Extended room temperature storage of epoxy resins

US10119001B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10119001-B2
Application numberUS-201615229067-A
CountryUS
Kind codeB2
Filing dateAug 4, 2016
Priority dateFeb 6, 2014
Publication dateNov 6, 2018
Grant dateNov 6, 2018

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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

Official abstract text for this publication.

Uncured epoxy resin for use in making prepreg for aerospace applications. The resin includes an epoxy resin component comprising difunctional epoxy resin, trifunctional epoxy resin and/or tetrafunctional epoxy resin and a sufficient amount of [3-(4-aminobenzoyl) oxyphenyl]4-aminobenzoate (3-ABOAB), as a curing agent, such that the uncured resin can be stored at room temperature of at least 6 weeks and wherein the uncured resin can be fully cured in no more than 2 hours at a temperature of between 175° C. and 185° C.

First claim

Opening claim text (preview).

What is claimed is: 1. A prepreg which can be stored at room temperature for at least 6 weeks and which can be fully cured in no more than 2 hours at a temperature of between 165° C. and 190° C., said prepreg comprising: a fiber reinforcement; an uncured resin comprising: an epoxy resin component comprising a trifunctional epoxy resin selected from the group consisting of triglycidyl-m-aminophenol and triglycidyl-p-aminophenol; and a curing agent comprising a sufficient amount of [3-(4-aminobenzoyl) oxyphenyl]4-aminobenzoate such that the stoichiometric ratio between said epoxy resin component and said curing agent is between 0.65:1 and 1.1:0.8 and wherein said uncured resin can be stored at room temperature for at least 6 weeks and wherein said prepreg can be fully cured in no more than 2 hours at a temperature of between 165° C. and 190° C. 2. A prepreg according to claim 1 wherein said epoxy resin component additionally comprises diglycidyl ether of bisphenol F. 3. A prepreg according to claim 2 wherein said epoxy resin component additionally comprises N,N,N′,N′-tetraglycidyl-4,4′-diaminodiphenyl methane. 4. A prepreg according to claim 1 wherein the said uncured resin comprises a soluble thermoplastic and insoluble thermoplastic particles. 5. A prepreg according to claim 4 wherein said soluble thermoplastic comprises polyethersulfone. 6. A prepreg according to claim 5 wherein said insoluble thermoplastic particles comprise polyamide particles. 7. A prepreg according to claim 1 wherein said epoxy resin component consists of triglycidyl-m-aminophenol and wherein the stoichiometric ratio between said triglycidyl-m-aminophenol and said curing agent is between 0.7:1 and 0.95:1. 8. A prepreg according to claim 7 wherein the said uncured resin comprises a soluble thermoplastic and insoluble thermoplastic particles. 9. A prepreg according to claim 8 wherein said soluble thermoplastic comprises polyethersulfone. 10. A prepreg according to claim 9 wherein said insoluble thermoplastic particles comprise polyamide particles. 11. A prepreg according to claim 2 wherein the said uncured resin comprises a soluble thermoplastic and insoluble thermoplastic particles. 12. A prepreg according to claim 11 wherein said soluble thermoplastic comprises polyethersulfone. 13. A prepreg according to claim 12 wherein said insoluble thermoplastic particles comprise polyamide particles. 14. A prepreg according to claim 3 wherein the said uncured resin comprises a soluble thermoplastic and insoluble thermoplastic particles. 15. A prepreg according to claim 14 wherein said soluble thermoplastic comprises polyethersulfone. 16. A prepreg according to claim 15 wherein said insoluble thermoplastic particles comprise polyamide particles. 17. A composite material comprising a prepreg according to claim 1 which has been cured. 18. A composite material according to claim 17 wherein said composite material forms at least part of a primary structure of an aircraft. 19. A method for making a prepreg which can be stored at room temperature for at least 6 weeks and which can be fully cured in no more than 2 hours at a temperature of between 165° C. and 190° C., said method comprising the steps of: providing an uncured resin which can be stored at room temperature for at least 6 weeks and which can be fully cured in no more than 2 hours at a temperature of between 165° C. and 190° C., said uncured resin comprising: an epoxy resin component comprising a bifunctional epoxy resin selected from the group consisting of triglycidyl-m-aminophenol and triglycidyl-p-aminophenol; a curing agent comprising a sufficient amount of [3-(4-aminobenzoyl) oxyphenyl]4-aminobenzoate such that the stoichiometric ratio between said epoxy resin component and said curing agent is between 0.65:1 and 1.1:0.8 and wherein said uncured resin can be stored at room temperature for at least 6 weeks and wherein said uncured resin can be fully cured in no more than 2 hours at a temperature of between 165° C. and 190° C.; and combining said uncured resin with a fibrous reinforcement to provide said prepreg. 20. A method for storing an uncured resin at room temperature for up to six weeks or more, said method comprising the steps of: A) providing an uncured resin which can be stored at room temperature for at least 6 weeks and which can be fully cured in no more than 2 hours at a temperature of between 165° C. and 190° C., said uncured resin comprising: a) an epoxy resin component comprising a bifunctional epoxy selected from the group consisting of triglycidyl-m-aminophenol and triglycidyl-p-aminophenol; b) a curing agent comprising a sufficient a count of [3-(4-aminobenzoyl) oxyphenyl]4-aminobenzoate such that the stoichiometric ratio between said epoxy resin component and said curing agent is between 0.651 and 1.1:0.8 and wherein said uncured resin can be stored at room temperature of at least 6 weeks and wherein said uncured resin can be fully cured in no more than 2 hours at a temperature of between 165° C. and 190° C.; and B) storing said uncured resin for up to 6 weeks or more at room temperature.

Assignees

Inventors

Classifications

  • Polyamides derived from omega-amino carboxylic acids or from lactams thereof (C08L77/10 takes precedence) · CPC title

  • Polysulfones; Polyethersulfones · CPC title

  • Compositions of epoxy resins; Compositions of derivatives of epoxy resins · CPC title

  • Characterised by the use of polyamides obtained by reactions forming a carboxylic amide link in the main chain; Derivatives of such polymers · CPC title

  • Epoxy compounds containing three or more epoxy groups · CPC title

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What does patent US10119001B2 cover?
Uncured epoxy resin for use in making prepreg for aerospace applications. The resin includes an epoxy resin component comprising difunctional epoxy resin, trifunctional epoxy resin and/or tetrafunctional epoxy resin and a sufficient amount of [3-(4-aminobenzoyl) oxyphenyl]4-aminobenzoate (3-ABOAB), as a curing agent, such that the uncured resin can be stored at room temperature of at least 6 we…
Who is the assignee on this patent?
Hexcel Corp, Hexcel Composites Ltd
What technology area does this patent fall under?
Primary CPC classification C08G59/5033. Mapped technology areas include Chemistry & Metallurgy.
When was this patent published?
Publication date Tue Nov 06 2018 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). 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).