Stress relieved dovetail

作者: Anthony E. Hungler , Andrew J. Lammas , William T. Dingwell

DOI:

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摘要: A rotor blade includes an airfoil, integral platform, and a dovetail integrally joined to the platform. The neck extending between pair of lobes configured engage complementary slot in disk. undercut outer face for introducing stress concentration thereat. relieves at expense increasing high cycle fatigue life blade.

参考文章(10)
Frederick Charles Herzner, Stephen Charles Peterson, Jerome Allen Juenger, Stress-relieved rotor blade attachment slot ,(1991)
Andrew J. Lammas, Nicholas J. Kray, Richard J. Fallon, Stress relieving mount for an axial blade ,(1993)
Uy-Liem Nguyen, Bladed rotor of a turbo-machine ,(1995)
Scharf Herbert, Shaped article of ceramic material ,(1952)
Frank Andrew Pisz, Arthur S. Warnock, Roger Walter Heinig, Turbine blade attachment ,(1988)
Galke Volkmar J, Nguyen Uy-Liem, Meylan Pierre, Thermal protection of compressor rotor ,(1997)
Lori E. Matula, Thomas A. Lindstedt, Gas turbine engine blade ,(1990)