STRUCTURE ENSURING ATTENUATION OF ACOUSTIC WAVES AND THERMAL EXCHANGE

Abstract

A structure ensuring acoustic attenuation of a flow of a first fluid and heat exchange between a first fluid and a second fluid. The structure includes a first wall which is perforated, a second wall, and a plurality of intermediate walls extending between the first wall and the second wall. For each intermediate wall, there is a pipe intended to receive the second fluid and inscribed within the intermediate wall. Such a structure makes it possible to optimally integrate the acoustic wave attenuation function and the heat exchange function.

Claims

1. A structure providing acoustic attenuation of a flow of a first fluid and heat exchange between the first fluid and a second fluid, the structure comprising: a first wall which is perforated; a second wall; a plurality of intermediate walls extending between the first wall and the second wall; and for each of the intermediate walls, a pipe to receive a second fluid and inscribed within the intermediate wall, and wherein the pipe is located a distance from both the first wall and the second wall.

2. The structure according to claim 1, wherein each pipe has an elliptical profile.

3. A structure according to claim 1, wherein the structure comprises a partition wall integral with the intermediate wall and extending inside of the pipe and separating the pipe into two sub-pipes.

4. The structure according to claim 3, wherein the partition wall is a corrugated plate

5. The structure according to claim 3, wherein the partition wall has through holes connecting both sides of the partition wall.

6. An aircraft having a pod with an inner wall defining an air duct and where the inner wall comprises a structure according to claim 1, where the first wall is oriented toward an inside of the duct.

7. A structure providing acoustic attenuation of a flow of a first fluid and heat exchange between the first fluid and a second fluid, the structure comprising: a first wall which is perforated; a second wall; a plurality of intermediate walls extending between the first wall and the second wall; and for each of the intermediate walls, a pipe to receive a second fluid and inscribed within the intermediate wall, wherein the intermediate wall has a form of a double wall comprising two parallel walls extending between the first wall and the second wall and separated by a free space forming the pipe.

8. The structure according to claim 7, wherein the intermediate wall has a dividing wall which extends between the two parallel walls of the intermediate wall and which defines, at a level of the first wall, a chamber separated from the pipe by the dividing wall.

9. A structure according to claim 7, wherein the structure comprises a partition wall integral with the intermediate wall and extending inside of the pipe and separating the pipe into two sub-pipes.

10. The structure according to claim 9, wherein the partition wall is a corrugated plate.

11. The structure according to claim 9, wherein the partition wall has through holes connecting both sides of the partition wall.

12. The structure according to claim 9, wherein each partition wall has a part that extends beyond the first wall.

13. The structure according to claim 7, wherein each intermediate wall has a part that extends beyond the first wall.

14. The structure according to claim 7, wherein the structure has fins that extend along the first wall on a side opposite the pipe, and wherein each fin extends perpendicularly to the intermediate walls and is integral with the first wall.

15. An aircraft having a pod with an inner wall defining an air duct and where the inner wall comprises a structure according to claim 7, where the first wall is oriented toward an inside of the duct.

16. A structure providing acoustic attenuation of a flow of a first fluid and heat exchange between the first fluid and a second fluid, the structure comprising: a first wall which is perforated; a second wall; a plurality of intermediate walls extending between the first wall and the second wall; and for each of the intermediate walls, a pipe to receive a second fluid and inscribed within the intermediate wall, wherein the pipe is located a distance from both the first wall and the second wall, wherein the intermediate wall has a form of a double wall comprising two parallel walls extending between the first wall and the second wall and separated by a free space forming the pipe, wherein the structure comprises a partition wall integral with the intermediate wall and extending inside of the pipe and separating the pipe into two sub-pipes, and wherein the structure has fins that extend along the first wall on a side opposite the pipes, wherein each fin extends perpendicularly to the partition walls and wherein each fin is integral with the partition walls along which it is in contact.

Description

BRIEF DESCRIPTION OF DRAWINGS

[0025] Characteristics of the disclosure herein mentioned above, and other characteristics, will become more apparent from the following description of an embodiment, the description given with reference to the enclosed example figures, which include:

[0026] FIG. 1 shows a side view of a aircraft according to the disclosure herein;

[0027] FIG. 2 shows a perspective view of a structure according to a first embodiment of the disclosure herein;

[0028] FIG. 3 shows a perspective view of a structure according to a second embodiment of the disclosure herein;

[0029] FIG. 4 shows a perspective view of a structure according to a third embodiment of the disclosure herein;

[0030] FIG. 5 shows a perspective view of a structure according to a fourth embodiment of the disclosure herein;

[0031] FIG. 6 shows a perspective view of a structure according to a fifth embodiment of the disclosure herein; and

[0032] FIG. 7 shows a perspective view of a structure according to a sixth embodiment of the disclosure herein.

DETAILED DESCRIPTION

[0033] FIG. 1 shows an aircraft 10 which has a pod 20 inside of which is arranged a turbo engine. The inner wall of the pod 20 defines an air duct which passes through the turbo engine. Each of FIGS. 2 through 6 shows a structure that provides acoustic attenuation of a first fluid flowing along this structure and, heat exchange between the first fluid and a second fluid circulating inside of this structure.

[0034] In the description that follows, each structure is described as forming part of an inner wall of a pod 20 of an aircraft 10, but it can be used in another environment where it is necessary to attenuate the noise generated by the flow of a first fluid and to provide heat exchange between the first fluid and the second fluid.

[0035] FIG. 2 shows a structure 100 according to a first embodiment structure which has: [0036] a first wall 102 which is perforated; [0037] a second wall 104 located at a distance and, here, parallel to the first wall 102; [0038] a plurality of intermediate walls 106 extending between the first wall 102 and the second wall 104, here extending perpendicularly to the first wall 102 and to the second wall 104; and [0039] for each intermediate wall 106, a pipe 108 within the intermediate wall 106.

[0040] All the intermediate walls 106 are parallel to one another and thus create corridors 112 and the holes 110 in the first wall 102 ensure the passage between the outside of the first wall 102 and corridors 112.

[0041] In the case of FIG. 2, the pipes 108 are arranged at a distance from both the first wall 102 and of the second wall 104.

[0042] The intermediate walls 106 are made of a material of high thermal conductivity, such as a metallic material for example.

[0043] In the case of a flow of the first fluid in a duct, the first wall 102 is oriented toward the inside of the duct. The first fluid, which is here the air of the duct, flows along the first wall 102 and the holes 110 allow part of the air to penetrate into the corridors 112 and thereby attenuate acoustic waves generated by the flow of the air.

[0044] A second fluid, which can be oil for example, flows through the pipes 108 and the oil cools by heat exchange with the first fluid through the walls of the pipe 108 and intermediate walls 106.

[0045] The fact placing each pipe 108 at a distance from the first wall 102 limits the risks of damage to the pipes in the event of impacts on the first wall 102.

[0046] In the embodiment of the disclosure herein presented here, the structure 100 consists of or comprises a plurality of formed sections of substantially rectangular cross-section where the formed sections are secured to one other and where each pipe 108 is encapsulated between the two neighbouring walls of two adjacent formed sections.

[0047] The structure can be assembled by all appropriate techniques according to the materials implemented, such as brazing, welding, and bonding from preformed or extruded parts, for example.

[0048] The structure 100 ensures cross-current or parallel flow between the first fluid and the second fluid, in either a co-current or a counter-current flow configuration.

[0049] FIG. 3 shows a structure 200 according to a second embodiment that features the same elements as the structure 100 according to the first embodiment except in that the structure 200 has a partition wall 214 that separates each pipe 208 in two sub-pipes 208a-b. The partition wall 214 is also made of a material of high thermal conductivity. The partition wall 214 is integral with the intermediate wall 106 and extends it on the inside of the pipe 208. Such a partition wall 214 improves the heat exchange between the first fluid and the second fluid.

[0050] The structure 200 ensures cross-current or parallel flow between the first fluid and the second fluid, in either co-current or counter-current flow configurations.

[0051] FIG. 4 shows a structure 300 according to a third embodiment having the same elements as the structure 200 according to the second embodiment except in that each partition wall 314 has a part 316 that extends beyond the first wall 102, i.e. inside the duct in order ensure better heat exchange between the first fluid and the second fluid. Each part 316 is thus parallel to the partition wall 314 that it extends and to the pipes 208 of the structure 300. The structure 300 ensures cross-current or parallel flow between the first fluid and the second fluid, in either co-current or counter-current flow configurations.

[0052] FIG. 5 shows a structure 400 according to a fourth embodiment having the same elements as the structure 200 according to the second embodiment except that it has fins 416 that extend along the first wall 102 on the side opposite the pipes 208. Each fin 416 is also made of a material of high thermal conductivity. Each fin 416 extends perpendicularly to the separation walls 414 and to the first wall 102, and is integral with the partition walls 414 along which it is in contact. The structure 400 ensures a cross-current flow between the first fluid and the second fluid.

[0053] FIG. 6 shows a structure 500 according to a fourth embodiment having the same elements as the structure 100 according to the first embodiment except that it has fins 516 that extend along the first wall 102 on the side opposite the pipes 108. Each fin 516 is also made of a material of high thermal conductivity. Each fin 516 extends perpendicularly to the intermediate walls 106 and the first wall 102, and is integral with the first wall 102. The structure 500 ensures a cross-current flow between the first fluid and the second fluid.

[0054] In a preferred embodiment, each pipe 108, 208 has an elliptical and non-circular profile, in particular with a ratio between the length of the major axis and the length of the minor axis in the order of 4 to 1. When a partition wall 214, 314, 414 is present, the pipe 208 takes the shape of two half-ellipses 208a and 208b. The elliptical shape increases the useful heat exchange surface area while limiting the surface area that is not acoustically treated.

[0055] In the embodiment of the disclosure herein presented in FIGS. 2 through 6, the major axis is perpendicular to the first and second walls 102 and 104.

[0056] The intermediate walls 106 are deformed by the presence of the pipes 108 and 208 and these distortions create a narrowing of the corridors 112 at the level of the pipes 108 and 208.

[0057] The placement of pipes 108, 208 of elliptical cross-section allows greater fluid flow cross-sections to be obtained in relation to circular cross-sections having the same impact on the acoustic surface treatment, which limits hydraulic head losses.

[0058] The elliptic cross-sections also make it possible to boost the heat exchange coefficient particularly when the width of the corridor becomes small in comparison with its height.

[0059] The elliptical sections also make it possible to have a heat exchange surface area between the fluid and the intermediate walls 106, and this exchange surface area is further increased when a partition plate is integrated into the pipe.

[0060] To increase the contact surface of the fluid in the pipe 208, split into two sub-pipes 208a-b, the partition wall 214, 314, 414 can be a corrugated plate.

[0061] Whether the partition wall 214, 314, 414 is corrugated or flat, it can have through holes connecting both sides of the partition wall 214, 314, 414 to ensure better homogenisation of the temperature of the second fluid and participate in the creation of local turbulence increasing the heat exchange coefficient on the side of the second fluid thus the exchange in general.

[0062] In the examples illustrated in FIGS. 2 through 6, the pipes 108, 208 are centred at mid-height of the partition walls 106 but moving them towards the first wall 102 helps to minimize the thermal resistance related to the length between the first wall 102 and the walls of the pipes 108, 208.

[0063] FIG. 7 shows a structure 600 according to a fifth embodiment which has: [0064] a first wall 102 which is perforated; [0065] a second wall 104; [0066] a plurality of intermediate walls 606 extending between the first wall 102 and the second wall 104; and [0067] for each intermediate wall 606, a pipe 608 intended to receive a fluid and inscribed or defined within the intermediate wall 606.

[0068] All the intermediate walls 606 are parallel to one another and thus create corridors 112 and the holes 110 in the first wall 102 ensure the passage between the outside of the first wall 102 and corridors 112.

[0069] In the case of FIG. 7, the intermediate wall 606 takes the form of a double wall consisting of or comprising two parallel walls extending between the first wall 102 and the second wall 104 and separated by a free space forming the pipe 608. That is to say that the pipe 608 is arranged between the two walls forming the intermediate wall 606.

[0070] The intermediate wall 606 has a dividing wall 612 which extends between the two walls of the intermediate wall 606 and defines, at the level of the first wall 102, a chamber 610 separated from the pipe 608 by the dividing wall 612. The pipe 608 is thus separated from the first wall 102 and by the chamber 610 which is filled with air or empty. Thus, in case of very high mechanical loads or in the case of impact, the chamber 610 constitutes a barrier which prevents the first fluid from mixing with the second fluid, by absorbing a part of the deformation energy.

[0071] As with the previous embodiments, the structure 600 may have a partition wall 614, possibly corrugated and pierced, integral with the intermediate wall 606 and extending inside the pipe 608 to separate the pipe 608 into two sub-pipes. The partition wall 614 can be corrugated and/or pierced.

[0072] The structure 600 can also include fins in accordance with those of the embodiment shown in FIG. 6.

[0073] The structure 600 can also have fins 616 which are derived from an extension of the walls forming the intermediate wall 606 beyond the first wall 102. In other words, each wall forming the intermediate wall 606 has a part 616 that extends beyond the first wall 102.

[0074] While at least one exemplary embodiment of the invention(s) is disclosed herein, it should be understood that modifications, substitutions and alternatives may be apparent to one of ordinary skill in the art and can be made without departing from the scope of this disclosure. This disclosure is intended to cover any adaptations or variations of the exemplary embodiment(s). In addition, in this disclosure, the terms “comprise” or “comprising” do not exclude other elements or steps, the terms “a”, “an” or “one” do not exclude a plural number, and the term “or” means either or both. Furthermore, characteristics or steps which have been described may also be used in combination with other characteristics or steps and in any order unless the disclosure or context suggests otherwise. This disclosure hereby incorporates by reference the complete disclosure of any patent or application from which it claims benefit or priority.