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Self-tuning impact damper for rotating blades.


U.S. patent: 6,827,551

Issued: December 7, 2004

Inventors: Kirsten P. Duffy, Gerald V. Brown and Ronald L. Bagley

Assigned: The United States of America UNITED STATES OF AMERICA. The name of this country. The United States, now thirty-one in number, are Alabama, Arkansas, Connecticut, Delaware, Florida, Georgia, Illinois, Indiana, Iowa, Kentucky, Louisiana, Maine, Maryland, Massachusetts, Michigan, Mississippi, Missouri, New Hampshire,  as represented by the Administrator of the National Aeronautics and Space Administration National Aeronautics and Space Administration (NASA), civilian agency of the U.S. federal government with the mission of conducting research and developing operational programs in the areas of space exploration, artificial satellites (see satellite, artificial),  

Keywords: The self-tuning impact damper uses the rotor speed to tune the resonant frequency resonant frequency,
n the specific frequency at which an object vibrates.
 of a rattling mass to an engine order excitation frequency.
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Title Annotation:Patent News
Author:Samples, Bob
Publication:Rubber World
Date:May 1, 2005
Words:63
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