VDM® Alloy 31

Alternative and trade names
Nicrofer 3127 hMo, VDM® Alloy 31
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Description

1.4562 (X1NiCrMoCu32-28-7) is an iron-nickel-chromium-molybdenum alloy with the addition of nitrogen. The alloy developed by VDM Metals closes the gap between high alloyed austenitic special stainless steels and nickel alloys. It shows the following features and properties:


  • Outstanding corrosion resistance in alkaline and acidic halide-containing media
  • Excellent resistance to sulfuric acid, even in highly concentrated form
  • Excellent resistance to corrosion and erosion in phosphoric acid media
  • Outstanding resistance to surface corrosion and local corrosion in chlorine dioxide bleaching plants in paper production
  • Excellent resistance in reducing and oxidizing media as well as in boiling azeotropic nitric acid
  • Good workability and weldability
  • VdTÜV-certification for pressure vessels with operating temperatures from -196 to 550 °C (-320.8 to 1,022 °F)
  • Certification according to ISO 15156/NACE MR 0175 up to level VI for acid gas applications in the oil and gas industry
  • ASME approval for pressure vessels up to 800°F (427°C)
  • Equivalent Materials

    This material data has been provided by VDM Metals.

    "Typical" values were obtained via a literature search. "Predicted" values were imputed via artificial intelligence technology. While we have placed significant efforts in ensuring data accuracy, "typical" and "predicted" data should be considered indicative and verified by appropriate material testing. Please do contact us if additional information on the the predicted data method is required.
    All metrics apply to room temperature unless otherwise stated. SI units used unless otherwise stated.
    Equivalent standards are similar to one or more standards provided by the supplier. Some equivalent standards may be stricter whereas others may be outside the bounds of the original standard.

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    Properties

    General

    PropertyTemperatureValue

    Density

    23.0 °C

    8.05 g/cm³

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    Mechanical

    PropertyTemperatureValueComment

    Elastic modulus

    20.0 °C

    198 GPa

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    100.0 °C

    189 GPa

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    200.0 °C

    183 GPa

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    300.0 °C

    176 GPa

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    400.0 °C

    170 GPa

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    500.0 °C

    163 GPa

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    600.0 °C

    158 GPa

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    Elongation

    23.0 °C

    40 %

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    for 20-550°C

    Impact strength, Charpy notched

    -20.0 °C

    1400 kJ/m²

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    20.0 °C

    1850 kJ/m²

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    Tensile strength

    20.0 °C

    650 MPa

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    100.0 °C

    630 MPa

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    200.0 °C

    580 MPa

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    300.0 °C

    530 MPa

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    400.0 °C

    500 MPa

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    500.0 °C

    470 MPa

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    550.0 °C

    450 MPa

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    Yield strength Rp0.2

    20.0 °C

    280 MPa

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    100.0 °C

    210 MPa

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    200.0 °C

    180 MPa

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    300.0 °C

    165 MPa

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    400.0 °C

    150 MPa

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    500.0 °C

    135 MPa

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    550.0 °C

    125 MPa

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    Thermal

    PropertyTemperatureValue

    Coefficient of thermal expansion

    100.0 °C

    1.43E-5 1/K

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    200.0 °C

    1.47E-5 1/K

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    300.0 °C

    1.51E-5 1/K

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    400.0 °C

    1.55E-5 1/K

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    500.0 °C

    1.57E-5 1/K

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    600.0 °C

    1.59E-5 1/K

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    Melting point

    1330 - 1370 °C

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    Thermal conductivity

    20.0 °C

    11.7 W/(m·K)

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    100.0 °C

    13.2 W/(m·K)

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    200.0 °C

    15 W/(m·K)

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    300.0 °C

    16.8 W/(m·K)

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    400.0 °C

    18.5 W/(m·K)

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    500.0 °C

    20.2 W/(m·K)

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    600.0 °C

    21.9 W/(m·K)

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    Electrical

    PropertyTemperatureValue

    Electrical resistivity

    20.0 °C

    1.04E-6 Ω·m

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    100.0 °C

    1.07E-6 Ω·m

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    200.0 °C

    1.1E-6 Ω·m

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    300.0 °C

    1.13E-6 Ω·m

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    400.0 °C

    1.16E-6 Ω·m

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    500.0 °C

    1.18E-6 Ω·m

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    600.0 °C

    1.2E-6 Ω·m

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    Magnetic

    PropertyTemperatureValue

    Relative magnetic permeability

    23.0 °C

    1 [-]

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    Chemical properties

    PropertyValueComment

    Carbon

    0.015 %

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    Chromium

    26 - 28 %

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    Copper

    1 - 1.4 %

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    Iron

    Balance

    Manganese

    2 %

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    max.

    Molybdenum

    6 - 7 %

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    Nickel

    30 - 32 %

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    Nitrogen

    0.15 - 0.25 %

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    Phosphorus

    0.02 %

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    max.

    Silicon

    0.3 %

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    max.

    Sulfur

    0.01 %

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    max.

    Technological properties

    Property
    Application areas

    Components for flue gas desulfurization plants, plants for the production of phosphoric acid, pipes and heat exchangers for sulfuric acids contaminated with chlorides, pipes containing ocean water and brackish water, condensers and chillers, pickling plants for sulfuric acid as well as nitric-hydrofluoric acid, treatment of sulfuric acids from waste, evaporation and crystallization of salts, components for the cellulose and paper industry, digestion of ores (e.g. in HIPAL plants), mineral oil production and ester synthesis, fine chemicals, strain-hardened transport and feed pipes as well as slicklines, wirelines and flowlines in the transport of oil and gas.

    Cold Forming

    The workpieces should be in the annealed condition for cold forming. VDM® Alloy 31 has a significantly higher work hardening rate than other widely used austenitic stainless steels. This must be taken into account during the design and selection of forming tools and equipment and during the planning of forming processes. Intermediate annealing is necessary for major cold forming work. For cold forming of > 15%, a final solution annealing must be conducted.

    Corrosion properties

    Optimal corrosion resistance is only ensured if the material is used in a solution annealed, clean and metallic bright condition. The chemical composition of VDM® Alloy 31 is designed to enable the achievement of a high corrosion resistance in halide-containing media. At the same time, the material has excellent resistance in pure and contaminated sulfuric acid over a broad range of concentrations and temperatures up to 80 °C.

    General machinability

    VDM® Alloy 31 should be machined in the heat-treated condition. Because of the considerably elevated tendency toward work hardening in comparison with low-alloy austenitic stainless steels, a low cutting speed and a feed level that is not too high should be selected and the cutting tool should be engaged at all times. An adequate depth of cut is important in order to cut below the previously formed strain-hardened zone. Optimum heat dissipation through the use of large quantities of suitable, preferably aqueous, lubricants has considerable influence on a stable machining process.

    Heat Treatment

    Solution annealing should take place at temperatures between 1,150 and 1,180°C (2,102 and 2,156°F). The retention time commences with material temperature equalization; longer times are generally considerably less critical than retention times that are too short. For maximum corrosion resistance, the workpieces must be quickly cooled from the annealing temperature of at least 1,100 to 500°C (2,012 to 932°F) with a cooling rate of >150 °C/min (>302 °F/min). The material must be placed in a furnace that has been heated up to the maximum annealing temperature before any heat treatment. The cleanliness requirements listed under "Heating" must be observed. For strip products, the heat treatment can be performed in a continuous furnace at a speed and temperature that is adapted to the strip thickness.

    Hot forming

    VDM® Alloy 31 should be hot-formed in a temperature range of 1,200 to 1,050°C (2,192 to 1,922°F) with subsequent rapid cooling in water or in air. For heating up, workpieces should be placed in a furnace that has been heated up to the maximum hot-forming temperature (solution annealing temperature). Once the furnace has reached its temperature again, the workpieces should remain in the furnace for around 60 minutes per 100 mm (3.94 in) of thickness. After this, they should be removed from the furnace immediately and formed within the temperature range stated above, with reheating necessary once the temperature reaches 1,050°C (1,922°F). Heat treatment after hot forming is recommended in order to achieve optimal properties.

    Other

    VDM® Alloy 31 has a face-centered cubic lattice. The 0.2% nitrogen content stabilizes the austentite and reduces the precipitation rate of intermetallic sigma phases.

    Welding

    VDM® Alloy 31 can be welded using conventional processes with metals of the same type as well as many other metals. This includes GTAW (TIG), GMAW (MIG/MAG) and plasma welding. Pulsed arc welding is preferred for gas-shielded welding processes. The use of a multi-component shielding gas (Ar + He + H2 + CO2) is recommended for the MAG processes. For welding, VDM® Alloy 31 should be in a solution-annealed condition and free of scale, grease and markings. When welding the root, care should be taken to achieve best quality root protection using pure argon (argon 4.6) so that the welding edge is free of oxides after welding the root. Root protection is also recommended for the first and, in certain cases depending on the welded construction, also for the second intermediate layer weld after root welding. Any tempering colors must be removed while the welding edge is still hot, preferably using a stainless steel brush.