Influence of an aluminide coating on the tmf life of a single crystal nickel-base superalloy

Journal of Engineering for Gas Turbines and Power

Volumn 121, Issue 4, 1999, Pages 687-690

  Affeldt, E E ^a  

^a MTU AERO ENGINES GMBH   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0012283794     PISSN: 07424795     EISSN: 15288919     Source Type: Journal    
DOI: 10.1115/1.2818527     Document Type: Article

References (11)

1. Bressers, J., Timm, J., Williams, S. J., Affeldt, E. E., and Bennett, A., 1996a, “Effects of Cycle Type and Coating on the TMF Lives of CMSX6,” AGARD-CP-569, advisory group for aerospace research and development, Neuilly-sur-Seine, France, pp. 91-910
2. Bressers, J., Timm, J., Williams, S. J., Bennett, A., and Affeldt, E. E., 1996b, “Effects of Cycle Type and Coating on the TMF Lives of a Single Crystal Nickel Based Gas Turbine Blade Material,” ASTM STP 1263, M. J. Verrilli, and M. G. Castelli, eds., American Society for Testing and Materials, Philadelphia, PA, pp. 56-67.
3. Chataigner, E., and Remy, L, 1996, “Thermomechanical Fatigue Behavior of Coated and Bare Nickel-Based Superalloy Single Crystals,” ASTM STP 1263, M. J. Verrilli and M. G. Castelli, eds., American Society for Testing and Materials, Philadelphia, PA, pp. 3-26.
4. Fleury, E„ and Remy, L., 1990, “Thermal Mechanical Fatigue of AMI Superalloy Single Crystals,” High Temperature Materials for Power Engineering 1990, E. Bachelet et al., eds., Kluwer Academic Publishers, London, pp. 1007-1016.
5. Heine, J. E., Warren, J. R., and Cowles, B. A., 1989, “Thermal Mechanical Fatigue of Coated Blade Materials,” Report No. WRDC-TR-87-4102, United Technologies Corporation, Pratt & Witney, West Palm Beach, FL, pp. 13-20.
6. Johnson, P. K., Arana, M., Ostolaza, K. M„ and Bressers, J., 1997, “Crack Initiation in a Coated and an Uncoated Nickel-Base Superalloy Under TMF Conditions,” J. of Eng. Materials and Technology, to be published.
7. Linde, L., and Henderson, P. J., 1994, “Thermo-Mechanical and Low Cycle Fatigue of a Coated Nickel-Base Superalloy,” Materials for Power Engineering, Part II, E. Bachelet et al., eds., Kluwer Academic Publishers, London, pp. 1367-1376.
8. Martinez-Esnaola, J. M., Arana, M., Bressers, J., Timm, J., Bennett, A., and Affeldt, E. E., 1996, “Crack Initiation in an Aluminide Coated Single Crystal During Thermomechanical Fatigue,” ASTM STP 1263, M. J. Verrilli and M. G. Castelli, eds., American Society for Testing and Materials, Philadelphia, PA, pp. 68-81.
9. Totemeier, T. C., Gale, W. F., and King, J. E., 1993, “Fracture Behaviour of an Aluminide Coating on a Single Crystal Nickel Base Superalloy,” Materials Science and Engineering, Vol. A169, pp. 19-26.
10. Totemeier, T. C., King, J. E., 1996, “Isothermal Fatigue of an Aluminide-Coated Single-Crystal Superalloy: Part I,” Metallurgical and Materials Transactions A, Vol. 27A, pp, 353-361.
11. Vasseur, E., and Remy, L., 1994, “High Temperature Low Cycle Fatigue and Thermal-Mechanical Fatigue Behaviour of an Oxide-Dispersion-Strengthened Nickel-Base Superalloy,” Mat. Science and Engng., A184, pp. 1-5.