A system for controlling the pitch of a propeller blade for an aircraft turbine engine, including a cup having an annular wall extending about an axis intended to be a pitch setting axis of the blade, and a bottom wall configured so as to cooperate in a form-fitting manner with a free end of the root so that the cup is prevented from rotating relative to the root about the axis, and a locking ring that is configured so as to be mounted within the cup and to cooperate respectively with the root and the annular wall of the cup in order to ensure axial retention of the root in the cup.
TURBOMACHINE D'AERONEF COMPORTANT DES AUBES D'HELICE A CALAGE VARIABLE
AIRCRAFT TURBINE ENGINE COMPRISING VARIABLE-PITCH PROPELLER BLADES
FLUGZEUGTURBINENTRIEBWERK MIT VERSTELLPROPELLERSCHAUFELN
2024-06-05
Patent
Elektronische Ressource
Französisch
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