Abstract: A diffusion barrier to help protect titanium aluminide alloys, including the coated alloys of the TiAl.gamma.+Ti.sub.3 Al (.alpha..sub.2) class, from oxidative attack and interstitial embrittlement at temperatures up to at least 1000.degree. C. is disclosed. The coating may comprise FeCrAlX alloys. The diffusion barrier comprises titanium, aluminum, and iron in the following approximate atomic percent:Ti-(50-55)Al-(9-20)Fe.This alloy is also suitable as an oxidative or structural coating for such substrates.
Type:
Grant
Filed:
October 21, 1996
Date of Patent:
July 7, 1998
Assignee:
The United States of America Government as represented by the Administrator of the National Aeronautics and Space Administration
Inventors:
Michael P. Brady, James L. Smialek, William J. Brindley