Aircraft seat attachment system provided with a system for locking an activation lever and/or for maintaining a clamping force by friction

1. An aircraft seat attachment comprising:

a body adapted to be attached to a seat,

a plunger mobile relative to the body, and

an activation lever adapted to drive movement of the plunger relative to the body, and

a friction force-maintaining system,

wherein the activation lever comprises a locking system adapted to go from a first open position corresponding to a free state of the activation lever, which can then move relative to the body, to a second closed position corresponding to a locked state of the activation lever, which is immobilized relative to the body, so that the position of the locking system enables visual detection of a state of the activation lever,

wherein the friction force-maintaining system is adapted to maintain by friction a force clamping the aircraft seat attachment to a rail in the locked state of the aircraft seat attachment so that the activation lever does not participate in maintaining said clamping force, and

wherein the friction force-maintaining system includes a wedging member adapted to slide between two plane linear non-parallel faces that are part of said body and said plunger, respectively, the wedging member being adapted to maintain the clamping force by friction once said wedging member has been moved by sliding between the two faces via the activation lever.

2. The aircraft seat attachment according to claim 1 , wherein the locking system is formed by a latch pivotally mounted to a body of the activation lever, said latch being respectively disengaged from a receptacle formed in the body of the aircraft seat attachment in the open position and engaged in said receptacle in the closed position.

3. The aircraft seat attachment according to claim 2 , wherein the locking system includes a tension spring member spring-loading the latch in a direction of the closed position.

4. The aircraft seat attachment according to claim 2 , wherein the latch has a beveled shape at a free end adapted to be inserted into the receptacle, said receptacle then having in its upper part a slope of corresponding shape.

5. The aircraft seat attachment according to claim 1 , wherein the face of the plunger along which the wedging member can slide corresponds to a face of a slot for guiding the wedging member.

6. The aircraft seat attachment according to claim 1 , wherein the face of the body along which the wedging member can slide is part of a linear inclined portion of said body.

7. The aircraft seat attachment according to claim 1 , wherein the activation lever includes at least one arm that is part of a spring adapted to push on the wedging member to cause the wedging member to slide between the faces of the plunger and the body to bring the aircraft seat attachment to the locked state.

8. The aircraft seat attachment according to claim 1 , wherein the activation lever includes at least one claw on an internal face adapted to come into contact with the wedging member so as to move the wedging member so as to allow the plunger to move away from the body to bring the aircraft seat attachment to an unlocked state.

9. An aircraft seat attachment comprising:

a body adapted to be attached to a seat,

a plunger mobile relative to the body,

an activation lever adapted to drive movement of the plunger relative to the body to enable, in a locked state of said aircraft seat attachment, clamping of a seat fixing rail lip between at least one boss of said body and the plunger, and

a friction force-maintaining system comprising a wedging member,

wherein the friction force-maintaining system is adapted to maintain by friction a force clamping the aircraft seat attachment to a rail in the locked state so that a line of the clamping force passes only through rigid elements comprising the body, the plunger, and the wedging member of the force-maintaining system, and in that the activation lever does not participate in maintaining said clamping force,

wherein the wedging member is adapted to slide between two plane linear non-parallel faces that are part of said body and said plunger, respectively, the wedging member being adapted to maintain the clamping force by friction once said wedging member has been moved by sliding between the two faces via the activation lever.

10. The aircraft seat attachment according to claim 9 , wherein the face of the plunger along which the wedging member can slide corresponds to a face of a slot for guiding the wedging member.

11. The aircraft seat attachment according to claim 9 , wherein the face of the body along which the wedging member can slide is part of a linear inclined portion of said body.

12. The aircraft seat attachment according to claim 9 , wherein the activation lever includes at least one arm that is part of a spring adapted to push on the wedging member to cause wedging member to slide between the faces of the plunger and the body to bring the aircraft seat attachment to the locked state.

13. The aircraft seat attachment according to claim 9 , wherein the activation lever includes at least one claw on an internal face adapted to come into contact with the wedging member so as to move wedging member so as to allow the plunger to move away from the body to bring the aircraft seat attachment to an unlocked state.

14. The aircraft seat attachment according to claim 9 , wherein the activation lever includes a locking system adapted to go from a first angular position called an “open position” corresponding to a free state of the activation lever, which can then move relative to the body, to a second angular position called a “closed position” corresponding to the locked state of the activation lever which is immobilized relative to the body, so that an angular position of the locking system enables visual detection of the state of the activation lever.

15. The aircraft seat attachment according to claim 14 , wherein the locking system is formed by a latch pivotally mounted to a body of the activation lever, said latch being respectively disengaged from a receptacle formed in the body of the aircraft seat attachment in the open position and engaged in said receptacle in the closed position.

16. The aircraft seat attachment according to claim 15 , wherein the locking system includes a tension spring member spring-loading the in a direction of the closed position.

17. The aircraft seat attachment according to claim 15 , wherein the latch has a beveled shape at a free end adapted to be inserted into the receptacle, said receptacle then having in its upper part a slope of corresponding shape.