JP2001225141A - Composite material and its production method - Google Patents

Composite material and its production method

Info

Publication number
JP2001225141A
JP2001225141A JP2000035026A JP2000035026A JP2001225141A JP 2001225141 A JP2001225141 A JP 2001225141A JP 2000035026 A JP2000035026 A JP 2000035026A JP 2000035026 A JP2000035026 A JP 2000035026A JP 2001225141 A JP2001225141 A JP 2001225141A
Authority
JP
Japan
Prior art keywords
dissimilar
base material
alloy
composite material
composite
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
Application number
JP2000035026A
Other languages
Japanese (ja)
Inventor
Yoshitaka Nagai
嘉隆 永井
Katsuyuki Takeya
桂之 竹谷
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.)
YKK Corp
Original Assignee
YKK Corp
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 YKK Corp filed Critical YKK Corp
Priority to JP2000035026A priority Critical patent/JP2001225141A/en
Publication of JP2001225141A publication Critical patent/JP2001225141A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21KMAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
    • B21K25/00Uniting components to form integral members, e.g. turbine wheels and shafts, caulks with inserts, with or without shaping of the components

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Forging (AREA)

Abstract

PROBLEM TO BE SOLVED: To provide a composite material easily supplying two or more kinds of materials, having a strong composite state and easily not coming off each other. SOLUTION: In a composite material in which a dissimilar material is embedded in a base material, the outer periphery of the dissimilar material is embedded in the base material plastically worked, further, the composite material is manufactured by forming while causing the base material 1 to flow into the space around the dissimilar material 2 having a small cross sectional area in a forming space, the dissimilar material 2 is embedded into the base material 1.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は、基礎材料とそれと
は特性の異なる異種材料とを複合させ、それぞれの材料
の特性を複合的に発揮せしめる複合材料、具体的には、
ゴルフクラブヘッドソール、バルブリフター等に応用し
得る複合材料に関するものである。
BACKGROUND OF THE INVENTION The present invention relates to a composite material in which a base material and a different material having different properties from each other are compounded, and the properties of each material are exhibited in a composite manner.
The present invention relates to a composite material applicable to golf club head soles, valve lifters, and the like.

【0002】[0002]

【従来の技術】一般に2種以上の材料を複合するために
は、ボルト締め、カシメ又は溶接による締結、接着によ
る接合等の手段が採られている。例えばゴルフクラブの
ソール部を例にとると、図8に示すようにソール部11
にウエイト部材12を溶接又はロー付けしたもの、ある
いは図9に示すようにくびれ14をもつウエイト部材1
3をカシメにより取付けたもの、さらにはバブルリフタ
ーについては、図10に示すようにバブルリフター15
の表層の一部に保護層16を溶接、ロー付けしたものが
ある。
2. Description of the Related Art Generally, in order to combine two or more kinds of materials, means such as bolting, caulking or welding, and bonding are used. For example, taking a sole portion of a golf club as an example, as shown in FIG.
Or a weight member 1 having a constriction 14 as shown in FIG.
3 is attached by caulking, and further, as for the bubble lifter, as shown in FIG.
The protective layer 16 is welded and brazed to a part of the surface layer.

【0003】しかしながら、これらの従来の固定方式で
は、繰り返し受ける振動、衝撃により、結合、接合が緩
んで異種材料が外れてしまう問題や加工が煩雑であると
いう問題があった。
[0003] However, in these conventional fixing methods, there are problems in that joining and joining are loosened due to repeated vibrations and shocks to cause dissimilar materials to come off, and that processing is complicated.

【0004】[0004]

【発明が解決しようとする課題】本発明は、下記(1)
〜(8)よりなる。 (1)基礎材料中に異種材料を埋め込んでなる複合材に
おいて、異種材料の外周が塑性加工された基礎材料で埋
め込まれてなることを特徴とする複合材料。
The present invention relates to the following (1)
To (8). (1) A composite material in which a heterogeneous material is embedded in a base material, wherein the outer periphery of the heterogeneous material is embedded with a plastically processed base material.

【0005】(2)異種材料が基礎材料と共に塑性加工
されている前記(1)記載の複合材料。 (3)基礎材料がチタン合金、アルミニウム合金、ステ
ンレスの如き塑性加工可能な材料である前記(1)又は
(2)記載の複合材料。
(2) The composite material according to (1), wherein the dissimilar material is plastically worked together with the base material. (3) The composite material as described in (1) or (2) above, wherein the base material is a plastically workable material such as a titanium alloy, an aluminum alloy, and stainless steel.

【0006】(4)異種材料がタングステン合金、銅合
金、超硬合金の如き高比重材料である前記(1)記載の
複合材料。 (5)異種材料が耐熱合金、耐磨耗性合金の如き塑性加
工可能な材料である前記(1)記載の複合材料。
(4) The composite material according to (1), wherein the different material is a high specific gravity material such as a tungsten alloy, a copper alloy, and a cemented carbide. (5) The composite material as described in (1) above, wherein the dissimilar material is a material that can be subjected to plastic working such as a heat-resistant alloy or a wear-resistant alloy.

【0007】(6)成形用上型と下型の対向面に広がる
成形空間部に材料押出部を開口させ、該材料押出部に基
礎材料を充填し、さらにその上に基礎材料より断面積の
小さい異種材料を継ぎ足し、これら基礎材料および異種
材料を加熱しながら押圧し、成形空間部に押出して塑性
加工し、同時に断面積の小さい異種材料の周縁の空間に
も基礎材料を流動させながら成形し、異種材料を基礎材
料中に埋め込むことを特徴とする複合材料の製造方法。
特にゴルフクラブヘッドの製造に際しては押圧方向とは
異なる方向の成形空間部に押出して塑性加工する。
(6) A material extruding portion is opened in a molding space extending over the opposing surfaces of the upper mold and the lower mold, and the material extruding portion is filled with a base material. A small dissimilar material is added, these basic materials and dissimilar materials are pressed while heating, extruded into the forming space and plastically processed, and at the same time, the base material is formed while flowing in the peripheral space of the dissimilar material having a small cross-sectional area. A method for producing a composite material, comprising embedding a dissimilar material in a base material.
In particular, when manufacturing a golf club head, the golf club head is extruded into a forming space in a direction different from the pressing direction and plastically processed.

【0008】(7)基礎材料と異種材料の少なくとも一
方を塑性加工温度まで加熱して成形する前記(6)記載
の複合材料の製造方法。 (8)基礎材料がチタン合金、アルミニウム合金、ステ
ンレスの如き塑性加工可能な材料であり、異種材料がタ
ングステン合金、銅合金、超硬合金の如き高比重材料又
は耐熱合金、耐摩耗性合金の如き塑性加工可能な材料で
ある前記(6)又は(7)記載の複合材料の製造方法。
(7) The method for producing a composite material according to (6), wherein at least one of the base material and the dissimilar material is heated to a plastic working temperature and molded. (8) The base material is a plastically workable material such as a titanium alloy, an aluminum alloy, or stainless steel, and the different material is a high specific gravity material such as a tungsten alloy, a copper alloy, or a cemented carbide, or a heat-resistant alloy or a wear-resistant alloy. The method for producing a composite material according to the above (6) or (7), wherein the composite material is a material that can be subjected to plastic working.

【0009】本発明の複合材料の基礎材料として用いら
れる材料は上記(3)に記載したチタン合金、アルミニ
ウム合金、ステンレスの如き塑性加工可能な材料である
が、とりわけ下記一般式(I)〜(IV)で示される超塑
性を有する急冷凝固Al基合金が好適に用いられる。
The material used as a basic material of the composite material of the present invention is a material which can be subjected to plastic working such as the titanium alloy, aluminum alloy and stainless steel described in the above (3), and particularly the following general formulas (I) to (I). A rapidly solidified Al-based alloy having superplasticity shown in IV) is preferably used.

【0010】(I)Ala1be (II)Ala1(b-c)2ce (III)Ala1(b-d)3de (IV)Ala1(b-c-d)2c3de (ただし、M1:Mn,Fe,Co,Ni,Moから選
ばれる少なくとも1種の元素、M2:V,Cr,Wから
選ばれる少なくとも1種の元素、M3:Li,Ca,M
g,Si,Cu,Znから選ばれる少なくとも1種の元
素、X:Nb,Hf,Ta,Y,Zr,Ti,Ag,希
土類元素および希土類元素の集合体(Mm:ミッシュメ
タル)から選ばれる少なくとも1種の元素、a,b,
c,d,eは原子パーセントで75≦a≦97、0.5
≦b≦15、0.1≦c≦5、0.5≦d≦5、0.5
≦e≦10)
(I) Al a M 1b X e (II) Al a M 1 (bc) M 2c X e (III) Al a M 1 (bd) M 3d X e (IV) Al a M 1 (bcd) M 2c M 3d X e (where M 1 : at least one element selected from Mn, Fe, Co, Ni, Mo; M 2 : at least one element selected from V, Cr, W; M 3 : Li, Ca, M
g, at least one element selected from Si, Cu, Zn, X: at least selected from Nb, Hf, Ta, Y, Zr, Ti, Ag, a rare earth element and an aggregate of rare earth elements (Mm: misch metal) One element, a, b,
c, d, and e are atomic percentages of 75 ≦ a ≦ 97, 0.5
≦ b ≦ 15, 0.1 ≦ c ≦ 5, 0.5 ≦ d ≦ 5, 0.5
≦ e ≦ 10)

【0011】異種材料としては、前記(4)に示したタ
ングステン合金、銅合金、超硬合金の如き高比重材料や
(5)に示した耐熱合金、耐摩耗性合金の如き塑性加工
可能な材料が用いられる。前者は複合過程において、主
としてそのままの形状を保って基礎材料の塑性流動によ
って包み込まれる。後者は基礎材料の塑性流動によって
包み込まれると共に自身も塑性変形して、表層の一部を
形成する。
The different materials include high specific gravity materials such as the tungsten alloys, copper alloys and cemented carbides described in (4) above, and materials capable of being plastically processed such as heat resistant alloys and wear resistant alloys described in (5). Is used. The former is wrapped by the plastic flow of the base material while maintaining its original shape in the compounding process. The latter is wrapped by the plastic flow of the base material and is also plastically deformed to form a part of the surface layer.

【0012】これを図面によって説明すると、図1にお
いて、1は基礎材料、2は異種材料で特に高比重高硬度
の材料である。これを上型3と下型4よりなる成形型の
上型3の材料供給口5に、まず基礎材料1を装入し、そ
の上に異種材料2を装入する。異種材料2は中央部にく
びれ部をもち、その最大径の部分の面積は、前記材料供
給口5の断面積より小さくしてある。これを上型3の内
部に設けた加熱体6により加熱しながら、ステム7によ
り押圧し、塑性加工する。
This will be described with reference to the drawings. In FIG. 1, reference numeral 1 denotes a base material, and 2 denotes a dissimilar material, particularly a material having a high specific gravity and a high hardness. First, the base material 1 is charged into the material supply port 5 of the upper mold 3 including the upper mold 3 and the lower mold 4, and the different material 2 is charged thereon. The dissimilar material 2 has a constricted portion at the center, and the area of the largest diameter portion is smaller than the cross-sectional area of the material supply port 5. This is pressed by a stem 7 while being heated by a heating body 6 provided inside the upper die 3 to perform plastic working.

【0013】塑性加工すると図2に示すように、基礎材
料1は押圧方向の直角方向に広がり、同時に異種材料2
の周囲のキャビティに入り込み、異種材料2を包み込む
ように埋め込む。
As shown in FIG. 2, when the plastic working is performed, the base material 1 spreads in a direction perpendicular to the pressing direction, and
, And is embedded so as to enclose the dissimilar material 2.

【0014】図3は異種材料2’として塑性加工可能な
材料を用いた例である。異種材料2’は基礎材料1の上
端に一部埋め込んだ状態で材料供給口5に装入し、これ
を押圧して成形する。すると図4に示すように、基礎材
料1が押圧方向の直角方向に広がり、ついで異種材料
2’が塑性加工される。この場合、異種材料2’は基礎
材料1の断面積より小さい断面積をもち、周囲にキャビ
ティが存在することと、下部の一部が基礎材料1の上端
に埋め込まれていることにより、基礎材料1は上記キャ
ビティ内に塑性流動するとともに、異種材料2’の基礎
材料1に埋め込まれた部分は先に、押圧方向と直角な方
向に流動し、キャビティ部分の基礎材料1が遅れて同方
向に流動するので、異種材料2’の断面は逆T形状とな
る。このため、異種材料2’は基礎材料から容易に脱落
しないようになる。
FIG. 3 shows an example in which a material which can be subjected to plastic working is used as the dissimilar material 2 '. The dissimilar material 2 ′ is inserted into the material supply port 5 while partially embedded in the upper end of the base material 1, and is pressed to be formed. Then, as shown in FIG. 4, the base material 1 spreads in a direction perpendicular to the pressing direction, and then the dissimilar material 2 'is plastically worked. In this case, the dissimilar material 2 ′ has a cross-sectional area smaller than the cross-sectional area of the base material 1, the existence of a cavity around the base material 1, and the lower part of the base material 1 being embedded in the upper end of the base material 1. 1 flows plastically into the cavity, and the portion of the dissimilar material 2 'embedded in the base material 1 first flows in a direction perpendicular to the pressing direction, and the base material 1 in the cavity portion is delayed in the same direction. Since it flows, the cross section of the dissimilar material 2 'has an inverted T shape. Therefore, the dissimilar material 2 'does not easily fall off from the base material.

【0015】図5は、異種材料2を2箇所に分け、それ
ぞれステム7により基礎材料1と共に型内に押圧し一体
に成形した例である。異種材料2は適宜の個数設けるこ
とができる。
FIG. 5 shows an example in which the dissimilar material 2 is divided into two parts, each of which is pressed together with the base material 1 by a stem 7 into a mold and integrally formed. An appropriate number of dissimilar materials 2 can be provided.

【0016】図6はバルブリフターに応用した例で、基
礎材料1で本体部を形成し、その上面に異種材料2を包
み埋め込んだ例である。製造を行うに際しては、上記と
同様に押圧方向とは異なる方向の成形空間部に押出して
成形加工することも可能であるとともに、押圧方向と同
方向の成形空間部に押圧して塑性加工することも可能で
ある。図7はゴルフクラブのソール部を基礎材料1で構
成し、ウエイト部材を異種材料2をもって構成して、前
述の図1、図2で説明した方法に準じて成形した例であ
る。なお、本発明において、基礎材料中に異種材料を埋
め込んだ状態とは異種材料の全表面を基礎材料により被
覆した状態及び製造の時の押圧面以外の面を基礎材料に
より被覆した状態を示す。
FIG. 6 shows an example in which the present invention is applied to a valve lifter, in which a main body is formed of a base material 1 and a different material 2 is wrapped and embedded on the upper surface thereof. When manufacturing, it is also possible to extrude into a molding space part in a direction different from the pressing direction and perform molding processing in the same manner as described above, and to perform plastic processing by pressing into the molding space part in the same direction as the pressing direction. Is also possible. FIG. 7 shows an example in which the sole portion of the golf club is formed of the base material 1 and the weight member is formed of the dissimilar material 2 and molded according to the method described with reference to FIGS. In the present invention, the state in which the different material is embedded in the basic material refers to a state in which the entire surface of the different material is covered with the basic material and a state in which the surface other than the pressing surface at the time of manufacturing is covered with the basic material.

【0017】[0017]

【発明の実施の形態】以下具体的な実施例によって本発
明を説明する。合金製のクラブヘッドはフェース部、フ
ェース部に続くホーゼル部、クラウン部、ソール部で主
として構成され、クラウン部とソール部とは一体となっ
て本体部を形成する。ソール部の内側に比重の大きな異
種合金を埋め込むことにより、ゴルフクラブのウエイト
として利用でき、かつソールの重心(クラブヘッドの重
心)をコントロールすることができる。
DESCRIPTION OF THE PREFERRED EMBODIMENTS The present invention will be described below with reference to specific examples. The alloy club head mainly includes a face portion, a hosel portion following the face portion, a crown portion, and a sole portion, and the crown portion and the sole portion are integrally formed to form a main body portion. By embedding a different alloy having a large specific gravity inside the sole portion, the alloy can be used as a weight of a golf club and the center of gravity of the sole (the center of gravity of the club head) can be controlled.

【0018】図1、2に示した上型3、下型4を成形部
がソール部の形になるように構成し、これにソール部を
形成する基礎材料として、JIS 5052アルミニウ
ム合金、AlbalNi10Cu1.0Ti1.0Zr1.0(wt
%)、急冷凝固アルミニウム合金よりなるものを、さら
にウエイト部を形成する異種材料としてCu,W,F
e,Tiよりなるものを材料供給口に装入し、400〜
600℃に加圧しながら型内に向って押圧成形する。
The upper mold 3 and the lower mold 4 shown in FIGS. 1 and 2 are formed so that the molding part has the shape of a sole part, and the base material for forming the sole part is JIS 5052 aluminum alloy, Al bal. Ni 10 Cu 1.0 Ti 1.0 Zr 1.0 (wt
%), A rapidly solidified aluminum alloy, and Cu, W, F
e, Ti is charged into the material supply port, and 400 to
While pressurizing at 600 ° C., press molding is performed toward the inside of the mold.

【0019】かかる方法によるとウエイト部は外部側に
露出することがなく、クラウン部、フェース部と組合せ
てゴルフクラブヘッドを構成した場合、カシメ法によっ
て製造した場合と違って、ウエイト部を構成する異種材
料が外部に露出せず、基礎材料と異種材料の境界面から
の腐食等が発生しない。
According to this method, the weight portion is not exposed to the outside, and when the golf club head is formed in combination with the crown portion and the face portion, the weight portion is formed differently from the case where the golf club head is manufactured by the caulking method. The dissimilar material is not exposed to the outside, and corrosion or the like does not occur from the interface between the base material and the dissimilar material.

【0020】つぎにバルブリフターの例を示すとAl−
Si系合金AlbalNi7Cu1.5Mn 2.5Ti1.0Zr1.0
Mg0.2(wt%)、急冷凝固アルミニウム合金よりな
るアルミニウム合金を基礎材料とし、異種材料としてS
iC,SKD61,SKH9,超硬合金よりなる耐摩耗
性を用い、図1、図2に示した成形法に準じて成形す
る。このように形成したバルブリフターはアルミニウム
合金を主体としながら、カム動作の衝撃・摩耗に耐える
ものを提供することができる。
Next, an example of a valve lifter will be described.
Si-based alloy AlbalNi7Cu1.5Mn 2.5Ti1.0Zr1.0
Mg0.2(Wt%), faster than rapidly solidified aluminum alloy
Aluminum alloy as a base material and S as a different material
Wear resistance made of iC, SKD61, SKH9, cemented carbide
Molding is performed according to the molding method shown in FIGS.
You. The valve lifter thus formed is made of aluminum
Withstands the impact and wear of cam operation while mainly using alloy
Things can be provided.

【0021】[0021]

【発明の効果】本発明によれば、基礎材料に特性の違っ
た異種材料を確実に固定することができる。又、異種材
料は必要個数の複数個を同時に固定することができる。
異種材料の材質を高比重材料に選択することにより、出
発時の異種材料の形そのままで基礎材料に埋め込むこと
ができる。あるいは塑性加工可能な材料を選択すること
により、出発の異種材料を変形させて埋め込むことがで
きる。
According to the present invention, different materials having different characteristics can be securely fixed to the base material. In addition, a required number of different materials can be simultaneously fixed.
By selecting the material of the dissimilar material as the high specific gravity material, the dissimilar material at the time of departure can be embedded in the basic material as it is. Alternatively, by selecting a material that can be subjected to plastic working, the starting dissimilar material can be deformed and embedded.

【0022】いずれにしても脱落しにくい異種材料を基
礎材料に埋め込まれることにより衝撃や摩耗に耐える複
合材料を容易に得ることができる。
In any case, a composite material resistant to impact and abrasion can be easily obtained by embedding a dissimilar material which does not easily fall into the base material.

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

【図1】本発明の実施例の成形開始時の説明図である。FIG. 1 is an explanatory diagram at the start of molding in an example of the present invention.

【図2】図1の成形後の説明図である。FIG. 2 is an explanatory view after molding of FIG. 1;

【図3】本発明の他の実施例の成形開始時の説明図であ
る。
FIG. 3 is an explanatory view of another embodiment of the present invention at the start of molding.

【図4】図3の成形後の説明図である。FIG. 4 is an explanatory view after molding of FIG. 3;

【図5】変形例の説明図である。FIG. 5 is an explanatory diagram of a modified example.

【図6】本発明を適用したバルブリフターの説明図であ
る。
FIG. 6 is an explanatory diagram of a valve lifter to which the present invention is applied.

【図7】本発明を適用したゴルフクラブヘッドソール部
の説明図である。
FIG. 7 is an explanatory diagram of a golf club head sole portion to which the present invention is applied.

【図8】従来のゴルフクラブヘッドソール部にウエイト
部材を溶接又はロー付けにより接合した例の説明図であ
る。
FIG. 8 is an explanatory view of an example in which a weight member is joined to a conventional golf club head sole portion by welding or brazing.

【図9】従来のゴルフクラブヘッドソール部にウエイト
部材をカシメ加工によりとり付けた例の説明図である。
FIG. 9 is an explanatory diagram of an example in which a weight member is attached to a conventional golf club head sole portion by caulking.

【図10】従来のバルブリフタの説明図である。FIG. 10 is an explanatory diagram of a conventional valve lifter.

【符号の説明】[Explanation of symbols]

1 基礎材料 2,2’ 異種材料 3 上型 4 下型 5 材料供給部 6 加熱体 7 ステム DESCRIPTION OF SYMBOLS 1 Basic material 2, 2 'Different material 3 Upper mold 4 Lower mold 5 Material supply part 6 Heating body 7 Stem

Claims (8)

【特許請求の範囲】[Claims] 【請求項1】 基礎材料中に異種材料を埋め込んでなる
複合材において、異種材料の外周が塑性加工された基礎
材料で埋め込まれてなることを特徴とする複合材料。
1. A composite material in which a dissimilar material is embedded in a base material, wherein the outer periphery of the dissimilar material is embedded with a plastically processed base material.
【請求項2】 異種材料が基礎材料と共に塑性加工され
ている請求項1記載の複合材料。
2. The composite material according to claim 1, wherein the dissimilar material is plastically worked together with the base material.
【請求項3】 基礎材料がチタン合金、アルミニウム合
金、ステンレスの如き塑性加工可能な材料である請求項
1又は2記載の複合材料。
3. The composite material according to claim 1, wherein the base material is a plastically workable material such as a titanium alloy, an aluminum alloy, and stainless steel.
【請求項4】 異種材料がタングステン合金、銅合金、
超硬合金の如き高比重材料である請求項1記載の複合材
料。
4. The different material is a tungsten alloy, a copper alloy,
The composite material according to claim 1, which is a high specific gravity material such as a cemented carbide.
【請求項5】 異種材料が耐熱合金、耐磨耗性合金の如
き塑性加工可能な材料である請求項1記載の複合材料。
5. The composite material according to claim 1, wherein the dissimilar material is a material that can be subjected to plastic working such as a heat-resistant alloy or a wear-resistant alloy.
【請求項6】 成形用上型と下型の対向面に広がる成形
空間部に材料押出部を開口させ、該材料押出部に基礎材
料を充填し、さらにその上に基礎材料より断面積の小さ
い異種材料を継ぎ足し、これら基礎材料および異種材料
を加熱しながら押圧し、成形空間部に押出して塑性加工
し、同時に断面積の小さい異種材料の周縁の空間にも基
礎材料を流動させながら成形し、異種材料を基礎材料中
に埋め込むことを特徴とする複合材料の製造方法。
6. A material extruding portion is opened in a molding space portion extending on a facing surface of an upper mold and a lower mold, and the material extruding portion is filled with a base material, and further has a smaller sectional area than that of the base material. The dissimilar materials are added, these basic materials and dissimilar materials are pressed while being heated, extruded into a molding space and plastically processed, and at the same time, the base material is molded while flowing in the peripheral space of the dissimilar material having a small cross-sectional area, A method for producing a composite material, comprising embedding a dissimilar material into a base material.
【請求項7】 基礎材料と異種材料の少なくとも一方を
塑性加工温度まで加熱して成形する請求項6記載の複合
材料の製造方法。
7. The method for producing a composite material according to claim 6, wherein at least one of the base material and the dissimilar material is heated to a plastic working temperature and molded.
【請求項8】 基礎材料がチタン合金、アルミニウム合
金、ステンレスの如き塑性加工可能な材料であり、異種
材料がタングステン合金、銅合金、超硬合金の如き高比
重材料又は耐熱合金、耐摩耗性合金の如き塑性加工可能
な材料である請求項6又は7記載の複合材料の製造方
法。
8. The base material is a plastically workable material such as a titanium alloy, an aluminum alloy, or stainless steel, and the different material is a high specific gravity material such as a tungsten alloy, a copper alloy, or a cemented carbide, or a heat-resistant alloy or a wear-resistant alloy. The method for producing a composite material according to claim 6, wherein the composite material is a material capable of plastic working.
JP2000035026A 2000-02-14 2000-02-14 Composite material and its production method Pending JP2001225141A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2000035026A JP2001225141A (en) 2000-02-14 2000-02-14 Composite material and its production method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2000035026A JP2001225141A (en) 2000-02-14 2000-02-14 Composite material and its production method

Publications (1)

Publication Number Publication Date
JP2001225141A true JP2001225141A (en) 2001-08-21

Family

ID=18559285

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2000035026A Pending JP2001225141A (en) 2000-02-14 2000-02-14 Composite material and its production method

Country Status (1)

Country Link
JP (1) JP2001225141A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2018029760A (en) * 2016-08-24 2018-03-01 基宏 蘇 Method for manufacturing iron golf club head by heterogeneous metal bonding

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2018029760A (en) * 2016-08-24 2018-03-01 基宏 蘇 Method for manufacturing iron golf club head by heterogeneous metal bonding

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