An aircraft rotor assembly has a yoke defining a plurality of bearing pockets. Each bearing pocket houses an axisymmetric elastomeric spherical bearing at least partially therein. The axisymmetric elastomeric spherical bearings comprise flap, lead-lag, and pitch hinges for rotor blades coupled thereto. The rotor blades maintain a first in-lane frequency of less than 1/rev through the use of damper assemblies coupled between adjacent blades.
ROTOR HUB WITH BLADE-TO-BLADE DAMPERS AND AXISYMMETRIC ELASTOMERIC SPHERICAL BEARINGS
MOYEU DE ROTOR A AMORTISSEURS AUBE-AUBE ET ROULEMENTS A ROTULE ELASTOMERES A SYMETRIE AXIALE
22.03.2019
Patent
Elektronische Ressource
Englisch
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