Inconel 600 Alloy Sheet, 0.037" Size
Inconel 600 Alloy Sheet, 0.037" Size
SKU:INC-8774a0
High-quality Inconel 600 Alloy Sheet, 0.037" size, offers superior corrosion resistance and reliability for critical applications.
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Inconel 600 Alloy Sheet, 0.037" Size
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Inconel 600 Alloy Sheet, 0.037" Size
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The Inconel 600 Alloy Sheet in 0.037" size is a high-performance nickel-chromium alloy with exceptional oxidation resistance at elevated temperatures. Designed for cryogenic to high heat applications, it offers superior corrosion resistance, making it ideal for various environments. With precise specifications meeting institutional procurement standards, this alloy ensures reliability and durability in critical operations.
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Product Specifications
Additional Information Additional Information
Its chromium content gives the alloy resistance to sulfur compounds and various oxidizing environments. The chromium content of the alloy makes it superior to commercially pure nickel under oxidizing conditions. In strong oxidizing solutions like hot, concentrated nitric acid, 600 has poor resistance. Alloy 600 is relatively un-attacked by the majority of neutral and alkaline salt solutions and is used in some caustic environments. The alloy resists steam and mixtures of steam, air and carbon dioxide.Alloy 600 is non-magnetic, has excellent mechanical properties and a combination of high strength and good workability and is readily weldable. Alloy 600 exhibits cold forming characteristics normally associated with chromium-nickel stainless steels.Typical corrosion applications include titanium dioxide production (chloride route), perchlorethylene syntheses, vinyl chloride monomer (VCM), and magnesium chloride. Alloy 600 is used in chemical and food processing, heat treating, phenol condensers, soap manufacture, vegetable and fatty acid vessels and many more.
Applications 0
Thermocouple sheaths.Ethylene dichloride (EDC) cracking tubes.Conversion of uranium dioxide to tetrafluoride in contact with hydrofluoric acid. Production of caustic alkalis particularly in the presence of sulfur compounds.Reactor vessels and heat exchanger tubing used in the production of vinyl chloride.Process equipment used in the production of chlorinated and fluorinated hydrocarbons.In nuclear reactors uses are for such components as control rod inlet stub tubes, reactor vessel components and seals, steam dryers and d separators in boiling water reactors. In pressurized water reactors it is used for control rod guide tubes and steam generator baffle plates etc. Furnace retort seals, fans and fixtures.Roller hearths and radiant tubes, in carbon nitriding processes especially.
Characteristics 0
Resistant to a wide range of corrosive media. The chromium content gives better resistance than Alloy 200 and 201 under oxidizing conditions, at the same time the high nickel gives good resistance to reducing conditions.Virtually immune to chlorine ion stress corrosion cracking.Demonstrates adequate resistance to organic acids such as acetic, formic and stearic.Excellent resistance to high purity water used in primary and secondary circuits of pressurized nuclear reactors.Little or no attack occurs at room and elevated temperatures in dry gases, such as chlorine or hydrogen chloride. At temperatures up to 550 ºC in these media, this alloy has been shown to be one of the most resistant of the common alloys.At elevated temperatures the annealed and solution annealed alloy shows good resistance to scaling and has high strength.The alloy also resists ammonia bearing atmospheres, as well as nitrogen and carburizing gases.Under alternating oxidizing and reducing conditions the alloy may suffer from selective oxidation.
Fabricating Inconel 0
Alloy 600 is non-magnetic, has excellent mechanical properties and a combination of high strength and good workability and is readily weldable. Alloy 600 exhibits cold forming characteristics normally associated with chromium-nickel stainless steels.600 sheet and plate are almost exclusively supplied in the annealed condition. Bar stock may need to be stress relieved, or annealed before performing any heading operations.
General Resistance Barrod Usa
AMS 5665 | B166
General Resistance Barrod Wkstf
17752
General Resistance Fitting Usa
B366
General Resistance Forging Usa
B564
General Resistance Forging Wkstf
17754
General Resistance General Resistance
Temperature | Oxidation | Corrosion
General Resistance Sheetplate Usa
AMS 5540 | B168
General Resistance Sheetplate Wkstf
17750
General Resistance Unified Numbering System Uns
N06600
General Resistance Weld Electrode
FM 182 | ENiCrFe-3
General Resistance Weld Wire
ERNiCr-3 | FM 82
General Resistance Werkstof
2.4816
Machinability Ratings Speed Percent Of B1112
Annealed: 22 | Cold Drawn: 39
Machinability Ratings Speed Surface
Annealed: 50 ft/mm | Cold Drawn: 65 ft/mm
Machining Section 0
These machinability ratios must be recognized as approximate values. They are a reasonable guide to relative tool life and lower required for cutting. It is obvious, however, that variables of speed, cutting oil, feed and depth of cut will significantly affect these ratios.The alloys described here work harden rapidly during machining and require more power to cut than do the plain carbon steels. The metal is 'gummy', with chips that tend to be stringy and tough. Machine tools should be rigid and used to no more than 75% of their rated capacity. Both work piece and tool should be held rigidly; tool overhang should be minimized. Rigidity is particularly important when machining titanium, as titanium has a much lower modulus of elasticity than either steel or nickel alloys. Slender work pieces of titanium tend to deflect under tool pressures causing chatter, tool rubbing and tolerance problems.Make sure that tools are always sharp. Change to sharpened tools at regular intervals rather than out of necessity. Titanium chips in particular tend to gall and weld to the tool cutting edges, speeding up tool wear and failure. Remember- cutting edges, particularly throw-away inserts, are expendable. Don't trade dollars in machine time for pennies in tool cost.Feed rate should be high enough to ensure that the tool cutting edge is getting under the previous cut thus avoiding work-hardened zones. Slow speeds are generally required with heavy cuts. Sulfur chlorinated petroleum oil lubricants are suggested for all alloys but titanium. Such lubricants may be thinned with paraffin oil for finish cuts at higher speeds. The tool should not ride on the work piece as this will work harden the material and result in early tool dulling or breakage. Use an air jet directed on the tool when dry cutting, to significantly increase tool life.Lubricants or cutting fluids for titanium should be carefully selected. Do not use fluids containing chlorine or other halogens (fluorine, bromine or iodine), in order to avoid risk of corrosion problems. The speeds are for single point turning operations using high speed steel tools. This information is provided as a guide to relative machinability, higher speeds are used with carbide tooling.
Mechanical Data Note
These machinability ratios must be recognized as approximate values. They are a reasonable guide to relative tool life and lower required for cutting. It is obvious, however, that variables of speed, cutting oil, feed and depth of cut will significantly affect these ratios.
Mechanical Elongation
55 to 35 %
Mechanical Hardness
B65 - 85
Mechanical Mechanical Type
Annealed
Mechanical Tensile Strength
80 to 105 ksi
Mechanical Yield Strength
30 to 50 ksi
Nominal Chemistry Chromium Cr
15.5
Nominal Chemistry Cobalt Co
Included in Nickel
Nominal Chemistry Iron Fe
8
Nominal Chemistry Maximum Carbon C
0.15
Nominal Chemistry Maximum Copper Cu
0.5
Nominal Chemistry Maximum Manganese Mn
1
Nominal Chemistry Maximum Silicon Si
0.5
Nominal Chemistry Minimum Nickel Ni
72
Nominal Chemistry Other
S 0.015 max
Physical Curie Temperature
-192 ºF
Physical Density
0.305 lb/in³
Physical Electrical Resistivity
620 ohm/cir-mil-ft
Physical Melting Range
2470 to 2575 ºF
Physical Specific Heat
0.109 Btu/lb ºF
Specifications Size
0.037 in