Encontrado 19 productos para "

incoloy 825 alloy

"
Calidad UNS N06600 Tubo de aleación de níquel con resistencia a la corrosión por cloruro y a las grietas por esfuerzo Fábrica

UNS N06600 Tubo de aleación de níquel con resistencia a la corrosión por cloruro y a las grietas por esfuerzo

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

Calidad Aleación resistente a la corrosión del molibdeno del cromo del níquel de la barra redonda de Hastelloy C-276 Fábrica
Calidad Aumento de las emisiones de gases de efecto invernadero Fábrica

Aumento de las emisiones de gases de efecto invernadero

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)

Calidad N06022 Hastelloy C-22 aleación resistente a la corrosión ASTM B622 Fábrica

N06022 Hastelloy C-22 aleación resistente a la corrosión 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

Calidad UNS N10276 Aleación de níquel resistente a la corrosión de alto rendimiento Fábrica

UNS N10276 Aleación de níquel resistente a la corrosión de alto rendimiento

Aleación de níquel resistente a la corrosión UNS N10276 Aleación de alto rendimiento

Calidad Superaleación de alta temperatura Aeroespacial Inconel 718 Barra redonda UNS N07718 Aleación de níquel Fábrica

Superaleación de alta temperatura Aeroespacial Inconel 718 Barra redonda UNS N07718 Aleación de níquel

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

Calidad En el caso de los productos de la categoría 2 del presente anexo, se utilizará el término "productos de la categoría 2 del presente anexo". Fábrica

En el caso de los productos de la categoría 2 del presente anexo, se utilizará el término "productos de la categoría 2 del presente anexo".

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

Calidad N07718 Superaleación de inconel de alta temperatura para turbinas aeroespaciales de alta resistencia Fábrica

N07718 Superaleación de inconel de alta temperatura para turbinas aeroespaciales de alta resistencia

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,