With operations spread across all 10 export locations and an annual turnover of 200,000 tons, we touch lives in every walk of life. Today, we supply steel to various sectors including Oil, Gas, Engineering and Construction, and are a leading structural steel distributor in the UAE.
Zecor And Zecor Z Material Manufacturer Supplier, Stockiest, Dealer, Trader, Distributors
MorcemCement 900 Supplier, Stockiest, Dealer, Trader, Distributors
A283 GR.C Stockiest In Saudi Arabia Supplier, Dealer, Trader, Distributors
A285 GR.C Stockiest In Saudi Arabia Supplier, Dealer, Trader, Distributors
High Nickel Material Manufacturer Supplier, Stockiest, Dealer, Trader, Distributors
Duranickel Alloy Supplier, Stockiest, Dealer, Trader, Distributors
Monel Alloy Supplier, Stockiest, Dealer, Trader, Distributors
Inconel Alloy Supplier, Stockiest, Dealer, Trader, Distributors
Nimonic Alloy Supplier, Stockiest, Dealer, Trader, Distributors
Nilo Alloy Supplier, Stockiest, Dealer, Trader, Distributors
Incoloy Alloy Supplier, Stockiest, Dealer, Trader, Distributors
Rubber Lines Spool Manufacturer Supplier, Stockiest, Dealer, Trader, Distributors
Nickel (59%), Chromium (15%), Cobalt (20%), Molybdenum, Aluminum, Titanium
Excellent high-temperature strength and oxidation resistance
Precipitation-hardenable alloy
Maintains strength and creep resistance up to 950°C (1742°F)
Gas turbines, jet engines, industrial gas turbines
Nickel (balance), Chromium (15-16%), Cobalt (up to 18%), Aluminum, Titanium, Molybdenum
High-temperature strength and resistance to oxidation and creep
Suitable for long-term use at temperatures up to 1050°C (1922°F)
Turbine blades, discs, and other high-temperature components in gas turbines and jet engines
Nickel (50-55%), Chromium (19-21%), Molybdenum (5.6-6.1%), Cobalt (20%) with Titanium and Aluminum
Good combination of high strength and ductility
Excellent weldability and formability
Maintains mechanical properties up to 800°C (1472°F)
Aerospace components, gas turbine engines, and combustion chambers
Nickel (42-47%), Chromium (11-14%), Iron (balance), Molybdenum (5.5-6.5%), Titanium, Aluminum
High strength and corrosion resistance
Good stability and resistance to stress cracking
Operates well at temperatures up to 650°C (1200°F)
Turbine rotors, shafts, and other components for aerospace and power generation
Nickel (45-50%), Chromium (14-16%), Iron (balance), Titanium, Molybdenum
High tensile and creep strength
Good oxidation and corrosion resistance
Suitable for long-term use at temperatures up to 750°C (1382°F)
Gas turbine blades, discs, and high-temperature fasteners
Nickel (40-45%), Chromium (14-18%), Iron (balance), Titanium, Molybdenum
Good high-temperature strength and oxidation resistance
Precipitation-hardenable for enhanced mechanical properties
Stable up to 750°C (1382°F)
Gas turbine components, nuclear reactors, and high-temperature fasteners
Nickel (63%), Chromium (28-29%), Iron (balance)
High creep and oxidation resistance
Excellent mechanical properties at elevated temperatures
Suitable for use up to 950°C (1742°F)
Gas turbine components, aerospace parts, and high-temperature fasteners
Nickel (35%), Cobalt (35%), Chromium (20%), Molybdenum (10%)
Excellent corrosion resistance, including in saltwater and acidic environments
High tensile strength and resistance to stress corrosion cracking
Biocompatible, making it suitable for medical applications
Medical devices, fasteners, springs, aerospace components, marine environments
Nickel (75%), Chromium (20%), Iron (balance)
Good mechanical properties and oxidation resistance at elevated temperatures
Easily fabricated and weldable
Suitable for use at temperatures up to 1000°C (1832°F)
Gas turbine components, heat treating equipment, and nuclear reactors
Nickel (75%), Chromium (19-21%), Titanium, Aluminum
High strength and excellent oxidation resistance
Good creep resistance at temperatures up to 815°C (1500°F)
Precipitation-hardenable for enhanced mechanical properties
Turbine blades, discs, bolts, and other high-temperature components
Nickel (balance), Chromium (19-21%), Cobalt, Titanium, Aluminum
Excellent high-temperature strength and oxidation resistance
Suitable for use in extreme environments
Good mechanical properties at elevated temperatures
Gas turbines, jet engines, and industrial heating systems
Nickel (balance), Chromium (18-21%), Cobalt (15-21%), Titanium, Aluminum
High tensile and creep-rupture strength
Excellent oxidation and corrosion resistance at high temperatures
Suitable for long-term use at temperatures up to 920°C (1688°F)
Turbine blades, discs, and other high-temperature components in jet engines and gas turbines
| Alloy | Composition | Properties | Applications |
|---|---|---|---|
| Nimonic 105 | Ni (59%), Cr (15%), Co (20%), Mo, Al, Ti | High-temperature strength, oxidation resistance, creep resistance | Gas turbines, jet engines, industrial gas turbines |
| Nimonic 115 | Ni (balance), Cr (15-16%), Co (up to 18%), Al, Ti, Mo | High-temperature strength, oxidation resistance, creep resistance up to 1050°C (1922°F) | Turbine blades, discs, high-temperature components in gas turbines and jet engines |
| Nimonic 263 | Ni (50-55%), Cr (19-21%), Mo (5.6-6.1%), Co (20%), Al, Ti | Good strength, ductility, weldability, formability, stable up to 800°C (1472°F) | Aerospace components, gas turbine engines, combustion chambers |
| Nimonic 901 | Ni (42-47%), Cr (11-14%), Fe (balance), Mo (5.5-6.5%), Ti, Al | High strength, corrosion resistance, stability up to 650°C (1200°F) | Turbine rotors, shafts, aerospace, and power generation components |
| Nimonic PE11 | Ni (45-50%), Cr (14-16%), Fe (balance), Ti, Mo | High tensile strength, creep strength, oxidation resistance, stable up to 750°C (1382°F) | Gas turbine blades, discs, high-temperature fasteners |
| Nimonic PE16 | Ni (40-45%), Cr (14-18%), Fe (balance), Ti, Mo | High-temperature strength, oxidation resistance, precipitation-hardenable | Gas turbine components, nuclear reactors, high-temperature fasteners |
| Nimonic PK33 | Ni (63%), Cr (28-29%), Fe (balance) | High creep and oxidation resistance, suitable for use up to 950°C (1742°F) | Gas turbine components, aerospace parts, high-temperature fasteners |
| Nimonic MP35N | Ni (35%), Co (35%), Cr (20%), Mo (10%) | Excellent corrosion resistance, high tensile strength, stress corrosion cracking resistance, biocompatible | Medical devices, fasteners, springs, aerospace, marine environments |
| Nimonic 75 | Ni (75%), Cr (20%), Fe (balance) | Good mechanical properties, oxidation resistance, easily fabricated, weldable, stable up to 1000°C (1832°F) | Gas turbine components, heat treating equipment, nuclear reactors |
| Nimonic 80A | Ni (75%), Cr (19-21%), Ti, Al | High strength, oxidation resistance, good creep resistance up to 815°C (1500°F), precipitation-hardenable | Turbine blades, discs, bolts, high-temperature components |
| Nimonic 86 | Ni (balance), Cr (19-21%), Co, Ti, Al | High-temperature strength, oxidation resistance, suitable for extreme environments | Gas turbines, jet engines, industrial heating systems |
| Nimonic 90 | Ni (balance), Cr (18-21%), Co (15-21%), Ti, Al | High tensile and creep-rupture strength, oxidation resistance up to 920°C (1688°F) | Turbine blades, discs, high-temperature components in jet engines and gas turbines |
