Details
| Originalsprache | Englisch |
|---|---|
| Titel des Sammelwerks | Proceedings / 11th International Conference THE "A" Coatings in Manufacturing Engineering |
| Erscheinungsort | Thessaloniki |
| Seiten | 179-184 |
| Seitenumfang | 6 |
| Publikationsstatus | Veröffentlicht - 2014 |
| Veranstaltung | 11th International Conference THE "A" Coatings in Manufacturing Engineering - Thessaloniki, Thessaloniki, Griechenland Dauer: 1 Okt. 2014 → 3 Okt. 2014 |
Abstract
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Proceedings / 11th International Conference THE "A" Coatings in Manufacturing Engineering. Thessaloniki, 2014. S. 179-184.
Publikation: Beitrag in Buch/Bericht/Sammelwerk/Konferenzband › Aufsatz in Konferenzband › Forschung
}
TY - GEN
T1 - Common application of Ni-based fillermetals and hotgascorrosion protection coatings by means of thermal spraying with subsequent heat treatment for near net shape turbineblade repairing
AU - Nicolaus, Martin
AU - Möhwald, Kai
AU - Maier, Hans Jürgen
PY - 2014
Y1 - 2014
N2 - In this research proposal, a hybrid technology is developed to near-net shape repair turbine blades. On the one hand, the hybrid technology takes into account process technology and manufacturing aspects and, on the other hand, incorporates material-technological mechanisms into this hybrid technology. In this way, the process chain for regenerating turbine blades can be shortened. The turbine blades considered here are components of high-pressure turbines and therefore this study focuses on nickel-based alloys. On the one hand, the nickel-based filler-metal required for repairing the turbine blades is applied together with the hot-gas corrosion protective layer by means of the APS and HVOF thermal spraying processes and secondly, these coating systems were subjected to a heat treatment.
AB - In this research proposal, a hybrid technology is developed to near-net shape repair turbine blades. On the one hand, the hybrid technology takes into account process technology and manufacturing aspects and, on the other hand, incorporates material-technological mechanisms into this hybrid technology. In this way, the process chain for regenerating turbine blades can be shortened. The turbine blades considered here are components of high-pressure turbines and therefore this study focuses on nickel-based alloys. On the one hand, the nickel-based filler-metal required for repairing the turbine blades is applied together with the hot-gas corrosion protective layer by means of the APS and HVOF thermal spraying processes and secondly, these coating systems were subjected to a heat treatment.
M3 - Conference contribution
SN - 978-960-98780-8-1
SP - 179
EP - 184
BT - Proceedings / 11th International Conference THE "A" Coatings in Manufacturing Engineering
CY - Thessaloniki
T2 - 11th International Conference THE "A" Coatings in Manufacturing Engineering
Y2 - 1 October 2014 through 3 October 2014
ER -