austenitic hastelloy c 22 alloy
"
ASTM B409 Incoloy 800 Rod Bar High Performance Nickel Iron Chromium Alloy
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
UNS N08825 Alloy Incoloy 825 Tubing Seamless For Oil And Gas
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
ASTM B407 UNS N08810 Incoloy 800H Pipe High Temperature Service Alloy
UNS N08810 is a nickel-iron-chromium alloy specifically designed for high-temperature service requiring good creep and rupture strength above 600C (1112F). It is a controlled chemistry version of UNS N08800 (Alloy 800), with tighter limits on carbon (0.05-0.10%) and a coarse grain size requirement (ASTM 5 or coarser) to optimize high-temperature properties. The alloy maintains an austenitic structure and offers excellent oxidation and carburization resistance, as well as
UNS N08811 Incoloy 800HT Pipe Seamless Nickel Iron Chromium Superalloy
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 High Temperature Inconel Superalloy For Aerospace Turbine High Strength
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,
High Strength Inconel 718 Precipitation Hardenable Nickel Chromium Superalloy
Inconel 718 is a precipitation-hardenable nickel-chromium superalloy that delivers exceptional strength from -423F (-253C) up to 1300F (700C). 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
