A rotor blade assembly includes a blade body having a leading edge and a trailing edge. A damper element is disposed within the blade body and along a forcing axis extending between the leading and trailing edges of the blade body to apply damping force in-plane with the blade body to damp load and oppose edgewise motion of the blade body associated with the load.
SYSTEMS AND METHODS FOR DAMPING ROTOR BLADE ASSEMBLIES
2017-02-09
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |