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Υψηλής θερμοκρασίας ανθεκτικό στην έλξη Incoloy 800HT Tube UNS N08811 Nickel Iron Chromium Alloy
UNS N08811 is a nickel-iron-chromium alloy specifically designed for high-temperature service with exceptional creep and rupture strength. It is a controlled chemistry version of UNS N08800 (Alloy 800), with tighter limits on carbon (0.06-0.10%), aluminum (0.15-0.60%), and titanium (0.15-0.60%) to optimize high-temperature performance. The alloy maintains an austenitic structure and offers excellent oxidation and carburization resistance, as well as good corrosion resistance
Αντίσταση στην οξείδωση και την καρβουρίωση Incoloy 800H Nickel Iron Chromium Alloy
Incoloy 800H is a nickel-iron-chromium superalloy specifically designed and optimized for exceptional creep and rupture strength at elevated temperatures. Unlike the standard Incoloy 800 grade, Alloy 800H features a controlled carbon content range of 0.05-0.10%, which provides significantly enhanced mechanical stability and performance in the 593°C to 982°C (1100°F to 1800°F) service temperature range. This austenitic alloy maintains a stable microstructure even after
ASTM B409 Incoloy 800 Rod Bar High Performance Nickel Iron Chromium
ASTM B409 Incoloy 800 is a nickel-iron-chromium alloy designed for high temperature service where both oxidation resistance and good corrosion resistance are required. Unlike standard stainless steels, Incoloy 800 maintains its strength and structural stability at elevated temperatures. Product Specifications Parameter Details Product Name Incoloy 800 / Alloy 800 / Incoloy® 800 UNS Designation N08800 Werkstoff Nr. 1.4876 British Standard BS 3075 NA15, BS 3076 NA15 Chinese
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
UNS N08825 Σύνθεση Incoloy 825 Σωλήνες χωρίς ραφή για πετρέλαιο και φυσικό αέριο
UNS N08825 is a nickel-iron-chromium alloy with significant additions of molybdenum, copper, and titanium. This austenitic nickel-iron-chromium alloy is specifically designed to provide exceptional resistance to both reducing and oxidizing acids, as well as stress-corrosion cracking and pitting in chloride-containing environments.What sets UNS N08825 apart is its stabilized structure – the addition of titanium prevents intergranular corrosion after welding, making it suitable
High Strength Inconel 625 UNS N06625 Κράμα Ανθεκτικό στη Διάβρωση
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
ΑΣΤΜ Β407 UNS N08810 Incoloy 800H Σωλήνες υψηλής θερμοκρασίας
UNS N08810 Κράμα υπηρεσίας υψηλής θερμοκρασίας ASTM B407
UNS N08811 Incoloy 800HT Σωλήνες χωρίς συγκόλληση Νικέλιο Σιδήρου Χρωμίου Υπερσυσκευάσματα
Incoloy 800HT represents the highest-performance member of the Incoloy 800 series of nickel-iron-chromium superalloys. Specifically engineered for maximum creep and rupture strength at elevated temperatures, Alloy 800HT features a tightly controlled chemistry with enhanced aluminum and titanium content combined with a precisely regulated carbon range of 0.06-0.10%. Compared to both standard Alloy 800 and Alloy 800H, this premium grade offers superior high-temperature
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,
