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 PDFInfo
- 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
Links
- 238000004519 manufacturing process Methods 0.000 title claims description 6
- 238000000034 method Methods 0.000 claims description 14
- 229920005989 resin Polymers 0.000 claims description 14
- 239000011347 resin Substances 0.000 claims description 14
- 238000000576 coating method Methods 0.000 claims description 13
- 239000003292 glue Substances 0.000 claims description 12
- 239000011248 coating agent Substances 0.000 claims description 10
- 239000004697 Polyetherimide Substances 0.000 claims description 7
- 239000004744 fabric Substances 0.000 claims description 7
- 239000010408 film Substances 0.000 claims description 7
- 229920001601 polyetherimide Polymers 0.000 claims description 7
- 239000003365 glass fiber Substances 0.000 claims description 5
- 238000007731 hot pressing Methods 0.000 claims description 4
- 239000004753 textile Substances 0.000 claims description 3
- 229920005992 thermoplastic resin Polymers 0.000 claims description 3
- 239000010409 thin film Substances 0.000 claims description 3
- 230000000694 effects Effects 0.000 claims description 2
- 239000010438 granite Substances 0.000 claims description 2
- 229910052500 inorganic mineral Inorganic materials 0.000 claims description 2
- 238000002360 preparation method Methods 0.000 claims description 2
- 229920002994 synthetic fiber Polymers 0.000 claims description 2
- 239000011800 void material Substances 0.000 claims description 2
- 229920006335 epoxy glue Polymers 0.000 claims 1
- 230000000977 initiatory effect Effects 0.000 claims 1
- 239000011707 mineral Substances 0.000 claims 1
- 238000005192 partition Methods 0.000 description 16
- 238000006116 polymerization reaction Methods 0.000 description 10
- 239000000853 adhesive Substances 0.000 description 7
- 230000001070 adhesive effect Effects 0.000 description 7
- 239000000835 fiber Substances 0.000 description 6
- 238000007596 consolidation process Methods 0.000 description 5
- 238000010411 cooking Methods 0.000 description 4
- 229920006332 epoxy adhesive Polymers 0.000 description 4
- 239000002313 adhesive film Substances 0.000 description 3
- 238000009826 distribution Methods 0.000 description 3
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 239000002131 composite material Substances 0.000 description 2
- 239000011888 foil Substances 0.000 description 2
- 239000011521 glass Substances 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000002557 mineral fiber Substances 0.000 description 2
- 239000012209 synthetic fiber Substances 0.000 description 2
- 241000257303 Hymenoptera Species 0.000 description 1
- 229920000784 Nomex Polymers 0.000 description 1
- 229920004738 ULTEM® Polymers 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 239000004760 aramid Substances 0.000 description 1
- 229920006231 aramid fiber Polymers 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000004043 dyeing Methods 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 230000005499 meniscus Effects 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 239000004763 nomex Substances 0.000 description 1
- 239000011120 plywood Substances 0.000 description 1
- 230000000379 polymerizing effect Effects 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 238000004321 preservation Methods 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 239000000779 smoke Substances 0.000 description 1
- 238000001228 spectrum Methods 0.000 description 1
- 239000004834 spray adhesive Substances 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 210000001519 tissue Anatomy 0.000 description 1
- 230000001988 toxicity Effects 0.000 description 1
- 231100000419 toxicity Toxicity 0.000 description 1
Images
Classifications
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
- E04B1/00—Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
- E04B1/62—Insulation or other protection; Elements or use of specified material therefor
- E04B1/74—Heat, sound or noise insulation, absorption, or reflection; Other building methods affording favourable thermal or acoustical conditions, e.g. accumulating of heat within walls
- E04B1/82—Heat, 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
- E04B1/84—Sound-absorbing elements
- E04B1/86—Sound-absorbing elements slab-shaped
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
- E04C2/30—Building 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
- E04C2/34—Building 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
- E04C2/36—Building 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
- E04C2/365—Building 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
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
- E04B1/00—Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
- E04B1/62—Insulation or other protection; Elements or use of specified material therefor
- E04B1/74—Heat, sound or noise insulation, absorption, or reflection; Other building methods affording favourable thermal or acoustical conditions, e.g. accumulating of heat within walls
- E04B2001/742—Use of special materials; Materials having special structures or shape
- E04B2001/748—Honeycomb materials
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24149—Honeycomb-like
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24273—Structurally defined web or sheet [e.g., overall dimension, etc.] including aperture
- Y10T428/24322—Composite web or sheet
- Y10T428/24331—Composite 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.
- 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.
- 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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
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)
- 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).
- Method according to Claim 1, characterised in that the skins (2, 3)consist of cloths of glass fibres impregnated with polyetherimide resin.
- Method according to Claim 1 or 2, characterised in that the two skins (2, 3) have different numbers of plies.
- 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.
- Method according to Claim 4, characterised in that the glue is a self-extinguishing glue.
- 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.
- 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.
- 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.
- Panel or the like obtained in accordance with the method according to any one of Claims 1 to 8.
- Panel according to Claim 9, characterised in that the core with a alveolar structure is a honeycomb (1).
- 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.
- 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%.
- 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.
- 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.
- 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.
- 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.
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)
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)
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)
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 |
-
1995
- 1995-06-08 FR FR9507020A patent/FR2735166B1/en not_active Expired - Fee Related
-
1996
- 1996-05-31 US US08/655,932 patent/US5888610A/en not_active Expired - Lifetime
- 1996-06-04 CA CA002178148A patent/CA2178148C/en not_active Expired - Fee Related
- 1996-06-05 DE DE69607783T patent/DE69607783T2/en not_active Expired - Lifetime
- 1996-06-05 EP EP96450012A patent/EP0747547B1/en not_active Expired - Lifetime
- 1996-06-05 ES ES96450012T patent/ES2147908T3/en not_active Expired - Lifetime
- 1996-06-07 CN CN96110380A patent/CN1078844C/en not_active Expired - Fee Related
Cited By (1)
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 |