Device for reducing the vibration generated by a rotorcraft lift rotor, and a rotor hub provided with such a device

1. A device for reducing the vibration of a rotorcraft main rotor provided with a hub and a plurality of blades, said device having a support together with at least one weight element, wherein said weight element is fastened to said support by connection means, and said weight element is connected to said connection means by guide means for guiding said weight element in movement in circular translation in a filter plane that is movable perpendicularly to an elevation axis of said device, said connection means including resilient return means serving to allow said filter plane to move in elevation while keeping the filter plane perpendicular to said elevation axis under the effect of said vibration;

wherein said guide means comprise a first link and a second link;

wherein said first link is fastened to said connection means by a first primary connection member allowing said first link to move in rotation about a first primary axis of rotation, said first link being fastened to said weight element by a first secondary connection member allowing said first link to move in rotation about a first secondary axis of rotation, said second link being fastened to said connection means by a second primary connection member allowing said second link to move in rotation about a second primary axis of rotation, said second link being fastened to said weight element by a second secondary connection member allowing said second link to move in rotation about a second secondary axis of rotation, said first and second primary axes of rotation and said first and second secondary axes of rotation being mutually parallel; and

wherein at least one primary connection member includes a primary fastener pin co-operating with a primary rotary member.

2. A device according to claim 1 , wherein said resilient means extend from a first end zone towards a second end zone, and said first end zone is fastened to said support and said second end zone is fastened to said guide means.

3. A device according to claim 1 , wherein the first and second primary axes and the first and second secondary axes are mutually parallel, and the first distance between the first primary axis and the first secondary axis is equal to the second distance between the second primary axis and the second secondary axis.

4. A device according to claim 1 , wherein at least one secondary connection member comprises a secondary fastener pin co-operating with a secondary rotary member.

5. A device according to claim 1 , wherein said weight element comprises a bottom mass and a top mass that are disposed on either side of said guide means, the bottom mass and the top mass each being capable of receiving adjustment masses.

6. A device according to claim 1 , wherein said resilient means comprise two flexible blades, said guide means being located between said flexible blades.

7. A device according to claim 1 , wherein said resilient means comprise fastener means and a resilient member, said resilient member being fastened to said support and to said fastener means, extending in elevation along said elevation axis, said guide means being fastened to said fastener means.

8. A rotor provided with a hub, wherein the rotor includes a device according to claim 1 .

9. A device for reducing the vibration of a rotorcraft main rotor provided with a hub and a plurality of blades, said device having a support together with at least one weight element, wherein said weight element is fastened to said support by connection means, and said weight element is connected to said connection means by guide means for guiding said weight element in movement in circular translation in a filter plane that is movable perpendicularly to an elevation axis of said device, said connection means including resilient return means serving to allow said filter plane to move in elevation while keeping the filter plane perpendicular to said elevation axis under the effect of said vibration;

wherein said guide means comprise a first link and a second link; and

wherein said first link is fastened to said connection means by a first primary connection member allowing said first link to move in rotation about a first primary axis of rotation, said first link being fastened to said weight element by a first secondary connection member allowing said first link to move in rotation about a first secondary axis of rotation, said second link being fastened to said connection means by a second primary connection member allowing said second link to move in rotation about a second primary axis of rotation, said second link being fastened to said weight element by a second secondary connection member allowing said second link to move in rotation about a second secondary axis of rotation, said first and second primary axes of rotation and said first and second secondary axes of rotation being mutually parallel.

10. A device according to claim 9 , wherein said resilient means extend from a first end zone towards a second end zone, and said first end zone is fastened to said support and said second end zone is fastened to said guide means.

11. A device according to claim 9 , wherein at least one primary connection member includes a primary fastener pin co-operating with a primary rotary member.

12. A device according to claim 9 , wherein the first and second primary axes and the first and second secondary axes are mutually parallel, and the first distance between the first primary axis and the first secondary axis is equal to the second distance between the second primary axis and the second secondary axis.

13. A device according to claim 9 , wherein at least one secondary connection member comprises a secondary fastener pin co-operating with a secondary rotary member.

14. A device according to claim 9 , wherein said weight element comprises a bottom mass and a top mass that are disposed on either side of said guide means, the bottom mass and the top mass each being capable of receiving adjustment masses.

15. A device according to claim 9 , wherein said resilient means comprise two flexible blades, said guide means being located between said flexible blades.

16. A device according to claim 9 , wherein said resilient means comprise fastener means and a resilient member, said resilient member being fastened to said support and to said fastener means, extending in elevation along said elevation axis, said guide means being fastened to said fastener means.

17. A device for reducing vibration of a rotorcraft main rotor provided with a hub and a plurality of blades, said device comprising:

a support;

connection means fastened to the support and comprising resilient return means;

guide means connected to the connection means and comprising a first link and a second link; and

at least one weight element fastened to the guide means, wherein the guide means are configured to guide the weight element in movement in circular translation in a filter plane that is movable perpendicularly to an elevation axis of the device;

wherein the resilient return means are configured to allow the filter plane to move in elevation while maintaining the filter plane perpendicular to the elevation axis under the effect of vibration;

wherein the first link is fastened to the connection means by a first primary connection member allowing the first link to move in rotation about a first primary axis of rotation;

wherein the first link is fastened to the weight element by a first secondary connection member allowing the first link to move in rotation about a first secondary axis of rotation;

wherein the second link is fastened to the connection means by a second primary connection member allowing the second link to move in rotation about a second primary axis of rotation;

wherein the second link is fastened to the weight element by a second secondary connection member allowing the second link to move in rotation about a second secondary axis of rotation; and

wherein the first and second primary axes of rotation and the first and second secondary axes of rotation are mutually parallel.