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NASA NTRS · 20050051584

Self-Tuning Impact Damper for Rotating Blades

Abstract

A 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.

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BibTeXRIS

Kirsten P Duffy, Gerald V Brown, Ronald L Bagley. 2004-12-07. Self-Tuning Impact Damper for Rotating Blades. https://ntrs.nasa.gov/citations/20050051584

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