Gas-guiding pipe comprising a noise-attenuating covering with variable porosity
View Patent ↗A noise-attenuating covering configured for example for a pipe for guiding gases along a gas path. The covering includes a wall defining the gas path and at least one resonance cavity, the wall being pierced with holes for fluid communication between the gas path and the resonance cavity to attenuate noise. The holes have substantially identical diameters and, since the pipe is arranged to guide the gases in the downstream direction, a number of the openings per wall surface unit decreases continuously along the gas path in the downstream direction, such as to confer on the wall substantially constant acoustic resistance along the gas path, for which the noise attenuation is optimized along the gas path.
1. A duct for guiding gas along a gas path, comprising:
an outer wall;
a noise-attenuating covering disposed inside the outer wall, the covering comprising an inner wall delimiting the gas path and at least one resonance cavity arranged between the outer wall and the inner wall, the inner wall being pierced with holes for placing the gas path in fluidic communication with the at least one resonance cavity for the attenuation of noise; and
upstream and downstream transverse walls which close the at least one resonance cavity at upstream and downstream ends of the at least one resonance cavity, respectively,
wherein the upstream and downstream transverse walls define upstream and downstream apertures of the duct, respectively,
wherein the holes have substantially equal diameters, and
wherein the duct guides the gas from upstream to downstream, and a number of the holes per unit of surface area of the inner wall reduces continuously along the gas path, from upstream to downstream, to confer on the inner wall a substantially constant acoustic resistance along the gas path.
2. The duct as claimed in claim 1 , wherein the number of holes per unit of surface area of the wall reduces by at least 5% between an upstream end and a downstream end of the duct.
3. The duct as claimed in claim 1 , wherein the duct extends generally along an axis, and a longitudinal distance between successive holes reduces continuously along the gas path from upstream to downstream.
4. A gas exhaust nozzle of a gas turbine engine comprising:
a duct for guiding gas as claimed in claim 1 .
5. A gas turbine engine comprising:
a gas exhaust nozzle as claimed in claim 4 .
6. The duct as claimed in claim 1 , wherein the upstream and downstream transverse walls are in contact with the inner wall.
7. The duct as claimed in claim 6 , wherein the upstream and downstream transverse walls are in sliding contact with the inner wall.
8. The duct as claimed in claim 1 , wherein the at least one resonance cavity is a single cavity with a plurality of openings.
9. The duct as claimed in claim 1 , further comprising stiffeners placed transversely between the outer wall and the inner wall which stiffen the duct.
10. The duct as claimed in claim 2 , wherein the number of holes per unit of surface area of the wall reduces by between 5% and 10% between the upstream end and the downstream end of the duct.
11. The duct as claimed in claim 1 , wherein the duct extends generally along an axis, and a transverse distance between successive holes reduces continuously along the gas path from upstream to downstream.
12. The duct as claimed in claim 11 , wherein the axis is curvilinear.
13. The duct as claimed in claim 11 , wherein the axis is rectilinear.