Accession Number : AD0164373
Title : Independent Self Adjusting Vibration Damper.
Descriptive Note : Patent,
Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C
Personal Author(s) : Crick,Virlon
Report Date : 27 MAR 1973
Pagination or Media Count : 3
Abstract : The patent relates to a device whereby the torque-transmitting connections between a turbine rotor and the individual turbine blades include centrifugally responsive vibration damping elements. The device has limited freedom to swing an individual coupling shafts between plates securing each blade to the rotor assembly. The torque transfer value varies as the speed varies, to damp vibrations due to speed fluctuations.
Descriptors : *Vibration, *Damping, *Patents, Turbine blades, Turbine wheels, Torque
Subject Categories : Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE