Hot Corrosion of Coated Superalloys in a Gas Turbine Environment.
Progress rept. no. 4, 1 Apr-1 Sep 69,
SOLAR TURBINES INTERNATIONAL SAN DIEGO CA
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Final results on Phase I Hot Corrosion Rig Testing and Analysis of 39 coating-alloy combinations are presented. Alloys included are B1900, 713C, IN-100, Rene 41, SEL-15, U-700, WI-52 and X-40. Rig tests were performed for up to 150 hours at 1650F and 1800F on nickel-base alloys and 1800F and 2000F on cobalt-base alloys in a high-velocity environment obtained from the combustion of JP-5 fuel and air and ingestion of 35 parts sea salt per 1,000,000 parts air. Author
- Coatings, Colorants and Finishes
- Properties of Metals and Alloys
- Jet and Gas Turbine Engines