TW200831682A - Cold work die steel, die, and method for production of cold work die steel - Google Patents

Cold work die steel, die, and method for production of cold work die steel Download PDF

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TW200831682A
TW200831682A TW096138897A TW96138897A TW200831682A TW 200831682 A TW200831682 A TW 200831682A TW 096138897 A TW096138897 A TW 096138897A TW 96138897 A TW96138897 A TW 96138897A TW 200831682 A TW200831682 A TW 200831682A
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steel
dimensional deformation
less
hardness
amount
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TW096138897A
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Chinese (zh)
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Shogo Murakami
Tsuyoshi Tonomura
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Kobe Steel Ltd
Nippon Koshuha Steel Co Ltd
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Priority claimed from JP2006294528A external-priority patent/JP4266383B2/en
Priority claimed from JP2007047490A external-priority patent/JP4266384B2/en
Application filed by Kobe Steel Ltd, Nippon Koshuha Steel Co Ltd filed Critical Kobe Steel Ltd
Publication of TW200831682A publication Critical patent/TW200831682A/en

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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/42Ferrous alloys, e.g. steel alloys containing chromium with nickel with copper
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/26Methods of annealing
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D6/00Heat treatment of ferrous alloys
    • C21D6/004Heat treatment of ferrous alloys containing Cr and Ni
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D6/00Heat treatment of ferrous alloys
    • C21D6/02Hardening by precipitation
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D7/00Modifying the physical properties of iron or steel by deformation
    • C21D7/13Modifying the physical properties of iron or steel by deformation by hot working
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/46Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/001Ferrous alloys, e.g. steel alloys containing N
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/02Ferrous alloys, e.g. steel alloys containing silicon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/04Ferrous alloys, e.g. steel alloys containing manganese
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/06Ferrous alloys, e.g. steel alloys containing aluminium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/44Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/46Ferrous alloys, e.g. steel alloys containing chromium with nickel with vanadium
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D2211/00Microstructure comprising significant phases
    • C21D2211/008Martensite

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Heat Treatment Of Articles (AREA)
  • Heat Treatment Of Steel (AREA)

Abstract

Disclosed is a cold work die steel which comprises (by mass): C: 0.20-0.60%, Si: 0.5-2.00%, Mn: 0.1-2%, Cr: 3.00-9.00%, Al: 0.3-2.0%, Cu: 1.00-5%, Ni: 1.00-5%, Mo: 0.5-3% and/or W: 2% or less (including 0%), and S: 0.10% or less (excluding 0%) wherein these components satisfy the following requirements (1) to (3) [wherein each square bracket [ ] means a content (%) of each element]: (1) [Cr] x [C] ≤ 3.00; (2) [Cu]/[Ni]: 0.5-2.2; and (3) [Mo]+0.5 x [W]: 0.5-3.0%, with the remainder being iron and unavoidable impurities. Also disclosed is a die produced by using the steel. Further disclosed is a method for producing the cold work die steel.

Description

200831682 九、發明說明 【發明所屬之技術領域】 本發明係關於冷加工模具用鋼及模具以及冷加工 用鋼之製造方法,更詳細地說,係關於可作爲:將汽 鋼板、家電用鋼板等在常溫或高溫下進行衝製成形( ‘ 、彎折、打凸、修邊等)所使用的模具的素材之有用 具鋼、以及模具鋼之製造方法。 【先前技術】 汽車用鋼板、家電用鋼板等的成形加工所採用的 ,隨著鋼板的高強度化,乃被要求必須改善該模具的 壽命。尤其是汽車用鋼板’因爲考慮到環境問題,要 汽車的省油性能,拉伸強度約5 90MPa以上的高張力 的需求急速地增高,但是伴隨而來的是,模具的表面 會提早受損傷,而發生「咬住現象」(衝製成形時發 φ 結現象),因而產生了模具壽命極端地縮短之問題。 模具係由:模具母材(模具用鋼)與施作於其表 表面硬化層(表面皮膜)所構成的。母材的模具用鋼 般而言,是利用退火·^切削加工—淬火回火處理(本 * 明書中,特別是將淬火處理稱爲熔體化處理;將回火 稱爲時效處理)來製造的。 作爲模具用鋼(冷壓鑄模用鋼),以往迄今係廣 用:以JIS SKD1 1爲代表的高C高Cr的合金工具鋼 進一步改善了耐磨損性的以JI S S KH 5 1爲代表的高速 模具 車用 衝孔 的模 模具 使用 提昇 鋼板 皮膜 生燒 面的 , -- 案說 處理 泛採 ;更 工具 -5- 200831682 鋼等。這些工具鋼主要係藉由Cr系碳化物、Mo、W、V 系碳化物的析出硬化來謀求硬度的提昇。此外,基於同時 提高耐磨損性與韌性的兩種性質之目的,也採用了將 JIS SKH51中的C、Mo、W、V等的合金含有量予以減少 後的低合金筒速工具鋼(一般稱爲:matrix-hsis)。 爲了要進一步改善冷加工模具用鋼的特性,例如:在 專利文獻1〜專利文獻3中,有人提出鋼中成分的改良技 術之方案。 專利文獻1所揭示的方案是想要更爲提昇matrix-hsis (低合金高速工具鋼)的硬度,是藉由令其含有大量的 Nb及/或Ta,以抑制高溫淬火後的結晶粒的粗大化,因而 能夠進行高溫淬火,以謀求高硬度化(提高耐磨損性)的 方法。 專利文獻2所揭示的是關於可達成尺寸變形抑制特性 與高硬度特性之冷壓鑄模用鋼,主要是揭示出:(A)將 因爲淬火時的殘留沃斯田鐵的分解所產生的回火時的膨脹 尺寸變形與因爲Ni-Al系金屬間化合物的析出強化所產生 的尺寸變形抑制作用互相抵.消;(B )利用依據特定的鋼 中成分所算出的偏析指數K來更爲抑制尺寸變形。專利文 獻2的第1圖係顯示出以能夠獲得最大硬度的溫度來進行 回火處理。 專利文獻3係揭示:基於能夠抑制淬火回火處理所導 致的尺寸變化量(尺寸變形),尤其是抑制回火時的膨脹 尺寸變形,以提昇硬度之目的,而添加入適量的Ni、A1, -6- 200831682 並且添加入與該Ni、A1相應的適量的Cu之冷壓鑄模用鋼 。而且也揭示出:調整C以及Cr的含有量,令金屬組織 中的碳化物分布更細微地分散的話,就可以提昇「耐咬住 的特性」。 另外,專利文獻4係揭示:基於降低模具製造成本之 目的,並不採行傳統之先進行切削加工之後才進行淬火回 火處理的方式,而是從淬火回火狀態就進行切削加工(淬 火回火—切削加工)之「預先硬化鋼」的技術。具體而言 ,係揭示出:雖然硬度高卻仍可發揮良好的被切削性之可 在常溫下進行衝孔加工的鋼,尤其是C、Si、以及S的含 有量被適量地控制後的預先硬化鋼。然而,就目前現狀而 言,採用預先硬化鋼的模具的壽命較短,尙未達到實用化 的階段。 上述的專利文獻1〜4,主要是揭示:藉由控制鋼中成 分來抑制熱處理後(時效處理後或回火處理後)的尺寸變 形(尺寸變化),但是,後述的專利文獻5〜7,主要是揭 示:藉由控制淬火、回火等等的熱處理條件來控制尺寸變 形的技術。 其中的專利文獻5係揭示出:藉由分別實施1 5 0〜4 5 0 。(:的低溫回火與4 8 〇〜5 5 0 °C的高溫回火各一次以上,來抑 制淬火回火後的尺寸變化的方法。 專利文獻6係揭示出:執行淬火-0〜-20 (TC的低溫 處理—5 00 °C以下的低溫回火之方法。詳細地說,是揭示 出:藉由以上述的溫度來進行低溫處理,以調整殘留沃斯 200831682 田鐵量,來控制尺寸變化,接下來,進行低溫回火以達成 目標尺寸的方法。 專利文獻7係揭示出:藉由調整鋼中成分來提高淬火 性,藉由控制波來鐵的轉態界限以及以氣體冷卻來進行淬 火時的冷卻速度,以資達成預定的硬度之方法,藉以既可 確保作爲模具所需的硬度又可謀求減少熱處理後的變形。 〔專利文獻1〕日本特開平1 0-3 3 0 894號公報 φ 〔專利文獻2〕日本特開2006-152356號公報 〔專利文獻3〕日本特開2006-169624號公報 〔專利文獻4〕日本特開2002-241 894號公報 〔專利文獻5〕日本特開平9- 1 25204號公報 〔專利文獻6〕日本特開2001-172748號公報 〔專利文獻7〕日本特開2002-167644號公報 【發明內容】 • 〔發明所欲解決的課題〕 對於冷加工模具用鋼所要求的特性,除了前述的高硬 • 度化、具有優異的熱處理後的尺寸變形抑制性之外,還可 以舉出:優異的焊接修補性。 所謂「焊接修補」,主要是藉由焊接來將模具的損傷 (詳細地說,表面硬化層的瑕疵、凹凸等等)加以補正、 修補,基於謀求模具的再生利用之目的而執行的,例如: 目前已經廣泛使用中的利用氬焊來實施的增厚焊接等等。 如前所述’因爲拉伸強度約5 80MPa以上的高張力鋼的需 -8 - 200831682 求增大而導致模具的壽命極端地降低,爲了要減少經費, 乃必須頻繁地對於模具進行焊接修補的作業。 然而,如果對於具有硬化皮膜的模具實施焊接修補的 話,焊接部週邊的硬度的差異程度變大,變得容易發生龜 裂、咬住現象。尤其是會明顯地出現:焊接後的熱影響部 (Heat Affected Zone,HAZ)的軟化(HAZ 軟化),因 此,焊接修補後的模具壽命降低的這種情事將會造成問題 。ΗAZ軟化係在稍微離開融合部(焊接金屬與母材的境界 部,也稱爲「焊接熔融線」)的區域中出現的現象,在該 區域中,加熱溫度是較之融合部更低,因爲是從細粒的沃 斯田鐵來進行轉態,所以淬火性會降低,軟質的肥粒鐵相 所佔的比例變多,在更遠離融合部的地方,係處在高溫回 火的狀態,所以被認爲是硬度降低。第1圖(a )係顯示 將母材彼此之間利用焊接金屬焊接後的狀態之示意圖;第 1圖(b )係第1圖(a )中所示的A區域的硬度分布的示 意圖。如第1圖(b)所示,隨著愈爲遠離融合部,HAZ 的硬度愈降低而變軟。一旦HAZ軟化的話,以後即使再 實施表面硬化處理,也無法充分發揮表面硬化層的保護作 用,表面硬化層將很快就會損傷,因而降低模具的壽命。 此外,焊接修補作業係如前所述,除了是在母材上施 作了表面硬化皮膜之後才被執行的之外,也有的是在母材 上被施作表面硬化皮膜之前就被執行的。尤其是針對於拉 伸強度約590MPa以上的高張力鋼板使用模具進行衝壓成 形時,很難衝壓出與想要的形狀一致的形狀,因此有時候 -9- 200831682 會預先實施試衝壓以及焊接修補(增厚焊接),才能衝_ 出所期待的形狀。在試衝壓過程中,係先進行焊接修補之 後,不再做熱處理就進行衝壓成形,因此在HAZ軟化部 很容易產生瑕疵。這種發生在Η AZ軟化部的瑕疵,也會 殘留在以後所實施的硬化處理所形成的表面皮膜上,因此 ,這種殘留部分被認爲是:將成爲皮膜損傷的起點。此外 ,不僅是在ΗΑΖ軟化部,就連在硬化部也會發生(請參 考第1圖、第7圖),在硬化部容易產生龜裂、缺口而造 成問題。 因此,業界莫不期待有人能夠提供:一種既可抑制焊 接修補時的ΗΑΖ軟化,又可很容易實施轉角部的增厚焊 接之具有優異的焊接修補性之模具用鋼。然而,前述的專 利文獻都是對於焊接修補性完全沒有做任何的考量,因此 ’焊接修補後的模具壽命降低乃是其問題所在。 本發明係有鑒於上述情事而開發完成的,其目的係在 於提供:硬度很高,具有優異的熱處理後的尺寸變形抑制 性’焊接修補性亦良好的冷加工模具用鋼、以及模具。 又’本發明的另一目的係在於提供:可有效率地製造 出硬度很高,具有優異的熱處理後的尺寸變形抑制性的冷 加工模具用鋼之製造方法。 〔用以解決課題之手段〕 亦即,本發明係關於下列的1〜1 2的發明。 -10- 200831682 1. 以質量%換算,符合 C : 〇·20 〜0.60%、 s i : 0 · 5 〜2.0 0 %、 Μ η : 〇 . 1 〜2 %、。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 。 Or a tool for forming a material for a mold used for punching (', bending, embossing, trimming, etc.) at a high temperature, and a method for manufacturing the mold steel. [Prior Art] For the forming of steel sheets for automobiles and steel sheets for home appliances, it is required to improve the life of the molds as the strength of the steel sheets increases. Especially for automotive steel sheets, because of the environmental problems, the fuel-saving performance of automobiles and the demand for high tensile strength of about 5 90 MPa or more are rapidly increasing, but it is accompanied by the early damage of the surface of the mold. A "biting phenomenon" occurs (a φ junction phenomenon occurs when the shape is formed), which causes a problem that the life of the mold is extremely shortened. The mold is composed of a mold base material (steel steel) and a surface hardened layer (surface film) applied thereto. The mold of the base metal is made of annealing and tempering by means of annealing and metal cutting (in this book, especially the quenching process is called melt processing; the tempering is called aging treatment). made. Steel for molds (steel for cold die casting) has been widely used in the past: JI SS KH 5 1 is a representative of high-C high-Cr alloy tool steel represented by JIS SKD1 1 and further improved wear resistance. The mold for punching the high-speed mold car uses the raised steel film to burn the surface, -- the case is treated with general mining; more tools -5 - 200831682 steel. These tool steels are mainly used for precipitation hardening of Cr-based carbides, Mo, W, and V-based carbides to improve hardness. In addition, based on the simultaneous improvement of the two properties of wear resistance and toughness, a low alloy tube speed tool steel in which the alloy contents of C, Mo, W, V, etc. in JIS SKH51 are reduced is also used. Called: matrix-hsis). In order to further improve the characteristics of the steel for cold working molds, for example, Patent Document 1 to Patent Document 3 propose a technique for improving the composition of steel. The solution disclosed in Patent Document 1 is intended to enhance the hardness of matrix-hsis (low alloy high speed tool steel) by suppressing the coarseness of crystal grains after high temperature quenching by containing a large amount of Nb and/or Ta. Therefore, it is possible to carry out high-temperature quenching to achieve high hardness (increased wear resistance). Patent Document 2 discloses a steel for cold die casting which can achieve dimensional deformation suppression characteristics and high hardness characteristics, and mainly discloses: (A) tempering due to decomposition of residual Worth iron during quenching The dimensional deformation at the time of deformation and the suppression of the dimensional deformation caused by the precipitation strengthening of the Ni-Al intermetallic compound cancel each other; (B) the size is further suppressed by using the segregation index K calculated from the specific steel component. Deformation. The first diagram of Patent Document 2 shows that the tempering treatment is performed at a temperature at which the maximum hardness can be obtained. Patent Document 3 discloses that an amount of Ni and A1 is added for the purpose of improving hardness by suppressing the dimensional change amount (size deformation) caused by the quenching and tempering treatment, in particular, suppressing the expansion dimensional deformation during tempering. -6- 200831682 A steel for cold die casting mold containing an appropriate amount of Cu corresponding to the Ni and A1 is added. Further, it has been revealed that the "biting resistance" can be improved by adjusting the content of C and Cr so that the carbide distribution in the metal structure is more finely dispersed. Further, Patent Document 4 discloses that, for the purpose of reducing the manufacturing cost of the mold, the conventional method of performing the quenching and tempering treatment after the cutting processing is first performed, but the cutting processing is performed from the quenching and tempering state (quenching back) Fire-cutting technology for "pre-hardened steel". Specifically, it is disclosed that the steel which can perform punching at normal temperature, which exhibits good machinability, is high in hardness, and in particular, the amount of C, Si, and S is controlled in an appropriate amount. Hardened steel. However, as far as the current situation is concerned, molds using pre-hardened steel have a short life span and have not reached the stage of practical use. In the above-mentioned Patent Documents 1 to 4, it is mainly disclosed that the dimensional deformation (size change) after heat treatment (after aging treatment or after tempering treatment) is suppressed by controlling the components in the steel, but Patent Documents 5 to 7, which will be described later, Mainly to reveal: a technique for controlling dimensional deformation by controlling heat treatment conditions such as quenching, tempering, and the like. Patent Document 5 therein discloses that: 1 50 to 4 50 are respectively implemented. (: A method of suppressing the dimensional change after quenching and tempering at a low temperature tempering and a high temperature tempering of 4 8 〇 5 5 5 ° C. Patent Document 6 discloses: performing quenching - 0 to -20 (TC low temperature treatment - low temperature tempering method below 500 ° C. In detail, it is revealed that the temperature change is controlled by low temperature treatment at the above temperature to adjust the amount of residual Worth 200831682 field iron, Next, a method of low-temperature tempering to achieve a target size is disclosed. Patent Document 7 discloses that the quenching property is improved by adjusting the composition of the steel, and the quenching property of the iron is controlled, and quenching is performed by gas cooling. In order to achieve the hardness required for the mold, it is possible to reduce the hardness required for the mold and to reduce the deformation after the heat treatment. [Patent Document 1] Japanese Patent Laid-Open No. Hei 1 0-3 3 0 894 [Patent Document 2] Japanese Laid-Open Patent Publication No. Hei. No. 2006-169624 (Patent Document 4) JP-A-2002-241 894 (Patent Document 5) [Patent Document 6] Japanese Laid-Open Patent Publication No. 2001-172748 (Patent Document 7) JP-A-2002-167644 [Summary of the Invention] [Problems to be Solved by the Invention] Requirements for Steel for Cold Working Dies In addition to the above-mentioned high hardness and high dimensionality, and excellent dimensional deformation inhibition after heat treatment, it is also excellent in weld repairability. The so-called "welding repair" mainly involves welding the mold. The damage (in detail, the flaw, the unevenness of the surface hardened layer, etc.) is corrected and repaired, and is performed for the purpose of recycling the mold, for example, thickening by argon welding which has been widely used at present. Welding, etc. As mentioned above, because the increase in the tensile strength of high tensile steel of about 580 MPa or more is required to increase the life of the mold, the mold life is extremely reduced. In order to reduce the cost, it is necessary to frequently apply to the mold. Perform welding repair work. However, if welding repair is performed on a mold having a hardened film, the difference in hardness around the welded portion The degree becomes large, and it becomes prone to cracking and biting. In particular, it will appear clearly: softening of the Heat Affected Zone (HAZ) after welding (HAZ softening), therefore, the life of the mold after welding repair This reduction in the situation will cause problems. The AZ softening phenomenon occurs in a region slightly away from the fusion portion (the boundary between the weld metal and the base metal, also called the "welding melting line"), in which heating is performed. The temperature is lower than that of the fusion part, because it is transferred from the fine grain of the Worthite iron, so the hardenability is reduced, and the proportion of the soft ferrite iron phase is increased, and it is farther away from the fusion part. It is in a state of high temperature tempering, so it is considered to be a decrease in hardness. Fig. 1(a) is a view showing a state in which the base materials are welded to each other by a weld metal, and Fig. 1(b) is a view showing the hardness distribution of the A region shown in Fig. 1(a). As shown in Fig. 1(b), the hardness of the HAZ decreases and becomes softer as it moves away from the fusion portion. When the HAZ is softened, even if the surface hardening treatment is carried out later, the surface hardening layer cannot be sufficiently protected, and the surface hardened layer is quickly damaged, thereby reducing the life of the mold. Further, the welding repairing operation is carried out as described above except that the surface hardening film is applied to the base material, and is also performed before the base material is applied as the surface hardening film. In particular, when a high-tensile steel sheet having a tensile strength of about 590 MPa or more is formed by press molding using a mold, it is difficult to press a shape that matches the desired shape. Therefore, sometimes the test press and the weld repair are performed in advance - 9-200831682 ( Thickening the weld) to get the shape you want. In the trial press process, after the weld repair is performed, the press forming is performed without performing the heat treatment, so that the flaw is easily generated in the HAZ softened portion. This enthalpy which occurs in the softening portion of the ΗAZ also remains on the surface film formed by the hardening treatment to be carried out later. Therefore, such a residual portion is considered to be a starting point for damage of the film. In addition, it occurs not only in the softening portion but also in the hardened portion (refer to Figs. 1 and 7), and cracks and notches are likely to occur in the hardened portion, which causes problems. Therefore, the industry does not expect anyone to provide a mold steel which can suppress the softening of the weld at the time of welding repair and can easily carry out the thick welding of the corner portion and has excellent weld repairability. However, the aforementioned patent literature does not make any consideration for solder repairability, so the reduction in mold life after solder repair is the problem. The present invention has been made in view of the above circumstances, and an object thereof is to provide a steel for cold working die and a mold which have high hardness and excellent dimensional deformation suppression after heat treatment. Further, another object of the present invention is to provide a method for producing a steel for cold working mold which has high hardness and excellent dimensional deformation inhibition after heat treatment. [Means for Solving the Problem] That is, the present invention relates to the following inventions of 1 to 12. -10- 200831682 1. In terms of mass %, it conforms to C: 〇·20 ~0.60%, s i : 0 · 5 ~2.0 0 %, Μ η : 〇 . 1 〜 2 %,

Cr * 3.00 〜9.00%、 A1 : 〇·3 〜2.0%、 C u : 1 · 0 0 〜5 %、 • Ni : 1 ·〇〇,〜5%、 Μ 〇 : 〇 · 5〜3 %及/或W : 2 %以下(含〇 % )、 S ·· 〇. 1 〇 % 以下(不含 〇 % )、 下列數式(1)〜(3) {〔〕是代表各元素的含有量 (% )之意} 數式(1 ) 〔 Cr〕X〔 C〕€ 3.00、 數式(2 ) 〔 Cu〕/〔 Ni〕: 0.5 〜2‘2、 數式(3 ) 〔 Μ〇〕+ 〇·5χ〔 W〕: 〇·5 〜3.0% φ 之要件,其餘部分是鐵以及不可避免的雜質之冷加工 模具用鋼。 2. 又含有V : 0.5 %以下(不含〇% )之上述1所述之 冷加工模具用鋼。 3. 又含有從由1^、2^、1^、丁3、及>^所組成的群 所選出的至少一種元素,合計爲0.5 %以下(不含0% )之 上述1或2所述的冷加工模具用鋼。 4. 又含有Co : 10%以下(不含0% )之上述1〜3的 任一種所述的冷加工模具用鋼。 -11 - 200831682 5 .以下列數式所表示的麻田散鐵轉態點(Ms點): 係Ms點 =550-361x [ C] -39χ〔 Μη〕-35χ〔 V〕-2〇Χ〔 Cr〕 -17x〔Ni〕-10x〔Cu〕-5χ(〔Mo〕+〔W〕) + 1 5x〔 Co〕+ 30x〔 A1〕 {式中的〔〕是代表各元素的含有量(%)之意} 爲170 °C以上之上述1〜4的任一種所述的冷加工模具 用鋼。 6 ·使用上述1〜5的任一種所述的冷加工模具用鋼所 製得的模具。 7. 一種冷加工模具用鋼之製造方法,是針對符合上 述1所述的組成分之鋼,又包含:備好符合下列數式(4 ){式中的〔〕是代表各元素的含有量(%)之意} 數式(4) 〔Cu〕/〔C〕:4.0 〜15 的要件的鋼之工序;以及 以符合下列數式(5 )的條件來進行熔體化處理及時 效處理的工序, ΤΑ-1 0 ^ T2 ^ TA + 1 〇 …(5 ) 數式(5 )中, TA= 0.29xTl-2.63x [ Cu ] /〔 C〕+ 225, τ 1係熔體化溫度(°C )、 T2係時效溫度(°C )。 8. 前述鋼係含有V : 0.5%以下(不含〇%)之上述7 所述的製造方法。 -12· 200831682 9·前述鋼係含有從由Ti、Zr、Hf、Ta、及Nb所組 成的群所選出的至少一種元素’合計爲〇 · 5 %以下(不含 0% )之上述7或8所述的製造方法。 10.前述鋼係含有Co: 10%以下(不含〇%)之上述 7〜9的任一種所述的製造方法。 11·以下列數式所表示的麻田散鐵轉態點(M S點) φ 係Ms點 =550-361x〔C〕 -39x〔Mn〕 -35x〔V〕 -20x〔Cr〕 -17x〔Ni〕-10x〔Cu〕-5x( 〔Mo〕+ [ W )) + 1 5x〔 Co〕+ 30x〔 A1〕 爲170°C以上之上述7〜10的任一種所述的製造方法 〇 12·由上述7〜1 1的任一種所述的製造方法所製得的 模具。 〔發明之效果〕 本發明的冷加工模具用鋼,係如上所述般地,適切地 控制合金成分,因此硬度很高且具有優異的熱處理後的尺 寸變形抑制性,焊接修補性也良好。因此,採用上述的冷 加工模具用鋼所製得的模具,特別適用於作爲拉伸強度約 5 90MPa以上的高張力鋼板的成形用模具,可更爲提高壽 命’尤其是焊接修補後的壽命。 又,本發明的製造方法,鋼中成分、以及熔體化處理 -13- 200831682 及時效處理的條件係被適切地控制,因此可以有效率地製 造出:硬度很高,具有優異的熱處理後的尺寸變形抑制性 之冷加工模具用鋼。因此,使用本發明的製造方法所製得 的模具,特別適用於作爲拉伸強度約5 9 0 Μ P a以上的高張 力鋼板的成形用模具,可更爲提高壽命,尤其是焊接修補 後的壽命。 φ 【實施方式】 〔用來實施發明之最佳形態〕 以下將詳細說明本發明。又,本說明書中的百分率, 如果未特別加以限定的話,分別都是以質量作爲基準。此 外,以質量所定義的所有的百分率係與以重量所定義的所 有的百分率都是相同的。 首先,詳細說明本發明的第1種態樣之冷加工模具用 鋼。 # 本發明人等,爲了想要提供:冷加工模具用鋼所被要 求的各種特性之中,特別是提高了硬度、熱處理後的尺寸 變形抑制性、焊接修補性等的特性之冷加工模具用鋼,首 先針對於採用了習知的JIS SKD 1 1、matrix-hsis (低合金 高速工具鋼)的模具,該模具的表面皮膜受損傷而發生「 咬住現象」的原因加以探索。 第2圖(a)係採用Jis SKD1 1作爲模具用鋼,在其 上面施作了 TiN的皮膜後的模具表面發生了「咬住現象」 的狀態所示的光學顯微鏡照片;第2圖(b )及第2圖(c -14- 200831682 )係其中一部分放大後的光學顯微鏡照片。爲了提供 起見’第2圖(d )係施作TiN的皮膜之前的模具母 光學顯微鏡照片。在第2圖(d)中,看起來白白的 是Cr系碳化物。從第2圖(b )及第2圖(c )可以 ,在皮膜已經剥離後的區域中,硬質的粗大Cr系碳 (主要是含有Cr、Fe之約1〜50 // m程度的碳化物) 面析出’可得知是以該碳化物作爲起點而發生龜裂的 由上述的觀察結果,本發明人等想出:因爲發生 (咬住現象)的起點是上述的粗大Cr系碳化物,只 可能地抑制該碳化物的生成(不要讓它生成)的話, 以防止表面皮膜的剥離,而能夠改善模具的壽命。 基於上述的創見,本發明人等更進一步地不斷加 討。其結果係查明了:若想要抑制粗大碳化物的生成 謀求改善前述的特性的話,不只要適切地控制C量, 要積極地添加各種合金成分,適切地控制合金的成分 的做法是極爲重要的。詳細地說,係找出:想要獲得 待的特性,並不是像傳統做法那樣地藉由控制碳化物 求硬度的增加,而是積極地添加合金成分(尤其是 Cu、Ni、Mo、W ),藉由合金元素的析出硬化來謀求 硬度的做法比較有效,主要是利用Al-Ni系金屬間化 的析出硬化、Mo或W與C形成的碳化物所導致的二 化的話即可的這種創見,再不斷進行實驗後的結果, 完成了本發明的構成要件。 在本說明書中,所稱的「硬度很高」係指:以後 参考 材的 部分 看出 化物 在表 〇 龜裂 要儘 就可 以檢 ,以 並且 設計 所期 來謀 A1、 增加 合物 次硬 終於 述的 -15- 200831682 實施例中所述的方法來測定最大硬度時,最大硬度爲 65 0HV以上的硬度之意。 本發明之第1態樣中,「熱處理後的尺寸變形(尺寸 變化率)」係指:分別測定時效處理前後的厚度、寬度、 長度的3個方向時,根據它們的平均値、及最大値與最小 値的差値這兩方面來進行評估。爲了便於説明起見,將前 者稱爲「尺寸變形率的平均値」,將後者稱爲「尺寸變形 率的差値」。是以,本發明的第1態樣中,利用「尺寸變 形率的平均値」及「尺寸變形率的差値」的這兩者來進行 評估熱處理後的尺寸變形的這一種做法,係與只測定前者 (尺寸變形率的平均値)之專利文獻2的技術不同。根據 本發明人等的實驗結果可知,如果想要充分地抑制熱處理 後的尺寸變形,如果採用專利文獻2的這種方式只是將尺 寸變形率的平均値變小而已的做法是不夠的,將厚度、寬 度、長度的所有方向上的尺寸變形(差異程度)都予以縮 小的做法乃是不可或缺的,例如:根據本發明人等的實驗 結果可以得知:即使是抑制了尺寸變形率的平均値,但是 有時候尺寸變形率的差値卻是變大(也有相反的情況)( 請參考後述的實施例)。再者,在本發明的第1態樣中, 所謂「熱處理後的尺寸變形很小(具有優異的尺寸變形抑 制性)」係指:依據後述的實施例的欄中所述的方法來測 定熱處理前後的尺寸變化時,尺寸變形率的平均値是 ±0.05%的範圍内,而且尺寸變形率的差値是0·08%以下者 -16- 200831682 又,在本說明書中,「焊接修補性」係以HAZ軟化 幅度來進行評比。所謂「具有優異的焊接修補性」係指: 以後述的實施例的攔中所述的方法來測定HAZ軟化幅度 時,位在6.5mm以下的範圍内者。 本發明的第1態樣的鋼中成分係如以下所詳述’不僅 是將對於析出硬化具有幫助的各種合金元素的含有量控制 在預定範圍,而且是如下列數式(1)〜(3)所不般地’ φ 也將與預定的元素之間的平衡加以適切地控制,藉此來謀 求改善上述特性。如後述的實施例所示,如果無法符合這 些要件的其中一個要件的話,就無法確保所期待的特性。 尤其是,本發明中,將Cu和Ni和A1的三者全部都添加 的做法是不可欠缺的,例如:前述專利文獻1、專利文獻 3的那種不含這三者其中一種元素的成分的鋼,則無法獲 得所期待的效果,這種事實已經由實驗加以確認出來(請 參考後述的實施例)。 • 此處,若將本發明的第1態樣的鋼中成分依據:本發 明的第1態樣中的主要改善目標的「焊接修補性」(以 ΗAZ軟化幅度來加以評比)與「熱處理後的尺寸變形抑制 性」(以長度方向的尺寸變形率與尺寸變形率的差値之兩 者來加以評比)之關係來加以整理的話,大致上係如以下 所示者。 首先,如果想要提昇焊接修補性(讓ΗΑΖ軟化幅度 變小)的話’主要將〔Cr〕X〔 C〕的上限、Ms點(下限 )、C量(下限)、A1量(下限)、Ni量(下限)、〔 -17- 200831682Cr * 3.00 ~ 9.00%, A1 : 〇 · 3 ~ 2.0%, C u : 1 · 0 0 〜 5 %, • Ni : 1 · 〇〇, ~5%, Μ 〇: 〇· 5~3 % and / Or W: 2% or less (including 〇%), S ·· 〇. 1 〇% or less (excluding 〇%), the following formula (1) to (3) {[] represents the content of each element (%) Meaning) Equation (1) [Cr]X[C]€ 3.00, Equation (2) [Cu]/[Ni]: 0.5~2'2, Equation (3) [Μ〇]+ 〇· 5χ[W]: 〇·5 to 3.0% φ of the required parts, the rest is iron and steel for cold working molds with unavoidable impurities. 2. The steel for cold working die according to the above 1, which contains V: 0.5% or less (excluding 〇%). 3. Further containing at least one element selected from the group consisting of 1^, 2^, 1^, 丁3, and >^, which is 0.5% or less (excluding 0%) of the above 1 or 2 Steel for cold working die. 4. The steel for cold working die according to any one of the above 1 to 3, which has a Co: 10% or less (excluding 0%). -11 - 200831682 5. The transition point of Mastite iron (Ms point) expressed by the following formula: Ms point = 550-361x [C] -39χ[ Μη]-35χ[ V]-2〇Χ[ Cr -7x[Ni]-10x[Cu]-5χ([Mo]+[W]) + 1 5x[ Co]+ 30x[ A1] {] in the formula represents the content (%) of each element The steel for cold working die according to any one of the above 1 to 4, which is 170 ° C or higher. 6. A mold obtained by using the steel for cold working die according to any one of the above 1 to 5. A method for producing a steel for cold working mold, which is directed to a steel according to the composition described in the above 1, further comprising: preparing a quantity corresponding to the following formula (4): wherein the [] represents the content of each element ( %) (5) [Cu]/[C]: a steel step of the requirements of 4.0 to 15; and a process of performing melt treatment and aging treatment under the conditions of the following formula (5) , ΤΑ-1 0 ^ T2 ^ TA + 1 〇...(5 ) In the formula (5), TA = 0.29xTl-2.63x [ Cu ] /[ C]+ 225, τ 1 is the melting temperature (°C ), T2 system aging temperature (°C). 8. The steel system contains the production method described in the above 7 of V: 0.5% or less (excluding 〇%). -12· 200831682 9. The steel system contains at least one element selected from the group consisting of Ti, Zr, Hf, Ta, and Nb, which is 〇·5 % or less (excluding 0%) of the above 7 or The manufacturing method described in 8. 10. The steel system according to any one of the above 7 to 9 wherein Co: 10% or less (excluding 〇%) is contained. 11. The transition point of the methadrite iron (MS point) expressed by the following formula φ Ms point = 550-361x [C] -39x [Mn] -35x [V] -20x [Cr] -17x [Ni] -10x [Cu]-5x ( [Mo] + [ W )) + 1 5x [ Co ] + 30x [ A1 ] The production method according to any one of the above 7 to 10 of 170 ° C or higher is the above-mentioned A mold obtained by the production method according to any one of 7 to 11. [Effect of the Invention] The steel for cold working die of the present invention has a high hardness and excellent dimensional deformation inhibition after heat treatment, and has excellent weld repairability, as described above. Therefore, the mold obtained by using the above-described steel for cold working die is particularly suitable for a molding die for a high tensile steel sheet having a tensile strength of about 5 90 MPa or more, which can further improve the life life, especially after welding repair. Further, in the production method of the present invention, the conditions in the steel and the conditions for the timely treatment of the melt treatment-13-200831682 are appropriately controlled, so that it can be efficiently produced: high hardness, excellent heat treatment Steel for cold working die with dimensional deformation inhibition. Therefore, the mold obtained by using the production method of the present invention is particularly suitable for a molding die for a high-tensile steel sheet having a tensile strength of about 590 Å or more, which can further improve the life, especially after welding repair. life. [Embodiment] [Best Mode for Carrying Out the Invention] Hereinafter, the present invention will be described in detail. Further, the percentages in the present specification are based on mass unless otherwise specified. In addition, all percentages defined by mass are the same as all percentages defined by weight. First, the steel for cold working die according to the first aspect of the present invention will be described in detail. In order to provide the steel for cold working die which has characteristics such as hardness, dimensional deformation inhibition after heat treatment, and weld repairability, the inventors of the present invention are required to provide the steel for cold working die. First, the use of a conventional JIS SKD 1 1 and matrix-hsis (low alloy high speed tool steel) mold was used to investigate the cause of the "biting phenomenon" caused by damage to the surface film of the mold. Fig. 2(a) is an optical micrograph showing the state in which the surface of the mold after the film of TiN is applied to the mold steel using Jis SKD1 1 as a mold steel; Fig. 2 (b) And Fig. 2 (c - 14 - 200831682) is a part of the enlarged optical microscope photograph. For the sake of providing, 'Fig. 2(d) is an optical micrograph of the mold before applying the film of TiN. In Fig. 2(d), what appears to be white is Cr-based carbide. From Fig. 2(b) and Fig. 2(c), in the region where the film has been peeled off, hard coarse Cr-based carbon (mainly a carbide containing about 1 to 50 // m of Cr and Fe) In the above-mentioned observation, the inventors of the present invention have thought that the origin of the (biting phenomenon) is the above-mentioned coarse Cr-based carbide. It is only possible to suppress the formation of the carbide (do not let it be formed), thereby preventing the peeling of the surface film and improving the life of the mold. Based on the above-mentioned novelty, the present inventors have further continually added. As a result, it has been found that if it is desired to suppress the formation of coarse carbides and to improve the above-described characteristics, it is extremely important to appropriately control the amount of C, and to actively add various alloy components and appropriately control the composition of the alloy. of. In detail, it is found that in order to obtain the characteristics to be treated, it is not the conventional method of controlling the increase in hardness of the carbide, but actively adding the alloy composition (especially Cu, Ni, Mo, W). It is effective to obtain hardness by precipitation hardening of alloying elements, and it is mainly possible to use the precipitation hardening of Al-Ni-based intermetallicization, and the carbonization by Mo or W and C. Transcend, and continued to carry out the results of the experiment, completed the components of the present invention. In this specification, the term "high hardness" means that after the reference material is found, the material can be inspected after the crack is formed, and the design is expected to be A1. -15-200831682 The method described in the examples is intended to measure the maximum hardness, and the maximum hardness is 65 0 HV or more. In the first aspect of the present invention, the "size deformation (dimension change rate) after heat treatment" means that when the thickness, the width, and the length of the aging treatment are measured in three directions, the average enthalpy and the maximum enthalpy are measured. Evaluate with the smallest difference between the two. For the sake of explanation, the former is referred to as "average 尺寸 of the dimensional deformation rate", and the latter is referred to as "the difference of the dimensional deformation rate". In the first aspect of the present invention, the "size 变形 of the dimensional deformation rate" and the "difference of the dimensional deformation rate" are used to evaluate the dimensional deformation after the heat treatment. The technique of Patent Document 2 in which the former (average 尺寸 of the dimensional deformation ratio) is measured is different. According to the results of experiments by the inventors of the present invention, if it is desired to sufficiently suppress the dimensional deformation after the heat treatment, it is not sufficient to reduce the average enthalpy of the dimensional deformation ratio by the method of Patent Document 2, and the thickness is not sufficient. It is indispensable to reduce the dimensional deformation (degree of difference) in all directions of the width and the length. For example, according to the experimental results of the present inventors, it is known that even the average deformation rate is suppressed.値, but sometimes the difference in the dimensional deformation rate is large (there is also the opposite case) (please refer to the example described later). In the first aspect of the present invention, the "size deformation after heat treatment is small (having excellent dimensional deformation inhibition property)" means that the heat treatment is measured according to the method described in the column of the examples to be described later. When the size changes before and after, the average 値 of the dimensional deformation rate is within the range of ±0.05%, and the difference in the dimensional deformation ratio 0 is 0.08% or less -16-200831682 In addition, in the present specification, "welding repairability" The HAZ softening amplitude is used for comparison. The term "excellent weld repairability" means a method in which the HAZ softening width is measured within the range of 6.5 mm or less when the method described in the following examples is used. The composition of the steel according to the first aspect of the present invention is not limited to the content of various alloying elements which contribute to precipitation hardening in a predetermined range, and is the following formula (1) to (3). The φ is also appropriately controlled by the balance between the predetermined elements and the like, thereby improving the above characteristics. As shown in the later-described embodiment, if one of the requirements of these requirements is not met, the desired characteristics cannot be ensured. In particular, in the present invention, it is indispensable to add all of Cu, Ni, and A1, for example, the components of the above-mentioned Patent Document 1 and Patent Document 3 which do not contain one of the three elements. Steel, the fact that the desired effect cannot be obtained, has been confirmed by experiments (please refer to the examples described later). In the steel according to the first aspect of the present invention, the "welding repairability" (measured by the ΗAZ softening range) and the "after heat treatment" are based on the main improvement target of the first aspect of the present invention. The relationship between the dimensional deformation inhibition property (the difference between the dimensional deformation rate in the longitudinal direction and the dimensional deformation ratio) is roughly as follows. First, if you want to improve the weld repairability (so that the softening width of the crucible is small), the upper limit of the [Cr]X[C], the Ms point (lower limit), the C amount (lower limit), the A1 amount (lower limit), and Ni. Quantity (lower limit), [ -17- 200831682

Cu〕/〔Ni〕(上限、下限)、〔Mo〕+0.5x〔W〕 限)、V量(上限)予以適切地控制的做法是很重要 亦即,作爲可使HAZ軟化幅度變小的設計指針,並 利用麻田散鐵的生成所導致的硬化,而是除了將C量 在約0.2〜0.6 0 %程度的低C化之外,利用添加合金成 主要是 Al、Cu、Ni、Mo、W )所導致的析出硬化( :ε -Cu、Ni-Al系金屬間化合物、Ni-Mo系金屬間化 )。這些析出物會在基質中細微地整合析出,因此硬 明顯地增加。 尤其是Cu、Ni、A1是重要的析出硬化元素,是 抑制HAZ軟化有很大的幫助的元素。經由實驗結果 確認出:實質上未添加這些元素的其中一種元素的鋼 無法或得所期待的HAZ軟化抑制作用。 此外,以得知〔Cu〕/〔 Ni〕的比(〔Cu )對〔 的比)係與抑制HAZ軟化具有密切的關係,藉由適 控制上述的比率,可抑制HAZ軟化。第6圖係顯示 後述的實施例所述的方法來測定HAZ軟化幅度時之 〔Cu〕/〔 Ni〕的比對於HAZ軟化幅度之影響的圖表 個圖表係將後述的表3的No.7、8、10、表4的No 35、及37的結果標示出來的圖表。如第6圖所示, 得知〔Cu〕/〔 Ni〕的比係與HAZ軟化幅度具有密切 係,藉由將上述的比控制在0.5〜2.2的範圍内,就可 HAZ軟化幅度抑制在本發明所制定的範圍内(6.5mm (下 的。 不是 抑制 分( 例如 合物 度會 對於 已經 ,並 Ni ) 切地 出以 。這 • 3 1〜 可以 的關 以將 以下 -18- 200831682 另外,如果想要將熱處理後的尺寸變形儘量地變小, 主要是適切地控制Cr與C的含有量的乘積(〔Cr〕x〔C 〕的上限)、C量(上限)、Si量(上限)、Μη量(上 限)、Ms點(下限)、A1量(上限)、Ni量(上限)、 Cr量(上限)、〔Mo〕+ 0.5x〔 W〕(上限)的做法是很 重要。在本發明中,係以低C作爲基本,因此Ms點變高 ’原本殘留沃斯田鐵量的生成就很少了,而且又適切地控 制Cu、Ni、A1等的合金成分的含有量,所以可明顯地抑 制特別是在約400〜5 5 0 °C的時效處理後的膨脹、表面硬化 處理後的收縮。這是被認爲:藉由上述合金成分的添加, 例如:在約400〜500 °C的低溫域中,主要是生成ε-Cu, 在約45〇〜53〇°C的中間溫度域中,主要是生成Ni- ( A1, Mo )系金屬間化合物,在約5 00〜55 0 °C的高溫域中,主 要是生成Mo-V系碳化物,而這些析出物的結晶構造( FCC構造)係與基質(BCC構造)不同,因此體積會收縮 ,這種現象對於抑制熱處理後的尺寸變形具有幫助。又, 本發明的成分係設計成:極力地不要析出粗大的Cr系碳 化物,因此,被認爲:結晶構造無論是對於哪一個方向都 是等方的,即使是在大型複雜形狀的模具製造時,也可以 有效地抑制熱處理後的尺寸變形。 以下將說明本發明的第1態樣的鋼中成分。 C : 0.20- 0.60% C係可確保硬度及耐磨損性,對於抑制HAZ軟化幅度 -19- 200831682 也有幫助的元素。又,如果是利用CVD法在模具母材表 面生成VC、TiC之類的碳化物皮膜的情況下,C濃度太低 的話,將會衍生皮膜的厚度變薄之類的問題。考慮到這種 問題,而且又要使上述作用有效地發揮,乃將C量的下限 選定爲0.20%。C量以0.22%以上爲宜。惟,添加過量的 話,殘留沃斯田鐵將會增加,如果不執行高溫的時效處理 的話,將無法獲得所期待的硬度,而且時效處理後將會膨 脹,使得尺寸變形變大,因此乃將上限選定爲0.60%。C 量是0.50%以下爲宜,0.45%以下更好。 S i : 0.5 〜2.0 0 %Cu]/[Ni] (upper limit, lower limit), [Mo]+0.5x [W] limit), and the amount of V (upper limit) are appropriately controlled, that is, as the HAZ softening amplitude is made small Designing the pointer and using the hardening caused by the formation of the granulated iron, but in addition to the low C of the C amount of about 0.2 to 0.6 0%, the addition of the alloy is mainly Al, Cu, Ni, Mo, Precipitation hardening due to W): ε-Cu, Ni-Al intermetallic compound, Ni-Mo intermetallicization. These precipitates are finely integrated and precipitated in the matrix, so the hardness is remarkably increased. In particular, Cu, Ni, and A1 are important precipitation hardening elements, and are elements which greatly inhibit the softening of HAZ. From the experimental results, it was confirmed that the steel in which one element of these elements was not substantially added could not achieve the desired HAZ softening inhibition effect. Further, it is known that the ratio of [Cu] / [Ni] (the ratio of [Cu) to [the ratio" is closely related to the suppression of HAZ softening, and by appropriately controlling the above ratio, HAZ softening can be suppressed. Fig. 6 is a graph showing the influence of the ratio of [Cu] / [Ni] on the HAZ softening width when the HAZ softening width is measured by the method described in the examples below, which is No. 7 of Table 3 to be described later. 8, 10, Table 4, No 35, and 37 results are shown in the chart. As shown in Fig. 6, it is known that the ratio of [Cu]/[Ni] is closely related to the HAZ softening range, and by controlling the above ratio within the range of 0.5 to 2.2, the HAZ softening amplitude can be suppressed. Within the scope of the invention (6.5mm (the lower. is not the inhibition points (such as the degree of the compound will already be, and Ni) cut out. This • 3 1 ~ can be closed to the following -18- 200831682 In addition, If it is desired to reduce the dimensional deformation after heat treatment as much as possible, it is mainly appropriate to control the product of the content of Cr and C (the upper limit of [Cr]x[C]), the amount of C (upper limit), and the amount of Si (upper limit). , Μ η amount (upper limit), Ms point (lower limit), A1 amount (upper limit), Ni amount (upper limit), Cr amount (upper limit), [Mo] + 0.5x [W] (upper limit) are important. In the present invention, the low C is essential, and therefore the Ms point becomes high. The generation of the original residual Worth iron amount is small, and the content of the alloy composition such as Cu, Ni, and A1 is appropriately controlled, so that it is obvious Suppression, especially after aging treatment at about 400~5 50 °C, table Shrinkage after surface hardening treatment. This is considered to be: by the addition of the above alloy composition, for example, in the low temperature range of about 400 to 500 ° C, mainly ε-Cu is formed, at about 45 〇 to 53 〇 ° In the intermediate temperature range of C, mainly Ni-(A1, Mo)-based intermetallic compounds are formed, and in the high temperature region of about 50,000 to 55 ° C, mainly Mo-V-based carbides are formed, and these precipitates are formed. The crystal structure (FCC structure) is different from the matrix (BCC structure), so the volume shrinks, which is helpful for suppressing dimensional deformation after heat treatment. Moreover, the composition of the present invention is designed to: do not precipitate coarsely Since the Cr-based carbide is considered to have a crystal structure in which direction is uniform, it is possible to effectively suppress dimensional deformation after heat treatment even in the production of a mold having a large-complex shape. The steel component of the first aspect of the present invention C: 0.20 - 0.60% C is an element which can ensure hardness and wear resistance, and is also useful for suppressing HAZ softening range -19-200831682. Further, if it is by CVD method In the mold When a carbide film such as VC or TiC is formed on the surface of the material, if the C concentration is too low, the thickness of the film is reduced. In view of such a problem, the above effects are effectively exerted. The lower limit of the amount of C is selected to be 0.20%. The amount of C is preferably 0.22% or more. However, if the addition is excessive, the residual Worthite iron will increase, and if the high temperature aging treatment is not performed, the expected result will not be obtained. The hardness is increased after the aging treatment, so that the dimensional deformation becomes large, so the upper limit is selected to be 0.60%. The amount of C is preferably 0.50% or less, more preferably 0.45% or less. S i : 0.5 ~2.0 0 %

Si是製鋼時有用的脫氧元素,對於硬度的提昇與確保 被切削性確保有幫助的元素。又,Si對於抑制基質的麻田 散鐵的回火軟化,抑制HAZ軟化幅度也是有用的。爲了 使其發會這種作用,將Si量的下限選定爲0.5%。惟,添 加過量的話,偏析將會變大,不僅是熱處理後的尺寸變形 變大,韌性也會降低,因此將上限選定爲2.00%。Si量的 下限是1%爲宜,1.2%更好,另外,Si量的上限是1.85% 爲宜。 Μ η : 〇 · 1 〜2 % Μη是用來確保淬火性有用的元素,但是,添加過量 的話,M s點會明顯地降低,殘留沃斯田鐵會增加,因此 如果不執行高溫的時效處理的話,就無法獲得所期待的硬 -20- 200831682 度。考慮到這些原因,乃將Μη的含有量選定在 。Μη量的下限是0.1 5 %爲宜,另外,Μη量的I 爲宜,0.5%更好,0.35%尤佳。Si is a deoxidizing element that is useful in steel making, and is an element that contributes to the improvement of hardness and ensuring machinability. Further, Si is also useful for suppressing the temper softening of the matrix of the loose iron of the matrix and suppressing the softening amplitude of the HAZ. In order to make this effect, the lower limit of the amount of Si was selected to be 0.5%. However, if an excessive amount is added, the segregation will become large, and not only the dimensional deformation after heat treatment becomes large, but also the toughness is lowered, so the upper limit is selected to be 2.00%. The lower limit of the amount of Si is preferably 1%, more preferably 1.2%, and the upper limit of the amount of Si is preferably 1.85%. Μ η : 〇· 1 ~2 % Μη is an element useful for ensuring hardenability. However, if the addition is excessive, the M s point will be significantly lowered, and the residual Worth iron will increase, so if high temperature aging treatment is not performed If you do not, you will not get the expected hard -20- 200831682 degrees. For these reasons, the content of Μη is selected. The lower limit of the amount of Μη is preferably 0.15%, and the I of the amount of Μη is preferably 0.5%, more preferably 0.35%.

Cr : 3.0 0 ~ 9.00%Cr : 3.0 0 ~ 9.00%

Cr是用來確保預定的硬度有用的元素。Cr 3.0 0%的話,淬火性不足,局部生成變韌鐵’因 降低,無法確保耐磨損性。Cr量是3.5%以上爲 以上更好。惟,添加過量的話,粗大的Cr系碳 大量生成,熱處理後會收縮,皮膜的耐久性會降 將上限選定爲9.00%。Cr量是以7.0%以下爲宜 下更好,6.0%以下尤佳。 A1 : 0 · 3 〜2.0 % A1是想要謀求利用Ni3Al之類的Al-Ni系金 物的析出強化所導致的提昇硬度所必須的元素’ HAZ軟化幅度也有幫助。又,A1也可以作爲脫 慮到這些因素,乃將A1的下限選定爲0 · 3 %。惟 量的話,偏析將會變大,不僅熱處理後的尺寸變 是尺寸變形率的差値)將會變大,也會導致韌性 此將其上限選定爲2.0%。A1量是0.50%以上1· 宜,0.7%以上1.6%以下更好。Cr is an element useful for ensuring a predetermined hardness. When Cr 3.0 is 0%, the hardenability is insufficient, and the localized toughened iron is lowered, and the wear resistance cannot be ensured. It is more preferable that the amount of Cr is 3.5% or more. However, when excessively added, coarse Cr-based carbon is formed in a large amount, and shrinks after heat treatment, and the durability of the film is lowered to the upper limit of 9.00%. The amount of Cr is preferably 7.0% or less, more preferably 6.0% or less. A1 : 0 · 3 〜 2.0 % A1 is an element necessary for improving the hardness due to precipitation strengthening of Al-Ni-based gold such as Ni3Al. The HAZ softening range is also helpful. Further, A1 can also take these factors as a concern, and the lower limit of A1 is selected to be 0 · 3 %. In the case of the amount, the segregation will become larger, and not only the dimensional change after the heat treatment is the difference in the dimensional deformation rate, but also the toughness, which will result in the upper limit of 2.0%. The amount of A1 is preferably 0.50% or more, more preferably 0.7% or more and 1.6% or less.

Cu : 1.0 0 〜5 % 上述範圍 限是1 % 量若未滿 此硬度會 宜,4.0% 化物將會 低,因此 ,6.5%以 屬間化合 對於抑制 氧劑。考 ,添加過 化(尤其 降低,因 8 %以下爲 -21 - 200831682Cu : 1.0 0 〜5 % The above range is 1%. If the amount is less than the hardness, the hardness will be 4.0%, so 6.5% will be combined with the oxidant. Test, added over (especially reduced, because 8 % or less is -21 - 200831682

Cu是想要謀求利用ε _Cu的析出強化所導致的提昇硬 度所必須的元素,對於抑制HAZ軟化幅度也有幫助。惟 ’添加過量的話,容易發生鍛造龜裂,因此將上限選定爲 5%。Cu量是2.0%以上4.0%以下爲宜。 N i : 1 · 0 0 〜5 %Cu is an element necessary for improving the hardness due to precipitation strengthening of ε_Cu, and is also useful for suppressing the HAZ softening range. However, if the addition is excessive, the forging crack is likely to occur, so the upper limit is selected to be 5%. The amount of Cu is preferably 2.0% or more and 4.0% or less. N i : 1 · 0 0 ~5 %

Ni是想要謀求利用Ni3Al之類的Al-Ni系金屬間化合 物的析出強化所導致的提昇硬度所必須的元素,對於抑制 ΗAZ軟化幅度也有幫助。又,Ni可藉由與Cu —起倂用, 而可抑制因Cu的添加過量所導致的熱間脆性,亦可防止 鍛造時的龜裂。惟,添加過量的話,殘留沃斯田鐵將會增 加,如果不以高溫執行時效處理的話,不僅將無法確保預 定的硬度,熱處理後將會膨脹。Ni量是以1.5 %以上4.0% 以下爲宜。Ni is an element necessary for improving the hardness by precipitation strengthening of an Al-Ni-based intermetallic compound such as Ni3Al, and is also useful for suppressing the softening range of ΗAZ. Further, Ni can be used together with Cu to suppress thermal brittleness due to excessive addition of Cu, and to prevent cracking during forging. However, if the addition is excessive, the residual Worthite iron will increase. If the aging treatment is not performed at a high temperature, not only the predetermined hardness will be ensured, but also the heat will be expanded. The amount of Ni is preferably 1.5% or more and 4.0% or less.

Mo : 0.5〜3%及/或W : 2%以下(含〇% )Mo : 0.5 to 3% and/or W: 2% or less (including 〇%)

Mo及W均爲除了可形成M6C型碳化物之外,亦可形 成Ni3Mo系金屬間化合物,是對於析出強化具有幫助的元 素。惟,Mo、W添加過量的話,上述的碳化物等等將會 過量生成,除了導致韌性降低之外,熱處理後的尺寸變形 (尤其是尺寸變形率的差値)會變大,因此乃設定在上述 範圍。本發明中,Mo是必要成分,W是可選擇性添加的 元素,但是,亦可同時倂用這兩種元素。Mo是0.5 %以上 3%以下爲宜,0.7%以上2.5%以下更好。又,W是2%以下 -22- 200831682 爲宜,1 ·5%以下更好。 S : 0.10%以下(不含〇% )Both Mo and W can form a Ni3Mo-based intermetallic compound in addition to the M6C-type carbide, and are elements which contribute to precipitation strengthening. However, if Mo and W are excessively added, the above-mentioned carbides and the like are excessively formed, and in addition to the decrease in toughness, the dimensional deformation after heat treatment (especially the difference in dimensional deformation ratio) becomes large, and thus is set in The above range. In the present invention, Mo is an essential component, and W is an element which can be selectively added, but these two elements can also be used at the same time. Mo is preferably 0.5% or more and 3% or less, more preferably 0.7% or more and 2.5% or less. Further, W is 2% or less -22- 200831682 is preferable, and 1 % or less is more preferable. S : 0.10% or less (excluding 〇%)

s是用以確保被切削性有用的元素,但是添加過量的 話’將會產生焊接龜裂,因此將其上限選定爲0 . i 0 %。S 量是0.07%以下爲宜,〇·05%以下更好,〇.〇25%以下尤佳 〇 此外,本發明的第1態樣必須符合下列數式(1 )〜 (3)的衣:件{ 〔 }是表不各兀素的含有量(%)之意}。 數式(1 ) 〔 Cr〕X〔 C〕€ 3.00 上述數式(1 )是基於抑制粗大的Cr系碳化物的生成 之目的而被設定的,〔Cr〕與〔C〕的乘積若超過3.00的 話’熱處理後的尺寸變形會變大,表面皮膜的耐久性會降 低。〔Cr〕與〔C〕的乘積是ΐ·8〇以下爲宜,17〇以下更 好。此外’其下限,基於抑制熱處理後的尺寸變形抑制之 類的觀點’雖然是較小爲佳,但是考慮到想要有效地發揮 因爲添加Cr、C所導致的上述作用的話,大槪是以0.8爲 宜。 數式(2) 〔 Cu〕/〔 Ni〕: 0·5 〜2·2 上述數式(2 )主要是被設定作爲:利用ε -Cu的析出 強化來抑制ΗAZ軟化幅度的參數(請參考後述的實施例 )。爲使其有效地發揮這種作用,將〔Cu〕對〔Ni〕的比 -23- 200831682 選定爲0.5。惟,上述的比變大的話,將會發生鍛造龜裂 ,因此將其上限選定爲2.2。上述的比是0.7以上1.5以下 爲宜,0.85以上1.2以下更好。 數式(3) [ Mo ] + 0.5x [ W ] : 0.5 〜3·0% 構成上述數式(3 )的Mo、W係如前所述,是對於析 出強化有幫助的元素,上述數式(3 )主要是被設定作爲 :用來確保因這些元素的析出強化所導致的硬度提昇的參 數,對於抑制HAZ軟化幅度也是有效。在上述數式(3 ) 中,〔W〕的係數(0.5 )是考慮到Mo的原子量是W的約 1 /2之因素而選定的。爲了要有效地使其發揮這些作用, 將上述數式(3 )的下限選定爲0 · 5 %。惟,Μ 〇、W的量添 加過量的話,上述碳化物就會過量添加,除了導致朝性降 低之外,熱處理後的尺寸變形(尤其是尺寸變形率的差値 )將會變大,所以將上述數式(3 )的上限選定爲3.0 %。 上述數式(3 )的下限是1.0 %爲宜,1 · 2 %更好,另外,其 上限是2.8%爲宜。 本發明的第1態樣的鋼中成分係如上所述,其餘部分 是鐵以及不可避免的雜質。至於不可避雜質,例如:可以 舉出在製造過程中不可避免地混入的元素等等,例如:ρ 、Ν、Ο之類的元素。Ρ量大槪是0.05 %以下爲宜,〇.〇3 % 以下更好。Ν量大槪是3 5 0ppm以下爲宜,200ppm以下更 好,150ppm以下尤佳。〇量大槪是5〇ρριη以下爲宜, 3 0 p p m以下更好,2 0 p p m以下尤佳。 此外,本發明亦可基於改善其他的特性之目的,添加 -24 - 200831682 入以下的成分。 V : 0.5%以下(不含0% ) V是可形成VC之類的碳化物而對於提昇硬度有幫助 ,是抑制HAZ軟化幅度有效的元素。又,在母材表面實 施:氣體氮化、鹽浴氮化、電漿氮化之類的氮化處理以形 成擴散硬化層的時候,是提昇表面硬度、提昇硬化層深度 有效的元素。若想要有效地使其發揮這種作用,V量大槪 是添加0.05%以上爲宜。惟,添加過量的話,固熔C量會 降低,會導致母相也就是麻田散鐵組織的硬度降低,因此 其上限選定在0.5%爲宜。V量在0.4%以下更好,0.30%以 下尤佳。 由Ti、Zr、Hf、Ta、及Nb所組成的群所選出的至少 一種元素合計0.5 %以下(不含0% ),這些元素皆爲氮化 物形成元素,是對於因該氮化物及A1N的微細分散化及結 晶粒微細化所導致的韌性提昇有幫助的元素。若想要有效 地使其發揮這種作用,大槪是要添加Ti爲0.01 %以上,Zr 爲0.02%以上,Hf爲 0.04%以上,Ta爲 0.04%以上,Nb 爲0.02%以上爲宜。惟,添加過量的話,固熔C量會降低 而導致麻田散鐵的硬度降低,因此上述元素的合計量選定 在0.5%爲宜。上述元素合計量是0.4%以下更好,0·30%以 下尤佳。此外,上述的元素可以單獨地添加,也可以合倂 添加2種以上。 -25- 200831682 C ο : 1 0 %以下(不含〇 % )s is an element useful for ensuring machinability, but if it is excessively added, a weld crack will occur, so the upper limit is selected to be 0. i 0 %. The amount of S is preferably 0.07% or less, more preferably 〇·5% or less, and more preferably 25% or less. Further, the first aspect of the present invention must conform to the following formulas (1) to (3): The piece { 〔 } is the meaning of the content (%) of each element. Formula (1) [Cr]X[C]€ 3.00 The above formula (1) is set for the purpose of suppressing the formation of coarse Cr-based carbides, and the product of [Cr] and [C] exceeds 3.00. In the case of 'the dimensional deformation after heat treatment, the durability of the surface film is lowered. The product of [Cr] and [C] is preferably ΐ·8〇 or less, and 17〇 or less is more preferable. Further, 'the lower limit is based on the viewpoint of suppressing the suppression of the dimensional deformation after the heat treatment,' although it is preferably small, but considering that it is intended to effectively exert the above-described effects due to the addition of Cr and C, the 槪 is 0.8. It is appropriate. Formula (2) [Cu]/[Ni]: 0·5 ~2·2 The above formula (2) is mainly set as a parameter for suppressing the softening width of ΗAZ by precipitation strengthening of ε-Cu (please refer to the following) Example). In order to effectively exert this effect, the ratio of [Cu] to [Ni] was selected to be 0.5 to 200831682. However, if the above ratio becomes larger, forging cracks will occur, so the upper limit is selected to be 2.2. The above ratio is preferably 0.7 or more and 1.5 or less, more preferably 0.85 or more and 1.2 or less. (3) [ Mo ] + 0.5x [ W ] : 0.5 〜3·0% The Mo and W systems constituting the above formula (3) are elements which are helpful for precipitation strengthening as described above, and the above formula (3) It is mainly set as a parameter for ensuring the hardness increase due to precipitation strengthening of these elements, and is also effective for suppressing the HAZ softening range. In the above formula (3), the coefficient (0.5) of [W] is selected in consideration of a factor that the atomic weight of Mo is about 1 /2 of W. In order to effectively exert these effects, the lower limit of the above formula (3) is selected to be 0.5%. However, if the amount of Μ 〇 and W is excessively added, the above-mentioned carbides are excessively added, and in addition to causing a decrease in the directionality, the dimensional deformation after heat treatment (especially the difference in dimensional deformation rate) will become large, so The upper limit of the above formula (3) is selected to be 3.0%. The lower limit of the above formula (3) is preferably 1.0%, more preferably 1-2%, and the upper limit is preferably 2.8%. The composition of the steel of the first aspect of the present invention is as described above, and the remainder is iron and unavoidable impurities. As for the unavoidable impurities, for example, elements which are inevitably mixed in the manufacturing process, etc., such as elements such as ρ, Ν, Ο, etc., can be cited. The amount of sputum is preferably 0.05% or less, and 〇. 〇 3% is better. The amount of sputum is preferably less than 305 ppm, more preferably less than 200 ppm, and preferably less than 150 ppm. The amount of sputum is preferably 5 〇ρριη, more preferably 3 0 p p m or less, and 2 0 p p m or less. Further, the present invention can also add -24 - 200831682 to the following components for the purpose of improving other characteristics. V: 0.5% or less (excluding 0%) V is a carbide which can form a VC and is useful for improving the hardness and is an effective element for suppressing the HAZ softening range. Further, when the nitriding treatment such as gas nitriding, salt bath nitriding, or plasma nitriding is performed on the surface of the base material to form a diffusion hardened layer, it is an element effective for improving the surface hardness and increasing the depth of the hardened layer. If it is desired to effectively exert such a function, the amount of V is preferably 0.05% or more. However, if the addition is excessive, the amount of solid solution C will decrease, which will result in a decrease in the hardness of the parent phase, which is the structure of the granulated iron structure. Therefore, the upper limit is preferably set at 0.5%. The amount of V is preferably 0.4% or less, and more preferably 0.30% or less. At least one element selected from the group consisting of Ti, Zr, Hf, Ta, and Nb is 0.5% or less (excluding 0%), and these elements are all nitride forming elements for the nitride and A1N. An element that contributes to the improvement of toughness caused by fine dispersion and grain refinement. In order to effectively perform such a function, it is preferable to add Ti to 0.01% or more, Zr to 0.02% or more, Hf to 0.04% or more, Ta to 0.04% or more, and Nb to 0.02% or more. However, if the amount of addition is excessive, the amount of solid solution C is lowered, and the hardness of the granulated iron is lowered. Therefore, the total amount of the above elements is preferably 0.5%. The total amount of the above elements is preferably 0.4% or less, and more preferably 0. 30% or less. Further, the above elements may be added singly or in combination of two or more. -25- 200831682 C ο : 1 0 % or less (excluding 〇 % )

Co是提高Ms點,減少殘留沃斯田鐵之有效的元素, 可利用其來提高硬度。若想要有效地使其發揮這種作用, 大槪是要添加C 〇量1 %以上爲宜。惟,添加過量的話,會 導致成本等的上昇,乃將上限選定在10%爲宜。Co量的 上限在5.5 %更好。 麻田散鐵轉態點(M s點)g 1 7 0 °C Ms點 = 550-361x〔C〕-39x〔Mn〕-35x [ V ] -20x [ Cr ] -17x〔Ni〕-l〇x〔Cu〕-5x(〔Mo〕+ [ W ]) + 1 5 x [ C o ] + 3 0 x [ A1 ] {式中,〔〕是代表各元素的含有量(%)之意} 在本發明中,Ms點主要是當作:硬度、抑制熱處理 後的尺寸變形的指標,如果Ms點未達1 70 °C的話,殘留 沃斯田鐵會增大,如果不執行高溫的時效處理的話,將無 法獲得所期待的硬度,而且會導致熱處理後的膨脹。Ms 點是愈高愈好,大槪是23 0°C以上更好,23 5 °C以上尤佳, 2 5 0 °C以上最好。此外,其上限値,基於上述作用的觀點 ,雖然並沒有特別的限定,但是考慮到構成Ms點之上述 元素的添加所產生的作用效果等等因素的話,大槪是以 350°C爲宜,320°C更好。 又,本發明也包含:使用上述的模具用鋼所製得的模 具。模具的製造方法並無特別的限定,可以舉出例如:將 上述鋼熔製後,進行熱間鍛造之後,實施退火(例如:在 -26- 200831682 約70 0 °C保持7小時之後,以約17°C /hr的平均冷卻速度 在爐中冷卻到約400 °C爲止,然後進行放置冷卻)使其軟 化之後,利用切削加工等等將其粗加工成爲預定的形狀, 然後,以約950〜1150°C的溫度進行熔體化處理—進行約 4 00〜5 3 0°C的時效處理,以獲得所期待的硬度之方法。 接下來,詳細説明本發明的第2態樣之冷加工模具用 鋼的製造方法。 本發明人爲了要提供:就冷加工模具用鋼所被要求的 各種特性當中特別是提高了硬度、熱處理後的尺寸變形抑 制性、焊接修補性(將模具的損傷等利用焊接來修補時的 模具壽命特性)等的特性之冷加工模具用鋼,不斷地加以 檢討。其結果,終於找到了 :只要適切地控制鋼中成分的 話’就可以達成所期待的目的之創見(本發明的第1態樣 )° 本發明的第1態樣之後,接下來,本發明人爲了想要 特別地進一步改善熱處理後的尺寸變形抑制性,乃以先前 的申請案所揭示的鋼中成分作爲基礎,更進一步地不斷檢 討。其結果,找出了:使用本發明的第1態樣所揭示的鋼 ’而且以適切的條件來執行熔體化處理及時效處理的話, 即可有效率地獲得可更進一步抑制熱處理後的尺寸變化的 冷加工模具用鋼。 亦即’本發明的第2態樣所揭示的製造方法的特徵是 在於:界定出可以有效率地製造出本發明的第i態樣之中 的可進一步抑制其熱處理後的尺寸變化的冷加工模具用鋼 -27- 200831682 的較佳的製造條件。詳細地說,係在於:將熔體化溫度及 時效溫度,以對於熱處理後的尺寸變形抑制性最有幫助的 參數(Cu與C的質量比率)來加以界定的這種做法上具 有特徵。根據本發明的第2態樣所揭示的製造方法,即使 不實施例如··專利文獻5所述的「1次以上的兩段階回火 處理」、專利文獻6所述的低溫處理之類的特別的熱處理 ’只要與以往相同地實施一次回火處理(時效處理),即 可獲得較之以往的冷加工模具用鋼更能夠抑制熱處理後的 尺寸變化之冷加工模具用鋼,所以其生產性極優異。 此處,先說明從本發明的第1態樣發展到本發明的第 2態樣的冷加工模具用鋼的製造方法之緣由經過。 本發明人先針對於以往使用 JIS SKD1 1、matrix-hsis (低合金高速工具鋼)的模具中,爲何模具的表面皮膜會 損傷而發生咬住現象的原因加以探索。其結果得知了:在 皮膜剥離後的領域中,係有··含硬質的粗大的Cr系碳化 物(主要含有Cr、Fe之約1〜50 μ m程度的碳化物)在表 面析出,並且是以該碳化物爲起點而發生龜裂。 基於上述的結果,本發明人係認爲:因爲發生咬住現 象的起點係上述的粗大的Cr系碳化物,只要能夠儘量地 抑制該碳化物的生成的話(不使其生成的話)就可以防止 表面皮膜的剥離,而得以改善模具的壽命。 基於上述的創見,本發明人更進一步地加以檢討。其 結果’找出了 ·如果想要抑制粗大的礙化物的生成來謀求 改善前述特性的話,除了要適切地控制C量之外,積極地 -28- 200831682 添加各種合金成分,適切地控制合金成分設計的做法是極 爲重要的。詳細地說,是找到了:想要獲得所期待的特性 ,並不是如以往那樣地只是藉由控制碳化物來謀求硬度的 增加,而是要積極地添加合金成分(尤其是A1 ' Cu、Ni 、Mo、W)來謀求因合金元素的析出硬化所帶來的硬度增 加的做法才是有效的,主要是利用Al-Ni系金屬間化合物 的析出硬化,Mo、W與C形成碳化物時的二次硬化的話 ,就可以達成增加硬度的這種創見。 以上所說明的就是到達本發明的第1態樣的緣由經過 。其後,本發明人爲了想要提供:不必實施特別的熱處理 ,只要和以往同樣地實施一次熔體化處理和時效處理就可 以很容易獲得具有更優異的熱處理後的尺寸變形抑制性之 冷加工模具用鋼之高生產性的製造方法,乃更進一步進行 檢討。其結果,找到了 :使用上述的鋼進行熔體化處理及 時效處理的時候,如後述的實施例所示般地,只要將這兩 者的溫度(熔體化溫度及時效溫度),利用與對於熱處理 後的尺寸變形抑制性最有幫助的「Cu與C的質量比率」 的關係來好好地加以界定的話,就可以達成所期待的目的 之這種創見,進而完成了本發明的第2態樣的製造方法。 具體而言,係得知了:當熔體化溫度(°C )爲T1, 時效處理溫度(°C )爲T2,Cu與C的質量比率爲〔Cu〕/ 〔C〕,以下列數式 0·29χΤ1-2·63χ〔 Cu〕/〔 C〕+ 225 來表示的數値爲ΤΑ時,只要在T2符合下列數式(5 -29- 200831682 TA-10S T2S TA+ 1〇 …數式(5) 的範圍内(亦即,TA± 10 °C )來進行熔體化處理及時 效處理的話,即可獲得:在熱處理後的平均尺寸變形率及 最大尺寸變形率(詳細容後詳述)的兩方面上都符合本發 明的第2態樣所揭示的範圍之具有極優異的尺寸變形抑制 性的鋼(請參考實施例的表7 )。 本說明書中所稱的「熔體化處理」係與淬火處理的意 義相同,「時效處理」係與回火處理的意義相同。 在本說明書中,所謂的「硬度很高」係指:根據後述 的實施例的欄中所述的方法來測定硬度時,硬度爲650ΗV 以上者之意。 在本發明的第2態樣中,「熱處理後的尺寸變形(尺 寸變化率)」係就分別測定時效處理前後的厚度(△ χ ) 、寬度(Ay)、長度(Δζ)的三個方向時,該等的平均 値〔(Δχ+Δγ+Δζ) /3〕、以及上述的 ΔΧ、Ay、Δζ 的最大値(絕對値)的兩方面都進行評比。爲了説明上的 方便起見’將SU者稱爲「尺寸變形率的平均値或平均尺寸 變形率」,將後者稱爲「尺寸變形率的最大値或最大尺寸 變形率」。是以,在本發明的第2態樣中,同時使用「尺 寸變形率的平均値」及「尺寸變形率的最大値」之兩者來 對於熱處理後的尺寸變形進行評比的這一點,係與專利文 獻2所揭示的只測定前者(尺寸變形率的平均値)的習知 技術不相同。根據本發明人的實驗結果可得知:想要充分 -30- 200831682 地抑制熱處理後的尺寸變形的話,如果採用專利文獻2所 揭示的這種只是儘可能地使尺寸變形率的平均値變小的做 法是不夠的,而是要令厚度、寬度、長度的所有方向上的 尺寸變形(差異程度)都變小的做法是不可欠缺的,有時 候會有:即使是抑制了尺寸變形率的平均値,尺寸變形率 的差値還是變大的情況(也會有相反的情況)(請參考後 述的實施例)。此外,在本發明的第2態樣中,所謂的「 φ 熱處理後的尺寸變形很小(具有優異的尺寸變形抑制性) 」係指:根據後述的實施例的欄中所述的方法來測定熱處 理前後的尺寸變化時,尺寸變形率的平均値是±0.03 %的範 圍内而且尺寸變形率的最大値(絕對値)是0.0 5 %以下之 意。 此外,上述本發明的第2態樣中的評比基準(方法及 其水準)在以下的各點係與前述本發明的第1的態樣不同 〇 • 首先,無論是本發明的第1態樣或者本發明的第2態 樣,雖然都是採用「尺寸變形率的平均値」作爲熱處理後 的尺寸變形的評比基準,但是本發明的第1態樣係將合格 基準制定爲±0.05%,而本發明的第2態樣則是較之本發明 的第1態樣更嚴格,係將合格基準制定爲土〇.〇3%。 此外,在本發明的第1態樣中,是採用「尺寸變形率 的差値」,亦即前述的Δχ、Ay、Δζ之中的最大値與最 小値的差値(絕對値),相對地,本發明的第2態樣中, 則是如上所述地採用「尺寸變形率的最大値」。這是因爲 -31 - 200831682 基於所謂「想要提供較之本發明的第1態樣 尺寸變形抑制性的鋼的話,必須將熱處理後 差異程度)最大的部分(最大値)予以儘可 認知,才會除了上述的本發明的第1態樣的 「尺寸變形率的差値」之外,又採用了「尺 大値」。如後述的實施例所示,縱然是符合 1態樣所規定的「尺寸變形率的差値」,但 法符合本發明的第2態樣所規定的「尺寸變 」的條件者(請參考後述的實施例),這種 本發明的第2態樣中的「具有優異的熱處理 抑制性的鋼」。 本發明的第2態樣的鋼中成分係如以下 是將對於析出硬化有幫助的各種合金元素的 預定範圍內,也又如下數式(1)〜(4)所 地控制預定的元素之間的平衡,藉此來謀求 性。如後述的實施例所示,如果無法符合這 一種要件的話,就無法確保所期待的特性。 的第2態樣,添加Cu和Ni和A1的三種元 可欠缺的,例如:經由實驗結果已經確認出 獻1、專利文獻3的那一種不含Cu和Ni矛丨 種元素的成分的鋼,是無法獲得所期待的效 特別是本發明的第2態樣,爲了要盡量 的尺寸變形變小,除了主要採用構成前述& 〔Cu〕與〔C〕的質量比率之外,適切地控奇 具有更優異的 的尺寸變形( 能地變小」之 説明中所述的 寸變形率的最 了本發明的第 是還是會有無 形率的最大値 鋼並無法稱爲 後的尺寸變形 所詳述,不僅 含有量控制在 示地,也適切 改善上述的特 些要件的任何 尤其是本發明 素的做法是不 前述的專利文 []A1的其中一 果的。 地將熱處理後 5數式(5 )的 时Cr與C的 -32-Co is an effective element for increasing the Ms point and reducing the residual Worth Iron, which can be used to increase the hardness. If you want to effectively play this role, it is advisable to add more than 1% of C. However, if the addition is excessive, the cost and the like will increase, and it is preferable to set the upper limit at 10%. The upper limit of the amount of Co is better at 5.5%. Ma Tian loose iron transition point (M s point) g 1 70 °C Ms point = 550-361x [C]-39x [Mn]-35x [ V ] -20x [ Cr ] -17x [Ni]-l〇x [Cu]-5x([Mo]+ [ W ]) + 1 5 x [ C o ] + 3 0 x [ A1 ] {wherein, [] is the meaning of the content (%) of each element} In the invention, the Ms point is mainly used as an index for hardness and suppression of dimensional deformation after heat treatment. If the Ms point is less than 1 70 ° C, the residual Worth iron will increase, if high temperature aging treatment is not performed, The expected hardness will not be obtained and will cause expansion after heat treatment. The higher the Ms point, the better, the greater the 槪 is better than 23 0 °C, the best above 23 5 °C, and the best above 250 °C. In addition, the upper limit 値, based on the above-mentioned action, is not particularly limited, but considering the effect of the addition of the above-mentioned elements constituting the Ms point, etc., it is preferable to use 350 ° C. 320 ° C is better. Further, the present invention also encompasses a mold obtained by using the steel for a mold described above. The method for producing the mold is not particularly limited, and for example, after the steel is melted, it is subjected to hot forging and then annealed (for example, after 770-200831682 is held at about 70 ° C for 7 hours, The average cooling rate of 17 ° C / hr is cooled in the furnace to about 400 ° C, and then placed and cooled to soften it, and then rough-processed into a predetermined shape by cutting or the like, and then, about 950 ° The melt treatment is carried out at a temperature of 1150 ° C - an aging treatment of about 4 to 5 30 ° C is carried out to obtain a desired hardness. Next, a method of producing the steel for cold working die according to the second aspect of the present invention will be described in detail. In order to provide, among the various characteristics required for the steel for cold working molds, the inventors have improved the hardness, the dimensional deformation inhibition after heat treatment, and the weld repairability (the mold life when the mold is damaged by welding, etc.) Steel for cold working molds with characteristics such as characteristics) is continuously reviewed. As a result, it has finally been found that, as long as the components in the steel are appropriately controlled, it is possible to achieve the desired purpose (the first aspect of the present invention). After the first aspect of the present invention, the inventor In order to further particularly improve the dimensional deformation inhibition after heat treatment, it is further reviewed based on the composition of the steel disclosed in the prior application. As a result, it has been found that, by using the steel disclosed in the first aspect of the present invention and performing the melt treatment and the aging treatment under appropriate conditions, it is possible to efficiently obtain the size which can further suppress the heat treatment. Varying cold working die steel. That is, the manufacturing method disclosed in the second aspect of the present invention is characterized in that it is possible to efficiently manufacture a cold working mold which can further suppress the dimensional change after heat treatment among the ith aspect of the present invention. The preferred manufacturing conditions for steel -27-200831682. In detail, it is characterized in that the melt temperature and the aging temperature are defined by a parameter (the mass ratio of Cu to C) which is most helpful for the dimensional deformation inhibition after heat treatment. According to the manufacturing method disclosed in the second aspect of the present invention, the "two-stage two-stage tempering treatment" described in Patent Document 5 and the low-temperature treatment described in Patent Document 6 are not carried out. In the heat treatment of the present invention, the tempering treatment (aging treatment) can be carried out in the same manner as in the related art, and the cold-working mold steel which can suppress the dimensional change after the heat treatment can be obtained. Here, the reason for the development of the method for producing a steel for cold working die according to the first aspect of the present invention to the second aspect of the present invention will be described. The present inventors first explored the reason why the surface film of the mold was damaged and the seizure phenomenon occurred in a mold using JIS SKD1 1 and matrix-hsis (low alloy high speed tool steel). As a result, it has been found that in the field after the peeling of the film, a hard, coarse Cr-based carbide (a carbide mainly containing Cr and Fe of about 1 to 50 μm) is precipitated on the surface, and Cracking occurs with this carbide as a starting point. Based on the results described above, the present inventors have considered that the origin of the biting phenomenon is the above-described coarse Cr-based carbide, and it is possible to prevent the formation of the carbide as much as possible (not to generate it). The peeling of the surface film improves the life of the mold. Based on the above-mentioned novelty, the inventors further reviewed it. As a result, it is found that if it is desired to suppress the formation of coarse inhibitors and to improve the above-mentioned characteristics, in addition to appropriately controlling the amount of C, various alloy components are actively added -28-200831682, and the alloy composition is appropriately controlled. The design approach is extremely important. In detail, it was found that in order to obtain the desired characteristics, it is not the conventional method of controlling the carbide to increase the hardness, but to actively add the alloy component (especially A1 'Cu, Ni). Mo, W) is effective in order to increase the hardness due to precipitation hardening of alloying elements, mainly by precipitation hardening of Al-Ni-based intermetallic compounds, and when carbides are formed by Mo, W and C. In the case of secondary hardening, the idea of increasing the hardness can be achieved. What has been described above is that the reason for reaching the first aspect of the present invention is passed. Then, the inventors of the present invention have been able to easily obtain a cold working die having a more excellent dimensional deformation inhibition after heat treatment, as long as it is not necessary to carry out a special heat treatment, as long as the melt treatment and the aging treatment are carried out in the same manner as in the related art. The high-productivity manufacturing method of steel is further reviewed. As a result, it was found that when the above-described steel is used for the melt treatment and the aging treatment, as shown in the examples described later, the temperature of both of them (melt temperature and time-dependent temperature) is utilized. The relationship between the "mass ratio of Cu to C" which is most helpful for the dimensional deformation inhibition after heat treatment is well defined, and the desired effect can be achieved, and the second aspect of the present invention is completed. Kind of manufacturing method. Specifically, it is known that when the melt temperature (°C) is T1, the aging treatment temperature (°C) is T2, and the mass ratio of Cu to C is [Cu]/[C], in the following formula 0·29χΤ1-2·63χ[ Cu]/[ C]+ 225 When the number 値 is ΤΑ, as long as T2 meets the following formula (5 -29- 200831682 TA-10S T2S TA+ 1〇... In the range of (ie, TA ± 10 °C) for the melt treatment and the aging treatment, the average dimensional deformation rate and the maximum dimensional deformation rate after heat treatment (detailed in detail) can be obtained. Both of them are steels having extremely excellent dimensional deformation inhibition in the range disclosed in the second aspect of the present invention (refer to Table 7 of the examples). The "melting treatment" referred to in the present specification is In the same meaning as the tempering treatment, the term "aging treatment" has the same meaning as the tempering treatment. In the present specification, the term "high hardness" means that the hardness is measured according to the method described in the column of the examples described later. In the second aspect of the present invention, the hardness is 650 ΗV or more. The dimensional deformation (dimensional change rate) is the average 値 [(Δχ + Δγ + Δζ) when the thicknesses (Δ χ ), width (Ay), and length (Δζ) are measured before and after the aging treatment. /3], and the above-mentioned ΔΧ, Ay, Δζ maximum 値 (absolute 値) are evaluated. For the sake of convenience, the SU is called “the average 値 or average size deformation of the dimensional deformation rate”. The latter is referred to as "the maximum 値 or the maximum dimensional deformation rate of the dimensional deformation rate." In the second aspect of the present invention, the "average 尺寸 of the dimensional deformation rate" and the "dimensional deformation rate" are simultaneously used. The evaluation of the dimensional deformation after heat treatment in both of the maximum 値 is different from the conventional technique of measuring only the former (average 尺寸 of the dimensional deformation ratio) disclosed in Patent Document 2. According to the present inventors As a result of the experiment, it is known that if the dimensional deformation after the heat treatment is suppressed by the full -30-200831682, if the average 値 of the dimensional deformation ratio is made as small as possible as disclosed in Patent Document 2, It is not enough, but it is indispensable to make the dimensional deformation (degree of difference) in all directions of thickness, width and length become small. Sometimes it is: even if the average deformation of the dimensional deformation rate is suppressed, The case where the difference in the dimensional deformation ratio is still large (there is also the opposite case) (please refer to the embodiment described later). Further, in the second aspect of the present invention, the so-called "φ is very deformed after heat treatment. Small (having excellent dimensional deformation inhibition) means that when the dimensional change before and after the heat treatment is measured according to the method described in the column of the examples to be described later, the average 尺寸 of the dimensional deformation ratio is within ±0.03% and the size The maximum 値 (absolute 値) of the deformation rate is less than 0.05%. Further, the evaluation criteria (method and level) in the second aspect of the present invention are different from the first aspect of the present invention in the following points: First, regardless of the first aspect of the present invention Or, in the second aspect of the present invention, the "average 尺寸 of the dimensional deformation ratio" is used as the evaluation standard for the dimensional deformation after the heat treatment, but the first aspect of the present invention sets the qualification standard to ±0.05%. The second aspect of the present invention is stricter than the first aspect of the present invention, and the qualification standard is defined as 〇3%. Further, in the first aspect of the present invention, the "difference in the dimensional deformation ratio", that is, the difference 値 (absolute 値) between the maximum 値 and the minimum χ among the above Δχ, Ay, and Δζ is used. In the second aspect of the present invention, the "maximum defect of the dimensional deformation ratio" is adopted as described above. This is because -31 - 200831682 is based on the fact that the part (maximum enthalpy) that has the greatest degree of difference in heat treatment after heat treatment is required to provide the steel according to the first aspect of the present invention. In addition to the "difference in dimensional deformation rate" of the first aspect of the present invention described above, "large ruler" is used. As shown in the later-described embodiment, the "size change rate" specified in the first aspect of the present invention is satisfied, as shown in the following description. Example) "Steel having excellent heat treatment inhibition property" in the second aspect of the invention. The composition of the steel in the second aspect of the present invention is as follows in the predetermined range of various alloying elements which contribute to precipitation hardening, and is also controlled between the predetermined elements by the following formulas (1) to (4). The balance is used to seek sex. As shown in the later-described embodiment, if such a requirement cannot be met, the desired characteristics cannot be ensured. In the second aspect, the addition of three elements of Cu, Ni, and A1 may be lacking, for example, it has been confirmed from the experimental results that the steel of the composition of the patent document 3 does not contain Cu and Ni spear elements. In particular, the second aspect of the present invention is not obtained, and in order to reduce the dimensional deformation as much as possible, in addition to the mass ratio which constitutes the above & [Cu] and [C], it is appropriate to control The most indirect deformation rate described in the description of the more excellent dimensional deformation (the ability to become smaller) is that the maximum amount of the indifference steel which is invisible is not described as the subsequent dimensional deformation. In addition to the fact that the content is controlled at the site, and any of the above-mentioned specific elements are appropriately improved, the method of the present invention is not one of the above-mentioned patents [] A1. ) when Cr and C -32-

200831682 含有量的乘積(〔以〕乂〔(:〕的上限)、ci Si量(上限)、Μη量(上限)、Ms點(下 (上限)、Ni量(上限)、Cr量(上限)、 X〔 W〕(上限)的做法也是很重要的。本發 作爲基本,所以Ms點會變高而殘留沃斯田鑲 本就很少,除此之外,又適切地控制Cu、Ni 合金成分的含有量,因此,可以很明顯地抑 4 00〜5 5 0 °C的時效處理後、表面硬化處理後的 。這是被認爲:藉由上述合金成分的添加, 400〜500 °C的低溫域時主要是生成ε -Cu,在 °C的中間溫度域時主要是生成Ni-(Al,Mo) 合物,在約5 0 0〜5 5 0 °C的高溫域時,主要是召 碳化物,但是這些析出物的結晶構造(FCC || 質(BCC構造)不同,所以體積會收縮,這f 的尺寸變形抑制有幫助。又,本發明是將成夭 地不要析出粗大的Cr系碳化物,因此結晶 哪一個方向都是等方向性,因此被認爲即使 形狀的模具製造上,亦可有效地抑制熱處理 又’本發明的第2態樣,爲了要提昇焊渥 HAZ軟化幅度變小)主要是適切地控制〔Cr〕 限、Ms點(下限)、C量(下限)、A1量| 量(下限)、〔Cu〕/〔 Ni〕(上限、下限) 〇.5x〔W〕(下限)、乂量(上限)。亦即, (上限)、 展)、A1量 [Mo ) +0.5 明係以低 C 量的生成原 、A1之類的 制特別是約 膨脹、收縮 例如:在約 約 450〜530 系金屬間化 L成Mo-V系 f造)係與基 〖於熱處理後 ‘設計成極力 〖造無論是於 :在大型複雜 :的尺寸變形 ^修補性(使 X〔 C〕的上 :下限)、Ni 、〔Mo〕+ 作爲用來使 -33- 200831682 ΗAZ軟化幅度變小的設計指針,並不是要利用麻田散鐵的 生成所導致的硬化,而是不僅將C量控制在約〇 . 2〜0.6 0 % 程度的低C量,而且是利用因合金成分(主要是添加A1 、Cu、Ni、Mo、W )的添加所導致的析出硬化(例如: ε -Cu、Ni-Al系金屬間化合物、Ni-Mo系金屬間化合物) 。這些的析出物係在基質中細微地整合析出,所以硬度會 顯著地增加。 φ 尤其是Cu、Ni、A1是重要的析出硬化元素,是對於 抑制HAZ軟化有很大的幫助的元素。經由實驗的結果已 經確認出:未實質性地添加這些元素的其中一種元素的鋼 係無法獲得所期待的HAZ軟化抑制作用。 此外已知:〔Cu〕/〔 Ni〕的比(〔Cu〕對於〔Ni〕 的比)係與HAZ軟化的抑制有密接的關係,藉由適切地 控制上述的比率,可以抑制HAZ軟化。 以下將說明本發明的第2態樣的鋼中成分。 C: 0.20 〜0.60% C係用來確保硬度及耐磨損性,是對於抑制HAZ軟化 幅度有幫助的元素。又,利用CVD法在模具母材的表面 生成VC、TiC之類的碳化物皮膜的時候,如果C濃度太 低的話’也會有皮膜的厚度變薄之類的問題發生。若考慮 到這些因素,並想要有效發揮上述作用的話,乃將C量的 下限選定爲0.20%。C量是0.22%以上爲宜。惟,添加過 量的話,殘留沃斯田鐵會增加,如果不執行高溫的時效處 -34- 200831682 理的話,不僅無法獲得所期待的硬度,時效處理後會發生 膨脹等現象,尺寸變形會變大,因此乃將上限選定爲 0.60%。C量是0.50%以下爲宜,0.45%以下更好。 S i : 0 · 5 〜2 · 0 0 %200831682 Product of the content ([] is the upper limit of [(:]), ci Si (upper limit), Μη (upper limit), Ms point (lower (upper limit), Ni amount (upper limit), Cr amount (upper limit) The method of X[W] (upper limit) is also very important. As the basics, the Ms point will become high and there will be little Vastfield inlays. In addition, the Cu and Ni alloys are properly controlled. The content of the component can therefore be significantly suppressed after the aging treatment of 4 00 to 5 50 ° C, after the surface hardening treatment. This is considered to be: by the addition of the above alloy composition, 400 to 500 ° C In the low temperature region, ε-Cu is mainly formed, and in the intermediate temperature range of °C, Ni-(Al,Mo) compounds are mainly formed, and in the high temperature region of about 50,000 to 550 °C, mainly Carbides are called, but the crystal structure of these precipitates (FCC || quality (BCC structure) is different, so the volume shrinks, and the deformation inhibition of f is helpful. Moreover, the present invention does not precipitate coarse Cr. Carbide, so which direction of crystallization is isotropic, so it is considered that even the shape of the mold In terms of manufacturing, it is also possible to effectively suppress the heat treatment and the second aspect of the present invention, in order to increase the softening amplitude of the HAZ of the weld bead, it is mainly to appropriately control the [Cr] limit, the Ms point (lower limit), and the C amount ( Lower limit), A1 amount | Quantity (lower limit), [Cu]/[Ni] (upper limit, lower limit) 〇.5x [W] (lower limit), 乂 quantity (upper limit), that is, (upper limit), spread), A1 The amount of [Mo ) +0.5 is based on the formation of a low C amount, and the formation of A1, in particular, about expansion and contraction, for example, in the case of about 450 to 530, intermetallicization of L into a Mo-V system. Base 〖after heat treatment' is designed to be as strong as possible. Manufactured in: large-scale complex: dimensional deformation ^ repairability (making X[C] upper: lower limit), Ni, [Mo]+ as used to make -33- 200831682 The design pointer of ΗAZ softening is not to use the hardening caused by the formation of granulated iron, but not only the amount of C is controlled to a low C amount of about 2 to 0.6 0 %, but also the utilization factor. Precipitation hardening due to the addition of alloy components (mainly A1, Cu, Ni, Mo, W) (for example: ε -Cu, Ni -Al-based intermetallic compound, Ni-Mo-based intermetallic compound). These precipitates are finely integrated and precipitated in the matrix, so the hardness is remarkably increased. φ, in particular, Cu, Ni, and A1 are important precipitation hardening elements and are important elements for suppressing HAZ softening. As a result of the experiment, it has been confirmed that the steel system which does not substantially add one of these elements cannot obtain the desired HAZ softening inhibition effect. Further, it is known that the ratio of [Cu] / [Ni] (the ratio of [Cu] to [Ni]) is in close contact with the suppression of HAZ softening, and by appropriately controlling the above ratio, HAZ softening can be suppressed. Hereinafter, the steel component in the second aspect of the present invention will be described. C: 0.20 to 0.60% C is used to ensure hardness and abrasion resistance, and is an element that helps to suppress the HAZ softening range. When a carbide film such as VC or TiC is formed on the surface of the mold base material by the CVD method, if the C concentration is too low, there is a problem that the thickness of the film is reduced. If these factors are taken into consideration and the above-mentioned effects are to be effectively exerted, the lower limit of the amount of C is selected to be 0.20%. The amount of C is preferably 0.22% or more. However, if the addition is excessive, the residual Worthite iron will increase. If the high-temperature aging is not performed, the expected hardness will not be obtained, and the expansion will occur after the aging treatment, and the dimensional deformation will become large. Therefore, the upper limit is selected to be 0.60%. The amount of C is preferably 0.50% or less, more preferably 0.45% or less. S i : 0 · 5 〜 2 · 0 0 %

Si是可作爲製鋼時有用的脫氧元素,是對於硬度的提 昇與確保被切削性有幫助的元素。又,Si對於抑制基質的 麻田散鐵的回火軟化,抑制HAZ軟化幅度也很有用。爲 了使其有效地發揮這種作用,乃將Si量的下限選定爲 0.5 %。惟,添加過量的話,偏析會變大,不僅熱處理後的 尺寸變形會變大,韌性也會降低,因此將上限選定爲 2.00%。Si量的下限以1%爲宜,1.2%更好,另外,Si量 的上限是以1 . 8 5 %爲宜。 Μη : 0· 1 〜2% • Μη是可作爲確保淬火性之有用的元素,但是添加過 量的話,Ms點會明顯地降低,殘留沃斯田鐵會增加,所 以如果不執行高溫的時效處理的話,就無法獲得所期待的 硬度。考慮到這些因素,乃將Μη的含有量選定在上述範 圍。Μη量的下限是以〇.15 %爲宜,另外,Μη量的上限是 以1%爲宜,0.5%更好,0.35%尤佳。Si is a deoxidizing element which can be used as a steel material, and is an element which contributes to the improvement of hardness and the machinability. Further, Si is also useful for suppressing the temper softening of the matrix of the granulated iron and suppressing the softening of the HAZ. In order to effectively perform this effect, the lower limit of the amount of Si is selected to be 0.5%. However, if the addition is excessive, the segregation becomes large, and not only the dimensional deformation after heat treatment becomes large, but also the toughness is lowered, so the upper limit is selected to be 2.00%. The lower limit of the amount of Si is preferably 1%, more preferably 1.2%, and the upper limit of the amount of Si is preferably 1.85%. Μη : 0· 1 ~2% • Μη is a useful element for ensuring hardenability, but if it is added excessively, the Ms point will be significantly lowered, and the residual Worth iron will increase, so if high temperature aging treatment is not performed, , the expected hardness cannot be obtained. In consideration of these factors, the content of Μη is selected in the above range. The lower limit of the amount of Μη is preferably 〇15%, and the upper limit of the amount of Μη is preferably 1%, more preferably 0.5%, and particularly preferably 0.35%.

Cr: 3.00 〜9.00%Cr: 3.00 ~ 9.00%

Cr是可作爲用來確保預定的硬度之有用的元素。Cr -35- 200831682 量若未滿3.0 0 %的話,淬火性會不足而會局部 鐵,因此硬度會降低,無法確保耐磨損性。 3. 5 %以上爲宜,4.0%以上更好。惟,添加過量 生成大量的粗大的Cr系碳化物,熱處理後會 皮膜的耐久性,因此將上限選定爲 9.00%。 7.0%以下爲宜,6.5%以下更好,6.0%以下尤佳 A1 : 0.3 〜2.0% A1是用以謀求因爲Ni3Al之類的Al-Ni系 物的析出強化所導致的硬度提昇所必要的元素 HAZ軟化幅度也有幫助。又,A1也可以當作 慮到這些因素,乃將A1的下限選定爲〇 · 3 %。 量的話,偏析會變大,不僅熱處理後的尺寸變 尺寸變形率的差値)會變大,也會導致韌性的 將其上限選定爲2·0%。A1量係以0.50%以上 宜,0.7%以上1.6%以下更好。 C u · 1.00 〜5%Cr is a useful element for ensuring a predetermined hardness. If the amount of Cr -35- 200831682 is less than 3.0%, the hardenability will be insufficient and local iron will be formed, so the hardness will be lowered and the wear resistance cannot be ensured. 3. More than 5% is better, and 4.0% is better. However, excessive addition of a large amount of coarse Cr-based carbide is formed, and the durability of the film is obtained after the heat treatment, so the upper limit is selected to be 9.00%. 7.0% or less is more preferable, 6.5% or less is more preferable, and 6.0% or less is more preferably A1: 0.3 to 2.0%. A1 is an element necessary for improving the hardness due to precipitation strengthening of an Al-Ni-based material such as Ni3Al. The HAZ softening range is also helpful. Also, A1 can be considered as taking these factors into consideration, and the lower limit of A1 is selected as 〇 · 3 %. In the case of the amount, the segregation becomes large, and not only the difference in dimensional deformation rate after heat treatment, but also the upper limit of the toughness is selected to be 2.0%. The amount of A1 is preferably 0.50% or more, more preferably 0.7% or more and 1.6% or less. C u · 1.00 ~ 5%

Cu是用以謀求因爲ε -Cu的析出強化所導 所必要的元素’對於抑制HAZ軟化幅度也有 添加過量的話,變得容易發生鍛造龜裂’因此 定爲5%。Cu量是以2.0%以上4.0%以下爲宜。 N i : 1 · 0 0 〜5 % 地生成變韌 Cr量是以 的話,將會 收縮,降低 Cr量是以 金屬間化合 ,對於抑制 脫氧劑。考 惟,添加過 化(尤其是 降低,因此 1 . 8 %以下爲 致的硬提昇 幫助。惟, 將其上限選 -36- 200831682Cu is an element which is required to be guided by the precipitation strengthening of ε-Cu. When the amount of the softening of the HAZ is excessively increased, the forged crack is likely to occur. The amount of Cu is preferably 2.0% or more and 4.0% or less. N i : 1 · 0 0 ~5 % The amount of toughened Cr is formed, and it will shrink, and the amount of Cr will be reduced by intermetallic, and the deoxidizer will be suppressed. However, the addition is over (especially reduced, so less than 1.8% of the hard lifting help. However, the upper limit is selected -36- 200831682

Ni是用以謀求因爲Ni3Al之類的Al-Ni系金屬間化合 物的析出強化所導致的硬度提昇所必要的元素,對於抑制 ΗAZ軟化幅度也有幫助。又,Ni係可與Cu —起倂用,藉 此可以抑制因Cu的添加過量所導致的熱間脆性,也可以 防止鍛造時的龜裂。惟,添加過量的話,殘留沃斯田鐵會 增加,如果不執行高溫的時效處理的話,不僅無法確保預 定的硬度,熱處理後也會產生膨脹。Ni量係以1.5%以上 4.0%以下爲宜。Ni is an element necessary for improving the hardness due to precipitation strengthening of an Al-Ni-based intermetallic compound such as Ni3Al, and is also useful for suppressing the softening range of ΗAZ. Further, the Ni system can be used together with Cu, whereby the bridging property at the time of forging can be prevented by suppressing the hot brittleness due to the excessive addition of Cu. However, if the addition is excessive, the residual Worthite iron will increase. If the high-temperature aging treatment is not performed, not only the predetermined hardness but also the expansion after heat treatment will be ensured. The Ni amount is preferably 1.5% or more and 4.0% or less.

Mo : 0.5〜3%及/或W : 2%以下(含0% )Mo : 0.5 to 3% and/or W: 2% or less (including 0%)

Mo及W皆爲除了可形成M6C型碳化物之外,亦可形 成Ni3Mo系金屬間化合物等,是對於析出強化有幫助的元 素。惟,Mo、W添加過量的話,上述的碳化物等將會生 成過剩,不僅會導致韌性的降低,熱處理後的尺寸變形( 尤其是尺寸變形率的差値)會變大,因此乃設定在上述範 圍。本發明中雖然是以Mo作爲必要成分,W係當作選擇 元素,但是亦可將兩種都倂用。Mo係以0.5 %以上3 %以 下爲宜,0.7%以上2.5%以下更好。又,W則是2%以下爲 宜,1 .5 %以下更好。 S : 0 · 1 0 %以下(不含0 % ) S是用來確保被切削性之有用的元素,但是添加過量 的話,會產生焊接龜裂,因此將上限選定爲0.1 0 %。S量 是以 0.07%以下爲宜,0.05%以下更好,0.025%以下尤佳 -37- 200831682 此外,本發明必須符合下列數式(1 )〜(4 )的要件 {〔〕是代表各元素的含有量(%)之意}。 數式(1 ) 〔 Cr〕X〔 C〕S 3.00 上述數式(1 )是基於抑制粗大的C r系碳化物的生成 之目的而設定的,〔Cr〕與〔C〕的乘積超過3.00的話, 熱處理後的尺寸變形會變大,表面皮膜的耐久性會降低。 〔Cr〕與〔C〕的乘積係以1.80以下爲宜,1.70以下更好 。此外,其下限,基於抑制熱處理後的尺寸變形等等的觀 點,雖然是愈小愈好,但是,也考慮到想要有效地發揮因 Cr、C的添加所帶來的上述作用的話,大槪是以0.8爲宜 〇 數式(2) 〔Cu〕/〔Ni〕:0·5〜2·2 上述數式(2 )主要是被設定作爲用來利用ε -Cu的析 出強化以抑制HAZ軟化幅度的參數(請參考後述的實施 例)。爲了有效發揮這種作用,將〔C u〕對〔N i〕的比値 設定爲〇 · 5。惟,上述比値變大的話,會發生鍛造龜裂, 因此將其上限選定爲2·2。上述比値是〇.7以上〗.5以下爲 宜,0.8 5以上1.2以下更好。 數式(3 ) 〔 Mo〕+ 〇.5x〔 W〕: 0.5 〜3.0% 構成上述數式(3 )的Mo、W係如前所述,是對於析 出強化有幫助的元素,上述數式(3)主要是被設定作爲 用來確保因這些元素的析出強化所帶來的硬度提昇的參數 ,對於抑制HAZ軟化幅度也有效。上述數式(3 )中,〔 -38- 200831682 w〕的係數(0.5)是考慮到Mo的原子量是w的約1/2而 決定的。爲了要有效地使其發揮這些作用,乃將上述數式 (4 )的下限選定爲〇. 5 %。惟’ Mo、W的量添加過量的話 ,上述碳化物將會過剩添加,不僅會導致韌性的降低,熱 處理後的尺寸變形(尤其是尺寸變形率的差値)會變大, 因此將上述數式(3 )的上限選定爲3.0%。上述數式(3 )的下限係1.0%爲宜,1.2%更好,另外,其上限是2.8% 爲宜。 數式(4) 〔 Cu〕/〔 C〕: 4.0 〜15 上述數式(4 )的定位,主要是作爲用來使熱處理後 (時效處理後)的硬度的峰値更往低溫側移動的參數,藉 此,以謀求熱處理後的尺寸變形抑制性。一般而言,時效 處理(回火)後的膨脹尺寸變形係因爲熔體化處理(淬火 )時的殘留沃斯田鐵的開放(分解)而發生的(例如:請 參考後述的第9圖),如上述數式(4 )所示般地,可知 只要適切地控制具有可將時效後的硬度峰値往低溫側移動 的作用之Cu與具有與殘留沃斯田鐵密切的相關關係的C 的質量比(〔Cu〕/〔 C〕之比値)的話,就可以顯著地控 制熱處理後的尺寸變形。 第1圖是顯示出:以後述的實施例所述的方法來測定 尺寸變形率(平均値及最大値)時的〔Cu〕/〔 C〕的比値 對於尺寸變形率的影響之圖表。這個圖表是將後述的表7 的 Νο·44(鋼種 A) 、52(鋼種 C) 、56(鋼種 D) 、70 (鋼種J ) 、7 2 (鋼種Κ)的結果標示出來。這些鋼種含 -39- 200831682Both Mo and W can form a Ni3Mo-based intermetallic compound in addition to the M6C-type carbide, and are useful for precipitation strengthening. However, when Mo and W are excessively added, the above-mentioned carbides and the like are excessively formed, which not only causes a decrease in toughness, but also causes dimensional deformation (especially, the difference in dimensional deformation ratio) after heat treatment to be large. range. In the present invention, although Mo is used as an essential component and W is used as a selection element, both may be used. The Mo system is preferably 0.5% or more and 3% or less, more preferably 0.7% or more and 2.5% or less. Further, W is preferably 2% or less, more preferably 1.5% or less. S : 0 · 1 0 % or less (excluding 0 %) S is a useful element for ensuring machinability. However, if excessive addition occurs, weld cracking occurs, so the upper limit is selected to be 0.10%. The amount of S is preferably 0.07% or less, more preferably 0.05% or less, more preferably 0.025% or less, and particularly preferably -37-200831682 In addition, the present invention must conform to the following formulas (1) to (4): {[] represents each element The meaning of the content (%)}. Formula (1) [Cr]X[C]S 3.00 The above formula (1) is set for the purpose of suppressing the formation of coarse Cr-based carbides, and the product of [Cr] and [C] exceeds 3.00. The dimensional deformation after heat treatment becomes large, and the durability of the surface film is lowered. The product of [Cr] and [C] is preferably 1.80 or less, more preferably 1.70 or less. In addition, the lower limit is based on the viewpoint of suppressing dimensional deformation after heat treatment, etc., and the smaller the better, but it is also considered to be effective in exerting the above-mentioned effects due to the addition of Cr and C. 0.8 is the appropriate formula (2) [Cu] / [Ni]: 0 · 5 ~ 2 · 2 The above formula (2) is mainly set to use the precipitation strengthening of ε - Cu to inhibit HAZ softening The parameters of the amplitude (please refer to the embodiment described later). In order to effectively perform this effect, the ratio 〔 of [C u] to [N i] is set to 〇 · 5. However, if the above ratio becomes larger, forging cracking occurs, so the upper limit is selected to be 2·2. The above ratio is preferably 7.7 or more and .5 or less is preferably 0.85 or more and 1.2 or less. Formula (3) [Mo]+ 〇.5x [W]: 0.5 to 3.0% The Mo and W systems constituting the above formula (3) are elements which are helpful for precipitation strengthening as described above, and the above formula ( 3) It is mainly set as a parameter for ensuring the hardness increase due to precipitation strengthening of these elements, and is also effective for suppressing the HAZ softening range. In the above formula (3), the coefficient (0.5) of [ -38 - 200831682 w] is determined in consideration of the atomic weight of Mo being about 1/2 of w. In order to effectively perform these functions, the lower limit of the above formula (4) is selected to be 〇. 5 %. However, if the amount of Mo and W is excessively added, the above-mentioned carbides will be excessively added, which not only causes a decrease in toughness, but also causes dimensional deformation (especially, the difference in dimensional deformation ratio) after heat treatment, so that the above formula The upper limit of (3) is selected to be 3.0%. The lower limit of the above formula (3) is preferably 1.0%, more preferably 1.2%, and the upper limit is preferably 2.8%. Formula (4) [Cu]/[C]: 4.0 to 15 The positioning of the above formula (4) is mainly used as a parameter for moving the peak of the hardness after heat treatment (after aging treatment) to the low temperature side. Thereby, dimensional deformation inhibition after heat treatment is sought. In general, the expansion dimensional deformation after the aging treatment (tempering) occurs due to the opening (decomposition) of the residual Worth iron during the melt treatment (quenching) (for example, please refer to FIG. 9 described later). As shown in the above formula (4), it is understood that Cu having an action of shifting the hardness peak after aging to the low temperature side and C having a close correlation with the residual Worthite iron are appropriately controlled. When the mass ratio (ratio of [Cu]/[C]), the dimensional deformation after heat treatment can be remarkably controlled. Fig. 1 is a graph showing the effect of the ratio 〔 of [Cu]/[C] when measuring the dimensional deformation ratio (average 値 and maximum 値) by the method described in the examples described later on the dimensional deformation ratio. This chart indicates the results of Νο.44 (steel type A), 52 (steel type C), 56 (steel type D), 70 (steel type J), and 7 2 (steel type) of Table 7 to be described later. These steel grades include -39- 200831682

有大致同等程度的C、Si、Μη、Cr、Al、Cu、Ni、Mo、W 。如第8圖所示般地,可知〔Cu〕/〔 C〕的比値係與尺寸 變形率具有密切的關係,藉由將上述的比値控制在4 · 0〜 1 5的範圍内,就可以將尺寸變形率抑制在本發明的第2態 樣所規定的範圍内(尺寸變形率的平均値爲±0· 03 %以下、 尺寸變形率的最大値爲0.05%以下)。 〔Cu〕/〔 C〕的比値如果未滿4 · 0的話,峰値硬度時 的時效溫度較之殘留沃斯田鐵開始分解時的溫度更高出許 多,因此,時效處理後的膨脹量會變大,另外,上述的比 値如果超過1 5的話,隨著時效溫度的上昇的收縮(與熔 體化處理後的膨脹互相抵消)不再產生,無論是哪一種, 都無法獲得預定的耐尺寸變形抑制性。上述的比値是以 5.0以上1 3以下爲宜,6.0以上1 2以下更好。 本發明的第2態樣的鋼中成分係如上所述,其餘部分 是鐵以及不可避免的雜質。不可避雜質,例如:是可舉出 在製造過程中不可避地混入的元素等等,例如:P、N、Ο 等等。P量大槪是0.05 %以下爲宜,0.03 %以下更好。N量 大槪是350ppm以下爲宜,200ppm以下更好,150ppm以 下尤佳。〇量大槪是50ppm以下爲宜,30ppm以下更好, 20Ppm以下尤佳。 本發明又基於更爲改善其他的特性之目的,亦可添加 以下的成分。 V : 0 · 5 %以下(不含〇 % ) V是可形成Vc之類的碳化物而對於提昇硬度有幫助 -40- 200831682 ,是抑制HAZ軟化幅度有效的元素。此外,在母材表面 實施氣體氮化、鹽浴氮化、電漿氮化之類的氮化處理以形 成擴散硬化層的時候,是提昇表面硬度、提昇硬化層深度 之有效的元素。想要有效地使其發揮這種作用,V量大槪 是添加〇 . 〇 5 %以上爲宜。惟,添加過量的話’固熔c量會 降低,會導致母相也就是麻田散鐵組織的硬度降低,因此 將其上限選定爲〇·5 %爲宜。V量爲0.4%以下更好,0.30% 以下尤佳。 從由Ti、Zr、Hf、Ta、及Nb所組成的群所選出的至 少一種元素合計爲0.5 %以下(不含0% ) 這些元素都是氮化物形成元素,是對於該氮化物及 A1N的微細分散化及結晶粒微細化所導致的韌性提昇有幫 助的元素。想要有效地使其發揮這種作用,大槪的添加量 ,Ti是0.01%以上、Zr是0.02%以上、Hf是0.04%以上、 Ta是0.04%以上、Nb是0.02%以上爲宜。惟,添加過量 的話,固熔C量會降低而導致麻田散鐵的硬度降低,因此 ,上述元素的合計量是0.5 %爲宜。上述元素的合計量是 0.4 %以下更好,0 · 3 0 %以下尤佳。此外,上述的元素既可 單獨地添加,亦可倂用兩種以上。There are approximately the same degree of C, Si, Μη, Cr, Al, Cu, Ni, Mo, W. As shown in Fig. 8, it can be seen that the specific enthalpy of [Cu]/[C] has a close relationship with the dimensional deformation ratio, and by controlling the above-mentioned specific enthalpy within the range of 4 · 0 to 15 The dimensional deformation ratio can be suppressed within the range defined by the second aspect of the present invention (the average 値 of the dimensional deformation ratio is ±0·03% or less, and the maximum 尺寸 of the dimensional deformation ratio is 0.05% or less). If the ratio of [Cu]/[C] is less than 4 · 0, the aging temperature at the peak hardness is much higher than the temperature at which the residual Worth iron begins to decompose. Therefore, the amount of expansion after aging treatment If the above ratio is more than 15 , the shrinkage with the increase in the aging temperature (which cancels out the expansion after the melt treatment) is no longer generated, and no matter which one, the predetermined one cannot be obtained. Resistance to dimensional deformation inhibition. The above ratio is preferably 5.0 or more and 1 or less, more preferably 6.0 or more and 1 or less. The components in the steel of the second aspect of the present invention are as described above, and the rest are iron and unavoidable impurities. Unavoidable impurities, for example, include elements that are inevitably mixed in during the manufacturing process, such as P, N, Ο, and the like. The amount of P is preferably 0.05% or less, more preferably 0.03% or less. The amount of N is preferably 350 ppm or less, more preferably 200 ppm or less, and particularly preferably 150 ppm or less. The amount of sputum is preferably less than 50 ppm, more preferably less than 30 ppm, and preferably less than 20 pm. The present invention is further based on the object of further improving other characteristics, and the following components may be added. V : 0 · 5 % or less (excluding 〇 % ) V is a carbide which can form Vc and is useful for lifting hardness -40- 200831682 , which is an effective element for suppressing the softening of HAZ. Further, when the surface of the base material is subjected to nitriding treatment such as gas nitriding, salt bath nitriding, or plasma nitriding to form a diffusion hardened layer, it is an effective element for improving the surface hardness and increasing the depth of the hardened layer. In order to effectively play this role, the amount of V is greater than that of 〇 〇 5% or more. However, if the amount of addition is too large, the amount of solid solution c will decrease, which will result in a decrease in the hardness of the parent phase, which is the structure of the granulated iron structure. Therefore, it is preferable to set the upper limit to 〇·5%. The amount of V is preferably 0.4% or less, more preferably 0.30% or less. At least one element selected from the group consisting of Ti, Zr, Hf, Ta, and Nb is 0.5% or less (excluding 0%). These elements are all nitride forming elements for the nitride and A1N. An element that contributes to the improvement of toughness caused by fine dispersion and grain refinement. In order to effectively exert such an effect, it is preferable that Ti is added in an amount of 0.01% or more, Zr is 0.02% or more, Hf is 0.04% or more, Ta is 0.04% or more, and Nb is 0.02% or more. However, if the amount of addition is excessive, the amount of solid solution C is lowered and the hardness of the granulated iron is lowered. Therefore, the total amount of the above elements is preferably 0.5%. The total amount of the above elements is preferably 0.4% or less, and more preferably 0.30% or less. Further, the above elements may be added singly or in combination of two or more.

Co : 10%以下(不含0% )Co : 10% or less (excluding 0%)

Co係用來提高Ms點,減少殘留沃斯田鐵之有效的元 素,藉此可提高硬度。爲了使其有效地發揮上述作用,Co 量大槪是1 %以上爲宜。惟,添加過量的話,會導致成本 等的上昇,乃將上限選定爲10%爲宜。Co量的上限爲 -41 - 200831682 5.5%更好。 麻田散鐵轉態點(M s點)g 1 7 0 °C Ms點 = 550-361x〔C〕-3 9x〔Mn〕-35x〔V〕-2 0x〔Cr〕 -17x[Ni] -10x[Cu] -5x( [Mo] + [W]) + 15x [ Co ) + 3 0x [ A1 ) {式中的〔〕是代表各元素的含有量(%)之意} 在本發明中,Ms點主要是作爲硬度、熱處理後的尺 寸變形抑制的指標,如果Ms點未滿170°C的話,殘留沃 斯田鐵會增大,如果不執行高溫的時效處理的話,不僅無 法獲得所期待的硬度,也會導致熱處理後的膨脹。Ms點 是愈高愈好,大約23 0 °C以上更好,23 5 °C以上尤佳,250 °C以上最好。此外,其上限,基於上述作用的觀點,雖然 並無特別的限定,但是考量到構成Ms點之上述元素的添 加所帶來的作用效果等等因素的話,大約是3 5 0 °C爲宜, 320°C更好。 其次,說明製造本發明的第2態樣之模具用鋼的方法 〇 本發明的製造方法係包含:製備符合前述要件的鋼之 工序、以及以符合下列數式(5 )的條件來執行熔體化處 理及時效處理的工序。 ΤΑ-1 0 ^ T2 ^ T A + 1〇 …(5) 式中, ΤΑ - 0.29xT 1 -2.63x C Cu ] /〔C〕+ 225, -42- 200831682 τ 1是代表熔體化溫度(°c ), T2是代表時效溫度(°C )。 具體而言,先熔製出符合前述要件的鋼之後,進行熱 間锻造,然後進行退火(例如:以約7 0 0 X:保持7小時之 後,以約17°C /hr的平均冷卻速度進行爐中冷卻至約400 °C之後,放冷)使其軟化之後,藉由切削加工等,而粗加 工成爲預定的形狀,然後再以上列數式(5 )的條件執行 熔體化處理及時效處理即可。 如前所述,本發明的第2態樣係採用:熔體化處理時 的殘留沃斯田鐵量較少的鋼中成分,而且進一步以上列數 式(5 )所示般地,將Cu與C的質量比(〔Cu ) /〔 C ) )藉由熔體化溫度Τ 1及時效溫度T2的關係來加以控制的 話,即可在時效處理後殘留沃斯田鐵分解膨脹之前,就調 整成讓時效後的硬度達到峰値,因此,可以同時謀求熱處 理後的尺寸變形抑制與硬度的兩種作用效果。一般而言, 在製造模具用鋼時,是利用約9 5 0〜1 1 5 0 °C的溫度來執行 熔體化處理—以約400〜5 3 0 °C的溫度來執行時效處理,以 賦予其所期待的硬度,但是,根據本發明人的實驗結果得 知:即使在上述的範圍內執行熔體化處理及時效處理,有 時候也無法獲得所期待的硬度,而且有時候也無法充分地 抑制熱處理後的尺寸變形(請參考後述的實施例),因此 ,乃界定出上列數式(5 )。 將本發明的上述機制與前述專利文獻2 (相當於傳統 的高C高Cr鋼)的方法進行比較的話,專利文獻2是如 -43- 200831682 本案的第2圖(相當於專利文獻2的第1圖)所示般地, 在殘留沃斯田鐵有某些程度分解的時間點,執行可讓回火 時的尺寸變形趨於零的這種回火處理,相對地,本發明則 是以殘留沃斯田鐵開始分解之前或者剛開始分解隨後的溫 度來執行回火處理,在這一點上,兩者是不同的。亦即, 本發明與傳統的高C高C r鋼相比較,大槪是以較低的溫 度來執行時效處理(具體而言,大槪是約5 0 0 °C以下的低 溫度)。根據本發明,並不像專利文獻2那樣地在熱處理 後的尺寸變形激烈的領域(第3圖中的A領域)中執行時 效處理,而是在被認爲是可生成大量的穩定的殘留沃斯田 鐵的領域(第3圖中的B領域)內執行時效處理,因此, 可獲得較之專利文獻2所揭示的鋼的尺寸變形的差異程度 更小的鋼。又,以這種方式在比較低溫度的領域執行時效 處理的話,殘留沃斯田鐵的穩定性可以提昇,殘留沃斯田 鐵的經時變化變小,所以亦可獲得熱處理後的尺寸變形的 經時性變化變小之效果。 時效溫度T2是以上述的TA±5°C爲宜。 又,熔體化溫度T1係可採用在製造模具用鋼時,較 之一般所採用的範圍更低的溫度,如此一來,可讓熱處理 變形更少。具體而言,大槪是900〜1150 °C的範圍内爲宜 〇 本發明是只要將熔體化處理及時效處理的溫度以上述 的的方式適切地控制即可,這些的時間並無特別的限定, 只要以製造模具用鋼時一般所採用的條件來實施就可以了 -44- 200831682 ,大槪是將熔體化時間(加熱時間)控制在1〜5小時程 度,將時效時間(保持時間)控制在2〜8小時的程度就 可以了。 〔實施例〕 以下將舉出實施例更爲具體地說明本發明,但是本發 明原本就不受下列實施例的限制,在可適合前述與後述的 要旨的範圍內施加適當的變更來予以實施都是可能的,這 些也都是包含在本發明的技術範圍內。 首先,說明本發明的第1態樣的實施例如下。 使用表1及表2所述的各種鋼種No .,以真空感應熔 解爐熔製150kg的鋼胚之後,加熱到約900〜1 150°C,鍛 造成兩片40mmTx75mmWx約2000mmL的鋼板,然後以約 6 0°C /hr的平均冷卻速度慢慢地進行冷卻。冷卻到達100 °C 以下的溫度之後,再度加熱至約8 5 0 °C的溫度,以約5 0 °C /hr的平均冷卻速度慢慢地進行冷卻(進行退火)。 使用以上述方法所製得的各種退火材,進行下列(1 )〜(4 )的試驗。 (1 )硬度試驗(測定最大硬度) 從上述的退火材切出尺寸爲大約 20mmTx20mmWx 1 5mmL的試驗片來當作硬度測定用試驗片,對此試驗片實 施以下的熱處理。 熔體化處理(淬火處理):以約1〇2〇〜l 〇30°C進行 -45- 200831682 1 20分鐘的加熱空氣中冷卻—時效處理(回火處理): 以約400〜5 60 °C保持約3小時―放冷。 如上所述,利用畢式硬度計(AK AS HI公司製造的規 格AVK,荷重5kg)來測定將回火溫度在約400〜5 60°C的 範圍内作變化時的硬度,並且找出最大硬度(HV )。在 本實施例中,是將最大硬度爲6 5 0HV以上者視爲合格( 〇)。 (2 )尺寸變形試驗(測定尺寸變形率的平均値及尺 寸變形率的差値) 從上述的退火材切出尺寸爲大約 40mmTx70mmWx 1 OOmmL的試驗片來當作尺寸變形測定用試驗片。對此試 驗片實施與上述(1 )的硬度試驗相同的熔體化處理之後 ,以到達最大硬度的溫度來進行回火處理。其次,以下述 的方式來測定「尺寸變形率的平均値」及「尺寸變形率的 差値」,依據下列的基準將這兩種評比都爲合格(〇)者 ,視爲具有優異的熱處理後的尺寸變形抑制性(合格)。 (2 -1 )測定尺寸變形率的平均値 針對上述的尺寸變形測定用試驗片(退火後熔體化處 理前)及回火後的試驗片,分別測定厚度、寬度、長度之 3個方向,求出熱處理前後的厚度的差値、寬度的差値、 及長度的差値,將這些的平均値(百分率)當作「尺寸變 形率的平均値」。本實施例中係將「尺寸變形率的平均値 」± 0 · 0 5 %以内者視爲合格(〇),將超過± 0.0 5 %者視爲不 -46- 200831682 合格(X)。 (2-2)測定尺寸變形率的差値 針對上述的尺寸變形測定用試驗片(退火後熔體化處 理前)及回火後的試驗片,分別測定厚度、寬度、長度之 3個方向,求出熱處理前後的厚度的差値、寬度的差値、 及長度的差値。將這些差値之中的最大値與最小値的差値 (百分率)當作「尺寸變形率的差値」。將尺寸變形率的 φ 差値爲0.08%以下者視爲合格(〇),將超過0.08%者視 爲不合格(X )。 (3 )焊接試驗(測定界限預熱溫度、以及HAZ軟化 幅度) 從上述的退火材切出尺寸大約爲 40mmT x45mmW x 7 5 mmL的試驗片來當作焊接用試驗片。對此試驗片,係與 上述(2 )的尺寸變形試驗同樣地實施熔體化處理及回火 處理。 Φ 其次,對於以這種方式所獲得的回火材實施加工,而 製得如第3圖(a )所示的板材。第3圖(a )的板材係具 有如第3圖(b )所示的溝部。接下來,使用具有如表3 所示的組成分(其餘部分:鉄及不可避免的雜質;單位: 質量% )的TIG焊條(日本優特客(:χ尹夕)株式會社所 製造的「TIG-Tectic 5HSS」、φ 2.4mm ),對於上述板材 的溝部依照下列條件實施增厚焊接。 焊接條件: 電流:150A、電壓:11V、焊接速度:9.5〜14cm/mm -47- 200831682 每一次焊接之間溫度:預熱溫度以下 入熱:7.1 〜1 〇.4kJ/cm 預熱:無預熱、有預熱(1 〇 〇 °C、2 0 〇 、3 0 0 、4 0 0 °C ) 此外,針對表2的No.22及No.23 (兩者都是模擬傳 統的高C高Cr鋼的鋼),爲了防止焊接時對於母材成分 的影響,係如第.4圖所示般地,將焊接材料加厚在開口面 (預堆邊焊)。實施預堆邊焊時,係採用下列組成分的預 堆邊焊焊接用TIG焊條〔株式會社神戸製鋼所製造的「 TGS-5 0」、Φ 2.4mm〕來進行單層增厚焊接。焊接條件係 與上述相同。 預堆邊焊焊接用TIG焊條的組成分:〇.〇9%C-0.93 % Si -1.9 5%Mn-0.00 9%P-0.0 1%S (其餘部分:鉄及不可避免的 雜質;單位:質量%) 以上述的方式改變預熱條件時,測定了在焊接金屬( DEPO)及HAZ部的雙方都不會發生龜裂的溫度的最低値 (界限預熱溫度)。界限預熱溫度愈低是意味著愈不容易 龜裂。在本實施例中,是將界限預熱溫度爲200°C以下者 視爲良好(〇),將超過200°C者是爲不良(X )。 又,爲了調查以上述的界限預熱溫度進行增厚焊接後 的試驗片剖面的硬度分布,從板厚的1 /4部位的焊接熔融 線(融合線)位置起至離開3 0mm的位置爲止,以每次 1 mm的節距連續地測定了硬度。將從焊接金屬中央部起至 硬度降低到600HV以下的位置爲止的距離當作「HAZ軟 -48- 200831682 化幅度」。爲了提供参考起見,在前述的第1圖中係 出ΗAZ軟化幅度的測定領域。在本實施例中,係將 軟化幅度爲6.5mm以下者評比成具有優異的焊接修補 〇),將超過6.5mm者評比成焊接修補性不佳(X) 〇 (4 )韌性試驗 針對上述的退火材實施了以下的熱處理。 熔體化處理(淬火處理):以約1 0 2 0〜1 〇 3 0 °C 120分鐘加熱-> 空氣中冷卻—時效處理(回火處理) 約400〜5 60 °C保持約3小時―空氣中冷卻或放冷。 其次,如第5圖所示般地,切出具有l〇mmR的 缺口部之試驗片來作爲韌性測定用試驗片(夏丕氏衝 驗片)。使用這種試驗片來實施夏丕氏衝撃試驗,並 定了在室溫時的吸收能量(夏丕氏衝撃値)。夏丕氏 試驗片係各採取3支,將這3支的平均値當作夏丕氏 値。在本實施例中,係將夏丕氏衝撃値爲15J以上者 成「韌性優異」。 將迨些結果顯不於表4〜5。 顯示 HAZ 性( 進行 :以 V型 撃試 且測 衝撃 衝撃 評比 -49- 200831682Co is used to increase the Ms point and reduce the effective elements of the residual Worthite iron, thereby increasing the hardness. In order to effectively exert the above effects, the Co amount is preferably 1% or more. However, if the addition is excessive, the cost and the like will increase, and it is preferable to select the upper limit as 10%. The upper limit of the amount of Co is -41 - 200831682 5.5% is better.麻田散铁转点点(M s点)g 1 70 °C Ms point = 550-361x[C]-3 9x[Mn]-35x[V]-2 0x[Cr] -17x[Ni] -10x [Cu] -5x( [Mo] + [W]) + 15x [ Co ) + 3 0x [ A1 ) {] is a meaning of the content (%) of each element} In the present invention, Ms The point is mainly used as an index for suppressing the dimensional deformation after hardness and heat treatment. If the Ms point is less than 170 ° C, the residual Worth iron will increase. If the high temperature aging treatment is not performed, the desired hardness cannot be obtained. It also causes expansion after heat treatment. The higher the Ms point, the better, about 23 ° C or better, 23 5 ° C or more, and 250 ° C or better. In addition, the upper limit is not particularly limited, but it is preferably about 350 °C in consideration of factors such as the effect of the addition of the above-mentioned elements constituting the Ms point, and the like. 320 ° C is better. Next, a method of producing a steel for a mold according to a second aspect of the present invention will be described. The production method of the present invention comprises the steps of: preparing a steel conforming to the above requirements, and performing the melt under the conditions of the following formula (5). Process the treatment of timeliness. ΤΑ-1 0 ^ T2 ^ TA + 1〇 (5) where ΤΑ - 0.29xT 1 -2.63x C Cu ] /[C]+ 225, -42- 200831682 τ 1 represents the melt temperature (° c), T2 is the representative aging temperature (°C). Specifically, after the steel conforming to the above requirements is first melted, hot forging is performed, followed by annealing (for example, after about 7 00 X: for 7 hours, at an average cooling rate of about 17 ° C / hr. After cooling in a furnace to about 400 ° C, cooling, softening, and then roughing into a predetermined shape by cutting or the like, and then performing melt processing and time-effects under the conditions of the above formula (5) Just handle it. As described above, in the second aspect of the present invention, the composition of the steel having a small amount of residual Worthite iron during the melt treatment is used, and Cu and C are further represented by the above formula (5). The mass ratio ([Cu ) / [ C ) ) is controlled by the relationship between the melt temperature Τ 1 and the aging temperature T2, and then it can be adjusted before the decomposition and expansion of the Worthite iron after the aging treatment. Since the hardness after aging reaches a peak, it is possible to simultaneously achieve both effects of dimensional deformation suppression and hardness after heat treatment. In general, in the production of steel for molds, the melt treatment is performed at a temperature of about 950 to 1150 ° C - aging treatment is performed at a temperature of about 400 to 530 ° C, According to the experimental results of the present inventors, it has been found that even if the melt treatment and the aging treatment are performed within the above range, the desired hardness is sometimes not obtained, and sometimes it is not sufficient. The dimensional deformation after heat treatment is suppressed (refer to the examples described later), and therefore, the above formula (5) is defined. When the above-described mechanism of the present invention is compared with the method of the above-mentioned Patent Document 2 (corresponding to the conventional high-C high-Cr steel), Patent Document 2 is the second drawing of the present invention as in -43-200831682 (corresponding to the patent document 2) As shown in Fig. 1 , in the case where the residual Worth iron has a certain degree of decomposition, the tempering process which makes the dimensional deformation at the time of tempering tend to zero is performed, and the present invention is relatively The tempering process is performed before the residual Worth Iron begins to decompose or just begins to decompose the subsequent temperature, and at this point, the two are different. That is, the present invention performs aging treatment at a lower temperature (specifically, a large enthalpy is a low temperature of about 50,000 ° C or less) as compared with the conventional high C high C r steel. According to the present invention, the aging treatment is not performed in the field where the dimensional deformation after heat treatment is intense (the A field in Fig. 3) as in Patent Document 2, but it is considered to be capable of generating a large amount of stable residual wavy. The aging treatment is performed in the field of the field iron (the field B in Fig. 3), and therefore, steel having a smaller degree of difference from the dimensional deformation of the steel disclosed in Patent Document 2 can be obtained. Further, by performing aging treatment in a relatively low temperature field in this manner, the stability of the residual Worthite iron can be improved, and the change over time of the remaining Worthite iron becomes small, so that dimensional deformation after heat treatment can also be obtained. The effect of the change over time becomes smaller. The aging temperature T2 is preferably TA ± 5 ° C as described above. Further, the melt temperature T1 can be used in the production of steel for a mold, which is lower than the range generally employed, so that the heat treatment can be less deformed. Specifically, it is preferable that the large enthalpy is in the range of 900 to 1150 ° C. The present invention is suitable in that the temperature of the melt treatment and the aging treatment is appropriately controlled in the above manner, and the time is not particularly limited. The limitation is as long as it is carried out under the conditions generally used in the manufacture of steel for molds. -44- 200831682, the smelting time (heating time) is controlled to the extent of 1 to 5 hours, and the aging time (holding time) ) Control can be done in 2 to 8 hours. [Examples] Hereinafter, the present invention will be specifically described by way of examples, but the present invention is not limited to the following examples, and may be applied with appropriate modifications within the scope applicable to the above-mentioned gist. It is possible that these are also included in the technical scope of the present invention. First, the implementation of the first aspect of the present invention will be described. Using the various steel types No. described in Tables 1 and 2, 150 kg of steel embryos were melted in a vacuum induction melting furnace, heated to about 900 to 1 150 ° C, and forged into two sheets of 40 mm Tx 75 mm W x about 2000 mm L steel sheets, and then about The average cooling rate of 60 ° C / hr was slowly cooled. After cooling to a temperature of 100 ° C or less, it was again heated to a temperature of about 850 ° C, and slowly cooled (annealed) at an average cooling rate of about 50 ° C /hr. The following tests (1) to (4) were carried out using various annealed materials obtained by the above methods. (1) Hardness test (measurement of maximum hardness) A test piece having a size of about 20 mm Tx 20 mm Wx 1 5 mmL was cut out from the above-mentioned annealed material to obtain a test piece for hardness measurement, and the test piece was subjected to the following heat treatment. Melt treatment (quenching treatment): at about 1〇2〇~l 〇30°C -45- 200831682 1 20 minutes of heating in air cooling - aging treatment (tempering treatment): about 400~5 60 ° C keeps about 3 hours - let cool. As described above, the hardness at the time of changing the tempering temperature in the range of about 400 to 5 60 ° C was measured by a Hardness Durometer (AVK, manufactured by AK AS HI, load: 5 kg), and the maximum hardness was found. (HV). In the present embodiment, those having a maximum hardness of 650 HV or more are regarded as pass ((). (2) Dimensional deformation test (measuring the difference between the average 値 and the dimensional deformation rate of the dimensional deformation ratio) A test piece having a size of about 40 mm Tx 70 mmW x 1 OO mmL was cut out from the above-mentioned annealed material to obtain a test piece for measuring the dimensional deformation. This test piece was subjected to the same melt treatment as the hardness test of the above (1), and then tempered at a temperature at which the maximum hardness was reached. Then, the "average 尺寸 of the dimensional deformation rate" and the "difference of the dimensional deformation rate" are measured in the following manner, and both of the evaluations are qualified according to the following criteria, and it is considered to have excellent heat treatment. Dimensional deformation inhibition (qualified). (2 -1 ) Measurement of the average dimensional deformation rate 値 The test piece for the dimensional deformation measurement (before the post-annealing melt treatment) and the tempered test piece were measured for three directions of thickness, width, and length, respectively. The difference 厚度 of the thickness before and after the heat treatment, the difference in width, and the difference in length were determined, and the average enthalpy (percentage) of these was taken as the "average 尺寸 of the dimensional deformation ratio". In the present embodiment, those who are "average 値 of the dimensional deformation rate" ± 0 · 0 5 % are regarded as qualified (〇), and those exceeding ± 0.0 5 % are regarded as not -46-200831682 qualified (X). (2-2) Measurement of the difference in dimensional deformation ratio The test piece for the dimensional deformation measurement (before the post-annealing melt treatment) and the test piece after the tempering were measured for three directions of thickness, width, and length, respectively. The difference 厚度 of the thickness before and after the heat treatment, the difference 宽度 of the width, and the difference in length were determined. The difference (percentage) between the maximum 値 and the minimum 这些 among these rates is taken as the "difference in the dimensional deformation rate". When the difference φ of the dimensional deformation ratio is 0.08% or less, it is regarded as pass (〇), and when it exceeds 0.08%, it is regarded as unacceptable (X). (3) Welding test (measurement limit preheating temperature and HAZ softening range) A test piece having a size of about 40 mmT x 45 mmW x 7.5 mm was cut out from the annealed material described above as a test piece for welding. The test piece was subjected to a melt treatment and a tempering treatment in the same manner as the dimensional deformation test of the above (2). Φ Next, the tempering material obtained in this manner is processed to obtain a sheet as shown in Fig. 3(a). The sheet material of Fig. 3(a) has a groove portion as shown in Fig. 3(b). Next, a TIG electrode (the other part: 鉄 and unavoidable impurities; unit: mass %) having the composition shown in Table 3 ("TIG" manufactured by Yokohama Co., Ltd., Japan) was used. -Tectic 5HSS", φ 2.4 mm), thickening welding was performed on the groove portion of the above-mentioned sheet material in accordance with the following conditions. Welding conditions: Current: 150A, voltage: 11V, welding speed: 9.5~14cm/mm -47- 200831682 Temperature between each welding: Preheating temperature below heat: 7.1 ~1 〇.4kJ/cm Preheating: no pre- Heat, preheating (1 〇〇 °C, 2 0 〇, 300 °, 300 ° C) In addition, for No. 22 and No. 23 of Table 2 (both are analog traditional high C high In order to prevent the influence on the base material composition during welding, the welding material is thickened on the opening surface (pre-stack welding) as shown in Fig. 4 . In the pre-stacking welding, the TIG welding rod ("GSS-5 0", Φ 2.4 mm) manufactured by Kobelco Co., Ltd. was used for the pre-stack welding. The welding conditions are the same as described above. Composition of TIG welding rod for pre-stack welding: 〇.〇9%C-0.93 % Si -1.9 5%Mn-0.00 9%P-0.0 1%S (the rest: 鉄 and inevitable impurities; unit: Mass %) When the preheating conditions were changed as described above, the lowest temperature (limit preheating temperature) at which the crack did not occur in both the weld metal (DEPO) and the HAZ portion was measured. The lower the preheating temperature of the boundary, the less likely it is to crack. In the present embodiment, it is considered that the limit preheating temperature is 200 °C or less, and it is considered to be good (X). In addition, in order to investigate the hardness distribution of the cross section of the test piece after thickening and welding by the above-described limit preheating temperature, from the position of the weld fusion line (fusion line) of the 1/4 portion of the sheet thickness to the position of leaving the 30 mm. The hardness was continuously measured at a pitch of 1 mm each time. The distance from the center of the weld metal to the position where the hardness is reduced to 600 HV or less is regarded as "HAZ soft -48- 200831682". For the purpose of reference, the field of measurement of the softening amplitude of ΗAZ is shown in the first drawing. In this embodiment, the softening width is 6.5 mm or less, which is superior to the welding repair 〇), and the 6.5 mm is evaluated as the poor weld repairing property (X) 〇 (4) Toughness test for the above annealing The following heat treatment was carried out on the material. Melt treatment (quenching treatment): heating at about 1 0 2 0~1 〇3 0 °C for 120 minutes -> cooling in air - aging treatment (tempering treatment) about 400~5 60 °C for about 3 hours ―Cooling or cooling in the air. Then, as shown in Fig. 5, a test piece having a notch portion of l〇mmR was cut out as a test piece for measuring toughness (Xia's test piece). This test piece was used to carry out the Chardonnay test and to determine the absorbed energy at room temperature (Xia's). The Xia's test film system took 3 pieces each, and the average of these 3 pieces was taken as Xia's. In the present embodiment, it is "excellent in toughness" in which Xia's is washed into 15J or more. These results are not shown in Tables 4 to 5. Display HAZ sex (for: V-type test and test rushing rushing evaluation -49- 200831682

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(0 Έ <〇 CVJ 1 -16 1 309 157 286 | in a> cm CO o 」20 CO eg 308 CM CM C7 342 ] ?si CO CM u> CO IO Csl CO S CM co QO esi 1—· oo C4 CM 288 | [Μ〇> [W]/2 «Μ °1 $ a CO CV{ CM s co Ol a CSJ 04 5 $ eg CM· S S 0.30 3.15 $ 1.2t 1 0.63 α> ο g 1.02 o ㈣ o O lo.so 0.33 0.02 60.20 .〇 2.30 〇 S 〇 o g g [Cr> [C] 18.03 8.46 0.94 3.02 Si· 严 s 1.23 s 1.24 1.19 co 〇{ 1.19 o <N 00 0.75 2.25 1.28 s Sj |質(單位:質量%) 2 ο ο ο ο O o o o o o o o o o' o O o o o o 〇 o ο ο ο ο o o o o o o o o o o o o o o o o o o 主 ο ο ο ο o o o o o o o o o o o o o o o o o o Μ ο ο ο ο o o o o o o o o o o o o o o o o o o 爱 ο ο ο ο o o o o o o o o o o o o o o o o o _〇 ο ο ο ο o o o o o o o o o o o o o o o o o 0.40 > 0.25 0.09 0.20 0.20 04 0.20 ca 0.20 0.22 0.20 0.20 0.20 0.20 0.20 0,20 0-20 0.22 0.20 0.20 I0.60 0.20 CO 0.005 0.007 0.004 0.004 0.004 0.004 0110 0.004 0.004 0.005 0.004 0.004 0.004 Γο,οοί 0.0041 0.004 0.004 0.004 0.003 0.004] 0.005 0.004 ο. 0.018 0.019 0.018 0.020 0.019 0.019 ^.019 0.019 0.018 0.018 0.018 0.019 0.018 0.018 0.018 0.018 0.020 0.019 0.019 ^019 [0.019] 账 S PER ο 10.00151 0.0007 10.0013] 0.0013 0.0015 0.0013 10.0014 10.0015 0.0013 0.0013 f 0,0015] 10.0013 10.00141 |a〇D14| 10.0013 0.0015 0.0013 0.0014 0.0015 10.0013] 0.0014 0.0013 親 K- ζ 0.0130 0.0068 0.0140 0.0131 ΓΟ0135 0.0142 0.0140 0.0141 0.0135 |aoi33| 0.0140 0.0131 10,0129 0.0135 0.0141 |a〇135| 0.0135 0.0132 0.0140 | 0.01411 0.01381 0.0133 S 0.35 0.39 0.02 0.02 0.02 0.02 0.02 0.02 0.02 0.02 0,02 0.02 0.02 0.02 0.02 0.02 0.02 0.02 0.20 2.00 0.02 0.02 醱 Φ •鍍 ο g 0.91 8 8 iq a o S! 5 S 5 8 8 esi 0.20 2.15 S S t ζ D.08 0.44 2.97 2.95 M 2.98 οί 2.98 2.98 网 6.10 2.98 m 0,05 2.97 CM c> 2.99 2.97 2.98 2.99 ㈣ 2.96 δ 0.05 0.40 ο CO 1 3.02 s 3.03 3.01 3.02 o o 3.02 0.98 0.05 3 CO 3.01 3.03 3.01 3.02 1 3.03 3.02 3.01 0.05 0.33 , 1.02 o p g 0.48 2.05 p 1.02 1.02 w g 0.05 w 1.01 p 1.02 p 'T— w g ό 12.10 8.38 「4.93 ㈣ 4.96 4.94 4.90 4.97 4.96 4.96 4.93 4.98 4.93 2.99 o a> 4.94 4.95 4.95 0.42 0·60 0.28 0.28 0.28 2.10 0.28| 0.28 0.29 0.29 0.28 0.26 0.27 0.27 0.27 0.26 0.28 0.28 0.27 L^5j 0.28 0.26 <〇 0.35 1.06 C>l <〇 ㈣ 「2.02 IX> CO to CO 1.33 1.33 €M C> 1.32 1.32 €*>· 1.39 1» c> CNi co s M CM 〇 ο $ ο <C> 0.25 0.25 0.24 0.25 0.25 0.25 0.24 0.25 0.24 0.24 H 0.25 0.25 0.25 0.26 M 0.25 0.25 i C0 CM ir> CM 5 S S Jo S 8 S S 〇 5 o -51 - 200831682 [表3] 其餘部分:鐵以及不可避免的雜質(單位:質量%) C Si Μη V Ni Cr Mo Cu Al P S V 0.25 0.40 1.40 0.2 3.0 5.0 2.3 3.0 1.0 0.02 0.005 0.2 [表4](0 Έ <〇CVJ 1 -16 1 309 157 286 | in a> cm CO o ”20 CO eg 308 CM CM C7 342 ] ?si CO CM u> CO IO Csl CO S CM co QO esi 1—· oo C4 CM 288 | [Μ〇> [W]/2 «Μ °1 $ a CO CV{ CM s co Ol a CSJ 04 5 $ eg CM· SS 0.30 3.15 $ 1.2t 1 0.63 α> ο g 1.02 o (4) o O lo.so 0.33 0.02 60.20 .〇2.30 〇S 〇ogg [Cr> [C] 18.03 8.46 0.94 3.02 Si· Strict s 1.23 s 1.24 1.19 co 〇{ 1.19 o <N 00 0.75 2.25 1.28 s Sj | Unit: mass%) 2 ο ο ο ο O ooooooooo' o O oooo 〇o ο ο ο ο oo oooooooooooooooooo master ο ο ο oooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooooo ; 0.25 0.09 0.20 0.20 04 0.20 ca 0.20 0.22 0.20 0.20 0.20 0.20 0.20 0,20 0-20 0.22 0.20 0.20 I0.60 0.20 CO 0.005 0.007 0.004 0.004 0.004 0.004 0110 0.004 0.004 0.005 0.004 0.004 0.004 Γο,οοί 0.0041 0. 004 0.004 0.004 0.003 0.004] 0.005 0.004 ο. 0.018 0.019 0.018 0.020 0.019 0.019 ^.019 0.019 0.018 0.018 0.018 0.019 0.018 0.018 0.018 0.018 0.020 0.019 0.019 ^019 [0.019] Account S PER ο 10.00151 0.0007 10.0013] 0.0013 0.0015 0.0013 10.0014 10.0015 0.0013 0.0013 f 0,0015] 10.0013 10.00141 |a〇D14| 10.0013 0.0015 0.0013 0.0014 0.0015 10.0013] 0.0014 0.0013 Pro K- ζ 0.0130 0.0068 0.0140 0.0131 ΓΟ0135 0.0142 0.0140 0.0141 0.0135 |aoi33| 0.0140 0.0131 10,0129 0.0135 0.0141 |a〇135| 0.0135 0.0132 0.0140 | 0.01411 0.01381 0.0133 S 0.35 0.39 0.02 0.02 0.02 0.02 0.02 0.02 0.02 0.02 0,02 0.02 0.02 0.02 0.02 0.02 0.02 0.02 0.20 2.00 0.02 0.02 酦Φ • Plated ο g 0.91 8 8 iq ao S! 5 S 5 8 8 Esi 0.20 2.15 SS t ζ D.08 0.44 2.97 2.95 M 2.98 οί 2.98 2.98 net 6.10 2.98 m 0,05 2.97 CM c> 2.99 2.97 2.98 2.99 (4) 2.96 δ 0.05 0.40 ο CO 1 3.02 s 3.03 3.01 3.02 oo 3.02 0.98 0.05 3 CO 3.01 3.03 3.01 3.02 1 3.03 3.02 3.01 0.05 0.33 , 1.02 opg 0.48 2.05 p 1.02 1.02 wg 0.05 w 1.01 p 1.02 p 'T- wg ό 12.10 8.38 "4.93 (4) 4.96 4.94 4.90 4.97 4.96 4.96 4.93 4.98 4.93 2.99 o a> 4.94 4.95 4.95 0.42 0·60 0.28 0.28 0.28 2.10 0.28| 0.28 0.29 0.29 0.28 0.26 0.27 0.27 0.27 0.26 0.28 0.28 0.28 0.27 L^5j 0.28 0.26 <〇0.35 1.06 C>l <〇(4) "2.02 IX> CO to CO 1.33 1.33 €M C> 1.32 1.32 €*>· 1.39 1» c> CNi co s M CM 〇ο $ ο <C> 0.25 0.25 0.24 0.25 0.25 0.25 0.24 0.25 0.24 0.24 H 0.25 0.25 0.25 0.26 M 0.25 0.25 i C0 CM ir> CM 5 SS Jo S 8 SS 〇5 o -51 - 200831682 [Table 3] The rest: Iron and inevitable impurities (unit: mass%) C Si Μη V Ni Cr Mo Cu Al PSV 0.25 0.40 1.40 0.2 3.0 5.0 2.3 3.0 1.0 0.02 0.005 0.2 [Table 4]

No. 最大硬度 HAZ 軟化幅度 界限預熱溫度 尺寸變形率 的平均値 尺寸變形率 的差値 夏丕氏衝擊値 HV mm °C % % J 1 685 5.1 100 0.01 0.04 22 2 702 5.3 100 -0Ό1 0.05 20 3 710 4.8 25 0 0.06 19 4 715 4.5 100 0.02 0.05 17 5 713 4.6 100 -0.02 0.04 18 6 655 6Λ too 0.02 0.07 27 7 663 5.9 too 0.01 0.05 24 8 679 5.6 100 0 0.05 22 9 712 6.2 too 0.02 0.06 17 10 682 5.6 100 0 0.04 20 11 660 6.4 100 0.01 0.04 25 12 688 5.0 100 -0.05 0.08 22 13 683 5.1 100 0.01 0.04 35 14 683 5.0 100 0.01 0.04 33 15 685 5.1 too 0.01 0.04 33 16 680 5.0 too 0.01 0.04 32 17 710 5.2 200 0.03 0.05 17 18 720 5.3 200 0.03 0.04 16 19 685 5.1 200 Q.D3 0.05 22 20 680 5.3 200 0.04 0.05 21 21 722 4.9 200 0 0.03 25 -52· 200831682 [表5]No. Maximum hardness HAZ Softening range limit Preheating temperature Dimensional deformation rate Average 値 Size Deformation rate difference 値 丕 値 値 HV mm °C % % J 1 685 5.1 100 0.01 0.04 22 2 702 5.3 100 -0Ό1 0.05 20 3 710 4.8 25 0 0.06 19 4 715 4.5 100 0.02 0.05 17 5 713 4.6 100 -0.02 0.04 18 6 655 6Λ too 0.02 0.07 27 7 663 5.9 too 0.01 0.05 24 8 679 5.6 100 0 0.05 22 9 712 6.2 too 0.02 0.06 17 10 682 5.6 100 0 0.04 20 11 660 6.4 100 0.01 0.04 25 12 688 5.0 100 -0.05 0.08 22 13 683 5.1 100 0.01 0.04 35 14 683 5.0 100 0.01 0.04 33 15 685 5.1 too 0.01 0.04 33 16 680 5.0 too 0.01 0.04 32 17 710 5.2 200 0.03 0.05 17 18 720 5.3 200 0.03 0.04 16 19 685 5.1 200 Q.D3 0.05 22 20 680 5.3 200 0.04 0.05 21 21 722 4.9 200 0 0.03 25 -52· 200831682 [Table 5]

Να. 最大硬度 HAZ^化幅度 界限預熱溫度 尺寸變形率 的卒均値 尺寸變形率 的差値 夏丕氏衝擊値 HV mm °C % % J 22 690 11.0 400 0.06 0.15 10 23 720 10.5 400 0.01 0.12 13 24 645 7.0 25 -0.02 0.04 35 25 715 5.2 300 0.06 0.10 14 26 725 4.5 too 0.05 0.09 12 27 722 5.1 100 0.06 0.08 15 28 688 5.3 300 0.01 0Ό4 19 29 638 8.4 100 0.04 0Ό5 33 30 700 4.6 too -0.02 0.09 19 31 640 7.5 100 0.03 0.04 20 32 646 6.3 100 0.06 0.08 40 33 645 6.6 100 0.05 0.04 37 34 620 7.5 100 0.06 003 30 35 625 7.3 100 0.06 0.04 29 36 630 7.0 100 0.06 0.03 33 37 661 7.0 too 0.01 0.03 19 38 647 6.5 100 0Ό2 0.05 39 39 683 4.9 100 -0.06 0Ό9 21 40 629 6.9 100 0.05 0.05 35 41 723 5.0 100 0.03 0.10 13 42 640 7.0 too 0.02 0.05 35 43 630 7.7 100 0.02 0.04 33 從表4及表5可以獲得以下的考察結果。 表4的No. 1〜21分別係使用了符合本發明的所有要 件之表1的N 0.1〜2 1之例’全部都是不僅硬度很高’具 有優異的熱處理後的尺寸變形抑制性及焊接修補性之外’ 韌性也高,界限預熱溫度也在200 °C以下屬於良好等級。 相對於此,表5的N 〇 · 2 2〜4 3分別是使用了未符合本 發明所界定的要件的其中一種要件之表2的N 〇 . 2 2〜4 3之 例,具有以下的缺失。 -53- 200831682 表5的No.22及23都是使用了模擬傳統的高C高Cr 鋼之表2的No.22及23之例,因爲〔Cr〕與〔C〕的乘積 很大,Ms點很低,HAZ軟化幅度及尺寸變形率的差値都 增加了。此外,因爲這些鋼種是回火溫度愈低的話,硬度 就變得愈高,所以將使用上述鋼種時的回火溫度選定爲 5 1 〇 °C,並且測定各種特性。 表5的No.24係使用了 C量很少的表2的No.24之例 ,可看出硬度的降低與HAZ軟化幅度的增加。 表5的No.25係使用了 C量很多,〔C〇與〔C〕的 乘積很大,Ms點很低之表2的Νο·25之例,熱處理後的 尺寸變形抑制性不佳。 表5的No.26係使用了 Si量很多之表2的No.26之 例,熱處理後的尺寸變形率的平均値雖然良好,但是尺寸 變形率的差値卻很大。 表5的No .27係使用了 Μη量很多,Ms點很低的表2 的No. 27之例,熱處理後的尺寸變形率的平均値很大。 表5的No.28係使用了 S量很多之表2的No.28之例 ’界限預熱溫度變高,有發生焊接龜裂之虞慮。 表5的No.29係使用了Al量很少的表2的No·29之 例,可看出硬度的降低與HAZ軟化幅度的增加。 表5的Νο·30係使用了 A1量很多的表2的No.30之 例,熱處理後的尺寸變形率的平均値雖然良好,但是尺寸 變形率的差値卻很大。 表5的Νο·3 1係使用了 Ni量很少,〔Cu〕/〔 Ni〕的 _ 54 - 200831682 比値很大的表2的Νο·31之例,可看出硬度的降 軟化幅度的增加。 表5的No.32係使用了 Ni量很多的表2的 例,硬度會降低而且熱處理後的尺寸變形率的平 加了。 表5的Νο·33係使用了 Cu量很少,〔Cu〕/ 比値很小的表2的No · 3 3之例,可看出硬度的降 軟化幅度的增加。 表5的No.34係模擬並未實質地添加Cu量 ,係使用了 Cu量只有0.05%極端地少,〔Cu〕/ 比値很小之表2的No. 34,所以可看出硬度的降> 軟化幅度的增加。此外,熱處理後的尺寸變形率 也增加了。 表5的No.35係模擬了並未實質地添加Ni 例,係使用了 Ni量只有〇· 05 %極端地少,〔Cu : 的比値很小之表2的No · 3 5,因此除了可看出硬 與HAZ軟化幅度的增加之外,熱處理後的尺寸 平均値也增加了。 表5的No.36係模擬了並未實質地添加A1 例,係使用了 A1量只有〇 · 〇 5 %極端地少之表2的 因此除了可看出硬度的降低與HAZ軟化幅度的 ,熱處理後的尺寸變形率的平均値也增加了。 表5的No.3 7,Cu量及Ni量雖然符合本發 ,但是係使用了〔 C u〕/〔 N i〕的比値很小之表2 低與HAZ Νο·32 之 均値也增 ’〔Ni〕的 低與HAZ 的鋼之例 〔N i〕的 低與HAZ 的平均値 量的鋼之 〕/〔 Ni〕 度的降低 變形率的 量的鋼之 f N 〇 . 3 6, 增加之外 明的範圍 白勺N 〇 · 3 7 -55- 200831682 之例,HAZ軟化幅度有所增加。 表5的Νο·38係使用了 Cr量很少之表2的No.38之 例,硬度有所降低。 表5的>^〇.39係使用了(:1:量很多之表2的:^〇.39之 例,熱處理後的尺寸變形抑制性不佳。 表5的Νο·40係使用了〔 Mo〕+ 〇.5x〔 W〕的合計量 很少之表2的Νο·40之例,可看出硬度的降低與HAZ軟 化幅度的增加。 表5的Ν 〇 · 4 1係使用了〔 Μ 〇〕+ 〇 · 5 X〔 W〕的合計量 很多之表2的No.41之例,熱處理後的尺寸變形率的平均 値雖然良好,但是尺寸變形率的差値卻很大。 表5的No ·42係使用了 Ti量很多之表2的No .42之 例,可看出硬度的降低與HAZ軟化幅度的增加。 爲了提供参考起見,在第7圖中將依照前述的方法所 獲得的硬度分布的曲線標示出來。圖中,本發明鋼() 係表示表1的Ν 〇 · 4的結果,S KD 1 1的傳統鋼(♦)係表 示表2的No· 22的結果。由第7圖所示的結果可得知:使 用本發明鋼的話,可較之傳統鋼,更明顯地抑制焊接後的 HAZ軟化。 接下來,說明本發明的第2態樣的實施例如下。 使用表6所記載的鋼種A〜K,在真空感應熔解爐中 熔製150kg的鋼胚之後,加熱到約900〜1150°C,鍛造成 兩片40mmTx75mmWx約2000mmL的鋼板,然後,以約60 它/hr的平均冷卻速度慢慢地進行冷卻。冷卻到達1 00 °C以 -56- 200831682 下的溫度之後,再度加熱到約8 5 0 °C的名 的平均冷卻速度慢慢地進行冷卻(進行 使用以上述的方式所製得的各退4 )〜(2 )的試驗。 (1 )硬度試驗(測定硬度) 從上述的退火材切出尺寸大約爲 1 5 m m L的試驗片來當作硬度測定用試驗 φ 以表2所記載的條件實施熔體化處理— 處理之後,予以放冷。熔體化處理時間 處理時間約3時間。 利用畢氏硬度計(AKAS HI社製造 5kg )測定時效處理後的硬度,以調查; 實施例中,係將硬度爲650HV以上者視 (2 )尺寸變形試驗(測定尺寸變 寸變形率的最大値) # 從上述的退火材切出尺寸大約爲 lOOmmL的試驗片來當作尺寸變形測定 • 以表2所記載的條件實施熔體化處理— 理之後,予以放冷。接下來,以下列的 變形率的平均値」及「尺寸變形率的最 基準,將這些項的評比都爲合格) 的尺寸變形抑制性優異(合格)。 (2 -1 )測定尺寸變形率的平均値 昆度,以約50°C/hr 退火)。 〔材,進行下列(1 20mmT x20mmW χ 片,對此試驗片, 空氣中冷卻—時效 約120分鐘,時效 的規格 AVK,荷重 硬度(HV )。在本 •爲合格(〇 )。 形率的平均値及尺 〖40mmT χ 70mm W χ 用試驗片,然後, •風扇吹冷時效處 方式來測定「尺寸 大値」,依照下列 者,視爲熱處理後 (平均尺寸變形率 -57- 200831682 針對上述的尺寸變形測定用試驗片(退火後熔體 理前)及時效後的試驗片,分別測定厚度、寬度、長 3個方向,求出熱處理前後的厚度的差値、寬度的差 及長度的差値,將這些差値的平均値(百分率)當作 寸變形率的平均値」。在本實施例中,係將「尺寸變 的平均値」±0 · 〇 3 %以内者視爲合格(〇),將超過± 0 者視爲不合格(X )。 Φ ( 2-2 )測定尺寸變形率的最大値(最大尺寸變 ) 針對上述的尺寸變形測定用試驗片(退火後熔體 理前)及時效後的試驗片,分別測定厚度、寬度、長 3個方向,求出熱處理前後的厚度的差値、寬度的差 及長度的差値,將這些的最大値的絕對値(百分率) 「尺寸變形率的最大値」。將尺寸變形率的最大 0.05%以下者視爲合格(〇),將超過0.05%者視爲 # 格(X )。 (2-3 )測定尺寸變形率的差値 _ 爲了提供参考起見,也測定了上述本發明的第1 的説明中所述的「尺寸變形率的差値」。具體而言, 於上述的尺寸變形測定用試驗片(退火後熔體化處理 及時效後的試驗片,分別測定厚度、寬度、長度的3 向,求出熱處理前後的厚度的差値、寬度的差値、及 的差値。將這些當中的最大値與最小値的差値(百分 當作「尺寸變形率的差値」。將尺寸變形率的差 化處 度的 値、 「尺 形率 .03% 形率 化處 度的 値、 當作 値爲 不合 態樣 針對 前) 個方 長度 率) 値在 -58· 200831682Να. Maximum hardness HAZ^ Width limit Preheating temperature Dimensional deformation rate 卒 値 値 变形 变形 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値 値13 24 645 7.0 25 -0.02 0.04 35 25 715 5.2 300 0.06 0.10 14 26 725 4.5 too 0.05 0.09 12 27 722 5.1 100 0.06 0.08 15 28 688 5.3 300 0.01 0Ό4 19 29 638 8.4 100 0.04 0Ό5 33 30 700 4.6 too -0.02 0.09 19 31 640 7.5 100 0.03 0.04 20 32 646 6.3 100 0.06 0.08 40 33 645 6.6 100 0.05 0.04 37 34 620 7.5 100 0.06 003 30 35 625 7.3 100 0.06 0.04 29 36 630 7.0 100 0.06 0.03 33 37 661 7.0 too 0.01 0.03 19 38 647 6.5 100 0Ό2 0.05 39 39 683 4.9 100 -0.06 0Ό9 21 40 629 6.9 100 0.05 0.05 35 41 723 5.0 100 0.03 0.10 13 42 640 7.0 too 0.02 0.05 35 43 630 7.7 100 0.02 0.04 33 From Table 4 and Table 5 The following findings can be obtained. Nos. 1 to 21 of Table 4 are examples of N 0.1 to 2 1 using Table 1 in accordance with all the requirements of the present invention. "All of them are not only high in hardness", and have excellent dimensional deformation inhibition after heat treatment and welding. In addition to the repairability, the toughness is also high, and the preheating temperature of the boundary is also a good grade below 200 °C. On the other hand, N 〇 · 2 2 to 4 3 of Table 5 are examples of N 〇. 2 2 to 4 3 of Table 2 which are not one of the requirements of the requirements defined by the present invention, and have the following defects. . -53- 200831682 No. 22 and 23 of Table 5 are examples of No. 22 and 23 of Table 2 which simulates a conventional high-C high-Cr steel because the product of [Cr] and [C] is large, Ms The point is very low, and the difference between the HAZ softening range and the dimensional deformation rate is increased. Further, since these steel grades have a lower tempering temperature, the hardness becomes higher. Therefore, the tempering temperature when the above steel grade is used is selected to be 5 1 〇 ° C, and various characteristics are measured. In No. 24 of Table 5, the example of No. 24 of Table 2 having a small amount of C was used, and the decrease in hardness and the increase in the degree of softening of HAZ were observed. In No. 25 of Table 5, the amount of C is large, and the product of [C〇 and [C] is large, and the Ms point is very low. The example of Νο·25 of Table 2 has poor dimensional deformation inhibition after heat treatment. In No. 26 of Table 5, the No. 26 of Table 2 having a large amount of Si was used, and although the average 尺寸 of the dimensional deformation ratio after the heat treatment was good, the difference in the dimensional deformation ratio was large. In No. 27 of Table 5, the example of No. 27 of Table 2 in which the amount of Μη is large and the Ms point is very low is used, and the average 値 of the dimensional deformation ratio after heat treatment is large. No. 28 in Table 5 is an example of No. 28 in Table 2 in which the amount of S is large. The limit preheating temperature is high, and there is a concern that weld cracking may occur. In No. 29 of Table 5, the No. 29 of Table 2 in which the amount of Al was small was used, and the decrease in hardness and the increase in the HAZ softening range were observed. In the case of No. 30 of Table 2 in which the amount of A1 is large, the average enthalpy of dimensional deformation ratio after heat treatment is good, but the difference in dimensional deformation ratio is large. In Table 5, Νο·3 1 uses a small amount of Ni, and [Cu]/[Ni] _ 54 - 200831682 is an example of Νο·31 of Table 2 which is very large, and it can be seen that the hardness is softened. increase. In the example No. 32 of Table 5, the example of Table 2 having a large amount of Ni was used, and the hardness was lowered and the dimensional deformation ratio after the heat treatment was increased. In the case of Νο·33 in Table 5, the amount of Cu was small, and the case of No. 3 of Table 2 in which [Cu] / 値 was small was small, and the increase in the softening degree of hardness was observed. In the No. 34 series of Table 5, the amount of Cu was not substantially added, and No. 34 of Table 2, which has an extremely small amount of Cu of 0.05% and a small amount of [Cu] / is used, is used. Drop > Increase in softening. In addition, the dimensional deformation rate after heat treatment is also increased. No. 35 in Table 5 simulates the case where Ni is not substantially added, and the amount of Ni is only 〇·05% is extremely small, and the ratio of Cu: is smaller than that of No. 3 of Table 2, so It can be seen that in addition to the increase in hardness and HAZ softening amplitude, the average size of the heat treatment after heat treatment is also increased. No. 36 in Table 5 simulates the case where A1 is not substantially added, and the amount of A1 is only 〇·〇5% which is extremely small in Table 2, so that the hardness reduction and the HAZ softening range can be seen, heat treatment The average 値 of the dimensional deformation rate also increases. In Table 5, No. 3, the amount of Cu and the amount of Ni are in accordance with the present invention, but the ratio of [C u]/[N i] is small, and the uniformity of HAZ Νο·32 is also increased. '[Ni] is lower than the case of HAZ steel [N i] and the average amount of HAZ is steel] / [Ni] degree of reduction of deformation rate of steel f N 〇. 3 6, increase In the case of N 〇· 3 7 -55- 200831682, the HAZ softening range has increased. In the case of No. 38 of Table 2 in which the amount of Cr is small, the hardness is lowered. In the example of Table 2: (1: a large amount of Table 2: ^〇.39, the dimensional deformation inhibition after heat treatment is not good. The Νο·40 series of Table 5 is used [ The total amount of Mo]+ 〇.5x[ W] is very small. In the case of Νο·40 of Table 2, it can be seen that the hardness is reduced and the HAZ softening amplitude is increased. Table 5 of Ν 〇 · 4 1 is used [ Μ 〇]+ 〇· 5 X [W] The total number of the No. 41 in Table 2 is good, although the average 尺寸 of the dimensional deformation ratio after heat treatment is good, but the difference in dimensional deformation ratio is large. The No. 42 system used the example of No. 42 of Table 2 in which the amount of Ti was large, and the decrease in hardness and the increase in the degree of softening of the HAZ were observed. For the sake of reference, the method according to the foregoing method will be obtained in FIG. The curve of the hardness distribution is indicated. In the figure, the steel () of the present invention represents the result of Ν 〇 4 of Table 1, and the conventional steel (♦) of S KD 1 1 represents the result of No. 22 of Table 2. As can be seen from the results shown in Fig. 7, when the steel of the present invention is used, the HAZ softening after welding can be more significantly suppressed than that of the conventional steel. The second aspect of the invention is as follows. Using the steel grades A to K described in Table 6, 150 kg of steel embryos are melted in a vacuum induction melting furnace, and then heated to about 900 to 1150 ° C, forging two pieces of 40 mm Tx 75 mm Wx. A steel plate of about 2000 mmL is then slowly cooled at an average cooling rate of about 60 hr / hr. After cooling to 100 ° C at a temperature of -56-200831682, it is heated again to a temperature of about 850 °C. The average cooling rate is gradually cooled (the test using each of the retreats 4 to 2) obtained in the above manner is performed. (1) Hardness test (measurement hardness) The size of the annealed material is approximately The test piece of 1 5 mm L was used as the test for hardness measurement φ. The melt treatment was carried out under the conditions described in Table 2. After the treatment, it was allowed to cool. The time for the treatment of the melt treatment was about 3 times. The hardness after the aging treatment was measured by AKAS HI, and the hardness was 650 HV or more in the examples. (2) The dimensional deformation test (the maximum 値 of the dimensional change rate) Annealed material cut out size For the test piece of 100 mmL, it was measured as a dimensional deformation. After the melt treatment was carried out under the conditions described in Table 2, it was allowed to cool. Next, the average deformation rate of the following deformation rate and the "size deformation rate" In the most standard, the evaluation of the dimensional deformation of these items is acceptable. (2 -1 ) The average 値 degree of the dimensional deformation rate is measured and annealed at about 50 ° C / hr.) The following (1 20mmT x 20mmW , piece, this test piece, air cooling - aging for about 120 minutes, aging specification AVK, load hardness (HV). In this • is qualified (〇). The average 値 and the rule of the shape rate 〖40mmT χ 70mm W χ test piece, then, • fan cooling aging method to determine the "size 値", according to the following, considered as heat treatment (average size deformation rate -57- 200831682 The test piece for measuring the dimensional deformation (pre-annealed before melting) was measured for thickness, width, and length in three test directions, and the difference in thickness and width between before and after heat treatment were determined. For the difference in length, the average 値 (percentage) of these rates is taken as the average 値 of the deformation rate. In this embodiment, the average 値 of the dimensional change is ±0 · 〇3 % or less. Qualified (〇), the one exceeding ± 0 is regarded as unacceptable (X). Φ ( 2-2 ) The maximum 値 of the dimensional deformation rate (maximum dimensional change) The test piece for the above dimensional deformation measurement (melted after annealing) Before and after the test, the thickness, width, and length of the test piece were measured, and the difference 厚度, the difference in width, and the difference in length of the thickness before and after the heat treatment were determined, and the absolute enthalpy of the maximum enthalpy (%) ) "ruler The maximum deformation rate is 値". The maximum value of the deformation rate of 0.05% or less is regarded as qualified (〇), and the case where more than 0.05% is regarded as #格(X). (2-3) The difference of the dimensional deformation rate is measured _ In order to provide a reference, the "dimensional deformation rate difference" described in the first aspect of the present invention is also measured. Specifically, the above-described dimensional deformation measurement test piece (melting after annealing) In the test piece after the time-effect, the thickness, the width, and the length of the three directions were measured, and the difference in thickness, the difference in width, and the difference in thickness before and after the heat treatment were determined. The difference between the maximum 値 and the minimum 这些 among these (Percentage is regarded as "the difference in dimensional deformation rate". The difference between the dimensional deformation rate and the "shape rate.03% of the shape rate" is regarded as the ambiguity. ) Square length rate) - at -58· 200831682

0.08%以下者視爲合格(〇),將超過0.08%者視爲不合 格(X )。 將這些結果顯示於表7。 -59- 200831682Those below 0.08% are considered qualified (〇), and those exceeding 0.08% are considered as unqualified (X). These results are shown in Table 7. -59- 200831682

12.041 12,001 14.001 7.50 I 4,44 I 0.03 I 0.40 I 3.92 I 16.001 0> 296 CO CM 303 278 ΙΟ CM τ— ΙΟ €Μ -261 -16 308 278 [Mo]+ m/2 1.80 1.22 1.80 1.22 0.90 OJ CM· τ— ΙΔ^ a 1.02 Ρ 0.52 0.83 卜 Ρ 2.00 0.63 0.91 0.33 [Cr]* [C] S S 〇> ιηχ S CO 2.00 18.03 8.46 « CVI 1,23 m:Mi%) ο ο ο Ο .〇 to ο ο ο ο ο ο ο ο Ο ο ο ο ο ο ο ο 生 ο ο ο ο ο ο ο ο ο ο ο Μ ο • ο ο ο ο ο ο ο ο ο ο 受 ο ο ο ο Ό ο ο ο ο ο ο ο ο ο Ο ο ο ο ο ο ο > ό 0.20 ▼— CM· ο 0.20 0.20 0.20 0.25 0.09 0.21 ο nmr tof 00 0.004 0.005 0·004 0.004 0.005 0.004 0.004 0.005 0·007 0Ό04] 0.004 其餘部分:鐵以及不可避免的雜ί CL 0.018 0.020 0.019 0.019 0.020 0.019 0.019 0.018 0.019 0.019 0.019 Ο 0.0013 0.00141 0.0013 0.0013 0.0014 0.0013 0.0013 0.0015 0.0007 0.00131 0.0013 ζ 0.0148 0.01411 0.0129 0.0140 I 0.0141 0.0140 0-0140 O.Q13〇| 0,00681 0.0131 0.0131 0.02 ο 0.02 0.02 ο 0.02 ο 0.35 0.39 0.02 0.02 S S 5 S S 5 ①· ο 0:91 5 2 Μ 2.98 2.99 Μ 3.00 \2Μ\ 1.00 0.08 0.44 2.98 2.98 d 1 3.00 ㈣ Μ 3.50 3.00 2-00 0.05 0.40 0.98 4.00 < 1.09 ρ 1.02 Μ 〇 τ— S 0.35 0.05 0.33 Μ 1.02 ό 4,95 4.96 4.97 4.99 to 0> 4,45 4.45 12.10 8.38 4.93 4.93 0.28 0.28 0.29 0.29 0.28 L^sj 0.42 0.60 0.26 0.26 ω 1.32 1-39 Μ CO 1.39 Μ ιη CO 0.35 1.06 Μ 1.33 ο 0.25 0.25 0.24 0.25 0.25 0.40 0.45 1.49 1.01 Μ 0.25 鋼種 < CQ ο ο Ιϋ U. ο X12.041 12,001 14.001 7.50 I 4,44 I 0.03 I 0.40 I 3.92 I 16.001 0> 296 CO CM 303 278 ΙΟ CM τ— ΙΟ €Μ -261 -16 308 278 [Mo]+ m/2 1.80 1.22 1.80 1.22 0.90 OJ CM · τ— ΙΔ^ a 1.02 Ρ 0.52 0.83 Ρ 2.00 0.63 0.91 0.33 [Cr]* [C] SS 〇> ιηχ S CO 2.00 18.03 8.46 « CVI 1,23 m:Mi%) ο ο ο Ο .〇to ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο ο : iron and inevitable miscellaneous CL 0.018 0.020 0.019 0.019 0.020 0.019 0.019 0.018 0.019 0.019 0.019 Ο 0.0013 0.00141 0.0013 0.0013 0.0014 0.0013 0.0013 0.0015 0.0007 0.00131 0.0013 ζ 0.0148 0.01411 0.0129 0.0140 I 0.0141 0.0140 0-0140 O.Q13〇| 0, 00681 0.0131 0.0131 0.02 ο 0.02 0.02 ο 0.02 ο 0.35 0.39 0.02 0.02 SS 5 SS 5 1· ο 0:91 5 2 Μ 2.98 2.99 Μ 3.00 \2Μ\ 1.00 0.08 0.44 2.98 2.98 d 1 3.00 (4) Μ 3.50 3.00 2-00 0.05 0.40 0.98 4.00 < 1.09 ρ 1.02 Μ 〇τ — S 0.35 0.05 0.33 Μ 1.02 ό 4,95 4.96 4.97 4.99 to 0> 4,45 4.45 12.10 8.38 4.93 4.93 0.28 0.28 0.29 0.29 0.28 L^sj 0.42 0.60 0.26 0.26 ω 1.32 1-39 Μ CO 1.39 Μ ιη CO 0.35 1.06 Μ 1.33 ο 0.25 0.25 0.24 0.25 0.25 0.40 0.45 1.49 1.01 Μ 0.25 steel type < CQ ο ο Ιϋ U. ο X

-60- 200831682 [表7]-60- 200831682 [Table 7]

No. 鋼種 熔體化 溫度 TK°C) 時效溫度T2(〇C) 硬度 (HV) 尺寸變形率(%) ΤΑ* 本發明範圍 (TA±10) 實測値 平均値 最大値 差値 44 A 1020 489 479-499 490 675 0.010 0.030 0.040 45 950 469 459-479 470 678 0.000 0.020 0.040 46 1020 489 479-499 520 640 0.035 0.060 0.050 47 1020 489 479-499 460 642 0.035 0.060 0.050 48 B 1020 489 479-499 490 685 0.010 0.030 0.040 49 950 469 459-479 470 683 0.000 0.020 0.040 50 1020 489 479-499 520 652 0.040 0.065 D.050 51 1020 489 479-499 460 649 0.035 0.060 0.050 52 C 1020 504 494-514 500 655 0.020 0.050 0.060 53 950 484 474-494 485 654 0.010 0.045 0.070 54 1020 504 494-514 530 625 0.030 0.065 0.070 55 1020 504 494-514 460 620 0.035 0.070 0.070 56 D 1020 495 485-505 495 679 0.000 0.025 0.050 57 950 474 464-484 475 675 -0.010 0.035 0.050 58 1020 495 485-505 530 670 0.030 0.055 0.050 59 E 1020 484 474-494 485 713 -0.020 0.040 0.040 60 950 464 454-474 465 710 - 0.030 0.050 0.035 61 950 464 454-474 480 680 -0.050 0.070 0:035 62 F 1020 501 491-511 500 710 0.030 0.050 0.040 63 950 48t 471-491 480 720 ooto 0.030 Q.035 64 1020 501 491-511 520 675 0.050 0.070 0.040 65 G 1020 509 499-519 510 700 0.030 0.050 0.040 66 950 489 479-499 490 695 0.020 0.040 0.040 67 1020 509 499-519 530 690 0.060 0.080 0.040 68 H 1020 521 511-531 520 690 0.060 0.135 0.150 69 I 1020 520 510-530 520 720 0.010 0.070 0.120 70 J 1020 510 500-520 510 645 0·03 ❹ 0.060 0.060 71 950 490 480-500 490 640 0.025 0.055 0.060 72 K 1020 479 469-489 480 720 0.025 0.055 0.060 73 950 458 448-468 460 715 0.020 0.065 0.060 ※丁八 * =0.29 x T 卜2·63 X [Cu]/[C]+225 -61 - 200831682 從表7可以獲得以下的考察結果。 首先,表7的No.44〜47是針對使用了鋼中成分符合 本發明的要件之表6的鋼種A,將熔體化溫度T1及時效 溫度T2作各種變化時的特性加以調查的。 其中,No.44及No.45是時效溫度T2符合本發明的 範圍(TA± 10。(:)之本發明例,兩者都是硬度很高,具有 優異的熱處理後的尺寸變形抑制性(不只是尺寸變形率的 差値,平均尺寸變形率及最大尺寸變形率全部都優異)° 相對於此,No. 46是時效溫度T2超出本發明的範圍 之比較例,No. 47是時效溫度T2低於本發明的範圍之比 較例,兩者都是硬度低,而且熱處理後的尺寸變形率的差 値雖然是良好,但是平均尺寸變形率及最大尺寸變形率則 是降低。 又,表7的No.48〜51是針對使用了鋼中成分符合本 發明的要件之表6的鋼種B,將熔體化溫度τ 1及時效溫 # 度T2作各種變化時的特性加以調查的。 其中,No·4 8及No. 49是時效溫度T2符合本發明的 範圍(TA;tlO°C )之本發明例,兩者都是硬度很高,具有 優異的熱處理後的尺寸變形抑制性。 相對於此,No. 50是時效溫度T2超出本發明的範圍 之比較例,No.51是時效溫度T2低於本發明的範圍之比 較例,兩者都是熱處理後的尺寸變形率的差値雖然是良好 ,但是平均尺寸變形率及最大尺寸變形率則是降低。又, No.51則是硬度也降低。 -62- 200831682 又,表7的No .52〜55是針對使用了鋼 發明的要件之表6的鋼種C,將熔體化溫度 度T2作各種變化時的特性加以調查的。 其中,No.52及No.53係時效溫度T2 範圍(TA±10°C )之本發明例,兩者都是硬 優異的熱處理後的尺寸變形抑制性。 相對於此,No. 54是時效溫度T2超出 之比較例,No. 55是時效溫度T2低於本發 較例,可以看出硬度的降低與熱處理後的最 的增加。又,No.54的熱處理後的平均尺寸 〇 又,表7的Ν〇·56〜58是針對使用了鋼 發明的要件之表6的鋼種D,將熔體化溫度 度Τ2作各種變化時的特性加以調查的。 其中,No· 56及No. 57係時效溫度Τ2 範圍(TA±10°C )之本發明例,兩者都是硬 優異的熱處理後的尺寸變形抑制性。 相對於此,No· 58是時效溫度T2超出 之比較例,熱處理後的最大尺寸變形率增加 又,表7的No.59〜61是針對使用了鋼 發明的要件之表6的鋼種E,將熔體化溫度 度T2作各種變化時的特性加以調查的。 其中’ Νο·59及Νο·60係時效溫度T2 範圍(TA±10°C )之本發明例,兩者都是硬 中成分符合本 T 1及時效溫 符合本發明的 度很高,具有 本發明的範圍 明的範圍之比 大尺寸變形率 變形率也增加 中成分符合本 T1及時效溫 符合本發明的 度很高,具有 本發明的範圔 〇 中成分符合本 τ 1及時效溫 符合本發明的 度很高,具有 -63- 200831682 優異的熱處理後的尺寸變形抑制性。 相對於此,Νο·61是時效溫度T2超出本發明的範圍 之比較例,雖然熱處理後的尺寸變形率的差値良好,但是 平均尺寸變形率及最大尺寸變形率則降低。 又,表7的No· 62〜64是針對使用了鋼中成分符合本 發明的要件之表6的鋼種F,將熔體化溫度τ1及時效溫 度T2作各種變化時的特性加以調查的。 其中,Νο·62及Νο·63係時效溫度T2符合本發明的 範圍(TA±10°C )之本發明例,兩者均爲硬度很高,具有 優異的熱處理後的尺寸變形抑制性。 相對於此,No· 64係時效溫度T2超出本發明的範圍 之比較例,熱處理後的尺寸變形率的差値雖然是良好,但 是,平均尺寸變形率及最大尺寸變形率則降低。 又,表7的No.65〜67是針對使用了鋼中成分符合本 發明的要件之表6的鋼種G,將熔體化溫度τ1及時效溫 度T2作各種變化時的特性加以調查的。 其中,No.65及Νο·66係時效溫度T2符合本發明的 範圍(TA±10°C)之本發明例,兩者均爲硬度很高,具有 優異的熱處理後的尺寸變形抑制性。 相對於此,No . 6 7係時效溫度T2超出本發明的範圍 之比較例,熱處理後的尺寸變形率的差値雖然是良好,但 是,平均尺寸變形率及最大尺寸變形率則降低。 以下所示的N 〇 ·都是在熔體化溫度及時效溫度符合本 發明的要件,但是因爲鋼中成分未符合本發明的範圍所以 -64 - 200831682 會產生各種缺點的比較例。No. Steel seed melting temperature TK°C) Aging temperature T2 (〇C) Hardness (HV) Size deformation rate (%) ΤΑ* Scope of the invention (TA±10) 値 値 値 値 値 A A 44 A 1020 489 479-499 490 675 0.010 0.030 0.040 45 950 469 459-479 470 678 0.000 0.020 0.040 46 1020 489 479-499 520 640 0.035 0.060 0.050 47 1020 489 479-499 460 642 0.035 0.060 0.050 48 B 1020 489 479-499 490 685 0.010 0.030 0.040 49 950 469 459-479 470 683 0.000 0.020 0.040 50 1020 489 479-499 520 652 0.040 0.065 D.050 51 1020 489 479-499 460 649 0.035 0.060 0.050 52 C 1020 504 494-514 500 655 0.020 0.050 0.060 950 484 474-494 485 484 475 675 -0.010 0.035 0.050 58 1020 495 485-505 530 670 0.030 0.055 0.050 59 E 1020 484 474-494 485 713 -0.020 0.040 0.040 60 950 464 454-474 465 710 - 0.030 0.050 0.035 61 950 464 454-474 480 680 -0.050 0.070 0:035 62 F 1020 501 491-511 500 710 0.030 0.050 0.040 63 950 48t 471-491 480 720 ooto 0.030 Q.035 64 1020 501 491-511 520 675 0.050 0.070 0.040 65 G 1020 509 499-519 510 700 0.030 0.050 0.040 66 950 489 479-499 490 695 0.020 0.040 0.040 67 1020 509 499-519 530 690 0.060 0.080 0.040 68 H 1020 521 511-531 520 690 0.060 0.135 0.150 69 I 1020 520 510-530 520 720 0.010 0.070 0.120 70 J 1020 510 500-520 510 645 0·03 ❹ 0.060 0.060 71 950 490 480-500 490 640 0.025 0.055 0.060 72 K 1020 479 469-489 480 720 0.025 0.055 0.060 73 950 458 448-468 460 715 0.020 0.065 0.060 ※丁八* =0.29 x T Bu 2·63 X [Cu]/[C]+225 -61 - 200831682 The following findings can be obtained from Table 7. First, No. 44 to 47 of Table 7 were investigated for the characteristics of the steel type A in Table 6 in which the steel component was in accordance with the requirements of the present invention, and the melting temperature T1 and the aging temperature T2 were variously changed. Among them, No. 44 and No. 45 are aging temperature T2 in accordance with the range of the present invention (TA ± 10 (:)), both of which have high hardness and excellent dimensional deformation inhibition after heat treatment ( Not only the difference in the dimensional deformation ratio, but also the average dimensional deformation ratio and the maximum dimensional deformation ratio are excellent.) In contrast, No. 46 is a comparative example in which the aging temperature T2 is outside the range of the present invention, and No. 47 is the aging temperature T2. In the comparative examples which are less than the range of the present invention, both of them have low hardness, and the difference in dimensional deformation ratio after heat treatment is good, but the average dimensional deformation ratio and the maximum dimensional deformation ratio are lowered. No. 48 to 51 are inspected for the steel type B in Table 6 which is a component of the steel in accordance with the requirements of the present invention, and the melting temperature τ 1 and the effective temperature # degree T2 are variously changed. 4 8 and No. 49 are examples of the invention in which the aging temperature T2 is in the range of the present invention (TA; t10 ° C), both of which have high hardness and excellent dimensional deformation inhibition after heat treatment. , No. 50 is the aging temperature T2 is beyond this In the comparative example of the range of the brightening, No. 51 is a comparative example in which the aging temperature T2 is lower than the range of the present invention, and both of them are the difference in the dimensional deformation ratio after the heat treatment, although the average dimensional deformation ratio and the maximum dimensional deformation are good. In addition, No. 51 has a lower hardness. -62- 200831682 Further, No. 52 to 55 of Table 7 are the steel type C of Table 6 which uses the requirements of the steel invention, and the melting temperature is set. The degree T2 was investigated for various characteristics. Among them, No. 52 and No. 53 are examples of the present invention in the range of the aging temperature T2 (TA ± 10 ° C), both of which are hard and excellent dimensional deformation after heat treatment. In contrast, No. 54 is a comparative example in which the aging temperature T2 is exceeded, and No. 55 is an aging temperature T2 lower than the comparative example, and the decrease in hardness and the most increase after heat treatment can be seen.约·56~58 of Table 7 is a steel type D of Table 6 which uses the requirements of the steel invention, and the characteristics of the melt temperature Τ2 are variously changed. Among them, No. 56 and No. 57 are aging temperature Τ 2 range (TA ± 10 In the example of the present invention, both of them are hard deformation excellent in dimensional deformation after heat treatment. On the other hand, No. 58 is a comparative example in which the aging temperature T2 is exceeded, and the maximum dimensional deformation rate after heat treatment is increased. No. 59 to 61 of 7 are inspected for the steel type E of Table 6 using the requirements of the steel invention, and the characteristics of the melt temperature T2 are variously changed. Among them, 'Νο·59 and Νο·60 are aging. The temperature T2 range (TA ± 10 ° C) is an example of the present invention, both of which are hard components. The T 1 and the time effect temperature are in accordance with the present invention, and the degree of the scope of the present invention is larger than that of the large-size deformation. The rate of deformation rate is also increased. The composition of the present invention conforms to the T1 and the time effect temperature is high according to the invention, and the composition of the invention has the high degree of conformity with the present τ 1 and the time effect temperature according to the invention, and has a high degree of -63-200831682 Excellent dimensional deformation inhibition after heat treatment. On the other hand, Νο·61 is a comparative example in which the aging temperature T2 is outside the range of the present invention, and although the difference in dimensional deformation ratio after heat treatment is good, the average dimensional deformation ratio and the maximum dimensional deformation ratio are lowered. In addition, No. 62 to 64 of Table 7 are inspected for the characteristics of the steel type F in Table 6 in which the steel component is in accordance with the requirements of the present invention, and the melt temperature τ1 and the temperature T2 are variously changed. Among them, Νο·62 and Νο·63 are examples of the present invention in which the aging temperature T2 is in the range of the present invention (TA ± 10 ° C), both of which have high hardness and excellent dimensional deformation inhibition after heat treatment. On the other hand, in the comparative example in which the No. 64 aging temperature T2 is outside the range of the present invention, the difference in the dimensional deformation ratio after the heat treatment is good, but the average dimensional deformation ratio and the maximum dimensional deformation ratio are lowered. In addition, No. 65 to 67 of Table 7 are inspected for the characteristics of the steel type G in Table 6 in which the steel component is in accordance with the requirements of the present invention, and the melt temperature τ1 and the temperature T2 are variously changed. Among them, No. 65 and Νο·66 are examples of the present invention in which the aging temperature T2 is in the range of the present invention (TA ± 10 ° C), and both of them have high hardness and excellent dimensional deformation inhibition after heat treatment. On the other hand, in the comparative example in which the aging temperature T2 of the No. 6 7 is outside the range of the present invention, the difference in the dimensional deformation ratio after the heat treatment is good, but the average dimensional deformation ratio and the maximum dimensional deformation ratio are lowered. The N 〇 shown below all meet the requirements of the present invention at the melt temperature and the aging temperature, but since the composition of the steel does not conform to the scope of the present invention, -64 - 200831682 produces a comparative example of various disadvantages.

No.68及No.69都是使用了模擬傳統的高C高Cr鋼 之表6的鋼種Η及鋼種I之例,因爲是使用了〔Cr〕與〔 C〕的乘積很大,〔Cu〕與〔C〕的比値很小,Ms點很低 的鋼種,所以熱處理後的平均尺寸變形率、最大尺寸變形 率、尺寸變形率全都增加。此外,這些鋼種在回火溫度很 低的情況,可獲得很高的硬度,所以將使用上述鋼種時的 回火溫度設定爲510°C,並且測定了各種特性。Both No. 68 and No. 69 are examples in which the steel type Η and the steel type I of Table 6 which simulates the conventional high-C high-Cr steel are used, because the product of [Cr] and [C] is large, [Cu] The ratio of [C] is small and the Ms point is very low. Therefore, the average dimensional deformation rate, the maximum dimensional deformation rate, and the dimensional deformation rate after heat treatment are all increased. Further, in the case where these steel grades have a very high tempering temperature, a high hardness can be obtained, so the tempering temperature when the above steel grade is used is set to 510 ° C, and various characteristics are measured.

No.70 及 No.71 係使用了 Cu 量很少,〔Cu〕/〔 Ni〕 的比値及〔Cu〕/〔 C〕的比値很小之表6的鋼種J之例, 可看出硬度的降低與最大尺寸變形率的增加。No. 70 and No. 71 are examples of the steel type J of Table 6 in which the amount of Cu is small, the ratio of [Cu]/[Ni], and the ratio of [Cu]/[C] are small. The decrease in hardness and the increase in the maximum dimensional deformation rate.

No.72及No.73係使用了〔Cu〕與〔C〕的比値很大 的表6的鋼種K之例,兩者皆增加了最大尺寸變形率。 此外,在本實施例中,雖然未顯示出尺寸變形率的經 時性變化,但可以預測到只要以符合本發明的要件的條件 下來執行熔體化處理—時效處理的話,即可既可維持高硬 度與良好的尺寸變形特性,而且又可將尺寸變形率的經時 性變變化抑制得很小。 以上說明雖然是參照特定的態樣來詳細地說明了本發 明,但只要是不脫離本發明的精神和範圍所作的各種變更 及修正皆是有可能的,對於業者而言是可達成的。 此外,本案係依據2006年10月17日提出申請之日 本發明專利申請案(特願2006 — 28303 8 )、2006年1〇月 30日提出申請之日本發明專利申請案(特願 2006- -65- 200831682 2 94 528)及2007年2月27日提出申請之日本發明專利申 請案(特願2007— 047490)而完成的。 又,此處所被引用的所有的參考,係指參考該文獻的 整體之意。 〔產業上的可利用性〕 本發明的冷加工模具用鋼係如上所述,係適切地控制 合金成分,因此硬度很高,具有優異的熱處理後的尺寸變 形抑制性,焊接修補性也良好。因此,使用上述的冷加工 模具用鋼所製得的模具,特別適合作爲拉伸強度約 5 9 OMPa以上的高張力鋼板的成形用模具來使用,可更爲 提昇壽命尤其是焊接修補後的壽命。 又,本發明的製造方法係適切地控制鋼中成分、以及 熔體化處理及時效處理的條件,因此可有效率地製造出硬 度很高,具有優異的熱處理後的尺寸變形抑制性的冷加工 模具用鋼。因此,使用本發明的製造方法所獲得的模具特 別適合作爲拉伸強度約5 90MPa以上的高張力鋼板的成形 用模具來使用,可更爲提昇壽命尤其是焊接修補後的壽命 【圖式簡單說明】 第1圖是顯示將母材彼此之間利用焊接金屬焊接時的 狀態的示意圖;第1圖(a )是焊接部的剖面圖,第1圖 (b)是第1圖(a)中所示的A區域的硬度分布之示意圖 -66 - 200831682 第2圖(a)係採用JIS SKD11作爲模具用鋼,在其 上面施作TiN的皮膜厚的模具表面發生「咬住現象」的狀 態時所示的光學顯微鏡照片;第2圖(b )及第2圖(c ) 係將其中一部分放大後的光學顯微鏡照片;第2圖(d ) 係施作TiN的皮膜之前的模具母材的光學顯微鏡照片。 第3圖(a )係顯示實施例所採用的焊接用試驗片的 φ 形狀之槪略圖;第3圖(b )係將溝部放大後的剖面圖。 第4圖係施作了預堆邊焊後的試驗片的樣子之示意槪 略圖。 第5圖係實施例所採用的夏丕氏衝撃試驗片的形狀之 槪略圖。 第6圖係顯示〔Cu〕/〔 Ni〕的比與HAZ軟化幅度度 的關係之圖表。 第7圖係顯示硬度分布曲線之圖表。 φ 第8圖係顯示〔Cu〕/〔C〕的比與尺寸變形率(平均 値、最大値)的關係之圖表。 _ 第9圖係顯示時效處理對於硬度與尺寸變化(尺寸變 形率)之影響的示意圖。 第1 〇圖係顯示時效處理對於尺寸變形量之影響的示 意圖。 -67-No. 72 and No. 73 are examples in which the steel type K of Table 6 having a large ratio of [Cu] and [C] is used, and both have the maximum dimensional deformation ratio. Further, in the present embodiment, although the temporal change of the dimensional deformation ratio is not shown, it can be predicted that the melt processing-aging treatment can be maintained as long as the conditions complying with the requirements of the present invention are performed. High hardness and good dimensional deformation characteristics, and the temporal change of dimensional deformation rate can be suppressed to a small extent. The present invention has been described in detail with reference to the specific embodiments thereof, and it is possible to make various changes and modifications without departing from the spirit and scope of the invention. In addition, the case is based on the Japanese invention patent application filed on October 17, 2006 (Japanese Patent Application No. 2006-28308 8), and the Japanese invention patent application filed on January 30, 2006 (Special Wish 2006--65) - 200831682 2 94 528) and the Japanese invention patent application filed on February 27, 2007 (Japanese Patent No. 2007-047490). Further, all references cited herein refer to the entirety of the document. [Industrial Applicability] The steel for cold working mold of the present invention has a high hardness, excellent dimensional deformation inhibition after heat treatment, and excellent weld repairability, as described above. Therefore, the mold obtained by using the steel for cold working die described above is particularly suitable for use as a molding die for a high tensile steel sheet having a tensile strength of about 5 9 OMPa or more, which can further improve the life, particularly the life after welding repair. Moreover, the manufacturing method of the present invention appropriately controls the components in the steel and the conditions of the melt treatment and the aging treatment, so that the cold working mold having high hardness and excellent dimensional deformation inhibition after heat treatment can be efficiently produced. Use steel. Therefore, the mold obtained by using the production method of the present invention is particularly suitable for use as a molding die for a high tensile steel sheet having a tensile strength of about 5 90 MPa or more, which can further improve the life, especially the life after welding repair. Fig. 1 is a schematic view showing a state in which the base materials are welded to each other by a weld metal; Fig. 1(a) is a cross-sectional view of the welded portion, and Fig. 1(b) is a view of Fig. 1(a) Schematic diagram of the hardness distribution of the A region shown in Fig.-66 - 200831682 Fig. 2 (a) is a state in which JIS SKD11 is used as a steel for a mold, and a "biting phenomenon" occurs on the surface of a mold having a film thickness of TiN. Optical micrographs shown; Fig. 2(b) and Fig. 2(c) are optical micrographs showing a part of the enlarged microscope; Fig. 2(d) is an optical microscope of the mold base before applying the film of TiN photo. Fig. 3(a) is a schematic view showing the shape of φ of the test piece for welding used in the embodiment, and Fig. 3(b) is a cross-sectional view showing the groove portion enlarged. Fig. 4 is a schematic diagram showing the appearance of a test piece after pre-stacking welding. Fig. 5 is a schematic view showing the shape of a Xia's smashing test piece used in the examples. Fig. 6 is a graph showing the relationship between the ratio of [Cu]/[Ni] and the degree of HAZ softening. Figure 7 is a graph showing the hardness distribution curve. Fig. 8 is a graph showing the relationship between the ratio of [Cu]/[C] and the dimensional deformation ratio (average 値, maximum 値). _ Fig. 9 is a schematic diagram showing the effect of aging treatment on hardness and dimensional change (size deformation rate). The first diagram shows the effect of the aging treatment on the amount of dimensional deformation. -67-

Claims (1)

200831682 十、申請專利範園 符合: 1 · 一種冷加工模具用鋼,以質量%換算,係 C : 0.20 〜0.60%、 s i : 〇 · 5 〜2.0 0 %、 Μ η : 0 · 1 〜2 %、 C r : 3.00 〜9.00%、 A1 : 〇 · 3 〜2.0 %、200831682 X. Patent application for Fan Park is in accordance with: 1 · A steel for cold working die, converted by mass %, C: 0.20 ~ 0.60%, si : 〇 · 5 ~ 2.0 0 %, Μ η : 0 · 1 〜 2 %, C r : 3.00 ~ 9.00%, A1 : 〇 · 3 ~ 2.0 %, Cu : 1.00 〜5%、 Ni: 1.00 〜5%、 Μ 〇 : 〇 · 5〜3 %及/或W : 2 %以下(含0 % )、 S : 〇 . 1 〇 %以下(不含0 % )、 各元素的 下列數式(1 )〜(3 ) {式中的〔〕是代表 含有量(%)之意} 數式(1 ) 〔 Cr〕X〔 c〕g 3·00、 數式(2 ) 〔 Cu〕/〔 Ni〕·· 0.5 〜2·2、 數式(3 ) 〔 Mo〕+ 〇·5χ〔 W〕: 0· 5 〜3.0% 雜質。 具用鋼, 工模具用 組成的群 0 % )。 所述的冷 0 % )。 的要件,而且其餘部分是鐵以及不可避免的 2. 如申請專利範圍第1項所述的冷加工模 其中又含有V : 0.5%以下(不含〇% )。 3. 如申請專利範圍第1或2項所述的冷力口 鋼,其中又含有:由Ti、Zr、Hf、Ta、及Nb所 所選出的至少一種元素’合計爲0 · 5 %以下(不含 4. 如申請專利範圍第1至3項的任何一項 加工模具用鋼’其中又含有co ·· 10%以下(不含 -68- 200831682 5 ·如申請專利範圍第1至4項的任何一項所述的冷 加工模具用鋼,其中,由下列數式所代表的麻田散鐵轉態 點(Ms點): Ms點 =5 5 0-3 6 1 X [ C ] -39χ〔Μη〕-35χ [ V ) -20x〔Cr〕 -17x〔Ni〕-10x〔Cu〕-5x(〔Mo〕+〔W〕) + 1 5x〔 Co〕+ 30x〔 A1〕 {式中的〔〕是代表各元素的含有量(%)之意} 是17〇°C以上。 6. —種模具,係使用如申請專利範圍第1至5項的 任何一項所述的冷加工模具用鋼所製得的。 7. 一種冷加工模具用鋼之製造方法,該冷加工模具 用鋼是符合申請專利範圍第1項所述的組成分的鋼,又包 含: 製備符合下列數式(4) {式中的〔〕是代表各元素 的含有量(%)之意} (4 ) 〔 Cu〕/〔 C〕: 4.0 〜15 的要件的鋼之工序; 以符合下列數式(5 )的條件來進行熔體化處理及時 效處理的工序; TA-10^ T2^ ΤΑ+ 10 ··· ( 5 ) 式中, TA=0.29xTl-2.63x〔Cu〕/〔C〕+ 225, τ 1是表示熔體化溫度(°c ) ’ -69- 200831682 T2是表示時效溫度(°C )。 8 ·如申請專利範圍第7項所述的冷加工模具用鋼之 製造方法,其中,前述鋼係含有V : 0 · 5 %以下(不含0 % )°Cu: 1.00 to 5%, Ni: 1.00 to 5%, Μ 〇: 〇· 5 to 3 % and/or W: 2% or less (including 0%), S: 〇. 1 〇% or less (excluding 0%) ), the following formula (1) to (3) of each element: {] in the formula is the meaning of the content (%). Equation (1) [Cr]X[c]g 3·00, number formula (2) [Cu]/[Ni]·· 0.5 〜2·2, the formula (3) [Mo]+ 〇·5χ [W]: 0·5 ~3.0% Impurity. For steel, the mold is composed of 0%). Said cold 0%). The requirements, and the rest are iron and inevitable 2. The cold working die as described in the first paragraph of the patent application contains V: 0.5% or less (excluding 〇%). 3. The cold-forced steel according to claim 1 or 2, further comprising: at least one element selected from Ti, Zr, Hf, Ta, and Nb' totaling 0. 5 % or less ( Excluded 4. For any of the steels for processing molds in the scope of patent application Nos. 1 to 3, which contain co··10% or less (excluding -68-200831682 5 • as required by patent applications Nos. 1 to 4) Any of the steels for cold working die according to any one of the following, wherein the transition point (Ms point) of the granita iron represented by the following formula: Ms point = 5 5 0 - 3 6 1 X [ C ] - 39 χ [Μη] -35χ [ V ) -20x [Cr] -17x [Ni]-10x [Cu]-5x ([Mo]+[W]) + 1 5x[ Co]+ 30x[ A1] {] is a representative The content of each element (%) is more than 17 ° C. 6. A mold is obtained by using a steel for cold working die according to any one of claims 1 to 5. 7. A method for producing a steel for cold working die, the steel for cold working die being a steel according to the composition component of the first application patent scope, and comprising: the preparation conforming to the following formula (4) [] in the formula [] is the meaning of the content (%) of each element} (4) [Cu] / [C]: the procedure of the steel of the requirements of 4.0 to 15; to satisfy the conditions of the following formula (5) The process of melt treatment and aging treatment; TA-10^ T2^ ΤΑ+ 10 ··· ( 5 ) where TA=0.29xTl-2.63x[Cu]/[C]+ 225, τ 1 is The method of producing a steel for cold working die according to claim 7, wherein the steel system contains the aging temperature (°C). V : 0 · 5 % or less (excluding 0 %) ° 9.如申請專利範圍第7或8項所述的冷加工模具用 鋼之製造方法,其中,前述鋼係含有由Ti、Zr、Hf、Ta、 及Nb所組成的群所選出的至少一種元素,合計爲0.5%以 下(不含0 % )。 1 〇.如申請專利範圍第7至9項的任何一項所述的冷 加工模具用鋼之製造方法,其中,前述鋼係含有Co : 10% 以下(不含〇 % )。 1 1 .如申請專利範圍第7至1 〇項的任何一項所述的 冷加工模具用鋼之製造方法,其中’由下列數式所代表的 麻田散鐵轉態點(Ms點): Ms點 =550-361x(C] -39x[Mn] -35x(V] -20x[Cr] -17x〔Ni〕-l〇x〔Cu〕-5x(〔M〇〕+〔W〕) + 1 5x〔 Co〕+ 30x〔 A1〕 是1 7 0 °C以上。 i 2. —種模具,是根據如申請專利範圍第7至1 1項 的任何一項所述的冷加工模具用鋼之製造方法所$ ^的 -70-The method for producing a steel for cold working die according to the seventh aspect of the invention, wherein the steel system contains at least one element selected from the group consisting of Ti, Zr, Hf, Ta, and Nb. The total is 0.5% or less (excluding 0%). The method for producing a steel for cold working die according to any one of claims 7 to 9, wherein the steel system contains Co: 10% or less (excluding 〇%). The method for producing a steel for cold working die according to any one of claims 7 to 1, wherein the transition point of the granulated iron (Ms point) represented by the following formula: Ms point =550-361x(C) -39x[Mn] -35x(V] -20x[Cr] -17x[Ni]-l〇x[Cu]-5x([M〇]+[W]) + 1 5x[ Co]+ 30x[ A1] is a temperature of 170 ° C or more. i 2. The mold is a method for producing a steel for cold working die according to any one of claims 7 to 11. ^-70-
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