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

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United States of America Patent

PATENT NO 8639399
APP PUB NO 20120158217A1
SERIAL NO

13333196

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Abstract

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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.

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Patent Owner(s)

  • LORD CORPORATION

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Altieri, Russell E Cary, US 29 300
Badre-Alam, Askari Apex, US 32 356
Jolly, Mark R Raleigh, US 71 2351
Meyers, Andrew D Apex, US 13 334

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