TWI812545B - Method of manufacturing golf club head components - Google Patents
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- TWI812545B TWI812545B TW111143763A TW111143763A TWI812545B TW I812545 B TWI812545 B TW I812545B TW 111143763 A TW111143763 A TW 111143763A TW 111143763 A TW111143763 A TW 111143763A TW I812545 B TWI812545 B TW I812545B
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- 238000004519 manufacturing process Methods 0.000 title claims abstract description 16
- 238000010438 heat treatment Methods 0.000 claims abstract description 18
- 229910000838 Al alloy Inorganic materials 0.000 claims abstract description 11
- 238000012805 post-processing Methods 0.000 claims abstract description 10
- 238000003466 welding Methods 0.000 claims description 9
- 230000032683 aging Effects 0.000 claims description 6
- 238000010791 quenching Methods 0.000 claims description 4
- 230000000171 quenching effect Effects 0.000 claims description 4
- 238000004026 adhesive bonding Methods 0.000 claims description 3
- 238000000034 method Methods 0.000 abstract description 14
- 238000007493 shaping process Methods 0.000 abstract 1
- 239000000463 material Substances 0.000 description 10
- 238000010586 diagram Methods 0.000 description 5
- 238000013461 design Methods 0.000 description 4
- 238000005242 forging Methods 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 4
- 229910001008 7075 aluminium alloy Inorganic materials 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 229910001094 6061 aluminium alloy Inorganic materials 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 239000002131 composite material Substances 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000003698 laser cutting Methods 0.000 description 2
- 230000011218 segmentation Effects 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000005304 joining Methods 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000035882 stress Effects 0.000 description 1
- 230000037303 wrinkles Effects 0.000 description 1
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Abstract
一種高爾夫球桿頭部件的製造方法,包含一加熱步驟、一成形步驟、一分割步驟、一後處理步驟,及一結合步驟。在該加熱步驟中,將複數以高強度鋁合金製成的胚料升溫進行固溶化處理。在該成形步驟中,準備一包括複數模穴的模具,每一模穴具有複數成形區域,每一成形區域具有至少一相對高溫區及至少一相對低溫區,將該等胚料分別置入該等模穴中,使該等胚料成形為複數分別對應該等模穴且具有至少兩種局部強度的鈑件。在該分割步驟中,將每一鈑件分割成複數工件。在該後處理步驟中,將每一工件製成一高爾夫球桿頭部件。該等鈑件具有兩種不同的強度而兼具強度及韌性。A method for manufacturing a golf club head component includes a heating step, a shaping step, a dividing step, a post-processing step, and a combining step. In this heating step, a plurality of blanks made of high-strength aluminum alloy are heated up and subjected to solution treatment. In the forming step, a mold including a plurality of mold cavities is prepared. Each mold cavity has a plurality of forming areas. Each forming area has at least one relatively high temperature area and at least one relatively low temperature area. The blanks are respectively placed into the forming areas. In the mold cavities, the blanks are formed into a plurality of sheet parts corresponding to the mold cavities and having at least two local strengths. In this dividing step, each sheet piece is divided into multiple workpieces. In this post-processing step, each workpiece is formed into a golf club head component. These sheet parts have two different strengths and have both strength and toughness.
Description
本發明是有關於一種製造方法,特別是指一種高爾夫球桿頭部件的製造方法。 The present invention relates to a manufacturing method, in particular to a manufacturing method of golf club head components.
目前常見的空心高爾夫球桿頭多以頂板、底板,及打擊面板等部件透過焊接或其它結合方式組裝而成,這些部件通常依不同需求而以金屬或複合材料等材質透過鍛造而得,藉由此種多件式鍛造方法雖然可以製得不同的板狀部件,但受限於鍛造特性的限制,其無法製得外型較複雜的部件,且也無法使用強度較高的材質進行鍛造;此外,一般鍛造製程每次一個的產量也尚有改善之空間。目前市面上雖然有高爾夫球桿頭使用高強度鋁合金製成,但其多是透過冷成形方式製得,由於在強度及韌性上的拿捏難以兩全,故有功能性不足之問題。 At present, the common hollow golf club heads are mostly assembled by welding or other combination methods such as the top plate, sole plate, and impact panel. These parts are usually made of metal or composite materials through forging according to different needs. Although this multi-piece forging method can produce different plate-shaped components, it is limited by the forging characteristics and cannot produce components with more complex shapes, nor can it be forged with materials with higher strength; in addition, , there is still room for improvement in the output of one piece at a time in the general forging process. Although there are golf club heads currently on the market made of high-strength aluminum alloys, most of them are made through cold forming. Since it is difficult to achieve both strength and toughness, there is a problem of insufficient functionality.
因此,本發明之目的,即在提供一種可克服上述問題的 高爾夫球桿頭部件的製造方法。 Therefore, the object of the present invention is to provide a method that can overcome the above problems. Methods of manufacturing golf club head components.
於是,本發明高爾夫球桿頭部件的製造方法,包含一加熱步驟、一成形步驟、一分割步驟、一後處理步驟,及一結合步驟。在該加熱步驟中,將複數以高強度鋁合金製成的胚料置入一加熱爐內,並升溫至攝氏200度至攝氏560度。在該成形步驟中,準備一包括複數模穴的模具,該模具之每一模穴具有複數彼此相互連通的成形區域,每一成形區域具有至少一相對高溫區,及至少一相對低溫區,將該等胚料從該加熱爐移出後傳送至該模具內,並分別置入該等模穴中,使該等胚料成形為複數分別對應該等模穴且具有至少兩種局部強度的鈑件,接著透過該模具保壓以對該等鈑件進行模內淬火。在該分割步驟中,將每一鈑件分割成複數分別對應該等成形區域之形狀的工件,對該等工件進行修邊,從而使每一工件具有至少一嵌合結構。在該後處理步驟中,開模後將該等工件移出模具並進行人工時效處理。在該結合步驟中,另外準備一副鈑體,接著將每一工件的該至少一嵌合結構與該副鈑體嵌合,並另外透過焊接、鉚接、鎖固或塗膠方式接合該工件及該副鈑體的嵌合處,從而製得一高爾夫球桿頭部件。 Therefore, the manufacturing method of the golf club head component of the present invention includes a heating step, a forming step, a dividing step, a post-processing step, and a bonding step. In this heating step, a plurality of blanks made of high-strength aluminum alloy are placed in a heating furnace and the temperature is raised to 200 degrees Celsius to 560 degrees Celsius. In the forming step, a mold including a plurality of mold cavities is prepared. Each mold cavity of the mold has a plurality of interconnected forming areas. Each forming area has at least one relatively high temperature area and at least one relatively low temperature area. The blanks are transferred from the heating furnace to the mold and placed into the mold cavities respectively, so that the blanks are formed into a plurality of sheet parts corresponding to the mold cavities and having at least two local strengths. , and then through the mold holding pressure to perform in-mold quenching on the sheet parts. In the dividing step, each sheet piece is divided into a plurality of workpieces corresponding to the shapes of the forming regions, and the workpieces are trimmed so that each workpiece has at least one fitting structure. In this post-processing step, after the mold is opened, the workpieces are removed from the mold and subjected to artificial aging treatment. In the combining step, an additional sheet body is prepared, and then the at least one fitting structure of each workpiece is fitted to the secondary sheet body, and the workpieces are further joined by welding, riveting, locking or gluing. The fitting part of the auxiliary sheet body is used to obtain a golf club head component.
本發明之功效在於:透過本製造方法除了可將高強度的鋁合金成形出形狀複雜的鈑件外,透過局部加熱的方式,還能使同一片鈑件具有至少兩種不同的局部強度,且這兩種局部強度可依設 計需求進行調整,以使該鈑件兼具強度及韌性,可配合球頭功能性進行設計,在強度方面,以7075/6061鋁合金為例,本發明製得的鈑件可較一般F料鋁材提升約1.5~1.7倍之強度,並透過熱成形解決習知高強度鋁合金在冷成形時容易破裂及變形之問題。此外,本製造方法可一次製得多個高爾夫球桿頭部件,大幅提升產能及生產效率。 The effect of the present invention is that in addition to forming sheet parts with complex shapes from high-strength aluminum alloys through this manufacturing method, the same sheet piece can also have at least two different local strengths through local heating, and These two local strengths can be set according to Adjustments are made according to the design requirements so that the sheet parts have both strength and toughness and can be designed to match the functionality of the ball head. In terms of strength, taking 7075/6061 aluminum alloy as an example, the sheet parts produced by the present invention can be compared with ordinary F materials. The strength of aluminum materials is increased by about 1.5 to 1.7 times, and hot forming solves the problems of conventional high-strength aluminum alloys that are prone to cracking and deformation during cold forming. In addition, this manufacturing method can produce multiple golf club head parts at one time, greatly improving production capacity and production efficiency.
11:加熱步驟 11:Heating step
12:成形步驟 12: Forming steps
13:分割步驟 13: Segmentation steps
14:後處理步驟 14: Post-processing steps
15:結合步驟 15: Combining steps
2:模具 2: Mold
21:模穴 21:Mold cavity
211:成形區域 211: Forming area
3:鈑件 3: Sheet parts
31:軟區 31:Soft zone
32:硬區 32:Hard area
4:工件 4: Workpiece
41:嵌合塊 41: Chimeric block
5:副鈑體 5: Sub-body
51:嵌合槽 51: Fitting slot
6:高爾夫球桿頭部件 6: Golf club head parts
本發明之其它的特徵及功效,將於參照圖式的實施方式中清楚地呈現,其中:圖1是一流程圖,說明本發明高爾夫球桿頭部件之一實施例;圖2是一示意圖,說明該模具的每一模穴中具多個零件結合為一穴;圖3是一示意圖,說明該模具中有四個模穴而共計有二十四個成形區域,本示意圖省略該等模穴的具體輪廓;圖4是一示意圖,說明該模穴的二相對高溫區及一相對低溫區;圖5是一示意圖,說明該實施例中之一分割步驟;圖6是一立體圖,說明該實施例中之一後處理步驟所製得的其中一工件;及圖7是一立體圖,說明該實施例中之一結合步驟製得的一高爾 夫球桿頭部件。 Other features and effects of the present invention will be clearly presented in the embodiments with reference to the drawings, in which: Figure 1 is a flow chart illustrating an embodiment of the golf club head component of the present invention; Figure 2 is a schematic diagram, It shows that each mold cavity of the mold has multiple parts combined into one cavity; Figure 3 is a schematic diagram showing that there are four mold cavities and a total of twenty-four forming areas. This schematic diagram omits these mold cavities. The specific outline; Figure 4 is a schematic diagram illustrating two relatively high temperature areas and a relatively low temperature area of the mold cavity; Figure 5 is a schematic diagram illustrating one of the dividing steps in this embodiment; Figure 6 is a perspective view illustrating the implementation One of the workpieces produced by one of the post-processing steps in the example; and Figure 7 is a perspective view illustrating a Gower produced by one of the combining steps in the example. golf club head parts.
參閱圖1,本發明高爾夫球桿頭部件的製造方法之一實施例,包含一加熱步驟11、一成形步驟12、一分割步驟13、一後處理步驟14,及一結合步驟15。在該加熱步驟11中,將複數以高強度鋁合金製成的胚料分別置入一加熱爐內,並升溫至攝氏200度至攝氏560度。
Referring to FIG. 1 , one embodiment of the manufacturing method of golf club head components of the present invention includes a
參閱圖1至圖4,在該成形步驟12中,準備一包括四個模穴21的模具2,每一模穴21具有六個彼此相互連通而排成一列的成形區域211,每一成形區域211的形狀為所要成形之形狀。該成形區域211具有二相對高溫區,及一位於該等相對高溫區之間的相對低溫區。(各成形區域211亦可全為相同溫度)將該等胚料由該加熱爐移出後,輸送至該模具2內,並分別置入該等模穴21中,然後將該模具2合模後該使該等胚料成形為複數分別對應該等模穴21的鈑件3,每一鈑件3對應該等相對高溫區會形成韌性較佳的軟區31,而對應該相對低溫區則會形成強度較高的硬區32,使得該鈑件3具有兩種不同的局部強度。接著該等鈑件3在該模具2內經過保壓時間以進行模內淬火,保壓時間依軟硬區強度不同而有所差異,具體而言係透過不同的時間溫度曲線,來控制材料內部金相組織,以達到控制材料的抗拉強度,從而能調整控制該等鈑件3的強度。開模後取出
該等鈑件3,使其自然冷卻至常溫。透過前述熱成形工序所製得的該等鈑件3,可提升材料延伸性及成形性,並使其抽形深度加深且減少材料內應力所造成的回彈,可克服習知冷沖壓成形所產生的回彈、皺褶,及破裂等問題。本實施例所採用的局部加熱方式,可在同一片鈑件3上產生兩種不同的局部強度,並可依設計需求進行局部強度的強弱調整,如此可使該鈑件3兼具強度及韌性而提升良率,並配合球頭所需的功能性進行調整,達到調整球頭打擊特性或手感之作用。
Referring to Figures 1 to 4, in the forming
參閱圖1、圖3、圖5,及圖6,在該分割步驟13中,將每一鈑件3以雷射切割方式分割成六個分別對應該等成形區域211之形狀的工件4,切割方式可依製程需求採全周切割或局部免切割,由於高強度鋁合金的材質強度較高,以一般刀具進行切割會對刀具產生較大的耗損,因此以雷射方式進行切割為佳;接著對該等工件4進行修邊,從而使每一工件4具有複數嵌合結構,該工件4可以是高爾夫球桿頭的底板或頂板,該嵌合結構可以是嵌合塊41(見圖7)或嵌合槽。在該後處理步驟14中,開模後將該等工件4移出該模具2並進行人工時效處理,以7075鋁合金為例可接續對該等工件4進行攝氏120度且持續6至24小時的人工時效處理,時效時間及溫度依需求機性強度而會有所不同。參閱圖1及圖7,在該結合步驟15中,另外準備一具有匹配該工件4之嵌合結構的副鈑體5,該副鈑體
5可透過與該工件4相同的方式及材料製成,也可透過一般冷成形方式製成,或是以複合材料製成。將該工件4之該等嵌合結構與該副鈑體5兩兩相互嵌合,並透過焊接、鉚接、鎖固或塗膠方式接合該工件4與該副鈑體5的嵌合處,從而製得一高爾夫球桿頭部件6。以圖7為例,是將該工件4上的嵌合塊41嵌合於該副鈑體5上的一嵌合槽51中,當然也可以反過來設置,或採其它的嵌合設計。當接合方式為焊接時,可以選用點焊、間隔弧焊或全周弧焊來進行。本實施例藉由零件相互嵌合方式提升焊接及球頭精度,並可降低該工序及治具的開發費用。此外,該工件4上依設計需求而有局部強度不同的該等軟區31及該硬區32,能使該高爾夫球桿頭部件6產生對應的功能性。
Referring to Figures 1, 3, 5, and 6, in the dividing
綜上所述,有別於一般以冷沖壓方式加工高強度鋁合金,本發明可將較難加工的高強度鋁合金製成形狀較為複雜的板狀部件,使得該高爾夫球桿頭部件6具備高強度鋁合金質輕且強度高(抗拉強度可達543MPa)之特性,若以7075/6061鋁合金為例,可較一般F料鋁材提升約1.5~1.7倍的強度;此外,透過本實施例可一次製得二十四個或其它數量的高爾夫球桿頭部件6,大幅提高產量及效率,故確實能達成本發明之目的。
To sum up, unlike the general processing of high-strength aluminum alloys by cold stamping, the present invention can make plate-shaped parts with relatively complex shapes from high-strength aluminum alloys that are difficult to process, so that the golf
惟以上所述者,僅為本發明之實施例而已,當不能以此限定本發明實施之範圍,凡是依本發明申請專利範圍及專利說明書 內容所作之簡單的等效變化與修飾,皆仍屬本發明專利涵蓋之範圍內。 However, the above are only examples of the present invention and should not be used to limit the scope of the present invention. Any application for patent scope and patent specification based on the present invention Simple equivalent changes and modifications to the content are still within the scope of the patent of the present invention.
11:加熱步驟 11:Heating step
12:成形步驟 12: Forming steps
13:分割步驟 13: Segmentation steps
14:後處理步驟 14: Post-processing steps
15:結合步驟 15: Combining steps
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US20200147677A1 (en) * | 2018-11-13 | 2020-05-14 | Taylor Made Golf Company, Inc | Cluster for and method of casting golf club heads |
US11235380B2 (en) * | 2018-11-13 | 2022-02-01 | Taylor Made Golf Company, Inc. | Cluster for and method of casting golf club heads |
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WO2009148968A2 (en) * | 2008-06-02 | 2009-12-10 | Callaway Golf Company | A method for constructing a multiple piece golf club head |
US20160175666A1 (en) * | 2014-12-18 | 2016-06-23 | Taylor Made Golf Company, Inc. | Investment-casting of thin-walled golf club-heads |
TW201932165A (en) * | 2018-01-25 | 2019-08-16 | 復盛應用科技股份有限公司 | Alloy for manufacturing a golf club head and a method using the alloy thereof |
WO2019165467A1 (en) * | 2018-02-26 | 2019-08-29 | Karsten Manufacturing Corporation | Multi-material iron golf club head |
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