MOQ: | 150kgs |
Price: | Negotiatable |
Standard Packaging: | Wood box |
Delivery Period: | 2-30days |
Payment Method: | L/C,D/A,D/P,T/T,Western Union,MoneyGram |
Supply Capacity: | 300 Ton per Month |
Nimonic 263 Rod: High-Performance Nickel-Cobalt Alloy for Extreme Environments
Nimonic 263 Rod (UNS N07263, W. Nr. 2.4650) is a high-strength, age-hardenable nickel-cobalt-chromium-molybdenum alloy engineered for demanding applications in gas turbines and other high-temperature environments. Renowned for its exceptional fabrication characteristics and intermediate temperature tensile ductility, it is ideally suited for components requiring both strength and formability.
Element | Min (%) | Max (%) |
---|---|---|
C | 0.04 | 0.08 |
Si | – | 0.40 |
Mn | – | 0.60 |
S | – | 0.007 |
Ag | – | 0.0005 |
Al | 0.30 | 0.60 |
B | – | 0.005 |
Bi | – | 0.0001 |
Co | 19.0 | 21.0 |
Cr | 19.0 | 21.0 |
Cu | – | 0.20 |
Fe | – | 0.70 |
Mo | 5.60 | 6.10 |
Pb | – | 0.002 |
Ti | 1.90 | 2.40 |
Ti+Al | 2.40 | 2.80 |
Ni | Balance | – |
Condition | Tensile Strength (MPa) | Yield Strength (MPa) | Elongation (%) | Operating Temp. (°C) |
---|---|---|---|---|
Annealed | 800–1000 | – | – | Up to 800 |
Annealed + Aged | 1000–1200 | – | – | Up to 800 |
Spring Temper | 1200–1500 | – | – | Up to 800 |
Spring Temper + Aged | 1000–1200 | – | – | Up to 800 |
Property | Value |
---|---|
Density | 8.36 g/cm³ |
Melting Point | 1300-1355 °C |
Coefficient of Expansion | 10.3 μm/m·°C |
Modulus of Elasticity | 224 kN/mm² |
Condition | Temperature (°C) | Time | Cooling Method |
---|---|---|---|
Solution Treatment | 1150 | 1.5–2.5 hrs | Water Quench |
Age Hardening | 800 | 8 hrs | Air Cooling |
MOQ: | 150kgs |
Price: | Negotiatable |
Standard Packaging: | Wood box |
Delivery Period: | 2-30days |
Payment Method: | L/C,D/A,D/P,T/T,Western Union,MoneyGram |
Supply Capacity: | 300 Ton per Month |
Nimonic 263 Rod: High-Performance Nickel-Cobalt Alloy for Extreme Environments
Nimonic 263 Rod (UNS N07263, W. Nr. 2.4650) is a high-strength, age-hardenable nickel-cobalt-chromium-molybdenum alloy engineered for demanding applications in gas turbines and other high-temperature environments. Renowned for its exceptional fabrication characteristics and intermediate temperature tensile ductility, it is ideally suited for components requiring both strength and formability.
Element | Min (%) | Max (%) |
---|---|---|
C | 0.04 | 0.08 |
Si | – | 0.40 |
Mn | – | 0.60 |
S | – | 0.007 |
Ag | – | 0.0005 |
Al | 0.30 | 0.60 |
B | – | 0.005 |
Bi | – | 0.0001 |
Co | 19.0 | 21.0 |
Cr | 19.0 | 21.0 |
Cu | – | 0.20 |
Fe | – | 0.70 |
Mo | 5.60 | 6.10 |
Pb | – | 0.002 |
Ti | 1.90 | 2.40 |
Ti+Al | 2.40 | 2.80 |
Ni | Balance | – |
Condition | Tensile Strength (MPa) | Yield Strength (MPa) | Elongation (%) | Operating Temp. (°C) |
---|---|---|---|---|
Annealed | 800–1000 | – | – | Up to 800 |
Annealed + Aged | 1000–1200 | – | – | Up to 800 |
Spring Temper | 1200–1500 | – | – | Up to 800 |
Spring Temper + Aged | 1000–1200 | – | – | Up to 800 |
Property | Value |
---|---|
Density | 8.36 g/cm³ |
Melting Point | 1300-1355 °C |
Coefficient of Expansion | 10.3 μm/m·°C |
Modulus of Elasticity | 224 kN/mm² |
Condition | Temperature (°C) | Time | Cooling Method |
---|---|---|---|
Solution Treatment | 1150 | 1.5–2.5 hrs | Water Quench |
Age Hardening | 800 | 8 hrs | Air Cooling |