Prepreg with variable cure rate resin composition

US2018290339A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2018290339-A1
Application numberUS-201615762175-A
CountryUS
Kind codeA1
Filing dateSep 27, 2016
Priority dateSep 28, 2015
Publication dateOct 11, 2018
Grant date

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  1. Title

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  2. Abstract

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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

Official abstract text for this publication.

A prepreg comprising a layer of impregnated reinforcing fibers comprising at least one layer of reinforcing fibers impregnated by a resin composition comprising at least a thermosetting resin, a curing agent and an accelerator, such that the accelerator has a gradient concentration which is more concentrated in the resin composition in the vicinity of the reinforcing fibers than further away. The resin composition comprising a first resin composition impregnates the reinforcing fibers to provide a layer of impregnated reinforcing fibers and a surface layer comprising a second resin composition is formed on the layer of impregnated reinforcing fibers, wherein the first resin composition has at least one peak exotherm occurring at a time earlier than and/or at a temperature lower than any peak exotherm of the second resin composition. The heat generation from the first resin composition is tailored to initiate or speed up the curing of the second resin composition, leading to a substantial reduction of cure cycle time of the prepreg. Excellent handling and processing abilities of the uncured prepreg and excellent physical, thermal and mechanical properties when cured are achieved.

First claim

Opening claim text (preview).

What is claimed is: 1 . A prepreg comprising a layer of impregnated reinforcing fibers comprising at least one layer of reinforcing fibers impregnated by a resin composition comprising at least a thermosetting resin, a curing agent and an accelerator, such that the accelerator has a gradient concentration which is more concentrated in the resin composition in the vicinity of the reinforcing fibers than further away. 2 . The prepreg of claim 1 , wherein the resin composition comprises a first resin composition impregnating the reinforcing fibers and a surface layer comprising a second resin composition formed on the layer of impregnated reinforcing fibers, wherein the first resin composition has at least one peak exotherm occurring at a time earlier than and/or at a temperature lower than any peak exotherm of the second resin composition and the first resin composition generates an amount of heat during exotherm that is at least equal to the amount of heat generated by the second resin composition during exotherm, such that the generated heat from the first resin composition is configured to initiate or speed up reaction of the second resin composition, allowing the prepreg to be cured at a cure temperature in a reduced dwell time for a given desired degree of cure. 3 . The prepreg of claim 2 , wherein the first resin composition comprises the thermosetting resin, the curing agent and the accelerator. 4 . The prepreg of claim 3 , wherein the first resin composition further comprises a thermoplastic resin, a filler or a combination thereof. 5 . The prepreg of claim 3 , wherein the second resin composition comprises at least a thermosetting resin and a curing agent and wherein the thermosetting resin of the second resin composition is the same as or different from the thermosetting resin of the first resin composition and the curing agent of the second resin composition is the same as or different from the curing agent of the first resin composition. 6 . The prepreg of claim 5 further comprising an interlayer toughener, wherein the interlayer toughener is localized on a surface of impregnated reinforcing fibers to which the surface layer is applied. 7 . The prepreg of claim 6 , wherein the second resin composition further comprises a thermoplastic resin, a filler, or a combination thereof. 8 . The prepreg of claim 6 , wherein the second resin composition further comprises an accelerator that is the same as or different from the accelerator present in the first resin composition 9 . The prepreg of claim 3 , wherein the second resin composition comprises at least a thermoplastic resin or at least a thermosetting resin and no curing agent, or a combination. 10 . The prepreg of claim 2 , wherein the first resin composition comprises the thermosetting resin and the curing agent and no accelerator, and the second resin composition comprises at least a thermosetting resin, the accelerator and no curing agent, wherein the thermosetting resin of the second resin composition is the same as or different from the thermosetting resin of the first resin composition, wherein the accelerator, the curing agent, or both diffuse into the other resin composition when the prepreg is heated and accelerate curing of the prepreg. 11 . The prepreg of claim 6 , further comprising a breather layer comprising a high-aspect-ratio material, wherein the high-aspect ratio material is localized on the surface of the layer of reinforcing fibers and wherein the breather layer is configured to provide a network of air channels in the prepreg through which trapped air pockets and volatiles in the prepreg diffuse under vacuum during curing of the prepreg. 12 . The prepreg of claim 11 , wherein the breather layer is configured to allow at least a portion of the high-aspect ratio material to infiltrate the layer of reinforcing fibers. 13 . The prepreg of claim 1 , wherein the prepreg when isothermally cured at 177° C. (350° F.) for at most 60 minutes achieves a degree of cure of at least 93% and a glass transition temperature of at least 175° C. 14 . The prepreg of claim 13 , wherein the prepreg when isothermally cured at 177° C. (350° F.) for at most 60 minutes achieves a degree of cure is at least 93% and the glass transition temperature is at least 190° C. 15 . The prepreg of claim 14 , wherein the prepreg when isothermally cured at 177° C. (350° F.) for at most 30 minutes achieves a degree of cure of at least 90% and the glass transition temperature is at least 190° C. 16 . A prepreg comprising a layer of impregnated reinforcing fibers comprising at least one layer of reinforcing fibers impregnated by a resin composition comprising at least an epoxy resin, a diaminodiphenylsulfone, a dihydrazide, and an interlayer toughener, wherein the dihydrazide is tailored to have a gradient concentration which is more concentrated in the resin composition in the vicinity of the reinforcing fibers than further away, wherein the interlayer toughener is localized on the surface of the layer of the reinforcing fibers, and wherein the prepreg when cured at 177° C. (350° F.) for at most 60 minutes achieves a degree of cure of at least 93% and a glass transition temperature of at least 175° C. 17 . A manufacturing method for the prepreg of claim 1 comprising (1) impregnating a first resin composition onto one side or both sides of a plurality of reinforcing fibers to form an impregnated plurality of reinforcing fibers, (2) applying a second resin composition onto one side or both sides of the impregnated plurality of reinforcing fibers, wherein the first resin composition comprises at least a thermosetting resin, a curing agent and an accelerator and the second resin composition comprises at least a thermosetting resin and a curing agent, wherein the thermosetting resin present in the second resin composition is the same as or different from the thermosetting resin present in the first resin composition and the curing agent present in the second resin composition is the same as or different from the curing agent present in the first resin composition. 18 . A manufacturing method for the prepreg of claim 6 comprising (1) impregnating the first resin composition onto one side or both sides of a plurality of reinforcing fibers to form an impregnated plurality of reinforcing fibers, (2) applying the second resin composition onto one side or both sides of the impregnated plurality of reinforcing fibers. 19 . A manufacturing method for the prepreg of claim 9 comprising (1) impregnating the first resin composition onto one side or both sides of a plurality of reinforcing fibers to form an impregnated plurality of reinforcing fibers, (2) applying the second resin composition onto one side or both sides of the impregnated plurality of reinforcing fibers. 20 . A manufacturing method for the prepreg of claim 10 comprising (1) impregnating the first resin composition onto one side or both sides of a plurality of reinforcing fibers to form an impregnated plurality of reinforcing fibers, (2) applying the second resin composition onto one side or both sides of the impregnated plurality of reinforcing fibers. 21 . A method of manufacturing a composite article comprising curing the prepreg of claim 1 . 22 . A method of manufacturing a composite article comprising curing the prepreg of claim 6 . 23 . A method of manufacturing a composite article comprising curing the prepreg of claim 9 .

Assignees

Inventors

Classifications

  • B29B11/16Primary

    comprising fillers or reinforcement {(non-woven fabrics per se D04H1/00, D04H3/00)} · CPC title

  • Characterised by the use of epoxy resins; Derivatives of epoxy resins · CPC title

  • Use of {EP, i.e.} epoxy resins {or derivatives thereof}, as moulding material · CPC title

  • Polycondensates having nitrogen-containing heterocyclic rings in the main chain; Polyhydrazides; Polyamide acids or similar polyimide precursors · CPC title

  • Characterised by the use of polyethers obtained by reactions forming an ether link in the main chain; Derivatives of such polymers · CPC title

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What does patent US2018290339A1 cover?
A prepreg comprising a layer of impregnated reinforcing fibers comprising at least one layer of reinforcing fibers impregnated by a resin composition comprising at least a thermosetting resin, a curing agent and an accelerator, such that the accelerator has a gradient concentration which is more concentrated in the resin composition in the vicinity of the reinforcing fibers than further away. T…
Who is the assignee on this patent?
Toray Industries
What technology area does this patent fall under?
Primary CPC classification B29B11/16. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Thu Oct 11 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).