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Forged Inconel 718 rings and high-performance industrial components

Inconel 718 Forging: High-Strength Aerospace & Energy Components

Inconel 718 forging is the process of shaping nickel-chromium superalloys under extreme heat and pressure to optimize grain flow and structural integrity for high-temperature environments. Common applications include turbine disks, compressor blades, rocket engine thrust chambers, downhole tool shafts, and high-pressure valve bodies.

Inconel 718 Forging: High-Strength Aerospace & Energy Components

Precision forged Inconel 718 (UNS N07718) engineered for high-stress applications up to 700°C. ForceBeyond provides AS9100-certified forging solutions with optimized grain refinement from our co-owned global facilities.

As a core pillar of our comprehensive Superalloy Forging Services, ForceBeyond specializes in the precision manufacturing of Inconel 718 (UNS N07718) components. Engineered for mission-critical environments, our forged 718 provides a superior structural alternative to cast parts, offering the refined grain structure and fatigue resistance required for high-stress applications up to 700°C (1,292°F).

Leveraging our Tier-1.5 “Tri-Regional” model, we provide US-based engineering oversight with high-capacity production from our co-owned facilities in South Korea and Taiwan, ensuring both metallurgical excellence and supply chain resilience.

Inconel 718 Precision Forged Component

The Tier-1.5 Forging Advantage: From Billet to Finished Part

Traditional supply chains are fragmented, forcing you to manage separate forge and machine shops. ForceBeyond’s Tier-1.5 model integrates Inconel 718 Forging with our precision Inconel 718 Machining centers.

By taking total ownership of the metallurgical lifecycle, we ensure:

  • Controlled Grain Flow: Optimizing the forging process to align grain flow with the part’s primary stress axes.
  • Reduced Buy-to-Fly Ratio: Near-net-shape forging techniques that minimize raw material waste and machining cycle times.
  • Single-Source Traceability: Full heat-lot documentation from the initial melt through forging, heat treatment, and final NDT.

While our forging process optimizes grain flow for high-stress rotating components, parts with extremely complex internal cooling channels or non-symmetrical housings may be better suited for our Inconel 718 Casting solutions utilizing Vacuum Induction Melting (VIM).

Why Forged Inconel 718?

Inconel 718 is a precipitation-hardenable nickel-chromium alloy. While casting is common for complex static parts, forging is mandatory for rotating or high-pressure components. Our forging process breaks down the cast dendritic structure and creates a directed grain flow, significantly increasing fatigue life and structural reliability.

The Mechanical Advantage

  • Yield Strength: Retains 1,035 MPa at temperatures up to 700°C (1,292°F).
  • Creep Resistance: Optimized for long-term stability under high-stress thermal loads.
  • Workability: Excellent weldability and cryogenic properties compared to other nickel superalloys.

Technical Specifications & Standards

We forge Inconel 718 to comply with the most stringent global standards, ensuring seamless integration into Tier-1 aerospace and energy supply chains.

Industry Standards Compliance

  • Aerospace: AMS 5662 (Solution Annealed), AMS 5663 (Precipitation Hardened)
  • Oil & Gas: NACE MR0175 / ISO 15156
  • General: ASTM B637, UNS N07718
Mechanical Properties (Forged & Aged)
Property Metric Imperial
Tensile strength 1,275 MPa 185 ksi
Yield strength 1,035 MPa 150 ksi
Elongation 12%–15% 12%–15%
Reduction of area 15%–20% 15%–20%
Typical hardness 36–44 HRC 36–44 HRC
Density 8.19 g/cm³ 0.296 lb/in³

Specialized Forging Processes for 718

  • Closed-Die Forging: For high-precision, near-net-shape turbine disks and compressor blades.
  • Seamless Rolled Rings: Ideal for engine casings and structural rings up to 3,500mm OD.
  • Open-Die Forging: Cost-effective for shafts, custom blocks, and prototypes up to 5,000kg.

Quality Assurance & NDT Protocol

Every Inconel 718 forging undergoes rigorous testing at our co-owned facilities to ensure zero defects:

  • Ultrasonic Testing (UT): Performed to AMS 2154 standards to identify internal inclusions or porosity.
  • Fluorescent Penetrant Inspection (FPI): For surface crack detection in complex geometries.
  • Macro-Etch Testing: To verify the integrity and directionality of the forged grain flow.
  • Mechanical Verification: Tensile and creep testing on witness coupons from every heat lot.

FAQ: Sourcing Inconel 718 Forgings

How does ForceBeyond manage Inconel 718 lead times?

By maintaining a strategic billet inventory in our USA and Asian hubs, we can often bypass the 40+ week mill delays, delivering custom forgings in 14-18 weeks.

What is the difference between AMS 5662 and AMS 5663?

AMS 5662 is for material in the solution-treated condition (easier to machine). AMS 5663 is for material that has been precipitation (age) hardened for maximum strength.

Request an Inconel 718 Technical Consultation

Direct access to our Delaware-based engineering team. Feasibility reviews delivered within 48 hours.

Sources

Our Internal Resources for Die Casting, Investment casting, Forging and Sand Casting