LEAD BABBIT

Alloy Digest ◽  
1973 ◽  
Vol 22 (7) ◽  

Abstract Lead Babbit comprises a family of alloys used to cut down on friction in moving parts of machines. Alloys 7, 8 and 13 are essentially lead-antimony-tin alloys. Alloy 15 is an arsenical (about 1% arsenic) lead-base alloy. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive strength as well as fatigue. It also includes information on high temperature performance and corrosion resistance as well as casting, forming, heat treating, and machining. Filing Code: Pb-10. Producer or source: White metal bearing alloy producers.

Alloy Digest ◽  
1973 ◽  
Vol 22 (4) ◽  

Abstract Tin Babbit comprises a family of essentially tin-antimony-copper alloys used to minimize friction in moving parts of machines. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive 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, and machining. Filing Code: Sn-3. Producer or source: White metal bearing alloy producers.


Alloy Digest ◽  
1956 ◽  
Vol 5 (9) ◽  

Abstract SILVER-MAGNESIUM-NICKEL is a hardenable silver-base alloy that offers a unique combination of properties for electrical and electronic use. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive strength as well as fracture toughness and creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, and joining. Filing Code: Ag-2. Producer or source: Handy & Harman.


Alloy Digest ◽  
1952 ◽  
Vol 1 (2) ◽  

Abstract Flylite ZRE-1 is a creep resistant magnesium-base alloy primarily designed for jet engine components and other high temperature applications. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive strength as well as creep. It also includes information on high temperature performance as well as casting, heat treating, machining, and joining. Filing Code: Mg-2. Producer or source: Howard Foundry Company.


Alloy Digest ◽  
1971 ◽  
Vol 20 (6) ◽  

Abstract 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.


Alloy Digest ◽  
1972 ◽  
Vol 21 (7) ◽  

Abstract UDIMET 105 is a nickel-base alloy which was developed for service at elevated temperatures. 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-175. Producer or source: Special Metals Corporation.


Alloy Digest ◽  
1977 ◽  
Vol 26 (4) ◽  

Abstract STOODY 4 is a cobalt-chromium-tungsten alloy with excellent high-temperature strength and excellent resistance to corrosion. This alloy derives its high-temperature strength from the high tungsten-to-carbon ratio which allows a large percentage of tungsten to remain in solid solution. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive strength. It also includes information on high temperature performance and corrosion resistance as well as heat treating, machining, and joining. Filing Code: Co-75. Producer or source: WRAP Division, Stoody Company.


Alloy Digest ◽  
1976 ◽  
Vol 25 (10) ◽  

Abstract WALLEX No. 40 is a self-fluxing, cobalt-base hard-surfacing alloy with excellent resistance to a combination of corrosion and abrasion and relatively good impact properties. It has excellent red hardness and weldability. It is supplied only as atomized powder for application with Wall Colmonoy's SPRAYWELD and FUSEWELD processes. This datasheet provides information on composition, physical properties, hardness, elasticity, and compressive strength as well as fracture toughness. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, and powder metal forms. Filing Code: Co-74. Producer or source: Wall Colmonoy Corporation.


Alloy Digest ◽  
1959 ◽  
Vol 8 (11) ◽  

Abstract BIRMABRIGHT B.B.5 is a corrosion resistant, medium-strength magnesium-aluminum alloy in both the cast and wrought conditions. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive strength as well as fatigue. It also includes information on high temperature performance and corrosion resistance as well as casting, forming, heat treating, machining, and joining. Filing Code: Al-85. Producer or source: Birmabright Ltd.


Alloy Digest ◽  
1957 ◽  
Vol 6 (6) ◽  

Abstract JESSOP G.39 is an austenitic nickel-base alloy having low coefficient of expansion and good thermal shock resistance. 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 heat treating and machining. Filing Code: Ni-35. Producer or source: Wm. Jessop & Sons Ltd.


Alloy Digest ◽  
1974 ◽  
Vol 23 (1) ◽  

Abstract AMDRY 754 is a nickel-base alloy formulated to provide good resistance to combinations of abrasion, corrosion, heat, impact shock and oxidation. It is deposited by spraying on the desired surface at a thickness usually limited to a maximum of 0.080 inch. Properties are on the deposit. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive strength. It also includes information on high temperature performance and corrosion resistance as well as heat treating, machining, and powder metal forms. Filing Code: Ni-199. Producer or source: Alloy Metals Inc..


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