Steel Grade Equivalents Table
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gangsteel produced and exported DIN 1.0570 and ST 52-3 steel plate as common carbon structural steel. Gangsteel supply DIN17100 ST52-3 ST52-3N Steel plate low alloy and high strength steel plate. DIN 17100 ST52-3 steel plate price and stock supplier.ST 52-3 steel plate is one mainly of Carbon structural steel, ST 52-3 is a type of steel sheet under DIN standard which is used to build ship, bridge, belongs to high strength sheet.
If you have any requirement for ST 52-3 structure steel plate,under DIN17100 standard ST 52-3 steel plate, under DIN17100 standard, please contact us.
1.Steel Grade : ST 52-3 (1.0570)
2. Standard: DIN 17100 steels for general structural purposes
3. Approval By Third Party :ABS, DNV, GL, CCS, LR , RINA, KR, TUV, CE
4. Classification: General structural purposes
5. Product form : super heavy steel plate
The planes of most shear pressure range and most damage are examined because the critical aircraft. Fatigue lives are evaluated by rainflow cycle counting on the shear pressure history and applying the Miner-Palmgren harm rule. Predicted lives are compared with experimental lives obtained on S45C steel.
DIN17100 ST52-3 ST52-3N Steel plate Chemical composition of heat analysis:
|
DIN |
ASTM |
EN |
JIS |
Chemical Composition |
C.E. |
||||||||||
|
C |
Si |
Mn |
Cr |
Mo |
Ni |
V |
W |
S |
P |
CU |
|||||
|
17100 St52-3N |
A572-50 |
10025-2:2004 S355J2+N |
G3106 SM490YB |
max 0.22 |
max 0.55 |
max 1.60 |
– |
– |
– |
– |
– |
max 0.035 |
max 0.035 |
– |
max 0.047 |
St52-3 steel data sheet – 2, Chemical composition (product analysis) according to DIN 17100 and DIN EN 10025: 1993.
|
Chemical Composition (product analysis), %, ≤ |
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|
Country (Region) |
Standard |
Steel Grade (Steel number) |
C |
Si |
Mn |
P |
S |
N |
Cu |
Thickness (d) (mm) |
Method of deoxidation |
|
Germany |
DIN 17100: 1980 |
St52-3 (1.0570) |
0.22 |
0.60 |
1.70 |
0.065 |
0.065 |
– |
≤ 30 |
Fully Killded |
|
|
0.24 |
30 <d ≤100 |
||||||||||
|
European Union |
EN 10025: 1993 |
S355J2G3 (1.0570) |
0.22 |
0.60 |
1.70 |
0.045 |
0.045 |
– |
≤ 30 |
||
|
0.24 |
30 <d ≤100 |
||||||||||
|
EN 10025-2: 2004 |
S355J2 (1.0577) |
0.22 |
0.60 |
1.70 |
0.035 |
0.035 |
– |
0.60 |
≤ 30 |
||
|
0.24 |
30 <d ≤100 |
||||||||||
St52-3 Steel Properties
Physical Properties
- Material St 52-3 Density: 7.85 g/cm3
- Melting point: 1420-1460 °C (2590-2660 °F)
DIN17100 ST52-3 ST52-3N Steel plate mechanical properties steel plate
|
Thickness (mm) |
Yield Strength Reh min (N / mm2) |
Tensile Strength Rm min (N / mm2) |
Elongation A5 min (%) |
Impact Values Charpy-V-Notch Longitudinal Average from 3 Speimens Thk. >10<150mm. |
|
3<thk<100 |
315-355 |
490-630 |
max 22 |
27 Joules at -20 C |
St52-3 steel data sheet – 1, Chemical composition (ladle analysis) according to DIN 17100 and DIN EN 10025: 1993.
|
Chemical Composition (ladle analysis), %, ≤ |
|||||||||||
|
Country (Region) |
Standard |
Steel Grade (Steel number) |
C |
Si |
Mn |
P |
S |
N |
Cu |
Thickness (d) (mm) |
Method of deoxidation |
|
Germany |
DIN 17100: 1980 |
St52-3 (1.0570) |
0.20 |
0.55 |
1.60 |
0.040 |
0.040 |
– |
≤ 30 |
Fully Killded |
|
|
0.22 |
30 <d ≤100 |
||||||||||
|
European Union |
EN 10025: 1993 |
S355J2G3 (1.0570) |
0.20 |
0.55 |
1.60 |
0.035 |
0.035 |
– |
≤ 30 |
||
|
0.22 |
30 <d ≤100 |
||||||||||
|
EN 10025-2: 2004 |
S355J2 (1.0577) |
0.20 |
0.55 |
1.60 |
0.025 |
0.025 |
– |
0.55 |
≤ 30 |
||
|
0.22 |
30 <d ≤100 |
||||||||||
DIN17100 ST52-3 EQUIVALENT STEEL GRADES
| EN 10025 – 2 |
EN 10025+A1 |
?SN |
DIN 17100 |
||
|
EN10027-1 |
EN10027-2 |
EN10027-1 Grade |
EN10027-2 Grade |
|
|
|
S235JR2 |
1.0038 |
S235JRG2 |
1.0038 |
11375 |
RSt 37-2 |
|
S235J0 |
1.0114 |
S235J0 |
1.0114 |
11378 |
St 37-3U |
|
|
– |
S235J2GR3 |
1.0116 |
11378 |
St 37-3N |
|
S235J2 |
1.0117 |
S235J2G4 |
1.0117 |
– |
– |
|
S275JR |
1.0044 |
S275JR |
1.0044 |
11443 |
St 44-2 |
|
S275J0 |
1.0143 |
S275J0 |
1.0143 |
11445 |
St 44-3U |
|
|
– |
S275J2GR3 |
1.0144 |
11448 |
St 44-3N |
|
S275J2 |
1.0145 |
S275J2G4 |
1.0145 |
– |
– |
|
S355JR |
1.0045 |
S355JR |
1.0045 |
11523 |
St 52-3 |
|
S355J0 |
1.0553 |
S355J0 |
1.0553 |
11523 |
St 52-3U |
|
|
– |
S355J2G3 |
1.057 |
11503 |
St 52-3N |
|
S355J2 |
1.0577 |
S355J2G4 |
1.0577 |
– |
– |
Material St 52-3 Datasheet – 3
|
Yield strength (≥ N/mm2); Thickness (d) mm |
||||||
|
Steel (Steel number) |
d≤16 |
16< d ≤40 |
40< d ≤63 |
63< d ≤80 |
80< d ≤100 |
>100 |
|
St52-3 |
355 |
345 |
335 |
325 |
315 |
by agreement |
Tensile Strength
Material St 52-3 Datasheet – 4
|
Tensile strength (≥ N/mm2); Thickness (d) mm |
|||
|
Steel (Steel number) |
d<3 |
3 ≤ d ≤ 100 |
>100 |
|
St 52-3 |
515-680 |
490-630 |
by agreement |
Note: 1MPa = 1N/mm2
Elongation
Material St 52-3 Datasheet – 5
|
Elongation (≥, %); Thickness (d), mm |
||||||||
|
Steel (Steel number) |
0.5 ≤d <1 |
1≤ d <1,5 |
1,5≤ d <2 |
2≤ d <2,5 |
2,5≤ d <3 |
|||
|
St52-3U |
14 |
15 |
16 |
17 |
18 |
|||
|
St52-3N |
12 |
13 |
14 |
15 |
16 |
|||
|
Elongation (≥, %); Thickness (d), mm |
||||||||
|
Steel (Steel number) |
3 ≤d ≤40 |
40< d ≤63 |
63 < d ≤100 |
>100 |
||||
|
St52-3 |
22 |
21 |
20 |
by agreement |
||||
|
St52-3N |
20 |
19 |
18 |
|||||
1.0570+ar
It is discovered that each parameters can correlate check data inside an acceptable accuracy regardless of which aircraft is used for the critical aircraft. Garud1 (J. Test. Evaluations 1981, 9, 165) reviewed the results of multiaxial fatigue researches proposed as much as 1980 in chronological order and evaluated them. In this paper multiaxial fatigue researches which have been suggested after 1980 were categorized into the 5 viewpoints and some problems which existed in those research had been examined. During these intervals major progresses in multiaxial fatigue analysis are the consideration of anisotropy of supplies and the suggestion of the vitality technique utilizing Mohr’s circles. Additionally, existing equations or parameters have been modified to consider the mean stress, loading path, and so on.
- The crucial aircraft resulting in Mode I fracture is driven by the principal stress and strain, and the opposite, resulting in Mode II fracture, is pushed by the maximum shear stress and strain.
- A new low-cycle multiaxial fatigue life prediction methodology based mostly on the idea of an effective shear pressure is proposed.
- The mode of crack initiation and propagation is determined by materials, temperature, strain range, and stress and pressure histories, but not on the relative magnitude of the digital pressure-energy parameters.
- Biaxial fatigue knowledge obtained from the literature were analyzed for Type 304 stainless-steel examined at room and elevated temperatures and for SAE 1045 metal tested at room temperature underneath in-section and ninety° out-of-phase loading conditions.
Proportional and nonproportional tension–torsion fatigue tests were performed on LY12CZ aluminum alloy. Two forms of tubular specimens were used, one is smooth and the other is notched.
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A new critical aircraft criterion including the pressure and stress parameters is proposed. It is demonstrated that the proposed criterion gives higher satisfactory results for all of the three checked materials. A new method is proposed for multiaxial fatigue life prediction using correlation parameters based mostly on digital pressure vitality as a measure of fatigue injury on critical planes of fracture.
The experimentally observed fatigue lives of proportional and non-proportional multiaxial strain managed low-cycle fatigue tests from un-notched tubular specimens, have been in contrast with the expected lives of the proposed strategy showing in all instances a great DIN 17100 ST 52-3 agreement. In this paper several multiaxial fatigue criteria are reviewed. The standards are divided into three teams, according to the parameters used to explain the fatigue life or fatigue power of materials.
Among the pressure criteria, the Kandil, Brown and Miller’s criterion has the most effective correlation with the experimental data of the materials employed. The Farahani’s criterion yields essentially the most passable outcome among the many power standards. Its fatigue life correlation for 1045HR metal and 304 stainless-steel fell within components of two and 3, respectively.
The proposed mannequin, which is formulated as a generalised equal pressure, takes under consideration the effect of non-symmetrical loading cycles. The primary benefit of the model relies on the small variety of materials parameters to be recognized. The axial cyclic stress-strain curve, the essential pressure-life curve (Manson-Coffin) and a further life curve obtained beneath zero to rigidity strain controlled axial fatigue tests are enough to allow utility of the proposed criterion in all loading circumstances.
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