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Publication Number:  FHWA-HRT-11-062    Date:  November 2011
Publication Number: FHWA-HRT-11-062
Date: November 2011

 

Improved Corrosion-Resistant Steel for Highway Bridge Construction

CHAPTER 3. MECHANICAL PROPERTIES OF TEST STEELS

TEMPERING STUDY TO ACHIEVE TARGETED STRENGTH

In the as-normalized condition, martensitic and dual-phase steels exhibit relatively high hardness, TS, and YS. The procedure to reduce the hardness and strength properties of steels is called tempering. Tempering involves heating the steel to a suitable temperature, after which the room temperature strengths and hardness are less than in the as-normalized condition. Up to a critical temperature, which is unique for each steel, the higher the tempering temperature, the lower are the resulting YS, TS, and hardness. To achieve a minimum YS of 50 ksi (345 MPa), commercially produced as-hot-rolled ASTM A1010 steel plates are tempered between 1,300 and 1,360 °F (704 and 738 °C). To obtain a YS of 70 to 85 ksi (482 to 586 MPa), which was one of the targets of this project, a somewhat lower tempering temperature needed to be identified.

The 0.3125-inch (14.3-mm)-thick as-normalized plate samples were divided into five pieces. One piece was used for determining the as-normalized mechanical properties of each steel. The other four pieces were heated to a specific tempering temperature for 20 minutes. Brinell hardness tests were conducted on each piece. Tensile specimens were machined to determine the yield and tensile properties as a function of tempering temperature (see figure 5). The intention was to determine the tempering temperature range over which a YS of 70 to 85 ksi (482 to 586 MPa) can be achieved for each candidate steel.

Table 5. Hardness of experimental steels as a function of tempering temperature.

Steel

Heat

As-Normalized

1,200 ºF

1,250 ºF

1,300 ºF

1,350 ºF

11Cr

67-V1-77

285

200

190

177

171

9Cr

67-V1-68

313

211

200

190

191

9Cr 2Si

67-V1-71

256

209

198

190

192

7Cr 2Si

67-V1-73

258

209

198

196

194

7Cr 2Al

67-V1-75

154

152

147

152

149

5Cr 2Si 2Al

67-V1-80

200

203

203

199

202

°C = (°F-32)/1.8

The results of the hardness tests on tempered coupons of all six steels are shown in figure 25. The hardness of the dual-phase and martensitic experimental steels decreased, as expected, when the tempering temperature increased. The hardness of the two Al-containing steels did not change during tempering. This was not unexpected based on the ferritic microstructure of these two steels, since tempering is a metallurgical phenomenon that applies to steels that have martensite in the microstructure.

This bar graph shows the hardness of the experimental steels after tempering. Brinell hardness (HBW) is plotted on the y-axis ranging from 120 to 340 HBW in increments of 20 HBW. Tempering temperature is plotted on the x-axis ranging from 0 to 1,600 ºF (-18 to 871 ºC) in increments of 200 ºF (111 ºC). There are six differently colored sets of data symbols, and a legend identifies the data symbol and color for each steel. The steels are 11Cr, 9Cr, 9Cr2Si, 7Cr2Si, 7Cr2Al, and 5Cr2Si2Al. For four of the steels, the hardness declines as the temperature increases from starting values of 256 to 313 HBW to ending values of 170 to 200 HBW at 1,350 ºF (732 ºC). Two of the steels that start with hardness values of 154 and 200 HBW maintain about constant hardness at all tempering temperatures.

Figure 25. Graph. Hardness of the experimental steels after tempering.

The tensile properties of the 0.3125-inch (14.3-mm)-thick plates were measured using standard ASTM A370 round tensile specimens with a gauge diameter of 0.357 inches (9.1 mm) and a 1-inch (25.4-mm) gauge length.(16) The specimens were machined from the transverse direction of the plates, which is the standard orientation of tensile specimens made from commercially produced bridge plates. Crosshead speed was held constant throughout the tensile test at 0.080 inches per minutes (2 mm per minute). In addition to the standard tensile test quantities of 0.2 percent YS, ultimate TS, EL, and reduction of area (RA), the strain hardening coefficient (the n-value) was also calculated between strain values of 0.030 and the strain at the maximum load.

The as-normalized tensile properties of the six experimental steels are presented in table 6. The properties of the 11Cr steel are similar to a commercially produced ASTM A1010 as-normalized plate. This plate exhibited continuous yielding behavior, as expected for a dual-phase steel. The 9Cr steel, with its fully martensitic microstructure, was somewhat stronger than the 11Cr steel in the as-normalized condition, and it was consequently considerably less ductile. The tensile specimen unexpectedly broke after only 9 percent elongation. The two lower Cr steels with 2 percent Si had equal tensile behavior to each other, but these steels were considerably lower strength than the 11Cr and 9Cr steels. The YS of the two high Si steels was essentially 80 ksi (550 MPa) in the as-normalized condition. This is within one of the targeted YS ranges of 70 to 85 ksi (482 to 586 MPa). The 7Cr2Al steel had low tensile properties in the as-normalized condition. The as-normalized YS of this steel was just enough to achieve the 50- to 65-ksi (345- to 448-MPa) targeted YS range. A flaw in the tensile specimen caused it to fail outside the gauge length so no elongation value could be determined for this steel. However, the reduction in area value of only 14 percent indicates the steel has limited tensile ductility. Although the 5Cr2Si2Al steel is not as weak as the 7Cr2Al steel, its ductility is worse.

Table 6. Tensile properties of as-normalized steel plates.

Steel

Hardness (HBW)

0.2 Percent YS (ksi)

TS (ksi)

EL (Percent)

RA (Percent)

n-value

Comment

11Cr

285

91.9

134.5

23.1

57.8

Continuous yielding

9Cr

313

109.8

148.3

9.0

39.7

Broke at
9 percent

9Cr2Si

256

80.4

121.7

29.6

64.0

0.118

Continuous yielding

7Cr2Si

258

79.1

121.1

29.9

68.8

0.120

Continuous yielding

7Cr2Al

154

54.5

70.2

14.0

0.173

Broke outside reduced section

5Cr2Si2Al

200

76.6

81.5

2.1

2.6

Broke at
2.1 percent

1 ksi = 6.89 MPa

— Indicates that the value could not be determined due to experimental difficulties.

The tensile properties of the experimental steels were measured after various tempering treatments. The detailed results of these extensive tempering studies are presented in appendix B of this report. A summary of the YS of the tempered coupons of all six steels are shown in figure 26, and TS is shown in figure 27.

This graph shows the yield strength (YS) of experimental steels after normalizing and tempering. On the y-axis, 0.2 percent YS is plotted from 50 to 100 ksi (345 to 689 MPa) in increments of 10 ksi (68.9 MPa). Tempering temperature is plotted on the x-axis ranging from 1,150 to 1,400 ºF (621 to 760 ºC) in increments of 50 ºF (28 ºC). There are six differently colored sets of data symbols, and a legend identifies the data symbol and color for each steel.  The steels are 11Cr, 9Cr, 9Cr2Si, 7Cr2Si, 7Cr2Al, and 5Cr2Si2Al. For steels 11Cr and 9Cr, YS declines as the temperature increases from starting values about 90 ksi (620 MPa) at 1,200 ºF (649 ºC). Steel 11Cr declines in a straight line to 53 ksi (365 MPa), and steel 9 Cr declines to 72 ksi (496 MPa) at 1,350 ºF (732 ºC). Steels 9Cr2Si and 7Cr2Si have the same YS of 78 ksi (537 MPa) at 1,200 ºF (649 ºC), and both decline to about 67 ksi (462 MPa) at 1,300 ºF (704 ºC). At 1,350 ºF (732 ºC), the 9Cr2Si steel becomes stronger, reaching 73 ksi (503 MPa), while the 7Cr2Si steel remains about 65 ksi (448 MPa). The 5Cr2Si2Al steel has a constant YS of about 74 ksi (510 MPa) at all temperatures. The 7Cr2Al steel has the lowest YS of about 53 ksi (365 MPa) at all temperatures.
1 ksi = 6.89 MPa
°C = (°F-32)/1.8

Figure 26. Graph. YS of experimental steels after normalizing and tempering.

This graph shows tensile strength (TS) of experimental steels after normalizing and tempering. TS is plotted on the y-axis ranging from 60 to 110 ksi (413 to 758 MPa) in increments of 10 ksi (68.9 MPa). Tempering temperature is plotted on the x-axis ranging from 1,150 to 1,400 ºF (621 to 760 ºC) in increments of 50 ºF (28 ºC). There are six differently colored sets of data symbols, and a legend identifies the data symbol and color for each steel. The steels are 11Cr, 9Cr, 9Cr2Si, 7Cr2Si, 7Cr2Al, and 5Cr2Si2Al. Four of the steels, 11Cr, 9Cr, 9Cr2Si, and 7Cr2Si, have the same 100 ksi (689 MPa) TS at 1,200 ºF (649 ºC). TS declines for these steels as the tempering temperature increases. Steel 11Cr declines the most to 80 ksi (551 MPa) at 1,350 ºF (732 ºC). Steels 9Cr and 7Cr2Si both decline to about 87 ksi (599 MPa) at 1,350 ºF (732 ºC). Steel 9Cr2Si declines to 90 ksi (620 MPa) at 1,300 ºF (704 ºC) but then increases to 96 ksi (661 MPa) at 1,350 ºF (732 ºC). The 7Cr2Al steel increases from a low starting TS of 77 ksi 
(531 MPa) to a maximum of 84 ksi (579 MPa) at 1,300 ºF (704 ºC), then it declines to 80 ksi (551 MPa) at 1,350 ºF (732 ºC). The 5Cr2Si2Al steel has a constant TS of about 71 ksi (489 MPa) at all temperatures.
1 ksi = 6.89 MPa
°C = (°F-32)/1.8

Figure 27. Graph. TS of experimental steels after normalizing and tempering.

The 11Cr steel responded to tempering as expected. As the tempering temperature increased, YS and TS continuously decreased. The 9Cr and the 7Cr2Si steels responded to tempering in the same manner. The 9Cr2Si steel exhibited an unexpected increase in YS and TS when the tempering temperature increased from 1,300 to 1,350 °F (704 to 732 °C). Interestingly, the 7Cr2Al and 5Cr2Si2Al steels maintained essentially the same YS as the tempering temperature increased.

All of the steels, except 5Cr2Si2Al, can be normalized and tempered to achieve the targeted 50- to 65-ksi (345- to 448-MPa) YS range and greater than the 70-ksi (482-MPa) minimum TS requirement representative of ASTM A709-50W.(2) All of the steels, except 5Cr2Si2Al and 7Cr2Al, can be normalized and tempered to achieve the ASTM A709-70W target YS of 70 to 85 ksi (482 to 586 MPa) and the TS requirement of 85 to 110 ksi (586 to 758 MPa).

MEASUREMENT OF IMPACT PROPERTIES

To prepare the experimental steels for CVN impact testing, 0.3125-inch (14.3-mm)-thick as-normalized plates were tempered at two different temperatures. The tempering temperatures used for each steel were based on the data in figure 26 and are presented in table 7. Coupons for corrosion testing, which is described later in this report, were also prepared by tempering, as shown in table 7. The target YS level for the CVN impact tests was between 50 and 65 ksi (345 and 448 MPa) to represent a 50-ksi (345-MPa) minimum YS steel, and it was between 70 and 85 ksi (482 and 586 MPa) to represent a 70-ksi (482-MPa) minimum YS steel. Since three of the steels (9Cr, 7Cr2Al, and 5Cr2Si2Al) met the latter strength range in the as-normalized condition, they were impact tested as-normalized in only one tempered condition.

Table 7. Tempering temperatures for CVN impact energy and corrosion studies.

 

Steel

Aim > 50 ksi YS
Tempering Temperature (ºF)

Aim > 70 ksi YS
Tempering Temperature (ºF)

11Cr

1,350

1,200

9Cr

1,350

As-normalized

9Cr2Si

1,350

1,200

7Cr2Si

1,350

1,200

7Cr2Al

1,200

As-normalized

5Cr2Si2Al

1,200

As-normalized

1 ksi = 6.89 MPa

°C = (°F-32)/1.8

The CVN impact test absorbed energies of the experimental steels and were determined at four test temperatures: 70, 40, 10, and -10 °F (21, 4, -12, and -23 °C). Two or three Charpy test bars were tested at each temperature. The results are tabulated in table 8 and shown in figure 28 and figure 29.

Table 8. CVN impact test results (ft-lb).

Steel

Aim > 50 ksi YS

Aim > 70 ksi YS

-10 ºF

10 ºF

40 ºF

70 ºF

-10 ºF

10 ºF

40 ºF

70 ºF

FC, minimum

 

> 30

 

 

> 35

 

 

 

NFC, minimum

 

> 20

 

 

> 25

 

 

 

11Cr

85

109

118

154

80

100

114

124

9Cr

 

4

7

61

 

4

11

39

9Cr2Si

 

8

32

46

 

4

6

24

7Cr2Si

 

3

19

34

 

7

8

13

7Cr2Al

 

 

 

4

 

 

 

4

5Cr2Si 2Al

 

 

 

3

 

 

 

3

1 ft-lb = 0.1383 m-kg

°C = (°F-32)/1.8

1 ksi = 6.89 MPa

Note: Bold values indicate results that failed to meet the bridge steel CVN impact toughness requirement. Empty cells indicate tests were not conducted because the steels were found to have low impact energies from the results of testing at higher temperatures.

Table 8 also shows the FC and NFC CVN minimum requirements for the two steel strength levels of 50 and 70 ksi (345 and 482 MPa). If a steel plate fails to meet the absorbed energy levels in this table, the plate cannot be used because bridge safety might be compromised.

This bar graph shows the average Charpy V-notch (CVN) absorbed energy values for experimental steels tempered to achieve a yield strength (YS) greater than 50 ksi (345 MPa). CVN is plotted on the y-axis ranging from 0 to 180 ft-lb (0 to 244 J) in increments of 20 ft-lb (27 J).  Test temperature is on the x-axis with four test temperatures: 70, 40, 10, and -10 ºF (21, 4, -12, and -23 ºC). In the 10 ºF (-12 ºC) portion, there are two horizontal lines: one at 30 ft-lb (41 J) designated fracture critical (FC), and one at 20 ft-lb (27 J) designated nonfracture-critical (NFC). Different colored bars at each test temperature represent steels 11Cr, 9Cr, 9Cr2Si, 7Cr2Si, 7Cr2Al, and 5Cr2Si2Al. At all temperatures, the bar for steel 11Cr is significantly higher than any of the other steels. At 70 ºF (21 ºC), the 11Cr bar is 154 ft-lb (209 J), the 9Cr bar is 61 ft-lb (83 J), the 9Cr2Si bar is 46 ft-lb (62 J), and the 7Cr2Si bar is 34 ft-lb (46 J). The bars for 7Cr2Al and 5Cr2Si2Al are short at 4 and 3 ft-lb (5.4 and 4.1 J), respectively. At 40 ºF (4 ºC), the 11Cr bar is 118 ft-lb (160 J), the 9Cr2Si bar is 32 ft-lb (43 J), the 7Cr2Si bar is 19 ft-lb (26 J), and the 9Cr bar is 7 ft-lb (9.5 J). There are no data for the 7Cr2Al or 5Cr2Si2Al steels at 40, 10, and -10 ºF (4, -12, and -23 ºC). At 10 ºF (-12 ºC), the 11Cr bar is 109 ft-lb (148 J), and the 9Cr, 9Cr2Si, and 7Cr2Si bars are between 3 and 8 ft-lb (4.1 and 11 J). At -10 ºF (-23 ºC), the 11Cr bar is the only one shown at 85 ft-lb (115 J).
°C = (°F-32)/1.8
1 ft-lb = 1.3558 J

Figure 28. Graph. Average CVN absorbed energy values for experimental steels tempered to achieve YS greater than 50 ksi (345 MPa).

This bar graph shows the average Charpy V-notch (CVN) absorbed energy values for experimental steels tempered to achieve a yield strength (YS) greater than 70 ksi (482 MPa). CVN is plotted on the y-axis ranging from 0 to 140 ft-lb (0 to 190 J) in increments of 20 ft-lb (27 J). Test temperature is shown on the x-axis with four test temperatures: 70, 40, 10, and -10 ºF (21, 4, -12, and -23 ºC). In the -10 ºF (-12 ºC) portion, there are two horizontal lines: one at 35 ft-lb (47 J) designated fracture critical (FC), and one at 25 ft-lb (34 J) designated nonfracture-critical (NFC). Different colored bars at each test temperature represent steels 11Cr, 9Cr, 9Cr2Si, 7Cr2Si, 7Cr2Al, and 5Cr2Si2Al. At all temperatures, the bar for steel 11Cr is significantly higher than any of the other steels. At 70 ºF (21 ºC), the 11Cr bar is 124 ft-lb (168 J), the 9Cr bar is 39 ft-lb (53 J), the 9Cr2Si bar is 24 ft-lb (33 J), and the 7Cr2Si bar is 13 ft-lb (18 J). The bars for 7Cr2Al and 5Cr2Si2Al are very short at 4 and 3 ft-lb (5.4 and 4.1 J), respectively. At 40 ºF (4 ºC), the 11Cr bar is 114 ft-lb (155 J), the 9Cr bar is 11 ft-lb (15 J), the 7Cr2Si bar is 8 ft-lb (11 J), and the 9Cr2Si bar is 6 ft-lb (8 J). There are no data for the 7Cr2Al or 5Cr2Si2Al steels at 40, 10, or -10 ºF (4, -12, or -23 ºC). At 10 ºF (-12 ºC), the 11Cr bar is 100 ft-lb (136 J), and the 9Cr, 9Cr2Si, and 7Cr2Si bars are between 4 and 8 ft-lb (5.4 and 11 J). At -10 ºF (-23 ºC), the 11Cr bar is the only one shown at 80 ft-lb (108 J).
°C = (°F-32)/1.8
1 ft-lb = 1.3558 J

Figure 29. Graph. Average CVN absorbed energy values for experimental steels tempered to achieve YS greater than 70 ksi (482 MPa).

At the 50-ksi (345-MPa) YS level, only 11Cr representing the ASTM A1010 steel exhibited sufficient impact toughness to be a candidate for bridge construction. Similarly, at the 70-ksi (482-MPa) YS level, only 11Cr was a candidate due to the low impact toughness of the other experimental steels. Figure 25 and figure 26 illustrate the significantly superior impact energies for the ASTM A1010 steel compared to the other experimental plates. The impact toughness results for the experimental steels were disappointing, but they may be explained by the optimum dual-phase microstructure of 11Cr with fine grain size compared to the other steels. While further metallurgical development of the lower Cr steels is possible to improve impact toughness, it is desirable to determine the corrosion performance of the lower Cr steels to determine if there is a strong incentive for such work.

 

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