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Corrosion and corrosion prevention in gas turbines
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Kolkman, H. J. Mom, A. J. A. |
| Copyright Year | 1985 |
| Description | The conditions governing the corrosion behavior in gas turbines are surveyed. Factors such as temperature, relative humidity, the presence of sulfur and nitrogen dioxide, and fuel quality are discussed. Electromechanical corrosion at relatively low temperature in compressors; oxidation; and hot corrosion (sulfidation) at high temperature in turbines are considered. Corrosion prevention by washing and rinsing, fueld additives, and corrosion resistant materials and coatings are reviewed. |
| File Size | 1678911 |
| Page Count | 43 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19860012073 |
| Archival Resource Key | ark:/13960/t9d55hq07 |
| Language | English |
| Publisher Date | 1985-11-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Sprayed Coatings Sulfur Compounds Service Life Electrochemical Corrosion Nickel Coatings Hot Corrosion Jet Engines Fuel Corrosion Corrosion Prevention Gas Turbines Compressor Blades Ceramic Coatings Corrosion Tests Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |