Turbine blade retaining apparatus
作者： Jean Chamoun , Benoit Douville , Nicholas Grivas
DOI:
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摘要: An apparatus for retaining blade to a rotor disc of turbine engines includes positioning member integrally stopping the root when sliding into an attachment slot disc, and locking in slots.
lens.org 参考文章(21)
Jerry H. Moore, Blade lock for a rotor disk and rotor blade assembly ,(1990)
Larry Earl Glassburn, Turbomachine with balancing means ,(1974)
Christopher C. Glynn, Richard L. Horvath, James C. Przytulski, Philip H. Stoughton, Richard A. Wesling, Robert J. Corsmeier, Turbine blade inner end attachment structure ,(1990)
Claudio Brumen, Locking of rotor blades on a rotor disk ,(1980)
James Charles Gautreau, Chris A. Rickert, Nicholas Francis Martin, Compressor blade with dovetail slotted to reduce stress on the airfoil leading edge ,(2004)
Edward C. Hill, Peter T. Vercellone, Wesley D. Brown, Turbine rotor retention system ,(1988)
Christopher C. Glynn, Richard J. Fallon, Andrew J. Lammas, Roger C. Walker, Dovetail sealing device for axial dovetail rotor blades ,(1992)
Ronald Eugene Schlechtweg, Alan Walker, Robert Ingram Ackerman, Boltless turbine nozzle/stationary seal mounting ,(1992)
Hugoson B, Vettel N, Sideplate for turbine blade ,(1971)
Robert J. Meade, Richard W. Albrecht, Turbine disk interstage seal anti-rotation key through disk dovetail slot ,(1993)