Preform, fiber-reinforced composite material, and method of manufacturing fiber-reinforced composite material

US2018264754A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2018264754-A1
Application numberUS-201615548268-A
CountryUS
Kind codeA1
Filing dateFeb 2, 2016
Priority dateFeb 5, 2015
Publication dateSep 20, 2018
Grant date

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

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A preform includes a plurality of reinforcement fiber layers connected to each other by binder resin, the binder resin containing spacer particles insoluble in the binder resin, the spacer particles accounting for a volume proportion of 10% to 80% in the binder resin present in interlaminar gaps between the reinforcement fiber layers.

First claim

Opening claim text (preview).

1 - 17 . (canceled) 18 . A preform comprising a plurality of reinforcement fiber layers connected to each other by binder resin, the binder resin containing spacer particles insoluble in the binder resin, the spacer particles accounting for a volume proportion of 10% to 80% in the binder resin present in interlaminar gaps between the reinforcement fiber layers. 19 . The preform as set forth in claim 18 , wherein the spacer particles have a sphericity of 75 to 100 and a particle diameter distribution index of 1 to 5. 20 . The preform as set forth in claim 18 , wherein the spacer particles have an average particle diameter of 1 to 50 μm. 21 . The preform as set forth in claim 18 , wherein content of the spacer particles is 2 to 9 g/m 2 in each interlaminar gap between reinforcement fiber layers. 22 . The preform as set forth in claim 18 , wherein the spacer particles are polymer particles having a glass transition temperature of 80° C. or more. 23 . The preform as set forth in claim 18 , wherein the spacer particles are of at least one resin compound selected from the group consisting of polyamide, polyamide-imide, polyimide, polycarbonate, polyphenylene sulfide, polyphenylene ether, polyether ether ketone, and copolymers thereof. 24 . The preform as set forth in claim 18 , wherein the binder resin contains thermosetting resin. 25 . The preform as set forth in claim 24 , wherein the thermosetting resin is epoxy resin. 26 . The preform as set forth in claim 25 , wherein solid epoxy resin is contained as the epoxy resin. 27 . The preform as set forth in claim 25 comprising, as the epoxy resin, at least one epoxy resin compound selected from the group consisting of bisphenol type epoxy resin, novolac type epoxy resin, and aralkyl type epoxy resin. 28 . The preform as set forth in claim 24 , wherein the binder resin contains a thermoplastic resin soluble in the thermosetting resin contained in the binder resin. 29 . The preform as set forth in claim 28 , wherein the thermoplastic resin is at least one selected from the group consisting of polyethersulfone, polysulfone, polyetherimide, polyvinyl acetal, polymethyl methacrylate, and phenoxy resin. 30 . The preform as set forth in claim 28 , wherein the thermoplastic resin has a glass transition temperature of 150° C. or more. 31 . A fiber reinforced composite material produced by impregnating the preform as set forth in claim 18 with matrix resin and curing the matrix resin. 32 . The fiber reinforced composite material as set forth in claim 31 , wherein an interlaminar gap thickness is 1 to 3 times as large as an average particle diameter of the spacer particles. 33 . The fiber reinforced composite material as set forth in claim 31 , wherein an interlaminar gap thickness is 1 to 150 μm. 34 . A method of producing a fiber reinforced composite material comprising injecting matrix resin into the preform as set forth in claim 18 and curing the matrix resin, the binder resin being dissolved in the matrix resin during the step of injecting and curing the matrix resin while the spacer particles are not dissolved in the matrix resin and remain in interlaminar gaps, the thickness of the interlaminar gaps being 1 to 3 times as large as an average particle diameter of the spacer particles.

Assignees

Inventors

Classifications

  • and impregnating by vacuum or injection · CPC title

  • with carbon fibres · CPC title

  • B29C70/025Primary

    with particular filler · CPC title

  • another layer {next to it} also being fibrous or filamentary {(relative arrangement of fibres or filaments of different layers B32B5/12)} · CPC title

  • B32B5/28Primary

    impregnated with or embedded in a plastic substance {(not used)} · CPC title

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What does patent US2018264754A1 cover?
A preform includes a plurality of reinforcement fiber layers connected to each other by binder resin, the binder resin containing spacer particles insoluble in the binder resin, the spacer particles accounting for a volume proportion of 10% to 80% in the binder resin present in interlaminar gaps between the reinforcement fiber layers.
Who is the assignee on this patent?
Toray Industries
What technology area does this patent fall under?
Primary CPC classification B29C70/025. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Thu Sep 20 2018 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).