MUELLER ALLOY No. 6741 (formerly 600 Alloy) is a high-strength bearing alloy intended for use in applications requiring a combination of outstanding wear characteristics and high bearing strength. 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: Cu-235. Producer or source: Mueller Brass Company.

INLAND HI-FORM Steels are a low-carbon, low or intermediate-manganese, low-sulfur, aluminum-killed, fine-grain, columbium and/or phosphorus-bearing series of high-strength steels providing greatly enhanced forming and bending properties. These steels are furnished in minimum yield strength levels from 40,000 to 80,000 psi. They are used widely in the transportation and mobile-equipment industries. See also Ispat Inland Cal Hi-Form 80Y100T, Alloy Digest CS-136, May 2003. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SA-346. Producer or source: Ispat Inland Inc..

Copper Alloy No. 674 is a non-heat-treatable, high-strength bearing alloy for applications requiring good bearing properties, especially in conjunction with hardened steel mating surfaces, and the ability to stand up under moderately high loads. It has outstanding resistance to wear along with high bearing strength. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fatigue. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Cu-287. Producer or source: Copper alloy producers.

COMPO H is an oil-impregnated sintered bronze, produced by powder metallurgy techniques, which is widely used in automotive, applicance, farm equipment, and aircraft industry applications. This datasheet provides information on composition, physical properties, tensile properties, and compressive strength. and bearing strength It also includes information on corrosion resistance Filing Code: Cu-246. Producer or source: Bound Brook Bearing Corporation of America.

NORAL 162 is an age-hardenable aluminum casting alloy. It has low thermal expansion, good high temperature strength and bearing (frictional) properties. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive, shear, and bearing 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-123. Producer or source: Alcan Industries Ltd.

Ti-6Al-2Sn-4Zr-2Mo is a super-alpha titanium alloy providing an excellent combination of creep strength, tensile strength, toughness and stability to 1050 F. It is recommended for airframe and gas turbine engine requirements. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive, shear, and bearing strength as well as creep. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Ti-52. Producer or source: Titanium Metals Corporation of America.

NORAL C77S is a high strength, heat treatable, wrought aluminum alloy that is recommended for highly stressed components. It responds to the precipitation hardening heat treatment, producing tensile strengths in excess of all other aluminum alloys. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive, shear, and bearing strength as well as fracture toughness and fatigue. It also includes information on as well as forming, heat treating, machining, and joining. Filing Code: Al-10. Producer or source: Northern Aluminium Company Ltd.

DOWMETAL-C is a heat-treatable magnesium-base alloy suitable for sand and permanent mold castings. It has high tensile strength and good yield strength. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive, shear, and bearing strength as well as fracture toughness and fatigue. It also includes information on corrosion resistance as well as heat treating, machining, joining, and surface treatment. Filing Code: Mg-13. Producer or source: The Dow Chemical Company.

Carpenter CP Titanium Grade 4 is the highest-strength grade of the unalloyed grades 1-4. It competes with steels and nickel alloys with its combination of corrosion resistance, fatigue properties, and high strength. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive, shear, and bearing strength as well as fatigue. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: TI-128. Producer or source: Carpenter Technology Corporation.

MONEL Alloy K-500 combines the excellent corrosion resistance characteristics of the MONEL nickel-copper alloys with the added advantages of greaterr strength and hardness. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties and bearing strength 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: Ni-119. Producer or source: Huntington Alloy Products Division.

CRUCIBLE A-70 is a grade of commercially pure titanium that is used where higher strength is required than is achieved with grade A-55. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive, shear, and bearing strength as well as fracture toughness, creep, and fatigue. 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: Ti-63. Producer or source: Crucible Specialty Metals Division, Colt Industries.

NORAL 19S is an age-hardenable, wrought aluminum alloy that retains its strength well at elevated temperatures. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive, shear, and bearing strength as well as fracture toughness and fatigue. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Al-119. Producer or source: Alcan Industries Ltd.

Magnesium AZ80A is a heat treatable, magnesium alloy recommended for forgings and extrusions requiring high fatigue strength and good creep resistance. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive, shear, and bearing strength as well as fatigue. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, joining, and surface treatment. Filing Code: Mg-55. Producer or source: The Dow Metal Products Company.

Ti-5Al-2.5Sn is a medium strength all alpha titanium alloy, designed primarily for use in sheet and strip form. It possesses excellent resistance to oxidation up to 1200 F and excellent creep resistance to 800 F. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive, shear, and bearing strength 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: Ti-43. Producer or source: Titanium Metals Corporation of America.

Aluminum 7039 is a wrought, heat treatable alloy having good weldability and good corrosion resistance combined with high strength. It is recommended for cryogenic applications. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive, shear, and bearing strength as well as fracture toughness and fatigue. It also includes information on low temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-154. Producer or source: Kaiser Aluminum & Chemical Corporation.

REM-CRU A-70 is the grade of unalloyed titanium used where higher strength is required. It is specified for many moderately stressed aircraft parts. (Formerly known as RC-70.) This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive, shear, and bearing strength 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: Ti-16. Producer or source: Rem-Cru Titanium Inc..

MELTRON ZW6 is a heat treatable wrought magnesium alloy containing zinc and zirconium. It is recommended for extrusions where high strength and good toughness are required. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive, shear, and bearing strength as well as fracture toughness and fatigue. It also includes information on corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Mg-37. Producer or source: Magnesium Elektron Inc..

Magnesium HK31 is a magnesium-base alloy possessing extraordinary resistance to creep and maintaining excellent strength through the temperature range of 300-700 F. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive, shear, and bearing strength as well as creep and fatigue. It also includes information on low and high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Mg-39. Producer or source: Brooks & Perkins Inc..

NORAL 62S is an aluminum extrusion alloy that responds to an age hardening heat treatment. It has good strength and excellent fabricating characteristics. This datasheet provides information on composition, physical properties, hardness, tensile properties, and compressive, shear, and bearing strength as well as fracture toughness and fatigue. It also includes information on as well as forming, heat treating, machining, and joining. Filing Code: Al-77. Producer or source: Northern Aluminium Company Ltd.

MAGNESIUM AZ61A is a magnesium extrusion alloy having a strength level between that of AZ31B and ZK60A. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive, shear, and bearing strength as well as fatigue. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Mg-43. Producer or source: The Dow Chemical Company.