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    INCREASE IN THE TOUGHNESS OF A MATERIAL OBTAINED FROM A CURABLE COMPOSITION COMPRISING AT LEAST ONE VINYL ESTER MONOMER
    2.
    发明申请
    INCREASE IN THE TOUGHNESS OF A MATERIAL OBTAINED FROM A CURABLE COMPOSITION COMPRISING AT LEAST ONE VINYL ESTER MONOMER 有权
    从包含至少一个乙烯基单体的可固化组合物获得的材料的粗糙度增加

    公开(公告)号：US20120277383A1

    公开(公告)日：2012-11-01

    申请号：US13500844

    申请日：2010-10-08

    Applicant: Mickael Krzeminski ,  Brigitte Defoort ,  Xavier Coqueret

    Inventor： Mickael Krzeminski ,  Brigitte Defoort ,  Xavier Coqueret

    IPC: C08L81/06

    CPC classification number: C08F283/00 ,  C08L63/10 ,  C08L81/06 ,  C09J4/06 ,  C08F220/30 ,  C08F226/06 ,  C08L81/00

    Abstract: A method increases the toughness of a material obtained by curing a composition that includes at least one vinyl ester monomer. The method includes the incorporation into the composition of a sulfonated polyaromatic thermoplastic polymer, which is achieved by dissolving the vinyl ester monomer and the thermoplastic polymer in a reactive diluent in which they are both soluble. The resulting curable composition includes at least one vinyl ester monomer, and very high toughness materials can be made from it. A curable composition can include at least one vinyl ester monomer, a sulfonated polyaromatic thermoplastic polymer and a N-vinyl lactam. The compositions can be used in the aeronautical, space, railway, nautical, automotive industries, arms and other industries.

    Abstract translation: 一种方法提高了通过固化包含至少一种乙烯酯单体的组合物获得的材料的韧性。 该方法包括通过将乙烯基酯单体和热塑性聚合物溶解在它们都可溶的反应性稀释剂中而实现的将磺化多芳族热塑性聚合物掺入组合物中。 得到的可固化组合物包括至少一种乙烯基酯单体，并且可以从其制备非常高韧性的材料。 可固化组合物可以包括至少一种乙烯基酯单体，磺化多芳族热塑性聚合物和N-乙烯基内酰胺。 该组合物可用于航空，航天，铁路，航海，汽车工业，武器等行业。

    Increase in the toughness of a material obtained from a curable composition comprising at least one vinyl ester monomer
    3.
    发明授权
    Increase in the toughness of a material obtained from a curable composition comprising at least one vinyl ester monomer 有权
    由包含至少一种乙烯基酯单体的可固化组合物获得的材料的韧性提高

    公开(公告)号：US08618186B2

    公开(公告)日：2013-12-31

    申请号：US13500844

    申请日：2010-10-08

    Applicant: Mickael Krzeminski ,  Brigitte Defoort ,  Xavier Coqueret

    Inventor： Mickael Krzeminski ,  Brigitte Defoort ,  Xavier Coqueret

    IPC: C08F283/00 ,  C08J3/28 ,  C08L63/10 ,  C08L81/06

    CPC classification number: C08F283/00 ,  C08L63/10 ,  C08L81/06 ,  C09J4/06 ,  C08F220/30 ,  C08F226/06 ,  C08L81/00

    Abstract: A method increases the toughness of a material obtained by curing a composition that includes at least one vinyl ester monomer. The method includes the incorporation into the composition of a sulfonated polyaromatic thermoplastic polymer, which is achieved by dissolving the vinyl ester monomer and the thermoplastic polymer in a reactive diluent in which they are both soluble. The resulting curable composition includes at least one vinyl ester monomer, and very high toughness materials can be made from it. A curable composition can include at least one vinyl ester monomer, a sulfonated polyaromatic thermoplastic polymer and a N-vinyl lactam. The compositions can be used in the aeronautical, space, railway, nautical, automotive industries, arms and other industries.

    Abstract translation: 一种方法提高了通过固化包含至少一种乙烯酯单体的组合物获得的材料的韧性。 该方法包括通过将乙烯基酯单体和热塑性聚合物溶解在它们都可溶的反应性稀释剂中而实现的将磺化多芳族热塑性聚合物掺入组合物中。 得到的可固化组合物包括至少一种乙烯基酯单体，并且可以从其制备非常高韧性的材料。 可固化组合物可以包括至少一种乙烯基酯单体，磺化多芳族热塑性聚合物和N-乙烯基内酰胺。 该组合物可用于航空，航天，铁路，航海，汽车工业，武器等行业。

    MULTILAYERED WALL ESPECIALLY CONSISTING OF GOSSAMER-TYPE INFLATABLE STRUCTURES
    4.
    发明申请
    MULTILAYERED WALL ESPECIALLY CONSISTING OF GOSSAMER-TYPE INFLATABLE STRUCTURES 审中-公开
    多层墙壁特别包含GOSSAMER型可充气结构

    公开(公告)号：US20090211188A1

    公开(公告)日：2009-08-27

    申请号：US11574030

    申请日：2005-08-10

    Applicant: Brigitte Defoort ,  Dominique Lacour

    Inventor： Brigitte Defoort ,  Dominique Lacour

    IPC: E04C2/20

    CPC classification number: B32B27/065 ,  B32B5/18 ,  B32B7/12 ,  B32B27/08 ,  B32B27/12 ,  B32B27/281 ,  B32B2260/021 ,  B32B2260/046 ,  B32B2266/025 ,  H01Q1/081

    Abstract: A multilayer wall includes Gossamer-type rigidifiable and inflatable structures, the wall including a layer of a composite material that can be rigidified by polymerisation, and is flanked, on the inside, by a gas-impermeable layer, and, on the outside, by at least one anti-adhesion and protection layer. The multilayer wall is characterised in that the external layer is partially permeable to gas and impermeable to liquid or viscous phases of the matrix of the composite material.

    Abstract translation: 多层壁包括Gossamer型可刚性和可膨胀的结构，该壁包括复合材料层，该复合材料层可通过聚合而被硬化，并且在内侧由不透气层侧面，并且在外侧由 至少一个防粘附和保护层。 多层壁的特征在于，外层对于气体是部分透气的，并且对于复合材料的基质的液体或粘性相是不可渗透的。

    High toughness vinylester and/or epoxy resin-based material, its process of manufacture, composite material comprising it and uses thereof
    5.
    发明授权
    High toughness vinylester and/or epoxy resin-based material, its process of manufacture, composite material comprising it and uses thereof 失效
    高韧性乙烯基酯和/或环氧树脂基材料，其制造方法，包含它的复合材料及其用途

    公开(公告)号：US07556853B2

    公开(公告)日：2009-07-07

    申请号：US12053995

    申请日：2008-03-24

    Applicant: Estelle Chauray ,  Brigitte Defoort ,  Frederic Boursereau ,  Alain Soum

    Inventor： Estelle Chauray ,  Brigitte Defoort ,  Frederic Boursereau ,  Alain Soum

    IPC: B32B27/04

    CPC classification number: C08L55/005 ,  C08L63/10 ,  C08L71/00 ,  Y10T428/24994 ,  Y10T428/31 ,  Y10T428/31511 ,  Y10T428/31938 ,  C08L2666/02

    Abstract: The invention relates to a material with high fracture toughness based on a vinyl ester resin and/or on an epoxide resin and to its process of manufacture.This material comprises at least one polymerized resin chosen from vinyl ester resins and epoxide resins which can be polymerized at a temperature of less than 70° C. and their blends, and a thermoplastic adjuvant present in this resin in the form of particles, and exhibits a fracture toughness (KIc) of greater than or equal to 1.2 MPa·m1/2 as determined according to Standard ISO 13586:2000.It also relates to a composite material comprising a matrix composed of said material and a reinforcement.Applications: automobile, railway, ship-building, aeronautical, aerospatial and other industries.

    Abstract translation: 本发明涉及一种基于乙烯基酯树脂和/或环氧树脂具有高断裂韧性的材料及其制造方法。 该材料包括至少一种选自乙烯基酯树脂和可在低于70℃的温度下聚合的环氧树脂的聚合树脂及其共混物，以及以该颗粒形式存在于该树脂中的热塑性助剂，以及展品 根据标准ISO 13586：2000测定的断裂韧性（KIc）大于或等于1.2MPa.m1 / 2。 它还涉及一种复合材料，其包括由所述材料和增强材料组成的基体。 应用范围：汽车，铁路，造船，航空航天等行业。

    Method For Enhancing Adherence of Carbon Fibers With Respect to an Organic Matrix
    6.
    发明申请
    Method For Enhancing Adherence of Carbon Fibers With Respect to an Organic Matrix 有权
    提高碳纤维对有机矩阵的粘附性的方法

    公开(公告)号：US20080255332A1

    公开(公告)日：2008-10-16

    申请号：US12065983

    申请日：2006-09-15

    Applicant: Brigitte Defoort ,  Philippe Ponsaud ,  Xavier Coqueret

    Inventor： Brigitte Defoort ,  Philippe Ponsaud ,  Xavier Coqueret

    IPC: C08F24/00

    CPC classification number: D01F11/16 ,  C08J5/06 ,  D01F11/14 ,  D06M14/36 ,  D06M2101/40 ,  D06M2200/50

    Abstract: The invention relates to a process for improving the adhesion of carbon fibres with regard to an organic matrix forming a composite material with these fibres, this composite material being obtained by bringing the fibres into contact with a resin which can be cured by chain polymerization and then polymerizing the resin, which process is characterized in that it comprises the grafting, to the surface of the fibres, before they are brought into contact with the resin, of groups capable of acting as chain transfer agents during the polymerization of said resin.Fields of application: aeronautical, aerospatial, railway, ship building and automobile industries but also the armaments industry, the industry of sports and leisure articles, and the like.

    Abstract translation: 本发明涉及一种改善碳纤维与这些纤维形成复合材料的有机基质的粘附性的方法，该复合材料通过使纤维与可通过链聚合固化的树脂接触而获得，然后 使树脂聚合，其特征在于它包括在与所述树脂接触的同时，在所述树脂的聚合期间将能够作为链转移剂的基团接枝到纤维的表面。 应用领域：航空，航空航天，铁路，船舶建筑和汽车工业，还有军工业，体育休闲用品行业等。

    Method for improving mechanical strength of bondings made with an adhesive based on curable resin by chain polymerization
    7.
    发明授权
    Method for improving mechanical strength of bondings made with an adhesive based on curable resin by chain polymerization 失效
    用于通过链式聚合提高用基于可固化树脂的粘合剂制成的粘结机械强度的方法

    公开(公告)号：US08282764B2

    公开(公告)日：2012-10-09

    申请号：US12299044

    申请日：2007-05-10

    Applicant: Brigitte Defoort ,  Philippe Ponsaud ,  Xavier Cocqueret

    Inventor： Brigitte Defoort ,  Philippe Ponsaud ,  Xavier Cocqueret

    IPC: B32B37/12

    CPC classification number: C09J5/02 ,  C09J2463/006

    Abstract: The invention relates to a process that makes it possible to improve the mechanical strength of bonds between substrates when these bonds are produced by means of an adhesive that comprises a resin that can be cured by chain polymerization, and in particular a resin that can be cured under the effect of ionizing or light radiation.This process is characterized in that it comprises the grafting of groups capable of acting as chain transfer agents during the polymerization of said resin to the surface of the substrates, before the latter are brought into contact with the adhesive.Applications: assembling of structural, engine, passenger compartment or bodywork parts in the aeronautical, space, railway, ship-building and automotive industries.

    Abstract translation: 本发明涉及一种方法，其可以通过包含可通过链式聚合固化的树脂的粘合剂生产这些粘合剂，特别是能够固化的树脂，从而提高基材之间的粘结的机械强度 在电离或光辐射的作用下。 该方法的特征在于，在将所述树脂与粘合剂接触之前，其包括在所述树脂聚合成基材表面期间能够作为链转移剂的基团的接枝。 应用：航空，太空，铁路，造船和汽车行业的结构，发动机，客舱或车身部件的组装。

    Rigidification of structures to be deployed by inflating, particularly for use in space
    9.
    发明授权
    Rigidification of structures to be deployed by inflating, particularly for use in space 有权
    通过膨胀，特别是用于空间来部署的结构的刚性

    公开(公告)号：US08025942B2

    公开(公告)日：2011-09-27

    申请号：US11577758

    申请日：2005-10-20

    Applicant: Brigitte Defoort ,  Xavier Coqueret ,  Dominique Lacour

    Inventor： Brigitte Defoort ,  Xavier Coqueret ,  Dominique Lacour

    IPC: B32B27/12 ,  B32B27/14

    CPC classification number: C08G59/68 ,  Y10T428/13 ,  Y10T428/1303 ,  Y10T428/1352 ,  Y10T428/1359 ,  Y10T428/139 ,  Y10T428/31721 ,  Y10T428/31786

    Abstract: The invention relates to the stiffening of inflatably deployable structures, in particular for space use.More specifically, the invention relates to a flexible membrane for inflatably deployable structures, that comprises one layer of a composite and at least one polymer film that is permeable to visible radiation covering one of the faces of this layer, said composite being formed from a fibrous material impregnated with a composition incorporating an epoxide or epoxy/acrylate resin and a photoinitiator, and which is characterized in that the photoinitiator is an iron-arene complex salt of general formula (I): where A is an arene group, while X is a non-nucleophilic anion. Applications: manufacture of devices of the following types: radars, solar panels, reflectors, solar shields, antennas, solar mirrors or sails, intended to equip orbital vehicles or vehicles for space or planetary exploration.

    Abstract translation: 本发明涉及可膨胀展开结构的加强，特别是用于空间使用。 更具体地，本发明涉及一种用于可膨胀展开结构的柔性膜，其包括一层复合材料和至少一层聚合物膜，该聚合物膜可透过该层的一个表面的可见辐射，所述复合材料由纤维状 浸渍有包含环氧化物或环氧/丙烯酸酯树脂和光引发剂的组合物的材料，其特征在于光引发剂是通式（I）的铁 - 芳烃络合盐：其中A是芳族基团，而X是 非亲核阴离子。 应用：制造以下类型的设备：雷达，太阳能电池板，反射器，太阳能屏蔽，天线，太阳能反射镜或帆，旨在配备轨道车辆或车辆进行太空或行星探测。

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