Improved high cycle fatigue damage tolerance of turbine-engine compressor components by low plasticity burnishing

Journal of Engineering for Gas Turbines and Power

Volumn 130, Issue 1, 2008, Pages

  Prevéy, Paul S ^a   Jayaraman, N ^a   Ravindranath, Ravi A ^b   Shepard, Michael ^c  

^a Lambda Technologies   (United States)

^b NAVAL AIR SYSTEMS COMMAND   (United States)

^c AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

Compressor components; Damage tolerance; Fatigue cracking; Fatigue design diagram; FDD; FOD; Foreign object damage; High cycle fatigue; Low plasticity burnishing; Mitigation of damage; Residual stress; Surface treatment

Indexed keywords

BURNISHING; CONTROL SYSTEMS; DAMAGE TOLERANCE; FATIGUE DAMAGE; MACHINE DESIGN; MONITORING; QUALITY CONTROL; RESIDUAL STRESSES; STRESS CONCENTRATION; TURBINES;

COMPRESSOR COMPONENT; COMPUTER NUMERICAL CONTROL; LOW PLASTICITY BURNISHING; REAL-TIME PROCESS MONITORING;

COMPRESSORS;

BURNISHING; COMPRESSORS; CONTROL SYSTEMS; DAMAGE TOLERANCE; FATIGUE DAMAGE; MACHINE DESIGN; MONITORING; QUALITY CONTROL; RESIDUAL STRESSES; STRESS CONCENTRATION; TURBINES;

EID: 42149112782     PISSN: 07424795     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.2771244     Document Type: Article

References (17)

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