Search Results for superchargers

Crucible A-286 is an age-hardenable austenitic Fe-Ni-Cr alloy designed for service up to 704 deg C (1300 deg F) on jobs requiring high strength and good corrosion resistance at the operating temperature. The alloy offers high ductility in notched sections. Crucible A-286 is used in jet engines and superchargers for various high-temperature components and is one of the few age-hardenable alloys used for bolting in the ASME Boiler and Pressure Vessel Code. This datasheet provides information on composition, physical properties, hardness, 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: SS-851. Producer or source: Crucible Specialty Metals.

PYROMET A-286 is an age-hardenable austenitic iron-nickel-chromium alloy designed for service up to 1300 F (704 C) on jobs requiring high strength and good corrosion resistance at the operating temperature. It offers high ductility in notched sections. Pyromet A-286 is used in jet engines and superchargers for various high-temperature components. 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 forming, heat treating, machining, and joining. Filing Code: SS-340. Producer or source: Carpenter.

Böhler (or Boehler) T200 is an age-hardenable austenitic Fe-Ni-Cr alloy designed for service up to 704 deg C (1300 deg F) on jobs requiring high strength and good corrosion resistance at the operating temperature. The alloy offers high ductility in notched sections. The alloy is used in jet engines and superchargers for various high-temperature components and is one of the few age-hardenable alloys used for bolting in the ASME Boiler and Pressure Vessel Code. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness and creep. It also includes information on forming, heat treating, and machining. Filing Code: SS-1205. Producer or source: Böhler-Uddeholm Specialty Metals Inc..

REPUBLIC RS-140X is a titanium alloy containing iron, chromium and aluminum as its principal alloying additions. It is primarily a bar and forging alloy. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness. It also includes information on forming, heat treating, machining, and joining. Filing Code: Ti-7. Producer or source: Republic Steel Corporation, Titanium Division.

MEEHANITE HSV is an iron developed essentially for long, continuous heating at temperatures up to 1600 F. It was designed to provide good load-bearing capacity at elevated temperatures. 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 casting, heat treating, machining, joining, and surface treatment. Filing Code: CI-41. Producer or source: Meehanite Metal Corporation.

UNITEMP A-286 is an austenitic stainless steel suitable for applications requiring moderately high strength to 1300 F and oxidation resistance to about 1500 F. It is also satisfactory for service as low as 423 F in two conditions: (1) Solution treated plus aged and (2) Cold worked plus aged. This alloy is also used in high-strength non-magnetic applications because it remains essentially non-magnetic even after severe cold working. This datasheet provides information on composition, physical properties, hardness, elasticity, 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: SS-295. Producer or source: Cyclops.

Timken 16-15-6 is a non-magnetic, 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, microstructure, hardness, and tensile properties as well as creep. It also includes information on forming, heat treating, machining, and joining. Filing Code: SS-150. Producer or source: Timken Roller Bearing Company.

Allvac A-286 is an age-hardening austenitic stainless steel and a superalloy. Its high strength and corrosion resistance give it many applications including bolting. This datasheet provides information on composition, physical properties, hardness, 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: SS-911. Producer or source: Allvac Metals Company.

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.

G-E ALLOY X-63 is a cobalt-base alloy having excellent oxidation and corrosion resistance. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on high temperature performance and corrosion resistance as well as heat treating, machining, and joining. Filing Code: Co-19. Producer or source: General Electric Company, Metallurgical Products Department. Originally published March 1960, revised June 1963.

MAGNESIUM ALLOY-TA54A is a general purpose hammer-forging alloy having intermediate strength. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Mg-44. Producer or source: Aluminum Company of America.

LESCALLOY 5616 is a hardenable chromium-nickel-tungsten alloy steel recommended for service temperatures up to 1200 F in highly stressed parts. 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: SA-195. Producer or source: Latrobe Steel Company.

ALUMINUM ALLOY(S) 206.0 and A206.0 are structural castings in the heat treated temper for applications requiring high tensile and yield strengths with moderate elongation. This datasheet provides information on composition, physical properties, tensile properties, and compressive, shear, and bearing strength as well as fatigue. It also includes information on as well as heat treating. Filing Code: AL-335. Producer or source: Various aluminum companies.

Electralloy A-286 is an austenitic precipitation-hardening Fe-Ni-Cr alloy. It is used for applications requiring high strength and corrosion resistance up to 650 deg C (1200 deg F), and for lower-stress applications at higher temperatures. It has applications at ambient temperatures where a heat treatable, nonmagnetic material is required. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SS-977. Producer or source: Electralloy, a Division of G.O. Carlson Inc.

Aluminum A357 is a high strength, pressure tight sand and permanent mold aluminum casting alloy. It is age-hardenable. It is recommended for cast gear cases, cylinder heads, transmission cases and strong structural castings. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on high temperature performance and corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Al-163. Producer or source: Aluminum Company of America.

Altemp V36 is a cobalt-base alloy recommended for high temperature applications. It has high oxidation and corrosion resistance. It shows a slight response to a precipitation-hardening heat treatment. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep, deformation, and fatigue. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Co-25. Producer or source: Allegheny Ludlum Corporation.

PANDEX VAC ARC is a precipitation hardening, austenitic, heat resisting alloy designed for service at elevated temperatures where high strength and good corrosion resistance are required. This datasheet provides information on composition, physical properties, hardness, elasticity, 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, and joining. Filing Code: SS-115. Producer or source: Latrobe Steel.

BA.46 is a heat treatable aluminum casting alloy. It is recommended for high strength, pressure-tight castings. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on corrosion resistance as well as heat treating and machining. Filing Code: Al-24. Producer or source: The British Aluminium Company Ltd.

BA.LMB is a heat treatable aluminum casting alloy. It is recommended for high strength, pressure-tight castings. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on high temperature performance and corrosion resistance as well as heat treating, machining, and joining. Filing Code: Al-162. Producer or source: The British Aluminium Company Ltd.

Aluminum A356 is a sand and permanent mold casting alloy that responds to an age-hardening heat treatment. It is recommended for aircraft and missile components where high strength and corrosion resistance are required. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on heat treating, machining, and joining. Filing Code: Al-192. Producer or source: Aluminum Company of America.