VIbration Dampening For Horizontal Stabilizers

Systems and methods provide for the mitigation of vibrational forces acting on a horizontal stabilizer of an aircraft. According to one aspect, a damper is coupled to a front portion of a horizontal stabilizer to dampen vibrations in a first degree of freedom, with another damper coupled to a mounti...

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Bibliographische Detailangaben
Hauptverfasser: Golshany Sina Sam, Tretow Paul R, Erickson Todd W, Huntly David M
Format: Patent
Sprache:eng
Schlagworte:
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