System for controlling variable geometry apparatuses in a turbine engine

1. A control system for controlling at least first and second variable-geometry devices in a turbomachine, the system comprising:

an actuator that actuates the first and second devices;

the first device including at least one stage of variable-pitch stator vanes and the second device constituting an air-bleed valve for a body of the turbomachine;

the control system configured to control progressive opening of the vane stage and progressive closing of the air-bleed valves as an actuation parameter of the actuator increases.

2. A control system according to claim 1 , configured to close air feed valves such that the variable-pitch stator vanes begin to open during closure of the air-bleed valves, with progressive increase of an actuation parameter of the actuator.

3. A control system according to claim 2 , wherein, when the air feed valve is substantially closed, the control system is configured to perform a major fraction of closure of the vanes of a stage of variable-pitch stator vanes.

4. A control system according to claim 1 , wherein the vane stage includes of a plurality of vanes, each mounted to pivot on a casing of the turbomachine, and a control ring surrounding the casing and connected to each of the vanes of the stage via respective levers, the actuator configured to cause the control ring of the stage to turn by a driver member that is pivotally mounted on the casing.

5. A control system according to claim 1 , wherein the actuator includes a movable control member with movement thereof transmitting commands to the first and second devices.

6. A control system according to claim 1 , wherein the actuator is configured to actuate the first device by varying a parameter over an actuation range for the first device outside which it cannot act on the first device, the actuator being arranged to actuate the second device by causing the same parameter to vary over an actuation range for the second device, outside which it cannot act on the second device, at least a fraction of the first device actuation range lying outside the second device actuation range.

7. A control system according to claim 6 , wherein a second device actuation range is included within the first device actuation range.

8. A control system according to claim 1 , wherein the connection between the actuator and one of the first and second devices includes a declutching device configured to declutch the drive of the device by the actuator over a range of values of an actuation parameter of the actuator.

9. A control system according to claim 8 , wherein the declutching device comprises a first control member that is movable in an empty space of a second control member, the empty space providing lost motion for the second device.

10. A control system according to claim 9 , further comprising return means that maintain a control member of one of the first and second devices in a predetermined position, at least when an actuation parameter varies over a range situated outside an actuation range of the one of the first and second device.

11. A control system according to claim 1 , further comprising an actuation scaling device arranged in the connection between the actuator and one of the devices.

12. A control system according to claim 11 , wherein the actuation scaling device comprises a follower member pivotally mounted on the casing, and an additional pivoting member interposed between the follower member and the device comprising the vane stage, to transmit the control from the actuator to the device, the additional pivoting member being mounted to pivot both on the casing and on the follower member.

13. A turbomachine including a control system according to claim 1 .