Abstract
The life span of gas turbine coatings may be restricted by type II hot corrosion when exposed at elevated temperatures in aggressive environments during service. Herein, the temperature dependence of corrosion morphologies and kinetics of NiAl coating on a second-generation single crystalline Ni-based superalloy is studied to provide an insight into the possible corrosion mechanisms. A series of tests are performed at 600–800 °C in air-300 ppm SO2 atmosphere with Na2SO4–20% K2SO4 salt mixture as deposit. Severe attack is observed at both 700 and 750 °C after 24 h exposure, whereas at 600 and 800 °C, only a minor attack is found. The results indicate that the corrosion rate is strongly governed by Na2SO4–NiSO4 liquid formation, and temperature affects the attack rate of the outer coating (mainly β-NiAl phase) primarily by changing the required minimum SO3 partial pressure to stabilize this liquid. The influence of temperature and (Formula presented.) on phase equilibrium of the salt and oxide mixture is calculated with an in-house developed thermodynamic database. The predicted minimum (Formula presented.) for liquid formation calculated with the database is consistent with the experimental results.
Original language | English |
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Article number | 1901244 |
Journal | Advanced Engineering Materials |
Volume | 22 |
Issue number | 6 |
DOIs | |
State | Published - Jun 1 2020 |
Externally published | Yes |
Funding
Mr. H. Cosler is kindly acknowledged for performing the hot corrosion tests. The authors are grateful to Dr. E. Wessel and Dr. D. Gr?ner for the SEM analysis. The authors are grateful to China Scholarship Council (no. 201708440229) for the financial support of this work. This work has also been supported by the German Federal Ministry of Economics under grant nos. 20T1522A and 0327773K and MTU Aero Engines AG. Mr. H. Cosler is kindly acknowledged for performing the hot corrosion tests. The authors are grateful to Dr. E. Wessel and Dr. D. Grüner for the SEM analysis. The authors are grateful to China Scholarship Council (no. 201708440229) for the financial support of this work. This work has also been supported by the German Federal Ministry of Economics under grant nos. 20T1522A and 0327773K and MTU Aero Engines AG.
Funders | Funder number |
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German Federal Ministry of Economics | 0327773K, 20T1522A |
Methodist Theological University | |
Bundesministerium für Wirtschaft und Technologie | |
China Scholarship Council | 201708440229 |
Keywords
- NaSO–KSO deposits
- aluminide coatings
- temperature dependence
- type II hot corrosion