JP2518980B2 - Method for drilling precision aluminum alloy product with holes - Google Patents

Method for drilling precision aluminum alloy product with holes

Info

Publication number
JP2518980B2
JP2518980B2 JP3147768A JP14776891A JP2518980B2 JP 2518980 B2 JP2518980 B2 JP 2518980B2 JP 3147768 A JP3147768 A JP 3147768A JP 14776891 A JP14776891 A JP 14776891A JP 2518980 B2 JP2518980 B2 JP 2518980B2
Authority
JP
Japan
Prior art keywords
hole
holes
forging
aluminum alloy
product
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.)
Expired - Lifetime
Application number
JP3147768A
Other languages
Japanese (ja)
Other versions
JPH05123809A (en
Inventor
知一 川村
末吉 山口
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
HIGASHINIPPON TANZO KK
Furukawa Electric Co Ltd
Original Assignee
HIGASHINIPPON TANZO KK
Furukawa Electric Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by HIGASHINIPPON TANZO KK, Furukawa Electric Co Ltd filed Critical HIGASHINIPPON TANZO KK
Priority to JP3147768A priority Critical patent/JP2518980B2/en
Publication of JPH05123809A publication Critical patent/JPH05123809A/en
Application granted granted Critical
Publication of JP2518980B2 publication Critical patent/JP2518980B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は、底があり内壁が垂直で
寸法精度の高い穴を有する精密アルミニウム製品の穴を
冷間鍛造によって仕上げる穴加工方法に関するものであ
る。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a hole machining method for finishing a hole of a precision aluminum product having a hole having a bottom and a vertical inner wall with a high dimensional accuracy by cold forging.

【0002】[0002]

【従来の技術】例えば、コンプレッサのピストンを圧入
する穴を有し、全体としてピストンを支持する構造の受
け板のように、要求される寸法精度が高く、底があり垂
直な内壁面の穴を有する精密アルミニウム合金製品の穴
加工においては、温間鍛造又は熱間鍛造により製品寸法
に近い形状の半製品を加工し、この半製品の穴の部分を
ボ−ルエンドミルなどで切削加工により仕上げていた。
これは、温間鍛造(例えば150〜300℃)や熱間鍛
造(例えば350〜500℃)では大まかな穴寸法の加
工は可能であるが、寸法精度を高めることができないこ
とによる。
2. Description of the Related Art For example, like a receiving plate having a hole for press-fitting a piston of a compressor and supporting the piston as a whole, a hole having a high dimensional accuracy and having a bottom and a vertical inner wall surface is required. In the drilling of precision aluminum alloy products we have, semi-finished products with a shape close to the product dimensions are processed by warm forging or hot forging, and the holes of this semi-finished product are finished by cutting with a ball end mill etc. It was
This is because warm forging (for example, 150 to 300 ° C.) and hot forging (for example, 350 to 500 ° C.) can process rough hole dimensions, but cannot improve dimensional accuracy.

【0003】[0003]

【発明が解決しようとする課題】従来は、温間鍛造又は
熱間鍛造で加工された半製品の穴の部分を切削により仕
上げていたので、切削に手間がかかってコスト高になっ
ていた。また、例えば穴底が凹球面であるような場合、
或いは実施例にあるように高強度及び耐磨耗性を有する
硬いアルミニウム合金(例えばAlーSi系合金)の場
合は、切削加工がより一層困難となってさらに高価にな
る欠点があった。本発明の課題は、このような穴加工の
問題点を解決し、より能率的で寸法精度の高い穴加工が
できる精密アルミニウム製品の穴加工方法を提供するこ
とにある。
Conventionally, since the hole portion of the semi-finished product processed by warm forging or hot forging has been finished by cutting, it takes a lot of time and labor to cut the cost. Also, for example, when the hole bottom is a concave spherical surface,
Alternatively, as described in the examples, in the case of a hard aluminum alloy having high strength and abrasion resistance (for example, an Al-Si alloy), there is a drawback that the cutting process becomes more difficult and the cost becomes higher. An object of the present invention is to provide a method for drilling a precision aluminum product, which solves the problem of such drilling and enables more efficient drilling with high dimensional accuracy.

【0004】[0004]

【課題を解決するための手段】前述の課題を達成するた
めの本発明方法は、底があり内壁が垂直な穴を有する精
密アルミニウム合金製品の穴を冷間鍛造によって精密に
仕上げる穴加工方法であって、まず押出材をスライスし
たアルミニウム合金ブランク材を150〜300℃の温
度で温間鍛造により概略寸法の穴に成形加工し、次にこ
れを焼鈍し、続いて冷間鍛造によって所定の精密寸法の
穴に仕上げることを特徴とする穴を有する精密アルミニ
ウム製品の穴加工方法である。
The method of the present invention for achieving the above-mentioned object is a hole drilling method for precisely finishing a hole of a precision aluminum alloy product having a bottom and an inner wall having a vertical hole by cold forging. Therefore, first, an aluminum alloy blank obtained by slicing an extruded material is formed into a hole having an approximate size by warm forging at a temperature of 150 to 300 ° C., then this is annealed, and then cold forged to a predetermined precision. A method of drilling a precision aluminum product having a hole characterized by finishing the hole to a size.

【0005】[0005]

【作用】以下本発明について、詳細に説明する。本発明
に係る穴加工方法においては、まず押出材をスライスし
たアルミニウム合金ブランク材を150〜300℃で温
間鍛造により穴の概略寸法に成形加工して半製品とする
ものであるが、これは図1に示すごとく、金型ダイスの
中子11をブランク材41に押し込むことにより所定穴
の概略寸法に成形加工するものである。ここで、アルミ
ニウム合金ブランク材に、実施例にあるように鋳物では
なく押出材をスライスして使用するのは、押出材のほう
が材料の表面及び内部の欠陥が少ないからである。
The present invention will be described in detail below. In the hole drilling method according to the present invention, first, an aluminum alloy blank material obtained by slicing an extruded material is formed into a semi-finished product by warm forging into the approximate size of a hole, which is a semi-finished product. As shown in FIG. 1, the core 11 of the mold die is pushed into the blank material 41 to perform the molding process into the approximate size of the predetermined hole. Here, the reason why the extruded material is sliced and used as the aluminum alloy blank material instead of the casting as in the embodiment is that the extruded material has fewer defects on the surface and inside of the material.

【0006】また、ここで穴加工に温間鍛造を採用する
のは、穴の成形加工が容易であり、金型(ダイスの中子
11)に抜き勾配が不要だからである。なお、一般に3
00℃以下で鍛造する場合を温間鍛造、300℃を越え
る温度で鍛造する場合を熱間鍛造というが、熱間鍛造の
場合は、温度が高いためブランク材料の表面を潤滑処理
しても潤滑の効果がなく、熱間鍛造で使用する金型に抜
き勾配を必要とし、この抜き勾配は後の冷間鍛造のとき
に矯正できないため、内壁に垂直な部分をもつ穴を加工
することができない。従って本発明においては、温間鍛
造を採用するものである。
Further, the reason why warm forging is adopted for the hole processing is that the hole is easily formed and the die (die core 11) does not need a draft. In addition, generally 3
Forging at 00 ° C or lower is called warm forging, and forging at a temperature over 300 ° C is called hot forging. In the case of hot forging, the temperature is high, so even if the surface of the blank material is lubricated, it is lubricated. Is not effective and requires a draft in the die used for hot forging, and this draft cannot be corrected during the subsequent cold forging, so it is not possible to machine a hole with a vertical portion on the inner wall. . Therefore, in the present invention, warm forging is adopted.

【0007】また、温間鍛造の温度が150℃未満では
穴の成形加工が困難であり、300℃を越えるとブラン
ク材料の表面に塗布する潤滑剤の効果がなくなり金型
(図1のダイスの中子11)が抜けなくなり、金型に抜
き勾配が必要となる。穴の壁面に勾配がつくと最後の冷
間鍛造によって内壁が垂直な穴を所定寸法に仕上げるこ
とができない。従って温間鍛造温度は150〜300℃
とする。温間鍛造における温度の選択は、材料であるア
ルミニウム合金の硬さと穴形状の複雑さないしは寸法に
よって選択される。一般に軟らかい材料の場合、及び要
求される寸法精度が比較的低い場合は低い温度が選択さ
れ、その逆の場合は高い温度が選択される。
If the temperature of the warm forging is less than 150 ° C., it is difficult to form the hole, and if it exceeds 300 ° C., the effect of the lubricant applied to the surface of the blank material is lost and the die (the die of FIG. The core 11) does not come off, and a draft is required for the mold. If the wall surface of the hole is sloped, the final cold forging cannot finish the hole whose inner wall is vertical to a predetermined size. Therefore, the warm forging temperature is 150 to 300 ° C.
And The temperature for warm forging is selected according to the hardness of the aluminum alloy as a material and the complexity or size of the hole shape. Generally, for soft materials, and when the required dimensional accuracy is relatively low, low temperatures are selected, and vice versa.

【0008】前述の如く温間鍛造によって穴加工した半
製品は、次に焼鈍するが、これは温間鍛造によって加工
硬化した材料を再結晶軟化させるためである。この焼鈍
条件は、通常行われている条件が採用される。本発明に
おいては、続いて冷間鍛造により、内壁が垂直な所定の
精密な寸法の穴に仕上げ加工され、以後の加工は一切不
要である。冷間鍛造後の寸法精度は、後述の実施例で明
らかなごとく、例えば設計寸法の±0.06mm以下程
度である。
The semi-finished product which has been hole-formed by warm forging as described above is then annealed, in order to recrystallize and soften the work-hardened material by warm forging. As this annealing condition, a condition that is usually performed is adopted. In the present invention, the inner wall is then finished by vertical cold forging into a hole having a predetermined precision dimension, and no further processing is required. The dimensional accuracy after cold forging is, for example, about ± 0.06 mm or less of the design dimension, as will be apparent from the examples described later.

【0009】本発明に係る穴加工方法によれば、温間鍛
造によって加工される半製品の穴の部分は概略の形状及
び寸法(例えば設計寸法の85%)であるが、これを冷
間鍛造することにより穴の寸法精度が矯正(例えば設計
寸法の15%)され、設計上の寸法との誤差が非常に小
さい穴を有する精密な製品が切削加工なしに量産され
る。また、冷間鍛造のときの塑性加工によって穴の部分
の強度及び耐摩耗性が増大する。
According to the hole drilling method of the present invention, the hole portion of the semi-finished product machined by warm forging has an approximate shape and size (for example, 85% of the designed size), but this is cold forged. By doing so, the dimensional accuracy of the hole is corrected (for example, 15% of the designed size), and a precise product having a hole with a very small error from the designed size is mass-produced without cutting. In addition, the plastic working during cold forging increases the strength and wear resistance of the hole portion.

【0010】[0010]

【実施例】図1及び図2は本発明方法の実施例で使用す
る鍛造用の金型(ダイス1、ダイスの中子11、パンチ
3等)の例を、図3及び図4は本発明方法の実施例で加
工する穴付きアルミニウム合金製品をそれぞれ示すもの
で、図3及び図4の製品4は自動車のエヤコンにおける
図示しないコンプレッサのピストンを受ける輪状の受け
金であり、その外周部に図示しないコンプレッサのピス
トンをそれぞれ圧入するための穴4aを等角度(ほぼ7
2度)間隔に有し、中央に打ち抜きによる孔4bを有し
ており、前記穴4aは凹球面状の内底を有している。
1 and 2 show examples of forging dies (die 1, die core 11, punch 3, etc.) used in the examples of the method of the present invention, and FIGS. 3 and 4 show the present invention. FIGS. 3 and 4 respectively show an aluminum alloy product with a hole to be machined in the embodiment of the method, and the product 4 in FIGS. 3 and 4 is a ring-shaped receiving member for receiving a piston of a compressor (not shown) in an automobile air conditioner, and is shown on an outer periphery thereof Do not press the holes 4a for press-fitting the pistons of the compressors at equal angles (approximately 7
The holes 4b are provided at intervals of 2 degrees and have a punched hole 4b in the center, and the hole 4a has a concave spherical inner bottom.

【0011】図4における製品4の直径Lは97mm、
孔4bの直径lは35mm、穴4a相互の中心を結ぶ円
の直径は75mm、穴4aの直径Rは14.3mm、穴
4aの垂直壁の深さd1は5.5mm、凹球面状の内底
の半径d2は7.15mmにそれぞれ設計されている。
The diameter L of the product 4 in FIG. 4 is 97 mm,
The diameter l of the hole 4b is 35 mm, the diameter of the circle connecting the centers of the holes 4a is 75 mm, the diameter R of the hole 4a is 14.3 mm, the vertical wall depth d1 of the hole 4a is 5.5 mm, and the inside of the concave spherical surface is The bottom radius d2 is designed to be 7.15 mm.

【0012】鍛造用の金型は、SKD−11とSKH−
9のほぼ中間の鋼材で製造されており、機台10上に固
定されたダイス1とパンチ3等から構成されている。ダ
イス1内には前記製品4の穴4aを成形するための中子
11を有し、中央部にはノックアウトピン2が設けら
れ、このノックアウトピン2の上部中央には、材料のフ
ラッシュの逃げ孔20が形成されている。
Molds for forging are SKD-11 and SKH-
It is made of a steel material approximately in the middle of No. 9, and is composed of a die 1, a punch 3 and the like fixed on a machine base 10. The die 1 has a core 11 for forming the hole 4a of the product 4, a knockout pin 2 is provided at the center, and a knockout hole for flushing the material is provided at the center of the upper part of the knockout pin 2. 20 are formed.

【0013】以下本発明方法の一実施例を具体的に説明
すると、先ずケイ素10%を含むA4032合金(Al
ー12%Siー1.0%Mg合金)に近い組成のアルミ
ニウム合金により、直径ほぼ100mmの中空棒材を押
出成形し、これを肉厚16mm程度にスライスした図1
のブランク材料41を製造する。
An embodiment of the method of the present invention will be specifically described below. First, an A4032 alloy containing 10% silicon (Al
-12% Si-1.0% Mg alloy), an aluminum alloy having a composition close to that of (12% Si-1.0% Mg alloy) was extruded to form a hollow rod having a diameter of approximately 100 mm, and the hollow rod was sliced to a thickness of about 16 mm.
Blank material 41 is manufactured.

【0014】この材料41の表面にナトリウム系金属石
鹸からなる潤滑剤を塗布(皮膜厚さ1ミクロン程度)し
た後、これを図示しない炉内に供給して300℃程度に
加熱し、次いで図1のダイス1内に供給してパンチ3に
より63kg/mm2 程度で0.5秒程度加圧し、図2
の半製品40を温間鍛造加工する。この半製品40は、
前記温間鍛造後ダイス1からノックアウトして室温まで
冷却する。この温間鍛造の金型(ダイス1及びパンチ3
等)の寸法は、図3及び図4の製品4の寸法よりやや大
きく設定されているが、半製品40は冷却することによ
って縮小し、設計寸法のほぼ85%程度の寸法精度の半
製品40が製造される。
After applying a lubricant composed of sodium metal soap to the surface of the material 41 (film thickness of about 1 micron), this is supplied into a furnace (not shown) and heated to about 300 ° C., and then, as shown in FIG. 2 into the die 1, and the punch 3 applies a pressure of about 63 kg / mm 2 for about 0.5 seconds.
The semi-finished product 40 of 1. is warm forged. This semi-finished product 40 is
After the warm forging, the die 1 is knocked out and cooled to room temperature. This warm forging die (die 1 and punch 3
3) is set to be slightly larger than the size of the product 4 in FIGS. 3 and 4, but the semi-finished product 40 is reduced by cooling, and the semi-finished product 40 with a dimensional accuracy of about 85% of the design size is obtained. Is manufactured.

【0015】次に前記半製品40を図示しない炉内に供
給し、320℃程度でほぼ2時間焼鈍した後、8時間程
度かけて常温まで徐冷する。
Next, the semi-finished product 40 is supplied into a furnace (not shown), annealed at about 320 ° C. for about 2 hours, and then gradually cooled to room temperature over about 8 hours.

【0016】前記冷却後、半製品40の表面を前述した
潤滑処理の要領と同様に潤滑処理し、図1の金型と同じ
構造で製品4の設計寸法とほぼ同寸法の別の金型によ
り、常温下で前記温間鍛造の場合と同様な圧力で同様な
時間加圧することによって冷間鍛造し、15%程度形状
及び寸法を矯正するとともに塑性加工し、内側に押し出
された図2のフラッシュ42の部分を図示しないプレス
でカットして製品4を製造した。
After the cooling, the surface of the semi-finished product 40 is lubricated in the same manner as the above-mentioned lubrication process, and another mold having the same structure as the mold of FIG. The cold forging by pressing at the same pressure as that in the warm forging for the same time at room temperature for about 15% to correct the shape and dimension and plastic working, and the extruded flash shown in FIG. A product 4 was manufactured by cutting a portion 42 with a press (not shown).

【0017】以上の要領で製品4を30個製造したとこ
ろ、穴4aの垂直壁の深さd1は設計値の±0.06m
m以下、穴4aにおける凹球面底の半径d2は設計値の
+0.025mm以内、穴4aの直径Rは設計値の+
0.02mm以内、穴4aの中心間隔は設計値の±1
0′以下であった。また、温間鍛造又は熱間鍛造によっ
て半製品を加工し、この半製品の前記穴の部分を切削加
工して必要な寸法精度を確保する場合に比べ、量産性が
はるかに向上するとともに、穴4aの部分は塑性加工に
より強度及び耐摩耗性が向上した。
When 30 products 4 were manufactured by the above procedure, the vertical wall depth d1 of the hole 4a was ± 0.06 m, which is the design value.
m or less, the radius d2 of the concave spherical bottom of the hole 4a is within +0.025 mm of the design value, and the diameter R of the hole 4a is + of the design value.
Within 0.02 mm, center distance between holes 4a is ± 1 of design value
It was less than 0 '. In addition, the semi-finished product is processed by warm forging or hot forging, and the mass productivity is much improved as compared with the case where the hole portion of the semi-finished product is cut and the required dimensional accuracy is secured. The portion 4a had improved strength and wear resistance due to plastic working.

【0018】なお、前記実施例では、製品4の穴4aは
丸穴で凹球面上の内底を有しているが、本発明方法はこ
のような穴4aをもつアルミニウム合金製品の加工のみ
でなく、平底の穴や錐形底の穴,多角穴などをもつアル
ミニウム合金製品を加工する場合にも有効であり、むし
ろこのような形状の穴を有する製品の方が、冷間鍛造時
の加圧抵抗や変形量が小さいのでより精密にかつより容
易に加工することができる。また、本発明方法は、アル
ミニウム及びアルミニウム合金からなる製品に限らず、
例えば銅及びその合金やマグネシウム系その他の金属か
らなる精密な孔を有する製品の加工にも適用することが
できるものである。
Although the hole 4a of the product 4 is a round hole and has an inner bottom on a concave spherical surface in the above-mentioned embodiment, the method of the present invention can be applied only to the processing of an aluminum alloy product having such a hole 4a. However, it is also effective when processing aluminum alloy products with flat bottom holes, conical bottom holes, polygonal holes, etc. Rather, products with holes of this shape are more suitable for cold forging. Since the piezoresistive force and the amount of deformation are small, it can be processed more precisely and easily. The method of the present invention is not limited to products made of aluminum and aluminum alloys,
For example, it can be applied to the processing of products having precise holes made of copper and its alloys, magnesium and other metals.

【0019】[0019]

【発明の効果】本発明方法によれば、温間鍛造によって
穴を概略寸法に成形加工して半製品とし、次にこれを焼
鈍し、続いて冷間鍛造によって穴の寸法を高い寸法精度
に矯正するとともに塑性加工をするので、従来のように
切削により穴寸法を矯正する場合に比べ量産性がはるか
に向上し、低コストで穴を有するアルミニウム合金製品
を提供することができるほか、製品の穴の部分の強度及
び耐摩耗性も向上する等工業上顕著な効果を有するもの
である。
According to the method of the present invention, a hole is formed into a semi-finished product by warm forging into a semi-finished product, which is then annealed and then cold forged to obtain a hole with high dimensional accuracy. Since it is straightened and plastically worked, mass productivity is much improved compared to the conventional case where the hole size is straightened by cutting, and it is possible to provide aluminum alloy products with holes at low cost. It has a notable industrial effect such that the strength and wear resistance of the hole portion are improved.

【図面の簡単な説明】[Brief description of drawings]

【図1】本発明方法の実施例で使用される鍛造用金型に
材料を供給した状態の断面図である。
FIG. 1 is a cross-sectional view showing a state in which a material is supplied to a forging die used in an embodiment of the method of the present invention.

【図2】図1の金型において材料を加圧した状態の半裁
断面図である。
FIG. 2 is a half sectional view showing a state where a material is pressed in the mold of FIG.

【図3】本発明方法の実施例で製造される穴を有する精
密アルミニウム合金製品の平面図である。
FIG. 3 is a plan view of a precision aluminum alloy product having holes manufactured by the method of the present invention.

【図4】図3の矢印A−Aに沿う断面図である。FIG. 4 is a sectional view taken along arrow AA in FIG. 3;

【符号の説明】[Explanation of symbols]

1 ダイス 11 中子 2 ノックアウトピン 20 逃げ孔 3 パンチ 4 製品 40 半製品 41 ブランク材料 42 フラッシュ 1 Die 11 Core 2 Knockout Pin 20 Escape Hole 3 Punch 4 Product 40 Semi-finished Product 41 Blank Material 42 Flash

───────────────────────────────────────────────────── フロントページの続き (56)参考文献 特開 昭63−119942(JP,A) 特開 平2−200334(JP,A) 実開 平3−9242(JP,U) ─────────────────────────────────────────────────── ─── Continuation of the front page (56) References JP-A-63-119942 (JP, A) JP-A-2-200334 (JP, A) JP-A-3-9242 (JP, U)

Claims (1)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 底があり内壁が垂直な穴を有する精密ア
ルミニウム合金製品の穴を冷間鍛造によって精密に仕上
げる穴加工方法であって、まず押出材をスライスしたア
ルミニウム合金ブランク材を150〜300℃の温度で
温間鍛造により概略寸法の穴に成形加工して半製品と
し、次にこれを焼鈍し、続いて冷間鍛造によって所定の
精密寸法の穴に仕上げることを特徴とする穴を有する精
密アルミニウム合金製品の穴加工方法。
1. A precision tool having a bottom and an inner wall having a vertical hole.
Precisely finish the hole of the aluminum alloy product by cold forging
This is a drilling method for drilling holes.
Luminium alloy blank at a temperature of 150-300 ℃
Warm forging to form holes with approximate dimensions to produce semi-finished products
Then, this is annealed, followed by cold forging
Precision with holes characterized by finishing to holes with precise dimensions
Drilling method for dense aluminum alloy products.
JP3147768A 1991-05-23 1991-05-23 Method for drilling precision aluminum alloy product with holes Expired - Lifetime JP2518980B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3147768A JP2518980B2 (en) 1991-05-23 1991-05-23 Method for drilling precision aluminum alloy product with holes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3147768A JP2518980B2 (en) 1991-05-23 1991-05-23 Method for drilling precision aluminum alloy product with holes

Publications (2)

Publication Number Publication Date
JPH05123809A JPH05123809A (en) 1993-05-21
JP2518980B2 true JP2518980B2 (en) 1996-07-31

Family

ID=15437740

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3147768A Expired - Lifetime JP2518980B2 (en) 1991-05-23 1991-05-23 Method for drilling precision aluminum alloy product with holes

Country Status (1)

Country Link
JP (1) JP2518980B2 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2386576B (en) * 2002-03-06 2004-02-25 Adcock Tech Ltd A method of manufacture of a metallic component, apparatus when used in the method and a method of finishing a metallic component
KR101483236B1 (en) * 2012-11-19 2015-01-16 서영정밀주식회사 Method of Precision Processing for Inner and Outer Diameter of Fixed Secondary Piston with Forging Processing
JP6362263B2 (en) * 2013-11-26 2018-07-25 昭和電工株式会社 Hard disk drive device forged shape material for case body, case body, method for producing forged shape material for case body, and method for producing case body

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63119942A (en) * 1986-11-07 1988-05-24 Diesel Kiki Co Ltd Manufacture of parts for compressor or the like
JPH02200334A (en) * 1989-01-27 1990-08-08 Hiroshima Alum Kogyo Kk Manufacture of forged part
JP3009242U (en) * 1994-09-20 1995-04-04 栄次 丸子 Electronic water continuous production equipment

Also Published As

Publication number Publication date
JPH05123809A (en) 1993-05-21

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