Vibration damping apparatus for helicopter rotor

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United States of America Patent

PATENT NO 5639214
SERIAL NO

08634872

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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An apparatus has at least one pendulous member mounted on a rotor so as to be able to swing about an axis of pendular motion spaced at a distance from the center of inertia of the pendulous member. The pendulous member is pivotably mounted on its own axis of rotation parallel to the axis of pendular motion and situated substantially closer to the center of inertia of the pendulous member than to the axis of pendular motion.

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First Claim

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Patent Owner(s)

  • AIRBUS HELICOPTERS

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Guimbal, Bruno Les Milles, FR 12 185

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