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公开(公告)号：US11332607B2
公开(公告)日：2022-05-17
申请号：US15734008
申请日：2019-06-13
Applicant: HEXCEL COMPOSITES LIMITED
Inventor： Dana Blair
IPC: C08J5/24 , C08L63/04 , C08L63/02 , C08L63/00 , C08G59/38 , C08G59/24 , C08G59/30 , C08G59/40 , C08J5/04 , C08K3/02 , C08K3/22 , C08K3/32 , C08K5/3492 , C08K5/52
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.
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公开(公告)号：US20160369074A1
公开(公告)日：2016-12-22
申请号：US15100303
申请日：2014-12-24
Applicant: Hexcel Composites Limited
Inventor： Philip Hadley , Ben Tipler , Dana Blair
CPC classification number: C08J5/24 , C08J3/126 , C08J5/10 , C08J2363/00 , C08J2377/00 , C08J2400/24 , C08J2463/00 , C08J2477/00
Abstract: This invention relates to an additive for a thermoset resin matrix having a core and a reactive cross-linked thermoset coating. The reactive cross-linked thermoset coating is the reaction product of a thermoset resin and a curative in a dispersant.
Abstract translation: 本发明涉及一种用于具有芯和反应性交联热固性涂层的热固性树脂基质的添加剂。 反应性交联热固性涂层是热固性树脂和分散剂中的固化剂的反应产物。
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Patent Agency Ranking
公开(公告)号：US20150179298A1
公开(公告)日：2015-06-25
申请号：US14405880
申请日：2013-06-14
Applicant: Hexcel Composites Limited
Inventor： Martin Simmons , Dana Blair , David Tilbrook
IPC: H01B1/24
CPC classification number: H01B1/24 , B29C70/025 , B32B5/022 , B32B5/12 , B32B5/26 , B32B5/28 , B32B17/04 , B32B2250/20 , B32B2260/023 , B32B2260/046 , B32B2262/0269 , B32B2262/101 , B32B2262/106 , B32B2307/202 , B32B2307/518 , B32B2307/54 , B32B2307/558 , B32B2307/718 , B32B2605/18 , B64C1/00 , B64C2001/0072 , C08J5/24 , C08J2363/00 , C08J2477/02 , C08J2481/06 , Y02T50/43
Abstract: A prepreg comprising a fibre reinforced curable resin, the prepreg containing electrically conductive particles in the range of from 0.5 to 10% by weight based on the resin, the electrically conductive particles comprising potato shaped graphite.
Abstract translation: 一种包含纤维增强固化树脂的预浸料，所述预浸料含有基于树脂为0.5-10重量％的导电颗粒，所述导电颗粒包含马铃薯状石墨。
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公开(公告)号：US09034975B2
公开(公告)日：2015-05-19
申请号：US13904306
申请日：2013-05-29
Applicant: Hexcel Corporation , Hexcel Composites Limited
Inventor： Maureen Boyle , Dana Blair , Yi-Jui Wu , Yen-Seine Wang , Bryce Floryancic , Paul Mackenzie
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。
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公开(公告)号：US20140217332A1
公开(公告)日：2014-08-07
申请号：US14249380
申请日：2014-04-10
Applicant: Hexcel Corporation , Hexcel Composites Limited
Inventor： Martin Simmons , Dana Blair , David Tilbrook , Maureen Boyle
CPC classification number: H01B1/24 , B29C70/025 , B32B5/022 , B32B5/12 , B32B5/26 , B32B5/28 , B32B17/04 , B32B2250/20 , B32B2260/023 , B32B2260/046 , B32B2262/0269 , B32B2262/101 , B32B2262/106 , B32B2307/202 , B32B2307/518 , B32B2307/54 , B32B2307/558 , B32B2307/718 , B32B2605/18 , B64C1/00 , B64C2001/0072 , C08J5/24 , C08J2363/00 , C08J2477/02 , C08J2481/06 , Y02T50/43
Abstract: A prepreg comprising a fibre reinforced curable resin, the curable resin being composed of 25 to 35 weight percent tetrafunctional epoxy resin based on the total weight of the curable resin; 18 to 28 weight percent difunctional epoxy resin; 4 to 18 weight percent polyether sulfone; 2 to 10 weight percent polyamide 12 particles; 2 to 10 weight percent polyamide 11 particles; 1 to 8 weight percent potato shaped graphite particles; and 17.4 to 27.4 weight percent of a curing agent for said curable resin.
Abstract translation: 一种预浸料，其包含纤维增强固化树脂，所述可固化树脂由25至35重量％的四官能环氧树脂组成，基于所述可固化树脂的总重量; 18〜28重量％双官能环氧树脂; 4至18重量％的聚醚砜; 2至10重量％的聚酰胺12颗粒; 2至10重量％的聚酰胺11颗粒; 1至8重量％的马铃薯状石墨颗粒; 和17.4〜27.4重量％的所述固化性树脂的固化剂。
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公开(公告)号：US09868833B2
公开(公告)日：2018-01-16
申请号：US15100303
申请日：2014-12-24
Applicant: Hexcel Composites Limited
Inventor： Philip Hadley , Ben Tipler , Dana Blair
CPC classification number: C08J5/24 , C08J3/126 , C08J5/10 , C08J2363/00 , C08J2377/00 , C08J2400/24 , C08J2463/00 , C08J2477/00
Abstract: This invention relates to an additive for a thermoset resin matrix having a core and a reactive cross-linked thermoset coating. The reactive cross-linked thermoset coating is the reaction product of a thermoset resin and a curative in a dispersant.
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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。
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