PYROMET alloy 88 is an age hardenable nickel-base alloy with high strength good corrosion and oxidation resistance. It possesses low creep rate in the temperature range 1200-1500 F (650-820 C). Above 1500 F (820 C), the effect of age hardening is lost and the alloy is used in the annealed condition. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on corrosion resistance as well as forming, heat treating, and machining. Filing Code: Ni-185. Producer or source: Carpenter Technology Corporation. Originally published February 1973, revised August 1989.

HAYNES ALLOY No. 214 is a nickel-base alloy with excellent oxidation resistance to 2200 F (1205 C), attributable to the tenacious and protective A1203-type film which is modified by a small but effective amount of yttrium. The alloy is also useful in carburizing service and in resisting chlorine contaminated atmospheres. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, and joining. Filing Code: Ni-336. Producer or source: Cabot Corporation.

HAYNES alloy No. 263 is a vacuum-melted and electroflux-refined high-temperature nickel-base alloy. It has good formability and weldability. It was developed by Rolls Royce. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep, and deformation. It also includes information on corrosion resistance as well as forming, heat treating, and joining. Filing Code: Ni-352. Producer or source: Haynes International Inc..

ALLVAC I-700 is a nickel-base alloy solid-solution strengthened by appreciable additions of cobalt, chromium and molybdenum. It is precipitation hardenable by virtue of aluminum and titanium additions. It is produced by vacuum induction melting followed by vacuum are remelting. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-377. Producer or source: Allvac Inc..

NICKEL VAC H-X is a non-heatreatable nickel-base alloy with excellent cold forming and welding characteristics. It has good strength and oxidation resistance up to 2200 F(1204 C). This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-381. Producer or source: Teledyne Allvac.

PYROMET alloy 41, a precipitation hardening nickel-base alloy possesses high strength in the 1200/1800 F (649/986 C) temperature range This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-237. Producer or source: Carpenter Technology Corporation. Originally published December 1976, revised October 1991.

PYROMET alloy M-252 was designed for use in highly stressed parts operating at temperatures up to 1600 F (871 C). This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, and machining. Filing Code: Ni-397. Producer or source: Carpenter Technology Corporation.

NICROBELL alloys were developed to be compatible with and complimentary to the thermoelectric conductors used for thermocouples and other conducting cables. This datasheet provides information on composition and physical properties. Filing Code: Ni-453. Producer or source: Nicrobell Pty Ltd.

P/M RENE 95 is a high strength, high temperature alloy used for rotating jet turbine components. Supersolvus P/M Rene 95 provides even higher temperature creep and stress-rupture resistance than standard Rene 95. Both are available as-HIP performs. A typical application is a high pressure turbine disc. This datasheet provides information on composition and tensile properties as well as creep. It also includes information on high temperature performance as well as heat treating and powder metal forms. Filing Code: Ni-434. Producer or source: Crucible Compaction Metals.

PYROMET Alloy 80A, a high-temperature nickel-base alloy is characterized by its excellent creep resistance, high fatigue properties under very arduous conditions and high oxidation resistance. This datasheet provides information on composition, physical properties, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, and machining. Filing Code: Ni-189. Producer or source: Carpenter Technology Corporation. Originally published April 1973, revised October 1989.

Carlson Alloy C601 is characterized by high tensile, yield and creep-rupture strengths for high temperature service. The alloy is not embrittled by extended exposure to high temperatures and has excellent resistance to stress-corrosion cracking, to carburizing, nitriding and sulfur containing environments. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on forming, heat treating, machining, and joining. Filing Code: Ni-458. Producer or source: G.O. Carlson Inc.

This alloy improves upon the excellent high-temperature corrosion resistance of INCONEL alloy 690 (see Alloy Digest Ni-266, March 1981) through an addition of aluminum. Inconel Alloy 693 is typically 61% Ni, 29% Cr, 3.3% Al, and 0.7% Nb, with the balance being principally iron. By virtue of its contents of chromium and aluminum, alloy 693 offers particularly good resistance to oxidation, carburization, sulfidation, and special resistance to metal dusting. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming and heat treating. Filing Code: Ni-617. Producer or source: Special Metals Corporation.

INCONEL ALLOY 601GC is a nickel-chromium-iron alloy with additions of aluminum, zirconium, and nitrogen to resist oxidation and micro-alloy, the last to pin the grain boundaries and prevent grain growth at high temperatures. Maintaining finer grain sizes especially helps low cycle fatigue life. This datasheet provides information on composition, physical properties, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as heat treating and joining. Filing Code: Ni-410. Producer or source: Inco Alloys International Inc..

NICROFER 4722 Co is a high-strength matrix-stiffened nickel-chromium-molybdenum-iron alloy with cobalt and tungsten additions. It has excellent oxidation resistance up to 2190 F (1200 C). This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-358. Producer or source: Vereingte Deutsche Metallwerke AG.

The Microcast-X process produces a finer grain size than earlier produced castings which improves mechanical properties in IN-718 without negative impact on rupture properties in temperatures of interest for applications in the aerospace market. This datasheet provides information on composition, microstructureelasticity, and tensile properties as well as fatigue. It also includes information on casting and heat treating. Filing Code: Ni-482. Producer or source: Howmet Corporation.

Grade ET50N is a 50 Nickel-50 Chromium type alloy developed for resistance to flue gas corrosion, particularly Bunker C oil with high sulfur and vanadium. This datasheet provides information on composition, physical properties, and tensile properties as well as creep. It also includes information on joining. Filing Code: Ni-485. Producer or source: Schmidt & Clemens Inc.

P/M LOW CARBON ASTROLOY offers good ductility and oxidation resistance in addition to excellent strength at high temperatures. This datasheet provides information on composition, physical properties, microstructure, and elasticity as well as creep. It also includes information on high temperature performance as well as heat treating. Filing Code: Ni-428. Producer or source: Crucible Compaction Metals.

Nicrofer 4626MoW is a solid-solution nickel-base alloy with equal additions of molybdenum, cobalt and tungsten. The alloy is normally used above 1472 F (800 C) and has good mechanical strength with resistance to creep, carburization, oxidation and sulfidation. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-436. Producer or source: VDM Technologies Corporation.

Nicrofer 5120 CoTi is a precipitation-hardening alloy developed by Rolls-Royce. The alloy has good oxidation resistance with excellent creep-rupture values. This datasheet provides information on composition, physical properties, and elasticity. It also includes information on forming, heat treating, machining, and joining. Filing Code: Ni-438. Producer or source: VDM Technologies Corporation.

HAYNES ALLOY No. 150 is a cobalt-base alloy with excellent thermal shock resistance. It has a higher melting point than other cobalt-and nickel-base high-temperature alloys and resists high-temperature corrosion in air and air-sulfur dioxide atmospheres. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Co-84. Producer or source: Haynes International Inc..