Customization: | Available |
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Application: | Aviation, Electronics, Industrial, Medical, Chemical |
Standard: | JIS, GB, DIN, ASTM, AISI |
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ASTM F96 Stock Monel K500 Nickel Based Alloy Tube for oil well industry
Material | Monel/Inconel/Hastelloy/Duplex Steel/PH Steel/Nickel Alloy |
Shape | Round,Forging,Ring,Coil,Flange,Disc,Foil,Spherical,Ribbon,Square,Bar,Pipe,Sheet |
Grade | Duplex: 2205(UNS S31803/S32205),2507(UNS S32750),UNS S32760(Zeron 100),2304,904L |
Others:253Ma,254SMo,654SMo,F50(UNSS32100)F60,F61,F65,1J22,N4,N6 etc | |
Alloy : Alloy 20/28/31 | |
Hastelloy:HastelloyB/ -2/B-3/C22/C-4/S/ C276/C-2000/G-35/G-30/X/N/g | |
Hastelloy B / UNS N10001,Hastelloy B-2 / UNS N10665 / DIN W. Nr. 2.4617,Hastelloy C, Hastelloy C-4 / UNS N06455 / DIN W. Nr. 2.4610,Hastelloy C-22 / UNS N06022 / DIN W. Nr. 2.4602, Hastelloy C-276 / UNS N10276 / DIN W. Nr. 2.4819,Hastelloy X / UNS N06002 / DIN W. Nr. 2.4665 |
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Haynes: Haynes 230/556/188 | |
Inconel 600/601/602CA/617/625/713/718/738/X-750,Carpenter 20 | |
Inconel 718 / UNS N07718 / DIN W. Nr. 2.4668,Inconel 601 / UNS N06601 / DIN W. Nr. 2.4851, Inconel 625 / UNS N06625 / DIN W. Nr. 2.4856,Inconel 725 / UNS N07725,Inconel X-750 / UNS N07750 / DIN W. Nr. 2.4669,Inconel 600 / UNS N06600 / DIN W. Nr. 2.4816 |
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Incoloy: Incoloy 800/800H/800HT/825/925/926; | |
GH: GH2132,GH3030,GH3039,GH3128,GH4180,GH3044 | |
Monel: Monel 400/K500/R405 | |
Nitronic: Nitronic 40/50/60; | |
Nimonic: Nimonic 75/80A/90/A263 ; | |
Specification |
Wire: 0.01-10mm Strip: 0.05*5.0-5.0*250mm Bar: φ4-50mm;Length 2000-5000mm Pipe: φ6-273mm;δ1-30mm;Length 1000-8000mm Sheet: δ 0.8-36mm;Width 650-2000mm;Length 800-4500mm |
Product Characteristics |
1.According to the preparation process can be divided into deformation superalloys, casting superalloys and powder metallurgy superalloys. 2.According to the strengthening mode, there are solid solution strengthening type, precipitation strengthening type, oxide dispersion strengthening type and fiber strengthening type, etc.. |
Standard | GB,AISI,ASTM,DIN,EN,SUS,UNS etc |
Inspection | ISO,SGS,BV and so on. |
Application |
High temperature components such as turbine blades, guide vanes, turbine disks, high pressure compressor disks,machine manufacturing and combustion chambers used in the manufacture of aviation, naval and industrial gas turbines |
Packaging |
1. cases packed in wooden cases 2. paper packaging 3. plastic packing 4. foam packaging Packaging according to customer requirements or products |
Delivery | 7-25days or According to the product |
Payment | L/C,D/A,D/P,T/T,Western Union,MoneyGram,According to customer requirements payments for offline orders. |
Super alloys contain many elements in different combinations so as to achieve a desired result. They have the ability to function at very high temperatures and under severe mechanical stress, and also where high surface stability is required. They have good creep and oxidation resistance. There are three groups of alloys, namely cobalt-based, nickel-based, and iron-based alloys.
Nickelvac K-500 is an age-hardenable version of Monel 400 alloy. It has high strength and sea water corrosion resistance. The following datasheet gives more details about Nickelvac K-500.
The following table shows the chemical composition of Nickelvac K-500.
Element | Content (%) |
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Nickel, Ni | 66 |
Copper, Cu | 29 |
Aluminum, Al | 2.7 |
Iron, Fe | 1 |
Manganese, Mn | 0.7 |
Tungsten, W | 0.6 |
Silicon, Si | 0.25 |
Carbon, C | 0.1 |
Sulfur, S | 0.01 |
The physical properties of Nickelvac K-500 are outlined in the following table.
Properties | Metric | Imperial |
---|---|---|
Density | 8.45 g/cm³ | 0.305 lb/in³ |
Melting point | 1338°C | 2440°F |
The mechanical properties of Nickelvac K-500 are given in the following table.
Properties | Metric | Imperial |
---|---|---|
Tensile strength | 1000 MPa | 145000 psi |
Yield strength (at strain 0.200%) | 655 MPa | 95000 psi |
Elongation at break | 22% | 22% |
Reduction of area | 40% | 40% |
Hardness, Rockwell C | 27 | 27 |
Other designations that are equivalent to Nickelvac K-500 include:
Nickelvac K-500 is machined in the annealed condition.
Nickelvac K-500 can be formed using standard methods in the annealed condition.
Nickelvac K-500 is welded using all conventional methods in the annealed condition. After this process, stress-relief annealing is performed for the finished weldment.
Nickelvac K-500 is heat treated by annealing. It can also be precipitation-hardened by performing aging heat treatment.
Nickelvac K-500 is forged at 1038 to 1149°C (1900 to 2100°F) followed by quenching in water.
Nickelvac K-500 is hot worked at 872 to 1149°C (1600 to 2100°F) followed by quenching in water. It should not be cooled below 872°C (1600°F).
Nickelvac K-500 can be cold worked using standard methods
Nickelvac K-500 is annealed at 1038°C (1900°F) followed by quenching in water.
Annealed or slightly cold-worked material is age-hardened at 608°C (1125°F ) for 16 h followed by cooling in a furnace. Severely cold-worked material is aged at 538°C (1000°F) for 6 h followed by cooling in a furnace.
Super alloy Nickelvac K-500 is used in impellers, sea water pump shafts, and oil well industry for valve trim and other components.