Types : HYDRAULIC TUBE HORN TUBE CAPILLARY TUBE
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1 Inconel alloys are oxidation and corrosion resistant materials well suited for service in extreme environments. It is common in gas turbine blades, seals, and combustors, as well as turbocharger rotors and seals, electric submersible well pump motor shafts, high temperature fasteners, chemical processing and pressure vessels, heat exchanger tubing, steam generators in nuclear pressurized water reactors and others. We offer a broad range of inconel products including pipes, tubes, sheets & plates, flanges, fittings, etc. Inconel Pipes Inconel pipes feature seamless fabrication for better flow characteristic. These pipes can be readily welded for a leak proof connection. The highly durable inconel pipes can be used for variety of corrosive media across industries. Specifications Range : 15 NB UP TO 600 NB IN SCH 5S, 10S,10, 20, 40S, 40, STD, 60, 80S, 80, XS, 100, 120, 140, 160 & XXS Type : SEAMLESS / ERW / WELDED/ FABRICATED Form : ROUND, COIL, SQUARE, RECTANGULAR, HYDRAULIC ETC. Length : SINGLE RANDOM, DOUBLE RANDOM & CUT LENGTH End : PLAIN END, BEVELLED END, THREADED Grades: ASTM / ASME UNS 6600 INCONEL 600 ASTM / ASME UNS 6601 INCONEL 601 ASTM / ASME UNS 6625 INCONEL 625 ASTM / ASME UNS 7718 INCONEL 718 ASTM / ASME UNS 7751 INCONEL X-750 ASTM / ASME UNS 8800 INCONEL 800 ASTM / ASME UNS 8810/11 INCOLOY 800H ASTM / ASME UNS 8825 INCOLOY 825 Inconel Tubes Our range of inconel tubes are widely used for critical applications in industries like oil & gas, aviation, aerospace, petrochemical, natural gas, etc. These tubes have excellent strength with perfect finish. Specifications Range : 6.35 mm OD upto 254 mm OD in 0.6 TO 20 mm thickness. Type : SEAMLESS / ERW / WELDED/ CDW Form : ROUND, SQUARE, RECTANGULAR, COIL, 'U' SHAPE, PAN CAKE, Types : HYDRAULIC TUBE HORN TUBE CAPILLARY TUBE
2 BOILER TUBE PRECISION TUBE LENGTH : SINGLE RANDOM,DOUBLE RANDOM & REQUIRED LENGTH End : PLAIN END, BEVELLED END, THREADED Grades : UNS 8825 INCONEL (825) UNS 6600 (INCONEL 600) UNS 6601 (INCONEL 601) UNS 6625 (INCONEL 625) Inconel Sheets & Plates Inconel sheets and plates are used in a wide range of applications including structural, mechanical & general engineering purposes. These sheets and plates can withstand tremendous amount of weights and pressure. We can offer sheet and plates in variety of grades and lengths as per the client's requirement. Specifications Range : 0.5 mm To 200 mm thick in 1000 mm TO 2500 mm width & 2500 mm to mm Length available with NACE MR Grades: UNS 8800 (INCONEL 800) UNS 8825 (INCONEL 825) UNS 6600 (INCONEL 600) UNS 6601 (INCONEL 601) UNS 6625 (INCONEL 625) Inconel Rod Inconel rods have an excellent mechanical properties and provide good resistance to oxidation. These pipes find extensive application in furnace muffles, electronic components, heat treating equipment, steam generator tubing, heat exchangers, etc. Specifications Grades : UNS 8800 (INCONEL 800) UNS 8825 (INCONEL 825) UNS 6600 (INCONEL 600) UNS 6601 (INCONEL 601) UNS 6625 (INCONEL 625) Inconel Fittings Our comprehensive range of inconel fittings provide good oxidation resistance at higher temperatures. Easy to install, these fittings comply with international standards. We can offer a variety of inconel fittings including Elbow 90 deg, Elbow 45 deg, Cross, Tee,Coupling, Half Coupling & Cap, etc.
3 Specifications Grades: Inconel 800 (UNS No. N08800) Inconel 825 (UNS No. N08825) Inconel 600 (UNS No. N06600) Inconel 625 (UNS No. N06625) Inconel 601 (UNS No. N06601) Inconel Flanges We offer a wide range of inconel flanges with accurate drill holes for easy installation. These flanges are used as backing to support different structure. They can be used for pipelines, bellows, ducts, wheels, etc. Form : Slip On Flanges, Socket Weld Flanges, Blind Flanges, Lapped Flanges, Screwed Flanges, Weld Neck Flanges, Reducing Flanges, Spectacle Flanges, Slip On Boss Flanges, Plate Flanges, Plate Blank Flanges, Screwed Boss Flanges. Grades: Inconel 800 (UNS No. N08800) Inconel 825 (UNS No. N08825) Inconel 600 (UNS No. N06600) Inconel 625 (UNS No. N06625) Inconel 601 (UNS No. N06601) Super Alloy Inconel600 Technical Data Related Metals: VLX600(tm) AL 600(tm) Ferrochronin 600(tm) Nickelvac 600(tm) Nicrofer 7216 LC(tm) Pyromet Alloy 600(tm) Sanicro 70(tm) CM 600(tm) Pyromet 600(tm) Specifications: AMS 5540 AMS 5580 AMS 5665 AMS 5687 ASTM B163 ASTM B166 ASTM B167 ASTM B168 ASTM B516 ASTM B517 ASTM B564 DIN
4 MIL N MIL N MIL N-6710 MIL T QQ W390 UNS N06600 Chemistry Data Carbon 0.15 max Chromium Copper 0.5 max Iron 6-10 Manganese 1 max Nickel Balance Silicon 0.5 max Sulphur max General Information Principal Design Features A general purpose structural engineering material for use at high temperatures where strength, stability, and durability are important. The alloy also has very good corrosion resistance. When considering this alloy, also investigate Alloy 690, which doub Applications Heaters, heat exchangers, chemical process equipment, heat treat furnace components and fixtures and gas turbine components. Machinability Conventional machining techniques used for iron based alloys may be used. This alloy does work-harden during machining and has higher strength and "gumminess" not typical of steels. Heavy duty machining equipment and tooling should be used
5 to minimize c Forming This alloy has good ductility and may be readily formed by all conventional methods. Because the alloy is stronger than regular steel it requires more powerful equipment to accomplish forming. Heavy-duty lubricants should be used during cold forming. I Corrosion Resistance General corrosion resistance is good in many acid solutions, both oxidizing and reducing acids, as well as being resistant to salts. It is basically completely resistant to corrosion by organic acids. Because of the high nickel content the alloy is virt Welding The commonly used welding methods work well with this alloy. Matching alloy filler metal should be used. If matching alloy is not available then the nearest alloy richer in the essential chemistry (Ni, Co, Cr, Mo) should be used. All weld beads should Heat Treatment Solution anneal at 1850 F for 15 minutes at temperature and air cool. Forging Forging may be done in the temperature range of 2250 F to 1900 F. Hot Working The hot work temperature range is 2250 F to 1600 F. The alloy has low ductility in the range of 1200 F to 1600 F and working in that temperature range should be avoided. Cold Working
6 Cold forming may be done using standard tooling although plain carbon tool steels are not recommended for forming as they tend to produce galling. Soft die materials (bronze, zinc alloys, etc.) minimize galling and produce good finishes, but die life is Physical Data Density (lb / cu. in.) Specific Gravity 8.47 Specific Heat (Btu/lb/Deg F - [ Deg F]) Electrical Resistivity (microhm-cm (at 68 Deg F)) 620 Melting Point (Deg F) 2550 Thermal Conductivity 103 Mean Coeff Thermal Expansion 5.8 Magnetic Permeability 1.01 Modulus of Elasticity Tension 31.1 Reduction of Area 60 Mechanical Data MSO currently has no data available for this grade. Super Alloy Inconel 601 Related Metals: Pyromet Alloy 601(tm) Nicrofer 6023(tm) Ferrochronin 601(tm) Pyromet 601(tm) Specifications: AMS 5715 AMS 5870 ASTM B166
7 ASTM B167 ASTM B168 DIN UNS N06601 Chemistry Data Aluminum Carbon 0.1 max Chromium Copper 1 max Iron Balance Manganese 1 max Nickel Silicon 0.5 max Sulphur max General Information Principal Design Features A nickel-chromium-iron alloy with excellent resistance to high temperature oxidation. A general purpose material for applications where heat and corrosion resistance are the primary considerations. Applications A construction alloy for heat treat furnace fixtures and components such as annealing tubes, muffles, flame shields. Also useful for chemical process equipment such as combustor components, process heaters, and condenser tubes. Machinability Conventional machining techniques used for iron based alloys may be used. This alloy does work-harden during machining and has higher strength and "gumminess" not typical of steels. Heavy duty machining equipment and tooling should be used
8 to minimize ch Forming This alloy has good ductility and may be readily formed by all conventional methods. Because the alloy is stronger than regular steel it requires more powerful equipment to accomplish forming. Heavy-duty lubricants should be used during cold forming. I Corrosion Resistance The alloy has good corrosion resistance to nitric acid and to low concentrations of phosphoric acid. It does not resist hydrochloric, sulfuric, or hydrofluoric acids. Resistance to attack by sodium hydroxide solutions is good. The alloy is also very Welding The commonly used welding methods work well with this alloy. Matching alloy filler metal should be used. If matching alloy is not available then the nearest alloy richer in the essential chemistry (Ni, Co, Cr, Mo) should be used. All weld beads should Heat Treatment The alloy is not hardened or strengthened by heat treatment. Forging Forging should be done in the temperature range of 2250 F to 1900 F. Hot Working Hot work in the range of 2250 F to 1600 F. Avoid working in the range of 1400 F to 1000 F as the alloy is apt to thermal crack in that region. Cold Working
9 Cold forming may be done using standard tooling although plain carbon tool steels are not recommended for forming as they tend to produce galling. Soft die materials (bronze, zinc alloys, etc.) minimize galling and produce good finishes, but die life is Annealing Annealing following cold working may be necessary. The annealing temperature is 2100 F and the alloy should be rapidly cooled through the range of 1400 to 1000 F to avoid thermal cracking. Hardening The alloy hardens by cold working only. Physical Data Density (lb / cu. in.) Specific Gravity 8.11 Specific Heat (Btu/lb/Deg F - [ Deg F]) Electrical Resistivity (microhm-cm (at 68 Deg F)) 710 Melting Point (Deg F) 2460 Thermal Conductivity 87 Mean Coeff Thermal Expansion 7.6 Magnetic Permeability Modulus of Elasticity Tension Mechanical Data MSO currently has no data available for this grade.
10 Super Alloy Inconel625 Related Metals: Nicrofer 6020 hmo(tm) VLX625(tm) Udimet 625(tm) Nickelvac 625(tm) HAYNES(r) 625 alloy Custom Age 625 Plus Alloy(tm) Chronin 625(tm) Altemp 625(tm) Pyromet Alloy 625(tm) Custom Age 625 +(tm) HAYNES(r) 625 alloy(tm) Nicrofer 6020(tm) Pyromet 625(tm) Specifications: AMS 5581 AMS 5599 AMS 5666 AMS 5837 AMS 5879 ASTM B366 ASTM B443 ASTM B444 ASTM B446 ASTM B704 ASTM B705 DIN GE B50TF133 MIL E (RN625) UNS N06625 Chemistry Data Aluminum 0.4 max Carbon 0.1 max Chromium Cobalt 1 max Iron 5 max Manganese 0.5 max Molybdenum 8-10 Nickel Balance
11 Niobium Phosphorus max Silicon 0.5 max Sulphur max Titanium 0.4 max General Information Principal Design Features This nickel-chromium-molybdenum wrought alloy is an excellent general purpose material for elevated temperature use in high strength, oxidation problem applications. It also has excellent corrosion resistance to many acids and resists intergranular attac Applications The alloy finds use in high temperature applications such as heat exchangers and gas turbine components. Because of its good corrosion resistance it is also used in wet scrubbers and some acid process equipment. Machinability May be machined by conventional means. However the alloy tends to work harden ahead of cutting and rigid tooling is essential to avoid chatter and work hardening in front of the tool edge. Forming This alloy can be cold formed by conventional means and tooling. The alloy does work harden during cold working with an attendant increase in strength. This increase in strength may be of value for moderate temperature applications and, in these instanc Corrosion Resistance This alloy has very good corrosion resistance to a wide variety of acids and chemicals. As an example it is suited for use with
12 both hydrochloric and nitric acid. It resists chloride pitting/ crevice corrosion and chloride stress-corrosion cracking and Welding Welding is readily accomplished using matching alloy filler metal for the conventional welding techniques. Heat Treatment The alloy is furnished in the solution annealed condition. This is done at 2150 F for sufficient time dependent upon section thickness. Following the anneal the alloy may be air cooled. Forging Hot forging can be done by heating the billet to F, but not over Heavy forging may then be done down to a billet temperature of 1850 F and light forging down to 1700 F. Final reductions of 15 to 20% minimum are recommended to maintain Hot Working Hot forming may be done by heating the alloy to 2150 F. Because this alloy is engineered for good strength at high temperatures it will resist hot deformation and therefore requires powerful equipment to perform hot forming. Cold Working The alloy can be cold formed by conventional methods and tooling. See also the comments under "Forming" regarding work hardening. Annealing Because the alloy work hardens during hot or cold forming it may be necessary to anneal such parts in order to complete forming operations. Annealing is done at 1800 to 2000 F and air cooled. Stress relief of cold worked parts may be accomplished at 110 Aging
13 The alloy derives its strength from its basic chemical composition. Thus aging or precipitation hardening is not applicable as a heat treatment. Tempering Not applicable. Hardening Cold working does harden the alloy and improve strength, dependent upon the amount of cold working. The alloy can be used in this higher strength cold worked condition or may be annealed at 2150 F to restore original mechanical properties. Physical Data Density (lb / cu. in.) Specific Heat (Btu/lb/Deg F - [ Deg F]) Melting Point (Deg F) 2425 Poissons Ratio Thermal Conductivity 74 Mean Coeff Thermal Expansion 7.3 Modulus of Elasticity Tension 29.2 Reduction of Area 70 Mechanical Data MSO currently has no data available for this grade.
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