incoloy nickel iron chromium alloy
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ASTM B407 UNS N08810 Incoloy 800H Rohr-Hochtemperatur-Dienstlegierung
UNS N08810 Hochtemperatur-Einsatzlegierung ASTM B407
UNS N06600 Nickellegierungsrohr mit Chlorid-Spannungskorrosionsrissbeständigkeit
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
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
Korrosionsbeständige Hastelloy C-276-Rundstab-Nickel-Chrom-Molybdän-Legierung
Hastelloy C-276 Korrosionsbeständige Nickellegierung
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)
Hohe Festigkeit Inconel 718 Niederschlaggehärtetes Nickel-Chrom-Superlegierung
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
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,
