Determination of the crack propagation life of a planetary gear carrier

Annual Forum Proceedings - American Helicopter Society

Volumn 2, Issue , 2004, Pages 1229-1237

  Sahrmann, Glenn J ^a  

^a U S ARMY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

GEAR CARRIER; OIL PRESSURE; RISK MITIGATION; ULTRASONIC PROBES;

AEROSPACE ENGINEERING; FINITE ELEMENT METHOD; GEAR TEETH; HELICOPTERS; MICROSTRUCTURE; RISK ASSESSMENT; SPLINES;

CRACK PROPAGATION;

EID: 4143140835     PISSN: 07334249     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (3)

1. Yuen, A., Hopkins, S.W., Leverant, G.R., and Rau, C.A., "Correlations between Fracture Surface Appearance and Fracture Mechanics Parameters for Stage II Fatigue Crack Propagation in Ti-6Al-4V" Metallurgical Transactions, Vol. 5, August 1974, 1833-1842.
2. Lenets, Y.N. and Bellows, R.S., "Crack Propagation Life Prediction for Ti-6Al-4V based on striation spacing measurements." International Journal of Fatigue, Vol. 22, 2000, 521-529.
3. Morrissey, R.J., McDowell, D.L., and Nicholas, T., "Frequency and stress ratio effects in high cycle fatigue of Ti-6Al-4V" International Journal of Fatigue, Vol. 21, 1999, 679-685.