incoloy 825 alloy
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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
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)
UNS N06022 Hastelloy C-22 Legierung Korrosionsbeständig ASTM B622
UNS N06022 is a nickel-chromium-molybdenum alloy renowned for its exceptional resistance to both oxidizing and reducing corrosive media. With a higher chromium content than C-276, plus controlled additions of tungsten, this alloy offers superior resistance to pitting, crevice corrosion, and stress-corrosion cracking in aggressive environments. UNS N06022 provides outstanding performance in wet chlorine, hydrochloric acid, sulfuric acid, and mixed acid solutions where many
UNS N10276 Nickellegierung, korrosionsbeständig, hohe Leistung
Korrosionsbeständige Hochleistungslegierung aus Nickellegierung UNS N10276
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
ASTM B407 UNS N08810 Incoloy 800H Rohr-Hochtemperatur-Dienstlegierung
UNS N08810 Hochtemperatur-Einsatzlegierung ASTM B407
Hohe Festigkeit Inkonel 625 UNS N06625 Legierung Korrosionsbeständig
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 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,
