TW201313363A - Method for integrally forming a composite metal - Google Patents
Method for integrally forming a composite metal Download PDFInfo
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- TW201313363A TW201313363A TW101134720A TW101134720A TW201313363A TW 201313363 A TW201313363 A TW 201313363A TW 101134720 A TW101134720 A TW 101134720A TW 101134720 A TW101134720 A TW 101134720A TW 201313363 A TW201313363 A TW 201313363A
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- 239000002184 metal Substances 0.000 title claims abstract description 127
- 229910052751 metal Inorganic materials 0.000 title claims abstract description 127
- 239000002131 composite material Substances 0.000 title claims abstract description 72
- 238000000034 method Methods 0.000 title claims abstract description 35
- 239000000956 alloy Substances 0.000 claims abstract description 60
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 57
- 238000005245 sintering Methods 0.000 claims abstract description 30
- 239000000463 material Substances 0.000 claims abstract description 12
- 238000001746 injection moulding Methods 0.000 claims abstract description 7
- 239000000843 powder Substances 0.000 claims description 64
- 238000000465 moulding Methods 0.000 claims description 32
- 238000002360 preparation method Methods 0.000 claims description 12
- 150000002739 metals Chemical class 0.000 claims description 11
- 239000011230 binding agent Substances 0.000 claims description 8
- 238000002844 melting Methods 0.000 claims description 7
- 230000008018 melting Effects 0.000 claims description 7
- 238000003825 pressing Methods 0.000 claims description 6
- 239000004372 Polyvinyl alcohol Substances 0.000 claims description 2
- 238000010438 heat treatment Methods 0.000 claims description 2
- 239000012188 paraffin wax Substances 0.000 claims description 2
- 229920002689 polyvinyl acetate Polymers 0.000 claims description 2
- 239000011118 polyvinyl acetate Substances 0.000 claims description 2
- 229920002451 polyvinyl alcohol Polymers 0.000 claims description 2
- 210000001161 mammalian embryo Anatomy 0.000 claims 1
- 239000012255 powdered metal Substances 0.000 abstract 3
- 239000007769 metal material Substances 0.000 abstract 2
- 238000000748 compression moulding Methods 0.000 abstract 1
- 230000005484 gravity Effects 0.000 description 25
- 238000005266 casting Methods 0.000 description 7
- 238000004519 manufacturing process Methods 0.000 description 7
- 229910001030 Iron–nickel alloy Inorganic materials 0.000 description 4
- OWUGOENUEKACGV-UHFFFAOYSA-N [Fe].[Ni].[W] Chemical compound [Fe].[Ni].[W] OWUGOENUEKACGV-UHFFFAOYSA-N 0.000 description 3
- 238000002347 injection Methods 0.000 description 3
- 239000007924 injection Substances 0.000 description 3
- 238000005520 cutting process Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000002861 polymer material Substances 0.000 description 2
- 238000006116 polymerization reaction Methods 0.000 description 2
- 238000003672 processing method Methods 0.000 description 2
- 239000001993 wax Substances 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 238000000889 atomisation Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 238000005469 granulation Methods 0.000 description 1
- 230000003179 granulation Effects 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- UGKDIUIOSMUOAW-UHFFFAOYSA-N iron nickel Chemical compound [Fe].[Ni] UGKDIUIOSMUOAW-UHFFFAOYSA-N 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
Classifications
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- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63B—APPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
- A63B53/00—Golf clubs
- A63B53/04—Heads
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63B—APPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
- A63B53/00—Golf clubs
- A63B53/04—Heads
- A63B53/047—Heads iron-type
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/22—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces for producing castings from a slip
- B22F3/225—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces for producing castings from a slip by injection molding
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63B—APPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
- A63B53/00—Golf clubs
- A63B53/04—Heads
- A63B2053/0491—Heads with added weights, e.g. changeable, replaceable
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63B—APPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
- A63B2209/00—Characteristics of used materials
- A63B2209/02—Characteristics of used materials with reinforcing fibres, e.g. carbon, polyamide fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
- B22F2998/10—Processes characterised by the sequence of their steps
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- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Physical Education & Sports Medicine (AREA)
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Mechanical Engineering (AREA)
- Powder Metallurgy (AREA)
- Golf Clubs (AREA)
Abstract
Description
本發明係關於一種複合金屬之一體成型方法，特別是運用於異質金屬或不同比重合金之一體成型方法。 The invention relates to a method for forming a composite metal body, in particular to a method for forming a heterogeneous metal or a different specific gravity alloy.
請配合參照第1圖，習知複合金屬配重體之成型方法，係如中華民國公告M291310號「具有高比重複合配重體之高爾夫球桿頭」專利案所示，其係於一高爾夫球桿頭的本體91上設有一高比重的複合配重體92，該配重體92係由異質金屬之一配重外層921及一配重內層922構成。 Please refer to Figure 1 for a method of forming a composite metal weight body, as shown in the patent of the Republic of China Bulletin M291310 "Golf Club Head with High Specific Gravity Weight Body", which is attached to a golf ball. The body 91 of the club head is provided with a composite weight body 92 of high specific gravity, and the weight body 92 is composed of a weighted outer layer 921 and a weight inner layer 922 of a heterogeneous metal.
其中該配重體92之成型方法，係先運用鑄造技術製作該配重外層921，再運用壓合技術使該配重內層922之金屬粉末與該配重外層921互相結合，並運用燒結技術使該配重內層922成型，最後即可將該配重體92焊接固定於該本體91。 The method for molding the weight body 92 is to first make the outer layer 921 of the weight by using a casting technique, and then use a pressing technique to combine the metal powder of the inner layer 922 of the weight with the outer layer 921 of the weight, and use the sintering technology. The weight inner layer 922 is molded, and finally the weight body 92 can be welded and fixed to the body 91.
然而，該習知配重體92之成型方法必須先鑄造該配重外層921，再經由壓合及燒結方式使該配重內層922與該配重外層921結合為一體，因此至少必須經過鑄造、壓合及燒結等工序，製作上較不方便。 However, the molding method of the conventional weight body 92 must first cast the weight outer layer 921, and then combine the weight inner layer 922 and the weight outer layer 921 by pressing and sintering, so at least casting must be performed. Processes such as press-fitting and sintering are inconvenient to manufacture.
而且，運用鑄造及燒結方式成型該配重外層921及配重內層922時，由於鑄造及燒結之加工特性不同，對於材料的成型性質要求也有所不同，例如：以相同成分但不同比重的合金分別製作該配重外層921及配重內層922時，該合金材料本身的成型性質必須同時符合鑄造及燒結的加 工特性要求，但是並非所有的合金材料都能夠同時適用於鑄造及燒結成型，因此該習知的成型方法使得材料的選擇受到限制。 Moreover, when the weighted outer layer 921 and the weight inner layer 922 are formed by casting and sintering, the molding properties of the material are different due to different processing characteristics of casting and sintering, for example, alloys having the same composition but different specific gravities When the weight outer layer 921 and the weight inner layer 922 are respectively produced, the molding property of the alloy material itself must conform to the casting and sintering addition. The characteristics of the work require, but not all alloy materials can be applied to both casting and sintering, so the conventional molding method limits the choice of materials.
另外，該習知配重體92之成型方法係先鑄造該配重外層921之後，再壓合及燒結該配重內層922，因此該配重外層921及配重內層922並非同時一體成型，使得該配重外層921及配重內層922之間的結合強度不足。 In addition, the conventional weight body 92 is formed by casting the weight outer layer 921 and then pressing and sintering the weight inner layer 922. Therefore, the weight outer layer 921 and the weight inner layer 922 are not integrally formed at the same time. The bonding strength between the weight outer layer 921 and the weight inner layer 922 is insufficient.
本發明之目的係提供一種複合金屬之一體成型方法，係可簡化製成工序，製作較為方便。 The object of the present invention is to provide a method for forming a composite metal, which can simplify the manufacturing process and is convenient to manufacture.
本發明之另一目的係提供一種複合金屬之一體成型方法，係可使複合金屬之材料選擇較不受限制。 Another object of the present invention is to provide a method for forming a composite metal body which is capable of making the material selection of the composite metal less restrictive.
本發明之又一目的係提供一種複合金屬之一體成型方法，係可提升複合金屬之間的結合強度。 Another object of the present invention is to provide a method for forming a composite metal body which can improve the bonding strength between the composite metals.
根據本發明一種複合金屬之一體成型方法，係包含：一製備步驟，製備至少二種金屬或合金粉末；一成型步驟，利用壓製成型方式將其中一種金屬或合金粉末壓製成一單胚料，再將該單胚料與其他金屬或合金粉末壓製成一複合金屬胚料；及一燒結步驟，將該複合金屬胚料燒結形成一複合金屬成品。 A method for forming a composite metal body according to the present invention comprises: a preparation step of preparing at least two kinds of metal or alloy powders; and a molding step of pressing one of the metal or alloy powders into a single billet by press molding, and then The single blank is pressed into a composite metal blank with another metal or alloy powder; and a sintering step is performed to sinter the composite metal blank to form a composite metal product.
根據本發一種複合金屬之一體成型方法，還可以包含：一製備步驟，製備至少二種金屬或合金粉末；一成型步驟，利用射出成型方式將其中一種金屬或合金粉末注入一模具中以成型一單胚料，再將該單胚料置於另一模具中， 並注入其他金屬或合金粉末以成型一複合金屬胚料；及一燒結步驟，將該複合金屬胚料燒結形成一複合金屬成品。 According to the present invention, a method for forming a composite metal body may further comprise: a preparation step of preparing at least two kinds of metal or alloy powders; and a molding step of injecting one of the metal or alloy powders into a mold by injection molding to form a mold. a single billet, and then placing the single billet in another mold, And injecting another metal or alloy powder to form a composite metal blank; and a sintering step, sintering the composite metal blank to form a composite metal product.
為讓本發明之上述及其他目的、特徵及優點能更明顯易懂，下文特舉本發明之較佳實施例，並配合所附圖式，作詳細說明如下： The above and other objects, features and advantages of the present invention will become more <RTIgt;
請參照第2圖所示，本發明複合金屬之一體成型方法係包含一製備步驟S1、一成型步驟S2及一燒結步驟S3。其中該製備步驟S1係製備至少二種金屬或合金粉末；該成型步驟S2係將該至少二種金屬或合金粉末製成一複合金屬胚料；該燒結步驟S3係將該複合金屬胚料燒結形成一複合金屬成品。 Referring to FIG. 2, the composite metal forming method of the present invention comprises a preparation step S1, a molding step S2 and a sintering step S3. Wherein the preparation step S1 is to prepare at least two kinds of metal or alloy powders; the molding step S2 is to form the at least two metals or alloy powders into a composite metal blank; and the sintering step S3 is to form the composite metal blank by sintering. A composite metal finished product.
該製備步驟S1係製備至少二種金屬或合金粉末，例如：至少二種異質純金屬粉末、至少二種異質合金粉末，或至少二種同質但不同比重的合金粉末。更詳言之，該製備步驟S1可選擇切削法(Machining)、滾磨法(Milling)、霧化法(Atomization)、成粒法(Granulation)、電解堆積法(Electrolytic Deposition)或還原法(Reduction Method)等其中之一，將至少二種異質純金屬製成粉末，以獲得該至少二種異質純金屬粉末。當製備至少二種異質合金粉末或不同比重的合金粉末時，可選擇先將數種純金屬製成粉末後，再將該數種純金屬粉末依照所需比例混合，以獲得該至少二種異質合金粉末，或至少二種同質但不同比重的合金粉末，另外，亦可選擇先製備至少二種異質合金或 不同比重的合金，再將該至少二種異質合金或不同比重的合金製成粉末，同樣可獲得該至少二種異質合金粉末，或至少二種同質但不同比重的合金粉末。 The preparation step S1 is to prepare at least two metal or alloy powders, for example, at least two heterogeneous pure metal powders, at least two heterogeneous alloy powders, or at least two homogeneous but different specific gravity alloy powders. More specifically, the preparation step S1 may be selected by Machining, Milling, Atomization, Granulation, Electrolytic Deposition or Reduction. At least one of the heterogeneous pure metals is powdered to obtain the at least two heterogeneous pure metal powders. When preparing at least two kinds of heteroalloy powders or alloy powders of different specific gravities, it is optional to first make a plurality of pure metals into powders, and then mixing the plurality of pure metal powders according to a desired ratio to obtain the at least two kinds of heterogeneous Alloy powder, or at least two alloy powders of the same homogeneity but different specific gravity, or alternatively, at least two heterogeneous alloys may be prepared first or The alloys of different specific gravities may be further powdered by the at least two heterogeneous alloys or alloys of different specific gravities, and the at least two heteroalloy powders or at least two homogenous but different specific gravity alloy powders may be obtained.
該成型步驟S2係可選擇壓製成型(PM)或射出成型(MIM)其中之一，將該至少二種金屬或合金粉末製成一複合金屬胚料。更詳言之，運用壓製成型(PM)將該至少二種金屬或合金粉末製成該複合金屬胚料時，係採用多數個模具並依序對該至少二種金屬或合金粉末進行多數道壓製，以形成該複合金屬胚料。舉例而言，欲將二種異質純金屬粉末壓製成該複合金屬胚料時，係先將其中一種純金屬粉末填入一模具內壓製成一單胚料，再將該單胚料置於另一模具內，並填入另一種純金屬粉末進行壓製，使該二種異質純金屬粉末被壓製聚合成該複合金屬胚料。該成型步驟S2係以一預定壓力進行壓製，該預定壓力係依據該單胚料及複合金屬胚料之形狀，以及所壓製金屬粉末之材質而有所不同，且該預定壓力較佳為20~100噸。 The forming step S2 is one of press molding (PM) or injection molding (MIM), and the at least two metals or alloy powders are made into a composite metal blank. More specifically, when the at least two metals or alloy powders are formed into the composite metal blank by press molding (PM), a plurality of molds are used, and the at least two metals or alloy powders are sequentially pressed in a plurality of ways. To form the composite metal blank. For example, when two kinds of heterogeneous pure metal powders are to be pressed into the composite metal blank, one of the pure metal powders is first filled into a mold and pressed into a single billet, and then the single billet is placed in another The mold is filled with another pure metal powder for pressing, and the two heterogeneous pure metal powders are press-polymerized into the composite metal billet. The molding step S2 is performed at a predetermined pressure, which is different according to the shape of the single blank and the composite metal blank, and the material of the pressed metal powder, and the predetermined pressure is preferably 20 to 100. Ton.
再者，運用射出成型(MIM)將該至少二種金屬或合金粉末製成該複合金屬胚料時，係採用多數個射出模具並依序將該至少二種金屬或合金粉末進行多數道射出，以形成該複合金屬胚料。舉例而言，欲將二種異質純金屬粉末射出成型該複合金屬胚料時，係先將其中一種純金屬粉末注入一射出模具中以成型為一單胚料，再將該單胚料置於另一射出模具內，並注入另一種純金屬粉末，使該二種異質純金屬粉末在該模具內聚合成該複合金屬胚料。另外，進行射出成型時，可以在該二種異質金屬粉末中添加高分 子材料作為黏結劑，以增加該二種異質純金屬粉末之聚合力，所添加之高分子材料可為聚乙烯醇、聚醋酸乙烯酯或蠟基黏結劑等其中之一，且較佳選擇為蠟基黏結劑，更佳為石蠟(Paraffin)。 Furthermore, when the at least two metals or alloy powders are formed into the composite metal blank by injection molding (MIM), a plurality of injection molds are used, and at least two kinds of metal or alloy powders are sequentially ejected in a plurality of ways. To form the composite metal blank. For example, when two kinds of heterogeneous pure metal powders are to be injection molded into the composite metal blank, one of the pure metal powders is first injected into an injection mold to form a single blank, and then the single blank is placed. Another shot is injected into the mold and another pure metal powder is injected to polymerize the two heterogeneous pure metal powders into the composite metal billet in the mold. In addition, when injection molding is performed, high scores can be added to the two kinds of heterogeneous metal powders. The sub-material is used as a binder to increase the polymerization force of the two heterogeneous pure metal powders, and the added polymer material may be one of polyvinyl alcohol, polyvinyl acetate or wax-based binder, and is preferably selected as A wax-based adhesive, more preferably paraffin.
該燒結步驟S3係將該複合金屬胚料燒結形成一複合金屬成品。更詳言之，該燒結步驟S3係將該複合金屬胚料加熱至一預定溫度，並持續一預定時間，使聚合形成該複合金屬胚料之該至少二種金屬或合金粉末的表面再結晶，以提升各該金屬或合金粉末之間的機械強度及結合強度，進而一體形成該複合金屬成品。其中，該燒結步驟S3之預定溫度係依據所燒結金屬或合金粉末之材質及比重而有所不同，該預定溫度一般係低於所燒結金屬或合金粉末之熔點，例如：欲將二種不同熔點的金屬或合金粉末燒結形成該複合金屬成品時，該預定溫度係低於熔點較低之該金屬或合金粉末的熔點，且較佳為1370~1450℃，而該燒結步驟S3之預定時間較佳為1小時。另外，欲將至少二種同質但不同比重的合金粉末燒結形成該複合金屬成品時，該預定溫度係依據所燒結合金粉末之比重而有所不同，一般而言，合金材料的比重越大則熔點越高，亦即比重越大則該預定溫度也越高。 The sintering step S3 is to sinter the composite metal blank to form a composite metal product. More specifically, the sintering step S3 is to heat the composite metal billet to a predetermined temperature for a predetermined time to recrystallize the surface of the at least two metal or alloy powders which are polymerized to form the composite metal billet. The composite metal finished product is integrally formed by increasing the mechanical strength and bonding strength between the respective metal or alloy powders. Wherein, the predetermined temperature of the sintering step S3 is different according to the material and specific gravity of the sintered metal or alloy powder, and the predetermined temperature is generally lower than the melting point of the sintered metal or alloy powder, for example, two different melting points are to be used. When the metal or alloy powder is sintered to form the finished metal product, the predetermined temperature is lower than the melting point of the metal or alloy powder having a lower melting point, and is preferably 1370 to 1450 ° C, and the predetermined time of the sintering step S3 is preferably It is 1 hour. In addition, when at least two homogeneous but different specific gravity alloy powders are to be sintered to form the composite metal product, the predetermined temperature varies depending on the specific gravity of the sintered alloy powder. Generally, the higher the specific gravity of the alloy material, the melting point. The higher, that is, the greater the specific gravity, the higher the predetermined temperature.
此外，進行燒結步驟S3時，為避免金屬或合金粉末與大氣接觸而氧化，可使用還原性氣體以阻止高溫時形成有害的氧化層。 Further, when the sintering step S3 is performed, in order to prevent oxidation of the metal or alloy powder in contact with the atmosphere, a reducing gas may be used to prevent formation of a harmful oxide layer at a high temperature.
本發明複合金屬之一體成型方法亦可於該成型步驟S2之後施以一脫黏步驟S4。更詳言之，該成型步驟S2若 選擇射出成型(MIM)時，係於該至少二種金屬或合金粉末添加高分子材料作為黏結劑，以增加該金屬或合金粉末之聚合力，因此該成型步驟S2之後，可藉由該脫黏步驟S4去除該黏結劑，該脫黏步驟S4係可採用加熱方式以去除該黏結劑。 The composite metal one-piece molding method of the present invention may also apply a debonding step S4 after the molding step S2. More specifically, if the molding step S2 is When injection molding (MIM) is selected, a polymer material is added as a binder to the at least two metals or alloy powders to increase the polymerization force of the metal or alloy powder, and thus the debonding can be performed after the molding step S2. Step S4 removes the binder, and the debonding step S4 may be performed by heating to remove the binder.
本發明複合金屬之一體成型方法亦可於該燒結步驟S3之後施以一表面修整步驟S5。更詳言之，該表面修整步驟S5係可運用切削、研磨或切割等方式，對該複合金屬成品表面進行修整，以獲得所需配件。 The composite metal one-piece molding method of the present invention may also apply a surface finishing step S5 after the sintering step S3. More specifically, the surface finishing step S5 can be used to trim the surface of the finished metal product by cutting, grinding or cutting to obtain the desired fitting.
本發明之成型方法係可運用於各種複合金屬配件之製作，舉例而言，製作一高爾夫球桿頭之雙比重配重體時，係先進行製備步驟S1，以製備二種不同比重的鎢-鐵-鎳(W-Fe-Ni)合金粉末，再依序進行成型步驟S2及燒結步驟S3，以形成該雙比重配重體，其中，該製備步驟S1、成型步驟S2及燒結步驟S3之詳細操作方式已如前述，故不再贅述。 The molding method of the present invention can be applied to the production of various composite metal fittings. For example, when manufacturing a double specific gravity weight body of a golf club head, the preparation step S1 is first performed to prepare two different specific gravity tungsten. Iron-nickel (W-Fe-Ni) alloy powder, which is sequentially subjected to a molding step S2 and a sintering step S3 to form the double specific gravity weight body, wherein the preparation step S1, the molding step S2 and the sintering step S3 are detailed The operation mode is as described above, so it will not be described again.
由於該雙比重配重體係由二種不同比重的鎢-鐵-鎳合金所構成，例如：該雙比重配重體可為內、外雙層結構，外層可採用低比重(9.3~14g/cm3)的鎢-鐵-鎳合金，內層可採用高比重(14~18g/cm3)的鎢-鐵-鎳合金，因此當該雙比重配重體利用焊接技術結合於一高爾夫球桿頭時，不僅可以克服高比重合金因為熔點高，所導致焊接困難及易產生裂紋的問題，也可以解決高比重合金與該高爾夫球桿頭本體的色差問題。 Since the double specific gravity system is composed of two different proportions of tungsten-iron-nickel alloy, for example, the double specific gravity weight body can be an inner and outer double layer structure, and the outer layer can adopt a low specific gravity (9.3 to 14 g/cm). 3 ) Tungsten-iron-nickel alloy, the inner layer can be a tungsten-iron-nickel alloy with a high specific gravity (14~18g/cm 3 ), so when the double specific gravity weight body is welded to a golf club head by welding technology In addition, it is possible to overcome the problem that the high specific gravity alloy has a high melting point, causes welding difficulties and is prone to cracking, and can also solve the problem of chromatic aberration between the high specific gravity alloy and the golf club head body.
如上所述，本發明複合金屬之一體成型方法，係將該 至少二種金屬或合金粉末，經由成型步驟S2製成該複合金屬胚料後，再施以一次燒結，使該至少二種金屬或合金粉末一體燒結成型為複合金屬成品，以達到簡化製成工序，使製作更為方便之功效。 As described above, the composite metal forming method of the present invention is After at least two kinds of metal or alloy powders are formed into the composite metal blank through the molding step S2, and then sintered once, and the at least two kinds of metal or alloy powders are integrally sintered into a composite metal product to simplify the manufacturing process. To make the production more convenient.
本發明複合金屬之一體成型方法，係將該至少二種金屬或合金粉末成型為該複合金屬胚料後，即一體燒結成型為複合金屬成品，故利用“單一加工方式”即可製作，因此在材料的選擇方面，較不需要考慮材料本身對於加工法的適應性因素，具有材料選擇較不受限制之功效。 The method for forming a composite metal according to the present invention is characterized in that the at least two kinds of metal or alloy powders are formed into the composite metal blank, that is, integrally sintered into a composite metal product, so that the "single processing method" can be used, so In terms of material selection, it is less necessary to consider the adaptability of the material itself to the processing method, and the effect of material selection is not limited.
本發明複合金屬之一體成型方法，係將該至少二種金屬或合金粉末成型為該複合金屬胚料後，即一體燒結成型為複合金屬成品，使該至少二種金屬或合金粉末係的表面係同時形成再結晶層，具有提升各該金屬或合金粉末之間的機械強度及結合強度之功效。 The method for forming a composite metal according to the present invention is to form at least two metal or alloy powders into the composite metal blank, that is, integrally sintered into a composite metal product, and the surface of the at least two metal or alloy powder systems is formed. At the same time, a recrystallized layer is formed, which has the effect of improving the mechanical strength and bonding strength between the respective metal or alloy powders.
雖然本發明已利用上述較佳實施例揭示，然其並非用以限定本發明，任何熟習此技藝者在不脫離本發明之精神和範圍之內，相對上述實施例進行各種更動與修改仍屬本發明所保護之技術範疇，因此本發明之保護範圍當視後附之申請專利範圍所界定者為準。 While the invention has been described in connection with the preferred embodiments described above, it is not intended to limit the scope of the invention. The technical scope of the invention is protected, and therefore the scope of the invention is defined by the scope of the appended claims.
S1‧‧‧製備步驟 S1‧‧‧Preparation steps
S2‧‧‧成型步驟 S2‧‧‧ molding steps
S3‧‧‧燒結步驟 S3‧‧‧Sintering step
S4‧‧‧脫黏步驟 S4‧‧‧ Debonding step
S5‧‧‧表面修整步驟 S5‧‧‧ surface finishing steps
91‧‧‧本體 91‧‧‧Ontology
92‧‧‧配重體 92‧‧‧weights
921‧‧‧配重外層 921‧‧‧With weight outer layer
922‧‧‧配重內層 922‧‧‧weight inner layer
第1圖：習知高爾夫球桿頭的本體及配重體之立體分解圖。 Figure 1: An exploded perspective view of the body and weight of a conventional golf club head.
第2圖：本發明成型方法之操作步驟示意圖。 Fig. 2 is a schematic view showing the operation steps of the molding method of the present invention.
S1‧‧‧製備步驟 S1‧‧‧Preparation steps
S2‧‧‧成型步驟 S2‧‧‧ molding steps
S3‧‧‧燒結步驟 S3‧‧‧Sintering step
S4‧‧‧脫黏步驟 S4‧‧‧ Debonding step
S5‧‧‧表面修整步驟 S5‧‧‧ surface finishing steps
Claims (9)
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| CN201110285178.1A CN103008662B (en) | 2011-09-23 | 2011-09-23 | Integrally forming method for compound metals |
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| CN104190940B (en) * | 2014-08-20 | 2016-06-15 | 常熟市良益金属材料有限公司 | The preparation method of a kind of double metallic composite material |
| CN104190939A (en) * | 2014-08-20 | 2014-12-10 | 常熟市良益金属材料有限公司 | Preparation method for laminated composite metal material |
| CN106541140B (en) * | 2016-11-08 | 2019-03-29 | 西安科技大学 | A kind of preparation method of double metallic composite material |
| CN110857150A (en) * | 2018-08-22 | 2020-03-03 | 浙江恒成硬质合金有限公司 | Balancing weight for satellite and manufacturing process thereof |
| CN109589569A (en) * | 2018-11-28 | 2019-04-09 | 东莞市亿东数控科技有限公司 | A kind of clump weight and its manufacturing method of layer stack forming |
| CN113020602B (en) * | 2021-03-12 | 2022-10-21 | 东莞市亿东数控科技有限公司 | High-density golf head counterweight block |
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| JP2531624B2 (en) * | 1986-02-24 | 1996-09-04 | 三菱マテリアル株式会社 | Method for producing cored W alloy sintered body having high toughness and high strength |
| JP3089701B2 (en) * | 1991-04-23 | 2000-09-18 | 住友電気工業株式会社 | Manufacturing method of tungsten heavy alloy composite products |
| JPH05195022A (en) * | 1991-10-18 | 1993-08-03 | Fujitsu Ltd | Production of sintered compact and magnet base |
| CA2129874C (en) * | 1993-09-03 | 1999-07-20 | Richard M. Douglas | Powder for use in thermal spraying |
| DE10053199B4 (en) * | 1999-10-28 | 2008-10-30 | Denso Corp., Kariya-shi | Method for producing a metal composite compact |
| JP4225725B2 (en) * | 2001-12-17 | 2009-02-18 | ダイワ精工株式会社 | Manufacturing method of sports equipment using tungsten |
| JP2005089777A (en) * | 2003-09-12 | 2005-04-07 | Aisin Seiki Co Ltd | Method of producing composite sintered member |
| DE102004002714B3 (en) * | 2004-01-19 | 2005-05-19 | SCHWäBISCHE HüTTENWERKE GMBH | To produce sintered components, of light metal alloys, the powder is compressed into a green compact to be give a low temperature sintering followed by further compression and high temperature sintering |
| SE0401041D0 (en) * | 2004-04-21 | 2004-04-21 | Hoeganaes Ab | Sintered metal parts and method of manufacturing thereof |
| TWI246947B (en) * | 2004-06-10 | 2006-01-11 | Taiwan Powder Technologies Co | Method for making sintered body of metal powder and sintered body prepared therefrom |
| CN1718791A (en) * | 2005-06-24 | 2006-01-11 | 北京科技大学 | Method of preparing stainless steel composite material |
| CN101594954A (en) * | 2006-08-07 | 2009-12-02 | 昆士兰大学 | Metal injection moulding method |
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| DE102008051784B4 (en) * | 2008-10-17 | 2012-02-02 | H.C. Starck Gmbh | Process for the preparation of molybdenum metal powder, molybdenum metal powder and its use |
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