TWI235677B - Low density and high ductility ferric-based alloy material for golf iron club head - Google Patents

Low density and high ductility ferric-based alloy material for golf iron club head Download PDF

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TWI235677B
TWI235677B TW93119421A TW93119421A TWI235677B TW I235677 B TWI235677 B TW I235677B TW 93119421 A TW93119421 A TW 93119421A TW 93119421 A TW93119421 A TW 93119421A TW I235677 B TWI235677 B TW I235677B
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alloy
iron
alloy material
ductility
golf
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TW93119421A
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TW200600160A (en
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Jr-Ye Jau
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Ota Precision Ind Co Ltd
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Abstract

This invention relates to a low density and high ductility ferric-based alloy material for golf iron club head wherein the alloy material comprises 23.0 to 30.0 wt% manganese, 6.3 to 10.0 wt% aluminum, 0.8 to 1.05 wt% carbon, 5.0 to 9.0 wt% chromium, and 0.2 to 0.4 wt% cobalt, wherein 0.6 to 1.0 wt% silicon and 0.2 to 0.4 wt% nitrogen can also be added, and iron is taken as the base material for the rest weight ratio of the combination. Although the added chromium has excellent anti-corrosiveness against the atmosphere, at 550 to 670 DEG C for alloy aging treatment, educt such as B2, DO3 and Cr7C3 will be produced and the alloy hardness will raise quickly with embrittled phenomenon. Therefore, after an appropriate casting process is performed on the added chromium, a forging processing at 1000 to 1050 DEG C is executed to remove the double-phase organization composed of ferrite (alpha) and austenite (gamma), and extremely good surface properties can be obtained. Again by way of heating treatment at 1030 to 1080 DEG C for 15 to 60 minutes and at 450 to 850 DEG C for 4 to 24 hours, its metallographic organization becomes complete austenite and twin crystal structure, and thus the precipitation of carbide like kappa and Cr7C3 can be delayed and the combination of extremely good ductility and tensile strength can be obtained. Therefore the alloy can achieve the design object of golf iron club head with high strength, low density, high ductility, high antirust nature and excellent surface properties.

Description

l235677 狄、發明說明: 【發明所屬之技術領域】 本發明關於一種低密度高延展性鐵基之高爾夫球鐵桿 碩合金材料,尤指一種具有低密度、高延展性及高防銹特 性 ’且由適合高爾夫球之鍛造鐵桿頭,以達到良好的設計 文化空間、高強度、高延展性、高防銹性及優良的鍛造表 面等要求之實用性材料者。 【先前技術】 合金是指「在一種金屬裡,加入一種或一種以上之他 種金屬或非金屬,所形成具有金屬特性的物質」。在學術 上,金屬是指純金屬元素而言,而所謂「純」金屬乃一種 相對的說法而已,其中多少會存在微量元素或化合物,稱 為雜貝反之若疋為了某些特殊目的而加入或保留的元 素則稱為「合金元素」,所以一般所稱之純金屬是指非故 意加入合金元素之精煉元素。 當純金屬添加他種金屬或非金屬合金元素而配製成合 金後其本身的性質也會發生變化,例如熔點降低、強度 升高、延展性降低、電阻增大、導熱度降低、熱處理性能 增進、耐純變化及磁性變化等等,&因為純金屬配製成 合金後,其機械、物理及化學性質均獲得改善,因此可隨 著機械、器具之設計需I,選用適#的合金元素並控制其 含量、製造程序、加工程序、熱處理程序,以配製成合用 的合金材料。l235677 D. Description of the invention: [Technical field to which the invention belongs] The present invention relates to a low-density and high-ductility iron-based golf iron master alloy material, especially a kind of low-density, high-ductility and high rust-proof characteristics. Suitable for golf iron forged iron head, to achieve a good design culture space, high strength, high ductility, high rust resistance and excellent forged surface and other practical materials. [Prior art] Alloy refers to "a substance with metallic properties formed by adding one or more other metals or non-metals to a metal". Academically, metal refers to pure metal elements, and the so-called "pure" metal is a relative term. How many trace elements or compounds are present, it is called miscellaneous. For some special purposes, it is added or The retained elements are called "alloying elements", so pure metals are generally referred to as refining elements that are not intentionally added to alloying elements. When pure metals are added to other metals or non-metal alloy elements to form alloys, their own properties will also change, such as lower melting point, higher strength, lower ductility, higher resistance, lower thermal conductivity, and improved heat treatment performance. , Resistance to pure changes and magnetic changes, etc., because pure metals are formulated into alloys, their mechanical, physical, and chemical properties have been improved. Therefore, as the design of machinery and appliances requires I, the appropriate alloy elements can be selected. And control its content, manufacturing procedures, processing procedures, heat treatment procedures to formulate a suitable alloy material.

例如·工業上經常利用的高強度低合金鋼(HSLA 1235677 及合金工具鋼即是,其中’高強度低合金鋼 :内之少量合金元素…ι、ν,,經過高溫:::2: 备的尚壓淬水程序,而獲得高強度為其特色,且 一、 於公路及鐵路橋樑、鐵路貨客車廂、大 “運用 械或挖土工具等。此外’合金卫具鋼則是藉著添力 、Mo、V、Ni等合金元素,使該些合金元素在 化物,使其具有硬化深度較深、耐磨耗 π >、妷 木7靨耗及耐鬲溫軟化的特 …-般可作為切削工具或熱加工模具,或是耐受 耐磨之場合。 f 高爾夫球運動迷人之處即在於其球場環境大自缺化, 且運動量和緩;同日夺,其又是強調自我挑戰的球類運動, 且其運動年齡層十分廣泛,可從5〜6至8g,歲。而其使 用的球具亦是十分複雜與繁多,—套完整的高爾夫球具包 含有木桿桿頭(w〇〇d) 3〜5支、鐵桿桿頭7〜8支、劈起桿 桿頭(pw)丨支、砂坑桿桿頭(sw)丨支、推桿桿頭7 P咖Ο ^支,以及組裝用桿身(分為金屬桿與碳纖維桿) 、膠套(為吸收球頭與球桿接觸面的摩擦力與美觀)及橡 膠材質之握把(為減緩擊球振動與握球桿之觸覺)。前述中 ,尚爾夫球頭木桿頭(Wood) —般呈中空球形,包括:桿頭 部分(用以結合桿身之基座)' 打擊面、底面與頂蓋(用以支 撐求頭本體)’其基本桿身長度較長,主要目的使用在開球 或長距離打擊,且依桿頭斜度及桿身長度可分為:丨號( driver)、2 號(brassie)、3 號(sp〇〇n)、4 號(⑽吻 )及5號(cleek),近來又有7號及9號木桿推出,使用 1235677 者可依個人技巧、體能及喜好選擇。 約介於45〜47英吋之間 =干、干身長度 才干碩斜度則大致在於8〜11度之 内,2號以後之木桿的桿身 則以3〜5度遞増,桿身Γ二 央时遞減,桿頭斜度 .^ 身長度越長越能將球打得遠,桿頭斜 度越大越能將球打得高。 斜 鐵==用高爾夫球鐵桿係泛指鐵桿、劈 比太mf至目軚點,其特徵為球飛行距離 比木♦干勒短’但可將球 鐵桿長約39.5英时,产頭:厂且方向谷易掌握。1號 以〇5英#、Γ / 度,2號桿以後桿身長度 距離選:、=:斜度以4度遞增,使用者可依目標 =擇適合的球桿擊球。此外,近年來, ::木桿及鐵桿優點’並兼具長距離打擊與準確性打擊: =鐵桿頭製成空心之設計出現。鐵桿尚二二 周圍作近距離切球用的劈 、 擊球的沙坑h 干(⑽叫Wedge)及用於沙坑 桿因: = ·),兩者皆屬於挖起桿,這類球 控H重,斜度Μ,所以㈣將球擊高及短距離的 目前高爾夫球鐵桿頭之製造 法與锻造加工法兩種,請配合參看一要為精:脫蠛鑄造 也有少部份利用表面鑛層或鎮板加工 斤不,另外 蠟鑄造法的成太,心 败力I整體而言,精密脫 點。而工掌::最Γ,但鍛造加工法具有較多方面的優 锻造加工Lr 製作鐵桿頭之精密脫_造法與 法的δ金材料機械性質係如附件一之表二所示。 ,又而言,目前高爾夫球桿頭設計的原理及考量因素 1235677 之基本特 其設計方 ,以及各球頭專利發明(材料發明、結構改良 徵,主要係為達到成功的擊球及良好的擊球點 向有: ’ 1·球頭大型化 250cc之間,近年 310cc 或 340 〜360cc 之間, 400〜46〇CC,其特點是可增大球桿 功擊球機率並增加擊球距離。 過去幾年,木桿頭的體積約在 來陸續推出的球頭體積則約在 240280 2001年後甚至可達到 的擊球甜蜜區,以提高成 2 ·低重心·為達 性 '提高擊球距離, 新趨勢。 穩定的揮擊與擊球點,並增加扭轉慣 降低重心乃為高爾夫球椁頭設計的最 HR芏軋阻力及凹昔沐改乂 … Μ強化打擊面設計··為達穩定的 揮擊與擊球點並降低扭轉能量損失,最近的發展趨 腦設計改變桿頭形狀,以減低風阻係數並及改變不同 心與甜蜜區,甚至不认θ1上 不_疋鐵杯頭或木桿頭之打擊面均可利 用高壓擠入方式製作打擊面。 過去,本發明者曾經高爾夫球鐵桿球頭 與結構分析,結果顯示,高爾夫鐵桿頭主要可分為三二 分,包括: 1·打擊面:為主要受力點,用以直接接觸高爾夫球 :般其厚度大約在2.5〜3.5mm之間,其基本需求為不會· 形的材料強度與最高的延伸率或㈣,目前材料其延伸^ 大約在要求在30〜40% ’抗拉強度大約在7〇, ^ 1〇0〜15〇kS1之間。此外,—般球頭要求要有敎的桿面, χ235677 因一般擊球時,球與桿面的擊球時約間為〇 〇〇45秒,此時 中管對擊球好壞並無影響,而桿面的穩定與否,卻是擊球 好壞的絕對因f ’所以大尺寸的桿面,以增加擊球甜蜜區 ’稭以提昇擊球穩定性,為設計的考量重點,·&外,減少 鐵才干頭打擊面角度變形,以及增加打擊面材料韌性(容易 彈性㈣)及增加接觸時間,藉以提昇穩^性與高爾夫球 飛行角度,亦為設計因素之一。 心2·底面·用以主要支撐高爾夫球頭本體形狀,為次要 力』&其厚度大約在3.G〜5.Gmm之間,因與地面直 妾接觸’其基本需求為材料耐磨性、耐蝕性與強度,目前 材料其抗拉強度大約在8〇〜15〇ksi之間。 .仟部·用以支撐 8维干2,—般厚度大約在2.2〜3.5咖之間,孔内徑大約名 =_之間’其基本需求為孔徑軸與打擊面角度(傾角與 ”角),一般使用與本體相同之材質。 整體而言,低重心、 a, sh ^ . -工轧阻力及強化打擊面雖可達 成功擊球與良好擊球點、增加 ^ 目的,作整V > 貝、耠鬲擊球距離等 仁整體而-,以南爾夫球鐵桿頭來說 形狀變化較多,所以晷电田⑷ 水兄*於其本身 兼且右嗝A 求用以裝作鐵桿頭的合金材料必須 兼/、有適當強度及高延展特性,同時 、 是目前工業用的合金材料並 人人:備有耐則生。但 求,以鈦合金斑析出不銹㈣&王°乎鐵桿頭的性能要 亦很好,惟㈣= 其雖具有耐餘性,強度 准超過鐵杯頭所需报多,且 不盡理想,又以AISI3〇4t I伸率或轫衝值並 不錢鋼來說,其抗拉強度大約為 !235677 7〇〜75Ksi左右’雖然延伸率 4σ 手約可達40〜60%,可拎如躲 刼控性,但球頭使用一段時 s力擊球 ,即;W 子間後’打擊面角強會產生變化 尽P強度仍嫌不足,所以a今 7 刖仍以锻造軟鐵S 2 5 C兼且 素材8加抗拉強纽3G〜35%延伸率為製作鐵桿頭之較佳 ’、,惟其鍛造後之耐蝕性仍稍嫌不足。 而就目前高爾夫球桿製造業的同共經驗,最佳的鐵桿 頭製作合金材料之抗拉強度應為鍛造軟鐵之1G〜i 5 2 右,即抗拉強度約80〜100ksi,降伏強度約5〇〜75ksi,延 伸率必須超過4G%且愈高愈好,以及低於7 9g/em3的密度 ’同時具備耐㈣,則可製作出打擊性能最佳的高爾夫球 鐵桿頭或空心鐵桿頭。 近一、二十年來,鐵一鋁一錳合金鋼系列經過國内外 專家學者廣泛的研究,顯示不同的合金設計能使鐵一鋁— 結合金鋼分別具有高強度、高韌性、耐低溫、耐高溫及耐 磨耗等特性,下列論文對這些性質均有詳細的描述。For example, high-strength low-alloy steels (HSLA 1235677 and alloy tool steels that are often used in industry are among them, 'high-strength low-alloy steel: a small amount of alloying elements ... ι, ν, after high temperature ::: 2: It is still under pressure and quenched, and it is characterized by high strength. First, it is used in roads and railway bridges, railroad passenger cars, large "appliances or earth-moving tools, etc." Mo, V, Ni and other alloy elements make these alloy elements in the compound, which has a deeper hardening depth, wear resistance π >, Tochigi 7 consumption and high temperature softening resistance ...-generally can be used as cutting Tools or hot working molds, or occasions that are resistant to abrasion. F The fascination of golf is that its golf course environment is self-defeating and the amount of exercise is gentle; on the same day, it is a ball game that emphasizes self-challenge. And its sports age range is very wide, it can be from 5 to 6 to 8g, and its golf equipment is very complicated and numerous, a complete set of golf equipment includes a wood club head (wo 〇d) 3 to 5 sticks, 7 to 8 iron heads, wedges Head (pw) 丨 support, sand pit club head (sw) 丨 support, putter head 7 P coffee 0 ^ support, as well as assembly shaft (divided into metal rod and carbon fiber rod), rubber sleeve (for absorption ball The frictional and beautiful appearance of the contact surface between the head and the club) and the rubber grip (in order to slow down the vibration of the shot and the feel of the club). In the foregoing, the wood head of the golf club (Salf) is generally hollow. Spherical, including: the head part (used to combine with the base of the shaft) 'hitting surface, bottom surface and top cover (used to support the head body)' The basic shaft length is longer, the main purpose is to use in kicking or long Distance strike, and can be divided into: 丨 (driver), 2 (brassie), 3 (sp0〇n), 4 (snoot kiss) and 5 (cleek) according to the club head slope and shaft length Recently, No. 7 and No. 9 wooden poles have been launched. Those who use 1235677 can choose according to their personal skills, physical fitness and preferences. About 45 ~ 47 inches = dry, dry length is only about 8 Within ~ 11 degrees, the shafts of wooden rods after 2 are progressively increased by 3 ~ 5 degrees. When the shaft Γ is reduced, the club head slopes. ^ The longer the body length, the more It can hit the ball farther, and the larger the club head slope, the higher the ball can be hit. Inclined iron == Use golf irons to refer to irons in general, the split ratio is too mf to the eye point, which is characterized by the ball flying distance than wood ♦ When the dry iron is short, but the iron can be about 39.5 inches long, the production head: the factory and the direction of the valley are easy to grasp. The No. 1 is 〇〇5 英 #, Γ / degree, the length of the shaft after the No. 2 shaft is selected :, = : Incline increases by 4 degrees, users can choose the right club to hit the ball according to the goal. In addition, in recent years, :: the advantages of wood and iron 'have both long-distance strike and accuracy strike: = iron head system A hollow design appears. The irons are still used to cut the ball at a close distance, the sand bunker h is called (wedge), and the bunker is used for: = ·), both of which belong to digging. This type of ball controls H weight and inclination M, so there are two methods of manufacturing and forging of the current golf iron head for hitting the ball high and short distance. A small part of the surface ore layer or town plate processing is not enough. In addition, the success of the wax casting method, the heart failure I as a whole, precision off-point. The work palm :: the most Γ, but the forging process has many advantages. The mechanical properties of the δ gold material of the precision demolition method and method of iron head forging Lr are shown in Table 2 of Annex 1. In addition, the current design principles and considerations of the current golf club head 1235677 are based on its original design method, as well as patent inventions (material inventions, structural improvement features, etc., mainly for achieving successful shots and good shots). The ball point directions are: '1. The size of the ball head is between 250cc, 310cc or 340 to 360cc, and 400 to 46oCC in recent years. It is characterized by increasing the chance of hitting the club and increasing the distance. In the past few years, the volume of wooden club heads has been successively introduced. The volume of ball heads that have been successively introduced is about 240280. After 2001, it can even reach the sweet area of hitting, in order to increase it to 2 · low center of gravity. New trend: Stable swing and hitting points, and increasing the inertia and lowering the center of gravity are the most HR rolling resistance and change of concave design for golf gimmicks. Μ Strengthening the design of the impact surface ... Strike and hit points and reduce torsional energy loss. Recent developments in brain design have changed the shape of the club head to reduce the coefficient of wind resistance and change the discentric and sweet areas, even disregarding θ1. Hitting face High-pressure extrusion can be used to make the hitting surface. In the past, the inventors have analyzed the golf iron head and structure analysis, and the results show that the golf iron head can be divided into three or two points, including: 1. The hitting surface: the main force Point for direct contact with the golf ball: generally its thickness is between 2.5 ~ 3.5mm, and its basic requirements are inflexible material strength and the highest elongation or ㈣. At present, the material's extension ^ is about 30 ~ 40% 'Tensile strength is between 70, ^ 100 ~ 15kS1. In addition, the general club head requires a sloping face, χ235677 due to the general impact of the ball and the face The ball time is about 0.0045 seconds. At this time, the middle tube has no effect on the quality of the shot, but the stability of the face is the absolute size of the shot. In order to increase the sweetness of the hitting area to improve the stability of the hitting, it is the key point of design considerations. In addition, reduce the angle deformation of the hitting surface of the iron talent head, and increase the toughness of the hitting surface material (easy elasticity) and increase contact time To improve stability and golf The angle of travel is also one of the design factors. Heart 2 · Bottom surface · Mainly supports the shape of the body of the golf head, which is a secondary force "& Its thickness is between 3.G ~ 5.Gmm, because it is straight to the ground The basic requirements of 妾 contact 'are the material's abrasion resistance, corrosion resistance and strength. At present, the tensile strength of the material is between 80 ~ 150ksi. 仟 The part is used to support 8-dimensional dry 2-the general thickness is about Between 2.2 ~ 3.5 coffee, the diameter of the hole is approximately equal to __. The basic requirement is the angle of the aperture axis and the striking surface (tilt angle and angle), and generally use the same material as the body. Overall, the low center of gravity, a, sh ^. -Although the rolling resistance and the strengthening of the striking surface can reach a successful batting and good batting points, increase the purpose of ^, for the whole V > shell, cricket batting distance, etc. For golf ball iron heads, the shape changes a lot, so 晷 Dian Tian⑷ Shui Xiong * also has the right 嗝 A. The alloy material used as the iron head must have / have appropriate strength and high elongation characteristics. , Is the current industrial alloy material and everyone: with resistance is born. However, it is required that the performance of stainless steel ㈣ &wang; iron heads with titanium spots is also very good, but ㈣ = although it has redundancy, its strength must exceed that required for iron cup heads, and it is not ideal, In terms of AISI304t I elongation or punching value, the tensile strength is about! 235677 70 ~ 75Ksi. Although the elongation rate is 4σ, the hand can reach about 40 ~ 60%, which can be avoided. It is controllable, but the ball hits the ball with s force for a period of time, that is, the W surface will be changed after the strike angle is strong, so the strength of P is still insufficient, so a 7 今 is still forged soft iron S 2 5 C Also, the material 8 plus tensile strength 3G ~ 35% elongation is better for making iron heads, but the corrosion resistance after forging is still slightly insufficient. According to the common experience of the current golf club manufacturing industry, the optimal tensile strength of the alloy material for iron head manufacturing should be about 1G ~ i 5 2 of forged soft iron, that is, the tensile strength is about 80 ~ 100ksi, and the yield strength is about 50 ~ 75ksi, the elongation must exceed 4G% and the higher the better, and the density lower than 79g / em3. At the same time, it has the resistance to rubbing, and can produce the best golf iron head or hollow iron head. In the past one or two decades, the iron-aluminum-manganese alloy steel series has been extensively studied by experts and scholars at home and abroad. It has been shown that different alloy designs can make iron-aluminum-combined gold steel have high strength, high toughness, low temperature resistance, and resistance. The characteristics of high temperature and wear resistance are described in detail in the following papers.

Schmatz,D· J.所發表,I960 年,Trans· ASM,第 52 冊 ’ 898 頁,標題 “ Structure and Properties of AustenticSchmatz, D. J., I960, Trans. ASM, Vol. 52 ’898, titled“ Structure and Properties of Austentic

Alloys Containing Aluminum and Silicon” 、Krivonogov, G. S·等人所發表,1975 年,phys· Met. & Metallog,第 4 冊 ’ 29 頁,標題 “ Phase Trasformation Kinetics in Steel 9G28Yu9MVB” 、Banerji,S· K.所發表,1978 年,4 月, Met. Prog,,59 頁,標題 “ An Austenitic Stainless Steel Without Nickel or Chromium,” 、Charles,J.等人所發表, 1981 年,Met. Prog.,71 頁,標題 Phase Decomposition of 10 1235677Alloys Containing Aluminum and Silicon ", Krivonogov, G.S., et al., 1975, phys. Met. &Amp; Metallog, Booklet 4 '29, titled" Phase Trasformation Kinetics in Steel 9G28Yu9MVB ", Banerji, S · Published by K., April 1978, Met. Prog, p. 59, titled "An Austenitic Stainless Steel Without Nickel or Chromium," published by Charles, J., et al., 1981, Met. Prog., 71 Page, Title Phase Decomposition of 10 1235677

Rapidly Solidified Fe-Mn-Al-C Austenitic Alloys” 、Grcia, J.等人所發表,1982年,Met· Prog·,47頁 ,標題 Development of Oxidation Resistant Fe-Mn-Al Alloys” 、 Wang,R·等人所發表,1983年,Met· Prog.,72頁,標題 New Stainless Steel Without Nickel or Chromiun for alloys Applications” 、Benz,J. C.等人所發表,1985 年, J. Met.,36 頁,標題 “An Assessment of Fe-Mn-Al Alloys as Substitutes for Stainless Steels” ,J. Charles·等人所發 表,1981 年,Met· Prog,71 頁,標題 “New Cryogenic Materials” 、Ham,K. Η·等人所發表,1986 年,Scripta Metall,第 20 冊,33 頁,標題 “ TEM Evidence of Modulated Structure in Fe-Mn-Al-C Alloys” 、Tjong,S· C.所發表,1990年,Mater· Char,第24冊,275頁,標題 “ Electron Microscope Observations of PhaseRapidly Solidified Fe-Mn-Al-C Austenitic Alloys ", Grcia, J., et al., 1982, Met · Prog ·, p. 47, title" Development of Oxidation Resistant Fe-Mn-Al Alloys ", Wang, R · Published by others, 1983, Met · Prog., Page 72, titled New Stainless Steel Without Nickel or Chromiun for alloys Applications ", published by Benz, JC, and others, 1985, J. Met., Page 36, title" An Assessment of Fe-Mn-Al Alloys as Substitutes for Stainless Steels ", published by J. Charles · et al., 1981, Met · Prog, page 71, titled" New Cryogenic Materials ", Ham, K. Η · et al. Published, 1986, Scripta Metall, Volume 20, 33 pages, titled "TEM Evidence of Modulated Structure in Fe-Mn-Al-C Alloys", Tjong, S.C., 1990, Mater Char, Booklet 24, page 275, entitled "Electron Microscope Observations of Phase

Decompositions in an Austentic Fe-8.7Al-29.7Mn-l.04C Alloy” ,Hwang,C· N·等人所發表,1993 年,Scripta Metall ,第 28 冊,109 頁,標題 “ Grain Boundary Precipitation in an Fe_7.8Al-1.7Mn-0.8Si-1.0C Alloy” 、 Liu,T· F.所發表,1990年,美國專利第4968357號,標題 “ Hot-Rolled Alloy Steel Plate” 。 綜合上述研究結果,其主要成份為鐵、鋁、錳、碳, 锰元素的添加主要可穩定沃斯田鐵相,使此合金在室溫或 低溫均為面心立方(FCC )結構,以改善Fe_Al或Fe-Al-C 合金的脆性,而使此合金具有良好的動性與加工性,铭元 1235677 強化:辛广金的抗氧化性和抗難,碳主要可析出 备速、、卒火合金於咖〜12啊間做㈣化熱處理後 广!:,並於450〜灣間做時效處理。當合金在泮火 狀態時為單一沃斯田鐵相,、… Ψ 熱處理時,百先會有細微 (Fe,Mn)3AlCx /c相碳化物均勻 J J蝥合(coherent)在基地内 析出。此外,依成份不同在長時間時效處理後,在晶界上 會產生-Μη或r —々+ ^ 7 召_Mn+a相等相分解反應 ’此日日界粗大召-Μη析出妨7 ϋ定、生;、,, 、 何出物將造成材料延性降低。因此, 在沃斯田鐵基地產生均勺敕 7 9且整合之κ相碳化物,而沒有粗 大的⑽析出物於晶界形成,乃為鐵—銘—猛―破合金 獲致咼強度及高勃性之重要方法。 依據上述的研究成果發現,鐵-紹-猛合金主要成份 範圍為鐵、5〜12w.t.%的紹、2〇〜35w t %的猛及㈠〜 !·_的碳’其經固溶化、淬火及時效處理&,依合金 成份不同,其抗拉強度介於8〇〜2〇〇ksi之間,降伏強度介 於60〜臟S1之間,而延伸率則介於62〜25%之間,如附 件-之表三及表四所示,係分別為過去專家學者研究之典 型鐵一鋁一錳合金成份與其機械性質比較表。 過去發明者曾經對鐵·10%|g_3mi%碳合金及@_ 動-30%猛-0.8%碳合金進行研究分析,其結果顯示,鐵-10%銘-30%猛-1%碳合金經過〇 5〜2小時的11〇〇〇C熱處理 後,其硬度值A HRb82.7〜88 9,抗拉強度值為⑴〜 1觸,降伏強度值為79.7〜971^,延伸率則為58 9〜 63‘3%’其晶粒尺寸(d)與抗拉強度(σ)之Hall-Petch 12 1235677 關係式為σ =68·72 + 21 ·2χ d_0.46,經鹽霧試驗以高濃度鹽 水喷射48小時後顯示其抗蝕性不佳,且其在其他專家學者 所研究之熱加工條件溫度1050〜12〇〇〇c熱鍛加工後之材料 表面粗糙度為Ra=3.1〜5.9#m。而鐵-8%鋁-30%錳-0.8%碳 合金,其經過0·5〜2小時1100X;之熱處理後,其抗拉強 度值為110〜120ksi,與鐵_1〇%鋁_3〇。/。錳_1%碳之合金差異 不大/、有降伏強度值為71.1〜83.1 ksi變化稍大,其延伸 率亦維持纟58.5〜64·7%之間,晶粒尺寸⑷與抗拉強度 (σ )之 Hall_Petch 關係式為 σ =69·25 + 23·6χ d_0.45,經 鹽霧試驗以高濃度鹽水噴射48小時後顯示其抗則生不佳, 且其在專豕學者所研究之熱加工條件溫度〜I]⑻。◦熱 鍛加工後之材料表面粗糙度為Ra=3.2〜5.7#m。 【發明内容】 八有於此本發明者乃利用合金設計與製程處理之理 心 十出本么月鬲爾夫球鐵桿頭合金材料,藉以提供_ 種具有低松度(密度在/ 3 〇 又隹6.78〜7.〇5g/cm3之間)及高延展特Decompositions in an Austentic Fe-8.7Al-29.7Mn-l.04C Alloy ", published by Hwang, C · N ·, et al., 1993, Scripta Metall, Vol. 28, p. 109, title" Grain Boundary Precipitation in an Fe_7 .8Al-1.7Mn-0.8Si-1.0C Alloy ", published by Liu, TF, 1990, U.S. Patent No. 4968357, titled" Hot-Rolled Alloy Steel Plate ". Based on the results of the above studies, the main ingredients For iron, aluminum, manganese, carbon, the addition of manganese mainly stabilizes the Wastfield iron phase, making this alloy a face-centered cubic (FCC) structure at room temperature or low temperature to improve Fe_Al or Fe-Al-C alloys The brittleness of the alloy makes this alloy have good mobility and processability. Mingyuan 1235677 strengthens: the oxidation resistance and resistance of Xin Guangjin, carbon can be mainly precipitated and prepared, and the quenching alloy can be converted into caustic ~ 12 ah Wide after heat treatment !: and aging treatment between 450 ~ wan. When the alloy is in the beating state, it is a single Vostian iron phase, ... Ψ During heat treatment, Baixian will have fine (Fe, Mn) 3AlCx / c Phase carbides uniformly JJ coherent precipitated in the base. In addition, Depending on the composition, after a long-term aging treatment, -Mη or r —々 + ^ 7 will be generated on the grain boundaries. The phase decomposition reaction of _Mn + a is equal to this. ; ,,,, and what will produce the material will reduce the ductility of the material. Therefore, even 敕 7 9 and integrated κ phase carbides will be generated at the Wotsian Iron Base, without coarse precipitates forming at the grain boundaries. The iron-ming-mighty-broken alloy is an important method to obtain the strength and high robustness of the alloy. According to the above research results, it is found that the main components of the iron-shao-mighty alloy are iron, 5 ~ 12w.t.% of Shao, 2〇 ~ 35w t% of fierce and ㈠ ~! __ carbon 'It is solid solution, quenched and aging treatment &, depending on the composition of the alloy, its tensile strength is between 80 ~ 2000ksi, drop strength It is between 60 ~ dirty S1, and the elongation is between 62 ~ 25%. As shown in Tables 3 and 4 of the appendix-, they are typical iron-aluminum-manganese alloy components studied by experts and scholars in the past. Comparison table with its mechanical properties. In the past, the inventors have studied iron · 10% | g_3mi% carbon alloy and @_ 动 -30% 猛 -0.8% carbon alloy The analysis shows that the iron -10%, -30%, and -1% carbon alloys have been subjected to a 11,000 ° C heat treatment for 5 to 2 hours, and their hardness values are A HRb 82.7 to 88 9, and tensile strength values. For ⑴ ~ 1 contact, the drop strength value is 79.7 ~ 971 ^, and the elongation is 58 9 ~ 63'3% '. The Hall-Petch 12 1235677 relationship between the grain size (d) and the tensile strength (σ) is σ = 68 · 72 + 21 · 2χ d_0.46. After spraying with high-concentration salt water for 48 hours after salt spray test, it shows that the corrosion resistance is not good, and the temperature of hot processing conditions studied by other experts and scholars is 1050 ~ 12. 〇〇cThe surface roughness of the material after hot forging is Ra = 3.1 ~ 5.9 # m. For iron-8% aluminum-30% manganese-0.8% carbon alloy, after 0.5 ~ 2 hours 1100X; after heat treatment, its tensile strength value is 110 ~ 120ksi, and iron-10% aluminum_3〇 . /. Manganese _1% carbon alloys have little difference / with reduced yield strength values ranging from 71.1 to 83.1 ksi. The elongation also maintains between 纟 58.5 ~ 64 · 7%, grain size ⑷ and tensile strength (σ The Hall_Petch relation of) is σ = 69 · 25 + 23 · 6χ d_0.45. After spraying with high concentration saline for 48 hours after salt spray test, it shows poor resistance, and it is hot-processed by scholars. Conditional temperature ~ I] ⑻. ◦The surface roughness of the material after hot forging is Ra = 3.2 ~ 5.7 # m. [Summary of the Invention] The present inventors have made use of the principles of alloy design and process treatment to produce a variety of alloy materials with low looseness (density in / 3 〇 and隹 6.78 ~ 7.05g / cm3) and high extension special

性(延伸率65%以上、,. A 抗拉強度;丨於8〇〜13〇ksi之間, 降伏強度"於6G〜75ksi之間,且具有抗#性之素材,有 別=過去專家學者所研究設計之範4,並且更符合用以製 作咼爾夫球鐵桿頭或空 > 4二U鐵桿頭之南強度、高延展性、古 防銹性及優良鍛造加τ &热> ^ k Μ工性要求的實用性材料者。 本發明設計之主敢g Μ 王要目的係在於:提供一種低密度、古 延展性、高強度及离JJ* Μ ^ 0錢特性的高爾夫球鐵桿頭合金材料 13 1235677 為達成前揭目的,本發明所提出之技術方案係令該合 金材料主要具有23.0〜3〇.〇w.t·%錳、6.3〜lO.Ow.t·%鋁、 0.8 l.〇5w.t·% 碳、3.0 〜9.0%w.t.絡、0.2 〜lO.Ow.t·%始’其 中亦可添加〇·6〜l.〇w.t·%矽、〇.2〜〇.4w.t.%氮,且其餘重量 比例均以鐵為基材組合而成。由於添加鉻元素具有極佳的 抗大氣餘腐性,且在55〇〜67〇〇C之時效處理,會產生B2、 DC>3、Ci^C3等析出物,造成合金硬度急升與脆化現象。添 加始70素經由適當的鑄造程序後,經由1000〜1050GC溫度 下锻造處理,去除由肥粒鐵(“)及沃斯田鐵(〇所組成的雙 相組織’可獲致極佳的表面性質;再經由1030〜1080GC溫 度I5〜60分鐘熱處理及45〇〜85〇〇c溫度4〜24小時熱處理, 其金相組織為完全沃斯田鐵和雙晶結構,可延遲/c、Cr7C3 等碳化物析出,即可獲得極佳的延展性與抗拉強度組合, 故使得該合金可達到高強度、低密度、高延展性、高防銹 性及優異的表面性質之高爾夫球頭鐵桿頭設計目的。 【實施方式】 為使貴審查委員能更進一步瞭解本發明之組成成份 及其機械性質,茲附以圖式詳細說明如后: 本發明係關於一種低密度高延展性鐵基之高爾夫球鐵 桿頭合金材料,請配合參看附件二表一所示,其主要之元 素組成成份包括有鐵、錳、鋁、碳、鉻、鈷,其中亦可添 加石夕、氣;其中,猛之成分為23.0〜3〇.〇w.t.〇/0、|呂之成分 為6.3〜l〇.〇w.t_%、碳之成份為〇 8〜1〇5w t %、鉻之成份 Ϊ235677 為3.0〜9.0w.t.%、鈷之成份為〇.2%〜1〇〇wt%,矽之成份 為0.6〜l.Ow.t·%、氮之成份為〇·2〜〇.4w.t·%,其餘重量比 例均以鐵為基材所組合而成合金材料。 以下即配合實施例詳細說明,如附侔—本—α Α ⑴—衣二所示,編 號丨〜⑺為本發明之成分範疇,編號u〜15為比較實施例 〇 再由第一圖及第二圖所示可知,鐵_23 89^%錳_ 6.30w.t·% 鋁-0.82w.t_% 碳-3.67w.t_% 鉻-3.98wt%鈷所組成 之編號1合金材料,經1030°C溫度15分鐘及45(rc溫度 泰 4〜12小時熱處理後,其機械性質為抗拉強度值為n2.3ksi ’降伏強度值為68.3ksi,延伸率可達67·2%,再經1〇〇〇(>c 熱鍛加工後表面粗糙度可達2.5# m。若i〇8(rc溫度6〇分 鐘及850。(:溫度12〜24小時熱處理後,其機械性質則變化 為抗拉強度值為114.8ksi,降伏強度值為63.1ksi,延伸率 可達7 3 · 9 %,再經1 〇 5 〇 °C熱鍛加工後表面粗糙度可達2.1 // m。且其球頭經鹽霧試驗48小時及高爾夫球砲擊3〇〇〇 發试驗均合格。同樣的,編號2〜1 〇合金材料之成分在本 眷 發明範疇内,經1〇3〇°c溫度15分鐘及450°C溫度4〜12小 時或1080°C溫度60分鐘及850°C溫度12〜24小時熱處理後 ’其機械性質抗拉強度值介於106.1〜119.4ksi之間,降伏 強度值則介於62.6〜74.7ksi之間,延伸率可達65.9〜 76.1%,表面粗糙度達2 8 # m以下,且鹽霧試驗48小時 及高爾夫球砲擊試驗均合格。 而菖合金材料中不添加始(比較例編號1 1、1 2、1 3合 15 1235677 金材料)時,雖然其機械性質部分符合要求,但是會產生 B2、⑽3、⑽3等析出物,造成合金硬度急升與脆化現象 。。換言之,必須添加鈷可延遲λ等碳化物析出,即 可獲得極佳的延展性與抗拉強度組合。 、本發明合金範圍材料,經由1000°c之溫度熱鍛加工, 並經1030 C溫度15分鐘及45(rc溫度4〜12小時熱處理, 則合金材料之延展性可到達65.9%;若經1080。(:溫度6〇 刀鐘及850 C溫度12〜24小時熱處理,則合金材料之延展 性可提昇到70%以上。 ▲ 本發明經由前揭技術方案之設計,該合金鑄件沃斯 田鐵基地電子顯微鏡明視野圖,如第三圖所示;該合金鑄 件肥粒相中D〇3[l〇〇]軸之電子顯微鏡擇趨繞射圖,如第四 圖所不,該合金鑄件[U1].電子顯微鏡暗視野圖,如第五 圖所不’该合金電子顯微鏡明視野圖,如第六圖所示;該 合金經570GC時效處理!^"]軸之電子顯微鏡明視野圖,如 第七圖所示;該合金經57〇〇c時效處理之電子顯微鏡暗視 野圖,如第八圖所示;鑄件κ相碳化物之電子顯微鏡暗視鲁 野圖,如第九圖所示;其α相區之i 10軸方向電子顯微鏡 擇區繞射圖,如第十圖所示;D〇3相^之電子顯微鏡 日曰視野圖,如第十一圖所示;該合金鍛造,經1〇8〇。^固溶 處理60分鐘’水淬之顯微結構金相圖,如第十二圖所示·, 該合金鍛件固溶&相碳化物之電子顯微鏡明視野圖,如第 十三圖所示。 以下再分別針對各種添加合金元素之設計比例、限制 16 1235677 範圍及其對於合金材料性質之影響一一說明如下. 掹:料常是與鐵共存,由於絲易與硫結合,可消 除硫對於合金材料造成熱脆性 合金材料中的氧化物,在響而且猛能去除 ⑽,且與㈣相容合成^與奴結合成 體而言,當猛含量低於―。時(Extension rate of 65% or more, A tensile strength; between 80 ~ 130ksi, undulation strength " between 6G ~ 75ksi, and materials with resistance #different = past experts The standard 4 studied and designed by scholars is more in line with that used to make golf club heads or hollow > 4 2U iron heads with south strength, high ductility, ancient rust resistance and excellent forging plus τ & heat & gt ^ k Μ practical material requirements. The main objective of the design of the present invention is to provide a golf ball with low density, ancient ductility, high strength and JJ * Μ ^ 0 characteristics. Iron head alloy material 13 1235677 In order to achieve the purpose of the previous disclosure, the technical solution proposed by the present invention makes the alloy material mainly have 23.0 ~ 30.0 wt ·% manganese, 6.3 ~ 10.Ow.t ·% aluminum, 0.8 l 〇5w.t ·% carbon, 3.0 ~ 9.0% wt, 0.2 ~ 10.ww.t ·%, of which 0.6 ~ 1.0wt.% Silicon, 0.2 ~ 0.4w .t.% nitrogen, and the rest of the weight ratio is based on the combination of iron. As chromium is added, it has excellent resistance to atmospheric residual corrosion, and it is aged at 55 ~ 67〇C. B2, DC > 3, Ci ^ C3 and other precipitates are generated, causing the hardness of the alloy to rise sharply and embrittlement. After adding the first 70 elements through the appropriate casting process, the forging process is performed at a temperature of 1000 ~ 1050GC to remove the iron from the fertilizer ( ") And Vostian iron (〇 formed by the dual-phase structure 'can achieve excellent surface properties; and then through 1030 ~ 1080GC temperature I5 ~ 60 minutes heat treatment and 45 ~ 8500c temperature 4 ~ 24 hours heat treatment, Its metallurgical structure is a complete Vosstian iron and twin crystal structure, which can delay the precipitation of carbides such as / c, Cr7C3, and can obtain an excellent combination of ductility and tensile strength, so that the alloy can achieve high strength, low Design goals of golf head iron heads with high density, high ductility, high rust resistance, and excellent surface properties. [Embodiment] In order to allow your reviewers to further understand the composition and mechanical properties of the present invention, herewith The detailed description of the drawings is as follows: The present invention relates to a low-density and high-ductility iron-based golf iron head alloy material. Please refer to Table 1 in Appendix II. The main elements include , Manganese, aluminum, carbon, chromium, cobalt, among which Shixi and gas can also be added; among them, the composition of fierce is 23.0 ~ 30.0 wt% / 0, and the composition of Lu is 6.3 ~ l0.0%. t_%, the composition of carbon is 08 ~ 105wt%, the composition of chromium Ϊ235677 is 3.0 ~ 9.0wt%, the composition of cobalt is 0.2% ~ 100wt%, and the composition of silicon is 0.6 ~ l. Ow.t.%, nitrogen components are 0.2 ~ 0.4 w.t.%, and the rest of the weight ratio is made of iron as the base material to form an alloy material. The following is a detailed description in conjunction with the examples. As shown in the attached 侔 — 本 —α Α ⑴— 衣 二, the numbers 丨 ~ ⑺ are the components of the present invention, and the numbers u ~ 15 are comparative examples. As shown in the two figures, it is known that iron_23 89 ^% manganese_ 6.30wt ·% aluminum-0.82w.t_% carbon-3.67w.t_% chromium-3.98wt% cobalt composed of No. 1 alloy material, after 1030 ° C The temperature is 15 minutes and 45 ° C. After 4 to 12 hours of heat treatment, its mechanical properties are tensile strength value of n2.3ksi, 'dropping strength value of 68.3ksi, elongation of up to 67.2%, and then 10%. 〇 (&c; c The surface roughness after hot forging can reach 2.5 # m. If i〇8 (rc temperature 60 minutes and 850. (: temperature 12 ~ 24 hours after heat treatment, its mechanical properties will change to tensile strength The value is 114.8ksi, the drop strength value is 63.1ksi, the elongation can reach 73.9%, and the surface roughness can reach 2.1 // m after hot forging at 105 ° C. And the ball end is salted. The fog test for 48 hours and the 3,000 shots of the golf ball were all qualified. Similarly, the composition of the alloy material numbered 2 to 10 is within the scope of the invention of the family, and the temperature is 10 minutes at 1030 ° C for 15 minutes. The temperature of 450 ° C is 4 ~ 12 hours or the temperature of 1080 ° C is 60 minutes and the temperature of 850 ° C is 12 ~ 24 hours. After heat treatment, its mechanical properties have a tensile strength value between 106.1 ~ 119.4ksi, and the yield strength value is between 62.6 Between ~ 74.7ksi, the elongation can reach 65.9 ~ 76.1%, the surface roughness can be less than 2 ## m, and the salt spray test for 48 hours and the golf shot test are acceptable. However, no addition of rhenium alloy material (comparative example) No. 1 1, 1 2, 1 3 in 15 1235677 gold material), although its mechanical properties partially meet the requirements, it will produce precipitates such as B2, ⑽3, ⑽3, causing the alloy hardness to rise sharply and embrittlement. In other words, Cobalt must be added to retard the precipitation of carbides such as λ to obtain an excellent combination of ductility and tensile strength. The alloy range material of the present invention is hot forged at a temperature of 1000 ° C and subjected to a temperature of 1030 C for 15 minutes and 45 (rc temperature 4 to 12 hours heat treatment, the ductility of the alloy material can reach 65.9%; if 1080. (: temperature 60 knife clock and 850 C temperature 12 to 24 hours heat treatment, the alloy material ductility can be improved More than 70%. ▲ The present invention Based on the design of the front-revealing technical plan, the bright field view of the electron microscope of the Vostian Iron Base of the alloy casting is shown in the third picture; the electron microscope selection of the D03 [100] axis in the fat phase of the alloy casting Diffraction pattern, as shown in the fourth figure, the alloy casting [U1]. Dark field view of the electron microscope, as shown in the fifth figure. Bright field view of the alloy electron microscope, as shown in the sixth figure; Aging treatment! ^ &Quot;] A bright field diagram of an electron microscope of an axis, as shown in the seventh figure; A dark field diagram of the electron microscope, which is subjected to 5700c aging treatment, as shown in the eighth figure; κ phase carbides of the casting Luye diagram of electron microscope scotopic vision, as shown in the ninth diagram; selected area diffraction pattern of the i 10-axis direction electron microscope of the alpha phase region, as shown in the tenth diagram; electron microscope of D03 phase ^ The perspective view is shown in the eleventh figure; the alloy is forged and subjected to 1080. ^ Solution-treated 60 minutes' water-quenched microstructure metallographic diagram, as shown in Figure 12. · The electron microscope bright field diagram of the alloy forged & phase carbide, as shown in Figure 13 . The following is a description of the design proportions of various added alloy elements, the limits of the range of 16 1235677, and their effects on the properties of alloy materials. 掹: Materials often coexist with iron. Due to the combination of silk and sulfur, sulfur can be eliminated. The material causes the oxides in the hot-brittle alloy material to remove radon, and it is compatible with radon and synthesized with the combination of slave and slave, when the radon content is lower than-. Time

大於3丄/〇時,則將促使/? -Μη相 在晶界析出,造成脆性。因此,本發明之 量應嚴格限制在23〜30wt %之間。 -、、猛含 長,:成:::種極佳的脫氧劑,其不僅可仰制結晶粒成 延展性、加工性及…整體::=:合丄材料之 6.3w.t·%時,將使合金田呂3里低於 ,反+之降伏強度低於預期目標55kS1 右鋁έ置大於7.8w_t%時 目標7〇ksi。因此,太路a日+人 1仇強度大於預期 mu i 合金㈣M +When it is larger than 3 丄 / 〇, the /?-Mn phase will be precipitated at the grain boundary, resulting in brittleness. Therefore, the amount of the present invention should be strictly limited to between 23 and 30% by weight. -、、 Contains long and strong ::::: An excellent deoxidizer, which can not only make crystal grains into ductility, processability, and ... whole :: == 6.3wt ·% of composite materials, will Make the alloy Tianlu 3 li lower, and the reverse + lowering strength is lower than the expected target 55kS1 when the right aluminum handle is greater than 7.8w_t%, the target 70ksi. Therefore, the strength of Tailu a day + person 1 is greater than expected mu i alloy ㈣M +

制在6.3〜i0.0w t %之間。 屑”口限 碳:碳元素除了為碳化物析出作用外, 鐵穩定相之元素,隨著碳含量 疋/田 鐵愈穩定。整體而言,當碳含量大於肥粒鐵減少而沃斯田 料即可稃定开n浙抖 大於〇_5w.t%時’合金材 期目才二 鐵相,而為使降伏強度達到介於預 期目標55〜70hi夕門 jJ "么頂 0 本毛明之合金材料其碳含|f 格限制在O.M.Okt o/o之間。 十-厌3里應嚴 鉻:在合金材料中添加鉻時,不僅可增加合金材料的 17 1235677 腐蝕及氧化抵抗性,又可提昇合金材料之硬化能及高溫強 度尤其是對於高碳鋼之耐磨耗性更有極顯著之效果。整 體而言,當鉻含量低於5.0w.t.%時,將使該合金材料所作 ’载杯頭不符合鹽霧試驗標準,而當鉻含量大於9 Ow j % =’則其延伸率將低於65%之預期目標。因此,本發明之 材料其鉻含量應嚴格限制在5.0〜9_0w.t_%之間。若鉻 含量低於5.0w.t·%,則應加以電鍍處理,以增加其抗㈣ 疋現令超硬性高速 、 ▼,〜,丨〜…又,丨土同逆綱甲敢重要 必添加之元辛。φ i_ ” 要係了 ^加一久硬化能,紅硬性和熱硬 *。由於钻元素溶人肥粒鐵(《_Fe)及沃斯田鐵(A)中可辦 鐵鍵與鐵鐵鍵的共價結合力,所以銘元素無論在^ 面溫皆可強化合金的基體,以及提高鐵基合金之炼點 =此,本發明之合金㈣訪含量應嚴格限 lO.Ow.t·%之間。 及抑!\:石夕在合金材料内有防止氣孔形成、增進收縮作用 及、加鋼液流動性特點 將使延伸率低於仁疋田石夕3 I大於Mw.t.%時, 料若能添力,_〇6〜1()°之預期目標。因此’本發明之合金材 。 · w.tv。之矽,將有助於鑄件原料之製程 氮·在合金材料中 沃斯田鐵相,且可達到 降低材料韌性。因此, 在 〇·2〜0.4w.t.o/〇之間。 、、4、加氮時,可穩定合金材料之FCC 晶粒細化作用。當氮含量過大時, 本發明之合金材料其氮含量宜限制 18 1235677 整體而言,以本發明之合金材料製作高爾夫球鐵桿頭 時’右是以鍛造成型m麵〜丨㈣。c溫度熱锻造, 可得到Ra=3#m以下之最佳表面精度,若在刪叫細 C溫度熱加工除了會增加氧化層夕卜將使工件之表面粗度 Ra大於3 # m,不利於高爾夫球頭品質。 藉由上述設計,使本發明高爾夫球鐵桿頭合金材料具 有以下優點: 1·機械強度:由於紹、鐘、碳之含量適當控制,其抗 拉強度值可介於110〜120ksi之間,降伏強度值可介於65 :75kS1之間,若以該合金材料製作鐵桿頭,將可發揮高爾 夫球鐵桿頭或空心鐵頭的最佳要求。 ^低密度:由於合金中添加63〜1〇加丄%之銘元素 ’且該合金材料為面心立方結構(FCC),故可以有效降 低合:材料之密度1 6.78〜7.〇5g/cm3,若以該合金材料製 作鐵桿頭,在同樣曹詈柏政 J银董里規格限制之下可得較大的鐵桿頭體 積’使鐵桿頭具有較大的形狀設計變化空間。 3·同延展性:其合金材料中除了添加紹以增加延展性 J加鈷,可延遲K C^C3等碳化物析出,防止合金 1急升與脆化現象’獲得極佳較展性與抗拉強度組合 八 金材料又可經過1030°C溫度15分鐘及45(TC溫度 寺熱處理’則合金材料之延展性可到達Μ .9%;若 =吖溫度6〇分鐘及850t溫度12〜24小時熱處理,則 &金材料之延展性可提昇到70%以上。 4.耐餘性:因為其合金材料中添加鉻,該些元素對於 19 1235677 抗大氣蝕腐性均有極佳 桿頭或空心鐵頭的製造成1時將可減少高爾夫球鐵 表卞上所述,名、态 下,本發日月所設的合金成分控制及鍛造溫度條件之 度、高延展性、;=夫球鐵桿頭合金材料,具有低密 品質等特點1為製作言爾去::t驗、及南的锻造表面 應符合發明專# ° ;鐵才干碩之最佳合金材料, "專利要件,妥依法提出申請。 【圖式簡單說明】 (一)圖式部分 Q ·本發明合金經1 、土1c,故溶化處理3〇分 第 圖 鐘後,水淬之金相顯微結構。 •本發明合金經^ $ η 0 nJL· j. 玉、工55〇 c,時效處理4小時後 第三圖 第四圖 第五圖 第六圖 苐七圖 第八圖 水淬之金相顯微結構。 :本發明合金鑄件沃斯田鐵基地電子顯微鏡 明視野圖。 本發明合金鑄件肥粒相中D〇3[1〇〇]軸之電 子顯微鏡擇趨繞射圖。 本么明合金鑄件[1 1 i ]軸電子顯微鏡暗視野 圖。 本發明合金電子顯微鏡明視野圖。 本發明合金經570〇C時效處理以丨丨]軸之電 子顯微鏡明視野圖。 本發明合金經570GC時效處理之電子顯微 鏡暗視野圖。 20 丄235677 第九圖··鏟从 ^ 、件/C相碳化物之電子顯微鏡暗視野照片 〇 第十圖 : 士 01目區之110軸方向電子顯微鏡擇區繞射 圖。 第十一圖:DO him 3相-1 1 1之電子顯微鏡暗視野照片 圖本發明合金鍛造,經1〇8〇°C固溶處理 第一 60分鐘,水淬之顯微結構金相圖。 圖·本發明合金鍛件固溶K相碳化物之電子 鲁 顯微鏡明視野照片。 (一) 凡件代表符號:無 (二) 附件部份: 附件一: •係精密脫蠟鑄造法與鍛造加工法所製作之 鐵桿頭特性比較表。 •係目則用以製作鐵桿頭之材料機械性質比 較表。 φ 表二·係目前學術界已研究發表之典型鐵一鋁一 錳合金成份表。 表四·係目别學術界已研究發表之典型鐵一鋁一 猛合金的機械性質比較表。 附件二: ~ 係本發明之實施例組成成份表。 係本發明之實施例材料特性比較表。 21The system is between 6.3 ~ i0.0w t%. "Clips" limit carbon: In addition to the precipitation of carbides, the element of the iron stable phase becomes more stable with the carbon content of 疋 / field iron. In general, when the carbon content is greater than the iron content of the fertilizer, Fes can be reduced. When it is determined that n is greater than 0_5w.t%, the alloy phase is only ferrous, and in order to achieve the yield strength between the expected target of 55 ~ 70hi Ximen jJ " Moding 0 this Maoming alloy material Its carbon content f is limited to OMOkt o / o. Ten-anion 3 should be strict chromium: When chromium is added to the alloy material, not only can it increase the corrosion resistance and oxidation resistance of the alloy material 17 1235677, but also improve The hardening energy and high temperature strength of the alloy material, especially for the wear resistance of high carbon steel, have a more significant effect. In general, when the chromium content is less than 5.0wt%, the alloy material will make Does not meet the salt spray test standards, and when the chromium content is greater than 9 Ow j% = ', its elongation will be lower than the expected target of 65%. Therefore, the chromium content of the material of the present invention should be strictly limited to 5.0 ~ 9_0w.t_% If the chromium content is less than 5.0wt ·%, it should be electroplated to Increasing its resistance to 疋 now makes super-hard high-speed, ▼, ~, 丨 ~ ... and, 丨 soil and inverse Ganga must be important to add the element Xin. Φ i_ ”to be tied ^ plus a long-term hardening energy, red hardness and heat hard*. As the drilling element can dissolve the fertile grain iron ("_Fe") and Vostian Iron (A), the covalent bonding force between iron bond and iron-iron bond can be used, so Ming element can strengthen the matrix of the alloy regardless of the surface temperature, And increase the refining point of the iron-based alloy = this, the alloy visit content of the present invention should be strictly limited to lO.Ow.t.%. And suppression! \: Shi Xi has the function of preventing the formation of pores in the alloy material, improving the shrinkage effect, and adding the fluidity of the molten steel, which will make the elongation lower than that of Renxi Tianshi Xi 3 I greater than Mw.t.%, if the material can Tim Li, _〇6 ~ 1 () ° is the expected goal. Therefore, the alloy material of the present invention. W.tv. Silicon will help the process of casting raw materials. Nitrogen · In the alloy material, Wastfield iron phase, and can reduce the toughness of the material. Therefore, it is between 0.2 and 0.4 w.t.o / 〇. When the nitrogen is added, the FCC grain refinement of the alloy material can be stabilized. When the nitrogen content is too large, the nitrogen content of the alloy material of the present invention should be limited. 18 1235677 In general, when the golf iron head is made of the alloy material of the present invention, the right side is a forged m-plane ~ 丨 ㈣. C temperature hot forging can get the best surface accuracy below Ra = 3 # m. If it is called fine C temperature hot working, it will increase the oxide layer, and the surface roughness Ra of the workpiece will be greater than 3 #m, which is not good for Golf head quality. With the above design, the golf iron head alloy material of the present invention has the following advantages: 1. Mechanical strength: Due to the proper control of the content of Shao, Zhong, and carbon, its tensile strength value can be between 110 ~ 120ksi, and the drop strength The value can be between 65: 75kS1. If the iron head is made of this alloy material, the best requirements of a golf iron head or a hollow iron head will be exerted. ^ Low density: As the alloy is added with 63 ~ 10 plus 丄% inscription element, and the alloy material has a face-centered cubic structure (FCC), it can effectively reduce the density of the material: 1 6.78 ~ 7.05 g / cm3 If iron alloy heads are made of this alloy material, a larger iron head volume can be obtained under the same Cao Yubaizheng J Yin Dongli's specifications, so that the iron head has a larger space for shape design changes. 3 · Same ductility: In addition to the addition of Sha to increase the ductility of J and cobalt, it can delay the precipitation of carbides such as KC ^ C3 and prevent the rapid rise and embrittlement of Alloy 1 'to obtain excellent ductility and tensile strength. The strength combination of eight gold materials can be subjected to a temperature of 1030 ° C for 15 minutes and 45 (TC temperature temple heat treatment ', then the ductility of the alloy material can reach M. 9%; if == acridine temperature 60 minutes and 850t temperature 12 ~ 24 hours heat treatment , Then the ductility of & gold materials can be increased to more than 70%. 4. Residual resistance: Because chromium is added to its alloy materials, these elements have excellent club heads or hollow iron for 19 1235677 atmospheric corrosion resistance When the head is manufactured to 1, it will reduce the golf iron watch as described above. In the name and state, the alloy composition control and forging temperature conditions set by the present sun and the moon are high, and the ductility is high; Alloy materials with low-density quality, etc. 1 for making speeches: The test surface and the forged surface of the south should conform to the invention # °; the best alloy material for iron talents, " patent requirements, properly apply according to law [Schematic description] (I) Schematic part Q · The alloy of the invention has undergone 1 and soil 1c, so the metallurgical microstructure of the water-quenched metal is 30 minutes after the melting process. Figure • The alloy of the invention is treated with ^ $ η 0 nJL · j. The third figure, the fourth figure, the fifth figure, the sixth figure, the seventh figure, and the eighth figure. Water-quenched metallurgical microstructures .: A bright field view of an electron microscope of the alloy casting Vostian Iron Base of the present invention. Selective diffraction pattern of the electron microscope on the D03 [100] axis. Dark field view of the [1 1 i] axis electron microscope of this alloy casting. Bright field view of the electron microscope of the alloy of the present invention. Bright-field view of an electron microscope with C aging treatment on the axis of 丨 丨]. Dark-field view of an electron microscope with 570GC aging treatment of the alloy of the present invention. 20 235677 Ninth image ·· Electron of shovel from ^, pieces / C phase carbide Dark field photo. Tenth image: Selected area diffraction pattern of 110-axis direction electron microscope in the Shi 01 mesh area. Figure eleven: DO him 3-phase-1 1 1 dark field photo image of the electron microscope. The first 60 minutes of solution treatment at 108 ° C Metallurgical diagram of the microstructure of water quenching. Figure · Electrical microscope micrograph of the solid solution of K-phase carbides of the alloy forging of the present invention. (1) Symbols of all parts: None (II) Attachment part: Attachment 1: • It is a comparison table of the characteristics of iron heads produced by precision dewaxing casting method and forging process. • It is a comparison table of the mechanical properties of materials used to make iron heads. Φ Table 2 is a typical iron that has been researched and published by the academic community. Table of the composition of an aluminum-manganese alloy. Table 4: A comparison table of the mechanical properties of typical iron-aluminum-manganese alloys that have been researched and published by academic circles. Attachment 2: ~ is the composition list of the embodiment of the present invention. This is a comparison table of the material properties of the examples of the present invention. twenty one

Claims (1)

1235677 拾、申請專利範圍: 1·一種低密度高延展性鐵基之高爾夫球鐵桿頭合金 材料,其合金材料具有23·〇〜30 0w t.%錳、6 3〜i〇 〇w t % 铭、〇·8〜i.〇5w.t·%碳、5 〇〜9 〇w t %鉻、〇 2〜1〇 〇w」%鈷 ’其餘比例以鐵為基材所組合而成;及將合金材料在丨〇〇〇 〜1050C溫度熱锻加工,使合金鍛材可提昇表面性質,且 表面粗糖度達到3 // m以下。 2 ·如申請專利範圍第1項所述之低密度高延展性鐵 基之高爾夫球鐵桿頭合金材料,其中合金材料添加 0.6〜l.Ow.t·%矽及 〇·2〜〇.4w」·%氮。 拾壹、圖式: 如次頁1235677 Scope of patent application: 1. A low-density and high-ductile iron-based golf iron head alloy material, the alloy material of which has 23.0 ~ 30 0w t.% Manganese, 6 3 ~ i〇〇wt% Ming, 〇 · 8 ~ i.〇5w.t ·% carbon, 50 ~ 90 wt% chromium, 02 ~ 100w "% cobalt" The remaining ratio is made by combining iron as the base material; and alloy material Hot forging at 丨 〇〇〇 ~ 〇1050C, so that the surface properties of the alloy forging can be improved, and the surface coarse sugar content is below 3 // m. 2 · The low-density and high-ductility iron-based golf iron head alloy material described in item 1 of the scope of the patent application, wherein the alloy material is added with 0.6 ~ l.Ow.t ·% silicon and 0.2 ~ 0.4w " ·%nitrogen. Pick up, schema: as the next page 22twenty two
TW93119421A 2004-06-30 2004-06-30 Low density and high ductility ferric-based alloy material for golf iron club head TWI235677B (en)

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