Epoxy resin composition, prepreg, and carbon fiber-reinforced composite material

    公开(公告)号:US11034810B2

    公开(公告)日:2021-06-15

    申请号:US16491050

    申请日:2018-03-05

    IPC分类号: C08J5/24 C08L63/00

    摘要: An object of the present invention is to provide an epoxy resin composition capable of providing a carbon fiber-reinforced composite material that is excellent in moldability, heat resistance, and mechanical properties such as tensile strength and compression strength, and a prepreg. The present invention provides an epoxy resin composition containing at least components [A] to [D] shown below: [A]: an epoxy resin having a xylene group; [B]: a glycidyl amine epoxy resin having three or more glycidyl groups in a molecule; [C]: a thermoplastic resin; and [D]: an aromatic polyamine, the epoxy resin composition containing 10 to 80 parts by mass of the component [A] and 20 to 90 parts by mass of the component [B] based on 100 parts by mass in total of epoxy resins, and also 1 to 25 parts by mass of the component [C] based on 100 parts by mass in total of epoxy resins.

    PREPREG AND FIBER REINFORCED COMPOSITE MATERIAL

    公开(公告)号:US20170226299A1

    公开(公告)日:2017-08-10

    申请号:US15128583

    申请日:2015-03-19

    发明人: Atsuhito Arai

    摘要: A prepreg containing at least the following components [A]-[F], wherein the ratio Ne/Nd of the number of structures Ne of component [F] present in a range of outside 110% of the particle diameter of component [E] and the number of structures Nd of component [F] present in a range outside 110% of the particle diameter of component [D] is 0.25 or higher. [A]: Carbon fibers, [B] thermosetting resin, [C]: curing agent, [D]: particles composed mainly of thermoplastic resin having a primary particle number-average particle size of 5-50 μm, [E]: conductive particles different from component [D] and having a primary particle number-average particle size in the range of a specific expression, [F]: filler comprising a carbon material.

    PREPREG
    8.
    发明申请
    PREPREG 有权

    公开(公告)号:US20230048074A1

    公开(公告)日:2023-02-16

    申请号:US17788402

    申请日:2020-12-10

    IPC分类号: C08J5/24 C08L63/00

    摘要: The present invention addresses the problem of providing a prepreg that yields a carbon fiber composite material that has exceptional tensile strength, heat resistance, and impact resistance and is suitable as a structural material of an aircraft body, wherein the resin composition used in the prepreg furthermore has exceptional viscosity stability, the prepreg containing a resin composition that contains carbon fibers and at least the constituent elements [A]—[D] as defined.

    Prepreg and carbon fiber reinforced material

    公开(公告)号:US11208541B2

    公开(公告)日:2021-12-28

    申请号:US16633904

    申请日:2018-05-28

    摘要: A prepreg, which includes a carbon fiber reinforced material, has excellent Mode I interlaminar toughness, Mode II interlaminar toughness, and tensile strength. The prepreg includes the following constituents [A] to [C] and satisfies the following conditions (I) and (II): [A]: a carbon fiber; [B]: an epoxy resin; and [C]: a hardener for [B], and (I) a surface oxygen concentration O/C of [A] measured by X-ray photoelectron spectroscopy is 0.10 or more; and (II) a cured product obtained by curing [B] and [C] includes a resin region having molecular anisotropy exhibiting interference fringes in polarizing microscope observation in a crossed Nicol state.