Inconel 718 Nickel-Chromium-Iron Precipitation-Hardening Superalloy Seamless Tube

Inconel718 is a nickel-based superalloy renowned for its exceptional combination of:

Chemical Composition (wt%)

Element

Content (%)

Function

Ni (Nickel)

50-55

Base matrix, enhances corrosion resistance

Cr (Chromium)

17-21

Oxidation resistance

Fe (Iron)

Balance

Cost-effective reinforcement

Nb (Niobium)

4.75-5.5

Primary strengthening phase (γ”) formation

Mo (Molybdenum)

2.8-3.3

Solid-solution strengthening

Ti (Titanium)

0.65-1.15

Secondary strengthening phase (γ’) formation

Al (Aluminum)

0.35-0.7

Oxidation protection

C (Carbon)

≤0.08

Minimizes carbide precipitation

Mn (Manganese)

≤0.35

Sulfur neutralization

Si (Silicon)

≤0.35

Deoxidation

P (Phosphorus)

≤0.015

Minimizes brittleness

S (Sulfur)

≤0.015

Reduces hot cracking

Property

Value

Test Standard

Size Range

OD: 6-610mm, WT: 0.5-50mm

ASTM B829

Hardness

35-40 HRC (after aging)

ASTM E18

Density

8.19 g/cm³

ASTM E112

Yield Strength

≥1030 MPa (RT)

ASTM E8

Tensile Strength

≥1275 MPa (RT)

ASTM E8

Elongation

≥12%

ASTM E8

Thermal Conductivity

11.5 W/m·K (100°C)

ASTM E1461

I. Performance Characteristics

1. High-Temperature Performance

1.1 Maintains stable mechanical properties from -253°C to 700°C, with a short-term service life limit of 982°C

1.2 Excellent creep resistance, due to the precipitation strengthening effect of the γ’ phase (Ni3Nb)

1.3 Ranks among the highest yield strength alloys below 650°C

2. Corrosion Resistance

2.1 Resists attack by acids, alkalis, salts, and media containing hydrogen sulfide and chlorides

2.2 Forms a dense Cr₂O₃ oxide film on the surface, with an oxidation resistance temperature of up to 800°C

3. Mechanical Properties

3.1 Tensile strength ≥1300 MPa, yield strength >1000 MPa

3.2 Combines high ductility (elongation ≥12%) with fatigue resistance

4. Processing Advantages

4.1 Excellent weldability, no tendency to crack after welding

4.2 Highly sensitive to heat treatment, requiring precise control of process parameters.

II. Main Applications

1. Aerospace

1.1 High-temperature components such as engine turbine discs, combustion chambers, and nozzles

1.2 Rocket engine casings and fuel delivery pipelines

2. Energy and Chemicals

2.1 Nuclear reactor structural materials and fuel element cladding

2.2 Oil well casing and corrosion-resistant valves in oil and gas production

3. Special Industrial Applications

3.1 High-temperature automotive turbocharger piping

3.2 Seawater-resistant hydraulic system piping for ships

Surface Treatment

Why Choose Us ?

Applications & Industries

titanium alloy bars are used to make aircraft structural components

Aerospace:

High-power density actuators.

Electronics:

Precision sensors & MEMS components.

titanium alloys bars are used to make heat exchangers

Energy:

Magnetic coupling devices for turbines.

Workshop & Packaging

  • Manufacturing: Cold drawing process with controlled annealing
  • Quality Control: Eddy current testing for defects
  • Packaging: VCI (Vapor Corrosion Inhibitor) wrapping + shock-proof crates

Frequently Asked Questions

Q1: Can Inconel718 be used in cryogenic environments?

Yes, it retains toughness down to -253°C (liquid hydrogen temperature).

Typically 4-6 weeks with expedited options available.

Inconel718 offers higher strength but lower pitting resistance.

Recommended for full strength recovery (720°C/8h aging).

A: Yes, it retains toughness and stability from -253°C to 700°C due to its γ”/γ’ precipitation phases.

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