REFRACTALOY 70

Alloy Digest ◽  
1961 ◽  
Vol 10 (8) ◽  

Abstract REFRACTALOY 70 is a super heat and oxidation resistant alloy containing high percentages of nickel, chromium, cobalt and molybdenum. It has an exceedingly low creep rate at elevated temperatures and shows marked high temperature stability. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as creep. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Co-2. Producer or source: Westinghouse Electric Corporation. Originally published July 1953, revised August 1961.

Alloy Digest ◽  
1955 ◽  
Vol 4 (8) ◽  

Abstract REFRACTALOY 80 is a super heat and oxidation resistant alloy containing high percentages of cobalt, chromium nickel and molybdenum. It has an exceedingly low creep rate at elevated temperatures and shows marked high temperature stability. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Co-7. Producer or source: Westinghouse Electric Corporation.


Alloy Digest ◽  
1955 ◽  
Vol 4 (7) ◽  

Abstract CUPALOY is an age hardenable, high conductivity copper alloy with higher mechanical properties than copper, especially at elevated temperatures. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as deformation, and fatigue. It also includes information on high temperature performance, corrosion and wear resistance as well as forming, heat treating, and machining. Filing Code: Cu-28. Producer or source: Westinghouse Electric Corporation.


Alloy Digest ◽  
1954 ◽  
Vol 3 (2) ◽  

Abstract REFRACTALOY 26 is a high heat resistant alloy of nickel, chromium, cobalt and iron, possessing high creep and endurance strengths along with high ductility at elevated temperatures. It responds to precipitation-hardening heat treatment. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as creep and fatigue. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Ni-8. Producer or source: Westinghouse Electric Corporation.


Alloy Digest ◽  
1974 ◽  
Vol 23 (11) ◽  

Abstract HASTELLOY Alloy C-4 is a nickel-chromium-molybdenum alloy with outstanding high-temperature stability as shown by high ductility and corrosion resistance even after long-time aging in the range 1200-1900 F. Alloy C-4 also has excellent resistance to stress-corrosion cracking and to oxidizing atmospheres up to 1900 F. 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: Ni-211. Producer or source: Stellite Division, Cabot Corporation.


Alloy Digest ◽  
1989 ◽  
Vol 38 (1) ◽  

Abstract UNS NO6455 is a nickel-chromium-molybdenum alloy with outstanding high-temperature stability as shown by high ductility and corrosion resistance even after long-time aging in the range 1200-1900 F. The alloy also has excellent resistance to stress-corrosion cracking and to oxidizing atmospheres up to 1900 F. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-367. Producer or source: Nickel and nickel alloy producers.


Alloy Digest ◽  
1965 ◽  
Vol 14 (7) ◽  

Abstract TD-NICKEL is a dispersion hardened nickel alloy offering high-temperature stability and useful mechanical properties virtually to the melting point of the base metal. It is easy to fabricate. It is capable of operating for long periods of time at high temperatures without degradation of mechanical properties. This datasheet provides information on composition, physical properties, 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, and joining. Filing Code: Ni-103. Producer or source: E. I. DuPont de Nemours & Company Inc..


Alloy Digest ◽  
2006 ◽  
Vol 55 (6) ◽  

Abstract HPM X-750 is a precipitation-hardenable nickel-chromium alloy that is well suited for a wide range of corrosive and oxidizing environments where strength must be maintained to elevated temperatures. The alloy composition provides a product that performs well at elevated temperatures up to 700 deg C (1300 deg F). The strength can be increased by heat treatment. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on high temperature performance as well as forming, heat treating, and joining. Filing Code: Ni-638. Producer or source: Hamilton Precision Metals.


Alloy Digest ◽  
1962 ◽  
Vol 11 (8) ◽  

Abstract Westinghouse Alloy B33 is a columbium-base alloy for high temperature applications requiring moderate strength where excellent fabricability, weldability, and resistance to liquid metal corrosion are prime requisites. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and bend strength. 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: Cb-1. Producer or source: Westinghouse Electric Corporation.


Alloy Digest ◽  
1967 ◽  
Vol 16 (2) ◽  

Abstract HARVEY HA8116 is an alpha titanium-base alloy having outstanding creep resistance and high temperature stability. It is non-heat treatable. This datasheet provides information on composition, physical properties, and tensile properties as well as creep. It also includes information on high temperature performance as well as forming, heat treating, and machining. Filing Code: Ti-50. Producer or source: Harvey Aluminum Company.


Alloy Digest ◽  
2007 ◽  
Vol 56 (6) ◽  

Abstract Timetal 6-2-4-2 has a combination of tensile strength, creep strength, toughness, and high-temperature stability for long-term application at temperatures up to 538 deg C (1000 deg F). This datasheet provides information on composition, physical properties, microstructure, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance as well as forming, heat treating, and joining. Filing Code: TI-140. Producer or source: Timet.


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