Systems and methods for manufacturing large contoured parts from thermoplastic laminate sheets
US-12172396-B2 · Dec 24, 2024 · US
US2020079917A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2020079917-A1 |
| Application number | US-201816611344-A |
| Country | US |
| Kind code | A1 |
| Filing date | Apr 5, 2018 |
| Priority date | May 10, 2017 |
| Publication date | Mar 12, 2020 |
| Grant date | — |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
Provided is a method for producing a fiber-reinforced composite material exhibiting high heat resistance and excellent appearance quality. It is a method for producing a fiber-reinforced composite material, which includes disposing a prepreg containing a reinforced fiber being impregnated with an epoxy resin composition in a mold, pressurizing and heating the prepreg at 0.2 to 2.5 MPa and 130° C. to 200° C. as primary curing, and then further heating the prepreg at 210° C. to 270° C. for 10 minutes or more as secondary curing.
Opening claim text (preview).
1 . A method for producing a fiber-reinforced composite material, the method comprising: disposing a prepreg containing a reinforced fiber being impregnated with an epoxy resin composition in a mold; pressurizing and heating the prepreg at 0.2 to 2.5 MPa and 130° C. to 200° C. as primary curing; and then further heating the prepreg at 210° C. to 270° C. for 10 minutes or more as secondary curing. 2 . The method for producing a fiber-reinforced composite material according to claim 1 , wherein an internal pressure applying member with a tube or bag-shape is disposed inside the prepreg, and a high pressure gas is introduced into the internal pressure applying member to apply pressure to the prepreg during the primary curing. 3 . The method for producing a fiber-reinforced composite material according to claim 1 or 2 , wherein the epoxy resin composition satisfies condition (1) below: (1) a glass transition temperature of a cured product obtained by subjecting the epoxy resin composition to curing at 180° C. for 30 minutes and then to curing at 240° C. for 30 minutes is 220° C. or more. 4 . The method for producing a fiber-reinforced composite material according to any one of claims 1 to 3 , wherein the epoxy resin composition satisfies condition (2) below: (2) a resin viscosity (η40) at 40° C. and a minimum viscosity (ηmin) satisfy a relational expression of: 2.5<Log(η40)−Log(ηmin)≤3.5. 5 . The method for producing a fiber-reinforced composite material according to any one of claims 1 to 4 , wherein the epoxy resin composition satisfies condition (3) below: (3) a minimum viscosity when a viscosity is measured at a temperature raising rate of 1.5° C./min is in a range of 90° C. to 120° C. and a value of the minimum viscosity is 4.0 Pa·s or less. 6 . The method for producing a fiber-reinforced composite material according to any one of claims 1 to 5 , wherein the epoxy resin composition is an epoxy resin composition containing constituents [A] to [C] below: [A] a tri- or higher functional epoxy resin having an aromatic ring [B] an aromatic amine curing agent [C] a curing accelerator 7 . The method for producing a fiber-reinforced composite material according to claim 6 , wherein the constituent [A] is contained in an amount of 80 parts by mass or more in 100 parts by mass of all epoxy resins in the epoxy resin composition. 8 . The method for producing a fiber-reinforced composite material according to claim 6 or 7 , wherein the constituent [A] includes at least one selected from the group consisting of tetraglycidyldiaminodiphenylmethane, a novolac epoxy resin, and an epoxy resin represented by Formula (i) below: 9 . The method for producing a fiber-reinforced composite material according to any one of claims 6 to 8 , wherein a number of active hydrogen groups in the constituent [B] with respect to a number of epoxy groups in all epoxy resins in the epoxy resin composition is 0.2 to 0.6. 10 . The method for producing a fiber-reinforced composite material according to any one of claims 6 to 9 , wherein the constituent [B] includes at least one selected from the group consisting of 4,4′-diaminodiphenyl sulfone and 3,3′-diaminodiphenyl sulfone. 11 . The method for producing a fiber-reinforced composite material according to any one of claims 1 to 10 , wherein the reinforced fiber is a carbon fiber.
using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding · CPC title
unidirectional · CPC title
Carbon · CPC title
Characterised by the use of epoxy resins; Derivatives of epoxy resins · CPC title
Elements · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.