Acoustic processing structure particularly adapted to the air inlet of an aircraft nacelle

1. An acoustic treatment structure for a leading edge onto which an aerodynamic stream flows, from the outside to the inside, comprising:

at least one acoustically resistive substructure ( 30 ),

at least one alveolar substructure comprising strips ( 32 ) of cells, arranged in a direction that is essentially perpendicular to the direction of flow of the aerodynamic stream, and

at least one reflective layer ( 34 ),

wherein each strip ( 32 ) of cells comprises

i) a first support part ( 36 ) with a U-shaped cross-section in the longitudinal direction, and an open surface that is opposite to the bottom of the U shape, the open surface flattened against the acoustically resistive substructure ( 30 ), the first support part ( 36 ) made in one piece that obtains boxes that are airtight relative to one another, the first support part ( 36 ) delimiting a space within the U shape and the acoustically resistive substructure ( 30 ), and

ii) at least a second partitioning part ( 38 ) partitioning the space delimited by the support ( 36 ) and the acoustically resistive substructure ( 30 ) into cells,

wherein each strip ( 32 ) of cells is displaced from an adjacent strip ( 32 ) of cells by a predetermined distance to form a plurality of flexibility regions on the acoustically resistive substructure ( 30 ) arranged longitudinally between the strips ( 32 ) of cells,

wherein the acoustic treatment structure is constructed and arranged to conform to a shape of the leading edge by flexing along the flexibility regions of the acoustically resistive structure ( 30 );

wherein the two U-shaped branches of the support part ( 36 ) comprise—at their distal ends of the base—a flange ( 39 ) that offers a support surface that can be flattened against the acoustically resistive substructure ( 30 ).

2. Acoustic treatment structure according to claim 1 , wherein the support parts ( 36 ) of the strips are connected to the acoustically resistive substructure ( 30 ).

3. Acoustic treatment structure according to claim 1 , wherein the partitioning part ( 38 ) comprises a plate ( 40 ) whose shapes make it possible to alternately connect the side walls of the support ( 36 ) in a U, arranged perpendicularly to the bottom of the support part ( 36 ).

4. Acoustic treatment structure according to claim 1 ,

wherein the acoustically resistive substructure ( 30 ) comprises plural layers comprised of i) at least one resistive layer that comprises microperforations and ii) at least one structural layer that comprises filled zones for taking up stresses delimiting openings ( 46 ) that release microperforations of the resistive layer, and

wherein the strips ( 32 ) are attached to the acoustically resistive substructure ( 30 ) so as to make the spacing between the strips ( 32 ) coincide with a filled zone.

5. Acoustic treatment structure according to claim 4 ,

wherein the at least one resistive layer is disposed between the at least one structural layer and the at least one alveolar substructure,

wherein the filled zones are non-perforated and arranged in a plurality of strips, a first series of the plurality of strips being arranged in a first direction, a second series of the plurality of strips being arranged in a second direction perpendicular to the first direction, at least some of the first series of the plurality of strips coinciding with the plurality of flexibility regions on the acoustically resistive substructure ( 30 ),

wherein each opening ( 46 ) is defined by two strips from the first series of the plurality of strips and two strips from the second series of the plurality of strips.

6. Acoustic treatment structure according to claim 1 , wherein the acoustically resistive substructure ( 30 ) comprises channels ( 48 ) that are designed for the hot air of a defrosting system.

7. Acoustic treatment structure according to claim 6 , wherein the channels ( 48 ) are disposed along the plurality of flexibility regions between adjacent strips ( 32 ) of cells.

8. Aircraft nacelle comprising an air intake that comprises—at at least one part of its surface—an acoustic treatment structure according to claim 1 .

9. Acoustic treatment structure according to claim 1 , wherein the support parts ( 36 ) of the strips are connected to the acoustically resistive substructure ( 30 ).

10. An acoustic treatment structure for a leading edge onto which an aerodynamic stream flows, from the outside to the inside, comprising:

an acoustically resistive substructure ( 30 );

at least one alveolar substructure comprising plural strips ( 32 ) of cells, arranged in a direction essentially perpendicular to a direction of flow of the aerodynamic stream, the strips ( 32 ) of cells being insulated with respect to one another so as not to allow a flow of air between two points that are spaced in a longitudinal direction and are provided in two different strips; and

a reflective layer ( 34 ),

wherein each strip ( 32 ) of cells comprises

i) a support part ( 36 ) with a one-piece U-shaped cross-section in the longitudinal direction, and an open surface that is opposite to a bottom of the U shape, the open surface connected against the acoustically resistive substructure ( 30 ), the support part ( 36 ) made in one piece that obtains boxes that are airtight relative to one another, the support part ( 36 ) delimiting a space within the U shape and the acoustically resistive substructure ( 30 ), and

ii) a partitioning part ( 38 ) partitioning the space delimited by the support ( 36 ) and the acoustically resistive substructure ( 30 ) into acoustic cells, and

wherein the reflective layer ( 34 ) is located on the bottom of the U shape,

wherein each strip ( 32 ) of cells is displaced from an adjacent strip ( 32 ) of cells by a predetermined distance to form a plurality of flexibility regions on the acoustically resistive substructure ( 30 ) arranged longitudinally between the strips ( 32 ) of cells,

wherein the acoustic treatment structure is constructed and arranged to conform to a shape of the leading edge by flexing along the flexibility regions of the acoustically resistive structure ( 30 );

wherein each support part ( 36 ) is independent from the other support parts ( 36 ) and not in contact with each other,

wherein each support part ( 36 ) comprises a flange ( 39 ) connecting the open surface against the acoustically resistive substructure ( 30 ).

11. The acoustic treatment structure of claim 10 , wherein,

each support part ( 36 ) connected with an adjacent support part ( 36 ), and

adjacent support parts ( 36 ) sharing a flange ( 39 ) connecting the open surface against the acoustically resistive substructure ( 30 ).

12. The acoustic treatment structure of claim 10 , wherein the partitioning part ( 38 ) comprises a corrugated plate ( 40 ) extending in the longitudinal plane so as to delimit the acoustic cells within side walls of the support part ( 36 ).

13. The acoustic treatment structure of claim 10 , wherein the partitioning part ( 38 ) comprises a castellated form ( 40 ) extending in the longitudinal plane so as to delimit the acoustic cells within side walls of the support part ( 36 ).

14. The acoustic treatment structure of claim 10 , wherein the partitioning part ( 38 ) comprises a saw-tooth-shape ( 40 ) extending in the longitudinal plane so as to delimit the acoustic cells within side walls of the support part ( 36 ).

15. The acoustic treatment structure of claim 10 , wherein the partitioning part ( 38 ) comprises plural walls independent of each other and each wall defining a cylinder ( 40 ), the plural walls defining plural cylinders ( 40 ) arranged one behind another.

16. The acoustic treatment structure of claim 10 , in combination with an aircraft nacelle.

17. The acoustic treatment structure of claim 10 ,

wherein the acoustically resistive substructure ( 30 ) comprises plural layers comprised of i) at least one resistive layer that comprises microperforations and ii) at least one structural layer that comprises filled zones for taking up stresses delimiting openings ( 46 ) that release microperforations of the resistive layer, and

wherein the strips ( 32 ) are attached to the acoustically resistive substructure ( 30 ) so as to make the spacing between the strips ( 32 ) coincide with a filled zone,

wherein the at least one resistive layer is disposed between the at least one structural layer and the at least one alveolar substructure,

wherein the filled zones are non-perforated and arranged in a plurality of strips, a first series of the plurality of strips being arranged in a first direction, a second series of the plurality of strips being arranged in a second direction perpendicular to the first direction, at least some of the first series of the plurality of strips coinciding with the plurality of flexibility regions on the acoustically resistive substructure ( 30 ),

wherein each opening ( 46 ) is defined by two strips from the first series of the plurality of strips and two strips from the second series of the plurality of strips.

18. The acoustic treatment structure of claim 10 ,

wherein the acoustically resistive substructure ( 30 ) comprises channels ( 48 ) that are designed for the hot air of a defrosting system,

wherein the channels ( 48 ) are disposed along the plurality of flexibility regions between adjacent strips ( 32 ) of cells.