ALUMINUM A332.0

ALUMINUM 413.0 is normally classified as a die-casting alloy; however, it also can be used for sand and permanent-mold castings. Its high silicon content (12%) lowers its melting temperature and increases its fluidity, thus improving its castability. It is used for intricate thin-walled castings requiring pressure tightness, toughness and good resistance to corrosion. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fracture toughness and fatigue. It also includes information on high temperature performance and corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Al-231. Producer or source: Various aluminum companies.

ALUMINUM 850.0 is an aluminum-tin-nickel-copper alloy for bearings. It is used principally in the form of permanent-mold castings which, because of their rapid solidification, are characterized by a fine, dense, fatigue-resistant structure. Solid bearings machined from permanent-mold castings of this alloy are used principally in the artificially aged T5 temper for heavy-duty engine bearings. In this field Aluminum 850.0 alloy has provided satisfactory performance under conditions of very high unit loading at medium speeds and temperatures. 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, forming, heat treating, machining, joining, and surface treatment. Filing Code: Al-252. Producer or source: Various aluminum companies.

ALUMINUM 380.0 is a copper-silicon type of aluminum die-casting alloy. It has good castability and fairly good machinability; it is the most widely used aluminum die-casting alloy. It has satisfactory strength and ductility. Among the many applications of Aluminum 380.0 are internal combustion engine parts, pressure-tight castings, ornamental castings and machine frames. This datasheet provides information on composition, physical properties, elasticity, tensile properties, 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, joining, and surface treatment. Filing Code: Al-239. Producer or source: Various aluminum companies.

ALUMINUM 520.0 is an aluminum-magnesium casting alloy containing nominally 10% magnesium. It is characterized by an excellent combination of machinability, mechanical properties and resistance to corrosion. Typical applications are railroad passenger car frames and marine parts. 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-237. Producer or source: Various aluminum companies.

Inconel Alloy 725HS is a Ni-Cr-Mo-Cb alloy that is age hardenable and is a higher strength version of Inconel alloy 725 (see Alloy Digest Ni-445, January 1994). The alloy is corrosion resistant and is often used in fastener or marine fabrication applications. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear strength as well as fracture toughness. It also includes information on high temperature performance and corrosion resistance as well as heat treating and machining. Filing Code: Ni-604. Producer or source: Special Metals Corporation.

AA 355.0 is a general-purpose, high-strength casting alloy containing silicon and copper as the major alloying elements. Its casting characteristics are excellent and it is recommended for pressure-tight castings. It can be age hardened and has good resistance to corrosion. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness. It also includes information on high temperature performance and corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Al-291. Producer or source: Various aluminum companies.

MUELLER ALLOY 1820 (formerly MBCo 902) is a chromium-copper alloy with high electrical conductivity, high mechanical strength, and superior creep, fatigue and wear properties. It is used for resistance welding electrodes, switchgear, and electrical and electronic parts. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fracture toughness. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Cu-257. Producer or source: Mueller Brass Company.

Federated F050 is a 5% silicon-aluminum casting alloy recommended for intricate design and thin wall castings. It produces pressure tight castings and has a high resistance to corrosion. The F050 PT grade is specially processed during manufacture to reduce the apparent solidification shrinkage with no change in the chemical specification or mechanical properties. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fracture toughness and fatigue. It also includes information on high temperature performance and corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Al-114. Producer or source: Federated Metals Corporation, ASARCO Inc..

UNS No. A03560 is a heat-treatable aluminum casting alloy. Normally it is used only when heat-treated (aged) strengths are required. It is recommended for high-strength, pressure-tight castings, intricate shapes and where good resistance to corrosion is needed. Its many applications include crank cases, gear cases, oil pans, airframe fittings and instrument housings. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness. It also includes information on high temperature performance and corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Al-274. Producer or source: Various aluminum companies.

Aluminum Alloys 360 and A360 are die casting alloys having good strength, good corrosion resistance, and excellent castability. Alloy A360 is a purer form of Alloy 360, having lower impurity maximums. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear strength as well as fatigue. It also includes information on high temperature performance and corrosion resistance as well as heat treating, machining, and joining. Filing Code: Al-103. Producer or source: Aluminum Company of America.

ALUMINUM 122 is an aluminum sand and permanent mold casting alloy recommended for applications where good high temperature strength, high hardness, resistance to wear and good machinability are required. It responds to an age-hardening heat treatment. 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 heat treating, machining, and joining. Filing Code: Al-48. Producer or source: Aluminum Company of America.

AISI Type 204 is a chromium-nickel-manganese type stainless steel comparable in properties to Type 304 stainless steel. It is austenitic, non-magnetic, and highly corrosion resistant. 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 high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: SS-163. Producer or source: Stainless steel mills.

NUCALLOY 41 is a nickel-chromium-boron alloy developed as an alternative to cobalt-base alloys in applications where the presence of cobalt is undesirable. It is finding wide acceptance because of its toughness and high resistance to attack by many chemicals. It has superior wear resistance which is derived from the presence of hard nickel borides (and to a lesser extent chromium carbides) tightly held in a tough nickel-rich matrix. Among its many uses are cylinder liners, glass plant applications and valve components for nuclear applications. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive strength as well as fracture toughness. It also includes information on high temperature performance and corrosion resistance as well as heat treating, machining, and joining. Filing Code: Ni-236. Producer or source: Stoody Company.

AMDRY 850 is a cobalt-base alloy formulated to provide maximum resistance to combinations of abrasion, corrosion, heat and oxidation. It has superior resistance to certain corrosive media and higher hot hardness than nickel-base alloys. Produced in powder form, it allows large areas and cylindrical shaped parts to be hardfaced by spraying and fusing, which is faster and more economical than alternative methods. Sprayed deposits are usually limited to a thickness of 0.080-inch. The data pertain to the deposit after fusing. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive strength as well as fracture toughness. It also includes information on high temperature performance and corrosion resistance as well as heat treating and machining. Filing Code: Co-70. Producer or source: Alloy Metals Inc..

Republic RS-110A is a titanium alloy containing manganese as its principle alloying element. The alloy is a medium strength, highly formable sheet alloy which has been used extensively as an aircraft structural material. 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, joining, and surface treatment. Filing Code: Ti-35. Producer or source: Republic Steel Corporation, Titanium Division.