Nickel and cobalt-base superalloy blades and vanes in the hot sections of all gas turbines are coated to enhance resistance to hot corrosion. Pack cementation aluminizing, invented in 1911, is the most widely used coating process. Corrosion resistance of aluminide coatings can be increased by modification with chromium, platinum, or silicon. Chromium diffusion coatings can be used at lower temperatures. Formation and degradation mechanisms are reasonably well understood and large-scale manufacturing processes for these coatings are gradually being automated. Pack cementation and related diffusion coatings serve well for most aircraft engine applications. The trend for industrial and marine engines is more toward the use of overlay coatings because of the greater ease of designing these to meet a wide variety of corrosion conditions.
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January 1988
Research Papers
Pack Cementation Coatings for Superalloys: A Review of History, Theory, and Practice
G. W. Goward,
G. W. Goward
Turbine Components Corporation, Branford, CT 06405
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L. W. Cannon
L. W. Cannon
Turbine Components Corporation, Branford, CT 06405
Search for other works by this author on:
G. W. Goward
Turbine Components Corporation, Branford, CT 06405
L. W. Cannon
Turbine Components Corporation, Branford, CT 06405
J. Eng. Gas Turbines Power. Jan 1988, 110(1): 150-154 (5 pages)
Published Online: January 1, 1988
Article history
Received:
February 4, 1987
Online:
October 15, 2009
Citation
Goward, G. W., and Cannon, L. W. (January 1, 1988). "Pack Cementation Coatings for Superalloys: A Review of History, Theory, and Practice." ASME. J. Eng. Gas Turbines Power. January 1988; 110(1): 150–154. https://doi.org/10.1115/1.3240078
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