Method for manufacturing high strength galvanized steel sheet having excellent stability of mechanical properties, formability, and coating appearance

Information

  • Patent Grant
  • 9340859
  • Patent Number
    9,340,859
  • Date Filed
    Friday, June 1, 2012
    12 years ago
  • Date Issued
    Tuesday, May 17, 2016
    8 years ago
Abstract
A method of manufacturing a high strength galvanized steel sheet has a first heating step including heating to 400° C. to 750° C. in an atmosphere containing O2: 0.1 to 20 percent and H2O: 1 to 50 percent and heating to 600° C. to 850° C. in an atmosphere containing O2: 0.01 to less than 0.1 percent and H2O: 1 to 20 percent is applied to a steel sheet, a second heating step includes holding the steel sheet in an atmosphere containing H2: 1 to 50 percent and having a dew point of 0° C. or lower at 750° C. to 900° C. for 15 to 600 s, cooling to a temperature of 450° C. to 550° C., and holding is performed at that temperature for 10 to 200 s, and a galvanization treatment is applied.
Description
TECHNICAL FIELD

This disclosure relates to a method of manufacturing a high strength galvanized steel sheet suitable for a member used in the industrial fields of automobiles, electric appliances and the like and which has excellent stability of mechanical properties, formability, and, in addition, coating appearance.


BACKGROUND

In recent years, enhancement of fuel economy of the automobile has become an important issue from the viewpoint of global environmental conservation. Consequently, there is an active movement afoot to reduce the thickness through increases in strength of car body materials to reduce the weight of a car body itself.


However, an increase in strength of a steel sheet causes reduction in ductility, that is, reduction in formability. Therefore, development of materials having high strength and high formability in combination has been desired.


Furthermore, in forming of the high strength steel sheet into a complicated shape, e.g., an automobile component, occurrences of cracking and necking in a punch stretch portion or a stretch flange portion cause serious issues. Therefore, a high strength steel sheet which can overcome the issues on occurrences of cracking and necking and which has high ductility and high hole expansion property in combination has also been required.


Moreover, shape fixability is degraded by an increase in strength and thickness reduction of a steel sheet significantly. To cope with this, in press forming, it has been widely performed that changes in shape after release from a mold is predicted and the mold is designed in expectation of the amount of change in shape. However, if the tensile strength (TS) of a steel sheet is changed, deviation from the expected amount, in which the tensile strength is assumed to be constant, becomes large and odd shapes occur. Consequently, reworking, e.g., sheet-metal working of the shape on a one-by-one basis, becomes necessary after press-forming, and efficiency in mass production is degraded significantly. Therefore, it is required that variations in TS of the steel sheet are minimized.


As for an improvement of formability of the high strength steel sheet, heretofore, various multi phase high strength galvanized steel sheets, e.g., a ferrite-martensite dual-phase steel and a TRIP steel taking advantage of the transformation induced plasticity of retained austenite, have been developed.


For example, Japanese Unexamined Patent Application Publication No. 2001-140022 discloses a method of manufacturing a galvanized steel sheet having excellent ductility by specifying the chemical composition to be within a specific range and, in addition, specifying the volume ratios of retained austenite and martensite and the manufacturing conditions. Meanwhile, Japanese Unexamined Patent Application Publication No. 04-026744 discloses a galvanized steel sheet having excellent ductility by specifying the chemical composition to be within a specific range and, in addition, specifying the specific manufacturing condition. Japanese Unexamined Patent Application Publication No. 2007-182625 discloses a galvannealed steel sheet having excellent ductility by specifying the chemical composition to be within a specific range and, in addition, specifying the volume ratios of ferrite, bainitic ferrite, and retained austenite within specific ranges. Meanwhile, Japanese Unexamined Patent Application Publication No. 2000-212684 discloses a method of manufacturing a high strength cold rolled steel sheet which contains ferrite, bainite, and 3% or more of retained austenite and in which variations in elongation in the sheet width direction have been reduced.


However, in JP '022, JP '744 and JP '625, an improvement in ductility of the high strength thin steel sheet is the main purpose. Therefore, the hole expansion property is not taken into consideration. Also, in JP '684, only variations in the total elongation EL in the sheet width direction are described, and variations in mechanical properties due to the component composition and the production condition are not taken into consideration. As described above, in every technology, a high strength galvanized steel sheet having high ductility and high hole expansion property in combination and, in addition, having excellent stability of mechanical properties has not been obtained.


It could therefore be helpful to provide a method of manufacturing a high strength galvanized steel sheet having a tensile strength TS of 540 MPa or more and having excellent stability of mechanical properties and formability (high ductility and high hole expansion property) and, in addition, excellent coating appearance.


SUMMARY

We thus provide:

    • (1) A method for manufacturing a high strength galvanized steel sheet having excellent stability of mechanical properties, formability, and coating appearance, characterized by including the steps of applying a first heating step to the steel sheet containing C: 0.04% or more and 0.13% or less, Si: 0.7% or more and 2.3% or less, Mn: 0.8% or more and 2.0% or less, P: 0.1% or less, S: 0.01% or less, Al: 0.1% or less, N: 0.008% or less, and the remainder composed of Fe and incidental impurities, on a percent by mass basis, in which, in the former part, heating is performed in an atmosphere containing O2: 0.1 to 20 percent by volume and H2O: 1 to 50 percent by volume such that the temperature thereof becomes within the range of 400° C. to 750° C. and, in the latter part, heating of the steel sheet is performed in an atmosphere containing O2: 0.01 to less than 0.1 percent by volume and H2O: 1 to 20 percent by volume such that the temperature of the steel sheet becomes within the range of 600° C. to 850° C., applying a second heating step to the resultant steel sheet, in which holding of the steel sheet is performed in an atmosphere containing H2: 1 to 50 percent by volume and having a dew point of 0° C. or lower in a temperature range of 750° C. to 900° C. for 15 to 600 s, cooling to a temperature range of 450° C. to 550° C. is performed, and holding is performed in the temperature range of 450° C. to 550° C. for 10 to 200 s, and applying a galvanization treatment, wherein an obtained galvanized steel sheet includes 75% or more of ferrite phase, 1.0% or more of bainitic ferrite phase, and 1.0% or more and 10.0% or less of pearlite phase, on an area ratio basis, the area ratio of martensite phase is 1.0% or more and less than 5.0%, and the area ratio of martensite phase/(area ratio of bainitic ferrite phase+area ratio of pearlite phase) 0.6 is satisfied.
    • (2) The method for manufacturing a high strength galvanized steel sheet having excellent stability of mechanical properties, formability, and coating appearance, according to the above-described item (1), characterized in that the above-described steel sheet further contains at least one type of element selected from Cr: 1.0% or less, V: 0.5% or less, Mo: 0.5% or less, Ni: 1.0% or less, and Cu: 1.0% or less on a percent by mass basis.
    • (3) The method for manufacturing a high strength galvanized steel sheet having excellent stability of mechanical properties, formability, and coating appearance, according to the above-described item (1) or item (2), characterized in that the above-described steel sheet further contains at least one type of element selected from Ti: 0.1% or less, Nb: 0.1% or less, and B: 0.0050% or less on a percent by mass basis.
    • (4) The method for manufacturing a high strength galvanized steel sheet having excellent stability of mechanical properties, formability, and coating appearance, according to any one of the above-described items (1) to (3), characterized in that the above-described steel sheet further contains at least one type of element selected from Ca: 0.005% or less and REM: 0.005% or less on a percent by mass basis.
    • (5) The method for manufacturing a high strength galvanized steel sheet having excellent stability of mechanical properties, formability, and coating appearance, according to any one of the above-described items (1) to (4), characterized in that the former part of the above-described first heating step is performed with a direct fired furnace or a non-oxidizing furnace under the condition of the air ratio of 1 or more and 1.3 or less and the latter part of the above-described first heating step is performed with a direct fired furnace or a non-oxidizing furnace under the condition of the air ratio of 0.6 or more and less than 1.
    • (6) The method for manufacturing a high strength galvanized steel sheet having excellent stability of mechanical properties, formability, and coating appearance, according to any one of the above-described items (1) to (5), characterized in that, after the above-described galvanization treatment is applied, an alloying treatment of zinc coating is performed at a temperature of 500° C. to 600° C. under the condition satisfying the following formula:

      0.45≦exp[200/(400−T)]×ln(t)≦1.0
    • where
      • T: average holding temperature (° C.) at a temperature of 500° C. to 600° C.,
      • t: holding time (s) at a temperature of 500° C. to 600° C., and
      • exp(X) and ln(X) represent an exponential function and natural logarithm, respectively, of X.


In this regard, every % indicating a component of a steel is on a percent by mass basis. Furthermore, “high strength galvanized steel sheet” refers to a galvanized steel sheet having a tensile strength TS of 540 MPa or more.


Moreover, regardless of whether an alloying treatment is performed or not, steel sheets in which a zinc coating is applied to a steel sheet by galvanization are generically called galvanized steel sheets. That is, the galvanized steel sheets include both galvanized steel sheets not subjected to an alloying treatment and galvannealed steel sheets subjected to an alloying treatment.


A high strength galvanized steel sheet, which has a tensile strength TS of 540 MPa or more, which has excellent formability and stability of mechanical properties because of high ductility and high hole expansion property and, furthermore, which has excellent coating appearance, is obtained. In the case where the high strength galvanized steel sheet is applied to, for example, an automobile structural member, enhancement of fuel economy due to weight reduction of a car body can be facilitated. Therefore, an industrial utility value is very large.





BRIEF DESCRIPTION OF THE DRAWINGS


FIG. 1 is a diagram showing the relationship between the annealing temperature (T1) and TS.



FIG. 2 is a diagram showing the relationship between the annealing temperature (T1) and EL.



FIG. 3 is a diagram showing the relationship between the cooling average holding temperature (T2) and TS.



FIG. 4 is a diagram showing the relationship between the cooling average holding temperature (T2) and EL.





DETAILED DESCRIPTION

We found the following:

    • By specifying the Si content to be more than or equal to a predetermined amount by virtue of intentional addition of Si, an improvement of ductility due to an improvement of a work hardening property of ferrite, ensuring of strength due to solution hardening of ferrite, and an improvement of hole expansion property due to relaxation of hardness difference from a secondary phase become possible.
    • By making the most of bainitic ferrite and pearlite, the hardness difference between mild ferrite and hard martensite can be relaxed and the hole expansion property can be improved.
    • If much hard martensite is present in a final microstructure, a large hardness difference occurs at an interface between the mild ferrite phase and a different phase, so that the hole expansion property is degraded. Therefore, untransformed austenite, which is transformed to martensite finally, is converted to pearlite and, thereby, a microstructure including ferrite, bainitic ferrite, pearlite, a small amount of martensite is formed, so that the hole expansion property can be improved while high ductility is maintained. In addition, the area ratio of each of the above-described phases is controlled appropriately and, thereby, the stability of mechanical properties can be ensured.


Meanwhile, it has been known that the coating appearance is degraded if Si is contained. Usually, as for a galvanized steel sheet, a heat treatment is performed in a reducing atmosphere and, thereafter, a galvanization treatment is performed. Si added to the steel is an easy-to-be-oxidized element and, therefore, is selectively oxidized even in the commonly used reducing atmosphere to form Si oxide on the surface of the steel sheet. The resulting oxide reduces the wettability with molten zinc during a coating treatment and cause bare spots. Therefore, the wettability is reduced along with an increase in the Si concentration in the steel and bare spots occurs frequently.


To cope with such problems, the wettability with the molten zinc can be improved by heating the steel sheet in advance in an oxidizing atmosphere to form iron oxide on the surface and, thereafter, performing reduction annealing. On the other hand, iron oxide peeled from the steel sheet surface at the initial stage of the reduction annealing may adhere to a roll and cause a scale mark on the steel sheet surface. As a result of our efforts to find a solution to such an issue linked to peeling of iron oxide from the steel sheet surface, we found that the peeling of iron oxide was suppressed by heating the steel sheet in a slightly oxidizing atmosphere after iron oxide was formed to reduce the outermost surface of iron oxide.


Our methods and steel sheets will now be described below in detail.


(1) Initially, the component composition will be described.


(a) C: 0.04% or More and 0.13% or Less


Carbon is an austenite forming element and is an element indispensable for strengthening a steel. It is difficult to ensure predetermined strength if the C content is less than 0.04%. On the other hand, if the C content is more than 0.13%, a welded zone and a heat-affected zone are hardened significantly, and the mechanical characteristics of the welded zone are degraded, so that the spot weldability, the arc weldability, and the like are degraded. Therefore, the C content is 0.04% or more and 0.13% or less.


(b) Si: 0.7% or More and 2.3% or Less


Silicon is a ferrite forming element and is also an element effective in solution hardening. It is necessary that 0.7% or more of Si be contained to ensure good ductility due to an improvement in work hardening property of the ferrite phase. Furthermore, it is also necessary that 0.7% or more be contained to ensure a predetermined area ratio of bainitic ferrite phase and ensure good hole expansion property. However, if Si is excessively contained, degradation of surface quality due to an occurrence of red scale and the like and degradation of deposition and adhesion of the coating are caused. Therefore, the Si content is 0.7% or more and 2.3% or less, and preferably 1.2% or more and 1.8% or less.


(c) Mn: 0.8% or More and 2.0% or Less


Manganese is an element effective in strengthening a steel. Furthermore, Mn is an element to stabilize austenite and an element necessary to adjust the ratio of a secondary phase. For this purpose, it is necessary that 0.8% or more of Mn be contained. On the other hand, if the content is excessive and is more than 2.0%, the area ratio of martensite phase in the secondary phase increases and it becomes difficult to ensure the stability of mechanical properties. Moreover, an increase in cost is brought about because an alloy cost of Mn has increased in recent years. Therefore, the Mn content is 0.8% or more and 2.0% or less, and preferably 1.0% or more and 1.8% or less.


(d) P: 0.1% or Less


Phosphorus is an element effective in strengthening a steel. However, if the content is excessive and is more than 0.1%, embrittlement is caused by grain boundary segregation, and the impact resistance is degraded. Furthermore, if the content is more than 0.1%, an alloying rate is reduced significantly. Therefore, the P content is 0.1% or less.


(e) S: 0.01% or Less


Sulfur forms inclusions, e.g., MnS, to cause degradation in impact resistance and cracking along a metal flow of a welded zone. Therefore, the content thereof is minimized, although the S content is 0.01% or less from the viewpoint of production cost.


(f) al: 0.1% or Less


Coarse Al2O3 is generated and the quality of steel sheets is degraded if the Al content is more than 0.1%. Therefore, the Al content is 0.1% or less. Meanwhile, in the case where Al is added for deoxidation of a steel, it is preferable that the content is 0.01% or more because, if the content thereof is less than 0.01%, a large number of coarse oxides of Mn, Si, and the like are dispersed in the steel to degrade the quality. Therefore, the preferable range of the Al content is 0.01% to 0.1%.


(g) N: 0.008% or Less


Nitrogen is an element which degrades the aging resistance of a steel to a greatest extent and preferably is minimized. Degradation of the aging resistance becomes significant if the content thereof is more than 0.008%. Therefore, the N content is 0.008% or less.


The remainder is composed of Fe and incidental impurities. However, besides these elements, at least one type selected from the following elements can be added, as necessary.


(h) at Least One Type Selected from Cr: 1.0% or Less, V: 0.5% or Less, Mo: 0.5% or Less, Ni: 1.0% or Less, and Cu: 1.0% or Less


Chromium, vanadium, and molybdenum have a function of improving the balance between strength and ductility and, therefore, can be added as necessary. However, if Cr, V, and Mo are added to exceed Cr: 1.0%, V: 0.5%, and Mo: 0.5%, respectively, the secondary phase ratio becomes too large, and concerns rise over a significant increase in strength and the like. Furthermore, an increase in cost is brought about. Therefore, in the case where these elements are added, the individual amounts thereof are Cr: 1.0% or less, V: 0.5% or less, and Mo: 0.5% or less. So that the above-described effects are effectively exerted, Cr: 0.05% or more, V: 0.005% or more, and Mo: 0.005% or more are preferable.


Nickel and copper are elements effective in strengthening a steel and can be added as necessary. Furthermore, there is a function of facilitating internal oxidation to improve adhesion of the coating. However, if both Ni and Cu, more than 1.0% each, are contained, formability of the steel sheet is degraded. Moreover, an increase in cost is brought about. Therefore, in the case where Ni and Cu are added, the content of each of them is 1.0% or less. In this regard, so that the above-described effects are effectively exerted, each of the contents of Ni and Cu is preferably 0.05% or more.


(i) at Least One Type Selected from Ti: 0.1% or Less, Nb: 0.1% or Less, and B: 0.0050% or Less


Titanium and niobium are elements effective in precipitation hardening of steel and can be added as necessary. However, if each of the contents thereof is more than 0.1%, the formability and the shape fixability are degraded. Furthermore, an increase in cost is brought about. Therefore, in the case where Ti and Nb are added, the content of each of them is 0.1% or less. In this regard, so that the above-described effects are effectively exerted, each of the contents of Ti and Nb is preferably 0.01% or more.


Boron functions to suppress generation and growth of ferrite from austenite grain boundaries and, therefore, can be added as necessary. However, if 0.0050% is exceeded, formability is degraded. Furthermore, an increase in cost is brought about. Therefore, in the case where B is added, the content thereof is 0.0050% or less. In this regard, so that the above-described effects are effectively exerted, the content thereof is preferably 0.0003% or more.


(j) at Least One Type Selected from Ca: 0.005% or Less and REM: 0.005% or Less


Calcium and REM (Rare Earth Metal) are elements effective in spheroidizing the shape of a sulfide to improve an adverse influence of the sulfide on the hole expansion property. However, if the content is excessive, increases in inclusions and the like are caused and lead to surface and internal defects and the like. Therefore, in the case where Ca and REM are added, each of the contents thereof is 0.005% or less. In this regard, so that the above-described effects are effectively exerted, each of the content thereof is preferably 0.001% or more.


(2) Next, a steel microstructure will be described.


(a) Area Ratio of Ferrite Phase: 75% or More


To ensure good ductility, it is necessary that a ferrite phase be 75% or more on an area ratio basis.


(b) Area Ratio of Bainitic Ferrite Phase: 1.0% or More


It is necessary to reduce a hardness difference between the mild ferrite and the hard martensite to ensure good hole expansion property. Consequently, it is necessary that the area ratio of bainitic ferrite phase be 1.0% or more.


(c) Area Ratio of Pearlite Phase: 1.0% or More and Less than 10.0%


The area ratio of pearlite phase is specified to be 1.0% or more to ensure good hole expansion property. To ensure predetermined balance between the strength and the ductility, the area ratio of pearlite phase is 10.0% or less.


(d) Area Ratio of Martensite Phase: 1.0% or More and Less than 5.0%


The area ratio of martensite phase is specified to be 1.0% or more to ensure predetermined balance between the strength and the ductility. To ensure good stability of mechanical properties, it is necessary that the area ratio of martensite phase having a large influence on the tensile characteristics (TS, EL) is less than 5.0%.


(e) Area Ratio of Martensite Phase/(Area Ratio of Bainitic Ferrite Phase+Area Ratio of Pearlite phase)≦0.6


To ensure good stability of mechanical properties, it is necessary that, in the phase configuration of the secondary phase, the amount of martensite, which causes variations in mechanical properties, be reduced and the amounts of bainitic ferrite and pearlite milder than martensite be increased, i.e., the area ratio of martensite phase/(area ratio of bainitic ferrite phase+area ratio of pearlite phase)≦0.6 be satisfied.


Meanwhile, retained austenite, tempered martensite, and carbides, e.g., cementite, may be generated besides ferrite, bainitic ferrite, pearlite, and martensite. However, our purposes can be achieved insofar as the above-described area ratios of ferrite, bainitic ferrite, pearlite, and martensite phases are satisfied.


In this regard, the area ratios of ferrite, bainitic ferrite, pearlite, and martensite phases refer to proportions of the areas of the individual phases constituting an observation area.


Our high strength galvanized steel sheet includes the steel sheet having the above-described component composition and the above-described steel microstructure and serving as a substrate steel sheet and a coating film through galvanization or a coating film subjected to an alloying treatment after the galvanization on the substrate steel sheet.


(3) Next, Production Conditions Will be Described.


The high strength galvanized steel sheet is produced by subjecting a steel sheet obtained from a steel having the component composition conforming to the above-described component composition range to two steps of heating treatments described below and, thereafter, subjecting to a galvanization treatment or further subjecting to an alloying treatment after the galvanization treatment.


(a) Production of Steel Sheet


A steel having the above-described component composition is produced by melting, made into a slab through roughing slabbing or continuous casting, and made into a hot rolled steel sheet through hot rolling by a known method. In performing hot rolling, it is preferable that the slab be heated to 1,100° C. to 1,300° C., and hot rolled at a final finishing temperature of 850° C. or higher, and the resulting steel sheet be coiled at 400° C. to 650° C. In the case where the coiling temperature exceeds 650° C., carbides in the hot rolled steel sheet may become coarse and required strength may not be obtained in some cases because such coarse carbides are not dissolved completely during soaking in annealing. Subsequently, a pickling treatment is performed by a known method. The hot rolled steel sheet thus obtained may be used as the above-described steel sheet, or the hot rolled steel sheet after pickling is performed may be further cold-rolled and the resulting cold rolled steel sheet may be used as the above-described steel sheet. In performing the cold rolling, the condition thereof is not necessarily specifically limited, although it is preferable that the cold rolling is performed at the cold reduction ratio of 30% or more. This is because if the cold reduction ratio is low, in some cases, recrystallization of ferrite is not facilitated, unrecrystallized ferrite remains, and the ductility and the hole expansion property are degraded.


(b) Heating Treatment


(i) First Heating Step


As for a first heating step, in the former part, the steel sheet is heated in an atmosphere containing O2: 0.1 to 20 percent by volume and H2O: 1 to 50 percent by volume such that the temperature thereof becomes 400° C. to 750° C. and, in the latter part, the steel sheet is heated in an atmosphere containing O2: 0.01 to less than 0.1 percent by volume and H2O: 1 to 20 percent by volume such that the temperature thereof becomes 600° C. to 850° C.


First Heating Step Former Part


The first heating step former part is performed to oxidize the steel sheet, and the O2 is 0.1 percent by volume or more because an amount sufficient to induce oxidation is required. In this regard, O2 is preferably 20 percent by volume or less, which is the same level as the air, for reason of economy. To facilitate oxidation, H2O is 1 percent by volume or more. In this regard, H2O is preferably 50 percent by volume or less in consideration of a humidification cost. In the step of the former part, if the temperature after the heating is lower than 400° C., oxidation is not induced easily. If the temperature is higher than 750° C., oxidation is induced excessively and iron oxide is peeled by a roll in a second heating step. Therefore, in the former part, heating is performed such that the steel sheet temperature becomes 400° C. or higher and 750° C. or lower.


First Heating Step Latter Part


The first heating step latter part is performed to reduce the steel sheet surface which has been oxidized once and suppress an occurrence of bruise. For that purpose, the heating in the latter part is performed under the condition in which the steel sheet surface can be reduced, but peeling of iron oxide does not occur, that is, the condition of low-temperature reduction heating in a low-oxygen concentration atmosphere to reduce the steel sheet surface, which has been oxidized once in the former part, to such an extent that peeling of iron oxide does not occur in the following second heating step. In this case, O2 is less than 0.1 percent by volume because reduction cannot be induced when O2 is 0.1 percent by volume or more. However, 0.01 percent by volume or more of O2 is necessary. If a large amount of H2O is contained, the steel sheet is oxidized and, therefore, H2O is 20 percent by volume or less. However, 1 percent by volume or more of H2O is necessary. If the steel sheet temperature is lower than 600° C., reduction is not induced easily, and if the temperature is higher than 850° C., the heating cost increases. Therefore, in the latter part, heating is performed such that the steel sheet temperature is 600° C. or higher and 850° C. or lower.


In the case where the heating in the former part is performed with a direct fired furnace (DFF) or a non-oxidizing furnace (NOF), it is preferable that the heating be performed under the condition in which a C gas generated in a coke oven is used as a fuel gas and the air ratio is 1 or more and 1.3 or less. This is because if the air ratio is less than 1, oxidation of the steel sheet is not induced and if the air ratio is more than 1.3, pick up occurs by excessive oxidation. Meanwhile, in the case where the heating in the latter part is performed with a direct fired furnace (DFF) or a non-oxidizing furnace (NOF), it is preferable that the heating be performed under the condition in which a C gas generated in a coke oven is used as a fuel gas and the air ratio is 0.6 or more and less than 1. This is because if the air ratio is 1 or more, iron oxide on the steel sheet surface cannot be reduced and if the air ratio is less than 0.6, the combustion efficiency decreases.


(ii) Second Heating Step


The second heating step is performed successively to the first heating step and induces reduction and adjusts the steel sheet microstructure, wherein holding of the steel sheet is performed in an atmosphere containing H2: 1 to 50 percent by volume and having a dew point of 0° C. or lower at a temperature of 750° C. to 900° C. for 15 to 600 s, cooling to a temperature of 450° C. to 550° C. is performed, and holding is performed at a temperature of 450° C. to 550° C. for 10 to 200 s.


Atmosphere Containing H2: 1 to 50 Percent by Volume and Having Dew Point of 0° C. or Lower


If H2 is less than 1 percent by volume and the dew point is higher than 0° C., iron oxide generated in the first heating step is hardly reduced and, therefore, even if iron oxide sufficient to ensure wettability is generated in the first heating step, on the contrary, wettability is degraded. If H2 is more than 50 percent by volume, an increase in cost is brought about. If the dew point is lower than −60° C., industrial implementation is difficult and, therefore, the dew point is preferably −60° C. or higher.


Holding in Temperature Range of 750° C. to 900° C. for 15 to 600 s


Annealing, which is holding the steel sheet at a temperature of 750° C. to 900° C., specifically in a single phase region of austenite or in a two-phase region of austenite and ferrite, for 15 to 600 s, is performed. In the case where the annealing temperature is lower than 750° C. or the holding time is less than 15 s, hard cementite in the steel sheet is not dissolved sufficiently so that the hole expansion property is degraded and, furthermore, a predetermined area ratio of martensite phase is not obtained, so that the ductility is degraded. On the other hand, if the annealing temperature is higher than 900° C., austenite grains grow significantly, it becomes difficult to ensure bainitic ferrite due to bainite transformation which occurs in the holding after cooling so that the hole expansion property is degraded. Moreover, the area ratio of martensite phase/(area ratio of bainitic ferrite phase+area ratio of pearlite phase) exceeds 0.6, so that good stability of mechanical properties is not obtained. In addition, if the holding time exceeds 600 s, austenite becomes coarse, it becomes difficult to ensure predetermined strength, and an increase in cost associated with large energy consumption may be brought about.


Holding in Temperature Range of 450° C. to 550° C. for 10 to 200 s


After the above-described annealing is performed, cooling to a temperature of 450° C. to 550° C. is performed, followed by holding at a temperature of 450° C. to 550° C. for 10 to 200 s. If the holding temperature is higher than 550° C. or the holding time becomes less than 10 s, bainite transformation is not facilitated, and the area ratio of bainitic ferrite phase becomes less than 1.0%, so that a predetermined hole expansion property is not obtained. Meanwhile, if the holding temperature becomes lower than 450° C. or the holding time exceeds 200 s, most of the secondary phase is converted to austenite and bainitic ferrite, which are generated through facilitation of bainite transformation and which contain large amounts of carbon in solid solution. Then a predetermined area ratio of pearlite phase of 1.0% or more is not obtained and, furthermore, the area ratio of hard martensite phase becomes 5.0% or more so that good hole expansion property and stability of mechanical properties are not obtained.


(c) Galvanization Treatment


After the above-described second heating step, the steel sheet is dipped into a coating bath at a usual bath temperature to be galvanized, and the amount of deposition of coating is adjusted through gas wiping or the like, followed by cooling, so that a galvanized steel sheet having a coating layer not subjected to alloying is obtained.


In the case where a galvanized steel sheet subjected to an alloying treatment is produced, after the galvanization treatment is performed, the alloying treatment of zinc coating is performed at a temperature of 500° C. to 600° C. under the condition satisfying the following formula:

0.45≦exp[200/(400−T)]×ln(t)≦1.0

where

    • T: average holding temperature (° C.) at a temperature of 500° C. to 600° C.,
    • t: holding time (s) at a temperature of 500° C. to 600° C., and
    • exp(X) and ln(X) represent an exponential function and natural logarithm, respectively, of X.


If exp[200/(400−T)]×ln(t) is less than 0.45, much martensite is present in a steel microstructure after the alloying treatment, the above-described hard martensite adjoins mild ferrite to cause a large hardness difference between different phases so that the hole expansion property is degraded. Furthermore, the area ratio of martensite phase/(area ratio of bainitic ferrite phase+area ratio of pearlite phase) is more than 0.6 and, thereby, the stability of mechanical properties is impaired. Moreover, deposition property of the galvanization layer is degraded. If exp[200/(400−T)]×ln(t) exceeds 1.0, most of untransformed austenite is transformed to cementite or pearlite and, as a result, predetermined balance between the strength and the ductility is not ensured.


Meanwhile, at a temperature lower than 500° C., alloying of the coating layer is not facilitated, and it is difficult to obtain a galvannealed steel sheet. Also, at a temperature exceeding 600° C., most of the secondary phase is converted to pearlite so that a predetermined area ratio of martensite phase is not obtained and the balance between the strength and the ductility is degraded.


An alloying treatment is performed at a temperature of 500° C. to 600° C. such that exp[200/(400−T)]×ln(t) satisfies the above-described range and, thereby, a high strength galvanized steel sheet can be obtained without an occurrence of such problems.


A high strength galvanized steel sheet, which has a tensile strength TS of 540 MPa or more, which has excellent formability and stability of mechanical properties, and which also has excellent coating appearance, is thus obtained.



FIG. 1 and FIG. 2 are diagrams showing the organized relationships between the annealing temperature (T1) and TS and between the annealing temperature (T1) and EL in the second heating step with respect to Nos. 15, 16, and 17 of Steel A, which are our examples, (Table 2 and Table 5) and Nos. 18, 19, and 20 of Steel H, which are comparative examples, (Table 2 and Table 5) in Examples described later. Also, FIG. 3 and FIG. 4 are diagrams showing the organized relationships between the average holding temperature (T2) during cooling after annealing and TS and between the average holding temperature (T2) and EL in the second heating step with respect to Nos. 21, 22, and 23 of Steel A, which are our examples, (Table 2 and Table 5) and Nos. 24, 25, and 26 of Steel H, which are comparative examples, (Table 2 and Table 5) in Examples described later.


As is clear from FIGS. 1 and 2, variations in TS and EL associated with changes in annealing temperature of Steel A of our example are small, whereas variations in TS and EL of Steel H of the comparative example are large. Also, as is clear from FIGS. 3 and 4, variations in TS and EL associated with changes in average holding temperature of Steel A of our example are small, whereas variations in TS and EL of Steel H of the comparative example are large.


As is clear from the above-described results, a high strength galvanized steel sheet having high stability of mechanical properties is obtained according to our methods.


By the way, in a series of heat treatments in our manufacturing method, the holding temperature is not necessarily constant insofar as the temperature is in the above-described range. Furthermore, even in the case where the cooling rate is changed during cooling, there is no problem insofar as the rate is in the specified range. Moreover, the steel sheet may be subjected to a heat treatment by any equipment insofar as only the heat history specified in our method is satisfied. In addition, it is also in the scope of our methods that our steel sheets are subjected to temper rolling after the heat treatment for the purpose of shape correction.


In this regard, typically, the steel sheet is usually produced from a steel through the individual steps of steel making, casting, hot rolling, and the like. However, for example, the steel sheet may be produced through thin wall casting or the like, where a part of or whole hot rolling step is omitted.


EXAMPLES

A steel having a component composition shown in Table 1, where the remainder was composed of Fe and incidental impurities, was produced by melting with a converter, and made into a slab by a continuous casting method. The resulting slab was heated to 1,200° C., then hot rolled to a sheet thickness of 3.2 mm at a finishing temperature of 870° C. to 920° C., and coiled at 520° C. Subsequently, the resulting hot rolled sheet was pickled to produce a hot rolled steel sheet. A part of the hot rolled steel sheet was served as a pickled hot rolled steel sheet, and the remainder was further subjected to cold rolling to produce a cold rolled steel sheet. Then, the hot rolled steel sheet after pickling and the cold rolled steel sheet obtained as described above were subjected to an annealing treatment, a galvanization treatment and, furthermore, an alloying treatment of the coating layer with a continuous galvanization line under the production condition shown in Tables 2 to 4 to obtain a galvanized steel sheet (galvanized steel with cold rolled steel sheet substrate: Nos. 1 to 90, galvanized steel with hot rolled steel sheet substrate: Nos. 91 and 92). The amount of deposition of coating was specified to be 30 to 50 g/m2 on one surface basis. Galvanized steel sheets, which were not subjected to an alloying treatment after a galvanization treatment, were also produced partly.










TABLE 1







Steel
Chemical component (percent by mass)


















type
C
Si
Mn
Al
P
S
N
Ni
Cu
Cr
V





A
0.085
1.48
1.41
0.029
0.016
0.0020
0.0029






B
0.094
1.49
1.40
0.031
0.017
0.0021
0.0030






C
0.077
1.51
1.39
0.030
0.015
0.0022
0.0031






D
0.084
1.55
1.40
0.031
0.017
0.0021
0.0030






E
0.086
1.45
1.39
0.030
0.015
0.0022
0.0031






F
0.084
1.50
1.49
0.031
0.017
0.0021
0.0030






G
0.086
1.50
1.30
0.030
0.015
0.0022
0.0031






H
0.084

0.24

1.81
0.035
0.026
0.0020
0.0036


0.15
0.061


I
0.094

0.25

1.80
0.035
0.026
0.0020
0.0036


0.16
0.062


J
0.076

0.25

1.79
0.035
0.026
0.0020
0.0036


0.16
0.062


K
0.086

0.29

1.80
0.035
0.026
0.0020
0.0036


0.14
0.060


L
0.085

0.20

1.80
0.035
0.026
0.0020
0.0036


0.16
0.059


M
0.085

0.23

1.91
0.035
0.026
0.0020
0.0036


0.15
0.059


N
0.085

0.23

1.72
0.035
0.026
0.0020
0.0036


0.15
0.058


O
0.104
1.37
1.22
0.031
0.012
0.0019
0.0036






P
0.055
1.53
1.68
0.032
0.021
0.0027
0.0039






Q
0.092
0.98
1.63
0.039
0.023
0.0028
0.0032






R
0.076
1.47
1.32
0.028
0.018
0.0019
0.0035


0.18



S
0.079
1.55
1.38
0.026
0.012
0.0018
0.0031



0.055


T
0.090
1.41
1.32
0.030
0.013
0.0030
0.0030






U
0.085
1.52
1.42
0.026
0.008
0.0025
0.0032






V
0.081
1.46
1.35
0.029
0.011
0.0027
0.0029






W
0.076
1.52
1.19
0.031
0.018
0.0023
0.0036
0.21
0.14




X
0.093
1.46
1.33
0.030
0.009
0.0030
0.0033






Y

0.151

1.42
1.50
0.039
0.022
0.0026
0.0034






Z
0.102

0.39

1.71
0.030
0.019
0.0028
0.0031






AA
0.056
1.22

2.39

0.028
0.016
0.0019
0.0033
















Steel
Chemical component (percent by mass)















type
Mo
Nb
Ti
B
Ca
REM
Remarks





A






Invention example


B






Invention example


C






Invention example


D






Invention example


E






Invention example


F






Invention example


G






Invention example


H






Comparative example


I






Comparative example


J






Comparative example


K






Comparative example


L






Comparative example


M






Comparative example


N






Comparative example


O






Invention example


P






Invention example


Q






Invention example


R






Invention example


S






Invention example


T
0.046





Invention example


U

0.021




Invention example


V


0.019
0.0020


Invention example


W






Invention example


X




0.0020
0.0010
Invention example


Y






Comparative example


Z






Comparative example


AA






Comparative example





Underlined portion: out of the scope of the present invention
















TABLE 2








First heating step former part
First heating step latter part














Heating

Heating

Second heating step



























tempera-




tempera-



Dew




Steel
O2
H2O

ture
Air
O2
H2O

ture
Air
Furnace
H2
point



No.
type
%
%
Others
° C.
ratio
%
%
Others
° C.
ratio
type
%
° C.
Others





1
A
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













2
B
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













3
C
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













4
D
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













5
E
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













6
F
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













7
G
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













8
H
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













9
I
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













10
J
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













11
K
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













12
L
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













13
M
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













14
N
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













15
A
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













16
A
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













17
A
2
15
N2, CO2,
680
1.15
0.01
5
N2, CO2, CO
700
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













18
H
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













19
H
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













20
H
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













21
A
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













22
A
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













23
A
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













24
H
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













25
H
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













26
H
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













27
A
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













28
A
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













29
A
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













30
A
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2















Second heating step























Average











holding
Holding










temperature
time after








Heating

after cooling
cooling up
Average







tempera-

up to dipping
to dipping
holding







ture
Annealing
into coating
into coating
tempera-
Holding
exp(200/





T1
time
bath T2
bath
ture: T
time: t
(400 − T)) ×




No.
° C.
s
° C.
s
° C.
s
In(t)
Remarks






1
855
160
495
60
570
15
0.835
Invention example



2
855
160
495
60
570
15
0.835
Invention example



3
855
160
495
60
570
15
0.835
Invention example



4
855
160
495
60
570
15
0.835
Invention example



5
855
160
495
60
570
15
0.835
Invention example



6
855
160
495
60
570
15
0.835
Invention example



7
855
160
495
60
570
15
0.835
Invention example



8
830
160
495
60
520
15
0.511
Comparative example



9
830
160
495
60
520
15
0.511
Comparative example



10
830
160
495
60
520
15
0.511
Comparative example



11
830
160
495
60
520
15
0.511
Comparative example



12
830
160
495
60
520
15
0.511
Comparative example



13
830
160
495
60
520
15
0.511
Comparative example



14
830
160
495
60
520
15
0.511
Comparative example



15
850
160
495
60
570
15
0.835
Invention example



16
800
160
495
60
570
15
0.835
Invention example



17
750
160
495
60
570
15
0.835
Invention example



18
850
160
495
60
520
15
0.511
Comparative example



19
800
160
495
60
520
15
0.511
Comparative example



20
750
160
495
60
520
15
0.511
Comparative example



21
850
160
530
60
570
15
0.835
Invention example



22
850
160
500
60
570
15
0.835
Invention example



23
850
160
470
60
570
15
0.835
Invention example



24
830
160
530
60
520
15
0.511
Comparative example



25
830
160
500
60
520
15
0.511
Comparative example



26
830
160
470
60
520
15
0.511
Comparative example



27
860
120
500
40
580
10
0.758
Invention example



28
780
120
500
40
580
10
0.758
Invention example



29
840
280
530
100
555
25
0.886
Invention example



30
840
280
470
100
555
25
0.886
Invention example





Underlined portion: out of the scope of the present invention
















TABLE 3








First heating step former part
First heating step latter part














Heating

Heating

Second heating step



























tempera-




tempera-



Dew




Steel
O2
H2O

ture
Air
O2
H2O

ture
Air
Furnace
H2
point



No.
type
%
%
Others
° C.
ratio
%
%
Others
° C.
ratio
type
%
° C.
Others





31
A
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













32
A
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













33
O
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













34
O
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













35
O
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













36
A
2
15
N2, CO2,
750
1.15
0.01
5
N2, CO2, CO
800
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













37
A
2
15
N2, CO2,
680
1.15
0.01
5
N2, CO2, CO
700
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













38
A
0.5
15
N2, CO2,
700
1.10
0.01
5
N2, CO2, CO
720
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













39
A
0.5
15
N2, CO2,
680
1.10
0.01
5
N2, CO2, CO
700
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













40
A
0.5
15
N2, CO2,
600
1.10
0.01
5
N2, CO2, CO
650
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













41
A
0.1
15
N2, CO2,
680
1.05
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













42
A
8
15
N2, CO2,
680
1.25
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













43
A
0.1
15
N2, CO2,
550
1.05
0.01
5
N2, CO2, CO
630
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













44
A
0.1
15
N2, CO2,
480
1.05
0.01
5
N2, CO2, CO
610
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













45
A
2
15
N2, CO2,
750
1.15
0.01
5
N2, CO2, CO

880

0.85
DFF
10
−35
N2, CO2, CO






CO, H2













46
A
2
15
N2, CO2,
450
1.15
0.01
5
N2, CO2, CO

470

0.85
DFF
10
−35
N2, CO2, CO






CO, H2













47
A
2
15
N2, CO2,
700
1.15

2  

15
N2, CO2, CO
750

1.15

DFF
10
−35
N2, CO2, CO






CO, H2













48
A
2
15
N2, CO2,
700

0.85

0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













49
A
10
15
N2, CO2,
660

1.35

0.01
5
N2, CO2, CO
680
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













50
A
2
15
N2, CO2,
660
1.15
0.01
5
N2, CO2, CO
680
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













51
O
2
15
N2, CO2,
570
1.15
0.01
5
N2, CO2, CO
600
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













52
O
2
15
N2, CO2,

800

1.15
0.01
5
N2, CO2, CO
850
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













53
P
2
15
N2, CO2,
750
1.15
0.01
5
N2, CO2, CO
800
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













54
P
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













55
P
2
15
N2, CO2,
740
1.15
0.01
5
N2, CO2, CO
780
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













56
P
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













57
P
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













58
P
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













59
Q
0.5
15
N2, CO2,
650
1.10
0.01
5
N2, CO2, CO
700
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













60
Q
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2















Second heating step























Average











holding
Holding time










temperature
after










after cooling
cooling up
Average







Hheating

up to dipping
to dipping
holding







tempera-
Annealing
into coating
into coating
tempera-
Holding
exp(200/





ture T1
time
bath T2
bath
ture: T
time: t
(400 − T)) ×




No.
° C.
s
° C.
s
° C.
s
In(t)
Remarks






31
840
180
480
120 



Invention example



32
780
180
480
120 



Invention example



33
850
165
520
60
565
15
0.806
Invention example



34
850
165
470
60
565
15
0.806
Invention example



35
800
160
495
50
545
15
0.682
Comparative example



36
855
160
495
60
570
15
0.835
Invention example



37
855
160
495
60
570
15
0.835
Invention example



38
750
160
495
60
520
15
0.511
Invention example



39
750
160
495
60
520
15
0.511
Invention example



40
750
160
495
60
520
15
0.511
Invention example



41
750
160
495
60
520
15
0.511
Invention example



42
750
160
495
60
520
15
0.511
Invention example



43
750
280
530
100 
555
25
0.886
Invention example



44
750
280
530
100 
555
25
0.886
Invention example



45
900
160
495
60
570
15
0.835
Comparative example



46
750
160
530
100 
555
25
0.886
Comparative example



47
855
160
495
60
570
15
0.835
Comparative example



48
855
160
495
60
570
15
0.835
Comparative example



49
855
160
495
60
570
15
0.835
Comparative example



50

700

160
495
60
570
15
0.835
Comparative example



51

650

180
500
60
555
15
0.745
Comparative example



52

935

230
485
65
570
15
0.835
Comparative example



53
860
180
490
55
575
12
0.792
Invention example



54
780
180
490
55
575
12
0.792
Invention example



55
830

850

505
55
580
12
0.818
Comparative example



56
840
5
495
45
570
12
0.766
Comparative example



57
860
160

600

45
570
12
0.766
Comparative example



58
810
170

130

60
560
12
0.712
Comparative example



59
845
190
520
70
565
18
0.860
Invention example



60
830
200
480
4
555
18
0.795
Comparative example





Underlined portion: out of the scope of the present invention
















TABLE 4








First heating step former part
First heating step latter part














Heating

Heating

Second heating step



























tempera-




tempera-



Dew




Steel
O2
H2O

ture
Air
O2
H2O

ture
Air
Furnace
H2
point



No.
type
%
%
Others
° C.
ratio
%
%
Others
° C.
ratio
type
%
° C.
Others





61
Q
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













62
Q
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













63
Q
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













64
Q
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













65
Q
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













66
R
0.5
15
N2, CO2,
650
1.10
0.01
5
N2, CO2, CO
700
0.85
NOF
10
−35
N2, CO2, CO






CO, H2













67
R
2
15
N2, CO2,
640
1.15
0.01
5
N2, CO2, CO
680
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













68
R
2
15
N2, CO2,
500
1.15
0.01
5
N2, CO2, CO
620
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













69
S
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













70
T
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
730
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













71
U
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













72
U
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
720
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













73
U
2
15
N2, CO2,
650
1.15
0.01
5
N2, CO2, CO
680
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













74
V
2
15
N2, CO2,
600
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













75
W
2
15
N2, CO2,
720
1.15
0.01
5
N2, CO2, CO
750
0.85
NOF
10
−35
N2, CO2, CO






CO, H2













76
X
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













77
X
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













78
X
2
15
N2, CO2,
680
1.15
0.01
5
N2, CO2, CO
700
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













79
Y
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
820
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













80
Y
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













81
Y
2
15
N2, CO2,
600
1.15
0.01
5
N2, CO2, CO
680
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













82
Z
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













83
Z
2
15
N2, CO2,
750
1.15
0.01
5
N2, CO2, CO
780
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













84
Z
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













85
AA
0.5
15
N2, CO2,
680
1.10
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













86
AA
2
15
N2, CO2,
700
1.15
0.01
5
N2, CO2, CO
750
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













87
AA
2
15
N2, CO2,
600
1.15
0.01
5
N2, CO2, CO
680
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













88
A
0.1
15
N2, CO2,
650
1.05
0.01
5
N2, CO2, CO
700
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













89
A
0.1
15
N2, CO2,
650
1.05
0.01
5
N2, CO2, CO
700
0.85
NOF
10
−35
N2, CO2, CO






CO, H2













90
A
0.1
15
N2, CO2,
520
1.05
0.01
5
N2, CO2, CO
600
0.85
DFF
10
−35
N2, CO2, CO






CO, H2













91
A
0.1
15
N2, CO2,
540
1.05
0.01
5
N2, CO2, CO
600
0.85
NOF
10
−35
N2, CO2, CO






CO, H2













92
A
0.1
15
N2, CO2,
520
1.05
0.01
5
N2, CO2, CO
600
0.85
DFF
10
−35
N2, CO2, CO






CO, H2















Second heating step























Average











holding
Holding










temperature
time after










after cooling
cooling up
Average







Heating

up to dipping
to dipping
holding







tempera-
Annealing
into coating
into coating
tempera-
Holding
exp(200/





ture T1
time
bath T2
bath
ture: T
time: t
(400 − T)) ×




No.
° C.
s
° C.
s
° C.
s
In(t)
Remarks






61
845
180
510

410

560
18
0.828
Comparative example



62
840
200
510
55
570
40

1.138

Comparative example



63
845
170
520
60
510
6

0.291

Comparative example



64
810
190
490
70

660

18

1.339

Comparative example



65
820
210
485
65

470

18

0.166

Comparative example



66
860
230
495
90
555
22
0.851
Invention example



67
820
230
495
90
555
22
0.851
Invention example



68
790
220
495
85
555
22
0.851
Invention example



69
840
200
495
75
560
20
0.858
Invention example



70
840
100
500
45
575
11
0.765
Invention example



71
840
190
520
65
555
18
0.795
Invention example



72
810
190
520
70
555
18
0.795
Invention example



73
780
200
520
65
555
18
0.795
Invention example



74
825
260
510
110 
550
26
0.859
Invention example



75
840
110
540
40
580
9
0.723
Invention example



76
850
170
495
60
570
14
0.814
Invention example



77
820
180
495
60
570
14
0.814
Invention example



78
790
180
495
60
570
14
0.814
Invention example



79
870
160
490
55
570
15
0.835
Comparative example



80
800
160
490
55
570
15
0.835
Comparative example



81
750
160
490
55
570
15
0.835
Comparative example



82
860
180
540
60
560
15
0.776
Comparative example



83
860
180
500
60
560
15
0.776
Comparative example



84
860
180
470
60
560
15
0.776
Comparative example



85
850
210
500
45
575
12
0.792
Comparative example



86
800
210
500
45
575
12
0.792
Comparative example



87
750
210
500
45
575
12
0.792
Comparative example



88
850
160
495
60
555
25
0.886
Invention example



89
800
160
495
60
555
25
0.886
Invention example



90
750
160
495
60
555
25
0.886
Invention example



91
850
160
495
60
555
25
0.886
Invention example



92
850
160
495
60
555
25
0.886
Invention example





Underlined portion: out of the scope of the present invention






The area ratios of ferrite, bainitic ferrite, pearlite, and martensite phases of the resulting galvanized steel sheet were determined by polishing a sheet thickness cross-section parallel to a rolling direction of the steel sheet, performing etching with 3% nital, and observing 10 visual fields with a SEM (scanning electron microscope) at a magnification of 2,000 times through the use of Image-Pro of Media Cybernetics, Inc. At that time, it was difficult to distinguish martensite and retained austenite. Therefore, the resulting galvanized steel sheet was subjected to a tempering treatment at 200° C. for 2 hours. Thereafter, the microstructure of a sheet thickness cross-section parallel to the rolling direction of the steel sheet was observed by the above-described method, and the aria ratio of tempered martensite phase determined by the above-described method was taken as the aria ratio of martensite phase.


Meanwhile, the volume ratio of retained austenite phase was determined on the basis of diffracted X-ray intensity of a face at one-quarter sheet thickness, where the steel sheet was grounded up to the one-quarter face in the sheet thickness direction. The Co—Kα line was used as the incident X-ray, the intensity ratios were determined with respect to all combinations of integrated intensities of peaks of {111}, {200}, {220}, and {311} planes of retained austenite phase and {110], {200}, and {211} planes of ferrite phase, and the average value of them was taken as the volume ratio of retained austenite phase.


Meanwhile, a tensile test was performed on the basis of JIS Z 2241 by using JIS No. 5 test piece, where a sample was taken such that a tensile direction became in the direction orthogonal to the rolling direction of the steel sheet, the TS (tensile strength) and the EL (total elongation) were measured, and the case of TS×EL≧19,000 MPa·% was evaluated as good ductility.


As for the stability of mechanical properties, (A) amounts of variations in TS and EL were examined with respect to steel sheets, where only the annealing temperatures T1 were different and the conditions other than the annealing temperature T1 were the same, and the amounts of variations (ΔTS and ΔEL) relative to 20° C. of change in the annealing temperature were determined from the resulting amounts of variations in TS and EL, in addition, (B) amounts of variations in TS and EL were examined with respect to steel sheets, where only the average holding temperatures T2 after the cooling up to the dipping into a coating bath were different and the conditions other than the average holding temperatures T2 after the cooling up to the dipping into a coating bath were the same, and the amounts of variations (ΔTS and ΔEL) relative to 20° C. of change in the average holding temperature after the cooling up to the dipping into a coating bath were determined from the resulting amounts of variations in TS and EL, and the evaluation was performed on the basis of each of the amounts of variations in TS (ΔTS) and the amounts of variations in EL (ΔEL) relative to the 20° C. of temperature change.


In addition, the hole expansion property (stretch flangeability) of the galvanized steel sheet obtained as described above was measured. The hole expansion property (stretch flangeability) was measured on the basis of the Japan Iron and Steel Federation Standard JFST1001. Each of the resulting steel sheets was cut into 100 mm×100 mm, and a hole having a diameter of 10 mm was punched with a clearance of 12%±1% when the sheet thickness was 2.0 mm or more and with a clearance of 12%±2% when the sheet thickness was less than 2.0 mm. Thereafter, a 60° cone punch was pushed into the hole while being held with a blank holder pressure of 9 ton by using a dice having an inside diameter of 75 mm, a hole diameter at the limit of occurrence of cracking was measured, a critical hole expansion ratio λ (%) was determined from the following formula, and the stretch flangeability was evaluated on the basis of the value of the resulting critical hole expansion ratio, and the case of λ≧70(%) was evaluated as good:

Critical hole expansion ratio λ(%)={(Df−D0)/D0}×100

where Df represents a hole diameter (mm) when cracking occurred and D0 represents an initial hole diameter (mm).


Meanwhile, the surface appearance was examined by a method described below.


Presence or absence of appearance defects, e.g., non-coating and bruise, was visually determined. The case where there was no appearance defect was evaluated as good (◯), the case where there were a few appearance defects, but most part were good was evaluated as good for the most part (Δ), and the case where there were appearance defects was evaluated as poor (x).


The results obtained as described above are shown in Tables 5 to 7.




















TABLE 5









Sheet
Area ratio
Area ratio
Area ratio
Area ratio
Volume ratio







Steel
thickness
of F
of M
of BF
of P
of RA
M/
TS
EL
λ


No.
type
(mm)
(%)
(%)
(%)
(%)
(%)
(BF + P)
(MPa)
(%)
(%)





1
A
1.4
87.6
2.2
3.6
4.4
1.2
0.28
626
32.9
102 


2
B
1.4
84.1
3.5
4.2
5.1
2.2
0.38
645
32.4
89


3
C
1.4
88.9
1.7
3.2
4.1
0.8
0.23
611
33.2
111 


4
D
1.4
88.8
1.8
4.1
3.2
1.2
0.25
632
33.2
98


5
E
1.4
86.2
3.0
3.6
4.8
0.9
0.36
623
33.1
104 


6
F
1.4
85.7
3.8
3.6
3.2
2.2
0.56
645
32.4
88


7
G
1.4
88.2
1.5
4.0
4.9
0.7
0.17
609
33.4
110 


8
H
1.4
83.9

13.2


0.8


0.7

0.7

8.80

624
27.6

53



9
I
1.4
82.5

14.8


0.5


0.4

0.8

16.4

689
25.2

44



10
J
1.4
86.8

10.7


0.7


0.3

0.7

10.7

589
29.5

60



11
K
1.4
84.5

13.0


0.8


0.7

0.5

8.67

630
27.8

49



12
L
1.4
83.4

14.7


0.6


0.4

0.5

14.70

618
27.8

52



13
M
1.4
81.9

15.2


0.9


0.4

1.1

11.69

691
26.0

45



14
N
1.4
84.4

12.4


0.9


0.6

0.6

8.27

601
28.6

55



15
A
1.4
87.6
2.4
3.6
5.1
0.9
0.28
612
33.6
110 


16
A
1.4
87.4
2.3
3.7
5.0
1.1
0.26
621
33.2
105 


17
A
1.4
87.5
2.2
3.6
4.8
1.3
0.26
630
33.0
103 


18
H
1.4
84.9

12.2


0.8


0.8

0.5

7.63

608
28.1

58



19
H
1.4
83.8

13.2


0.7


0.8

0.6

8.80

649
26.8

50



20
H
1.4
82.8

14.1


0.6


0.6

0.7

11.75

688
24.9

42



21
A
1.4
87.6
2.4
3.6
4.7
1.2
0.29
632
33.1
99


22
A
1.4
87.9
2.1
3.8
4.8
1.0
0.24
627
33.3
103 


23
A
1.4
87.4
2.0
4.1
4.7
1.3
0.23
622
33.6
112 


24
H
1.4
83.1

13.9


0.7


0.7

0.7

9.93

661
26.5

48



25
H
1.4
84.1

13.2


0.8


0.5

0.9

10.15

628
28.2

54



26
H
1.4
84.8

12.3


0.8


0.6

1.0

8.79

599
29.1

61



27
A
0.8
85.6
3.8
4.9
2.7
2.1
0.50
648
31.5
89


28
A
0.8
84.5
4.2
5.2
2.6
2.5
0.54
659
30.8
86


29
A
2.3
86.1
2.1
4.8
5.8
0.5
0.20
606
35.2
111 


30
A
2.3
85.9
1.8
5.4
6.0
0.4
0.16
600
35.8
123 



















ΔT1/
ΔT2/






TS × EL
Δ20° C.
Δ20° C.
Surface

















No.
(MPa · %)
ΔTS
ΔEL
ΔTS
ΔEL
appearance
Remarks






1
20595





Invention example



2
20898





Invention example



3
20285





Invention example



4
20982





Invention example



5
20621





Invention example



6
20898





Invention example



7
20341





Invention example



8

17222






Comparative example



9

17363






Comparative example



10

17376






Comparative example



11

17514






Comparative example



12

17180






Comparative example



13

17966






Comparative example



14

17189






Comparative example



15
20563
3.6
0.12



Invention example



16
20617





Invention example



17
20790





Invention example



18

17085

16.0 
0.64



Comparative example



19

17393






Comparative example



20

17131






Comparative example



21
20919


3.3
0.16

Invention example



22
20879





Invention example



23
20899





Invention example



24

17517



20.6 
0.86

Comparative example



25

17710






Comparative example



26

17431






Comparative example



27
20412
3.6
0.26



Invention example



28
20297





Invention example



29
21331


2.0
0.20

Invention example



30
21480





Invention example





Underlined portion: out of the scope of the present invention


F: ferrite, M: martensite, BF: bainitic ferrite, P: pearlite, RA: retained austenite


M/(BF + P): Area ratio of M/(Area ratio of BF + Area ratio of P)
























TABLE 6









Sheet
Area ratio
Area ratio
Area ratio
Area ratio
Volume ratio







Steel
thickness
of F
of M
of BF
of P
of RA
M/
TS
EL
λ


No.
type
(mm)
(%)
(%)
(%)
(%)
(%)
(BF + P)
(MPa)
(%)
(%)





31
A
1.4
83.8
4.2
6.4
1.8
3.1
0.51
654
34.1
87


32
A
1.4
84.2
4.4
6.5
1.7
2.8
0.54
661
34.2
84


33
O
1.4
84.9
3.5
5.4
4.9
0.8
0.34
648
32.4
92


34
O
1.4
83.9
3.7
5.8
5.1
1.1
0.34
640
32.8
97


35
O
1.4
85.1

6.8

2.2
3.2
1.8

1.26

628
30.6

67



36
A
1.4
87.8
2.1
3.8
4.1
1.4
0.27
628
33.2
96


37
A
1.4
87.6
2.4
3.9
4.2
1.3
0.30
624
32.8
101 


38
A
1.4
88.4
3.4
2.9
3.6
1.0
0.52
620
31.8
79


39
A
1.4
88.9
3.2
2.9
3.4
0.9
0.51
611
32.4
80


40
A
1.4
88.2
3.6
3.0
3.8
0.7
0.53
615
32.6
76


41
A
1.4
88.9
3.0
2.4
3.6
1.4
0.50
618
32.3
75


42
A
1.4
88.4
3.5
2.8
3.6
1.0
0.55
612
32.8
78


43
A
2.3
87.1
2.5
4.2
5.1
0.7
0.27
608
35.6
121 


44
A
2.3
86.9
2.3
5.0
5.2
0.6
0.23
605
36.0
109 


45
A
1.4
87.6
2.3
4.2
3.8
1.9
0.29
609
32.8
102 


46
A
2.3
87.6
2.2
4.1
5.2
0.6
0.24
608
33.6
82


47
A
1.4
88.2
2.4
3.6
3.6
1.6
0.33
619
32.4
88


48
A
1.4
87.6
2.8
3.8
3.8
1.5
0.37
621
32.8
96


49
A
1.4
87.9
2.9
3.9
3.9
1.3
0.37
617
32.6
92


50
A
1.4
84.8

0.3

2.8
3.4
0.5
0.05
601
28.9

62



51
O
1.4
84.6

0.2

2.9
3.2
0.8
0.03
620
29.7

64



52
O
1.4
88.9
4.7

0.8

3.7
0.3

1.04

615
30.1

65



53
P
1.2
87.8
2.7
4.1
3.8
0.7
0.34
618
32.8
101 


54
P
1.2
85.7
2.8
4.5
3.7
0.8
0.34
623
32.6
104 


55
P
1.2
86.2

0.4

3.2
6.2
0.1
0.04
562
31.6
90


56
P
1.2
85.2

0.3

2.1
2.8
0.5
0.06
603
31.2

62



57
P
1.2
86.1
3.5

0.6

7.6
0.5
0.43
621
27.8
89


58
P
1.2
85.1

8.1

1.2
3.2
1.5

1.84

645
26.4

65



59
Q
1.6
87.8
2.1
4.1
4.4
0.6
0.25
620
32.8
100 


60
Q
1.6
86.2
4.8

0.2

7.2
0.2

0.65

640
26.9

69




















ΔT1/
ΔT2/






TS × EL
Δ20° C.
Δ20° C.
Surface

















No.
(MPa · %)
ΔTS
ΔEL
ΔTS
ΔEL
appearance
Remarks






31
22301
2.3
0.03



Invention example



32
22606





Invention example



33
20995


2.6
0.13

Invention example



34
20992





Invention example



35
19217





Comparative example



36
20850





Invention example



37
20467




Δ
Invention example



38
19716





Invention example



39
19796





Invention example



40
20049





Invention example



41
19961





Invention example



42
20074





Invention example



43
21645





Invention example



44
21780




Δ
Invention example



45
19975




x
Comparative example



46
20429




x
Comparative example



47
20056




x
Comparative example



48
20369




x
Comparative example



49
20114




x
Comparative example



50

17369





x
Comparative example



51

18414





x
Comparative example



52

18512





x
Comparative example



53
20270
1.3
0.05



Invention example



54
20310





Invention example



55

17759





x
Comparative example



56

18814





x
Comparative example



57

17264





x
Comparative example



58

17028





x
Comparative example



59
20336




Δ
Invention example



60

17216





x
Comparative example





Underlined portion: out of the scope of the present invention


F: ferrite, M: martensite, BF: bainitic ferrite, P: pearlite, RA: retained austenite


M/(BF + P): Area ratio of M/(Area ratio of BF + Area ratio of P)
























TABLE 7









Sheet
Area ratio
Area ratio
Area ratio
Area ratio
Volume ratio







Steel
thickness
of F
of M
of BF
of P
of RA
M/
TS
EL
λ


No.
type
(mm)
(%)
(%)
(%)
(%)
(%)
(BF + P)
(MPa)
(%)
(%)





61
Q
1.6
80.1

0.6

6.4

10.3

0.1
0.04

538

30.1
85


62
Q
1.6
84.1

0.5

4.5

10.4

0.3
0.03
592
31.2
85


63
Q
1.6
79.1

6.3

8.4
1.6
3.8

0.63

654
31.2

50



64
Q
1.6
84.2

0.3

4.4

10.5

0.2
0.02
595
31.6
87


65
Q
1.6
79.1

6.5

8.4
1.4
4.1

0.66

650
31.2

55



66
R
2.0
87.8
1.6
3.6
5.2
0.8
0.18
615
34.0
112 


67
R
2.0
87.6
1.7
3.7
5.0
1.2
0.20
617
33.8
108 


68
R
2.0
87.5
1.8
3.8
5.1
1.3
0.20
620
33.2
102 


69
S
1.8
87.6
2.0
3.2
5.0
1.0
0.24
626
33.1
108 


70
T
1.0
86.4
3.8
4.3
3.2
1.9
0.51
631
32.4
95


71
U
1.6
87.2
2.4
3.6
4.8
1.4
0.29
628
32.9
102 


72
U
1.6
87.3
2.5
3.6
4.8
1.2
0.30
631
32.6
100 


73
U
1.6
87.5
2.6
3.5
4.9
1.3
0.31
635
32.2
99


74
V
2.3
86.8
1.6
4.0
6.2
0.6
0.16
613
35.1
121 


75
W
0.8
85.2
4.2
5.2
2.8
2.3
0.53
640
32.4
92


76
X
1.4
87.4
2.1
3.5
4.9
1.1
0.25
625
32.9
99


77
X
1.4
87.2
2.2
3.6
5.0
1.2
0.26
627
32.6
100 


78
X
1.4
87.0
2.4
3.7
5.2
1.3
0.27
630
32.4
95


79
Y
1.4
81.4

14.3


0.6


0.2

2.2

17.88

596
31.6

60



80
Y
1.4
83.1

12.8


0.7


0.3

2.5

12.80

652
29.1

45



81
Y
1.4
85.2

10.7


0.8


0.5

2.6

8.23

698
26.4

38



82
Z
1.4
84.4

12.1


0.4


0.4

0.7

15.13

645
29.0

41



83
Z
1.4
86.4

10.3


0.6


0.6

0.9

8.58

621
29.8

50



84
Z
1.4
87.6

8.9


0.8


0.3

1.2

8.09

596
30.1

57



85
AA
1.2
88.2

6.2


0.8


0.7

2.6

4.13

609
30.5

62



86
AA
1.2
85.4

8.2


0.8


0.6

3.4

5.86

641
29.4

48



87
AA
1.2
82.1

10.4


0.7


0.6

3.8

8.00

684
27.9

40



88
A
2.3
87.8
2.0
3.2
5.6
1.2
0.23
610
34.8
120 


89
A
2.3
87.9
2.2
3.0
5.2
1.2
0.27
606
35.0
115 


90
A
2.3
87.1
1.9
3.6
5.9
1.2
0.20
603
34.9
114 


91
A
2.6
86.9
3.4
3.5
4.2
1.7
0.44
619
36.1
118 


92
A
3.2
87.1
3.2
3.1
4.5
1.9
0.42
612
36.8
123 



















ΔT1/
ΔT2/






TS × EL
Δ20° C.
Δ20° C.
Surface

















No.
(MPa · %)
ΔTS
ΔEL
ΔTS
ΔEL
appearance
Remarks






61

16194





x
Comparative example



62

18470





x
Comparative example



63
20405




x
Comparative example



64

18802





x
Comparative example



65
20280




x
Comparative example



66
20910
1.4
0.22


Δ
Invention example



67
20855





Invention example



68
20584





Invention example



69
20721





Invention example



70
20444





Invention example



71
20661
2.3
0.23



Invention example



72
20571





Invention example



73
20447





Invention example



74
21516





Invention example



75
20736





Invention example



76
20563
1.6
0.16



Invention example



77
20440





Invention example



78
20412





Invention example



79

18834

17.3 
0.86


x
Comparative example



80

18973





x
Comparative example



81

18427





x
Comparative example



82

18705



14.0
0.31
x
Comparative example



83

18506





x
Comparative example



84

17940





x
Comparative example



85

18575

15.0 
0.52


x
Comparative example



86

18845





x
Comparative example



87
19084




x
Comparative example



88
21228
1.4
0.04



Invention example



89
21210





Invention example



90
21045




Δ
Invention example



91
22346





Invention example



92
22522





Invention example





Underlined portion: out of the scope of the present invention


F: ferrite, M: martensite, BF: bainitic ferrite, P: pearlite, RA: retained austenite


M/(BF + P): Area ratio of M/(Area ratio of BF + Area ratio of P)






Since every one of our galvanized steel sheets has TS of 540 MPa or more and λ of 70% or more to exhibit excellent hole expansion property and, furthermore, satisfies TS×EL≧19,000 MPa·% so that the balance between the strength and the ductility is high, it is clear that a high strength galvanized steel sheet having excellent formability is obtained by our methods of manufacturing high strength galvanized steel sheets. Moreover, the values of ΔTS and ΔEL are small and, therefore, it is clear that a high strength galvanized steel sheet having excellent stability of mechanical properties is obtained. On the other hand, in the comparative examples, at least one of the ductility and the hole expansion property is poor, or the stability of mechanical properties is not favorable.


Meanwhile, it is clear that our high strength galvanized steel sheets do not include non-coating and has excellent surface appearance, whereas in the comparative example, non-coating occurs and the surface appearance is poor.


INDUSTRIAL APPLICABILITY

The high strength galvanized steel sheets have a tensile strength TS of 540 MPa or more, exhibit high ductility and high hole expansion property, and further have excellent stability of mechanical properties. In the case where the high strength galvanized steel sheets are applied to, for example, an automobile structural member, enhancement of fuel economy due to weight reduction of a car body can be facilitated. Therefore, an industrial utility value is very large.

Claims
  • 1. A method of manufacturing a high strength galvanized steel sheet having excellent stability of mechanical properties, formability, and coating appearance, comprising: applying a first heating step to a steel sheet containing C: 0.04% or more and 0.13% or less, Si: 0.7% or more and 2.3% or less, Mn: 0.8% or more and 2.0% or less, P: 0.1% or less, S: 0.01% or less, Al: 0.1% or less, N: 0.008% or less, and the remainder composed of Fe and incidental impurities, on a percent by mass basis, in which, in a former part, heating is performed in an atmosphere containing O2: 0.1 to 20 percent by volume and H2O: 1 to 50 percent by volume at a temperature of 400° C. to 750° C. and, in a latter part, heating is performed in an atmosphere containing O2: 0.01 to less than 0.1 percent by volume and H2O: 1 to 20 percent by volume at a temperature of 600° C. to 850° C.;applying a second heating step to the resultant steel sheet, in which holding is performed in an atmosphere containing H2: 1 to 50 percent by volume and having a dew point of 0° C. or lower at a temperature of 750° C. to 900° C. for 15 to 600 s, cooling to a temperature of 450° C. to 550° C. is performed, and holding is performed at a temperature of 450° C. to 550° C. for 10 to 200 s; andapplying a galvanization treatment,wherein the galvanized steel sheet includes 75% or more of ferrite phase, 1.0% or more of bainitic ferrite phase, and 1.0% or more and 10.0% or less of pearlite phase, on an area ratio basis, the area ratio of martensite phase is 1.0% or more and less than 5.0%, and the area ratio of the martensite phase/(area ratio of bainitic ferrite phase+area ratio of pearlite phase)<0.6 is satisfied.
  • 2. The method according to claim 1, wherein the steel sheet further contains at least one type of element selected from Cr: 1.0% or less, V: 0.5% or less, Mo: 0.5% or less, Ni: 1.0% or less, and Cu: 1.0% or less on a percent by mass basis.
  • 3. The method according to claim 1, wherein the steel sheet further contains at least one type of element selected from Ti: 0.1% or less, Nb: 0.1% or less, and B: 0.0050% or less on a percent by mass basis.
  • 4. The method according to claim 1, wherein the steel sheet further contains at least one type of element selected from Ca: 0.005% or less and REM: 0.005% or less on a percent by mass basis.
  • 5. The method according to claim 1, wherein the former part of the first heating step is performed with a direct fired furnace or a non-oxidizing furnace under the condition of an air ratio of 1 or more and 1.3 or less and the latter part of the first heating step is performed with a direct fired furnace or a non-oxidizing furnace under the condition of an air ratio of 0.6 or more and less than 1.
  • 6. The method according to claim 1, wherein, after the galvanization treatment is applied, an alloying treatment of zinc coating is performed at a temperature of 500° C. to 600° C. under conditions satisfying Formula (1): 0.45≦exp[200/(400−T)]×ln(t)≦1.0  (1)
  • 7. The method according to claim 2, wherein the steel sheet further contains at least one type of element selected from Ti: 0.1% or less, Nb: 0.1% or less, and B: 0.0050% or less on a percent by mass basis.
  • 8. The method according to claim 2, wherein the steel sheet further contains at least one type of element selected from Ca: 0.005% or less and REM: 0.005% or less on a percent by mass basis.
  • 9. The method according to claim 3, wherein the steel sheet further contains at least one type of element selected from Ca: 0.005% or less and REM: 0.005% or less on a percent by mass basis.
  • 10. The method according to claim 2, wherein the former part of the first heating step is performed with a direct fired furnace or a non-oxidizing furnace under the condition of an air ratio of 1 or more and 1.3 or less and the latter part of the first heating step is performed with a direct fired furnace or a non-oxidizing furnace under the condition of an air ratio of 0.6 or more and less than 1.
  • 11. The method according to claim 3, wherein the former part of the first heating step is performed with a direct fired furnace or a non-oxidizing furnace under the condition of an air ratio of 1 or more and 1.3 or less and the latter part of the first heating step is performed with a direct fired furnace or a non-oxidizing furnace under the condition of an air ratio of 0.6 or more and less than 1.
  • 12. The method according to claim 4, wherein the former part of the first heating step is performed with a direct fired furnace or a non-oxidizing furnace under the condition of an air ratio of 1 or more and 1.3 or less and the latter part of the first heating step is performed with a direct fired furnace or a non-oxidizing furnace under the condition of an air ratio of 0.6 or more and less than 1.
Priority Claims (1)
Number Date Country Kind
2011-123786 Jun 2011 JP national
PCT Information
Filing Document Filing Date Country Kind 371c Date
PCT/JP2012/064730 6/1/2012 WO 00 2/24/2014
Publishing Document Publishing Date Country Kind
WO2012/165661 12/6/2012 WO A
US Referenced Citations (1)
Number Name Date Kind
8911574 Ootsuka Dec 2014 B2
Foreign Referenced Citations (13)
Number Date Country
2 840 161 Feb 2015 EP
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2007-291498 Nov 2007 JP
2010-196083 Sep 2010 JP
2009081997 Jul 2009 WO
2009099251 Aug 2009 WO
2010098416 Sep 2010 WO
2011090179 Jul 2011 WO
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Non-Patent Literature Citations (1)
Entry
Supplementary European Search Report dated May 4, 2015 of corresponding European Application No. 12792750.7.
Related Publications (1)
Number Date Country
20140174608 A1 Jun 2014 US