Maraging 250™(also referred to as Maraging C25™ and Vascomax 250™) is a vacuum induction melted plus vacuum arc melted, low-carbon, nickel-cobalt-molybdenum high temperature alloy capable of attaining yield strengths in excess of 240 KSI (1655 MPA) through a simple, low temperature heat treatment. Maraging 250™ exhibits good ductility at high strength levels and is readily welded. Maraging C250™ is one of a family of "maraging" nickel steels (including Maraging 300™ and 350™), which are ductile in the solution treated condition and attains ultrahigh tensile strength by aging at temperatures in the range of 850/950 °F (454/510 °C). Available forms are seamless pipe, welded pipe, seamless tube, welded tube, bar, wire, sheet, plate, forgings, pipe fittings and flanges.
Sheet/Plate | AMS 6520 |
Round Bar/Wire | AMS 6512, MIL-S-46850, ASTM A538 |
C | MN | P | S | Si | Cr | Ni | Mo | Cu | Co | Cb | Ti | Al | Fe | B | Zr |
.03 max | .10 max | .01 max | .01 max | .10 max | 18.5 | 4.8 | 7.5 | 0.4 | 0.1 | 0.004 | 0.01 |
SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.
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INCONEL® alloy 718 (UNS N07718/W.Nr. 2.4668) is a high-strength, corrosion-resistant nickel chromium material used at -423° to 1300°F. Typical composition limits are shown in Table 1. The age-hardenable alloy can be readily fabricated, even into complex parts. Its welding characteristics, especially its resistance to postweld cracking, are outstanding. The ease and economy with which INCONEL alloy 718 can be fabricated, combined with good tensile, fatigue, creep, and rupture strength, have resulted in its use in a wide range of applications. Examples of these are components for liquid fueled rockets, rings, casings and various formed sheet metal parts for aircraft and land-based gas turbine engines, and cryogenic tankage. It is also used for fasteners and instrumentation parts.
Chemical Compositiona , %
Nickel (plus Cobalt) .......................................................50.00-55.00 Chromium......................................................................17.00-21.00
Iron .....................................................................................Balance*
Niobium (plus Tantalum)............................................4.75-5.50
Molybdenum .....................................................................2.80-3.30 Titanium.............................................................................0.65-1.15
Aluminum ..........................................................................0.20-0.80
Cobalt ...............................................................................1.00 max. Carbon..............................................................................0.08 max.
Manganese .......................................................................0.35 max.
Silicon ...............................................................................0.35 max. Phosphorus.....................................................................0.015 max. Sulfur...............................................................................0.015 max.
Boron ..............................................................................0.006 max. Copper..............................................................................0.30 max
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SIZE 0.5MM TO 6MM DIA WIRE.
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SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
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A-286 ALLOY
A-286 alloy is an age-hardenable iron base superalloy for applications requiring high strength from -320°F up to 1000°F long time, 1300-1500°F short time. Oxidation resistance is high for continuous service to 1500°F, intermittent to 1800°F. Aqueous corrosion resistance is comparable to 316/316L stainless. Heat treatment according to AMS 5525 requires a solution anneal at 1800°F, air cool. Age at 1325°F for 16 hours and then air cool.
Common Trade NamesA286 Stainless, A286 Alloy
InventoryA-286 Sheet, A-286 Coil, A-286 Round Bar, A-286 Hex Bar
SpecificationsUNS S66286, Werkstoff 1.4980, EN 1.4980
AMS: 5525, 5804, 5732, 5737
GE B50T1181, GE B50T12, GE B50T81
Cr | Ni | Mo | Co | Va | Al | Ti | B | C | Fe | Mn | Si | Ph | S | |
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
MIN | 13.5 | 24.0 | 1.0 | - | 0.1 | - | 1.9 | 0.003 | - | - | - | - | - | - |
MAX | 16.0 | 27.0 | 1.5 | 1.0 | 0.5 | 0.35 | 2.35 | 0.01 | 0.08 | Balance | 2.0 | 1.0 | 0.025 | 0.025 |
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Inconel 713C offers outstanding resistance to thermal fatigue and good castability while offering exceptional rupture strength at 1700°F (927°C). Inconel 713C is a nickel-chromium alloy that is ideally suited for jet engine gas turbine blades.
CHEMICAL COMPOSITION OF INCONEL™ 713CSIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.
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With a high creep and rupture strength to 1400°F (760°C), Incoloy™ 901is a nickel-iron-chromium alloy ideally suited for gas turbine and aircraft applications. Because of its high nickel content, it can be joined with ferritic alloy steels without thermal expansion provisions.
CHEMICAL COMPOSITION OF INCOLOY™ 901SIZE 6MM TO 200MM DIA ROUND BAR.
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SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.
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Nitronic 50® stainless steel is an austenitic stainless steel with a blend of strength and corrosion resistance that is higher than stainless steel grades 316, 316/316L, 317, and 317/317L .
The high strength, corrosion resistance, and low magnetic permeability of this alloy allows it to be used as a material for medical implants.
The following sections will discuss in detail about stainless steel grade NITRONIC®50 (XM-19).
Chemical CompositionThe chemical composition of stainless steel grade NITRONIC® 50 (XM-19) is outlined in the following table.
Element | Content (%) |
---|---|
Chromium, Cr | 20.5-23.5 |
Nickel, Ni | 11.5-13.5 |
Manganese, Mn | 4-6 |
Molybdenum, Mo | 1.5-3 |
Silicon, Si | 1 max |
Nitrogen, N | 0.20-0.40 |
Niobium, Nb | 0.10-0.30 |
Vanadium, Va | 0.10-0.30 |
Phosphorous, P | 0.04 max |
Carbon, C | 0.06 max |
Sulfur, S | 0.010 max |
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Valve stems, fasteners, screens, wear plates and pins
DescriptionNitronic 60® is an austenitic stainless steel that has about twice the yield strength of 304 with better corrosion resistance. The alloy has excellent high temperature oxidation resistance. In addition Nitronic® 60 and has outstanding galling resistance.
Chemistry TypicalCarbon: 0.10 max
Manganese: 7.00-9.00
Silicon: 3.5-4.5
Chromium: 16.00-18.00
Nickel: 8.00-9.00
Nitrogen: 0.08-0.18
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Alloy steels comprise a wide variety of steels with compositions that exceed the limitations of Si, Va, Cr, Ni, Mo, Mn, B and C allocated for carbon steels. In comparison with carbon steels, alloy steels are more responsive to mechanical and heat treatments.
Alloy steels can be used in specific melting and deoxidization processes for particular applications. These steels have elements such as chromium, cobalt, nickel, etc.
Maraging 300 alloy steel is a very high strength iron base, molybdenum, cobalt and nickel alloy. The following datasheet provides an overview of maraging 300 alloy steel.
Chemical CompositionThe chemical composition of maraging 300 alloy steel is outlined in the following table.
Element | Content (%) |
---|---|
Iron, Fe | 67 |
Nickel, Ni | 18.5 |
Cobalt, Co | 9 |
Molybdenum, Mo | 4.8 |
Titanium, Ti | 0.6 |
Aluminum, Al | 0.1 |
Silicon, Si | 0.10 |
Manganese, Mn | 0.10 |
Carbon, C | 0.030 |
Zirconium, Zr | 0.01 |
Phosphorous, P | 0.010 |
Sulfur, S | 0.010 |
Boron, B | 0.0030 |
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Chemical Composition Limits | |||||||||||
Weight% | Ni | Fe | Cr | Mo | Cu | Ti | C | Mn | S | Si | Al |
Alloy 28 | 30-32 | 22 min | 26-28 | 3-4 | 0.60-1.40 | - | 0.02 max | 2 max | 0.03 max | 0.70 max | - |
Alloy 28 (UNS N08028, W. Nr. 1.4563) is a nickel-iron-chromium alloy with additions of molybdenum and copper. It has excellent resistance to both reducing and oxidizing acids, to stress-corrosion cracking, and to localise attack such as pitting and crevice corrosion. The alloy are especially resistant to sulphuric and phosphoric acid. Used for chemical processing, pollution control equipment, oil and gas well piping, nuclear fuel reprocessing, acid production and pickling equipment.
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With better strength at higher temperatures, Stainless steel 422 is an appealing alternative to Stainless 403. It offers ductility and strength from room temperature to 1200°F (649°C) and resists scaling and oxidation to 1400°F (760°C).
CHEMICAL COMPOSITION OF STAINLESS STEEL 422SIZE 6MM TO 200MM DIA ROUND BAR.
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SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.
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SIZE 6MM TO 200MM DIA ROUND BAR.
SIZE 1MM TO 100MM THICKNESS PLATE.
SIZE 6MM TO 350MM OD PIPE .
SIZE 0.5MM TO 6MM DIA WIRE.
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The INCOLOY® 800 series of alloys, invented by the Special Metals Corporation Group of Companies, is the result of years of monitoring and maintaining the ultimate chemical properties for high-temperature strength and resistance to oxidation, carburization and other types of high-temperature corrosion. Each one a refinement of the one before, these alloys have set the industry standard in hightemperature applications requiring optimum creep and rupture properties. INCOLOY nickel-iron-chromium alloy 800 was introduced to the market in the 1950s to fill the need for a heat- and corrosion-resistant alloy with a relatively low nickel content since nickel was, at the time, designated a “strategic” metal. Over the past forty years it has been widely used for its strength at high temperatures and its ability to resist oxidation, carburization, and other types of high-temperature corrosion. Applications include furnace components and equipment, petrochemical furnace cracker tubes, pigtails and headers, and sheathing for electrical heating elements.
CHEMICAL% 800 800H 800HT
Nickel 30.0-35.0 30.0-35.0 30.0-35.0
Chromium 19.0-23.0 19.0-23.0 19.0-23.0
Iron 39.5 min. 39.5 min. 39.5 min.
Carbon 0.10 max. 0.05-0.10 0.06-0.10
Aluminum 0.15-0.60 0.15-0.60 0.25-0.60
Titanium 0.15-0.60 0.15-0.60 0.25-0.60
Aluminum + Titanium 0.30-1.20 0.30-1.20 0.85-1.20
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Nickel 200 (UNS N02200/W.Nr. 2.4060 & 2.4066) is commercially pure (99.6%) wrought nickel. It has good mechanical properties and excellent resistance to many corrosive environments. Other useful features of the alloy are its magnetic and magnetostrictive properties, high thermal and electrical conductivities, low gas content and low vapor pressure. Chemical composition is shown in Table 1. The corrosion resistance of Nickel 200 makes it particularly useful for maintaining product purity in the handling of foods, synthetic fibers, and caustic alkalies; and also in structural applications where resistance to corrosion is a prime consideration. Other applications include chemical shipping drums, electrical and electronic parts, aerospace and missile components.
Chemical Composition, %
Nickel (plus cobalt) ......................................................99.0 min. Copper........................................................................0.25 max. Iron..............................................................................0.40 max.
Manganese .................................................................0.35 max. Carbon........................................................................0.15 max.
Silicon .........................................................................0.35 max.
Sulfur ..........................................................................0.01 max.
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Nitronic 60 is truly an all purpose metal. This fully austenitic alloy was originally designed as a temperature alloy, and subsequently has good high temperature properties for temperatures around 1800ºF. The oxidation resistance of Nitronic 60 is similar to Type 309 S.S., and far superior to Type 304S.S. This grade is best known for its wear and galling resistance.
The additions of Silicon and Manganese have given this alloy a matrix to inhibit wear, galling, and fretting even in the annealed condition. Higher strengths are attainable through cold working the material and is still fully austenitic after severe cold-working. This working does not enhance the anti-galling properties as is normal for carbon steels and some stainless steels. The benefit to the cold or hot work put into the material is added strength and hardness, and the wear resistance does not decrease noticeably. Chromium and Nickel additions give it comparable corrosion to 304 and 316 stainless steels, while having approximately twice the yield strength. The high mechanical strength in annealed parts permits use of reduced cross sections for weight, and cost reductions through the use of thinner stock.
Iron (Fe)59.1 to 65.4 %
Chromium (Cr)16 to 18 %
Nickel (Ni)8.0 to 9.0 %
Manganese (Mn)7.0 to 9.0 %
Silicon (Si)3.5 to 4.5 %
Nitrogen (N)0.080 to 0.18 %
Carbon (C)0 to 0.1 %
Phosphorus (P)0 to 0.060 %
Sulfur (S)0 to 0.030 %
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SIZE 6MM TO 200MM DIA ROUND BAR.
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SIZE 6MM TO 350MM OD PIPE .
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SIZE 6MM TO 200MM DIA ROUND BAR.
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SIZE 6MM TO 350MM OD PIPE .
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Applications
Superior resistance to hydrochloric acid, aluminum chloride catalysts and other strongly reducing chemicals. Excellent high-temperature strength in inert and vacuum atmospheres.
Hastelloy B2 is a nickel-molybdenum alloy particularly suited for equipment handling reducing chemical environments .
Applications in the chemical process industry involving sulfuric, phosphoric, hydrochloric and acetic acid. Temperature uses vary from ambient temperature to 1500°F depending on the environments (please call for technical advice).
Chemistry
Chemical Requirements | |||||||
---|---|---|---|---|---|---|---|
| Ni | Mo | Fe | Cr | C | Si | Mn |
Max | Bal. | 30.0 | 2.0 | 1.0 | 0.02 | 0.10 | 1.0 |
Min |
| 26.0 |
|
|
|
|
|
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Chemical Composition, %
Ni | Mo | Cr | Fe | W | Co | Mn | C |
---|---|---|---|---|---|---|---|
Remainder | 15.0-17.0 | 14.5-16.5 | 4.0-7.0 | 3.0-4.5 | 2.5 max | 1.0 max | .01 max |
V | P | S | Si | ||||
.35 max | .04 max | .03 max | .08 max |
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SIZE 6MM TO 200MM DIA ROUND BAR.
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The high strength, corrosion resistance, and low magnetic permeability of this alloy allows it to be used as a material for medical implants.
The following sections will discuss in detail about stainless steel grade NITRONIC®50 (XM-19).
Chemical CompositionThe chemical composition of stainless steel grade NITRONIC® 50 (XM-19) is outlined in the following table.
Element | Content (%) |
---|---|
Chromium, Cr | 20.5-23.5 |
Nickel, Ni | 11.5-13.5 |
Manganese, Mn | 4-6 |
Molybdenum, Mo | 1.5-3 |
Silicon, Si | 1 max |
Nitrogen, N | 0.20-0.40 |
Niobium, Nb | 0.10-0.30 |
Vanadium, Va | 0.10-0.30 |
Phosphorous, P | 0.04 max |
Carbon, C | 0.06 max |
Sulfur, S | 0.010 max |
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Product Details:
Minimum Order Quantity | 10 Kilogram |
Size Diameter | 6MM TO 200MM DIA ROUND BAR. |
Material Grade | Nickel |
Color | Gray |
Usage/Application | Industry |
Alloy | With Alloy |
Shape | Round |
Product Type | Nickel Alloy |
INCONEL® nickel-chromium-iron alloy 601 (UNS N06601/W.Nr. 2.4851) is a general-purpose engineering material for applications that require resistance to heat and corrosion. An outstanding characteristic of INCONEL alloy 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. The limiting chemical composition of INCONEL alloy 601 is listed in Table 1. The composition is a facecentered-cubic solid solution with a high degree of metallurgical stability. The alloy's nickel base, in conjunction with substantial chromium content, provides resistance to many corrosive media and high temperature environments. Oxidation resistance is further enhanced by the aluminum content.
CHEMICAL %
Nickel ..........................................................................58.0-63.0 Chromium....................................................................21.0-25.0
Iron ............................................................................Remainder
Aluminum ........................................................................1.0-1.7 Carbon........................................................................0.10 max.
Manganese ...................................................................1.0 max.
Sulfur ........................................................................0.015 max.
Silicon .........................................................................0.50 max. Copper..........................................................................1.0 max.
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INCOLOY® alloy 945 (UNS N09945) is a high-strength, corrosion-resistant alloy designed for demanding applications in the oil and gas industry. The properties of this age hardenable nickel-iron-chromium alloy are enhanced by its contents of molybdenum, copper, niobium, titanium, and aluminum. The chemical composition of alloy 945 is seen in Table 1. The alloy’s nickel content results in resistance to chlorideinduced stress corrosion cracking. Nickel, in conjunction with the molybdenum and copper, also gives alloy 945 outstanding resistance to general corrosion in reducing media. Molybdenum also imparts resistance to localized attack (pitting and crevice corrosion). The alloy’s content of chromium provides resistance in oxidizing environments. Niobium, titanium and aluminum participate in the age hardening reaction that occurs during heat treatment. Their interaction forms gamma prime and gamma double prime precipitates, which strengthen the alloy. INCOLOY alloy 945 is suitable for downhole oil and gas applications requiring high strength and corrosion resistance in aggressive sour wells containing high levels of hydrogen sulfide and chorides. Because of the alloy’s resistance to stress cracking in environments rich in hydrogen sulfide, it is suitable for downhole and surface gas-well components including tubular products, valves, hangers, landing nipples, tool joints and packers. The alloy can also be used for fasteners, pump shafting and high strength piping systems.
Chemical Composition of INCOLOY alloy 945, wt %
Nickel ......…………………………………..…..45.0-55.0
Chromium ..…………………………………….19.5-23.0
Iron ……………….………………………………Balance
Molybdenum …….………………………………..3.0-4.0
Niobium .…………………………………………..2.5-4.5
Copper …………………………………………….1.5-3.0
Titanium ….………………………………………..0.5-2.5
Aluminum ….…………………………………….0.01-0.7
Manganese ...……………………………………1.0 max.
Silicon …..………………………………………..0.5 max.
Sulfur …..……………………………………….0.03 max.
Phosphorous .………………………………….0.03 max.
Carbon …..…………………………………0.005 to 0.04
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The chemical composition of Alloy 800 is:
Ni | Cr | Fe | C | Al | Ti | Al+Ti |
---|---|---|---|---|---|---|
30.0-35.0 | 19.0-23.0 | 39.5 min | 0.10 max | 0.15-0.60 | 0.15-0.60 | 0.30-1.20 |
The chemical composition of alloy 800H is:
Ni | Cr | Fe | C | Al | Ti | Al+Ti |
---|---|---|---|---|---|---|
30.0-35.0 | 19.0-23.0 | 39.5 min | 0.05-0.10 | 0.15-0.60 | 0.15-0.60 | 0.30-1.20 |
The chemical composition of Alloy 800HT is :
Ni | Cr | Fe | C | Al | Ti | Al+Ti |
---|---|---|---|---|---|---|
30.0-35.0 | 19.0-23.0 | 39.5 min | 0.06-0.10 | 0.25-0.60 | 0.25-0.60 | 0.85-1.2 |
The forms of INCOLOY 800H/800HT are:
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The chemical composition of Alloy 800 is:
Ni | Cr | Fe | C | Al | Ti | Al+Ti |
---|---|---|---|---|---|---|
30.0-35.0 | 19.0-23.0 | 39.5 min | 0.10 max | 0.15-0.60 | 0.15-0.60 | 0.30-1.20 |
The chemical composition of alloy 800H is:
Ni | Cr | Fe | C | Al | Ti | Al+Ti |
---|---|---|---|---|---|---|
30.0-35.0 | 19.0-23.0 | 39.5 min | 0.05-0.10 | 0.15-0.60 | 0.15-0.60 | 0.30-1.20 |
The chemical composition of Alloy 800HT is :
Ni | Cr | Fe | C | Al | Ti | Al+Ti |
---|---|---|---|---|---|---|
30.0-35.0 | 19.0-23.0 | 39.5 min | 0.06-0.10 | 0.25-0.60 | 0.25-0.60 | 0.85-1.2 |
The forms of INCOLOY 800H/800HT are:
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