HOME FEATURED INVENTORY ALL PRODUCTS PROCESSING SERVICES QUALITY ABOUT US CONTACT US L605 is a cobalt-chromium-tungsten-nickel alloy. It has good formability, high strength to 1500°F, and good oxidation resistance to 2000°F. L605 is non-magnetic and have excellent resistance to hot and corrosive atmospheres. It is especially resistant to carburizing atmospheres up to 1600ºF. The high chromium content makes it resistant to corrosion in a wide range of environments such as wet chlorine, hydrochloric acid and nitric acid. For maximum ductility, fabricated components should be annealed 2150-2250°F followed by a rapid cooling. Common stock sizes: .250” to 2.50” diameters. Common Specifications: Industry Trade Names: Common Applications: Composition Element Min. Max. Carbon 0.05 0.15 Manganese 1.00 2.00 Silicon -- 0.40 Phosphorus -- 0.040 Sulfur -- 0.030 Chromium 19.00 21.00 Nickel 9.00 11.00 Tungsten 14.00 16.00 Iron -- 3.00 Cobalt remainder LINE CARD Aerospace Defense Medical Oil & Gas Power Generation COMPANY Featured Inventory Products About Us Processing Services Quality INVENTORY Alloy Steels Aluminum Cobalt Alloys Nickel Alloys Stainless Steel Titanium SIGN UP FOR OUR NEWSLETTER & QUANTITY UPDATES SUBSCRIBE © Copyright 2021 ROCKWELL INDUSTRIES INTERNATIONAL CORP.

HOME FEATURED INVENTORY ALL PRODUCTS PROCESSING SERVICES QUALITY ABOUT US CONTACT US Inconel 718 is a nickel-chromium-molybdenum alloy designed to resist a wide range of corrosive environments, pitting and crevice corrosion. This nickel alloy also displays high tensile and creep-rupture properties at elevated temperatures. 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, the niobium acts with the molybdenum to stiffen the alloy’s matrix and provide high strength without a strengthening heat treatment. Other popular nickel alloys are often 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. Common applications are jet engine components, bolts, fasteners, afterburners, oil & gas. Common stock sizes: .500” to 12.000” diameters. Common Specifications: Industry Trade Names: Composition Element Min. Max. Carbon -- 0.8 Manganese -- 0.35 Silicon -- 0.35 Phosphorus -- 0.010 Sulfur -- 0.015 Chromium 17.00 21.00 Nickel 50.00 55.00 Molybdenum 2.80 3.30 Copper -- 0.30 Columbium (Niobium) 4.75 5.50 Titanium 0.65 1.15 Aluminum 0.20 0.80 Cobalt -- 1.00 Boron -- 0.006 Lead -- 0.0005 (5 ppm) Bismuth -- 0.00003 (0.3 ppm) Selenium -- 0.0003 (3ppm) Iron remainder LINE CARD Aerospace Defense Medical Oil & Gas Power Generation COMPANY Featured Inventory Products About Us Processing Services Quality INVENTORY Alloy Steels Aluminum Cobalt Alloys Nickel Alloys Stainless Steel Titanium SIGN UP FOR OUR NEWSLETTER & QUANTITY UPDATES SUBSCRIBE © Copyright 2021 ROCKWELL INDUSTRIES INTERNATIONAL CORP.