vierkantrohr st 52-3
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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
A parameter given by way of the maximum regular stress range and the hydrostatic stress vary is found to correlate fatigue lives reasonably properly. This parameter accurately predicts the experimental development that in-section loading is extra damaging than out-of-phase DIN 17100 ST 52-3 loading underneath a given ratio of axial/shear stress amplitudes. Models for tensile and compressive mean stress effects have also been proposed based mostly on the uniaxial check results. effect, depending on the plastic strain previous to unloading.
Multiaxial fatigue standards are applied to the evaluation of helical compression springs. The critical airplane approaches, Fatemi–Socie and Wang–Brown, and the Coffin–Manson technique based on shear deformation, have been used to foretell fatigue lives of the springs beneath constant amplitude loading. Experimental fatigue lives are compared with the multiaxial fatigue criteria predictions. The stress evaluation was carried out within the finite component code ANSYS, and the multiaxial fatigue examine was performed using the fatigue software program nCode. A failure evaluation was conducted in order to determine the fatigue crack initiation point and a comparison of that location with essentially the most broken zone predicted by the numerical analysis is made.
w.nr. 1.0570
The proposed concept considers the combined effect of load mean stresses and cyclically stabilized residual stresses. It is pointed out that the yield strength isn’t a succesful measure to find out whether residual stresses have “low” or “extreme” impact on the fatigue strength of welded steels. It is quite really helpful to evaluate residual stress results based mostly on the effective stress ratio reflecting native loading conditions.
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), %, ≤ |
|||||||||||
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 |
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The mode of crack initiation and propagation is determined by materials, temperature, pressure range, and stress and strain histories, but not on the relative magnitude of the virtual strain-power parameters. Biaxial fatigue data obtained from the literature were analyzed for Type 304 chrome steel tested at room and elevated temperatures and for SAE 1045 steel examined at room temperature underneath in-section and ninety° out-of-phase loading circumstances. Comparisons are made between experimental knowledge and theoretical predictions to show the effectiveness of the proposed technique. A new low-cycle multiaxial fatigue life prediction methodology primarily based on the idea of an efficient shear strain is proposed. This efficient shear strain is derived by averaging the whole shear strains appearing on all planes passing by way of a material point.
The Farahani’s criterion yields probably the most satisfactory end result among the vitality criteria. Its fatigue life correlation for 1045HR steel and 304 stainless-steel fell inside elements of 2 and 3, respectively.
The cyclic pressure power density parameter W for the important or failure aircraft has been successfully applied in predicting the multiaxial fatigue life of an iron-base and a nickel-base alloy. This parameter has the benefit of being impartial of loading situation, permitting a universal energy-life curve to be determined for a variety of torsion, pressure and bending stress and pressure states.
- The proposed model, which is formulated as a generalised equal strain, takes into consideration the impact of non-symmetrical loading cycles.
- This efficient shear pressure is derived by averaging the whole shear strains performing on all planes passing by way of a fabric point.
- The axial cyclic stress-strain curve, the essential strain-life curve (Manson-Coffin) and a further life curve obtained underneath zero to pressure strain controlled axial fatigue checks are enough to permit software of the proposed criterion in all loading circumstances.
- A new low-cycle multiaxial fatigue life prediction methodology based on the idea of an efficient shear strain is proposed.
It is found that each parameters can correlate test information within an appropriate accuracy no matter which plane is used for the important plane. Garud1 (J. Test. Evaluations 1981, 9, one hundred sixty five) 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 advised after 1980 have been categorised into the five viewpoints and some issues which existed in these studies were examined.
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