Meaning
Nickel based superalloys containing niobium and molybdenum provide high strength and resistance to hydrogen embrittlement at elevated temperatures. Components made from alloy 718 are used in jet engines, gas turbines and high pressure oilfield equipment. The material is known for its excellent weldability and resistance to post weld cracking.
It maintains its mechanical properties from cryogenic temperatures up to approximately seven hundred degrees Celsius.
Material Specification
Chemical requirements for these alloys are governed by international standards like API 6ACRA or ASTM B637. Producing alloy 718 involves vacuum induction melting followed by vacuum arc remelting to ensure a high level of purity. The addition of niobium allows for precipitation hardening, which creates the strength needed for demanding structural applications.
Tight control of the grain size is required to maximize fatigue resistance in rotating parts.
Processing Path
Manufacturing sequences include forging, solution annealing and age hardening.
Thermal Stability
Resistance to softening at high temperatures allows the material to function in the hot sections of industrial machinery. While alloy 718 is durable, it can become susceptible to stress corrosion cracking if the heat treatment is not performed correctly. Designers must account for the expansion rates and creep strength of the material over long service lives.
The alloy remains a standard choice for parts that must survive both high stress and corrosive fluids.