公开(公告)号：US20150210847A1

公开(公告)日：2015-07-30

申请号：US14422721

申请日：2013-09-25

Applicant: Hexcel Composites Limited

Inventor： Stephen Mortimer ,  Scott Stevens

IPC: C08L63/00 ,  C08L67/00 ,  C08L79/08 ,  C08L33/04 ,  C08L79/04

CPC classification number: C08L63/00 ,  C08G59/245 ,  C08G59/5033 ,  C08G59/504 ,  C08J5/24 ,  C08L33/04 ,  C08L67/00 ,  C08L79/04 ,  C08L79/08 ,  C08L2205/025 ,  C08L2205/03 ,  C08L51/04

Abstract: A resin composition for producing a composite part, comprising a first resin component comprising a glycidyl ether epoxy resin, a second resin component comprising a naphthalene based epoxy resin, and an amino-phenyl fluorene curative; wherein the epoxy resin components a) and b) contain up to 33 wt % of the second resin component.

Abstract translation: 一种复合部件的制造用树脂组合物，其含有包含缩水甘油醚环氧树脂的第一树脂组分，包含萘系环氧树脂的第二树脂组分和氨基苯基芴固化剂; 其中所述环氧树脂组分a）和b）含有至多33重量％的第二树脂组分。

公开(公告)号：US20140316551A1

公开(公告)日：2014-10-23

申请号：US14360396

申请日：2012-12-21

Applicant: Hexcel Composites Limited

Inventor： John Ellis ,  Andrea Caballero

IPC: B05C11/00

CPC classification number: B05C11/00 ,  B29C70/50 ,  B29C70/54 ,  B32B41/00 ,  B32B2310/028 ,  G01N27/90 ,  G01N29/0663 ,  G01N29/07 ,  G01N29/4472 ,  G01N33/442 ,  G01N2291/0231 ,  G01R35/00 ,  Y02P80/40

Abstract: A method of controlling a process for the manufacture of a multicomponent sheet material having a desired pre-determined parameter comprising applying an acoustic or an electromagnetic signal to interact with the sheet material whereby the interaction modifies the applied signal, detecting the modified signal, comparing the modified signal or data derived from it with data relating to the pre-determined parameter and modifying at least one step of the process whereby the data relating to the modified signal is modified towards the data relating to the pre-determined parameter.

Abstract translation: 一种控制用于制造具有期望的预定参数的多组分片材的方法的方法，包括施加声学或电磁信号以与片材相互作用，由此相互作用修改施加的信号，检测修改的信号，比较 修改的信号或从其导出的数据，其具有与预定参数相关的数据，并修改该过程的至少一个步骤，由此将与修改信号有关的数据修改为与预定参数相关的数据。

公开(公告)号：US20140110877A1

公开(公告)日：2014-04-24

申请号：US14133965

申请日：2013-12-19

Applicant: Hexcel Composites Limited

Inventor： Stephen Mortimer ,  John Cawse

IPC: B29C70/02

CPC classification number: B29C70/025 ,  B29C70/086 ,  C08J5/24

Abstract: A non-fibrous, apertured membrane comprises at least one thermoplastic polymeric material and has a discrete porous structure. The membrane is soluble in the thermoset matrix polymer of a composite material.

Abstract translation: 非纤维状多孔膜包含至少一种热塑性聚合物材料并且具有离散的多孔结构。 膜可溶于复合材料的热固性基质聚合物。

公开(公告)号：US20130260022A1

公开(公告)日：2013-10-03

申请号：US13904306

申请日：2013-05-29

Applicant: Hexcel Composites Limited ,  Hexcel Corporation

Inventor： Maureen Boyle ,  Dana Blair ,  Yi-Jui Wu ,  Yen-Seine Wang ,  Bryce Floryancic ,  Paul Mackenzie

IPC: B32B38/08

CPC classification number: B32B38/08 ,  C08G59/184 ,  C08G59/4042 ,  C08G59/5033 ,  C08J5/24 ,  C08J2363/00 ,  C08L63/00 ,  C08L2205/035 ,  Y10T428/254

Abstract: Composite material that contain epoxy resin which is toughened and strengthened with thermoplastic materials and a blend of insoluble particles. The uncured matrix resins include an epoxy resin component, a soluble thermoplastic component, a curing agent and an insoluble particulate component composed of elastic particles and rigid particles. The uncured resin matrix is combined with a fibrous reinforcement and cured/molded to form composite materials that may be used for structural applications, such as primary structures in aircraft.

Abstract translation: 含有环氧树脂的复合材料，其用热塑性材料增韧和增强，以及不溶性颗粒的混合物。 未固化的基质树脂包括环氧树脂组分，可溶性热塑性组分，固化剂和由弹性颗粒和刚性颗粒组成的不溶性颗粒组分。 将未固化的树脂基质与纤维增强剂结合并固化/模制以形成可用于结构应用的复合材料，例如飞行器中的主要结构。

公开(公告)号：US12240954B2

公开(公告)日：2025-03-04

申请号：US17770567

申请日：2020-09-23

Applicant: HEXCEL COMPOSITES LIMITED

Inventor： Mark Whiter

IPC: C08J5/24 ,  B29C70/18 ,  B32B5/02 ,  B32B27/20 ,  B32B27/38 ,  B29K63/00 ,  B29K309/08

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.

公开(公告)号：US20240158627A1

公开(公告)日：2024-05-16

申请号：US17768263

申请日：2020-09-22

Applicant: HEXCEL COMPOSITES LIMITED

Inventor： Martin Richard SIMMONS ,  Scott THOMPSON ,  Stephen MORTIMER

IPC: C08L63/00 ,  C08G59/50 ,  C08L87/00

CPC classification number: C08L63/00 ,  C08G59/504 ,  C08L87/00 ,  C08L2205/035

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.

公开(公告)号：US11702516B2

公开(公告)日：2023-07-18

申请号：US16769762

申请日：2018-12-20

Applicant: HEXCEL COMPOSITES LIMITED

Inventor： David Allan Tilbrook ,  Christopher Robert Mason ,  Martin Richard Simmons

IPC: C08J3/24 ,  C08G59/50 ,  C08K9/10 ,  C08L63/00 ,  C08J5/24 ,  C08K5/3445 ,  C08K5/13 ,  C08K5/09

CPC classification number: C08J3/241 ,  C08G59/50 ,  C08J5/243 ,  C08K5/09 ,  C08K5/13 ,  C08K5/3445 ,  C08K9/10 ,  C08L63/00 ,  C08J2363/00

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.

公开(公告)号：US20220212424A1

公开(公告)日：2022-07-07

申请号：US17602095

申请日：2020-04-02

Applicant: Hexcel Composites Limited ,  Hexcel Holding GMBH ,  Hexcel Corporation

Inventor： Johannes MOSER ,  Yu-Chen HUNG ,  Erin REAGAN

IPC: B29C70/52 ,  B29C70/54 ,  B29C70/68

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).

公开(公告)号：US20210246276A1

公开(公告)日：2021-08-12

申请号：US17049869

申请日：2019-05-17

Applicant: HEXCEL COMPOSITES LIMITED ,  HEXCEL HOLDING GMBH

Inventor： Nicholas VERGE ,  Thorsten GANGLBERGER

IPC: C08J5/24 ,  C08G59/24 ,  C08G59/40

Abstract: A curative resin containing at least 50 wt % of an epoxy phenolic resin comprising a mixture of a carboxylic hydrazide and a hydroxy substituted urone.

公开(公告)号：US20210214550A1

公开(公告)日：2021-07-15

申请号：US15734008

申请日：2019-06-13

Applicant: HEXCEL COMPOSITES LIMITED

Inventor： Dana BLAIR

IPC: C08L63/04 ,  C08G59/30 ,  C08G59/24 ,  C08G59/40 ,  C08K3/02 ,  C08K3/22 ,  C08K3/32 ,  C08K5/3492 ,  C08K5/52 ,  C08J5/04 ,  C08J5/24

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.