Inconel 718 Heat Treatment Guide - AMS 5662/5663, Aging Schedules & Machining Tips | Shanghai Hangbo Alloy Group

Date: 2026年8月15日 Categories: News Views: 231

By Shanghai Hangbo Alloy Group Co., Ltd. - China Supplier | ISO 9001:2015 | Est. 2012

Contact: sales@hangboalloy.com | hangbo@nickel-alloy.com | WhatsApp (Lisa): +86 13611656360

Quick Answer: What Is the Correct Inconel 718 Heat Treatment?

Inconel 718 (UNS N07718) requires a two-step precipitation-hardening cycle to reach 1,275+ MPa tensile: Solution anneal at 927-1010C (AMS 5662) or 954-982C (AMS 5663), followed by aging at 718C for 8 hours + 621C for 8 hours total (double age). The critical secret: the 718C/8h step precipitates gamma-double-prime (γ″) while the 621C/8h step precipitates fine gamma-prime (γ′) — together delivering peak strength. This guide covers both AMS conditions, machining, and cost.

The Two AMS Heat Treatment Schedules

Parameter AMS 5662 (Annealed) AMS 5663 (Solution)
Solution 927-1010C / 1h / AC 954-982C / 1h / AC
Age Step 1 718C / 8h / furnace cool 718C / 8h / furnace cool
Age Step 2 621C / 8h / AC 621C / 8h / AC
Tensile >= 1275 MPa >= 1275 MPa
Yield >= 1034 MPa >= 1034 MPa
Elongation >= 12% >= 12%

Difference: AMS 5663 specifies a tighter, higher solution temperature for grain-size control in critical rotating components.

Why Double Aging? (The Metallurgy)

Inconel 718 hardens via TWO precipitates:

  1. γ″ (Ni₃Nb) — precipitated at 718C; the PRIMARY strengthener. Tetragonal, disc-shaped.
  2. γ′ (Ni₃(Al,Ti)) — precipitated at 621C; secondary fine strengthening.

Aging only at 718C leaves coarse γ″ without the fine γ′ that provides additional strength and creep resistance. The 621C step is the "fine-tune."

Machining Inconel 718: 7 Practical Tips

Tip Detail
1. Carbide grades Use ceramic or coated carbide (CBN for finishing)
2. Speed 25-40 m/min turning (1/3 of steel speed)
3. Feed Heavy feed preferred (work-hardens rapidly)
4. Depth >= 0.5 mm per pass — skip spring passes
5. Coolant Flooded, high-pressure — never dry
6. Rigidity Rigid setup mandatory (chatter = work-hardening)
7. Tool angle Positive rake; hone edges

Condition & Product Matrix

Condition Tensile (MPa) Typical Use
Annealed (AMS 5662) 965-1170 Machining blanks, non-critical
Solution + Aged (AMS 5663) >= 1275 Aerospace fasteners, discs
Direct-Aged (DA) >= 1380 Highest strength, limited ductility
Cold-Worked 1400+ Springs, retainers

Price Guide (2026, EXW)

Form Price
Round Bar Ø50-150 mm \$28-45/kg
Plate 10-50 mm \$30-48/kg
Wire Ø2-5 mm \$35-55/kg

Inconel 718 vs A-286 (Quick Comparison)

Property 718 A-286
Tensile (aged) >= 1275 MPa >= 895 MPa
Max Temp 650C 700C
Cost 2-3x A-286 Baseline
Weldability Good (strain-age risk) Excellent

Why Buy From Shanghai Hangbo?

  • AMS 5662/5663 certified bars, plates, wire in stock.
  • EN 10204 3.1 MTC with chemistry + mechanicals per heat.
  • Triple aging performed in-house on request.
  • SGS/TUV/BV inspection available.
  • VIM+ESR melting traceability.

Contact & Complete Product Range

Shanghai Hangbo Alloy Group Co., Ltd. - China Supplier

Email: sales@hangboalloy.com | WhatsApp (Lisa): +86 13611656360 | www.nickel-alloy.com

All Grades

Ni: NI200-N6 | Monel: 400-502, K-500, R-405 | Inconel: 600-740H, X-750, 725 | Incoloy: 800-27-7MO | Hastelloy: C-276-HYBRID-BC1, N | Super Austenitic: 904L-AL-6XN | Chromium-Rich: Alloy 33 | High-Strength Stainless: Nitronic 50/60, PH13-8Mo | Chlorination: Alloy 45 | Nimonic: 75-263 | Haynes: 25-HR-160 | RA: 330/333 | Precision: 1J22-4J45 | High-Strength: 18Ni250-AerMet100 | Heating: Cr20Ni80/60 | Specialty: Alloy 20-602CA

Product Forms: Bars(6-500mm) | Tubes(OD 6-610mm) | Plates(0.1-100mm) | Forgings | Welded Pipes | Fittings | Wire(0.05-10mm) | Strip(0.02-4.0mm)

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