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UNS N07718 Inconel Superalloy อุณหภูมิสูงสำหรับกังหันการบินและอวกาศที่มีความแข็งแรงสูง
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,
ความแข็งแรงสูง Inconel 718 ฝนแข็งไนเคิลโครเมียม 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, Inconel 718 exhibits outstanding weldability – even in complex, thin-walled
Incoloy 825 บาร์โลหะผสมที่ทนต่อการกัดกร่อน 825 UNS N08825 สำหรับการแปรรูปทางเคมี
Incoloy 825 is a nickel-iron-chromium alloy engineered for exceptional corrosion resistance in a wide range of demanding environments. The chemical composition of this nickel-based alloy, fortified with molybdenum, copper, and titanium, provides superior performance against reducing acids like sulfuric and phosphoric acid, as well as oxidizing media such as nitric acid. Unlike many corrosion-resistant alloys that excel only in specific environments, Incoloy 825 offers
ASTM B409 Incoloy 800 สตาร์บาร์ ความสามารถสูง นิเคิลเหล็ก โครเมียมสกัด
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
สารสับสนุนความร้อนสูง Aerospace Inconel 718 Round Bar UNS N07718 สารสับสนุนนิเคิล
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
Inconel 625 UNS N06625 ความแข็งแรงสูงทนต่อการกัดกร่อนของโลหะผสม
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
อุณหภูมิสูง ทนต่อการลากลาก Incoloy 800HT Tube UNS N08811 นิเคิลเหล็กโครเมียมสกัดเหล็ก
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
UNS N06600 ท่อโลหะผสมนิกเกิลที่มีความต้านทานการกัดกร่อนจากการแตกร้าวความเครียดจากคลอไรด์
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
