Search Results for high-temperature alloys

Nicrofer 5520 Co B is a Ni-Cr-Co-Mo-Nb high temperature alloy improved in strength over Nicrofer 5520 Co (Alloy Digest Ni-480, March 1995). 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-725. Producer or source: ThyssenKrupp VDM GmbH.

PYROMET X-751 is an age hardenable nickel-base alloy with good stress-rupture properties at 1600 F. It is highly resistant to chemical corrosion and oxidation. 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: Ni-190. Producer or source: Carpenter Technology Corporation.

PYROMET 90 is a precipitation-hardenable nickel-base alloy with high strength at high temperatures. It is highly resistant to oxidation, scaling, heat and corrosion. 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, joining, and surface treatment. Filing Code: Ni-192. Producer or source: Carpenter Technology Corporation.

WESTINGHOUSE W545 is a heat treatable iron-base alloy having good high temperature strength and oxidation resistance. It is corrosion and heat resistant. Temperature range of principal usage is 1100 F. to 1350 F. Made by Consumable Electrode Vacuum Arc Melting Only. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as creep. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: SS-87. Producer or source: Midvale-Heppenstall Company.

AISI No. 685 is a nickel-base, austenitic, precipitation-hardenable alloy. It has excellent tensile and stress-rupture strength to 1400 F and high resistance to corrosion and oxidation at temperatures at least to 1600 F. It is used widely in airframe assemblies, gas turbine engines and missile systems. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as fracture toughness and creep. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-271. Producer or source: Nickel alloy mills.

PYROMET 751 is an age-hardenable nickel-base alloy with good stress-rupture properties to 1600 F. Its creep rate is low under high stresses at 1200-1500 F. It is highly resistant to chemical corrosion and oxidation. 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-335. Producer or source: Carpenter Technology Corporation.

TIMETAL 1100, a near alpha alloy, was developed for elevated temperature use around 1100 F (600 C). The alloy is to be used in the beta processed condition. The alloy offers the highest combination of strength, creep resistance, fracture toughness, and stability of any commercially available titanium alloy. This datasheet provides information on composition, physical properties, and tensile properties as well as creep and fatigue. It also includes information on high temperature performance as well as forming and heat treating. Filing Code: TI-104. Producer or source: Timet.

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.

COLUMBIUM ALLOY SU-31 is a columbium-base alloy designed to operate at temperatures up to 1300 C (2372 F). This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep and fatigue. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Cb-18. Producer or source: Kawecki Berylco Industries Inc..

INCONEL Alloy 617 is a solid solution nickel-chromium-cobalt-molybdenum alloy having excellent high-temperature strength and oxidation resistance. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as fracture toughness and creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-179. Producer or source: Huntington Alloy Products Division, An INCO Company.

HASTELLOY alloy S is a nickel-base high-temperature alloy having excellent thermal stability, good high-temperature mechanical properties and excellent resistance to oxidation up to 2000 F. 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-184. Producer or source: Stellite Division, Cabot Corporation.

MAR-M Alloy 432 is a nickel-base alloy for castings requiring high tensile and creep strengths, excellent hot corrosion resistance and good thermal stability in the temperature range 1200-1800 F (649-982 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 casting, heat treating, machining, joining, and surface treatment. Filing Code: Ni-194. Producer or source: Licensees of Martin Marietta Corporation.

WC-3015 is a columbium-base alloy developed for structural applications in high-temperature oxidizing environments. It is characterized by good oxidation resistance, good mechanical properties and compatibility with silicide coatings. Cold-rolled sheet can be joined and welded without cracking. 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, joining, and surface treatment. Filing Code: Cb-21. Producer or source: Wah Chang, a Teledyne Corporation.

HASTELLOY Alloy C-4 is a nickel-chromium-molybdenum alloy with outstanding high-temperature stability as shown by high ductility and corrosion resistance even after long-time aging in the range 1200-1900 F. Alloy C-4 also has excellent resistance to stress-corrosion cracking and to oxidizing atmospheres up to 1900 F. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-211. Producer or source: Stellite Division, Cabot Corporation.

HAYNES Alloy No. 36 is a cobalt-base alloy having excellent strength at temperatures up to 1800 deg. F. It is the cast modification of wrought HAYNES Alloy No. 25 and has been used successfully in jet engine blading and nozzle vanes. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness and creep. It also includes information on high temperature performance and corrosion resistance as well as heat treating, machining, and joining. Filing Code: Co-17. Producer or source: Haynes Stellite Company.

The 16-25-6 alloy developed by the Timken Roller Bearing Company, Steel and Tube Division, is a nonmagnetic, austenitic, corrosion and heat resistant steel having high creep resistance at elevated temperatures and good corrosion and oxidation resistance. It age-hardens at elevated temperatures after solution quenching, and possesses very high mechanical properties. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness, creep, and deformation. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: SS-12. Producer or source: Timken Roller Bearing Company. Originally published November 1953, revised February 1960.

DCM ALLOY is a cast age-hardenable nickel-base high temperature alloy recommended for its high stress-temperature range of operation. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance as well as heat treating, machining, joining, and surface treatment. Filing Code: Ni-59. Producer or source: Metals Division, Kelsey Hayes Company.

Haynes No. 713C is a nickel-base, vacuum melted, vacuum-cast alloy with excellent high-strength characteristics through 1800 F. It combines extraordinarily high strength with good ductility. It is a precipitation-hardening investment-cast alloy. This datasheet provides information on composition, physical properties, and tensile properties as well as fracture toughness and creep. It also includes information on low and high temperature performance, and corrosion resistance as well as machining. Filing Code: Ni-64. Producer or source: Haynes Stellite Company.

Pyromet Alloy 617 is both oxidation resistant and very strong at high temperatures. It has one of the highest allowable stress values in the ASME Boiler and Pressure Vessel Code at 982 deg C (1800 deg F). This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear strength. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, and machining. Filing Code: Ni-695. Producer or source: Carpenter Specialty Alloys.

ALLOY 188 is a cobalt-base alloy designed for critical high-temperature applications up to 2000 F. It offers the excellent oxidation resistance of the chromium-nickel alloys (through a minute addition of lanthanum) and good post-aging ductility. It is primarily a solid-solution-strengthened alloy, is readily cold worked to increase strength and hardness, and is weldable by conventional methods. It is used in the aerospace, chemical and nuclear fields. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Co-76. Producer or source: Superior Tube Company.