Control assembly for a stage of variable-pitch vanes for a turbine engine
AssigneeSafran Aircraft Engines
InventorOlivier Bazot
Life of this patent
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AssigneeSafran Aircraft Engines
InventorOlivier Bazot
Estimating the term…
A control assembly for a stage of variable-pitch vanes for a turbine engine generally includes an actuating ring having an annular body, a vane guidance means for connecting to the cylindrical pivots of the variable pitch vanes, a rotating means for rotating the actuating ring about a casing of the turbine engine, and a centering means for cooperating with the casing to center the actuating ring. The centering means may have at least one skid bearing against the casing. At least one of the skid or the rod may be configured to cooperate by radial sliding with an inner wall of a housing. The skid may be configured to be mobile during operation by sliding between a radially internal position and a radially external position.
A control assembly for a stage of variable-pitch vanes for a turbine engine, each variable-pitch vane having a cylindrical pivot at a radially outer end thereof, the control assembly comprising:
A control assembly for a stage of variable-pitch vanes for a turbine engine, each variable-pitch vane having a cylindrical pivot at a radially outer end thereof, the control assembly comprising:
Dependencies are inferred from the claim text.