Fluid elastomeric damper assembly including internal pumping mechanism and volume compensator
AssigneeLord Corporation
InventorDONALD D. RUSSELL
Life of this patent
Estimating the term…
Loading patent…
AssigneeLord Corporation
InventorDONALD D. RUSSELL
Estimating the term…
Rotary wing system with a rotating blade rotating about a rotation axis. The system includes a fluid damper with a damper fluid for controlling a troublesome motion. The fluid damper has an inboard end and an outboard end, the damper inboard end attached to a first rotary wing system inboard member proximate the rotation axis and the outboard end attached to a second rotary wing system outboard member distal from the rotation axis. The fluid damper contains a damper fluid volume in at least a first working chamber which is worked by a relative motion between said first rotary wing system inboard member and said second rotary wing system outboard member to control the troublesome motion. The damper includes a volume compensator channel in fluid communication with the damper fluid, the volume compensator channel including a centrifugal force mass member movable along a volume compensating length of the volume compensating channel, wherein a rotation about the rotation axis forces the centrifugal force mass member towards an outboard end of the volume compensating channel and pushes damper fluid from the volume compensator channel towards the at least first working chamber.
A rotary wing system with at least one rotating blade rotating about a rotation axis, said rotary wing system having a troublesome motion when rotating about said rotation axis, said system including a fluid damper with a damper fluid for controlling said troublesome motion, said fluid damper having an inboard end and an outboard end, said fluid damper inboard end attached to a first rotary wing system inboard member proximate said rotation axis and said outboard end attached to a second rotary wing system outboard member distal from said rotation axis, said fluid damper containing a damper fluid volume in at least a first working chamber which is worked by a relative motion between said first rotary wing system inboard member and said second rotary wing system outboard member to control said troublesome motion, said fluid damper including a volume compensator channel in fluid communication with said damper fluid, said volume compensator channel including a centrifugal force mass member movable along a volume compensating length of said volume compensating channel, wherein a rotation about said rotation axis forces said centrifugal force mass member towards an outboard end of said volume compensating channel and pushes damper fluid from said volume compensator channel towards said at least first working chamber.
A method for controlling a rotating blade, the method comprising:
A rotating blade damper for a blade rotating about a rotation axis, said blade damper including a fluid damper with a damper fluid for controlling a troublesome blade motion, said fluid damper having an inboard end and an outboard end, said fluid damper inboard end for attachment to a first inboard member and said outboard end for attachment to a second outboard member, said fluid damper containing a damper fluid volume in at least a first working chamber which is worked by a relative motion between said inboard end and said outboard end to control said troublesome motion, said blade damper including a volume compensator channel in fluid communication with said damper fluid, said volume compensator channel including a centrifugal force mass member movable along a volume compensating length of said volume compensating channel, wherein a rotation about said rotation axis forces said centrifugal force mass member towards an outboard end of said volume compensating channel and pushes damper fluid from said volume compensator channel towards said at least first working chamber.
A method of making a damper, said method including:
A method of making a rotating blade machine, said method comprising:
A method of making a rotary wing aircraft machine, said method comprising:
An apparatus as shown.
An apparatus as described herein.
Dependencies are inferred from the claim text.