JPH0711024B2 - Manufacturing method of hot rolled steel and its material prediction method - Google Patents
Manufacturing method of hot rolled steel and its material prediction methodInfo
- Publication number
- JPH0711024B2 JPH0711024B2 JP2392190A JP2392190A JPH0711024B2 JP H0711024 B2 JPH0711024 B2 JP H0711024B2 JP 2392190 A JP2392190 A JP 2392190A JP 2392190 A JP2392190 A JP 2392190A JP H0711024 B2 JPH0711024 B2 JP H0711024B2
- Authority
- JP
- Japan
- Prior art keywords
- ferrite
- grain size
- calculated
- strain
- model
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P10/00—Technologies related to metal processing
- Y02P10/20—Recycling
Landscapes
- Heat Treatment Of Steel (AREA)
Description
【発明の詳細な説明】 〔産業上の利用分野〕 本発明は、熱間圧延、Ar3変態温度未満の温度域で全圧
延パスを行う際及びAr3変態温度以上の温度域から圧延
を開始しAr3変態温度未満のフェライト変態が生じる温
度域、つまりパーライト及びベーナイトの生じない温度
域で圧延を終了する熱間圧延の実施による厚板及びホッ
トストリップ等の鋼材の製造に際し、所要材質とその製
造条件に沿って生まれる組織構成との関係から材質値を
予測する方法およびその予測方法を利用した目標材質値
の鋼板を製造する方法に関するものである。BACKGROUND OF THE INVENTION [FIELD OF THE INVENTION The present invention, hot rolling, starting rolling from when and Ar 3 transformation temperature or higher temperature region of performing full rolling pass in a temperature range of less than Ar 3 transformation temperature In the temperature range in which ferrite transformation below the Ar 3 transformation temperature occurs, that is, in the production of steel materials such as thick plates and hot strips by carrying out hot rolling that terminates rolling in a temperature range in which pearlite and bainite do not occur, the required material and its The present invention relates to a method of predicting a material value from a relationship with a microstructure that is produced according to manufacturing conditions, and a method of manufacturing a steel sheet having a target material value using the predicting method.
従来、強度の推定モデルについては、成分、熱間圧延終
了温度、巻き取りもしくは冷却停止温度を変数にした簡
単な重回帰によるものがあるばかりで、ミクロ組織、フ
ェライト粒径等の影響が考慮されていない。このような
非厳密な重回帰モデルが使用に耐えたのは、モデルが一
つの圧延工場での製品のみを対象とし、その製造条件も
一定の加熱条件から開始され、変態前のオーステナイト
粒径を決める圧延終了温度を含む圧延条件は製品厚や成
分から、また変態挙動を支配する冷却温度域や冷却速度
も圧延終了温度と巻き取り温度から自動的に定まるとい
った強い拘束条件下で使用されていることによってい
る。Conventionally, strength estimation models are based on simple multiple regression using variables such as composition, hot rolling end temperature, coiling or cooling stop temperature, and the effects of microstructure, ferrite grain size, etc. are taken into consideration. Not not. The use of such an inexact multiple regression model is that the model is intended for products in one rolling mill only, the manufacturing conditions are also started from constant heating conditions, and the austenite grain size before transformation is determined. The rolling conditions including the rolling end temperature are determined based on the product thickness and composition, and the cooling temperature range and cooling rate that govern the transformation behavior are automatically determined from the rolling end temperature and the winding temperature. It depends.
このために従来のモデルは上記のような特定の条件下で
しか使用できず、他のラインへの適用や、広範に圧延条
件や、その後の冷却条件を変える事によって圧延材の材
質の範囲を拡大しようとする要請に答えられないもので
あった。For this reason, the conventional model can be used only under the specific conditions as described above, and the range of the material of the rolled material can be changed by applying it to other lines or widely changing the rolling condition and the cooling condition thereafter. I could not answer the request to expand.
これに対して、鋼材の材質をミクロ的な組織と対応づけ
て記述したモデルが従来よりある。鋼材の材質は一般に
ミクロ的な組織で決まる項と粒径で決まる項とその他の
強化機構の項で決まる項の和で表示出来る。On the other hand, there is a conventional model in which the material of the steel material is described in association with the microstructure. Generally, the material of steel can be expressed as the sum of the terms determined by the microstructure, the grain size, and the terms of other strengthening mechanisms.
例えば引っ張り強さ(TS)については式のように表示で
きることが知られている。For example, it is known that the tensile strength (TS) can be expressed as an equation.
TS=f(σf、σp、σb、σm、Vf、Vp、Vb、Vm、df)こ
こで、σは各組織の強度を示すパラメータであり、Vは
各組織の体積分率を表すパラメータでありdは粒径を表
す。TS = f (σ f , σ p , σ b , σ m , V f , V p , V b , V m , d f ), where σ is a parameter indicating the strength of each tissue, and V is each tissue Is a parameter showing the volume fraction of and d is the particle size.
また、添え字f、p、b、mは、それぞれフェライト、
パーライト、ベーナイト、マルテンサイトを示す。The subscripts f, p, b, and m are ferrite,
Indicates pearlite, bainite, martensite.
これらの知見に基づいて、鋼材の材質をミクロ的な組織
と対応づけて記述したモデルを用いて材質を調整する試
みは既に存在しており、例えば特公昭58−2246号公報、
特開昭59−67324号公報等に提案が行なわれている。Based on these findings, there is already an attempt to adjust the material using the model described by associating the material of the steel material with the microscopic structure, for example, Japanese Patent Publication No. 58-2246.
A proposal is made in Japanese Patent Laid-Open No. 59-67324.
特公昭58−2246号公報では冷却曲線から変態組織体積率
を求め、この変態組織体積率から鋼材の材質を予測する
方法について述べているが、組織の硬さ、粒径、熱間圧
延の効果に対する考慮が全く成されておらず、充分な精
度が出せないものである。Japanese Examined Patent Publication No. 58-2246 describes a method for obtaining a transformation structure volume ratio from a cooling curve and predicting the material quality of a steel material from this transformation structure volume ratio.The hardness of the structure, the grain size, and the effect of hot rolling are described. Is not considered at all, and sufficient accuracy cannot be obtained.
また特開昭59−67324号公報では実機圧延機の圧延荷重
から最終到達オーステナイト粒径、残留歪を計算し、そ
の後の冷却過程でフェライト粒径を計算し、フェライト
粒径と冷却速度により得られる組織強化パラメータによ
り強度を推定する方法について述べているが、ミクロ組
織の硬さ、体積率が考慮されていないので、充分な精度
が出せないものである。Further, in JP-A-59-67324, the final reached austenite grain size and residual strain are calculated from the rolling load of the actual rolling mill, and the ferrite grain size is calculated in the subsequent cooling process, which is obtained by the ferrite grain size and cooling rate. Although the method of estimating the strength by the tissue strengthening parameter is described, the hardness and volume fraction of the microstructure are not taken into consideration, so that sufficient accuracy cannot be obtained.
本発明者等はこれ等の課題を解決し、Ar3変態点以上で
の熱間圧延による鋼材の製造全般に所要材質とその製造
条件に沿って生まれる組織構成との関係から適用できる
製造方法を提供するものとして特開昭62−158816号公報
の提案を行なっている。しかし、含有Si量が0.1%以上
の領域では必ずしも、特開昭62−158816号公報の提案が
精度の良くない部分があったため、新たにAr3変態点以
上での熱間圧延においてSiを重量%で0.1%近傍を含む
炭素鋼に対してより精度よく、0.2%程度以上を含有す
る炭素鋼に対しては全く新しく適用出来る製造方法を提
供するものとして、特願昭63−127582号を提案した。The present inventors have solved these problems, a manufacturing method that can be applied from the relationship between the required material and the structure of the structure produced along with the manufacturing conditions in the overall manufacturing of steel by hot rolling at the Ar 3 transformation point or higher. A proposal of Japanese Patent Laid-Open No. 62-158816 is made as a provision. However, not necessarily in the region of 0.1% or more containing Si amount, since the proposal of JP-A-62-158816 there was a poor portion of the precision, the weight of Si in the hot rolling at the newly than the Ar 3 transformation point Japanese Patent Application No. 63-127582 is proposed to provide a manufacturing method that is more accurate for carbon steel containing around 0.1% in% and is completely new to carbon steel containing 0.2% or more. did.
上記の特開昭62−158816号公報および特開平1−298114
号の提案はAr3変態点以上での熱間圧延を行なう場合に
のみ適用出来る製造方法であり、圧延中に変態したフェ
ライトの結晶粒径変化や残留歪の計算を考慮していない
ため、Ar3変態温度以上からAr3変態温度未満に亘る熱間
圧延及びAr3変態点未満で熱間圧延を行なう場合には適
用出来ない。しかし、Ar3変態温度未満の温度域での熱
間圧延はフェライト粒の微細化をもたらした集合組織の
コントロールを可能にすることなどから非常に有用であ
り、このような場合に適用できる材質予測技術およびそ
の利用技術の開発が課題となっていた。JP-A-62-158816 and JP-A-1-298114 mentioned above.
The proposed method is a manufacturing method that can be applied only when hot rolling above the Ar 3 transformation point and does not take into account the calculation of the grain size change and residual strain of ferrite transformed during rolling. It cannot be applied to hot rolling from 3 transformation temperature to Ar 3 transformation temperature and hot rolling below Ar 3 transformation point. However, hot rolling in the temperature range below the Ar 3 transformation temperature is very useful because it enables control of the texture that has caused the refinement of ferrite grains, and the material prediction that can be applied in such cases The development of technology and its utilization technology has been an issue.
本発明の目的は、前記した従来技術の欠点を悉く解消
し、熱間圧延鋼材の材質を支配する冶金的な要因を介し
て少なくともAr3変態温度未満でフェライト変態が生じ
る温度域での圧延パスを含む熱間圧延を行なった熱間圧
延鋼材の材質を予測しての製造方法を提供するものであ
る。その基本的な手段は、 通常の炭素鋼の熱間鋳片を全圧延パスにおける圧延温
度がAr3変態温度未満でフェライト変態が生じる温度域
となる温度条件で熱間圧延した後冷却して熱間圧延鋼材
を製造するに際し、前記熱間圧延鋼材の鋼材条件、加熱
条件、圧延条件および冷却条件等の製造条件に基づい
て、予め定めた初期粒径モデルより加熱炉抽出時の圧延
前平均オーステナイト粒径doを求め、該doおよび前記製
造条件に基づいて予め定めたフェライト再結晶モデル、
フェライト変態モデル、フェライト変態時の粒径変換比
モデルを用いて、各圧延パス毎に、オーステナイト、フ
ェライトそれぞれの占積率、平均粒径および残留歪を計
算することにより、最終圧延パス後のオーステナイト、
フェライトそれぞれの占積率Xa、Xf、平均粒径a、
f、残留歪Δεa、Δεfを求め、該Xa、Xf、a、
f、Δεa、Δεfに基づいて予め定めた各組織(フェ
ライト、パーライト、ベーナイト、マルテンサイト)の
変態モデルおよび硬度モデルにより冷却完了後の各組織
それぞれの占積率、硬度を算出し、同時に予め定めたフ
ェライト変態時の粒径変換比モデルおよび取巻後のフェ
ライト粒成長モデルを用いて最終平均フェライト粒径を
算出し、該最終平均フェライト粒径と各組織それぞれの
占積率及び硬度から予め定めた材質モデルより前記熱間
圧延鋼材の材質予測値を計算することを特徴とする熱間
圧延鋼材の製造方法。The object of the present invention is to eliminate the drawbacks of the prior art described above, through a metallurgical factor controlling the material of the hot rolled steel material, at least a rolling pass in a temperature range where ferrite transformation occurs below the Ar 3 transformation temperature. The present invention provides a manufacturing method for predicting the material quality of a hot rolled steel material that has been hot rolled including. The basic unit is cooled after hot rolling at a temperature where the conventional hot slab of carbon steel rolling temperature in all rolling pass is temperature range where ferrite transformation occurs in less than Ar 3 transformation temperature heat During the production of hot-rolled steel, based on manufacturing conditions such as steel conditions of the hot-rolled steel, heating conditions, rolling conditions and cooling conditions, average austenite before rolling at the time of furnace extraction from a predetermined initial grain size model The grain size do is determined, and a ferrite recrystallization model determined in advance on the basis of the do and the manufacturing conditions,
Austenite after the final rolling pass is calculated by calculating the space factor, average grain size and residual strain of austenite and ferrite for each rolling pass using the ferrite transformation model and the grain size conversion ratio model during ferrite transformation. ,
Space factor Xa , Xf , average grain size a , of each ferrite
f , residual strains Δε a , Δε f are calculated, and the X a , X f , a ,
Based on f , Δε a , and Δε f , the space factor and hardness of each structure after completion of cooling are calculated by the transformation model and hardness model of each structure (ferrite, pearlite, bainite, martensite) determined in advance and at the same time. A final average ferrite grain size is calculated using a predetermined grain size conversion ratio model during ferrite transformation and a ferrite grain growth model after winding, and from the final average ferrite grain size and the space factor and hardness of each structure. A method of manufacturing a hot rolled steel product, comprising calculating a material predictive value of the hot rolled steel product from a predetermined material model.
前記熱間圧延鋳片を全圧延パスにおいて圧延温度がAr
3変態温度未満でフェライト変態が生じる温度域で熱間
圧延を行なう場合、各圧延パスでは、予め定めたフェラ
イト変態モデルを用いて前パス以後に変態したフェライ
トの占積率を求め、全フェライトおよび全オーステナイ
トの占積率を計算し、オーステナイトの部分については
前記オーステナイト再結晶モデルを用いて前記各グルー
プの平均粒径と残留歪を求め、フェライトの部分につい
ては、前パス以後に変態したフェライトについて粒径変
換比モデルを用いて該フェライトの平均粒径を求め、該
フェライトの残留歪を零とし、該フェライトと前パス以
前に変態したフェライトとの平均フェライト粒径および
平均残留歪を求め、該フェライト粒径を該パスの入側粒
径とし、該平均残留歪を入側残留歪とし、該パスの付加
歪に該入側残留歪を加えた実効歪が再結晶の限界歪より
も大きい場合は、再結晶、未再結晶の2つのグループに
分け、該実効歪が該限界歪よりも小さい場合は、未再結
晶グループのみとし、前記入側粒径、前記実効歪および
前記製造条件より、予め定めたフェライト再結晶モデル
を用いて各グループにおける占積率および平均粒径を計
算し、各パス毎に平均フェライト粒径および残留歪を繰
り返し計算し、最終圧延パス後のオーステナイト及びフ
ェライトそれぞれの占積率、平均粒径及び残留歪を求
め、その後は、該各計算値より冷却完了後の各組織(フ
ェライト、パーライト、ベーナイト、マルテンサイト)
それぞれの体積率、硬度を算出し、同時に最終平均フェ
ライト粒径を算出することを特徴とする請求項1に記載
の熱間圧延鋼材の製造方法。The rolling temperature of the hot rolled slab is Ar in all rolling passes.
When performing hot rolling in a temperature range where ferrite transformation occurs below 3 transformation temperatures, in each rolling pass, the space factor of ferrite transformed after the previous pass is calculated using a predetermined ferrite transformation model, and all ferrite and Calculate the space factor of all austenite, the average grain size and residual strain of each group using the austenite recrystallization model for the austenite portion, for the ferrite portion, for the ferrite transformed after the previous pass The average grain size of the ferrite is determined using a grain size conversion ratio model, the residual strain of the ferrite is set to zero, the average ferrite grain size and the average residual strain of the ferrite and the ferrite transformed before the previous pass are determined, Let the ferrite grain size be the inlet side grain size of the path, the average residual strain be the inlet side residual strain, and the inlet side residual strain to be the additional strain of the pass. When the added effective strain is larger than the critical strain of recrystallization, it is divided into two groups of recrystallized and unrecrystallized, and when the effective strain is smaller than the critical strain, only the unrecrystallized group is used. From the entry side grain size, the effective strain and the manufacturing conditions, the space factor and the average grain size in each group were calculated using a predetermined ferrite recrystallization model, and the average ferrite grain size and the residual strain were calculated for each pass. Repeatedly calculated, the space factor of each of the austenite and ferrite after the final rolling pass, the average grain size and the residual strain are determined, and thereafter, the microstructures after completion of cooling (ferrite, pearlite, bainite, martensite) from the calculated values. )
The method for producing a hot-rolled steel product according to claim 1, wherein each volume ratio and hardness are calculated, and at the same time, the final average ferrite grain size is calculated.
フェライトの部分についての平均粒径及び残留歪を計
算するにあたり、前記実効歪εが(1)式で与えられるε
mよりも大きい場合には、再結晶及び未再結晶の2つの
グループに分け、圧延直後での再結晶占積率ffDおよび
粒径dfDを(2)(3)式を用いて求め、その後に再結晶した
部分の占積率ffSを(4)式から計算し、パス間での再結晶
粒径の変化を(5)式から求め、未再結晶領域の占積率ffN
および粒径dfNを(6)(7)式で計算し、実効歪εがεmよ
りも小さい場合には、未再結晶領域の占積率ffNおよび
粒径dfNのみを(6)(7)式から計算し、次パス直前の平均
フェライト粒径fを(8)式で計算し、パス間での歪の
回復を考慮して次パス直前の残留歪Δεを(9)式を用い
て計算することを特徴とする請求項2に記載の熱間圧延
鋼材の製造方法。In calculating the average grain size and residual strain of the ferrite part, the effective strain ε is given by the formula (1).
When it is larger than m, it is divided into two groups, recrystallized and non-recrystallized, and the recrystallization space factor f fD and the grain size d fD immediately after rolling are obtained by using the equations (2) and (3), Then, the space factor f fS of the recrystallized portion is calculated from the equation (4), the change in the recrystallized grain size between the passes is obtained from the equation (5), and the space factor f fN of the unrecrystallized region is calculated.
And the grain size d fN are calculated by the equations (6) and (7), and when the effective strain ε is smaller than ε m , only the space factor f fN of the unrecrystallized region and the grain size d fN are (6) Calculated from Eq. (7), the average ferrite grain size f immediately before the next pass is calculated by Eq. (8), and the residual strain Δε immediately before the next pass is given by Eq. (9) considering the recovery of strain between passes. It calculates using, The manufacturing method of the hot rolling steel material of Claim 2 characterized by the above-mentioned.
εm=h(dfi,,T) (1) ffD=h(dfi,ε,,T) (2) dfD=h(dfi,ε,T) (3) ffS=h(ε,T,t) (4) dfS=h(dfD,T,t) (5) ffN=h(ffD,ffS) (6) dfN=h(dfi,ε) (7)f =h(ffD,ffS,ffN,dfS,dfN) (8) Δεf=h(ffD,ffN,εm,ε,T,(%C)) (9) ここで、dfiはパス入側のフェライト粒径(μm)、
は歪速度(s-1)、Tは圧延温度(℃)、εは加工歪、
tは加工後の時間(秒)、(%C)は炭素含有量(重量
%)。ε m = h (d fi ,, T) (1) f fD = h (d fi , ε ,, T) (2) d fD = h (d fi , ε, T) (3) f fS = h ( ε, T, t) (4) d fS = h (d fD , T, t) (5) f fN = h (f fD , f fS ) (6) d fN = h (d fi , ε) (7 ) f = h (f fD , f fS , f fN , d fS , d fN ) (8) Δε f = h (f fD , f fN , ε m , ε, T, (% C)) (9) where And d fi is the ferrite grain size (μm) on the path entry side,
Is strain rate (s -1 ), T is rolling temperature (° C), ε is working strain,
t is the time after processing (seconds), (% C) is the carbon content (% by weight).
通常の炭素鋼の熱間鋳片をAr3変態温度以上の温度域
から圧延を開始しAr3変態温度未満の温度域で圧延を終
了した後冷却して熱間圧延鋼材を製造するに際し、前記
熱間圧延鋼材の鋼材条件、加熱条件、圧延条件および冷
却条件等の製造条件に基づいて、予め定めた初期粒径モ
デルより加熱炉抽出時の圧延前平均オーステナイト粒径
doを求め、該doおよび前記製造条件に基づいて予め定め
たオーステナイト再結晶モデル、フェライト再結晶モデ
ル、フェライト変態モデル、フェライト変態時の粒径変
態比モデルを用いて、Ar3変態温度以上の温度域におけ
る圧延パスではオーステナイトの平均粒径および残留歪
を計算し、Ar3変態温度未満の温度域における圧延パス
ではオーステナイト、フェライトそれぞれの占積率、平
均粒径および残留歪を計算することにより、最終圧延パ
ス後のオーステナイト、フェライトそれぞれの占積率
Xa、Xf、平均粒径a、f、残留歪Δεa、Δεfを
求め、該Xa、Xf、a、f、Δεa、Δεfに基づい
て予め定めた各組織(フェライト、パーライト、ベーナ
イト、マルテンサイト)の変態モデルおよび硬度モデル
により冷却完了後の各組織それぞれの占積率、硬度を算
出し、同時に予め定めたフェライト変態時の粒径変換比
モデルおよび取巻後のフェライト粒成長モデルを用いて
最終平均フェライト粒径を算出し、該最終平均フェライ
ト粒径と各組織それぞれの占積率及び硬度から予め定め
た材質モデルより前記熱間圧延鋼材の材質予測値を計算
し、該材質予測値と材質目標値とが一致するように前記
製造条件の一部を修正し、修正後の製造条件に基づいて
熱間鋼材を製造して目標材質を得ることを特徴とする熱
間圧延鋼材の製造方法。When producing a hot-rolled steel product, the hot cast slab of ordinary carbon steel is rolled from a temperature range of Ar 3 transformation temperature or higher and finished rolling in a temperature range of less than Ar 3 transformation temperature and then cooled to produce a hot rolled steel material, Average austenite grain size before rolling when extracting the heating furnace from a predetermined initial grain size model based on manufacturing conditions such as steel material conditions, heating conditions, rolling conditions and cooling conditions of hot rolled steel products
Obtaining do, using an austenite recrystallization model, a ferrite recrystallization model, a ferrite transformation model, and a grain size transformation ratio model at the time of ferrite transformation, which are predetermined based on the do and the manufacturing conditions, and a temperature of Ar 3 transformation temperature or higher. In the rolling pass in the region, the average grain size and residual strain of austenite are calculated, and in the rolling pass in the temperature region below the Ar 3 transformation temperature, austenite, the space factor of each ferrite, by calculating the average grain size and residual strain, Space factor of austenite and ferrite after the final rolling pass
Xa , Xf , average grain diameters a , f , residual strains Δε a , Δε f are determined, and the respective textures (ferrite, predetermined) based on the X a , X f , a , f , Δε a , Δε f are determined. The space factor and hardness of each structure after cooling is calculated by the transformation model of pearlite, bainite, martensite) and hardness model, and at the same time, the grain size conversion ratio model at the time of ferrite transformation and the ferrite after surrounding The final average ferrite grain size is calculated using a grain growth model, and the material prediction value of the hot-rolled steel is calculated from the material model determined in advance from the final average ferrite grain size and the space factor and hardness of each structure. A part of the manufacturing conditions is corrected so that the predicted value of the material and the target value of the material match, and the hot steel is manufactured based on the corrected manufacturing conditions to obtain the target material. Of cold rolled steel .
鋼材温度がAr3変態温度以上の温度域における圧延パ
スでは、オーステナイトの平均粒径および残留歪を計算
し、鋼材温度がAr3変態温度未満の温度域の圧延パスで
は、予め定めたフェライト変態モデルを用いて前パス以
後に変態したフェライトの占積率を求め、全フェライト
および全オーステナイトの占積率を計算し、オーステナ
イトの部分については前記オーステナイト再結晶モデル
を用いて前記各グループの平均粒径と残留歪を求め、フ
ェライトの部分については、前パス以後に変態したフェ
ライトについて粒径変換比モデルを用いて該フェライト
の平均粒径を求め、該フェライトの残留歪を零とし、該
フェライトと前パス以前に変態したフェライトとの平均
フェライト粒径および平均残留歪を求め、該フェライト
粒径を該パスの入側粒径とし、該平均残留歪を入側残留
歪とし、該パスの付加歪に該入側残留歪を加えた実効歪
が再結晶の限界歪よりも大きい場合は、再結晶、未再結
晶の2つのグループに分け、該実効歪が該限界歪よりも
小さい場合は、未再結晶グループのみとし、前記入側粒
径、前記実効歪および前記製造条件より、予め定めたフ
ェライト再結晶モデルを用いて各グループにおける占積
率および平均粒径を計算し、各パス毎に平均フェライト
粒径および残留歪を繰り返し計算し、最終圧延パス後の
オーステナイト及びフェライトそれぞれの占積率、平均
粒径及び残留歪を求め、その後は、該各計算値より冷却
完了後の各組織(フェライト、パーライト、ベーナイ
ト、マルテンサイト)それぞれの体積率、硬度を算出
し、同時に最終平均フェライト粒径を算出することを特
徴とする請求項4に記載の熱間圧延鋼材の製造方法。The rolling pass steel temperature in the Ar 3 transformation temperature or higher temperature range, the average particle size and residual strain of austenite was calculated, in the rolling pass temperature range below the steel temperature is Ar 3 transformation temperature, a predetermined ferrite transformation model Obtain the space factor of the ferrite transformed after the previous pass using, calculate the space factor of all ferrite and all austenite, for the austenite portion using the austenite recrystallization model the average grain size of each group For the ferrite part, the average grain size of the ferrite was determined using the grain size conversion ratio model for the ferrite transformed after the previous pass, and the residual strain of the ferrite was set to zero, and The average ferrite grain size and average residual strain of the ferrite transformed before the pass are calculated, and the ferrite grain size is calculated as the entrance grain of the pass. If the effective strain obtained by adding the input residual strain to the additional strain of the path is larger than the critical strain of recrystallization, the average residual strain is defined as the input residual strain. When divided into groups, when the effective strain is smaller than the critical strain, only the non-recrystallized group is used, and from the entrance side grain size, the effective strain, and the manufacturing conditions, a predetermined ferrite recrystallization model is used. The space factor and average grain size in the group are calculated, the average ferrite grain size and residual strain are repeatedly calculated for each pass, and the space factor, average grain size and residual strain of austenite and ferrite after the final rolling pass are calculated. Then, the volume ratio and hardness of each structure (ferrite, pearlite, bainite, martensite) after completion of cooling are calculated from the calculated values, and at the same time, the final average ferrite grain size is calculated. The method for manufacturing a hot-rolled steel product according to claim 4, characterized in that.
フェライトの部分についての平均粒径及び残留歪を計
算するにあたり、前記実効歪εが(1)式で与えられるε
mよりも大きい場合には、再結晶及び未再結晶の2つの
グループに分け、圧延直後での再結晶占積率ffDおよび
粒径dfDを(2)(3)式を用いて求め、その後に再結晶した
部分の占積率ffSを(4)式から計算し、パス間での再結晶
粒径の変化を(5)式から求め、未再結晶領域の占積率ffN
および粒径dfNを(6)(7)式で計算し、実効歪εがεmよ
りも小さい場合には、未再結晶領域の占積率ffNおよび
粒径dfNのみを(6)(7)式から計算し、次パス直前の平均
フェライト粒径fを(8)式で計算し、パス間での歪の
回復を考慮して次パス直前の残留歪Δεを(9)式を用い
て計算することを特徴とする請求項5に記載の熱間圧延
鋼材の製造方法。In calculating the average grain size and residual strain of the ferrite part, the effective strain ε is given by the formula (1).
When it is larger than m, it is divided into two groups, recrystallized and non-recrystallized, and the recrystallization space factor f fD and the grain size d fD immediately after rolling are obtained by using the equations (2) and (3), Then, the space factor f fS of the recrystallized portion is calculated from the equation (4), the change in the recrystallized grain size between the passes is obtained from the equation (5), and the space factor f fN of the unrecrystallized region is calculated.
And the grain size d fN are calculated by the equations (6) and (7), and when the effective strain ε is smaller than ε m , only the space factor f fN of the unrecrystallized region and the grain size d fN are (6) Calculated from Eq. (7), the average ferrite grain size f immediately before the next pass is calculated by Eq. (8), and the residual strain Δε immediately before the next pass is given by Eq. (9) considering the recovery of strain between passes. It calculates using, The manufacturing method of the hot rolling steel material of Claim 5 characterized by the above-mentioned.
εm=h(dfi,,T) (1) ffD=h(dfi,ε,,T) (2) dfD=h(dfi,ε,T) (3) ffS=h(ε,T,t) (4) dfS=h(dfD,T,t) (5) ffN=h(ffD,ffS) (6) dfN=h(dfi,ε) (7)f =h(ffD,ffS,ffN,dfS,dfN) (8) Δεf=h(ffD,ffN,εm,ε,T,(%C)) (9) ここで、dfiはパス入側のフェライト粒径(μm)、
は歪速度(s-1)、Tは圧延温度(℃)、εは加工歪、
tは加工後の時間(秒)、(%C)は炭素含有量(重量
%)である。ε m = h (d fi ,, T) (1) f fD = h (d fi , ε ,, T) (2) d fD = h (d fi , ε, T) (3) f fS = h ( ε, T, t) (4) d fS = h (d fD , T, t) (5) f fN = h (f fD , f fS ) (6) d fN = h (d fi , ε) (7 ) f = h (f fD , f fS , f fN , d fS , d fN ) (8) Δε f = h (f fD , f fN , ε m , ε, T, (% C)) (9) where And d fi is the ferrite grain size (μm) on the path entry side,
Is strain rate (s -1 ), T is rolling temperature (° C), ε is working strain,
t is a time (second) after processing, and (% C) is a carbon content (% by weight).
まず、本発明の適用可能な通常の炭素鋼の成分を基準す
ると、重量%でC:0.02〜0.4%、Mn:0.2〜1.2%、Si≦2
%を必ず含んで特別な合金元素は添加されていないもの
とする。First, based on the components of a normal carbon steel to which the present invention is applicable, C: 0.02 to 0.4%, Mn: 0.2 to 1.2%, and Si ≤ 2 by weight%.
% Is always included and no special alloying element is added.
以下に本発明における材質計算方法の説明及びその作用
について述べる。The description of the material calculation method and the operation thereof according to the present invention will be described below.
熱間圧延鋼材の材質は成分のみならず圧延条件、冷却条
件等の製造条件により変化する。鋼材の材質が鋼材のミ
クロ組織と対応付けられることから、ミクロ組織を介す
るとにより製造条件から材質を予測するモデルが従来よ
り構築されている(特開昭−62−158816号および特開平
1−298114号を参照)。その従来モデルはAr3変態温度
以上での圧延のみを行なうことを前提としており、最終
的な熱間圧延鋼材のミクロ組織を予測するモデルとその
ミクロ組織から材質を予測するモデルの2つから構成さ
れている。第3図はこの従来モデルにおける計算の流れ
図を示している。以後の従来モデルの説明におていは、
第3図を参照されたい。The material of the hot rolled steel material varies depending not only on the composition but also on manufacturing conditions such as rolling conditions and cooling conditions. Since the material of the steel material is associated with the microstructure of the steel material, a model for predicting the material from the manufacturing conditions by using the microstructure has been conventionally constructed (JP-A-62-158816 and JP-A-1-158816). See 298114). The conventional model is premised on rolling only at the Ar 3 transformation temperature or higher, and is composed of two models: a model for predicting the final microstructure of hot-rolled steel and a model for predicting the material from that microstructure. Has been done. FIG. 3 shows a flow chart of calculation in this conventional model. In the following explanation of the conventional model,
See FIG.
ミクロ組織を予測するには、まず、鋼材の成分と加熱炉
での加熱条件を基にして(10)式で示される初期オーステ
ナイト粒径モデルにより加熱炉抽出後のオーステナイト
粒径daoを計算し、その値と鋼材の成分や各パスでの圧
延条件を基にして(11)〜(21)式で示されるオーステナイ
ト再結晶モデルより、各パス毎に圧延後の平均オーステ
ナイト粒径aiおよび残留歪Δεiを計算し、それを繰
り返して最終圧延パス後の平均オーステナイト粒径およ
び残留歪を求める。更に、その後の冷却工程に対応し
て、最終圧延パス後の平均オーステナイト粒径および残
留歪と鋼材の成分、冷却条件を基にして(22)式で示され
るフェライト変態モデル、(23)式で示されるパーライト
変態モデルおよび(24)式で示されるベーナイト変態モデ
ルにより各組織の占積率を求め、残りの部分をマルテン
サイトの占積率として求め、同時に、(25)〜(27)式で示
される各組織の硬度モデルから各組織の硬度を求める。
また、オーステナイトからフェライトに変態する時に粒
径が変化するので、最終圧延パス後の平均オーステナイ
ト粒径および残留歪とフェライト占積率、冷却条件より
求めたAr3変態温度を基にして(28)式で示される粒径変
換比モデルより変態直後のフェライト粒径を求め、更に
取巻後の粒成長を考慮に入れ、変態直後のフェライト粒
径および巻取温度を基にして(29)式で示される取巻後の
粒成長モデルから最終フェライト粒径を求める。以上の
ようにして求めたミクロ組織の各因子(各組織の占積率
・硬さ、最終フェライト粒径)を基にして、(30)〜(32)
式で示される材質モデルより最終的な熱間圧延鋼材の材
質値(引張強さ、降伏応力、全伸び)を予測する。To predict the microstructure, first calculate the austenite grain size d ao after the furnace extraction by the initial austenite grain size model shown in Eq. (10) based on the steel composition and the heating conditions in the furnace. , The average austenite grain size ai and residual strain after rolling for each pass based on the austenite recrystallization model shown in Eqs. (11) to (21) based on the value and the steel composition and rolling conditions in each pass. Δε i is calculated and repeated to obtain the average austenite grain size and residual strain after the final rolling pass. Further, corresponding to the subsequent cooling step, the average austenite grain size and residual strain after the final rolling pass and the components of the steel material, the ferrite transformation model shown in the formula (22) based on the cooling conditions, in the formula (23) The space factor of each structure is obtained by the pearlite transformation model shown and the bainite transformation model shown in Eq. (24), and the remaining portion is obtained as the space factor of martensite, and at the same time, in Eqs. (25) to (27). The hardness of each tissue is determined from the hardness model of each tissue shown.
Further, since the grain size changes when transforming from austenite to ferrite, based on the average austenite grain size after the final rolling pass and residual strain and ferrite space factor, Ar 3 transformation temperature obtained from cooling conditions (28) The ferrite grain size immediately after transformation is calculated from the grain size conversion ratio model shown in the equation, and further, taking into consideration the grain growth after winding, based on the ferrite grain size immediately after transformation and the winding temperature, The final ferrite grain size is determined from the grain growth model after winding shown. Based on the factors of the microstructure (space factor / hardness of each structure, final ferrite grain size) obtained as described above, (30) to (32)
Predict the final material value (tensile strength, yield stress, total elongation) of the hot-rolled steel from the material model represented by the formula.
しかし、このモデルの場合は第2図(a)において圧延パ
スを鋸歯状に示したように最終圧延パスにおいてもAr3
変態点以上の温度で熱間圧延を行なうことを前提として
おり、第2図(b)の(I)に示したようにAr3変態温度以
上の温度域から圧延を開始し、Ar3変態点未満のフェラ
イト変態が生じる温度域で圧延を終了する熱間圧延を行
なう場合に適用した場合には、及び第2図(b)の(II)
や(III)に示すように全圧パスの圧延温度がAr3変態温
度未満の温度域の場合には従来のモデルでは圧延中に生
成したフェライトの再結晶や粒成長などの挙動を計算で
きないため、材質予測精度は極端に悪化していた。そこ
で本発明者等が考えた結果、Ar3変態点未満のフェライ
ト変態が生じる温度域での熱間圧延の材質変化も精度良
く予測するためには、フェライト域での再結晶、粒成
長、静的回復挙動をそれぞれ定式化し、圧延後の平均フ
ェライト粒径および残留歪を求めるフェライト再結晶モ
デルを新たに作成する必要がある。当発明者等はそのフ
ェライト再結晶モデルを作成するために、各種成分の鋼
材を種々な加工条件にて熱間加工しその冶金的ミクロ組
織を解析して、その因果関係を探索したのである。However, Ar 3 is also in the final rolling pass as shown rolling path serrated in Figure 2 in the case of this model (a)
Has assumed to perform hot rolling at lower than the transformation point temperature, rolling from Ar 3 transformation temperature or higher temperature range to start as shown in the second diagram of (b) (I), Ar 3 transformation point When applied when performing hot rolling that terminates rolling in the temperature range in which ferrite transformation below occurs, and (II) in Fig. 2 (b)
As shown in (III) and (III), when the rolling temperature in the total pressure pass is in the temperature range below the Ar 3 transformation temperature, the conventional model cannot calculate the behavior such as recrystallization and grain growth of the ferrite generated during rolling. However, the accuracy of material prediction was extremely poor. Therefore, as a result of consideration by the present inventors, in order to accurately predict the material change of hot rolling in a temperature range in which ferrite transformation below the Ar 3 transformation point occurs, recrystallization in the ferrite zone, grain growth, and static It is necessary to formulate the respective dynamic recovery behavior and newly create a ferrite recrystallization model for obtaining the average ferrite grain size and residual strain after rolling. In order to create the ferrite recrystallization model, the present inventors hot-worked steel materials of various components under various processing conditions, analyzed their metallurgical microstructures, and searched for their causal relationship.
その工夫点は圧延後の平均粒径および残留歪を求めるた
めに、フェライト再結晶モデルとこれまでの各モデルと
を組み合わせなければならない点にあった。その計算の
流れ図を第1図に示す。その計算方法について説明す
る。Ar3変態温度以上での熱間圧延パスでは、従来のオ
ーステナイト再結晶モデルのみを用いて平均オーステナ
イト粒径および残留歪を求める。圧延温度がAr3変態温
度未満の圧延パスは(但し、パーライト及びベーナイト
が生じない温度域)、まず、歪誘起変態の効果を取り込
んでいる従来のフェライト変態モデルを用いてフェライ
ト占積率を計算し、オーステナイト占積率を1からフェ
ライト占積率を差し引くことにより求め、次に粒径変換
比をモデルを用いて前パス以後に変態した変態直後のフ
ェライトの粒径を求める。オーステナイトの部分につい
てはオーステナイト再結晶モデルを用いて平均オーステ
ナイト粒径および残留歪を求め、フェライトの部分につ
いては新規に見出したフェライト再結晶モデルを用いて
平均フェライト粒径および残留歪を求める。この際、フ
ェライトが最初に生成した直後の圧延パスでは粒径変換
比モデルを用いて計算した変態直後のフェライト粒径を
入側粒径とし入側残留歪は零とし、その後の圧延パスで
は前パスまでに生成した歪を受けたフェライトと前パス
以後に新しく生成した変態直後のフェライトとの平均粒
径および平均残留歪を、それぞれ入側粒径および入側残
留歪とする。以上の計算を最終圧延パスまで繰り返し
て、最終圧延パス後全パスによるオーステナイト、フェ
ライトそれぞれの平均粒径および残留歪を求めて、その
後は変態モデル以降につなげる。The ingenuity was that the ferrite recrystallization model and each of the previous models had to be combined in order to obtain the average grain size and residual strain after rolling. The flow chart of the calculation is shown in FIG. The calculation method will be described. In the hot rolling pass above the Ar 3 transformation temperature, the average austenite grain size and residual strain are determined using only the conventional austenite recrystallization model. For the rolling pass where the rolling temperature is below the Ar 3 transformation temperature (however, in the temperature range where pearlite and bainite do not occur), first calculate the ferrite space factor using the conventional ferrite transformation model that incorporates the effect of strain-induced transformation. Then, the austenite space factor is determined by subtracting the ferrite space factor from 1, and then the grain size conversion ratio is used to determine the grain size of ferrite immediately after transformation transformed after the previous pass using a model. For the austenite part, the average austenite grain size and residual strain are determined using the austenite recrystallization model, and for the ferrite part, the newly found ferrite recrystallization model is used to determine the average ferrite grain size and residual strain. At this time, in the rolling pass immediately after the ferrite was first formed, the ferrite grain size immediately after transformation calculated using the grain size conversion ratio model was set as the inlet side grain size and the inlet side residual strain was set to zero, and in the subsequent rolling passes, The average grain size and the average residual strain of the ferrite that has undergone strain generated up to the pass and the ferrite that has newly generated after the previous pass and has just undergone transformation are referred to as the inlet side grain size and the inlet side residual strain, respectively. The above calculation is repeated up to the final rolling pass to obtain the average grain size and residual strain of austenite and ferrite by all passes after the final rolling pass, and then connect to the transformation model and thereafter.
以下はフェライト再結晶モデルについて説明する。フェ
ライトの場合、従来より動的再結晶は起こさないことが
定説とされてきたが、本発明者等は圧縮型熱間加工シミ
ュレータによる熱間加工後即冷を行なった実験により、
熱間加工直後でも再結晶が生じることを発見した。この
再結晶組織は動的再結晶組織と静的再結晶組織の混合組
織であると考えられる。この再結晶は実効歪が(1)式で
示す臨界歪εmよりも大きい場合に生じ、その再結晶占
積率ffDは(2)式で表せる。なお、実効歪とは、その圧延
パスでの付加歪にそれ以前の圧延パスによる残留歪を加
えた実効的な歪であり、残留歪がある場合には、この実
効歪を計算に用い必要がある。εmは初期粒径が大きい
ほど、歪速度が大きいほど、圧延温度が低いほど大き
く、また、ffDは初期粒径が小さいほど、歪が大きいほ
ど、圧延温度が高いほど大きくなる。また、この圧延直
後に生じた再結晶の再結晶粒径dfDは付加歪が大きいほ
ど、初期粒径が小さいほど、温度が低いほど細粒とな
り、(3)式で示すことが出来る。The ferrite recrystallization model will be described below. In the case of ferrite, it has been conventionally established that dynamic recrystallization does not occur, but the inventors of the present invention conducted an immediate cooling after hot working using a compression type hot working simulator,
It was discovered that recrystallization occurs even immediately after hot working. This recrystallization structure is considered to be a mixed structure of dynamic recrystallization structure and static recrystallization structure. This recrystallization occurs when the effective strain is larger than the critical strain ε m shown in equation (1), and the recrystallization space factor f fD can be expressed by equation (2). The effective strain is the effective strain obtained by adding the residual strain of the rolling pass before that to the additional strain of the rolling pass.If there is residual strain, it is necessary to use this effective strain for calculation. is there. ε m increases as the initial grain size increases, the strain rate increases, and the rolling temperature decreases, and f fD increases as the initial grain size decreases, the strain increases, and the rolling temperature increases. Further, the recrystallized grain size d fD of the recrystallization generated immediately after this rolling becomes finer as the additional strain is larger, the initial grain size is smaller, and the temperature is lower, which can be expressed by the formula (3).
この圧延直後に生じる再結晶が生じた場合、等価保持す
るとそれに引き続いてその後も静的に再結晶占積率が増
加するが、その速度は歪が大きいほど、圧延温度が高い
ほど速く、その増加分ffSは(4)式で示せる。その時の粒
径の成長速度は温度が高いほど速く、(5)式で表せる。If recrystallization that occurs immediately after this rolling occurs, the recrystallization space factor will statically increase after that when it is held equivalent, but the speed increases as the strain increases and the rolling temperature increases, and the increase increases. The minute f fS can be expressed by equation (4). The growth rate of the grain size at that time is higher as the temperature is higher, and can be expressed by equation (5).
再結晶をしなかった部分は未再結晶部分として、その占
積率ffNは(6)式で表せ、粒径dfNは偏平化の効果を取り
込んで(7)式で表現できる。The portion that has not been recrystallized is an unrecrystallized portion, and the space factor f fN can be expressed by equation (6), and the grain size d fN can be expressed by equation (7) by incorporating the effect of flattening.
従って、付加歪が再結晶の限界εmよりも大きい場合
は、再結晶領域と未再結晶領域の2つのグループに分け
てそれぞれの占積率および粒径を計算し、付加歪がεm
よりも小さい場合は再結晶が生じないので、未再結晶域
の粒径のみを計算するものである。そして、圧延後の時
間tを経過した時の平均フェライト粒径aは、各再結
晶の形態に属する粒の占める占積率及び時間tの間に成
長した各結晶粒の粒径を用いて2次元平均を用い(8)式
で計算する。Therefore, when the additional strain is larger than the recrystallization limit ε m , the space factor and the grain size of each of the two groups of the recrystallized region and the non-recrystallized region are calculated, and the additional strain is ε m.
If it is smaller than this, recrystallization does not occur, so only the grain size in the non-recrystallized region is calculated. The average ferrite grain size a after a lapse of time t after rolling is calculated by using the space factor occupied by grains belonging to each recrystallization form and the grain size of each crystal grain grown during the time t. Calculate using equation (8) using the dimensional average.
またこの時間tの間の歪の解放については、加工直後に
再結晶した粒内には平均としてεm、その後再結晶した
結晶粒には零、未再結晶粒には実効歪が残り、更にそれ
らの歪は時間tの間に静的に回復するとして(9)式で計
算され、それらの合計から残留歪Δεを求めることが出
来る数式モデルを新たに見出したものである。Regarding the release of strain during this time t, ε m is averaged in the grains recrystallized immediately after processing, zero is retained in the recrystallized grains thereafter, and effective strain remains in the non-recrystallized grains. These strains are calculated by the equation (9) assuming that they are statically recovered during the time t, and a new mathematical model for finding the residual strain Δε from the sum of them is newly found.
以上のようにしてフェライトを熱間圧延した場合の平均
粒径と残留歪を求めることができる。As described above, the average grain size and the residual strain when the ferrite is hot rolled can be obtained.
前述のようにこのフェライト結晶モデルを公知のAr3変
態点以上で熱間圧延する場合には鋼板の材質を予測する
モデルに組み込むことにより、Ar3変態点未満でフェラ
イトの生じる温度域での熱間圧延パスにおける鋼板の材
質を精度良く予測することが可能である。したがって、
その材質予測方法を利用すると、この熱間圧延鋼材の材
質予測方法によって計算される材質予測値と所定の材質
目標値との差が可能なかぎり小さくなるような製造条件
を求めることにより、所定の材質目標値に対する熱間鋼
材の目標製造条件を予め決定することが可能である。As described above, when this ferrite crystal model is hot-rolled at a known Ar 3 transformation point or higher, by incorporating it into the model that predicts the material of the steel sheet, the heat in the temperature range where ferrite occurs below the Ar 3 transformation point It is possible to accurately predict the material of the steel plate in the hot rolling pass. Therefore,
By using the material prediction method, by determining manufacturing conditions such that the difference between the material prediction value calculated by this hot rolling steel material prediction method and the predetermined material target value is as small as possible, It is possible to predetermine the target manufacturing conditions of the hot steel material with respect to the material target value.
更に、熱間圧延鋼材の製造工程上の設備を改造したり、
新規に追加したり、削除したりする場合の設備仕様を決
定するに当り、鋼材の材質作り込み面からの検討におけ
る強力な手段としても使用することが可能である。Furthermore, remodeling the equipment in the manufacturing process of hot rolled steel,
It can also be used as a powerful tool in the examination from the aspect of the material fabrication of steel materials in determining the equipment specifications when newly adding or deleting.
また、実際に熱間圧延鋼材の製造の途中において、実際
の製造条件が目標製造条件とずれた場合、本発明の熱間
圧延鋼材の製造方法を用いて、改めて実際の製造条件で
材質予測値を計算し、その材質予測値が材質目標値と合
致するように、それ以後の目標製造条件の一部を修正す
ることにより最終的に材質目標値に非常に近い材質をも
った熱間圧延鋼材を製造することか可能である。この熱
間圧延鋼材の製造方法は、冶金学的理論に基づいている
ことから、各製造ラインの特性や製造方法の変化などに
対応でき、かつ、効率良く、歩留まり良く必要な材質の
鋼材を製造することが出来る。Also, during the actual production of hot rolled steel, if the actual production conditions deviate from the target production conditions, using the hot rolled steel production method of the present invention, the material prediction value again under the actual production conditions. Is calculated, and some of the subsequent target manufacturing conditions are modified so that the predicted value of the material matches the target material value, and finally the hot rolled steel material with a material very close to the target material value It is possible to manufacture Since this hot rolled steel manufacturing method is based on metallurgical theory, it can respond to changes in the characteristics of each manufacturing line and manufacturing method, and efficiently manufactures the required steel material with good yield. You can do it.
εm=h(dfi,,T) (1) ffD=h(dfi,ε,,T) (2) dfD=h(dfi,ε,T) (3) ffS=h(ε,T,t) (4) dfS=h(dfD,T,t) (5) ffN=h(ffD,ffS) (6) dfN=h(dfi,ε) (7)f =h(ffD,ffS,ffN,dfS,dfN) (8) Δεf=h(ffD,ffN,εm,ε,T,(%C)) (9) ここで、dfiはパス入側のフェライト粒径(μm)、
は歪速度(s-1)、Tは圧延温度(℃)、εは加工歪、
tは加工後の時間(秒)、(%C)は炭素含有量(重量
%)である。ε m = h (d fi ,, T) (1) f fD = h (d fi , ε ,, T) (2) d fD = h (d fi , ε, T) (3) f fS = h ( ε, T, t) (4) d fS = h (d fD , T, t) (5) f fN = h (f fD , f fS ) (6) d fN = h (d fi , ε) (7 ) f = h (f fD , f fS , f fN , d fS , d fN ) (8) Δε f = h (f fD , f fN , ε m , ε, T, (% C)) (9) where And d fi is the ferrite grain size (μm) on the path entry side,
Is strain rate (s -1 ), T is rolling temperature (° C), ε is working strain,
t is a time (second) after processing, and (% C) is a carbon content (% by weight).
dao=h(α,To,to) (10) ここで、daoは加熱炉抽出時のオーステナイト粒径、α
は加熱速度、Toは加熱温度、toは保持時間である。d ao = h (α, T o , t o ) (10) where d ao is the austenite grain size at the time of furnace extraction, α
Is the heating rate, T o is the heating temperature, and t o is the holding time.
εc=h(dai,T) (11) faD=h(dai,ε,,T) (12) daD=h(,T,(%C),(%Mn) (13) faS=h(ε,T,t) (14) daS=h(dai,ε) (15) faN=h(faD,faS) (16) daN=h(dai,ε) (17) daDG=h(daD,T,t) (18) daSG=h(daS,T,t,(%C),(%Mn),(%Si)) (19)a =h(faD,faS,faN,daDG,daSG,daN) (20) Δεa=h(faD,faN,εc,ε,T,t) (21) ここで、faD,faS,faNはそれぞれオーステナイトの動的
再結晶占積率、静的再結晶占積率、未再結晶占積率であ
り、daD、daS、daNはそれぞれオーステナイトの動的再結
晶粒径、静的再結晶粒径、未再結晶粒径であり、daDG、d
aSGはそれぞれオーステナイトの動的再結晶および静的
再結晶粒の粒成長後の粒径である。また、εcは動的再
結晶の臨界歪、a、Δεaはそれぞれ各圧延パス後の
オーステナイトの平均粒径および残留歪であり、daiは
各パスの入側オーステナイト粒径、(%Mn)および(%
Si)はそれぞれMnおよびSiの含有量(重量%)である。ε c = h (d ai , T) (11) f aD = h (d ai , ε ,, T) (12) d aD = h (, T, (% C), (% Mn) (13) f aS = h (ε, T, t) (14) d aS = h (d ai , ε) (15) f aN = h (f aD , f aS ) (16) d aN = h (d ai , ε) (17) d aDG = h (d aD , T, t) (18) d aSG = h (d aS , T, t, (% C), (% Mn), (% Si)) (19) a = h (f aD , f aS , f aN , d aDG , d aSG , d aN ) (20) Δε a = h (f aD , f aN , ε c , ε, T, t) (21) where f aD , f aS , and f aN are the dynamic recrystallization space factor, static recrystallization space factor, and unrecrystallized space factor of austenite, and d aD , d aS , and d aN are the austenite dynamics. Recrystallized grain size, static recrystallized grain size, unrecrystallized grain size, d aDG , d
aSG is the grain size of austenite after grain growth of dynamic recrystallization and static recrystallization. Further, ε c is the critical strain of dynamic recrystallization, a and Δε a are the average grain size and residual strain of austenite after each rolling pass, and d ai is the inlet side austenite grain size of each pass, (% Mn )and(%
Si) is the content (wt%) of Mn and Si, respectively.
Xf=h(a,Δεa,T,t,(%C),(%Mn),(%S
i)) (22) Xp=h(a,Δεa,T,t,(%C),(%Mn),(%S
i)) (23) Xb=h(a,Δεa,T,t,(%C),(%Mn),(%S
i)) (24) ここで、Xf、Xp、Xbはそれぞれフェライト、パーライト、
ベーナイトの占積率であり、Tは冷却中の温度(℃)、
tは冷却時間(秒)である。X f = h ( a , Δε a , T, t, (% C), (% Mn), (% S
i)) (22) X p = h ( a , Δε a , T, t, (% C), (% Mn), (% S
i)) (23) X b = h ( a , Δε a , T, t, (% C), (% Mn), (% S
i)) (24) where X f , X p , and X b are ferrite, pearlite, and
The space factor of bainite, T is the temperature (° C) during cooling,
t is a cooling time (second).
Hf=h(CR,T,t,(%C),(%Mn),(%Si)) (25) Hp=h(CR,Xp,T,t,(%Mn),(%Si)) (26) Hb=h(CR,T,t,(%C),(%Mn),(%Si)) (27) ここで、Hf、Hp、Hbはそれぞれフェライト、パーライト、
ベーナイトの硬度であり、CRは冷却速度である。H f = h (CR, T, t, (% C), (% Mn), (% Si)) (25) H p = h (CR, X p , T, t, (% Mn), (% Si)) (26) H b = h (CR, T, t, (% C), (% Mn), (% Si)) (27) where H f , H p , and H b are ferrite, Perlite,
Hardness of bainite, CR is cooling rate.
dfO=h(Xf,a,Δεa,T,(C%),(%Mn),(%S
i)) (28) dfC=h(dfO,CT,XfR,dfr) (29) ここで、dfO、dfCはそれぞれ変態直後のフェライト粒
径、巻取後の最終フェライト粒径、XfR,dfRは冷却直前
のフェライト占積率、フェライト粒径CTは巻取温度
(℃)である。d fO = h (X f , a , Δε a , T, (C%), (% Mn), (% S
i)) (28) d fC = h (d fO , CT, X fR , d fr ) (29) where d fO and d fC are the ferrite grain size immediately after transformation and the final ferrite grain size after winding, respectively. , X fR , d fR are the ferrite space factor immediately before cooling, and the ferrite grain size CT is the coiling temperature (℃).
TS=h(dfC,Xf,Xp,Xb,Xm,Hf,Hp,Hb) (30) YS=h(dfC,Xf,Xp,Xb,Xm,Hf,Hp,Hb) (31) T.E1=h(dfC,Xf,Xp,Xb,Xm,Hf,Hp,Hb) (32) ここで、Xmはマルテンサイトの占積率、TS、YS、T.E1は
それぞれ引張り強度、降伏強度、全伸びである。TS = h (d fC , X f , X p , X b , X m , H f , H p , H b ) (30) YS = h (d fC , X f , X p , X b , X m , H f , H p , H b ) (31) T.E1 = h (d fC , X f , X p , X b , X m , H f , H p , H b ) (32) where X m Is the space factor of martensite, TS, YS, and T.E1 are tensile strength, yield strength, and total elongation, respectively.
第4図〜第6図に示す●印は、第2図(b)の(I)のケ
ースを実施し、○印は第2図(b)の(II)又は(III)を
実施した際の各々の目標値として設定した最終的な熱間
圧延鋼材の材質値、すなわち引張り強度、降伏強度、全
伸びと、本発明における熱間圧延鋼材の材質計算方法を
用いて目標製造条件を設定し、かつ、実際の製造条件の
補正を行ないながら製造を行ない、最終的に得た材質の
実測値との対応を示している。このとき用いた試供鋼の
成分は表1に示すとおりであり、本発明のモデル式とし
ては(1)〜(9)式をそれぞれ具体的な形の数式にした(41)
〜(49)式を用い、そのほかの必要な前記関係式は(10)〜
(32)式として、特開昭62−158816号及び特開平1−2981
14号から引用して具体的に後記(50)〜(72)式に掲載の各
式及び各係数を使用した。その各式での計算に用いた各
係数は表2に示すとおりである。第4図〜第6図からわ
かるように本発明方法によると、精度よく目標材質をも
った熱間圧延鋼材を製造できる。The mark ● shown in FIGS. 4 to 6 indicates the case of (I) of FIG. 2 (b), and the mark ○ indicates the case of (II) or (III) of FIG. 2 (b). The material value of the final hot-rolled steel set as each target value of, i.e., tensile strength, yield strength, total elongation, and the target manufacturing conditions are set using the material calculation method of the hot-rolled steel in the present invention. Moreover, the manufacturing process is performed while the actual manufacturing conditions are corrected, and the correspondence with the actually measured value of the finally obtained material is shown. The components of the sample steel used at this time are as shown in Table 1, and as the model formulas of the present invention, formulas (1) to (9) were each made into a concrete formula (41).
~ (49) is used, and the other necessary relational expressions are (10) ~
The formula (32) is represented by JP-A-62-158816 and JP-A-1-2981.
Each formula and each coefficient described in the following formulas (50) to (72) are quoted from No. 14 and used concretely. Table 2 shows each coefficient used for the calculation in each equation. As can be seen from FIGS. 4 to 6, according to the method of the present invention, the hot rolled steel material having the target material can be accurately manufactured.
〔フェライト再結晶モデル〕 <再結晶モデル> εm=A1・dfoi a・εb・exp(Az/RTi) (41) ffD=1−exp{−(εi−εm)/k1} (42) k1=A3・dfoi c・exp(A4/RTi) dfD=A5・εi −d・dfoi e・exp(-AG/RTi) (43) ffS=1-exp{-(ti/k2} (44) k2=A7・ε−f・exp(A8/RT) dfS 2=dfD 2+A9・exp(-A10/RTi)・ti (45) <未再結晶モデル> ffN=1-ffD-ffS (46) dfN=dfoi・exp(1−εi/4) (47) <平均粒径モデル>fi =ffD+ffS)/dfS 2+ffN/dfN 2}-1/2 (48) <回復モデル> Δεfi=(ffD・εm+ffN・εi)・exp{−ti/
τk)9 (49) τk=k3・exp(k4/RTi) k3=A11・exp[-exp{-A12・(%C)+A13}] k4=exp{-A14・(%C)+A15}+A16 ここで、dfoiはi回目のパス前のフェライトの初期粒径
(μm)、iは歪速度(s-1)、Tiは加工温度
(℃)、εiは加工歪、tiは加工後の時間(秒)、(%
C)は炭素含有量(重量%)であり、a、b、c、d、
e、f、g、A1〜A16は実験より求める。 [Ferrite recrystallization model] <Recrystallization model> ε m = A 1 · d foia a ε b · exp (A z / RT i ) (41) f fD = 1-exp {− (ε i −ε m ) / K 1 } (42) k 1 = A 3・ d foi c・ exp (A 4 / RT i ) d fD = A 5・ ε i −d・ d foi e・ exp (-A G / RT i ) ( 43) f fS = 1-exp {-(t i / k 2 } (44) k 2 = A 7・ ε −f・ exp (A 8 / RT) d fS 2 = d fD 2 + A 9・ exp ( -A 10 / RT i ) ・ t i (45) < Unrecrystallized model> f fN = 1-f fD -f fS (46) d fN = d foi・ exp (1-ε i / 4) (47) <Average particle size model> fi = f fD + f fS ) / d fS 2 + f fN / d fN 2 } -1/2 (48) <Recovery model> Δε fi = (f fD · ε m + f fN · ε i ) ・ exp {−t i /
τ k ) 9 (49) τ k = k 3 · exp (k 4 / RT i ) k 3 = A 11 · exp [-exp {-A 12 · (% C) + A 13 }] k 4 = exp {- A 14 · (% C) + A 15 } + A 16 where d foi is the initial grain size (μm) of the ferrite before the i-th pass, i is the strain rate (s −1 ), and T i is the processing temperature ( ℃), ε i is the processing strain, t i is the time (second) after processing, (%
C) is the carbon content (% by weight), a, b, c, d,
e, f, g, and A 1 to A 16 are obtained by experiments.
<初期オーステナイト粒径モデル> daO 2=(k5・α−h)2+A17・exp(-A18/To)toi (50) k5=A19{To-1173)/100}3+A20 h、i、A17〜A20は実験により求める。<Initial austenite grain size model> d aO 2 = (k 5 · α −h ) 2 + A 17 · exp (-A 18 / To) to i (50) k 5 = A 19 {To-1173) / 100} 3 + A 20 h, i, A 17 to A 20 are experimentally determined.
αは加熱速度、Toは加熱温度、toは保持時間。α is the heating rate, To is the heating temperature, and to is the holding time.
<動的再結晶モデル> εc=A21・daoij・exp(A22/RTi) (51) Tiは圧延温度、Rは気体定数である。<Dynamic Recrystallization Model> ε c = A 21 · d aoij · exp (A 22 / RT i ) (51) T i is the rolling temperature and R is the gas constant.
o、A20、A21は実験により求める。o, A 20 , and A 21 are obtained by experiments.
faD=1−exp[−{(εi−εc)/(εs−εi)}
M] (52) εs=A23・{1-exp(-daoi/K6)} k6=A24・-k・exp(-A25/Ti) M=A26・exp(A27/Ti) daD=K7・Zl (53) K7=A28・Qo-A29 Q=A30-A31・Ceq Ceq=(%C)+(%Mn)/6 Z=・exp(Qo/RT) K、l、A23〜A31は実験により求める。f aD = 1-exp [-{(ε i −ε c ) / (ε s −ε i )}
M ] (52) ε s = A 23・ {1-exp (-d aoi / K 6 )} k 6 = A 24・ -k ・ exp (-A 25 / T i ) M = A 26・ exp (A 27 / T i ) d aD = K 7・ Z l (53) K 7 = A 28・ Q o -A 29 Q = A 30 -A 31・ C eq C eq = (% C) + (% Mn) / 6 Z = · exp (Q o / RT) K, 1, A 23 to A 31 are experimentally determined.
<静的再結晶モデル> faS=(1-fD)[1-exp{-(ti/τS)m}] (54) τS=A32・ε−n・exp(A33/RTi) m、n、A32〜A33は実験により求める。<Static recrystallization model> f aS = (1-f D ) [1-exp {-(t i / τ S ) m }] (54) τ S = A 32 · ε −n · exp (A 33 / RT i ) m, n, A 32 to A 33 are experimentally determined.
daS=A34・daoi o・ε−p (55) <未再結晶モデル> faN=1−faD−faS (56) o、p、A34は実験により求める。d aS = A 34 · d ao o · ε −p (55) < Unrecrystallized model> f aN = 1−f aD −f aS (56) o, p, and A 34 are obtained by experiments.
daN=daoi・exp(−ε/4) (57) <粒成長モデル> daDG 2=daD 2+A35・exp(-A36/RTi)・ti q (58) daSG 2=daS 2 +A37・(%C)−γ・(%Si)−S・(%Mn)−t・ex
p(−A38/RTi)・ti u (59) q、r、s、t、u、A35〜A38は実験より求める。d aN = d aoi・ exp (−ε / 4) (57) <Grain growth model> d aDG 2 = d aD 2 + A 35・ exp (-A 36 / RT i ) ・ t i q (58) d aSG 2 = d aS 2 + A 37・ (% C) −γ・ (% Si) −S・ (% Mn) −t・ ex
p (−A 38 / RT i ) · t i u (59) q, r, s, t, u, A 35 to A 38 are obtained by experiments.
<平均粒径モデル>ai =(faD/daDG 2+faS/daSG 2+faN/aaN 2)-1/2 (60) <回復モデル> Δεai=(faD・εc+faN・εi)・exp{−(ti/τ
K)v (61) τK=A39・exp(A40/RTi) v、A39、A40は実験より求める。<Average particle size model> ai = (f aD / d aDG 2 + f aS / d aSG 2 + f aN / a aN 2 ) -1/2 (60) <Recovery model> Δε ai = (f aD · ε c + f aN・ ε i ) ・ exp {-(t i / τ
K ) v (61) τ K = A 39 · exp (A 40 / RT i ) v, A 39 , and A 40 are obtained by experiments.
Xf/Xfmax=1-exp{-K4・(ti−τI)w}(Si%<0.1wt
%) (62) K8=1/2.24・(2.24・k9/ai+A41・Δεai 2)・(1+A
42・Δεai)k10 k9=(1/2){γ2−β・γ2・(α2−γ2)−1/2・
k11+β・(α2−γ2)−1/2・k12} α=exp(Δε)、β=1、γ=exp(−Δε) k11=▲∫u o▼(1−K9 2・sin2θ)1/2dθ k12=▲∫u o▼(1−K9 2・sin2θ)1/2dθ u=arccos(γ/α) K13={α2・(β2−γ2)/β2・(α2−
γ2)}1/2 K10=exp{A43-A44・(%C)−A45・(%Mn)+A46・(T-2
73)-A47・(T-273)2} τ1=exp(−A48・ln k10+A49・ln T+A50/T-A51) Xfmax=1-(%C)/{A52+A53・(T-273)+A54・(T-273)2}(T≧9
93K) =1−(%C)/{A52+A53・720)+A54・7202}
(T<993K) ω、A41〜A54は実験により求める。X f / X fmax = 1-exp {-K 4 · (t i −τ I ) w } (Si% <0.1wt
%) (62) K 8 = 1 / 2.24 ・ (2.24 ・ k 9 / ai + A 41・ Δε ai 2 ) ・ (1 + A
42・ Δε ai ) k 10 k 9 = (1/2) {γ 2 −β ・ γ 2・ (α 2 −γ 2 ) −1/2・
k 11 + β · (α 2 −γ 2 ) −1 / 2 · k 12 } α = exp (Δε), β = 1, γ = exp (−Δε) k 11 = ▲ ∫ u o ▼ (1-K 9 2・ sin 2 θ) 1/2 dθ k 12 = ▲ ∫ u o ▼ (1-K 9 2・ sin 2 θ) 1/2 dθ u = arccos (γ / α) K 13 = {α 2・ (β 2- γ 2 ) / β 2 · (α 2 −
γ 2 )} 1/2 K 10 = exp {A 43 -A 44・ (% C) −A 45・ (% Mn) + A 46・ (T-2
73) -A 47・ (T-273) 2 } τ 1 = exp (−A 48・ ln k 10 + A 49・ ln T + A 50 / TA 51 ) X fmax = 1-(% C) / {A 52 + A 53・ (T-273) + A 54・ (T-273) 2 } (T ≧ 9
93K) = 1 - (% C ) / {A 52 + A 53 · 720) + A 54 · 720 2}
(T <993K) ω, A 41 to A 54 are experimentally obtained.
Xf/Xfmax=1-[{1+K14/x・(t−τ2)}−x](Si%≧
0.1wt%) (62)′ K14=1/2.24・(2.24・k9/ai+A41・Δεai 2+A55)・(1+A42・Δεai)・k15 k15=exp[-A56+A57・ln(%Si)+A58・{ln(%Si)}2-A59・(%C)-A60・(%Mn)+A61・(T-273)-A
62・(T-273)2] τ2=τf/{1/2.24・(2.24・k9/ai+A41・Δεai 2+A55)・(1+A42・Δ
εai)} τf=exp[−A63-A64・ln(%Si)-A65・{ln(%Si)}2+A65・(%C)+A67・(%Mn)-A68・(T-27
3)-A69・(T-273)2] x=A70+A71・ln(%Si)+A72・{ln(%Si)}2 A55〜A72は実験により求める。X f / X fmax = 1-[{1 + K 14 / x ・ (t−τ 2 )} −x ] (Si% ≧
0.1wt%) (62) ′ K 14 = 1 / 2.24 ・ (2.24 ・ k 9 / ai + A 41・ Δε ai 2 + A 55 ) ・ (1 + A 42・ Δε ai ) ・ k 15 k 15 = exp [-A 56 + A 57・ ln (% Si) + A 58・ {ln (% Si)} 2 -A 59・ (% C) -A 60・ (% Mn) + A 61・ (T-273) -A
62・ (T-273) 2 ] τ 2 = τ f /{1/2.24 ・ (2.24 ・ k 9 / ai + A 41・ Δε ai 2 + A 55 ) ・ (1 + A 42・ Δ
ε ai )} τ f = exp [−A 63 -A 64・ ln (% Si) -A 65・ {ln (% Si)} 2 + A 65・ (% C) + A 67・ (% Mn)- A 68 / (T-27
3) -A 69 · (T-273) 2 ] x = A 70 + A 71 · ln (% Si) + A 72 · {ln (% Si)} 2 A 55 to A 72 are experimentally determined.
Xp/Xpmax=1-exp{-k16・(ti−τ3)y}(Si%<0.1wt%)
(63) K16=1/2.24・(2.24・k9・K17/ai+A73・k18・Δεai 2)・
(1+A74・Δεai)k19 K17=(1-Xf)2/3 K18=(1-Xf) K19=exp{A75-A76・(%C)-A77・(%Mn)+A78・(T-273)+A79・(T-
273)2} τ3=exp(−A80・ln K16+A81・ln T+A82/T-A83) Xpmax=1-Xfmax Xp=1-exp[{1+k14/x・(t−τ2)}-x(Si%≧0.1wt%) (6
3)′ A73〜A83は実験により求める。Xp / X pmax = 1-exp {-k 16・ (t i −τ 3 ) y } (Si% <0.1wt%)
(63) K 16 = 1 / 2.24 ・ (2.24 ・ k 9・ K 17 / ai + A 73・ k 18・ Δε ai 2 ) ・
(1 + A 74・ Δε ai ) k 19 K 17 = (1-X f ) 2/3 K 18 = (1-X f ) K 19 = exp {A 75 -A 76・ (% C) -A 77・ (% Mn) + A 78・ (T-273) + A 79・ (T-
273) 2 } τ 3 = exp (−A 80・ ln K 16 + A 81・ ln T + A 82 / TA 83 ) X pmax = 1-X fmax Xp = 1-exp [{1 + k 14 / x ・(T-τ 2 )} -x (Si% ≧ 0.1wt%) (6
3) 'A 73 to A 83 are obtained by experiments.
<ベンナイト変態モデル> Xb/Xbmax=1-exp{-k20・(ti−τ4)y}(Si%<0.1wt
%) (64) K20=1/2.24・(2.24・k9・K21/ai+A84・k22・Δεai 2)・(1+A
85・Δεai)k23 K21=(1-Xf-Xp)2/3 K22=(1-Xf-Xp) K23=exp{A86-A87・(%C)-A88・(%Mn)+A89・(T-273)-A90・(T-
273)2} τ4=exp(−A91・ln K20+A92・ln T+A93/T-A94) Xbmax=1-Xfmax-Xpmax y、A84〜A94は実験により求める。<Bennite transformation model> X b / X bmax = 1-exp {-k 20 · (t i −τ 4 ) y } (Si% <0.1 wt
%) (64) K 20 = 1 / 2.24 ・ (2.24 ・ k 9・ K 21 / ai + A 84・ k 22・ Δε ai 2 ) ・ (1 + A
85・ Δε ai ) k 23 K 21 = (1-X f -X p ) 2/3 K 22 = (1-X f -X p ) K 23 = exp {A 86 -A 87・ (% C)- A 88・ (% Mn) + A 89・ (T-273) -A 90・ (T-
273) 2 } τ 4 = exp (−A 91・ ln K 20 + A 92・ ln T + A 93 / TA 94 ) X bmax = 1-X fmax -X pmax y, A 84 to A 94 are obtained by experiments. .
Xb/Xbmax=1-exp{-k24・(ti−τ5)}z} Si%≧0.1wt
%) (64)′ K24=1/2.24・(2.24・k9/ai+A41・Δεai 2+A55)・(1+A42・
Δεai)k25 K25=exp[-A95-A86・(%Si)2-A97・(%C)-A98・(%Mn)+A99・(T-
273)-A100・(T-273)2] τ5=τb{1/2.24・(2.24・k9/ai+A41・Δεai 2+A55)2・
(1+A42・Δεai)} τb=exp[−A101+A102・(%Si)-A103・(%Si)2+A104(%C) +A105・(%Mn)-A106・(T-273)+A107・(T-273)2] z、A95〜A107は実験により求める。X b / X bmax = 1-exp {-k 24・ (t i −τ 5 )} z } Si% ≧ 0.1wt
%) (64) ′ K 24 = 1 / 2.24 ・ (2.24 ・ k 9 / ai + A 41・ Δε ai 2 + A 55 ) ・ (1 + A 42・
Δε ai ) k 25 K 25 = exp [-A 95 -A 86・ (% Si) 2 -A 97・ (% C) -A 98・ (% Mn) + A 99・ (T-
273) -A 100・ (T-273) 2 ] τ 5 = τ b {1 / 2.24 ・ (2.24 ・ k 9 / ai + A 41・ Δε ai 2 + A 55 ) 2・
(1 + A 42・ Δε ai )} τ b = exp [−A 101 + A 102・ (% Si) -A 103・ (% Si) 2 + A 104 (% C) + A 105・ (% Mn) -A 106 · (T-273) + A 107 · (T-273) 2 ] z, A 95 to A 107 are obtained by experiments.
<フェライト硬さモデル> Hf=Hfo+B1・exp[B2/T] (65) Hfo=B3+B4・(%C)+B5・(%Mn)+B6・(%Si)-B7・ln tc(T≧923
K) =B3+B4・(%C)+B5・(%Mn)+B6・(%Si)-B7・ln tc -B8[1、exp{-B9・((T-773)/(923-T))A)・ln tc (723K≦T
<923K) tc=(Ar3-T)/CR A、B1〜B9は実験により求める。<Ferrite hardness model> H f = H fo + B 1・ exp [B 2 / T] (65) H fo = B 3 + B 4・ (% C) + B 5・ (% Mn) + B 6・(% Si) -B 7・ ln t c (T ≧ 923
K) = B 3 + B 4・ (% C) + B 5・ (% Mn) + B 6・ (% Si) -B 7・ ln t c -B 8 [1, exp {-B 9・ (( T-773) / (923-T)) A ) ・ ln t c (723K ≦ T
<923K) t c = (Ar 3 -T) / CR A, B 1 to B 9 are obtained by experiments.
CRは冷却速度である。CR is the cooling rate.
Hp=Σ{ΔXp・K25}/ΣΔXp (66) K26=B10-B11・(Ae1-T)−1 Ae1=B12-B13・(%Mn)+B14・(%Si) B10〜B14は実験により求める。H p = Σ {ΔX p · K 25 } / ΣΔX p (66) K 26 = B 10 -B 11 · (Ae 1 -T) −1 Ae 1 = B 12 -B 13 · (% Mn) + B 14・ (% Si) B 10 to B 14 are obtained by experiments.
ΔXpは各温度で現われたパーライト量である。ΔX p is the amount of pearlite that appears at each temperature.
<ベーナイト変態モデル> Hb=B15+B16・(%C)B+B17・(%Si)-B19・(T-273)c・ln tc (6
7) B、C、B15〜B19は実験により求める。<Bainite transformation model> H b = B 15 + B 16 · (% C) B + B 17 · (% Si) -B 19 · (T-273) c · ln t c (6
7) B, C, B 15 ~B 19 is determined by experiment.
dfo=exp{B20+B21・ln Xf-B22・K27-B23・K28-B24・ln(1+A42
・Δε)− <粒径変換比モデル> B25・ln(%C)-B26・ln(%Mn)} (68) K27=ln[{B27-B28・(%Si)+B29・(%Si)2}3・{(2.24/40)/(2.24/40+A55}] K28=ln(2.24・k9/ai+A41・Δεai 2+A55) 〔巻取後の粒成長モデル〕 df={Xf/R/dfR 2+(1-XfR)/dfc 2}-1/2 (69) dfc=dfo (T≦723K) =dfo+B30・exp(-B31/T) (T>723K) B20〜B31は実験により求める。d fo = exp {B 20 + B 21・ ln X f -B 22・ K 27 -B 23・ K 28 -B 24・ ln (1 + A 42
· Δε) - <particle size conversion ratio model> B 25 · ln (% C ) -B 26 · ln (% Mn)} (68) K 27 = ln [{B 27 -B 28 · (% Si) + B 29・ (% Si) 2 } 3・ {(2.24 / 40) / (2.24 / 40 + A 55 }] K 28 = ln (2.24 ・ k 9 / ai + A 41・ Δε ai 2 + A 55 ) Grain growth model after removal] d f = {X f / R / d fR 2 + (1-X fR ) / d fc 2 } -1/2 (69) d fc = d fo (T ≦ 723K) = d fo + B 30 · exp (-B 31 / T) (T> 723K) B 20 to B 31 are determined by experiments.
TS=B32+B33・Xf・df -1/2+B34・Xb・da -1/2 +B35・Xm 1/2+B36・(Hf・Xf+Hp・Xp+Hb・Xb) (70) YS=B37+B33・Xf・df -1/2+B39・Xb・da -1/2 +B40・Xm 1/2+B41・(Hf・Xf+Hp・Xp+Hb・Xb) (71) T.E1=B42-B43・Xf・df -1/2-B44・Xb・da -1/2 -B45・Xm 1/2-B46・(Hf・Xf+Hp・Xp+Hb・Xb) (72) B32〜B46は実験により求める。TS = B 32 + B 33・ X f・ d f -1/2 + B 34・ X b・ d a -1/2 + B 35・ X m 1/2 + B 36・ (H f・ X f + (H p・ X p + H b・ X b ) (70) YS = B 37 + B 33・ X f・ d f -1/2 + B 39・ X b・ d a -1/2 + B 40・ X m 1/2 + B 41・ (H f・ X f + H p・ X p + H b・ X b ) (71) T.E1 = B 42 -B 43・ X f・ d f -1/ 2- B 44・ X b・ d a -1/2 -B 45・ X m 1/2 -B 46・ (H f・ X f + H p・ X p + H b・ X b ) (72) B 32 ~ B 46 is obtained by experiment.
以上に説明した本発明での方法により、Ar3変態点以下
でパーライト及びベーナイトが生じない温度域で熱間圧
延を行なう場合の熱間圧延鋼材の材質を予測し、かつそ
の推定値に基づいて成分、製造条件を設定することによ
り、材質を精度よく目標値にコントロールした熱間圧延
鋼材を効率よく、歩留まり高く、低コストの下に製造出
来るなど、熱間圧延によって鋼材を製造する分野にもた
らす効果は大きい。By the method of the present invention described above, predict the material of hot rolled steel when performing hot rolling in a temperature range where pearlite and bainite do not occur below the Ar 3 transformation point, and based on the estimated value By setting the components and manufacturing conditions, it is possible to produce hot rolled steel products that are controlled to target values with high precision, efficiently, with high yield and at low cost. The effect is great.
第1図は本発明の材質計算における熱間圧延時の粒径と
残留歪を計算する部分の流れを図を示している。 第2図は、従来の方法で適用可能な熱間圧延(a)および
本発明方法で適用可能な熱間圧延(b)の鋼材温度推移の
模式図を示している。 第3図は、Ar3変態点以上の温度域での熱間圧延を行な
う場合にしか適用できない従来の材質計算の流れ図を示
している。 第4図、第5図、第6図は、それぞれ、実際に引張り試
験より得られた機械的特性値、つまり、引張り強さTS、
降伏応力YS、全伸びE1と本発明でのそれらの計算値との
対応関係図を示している。FIG. 1 shows the flow of the part for calculating the grain size and residual strain during hot rolling in the material calculation of the present invention. FIG. 2 shows a schematic diagram of steel material temperature transitions in hot rolling (a) applicable by the conventional method and hot rolling (b) applicable by the method of the present invention. FIG. 3 shows a flow chart of the conventional material calculation that can be applied only when hot rolling is performed in a temperature range not lower than the Ar 3 transformation point. 4, 5 and 6 show the mechanical characteristic values actually obtained by the tensile test, that is, the tensile strength TS,
The correspondence diagram of the yield stress YS and the total elongation E1 and their calculated values in the present invention is shown.
───────────────────────────────────────────────────── フロントページの続き (72)発明者 脇田 淳一 大分県大分市大字西ノ洲1番地 新日本製 鐵株式会社大分製鐵所内 (72)発明者 江坂 一彬 大分県大分市大字西ノ洲1番地 新日本製 鐵株式会社大分製鐵所内 ─────────────────────────────────────────────────── ─── Continuation of the front page (72) Inventor Junichi Wakita 1 Nishinosu, Oita, Oita-shi, Oita Pref., Nippon Steel Co., Ltd. Oita Works (72) Inventor Isaichi Esaka 1-Nishinozu, Oita, Japan New Japan Oita Steel Works, Ltd.
Claims (6)
ける圧延温度がAr3変態温度未満でフェライト変態が生
じる温度域となる温度条件で熱間圧延した後冷却して熱
間圧延鋼材を製造するに際し、前記熱間圧延鋼材の鋼材
条件、加熱条件、圧延条件および冷却条件等の製造条件
に基づいて、予め定めた初期粒径モデルより加熱炉抽出
時の圧延前平均オーステナイト粒径doを求め、該doおよ
び前記製造条件に基づいて予め定めたフェライト再結晶
モデル、フェライト変態モデル、フェライト変態時の粒
径変換比モデルを用いて、各圧延パス毎に、オーステナ
イト、フェライトそれぞれの占積率、平均粒径および残
留歪を計算することにより、最終圧延パス後のオーステ
ナイト、フェライトそれぞれの占積率Xa、Xf、平均粒径
a、f、残留歪Δεa、Δεfを求め、該Xa、Xf、
a、f、Δεa、Δεfに基づいて予め定めた各組
織(フェライト、パーライト、ベーナイト、マルテンサ
イト)の変態モデルおよび硬度モデルにより冷却完了後
の各組織それぞれの占積率、硬度を算出し、同時に予め
定めたフェライト変態時の粒径変換比モデルおよび取巻
後のフェライト粒成長モデルを用いて最終平均フェライ
ト粒径を算出し、該最終平均フェライト粒径と各組織そ
れぞれの占積率及び硬度から予め定めた材質モデルより
前記熱間圧延鋼材の材質予測値を計算することを特徴と
する熱間圧延鋼材の製造方法。1. A hot rolled slab of ordinary carbon steel is hot-rolled under a temperature condition in which the rolling temperature in all rolling passes is less than the Ar 3 transformation temperature and in a temperature range in which ferrite transformation occurs, followed by cooling and hot rolling. When manufacturing a steel material, based on manufacturing conditions such as steel material conditions of the hot rolled steel material, heating conditions, rolling conditions and cooling conditions, the average austenite grain size before rolling at the time of furnace extraction from a predetermined initial grain size model The do is determined, and the ferrite recrystallization model, the ferrite transformation model, and the grain size conversion ratio model at the time of ferrite transformation, which are predetermined based on the do and the manufacturing conditions, are used to determine the austenite and ferrite occupancy for each rolling pass. By calculating the product factor, average grain size and residual strain, the space factors Xa , Xf , and average grain size of the austenite and ferrite after the final rolling pass are calculated.
a , f , residual strains Δε a , Δε f are obtained, and the X a , X f ,
Based on a , f , Δε a , and Δε f , the space factor and hardness of each structure after completion of cooling were calculated by a transformation model and hardness model of each structure (ferrite, pearlite, bainite, martensite) determined in advance. At the same time, the final average ferrite grain size is calculated using a grain size conversion ratio model during predetermined ferrite transformation and a ferrite grain growth model after winding, and the final average ferrite grain size and the space factor of each structure and A method of manufacturing a hot rolled steel product, characterized in that a material predictive value of the hot rolled steel product is calculated from a hardness-determined material model.
延温度がAr3変態温度未満でフェライト変態が生じる温
度域で熱間圧延を行なう場合、各圧延パスでは、予め定
めたフェライト変態モデルを用いて前パス以後に変態し
たフェライトの占積率を求め、全フェライトおよび全オ
ーステナイトの占積率を計算し、オーステナイトの部分
については前記オーステナイト再結晶モデルを用いて前
記各グループの平均粒径と残留歪を求め、フェライトの
部分ついては、前パス以後に変態したフェライトについ
て粒径変換比モデルを用いて該フェライトの平均粒径を
求め、該フェライトの残留歪を零とし、該フェライトと
前パス以前に変態したフェライトとの平均フェライト粒
径および平均残留歪を求め、該フェライト粒径を該パス
の入側粒径とし、該平均残留歪を入側残留歪とし、該パ
スの付加歪に該入側残留歪を加えた実効歪が再結晶の限
界歪よりも大きい場合は、再結晶、未再結晶の2つのグ
ループに分け、該実効歪が該限界歪よりも小さい場合
は、未再結晶グループのみとし、前記入側粒径、前記実
効歪および前記製造条件より、予め定めたフェライト再
結晶モデルを用いて各グループにおける占積率および平
均粒径を計算し、各パス毎に平均フェライト粒径および
残留歪を繰り返し計算し、最終圧延パス後のオーステナ
イト及びフェライトそれぞれの占積率、平均粒径及び残
留歪を求め、その後は、該各計算値より冷却完了後の各
組織(フェライト、パーライト、ベーナイト、マルテン
サイト)それぞれの体積率、硬度を算出し、同時に最終
平均フェライト粒径を算出することを特徴とする請求項
1に記載の熱間圧延鋼材の製造方法。2. When the hot-rolled slab is hot-rolled in a temperature range in which the ferrite temperature is lower than the Ar 3 transformation temperature in all rolling passes, a predetermined ferrite transformation model is used in each rolling pass. Obtain the space factor of the ferrite transformed after the previous pass using, calculate the space factor of all ferrite and all austenite, for the austenite portion using the austenite recrystallization model the average grain size of each group For the ferrite part, the average grain size of the ferrite was calculated using the grain size conversion ratio model for the ferrite transformed after the previous pass, and the residual strain of the ferrite was set to zero, and the ferrite and the previous pass were determined. The average ferrite grain size and average residual strain with the previously transformed ferrite are determined, and the ferrite grain size is defined as the entrance-side grain size of the path. When the average residual strain is defined as the inlet-side residual strain and the effective strain obtained by adding the inlet-side residual strain to the additional strain of the path is larger than the critical strain of recrystallization, it is divided into two groups, recrystallized and unrecrystallized. When the effective strain is smaller than the critical strain, only the non-recrystallized group is used, and a ferrite recrystallization model determined in advance is used for each group based on the entrance side grain size, the effective strain and the manufacturing conditions. Calculate the product factor and average grain size, repeatedly calculate the average ferrite grain size and residual strain for each pass, and obtain the space factor, average grain size and residual strain of austenite and ferrite after the final rolling pass, and then Is to calculate the volume fraction and hardness of each structure (ferrite, pearlite, bainite, martensite) after completion of cooling from the calculated values, and at the same time to calculate the final average ferrite grain size. Method for manufacturing a hot-rolled steel according to claim 1,.
残留歪を計算するにあたり、前記実効歪εが(1)式で与
えられるεmよりも大きい場合には、再結晶及び未再結
晶の2つのグループに分け、圧延直後での再結晶占積率
ffDおよび粒径dfDを(2)(3)式を用いて求め、その後に再
結晶した部分の占積率ffSを(4)式から計算し、パス間で
の再結晶粒径の変化を(5)式から求め、未再結晶領域の
占積率ffNおよび粒径dfNを(6)(7)式で計算し、実効歪ε
がεmよりも小さい場合には、未再結晶領域の占積率f
fNおよび粒径dfNのみを(6)(7)式から計算し、次パス直
前の平均フェライト粒径fを(8)式で計算し、パス間
での歪の回復を考慮して次パス直前の残留歪Δεを(9)
式を用いて計算することを特徴とする請求項2に記載の
熱間圧延鋼材の製造方法。 εm=h(dfi,,T) (1) ffD=h(dfi,ε,,T) (2) dfD=h(dfi,ε,T) (3) ffS=h(ε,T,t) (4) dfS=h(dfD,T,t) (5) ffN=h(ffD,ffS) (6) dfN=h(dfi,ε) (7)f =h(ffD,ffS,ffN,dfS,dfN) (8) Δεf=h(ffD,ffN,εm,ε,T,(%C)) (9) ここで、dfiはパス入側のフェライト粒径(μm)、
は歪速度(s-1)、Tは圧延温度(℃)、εは加工歪、
tは加工後の時間(秒)、(%C)は炭素含有量(重量
%)。3. When calculating the average grain size and residual strain of a ferrite part, when the effective strain ε is larger than ε m given by the equation (1), recrystallized and unrecrystallized 2 Divided into two groups, recrystallization space factor immediately after rolling
The f fD and the grain size d fD are obtained by using the equations (2) and (3), and the space factor f fS of the recrystallized part is calculated from the equation (4). The change is calculated from Eq. (5), the space factor f fN and the grain size d fN of the unrecrystallized region are calculated by Eqs . (6) and (7), and the effective strain
Is smaller than ε m, the space factor f of the unrecrystallized region is
Only fN and grain size d fN are calculated from Eqs . (6) and (7), the average ferrite grain size f immediately before the next pass is calculated using Eq. (8), and strain recovery between passes is taken into consideration. The residual strain Δε immediately before is (9)
The method for manufacturing hot-rolled steel product according to claim 2, wherein the hot-rolled steel product is calculated using a formula. ε m = h (d fi ,, T) (1) f fD = h (d fi , ε ,, T) (2) d fD = h (d fi , ε, T) (3) f fS = h ( ε, T, t) (4) d fS = h (d fD , T, t) (5) f fN = h (f fD , f fS ) (6) d fN = h (d fi , ε) (7 ) f = h (f fD , f fS , f fN , d fS , d fN ) (8) Δε f = h (f fD , f fN , ε m , ε, T, (% C)) (9) where And d fi is the ferrite grain size (μm) on the path entry side,
Is strain rate (s -1 ), T is rolling temperature (° C), ε is working strain,
t is the time after processing (seconds), (% C) is the carbon content (% by weight).
上の温度域から圧延を開始しAr3変態温度未満の温度域
で圧延を終了した後冷却して熱間圧延鋼材を製造するに
際し、前記熱間圧延鋼材の鋼材条件、加熱条件、圧延条
件および冷却条件等の製造条件に基づいて、予め定めた
初期粒径モデルより加熱炉抽出時の圧延前平均オーステ
ナイト粒径doを求め、該doおよび前記製造条件に基づい
て予め定めたオーステナイト再結晶モデル、フェライト
再結晶モデル、フェライト変態モデル、フェライト変態
時の粒径変態比モデルを用いて、Ar3変態温度以上の温
度域における圧延パスではオーステナイトの平均粒径お
よび残留歪を計算し、Ar3変態温度未満の温度域におけ
る圧延パスではオーステナイト、フェライトそれぞれの
占積率、平均粒径および残留歪を計算することにより、
最終圧延パス後のオーステナイト、フェライトそれぞれ
の占積率Xa、Xf、平均粒径a、f、残留歪Δεa、
Δεfを求め、該Xa、Xf、a、f、Δεa、Δεf
に基づいて予め定めた各組織(フェライト、パーライ
ト、ベーナイト、マルテンサイト)の変態モデルおよび
硬度モデルにより冷却完了後の各組織それぞれの占積
率、硬度を算出し、同時に予め定めたフェライト変態時
の粒径変換比モデルおよび取巻後のフェライト粒成長モ
デルを用いて最終平均フェライト粒径を算出し、該最終
平均フェライト粒径と各組織それぞれの占積率及び硬度
から予め定めた材質モデルより前記熱間圧延鋼材の材質
予測値を計算し、該材質予測値と材質目標値とが一致す
るように前記製造条件の一部を修正し、修正後の製造条
件に基づいて熱間鋼材を製造して目標材質を得ることを
特徴とする熱間圧延鋼材の製造方法。The 4. usual hot slab is cooled after exiting the rolling in a temperature range of less than Ar 3 starts rolling from a temperature range of not lower than transformation temperature Ar 3 transformation temperature hot rolled steel carbon steel During production, the steel material conditions of the hot rolled steel material, heating conditions, based on manufacturing conditions such as rolling conditions and cooling conditions, the pre-rolling average austenite grain size do at the time of furnace extraction from a predetermined initial grain size model calculated, the do and on the basis of the production conditions predetermined austenite recrystallization model, ferrite recrystallization model, ferrite transformation model, using a particle size transformation ratio model during ferrite transformation, the Ar 3 transformation temperature or higher temperature range the rolling pass computes the average particle size and residual strain of austenite, Ar 3 austenite in rolling pass in a temperature range below the transformation temperature, ferrite respective space factor, the average particle diameter and By calculating the Tomeibitsu,
The final rolling pass after the austenite, ferrite respective space factor X a, X f, average particle size a, f, residual strain [Delta] [epsilon] a,
Δε f is obtained and the X a , X f , a , f , Δε a , and Δε f are calculated.
Based on the transformation model of each structure (ferrite, pearlite, bainite, martensite) and hardness model, the space factor and hardness of each structure after completion of cooling are calculated based on the The final average ferrite grain size is calculated using the grain size conversion ratio model and the ferrite grain growth model after surrounding, and the final average ferrite grain size and the space factor and hardness of each structure are determined from the material model determined in advance from the material model. Calculate the material prediction value of the hot rolled steel, modify some of the manufacturing conditions so that the material prediction value and the material target value match, and manufacture the hot steel material based on the modified manufacturing conditions. A method for producing hot-rolled steel, characterized by obtaining a target material by means of
ける圧延パスでは、オーステナイトの平均粒径および残
留歪を計算し、鋼材温度がAr3変態温度未満の温度域の
圧延パスでは、予め定めたフェライト変態モデルを用い
て前パス以後に変態したフェライトの占積率を求め、全
フェライトおよび全オーステナイトの占積率を計算し、
オーステナイトの部分については前記オーステナイト再
結晶モデルを用いて前記各グループの平均粒径と残留歪
を求め、フェライトの部分については、前パス以後に変
態したフェライトについて粒径変換比モデルを用いて該
フェライトの平均粒径を求め、該フェライトの残留歪を
零とし、該フェライトと前パス以前に変態したフェライ
トとの平均フェライト粒径および平均残留歪を求め、該
フェライト粒径を該パスの入側粒径とし、該平均残留歪
を入側残留歪とし、該パスの付加歪に該入側残留歪を加
えた実効歪が再結晶の限界歪よりも大きい場合は、再結
晶、未再結晶の2つのグループに分け、該実効歪が該限
界歪よりも小さい場合は、未再結晶グループのみとし、
前記入側粒径、前記実効歪および前記製造条件より、予
め定めたフェライト再結晶モデルを用いて各グループに
おける占積率および平均粒径を計算し、各パス毎に平均
フェライト粒径および残留歪を繰り返し計算し、最終圧
延パス後のオーステナイト及びフェライトそれぞれの占
積率、平均粒径及び残留歪を求め、その後は、該各計算
値より冷却完了後の各組織(フェライト、パーライト、
ベーナイト、マルテンサイト)それぞれの体積率、硬度
を算出し、同時に最終平均フェライト粒径を算出するこ
とを特徴とする請求項4に記載の熱間圧延鋼材の製造方
法。5. The rolling pass in the temperature range where the steel material temperature is above the Ar 3 transformation temperature, the average grain size and residual strain of austenite are calculated, and in the rolling pass where the steel material temperature is below the Ar 3 transformation temperature, Using the defined ferrite transformation model, the space factor of ferrite transformed after the previous pass is calculated, and the space factor of all ferrite and all austenite is calculated,
For the austenite part, the average grain size and residual strain of each group are obtained using the austenite recrystallization model, and for the ferrite part, the grain size conversion ratio model is used for the ferrite transformed after the previous pass. Of the ferrite, the residual strain of the ferrite is set to zero, the average ferrite grain size and the average residual strain of the ferrite and the ferrite transformed before the previous pass are determined, and the ferrite grain size is calculated as the entrance grain of the pass. When the effective strain obtained by adding the inlet residual strain to the additional strain of the path is larger than the critical strain of recrystallization, the recrystallization and the unrecrystallized When divided into two groups, the effective strain is smaller than the critical strain, only the non-recrystallized group,
From the inlet side grain size, the effective strain and the manufacturing conditions, the space factor and the average grain size in each group are calculated using a predetermined ferrite recrystallization model, and the average ferrite grain size and the residual strain are calculated for each pass. Is repeatedly calculated, the space factor of each of the austenite and ferrite after the final rolling pass, the average grain size and the residual strain are obtained, and thereafter, each structure after completion of cooling from each calculated value (ferrite, pearlite,
The method for producing a hot-rolled steel product according to claim 4, wherein the volume ratio and hardness of each of bainite and martensite) are calculated, and at the same time, the final average ferrite grain size is calculated.
残留歪を計算するにあたり、前記実効歪εが(1)式で与
えられるεmよりも大きい場合には、再結晶及び未再結
晶の2つのグループに分け、圧延直後での再結晶占積率
ffDおよび粒径dfDを(2)(3)式を用いて求め、その後に再
結晶した部分の占積率ffSを(4)式から計算し、パス間で
の再結晶粒径の変化を(5)式から求め、未再結晶領域の
占積率ffNおよび粒径dfNを(6)(7)式で計算し、実効歪ε
がεmよりも小さい場合には、未再結晶領域の占積率f
fNおよび粒径dfNのみを(6)(7)式から計算し、次パス直
前の平均フェライト粒径fを(8)式で計算し、パス間
での歪の回復を考慮して次パス直前の残留歪Δεを(9)
式を用いて計算することを特徴とする請求項5に記載の
熱間圧延鋼材の製造方法。 εm=h(dfi,,T) (1) ffD=h(dfi,ε,,T) (2) dfD=h(dfi,ε,T) (3) ffS=h(ε,T,t) (4) dfS=h(dfD,T,t) (5) ffN=h(ffD,ffS) (6) dfN=h(dfi,ε) (7)f =h(ffD,ffS,ffN,dfS,dfN) (8) Δεf=h(ffD,ffN,εm,ε,T,(%C)) (9) ここで、dfiはパス入側のフェライト粒径(μm)、
は歪速度(s-1)、Tは圧延温度(℃)、εは加工歪、
tは加工後の時間(秒)、(%C)は炭素含有量(重量
%)である。6. When calculating the average grain size and residual strain of a ferrite part, when the effective strain ε is larger than ε m given by the equation (1), recrystallization and non-recrystallization are performed. Divided into two groups, recrystallization space factor immediately after rolling
The f fD and the grain size d fD are obtained by using the equations (2) and (3), and the space factor f fS of the recrystallized part is calculated from the equation (4). The change is calculated from Eq. (5), the space factor f fN and the grain size d fN of the unrecrystallized region are calculated by Eqs . (6) and (7), and the effective strain
Is smaller than ε m, the space factor f of the unrecrystallized region is
Only fN and grain size d fN are calculated from Eqs . (6) and (7), the average ferrite grain size f immediately before the next pass is calculated using Eq. (8), and strain recovery between passes is taken into consideration. The residual strain Δε immediately before is (9)
The method for manufacturing hot-rolled steel product according to claim 5, wherein the hot-rolled steel product is calculated using a formula. ε m = h (d fi ,, T) (1) f fD = h (d fi , ε ,, T) (2) d fD = h (d fi , ε, T) (3) f fS = h ( ε, T, t) (4) d fS = h (d fD , T, t) (5) f fN = h (f fD , f fS ) (6) d fN = h (d fi , ε) (7 ) f = h (f fD , f fS , f fN , d fS , d fN ) (8) Δε f = h (f fD , f fN , ε m , ε, T, (% C)) (9) where And d fi is the ferrite grain size (μm) on the path entry side,
Is strain rate (s -1 ), T is rolling temperature (° C), ε is working strain,
t is a time (second) after processing, and (% C) is a carbon content (% by weight).
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2517089 | 1989-02-03 | ||
| JP1-25170 | 1989-02-03 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH02290916A JPH02290916A (en) | 1990-11-30 |
| JPH0711024B2 true JPH0711024B2 (en) | 1995-02-08 |
Family
ID=12158531
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2392190A Expired - Lifetime JPH0711024B2 (en) | 1989-02-03 | 1990-02-02 | Manufacturing method of hot rolled steel and its material prediction method |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0711024B2 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113063813B (en) * | 2021-03-15 | 2023-11-10 | 鞍钢股份有限公司 | Method for establishing continuous cooling phase change model of steel material |
-
1990
- 1990-02-02 JP JP2392190A patent/JPH0711024B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| JPH02290916A (en) | 1990-11-30 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US6430461B1 (en) | Process for monitoring and controlling the quality of rolled products from hot-rolling processes | |
| WO1992021970A1 (en) | Method of estimating material of steel product | |
| CN104602830A (en) | Material structure prediction device, product manufacturing method, and material structure prediction method | |
| KR102448426B1 (en) | How the annealing furnace works | |
| JP2597986B2 (en) | Manufacturing method of hot rolled steel | |
| McQueen | Metal forming: Industrial, mechanical computational and microstructural | |
| Lenard | Modelling hot deformation of steels: an approach to understanding and behaviour | |
| JP6068146B2 (en) | Set value calculation apparatus, set value calculation method, and set value calculation program | |
| CN1330930C (en) | Flexible measurement method for grain sizes of steel plate internal structure during rolling process | |
| Ning et al. | Effect of rolling pass on porosity void closure of bloom during hot-core heavy reduction rolling | |
| Kim et al. | Prediction of the wear profile of a roll groove in rod rolling using an incremental form of wear model | |
| JPH0711024B2 (en) | Manufacturing method of hot rolled steel and its material prediction method | |
| Muojekwu et al. | Thermomechanical history of steel strip during hot rolling-A comparison of conventional cold-charge rolling and hot-direct rolling of thin slabs | |
| EP4527952A1 (en) | Hot-rolled steel strip annealing method, and electromagnetic steel sheet production method using said annealing method | |
| JP2672572B2 (en) | Manufacturing method of hot rolled steel | |
| McQueen et al. | Hot workability testing techniques | |
| Kurpe et al. | Finite-element simulation of Steckel mill rolling | |
| KR100931222B1 (en) | Cooling Control Method of High Carbon Hot Rolled Sheets Considering Phase Transformation and Edge Crack Prevention | |
| JP2509487B2 (en) | Steel plate material prediction method | |
| Byon et al. | Predictions of roll force under heavy-reduction hot rolling using a large-deformation constitutive model | |
| Harding | Temperature and structural changes during hot rolling. | |
| Vorozheva et al. | Assessment of Deformation Behavior of Thin Slabs by the Method of Quantitative Metallography | |
| Schmickl et al. | Prediction of ferrite grain size after warm deformation of low carbon steel | |
| JP7338599B2 (en) | Method for predicting generation of blister scale, method for controlling rolling mill, and method for generating prediction model for generation of blister scale | |
| Muntin | Technological features of the production of steel strips of various ranges in casting and rolling complexes |