EP0747547B1 - Method of fabrication of a plate or the like with structural and acoustic features and plate obtained this way - Google Patents

Method of fabrication of a plate or the like with structural and acoustic features and plate obtained this way Download PDF

Info

Publication number
EP0747547B1
EP0747547B1 EP96450012A EP96450012A EP0747547B1 EP 0747547 B1 EP0747547 B1 EP 0747547B1 EP 96450012 A EP96450012 A EP 96450012A EP 96450012 A EP96450012 A EP 96450012A EP 0747547 B1 EP0747547 B1 EP 0747547B1
Authority
EP
European Patent Office
Prior art keywords
skins
skin
glue
panel
order
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP96450012A
Other languages
German (de)
French (fr)
Other versions
EP0747547A1 (en
Inventor
Alain Fournier
Bruno Pelouze
Pierre Tiefenbach
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Aerospatiale Matra
Original Assignee
Airbus Group SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Group SAS filed Critical Airbus Group SAS
Publication of EP0747547A1 publication Critical patent/EP0747547A1/en
Application granted granted Critical
Publication of EP0747547B1 publication Critical patent/EP0747547B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04BGENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B1/00Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
    • E04B1/62Insulation or other protection; Elements or use of specified material therefor
    • E04B1/74Heat, sound or noise insulation, absorption, or reflection; Other building methods affording favourable thermal or acoustical conditions, e.g. accumulating of heat within walls
    • E04B1/82Heat, sound or noise insulation, absorption, or reflection; Other building methods affording favourable thermal or acoustical conditions, e.g. accumulating of heat within walls specifically with respect to sound only
    • E04B1/84Sound-absorbing elements
    • E04B1/86Sound-absorbing elements slab-shaped
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/30Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
    • E04C2/34Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts
    • E04C2/36Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by transversely-placed strip material, e.g. honeycomb panels
    • E04C2/365Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by transversely-placed strip material, e.g. honeycomb panels by honeycomb structures
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04BGENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B1/00Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
    • E04B1/62Insulation or other protection; Elements or use of specified material therefor
    • E04B1/74Heat, sound or noise insulation, absorption, or reflection; Other building methods affording favourable thermal or acoustical conditions, e.g. accumulating of heat within walls
    • E04B2001/742Use of special materials; Materials having special structures or shape
    • E04B2001/748Honeycomb materials
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24149Honeycomb-like
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24273Structurally defined web or sheet [e.g., overall dimension, etc.] including aperture
    • Y10T428/24322Composite web or sheet
    • Y10T428/24331Composite web or sheet including nonapertured component

Description

La présente invention a trait à un procédé de fabrication d'un panneau ou analogue à propriétés structurale et acoustique et plus précisément d'une structure du type sandwich formée d'une âme alvéolaire revêtue sur ses deux faces, présentant des capacités à la fois de résistance à des charges importantes et d'atténuation acoustique. Un procédé de ce genre est décrit dans le document US-A-5 037 498.The present invention relates to a method of manufacturing a panel or analogous to structural and acoustic properties and more precisely to a sandwich type structure formed by a honeycomb core coated on both faces, having both resistance to loads capacities important and acoustic attenuation. A process of this kind is described in document US-A-5,037,498.

Bien que décrite ci-après dans son application à la réalisation notamment de cloisons de fuselage d'aéronefs, l'invention est évidemment susceptible d'applications dans tout autre domaine où s'avère nécessaire ou souhaitable d'utiliser une structure du type panneau sandwich alliant légèreté, grande résistance mécanique et propriétés acoustiques.Although described below in its application to the realization in particular of aircraft fuselage bulkheads, the invention is obviously susceptible applications in any other area where is necessary or desirable to use a sandwich panel structure combining lightness, great mechanical resistance and acoustic properties.

On sait que les aéronefs du type turbopropulseur posent des problèmes d'isolation acoustique de l'habitacle intérieur vis à vis notamment des bruits et vibrations engendrées par les moteurs, les hélices, des bruits aérodynamiques, etc...We know that turboprop aircraft pose problems sound insulation of the interior passenger compartment, in particular against noise and vibrations generated by engines, propellers, aerodynamic noise, etc ...

Jusqu'à présent on n'a pas encore résolu de manière satisfaisante l'isolation phonique en particulier de la cabine passager vis à vis de la partie cargo et l'invention vise précisément à proposer un nouveau type de panneau apte à la réalisation de cloisons de cabine passager.So far we have not yet resolved satisfactorily soundproofing in particular of the passenger cabin with respect to the part cargo and the invention aims precisely to propose a new type of panel suitable for the production of passenger cabin partitions.

De telles cloisons doivent nécessairement être des éléments structuraux, c'est-à-dire aptes à supporter des charges ou efforts, en particulier normalement au plan des cloisons, pouvant être très importants. Elles doivent en effet contenir, côté soute, les bagages en cas de crash de l'aéronef, ou résister en cas de dépressurisation brutale de la cabine ou de la soute.Such partitions must necessarily be structural elements, that is to say capable of supporting loads or efforts, in particular normally in terms of partitions, which can be very large. They must indeed contain, on the hold side, baggage in the event of an aircraft crash, or resist abrupt depressurization of the cabin or hold.

De plus, ces cloisons doivent présenter, côté cabine, un aspect esthétique, c'est-à-dire être décorées en accord avec le reste de la cabine.In addition, these partitions must have an aspect, cabin side aesthetic, that is to say being decorated in accordance with the rest of the cabin.

Il n'existe pas actuellement de panneaux satisfaisant d'une part aux contraintes habituelles de légèreté et de résistance au feu, mais également aux différents impératifs ci-dessus.There are currently no signs satisfying on the one hand the usual constraints of lightness and fire resistance, but also different imperatives above.

Les panneaux structuraux destinés à réduire par exemple les effets d'un crash n'ont pas de propriétés de traitement du bruit.Structural panels intended to reduce for example the effects of a crash have no noise processing properties.

Par ailleurs, on connaít des panneaux du type sandwich formé d'une âme en particulier en nid d'abeilles, flanquée, d'un côté, d'une feuille métallique perforée et, de l'autre côté, d'une feuille métallique non perforée, utilisés pour leurs propriétés d'atténuation du bruit, par exemple comme revêtements en certains emplacements de la nacelle de turbomoteurs afin d'absorber au moins partiellement l'énergie sonore des flux de gaz à grande vitesse.Furthermore, there are known sandwich type panels formed of a core in particular honeycomb, flanked, on one side, by a metallic foil perforated and, on the other side, an unperforated metal sheet, used for their noise attenuation properties, for example as coatings in certain locations in the turbine engine nacelle to absorb at least partially the sound energy of high speed gas flows.

Cependant, de telles structures se sont révélées manquer de solidité lorsqu'on a voulu les utiliser dans des environnements sévères pour réaliser à la fois une atténuation du bruit et une conservation de l'intégrité structurale.However, such structures have been found to lack strength when we wanted to use them in harsh environments to achieve both noise attenuation and preservation of structural integrity.

Par le brevet US N° 3.166.149, on connaít des panneaux du type ci-dessus mais plus sophistiqués en ce qui concerne la nature du revêtement composite à perforations rapporté sur l'une des faces de l'âme en nid d'abeilles. Ce revêtement est constitué, d'une part, d'un treillis en fibres de verre pré-imprégnées de résine polymérisée à des fins de rigidification du treillis avant sa fixation par collage sur l'une des faces du nid d'abeilles. Sur la face externe du treillis est, d'autre part, collée une feuille en matériau poreux, elle-même recouverte d'un revêtement mince, décoratif, perforé, éventuellement amovible, ne participant pas à la rigidité de l'ensemble.By US Patent No. 3,166,149, we know panels of the above type but more sophisticated with regard to the nature of the coating composite with perforations attached to one of the faces of the honeycomb core. This coating consists, on the one hand, of a lattice of prepreg glass fibers of polymerized resin to stiffen the trellis before it fixing by gluing on one side of the honeycomb. On the outside of the on the other hand, a sheet of porous material is glued, itself covered with a thin, decorative, perforated, possibly removable coating, not participating in the rigidity of the whole.

Si un tel panneau est considéré dans ledit brevet comme susceptible d'être utilisé pour réaliser des cloisons, ses rigidité et résistance structurales sont néanmoins insuffisantes pour résister à des charges importantes telles que celles résultant d'un crash. If such a panel is considered in said patent as susceptible to be used to make partitions, its rigidity and structural strength are nevertheless insufficient to withstand heavy loads such as those resulting from a crash.

En outre, les matériaux généralement utilisés pour constituer l'âme en nid d'abeilles et le revêtement non perforé, à savoir un feuillard d'aluminium et une feuille d'aluminium respectivement, conduisent à des structures composites présentant des masses surfaciques trop importantes.In addition, the materials generally used to constitute the nest core bees and the non-perforated coating, namely an aluminum strip and a aluminum foil respectively, lead to composite structures with too large surface masses.

L'invention a pour but de proposer un nouveau type de panneau susceptible en particulier de concilier les exigences les plus sévères en matière de légèreté, de rigidité et résistance mécanique.The invention aims to propose a new type of panel likely in particular to reconcile the most severe requirements in terms of lightness, rigidity and mechanical resistance.

A cet effet, l'invention a pour objet un procédé de fabrication d'un panneau ou analogue à propriétés structurale et acoustique, du type sandwich constitué d'une âme à structure alvéolaire ouverte revêtue sur ses deux faces, caractérisé en ce qu'il consiste :

  • à réaliser une première et une seconde peau par drapage et pressage à chaud dans des conditions de pression et température appropriées d'au moins deux plis de tissu de fibres minérales ou synthétiques imprégnées d'une résine thermoplastique,
  • à réaliser dans l'une des peaux des perforations d'un diamètre de l'ordre de 0,5 à 1,5 mm, avec une proportion de vide à la surface de la peau de l'ordre de 10 à 25%,
  • à appliquer sur l'une des faces de chaque peau, après préparation, un revêtement de colle époxy,
  • à former un sandwich comprenant ladite âme à structure alvéolaire ouverte avec les deux peaux sur ses faces opposées, les revêtements de colle étant en contact avec l'âme,
  • puis à presser à chaud le sandwich à des fins de polymérisation de la colle dans des conditions de température, pression et durée évitant toute obstruction même partielle des perforations de la peau perforée.
To this end, the subject of the invention is a method of manufacturing a panel or the like with structural and acoustic properties, of the sandwich type consisting of a core with open honeycomb structure coated on its two faces, characterized in that it consists of:
  • producing a first and a second skin by draping and hot pressing under conditions of appropriate pressure and temperature of at least two plies of fabric of mineral or synthetic fibers impregnated with a thermoplastic resin,
  • to make perforations in one of the skins with a diameter of the order of 0.5 to 1.5 mm, with a proportion of void on the surface of the skin of the order of 10 to 25%,
  • to be applied to one of the faces of each skin, after preparation, a coating of epoxy adhesive,
  • forming a sandwich comprising said core with open honeycomb structure with the two skins on its opposite faces, the adhesive coatings being in contact with the core,
  • then hot pressing the sandwich for the purpose of polymerizing the adhesive under conditions of temperature, pressure and duration avoiding any obstruction, even partial, of the perforations of the perforated skin.

Avantageusement les deux peaux sont constituées de tissus de fibres de verre imprégnées de résine polyétherimide.Advantageously, the two skins are made of fabrics of fibers of glass impregnated with polyetherimide resin.

Les deux peaux sont constituées d'un même nombre de plis, mais avantageusement peuvent avoir un nombre différent, une telle répartition dissymétrique des peaux de part et d'autre de l'âme centrale permettant de réduire la masse et le coût du panneau, sans nuire à sa planéité, du fait de la fabrication en multiphase du panneau, c'est-à-dire la consolidation séparée des éléments du panneau avant la cuisson de l'ensemble. C'est ainsi que la peau non perforée peut comporter un nombre de plis, trois par exemple, inférieur à celui, quatre par exemple, de la peau perforée, le nombre de plis étant directement lié aux efforts susceptibles de s'appliquer au panneau.The two skins are made up of the same number of folds, but advantageously can have a different number, such a distribution asymmetrical skins on either side of the central core allowing reduce the mass and cost of the panel, without affecting its flatness, due to the multiphase manufacturing of the panel, i.e. separate consolidation of elements of the panel before cooking the whole. This is how the skin non-perforated may have a number of plies, three for example, less than that, for example four, of the perforated skin, the number of folds being directly related to the forces likely to apply to the panel.

Suivant un mode préféré de mise en oeuvre, le revêtement de colle époxy est appliqué sous la forme d'un film mince de très faible masse surfacique et le cycle de polymérisation comporte une montée en température à un premier palier d'une valeur et d'une durée suffisantes pour faire fluer la colle sans pour autant lancer de manière significative sa polymérisation, afin de ne pas obstruer les perforations de la peau, puis à un second palier d'une valeur et d'une durée suffisantes pour réaliser ladite polymérisation.According to a preferred embodiment, the coating of epoxy adhesive is applied in the form of a thin film of very low surface mass and the polymerization cycle involves a rise in temperature to a first level of sufficient value and duration to cause the glue to flow without as much to significantly initiate its polymerization, so as not to obstruct skin perforations, then at a second level of value and duration sufficient to carry out said polymerization.

L'invention a également pour objet le panneau obtenu conformément au procédé ci-dessus, un tel panneau étant par exemple dimensionné, conformé et pourvu d'éléments de bordures, d'inserts et autres aménagements pour la constitution d'éléments de cloison de fuselage d'aéronefs. De tels éléments de cloison se sont révélés présenter d'excellentes propriétés d'atténuation acoustique pour des fréquences supérieures à 500 Hz et de résistance à des charges importantes appliquées normalement à la cloison. C'est ainsi, par exemple, qu'un panneau selon l'invention d'une surface de 1,5 m2 a résisté à des efforts de l'ordre de 900 daN.The subject of the invention is also the panel obtained in accordance with the above process, such a panel being for example dimensioned, shaped and provided with border elements, inserts and other arrangements for the construction of fuselage bulkhead elements. aircraft. Such partition elements have been found to have excellent acoustic attenuation properties for frequencies above 500 Hz and resistance to heavy loads normally applied to the partition. Thus, for example, a panel according to the invention with a surface of 1.5 m 2 withstood forces of the order of 900 daN.

De plus, notamment la face perforée d'une telle cloison, peut être facilement traitée esthétiquement, soit par teinture dans la masse de la résine de la peau, avec un aspect de surface en relief, par exemple un granité, obtenu au moulage, soit par thermogainage d'un revêtement tel qu'un film décor perforé, soit par application d'un tel revêtement ou d'un textile acoustiquement transparent.In addition, in particular the perforated face of such a partition, can be easily treated aesthetically, either by dyeing the bulk of the resin the skin, with a relief surface appearance, for example a granita, obtained at molding, either by thermo-sheathing a coating such as a perforated decorative film, either by applying such a coating or acoustically textile transparent.

D'autres caractéristiques et avantages ressortiront de la description qui va suivre d'un mode de réalisation d'un panneau selon l'invention, description donnée à titre d'exemple uniquement et en regard du dessin annexé sur lequel :

  • Figure 1 est une vue en coupe et en éclaté schématique d'une structure de panneau selon l'invention ;
  • Figure 2 est une vue en perspective partielle et en arraché d'un panneau réalisé, du type illustré en figure 1, et
  • Figure 3 est une courbe illustrant un cycle de cuisson préférentiel du panneau.
Other characteristics and advantages will emerge from the following description of an embodiment of a panel according to the invention, description given by way of example only and with reference to the appended drawing in which:
  • Figure 1 is a schematic sectional and exploded view of a panel structure according to the invention;
  • FIG. 2 is a partial perspective view and a cutaway view of a panel produced, of the type illustrated in FIG. 1, and
  • Figure 3 is a curve illustrating a preferred cooking cycle of the panel.

Sur la figure 1 on a schématisé un panneau sandwich vu sur la tranche et comprenant une âme centrale à structure alvéolaire ouverte 1, flanquée de part et d'autre d'une peau, à savoir une peau inférieure multiplis 2 et une peau supérieure multiplis 3.In Figure 1 we have schematically shown a sandwich panel seen on the edge and comprising a central core with an open honeycomb structure 1, flanked by and on the other side of a skin, namely a 2-ply lower skin and a skin upper multiply 3.

Conformément à l'invention, chaque peau 2,3 est constituée de plusieurs plis formés chacun d'un tissu de fibres synthétiques ou minérales imprégnées d'une résine thermoplastique et chaque peau est consolidée avant assemblage du sandwich. A cet effet, un tissu de fibres pré-imprégnées est drapé suivant plusieurs couches ou plis superposés sur une surface plane appropriée. L'ensemble est compacté à température appropriée suivant la nature des fibres et de la résine en sorte d'obtenir une peau rigide autoportante. Une telle opération, appelée communément consolidation, est en soi bien connue de l'homme du métier et il n'est pas nécessaire de donner plus amples détails.According to the invention, each skin 2,3 is made up of several pleats each formed from a fabric of impregnated synthetic or mineral fibers of a thermoplastic resin and each skin is consolidated before assembly sandwich. To this end, a fabric of prepreg fibers is draped according to several layers or folds superimposed on a suitable flat surface. The assembly is compacted at an appropriate temperature according to the nature of the fibers and resin so as to obtain a rigid self-supporting skin. Such a operation, commonly called consolidation, is in itself well known to skilled in the art and there is no need to give further details.

Toutefois, préférentiellement, on utilisera des fibres de verre du type E imprégnées à raison de 30 à 35% de résine polyétherimide. Plus précisément encore, comme fibres et résine particulièrement appropriées, on peut citer, d'une part, les tissus de fibres de verre E connues dans le commerce sous la désignation "7781" et, d'autre part, la résine polyétherimide dénommée commercialement "ULTEM"® fabriquée par la Société GENERAL ELECTRIC.However, preferably, type E glass fibers will be used impregnated with 30 to 35% polyetherimide resin. More precisely still, as particularly suitable fibers and resin, there may be mentioned, on the one hand, the E glass fiber fabrics known in the trade under the designation "7781" and, on the other hand, the polyetherimide resin called commercially "ULTEM" ® manufactured by GENERAL ELECTRIC.

L'une des peaux, en l'occurrence la peau supérieure 3, les termes "supérieure" et "inférieure" n'ayant pas en fait de signification pratique puisque le sandwich final peut être utilisé dans n'importe quelle position dans l'espace, est en outre, conformément à l'invention, muni, après consolidation, d'une pluralité de trous identiques 4 traversant normalement l'épaisseur de la peau.One of the skins, in this case the upper skin 3, the terms "superior" and "inferior" having in fact no practical significance since the final sandwich can be used in any position in space, is further, in accordance with the invention, provided, after consolidation, with a plurality of identical holes 4 normally passing through the thickness of the skin.

De préférence, la proportion, en surface totale de la peau 3, des vides ou trous 4 est de l'ordre de 10 à 25% et le diamètre des trous 4 est de l'ordre de 0,5 à 1,5 mm et plus particulièrement encore de 1 mm pour un pourcentage des vides de l'ordre de 23%. Il est par ailleurs préférable que le diamètre des trous soit supérieur ou égal à l'épaisseur de la peau.Preferably, the proportion, in total area of the skin 3, of the voids or holes 4 is around 10 to 25% and the diameter of holes 4 is around 0.5 to 1.5 mm and more particularly still 1 mm for a percentage of voids of the order of 23%. It is also preferable that the diameter of the holes is greater than or equal to the thickness of the skin.

Par ailleurs, la distribution des trous est uniforme sur toute la surface.Furthermore, the distribution of the holes is uniform over the entire surface.

Les peaux 2 et 3 sont avantageusement réalisées à partir des mêmes fibres et résine et, suivant une autre caractéristique de l'invention, comportent un nombre de plis différent, celui de la peau perforée 3 étant par exemple supérieur à celui de la peau non perforée 2.The skins 2 and 3 are advantageously made from the same fibers and resin and, according to another characteristic of the invention, comprise a different number of folds, that of the perforated skin 3 being for example higher than that of unperforated skin 2.

A titre d'exemple, la peau non perforée 2 comporte trois plis : 2a, 2b, 2c et la peau perforée 3 en comporte quatre : 3a, 3b, 3c, 3d.For example, the non-perforated skin 2 has three folds: 2a, 2b, 2c and the perforated skin 3 has four: 3a, 3b, 3c, 3d.

Une fois les peaux 2,3 consolidées, on procède à leur assemblage, par collage, à l'âme 1. Celle-ci est, d'une manière générale, une structure à alvéoles ouverts suivant un axe perpendiculaire au plan médian de l'âme et, en particulier est constitué d'une structure en nid d'abeilles, par exemple réalisée en un papier de fibres aramides tel que celui dénommé commercialement "NOMEX"®.Once the skins 2,3 have been consolidated, they are assembled, by bonding, to the core 1. This is, in general, a honeycomb structure open along an axis perpendicular to the median plane of the soul and, in particular consists of a honeycomb structure, for example made of paper aramid fibers such as that known commercially as "NOMEX" ®.

L'une des faces de chaque peau 2, 3 est revêtue d'une colle époxy appropriée, appliquée de façon la plus régulière possible. Par exemple, la colle sera appliquée par pulvérisation, mais, de préférence, elle sera constituée d'un film mince de très faible masse surfacique, de l'ordre de 70 g/m2 par exemple. Plus particulièrement encore, le film adhésif dénommé SCOTCH-WELD® AF 163-2U fabriqué par la Société 3M convient remarquablement. Il est à noter que cette colle est auto-extinguible et que, d'une manière préférentielle, on utilisera une colle ayant cette propriété.One of the faces of each skin 2, 3 is coated with an appropriate epoxy adhesive, applied as evenly as possible. For example, the adhesive will be applied by spraying, but preferably it will consist of a thin film of very low surface mass, of the order of 70 g / m 2 for example. More particularly still, the adhesive film called SCOTCH-WELD® AF 163-2U manufactured by the company 3M is remarkably suitable. It should be noted that this adhesive is self-extinguishing and that, preferably, an adhesive having this property will be used.

Ensuite, les parties 1,2,3 du sandwich sont superposées sur un plateau de presse chauffante et soumises à un cycle de cuisson à des fins de polymérisation de la colle.Then, the 1,2,3 parts of the sandwich are superimposed on a tray heating press and subjected to a cooking cycle for the purpose of adhesive polymerization.

Conformément à l'invention et dans le cas de l'utilisation du film d'adhésif de la Société 3M, le cycle de polymérisation est opéré à pression constante, de l'ordre de 1 bar ou un peu plus, et en amenant la température à un premier palier 5, aux environs de 80°C ,puis à un second palier 6, aux environs de 130°C, avant de redescendre à une température de l'ordre de 50°C à laquelle la pression est supprimée et le panneau démoulé. According to the invention and in the case of the use of the adhesive film from 3M, the polymerization cycle is operated at constant pressure, around 1 bar or a little more, and bringing the temperature to a first level 5, around 80 ° C, then at a second level 6, around 130 ° C, before going down to a temperature of the order of 50 ° C at which the pressure is removed and the panel is demolded.

La figure 3 illustre un cycle du type ci-dessus, au cours duquel le palier 5 de température à 80°C est maintenu pendant 30 minutes et le palier 6 à 130°C pendant 60 minutes, une pression de 1,2 bar étant maintenue pendant tout le cycle.FIG. 3 illustrates a cycle of the above type, during which the bearing 5 temperature at 80 ° C is maintained for 30 minutes and the level 6 at 130 ° C for 60 minutes, a pressure of 1.2 bar being maintained throughout cycle.

La température du premier palier 5 et la durée de celui-ci sont déterminées de façon à être suffisantes pour faire fluer la colle sans pour autant et de manière significative lancer la phase de polymérisation.The temperature of the first stage 5 and the duration thereof determined to be sufficient to cause the glue to flow without and significantly initiate the polymerization phase.

Au cours de ce premier palier 5, la colle va se liquéfier et au niveau des trous de la peau perforée le film va se rompre et le matériau de la colle va s'agglutiner en formant un ménisque à l'interface peau 3 - âme 1 et sur le pourtour de chaque trou 4.During this first level 5, the glue will liquefy and at the level of the perforated skin holes the film will break and the glue material will clump together to form a meniscus at the skin 3 - core 1 interface and on the around each hole 4.

Quant au second palier de température 6, il est effectué à une température et pendant une durée suffisantes pour permettre une polymérisation totale.As for the second temperature level 6, it is carried out at a temperature and for a sufficient time to allow polymerization total.

Dans le cas de l'application de la colle par pulvérisation, les trous 4 ne seront pas bouchés et le cycle de polymérisation est opéré à la manière habituelle et ne comporte pas les deux paliers de température de la figure 3.In the case of spray adhesive application, the holes 4 do not will not be blocked and the polymerization cycle is operated in the manner usual and does not include the two temperature levels of Figure 3.

La figure 2 illustre un panneau réalisé selon le schéma d'empilage de la figure 1.FIG. 2 illustrates a panel produced according to the stacking diagram of the figure 1.

Dans la pratique on réalisera directement le panneau aux formes et dimensions de la cloison ou élément de cloison à obtenir, par exemple pour séparer les zones soute et passager d'un aéronef type turbopropulseur.In practice, the panel will be directly shaped and dimensions of the partition or partition element to be obtained, for example for separate the hold and passenger areas of a turboprop aircraft.

A cet effet, après consolidation des peaux, dont le nombre de plis de chacune sera déterminé en fonction de la nature et l'emplacement de la cloison à réaliser, on effectuera un détourage des peaux au laser, puis éventuellement un pliage et un soyage. De même, le nid d'abeilles sera usiné, soyé et détouré.To this end, after consolidation of the skins, the number of folds of each will be determined according to the nature and location of the partition to be carried out, a laser clipping of the skins will be carried out, then possibly folding and sinking. Likewise, the honeycomb will be machined, crimped and cut.

Les faces à coller des peaux seront poncées, dépoussiérées, dégraissées et enduites ou revêtues d'un film d'adhésif époxy approprié.The faces to be glued on the skins will be sanded, dusted, degreased and coated or coated with a suitable epoxy adhesive film.

Les trois éléments constitutifs du sandwich seront ensuite mis en place dans un moule, et complétés par des éléments de bordure, de renfort, des inserts etc... The three components of the sandwich will then be put in place in a mold, and supplemented by border elements, reinforcement, inserts etc ...

Le moule enfin sera alors placé entre les plateaux d'une presse chauffante pour y subir ledit cycle de polymérisation de la colle ou adhésif.The mold will then be placed between the plates of a heating press to undergo said polymerization cycle of the glue or adhesive.

Les panneaux, cloisons ou éléments de cloison ainsi obtenus peuvent être plats ou cintrés ou présenter des parties planes formant un angle entre elles.The panels, partitions or partition elements thus obtained can be flat or curved or have flat parts forming an angle between them.

A titre d'exemple, le procédé de l'invention permet d'obtenir des peaux consolidées, prêtes à l'assemblage, multiplis, chaque pli ayant une épaisseur de 0,25mm et une masse surfacique de 450 g/m2 pour un pli non perforé et de 350 g/m2 pour un pli perforé, les tissus de fibres étant constitués de verre E, d'une masse surfacique de 300 g/m2, d'une épaisseur de 20/100 de millimètre, d'armure satin 8, avec un nombre de fils de chaíne de 22 et de fils de trame de 20, cependant que la résine est du type polyétherimide.By way of example, the method of the invention makes it possible to obtain consolidated skins, ready for assembly, plywood, each ply having a thickness of 0.25mm and a surface mass of 450 g / m 2 for a ply non-perforated and 350 g / m 2 for a perforated ply, the fiber fabrics being made of E glass, a surface mass of 300 g / m 2 , with a thickness of 20/100 of a millimeter, weave satin 8, with a number of warp threads of 22 and weft threads of 20, while the resin is of the polyetherimide type.

La consolidation des peaux avant assemblage, conformément à l'invention, permet de réaliser des panneaux dissymétriques présentant une face renforcée à nombre de plis supérieur à celui de l'autre face.Consolidation of the skins before assembly, in accordance with the invention makes it possible to produce asymmetrical panels having one face reinforced with more folds than the other side.

Si l'on avait employé la technique habituelle de réalisation en co-cuisson de ce panneau sandwich, il aurait fallu disposer autant de plis de chaque côté du nid d'abeilles pour éviter toute déformation ou voilage du panneau en cours de polymérisation. Ceci aurait conduit à placer inutilement un pli supplémentaire sur l'une des faces.If we had used the usual technique of co-cooking of this sandwich panel, there should have been as many folds on each side honeycomb to prevent any deformation or buckling of the panel in progress polymerization. This would have unnecessarily placed an additional fold on one of the faces.

La technique de l'invention permet d'enlever un tel pli sur la face moins sollicitée, ce qui abaisse la masse de l'ensemble et le coût. En outre, les surfaces du panneau sandwich demeurent parfaitement planes malgré la répartition dissymétrique des peaux.The technique of the invention makes it possible to remove such a fold on the less face solicited, which lowers the mass of the assembly and the cost. In addition, sandwich panel surfaces remain perfectly flat despite the asymmetrical distribution of skins.

D'une manière générale, l'épaisseur de l'âme 1 est directement liée au spectre de fréquences que l'on désire atténuer. Pour les fréquences plus particulièrement visées dans les applications notamment aux cloisons d'avions du type turbopropulseur, c'est-à-dire des fréquences dans la gamme 1200 à 2000 Hz, l'épaisseur de l'âme 1 sera typiquement de l'ordre de vingt millimètres.In general, the thickness of the core 1 is directly linked to the frequency spectrum that one wishes to attenuate. For higher frequencies particularly targeted in applications in particular to aircraft partitions turboprop type, i.e. frequencies in the 1200 to 2000 Hz, the thickness of the core 1 will typically be of the order of twenty millimeters.

Quant au diamètre des trous 4, il est lié assez étroitement au pourcentage de vide dans la peau perforée, étant entendu par ailleurs que le couple de ces deux paramètres (diamètre des trous et pourcentage de vide) pourra évoluer en fonction des caractéristiques ou propriétés acoustiques des éventuels éléments de revêtements décoratifs dont pourrait être munie la peau perforée.As for the diameter of the holes 4, it is fairly closely related to the percentage vacuum in the perforated skin, it being understood that the pair of these two parameters (diameter of the holes and percentage of vacuum) can change in function of the acoustic characteristics or properties of any elements decorative coverings which could be provided on the perforated skin.

En effet, outre les propriétés structurales, d'atténuation acoustique et de légèreté des panneaux ou cloisons obtenus conformément à l'invention, il faut également noter leur aptitude à une décoration facile et économique, soit par l'utilisation pour les peaux d'une résine teintée dans la masse, soit par la constitution sur la face visible de la peau d'un état de surface esthétique, par exemple aspect granité, communiqué par le moule sur lequel sont drapés les plis, soit encore par revêtement, par exemple de la peau perforée, par thermogainage d'un film décor perforé ou collage d'un tel film ou d'un revêtement textile acoustiquement transparent.In fact, in addition to the structural properties, acoustic attenuation and lightness of the panels or partitions obtained in accordance with the invention, it is necessary also note their ability to decorate easily and economically, either by the use for the skins of a resin dyed in the mass, either by the constitution on the visible face of the skin of an aesthetic surface state, by example granite aspect, communicated by the mold on which the folds, or again by coating, for example of the perforated skin, by thermogainage of a perforated decorative film or bonding of such a film or of a acoustically transparent textile covering.

Enfin, les panneaux, cloisons ou autres produits obtenus conformément au procédé de l'invention, satisfont à la norme FAR 25 § 853 (critères de Feu/Fumée/Toxicité) applicable aux avions commerciaux, notamment du fait du choix pour les peaux d'une résine polyétherimide.Finally, panels, partitions or other products obtained in accordance to the process of the invention, comply with standard FAR 25 § 853 (criteria for Fire / Smoke / Toxicity) applicable to commercial aircraft, in particular due to the choice for the skins of a polyetherimide resin.

Claims (16)

  1. Method of manufacturing a panel or the like with structural and acoustic properties of the sandwich type consisting of a core with an open alveolar structure (1) clad on its two faces, characterised in that it comprises:
    producing first and second skins (2, 3) by the corrugation and hot pressing, under suitable pressure and temperature conditions, of at least two plies of cloth of mineral or synthetic fibres impregnated with a thermoplastic resin,
    producing, in one of the skins (2, 3), perforations (4) with a diameter of the order of 0.5 to 1.5 mm, with a proportion of void on the surface of the skin of the order of 10 to 25%,
    applying to one of the faces of each skin, after preparation, a covering of epoxy glue,
    forming a sandwich comprising said core with open alveolar structure (1) with the two skins (2, 3) on its opposite faces, the coatings of glue being in contact with the core,
    then hot pressing the sandwich for the purpose of polymerisation of the glue under conditions of temperature, pressure and duration preventing any obstruction, even partial, of the perforations in the perforated skin (3).
  2. Method according to Claim 1, characterised in that the skins (2, 3)consist of cloths of glass fibres impregnated with polyetherimide resin.
  3. Method according to Claim 1 or 2, characterised in that the two skins (2, 3) have different numbers of plies.
  4. Method according to Claims 1 to 3, characterised in that the coating of glue is a thin film with a very low mass per surface area.
  5. Method according to Claim 4, characterised in that the glue is a self-extinguishing glue.
  6. Method according to Claim 4 or 5, characterised in that the film of glue is the film known as SCOTCH-WELD® AF 163-2U from the 3M Company.
  7. Method according to one of Claims 4 to 6, characterised in that the polymerisation step is effected in accordance with a cycle including a rise in temperature to a first level with a sufficient value and duration to cause the glue to flow without significantly initiating its polymerisation, and then to a second level with a sufficient value and duration to effect said polymerisation.
  8. Method according to Claim 7, characterised in that said first temperature level is maintained for a period of the order of 30 minutes and said second temperature level is maintained for a period of the order of 60 minutes.
  9. Panel or the like obtained in accordance with the method according to any one of Claims 1 to 8.
  10. Panel according to Claim 9, characterised in that the core with a alveolar structure is a honeycomb (1).
  11. Panel according to Claim 9 or 10, characterised in that it comprises an unperforated skin (2) with three plies and a perforated skin (3) with four plies, each ply having a thickness of 0.25 mm and consisting of E type glass fibres impregnated with polyetherimide resin.
  12. Panel according to one of Claims 9 to 11, characterised in that the perforated skin (3) comprises perforations with a diameter of the order of 1 mm, the percentage of voids in the skin being the order of 23%.
  13. Panel according to one of Claims 9 to 12, characterised in that the resin in at least one of the skins (2, 3) is coloured in its mass.
  14. Panel according to one of Claims 9 to 12, characterised in that the visible face of at least one of the skins (2, 3) is covered by heat-sheathing with a decorated film, perforated or otherwise.
  15. Panel according to one of Claims 9 to 12, characterised in that the visible face of at least one of the skins (2, 3) is covered with a textile, acoustically transparent or otherwise.
  16. Panel according to one of Claims 9 to 12, characterised in that the visible face of at least one of the skins (2, 3) has a surface appearance in relief, notably a granite.
EP96450012A 1995-06-08 1996-06-05 Method of fabrication of a plate or the like with structural and acoustic features and plate obtained this way Expired - Lifetime EP0747547B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9507020 1995-06-08
FR9507020A FR2735166B1 (en) 1995-06-08 1995-06-08 METHOD FOR MANUFACTURING A PANEL OR THE LIKE WITH STRUCTURAL AND ACOUSTIC PROPERTIES AND PANEL SO OBTAINED

Publications (2)

Publication Number Publication Date
EP0747547A1 EP0747547A1 (en) 1996-12-11
EP0747547B1 true EP0747547B1 (en) 2000-04-19

Family

ID=9479939

Family Applications (1)

Application Number Title Priority Date Filing Date
EP96450012A Expired - Lifetime EP0747547B1 (en) 1995-06-08 1996-06-05 Method of fabrication of a plate or the like with structural and acoustic features and plate obtained this way

Country Status (7)

Country Link
US (1) US5888610A (en)
EP (1) EP0747547B1 (en)
CN (1) CN1078844C (en)
CA (1) CA2178148C (en)
DE (1) DE69607783T2 (en)
ES (1) ES2147908T3 (en)
FR (1) FR2735166B1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007060668A1 (en) 2007-12-17 2009-06-18 Airbus Deutschland Gmbh Sandwich panel for sound absorption

Families Citing this family (72)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6284089B1 (en) * 1997-12-23 2001-09-04 The Boeing Company Thermoplastic seam welds
FR2779379B1 (en) * 1998-06-05 2000-08-25 Peguform France PROCESS FOR PRODUCING A REINFORCED COMPOSITE STRUCTURE PANEL OF THE SANDWICH TYPE WITH AN ALVEOLAR CORE AND PANEL PRODUCED ACCORDING TO SUCH A PROCESS
AT408007B (en) * 1999-08-16 2001-08-27 Wimmer Peter Dipl Ing Structural panel with a metal fabric
DE19943320A1 (en) * 1999-09-10 2001-03-15 Hauni Maschinenbau Ag Arrangement for reducing the noise level on production machines in the tobacco processing industry
GB2361718A (en) * 2000-04-26 2001-10-31 Wang Chao Shun Sound reduction device within a soundproof wall
US6500516B2 (en) 2001-02-02 2002-12-31 Panelite Llc Light transmitting panels
US6890023B2 (en) * 2002-04-19 2005-05-10 Patent Holding Company Reinforced composite inner roof panel of the cellular core sandwich-type and method of making same
US6748876B2 (en) 2001-10-30 2004-06-15 Patent Holding Company Reinforced composite pallet assembly of the sandwich-type with a locally crushed cellular core
US6823803B2 (en) 2001-10-30 2004-11-30 Patent Holding Company Assembly for enclosing and protecting a plurality of meters for storage or transportation purposes and carrier and pallet for use therein
US6655299B2 (en) 2001-10-30 2003-12-02 Patent Holding Company Reinforced composite pallet assembly of the cellular core sandwich-type
US8158539B2 (en) * 2001-11-07 2012-04-17 Flexform Technologies, Llc Heat deflection/high strength panel compositions
US20040097159A1 (en) * 2001-11-07 2004-05-20 Balthes Garry E. Laminated composition for a headliner and other applications
US8071491B2 (en) * 2001-11-07 2011-12-06 FledForm Technologies, LLC Process, composition and coating of laminate material
US8012889B2 (en) * 2001-11-07 2011-09-06 Flexform Technologies, Llc Fire retardant panel composition and methods of making the same
US20030162461A1 (en) * 2002-02-22 2003-08-28 Balthes Garry E. Process, composition and coating of laminate material
US6773756B2 (en) * 2002-03-20 2004-08-10 Bayer Polymers Llc Process to manufacture three dimensionally shaped substrate for sound abatement
FR2840302B1 (en) * 2002-06-03 2004-07-16 Aventis Pharma Sa ISOINDOLONE DERIVATIVES, PREPARATION METHOD AND INTERMEDIARY THEREOF AS MEDICAMENTS AND PHARMACEUTICAL COMPOSITIONS COMPRISING SAME
JP2004062074A (en) * 2002-07-31 2004-02-26 Toyota Motor Corp Sound absorbing equipment
FR2859229B1 (en) * 2003-08-29 2006-03-03 Gravicolor COMPLEX MATERIAL FOR COATING WALLS, CEILINGS OR SOILS FOR CORRECTING THE ACOUSTIC OF A LOCAL BY ABSORPTION
KR100569159B1 (en) * 2004-07-26 2006-04-10 (주)시공사 Curved Panel for Sound Reflection Board and Method for Preparing the Same
US7906176B2 (en) * 2004-12-17 2011-03-15 Flexform Technologies, Llc Methods of manufacturing a fire retardant structural board
US7434659B2 (en) * 2005-04-04 2008-10-14 Hexcel Corporation Acoustic septum cap honeycomb
US20070141318A1 (en) * 2005-12-16 2007-06-21 Balthes Garry E Composition and method of manufacture for a fiber panel having a finishable surface
FR2912100B1 (en) * 2007-02-06 2009-05-08 Cera ACOUSTIC PROTECTION PANEL FOR MOTOR VEHICLE COMPRISING AN IMPREGNATED SEAL LAYER
JP2009062977A (en) * 2007-08-15 2009-03-26 Rohr Inc Linear acoustic liner
DE102007044388B4 (en) * 2007-09-18 2012-08-02 Airbus Operations Gmbh Pressure bulkhead and method for dividing an aircraft or spacecraft
DE102007060662B4 (en) * 2007-12-17 2014-07-24 Airbus Operations Gmbh Flugzeugkabinenpaneel
US20090163115A1 (en) * 2007-12-20 2009-06-25 Spirit Aerosystems, Inc. Method of making acoustic holes using uv curing masking material
EP2283480A4 (en) * 2008-05-22 2016-11-09 3M Innovative Properties Co Multilayer sound absorbing structure comprising mesh layer
US8117972B2 (en) * 2008-07-09 2012-02-21 Global Ip Holdings, Llc Kit and shelving system to store work tools, equipment and supplies in a motor vehicle and plastic shelf for use therein
US20100108438A1 (en) * 2008-11-03 2010-05-06 William Christopher Duffy Panel for acoustic damping and fire protection applications
DE102008062703A1 (en) * 2008-12-17 2010-07-01 Airbus Deutschland Gmbh Aircraft cabin panel for sound absorption
US8292027B2 (en) 2009-04-21 2012-10-23 E I Du Pont De Nemours And Company Composite laminate for a thermal and acoustic insulation blanket
US8607928B2 (en) 2009-04-21 2013-12-17 E I Du Pont De Nemours And Company Composite flame barrier laminate for a thermal and acoustic insulation blanket
ES2365196T3 (en) * 2009-10-16 2011-09-26 Rieter Technologies Ag SANDWICH TYPE CONSTRUCTION AS A PANEL FOR THE AUTOMOTIVE INDUSTRY.
US8220588B2 (en) * 2010-03-31 2012-07-17 The Boeing Company Unitized engine nacelle structure
US9050766B2 (en) 2013-03-01 2015-06-09 James Walker Variations and methods of producing ventilated structural panels
US9604428B2 (en) 2010-08-24 2017-03-28 James Walker Ventilated structural panels and method of construction with ventilated structural panels
US8534018B2 (en) * 2010-08-24 2013-09-17 James Walker Ventilated structural panels and method of construction with ventilated structural panels
US9091049B2 (en) 2010-08-24 2015-07-28 James Walker Ventilated structural panels and method of construction with ventilated structural panels
GB2485165A (en) * 2010-11-03 2012-05-09 Timothy John Sweatman A laminated panel for acoustic insulation
FI20115485A (en) * 2011-05-19 2012-11-20 Yeseco Oy Acoustics plate
US11214035B2 (en) 2012-05-24 2022-01-04 Global Ip Holdings, Llc Marine decking with sandwich-type construction and method of making same
US11518136B2 (en) 2012-05-24 2022-12-06 Global Ip Holdings, Llc Marine decking with sandwich-type construction and method of making same
US20170267315A1 (en) 2012-05-24 2017-09-21 Global Ip Holdings, Llc Marine decking with sandwich-type construction and method of making same
US10532499B2 (en) 2013-02-08 2020-01-14 Global Ip Holdings, Llc Method of making a laminated trim component
US10279512B2 (en) 2013-02-08 2019-05-07 Global Ip Holdings, Llc Method of making a laminated trim component at a molding station
US10618203B2 (en) 2013-02-08 2020-04-14 Global Ip Holdings, Llc Method of making a trimmed, laminated trim component
CN104698763B (en) * 2013-12-10 2017-12-29 上海微电子装备(集团)股份有限公司 Sound-adsorbing sound-insulating hung device and lithographic equipment
CN103862764B (en) * 2013-12-23 2017-01-25 中航复合材料有限责任公司 Method for preparing honeycomb interlayer structure composite material by adopting liquid formation technology
CN103803015B (en) * 2014-01-20 2016-08-17 江苏海事职业技术学院 A kind of can the bulkhead of naval vessel superstructure of antiknock and noise control
CN103803028B (en) * 2014-01-20 2016-03-02 江苏海事职业技术学院 The platform bulkhead structure of a kind of antiknock, fire prevention, insulation, noise reduction
US9693166B2 (en) * 2014-06-24 2017-06-27 The Boeing Company Automated production of acoustic structures
CN104385758A (en) * 2014-12-03 2015-03-04 成都飞机工业(集团)有限责任公司 Method for stabilizing U-shaped composite material honeycomb sandwich part honeycomb core
JP6577716B2 (en) * 2015-02-13 2019-09-18 三菱航空機株式会社 Aircraft reinforcement structure
CN105173059A (en) * 2015-08-13 2015-12-23 中国航空工业集团公司西安飞机设计研究所 Double-layer honeycomb noise reduction structure
US10773881B2 (en) * 2015-10-05 2020-09-15 Advanced Composite Structures, Llc Air cargo container and curtain for the same
CN105332443B (en) * 2015-11-25 2017-10-13 苏州富通高新材料科技股份有限公司 Reclaim the insulated wall that tubing is recycled
CN107299733A (en) * 2016-04-14 2017-10-27 黑龙江智鹏建材有限公司 Without electricity consumption but can adaptively temperature adjustment and fire extinguishing outer wall heat insulating and decorating plate
FR3053627B1 (en) * 2016-07-05 2021-07-30 Porcher Ind COMPOSITE SHEET BASED ON FABRIC AND CONTROLLED POROSITY POLYETHERIMIDE
FR3056936B1 (en) * 2016-10-03 2018-10-05 Airbus Operations METHOD FOR MANUFACTURING AN ACOUSTIC PANEL REINFORCED BY AT LEAST ONE LAYER OF THERMOPLASTIC COMPOSITE MATERIAL
CN106379482A (en) * 2016-10-28 2017-02-08 刘跃平 Biomimetic combination beam plate structure and boat
CN108018989A (en) * 2016-10-31 2018-05-11 张跃 A kind of sealed tube core type composite plate and load-bearing material for building
US10927543B2 (en) * 2017-06-19 2021-02-23 The Boeing Company Acoustic attenuation structure
CN109393688A (en) * 2017-08-16 2019-03-01 张跃 A kind of luggage structure
JP6482040B2 (en) * 2017-08-25 2019-03-13 東京ブラインド工業株式会社 Sound absorbing panel using paper core material
US11851270B2 (en) 2017-10-10 2023-12-26 Advanced Composite Structures, Llc Latch for air cargo container doors
CN110815901A (en) * 2019-10-17 2020-02-21 成都飞机工业(集团)有限责任公司 Method for controlling through hole rate of acoustic lining wall plate made of honeycomb sandwich composite material
MX2020011446A (en) * 2019-10-31 2021-05-03 Gold Bond Building Products Llc Gypsum panel containing a fluted layer.
CN112621134B (en) * 2020-12-22 2022-04-19 江苏盈达机电科技有限公司 Grid type clean plate and production process thereof
WO2022221383A1 (en) * 2021-04-13 2022-10-20 Hercutech Inc. Systems and methods for a wall assembly having an acoustic panel
FR3133372A1 (en) * 2022-03-11 2023-09-15 Safran Seats FURNITURE ELEMENT PROVIDED WITH A NOISE-ATTENUATING COMPOSITE PANEL

Family Cites Families (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3166149A (en) * 1965-01-19 Damped-resonator acoustical panels
US3439774A (en) * 1966-01-21 1969-04-22 Boeing Co Sound energy absorbing apparatus
US4379191A (en) * 1975-08-13 1983-04-05 Rohr Industries, Inc. Honeycomb noise attenuation structure
GB2056367B (en) * 1979-07-06 1983-06-02 Rohr Industries Inc Process for producing noise attenuation panels
US4300978A (en) * 1979-07-06 1981-11-17 Rohr Industries, Inc. Bonding tool for venting honeycomb noise attenuation structure during manufacture
CH633604A5 (en) * 1979-07-24 1982-12-15 Jean Foufounis Sandwich-type panel
US4384020A (en) * 1980-12-22 1983-05-17 Rohr Industries, Inc. Honeycomb noise attenuating structures
FR2525963A1 (en) * 1982-04-29 1983-11-04 Aerospatiale METHOD FOR MANUFACTURING HIGH-PERFORMANCE THERMAL PROTECTION MATERIAL, AND MATERIAL THUS OBTAINED
EP0144318A1 (en) * 1983-05-27 1985-06-19 The Boeing Company Lightweight, fire-retardant structural panel
US4630416A (en) * 1985-05-09 1986-12-23 Haworth, Inc. Acoustical panel
US4671841A (en) * 1986-01-06 1987-06-09 Rohr Industries, Inc. Method of making an acoustic panel with a triaxial open-weave face sheet
FR2609179B1 (en) * 1986-12-30 1989-08-18 Sfim PROCESS FOR REALIZING A REFLECTIVE FACE ON AN ALVEOLAR STRUCTURE IN ORDER TO OBTAIN AN ULTRA-LIGHT MIRROR
US4824711A (en) * 1987-01-29 1989-04-25 The United States Of America As Represented By The United States National Aeronautics And Space Administration Ceramic honeycomb structures and method thereof
DE3872911T2 (en) * 1987-03-31 1992-12-03 Asahi Chemical Ind FABRICS WITH A MULTILAYER STRUCTURE AND A COMPOSITE MATERIAL CONTAINING THIS FABRIC.
US4856887A (en) * 1987-04-01 1989-08-15 Hughes Aircraft Company Lightweight silicon carbide mirror
DE3861011D1 (en) * 1987-10-30 1990-12-13 Ciba Geigy Gmbh COMPOSITE PANEL FOR SURFACING SURFACES OF CONSTRUCTIONS.
FR2630831B1 (en) * 1988-04-28 1992-10-02 Sfim ULTRA-LIGHT MIRROR
JPH02175238A (en) * 1988-12-28 1990-07-06 Jamco Corp Method for continuously molding honeycomb panel
US4990391A (en) * 1989-02-03 1991-02-05 Rohr Industries, Inc. Reticulated core to perforate sheet bonding and galvanic barrier
US4879152A (en) * 1989-02-15 1989-11-07 Green Patrick H Composite panel structure
DE3913255A1 (en) * 1989-04-22 1990-10-25 Brigitte Schmelzle Sound-absorbing ceiling cladding panel - has perforated stiffening plate glued to rear of honeycomb grille of corrugated strips
US5041323A (en) * 1989-10-26 1991-08-20 Rohr Industries, Inc. Honeycomb noise attenuation structure
DE4030529A1 (en) * 1990-09-27 1992-04-02 Dornier Gmbh METHOD FOR PRODUCING SANDWICH STRUCTURES FROM FIBER REINFORCED CERAMICS
GB9101395D0 (en) * 1991-01-22 1991-03-06 Short Brothers Plc Structural cellular component
FR2684092B1 (en) * 1991-11-21 1994-03-04 Pechiney Recherche PROCESS FOR THE PREPARATION OF LARGE SPECIFIC METAL CARBIDES FROM ACTIVATED CARBON FOAMS.
FR2710874B1 (en) * 1993-10-04 1995-12-22 Aerospatiale Rigid, self-supporting sheet material for acoustic attenuation and panel made of such material.
CN2185647Y (en) * 1993-12-31 1994-12-21 西安石油学院 Multi-sharp-toothed deep hole drill

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007060668A1 (en) 2007-12-17 2009-06-18 Airbus Deutschland Gmbh Sandwich panel for sound absorption

Also Published As

Publication number Publication date
FR2735166A1 (en) 1996-12-13
FR2735166B1 (en) 1997-08-29
CA2178148A1 (en) 1996-12-09
CN1141866A (en) 1997-02-05
CN1078844C (en) 2002-02-06
ES2147908T3 (en) 2000-10-01
EP0747547A1 (en) 1996-12-11
CA2178148C (en) 2008-01-29
DE69607783D1 (en) 2000-05-25
DE69607783T2 (en) 2000-11-23
US5888610A (en) 1999-03-30

Similar Documents

Publication Publication Date Title
EP0747547B1 (en) Method of fabrication of a plate or the like with structural and acoustic features and plate obtained this way
EP0747285B1 (en) Sandwich panel using a composite material and method of making it
CA2329832C (en) Procedure for producing an acoustically resistive layer, the resulting resistive layer, and wall using the layer
CA2441477C (en) Sound attenuation panel comprising a resistive layer with reinforced structural component
EP1355294B1 (en) Multicomponent acoustically-resistive layer for a sound-absorbing panel and panel having such a layer
EP1157372B1 (en) Method for making a sound reducing panel with resistive layer having structural property and resulting panel
CA2364951C (en) Procedure for manufacturing a protected laminated soundproofing panel and the acoustic panel produced by the procedure
EP0897174B1 (en) Sound absorbing panel featuring at least one acoustically resistive layer, and its manufacturing process
FR2721000A1 (en) Composite rectifier blade, rectifier comprising it, for anti-torque device with rotor and stator rectifier careened, and their method of manufacture.
CA2488818C (en) Method for making a soundproofing panel with at least one double resonator
EP0711652B1 (en) Process for obtaining composite panels of the sandwich type and panels so obtained
FR2939766A1 (en) CENTRAL PYLONE OF AIRCRAFT.
EP2941903B1 (en) Loudspeaker membrane and method for manufacturing such a membrane
FR2563153A1 (en) Composite panel, especially intended for aircraft furniture
WO2015082843A1 (en) Sandwich panel comprising a honeycomb structure provided with reinforcements on the edges of said structure
EP0786320B1 (en) Process for the manufacture of composite articles having high dimensional accuracy by curing with ionizing rays
CA2735953A1 (en) Reinforced composite sandwich panel
FR2710874A1 (en) Rigid sheet-like and self-supporting material for acoustic attenuation and panel made of such a material
FR2735064A1 (en) Prodn. of composite material microporous sandwich panel skins
FR3013629A1 (en) SOUND CONTROL PANEL AND AIRCRAFT
EP3575069B1 (en) Method for manufacturing an optimised sandwich panel
BE1003935A3 (en) Mica or mica paper-based laminate
EP3043347A1 (en) Soundproofing trim panel, and aircraft

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): DE ES GB IT NL

17P Request for examination filed

Effective date: 19970529

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

17Q First examination report despatched

Effective date: 19990706

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): DE ES GB IT NL

REF Corresponds to:

Ref document number: 69607783

Country of ref document: DE

Date of ref document: 20000525

ITF It: translation for a ep patent filed

Owner name: STUDIO INGG. FISCHETTI & WEBER

RAP2 Party data changed (patent owner data changed or rights of a patent transferred)

Owner name: AEROSPATIALE MATRA

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2147908

Country of ref document: ES

Kind code of ref document: T3

NLT2 Nl: modifications (of names), taken from the european patent patent bulletin

Owner name: AEROSPATIALE MATRA

GBT Gb: translation of ep patent filed (gb section 77(6)(a)/1977)

Effective date: 20001219

REG Reference to a national code

Ref country code: GB

Ref legal event code: 732E

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed
REG Reference to a national code

Ref country code: GB

Ref legal event code: IF02

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: NL

Payment date: 20090616

Year of fee payment: 14

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20090618

Year of fee payment: 14

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: ES

Payment date: 20100625

Year of fee payment: 15

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20100625

Year of fee payment: 15

REG Reference to a national code

Ref country code: NL

Ref legal event code: V1

Effective date: 20110101

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20100605

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20110101

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20100605

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 69607783

Country of ref document: DE

Effective date: 20120103

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20120103

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20120717

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20110606

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20130625

Year of fee payment: 18

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20140605