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

st52.3n

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.

st52.3n

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.

ST52-3

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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st52.3n