Nimonic 115 Bars

Nimonic 115 bars are a form of chromium-nickel-cobalt superalloy. This alloy contains a nominal composition of 16 wt. Per cent nickel, 15 wt. per cent chromium, and two wt. Percent cobalt. The atoms combine to form a face-centred, cubic crystal structure and give high alloy strength at elevated temperatures. Notable characteristics of Nimonic 115 bars include excellent oxidation properties, resistance to carburization, and resistance to sulfidation and chloride ion stress corrosion cracking. Additionally, their relatively high creep rupture strength makes them an ideal choice for aerospace applications that require components that can operate at elevated temperatures without suffering from premature fatigue or melting from heat soak caused by the friction of air friction against the material surface during flight.

115 Nimonic bars are widely used for high temperatures and dynamic load applications. Its excellent high-temperature strength characteristics make it an ideal material for components in gas turbines, thermal engines, and rocket motors. Nimonic 115 has outstanding tensile strength and positive features like resistance to stress rupture, creep deformation, and hot corrosion. Additionally, this nickel-base alloy provides excellent wear resistance at elevated temperatures. This makes it an ideal material to be used in various aircraft parts that may also include piston engine components. In short, the versatility of Nimonic 115 bars makes them one of the most preferred alloys across a broad range of industries where temperature capability plays a significant role in their application requirements.