Source: http://www.docstoc.com/docs/56182143/High-Carbon-Steel-And-Production-Method-Thereof---Patent-7147730
Timestamp: 2015-07-29 06:09:48
Document Index: 544753856

Matched Legal Cases: ['Art 1', 'Art 2', 'Art 1', 'Art 2', 'Art 3', 'Art 4', 'Art 5', 'Art 1', 'Art 2', 'Art 3', 'Art 4', 'Art 5']

High Carbon Steel And Production Method Thereof - Patent 7147730 by Patents-199
56182143
The present invention relates to a high carbon steel sheet having chemical composition specified by JIS G 4051 (Carbon steels for machine structural use), JIS G 4401 (Carbon tool steels) or JIS G 4802 (Cold-rolled steel strips for springs), andin particular to a high carbon steel sheet having excellent hardenability and toughness, and workability with a high dimensional precision, and a method of producing the same.BACKGROUND ARTHigh carbon steel sheets having chemical compositions specified by JIS G 4051, JIS G 4401 or JIS G 4802 have conventionally much often been applied to parts for machine structural use such as washers, chains or the like. Such high carbon steelsheets have accordingly been demanded to have good hardenability, and recently not only the good hardenability after quenching treatment but also low temperature--short time of quenching treatment for cost down and high toughness after quenchingtreatment for safety during services. In addition, since the high carbon steel sheets have large planar anisotropy of mechanical properties caused by production process such as hot rolling, annealing and cold rolling, it has been difficult to apply thehigh carbon steel sheets to parts as gears which are conventionally produced by casting or forging, and demanded to have workability with a high dimensional precision.Therefore, for improving the hardenability and the toughness of the high carbon steel sheets, and reducing their planar anisotropy of mechanical properties, the following methods have been proposed.(1) JP-A-5-9588, (the term "JP-A" referred to herein signifies "Unexamined Japanese Patent Publication") (Prior Art 1): hot rolling, cooling down to 20 to 500.degree. C. at a rate of 10.degree. C./sec or higher, reheating for a short time, andcoiling so as to accelerate spheroidization of carbides for improving the hardenability.(2) JP-AP-5-98388 (Prior Art 2): adding Nb and Ti to high carbon steels containing 0.30 to 0.70% of C so as to form carbonitrid
United States Patent: 7147730
High carbon steel and production method thereof
To provide a high carbon steel sheet having excellent hardenability and
toughness, and low planar anisotropy of tensile properties affecting
workability, and a method of producing the same.A high car steel sheet
having chemical composition specified by JIS G 4051 (Carbon steels for
machine structural use), JIS G 4401 (Carbon tool steels) or JIS G 4802
(Cold-rolled steel strips for springs), wherein more than 50 carbides
having a diameter of 1.5 .mu.m or larger exist in 2500 .mu.m.sup.2, the
ratio of number of carbides having a diameter of 0.6 .mu.m or less with
respect to all the carbides is 80% or more, and the .DELTA.r is more than
-0.15 to less than 0.15, herein .DELTA.r=(r0+r90-2.times.r45)/4, and r0,
r45, and r90 shows a r-value of the directions of 0.degree. (L),
45.degree. (S) and 90.degree. (C) with respect to the rolling direction
Nakamura; Nobuyuki (Fukuyama, JP), Fujita; Takeshi (Fukuyama, JP), Ito; Katsutoshi (Fukuyama, JP), Takada; Yasuyuki (Fukuyama, JP)
10/665,865
09961843Sep., 20016652671
PCT/JP01/00404Jan., 2001
2000-018280
148/541  ; 148/603; 148/651
C21D 8/02&amp;nbsp(20060101)
148/603,651,653,659,661,541,547
403044422
5-9588
5-98388
6-271935
409087805
52-47512
2000-328172
Patent Abstracts of Japan, vol. 018, No. 686 (C-1292), Dec. 26, 1994 of JP 06 271935 A ( Nippon Steel Corp), Sep. 27, 1994. cited by other
Patent Abstracts of Japan, vol. 1997, No. 01, Jan. 31, 1997 of JP 08 246051 A (Sumitomo Metal Ind Ltd), Sep. 24, 1996. cited by other
Patent Abstracts of Japan, vol. 016, No. 383 (C-0974), Aug. 17, 1992 of JP 04 124216 A (Sumitomo Metal Ind Ltd), Apr. 24, 1992. cited by other
Patent Abstracts of Japan, vol. 1996, No. 09, Sep. 30, 1996 of JP 08 120405 A (Sumitomo Metal Ind Ltd), May 14, 1996. cited by other
Fukui et al, &quot;Formable High Carbon Cold Rolled Steel Sheet Utilizing Graphitization of Cementite&quot;, Report of the ISIJ Meeting of Current Advances in Materials and Processes, vol. 1 (1988), p. 1729, Published by The Iron and Steel Institute of Japan
(with English language translation). cited by other
JIS G 4051 (1979). cited by other
JIS G 4401 (1983). cited by other
JIS G 4802 (1983). cited by other
JIS G 4802:1999 (1999). cited by other
JIS G 4401:2000 (2000). cited by other.
09/961,843 filed Sep. 24, 2001 now U.S. Pat. No. 6,652,671, which is a
continuation application of International Application PCT/JP01/00404
filed Jan. 23, 2001.
1.  A method of producing a high carbon steel sheet, comprising the steps of: hot rolling a steel having chemical composition specified by JIS G 4051, JIS G 4401 or JIS
G 4802, coiling the hot rolled steel sheet at 520 to 600.degree.  C., descaling the coiled steel sheet, annealing the descaled steel sheet at 640 to 690.degree.  C. for 20 hr or longer (primary annealing), cold rolling the annealed steel sheet at a
reduction rate of 50% or more, and annealing the cold rolled steel sheet at 620 to 680.degree.  C. (secondary annealing), and wherein the temperature T1 of the primary annealing and the temperature T2 of the secondary annealing satisfy the following
formula (1), 1024-0.6.times.T1.ltoreq.T2.ltoreq.1202-0.80.times.T1 .  . . (1).
2.  A method of producing a high carbon steel sheet, comprising the steps of: continuously casting into slab a steel having chemical composition specified by JIS G 4051, JIS G 4401 or JIS G 4802, rough rolling the slab to sheet bar without
reheating the slab or after reheating the slab cooled to a certain temperature, finish rolling the sheet bar after reheating the sheet bar to Ar3 transformation point or higher, coiling the finish rolled steel sheet at 500 to 650.degree.  C., descaling
the coiled steel sheet, annealing the descaled steel sheet at a temperature T1 of 630 to 700.degree.  C. for 20 hr or longer (primary annealing), cold rolling the annealed steel sheet at a reduction rate of 50% or higher, and annealing the cold rolled
steel sheet at a temperature T2 of 620 to 680.degree.  C. (secondary annealing), wherein the temperature T1 and the temperature T2 satisfy the following formula (2), 1010-0.59.times.T1.ltoreq.T2.ltoreq.1210-0.80.times.T1 .  . . (2).
3.  A method of producing a high carbon steel sheet, comprising the steps of: continuously casting into slab a steel having chemical composition specified by JIS G 4051, JIS G 4401 or JIS G 4802, rough rolling the slab to sheet bar without
reheating the slab or after reheating the slab cooled to a certain temperature, finish rolling the sheet bar during reheating the rolled sheet bar to Ar3 transformation point or higher, coiling the finish roiled steel sheet at 500 to 650.degree.  C.,
descaling the coiled steel sheet, annealing the descaled steel sheet at a temperature T1 of 630 to 700.degree.  C. for 20 hr or longer (primary annealing), cold rolling the annealed steel sheet at a reduction rate of 50% or higher, and annealing the cold
rolled steel sheet at a temperature T2 of 620 to 680.degree.  C. (secondary annealing), wherein the temperature T1 and the temperature T2 satisfy the following formula (2) 1010-0.59.times.T1.ltoreq.T2.ltoreq.1210-0.80.times.T1 .  . . (2).
The present invention relates to a high carbon steel sheet having chemical composition specified by JIS G 4051 (Carbon steels for machine structural use), JIS G 4401 (Carbon tool steels) or JIS G 4802 (Cold-rolled steel strips for springs), and
in particular to a high carbon steel sheet having excellent hardenability and toughness, and workability with a high dimensional precision, and a method of producing the same.
High carbon steel sheets having chemical compositions specified by JIS G 4051, JIS G 4401 or JIS G 4802 have conventionally much often been applied to parts for machine structural use such as washers, chains or the like.  Such high carbon steel
sheets have accordingly been demanded to have good hardenability, and recently not only the good hardenability after quenching treatment but also low temperature--short time of quenching treatment for cost down and high toughness after quenching
treatment for safety during services.  In addition, since the high carbon steel sheets have large planar anisotropy of mechanical properties caused by production process such as hot rolling, annealing and cold rolling, it has been difficult to apply the
high carbon steel sheets to parts as gears which are conventionally produced by casting or forging, and demanded to have workability with a high dimensional precision.
Therefore, for improving the hardenability and the toughness of the high carbon steel sheets, and reducing their planar anisotropy of mechanical properties, the following methods have been proposed.
(1) JP-A-5-9588, (the term &quot;JP-A&quot; referred to herein signifies &quot;Unexamined Japanese Patent Publication&quot;) (Prior Art 1): hot rolling, cooling down to 20 to 500.degree.  C. at a rate of 10.degree.  C./sec or higher, reheating for a short time, and
coiling so as to accelerate spheroidization of carbides for improving the hardenability.
(2) JP-AP-5-98388 (Prior Art 2): adding Nb and Ti to high carbon steels containing 0.30 to 0.70% of C so as to form carbonitrides for restraining austenite grain growth and improving the toughness.
(3) &quot;Material and Process&quot;, vol. 1 (1988), p. 1729 (Prior Art 3): hot rolling a high carbon steel containing 0.65% of C, cold rolling at a reduction rate of 50%, batch annealing at 650.degree.  C. for 24 hr, subjecting to secondary cold rolling
at a reduction rate of 65%, and secondary batch annealing at 680.degree.  C. for 24 hr for improving the workability; otherwise adjusting the chemical composition of a high carbon steel containing 0.65% of C, repeating the rolling and the annealing as
above mentioned so as to graphitize cementites for improving the workability and reducing the planar anisotropy of r-value.
(4) JP-A-10-152757 (Prior Art 4): adjusting contents of C, Si, Mn, P, Cr, Ni, Mo, V, Ti and Al, decreasing S content below 0.002 wt %, so that 6 .mu.m or less is the average length of sulfide based non metallic inclusions narrowly elongated in
the rolling direction, and 80% or more of all the inclusions are the inclusions whose length in the rolling directions is 4 .mu.m or less, whereby the planar anisotropy of toughness and ductility is made small.
(5) JP-A-6-271935 (Prior Art 5), hot rolling, at Ar3 transformation point or higher, a steel whose contents of C, Si, Mn, Cr, Mo, Ni, B and Al were adjusted, cooling at a rate of 30.degree.  C./sec or higher, coiling at 550 to 700.degree.  C.,
descaling, primarily annealing at 600 to 680.degree.  C., cold rolling at a reduction rate of 40% or more, secondarily annealing at 600 to 680.degree.  C., and temper rolling so as to reduce the planar shape anisotropy caused by quenching treatment.
However, there are following problems in the above mentioned prior arts.
Prior Art 1: Although reheating for a short time, followed by coiling, a treating time for spheroidizing carbides is very short, and the spheroidization of carbides is insufficient so that the good hardenability might not be probably sometimes
provided.  Further, for reheating for a short time until coiling after cooling, a rapidly heating apparatus such as an electrically conductive heater is needed, resulting in an increase of production cost.
Prior Art 2: Because of adding expensive Nb and Ti, the production cost is increased.
Prior Art 3: .DELTA.r=(r0+r.pi.-2.times.r45)/4 is -0.47, which is a parameter of planar anisotropy of r-value (r0, r45, and r90 shows a r-value of the directions of 0.degree.  (L), 45.degree.  (S) and 90.degree.  (C) with respect to the rolling
direction respectively).  .DELTA.max of r-value being a difference between the maximum value and the minimum value among r0, r45, and r90 is 1.17.  Since the .DELTA.r and the .DELTA.max of r-value are high, it is difficult to carry out a forming with a
Besides, by graphitizing the cementites, the .DELTA.r decreases to 0.34 and the .DELTA.max of r-value decreases to 0.85, but the forming could not be carried out with a high dimensional precision.  In case graphitizing, since a dissolving speed
of graphites into austenite phase is slow, the hardenability is remarkably degraded.
Prior Art 4: The planar anisotropy caused by inclusions is decreased, but the forming could not be always carried out with a high dimensional precision.
Prior Art 5: Poor shaping caused by quenching treatment could be improved, but the forming could not be always carried out with a high dimensional precision.
The present invention has been realized to solve above these problems, and it is an object of the invention to provide a high carbon steel sheet having excellent hardenability and toughness, and workability with a high dimensional precision, and
a method of producing the same.
The present object could be accomplished by a high carbon steel sheet having chemical composition specified by JIS G 4051, JIS G 4401 or JIS G 4802, in which the ratio of number of carbides having a diameter of 0.6 .mu.m or less with respect to
all the carbides is 80% or more, more than 50 carbides having a diameter of 1.5 .mu.m or larger exist in 2500 .mu.m.sup.2 of observation field area of electron microscope, and the .DELTA.r being a parameter of planar anisotropy of r-value is more than
-0.15 to less than 0.15.
The above mentioned high carbon steel sheet can be produced by a method comprising the steps of: hot rolling a steel having chemical composition specified by JIS G 4051, JIS G 4401 or JIS G 4802, coiling the hot rolled steel sheet at 520 to
600.degree.  C., descaling the coiled steel sheet, primarily annealing the descaled steel sheet at 640 to 690.degree.  C. for 20 hr or longer, cold rolling the annealed steel sheet at a reduction rate of 50% or more, and secondarily annealing the cold
rolled steel sheet at 620 to 680.degree.  C.
The JIS G standards JIS G 4051 (1979), JIS G 4401:2000 and JIS G 4802:1999 and particularly the section of each disclosing the chemical composition, are hereby incorporated by reference.
FIG. 1 shows the relationship between maximum diameter Dmax of carbide when 80% or more is the ratio of number of carbides having diameters .ltoreq.  Dmax with respect to all the carbides and hardness after quenching treatment;
FIG. 2 shows the relationship between number of carbides having a diameter of 1.5 .mu.m or larger which exist in 2500 .mu.m.sup.2 of observation field area of electron microscope and austenite grain size;
FIG. 3 shows the relationship between primary annealing temperature, secondary annealing temperature and .DELTA.max of r-value; and
FIG. 4 shows the another relationship between primary annealing temperature, secondary annealing temperature and .DELTA.max of r-value.
As to the high carbon steel sheet containing chemical composition specified by JIS G 4051, JIS G 4401 or JIS G 4802, we investigated the hardenability, the toughness and the dimensional precision when forming, and found that the existing
condition of carbides precipitated in steel was a governing factor over the hardenability and the toughness, while the planar anisotropy of r-value was so over the dimensional precision when forming, and in particular for providing an enough dimensional
precision when forming, the planar anisotropy of r-value should be made smaller than that of the prior art.  The details will be explained as follows.
(i) Hardenability and toughness
By making a steel having, by wt %, C: 0.36%, Si: 0.20%, Mn: 0.75%, P: 0.011%, S: 0.002% and Al: 0.020%, hot rolling at a finishing temperature of 850.degree.  C., coiling at a coiling temperature of 560.degree.  C., pickling, primarily annealing
at 640 to 690.degree.  C. for 40 hr, cold rolling at a reduction rate of 60%, and secondarily annealing at 610 to 690.degree.  C. for 40 hr, steel sheets were produced.  Cutting out samples of 50.times.100 mm from the produced steel sheets, and heating
at 820.degree.  C. for 10 sec, followed by quenching into oil at around 20.degree.  C., the hardness was measured and carbides were observed by an electron microscope.
The hardness was averaged over 10 measurements by Rockwell C Scale (HRc).  If the average HRc is 50 or more, it may be judged that the good hardenability is provided.
The carbides were observed using a scanning electron microscope at 1500 to 5000 magnifications after polishing the cross section in a thickness direction of the steel sheet and etching it with a picral.  Further, measurements were made on the
size and the number of carbides in an observation field area of 2500 .mu.m.sup.2.  The reason for preparing the observing field area of 2500 .mu.m.sup.2 was that if an observing field area was smaller than this, the number of observable carbides was
small, and the size and the number of carbides could not be measured precisely.
FIG. 1 shows the relationship between maximum diameter Dmax of carbide when 80% or more is the ratio of number of carbides having diameters .ltoreq.  Dmax with respect to all the carbides and hardness after quenching treatment.
If the ratio of number of carbides having a diameter of 0.6 .mu.m or less with respect to all the carbides is 80% or more, the HRc exceeds 50 and the good hardenability may be obtained.  This is considered to be because fine carbides below 0.6
.mu.m in diameter are rapidly dissolved into austenite phase when quenching.
But, if the diameter of all the carbides are below 0.6 .mu.m, all the carbides are dissolved into the austenite phase when quenching, so that the austenite grains are remarkably coarsened and the toughness might be deteriorated.  For avoiding it,
as shown in FIG. 2, more than 50 carbides having a diameter of 1.5 .mu.m or larger should exist in 2500 .mu.m.sup.2 of observation field area of electron microscope.
(ii) Dimensional precision when forming
For improving the dimensional precision when forming, it is necessary that the .DELTA.r is made small as described above.  But it is not known how small the .DELTA.r should be made to obtain an equivalent dimensional precision in gear parts
conventionally produced by casting or forging.  So, the relationship between .DELTA.r and dimensional precision when forming was studied.  As a result, it was found that if the .DELTA.r was more than -0.15 to less than 0.15, the equivalent dimensional
precision in gear parts produced by casting or forging could be provided.
If the .DELTA.max of r-value instead of the .DELTA.r is made less than 0.2, the forming can be conducted with a higher dimensional precision.
The high carbon steel sheet under the existing condition of carbides as mentioned in (i) and having a .DELTA.r of more than -0.15 to less than 0.15 as mentioned in (ii), can be produced by a method comprising the steps of: hot rolling a steel
having chemical composition specified by JIS G 4051, JIS G 4401 or JIS G 4802, coiling the hot rolled steel sheet at 520 to 600.degree.  C., descaling the coiled steel sheet, primarily annealing the descaled steel sheet at 640 to 690.degree.  C. for 20
hr or longer, cold rolling the annealed steel sheet at a reduction rate of 50% or more, and secondarily annealing the cold rolled steel sheet at 620 to 680.degree.  C. Detailed explanation will be made therefore as follows.
(1) Coiling Temperature
Since the coiling temperature lower than 520.degree.  C. makes pearlite structure very fine, carbides after the primary annealing are considerably fine, so that carbides having a diameter of 1.5 .mu.m or larger cannot be produced after the
secondary annealing.  In contrast, exceeding 600.degree.  C., coarse pearlite structure is generated, so that carbides having a diameter of 0.6 .mu.m or less cannot be produced after the secondary annealing.  Accordingly, the coiling temperature is
defined to be 520 to 600.degree.  C.
(2) Primary Annealing
If the primary annealing temperature is higher than 690.degree.  C., carbides are too much spheroidized, so that carbides having a diameter of 0.6 .mu.m or less cannot be produced after the secondary annealing.  On the other hand, being lower
than 640.degree.  C., the spheroidization of carbides is difficult, so that carbides having a diameter of 1.5 .mu.m or larger cannot be produced after the secondary annealing.  Accordingly, the primary annealing temperature is defined to be 640 to
690.degree.  C. The annealing time should be 20 hr or longer for uniformly spheroidizing.
(3) Cold Reduction Rate
In general, the higher the cold reduction rate, the smaller the .DELTA.r, and for making .DELTA.r more than -0.15 to less than 0.15, the cold reduction rate of at least 50% is necessary.
(4) Secondary Annealing
If the secondary annealing temperature exceeds 680.degree.  C., carbides are greatly coarsened, the grain grows markedly, and the .DELTA.r increases.  On the other hand, being lower than 620.degree.  C., carbides become fine, and
recrystallization and grain growth are not sufficient, so that the workability decreases.  Thus, the secondary annealing temperature is defined to be 620 to 680.degree.  C. For the secondary annealing, either a continuous annealing or a box annealing
For producing the high carbon steel sheet under the existing condition of carbides as mentioned in (i) and having a .DELTA.max of r-value of less than 0.2 as mentioned in (ii), the primary annealing temperature T1 and the secondary annealing
temperature T2 in the above method should satisfy the following formula (1).  1024-0.6.times.T1.ltoreq.T2.ltoreq.1202-0.80.times.T1 .  . . (1)
Detailed explanation will be made therefore as follows.
By making a slab of, by wt %, C: 0.36%, Si: 0.20%, Mn: 0.75%, P: 0.011%, S: 0.002% and Al: 0.020%, hot rolling at a finishing temperature of 850.degree.  C. and coiling at a coiling temperature of 560.degree.  C., pickling, primarily annealing at
640 to 690.degree.  C. for 40 hr, cold rolling at a reduction rate of 60%, and secondarily annealing at 610 to 690.degree.  C. for 40 hr, steel sheets were produced, and the .DELTA.max of r-value was measured.
As seen in FIG. 3, if the primary annealing temperature T1 is 640 to 690.degree.  C. and the secondary annealing temperature T2 is in response to the primary annealing temperature T1 to satisfy the above formula (1), the .DELTA.max of r-value is
At this time, if the secondary annealing temperature is higher than 680.degree.  C., carbides are coarsened, and carbides having a diameter of 0.6 .mu.m or less cannot be obtained.  In contrast, being lower than 620.degree.  C., carbides having a
diameter of 1.5 .mu.m or larger cannot be obtained.  Therefore, the secondary annealing temperature is defined to be 620 to 680.degree.  C. For the secondary annealing, either a continuous annealing or a box annealing will do.
The .DELTA.max of r-value can be made smaller, if the high carbon steel sheet is produced by such a method comprising the steps of: continuously casting into slab a steel having chemical composition specified by JIS G 4051, JIS G 4401 or JIS G
4802, rough rolling the slab to sheet bar without reheating the slab or after reheating the slab cooled to a certain temperature, finish rolling the sheet bar (rough rolled slab) after reheating the sheet bar to Ar3 transformation point or higher,
coiling the finish rolled steel sheet at 500 to 650.degree.  C., descaling the coiled steel sheet, primarily annealing the descaled steel sheet at a temperature T1 of 630 to 700.degree.  C. for 20 hr or longer, cold rolling the annealed steel sheet at a
reduction rate of 50% or higher, and secondarily annealing the cold rolled steel sheet at a temperature T2 of 620 to 680.degree.  C., wherein the temperature T1 and the temperature T2 satisfy the following formula (2).
1010-0.59.times.T1.ltoreq.T2.ltoreq.1210-0.80.times.T1 .  . . (2)
At this time, instead of finish rolling the sheet bar after reheating the sheet bar to Ar3 transformation point or higher, by finish rolling the sheet bar during reheating the rolled sheet bar to Ar3 transformation point or higher the similar
effect is available.  Detailed explanation will be made therefor as follows.
(5) Reheating the Sheet Bar
By finish rolling the sheet bar after reheating the sheet bar to Ar3 transformation point or higher or during reheating the rolled sheet bar to Ar3 transformation point or higher, crystal grains are uniformed in a thickness direction of steel
sheet during rolling, the dispersion of carbides after the secondary annealing is small, and the planar anisotropy of r-value becomes smaller.  Accordingly, more excellent hardenability and toughness, and higher dimensional precision when forming are
obtained.  The reheating time should be at least 3 seconds.  As the reheating time is short like this, an induction heating is preferably applied.
(6) Coiling Temperature and Primary Annealing Temperature
If the sheet bar is reheated as above mentioned, the ranges of the coiling temperature and the primary annealing temperature are respectively enlarged to 500 to 650.degree.  C. and 630 to 700.degree.  C. as compared with the case where the sheet
bar is not reheated.
(7) Relationship Between Primary Annealing Temperature T1 and Secondary Annealing Temperature T2
By making a slab of, by wt %, C: 0.36%, Si: 0.20%, Mn: 0.75%, P: 0.011%, S: 0.002% and Al: 0.020%, rough rolling, reheating the sheet bar at 1010.degree.  C. for 15 sec by an induction heater, finish rolling at 850.degree.  C., coiling at
560.degree.  C., pickling, primarily annealing at 640 to 700.degree.  C. for 40 hr, cold rolling at a reduction rate of 60%, and secondarily annealing at 610 to 690.degree.  C. for 40 hr, steel sheets were produced.  Measurements were made on the (222)
integrated reflective intensity in the thickness directions (surface, 1/4 thickness and 1/2 thickness) by X-ray diffraction method.
As shown in Table 1, by reheating the sheet bar, the .DELTA.max of (222) intensity being a difference between the maximum value and the minimum value of (222) integrated reflective intensity in the thickness direction becomes small, and therefore
the structure is more uniformed in the thickness direction.
As seen in FIG. 4, within the range satisfying the above formula (2), the .DELTA.max of r-value less than 0.15 is obtained.  The range satisfying the above formula (2) is wider than that of the formula (1).
TABLE-US-00001 TABLE 1 Integrated reflective intensity (222) Reheating of Primary Secondary 1/4 sheet bar annealing annealing thick- 1/2 (.degree.  C. .times.  sec) (.degree.  C. .times.  hr) (.degree.  C. .times.  hr) Surface ness thickness
.DELTA.max 1010 .times.  15 640 .times.  40 610 .times.  40 2.81 2.95 2.89 0.14 1010 .times.  15 640 .times.  40 650 .times.  40 2.82 2.88 2.95 0.13 1010 .times.  15 640 .times.  40 690 .times.  40 2.90 2.91 3.02 0.12 1010 .times.  15 680 .times.  40 610
.times.  40 2.37 2.35 2.46 0.11 1010 .times.  15 680 .times.  40 650 .times.  40 2.40 2.36 2.47 0.11 1010 .times.  15 680 .times.  40 690 .times.  40 2.29 2.34 2.39 0.10 -- 640 .times.  40 610 .times.  40 2.70 3.01 2.90 0.31 -- 640 .times.  40 650
.times.  40 2.75 2.87 2.99 0.24 -- 640 .times.  40 690 .times.  40 2.81 2.90 3.05 0.24 -- 680 .times.  40 610 .times.  40 2.34 2.27 2.50 0.23 -- 680 .times.  40 650 .times.  40 2.39 2.23 2.51 0.28 -- 680 .times.  40 690 .times.  40 2.25 2.37 2.45 0.20
For improving sliding property, the high carbon steel sheet of the present invention may be galvanized through an electro-galvanizing process or a hot dip Zn plating process, followed by a phosphating treatment.
To produce the high carbon steel sheet of the present invention, a continuous hot rolling process using a coil box may be applicable.  In this case, the sheet bar may be reheated through rough rolling mills, before or after the coil box, or
before and after a welding machine.
By making a slab containing the chemical composition specified by S35C of JIS G 4051 (by wt %, C: 0.35%, Si: 0.20%, Mn: 0.76%, P: 0.016%, S: 0.003% and Al: 0.026%) through a continuous casting process, reheating to 1100.degree.  C., hot rolling,
coiling, primarily annealing, cold rolling, secondarily annealing, under the conditions shown in Table 2, and temper rolling at a reduction rate of 1.5%, the steel sheets A H of 1.0 mm thickness were produced.  Herein, the steel sheet H is a conventional
high carbon steel sheet.  The existing condition of carbides and the hardenability were investigated by the above mentioned methods.  Further, mechanical properties and austenite grain size were measured as follows.
JIS No. 5 test pieces were sampled from the directions of 0.degree.  (L), 45.degree.  (S) and 90.degree.  (C) with respect to the rolling direction, and subjected to the tensile test at a tension speed of 10 mm/min so as to measure the mechanical
properties in each direction.  The .DELTA.max of each mechanical property, that is, a difference between the maximum value and the minimum value of each mechanical property, and the .DELTA.r were calculated.
(b) Austenite Grain Size
The cross section in a thickness direction of the quenched test piece for investigating the hardenability was polished, etched, and observed by an optical microscope.  The austenite grain size number was measured following JIS G 0551.
As to the inventive steel sheets A C, the existing condition of carbides is within the range of the present invention, and therefore the HRc after quenching is above 50 and the good hardenability is obtained.  The austenite grain size of these
steel sheets is small, and therefore the excellent toughness is obtained.  In addition, the .DELTA.r is more than -0.15 to less than 0.15, that is, the planar anisotropy is very small, and accordingly the forming is carried out with a high dimensional
precision.  At the same time, the .DELTA.max of yield strength and tensile strength is 10 MPa or lower, the .DELTA.max of the total elongation is 1.5% or lower, and thus each planar anisotropy is very small.
In contrast, the comparative steel sheets D H have large .DELTA.max of the mechanical properties and .DELTA.r.  The steel sheet D has coarse austenite grain size.  In the steel sheets E, G, and H, the HRc is less than 50.
TABLE-US-00002 TABLE 2 Coiling Primary Cold Secondary Steel temperature annealing reduction annealing Number of carbides Ratio of carbides Remark sheet (.degree.  C.) (.degree.  C. .times.  hr) rate (%) (.degree.  C. .times.  hr) larger than 1.5
.mu.m smaller than 0.6 .mu.m (%) Remark A 580 650 .times.  40 70 680 .times.  40 89 84 Present invention B 560 640 .times.  20 60 660 .times.  40 84 87 Present invention C 540 660 .times.  20 65 640 .times.  40 81 93 Present invention D 500 640 .times.
40 60 660 .times.  40 64 96 Comparative example E 560 710 .times.  40 65 660 .times.  40 103 58 Comparative example F 540 660 .times.  20 40 680 .times.  40 86 84 Comparative example G 550 640 .times.  20 60 720 .times.  40 98 61 Comparative example H
620 -- 50 690 .times.  40 74 70 Comparative example
TABLE-US-00003 TABLE 3 Hard- Auste- ness tine after Grain Mechanical properties before quenching quench- size Steel Yield strength (MPa) Tensile strength (MPa) Total elongation (%) r-value ing (size sheet L S C .DELTA.max L S C .DELTA.max L S C
.DELTA.max L S C .DELTA.r (H- Rc) No.) Remark A 395 391 393 4 506 502 507 5 35.7 36.4 35.9 0.7 1.06 0.97 1.04 0.04 52 11- .6 Present inven- tion B 405 404 411 7 504 498 507 9 35.8 36.8 36.2 1.0 1.12 0.98 1.23 0.10 54 11- .3 Present inven- tion C 409 406
414 8 509 505 513 8 35.2 36.4 35.3 1.2 0.98 1.19 1.05 -0.09 56 1- 0.7 Present inven- tion D 369 362 370 8 499 496 503 9 30.1 29.3 31.0 1.7 1.16 0.92 1.33 0.16 57 8.- 6 Compa- rative example E 370 379 375 9 480 484 481 4 36.9 36.0 36.4 0.9 1.15 0.96 1.47
0.18 44 12- .2 Compa- rative example F 374 377 385 11 474 480 488 14 35.7 34.6 36.3 1.7 1.25 0.96 1.46 0.20 53 - 11.2 Compa- rative example G 372 376 379 7 496 493 498 5 38.0 37.7 37.7 0.3 1.14 0.94 1.64 0.23 40 12- .1 Compa- rative example H 317 334 320
17 501 516 510 15 36.5 34.6 35.5 1.9 1.12 0.92 1.35 0.16 49 - 11.6 Compa- rative example
By making a slab containing the chemical composition specified by S35C of JIS G 4051 (by wt %, C: 0.36%, Si: 0.20%, Mn: 0.75%, P: 0.011%, S: 0.002% and Al: 0.020%) through a continuous casting process, reheating to 1100.degree.  C., hot rolling,
coiling, primarily annealing, cold rolling, secondarily annealing, under the conditions shown in Table 4, and temper rolling at a reduction rate of 1.5%, the steel sheets 1 19 of 2.5 mm thickness were produced.  Herein, the steel sheet 19 is a
conventional high carbon steel sheet.  The same measurements as in Example 1 were conducted.  The .DELTA.max of r-value was calculated in stead of .DELTA.r.
As to the inventive steel sheets 1 7, the existing condition of carbides is within the range of the present invention, and therefore the HRc after quenching is above 50 and the good hardenability is obtained.  The austenite grain size of these
steel sheets is small, and therefore the excellent toughness is obtained.  In addition, the .DELTA.max of r-value is below 0.2, that is, the planar anisotropy is extremely small, and accordingly the forming is carried out with a high dimensional
In contrast, the comparative steel sheets 8 19 have large .DELTA.max of the mechanical properties.  The steel sheets 8, 10, 17 and 18 have coarse austenite grain size.  In the steel sheets 9, 11, 15, 16 and 19, the HRc is less than 50.
TABLE-US-00004 TABLE 4 Coiling Primary Cold Secondary Number of Ratio of carbides Steel temperature annealing reduction annealing Secondary annealing carbides larger smaller than 0.6 .mu.m sheet (.degree.  C.) (.degree.  C. .times.  hr) rate (%)
(.degree.  C. .times.  hr) range by the formula (1) than 1.5 .mu.m (%) Remark 1 580 640 .times.  40 70 680 .times.  40 640 680 56 85 Present invention 2 530 640 .times.  20 60 680 .times.  40 640 680 52 87 Present invention 3 595 640 .times.  40 60 680
.times.  20 640 680 64 81 Present invention 4 580 660 .times.  40 60 660 .times.  40 628 674 61 83 Present invention 5 580 680 .times.  20 60 640 .times.  40 620 658 63 82 Present invention 6 580 640 .times.  40 50 660 .times.  40 640 680 56 85 Present
invention 7 580 640 .times.  40 70 640 .times.  40 640 680 54 86 Present invention 8 510 640 .times.  20 60 680 .times.  40 640 680 30 92 Comparative example 9 610 640 .times.  20 60 680 .times.  20 640 680 68 61 Comparative example 10 580 620 .times.
40 60 680 .times.  40 -- 32 90 Comparative example 11 580 720 .times.  40 60 680 .times.  40 -- 68 65 Comparative example 12 580 640 .times.  15 70 680 .times.  40 640 680 54 86 Comparative example 13 580 640 .times.  40 30 680 .times.  40 640 680 58 84
Comparative example 14 580 660 .times.  20 60 620 .times.  40 628 674 60 84 Comparative example 15 580 640 .times.  20 60 700 .times.  40 640 680 66 73 Comparative example 16 580 640 .times.  40 60 690 .times.  40 640 680 67 70 Comparative example 17 580
690 .times.  40 60 615 .times.  40 620 650 33 88 Comparative example 18 500 640 .times.  20 60 640 .times.  20 640 690 45 88 Comparative example 19 620 -- 50 690 .times.  40 -- 51 67 Comparative example
TABLE-US-00005 TABLE 5 Hard- Auste- ness tine after Grain Mechanical properties before quenching quench- size Steel Yield strength (MPa) Tensile strength (MPa) Total elongation (%) r-value ing (size sheet L S C .DELTA.max L S C .DELTA.max L S C
.DELTA.max L S C .DELTA.max - (HRc) No.) Remark 1 398 394 402 8 506 508 513 5 36.2 37.4 37.0 1.2 1.07 0.99 1.00 0.08 54 11- .1 Present inven- tion 2 410 407 412 5 513 512 516 4 36.8 38.0 36.8 1.2 1.02 1.01 1.11 0.10 56 10- .9 Present inven- tion 3 350
348 351 3 470 474 472 2 36.3 36.8 36.2 0.6 1.01 1.01 1.09 0.08 51 11- .6 Present inven- tion 4 395 398 404 9 507 506 509 3 36.6 37.5 37.3 0.9 1.09 0.99 1.01 0.10 52 11- .5 Present inven tion 5 392 397 400 8 502 503 501 2 37.9 38.2 38.0 0.3 0.95 1.13 1.00
0.18 51 11- .5 Present inven- tion 6 401 398 407 9 509 509 512 3 37.5 37.9 38.5 1.0 0.94 1.07 1.02 0.13 53 11- .3 Present inven- tion 7 404 401 410 9 510 509 512 3 35.3 36.7 36.6 1.4 1.03 1.18 1.01 0.17 55 11- .0 Present inven tion 8 374 367 374 7 507
505 508 3 29.9 28.4 31.3 2.9 1.17 1.01 1.43 0.42 58 8.- 3 Compa- rative example 9 371 386 380 15 482 491 485 9 27.1 25.0 26.7 2.1 1.14 0.93 1.31 0.38 40 1- 2.0 Compa- rative example 10 395 396 399 4 512  512 515 3 27.0 25.4 28.2 2.8 1.27 0.98 1.28 0.30
58 8- .9 Compa- rative example 11 372 384 380 12 484 489 485 5 37.7 36.9 37.3 0.8 1.24 1.00 1.34 0.34 42 - 12.0 Compa- rative example 12 390 384 377 13 490 500 498 10 29.0 24.9 29.4 4.5 1.19 0.94 1.29 0.35 56- 10.9 Compa- rative example 13 372 383 390 18
480 486 493 13 35.5 33.7 36.5 2.8 1.02 0.96 1.48 0.52 53- 11.3 Compa- rative example 14 404 401 410 9 510 508 513 5 35.1 37.0 36.7 1.9 1.01 1.28 0.94 0.34 52 1- 1.4 Compa- rative example 15 385 386 376 10 503 501 506 5 37.5 36.8 36.4 1.1 1.28 1.00 1.31
0.31 45 - 11.8 Compa- rative example 16 388 389 378 11 504 501 507 6 37.3 36.5 36.0 1.3 1.18 0.98 1.36 0.38 43 - 11.9 Compa- rative example 17 410 406 417 11 513 510 515 5 35.3 36.7 36.5 1.4 1.02 1.26 0.92 0.34 56 - 9.9 Compa- rative example 18 412 406
415 9 514 511 519 8 35.1 36.5 36.3 1.4 0.97 1.22 0.88 0.34 57 9- .4 Compa- rative example 19 322 335 322 13 510 519 514 9 36.1 34.1 35.9 2.0 1.12 0.93 1.36 0.43 43 - 12.0 Compa- rative example
By making a slab containing the chemical composition specified by S65C-CSP of JIS G 4802 (by wt %, C: 0.65%, Si: 0.19%, Mn: 0.73%, P: 0.011%, S: 0.002% and Al: 0.020%) through a continuous casting process, reheating to 1100.degree.  C., hot
rolling, coiling, primarily annealing, cold rolling, secondarily annealing, under the conditions shown in Table 6, and temper rolling at a reduction rate of 1.5%, the steel sheets 20 38 of 2.5 mm thickness were produced.  Herein, the steel sheet 38 is a
conventional high carbon steel sheet.  The same measurements as in Example 2 were conducted.
As to the inventive steel sheets 20 26, the existing condition of carbides is within the range of the present invention, and therefore the HRc after quenching is above 50 and the good hardenability is obtained.  The austenite grain size of these
precision.  At the same time, the .DELTA.max of yield strength and tensile strength is 15 MPa or lower, the .DELTA.max of the total elongation is 1.5% or lower, and thus each planar anisotropy is very small.
In contrast, the comparative steel sheets 27 38 have large .DELTA.max of the mechanical properties.  The steel sheets 27, 29 and 36 have coarse austenite grain size.  In the steel sheets 28 and 38, the HRc is less than 50.
TABLE-US-00006 TABLE 6 Coiling Primary Cold Secondary Number of Ratio of carbides Steel temperature annealing reduction annealing Secondary annealing carbides larger smaller than 0.6 .mu.m sheet (.degree.  C.) (.degree.  C. .times.  hr) rate (%)
(.degree.  C. .times.  hr) range by the formula (1) than 1.5 .mu.m (%) Remark 20 560 640 .times.  40 70 680 .times.  40 640 680 86 86 Present invention 21 530 640 .times.  20 60 680 .times.  40 640 680 82 88 Present invention 22 595 640 .times.  40 60
680 .times.  20 640 680 94 82 Present invention 23 560 660 .times.  40 60 660 .times.  40 628 674 90 83 Present invention 24 560 680 .times.  20 60 640 .times.  40 620 658 92 83 Present invention 25 560 640 .times.  40 50 660 .times.  40 640 680 87 85
Present invention 26 560 640 .times.  40 70 640 .times.  40 640 680 83 86 Present invention 27 510 640 .times.  20 60 680 .times.  40 640 680 44 93 Comparative example 28 610 640 .times.  20 60 680 .times.  20 640 680 101 62 Comparative example 29 560
620 .times.  40 60 680 .times.  40 -- 47 91 Comparative example 30 560 720 .times.  40 60 680 .times.  40 -- 100 64 Comparative example 31 560 640 .times.  15 70 680 .times.  40 640 680 83 87 Comparative example 32 560 640 .times.  40 30 680 .times.  40
640 680 88 85 Comparative example 33 560 660 .times.  20 60 620 .times.  40 630 674 89 84 Comparative example 34 560 640 .times.  20 60 700 .times.  40 640 680 98 72 Comparative example 35 560 640 .times.  40 60 690 .times.  40 640 680 99 70 Comparative
example 36 560 690 .times.  40 60 615 .times.  40 620 650 49 89 Comparative example 37 610 690 .times.  40 50 650 .times.  40 610 650 96 77 Comparative example 38 620 -- 50 690 .times.  40 -- 100 65 Comparative example
TABLE-US-00007 TABLE 7 Hard- Auste- ness tine after Grain Mechanical properties before quenching quench- size Steel Yield strength (MPa) Tensile strength (MPa) Total elongation (%) r-value ing (size sheet L S C .DELTA.max L S C .DELTA.max L S C
.DELTA.max L S C .DELTA.max - (HRc) No.) Remark 20 412 406 413 7 515 518 523 8 34.2 35.7 35.2 1.5 1.04 0.96 0.97 0.08 63 1- 1.2 Present inven- tion 21 422 419 427 8 524 521 526 5 35.1 36.0 34.6 1.4 0.98 1.00 1.06 0.08 64 1- 1.0 Present inven- tion 22 365
360 363 5 480 483 480 3 34.5 35.0 34.1 0.9 0.97 0.98 1.07 0.10 60 1- 1.7 Present inven- tion 23 409 409 416 7 518 514 519 5 34.7 35.7 34.2 1.5 1.02 0.97 0.93 0.09 61 1- 1.6 Present inven- tion 24 405 410 415 10 511 512 512 1 35.8 36.1 36.2 0.4 0.89 1.11
0.94 0.19 60 - 11.6 Present inven- tion 25 416 412 423 11 519 517 523 6 35.4 36.0 36.7 1.3 0.92 1.03 0.95 0.14 62 - 11.4 Present inven- tion 26 417 414 424 10 521 515 524 9 33.4 34.9 34.7 1.5 1.00 1.15 0.98 0.17 63 - 11.1 Present inven- tion 27 385 380
388 8 518 515 518 3 28.2 24.8 28.2 3.4 1.22 0.96 1.28 0.32 66 8- .4 Compa- rative example 28 385 400 395 15 489 500 493 11 25.7 23.2 25.2 2.5 1.15 0.89 1.22 0.33 48- 12.2 Compa- rative example 29 406 410 413 7 519 523 526 7 25.5  24.0 26.7 2.7 1.21 0.97
1.36 0.39 66 9- .0 Compa- rative example 30 384 397 394 13 492 500 496 8 35.8 34.6 35.6 1.2 1.20 0.90 1.18 0.30 50 - 12.1 Compa- rative example 31 405 398 389 16 500 510 511 11 27.1 22.4 27.4 5.0 0.94 1.25 0.97 0.31 64- 11.1 Compa- rative example 32 386
396 406 20 486 497 503 17 33.7 31.9 34.8 2.9 0.81 1.17 0.94 0.36 62- 11.4 Compa- rative example 33 416 412 425 13 521 516 523 7 33.2 35.1 34.8 1.9 1.04 1.32 1.01 0.31 61 - 11.5 Compa- rative example 34 402 391 388 14 512 510 515 5 35.7 34.8 34.3 1.4 1.22
0.97 1.34 0.37 53 - 11.9 Compa- rative example 35 405 395 394 11 514 511 517 6 35.5 34.8 34.1 1.4 1.17 0.88 1.18 0.30 51 - 12.0 Compa- rative example 36 420 417 431 14 523 519 525 6 33.3 34.8 34.5 1.5 1.00 1.26 0.93 0.33 65 - 10.0 Compa- rative example
37 375 363 370 12 482 490 485 8 34.3 35.2 34.0 1.2 1.21 0.93 1.24 0.31 56 - 11.8 Compa- rative example 38 336 350 331 19 517 528 526 11 34.5 32.4 33.8 2.1 1.10 0.83 1.29 0.44 46- 12.4 Compa- rative example
coiling, primarily annealing, cold rolling, secondarily annealing, under the conditions shown in Tables 8 and 9, and temper rolling at a reduction rate of 1.5%, the steel sheets 39 64 of 2.5 mm thickness were produced.  In this example, the reheating of
sheet bar was conducted for some steel sheets.  Herein, the steel sheet 64 is a conventional high carbon steel sheet.  The same measurements as in Example 2 were conducted.  The .DELTA.max of (222) intensity as above mentioned was also measured.
The results are shown in Tables 8 12.
As to the inventive steel sheets 39 52, the existing condition of carbides is within the range of the present invention, and therefore the HRc after quenching is above 50 and the good hardenability is obtained.  The austenite grain size of these
precision.  At the same time, the .DELTA.max of yield strength and tensile strength is 10 MPa or lower, the .DELTA.max of the total elongation is 1.5% or lower, and thus each planar anisotropy is very small.  In particular, the steel sheets 39 45 of
which the sheet bar was reheated have small .DELTA.max of (222) intensity in the thickness direction, and therefore more uniformed structure in the thickness direction.
In contrast, the comparative steel sheets 53 64 have large .DELTA.max of the mechanical properties.  The steel sheets 53, 55, 62 and 63 have coarse austenite grain size.  In the steel sheets 54, 56, 60, 61 and 64, the HRc is less than 50.
TABLE-US-00008 TABLE 8 Coiling Cold Secondary Ratio of carbides Reheating of tempe- Primary reduc- Secondary annealing range Number of smaller than Steel sheet bar rature annealing tion annealing by the formula carbides larger 0.6 .mu.m sheet
(.degree.  C. .times.  sec) (.degree.  C.) (.degree.  C. .times.  hr) rate (%) (.degree.  C. .times.  hr) (1) than 1.5 .mu.m (%) Remark 39 1050 .times.  15 580 640 .times.  40 70 680 .times.  40 632 680 55 86 Present invention 40 1100 .times.  3 530 640
.times.  20 60 680 .times.  40 632 680 52 87 Present invention 41 950 .times.  3 595 640 .times.  40 60 680 .times.  20 632 680 64 81 Present invention 42 1050 .times.  15 580 660 .times.  40 60 660 .times.  40 620 680 60 84 Present invention 43 1050
.times.  15 580 680 .times.  20 60 640 .times.  40 620 666 62 82 Present invention 44 1050 .times.  15 580 640 .times.  40 50 660 .times.  40 632 680 56 85 Present invention 45 1050 .times.  15 580 640 .times.  40 70 640 .times.  40 632 680 54 86 Present
invention 46 -- 580 640 .times.  40 70 680 .times.  40 632 680 56 85 Present invention 47 -- 530 640 .times.  20 60 680 .times.  40 632 680 53 86 Present invention 48 -- 595 640 .times.  40 60 680 .times.  20 632 680 64 81 Present invention 49 -- 580 660
.times.  40 60 660 .times.  40 620 680 61 83 Present invention 50 -- 580 680 .times.  20 60 640 .times.  40 620 666 63 82 Present invention 51 -- 580 640 .times.  40 50 660 .times.  40 632 680 56 85 Present invention 52 -- 580 640 .times.  40 70 640
.times.  40 632 680 55 85 Present invention 53 1050 .times.  15 510 640 .times.  20 60 680 .times.  40 632 680 30 92 Comparative example 54 1100 .times.  3 610 640 .times.  20 60 680 .times.  20 632 680 67 61 Comparative example 55 950 .times.  3 580 620
.times.  40 60 680 .times.  40 -- 32 89 Comparative example 56 1050 .times.  15 580 720 .times.  40 60 680 .times.  40 -- 68 65 Comparative example 57 1050 .times.  15 580 640 .times.  15 70 680 .times.  40 632 680 55 86 Comparative example 58 1050
.times.  15 580 640 .times.  40 30 680 .times.  40 632 680 58 84 Comparative example 59 1050 .times.  15 580 660 .times.  20 60 610 .times.  40 620 680 60 84 Comparative example 60 1050 .times.  15 580 640 .times.  20 60 700 .times.  40 632 680 66 74
Comparative example 61 1050 .times.  15 580 640 .times.  40 60 690 .times.  40 632 680 66 70 Comparative example 62 1050 .times.  15 580 690 .times.  40 60 615 .times.  40 620 658 33 88 Comparative example 63 1050 .times.  15 520 640 .times.  20 60 640
.times.  20 632 680 45 88 Comparative example 64 1050 .times.  15 620 -- 50 690 .times.  40 -- 33 87 Comparative example
TABLE-US-00009 TABLE 9 Secondary Reheating of Coiling Primary Cold Secondary annealing range Number of Ratio of carbides Steel sheet bar temperature annealing reduction annealing by the formula carbides larger smaller than 0.6 sheet (.degree.
C. .times.  sec) (.degree.  C.) (.degree.  C. .times.  hr) rate (%) (.degree.  C. .times.  hr) (l) than 1.5 .mu.m .mu.m (%) Remark 52 -- 580 640 .times.  40 70 640 .times.  40 632 680 55 85 Present invention 53 1050 .times.  15 510 640 .times.  20 60 680
.times.  40 632 680 30 92 Comparative example 54 1100 .times.  3 610 640 .times.  20 60 680 .times.  20 632 680 67 61 Comparative example 55 950 .times.  3 580 620 .times.  40 60 680 .times.  40 -- 32 89 Comparative example 56 1050 .times.  15 580 720
.times.  40 60 680 .times.  40 -- 68 65 Comparative example 57 1050 .times.  15 580 640 .times.  15 70 680 .times.  40 632 680 55 86 Comparative example 58 1050 .times.  15 580 640 .times.  40 30 680 .times.  40 632 680 58 84 Comparative example 59 1050
.times.  15 580 660 .times.  20 60 610 .times.  40 620 680 60 84 Comparative example 60 1050 .times.  15 580 640 .times.  20 60 700 .times.  40 632 680 66 74 Comparative example 61 1050 .times.  15 580 640 .times.  40 60 690 .times.  40 632 680 66 70
Comparative example 62 1050 .times.  15 580 690 .times.  40 60 615 .times.  40 620 658 33 88 Comparative example 63 1050 .times.  15 520 640 .times.  20 60 640 .times.  20 632 680 45 88 Comparative example 64 1050 .times.  15 620 -- 50 690 .times.  40 --
33 87 Comparative example
TABLE-US-00010 TABLE 10 Hard- Auste- ness tine after grain Mechanical properties before quenching quench- size Steel Yield strength (MPa) Tensile strength (MPa) Total elongation (%) r-value ing (size sheet L S C .DELTA.max L S C .DELTA.max L S C
.DELTA.max L S C .DELTA.max (HRc) No.) Remark 39 398 394 398 4 506 508 512 6 36.5 37.4 37.0 0.9 1.07 0.99 1.02 0.08 55 1- 1.0 Present inven- tion 40 410 407 410 3 514 512 516 4 36.8 37.7 36.8 0.9 1.04 1.01 1.11 0.10 56 1- 0.9 Present inven- tion 41 351
348 350 3 470 474 473 4 36.4 36.8 36.2 0.6 1.03 1.01 1.09 0.08 51 1- 1.6 Present inven- tion 42 395 398 400 5 508 506 509 3 36.8 37.5 37.3 0.7 1.09 0.99 1.02 0.10 53 1- 1.4 Present inven- tion 43 395 397 400 5 501 503 501 2 37.9 38.2 38.1 0.3 0.95 1.09
1.00 0.14 52 1- 1.4 Present inven- tion 44 401 399 404 5 509 510 512 3 37.7 37.9 38.5 0.8 0.94 1.07 1.04 0.13 53 1- 1.3 Present inven- tion 45 404 401 405 4 511 509 512 3 35.7 36.7 36.6 1.0 1.03 1.15 1.01 0.14 55 1- 1.0 Present inven- tion 46 397 394 402
8 506 508 513 7 36.2 37.4 37.1 1.2 1.14 0.99 1.00 0.15 54 1- 1.1 Present inven- tion 47 409 407 412 5 514 512 516 4 36.8 38.0 36.9 1.2 1.02 1.01 1.14 0.16 55 1- 1.0 Present inven- tion 48 351 348 351 3 470  474 469 5 36.4 36.8 36.2 0.6 1.01 0.98 1.13
0.15 51 1- 1.8 Present inven- tion 49 395 397 404 9 507 505 509 4 36.6 37.5 37.2 0.9 1.13 0.96 1.01 0.17 52 1- 1.5 Present inven- tion 50 392 396 400 8 502 505 501 4 37.2 38.2 38.0 1.0 0.95 1.14 1.00 0.19 51 1- 1.5 Present inven- tion 51 403 398 407 9
509 505 512 3 37.5 37.7 38.5 1.0 0.94 1.12 1.02 0.18 53 1- 1.3 Present inven- tion
TABLE-US-00011 TABLE 11 Hard- Auste- ness tine after grain Mechanical properties before quenching quench- size Steel Yield strength (MPa) Tensile strength (MPa) Total elongation (%) r-value ing (size sheet L S C .DELTA.max L S C .DELTA.max L S C
.DELTA.max L S C .DELTA.max (HRc) No.) Remark 52 405 401 410 9 510 507 512 5 35.3 36.7 36.4 1.4 1.03 1.19 1.00 0.19 54 1- 1.1 Present inven- tion 53 372 364 374 10 507 503 508 5 29.8 28.4 31.3 2.9 1.26 1.02 1.37 0.35 58 - 8.3 Com- parative example 54 371
386 379 15 482 491 484 9 27.1 25.0 26.3 2.1 1.27 0.98 1.27 0.29 41 - 12.0 Com- parative example 55 392 396 399 7 512 509 515 6 27.2 25.4 28.2 2.8 1.33 1.04 1.38 0.32 58 9- .0 Com- parative example 56 372 385 380 13 484 489 486 5 37.7 36.6 37.3 1.1 1.23
0.95 1.25 0.30 42 - 12.0 Com- parative example 57 390 384 378 12 490 500 497 10 28.8 24.9 29.4 4.5 1.16 0.89 1.20 0.31 55- 10.9 Com- parative example 58 372 385 390 18 480 487 493 13 35.4 33.7 36.5 2.8 0.88 1.19 0.91 0.31 53- 11.3 Com- parative example
59 405 401 410 9 510 506 513 7 35.1 37.0 36.6 1.9 1.01 1.27 0.94 0.33 52 1- 1.4 Com- parative example 60 383 386 376 10 504 501 506 5 37.5 36.9 36.4 1.1 1.18 0.94 1.29 0.35 45 - 11.7 Com- parative example 61 387 389 378 11 503 501 507 6 37.3 36.6 36.0
1.3 1.16 1.00 1.45 0.45 44 - 11.9 Com- parative example 62 410 404 417 13 513 507 515 8 35.3 36.7 36.1 1.4 0.87 1.17 0.88 0.29 56 - 9.9 Com- parative example 63 411 406 415 9 515 511 515 8 35.1 38.5 36.0 1.4 1.02 1.32 1.00 0.32 57 9- .4 Com- parative
example 64 323 335 322 13 510 519 513 9 36.1 34.1 35.5 2.0 1.10 0.93 1.35 0.40 43 - 12.0 Com- parative example
TABLE-US-00012 TABLE 12 Integrated reflective intensity (222) Steel 1/4 1/2 sheet Surface thickness thickness .DELTA.  max Remark 39 2.80 2.79 2.90 0.11 Present invention 40 2.85 2.92 3.00 0.15 Present invention 41 2.87 2.93 3.00 0.13 Present
invention 42 2.72 2.80 2.84 0.12 Present invention 43 2.54 2.60 2.66 0.12 Present invention 44 2.85 2.93 2.99 0.14 Present invention 45 2.88 3.01 2.95 0.13 Present invention 46 2.75 2.90 3.03 0.28 Present invention 47 2.77 3.06 2.98 0.29 Present
invention 48 2.79 2.74 3.02 0.28 Present invention 49 2.65 2.77 2.90 0.25 Present invention 50 2.48 2.58 2.75 0.27 Present invention 51 2.80 3.02 2.97 0.22 Present invention 52 2.83 2.80 3.04 0.24 Present invention 53 2.81 2.88 2.96 0.15 Comparative
example 54 2.84 2.87 2.98 0.14 Comparative example 55 2.90 3.04 2.99 0.14 Comparative example 56 2.20 2.28 2.32 0.12 Comparative example 57 2.82 2.93 2.91 0.11 Comparative example 58 2.83 2.90 2.98 0.15 Comparative example 59 2.73 2.79 2.86 0.13
Comparative example 60 2.85 2.92 3.00 0.15 Comparative example 61 2.82 2.96 2.93 0.14 Comparative example 62 2.38 2.42 2.53 0.15 Comparative example 63 2.83 2.88 2.96 0.13 Comparative example 64 2.33 2.39 2.48 0.15 Comparative example
rolling, coiling, primarily annealing, cold rolling, secondarily annealing, under the conditions shown in Tables 13 and 14, and temper rolling at a reduction rate of 1.5%, the steel sheets 65 90 of 2.5 mm thickness were produced.  In this example, the
reheating of sheet bar was conducted for some steel sheets.  Herein, the steel sheet 90 is a conventional high carbon steel sheet.  The same measurements as in Example 4 were conducted.
The results are shown in Tables 13 17.
As to the inventive steel sheets 65 78, the existing condition of carbides is within the range of the present invention, and therefore the HRc after quenching is above 50 and the good hardenability is obtained.  The austenite grain size of these
precision.  At the same time, the .DELTA.max of yield strength and tensile strength is 15 MPa or lower, the .DELTA.max of the total elongation is 1.5% or lower, and thus each planar anisotropy is very small.  In particular, the steel sheets 65 71 of
In contrast, the comparative steel sheets 79 90 have large .DELTA.max of the mechanical properties.  The steel sheets 79, 81 and 88 have coarse austenite grain size.  In the steel sheet 80, the HRc is less than 50.
TABLE-US-00013 TABLE 13 Secondary Reheating of Coiling Primary Cold Secondary annealing range Number of Ratio of carbides Steel sheet bar temperature annealing reduction annealing by the formula carbides larger smaller than 0.6 sheet (.degree.
C. .times.  sec) (.degree.  C.) (.degree.  C. .times.  hr) rate (%) (.degree.  C. .times.  hr) (l) than 1.5 .mu.m .mu.m (%) Remark 65 1050 .times.  15 580 640 .times.  40 70 680 .times.  40 632 680 85 87 Present invention 66 1100 .times.  3 530 640
.times.  20 60 680 .times.  40 632 680 82 88 Present invention 67 950 .times.  3 595 640 .times.  40 60 680 .times.  20 632 680 94 82 Present invention 68 1050 .times.  15 560 660 .times.  40 60 660 .times.  40 620 680 89 84 Present invention 69 1050
.times.  15 560 680 .times.  20 60 640 .times.  40 620 666 91 83 Present invention 70 1050 .times.  15 560 640 .times.  40 50 660 .times.  40 632 680 87 85 Present invention 71 1050 .times.  15 560 640 .times.  40 70 640 .times.  40 632 680 83 86 Present
invention 72 -- 560 640 .times.  40 70 680 .times.  40 632 680 86 86 Present invention 73 -- 530 640 .times.  20 60 680 .times.  40 632 680 83 87 Present invention 74 -- 595 640 .times.  40 60 680 .times.  20 632 680 94 82 Present invention 75 -- 560 660
.times.  40 60 660 .times.  40 620 680 90 83 Present invention 76 -- 560 680 .times.  20 60 640 .times.  40 620 686 92 83 Present invention 77 -- 560 640 .times.  40 50 660 .times.  40 632 680 87 85 Present invention
TABLE-US-00014 TABLE 14 Secondary Reheating of Coiling Primary Cold Secondary annealing range Number of Ratio of carbides Steel sheet bar temperature annealing reduction annealing by the formula carbides larger smaller than 0.6 sheet (.degree.
C. .times.  sec) (.degree.  C.) (.degree.  C. .times.  hr) rate (%) (.degree.  C. .times.  hr) (l) than 1.5 .mu.m .mu.m (%) Remark 78 -- 560 640 .times.  40 70 640 .times.  40 632 680 84 85 Present invention 79 1050 .times.  15 510 640 .times.  20 60 680
.times.  40 632 680 44 93 Comparative example 80 1100 .times.  3 610 640 .times.  20 60 680 .times.  20 632 680 100 62 Comparative example 81 950 .times.  3 560 620 .times.  40 60 680 .times.  40 -- 47 90 Comparative example 82 1050 .times.  15 560 720
.times.  40 60 680 .times.  40 -- 100 64 Comparative example 83 1050 .times.  15 560 640 .times.  15 70 680 .times.  40 632 680 84 87 Comparative example 84 1050 .times.  15 560 640 .times.  40 30 680 .times.  40 632 680 88 85 Comparative example 85 1050
.times.  15 560 660 .times.  20 60 610 .times.  40 620 680 89 84 Comparative example 86 1050 .times.  15 560 640 .times.  20 60 700 .times.  40 632 680 98 73 Comparative example 87 1050 .times.  15 560 640 .times.  40 60 690 .times.  40 632 680 98 70
Comparative example 88 1050 .times.  15 560 690 .times.  40 60 615 .times.  40 620 680 49 89 Comparative example 89 1050 .times.  15 600 690 .times.  20 50 650 .times.  40 632 680 96 77 Comparative example 90 1050 .times.  15 610 -- 50 690 .times.  40 --
99 71 Comparative example
TABLE-US-00015 TABLE 15 Hard- Auste- ness tine after Grain Mechanical properties before quenching quench- size Steel Yield strength (MPa) Tensile strength (MPa) Total elongation (%) r-value ing (size sheet L S C .DELTA.max L S C .DELTA.max L S C
.DELTA.max L S C .DELTA.max (HRc) No.) Remark 65 412 406 412 6 515 518 521 6 34.7 35.7 35.2 1.0 1.04 0.96 0.98 0.08 64 1- 1.1 Present inven- tion 66 422 419 424 5 523 521 526 5 35.1 36.0 35.1 0.9 0.98 1.02 1.06 0.08 64 1- 1.0 Present inven- tion 67 364
360 363 4 480 483 481 3 34.5 35.0 34.3 0.7 0.97 0.99 1.07 0.10 60 1- 1.7 Present inven- tion 68 409 409 415 6 517 514 519 5 34.7 35.7 34.7 1.0 1.02 0.96 0.93 0.09 62 1- 1.5 Present inven- tion 69 405 410 412 7 511 511 512 1 35.8 36.0 36.2 0.4 0.92 1.06
0.94 0.14 61 1- 1.5 Present inven- tion 70 416 412 421 9 520 517 523 6 35.9 36.0 36.7 0.8 0.89 1.03 0.96 0.14 62 1- 1.4 Present inven- tion 71 417 414 421 7 521 515 521 6 33.9 34.9 34.7 1.0 1.00 1.12 0.98 0.14 63 1- 1.1 Present inven- tion 72 411 406 413
7 515 519 523 8 34.2 35.7 35.3 1.5 1.08 0.93 0.97 0.15 63 1- 1.2 Present inven- tion 73 423 419 427 8 523 521 526 5 35.3 36.0 34.6 1.4 0.94 1.00 1.10 0.16 63 1- 1.1 Present inven- tion 74 365 360 362 5 479  483 480 4 34.6 35.0 34.1 0.9 0.95 0.98 1.12
0.17 60 1- 1.7 Present inven- tion 75 410 409 416 7 517 514 519 5 34.6 35.7 34.2 1.5 1.07 0.97 0.91 0.16 61 1- 1.6 Present inven- tion 76 405 408 415 10 511 512 514 3 35.4 36.1 36.6 1.2 0.92 1.11 0.95 0.19 60 - 11.6 Present inven- tion 77 417 412 423 11
518 517 523 6 35.4 36.1 36.7 1.3 0.89 1.07 0.95 0.18 62 - 11.4 Present inven- tion
TABLE-US-00016 TABLE 16 Hard- Auste- ness tine after grain Mechanical properties before quenching quench- size Steel Yield strength (MPa) Tensile strength (MPa) Total elongation (%) r-value ing (size sheet L S C .DELTA.max L S C .DELTA.max L S C
.DELTA.max L S C .DELTA.max (HRc) No.) Remark 78 418 414 424 10 520 515 524 9 33.4 34.9 34.5 1.5 1.00 1.17 0.98 0.19 62 - 11.2 Present inven- tion 79 385 380 390 10 518 515 520 5 28.0 24.8 28.2 3.4 1.18 0.92 1.25 0.33 66 - 8.4 Com- parative example 80
385 400 394 15 489 500 494 11 25.7 23.2 25.0 2.5 1.12 0.88 1.22 0.34 49- 12.2 Com- parative example 81 406 410 415 9 519 522 526 7 25.3 24.0 26.7 2.7 1.18 1.01 1.42 0.41 66 9- .1 Com- parative example 82 384 397 392 13 492 500 497 8 35.8 34.3 35.6 1.5
1.18 0.93 1.32 0.39 50 - 12.1 Com- parative example 83 405 397 389 16 500 509 511 11 27.0 22.4 27.4 5.0 1.24 0.90 1.27 0.37 63- 11.1 Com- parative example 84 386 398 406 20 486 496 503 17 33.4 31.9 34.8 2.9 0.81 1.16 0.93 0.35 62- 11.4 Com- parative
example 85 418 412 425 13 521 516 524 8 33.2 35.1 34.5 1.9 1.02 1.23 0.86 0.37 61 - 11.5 Com- parative example 86 402 393 388 14 512 509 515 6 35.7 34.9 34.3 1.4 1.24 0.95 1.25 0.30 53 - 11.8 Com- parative example 87 406 395 394 12 514 510 517 7 35.5
34.7 34.1 1.4 1.11  0.86 1.19 0.33 52 - 12.0 Com- parative example 88 421 417 431 14 523 518 525 7 33.3 34.8 34.3 1.5 1.00 1.26 0.92 0.34 65 - 10.0 Com- parative example 89 375 363 369 12 482 490 486 8 34.3 35.4 34.0 1.4 1.17 0.99 1.40 0.41 58 - 11.8
Com- parative example 90 338 350 331 19 517 528 524 11 34.5 32.4 33.6 2.1 1.13 0.83 1.29 0.42 54- 11.9 Com- parative example
TABLE-US-00017 TABLE 17 Integrated reflective intensity (222) Steel 1/4 1/2 sheet Surface thickness thickness .DELTA.  max Remark 65 2.87 2.82 2.97 0.15 Present invention 68 2.83 2.86 2.94 0.11 Present invention 67 2.85 2.90 2.97 0.12 Present
invention 68 2.75 2.81 2.86 0.11 Present invention 69 2.58 2.64 2.71 0.13 Present invention 70 2.84 2.91 2.96 0.12 Present invention 71 2.85 2.99 2.95 0.14 Present invention 72 2.73 2.85 3.02 0.29 Present invention 73 2.76 3.03 2.97 0.27 Present
invention 74 2.78 2.92 3.04 0.26 Present invention 75 2.69 2.82 2.96 0.27 Present invention 76 2.50 2.64 2.75 0.25 Present invention 77 2.81 3.03 2.99 0.22 Present invention 78 2.79 2.87 3.03 0.24 Present invention 79 2.83 2.87 2.96 0.13 Comparative
example 80 2.84 2.88 2.99 0.15 Comparative example 81 2.92 3.03 2.95 0.11 Comparative example 82 2.22 2.26 2.34 0.12 Comparative example 83 2.85 2.97 2.92 0.12 Comparative example 84 2.88 2.94 3.02 0.14 Comparative example 85 2.73 2.75 2.87 0.14
Comparative example 86 2.84 2.87 2.99 0.15 Comparative example 87 2.86 3.01 2.92 0.15 Comparative example 88 2.40 2.42 2.54 0.14 Comparative example 89 2.89 2.98 3.04 0.15 Comparative example 90 2.37 2.40 2.50 0.13 Comparative example
"High Carbon Steel And Production Method Thereof - Patent 7147730"
http://img.docstoccdn.com/thumb/206/31467171.png
CARBON STEEL _ HSLA STEEL
Carbon Steel Plate _Injury_
Stainless Steel Description of Production Services
GALVANIZED CARBON STEEL _ GALVANIZED HSLA STEEL
PRODUCTION AND PROPERTIES OF HIGH-STRENGTH NICKEL-ALLOY STEEL Reactions in the production of high-carbon ferromanganese from Top Documents