High cycle fatigue in a single crystal superalloy: Time dependence at elevated temperature

Proceedings of the International Symposium on Superalloys

Volumn , Issue , 2004, Pages 657-666

  Wright, P K ^a   Jain, M ^a   Cameron, D ^b  

^a GE AVIATION   (United States)

^b HONEYWELL   (United States)

Author keywords

Environmental coatings; High cycle fatigue; Rupture; Single crystal superalloys

Indexed keywords

AIRCRAFT ENGINES; AIRFOILS; FATIGUE OF MATERIALS; HIGH TEMPERATURE APPLICATIONS; SINGLE CRYSTALS; STRESS ANALYSIS; THERMAL GRADIENTS;

ENVIRONMENTAL COATINGS; HIGH CYCLE FATIGUE; RUPTURE; SINGLE CRYSTAL SUPERALLOYS;

SUPERALLOYS;

EID: 23744463653     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.7449/2004/superalloys_2004_657_666     Document Type: Conference Paper

References (4)

1. th International Symposium on Superalloys, Seven Springs, TMS (1988), p235ff.
2. S. E. Cunningham, G.P. DeLuca, and F.K. Haake, Crack Growth and Life Prediction in Single Crystal Nickel Superalloys, Volume 1, WL-TR-94-4089, Feb 1996, Wright Patterson AFB.
3. K. Walker, "The Effect of Stress Ratio During Crack Propagation and Fatigue for 2024-T3 and 7075-T6 Aluminum", Effects of Environment and Complex Load History on Fatigue Life, ASTM STP621, 1970, pp1-14.
4. C.S. Wukusick, L. Buchakjian, "Property Balanced Nickel Base Superalloys for Producing Single Crystal Articles", U.S. Patent 6,074,602, (2000).