초록 ▼

A hollow rotor hub is provided at the top of the rotor shaft for a multi-bladed helicopter. The blades being mounted to the rotor hub on spherical elastomeric bearings which provide for coincident rotor blade hinges for blade pitch, flap and lead-lag motions. The invention discloses a lead-lag dampe

A hollow rotor hub is provided at the top of the rotor shaft for a multi-bladed helicopter. The blades being mounted to the rotor hub on spherical elastomeric bearings which provide for coincident rotor blade hinges for blade pitch, flap and lead-lag motions. The invention discloses a lead-lag damper contained in a housing at the center of the hollow rotor hub. The damper consists of a series of damping plates, each plate being connected to one of the rotor blades. The damping plates are separated from each other and from the damper housing by elastomeric layers bonded to the plates and to the housing. Lead-lag damping is provided by the shear in the elastomeric layers. The damper may be fastened to the air frame in a conventional manner, it may be mounted on a spindle for rotation about the rotor axis independent of rotor shaft rotation or may be free-floating and attached only to the rotor blades and not to the rotor shaft. With suitable selection of elastomeric damping material properties, it can provide blade to hub damping, blade to blade damping or combinations thereof.

대표청구항 ▼

A rotor hub for a helicopter rotor rotatable about a rotor axis,said hub comprising; a rotor shaft having a central opening at its upper end and extending at least partially through its length along the rotor axis; a plurality of rotor blades attached to said rotor shaft and rotatable therewith abou

A rotor hub for a helicopter rotor rotatable about a rotor axis,said hub comprising; a rotor shaft having a central opening at its upper end and extending at least partially through its length along the rotor axis; a plurality of rotor blades attached to said rotor shaft and rotatable therewith about the rotor axis; spherical bearing means for attaching said rotor blades to said rotor shaft, said spherical bearings providing for motion of said blades in blade pitch, flap and lead-lag directions, the hinge points of said motions being coincident in the spherical bearing; a damper assembly assembled in the central opening of said rotor shaft for providing damping in the lead-lag direction, said damper comprising; a damper housing assembled in said rotor shaft and centered on the rotor axis said housing being a hollow structure having upper and lower walls; a plurality of damper plates mounted in said damper housing, one plate being provided for each of said rotor blades; elastomeric material assembled between said plates and between said plates and the damper housing; means for attaching each of said blades to a separate one of said damper plates.