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    Composite materials
    2.
    发明授权
    Composite materials 有权
    复合材料

    公开(公告)号：US09181407B2

    公开(公告)日：2015-11-10

    申请号：US13703047

    申请日：2011-06-14

    Applicant: Steve Mortimer

    Inventor： Steve Mortimer

    IPC: C08J3/24 ,  C08J5/24

    CPC classification number: C08J3/24 ,  C08J5/24

    Abstract: A process for the manufacture of a cured composite material, the process comprising the steps of blending together a liquid curable resin and a curing agent having a melting point greater than 100° C. to form a liquid blend of curable resin and curing agent, at least partially impregnating a structural fiber arrangement with the blended curable resin and curing agent to form a curable composite material, followed by curing the composite material by exposure to elevated temperature and at a pressure of no greater than 3 bar absolute to form a cured composite material.

    Abstract translation: 一种固化复合材料的制造方法，该方法包括以下步骤：将液体可固化树脂和熔点大于100℃的固化剂混合在一起，以形成可固化树脂和固化剂的液体共混物，在 用混合的可固化树脂和固化剂至少部分地浸渍结构纤维布置以形成可固化的复合材料，然后通过暴露于升高的温度和不大于3巴的绝对压力固化复合材料，以形成固化的复合材料 。

    MOULDING PROCESSES
    4.
    发明申请
    MOULDING PROCESSES 审中-公开
    成型工艺

    公开(公告)号：US20110049426A1

    公开(公告)日：2011-03-03

    申请号：US12991040

    申请日：2009-05-14

    Applicant: Neal Patel ,  Steve Mortimer

    Inventor： Neal Patel ,  Steve Mortimer

    IPC: C08L63/00 ,  B29C45/14 ,  C08G59/14 ,  C09K19/52

    CPC classification number: C08G59/245 ,  B29C70/443 ,  B29C70/48 ,  C08J5/24 ,  C08J2363/00 ,  C08L63/00

    Abstract: Use of a resin system for making a composite material in a liquid moulding process. The resin system comprises an epoxy component and at least one curing agent, and at least 35 wt. % of the epoxy component is one or more naphthalene based epoxy resin. There is also provided a cured composite material, and a method of making the cured composite material in a liquid moulding process which comprises placing fibre reinforcement and the resin system in a mould and curing. The resin system and the methods of making a cured composite material are particularly applicable to liquid moulding processed such as resin trans moulding (RTM), vacuum assisted resin transfer moulding (VARTM), Seeman composite resin infusion moulding (SCRIMP), resin infusion under flexible tooling (RIFT), and liquid resin infusion (LRI).

    Abstract translation: 在液体成型工艺中使用用于制备复合材料的树脂体系。 树脂体系包含环氧组分和至少一种固化剂，并且至少35wt。 ％的环氧组分是一种或多种萘基环氧树脂。 还提供了固化的复合材料，以及使固化的复合材料成为液态成型工艺的方法，该方法包括将纤维增强物和树脂体系放置在模具中并固化。 树脂体系和固化复合材料的制备方法特别适用于树脂反式成型（RTM），真空辅助树脂传递模塑（VARTM），塞曼复合树脂浸渍成型（SCRIMP），柔性树脂注入 加工（RIFT）和液体树脂输液（LRI）。

    COMPOSITE MATERIALS
    7.
    发明申请
    COMPOSITE MATERIALS 有权
    复合材料

    公开(公告)号：US20130090414A1

    公开(公告)日：2013-04-11

    申请号：US13703047

    申请日：2011-06-14

    Applicant: Steve Mortimer

    Inventor： Steve Mortimer

    IPC: C08J3/24

    CPC classification number: C08J3/24 ,  C08J5/24

    Abstract: A process for the manufacture of a cured composite material, the process comprising the steps of blending together a liquid curable resin and a curing agent having a melting point greater than 100° C. to form a liquid blend of curable resin and curing agent, at least partially impregnating a structural fibre arrangement with the blended curable resin and curing agent to form a curable composite material, followed by curing the composite material by exposure to elevated temperature and at a pressure of no greater than 3 bar absolute to form a cured composite material.

    Abstract translation: 一种固化复合材料的制造方法，该方法包括以下步骤：将液体可固化树脂和熔点大于100℃的固化剂混合在一起，以形成可固化树脂和固化剂的液体共混物，在 用混合的可固化树脂和固化剂至少部分地浸渍结构纤维布置以形成可固化的复合材料，然后通过暴露于升高的温度和不大于3巴的绝对压力固化复合材料，以形成固化的复合材料 。

    Manufacture of void-free laminates and use thereof
    10.
    发明授权
    Manufacture of void-free laminates and use thereof 有权
    无空隙层压板的制造及其用途

    公开(公告)号：US06391436B1

    公开(公告)日：2002-05-21

    申请号：US09315064

    申请日：1999-05-20

    Applicant: Guo Feng Xu ,  Linas Repecka ,  Steve Mortimer ,  Steve Peake ,  Jack Boyd

    Inventor： Guo Feng Xu ,  Linas Repecka ,  Steve Mortimer ,  Steve Peake ,  Jack Boyd

    IPC: B32B2704

    CPC classification number: B32B5/26 ,  B29C70/44 ,  B29C70/546 ,  B32B27/04 ,  C08G59/32 ,  C08G59/3218 ,  C08G59/38 ,  C08J5/24 ,  C08J2363/00 ,  C08L63/00 ,  Y10T428/249928 ,  Y10T428/249933 ,  Y10T428/24994 ,  Y10T428/249942 ,  Y10T428/249944 ,  Y10T428/249945 ,  Y10T428/249947

    Abstract: The invention provides a method of forming a void-free laminate, comprising the steps of: (a) enclosing a partially impregnated prepreg in a vacuum envelope, said partially impregnated prepreg comprising a fiber layer partially impregnated with a resin composition; and (b) heating said partially impregnated prepreg under vacuum to withdraw air present in said partially impregnated prepreg and to cause said resin composition (i) to fully infuse into said fiber layer and (ii) to cure thereby forming said void-free laminate. The present invention further provides novel combinations of modified epoxy resins that may be employed with the methods disclosed. The void-free laminates may be utilized for the manufacture of parts for the aerospace and aircraft industries.

    Abstract translation: 本发明提供了一种形成无空隙层压体的方法，包括以下步骤：（a）将部分浸渍的预浸渍料封装在真空外壳中，所述部分浸渍的预浸料坯包含部分浸渍有树脂组合物的纤维层; 和（b）在真空下加热所述部分浸渍的预浸料坯以抽出存在于所述部分浸渍的预浸料坯中的空气，并使所述树脂组合物（i）完全注入所述纤维层，和（ii）固化，从而形成所述无空隙层压板。 本发明还提供可与所公开方法一起使用的改性环氧树脂的新颖组合。 无空隙层压板可用于制造航空航天和航空工业的部件。

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