# Alloy 601 (UNS N06601) High-Temperature Nickel-Chromium-Iron Material
## Introduction to Alloy 601
Alloy 601, also known by its UNS designation N06601, is a high-performance nickel-chromium-iron material designed for extreme temperature applications. This alloy combines excellent mechanical properties with outstanding resistance to oxidation and carburization, making it a preferred choice for demanding industrial environments.
## Chemical Composition
The unique properties of Alloy 601 stem from its carefully balanced chemical composition:
– Nickel (Ni): 58-63%
– Chromium (Cr): 21-25%
– Iron (Fe): Balance
– Aluminum (Al): 1.0-1.7%
– Carbon (C): 0.10% max
– Manganese (Mn): 1.0% max
– Silicon (Si): 0.50% max
– Copper (Cu): 1.0% max
– Sulfur (S): 0.015% max
## Key Properties and Characteristics
### High-Temperature Performance
Alloy 601 maintains excellent mechanical strength at elevated temperatures up to 2200°F (1200°C). The aluminum content in the alloy forms a protective oxide scale that enhances its resistance to oxidation and scaling.
### Corrosion Resistance
The material exhibits outstanding resistance to:
– Oxidation in air up to 2200°F (1200°C)
– Carburizing environments
– Sulfur-containing atmospheres
– Nitriding conditions
– Chloride stress corrosion cracking
### Mechanical Properties
Typical room temperature mechanical properties include:
– Tensile Strength: 85-110 ksi (586-758 MPa)
– Yield Strength: 35-80 ksi (241-552 MPa)
– Elongation: 30-55%
## Applications of Alloy 601
Due to its exceptional properties, Alloy 601 finds use in numerous demanding applications:
### Industrial Heating
– Radiant tubes
– Muffles
– Retorts
– Furnace rollers and belts
### Chemical Processing
– Catalyst grids in nitric acid production
– Combustion chambers
– Thermal reactors
### Power Generation
– Heat exchangers
– Superheater tubes
– Combustion liners
### Aerospace
– Afterburner components
– Combustion chambers
– Turbine seals
## Fabrication and Welding
Alloy 601 can be readily fabricated using standard techniques:
### Forming
The material can be hot or cold worked, though hot working is preferred for heavy reductions. Annealing at 1900-2100°F (1038-1149°C) is recommended after cold working.
### Welding
Common welding methods include:
– Gas tungsten arc welding (GTAW/TIG)
– Gas metal arc welding (GMAW/MIG)
– Shielded metal arc welding (SMAW)
Post-weld heat treatment is generally not required but may be beneficial for some applications.
## Comparison with Similar Alloys
Alloy 601 offers several advantages over comparable materials:
### vs. Alloy 600
– Better oxidation resistance at high temperatures
– Higher creep rupture strength
– Improved carburization resistance
### vs. Alloy 800H/HT
– Superior oxidation resistance
Keyword: Alloy 601 UNS N06601
– Better mechanical properties at elevated temperatures
– More resistant to thermal cycling
## Standards and Specifications
Alloy 601 is covered by numerous international standards, including:
– ASTM B168 (Plate, sheet, and strip)
– ASTM B166 (Rod, bar, and wire)
– ASTM B167 (Seamless pipe and tube)
– AMS 5711 (Aerospace material specification)
– DIN 2.4851 (German standard)
## Conclusion
Alloy 601 (UNS N06601) stands out as a versatile high-temperature material that combines excellent oxidation resistance