Elastic strut having an integrated hydromechanical resonator in particular for the suspension of a transmission box on a rotor aircraft and a suspension device using such a strut

Claim 2

An elastic strut incorporating a hydromechanical resonator having a weight/spring system providing a hydraulic amplification of a displacement of a beating weight, said strut comprising: a body constituted by an inner tubular element (1) and an outer tubular element (2) which is coaxial with the inner tubular element; two hydraulic chambers respectively disposed inside ends of said tubular elements; two cylindrical bearings composed of an elastomer material for interconnecting in a sealed and elastic manner ends of the two tubular elements so as to permit the two tubular elements, under the effect of axial forces, limited relative displacements with an elastic return to a mean position and to ensure a sealed closure of said two hydraulic chambers; a liquid having a low viscosity filling said two chambers; a beating weight; two opposed springs cooperative with said beating weight for biasing said weight to a neutral position, said beating weight constituting a double-sided hollow piston; a third closed hydraulic chamber constituted inside the inner tubular element (1) and filled with said liquid having a low viscosity; two coaxially opposed hollow cylinders in said third closed hydraulic chamber, said piston being slidably mounted on said two hollow cylinders, said two hollow cylinders each opening onto a respective one of said hydraulic chambers disposed at respective ends of said tubular elements.

Claim 3

An elastic strut according to claim 1, comprising closing members for closing ends of said inner element, said cylinders being tubular bosses connected to said closing members and extending inside said inner element, said piston being biased to said neutral position by said two springs which are disposed around said tubular bosses on opposite sides of said piston.

Claim 4

An elastic strut according to claim 1, wherein each of said hydraulic chambers comprises end walls of different areas, the end walls having the largest areas being outer walls and the end walls having the smallest areas being constituted by said double piston.

Claim 5

An elastic strut according to claim 3, wherein each of said inner and outer elements comprises outer fixing means for introducing axial forces.

Claim 6

A suspension device comprising bars for a main transmission box on a structure of a fuselage of a rotor aircraft, wherein each of said bars comprises an elastic strut incorporating a hydromechanical resonator having a weight/spring system providing a hydraulic amplification of a displacement of a beating weight, said strut comprising a body constituted by an inner tubular element (1) and an outer tubular element (2) which is coaxial with the inner tubular element; two hydraulic chamber respectively disposed inside ends of said tubular elements; two cylindrical bearings composed of an elastomer material for interconnecting in a sealed and elastic manner ends of the two tubular elements so as to permit the two tubular elements, under the effect of axial forces, limited relative displacements with an elastic return to a mean position and to ensure a sealed closure of said two hydraulic chambers; a liquid having a low viscosity filling said two chambers; a beating weight; to opposed springs cooperative with said beating weight for biasing said weight to a neutral position, said beating weight constituting a double-sided hollow piston; a third closed hydraulic chamber constituted inside the inner tubular element (1) and filled with said liquid having a low viscosity, two coaxially opposed hollow cylinders in said third closed hydraulic chamber, said piston being slidably mounted on said two hollow cylinders, said two hollow cylinders each opening onto a respective one of said hydraulic chambers disposed at respective ends of said tubular elements.

Claim 7

A suspension device comprising bars for a main transmission box on a structure of a fuselage of a rotor aircraft, wherein each of said bars comprises an elastic strut incorporating a hydromechanical resonator having a weight/spring system providing a hydraulic amplification of a displacement of a beating weight, said strut comprising a body constituted by an inner tubular element (1) and an outer tubular element (2) which is coaxial with the inner tubular element; two hydraulic chamber respectively disposed inside ends of said tubular elements; two cylindrical bearings composed of an elastomer material for interconnecting in a sealed and elastic manner ends of the two tubular elements so as to permit the two tubular elements, under the effect of axial forces, limited relative displacements with an elastic return to a mean position and to ensure a sealed closure of said two hydraulic chambers; a liquid having a low viscosity filling said two chambers; a beating weight; to opposed springs cooperative with said beating weight for biasing said weight to a neutral position, said beating weight constituting a double-sided hollow piston; a third closed hydraulic chamber constituted inside the inner tubular element (1) and filled with said liquid having a low viscosity, two coaxially opposed hollow cylinders in said third closed hydraulic chamber, said piston being slidably mounted on said two hollow cylinders, said two hollow cylinders each opening onto a respective one of said hydraulic chambers disposed at respective ends of said tubular elements.