WO2013050694A1 - Panneau d'atténuation acoustique structural - Google Patents
Panneau d'atténuation acoustique structural Download PDFInfo
- Publication number
- WO2013050694A1 WO2013050694A1 PCT/FR2012/052226 FR2012052226W WO2013050694A1 WO 2013050694 A1 WO2013050694 A1 WO 2013050694A1 FR 2012052226 W FR2012052226 W FR 2012052226W WO 2013050694 A1 WO2013050694 A1 WO 2013050694A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- acoustic
- skin
- acoustic structure
- panel according
- shell
- Prior art date
Links
Classifications
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K11/00—Methods or devices for transmitting, conducting or directing sound in general; Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/002—Devices for damping, suppressing, obstructing or conducting sound in acoustic devices
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K11/00—Methods or devices for transmitting, conducting or directing sound in general; Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/16—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/162—Selection of materials
- G10K11/168—Plural layers of different materials, e.g. sandwiches
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K11/00—Methods or devices for transmitting, conducting or directing sound in general; Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/16—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/172—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general using resonance effects
Definitions
- the present invention relates to an acoustic attenuation panel for a turbojet engine nacelle, to nacelle elements provided with such panels and to associated manufacturing processes.
- honeycomb-type acoustic absorption material commonly called “honeycomb” structure
- porous material structure usually comprise a structural honeycomb-type acoustic absorption material (commonly called “honeycomb” structure) or porous material structure.
- This acoustic absorption material is coated on its underside, that is to say not in contact with the air flow inside the nacelle, an inner skin impervious to air, called “ full "whose role is that of acoustic reflector.
- resistive "or” acoustic a perforated outer skin permeable to air, whose role is to dissipate acoustic energy.
- Such acoustic panels beyond their primary function must, in addition, have sufficient mechanical properties to transfer the forces, including aerodynamic they receive to the structural links of the nacelle, otherwise the risk of degrading the qualities of acoustic attenuation it offers.
- Acoustic attenuation panels in particular are known in which stiffeners and / or spacers are placed between the two skins of the panels concerned and / or one of the skins and the acoustic structure to ensure good structural strength of the panels. .
- spacers and / or stiffeners are most often distributed within the acoustic structure along the panel.
- Such defects are all the more present when the acoustic structure is complex, formed of one or more stacked and / or juxtaposed alveolar core blocks.
- the presence of the spacers within the acoustic structure affect the effective acoustic surface of the panels and the mass of the latter.
- Document FR 2 933 224 discloses, in addition, a panel in which a skin, not in contact with the acoustic structure, is autoraidie to ensure good structural strength of the panels.
- stiffeners are applied internally to the structure, the acoustic surface is reduced as well.
- An object of the present invention is therefore to provide an acoustic attenuation panel whose effective acoustic surface is optimized while respecting the structural properties to which such a panel must respond.
- Another object of the present invention is to provide an acoustic attenuation panel which makes it possible to absorb the stacking tolerances of complex acoustic structures.
- Another object of the present invention is to provide an acoustic attenuation panel that provides anti-corrosion protection to the acoustic structure that constitutes it, in a simple and effective manner.
- the subject of the present invention is an acoustic attenuation panel comprising the following main elements:
- an acoustic structure comprising an acoustic absorption material and disposed between the resistive skin and the solid skin
- the solid skin is structural and is configured to form at least one transverse spacer between the solid skin and the resistive skin of the sound attenuation panel.
- Spacer means an element suitable for:
- the present invention eliminates any spacer or reinforcement embedded in the acoustic structure, which promotes an increase in the effective acoustic surface of the panel relative to a sound attenuation panel of the prior art of the same dimensions.
- the acoustic structure is provided with a skin whose structural properties are sufficient to eliminate any use of structuring acoustic structure.
- acoustic holes are no longer clogging. It remains only to control the good peripheral bonding of the resistive skin on the shell with lower levels of requirement than in the prior art since the resistive skin is not considered as structural, hence a reduction of non conformities.
- the acoustic panel of the present invention makes it easier to mount the acoustic structure and the resistive skin on the solid skin, which ensures a good industrial feasibility, namely a speed of execution, a reduction in costs. of production to the extent that the assembly steps of the panel are extremely small compared to the prior art but also ease of maintenance and repair due to simplification of assembly of the panel concerned.
- the acoustic attenuation panel of the invention comprises one or more of the following optional features considered alone or according to all the possible combinations: -
- the solid skin is configured to form a transverse spacer between the solid skin and the resistive skin on either side of the acoustic structure, forming a receiving shell in the concavity of which is housed the acoustic structure;
- the solid skin comprises at least one return running along at least part of the periphery of the acoustic structure towards the resistive skin;
- the solid skin is formed at least in part by a double wall in which is formed a reinforcing structure
- the inner surface of the skin, facing the acoustic surface, has a roughness
- the acoustic structure is housed in the concavity of the shell by embedding;
- the acoustic structure is housed in the concavity of the shell, by compression, by means of elastic means and / or by means of mechanical fixing means;
- the elastic means comprises means for anchoring the acoustic structure
- these anchoring means comprise a corrugated acoustic structure and / or an acoustic structure having teeth on one and / or the other of these faces;
- the elastic means comprises drainage means at the interface between the acoustic structure and the solid skin, able to compress in the thickness;
- the elastic means comprises dampers extending from the surface of the acoustic structure facing a bearing surface of the solid skin and / or the resistive skin;
- the dampers are in the form of point bulbs of elastic material reported on the surface of the acoustic structure
- the present invention relates to a nacelle element comprising an acoustic panel according to the invention.
- FIGS. 1a to 1d are sectional views of a method of manufacturing a panel according to a first embodiment of the present invention
- FIGS. 2a to 2b, 3a to 3b, 4a, 5a, 6a, 6c, 7a to 7b, 8 are sectional views of other embodiments of the panel according to the present invention.
- FIGS. 4b, 5b, 6b are enlarged views, respectively zones A, B, C of FIGS. 4a, 5a, 6a. ;
- Fig. 9 is a sectional view of a solid skin of a panel according to another embodiment of the present invention.
- an acoustic attenuation panel With reference to FIGS. 1a to 1d, an acoustic attenuation panel
- 100 includes:
- an acoustic structure 130 comprising an acoustic absorption material and disposed between the resistive skin 1 10 and the full skin 120.
- the acoustic structure 130 may comprise a cellular structure formed of cells with cellular core or NIDA, as illustrated in these figures.
- it may comprise a porous material having acoustic absorption qualities to replace the nida.
- This porous material has an open structure, that is to say open cells able to absorb the energy of acoustic waves.
- foam-type material or in expanded form.
- This acoustic structure 130 may be acoustically distributed or not. It may comprise a single or multiple resonator, be formed of several layers of alveolar / porous or not, separated or not by septa.
- the acoustic structure 130 is formed of a distributed acoustic structure comprising a first and a second layer 131, 132 of superimposed cellular cells separated by a septum 133. cells of the two layers 131, 132 being identical or not.
- the resistive skin 1 10 in contact with the aerodynamic flow is, in turn, perforated multiple holes 1 1 1 positioned in a defined arrangement according to the desired acoustic attenuation.
- the solid skin 120 is structural and is configured to form at least one transverse spacer 121 between the solid skin 120 and the resistive skin 1 10 of the acoustic attenuation panel 100.
- the full skin 120 is configured to form a spacer 121, 122 transverse between the solid skin 120 and the resistive skin 1 10 on either side of the acoustic structure 130, thus forming a shell 123 for receiving the structure acoustic 130.
- the two spacers are formed by two set return interfaces 121, 122 on either side of the acoustic structure 130, at least partly along the periphery of the acoustic structure 130 towards the resistive skin 1 10 with which he is in punctual contact or not.
- these returns 121, 122 each have an inverted L shape, one of the branches 121a, 122a interfaces with the acoustic structure 130 and is extended by the other branch 122b, 123b which makes the interface with the resistive skin 1 10.
- the acoustic structure 130 is held in place by the returns
- the shell 123 forms an impression of the acoustic structure 130 that it houses and more particularly, the concavity of the shell 123 has a shape and dimensions adapted to receive the structure 130 associated acoustics.
- the shell bottom 123 comprises an internal return 124, in the direction of the acoustic structure 1 30, defining two depth levels for the corresponding shell 123, each respectively to the first and second layers 131, 132 of the corresponding acoustic structure 130.
- such a shell 123 makes it possible to absorb the stacking tolerances of the various layers of the complex acoustic structures 130.
- this full shell 123 is monolithic.
- the acoustic structure 130 and the resistive skin 1 10 are, for their part, non-structuring.
- the full skin 120 or shell 123 is, therefore, formed by a thermosetting material of composite type for example, by a thermoplastic material which can be reinforced or not or by a metallic material.
- the shell 123 may have an inner surface, in its concavity, smooth or rough depending on the material in which it is formed.
- a surface treatment of the shell 123 may be provided before placing the acoustic structure 130 in its concavity.
- a fabric to be delaminated may be removed at the time of installation of the acoustic structure 130, to obtain a gross internal surface of attachment of said structure 130.
- this hull In another variant embodiment illustrated in FIG. 9, this hull
- It incorporates reinforcements on all or part of its structure. More particularly, it may be formed at least in part by a double wall 126,126 'forming a space i in which a reinforcing structure 125 is put in place.
- the space i formed extends over a portion of the outer face of the shell portion 123 forming a bottom, opposite the concavity of the shell 123.
- this reinforcing structure 125 may be a honeycomb core structure.
- An alternative embodiment may also provide for reinforcing, in a similar manner, all or part of one or more returns 121, 122, 124 of the shell 123.
- the acoustic structure 123 is housed in the concavity of the shell 123, by compression, using:
- a first method of manufacturing the panel illustrated in Figures 1a to 1d is as follows.
- the acoustic structure 130 is put in place in the receiving shell 120, either by embedding or by deformation of the acoustic structure 130 or without deformation of the acoustic structure 130 in the event of fitting without play between the shell 123 and the acoustic structure 130.
- the respective length d, e of the first 131 and the second 132 layers of the acoustic structure 130 is greater than the length f, g of the housing. of the hull 123 intended to receive it, respectively, in its concavity, this in order to embed and block the different layers of the acoustic structure 130 in the shell 123.
- the acoustic structure 130 can be in simple contact with the shell 123 or, if necessary, in contact by a mechanical means of fixing such as adhesive deposition.
- the glue used may be any type of glue known to those skilled in the art.
- At least one ply 1 of glue may be deposited on the surface of the shell bottom 123 and / or the surface of the first layer 131 of the acoustic structure 130 in contact with this shell bottom 123 may be pre-glued and / or crosslinked.
- a septum 133 can be achieved by any suitable means.
- it can be achieved by pre-gluing the surface of the first layer 131 of the acoustic structure 130 in contact with the septum 133, followed by crosslinking.
- the 130 may be made similarly to the first layer 131.
- At least one ply of glue 2 can be deposited on the surface of the shell bottom 123 remained free after the establishment of the first layer 131 if necessary, and / or the surface of the second layer 132 of the acoustic structure 130 in contact with this bottom and septu m 133 where appropriate or the first acoustic layer 131.
- an adhesive deposit can be made on the surface of the second acoustic layer 132 facing the skin 1 10, in association or not with a glue deposit on the surface of the returns 121 b122b of the shell 123 opposite said resistive skin 1 10.
- the bonding is performed so as not to obstruct the acoustic holes, in order to avoid any limitation of the sound absorption.
- pressure is then exerted on the entire panel 100 and, more particularly, on the external surface of the shell 123, in order to make all the collages.
- the pressure can be exerted by any known device and can be gaseous or mechanical.
- these collages under pressure can be made, if necessary hot in an oven, or even cold.
- the acoustic assembly formed by the acoustic structure 130 and the resistive skin 1 10 may be preassembled, in particular but not exclusively as described previously with reference to FIGS. 1a to 1d, before any installation of the structure acoustic 130 in the hull 123.
- the acoustic structure and the shell have complementary shapes and dimensions allowing the fit-free fit of the acoustic structure 130 in the concavity of the shell 123 to be set without play, without deformation of the acoustic structure 130 .
- drainage means 10 of the acoustic panel 100 are placed in the bottom of the shell 123, thanks to the presence of a clearance between the acoustic set and hull bottom 123.
- These creasing means 1 0 also have elastic properties.
- these drainage means 10 may include, but are not limited to, one or more perforated rabbets, one or more embossed meshes, or one or more fibrous assemblies having entangled fibers, such as a felt.
- the drainage means 10 of the acoustic panel 100 are preferably used in a temperature environment of less than 100 ° C, they can be made in commercially available materials at low cost.
- a felt in particular, may be formed from a material chosen from felt materials incorporating as required by the person skilled in the art at least: the porosity of the felt, the tortuosity of the fibers, the aspect ratio, the average size of the fibers, the entanglement rate, which provides good elasticity in the thickness of the felt.
- This felt must have properties of resistance to water and fluids of any kind encountered in the aeronautics.
- the thickness of the felt is compatible with the desired compression value.
- the drainage means 10 are preferably placed in simple contact with the bottom of the shell 123 and the acoustic structure 130.
- the presence of the drainage means 10 allow pressure contact of the acoustic assembly on the shell 123.
- FIGS. 3a to 5b Three other embodiments are illustrated in FIGS. 3a to 5b.
- the acoustic structure 130 is made and recessed with play or without play in the shell 123 by simple contact. More particularly, no glue deposit takes place between the acoustic structure 130 and the shell 123, or between the different elements constituting the acoustic structure 130, namely between the different acoustic layers 131, 132 and between the different acoustic layers 131 , 132 and 133, where applicable.
- Gluing is replaced by anchoring means 20 by simple contact of the acoustic structure 130 in the shell 123.
- acoustic panels 100 are simplified by eliminating controlled atmosphere environments, protective clothing and reducing manufacturing steps, in the absence of the adhesive crosslinking steps.
- a first variant of the anchoring means 20 comprises an acoustic structure whose various acoustic layers 131, 132 are corrugated.
- Each corrugated acoustic structure 130 must correspond, at least, to the following characteristic: the deformation force of the acoustic structure 130 must be less than the stiffness of the corresponding acoustic panel 100, while ensuring an effective jamming of the acoustic structure 130 in the hull 123 of the panel.
- the characteristics of the corrugation namely in particular the length, the height, the deflection, the amplitude, the configuration of the undulation, are defined according to the desired shaping force, in particular by tests, experiments and / or calculations. .
- the arrow and the height of the acoustic structure 130 are defined so that a residual deformation remains of the acoustic structure 130 once the resistive skin 1 reported on said structure 130.
- the assembly of the panel is as follows.
- corrugated acoustic first layer 131 is successively put in place, the septum 133 if appropriate, the second corrugated acoustic layer 132 (FIG. 3a) and the resistive skin 11 in and against the shell 123 (FIG. 3b).
- a pressure (illuminated by arrows) is then exerted on the reinforcements 121, 122 of the shell 123 at the interface with the resistive skin 1 10 is on the entire shell 123, similar to the other embodiments described above.
- a second variant of the anchoring means 20 comprises an acoustic structure in which at least the face of the acoustic structure facing the shell 123 has teeth 21, in order to improve the anchoring of the acoustic structure 130 on this shell 123.
- These teeth 21 may be provided on the entire face or only on one or more parts thereof.
- the walls of the acoustic layers, and in particular cells with a cellular core opposite a septum 133 and / or resistive skin 1, 10 are also dentated.
- the teeth 21 are more or less marked, according to the choice of the skilled person and the desired adhesion of the acoustic structure 130 on the skins 1 10,120 opposite.
- the teeth 21 are shaped so as to minimize their contact surface with their bearing surface, namely, a skin 120, 10, a septum 133 or other.
- FIGS. 4a to 4b and 5a to 5b show two embodiments of the same embodiment of a toothed acoustic structure 21, the teeth of the embodiment of FIGS. 56a to 5b being thinner and sharper than those of FIG. embodiment of FIGS. 4a to 4b.
- the mounting of the panel 100 of the embodiments 4a and 5a is identical to that of Figures 3a to 3c.
- the pressure exerted on the shell 123 puts elastic stress in the acoustic structure 130 by deformation of the teeth 21, or even cells in the framework of alveolar acoustic structure 130.
- drainage means 10 at the bottom of the shell 123 before any acoustic structure 130 with teeth is placed in place.
- These drainage means 10 may be similar to those described in relation to FIGS. 2a to 2b.
- the walls of the acoustic layers 131, 132 facing the drainage means 10 may have teeth 21.
- the acoustic structure 130 comprises at least one surface facing the inner surface of the shell bottom 123 provided with elastic means 30.
- These elastic means 30 may be provided on the entire surface, only on one or more parts of the latter or punctually along the latter.
- the walls of the acoustic layers 131, 132 and in particular cells with a cellular core facing a septum 133 and / or resistive skin 1 10 are also provided with elastic means.
- These elastic means have a low amplitude elasticity which ensure the contact of the acoustic structure 130 under a slight stress at its interface with the shell 123 and, where appropriate, a septum 133 or the resistive skin 1 10.
- These elastic means 30 may comprise a deposit of elastic material such as the rubber, as shown in Figures 6a and 6b, or any other suitable elastic means reported or formed on the corresponding faces of the layers 131, 132 of the acoustic structure 130.
- the number, shape and arrangement of said elastic means are adapted by those skilled in the art, in particular to promote uniform contact of the acoustic structure 130 on these different supports.
- each acoustic layer comprises, on each of these faces, point deposits or bulbs 31 of elastic rubber on each of the cellular cells.
- This deposit can be achieved by dipping the acoustic structure 30 before forming the latter.
- each deposit of elastic material is adapted to allow crushing of the acoustic structure 130 under pressure of a few tenths of a mm.
- Such deposits offer, advantageously, a coherent contact surface between the acoustic structure 130 and the support concerned, notmmanet the acoustic skin 1 10, which results in insulation cells alveolar, where appropriate and ensures a performance optimal acoustics by eliminating any leakage between each cell and acoustic skin 1 10.
- such deposits form a protection against corrosion of the acoustic structure 130 of metal material, for example, by providing a seal to the faces of the latter on which they are present.
- the pressure exerted on the shell 123 puts elastic stress in the acoustic structure 130 by deformation of the bulbs 31, or even cells in the framework of cellular acoustic structure.
- the thickness of the acoustic structure 130 added to that of the elastic bulbs 31 must be greater than the depth of the shell 123 receiving the structure 130.
- An alternative embodiment can provide several types of elastic elements on the same face of the acoustic structure 130 or from one face to the other of the acoustic structure 130.
- FIGS. 7a and 7b Another embodiment is illustrated, in two variants, in FIGS. 7a and 7b.
- the acoustic structure 130 is kept in contact on the resistive skin 1 10 and in the shell 123, by compression, by means of mechanical fixing means 40.
- the fixing means are adapted to fix, between them, the shell 123 and the resistive skin 1 10, at the level of the lateral returns 121, 122 of the shell 123.
- an acoustic attenuation panel 100 is obtained, the acoustic effective surface of which is optimized by transferring to the shell interface 123 / resistive skin interface 1 10, the fixing links. Any obstruction of the acoustic holes of the acoustic structure 130 by the fastening means is avoided.
- the mechanical fastening means 40 comprise rivets 41 or bolts, fixing the resistive skin 1 to the branch 121 a, 122 b or 121 b, 122 b of the return 121, 122 of FIG. interface of the hull 123 facing.
- These rivets 41 cooperate with orifices provided on the returns and the resistive skin 1 10 adapted to be travsersés by the rivets 41.
- a peripheral return 11.1 13 of the resistive skin 1 10 in the direction of the acoustic structure 130 extending opposite a return 121 a, 122 a of the shell 123 defining the interface of the shell 123 and the acoustic structure 130, on the thickness of the acoustic structure 130.
- the return 1 12.1 13 peripheral is thus perpendicular to the base plane of the resistive skin 1 10.
- the resistive skin 1 10 and the shell 123 are thus fixed by their reinforcements placed side by side with a layer of the acoustic structure.
- the mechanical fixing means are formed by a material that is not necessarily structural as a function of the loadings and the temperature, it may be optionally of synthetic material or aluminum base.
- resilient means 30 may be associated with the mechanical fixing means 40.
- the mechanical fixing means comprise an expansive foam bonding of the acoustic structure 123 in the shell 123.
- the acoustic assembly with acoustic structure 130 and resistive skin 1 10, is formed by any suitable means, prior to the installation of the acoustic structure 130 in the receiving envelope that forms the hull 123.
- the various acoustic layers 131, 132 and the septa 133, if any, are precoated on the resistive skin 1 10.
- an expansive foam deposit 50 is made at the periphery of the acoustic structure 130.
- the acoustic assembly formed in the concavity of the shell 123 is placed. It should be noted that, in this frame, the dimensions of the acoustic structure 130 have been adapted to leave a clearance between the reinforcements 121, 122 of the cock 1 23 and the acoustic structure 1 30, this game is filled. by the expansive foam 50.
- the panel is subsequently polymerized by any suitable means. During the polymerization, the foam 50 is extended against the returns of the shell 123 and in the surrounding cells alveolar if the acoustic structure is nest egg.
- an acoustic panel is obtained in which the resistive skin 1 10 is glued to the shell and to the acoustic structure.
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- Engineering & Computer Science (AREA)
- Acoustics & Sound (AREA)
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- Soundproofing, Sound Blocking, And Sound Damping (AREA)
Abstract
Description
Claims
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201280048519.6A CN103858159A (zh) | 2011-10-04 | 2012-10-02 | 结构性声衰减板 |
EP12775807.6A EP2764510A1 (fr) | 2011-10-04 | 2012-10-02 | Panneau d'atténuation acoustique structural |
RU2014117115/28A RU2014117115A (ru) | 2011-10-04 | 2012-10-02 | Структурная звукопоглощающая панель |
CA2848248A CA2848248A1 (fr) | 2011-10-04 | 2012-10-02 | Panneau d'attenuation acoustique structural |
BR112014006561A BR112014006561A2 (pt) | 2011-10-04 | 2012-10-02 | elemento de nacela e painel de atenuação acústica estrutural do mesmo |
US14/243,326 US20140326536A1 (en) | 2011-10-04 | 2014-04-02 | Structural acoustic attenuation panel |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1158936A FR2980902B1 (fr) | 2011-10-04 | 2011-10-04 | Panneau d'attenuation acoustique structural |
FR11/58936 | 2011-10-04 |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US14/243,326 Continuation US20140326536A1 (en) | 2011-10-04 | 2014-04-02 | Structural acoustic attenuation panel |
Publications (1)
Publication Number | Publication Date |
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WO2013050694A1 true WO2013050694A1 (fr) | 2013-04-11 |
Family
ID=47071391
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/FR2012/052226 WO2013050694A1 (fr) | 2011-10-04 | 2012-10-02 | Panneau d'atténuation acoustique structural |
Country Status (8)
Country | Link |
---|---|
US (1) | US20140326536A1 (fr) |
EP (1) | EP2764510A1 (fr) |
CN (1) | CN103858159A (fr) |
BR (1) | BR112014006561A2 (fr) |
CA (1) | CA2848248A1 (fr) |
FR (1) | FR2980902B1 (fr) |
RU (1) | RU2014117115A (fr) |
WO (1) | WO2013050694A1 (fr) |
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JP5486640B2 (ja) * | 2012-06-08 | 2014-05-07 | 東海ゴム工業株式会社 | 振動部材取付構造 |
JP6484408B2 (ja) * | 2014-06-24 | 2019-03-13 | ニチアス株式会社 | 防音材、及び防音カバーの製造方法 |
FR3036307B1 (fr) * | 2015-05-22 | 2017-06-02 | Halcyon | Procede ameliore de fabrication d'une piece metallique du type sandwich presentant une forme non-developpable |
US9783316B2 (en) | 2015-06-22 | 2017-10-10 | Rohr, Inc. | Acoustic panel assembly with a folding chamber |
US10436118B2 (en) | 2017-06-19 | 2019-10-08 | Rohr, Inc. | Acoustic panel with folding chamber |
FR3068007B1 (fr) | 2017-06-23 | 2021-07-16 | Safran Nacelles | Dispositif de traitement acoustique pour nacelle de turboreacteur d'aeronef |
FR3074223A1 (fr) * | 2017-11-28 | 2019-05-31 | Airbus Operations | Panneau d’attenuation acoustique pour aeronef. |
US11315538B2 (en) | 2017-12-13 | 2022-04-26 | The Boeing Company | Anti-resonant panels |
US11056092B2 (en) * | 2017-12-13 | 2021-07-06 | The Boeing Company | Anti-resonant panel and methods of making the same |
FR3090471A1 (fr) * | 2018-12-24 | 2020-06-26 | Airbus Operations (S.A.S.) | Procédé de fabrication d’une structure d’absorption acoustique comprenant un panneau alvéolaire intégrant des éléments acoustiques et structure d’absorption acoustique obtenue à partir dudit procédé |
WO2020165619A1 (fr) * | 2019-02-13 | 2020-08-20 | 日産自動車株式会社 | Structure d'insonorisation |
WO2020165621A1 (fr) * | 2019-02-13 | 2020-08-20 | 日産自動車株式会社 | Structure d'insonorisation |
GB2583751B (en) * | 2019-05-09 | 2022-02-02 | Safran Nacelles Ltd | Acoustic panel |
FR3100918A1 (fr) * | 2019-09-12 | 2021-03-19 | Safran Nacelles | Panneau acoustique pour un ensemble propulsif d’aeronef, et son procede de fabrication |
GB2588204B (en) | 2019-10-15 | 2022-09-14 | Safran Nacelles Ltd | Aircraft nacelle inlet |
CN113123875B (zh) * | 2019-12-31 | 2022-07-08 | 中国航发商用航空发动机有限责任公司 | 航空发动机吸声装置及航空发动机 |
US20220139364A1 (en) * | 2020-11-02 | 2022-05-05 | Pratt & Whitney Canada Corp. | Sandwich-structured panels and method of manufacture |
US20230167774A1 (en) * | 2021-12-01 | 2023-06-01 | Rohr, Inc. | Attachment ring insulator systems, methods, and assemblies |
FR3134220A1 (fr) * | 2022-04-01 | 2023-10-06 | Airbus Operations (S.A.S.) | Panneau acoustique comprenant au moins deux structures alvéolaires imbriquées l’une dans l’autre, aéronef comportant au moins un tel panneau acoustique |
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US4759513A (en) * | 1986-09-26 | 1988-07-26 | Quiet Nacelle Corporation | Noise reduction nacelle |
GB9424495D0 (en) * | 1994-12-05 | 1995-01-25 | Short Brothers Plc | Aerodynamic low drag structure |
FR2787509B1 (fr) * | 1998-12-21 | 2001-03-30 | Aerospatiale | Structure d'entree d'air pour moteur d'aeronef |
GB0016149D0 (en) * | 2000-06-30 | 2000-08-23 | Short Brothers Plc | A noise attenuation panel |
GB2418957B (en) * | 2003-10-22 | 2006-07-05 | Rolls Royce Plc | A liner for a gas turbine engine casing |
FR2869360B1 (fr) * | 2004-04-27 | 2006-07-14 | Airbus France Sas | Ensemble reducteur de bruit pour turboreacteur d'aeronef |
FR2928625B1 (fr) * | 2008-03-14 | 2012-11-30 | Aircelle Sa | Dispositif de degivrage electrique |
-
2011
- 2011-10-04 FR FR1158936A patent/FR2980902B1/fr not_active Expired - Fee Related
-
2012
- 2012-10-02 EP EP12775807.6A patent/EP2764510A1/fr not_active Withdrawn
- 2012-10-02 CN CN201280048519.6A patent/CN103858159A/zh active Pending
- 2012-10-02 RU RU2014117115/28A patent/RU2014117115A/ru not_active Application Discontinuation
- 2012-10-02 BR BR112014006561A patent/BR112014006561A2/pt not_active IP Right Cessation
- 2012-10-02 WO PCT/FR2012/052226 patent/WO2013050694A1/fr active Application Filing
- 2012-10-02 CA CA2848248A patent/CA2848248A1/fr not_active Abandoned
-
2014
- 2014-04-02 US US14/243,326 patent/US20140326536A1/en not_active Abandoned
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WO1997039439A1 (fr) * | 1996-04-15 | 1997-10-23 | M. Faist Gmbh & Co. Kg | Element multicouche absorbant le son |
US6123170A (en) * | 1997-08-19 | 2000-09-26 | Aerospatiale Societe Nationale Industrielle | Noise reducing connection assembly for aircraft turbine housings |
US6173807B1 (en) * | 1998-04-13 | 2001-01-16 | The Boeing Company | Engine nacelle acoustic panel with integral wedge fairings and an integral forward ring |
US6123172A (en) * | 1999-07-22 | 2000-09-26 | Lydall, Inc. | Thermal and acoustical insulating shield |
DE10054120A1 (de) * | 2000-10-31 | 2002-05-16 | Karl Bachl Gmbh & Co Kg | Dämmelement |
FR2933224A1 (fr) | 2008-06-25 | 2010-01-01 | Aircelle Sa | Panneau accoustique pour une tuyere d'ejection |
Non-Patent Citations (1)
Title |
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See also references of EP2764510A1 |
Also Published As
Publication number | Publication date |
---|---|
FR2980902A1 (fr) | 2013-04-05 |
EP2764510A1 (fr) | 2014-08-13 |
US20140326536A1 (en) | 2014-11-06 |
CN103858159A (zh) | 2014-06-11 |
RU2014117115A (ru) | 2015-11-10 |
CA2848248A1 (fr) | 2013-04-11 |
BR112014006561A2 (pt) | 2017-03-28 |
FR2980902B1 (fr) | 2013-09-13 |
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