Device for locking the pitch and for feathering adjustable-pitch fan blades of a turbine engine propeller

1. A device for locking the pitch and for feathering adjustable-pitch fan blades of a turbine engine propeller, the device comprising:

an actuator having at least one movable portion extending parallel to an axis of rotation of the propeller and designed to be coupled to pivots of the fan blades of the propeller in order to modify their pitch angle when it slides;

a movable part that is movable relative to the actuator having first mechanical means suitable for co-operating with the actuator when in a fan blade pitch-unlocking position in order to enable the actuator movable portion to slide over an extended actuator stroke; and second mechanical means distinct from the first mechanical means and suitable for co-operating with the actuator when in a fan blade pitch-locking position in order to enable the actuator movable portion to slide over an actuator stroke that is shorter than the extended actuator stroke; and

drive means for moving the movable part between the unlocking position of the actuator and the locking position of the actuator.

2. The device according to claim 1 , wherein the actuator movable portion comprises a flat and the first mechanical means of the movable part include a notch formed in a portion facing the movable portion of the actuator and along which the flat of the movable portion of the actuator can slide when in the fan blade pitch-unlocking position.

3. The device according to claim 1 , wherein the movable portion of the actuator comprises a flat and the second mechanical means of the movable part include an abutment against which the flat of the movable portion of the actuator comes into abutment when in the fan blade pitch-locking position.

4. The device according to claim 1 , wherein the movable part further comprises third mechanical means distinct from the first and second mechanical means and suitable for co-operating with the actuator to move it into a fan blade feathered position.

5. The device according to claim 4 , wherein the movable portion of the actuator comprises a flat and the third mechanical means of the movable part include a ramp projecting from a lateral surface of said movable part and forming a cam path along which the flat of the actuator movable portion slides in order to bring the actuator movable portion into the fan blade feathered position.

6. The device according to claim 1 , wherein the movable part comprises a ring centered on the axis of rotation of the propeller, the first mechanical means are configured to co-operate with the actuator in the fan blade pitch-unlocking position to allow the actuator movable portion to slide along an extended actuator stroke, the second mechanical means are angularly offset relative to the first mechanical means and are configured to co-operate with the actuator when in the fan blade pitch-locking position to allow the actuator movable portion to slide over an actuator stroke that is shorter than the extended actuator stroke, and the drive means comprise means for causing the ring to pivot about the axis of rotation of the propeller.

7. The device according to claim 6 , wherein the means for causing the ring to pivot about the axis of rotation of the propeller comprise drive means having a gearwheel meshing with teeth carried by the ring.

8. The device according to claim 7 , wherein the teeth of the ring are positioned at an outer periphery of the ring and extend angularly over a portion of said ring.

9. The device according to claim 6 , wherein the movable portions of the actuator are positioned inside the ring.

10. The device according to claim 1 , wherein the extended actuator stroke corresponds substantially to the stroke allowed to the actuator in flight.

11. The device according to claim 1 , comprising at least three movable actuator portions regularly distributed around the axis of rotation of the propeller.

12. The system for controlling the pitch of fan blades of a turbine engine having at least one propeller with adjustable pitch fan blades, said propeller being constrained to rotate with a rotary ring, the fan blades being coupled, in order to adjust their pitch, to a system comprising an actuator and a load transfer bearing, the system further comprising a device according to claim 1 .

13. The turbine engine comprising at least one set of adjustable pitch fan blades and a fan blade pitch coupling system according to claim 12 .