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Turbine Component Restoration by Diffusion Brazing Alloy Metals, Incorporated, Troy, MI

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Henmanek, Frank J., author.
Conference Name:
Annual Aerospace/Airline Plating and Metal Finishing Forum and Exposition (1984-03-26 : Miami Beach, Florida, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1984
Summary:
Operating components found in today's high performance aircraft and industrial gas turbines are subject to the most demanding conditions and hostile operating environments imaginable. As such, sophisticated part designs and advanced materials are being utilized to overcome the stringent demands encountered in these engines. Most distressed parts include blades, vanes, shrouds, frames, combustors, et cetera These are generally constructed of high strength, heat resistant nickel or cobalt base alloys. Their costs are high, often in the tens of thousands of dollars. When damage occurs, usually thermal fatigue cracking, the part is no longer serviceable and must be repaired or worse - retired and replaced. Weld repair, though satisfactory, has inherent problems. This paper discusses activated diffusion brazing as a viable repair procedure for crack healing
Notes:
Vendor supplied data
Publisher Number:
840820
Access Restriction:
Restricted for use by site license

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