Nickel & Cobalt Alloys

N06230 Supply Detail

Category

  • Bar and Rod

  • Plate and Sheet

  • Strip

  • Pipe and Tube

  • Wire

  • Welding

  • Powder Material

  • Cast Products

  • Forged Products

  • Fittings

  • Fastening

    Forms & Sizes

    Round Bar:
    φ2–500 mm, 1–6 m length

    Flat/Square Bar:
    4–100 mm thickness/width

    Hex Bar:
    A/F 3–100 mm

    Hollow Bar:
    OD 20–300 mm

    Forms & Sizes

    Sheet:
    0.3–6 mm thickness

    Medium Plate:
    6–25 mm thickness

    Heavy Plate:
    25–100 mm thickness

    Forms & Sizes

    Standard Strip:
    0.05–3 mm thick,
    10–600 mm wide

    Precision strip:
    0.01–0.5 mm thick,
    tight tolerance ±0.005 mm

    Foil:
    0.005–0.1 mm thick

    Forms & Sizes

    Seamless Tube:
    OD 6–450 mm,
    WT 1–50 mm,
    1–12 m length

    Welded Tube:
    OD 10–600 mm,
    WT 1–20 mm

    Capillary Tube:
    OD 1–10 mm,
    WT 0.1–2 mm

    Forms & Sizes

    Wire Form:
    Cold Drawn Wire,
    Bright Wire,
    Spring Wire,
    Fine Wire,
    Ultra-fine Wire

    General Diameter:
    φ0.1–10 mm

    Coil Weight:
    50–500 kg,
    customizable tolerance

    Forms & Sizes

    Solid Wire:
    φ0.8–4.0 mm

    Flux-cored Wire:
    φ1.2–4.0 mm

    Welding Rod:
    φ2.0–5.0 mm

    Forms & Sizes

    Powder Form:
    AM 3D Printing Powder,
    Spherical Powder,
    Gas-atomized Powder,
    Water-atomized Powder

    Particle Size:
    10–150 μm

    Sphericity:
    ≥90% for AM grade

    Forms & Sizes

    Cast Ingot:
    φ200–800 mm

    Precision Casting:
    min wall 0.5 mm

    Cast Pipe:
    OD 100–600 mm,
    WT 10–50 mm

    Forms & Sizes

    Forged Bar:
    Φ35–500 mm

    Forged Ring:
    OD 200–2000 mm

    Forging Weight:
    1–5000 kg

    Forms & Sizes

    Fittings Form:
    Elbow, Tee, Reducer, Flange, Cap, Outlet, Lap Joint

    Size range:
    1/2''–24'' (DN15–DN600)

    Wall thickness:
    Sch10–Sch160, STD, XS, XXS

    Pressure Class:
    150–2500 LB

    Forms & Sizes

    Fastening Form:
    Bolt, Nut, Screw, Stud, Washer, Pin, Rivet

    Metric: M3–M64

    Imperial: #4–2.5''

    Length: 6–500 mm

N06230 Product Description

Overview

N06230 is a nickel–chromium–tungsten–molybdenum alloy with a small lanthanum addition, combining excellent high-temperature strength, outstanding oxidation resistance and exceptional long-term thermal stability. This datasheet presents the material within the American (ASTM / ASME / SAE-AMS / UNS) standard system.

The nickel base with ~22% chromium and a lanthanum micro-addition gives outstanding resistance to oxidising environments for prolonged exposure to about 1149 °C (2100 °F), together with premier resistance to nitriding atmospheres. Tungsten (~14%) and molybdenum (~2%) provide solid-solution strengthening, while the alloy also offers lower thermal expansion than most high-temperature alloys and a pronounced resistance to grain coarsening with prolonged high-temperature exposure. A key attribute is its long-term stability: it does not form embrittling sigma or mu phases even after 16,000 hours of exposure between 649 and 870 °C, retaining excellent ductility.

It is readily fabricated, formed, welded and castable. It may be forged or hot-worked from ~1177 °C (2150 °F), and is readily cold-formed owing to its good ductility. Typical applications include gas-turbine combustion hardware and transition ducts, petrochemical and thermal-processing equipment, nitric-acid production, and other components requiring a balance of strength, oxidation/nitridation resistance and stability.

1. Physical Properties

Values per manufacturer (Haynes / Ulbrich) data, solution-annealed condition.

Property Value Unit
Density 8.97 g/cm³
Melting range 1301–1371 °C
Young's modulus (20 °C) 211 GPa
Specific heat capacity (21 °C) 397 J/kg·K
Thermal conductivity (20 °C) 8.9 W/m·K
Coefficient of thermal expansion (20–100 °C) 12.7 µm/m·°C
Electrical resistivity (20 °C) 1.25 µΩ·m
Maximum oxidation-resistance temperature ~1149 °C
Structure Austenitic (FCC)

2. Chemical Composition (Limiting, wt %)

Limiting composition per ASTM B435 (UNS N06230).

Element Symbol Min % Max % Role in Alloy
Nickel Ni Balance (47–65) Base element; FCC matrix
Chromium Cr 20.0 24.0 Oxidation + corrosion resistance
Tungsten W 13.0 15.0 Solid-solution strengthening
Molybdenum Mo 1.0 3.0 Solid-solution strengthening
Cobalt Co 5.0 Residual
Iron Fe 3.0 Residual
Manganese Mn 0.30 1.0 Deoxidiser; controls sulphur
Silicon Si 0.25 0.75 Deoxidiser
Aluminium Al 0.20 0.50 Oxidation resistance
Carbon C 0.05 0.15 Carbide strengthening
Lanthanum La 0.005 0.050 Oxide-scale adhesion (key micro-addition)
Boron B 0.015 Grain-boundary strengthening

Key feature: the lanthanum micro-addition improves oxide-scale adhesion, contributing to oxidation resistance to ~1149 °C and excellent thermal stability.

3. Mechanical Properties

Typical room-temperature properties, solution-annealed condition.

Property Value Source
Ultimate tensile strength ≥760 MPa (110 ksi) Solution-annealed (ASTM/Ulbrich min)
0.2% proof strength (yield) ≥310 MPa (45 ksi) Solution-annealed
Elongation at break ≥40 % Solution-annealed
Hardness ~90–95 HRB Solution-annealed

The alloy can be cold-rolled to various tempers for higher strength. Its outstanding thermal stability means it does not form sigma/mu phases even after very long mid-temperature exposure, retaining ductility. Values are typical or specified minima; confirm against the mill test certificate.

4. Oxidation and High-Temperature Resistance

Environment Performance Notes
High-temperature oxidation Outstanding To ~1149 °C (2100 °F) prolonged; La-stabilised scale
Nitriding atmospheres Premier A key advantage of alloy 230
Long-term thermal stability Outstanding No sigma/mu phase after 16,000 h at 649–870 °C
Thermal cycling Excellent Low expansion; scale adhesion
Grain coarsening Resistant Stable grain size at high temperature
High-temperature strength / creep Excellent W + Mo solid-solution + carbides
Carburisation Good Typical of high-Ni-Cr

5. Heat Treatment

A solid-solution nickel-base alloy; strengthened by solid solution, carbides and cold work. Heat treatment is solution annealing.

Solution Anneal Temperature: ~1177–1232 °C (2150–2250 °F), followed by rapid cooling Purpose: dissolves carbides, restores ductility and develops optimum properties.

Hot or cold worked parts are annealed and cooled rapidly to ensure the best balance of properties. Hot working is carried out from ~1177 °C (2150 °F). Owing to its thermal stability, the alloy resists embrittlement during service.

6. Weldability and Joining

Excellent welding and forming characteristics; welding behaviour is similar to Hastelloy X. Joined by gas-tungsten-arc (GTAW), gas-metal-arc (GMAW), shielded-metal-arc (SMAW) and resistance welding, using matching filler. The alloy is also castable.

Welding Process Applicability Filler / Consumable
GTAW / TIG · GMAW / MIG Excellent AWS A5.14 ERNiCrWMo-1 (matching 230 filler)
SMAW / stick Good AWS A5.11 ENiCrWMo-1
Resistance welding Good

Use matching-composition filler. Anneal and rapidly cool fabricated parts for the best balance of properties.

7. Machinability and Fabrication

Machining Guidelines

Parameter Recommendation
Work hardening Moderate-to-high; rigid setup, sharp tooling, positive rake
Cutting Low-to-moderate speed, ample feed; flood coolant
Preferred condition Solution-annealed

Forming Processes

Process Notes
Hot working From ~1177 °C (2150 °F)
Cold forming Readily cold-formed (good ductility); cold-rollable to tempers
Casting Castable by air-melt sand or vacuum methods
Solution anneal ~1177–1232 °C, rapid cool, after forming

8. Applications

Industry Typical Components Key Requirements
Gas turbines Combustion cans, transition ducts, hot-section hardware Oxidation to 1149 °C + strength + stability
Petrochemical Catalyst-grid supports, reformer/cracking hardware Nitridation + thermal stability
Thermal processing Furnace internals, fixtures, retorts Oxidation + grain-coarsening resistance
Nitric-acid production High-temperature process hardware Nitriding-environment resistance
Aerospace High-temperature ducting and structures Strength + low expansion
Power / energy High-temperature structural components Long-term thermal stability

9. Available Product Forms and Standards (ASTM / ASME / AMS System)

Product Form ASTM Standard ASME Code AMS
Sheet, strip and plate ASTM B435 ASME SB-435 AMS 5878
Bar and rod ASTM B572 ASME SB-572 AMS 5891
Forgings ASTM B564 ASME SB-564 AMS 5891
Seamless pipe and tube ASTM B622 ASME SB-622
Welded pipe / tube ASTM B619 / B626 ASME SB-619 / SB-626
Fittings ASTM B366 ASME SB-366
Welding consumables AWS A5.14 ERNiCrWMo-1 · AWS A5.11 ENiCrWMo-1 AMS 5839

Nickel-base high-temperature alloy. UNS N06230. ASME Boiler Code approved (e.g. Section I to 899 °C). GE B50TF246.

10. Comparison with Related Alloys (UNS System)

UNS Ni/Co Cr % Other Best Used For
N06230 Ni bal 20–24 W 14, Mo 2, La Oxidation to 1149°C + nitriding + stability
R30188 Co bal 20–24 W 14, Ni 22, La Cobalt-base; oxidation to 1095°C
R30605 Co bal 19–21 W 15, Ni 10 Cobalt-base; strongest fabricable Co alloy
N06002 Ni bal 20.5–23 Mo 9, Fe 18 Ni-base; combustor; oxidation to 1200°C
N06625 Ni bal 20–23 Mo 9, Nb Ni-base; aqueous corrosion + strength

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