NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Self-Tuning Impact Damper for Rotating BladesA self-tuning impact damper is disclosed that absorbs and dissipates vibration energy in the blades of rotors in compressors and/or turbines thereby dramatically extending their service life and operational readiness. The self-tuning impact damper uses the rotor speed to tune the resonant frequency of a rattling mass to an engine order excitation frequency. The rating mass dissipates energy through collisions between the rattling mass and the walls of a cavity of the self-tuning impact damper, as well as though friction between the rattling mass and the base of the cavity. In one embodiment, the self-tuning impact damper has a ball-in-trough configuration with tire ball serving as the rattling mass.
Document ID
20050051584
Acquisition Source
Glenn Research Center
Document Type
Other - Patent
Authors
Kirsten P Duffy
Gerald V Brown
Ronald L Bagley
Date Acquired
August 22, 2013
Publication Date
December 7, 2004
Subject Category
Mechanical Engineering
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-6,827,551
Patent Application
US-Patent-Appl-SN-498794
No Preview Available