inconel incoloy tube

Thus precipitation-hardening treatments are not required. This combination of elements also is responsible for superior resistance to a wide range of corrosive environments of unusual severity as well as to high-temperature effects such as oxidation and carburization.

Inconel 600 alloy is a nickel-chromium stabilized alloy. It has very good oxidation resistance at higher temperatures. In addition, it has excellent resistance to carburizing and chloride-containing atmospheres. It is a non-magnetic alloy with very good mechanical properties. Inconel 601 is a chromium and nickel based material for applications requiring heat and corrosion resistance. This material stands out for its resistance to high temperature oxidation.
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800H can not be corroded in many kinds of media. Its high nickel content made it have good stress corrosion resistance cracking properties in the water corrosion condition. High Chromium content made it can better resist pitting and crevice corrosion cracking. This alloy can resist nitric acid and organic acid corrosion, but it is not so fine in the sulfuric acid and hydrochloric acid.

Inconel 601 nickel-chromium-iron alloy is a general-purpose engineering material for applications that require resistance to heat and corrosion. The outstanding characteristic of Inconel 601 is its resistance to high-temperature oxidation. The alloy also has good resistance to aqueous corrosion, has high mechanical strength, and is readily formed, machined, and welded.

Alloy 718 was initially developed for the aerospace industry but its excellent strength and corrosion resistance were recognised by the oil industry and it is now widely used in this field as well.

Alloy 718 is a nickel-chromium alloy which can be heat-treated to give high strength, good corrosion resistance, ease of formability and which can be welded with good resistance to strain age cracking. The alloy can be used at temperatures up to 700oC.

Alloy 718 for the oil industry is heat treated such that the hardness does not exceed 40HRC which is the maximum allowed by NACE MR-01-75/ ISO 15156: 3 to prevent stress corrosion cracking. The major applications in this field are Valves and precision tubing.

Alloy 718 for aerospace and power generation is heat treated to give maximum strength and high creep resistance with typical hardness values exceeding 42HRC. The major applications are components for gas turbines, aircraft engines, fasteners and other high strength applications.

Our Inconel 625 Piggable Bend is very tough at extremely high temperatures and resists corrosion caused by caustic alkalis in the chemical industry. We manufacture UNS N06600 Inconel 600 Long Radius Elbow is niobium stabilized for the aerospace industry, while Inconel WNR 2.4851 Welded Elbow has high yield strength and can be hot and cold worked.

UNS N07718 Inconel Long Radius Elbows are 1.5 times larger than the nominal diameter of the pipe and withstand high pressure and heat. Industries such as cement and sugar use Inconel elbows for better and uniform product flow. Premium Inconel ASTM B366 UNS N06625 Seamless Bends, Bend Radius Range R=3D-10D, Bend Angles From 10 Degrees To 180 Degrees, Available From Stock.

Nickel Inconel 601 is a member of the austenitic nickel-chromium based super alloys. It is used for applications that require extremely high resistance to heat, and very high resistance to oxidation and corrosion at higher temperatures. It has excellent mechanical properties and is easily workable with standard procedures.

Alloy 625 is a nickel-chromium alloy used for its high strength, excellent fabricability and outstanding corrosion resistance. Service temperatures can range from cryogenic to 980¡ãC (1800¡ãF). Alloy 625 strength is derived from the solid solution strengthening effect of molybdenium and niobium on its nickel-chromium matrix.

Alloy 825 (UNS N08825) is an austenitic nickel-iron-chromium alloy with additions of molybdenum, copper and titanium. It was developed to provide exceptional corrosion resistance in both oxidizing and reducing environments. The alloy is resistant to chloride stress-corrosion cracking and pitting. The addition of titanium stabilizes Alloy 825 against sensitization in the as-welded condition making the alloy resistant to intergranular attack after exposure to temperatures in a range that would sensitize unstabilized stainless steels. The fabrication of Alloy 825 is typical of nickel-base alloys, with material being readily formable and weldable by a variety of techniques.