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Model No: Alloy 718

UNS N07718 / Alloy 718 / 2.4668

ZYTC Alloy is a certified manufacturer of high-performance alloy 718 (UNS N07718 / 2.4668) nickel superalloy. Our products meet AMS and ASTM standards and are available in bar, plate, billet, and custom forgings. Request a free quote and technical data today.
Delivery :
FOB
minimum order :
50 kilograms
Supply Ability :
5000kilograms / Month
Stock Time :
7-10Day
Country of Origin :
CHINA
Quantity :
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ZYTC Alloy 718 (UNS N07718) Precipitation-Hardenable Nickel Superalloy 

As an ISO 9001 and AS9120 certified supplier, ZYTC Alloy presents this technical guide for Inconel 718 for confident material evaluation.

I. Product Information

  • Material Name: Inconel 718 Nickel-Chromium Superalloy (UNS N07718 / W.Nr. 2.4668)
  • Material Definition: A precipitation-hardenable nickel-chromium superalloy offering exceptional high strength, creep resistance, and fatigue life up to 704°C (1300°F) , with oxidation resistance to 982°C (1800°F) .
  • Core Value Proposition: Maintains high mechanical properties at elevated temperatures while offering excellent weldability. Slow aging response reduces cracking risk during heat treatment.
  • Key Advantages: Precipitation strengthened (γ'' phase) | Slow aging response for better weldability | NACE compliant for sour service | Versatile heat treatment options
  • Certification: ISO 9001 and AS9120 certified
  • Product Forms: Bar & Rod | Plate, Sheet & Strip | Tube & Pipe | Wire | Forgings & Rings | Fasteners

II. Material Standards & Specifications

AMS Standard

Product Form

AMS 5589/5590

Tubing

AMS 5596/5597

Foil, Plate, Sheet, Strip

AMS 5662/5663/5664

Bar, Forgings, Rings

AMS 5832/5962

Wire, Bar

*NACE MR0175/ISO 15156 compliant for sour service.*

 

III. Chemical Composition (wt%)

Element

Min

Max

Ni+Co

50.0

55.0

Cr

17.0

21.0

Nb+Ta

4.75

5.50

Mo

2.80

3.30

Ti

0.65

1.15

Al

0.20

0.80

Fe

Balance

-

C

-

0.08

Mn

-

0.35

Si

-

0.35

B

-

0.006

Co

-

1.0

 

IV. Service Conditions & Material Selection Boundaries

Suitable Conditions:

  1. Elevated Temperature High-Stress: Up to 704°C (1300°F) for strength-critical components
  2. Aerospace Propulsion: Jet engine rotating parts requiring high fatigue/creep resistance
  3. Sour Gas Service: H₂S environments per NACE MR0175
  4. Cryogenic Applications: Excellent low-temperature toughness
  5. Welded Assemblies: Can be welded before final aging

Typical Applications:

  • Aerospace: Turbine disks, blades, shafts, rocket motor components
  • Oil & Gas: Wellhead equipment, BOPs, downhole tools, sour service valves
  • Energy: Gas turbine components, nuclear reactor internals
  • Industrial: High-strength fasteners, springs, cryogenic storage

Selection Boundaries:

  • >704°C Continuous Service: Consider Inconel 625 or 601
  • Severe Aqueous Corrosion: Consider Inconel 625 or Hastelloy C-276
  • Oxidation >982°C: Consider Inconel 601 or 602 CA
  • Cost-Sensitive: Consider 17-4 PH or A-286

 

V. Manufacturing Process & Heat Treatment

Heat Treatment:

Process

Parameters

Outcome

Solution Anneal

925-1010°C + rapid quench

Dissolves elements; recrystallizes

Standard Aging

718°C/8hr → 620°C/18hr

Maximum strength (γ'' precipitate)

Alternate Aging

760°C single step

Improved ductility

NACE Aging

Specialized cycle

Sour service compliance

Fabrication:

  • Welding: Excellent using GTAW/TIG. Use matching filler metal. Can be aged after welding.
  • Hot Working: 927-1065°C (1700-1950°F)
  • Machining: Requires rigid setups, positive feeds, sharp tooling

 

VI. Mechanical Properties

Condition

Tensile Strength

Yield Strength

Elongation

Solution Annealed

965 MPa (140 ksi)

550 MPa (80 ksi)

45%

Standard Aged

1380 MPa (200 ksi)

1100 MPa (160 ksi)

20%

NACE Compliant

1240 MPa (180 ksi)

965 MPa (140 ksi)

20%

Hardness: Aged condition ~40 HRC. Contact for certified test reports.

VII. Material Comparison Guide

Dimension

Alloy 718

Alloy 625

Alloy 600

Primary Strength

Highest Strength to 704°C

Strength + Corrosion

High-Temp Oxidation

Strengthening

Precipitation (γ'')

Solid-Solution

Solid-Solution

Max Temp (Strength)

704°C (1300°F)

982°C (1800°F)

1093°C (2000°F)

Yield Strength

1100 MPa (160 ksi)

414 MPa (60 ksi)

240-345 MPa

Weldability

Excellent

Excellent

Excellent

Corrosion Resistance

Good

Excellent

Very Good

Typical Use

Jet engines, oil & gas tools, high-strength fasteners

Marine, chemical, FGD

Furnace, nuclear, caustic

Procurement Recommendation:

  • Choose alloy 718 for maximum strength up to 704°C in aerospace rotating components, high-pressure oil & gas tools, and sour service applications.
  • Choose alloy 625 for strength + corrosion resistance across high-temperature and aqueous environments.
  • Choose alloy 600 for cost-effective high-temperature service where extreme strength not required.

 

Request a Quote or Sample Today:

For aerospace, oil & gas, or energy applications demanding Inconel 718's exceptional high-strength performance, contact ZYTC Alloy today.

Contact us for a free sample and competitive quote. Our technical team is ready to assist with material selection and heat treatment specifications.

Contact Us:

Email:daisy@zytcsteel.com

WhatsApp/WeChat: +86 17335753350