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Alloys primarily of nickel and chromium. These are usually chosen for their behaviour at high temperatures, either resistance to chemical and physical erosion, or to mechanical creep . Pages in category "Nickel–chromium alloys"
Machinability is the ease with which a metal can be cut permitting the removal of the material with a satisfactory finish at low cost. [1] Materials with good machinability (free machining materials) require little power to cut, can be cut quickly, easily obtain a good finish, and do not cause significant wear on the tooling.
Originally developed to produce oxide-dispersion strengthened (ODS) nickel- and iron-base superalloys for applications in the aerospace industry, [1] MA has now been shown to be capable of synthesizing a variety of equilibrium and non-equilibrium alloy phases starting from blended elemental or pre-alloyed powders. [2]
Monel alloy 405, also known as Monel R405, is the free-machining grade of alloy 400. [26] The nickel, carbon, manganese, iron, silicon & copper percent remains the same as alloy 400, but the sulfur is increased from 0.024 max to 0.025-0.060%. Alloy 405 is used chiefly for automatic screw machine stock and is not generally recommended for other ...
Upload file; Search. Search. Appearance. Donate; Create account; ... Download as PDF; Printable version; ... Nickel alloys are alloys with nickel as principal element.
Inconel alloys are oxidation- and corrosion-resistant. When heated, Inconel forms a thick, stable, passivating oxide layer protecting the surface from further attack. Inconel retains strength over a wide temperature range, attractive for high-temperature applications where aluminum and steel would succumb to creep as a result of thermally ...
Hiduminium or R.R. alloys (2% copper, iron, nickel): used in aircraft pistons Hydronalium (up to 12% magnesium, 1% manganese): used in shipbuilding, resists seawater corrosion Italma (3.5% magnesium, 0.3% manganese): formerly used to make coinage of the Italian lira
René 41 is a nickel-based high temperature alloy developed by General Electric.It retains high strength in the 600–1,000 °C (1,200–1,800 °F) temperature range. It is used in jet engine and missile components, and other applications that require high strength at extreme temperatures.