JP6377745B2 - 超高強度鋼板及びその製造方法 - Google Patents
超高強度鋼板及びその製造方法 Download PDFInfo
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- JP6377745B2 JP6377745B2 JP2016534517A JP2016534517A JP6377745B2 JP 6377745 B2 JP6377745 B2 JP 6377745B2 JP 2016534517 A JP2016534517 A JP 2016534517A JP 2016534517 A JP2016534517 A JP 2016534517A JP 6377745 B2 JP6377745 B2 JP 6377745B2
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- 238000004519 manufacturing process Methods 0.000 title claims description 28
- 229910000797 Ultra-high-strength steel Inorganic materials 0.000 title claims description 21
- 238000000034 method Methods 0.000 title claims description 17
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- 238000005098 hot rolling Methods 0.000 claims description 28
- 238000000137 annealing Methods 0.000 claims description 25
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 24
- 238000010438 heat treatment Methods 0.000 claims description 22
- 239000011651 chromium Substances 0.000 claims description 20
- 239000010960 cold rolled steel Substances 0.000 claims description 20
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 18
- 229910001566 austenite Inorganic materials 0.000 claims description 18
- 229910052799 carbon Inorganic materials 0.000 claims description 18
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims description 17
- 229910052748 manganese Inorganic materials 0.000 claims description 17
- 239000010936 titanium Substances 0.000 claims description 14
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 12
- 229910052804 chromium Inorganic materials 0.000 claims description 11
- 238000005097 cold rolling Methods 0.000 claims description 11
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 10
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 10
- 229910052782 aluminium Inorganic materials 0.000 claims description 10
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 10
- 229910052759 nickel Inorganic materials 0.000 claims description 10
- 239000010703 silicon Substances 0.000 claims description 10
- 229910052710 silicon Inorganic materials 0.000 claims description 10
- 238000004804 winding Methods 0.000 claims description 9
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 7
- 229910052698 phosphorus Inorganic materials 0.000 claims description 7
- 229910052717 sulfur Inorganic materials 0.000 claims description 7
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 claims description 6
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 claims description 6
- 229910052796 boron Inorganic materials 0.000 claims description 6
- 238000009713 electroplating Methods 0.000 claims description 6
- 229910052757 nitrogen Inorganic materials 0.000 claims description 6
- 239000011574 phosphorus Substances 0.000 claims description 6
- 239000011593 sulfur Substances 0.000 claims description 6
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims description 5
- 239000012535 impurity Substances 0.000 claims description 5
- 229910052742 iron Inorganic materials 0.000 claims description 5
- 238000007670 refining Methods 0.000 claims description 5
- 229910052718 tin Inorganic materials 0.000 claims description 5
- 229910052719 titanium Inorganic materials 0.000 claims description 5
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims description 4
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 4
- 238000007598 dipping method Methods 0.000 claims description 4
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- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 4
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- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
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- 229910000760 Hardened steel Inorganic materials 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 238000005246 galvanizing Methods 0.000 description 2
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- 238000011105 stabilization Methods 0.000 description 1
- CADICXFYUNYKGD-UHFFFAOYSA-N sulfanylidenemanganese Chemical compound [Mn]=S CADICXFYUNYKGD-UHFFFAOYSA-N 0.000 description 1
- 239000013077 target material Substances 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
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- C21D9/46—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
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- B21B3/00—Rolling materials of special alloys so far as the composition of the alloy requires or permits special rolling methods or sequences ; Rolling of aluminium, copper, zinc or other non-ferrous metals
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Description
炭素(C)は、オーステナイト相の安定化に寄与する元素であるため、その添加量が増加するほど、オーステナイト相の形成に有利である。但し、炭素の含量が0.4%未満では、変形時にα´(アルファ´´)−マルテンサイト相が形成されるため、加工時にクラックが発生し、延性が低くなるという短所がある。これに対し、Cの含量が0.7%を超える場合には、電気抵抗が増加し、電気抵抗を利用して溶接する3枚重ねスポット溶接時の溶接性が低下するという問題がある。したがって、本発明では、Cの含量を0.4〜0.7%に制限することが好ましい。
マンガン(Mn)は、炭素と共にオーステナイト相を安定化させるのに必須の元素である。但し、その含量が12%未満の場合には、成形性を害するα´(アルファ´)−マルテンサイト相が生成されて強度は増加するが、延性が急激に減少し、加工硬化率も少なくなる。これに対し、Mnの含量が24%を超える場合には、双晶の生成が抑制されて強度は増加するが、延性が減少し、電気抵抗が増加して溶接性が低下する。また、Mnの添加量が増加するほど、熱間圧延時にクラックが発生しやすく、製造原価が増加して経済的な面で不利である。したがって、本発明では、Mnの含量を12〜24%に制限することが好ましい。
アルミニウム(Al)は、通常、鋼の脱酸のための目的で添加されるが、本発明では、延性の向上及び耐遅れ破壊特性の向上のために添加される。即ち、Alは、フェライト相の安定した元素であるが、鋼の滑り面における積層欠陥エネルギーを増加させ、ε−マルテンサイト相の生成を抑制して延性及び耐遅れ破壊性を向上させる。また、Alは、Mnの添加量が低い場合にもε−マルテンサイト相の生成を抑制するため、マンガンの添加量を最小化し且つ加工性を向上させるのに大きく寄与する。したがって、このAlの添加量が0.01%未満の場合には、ε−マルテンサイト相が生成されて強度は増加するが、延性が急激に減少するという短所がある。これに対し、3.0%を超える場合には、双晶の発生を抑制して延性を減少させ、連続鋳造時の鋳造性を悪くし、熱間圧延時に鋼板の表面の酸化が多く発生して製品の表面品質を低下させる。したがって、本発明では、Alの含量を0.01〜3.0%に制限することが好ましい。
シリコン(Si)は、固溶強化する元素であって、固溶効果によって結晶粒度を減らすことにより鋼板の降伏強度を増加させる元素である。通常、Siが過剰に添加される場合は、表面にシリコン酸化層を形成して溶融めっき性を低下させることが知られている。
通常、リン(P)及び硫黄(S)は、鋼の製造時に不可避に含有される元素であるため、その含量をそれぞれ0.03%以下に制限する。特に、Pは偏析を発生させて鋼の加工性を減少させる。Sは粗大な硫化マンガン(MnS)を形成してフランジクラックのような欠陥を発生させる。そのため、鋼板の穴広げ性を減少させるため、これらの含量を最大限に抑制することが好ましい。
窒素(N)は、オーステナイト結晶粒内で凝固過程時にAlと作用して微細な窒化物を析出させ、双晶の発生を促進するため、鋼板の成形の際の強度と延性を向上させる。但し、その含量が0.04%を超える場合には、窒化物が過剰に析出されて熱間加工性及び延伸率を低下させるため、その上限を0.04%に制限することが好ましい。
ニッケル(Ni)は、オーステナイト相を安定化させるのに有効な元素であって、鋼板の強度を増加させるのに効果的な元素である。但し、その含量が0.05%未満で微量添加される場合には、上記の効果を得ることが困難であり、これに対し、1.0%を超える場合には、製造原価が増加するため非経済的である。したがって、本発明では、Niの含量を0.05〜1.0%に制限することが好ましい。
クロム(Cr)は、鋼板のめっき性を改善し強度を増加させるのに効果的な元素である。但し、その含量が0.05%未満の場合には、上述の効果を得ることが困難であり、これに対し、1.0%を超える場合には、製造原価が増加するため非経済的である。したがって、本発明では、Crの含量を0.05〜1.0%に制限することが好ましい。
スズ(Sn)は、上記クロム(Cr)と共に鋼板のめっき性を改善し強度を増加させるのに効果的な元素である。但し、その含量が0.01%未満の場合には、上述の効果を得ることが困難であり、これに対し、0.1%を超える場合には、製造原価が増加するため非経済的である。したがって、本発明では、Snの含量を0.01〜0.1%に制限することが好ましい。
チタン(Ti)は、炭素と結合して炭化物を形成する強炭化物元素であって、このときに形成された炭化物が結晶粒の成長を抑制することから結晶粒度の微細化に効果的な元素である。このTiは、ボロン(B)と複合添加される場合、柱状晶粒界に高温化合物を形成して粒界クラックを防止する。但し、その含量が0.005%未満で微量添加される場合には、上述の効果を得ることが困難である。これに対し、0.10%を超える場合には、過量のTiが結晶粒界に偏析して粒界脆化を起こしたり、析出相が過度に粗大化して結晶粒の成長効果を低下させる。したがって、本発明では、Tiの含量を0.005〜0.10%に制限することが好ましい。
ボロン(B)は、上記Tiと共に添加されて粒界の高温化合物を形成し、粒界クラックを防止する役割をする元素である。但し、このBの含量が0.0005%未満で微量添加される場合には、上述の効果を得ることが困難である。これに対し、0.0050%を超えると、ボロン化合物を形成してめっき性を低下させる。したがって、本発明では、Bの含量を0.0005〜0.0050%に制限することが好ましい。
本発明において高マンガン鋼のスラブを加熱して均質化処理するとき、加熱温度を1050〜1300℃に設定することが好ましい。
上記加熱によって均質化処理されたスラブに熱間圧延を施して鋼板に製造する。このとき、仕上げ熱間圧延の温度を850〜1000℃に設定することが好ましい。
上記熱間圧延された鋼板に熱延巻き取りを施す。このときの巻き取り温度は700℃以下であることが好ましい。
上述のような条件で熱間圧延を完了した後、鋼板の形状及び厚さを制御するために通常の条件で冷間圧延を行うことができる。このときの冷間圧下率は、顧客が求める厚さに合うように製造し、且つ強度及び延伸率を制御するための目的で30〜80%であることが好ましい。
上記冷間圧延された鋼板に連続焼鈍処理を施す。このときの連続焼鈍温度は400〜900℃であることが好ましい。これは、優れためっき性と高い強度を共に得るためである。
下記表1に示す成分系を有する鋼塊を1200℃の加熱炉で1時間維持した後、熱間圧延を行った。このときの熱間圧延仕上げ温度は900℃に設定し、熱間圧延後、650℃で巻き取りを行った。その後、上記熱延鋼板を利用して酸洗を行い、50%の冷間圧下率で冷間圧延を行った。その後、冷間圧延された試験片を焼鈍温度800℃、過時効温度400℃として連続焼鈍模擬熱処理を行った後、下記表2に示すように再圧延率を異ならせて再圧延を行った。
下記表3に示す成分系を有する鋼塊を1200℃の加熱炉で1時間維持した後、熱間圧延を行った。このときの熱間圧延仕上げ温度は900℃に設定し、熱間圧延後、650℃で巻き取りを行った。その後、上記熱延鋼板を利用して酸洗を行い、50%の冷間圧下率で冷間圧延を行った。その後、冷間圧延された試験片を焼鈍温度800℃、過時効温度400℃として連続焼鈍模擬熱処理を行った。また、上記冷延鋼板を上記と同じ条件で連続焼鈍模擬熱処理した後、溶融亜鉛浴の温度を460℃に設定して溶融亜鉛めっき模擬試験を行った。そして、上記と同じように連続焼鈍した鋼板に、下記表4に示すように再圧延率を異ならせて再圧延を施した。
下記表5に示す成分系を有する鋼塊を1200℃の加熱炉で1時間維持した後、熱間圧延を行った。このときの熱間圧延仕上げ温度は900℃に設定し、熱間圧延後、650℃で巻き取りを行った。その後、上記熱延鋼板を利用して酸洗を行い、50%の冷間圧下率で冷間圧延を行った。その後、冷間圧延された試験片を焼鈍温度800℃、過時効温度400℃として連続焼鈍模擬熱処理を行った。また、上記冷延鋼板を焼鈍温度800℃で連続焼鈍した後、溶融亜鉛浴の温度を460℃に設定して溶融亜鉛めっき模擬試験を行った。
Claims (10)
- 重量%で、炭素(C):0.4〜0.7%、マンガン(Mn):12〜24%、アルミニウム(Al):0.01〜3.0%、シリコン(Si):0.3%以下、リン(P):0.03%以下、硫黄(S):0.03%以下、窒素(N):0.04%以下と、残部鉄及びその他の不可避不純物とからなり、微細組織としてオーステナイト単相組織からなり、圧延方向の結晶粒の縦横比(b(圧延方向)/a(圧延方向の直角方向))が2以上となる結晶粒が70%以上であり、引張強度は1300MPa以上、降伏強度は1000MPa以上である、超高強度鋼板。
- 重量%で、炭素(C):0.4〜0.7%、マンガン(Mn):12〜24%、アルミニウム(Al):0.01〜3.0%、シリコン(Si):0.3%以下、リン(P):0.03%以下、硫黄(S):0.03%以下、窒素(N):0.04%以下、ニッケル(Ni):0.05〜1.0%、クロム(Cr):0.05〜1.0%及びスズ(Sn):0.01〜0.10%と、残部鉄及びその他の不可避不純物とからなり、微細組織としてオーステナイト単相組織からなり、圧延方向の結晶粒の縦横比(b(圧延方向)/a(圧延方向の直角方向))が2以上となる結晶粒が70%以上であり、引張強度は1300MPa以上、降伏強度は1000MPa以上である、超高強度鋼板。
- 重量%で、炭素(C):0.4〜0.7%、マンガン(Mn):12〜24%、アルミニウム(Al):0.01〜3.0%、シリコン(Si):0.3%以下、リン(P):0.03%以下、硫黄(S):0.03%以下、窒素(N):0.04%以下、チタン(Ti):0.005〜0.10%及びボロン(B):0.0005〜0.0050%と、ニッケル(Ni):0.05〜1.0%及びクロム(Cr):0.05〜1.0%のうち1種以上と、残部鉄及びその他の不可避不純物とからなり、微細組織としてオーステナイト単相組織からなり、圧延方向の結晶粒の縦横比(b(圧延方向)/a(圧延方向の直角方向))が2以上となる結晶粒が70%以上であり、引張強度は1300MPa以上、降伏強度は1000MPa以上である、超高強度鋼板。
- 前記鋼板は、冷延鋼板、溶融めっき鋼板、合金化溶融めっき鋼板及び電気めっき鋼板のうち1種である、請求項2または3に記載の超高強度鋼板。
- 前記鋼板の微細組織の平均粒度の大きさ(円相当径の平均値)が2〜10μmである、請求項1〜3のいずれか一項に記載の超高強度鋼板。
- 重量%で、炭素(C):0.4〜0.7%、マンガン(Mn):12〜24%、アルミニウム(Al):0.01〜3.0%、シリコン(Si):0.3%以下、リン(P):0.03%以下、硫黄(S):0.03%以下、窒素(N):0.04%以下であり、残部鉄及びその他の不可避不純物を含む鋼塊又は連鋳スラブを1050〜1300℃に加熱して均質化処理する段階と、
仕上げ熱間圧延温度を850〜1000℃として前記均質化処理された鋼塊又は連鋳スラブを熱間圧延する段階と、
前記熱間圧延された鋼板を200〜700℃で巻き取る段階と、
前記巻き取られた鋼板を30〜80%の冷間圧下率で冷間圧延する段階と、
前記冷間圧延された鋼板を400〜900℃で連続焼鈍処理する段階と、
前記連続焼鈍処理された鋼板を常温で30〜50%の圧延率で再圧延する段階と、
を含む、
微細組織としてオーステナイト単相組織からなり、前記再圧延後の圧延方向の結晶粒の横縦比(b(圧延方向)/a(圧延方向の直角方向))が2以上となる結晶粒が70%以上であり、引張強度は1300MPa以上、降伏強度は1000MPa以上である超高強度鋼板の製造方法。 - 前記鋼塊又は連鋳スラブは、ニッケル(Ni):0.05〜1.0%、クロム(Cr):0.05〜1.0%及びスズ(Sn):0.01〜0.10%をさらに含む、請求項6に記載の超高強度鋼板の製造方法。
- 前記鋼塊又は連鋳スラブは、チタン(Ti):0.005〜0.10%及びボロン(B):0.0005〜0.0050%をさらに含み、ニッケル(Ni):0.05〜1.0%及びクロム(Cr):0.05〜1.0%のうち1種以上をさらに含む、請求項6に記載の超高強度鋼板の製造方法。
- 前記焼鈍処理段階の後、電気めっき又は溶融めっき工程をさらに行う、請求項7または8に記載の超高強度鋼板の製造方法。
- 前記再圧延段階は、調質圧延、二重圧延、熱延精整及び連続圧延のうち一つの工程で行う、請求項6〜9のいずれか一項に記載の超高強度鋼板の製造方法。
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EP3095889A1 (en) * | 2015-05-22 | 2016-11-23 | Outokumpu Oyj | Method for manufacturing a component made of austenitic steel |
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WO2017203312A1 (en) * | 2016-05-24 | 2017-11-30 | Arcelormittal | Cold rolled and annealed steel sheet, method of production thereof and use of such steel to produce vehicle parts |
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WO2017203311A1 (en) * | 2016-05-24 | 2017-11-30 | Arcelormittal | Cold rolled and annealed steel sheet, method of production thereof and use of such steel to produce vehicle parts |
WO2017203310A1 (en) * | 2016-05-24 | 2017-11-30 | Arcelormittal | Method for producing a twip steel sheet having an austenitic microstructure |
WO2017203315A1 (en) | 2016-05-24 | 2017-11-30 | Arcelormittal | Cold rolled and annealed steel sheet, method of production thereof and use of such steel to produce vehicle parts |
WO2017203309A1 (en) * | 2016-05-24 | 2017-11-30 | Arcelormittal | Twip steel sheet having an austenitic matrix |
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- 2013-08-14 WO PCT/KR2013/007350 patent/WO2015023012A1/ko active Application Filing
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EP3034641B1 (en) | 2019-10-09 |
CN105473748A (zh) | 2016-04-06 |
EP3255170B1 (en) | 2021-03-31 |
EP3034641A4 (en) | 2016-11-16 |
US10144986B2 (en) | 2018-12-04 |
US20160186285A1 (en) | 2016-06-30 |
WO2015023012A1 (ko) | 2015-02-19 |
EP3255170A1 (en) | 2017-12-13 |
EP3034641A1 (en) | 2016-06-22 |
JP2016534224A (ja) | 2016-11-04 |
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