Section 3 Approval test programme
Clasification Society 2024 - Version 9.40
Clasifications Register Guidance Information - Guidance for Approval, Manufacture, Testing and Certification of High Manganese Austenitic Steel for Low Temperature Service, July 2022 - Chapter 3 Approval of a Works for the Manufacture of High Manganese Austenitic Steels - Section 3 Approval test programme

Section 3 Approval test programme

3.1 Selection of material

3.1.1 Generally, the initial approval test programme is to be carried out on at least two casts of each product selected for approval testing. The testing is in respect of specific types of products and if, for example, a works requests approval for both plates and sections or bars, it will be necessary to carry out tests on two casts rolled into plates and two casts rolled into sections or bars.

3.1.2 The dimensions of the products from each cast submitted for approval tests are to be representative of the range which will be manufactured and should include at least one batch of material of the maximum thickness and width or diameter which it is proposed to supply, i.e. material where the amount of hot working is at the minimum value proposed by the manufacturer. If an example representing the maximum width or diameter cannot be included, then agreement needs to be made on the maximum width or diameter that will be granted manufacturing approval based on the samples supplied.

3.1.3 With the exception of hot coiled strip, approval tests are to be carried out on a minimum of two rolled products of different thickness or diameter from each cast. For plate, wherever possible, these tests are to be carried out on one plate 15–20 mm thick and on another of the maximum thickness that will be produced, up to 40 mm. If specified through-thickness properties are required to be approved, wherever possible the tests are to be carried out on one plate of approximately 25 mm thickness and on another of approximately 40 mm thickness. For ingot cast material, one plate is to be representative of the top of the first ingot and the other is to be representative of the last ingot from the ladle. Similarly, for continuous casting, one plate is to be representative of the beginning of a cast and the other of material poured when the ladle is nearly empty.

3.1.4 For hot coiled strip, materials for approval are to be taken from two coils selected from different casts. The coils selected are to be representative of material from an ingot top end and an ingot bottom end or, in the case of continuously cast material, from the beginning of one cast and from the end of the other. Additionally, one coil should be of the maximum thickness that it is proposed to supply. In the case of works approval for plate cut from coil, works with a de-coiling plant which is already approved for plate will be allowed a reduction in the number of tests required.

3.1.5 Testing shall be carried out according to Ch 3 Rolled Steel Plates, Strip, Sections and Bars of the Rules for the Manufacture, Testing and Certification of Materials, July 2022, or to an agreed National Standard or proprietary specification. Details of the applicable testing standards shall be submitted.

3.1.6 Applicable specification. Copies of any material specifications should be submitted where these are not National/International Standards. English copies are preferred, although documents annotated in English will be acceptable.

3.2 Tests on base material

3.2.1 Type of tests

The tests to be carried out are indicated in Table 3.3.1 Tests on base material .

LR may require the additional tests to verify the relevant characteristics of high manganese austenitic steels compared with those of the conventional materials applied to cryogenic service.

Table 3.3.1 Tests on base material

Type of test Position of the samples and direction of the test specimens Remarks
1) Tensile test

Top and bottom,

L-direction & T-direction
Yield strength (ReH), tensile strength (Rm), elongation (A5), reduction in area (RA) are to be reported.
2) Impact test on non-aged specimens

Top and bottom, 1/4t,

L-direction & T-direction
At least testing temperature: −196°C
3) Impact test on strain aged specimens Top, 1/4t, L-direction At least testing temperature: −196°C
4) Drop weight test Top The test method should comply with ASTM E208 or equivalent method.
5) Micro examination Top Grain size determination
6) Chemical analysis (ladle and product) Top Contents of C, Mn, Si, P, S, Ni, Cr, Mo, Al, N, Nb, V, Ti, B, Zr, Cu, As, Sn, Bi, Pb, Ca, Sb, O, H are to be reported.
7) CTOD test Top, T-direction Test method should comply with ISO 12135, ASTM E1820, BS7448-1 or equivalent method.
8) S-N fatigue test Top, T-direction Test method should comply with ASTM E466 or equivalent method.
9) Fatigue crack growth rate test Top, T-direction Test method should comply with ASTM E647 or equivalent method.
10) General corrosion test Top Test method should comply with ASTM G31-21 or equivalent method.
11) Elastic modulus test Top Test method should comply with ASTM E494 or equivalent method.
12) Stress corrosion crack (SCC) test Top Test method should comply with ASTM G36 and G123 or equivalent method. Test specimen should comply with ASTM G30 or equivalent.
13) Sulphur prints Top  
14) Intergranular corrosion test Top This method should comply with ASTM A262 or equivalent method.

3.2.2 Test specimens and testing procedure

The test specimens and testing procedures are to be in accordance with Ch 2 Testing Procedures for Metallic Materials and Ch 3, 1.7 Dimensional tolerances of the Rules for the Manufacture, Testing and Certification of Materials, July 2022.

In particular, the following applies:

  1. Tensile test
    • Tensile test specimens are to be taken from one test sample.
    • Tensile tests are to be carried out at room temperature and −165°C.
    • Results of tensile tests at −165°C should be reported for reference.
    • Tensile tests should be carried out with a specimen of full thickness.

  2. Impact test on non-aged specimens
    • One set of three Charpy V-notch impact specimens is required for each impact test.
    • The Charpy V-notch impact test temperature should include −196°C at least.
    • In addition to the determination of the energy value, the lateral expansion and the percentage crystallinity are also to be reported. The percentage of the ductile fracture surface at −196°C should be 100 per cent by fractography (SEM).
    • Additionally, for each location, Charpy V-notch impact tests are to be carried out with appropriate temperature intervals (−196°C, −165°C, −100°C and −65°C) to verify the properties of toughness at each temperature for reference.

  3. Impact test on strain aged specimens
    • One set of three Charpy V-notch impact specimens is required for each impact test.
    • The test specimens which have been maintained for one hour at 250°C after a strain of 5 per cent has been applied, as a rule, are to be used.
    • The Charpy V-notch impact test temperature should include −196°C at least.
    • The result should be reported for reference.

  4. Drop weight test
    • Two specimens for drop weight test are to be taken from the surface of one test sample.
    • The test temperature is −196°C.
    • The test results should show no-break performance at −196°C.
    • Photographs of the test specimens are to be taken and enclosed with the test report.

  5. Micro examination
    • One test specimen for micrographic examination should be taken from one test sample.
    • All micrographs are to be taken at × 100 magnification and where austenite grain size exceeds ASTM E112 index 10 or equivalent, additionally at × 500 magnification.
    • The austenite grain size should be measured and the non-metallic inclusions are to be examined.
    • The micrographs are to be representative of the full thickness.
    • The result should be reported for reference.

  6. Chemical analysis
    • One test specimen for chemical analysis should be taken from one test sample.
    • Both the ladle and product analysis are to be reported.
    • The material for the product analysis should be taken from the tensile test specimen.

  7. CTOD test
    • Test specimens for CTOD test are to be taken from one test sample.
    • One set of three CTOD specimens is required for each test.
    • CTOD minimum value should be in accordance with the design specification for testing at room and cryogenic temperatures as per design conditions. As a guide, a minimum CTOD value of 0,2 mm is often required.

  8. S-N fatigue test
    • Sufficient number of test specimens to obtain an S-N curve are to be taken from test samples.
    • The test temperature is room temperature.
    • The S-N curve should be established and the result should be equal to or better than the FAT125-curve given by the International Institute of Welding (IIW) or C-curve in DNVGL-RP-C203-2020.
    • At the discretion of LR, on the basis of the available test results that at least three points from three stress ranges are sufficient to indicate that additional points are not needed and the available evidence is adequate to demonstrate fatigue properties, the S-N fatigue test may be waived.

  9. Fatigue crack growth rate test
    • One test specimen for fatigue crack growth rate test should be taken from one test sample.
    • The test temperature is room temperature.
    • The result should be reported for reference.
    • At the discretion of LR, if a manufacturer can prove that the fatigue crack growth rate is superior to that of the conventional material used for the particular design application, or provide an ECA assessment for the suitability of the material for a particular application with available fatigue crack growth rate data, then the fatigue crack growth rate test may be waived.

  10. General corrosion test
    • One test specimen for corrosion resistance should be taken from one test sample.
    • The result should be reported for reference.

  11. Elastic modulus test
    • One test specimen for elastic modulus test should be taken from one test sample.
    • The test temperature should include room temperature and −165°C at least.
    • The result should be reported for reference.

  12. Stress corrosion crack (SCC) test
    • One test specimen for stress corrosion crack test should be taken from one test sample.
    • The result should be reported for reference.

  13. Sulphur prints
    • Sulphur prints are to be taken from plate edges which are perpendicular to the axis of the ingot or slab. These sulphur prints are to be approximately 600 mm long, taken from the centre of the edge selected, i.e. on the ingot centreline, and are to include the full product thickness.

  14. Intergranular corrosion test
    • One test specimen for corrosion resistance should be taken from one test sample.
    • The result should be reported for reference.

3.2.3 Other tests

Additional tests may be required in the case of a newly developed type of steel, as deemed necessary by LR.

3.3 Weldability tests

3.3.1 General

Weldability tests are required for plates and are to be carried out on samples of the thickest plate.

3.3.2 Preparation and welding of the test assemblies

In general, the following test assemblies are to be prepared:

  1. One butt weld test assembly welded with a heat input of 15 kJ/cm ±10 per cent.
  2. One butt weld test assembly welded with a heat input of 30 kJ/cm ±10 per cent.
  3. Where steel is required to be approved for heat input levels higher than 30 kJ/cm, the maximum heat input to be approved should be used for the test assembly in agreement with LR.

The butt weld test assemblies are to be prepared with the weld seam longitudinal to the plate rolling direction, so that impact specimens will result in the transverse direction.

The bevel preparation should be preferably 1/2 V or K upon the test assembly thickness.

The welding procedure should be as far as possible in accordance with the normal welding practice used at the yards for the type of steel in question.

The welding parameters including welding process, consumables designation and diameter, preheating temperature, interpass temperature, heat input, number of passes, etc. are to be reported.

The maximum approved heat input level may be specified on the approval certificate.

3.3.3 Type of tests

The tests to be carried out are indicated in Table 3.3.2 Tests on weld material.

LR may require the additional tests to verify the relevant characteristics of high manganese austenitic steels compared with those of the conventional materials applied to cryogenic service.

Table 3.3.2 Tests on weld material

Type of test Position of the samples and direction of the test specimens Remarks
1) Transverse tensile test Top, T-direction (cross weld direction)  
2) Charpy impact test Top, 1/4t, T-direction (cross weld direction) Charpy impact test on centre of WM, FL, FL+1, FL+3 and FL+5
3) Ductile fracture toughness test J1C Top

(a) Test method should comply with ASTM E1820, ISO 15653 or equivalent method.

(b) This test may be omitted at the discretion of LR, if the manufacturer can provide the crack growth resistance curve of the material.

4) CTOD test Top, T-direction (cross weld direction) Test method should comply with ISO 15653, ASTM E1820, or equivalent method.
5) Hardness test Top  
6) Stress corrosion crack (SCC) test Top Test method should comply with ASTM G36 or equivalent method. Test specimen should comply with ASTM G58 or equivalent.
7) Micro and macro examination Top  
8) Bending test Top, L-direction  
9) S-N fatigue test Top, T-direction (cross weld direction) Test method should comply with ASTM E466 or equivalent method.
10) Fatigue crack growth rate test Top Test method should comply with ASTM E647 or equivalent method.
11) General corrosion test Top Test method should comply with ASTM G31-21 or equivalent method.
12) Intergranular corrosion test Top Test method should comply with ASTM A262 or equivalent method.

Mechanical properties for butt weld tests are defined in Table 3.3.3 Mechanical properties for butt weld tests.

Table 3.3.3 Mechanical properties for butt weld tests

Tensile Strength (N/mm2) Elongation % at Charpy Impact Energy, Average
Test Temp. (°C) Average Energy (J)
≥ 660 ≥ 22,0 −196 ≥ 27

3.3.4 Test specimens and testing procedure

  1. Transverse tensile test
    • Two tensile test specimens transverse to the weld are to be taken from one test assembly.
    • Tensile tests are to be carried out at room temperature and −165°C.
    • The results of the tensile test at −165°C should be reported for reference.
    • Tensile tests should be carried out with a specimen of full thickness.

  2. Charpy impact test
    • One set of three Charpy V-notch specimens transverse to the weld should be taken.
    • The fusion boundary should be identified by etching the specimens with a suitable reagent.
    • The impact test temperature should include −196°C at least.
    • Additionally, for each specimen, impact tests are to be carried out with appropriate temperature intervals (−196°C, −165°C, −100°C and 0°C) to verify the properties of toughness at each temperature for reference.

  3. Ductile fracture toughness test J1C
    • One test specimen should be taken from the test sample.
    • Test temperature should include cryogenic service temperature.
    • The test results are to show the satisfactory resistance to the unstable ductile fracture.

  4. CTOD test
    • CTOD test for three specimens transverse to the weld for each condition should be carried out at a position in the coarse grained heat affected zone (CGHAZ). An additional set of CTOD tests with notch positions such as FL+1, FL+3, and FL+5 may be required by LR.
    • CTOD minimum value should be in accordance with design specifications for testing at room and cryogenic temperatures as per design conditions.
    • As a guide, a minimum CTOD value of 0,2 mm is often required.

  5. Hardness test
    • Hardness tests HV 10 across the weldment. The indentations are to be made along a transverse line which is 1~2 mm beneath the plate surface on both the face side and the root side of the weld; the fusion line and the HAZ: at each 0,7 mm from the fusion line into unaffected base material (6 to 7 minimum measurements for each HAZ).
    • A sketch of the weld joint depicting groove dimensions, number of passes and hardness indentations should be attached to the test report, together with photomacrographs of the weld cross-section.
    • At least two rows of indentations are to be carried out in accordance with Figure 3.3.1 Examples of hardness test with rows of indentations in butt welds.
    • The result should be reported for reference.

  6. Stress corrosion cracking (SCC) test
    • One test specimen transverse to the weld for stress corrosion crack test should be taken from one test assembly.
    • The result should be reported for reference.

  7. Micro and macro examination
    • All micrographs are to be taken at × 100 magnification and where austenite grain size exceeds ASTM E112 index 10 or equivalent, additionally at × 500 magnification.
    • The austenite grain size should be measured and the non-metallic inclusions are to be examined.
    • The micrographs are to be representative of the full thickness.
    • Three examinations are to be made at the surface, one-quarter and mid-thickness of the product.
    • The result including metallurgical phases should be reported for reference.
    • One macroscopic photograph should be representative of the transverse section of the welded joint and should show absence of cracks, lack of penetration, lack of fusion and other injurious defects.

  8. Bending test
    • Longitudinal bending test should be carried out.
    • No fracture should be acceptable after a 180° bend over a former with a diameter four times the thickness of the test pieces.

  9. S-N fatigue test
    • Sufficient number of test specimens to obtain an S-N curve are to be taken from test samples.
    • The test temperature is room temperature.
    • The S-N curve should be established and the result should be equal to or better than the FAT90-curve in IIW or D-curve in DNVGL-RP-C203:2020.
    • At the discretion of LR, on the basis of the available test results that at least three points from three stress ranges are sufficient to indicate that additional points are not needed and the available evidence is adequate to demonstrate fatigue properties, the S-N fatigue test may be waived.

  10. Fatigue crack growth rate test
    • One test specimen for fatigue crack growth rate test should be taken from one test sample.
    • Notch in test specimen should be parallel to welding seam.
    • The test temperature is room temperature.
    • The result should be reported for reference.
    • At the discretion of LR, if a manufacturer can prove that the fatigue crack growth rate is superior to that of the conventional material used for the particular design application, or provide an ECA assessment for the suitability of the material for a particular application with available fatigue crack growth rate data, then the fatigue crack growth rate test may be waived.

  11. General corrosion test
    • One test specimen for corrosion resistance should be taken from one test sample.
    • The result should be reported for reference.

  12. Intergranular corrosion test
    • One test specimen for corrosion resistance should be taken from one test sample.
    • The result should be reported for reference.

Figure 3.3.1 Examples of hardness test with rows of indentations in butt welds


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