A study of the wear damage on gas turbine blades

In the present work, a study and description of the wear damage of the first-stage compressor blades of a gas turbine were conducted. The type of the equipment was a gas turbine Centaur 40 GT and the deterioration of the blades was after around 8000h of service. This equipment is located in the City...

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Bibliographische Detailangaben

Veröffentlicht in:	Engineering failure analysis 2016-03, Vol.61, p.88-99
Hauptverfasser:	Laguna-Camacho, J.R., Villagrán-Villegas, L.Y., Martínez-García, H., Juárez-Morales, G., Cruz-Orduña, M.I., Vite-Torres, M., Ríos-Velasco, L., Hernández-Romero, I.
Format:	Artikel
Sprache:	eng
Schlagworte:	Blades Damage Fatigue erosion Gas turbine blades Gas turbines Hot corrosion Pitting (corrosion) Pitting (wear) Scanning electron microscopy Turbine blades Wear Wear damage
Online-Zugang:	Volltext
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