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Schweißbare Inconel 625-Legierung, 625-Superlegierung, hochfest, korrosionsbeständig
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 N07718 Hochtemperatur-Inkonel-Superlegierung für Luftfahrtturbinen mit hoher Festigkeit
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,
Hochfeste Inconel 718 Nickel-Chrom-Superlegierung mit außergewöhnlicher Schweißbarkeit und Temperaturbeständigkeit bis 1300 °F
High Strength Inconel 718 Precipitation Hardenable Nickel Chromium Superalloy 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,
Austenitische Korrosionsbeständige Hastelloy C-22 Nickellegierung für schwere chemische Verarbeitung
Hastelloy C-22: Ultimate Corrosion-Resistant Nickel Alloy Hastelloy C-22 is a fully austenitic, advanced corrosion-resistant nickel-chromium-molybdenum-tungsten alloy. It offers outstanding resistance to both uniform corrosion in oxidizing media and localized attack (pitting, crevice corrosion) in reducing environments. Unlike standard alloys, C-22 provides exceptional resistance to stress corrosion cracking (SCC), intergranular attack, and weld heat-affected zone (HAZ)
Hochtemperatursuperlegierung Luftfahrt Inconel 718 Runde Bar UNS N07718 Nickellegierung
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
