16Co14Ni10Cr2Mo1
High-Strength16Co14Ni10Cr2Mo1
Co-Ni secondary-hardening ultra-high-strength steel (AF1410-type, GJB 2294).
Chemical Composition (%)
| C | 0.13 |
|---|---|
| CO | 13.5 |
| NI | 9.5 |
| CR | 1.8 |
| MO | 0.9 |
| TI | 0.015 |
Mechanical Properties
Tensile Strength:≥1515 MPa;Yield Strength:≥1380 MPa;Fracture Toughness KIC:≥110 MPa·m½
Chinese Standard
GJB 2294 16Co14Ni10Cr2Mo1
Equivalent Standards
AF1410
Equivalent Grades
UNS K92580
Applications
Aircraft structural forgings, fracture-critical parts.
Available Forms
Bar, Forging
Uses
Nickel/cobalt-base superalloy retaining high strength, creep and corrosion resistance at extreme temperature. Cobalt (≈14%) raises hot corrosion and wear resistance. Used in gas-turbine blades, aero-engine hot sections, combustors and advanced energy systems.
Heat Treatment
Solution treated 1050–1250 °C and aged (≈700–900 °C) to precipitate γ′/γ″ strengtheners; processed via vacuum induction + VAR/ESR for cleanliness.
Precautions
Machining is difficult — use ceramic/PCBN tools, generous coolant and rigid setups. Keep clean (vacuum/inert melting) to avoid inclusions; avoid contamination by low-melting elements.
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