A Survey of High-Temperature, Gas, Atmosphere Corrosion of Iron-Nickel-Chromium Alloys—Part II

CORROSION ◽  
1947 ◽  
Vol 3 (8) ◽  
pp. 383-405 ◽  
Author(s):  
James T. Gow
Keyword(s):  
High Temperature ◽  
Nickel Chromium ◽  
Chromium Alloys ◽  
Gas Atmosphere ◽  
Iron Nickel ◽  
Corrosion Of Iron ◽  
High Temperature Gas

Paper 7: Advanced Nickel-Chromium Base Alloys

1965 ◽  
Vol 180 (4) ◽  
pp. 160-171
Author(s):  
C. H. White ◽  
J. Heslop
Keyword(s):  
High Temperature ◽  
Binary System ◽  
Gas Turbine ◽  
Elevated Temperatures ◽  
High Strength ◽  
Gas Turbine Engine ◽  
Turbine Engine ◽  
Nickel Chromium ◽  
Chromium Alloys ◽  
Resistance To Oxidation

Nickel-chromium alloys have been in use since early in this century for high temperature applications because of their resistance to oxidation. Since the advent of the gas-turbine engine, more complex alloys capable of maintaining high strength at elevated temperatures have been developed from the simple binary system. These complex alloys were initially mainly strengthened by the precipitation of the Ni3(Ti, Al) phase but more recent alloys have been further strengthened by additions of cobalt, tungsten, molybdenum, niobium, and tantalum. The properties and applications of these alloys are discussed.

The mechanism of high temperature sulphur corrosion of nickel-chromium alloys

1966 ◽  
Vol 6 (2) ◽  
pp. 47-68 ◽  
Author(s):  
S. Mrowec ◽  
T. Werber ◽  
M. Zastawnik
Keyword(s):  
High Temperature ◽  
Nickel Chromium ◽  
Chromium Alloys

High Temperature Phosphidation of Nickel‐Chromium Alloys in Phosphorus Vapor

1979 ◽  
Vol 126 (11) ◽  
pp. 1948-1951 ◽  
Author(s):  
Yoshinori Sasaki ◽  
Yukio Iida ◽  
Shiro Ueda
Keyword(s):  
High Temperature ◽  
Nickel Chromium ◽  
Chromium Alloys
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