Nickel-Legierungen

Incoloy 800 is a nickel-iron-chromium alloy designed for exceptional strength and metallurgical stability under prolonged high-temperature service. With a nominal composition of 30-35% nickel and 19-23% chromium, this austenitic alloy maintains its microstructure even after extended exposure to elevated temperatures, offering excellent resistance to oxidation, carburization, and corrosion in both high-temperature and aqueous environments. Unlike standard stainless steels,

Inconel 625: The Ultimate Superalloy for Extreme Environments Inconel 625 is a nickel-chromium-molybdenum superalloy with niobium addition. This unique combination delivers exceptional high-temperature strength (from cryogenic to 1800°F/982°C) combined with outstanding corrosion resistance—including resistance to pitting, crevice corrosion, and oxidation. Unlike many high-strength alloys requiring complex heat treatment, Inconel 625 derives its strength from a solid solution

UNS N06625 is a nickel-chromium-molybdenum alloy with outstanding corrosion resistance and high strength over a broad temperature range from cryogenic to 980°C (1800°F). The addition of niobium (columbium) and tantalum provides exceptional resistance to pitting, crevice corrosion, and chloride ion stress-corrosion cracking. Unlike many high-temperature alloys, UNS N06625 does not rely on precipitation hardening for strength. Instead, it derives its high tensile and creep

UNS N07718 is a precipitation-hardenable nickel-chromium alloy containing significant amounts of iron, niobium, and molybdenum, along with minor additions of aluminum and titanium. Developed specifically for high-temperature and high-stress applications, this superalloy has become the standard material across aerospace, energy, and oil & gas industries. The alloy combines excellent corrosion resistance with exceptional mechanical strength and outstanding weldability,

Inconel 718 is a precipitation-hardenable nickel-chromium superalloy that delivers exceptional strength from -423°F (-253°C) up to 1300°F (700°C). Its unique combination of high tensile strength, fatigue resistance, creep rupture properties, and excellent weldability sets it apart from other high-strength superalloys. Unlike many precipitation-hardened alloys that are prone to post-weld cracking, Inconel 718 exhibits outstanding weldability – even in complex, thin-walled

UNS N07718 is a precipitation-hardenable nickel-chromium alloy containing significant amounts of iron, niobium, and molybdenum, along with minor additions of aluminum and titanium. Developed in the 1960s for jet engines and gas turbines, this superalloy has become the standard material across aviation, energy, space, and offshore industries. The alloy combines corrosion resistance with high strength and outstanding weldability, including resistance to post-weld cracking. UNS

UNS N06600 High Temperature Nickel Alloy Tube - Heat Resistant Nickel Chromium Alloy UNS N06600 (Inconel 600) is a nickel-chromium alloy specifically designed for high-temperature and corrosion-resistant applications. With a nominal composition of 72% Ni + 14-17% Cr, this alloy offers excellent oxidation resistance up to 1093°C (2000°F), good strength at elevated temperatures, and outstanding resistance to chloride-ion stress-corrosion cracking. The high-temperature nickel

Inconel 600 (UNS N06600, W.Nr. 2.4816, Alloy 600) is a standard engineering material that has proven itself across industries for over half a century. This nickel-chromium alloy delivers an exceptional combination of high temperature strength (up to 2000°F / 1093°C), excellent corrosion resistance, and superior workability. Unlike many high-performance alloys, Inconel 600 is not precipitation hardenable – it is strengthened only by cold work. This characteristic, combined

UNS N08810 Hochtemperatur-Einsatzlegierung ASTM B407