CRUCIBLE A-40

Alloy Digest ◽  
1959 ◽  
Vol 8 (7) ◽  

Abstract CRUCIBLE A-40 is a special grade of unalloyed titanium for applications requiring maximum ductility and formability. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive and shear strength as well as fracture toughness. 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-20. Producer or source: Crucible Steel Company of America, Titanium Division.

Alloy Digest ◽  
1954 ◽  
Vol 3 (1) ◽  

Abstract Ti-150A is a titanium-base alloy containing iron and chromium. It is used primarily in bars and forgings. It is heat treatable and work-hardenable. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fracture toughness. 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-2. Producer or source: Titanium Metals Corporation of America.


Alloy Digest ◽  
1957 ◽  
Vol 6 (7) ◽  

Abstract REM-CRU A-55 is the general purpose grade of unalloyed titanium for moderate to severe forming. (Formerly known as RC-55). This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive and shear 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-13. Producer or source: Rem-Cru Titanium Inc..


Alloy Digest ◽  
1984 ◽  
Vol 33 (6) ◽  

Abstract EASTERN STAINLESS TYPE 348 is a stabilized type of stainless steel free from the chromium carbide precipitates that cause intergranular corrosion. It is recommended for welded components that cannot be annealed after welding. It also is used for parts that are heated and cooled intermittently to temperatures between 800 and 1600 F. Type 348 is stabilized by an addition of columbium. Tantalum is restricted to 0.10% maximum and cobalt is restricted to 0.20% maximum. Because of these restrictions, Type 348 is recommended for use in applications such as those encountered in radioactive service. 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 forming, heat treating, machining, joining, and surface treatment. Filing Code: SS-447. Producer or source: Eastern Stainless Steel Company.


Alloy Digest ◽  
1958 ◽  
Vol 7 (1) ◽  

Abstract REM-CRU C-135AMo is a titanium-base alloy having good time-temperature-stress stability and deep hardenability. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear strength as well as fracture toughness, creep, and 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: Ti-14. Producer or source: Rem-Cru Titanium Inc..


Alloy Digest ◽  
1971 ◽  
Vol 20 (12) ◽  

Abstract UNITEMP N-155 is an iron-base austenitic alloy used over a wide temperature range from subzero to about 1800 or 1900 F. It has relatively good oxidation and corrosion resistance. It is used in such applications as turbine rotors, shafts and blades, afterburner parts, nozzles and combustion chambers. 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 as well as forming, heat treating, joining, and surface treatment. Filing Code: Fe-48. Producer or source: Cyclops Corporation.


Alloy Digest ◽  
1963 ◽  
Vol 12 (6) ◽  

Abstract DURANICKEL Alloy 301 is a wrought, age-hardenable nickel alloy having high strength, high corrosion and heat resistance. It is recommended for springs, diaphrams, bearings, pump and valve parts. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and 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: Ni-83. Producer or source: The International Nickel Company Inc..


Alloy Digest ◽  
1972 ◽  
Vol 21 (3) ◽  

Abstract COPPER ALLOY No. 230 is a single-phase brass containing 15% zinc which is the most widely used of the low zinc brasses. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear 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, and joining. Filing Code: Cu-252. Producer or source: Brass mills.


Alloy Digest ◽  
1969 ◽  
Vol 18 (2) ◽  

Abstract BRUSII Alloy 200C is a beryllium-nickel casting alloy having high resistance to wear, corrosion, thermal shock and oxidation. It is recommended for fuel pump impellers, turbines, non-sparking tools, molds for plastics and glass. 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, joining, and surface treatment. Filing Code: Ni-142. Producer or source: Brush Beryllium Company.


Alloy Digest ◽  
1968 ◽  
Vol 17 (9) ◽  

Abstract Brush Alloy 260-C is a beryllium nickel casting alloy having high strength, hardness and good corrosion resistance. It is recommended for fuel pump impellers, turbines, non-sparking tools, molds for plastics and glass. 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, joining, and surface treatment. Filing Code: Ni-138. Producer or source: Brush Beryllium Company.


Alloy Digest ◽  
1983 ◽  
Vol 32 (11) ◽  

Abstract ALUMINUM 852.0 contains higher concentrations of copper and nickel than either Aluminum 850.0 or Aluminum 851.0 alloy. The higher copper and nickel percentages and an addition of magnesium give Aluminum 852.0 higher strength and make it suitable for bearing applications requiring improved resistance to higher operating stresses (loads). Aluminum 852.0 is used for the production of castings by the sand and permanent-mold processes. It is normally supplied and used in the T5 temper. 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-248. Producer or source: Various aluminum companies.


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