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Inconel 718 Sheet
Minimum Order Quantity: 5 Kilogram
Product Brochure
Plate Type | Inconel Plate, Nickel Plate |
Usage/Application | Furnace, Chemical, Research |
Material | Nickel Alloys |
Material Grade | Inconel 718 |
Condition | New |
Steel Grade | Inconel 718 |
Shape | Rectangle, Square |
Inconel | Yes |
Size | 1-100mm |
Resistant Temperature | Inconel 718 |
Inconel 718 is a nickel-chromium-molybdenum alloy designed to resist a wide range of severely corrosive environments, pitting and crevice corrosion. This nickel steel alloy also displays exceptionally high yield, tensile, and creep-rupture properties at high temperatures. This nickel alloy is used from cryogenic temperatures up to long term service at 1200° F. One of the distinguishing features of Inconel 718’s composition is the addition of niobium to permit age hardening which allows annealing and welding without spontaneous hardening during heating and cooling. The addition of niobium acts with the molybdenum to stiffen the alloy’s matrix and provide high strength without a strengthening heat treatment. Other popular nickel-chromium alloys are age hardened through the addition of aluminum and titanium. This nickel steel alloy is readily fabricated and may be welded in either the annealed or precipitation (age) hardened condition. This superalloy is used in a variety of industries such as aerospace, chemical processing, marine engineering, pollution-control equipment, and nuclear reactors.
Maraging 300/Vascomax 300 (UNS K93120) Round Bar
Product Brochure
Usage/Application | Oil & Gas Industry |
Country of Origin | Made in India |
C |
.03 max |
MN |
.10 max |
P |
.01 max |
S |
.01 max |
Si |
.10 max |
Ni |
18.50 |
Mo |
4.80 |
Co |
9.00 |
Ti |
.60 |
Al |
.10 |
B |
.003 |
Zr |
.01 |
Maraging 250/Vascomax C250 (UNS K92890) Round Bar
Product Brochure
Usage/Application | Oil & Gas Industry |
Country of Origin | Made in India |
Weight% | Ni | Co | Mn | Si | C | Al | Mo | S | P | Ti | Fe | Cr | Cu |
C250 | 17.0 / 19.0 | 7.0 / 8.5 | 0.10 max | 0.10 max | 0.03 max | 0.05 / 0.15 | 4.6 / 5.2 | 0.010 max | 0.010 max | 0.3 / 0.5 | Bal | 0.50 | 0.50 |
Material | Condition | Ultimate Tensile (min) | Yield Strength (Min) | Elongation in 4D % (min) | Hardness | ||
Mpa | Ksi | Mpa | Ksi | ||||
Vascomax 250 | After Maraging heat treatment 900°F | 1758 | 255 | 1724 | 250 | 6 | ≥ 48 HRC |
Maraging 300/Vascomax 300 (UNS K93120) Sheet/Plate.
Product Brochure
Usage/Application | Oil & Gas Industry |
Country of Origin | Made in India |
C |
.03 max |
MN |
.10 max |
P |
.01 max |
S |
.01 max |
Si |
.10 max |
Ni |
18.50 |
Mo |
4.80 |
Co |
9.00 |
Ti |
.60 |
Al |
.10 |
B |
.003 |
Zr |
.01 |
Inconel 718 Flanges
Minimum Order Quantity: 1 Number
Product Brochure
Grade | Inconel 718 |
Product Type | Flanges |
Usage/Application | Furnace, Chemical |
Material Standard | ANSI B16.5, ASTM A351 |
Material | Inconel |
Color | Bright |
Condition | New |
Iso Certified | Yes |
Inconel 718 is a nickel-chromium-molybdenum alloy designed to resist a wide range of severely corrosive environments, pitting and crevice corrosion. This nickel steel alloy also displays exceptionally high yield, tensile, and creep-rupture properties at high temperatures. This nickel alloy is used from cryogenic temperatures up to long term service at 1200° F. One of the distinguishing features of Inconel 718’s composition is the addition of niobium to permit age hardening which allows annealing and welding without spontaneous hardening during heating and cooling. The addition of niobium acts with the molybdenum to stiffen the alloy’s matrix and provide high strength without a strengthening heat treatment. Other popular nickel-chromium alloys are age hardened through the addition of aluminum and titanium. This nickel steel alloy is readily fabricated and may be welded in either the annealed or precipitation (age) hardened condition. This superalloy is used in a variety of industries such as aerospace, chemical processing, marine engineering, pollution-control equipment, and nuclear reactors.