Device for controlling cyclic and collective pitch of a helicopter rotor
AssigneeCostruzioni Aeronautiche Giovanni Agusta S.p.A.
InventorEmilio Pariani
Life of this patent
Estimating the term…
Abstract
A device for controlling the cyclic and collective pitch of a helicopter rotor in which a fixed ring of an oscillating plate is maintained regularly fixed and is guided in its oscillations with respect to a drive shaft by a plurality of variable configuration supports uniformly distributed about the said drive shaft and connected to the said fixed ring by means of cylindrical pivots at least one of which is eccentric with respect to an axis rotation of an associated supported fork, which is perpendicular thereto.
Claims5
A cyclic and collective pitch control device for a helicopter rotor mounted on a drive shaft, said control device being supported by a fixed support and comprising:
- an oscillating plate mounted around and spaced away from said drive shaft, said plate including a fixed inner ring and an outer ring rotatably mounted on said inner ring, said outer ring being adapted to rotate with said drive shaft;
- a plurality of variable configuration supports uniformly distributed around said drive shaft and extending between said fixed support and the inner ring;
- each of said configuration supports including a cylindrical pivot perpendicular to said drive shaft for connecting said configuration support to said plate, and forks engaging said pivot and being rotatable about a fork axis perpendicular to the axis of the associated pivot, at least one of said pivots being eccentric;
- displacement means attached to said plate and adapted to oscillate said plate with respect to said shaft about axis substantially perpendicular thereto;
- and
- rotor blade control means connected to said outer ring.
Dependencies are inferred from the claim text.