The invention relates to an aircraft propulsion system (1) comprising a longitudinal axis (A1) and: – a propeller (2) mounted movably in rotation about the longitudinal axis (A1) and comprising a plurality of blades (20) distributed angularly with respect to said longitudinal axis; and – first means (3) for adjusting the pitch angle of said blades configured to modify the pitch angle of each blade as a function of the angular position of each blade about said longitudinal axis.
Propeller propulsion system for an aircraft comprising means for adjusting the pitch angle of the blades of the propeller and aircraft comprising such a propulsion system
