TWI645055B - Golf club head alloy and method for fabricating same - Google Patents

Golf club head alloy and method for fabricating same Download PDF

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TWI645055B
TWI645055B TW107100960A TW107100960A TWI645055B TW I645055 B TWI645055 B TW I645055B TW 107100960 A TW107100960 A TW 107100960A TW 107100960 A TW107100960 A TW 107100960A TW I645055 B TWI645055 B TW I645055B
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weight
parts
titanium
golf club
club head
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TW201930616A (en
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常傳賢
趙志燁
洪培容
謝佩娟
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大田精密工業股份有限公司
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C14/00Alloys based on titanium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/16Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of other metals or alloys based thereon
    • C22F1/18High-melting or refractory metals or alloys based thereon
    • C22F1/183High-melting or refractory metals or alloys based thereon of titanium or alloys based thereon

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Abstract

一種高爾夫球桿頭合金及其製造方法。該高爾夫球桿頭合金的製造方法包含步驟:提供一合金胚材,該合金胚材包含0.1至10重量份的鋯及77至99.9重量份的鈦;以及對該合金胚材在850至950℃進行一熱軋處理,以形成該高爾夫球桿頭合金,其中該高爾夫球桿頭合金的一晶相組成包含一等軸晶雙相結構,其中該等軸晶雙相結構包含一α鈦相與一β鈦相。 A golf club head alloy and a manufacturing method thereof. The method for manufacturing a golf club head alloy includes the steps of: providing an alloy preform, the alloy preform comprising 0.1 to 10 parts by weight of zirconium and 77 to 99.9 parts by weight of titanium; and the alloy preform at 850 to 950 ° C A hot rolling process is performed to form the golf club head alloy, wherein a crystal phase composition of the golf club head alloy includes an equiaxed crystal dual phase structure, wherein the equiaxed crystal dual phase structure includes an α titanium phase and A β titanium phase.

Description

高爾夫球桿頭合金及其製造方法 Golf club head alloy and manufacturing method thereof

本發明係關於一種合金及其製造方法,特別是關於一種高爾夫球桿頭合金及其製造方法。 The invention relates to an alloy and a manufacturing method thereof, and more particularly, to a golf club head alloy and a manufacturing method thereof.

高爾夫球桿頭發展過程中,從早期實心桿頭,重量、強度較低,到現今使用金屬材料可使桿頭強度越來越高,又可減輕重量與提高擊球成功率,故不斷開發低密度與高強度的合金。金屬材料可透過不同的加工處理方式與合金元素的搭配,研發應用於桿頭製造,甚至可結合非金屬的複合材料設計等,創造出能夠更具有操控、精準、遠距及錯誤容忍值更高的最佳球具。 In the development of golf club heads, from the early solid club heads, the weight and strength were low. Nowadays, the use of metal materials can make the club heads stronger and stronger, and can reduce the weight and increase the success rate of shots. Density and high strength alloy. Metal materials can be matched with alloy elements through different processing methods, research and development applied to the manufacturing of heads, and even combined with non-metal composite design, etc., to create more controllable, accurate, long-distance and higher error tolerance The best golf equipment.

另一方面,鈦合金亦應用於高爾夫球桿頭的領域。近年來,鈦合金球桿頭設計,漸漸強調高特徵時間之球桿頭開發設計,主要是增加打擊面的彈簧效應作為主要的設計理念,以增加擊球距離。 On the other hand, titanium alloys are also used in the field of golf club heads. In recent years, the design of titanium alloy club heads has gradually emphasized the development and design of club heads with high characteristic times, mainly by increasing the spring effect of the striking surface as the main design concept to increase the hitting distance.

然而,就現有的鈦合金球桿頭的材質方面,尚未找尋到適合材質組成,以增加打擊面的彈簧效應,進而增加擊球距離。 However, as far as the materials of the existing titanium alloy club heads are concerned, no suitable material composition has been found to increase the spring effect of the striking surface, thereby increasing the hitting distance.

故,有必要提供一種高爾夫球桿頭合金及其製造方法,以解決習用技術所存在的問題。 Therefore, it is necessary to provide a golf club head alloy and a manufacturing method thereof to solve the problems existing in conventional technology.

本發明之一目的在於提供一種高爾夫球桿頭合金的製造方法,其係利用特定的材質組成與特定溫度的熱軋處理,進而形成具有低楊氏係數的高爾夫球桿頭合金,以增加高爾夫球桿 頭的打擊面的彈簧效應,進而增加擊球距離。 An object of the present invention is to provide a method for manufacturing a golf club head alloy, which uses a specific material composition and a specific temperature for hot rolling treatment to form a golf club head alloy with a low Young's coefficient to increase the golf ball. Pole The spring effect of the striking surface of the head further increases the hitting distance.

本發明之另一目的在於提供一種高爾夫球桿頭合金,其具有等軸晶雙相結構,其中該等軸晶雙相結構包含一α鈦相與一β鈦,該等軸晶雙相結構可降低高爾夫球桿頭合金的楊氏係數,以增加高爾夫球桿頭的打擊面的彈簧效應,進而增加擊球距離。 Another object of the present invention is to provide a golf club head alloy having an equiaxed crystal dual-phase structure. The equiaxed crystal dual-phase structure includes an α titanium phase and a β titanium. The Young's coefficient of the golf club head alloy is reduced to increase the spring effect of the striking surface of the golf club head, thereby increasing the hitting distance.

為達上述之目的,本發明提供一種高爾夫球桿頭合金的製造方法,其包含步驟:提供一合金胚材,該合金胚材包含0.1至10重量份的鋯及77至99.9重量份的鈦;以及對該合金胚材在850至950℃進行一熱軋處理,以形成該高爾夫球桿頭合金,其中該高爾夫球桿頭合金的一晶相組成包含一等軸晶雙相結構,其中該等軸晶雙相結構包含一α鈦相與一β鈦相。 In order to achieve the above object, the present invention provides a method for manufacturing a golf club head alloy, comprising the steps of: providing an alloy preform, the alloy preform comprising 0.1 to 10 parts by weight of zirconium and 77 to 99.9 parts by weight of titanium; And performing a hot rolling treatment on the alloy blank at 850 to 950 ° C. to form the golf club head alloy, wherein a crystal phase composition of the golf club head alloy includes an equiaxed crystal dual phase structure, wherein The axial crystal dual-phase structure includes an α titanium phase and a β titanium phase.

在本發明之一實施例中,該合金胚材更包含一α鈦穩定材料。 In one embodiment of the present invention, the alloy blank further includes an alpha titanium stabilizing material.

在本發明之一實施例中,該α鈦穩定材料包含4.5至8.0重量份的鋁、大於零且小於或等於0.04重量份的碳、大於零且小於或等於0.04重量份的氮以及大於零且小於或等於0.10重量份的氧。 In one embodiment of the present invention, the α titanium stabilizing material includes 4.5 to 8.0 parts by weight of aluminum, greater than zero and less than or equal to 0.04 parts by weight of carbon, greater than zero and less than or equal to 0.04 parts by weight of nitrogen, and greater than zero and Less than or equal to 0.10 parts by weight of oxygen.

在本發明之一實施例中,該合金胚材更包含一β鈦穩定材料。 In one embodiment of the present invention, the alloy blank further includes a β- titanium stabilized material.

在本發明之一實施例中,該β鈦穩定材料包含釩、鉬、鉻及鐵,以及釩、鉬、鉻及鐵的總重係介於5.0至7.0重量份之間。 In one embodiment of the present invention, the β titanium stabilizing material includes vanadium, molybdenum, chromium, and iron, and the total weight of vanadium, molybdenum, chromium, and iron is between 5.0 and 7.0 parts by weight.

在本發明之一實施例中,該β鈦穩定材料包含0.5至3.0重量份的釩、0.5至2.5重量份的鉬、1.5至2.5重量份的鉻及1.5至2.5重量份的鐵。 In one embodiment of the present invention, the β titanium stabilizing material includes 0.5 to 3.0 parts by weight of vanadium, 0.5 to 2.5 parts by weight of molybdenum, 1.5 to 2.5 parts by weight of chromium, and 1.5 to 2.5 parts by weight of iron.

在本發明之一實施例中,在該熱軋處理的步驟後更包含一冷卻步驟,以使該高爾夫球桿頭合金冷卻至一室溫,其中該β鈦相在冷卻時形成一α’相。 In an embodiment of the present invention, a cooling step is further included after the hot rolling treatment step to cool the golf club head alloy to a room temperature, wherein the β titanium phase forms an α ′ phase when cooled. .

為達上述之另一目的,本發明提供一種高爾夫球桿頭合金,包含:0.1至10重量份的鋯;及77至99.9重量份的鈦,其中該高爾夫球桿頭合金的一晶相組成包含一等軸晶雙相結構,其中該等軸晶雙相結構包含一α鈦相與一β鈦相。 In order to achieve the above-mentioned another object, the present invention provides a golf club head alloy comprising: 0.1 to 10 parts by weight of zirconium; and 77 to 99.9 parts by weight of titanium, wherein a crystal phase composition of the golf club head alloy includes An equiaxed crystal dual-phase structure, wherein the equiaxed crystal dual-phase structure includes an α titanium phase and a β titanium phase.

在本發明之一實施例中,更包含:一α鈦穩定材料,包含4.5至8.0重量份的鋁、大於零且小於或等於0.04重量份的碳、大於零且小於或等於0.04重量份的氮以及大於零且小於或等於0.10重量份的氧;及一β鈦穩定材料,包含0.5至3.0重量份的釩、0.5至2.5重量份的鉬、1.5至2.5重量份的鉻及1.5至2.5重量份的鐵。 In one embodiment of the present invention, it further includes: an α titanium stabilizing material, comprising 4.5 to 8.0 parts by weight of aluminum, greater than zero and less than or equal to 0.04 parts by weight of carbon, and greater than zero and less than or equal to 0.04 parts by weight of nitrogen And oxygen greater than zero and less than or equal to 0.10 parts by weight; and a beta titanium stabilizing material comprising 0.5 to 3.0 parts by weight of vanadium, 0.5 to 2.5 parts by weight of molybdenum, 1.5 to 2.5 parts by weight of chromium, and 1.5 to 2.5 parts by weight Of iron.

在本發明之一實施例中,該高爾夫球桿頭合金的一抗拉強度介於1100至1250MPa之間,以及一楊氏係數介於80至100GPa之間。 In one embodiment of the present invention, a tensile strength of the golf club head alloy is between 1100 and 1250 MPa, and a Young's coefficient is between 80 and 100 GPa.

10‧‧‧方法 10‧‧‧Method

11‧‧‧步驟 11‧‧‧ steps

12‧‧‧步驟 12‧‧‧ steps

第1圖:本發明一實施例之高爾夫球桿頭合金的製造方法的流程示意圖。 FIG. 1 is a schematic flowchart of a method for manufacturing a golf club head alloy according to an embodiment of the present invention.

第2圖:本發明製得之高爾夫球桿頭合金的電子顯微圖。 Figure 2: Electron micrograph of a golf club head alloy prepared by the present invention.

第3圖:本發明製得之高爾夫球桿頭合金的另一電子顯微圖。 Figure 3: Another electron micrograph of a golf club head alloy prepared by the present invention.

第4圖:本發明製得之高爾夫球桿頭合金的再一電子顯微圖。 Figure 4: Still another electron micrograph of a golf club head alloy prepared by the present invention.

第5圖:本發明製得之高爾夫球桿頭合金的又一電子顯微圖。 Figure 5: Another electron micrograph of a golf club head alloy prepared by the present invention.

第6圖:本發明製得之高爾夫球桿頭合金的另一電子顯微圖。 Fig. 6: Another electron micrograph of a golf club head alloy prepared by the present invention.

為了讓本發明之上述及其他目的、特徵、優點能更明顯易懂,下文將特舉本發明較佳實施例,並配合所附圖式,作詳細說明如下。再者,本發明所提到的方向用語,例如上、下、頂、底、前、後、左、右、內、外、側面、周圍、中央、水平、橫向、垂直、縱向、軸向、徑向、最上層或最下層等,僅是參考附加圖式的方向。因此,使用的方向用語是用以說明及理解本發 明,而非用以限制本發明。 In order to make the above and other objects, features, and advantages of the present invention more comprehensible, the following describes the preferred embodiments of the present invention and the accompanying drawings in detail, as follows. Furthermore, the directional terms mentioned in the present invention include, for example, top, bottom, top, bottom, front, back, left, right, inside, outside, side, periphery, center, horizontal, horizontal, vertical, vertical, axial, The radial direction, the uppermost layer, or the lowermost layer, etc., are only directions referring to the attached drawings. Therefore, the directional terms used are used to explain and understand the present invention. It is not intended to limit the invention.

請參照第1圖所示,本發明一實施例之高爾夫球桿頭合金的製造方法10主要包含下列步驟11至12:提供一合金胚材,該合金胚材包含0.1至10重量份的鋯及77至99.9重量份的鈦;以及對該合金胚材在850至950℃進行一熱軋處理,以形成該高爾夫球桿頭合金,其中該高爾夫球桿頭合金的一晶相組成包含一等軸晶雙相結構,其中該等軸晶雙相結構包含一α鈦相與一β鈦相。本發明將於下文逐一詳細說明一實施例之上述各步驟的實施細節及其原理。 Please refer to FIG. 1, a method 10 for manufacturing a golf club head alloy according to an embodiment of the present invention mainly includes the following steps 11 to 12: providing an alloy blank material, the alloy blank material comprising 0.1 to 10 parts by weight of zirconium and 77 to 99.9 parts by weight of titanium; and a hot rolling treatment of the alloy blank at 850 to 950 ° C to form the golf club head alloy, wherein a crystal phase composition of the golf club head alloy includes an equiaxed Crystalline dual-phase structure, wherein the axial crystal dual-phase structure includes an α titanium phase and a β titanium phase. The present invention will detail the implementation details and principles of the above steps of the embodiment one by one in the following.

本發明第一實施例之高爾夫球桿頭合金的製造方法10首先係步驟11:提供一合金胚材,該合金胚材包含0.1至10重量份的鋯及77至99.9重量份的鈦。在本步驟11中,主要是透過添加特定範圍組成的鋯於鈦基質中,進而降低高爾夫球桿頭合金的楊氏係數,以增加高爾夫球桿頭的打擊面的彈簧效應,進而增加擊球距離。 The method 10 for manufacturing a golf club head alloy according to the first embodiment of the present invention is firstly step 11: providing an alloy preform, the alloy preform comprising 0.1 to 10 parts by weight of zirconium and 77 to 99.9 parts by weight of titanium. In this step 11, mainly by adding zirconium in a specific range to the titanium matrix, the Young's coefficient of the golf club head alloy is reduced, so as to increase the spring effect of the striking surface of the golf club head, thereby increasing the hitting distance. .

本發明第一實施例之高爾夫球桿頭合金的製造方法10最後係步驟12:對該合金胚材在850至950℃進行一熱軋處理,以形成該高爾夫球桿頭合金,其中該高爾夫球桿頭合金的一晶相組成包含一等軸晶雙相結構,其中該等軸晶雙相結構包含一α鈦相(α鈦相為六方最密堆積(HCP)晶體結構)與一β鈦相(β鈦相為體心立方堆積(BCC)晶體結構)。在本步驟12中,主要是透過特定溫度範圍的熱軋處理,以使鈦基質的相形成上述的等軸晶雙相結構。相關的實驗數據與顯微鏡圖將在後面段落進行詳述。 The method 10 for manufacturing a golf club head alloy according to the first embodiment of the present invention is the last step 12: a hot rolling treatment is performed on the alloy blank at 850 to 950 ° C. to form the golf club head alloy, wherein the golf ball The crystalline phase composition of the head alloy includes an equiaxed crystal dual-phase structure, wherein the equiaxed crystal dual-phase structure includes an α titanium phase (the α titanium phase is a hexagonal closest packing (HCP) crystal structure) and a β titanium phase (The β- titanium phase has a BCC crystal structure). In this step 12, the hot rolling treatment in a specific temperature range is mainly performed to make the phase of the titanium matrix to form the above-mentioned equiaxed crystal dual-phase structure. Relevant experimental data and microscope images will be detailed in the following paragraphs.

要提到的是,本發明之高爾夫球桿頭合金的製造方法10,至少是透過上述特定範圍的材質組成(例如鈦、鋯及/或後述的穩定材料)及/或至少是透過上述特定溫度的熱軋處理,以使所形成的高爾夫球桿頭合金具備低楊氏係數,以增加高爾夫球桿頭的打擊面的彈簧效應,進而增加擊球距離。 It should be mentioned that the manufacturing method 10 of the golf club head alloy of the present invention is at least through the above-mentioned specific range of material composition (for example, titanium, zirconium and / or stabilizing materials described later) and / or at least through the above-mentioned specific temperature. The hot-rolled treatment of the golf club head alloy has a low Young's coefficient to increase the spring effect of the striking surface of the golf club head, thereby increasing the hitting distance.

另一方面,可透過添加穩定材料於該合金胚材中以 使該α鈦相與該β鈦相穩定。在一實施例中,該合金胚材可包含有一α鈦穩定材料,例如該α鈦穩定材料包含4.5至8.0重量份的鋁、大於零且小於或等於0.04重量份的碳、大於零且小於或等於0.04重量份的氮以及大於零且小於或等於0.10重量份的氧。在另一實施例中,該合金胚材可包含一β鈦穩定材料,例如該β鈦穩定材料包含釩、鉬、鉻及鐵,以及釩、鉬、鉻及鐵的總重係介於5.0至7.0重量份之間。在一具體範例中,該β鈦穩定材料包含0.5至3.0重量份的釩、0.5至2.5重量份的鉬、1.5至2.5重量份的鉻及1.5至2.5重量份的鐵。要提到的是,該α鈦穩定材料與該β鈦穩定材料亦可同時添加於該合金胚材中,以使該α鈦相與該β鈦相較為穩定。 On the other hand, the α titanium phase and the β titanium phase can be stabilized by adding a stabilizing material to the alloy base material. In an embodiment, the alloy blank may include an alpha titanium stabilizing material. For example, the alpha titanium stabilizing material includes 4.5 to 8.0 parts by weight of aluminum, greater than zero and less than or equal to 0.04 parts by weight of carbon, and greater than zero and less than or equal to Equal to 0.04 parts by weight of nitrogen and 0.10 parts by weight or less of oxygen. In another embodiment, the alloy base material may include a β titanium stabilizing material. For example, the β titanium stabilizing material includes vanadium, molybdenum, chromium, and iron, and the total weight of vanadium, molybdenum, chromium, and iron is between 5.0 and Between 7.0 parts by weight. In a specific example, the β titanium stabilizing material includes 0.5 to 3.0 parts by weight of vanadium, 0.5 to 2.5 parts by weight of molybdenum, 1.5 to 2.5 parts by weight of chromium, and 1.5 to 2.5 parts by weight of iron. It should be mentioned that the α-titanium stabilizing material and the β- titanium stabilizing material can also be added to the alloy blank at the same time, so that the α-titanium phase and the β- titanium phase are more stable.

在一實施例中,在該熱軋處理的步驟12後更包含一冷卻步驟,以使該高爾夫球桿頭合金冷卻至一室溫,其中該β鈦相在冷卻時形成一α’相。具體而言,該β鈦相係高溫相,當其冷卻時會因其本身特性而形成α’相(麻田散體)。例如請參照第2圖,第2圖係本發明製得之高爾夫球桿頭合金的電子顯微圖。從第2圖可知,該高爾夫球桿頭合金的晶相組成為α鈦相+β鈦相的雙相等軸晶結構,具有α鈦相區域+α’鈦相區域。 In an embodiment, after step 12 of the hot rolling process, a cooling step is further included to cool the golf club head alloy to a room temperature, wherein the β titanium phase forms an α ′ phase when cooled. Specifically, the β titanium phase is a high-temperature phase, and when it is cooled, it forms an α 'phase (Matian powder) due to its own characteristics. For example, please refer to FIG. 2, which is an electron micrograph of a golf club head alloy prepared by the present invention. As can be seen from FIG. 2, the crystal phase composition of the golf club head alloy is a bi-equilibrium crystal structure of α titanium phase + β titanium phase, and has an α titanium phase region + α ′ titanium phase region.

請繼續參照第3圖,第3圖係本發明製得之高爾夫球桿頭合金的另一電子顯微圖。本案發明人進一步發現該高爾夫球桿頭合金中的α鈦相中具有次晶粒(subgrain;平均粒徑約0.8至1.2微米),此可使高爾夫球桿頭合金具有較高的機械強度。 Please continue to refer to FIG. 3, which is another electron micrograph of the golf club head alloy prepared by the present invention. The inventors further found that the α titanium phase in the golf club head alloy has subgrains (average particle diameter of about 0.8 to 1.2 microns), which can make the golf club head alloy have higher mechanical strength.

請繼續參照第4圖,第4圖係本發明製得之高爾夫球桿頭合金的再一電子顯微圖。本案發明人進一步發現該高爾夫球桿頭合金中的α’鈦相區域(β鈦相冷卻形成之麻田散體)中,可觀察到反相晶界(例如圖中類似迴紋針狀處),此反相晶界的形成可降低了楊氏係數。 Please continue to refer to FIG. 4, which is another electron micrograph of the golf club head alloy prepared by the present invention. The inventor of the present case further found that in the α 'titanium phase region of the golf club head alloy (Asa Intermediate formed by cooling the β titanium phase), inverse grain boundaries can be observed (such as in the figure like a paperclip). The formation of inverse grain boundaries can reduce the Young's coefficient.

請繼續參照第5圖,第5圖係本發明製得之高爾夫球桿頭合金的又一電子顯微圖。本案發明人進一步發現該高爾夫 球桿頭合金中的α’鈦相區域(β鈦相冷卻形成之麻田散體)中,可觀察到雙晶型麻田散體存在,此雙晶型麻田散體的形成可使高爾夫球桿頭合金具有較高的機械強度。 Please continue to refer to FIG. 5, which is another electron micrograph of the golf club head alloy prepared by the present invention. The inventor of the present case further found that in the α 'titanium phase region (the Asa powder formed by cooling the β titanium phase) in the golf club head alloy, the existence of the dual crystal Asa powder was observed. The formation of the dual crystal Asa powder can Golf club head alloys have high mechanical strength.

請繼續參照第6圖,第6圖係本發明製得之高爾夫球桿頭合金的另一電子顯微圖。本案發明人進一步發現該高爾夫球桿頭合金中的α鈦相區域中,可觀察到微小顆粒析出形成(參考第6圖中的圓圈處)。經過儀器的分析後得知,該微小顆粒為鈦-鋯(Ti-Zr)的富鋯之析出物,可使該高爾夫球桿頭合金具備低楊氏係數。 Please continue to refer to FIG. 6, which is another electron micrograph of the golf club head alloy prepared by the present invention. The inventors of the present invention further found that precipitation and formation of fine particles were observed in the α titanium phase region in the golf club head alloy (refer to the circle in FIG. 6). After analysis of the instrument, it was found that the fine particles were zirconia-rich precipitates of titanium-zirconium (Ti-Zr), so that the golf club head alloy could have a low Young's coefficient.

要提到的是,上述對於高爾夫球桿頭合金中所產生的的晶相及/或析出物的原因,至少是基於本發明的特定範圍的材質組成(例如鈦、鋯及/或後述的穩定材料)及/或至少是透過本發明的特定溫度的熱軋處理所形成。而這些晶相及/或析出可使高爾夫球桿頭合金具備低楊氏係數及高機械性質,以增加高爾夫球桿頭的打擊面的彈簧效應,進而增加擊球距離。 It should be mentioned that the above-mentioned reasons for the crystal phase and / or precipitates generated in the golf club head alloy are at least based on the material composition of the specific range of the present invention (for example, titanium, zirconium, and / or stability described later). Material) and / or at least formed by a hot rolling treatment at a specific temperature of the present invention. These crystal phases and / or precipitations can make golf club head alloys have low Young's coefficients and high mechanical properties, so as to increase the spring effect of the striking surface of the golf club head, thereby increasing the hitting distance.

另外,要提到的是,本發明中所使用的合金胚材的材質範圍是經過嚴格設計的,具體說明如下:鈦元素:添加量為77至99.9重量份(或wt%)的鈦,作為基質;鋯元素:添加量為0.1至10.0重量份(或wt%),可促使富鋯析出相形成以及反相晶界形成,有利於降低合金之楊氏係數;α鈦相穩定材料:鋁元素:添加量設計為4.5至8.0重量份(或wt%);碳、氮、氧元素:為避免α2相(Ti3Al)形成,本發明之碳、氮、氧元素需為低含量,其分別低於0.04重量份(或wt%)、0.04重量份(或wt%)、0.10重量份(或wt%);β鈦相穩定材料:添加特定比例的鐵、鉻、鉬與釩元素,來獲得次晶粒之顯微結構,進而增加材料強度;另外,為達特定熱軋條件(850至950℃,例如為900℃)後,可獲致α鈦相+β鈦相的等軸晶雙相結構,進而達到高爾 夫球桿頭合金的高強度特徵,本發明之鐵鉻鉬釩4種元素總量被嚴格限定於5.0~7.0wt%之間,包括:0.5至3.0重量份(或wt%)釩、0.5至2.5重量份(或wt%)鉬、1.5至2.5重量份(或wt%)鉻、及1.5至2.5重量份(或wt%)鐵。 In addition, it should be mentioned that the material range of the alloy blank used in the present invention has been strictly designed, and the specific description is as follows: Titanium element: titanium is added in an amount of 77 to 99.9 parts by weight (or wt%) as Matrix; Zirconium: Addition amount of 0.1 to 10.0 parts by weight (or wt%) can promote the formation of zirconium-rich precipitated phases and the formation of inverse grain boundaries, which is beneficial to reduce the Young's coefficient of the alloy; α titanium phase stabilization material: aluminum element : The added amount is designed to be 4.5 to 8.0 parts by weight (or wt%); carbon, nitrogen, and oxygen elements: In order to avoid the formation of the α2 phase (Ti 3 Al), the carbon, nitrogen, and oxygen elements of the present invention need to be low in content. Less than 0.04 parts by weight (or wt%), 0.04 parts by weight (or wt%), 0.10 parts by weight (or wt%); β titanium phase stable material: adding specific proportions of iron, chromium, molybdenum and vanadium elements to obtain The microstructure of the secondary grains further increases the strength of the material; in addition, after reaching the specific hot rolling conditions (850 to 950 ° C, for example, 900 ° C), an equiaxed crystal dual phase structure of α titanium phase + β titanium phase can be obtained In order to achieve the high strength characteristics of golf club head alloys, the total amount of the four elements of iron, chromium, molybdenum and vanadium of the present invention is strictly limited. Between 5.0 and 7.0 wt%, including: 0.5 to 3.0 parts by weight (or wt%) vanadium, 0.5 to 2.5 parts by weight (or wt%) molybdenum, 1.5 to 2.5 parts by weight (or wt%) chromium, and 1.5 to 2.5 parts by weight (or wt%) iron.

在本發明的另一態樣中,本發明提出一種高爾夫球桿頭合金,其可被加工以形成高爾夫球桿頭。該高爾夫球桿頭合金包含0.1至10重量份的鋯;及77至99.9重量份的鈦,其中該高爾夫球桿頭合金的一晶相組成包含一等軸晶雙相結構,其中該等軸晶雙相結構包含一α鈦相與一β鈦相。在一實施例中,該高爾夫球桿頭合金,更包含:一α鈦穩定材料,包含4.5至8.0重量份的鋁、大於零且小於或等於0.04重量份的碳、大於零且小於或等於0.04重量份的氮以及大於零且小於或等於0.10重量份的氧;及一β鈦穩定材料,包含0.5至3.0重量份的釩、0.5至2.5重量份的鉬、1.5至2.5重量份的鉻及1.5至2.5重量份的鐵。在另一實施例中,該高爾夫球桿頭合金的一抗拉強度介於1100至1250MPa之間,以及一楊氏係數介於80至100GPa之間。 In another aspect of the invention, the invention proposes a golf club head alloy that can be processed to form a golf club head. The golf club head alloy includes 0.1 to 10 parts by weight of zirconium; and 77 to 99.9 parts by weight of titanium, wherein a crystal phase composition of the golf club head alloy includes an equiaxed crystal dual-phase structure, wherein the axial crystals The two-phase structure includes an α titanium phase and a β titanium phase. In one embodiment, the golf club head alloy further comprises: an alpha titanium stabilizing material, including 4.5 to 8.0 parts by weight of aluminum, greater than zero and less than or equal to 0.04 parts by weight of carbon, greater than zero and less than or equal to 0.04 Parts by weight of nitrogen and 0.10 parts by weight or less of oxygen; and a beta titanium stabilizing material comprising 0.5 to 3.0 parts by weight of vanadium, 0.5 to 2.5 parts by weight of molybdenum, 1.5 to 2.5 parts by weight of chromium, and 1.5 To 2.5 parts by weight of iron. In another embodiment, the golf club head alloy has a tensile strength between 1100 and 1250 MPa, and a Young's coefficient between 80 and 100 GPa.

在一實施例中,該高爾夫球桿頭合金可以是透過前面段落所描述的高爾夫球桿頭合金的製造方法所製得。 In one embodiment, the golf club head alloy can be made by the method for manufacturing a golf club head alloy described in the previous paragraph.

以下將舉出數個實施例與數個比較例,以證明本發明實施例之高爾夫球桿頭合金的製作方法所製得的高爾夫球桿頭合金具備低楊氏係數及高強度的機械性質(抗拉強度)。 Several examples and comparative examples will be given below to prove that the golf club head alloy prepared by the method for manufacturing a golf club head alloy according to the embodiment of the present invention has low Young's coefficient and high strength mechanical properties ( tensile strength).

實施例1 Example 1

提供一合金胚材,該合金胚材包含86.78重量份的鈦、2.8重量份的鋯、5.1重量份的鋁、0.03重量份的碳、0.03重量份的氮、0.06重量份的氧、1.5重量份的鉻、1.6重量份的鐵、1.0重量份的釩及1.1重量份的鉬。接著,對該合金胚材在850至950℃進行一熱軋處理,以形成該高爾夫球桿頭合金(例如被軋製成板材),其中該高爾夫球桿頭合金的一晶相組成包含一等軸晶雙相結構,其中該等軸晶雙相結構包含一α鈦相與一β鈦相。 An alloy blank is provided, the alloy blank comprising 86.78 parts by weight of titanium, 2.8 parts by weight of zirconium, 5.1 parts by weight of aluminum, 0.03 parts by weight of carbon, 0.03 parts by weight of nitrogen, 0.06 parts by weight of oxygen, and 1.5 parts by weight Of chromium, 1.6 parts by weight of iron, 1.0 part by weight of vanadium, and 1.1 parts by weight of molybdenum. Next, a hot rolling treatment is performed on the alloy blank at 850 to 950 ° C. to form the golf club head alloy (for example, rolled into a sheet), wherein a crystal phase composition of the golf club head alloy includes first-class Axial crystal dual-phase structure, wherein the axial crystal dual-phase structure includes an α titanium phase and a β titanium phase.

實施例2至6及比較例1至3 Examples 2 to 6 and Comparative Examples 1 to 3

實施例2至6及比較例1至3的製作方式大致相同於實施例1,但其所使用的成份比例不同,如下表1所示(各成份的單位為重量份(或wt%))。 The manufacturing methods of Examples 2 to 6 and Comparative Examples 1 to 3 are substantially the same as those of Example 1, but the proportions of the components used are different, as shown in Table 1 below (the unit of each component is parts by weight (or wt%)).

接著,將實施例1至6與比較例1至3進行機械性質的分析。分析結果如下表2所示。 Next, Examples 1 to 6 and Comparative Examples 1 to 3 were analyzed for mechanical properties. The analysis results are shown in Table 2 below.

從上表2的分析結果可知,實施例1至6確實具備低楊氏係數(介於80至100GPa之間)、高抗拉強度(介於1100至1250MPa之間)、高降伏強度(介於1000至1050MPa之間)、及可接受的延伸率。比較例1至3的機械性質則為高楊氏係數、低抗拉強度及低降伏強度,且比較例2與3的延伸率過高,故比較例1至3不符合商用高爾夫球桿頭合金的要求。 From the analysis results in Table 2 above, Examples 1 to 6 do have a low Young's coefficient (between 80 and 100 GPa), a high tensile strength (between 1100 and 1250 MPa), and a high yield strength (between 1000 to 1050 MPa), and acceptable elongation. The mechanical properties of Comparative Examples 1 to 3 are high Young's coefficient, low tensile strength, and low yield strength, and the elongation of Comparative Examples 2 and 3 is too high, so Comparative Examples 1 to 3 do not meet the commercial golf club head alloys. Requirements.

雖然本發明已以較佳實施例揭露,然其並非用以限制本發明,任何熟習此項技藝之人士,在不脫離本發明之精神和範圍內,當可作各種更動與修飾,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。 Although the present invention has been disclosed in a preferred embodiment, it is not intended to limit the present invention. Any person skilled in the art can make various changes and modifications without departing from the spirit and scope of the present invention. The scope of protection shall be determined by the scope of the attached patent application.

Claims (4)

一種高爾夫球桿頭合金的製造方法,其包含步驟:提供一合金胚材,該合金胚材包含0.1至10重量份的鋯、77至99.9重量份的鈦、一α鈦穩定材料及一β鈦穩定材料,其中該α鈦穩定材料包含4.5至8.0重量份的鋁、大於零且小於或等於0.04重量份的碳、大於零且小於或等於0.04重量份的氮以及大於零且小於或等於0.10重量份的氧,該β鈦穩定材料包含0.5至3.0重量份的釩、0.5至2.5重量份的鉬、1.5至2.5重量份的鉻及1.5至2.5重量份的鐵,以及釩、鉬、鉻及鐵的總重係介於5.0至7.0重量份之間;以及對該合金胚材在850至950℃進行一熱軋處理,以形成該高爾夫球桿頭合金,其中該高爾夫球桿頭合金的一晶相組成包含一等軸晶雙相結構,其中該等軸晶雙相結構包含一α鈦相與一β鈦相,其中該α鈦相具有鈦-鋯的富鋯之析出物。A method for manufacturing a golf club head alloy, comprising the steps of: providing an alloy preform, the alloy preform comprising 0.1 to 10 parts by weight of zirconium, 77 to 99.9 parts by weight of titanium, an alpha titanium stabilizing material, and a beta titanium Stabilizing material, wherein the α titanium stabilizing material comprises 4.5 to 8.0 parts by weight of aluminum, greater than zero and less than or equal to 0.04 parts by weight of carbon, greater than zero and less than or equal to 0.04 parts by weight of nitrogen, and greater than zero and less than or equal to 0.10 weight Part of oxygen, the beta titanium stabilizing material contains 0.5 to 3.0 parts by weight of vanadium, 0.5 to 2.5 parts by weight of molybdenum, 1.5 to 2.5 parts by weight of chromium, and 1.5 to 2.5 parts by weight of iron, and vanadium, molybdenum, chromium, and iron The total weight is between 5.0 and 7.0 parts by weight; and a hot rolling treatment is performed on the alloy blank at 850 to 950 ° C to form the golf club head alloy, wherein a crystal of the golf club head alloy The phase composition includes an equiaxed crystal dual-phase structure, wherein the equiaxed crystal dual-phase structure includes an α titanium phase and a β titanium phase, wherein the α titanium phase has a zirconium-rich precipitate of titanium-zirconium. 如申請專利範圍第1項所述之高爾夫球桿頭合金的製造方法,其中在該熱軋處理的步驟後更包含一冷卻步驟,以使該高爾夫球桿頭合金冷卻至一室溫,其中該β鈦相在冷卻時形成一α’相,其中該α’相中具有反相晶界。The method for manufacturing a golf club head alloy according to item 1 of the patent application scope, further comprising a cooling step after the step of hot rolling to cool the golf club head alloy to a room temperature, wherein The β titanium phase forms an α 'phase when cooled, wherein the α' phase has a reverse grain boundary. 一種高爾夫球桿頭合金,包含:0.1至10重量份的鋯;77至99.9重量份的鈦,其中該高爾夫球桿頭合金的一晶相組成包含一等軸晶雙相結構,其中該等軸晶雙相結構包含一α鈦相與一β鈦相,其中該α鈦相具有鈦-鋯的富鋯之析出物;一α鈦穩定材料,包含4.5至8.0重量份的鋁、大於零且小於或等於0.04重量份的碳、大於零且小於或等於0.04重量份的氮以及大於零且小於或等於0.10重量份的氧;及一β鈦穩定材料,包含0.5至3.0重量份的釩、0.5至2.5重量份的鉬、1.5至2.5重量份的鉻及1.5至2.5重量份的鐵以及釩、鉬、鉻及鐵的總重係介於5.0至7.0重量份之間。A golf club head alloy comprising: 0.1 to 10 parts by weight of zirconium; 77 to 99.9 parts by weight of titanium, wherein a crystal phase composition of the golf club head alloy includes an equiaxed crystal dual-phase structure, wherein the axes The crystalline biphasic structure includes an α titanium phase and a β titanium phase, wherein the α titanium phase has titanium-zirconium-rich zirconium precipitates; an α titanium stable material containing 4.5 to 8.0 parts by weight of aluminum, greater than zero and less than Or greater than 0.04 parts by weight of carbon, greater than zero and less than or equal to 0.04 parts by weight of nitrogen, and greater than zero and less than or equal to 0.10 parts by weight of oxygen; and a beta titanium stabilizing material comprising 0.5 to 3.0 parts by weight of vanadium, 0.5 to The total weight of 2.5 parts by weight of molybdenum, 1.5 to 2.5 parts by weight of chromium and 1.5 to 2.5 parts by weight of iron and vanadium, molybdenum, chromium and iron is between 5.0 and 7.0 parts by weight. 如申請專利範圍第3項所述之高爾夫球桿頭合金,其中該高爾夫球桿頭合金的一抗拉強度介於1100至1250MPa之間,以及一楊氏係數介於80至100GPa之間。The golf club head alloy according to item 3 of the patent application scope, wherein the golf club head alloy has a tensile strength between 1100 and 1250 MPa and a Young's coefficient between 80 and 100 GPa.
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