Alloy 80A (UNS N07080) – High-Performance Nickel-Chromium Alloy for Extreme Environments

Alloy 80A (UNS N07080) – High-Performance Nickel-Chromium Alloy for Extreme Environments

# Alloy 80A (UNS N07080) – High-Performance Nickel-Chromium Alloy for Extreme Environments

Introduction to Alloy 80A

Alloy 80A, also known by its UNS designation N07080, is a high-performance nickel-chromium alloy specifically designed to withstand extreme environments. This superalloy combines excellent mechanical properties with outstanding resistance to oxidation and corrosion, making it a preferred choice for demanding applications across various industries.

Chemical Composition

The unique properties of Alloy 80A stem from its carefully balanced chemical composition:

  • Nickel (Ni): 70-80%
  • Chromium (Cr): 18-21%
  • Iron (Fe): ≤ 3.0%
  • Aluminum (Al): 1.0-2.0%
  • Titanium (Ti): 1.8-2.7%
  • Carbon (C): ≤ 0.10%
  • Other trace elements

Key Properties and Characteristics

Mechanical Strength

Alloy 80A maintains excellent tensile and creep strength at elevated temperatures, with typical tensile strength ranging from 800 to 1000 MPa at room temperature.

Oxidation Resistance

The high chromium content provides outstanding oxidation resistance at temperatures up to 1100°C (2012°F), making it suitable for high-temperature applications.

Corrosion Resistance

Alloy 80A demonstrates superior resistance to various corrosive environments, including sulfur-containing atmospheres and carburizing conditions.

Applications

Due to its exceptional properties, Alloy 80A finds applications in several critical industries:

  • Aerospace components (turbine blades, combustion chambers)
  • Power generation (gas turbine components)
  • Chemical processing equipment
  • Nuclear reactors
  • Heat treatment fixtures

Fabrication and Heat Treatment

Alloy 80A can be fabricated using standard techniques, though it requires special considerations:

  • Hot working should be performed between 1050-1200°C
  • Solution annealing at 1080-1120°C followed by rapid cooling
  • Aging treatment at 700-800°C to optimize mechanical properties

Comparison with Similar Alloys

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Property Alloy 80A Inconel 600 Nimonic 80A
Max Service Temp 1100°C 1150°C 1050°C
Tensile Strength 800-1000 MPa 550-690 MPa 900-1100 MPa
Primary Application Gas turbines Chemical processing
October 2025
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