corrosion resistant hastelloy c 276
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고강성 인코넬 625 UNS N06625 합금
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
높은 온도 크립 저항 인콜로이 800HT 튜브 UNS N08811 니켈 철 크롬 합금
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
산 내성 SS316 꿰매지 않는 파이프 저탄소 황에 대한 우수한 저항성
Acid-resistant 316 seamless tube is a premium austenitic stainless steel product specifically designed for service in acidic and chemically aggressive environments. The addition of 2-3% molybdenum distinguishes this grade from standard 304, providing significantly enhanced resistance to a wide range of acids, including sulfuric, phosphoric, acetic, and organic acids, as well as chloride-induced pitting and crevice corrosion. The seamless manufacturing process ensures uniform
고강성 인코넬 718 니켈 크롬 초연금, 예외적인 용접성과 1300°F까지의 온도 저항성
High Strength Inconel 718 Precipitation Hardenable Nickel Chromium 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,
UNS N08800 인콜로이 800 합금 800 파이프 니켈 철 크롬 합금 주문
Incoloy 800 is a nickel-iron-chromium alloy designed for exceptional strength and metallurgical stability under prolonged high-temperature service. With a nominal composition of 30-35% nickel and 19-23% chromium, this austenitic alloy maintains its microstructure even after extended exposure to elevated temperatures, offering excellent resistance to oxidation, carburization, and corrosion in both high-temperature and aqueous environments. Unlike standard stainless steels,
UNS N08825 석유 및 가스용 합금 인콜로이 825 튜브
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 B409 Incoloy 800 로드 바 고성능 니켈 철 크롬 합금
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 N07718 항공우주 터빈용 고온 인코넬 초연금
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,
고온 초연금 항공 우주 인코넬 718 원형 막 UNS N07718 니켈 합금
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
