Epsilon Composite

France

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Type PI
        Brevet 35
        Marque 10
Juridiction
        International 23
        États-Unis 16
        Canada 5
        Europe 1
Date
2026 juillet 1
2026 (AACJ) 2
2025 3
2024 6
2023 6
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Classe IPC
B29C 70/52 - Pultrusion, c.-à-d. façonnage et compression par traction continue à travers une matrice 9
B64B 1/08 - Structure de l'ossature 5
B29C 45/14 - Moulage par injection, c.-à-d. en forçant un volume déterminé de matière à mouler par une buse d'injection dans un moule ferméAppareils à cet effet en incorporant des parties ou des couches préformées, p. ex. moulage par injection autour d'inserts ou sur des objets à recouvrir 3
B29C 70/54 - Parties constitutives, détails ou accessoiresOpérations auxiliaires 3
E04B 1/58 - Assemblages pour les constructions du bâtiment en général d'éléments de construction en forme de barre 3
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Classe NICE
09 - Appareils et instruments scientifiques et électriques 7
42 - Services scientifiques, technologiques et industriels, recherche et conception 4
19 - Matériaux de construction non métalliques 3
07 - Machines et machines-outils 1
12 - Véhicules; appareils de locomotion par terre, par air ou par eau; parties de véhicules 1
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Statut
En Instance 9
Enregistré / En vigueur 36

1.

HVCRC

      
Numéro de série 99929648
Statut En instance
Date de dépôt 2026-07-08
Propriétaire EPSILON COMPOSITE (France)
Classes de Nice  ?
  • 09 - Appareils et instruments scientifiques et électriques
  • 42 - Services scientifiques, technologiques et industriels, recherche et conception

Produits et services

Electric cables; electrical transmission and distribution cables; conductor cables for high-voltage overhead power lines; composite cores, consisting primarily of both carbon fiber in a polymer matrix and glass fiber in a polymer matrix, for energy transmission and distribution cables Quality control during manufacturing, installation, maintenance and dismantling of electric cables, electric transmission and distribution cables, conductor cables for high-voltage power lines and composite cores for power transmission and distribution cables; technical supervision and inspection in the field of manufacturing, installation, maintenance and dismantling of electric cables, electric transmission and distribution cables, conductor cables for high-voltage power lines and composite cores for power transmission and distribution cables; installation and maintenance of electrical cable installations, electrical transmission and distribution cables, conductor cables for high-voltage power lines and composite cores for power transmission and distribution cables

2.

METHOD WITH INCREASED RELIABILITY FOR MANUFACTURING A COMPOSITE TUBULAR STRUCTURE COMBINING PULTRUSION AND FILAMENT WINDING

      
Numéro d'application 19257219
Statut En instance
Date de dépôt 2025-07-01
Date de la première publication 2026-01-01
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s)
  • Portoles, José
  • Chaumet, Yann

Abrégé

The present disclosure relates to a method for producing a tubular composite structure with a longitudinal axis, the method successively including a step of forming a manufacturing blank by stacking material to construct at least one tubular sandwich with a longitudinal axis, said tubular sandwich(S) comprising two filament winding layers based on raw resin and carbon fibers, and a series of pultruded spacers based on carbon fibers and at least partially cured resin, the pultruded spacers being arranged radially to the longitudinal axis between the two filament winding layers, and a step of curing the manufacturing blank to obtain the composite tubular structure.

Classes IPC  ?

  • B29C 70/52 - Pultrusion, c.-à-d. façonnage et compression par traction continue à travers une matrice
  • B29C 70/86 - Incorporation dans des couches de renforcement imprégnées cohérentes
  • B29K 63/00 - Utilisation de résines époxy comme matière de moulage
  • B29K 105/10 - Présentation, forme ou état de la matière moulée contenant des agents de renforcement, charges ou inserts de grande longueur, p. ex. ficelles, mèches, mats, tissus ou fils orientés
  • B29K 307/04 - Carbone

3.

DEVICE FOR DETECTING A DEFECT IN A STRUCTURAL ELEMENT MADE OF COMPOSITE MATERIAL

      
Numéro d'application 18859988
Statut En instance
Date de dépôt 2023-04-27
Date de la première publication 2025-12-25
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s)
  • Richard, Léo
  • Quetel, Lionel
  • Riboulet, Jean-François
  • Lyphout, Florent

Abrégé

The present invention relates to a device for detecting a defect in a structural element made of composite material. The device includes a structural element made of composite material and having an elongate shape, at least one detection optical fiber arranged inside the structural element, and a light-emitting device comprising a plurality of light sources connected to a strand of optical fibers, all of the strands being grouped into a bundle of strands.

Classes IPC  ?

  • G01N 21/88 - Recherche de la présence de criques, de défauts ou de souillures
  • G01N 21/84 - Systèmes spécialement adaptés à des applications particulières

4.

END PIECE FOR A PROFILED PART AND IN PARTICULAR FOR A GUIDE ROLLER

      
Numéro d'application 18860536
Statut En instance
Date de dépôt 2023-04-28
Date de la première publication 2025-10-09
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s) Soubaigne, Sébastien

Abrégé

An end piece for a profiled part is disclosed having a longitudinal axis ZZ, the dimensions of which allow it to be force-fitted into one end of the profiled part, the end piece including at least one cylindrical inner housing for accommodating a rotary adjustment member or a rotary working member in order to rotatably mount the profiled part on a fixed shaft, and the housing being terminated by an inwardly facing wall forming a stop for the rotary adjustment member or rotary working member. The end piece is flexible and includes, on its outer surface, a plurality of fins that project outward and extend longitudinally along the axis ZZ of the inner edge of the end piece in the direction of the outer face of the end piece, the fins being separated by grooves that extend longitudinally along the axis ZZ in the same direction as the fins.

Classes IPC  ?

  • B65G 39/02 - Adaptation des rouleaux individuels ou supports à cet effet
  • B29C 48/00 - Moulage par extrusion, c.-à-d. en exprimant la matière à mouler dans une matrice ou une filière qui lui donne la forme désiréeAppareils à cet effet
  • B29C 48/355 - Transporteurs pour les objets extrudés

5.

MULTIMATERIAL ROD WITH INSULATING FILM

      
Numéro d'application FR2025050132
Numéro de publication 2025/172676
Statut Délivré - en vigueur
Date de dépôt 2025-02-14
Date de publication 2025-08-21
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s)
  • Ferrer Goyeneche, Denis
  • Mahe, Nicolas
  • Laplassotte, Olivier
  • Portoles, José
  • Richard, Léo
  • Latron, Ambroise

Abrégé

The present invention relates to a multimaterial rod (10) comprising: - a core (16), extending in a direction of extension (AX), made of a composite material (12) based on carbon fibre, or formed of an assembly comprising a core made of a composite material (12) based on carbon fibre and a layer made of a composite material (14) based on glass fibre that surrounds the core; and - an outer shell (18) providing the core with electrical and/or UV and/or moisture insulation, wherein this outer shell (18) coating the core (16) along the direction of extension and being formed of a varnish that adheres mechanically and/or chemically to this core (16); wherein the shell (18) has an elongation at break that is substantially equal to or greater than the elongation at break of the core (16).

Classes IPC  ?

  • H01B 5/10 - Pluralité de fils ou analogues toronnés en forme de corde toronnés autour d'un espace, d'un matériau isolant ou d'un matériau conducteur dissemblable

6.

METHOD FOR DISCRIMINANT MONITORING OF A COMPOSITE MULTI-MATERIAL ASSEMBLY

      
Numéro d'application 18556659
Statut En instance
Date de dépôt 2022-04-28
Date de la première publication 2024-11-07
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s) Ferrer, Denis

Abrégé

The invention relates to a method for the discriminant monitoring of a composite multi-material assembly comprising at least one internal layer made of a first, electrically conductive composite material and a second layer made of a second, electrically insulating composite material, the second layer covering the first internal layer. The method comprises the following steps: preparing the composite multi-material assembly by exposing a portion of the internal layer constituting a first electrode; applying a second electrode to the surface of the second layer, earthing one of these electrodes; discriminant monitoring by means of generating a current between the first electrode and second electrode by applying a threshold voltage US pre-defined by calibration to be characteristic of a lack of structural defects, the appearance of a breakdown at a voltage lower than said threshold voltage US indicative of the presence of at least one structural defect in the composite assembly.

Classes IPC  ?

  • G01N 27/92 - Recherche ou analyse des matériaux par l'emploi de moyens électriques, électrochimiques ou magnétiques en recherchant la tension disruptive

7.

HIGH VOLTAGE CABLE WITH COMPOSITE CORE FOR LOW OPERATING TEMPERATURE

      
Numéro d'application 18579658
Statut En instance
Date de dépôt 2022-07-11
Date de la première publication 2024-10-17
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s) Gary, Baptiste

Abrégé

A high-voltage cable includes a composite core surrounded by an electrical conductor, wherein it is limited to 95° C.±5%, and the electrical conductor is made of hard aluminum with an aluminum ratio Ra of between 6 and 19, wherein Ra is calculated according to the following rule: Ra=Sc/Sa×100, where Sc is the cross-section of the composite core of the cable and Sa is the cross-section of the conductive aluminum of the cable. This makes it possible to obtain a cable with the same mass as current low-temperature cables, the same external diameter, at least the same mechanical strength and equivalent thermal expansion. This results in a cable in which the aluminum cross-section is increased by between 20% and 40% with the same mass.

Classes IPC  ?

  • H01B 1/24 - Matériau conducteur dispersé dans un matériau organique non conducteur le matériau conducteur comportant des compositions à base de carbone-silicium, du carbone ou du silicium
  • H01B 1/02 - Conducteurs ou corps conducteurs caractérisés par les matériaux conducteurs utilisésEmploi de matériaux spécifiés comme conducteurs composés principalement de métaux ou d'alliages
  • H01B 7/00 - Conducteurs ou câbles isolés caractérisés par la forme
  • H01B 7/18 - Protection contre les dommages provoqués par des facteurs extérieurs, p. ex. gaines ou armatures par l'usure, la contrainte mécanique ou la pression

8.

ECRC

      
Numéro d'application 235204200
Statut Enregistrée
Date de dépôt 2024-07-05
Date d'enregistrement 2026-01-30
Propriétaire EPSILON COMPOSITE (France)
Classes de Nice  ? 09 - Appareils et instruments scientifiques et électriques

Produits et services

(1) Câbles électriques; câbles électriques de transmission et de distribution; câbles conducteurs pour lignes d'alimentation électrique aérienne haute tension; noyaux composites pour câbles de transmission et de distribution d'énergie.

9.

ECRC

      
Numéro de série 79405418
Statut Enregistrée
Date de dépôt 2024-07-05
Date d'enregistrement 2025-12-02
Propriétaire EPSILON COMPOSITE (France)
Classes de Nice  ? 09 - Appareils et instruments scientifiques et électriques

Produits et services

Electric cables; electrical transmission and distribution cables; conductor cables for high-voltage overhead power lines; composite cores, consisting primarily of both carbon fiber in a polymer matrix and glass fiber in a polymer matrix, for energy transmission and distribution cables

10.

CARBOLAM

      
Numéro d'application 018987047
Statut Enregistrée
Date de dépôt 2024-02-16
Date d'enregistrement 2024-05-30
Propriétaire EPSILON COMPOSITE (France)
Classes de Nice  ? 19 - Matériaux de construction non métalliques

Produits et services

Building materials, not of metal.

11.

DEVICE FOR MECHANICAL ATTACHMENT TO THE END OF A TUBE

      
Numéro d'application 18256771
Statut En instance
Date de dépôt 2020-12-09
Date de la première publication 2024-01-25
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s)
  • Portoles, José
  • Ferrer, Denis
  • Dos Santos, Maxime

Abrégé

Attachment device including: —a conical insert in the form of a truncated cone, an internal ring which is provided with a recess in the form of a truncated cone the diameter of which narrows in the direction of the interior of the tube and the angle of which is equal to the angle of the truncated cone of the conical insert, and an external ring comprising a cylindrical portion the internal diameter of which is substantially equal to the external diameter of the tube, the external ring comprising a shoulder which partially closes an end of the external ring and which has a circular opening, the shoulder comprising an annular internal face which is intended to abut the end face of the tube and the transverse end face of the internal ring located at the side of the end of the tube.

Classes IPC  ?

  • F16B 7/02 - Assemblages de barres ou assemblages de tubes, p. ex. de section non circulaire, y compris les assemblages élastiques avec parties coniques
  • B64B 1/08 - Structure de l'ossature

12.

END PIECE FOR A PROFILED PART AND IN PARTICULAR FOR A GUIDE ROLLER

      
Numéro d'application EP2023061198
Numéro de publication 2023/213692
Statut Délivré - en vigueur
Date de dépôt 2023-04-28
Date de publication 2023-11-09
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s) Soubaigne, Sébastien

Abrégé

The invention relates to an end piece (10, 110) for a profiled part (35) having a longitudinal axis ZZ, the dimensions of which allow it to be force-fitted into one end of the profiled part, the end piece comprising at least one cylindrical inner housing (12, 14, 19) for accommodating a rotary adjustment member (20, 21, 120) or a rotary working member (30, 130) in order to rotatably mount the profiled part on a fixed shaft (50, 60), and the housing being terminated by an inwardly facing wall (11, 13) forming a stop for the rotary adjustment member or rotary working member. According to the main features of the invention, the end piece is flexible and comprises, on its outer surface, a plurality of fins that project outward and extend longitudinally along the axis ZZ of the inner edge of the end piece in the direction of the outer face of the end piece, the fins being separated by grooves (18) that extend longitudinally along the axis ZZ in the same direction as the fins.

Classes IPC  ?

  • F16C 13/02 - Paliers
  • F16C 27/02 - Paliers à contact lisse
  • F16C 27/04 - Roulements à billes ou à rouleaux, p. ex. à organes de roulement élastiques
  • F16C 27/06 - Paliers ou supports de paliers élastiques ou extensibles pour mouvement de rotation exclusivement par le moyen de parties en caoutchouc ou en un matériau analogue

13.

DEVICE FOR DETECTING A DEFECT IN A STRUCTURAL ELEMENT MADE OF COMPOSITE MATERIAL

      
Numéro d'application EP2023061123
Numéro de publication 2023/209097
Statut Délivré - en vigueur
Date de dépôt 2023-04-27
Date de publication 2023-11-02
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s)
  • Richard, Léo
  • Quetel, Lionel
  • Riboulet, Jean-François
  • Lyphout, Florent

Abrégé

The present invention relates to a device for detecting a defect in a structural element (3) made of composite material, characterized in that it comprises: - a structural element (3) made of composite material and having an elongate shape, - at least one detection optical fibre (33, 34, 35, 36) arranged inside the structural element (3), and - a light-emitting device (2) comprising a plurality of light sources (21) connected to a strand (5) of optical fibres, all of the strands (5) being grouped into a bundle (6) of strands.

Classes IPC  ?

  • G01M 5/00 - Examen de l'élasticité des structures ou ouvrages, p. ex. fléchissement de ponts ou d'ailes d'avions
  • G01M 11/08 - Test des propriétés mécaniques
  • F21V 8/00 - Utilisation de guides de lumière, p. ex. dispositifs à fibres optiques, dans les dispositifs ou systèmes d'éclairage
  • G02B 6/00 - Guides de lumièreDétails de structure de dispositions comprenant des guides de lumière et d'autres éléments optiques, p. ex. des moyens de couplage
  • G01N 21/88 - Recherche de la présence de criques, de défauts ou de souillures

14.

CORECHECK

      
Numéro d'application 1757419
Statut Enregistrée
Date de dépôt 2023-09-06
Date d'enregistrement 2023-09-06
Propriétaire EPSILON COMPOSITE (France)
Classes de Nice  ?
  • 09 - Appareils et instruments scientifiques et électriques
  • 42 - Services scientifiques, technologiques et industriels, recherche et conception

Produits et services

Electric cables; electrical transmission and distribution cables; conductor cables for high-voltage overhead power lines; composite cores for energy transmission and distribution cables. Quality control during manufacturing, installation, maintenance and dismantling of electric cables, electric transmission and distribution cables, conductor cables for high-voltage power lines and composite cores for power transmission and distribution cables; technical inspection during manufacturing, installation, maintenance and dismantling of electric cables, electric transmission and distribution cables, conductor cables for high-voltage power lines and composite cores for power transmission and distribution cables; manufacturing control, installation, maintenance and dismantling of electrical cable installations, electrical transmission and distribution cables, conductor cables for high-voltage power lines and composite cores for power transmission and distribution cables.

15.

CORECHECK

      
Numéro d'application 229200900
Statut Enregistrée
Date de dépôt 2023-10-09
Date d'enregistrement 2025-09-15
Propriétaire EPSILON COMPOSITE (France)
Classes de Nice  ?
  • 09 - Appareils et instruments scientifiques et électriques
  • 42 - Services scientifiques, technologiques et industriels, recherche et conception

Produits et services

(1) Câbles électriques; câbles électriques de transmission et de distribution; câbles conducteurs pour lignes d'alimentation électrique aérienne haute tension; noyaux composites pour câbles de transmission et de distribution d'énergie. (1) Contrôle de qualité lors de la fabrication, de l'installation, de la maintenance et du démontage de câbles électriques, câbles électriques de transmission et de distribution, câbles conducteurs pour lignes d'alimentation électrique aérienne haute tension et âmes composites pour câbles de transmission et de distribution d'énergie; contrôle technique lors de la fabrication, de l'installation, de la maintenance et du démontage de câbles électriques, câbles électriques de transmission et de distribution, câbles conducteurs pour lignes d'alimentation électrique aérienne haute tension et âmes composites pour câbles de transmission et de distribution d'énergie; contrôle de la fabrication, de l'installation, de la maintenance et du démontage d'installations de câbles électriques, câbles électriques de transmission et de distribution, câbles conducteurs pour lignes d'alimentation électrique aérienne haute tension et âmes composites pour câbles de transmission et de distribution d'énergie.

16.

CORECHECK

      
Numéro de série 79381511
Statut Enregistrée
Date de dépôt 2023-09-06
Date d'enregistrement 2025-01-28
Propriétaire EPSILON COMPOSITE (France)
Classes de Nice  ?
  • 09 - Appareils et instruments scientifiques et électriques
  • 42 - Services scientifiques, technologiques et industriels, recherche et conception

Produits et services

Electric cables; electrical transmission and distribution cables; conductor cables for high-voltage overhead power lines; composite cores, namely, armored cables for energy transmission and distribution cable Quality control during manufacturing, installation, maintenance and dismantling of electric cables, electric transmission and distribution cables, conductor cables for high-voltage power lines and composite cores for power transmission and distribution cables; technical supervision and inspection in the field of manufacturing, installation, maintenance and dismantling of electric cables, electric transmission and distribution cables, conductor cables for high-voltage power lines and composite cores for power transmission and distribution cables; installation and maintenance of electrical cable installations, electrical transmission and distribution cables, conductor cables for high-voltage power lines and composite cores for power transmission and distribution cables

17.

HIGH-VOLTAGE CABLE WITH COMPOSITE CORE FOR LOW OPERATING TEMPERATURE

      
Numéro d'application EP2022069259
Numéro de publication 2023/285350
Statut Délivré - en vigueur
Date de dépôt 2022-07-11
Date de publication 2023-01-19
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s) Gary, Baptiste

Abrégé

The invention relates to a high-voltage cable according to the invention, which comprises a composite core surrounded by an electrical conductor, characterised in that it is limited to 95°C ±5%, and in that the electrical conductor is made of hard aluminium with an aluminium ratio Ra of between 6 and 19 and preferably between 8 and 15, wherein Ra is calculated according to the following rule: Ra = Sc/Sa x 100, where Sc is the cross-section of the composite core of the cable and Sa is the cross-section of the conductive aluminium of the cable. This makes it possible to obtain a cable with the same mass as current low-temperature cables, the same external diameter, at least the same mechanical strength and equivalent thermal expansion. This results in a cable in which the aluminium cross-section is increased by between 20% and 40% with the same mass.

Classes IPC  ?

  • H01B 1/02 - Conducteurs ou corps conducteurs caractérisés par les matériaux conducteurs utilisésEmploi de matériaux spécifiés comme conducteurs composés principalement de métaux ou d'alliages

18.

ASSEMBLY OF DIAGONAL TUBES ON A MAIN TUBE OF A LATTICE BEAM MADE OF COMPOSITE MATERIAL

      
Numéro d'application FR2022050615
Numéro de publication 2022/243614
Statut Délivré - en vigueur
Date de dépôt 2022-03-31
Date de publication 2022-11-24
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s)
  • Portoles, José
  • Ferrer, Denis

Abrégé

Device for assembling secondary tubes on a main tube made of composite material, comprising a sleeve (10) mounted coaxially on the main tube and provided with two attachment regions (11, 13), the attachment regions being intended to be assembled rigidly together, the sleeve comprising means for connecting to at least one secondary tube. The inner surface part of the sleeve in contact with the outer surface of the main tube is peripheral and surrounds part of the inner surface (14) of the sleeve that is not in contact with the outer surface of the main tube so as to delimit a reserve (18) between the outer surface of the main tube and the sleeve that is filled with a filling agent, the assembly device comprising at least one projecting element (81) connected to the sleeve that is inserted into at least one cavity provided on the outer surface of the main tube, the projecting element being situated in the reserve (18).

Classes IPC  ?

  • B64B 1/00 - Aéronefs plus légers que l'air
  • F16S 3/08 - Assemblages d'éléments allongés formant ossature, p. ex. des armatures
  • F16B 2/10 - Brides ou colliers, c.-à-d. dispositifs de fixation dont le serrage est effectué par des forces effectives autres que la résistance à la déformation inhérente au matériau dont est fait le dispositif externes c.-à-d. agissant par contraction utilisant des mâchoires sur pivot
  • F16B 7/04 - Assemblages par brides ou clips
  • F16B 11/00 - Assemblage d'éléments structuraux ou parties de machines par collage ou en les pressant l'un contre l'autre, p. ex. soudage sous pression à froid
  • B64B 1/08 - Structure de l'ossature
  • F16B 7/18 - Assemblages de barres ou assemblages de tubes, p. ex. de section non circulaire, y compris les assemblages élastiques utilisant des éléments filetés
  • F16B 2/08 - Brides ou colliers, c.-à-d. dispositifs de fixation dont le serrage est effectué par des forces effectives autres que la résistance à la déformation inhérente au matériau dont est fait le dispositif externes c.-à-d. agissant par contraction utilisant des frettes ou des bandes
  • E04B 1/58 - Assemblages pour les constructions du bâtiment en général d'éléments de construction en forme de barre

19.

ASSEMBLY OF DIAGONAL TUBES ON A MAIN TUBE OF A LATTICE BEAM MADE OF COMPOSITE MATERIAL

      
Numéro de document 03216499
Statut En instance
Date de dépôt 2022-03-31
Date de disponibilité au public 2022-11-24
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s)
  • Portoles, Jose
  • Ferrer, Denis

Abrégé

Device for assembling secondary tubes on a main tube made of composite material, comprising a sleeve (10) mounted coaxially on the main tube and provided with two attachment regions (11, 13), the attachment regions being intended to be assembled rigidly together, the sleeve comprising means for connecting to at least one secondary tube. The inner surface part of the sleeve in contact with the outer surface of the main tube is peripheral and surrounds part of the inner surface (14) of the sleeve that is not in contact with the outer surface of the main tube so as to delimit a reserve (18) between the outer surface of the main tube and the sleeve that is filled with a filling agent, the assembly device comprising at least one projecting element (81) connected to the sleeve that is inserted into at least one cavity provided on the outer surface of the main tube, the projecting element being situated in the reserve (18).

Classes IPC  ?

  • B64B 1/00 - Aéronefs plus légers que l'air
  • B64B 1/08 - Structure de l'ossature
  • E04B 1/58 - Assemblages pour les constructions du bâtiment en général d'éléments de construction en forme de barre
  • F16B 2/08 - Brides ou colliers, c.-à-d. dispositifs de fixation dont le serrage est effectué par des forces effectives autres que la résistance à la déformation inhérente au matériau dont est fait le dispositif externes c.-à-d. agissant par contraction utilisant des frettes ou des bandes
  • F16B 2/10 - Brides ou colliers, c.-à-d. dispositifs de fixation dont le serrage est effectué par des forces effectives autres que la résistance à la déformation inhérente au matériau dont est fait le dispositif externes c.-à-d. agissant par contraction utilisant des mâchoires sur pivot
  • F16B 7/04 - Assemblages par brides ou clips
  • F16B 7/18 - Assemblages de barres ou assemblages de tubes, p. ex. de section non circulaire, y compris les assemblages élastiques utilisant des éléments filetés
  • F16B 11/00 - Assemblage d'éléments structuraux ou parties de machines par collage ou en les pressant l'un contre l'autre, p. ex. soudage sous pression à froid
  • F16S 3/08 - Assemblages d'éléments allongés formant ossature, p. ex. des armatures

20.

METHOD FOR DISCRIMINANT MONITORING OF A COMPOSITE MULTI-MATERIAL ASSEMBLY

      
Numéro d'application FR2022050810
Numéro de publication 2022/229562
Statut Délivré - en vigueur
Date de dépôt 2022-04-28
Date de publication 2022-11-03
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s) Ferrer, Denis

Abrégé

SSS being indicative of the presence of at least one structural defect in the composite assembly (1).

Classes IPC  ?

  • G01M 3/40 - Examen de l'étanchéité des structures ou ouvrages vis-à-vis d'un fluide par utilisation de moyens électriques, p. ex. par observation de décharges électriques
  • G01N 27/92 - Recherche ou analyse des matériaux par l'emploi de moyens électriques, électrochimiques ou magnétiques en recherchant la tension disruptive
  • G01R 31/08 - Localisation de défauts dans les câbles, les lignes de transmission ou les réseaux
  • G01R 31/11 - Localisation de défauts dans les câbles, les lignes de transmission ou les réseaux en utilisant des méthodes de réflexion d'impulsion
  • G01R 31/12 - Test de la rigidité diélectrique ou de la tension disruptive
  • G01R 31/16 - Construction de récipients de testsÉlectrodes pour de tels récipients
  • G01R 31/20 - Préparation des articles ou des spécimens pour faciliter le test
  • G01R 31/52 - Test pour déceler la présence de courts-circuits, de fuites de courant ou de défauts à la terre

21.

ANCHORAGE-TYPE REINFORCING DEVICE AND RELATED MANUFACTURING METHOD

      
Numéro d'application FR2022050521
Numéro de publication 2022/200727
Statut Délivré - en vigueur
Date de dépôt 2022-03-22
Date de publication 2022-09-29
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s) Portoles, José

Abrégé

The present invention relates to an anchorage-type reinforcing device (1) comprising: - at least one composite rigid part (11) of elongate shape comprising a first end (110) and a second end (111), said composite rigid part (11) comprising at least one bundle of continuous reinforcing fibers (112) and a polymeric matrix (113) impregnating said reinforcing fibers (112) and binding them together, and - at least one flexible part (12) constituted by free ends (114) of said reinforcing fibers, said free ends extending one at least of the first and second ends of the composite rigid part (11), said reinforcing device (1) being characterized in that the volume percentage of said reinforcing fibers (112) in said composite rigid part (11) is greater than 56% by volume, and in that said free ends of said reinforcing fibers (112) are sized and have a size content between 0.25% and 2% by weight, and preferably between 0.3% and 1.5% by weight of said free ends (114) of the reinforcing fibers (112). The present invention also relates to a method for manufacturing such a reinforcing device (1).

Classes IPC  ?

  • B29C 70/52 - Pultrusion, c.-à-d. façonnage et compression par traction continue à travers une matrice
  • E04C 5/07 - Éléments d'armature en un matériau autre qu'un métal, p. ex. en verre, en matière plastique
  • E04G 21/12 - Montage d'éléments d'armatureApplication de la précontrainte
  • E04G 23/02 - Réparation, p. ex. comblement des lézardesRestaurationModificationAgrandissement

22.

DEVICE FOR MECHANICAL ATTACHMENT TO THE END OF A TUBE

      
Numéro d'application FR2020052362
Numéro de publication 2022/123124
Statut Délivré - en vigueur
Date de dépôt 2020-12-09
Date de publication 2022-06-16
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s)
  • Portoles, José
  • Ferrer, Denis
  • Dos Santos, Maxime

Abrégé

Attachment device (10, 100) obtained by joining three components (12, 14 or 114, 18 or 118) to the end of a tube (16), comprising: - a conical insert (14, 114) in the form of a truncated cone the diameter of which narrows in the direction of the end of the tube, the conical insert (14, 114) having a receiving element (56), - an internal ring (12) which is provided with a recess (52) in the form of a truncated cone the diameter of which narrows in the direction of the interior of the tube and the angle of which is equal to the angle of the truncated cone of the conical insert, the external wall of the internal ring being cylindrical with a diameter substantially equal to the internal diameter of the tube (16), the insert being located in the recess of the internal ring. According to the main features of the invention, the attachment device comprises an external ring (18, 118) comprising a cylindrical portion the internal diameter of which is substantially equal to the external diameter of the tube, the internal wall of the cylindrical portion of the external ring being intended to come into contact with the cylindrical external wall of the tube (16), the external ring comprising a shoulder (28, 128) which partially closes an end of the external ring and which has a circular opening (38, 138), the shoulder comprising an annular internal face (48, 148) which is intended to abut the end face (26) of the tube (16) and the transverse end face (22) of the internal ring (12) located at the side of the end of the tube. The invention also relates to the method for assembling such an attachment device and the use thereof in the construction of a dirigible.

Classes IPC  ?

  • F16B 7/02 - Assemblages de barres ou assemblages de tubes, p. ex. de section non circulaire, y compris les assemblages élastiques avec parties coniques
  • B64B 1/08 - Structure de l'ossature
  • E04B 1/58 - Assemblages pour les constructions du bâtiment en général d'éléments de construction en forme de barre

23.

DEVICE FOR MECHANICAL ATTACHMENT TO THE END OF A TUBE

      
Numéro de document 03199532
Statut En instance
Date de dépôt 2020-12-09
Date de disponibilité au public 2022-06-16
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s)
  • Portoles, Jose
  • Ferrer, Denis
  • Dos Santos, Maxime

Abrégé

Attachment device (10, 100) obtained by joining three components (12, 14 or 114, 18 or 118) to the end of a tube (16), comprising: - a conical insert (14, 114) in the form of a truncated cone the diameter of which narrows in the direction of the end of the tube, the conical insert (14, 114) having a receiving element (56), - an internal ring (12) which is provided with a recess (52) in the form of a truncated cone the diameter of which narrows in the direction of the interior of the tube and the angle of which is equal to the angle of the truncated cone of the conical insert, the external wall of the internal ring being cylindrical with a diameter substantially equal to the internal diameter of the tube (16), the insert being located in the recess of the internal ring. According to the main features of the invention, the attachment device comprises an external ring (18, 118) comprising a cylindrical portion the internal diameter of which is substantially equal to the external diameter of the tube, the internal wall of the cylindrical portion of the external ring being intended to come into contact with the cylindrical external wall of the tube (16), the external ring comprising a shoulder (28, 128) which partially closes an end of the external ring and which has a circular opening (38, 138), the shoulder comprising an annular internal face (48, 148) which is intended to abut the end face (26) of the tube (16) and the transverse end face (22) of the internal ring (12) located at the side of the end of the tube. The invention also relates to the method for assembling such an attachment device and the use thereof in the construction of a dirigible.

Classes IPC  ?

  • B64B 1/08 - Structure de l'ossature
  • F16B 7/02 - Assemblages de barres ou assemblages de tubes, p. ex. de section non circulaire, y compris les assemblages élastiques avec parties coniques

24.

ECRC

      
Numéro d'application 1649334
Statut Enregistrée
Date de dépôt 2022-01-18
Date d'enregistrement 2022-01-18
Propriétaire EPSILON COMPOSITE (France)
Classes de Nice  ? 09 - Appareils et instruments scientifiques et électriques

Produits et services

Electric cables; electrical transmission and distribution cables; conductor cables for high-voltage overhead power lines; composite cores for energy transmission and distribution cables.

25.

LENGTH-ADJUSTABLE CONNECTING ROD PROVIDED WITH A RESISTIVE TORQUE DEVICE

      
Numéro d'application FR2020000032
Numéro de publication 2021/160941
Statut Délivré - en vigueur
Date de dépôt 2020-02-14
Date de publication 2021-08-19
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s)
  • Chaumet, Yann
  • Portoles, José
  • Albistur, Valentin

Abrégé

The invention relates to a length-adjustable connecting rod having a longitudinal axis (5), comprising a connecting-rod shank (50) provided with at least one internal thread (546), at least one bonding member (10, 20) comprising an external thread (106) cooperating with the internal thread of the connecting-rod shank, the screwing or unscrewing of the connecting-rod shank relative to the bonding member enabling the length of the connecting rod to be adjusted, and at least one resistive torque device between the connecting-rod shank and the bonding member, the resistive torque device comprising at least one pressing element (530, 730) and a bearing element (331), the pressing element exerting a force on the bearing element which opposes a resistance to the rotational movement of the connecting-rod shank relative to the bonding member. The bearing element (331) is rigidly connected to the bonding member (10, 20) and the pressing element (530, 730) is rigidly connected to the connecting-rod shank (50) and the force is exerted by the pressing element (530, 730) on the bearing element (331) in a transverse direction and perpendicular to the longitudinal axis (5) of the connecting rod. The invention also relates to the method for manufacturing and assembling the connecting rod.

Classes IPC  ?

26.

End-fitting for industrial machine rollers

      
Numéro d'application 16758595
Numéro de brevet 11098753
Statut Délivré - en vigueur
Date de dépôt 2018-08-16
Date de la première publication 2021-06-17
Date d'octroi 2021-08-24
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s)
  • Chaumet, Yann
  • Barbot, Yann

Abrégé

An end piece suitable for forming a spacer for a roll having two concentric tubes with axis, including spokes connecting two inner and outer cylindrical portions, and is where a fluid circuit originating from the center towards the periphery includes a first circumferential groove arranged in the inner cylindrical portion and a second circumferential groove arranged in the outer cylindrical portion connected by at least one pipe, such that the end piece makes it possible to reduce the weight of the roll by approximately 20%, to facilitate the balancing of the roll while ensuring accessibility to the inside of the roll between the two tubes and to enable easy mounting without indexing due to the circumferential grooves, and where the end piece with spokes enables access to the inside of the roll when it is mounted and thus enables both more accurate balancing than with solid end pieces that require the piercing of the outer tube and the invisibility of this balancing from the outside of the roll.

Classes IPC  ?

  • F16C 13/00 - Rouleaux, tambours, disques ou éléments analoguesPaliers ou leurs montages
  • B41F 13/10 - Cylindres de clichés
  • B41F 13/18 - Cylindres d'impression

27.

Mechanical reinforcement for a part made of composite material, in particular for a wind turbine blade of large dimensions

      
Numéro d'application 16727171
Numéro de brevet 10947855
Statut Délivré - en vigueur
Date de dépôt 2019-12-26
Date de la première publication 2020-07-09
Date d'octroi 2021-03-16
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s)
  • Lull, Stéphane
  • Ferrer, Denis
  • Portoles, José

Abrégé

The invention relates to a reinforcement, containing fibers and resin, for an element made of a composite material, particularly a wind turbine blade, characterized in that the reinforcement is produced by stacking at least two parts produced by pultrusion. A reinforcement, containing fibers and resin, for an element made of a composite material, particularly a wind turbine blade, is characterized in that the reinforcement is produced by stacking at least two parts produced by pultrusion.

Classes IPC  ?

  • F03D 1/06 - Rotors
  • F01D 5/28 - Emploi de matériaux spécifiésMesures contre l'érosion ou la corrosion
  • F03D 80/00 - Détails, composants ou accessoires non prévus dans les groupes
  • B29C 70/86 - Incorporation dans des couches de renforcement imprégnées cohérentes
  • B29L 31/08 - Pales pour rotors, stators, ventilateurs, turbines ou dispositifs analogues, p. ex. hélices

28.

TELESCOPIC STRETCHER

      
Numéro d'application IB2019059056
Numéro de publication 2020/089736
Statut Délivré - en vigueur
Date de dépôt 2019-10-23
Date de publication 2020-05-07
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s) Rey, Alexandre

Abrégé

The invention relates to a retractable stretcher (1) comprising two telescopic longitudinal members (2), a flexible canvas (4) connected to the longitudinal members (2) by a plurality of flexible connectors (5), a plurality of rings (6) arranged at the female end (7) of each of the sections (3) of the longitudinal members, said rings (6) serving as reinforcement of the female ends (7) of the longitudinal member sections (3) on which they are fastened.

Classes IPC  ?

29.

Main body of a doctor blade chamber, doctor blade chamber thereof and methods of manufacturing same

      
Numéro d'application 16629126
Numéro de brevet 11110701
Statut Délivré - en vigueur
Date de dépôt 2018-07-06
Date de la première publication 2020-04-30
Date d'octroi 2021-09-07
Propriétaire
  • BOBST LYON (France)
  • EPSILON COMPOSITE (France)
Inventeur(s)
  • Bazin, René
  • Fleury, Philippe
  • Mattrand, Julien
  • Willems, Steve Peter Daniel

Abrégé

A main body of doctor blade chambers including a first portion configured to hold a first doctor blade, a second portion configured to hold a second doctor blade, a third portion connecting the first portion and the second portion, a cavity intended to receive ink and defined at least by the first portion, the second portion and the third portion, characterized in that the main body is a single closed hollow profile extending along a longitudinal main axis X-X, the main body being made of pultruded composite material.

Classes IPC  ?

  • B41F 31/02 - Conduits, réservoirs, dispositifs d'alimentation ou de réglage du débit
  • B29C 70/52 - Pultrusion, c.-à-d. façonnage et compression par traction continue à travers une matrice
  • B29L 31/00 - Autres objets particuliers

30.

END-FITTING FOR INDUSTRIAL MACHINE ROLLERS

      
Numéro d'application FR2018052069
Numéro de publication 2019/081823
Statut Délivré - en vigueur
Date de dépôt 2018-08-16
Date de publication 2019-05-02
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s)
  • Chaumet, Yann
  • Barbot, Yann

Abrégé

The present invention concerns an end-fitting (2) intended to constitute a spacer for a roller consisting of two concentric tubes (10, 11) of axis xx', comprising spokes (20) linking two inner (201) and outer (200) cylindrical parts, characterised in that a fluid circuit extending from the centre towards the periphery comprises a first circumferential groove (50) arranged in the inner cylindrical part (201) and a second circumferential groove (41) arranged in the outer cylindrical part (200), linked by at least one pipe (22). This end-fitting (2) helps reduce the weight of the roller by approximately 20%, assists in the balancing of the roller by ensuring the inside of the roller is accessible between the two tubes (10, 11) and allows easy, index-free assembly as a result of the circumferential grooves (41, 50). An end-fitting with spokes allows access to the inside of the roller when it is mounted, and thus both allows finer balancing than with solid end-fittings which require the outer tube to be pierced, and allows this balancing to be invisible from the outside of the roller.

Classes IPC  ?

31.

MAIN BODY OF DOCTOR BLADE CHAMBER, DOCTOR BLADE CHAMBER THEREOF AND METHODS OF MANUFACTURING SAME

      
Numéro d'application FR2018051702
Numéro de publication 2019/008295
Statut Délivré - en vigueur
Date de dépôt 2018-07-06
Date de publication 2019-01-10
Propriétaire
  • BOBST LYON (France)
  • EPSILON COMPOSITE (France)
Inventeur(s)
  • Bazin, René
  • Fleury, Philippe
  • Mattrand, Julien
  • Willems, Steve Peter Daniel

Abrégé

The invention relates to a main body (2) of doctor blade chambers (1) comprising a first portion (2a) configured to hold a first doctor blade (3), a second portion (2b) configured to hold a second doctor blade (4), a third portion (2c) connecting the first portion (2a) and the second portion (2b), a cavity (2e) intended to receive ink and defined at least by the first portion (2a), the second portion (2b) and the third portion (2c), characterised in that the main body (2) is a single closed hollow profile extending along a longitudinal main axis X-X, the main body (2) being made of pultruded composite material.

Classes IPC  ?

  • B41F 31/02 - Conduits, réservoirs, dispositifs d'alimentation ou de réglage du débit
  • B29C 70/52 - Pultrusion, c.-à-d. façonnage et compression par traction continue à travers une matrice

32.

PROFILED MEMBER WITH A TEAR STRIP

      
Numéro d'application FR2017053180
Numéro de publication 2018/109297
Statut Délivré - en vigueur
Date de dépôt 2017-11-20
Date de publication 2018-06-21
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s)
  • Ferrer, Denis
  • Latron, Ambroise

Abrégé

A profiled member (1) having two faces (12, 13) and having at least one tear strip (2) with two edges (20, 21) arranged on and adhered to one face (12, 13) of said profiled member (1), the tear strip (2) having at least one non-adhered edge (20). The non-adhered edge (20) makes it possible not only to more easily take hold of and remove the tear strip, but also prevents a piece of the tear strip (2) from remaining on the profile member (1) and hindering the adhering of the profiled members to each other. The two edges (20, 21) of the tear strip (2) may be non-adhered, and, when the profile member (1) is covered by a tear strip (2) on each face, the two tear strips (2, 2') are each non-adhered on at least one side. The profile member can be either flat or circular.

Classes IPC  ?

  • B29C 70/54 - Parties constitutives, détails ou accessoiresOpérations auxiliaires
  • B29C 70/52 - Pultrusion, c.-à-d. façonnage et compression par traction continue à travers une matrice

33.

Hollow profile member such as a tube made of thermosetting composite materials and corresponding method

      
Numéro d'application 15579182
Numéro de brevet 10987836
Statut Délivré - en vigueur
Date de dépôt 2016-04-19
Date de la première publication 2018-05-10
Date d'octroi 2021-04-27
Propriétaire
  • EPSILON COMPOSITE (France)
  • SOMOCAP (France)
Inventeur(s)
  • Lull, Stéphane
  • Latron, Ambroise
  • Sorhouet, Fabrice
  • Nadeau, Jérôme
  • Clerc, Thomas

Abrégé

A method for overmolding a thermoplastic tip onto a hollow profile member made of thermosetting composite and to an assembly including a thermosetting profile member and a thermoplastic tip, wherein it includes machining the shape of the profile member made of thermosetting composite on the injection region; positioning a cap in the profile member; thermally conditioning the profile assembly and the cap; and injecting the tip with thermoplastic composite in order to create the junction of the profile member, the cap and the tip.

Classes IPC  ?

  • B29C 45/14 - Moulage par injection, c.-à-d. en forçant un volume déterminé de matière à mouler par une buse d'injection dans un moule ferméAppareils à cet effet en incorporant des parties ou des couches préformées, p. ex. moulage par injection autour d'inserts ou sur des objets à recouvrir
  • F16C 3/02 - ArbresManivelles

34.

Tube having a hybrid-type structure, in particular for an aircraft seat

      
Numéro d'application 15500960
Numéro de brevet 10343780
Statut Délivré - en vigueur
Date de dépôt 2015-07-16
Date de la première publication 2017-08-24
Date d'octroi 2019-07-09
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s)
  • Portoles, Jose
  • Nogues, Dominique
  • Landais, Matthieu

Abrégé

A hybrid tube, in particular for an aircraft seat structure includes ribs intended to receive the hybrid tube. The hybrid tube includes a monolithic carbon tube and at least one sleeve made from a ductile material and connected to the carbon tube by means of gluing, shrink-fitting or over-molding.

Classes IPC  ?

35.

LONGITUDINAL REINFORCING PROFILE FOR FLEXIBLE TUBULAR PIPE

      
Numéro d'application EP2016082657
Numéro de publication 2017/109221
Statut Délivré - en vigueur
Date de dépôt 2016-12-23
Date de publication 2017-06-29
Propriétaire
  • TECHNIP FRANCE (France)
  • EPSILON COMPOSITE (France)
Inventeur(s)
  • Lull, Stéphane
  • Portoles, José
  • Do, Anh Tuan

Abrégé

The invention relates to a composite longitudinal reinforcing profile (50) manufactured by pultrusion, comprising longitudinal carbon fibers (52) embedded in a polyepoxide resinous matrix (54) obtained by polymerization of a thermosetting blend comprising an epoxide prepolymer with at least one curing agent and optionally a catalyst. The epoxide prepolymer is a DiGlycidyl Ether of Bisphenol A (DGEBA) or a DiGlycidyl Ether of Bisphenol F (DGEBF) or a TetraGlycidyl Methylene DiAniline (TGMDA) and the at least one curing agent is a cycloaliphatic amine or an aromatic amine or a mixture of a cycloaliphatic amine with an aromatic amine .

Classes IPC  ?

  • C08G 59/50 - Amines
  • B29C 70/52 - Pultrusion, c.-à-d. façonnage et compression par traction continue à travers une matrice
  • B29D 99/00 - Matière non prévue dans les autres groupes de la présente sous-classe

36.

HOLLOW PROFILE MEMBER SUCH AS A TUBE MADE OF THERMOSETTING COMPOSITE MATERIALS AND CORRESPONDING METHOD

      
Numéro de document 02987540
Statut Délivré - en vigueur
Date de dépôt 2016-04-19
Date de disponibilité au public 2016-12-08
Date d'octroi 2022-01-11
Propriétaire
  • EPSILON COMPOSITE (France)
  • SOMOCAP (France)
Inventeur(s)
  • Lull, Stephane
  • Latron, Ambroise
  • Sorhouet, Fabrice
  • Nadeau, Jerome
  • Clerc, Thomas

Abrégé

The present invention relates to a method for overmoulding a thermoplastic tip (4, 5) onto a hollow profile member (1) made of thermosetting composite and to an assembly including a thermosetting profile member (1) and a thermoplastic tip (4, 5), the method being characterised in that it comprises the following steps: machining the shape of the profile member (1) made of thermosetting composite on the injection region; positioning a cap (2, 3) in the profile member (1); thermally conditioning the profile assembly (1) and the cap (2, 3); injecting the tip (4, 5) with thermoplastic composite in order to create the junction of the profile member (1), the cap (2, 3) and the tip (4, 5).

Classes IPC  ?

  • B29C 45/14 - Moulage par injection, c.-à-d. en forçant un volume déterminé de matière à mouler par une buse d'injection dans un moule ferméAppareils à cet effet en incorporant des parties ou des couches préformées, p. ex. moulage par injection autour d'inserts ou sur des objets à recouvrir

37.

HOLLOW PROFILE MEMBER SUCH AS A TUBE MADE OF THERMOSETTING COMPOSITE MATERIALS AND CORRESPONDING METHOD

      
Numéro d'application EP2016058674
Numéro de publication 2016/192888
Statut Délivré - en vigueur
Date de dépôt 2016-04-19
Date de publication 2016-12-08
Propriétaire
  • EPSILON COMPOSITE (France)
  • SOMOCAP (France)
Inventeur(s)
  • Lull, Stéphane
  • Latron, Ambroise
  • Sorhouet, Fabrice
  • Nadeau, Jérôme
  • Clerc, Thomas

Abrégé

The present invention relates to a method for overmoulding a thermoplastic tip (4, 5) onto a hollow profile member (1) made of thermosetting composite and to an assembly including a thermosetting profile member (1) and a thermoplastic tip (4, 5), the method being characterised in that it comprises the following steps: machining the shape of the profile member (1) made of thermosetting composite on the injection region; positioning a cap (2, 3) in the profile member (1); thermally conditioning the profile assembly (1) and the cap (2, 3); injecting the tip (4, 5) with thermoplastic composite in order to create the junction of the profile member (1), the cap (2, 3) and the tip (4, 5).

Classes IPC  ?

  • B29C 45/14 - Moulage par injection, c.-à-d. en forçant un volume déterminé de matière à mouler par une buse d'injection dans un moule ferméAppareils à cet effet en incorporant des parties ou des couches préformées, p. ex. moulage par injection autour d'inserts ou sur des objets à recouvrir

38.

TUBE HAVING A HYBRID-TYPE STRUCTURE, IN PARTICULAR FOR AN AIRCRAFT SEAT

      
Numéro d'application FR2015051948
Numéro de publication 2016/016538
Statut Délivré - en vigueur
Date de dépôt 2015-07-16
Date de publication 2016-02-04
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s)
  • Portoles, José
  • Nogues, Dominique
  • Landais, Matthieu

Abrégé

The invention relates to a hybrid tube (22), in particular for an aircraft seat structure S, said structure comprising ribs (10) intended to receive the hybrid tube (22), said hybrid tube (22) including a monolithic carbon tube (24) and at least one sleeve (26) made from a ductile material and connected to the carbon tube by means of gluing, shrink-fitting or over-moulding.

Classes IPC  ?

  • B64D 11/06 - Aménagements ou adaptations des sièges

39.

Mechanical reinforcement for a part made of composite material, in particular for a wind turbine blade of large dimensions

      
Numéro d'application 14004657
Numéro de brevet 10544688
Statut Délivré - en vigueur
Date de dépôt 2012-03-09
Date de la première publication 2014-01-02
Date d'octroi 2020-01-28
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s)
  • Lull, Stephane
  • Ferrer, Denis
  • Portoles, Jose

Abrégé

The invention relates to a reinforcement, containing fibers and resin, for an element made of a composite material, particularly a wind turbine blade, characterized in that said reinforcement is produced by stacking at least two parts produced by pultrusion. A reinforcement, containing fibers and resin, for an element made of a composite material, particularly a wind turbine blade, is characterized in that the reinforcement is produced by stacking at least two parts produced by pultrusion.

Classes IPC  ?

  • F01D 5/28 - Emploi de matériaux spécifiésMesures contre l'érosion ou la corrosion
  • F03D 80/00 - Détails, composants ou accessoires non prévus dans les groupes

40.

IMPROVED METHOD FOR PULTRUSION BY VIBRATION AND DEVICE FOR IMPLEMENTING THE METHOD

      
Numéro d'application FR2012053045
Numéro de publication 2013/093369
Statut Délivré - en vigueur
Date de dépôt 2012-12-21
Date de publication 2013-06-27
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s)
  • Pitie, Kévin
  • Portoles, José
  • Carrere, Noël
  • Louart, Frédéric

Abrégé

The invention relates to a method for manufacturing a part made of a composite material by pultrusion, the method consisting of manufacturing a continuous profile section (P) made of a composite material from a reinforcement (R) impregnated with a matrix and pulled through a die (10), which gradually shapes the composite material into the cross-section of the profile section (P) to be manufactured, the manufacturing method including at least three consecutive steps performed in the die (10): a first step of starting to shape the composite material, an intermediate step of starting to harden the matrix, and a final step of finishing the hardening of the matrix and finishing the shaping of the composite material, the manufacturing method being characterised in that vibrations are applied to the die during the first and/or final step, and in that no vibrations are applied to the die during the intermediate step. The invention also relates to a die for implementing said method, to a pultrusion manufacturing line including said die, and to a part made of a composite material obtained by said method.

Classes IPC  ?

  • B29C 70/52 - Pultrusion, c.-à-d. façonnage et compression par traction continue à travers une matrice

41.

Method for the continuous production of a connecting part made from composite material

      
Numéro d'application 13637060
Numéro de brevet 08808488
Statut Délivré - en vigueur
Date de dépôt 2011-03-24
Date de la première publication 2013-01-24
Date d'octroi 2014-08-19
Propriétaire Epsilon Composite (France)
Inventeur(s)
  • Nogues, Dominique
  • Louart, Frederic
  • Maumus, Jean-Pierre

Abrégé

A method for producing a connecting part (30), such as a connecting rod for an aircraft, made from a composite material, the connecting part including at least one hollow body (32) and at least one yoke (34) at each of the ends (36) of the body (32), is characterized in that the body (32) and the yokes (34) of the connecting part (30) are produced from a single section (P, P1, P2) made from a composite material and obtained using a continuous production process.

Classes IPC  ?

  • B29C 70/52 - Pultrusion, c.-à-d. façonnage et compression par traction continue à travers une matrice
  • B29C 70/54 - Parties constitutives, détails ou accessoiresOpérations auxiliaires
  • F16C 7/02 - Structure des bielles de longueur fixe
  • B29L 31/06 - Tiges, p. ex. bielles

42.

EPSILON COMPOSITE

      
Numéro d'application 1129321
Statut Enregistrée
Date de dépôt 2012-03-16
Date d'enregistrement 2012-03-16
Propriétaire EPSILON COMPOSITE (France)
Classes de Nice  ?
  • 07 - Machines et machines-outils
  • 12 - Véhicules; appareils de locomotion par terre, par air ou par eau; parties de véhicules
  • 19 - Matériaux de construction non métalliques
  • 22 - Cordes; filets; tentes, auvents, voiles et sacs; matières de rembourrage

Produits et services

Parts of machine tools of composite materials made with carbon fiber; parts of robots (machines) of composite materials made with carbon fiber; rollers of composite materials made with carbon fiber for printing (machines); rollers of composite materials for conveyors (machines); rollers of composite materials for transferring cargo; axles for machines; machine frames of composite materials; wind turbine blades of composite materials made with carbon fiber. Structural connecting rods for aircraft, not of metal; structural connecting rods for aircraft, of composite materials made with carbon fiber. Non-metallic building materials; building materials made with carbon fiber; building frameworks of composite materials made with carbon fiber; non-metallic profiles; profiles, not of metal, made with carbon fiber; posts and girders, not of metal; posts and girders of composite materials made with carbon fiber; non-metal props; struts of composite materials made with carbon fiber; masts poles not of metal; masts, belts, walers (not of metal), ribs (not of metal), reinforcements (not of metal) of composite materials made with carbon fiber; riser pipes made with carbon fiber; tubes, pipes and pipework, not of metal, made with carbon fiber; protective envelopes, not of metal, made with carbon fiber. Non-metallic cable; umbilicals made with carbon fiber; frames made with carbon fiber for undersea cables.

43.

MECHANICAL REINFORCEMENT FOR A PART MADE OF A COMPOSITE MATERIAL, PARTICULARLY A LARGE WIND-TURBINE BLADE

      
Numéro d'application FR2012050497
Numéro de publication 2012/123667
Statut Délivré - en vigueur
Date de dépôt 2012-03-09
Date de publication 2012-09-20
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s)
  • Lull, Stéphane
  • Ferrer, Denis
  • Portoles, José

Abrégé

The invention relates to a reinforcement (26), containing fibers and resin, for an element made of a composite material, particularly a wind turbine blade, characterized in that said reinforcement (26) is produced by stacking at least two parts (30) produced by pultrusion.

Classes IPC  ?

  • F03D 1/06 - Rotors
  • F03D 11/00 - Détails, parties constitutives ou accessoires non couverts par les autres groupes de la présente sous-classe ou présentant un intérêt autre que celui visé par ces groupes

44.

METHOD FOR THE CONTINUOUS PRODUCTION OF A CONNECTING PART MADE FROM COMPOSITE MATERIAL

      
Numéro d'application FR2011050626
Numéro de publication 2011/117546
Statut Délivré - en vigueur
Date de dépôt 2011-03-24
Date de publication 2011-09-29
Propriétaire EPSILON COMPOSITE (France)
Inventeur(s)
  • Nogues, Dominique
  • Louart, Frédéric
  • Maumus, Jean Pierre

Abrégé

The invention relates to a method for producing a connecting part (30), such as a connecting rod for an aircraft, made from a composite material, said connecting part comprising at least one hollow body (32) and at least one yoke (34) at each of the ends (36) of the body (32), characterised in that the body (32) and the yokes (34) of the connecting part (30) are produced from a single section (P, P1, P2) made from a composite material and obtained using a continuous production process.

Classes IPC  ?

  • B29C 70/52 - Pultrusion, c.-à-d. façonnage et compression par traction continue à travers une matrice
  • B29C 70/54 - Parties constitutives, détails ou accessoiresOpérations auxiliaires
  • F16C 7/00 - Bielles ou organes de liaisons similaires pivotant aux deux extrémitésStructure des pieds de bielles

45.

EPSILON COMPOSITE

      
Numéro d'application 783161
Statut Enregistrée
Date de dépôt 2002-04-09
Date d'enregistrement 2002-04-09
Propriétaire EPSILON COMPOSITE (France)
Classes de Nice  ? 19 - Matériaux de construction non métalliques

Produits et services

Composite materials, namely composite building materials.