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  • licopter active noise control systemUS5316240 *Aug 12, 1992May 31, 1994Aerospatiale Societe Nationale IndustrielleMethod and device for filtering the vibratory excitations transmitted between two parts especially between the rotor and the fuselage of a helicopterUS5327061Jun 26, 1992Jul 5, 1994Hughes Aircraft CompanyForce (torque) nulling inertially servoed structural interfaceUS5332061Mar 12, 199
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