PYRAD49D Nickel alloys
Spécifications
- Common nameHASTELLOY X
- EUNiCr21Fe18Mo9
- USAUNS:N06002
Typical composition
- C0,09
- NiBase
- Cr22
- Mo9
- Si≤ 1.00
- Mn≤ 1.00
- Co1,5
- W18,5
Applications
• Sheet fabrications for jet engines.
• Guide vanes for jet engines.
• Injection nozzles and cones.
• Hot gas manifolds.
• Combustion chamber components.
• Sheet fabrications and hearths for furnaces operating continuously at 1100 °C.
Mechanical properties
Precipitation hardened, nickel-based superalloy with:
• Very good resistance to oxidation.
• Very good mechanical properties at high temperatures.
Mechanical features
- Heat treatmentH
- UTS (N/mm²)790
- A (%)54
- Solution treated : H
Annealed : R - Thermo-mechanical treatment : TM
Quenched and tempered : T+RV - Sub-zero treatment : F
Solution treated and aged : T+RV
PYRAD49D_FR
Download
(PDF, 316 KB)