incoloy 825 alloy
"
UNS N06600 Nikkelgelegeerde buis met chloride-stresscorrosie-kraakbestendigheid
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
Corrosiebestendige Hastelloy C-276 Ronde staaf Nickel Chroom Molybdeen legering
Hastelloy C-276 corrosiebestendige nikkellegering
Austenitische corrosiebestendige Hastelloy C-22 nikkellegering voor zware chemische verwerking
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 legering corrosiebestendig 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 Nikkellegering Corrosiebestendig, hoge prestaties
UNS N10276 Corrosiebestendige nikkellegering Hoogwaardige legering
Hoogtemperatuur Superlegering Aerospace Inconel 718 Ronde staaf UNS N07718 Nikkellegering
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 buis met hoge temperatuur
UNS N08810 Hoge temperatuur servicelegering ASTM B407
Hoge sterkte Inconel 625 UNS N06625 Corrosiebestendig legering
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 Inconel-superlegering op hoge temperatuur voor lucht- en ruimtevaartturbine Met hoge sterkte
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,
