The influence of cobalt on the tensile and stress-rupture properties of the nickel-base superalloy mar-m247

1982 ◽  
Vol 13 (10) ◽  
pp. 1767-1774 ◽  
Author(s):  
M. V. Nathal ◽  
R. D. Maier ◽  
L. J. Ebert
Alloy Digest ◽  
1981 ◽  
Vol 30 (7) ◽  

Abstract AISI No. 664 is a nickel-base high-temperature alloy that can be precipitation hardened because of its contents of aluminum and titanium. Vacuum melting is used in its production to provide excellent quality and reproducability. It is used for applications requiring a good combination of creep and stress-rupture properties up to about 1500 F. Typical applications are gas-turbine components, airframes and fasteners. This datasheet provides information on composition, physical properties, 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: Ni-269. Producer or source: Nickel alloy producers.


1973 ◽  
Vol 95 (1) ◽  
pp. 10-14 ◽  
Author(s):  
R. L. Cairns ◽  
J. S. Benjamin

A dispersion strengthened nickel-base superalloy, designated IN-853, has been made by a new process called “Mechanical Alloying.” This provides a long sought combination of properties typical of dispersion strengthened and precipitation hardened materials. The alloy has flat rupture curves over a wide temperature range. Rupture stress/temperature curves for the alloy show a transition separating the low temperature regime where precipitation hardening controls the strength, and the high temperature range where dispersion strengthening predominates. The slope of a Larson-Miller plot of stress rupture test data also decreases at high values of that parameter. At high temperatures rupture stress is less sensitive to temperature changes than is the case with conventional nickel-base superalloys. At a fixed stress level the rupture life of the dispersion strengthened superalloy is more sensitive to temperature changes.


Alloy Digest ◽  
1987 ◽  
Vol 36 (2) ◽  

Abstract UNITEMP 625 is a nickel-base, austenitic, solution-strengthened high-performance alloy that provides excellent resistance to both high-temperature gaseous corrosion and aqueous corrosion coupled with good strength and stress-rupture properties to 1800 F. The alloy has good resistance to stress-corrosion cracking. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear 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, machining, and joining. Filing Code: Ni-344. Producer or source: Cyclops Corporation.


Alloy Digest ◽  
2010 ◽  
Vol 59 (4) ◽  

Abstract Electralloy ECHX is a solution-strengthened, nickel-base, high-performance alloy providing excellent resistance to high-temperature gaseous corrosion, coupled with good strength and stress rupture properties up to 1205 deg C (2200 deg F). 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: Ni-678. Producer or source: Electralloy, a Division of G.O. Carlson Inc.


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