Patent ID: 8141813

Claim:
A helicopter comprising a rotor, a fuselage, and a transmission connected functionally to said rotor; said helicopter also comprising a supporting body supporting at least said transmission, first connecting means connected to said supporting body, second connecting means connected to said fuselage, and elastic means interposed between said first and second connecting means; said first connecting means comprising a first connecting member having: a flange connected to said supporting body and defining an opening with a first axis transversal to a longitudinal axis of said fuselage; and a first and second appendix projecting from respective portions of said flange on opposite sides of said first axis; characterized in that each of said first and second appendix is V-shaped and comprises two sides converging on the opposite side to said first axis; in that said second connecting means comprise one pair of second connecting members located on the opposite sides of said first appendix and another pair of second connecting members located on the opposite sides of said second appendix; and in that said elastic means comprise at least a pair of first elastic members interposed between the opposite sides of said first appendix and the respective second connecting members, and at least a pair of second elastic members interposed between the opposite sides of said second appendix and the respective second connecting members.