HORIZTONAL STABILIZERS WITH VIBRATION DAMPENING

Systems and methods provide for the mitigation of vibrational forces acting on a horizontal stabilizer (102) of an aircraft. According to one aspect, a damper (106) is coupled to a front portion of a horizontal stabilizer (102) to dampen vibrations in a first degree of freedom, with another damper (...

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Bibliographische Detailangaben
Hauptverfasser: GOLSHANY, SINA SAM, HUNTLY, DAVID M, ERICKSON, TODD W, TRETOW, PAUL R
Format: Patent
Sprache:eng ; fre ; ger
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Zusammenfassung:Systems and methods provide for the mitigation of vibrational forces acting on a horizontal stabilizer (102) of an aircraft. According to one aspect, a damper (106) is coupled to a front portion of a horizontal stabilizer (102) to dampen vibrations in a first degree of freedom, with another damper (106) coupled to a mounting point (118) of the horizontal stabilizer (102) to dampen vibrations in a second degree of freedom. The dampers (106) may be passive, operating independently to mitigate vibrational forces, or active, applying a mitigating force to the horizontal stabilizer (102) based on real-time or estimated vibration states.