^^之不銹鋼微粒子 (SUS304製)實施射擊喷擊處理,將表面粗糙度值Rz值作成 2 # m後’於在2wt%鹽酸溶液中添加了 54g/L之氯化鋁六水 合物而調製之蝕刻液中,施以4〇〇c浸漬15分鐘之蝕刻處理 後、予以水洗,並以12(TC之熱風乾燥5分鐘,製作鋁合金 構件。 同實施例1進行铭合金構件之石夕結晶觀察時,所測定之铭 合金構件之某區域表面中觀察到之凹狀部的平均開口寬度G. The amount of eutectic bismuth formed on the surface of the aluminum alloy member is 0.001 gram or more per 1 square, and 1 gram or less. Regarding the distribution and the amount of 矽 曰 突出 突出 突出 , , , , , , , , , , , , , , , , , 改变 改变VQBa, and then treated in the same manner as in the above-mentioned Example 1, and the resin for use in 1 was used to prepare a test piece for the shear strength measurement test-a resin test piece (aluminum resin, Α σ body), and the above-mentioned I-lu resin type was carried out. The shear strength measurement test of the test piece was taken and evaluated. The results are shown together with the results of Example 1 in Table 1. Example 16: 098145276 41 201035330 A1 alloy die-casting material prepared by the application example 1 was cut out, and an A1 alloy piece having a size of 37.5 mm×37.5 mm×3 mm was cut out, and a single side of the A1 alloy piece was cut by only 0.6 mm on one side. An A1 alloy test piece having a cast muscle surface size of 37.5 mm x 37.5 mm x 2.4 mm. For the cast muscle surface of the A1 alloy test piece, a stainless steel fine particle (manufactured by SUS304) having a particle diameter of 1 〇〇 to 120 ^^ was used for the shot blasting treatment, and the surface roughness value Rz was made to be 2 #m after 'at 2 wt. The etching solution prepared by adding 54 g/L of aluminum chloride hexahydrate to the hydrochloric acid solution was immersed in 4 ° C for 15 minutes, washed with water, and dried by hot air of 12 (TC for 5 minutes). The aluminum alloy member was produced. The average opening width of the concave portion observed in the surface of a certain region of the alloy member was measured in the same manner as in the first embodiment.

鋁-樹脂試驗片的剪切強度測定試驗, 並實施上述 ’分別予以評估。 098145276 42 201035330 結果與實施例1之結果共同示於表1。 實施例17 : 由實施例1所製作之A1合金壓鑄鑄物,切出尺寸 37,5mmx37.5mmx3mm之A1合金片,並對於此A1合金片, 僅單側削面0.6mm,製作單面具有鑄肌面之尺寸 37.5mmx37.5mmx2.4mm的A1合金試驗片。對於此A1合金 試驗片的鑄肌面’使用粒徑2000〜2378/zm之氧化鋁微粒子 ◎(組成;Α!2〇3 : 96.6wt%、Ti02 : 2.4wt%、Si〇2 : 0.6wt0/〇、 及其他)Μ把氣擊處理,將表面粗链度值Rz值作成5〇# m 後’於在2wt%鹽酸溶液中添加了 54g/L之氯化鋁六水合物 而調製之蝕刻液中,施以4〇。(:浸潰15分鐘之蝕刻處理後、 予以水洗,並以120T:之熱風乾燥5分鐘,製作鋁合金構件。 同實施例1進行鋁合金構件之矽結晶觀察時,所測定之鋁 合金構件之某區域表面中觀察到之凹狀部的平均開口寬度 〇 及内部突出析出之共晶矽結晶的尺寸及其分佈,係凹狀部的 +均開Π寬度為以上且30/zm以下’更且相當球粒 徑為0.1//m以上且10# m以下,且在共晶部分中所存在之 僅有Si之分佈部位佔有55%。 又,鋁合金構件表面所形成之共晶矽析出量為每正方 為0.001克以上,1克以下,關於突出析出之矽結晶尺寸、 分佈及份量,即使改變觀察處亦幾乎全部無變化 接著,同上述實施例1進行處理,使用樹脂製作剪切強度 098145276 43 201035330 測定試驗用之鋁-樹脂試驗片(鋁-樹脂複合體),並實施上述 鋁-樹脂試驗片的剪切強度測定試驗,分別予以評估。 結果與實施例1之結果共同示於表1。 [表1] 實施例 No. A1合金試驗片 樹脂成形 鋁-楨ί脂一體成形品 Si結晶 凹狀部 表面粗糙度 金屬模具 溫度 CC) 剪切強度測定試驗 相當球 粒徑 (_ 共晶Si 結晶分佈 (%) Si析出量 (咖2) 平均開 口寬度 (㈣ Rz (//m) 測定值 (Ν) 評估 1 5.1 45 0.44 15 — 180 890 ◎ 2 4.3 55 0.62 20 5 180 1328 ◎ 3 6.4 30 0.32 5 — 180 710 ◎ 4 5.5 40 0.40 14 — 160 850 ◎ 5 5.7 35 0.36 8 — 180 760 ◎ 6 4.9 40 0.36 10 — 180 780 ◎ 7 5.1 30 0.32 9 — 180 730 ◎ 8 4.4 40 0.38 12 — 180 812 ◎ 9 0.8 40 0.40 1 — 180 530 〇 10 2.1 35 0.38 8 — 180 740 ◎ 11 5.3 75 0.82 15 — 180 390 〇 12 4.8 10 0.01 9 — 180 423 〇 13 4.1 40 0.40 11 — 180 820 ◎ 14 8.2 40 0.51 22 — 180 550 〇 15 9.6 45 0.62 25 — 180 440 〇 16 4.5 50 0.40 5 2 180 780 ◎ 17 5.8 55 0.65 28 50 180 1250 ◎ 比較例1 : 由實施例1所製作之A1合金壓鑄鑄物,切出尺寸 37.5mmx37.5mm><3mm之A1合金片,並對於此A1合金片, 將鑄肌面由兩面各削面 0.3mm ,製作尺寸 37.5mmx37.5mmx2.4mm 的 A1 合金試驗片。 其次,對於上述A1合金試驗片,於30wt%鹽酸溶液之蝕 44 098145276 201035330 刻液中施以90 C次潰20分鐘之姓刻處理後予以水洗,並 以12(TC之熱風乾燥5分鐘,製作合金構件。 同實施例1進行銘合金構件之石夕結晶觀察時,所測定之銘 合金構件之某區域表面中觀察到之凹狀部的平均開口寬度 及内部突出析出之共晶砂結晶的尺寸及其分佈,係凹狀部的 ’平均開口寬度為超過30㈣,相當球粒徑為(U 以上且 10ym以下,且在共晶部分中所存在之僅有以之分佈部位 ζ)佔有 100%。 又,鋁合金構件表面所形成之共晶矽析出量為每lm正方 超過1克,關於突出析出之石夕結晶尺寸、分佈及份量,即使 改變觀察處亦幾乎全部無變化。 接著,同上述實施例1處理,使用樹脂製作剪切強度測定 試驗用之鋁·樹脂試驗片(鋁-樹脂複合體),並實施上述鋁_ 知于脂试驗片的為切強度測定試驗,並且予以評估。 ❹ 結果示於表2。 比較例2 : 由實施例1所製作之A1合金壓鑄鑄物,切出尺寸 - 37.5mmx37.5mmx3mm之A1合金片,並對於此A1合金片, ' 僅單側削面0.6mm,製作單面具有鑄肌面之尺寸 37.5mmx37.5mmx2.4mm的A1合金試驗片。對於此A1合金 試驗片的鑄肌面,使用粒徑125〜149# m之#100氧化紹微粒 子(組成;Al2〇3 : 96.6wt%、Ti〇2 : 2.4wt%、Si〇2 : 〇.6wt%、 098145276 45 201035330The shear strength measurement test of the aluminum-resin test piece was carried out and evaluated as described above. 098145276 42 201035330 The results are shown in Table 1 together with the results of Example 1. Example 17: The A1 alloy die-casting cast produced by Example 1 was cut out of an A1 alloy piece having a size of 37, 5 mm x 37.5 mm x 3 mm, and the A1 alloy piece was cut with only one side of 0.6 mm to produce a single-sided cast muscle. A1 alloy test piece with a face size of 37.5 mm x 37.5 mm x 2.4 mm. For the cast muscle surface of this A1 alloy test piece, alumina fine particles having a particle diameter of 2000 to 2378/zm were used (composition; Α! 2〇3: 96.6 wt%, Ti02: 2.4 wt%, Si〇2: 0.6 wt0/ 〇, and other) Μ 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气 气In the middle, 4 is applied. (: After immersing for 15 minutes, it was washed with water, and dried by hot air at 120T for 5 minutes to produce an aluminum alloy member. When the crystallization of the aluminum alloy member was observed in the same manner as in Example 1, the aluminum alloy member was measured. The average opening width 凹 of the concave portion observed in the surface of a certain region and the size and distribution of the eutectic cerium crystal precipitated from the internal protrusion are the same as the above-mentioned width of the concave portion and 30/zm or less. The spherical particle diameter is 0.1/m or more and 10# m or less, and only the distribution portion of Si existing in the eutectic portion accounts for 55%. Further, the amount of eutectic cerium precipitated on the surface of the aluminum alloy member is Each square is 0.001 g or more and 1 g or less. Regarding the crystal size, distribution, and amount of the precipitated precipitate, almost no change is observed even if the observation position is changed. Then, the same as in the above Example 1 is used, and the shear strength 098145276 is used. 201035330 The aluminum-resin test piece (aluminum-resin composite) for the test was measured, and the shear strength measurement test of the above-mentioned aluminum-resin test piece was carried out and evaluated separately. Results and results of Example 1 Commonly shown in Table 1. [Table 1] Example No. A1 alloy test piece resin-molded aluminum-桢 脂 fat integrally molded product Si crystal concave portion surface roughness metal mold temperature CC) shear strength measurement test equivalent spherical particle size (_ eutectic Si crystal distribution (%) Si precipitation amount (coffee 2) average opening width ((iv) Rz (//m) measured value (Ν) Evaluation 1 5.1 45 0.44 15 — 180 890 ◎ 2 4.3 55 0.62 20 5 180 1328 ◎ 3 6.4 30 0.32 5 — 180 710 ◎ 4 5.5 40 0.40 14 — 160 850 ◎ 5 5.7 35 0.36 8 — 180 760 ◎ 6 4.9 40 0.36 10 — 180 780 ◎ 7 5.1 30 0.32 9 — 180 730 ◎ 8 4.4 40 0.38 12 — 180 812 ◎ 9 0.8 40 0.40 1 — 180 530 〇10 2.1 35 0.38 8 — 180 740 ◎ 11 5.3 75 0.82 15 — 180 390 〇12 4.8 10 0.01 9 — 180 423 〇13 4.1 40 0.40 11 — 180 820 ◎ 14 8.2 40 0.51 22 — 180 550 〇 15 9.6 45 0.62 25 — 180 440 〇 16 4.5 50 0.40 5 2 180 780 ◎ 17 5.8 55 0.65 28 50 180 1250 ◎ Comparative Example 1: A1 alloy produced by Example 1 Die casting, cut out A1 alloy sheet with a size of 37.5mmx37.5mm><3mm, A1 for this alloy sheet, the cast of both sides of the muscle surface surfacing 0.3mm, making the size 37.5mmx37.5mmx2.4mm A1 alloy test piece. Next, the above-mentioned A1 alloy test piece was subjected to a 90 C-crush for 20 minutes in an etching solution of 30 wt% hydrochloric acid solution for 44 minutes, and then washed with water and dried by 12 (TC hot air for 5 minutes). In the same manner as in the first embodiment, the average opening width of the concave portion observed in the surface of a certain portion of the alloy member and the size of the eutectic sand crystal precipitated from the inner protrusion were observed in the same manner as in the first embodiment. And its distribution, the average opening width of the concave portion is more than 30 (four), and the equivalent spherical particle diameter is (above U and below 10 ym, and only the distribution portion 在 existing in the eutectic portion) occupies 100%. Further, the amount of eutectic cerium precipitated on the surface of the aluminum alloy member was more than 1 gram per lm square, and almost no change was observed in the crystal size, distribution, and amount of the precipitated crystals. In the treatment of Example 1, an aluminum/resin test piece (aluminum-resin composite) for shear strength measurement test was prepared using a resin, and the above-mentioned aluminum was known as a test piece for shear strength. The results are shown in Table 2. Comparative Example 2: A1 alloy die-casting cast produced in Example 1, cut out an A1 alloy sheet having a size of -37.5 mm x 37.5 mm x 3 mm, and for this A1 alloy sheet, ' An A1 alloy test piece having a casting surface of 37.5 mm x 37.5 mm x 2.4 mm on one side was produced with only one side of the faceted surface of 0.6 mm. For the cast muscle surface of the A1 alloy test piece, a particle size of 125 to 149 #m was used. Oxidized microparticles (composition; Al2〇3: 96.6wt%, Ti〇2: 2.4wt%, Si〇2: 〇.6wt%, 098145276 45 201035330

及其他齡轉處理後,對於上述A 酸溶液之蝕刻液中,施 β 。- 以水洗,如啊㈣乾;^ 6分叙侧處理後予 分鐘’製物合金構件。 。仃1#金構件切結晶觀察時,所測定之銘 …構k某區域表面中觀察到之凹狀 及内部突出析出之共晶石夕結 見度 平均開π Μ #尺寸及其^佈,係凹狀部的 一 又,、、。過3〇/Zm,相當球粒徑為0.1/zm以上且 10/zm以下,且在共晶部分 佔有麵。 +所存权财8!之分佈部位 又1呂合金構件表面所形成之共晶石夕析出量為每im正方 為超=克’關於突出析出切結晶尺寸、分佈及份量,即 使改變觀察處亦幾乎全部無變化。 接著,同上述實施例1進行處理,使用樹脂製作剪切強度 測定試則之㈣愧試驗片.樹脂複合體),並實施上述 銘_樹脂試驗片的剪切強度測定試驗,並且予以評估。 結果與比較例1之結果共同示於表2。 比較例3 : 由實施例1所製作之A1合金壓鑄鑄物,切出尺寸 37.5mmx37.5mmx3mm之A1合金片,並對於此…合金片, 僅單側削面0.6mm,製作單面具有鑄肌面之尺寸 37.5mmx37.5mmx2.4mm的A1合金試驗片。對於此八丨合金 試驗片的鑄肌面,於30wt%鹽酸溶液之蝕刻液中,施以9〇 098145276 46 201035330 °C浸潰10分鐘之蝕刻處理後予以水洗,並以120°c之熱風 乾燥5分鐘,製作鋁合金構件。 同實施例1進行鋁合金構件之矽結晶觀察時,所測定之鋁 合金構件之某區域表面中觀察到之凹狀部的平均開口寬度 及内部突出析出之共晶矽結晶的尺寸及其分佈,係凹狀部的 平均開口寬度為超過30/z m,相當球粒徑為0.1 // m以上且 10//m以下,且在共晶部分中所存在之僅有Si之分佈部位 0 佔有100%。 又,鋁合金構件表面所形成之共晶矽析出量為每lm正方 為超過1克,關於突出析出之矽結晶尺寸、分佈及份量,即 使改變觀察處亦幾乎全部無變化。 接著,同上述實施例1進行處理,使用樹脂製作剪切強度 測定試驗用之鋁-樹脂試驗片(鋁-樹脂複合體),並實施上述 鋁-樹脂試驗片的剪切強度測定試驗,並且予以評估。 〇 結果與比較例1之結果共同示於表2。 比較例4 : 由實施例1所製作之A1合金壓鑄鑄物,切出尺寸 37.5mmx37.5mmx3.0mm之A1合金片,並對於此A1合金 片,將鑄肌面由兩面各削面 0.3mm,製作尺寸 37.5mmx37.5mmx2.4mm 的 A1 合金試驗片。 接著,同上述實施例1進行處理,使用樹脂製作剪切強度 測定試驗用之鋁-樹脂試驗片(鋁-樹脂複合體),並且予以評 098145276 47 201035330 估。 結果不於表2。 比較例5 : 由實施例1所製作之A1合金壓鑄鑄物,切出尺寸 37.5mmx37.5mmx3mm之A1合金片,並對於此A1合金片, 僅單側削面0.6mm ’製作單面具有鑄肌面之尺寸 37.5mmx37.5mmx2.4mm的A1合金試驗片。對於此A1合金 試驗片的鑄肌面’使用粒徑125〜l49//m之#1〇〇氧化|呂微粒 子(組成;Al2〇3 : 96.6wt%、Ti02 : 2,4wt%、Si02 : 〇.6wt〇/0、 及其他)實施氣擊處理。 接著,同上述實施例1進行處理,使用樹脂製作剪切強度測 定試驗用之鋁-樹脂試驗片(鋁-樹脂複合體),並且予以評估。 結果與比較例1之結果共同示於表2。 比較例6 : 由實施例1所製作之A1合金壓鑄鑄物,切出尺寸 37.5mmx37.5mmx3.0mm之A1合金片’並對於此A1合金 片,將鑄肌面由兩面各削面〇 3mm,製作尺寸 37.5mmx37.5mmx2.4mm 的 A1 合金試。 其次,對於上述A1合金試驗片’以机之5感氯氧化 納溶液實施浸潰5分鐘之银刻處理後予以水洗,並以 之熱風乾燥5分鐘,製作紹合金構件。 #著,同上述實施例1進行處理’使用樹脂製作剪切強度 098145276 48 201035330 測定試驗用之銘-樹脂試驗片(|呂-樹脂複合體),並且予以坪 估0 結果示於表2。 比較例7 : [A1合金試驗片之調製] 將含有Si : 9.0質量%、Fe : 0.Ή質量%、Cu : 2.46質量 %、Μη : 0.34 質量%、:Mg : 0.29 質量%、Zn : 0.69 質量〇/0、 〇After the other ageing treatment, β is applied to the etching solution of the above A acid solution. - Wash with water, such as ah (four) dry; ^ 6 minutes after the treatment, give minutes to the alloy component. . When the 仃1# gold member is cut and crystallized, the measured eutectic is observed in the surface of a certain area and the eutectic precipitated in the inner protrusion is π Μ 尺寸 尺寸 尺寸 尺寸 尺寸 尺寸 尺寸 尺寸One of the concave portions, again, . After 3 〇/Zm, the equivalent spherical particle diameter is 0.1/zm or more and 10/zm or less, and the surface is occupied in the eutectic portion. + The distribution of the deposited powers 8! The eutectic formed by the surface of the 1 Lu alloy component is the amount of precipitation per im square. The size, distribution and amount of the cut crystal are prominently precipitated, even if the observation is changed. No change at all. Then, the same procedure as in the above Example 1 was carried out, and (4) ruthenium test piece (resin composite) of the shear strength measurement test was prepared using a resin, and the shear strength measurement test of the above-mentioned resin test piece was carried out and evaluated. The results are shown together with the results of Comparative Example 1 in Table 2. Comparative Example 3: From the A1 alloy die-casting cast produced in Example 1, an A1 alloy sheet having a size of 37.5 mm x 37.5 mm x 3 mm was cut out, and the alloy sheet was cut only 0.6 mm on one side, and the cast surface was produced on one side. A1 alloy test piece having a size of 37.5 mm x 37.5 mm x 2.4 mm. The cast muscle surface of the gossip alloy test piece was immersed in an etching solution of 30 wt% hydrochloric acid solution by immersion for 9 minutes at 9 〇 145 145 145 145 145 145 145 145 145 145 145 145 145 145 145 145 145 145 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 , , , After 5 minutes, an aluminum alloy member was produced. When the crystallization of the aluminum alloy member was observed in the same manner as in Example 1, the average opening width of the concave portion observed on the surface of a certain region of the aluminum alloy member measured, and the size and distribution of the eutectic crystallization crystal precipitated inside, The average opening width of the concave portion is more than 30/zm, the equivalent spherical particle diameter is 0.1 // m or more and 10//m or less, and only the distribution portion 0 of Si existing in the eutectic portion accounts for 100%. . Further, the amount of eutectic cerium precipitated on the surface of the aluminum alloy member was more than 1 gram per lm square, and the crystal size, distribution and amount of ruthenium which were precipitated were almost unchanged even when the observation was changed. Then, the aluminum-resin test piece (aluminum-resin composite) for shear strength measurement test was prepared by using the resin in the same manner as in the above-mentioned Example 1, and the shear strength measurement test of the above-mentioned aluminum-resin test piece was carried out. Evaluation. 〇 The results are shown in Table 2 together with the results of Comparative Example 1. Comparative Example 4: From the A1 alloy die-casting cast produced in Example 1, an A1 alloy sheet having a size of 37.5 mm x 37.5 mm x 3.0 mm was cut out, and the cast muscle surface was made of 0.3 mm on both sides of the A1 alloy sheet. A1 alloy test piece with a size of 37.5 mm x 37.5 mm x 2.4 mm. Subsequently, the same procedure as in the above Example 1 was carried out, and an aluminum-resin test piece (aluminum-resin composite) for the shear strength measurement test was prepared using a resin, and evaluated by 098145276 47 201035330. The results are not in Table 2. Comparative Example 5: From the A1 alloy die-casting cast produced in Example 1, an A1 alloy piece having a size of 37.5 mm x 37.5 mm x 3 mm was cut out, and the A1 alloy piece was only one side cut surface 0.6 mm. A1 alloy test piece having a size of 37.5 mm x 37.5 mm x 2.4 mm. For the cast muscle surface of this A1 alloy test piece, the particle size of 125~l49//m was used to oxidize|lubric microparticles (composition; Al2〇3: 96.6 wt%, Ti02: 2, 4 wt%, SiO 2 : 〇 .6wt〇/0, and others) implement air hammer treatment. Next, the same procedure as in the above Example 1 was carried out, and an aluminum-resin test piece (aluminum-resin composite) for shear strength measurement test was prepared using a resin and evaluated. The results are shown together with the results of Comparative Example 1 in Table 2. Comparative Example 6: An A1 alloy die-cast product produced in Example 1 was cut out, and an A1 alloy sheet having a size of 37.5 mm x 37.5 mm x 3.0 mm was cut out. For this A1 alloy sheet, the cast muscle surface was cut from the both sides by 3 mm. A1 alloy test with dimensions of 37.5mm x 37.5mm x 2.4mm. Next, the above-mentioned A1 alloy test piece was subjected to silver etching for 5 minutes of immersion in a kinetic chlorination solution, and then washed with hot air and dried by hot air for 5 minutes to prepare a sinter alloy member. #着,进行处理进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行进行Comparative Example 7: [Preparation of A1 alloy test piece] Si: 9.0% by mass, Fe: 0.1% by mass, Cu: 2.46% by mass, Μη: 0.34% by mass, Mg: 0.29% by mass, Zn: 0.69 Quality 〇/0, 〇

Νι : 0.68質量%之A1合金熔融液,鑄入於使用貝殼砂之砂 型鑄造中’製作尺寸4〇mmx2〇〇mmx60mm的鑄物製品。另 外’此時之設定條件為熔融液溫度:72〇。(:。又,鑄造時的 冷卻速度為0.045°C/秒鐘。 由所传之每物製品’切出尺寸37.5mmx37.5nimx5mm的 A1合金片,並對此μ合金片,由兩面削面2 6mm,製作尺 寸 37.51^^37.5111111><2.4111111的八1 合金試驗片。 八一乂對於上述A1合金試驗片,於在10wt%鹽酸溶液中 添加了 54g/L之氣化銘六水合物而調製之独刻液中,施以 4〇C_ 1G分鐘之侧處理後料水洗,並以丨撕之熱 風乾燥5分鐘,製作鋁合金構件。 · 同只施例1進仃銘合金構件之石夕結晶觀察時,所測定之铭 口金構件之某區域表面中觀察到之凹狀部的平均開口寬度 更且相當球粒徑為超過10 及内4大出析出之共㈣結晶的尺寸及其分佈,係凹狀部的 平均開口寬度為超過30# m, 098145276 49 201035330 ,且在共晶部分中所存在之僅有 50%。Νι : 0.68 mass% of the A1 alloy melt was cast into a sand casting using shell sand to make a casting product having a size of 4 mm x 2 mm x 60 mm. Further, the setting conditions at this time were the melt temperature: 72 Torr. (:. Further, the cooling rate at the time of casting was 0.045 ° C / sec. The A1 alloy piece having a size of 37.5 mm x 37.5 nm x 5 mm was cut out from each of the products passed, and the μ alloy piece was cut by two sides of 2 μmm. , an eight-first alloy test piece having a size of 37.51^^37.5111111><2.4111111 was produced. Bayi's test piece for the above A1 alloy was prepared by adding 54 g/L of gasification hexahydrate to a 10 wt% hydrochloric acid solution. In the original solution, the side is treated with 4〇C_1G minutes, washed with water, and dried with hot air for 5 minutes to make aluminum alloy members. · The same example 1 is used in the composition of the alloy. When observed, the average opening width of the concave portion observed in the surface of a certain area of the gold component of the ingot is more than the size and distribution of the total (4) crystals of the larger spherical particle size exceeding 10 and the inner 4 The average opening width of the concave portion is more than 30 # m, 098145276 49 201035330, and only 50% is present in the eutectic portion.

Si <分佈部位佔有 又,鋁合金構件表面所形成之共晶矽 .Λ ΛΛ1 ^ )V , 1山 丨:為每lm正方 為0.001克以上,1克以下,關於突出 m 、乡士晶尺^寸、 分佈及份量,即使改變觀察處亦幾乎全部無料m 上述實,例1進行處理’使用樹:二。剪切強度 測定试驗用之鋁-樹脂試驗片(鋁_樹脂複人 、 、 口遐),並實施上述 鋁-樹脂試驗片的剪切強度測定試驗,祐 十且予以評估。 結果示於表2。 比較例8 : [A1合金試驗片之調製] 將含有化11質量%,:0.71質量%,:2 46質量%、 Μη : 0.36 質量%、Mg : 〇.29 質量%、〜:〇 79 質量%、见: 0.72質量%之A1合金賴液,以噴霧法製作合金粉末後, 進行冷軋、燒結’並以熱擠出製作尺寸9〇0、2〇〇麵的擠 出製品。另外,以噴霧法製作合金粉末時的冷卻速度為 300°C/秒鐘。 由所得之擠出製品,切出尺寸37.5mmx37 5mmx3_的 A1合金片,並對此A1合金片,將鑄肌面由兩個各削面 0.3mm ’製作尺寸37.5mmx37.5mmx2.4mm的A1合金試驗 其次’對於上述A1合金試驗片,於在10wt〇/o鹽酸溶液中 098145276 50 201035330 添加了 54g/L之氯化銘六水合物而調製之I虫刻液中,施以 40°C浸潰1〇分鐘之蝕刻處理後予以水洗,並以120°C之熱 風乾燥5分鐘,製作鋁合金構件。 同實施例1進行鋁合金構件之矽結晶觀察時,所測定之鋁 ^ 合金構件之某區域表面中觀察到之凹狀部的平均開口寬度 ' 及内部突出析出之共晶矽結晶的尺寸及其分佈,係凹狀部的 平均開口寬度為未滿0.1 "m,更且相當球粒徑為未滿0.1 f) ,且在共晶部分中所存在之僅有Si之分佈部位佔有 40%。 又,鋁合金構件表面所形成之共晶矽析出量為每lm正方 為0.001克以上,1克以下,關於突出析出之矽結晶尺寸、 分佈及份量,即使改變觀察處亦幾乎全部無變化。 接著,同上述實施例1進行處理,使用樹脂製作剪切強度 測定試驗用之铭-樹脂試驗片(銘-樹脂複合體),並實施上述 ◎ 鋁-樹脂試驗片的剪切強度測定試驗,並且予以評估。 結果示於表2。 098145276 51 201035330 [表2]Si < distribution part possesses, the eutectic 形成.Λ ^1 ^ )V formed on the surface of the aluminum alloy member, 1 hawthorn: 0.001 g or more per lm square, less than 1 gram, about the prominent m, the township crystal ruler ^ inch, distribution and weight, even if you change the observation point, almost all of the above m, the actual case, the case 1 is processed 'use tree: two. Shear strength The aluminum-resin test piece (aluminum-resin compound, sputum) for the test was measured, and the shear strength measurement test of the above-mentioned aluminum-resin test piece was carried out, and it was evaluated. The results are shown in Table 2. Comparative Example 8: [Preparation of A1 alloy test piece] 11% by mass, 0.71% by mass, 2% by mass, Μη: 0.36 mass%, Mg: 29.29 mass%, and 〇79 mass% See: 0.72% by mass of A1 alloy lysate, after alloying powder by spray method, cold rolling and sintering are performed, and extruded products having a size of 9〇0 and 2〇〇 are prepared by hot extrusion. Further, the cooling rate at the time of producing the alloy powder by the spray method was 300 ° C / sec. From the obtained extruded product, an A1 alloy piece having a size of 37.5 mm x 37 5 mm x 3 _ was cut out, and for the A1 alloy piece, the A1 alloy of the size of 37.5 mm x 37.5 mm x 2.4 mm was made from two different faces of 0.3 mm '. Next, 'For the above A1 alloy test piece, in the 10 〇 〇 / o hydrochloric acid solution 098145276 50 201035330 added 54g / L of chlorinated hexahydrate prepared in the I insect engraving, applied 40 ° C impregnation 1 After 蚀刻 minutes of etching treatment, it was washed with water and dried by hot air at 120 ° C for 5 minutes to prepare an aluminum alloy member. When the crystallization of the aluminum alloy member was observed in the same manner as in Example 1, the average opening width of the concave portion observed in the surface of a certain region of the aluminum alloy member and the size of the eutectic crystal precipitated by the internal protrusion and The distribution, the average opening width of the concave portion is less than 0.1 " m, and the equivalent spherical particle size is less than 0.1 f), and the only Si distribution portion present in the eutectic portion accounts for 40%. Further, the amount of eutectic cerium precipitated on the surface of the aluminum alloy member was 0.001 g or more and 1 g or less per lm square, and the crystal size, distribution, and amount of the ruthenium which were precipitated were almost unchanged even when the observation was changed. Then, the same procedure as in the above Example 1 was carried out, and a resin-test piece (Ming-resin composite) for shear strength measurement test was produced using a resin, and the shear strength measurement test of the above-mentioned ◎ aluminum-resin test piece was carried out, and To be assessed. The results are shown in Table 2. 098145276 51 201035330 [Table 2]

比車交例 No. A1合金試驗片 樹脂成形 鋁-樹脂一體成形品 Si結晶 凹狀部 表面粗 金屬模具 溫度 CC) 剪切強度測定試驗 相當球 粒徑 (um) 共晶Si 結晶分佈 (%) Si析埠量 (^n?) 平均開 口寬度 (um) Rz (//m) 測定值 (N) 評估 1 5.5 100 3.22 55 — 180 X 2 4.3 100 1.18 35 5 180 俊1) X 3 4.8 100 2.34 40 — 180 X 4 — — 0 — — 180 X 5 — — 0 — 5 180 85 X 6 — — 0 — — 180 _ X 7 18.5 50 0.50 32 — 180 53 X 8 0.01 40 0.40 0.05 — 180 42 X ※1)因為未黏合,故無法實施剪切強度試驗。 【圖式簡單說明】 圖1為說明Al-Si系合金鑄物之凝固組織的示意圖。 圖2為說明Al-Si系合金鑄物於蝕刻後之剖面組織的示意 圖。 圖3係以掃描電子顯微鏡觀察Al-Si系合金鑄物之蝕刻表 面的晝面。 圖4為說明用以測定鋁-樹脂複合體之剪切強度的試驗片 形狀圖。 圖5為鋁-樹脂試驗片之剪切強度測定試驗方法的說明 圖。 【主要元件符號說明】 1 初晶(2 -A1 098145276 52 201035330 2 Al-Si共晶部 3 共晶¢2 -A1 4 共晶Si 5 空隙部 6 鋁合金構件 7 樹脂成形體 8 固定用央具 9 螺栓 10 夾具 098145276 53Example No. A1 alloy test piece resin molding aluminum-resin integrally molded product Si crystal concave portion surface rough metal mold temperature CC) Shear strength measurement test equivalent spherical particle size (um) eutectic Si crystal distribution (%) Si enthalpy (^n?) Average opening width (um) Rz (//m) Measured value (N) Evaluation 1 5.5 100 3.22 55 — 180 X 2 4.3 100 1.18 35 5 180 Jun 1) X 3 4.8 100 2.34 40 — 180 X 4 — — 0 — — 180 X 5 — — 0 — 5 180 85 X 6 — — 0 — — 180 _ X 7 18.5 50 0.50 32 — 180 53 X 8 0.01 40 0.40 0.05 — 180 42 X ※1 Because the adhesive is not bonded, the shear strength test cannot be performed. BRIEF DESCRIPTION OF THE DRAWINGS Fig. 1 is a schematic view showing the solidification structure of an Al-Si alloy casting. Fig. 2 is a schematic view showing the cross-sectional structure of an Al-Si alloy cast after etching. Fig. 3 is a view showing the surface of the etched surface of the Al-Si alloy cast by a scanning electron microscope. Fig. 4 is a view showing the shape of a test piece for measuring the shear strength of the aluminum-resin composite. Fig. 5 is an explanatory view showing a test method for measuring the shear strength of an aluminum-resin test piece. [Description of main component symbols] 1 Primary crystal (2 -A1 098145276 52 201035330 2 Al-Si eutectic part 3 eutectic ¢ 2 -A1 4 eutectic Si 5 void part 6 aluminum alloy member 7 resin molded body 8 fixed centering device 9 bolt 10 fixture 098145276 53

Claims (1)

201035330 七、申请專利範圍: 種树月曰黏合性優異之銘合金構件,係於-部分表面或 全面具有複數個凹狀部的A1_Si系銘合金構件,該凹狀部係 在内面_有複數個由共晶石夕結晶所構成之凸部且平均開口 寬,為0.1//m以上且3〇以功以下,其特徵為,上述共晶矽 、、·《斤構成之凸。卩’係具有相當球粒徑為Q # m以上且 /zm以下之尺寸。 2·如申明專利_第卜項之樹絲合性優異之銘合金構 # 射線之賴分析進行%元素及銘元 素刀析日夺在共晶部分中所存在之僅有石夕的分佈部位佔有 5%以上且80%以下。 5胃專利範圍第丨或2項之樹脂黏合性優異之铭合金 構件’其中’上述由共晶石夕結晶所構成之凸部,係在上述凹 狀部内面以〇.〇〇lg/m2以J 上且1g/m以下之份量突出、析出。 4. 一種樹脂黏合性優異 第…項,任一項之銘合:::構體二:二請專利範圍 在複數個不具有上述共料結晶之凸部且^為,亦同時存 0.1 Am以上且3〇#m以下的凹狀部。 句開口寬度為 5.—種鋁合金,係構成申請專利範圚 之樹脂黏合性優異之鋁合金構件者,1至4項中任一項 5.0質量。/。以上且18質量%以下、.其特徵為,含有Si: 5.0質量%以下、Mg: ! 5質量%以下I’3資量%以下、Cu : 098145276 冲·】.5質量%以下, 54 201035330 組 且殘餘部分具有A1以及㈣可避免雜質所構成之成分 6. 一種樹脂黏合性優異之齡金構件之製造方法, 有申請專_圍第5狀成錄叙衫缝融液進行缚 造而製造銘合金構件的方法,其特徵為,在鑄造時之北曰 S!凝固溫度為7饥以上且彻。c以下之領域中,冷卻速^ 為o.rc/秒鐘以上且10(rc/秒鐘以下。 又 Ο 〇 \如申請專利第6項讀轉合㈣異種合金構件 之製造方法,其中,將已鑄造的鑄物體整形成指定形狀、尺 寸後,對表面以酸系液施行化學蝕刻處理。 8二申請專利範圍第7項之樹脂黏合性優異之銘合金構件 之裝=方法’射’在對表面峨系液施行化學綱處理之 處理前,預先賦予表面粗輪度尺2值為卜刚㈣的凹凸。 9=申請專利簡第8項之樹絲合性優異之銘合金構件 之製造方法’其中,具有表面粗链度Rz值為1〜之 凹凸的表面紅由使用氧化㉟微粒子或金屬微粒子之任一 者或兩者微粒子之喷擊處理所形成。 098145276 55 %201035330 VII. Patent application scope: The alloy component with excellent adhesion to the tree planting is attached to the A1_Si series alloy member with a plurality of concave portions on the surface or in part, and the concave portion is on the inner surface _ there are a plurality of The convex portion composed of the eutectic crystals has an average opening width of 0.1/m or more and 3 Å or less, and is characterized in that the eutectic enthalpy is formed. The 卩' series has a size in which the spherical particle diameter is Q #m or more and /zm or less. 2. For example, if the patent is _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5% or more and 80% or less. (5) The alloy part of the third or second item of the patent of the stomach is excellent in the adhesiveness of the resin. The above-mentioned convex portion composed of the eutectic crystal is formed on the inner surface of the concave portion by 〇.〇〇lg/m2. The amount of J and below 1 g/m is prominent and precipitated. 4. An excellent resin adhesion... Item: Any one of the following:::Structure 2: The scope of the patent is in a plurality of convex parts that do not have the above-mentioned compositing crystals, and ^ is also present at the same time. And 3〇 below the concave part of #m. The opening width of the sentence is 5. - A kind of aluminum alloy, which is an aluminum alloy member which is excellent in resin adhesion of the patent application, and one of the items 1 to 4 is 5.0 mass. /. The above is 18% by mass or less, and is characterized by containing Si: 5.0% by mass or less, Mg: 5% by mass or less, I'3% by weight or less, Cu: 098,145,276, 5%, and 5% by mass, 54 201035330 And the residual portion has A1 and (4) a component which can avoid impurities. 6. A method for producing a gold member having excellent resin adhesion, and the application of the special _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ A method of alloying members, characterized in that the solidification temperature of the north 曰S! at the time of casting is 7 hunger and more. In the following fields, the cooling rate ^ is o.rc/sec or more and 10 (rc/sec or less. Also Ο 〇\, as in Patent Application No. 6, read and turn (4) manufacturing method of dissimilar alloy members, among which After the cast object has been formed into a specified shape and size, the surface is chemically etched with an acid solution. The application of the alloy of the alloy with the excellent adhesion of the resin in the seventh paragraph of the patent application is as follows: Before the surface lanthanum solution is subjected to the treatment of the chemical treatment, the surface roughness of the surface is given to the surface roughness of the second step (4). 9 = The manufacturing method of the alloy member having excellent yarn affinity of the eighth item of the patent application' Among them, the surface red having the surface roughness Rz value of 1 to the unevenness is formed by the blasting treatment using either of the oxidized 35 fine particles or the metal fine particles or both of the fine particles. 098145276 55 %
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