JPS63145756A - Treatment of aluminum alloy surface - Google Patents
Treatment of aluminum alloy surfaceInfo
- Publication number
- JPS63145756A JPS63145756A JP29195786A JP29195786A JPS63145756A JP S63145756 A JPS63145756 A JP S63145756A JP 29195786 A JP29195786 A JP 29195786A JP 29195786 A JP29195786 A JP 29195786A JP S63145756 A JPS63145756 A JP S63145756A
- Authority
- JP
- Japan
- Prior art keywords
- aluminum alloy
- diameter
- recesses
- alloy stock
- depth
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 23
- 239000000956 alloy Substances 0.000 claims description 13
- 238000000034 method Methods 0.000 claims description 7
- 238000002844 melting Methods 0.000 claims 1
- 230000008018 melting Effects 0.000 claims 1
- 238000001816 cooling Methods 0.000 abstract description 3
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 abstract 1
- 229910052721 tungsten Inorganic materials 0.000 abstract 1
- 239000010937 tungsten Substances 0.000 abstract 1
- 239000011324 bead Substances 0.000 description 5
- 238000005520 cutting process Methods 0.000 description 4
- 238000004381 surface treatment Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 238000010521 absorption reaction Methods 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 230000005496 eutectics Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000007670 refining Methods 0.000 description 1
- 230000003746 surface roughness Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Abstract
Description
【発明の詳細な説明】 (産業上の利用分野) 本発明はアルミ合金表面の処理方法の改良に関する。[Detailed description of the invention] (Industrial application field) The present invention relates to an improvement in a method for treating the surface of an aluminum alloy.
(従来技術とその問題点)
一般に、例えば自動車用エンジンにおいては、高出力化
、低燃費化が追求されており、そのため、燃焼室内の温
度は上昇傾向にある。(Prior art and its problems) Generally, for example, in automobile engines, higher output and lower fuel consumption are pursued, and therefore the temperature in the combustion chamber tends to rise.
このため、アルミ合金製シリンダヘッドのバルブブリッ
ジ部等の熱負荷はより厳しくなり、従来の低圧鋳造シリ
ンダヘッドではバルブブリッジ部にクラック等が発生し
、水漏れ等が発生するという問題があった。For this reason, the thermal load on the valve bridge portion of the aluminum alloy cylinder head becomes more severe, and in conventional low-pressure casting cylinder heads, cracks and the like occur in the valve bridge portion, causing problems such as water leakage.
そこで、この対策として、第2図(a)のように、アル
ミ合金素材(バルブブリッジ)lの表面(上部)Iaを
、第2図(b)のように、TIGアーク等で再溶融して
表面組織を微細化し、ついで、第2図(c)のように冷
却した後、第2図(d)のように、この表面1aを所定
の高さhoで切削加工することにより、耐熱疲労特性を
向上させろことかできる方法が提案されている(特公昭
61−36566号公報参照)。Therefore, as a countermeasure to this problem, as shown in Fig. 2 (a), the surface (upper part) Ia of the aluminum alloy material (valve bridge) l is remelted using a TIG arc, etc., as shown in Fig. 2 (b). After refining the surface structure and cooling it as shown in FIG. 2(c), this surface 1a is cut at a predetermined height ho as shown in FIG. 2(d), thereby improving thermal fatigue resistance. A method has been proposed to improve this (see Japanese Patent Publication No. 61-36566).
しかしながら、上記従来の表面処理方法では、微細化部
tbの幅W°が狭く、かつ深さく1’ら浅いらのであり
、幅を広く、かつ深い微細化部1bを確保しようとした
場合には、TIGアーク、;)電流値を大きくしたりビ
ード数を多くしたりする必要があるために、ブローホー
ルの発生やビート間が不均一な微細化組織となるfこめ
に好ましくない、また、アルミ合金素1tlの表面1a
は再溶融化後に切削加工するために、微細化部1bが浅
いと切削時に大部分が除去されてしまうので、表面処理
の効果が得られないという問題があった。However, in the conventional surface treatment method described above, the width W° of the refined portion tb is narrow and the depth is shallow from 1'. , TIG arc, ;) Because it is necessary to increase the current value or increase the number of beads, it is undesirable because it causes blowholes and a fine structure with uneven bead spacing. Surface 1a of 1tl alloy element
Since cutting is performed after remelting, if the refined portion 1b is shallow, most of it will be removed during cutting, so there is a problem that the effect of surface treatment cannot be obtained.
(発明の目的)
本発明は上記従来の問題を解決するためになされた乙の
で、アルミ合金素材の表面に、幅が広く、かつ深い微細
化部を容易に得ることができるようにすることを目的と
するものである。(Objective of the Invention) The present invention has been made in order to solve the above-mentioned conventional problems, and therefore aims to make it possible to easily obtain wide and deep refined portions on the surface of an aluminum alloy material. This is the purpose.
(発明の措成)
このため本発明は、アルミ合金素材の表面に直径2〜4
a+m、深さ1〜4IIII11の凹部を面積率50%
・以上で形成し、ついで、この表面を、電極直径が凹部
より大径のTIGアークにより再溶融することを特徴と
するものである。(Construction of the Invention) For this reason, the present invention provides an aluminum alloy material with a diameter of 2 to 4 mm on the surface.
a+m, depth 1-4III11 concave area ratio 50%
- It is characterized in that it is formed as described above, and then this surface is remelted by a TIG arc whose electrode diameter is larger than that of the recess.
(発明の効果)
本発明によれば、アルミ合金素材の表面を凹凸化さけて
表面積を大きくすることにより、TIGアークの照射エ
ネルギーの吸収率を高めるようにした乙のであるから、
幅が広く、かつ深い微細化部が得られろようになる。(Effects of the Invention) According to the present invention, the absorption rate of TIG arc irradiation energy is increased by increasing the surface area by avoiding making the surface of the aluminum alloy material uneven.
It becomes possible to obtain a wide and deep finely divided portion.
また、幅が広いからビード数が少なくてすむので再溶融
欠陥が少なくなり、さらに深いから切削加工時に微細化
部の除去量が少なくてすむので表面処理の効果、つまり
、耐熱疲労特性が向上するようになる。In addition, because the width is wide, fewer beads are required, which reduces remelting defects, and because it is deeper, less fine parts need to be removed during cutting, which improves the effectiveness of surface treatment, that is, thermal fatigue resistance. It becomes like this.
(実施例)
以下、本発明の実施例を添付図面について詳細に説明す
る。(Embodiments) Hereinafter, embodiments of the present invention will be described in detail with reference to the accompanying drawings.
第1図(a)に示すように、アルミ合金表面の処理方法
は、まず、アルミ合金素材2の表面2aに、直径2〜4
+nm、深さ1〜41II11の凹部(球状ディンプル
)2c、・・・2cを面積率50%以上で形成する。As shown in FIG. 1(a), the method for treating the surface of an aluminum alloy is to first coat the surface 2a of an aluminum alloy material 2 with a diameter of 2 to 4 mm.
Concave portions (spherical dimples) 2c, .
面積率が50%未満では幅が広い微細化部2b(第2図
(b)参照)が得られない。幅を広くするためにビード
数を多くするとビード間の組織が粗大化する。また、微
細化部2bの深さら確保しにくいので、TAGアークの
電流値を大きくしたり、移動速度を遅くしたりする必要
があるが、ブローホール等の欠陥が発生する。If the area ratio is less than 50%, a wide refined portion 2b (see FIG. 2(b)) cannot be obtained. When the number of beads is increased to increase the width, the structure between the beads becomes coarser. In addition, since it is difficult to ensure the depth of the refined portion 2b, it is necessary to increase the current value of the TAG arc or slow down the moving speed, but defects such as blowholes occur.
また、凹部2cの直径が2n+m未満では照射エネルギ
ーの吸収率が低く微細化部2bめ幅が狭くなる。逆に4
IIII11を越えると、照射エネルギーが局部的に集
中し、必要範囲の微細化が不充分になる。Further, if the diameter of the recessed portion 2c is less than 2n+m, the absorption rate of irradiation energy is low and the width of the refined portion 2b is narrowed. On the contrary, 4
If it exceeds III11, the irradiation energy will be locally concentrated and the required range will be insufficiently refined.
さらに、凹部2Cの深さが1III+未満では、TIG
アークが一方的になり、幅が広い微細化部2bが得られ
ない。逆に4nmを越えると、切削加工を深くしないと
元形状が残るおそれがあり、また、TIGアーク長が不
均一になって、安定した深さの微細化部2bが得られな
い。Furthermore, if the depth of the recess 2C is less than 1III+, TIG
The arc becomes one-sided, and a wide refined portion 2b cannot be obtained. On the other hand, if it exceeds 4 nm, there is a risk that the original shape will remain unless the cutting process is deep, and the TIG arc length will become non-uniform, making it impossible to obtain the refined portion 2b with a stable depth.
つぎに、第1図(b)に示すように、このアルミ合金素
材2の表面2aを、T[qアークで再溶融して表面組織
を微細化する。Next, as shown in FIG. 1(b), the surface 2a of this aluminum alloy material 2 is remelted with a T[q arc to refine the surface structure.
このTIGアーク照射条件は、直径φが凹部2Cの直径
より大きい4.8nmの電[,3を用い、Arガスをア
シストガスとし、電流値:300A、移送速度: l
、 Om/ ll1in、アーク長:211II11と
するのが好適である。The TIG arc irradiation conditions were as follows: using an electric current of 4.8 nm whose diameter φ is larger than the diameter of the recess 2C, using Ar gas as an assist gas, current value: 300 A, transfer speed: 1
, Om/ll1in, arc length: 211II11.
そして、第1図(C)のように冷却した後、第1図(d
)のように、この表面2aを所定の高さhで切削加工す
る。After cooling as shown in Fig. 1(C), Fig. 1(d)
), this surface 2a is cut to a predetermined height h.
次に実施例を説明する。Next, an example will be described.
(1)AC4Dのアルミ合金素材2の表面2aに、直径
2mm、深さ4龍の凹部2Cを面積率60%で形成した
。 。(1) On the surface 2a of the AC4D aluminum alloy material 2, a recess 2C with a diameter of 2 mm and a depth of 4 mm was formed at an area ratio of 60%. .
(2)ついで、直径φが4.8mmの電極3.Arアシ
ストガス、′rri流値: 300A、 移送iiJ度
1.0m/+++in、アーク長2II1mの条件下で
TIGアークを照射した。(2) Next, electrode 3. whose diameter φ is 4.8 mm. TIG arc irradiation was performed under the following conditions: Ar assist gas, 'rri flow value: 300 A, transfer II J degree 1.0 m/+++in, and arc length 2 II 1 m.
(3)そして、このアルミ合金素材2を断面カットして
、微細化部2bを観察したところ、微細化部(溶融部)
2bの幅Wは12mmJ”さdは3.6醋であった。(3) Then, when this aluminum alloy material 2 was cut in cross section and the refined part 2b was observed, it was found that the refined part (melted part)
The width W of 2b was 12 mm J'' and the width d was 3.6 mm.
また、これを高さhで切削加工したところ、深さdの2
/3程度(2,4mm)の微細化部2bが確保できた。Also, when this was cut at a height h, the depth d was 2
A finer part 2b of about /3 (2.4 mm) could be secured.
なお、共晶Siの大きさは6μm程度であり、未処理部
が40μmであることから、微細化が確認できた。Note that the size of the eutectic Si was about 6 μm, and the untreated portion was 40 μm, so it was confirmed that the size was miniaturized.
(4)なお、比較のために、AC4Dのアルミ合全素材
2の表面2a(表面粗さ11μm)に前記(2)の条件
下でTIGアークを照射して、微細化部を観察したとこ
ろ、第2図(c)に示したように、微細化部の幅冑°は
8mm、深さd″は2 、1 mmであった。そして、
これを切削加工したところ、第2図(d)のように微細
化部の大部分が除去されてしまい、表面処理の効果が得
られなかった。(4) For comparison, the surface 2a (surface roughness 11 μm) of the AC4D aluminum alloy material 2 was irradiated with a TIG arc under the conditions of (2) above, and the finer parts were observed. As shown in Fig. 2(c), the width of the refined part was 8 mm, and the depth d'' was 2.1 mm.
When this was cut, most of the finer parts were removed as shown in FIG. 2(d), and the effect of surface treatment could not be obtained.
第1図(a)〜(d)は本発明に係るアルミ合金表面の
処理方法の説明図、第2図(a)〜(d)は従来のアル
ミ合金表面の処理方法の説明図である。
2・・・アルミ合金素材、2a・・・表面、2b・・・
微細化部、 2c・・・凹部。FIGS. 1(a) to 1(d) are explanatory diagrams of a method for treating an aluminum alloy surface according to the present invention, and FIGS. 2(a) to (d) are diagrams for explaining a conventional method for treating an aluminum alloy surface. 2... Aluminum alloy material, 2a... Surface, 2b...
Refinement part, 2c... recessed part.
Claims (1)
細化する方法であって、 アルミ合金素材の表面に直径2〜4mm、深さ1〜4m
mの凹部を面積率50%以上で形成し、ついで、この表
面を、電極直径が凹部より大径のTIGアークにより再
溶融することを特徴とするアルミ合金表面の処理方法。(1) A method of remelting the surface of an aluminum alloy material to refine its surface structure, which involves melting the surface of the aluminum alloy material with a diameter of 2 to 4 mm and a depth of 1 to 4 m.
1. A method for treating an aluminum alloy surface, which comprises forming recesses with an area ratio of 50% or more, and then remelting the surface using a TIG arc having an electrode diameter larger than that of the recesses.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP29195786A JPS63145756A (en) | 1986-12-08 | 1986-12-08 | Treatment of aluminum alloy surface |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP29195786A JPS63145756A (en) | 1986-12-08 | 1986-12-08 | Treatment of aluminum alloy surface |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS63145756A true JPS63145756A (en) | 1988-06-17 |
Family
ID=17775652
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP29195786A Pending JPS63145756A (en) | 1986-12-08 | 1986-12-08 | Treatment of aluminum alloy surface |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS63145756A (en) |
-
1986
- 1986-12-08 JP JP29195786A patent/JPS63145756A/en active Pending
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