CN100497694C - Low density alloy for golf club head - Google Patents
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- CN100497694C CN100497694C CNB2006101505687A CN200610150568A CN100497694C CN 100497694 C CN100497694 C CN 100497694C CN B2006101505687 A CNB2006101505687 A CN B2006101505687A CN 200610150568 A CN200610150568 A CN 200610150568A CN 100497694 C CN100497694 C CN 100497694C
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- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 65
- 239000000956 alloy Substances 0.000 title claims abstract description 65
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 28
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 25
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 24
- 229910000756 V alloy Inorganic materials 0.000 claims abstract description 23
- -1 titanium-aluminum-vanadium Chemical compound 0.000 claims abstract description 23
- 229910052720 vanadium Inorganic materials 0.000 claims abstract description 23
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims abstract description 23
- 229910052742 iron Inorganic materials 0.000 claims abstract description 14
- 239000010936 titanium Substances 0.000 claims abstract description 14
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims abstract description 13
- 239000011651 chromium Substances 0.000 claims abstract description 13
- 239000010703 silicon Substances 0.000 claims abstract description 13
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 13
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 13
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims abstract description 12
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims abstract description 12
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims abstract description 12
- 229910052796 boron Inorganic materials 0.000 claims abstract description 12
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 12
- 229910052750 molybdenum Inorganic materials 0.000 claims abstract description 12
- 239000011733 molybdenum Substances 0.000 claims abstract description 12
- 239000000203 mixture Substances 0.000 claims description 5
- 239000004411 aluminium Substances 0.000 claims 5
- 229910001069 Ti alloy Inorganic materials 0.000 abstract description 23
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 abstract description 12
- 239000011573 trace mineral Substances 0.000 abstract description 9
- 235000013619 trace mineral Nutrition 0.000 abstract description 9
- 230000005489 elastic deformation Effects 0.000 description 13
- 230000005484 gravity Effects 0.000 description 11
- 229910000883 Ti6Al4V Inorganic materials 0.000 description 10
- 238000004519 manufacturing process Methods 0.000 description 9
- 239000000463 material Substances 0.000 description 5
- 239000010935 stainless steel Substances 0.000 description 5
- 229910001220 stainless steel Inorganic materials 0.000 description 5
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 238000005266 casting Methods 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 229910052580 B4C Inorganic materials 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- INAHAJYZKVIDIZ-UHFFFAOYSA-N boron carbide Chemical compound B12B3B4C32B41 INAHAJYZKVIDIZ-UHFFFAOYSA-N 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 235000009508 confectionery Nutrition 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 238000007872 degassing Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000000635 electron micrograph Methods 0.000 description 1
- 238000005495 investment casting Methods 0.000 description 1
- JEIPFZHSYJVQDO-UHFFFAOYSA-N iron(III) oxide Inorganic materials O=[Fe]O[Fe]=O JEIPFZHSYJVQDO-UHFFFAOYSA-N 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
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- 238000004018 waxing Methods 0.000 description 1
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Abstract
一种高尔夫杆头的低密度合金,其包含重量百分比的钛84%至94%、铝6.5%至9.5%(或5.5%至8.5%)及钒1.5%以下(或3.0%以下)。该低密度合金以钛铝钒合金为主要合金成份,并可选择添加钼、铬、铁、硅及/或硼等微量元素,以组成密度在4.40g/cm3以下的钛合金,因而形成密度较低且伸长率较高的钛合金。
A low-density alloy for a golf club head, comprising 84% to 94% titanium, 6.5% to 9.5% aluminum (or 5.5% to 8.5%) and less than 1.5% vanadium (or less than 3.0%) by weight. The low-density alloy is mainly composed of titanium-aluminum-vanadium alloy, and trace elements such as molybdenum, chromium, iron, silicon and/or boron can be optionally added to form a titanium alloy with a density of less than 4.40g/ cm3 , thereby forming a titanium alloy with lower density and higher elongation.
Description
技术领域 technical field
本发明关于一种高尔夫杆头的低密度合金(Low-Density Alloy for Making aGolfClub Head),特别是关于通过控制钛、铝及钒的混合比例,并选择添加钼、铬、铁、硅及/或硼等微量元素,以供调整重心位置及提升弹性变形能力的高尔夫杆头的低密度合金。The present invention relates to a low-density alloy (Low-Density Alloy for Making a Golf Club Head), in particular to controlling the mixing ratio of titanium, aluminum and vanadium, and selectively adding molybdenum, chromium, iron, silicon and/or Boron and other trace elements are used to adjust the position of the center of gravity and improve the low-density alloy of the golf club head with elastic deformation ability.
背景技术 Background technique
传统高尔夫杆头大多是不锈钢,如SUS630或SUS431(美国钢铁协会AISI标准630型与431型),并以精密浇注法(去蜡法)所制成,但此种材料的密度较大,且强度较低,因此以上述材料制成的杆头,其壁厚必须达某一厚度以上,才能达到杆头的强度要求;然而,在实际使用上,由于要求杆头重量不得太重的杆头设计要点,造成以上述材料所制成的杆头体积无法加大,因此杆头击球面上的较佳击球点范围会大幅缩小,造成击球失败的机率大增。Traditional golf club heads are mostly made of stainless steel, such as SUS630 or SUS431 (American Iron and Steel Institute AISI standard 630 and 431), and are made by precision casting (waxing method), but this material has a high density and strong strength. Therefore, the wall thickness of the club head made of the above materials must reach a certain thickness in order to meet the strength requirements of the club head; however, in actual use, due to the requirement that the club head weight should not be too heavy The main point is that the volume of the club head made of the above materials cannot be increased, so the range of the best hitting point on the ball hitting surface of the club head will be greatly reduced, resulting in a great increase in the probability of hitting the ball.
为解决上述问题,产业界研发采用钛合金所制造的杆头,如美国专利第5,505,795号《高尔夫球杆制造方法(Method of manufacturing golf club)》、第5,643,108号《高尔夫杆头结构及其制造方法(Structure for golf club head and themethod of its manufacture)》、第6,832,961号《木杆的高尔夫杆头(Wood-typegolf club head)》、第6,880,222号《高尔夫杆头制造方法(Method of manufacturinga golf club head)》及第6,905,061号《高尔夫杆头制造方法(Method of makinga golf club head)》等采用Ti-6Al-4V的钛合金(即重量百分比6%铝及4%钒,其余为钛金属)以制作一高尔夫球杆头,由于钛合金的密度相对低于不锈钢,且其强度与不锈钢相当,并能呈现相对较高的弹性变形能力,因此可在不增加杆头重量的前提下,其允许加大高尔夫杆头的体积,使高尔夫杆头的较佳击球点面积增加,以提高击球成功率。In order to solve the above problems, the industry has developed club heads made of titanium alloys, such as U.S. Patent No. 5,505,795 "Method of manufacturing golf clubs" and No. 5,643,108 "Golf club head structure and its manufacturing method". (Structure for golf club head and the method of its manufacture)", No. 6,832,961 "Wood-type golf club head", No. 6,880,222 "Method of manufacturing a golf club head" " and No. 6,905,061 "Method of making golf club head (Method of makinga golf club head)" and so on use Ti-6Al-4V titanium alloy (that is, 6% aluminum and 4% vanadium by weight, and the rest is titanium metal) to make a Golf club head, because the density of titanium alloy is relatively lower than that of stainless steel, its strength is equivalent to that of stainless steel, and it can exhibit relatively high elastic deformation capacity, so it can increase the size of the golf ball without increasing the weight of the club head. The volume of the club head increases the sweet spot area of the golf club head to improve the success rate of hitting the ball.
另一方面,由于Ti-6Al-4V的钛合金的密度相对低于不锈钢,因此其可用于制造高尔夫球杆头的部分构件,藉此达成调整高尔夫杆头的重心位置,例如杆头本体、打击面板、盖板或配重块等,且由于其弹性变形能力(伸长率)相对高于不锈钢,因此通常利用其较佳弹性变形能力可在击球时能产生较大的弹性变形程度,并可用以相对减少高尔夫球在碰撞打击面板时造成的球体压缩变形,相对降低击球应力被阻尼吸收的程度,以避免击球应力的能量损失,进而提升击球距离。On the other hand, because the density of Ti-6Al-4V titanium alloy is relatively lower than that of stainless steel, it can be used to manufacture some components of the golf club head, thereby achieving the adjustment of the center of gravity of the golf club head, such as the club head body, impact Panels, cover plates or counterweights, etc., and because its elastic deformation capacity (elongation) is relatively higher than that of stainless steel, it can usually use its better elastic deformation capacity to produce a greater degree of elastic deformation when hitting the ball, and It can be used to relatively reduce the compression deformation of the ball caused by the impact of the golf ball on the hitting panel, and relatively reduce the degree to which the hitting stress is absorbed by damping, so as to avoid the energy loss of the hitting stress and increase the hitting distance.
然而,在考量杆头体积大型化及调整重心裕度下,有必要进一步改良上述钛合金,使其更降低密度,且另添加其它元素,但仍保有原机械强度,以提升钛合金的应用裕度。However, in consideration of increasing the size of the club head and adjusting the margin of the center of gravity, it is necessary to further improve the above-mentioned titanium alloy to reduce the density and add other elements, but still retain the original mechanical strength to increase the application margin of the titanium alloy. Spend.
其它相关钛合金,如下列表一所示,于此列举参考。Other related titanium alloys are listed in Table 1 below, which are listed here for reference.
表一、传统各种成份的钛合金组成及其机械强度Table 1. Composition and mechanical strength of traditional titanium alloys with various components
有鉴于此,本发明改良上述缺点,其利用低密度的钛铝钒合金制造一高尔夫杆头,钛铝钒合金包含重量百分比的钛84%至94%、铝6.5%至9.5%(或5.5%至8.5%)及钒1.5%以下(或3.0%以下),或选择添加钼、铬、铁、硅及/或硼等微量元素,以组成密度4.40g/cm3以下的钛合金,以供调整高尔夫杆头的整体重心及提升弹性变形能力,有利杆头大型化,并进而提升杆头的设计裕度。In view of this, the present invention improves above-mentioned shortcoming, and it utilizes low-density titanium-aluminum-vanadium alloy to manufacture a golf club head, and titanium-aluminum-vanadium alloy comprises titanium 84% to 94% by weight percentage, aluminum 6.5% to 9.5% (or 5.5% to 8.5%) and less than 1.5% vanadium (or less than 3.0%), or choose to add trace elements such as molybdenum, chromium, iron, silicon and/or boron to form a titanium alloy with a density of less than 4.40g/cm 3 for adjustment The overall center of gravity of the golf club head and the improved elastic deformation capability are conducive to the enlargement of the club head and further increase the design margin of the club head.
发明内容 Contents of the invention
本发明的主要目的是提供一种高尔夫杆头的低密度合金,其调整钛合金的铝及钒的比例,以降低密度及保有原机械强度,达到调整高尔夫杆头的整体重心及提升弹性变形能力的目的。The main purpose of the present invention is to provide a low-density alloy for the golf club head, which adjusts the ratio of aluminum and vanadium in the titanium alloy to reduce the density and maintain the original mechanical strength, so as to adjust the overall center of gravity of the golf club head and improve the elastic deformation capacity the goal of.
本发明的次要目的是提供一种高尔夫杆头的低密度合金,其调整钛合金的铝及钒的比例,并选择添加钼、铬、铁、硅及/或硼等微量元素,以降低密度及保有原机械强度,达到调整高尔夫杆头的整体重心及提升弹性变形能力的目的。The secondary purpose of the present invention is to provide a low-density alloy for a golf club head, which adjusts the ratio of aluminum and vanadium in the titanium alloy, and selectively adds trace elements such as molybdenum, chromium, iron, silicon and/or boron to reduce the density And maintain the original mechanical strength, to achieve the purpose of adjusting the overall center of gravity of the golf club head and improving the elastic deformation ability.
本发明的目的是这样实现的:一种高尔夫杆头的低密度合金,其包含重量百分比的钛84%至94%、铝5.5%至9.5%及钒3.0%以下,铁0.6%以下、硅0.6%以下、钼1.2%以下及铬1.2%以下。该低密度合金以钛铝钒合金为主要合金成份,并可选择添加硼等微量元素,以组成密度4.40g/cm3以下的钛合金,因而形成密度较低且伸长率较高的钛合金。The object of the present invention is achieved like this: a low-density alloy of a golf club head, which comprises 84% to 94% of titanium, 5.5% to 9.5% of aluminum and less than 3.0% of vanadium, less than 0.6% of iron and less than 0.6% of silicon by weight. % or less, molybdenum 1.2% or less and chromium 1.2% or less. The low-density alloy uses titanium-aluminum-vanadium alloy as the main alloy component, and can optionally add trace elements such as boron to form a titanium alloy with a density below 4.40g/cm 3 , thus forming a titanium alloy with a lower density and higher elongation. .
本发明的低密度合金选择铝的重量百分比调整至6.5%至9.5%之间。In the low-density alloy of the present invention, the percentage by weight of aluminum is adjusted to be between 6.5% and 9.5%.
本发明的低密度合金选择铝的重量百分比调整至5.5%至8.5%之间。In the low-density alloy of the present invention, the percentage by weight of aluminum is adjusted to be between 5.5% and 8.5%.
本发明的低密度合金选择钒的重量百分比调整至1.5%以下。In the low-density alloy of the present invention, the weight percentage of vanadium is selected to be adjusted to be below 1.5%.
本发明的主要优点是:The main advantages of the present invention are:
其利用低密度的钛铝钒合金制造一高尔夫杆头,钛铝钒合金包含重量百分比的钛84%至94%、铝6.5%至9.5%(或5.5%至8.5%)及钒1.5%以下(或3.0%以下),或选择添加钼、铬、铁、硅及/或硼等微量元素,以组成密度4.40g/cm3以下的钛合金,以供调整高尔夫杆头的整体重心及提升弹性变形能力,有利杆头大型化,并进而提升杆头的设计裕度。It utilizes a low-density titanium-aluminum-vanadium alloy to manufacture a golf club head. The titanium-aluminum-vanadium alloy contains 84% to 94% by weight of titanium, 6.5% to 9.5% (or 5.5% to 8.5%) of aluminum and less than 1.5% of vanadium ( or less than 3.0%), or choose to add trace elements such as molybdenum, chromium, iron, silicon and/or boron to form a titanium alloy with a density below 4.40g/cm3 for adjusting the overall center of gravity of the golf club head and improving elastic deformation capacity , which is conducive to the enlargement of the club head, and further improves the design margin of the club head.
附图说明 Description of drawings
图1:本发明高尔夫杆头的低密度合金的电子显微照相图。Figure 1: Electron micrograph of the low density alloy of the golf club head of the present invention.
具体实施方式 Detailed ways
为让本发明的上述目的、特征和优点能更明显易懂,下文特举本发明的较佳实施例,并配合所附图式,作详细说明如下:In order to make the above-mentioned purpose, features and advantages of the present invention more obvious and understandable, the preferred embodiments of the present invention are specifically cited below, together with the accompanying drawings, and are described in detail as follows:
本发明较佳实施例高尔夫杆头的低密度合金以钛铝钒合金为主要合金成份,其包含重量百分比的钛84%至94%、铝5.5%至9.5%及钒3.0%以下。The low-density alloy of the golf club head in the preferred embodiment of the present invention is mainly composed of titanium-aluminum-vanadium alloy, which contains 84% to 94% of titanium, 5.5% to 9.5% of aluminum and less than 3.0% of vanadium.
实施例1Example 1
如表二及附图1所示,本发明第一实施例的高尔夫杆头的低密度合金,其以钛金属(密度4.51g/cm3)、铝金属(密度2.70g/cm3)及钒金属(密度5.79g/cm3)为主要合金成份,钛铝钒合金是包含重量百分比的钛84%至94%、铝6.5%至9.5%及钒1.5%以下,以组成密度4.40g/cm3以下的钛合金,其较佳选用钛91%、铝8%及钒1%的钛铝钒合金(如表二所示的Ti-8Al-1V合金或Ti-7.5Al-0.05V合金)。As shown in Table 2 and accompanying drawing 1, the low-density alloy of the golf club head of the first embodiment of the present invention is made of titanium metal (density 4.51g/cm 3 ), aluminum metal (density 2.70g/cm 3 ) and vanadium Metal (density 5.79g/cm 3 ) is the main alloy component. Titanium-aluminum-vanadium alloy contains 84% to 94% by weight of titanium, 6.5% to 9.5% of aluminum and less than 1.5% of vanadium, with a composition density of 4.40g/cm 3 The following titanium alloys are preferably titanium-aluminum-vanadium alloys with 91% titanium, 8% aluminum and 1% vanadium (such as Ti-8Al-1V alloy or Ti-7.5Al-0.05V alloy shown in Table 2).
实施例2Example 2
本发明另一实施例的低密度合金是较佳在不改变原先钛的重量百分比84%至94%的前提下,将铝的重量百分比调整至5.5%至8.5%之间;另外,将钒的重量百分比同时调整至3.0%以下。此时,低密度合金仍保有本发明第一实施例的原机械强度。In the low-density alloy of another embodiment of the present invention, it is preferable to adjust the weight percentage of aluminum to between 5.5% and 8.5% without changing the original titanium weight percentage of 84% to 94%; in addition, the vanadium The weight percentage is adjusted below 3.0% at the same time. At this time, the low-density alloy still maintains the original mechanical strength of the first embodiment of the present invention.
实施例3Example 3
相较于本发明第一实施例的Ti-8Al-1V合金,实施例3的低密度合金略降低铝元素的含量,但不致影响低密度合金的伸长率性质;同时,低密度合金又略提高钒元素的含量。相对于本发明第一实施例的Ti-8Al-1V合金,该低密度合金略变动铝元素及钒元素比例。虽然该低密度合金与本发明的Ti-8Al-1V合金的铝元素及钒元素比例不同,但其未脱离本发明的低密度合金的技术范畴。Compared with the Ti-8Al-1V alloy of the first embodiment of the present invention, the low-density alloy of embodiment 3 slightly reduces the content of aluminum elements, but does not affect the elongation properties of the low-density alloy; at the same time, the low-density alloy slightly Increase the content of vanadium. Compared with the Ti-8Al-1V alloy of the first embodiment of the present invention, the proportion of aluminum and vanadium elements in this low-density alloy is slightly changed. Although the proportion of aluminum and vanadium elements in the low-density alloy is different from that of the Ti-8Al-1V alloy of the present invention, it does not deviate from the technical scope of the low-density alloy of the present invention.
以下本发明低密度合金与传统钛合金的比较特性是主要例举Ti-8Al-1V合金(或Ti-7.5Al-0.05V合金)与传统Ti-6Al-4V合金的比较做为说明。The following comparative characteristics of the low-density alloy of the present invention and the traditional titanium alloy mainly exemplify the comparison of the Ti-8Al-1V alloy (or Ti-7.5Al-0.05V alloy) and the traditional Ti-6Al-4V alloy for illustration.
相较于传统的Ti-6Al-4V合金,本发明通过相对提高铝添加量,可降低合金密度并改良韧性,以获得所需的低密度性质;通过相对降低钒添加量可有效提高铸造时的流动性及辅助除气效果,但不致影响合金的机械性质;钛铝钒合金是可选择使用于制造一高尔夫杆头的构件,例如杆头本体、打击面板、盖板及/或配重块等,其较佳是选自一打击面板。Compared with the traditional Ti-6Al-4V alloy, the present invention can reduce the alloy density and improve the toughness by relatively increasing the amount of aluminum added, so as to obtain the required low-density properties; by relatively reducing the amount of vanadium added, it can effectively improve the casting Fluidity and auxiliary degassing effect, but will not affect the mechanical properties of the alloy; titanium aluminum vanadium alloy is an optional component used in the manufacture of a golf club head, such as the club head body, striking panel, cover plate and/or counterweight, etc. , which is preferably selected from a striking panel.
另一方面,由于Ti-8Al-1V合金的密度(4.40至4.34g/cm3)相对低于Ti-6Al-4V合金的密度(4.42g/cm3),因此可用于高尔夫球杆头的部分构件以减轻其重量,但又不致大幅影响其机械性质,因此可供调整该高尔夫杆头的重心位置,例如杆头本体、打击面板、盖板或配重块等。On the other hand, since the density (4.40 to 4.34g/cm 3 ) of the Ti-8Al-1V alloy is relatively lower than that of the Ti-6Al-4V alloy (4.42g/cm 3 ), it can be used for parts of golf club heads components to reduce its weight without significantly affecting its mechanical properties, so that the center of gravity of the golf club head can be adjusted, such as the club head body, striking panel, cover or counterweight.
请参阅表二所示,其揭示本发明第二至第五实施例的高尔夫杆头的低密度合金。相较于第一实施例,第二至第五实施例进一步于Ti-8Al-1V合金中选择添加微量元素,例如重量百分比的钼1.2%以下、铬1.2%以下、铁0.6%以下、硅0.6%以下及硼1.0%以下。通过添加适量的钼可使合金析出均匀分布的碳化物,并提高耐热性,以减少合金的焊接热裂,亦可增加其硬化能力及高温强度;通过添加适量的铬以提升合金的防锈耐蚀性,增加高尔夫杆头的使用寿命;通过添加适量的铁以具有良好的塑性,便于进行加工处理;通过添加适量的硅以改善熔融金属的流动性;通过添加适量的硼,因其在高温下组织稳定,且具有较佳的抗氧化能力、韧性及塑性,可改善合金的机械性质。Please refer to Table 2, which reveals the low-density alloys of the golf club heads of the second to fifth embodiments of the present invention. Compared with the first embodiment, the second to fifth embodiments further selectively add trace elements to the Ti-8Al-1V alloy, such as molybdenum 1.2% or less, chromium 1.2% or less, iron 0.6% or less, silicon 0.6% by weight. % or less and boron 1.0% or less. By adding an appropriate amount of molybdenum, the alloy can precipitate uniformly distributed carbides and improve heat resistance, so as to reduce the welding hot crack of the alloy, and also increase its hardening ability and high temperature strength; by adding an appropriate amount of chromium to improve the rust resistance of the alloy Corrosion resistance, increase the service life of the golf club head; by adding an appropriate amount of iron to have good plasticity, which is convenient for processing; by adding an appropriate amount of silicon to improve the fluidity of molten metal; by adding an appropriate amount of boron, because it is in The structure is stable at high temperature, and has better oxidation resistance, toughness and plasticity, which can improve the mechanical properties of the alloy.
本发明第二实施例是添加重量百分比的钼0.25%至0.5%;The second embodiment of the present invention is to add 0.25% to 0.5% of molybdenum in weight percentage;
本发明第三实施例是添加重量百分比的铬0.4%至0.6%;The third embodiment of the present invention is to add 0.4% to 0.6% of chromium in weight percentage;
本发明第四实施例是添加重量百分比的铁0.2%至0.4%;The fourth embodiment of the present invention is to add 0.2% to 0.4% of iron in weight percentage;
本发明第五实施例是添加重量百分比的硅0.25%至0.35%。The fifth embodiment of the present invention is to add 0.25% to 0.35% silicon by weight.
除上述实施例外,本发明亦可选择添加重量百分比的硼1.0%以下以制成高尔夫杆头。本发明第二至第五实施例的钛铝钒合金同样亦可选择使用于高尔夫杆头的部分构件,例如杆头本体、打击面板、盖板及/或配重块等,其较佳选用一打击面板。In addition to the above-mentioned embodiments, the present invention can also choose to add less than 1.0% boron by weight to make a golf club head. The titanium-aluminum-vanadium alloys of the second to fifth embodiments of the present invention can also be optionally used in some components of the golf club head, such as the club head body, the striking panel, the cover plate and/or the counterweight, etc., preferably one Hit the panel.
藉此,上述第一至五实施例以钛铝钒合金为主要合金成份,并添加钼、铬、铁、硅及/或硼等微量元素,而形成一密度较Ti-6Al-4V钛合金低,且伸长率较Ti-6Al-4V钛合金高的高尔夫杆头,而在不超过材料本身的弹性限度(elasticlimit)前提下,低密度钛铝钒合金的伸长率E%(弹性变形能力)获得提升。因此利用其较佳的弹性变形能力可在击球时形成较大的弹性变形程度,进而提升击球距离。同时,利用该低密度Ti-8Al-1V合金(或Ti-7.5Al-0.05V合金)可降低高尔夫杆头的整体重量,并可用于高尔夫球杆头的部分构件,以调整高尔夫杆头的重心位置,例如杆头本体、盖板、打击面板或配重块等。因此,本发明可在不增加高尔夫杆头重量的前提下,使高尔夫杆头的体积大型化,增加高尔夫杆头的较佳击球点面积,以提高击球成功率。In this way, the above-mentioned first to fifth embodiments use titanium-aluminum-vanadium alloy as the main alloy component, and add trace elements such as molybdenum, chromium, iron, silicon and/or boron to form a titanium alloy with a lower density than Ti-6Al-4V titanium alloy. , and the elongation rate is higher than the golf club head of Ti-6Al-4V titanium alloy, and under the premise of not exceeding the elastic limit (elastic limit) of the material itself, the elongation rate E% (elastic deformation capacity) of the low-density titanium aluminum vanadium alloy ) gets boosted. Therefore, using its better elastic deformation ability can form a greater degree of elastic deformation when hitting the ball, thereby increasing the hitting distance. At the same time, the use of the low-density Ti-8Al-1V alloy (or Ti-7.5Al-0.05V alloy) can reduce the overall weight of the golf club head, and can be used for some components of the golf club head to adjust the center of gravity of the golf club head location, such as the clubhead body, cover, strike plate, or weights. Therefore, the present invention can enlarge the volume of the golf club head without increasing the weight of the golf club head, increase the area of the optimal hitting point of the golf club head, and improve the hitting success rate.
表二、不同重量百分比的钛铝钒合金及其机械性质的比较Table 2. Comparison of titanium aluminum vanadium alloys with different weight percentages and their mechanical properties
请参阅表二、三及四及附图1所示,其揭示本发明第六实施例的高尔夫杆头的低密度合金。相较于第一至五实施例,第六实施例是Ti-7.5Al-0.05V-0.2Si-0.06B4C的低密度合金,其包含重量百分比的铝7.2%至7.8%、钒0.02%至0.06%、硅0.22%、碳化硼0.06%、铁0.06%、碳0.04%、氮0.01%及氧0.21%,其余比例为钛。特别是本发明第六实施例的Ti-7.5Al-0.05V-0.2Si-0.06B4C的低密度合金具有相似于传统Ti-6Al-4V钛合金的机械性质,但其密度4.32克/立方公分是低于传统Ti-6Al-4V钛合金的密度(4.42克/立方公分)。在炮击测试(炮击速度55公尺/秒,#2炮击机)下,本发明的Ti-7.5Al-0.05V-0.2Si-0.06B4C的低密度合金应用于铸造制成打击面板,打击面板皆能通过炮击测试的标准。因此,利用Ti-7.5Al-0.05V-0.2Si-0.06B4C的低密度合金同样可降低高尔夫杆头的整体重量,并可用于高尔夫球杆头的部分构件以调整高尔夫杆头的重心位置,例如杆头本体、盖板、打击面板或配重块等。因此,本发明可在不增加高尔夫杆头重量的前提下,使高尔夫杆头的体积大型化,增加高尔夫杆头的较佳击球点面积,以提高击球成功率。Please refer to Tables 2, 3 and 4 and accompanying drawing 1, which disclose the low-density alloy of the golf club head according to the sixth embodiment of the present invention. Compared with the first to fifth embodiments, the sixth embodiment is a low-density alloy of Ti-7.5Al-0.05V-0.2Si-0.06B 4 C, which contains 7.2% to 7.8% by weight of aluminum and 0.02% of vanadium To 0.06%, silicon 0.22%, boron carbide 0.06%, iron 0.06%, carbon 0.04%, nitrogen 0.01% and oxygen 0.21%, the remaining proportion is titanium. In particular, the Ti-7.5Al-0.05V-0.2Si-0.06B 4 C low-density alloy of the sixth embodiment of the present invention has mechanical properties similar to the traditional Ti-6Al-4V titanium alloy, but its density is 4.32 grams/cubic Centimeter is lower than the density of traditional Ti-6Al-4V titanium alloy (4.42 g/cm3). Under the bombardment test (55 meters/second of bombardment velocity, #2 bombardment machine), the low-density alloy of Ti-7.5Al-0.05V-0.2Si-0.06B 4 C of the present invention is applied to casting and making striking panels, striking The panels are all able to pass the shell test standard. Therefore, the low-density alloy of Ti-7.5Al-0.05V-0.2Si-0.06B 4 C can also reduce the overall weight of the golf club head, and can be used in some components of the golf club head to adjust the center of gravity of the golf club head , such as the club head body, cover plate, striking panel or counterweight, etc. Therefore, the present invention can enlarge the volume of the golf club head without increasing the weight of the golf club head, increase the area of the optimal hitting point of the golf club head, and improve the hitting success rate.
表三、本发明第六实施例及传统合金的组成比较Table three, the sixth embodiment of the present invention and the composition comparison of traditional alloy
表四、由本发明第六实施例及传统合金铸造制成的打击面板进行炮击测试的比较(炮击速度55公尺/秒,#2炮击机)Table 4. Comparison of the shelling test of the strike panel made by the sixth embodiment of the present invention and the traditional alloy casting (the shelling speed is 55 m/s, #2 shelling machine)
如上所述,相较于传统高尔夫杆头较高密度、较低强度,且杆头体积无法加大,造成较佳击球点范围大幅缩小等缺点,本发明确实能利用低密度的Ti-8Al-1V等合金,或通过选择添加钼、铬、铁、硅及/或硼等微量元素组成密度4.40g/cm3以下的钛铝钒合金,以调整高尔夫杆头的整体重心及提升弹性变形能力,有利杆头大型化,并进而提升杆头设计裕度。As mentioned above, compared with the traditional golf club head with high density and low strength, and the volume of the club head cannot be increased, resulting in a significant reduction in the range of the best hitting point, the present invention can indeed use low-density Ti-8Al Alloys such as -1V, or by adding trace elements such as molybdenum, chromium, iron, silicon and/or boron to form a titanium-aluminum-vanadium alloy with a density below 4.40g/ cm3 , to adjust the overall center of gravity of the golf club head and improve the elastic deformation capacity , which is conducive to the enlargement of the club head, and further improves the design margin of the club head.
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CN101307417B (en) * | 2007-05-14 | 2010-12-22 | 蒋铭瑞 | Method for manufacturing high-strength titanium alloy golf club head component and product thereof |
CN102041408B (en) * | 2010-12-29 | 2012-11-28 | 洛阳双瑞精铸钛业有限公司 | High-elasticity titanium alloy material for golf head |
CN104436578B (en) * | 2013-09-16 | 2018-01-26 | 大田精密工业股份有限公司 | Golf club head and low density alloy thereof |
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CN105154800B (en) * | 2015-08-25 | 2017-01-25 | 山东建筑大学 | Method for preparing titanium alloy nanomaterials by warm extrusion of herringbone channel die |
CN109234567A (en) * | 2017-07-10 | 2019-01-18 | 复盛应用科技股份有限公司 | Alloy for golf club head and method for manufacturing golf club head by using alloy |
CN107747002A (en) * | 2017-11-01 | 2018-03-02 | 五华县新锐科技有限公司 | A kind of titanium alloy and its manufacture method applied to sporting goods |
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