Acoustic absorption structure comprising compartmentalized cells combining several types of resonators

Abstract

Acoustic absorption structure comprising compartmentalized cells combining several types of resonators. The invention relates to an acoustic absorption structure comprising a honeycomb structure (62), interposed between an acoustically resistive layer (64) and a reflective layer (66), which includes walls (68) delimiting cells (70) and, for at least one cell (70): at least one and at most three L-shaped partitions (72, 72'), impermeable and spaced apart, which delimit a straight compartment (70.1) and at least one L-shaped compartment (70.2, 70.3), in each L-shaped compartment (70.2, 70.3), an inclined acoustically resistive porous partition (80, 80') which has an openness ratio less than or equal to 15% and divides the L-shaped compartment (70.2, 70.3) into first and second zones (80.1, 80.2, 80.1', 80.2') forming two types of resonators. This arrangement increases the frequency range of the processed acoustic waves.The invention also relates to an aircraft comprising at least one such acoustic absorption structure. Figure 7.

Description

Title of the invention: Acoustic absorption structure comprising compartmentalized cells combining several types of resonators

[0001] The present application relates to a sound absorption structure comprising compartmentalized cells combining several types of resonators and to an aircraft comprising at least one such sound absorption structure.

[0002] According to one configuration, an aircraft propulsion system comprises a nacelle and a turbofan engine positioned inside the nacelle, which has, at the rear, a primary exhaust duct through which the exhaust gases from combustion are discharged. This primary exhaust duct includes, on its surface, a sound-absorbing structure to attenuate noise across several frequency bands, such as combustion noise (300-1000 Hz) and turbine operation noise (greater than or equal to 4000 Hz).

[0003] According to a first embodiment of the prior art, a sound-absorbing structure comprises at least one honeycomb structure positioned between an acoustically resistive (porous) layer in contact with a medium in which acoustic waves propagate and a reflective (impermeable) layer. The honeycomb structure comprises a multitude of tubular cells, each closed at one end by the acoustically resistive layer and at the other end by the reflective layer. These cells are not compartmentalized and are configured to generally target a single resonant frequency depending on the cell height. This first embodiment makes it possible to obtain a resonator suitable for attenuating sound waves with high frequencies.

[0004] This first embodiment is not entirely satisfactory because it only allows processing a small range of frequencies.

[0005] According to a second embodiment of the prior art, a sound-absorbing structure comprises first and second honeycomb structures positioned between an acoustically resistive layer in contact with a medium in which acoustic waves propagate and a reflective layer. This sound-absorbing structure includes an acoustically resistive porous partition interposed between the first and second honeycomb structures, the first honeycomb structure being interposed between the acoustically resistive layer and the acoustically resistive porous partition, and the second honeycomb structure being interposed between the reflective layer and the acoustically resistive porous partition.

[0006] This second embodiment makes it possible to obtain two types of resonators, a first Helmholtz type resonator at the level of the cells of the first alveolar structure, adapted to attenuate low frequency sound waves, as well as a second % wave type resonator at the level of the cells of the second alveolar structure, adapted to attenuate high frequency sound waves.

[0007] Although this second embodiment allows for a wider range of frequencies of the acoustic waves treated, it is not entirely satisfactory because the acoustic absorption structure has a significant thickness.

[0008] According to a third embodiment of the prior art illustrated in [Fig.1] and described in document EP2466095, an acoustic absorption structure comprises a plurality of bent cells 10, each bent cell 10 having a first compartment 10.1 which extends in a first direction between an acoustically resistive layer 12 in contact with a medium in which acoustic waves propagate and an acoustically resistive porous partition 14, substantially parallel to the acoustically resistive layer 12, and a second compartment 10.2 which extends in a second direction substantially perpendicular to the first direction between the acoustically resistive porous partition 14 and a reflective layer 16.

[0009] This third embodiment, like the second, allows for two types of resonators and broadens the frequency range of the treated acoustic waves. Although the use of angled cells 10 reduces the thickness of the acoustic absorption structure compared to the second embodiment, this third embodiment is not entirely satisfactory because the surface density at the cells is relatively low.

[0010] According to a fourth embodiment of the prior art illustrated in [Fig.2], the cells 20 of an acoustic absorption structure are positioned between an acoustically resistive layer 22 in contact with a medium in which acoustic waves propagate and a reflective layer 24. Each cell 20 comprises an inclined partition 26, porous at least in one area, dividing the cell 20 into two compartments 20.1, 20.2.

[0011] Like the second and third embodiments, this fourth embodiment makes it possible to obtain in each cell 20 two types of resonators and to broaden the range of frequencies of the acoustic waves treated.

[0012] According to a fifth embodiment of the prior art shown in [Fig. 3], the cells 30 of a sound-absorbing structure are positioned between an acoustically resistive layer 32 in contact with a medium in which acoustic waves propagate and a reflective layer 34. Each cell 30 comprises six V-shaped partitions 36 delimiting six angled compartments 30.1 to 30.6 and one compartment 30.7. Each angled compartment 30.1 to 30.6 comprises an acoustically resistive porous partition 38 dividing the angled compartment 30.1 to 30.6 into two zones.

[0013] Given the small surface area of ​​the acoustically resistive porous partition 38 and the minimum cross-sectional area of ​​the holes passing through it, regardless of their manufacturing method, each acoustically resistive porous partition 38 has a relatively high openness ratio, on the order of 20%. Unlike the second, third, and fourth embodiments, the acoustically resistive porous partitions 38 do not allow for two types of resonators to be obtained in the different angled compartments 30.1 to 30.6 due to their excessively high openness ratio.

[0014] Regardless of the prior art embodiment, there is a need to broaden the range of frequencies of the acoustic waves being treated.

[0015] For this purpose, the invention relates to an acoustic absorption structure comprising an acoustically resistive layer, a reflective layer and an alveolar structure interposed between the acoustically resistive layer and the reflective layer, said alveolar structure comprising a first face in contact with the acoustically resistive layer, a second face in contact with the reflective layer and walls parallel to a longitudinal direction which delimit cells each opening at the level of the first and second faces.

[0016] According to the invention, the alveolar structure comprises, for at least one cell: a. at least one and at most three L-shaped bulkheads, impermeable and spaced apart, each having first and second wings connected by a junction line, respectively substantially parallel to the longitudinal direction and perpendicular to the longitudinal direction, and delimiting a straight compartment and at least one L-shaped compartment, b. in each L-shaped compartment, an inclined acoustically resistive porous partition which has an openness rate of less than or equal to 15% and splits the L-shaped compartment into first and second zones forming two types of resonators.

[0017] By providing a limited number of L-shaped partitions, each inclined acoustically resistive porous partition has a sufficiently large surface area to allow for an openness ratio of less than 20%, thus enabling two types of resonators to be obtained in each of the first and second L-shaped compartments. Furthermore, the use of L-shaped compartments increases the distance traveled by acoustic waves within these compartments between the acoustically resistive layer and the resistive layer, while limiting the thickness of the honeycomb structure.

[0018] This solution makes it possible to increase the range of frequencies of the acoustic waves processed.

[0019] According to another feature, the various acoustically resistive porous partitions connect the different junction lines of the different L-shaped partitions, one of the acoustically resistive porous partitions being tangent to the second face of the honeycomb structure.

[0020] According to another feature, each cell comprises two L-shaped partitions delimiting a straight compartment and two L-shaped compartments.

[0021] According to another feature, the second wing of the first L-shaped partition and the acoustically resistive layer are separated by a first distance, the second wing of the second L-shaped partition and the reflective layer are separated by a second distance, and the second wings of the first and second L-shaped partitions are separated by a third distance. In addition, each cell has a cell height; the first, second, and third distances being between 25% and 40% of the cell height.

[0022] According to another characteristic, the first, second and third distances are substantially equal to each other.

[0023] According to another feature, the first wing of the first L-shaped partition and the wall are separated by a first maximum distance, the first wing of the second L-shaped partition and the wall are separated by a second maximum distance, and the first wings of the first and second L-shaped partitions are separated by a third maximum distance. In addition, each cell has a cell diameter; the first, second, and third maximum distances being between 25% and 40% of the cell diameter.

[0024] According to another characteristic, the first, second and third maximum distances are substantially equal to each other.

[0025] The invention also relates to an aircraft comprising at least one sound-absorbing structure according to one of the preceding characteristics.

[0026] Other features and advantages will become apparent from the following description of the invention, given by way of example only, with reference to the accompanying drawings, among which:

[0027] [Fig. 1] is a schematic representation of a cell of a sound-absorbing structure illustrating an embodiment of the prior art,

[0028] [Fig.2] is a schematic representation of a cell of an absorption structure acoustics illustrating another mode of realization of the earlier art,

[0029] [Fig.3] is a schematic representation of a cell of an absorption structure acoustics illustrating another mode of realization of the earlier art,

[0030] [Fig.4] is a side view of an aircraft,

[0031] [Fig.5] is a longitudinal section of part of a propulsion assembly,

[0032] [Fig.6] is a schematic perspective representation of a cell of a acoustic absorption structure illustrating an embodiment of the invention,

[0033] [Fig.7] is a schematic cross-section of the cell visible in [Fig.6],

[0034] [Fig.8] is a perspective section of a cell of an absorption structure acoustics illustrating one embodiment of the invention,

[0035] [Fig.9] is a diagram showing acoustic attenuation curves obtained at starting from the compartments of a cell of a sound absorption structure according to the invention.

[0036] In [Fig.4], an aircraft 40 is shown which has a fuselage 42, two wings 44 arranged on either side of the fuselage 42 and propulsion assemblies 46 fixed under the wings 44. Each propulsion assembly 46 comprises a nacelle 48 and a turbomachine 50 positioned inside the nacelle 48.

[0037] According to an embodiment visible in [Fig.5], the turbomachine 50 includes, at the rear, a primary ejection conduit 52, through which exhaust gases escape from the turbomachine 50, which is delimited on the outside by an outer wall 54 and on the inside by an inner wall 56 extended by a nozzle cone 58.

[0038] According to one configuration, the outer and inner walls 54, 56 each comprise at least one sound-absorbing structure 60.

[0039] Each acoustic absorption structure 60 comprises an outer surface SE in contact with a medium in which acoustic waves propagate and an inner surface SI opposite to the outer surface SE.

[0040] Although described as applied to a primary ejection duct 52, the invention is not limited to this application. Thus, the acoustic absorption structure 60 can be positioned on any wall that has an external surface SE in contact with a medium in which sound waves propagate.

[0041] Each sound-absorbing structure 60 comprises at least one honeycomb structure 62 interposed between an acoustically resistive layer 64 permeable to sound waves and a reflective layer 66 impermeable to sound waves. The acoustically resistive layer 64 has a first face 64.1 corresponding to the outer surface SE and a second face 64.2 oriented towards and connected to the honeycomb structure 62. The reflective layer 66 has a first face 66.1 corresponding to the inner surface SI and a second face 66.2 oriented towards and connected to the honeycomb structure 62.

[0042] The acoustically resistive layer 64, the reflective layer 66, the connection between the acoustically resistive layer 64 and the alveolar structure 62, and the connection between the reflective layer 66 and the alveolar structure 62 are not further described as they may be identical to those of the prior art.

[0043] The honeycomb structure 62 extends between a first face 62.1 in contact with the acoustically resistive layer 64 and a second face 62.2 in contact with the reflective layer 66 and comprises a multitude of walls 68 which each have first and second edges positioned respectively at the level of the first and second faces 62.1, 62.2. These walls 68 are configured to delimit cells 70 which each open at the level of the first and second faces 62.1, 62.2.

[0044] According to one embodiment, the walls 68 are tubular and parallel to a longitudinal direction DL. According to another configuration, the walls 68 are cylindrical.

[0045] According to an arrangement, each cell 70 has a cell diameter D70 between 9.6 and 19.1 mm and a cell height H70 between 30 and 70 mm.

[0046] For at least one cell, the alveolar structure 62 comprises at least one L-shaped partition 72 which has a first wing 74 substantially parallel to the longitudinal direction DL and a second wing 76 substantially perpendicular to the longitudinal direction DL. Each L-shaped partition 72 is impermeable.

[0047] For each L-shaped partition 72, the first wing 74 is substantially rectangular and has a first transverse edge 74.1 located at the level of the first face 62.1, a second transverse edge 74.2 substantially parallel to the first transverse edge 74.1 and connected to the second wing 76, as well as first and second longitudinal edges 74.3, 74.4 parallel to each other and connected to the wall 68. The second wing 76 comprises a first straight edge 76.1 connected to the second transverse edge 74.2 at a junction line 78 and a second curved edge 76.2 connected to the wall 68.

[0048] The L-shaped partition 72 delimits a straight compartment 70.1 empty delimited by a part of the acoustically resistive layer 64, the first and second wings 74, 76 of the L-shaped partition 72 as well as a part of the wall 68, said straight compartment 70.1 forming a % wave resonator adapted to attenuate sound waves with high frequencies.

[0049] The cell 70 includes at least one L-shaped compartment 70.2 separated from the right-hand compartment 70.1 by the L-shaped partition 72.

[0050] The honeycomb structure 62 comprises, for each L-shaped compartment 70.2, an inclined acoustically resistive porous partition 80, positioned within the L-shaped compartment 70.2 and dividing it into first and second zones 80.1, 80.2 located on either side of the acoustically resistive porous partition 80. This acoustically resistive porous partition 80 has an openness ratio of 15% or less, preferably 10% or less. Thus, the first and second zones 80.1, 80.2 form two types of resonators: a first Helmholtz-type resonator adapted to attenuate low-frequency sound waves, and a second resonator of the % wave type adapted to attenuate high-frequency sound waves.

[0051] According to one embodiment, the honeycomb structure 62 comprises at most three L-shaped partitions spaced apart from each other.

[0052] Ideally, the alveolar structure 62 comprises: a. two L-shaped partitions 72, 72' spaced apart, as illustrated in figures 6 to 8, delimiting an empty straight compartment 70.1 as well as the first and second L-shaped compartments 70.2, 70.3, b. and, for each of the first and second compartments in L 70.2, 70.3, an acoustically resistive porous partition 80, 80' inclined, one in each compartment in L 70.2, 70.3, dividing each into first and second zones 80.1, 80.2, 80.1', 80.2' situated on either side of the acoustically resistive porous partition 80, 80'.

[0053] According to one configuration, the various acoustically resistive porous partitions 80, 80' inclined are coplanar and connected to the various junction lines 78 of the various L-shaped partitions 72, 72', one of the acoustically resistive porous partitions 80' inclined being tangent to the second face 62.2 of the alveolar structure 62.

[0054] The second wing 76 of the first partition in L 72 and the acoustically resistive layer 64 are separated by a first distance DI substantially equal to a second distance D2 separating the second wing 76 of the second partition in L 72' and the reflective layer 66. The second wings 76 of the first and second partitions in L 72, 72' are separated by a third distance D3 substantially equal to the first and second distances D1, D2.

[0055] The first, second and third distances Dl, D2, D3 are between 25% and 40% of the cell height H70 of cell 70.

[0056] The first wing 74 of the first L-shaped partition 72 and the wall 68 are separated by a first maximum distance DM1 substantially equal to a second maximum distance DM2 separating the first wing 74 of the second L-shaped partition 72' and the wall 68. The first wings 74 of the first and second L-shaped partitions 72, 72' are separated by a third maximum distance DM3 substantially equal to the first and second maximum distances DM1, DM2.

[0057] The first, second and third maximum distances DM1, DM2, DM3 are between 25% and 40% of the cell diameter D70 of cell 70.

[0058] According to one configuration, the acoustically resistive layer 64 has a substantially constant opening ratio at the cell 70. Alternatively, the acoustically resistive layer 64 may have a non-constant opening ratio at the cell 70. For example, the areas at the right compartment 70.1 and the first and second compartments in L 70.2, 70.3 may have different opening ratios from one area to another.

[0059] Each of the inclined acoustically resistive porous partitions 80, 80' has a substantially constant openness ratio. Alternatively, at least one inclined acoustically resistive porous partition 80, 80' may have a non-constant openness ratio.

[0060] The invention makes it possible to obtain several types of resonators in a low-height cell 70. By providing a limited number of partitions in L 72, at most three, it is possible to obtain a surface area for each acoustically resistive porous partition 80, 80' inclined sufficiently large to allow for an opening rate of less than 20%, which makes it possible to obtain two types of resonators in each of the first and second compartments in L 70.2, 70.3.

[0061] Finally, providing compartments in L 70.2, 70.3 makes it possible to increase the distance traveled by the acoustic waves in the latter between the acoustically resistive layer 64 and the resistive layer 66. The different compartments in L 70.2, 70.3 being nested one inside the other, they have different lengths, which contributes to increasing the range of frequencies of the acoustic waves treated.

[0062] In the case of a cell 70 with a cell height H70 of approximately 40 mm, the distance traveled by the acoustic waves is approximately 15 mm in the right-hand compartment 70.1, approximately 30 mm in the first L-shaped compartment 70.2, and approximately 57.5 mm in the second L-shaped compartment 70.3. As illustrated in [Fig. 9], the right-hand compartment 70.1 provides acoustic wave attenuation that follows a first curve 84.1 with a peak at a frequency of approximately 2.55 kHz. The first L-shaped compartment 70.2 provides acoustic wave attenuation that follows a second curve 84.2 with a peak at a frequency of approximately 1.45 kHz. Finally, the second compartment in L 70.3 allows for an attenuation of acoustic waves which follows a third curve 84.3 presenting a peak for a frequency of the order of 0.75 kHz.

Claims

Demands

1. Acoustic absorption structure comprising an acoustically resistive layer (64), a reflective layer (66) and a honeycomb structure (62) interposed between the acoustically resistive layer (64) and the reflective layer (66), said honeycomb structure (62) comprising a first face (62.1) in contact with the acoustically resistive layer (64), a second face (62.2) in contact with the reflective layer (66) and walls (68) parallel to a longitudinal direction (DL), delimiting cells (70) which each open at the level of the first and second faces (62.1, 62.2), characterized in that the honeycomb structure (62) comprises, for at least one cell (70): a.at least one and at most three L-shaped partitions (72, 72'), impermeable and spaced apart, each having first and second wings (74, 76) connected by a junction line (78), respectively substantially parallel to the longitudinal direction (DL) and perpendicular to the longitudinal direction (DL), and delimiting a straight compartment (70.1) and at least one L-shaped compartment (70.2, 70.3), b. in each L-shaped compartment (70.2, 70.3), an acoustically resistive porous partition (80, 80') inclined which has an openness ratio less than or equal to 15% and splits the L-shaped compartment (70.2, 70.3) into first and second zones (80.1, 80.2, 80.1', 80.2') forming two types of resonators.

2. Acoustic absorption structure according to claim 1, characterized in that the various acoustically resistive porous partitions (80, 80') connect the various junction lines (78) of the various L-shaped partitions (72, 72'), one of the acoustically resistive porous partitions (80') being tangent to the second face (62.2) of the honeycomb structure (62).

3. Acoustic absorption structure according to any one of the preceding claims, characterized in that each cell (70) comprises two L-shaped partitions (72, 72') delimiting a straight compartment (70.1) and two L-shaped compartments (70.2, 70.3).

4. Acoustic absorption structure according to the preceding claim, characterized in that the second wing (76) of the first L-shaped partition (72) and the acoustically resistive layer (64) are separated by a first distance (D1), in that the second wing (76) of the second L-shaped partition (72') and the reflective layer (66) are separated by a second distance (D2), in that the second wings (76) of the first and second L-shaped partitions (72, 72') are separated by a third distance (D3) and in that each cell (70) has a cell height (H70); the first, second and third distances (D1, D2, D3) being between 25% and 40% of the cell height (H70) of the cell (70).

5. Acoustic absorption structure according to the preceding claim, characterized in that the first, second and third distances (D1, D2, D3) are substantially equal to each other.

6. Acoustic absorption structure according to any one of claims 3 to 5, characterized in that the first wing (74) of the first L-shaped partition (72) and the wall (68) are separated by a first maximum distance (DM1), in that the first wing (74) of the second L-shaped partition (72') and the wall (68) are separated by a second maximum distance (DM2), in that the first wings (74) of the first and second L-shaped partitions (72, 72') are separated by a third maximum distance (DM3) and in that each cell (70) has a cell diameter (D70); the first, second and third maximum distances (DM1, DM2, DM3) being between 25% and 40% of the cell diameter (D70) of the cell (70).

7. Acoustic absorption structure according to the preceding claim, characterized in that the first, second and third maximum distances (DM1, DM2, DM3) are substantially equal to each other.

8. Aircraft comprising at least one sound-absorbing structure according to one of the preceding claims.

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