VIBRATION ATTENUATOR

A vibration attenuator for a rotor of an aircraft has a track housing adapted for rotation relative to the rotor and configured for rotation at a second angular velocity greater than a first angular velocity of the rotor. A track is located within the track housing and has a reaction surface, a pair...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Heverly, David, Smith, Michael R, Stamps, Frank Bradley, Parham, Thomas C, Choi, Jouyoung Jason
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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