초록 ▼

The invention provides a device for acoustical treatment of the noise emitted by a bypass turbojet comprising a primary cowl having in an outer surface an inner annular acoustic treatment panel and a secondary cowl including in an inner surface an outer annular acoustic treatment panel arranged faci

The invention provides a device for acoustical treatment of the noise emitted by a bypass turbojet comprising a primary cowl having in an outer surface an inner annular acoustic treatment panel and a secondary cowl including in an inner surface an outer annular acoustic treatment panel arranged facing the inner panel. The inner and outer panels include respective central panel portions facing each other and extending axially over a common predetermined length, the length of the central panel portions lying in the range one-fifth to four-fifths of the total length of the panels, and the ratio between the acoustic resistances of the central panel portions being not less than 2.

대표청구항 ▼

1. A device for acoustically treating the noise emitted by a bypass turbojet, the device comprising: a primary cowl for surrounding a central core of the turbojet and including an inner annular acoustic treatment panel placed in an outer surface of the primary cowl; anda secondary cowl surrounding t

1. A device for acoustically treating the noise emitted by a bypass turbojet, the device comprising: a primary cowl for surrounding a central core of the turbojet and including an inner annular acoustic treatment panel placed in an outer surface of the primary cowl; anda secondary cowl surrounding the primary cowl to co-operate therewith to define an annular channel for passing a cold flow from the turbojet, the secondary cowl including an outer annular acoustic treatment panel placed in an inner surface of the secondary cowl, the outer panel facing the inner panel and extending axially over a same length as the inner panel;wherein each of the inner and outer panels are subdivided to include respective central panel portions facing each other and extending axially over a common predetermined length, a length of the central panel portions being in a range of one-fifth to four-fifths of a total length of the panels, and a ratio of an acoustic resistance of the central panel portion of the outer panel to an acoustic resistance of the central panel portion of the inner panel being asymmetric and not less than 2. 2. The device according to claim 1, wherein the ratio between the acoustic resistance of the central panel portion of the outer panel to the acoustic resistance of the central panel portion of the inner panel is in the range of 2 to 9. 3. The device according to claim 1, wherein the acoustic resistance of the central panel portion of the inner panel is in a range of 0.3 ρc to 0.6 ρc. 4. The device according to claim 1, wherein the acoustic resistance of the central panel portion of the outer panel is in a range of 1 ρc to 2.5 ρc. 5. The device according to claim 1, wherein the inner and outer panels are subdivided to include respective upstream and downstream end portions disposed at opposite ends of the respective central portions, the central portions of the panels each comprising an upstream part and a downstream part. 6. The device according to claim 5, wherein a ratio of an acoustic resistance of the upstream end portion of the outer panel to an acoustic resistance of the upstream end portion of the inner panel is in a range of 1.5 to 3. 7. The device according to claim 5, wherein a ratio of an acoustic resistance of the downstream end portion of the outer panel to an acoustic resistance of the downstream end portion of the inner panel is in a range of 1.5 to 3. 8. The device according to claim 5, wherein: a ratio of an acoustic resistance of the upstream part of the central panel portion of the outer panel to an acoustic resistance of the upstream end portion of the outer panel is in a range of 0.6 to 2.5;a ratio of the acoustic resistance of the upstream part of the central panel portion of the outer panel to an acoustic resistance of the downstream part of the central panel portion of the outer panel is in a range of 0.4 to 2.5; anda ratio of the acoustic resistance of the upstream part of the central panel portion of the outer panel to an acoustic resistance of the downstream end portion of the outer panel is in a range of 0.6 to 2.5. 9. The device according to claim 5, wherein: a ratio of an acoustic resistance of the upstream part of the central panel portion of the inner panel to an acoustic resistance of the upstream end portion of the inner panel is in a range of 0.4 to 1;a ratio of the acoustic resistance of the upstream part of the central panel portion of the inner panel to an acoustic resistance of the downstream part of the central panel portion of the inner panel is in a range of 0.5 to 2; anda ratio of the acoustic resistance of the upstream part of the central panel portion of the inner panel to an acoustic resistance of the downstream end portion of the inner panel is in a range of 0.4 to 1. 10. The device according to claim 5, wherein an acoustic resistance of the end portions of the outer panel is in a range of 1 ρc to 1.8 ρc. 11. The device according to claim 5, wherein an acoustic resistance of the end portions of the inner panel is in a range of 0.5 ρc to 1 ρc. 12. The device according to claim 5, wherein each of the inner and outer acoustic treatment panels includes at least one cellular-structure core sandwiched between a solid skin and a perforated skin, the central panel portion of the inner panel having a single layer, the end portions of the inner panel having a single layer or two layers, and the end and central panel portions of the outer panel having two layers. 13. A bypass turbojet including an acoustic treatment device according to claim 1.