System for controlling a plurality of functions of a turbojet engine

1. A control system for controlling a plurality of distinct functions of a turbojet engine that are not to be operated simultaneously, each function being associated with a respective actuation device, the system comprising:

an electric motor adapted to supply mechanical energy to each of the actuation devices;

at least one switching device interposed between the motor and the actuation devices; and

an electronic control unit for the at least one switching device and the electric motor

wherein the electronic control unit controls the at least one switching device to selectively distribute the mechanical energy supplied by the electric motor to one of the actuation devices based on the function to be operated by the one of the actuation devices, and controls the at least one switching device such that the other actuation devices that are not operated simultaneously with the one of the operating devices are not supplied in mechanical energy by the electric motor.

2. A system according to claim 1 , wherein the at least one switching device includes an inlet configured to receive the mechanical energy supplied by the electric motor and first and second outlets, the switching device being configured to switch the mechanical energy received at the inlet to one of the outlets preventing the mechanical energy to be supplied simultaneously at two actuation devices.

3. A system according to claim 2 , wherein the system includes a single switching device, each outlet of the switching device being connected to a respective actuation device.

4. A system according to claim 2 , wherein the system includes first and second switching devices, one of the outlets of the first switching device being connected to the inlet of the second switching device.

5. A system according to claim 2 , wherein at least one of the switching devices is configured to switch the mechanical energy received at the inlet thereof to the first outlet thereof on receiving an electric command signal and to the second outlet thereof in absence of an electric command signal.

6. A system according to claim 2 , wherein at least one of the switching devices is configured to switch the mechanical energy received at the inlet thereof to one of the outlets thereof as a function of a received mechanical command.

7. A system according to claim 2 , wherein the at least one switching device comprises:

an inlet shaft coupled to the inlet;

a first outlet shaft coupled to the first outlet;

a first friction disk coupled to the first outlet shaft;

a second outlet shaft coupled to the second outlet;

a second friction disk coupled to the second outlet shaft;

a metal plate rotatable with the inlet shaft and movable in translation;

a return spring connected at a first end to the inlet shaft and at a second end to the metal plate; and

an electromagnet,

wherein, when the electromagnet is not powered, the plate presses against the first friction disk such that the first outlet shaft rotates with the inlet shaft, and, when the electromagnet is powered, the plate presses against the second friction disk such that the second outlet shaft rotates with the inlet shaft.

8. A system according to claim 1 , wherein the electronic control unit is configured to adapt the electrical power delivered to the motor depending on the function that is to be controlled.

9. A system according to claim 1 , further comprising means for informing the electronic control unit of the motor about which actuation device is having energy distributed thereto.

10. A system according to claim 1 , wherein the functions controlled by the system comprise:

a thrust reverser; and

a maintenance cover.