Hexcel Corporation

United States of America

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IPC Class
C08J 5/24 - Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs 100
C08L 63/00 - Compositions of epoxy resinsCompositions of derivatives of epoxy resins 55
C08J 5/04 - Reinforcing macromolecular compounds with loose or coherent fibrous material 49
G10K 11/172 - Methods or devices for protecting against, or for damping, noise or other acoustic waves in general using resonance effects 36
B32B 5/02 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by structural features of a layer comprising fibres or filaments 34
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17 - Rubber and plastic; packing and insulating materials 69
24 - Textiles and textile goods 31
01 - Chemical and biological materials for industrial, scientific and agricultural use 24
06 - Common metals and ores; objects made of metal 22
12 - Land, air and water vehicles; parts of land vehicles 22
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1.

Analytical Method for Preparing PEKK for SLS Process

      
Application Number 18512268
Status Pending
Filing Date 2023-11-17
First Publication Date 2025-05-22
Owner Hexcel Corporation (USA)
Inventor
  • Grulke, David
  • Thomsen, Emily

Abstract

A method of preparing a polymer powder composition suitable for selective laser sintering and a powder composition obtained from the same. The polymer composition comprising at least two polyetherketoneketone polymorphs, each of the polymorphs having a different melting peak in a melting temperature range. The polymer is heated at a temperature below the lowest of the polymorphs melting peaks thereby decreasing the melting temperature range of the polymer composition. The treatment is especially useful with Cake B PEKK powder, which is otherwise unusable in SLS. Parts built from the treated powder using SLS have reduced surface anomalies and are easier to remove from the Cake bed.

IPC Classes  ?

  • C08J 3/00 - Processes of treating or compounding macromolecular substances
  • B29C 64/153 - Processes of additive manufacturing using only solid materials using layers of powder being selectively joined, e.g. by selective laser sintering or melting
  • B29K 71/00 - Use of polyethers as moulding material

2.

ANALYTICAL METHOD FOR PREPARING PEKK FOR SLS PROCESS

      
Application Number US2024055761
Publication Number 2025/106564
Status In Force
Filing Date 2024-11-13
Publication Date 2025-05-22
Owner HEXCEL CORPORATION (USA)
Inventor
  • Grulke, David
  • Thomsen, Emily

Abstract

A method of preparing a polymer powder composition suitable for selective laser sintering and a powder composition obtained from the same. The polymer composition comprising at least two polyetherketoneketone polymorphs, each of the polymorphs having a different melting peak in a melting temperature range. The polymer is heated at a temperature below the lowest of the polymorphs melting peaks thereby decreasing the melting temperature range of the polymer composition. The treatment is especially useful with Cake B PEKK powder, which is otherwise unusable in SLS. Parts built from the treated powder using SLS have reduced surface anomalies and are easier to remove from the Cake bed.

IPC Classes  ?

3.

SURFACING MATERIAL

      
Application Number 18686634
Status Pending
Filing Date 2022-09-05
First Publication Date 2025-05-01
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor
  • Tipler, Ben
  • Whiter, Mark

Abstract

There is provided a surfacing material comprising an ultraviolet (UV) resistant polymer layer, a thermocurable or thermoplastic resin layer and a fibrous support, wherein a first surface of the UV resistant polymer layer forms an outermost surface of the surfacing material and the second surface of the UV resistant polymer layer contacts a first surface of the thermocurable or thermoplastic resin layer, and the second surface of the thermocurable or thermoplastic resin layer contacts a first surface of the fibrous support. There is also provided methods of forming cured composite structures having an ultraviolet resistant outer surface utilising a surfacing material of the invention, and cured composite structures incorporating a UV resistant surfacing layer of the invention.

IPC Classes  ?

  • B32B 7/025 - Electric or magnetic properties
  • B32B 5/02 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by structural features of a layer comprising fibres or filaments
  • B32B 15/02 - Layered products essentially comprising metal in a form other than a sheet, e.g. wire, particles
  • B32B 15/14 - Layered products essentially comprising metal next to a fibrous or filamentary layer
  • B32B 15/20 - Layered products essentially comprising metal comprising aluminium or copper
  • B32B 27/08 - Layered products essentially comprising synthetic resin as the main or only constituent of a layer next to another layer of a specific substance of synthetic resin of a different kind
  • B32B 27/12 - Layered products essentially comprising synthetic resin next to a fibrous or filamentary layer
  • B32B 27/38 - Layered products essentially comprising synthetic resin comprising epoxy resins
  • B32B 27/40 - Layered products essentially comprising synthetic resin comprising polyurethanes

4.

A PREPREG, A PROCESS FOR ITS MANUFACTURE AND COMPOSITE MATERIALS MADE THEREFROM

      
Application Number GB2024052658
Publication Number 2025/083404
Status In Force
Filing Date 2024-10-17
Publication Date 2025-04-24
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor
  • Russell, Benjamin
  • Ramsdale-Capper, Roderick

Abstract

A prepreg comprising a structural layer of electrically conductive fibres having interstices therebetween, the structural layer having a first outer face and an essentially parallel second outer face, the faces each defining an x-y plane separated from each other by a distance equal to the thickness of the structural layer in a z-direction, orthogonal to the x-y plane; the electrically conductive fibres being parallel to the x-y planes; the prepreg comprising resin impregnated within the structural layer and present within the interstices between the fibres; and a first layer of resin in an x-y plane and in contact with the first outer face of the structural layer having a thickness in the z-direction; wherein a number of electrically conductive fibre ends deviate from being parallel to the x-y planes, extend out of the structural layer and into the z-direction, the deviating fibres entering and passing through essentially the entire thickness of the first layer of resin.

IPC Classes  ?

  • C08J 5/04 - Reinforcing macromolecular compounds with loose or coherent fibrous material
  • B29C 70/88 - Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced
  • B32B 5/06 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by structural features of a layer comprising fibres or filaments characterised by a fibrous layer needled to another layer, e.g. of fibres, of paper
  • B32B 27/04 - Layered products essentially comprising synthetic resin as impregnant, bonding, or embedding substance
  • C08J 5/24 - Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs

5.

THERMALLY CURABLE RESIN BLEND AND ITS USE IN COMPOSITE MATERIALS

      
Application Number GB2024052243
Publication Number 2025/062112
Status In Force
Filing Date 2024-08-29
Publication Date 2025-03-27
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor Whiter, Mark

Abstract

A thermally curable resin blend, comprising a) from 50 to 90 wt% cycloaliphatic curable epoxy resin having an epoxy equivalent weight of greater than 350, b) from 2 to 25 wt% of a tri- or tetra- functional epoxy reactive diluent having an epoxy equivalent weight of less than 200, and c) a curing agent; a process of thermally curing such a resin blend, the cured resin, a prepreg impregnated with the curable resin blend, and a composite material obtainable by curing such a prepreg.

IPC Classes  ?

  • C08G 59/24 - Di-epoxy compounds carbocyclic
  • C08G 59/38 - Epoxy compounds containing three or more epoxy groups together with di-epoxy compounds

6.

TOWPLY

      
Serial Number 99020584
Status Pending
Filing Date 2025-01-28
Owner Hexcel Corporation ()
NICE Classes  ? 17 - Rubber and plastic; packing and insulating materials

Goods & Services

Combination of continuous or discontinuous reinforcement fibers in the form of tape, fabric, non-woven, mat, or rovings impregnated with a thermoset, thermoplastic or other matrix material for use as a composite material; preimpregnated reinforcement fiber fabrics comprised of carbon, glass and aramid for use in the aerospace, space and defense, energy, transportation, automotive, machinery, tooling, sports and athletics, building and construction, and marine industries

7.

LIGHTNING STRIKE SURFACING MATERIAL

      
Application Number GB2024051606
Publication Number 2025/017271
Status In Force
Filing Date 2024-06-24
Publication Date 2025-01-23
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor Tipler, Ben

Abstract

There is provided a surfacing material comprising: a) a fibrous support layer having a first surface and an opposing second surface, a first edge and an opposing second edge, and first and second ends; and5 b) a lightning strike protection (LSP) layer having a first surface and an opposing second surface, a first edge and an opposing second edge, and first and second ends; wherein the first surface of the LSP layer contacts the second surface of the fibrous support layer, and the first edge of the LSP layer extends beyond the 10 first edge of the fibrous support layer. There is also provided methods for manufacturing a cured composite structure using the materials of the invention.

IPC Classes  ?

  • B32B 3/02 - Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions
  • B32B 3/04 - Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions characterised by a layer folded at the edge, e.g. over another layer
  • B32B 3/06 - Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions for securing layers togetherLayered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions for attaching the product to another member, e.g. to a support
  • B32B 3/30 - Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layerLayered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by a layer with cavities or internal voids characterised by a layer formed with recesses or projections, e.g. grooved, ribbed
  • B32B 5/02 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by structural features of a layer comprising fibres or filaments
  • B32B 5/26 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by the presence of two or more layers which comprise fibres, filaments, granules, or powder, or are foamed or specifically porous one layer being a fibrous or filamentary layer another layer also being fibrous or filamentary
  • B32B 7/05 - Interconnection of layers the layers not being connected over the whole surface, e.g. discontinuous connection or patterned connection
  • B32B 15/02 - Layered products essentially comprising metal in a form other than a sheet, e.g. wire, particles
  • B32B 15/14 - Layered products essentially comprising metal next to a fibrous or filamentary layer
  • B32B 15/20 - Layered products essentially comprising metal comprising aluminium or copper
  • B32B 27/36 - Layered products essentially comprising synthetic resin comprising polyesters
  • B32B 27/38 - Layered products essentially comprising synthetic resin comprising epoxy resins
  • B32B 27/40 - Layered products essentially comprising synthetic resin comprising polyurethanes
  • B32B 27/42 - Layered products essentially comprising synthetic resin comprising condensation resins of aldehydes, e.g. with phenols, ureas or melamines

8.

HEXSHAPE

      
Serial Number 99014388
Status Pending
Filing Date 2025-01-22
Owner Hexcel Corporation ()
NICE Classes  ? 24 - Textiles and textile goods

Goods & Services

Woven fabrics and non-woven textile fabrics used to manufacture reinforcements for composite materials in aerospace, space and defense, recreation, electrical, architectural, transportation, marine and general industrial fields; Woven and non-woven textile fabrics comprised of glass, carbon and aramid used to manufacture reinforcements for composite materials in aerospace, space and defense, military, marine, tooling, recreation, athletic equipment, electrical, architectural, construction, building, transportation, automotive, marine and general industrial fields

9.

REINFORCING MATERIAL COMPRISING A POROUS LAYER MADE OF A REACTIVE THERMOPLASTIC POLYMER AND ASSOCIATED METHODS

      
Application Number 18702740
Status Pending
Filing Date 2022-10-20
First Publication Date 2024-12-12
Owner HEXCEL REINFORCEMENTS SASU (France)
Inventor
  • Benethuiliere, Thibaut
  • Viard, Andréa
  • Pineau, Quentin
  • Dang, Patrick

Abstract

The present invention concerns a reinforcing material comprising at least one fibrous reinforcement associated on at least one of its faces with a thermoplastic porous layer, said thermoplastic porous layer(s) representing at most 10% of the total mass of the reinforcing material, preferably from 0.5 to 10% of the total mass of the reinforcing material, and more preferably from 2 to 6% of the total mass of the reinforcing material, characterized in that said thermoplastic porous layer or each of said thermoplastic porous layers present comprises a so-called reactive thermoplastic polymer or consists of one or more reactive thermoplastic polymers, a reactive thermoplastic polymer carrying —NH2 functions in an amount greater than 0.15 meq/g of reactive thermoplastic polymer and/or carrying —COOH functions in an amount greater than 0.20 meq/g of reactive thermoplastic polymer. The present invention concerns a reinforcing material comprising at least one fibrous reinforcement associated on at least one of its faces with a thermoplastic porous layer, said thermoplastic porous layer(s) representing at most 10% of the total mass of the reinforcing material, preferably from 0.5 to 10% of the total mass of the reinforcing material, and more preferably from 2 to 6% of the total mass of the reinforcing material, characterized in that said thermoplastic porous layer or each of said thermoplastic porous layers present comprises a so-called reactive thermoplastic polymer or consists of one or more reactive thermoplastic polymers, a reactive thermoplastic polymer carrying —NH2 functions in an amount greater than 0.15 meq/g of reactive thermoplastic polymer and/or carrying —COOH functions in an amount greater than 0.20 meq/g of reactive thermoplastic polymer. The invention also concerns processes for manufacturing such reinforcement materials, preforms, processes for manufacturing composite parts and composite parts using such reinforcement materials.

IPC Classes  ?

  • B32B 5/02 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by structural features of a layer comprising fibres or filaments
  • B32B 3/08 - Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions characterised by added members at particular parts
  • B32B 5/06 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by structural features of a layer comprising fibres or filaments characterised by a fibrous layer needled to another layer, e.g. of fibres, of paper
  • B32B 5/26 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by the presence of two or more layers which comprise fibres, filaments, granules, or powder, or are foamed or specifically porous one layer being a fibrous or filamentary layer another layer also being fibrous or filamentary
  • C08J 5/24 - Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
  • D04H 1/4334 - Polyamides
  • D04H 3/16 - Non woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between thermoplastic yarns or filaments produced by welding with bonds between thermoplastic filaments produced in association with filament formation, e.g. immediately following extrusion

10.

USE OF HYDROXY SUBSTITUTED URONES AS CURE ACCELERATORS

      
Application Number EP2024056422
Publication Number 2024/194067
Status In Force
Filing Date 2024-03-11
Publication Date 2024-09-26
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor Mason, Christopher

Abstract

Urone compounds containing at least 2 orthohydroxyphenyl urea units where the units are coupled via a divalent or multivalent bridging group which may be heterointerrupted are used as cure accelerators for thermosetting resin systems particularly fibre filled epoxy resin.

IPC Classes  ?

  • C08G 59/40 - Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups characterised by the curing agents used
  • C08G 59/68 - Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups characterised by the catalysts used
  • C08J 5/24 - Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
  • C08L 63/00 - Compositions of epoxy resinsCompositions of derivatives of epoxy resins

11.

CARBON FIBERS HAVING IMPROVED STRENGTH AND MODULUS AND AN ASSOCIATED METHOD AND APPARATUS FOR PREPARING SAME

      
Application Number 18570185
Status Pending
Filing Date 2022-08-19
First Publication Date 2024-09-12
Owner Hexcel Corporation (USA)
Inventor
  • Ruminski, Anne
  • Ferrin, Peter

Abstract

The invention is directed to carbon fibers having high tensile strength. The invention also provides a method and apparatus for making the carbon fibers. The method comprises advancing a precursor fiber through a plurality of passes through an oxidation oven, where stretching during the initial passes is minimized or eliminated entirely, or made negative, followed by controlled stretching over a series of passes, using rollers of increasing speed.

IPC Classes  ?

  • D01F 9/20 - Carbon filamentsApparatus specially adapted for the manufacture thereof by decomposition of organic filaments from polyaddition, polycondensation or polymerisation products
  • D02J 1/22 - Stretching or tensioning, shrinking or relaxing, e.g. by use of overfeed and underfeed apparatus, or preventing stretch
  • D02J 13/00 - Heating or cooling the yarn, thread, cord, rope, or the like, not specific to any one of the processes provided for in this subclass

12.

Method Of Printing With Polymer Powder And Siloxane Additive

      
Application Number 18642703
Status Pending
Filing Date 2024-04-22
First Publication Date 2024-08-22
Owner Hexcel Corporation (USA)
Inventor
  • Kline, Whitney
  • Winn, Alden
  • Varholak, Lawrence

Abstract

A powder composition suitable for use in selective laser sintering for printing an object. The powder composition includes a first fraction having a polyetherketoneketone (PEKK) powder having a plurality of particles. The powder composition includes a second fraction having a plurality of siloxane particles that is dry blended with the PEKK powder prior to selective laser sintering of the powder. In some embodiments, the powder composition includes a third fraction of carbon fiber. The powder composition when used in selective laser sintering results in parts with more consistent results and improves process economics.

IPC Classes  ?

  • C09D 11/102 - Printing inks based on artificial resins containing macromolecular compounds obtained by reactions other than those only involving unsaturated carbon-to-carbon bonds
  • B29C 64/153 - Processes of additive manufacturing using only solid materials using layers of powder being selectively joined, e.g. by selective laser sintering or melting
  • B29C 64/20 - Apparatus for additive manufacturingDetails thereof or accessories therefor
  • B29K 71/00 - Use of polyethers as moulding material
  • B33Y 10/00 - Processes of additive manufacturing
  • B33Y 30/00 - Apparatus for additive manufacturingDetails thereof or accessories therefor
  • B33Y 70/00 - Materials specially adapted for additive manufacturing
  • C09D 11/037 - Printing inks characterised by features other than the chemical nature of the binder characterised by the pigment

13.

UREA DERIVATIVES AND THEIR USE AS CURATIVES AND CURATIVE ACCELERATORS FOR RESIN SYSTEMS

      
Application Number 18041065
Status Pending
Filing Date 2021-08-21
First Publication Date 2024-08-08
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor Mason, Christopher

Abstract

Bisorthohydroxy aromatic urones and their use as curatives and cure accelerators in resin systems particularly epoxy resin systems provide formulations with good outlife, low curing temperatures and desirable glass transition temperatures after curing, they are particularly useful in prepregs used in the production of components for the aerospace and wind turbine industries.

IPC Classes  ?

  • C07C 275/40 - Derivatives of urea, i.e. compounds containing any of the groups the nitrogen atoms not being part of nitro or nitroso groups having nitrogen atoms of urea groups bound to carbon atoms of six-membered aromatic rings of a carbon skeleton being further substituted by nitrogen atoms not being part of nitro or nitroso groups
  • C08G 59/40 - Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups characterised by the curing agents used
  • C08J 5/24 - Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs

14.

REINFORCING MATERIAL COMPRISING TWISTED CARBON THREADS FOR THE MANUFACTURE OF COMPOSITE PARTS, AND CORRESPONDING METHODS AND USE

      
Application Number 17823032
Status Pending
Filing Date 2021-03-11
First Publication Date 2024-06-20
Owner HEXCEL REINFORCEMENTS SASU (France)
Inventor
  • Viard, Andréa
  • Beraud, Jean-Marc
  • Thiel, Jean-Benoit
  • Forestello, François

Abstract

The invention relates to a reinforcing material (1) consisting of a unidirectional reinforcing web (2) formed of one or more carbon reinforcing yarns (3), associated on each of its faces with a veil of polymeric fibers (4, 5) chosen from among nonwoven materials, the polymeric portion of the reinforcing material representing from 0.5% to 10% of the total weight of the reinforcing material (1), and preferably from 2% to 6% of its total weight, said unidirectional reinforcing web (2) comprising one or a series of reinforcing yarns (3) individually twisted having a twist of 3 turns/m to 15 turns/m, preferably from 6 turns/m to 12 turns/m.

IPC Classes  ?

  • D02G 3/26 - Yarns or threads characterised by constructional features with characteristics dependent on the amount or direction of twist
  • B29C 70/20 - Fibrous reinforcements only characterised by the structure of fibrous reinforcements using fibres of substantial or continuous length oriented in a single direction, e.g. roving or other parallel fibres
  • B29K 105/10 - Condition, form or state of moulded material containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns oriented
  • B29K 307/04 - Carbon
  • B32B 5/12 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by structural features of a layer comprising fibres or filaments characterised by the relative arrangement of fibres or filaments of adjacent layers
  • B32B 5/26 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by the presence of two or more layers which comprise fibres, filaments, granules, or powder, or are foamed or specifically porous one layer being a fibrous or filamentary layer another layer also being fibrous or filamentary
  • D04H 3/002 - Inorganic yarns or filaments
  • D04H 3/04 - Non woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments in rectilinear paths, e.g. crossing at right angles

15.

EPOXY RESIN COMPOSITIONS

      
Application Number 17768263
Status Pending
Filing Date 2020-09-22
First Publication Date 2024-05-16
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor
  • Simmons, Martin Richard
  • Thompson, Scott
  • Mortimer, Stephen

Abstract

There is provided a resin composition for producing a composite part, comprising: a) from 30 to 90 wt % by weight of the composition of an epoxy resin component; and b) from 5 to 50 wt % by weight of the composition of a curative component; wherein the epoxy resin component comprises N,N,N′,N′-tetraglycidyl-4,4′-diamino-3,3′-dimethyldiphenylmethane (M-TGDDM) in an amount of at least 30 wt % by weight of the epoxy resin component; and further wherein the curative component comprises one or more of a diaminodiphenyl sulfone, a diaminobenzophenone, a fluorene diamine, a methylene bis aniline, including hybrid methylene bis anilines, or a substituted diamine toluene. There is also provided the use of N,N,N′,N′-tetraglycidyl-4,4′-diamino-3,3′-dimethyldiphenylmethane (M-TGDDM) as a compression performance improving additive in a resin composition for producing a composite part. There are also provided curable composite components, cured composite components produced therefrom and the use of such components as aircraft components.

IPC Classes  ?

  • C08L 63/00 - Compositions of epoxy resinsCompositions of derivatives of epoxy resins
  • C08G 59/50 - Amines
  • C08L 87/00 - Compositions of unspecified macromolecular compounds, obtained otherwise than by polymerisation reactions only involving unsaturated carbon-to-carbon bonds

16.

Ultrasonic Welding of Prepreg Tape

      
Application Number GB2023052889
Publication Number 2024/100381
Status In Force
Filing Date 2023-11-06
Publication Date 2024-05-16
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor
  • Arcidiacono, Marco
  • Barrio, Jorge
  • Alvarez, Hector

Abstract

A process for forming a spliced prepreg tape by joining adjacent ends (22, 24) of a first and a second prepreg tape (2, 3, 4), each prepreg tape comprising a respective first and second prepreg layer (12, 18) comprising fibrous material and curable thermosetting resin, each prepreg tape further comprising a respective first and second releasable polymeric backing sheet (14), the process involving: peeling of the first polymeric backing sheet from the first prepreg layer, so as to provide a first peeled end region, and optionally peeling of the second polymeric backing sheet from the second prepreg layer, so as to provide a first peeled end region (30), and optionally a second peeled end region (32), over which peeled end region or regions the prepreg layer is separated from its respective polymeric backing sheet; overlapping the first and second prepreg tapes at the first peeled end region, and if present the second peeled end region, so as to form a preliminary spliced join (34, 38), the preliminary spliced join comprising first and second adjacent layers of prepreg and first and second adjacent layers of polymeric backing sheet; ultrasonically welding of the preliminary spliced join (36) to merge together the first and second adjacent layers of prepreg and to merge together the two adjacent layers of polymeric backing sheet to form the spliced prepreg tape.

IPC Classes  ?

  • B29C 70/38 - Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
  • B29C 65/08 - Joining of preformed partsApparatus therefor by heating, with or without pressure using ultrasonic vibrations
  • B29C 70/54 - Component parts, details or accessoriesAuxiliary operations

17.

CARBOXYLATE SALTS OF AMINE COMPOUNDS AS CURING AGENTS

      
Application Number 18334081
Status Pending
Filing Date 2023-06-13
First Publication Date 2024-05-09
Owner Hexcel Corporation (USA)
Inventor
  • Yurchenko, Michael
  • Lively, Brooks
  • Schmidt, Dale
  • Herren, Winston Clark

Abstract

Provided are sizing compositions, and more particularly, sizing compositions comprising an epoxy and a carboxylate salt of an amine compound for the treatment of carbon fiber. The structure of the amine used to make the carboxylate salts is RnXmQ, wherein Q is an amine-containing group, X is a polyether group, and R is an aryl or alkyl group, either linear or branched, saturated or unsaturated, or a combination thereof. m and n are integers greater than or equal to 0. The compositions reduce or eliminate sheen and luster on carbon fibers in finished goods. Carbon fiber-reinforced composite materials and carbon fibers incorporating said sizing compositions are also provided.

IPC Classes  ?

18.

CARBOXYLATE SALTS OF AMINE COMPOUNDS AS CURING AGENTS

      
Application Number US2023068339
Publication Number 2024/091716
Status In Force
Filing Date 2023-06-13
Publication Date 2024-05-02
Owner HEXCEL CORPORATION (USA)
Inventor
  • Yurchenko, Michael
  • Lively, Brooks
  • Schmidt, Dale
  • Herren, Winston Clark

Abstract

nmmQ, wherein Q is an amine-containing group, X is a polyether group, and R is an aryl or alkyl group, either linear or branched, saturated or unsaturated, or a combination thereof. m and n are integers greater than or equal to 0. The compositions reduce or eliminate sheen and luster on carbon fibers in finished goods. Carbon fiber-reinforced composite materials and carbon fibers incorporating said sizing compositions are also provided.

IPC Classes  ?

  • C08K 3/28 - Nitrogen-containing compounds
  • C08K 5/17 - AminesQuaternary ammonium compounds
  • C08K 5/29 - Compounds containing carbon-to-nitrogen double bonds

19.

IMPROVED UNIDIRECTIONAL PREPREGS

      
Application Number GB2023052788
Publication Number 2024/089419
Status In Force
Filing Date 2023-10-25
Publication Date 2024-05-02
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor
  • Sequeira, Leela
  • Blair, Dana
  • Mitchell, Benjamin
  • Snape, Michael
  • Roe, Emily

Abstract

A curable prepreg comprising a structural layer of unidirectional electrically conductive fibres having interstices therebetween, having a first outer face and an essentially parallel second outer face, and comprising thermosetting resin impregnated within the structural layer and present within the interstices, and a first layer of thermosetting resin in contact with the first outer face of the structural layer, wherein the ratio of the electrical conductivity in the x-direction, parallel to the conductive fibres, to the electrical conductivity in the y-direction perpendicular to the conductive fibres, is less than 1000.

IPC Classes  ?

  • C08J 5/24 - Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
  • C08J 5/04 - Reinforcing macromolecular compounds with loose or coherent fibrous material
  • C08J 5/10 - Reinforcing macromolecular compounds with loose or coherent fibrous material characterised by the additives used in the polymer mixture
  • B32B 5/12 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by structural features of a layer comprising fibres or filaments characterised by the relative arrangement of fibres or filaments of adjacent layers
  • B32B 5/26 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by the presence of two or more layers which comprise fibres, filaments, granules, or powder, or are foamed or specifically porous one layer being a fibrous or filamentary layer another layer also being fibrous or filamentary

20.

NEW REINFORCING MATERIALS BASED ON S- AND Z-TWISTED YARNS FOR THE MANUFACTURE OF COMPOSITE PARTS, METHODS AND USE

      
Application Number 18547744
Status Pending
Filing Date 2022-03-22
First Publication Date 2024-04-18
Owner HEXCEL REINFORCEMENTS SASU (France)
Inventor
  • Viard, Andréa
  • Beraud, Jean-Marc
  • Thiel, Jean-Benoît
  • Forestello, François

Abstract

The reinforcing material comprises a unidirectional reinforcing web (2) formed of one or a plurality of carbon yarns (3), associated on at least one of its faces, preferably on each of its faces, with a porous polymeric layer (4, 5), the polymeric portion of the reinforcing material representing from 0.5% to 10% of its total weight and preferably from 2% to 6% of its total weight, characterized in that said carbon yarns (3) are individually twisted having a twist from 3 turns/m to 15 turns/m, preferably from 6 turns/m to 12 turns/m, and comprise at least one S-twist yarn and at least one Z-twist yarn, from a selection according to claim 1.

IPC Classes  ?

  • B29C 70/20 - Fibrous reinforcements only characterised by the structure of fibrous reinforcements using fibres of substantial or continuous length oriented in a single direction, e.g. roving or other parallel fibres
  • B29C 70/08 - Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, with or without non-reinforced layers
  • B29C 70/38 - Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
  • B32B 3/18 - Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. apertured or formed of separate pieces of material characterised by an internal layer formed of separate pieces of material
  • B32B 5/02 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by structural features of a layer comprising fibres or filaments
  • B32B 5/26 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by the presence of two or more layers which comprise fibres, filaments, granules, or powder, or are foamed or specifically porous one layer being a fibrous or filamentary layer another layer also being fibrous or filamentary
  • D02G 3/02 - Yarns or threads characterised by the material or by the materials from which they are made
  • D02G 3/26 - Yarns or threads characterised by constructional features with characteristics dependent on the amount or direction of twist
  • D02G 3/44 - Yarns or threads characterised by the purpose for which they are designed
  • D04H 1/4334 - Polyamides

21.

A RESIN LAYER FOR USE IN COMPOSITE MATERIALS

      
Application Number GB2023052053
Publication Number 2024/033611
Status In Force
Filing Date 2023-08-03
Publication Date 2024-02-15
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor Russell, Benjamin

Abstract

A resin layer, having a generally planar form and having a first outer face and an essentially parallel second outer face, and supported on its first outer face by a supporting structure, parallel to and in contact with the first outer face, wherein the layer comprises a skeletal structure embedded within the resin, the skeletal structure comprising: a plurality of studs distributed throughout the plane of the layer, each stud having a length in the direction perpendicular to the plane of the layer, and terminating in a first end and a second end, the studs having a length extending from at least the first face to at least the second face; and a framework of solid connections, connecting each solid stud to a plurality of adjacent studs, particularly for use as part of a prepreg.

IPC Classes  ?

  • B32B 3/10 - Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. apertured or formed of separate pieces of material
  • B32B 3/12 - Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. apertured or formed of separate pieces of material characterised by a layer of regularly-arranged cells whether integral or formed individually or by conjunction of separate strips, e.g. honeycomb structure
  • B32B 3/30 - Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layerLayered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by a layer with cavities or internal voids characterised by a layer formed with recesses or projections, e.g. grooved, ribbed

22.

A PREPREG, A METHOD OF TESTING THEREOF AND A PROCESS FOR ITS MANUFACTURE

      
Application Number GB2023051445
Publication Number 2023/237856
Status In Force
Filing Date 2023-06-01
Publication Date 2023-12-14
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor
  • Lindsay, James
  • Caballero, Andrea
  • Arcidiacono, Marco

Abstract

A prepreg comprising a structural layer comprising fibres having interstices therebetween, and comprising curable thermosetting resin impregnated within the structural layer and present within the interstices, wherein the prepreg comprises a test region that is free of curable thermosetting resin; a method of testing the pregreg, wherein the method comprises the steps of a) carrying out a measurement test on a test area of the test region, followed by b) inferring a property of the prepreg from the results of the measurement; and a process for the manufacture of the prepreg, the process comprising the steps of: providing a structural layer comprising fibres, having a first face and a second face, and a first impregnating layer comprising curable thermosetting resin; bringing the first face of the structural layer into contact with the first impregnating layer; compressing the structural layer and first impregnation layer together so that curable resin impregnates the fibrous layer so that it is present between the interstices between the fibres, thereby forming the prepreg; wherein the first impregnating layer comprises a region where no impregnation occurs, thereby producing the test region of the prepreg that is free of curable resin.

IPC Classes  ?

  • C08J 5/24 - Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
  • B29C 70/54 - Component parts, details or accessoriesAuxiliary operations
  • B32B 5/28 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by the presence of two or more layers which comprise fibres, filaments, granules, or powder, or are foamed or specifically porous one layer being a fibrous or filamentary layer impregnated with or embedded in a plastic substance
  • B32B 3/02 - Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions

23.

REINFORCEMENT MATERIAL INCLUDING A POROUS LAYER MADE OF A PARTIALLY CROSS-LINKED THERMOPLASTIC POLYMER AND ASSOCIATED METHODS

      
Application Number 18365578
Status Pending
Filing Date 2023-08-04
First Publication Date 2023-11-23
Owner HEXCEL REINFORCEMENTS SASU (France)
Inventor
  • Viard, Andréa
  • Benethuiliere, Thibaut

Abstract

The present invention relates to a reinforcement material including at least one fiber reinforcement associated on at least one of its faces with a porous layer, the porous layer(s) representing no more than 10% of the total weight of the reinforcement material, preferably from 0.5 to 10% of the total weight of the reinforcement material, and most preferably from 2 to 6% of the total weight of the reinforcement material, characterized in that the porous layer contains a partially cross-linked thermoplastic polymer. Another object of the invention is a precursor material of such a reinforcement material, as well as their preparation method and the methods for manufacturing a preform or a composite part from such materials.

IPC Classes  ?

  • B29B 11/16 - Making preforms characterised by structure or composition comprising fillers or reinforcements

24.

Curatives

      
Application Number 17603209
Grant Number 11879052
Status In Force
Filing Date 2020-04-17
First Publication Date 2023-06-01
Grant Date 2024-01-23
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor Mason, Christopher Robert

Abstract

The host compound in a clathrate is an amino or hydroxyl containing aromatic phosphorous compound, clathrates containing a resin curative and their use in curable resin compositions to produce moulded articles particularly fibre reinforced articles.

IPC Classes  ?

25.

FLEX-CAP

      
Serial Number 98018517
Status Pending
Filing Date 2023-05-30
Owner Hexcel Corporation ()
NICE Classes  ? 06 - Common metals and ores; objects made of metal

Goods & Services

Metallic cellular core material and metallic sandwich panels for use in manufacturing aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial products; building materials, namely, metallic honeycomb and metallic sandwich panels.

26.

FLEX-CAP

      
Serial Number 98018543
Status Pending
Filing Date 2023-05-30
Owner Hexcel Corporation ()
NICE Classes  ? 17 - Rubber and plastic; packing and insulating materials

Goods & Services

Soundproofing materials for vehicles, vehicle engines, airplanes, and airplane engines in the nature of cellular core material with inserts for noise reduction

27.

FLEX-CAP

      
Application Number 018880900
Status Registered
Filing Date 2023-05-29
Registration Date 2023-10-03
Owner Hexcel Corporation (USA)
NICE Classes  ?
  • 06 - Common metals and ores; objects made of metal
  • 17 - Rubber and plastic; packing and insulating materials

Goods & Services

Metallic cellular core material and metallic sandwich panels for use in manufacturing aerospace, space and defence, recreation, electrical, architectural, marine, transportation and general industrial products; Metallic honeycomb and metallic sandwich panels. Soundproofing materials for airplane engines and other portions of airplanes in the nature of cellular core material with inserts for noise reduction.

28.

SURFACING MATERIAL

      
Application Number GB2022052255
Publication Number 2023/041895
Status In Force
Filing Date 2022-09-05
Publication Date 2023-03-23
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor
  • Tipler, Ben
  • Whiter, Mark

Abstract

There is provided a surfacing material comprising an ultraviolet (UV) resistant polymer layer, a thermocurable or thermoplastic resin layer and a fibrous support, wherein a first surface of the UV resistant polymer layer forms an outermost surface of the surfacing material and the second surface of the UV resistant polymer layer contacts a first surface of the thermocurable or thermoplastic resin layer, and the second surface of the thermocurable or thermoplastic resin layer contacts a first surface of the fibrous support. There is also provided methods of forming cured composite structures having an ultraviolet resistant outer surface utilising a surfacing material of the invention, and cured composite structures incorporating a UV resistant surfacing layer of the invention.

IPC Classes  ?

  • B32B 3/26 - Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layerLayered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by a layer with cavities or internal voids
  • B32B 5/02 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by structural features of a layer comprising fibres or filaments
  • B32B 7/09 - Interconnection of layers by mechanical means by stitching, needling or sewing
  • B32B 7/12 - Interconnection of layers using interposed adhesives or interposed materials with bonding properties
  • B32B 15/14 - Layered products essentially comprising metal next to a fibrous or filamentary layer
  • B32B 15/20 - Layered products essentially comprising metal comprising aluminium or copper
  • B32B 27/12 - Layered products essentially comprising synthetic resin next to a fibrous or filamentary layer
  • B32B 27/36 - Layered products essentially comprising synthetic resin comprising polyesters
  • B32B 27/38 - Layered products essentially comprising synthetic resin comprising epoxy resins
  • B32B 27/40 - Layered products essentially comprising synthetic resin comprising polyurethanes
  • B32B 37/12 - Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by using adhesives
  • F03D 1/06 - Rotors
  • B29C 35/02 - Heating or curing, e.g. crosslinking or vulcanising
  • B29C 37/00 - Component parts, details, accessories or auxiliary operations, not covered by group or

29.

CARBON FIBERS HAVING IMPROVED STRENGTH AND MODULUS AND AN ASSOCIATED METHOD AND APPARATUS FOR PREPARING SAME

      
Application Number US2022075199
Publication Number 2023/023640
Status In Force
Filing Date 2022-08-19
Publication Date 2023-02-23
Owner HEXCEL CORPORATION (USA)
Inventor
  • Ruminski, Anne
  • Ferrin, Peter

Abstract

The invention is directed to carbon fibers having high tensile strength. The invention also provides a method and apparatus for making the carbon fibers. The method comprises advancing a precursor fiber through a plurality of passes through an oxidation oven, where stretching during the initial passes is minimized or eliminated entirely, or made negative, followed by controlled stretching over a series of passes, using rollers of increasing speed.

IPC Classes  ?

  • D02J 1/22 - Stretching or tensioning, shrinking or relaxing, e.g. by use of overfeed and underfeed apparatus, or preventing stretch
  • D01F 9/12 - Carbon filamentsApparatus specially adapted for the manufacture thereof
  • C01B 32/05 - Preparation or purification of carbon not covered by groups , , ,
  • D02J 13/00 - Heating or cooling the yarn, thread, cord, rope, or the like, not specific to any one of the processes provided for in this subclass

30.

MOULDING MATERIAL

      
Application Number 17770015
Status Pending
Filing Date 2020-09-23
First Publication Date 2022-12-08
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor Whiter, Mark

Abstract

The present invention is concerned with a moulding material comprising: a) A primary non-woven fibre layer; b) A secondary non-woven fibre layer, and c) A resin layer; wherein the resin layer bonds the secondary non-woven fibre layer to a first surface of the primary non-woven fibre layer, and the resin layer is exposed on the second surface of the primary non-woven layer.

IPC Classes  ?

  • B32B 5/26 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by the presence of two or more layers which comprise fibres, filaments, granules, or powder, or are foamed or specifically porous one layer being a fibrous or filamentary layer another layer also being fibrous or filamentary
  • B32B 5/02 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by structural features of a layer comprising fibres or filaments
  • B32B 5/08 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by structural features of a layer comprising fibres or filaments the fibres or filaments of a layer being specially arranged or being of different substances
  • B32B 5/10 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by structural features of a layer comprising fibres or filaments characterised by a fibrous layer reinforced with filaments
  • B32B 7/09 - Interconnection of layers by mechanical means by stitching, needling or sewing
  • B32B 27/12 - Layered products essentially comprising synthetic resin next to a fibrous or filamentary layer
  • B32B 27/20 - Layered products essentially comprising synthetic resin characterised by the use of special additives using fillers, pigments, thixotroping agents

31.

Reinforcement material comprising a porous layer made of partially cross-linked thermoplastic polymer and associated methods

      
Application Number 17804202
Grant Number 11760058
Status In Force
Filing Date 2022-05-26
First Publication Date 2022-11-03
Grant Date 2023-09-19
Owner HEXCEL REINFORCEMENTS SASU (France)
Inventor
  • Viard, Andréa
  • Benethuiliere, Thibaut

Abstract

The present invention relates to a reinforcement material including at least one fiber reinforcement associated on at least one of its faces with a porous layer, the porous layer(s) representing no more than 10% of the total weight of the reinforcement material, preferably from 0.5 to 10% of the total weight of the reinforcement material, and most preferably from 2 to 6% of the total weight of the reinforcement material, characterized in that the porous layer contains a partially cross-linked thermoplastic polymer. Another object of the invention is a precursor material of such a reinforcement material, as well as their preparation method and the methods for manufacturing a preform or a composite part from such materials.

IPC Classes  ?

  • B32B 5/26 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by the presence of two or more layers which comprise fibres, filaments, granules, or powder, or are foamed or specifically porous one layer being a fibrous or filamentary layer another layer also being fibrous or filamentary
  • B32B 7/09 - Interconnection of layers by mechanical means by stitching, needling or sewing
  • B32B 7/027 - Thermal properties
  • B32B 3/10 - Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. apertured or formed of separate pieces of material
  • B32B 5/02 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by structural features of a layer comprising fibres or filaments
  • B32B 7/12 - Interconnection of layers using interposed adhesives or interposed materials with bonding properties
  • B32B 27/12 - Layered products essentially comprising synthetic resin next to a fibrous or filamentary layer
  • B32B 27/34 - Layered products essentially comprising synthetic resin comprising polyamides
  • B32B 37/06 - Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the heating method
  • C08F 283/00 - Macromolecular compounds obtained by polymerising monomers on to polymers provided for in subclass

32.

Surface finishing moulding material comprising a rheology-modified epoxy layer

      
Application Number 17770567
Grant Number 12240954
Status In Force
Filing Date 2020-09-23
First Publication Date 2022-09-15
Grant Date 2025-03-04
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor Whiter, Mark

Abstract

A moulding material which comprises: (a) a structural reinforcement layer comprising a fibrous reinforcement material optionally in combination with a second resin composition; and (b) a surface enhancing layer, for contacting a surface of a mould or tool, comprising a first non-woven fibre carrier in combination with a first resin composition containing a rheology modifier and a curing agent, wherein the first resin composition provides an external mould or tool-contacting surface of the moulding material. The moulding material can be cured to form a moulded article having a high quality surface finish that requires minimal preparation before painting and/or application in its intended use. The moulded article may be provided with sacrificial discontinuous indicator means to assist in uniform removal of a part of the surface enhancing layer of the moulded article for specific applications.

IPC Classes  ?

  • C08J 5/24 - Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
  • B29C 70/18 - Fibrous reinforcements only characterised by the structure of fibrous reinforcements using fibres of substantial or continuous length in the form of a mat, e.g. sheet moulding compound [SMC]
  • B32B 5/02 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by structural features of a layer comprising fibres or filaments
  • B32B 27/20 - Layered products essentially comprising synthetic resin characterised by the use of special additives using fillers, pigments, thixotroping agents
  • B32B 27/38 - Layered products essentially comprising synthetic resin comprising epoxy resins
  • B29K 63/00 - Use of epoxy resins as moulding material
  • B29K 309/08 - Glass

33.

HEXCEL

      
Application Number 1681758
Status Registered
Filing Date 2022-04-20
Registration Date 2022-04-20
Owner Hexcel Corporation (USA)
NICE Classes  ? 17 - Rubber and plastic; packing and insulating materials

Goods & Services

Plastic composite material in the form of sheets for use in manufacturing aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial projects; structural insulated construction panels, namely, non-metallic honeycomb-shaped structural insulated construction panels for use in the aerospace, space and defense, recreation, electrical, architectural, marine, transportation and building industries; tamping material made of thermoset or thermoplastic copolymeric material in the form of tape or mat for use as a composite material in manufacturing aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial projects; thermoplastic elastomer resins in the form of tape or mat for use as a composite material in further manufacture in the aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial industries; thermoplastic composite tapes or mats containing glass fiber for use as a composite material in the manufacture of other goods in the aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial industries; thermoplastic section tapes or mats for use as a composite material in the manufacture of façade and partitions for use as building materials for heat-insulating applications in the aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial industries; semi-processed thermoplastics in tape or mat form for use as a composite material in manufacturing aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial projects; plastic composite material in the form of tape or mat for use in manufacturing aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial projects; continuous or discontinuous fiber reinforced molding materials in the form of tape, fabric, non-woven, mat, tow or roving fully or partially impregnated with a thermoset, thermoplastic or other matrix material for use as a composite material in manufacturing aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial projects; non-metallic honeycomb for use in structural reinforcement, and aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial projects; synthetic resins for use in the manufacture of moulding compounds; carbon fibers not for textile use; material for thermal insulation and fire protection, namely, fire-resistant composite panels made of aramid, glass, carbon or ceramic fibers.

34.

PREPREG OR SEMIPREG PRECURSOR AND METHOD OF MANUFACTURING SAME

      
Application Number 17625157
Status Pending
Filing Date 2020-07-19
First Publication Date 2022-08-25
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor
  • Whiter, Mark
  • Tipler, Ben
  • Maillot, Mathilde

Abstract

A prepreg or semipreg precursor comprising a fibre reinforcement and a resin composition fused thereto, the resin composition containing at least one epoxy resin and a latent curing agent, wherein the epoxy resin and the latent curing agent form a solid phase at ambient temperature, the latent curing agent forming a discrete phase within the epoxy resin. The stabilized uncured resin composition and prepregs and semipregs incorporating the same are easy to handle, have desirable curing temperatures and show good outlife at ambient to mid range temperatures.

IPC Classes  ?

  • C08J 5/24 - Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
  • C08K 3/40 - Glass

35.

NATURE RANGE

      
Application Number 1673043
Status Registered
Filing Date 2022-06-14
Registration Date 2022-06-14
Owner Hexcel Corporation (USA)
NICE Classes  ? 17 - Rubber and plastic; packing and insulating materials

Goods & Services

Combination of continuous or discontinuous reinforcement fibers in the form of tape, fabric, non-woven, mat, tow or rovings impregnated with a thermoset, thermoplastic or other matrix material for use as a composite material; molding material for further manufacture consisting of reinforcing fiber pre-impregnated with a matrix resin.

36.

Nature Range

      
Application Number 1674114
Status Registered
Filing Date 2022-06-14
Registration Date 2022-06-14
Owner Hexcel Corporation (USA)
NICE Classes  ? 17 - Rubber and plastic; packing and insulating materials

Goods & Services

Combination of continuous or discontinuous reinforcement fibers in the form of tape, fabric, non-woven, mat, tow or rovings impregnated with a thermoset, thermoplastic or other matrix material for use as a composite material; Molding material for further manufacture consisting of reinforcing fiber pre-impregnated with a matrix resin.

37.

Peel ply for elongate composite matertals

      
Application Number 17602095
Grant Number 11697254
Status In Force
Filing Date 2020-04-02
First Publication Date 2022-07-07
Grant Date 2023-07-11
Owner
  • Hexcel Composites Limited (United Kingdom)
  • Hexcel Corporation (USA)
  • Hexcel Holding GmbH (Austria)
Inventor
  • Moser, Johannes
  • Hung, Yu-Chen
  • Reagan, Erin

Abstract

An assembly (113) for composite manufacture is provided. The assembly comprises a cured resin impregnated reinforcement material (112) comprising a fibre component and a resin matrix component, in which the resin matrix component comprises polyurethane, the assembly having a length to width ratio of at least 5:1, and the assembly defining a longitudinal direction (L) along its length; and a peel ply (116) in contact with the cured resin impregnated reinforcement material (112), the peel ply (116) comprising a woven layer having a plurality of longitudinal fibres (118) extending in the longitudinal direction (L); and a plurality of transverse fibres (120) extending in a transverse direction (T) normal to the longitudinal direction (L); in which the areal density of the plurality of transverse fibres (120) is higher than the areal density of the plurality of longitudinal fibres (118).

IPC Classes  ?

  • B29C 70/52 - Pultrusion, i.e. forming and compressing by continuously pulling through a die
  • B29C 70/54 - Component parts, details or accessoriesAuxiliary operations
  • B29C 70/68 - Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers

38.

Self-adhesive prepreg

      
Application Number 17604326
Grant Number 11680144
Status In Force
Filing Date 2020-04-17
First Publication Date 2022-07-07
Grant Date 2023-06-20
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor Rhodes, Michael

Abstract

A self-adhesive prepreg comprising a fibre reinforcement layer having a first side and a second side, wherein the first side of the fibre reinforcement layer has been pre-impregnated with a self-adhesive resin composition. The self-adhesive may be used as a structural reinforcement and is especially adapted for direct bonding to oily steel or galvanized steel in the automotive, aerospace and other sheet metal fabrication industries.

IPC Classes  ?

  • C08J 5/24 - Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
  • B32B 27/38 - Layered products essentially comprising synthetic resin comprising epoxy resins
  • C08G 59/30 - Di-epoxy compounds containing atoms other than carbon, hydrogen, oxygen, and nitrogen
  • C08G 59/32 - Epoxy compounds containing three or more epoxy groups
  • C08G 59/38 - Epoxy compounds containing three or more epoxy groups together with di-epoxy compounds
  • C08G 59/40 - Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups characterised by the curing agents used
  • C08G 59/68 - Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups characterised by the catalysts used
  • C08L 63/00 - Compositions of epoxy resinsCompositions of derivatives of epoxy resins
  • C08L 63/04 - Epoxynovolacs

39.

HEXCEL

      
Application Number 1663627
Status Registered
Filing Date 2022-04-25
Registration Date 2022-04-25
Owner Hexcel Corporation (USA)
NICE Classes  ? 24 - Textiles and textile goods

Goods & Services

Protective fabrics used in the manufacture of goods, namely, armored vehicles, clothing and protective walls; fiberglass fabrics for solar protection; and fiberglass, carbon and aramid reinforcement textiles for use in the commercial aerospace, space and defense, recreation, electrical, architectural, transportation, marine, and general industrial fields.

40.

HEXCEL

      
Application Number 1664207
Status Registered
Filing Date 2022-04-21
Registration Date 2022-04-21
Owner Hexcel Corporation (USA)
NICE Classes  ? 21 - HouseHold or kitchen utensils, containers and materials; glassware; porcelain; earthenware

Goods & Services

Reinforcement fibers made of glass and partially impregnated with polymeric resin for use in the manufacture of composite materials for aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial products; reinforcement fibers made of glass and partially impregnated with synthetic resin for use in the manufacture of composite materials for aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial products.

41.

HEXCEL

      
Application Number 1664219
Status Registered
Filing Date 2022-04-27
Registration Date 2022-04-27
Owner Hexcel Corporation (USA)
NICE Classes  ? 40 - Treatment of materials; recycling, air and water treatment,

Goods & Services

Custom manufacture of goods in the nature of airplane parts and fittings, satellites parts and fittings, engine parts and fittings, defense aircraft parts and fittings, space vehicle parts and fittings, launchers and launch pads and parts and fittings therefor, helicopter parts and fittings, turbine and nacelle parts and fittings, boats, canoes and dinghies and parts and fittings therefor, wheels, brackets, and ducts, and industrial parts to the order and specification of others; treatment of materials, namely, for the manufacture of thermoplastic products by extrusion, compression moulding and plastic injection; treatment of materials for use in the aerospace, aviation, satellite, military, space and defense industries; treatment of materials, namely, selective laser sintering for a wide variety of goods.

42.

NATURE RANGE

      
Serial Number 97437644
Status Pending
Filing Date 2022-06-01
Owner Hexcel Corporation ()
NICE Classes  ? 17 - Rubber and plastic; packing and insulating materials

Goods & Services

Molding material being semi-finished reinforcing plastic fibers pre-impregnated with a matrix resin for further manufacture in the aerospace, automotive, transportation, recreation and building industries, not for textile use; Molding material being semi-finished reinforcing natural epoxy matrix resin fibers for further manufacture in the aerospace, automotive, transportation, recreation and building industries, not for textile use; Molding material being semi-finished reinforcing thermal insulation thermoplastic fibers pre-impregnated with a matrix resin for further manufacture in the aerospace, automotive, transportation, recreation and building industries, not for textile use; Molding material being semi-finished reinforcing thermoplastic fibers pre-impregnated with a matrix resin for further manufacture in the aerospace, automotive, transportation, recreation and building industries, not for textile use; Molding material being semi-finished reinforcing thermoplastic fibers pre-impregnated with a matrix resin for insulation and heat resistance for further manufacture in the aerospace, automotive, transportation, recreation and building industries, not for textile use; Molding material being semi-finished reinforcing thermoplastic fibers pre-impregnated with a matrix resin for heat and acoustical insulation for further manufacture in the aerospace, automotive, transportation, recreation and building industries, not for textile use

43.

HEXCEL

      
Application Number 1662560
Status Registered
Filing Date 2022-04-19
Registration Date 2022-04-19
Owner Hexcel Corporation (USA)
NICE Classes  ? 06 - Common metals and ores; objects made of metal

Goods & Services

Metallic cellular core material and metallic sandwich panels for use in manufacturing aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial products.

44.

NATURE RANGE

      
Serial Number 97425516
Status Pending
Filing Date 2022-05-24
Owner Hexcel Corporation ()
NICE Classes  ? 17 - Rubber and plastic; packing and insulating materials

Goods & Services

Molding material being semi-finished reinforcing plastic fibers pre-impregnated with a matrix resin for further manufacture in the aerospace, automotive, transportation, recreation and building industries, not for textile use; Molding material being semi-finished reinforcing natural epoxy matrix resin fibers for further manufacture in the aerospace, automotive, transportation, recreation and building industries, not for textile use; Molding material being semi-finished reinforcing thermal insulation thermoplastic fibers pre-impregnated with a matrix resin for further manufacture in the aerospace, automotive, transportation, recreation and building industries, not for textile use; Molding material being semi-finished reinforcing thermoplastic fibers pre-impregnated with a matrix resin for further manufacture in the aerospace, automotive, transportation, recreation and building industries, not for textile use; Molding material being semi-finished reinforcing thermoplastic fibers pre-impregnated with a matrix resin for insulation and heat resistance for further manufacture in the aerospace, automotive, transportation, recreation and building industries, not for textile use; Molding material being semi-finished reinforcing thermoplastic fibers pre-impregnated with a matrix resin for heat and acoustical insulation for further manufacture in the aerospace, automotive, transportation, recreation and building industries, not for textile use

45.

HEXCEL

      
Application Number 1661714
Status Registered
Filing Date 2022-04-22
Registration Date 2022-04-22
Owner Hexcel Corporation (USA)
NICE Classes  ? 22 - Rope, netting, tents, awnings, sails and sacks; padding and stuffing materials

Goods & Services

Carbon fibers for use in manufacture, for textile use and for structural reinforcement.

46.

HEXCEL

      
Application Number 1662393
Status Registered
Filing Date 2022-04-19
Registration Date 2022-04-19
Owner Hexcel Corporation (USA)
NICE Classes  ? 12 - Land, air and water vehicles; parts of land vehicles

Goods & Services

Composite sandwich panels, structural parts and interiors of vehicles and aircraft.

47.

HEXCEL

      
Application Number 218944400
Status Registered
Filing Date 2022-04-27
Registration Date 2024-08-16
Owner Hexcel Corporation (USA)
NICE Classes  ? 40 - Treatment of materials; recycling, air and water treatment,

Goods & Services

(1) Custom manufacture of goods in the nature of airplane parts and fittings, satellites parts and fittings, automobile and aircraft engine parts, defense aircraft parts and fittings, space vehicle parts and fittings, space launchers and rocket launch pads and structural parts and fittings therefor, helicopter parts and fittings, aircraft turbine and nacelle being aircraft turbines parts and fittings, boats, canoes and dinghies and parts and fittings therefor, wheels for land vehicles and aircraft, bearing brackets for machines, and air conditioning and ventilating ducts to the order and specification of others; treatment of materials, namely, for the manufacture of thermoplastic synthetic resins, semi-processed by extrusion, compression moulding and plastic injection; treatment of materials for use in the aerospace, aviation, satellite, military, space and defense industries, namely, strengthening, reinforcing, weatherproofing and waterproofing of carbon fibers, structural honeycomb and synthetic resins; treatment of materials, namely, selective laser sintering 3D printing for others for a wide variety of goods.

48.

HEXCEL

      
Application Number 218943000
Status Pending
Filing Date 2022-04-25
Owner Hexcel Corporation (USA)
NICE Classes  ? 24 - Textiles and textile goods

Goods & Services

(1) Protective fabrics used in the manufacture of goods, namely, armored vehicles and protective walls; fiberglass fabrics for solar protection for use in land, sea and aerospace applications; and fiberglass, carbon and aramid reinforcement textiles for use in the commercial aerospace, space and defense, recreation, electrical, architectural, transportation, marine, and general industrial fields.

49.

HEXCEL

      
Application Number 218680100
Status Registered
Filing Date 2022-04-22
Registration Date 2023-12-29
Owner Hexcel Corporation (USA)
NICE Classes  ? 22 - Rope, netting, tents, awnings, sails and sacks; padding and stuffing materials

Goods & Services

(1) Carbon fibers for use in manufacture, for textile use and for structural reinforcement.

50.

HEXCEL

      
Application Number 218941800
Status Registered
Filing Date 2022-04-21
Registration Date 2024-12-27
Owner Hexcel Corporation (USA)
NICE Classes  ? 21 - HouseHold or kitchen utensils, containers and materials; glassware; porcelain; earthenware

Goods & Services

(1) Reinforcement fibers made of glass and partially impregnated with polymeric resin being glass fibers for reinforcing plastics for use in the manufacture of composite materials for aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial products; reinforcement fibers made of glass and partially impregnated with synthetic resin being glass fibers for reinforcing plastics for use in the manufacture of composite materials for aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial products.

51.

HEXCEL

      
Application Number 220830100
Status Registered
Filing Date 2022-04-20
Registration Date 2025-04-23
Owner Hexcel Corporation (USA)
NICE Classes  ? 17 - Rubber and plastic; packing and insulating materials

Goods & Services

(1) Plastic composite material in the form of sheets for use in manufacturing aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial projects; non-metallic honeycomb-shaped structural fire-resistant insulated construction panels for aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial projects; tamping material made of semi-processed thermoplastic polymer resins and thermosetting copolymeric resins in the form of tapes and mats for use as a composite material in manufacturing aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial projects; thermoplastic elastomer resins in the form of thread seal tapes and mats for use as a composite material in further manufacture in the aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial industries; thermoplastic composite tapes and mats containing glass fiber for insulation for use as a composite material in the manufacture of other goods in the aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial industries; semi-processed thermoplastic polymer resins in tape and mat form for use as a composite material in manufacturing aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial projects; plastic composite material in the form of plastic tape and mat for use in manufacturing aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial projects; non-metallic fiberglass insulation in the shape of a honeycomb for use in aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial projects; carbon fibers not for textile use; material for thermal insulation and fire protection, namely, fire-resistant composite insulated panels made of aramid, glass, carbon and ceramic fibers.

52.

HEXCEL

      
Application Number 218676800
Status Registered
Filing Date 2022-04-19
Registration Date 2024-08-16
Owner Hexcel Corporation (USA)
NICE Classes  ? 12 - Land, air and water vehicles; parts of land vehicles

Goods & Services

(1) Composite sandwich panels being structural parts for land vehicles, structural parts of land vehicles and aircraft.

53.

HEXCEL

      
Application Number 218819500
Status Registered
Filing Date 2022-04-19
Registration Date 2023-12-22
Owner Hexcel Corporation (USA)
NICE Classes  ? 06 - Common metals and ores; objects made of metal

Goods & Services

(1) Metallic cellular core material and metallic sandwich panels for use in manufacturing aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial products.

54.

UREA DERIVATIVES AND THEIR USE AS CURATIVES AND CURATIVE ACCELERATORS FOR RESIN SYSTEMS

      
Application Number EP2021072561
Publication Number 2022/034201
Status In Force
Filing Date 2021-08-12
Publication Date 2022-02-17
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor Mason, Christopher

Abstract

Bisorthohydroxy aromatic urones and their use as curatives and cure accelerators in resin systems particularly epoxy resin systems provide formulations with good outlife, low curing temperatures and desirable glass transition temperatures after curing, they are particularly useful in prepregs used in the production of components for the aerospace and wind turbine industries.

IPC Classes  ?

  • C07C 275/34 - Derivatives of urea, i.e. compounds containing any of the groups the nitrogen atoms not being part of nitro or nitroso groups having nitrogen atoms of urea groups bound to carbon atoms of six-membered aromatic rings of a carbon skeleton being further substituted by singly-bound oxygen atoms having nitrogen atoms of urea groups and singly-bound oxygen atoms bound to carbon atoms of the same non-condensed six-membered aromatic ring

55.

HEXCEL

      
Serial Number 97237064
Status Registered
Filing Date 2022-01-25
Registration Date 2023-03-21
Owner Hexcel Corporation ()
NICE Classes  ? 40 - Treatment of materials; recycling, air and water treatment,

Goods & Services

Custom manufacture of goods in the nature of airplane parts and fittings, satellites parts and fittings, engine parts and fittings, defense aircraft parts and fittings, space vehicle parts and fittings, launchers and launch pads and parts and fittings therefor, helicopter parts and fittings, turbine and nacelle parts and fittings, boats, canoes and dinghies and parts and fittings therefor, wheels, brackets, and ducts, and industrial parts to the order and specification of others; treatment of materials, namely, for the manufacture of thermoplastic products by extrusion, compression moulding and plastic injection; treatment of materials for use in the aerospace, aviation, satellite, military, space and defense industries, namely, strengthening, reinforcing, weatherproofing and waterproofing of carbon fiber, structural honeycomb and synthetic resins; treatment of materials, namely, selective laser sintering for a wide variety of goods

56.

Adhesive composition

      
Application Number 17297387
Grant Number 11873422
Status In Force
Filing Date 2019-12-03
First Publication Date 2022-01-20
Grant Date 2024-01-16
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor Rhodes, Michael

Abstract

An adhesive composition comprising a silane-modified epoxy resin, a dicyclopentadiene novolac epoxy resin and a curing agent. The composition shows good oily steel bonding, even in the absence of CTBN rubber or rubber adducts as toughening agents, with good Tg values of the cured resin and good Tg retention after hot wet aging.

IPC Classes  ?

  • C09J 163/04 - Epoxynovolacs
  • C08G 59/30 - Di-epoxy compounds containing atoms other than carbon, hydrogen, oxygen, and nitrogen
  • C08G 59/32 - Epoxy compounds containing three or more epoxy groups
  • C08G 59/40 - Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups characterised by the curing agents used
  • C08K 3/26 - CarbonatesBicarbonates
  • C09J 5/06 - Adhesive processes in generalAdhesive processes not provided for elsewhere, e.g. relating to primers involving heating of the applied adhesive
  • C08L 9/02 - Copolymers with acrylonitrile

57.

HEXCEL

      
Serial Number 97228743
Status Registered
Filing Date 2022-01-20
Registration Date 2023-08-08
Owner Hexcel Corporation ()
NICE Classes  ? 21 - HouseHold or kitchen utensils, containers and materials; glassware; porcelain; earthenware

Goods & Services

Reinforcement fibers made of glass and partially impregnated with polymeric resin for non-textile purposes for use in the manufacture of composite materials for aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial products; reinforcement fibers made of glass and partially impregnated with synthetic resin for non-textile purposes for use in the manufacture of composite materials for aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial products

58.

HEXCEL

      
Serial Number 97226512
Status Registered
Filing Date 2022-01-19
Registration Date 2023-07-25
Owner Hexcel Corporation ()
NICE Classes  ? 17 - Rubber and plastic; packing and insulating materials

Goods & Services

Plastic composite material in the form of sheets for use in manufacturing aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial projects; non-metallic honeycomb-shaped structural insulated construction panels for aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial projects; tamping material made of thermoset or thermoplastic copolymeric material in the form of tape or mat for use as a composite material in manufacturing aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial projects; Thermoplastic elastomer resins in the form of tape or mat for use as a composite material in further manufacture in the aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial industries; Thermoplastic composite tapes or mats containing glass fiber for use as a composite material in the manufacture of other goods in the aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial industries; Semi-processed thermoplastics in tape or mat form for use as a composite material in manufacturing aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial projects; Plastic composite material in the form of tape or mat for use in manufacturing aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial projects; non-metallic fiberglass insulation in the shape of a honeycomb for use in aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial projects; Carbon fibers not for textile use; Material for thermal insulation and fire protection, namely, fire-resistant composite panels made of aramid, glass, carbon or ceramic fibers

59.

HEXCEL

      
Serial Number 97219244
Status Registered
Filing Date 2022-01-14
Registration Date 2023-02-14
Owner Hexcel Corporation ()
NICE Classes  ? 01 - Chemical and biological materials for industrial, scientific and agricultural use

Goods & Services

Industrial adhesives

60.

HEXCEL

      
Serial Number 97217023
Status Registered
Filing Date 2022-01-13
Registration Date 2023-03-21
Owner Hexcel Corporation ()
NICE Classes  ? 24 - Textiles and textile goods

Goods & Services

Protective fabrics used in the manufacture of goods, namely armored vehicles, clothing and protective walls; fiberglass fabrics for solar protection for use in land, sea and aerospace applications; fiberglass, carbon and aramid reinforcement textiles for use in the commercial aerospace, space and defense, recreation, electrical, architectural, transportation, marine, and general industrial fields

61.

Method of manufacture of a composite material

      
Application Number 17293353
Grant Number 11358349
Status In Force
Filing Date 2019-11-08
First Publication Date 2022-01-13
Grant Date 2022-06-14
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor Arcidiacono, Marco

Abstract

A method of manufacture of a composite component is provided, the method comprising the steps of providing two layers of pre-preg composite material, one of which has an edge adjacent a surface of the other. Pressure and, optionally, vibrational energy is applied to the edge to thereby smooth the ply drop.

IPC Classes  ?

  • B29C 70/54 - Component parts, details or accessoriesAuxiliary operations
  • B29C 70/38 - Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
  • B29K 307/04 - Carbon
  • B29K 309/08 - Glass
  • B29L 31/08 - Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers

62.

HEXCEL

      
Serial Number 97214665
Status Registered
Filing Date 2022-01-12
Registration Date 2023-07-11
Owner Hexcel Corporation ()
NICE Classes  ?
  • 17 - Rubber and plastic; packing and insulating materials
  • 22 - Rope, netting, tents, awnings, sails and sacks; padding and stuffing materials

Goods & Services

Carbon fibers for use in manufacture and for structural reinforcement, other than for textile use Carbon fibers for textile use; Synthetic carbon fibers for use in the manufacture of fabrics, textiles for structural reinforcement

63.

HEXCEL

      
Serial Number 97212689
Status Registered
Filing Date 2022-01-11
Registration Date 2023-08-15
Owner Hexcel Corporation ()
NICE Classes  ? 12 - Land, air and water vehicles; parts of land vehicles

Goods & Services

Composite sandwich structural panels and structural parts for vehicles and aircraft

64.

HEXCEL

      
Serial Number 97210274
Status Registered
Filing Date 2022-01-10
Registration Date 2023-06-27
Owner Hexcel Corporation ()
NICE Classes  ? 06 - Common metals and ores; objects made of metal

Goods & Services

Metallic cellular core material and metallic sandwich panels for use in manufacturing aerospace, space and defense, recreation, electrical, architectural, marine, transportation and general industrial products

65.

Epoxy resin formulations

      
Application Number 15734008
Grant Number 11332607
Status In Force
Filing Date 2019-06-13
First Publication Date 2021-07-15
Grant Date 2022-05-17
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor Blair, Dana

Abstract

Formulations comprising from 10 to 80% by weight of the formulation of a halogenated epoxy resin; from 1 to 15% by weight of the formulation of an antimony based fire retardant; from 1 to 10% by weight of the formulation of an inorganic or non-polymeric organic phosphorous containing fire retardant; and from 1 to 30% by weight of the formulation of a curative system are provided. The formulations are particularly suitable for producing aircraft interior composite components having good fire retarding properties, low smoke emission, low smoke toxicity and low heat release properties. The formulations also have excellent processing and mechanical properties. Further components may be included in the compositions to improve various properties, including the fire retarding, low smoke emission, low smoke toxicity and low heat release properties and to also further improve the processing and mechanical properties, including toughness. Compositions produced from the formulations have excellent processing and mechanical properties, and may also have good surface finishes.

IPC Classes  ?

  • C08J 5/24 - Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
  • C08L 63/04 - Epoxynovolacs
  • C08L 63/02 - Polyglycidyl ethers of bis-phenols
  • C08L 63/00 - Compositions of epoxy resinsCompositions of derivatives of epoxy resins
  • C08G 59/38 - Epoxy compounds containing three or more epoxy groups together with di-epoxy compounds
  • C08G 59/24 - Di-epoxy compounds carbocyclic
  • C08G 59/30 - Di-epoxy compounds containing atoms other than carbon, hydrogen, oxygen, and nitrogen
  • C08G 59/40 - Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups characterised by the curing agents used
  • C08J 5/04 - Reinforcing macromolecular compounds with loose or coherent fibrous material
  • C08K 3/02 - Elements
  • C08K 3/22 - OxidesHydroxides of metals
  • C08K 3/32 - Phosphorus-containing compounds
  • C08K 5/3492 - Triazines
  • C08K 5/52 - Phosphorus bound to oxygen bound to oxygen only

66.

Or relating to curing agents

      
Application Number 17267889
Grant Number 11939421
Status In Force
Filing Date 2019-08-30
First Publication Date 2021-07-01
Grant Date 2024-03-26
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor
  • Mason, Christopher Robert
  • Verge, Nicholas

Abstract

A curative system comprising a combination of adipic acid dihydrazide and/or isophthalic dihydrazide and a clathrate in which the guest compound of the clathrate comprises an imidazole, an imidazoline or diazabicycloalkanes (DBCA).

IPC Classes  ?

  • C08G 59/40 - Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups characterised by the curing agents used
  • C07C 257/22 - Compounds containing carboxyl groups, the doubly-bound oxygen atom of a carboxyl group being replaced by a doubly-bound nitrogen atom, this nitrogen atom not being further bound to an oxygen atom, e.g. imino-ethers, amidines with replacement of the other oxygen atom of the carboxyl group by nitrogen atoms, e.g. amidines having nitrogen atoms of amidino groups further bound to nitrogen atoms, e.g. hydrazidines
  • C07D 235/00 - Heterocyclic compounds containing 1,3-diazole or hydrogenated 1,3-diazole rings, condensed with other rings
  • C07D 247/02 - Heterocyclic compounds containing rings having two nitrogen atoms as the only ring hetero atoms, according to more than one of groups having the nitrogen atoms in positions 1 and 3
  • C08G 59/00 - Polycondensates containing more than one epoxy group per moleculeMacromolecules obtained by reaction of epoxy polycondensates with monofunctional low-molecular-weight compoundsMacromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups
  • C08G 59/68 - Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups characterised by the catalysts used
  • C08G 59/70 - Chelates
  • C08K 5/25 - Carboxylic acid hydrazides
  • C08K 5/544 - Silicon-containing compounds containing nitrogen

67.

PREPREG COMPRISING THERMOPLASTIC TOUGHENED MATRIX RESINS CONTAINING NANOPARTICLES

      
Application Number US2020056456
Publication Number 2021/112961
Status In Force
Filing Date 2020-10-20
Publication Date 2021-06-10
Owner HEXCEL CORPORATION (USA)
Inventor
  • Zhu, Yan
  • Emmerson, Gordon T.

Abstract

Pre-impregnated composite material (prepreg) that can be cured/molded to form aerospace composite parts. The prepreg includes carbon reinforcing fibers and an uncured resin matrix. The resin matrix includes an epoxy resin component, polyethersulfone as a toughening agent, a thermoplastic particle component, a nanoparticle component and a curing agent

IPC Classes  ?

  • C08J 5/24 - Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs

68.

MOULDING MATERIAL

      
Application Number EP2020076515
Publication Number 2021/099010
Status In Force
Filing Date 2020-09-23
Publication Date 2021-05-27
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor Whiter, Mark

Abstract

The present invention is concerned with a moulding material comprising: a) A primary non-woven fibre layer; b) A secondary non-woven fibre layer, and c) A resin layer; wherein the resin layer bonds the secondary non-woven fibre layer to a first surface of the primary non-woven fibre layer, and the resin layer is exposed on the second surface of the primary non- woven layer.

IPC Classes  ?

  • B32B 5/02 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by structural features of a layer comprising fibres or filaments
  • B32B 5/26 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by the presence of two or more layers which comprise fibres, filaments, granules, or powder, or are foamed or specifically porous one layer being a fibrous or filamentary layer another layer also being fibrous or filamentary
  • B32B 7/03 - Layered products characterised by the relation between layers Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties Layered products characterised by the interconnection of layers with respect to the orientation of features
  • B32B 7/09 - Interconnection of layers by mechanical means by stitching, needling or sewing
  • B32B 27/12 - Layered products essentially comprising synthetic resin next to a fibrous or filamentary layer
  • B32B 27/20 - Layered products essentially comprising synthetic resin characterised by the use of special additives using fillers, pigments, thixotroping agents
  • B32B 27/38 - Layered products essentially comprising synthetic resin comprising epoxy resins

69.

SURFACE FINISHING MOULDING MATERIAL

      
Application Number EP2020076506
Publication Number 2021/099009
Status In Force
Filing Date 2020-09-23
Publication Date 2021-05-27
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor Whiter, Mark

Abstract

A moulding material which comprises: (a) a structural reinforcement layer comprising a fibrous reinforcement material optionally in combination with a second resin composition; and (b) a surface enhancing layer, for contacting a surface of a mould or tool, comprising a first non-woven fibre carrier in combination with a first resin composition containing a rheology modifier and a curing agent, wherein the first resin composition provides an external mould or tool-contacting surface of the moulding material. The moulding material can be cured to form a moulded article having a high quality surface finish that requires minimal preparation before painting and/or application in its intended use. The moulded article may be provided with sacrificial discontinuous indicator means to assist in uniform removal of a part of the surface enhancing layer of the moulded article for specific applications.

IPC Classes  ?

  • B29C 37/00 - Component parts, details, accessories or auxiliary operations, not covered by group or
  • B29C 70/08 - Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, with or without non-reinforced layers
  • B29C 70/64 - Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising fillers only the filler influencing the surface characteristics of the material, e.g. by concentrating near the surface or by incorporation into the surface by force
  • C08J 5/24 - Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
  • B32B 5/02 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by structural features of a layer comprising fibres or filaments
  • B32B 5/26 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by the presence of two or more layers which comprise fibres, filaments, granules, or powder, or are foamed or specifically porous one layer being a fibrous or filamentary layer another layer also being fibrous or filamentary
  • B32B 27/12 - Layered products essentially comprising synthetic resin next to a fibrous or filamentary layer
  • B32B 27/20 - Layered products essentially comprising synthetic resin characterised by the use of special additives using fillers, pigments, thixotroping agents
  • B32B 27/26 - Layered products essentially comprising synthetic resin characterised by the use of special additives using curing agents
  • B32B 27/38 - Layered products essentially comprising synthetic resin comprising epoxy resins

70.

ACOUSTIC BARRIER CAPS IN ACOUSTIC HONEYCOMB

      
Application Number US2020059630
Publication Number 2021/096792
Status In Force
Filing Date 2020-11-09
Publication Date 2021-05-20
Owner HEXCEL CORPORATION (USA)
Inventor
  • Haile, Merid Minasse
  • Bowen, Lisa Diane
  • Smith, Clark Russell

Abstract

Acoustic honeycomb structures that include cells in which a friction-locking insertion process is used to locate acoustic barriers within honeycomb cells to provide multiple degree of freedom (MDOF) acoustic liners having a variety of acoustic resonator depths. Solid polymer films are formed into acoustic barrier caps. The acoustic barrier caps are friction-locked and bonded to cell walls at one or more cell depths to form acoustically reflective hard walls that form effective bottom ends for acoustic resonators.

IPC Classes  ?

  • G10K 11/172 - Methods or devices for protecting against, or for damping, noise or other acoustic waves in general using resonance effects

71.

ACOUSTIC BARRIER CAPS IN ACOUSTIC HONEYCOMB

      
Document Number 03160817
Status Pending
Filing Date 2020-11-09
Open to Public Date 2021-05-20
Owner HEXCEL CORPORATION (USA)
Inventor
  • Haile, Merid Minasse
  • Bowen, Lisa Diane
  • Smith, Clark Russell

Abstract

Acoustic honeycomb structures that include cells in which a friction-locking insertion process is used to locate acoustic barriers within honeycomb cells to provide multiple degree of freedom (MDOF) acoustic liners having a variety of acoustic resonator depths. Solid polymer films are formed into acoustic barrier caps. The acoustic barrier caps are friction-locked and bonded to cell walls at one or more cell depths to form acoustically reflective hard walls that form effective bottom ends for acoustic resonators.

IPC Classes  ?

  • B64C 1/12 - Construction or attachment of skin panels
  • B64C 7/02 - Nacelles
  • G10K 11/172 - Methods or devices for protecting against, or for damping, noise or other acoustic waves in general using resonance effects

72.

Acoustic barrier caps in acoustic honeycomb

      
Application Number 16681149
Grant Number 11437008
Status In Force
Filing Date 2019-11-12
First Publication Date 2021-05-13
Grant Date 2022-09-06
Owner HEXCEL CORPORATION (USA)
Inventor
  • Haile, Merid Minasse
  • Bowen, Lisa Diane
  • Smith, Clark Russell

Abstract

Acoustic honeycomb structures that include cells in which a friction-locking insertion process is used to locate acoustic barriers within honeycomb cells to provide multiple degree of freedom (MDOF) acoustic liners having a variety of acoustic resonator depths. Solid polymer films are formed into acoustic barrier caps. The acoustic barrier caps are friction-locked and bonded to cell walls at one or more cell depths to form acoustically reflective hard walls that form effective bottom ends for acoustic resonators.

IPC Classes  ?

  • G10K 11/162 - Selection of materials
  • B32B 3/12 - Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. apertured or formed of separate pieces of material characterised by a layer of regularly-arranged cells whether integral or formed individually or by conjunction of separate strips, e.g. honeycomb structure
  • B32B 7/12 - Interconnection of layers using interposed adhesives or interposed materials with bonding properties
  • B32B 27/06 - Layered products essentially comprising synthetic resin as the main or only constituent of a layer next to another layer of a specific substance
  • B32B 37/12 - Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by using adhesives

73.

Polymer powder and article made from the same

      
Application Number 17151637
Grant Number 12005610
Status In Force
Filing Date 2021-01-18
First Publication Date 2021-05-13
Grant Date 2024-06-11
Owner Hexcel Corporation (USA)
Inventor
  • Defelice, Scott
  • Decarmine, Anthony

Abstract

A powder composition suitable for laser sintering for printing a three-dimensional object obtained by pre-heating a raw PEKK to evaporate a liquid solvent in the raw PEKK and the grinding the raw PEKK to form a PEKK powder, the powder composition having a first fraction comprising a polyetherketoneketone (PEKK) powder having a plurality of particles, the plurality of particles having a mean diameter D50 in the range of 30 μm to 150 μm. The plurality of particles of the first fraction are substantially non-spherical.

IPC Classes  ?

  • C08G 65/46 - Post-polymerisation treatment, e.g. recovery, purification, drying
  • B02C 23/10 - Separating or sorting of material, associated with crushing or disintegrating with separator arranged in discharge path of crushing or disintegrating zone
  • B29B 9/16 - Auxiliary treatment of granules
  • B29C 64/153 - Processes of additive manufacturing using only solid materials using layers of powder being selectively joined, e.g. by selective laser sintering or melting
  • B33Y 10/00 - Processes of additive manufacturing
  • B33Y 70/10 - Composites of different types of material, e.g. mixtures of ceramics and polymers or mixtures of metals and biomaterials
  • C08G 65/40 - Macromolecular compounds obtained by reactions forming an ether link in the main chain of the macromolecule from hydroxy compounds or their metallic derivatives derived from phenols from phenols and other compounds
  • C08J 3/12 - Powdering or granulating
  • C08J 5/04 - Reinforcing macromolecular compounds with loose or coherent fibrous material
  • C08L 71/12 - Polyphenylene oxides
  • B29K 71/00 - Use of polyethers as moulding material

74.

System for identifying parts formed in an additive manufacturing build

      
Application Number 16682762
Grant Number 11255763
Status In Force
Filing Date 2019-11-13
First Publication Date 2021-05-13
Grant Date 2022-02-22
Owner Hexcel Corporation (USA)
Inventor
  • Kline, Whitney
  • Winn, Alden

Abstract

A system and method for identifying test bars formed during a selective laser sintering build. A part cake is formed during a selective laser sintering build. The part cake comprises parts formed from a powder by selective laser sintering and unsintered powder around the formed parts. The parts include test bars for performing material testing. Each test bar includes a plurality of indentations in a first grip section and a second grip section. The plurality of indentations are arranged in a information providing pattern that is adapted to be readable after the test part is removed from the part cake.

IPC Classes  ?

  • G01N 3/08 - Investigating strength properties of solid materials by application of mechanical stress by applying steady tensile or compressive forces
  • B29C 64/153 - Processes of additive manufacturing using only solid materials using layers of powder being selectively joined, e.g. by selective laser sintering or melting
  • B29L 31/40 - Test specimens
  • G06K 19/06 - Record carriers for use with machines and with at least a part designed to carry digital markings characterised by the kind of the digital marking, e.g. shape, nature, code
  • G01N 3/02 - Investigating strength properties of solid materials by application of mechanical stress Details
  • G06K 1/12 - Methods or arrangements for marking the record carrier in digital fashion otherwise than by punching
  • B29C 64/393 - Data acquisition or data processing for additive manufacturing for controlling or regulating additive manufacturing processes
  • B33Y 80/00 - Products made by additive manufacturing
  • B33Y 70/00 - Materials specially adapted for additive manufacturing

75.

EPOXY RESIN COMPOSITIONS

      
Application Number EP2020076446
Publication Number 2021/083583
Status In Force
Filing Date 2020-09-22
Publication Date 2021-05-06
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor
  • Simmons, Martin
  • Thompson, Scott
  • Mortimer, Steve

Abstract

There is provided a resin composition for producing a composite part, comprising: a) from 30 to 90 wt% by weight of the composition of an epoxy resin component; and b) from 5 to 50 wt% by weight of the composition of a curative component; wherein the epoxy resin component comprises N,N,N',N'-tetraglycidyl-4,4'-diamino- 3,3'-dimethyldiphenylmethane (M-TGDDM) in an amount of at least 30 wt% by weight of the epoxy resin component; and further wherein the curative component comprises one or more of a diaminodiphenyl sulfone, a diaminobenzophenone, a fluorene diamine, a methylene bis aniline, including hybrid methylene bis anilines, or a substituted diamine toluene. There is also provided the use of N,N,N',N'-tetraglycidyl-4,4'-diamino-3,3'- dimethyldiphenylmethane (M-TGDDM) as a compression performance improving additive in a resin composition for producing a composite part. There are also provided curable composite components, cured composite components produced therefrom and the use of such components as aircraft components.

IPC Classes  ?

  • C08G 59/24 - Di-epoxy compounds carbocyclic
  • C08G 59/32 - Epoxy compounds containing three or more epoxy groups
  • C08G 59/50 - Amines
  • C08J 5/24 - Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
  • C08K 7/02 - Fibres or whiskers
  • C08L 63/00 - Compositions of epoxy resinsCompositions of derivatives of epoxy resins

76.

Thermoplastic toughened matrix resins containing nanoparticles

      
Application Number 16660934
Grant Number 11485833
Status In Force
Filing Date 2019-10-23
First Publication Date 2021-04-29
Grant Date 2022-11-01
Owner HEXCEL CORPORATION (USA)
Inventor
  • Zhu, Yan
  • Emmerson, Gordon T.

Abstract

Pre-impregnated composite material (prepreg) that can be cured/molded to form aerospace composite parts. The prepreg includes carbon reinforcing fibers and an uncured resin matrix. The resin matrix includes an epoxy resin component, polyethersulfone as a toughening agent, a thermoplastic particle component, a nanoparticle component and a curing agent.

IPC Classes  ?

  • C08J 5/24 - Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
  • B32B 27/20 - Layered products essentially comprising synthetic resin characterised by the use of special additives using fillers, pigments, thixotroping agents
  • B32B 27/26 - Layered products essentially comprising synthetic resin characterised by the use of special additives using curing agents
  • B32B 27/38 - Layered products essentially comprising synthetic resin comprising epoxy resins
  • C08K 3/013 - Fillers, pigments or reinforcing additives
  • C08K 3/04 - Carbon
  • C08K 5/00 - Use of organic ingredients
  • C08K 5/375 - Sulfides containing six-membered aromatic rings
  • C08K 5/41 - Compounds containing sulfur bound to oxygen
  • B64C 1/00 - FuselagesConstructional features common to fuselages, wings, stabilising surfaces or the like
  • C08L 63/00 - Compositions of epoxy resinsCompositions of derivatives of epoxy resins
  • C08K 3/26 - CarbonatesBicarbonates

77.

Method for SLS of PEKK and articles manufactured from the same

      
Application Number 16953551
Grant Number 11458678
Status In Force
Filing Date 2020-11-20
First Publication Date 2021-03-11
Grant Date 2022-10-04
Owner Hexcel Corporation (USA)
Inventor
  • Defelice, Scott
  • Decarmine, Anthony

Abstract

A process for layer-by-layer manufacturing a three-dimensional object from a powder and objects made from the same is described. The process includes the step of applying a layer of a powder on a bed of a laser sintering machine. The powder includes polyetherketoneketone. The process further includes the step of solidifying selected points of the applied layer of powder by irradiation using heat energy introduced by a laser having a power L and successively repeating the step of applying the powder and the step of solidifying the applied layer of powder until all cross sections of a three-dimensional object are solidified. L is between 1 W and 20 W. In some embodiments L is between 1 and 10 W. In some embodiments, the powder is recycled PEKK powder. In some embodiments, the powder includes carbon fiber.

IPC Classes  ?

  • B29C 64/153 - Processes of additive manufacturing using only solid materials using layers of powder being selectively joined, e.g. by selective laser sintering or melting
  • B29C 64/393 - Data acquisition or data processing for additive manufacturing for controlling or regulating additive manufacturing processes
  • B33Y 50/02 - Data acquisition or data processing for additive manufacturing for controlling or regulating additive manufacturing processes
  • B29K 71/00 - Use of polyethers as moulding material

78.

SELECTIVE CONTROL OF OXIDATION ATMOSPHERES IN CARBON FIBER PRODUCTION

      
Application Number US2020047023
Publication Number 2021/034945
Status In Force
Filing Date 2020-08-19
Publication Date 2021-02-25
Owner HEXCEL CORPORATION (USA)
Inventor
  • Ferrin, Peter Andrew
  • Thomas, Devon Cadwaladar Todd

Abstract

A method for making carbon fiber in which the tensile strength of carbon fiber is increased without dehumidifying the ambient air that enters every oxidation oven in a multiple oxidation oven system. A positive effect on tensile strength is provided when ambient air entering only the first oven in a series of oxidation ovens is dehumidified. In addition, the ambient air entering the last oven is not dehumidified when one or more of the preceding oxidation ovens is operated with dehumidified air.

IPC Classes  ?

  • D01D 10/02 - Heat treatment
  • D01F 6/18 - Monocomponent man-made filaments or the like of synthetic polymersManufacture thereof from homopolymers obtained by reactions only involving carbon-to-carbon unsaturated bonds from polymers of unsaturated nitriles, e.g. polyacrylonitrile, polyvinylidene cyanide
  • D01F 9/22 - Carbon filamentsApparatus specially adapted for the manufacture thereof by decomposition of organic filaments from polyaddition, polycondensation or polymerisation products from macromolecular compounds obtained by reactions only involving carbon-to-carbon unsaturated bonds from polyacrylonitriles
  • D01F 9/32 - Apparatus therefor

79.

IMPROVED THERMOCURABLE MOULDING PROCESS

      
Application Number EP2020072507
Publication Number 2021/032537
Status In Force
Filing Date 2020-08-11
Publication Date 2021-02-25
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor Verge, Nicholas

Abstract

A fast cure cycle for thermocurable resins coupled with long storage stability is achieved by applying a curative containing particulate cure initiator to the surface of a layer of the thermocurable resin and by employing conditions of temperature and pressure to drive the curative into the resin to cause rapid cure of the resin.

IPC Classes  ?

  • C08J 5/04 - Reinforcing macromolecular compounds with loose or coherent fibrous material
  • C08J 5/24 - Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
  • C08K 5/00 - Use of organic ingredients

80.

Selective control of oxidation atmospheres in carbon fiber production

      
Application Number 16546990
Grant Number 11299824
Status In Force
Filing Date 2019-08-21
First Publication Date 2021-02-25
Grant Date 2022-04-12
Owner HEXCEL CORPORATION (USA)
Inventor
  • Ferrin, Peter Andrew
  • Thomas, Devon Cadwaladar Todd

Abstract

A method for making carbon fiber in which the tensile strength of carbon fiber is increased without dehumidifying the ambient air that enters every oxidation oven in a multiple oxidation oven system. A positive effect on tensile strength is provided when ambient air entering only the first oven in a series of oxidation ovens is dehumidified. In addition, the ambient air entering the last oven is not dehumidified when one or more of the preceding oxidation ovens is operated with dehumidified air.

IPC Classes  ?

  • D01F 9/22 - Carbon filamentsApparatus specially adapted for the manufacture thereof by decomposition of organic filaments from polyaddition, polycondensation or polymerisation products from macromolecular compounds obtained by reactions only involving carbon-to-carbon unsaturated bonds from polyacrylonitriles
  • C01B 32/05 - Preparation or purification of carbon not covered by groups , , ,
  • D01F 9/32 - Apparatus therefor

81.

High temperature composite honeycomb

      
Application Number 16518528
Grant Number 10947354
Status In Force
Filing Date 2019-07-22
First Publication Date 2021-01-28
Grant Date 2021-03-16
Owner HEXCEL CORPORATION (USA)
Inventor
  • Loesch, Robert Charles
  • Haile, Merid Minasse
  • Ayle, Earl Frederick
  • Smith, Clark Russell

Abstract

Composite honeycomb that may be contoured to form composite honeycomb structures, which have tight radii of curvatures and/or compound curvatures, and which are suitable for use in high temperature environments. The method for making the composite honeycomb involves using high temperature prepreg to make a flexible composite honeycomb that is formed into a composite honeycomb precursor. A high temperature coating resin is applied to the composite honeycomb precursor to form the high temperature composite honeycomb.

IPC Classes  ?

  • C08J 5/24 - Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
  • C08J 5/04 - Reinforcing macromolecular compounds with loose or coherent fibrous material
  • B32B 27/38 - Layered products essentially comprising synthetic resin comprising epoxy resins

82.

HIGH TEMPERATURE COMPOSITE HONEYCOMB

      
Application Number US2020041756
Publication Number 2021/015971
Status In Force
Filing Date 2020-07-13
Publication Date 2021-01-28
Owner HEXCEL CORPORATION (USA)
Inventor
  • Loesch, Robert Charles
  • Haile, Merid Minasse
  • Ayle, Earl Frederick
  • Smith, Clark Russell

Abstract

Composite honeycomb that may be contoured to form composite honeycomb structures, which have tight radii of curvatures and/or compound curvatures, and which are suitable for use in high temperature environments. The method for making the composite honeycomb involves using high temperature prepreg to make a flexible composite honeycomb that is formed into a composite honeycomb precursor. A high temperature coating resin is applied to the composite honeycomb precursor to form the high temperature composite honeycomb

IPC Classes  ?

  • B32B 3/08 - Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions characterised by added members at particular parts
  • B32B 3/12 - Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. apertured or formed of separate pieces of material characterised by a layer of regularly-arranged cells whether integral or formed individually or by conjunction of separate strips, e.g. honeycomb structure
  • B32B 5/02 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by structural features of a layer comprising fibres or filaments
  • B32B 7/12 - Interconnection of layers using interposed adhesives or interposed materials with bonding properties
  • B32B 37/00 - Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
  • E04C 2/36 - 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

83.

PREPREG OR SEMIPREG PRECURSOR AND METHOD OF MANUFACTURING SAME

      
Application Number EP2020070388
Publication Number 2021/013770
Status In Force
Filing Date 2020-07-17
Publication Date 2021-01-28
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor
  • Whiter, Mark
  • Tipler, Ben
  • Maillot, Mathilde

Abstract

A prepreg or semipreg precursor comprising a fibre reinforcement and a resin composition fused thereto, the resin composition containing at least one epoxy resin and a latent curing agent, wherein the epoxy resin and the latent curing agent form a solid phase at ambient temperature, the latent curing agent forming a discrete phase within the epoxy resin. The stabilized uncured resin composition and prepregs and semipregs incorporating the same are easy to handle, have desirable curing temperatures and show good outlife at ambient to mid range temperatures.

IPC Classes  ?

  • C08L 63/00 - Compositions of epoxy resinsCompositions of derivatives of epoxy resins
  • C08J 3/24 - Crosslinking, e.g. vulcanising, of macromolecules
  • C08J 5/04 - Reinforcing macromolecular compounds with loose or coherent fibrous material
  • C08J 5/24 - Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs

84.

MATRIX RESINS TOUGHENED WITH HYBRID POLYAMIDE PARTICLES

      
Application Number US2020039294
Publication Number 2021/003047
Status In Force
Filing Date 2020-06-24
Publication Date 2021-01-07
Owner HEXCEL CORPORATION (USA)
Inventor Wang, Yen-Seine

Abstract

Pre-impregnated composite material (prepreg) that can be cured/molded to form aerospace composite parts. The prepreg includes carbon reinforcing fibers and an uncured resin matrix. The resin matrix includes an epoxy component, polyethersulfone as a toughening agent, and a curing agent. The resin matrix is also composed of a thermoplastic particle component that includes hybrid polyamide particles wherein each hybrid particle contains a mixture of amorphous and semi-crystalline polyamide.

IPC Classes  ?

  • C08J 5/24 - Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
  • C08J 5/04 - Reinforcing macromolecular compounds with loose or coherent fibrous material

85.

Curative composition and a resin composition containing the curative composition

      
Application Number 16769762
Grant Number 11702516
Status In Force
Filing Date 2018-12-20
First Publication Date 2020-12-10
Grant Date 2023-07-18
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor
  • Tilbrook, David Allan
  • Mason, Christopher Robert
  • Simmons, Martin Richard

Abstract

This invention relates to a curative composition and its use in curing epoxy resins and prepregs, adhesives and moulded materials derived therefrom. The curative composition comprises a clathrate comprising a host component and a guest component, the host comprising a carboxylic acid or ester compounds as defined or phenolphthalin and the guest comprising an imidazole or imidazoline component.

IPC Classes  ?

  • C08J 3/24 - Crosslinking, e.g. vulcanising, of macromolecules
  • C08G 59/50 - Amines
  • C08K 9/10 - Encapsulated ingredients
  • C08L 63/00 - Compositions of epoxy resinsCompositions of derivatives of epoxy resins
  • C08J 5/24 - Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
  • C08K 5/3445 - Five-membered rings
  • C08K 5/13 - PhenolsPhenolates
  • C08K 5/09 - Carboxylic acidsMetal salts thereofAnhydrides thereof

86.

POLYMER POWDER COMPOSITION FOR ADDITIVE MANUFACTURING

      
Application Number US2020022546
Publication Number 2020/242554
Status In Force
Filing Date 2020-03-13
Publication Date 2020-12-03
Owner HEXCEL CORPORATION (USA)
Inventor
  • Kline, Whitney
  • Winn, Alden
  • Varholak, Lawrence

Abstract

A powder composition suitable for use in selective laser sintering for printing an object. The powder composition includes a first fraction having a polyetherketoneketone (PEKK) powder having a plurality of particles. The powder composition includes a second fraction having a plurality of siloxane particles that is dry blended with the PEKK powder prior to selective laser sintering of the powder. In some embodiments, the powder composition includes a third fraction of carbon fiber. The powder composition when used in selective laser sintering results in parts with more consistent results and improves process economics.

IPC Classes  ?

  • C08G 64/00 - Macromolecular compounds obtained by reactions forming a carbonic ester link in the main chain of the macromolecule
  • C08G 63/02 - Polyesters derived from hydroxy carboxylic acids or from polycarboxylic acids and polyhydroxy compounds

87.

System for selective laser sintering

      
Application Number 16604934
Grant Number 11312069
Status In Force
Filing Date 2018-04-25
First Publication Date 2020-12-03
Grant Date 2022-04-26
Owner Hexcel Corporation (USA)
Inventor
  • Defelice, Scott
  • Decarmine, Anthony

Abstract

A system for producing an object from a powder by selective laser sintering. The system includes a chamber and a support platform in the chamber. A spreader applies a layer of powder to a bed surface. An irradiation source irradiates select points in the powdered layer prepared on the support platform. A radiant heater heats at least a portion of the bed surface. A temperature sensor monitors the temperature of select points on the bed surface. A controller adjusts the radiant heater in response to temperature data provided by the temperature sensor.

IPC Classes  ?

  • B29C 64/153 - Processes of additive manufacturing using only solid materials using layers of powder being selectively joined, e.g. by selective laser sintering or melting
  • B33Y 30/00 - Apparatus for additive manufacturingDetails thereof or accessories therefor
  • B33Y 50/02 - Data acquisition or data processing for additive manufacturing for controlling or regulating additive manufacturing processes
  • B29C 64/295 - Heating elements
  • B29C 64/393 - Data acquisition or data processing for additive manufacturing for controlling or regulating additive manufacturing processes
  • B29C 64/268 - Arrangements for irradiation using laser beamsArrangements for irradiation using electron beams [EB]
  • B29K 71/00 - Use of polyethers as moulding material

88.

Twice recycled polymer powder composition for additive manufacturing including PEKK, siloxane and carbon fiber

      
Application Number 16422283
Grant Number 11993722
Status In Force
Filing Date 2019-05-24
First Publication Date 2020-11-26
Grant Date 2024-05-28
Owner Hexcel Corporation (USA)
Inventor
  • Kline, Whitney
  • Winn, Alden
  • Varholak, Lawrence

Abstract

A powder composition suitable for use in selective laser sintering for printing an object. The powder composition includes a first fraction having a polyetherketoneketone (PEKK) powder having a plurality of particles. The powder composition includes a second fraction having a plurality of siloxane particles that is dry blended with the PEKK powder prior to selective laser sintering of the powder. In some embodiments, the powder composition includes a third fraction of carbon fiber. The powder composition when used in selective laser sintering results in parts with more consistent results and improves process economics.

IPC Classes  ?

  • C09D 11/102 - Printing inks based on artificial resins containing macromolecular compounds obtained by reactions other than those only involving unsaturated carbon-to-carbon bonds
  • B29C 64/153 - Processes of additive manufacturing using only solid materials using layers of powder being selectively joined, e.g. by selective laser sintering or melting
  • B29C 64/20 - Apparatus for additive manufacturingDetails thereof or accessories therefor
  • B29K 71/00 - Use of polyethers as moulding material
  • B33Y 10/00 - Processes of additive manufacturing
  • B33Y 30/00 - Apparatus for additive manufacturingDetails thereof or accessories therefor
  • B33Y 70/00 - Materials specially adapted for additive manufacturing
  • C09D 11/037 - Printing inks characterised by features other than the chemical nature of the binder characterised by the pigment

89.

Reinforcement material comprising a porous layer made of partially cross-linked thermoplastic polymer and associated methods

      
Application Number 16762104
Grant Number 11370196
Status In Force
Filing Date 2018-11-20
First Publication Date 2020-11-12
Grant Date 2022-06-28
Owner HEXCEL REINFORCEMENTS SASU (France)
Inventor
  • Viard, Andréa
  • Benethuiliere, Thibaut

Abstract

The present invention relates to a reinforcement material including at least one fiber reinforcement associated on at least one of its faces with a porous layer, the porous layer(s) representing no more than 10% of the total weight of the reinforcement material, preferably from 0.5 to 10% of the total weight of the reinforcement material, and most preferably from 2 to 6% of the total weight of the reinforcement material, characterized in that the porous layer contains a partially cross-linked thermoplastic polymer. Another object of the invention is a precursor material of such a reinforcement material, as well as their preparation method and the methods for manufacturing a preform or a composite part from such materials.

IPC Classes  ?

  • B32B 5/26 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by the presence of two or more layers which comprise fibres, filaments, granules, or powder, or are foamed or specifically porous one layer being a fibrous or filamentary layer another layer also being fibrous or filamentary
  • B32B 7/09 - Interconnection of layers by mechanical means by stitching, needling or sewing
  • B32B 7/027 - Thermal properties
  • B32B 3/10 - Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. apertured or formed of separate pieces of material
  • B32B 5/02 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by structural features of a layer comprising fibres or filaments
  • B32B 7/12 - Interconnection of layers using interposed adhesives or interposed materials with bonding properties
  • B32B 27/12 - Layered products essentially comprising synthetic resin next to a fibrous or filamentary layer
  • B32B 27/34 - Layered products essentially comprising synthetic resin comprising polyamides
  • B32B 37/06 - Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the heating method
  • C08F 283/00 - Macromolecular compounds obtained by polymerising monomers on to polymers provided for in subclass

90.

IMPROVEMENTS IN OR RELATING TO CURATIVES

      
Application Number EP2020060885
Publication Number 2020/216688
Status In Force
Filing Date 2020-04-17
Publication Date 2020-10-29
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor Mason, Chris

Abstract

The host compound in a clathrate is an amino or hydroxyl containing aromatic phosphorous compound, clathrates containing a resin curative and their use in curable resin compositions to produce moulded articles particularly fibre reinforced articles.

IPC Classes  ?

  • C07F 9/30 - Phosphinic acids [R2=P(:O)OH]Thiophosphinic acids
  • C08G 59/00 - Polycondensates containing more than one epoxy group per moleculeMacromolecules obtained by reaction of epoxy polycondensates with monofunctional low-molecular-weight compoundsMacromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups
  • C09J 163/00 - Adhesives based on epoxy resinsAdhesives based on derivatives of epoxy resins

91.

SELF-ADHESIVE PREPREG

      
Application Number EP2020060918
Publication Number 2020/216691
Status In Force
Filing Date 2020-04-17
Publication Date 2020-10-29
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor Rhodes, Michael

Abstract

A self-adhesive prepreg comprising a fibre reinforcement layer having a first side and a second side, wherein the first side of the fibre reinforcement layer has been pre-impregnated with a self-adhesive resin composition. The self-adhesive may be used as a structural reinforcement and is especially adapted for direct bonding to oily steel or galvanized steel in the automotive, aerospace and other sheet metal fabrication industries.

IPC Classes  ?

  • C08J 5/24 - Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs

92.

PEEL PLY FOR ELONGATE COMPOSITE MATERIALS

      
Application Number EP2020059469
Publication Number 2020/207905
Status In Force
Filing Date 2020-04-02
Publication Date 2020-10-15
Owner
  • HEXCEL COMPOSITES LIMITED (United Kingdom)
  • HEXCEL HOLDING GMBH (Austria)
  • HEXCEL CORPORATION (USA)
Inventor
  • Moser, Johannes
  • Hung, Yu-Chen
  • Reagan, Erin

Abstract

An assembly (113) for composite manufacture is provided. The assembly comprises a cured resin impregnated reinforcement material (112) comprising a fibre component and a resin matrix component, in which the resin matrix component comprises polyurethane, the assembly having a length to width ratio of at least 5:1, and the assembly defining a longitudinal direction (L) along its length; and a peel ply (116) in contact with the cured resin impregnated reinforcement material (112), the peel ply (116) comprising a woven layer having a plurality of longitudinal fibres (118) extending in the longitudinal direction (L); and a plurality of transverse fibres (120) extending in a transverse direction (T) normal to the longitudinal direction (L); in which the areal density of the plurality of transverse fibres (120) is higher than the areal density of the plurality of longitudinal fibres (118).

IPC Classes  ?

  • B29C 59/00 - Surface shaping, e.g. embossingApparatus therefor
  • B29C 65/00 - Joining of preformed partsApparatus therefor
  • B29C 70/54 - Component parts, details or accessoriesAuxiliary operations

93.

Rocket booster casings made with semipreg having a thermoplastic toughened novolac-based epoxy resin matrix

      
Application Number 16592589
Grant Number 10787997
Status In Force
Filing Date 2019-10-03
First Publication Date 2020-09-29
Grant Date 2020-09-29
Owner HEXCEL CORPORATION (USA)
Inventor
  • Baron, Kathlyn Lizette
  • Emmerson, Gordon
  • Wang, Yen-Seine

Abstract

A semipreg that can be cured/molded to form aerospace composite parts including rocket booster casings. The semipreg includes a fibrous layer and a resin layer located on one side of the fibrous layer. The resin layer includes an epoxy component that is a combination of a hydrocarbon epoxy novolac resin and a trifunctional epoxy resin and optionally a tetrafunctional epoxy resin. The resin matrix includes polyethersulfone as a toughening agent and a thermoplastic particle component.

IPC Classes  ?

  • F02K 9/34 - CasingsCombustion chambersLiners thereof
  • B29C 70/50 - Shaping or impregnating by compression for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
  • B29B 15/12 - Coating or impregnating of reinforcements of indefinite length
  • C08L 63/04 - Epoxynovolacs
  • C08L 77/06 - Polyamides derived from polyamines and polycarboxylic acids
  • C08L 79/08 - PolyimidesPolyester-imidesPolyamide-imidesPolyamide acids or similar polyimide precursors

94.

Unwinding of materials

      
Application Number 16756074
Grant Number 11358828
Status In Force
Filing Date 2018-10-18
First Publication Date 2020-08-13
Grant Date 2022-06-14
Owner
  • HEXCEL COMPOSITES LIMITED (United Kingdom)
  • HEXCEL CORPORATION (USA)
Inventor
  • Ellis, John
  • Loccisano, Anthony

Abstract

There is provide a process for unwinding material from a spool (2) wherein the angle (Θ) of take off at the first contact point (4) for the unwind is always in the range 0±20°, and wherein the first contact point (4) for the unwind is no more than 600 mm from the axis (3) of rotation of the spool (2). There is also provided an apparatus for the unwinding of material from a spool (2) comprising an axis (3) upon which a spool (2) may be rotatably mounted and a static first contact point (4) for the unwound material positioned no more than 600 mm from the centre of the axis (3), wherein the angle (Θ) of take off at the first contact point (4) for the unwind is always in the range 0±20°.

IPC Classes  ?

95.

Polymer powder and method of preparing the same

      
Application Number 16854290
Grant Number 11090838
Status In Force
Filing Date 2020-04-21
First Publication Date 2020-08-06
Grant Date 2021-08-17
Owner Hexcel Corporation (USA)
Inventor
  • Defelice, Scott
  • Decarmine, Anthony

Abstract

A powder composition suitable for use in laser sintering for printing a three-dimensional object. The powder composition includes a polyaryletherketone (PAEK) powder having a plurality of particles. The plurality of particles having a mean diameter of D50. The composition includes a plurality of carbon fibers having a mean length L50. L50 is greater than D50. The particles are substantially non-spherical. A portion of the carbon fiber is embedded into the particle via high intensity mixing.

IPC Classes  ?

  • C08L 71/12 - Polyphenylene oxides
  • B29B 9/16 - Auxiliary treatment of granules
  • B33Y 70/00 - Materials specially adapted for additive manufacturing
  • B29C 64/153 - Processes of additive manufacturing using only solid materials using layers of powder being selectively joined, e.g. by selective laser sintering or melting
  • B02C 23/10 - Separating or sorting of material, associated with crushing or disintegrating with separator arranged in discharge path of crushing or disintegrating zone
  • C08G 65/46 - Post-polymerisation treatment, e.g. recovery, purification, drying
  • B33Y 10/00 - Processes of additive manufacturing
  • C08G 65/40 - Macromolecular compounds obtained by reactions forming an ether link in the main chain of the macromolecule from hydroxy compounds or their metallic derivatives derived from phenols from phenols and other compounds
  • C08J 3/12 - Powdering or granulating
  • C08J 5/04 - Reinforcing macromolecular compounds with loose or coherent fibrous material
  • B29K 71/00 - Use of polyethers as moulding material

96.

HYBRID-CAP

      
Application Number 018272302
Status Registered
Filing Date 2020-07-14
Registration Date 2020-11-27
Owner Hexcel Corporation (USA)
NICE Classes  ?
  • 06 - Common metals and ores; objects made of metal
  • 17 - Rubber and plastic; packing and insulating materials

Goods & Services

Metallic cellular core material and metallic sandwich panels for use in manufacturing aerospace, space and defence, recreation, electrical, architectural, marine, transportation and general industrial products; Metallic honeycomb and metallic sandwich panels. Soundproofing materials for airplane engines and other portions of airplanes in the nature of cellular core material with inserts for noise reduction.

97.

IMPROVED THERMOCURABLE MOULDING PROCESS

      
Application Number EP2019086496
Publication Number 2020/127855
Status In Force
Filing Date 2019-12-19
Publication Date 2020-06-25
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor Verge, Nicholas

Abstract

A fast cure cycle for thermocurable resins coupled with long storage stability is achieved by applying a curative containing particulate cure initiator to the surface of a layer of the thermocurable resin and by employing conditions of temperature and pressure that drive the curative into the resin to cause rapid cure of the resin.

IPC Classes  ?

  • C08J 5/24 - Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
  • C08J 5/04 - Reinforcing macromolecular compounds with loose or coherent fibrous material
  • C08K 5/00 - Use of organic ingredients

98.

ADHESIVE COMPOSITION

      
Application Number EP2019083490
Publication Number 2020/115041
Status In Force
Filing Date 2019-12-03
Publication Date 2020-06-11
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor Rhodes, Michael

Abstract

An adhesive composition comprising a silane-modified epoxy resin, a dicyclopentadiene novolac epoxy resin and a curing agent. The composition shows good oily steel bonding, even in the absence of CTBN rubber or rubber adducts as toughening agents, with good Tg values of the cured resin and good Tg retention after hot wet aging.

IPC Classes  ?

  • C09J 163/04 - Epoxynovolacs
  • C08G 59/14 - Polycondensates modified by chemical after-treatment
  • C08G 59/32 - Epoxy compounds containing three or more epoxy groups
  • C08G 59/40 - Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups characterised by the curing agents used

99.

Polymer powder and object made from the same

      
Application Number 16778721
Grant Number 11161967
Status In Force
Filing Date 2020-01-31
First Publication Date 2020-05-28
Grant Date 2021-11-02
Owner Hexcel Corporation (USA)
Inventor
  • Kline, Whitney
  • Varholak, Lawrence

Abstract

A powder composition suitable for use in selective laser sintering for printing an object. The powder composition includes a first fraction including a plurality of polyaryletherketone (PAEK) particles having a mean diameter less than 30 microns, a second fraction having a plurality of polyaryletherketone (PAEK) particles having a mean diameter greater than 30 microns, and a third fraction having a plurality of carbon fibers. The first fraction and the second fraction are formed by an air classification separation performed on a pulverized powder. After the separation, the first fraction, the second fraction, and the third fraction are blended in a high intensity mixer. The powder composition when used in selective laser sinter results in parts with increased tensile strength and reduced surface roughness, among other improvements, as compared to similar powders omitting the first fraction. The PAEK may include polyetherketoneketone (PEKK).

IPC Classes  ?

  • C08K 7/06 - Elements
  • B33Y 70/00 - Materials specially adapted for additive manufacturing
  • B29B 9/02 - Making granules by dividing preformed material
  • B33Y 30/00 - Apparatus for additive manufacturingDetails thereof or accessories therefor

100.

METHOD OF MANUFACTURE OF A COMPOSITE MATERIAL

      
Application Number EP2019080759
Publication Number 2020/104221
Status In Force
Filing Date 2019-11-08
Publication Date 2020-05-28
Owner HEXCEL COMPOSITES LIMITED (United Kingdom)
Inventor Arcidiacono, Marco

Abstract

A method of manufacture of a composite component is provided, the method comprising the steps of providing two layers of pre-preg composite material, one of which has an edge adjacent a surface of the other. Pressure and, optionally, vibrational energy is applied to the edge to thereby smooth the ply drop.

IPC Classes  ?

  • B29C 70/54 - Component parts, details or accessoriesAuxiliary operations
  • B29C 70/38 - Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
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