Active noise control system in an aircraft and method to reduce the noise in the aircraft

An active noise control system for reducing the sound pressure level in one or more head areas of one or more seats in the interior of an aircraft fuselage includes multiple accelerometers mounted outside of the aircraft fuselage at or near the mounts of the aircraft's propulsion system. One or...

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Bibliographische Detailangaben
Hauptverfasser: Tonon, Devis, Schmid, David, Niquille, Philippe
Format: Patent
Sprache:eng
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