Helicopter rotor

1. A rotor for a helicopter, comprising:

a drive shaft rotating about a first axis;

a hub angularly integral with said drive shaft about said first axis;

at least two blades projecting from said hub on opposite sides of said first axis and elongated along respective second axes crosswise to said first axis, each said blade being movable with respect to said hub and to the other said blade about a respective third axis crosswise to the respective said second axis;

a number of dampers for damping oscillation of respective said blades about the respective said third axes, and which comprise respective first portions movable integrally with the respective said blades about the respective said third axes;

said dampers comprising respective second portions connected elastically to the respective first portions and functionally to each other;

said second portions of said dampers being connected rigidly to one another; and

a number of rigid rods interposed each between respective pair of said second portions of a respective pair of adjacent said dampers and alternating with said blades about said first axis:

each said damper comprising two second portions and being connected to two adjacent dampers;

one second portion of each damper being connected by one relative rod to a respective second portion of one of said adjacent dampers; the other second portion of each damper being connected by the other relative rod to a respective second portion of the other of said adjacent dampers.

2. A rotor as claimed in claim 1 , characterized in that each said damper is made at least partly of elastically deformable material, is in the form of a tubular body with respect to a fourth axis, and comprises:

two bases comprising said first portion and fixed to opposite walls of the respective said blade spaced apart along said fourth axis; and

a lateral surface comprising said second portion and surrounding said fourth axis.

3. A rotor as claimed in claim 2 , characterized in that each said blade comprises an appendix eccentric with respect to the relative said second axis; said appendix comprising said walls, and being acted on by an external member to rotate the respective said blade about the respective said second axis.

4. A rotor as claimed in claim 2 , characterized in that said first and said fourth axis are parallel.

5. A rotor as claimed in claim 1 , characterized by comprising a number of said blades and said dampers; and a number of said rods alternating with said blades about said first axis;

each said damper comprising two second portions and being connected to two adjacent dampers;

each second portion of each damper being connected by a relative rod to a respective second portion of one of said adjacent dampers.

6. A rotor as claimed in claim 5 , characterized in that said second portions of each said damper are located on the opposite side of the relative said fourth axis with respect to said first axis.

7. A rotor as claimed in claim 5 , characterized in that said rods extend on the opposite side of said fourth axes with respect to said first axis.

8. A rotor as claimed in claim 5 , characterized in that at least one of said second portions is interposed between said first axis and said fourth axis of the relative said damper.

9. A rotor as claimed in claim 8 , characterized in that the other of said second portions of each said damper is located to the side of the second axis of the relative blade.

10. A rotor as claimed in claim 9 , characterized in that each said rod connects said one of said second portions of the relative damper to said other of said second portions of the adjacent said damper.