Crocodile-type flight control surface for aircraft with locking mechanism for additional stiffness

A crocodile-type flight control surface comprising:

• an upper foil flap,
• a lower foil flap,
• an actuating mechanism configured to guarantee the rotational displacement of each foil flap about a joint axis, either in the same direction or in different directions, wherein the actuating mechanism comprises:
• a first actuator,
• a second actuator,
• an upper connecting rod fixed at one end to the upper foil flap and at another end to the first actuator and
• a lower connecting rod fixed at one end to the lower foil flap and at another end to the second actuator,
• the upper connecting rod and the lower connecting rod being mounted in a rotationally movable manner about the shared axis, wherein one of the connecting rods comprises a first shaft, whereas the other connecting rod comprises a second shaft which is hollow and in which is housed said first shaft, and
• a locking mechanism alternatively adopting a locking position in which the upper foil flap and the lower foil flap are fixed, with respect to each other, and an unlocking position in which the upper foil flap and the lower foil flap are free, with respect to each other, wherein the locking mechanism comprises:
• a plunger cylinder, the cylinder extending the second shaft and a piston extending the first shaft, defining a chamber between the bottom of the cylinder and the piston,
• an energy source connected to the chamber and adapted to adopt, alternatively, a pressurized position in which the energy source puts the chamber under pressure and tends to push back the piston from the bottom of the chamber and an unpressurized position in which the energy source does not place the chamber under pressure,
• a return travel means which prevents the piston from moving towards the bottom of the chamber, and,
• wherein that part of the inner surface of the cylinder takes the shape of a first frustum and part of the outer surface of the piston takes the shape of a second frustum, the two frustums being arranged such that in an unpressurized position corresponding to the locking position, their lateral surfaces are in contact, preventing any movement with respect to the other, and such that in a pressurized position corresponding to the unlocking position, their lateral surfaces are not in contact, allowing movements of one with respect to the other.