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Home > Equipments > China-famous-steel-producers  - The detailed information of 146mm 12Cr2Mo1R (H) plates for hydrogen heavy plate


 

The detailed information of 146mm 12Cr2Mo1R (H) plates for hydrogen heavy plate

146mm 12Cr2Mo1R (H) plates for petroleum chemistry
 
Heavy Plates with high strength, high pressure, high temperature in critical hydrogen contacting services. (Hydrogen Heavy Alloy Steel Plate)
•    Due to high technical requirements of anti-corrosion & high temperature & high pressure vessels or equipments for oil/chemistry/coal chemical industry, domestic market depends on importing materials in past years from DillingerHütte GmbH and Kobe Steel Ltd., Japan.
•    XG did preparation on equipments, ingredient design and process for the final production of plates for petroleum chemical industry. We focus on technology research such as smelting, casting, rolling and heat treatment and we finally succeed.
•    J coefficient and vTr 54 + Δ215 vTr 54 data are indispensible indicators. Metal composition should comply with X coefficient also.
•    Key technology of heavy plates for petroleum chemistry is as below:
1. Control of ingredient of P, S, Sn, Sb, As and especially P element and reasonable composition ratio design of Si and Mn .
2. All performance at 1/2 thickness of the plate be realized and well-controlled.
3. Optimized ingredient, reasonable process arrangement and realization of specific application of metallographic structure are assurance of complex mechanical properties, good weld ability and reliable performance.
 
Ingredient control of 130mm  12Cr2Mo1R(H)plates
Variety
Heat No.
 /DIV>
Location
C
Si
Mn
P
S
Cr
Mo
Ni
Cu
As
Sn
Sb
[H]
[O]
[N]
J
X
coefficient
coefficient
%
ppm
 /DIV>
 /DIV>
12Cr2Mo1R
C250029
Heat analysis
 /DIV>
0.12
0.16
0.34
0.008
0.0001
2.02
1.03
0.02
0.008
0.0096
0.007
0.0001
1.2
13
52
75
11.76
Component
head
0.12
0.17
0.36
0.008
0.0001
2.04
1.05
0.02
0.008
0.0096
0.007
0.0001
1.2
13
52
75
11.76
analysis
end
0.13
0.16
0.35
0.008
0.001
2.05
1.02
0.02
0.008
0.009
0.006
0.0001
1.2
13
53
74
11.75
Tempering embrittlement indicator Jless more and equel to 120,Calculating formola as below:
J=(Si%+Mn%)×(P%+Sn%)×104[element component%]
X=(10P+5Sb+4Sn+As)×102[el[ment component%]
 
•    Rolling Procedures: stable and required properties in the inside and core section of the plate can be achieved through low speed, high pressure rolling mill of 10000 tons  coarse and fine rolling mill so that the pressure and deformation can be reached to the inside of the plates
•    Heat Treatment Procedures and management: the key factors deciding the properties of the high strength, anti corrosion, high temperature proof heavy plate in chemical and petroleum industries depend on its metallographic structure. Thanks to the high toughness, stable structure, thermal fatigue resistance properties of kainite structure, it is desirable to achieve uniformly distributed kainite structure in the whole heavy plates, and it is proven the normalizing quick cooling+tempering  process can achieve ideal plates.
 
Mechanical performance
 
Variety
Dimensions
Heat treatment
Location
Plate
Tensile at normal temperature
Impact test
place
Rp0.2
Rm
A
ψ
temperature
impact energy
12Cr2Mo1R(H)
146mm
Max simulation welding status
head
top
477
594
26.5
75
-30°C
310
305
308
146mm
(690±14°C×32h )
under
475
595
27.5
74
-30°C
307
305
312
146mm
 
1/2t
456
579
24.9
65
-30°C
257
265
261
146mm
 
Diagonal at the end
top
480
601
26.4
73
-30°C
305
308
302
146mm
 
under
474
593
26.9
76
-30°C
312
308
300
146mm
 
1/2t
451
575
25.1
66
-30°C
264
258
270
146mm
Min simulation welding status
head
top
481
602
25.7
71
-30°C
308
301
309
146mm
(690±×8h )
under
479
600
26
73
-30°C
305
312
310
146mm
 
1/2t
459
578
24.3
62
-30°C
257
249
267
146mm
 
Diagonal at the end
top
479
599
26.1
71
-30°C
305
307
301
146mm
 
under
483
605
25.9
68
-30°C
309
310
304
146mm
 
1/2t
460
579
24.1
61
-30°C
249
251
256
•    Test results indicate that all mechanic performance is great and mostly even exceed. 
 
Mechanical performance
 
Variety
Dimensions
Heat treatment
Location
Plate
Tensile at normal temerature
Impact test
place
Rp0.2
Rm
A
ψ
temperature
impact energy
12Cr2Mo1R(H)
146mm
Max simulation welding status
head
top
477
594
26.5
75
-30°C
310
305
308
146mm
(690±14°C×32h )
under
475
595
27.5
74
-30°C
307
305
312
146mm
 
1/2t
456
579
24.9
65
-30°C
257
265
261
146mm
 
Diagonal at the end
top
480
601
26.4
73
-30°C
305
308
302
146mm
 
under
474
593
26.9
76
-30°C
312
308
300
146mm
 
1/2t
451
575
25.1
66
-30°C
264
258
270
146mm
Min simulation welding status
head
top
481
602
25.7
71
-30°C
308
301
309
146mm
(690±×8h )
under
479
600
26
73
-30°C
305
312
310
146mm
 
1/2t
459
578
24.3
62
-30°C
257
249
267
146mm
 
Diagonal at the end
top
479
599
26.1
71
-30°C
305
307
301
146mm
 
under
483
605
25.9
68
-30°C
309
310
304
146mm
 
1/2t
460
579
24.1
61
-30°C
249
251
256
 
•    Test results indicate that all mechanic performances of 146mm 12Cr2Mo1R (H) plates are great and reach the standards and even exceed required data.
 
12Cr2Mo1R(H)cool bend & hot tensile Properties
 
Cool bend test result
Variety
Dimensions
Heat treatment
Location at Width
Location at thickness
Cool bend=3a,180°C
12Cr2Mo1R(H)
146mm
Delivery status
head-mid
surface
qualified
146mm
end-mid
surface
qualified
 
Tensile result at high temperature
Variety
Dimension
Heat treatment
Temp.
Head-angle
End-diagonal
surface
1/4t
1/2t
surface
1/4t
1/2t
Rp0.2
Rm
Rp0.2
Rm
Rp0.2
Rm
Rp0.2
Rm
Rp0.2
Rm
Rp0.2
Rm
12Cr2Mo1R(H)
146mm
Delivery status
100°C 
468
621
460
614
456
608
470
625
459
616
458
610
146mm
150°C 
460
615
454
610
450
603
462
620
453
610
452
608
146mm
200°C 
454
610
450
603
446
599
458
615
450
605
449
600
146mm
250°C 
448
600
444
595
440
590
452
606
445
600
444
595
146mm
300°C 
439
590
435
587
430
578
441
592
436
589
431
580
146mm
350°C 
430
581
426
580
420
560
432
584
428
581
422
572
146mm
400°C 
421
570
416
570
410
551
423
576
420
570
411
556
146mm
415°C 
412
553
402
545
394
536
410
555
403
548
398
535
146mm
450°C 
400
532
390
519
380
509
411
536
385
516
379
511
146mm
500°C 
387
514
380
505
371
495
386
515
379
503
368
492
 
146mm 12Cr2Mo1R (H) hardness and distribution
Surface hardness test result
Variety
Dimensions
Heat treatment
Location
Hardness(HB)
12Cr2Mo1R(H)
146mm
Delivery status
head
201
205
203
206
202
146mm
end
203
207
202
205
201
146mm
Min simulation status after welding
head
195
194
196
195
197
146mm
end
194
196
195
197
196
Whole thickness hardness distribution
Variety
Dimension
Heat treatment
Location
Hardness(HB)
12Cr2Mo1R(H)
146mm
Delivery status
upper  surface
202
207
203
205
204
146mm
U/S 1/4
195
198
197
196
197
146mm
1/2
189
190
191
188
192
146mm
lower r surface
203
205
206
204
207
146mm
L/S 1/4
196
199
197
196
195
Hardness distributed at thickness-direction under delivery status

 

12Cr2Mo1R (H) tempera brittleness
Variety
Thickness
Heat treatment
 /B>
Heat treatment
 /B>
testing temperature
Akv1
Akv2
Akv3
average
test temp.
Akv1
Akv2
Akv3
average
 
12Cr2Mo1R(H)
146mm
Min simutation after welding
20°C
345
348
342
345
step-cooling testing status
20°C
348
352
350
350
146mm
0°C
342
329
334
335
0°C
338
335
327
333
146mm
-20°C
309
322
318
316
-20°C
296
309
315
307
146mm
-30°C
299
304
308
303
-30°C
289
297
285
290
146mm
-40°C
266
254
257
259
-40°C
262
258
261
261
146mm
-60°C
218
205
209
210
-60°C
158
142
120
140
146mm
-80°C
156
135
141
144
-80°C
65
55
71
63
146mm
-100°C
39
48
42
43
-100°C
28
35
38
34
 

Conversion curvies of tempered brittleness assessed by dat, a indicated in above form

  formula:vTr54 +3ΔvTr54

from the chart:vTr54=-96°C,vTr54'=-82°C.

vTr54 +3ΔvTr54=-54°C,10°C lower that the standard requirement.

12Cr2Mo1R (H) metallographic structure and nonmetallic inclusions
Metallographic structure & crystal size
Variety
thickness
location
organization
crystal size
1/4t
1/2t
1/4t
1/2t
12Cr2Mo1R(H)
146mm
head
tempered kainite
tempered kainite
8.0
7.5
12Cr2Mo1R(H)
146mm
end
tempered kainite
tempered kainite
8.0
7.5
Nonmetallic inclusions
Variety
Thickness
Location
Place at thickness
A type
B  type
C type
D type
R/S
F/S
R/S
F/S
R/S
F/S
R/S
F/S
12Cr2Mo1R(H)
146mm
head
upper  surface
0
0.5
0
1
0
0
1
0
146mm
upper 1/4t
0.5
0
0.5
0.5
0
0
0.5
0
146mm
1/2t
1
0
0
0.5
0.5
0
0
1
146mm
lower 1/4t
0
0.5
0.5
0
0.5
0
0
1
146mm
lowe surface
0.5
0
1
0
0.5
0.5
0
0.5
146mm
end
upper  surface
0
0
0.5
0
0
0
1
0
146mm
upper 1/4t
0.5
0
0.5
0
0
0
0
1.0
146mm
1/2t
0
0.5
0
0.5
0
0
1.0
0
146mm
lower 1/4t
0.5
0
0.5
0
0
0
0.5
0.5
146mm
lower surface
0
0.5
0
0
1
0
0
0
Note: R/S= Rough Series, F/S= Fine Series
 
12Cr2Mo1R (H) performance at thickness direction
Variety
Thickness
Heat treatment
Width place
Z-dirction tensile
1
2
3
average
12Cr2Mo1R(H)
146mm
delivery status
head
71
65
68
68
146mm
end
70
71
73
71
146mm
max simulation status after welding
(690±14°C×32h )
head
65
66
68
66
146mm
end
61
68
67
65
146mm
min simulation status after welding
(690±×8h )
head
72
63
69
68
146mm
end
69
66
70
68
Tensile test section area shrinkage meets 65% at the thickness direction. This indicates that the plate has strong lamellar tearing resistance capacity.
 
12Cr2Mo1R (H) welding process assessment
•    Arc welding and submerged arc welding test, heat input of arc welding is 15KJ/cm, and 45KJ/cm for submerged arc welding.
Test plate No.2407M025100, melting composition &chemical performance of the base metal indicates in form below. Dimensions of the base metal: 1200mm (rolling direction)×225mm(width)×146mm(thickness)
Composition of base metal
C
Si
Mn
P
Nb
V
Cr
0.12
0.16
0.34
0.008
0.005
0.004
2.02
Mo
Ni
Ti
Sn
As
Ceq
Pcm
1.03
0.02
0.002
0.0096
0.007
0.96
0.31
Performance of base metal
Rel/MPa
Rm/MPa
A/%
AKV   (-30°C)/J
Recorded
506
660
22
293,303,319
Standard
310
520-680
19
34
 
12Cr2Mo1R base metal hardness test
HV hardness testing point & values
test point
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
normal temp.
263
260
257
269
274
267
268
270
323
325
290
292
281
282
270
266
268
100°C
260
261
269
315
310
312
315
305
297
304
311
310
323
314
280
284
263
150°C
286
275
298
296
292
300
299
288
278
276
288
288
289
291
286
281
267
200°C
220
226
219
224
226
225
225
221
229
220
231
229
226
222
231
225
220
Note:Black-marked data are max. Hardness in weld affected area
 
Curves of hardness values

 
  Welding material & equipment
thickness
method
equipment
welding material
146mm
SAW
AC/DC1000 LIINCOLN
Wire: CHW-S11,flux CHF101 Pacific Co.
146mm
SMAW
DC400/ LINCOLN
Rod:Φ3.2/4.0mm CHH307/ Pacific co.
(save 1 rolling surface)
Process parameters of different lines on energy-given-board for welding
board No.
passes
wire diameter
Current  A
Voltage
Speed
Heat input KJ/cm
mm
V
mm/s
12Cr2Mo1R-11
1
Φ4.0
650
32
5-6
42
2~65
Φ4.0
700
33
5-6
46
average
45
 
12Cr1MoVR-12
1
Φ3.2
110
25
 
13.4
2~12
Φ4.0
145-175
26-28
 
11.1-17.8
average
15

Welding joints on the set of requirements

 

Result: Parts cutted from welding test board tempering in 690°C within 32 Hours & 8Hours, sample No. 12Cr2Mo1R-11-1 for 32 Hours and sample No.12Cr2Mo1R-11-2 for 8Hours. Samples remain welded.
 
Mechanical performance of welding joints
Tensile test for welded plate:
Tensile test samples:Matrix stretch & round stretch samples. Thickness 70mm for matrix stretch andΦ10mm bar cutted from ½ thickness of weld of the test sample. Tensile tests in normal temperature and high temperature results as follows:    Tensile strength of welding joints
sample No.
location
status
tensile strength MPa
fracture location
12Cr2Mo1R-11-1
welding joints
high temperature
530
weld
12Cr2Mo1R-11-1
welding joints
normal temperature
540
weld
12Cr2Mo1R-11-1
1/2thickness of weld
high temperature
550
12Cr2Mo1R-11-1
1/2thickness of weld
normal temperature
570
12Cr2Mo1R-11-2
welding joints
high temperature
550
weld
12Cr2Mo1R-11-2
welding joints
normal temperature
570
weld
12Cr2Mo1R-11-2
1/2thickness of weld
high temperature
580
12Cr2Mo1R-11-2
1/2thickness of weld
normal temperature
600
12Cr2Mo1R-12
welding joints
normal temperature
560,550
weld
standard requirement
520-680
 
Test result of bend and impact at weld and heat affected zone
Bending test and result:
2 side-bending sample & 2 surface-bending sampled=40mm. 180°bending angle under room temperature. No visal crack or stratification appears in sample.
Test results of impact and tempered brittleness:
Chirpy notch is used as impact sample standard. Samples are cutted from 1/2 thickness of joints exactly located at the weld center and heat affected zone. Testing temperature is -30°C. Qualified impact test results are as below:
Impact results of samples at different location
Sample No.
weld center(1/2 thickness)
HAZ 2mm(1/2t)
12Cr2Mo1R-11-1
128  126  100
276   257   278
12Cr2Mo1R-11-2
99   96   116
246   257   267
12Cr2Mo1R-12
168   186   200
246   257   267
Standard
more than and equel to 34J
Temperature-Impact Results
sample No.
temperature(°C)
weld impact value(J)
heat affected zone impact value(J)
12Cr2Mo1R-11-1
Normal
168,180,196
296,315,328
12Cr2Mo1R-11-1
0°C
180,185,176
290,300,310
12Cr2Mo1R-11-1
-10°C
170,178,168
300,285,270
12Cr2Mo1R-11-1
-20°C
158,160,154
260,265,270
12Cr2Mo1R-11-1
-30°C
130,120,110
255,258,260
12Cr2Mo1R-11-1
-40°C
120,100,105
248,240,252
12Cr2Mo1R-11-1
-60°C
68,60,55
200,210,224
12Cr2Mo1R-11-1
-80°C
38,15,24
120,32,65
12Cr2Mo1R-11-2
Normal
148,150,166
296,300,318
12Cr2Mo1R-11-2
0°C
160,155,146
280,290,290
12Cr2Mo1R-11-2
-10°C
150,148,138
280,285,260
12Cr2Mo1R-11-2
-20°C
138,120,124
250,255,260
12Cr2Mo1R-11-2
-30°C
100,90,90
245,238,240
12Cr2Mo1R-11-2
-40°C
90,80,75
228,220,222
12Cr2Mo1R-11-2
-60°C
58,40,45
160,110,124
12Cr2Mo1R-11-2
-80°C
28,15,20
60,22,45
 
Hardness test of welding joints at different location
Testing points shows at right
12Cr2Mo1R-11 hardness distribution

 
Hardness distribution and ingredient of welding joints
12Cr2Mo1R-12 hardness distribution

Hardness distributed at rage of 150-200, complying to requirements
12Cr2Mo1R-11 ingrediet of welding joints (%)
C
Si
Mn
P
S
Nb
V
Mo
0.087
0.37
0.70
0.007
0.002
0.005
0.004
1.01
Cr
Ni
Ti
Mo
Cu
Sn
As
1.94
0.02
0.002
1.03
0.01
0.0083
0.008
   12Cr2Mo1R-12 ingredient of welding joints(%)(%)
C
Si
Mn
P
S
Nb
V
Mo
0.11
0.18
0.38
0.007
0.002
0.005
0.004
0.95
Cr
Ni
Ti
Mo
Cu
Sn
As
1.92
0.02
0.002
1.03
0.11
0.0071
0.007
 
Testing results of welding process on 12Cr2Mo1R plate
Hard facing two samples of the plate welded by rod model L309-CHS062 produced by Atlantic Co.-till the hard face come to 3-4 mm thickness. One of the sample is welded by CHS132 again till the hard face come to 8mm thickness. Pieces cutted from the samples are tempered at 690°C 32H and 690°C 8H, testing results are as form13 below according to JB4708:
Assessment of hard facing welding process
standard
<, TD width=136>
12Cr2Mo1R-14
,
projects
testing values
remarks
shear strength of fusion surface
GB/T6396
300MPa
12Cr2Mo1R-13
320MPa
12Cr2Mo1R-14
ingredient
JB 4708
forms at right side
test of ferrite
tester calibrated by standard AWS4.2 reads on 6points at least.
4,4,4,5,5,4
12Cr2Mo1R-13
6,6,7,6,7,7
Te, st&, nbsp; of intergranular corrosion tendency
GB4334.5
qualified
12Cr2Mo1R-13
qualified
12Cr2Mo1R-14
bending test
JB4708
grade, qualified
12Cr2Mo1R-13
grade, qualified
12Cr2Mo1R-14
penetration test
JB/T4730
grade, qualified
12Cr2Mo1R-13
grade, qualified
12Cr2Mo1R-14
ultrasound  test
JB/T4730
grade, qualified
12Cr2Mo1R-13
grade, qualified
12Cr2Mo1R-14
form14:  ingredient of 12Cr2Mo1R-13 (%)
C
Si
Mn
P
S
Cr
Mo
Ni
Nb
Cu
0.047
0.56
0.95
0.027
0.012
19.8
0.11
9.7
0.58
0.19
form15:  ingredient of 12Cr2Mo1R-14 (%)
C
Si
Mn
P
S
Cr
Mo
Ni
Cu
0.027
0.47
1.85
0.020
0.009
24.2
0.19
13.09
0.092
Test result of 12Cr2Mo1R plate's weld ability:
Welding joints have good performance of tensile, bending, impact and welding.
 
Other Types of Heavy Plates in Hydrogen Conditions such as Petroleum Chemistry
Composition control:
Variety
Heat No.
C
Si
Mn
P
S
Cr
Mo
As
Sn
Sb
J coefficient
X
coefficient
15CrMoR
C250030
0.13
0.15
0.41
0.007
0.001
0.92
0.48
0.0095
0.008
0
84
11.15
SA387Gr11CL2
C280000
0.14
0.47
0.38
0.007
0
1.06
0.48
0.0093
0.008
0
127.5
11.13
C280001
0.14
0.48
0.38
0.007
0.001
1.05
0.48
0.0081
0.007
0
120.4
10.61
C280002
0.14
0.46
0.4
0.007
0.001
1.04
0.48
0.0081
0.006
0
111.8
10.21
C280003
0.14
0.46
0.37
0.007
0.001
1.04
0.48
0.0093
0.007
0
116.2
10.73
Customer requires that plate model15CrMoR(H) must meet X less than and equel to 15, mole 14Cr1MoR(H)meet J less than and equel to 150. X less than and equel to15, the formula of J&X coefficients is below:
J=(Si%+Mn%)×(P%+Sn%)×104[element content%]
X=(10P+5Sb+4Sn+As)×102[element content%]
 
Hydrogen Steel Plate 75, 130mm SA387Gr11CL2 (H)
Hydrogen steel plate SA387Gr11CL2 (H) Mechanical Test Properties:
Item
Test Lot
Sampling Location
138
Heat Treatment
Rel, MPa
Rm,MPa
A, %,
Impact Power J(-10°C)
Average Impact Power J
390°C Tensile
 
SA387Gr11CL2(H)
S2402L300-1
Thickness1/4
75
920 Normalizing Quick Cool
700 Tempering
445
597
25.8
228
231
240
233
375
 
R2402L300-1
Thickness1/2
75
430
565
22.9
217
209
247
224
358
 
S2402L300-2
Thickness1/4
75
920 Normalizing Quick Cool,700 tempering+690 simulating treatment after welding(14 hours temperature holding)
385
513
31.5
205
211
246
221
319
 
R2402L300-2
Thickness1/2
75
370
498
30.8
168
159
256
194
317
 
Item
Test Lot
Sampling Location
138
Heat Treatment
Rel, MPa
Rm,MPa
A, %
Impact Power J(-10°C)
Average Impact Power J
390°C Tensile
SA387Gr11CL2(H)
S2402L271-1
Thickness1/4
130
920 Normalizing Quick Cool
700 Tempering
425
536
28
207
214
220
214
355
R2402L271-1
Thickness1/2
130
410
515
26.5
138
175
175
163
340
S2402L271-2
Thickness1/4
130
920 Normalizing Quick Cool,700 tempering+690 simulating treatment after welding(14 hours temperature holding)
366
518
30
230
241
219
230
315
R2402L271-2
Thickness1/2
130
348
509
28.5
205
211
217
211
298
 
 


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