TW201829806A - Press hardened steel with increased toughness and method for production - Google Patents

Press hardened steel with increased toughness and method for production Download PDF

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TW201829806A
TW201829806A TW106141452A TW106141452A TW201829806A TW 201829806 A TW201829806 A TW 201829806A TW 106141452 A TW106141452 A TW 106141452A TW 106141452 A TW106141452 A TW 106141452A TW 201829806 A TW201829806 A TW 201829806A
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temperature
steel
rolling
pretreatment method
slab
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約翰 安卓 羅比杜克斯
伊拉斯姆思 阿摩亞騰
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美商Ak鋼鐵資產公司
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    • C21D8/00Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0294Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips involving a localised treatment
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21BROLLING OF METAL
    • B21B1/00Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations
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    • C21D1/18Hardening; Quenching with or without subsequent tempering
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    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0205Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips of ferrous alloys
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    • C21D8/00Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0221Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
    • C21D8/0226Hot rolling
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    • C21D8/00Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/04Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing
    • C21D8/0405Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing of ferrous alloys
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    • 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
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    • 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
    • C21D9/48Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals deep-drawing sheets
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/002Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21BROLLING OF METAL
    • B21B1/00Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations
    • B21B1/02Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations for rolling heavy work, e.g. ingots, slabs, blooms, or billets, in which the cross-sectional form is unimportant ; Rolling combined with forging or pressing
    • B21B2001/028Slabs

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Abstract

A method for processing a press hardenable steel includes first heating a slab of the press hardenable steel. The slab is heated to a re-heat furnace temperature of approximately 2300 DEG F. The slab is subjected to rolling into a steel sheet having a predetermined thickness. The temperature of the slab during rolling corresponds to a rolling temperature that is greater than or equal to 1600 DEG F. The steel sheet is coiled. The temperature of the steel sheet during coiling corresponds to a coiling temperature of approximately 1050 DEG F.

Description

韌性增加的加壓硬化鋼及製造方法Pressurized hardened steel with increased toughness and manufacturing method

本申請案係關於加壓硬化鋼、熱壓成型鋼、熱衝壓鋼或經加熱至奧氏體化(austenitization)溫度且在衝壓模具中成型及淬火以在最終零件中實現所需機械特性之任何其他鋼之改良。此等類型之鋼有時亦稱為「可加熱處理的含硼鋼」。在本申請案中,皆將其稱為「加壓硬化鋼」。This application relates to press hardened steel, hot formed steel, hot stamped steel or any which is heated to austenitization temperature and shaped and quenched in a stamping die to achieve the desired mechanical properties in the final part. Improvement of other steels. These types of steel are sometimes referred to as "heatable treated boron-containing steels". In the present application, they are referred to as "pressurized hardened steel".

加壓硬化鋼主要用作汽車中之結構部件,在汽車中高強度、低重量及改良的耐侵入性為汽車製造商所需。汽車結構中採用加壓硬化鋼之常見結構部件為B柱。 加壓硬化鋼之當前工業加工包括將坯料(一塊鋼板)加熱至高於A3 溫度(奧氏體化溫度)之溫度(通常在900-950℃範圍內),將材料保持在該溫度下一段持續時間,將奧氏體化之坯料放入熱衝壓模具中,使該坯料成型為所需形狀,且將材料於模具中淬火至低溫,從而形成麻田散體(martensite)。最終得到具有高的極限抗張強度及完全麻田散體微觀結構之材料。 先前技術之加壓硬化鋼之淬火態微觀結構為完全麻田散體。習知的加壓硬化鋼之極限拉伸強度為約1500 MPa,且總伸長率為約6%。Pressurized hardened steel is mainly used as a structural component in automobiles, and high strength, low weight and improved intrusion resistance in automobiles are required by automobile manufacturers. A common structural component of pressurized hardened steel in automotive construction is the B-pillar. Current industrial processing of press hardened steel involves heating the billet (a steel sheet) to a temperature above the A 3 temperature (austenification temperature) (usually in the range of 900-950 ° C), maintaining the material at that temperature for a sustained period of time. At a time, the austenitized blank is placed in a hot stamping die, the blank is formed into a desired shape, and the material is quenched in a mold to a low temperature to form a martensite. The result is a material with a high ultimate tensile strength and a complete Matian bulk microstructure. The quenched microstructure of the prior art pressurized hardened steel is a complete Ma Tian bulk. Conventional press hardened steels have an ultimate tensile strength of about 1500 MPa and a total elongation of about 6%.

藉由使用用於在加壓硬化條件下實現更高殘餘韌性的化學方法及加工,本申請案之鋼相比於當前可獲得的加壓硬化鋼合金有所改良。殘餘韌性係指在加壓硬化條件下材料所具有的韌性。 本發明鋼合金之實施例的強度-延展性特性包括大於或等於1100 MPa之極限拉伸強度及大約為8%的伸長率。The steel of the present application is improved over currently available press hardened steel alloys by the use of chemical methods and processing for achieving higher residual toughness under pressure hardening conditions. Residual toughness refers to the toughness of the material under pressure hardening conditions. The strength-ductility characteristics of the embodiment of the steel alloy of the present invention include an ultimate tensile strength of greater than or equal to 1100 MPa and an elongation of about 8%.

本申請案主張2016年11月28日申請之美國臨時申請案系列第62/426,788號,名稱為「韌性增加的加壓硬化鋼及製造方法(Press Hardened Steel with Increased Toughness and Method for Production)」的優先權;其揭示內容以引用之方式併入本文中。 由於其高強度特徵,加壓硬化鋼通常為理想的。在實踐中,此准許製造商製造相對於由非加壓硬化鋼製造的組件強度更高且重量更小的組件。此等高強度特徵通常由形成以麻田散體為主的微觀結構而實現。詳言之,在與加壓硬化鋼坯料相關的熱衝壓處理期間,坯料首先經歷奧氏體化熱處理。在此熱處理期間,坯料之溫度升高至高於坯料之特定成分的A3 溫度,從而使坯料之微觀結構轉變為以奧氏體為主。 一旦奧氏體化熱處理完成,則使用內部冷卻模具將坯料衝壓為預定形狀。除了使坯料成形之外,衝壓處理亦具有使坯料迅速冷卻至低於麻田散體起始溫度(Ms )之效果。因此,坯料之以奧氏體為主的微觀結構轉變為以麻田散體為主的微觀結構。因為麻田散體通常表徵為強且硬的微觀結構,所以衝壓處理通常導致強度高且硬度高的最終零件。 儘管最終熱衝壓零件之高強度對於各種應用通常為理想的,但在某些情況下額外的韌性可為理想的。舉例而言,如上文所描述,熱衝壓通常導致高強度及高硬度的最終零件。高水平硬度之最終零件通常具有相對低的延展性及因此相對低的韌性。因此,在某些情況下,可能需要讓加壓硬化鋼具有習知加壓硬化鋼之高強度特徵但殘餘韌性提高的特徵。 在上文所描述的熱衝壓處理之前,加壓硬化鋼經歷多個預處理步驟。圖1展示習知預處理方法(10)。預處理方法包括使鋼板經歷多個預處理步驟(20、30、40、50)。此等步驟(20、30、40、50)通常在熱衝壓之前且在形成最終熱衝壓處理之加壓硬化鋼坯料之前進行。一般而言,此等步驟(20、30、40、50)在連續軋機中之板材上進行。舉例而言,加壓硬化鋼最初以包含預定成分的鑄造厚塊開始。厚塊隨後進入再加熱鍋爐(20)且經歷大約2300℉ (1260℃)之再加熱溫度。 一旦厚塊藉由再加熱鍋爐(20)升高至再加熱溫度,則厚塊經歷粗輥壓(30)且隨後精輥壓(40)。此等輥壓步驟將厚塊厚度逐漸減少至最終板材厚度。在輥壓處理期間,厚塊溫度自初始2300℉ (1260℃)再加熱溫度不斷降至與粗輥壓(30)相關的粗壓溫度。在一些實例中,粗壓溫度大約為2000℉ (1093℃)。在精輥壓(40)期間,厚塊經歷大約1600℉ (871℃)之精壓溫度。隨著溫度降低,厚塊經歷輥壓操作,其在粗輥壓(30)期間使厚塊厚度降低相對大的量,逐漸變成在精輥壓(40)期間使厚塊厚度降低相對小的量。 以相對恆定的輥壓冷卻速率(12)使厚塊溫度自與再加熱鍋爐(20)相關的初始再加熱溫度降低至與精輥壓(40)相關的溫度。 完成輥壓後,加壓硬化鋼材料呈鋼板形式。在鋼板形式中,鋼板經歷成卷(50)。成卷(50)可在大約1200℉ (649℃)之成卷溫度下進行。在一些實例中,成卷(50)可在精壓(40)之後立即開始。因此,在一些實例中,成卷(50)可在大約1600℉ (871℃)下開始且降低至大約1200℉ (649℃)之成卷溫度。 在成卷(50)之前,如圖1中所示,鋼板可以一或多種不同冷卻速率(14、16)冷卻至成卷溫度。舉例而言,以第一冷卻速率(14)或第二冷卻速率(16),在約18℉/秒與約20℉/秒之間鋼板的冷卻相對緩慢。 在成卷(50)結束時,准許捲曲的鋼板冷卻至環境溫度或室溫。捲曲的鋼板隨後相繼地形成為加壓硬化的鋼材料之坯料。坯料可隨後經歷上文所描述之熱衝壓處理。 如上文所描述,在某些情況下,可能需要增加加壓硬化鋼零件之韌性。在某些情況下,利用改變上文所描述之預處理步驟之某些參數藉由細化加壓硬化鋼材料的粒度來可提高韌性。 圖2展示經修改之預處理方法(100)。如同上文所描述之預處理方法(10),本實例之預處理方法(100)包括一系列預處理步驟(120、130、140、150)。與上文所描述類似,此等步驟(120、130、140、150)通常在熱衝壓之前且在形成最終熱衝壓處理之加壓硬化鋼坯料之前進行。一般而言,此等步驟(120、130、140、150)在連續軋機中之板材上進行。舉例而言,加壓硬化鋼最初以包含預定成分的鑄造厚塊開始。厚塊隨後進入再加熱鍋爐(120),在鍋爐中厚塊經歷再加熱溫度。與關於再加熱鍋爐(20)上文所描述之再加熱溫度類似,本實例中之再加熱溫度為大約2300℉ (1260℃)。 一旦厚塊升高至再加熱鍋爐(120)之再加熱溫度,則厚塊經歷粗輥壓(130)且隨後精輥壓(140)。此使厚塊厚度逐漸減少至最終板材厚度。作為一實例,在輥壓處理期間,厚塊溫度自再加熱鍋爐(120)之初始2300℉ (1260℃)再加熱溫度不斷降低至與粗輥壓(130)相關的大約2000℉ (1093℃)之粗壓溫度。接下來,厚塊進一步降至與精輥壓(140)相關的大約1600℉ (871℃)之精壓溫度。不同於上文所描述之習知預處理方法(10)中的精輥壓(40),本實例中之精輥壓(140)在相對較低溫度下進行。如下文將更詳細地描述,當與經修改之成卷溫度結合進行時,此相對較低溫度可導致增加之晶粒細化。隨著溫度降低,厚塊經歷輥壓操作,其在粗輥壓(130)期間使厚塊厚度降低相對大的量,變成在精輥壓(140)期間使厚塊厚度降低相對小的量。 以相對恆定的輥壓冷卻速率(112)使厚塊溫度自與再加熱鍋爐(120)相關的初始再加熱溫度降低至與精輥壓(140)相關的溫度。此冷卻速率與先前處理之輥壓冷卻速率(12)類似。 完成輥壓後,加壓硬化鋼材料呈鋼板形式。在鋼板形式中,鋼板經歷成卷(150)。成卷(150)可在大約1050℉ (566℃)之成卷溫度下進行。在一些實例中,成卷(150)可在精壓(140)之後立即開始。因此,在一些實例中,成卷(150)可在大約1600℉ (871℃)下開始且降低至大約1050℉ (566℃)之成卷溫度。或者,在一些實例中,成卷(150)可延遲直至鋼板達至大約1050℉ (566℃)之成卷溫度。一旦達至成卷溫度(150),則對於全部成卷(150)可等溫保存鋼板。較佳地,精壓(140)在約1600℉ (871℃)之精壓溫度下進行,鋼板降至1050℉ (566℃)之成卷溫度,且在鋼板在成卷溫度下保存時進行成卷(150)。 無論怎樣達至成卷溫度,應理解,相對於關於習知預處理方法(10)上文所描述之成卷溫度,大約1050℉ (566℃)之成卷溫度通常較低。如將理解,此降低之成卷溫度可通常導致鋼板之晶粒細化提高,其可導致在熱衝壓之後最終工作產物之殘餘韌性增加。 在成卷(150)之前,如圖2中所示,以冷卻速率(114)鋼板可冷卻至成卷溫度。在本實例中,冷卻速率(114)在約35℉/秒與約50℉/秒之間。 不同於上文所描述之冷卻速率(14、16),本實例中之冷卻速率(114)通常相對較快。此相對較快速的冷卻速率可使用輸出輥道(run-out-table)加速冷卻方法實現。如將理解,此相對較快的冷卻速率(114)可通常導致在熱衝壓之後最終工作產物中的增加之晶粒細化及相關增加之殘餘韌性。 在成卷(150)結束時,准許捲曲的鋼板冷卻至環境溫度或室溫。捲曲的鋼板隨後相繼地形成為加壓硬化的鋼材料之坯料。坯料可隨後經歷上文所描述之熱衝壓處理。 如上文所描述,預處理方法(10、100)可使用包含預定成分的鑄造厚塊進行。應理解,厚塊之特定成分可變化,使得多種成分可藉由上文所描述之方法(10、100)來使用。如下文將更詳細地描述,可將各種元素添加至厚塊中以影響最終工作產物之多種冶金特性。 添加碳來降低麻田散體起始溫度、提供固溶體強化及增加鋼之硬化度。碳為一種奧氏體穩定劑。在某些實施例中,碳可以0.1-0.5質量%之濃度存在;在其他實施例中,碳可以0.2-0.30質量%之濃度存在。 添加錳來降低麻田散體起始溫度、提供固溶體強化及增加鋼之硬化度。錳為一種奧氏體穩定劑。在某些實施例中,錳可以1.0-10.0質量%之濃度存在;在其他實施例中,錳可以1.15-1.25質量%之濃度存在。 添加矽來提供固溶體強化。矽為一種肥粒鐵穩定劑。在某些實施例中,矽可以0.02-2.0質量%之濃度存在;在其他實施例中,矽可以0.24-0.30質量%之濃度存在。 添加鋁以用於在煉鋼期間脫氧且提供固溶體強化。鋁為一種肥粒鐵穩定劑。在某些實施例中,鋁可以0.0-2.0質量%之濃度存在;在其他實施例中,鋁可以0.02-1.0質量%之濃度存在。在其他實施例中,鋁完全視情況存在,且在一些實施例中可因此忽略或受限於雜質元素。 將鈦添加至集氮氣劑中。在某些實施例中,鈦可以0.0-0.045質量%之濃度存在;在其他實施例中,鈦可以0.035質量%之最大值的濃度存在。在其他實施例中,鈦完全視情況存在,且在一些實施例中可因此忽略或受限於雜質元素。 添加鉬來提供固溶體強化且增加鋼之硬化度。在某些實施例中,鉬可以0-4.0質量%之濃度存在;在其他實施例中,鉬可以0-1.0質量%之濃度存在。在其他實施例中,鉬完全視情況存在,且因此在一些實施例中可忽略或限於雜質元素。 添加鉻來降低麻田散體起始溫度,提供固溶體強化及增加鋼之硬化度。鉻為一種肥粒鐵穩定劑。在某些實施例中,鉻可以0-6.0質量%之濃度存在;在其他實施例中,鉻可以0.18-0.22質量%之濃度存在。 添加硼來增加鋼之硬化度。在某些實施例中,硼可以0-0.005質量%之濃度存在;在其他實施例中,硼可以0.003-0.005質量%之濃度存在。 添加鎳來提供固溶體強化且降低麻田散體起始溫度。鎳為一種奧氏體穩定劑。在某些實施例中,鎳可以0.0-1.0質量%之濃度存在;在其他實施例中,鎳可以0.02-0.5質量%之濃度存在。在其他實施例中,鎳完全視情況存在,且因此在一些實施例中可忽略或限於雜質元素。 添加鈮來提供改良之晶粒細化。鈮亦可增加硬度及強度。在某些實施例中,鈮可以0-0.090質量%之濃度存在。實例 1 除如所述下文之外,使用標準鋼製備方法來製備示於表1中之複數種合金成分。 表1 :成分範圍。成分以質量%為單位。 實例 2 實例1中之表1之成分4310經歷兩種上文所描述之預處理方法(10、100)。鋼經受模擬熱衝壓。將鋼加熱至大約930℃維持5分鐘且隨後在水冷銅模具中淬滅。經歷各預處理方法(10、100)外加模擬熱衝壓之樣品隨後經歷拉伸測試以生成應力-應變曲線。所得應力-應變曲線示於圖3中,其中預處理方法(10)以實線形式展示且預處理方法(100)以虛線形式展示。 如在圖3中可見,相對於經歷預處理方法(10)之樣品,經歷預處理方法(100)之樣品通常導致提高之殘餘韌性。在模擬熱衝壓之前,在熱輥壓條件下製備各樣品之顯微照片,且將其示於圖10及11中,其中圖10對應於預處理方法(10),且圖11對應於預處理方法(100)。如可見,相對於由預處理方法(10)製備之晶粒結構,預處理方法(100)通常導致更細化之晶粒結構。作為其結果,在圖3中觀測到提高之殘餘韌性。實例 3 實例1中之表1之成分4311經歷上文所描述之預處理方法(10、100)兩者。鋼經受模擬熱衝壓。將鋼加熱至大約930℃ 5分鐘且隨後在水冷銅模具中淬滅。經歷各預處理方法(10、100)外加模擬熱衝壓之樣品隨後經歷拉伸測試以生成應力-應變曲線。所得應力-應變曲線示於圖4中,其中預處理方法(10)以實線形式展示且預處理方法(100)以虛線形式展示。 如在圖4中可見,相對於經歷預處理方法(10)之樣品,經歷預處理方法(100)之樣品通常導致提高之殘餘韌性。在模擬熱衝壓之前,在熱輥壓條件下製備各樣品之顯微照片,且將其示於圖12及13中,其中圖12對應於預處理方法(10),且圖13對應於預處理方法(100)。如可見,相對於由預處理方法(10)製備之晶粒結構,預處理方法(100)通常導致更細化之晶粒結構。作為其結果,在圖4中觀測到提高之殘餘韌性。實例 4 實例1中之表1之成分4312經歷上文所描述之預處理方法(10、100)兩者。鋼經受模擬熱衝壓。將鋼加熱至大約930℃ 5分鐘且隨後在水冷銅模具中淬滅。經歷各預處理方法(10、100)外加模擬熱衝壓之樣品隨後經歷拉伸測試以生成應力-應變曲線。所得應力-應變曲線示於圖5中,其中預處理方法(10)以實線形式展示且預處理方法(100)以虛線形式展示。 如在圖5中可見,相對於經歷預處理方法(10)之樣品,經歷預處理方法(100)之樣品通常導致提高之殘餘韌性。在模擬熱衝壓之前,在熱輥壓條件下製備各樣品之顯微照片,且將其示於圖14及15中,其中圖14對應於預處理方法(10),且圖15對應於預處理方法(100)。如可見,相對於由預處理方法(10)製備之晶粒結構,預處理方法(100)通常導致更細化之晶粒結構。作為其結果,在圖5中觀測到提高之殘餘韌性。實例 5 實例1中之表1之成分4313經歷上文所描述之預處理方法(10、100)兩者。鋼經受模擬熱衝壓。將鋼加熱至大約930℃ 5分鐘且隨後在水冷銅模具中淬滅。經歷各預處理方法(10、100)外加模擬熱衝壓之樣品隨後經歷拉伸測試以生成應力-應變曲線。所得應力-應變曲線示於圖6中,其中預處理方法(10)以實線形式展示且預處理方法(100)以虛線形式展示。 如可見在圖6中,相對於經歷預處理方法(10)之樣品,經歷預處理方法(100)之樣品通常導致提高之殘餘韌性。在模擬熱衝壓之前,在熱輥壓條件下製備各樣品之顯微照片,且將其示於圖16及17中,其中圖16對應於預處理方法(10),且圖17對應於預處理方法(100)。如可見,相對於由預處理方法(10)製備之晶粒結構,預處理方法(100)通常導致更細化之晶粒結構。作為其結果,在圖6中觀測到提高之殘餘韌性或保持之延展性。實例 6 進一步使用雙邊緣-凹口拉伸測試評估具有上文實例1之表1中識別之各成分的樣品之韌性。各成分(例如4310、4311、4312、4313)的樣品經歷上文所描述之各預處理方法(10、100)。鋼隨後經受模擬加壓硬化程序,其中其在大約930℃下經奧氏體化300 s,且隨後在平的水冷模具中淬滅。隨後進行雙邊緣凹口的拉伸測試。隨後製備各成分之所得資料的曲線,如圖7及8中所示。舉例而言,圖7展示經歷預處理方法(100)之各樣品的結果。圖8展示經歷預處理方法(10)之各樣品的結果。對於圖7及8,各成分之資料可由符號識別。舉例而言,圓圈對應於成分4310,三角形對應於成分4311,星星對應於成分4312,且十字形對應於成分4313。 如在圖7及8中可見,在破裂之前,相比於經歷預處理方法(10)之材料,經歷預處理方法(100)之材料呈現較高尖峰負載/力。因此,圖7及8指示預處理方法(100)導致增加之韌性或保持之延展性。實例 7 進一步分析上文關於實例6所論述的資料。詳言之,在圖7及8中所示的力-位移曲線下之面積積分可用於獲得應變能之值。認為應變能為材料韌性之量度。因此,產生上文關於實例6所論述的各樣品之材料韌性之量測值。 所得各樣品的應變能隨後作為各樣品之對應成分中之鈮濃度之函數進行繪製。所得曲線圖示於圖9中。不同於上文所述之圖7及8,圖9利用不同符號流程以識別特異性資料點與成分之間的對應關係。舉例而言,在圖9中,圓圈對應於成分4310,十字形對應於成分4311,三角形對應於成分4312,且方形對應於成分4313。另外,因為經歷各預處理方法(10、100)之樣品的結果包括於單條曲線中,圖9描繪經歷預處理方法(10)之樣品與經歷預處理方法(100)之樣品的比較。在各情況下,鋼在測試之前經受模擬熱衝壓。在圖9中,實心符號代表加工方法(10),且空心符號代表加工方法(100)。 如在圖9中可見,經歷預處理方法(100)之樣品通常導致提高之應變能且因此增加之韌性。另外,觀測到韌性響應於具有增加之鈮的成分而部分增加。舉例而言,成分4313包括最高鈮濃度,且亦包括最高應變能或韌性量測值。實例 8 一種可加壓硬化鋼,其包含以鋼之總質量%計的: 其中該鋼經歷以下加工: (a) 將可加壓硬化鋼之厚塊加熱至大約2300℉之再加熱鍋爐溫度; (b) 將厚塊輥壓為具有預定厚度的鋼板,其中輥壓期間之厚塊溫度對應於高於或等於約1600℉ (871℃)之輥壓溫度;及 (c) 使鋼板成卷,其中成卷期間之鋼板溫度對應於大約1050℉之成卷溫度。實例 9 實例8或以下實例中之任一者之可加壓硬化鋼,其包含以鋼之總質量%計的: 0.10至0.50%碳; 0.00至0.005%硼; 0.0至6.0%鉻; 1.00至10.0%錳; 0.090%或更少的鈮; 0.02至2.00%矽; 0.0至2.0%鋁; 0.0至0.045%鈦; 0.0至4.0%鉬; 0.0至1.0%鎳;及 包括鐵及雜質之其餘部分。實例 10 實例8或9或以下實例中之任一者之可加壓硬化鋼,其包含0.2-0.3質量%碳。實例 11 實例8至10中之任一者或以下實例中之任一者的可加壓硬化鋼,其包含1.15-1.25質量%錳。實例 12 實例8至11中之任一者或以下實例中之任一者的可加壓硬化鋼,其包含0.24-0.30質量%矽。實例 13 實例8至12中之任一者或以下實例中之任一者的可加壓硬化鋼,其包含0.02-1.0質量%鋁。實例 14 實例8至13中之任一者或以下實例中之任一者的可加壓硬化鋼,其包含最大值為0.035質量%之鈦。實例 15 實例8至14中之任一者或以下實例中之任一者的可加壓硬化鋼,其包含0-1.0質量%鉬。實例 16 實例8至15中之任一者或以下實例中之任一者的可加壓硬化鋼,其包含0.18-0.22質量%鉻。實例 17 實例8至16中之任一者或以下實例中之任一者的可加壓硬化鋼,其包含0.003-0.005質量%硼。實例 18 實例8至17中之任一者或以下實例中之任一者的可加壓硬化鋼,其包含0.02-0.5質量%鎳。實例 19 實例8至18中之任一者或以下實例中之任一者的可加壓硬化鋼,其包含0-1.0質量%鉬。實例 20 實例8至19中之任一者或以下實例中之任一者的可加壓硬化鋼,其中輥壓步驟包括粗輥壓操作及精輥壓操作。實例 21 實例8至20中之任一者或以下實例中之任一者的可加壓硬化鋼,其中在粗輥壓操作期間之厚塊溫度高於或等於2000℉。實例 22 實例8至21中之任一者或以下實例中之任一者的可加壓硬化鋼,其中在精輥壓操作期間之厚塊溫度高於或等於約1600℉ (871℃)。實例 23 實例8至22中之任一者或以下實例中之任一者的可加壓硬化鋼,其進一步包含步驟:在使鋼板成卷之後熱衝壓至少一部分鋼板。實例 24 實例8至23中之任一者或以下實例中之任一者的可加壓硬化鋼,其進一步包含以下步驟:以第一冷卻速率將可加壓硬化鋼自再加熱鍋爐溫度冷卻至輥壓溫度,且以第二冷卻速率將可加壓硬化鋼自輥壓溫度冷卻至成卷溫度,其中第二冷卻速率高於第一冷卻速率。實例 25 實例8至24中之任一者或以下實例中之任一者的可加壓硬化鋼,其中將可加壓硬化鋼自輥壓溫度冷卻至成卷溫度之步驟使用輸出輥道加速冷卻方法進行。實例 26 實例8至25或以下實例中之任一者的可加壓硬化鋼,其中在粗輥壓操作期間之厚塊溫度為大約2000℉。實例 27 實例8至26之任一者的可加壓硬化鋼,其中在精輥壓操作期間之厚塊溫度為大約1600℉至1700℉。This application claims the US Provisional Application Serial No. 62/426,788, filed on November 28, 2016, entitled "Press Hardened Steel with Increased Toughness and Method for Production"Priority; the disclosure of which is incorporated herein by reference. Pressurized hardened steel is generally desirable due to its high strength characteristics. In practice, this allows the manufacturer to manufacture components that are stronger and less weight than components made from non-pressurized hardened steel. These high-intensity features are usually achieved by the formation of a microstructure dominated by the granules of the mai field. In particular, the billet is first subjected to an austenitizing heat treatment during the hot stamping process associated with the press hardened steel billet. During this heat treatment, the temperature of the blank rises to a temperature above the A 3 specific component of the blank, so that the microstructure of the blank into austenite-based. Once the austenitizing heat treatment is completed, the billet is punched into a predetermined shape using an internal cooling mold. In addition to shaping the blank, the stamping process also has the effect of rapidly cooling the billet to below the starting temperature (M s ) of the granules. Therefore, the austenite-based microstructure of the billet is transformed into a microstructure dominated by Ma Tian bulk. Because the Matian bulk is often characterized as a strong and hard microstructure, the stamping process typically results in a final part that is high in strength and high in hardness. While the high strength of the final hot stamped parts is often desirable for a variety of applications, in some cases additional toughness may be desirable. For example, as described above, hot stamping typically results in a final part of high strength and high hardness. The final part of high level hardness typically has a relatively low ductility and therefore relatively low toughness. Therefore, in some cases, it may be desirable to have the press-hardened steel have the characteristics of the high-strength characteristics of the conventional press-hardened steel but the residual toughness is improved. The press hardened steel is subjected to a plurality of pretreatment steps prior to the hot stamping process described above. Figure 1 shows a conventional pretreatment method (10). The pretreatment method involves subjecting the steel sheet to a plurality of pretreatment steps (20, 30, 40, 50). These steps (20, 30, 40, 50) are typically performed prior to hot stamping and prior to forming the final hard stamping treated press hardened steel billet. In general, these steps (20, 30, 40, 50) are carried out on a sheet in a continuous rolling mill. For example, press hardened steel initially begins with a cast slab containing a predetermined composition. The slab then enters the reheat boiler (20) and undergoes a reheat temperature of approximately 2300 °F (1260 °C). Once the slab is raised to the reheat temperature by the reheating boiler (20), the slab undergoes a rough roll (30) and then a fine roll (40). These rolling steps gradually reduce the thickness of the slab to the final sheet thickness. During the rolling process, the slab temperature is continuously reduced from the initial 2300 °F (1260 °C) reheating temperature to the coarse pressure temperature associated with the coarse roll pressure (30). In some examples, the roughing temperature is approximately 2000 °F (1093 °C). During the fine roll (40), the slab experiences a coining temperature of approximately 1600 °F (871 °C). As the temperature decreases, the slab undergoes a rolling operation which reduces the thickness of the slab by a relatively large amount during the rough rolling (30), gradually becoming a relatively small amount of thickness reduction during the sizing (40). . The chunk temperature is reduced from the initial reheat temperature associated with the reheat boiler (20) to the temperature associated with the fine roll pressure (40) at a relatively constant roll cooling rate (12). After the rolling is completed, the press-hardened steel material is in the form of a steel plate. In the form of a steel sheet, the steel sheet is subjected to a roll (50). The roll (50) can be carried out at a coil temperature of about 1200 °F (649 °C). In some examples, the roll (50) can begin immediately after coining (40). Thus, in some examples, the roll (50) can begin at about 1600 °F (871 °C) and reduce to a roll temperature of about 1200 °F (649 °C). Prior to forming the roll (50), as shown in Figure 1, the steel sheet can be cooled to a roll temperature at one or more different cooling rates (14, 16). For example, at a first cooling rate (14) or a second cooling rate (16), cooling of the steel sheet is relatively slow between about 18 °F/sec and about 20 °F/sec. At the end of the roll (50), the crimped steel sheet is allowed to cool to ambient or room temperature. The crimped steel sheet is subsequently successively formed as a blank of a press hardened steel material. The blank can then be subjected to the hot stamping process described above. As described above, in some cases it may be desirable to increase the toughness of press hardened steel parts. In some cases, the toughness can be improved by refining the particle size of the press hardened steel material by varying some of the parameters of the pretreatment steps described above. Figure 2 shows a modified pre-processing method (100). As with the pretreatment method (10) described above, the pretreatment method (100) of the present example includes a series of pretreatment steps (120, 130, 140, 150). Similar to that described above, these steps (120, 130, 140, 150) are typically performed prior to hot stamping and prior to forming the final hot stamped press hardened steel billet. In general, these steps (120, 130, 140, 150) are carried out on a sheet in a continuous rolling mill. For example, press hardened steel initially begins with a cast slab containing a predetermined composition. The slab then enters the reheat boiler (120) where the slab undergoes a reheat temperature. Similar to the reheating temperature described above with respect to the reheating boiler (20), the reheating temperature in this example is about 2300 °F (1260 °C). Once the slab is raised to the reheat temperature of the reheat boiler (120), the slab undergoes a rough roll (130) and then a fine roll (140). This gradually reduces the thickness of the slab to the final sheet thickness. As an example, during the rolling process, the slab temperature is continuously reduced from the initial 2300 °F (1260 °C) reheat temperature of the reheat boiler (120) to approximately 2000 °F (1093 °C) associated with the coarse roll pressure (130). The rough pressure temperature. Next, the slab is further reduced to a refining temperature of approximately 1600 °F (871 °C) associated with the fine roll pressure (140). Unlike the fine roll pressure (40) in the conventional pretreatment method (10) described above, the fine roll pressure (140) in this example is carried out at a relatively low temperature. As will be described in more detail below, this relatively lower temperature can result in increased grain refinement when performed in conjunction with the modified roll temperature. As the temperature decreases, the slab undergoes a rolling operation that reduces the thickness of the slab by a relatively large amount during the rough rolling (130), becoming a relatively small amount that reduces the thickness of the slab during the sizing (140). The chunk temperature is reduced from the initial reheat temperature associated with the reheat boiler (120) to the temperature associated with the fine roll pressure (140) at a relatively constant roll cooling rate (112). This cooling rate is similar to the previously processed roll cooling rate (12). After the rolling is completed, the press-hardened steel material is in the form of a steel plate. In the form of a steel sheet, the steel sheet is subjected to a roll (150). The roll (150) can be run at a roll temperature of about 1050 °F (566 °C). In some examples, the roll (150) can begin immediately after coining (140). Thus, in some examples, the roll (150) can begin at about 1600 °F (871 °C) and drop to a roll temperature of about 1050 °F (566 °C). Alternatively, in some examples, the roll (150) may be delayed until the steel sheet reaches a roll temperature of about 1050 °F (566 °C). Once the coiling temperature (150) is reached, the steel sheet can be isothermally stored for all rolls (150). Preferably, the coining (140) is carried out at a coining temperature of about 1600 °F (871 °C), the steel sheet is lowered to a coiling temperature of 1050 °F (566 °C), and is carried out when the steel sheet is stored at a coiling temperature. Volume (150). Regardless of how the coil temperature is reached, it is understood that the coiling temperature of about 1050 °F (566 °C) is generally lower relative to the coiling temperature described above with respect to the conventional pretreatment method (10). As will be appreciated, this reduced roll temperature can generally result in increased grain refinement of the steel sheet which can result in an increase in residual toughness of the final work product after hot stamping. Prior to winding (150), as shown in Figure 2, the steel sheet can be cooled to a coiling temperature at a cooling rate (114). In the present example, the cooling rate (114) is between about 35 °F/sec and about 50 °F/sec. Unlike the cooling rates (14, 16) described above, the cooling rate (114) in this example is typically relatively fast. This relatively fast cooling rate can be achieved using a run-out-table accelerated cooling method. As will be appreciated, this relatively fast cooling rate (114) can generally result in increased grain refinement in the final working product after hot stamping and associated increased residual toughness. At the end of the roll (150), the crimped steel sheet is allowed to cool to ambient or room temperature. The crimped steel sheet is subsequently successively formed as a blank of a press hardened steel material. The blank can then be subjected to the hot stamping process described above. As described above, the pretreatment method (10, 100) can be performed using a cast slab containing a predetermined composition. It will be appreciated that the specific composition of the chunks may vary such that the various components may be used by the methods (10, 100) described above. As will be described in more detail below, various elements can be added to the slab to affect the various metallurgical properties of the final work product. Carbon is added to reduce the initial temperature of the granules in the field, to provide solid solution strengthening and to increase the degree of hardening of the steel. Carbon is an austenite stabilizer. In certain embodiments, carbon may be present at a concentration of from 0.1 to 0.5% by mass; in other embodiments, the carbon may be present at a concentration of from 0.2 to 0.30% by mass. Manganese is added to reduce the initial temperature of the matrix in the field, to provide solid solution strengthening and to increase the degree of hardening of the steel. Manganese is an austenite stabilizer. In certain embodiments, manganese may be present at a concentration of from 1.0 to 10.0% by mass; in other embodiments, manganese may be present at a concentration of from 1.15 to 1.25 mass%. Add hydrazine to provide solid solution strengthening. It is a ferrite iron stabilizer. In certain embodiments, the ruthenium may be present at a concentration of from 0.02 to 2.0% by mass; in other embodiments, the ruthenium may be present at a concentration of from 0.24 to 0.30% by mass. Aluminum is added for deoxidation during steelmaking and provides solid solution strengthening. Aluminum is a ferrite iron stabilizer. In certain embodiments, aluminum may be present at a concentration of from 0.0 to 2.0% by mass; in other embodiments, aluminum may be present at a concentration of from 0.02 to 1.0% by mass. In other embodiments, aluminum is entirely present and may, in some embodiments, be omitted or limited to impurity elements. Titanium is added to the nitrogen collecting agent. In certain embodiments, titanium may be present at a concentration of from 0.0 to 0.045% by weight; in other embodiments, titanium may be present at a concentration that is a maximum of 0.035 mass%. In other embodiments, titanium is present entirely as appropriate, and in some embodiments may therefore be omitted or limited to impurity elements. Molybdenum is added to provide solid solution strengthening and increase the degree of hardening of the steel. In certain embodiments, molybdenum may be present at a concentration of from 0 to 4.0% by mass; in other embodiments, molybdenum may be present at a concentration of from 0 to 1.0% by mass. In other embodiments, molybdenum is present entirely as appropriate, and thus may be omitted or limited to impurity elements in some embodiments. The addition of chromium reduces the initial temperature of the granules in the field, provides solid solution strengthening and increases the degree of hardening of the steel. Chromium is a ferrite iron stabilizer. In certain embodiments, the chromium may be present at a concentration of from 0 to 6.0% by mass; in other embodiments, the chromium may be present at a concentration of from 0.18 to 0.22% by mass. Boron is added to increase the degree of hardening of the steel. In certain embodiments, boron may be present at a concentration of from 0 to 0.005% by mass; in other embodiments, boron may be present at a concentration of from 0.003 to 0.005% by mass. Nickel is added to provide solid solution strengthening and to reduce the initial temperature of the field. Nickel is an austenite stabilizer. In certain embodiments, nickel may be present at a concentration of from 0.0 to 1.0% by mass; in other embodiments, nickel may be present at a concentration of from 0.02 to 0.5% by mass. In other embodiments, nickel is completely present as appropriate, and thus may be omitted or limited to impurity elements in some embodiments. Niobium is added to provide improved grain refinement.铌 can also increase hardness and strength. In certain embodiments, the hydrazine may be present at a concentration of from 0 to 0.090% by mass. Example 1 A plurality of alloy compositions shown in Table 1 were prepared using standard steel preparation methods, except as described below. Table 1 : Range of ingredients. The ingredients are in mass %. The component 4310 of Table 1 in Example 2 of Example 2 was subjected to two pretreatment methods (10, 100) as described above. The steel is subjected to simulated hot stamping. The steel was heated to about 930 ° C for 5 minutes and then quenched in a water cooled copper mold. Samples subjected to various pretreatment methods (10, 100) plus simulated hot stamping were then subjected to a tensile test to generate a stress-strain curve. The resulting stress-strain curve is shown in Figure 3, where the pretreatment method (10) is shown in solid lines and the pretreatment method (100) is shown in dashed lines. As can be seen in Figure 3, the sample subjected to the pretreatment method (100) generally results in increased residual toughness relative to the sample subjected to the pretreatment method (10). Micrographs of each sample were prepared under hot rolling conditions prior to simulated hot stamping and are shown in Figures 10 and 11, wherein Figure 10 corresponds to pretreatment method (10) and Figure 11 corresponds to pretreatment Method (100). As can be seen, the pretreatment method (100) generally results in a finer grain structure relative to the grain structure prepared by the pretreatment method (10). As a result, an improved residual toughness was observed in FIG. Example 3 The ingredients 4311 of Table 1 in Example 1 were subjected to both the pretreatment methods (10, 100) described above. The steel is subjected to simulated hot stamping. The steel was heated to about 930 ° C for 5 minutes and then quenched in a water cooled copper mold. Samples subjected to various pretreatment methods (10, 100) plus simulated hot stamping were then subjected to a tensile test to generate a stress-strain curve. The resulting stress-strain curve is shown in Figure 4, where the pretreatment method (10) is shown in solid lines and the pretreatment method (100) is shown in dashed lines. As can be seen in Figure 4, the sample subjected to the pretreatment method (100) generally results in increased residual toughness relative to the sample subjected to the pretreatment method (10). Micrographs of each sample were prepared under hot rolling conditions prior to simulated hot stamping and are shown in Figures 12 and 13, wherein Figure 12 corresponds to pretreatment method (10) and Figure 13 corresponds to pretreatment Method (100). As can be seen, the pretreatment method (100) generally results in a finer grain structure relative to the grain structure prepared by the pretreatment method (10). As a result, an improved residual toughness was observed in FIG. Example 4 The ingredients 4312 of Table 1 in Example 1 were subjected to both the pretreatment methods (10, 100) described above. The steel is subjected to simulated hot stamping. The steel was heated to about 930 ° C for 5 minutes and then quenched in a water cooled copper mold. Samples subjected to various pretreatment methods (10, 100) plus simulated hot stamping were then subjected to a tensile test to generate a stress-strain curve. The resulting stress-strain curve is shown in Figure 5, where the pretreatment method (10) is shown in solid lines and the pretreatment method (100) is shown in dashed lines. As can be seen in Figure 5, the sample subjected to the pretreatment method (100) generally results in increased residual toughness relative to the sample subjected to the pretreatment method (10). Micrographs of each sample were prepared under hot rolling conditions prior to simulated hot stamping and are shown in Figures 14 and 15, wherein Figure 14 corresponds to pretreatment method (10) and Figure 15 corresponds to pretreatment Method (100). As can be seen, the pretreatment method (100) generally results in a finer grain structure relative to the grain structure prepared by the pretreatment method (10). As a result, an improved residual toughness was observed in FIG. Example 5 Component 4313 of Table 1 in Example 1 was subjected to both the pretreatment methods (10, 100) described above. The steel is subjected to simulated hot stamping. The steel was heated to about 930 ° C for 5 minutes and then quenched in a water cooled copper mold. Samples subjected to various pretreatment methods (10, 100) plus simulated hot stamping were then subjected to a tensile test to generate a stress-strain curve. The resulting stress-strain curve is shown in Figure 6, where the pretreatment method (10) is shown in solid lines and the pretreatment method (100) is shown in dashed lines. As can be seen in Figure 6, the sample subjected to the pretreatment method (100) generally results in increased residual toughness relative to the sample subjected to the pretreatment method (10). Micrographs of each sample were prepared under hot rolling conditions prior to simulated hot stamping and are shown in Figures 16 and 17, wherein Figure 16 corresponds to pretreatment method (10) and Figure 17 corresponds to pretreatment Method (100). As can be seen, the pretreatment method (100) generally results in a finer grain structure relative to the grain structure prepared by the pretreatment method (10). As a result thereof, an improved residual toughness or a maintainable ductility was observed in Fig. 6. Example 6 : The toughness of the samples having the ingredients identified in Table 1 of Example 1 above was further evaluated using a double edge-notch tensile test. Samples of the various components (e.g., 4310, 4311, 4112, 4313) were subjected to the various pretreatment methods (10, 100) described above. The steel was then subjected to a simulated press hardening procedure in which it was austenitized at about 930 ° C for 300 s and then quenched in a flat water-cooled mold. A tensile test of the double edge notch was then performed. A curve of the obtained data of each component was then prepared as shown in Figs. For example, Figure 7 shows the results of each sample subjected to the pretreatment method (100). Figure 8 shows the results of each sample subjected to the pretreatment method (10). For Figures 7 and 8, the data for each component can be identified by a symbol. For example, a circle corresponds to component 4310, a triangle corresponds to component 4311, a star corresponds to component 4312, and a cross corresponds to component 4313. As can be seen in Figures 7 and 8, the material undergoing the pretreatment method (100) exhibits a higher peak load/force prior to rupture than the material undergoing the pretreatment method (10). Thus, Figures 7 and 8 indicate that the pretreatment method (100) results in increased toughness or retained ductility. Example 7 further analyzes the information discussed above with respect to Example 6. In particular, the area integral under the force-displacement curve shown in Figures 7 and 8 can be used to obtain the value of the strain energy. The strain energy is considered to be a measure of the toughness of the material. Thus, measurements of the material toughness of each of the samples discussed above with respect to Example 6 were produced. The strain energy of each of the obtained samples was then plotted as a function of the concentration of ruthenium in the corresponding components of each sample. The resulting curve is shown in Figure 9. Unlike Figures 7 and 8 described above, Figure 9 utilizes different symbolic flows to identify the correspondence between specific data points and components. For example, in FIG. 9, the circle corresponds to component 4310, the cross corresponds to component 4311, the triangle corresponds to component 4312, and the square corresponds to component 4313. In addition, since the results of the samples subjected to the respective pretreatment methods (10, 100) are included in a single curve, FIG. 9 depicts a comparison of the sample subjected to the pretreatment method (10) with the sample subjected to the pretreatment method (100). In each case, the steel was subjected to simulated hot stamping prior to testing. In Fig. 9, the solid symbol represents the processing method (10), and the open symbol represents the processing method (100). As can be seen in Figure 9, the sample subjected to the pretreatment method (100) typically results in increased strain energy and thus increased toughness. In addition, it was observed that the toughness partially increased in response to the component having an increased enthalpy. For example, component 4313 includes the highest concentration of germanium and also includes the highest strain energy or toughness measurement. Example 8 A press hardenable steel comprising, based on the total mass % of steel: wherein the steel is subjected to the following processing: (a) heating the slab of press hardenable steel to a reheating boiler temperature of about 2300 °F; (b) pressing the slab into a steel sheet having a predetermined thickness, wherein the slab temperature during rolling corresponds to a rolling temperature higher than or equal to about 1600 °F (871 °C); and (c) rolling the steel sheet, The steel sheet temperature during the rolling period corresponds to a coiling temperature of about 1050 °F. Example 9 The press hardenable steel of any of Example 8 or any of the following examples, comprising: 0.10 to 0.50% carbon; 0.00 to 0.005% boron; 0.0 to 6.0% chromium; 1.00 to 10.0% manganese; 0.090% or less of bismuth; 0.02 to 2.00% 矽; 0.0 to 2.0% aluminum; 0.0 to 0.045% titanium; 0.0 to 4.0% molybdenum; 0.0 to 1.0% nickel; and the remainder including iron and impurities . Example 10 The press hardenable steel of any of Examples 8 or 9 or any of the following examples comprising 0.2-0.3 mass% carbon. Example 11 Example 8 to any one or any of the following examples of one of hardened steel pressurizable 10, comprising 1.15-1.25% by mass of manganese. Example 12 Examples 8 to 11 in any one or any of the following examples of one of the pressurizable hardened steel, which contains 0.24-0.30 mass% silicon. Example 13 Example 8 to any one or any of the following examples of one of the pressurizable 12 hardened steel, comprising 0.02 to 1.0 mass% aluminum. Example 14 Example 8 to any one or any of the following examples of one of hardened steel pressurizable 13, which comprises a maximum of 0.035% by mass of titanium. Example 15 Examples 8 to 14 in any one or any of the following examples of one of the pressurizable hardened steel, comprising 0 to 1.0% by mass molybdenum. Example 16 Example 8 to any one or any of the following examples of one of hardened steel pressurizable 15, containing 0.18-0.22 mass% of chromium. Example 17 Examples 8 to 16 in any one or any of the following examples of one of the pressurizable hardened steel, comprising by mass 0.003-0.005% boron. Example 18 Example 8 to 17 of any one or any of the following examples of one of the pressurizable hardened steel, comprising 0.02 to 0.5 mass% nickel. Example 19 Examples 8 to 18 in any of any one of the examples below or may be pressurized by a hardened steel, which contains 0 to 1.0% by mass molybdenum. Example 20 Examples 8 to 19 in any one or any of the following examples of one of the pressurizable hardened steel, wherein the rolling step includes a rough rolling operation and the finishing rolling operation. Example 21 Example 8 to any one or any of the following examples of one of hardened steel pressurizable 20, wherein the thickness of the block during the rough rolling operation temperature is higher than or equal to 2000 ℉. Example 22 Examples 8-21 of any one or any of the following examples of one of the pressurizable hardened steel wherein slabs during the rolling operation in the finishing temperature higher than or equal to about 1600 ℉ (871 ℃). Example 23 Examples 8 to 22 in any one or any of the following examples of one of hardened steel pressurizable, further comprising the step of: after the steel sheet into a roll at least part of a steel sheet for hot stamping. Example 24 Example 8 to any one of the following examples or according to any one of the hardened steel pressurizable 23, further comprising the steps of: at a first cooling rate may be pressurized from hardened steel reheat boiler is cooled to a temperature The temperature is rolled, and the press hardenable steel is cooled from the rolling temperature to the coiling temperature at a second cooling rate, wherein the second cooling rate is higher than the first cooling rate. Example 25 Example 8 to any one of the following examples or according to any one of the hardened steel pressurizable 24, wherein the pressurizable from hardened steel roll temperature was cooled to coiling temperature step to use the output of the accelerated cooling roller The method is carried out. Example 26. The press hardenable steel of any of Examples 8 to 25 or any of the following examples, wherein the chunk temperature during the rough rolling operation is about 2000 °F. Example 27 Examples 8-26 according to any one of the pressurizable hardened steel, wherein the thickness of the block during the operation of finishing rolling temperature of about 1600 deg.] F to 1700 ℉.

10‧‧‧預處理方法10‧‧‧Pretreatment method

12‧‧‧輥壓冷卻速率12‧‧‧Rolling cooling rate

14‧‧‧第一冷卻速率14‧‧‧First cooling rate

16‧‧‧第二冷卻速率16‧‧‧second cooling rate

20‧‧‧再加熱鍋爐20‧‧‧Reheating boiler

30‧‧‧粗輥壓30‧‧‧Rough roll pressure

40‧‧‧精輥壓40‧‧‧Fine roll pressure

50‧‧‧成卷50‧‧‧volume

100‧‧‧預處理方法100‧‧‧Pretreatment method

112‧‧‧輥壓冷卻速率112‧‧‧Rolling cooling rate

114‧‧‧冷卻速率114‧‧‧ cooling rate

120‧‧‧再加熱鍋爐120‧‧‧Reheating boiler

130‧‧‧粗輥壓130‧‧‧Rough roll pressure

140‧‧‧精輥壓140‧‧‧Fine roll pressure

150‧‧‧成卷150‧‧‧volume

圖1展示本發明合金之實施例的熱分佈及加工示意圖。 圖2展示本發明合金之實施例的另一個熱分佈及加工示意圖。 圖3展示成分4310的應力-應變曲線之曲線圖,其中來自第一預處理方法之結果以實線形式展示,且來自第二預處理方法之結果以虛線形式展示。 圖4展示成分4311的應力-應變曲線之曲線圖,其中來自第一預處理方法之結果以實線形式展示,且來自第二預處理方法之結果以虛線形式展示。 圖5展示成分4312的應力-應變曲線之曲線圖,其中來自第一預處理方法之結果以實線形式展示,且來自第二預處理方法之結果以虛線形式展示。 圖6展示成分4313的應力-應變曲線之曲線圖,其中來自第一預處理方法之結果以實線形式展示,且來自第二預處理方法之結果以虛線形式展示。 圖7展示在經歷第二預處理方法之後本發明合金之實施例的雙邊緣-凹口拉伸測試的結果。 圖8展示在經歷第一預處理方法之後本發明合金之實施例的雙邊緣-凹口拉伸測試的結果。 圖9展示作為鈮濃度之函數進行繪製的本發明合金之實施例之應變能計算結果。 圖10展示在經歷第一預處理方法之後成分4310之顯微照片。 圖11展示在經歷第二預處理方法之後成分4310之顯微照片。 圖12展示在經歷第一預處理方法之後成分4311之顯微照片。 圖13展示在經歷第二預處理方法之後成分4311之顯微照片。 圖14展示在經歷第一預處理方法之後成分4312之顯微照片。 圖15展示在經歷第二預處理方法之後成分4312之顯微照片。 圖16展示在經歷第一預處理方法之後成分4313之顯微照片。 圖17展示在經歷第二預處理方法之後成分4313之顯微照片。Figure 1 shows a schematic representation of the heat distribution and processing of an embodiment of the alloy of the present invention. Figure 2 shows another schematic diagram of heat distribution and processing of an embodiment of the alloy of the present invention. 3 shows a graph of stress-strain curves for component 4310, where the results from the first pretreatment method are shown in solid lines and the results from the second pretreatment method are shown in dashed lines. 4 shows a graph of stress-strain curves for component 4311, where the results from the first pretreatment method are shown in solid lines and the results from the second pretreatment method are shown in dashed lines. Figure 5 shows a graph of the stress-strain curve for component 4312, where the results from the first pretreatment method are shown in solid lines and the results from the second pretreatment method are shown in dashed lines. Figure 6 shows a graph of the stress-strain curve for component 4313, where the results from the first pretreatment method are shown in solid lines and the results from the second pretreatment method are shown in dashed lines. Figure 7 shows the results of a double edge-notch tensile test of an embodiment of the inventive alloy after undergoing a second pretreatment method. Figure 8 shows the results of a double edge-notch tensile test of an embodiment of the inventive alloy after undergoing the first pretreatment method. Figure 9 shows the results of strain energy calculations for an embodiment of the alloy of the present invention plotted as a function of erbium concentration. Figure 10 shows a photomicrograph of component 4310 after undergoing the first pretreatment method. Figure 11 shows a photomicrograph of component 4310 after undergoing a second pretreatment method. Figure 12 shows a photomicrograph of component 4311 after undergoing the first pretreatment method. Figure 13 shows a photomicrograph of component 4311 after undergoing a second pretreatment method. Figure 14 shows a photomicrograph of component 4312 after undergoing the first pretreatment method. Figure 15 shows a photomicrograph of component 4312 after undergoing a second pretreatment method. Figure 16 shows a photomicrograph of component 4313 after undergoing the first pretreatment method. Figure 17 shows a photomicrograph of ingredient 4313 after undergoing a second pretreatment method.

Claims (10)

一種加工可加壓硬化鋼之方法,該方法包含, (a) 將該可加壓硬化鋼之厚塊加熱至大約2300℉之再加熱鍋爐溫度; (b) 將該厚塊輥壓成為具有預定厚度之鋼板,其中輥壓期間該厚塊之溫度對應於高於或等於約1600℉ (871℃)之輥壓溫度;及 (c) 使該鋼板成卷,其中成卷期間該鋼板之溫度對應於大約1050℉之成卷溫度。A method of processing press hardenable steel, the method comprising: (a) heating the slab of the press hardenable steel to a reheating boiler temperature of about 2300 °F; (b) pressing the slab into a predetermined a steel plate having a thickness, wherein a temperature of the slab during rolling corresponds to a rolling temperature higher than or equal to about 1600 °F (871 ° C); and (c) winding the steel sheet, wherein a temperature of the steel sheet corresponds to a temperature during rolling The coiling temperature is about 1050 °F. 如請求項1之方法,其中該輥壓步驟包括粗輥壓操作及精輥壓操作。The method of claim 1, wherein the rolling step comprises a rough rolling operation and a fine rolling operation. 如請求項2之方法,其中該粗輥壓操作期間該厚塊之溫度高於或等於2000℉。The method of claim 2, wherein the temperature of the chunk during the rough rolling operation is greater than or equal to 2000 °F. 如請求項2之方法,其中該精輥壓操作期間該厚塊之溫度高於或等於約1600℉ (871℃)。The method of claim 2, wherein the temperature of the chunk during the precision rolling operation is greater than or equal to about 1600 °F (871 °C). 如請求項2之方法,其中該粗輥壓操作期間該厚塊之溫度為大約2000℉。The method of claim 2, wherein the temperature of the chunk during the coarse rolling operation is about 2000 °F. 如請求項2之方法,其中該精輥壓操作期間該厚塊之溫度為大約1600℉至1700℉。The method of claim 2, wherein the temperature of the chunk during the precision rolling operation is between about 1600 °F and 1700 °F. 如請求項1之方法,其進一步包含在使該鋼板成卷之後熱衝壓至少一部分該鋼板。The method of claim 1, further comprising hot stamping at least a portion of the steel sheet after the steel sheet is wound. 如請求項1之方法,其進一步包含以第一冷卻速率將該可加壓硬化鋼自該再加熱鍋爐溫度冷卻至該輥壓溫度,及以第二冷卻速率將該可加壓硬化鋼自該輥壓溫度冷卻至該成卷溫度,其中該第二冷卻速率高於該第一冷卻速率。The method of claim 1, further comprising cooling the press hardenable steel from the reheating boiler temperature to the rolling temperature at a first cooling rate, and applying the press hardenable steel to the second cooling rate The rolling temperature is cooled to the coiling temperature, wherein the second cooling rate is higher than the first cooling rate. 如請求項1之方法,其中將該可加壓硬化鋼自該輥壓溫度冷卻至該成卷溫度之該步驟使用輸出輥道加速冷卻方法進行。The method of claim 1, wherein the step of cooling the press hardenable steel from the rolling temperature to the coiling temperature is carried out using an output roller accelerated cooling method. 如請求項1之方法,其中該可加壓硬化鋼具有包含以下之成分: 0.10至0.50%碳; 0.00至0.005%硼; 0.0至6.0%鉻; 1.00至10.0%錳; 0.090%或更少之鈮; 0.02至2.00%矽; 0.0至2.0%鋁; 0.0至0.045%鈦; 0.0至4.0%鉬; 0.0至1.0%鎳;及 包括鐵及雜質之其餘部分。The method of claim 1, wherein the press hardenable steel has a composition comprising: 0.10 to 0.50% carbon; 0.00 to 0.005% boron; 0.0 to 6.0% chromium; 1.00 to 10.0% manganese; 0.090% or less铌; 0.02 to 2.00% 矽; 0.0 to 2.0% aluminum; 0.0 to 0.045% titanium; 0.0 to 4.0% molybdenum; 0.0 to 1.0% nickel; and the remainder including iron and impurities.
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