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Inconel 718

Inconel ® alloy 718

Precipitation hardenable alloy which gives corrosion resistance and high strength with excellent weldability. Excellent creep rupture strength at temperatures up to 700C. Uses include gas turbines, rocket motors, nuclear reactors and pumps.

Good strength/ductility properties from sub-zero temperatures to over 760°C

Excellent corrosion resistance and fatigue resistance in a wide variety of corrosive chemicals including seawater and industrial acids

Non-magnetic and spark resistant

Excellent resistance to stress corrosion cracking

Applications

Oil and Gas Industry:

  • Wellhead components, Safety Valves, Packers, Fasteners, Clamps, Downhole equipment for corrosive/sour service.

 

Nuclear Power Plant:

  • Containment vessels, Valves
  • Engineering applications between 760°C and cryogenic temperatures

 

Key Features:

  • Excellent corrosion resistance
  • Resistant to chloride stress corrosion
  • Resistant to sulphide stress cracking
  • High fatigue strength in seawater
  • High Strength and hardness
  • Low magnetic permeability

 

 


Inconel 718 Wire UNS No 7718

Inconel 718 Wire UNS No 7718
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Rs 4,500  / KgPrice on Request

Minimum Order Quantity: 1 Kg

Product Brochure

Wire Gauge36 SWG
TypeNickel Wire
ColorSilvery White
ApplicationIndustry
GradeNickel Base Alloy
Powder Or NotNot Powder
Introduction

Inconel 718, designated as UNS N07718 and Werkstoff Nr. 2.4668, is a nickel-chromium-iron superalloy that has gained worldwide acceptance for its exceptional mechanical strength, weldability, fatigue resistance, and corrosion resistance.

In its wire form, Inconel 718 becomes one of the most versatile materials for high-performance springs, fasteners, heating elements, aerospace components, and oilfield tools. The wire can be supplied in diameters ranging from 0.1 mm fine wire to several millimeters heavy wire depending on application needs.

 

Unlike many other superalloys that are difficult to weld or form, Inconel 718 wire offers excellent weldability, formability, and age-hardening capability, making it highly valuable in industries such as aerospace, defense, nuclear, oil & gas, marine, and medical.

 Chemical Composition of Inconel 718 Wire

 

ElementContent (%)
Nickel (Ni) 50.0 – 55.0
Chromium (Cr) 17.0 – 21.0
Iron (Fe) Balance
Niobium (Nb) + Tantalum (Ta) 4.75 – 5.50
Molybdenum (Mo) 2.80 – 3.30
Titanium (Ti) 0.65 – 1.15
Aluminum (Al) 0.20 – 0.80
Cobalt (Co) ≤ 1.0
Manganese (Mn) ≤ 0.35
Silicon (Si) ≤ 0.35
Carbon (C) ≤ 0.08
Copper (Cu) ≤ 0.30
Boron (B) ≤ 0.006
Mechanical Properties (Age-Hardened)
  • Tensile Strength: ~1375 MPa

  • Yield Strength (0.2%): ~1035 MPa

  • Elongation: 12–20%

  • Hardness: ~363 HB

  • Excellent fatigue resistance

  • Creep rupture strength maintained up to 650 °C

Physical Properties
  • Density: 8.19 g/cm³

  • Melting Range: 1260 – 1336 °C

  • Elastic Modulus: 200 GPa

  • Thermal Conductivity: 11.4 W/m·K

  • Specific Heat: 435 J/kg·K

  • Electrical Resistivity: 125 μΩ·cm

  • Magnetic Properties: Non-magnetic (annealed)

Quality Control & Testing
  • Tensile Testing: Ensures strength.

  • Bend Test: For spring wires.

  • Corrosion Testing: For marine and chemical uses.

  • NDT: Eddy current and ultrasonic inspection.

  • Dimensional Check: Diameter tolerance per ASTM/AMS.




Additional Information:

  • Item Code: UNSNO7718
  • Production Capacity: In kgs
  • Delivery Time: READY STOCK
  • Packaging Details: The packaging of the product is done using an effective method of packaging. It all includes- • Shrink-wrapping • Bubble wrapping • Carton boxes • Wooden crates/pallets/boxes

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Inconel 718 Sheet (UNS No 7718)

  • Inconel 718 Sheet (UNS No 7718)
  • Inconel 718 Sheet (UNS No 7718)
  • Inconel 718 Sheet (UNS No 7718)
  • Inconel 718 Sheet (UNS No 7718)
  • Inconel 718 Sheet (UNS No 7718)
  • Inconel 718 Sheet (UNS No 7718)
Inconel 718 Sheet (UNS No 7718)
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Rs 3,000  / KilogramPrice on Request

Minimum Order Quantity: 10 Kilogram

Product Brochure

Thickness6 mm
Grade718
ShapeRectangle
MaterialSteel
Usage/ApplicationIndustry
ApplicationIndustrial
Introduction to Inconel 718 Sheet

Inconel 718, designated as UNS N07718, is a high-strength, corrosion-resistant nickel-chromium alloy that is extensively used in environments exposed to extreme temperatures, pressure, and aggressive corrosion. When manufactured in sheet form, it is widely employed in aerospace structures, gas turbines, chemical processing equipment, nuclear reactors, and marine applications.

The sheet form of this alloy offers superior formability, fatigue resistance, and creep strength, which makes it ideal for components that require precision fabrication and long service life in high-stress environments.

Chemical Composition

The chemical composition of Inconel 718 is carefully engineered to balance mechanical performance and corrosion resistance:

 

ElementPercentage (%)
Nickel (Ni) 50.0 – 55.0
Chromium (Cr) 17.0 – 21.0
Iron (Fe) Balance
Niobium (Nb) + Tantalum (Ta) 4.75 – 5.50
Molybdenum (Mo) 2.80 – 3.30
Titanium (Ti) 0.65 – 1.15
Aluminum (Al) 0.20 – 0.80
Cobalt (Co) ≤ 1.0
Carbon (C) ≤ 0.08
Manganese (Mn) ≤ 0.35
Phosphorus (P) ≤ 0.015
Sulfur (S) ≤ 0.015
Silicon (Si) ≤ 0.35
Copper (Cu) ≤ 0.30
Boron (B) ≤ 0.006
Mechanical Properties

One of the defining strengths of Inconel 718 sheets is their impressive mechanical profile, especially under high temperatures and long-term loads:

PropertyValue
Tensile Strength Up to 1380 MPa
Yield Strength Up to 1100 MPa
Elongation ~12–23%
Hardness (Rockwell C) 33–45 HRC
Operating Temperature Range −250°C to 704°C
Creep Rupture Strength Excellent
Fatigue Resistance Outstanding
 Heat Treatment and Strengthening Mechanism

Inconel 718 achieves its strength through precipitation hardening via the formation of γ'' (gamma double prime – Ni3Nb) and γ' (gamma prime – Ni3(Al, Ti)) phases.

Specifications and Standards

Inconel 718 Sheets must comply with several international specifications for quality and traceability:

 

StandardDescription
ASTM B670 Standard Specification for Nickel-Chromium-Iron Alloy (UNS N07718) Sheet, Strip, and Plate
AMS 5596 Aerospace Specification for Sheet and Strip
ASME SB-670 Boiler and Pressure Vessel Code
ISO 15156 / NACE MR0175 For use in H₂S-containing environments in oil and gas production
Common Thicknesses
  • 0.8 mm, 1 mm, 2 mm, 3 mm, 4 mm, 5 mm

 



Additional Information:

  • Production Capacity: IN TONS
  • Delivery Time: READY STOCK
  • Packaging Details: The packaging of the product is done using an effective method of packaging. It all includes- • Shrink-wrapping • Bubble wrapping • Carton boxes • Wooden crates/pallets/boxes

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Inconel 718 Round Bar (Uns No 7718)

  • Inconel 718 Round Bar (Uns No 7718)
  • Inconel 718 Round Bar (Uns No 7718)
  • Inconel 718 Round Bar (Uns No 7718)
  • Inconel 718 Round Bar (Uns No 7718)
  • Inconel 718 Round Bar (Uns No 7718)
  • Inconel 718 Round Bar (Uns No 7718)
Inconel 718 Round Bar (Uns No 7718)
Get Best Quote
Rs 3,000  / KgPrice on Request

Minimum Order Quantity: 10 Kg

Product Brochure

Length6 meter
Grade718
ShapeRound
BrandIMPORTED
TypeBar
Material GradeINCONEL 718
Single Piece Length3 meter, 6 meter
Size0.1MM - 500MM
Usage/ApplicationIndustrial
MaterialInconel 718
 Introduction

Inconel 718 (UNS N07718 / W.Nr. 2.4668) is a nickel-chromium superalloy that has earned global recognition for its exceptional combination of high strength, corrosion resistance, and remarkable weldability. Unlike many other nickel alloys, Inconel 718 maintains outstanding performance from cryogenic temperatures up to about 704 °C (1300 °F).

 

The round bar form of Inconel 718 is widely used in industries such as aerospace, oil & gas, marine, chemical processing, and nuclear engineering, where both mechanical reliability and corrosion resistance are critical. Its ability to resist creep, stress rupture, fatigue, and oxidation makes it ideal for rotating parts, fasteners, shafts, and components exposed to extreme thermal and mechanical loads.

Chemical Composition of Inconel 718 Round Bar

 

ElementPercentage (%)
Nickel (Ni) 50.0 – 55.0
Chromium (Cr) 17.0 – 21.0
Iron (Fe) Balance
Niobium (Nb) + Tantalum (Ta) 4.75 – 5.50
Molybdenum (Mo) 2.80 – 3.30
Titanium (Ti) 0.65 – 1.15
Aluminum (Al) 0.20 – 0.80
Cobalt (Co) ≤ 1.0
Manganese (Mn) ≤ 0.35
Silicon (Si) ≤ 0.35
Carbon (C) ≤ 0.08
Copper (Cu) ≤ 0.30
Boron (B) ≤ 0.006
 Mechanical Properties (Annealed Condition)
  • Tensile Strength: ~1375 MPa

  • Yield Strength (0.2% offset): ~1035 MPa

  • Elongation: ~12 – 20%

  • Hardness: ~363 HB

  • Fatigue Strength: Excellent under cyclic loads

  • Creep-Rupture Strength: Outstanding up to 650 °C

Physical Properties
  • Density: 8.19 g/cm³

  • Melting Range: 1260 – 1336 °C

  • Elastic Modulus: ~200 GPa

  • Thermal Conductivity: 11.4 W/m·K at 100 °C

  • Specific Heat: 435 J/kg·K

  • Electrical Resistivity: 125 μΩ·cm

  • Magnetic: Non-magnetic in annealed condition

Testing & Quality Control
  • Mechanical Testing: Tensile, impact, hardness.

  • Corrosion Tests: Pitting and crevice testing.

  • NDT: Ultrasonic, Eddy current, MPI.

  • Dimensional Accuracy: Tolerances per ASTM/ASME.

  • Microstructural Analysis: To ensure correct γ′/γ″ precipitation.




Additional Information:

  • Production Capacity: 20 TONS
  • Delivery Time: READY STOCK
  • Packaging Details: The packaging of the product is done using an effective method of packaging. It all includes- • Shrink-wrapping • Bubble wrapping • Carton boxes • Wooden crates/pallets/boxes

View Complete details

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Inconel 718 Plate (UNS No 7718)

  • Inconel 718 Plate (UNS No 7718)
  • Inconel 718 Plate (UNS No 7718)
  • Inconel 718 Plate (UNS No 7718)
  • Inconel 718 Plate (UNS No 7718)
  • Inconel 718 Plate (UNS No 7718)
  • Inconel 718 Plate (UNS No 7718)
Inconel 718 Plate (UNS No 7718)
Get Best Quote
Rs 1,800  / KilogramPrice on Request

Minimum Order Quantity: 10 Kilogram

Product Brochure

TypePlate
Grade718
Usage/ApplicationChemical Handling
Plate TypeInconel Plate
 Introduction

Inconel 718, also known by its UNS designation N07718 and Werkstoff Nr. 2.4668, is one of the most widely used nickel-chromium superalloys in demanding engineering applications. Developed in the 1960s, it became a cornerstone alloy for aerospace engines, gas turbines, oil & gas equipment, and chemical process plants due to its unique balance of high strength, corrosion resistance, weldability, and fatigue performance.

 

In its plate form, Inconel 718 offers engineers a versatile material that can be cut, machined, formed, and fabricated into critical components such as heat shields, turbine casings, structural panels, and pressure vessel plates. Unlike some superalloys, Inconel 718 combines excellent mechanical strength with good fabrication properties, making it the preferred material for both high-temperature and cryogenic applications.

Chemical Composition of Inconel 718 Plate

 

ElementContent (%)
Nickel (Ni) 50.0 – 55.0
Chromium (Cr) 17.0 – 21.0
Iron (Fe) Balance
Niobium (Nb) + Tantalum (Ta) 4.75 – 5.50
Molybdenum (Mo) 2.80 – 3.30
Titanium (Ti) 0.65 – 1.15
Aluminum (Al) 0.20 – 0.80
Cobalt (Co) ≤ 1.0
Manganese (Mn) ≤ 0.35
Silicon (Si) ≤ 0.35
Carbon (C) ≤ 0.08
Copper (Cu) ≤ 0.30
Boron (B) ≤ 0.006
Mechanical Properties (Typical, Age-Hardened Condition)
  • Tensile Strength: ~1375 MPa

  • Yield Strength (0.2%): ~1035 MPa

  • Elongation: 12–20%

  • Hardness: ~363 HB

  • Creep-Rupture Strength: Excellent up to 650 °C

  • Fatigue Life: Very high under cyclic stresses

Physical Properties
  • Density: 8.19 g/cm³

  • Melting Range: 1260 – 1336 °C

  • Elastic Modulus: 200 GPa

  • Thermal Conductivity: 11.4 W/m·K at 100 °C

  • Specific Heat: 435 J/kg·K

  • Electrical Resistivity: 125 μΩ·cm

  • Magnetic Behavior: Non-magnetic (annealed condition)

 Heat Treatment and Microstructure

The strength of Inconel 718 plate is derived from precipitation hardening involving two primary phases:

  • γ′ (Ni₃(Al,Ti)) → enhances strength.

  • γ″ (Ni₃Nb) → main hardening phase unique to Inconel 718.

Testing & Quality Assurance
  • Chemical Analysis: Spectrographic and wet analysis.

  • Mechanical Testing: Tensile, hardness, impact tests.

  • Corrosion Testing: Pitting, crevice, intergranular corrosion.

  • NDT: Ultrasonic, radiographic, eddy current inspection.

  • Dimensional Tolerance: Per ASTM B670 and AMS standards.




Additional Information:

  • Production Capacity: IN TONS
  • Delivery Time: READY STOCK
  • Packaging Details: The packaging of the product is done using an effective method of packaging. It all includes- • Shrink-wrapping • Bubble wrapping • Carton boxes • Wooden crates/pallets/boxes

View Complete details

Yes! I am Interested Request a call back

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