发明名称 Self-tuning impact damper for rotating blades
摘要 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 rattling mass dissipates energy through collisions between the rattling mass and the walls of a cavity of the self-tuning impact damper, as well as through 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.
申请公布号 US6827551(B1) 申请公布日期 2004.12.07
申请号 US20000498794 申请日期 2000.02.01
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION 发明人 DUFFY KIRSTEN P.;BROWN GERALD V.;BAGLEY RONALD L.
分类号 F01D5/16;F01D5/26;(IPC1-7):F03B11/04 主分类号 F01D5/16
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