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201
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Chromium nickel manganese steel was developed as a satisfactory alternate for Type 301 for many applications.
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301
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Chromium nickel steel capable of attaining high tensile strength and ductility by moderate or severe cold working.
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302
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General purpose chromium nickel stainless steel. Its corrosion resistance is superior to that of Type 301. It can be cold worked to high tensile strengths but with slightly lower ductility than Type 301.
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304
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Low carbon chromium nickel stainless and heat resisting steel somewhat superior to Type 302 in corrosion resistance.
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304L
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Very low carbon chromium nickel steel with general corrosion resistance similar to Type 304 but with superior resistance to intergranular corrosion following welding or stress relieving. It is recommended for use in parts which are fabricated by welding and which cannot be subsequently annealed.
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305
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A high corrosion-resistant alloy with low rate of work hardening, designed for extra deep drawing and spinning.
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309
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High corrosion-resistant, chromium nickel grade with carbon limited to .08 to reduce carbon precipitation during welding.
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310
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Similar to 309 with higher resistance to corrosion and oxidation at elevated temperatures.
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316
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Chromium nickel stainless and heat resisting steel with superior corrosion resistance to other chromium nickel steels when exposed to many types of chemical corrodents; superior creep strength at elevated temperatures.
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316L
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Low carbon chromium nickel stainless steel with general corrosion resistance similar to Type 316 but with superior resistance to intergranular corrosion following welding or relieving. It is recommended for use in parts which are fabricated by welding and cannot be subsequently annealed.
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316TI
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Ti stabalized version of 316 with resistance to sensitization. (The formation of grain boundary chromium carbides at evaluated temperatures.)
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317L
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Similar to 316L but with additional molybdenum to improve corrosion resistance.
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321
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Chromium nickel steel containing titanium.Recommended for parts fabricated by welding which cannot be subsequently annealed. Also recommended for parts to be used at temperatures between 800°F and 1850°F.
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347
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Chromium nickel steel containing columbium and tantalum which is recommended for parts fabricated by welding which cannot be subsequently annealed. Also recommended for parts to be used at temperatures between 800°F and 1850°F.
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CARPENTER® 20 CB3, 10
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A highly corrosion-resistant alloy used in the chemical industry for applications where corrosion resistance is extremely critical,superior to the general run of 300 type stainless.
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2304
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A lean austenitic-ferritic duplex stainless steel with general corrosion resistance similar to 316, but with yield strength nearly double that of austenitic stainless steels.
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2205
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A nitrogen, molybdenum enhanced austenitic-ferritic duplex stainless steel with general corrosion resistance similar to 904L, but with a yield strength nearly double that of austenitic stainless steels.
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2507
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A super austenitic-ferritic duplex stainless steel with exceptional strength and corrosion resistance ideal for chemical process, petrochemical, and seawater applications.
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430
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General purpose grade, corrosion-resistant, straight chromium grade, non-heat-treatable.
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430LI
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Similar to straight 430 in corrosion and mechanical properties. The low interstitials provide improved transverse bending over straight 430.
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434
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Modification of Grade 430 designed for automotive trim and resistance to atmospheric corrosion.
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444
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A low carbon, low nitrogen, ferritic that provides pitting and crevice corrosion resistance superior to most ferritic grades.
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Grade 9 Ti 3-2.5
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Alpha-Beta alloy-considered very weldable. Superior to high strength C.P.Ti of equivalent strength level in weld toughness and useful temp. range. May be strengthened by cold working.
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Ti 15-3-3-3
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A cold formable metastable beta alloy available in foil and strip which is typically aged to high strengths after fabrication.
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Grade 21 Ti Beta 21 S
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A cold formable metastable beta alloy available in foil and strip with improved oxidation resistance, elevated temperature strength and creep resistance.
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Grade 5, Ti 6-4
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Grade 5 is the work horse of all titanium grades. It is also known as Ti-6AL-4V or simply Ti6-4. Its high strength, light weight and corrosion resistance enables it to be used in many applications. The most common is aerospace components. The alloy is also "age hardenable" by heat treatment to achieve even higher strengths
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Ti 6-2-4-2
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Ti 6Al-2Sn-4Zr-2Mo has good tensile creep and fatigue properties up to 1000 F. It is the most commonly used high temperature titanium alloy in jet engine compressors and airframe structures.
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410
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General purpose corrosion and heat resisting chromium steel. Good corrosion resistance and fair machining properties. Can be treated to RC35/45.
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420
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Chromium steel capable of hardening to a maximum of approximately RC53/58.
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440A
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High carbon grade, high chromium, capable of being heat treated to a hardness range of RC51/62.
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17-7PH®4
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A chromium nickel stainless steel with characteristics of good workability, easy hardening, high strength, and excellent mechanical properties at elevated temp., can be heat treated at relatively low temperature for high strength properties.
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17-4PH®4
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Precipitation hardening stainless steel with high strength and good corrosion resistance to 600°F. Used in aerospace, chemical, petrochemical, paper and metalworking industries.
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PH15-7Mo®4
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Similar to 17-7PH. alloy, but with molybdenum added for higher strength with heat treatment.
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A2864
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An iron, nickel chromium alloy designed for service up to 1300°F where high strength and corrosion resistance are required.
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AM 3508
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Similar to 17-7PH. alloy and PH15-7Mo. alloy, but with slightly higher elevated temperature capability.
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NIOBIUM TYPE 1
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Pure niobium, reactor grade, high melting point, corrosion resistant for use in medical and high temperature industrial applications.
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NITINOL
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NITINOL (an acronnym for Nickel Titanium Naval Ordinance Laboratory) is a family of intermetallic materials, which contain a nearly equal mixture of nickel (55 wt. %) and titanium. Other elements can be added to adjust the material properties. Nitinol exhibits unique bahavior such as "Shape Memory" and "Superelasticity". Nitinol is used for both consumer and medical applications.
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NIOBIUM TYPE 2
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a commercial grade alloy with an extremely high melting point and corrosion resistant properties. High thermal/electric conductivity, easily fabricated, bio compatible.
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ZIRCONIUM 702
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a refractory metal with excellent corrosion resistance. Zirconium 702 exhibits good ductility and good
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NICKEL 200
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Commercially pure nickel. High corrosion resistance. Used in food handling and electronics.
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NICKEL 201
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Similar to Nickel 200 except with a lower carbon content for better formability. Most applications in chemicals.
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PERMANICKEL 300
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Age - hardenable, high nickel alloy, with very good thermal electrical conductivity.
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MONEL® 4001
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A solid solution alloy with high strength and toughness over wide temp. ranges. Used in electronic components, springs.Corrosion resistant and oxidation resistance to 1000°F.
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MONEL® K-5001
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Similar to Monel. 400™ but with higher tensile strength; a precipitation hardening alloy. Used in oil well drilling collars, doctor blades. Good strength and ductility 423°F to 1200°F.
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INCONEL® 6001
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Has high corrosion and heat resistance combined with excellent strength and workability. Mainly used in corrosive atmospheres. Oxidation resistance to 2150°F.
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INCONEL® 6251
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Outstanding corrosion resistance with excellent fabricability. Good for cryogenic to high temp. applications up to 2000°F.
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INCONEL® 7181
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High strength and corrosion resistance for use in temp. ranges from -423°F to 1300°F. Nuclear applications.
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INCONEL® X-7501
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A precipitation hardening nickel-chromium alloy with useful strength to 1500°F. Good corrosion and oxidation resistance.
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INCOLOY® 8001
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Nickel-iron-chromium alloy that is carburization resistant at elevated temp.
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INCOLOY® 8251
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An alloy that is highly resistant to ggressively corrosive environments such as sulfuric, phosphoric acids and seawater.
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Ni-SpanC® 9021
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A nickel-iron-chromium alloy used in precision spring applications subject to severe temp. fluctuations.
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HASTELLOY® C-2762
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Used in chemical industry for resistance to oxidizing agents. Replaces Hastelloy. C™ with better fabricability.
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HASTELLOY C-22
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A versatile nickel chromium molybdenum tungsten alloy with resistance to a variety of industrial chemicals. Superior weldability.
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HASTELLOY G-30
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High chromium nickel base alloy with superior corrosion resistance to phosphoric acids and environments with highly oxidizing acids.
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HASTELLOY® B-3
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Used in chemical industry for resistance to hydrochloric acid, sulfuric acid, phosphoric acid. Oxidation atmosphere resistant to 1400°F.
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HASTELLOY® X2
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Jet engine components for afterburner sections, blades, tailpipes, furnace applications, honey-comb, bellows, ducting. Good strength and oxidation resistance to 2200°F.
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HAYNES® 2142
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Nickel based precipitation strengthened alloy with oxidation resistance to 2200°F. For furnace parts exposed to carburizing, chlorine contaminated and oxidizing atmospheres; gas turbine parts.
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HAYNES® 2302
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Nickel-chromium-tungsten-molybdenum alloy with outstanding resistance to oxidizing environments up to 2100°F for prolonged periods.
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HAYNES® 2422
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Age hardenable, nickel alloy for use up to 1300°F. Low thermal expansion, good oxidation resistance and excellent aged ductility. Suited for gas turbine engines and chemical process plants.
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MONEL® 4011
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An alloy mainly used for thermal and electronic applications. Sometimes called Constantan this alloy is 44% Nickel and 56% Copper.
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HAYNES® 1882
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A cobalt-based alloy with excellent high temperature strength and oxidation resistance to 2000°F, combined with outstanding post-standing ductility.
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HAYNES® 25 L-6052
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Jet engine components, combustion chambers, afterburner parts. Oxidation and carburization resistant to 1900°F. Good high temperature strength.
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WASPALOY6
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Jet engine turbine wheels, buckets, spacers, shafts. Good for high temperature applications.
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HAYNES® 263
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nickel base gamma prime strengthened alloy with 19% to 21% cobalt content. It offers high strength up to 1600 F. Haynes 263 alloy has good formability.
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Grade 1
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Low residual grade of commercially pure titanium available in foil and strip. Its excellent ductility when combined with proper grain size control makes this product ideal for deep drawing.
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Grade 2
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Alpha grade for applications requiring max. ductility and formability. Strength similar to austenitic stainless steel.
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Grade 3
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Alpha Phase C.P.Ti. Moderate strength with good formability. Used for airframes, chemical and similar applications.
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Grade 4
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Alpha phase C, pure Ti. Highest strength of the CP grades. Used for airframes and similar applications.
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Alloy