Nickel Alloy Plate

Inconel 713C Round Bar We Manufacture and Sell Inconel 713C Round Bar by Investment Casting,Bar Diameter form 6.0mm-300mm.More Detail information,Please contact us! Inconel 713C is a nickel-chromium alloy that is ideally suited for jet engine gas turbine blades.Inconel 713C offers outstanding resistance to thermal fatigue and good castability while offering exceptional rupture strength at 1700°F (927°C). Inconel 713C Round Bar Chemical Compositons: Alloy % Ni Cr Fe Mn Si Mo

Chemistry Chemical Requirements Ni Cr Mn Si N Mo C Max 9.00 18.00 9.00 4.5 0.18 0.75 0.10 Min 8.00 16.00 7.00 3.5 0.08 Tensile Data Mechanical Property Requirements Under 0.5″ Ultimate Tensile Yield Strength (0.2% OS) Elong. in 4D R/A Hardness Min 105 KSi 55 KSi 35% 55% Max Min 724 MPa 379 MPa Max Mechanical Property Requirements Over 0.5″ Ultimate Tensile Yield Strength (0.2% OS) Elong. R/A Hardness Min 95 KSi 50 KSi 35% 55% Max Min 655 MPa 345 MPa Max There are other high

Nickel 201 Common Trade Names: Nickel 201, LC Nickel 99.2 Nickel 201 has the same characteristics Nickel 200 but has lower carbon levels. These properties, and its chemical composition, make Nickel alloy 201 fabricatable and highly resistant to corrosive environments. Nickel 201 is useful in any environment above 600 oF. It is highly resistant to corrosion by neutral and alkaline salt solutions, fluorine and chlorine. Nickel alloy 201 also has low corrosion rates in neutral

Inconel 718 Common Trade Names: Inconel 718®, Nicrofer® 5219, Alvac® 718, Haynes® 718, Altemp® 718 Inconel 718 is a precipitation hardenable nickel-based alloy designed to display exceptionally high yield, tensile and creep-rupture properties at temperatures up to 1300°F (704°C). The age-hardening response of Inconel 718 permits annealing and welding without spontaneous hardening during heating and cooling. Nickel Alloy 718 has excellent weldability when compared to the

Alloy C276 - UNS N1027 Alloy C276 Equivalents: UNS N10276/ Hastelloy C-276/ Werkstoff 2.4819 Pipe (seamless and welded in random lengths and cut to size) Fittings (BW and forged fittings) Flanges (ANSI, DIN, EN, JIS) Bar (round, square and hexagonal in random lengths and cut to size) Forgings (Discs, Rings and forgings according to drawing) Plate and sheet (Full plates and cut to size) Applications Alloy C276: Alloy C276 has a very good resistance to a variety of chemical

Introduction INCOLOY alloys belong to the category of super austenitic stainless steels. These alloys have nickel-chromium-iron as the base metals, with additives such as molybdenum, copper, nitrogen and silicon. These alloys are known for their excellent strength at elevated temperatures and good corrosion resistance in a variety of corrosive environments. INCOLOY alloy 800 is an alloy of nickel, iron and chromium. The alloy is capable of remaining stable and maintaining its

Introduction Nicrofer 6023 alloy is a nickel-chromium-iron alloy with excellent resistance to corrosion and oxidation at elevated temperatures. The alloy is precipitation-hardenable, and exhibits good mechanical properties at high temperatures. The following datasheet will provide an overview of nicrofer 6023 alloy. Chemical Composition The chemical composition of nicrofer 6023 alloy is outlined in the following table. Element Content (%) Nickel, Ni 58-63 Chromium, Cr 21-25

Inconel 617 is a solid-solution, nickel-chromium-cobalt-molydenum alloy with an exceptional combination of high-temperature strength and oxidation resistance. The alloy also has excellent resistance to a wide range of corrosive environment, and it is readily formed and welded by conventional techniques. The high nickel and chromium contents make the alloy resistant to a variety of both reducing and oxidizing media. The aluminum, in conjunction with the chromium, provides

Inconel 713C is a nickel-chromium alloy that is ideally suited for jet engine gas turbine blades.Inconel 713C offers outstanding resistance to thermal fatigue and good castability while offering exceptional rupture strength at 1700°F (927°C). Inconel 713C sheet Chemical Compositons: Alloy % Ni Cr Fe Mn Si Mo Zr Ti Cu Co Al C S 713C Min. Bal 12.0 - - - 3.8 0.05 0.5 - 1.8 5.5 - - Max. 14.0 2.5 0.25 0.5 5.2 0.15 1.0 0.5 2.8 6.5 0.20 0.015 Inconl 713CSheet Physical properties

incoloy® alloy 330 is designated as UNS N08330 and W. Nr. 1.4886. Bars and Shapes: ASTM B 511, ASME SB 511 Billets and Bars: ASTM B 512, ASME SB 512 Pipe and tube: ASTM B 535; ASME SB 535, ASTM B 546; ASME SB 546, ASTM B 710; ASME SB 710, ASTM B739; ASME SB 739, ASTM B 829/ASME SB 829. Plate. Sheet and Strip: ASTM B 536, ASME SB 536, SAE AMS 5592 Bars, Wire, Forgings and Rings: SAE AMS 5716 Other: ASTM B 366/ASME SB 366 Chemical Composition The chemical composition of INCOLOY

Nimonic 75 is an 80/20 nickel-chromium alloy with controlled additions of titanium and carbon. First introduced in the 1940s for turbine blades in the prototype Whittle jet engines, it is now mostly used forsheet applications calling for oxidation and scaling resistance coupled with medium strength at high operating temperatures. It is still used in gas turbine engineering and also for industrial thermal processing,furnace components and heat-treatment equipment. Nimonic 75

Chemistry Nitronic 50 Chemical Requirements Ni Cr Mo Mn C Si Fe Max 13.5 23.5 3.00 6.0 0.06 1.00 Bal Min 11.5 20.5 1.50 4.0 Nitronic 50 Tensile Data Mechanical Property Requirements Ultimate Tensile Yield Strengtd (0.2% OS) Elong. R/A Hardness Min 100 KSi 55 KSi 35% 55% Max 293 Min 690 MPa 380 MPa Max There are other high strength properties available for sizes of bar, wire, sheet and plate. Inquire with a sales associate at High Performance Alloys for more information. See

Inconel 625LCF™ is specifically designed with low cycle fatigue resistance at temperatures up to 649°C (1200°F). The following datasheet will provide more details about Inconel 625LCF™. Chemical Composition The following table shows the chemical composition of Inconel 625LCF™. Element Content (%) Nickel, Ni ≥ 58 Chromium, Cr 20-23 Molybdenum, Mo 8-10 Iron, Fe ≤ 5 Niobium, Nb 3.15 – 4.15 Cobalt, Co ≤ 1 Manganese, Mn ≤ 0.50 Titanium, Ti ≤ 0.40 Aluminum, Al ≤ 0.40 Carbon, C ≤ 0

We are professional Inconel 686,UNS N06686,UNS No6686,Alloy 686,Inconel Alloy 686,inconel686,alloy686 material factory from China We could supply inconel 686 material in the forms of Forging parts,Forged Rings,Rolled Rings,forged shafts, hollow bars,tube sheets, forged discs,forged sleeves,round Bars,rods,flanges, Casting Parts,Pipe Fittings,elbows, reducer, tee, seamless pipe,Weled Pipes,tubings,gaskets,Plates,Sheets,Strips,Coils Wires,spring ,Fasteners,Machining Parts, and

Equivalent designations UNS N02200 DIN W. Nr. 2.4060, 2.4066 Nickel Alloy 200 Trade Name:Nickel 200;UNS N02200;W. Nr. 2.4060, 2.4066 Form ASTM Rod and bar B 160 Plate, sheet and strip B 162, B 906 Seamless pipe and tube B 161, B 829 Welded pipe B 725, B 775 Welded tube B 730, B 751 Welding fitting B 366 Forging B 564 Chemical composition % Ni Fe C Mn Si S Cu min 99 max 0.4 0.15 0.35 0.35 0.01 0.25 Physical properties Density 8.89 g/cm3 Melting range 1435-1446℃ Features:Nickel

Inconel 625LCF™ is specifically designed with low cycle fatigue resistance at temperatures up to 649°C (1200°F). The following datasheet will provide more details about Inconel 625LCF™. Chemical Composition The following table shows the chemical composition of Inconel 625LCF™. Element Content (%) Nickel, Ni ≥ 58 Chromium, Cr 20-23 Molybdenum, Mo 8-10 Iron, Fe ≤ 5 Niobium, Nb 3.15 – 4.15 Cobalt, Co ≤ 1 Manganese, Mn ≤ 0.50 Titanium, Ti ≤ 0.40 Aluminum, Al ≤ 0.40 Carbon, C ≤ 0

Alloy 600 - UNS N06600 Pipe (seamless and welded in random lengths and cut to size) Fittings (BW and forged fittings) Flanges (ANSI, DIN, EN, JIS) Bar (round, square and hexagonal in random lengths and cut to size) Forgings (Discs, Rings and forgings according to drawing) Plate and sheet (Full plates and cut to size) Applications Alloy 600: Alloy 600 is a nickel-chromium alloy with good oxidation resistance at high temperatures and resistance to chloride-ion stress-corrosion