Failure analysis of a set of compressor blades

Engineering Failure Analysis

Volumn 15, Issue 6, 2008, Pages 666-674

  Silveira, E ^a   Atxaga, G ^a   Irisarri, A M ^a  

^a TECNALIA RESEARCH AND INNOVATION   (Spain)

Author keywords

Compressor blades; Foreign object damage; Nickel base alloys

Indexed keywords

AIRCRAFT ENGINES; COMPRESSORS; ENERGY DISPERSIVE SPECTROSCOPY; FAILURE ANALYSIS; FRACTOGRAPHY; FRACTURE; NICKEL ALLOYS; OPTICAL MICROSCOPY; SCANNING ELECTRON MICROSCOPY;

COMPRESSOR BLADES; FOREIGN OBJECT DAMAGE;

TURBOMACHINE BLADES;

AIRCRAFT ENGINES; COMPRESSORS; ENERGY DISPERSIVE SPECTROSCOPY; FAILURE ANALYSIS; FRACTOGRAPHY; FRACTURE; NICKEL ALLOYS; OPTICAL MICROSCOPY; SCANNING ELECTRON MICROSCOPY; TURBOMACHINE BLADES;

EID: 40949163117     PISSN: 13506307     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.engfailanal.2007.10.002     Document Type: Article

References (5)

1. Nowell D., Dini D., and Duó P. Stress analysis of V notches with and without cracks, with application to foreign object damage. J Strain Anal Eng Des 38 5 (2003) 429-441
2. Suresh S. Fatigue of materials. 2nd ed. (1998), Cambridge University Press p. 237
3. http://www.boeing.com.
4. Federal Aviation Administration Part 139. Sec. 139.305; 2004.
5. Nowell D., Duo P., and Stewart I.F. Prediction of fatigue performance in gas turbine blades after foreign object damage. Int J Fatigue 25 9-11 (2003) 963-969