$Thermomechanical fatigue life prediction in gas turbine superalloys - A fracture mechanics approach$

Thermomechanical fatigue life prediction in gas turbine superalloys - A fracture mechanics approach

A model that was developed to predict thermomechanical fatigue crack initiation and estimate mode I crack growth of gas turbine hot section gas path superalloys is described. Coating thickness, single crystal anisotropy, cycle waveshape, dwell and thermal exposure are among the thermomechanical fati...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Veröffentlicht in:	AIAA journal 1995-06, Vol.33 (6), p.1114-1120
1. Verfasser:	Nissley, David M
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Applied sciences Continuous cycle engines: steam and gas turbines, jet engines Engines and turbines Exact sciences and technology Gases Mechanical engineering Mechanical engineering. Machine design Thermodynamics Turbines
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A model that was developed to predict thermomechanical fatigue crack initiation and estimate mode I crack growth of gas turbine hot section gas path superalloys is described. Coating thickness, single crystal anisotropy, cycle waveshape, dwell and thermal exposure are among the thermomechanical fatigue cracking effects captured by the model.
ISSN:	0001-1452 1533-385X
DOI:	10.2514/3.12804