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Ζυθοποιήσιμο Inconel 625 Σύνθετο 625 Υπερσύνθετο Υψηλής αντοχής στη διάβρωση
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 Υπερκράμα Inconel υψηλής θερμοκρασίας για τουρμπίνα αεροδιαστημικής υψηλής αντοχής
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,
Υψηλής αντοχής Inconel 718 Nickel Chromium Superalloy με εξαιρετική συγκολλητικότητα και αντοχή σε θερμοκρασίες έως 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,
Αυστενίτης ανθεκτικός στη διάβρωση Hastelloy C-22 Νικελικό κράμα για σκληρή χημική επεξεργασία
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)
Υψηλής θερμοκρασίας Superalloy Aerospace Inconel 718 Στρογγυλή ράβδος UNS N07718 Κράμα νικελίου
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
