Evaluation of standard life assessment procedures and life extension methodologies for fracture-critical components

International Journal of Fatigue

Volumn 23, Issue , 2001, Pages 11-19

  Boyd Lee, A D ^a   Harrison, G F ^a   Henderson, M B ^a  

^a DEFENCE SCIENCE AND TECHNOLOGY LABORATORY   (United Kingdom)

Author keywords

Inspection; Lifing methodologies; Risk assessment

Indexed keywords

CRACKS; FITS AND TOLERANCES; RISK ASSESSMENT; SERVICE LIFE; STRESS ANALYSIS;

AEROENGINES; CRACK DETECTIONS;

AIRCRAFT ENGINES;

EID: 0035210820     PISSN: 01421123     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0142-1123(01)00116-5     Document Type: Article

References (18)

1. Microstructure and alloy developments in Ni-based superalloys
2. Fatigue crack propagation in Ni-base superalloys - Effects of microstructure, load ratio and temperature
3. Fatigue crack growth resistant microstructures in polycrystalline Ni-base superalloys for aeroengines
4. Effects of environment and complex loading history on fatigue life
5. A statistical distribution function of wide applicability
6. Boostrap analysis of FCGR, application to the Paris relationship and to lifetime prediction
7. Short fatigue crack path determinants in polycrystalline Ni-base superalloys
8. The development of life extension methods for fracture-critical aero-engine components
9. Crack initiation and the short-to-long crack growth transition in a Ni-base superalloy
10. Lifing and life extension of fracture-critical aeroengine components