Low carbon microalloyed steel

Information

  • Patent Grant
  • 7727342
  • Patent Number
    7,727,342
  • Date Filed
    Wednesday, February 12, 2003
    21 years ago
  • Date Issued
    Tuesday, June 1, 2010
    14 years ago
Abstract
A low carbon microalloyed steel, comprising in weight % about: 0.05-0.30 C; 0.5-1.5 Mn; 0.04 max S; 0.025 max P; 1.0 max Si; 0.5-2.0 Ni; 0.05-0.30 V; 0-2.0 Cu; up to 0.0250 N; up to 0.2 Cb; up to 0.3 Cr; up to about 0.15 Mo; up to about 0.05 Al; balance Fe and minor additions and impurities. The steel has a carbon equivalent value, C.E., ranging between 0.3-0.65, calculated by the formula: C.E.=C+Mn+Si+Cu+Ni+Cr+Mo+V+Cb 6 15 5.
Description
BACKGROUND OF THE INVENTION

The present invention relates generally to the metallurgy of steel and, more particularly, to low carbon microalloyed steel compositions. It is common practice to use conventional microalloyed steels in various applications for bars and tubular products. However, there are needs for stronger and tougher microalloyed steels in a number of different applications such as, for example, in communication towers and hub assemblies.


SUMMARY OF THE INVENTION

The steels of the present invention are much more weldable and tougher than conventional microalloyed steels. The present invention is directed to an alloy broadly comprising in wt. %, about 0.05-0.30 C; up to 1.5 Mn; 1.0 max Si; 0.5-2 Ni; 0.05-0.3 V; up to 2 Cu; 10-250 ppm N; balance Fe and other minor additions and impurities.





BRIEF DESCRIPTION OF THE DRAWING


FIG. 1 is a graph schematically showing the relationship between the precipitation strengthening factor (ΔYSp) and the Ar3 temperature in the steels of the present invention.





DETAILED DESCRIPTION OF THE INVENTION

The family of microalloyed steels of the present invention provide better weldability and much higher impact toughness and tensile ductility than conventional microalloyed steels. A critical factor in the design of microalloyed ferrite pearlite steels is the extent to which precipitation strengthening supplements the base strength provided by solid solution and grain refinement. It is known that this precipitation strengthening factor, referred to as ΔYSp, is controlled by the ferrite transformation temperature, Ar3, all other things being equal. As the Ar3 temperature is lowered, ΔYSp increases up to a maximum and then decreases as a result of precipitation suppression through the usual kinetic limitations at lower temperatures. This relationship is graphically depicted in FIG. 1. The essential design factor for high strength involving precipitation is to adjust Ar3 by compositional means to allow this maximum to be obtained. Either under (lean) or over (rich) adjustment of the chemistry of the alloy may lead to underutilization of precipitation. Accordingly, two factors must be considered in order to optimize the precipitation according to the invention. The first factor is whether the base composition is too close to the critical limit for formation of bainite such that any further increase in either Mn or Ni (both lower the Ar3 temperature) causes unwanted bainite formation. The second factor is that for a given Ar3 temperature, Mn is less potent than Ni in that it suppresses precipitation. Thus, the invention requires the Mn levels to be below 1.5 wt. % and that the Ar3 temperature be controlled with elements which have a low tendency for forming bainite.


Consideration of these requirements shows that out of all the common alloying elements, Ni is the most effective. The results of a study to examine the effect of Ni on ΔYSp showed that 45 ksi minimum yield strength and as high as 80 ksi was possible for large bars or tubular products. The results are given in the following tables.


One presently preferred alloy composition according to the present invention contains in % by weight: 0.05-0.30 C, 0.5-1.5 Mn; 1.0 max Si; 0.5-2.0 Ni; 0.05-0.30 V; 0-2.0 Cu; 0.0050-0.0250 N; balance Fe and other minor additions and impurities. The S level is 0.04 wt. % max and preferably about 0.035 wt. % max. The P content is 0.025 wt. % max and preferably about 0.02 wt. % max. In the above composition, the C and N contents may preferably be 0.05-0.15 wt. % C and 0.0010-0.0250 wt. % N.


A further presently preferred embodiment of the present invention includes the alloy composition set forth above, also containing about 0.25-2.0 wt. % Cu. Copper in these microalloyed steels will form as ε-copper particles by both interphase precipitation and the normal nucleation and growth process, thus increasing strength by increasing ΔYSp, and maintaining high levels of toughness and tensile ductility as seen in Tables III and IV.


The alloy may also contain additional constituents such as Cr, Mo, Cb and Al, for example, 0.05-0.3 Cr, up to about 0.15 Mo, up to about 0.2 Cb, up to about 0.05 Al, and more preferably about 0.01-0.03 Al.









TABLE I







Chemical Compositions




















Heat















No.
C
Mn
P
S
Si
Cr
Ni
Mo
Cu
Al
V
N(ppm)
C.E.*























2032
0.08
0.52
0.005
0.004
0.25
0.12
1.03
0.03
0.01
0.022
0.144
103
0.34


2033
0.14
0.53
0.004
0.004
0.26
0.12
1.03
0.03
0.01
0.026
0.146
106
0.40


2034
0.07
0.52
0.004
0.004
0.27
0.11
1.03
0.03
0.01
0.026
0.152
20
0.33


2035
0.13
0.52
0.004
0.004
0.26
0.11
1.05
0.03
0.01
0.026
0.138
20
0.39


2036
0.07
0.98
0.005
0.004
0.25
0.11
1.04
0.03
0.01
0.021
0.143
107
0.40


2037
0.14
1.02
0.005
0.004
0.26
0.12
1.03
0.03
0.01
0.024
0.140
112
0.48


2057
0.06
1.03
0.004
0.005
0.26
0.12
1.03
0.03
0.01
0.025
0.146
174
0.40


2058
0.11
1.04
0.004
0.005
0.28
0.12
1.04
0.04
0.01
0.017
0.150
164
0.46


2059
0.08
1.06
0.004
0.005
0.26
0.12
1.54
0.03
0.01
0.023
0.131
186
0.46


2060
0.13
1.03
0.004
0.005
0.25
0.12
1.52
0.03
0.01
0.023
0.148
187
0.51


2061
0.07
1.03
0.004
0.005
0.27
0.12
1.04
0.03
0.01
0.024
0.249
184
0.44


2062
0.12
1.03
0.004
0.005
0.26
0.12
1.03
0.03
0.01
0.029
0.250
176
0.48


2063
0.08
1.02
0.004
0.006
0.26
0.12
1.03
0.03
0.50
0.025
0.152
180
0.46


2135
0.16
1.04
0.004
0.004
0.26
0.14
1.5
0.03
0.01
0.028
0.138
166
0.54


2136
0.26
1.00
0.003
0.004
0.26
0.13
1.5
0.03
0.01
0.028
0.137
170
0.63


2137
0.19
1.00
0.004
0.004
0.26
0.14
0.98
0.03
0.01
0.025
0.227
168
0.55


2138
0.28
1.00
0.004
0.003
0.26
0.14
0.96
0.03
0.01
0.028
0.218
156
0.63















*

C
.
E
.


=

C
+


Mn
+
Si

6

+


Cu
+
Ni

15

+


Cr
+
Mo
+
V
+
Cb

5



















TABLE II





Rolling Schedule
















(1)
All billets had a 2250° F. soak


(2)
Rolling Sequence:











Pass No.
Reduction (Inches)




1
2.625-2.000



2
2.000-1.750



3
1.750-1.500



4
1.500-1.250



5
 1.25-1.000



6
Cross Roll to Straighten Plate (No reduction)








(3)
Finish Rolling Temperature (approximately 1950° F. to 2000° F.)


(4)
No designation after heat number: Air cooled



“S” designation after heat number: Sand cooled to simulate the



mid-radius position of a 6-inch bar
















TABLE III







Tensile Properties and Hardness














Ultimate






Yield Strength
Tensile
Elongation
R.A.
Hardness


Heat No.
(0.2% offset) (ksi)
Strength (ksi)
(Percent in 1.4″)
(Percent)
(RB)















2032
54.6
70.3
32.0
77.1
81


2032 S
47.7
64.6
32.7
74.7
74


2033
61.3
80.8
28.9
70.6
87


2033 S
51.4
73.1
28.6
67.4
81


2034
50.2
68.3
31.1
76.9
80


2034 S
46.4
65.2
33.1
77.5
74


2035
56.4
79.2
27.8
71.1
86


2035 S
48.2
70.3
30.4
69.7
79


2036
61.9
79.7
28.2
77.1
87


2036 S
52.2
74.3
28.9
77.2
82


2037
70.3
90.8
28.4
72.1
92


2037 S
62.3
83.6
29.9
70.6
88


2057
64.8
84.9
28.0
75.8
91


2057 S
56.8
76.0
30.5
74.4
85


2058
68.3
87.4
28.4
74.2
92


2058 S
60.1
80.6
28.4
73.7
87


2059
71.0
95.1
26.1
72.9
95


2059 S
66.4
87.0
27.8
74.0
92


2060
75.6
101.6
24.4
68.3
98


2060 S
70.3
95.6
24.1
67.2
95


2061
69.8
90.6
26.2
75.3
94


2061 S
60.8
79.6
27.1
75.6
88


2062
74.8
100.2
23.8
65.5
97


2062 S
67.4
90.4
24.2
65.7
94


2063
70.8
90.8
26.6
71.8
93


2063 S
65.5
84.8
28.1
72.6
90


2135
80.3
109.7
23.5
67.9
98


2135 S
72.7
100.2
25.1
67.3
94


2136
89.2
129.2
20.3
53.7
103


2136 S
82.6
116.4
21.2
55.8
99


2137
89.2
118.3
21
54.7
100


2137 S
74.3
103.5
22.6
57.3
96


2138
103
136.7
15.9
39.5
104


2138 S
82.7
117.8
17.9
47.6
100
















TABLE IV





Impact Toughness


Charpy V-notch Impact Toughness (ft-lbs)


Test Temperature





















Heat No.
+40° F.
0° F.
−20° F.
−60° F.







2031
264.0
106.0
9.5
5.0





13.0
11.0




2032 S

262.0
20.0
8.0





260.0
113.0
7.5



2033
 79.5
10.5
10.5





 15.5
25.5
5.0




2033 S
 81.0
26.5
9.0





102.0
51.5
11.0




2034
270.0
7.0
6.5
3.0






5.5




2034 S
266.0
12.5
6.0
3.5





8.0
9.0




2035
 14.5
9.0
8.0





 9.0
12.0
3.5




2035 S
 10.0
9.0
5.5





 31.0
8.5
6.0




2036
 97.5
7.0
10.0





222.0
112.0
6.0




2036 S

280.0
160.0
4.0






8.0
9.5



2037
 68.5
57.5
44.0





 92.5
37.0
56.5




2037 S
110.0
81.5
91.5





121.0
90.0
70.0




2057
 84.5
107.5
7.5
5.0





108.0
53.0
23.0



2057 S
219.0
153.0
124.0
2.5






77.5
53.0



2058
112.0
84.5
53.5
9.5





57.0
43.0
16.0



2058 S
144.0
95.0
104.0
41.5





102.5
75.5
6.0



2059
 59.0
6.5
26.5
4.0






41.0
3.0



2059 S
107.0
88.5
49.5
9.5





81.0
51.5
7.0



2060
 32.5
8.5
6.0
2.0





29.5
6.0
4.5



2061
 45.5
24.5
24.5
5.0





14.5
6.0
8.0



2061 S
125.0
103.5
60.0
6.0





92.0
19.0
8.5



2062
 11.0
11.0
12.0
3.5





25.0
10.5
3.5



2062 S
 26.0
7.5
2.5
3.0





37.0
5.0
11.5



2063
 63.0
16.5
18.0
22.5





17.5
16.0
7.5



2063 S
127.0
115.0
74.5
57.5





76.5
52.5
7.5
















Heat No.
+250° F.
+205° F.
+150° F.
+68° F.
+32° F.





2135

75.5
48.5
24.5
19.0





66.0
18.5
7.0






30.5



2135 S

94.5
74.5
51.5
52.5





83.0
43.0
34.0






60.0



2136
 48.0
28.0
24.0
12.5





21.5
20.0
8.0







15.0



2136 S
 57.0
37.5
27.5
20.0





39.0
24.5
20.5







18.5



2137
 49.5
28.5
25.5
6.0





31.5
18.0
10.0







13.5



2137 S
 49.5
55.5
37.0
26.0





36.0
42.5
11.5







19.0



2138
 20.5
18.5
12.0
7.0




 23.0
13.5
14.0
10.0




 20.0


8.0



2138 S
 36.5
24.5
20.5
5.0




 31.5
24.0
21.0
9.5







8.0










The “C.E.” or carbon equivalent values reported in Table I may broadly range between 0.3 and 0.65 but, more preferably, are controlled within a range of 0.3 to 0.55 and, still more preferably, controlled within a range of 0.4-0.5 to ensure superior physical properties. The C.E. value of an alloy is calculated using the following formula:







C
.
E
.

=

C
+


Mn




+
Si

6

+


Cu
+
Ni


15






+


Cr
+
Mo
+
V
+
Cb

5







Various alloy compositions of the present invention are set forth in Table I which also includes the calculated C.E. values for each. Table II describes the rolling schedule for each of the steel alloy heats made from the compositions of Table I. It will be noted that the billets were either air cooled after completion of rolling or they were sand cooled to simulate the mid-radius position of a large diameter bar of, for example, a 6-inch diameter bar. These sand cooled rolled heats have an “S” designation in Tables III and IV while the rolled heats that, were air cooled have no letter designation in the tables.


While specific embodiments of the invention have been described in detail, it will be appreciated by those skilled in the art that various modifications and alternatives to those details could be developed in light of the overall teachings of the disclosure. The presently preferred embodiments described herein are meant to be illustrative only and not limiting as to the scope of the invention which is to be given the full breadth of the appended claims and any and all equivalents thereof.

Claims
  • 1. A low carbon microalloyed steel tube or bar, in a hot rolled and air cooled condition having a microstructure consisting precipitation strengthened ferrite and pearlite, said steel consisting essentially of in weight %: 0.06-0.30 C; 0.5-1.5 Mn; 0.04 max S; 0.025 max P; 1.0 max Si; >1.0-2.0 Ni; 0.05-0.30 V; 0.01-2.0 Cu; 0.0010-0.0250 N; up to 0.2 Cb; 0.05-0.3 Cr; up to 0.15 Mo; 0.01-0.03 Al; balance Fe and minor additions and impurities, and wherein said steel has a carbon equivalent value, C.E., ranging between 0.3-0.55, calculated by the formula:
  • 2. The steel of claim 1 containing 0.25-2.0 Cu.
  • 3. The steel of claim 1 containing >0.1-0.30 V.
  • 4. The steel of claim 1 containing 0.06-0.15 C.
  • 5. The steel of claim 1 in the form of a bar or tubular shape having a minimum yield strength of 45-80 ksi.
  • 6. The steel of claim 5 having a minimum yield strength of 65 ksi.
  • 7. A hot rolled and air cooled low carbon microalloyed steel in the form of a bar or tubular shape having a minimum yield strength of between 45-80 ksi and having a microstructure consisting of precipitation strengthened ferrite and pearlite, said steel consisting essentially of in weight %: 0.06-0.30 C; 0.5-1.5 Mn; 1.0 max Si; 0.04 max S; 0.025 max P; >1.0-2.0 Ni; >0.1-0.3 V; 0.01-2.0 Cu; 10-250 ppm N; up to 0.2 Cb; 0.05-0.3 Cr; up to 0.15 Mo; 0.01-0.03 Al; balance Fe and incidental additions and impurities; wherein said steel has a carbon equivalent value, C.E., of between about 0.3-0.55, derived from the following formula:
PCT Information
Filing Document Filing Date Country Kind 371c Date
PCT/US03/04090 2/12/2003 WO 00 3/18/2005
Publishing Document Publishing Date Country Kind
WO03/069008 8/21/2003 WO A
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4008103 Miyoshi et al. Feb 1977 A
6090226 Hasegawa et al. Jul 2000 A
6551419 Kanisawa et al. Apr 2003 B2
6866724 Ochi et al. Mar 2005 B2
20030221753 Toyooka et al. Dec 2003 A1
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Number Date Country
0 481 575 Apr 1992 EP
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Related Publications (1)
Number Date Country
20050178479 A1 Aug 2005 US