Active toggle lock for a thrust reverser of an aircraft nacelle

1. An active locking system of a movable element for a thrust reverser of an aircraft nacelle, the thrust reverser including a fixed structure and at least one movable element, the at least one movable element being mounted pivoting or translating between a direct jet position, which provides aerodynamic continuity of the aircraft nacelle, and a reverse jet position which opens at least one passage in the aircraft nacelle, the active locking system comprising:

an active locking device of the movable element, movable between a locking position and an unlocking position;

an actuator of the active locking device controlled by a command for actuating the active locking device;

a blocking device for blocking the active locking device in the unlocking position, the blocking device movable between a blocking position and an unblocking position; and

a device for displacing the blocking device,

wherein the command controls operation of the movable element towards the direct jet position, and the device for displacing the blocking device displaces the blocking device into the unblocking position when the movable element is at a predetermined position.

2. The active locking system according to claim 1 , wherein the blocking device includes two hinged arms, a first arm of the two hinged arms being fixedly connected to the active locking device and a second arm of the two hinged arms being fixedly connected to the fixed structure.

3. The active locking system according to claim 1 , wherein the device for displacing the blocking device is mechanically linked to the movable element.

4. The active locking system according to claim 1 , wherein the device for displacing the blocking device is a sliding member connected to the movable element that slides during operation of the movable element towards the direct jet position and towards the blocking device so as to displace the blocking device into the unblocking position when the movable element is in the predetermined position.

5. The active locking system according to claim 1 further comprising a blocking spring that exerts a force against the blocking device in a direction opposite to displacement of the device for displacing the blocking device during operation of the movable element towards the direct jet position, the blocking spring being compressed by the blocking device during the displacement of the device for displacing the blocking device during operation of the movable element towards the direct jet position.

6. A system for closing a pair of doors for a thrust reverser of an aircraft nacelle, the pair of doors being diametrically opposed and pivotally mounted between a direct jet position, which provides aerodynamic continuity of the aircraft nacelle, and a reverse jet position which opens at least one passage in the aircraft nacelle, the system comprising:

an actuator for closing the pair of doors including two first connecting rods, each first connecting rod being connected to a first lateral edge of each door of the pair of doors, the actuator being configured to operate each door of the pair of doors at least towards the direct jet position;

two sliding members, each of the two sliding members carrying a second connecting rod connected to a second lateral edge opposite to the first lateral edge of each door of the pair of doors, the second connecting rod of each sliding member being configured to be driven by the pair of doors when the actuator operates the pair of doors towards the direct jet position, so as to displace the two sliding members; and

an active locking system according to claim 1 for locking the pair of doors, wherein the device for displacing the blocking device comprises the two sliding members, wherein the at least one movable element comprises each of the pair of doors.

7. The system according to claim 6 further comprising a device for detecting a breakage of at least one of the first connecting rods or the second connecting rods.

8. A thrust reverser of an aircraft nacelle, the thrust reverser including at least one movable element mounted pivoting or translating between a direct jet position, which provides aerodynamic continuity of the aircraft nacelle, and a reverse jet position, which opens at least one passage in the aircraft nacelle, the thrust reverser comprising at least one active locking system according to claim 1 .

9. The thrust reverser according to claim 8 , wherein the at least one movable element is a translating cowl.

10. The thrust reverser according to claim 8 , wherein the at least one movable element comprises a pair of diametrically opposed pivoting doors.

11. The thrust reverser according to claim 10 further comprising a system for closing the pivoting doors, the system comprising:

an actuator for closing the pivoting doors including two first connecting rods, each first connecting rod being connected to a first lateral edge of each pivoting door, the actuator for closing the pivoting doors being configured to operate each pivoting door at least towards the direct jet position; and

two sliding members, each of the two sliding members carrying a second connecting rod connected to a second lateral edge opposite to the first lateral edge of each pivoting door, the second connecting rod of each sliding member being configured to be driven by the pivoting doors when the actuator operates the pivoting doors towards the direct jet position, so as to displace the two sliding members, wherein the two sliding members form the device for displacing each blocking device.

12. The thrust reverser according to claim 11 , wherein the system for closing the pivoting doors includes a device for detecting a breakage of at least one of the first connecting rods or the second connecting rods.