JPWO2019203893A5 - - Google Patents

Download PDF

Info

Publication number
JPWO2019203893A5
JPWO2019203893A5 JP2020524608A JP2020524608A JPWO2019203893A5 JP WO2019203893 A5 JPWO2019203893 A5 JP WO2019203893A5 JP 2020524608 A JP2020524608 A JP 2020524608A JP 2020524608 A JP2020524608 A JP 2020524608A JP WO2019203893 A5 JPWO2019203893 A5 JP WO2019203893A5
Authority
JP
Japan
Prior art keywords
thermoset
particles
forming
resin
prepreg
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP2020524608A
Other languages
Japanese (ja)
Other versions
JP2021502272A (en
Publication date
Application filed filed Critical
Priority claimed from PCT/US2018/059640 external-priority patent/WO2019203893A2/en
Publication of JP2021502272A publication Critical patent/JP2021502272A/en
Publication of JPWO2019203893A5 publication Critical patent/JPWO2019203893A5/ja
Pending legal-status Critical Current

Links

Description

「活性のある」(化学活性)熱硬化粒子と周囲の樹脂マトリックスの間のCTEの不適合が殆ど又は全く起こらず、その結果として、硬化した複合積層体は、剥離及び微小亀裂に対する改善された耐性を示すことが分かった。本明細書に開示される「活性のある」熱硬化粒子の使用は、周囲のマトリックス樹脂とは異なる化学的性質を有する熱可塑性又は架橋した熱可塑性強化粒子を層間強化粒子として使用する航空宇宙産業で使用される従来の方法からの逸脱である
Little or no CTE mismatch between the "active" (chemically active) thermoset particles and the surrounding resin matrix occurs, resulting in cured composite laminates with improved resistance to delamination and microcracking was found to show The use of "active" thermoset particles disclosed herein is an aerospace application that uses thermoplastic or crosslinked thermoplastic reinforcing particles that have different chemistries than the surrounding matrix resin as interlaminar reinforcing particles. It is a departure from conventional methods used in industry .

Claims (4)

繊維強化ポリマー複合構造体であって、
硬化性マトリックス樹脂を含浸させた又は注入した2枚以上の層の強化繊維であって、1種又は複数の熱硬化樹脂及び少なくとも1種の硬化剤を含む強化繊維;
強化繊維の隣接層間の層間領域に位置決めされた化学活性熱硬化粒子
を含み、
化学活性熱硬化粒子が、1種又は複数のエポキシ樹脂と、硬化剤として少なくとも1種のアミン化合物とを含む熱硬化性樹脂組成物から誘導され、エポキシ基のアミン基に対するモル比が、100%の全てのエポキシ基と反応するのに必要なアミンの量に不足であるか又は過剰であるような比であり、
それぞれの化学活性熱硬化粒子が、架橋ポリエポキシド及び共有結合を形成できる非架橋エポキシ官能基又は未反応のアミン基のいずれかを含む、繊維強化ポリマー複合構造体。
A fiber reinforced polymer composite structure comprising:
Two or more layers of reinforcing fibers impregnated or infused with a curable matrix resin, the reinforcing fibers comprising one or more thermosetting resins and at least one curing agent;
chemically active thermosetting particles positioned in the interlaminar regions between adjacent layers of reinforcing fibers;
The chemically active thermoset particles are derived from a thermoset resin composition comprising one or more epoxy resins and at least one amine compound as a curing agent, wherein the molar ratio of epoxy groups to amine groups is 100%. a ratio such that there is either an deficiency or excess of the amount of amine required to react with all the epoxy groups of
A fiber reinforced polymer composite structure wherein each chemically active thermoset particle contains either uncrosslinked epoxy functional groups or unreacted amine groups capable of forming covalent bonds with a crosslinked polyepoxide.
繊維強化ポリマー複合構造体を製造する方法であって、
(a)粒子の表面に化学活性官能基を有する熱硬化粒子を形成するステップ;
(b)複数のプリプレグプライを形成するステップであって、それぞれのプリプレグプライが硬化性マトリックス樹脂を含浸させた又は注入した強化繊維を含むステップ;
(c)それぞれのプリプレグプライの少なくとも1つの表面に熱硬化粒子を析出させるステップ;
(d)隣接するプリプレグプライ間に位置決めされた粒子が存在し、それによりプリプレグレイアップを形成するような積層配置でその上に、粒子を有するプリプレグプライをレイアップするステップ;
(e)プリプレグレイアップを圧密化するステップ;及び
(f)プリプレグレイアップを硬化するステップ;
を備え、
(a)における熱硬化粒子が、1種又は複数の熱硬化樹脂と少なくとも1種の硬化剤を含む熱硬化性樹脂組成物を形成し、熱硬化樹脂の硬化剤に対するモル比が、100%の全てのエポキシ樹脂と反応するのに必要なアミンの量に不足であるか又は過剰であるような比であり、熱硬化性樹脂組成物を硬化して化学的に反応性のある官能基を有する架橋樹脂を形成して、架橋樹脂を粉砕することにより形成され
(f)での硬化中に、熱硬化粒子の化学活性官能基は、粒子を取り囲むマトリックス樹脂と共有結合を形成する
方法。
A method of manufacturing a fiber reinforced polymer composite structure comprising:
(a) forming thermoset particles having chemically active functional groups on the surface of the particles;
(b) forming a plurality of prepreg plies, each prepreg ply comprising reinforcing fibers impregnated or infused with a curable matrix resin;
(c) depositing thermoset particles on at least one surface of each prepreg ply;
(d) laying up prepreg plies having particles thereon in a stacked arrangement such that there are particles positioned between adjacent prepreg plies thereby forming a prepreg layup;
(e) consolidating the prepreg layup; and (f) curing the prepreg layup;
with
The thermoset particles in (a) form a thermoset composition comprising one or more thermoset resins and at least one curing agent, wherein the molar ratio of thermoset resin to curing agent is 100%. A ratio that is inadequate or in excess of the amount of amine required to react with all of the epoxy resins and has functional groups that are chemically reactive to cure the thermosetting resin composition. Formed by forming a crosslinked resin and pulverizing the crosslinked resin ,
During curing in (f), the chemically active functional groups of the thermoset particles form covalent bonds with the matrix resin surrounding the particles.
繊維強化ポリマー複合構造体を製造する方法であって、
(a)粒子の表面に化学活性官能基を有する熱硬化粒子を形成するステップ;
(b)1種又は複数の熱硬化樹脂、少なくとも1種の硬化剤、及び熱硬化粒子を含む硬化性マトリックス樹脂組成物を形成するステップ;
(c)複数層の強化繊維に硬化性樹脂組成物を含浸させてプリプレグプライを形成し、それぞれのプリプレグプライが、硬化性マトリックス樹脂組成物を含浸させた又は注入した強化繊維を含み、熱硬化粒子が強化繊維層の外面に残存しているステップ;
(d)粒子を有するプリプレグプライを積層配置でその上にレイアップして、それによりプリプレグレイアップを形成するステップ;
(e)プリプレグレイアップを圧密化するステップ;及び
(f)プリプレグレイアップを硬化するステップ;
を備え、
(a)における熱硬化粒子が、1種又は複数の熱硬化樹脂と少なくとも1種の硬化剤を含む熱硬化性樹脂組成物を形成し、熱硬化樹脂の硬化剤に対するモル比が、100%の全てのエポキシ樹脂基と反応するのに必要なアミンの量に不足であるか又は過剰であるような比であり、熱硬化性樹脂組成物を硬化して化学的に反応性のある官能基を有する硬化樹脂を形成して、硬化樹脂を粉砕することにより形成され
(f)での硬化中に、熱硬化粒子の化学活性官能基は、粒子を取り囲むマトリックス樹脂と共有結合を形成する
方法。
A method of manufacturing a fiber reinforced polymer composite structure comprising:
(a) forming thermoset particles having chemically active functional groups on the surface of the particles;
(b) forming a curable matrix resin composition comprising one or more thermoset resins, at least one curing agent, and thermoset particles;
(c) impregnating multiple layers of reinforcing fibers with a curable resin composition to form prepreg plies, each prepreg ply comprising reinforcing fibers impregnated or infused with a curable matrix resin composition; the particles remaining on the outer surface of the reinforcing fiber layer;
(d) laying up prepreg plies having particles thereon in a stacked arrangement, thereby forming a prepreg layup;
(e) consolidating the prepreg layup; and (f) curing the prepreg layup;
with
The thermoset particles in (a) form a thermoset composition comprising one or more thermoset resins and at least one curing agent, wherein the molar ratio of thermoset resin to curing agent is 100%. A ratio such that the amount of amine is inadequate or in excess of the amount of amine required to react with all of the epoxy resin groups to cure the thermosetting resin composition to remove chemically reactive functional groups. Formed by forming a cured resin having and pulverizing the cured resin ,
During curing in (f), the chemically active functional groups of the thermoset particles form covalent bonds with the matrix resin surrounding the particles.
繊維強化ポリマー複合構造体を製造する方法であって、
(a)粒子の表面に化学活性官能基を有する熱硬化粒子を形成するステップ;
(b)前記熱硬化粒子を含まない第一硬化性樹脂組成物から樹脂フィルムを形成するステップ;
(c)1種又は複数の熱硬化樹脂、少なくとも1種の硬化剤、及び前記熱硬化粒子を含む第二硬化性樹脂組成物から樹脂フィルムを形成するステップ;
(d)熱及び圧力を用いて、第一硬化性樹脂組成物から形成した少なくとも1種の樹脂フィルムを1層の強化繊維に含浸させ、それにより1層の樹脂含浸強化繊維を形成するステップ;
(e)第二硬化性樹脂組成物から形成した少なくとも1種の樹脂フィルムを樹脂含浸強化繊維の層の一表面に接触させて、それにより粒子含有のプリプレグプライを形成するステップ;
(f)ステップ(d)及び(e)に従って追加の粒子含有プリプレグプライを形成するステップ;
(g)プリプレグプライを積層配置でレイアップして、それによりプリプレグレイアップを形成するステップ;
(h)プリプレグレイアップを圧密化するステップ;及び
(i)プリプレグレイアップを硬化するステップ;
を備え、
(a)における熱硬化粒子が、1種又は複数の熱硬化樹脂と少なくとも1種の硬化剤を含む熱硬化性樹脂組成物を形成し、熱硬化樹脂の硬化剤に対するモル比が、100%の全てのエポキシ樹脂と反応するのに必要なアミンの量に不足であるか又は過剰であるような比であり、熱硬化性樹脂組成物を硬化して化学的に反応性のある官能基を有する硬化樹脂を形成して、硬化樹脂を粉砕することにより形成され、並びに
(i)での硬化中に、熱硬化粒子の化学活性官能基は、粒子を取り囲むマトリックス樹脂と共有結合を形成する
方法。
A method of manufacturing a fiber reinforced polymer composite structure comprising:
(a) forming thermoset particles having chemically active functional groups on the surface of the particles;
(b) forming a resin film from the first curable resin composition that does not contain the thermoset particles;
(c) forming a resin film from a second curable resin composition comprising one or more thermoset resins, at least one curing agent, and said thermoset particles;
(d) impregnating a layer of reinforcing fibers with at least one resin film formed from the first curable resin composition using heat and pressure, thereby forming a layer of resin-impregnated reinforcing fibers;
(e) contacting one surface of the layer of resin-impregnated reinforcing fibers with at least one resin film formed from a second curable resin composition, thereby forming a particle-containing prepreg ply;
(f) forming additional particle-containing prepreg plies according to steps (d) and (e);
(g) laying up the prepreg plies in a stacked arrangement thereby forming a prepreg layup;
(h) consolidating the prepreg layup; and (i) curing the prepreg layup;
with
The thermoset particles in (a) form a thermoset composition comprising one or more thermoset resins and at least one curing agent, wherein the molar ratio of thermoset resin to curing agent is 100%. A ratio that is inadequate or in excess of the amount of amine required to react with all of the epoxy resins and has functional groups that are chemically reactive to cure the thermosetting resin composition. A method formed by forming a cured resin and pulverizing the cured resin, and during curing in (i) the chemically active functional groups of the thermoset particles form covalent bonds with the matrix resin surrounding the particles.
JP2020524608A 2017-11-08 2018-11-07 A method for producing a composite having interlayer strengthening particles and the composite thereof. Pending JP2021502272A (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201762583212P 2017-11-08 2017-11-08
US62/583,212 2017-11-08
PCT/US2018/059640 WO2019203893A2 (en) 2017-11-08 2018-11-07 Composites with interlaminar toughening particles and method of making the same

Publications (2)

Publication Number Publication Date
JP2021502272A JP2021502272A (en) 2021-01-28
JPWO2019203893A5 true JPWO2019203893A5 (en) 2023-02-16

Family

ID=66326625

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2020524608A Pending JP2021502272A (en) 2017-11-08 2018-11-07 A method for producing a composite having interlayer strengthening particles and the composite thereof.

Country Status (9)

Country Link
US (1) US11167502B2 (en)
EP (1) EP3707208A2 (en)
JP (1) JP2021502272A (en)
KR (1) KR20200079313A (en)
CN (1) CN111566164A (en)
AU (1) AU2018419535A1 (en)
BR (1) BR112020008922A2 (en)
CA (1) CA3081351A1 (en)
WO (1) WO2019203893A2 (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111556807B (en) * 2017-12-22 2023-09-08 布鲁尔科技公司 Laser releasable bonding material for 3D IC applications
US11105038B2 (en) * 2018-12-20 2021-08-31 Palo Alto Research Center Incorporated Fiber reinforced plastic enhanced by functionalized particle
WO2021095627A1 (en) * 2019-11-15 2021-05-20 東レ株式会社 Epoxy resin composition, prepreg, and fiber-reinforced composite material
EP4059977A4 (en) * 2019-11-15 2023-11-29 Toray Industries, Inc. Epoxy resin composition, prepreg, and fiber-reinforced composite material
US11376812B2 (en) 2020-02-11 2022-07-05 Helicoid Industries Inc. Shock and impact resistant structures
KR20220001228A (en) 2020-06-29 2022-01-05 주식회사 엘지에너지솔루션 Battery Module Having Barrier and Insulation Layer For Fire Suppression
KR102461792B1 (en) * 2020-12-15 2022-11-02 주식회사 이지컴퍼지트 Tow prepreg having high impact strength for the filament winding
US11852297B2 (en) 2021-06-01 2023-12-26 Helicoid Industries Inc. Containers and methods for protecting pressure vessels
US11346499B1 (en) 2021-06-01 2022-05-31 Helicoid Industries Inc. Containers and methods for protecting pressure vessels
CN114015095B (en) * 2021-11-25 2024-01-16 中国人民解放军国防科技大学 Continuous fiber reinforced epoxy resin prepreg with surface layer rich in metal particles and preparation method thereof
US11952103B2 (en) 2022-06-27 2024-04-09 Helicoid Industries Inc. High impact-resistant, reinforced fiber for leading edge protection of aerodynamic structures

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3789054T2 (en) * 1986-12-25 1994-07-07 Toray Industries Tough composite materials.
JPH0694515B2 (en) * 1986-12-25 1994-11-24 東レ株式会社 Prepreg
EP0820858B1 (en) * 1996-07-22 2000-11-02 Hexcel Corporation Honeycomb core materials with particulate reinforcement
TW467940B (en) * 1997-10-14 2001-12-11 Toray Industries Thermosetting resin composition for carbon-fiber reinforced composite material
WO2010046770A1 (en) * 2008-10-24 2010-04-29 Iq Tec Switzerland Gmbh Apparatus and method for making reactive polymer pre-pregs
US8846818B2 (en) 2009-05-29 2014-09-30 Cytec Technology Corp. Engineered cross-linked thermoplastic particles for interlaminar toughening
US9567426B2 (en) 2009-05-29 2017-02-14 Cytec Technology Corp. Engineered crosslinked thermoplastic particles for interlaminar toughening
EP2607411A1 (en) * 2011-12-22 2013-06-26 Hexcel Composites Ltd. Improvements in or relating to fibre reinforced materials
JP2013173812A (en) * 2012-02-23 2013-09-05 Toray Ind Inc Prepreg and carbon fiber-reinforced composite material
WO2015011549A1 (en) * 2013-07-24 2015-01-29 Toray Industries, Inc. Fiber reinforced polymer composition with interlaminar hybridized tougheners
JP6291223B2 (en) * 2013-11-19 2018-03-14 Jxtgエネルギー株式会社 Method for producing fiber-reinforced composite material, prepreg, particle-containing resin composition, and fiber-reinforced composite material
GB201322093D0 (en) * 2013-12-13 2014-01-29 Cytec Ind Inc Compositive materials with electrically conductive and delamination resistant properties
US9868833B2 (en) * 2013-12-24 2018-01-16 Hexcel Composites, Limited Improvements to matrix additives
US11292946B2 (en) * 2014-05-22 2022-04-05 Cytec Industries Inc. Functionalized polymer particles for use as toughening agent

Similar Documents

Publication Publication Date Title
US20230365765A1 (en) Articles and Methods for Manufacture of Nanostructure Reinforced Composites
CN104070709B (en) Composite construction
RU2015129475A (en) PARTICLE RIGIDITY INCREASE TO INCREASE DESTRUCTION VISCOSITY
JP2004510842A (en) Sheet (SMC) molding compound with vented structure for trapped gas
JPWO2019203893A5 (en)
CN108472920A (en) For composite part can release surface material
MX2015006612A (en) Bonding of composite materials.
JP2006501085A (en) Manufacturing method of composite material
US20040142143A1 (en) Moulding materials
US20240173942A1 (en) Permeable materials capable of lightning strike protection and use thereof in resin infusion processing
WO2012149939A2 (en) Method of preparing a composite laminate
JP2019199062A5 (en)
KR20190127685A (en) Prepreg and Fiber Reinforced Composites
JP2022514416A (en) Automatic stacking of prepreg tapes for forming composite parts
CN206653702U (en) A kind of thermosetting laminate that can be repeatedly molded
US10046539B2 (en) Secondary reinforcement at interface of laminate structure
US9821530B2 (en) Composite laminate including interlayers with through-plane regions fused to fiber beds
US10717109B2 (en) Nanotube enhancement of interlaminar performance for a composite component
JP7466468B2 (en) Ultra-thin prepreg sheet and its composite material
JP6882402B2 (en) How to make a composite material
EP3508459A1 (en) Fiber reinforced materials with improved fatigue performance
JP7021216B2 (en) Fiber reinforced plastic with serrated edges
JP7552244B2 (en) Method for manufacturing fiber-reinforced resin molded product with hard coat layer
KR102184814B1 (en) Epoxy resin composition having improved adhesion and fiber-rubber composite connecting material using the same
JP2024070039A (en) Manufacturing method for panel structure made by composite material, and panel structure made by composite material