Project Description
Ⅰ. Overview of ASTM A387 Chromoly Steel Plate:
ASTM A387 specification covers chromium-molybdenum alloy steel plates intended primarily for welded boilers and pressure vessels designed for elevated temperature service.
Ⅱ. Maximum Thickness
The maximum thickness of plates is limited only by the capacity of the composition to meet the specified mechanical property requirements.
Ⅲ. Chemical Requirements of ASTM A387 Chromoly Steel Plate
Elements |
Gr.2
|
Gr.12
|
Gr.11
|
Gr.22
|
Gr.22L
|
Gr.21
|
Gr.21L
|
Gr.5
|
Gr.9
|
Gr.91
|
S50460
|
K11757
|
K11789
|
K21590
|
K21590
|
K31545
|
K31545
|
S50200
|
K90941
|
K90901
|
|
Carbon, max | ||||||||||
Heat Analysis |
0.05-0.21
|
0.05-0.17
|
0.05-0.17
|
0.05-0.15A
|
0.10 max
|
0.05-0.15A
|
0.10 max
|
0.15 max
|
0.15 max
|
0.08-0.12
|
Product Analysis |
0.04-0.21
|
0.04-0.17
|
0.04-0.17
|
0.04-0.15A
|
0.12 max
|
0.04-0.15A
|
0.12 max
|
0.15 max
|
0.15 max
|
0.06-0.15
|
Manganese | ||||||||||
Heat Analysis |
0.55-0.80
|
0.40-0.65
|
0.40-0.65
|
0.30-0.60
|
0.30-0.60
|
0.30-0.60
|
0.30-0.60
|
0.30-0.60
|
0.30-0.60
|
0.30-0.60
|
Product Analysis |
0.50-0.88
|
0.35-0.73
|
0.35-0.73
|
0.25-0.66
|
0.25-0.66
|
0.25-0.66
|
0.25-0.66
|
0.25-0.66
|
0.25-0.66
|
0.25-0.66
|
Phosphorous, max | ||||||||||
Heat Analysis |
0.025
|
0.025
|
0.025
|
0.025
|
0.025
|
0.025
|
0.025
|
0.025
|
0.025
|
0.020
|
Product Analysis |
0.025
|
0.025
|
0.025
|
0.025
|
0.025
|
0.025
|
0.025
|
0.025
|
0.025
|
0.025
|
Sulfur, max | ||||||||||
Heat Analysis |
0.025
|
0.025
|
0.025
|
0.025
|
0.025
|
0.025
|
0.025
|
0.025
|
0.025
|
0.010
|
Product Analysis |
0.025
|
0.025
|
0.025
|
0.025
|
0.025
|
0.025
|
0.025
|
0.025
|
0.025
|
0.012
|
Silicon | ||||||||||
Heat Analysis |
0.15-0.40
|
0.15-0.40
|
0.50-0.80
|
0.50 max
|
0.50 max
|
0.50 max
|
0.50 max
|
0.50 max
|
1.00 max
|
0.20-0.50
|
Product Analysis |
0.13-0.45
|
0.13-0.45
|
0.44-0.86
|
0.50 max
|
0.50 max
|
0.50 max
|
0.50 max
|
0.55 max
|
1.05 max
|
0.18-0.56
|
Chromium | ||||||||||
Heat Analysis |
0.50-0.80
|
0.80-1.15
|
1.00-1.50
|
2.00-2.50
|
2.00-2.50
|
2.75-3.25
|
2.75-3.25
|
4.00-6.00
|
8.00-10.00
|
8.00-9.50
|
Product Analysis |
0.46-0.85
|
0.74-1.21
|
0.94-1.56
|
1.88-2.62
|
1.88-2.62
|
2.63-3.37
|
2.63-3.37
|
3.90-6.10
|
7.90-10.10
|
7.90-9.60
|
Molybdenum | ||||||||||
Heat Analysis |
0.45-0.60
|
0.45-0.60
|
0.45-0.60
|
0.90-1.10
|
0.90-1.10
|
0.90-1.10
|
0.90-1.10
|
0.45-0.65
|
0.90-1.10
|
0.85-1.05
|
Product Analysis |
0.40-0.65
|
0.40-0.65
|
0.40-0.70
|
0.85-1.15
|
0.85-1.15
|
0.85-1.15
|
0.85-1.15
|
0.40-0.70
|
0.85-1.15
|
0.80-1.10
|
Nickel, max | ||||||||||
Heat Analysis |
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
0.40
|
Product Analysis |
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
0.43
|
Vanadium | ||||||||||
Heat Analysis |
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
0.04 max
|
0.18-0.25
|
Product Analysis |
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
0.05 max
|
0.16-0.27
|
Columbium | ||||||||||
Heat Analysis |
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
0.06-0.10
|
Product Analysis |
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
0.05-0.11
|
Boron | ||||||||||
Heat Analysis |
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
Product Analysis |
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
Nitrogen | ||||||||||
Heat Analysis |
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
0.030-0.070
|
Product Analysis |
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
0.025-0.080
|
Aluminum, max | ||||||||||
Heat Analysis |
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
0.02
|
Product Analysis |
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
0.02
|
Titanium, max | ||||||||||
Heat Analysis |
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
0.01
|
Product Analysis |
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
0.01
|
Zirconium, max | ||||||||||
Heat Analysis |
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
0.01
|
Product Analysis |
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
…
|
0.01
|
A The carbon content for plates over 5 in. [125 mm] in thickness is 0.17 max on product analysis |
Ⅳ. Tensile Requirements
Grade 2 and 12
|
Grade 11
|
Grade 22, 21, 5, 9, 21L, 22L
|
|
Tensile Strength
Ksi(Mpa) |
55~80
(380~550) |
60~85
(415~585) |
60~85
(415~585) |
Yield Strength, min
Ksi(Mpa) |
33(230)
|
35(240)
|
30(205)
|
Elongation in 8 in.[200mm], min, %
|
18
|
19
|
…
|
Elongation in 2 in.[50mm], min, %
|
22
|
22
|
18
|
Reduction of area, min, %
|
…
|
…
|
45B
40C |
Grade 2
|
Grade 11
|
Grade 12
|
Grade 22, 21, 5, 9
|
Grade 91
|
|
Tensile Strength
Ksi(Mpa) |
70~90
(485~620) |
75~100
(515~690) |
65~85
(450~585) |
75~100
(515~690) |
85~110
(585~760) |
Yield Strength, min
Ksi(Mpa) |
45(310)
|
45(310)
|
40(275)
|
45(310)
|
60(415)
|
Elongation in 8 in.[200mm], min, %
|
18
|
18
|
19
|
…
|
…
|
Elongation in 2 in.[50mm], min, %
|
22
|
22
|
22
|
18
|
18
|
Reduction of area, min, %
|
…
|
…
|
45B
40C |
…
|
B: Measured on round test specimens.
C: Measured on flat specimen.
Ⅴ. Heat Treatment
1. Except for Grade 91, all plates shall be thermally treated either by annealing, normalizing- and -tempering, or, when permitted by the purchaser, accelerated cooling from the austenitizing temperature by air blasting or liquid quenching, followed by tempering. Minimum tempering temperatures shall be as follows:
Grade
|
Temperature, °F [°C]
|
2, 12, 11
|
1150 (620)
|
22, 22L, 21, 21L, 9
|
1250 (675)
|
5
|
1300 (705)
|
2. Grade 91 plates shall be thermally treated, either by normalizing-and-tempering or by accelerated cooling from the austenitizing temperature by air blasting or liquid quenching, followed by tempering. Grade 91 plates shall be austenitized at 1900 to 1975°F [1040 to 1080°C] and shall be tempered at 1350 to 1470°F [730 to 800°C].
3. Grade 5, 9, 21, 21L, 22, 22L, and 91 plates ordered without the heat treatment required by item 2 and item 3 shall be furnished in either the stress-relieved or the annealed condition