HIGH STRENGTH STEEL SHEET AND METHOD FOR PRODUCING THE SAME

Abstract
The present invention relates to A high strength steel sheet having a structure which is mainly composed of MD structure (Micro Duplex structure) comprising a ferrite matrix, and as a secondary phase, martensite or martensite and retained austenite, finely dispersed in said matrix, wherein the proportion that the MD structure occupies in the whole structure is 90% or more, wherein the proportion that the secondary phase present in the whole structure occupies in the whole structure is from 10 to 60%, wherein the secondary phase in the MD structure is present in ferrite grains and at grain boundary, in which the proportion of the secondary phase present in the ferrite grains is 50% or more, and wherein the average grain size of the secondary phase in the whole structure is 3 μm or less. The secondary phase is constituted of martensite, or martensite and retained austenite.
Description
TECHNICAL FIELD

The present invention relates to a high strength dual phase steel sheet having excellent elongation and stretch flangeability. In particular, it relates to a high strength dual phase steel sheet having excellent strength-elongation and stretch flangeability in high strength region of 590 MPa or more.


BACKGROUND OF THE INVENTION

In industrial fields of automobiles, electrical machinery and appliances, machinery and the like, steel sheets used by press forming are required to combine excellent strength and formability. In recent years, such demand characteristics are increasing more and more. Dual phase steel sheets (DP steel) having dual phase of ferrite and martensite, and TRIP steels comprising a structure containing ferrite, bainite and retained austenite are known as high strength steel sheets having excellent ductility. However, dual phase steel sheets such as DP steel and TRIP steel have the problem that stretch flangeability is poor.


To improve stretch flangeability in high strength steel sheets, a method of suppressing localization of strain by making the structure a single phase structure to homogenize processability in the structure, and a method of reducing strength difference between a soft phase and a hard phase in a dual phase structure are known. Regarding those two methods, for example, the following technologies are disclosed.


1. Single Phase Structure (See Patent Document 1)


A method of producing a martensite single phase steel sheet having tensile strength of from 880 to 1,170 MPa by bringing more balance to components and heat treatment conditions has been disclosed. For the production of a martensite single phase structure, soaking temperature necessary for austenitizing is set to 850° C. which is generally the industrially attainable temperature condition, and this made it possible to industrially achieve a martensite single phase structure. However, a steel sheet of a martensite single phase structure is that the structure is macroscopically uniform, so that stretch flangeability is excellent, but ductility (elongation) greatly deteriorates (EL<8%).


2. Reduction in Strength Difference of Dual Phase Structure (See Patent Document 2)


A steel sheet having a space factor of a low temperature transformation phase of 90% or more is heated and held in two phase regions of ferrite and austenite, thereby fine ferrite and austenite succeeding lath of a low temperature transformation phase can be formed. After the subsequent cooling, a structure in which ferrite and the low temperature transformation phase are finely dispersed in a lath state is finally formed. Such a finely dispersed low temperature transformation phase suppresses formation and growth of voids at the time of flange deformation, thereby improving stretch flangeability.


However, in this method, the structure become fine, but martensite which is a hard phase cannot be precipitated in grains. Furthermore, a grain size of martensite is 5 μm at the minimum, and the structure cannot sufficiently be homogenized. For this reason, improvement effect of stretch flangeability is not sufficient.


3. Fine Retained Austenite Steel Sheet (See Patent Document 3)


A steel sheet in which a secondary phase having an average grain size of 500 nm or less is finely dispersed in grains has been disclosed. High elongation and stretch flangeability are achieved by forming a starting point of fracture in the grains.


In this method, very expensive austenite stabilizing element such as Au, Ag or Ni must be added in order to form the secondary phase in the grains. Additionally, a concentrated region of the austenite stabilizing element must be formed in the grains in order to form the secondary phase in the grains, but to achieve this, a solution heat treatment at 1,270° C. or higher for 5 hours or more becomes necessary. Consequently, industrial problem in increase of time and cost remains in this method.


Patent Document 1: Japanese Patent No. 3729108


Patent Document 2: JP-A-2005-272954


Patent Document 3: JP-A-2005-179703


SUMMARY OF THE INVENTION

Accordingly, the present invention has an object to exhibit both elongation and stretch flangeability particularly in a high strength steel sheet of 590 MPa or more, and further to industrially realize such a high strength steel sheet.


To obtain a high strength steel sheet, it is necessary that a hard phase is a secondary phase, but when the hard phase is present at the grain boundary of a matrix, its interface becomes a starting point of fracture, and local elongation lowers. However, when a hard phase is not present, high strength cannot be obtained. When a hard phase can finely be present in the grains of a matrix, a starting point of fracture can be minimized, and as a result, local elongation of steel can be improved. It is known that local elongation of steel has a correlation with stretch flangeability thereof, and high stretch flangeability can be obtained by improving local elongation.


Thus, to improve stretch flangeability while maintaining high ductility in a high strength steel sheet of 590 MPa or more, it is important to be a dual phase steel sheet and to uniformly and finely precipitate a hard secondary phase in the grains of a matrix. Furthermore, it is important that the production of steel can industrially be realized.


In view of the above, the present inventors thought that the entire surface of a steel sheet is constituted of bainite in order to provide a steel sheet having improved stretch flangeability while maintaining high ductility even in a high strength region of 590 MPa or more, and thought to control the existence form of cementite in bainite. The reason that the matrix is bainite is that lath of bainitic ferrite constituting bainite is not grain boundary, and is therefore difficult to become a starting point of fracture. As a result of verification, cementite which is a hard phase could finely be dispersed among laths, but bainite is slightly poor in ductility, and the desired elongation was not obtained.


Subsequently, Si was added to improve elongation. By adding Si, precipitation of cementite is suppressed in the course of cooling, and austenite in which C is concentrated is formed among laths of bainitic ferrite. Furthermore, bainite transformation is completed, and cooling rate was controlled such that lath of bainitic ferrite disappears in the course of the subsequent cooling.


As a result, a structure comprising a ferrite phase and austenite finely dispersed therein was obtained in the cooling process. When austenite reached Ms point or lower, MD structure comprising a ferrite phase and martensite as a hard phase finely dispersed therein was obtained. However, in this method, a ferrite phase in which martensite is not dispersed in the ferrite phase was simultaneously formed. When such ferrite is present in the structure, strength deteriorates, and in addition, stretch flangeability deteriorats due to strength difference at the interface between the ferrite and MD.


In view of the above, the present inventors have further made researches and found that formation of ferrite which does not contain martensite can be suppressed by adding B. As a result, nearly the entire surface can be constituted of MD structure, and the present invention could be completed based on this finding.


When such unique components and heat treatment are employed, martensite having strength difference to a matrix smaller than a hard cementite can be uniformly and finely dispersed in ferrite grains. As a result, it was clarified that a dual phase steel sheet having excellent strength-stretch flangeability while maintaining high ductility can be provided even in a high strength region of 590 MPa or more.


Furthermore, DP steel, TRIP steel and the like described above are conventionally developed as the means to combine strength and ductility (elongation). DP steel comprises hard martensite and soft ferrite. The hard martensite ensures strength, and the soft ferrite ensures ductility (elongation). On the other hand, TRIP steel is that retained austenite generates deformation-induced transformation during deformation, thereby improving ductility (elongation). However, the ductility (elongation) used herein means uniform elongation, and those steel sheets are excellent to combine strength and ductility (uniform elongation), but had the disadvantage that local elongation is poor. It is known that local elongation has a high correlation with stretch flangeability, and improvement in local elongation is indispensable to obtain high stretch flangeability.


Accordingly, as a result of intensive investigations to provide a steel sheet which combines elongation and stretch flangeability even in a high strength region of 590 MPa or more, namely a steel sheet combining uniform elongation and local elongation in addition to strength, the present inventors have succeeded to develop a high strength steel sheet having excellent elongation and stretch flangeability, leading to the present invention.


Development process of the steel of the present invention and mechanism of exhibiting high properties are described below.


To combine strength and ductility, it is advantageous to be a dual phase structure in which a soft phase and a hard phase are combined, and the steel of the present invention has a dual phase structure comprising ferrite as a soft phase and martensite as a hard phase. However, even though a dual phase structure merely comprising soft ferrite and hard martensite is formed as in DP steel as described before, it is effective to combine strength and uniform elongation, but it is not sufficient to ensure excellent stretch flangeability. The reason that DP steel is poor in stretch flangeability includes size and existence position of martensite as a hard phase. Specifically, martensite in DP steel is generally large as about several ten μm, and grain boundary between martensite and ferrite is large tilt grain boundary. When deformation is added to a steel sheet, stress concentrates at grain boundary (large tilt grain boundary) as compared with the inside of grains. When interface having strength difference is present here, voids are generated in a moment, which is liable to lead to fracture. Such generation of voids and fracture have a correlation with local elongation, and a steel sheet that is liable to cause generation of voids and propagation of cracks is poor in local elongation. Grain boundary between ferrite and martensite in DP steel is just an interface having strength difference, and excellent stretch flangeability cannot be possessed for this reason. Furthermore, although it is considered that this tendency is decreased with decreasing a size of a hard phase, this effect cannot be obtained in a size of martensite in general DP steel.


In view of the above, the present inventors thought that as the means for improving stretch flangeability while maintaining excellent properties of DP steel (combining strength and uniform elongation), a dual phase structure having a soft phase (ferrite) and a hard phase (martensite) is basically formed, but martensite is finely dispersed in ferrite grains (or small tilt grain boundary). They further thought that even in the case of ensuring the same degree of strength, grain size of the individual martensite can be decreased as compared with the general DP steel, and by further making martensite present in grains (or small tilt grain boundary), it becomes possible to suppress generation of voids in the case that deformation has been generated. By those, it is possible to combine elongation and stretch flangeability, and in addition to this, it is expected that ductility (particularly, uniform elongation) is further improved by utilizing TRIP effect as a structure containing retained austenite. The steel of the present invention developed based on the above-described thoughts has a structure comprising ferrite as a matrix, and martensite and retained austenite, finely dispersed mainly in ferrite grains. Due to this structure, the steel combines elongation and stretch flangeability in addition to strength.





BRIEF DESCRIPTION OF THE DRAWING


FIG. 1 is a schematic view showing thermo-mechanical treatment in the Examples.





DETAILED DESCRIPTION OF THE INVENTION

The present invention relates to the following (1).


(1) A high strength steel sheet having a structure which is mainly composed of MD structure (Micro Duplex structure) comprising a ferrite matrix, and as a secondary phase, martensite or martensite and retained austenite, finely dispersed in said matrix,


wherein the proportion that the MD structure occupies in the whole structure is 90% or more,


wherein the proportion that the secondary phase present in the whole structure occupies in the whole structure is from 10 to 60%,


wherein the secondary phase in the MD structure is present in ferrite grains and at grain boundary, in which the proportion of the secondary phase present in the ferrite grains is 50% or more, and


wherein the average grain size of the secondary phase in the whole structure is 3 μm or less.


In the present invention, the secondary phase is constituted of martensite, or martensite and retained austenite.


The term “proportion” used herein means a proportion of area (area fraction). Furthermore, the term “whole structure” used herein means the entire of MD structure and other structures.


It is desirable that an average grain size of ferrite in the whole structure is 20 μm or less, and 20 or more secondary phases on the average are present in an observation view of 50 μm×50 μm in the whole structure.


Furthermore, it is desirable in the high strength steel sheet that the proportion that the retained austenite present in the whole structure occupies in the whole structure is 2% or more.


The high strength steel sheet has a composition comprising, in terms of % by mass, C: 0.02 to 0.3%; Si: 0.01 to 3%; Mn: 0.5 to 3%; B: 0.0001 to 0.005%; and Al: 0.01 to 1.5%, with the remainder being Fe and inevitable impurities.


The high strength steel sheet may further contain one or two or more of:


(1) Mo: 0.03 to 1%;


(2) at least one element selected from the group consisting of Nb, Ti and V in the total amount of from 0.01 to 0.1%;


(3) at least one of Ni: 0.5% or less (not including 0%) and Cu: 0.5% or less (not including 0%);


(4) Cr: 1.5% or less (not including 0%); and


(5) at least one of Ca: 0.003% or less (not including 0%) and REM (rare earth element): 0.003% or less (not including 0%).


In addition, a method for producing a high strength steel sheet according to the present invention comprises heating a steel sheet material comprising the above-described component compositions, and cooling the steel sheet material from a temperature of A3 point or higher to a temperature of Ms point or lower in a cooling rate of from 0.2 to 20° C./sec.


The steel sheet material is produced by appropriately conducting a hot rolling step and a cold rolling step. Those steps are not particularly limited, and the conditions generally practiced can appropriately be selected and employed. For example, as the hot rolling step, conditions of holding at about 1,200° C. for 30 minutes, conducting hot rolling at A3 point or higher, cooling in an average cooling rate of about 30° C./sec, and winding up at about 500 to 600° C. can be employed. In the cold rolling step, it is recommended to conduct cold rolling in a cold rolling ratio of about 30 to 70%, but it is not particularly limited to this.


After heating the steel sheet material at a temperature of A3 point or higher and holding the same at that temperature, the steel sheet material is cooled to a temperature of Ms point or lower, generally room temperature. As a result, the structure of the present invention comprising MD structure in major portion can be obtained, and stretch flangeability can be improved while maintaining high ductility, even in a high strength region of 590 MPa or more.


When the steel sheet material is heated to a temperature of A3 point or higher and held at that temperature, the entire surface of the structure converts into austenite. Then, when the steel sheet material is cooled in a cooling rate of 0.2 to 20° C./sec, a dual phase structure of ferrite-pearlite is generally obtained. However, because Si is added in the present invention, precipitation of cementite is suppressed, and as a result, bainitic ferrite begins to precipitate from the austenite interface. With the growth of lath of bainitic ferrite, austenite decreases its space factor, and austenite is finely dispersed among laths of bainitic ferrite.


The lath of bainitic ferrite is thermally unstable, and therefore disappears in the cooling process after completion of the bainite transformation. As a result, the state that austenite is finely dispersed in the grains of ferrite having bainite block size is obtained, and when the temperature becomes Ms point or lower by further cooling, austenite transforms into martensite. As a result, MD structure comprising ferrite matrix formed by disappearance of the lath of bainitic ferrite, and a secondary phase comprising martensite finely dispersed in the matrix can be obtained. When B is further added, formation of ferrite which does not contain martensite in the grains can be suppressed. Furthermore, when Mo is added, bainite transformation can be completed in a short period of time. Mo is effective to allow the lath of bainitic ferrite to disappear.


Furthermore, the steel sheet having the above-described structure morphology can be obtained by optimizing chemical compositions and production steps (thermo-mechanical treatment conditions) in an industrially possible range. Unclear points still remain regarding appearance mechanism of the above-described structure, and all is not always clarified to the detail. However, at the present, it is considered that the following explanation is possible.


The steel of the present invention can be produced by heating a steel sheet material comprising the above-described component composition controlled in an appropriate range, cooling the material from a temperature of A3 point or higher, subjecting the material to a processing of rolling reduction of 5% or more in a temperature range of 600 to 1,000° C., and then cooling the material to a temperature of Ms point or lower in a cooling rate of 0.2 to 20° C./sec. This production step (thermo-mechanical treatment) may be conducted in a hot rolling step or may be conducted after a hot rolling step and a cold rolling step, generally conducted (in this case, this thermo-mechanical treatment is conducted by reheating).


Accordingly, MD structure comprising ferrite as a matrix, and martensite and retained austenite, which are finely dispersed mainly in ferrites grains is formed. Thus, the structure of the present invention can be produced by forming an austenite single phase structure at a temperature of A3 point or higher, cooling, adding processing at a predetermined temperature and then cooling in an appropriate range.


As described above, the structure formation mechanism of the steel of the present invention is not clarified to the detail, but one explanation that is considered at the present is described below. Therefore, the following description is not construed to limit the technical scope of the present invention.


One of various structure design guidelines devised to obtain the structure of the present invention is described below.


The present inventors thought to obtain a structure comprising ferrite as a matrix, and martensite and retained austenite finely dispersed therein, using bainite transformation generated during the cooling process. For this, bainite is formed during the cooling step after processing, but in the steel of the present invention, a mixed structure of bainitic ferrite and cementite as in general bainite is not formed. Since cementite is harder than martensite, such is harmful to stretch flangeability. Furthermore, to ensure retained austenite which is essential in the steel of the present invention, it is necessary to concentrate C in austenite, and it is therefore necessary to prevent precipitation of cementite which disturbs to concentrate C. For this reason, in the steel of the present invention, Si and Al are added to suppress precipitation of cementite in the cooling process. Accordingly, austenite in which C is concentrated among laths of bainitic ferrite is formed. This austenite is transformed into martensite in the subsequent cooling step, or remains as retained austenite without transformation.


Lath of bainitic ferrite is small tilt grain boundary, and concentration of strain during deformation as in large tilt grain boundary described before is difficult to be generated. As a result, martensite and retained austenite present among laths of bainitic ferrite are difficult to become a starting point of fracture. The term “ferrite grain boundary” used herein means large tilt grain boundary of ferrite, and lath boundary which is difficult to become a starting point of fracture is not grain boundary.


However, it is difficult to observe small tilt grain boundary at the position that martensite and retained austenite are present, in the structure obtained by the present inventors. It suggests that the steel of the present invention has further excellent structure morphology based on the following reasons.


In the steel of the present invention, processing is added at a predetermined temperature region, and as a result, bainite transformation is accelerated and bainite transformation is completed in a short period of time. Additionally, since the subsequent cooling rate is set to relatively low condition, it is still present at relatively high temperature for a certain period of time even after bainite transformation. For this reason, it is considered that even lath (small tilt grain boundary) of bainitic ferrite disappears, and as a result, it is considered that a structure (MD structure) comprising ferrite grains and martensite and retained austenite mainly dispersed therein was obtained.


In the above description, one of thoughts considered at present is shown as appearance mechanism of the structure of the present invention, but only the steel comprising the bainitic ferrite as a matrix is not the object of the present invention. In other words, ferrite which is a matrix of MD structure of the present invention is not limited to only ferrite wherein lath of bainitic ferrite becomes unclear, but includes ferrite which is precipitated at relatively high temperature, like pro-eutectoid ferrite. Thus, the present invention includes all of MD structure steel sheets having structure morphology defined in the present application.


Furthermore, the present inventors have found in the course of the above investigations that when ferrite in which martensite and retained austenite are not present is present, not only strength deteriorates, but stretch flangeability deteriorates by strength difference at the interface between ferrite and MD structure. Based on this finding, formation of such martensite-free ferrite is suppressed by adding B, thereby nearly the entire surface is constituted of MD structure.


The present invention can provide a dual phase steel sheet having excellent strength-elongation and stretch flangeability while maintaining high ductility even in high strength region of 590 MPa or more by forming a structure comprising martensite, or martensite and retained austenite which have small strength difference to a matrix as compared with hard cementite, uniformly and finely dispersed in ferrite grains.


Furthermore, according to the present invention, such a dual phase steel sheet can be produced by industrially possible means.


The structure of the present invention in the case that the secondary phase is martensite is described below.


Ferrite which is a matrix means ferrite having martensite contained in grains, formed in the cooling process from A3 point, and this ferrite includes pro-eutectoid ferrite and ferrite from which lath of bainitic ferrite has disappeared. On the other hand, this ferrite does not include ferrite which does not contain fine martensite in grains even though it is pro-eutectoid ferrite and ferrite from which lath of bainitic ferrite has disappeared. In the present invention, ferrite containing martensite in grains and ferrite which does not contain fine martensite in grains can be identified by, for example, applying the structure after completion of cooling to repeller corrosion, and showing ferrite in gray and martensite in white by image analysis. The entire surface of ferrite which does not contain fine martensite in grains is gray. On the other hand, the MD structure of the present invention is that fine martensite is contained in a ferrite phase. Therefore, fine white spot can be confirmed in ferrite grains.


The structure of the present invention is mainly composed of MD structure, and the MD structure comprises ferrite as a matrix and martensite as a secondary phase. The martensite as a secondary phase is formed such that austenite present in the ferrite matrix transforms into martensite at Ms point or lower in the cooling process. When the area fraction of the whole structure is defined as 100%, the proportion of the MD structure is required to be 90% or more. Where the proportion of the MD structure is less than 90%, influence of the remainder increases, uniformity of the structure is impaired, and stretch flangeability deteriorates. The remainder includes retained austenite, pearlite, bainite, and ferrite which is not accompanied with martensite in grains. On the other hand, the proportion that the MD structure occupies in the whole structure is better as large, and the upper limit is not particularly defined. Furthermore, when the area fraction of the whole structure is defined as 100%, the proportion of martensite as a secondary phase present in the whole structure (martensite present in MD structure and other structures) is required to be from 10 to 60%, and the desired strength can be obtained by this proportion. When the proportion is less than 10%, sufficient strength is not obtained, and when it exceeds 60%, elongation deteriorates. The proportion is preferably in a range of from 20 to 60%, more preferably in a range of from 30 to 55%, and most preferably in a range of from 40 to 50%.


Martensite in the MD structure is nearly uniformly dispersed in ferrite grains and at ferrite grain boundary. When the whole of the martensite is defined as 100%, the proportion of martensite in ferrite grains is required to be 50% or more (namely, the proportion of martensite present at ferrite grain boundary is less than 50%), and the desired stretch flangeability can be obtained by this proportion. When the proportion is less than 50%, martensite present at ferrite grain boundary acts as a starting point of fracture, and stretch flangeability deteriorates. The proportion of martensite in ferrite grains is preferably 60% or more, and more preferably 70% or more.


In the present invention, the term “grain boundary of ferrite matrix” means block boundary of bainitic ferrite formed by bainite transformation during cooling, and, for example, when orientation difference of adjacent ferrites is measured by FE/SEM-EBSP (Electron Back Scatter Diffraction Pattern), large tilt grain boundary in which the orientation difference is 15° or more is defined as block boundary, i.e., grain boundary, and a region surrounded by the block boundary is defined as grain.


Next, the structure of the present invention in the case that the secondary phase is martensite and retained austenite is described below.


The structure of the steel of the present invention is mainly composed of a structure (MD structure) comprising ferrite grains as a matrix and contained therein, fine martensite and retained austenite, as a secondary phase. Ferrite which does not contain a fine secondary phase in grains and MD structure differ in structure morphology. Furthermore, influence giving to properties differs between those, and it is therefore necessary to distinguish those.


As the identification method, for example, those can be identified by, for example, subjecting a steel sheet containing those structures to repeller corrosion, and showing ferrite in gray and martensite and retained austenite in white by image analysis. The entire surface of ferrite which does not contain the fine secondary phase in grains is gray. On the other hand, the MD structure is that fine martensite and retained austenite are contained in a ferrite phase. Therefore, fine white spot can be confirmed in ferrite grains.


When the area fraction of the whole structure is defined as 100%, the proportion of the MD structure (ferrite+martensite+retained austenite) is required to be 90% or more. When the proportion of the MD structure is less than 90%, the influence of the remainder increases, uniformity of the structure is impaired and stretch flangeability deteriorates. The remainder includes ferrite which is not accompanied with the secondary phase in grains, pearlite and bainite. On the other hand, the proportion that the MD structure occupies in the whole structure is better as large, and the upper limit thereof is not particularly defined.


When the area fraction of the whole structure is defined as 100%, the proportion of martensite and retained austenite as a secondary phase present in the whole structure (martensite and retained austenite present in MD structure and other structures) is required to be from 10 to 60%, and the desired strength can be obtained by this proportion. When the proportion is less than 10%, sufficient strength is not obtained, and when it exceeds 60%, elongation deteriorates. The proportion is preferably in a range of from 15 to 55%, more preferably in a range of from 20 to 50%, and most preferably in a range of from 20 to 35%.


The proportion of the secondary phase (martensite and retained austenite in MD structure) in ferrite matrix is that when the whole of the secondary phase in MD structure is defined as 100%, the proportion of the secondary phase in ferrite grains is required to be 50% or more (the proportion of martensite and retained austenite on grain boundary is less than 50%), and the desired stretch flangeability can be obtained by this proportion. When the proportion is less than 50%, martensite and retained austenite present on the grain boundary act as a starting point of fracture, and stretch flangeability deteriorates. The proportion is better as large, and is preferably 60% or more, and more preferably 70% or more.


In the present invention, the term “grain boundary” means large tilt grain boundary, and for example, when orientation difference of adjacent grains is measured by FE/SEM-EBSP (Electron Back Scatter Diffraction Pattern), large tilt grain boundary in which the orientation difference is 15° or more is defined as grain boundary.


When the area fraction of the whole structure is defined as 100%, the proportion that retained austenite present in the whole structure (retained austenite present in MD structure and other structures) occupies in the whole structure is desirably 2% or more. When retained austenite is present as the secondary phase, the desired ductility (mainly uniform elongation) can be obtained. When the proportion is less than 2%, the expected ductility improvement effect is diluted. The proportion is preferably 5% or more, and more preferably 8% or more. The proportion of the retained austenite is better as large, but from a practical standpoint, the upper limit is about 20%.


In the structure of the present invention, an average grain size of the secondary phase present in the whole structure (the secondary phase present in MD structure and other structures) is required to be 3 μm or less. When the average grain size of the secondary phase is larger than 3 μm, starting points of fracture are localized, and as a result, sufficient stretch flangeability is not obtained. The average grain size of the secondary phase is better as small, and is preferably 2.5 μm or less, and more preferably 2 μm or less.


An average grain size of ferrite in the whole structure (ferrite present in MD structure and other structures) is preferably 20 μm or less, and the desired stretch flangeability can be obtained by this grain size. When the grain size exceeds 20 μm, local deformability deteriorates, and stretch flangeability deteriorates, which is not preferable. The average grain size is better as small, and is preferably 15 μm or less, and more preferably 10 μm or less.


On the other hand, the secondary phase in the whole structure (martensite, or martensite and retained austenite, present in MD structure and other structures) is required to be finely dispersed, and it is preferred that 20 or more secondary phases on the average are observed in an observation view of 50 μm×50 μm. When the number of the secondary phase is less than 20, the desired strength may not be ensured, or there is the possibility that stretch flangeability deteriorates, which is not preferable. The number of the secondary phase is preferably 30 or more, and more preferably 40 or more. The number is preferable as large, such as 50 or more, 80 or more, and 100 or more.


The MD structure steel sheet having the structure morphology of the present invention has a composition comprising, in terms of % by mass, C: 0.02 to 0.3%, Si: 0.01% to 3%, Mn: 0.5 to 3%, B: 0.0001 to 0.005%, and Al: 0.01 to 1.5%, with the remainder being Fe and inevitable impurities.


The composition may further contains one or two or more of:


(1) Mo: 0.03 to 1%;


(2) at least one element selected from the group consisting of Nb, Ti and V in the total amount of from 0.01 to 0.1%;


(3) at least one of Ni: 0.5% or less (not including 0%) and Cu: 0.5% or less (not including 0%);


(4) Cr: 1.5% or less (not including 0%); and


(5) at least one of Ca: 0.003% or less (not including 0%) and REM (rare earth element): 0.003% or less (not including 0%).


The above component composition is described below. In the followings, all the percentages are defined by mass, unless otherwise indicated. Additionally, all the percentages defined by mass are the same as those defined by weight, respectively.


C: 0.02 to 0.3%

C is an effective component to obtain strength of steel. The lower limit 0.02% is the minimum necessary amount to obtain a predetermined space factor of a secondary phase, thereby obtaining the desired strength. The upper limit 0.3% is that where C is added more than this amount, strength of martensite increases, and as a result, stretch flangeability deteriorates. The content of C is in a range of preferably from 0.03 to 0.25%, and more preferably from 0.04 to 0.20%.


Si: 0.01 to 3%

Si is an element to decrease the amount of a solid solution C in ferrite, to contribute to improvement of ductility such as elongation, and to suppress precipitation of cementite during bainite transformation. Si is added in an amount of 0.01% or more. When the amount of Si added is less than 0.01%, cementite precipitates during cooling, and martensite is not formed among laths. Additionally, it is difficult to ensure the desired amount of retained austenite. The content of Si is preferably 0.3% or more, and more preferably 0.5% or more. On the other hand, when Si is added in an amount exceeding 3%, cracks may be generated, resulting in deterioration of elongation and stretch flangeability. The content of Si is preferably 2.5% or less, and more preferably 2% or less.


Mn: 0.5 to 3%

Mn enables steel to have high strength by solid-solution hardening, and at the same time, improves hardenability of steel. Mn further has a function to accelerate formation of martensite. Such a function is recognized in the steel having Mn content of 0.5% or more. Mn content is preferably 0.7% or more, and more preferably 1% or more. On the other hand, when Mn is added in an amount exceeding 3%, stretch flangeability deteriorates. Mn content is preferably 2.5% or less, and more preferably 2% or less.


B: 0.0001 to 0.005%

B is important for the present invention. When B is added, formation of pro-eutectoid ferrite can be suppressed, thereby preventing precipitation of ferrite which is not accompanied with fine secondary phase in grains, such ferrite adversely affecting stretch flangeability. This effect is exhibited when B is added in an amount of 0.0001% or more. The amount of B added is preferably 0.0002% or more, and more preferably 0.0003% or more. On the other hand, when B is added in an amount exceeding 0.005%, the degree of segregation to grains increases, resulting in deterioration of stretch flangeability. For this reason, 0.005% is defined as the upper limit of B content. The amount of B is preferably 0.004% or less, and more preferably 0.003% or less.


Al: 0.01 to 1.5%

Al is used for deoxidation of steel. When the amount of Al is less than 0.01%, silicate inclusions retain, thereby resulting in deterioration of processability of steel. Therefore, the amount of Al added must be 0.01% or more. Furthermore, similar to Si, Al has the effect to prevent precipitation of cementite, and to contribute to ensuring retained austenite. The amount of Al added is preferably 0.03% or more, and more preferably 0.05% or more. However, the amount of Al exceeding 1.5% invites increase of surface mark, and retained austenite and martensite are liable to grow, inviting deterioration of elongation and stretch flangeability. For this reason, the upper limit of Al content is set at 1.5%. The amount of Al is preferably 1% or less, and more preferably 0.5% or less.


The steel sheet material of the present invention may further contain the following components in addition to the above-described essential components.


Mo: 0.03 to 1%

Mo is an element effective to accelerate bainite transformation and to accelerate disappearance of lath of bainitic ferrite during heat treatment. Mo further has the effect to suppress ferrite transformation and to improve hardenability. To obtain such effects, Mo is necessary in an amount of 0.03% or more. The amount of Mo is preferably 0.07% or more, and more preferably 0.1% or more. On the other hand, addition of Mo in an amount exceeding 1% results in increase of strength and deterioration of stretch flangeability. Therefore, the upper limit of Mo content is set at 1%. The amount of Mo is preferably 0.8% or less, and more preferably 0.6% or less.


Total of at least one element selected from the group consisting of Nb, Ti and V: 0.01 to 0.1%


Nb, Ti and V have the function to form a carbonitride and to increase strength of steel by precipitation strengthening and the function to refine grains, and can be added according to need. Such functions are not exhibited when the total amount of at least one of Nb, Ti and V added is less than 0.01%. On the other hand, when at least one of those is added in the total amount exceeding 0.1%, precipitate increases, resulting in remarkable deterioration of stretch flangeability. For this reason, the upper limit is set at 0.1%. The total amount is preferably 0.05% or less, and more preferably 0.03% or less.


At least one of Ni: 0.5% or less (not including 0%) and Cu: 0.5% or less (not including 0%)


Ni and Cu are elements effective to realize high strength while maintaining high strength-ductility balance, and are appropriately added. However, even though those are added in excess, the effect is saturated, and additionally, productivity deteriorates, such as generation of cracks during hot rolling. Therefore, the amounts of Ni and Cu added are suppressed to 0.5% or less, respectively. The amounts of those added are preferably 0.3% or less, and more preferably 0.2% or less, respectively. To effectively exhibit the effect, it is recommended to add Ni in an amount of 0.1% or more and/or Cu in an amount of 0.1% or more.


Cr: 1.5% or less (not including 0%)


Cr is an element effective to enhance strength of steel by improving hardenability, and is appropriately added. However, even though it added in excess, the effect is saturated, and additionally, ductility deteriorates. Therefore, the amount of Cr added is preferably suppressed to 1.5% or less. The amount of Cr added is preferably 1.0% or less, and more preferably 0.8% or less. To effectively exhibit the effect, it is recommended to add Cr in an amount of 0.1% or more.


At least one of Ca: 0.003% or less (not including 0%) and REM: 0.003% or less (not including 0%)


Ca and REM (rare earth element) are elements effective to control morphology of a sulfide in steel and to improve stretch flangeability, and are appropriately added. However, even though those are added in excess, the effect is saturated, and the excessive addition is not economical. Therefore, the amounts of Ca and REM added are 0.003% or less, respectively. To effectively exhibit the effect, it is recommended to add those in an amount of 0.0003% or more, respectively. Examples of REM include Sc, Y and lanthanoid.


Inevitable Impurities

The composition of the steel sheet according to the present invention is that the remainder other than the above-described components comprises Fe and inevitable impurities. Of the inevitable impurities, P and S are admitted to contain in an amount of P: 0.07% or less (not including 0%) and S: 0.07% or less (including 0%). When processability of a steel sheet is considered, the amount of P and S added is better as small. In particular, where the content of S is high, an inclusion (MnS) increases, which remarkably adversely affects stretch flangeability of a steel sheet. However, where S is added in the above range, the addition does not give influence to properties of a steel sheet.


Next, in the steel sheet according to the present invention, production conditions for obtaining the above-described structure are described below.


The steel sheet of the present invention can be produced by conducting a hot rolling step and a cold rolling step to produce a steel sheet material, and applying a heat treatment step to the steel sheet material. Specific processes of the hot rolling step and the cold rolling step are as described before. However, the production conditions are not limited to those steps, and may appropriately be according to the necessary processes.


The purpose of the heat treatment step is to finely and uniformly disperse martensite in a ferrite phase. When the heating temperature is lower than A3 point, the whole structure does not convert into austenite during heating and holding, and ferrite which is not accompanied with martensite in the state before the heat treatment remains partially. This ferrite has low strength, and forms an interface having large strength difference to MD. As a result, stretch flangeability deteriorates. When the heating temperature is A3 point or higher, such ferrite all disappears. Therefore, the upper limit of the heating temperature is not particularly defined, but from the relationship with practical operating level, it is recommended to appropriately control the heating temperature to a proper value.


To obtain a predetermined structure of the present invention by converting a major part of the structure into MD structure, in the above-described steel composition, it is necessary to set a cooling rate to a range of from 0.2 to 20° C./sec, and cool to Ms point or lower. In general, it is cooled to room temperature. When the cooling rate is less than 0.2° C./sec, ferrite which is not accompanied with martensite as a secondary phase is formed, and the proportion of ferrite and martensite in the MD structure becomes less than 90%, resulting in deterioration of strength and stretch flangeability. Furthermore, the proportion of martensite in ferrite grains decreases, and growth of an average grain size of martensite is generated. The cooling rate is preferably 0.5° C./sec or more, and more preferably 1° C./sec or more. On the other hand, when the cooling rate exceeds 20° C./sec, time and temperature sufficient to disappear lath of bainitic ferrite cannot be ensured, and as a result, elongation and stretch flangeability deteriorate. Where the cooling rate further increases, the whole structure is converted into martensite, and as a result, elongation remarkably deteriorates. For this reason, the cooling rate is required to be 20° C./sec or less. The cooling rate is preferably 15° C./sec or less, and more preferably 10° C./sec or less.


Next, in the steel sheet according to the present invention, other production conditions for obtaining the structure are described below.


The high strength steel sheet of the present invention, that is, MD steel sheet, can be obtained by heating a steel sheet material satisfying the component system as defined above, cooling the material from a temperature of A3 point or higher (for example, 1,200° C.), subjecting the material to a processing of rolling reduction of 5% or more in a temperature range of from 600 to 1,000° C., and then cooling the material to Ms point at a cooling rate of from 0.2 to 20° C./sec.


Heating and holding the steel sheet material at a temperature of A3 point or higher, and then subjecting the material to a processing at rolling reduction of 5% or more in a temperature range of from 600 to 1,000° C.:


The steel sheet of the present invention has MD structure comprising ferrite as a matrix and a secondary phase finely dispersed therein, on nearly the entire surface thereof. When the heating temperature is lower than A3 point, the structure during heating does not converts into austenite on the entire surface, and ferrite which is not accompanied with fine secondary phase is formed. The ferrite which is not accompanied with the fine secondary phase in grains contributes to the increase of elongation, but strength difference at the interface to the MD structure increases, and as a result, stretch flangeability deteriorates. The heating temperature is sufficient to be A3 point or higher, but from the relationship with a practical operating level, it is recommended to appropriately control the heating temperature to a proper value.


The subsequent addition of the processing of rolling reduction of 5% or more in a temperature range of from 600 to 1,000° C. is, for example, to accelerate bainite transformation to thereby facilitate obtaining fine MD structure, or to decrease an average grain size of ferrite. When the processing temperature is lower than 600° C., ferrite is precipitated, and when it is higher than 1,000° C., an average grain size of ferrite increases. Furthermore, where processing ratio is lower than 5%, bainite transformation is not accelerated. The upper limit of the processing ratio is practically about 90%, but the processing ratio higher than that has no problem. The processing temperature is preferably in a range of from 620 to 980° C., and more preferably in a range of 650 to 950° C. The rolling reduction is preferably in a range of from 8 to 85%, more preferably from 10 to 80%, and further preferably from 10 to 60%.


Cooling the steel sheet material to room temperature at a cooling rate of from 0.2 to 20° C./sec:


To obtain a predetermined structure of the present invention by converting a major part of the structure into MD structure, in the above-described steel composition, it is necessary to set a cooling rate to a range of from 0.2 to 20° C./sec. In general, it is cooled to room temperature. When the cooling rate is less than 0.2° C./sec, ferrite which is not accompanied with a secondary phase in grains is formed, and the proportion of the MD structure becomes less than 90%, resulting in deterioration of strength and stretch flangeability. The cooling rate is preferably 0.5° C./sec or more, and more preferably 1° C./sec or more. On the other hand, where the cooling rate exceeds 20° C./sec, the whole structure converts into martensite, and as a result, elongation remarkably deteriorates. For this reason, the cooling rate is required to be 20° C./sec or less. The cooling rate is preferably 15° C./sec or less, and more preferably 10° C./sec or less.


EXAMPLE

Examples in the case that the secondary phase is martensite are described below.


Steels 1A to 5F having the component compositions shown in Tables 1 to 5 were melt to form slabs. The slabs were heated to 1,150° C., hot rolled to a sheet thickness of 3.0 mm at 800° C. and then taken up at 550° C. Surface scale was removed by acid pickling, followed by cold rolling to a sheet thickness of 1.2 mm. Each of the steel sheet materials thus obtained was heated and held at each temperature shown in Tables 6 to 9, and then subjected to heat treatment which cools to each stop temperature at a cooling rate shown in Tables 6 to 9.









TABLE 1







Chemical component of specimen










Chemical component (mass %)




















Steel code
C
Si
Mn
P
S
Al
B
Mo
Other
Ac3 (° C.)
Ms point (° C.)
Remarks






















1A
0.008
0.69
1.89
0.008
0.005
0.23
0.0009
0.87

950
476
Comparison


1B
0.03
1.71
1.22
0.01
0.005
0.17
0.0008
0.56

969
494
Invention


1C
0.03
1.55
2.35
0.008
0.004
0.03
0.0005
0

944
448
Invention


1D
0.08
1.28
1.31
0.009
0.006
0.13
0.0012
0.06

912
474
Invention


1E
0.07
0.62
0.67
0.01
0.005
0.26
0.0034
0

884
506
Invention


1F
0.011
0.09
0.84
0.01
0.005
0.61
0.0011
0.13

897
531
Invention


1G
0.09
1.07
1.17
0.007
0.004
0.95
0.0019
0

897
500
Invention


1H
0.13
2.43
1.67
0.008
0.005
0.05
0.0016
0.45

960
437
Invention


1I
0.12
1.61
2.27
0.01
0.005
0.08
0.0007
0

912
421
Invention


1J
0.18
0.58
1.34
0.008
0.005
0.13
0.0009
0.23

857
436
Invention


1K
0.19
2.17
0.66
0.01
0.006
0.35
0.0015
0

919
466
Invention


1M
0.09
0.008
1.78
0.009
0.005
1.09
0.0018
0.56

867
478
Comparison


1N
0.05
0.02
2.21
0.011
0.005
0.23
0.0023
0.87

893
448
Invention


1O
0.04
0.03
1.25
0.01
0.007
0.81
0.0036
0.13

875
510
Invention


1P
0.08
0.046
1.81
0.01
0.005
0.33
0.0012
0.08

857
460
Invention


1Q
0.13
0.052
1.19
0.009
0.006
0.76
0.0018
0

839
479
Invention


1R
0.06
1.32
1.42
0.011
0.005
0.09
0.0008
0.32

929
474
Invention


1S
0.08
1.34
1.46
0.01
0.005
0.12
0.0009
0

912
468
Invention


1T
0.07
1.23
1.51
0.009
0.006
0.22
0.0015
0.28

920
471
Invention


1U
0.18
1.81
2.34
0.01
0.005
0.07
0.0028
0

905
396
Invention


1V
0.07
2.35
1.02
0.011
0.005
0.34
0.0019
0.34

972
493
Invention


1W
0.12
2.33
1.91
0.007
0.004
0.67
0.0007
0

944
452
Invention


1X
0.04
2.68
1.54
0.01
0.005
0.58
0.0035
0.32

999
490
Invention


1Y
0.17
2.76
1.83
0.009
0.005
0.32
0.0018
0

950
427
Invention


1Z
0.08
3.34
0.76
0.011
0.006
0.87
0.0009
0.04

995
517
Comparison
















TABLE 2







Chemical component of specimen










Chemical component (mass %)




















Steel code
C
Si
Mn
P
S
Al
B
Mo
Other
Ac3 (° C.)
Ms point (° C.)
Remarks






















2A
0.16
1.18
0.38
0.01
0.005
1.07
0.0006
0.23

889
508
Comparison


2B
0.14
0.05
0.56
0.008
0.004
0.09
0.0014
0.65

857
477
Invention


2C
0.07
0.74
0.52
0.01
0.005
0.32
0.0027
0

889
514
Invention


2D
0.03
1.42
1.64
0.008
0.005
0.08
0.0011
0.28

947
476
Invention


2E
0.06
1.3
0.79
0.009
0.006
0.61
0.0013
0

918
516
Invention


2F
0.04
2.08
1.27
0.01
0.003
0.88
0.0016
0.18

968
512
Invention


2G
0.05
0.96
1.29
0.01
0.004
0.12
0.0035
0

908
485
Invention


2H
0.04
1.74
1.85
0.01
0.005
0.92
0.0017
0.24

955
490
Invention


2I
0.07
1.42
1.83
0.011
0.005
0.81
0.0014
0

920
478
Invention


2J
0.13
2.2
2.25
0.009
0.006
0.07
0.0033
0.46

950
415
Invention


2K
0.18
1.08
2.3
0.01
0.005
0.54
0.0025
0

872
412
Invention


2L
0.1
0.96
2.81
0.007
0.007
1.23
0.0026
0.34

899
440
Invention


2M
0.14
0.74
2.82
0.01
0.006
0.91
0.0044
0

867
417
Invention


2N
0.08
0.52
3.25
0.011
0.005
0.47
0.0023
0.65

896
405
Comparison


2O
0.03
1.44
1.36
0.012
0.006
0.006
0.0027
0.56

957
484
Comparison


2P
0.08
1.37
1.75
0.008
0.005
0.02
0.0015
0.47

929
451
Invention


2Q
0.12
1.36
2.41
0.008
0.005
0.02
0.0012
0

900
413
Invention


2R
0.15
2.33
1.52
0.01
0.005
0.98
0.0003
0.23

943
465
Invention


2S
0.04
0.31
1.98
0.01
0.005
0.12
0.002
0

883
462
Invention


2T
0.05
1.29
1.1
0.008
0.005
0.81
0.0011
0.78

947
509
Invention


2U
0.03
1.36
1.38
0.009
0.005
0.79
0.0015
0

936
509
Invention


2V
0.08
1.33
1.79
0.01
0.003
1.28
0.0008
0.05

914
489
Invention


2W
0.06
2.31
0.78
0.01
0.004
1.35
0.0004
0

964
538
Invention


2X
0.08
1.89
1.34
0.01
0.005
1.67
0.0017
0.16

942
518
Comparison


2Y
0.09
0.86
1.59
0.011
0.005
0.08
0.0016
0.03

888
458
Invention


2Z
0.12
1.87
1.73
0.01
0.005
0.45
0.0024
0.11

927
452
Invention
















TABLE 3







Chemical component of specimen










Chemical component (mass %)




















Steel code
C
Si
Mn
P
S
Al
B
Mo
Other
Ac3 (° C.)
Ms point (° C.)
Remarks






















3A
0.07
2.12
2.64
0.008
0.007
0.09
0.0014
0.34

962
423
Invention


3B
0.17
1.19
1.04
0.008
0.005
0.73
0.0018
0.81

905
466
Invention


3C
0.05
1.07
1.08
0.007
0.006
0.77
0.0014
1.19

950
507
Comparison


3D
0.04
0.85
0.66
0.009
0.004
0.33
0
0.3

917
518
Comparison


3E
0.09
2.52
1.75
0.01
0.005
0.49
0.0001
0.12

966
463
Invention


3F
0.12
0.12
2.36
0.01
0.004
0.18
0.0001
0

845
420
Invention


3G
0.15
0.27
1.09
0.01
0.005
0.97
0.0005
0.81

869
478
Invention


3H
0.11
1.52
2.04
0.008
0.005
0.38
0.0005
0

911
442
Invention


3I
0.03
2.49
0.55
0.012
0.005
1.23
0.0011
0.34

997
553
Invention


3J
0.08
1.04
1.67
0.008
0.005
1.03
0.001
0

899
487
Invention


3K
0.05
1.82
1.78
0.011
0.006
0.49
0.0019
0.23

953
476
Invention


3L
0.09
0.26
2.68
0.01
0.004
0.05
0.0022
0

861
414
Invention


3M
0.11
1.28
1.73
0.009
0.005
0.08
0.0047
0.28

909
444
Invention


3N
0.04
1.82
1.88
0.01
0.005
0.58
0.0048
0

951
480
Invention


3O
0.19
1.45
0.89
0.011
0.005
0.69
0.0077
0.51

902
465
Comparison


3P
0.05
1.06
1.6
0.007
0.003
1.10
0.0012
0.77
Ti: 0.02
936
499
Invention


3Q
0.12
1.62
0.96
0.01
0.005
0.58
0.0009
0.36
Ti: 0.02
923
485
Invention


3R
0.08
2.41
1.26
0.01
0.005
0.22
0.0011
0.52
Ti: 0.08
977
476
Invention


3S
0.04
1.09
2.17
0.01
0.004
0.62
0.0004
0
Ti: 0.08
918
470
Invention


3T
0.09
0.46
0.97
0.008
0.006
0.08
0.0012
0.89
Ti: 0.12
898
478
Comparison


3U
0.12
1.66
1.78
0.009
0.005
0.07
0.0017
0.34
Nb: 0.02
925
438
Invention


3V
0.07
1.24
1.83
0.008
0.007
0.32
0.0005
0
Nb: 0.02
912
463
Invention


3W
0.17
0.73
2.14
0.011
0.006
1.04
0.0014
0.65
Nb: 0.08
879
433
Invention


3X
0.05
0.78
1.48
0.01
0.005
0.62
0.0019
0
Nb: 0.08
899
493
Invention


3Y
0.03
1.83
1.54
0.12
0.005
0.78
0.0021
0.49
Nb: 0.12
972
500
Comparison


3Z
0.08
2.22
1.92
0.01
0.004
0.93
0.0016
0.22
V: 0.02
961
472
Invention
















TABLE 4







Chemical component of specimen










Chemical component (mass %)




















Steel code
C
Si
Mn
P
S
Al
B
Mo
Other
Ac3 (° C.)
Ms point (° C.)
Remarks






















4A
0.15
1.69
1.77
0.009
0.005
0.22
0.0034
0
V: 0.02
909
433
Invention


4B
0.11
2.3
0.92
0.01
0.003
0.79
0.0008
0.08
V: 0.08
956
495
Invention


4C
0.08
0.39
0.59
0.007
0.006
1.17
0.0017
0
V: 0.08
878
530
Invention


4D
0.07
1.71
1.18
0.01
0.005
0.98
0.0014
0.04
V: 0.12
946
504
Comparison


4E
0.05
1.96
0.67
0.01
0.005
0.82
0.0018
0.35
Ti: 0.02, Nb: 0.02
963
529
Invention


4F
0.09
2.07
2.45
0.01
0.004
0.05
0.0023
0
Ti: 0.02, Nb: 0.02
942
423
Invention


4G
0.06
1.37
0.72
0.008
0.007
0.09
0.0031
0.65
Ti: 0.03, V: 0.03
945
499
Invention


4H
0.04
1.22
0.92
0.008
0.006
0.84
0.0004
0
Ti: 0.03, V: 0.03
927
524
Invention


4I
0.11
1.08
2.15
0.008
0.005
0.48
0.0026
0.31
Nb: 0.04, V: 0.04
905
438
Invention


4J
0.13
0.11
2.4
0.011
0.005
0.08
0.0011
0
Nb: 0.04, V: 0.04
846
410
Invention


4K
0.08
1.47
0.86
0.008
0.005
0.33
0.0013
0.15
Ti: 0.02, Nb: 0.03
927
495
Invention











V: 0.04


4L
0.05
1.57
1.39
0.009
0.005
0.38
0.0031
0
Ti: 0.02, Nb: 0.03
939
488
Invention











V: 0.04


4M
0.03
1.24
1.54
0.012
0.005
0.81
0.0014
0.72
Ti: 0.05, Nb: 0.05
958
498
Comparison











V: 0.05


4N
0.08
2.38
1.36
0.011
0.004
1.40
0.0019
0.37
Ni: 0.3
966
503
Invention


4O
0.11
1.29
1.08
0.01
0.005
0.38
0.0008
0
Ni: 0.3
896
474
Invention


4P
0.1
0.96
0.78
0.01
0.005
0.09
0.0034
0.79
Ni: 0.6
904
472
Comparison


4Q
0.09
2.24
0.94
0.011
0.003
0.03
0.0045
0.16
Cu: 0.3
954
478
Invention


4R
0.13
1.54
1.29
0.008
0.007
0.64
0.0029
0.47
Cu: 0.3
920
467
Invention


4S
0.18
0.73
2.06
0.007
0.005
0.11
0.0013
0.31
Cu: 0.6
866
400
Comparison


4T
0.03
2.08
1.63
0.011
0.005
0.43
0.0006
0.56
Ni: 0.2, Cu: 0.2
982
484
Invention


4U
0.1
1.39
0.87
0.01
0.005
0.63
0.0003
0
Ni: 0.2, Cu: 0.2
905
497
Invention
















TABLE 5







Chemical component of specimen











Steel
Chemical component (mass %)
Ac3
Ms point




















code
C
Si
Mn
P
S
Al
B
Mo
Other
(° C.)
(° C.)
Remarks






















4V
0.08
0.54
1.45
0.01
0.004
1.24
0.0006
0.68
Cr: 0.2
898
494
Invention


4W
0.05
1.87
1.9
0.008
0.005
0.45
0.0018
0
Cr: 0.2
948
467
Invention


4X
0.06
0.94
1.44
0.011
0.006
0.98
0.0031
0.22
Cr: 0.5
909
490
Invention


4Y
0.09
1.73
1.51
0.008
0.005
1.19
0.0023
0
Cr: 0.5
926
484
Invention


4Z
0.08
1.23
1.63
0.01
0.005
0.97
0.0017
0.75
Cr: 0.8
931
467
Invention


5A
0.18
0.57
0.9
0.01
0.005
0.66
0.0022
0
Cr: 0.8
849
454
Invention


5B
0.16
1.11
1.27
0.012
0.005
1.29
0.0034
0.36
Cr: 1.6
890
448
Comparison


5C
0.07
2.05
2.88
0.01
0.003
0.18
0.002
0.09
Ca: 0.002
951
417
Invention


5D
0.08
1.06
1.5
0.009
0.005
0.11
0.0005
0
Ca: 0.002
900
466
Invention


5E
0.04
1.43
1.27
0.008
0.004
0.30
0.004
0.26
REM: 0.002
942
496
Invention


5F
0.13
0.92
1.66
0.01
0.006
0.52
0.0013
0.05
REM: 0.002
880
454
Invention
















TABLE 6







Heat treatment condition










Heat treatment condition

















Cooling





Heating
Cooling
stop


Material
Steel
temperature
rate
temperature


No.
code
(° C.)
(° C./sec)
(° C.)
Remarks















1
1A
1000
2
10
Comparison


2
1B
1000
2
10
Invention


3
1C
1000
2
10
Invention


4
1D
800
2
10
Comparison


5
1D
850
2
10
Comparison


6
1D
900
2
10
Comparison


7
1D
1000
2
10
Invention


8
1D
1100
2
10
Invention


9
1D
1200
2
10
Invention


10
1E
1000
2
10
Invention


11
1F
1000
2
10
Invention


12
1G
1000
2
10
Invention


13
1H
1000
2
10
Invention


14
1I
1000
2
10
Invention


15
1J
1000
2
10
Invention


16
1K
1000
2
10
Invention


18
1M
1000
2
10
Comparison


19
1N
1000
2
10
Invention


20
1O
1000
2
10
Invention


21
1P
1000
2
10
Invention


22
1Q
1000
2
10
Invention


23
1R
1000
0.05
10
Comparison


24
1R
1000
0.1
10
Comparison


25
1R
1000
0.3
10
Invention


26
1R
1000
0.5
10
Invention


27
1R
1000
1
10
Invention


28
1R
1000
5
10
Invention


29
1R
1000
10
10
Invention


30
1R
1000
20
10
Invention


31
1R
1000
30
10
Comparison


32
1R
1000
50
10
Comparison


33
1R
1000
100
10
Comparison


34
1R
1000
500
10
Comparison


35
1S
1000
0.05
10
Comparison
















TABLE 7







Heat treatment condition










Heat treatment condition

















Cooling





Heating
Cooling
stop


Material
Steel
temperature
rate
temperature


No.
code
(° C.)
(° C./sec)
(° C.)
Remarks















36
1S
1000
0.1
10
Comparison


37
1S
1000
0.3
10
Invention


38
1S
1000
0.5
10
Invention


39
1S
1000
1
10
Invention


40
1S
1000
5
10
Invention


41
1S
1000
10
10
Invention


42
1S
1000
20
10
Invention


43
1S
1000
30
10
Comparison


44
1S
1000
50
10
Comparison


45
1S
1000
100
10
Comparison


46
1S
1000
500
10
Comparison


47
1T
1000
2
10
Invention


48
1U
1000
2
10
Invention


49
1V
1000
2
10
Invention


50
1W
1000
2
10
Invention


51
1X
1000
2
10
Invention


52
1Y
1000
2
10
Invention


53
1Z
1000
2
10
Comparison


54
2A
1000
2
10
Comparison


55
2B
1000
2
10
Invention


56
2C
1000
2
10
Invention


57
2D
1000
2
20
Invention


58
2D
1000
2
100
Invention


59
2D
1000
2
300
Invention


60
2D
1000
2
500
Comparison


61
2E
1000
2
10
Invention


62
2F
1000
2
10
Invention


63
2G
1000
2
10
Invention


64
2H
1000
2
10
Invention


65
2I
1000
2
10
Invention


66
2J
1000
2
10
Invention


67
2K
1000
2
10
Invention


68
2L
1000
2
10
Invention


69
2M
1000
2
10
Invention


70
2N
1000
2
10
Comparison
















TABLE 8







Heat treatment condition










Heat treatment condition

















Cooling





Heating
Cooling
stop


Material
Steel
temperature
rate
temperature


No.
code
(° C.)
(° C./sec)
(° C.)
Remarks















71
2O
1000
2
10
Comparison


72
2P
1000
2
10
Invention


73
2Q
1000
2
10
Invention


74
2R
1000
2
10
Invention


75
2S
1000
2
10
Invention


76
2T
1000
2
10
Invention


77
2U
1000
2
10
Invention


78
2V
1000
2
10
Invention


79
2W
1000
2
10
Invention


80
2X
1000
2
10
Comparison


81
2Y
1000
2
10
Invention


82
2Z
1000
2
10
Invention


83
3A
1000
2
10
Invention


84
3B
1000
2
10
Invention


85
3C
1000
2
10
Comparison


86
3D
1000
2
10
Comparison


87
3E
1000
2
10
Invention


88
3F
1000
2
10
Invention


89
3G
1000
2
10
Invention


90
3H
1000
2
10
Invention


91
3I
1000
2
10
Invention


92
3J
1000
2
10
Invention


93
3K
1000
2
10
Invention


94
3L
1000
2
10
Invention


95
3M
1000
2
10
Invention


96
3N
1000
2
10
Invention


97
3O
1000
2
10
Comparison


98
3P
1000
2
10
Invention


99
3Q
1000
2
10
Invention


100
3R
1000
2
10
Invention


101
3S
1000
2
10
Invention


102
3T
1000
2
10
Comparison


103
3U
1000
2
10
Invention


104
3V
1000
2
10
Invention


105
3W
1000
2
10
Invention
















TABLE 9







Heat treatment condition










Heat treatment condition

















Cooling





Heating
Cooling
stop


Material
Steel
temperature
rate
temperature


No.
code
(° C.)
(° C./sec)
(° C.)
Remarks





106
3X
1000
2
10
Invention


107
3Y
1000
2
10
Comparison


108
3Z
1000
2
10
Invention


109
4A
1000
2
10
Invention


110
4B
1000
2
10
Invention


111
4C
1000
2
10
Invention


112
4D
1000
2
10
Comparison


113
4E
1000
2
10
Invention


114
4F
1000
2
10
Invention


115
4G
1000
2
10
Invention


116
4H
1000
2
10
Invention


117
4I
1000
2
10
Invention


118
4J
1000
2
10
Invention


119
4K
1000
2
10
Invention


120
4L
1000
2
10
Invention


121
4M
1000
2
10
Comparison


122
4N
1000
2
10
Invention


123
4O
1000
2
10
Invention


124
4P
1000
2
10
Comparison


125
4Q
1000
2
10
Invention


126
4R
1000
2
10
Invention


127
4S
1000
2
10
Comparison


128
4T
1000
2
10
Invention


129
4U
1000
2
10
Invention


130
4V
1000
2
10
Invention


131
4W
1000
2
10
Invention


132
4X
1000
2
10
Invention


133
4Y
1000
2
10
Invention


134
4Z
1000
2
10
Invention


135
5A
1000
2
10
Invention


136
5B
1000
2
10
Comparison


137
5C
1000
2
10
Invention


138
5D
1000
2
10
Invention


139
5E
1000
2
10
Invention


140
5F
1000
2
10
Invention









Microstructure and dynamic properties were examined on each of steel sheets obtained above by the following procedures.


Microstructure of each steel was determined by the following method.


Each of steel sheet Nos. 1 to 140 after heat treatment was cut into a test piece for microstructure observation of 10 mm×10 mm×1.2 mm. The test piece was embedded with a cold rolled resin such that the observation position is a position of ¼ of a sheet thickness in a rolled direction. Impression as a landmark was formed with a Vickers tester so as to conduct identification on the structure observation place. The impression was corroded with repeller, and the structure was observed at five positions using an optical microscope in a magnification of 1,000. When the structure photograph after repeller corrosion was image analyzed, ferrite is observed gray, and martensite and retained austenite were observed white. After microstructure observation with an optical microscope, buff polishing and electrolysis polishing were conducted to an extent such that the Vickers impression does not disappear, and structure observation was conducted on the place at a step distance of 100 nm using FE/SEM-EBSP. A boundary having an orientation difference of 15° or more of grains was considered as grain boundary, and the grain boundary was identified.


Optical microphotograph and FE/SEM-EBSP structure photograph were combined as the standard of Vickers impression, and the structure was evaluation.


MD Structure:


The MD structure contains fine martensite (secondary phase) in ferrite grains as a matrix, as described above. The observation results of optical microscope and FE/SEM-EBSP were combined, a structure in which many martensite are present in the inside of grains surrounded by large tilt grain boundary (i.e., in the grains) was identified as MD structure, and its space factor was obtained.


There is the possibility that pearlite, bainite, retained austenite, ferrite which is not accompanied with martensite in grains, and the like are contained as other structures. Identification method of those structures is as follow.


Retained Austenite:


Retained austenite has an FCC structure, and therefore can be identified with FE/SEM-EBSP. Area fraction of austenite in the observation view was determined.


Pearlite:


Pearlite has a lamella structure of ferrite and cementite, and the cementite can be identified with FE/SEM-EBSP. In the Examples, the area fraction of pearlite in the observation view was determined.


Bainite:


Bainite is that lath is present in ferrite grains identified with FE/SEM-EBSP. Structure in which lath is present in ferrite grains was judged as bainite, and area fraction of bainite in the observation view was determined.


Ferrite which is not Accompanied with Martensite in Grains:


Structure in which martensite cannot be confirmed in ferrite grains identified with FE/SEM-EBSP is considered as ferrite which is not accompanied with martensite in grains, and is judged as a structure different from MD structure. Area fraction of ferrite which is not accompanied with martensite in grains in the observation view was determined.


Structure in which MD structure is not observed in the observation view is judged that MD is not present. When the whole structure is defined as 100%, in the case that the total of area fractions of other structures (retained austenite, pearlite, bainite, ferrite which is not accompanied with martensite in grains, and the like) exceeds 10%, the defined structure is not formed. In this case, it was judged that MD is partial.


On the other hand, in the case that the space factor of MD structure occupies 90% or more of the whole structure, the following further detailed investigation was conducted.


Space Factor and Average Grain Size of Martensite:


Space factor of martensite in the whole structure used area fraction of white portion in the whole structure by image analyzing an optical microphotograph. By combining with an image of FE/SEM-EBSP, martensite present in ferrite grains and martensite present at grain boundary were separated. Retained austenite is also observed as a white portion, but austenite can be distinguished from retained austenite by identifying retained austenite which has an FCC structure, with FE/SEM-EBSP. Retained austenite was removed by image analysis of FE/SEM-EBSP, and the space factor of martensite was determined.


On the other hand, an average grain size (particle diameter) of martensite was determined by the following method. Five places of the observation view having a size of 20 μm×20 μm were randomly extracted from a SEM observation photograph (magnification 3,000 times), an average grain size (diameter of a corresponding circle) of martensite and retained austenite in the respective observation views was determined, and its average value was used as a grain size of martensite in the whole structure.


Dynamic properties of each steel were determined by the following methods.


Tensile Properties:


JIS No. 5 test piece obtained from a vertical direction of a steel sheet rolled direction was used, and tensile strength (TS) and Elongation (EL) were measured according to JIS Z 2241. Test pieces having TS of 590 MPa or more and EL of 10% or more were considered as acceptable products. Elongation from strain corresponding to tensile strength to breaking strain was designated as local elongation.


Stretch Flangeability:


Hole expanding ratio λ was measured as stretch flangeability. The hole expanding ratio λ was measured according to JISF (The Japan Iron and Steel Federation) standard (JFST 1001-1996). Steels having λ of 80% or more were considered as acceptable products.


The results obtained are shown in Tables 10 to 15 below.









TABLE 10







Measurement results










Structure parameter















Af of α′
Grain size





Af of α′
in α grain
of α′ in
Dynamic properties




















Presence
Af of MD
in entire
of entire
entire

Total
Local




Material
Steel
or absence
structure
structure
structure
structure
TS
elongation
elongation
λ


No.
code
of MD
(%)
(%)
(%)
(μm)
(MPa)
(%)
(%)
(%)
Remarks





















1
1A

94.5
18.8
70.9
1.5
532
32.9
25.1
169.2
Comparison


2
1B

95.9
27.2
71.9
1.7
668
27.6
19.8
136.8
Invention


3
1C

95.0
45.5
71.3
1.7
933
18.8
10.2
96.5
Invention


4
1D
Partial
28.1



687
18.3
6.5
39.5
Comparison


5
1D
Partial
50.1



715
17.5
6.7
45.2
Comparison


6
1D
Partial
87.4



766
16.4
6.3
43.3
Comparison


7
1D

95.4
42.5
77.6
1.6
854
17.2
10.5
105.8
Invention


8
1D

94.1
43.6
77.7
1.6
832
18.4
11.4
108.5
Invention


9
1D

94.1
41.3
78.8
1.7
844
19.4
12.3
110.1
Invention


10
1E

90.4
31.9
67.8
1.9
729
24.0
18.0
123.4
Invention


11
1F

91.1
29.7
68.3
1.5
696
25.1
18.9
129.3
Invention


12
1G

91.1
39.3
68.3
2.1
849
21.9
14.1
107.3
Invention


13
1H

96.5
58.6
72.4
2.3
1289
14.7
6.2
80.3
Invention


14
1I

94.8
57.4
71.1
2.3
1189
14.7
6.3
85.7
Invention


15
1J

93.6
45.9
70.2
2.6
949
19.6
11.6
95.9
Invention


16
1K

92.3
57.9
69.2
2.7
1119
15.6
9.7
80.4
Invention


18
1M
None




843
9.2
4.4
67.4
Comparison


19
1N

94.8
36.7
71.1
1.8
801
21.9
13.5
112.4


20
1O

92.4
23.2
69.3
1.7
597
29.3
22.4
150.7
Invention


21
1P

93.9
30.1
70.4
2.0
711
26.0
17.2
128.3
Invention


22
1Q

91.2
31.6
68.4
2.3
724
24.2
17.4
124.3
Invention


23
1R
None




641
26.2
10.5
41.5
Comparison





α: Ferrite,


α′: Martensite,


Af: Area fraction,


TS: Tensile strength,


λ: Hole expanding ratio













TABLE 11







Measurement results










Structure parameter















Af of α′
Grain size





Af of α′
in α grain
of α′ in
Dynamic properties




















Presence
Af of MD
in entire
of entire
entire

Total
Local




Material
Steel
or absence
structure
structure
structure
structure
TS
elongation
elongation
λ


No.
code
of MD
(%)
(%)
(%)
(μm)
(MPa)
(%)
(%)
(%)
Remarks





















24
1R
Partial
72.9



732
18.1
7.1
52.3
Comparison


25
1R

96.1
38.0
78.4
1.5
867
19.4
14.8
102.5
Invention


26
1R

96.7
39.3
77.4
1.7
856
20.5
14.9
112.9
Invention


27
1R

96.4
40.9
78.6
1.4
876
20.2
15.9
108.7
Invention


28
1R

96.3
38.5
80.0
1.4
873
19.2
15.7
112.4
Invention


29
1R

96.0
38.2
78.4
1.5
884
20.9
15.9
115.3
Invention


30
1R

95.4
38.9
80.3
1.6
871
20.8
16.2
105.8
Invention


31
1R
None




1021
9.2
4.7
74.3
Comparison


32
1R
None




1101
8.4
4.1
72.1
Comparison


33
1R
None




1209
8.1
3.6
79.4
Comparison


34
1R
None




1234
7.5
3.8
76.1
Comparison


35
1S
None




611
25.9
10.5
38.5
Comparison


36
1S
Partial
62.8



722
17.3
6.9
45.9
Comparison


37
1S

95.1
37.6
77.6
1.7
856
20.4
15.6
100.5
Invention


38
1S

95.7
38.9
76.7
1.9
844
20.9
14.7
109.2
Invention


39
1S

95.4
40.5
77.8
1.6
860
19.7
16.1
106.5
Invention


40
1S

95.3
38.1
79.2
1.6
861
18.7
15.5
110.9
Invention


41
1S

95.0
37.8
77.6
1.7
863
21.3
15.7
112.3
Invention


42
1S

94.5
38.5
79.5
1.8
859
20.5
16.0
101.6
Invention


43
1S
None




989
9.5
4.5
72.1
Comparison


44
1S
None




1088
82
3.9
70.9
Comparison


45
1S
None




1173
7.9
3.4
76.5
Comparison


46
1S
None




1198
7.2
3.5
75.5
Comparison





α: Ferrite,


α′: Martensite,


Af: Area fraction,


TS: Tensile strength,


λ: Hole expanding ratio













TABLE 12







Measurement results










Structure parameter















Af of α′
Grain size





Af of α′
in α grain
of α′ in
Dynamic properties




















Presence
Af of MD
in entire
of entire
entire

Total
Local




Material
Steel
or absence
structure
structure
structure
structure
TS
elongation
elongation
λ


No.
code
of MD
(%)
(%)
(%)
(μm)
(MPa)
(%)
(%)
(%)
Remarks





















47
1T

92.1
39.6
69.0
2.0
854
21.7
13.5
106.6
Invention


48
1U

95.0
64.8
71.2
2.6
1221
14.3
5.8
87.7
Invention


49
1V

93.4
48.4
70.1
1.9
986
18.9
11.4
92.2
Invention


50
1W

93.6
63.4
70.2
2.3
1201
14.6
6.7
84.9
Invention


51
1X

97.0
62.3
72.7
1.7
1184
14.8
7.5
96.0
Invention


52
1Y

93.3
68.1
70.0
2.6
1271
13.8
6.0
90.8
Invention


53
1Z

90.1
66.3
67.5
2.0
1245
9.1
3.0
72.3
Comparison


54
2A
Partial
72.5



661
26.5
20.9
54.7
Comparison


55
2B

94.5
25.7
70.8
2.4
635
27.6
21.7
141.8
Invention


56
2C

90.9
24.2
68.2
1.9
623
29.5
22.7
146.7
Invention


57
2D

94.1
45.1
75.6
1.7
865
18.7
13.2
100.4
Invention


58
2D

94.3
44.5
78.9
1.8
878
18.6
13.3
108.1
Invention


59
2D

94.5
48.1
77.5
1.8
855
17.9
12.8
107.3
Invention


60
2D
None




954
9.8
4.8
79.8
Comparison


61
2E

91.2
28.4
68.4
1.9
676
25.9
19.7
133.2
Invention


62
2F

92.9
46.2
69.7
1.7
953
19.6
11.7
95.4
Invention


63
2G

91.5
29.0
68.6
1.8
695
26.6
18.6
131.4
Invention


64
2H

95.4
51.9
71.5
1.7
1038
18.0
9.2
87.5
Invention


65
2I

93.3
49.9
70.0
1.9
1009
18.5
9.8
90.1
Invention


66
2J

98.5
53.3
73.9
2.3
1200
14.6
6.2
85.0
Invention


67
2K

94.9
54.0
71.1
2.6
1210
14.5
6.0
84.4
Invention


68
2L

95.4
55.6
71.6
2.1
1100
17.1
6.8
82.6
Invention


69
2M

96.6
58.6
72.4
2.4
1129
15.5
6.3
89.7
Invention





α: Ferrite,


α′: Martensite,


Af: Area fraction,


TS: Tensile strength,


λ: Hole expanding ratio













TABLE 13







Measurement results










Structure parameter















Af of α′
Grain size





Af of α′
in α grain
of α′ in
Dynamic properties




















Presence
Af of MD
in entire
of entire
entire

Total
Local




Material
Steel
or absence
structure
structure
structure
structure
TS
elongation
elongation
λ


No.
code
of MD
(%)
(%)
(%)
(μm)
(MPa)
(%)
(%)
(%)
Remarks





















70
2N

98.4
55.4
73.8
2.0
1242
15.2
4.3
73.1
Comparison


71
2O

96.4
35.1
72.3
1.7
787
9.5
3.5
65.8
Comparison


72
2P

96.9
47.5
72.7
2.0
972
19.2
10.6
93.5
Invention


73
2Q

95.2
56.7
71.4
2.3
1174
14.9
6.3
86.6
Invention


74
2R

94.2
58.5
70.6
2.4
1128
15.5
8.2
89.8
Invention


75
2S

93.8
28.8
70.3
1.7
691
26.7
17.7
132.1
Invention


76
2T

97.3
37.6
73.0
1.8
824
22.5
14.9
110.6
Invention


77
2U

91.8
35.1
68.8
1.7
776
22.5
15.5
116.0
Invention


78
2V

93.6
52.7
70.2
2.0
1050
17.8
9.1
86.6
Invention


79
2W

92.7
45.6
69.5
1.9
933
18.7
12.6
96.4
Invention


80
2X

94.8
66.7
71.1
3.8
1100
7.9
4.5
81.8
Comparison


81
2Y

92.7
37.6
69.6
2.1
824
22.5
14.1
110.6
Invention


82
2Z

93.9
56.1
70.4
2.3
1186
15.9
7.3
86.5
Invention


83
3A

96.8
56.4
72.6
1.9
1106
17.0
7.0
82.2
Invention


84
3B

97.4
55.6
73.0
2.6
1084
16.1
9.6
83.0
Invention


85
3C
Partial
88.7



803
24.8
18.2
72.1
Comparison


86
3D
Partial
41.9



589
29.7
23.7
52.7
Comparison


87
3E

94.0
57.3
70.5
2.1
1120
16.8
8.1
81.1
Invention


88
3F

95.1
44.7
71.3
2.3
920
19.0
10.5
97.8
Invention


89
3G

97.6
41.5
73.2
2.4
873
20.1
13.4
103.1
Invention


90
3H

94.0
57.8
70.5
2.2
1117
15.7
7.6
80.6
Invention


91
3I

91.9
43.7
68.9
1.7
905
19.3
13.5
99.4
Invention


92
3J

92.8
45.1
69.6
2.0
937
19.9
11.4
97.1
Invention





α: Ferrite,


α′: Martensite,


Af: Area fraction,


TS: Tensile strength,


λ: Hole expanding ratio













TABLE 14







Measurement results










Structure parameter















Af of α′
Grain size





Af of α′
in α grain
of α′ in
Dynamic properties




















Presence
Af of MD
in entire
of entire
entire

Total
Local




Material
Steel
or absence
structure
structure
structure
structure
TS
elongation
elongation
λ


No.
code
of MD
(%)
(%)
(%)
(μm)
(MPa)
(%)
(%)
(%)
Remarks





















93
3K

95.0
50.8
71.3
1.8
1022
18.3
9.6
89.0
Invention


94
3L

96.1
47.6
72.1
2.1
963
18.2
9.1
93.4
Invention


95
3M

95.3
52.9
71.5
2.2
1053
17.8
9.2
86.3
Invention


96
3N

93.5
52.3
70.1
1.7
1044
17.9
9.1
87.0
Invention


97
3O

94.4
62.7
70.8
2.7
1191
14.7
8.4
75.6
Comparison


98
3P

98.9
44.6
74.2
1.8
929
20.0
11.6
97.9
Invention


99
3Q

93.4
47.1
70.0
2.3
956
18.3
11.9
94.1
Invention


100
3R

95.7
54.5
71.8
2.0
1077
17.4
9.5
84.4
Invention


101
3S

94.4
44.0
70.8
1.7
910
19.2
11.0
98.9
Invention


102
3T

97.8
27.3
73.4
2.1
659
26.6
20.1
66.6
Comparison


103
3U

95.9
58.2
72.0
2.3
1132
16.6
7.9
80.2
Invention


104
3V

93.3
43.6
70.0
1.9
914
20.4
11.6
99.5
Invention


105
3W

96.7
58.2
72.5
2.6
1273
13.7
5.5
86.7
Invention


106
3X

92.1
31.7
69.1
1.8
735
25.1
16.9
124.2
Invention


107
3Y

96.4
47.3
72.3
1.7
960
18.2
10.9
73.8
Comparison


108
3Z

95.4
55.9
71.6
2.0
1248
15.1
6.3
82.7
Invention


109
4A

93.1
56.7
69.8
2.4
1205
14.5
6.9
84.7
Invention


110
4B

90.9
53.2
68.2
2.2
1049
16.7
10.3
85.8
Invention


111
4C

91.2
27.2
68.4
2.0
658
26.6
20.7
136.9
Invention


112
4D

91.5
44.5
68.6
1.9
928
20.1
12.3
68.1
Comparison


113
4E

92.3
37.4
69.3
1.8
820
22.6
15.6
111.0
Invention


114
4F

95.4
54.6
71.5
2.1
1165
15.0
6.3
83.2
Invention


115
4G

95.0
30.3
71.2
1.9
704
24.9
18.8
127.8
Invention


116
4H

90.3
26.8
67.7
1.7
653
26.8
20.4
137.9
Invention





α: Ferrite,


α′: Martensite,


Af: Area fraction,


TS: Tensile strength,


λ: Hole expanding ratio













TABLE 15







Measurement results










Structure parameter















Af of α′
Grain size





Af of α′
in α grain
of α′ in
Dynamic properties




















Presence
Af of MD
in entire
of entire
entire

Total
Local




Material
Steel
or absence
structure
structure
structure
structure
TS
elongation
elongation
λ


No.
code
of MD
(%)
(%)
(%)
(μm)
(MPa)
(%)
(%)
(%)
Remarks





















117
4I

96.9
58.1
72.7
2.2
1132
16.6
7.4
80.2
Invention


118
4J

95.2
47.0
71.4
2.3
955
18.3
9.7
94.2
Invention


119
4K

91.3
34.2
68.5
2.0
773
23.9
16.7
118.0
Invention


120
4L

91.8
40.0
68.9
1.8
860
21.6
13.5
105.9
Invention


121
4M

98.3
40.6
73.7
1.7
859
20.4
13.1
64.8
Comparison


122
4N

94.8
57.1
71.1
2.0
1207
15.6
7.6
85.2
Invention


123
4O

90.8
39.4
68.1
2.2
851
21.8
14.2
107.0
Invention


124
4P

96.4
33.7
72.3
2.1
765
24.2
17.0
59.2
Comparison


125
4Q

91.7
48.0
68.7
2.1
971
18.0
11.6
92.7
Invention


126
4R

95.4
55.8
71.5
2.3
1097
17.1
9.2
82.8
Invention


127
4S

96.6
56.9
72.5
2.6
1164
16.2
7.1
78.0
Comparison


128
4T

97.3
49.0
73.0
1.7
995
18.8
10.3
91.4
Invention


129
4U

90.1
36.9
67.6
2.1
803
21.8
15.5
112.1
Invention


130
4V

97.7
40.2
73.3
2.0
863
21.5
13.3
105.5
Invention


131
4W

93.5
51.6
70.1
1.8
1034
18.1
9.2
87.9
Invention


132
4X

93.8
39.5
70.4
1.9
852
21.8
13.6
106.8
Invention


133
4Y

92.2
55.4
69.2
2.1
1091
17.2
8.9
83.3
Invention


134
4Z

98.9
51.8
74.1
2.0
1037
18.0
9.6
87.6
Invention


135
5A

90.2
41.7
67.6
2.6
876
20.0
13.6
102.7
Invention


136
5B

94.4
58.8
70.8
2.5
1133
7.5
4.8
79.5
Comparison


137
5C

97.5
58.9
73.2
1.9
1133
15.4
6.1
88.4
Invention


138
5D

92.2
36.2
69.1
2.0
803
23.1
14.8
113.5
Invention


139
5E

93.6
36.4
70.2
1.7
805
23.0
15.1
113.2
Invention


140
5F

93.1
49.0
69.9
2.3
985
17.8
10.3
91.4
Invention





α: Ferrite,


α′: Martensite,


Af: Area fraction,


TS: Tensile strength,


λ: Hole expanding ratio






From the results shown in Tables 10 to 15, it can be considered as follows. The following alphabets all mean steel codes in Tables 1 to 15, and the following Nos. all mean material Nos. in Tables 6 to 15. Nos. 2 to 3, 7 to 16, 19 to 22, 25 to 30, 37 to 42, 47 to 52, 55 to 59, 61 to 69, 72 to 79, 81 to 84, 87 to 96, 98 to 101, 103 to 106, 108 to 111, 113 to 120, 122 to 123, 125 to 126, 128 to 135 and 137 to 140 all are examples that high strength steel sheets having the structure defined in the present invention were produced by the production method defined in the present invention using steel species satisfying the scope of the present invention (1B to 1K, 1N to 1Y, 2B to 2M, 2P to 2W, 2Y to 3B, 3E to 3N, 3P to 3S, 3U to 3X, 3Z to 4C, 4E to 4L, 4N to 4O, 4Q to 4R, 4T to 5A and 5C to 5F in Tables 1 to 5). The high strength steel sheets shown by the above Nos. all have excellent tensile strength, elongation and stretch flangeability.


Contrary to this, the following examples that are not satisfied with any one of the requirements specified in the present invention have the following disadvantages.


No. 1 is an example using steel code 1A having a small C content. Because the proportion of martensite in the whole structure is lower than the range defined, tensile strength was decreased.


Nos. 4 to 6 each use steel code 1D having a component composition which is satisfied with the provision of the present invention. However, the heating and holding temperature of the heat treatment is not A3 point or higher, and the area fraction of α+α′ is less than 90%. Therefore, stretch flangeability was decreased.


No. 18 is an example using steel code 1M having a small Si content. Because it has a bainite structure over the entire surface and MD is not present, elongation is low.


Nos. 23 to 24 each use steel code 1R having a component composition which is satisfied with the provision of the present invention, and Nos. 35 to 36 each use steel code 1S having a component composition which is satisfied with the provision of the present invention. However, the cooling rate of the heat treatment is slower than the range defined, and as a result, ferrite which is not accompanied with martensite in grains was formed. No. 23 and No. 35 each have a ferrite-pearlite structure, and MD is not present. No. 24 and No. 36 each are that ferrite which is not accompanied with martensite in grains is formed and the area fraction of α+α′ is less than 90%. Therefore, stretch flangeability is low.


Nos. 31 to 34 each use steel code 1R having a component composition which is satisfied with the provision of the present invention, and Nos. 43 to 46 each use steel code 1S having a component composition which is satisfied with the provision of the present invention. However, the cooling rate of the heat treatment is slower than the range defined. Therefore, Nos. 31 and 32 and Nos. 43 and 44 are that lath of bainite does not completely disappear, thereby a bainitic ferrite-martensite structure is formed and MD is not present. As a result, elongation and stretch flangeability were decreased. Furthermore, No. 33 and 34 and Nos. 45 and 46 each are that a martensite single phase structure is formed, and elongation and stretch flangeability were decreased. No. 53 is an example using steel code 1Z having a large Si content. Because Si was added in a large amount, elongation and stretch flangeability were decreased.


No. 54 is an example using steel code 2A having a small Mn content.


Because pearlite was formed and α+α′ was less than 90%, stretch flangeability is low. No. 60 uses steel code 2D which is satisfied with the provision of the present invention. However, because the cooling stop temperature exceeds Ms point, a bainite structure was formed on the entire surface, and elongation and stretch flangeability were decreased.


No. 70 is an example using steel code 2N having a large Mn content, and stretch flangeability was decreased.


No. 71 is an example using steel code 2O having a small Al content.


Compounds of Si, Mn and O were unavoidably formed, and elongation and stretch flangeability were decreased.


No. 80 is an example using steel code 2X having a large Al content. Course martensite was formed in a large amount, and the area fraction of α′ in the whole structure and an average gain size of α′ exceeded the defined ranges. As a result, elongation and stretch flangeability was decreased.


No. 85 is an example using steel code 3C having a large Mo content. Because course retained austenite was formed in a large amount and α+α′ was less than 90%, stretch flangeability was decreased.


No. 86 is an example using steel code 3D having a small B content. Because ferrite which is not accompanied with martensite in grains was precipitated and α+α′ was less than 90%, stretch flangeability was decreased.


No. 97 is an example using steel code 3O having a large B content. Stretch flangeability was decreased due to segregation of B.


No. 102 is an example using steel code 3T having a large Ti content. Because precipitate was increased, stretch flangeability was decreased. No. 107 is an example using steel code 3Y having a large Nb content. Because precipitate was increased, stretch flangeability was decreased. No. 112 is an example using steel code 4D having a large V content. Because precipitate was increased, stretch flangeability was decreased. No. 121 is an example using steel code 4M having a large total addition amount of Ti, Nb and V Because precipitate was increased, stretch flangeability was decreased.


No. 124 is an example using steel code 4P having a large Ni content. Because Ni was added in a large amount, it is liable to break and stretch flangeability was decreased.


No. 127 is an example using steel code 4S having a large Cu content. Because Cu was added in a large amount, it is liable to break and stretch flangeability was decreased.


No. 136 is an example using steel code 5B having a large Cr content. Because Cr was added in a large amount, it is liable to break and stretch flangeability was decreased.


Next, examples in the case that the secondary phase is martensite and retained austenite are described below.


Steels A to W having component compositions shown in Table 16 were melted to form slabs. The slabs were heated to 1,200° C., hot rolled to a sheet thickness of 3.0 mm at 800° C. and then taken up at 550° C. The thermo-mechanical treatment (heating temperature T1 (° C.), processing temperature T2 (° C.), rolling reduction P (%), cooling rate R (° C./sec)) shown in FIG. 1 and Table 17 was conducted to cool to room temperature, and thickness reduction processing was conducted so as to be a sheet thickness of 1.2 mm.









TABLE 16







Chemical component of specimen










Steel
Chemical component (mass %)
Ac3



















code
C
Si
Mn
P
S
Al
Mo
B
Other
(° C.)
Remarks





















A
0.05
1.4
1.3
0.01
0.005
0.05
0.3
0.0008
Cr: 0.65, Ti: 0.015
923
Invention


B
0.03
1.3
1.4
0.01
0.005
0.05
0.3
0.0007

927
Invention


C
0.08
1.4
1.4
0.01
0.005
0.03
0.3
0.0007

902
Invention


D
0.25
1.5
1.5
0.01
0.005
0.05
0
0.0009

858
Invention


E
0.35
1.7
2.5
0.01
0.005
0.05
0.3
0.0005

827
Comparison


F
0.12
0.008
1.4
0.01
0.005
0.05
0.3
0.0005

834
Comparison


G
0.10
0.03
1.4
0.01
0.005
1.1
0.3
0.0008

1262
Invention


H
0.05
0.28
0.7
0.01
0.005
0.05
0.3
0.0003

893
Invention


I
0.07
3.6
2.5
0.01
0.005
0.05
0.3
0.0008

979
Comparison


J
0.05
0.4
0.3
0.01
0.005
0.06
0
0.0005

904
Comparison


K
0.09
1.5
3.6
0.01
0.005
0.05
0.3
0.0008

845
Comparison


L
0.05
0.03
2.2
0.01
0.005
0.005
0.3
0.0008

818
Comparison


M
0.05
1.5
1.5
0.01
0.005
0.05
0
0.001

914
Invention


N
0.05
1.4
1.4
0.01
0.005
0.05
0.7
0.0006

934
Invention


O
0.07
1.2
2.2
0.01
0.005
0.05
1.3
0.0008

912
Comparison


P
0.05
1.2
0.9
0.01
0.005
0.05
0.1
0

921
Comparison


Q
0.05
1.5
1.4
0.01
0.005
0.05
0
0.0035

917
Invention


R
0.05
1.5
1.3
0.01
0.005
0.05
0.3
0.007

929
Comparison


S
0.10
1.4
1.3
0.01
0.005
0.05
0.3
0.0008
Ti: 0.015, Nb: 0.012
912
Invention


T
0.05
1.4
1.3
0.01
0.005
0.05
0.3
0.0008
V: 0.0012
926
Invention


U
0.05
1.4
1.3
0.01
0.005
0.05
0.3
0.0008
Ni: 0.1, Cu: 0.1
921
Invention


V
0.07
1.2
1.2
0.01
0.005
0.05
0.3
0.0008
Ca: 0.002, REM: 0.002
910
Invention


W
0.01
0.5
1.2
0.01
0.005
0.05
0.3
0.0008

913
Comparison


X
0.01
0.3
1.8
0.01
0.005
0.05
0.3
0.0007

886
Comparison
















TABLE 17







Heat treatment condition










Heat treatment condition
















Heating
Heating

Cooling





temperature
temperature
Rolling
temperature


Material
Steel
T1
T2
reduction P
R


No.
code
(° C.)
(° C.)
(%)
(° C.)
Remarks
















141
A
1200
900
30
10
Invention


142
B
1200
900
30
10
Invention


143
C
1250
800
30
10
Invention


144
D
1200
800
20
5
Invention


145
E
1200
950
10
18
Comparison


146
F
1200
750
40
7
Comparison


147
G
1300
700
50
10
Invention


148
H
1250
800
30
10
Invention


149
I
1200
800
30
15
Comparison


150
J
1250
700
40
0.5
Comparison


151
K
1200
900
20
15
Comparison


152
L
1200
900
30
10
Comparison


153
M
1250
800
30
10
Invention


154
N
1200
650
30
0.5
Invention


155
O
1200
900
10
15
Comparison


156
P
1200
700
30
0.5
Comparison


157
Q
1200
750
30
0.5
Invention


158
R
1200
900
10
15
Comparison


159
S
1300
700
30
10
Invention


160
T
1300
700
40
10
Invention


161
U
1200
800
30
10
Invention


162
V
1200
700
30
10
Invention


163
W
1200
700
30
0.5
Comparison


164
C
1200
550
30
1
Comparison


165
C
1300
1050
10
0.5
Comparison


166
C
1200
900
2
15
Comparison


167
C
1200
900
10
0.1
Comparison


168
C
1200
900
10
25
Comparison


169
X
1250
900
50
0.5
Comparison









Microstructure observation was conducted on each steel sheet obtained above in the following procedures, and dynamic properties were evaluated by a tensile test and a hole expanding test.


Microstructure of each steel sheet was identified by the following method.


Each steel sheet was cut into a test piece for microstructure observation of 10 mm×10 mm×1.2 mm. The test piece was embedded in a cold rolled resin, and a position of ¼ of a sheet thickness in a rolled direction was observed. In such a case, impression as a landmark was formed with a Vickers tester so as to conduct identification on the structure observation place. The impression was corroded with repeller, and the structure was observed at five positions using an optical microscope with a magnification of 1,000. When the structure photograph after repeller corrosion was image analyzed, ferrite was observed gray, and martensite and retained austenite were observed white. After microstructure observation with an optical microscope, buff polishing and electrolysis polishing were conducted to an extent such that the Vickers impression does not disappear, and structure observation was conducted on the place at a step distance of 100 nm using FE/SEM-EBSP. A boundary having an orientation difference of 15° or more of grains was considered as grain boundary, and thus the grain boundary was identified.


Optical microphotograph and FE/SEM-EBSP structure photograph were combined as the standard of Vickers impression, and the structure was evaluated.


MD Structure:


The MD structure contains fine martensite or retained austenite (secondary phase) in ferrite grains as a matrix, as described above. The observation results of optical microscope and FE/SEM-EBSP were combined, a structure in which many martensite or retained austenite are present in the inside of grains surrounded by large tilt grain boundary (i.e., in the grains) was identified as MD structure, and its space factor was obtained.


There is the possibility that pearlite, bainite, ferrite which is not accompanied with martensite or retained austenite in grains, and the like are contained as other structures. Identification method of those structures is as follow.


Pearlite:


Pearlite has a lamella structure of ferrite and cementite, and the cementite can be identified with FE/SEM-EBSP. In the Examples, the space factor of pearlite in the observation view was determined.


Bainite:


Bainite is that lath is present in ferrite grains identified with FE/SEM-EBSP. Structure in which lath is present in ferrite grains was judged as bainite, and space factor of bainite in the observation view was determined.


Ferrite which is not Accompanied with Martensite or Retained Austenite in Grains:


Structure in which martensite or retained austenite cannot be confirmed in ferrite grains identified with FE/SEM-EBSP is considered as ferrite which is not accompanied with martensite or retained austenite in grains, and is judged as a structure different from MD structure. Space factor of ferrite which is not accompanied with martensite or retained austenite in grains in the observation view was determined.


Structure in which MD structure is not observed in the observation view is judged that MD is not present. When the whole structure is defined as 100%, in the case that the total of space factors of other structures (pearlite, bainite, ferrite which is not accompanied with martensite or retained austenite in grains, and the like) exceeds 10%, the defined structure is not formed. In this case, it was judged that MD is partial.


Proportion that secondary phase in the entire phase occupies in the whole structure:


Average Grain Size of Ferrite in the Entire Phase:


Proportion of Secondary Phase Present in Ferrite Grains in MD Structure:


First, the space factor of the secondary phase (martensite and retained austenite) in the whole structure used a space factor of white portion in the whole structure by image analyzing an optical microphotograph. Next, an average grain size (diameter of a corresponding circle) of ferrite was obtained using an image of FE/SEM-EBSP, and by combining with the optical microphotograph, the secondary phase present in the MD structure was separated into the secondary phase present in ferrite grains and the secondary phase present at grain boundary, thereby the space factor of the secondary phase present in grains of the whole secondary phase present in the MD structure was obtained.


Proportion that Retained Austenite in the Whole Structure Occupies in the Whole Structure:


On the other hand, martensite and retained austenite can be distinguished by identifying retained austenite having an FCC structure with FE/SEM-EBSP. However, retained austenite is an important structure in the present invention, and quantitative measurement of the space factor is indispensable to effectively exhibit the effect of the present invention. For this reason, a method of measuring a space factor of retained austenite by analyzing an image of FE/SEM-EBSP is considered, but in the Examples, the space factor of retained austenite was calculated by a saturated magnetization method which can obtain a measurement value of further high accuracy. It is considered that the value measured by the saturated magnetization method is a volume fraction, but the volume fraction can be regarded as being equivalent with an area fraction.


Average Grain Size and Number of Secondary Phase in the Whole Structure:


On the other hand, the average grain size (average particle size of secondary phase particles) and the number of the secondary phase (martensite and retained austenite) were obtained by the following methods. Regarding the average grain size, five places of observation view of 20 μm×20 μm are randomly extracted from SEM observation photograph (magnification; 3,000), average grain sizes (diameters of corresponding circles) of martensite and retained austenite in the respective observation views are obtained, and the average value thereof was used as an average grain size of martensite and retained austenite in the whole structure. Regarding the number, five places of observation view of 50 μm×50 μm are randomly extracted from the above optical microphotograph, and the numbers of the secondary phase particles observed thereon were averaged.


Various dynamic properties of steel were obtained by the following methods.


Tensile Properties:


Using JIS No. 5 test piece obtained from a vertical direction of a steel sheet rolled direction, tensile strength (TS), uniform elongation (u-EL), local elongation (1-EL) and total elongation (t-EL=u-EL+1-EL) were measured according to JIS Z 2241. Test pieces having TS of 590 MPa or more and t-EL of 10% or more were considered as acceptable products. Strain amount of from the maximum load point to breakage was considered as local elongation.


Stretch Flangeability:


Hole expanding ratio λ was measured as stretch flangeability. The hole expanding ratio λ was measured according to JISF (The Japan Iron and Steel Federation) standard (JFST 1001-1996). Steels having λ of 80% or more were considered as acceptable products.


The results obtained are shown in Tables 18 and 19 below.









TABLE 18





Measurement results

















Structure parameter





















Af of











second

Average







structure
Average
grain






Af of
in
grain
size of
Number






second
α grain
size of
secondary
of
Vf of γ




Presence
Af of
structure
in
α in
phase
secondary
in




or
MD
in entire
MD
entire
in entire
phase
entire


Test
Steel
absence
structure
structure
structure
structure
structure
in entire
structure


No.
code
of MD
(%)
(%)
(%)
(μm)
(μm)
structure
(%)





141
A

96.6
28.5
78.4
11.3
0.4
153
0.5


142
B

95.8
26.1
78.7
11.7
0.6
144
0.3


143
C

96.9
25.8
74.5
9.6
0.3
168
0.8


144
D

95.3
29.4
74.0
9.2
1.4
104
8.8


145
E
None









146
F
None









147
G

97.1
27.3
71.9
6.8
0.7
139
7.3


148
H

96.5
25.4
74.9
9.5
0.5
161
1.0


149
I
None









150
J
Partial
68.7
17.3
73.4
13.5
0.7
121
1.7


151
K
Partial
83.1
31.7
72.5
12.3
3.2
134
0.7


152
L
Partial
86.5
22.7
70.2
11.6
0.6
140
0.0


153
M

95.6
24.9
75.5
9.9
0.4
166
0.8


154
N

94.2
26.4
72.9
7.8
0.4
159
1.0


155
O
Partial
65.8
62.8
76.2
11.2
4.1
73
0.8













Dynamic properties


















Total
Uniform
Local





Test
TS
elongation
elongation
elongation
λ



No.
(MPa)
(%)
(%)
(%)
(%)
Remarks







141
870
25.8
9.2
16.6
101.7
Invention



142
618
29.5
12.1
17.4
103.4
Invention



143
784
27.7
13.9
13.8
93.9
Invention



144
1205
22.8
9.9
12.9
95.1
Invention



145
1298
4.9
1.8
3.1
19.3
Comparison



146
992
9.6
7.4
2.2
45.2
Comparison



147
892
27.4
15.8
11.6
88.6
Invention



148
811
26.9
12.7
14.2
96.2
Invention



149
1318
3.1
1.0
2.1
17.5
Comparison



150
433
30.4
21.9
8.5
67.5
Comparison



151
1179
8.4
3.4
5.0
31.3
Comparison



152
682
9.5
7.7
1.8
32.7
Comparison



153
844
26.2
13.2
13.0
94.2
Invention



154
852
24.9
12.8
12.1
93.4
Invention



155
1158
8.5
4.2
4.3
30.6
Comparison







α: Ferrite,



γ: Retained austenite,



Af: Area fraction,



Vf: Volume fraction,



TS: Tensile strength,



λ: Hole expanding ratio













TABLE 19





Measurement results

















Structure parameter





















Af of











second

Average







structure
Average
grain






Af of
in
grain
size of
Number






second
α grain
size of
secondary
of
Vf of γ




Presence
Af of
structure
in
α in
phase
secondary
in




or
MD
in entire
MD
entire
in entire
phase
entire


Test
Steel
absence
structure
structure
structure
structure
structure
in entire
structure


No.
code
of MD
(%)
(%)
(%)
(μm)
(μm)
structure
(%)





156
P
Partial
63.2
16.4
72.5
13.8
0.7
131
1.7


157
Q

95.5
25.9
76.3
10.1
0.7
149
0.9


158
R
Partial
88.7
24.1
75.2
10.9
0.7
141
0.9


159
S

95.6
28.3
70.4
5.4
0.3
172
4.2


160
T

95.2
27.8
71.0
5.9
0.4
169
4.1


161
U

93.8
25.9
73.9
9.5
0.5
158
5.8


162
V

96.7
25.7
75.4
8.6
0.6
146
5.1


163
W
Partial
87.4
22.8
71.6
11.9
0.6
138
1.5


164
C
Partial
56.7
11.6
72.4
17.5
0.8
99
0.8


165
C

94.9
27.5
78.3
22.4
1.1
118
0.8


166
C
Partial
71.1
57.3
72.7
15.8
3.6
103
1.1


167
C
Partial
60.4
16.5
70.1
17.2
0.7
74
0.9


168
C
None









169
X

92.4
9.2
45.8
8.5
0.6
82
0.0













Dynamic properties


















Total
Uniform
Local





Test
TS
elongation
elongation
elongation
λ



No.
(MPa)
(%)
(%)
(%)
(%)
Remarks







156
519
27.7
18.5
9.2
64.7
Comparison



157
993
23.4
12.8
10.6
92.8
Invention



158
850
18.6
15.0
3.6
36.2
Comparison



159
987
28.6
18.4
10.2
99.3
Invention



160
963
28.5
18.3
10.2
100.1
Invention



161
940
25.4
15.8
9.6
89.9
Invention



162
699
29.3
18.5
10.8
97.5
Invention



163
512
27.0
16.7
10.3
89.5
Comparison



164
719
24.8
15.9
8.9
78.9
Comparison



165
767
23.9
14.8
9.1
76.3
Comparison



166
1087
10.4
8.4
2.0
33.8
Comparison



167
630
26.9
18.8
8.1
77.3
Comparison



168
1302
3.2
0.9
2.3
21.9
Comparison



169
487
32.2
18.6
13.6
93.2
Comparison







α: Ferrite,



γ: Retained austenite,



Af: Area fraction,



Vf: Volume fraction,



TS: Tensile strength,



λ: Hole expanding ratio






Test Nos. 141, 142, 143, 144, 147, 148, 153, 154, 157, 159, 160, 161 and 162 each were satisfied with the provision of the present invention in structure morphology, and showed good properties in all of tensile strength TS, total elongation t-EL and hole expanding ratio λ. Average grain sizes of the secondary phases are all in a range of 3 μm or less.


On the other hand, No. 145 used steel E having C content larger than the range defined in the present application. As a result, nearly the entire surface was converted into martensite structure, and total elongation and λ were deficient.


No. 146 used steel F having Si content smaller than the range defined in the present application. As a result, the structure of bainite+martensite was formed, and total elongation and λ were deficient.


No. 149 used steel I having Si content larger than the range defined in the present application. As a result, nearly the entire surface was converted into martensite structure, and total elongation and λ were deficient.


No. 150 used steel J having Mn content smaller than the range defined in the present application. As a result, hardenability was poor, and ferrite was precipitated. As a result, TS and λ were deficient.


No. 151 used steel K having Mn content larger than the range defined in the present application. As a result, the structure of MD+martensite was formed, and total elongation and λ were deficient.


No. 152 used steel L having Al content smaller than the range defined in the present application. As a result, compounds of Si, Mn and O were unavoidably formed, and total elongation and λ were deficient.


No. 155 used steel O having Mo content larger than the range defined in the present application. As a result, the structure of MD+martensite was formed, and total elongation and λ were deficient.


No. 156 used steel P having B content smaller than the range defined in the present application. As a result, ferrite was precipitated, and TS and λ were deficient.


No. 158 used steel R having B content larger than the range defined in the present application. As a result, deterioration of λ which was considered due to grain segregation was generated.


No. 163 used steel W having C content smaller than the c range defined in the present application. As a result, ferrite was precipitated, and TS was deficient.


No. 164 was that the processing temperature T2 is lower than the range defined in the present application. As a result, ferrite was precipitated, and λ was decreased.


No. 165 was that the processing temperature T2 is higher than the range defined in the present application. As a result, the average grain size of the matrix ferrite is larger than the prescribed range, and λ was decreased.


No. 166 was that rolling reduction is lower than the range defined in the present application. As a result, bainite transformation is not accelerated, thereby forming the structure of MD+martensite. As a result, λ was decreased.


No. 167 was that the cooling rate was lower than the range defined in the present application. As a result, ferrite was precipitated, and λ was decreased.


No. 168 was that the cooling rate is higher than the range defined in the present application. As a result, martensite structure was formed, and total elongation and λ were decreased.


No. 169 used steel X having C content smaller than the range defined in the present application. As a result, the proportion of the secondary phase in the whole structure was reduced, and TS was decreased.


While the present invention has been described in detail and with reference to specific embodiments thereof, it will be apparent to one skilled in the art that various changes and modifications can be made therein without departing from the scope thereof.


This application is based on Japanese Patent Application No. 2006-283517 filed Oct. 18, 2006 and Japanese Patent Application No. 2006-283579 filed Oct. 18, 2006, the entire contents thereof being hereby incorporated by reference.


Further, all references cited herein are incorporated in their entireties.

Claims
  • 1. A high strength steel sheet having a structure which is mainly composed of MD structure (Micro Duplex structure) comprising a ferrite matrix, and as a secondary phase, martensite or martensite and retained austenite, finely dispersed in said matrix, wherein the proportion that the MD structure occupies in the whole structure is 90% or more,wherein the proportion that the secondary phase present in the whole structure occupies in the whole structure is from 10 to 60%,wherein the secondary phase in the MD structure is present in ferrite grains and at grain boundary, in which the proportion of the secondary phase present in the ferrite grains is 50% or more, andwherein the average grain size of the secondary phase in the whole structure is 3 μm or less.
  • 2. The high strength steel sheet as claimed in claim 1, wherein the secondary phase is constituted of martensite.
  • 3. The high strength steel sheet as claimed in claim 1, wherein the secondary phase is constituted of martensite and retained austenite.
  • 4. The high strength steel sheet as claimed in claim 2, wherein an average grain size of ferrite in the whole structure is 20 μm or less, and wherein 20 or more secondary phases on the average are present in an observation view of 50 μm×50 μm in the whole structure.
  • 5. The high strength steel sheet as claimed in claim 3, wherein an average grain size of ferrite in the whole structure is 20 μm or less, and wherein 20 or more secondary phases on the average are present in an observation view of 50 μm×50 μm in the whole structure.
  • 6. The high strength steel sheet as claimed in claim 5, wherein the proportion that the retained austenite present in the whole structure occupies in the whole structure is 2% or more.
  • 7. The high strength steel sheet as claimed in claim 2, comprising, in terms of % by mass, C: 0.02 to 0.3%;Si: 0.01 to 3%;Mn: 0.5 to 3%;B: 0.0001 to 0.005%; andAl: 0.01 to 1.5%,with the remainder being Fe and inevitable impurities.
  • 8. The high strength steel sheet as claimed in claim 3, comprising, in terms of % by mass, C: 0.02 to 0.3%;Si: 0.01 to 3%;Mn: 0.5 to 3%;B: 0.0001 to 0.005%; andAl: 0.01 to 1.5%,with the remainder being Fe and inevitable impurities.
  • 9. The high strength steel sheet as claimed in claim 7, further comprising Mo: 0.03 to 1%.
  • 10. The high strength steel sheet as claimed in claim 8, further comprising Mo: 0.03 to 1%.
  • 11. The high strength steel sheet as claimed in claim 7, further comprising at least one element selected from the group consisting of Nb, Ti and V in the total amount of from 0.01 to 0.1%.
  • 12. The high strength steel sheet as claimed in claim 8, further comprising at least one element selected from the group consisting of Nb, Ti and V in the total amount of from 0.01 to 0.1%.
  • 13. The high strength steel sheet as claimed in claim 7, further comprising at least one of Ni: 0.5% or less, andCu: 0.5% or less.
  • 14. The high strength steel sheet as claimed in claim 8, further comprising at least one of Ni: 0.5% or less, andCu: 0.5% or less.
  • 15. The high strength steel sheet as claimed in claim 7, further comprising Cr: 1.5% or less.
  • 16. The high strength steel sheet as claimed in claim 8, further comprising Cr: 1.5% or less.
  • 17. The high strength steel sheet as claimed in claim 7, further comprising at least one of Ca: 0.003% or less, andREM: 0.003% or less.
  • 18. The high strength steel sheet as claimed in claim 8, further comprising at least one of Ca: 0.003% or less, andREM: 0.003% or less.
  • 19. A method for producing a high strength steel sheet, which comprises: heating a steel sheet material comprising, in terms of % by mass,C: 0.02 to 0.3%,Si: 0.01 to 3%,Mn: 0.5 to 3%,B: 0.0001 to 0.005%, andAl: 0.01 to 1.5%,with the remainder being Fe and inevitable impurities; andcooling the steel sheet material from a temperature of A3 point or higher to a temperature of Ms point or lower in a cooling rate of from 0.2 to 20° C./sec.
  • 20. A method for producing a high strength steel sheet, which comprises: cooling, from a temperature of A3 point or higher, a steel sheet material comprising, in terms of % by mass,C: 0.02 to 0.3%,Si: 0.01 to 3%,Mn: 0.5 to 3%,B: 0.0001 to 0.005%, andAl: 0.01 to 1.5%,with the remainder being Fe and inevitable impurities;subjecting said material to a processing of rolling reduction of 5% or more in a temperature range of from 600 to 1,000° C.; and thencooling said material to a temperature of Ms point or lower in a cooling rate of from 0.2 to 20° C./sec.
Priority Claims (2)
Number Date Country Kind
2006-283517 Oct 2006 JP national
2006-283579 Oct 2006 JP national