Abstract: A method and system is disclosed for controlling problematic vibrations in an aircraft having. The method and system have the ability to cancel problematic rotary wing helicopter vibrations using independent active force generator power and with distributed communications therebetween.
Type:
Grant
Filed:
December 21, 2011
Date of Patent:
January 28, 2014
Assignee:
Lord Corporaiton
Inventors:
Mark R. Jolly, Askari Badre-Alam, Russell E. Altieri, Andrew D. Meyers