Tunable mass damper assembly for a rotor blade
AssigneeLockheed Martin Corporation
InventorsJohn C. Cox, Steven P. Lozano, David H. Hunter, Emmett Emile Menair, Jacob Adam Fehrman, John Devin Carroll
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AssigneeLockheed Martin Corporation
InventorsJohn C. Cox, Steven P. Lozano, David H. Hunter, Emmett Emile Menair, Jacob Adam Fehrman, John Devin Carroll
Estimating the term…
A tunable mass damper assembly is attachable to a rotor blade. The tunable mass damper assembly comprises a base configured to be attached to the rotor blade and a pendulum mass structure movably attached to the base and configured to move relative to the base in accordance with a rotational speed of the rotor blade about a rotor axis. The pendulum mass structure is configured to reduce vibratory forces of the rotor blade induced by a rotation of the rotor blade about the rotor axis. An entirety of the pendulum mass structure being configured to be contained within and enclosed by the rotor blade.
A tunable mass damper assembly attachable to a rotor blade comprising a leading edge and a trailing edge, the tunable mass damper assembly comprising:
Dependencies are inferred from the claim text.