JPH05123809A - Working method for precise aluminum product having hole - Google Patents
Working method for precise aluminum product having holeInfo
- Publication number
- JPH05123809A JPH05123809A JP14776891A JP14776891A JPH05123809A JP H05123809 A JPH05123809 A JP H05123809A JP 14776891 A JP14776891 A JP 14776891A JP 14776891 A JP14776891 A JP 14776891A JP H05123809 A JPH05123809 A JP H05123809A
- Authority
- JP
- Japan
- Prior art keywords
- hole
- product
- forging
- semi
- finished 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.)
- Granted
Links
- 238000000034 method Methods 0.000 title claims abstract description 21
- 229910052782 aluminium Inorganic materials 0.000 title claims description 15
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title claims description 15
- 239000000047 product Substances 0.000 claims abstract description 37
- 238000005242 forging Methods 0.000 claims abstract description 33
- 239000011265 semifinished product Substances 0.000 claims abstract description 33
- 238000010273 cold forging Methods 0.000 claims abstract description 13
- 238000005266 casting Methods 0.000 claims abstract description 7
- 229910000838 Al alloy Inorganic materials 0.000 abstract description 5
- 238000004519 manufacturing process Methods 0.000 abstract description 2
- 238000001125 extrusion Methods 0.000 abstract 1
- 230000001050 lubricating effect Effects 0.000 abstract 1
- 238000003825 pressing Methods 0.000 abstract 1
- 239000000463 material Substances 0.000 description 10
- 229910045601 alloy Inorganic materials 0.000 description 6
- 239000000956 alloy Substances 0.000 description 6
- 238000005520 cutting process Methods 0.000 description 6
- 238000003672 processing method Methods 0.000 description 3
- 238000005482 strain hardening Methods 0.000 description 3
- 238000001816 cooling Methods 0.000 description 2
- 238000005461 lubrication Methods 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- KEAYESYHFKHZAL-UHFFFAOYSA-N Sodium Chemical compound [Na] KEAYESYHFKHZAL-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 239000000498 cooling water Substances 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000011010 flushing procedure Methods 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000001151 other effect Effects 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 239000000344 soap Substances 0.000 description 1
- 239000007779 soft material Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
Landscapes
- Forging (AREA)
Abstract
Description
【0001】[0001]
【産業上の利用分野】本発明は、内壁の全部又は一部が
垂直であって、比較的高い寸法精度が要求される穴を有
する精密なアルミニウム又はアルミニウム合金(以下単
に「アルミニウム」という。)製品の加工方法に関する
ものである。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a precision aluminum or aluminum alloy (hereinafter simply referred to as "aluminum") in which all or part of the inner wall is vertical and has holes which require relatively high dimensional accuracy. The present invention relates to a method of processing a product.
【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垂直な内壁面
の穴を有する精密アルミニウム製品においては、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(15
0〜300℃)や熱間鍛造(300〜500℃)では大
まかな加工度は得られるが、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, a precision aluminum product having a hole for press-fitting a piston of a compressor and a hole for a vertical inner wall surface having a high dimensional accuracy required, such as a receiving plate having a structure for supporting the piston as a whole. In the above, a semi-finished product having a shape close to the product size was processed by warm forging or hot forging, and the hole portion of this semi-finished product was finished by cutting with a ball end mill or the like. This is warm forging (15
This is because the rough working ratio can be obtained by hot forging (300 to 500 ° C.), but the dimensional accuracy cannot be improved.
【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
は、切削加工がより一層高度になってさらに高価になる
欠点があった。本発明の目的は、このような問題点を解
決し、より能率的に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. Further, for example, when the bottom of the hole is a concave spherical surface, there is a drawback that the cutting process becomes more sophisticated and more expensive. An object of the present invention is to solve the above problems and provide a method for processing a precision aluminum product capable of more efficiently performing hole processing with high dimensional accuracy.
【0004】[0004]
【課題を解決するための手段】本発明方法は前述の目的
を達成するため、製品寸法よりやや大きな寸法の金型に
より150〜350℃で温間鍛造又は熱間鍛造によって
半製品を加工する工程と、この半製品を製品寸法とほぼ
同寸法の金型により冷間鍛造する工程とを含んでいる。
温間鍛造及び熱間鍛造における温度の選択は、材料であ
るアルミニウム又はその合金の硬さと穴形状の複雑さな
いし寸法によって選択される。一般に軟らかい材料の場
合、及び穴形状が単純で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。In order to achieve the above-mentioned object, the method of the present invention is a step of processing a semi-finished product by warm forging or hot forging at 150 to 350 ° C. with a die having a size slightly larger than the product size. And a step of cold forging this semi-finished product with a die having substantially the same size as the product size.
The temperature selection in warm forging and hot forging is selected depending on the hardness of the material aluminum or its alloy and the complexity of the hole shape. Generally, for soft materials, and when the hole shape is simple and the required dimensional accuracy is relatively low, low temperatures are selected, and vice versa.
【0005】本発明方法において、要求される穴の寸法
精度が比較的低いものについては、半製品を温間鍛造又
は熱間鍛造によって加工することに代え、鋳造によって
加工することができる。In the method of the present invention, if the required hole dimensional accuracy is relatively low, the semi-finished product can be processed by casting instead of being warm forged or hot forged.
【0006】前記の各加工方法において、半製品の加工
時の加工硬化の程度が高い材料の場合には、鍛造又は鋳
造による半製品を冷間鍛造する前に焼鈍するのが望まし
い。In each of the above processing methods, in the case of a material having a high degree of work hardening during processing of a semi-finished product, it is desirable to anneal the semi-finished product by forging or casting before cold forging.
【0007】[0007]
【作用】本発明に係る加工方法によれば、温間鍛造又は
熱間鍛造若しくは鋳造によって加工される半製品の穴の
部分の寸法精度は低いが、これを冷間鍛造することによ
り穴の寸法精度が矯正され、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 processing method of the present invention, the dimensional accuracy of the hole portion of the semi-finished product processed by warm forging, hot forging, or casting is low, but the size of the hole is reduced by cold forging. Precision products will be mass-produced that have holes with precision corrected and very small deviation from design dimensions. Also,
The plastic working during cold forging increases the strength and wear resistance of the hole portion.
【0008】[0008]
【実施例】図1及び図2は本発明方法の実施例で使用す
る鍛造用の金型の例を、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、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72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 a die for forging used in an example of the method of the present invention, and FIG. 4 shows an aluminum product with a hole to be machined in the example of the method of the present invention.
The product 4 of FIGS. 3 and 4 is a ring-shaped receiving member for receiving a piston of a compressor (not shown) in an automobile, and holes 4a for press-fitting pistons of the compressor (not shown) are equiangularly (almost 72 degrees) provided on the outer periphery. To have
It has a hole 4b formed by punching in the center, and the hole 4a
Has a concave spherical inner bottom.
【0009】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, and the depth d1 of the vertical wall of the hole 4a is 5.5 mm. The bottom radius d2 is designed to be 7.15 mm.
【0010】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-9.
It is made of a steel material in the middle of the above and is composed of a die 1 and a punch 3 fixed on a machine base 10. A core 11 for forming the hole 4a of the product 4 in the die 1.
And a knockout pin 2 is provided in the central portion thereof, and an escape hole 20 for flushing the material is formed in the upper center of the knockout pin 2.
【0011】以下本発明方法の第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の材料41を製造する。The first embodiment of the method of the present invention will be described in detail below. First, an aluminum alloy having a composition close to that of an A4032 alloy containing 10% silicon has a diameter of approximately 100 mm.
1 is extruded and sliced to have a wall thickness of about 16 mm to produce the material 41 of FIG.
【0012】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を鍛造加工する。この半製品40は、前記
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。この温間鍛造のダイス1及びパンチ3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。A lubricant made of sodium metal soap is applied to the surface of the material 41 (coating thickness is about 1 micron), and this is fed into a furnace (not shown) and heated to about 300 ° C. 2 into the die 1 and pressurizing with a punch 3 at about 63 kg / mm 2 for about 0.5 seconds.
The forged semi-finished product 40 is forged. After the forging, the semi-finished product 40 is knocked out from the die 1 and cooled to room temperature. The dimensions of the warm forging die 1 and the punch 3 are set to be slightly larger than the dimensions of the product 4 shown in FIGS. 3 and 4, but the semi-finished product 40 is reduced by cooling and is approximately 85% of the designed size. A semi-finished product 40 having a dimensional accuracy of a degree is manufactured.
【0013】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時間保持した後、8時間程
度かけて徐冷する。Next, the semi-finished product 40 is fed into a furnace (not shown), held at about 320 ° C. for about 2 hours, and then gradually cooled over about 8 hours.
【0014】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、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. By extruding inward at room temperature, the same pressure as in the case of warm forging is applied for the same time to correct the shape and size by about 15%, and plastic working is performed.
The product 4 was manufactured by cutting a portion of the flash 42 of FIG.
【0015】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 spacing of holes 4a is ± 1 of design value
It was less than 0 '. In addition, the semi-finished product is machined by warm forging or hot forging, and the productivity of the semi-finished product is much improved as compared with the case where the hole portion of the semi-finished product is cut to ensure the required dimensional accuracy. The portion 4a has improved strength and wear resistance due to plastic working.
【0016】次に本発明方法の第二実施例を説明する
と、製品4の設計寸法と同じ寸法の図示しない鋳型(金
型)を予め準備し、鋳物用アルミニウム合金AC4Aを
720℃程度で溶解させ、この溶湯を前記鋳型内に注入
し、鋳型の周囲に冷却水を供給して2〜3分間冷却し、
鋳型内から取り出した合金塊の湯口及び湯溜まりをプレ
スでカットし、製品の設計寸法のほぼ70%程度の寸法
精度をもつ図示しない半製品を製造した。この半製品
を、前記第一実施例の場合と同様に焼鈍し、これを表面
潤滑処理後前述と同様な要領で冷間鍛造により、30%
程度形状及び寸法を矯正するとともに塑性加工し、内側
に形成されたフラッシュの部分をプレスでカットして製
品4を製造した。Next, a second embodiment of the method of the present invention will be described. A mold (mold) (not shown) having the same size as the design size of the product 4 is prepared in advance, and the casting aluminum alloy AC4A is melted at about 720 ° C. Injecting this molten metal into the mold, supplying cooling water around the mold to cool it for 2 to 3 minutes,
The sprue and puddle of the alloy lump taken out from the mold were cut by a press to manufacture a semi-finished product (not shown) having a dimensional accuracy of about 70% of the design dimension of the product. This semi-finished product is annealed in the same manner as in the first embodiment, and after surface lubrication treatment, it is subjected to cold forging in the same manner as described above to obtain 30%.
The product 4 was manufactured by straightening the shape and dimensions, plastically working the same, and cutting the flash portion formed inside with a press.
【0017】前記第二実施例の要領で製品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±
0.09mm以下、穴4aにおける凹球面底の半径d2
は設計値の+0.035mm以内、穴4aの直径Rは設
計値の+0.04mm以内、穴4aの中心間隔は設計値
の±15′以下であった。この実施例の加工方法の他の
効果は、前記実施例の方法と同様であった。When 30 products 4 were manufactured according to the procedure of the second embodiment, the depth d1 of the vertical wall of the hole 4a was ± the design value.
0.09 mm or less, the radius d2 of the concave spherical bottom in the hole 4a
Was within +0.035 mm of the design value, the diameter R of the hole 4a was within +0.04 mm of the design value, and the center interval of the holes 4a was within ± 15 'of the design value. Other effects of the processing method of this embodiment were the same as those of the above-mentioned embodiment.
【0018】前記各実施例では、半製品を冷間鍛造する
前に焼鈍したが、加工硬化が比較的小さい合金を使用す
る場合、例えばA6000系のアルミニウム合金を使用
する場合は半製品を焼鈍しないで冷間鍛造することがで
きる。In each of the above embodiments, the semi-finished product was annealed before cold forging. However, when an alloy having a relatively small work hardening is used, for example, when an A6000 series aluminum alloy is used, the semi-finished product is not annealed. It can be cold forged.
【0019】前記各実施例では、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
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又はそ
の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孔付き製品の
加工にも適用することができるものである。In each of the above-mentioned embodiments, the hole 4a of the product 4 is a round hole and has an inner bottom on a concave spherical surface, but the method of the present invention is not limited to the processing of an aluminum product having such a hole 4a.
It is also effective when processing aluminum products with flat-bottomed holes, conical-shaped holes, polygonal holes, etc. Rather, products with such shaped holes are more resistant to pressure resistance during cold forging. Since the amount of deformation is small, it can be processed more precisely and easily. Further, the method of the present invention is not limited to products made of aluminum or its alloys, but can also be applied to the processing of products with precision holes made of, for example, copper and its alloys, magnesium and other metals.
【0020】一般に300℃以下で鍛造する場合を温間
鍛造、300℃以上で鍛造する場合を熱間鍛造という
が、350℃より高い温度で熱間鍛造する場合は、材料
の表面を潤滑処理しても効果がなく、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。Generally, forging at 300 ° C. or lower is called warm forging, and forging at 300 ° C. or higher is called hot forging. When hot forging is performed at a temperature higher than 350 ° C., the surface of the material is lubricated. However, there is no effect, and a draft used in the hot forging requires a draft. This draft cannot be corrected during cold forging, and therefore a hole having a portion perpendicular to the inner wall cannot be machined.
【0021】[0021]
【発明の効果】本発明方法によれば、寸法精度は劣るが
加工度の大きい温間鍛造又は熱間鍛造若しくは鋳造によ
って半製品を加工し、加工度は小さいが高い寸法精度が
得られる冷間鍛造によって穴の寸法を矯正するとともに
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
で穴付きアルミニウム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が向上する。According to the method of the present invention, a semi-finished product is processed by warm forging or hot forging or casting, which has a poor dimensional accuracy but a large working ratio, and a cold working which has a small working ratio but high dimensional accuracy. Since the hole size is corrected by forging and plastic working is performed, mass productivity is much improved compared to the conventional case where the hole size is corrected by cutting, and aluminum products with holes can be provided at low cost. In addition, the strength and wear resistance of the holes of the product are improved.
【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 in which 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
密アルミニウム製品の平面図である。FIG. 3 is a plan view of a precision aluminum 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。4 is a cross-sectional view taken along the arrow AA of FIG.
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 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 Material 42 Flash
Claims (3)
り150〜350℃で温間鍛造又は熱間鍛造によって半
製品を加工する工程と、この半製品を製品寸法とほぼ同
寸法の金型により冷間鍛造する工程とを含むことを特徴
とする、穴を有する精密アルミニウム製品の加工方法。1. A step of processing a semi-finished product by warm forging or hot forging at 150 to 350 ° C. with a mold having a size slightly larger than the product size, and the semi-finished product having a size substantially the same as the product size. Cold forging step, and a method for processing a precision aluminum product having a hole.
品を鋳造する工程と、この半製品を製品寸法とほぼ同寸
法の金型により冷間鍛造する工程とを含むことを特徴と
する、穴を有する精密アルミニウム製品の加工方法。2. A step of casting a semi-finished product with a mold having substantially the same size as the product size, and a step of cold forging the semi-finished product with a die having substantially the same size as the product size. A method for processing precision aluminum products having holes.
を特徴とする、請求項1又は2に記載の穴を有する精密
アルミニウム製品の加工方法。3. The method for processing a precision aluminum product having a hole according to claim 1, wherein the semi-finished product is annealed before cold forging.
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 true JPH05123809A (en) | 1993-05-21 |
JP2518980B2 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) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2386576A (en) * | 2002-03-06 | 2003-09-24 | Adcock Tech Ltd | Deforming a component with a die tool |
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 |
JP2015127064A (en) * | 2013-11-26 | 2015-07-09 | 昭和電工株式会社 | Hard disk drive device case body forging roughly formed material, case body, manufacturing method of case body forging roughly formed material and manufacturing method of case body |
Citations (3)
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 |
-
1991
- 1991-05-23 JP JP3147768A patent/JP2518980B2/en not_active Expired - Lifetime
Patent Citations (3)
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 |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2386576A (en) * | 2002-03-06 | 2003-09-24 | Adcock Tech Ltd | Deforming a component with a die tool |
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 |
JP2015127064A (en) * | 2013-11-26 | 2015-07-09 | 昭和電工株式会社 | Hard disk drive device case body forging roughly formed material, case body, manufacturing method of case body forging roughly formed material and manufacturing method of case body |
Also Published As
Publication number | Publication date |
---|---|
JP2518980B2 (en) | 1996-07-31 |
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