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Article Delving into The Popular Heat-Treating Methods of Specialty Alloys Image

Heat treating boosts a metal’s workability, which helps manufacturers modify metals to meet the specific requirements of an application. Critical in manufacturing high-quality products, this thermal process involves heating a metal to near or just above its critical temperature, holding it there for a time, and then cooling the metal in a medium, such as air, water, brine, or molten salts. Heat treating alters a metal’s mechanical properties, metallurgical structure, or residual stress state. Manufacturers also use heat treating in making other materials, including glass.

Several types of heat treating exist. They include annealing, normalizing, hardening, tempering, and induction hardening. The different types of heat treatment are used for different purposes. Heat treating improves a metal’s machinability, boosts its wear resistance and durability, and improves its strength, toughness, and elasticity. Plus, it alters a metal’s longevity and magnetic properties. Heat treating is ideal for modifying various metals, including aluminum, stainless steel, and nickel and cobalt alloys.

Heat Treating Aluminum Alloys

Manufacturers use the term “heat-treatable” to differentiate those aluminum alloys that can be strengthened by heating and cooling versus those that can’t. “Non-heat-treatable” alloys depend mainly on cold work to increase strength, while other alloys utilize heating to decrease strength and ductility, a process called annealing. Heat treating increases the strength of aluminum alloys and encompasses a three-step process:

  • Solution
    Heat Treatment: This step involves heating an alloy to a suitable temperature, at which
    it’s held until one or more constituents enter into a solid solution. The aluminum
    is then cooled rapidly to hold these constituents in solution.
  • Quenching:
    This step involves the rapid cooling of the workpieces
    in water, oil, or air to obtain specific material properties (development of supersaturation).
  • Age
    Hardening: The final step involves
    the spontaneous hardening of a metal that takes place after it’s quenched and
    then stored at ambient temperature or treated with mild heat

Aluminum alloys commonly used in aircraft and other aerospace structures include 7068, 7075, 6061, 6063, 2024, 5052, and 7050. They’re also used in manufacturing automotive parts, including wheels, engine components, and aluminum suspensions.

Heat Treating Stainless Steel

Stainless steel is a poor conductor of heat. So, manufacturers often harden stainless steels, like Custom 455, by cold working them and then heat treating them. Custom 455 comes in 4 different specs, AMS 5860, AMS 5672, AMS 5617, and AMS 5578. These stainless steels yield different properties depending on how they are heat treated. For example, AMS 5617 wire is cold drawn or shaved after solution heat treatment, depending on the spec and alloy shape.

Four types of heat-treating methods for stainless steel exist—austenitic, ferritic, and martensitic stainless steel, and precipitation hardening. Manufacturers use these different methods based on the different characteristics of the steel grades. Stainless steel is used widely in the food and beverage, construction and architecture, power generation, and oil, gas, and chemical processing industries.

Heat Treating Nickel and Cobalt Alloys

Nickel and cobalt alloys feature great strength and wear-resistant properties at high temperatures. They may be subjected to one or more of five principal types of heat treatment, depending on chemical composition, fabrication requirements, and intended service. These methods include  

  • Annealing—generally
    carried out at temperatures between 705 and 1205°C to produce a recrystallized
    grain structure and softening in work-hardened alloys.
  • Stress
    Relieving—involves
    temperatures for nickel and nickel alloys ranging from 425 to 870°C to remove
    or reduce stresses.
  • Stress
    Equalizing—helps balance stresses in
    cold-worked material without significantly decreasing the mechanical strength
    produced by cold working
  • Solution
    Treating—deposits age-hardening
    constituents and carbides into a solid solution through a high-temperature
    treatment.
  • Age
    Hardening—conducted at intermediate
    temperatures (425 to 870°C) and used to develop maximum strength by
    precipitation of a dispersed phase throughout the matrix.

Popular nickel alloys include Incoloy 909, Inconel 718, Inconel 625, and Inconel 601, while MP35N, L-605, and Hayne 188 represent the most prevalent cobalt alloys.

These alloys often replace steel in aircraft jet engines, with the most popular use for the high-temperature cobalt alloy being in gas turbine (turbojet) aircraft engines. Additional applications for nickel and cobalt alloys include engine plumbing, pumps, valves, piping systems, processing equipment, turbines, assemblies, tools, chemical processing, and oil and gas well piping.

Image by Михаил Каменский from Pixabay

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