Abstract
Specimens designed to reproduce the state of stress of the dovetail joint between blade and disk in a typical gas-turbine configuration have been tested in a 250-kN capacity biaxial fatigue machine. The materials tested were Ti-IMI 829 (disk and blade), Inco 901 and steel FV535 (blades only). The investigation highlights the importance of fretting at the disk/blade interface. A design parameter that combines fretting damage and peak stress is proposed as a basis for the life assessment of the joints.
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References
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Boddington, P.H.B., Chen, K.C. and Ruiz, C., “Numerical Stress Analysis of Dovetail Joints,” to be published in J. Computers & Structures.
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Boddington, P.H.B., “Fatigue Failure Mechanisms in Dovetail Blade Root Fixings,” PhD Thesis, OUEL (1982).
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Ruiz, C., Boddington, P.H.B. & Chen, K.C. An investigation of fatigue and fretting in a dovetail joint. Experimental Mechanics 24, 208–217 (1984). https://doi.org/10.1007/BF02323167
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DOI: https://doi.org/10.1007/BF02323167