Incoloy 800h Nickel Alloy Seamless Tube Coil High Strength Corrosion Resistant 58% Ni 30% Elongation 800ht 825 925 Monel Inconel

Product Description

Company Profile

 

Product Description

1. Introduction

Inconel 601, also known as Alloy 601 or UNS N06601, is a nickel-chromium-based superalloy renowned for its exceptional resistance to high-temperature oxidation, corrosion, and mechanical degradation. Developed for applications requiring durability in extreme conditions, this alloy combines metallurgical stability with versatile processing capabilities, making it a cornerstone material in industries such as aerospace, energy, chemical processing, and thermal engineering. This comprehensive overview explores its composition, properties, manufacturing, applications, and technical specifications.

2. Chemical Composition

The alloy's unique performance stems from its carefully balanced :

 

• Nickel (Ni): 58-63%
• Chromium (Cr): 21-25%
• Iron (Fe): Balanced (typically ~10%)
• Aluminum (Al): 1.0-1.7%
• Carbon (C): ≤0.1%
• Manganese (Mn): ≤1.0%
• Silicon (Si): ≤0.5%
• Sulfur (S): ≤0.015%

 

The high nickel content provides resistance to chloride-ion stress corrosion and general corrosion. Chromium enhances oxidation resistance and protects against sulfidation, while aluminum forms a dense, adherent AlO oxide layer that prevents spalling even during thermal cycling. The face-centered cubic (FCC) lattice structure ensures metallurgical stability and ductility.

3. Key Properties

3.1 High-Temperature Oxidation Resistance

Inconel 601 excels in oxidizing environments up to 1,204°C (2,200°F). Its aluminum and chromium content promotes the formation of a self-healing oxide scale that resists cracking and peeling, even under cyclic heating and cooling. For example, at 1,100°C, the oxide layer remains stable, ensuring long-term protection. This property makes it ideal for applications like furnace components and exhaust systems.

3.2 Mechanical Strength

• Room Temperature:
  • Tensile Strength: 600-650 MPa (solution-treated/annealed)
  • Yield Strength: 240-300 MPa
  • Elongation: 30%
  • Hardness: ≤220 HB
• Elevated Temperatures:
  • At 1,000°C, tensile strength remains ~110 MPa, and yield strength ~85 MPa.
  • Creep rupture strength is optimized above 500°C due to controlled carbon content and grain size.

 

The alloy retains ductility after prolonged service, avoiding embrittlement common in other high-temperature materials.

3.3 Corrosion Resistance

• Aqueous Corrosion: Resistant to saltwater, acidic solutions, and alkalis.
• Sulfidation: High chromium and aluminum content protect against sulfur-bearing atmospheres.
• Stress Corrosion Cracking (SCC): The nickel-rich matrix mitigates SCC in chloride environments.

 

However, it is not recommended for strongly reducing or high-sulfur environments.

3.4 Physical and Thermal Properties

• Density: 8.1 g/cm³
• Melting Point: 1,320-1,370°C
• Thermal Expansion: 13-15 × 10/K (20-100°C)
• Thermal Conductivity: ~12 W/(m·K) at 100°C
• Electrical Resistivity: 1.290 µΩ·m at 20°C
• Modulus of Elasticity: 207 GPa at 20°C

4. Manufacturing and Processing

4.1 Production Methods

• Melting: Vacuum induction melting (VIM) or electroslag remelting (ESR) ensures purity and homogeneity.
• Casting: Used for complex shapes like turbine components, with sand casting and investment casting techniques employed.
• Forming: Hot working at 1,150-1,200°C and cold working with intermediate annealing (1,000-1,200°C) to reduce stress.

4.2 Heat Treatment

• Solution Treatment: 1,150-1,200°C followed by rapid cooling to dissolve carbides and improve corrosion resistance.
• Annealing: 1,000-1,200°C to relieve stress and optimize ductility.
• Aging: 870-925°C to enhance creep resistance through precipitate formation.

4.3 Machining and Welding

• Machining: Requires carbide tools with high cutting speeds (50-150 m/min) and coolant to minimize tool wear.
• Welding: Suitable for GTAW (TIG), GMAW (MIG), and laser welding. Use ERNiCrFe-11 or ENiCrFe-3 ,followed by post-weld heat treatment (1,120-1,170°C) to restore properties.

5. Applications

5.1 Aerospace Industry

• Gas Turbines: Combustion chambers, exhaust systems, and hot-section components requiring resistance to 1,100°C+.
• Aircraft Engines: Turbine blades and seals exposed to oxidative and thermal stress.

5.2 Energy and Power Generation

• Fossil Fuel Plants: Boiler tubes, superheaters, and reheaters in coal-fired power stations.
• Nuclear Industry: Steam generator tubing and reactor components due to resistance to radiation and corrosion.

5.3 Chemical Processing

• Reactors and Vessels: Handling corrosive media like acids, alkalis, and high-temperature gases.
• Heat Exchangers: Resisting fouling and degradation in petrochemical refining.

5.4 Thermal Processing

• Furnace Components: Trays, baskets, and fixtures for heat treatment processes up to 1,200°C.
• Industrial Heating Elements: Maintaining structural integrity in continuous operation.

5.5 Environmental Control

• Pollution Control Systems: Incinerator linings and exhaust stacks for waste-to-energy facilities.

6. Standards and Specifications

Inconel 601 complies with international standards, including:

 

• ASTM: B166 (bar/wire), B167 (pipe/tube), B168 (plate/sheet), B564 (forgings).
• ASME: SB166, SB167, SB168, SB564.
• ISO: ISO 6208 (forgings), ISO 9723 (bars).
• EN: W.Nr. 2.4851 (European designation).

 

These standards ensure consistency in composition, mechanical properties, and dimensional tolerances across global markets.

7. Advantages and Limitations

Advantages:

 

• Exceptional oxidation resistance at temperatures up to 1,200°C.
• High strength and ductility across a broad temperature range.
• Versatile processing capabilities (forming, welding, machining).
• Resistance to chloride SCC and sulfidation.

 

Limitations:

 

• Not suitable for strongly reducing or high-sulfur environments.
• Higher cost compared to stainless steels.
• Requires specialized tooling and techniques for machining and welding.

8. Conclusion

Inconel 601 stands as a testament to the advancements in superalloy engineering, offering a unique blend of high-temperature performance, corrosion resistance, and processability. Its ability to maintain structural integrity in extreme conditions has solidified its role in critical applications across aerospace, energy, and industrial sectors. As industries continue to demand materials capable of withstanding harsher environments, Inconel 601 remains a benchmark for reliability and innovation. By leveraging its metallurgical strengths and adhering to rigorous standards, engineers can confidently design systems that push the boundaries of thermal and chemical endurance.

 

Grades		Chemical Composition(wt)%
		C	Cr	Ni	Ti	Fe	Co	Mn	Si	Mo	Cu	W	p	s	Al	Nb	V	B	Zr	O+N	H
Inconel601	Max	0.1	25	-	-	15	-	1	0.5	-	1	-	0.03	0.015	1.7	-	-	-	-	-	-
	Min	-	21	-	-	10	-	-	-	-	-	-	-	-	1.0	-	-	-	-	-	-

 

Detailed Photos

 

Packaging & Shipping