发明名称 HYBRID ACTIVE-PASSIVE NOISE AND VIBRATION CONTROL SYSTEM FOR AIRCRAFT
摘要 <p>A hybrid active-passive system (20) for reducing noise within a passenger compartment and vibration of a fuselage of a vehicle, such as an aircraft (turboprop, turbofan, or helicopter). The hybrid active-passive system (20) includes, in combination: an active acoustic producer such as a loudspeaker (35), Active Vibration Absorber (AVA) (34), or active absorber assembly (39) for producing antinoise within the compartment (42), and a passive resonant device, such as a passive Tuned Vibration Absorber (TVA) (36), or passive TVA assembly (37) for controlling vibration of the fuselage or structural supports interconnecting the disturbance source (e.g. power plants (26), propellers (28a), gearbox (57), main rotor (28m), tail rotor (28t)) and the fuselage wall (25).</p>
申请公布号 WO1998016916(A1) 申请公布日期 1998.04.23
申请号 US1997012010 申请日期 1997.07.10
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