Distributed active vibration control systems and rotary wing aircraft with suppressed vibrations

摘要

An aircraft with at least one rotating machine that comprises a structure and air, generate a vibration problem, the aircraft, a power source for outputting a plurality of electromagnetic force generator power output (power source); The air structure comprising a plurality of distributed active vibration control system site (site); A first distributed electronic control system and a first and a electromagnetic driving mass, a first distributed active vibration control system on a fixed site on the air structure, at least a first distributed active vibration electromagnetic force generator; Second distribution control electronic system and a second and a electromagnetic driving mass, a second distribution site, the active vibration control system in a fixed structure on the air, at least a second distributed active vibration electromagnetic force generator; A plurality of power distribution lines to couple the electromagnetic power generator and the power source, the power output of the electromagnetic force generator, a plurality of power distribution lines to be output to the electromagnetic force generator; Said at least a first distributed electronic control system and a second distributed electronic control systems as distributed force generator data communications network connecting together the distributing electronic control systems the distribution of the power distribution line and independently to minimize the vibrations to which the problem and a, distributed force generator data communications network to communicate the power generator vibration control data through the force generator data communications network. ;