JPH02165838A - Forming method for composite cylindrical parts - Google Patents
Forming method for composite cylindrical partsInfo
- Publication number
- JPH02165838A JPH02165838A JP31787788A JP31787788A JPH02165838A JP H02165838 A JPH02165838 A JP H02165838A JP 31787788 A JP31787788 A JP 31787788A JP 31787788 A JP31787788 A JP 31787788A JP H02165838 A JPH02165838 A JP H02165838A
- Authority
- JP
- Japan
- Prior art keywords
- billet
- composite
- duplex
- extrusion
- hole
- 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
- 239000002131 composite material Substances 0.000 title claims description 41
- 238000000034 method Methods 0.000 title claims description 6
- 238000001125 extrusion Methods 0.000 claims abstract description 19
- 239000000463 material Substances 0.000 claims abstract description 11
- 238000009792 diffusion process Methods 0.000 claims abstract description 9
- 238000005242 forging Methods 0.000 claims description 5
- 238000005520 cutting process Methods 0.000 claims description 2
- 238000005304 joining Methods 0.000 abstract description 4
- 238000005096 rolling process Methods 0.000 abstract 1
- 239000000853 adhesive Substances 0.000 description 7
- 230000001070 adhesive effect Effects 0.000 description 7
- 238000000465 moulding Methods 0.000 description 7
- 238000003825 pressing Methods 0.000 description 3
- 229910001199 N alloy Inorganic materials 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- 230000002411 adverse Effects 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 231100000989 no adverse effect Toxicity 0.000 description 1
- 238000004904 shortening Methods 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、内外層が相異なった材質の複合筒状部品の成
形方法に関する。DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention relates to a method for molding a composite cylindrical part whose inner and outer layers are made of different materials.
(従来の技術)
従来、複合筒状部品を成形するには、内層部と外層部と
を個別に成形後に、両者を接着剤を介して嵌合したり、
圧入嵌合していた。(Prior Art) Conventionally, in order to mold a composite cylindrical part, an inner layer part and an outer layer part are individually molded, and then the two parts are fitted together using an adhesive.
It was a press fit.
(発明が解決しようとする課題)
内外層部を個別に成形すると工程が多くコストが嵩み、
また、相対的な寸法誤差も大きくなる。(Problem to be solved by the invention) Molding the inner and outer layers separately requires many steps and increases costs;
Additionally, relative dimensional errors also increase.
更に、内外層部を接着剤を介して嵌合する場合、接着力
不足になったり、接着剤のための隙間により両者が偏心
したり、接着剤蒸気が悪影響を及ぼすことがある。また
、内外層部を圧入嵌合する場合、残留応力によるひずみ
が生じるという問題がある。Furthermore, when the inner and outer layers are fitted together using an adhesive, the adhesive force may be insufficient, the gap between the two may become eccentric, or the adhesive vapor may have an adverse effect. Furthermore, when the inner and outer layers are press-fitted, there is a problem in that distortion occurs due to residual stress.
本発明は上記課題を解決することを目的とする。The present invention aims to solve the above problems.
(課題を解決するための手段)
本発明の特徴とするところは、内外層が相異なった材質
の複合筒状部品17を押出成形するに際し、まず、外層
材製の有底筒状ビレット1に、内層材製のビレット2を
嵌入して複合ビレット3を形成し、この複合ビレット3
の軸心に通孔5を設け、複合ビレット3を押出成形型6
内に、底部側が押出ロア側となるように装填すると共に
、通孔5に中子軸4を挿通し、複合ビレット3を押出ロ
アから押出すことで内外ビレット1.2を拡散接合させ
つつ複合パイプ12に成形し、次に、この複合パイプ1
2を一定長さに切断してから型鍛造して複合筒状部品1
7に成形する点にある。(Means for Solving the Problems) A feature of the present invention is that when extruding a composite cylindrical part 17 whose inner and outer layers are made of different materials, first, a bottomed cylindrical billet 1 made of the outer layer material is , a billet 2 made of inner layer material is inserted to form a composite billet 3, and this composite billet 3
A through hole 5 is provided in the axis of the composite billet 3 into an extrusion mold 6.
At the same time, the core shaft 4 is inserted into the through hole 5, and the composite billet 3 is extruded from the extrusion lower, thereby diffusion bonding the inner and outer billets 1.2 and forming the composite billet. formed into a pipe 12, and then this composite pipe 1
2 is cut to a certain length and then die-forged to form a composite cylindrical part 1.
It is at the point where it is formed into 7.
(作 用)
本発明方法によれば、複合パイプの内外層は同時に一工
程で押出成形され、また、内外層の接合は、押出されつ
つ拡散接合することでなされる。(Function) According to the method of the present invention, the inner and outer layers of the composite pipe are simultaneously extruded in one step, and the inner and outer layers are joined by diffusion bonding while being extruded.
このような複合パイプを一定長さに切断して型鍛造した
筒状製品の内外層は拡散接合により接着されているため
、接着剤は不要で、内外層間に隙間や残質応力が生じる
こともない。また、内外層の接合後に成形するため、相
対的な寸法誤差もない。The inner and outer layers of such a cylindrical product, which is made by cutting a composite pipe to a certain length and die-forging it, are bonded by diffusion bonding, so there is no need for an adhesive, and there is a risk that gaps or residual stress may occur between the inner and outer layers. do not have. Furthermore, since the molding is performed after the inner and outer layers are joined, there is no relative dimensional error.
(実施例) 以下、本発明の実施例を図面を参照し説明する。(Example) Embodiments of the present invention will be described below with reference to the drawings.
まず、第1図に示すような、有底円筒状ビレット1に、
円柱状ビレット2を内嵌して複合ビレット3とする。こ
の際、外層ビレット1の内周面と内層ビレット2の外周
面との間には約0.1膿の隙間ができるようにする。First, a cylindrical billet 1 with a bottom as shown in FIG.
A cylindrical billet 2 is fitted inside to form a composite billet 3. At this time, a gap of about 0.1 mm is created between the inner circumferential surface of the outer billet 1 and the outer circumferential surface of the inner billet 2.
外層ビレット1は本実施例では、材質をN合金A606
1とし、冷間圧縮により成形した。In this embodiment, the outer layer billet 1 is made of N alloy A606.
1 and molded by cold compression.
内層ビレット2は本実施例では、材質をステンレス鋼5
US416とし、冷間圧縮により成形した。In this embodiment, the material of the inner billet 2 is stainless steel 5.
US416 and molded by cold compression.
次に、複合ビレット3の軸心に、後述の中子軸4が挿入
される通孔5を設ける。本実施例では通孔5は機械加工
により設けた。Next, a through hole 5 is provided in the axial center of the composite billet 3, into which a core shaft 4, which will be described later, is inserted. In this example, the through hole 5 was provided by machining.
そして、第3図に示すように、間接押出用成形金型6に
複合ビレット3を、その底部側が押出ロア側となるよう
に装填する。ここで成形金型6は、押出ロアを有するグ
イ本体8と、これを囲む筒状成形コンテナ9と、この成
形コンテナ9の下端を閉塞するシールブロック10と、
図外押圧機構に連動連結されたステムプラテン11とを
備えている。Then, as shown in FIG. 3, the composite billet 3 is loaded into the mold 6 for indirect extrusion so that the bottom side of the billet is on the extrusion lower side. Here, the molding die 6 includes a goo body 8 having an extrusion lower, a cylindrical molding container 9 surrounding this, and a seal block 10 closing the lower end of this molding container 9.
The stem platen 11 is operatively connected to a pressing mechanism (not shown).
そしてシールブロック10に中子軸4が取付けられ、こ
の中子軸4が複合ビレット3の通孔5に挿通される。Then, the core shaft 4 is attached to the seal block 10, and the core shaft 4 is inserted into the through hole 5 of the composite billet 3.
しかる後に、ステムプラテン11によりグイ本体8を圧
下させることで、押出ロアから複合ビレット3を押出す
。これにより、内外ビレット1.2は拡散接合されつつ
、外層N合金製で内層がステンレス類の複合丸パイプ1
2に成形される。ここで、押出温度は、480℃とし、
押出比は10〜30°Cとした。Thereafter, the goo body 8 is pushed down by the stem platen 11 to extrude the composite billet 3 from the extrusion lower. As a result, the inner and outer billets 1.2 are diffusion bonded, while the composite round pipe 1 whose outer layer is made of N alloy and whose inner layer is made of stainless steel.
It is formed into 2. Here, the extrusion temperature is 480°C,
The extrusion ratio was 10-30°C.
そして、複合パイプ12を、第4図のように一定長に切
断し、しかる後に、第5図に示すように型鍛造を行なう
。鍛造装置は、ダイス13と、図外押圧機構に連動連結
されたバンチ14と、ノックピン15とで主構成され、
バンチ14を第5図中左方の状態から右方のように圧下
することで、第6図示のような外層部にフランジ16を
有する筒状部品17に成形する。本実施例では、この筒
状部品17はさらに切削加工され、第7図に示すような
OA機器用ハードディスクドライブモータのロータ兼用
ハブ18とされ、軸中心に回転駆動されると共に、その
外周に磁気ディスクが装着可能とされる。The composite pipe 12 is then cut to a certain length as shown in FIG. 4, and then die forged as shown in FIG. The forging device mainly includes a die 13, a bunch 14 interlocked with a pressing mechanism (not shown), and a knock pin 15.
By pressing down the bunch 14 from the left side in FIG. 5 to the right side, it is formed into a cylindrical part 17 having a flange 16 on the outer layer as shown in FIG. 6. In this embodiment, this cylindrical part 17 is further machined to form a hub 18 that also serves as a rotor for a hard disk drive motor for office automation equipment as shown in FIG. Discs can be installed.
なお、複合筒状部品の材質は上記実施例に限定されず、
また丸部に限らず角筒としてもよい。さらに、間接押出
に限らず直接押出としてもよい。Note that the material of the composite cylindrical part is not limited to the above embodiments,
Further, the shape is not limited to a round part, and may be a square cylinder. Furthermore, not only indirect extrusion but also direct extrusion may be used.
また、内外ビレットの成形方法も特に限定されず、形状
も角筒、角柱等でもよく、通孔もビレット成形と同時に
成形しておいてもよい。Furthermore, the method of forming the inner and outer billets is not particularly limited, and the shapes may be square cylinders, prisms, etc., and the through holes may be formed at the same time as billet forming.
(発明の効果)
本発明によれば、複合パイプの内外層を個別に押出成形
することなく同時に押出成形でき、しかも、押出と同時
に内外層は拡散接合されるために別途接合手段を講じる
必要はない。そして、この複合パイプを型鍛造すること
によって複合筒状部品を得ることから、製造工程の短縮
により製造コストが低減され、また、その内外層は拡散
接合により接着され、内外層間に隙間はなく、また、内
外層を嵌合後に成形することから内外層間の相対的な寸
法誤差を下級的小さくでき、寸法精度の高い部品を得る
ことができる。もちろん、内外層の接合用接着剤が不要
で接着剤蒸気による悪影響はなく、また圧入嵌合したよ
うな場合の残留応力によるひずみが生じるようなことも
ない。(Effects of the Invention) According to the present invention, the inner and outer layers of a composite pipe can be extruded at the same time without being extruded separately, and the inner and outer layers are diffusion bonded simultaneously with extrusion, so there is no need to provide a separate bonding method. do not have. Since a composite cylindrical part is obtained by die forging this composite pipe, manufacturing costs are reduced by shortening the manufacturing process, and the inner and outer layers are bonded by diffusion bonding, so there is no gap between the inner and outer layers. Further, since the inner and outer layers are molded after being fitted, the relative dimensional error between the inner and outer layers can be reduced to a minimum, and a component with high dimensional accuracy can be obtained. Of course, there is no need for adhesive for joining the inner and outer layers, there is no adverse effect from adhesive vapor, and no distortion occurs due to residual stress when press-fitted.
図面は本発明の実施例に係り、第1図は複合ビレットの
断面図、第2図は通孔を設けた複合ビレットの断面図、
第3図は成形型の断面図、第4図は複合パイプの断面図
、第5図は鍛造装置に断面図、第6図は複合筒状部品の
断面図、第7図はモータのロータ兼用ハブの断面図であ
る。
1・・・外層ビレット、2・・・内層ビレット、3・・
・複合ビレット、4・・・中子軸、5・・・通孔、6・
・・成形型、7・・・押出口、12・・・複合パイプ、
17・・・筒状複合部品。The drawings relate to embodiments of the present invention; FIG. 1 is a sectional view of a composite billet, FIG. 2 is a sectional view of a composite billet provided with through holes,
Figure 3 is a sectional view of the mold, Figure 4 is a sectional view of the composite pipe, Figure 5 is a sectional view of the forging device, Figure 6 is a sectional view of the composite cylindrical part, and Figure 7 is also used as the rotor of the motor. FIG. 3 is a cross-sectional view of the hub. 1... Outer layer billet, 2... Inner layer billet, 3...
・Composite billet, 4... Core shaft, 5... Through hole, 6.
... Molding die, 7... Extrusion port, 12... Composite pipe,
17...Cylindrical composite part.
Claims (1)
を押出成形するに際し、まず、外層材製の有底筒状ビレ
ット(1)に、内層材製のビレット(2)を嵌入して複
合ビレット(3)を形成し、この複合ビレット(3)の
軸心に通孔(5)を設け、複合ビレット(3)を押出成
形型(6)内に、底部側が押出口(7)側となるように
装填すると共に、通孔(5)に中子軸(4)を挿通し、
複合ビレット(3)を押出口(7)から押出すことで内
外ビレット(1)(2)を拡散接合させつつ複合パイプ
(12)に成形し、次に、この複合パイプ(12)を一
定長さに切断してから型鍛造して複合筒状部品(17)
に成形することを特徴とする複合筒状部品の成形方法。(1) Composite cylindrical part whose inner and outer layers are made of different materials (17)
When extrusion molding, first, a billet made of an inner layer material (2) is fitted into a bottomed cylindrical billet made of an outer layer material (1) to form a composite billet (3), and the composite billet (3) is A through hole (5) is provided in the axial center, and the composite billet (3) is loaded into the extrusion mold (6) with the bottom side facing the extrusion port (7), and the core is inserted into the through hole (5). Insert the shaft (4),
By extruding the composite billet (3) from the extrusion port (7), the inner and outer billets (1) and (2) are diffusion bonded and formed into a composite pipe (12), and then this composite pipe (12) is cut into a certain length. Composite cylindrical parts (17) are made by cutting and die forging.
A method for forming a composite cylindrical part, which is characterized by forming a composite cylindrical part.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP31787788A JPH02165838A (en) | 1988-12-15 | 1988-12-15 | Forming method for composite cylindrical parts |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP31787788A JPH02165838A (en) | 1988-12-15 | 1988-12-15 | Forming method for composite cylindrical parts |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH02165838A true JPH02165838A (en) | 1990-06-26 |
Family
ID=18093057
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP31787788A Pending JPH02165838A (en) | 1988-12-15 | 1988-12-15 | Forming method for composite cylindrical parts |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH02165838A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2021524380A (en) * | 2018-05-22 | 2021-09-13 | エービー サンドビック マテリアルズ テクノロジー | Tubular elements and tubular assemblies |
-
1988
- 1988-12-15 JP JP31787788A patent/JPH02165838A/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2021524380A (en) * | 2018-05-22 | 2021-09-13 | エービー サンドビック マテリアルズ テクノロジー | Tubular elements and tubular assemblies |
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