Application of low plasticity burnishing to improve damage tolerance of a ti-6AL-4V first stage fan blade

44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

Volumn , Issue , 2003, Pages

  Prevéy, Paul S ^a   Hornbach, Douglas ^a   Ravindranath, Ravi ^b   Cammett, J T ^c  

^a Lambda Technologies   (United States)

^b NAVAL AIR SYSTEMS COMMAND   (United States)

^c US Naval Aviation Depot   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPRESSIVE ZONE; ENDURANCE LIMIT; FATIGUE LIFE MODEL; FATIGUE STRENGTH; FOREIGN OBJECT DAMAGE(FOD); LOW PLASTICITY BURNISHING; SIZE AND SHAPE; THROUGH-THICKNESS COMPRESSIONS;

BURNISHING; DAMAGE TOLERANCE; PLASTICITY; STRESS CONCENTRATION; STRUCTURAL DYNAMICS; TITANIUM ALLOYS; X RAY DIFFRACTION;

FATIGUE OF MATERIALS;

EID: 84896835451     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)

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9. th Nat. Turbine Engine HCF Conference.
10. th National Turbine Engine HCF Conf., 2000.
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12. "Longer Life with Low Plasticity Burnishing, " Manufacturing Engineering, SME, ed. B. Hogan, Dec., 2001.
13. J. Fitzgerald and R. Wei, "A Test Procedure for Determining the Influence of Stress Ration on Fatigue Crack Growth, " Journal of Testing and Evaluation, v. 2, No. 2, ASTM, (1974), pp. 67-70.