Processing tip treatment bars in a gas turbine engine
This invention relates to the processing of tip treatment bars of a rotor casing for a gas turbine engine. Tip treatment bars of a rotor casing for a gas turbine engine are subjected to a process which induces compressive stress within the bars The process may be a laser shock peening process applie...
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Patent |
| Sprache: | eng |
| Online-Zugang: | Volltext bestellen |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| Zusammenfassung: | This invention relates to the processing of tip treatment bars of a rotor casing for a gas turbine engine.
Tip treatment bars of a rotor casing for a gas turbine engine are subjected to a process which induces compressive stress within the bars The process may be a laser shock peening process applied to opposite sides of each bar The processing of the tip treatment bars renders them less susceptible to fatigue failure. |
|---|